1 U.S. Department of Transportation
FEDERAL AVIATION ADMINISTRATION



## REGULATORY EVALUATION

QUALIFICATION, SERVICE AND USE OF CREWMEMBERS AND AIRCRAFT DISPATCHERS

FINAL RULEMAKING (14 CFR PART 121)

Office of Aviation Policy and Plans Regulatory Analysis Division

Volpe National Transportation System Center George Thurston

October 201 32 TABLE OF CONTENTS

I. INTRODUCTION

.................................................................................... ... 3

II

. BACKGROUND

........................................................................... . ......... ... 5

III . GENERAL BENEFIT

- COST ANALYSIS ASSUMPTIONS

........................ .... ... 10

IV . BENEFIT ANALYSIS

........................................................................... ... 1 1

V. COST ANALYSIS

........................................................................... ...... ... 3 5

VI . BENEFIT COST SUMMARY

............................................................... .. .. .. ..6 6

VII . APPENDICES

.................................................................. .. ......... . ... ... . .. .. 6 93 I. INTRODUCTION
In January 2009, the FAA published a n otice of p roposed r ulemaking (NPRM) for “Qualification, Service, a nd Use of Crewmembers a nd Aircraft Dispatchers”. Based on a public
meeti ng and comments, along with an increase in the NPRM scope, the FAA updated the NPRM
and the regulator y evaluation . We then published a supplemental notice of proposed rulemaking (SNP R M) in May 2011. After reviewing the changes proposed in the NPRM and the SNPRM, the agency has decided to move forward with a final rule that increases safety benefit by
includ ing certain provisions that enhance pilot training for rare, but high risk scenarios. This
focu s reduces the overall requirements as proposed in the NPRM and SNPRM.

The final rule adds safety

- critical tasks to pilot training such as recovery from stall and upset with an emphasis on manual handling skills. In addition, the final rule requires enhan ced runway safety training, training on pilot monitoring duties for the pilot not flying to be incorporated into existing requirements for scenario

- based flight training
, and requires air carriers to implement remedial training programs for pilots. The FA A expects these changes to contribute to a reduction in aviation accidents. Additionally, the final rule revises recordkeeping requirements for communications between the flightcrew and dispatch; ensures that personnel identified as flight attendants have completed flight attendant training and qualification requirements; provides civil enforcement authority against those making fraudulent statements; and, provides a number of conforming and technical changes to existing air carrier crewmember training and qualification requirements. The final rule also includes provisions that codify current processes that provide training efficiencies for certificate holders who operate multiple aircraft types with similar design and flight handling characteristics.

In developing the training and evaluation requirements, the FAA reviewed the current requirements in subparts A, M, N, O
, P, T, V and Y as well as the flight training tasks listed in Appendix E (flight training requirements), Appendix F (proficiency check requirements), and Appendix H (advanced simulation) of part 121.4 Table 1 shows t he FAA ’s estimate for the base case costs, including the low and high cost range
, in 2012 dollars . Table 1 also shows our estimated potential quantified safety benefits using a 22

- year historical accident analysis period

.

Table 1
Total Benefits and Costs ( 2012 $ Millions ) From 2019 to 20285 II . BACKGROUND
The regulations governing training and qualification requirements for crewmembers engaged in operations under p art 121 are found in 14 CFR part 121 subparts N and O 1

. Subpart N prescribes the requirements for establishing and maintaining a training program for
crewmember s , aircraft dispatchers, and other operations personnel and requirements for the use of training devices in conducting the program. Subpart O prescribes crewmember qualifications
related to the final rule . Appendix E to part 121 establishes the training tasks requir ed for initial, transition, and upgrade pilot flight training. Appendix F to part 121 establishes the tasks for pilot proficiency checks. Appendix H to part 121 provides guidelines and a means for using advanced airplane simulators for flight crew trainin g and checking.

This rule is necessary to address several National Transportation Safety Board (NTSB)
recommendations and addresses the requirements in the Airline Safety and Federal Aviation
Administration Extension Act of 2010 (the 2010 Act)

. 2 Under the 2010 Act, Congress directed the FAA to conduct rulemaking to ensure that all flightcrew members receive ground training and flight training in recognizing and avoiding stalls, recovering from stalls, and recognizing and avoiding upset of an aircraft, a s well as the proper techniques to recover from upset. The 2010 Act also directed the FAA to ensure air carriers develop remedial training programs for flight crew members who have demonstrated performance deficiencies or experienced failures in the
train ing environment.

The FAA reviewed the crewmember and aircraft dispatcher training regulations to identify improvements in training program content and application

. Although the agency’s review is ongoing, we have identified the following areas where ch anges were necessary to the current
rules :

• Fraud and falsification,

• Personnel identified as flight attendants,

1 Further references to part 121 operators include both part 121 and part 121/135 operators listed in the FAA National Vital Information Subsystem (NVIS) database

. 2 Public Law 111

- 216.6 • Proficiency checks for pilots in command (PIC)
,

• Related aircraft differences training,

• Training equipment other than Flight Simulation Training Device ( FSTD ) approved under part 60,

• Approval of FSTDs,

• Pilot monitoring,

• Remedial training
,

• Communication record for domestic and flag operations,

• Training for instructors and check airmen who serve in FSTDs,

• Extended envelope flight training maneuvers and procedures,

• Extended envelope ground training subjects,

• Runway safety maneuvers and procedures , and

• Crosswinds maneuvers with gusts

.

On May 20, 2011, the FAA published the Supplemental Notice of Proposed Rulemaking (SNPRM) . Following a fo ur month comment period ending on September 19, 2011
, t he FAA
received 134 comments on the SNPRM and regulator y evaluation. 3 These comments came from air carriers, trade associations, labor unions, the National Transportation Safety Board (NTSB),
the F ami lies of Continental Flight 3407, and many individual commenters. The FAA fully
considered these comments in developing the final rule and regulatory evaluation.

One of the commenters ’ major concern s was the proposal would cause additional training , and

t herefore costs, to operators who train their pilots under the Advanced Qualification Program (AQP)

. Based upon further review of the final rule requirements and AQP curriculums, the FAA has concluded that the final rule contains training tasks that are no t currently included in existing pilot AQP s . Therefore, the final rule will increase the training costs for all pilots who operate in part 121 service, including those who train under an AQP

.

3 http://www.regulations.gov/#!docketDetail;dct=PS+O+SR+FR;rpp=10;so=ASC;sb=postedDate;po=280;D=FAA

2008

- 0677 . Accessed March 22, 2013.7 Based on public comments and further agency review of the proposal
, the FAA made the following changes to the regulatory evaluation for the final rule:

• Re

- estimated costs and benefits to correspond directly to the provisions of this final rule.
The final rule focuses on safety

- critical enhancements to pilot trai ning for rare, but high

risk scenarios.

• Assumed that the final rule will affect all AQP and non

- AQP trained pilo ts in command, second in command pilots , check pilots, and flight instructor s by adding simulator and ground school time to their current training curriculum.

• Accounted for paperwork costs documenting the required revisions to part 121 operators pilot training programs.

• Updated the value of averted fatalit ies , injur ies, accident investigation and medical costs based on current U.S. Department of Transportation (DOT) guidance. 4

• Updated the hourly wages and benefits for aircraft crew member s with current hourly wages from the Bureau of Labor Statistics (BLS)

.

• Removed airfare, hotel, and per diem travel costs from the cost estimates because the FAA believes operators will be able to complete the new final rule training requirements
within their current initial, upgrade, transition, or recurrent simulator and gro und school training days. The FAA conducted a sensitivity analysis on the costs of the final rule adding an additional day of travel. The result s of the sensitivity analysis are shown in Appendix 10. Even with the cost of an extra day of travel, the ben efits of the final rule
still exceed the costs.

• Conducted a new accident analysis that took into account the mitigations of other final rulemakings for the same accidents in determining the probability of effectiveness for th is
final rule.

• A ssume s that t he “Flight Simulation Training Devices Qualification Standards For Extended Envelope and Adverse Weather Event Training Tasks” rulemaking (RIN 2120

- AK08) rulemaking is in place by the time compliance is required with the new pilot training requirements bec ause amendments to FSTD qualification and evaluation

4 “Revised Departmental Guidance 2013: Treatment of the Valu e of Preventing Fatalities and Injuries in Preparing Economic Analysis.” a vailable at http://www.dot.gov/regulations/economic

- values

- used

- in

- analysis8 standards in part 60 are needed to support the new full flight simulator training requirements in this final rule. In addition, the agency recognizes that the final rule on Pilot Certification and Quali fication Requirements for Air Carrier Operations will be in place at the time that compliance is required with the pilot training requirements in this
final rule.

• Included a table in Appendix 13 comparing the probability of effectiveness rating s of the

o verlapping accidents from the Flightcrew Member Duty and Rest Requirements final rule, the Pilot Certification and Qualification Requirements final rule and this final rule.

• Updated employment growth rates for pilots based on current FAA forecasts and actu al February 2013 employment statistics for part 121 operator s

.

• Updated the hourly simulator costs from the $550 estimate used in the SNPRM to $500 for the final rule based on updated FAA Flight Standards Service (AFS) data. This revised cost maintains consistency with analysis from the “ Pilot Certification and Qualification Requirements for Air Carrier Operations ” final rule published on July 15, 2013 (78 FR 42324)

.

• C onducted a sensitivity analysis on the hourly simu lator rental rate using the $550 rate
from the SNPRM. We estimated $323.1 million for the total costs using the $550 hourly

rate

. The total benefits
, as shown in Table 22
, exceed the costs for the $550 hourly
simulator rental rate

.

• I nitiated the “ Flight Simulation Training Device Qualification Standards for Extended Envelope and Adverse Weather Event Training Tasks ” rulemaking to amend 14 CFR Part
60 to require the additional programming and upgrades to simulators
, which will be
needed to comply with extended envelope training required by the final rule

. T he FAA
estimates that the $500 hourly simulator rental rate assum ed in this analysis includes all upgrades expected to be required by th e Flight Simulation Training Device rulemaking

. As an alternat ive, we also conducted a sensitivity analysis using $600 for an hourly
simulator rental rate. We estimated $332.4 million for the total costs with the $600 hourly rate. The total benefits as shown in Table 22 also exceed the costs for $ 60 0 hourly
simulat or rental rate

.

• Conducted a sensitivity analysis to explore the effect of reducing the historical analysis period from the 22 year period to 10 years in response to comments disputing the use of a9 22

- year time frame for accidents. Appendix 14 shows that u sing the 10

- year period, the
estimated benefits of this final rule increase by approximately 17 percent.

• Changed the pilot ground school distance learning 5 percentage from the 80 percent estimate used in the SNPRM to 100 percent, because the FAA allows 100 percent of non

hands on pilot ground training to be accomplished via distance learning. 6 Therefore, the
FAA assumes that 100% of the non

- hands on pilot g round training required by the final
rule can be done via distance learning.

5 D istance learning allows pilots to train out of the classroom (such as at home ). 6 FAA Order 8900.1, Vol.3, Ch. 19, Sec. 5, Para. 3

- 120 9 ( July 15, 2013 ). The FAA notes pilot ground school training requirements include hands

- on emergency equipment training (current §121.417(c) re quires that every 24 months, pilots must perform hands

- on drills on aircraft emergency equipment) that may not be accomplished via distance learning

. The costs for those hands

- on drills are not included in this cost analysis because th ey are currently req uired.10 III . GENERAL BENEFIT

- COST ANALYSIS ASSUMPTI O NS

This section details the derivation of the FAA’s estimation of the benefits and costs. First, we discuss general assumptions u sed in our estimation of the benefits and costs. Then we explain
the estimation of the quantified benefits and discuss the qualitative benefits . Next, we discuss the estimation of the quantified costs. Lastly, we summarize the estimated benefits and cos ts for
th e final rule

.

The benefit and cost analysis for th e regulatory evaluation is based on the following factors/assumptions :

• The analysis is conducted in constant dollars with 2012 as the base year.

• The estimates of costs and benefits reported in this evaluation include both 2012 dollar
values and present values. Benefits and costs are calculated in present values using both 3 percent and 7 percent discount rate s as prescribed by OMB in Circular A

- 4.

• This final rule will be published in late 2013

.

• This final rule w ill become effective in 2014, 120 days after its publication . C ompliance is required on the effective date (120 days) for a few of the provisions , including f or example all technical amendments, §§ 121.9 (falsification)
, 121.392 (id entification of personnel as flight attendants), and 121.711 (communication records). Compliance with the provisions related to training is required within 5 years after the effective date. We note, however, that individual air carriers may submit proposed training program revisions for approval at any point after the effective date. The agency will work with each air carrier to meet their implementation needs.

• Although some incidental cos ts are expected to occur prior to 2019, t he primary analysis period for costs and benefits extends for 1 0 years , from 2019 through 2028. This period was
selected because annual costs and benefits will have reached a steady state by 2019.11 IV. BENEFIT ANALYSIS

The FAA c ontracted Volpe National Transportation System Center to assist the FAA with the
estimation of the final rule’s benefits and the forecast of future accidents, fatalities and injuries

. The FAA estimates of the phased

- in benefits of this final rule over the analysis interval are shown in Table 1

. The se benefits are anticipated to result from the additional operational and training require ments of the final rule. The FAA estimates that these requirements will reduce the probability of aviation accidents . R educing the probability of their recurrence generates benefits in the form of reductions in the expected fatalities, injuries, and other costs resulting from such accidents. The regulations will enhance traditional pilot training programs by requiring training in areas that NTSB and FAA have identified as critical to preventing the recurrence of certain types of accidents.

Benefit Assumptions

In addition to the general assumptions identified at the beg inning of this section, the FAA made the following specific assumptions to facilitate the benefit analysis for this regulatory evaluation:

• Safety benefits will be realized beginning in 2019, when compliance is required with the

new training provisions in t he final rule.

• Past accident history from 1988 to 2009 (22 years) is an appropriate basis on which to
forecast the likely future occurrence of the types of accidents that the training and other provisions of this rule will help to prevent. The Accident P opulation and Scoring section provides the reasons for a 22

- year benefit period

.

Accident Population and Scoring

The FAA expects that the major benefit of th e final rule will be to prevent or reduce the probability of certain types of aircraft accidents in the future

. For the benefits analysis, the FAA analyzed the causal factors, as determined by the NTSB, for past accidents that occurred in part 121 operations. The objective of the analysis was to determine if an accident could have been prevented or mitigated by the training provisions in the final ru le. In 1988, Delta flight 1141 crashed shortly after lifting off from the runway at the Dallas

- Fort Worth Inte rnational Airport12 (DCA88MA072). In its final report, the NTSB determined that one causal fac tor for the accident was “The captain and first officer’s inadequate cockpit discipline which resulted in the flightcrew’s attempt to take off without wing flaps and slats properly configured.”

As a result of the accident investigation, the NTSB made rec ommendations to the FAA that emphasized the importance of training and manual procedures regarding “the roles of each flight crewmember in visually confirming the accomplishment of all operating checklist items,” as well as the “verification of flap positi on during stall recognition and recovery procedures.”

The FAA determined that the pilot monitoring training and operational provisions may have prevented or mitigated this accident. The pilot monitoring training will provide pilots an opportunity to practice monitoring skills in an environment that closely simulates real line operations. The operational requirements will require flightcrew members to follow air carrier procedures reg arding pilot monitoring. Together, these provisions establish an active requirement for the pilot not flying the aircraft to remain engaged throughout the flight by monitoring the pilot flying, as well as the position of the aircraft, the flight instrumen ts, the configuration of the aircraft, etc. The provisions will ensure that the pilot monitoring is prepared to notify the pilot flying of any anomalies or to assume the flying responsibilities if necessary. If these requirements had been in place at the time of this accident, the pilot monitoring may have identified the incorrect configuration and notified the pilot flying prior to takeoff.

Therefore, the FAA initiated the historical accident interval for the benefits analysis with this
accident in 1988. The FAA concluded the accident interval in 2009 with the Colgan accident because, at this time, the NTSB still has not finalized its reports on the major accidents (that may be pertinent to this training rule) that occurred in 2010 and 2011. This is why the FAA uses the same 22 year accident interval (1988

- 2009) for the benefits analysis in the final rule as in the
SNPRM.

The FAA identified 10 additional major accidents with casual factors identified by the NTSB that are addressed by the provisions in the final rule that occurred during this 22 year accident interval. The FAA cited these accidents in the benefits analysis b ased on pertinent accident13 causal factors, regardless of whether or not there were open NTSB recommendations associated
with those accidents.

In response to comments questioning the use of a 22

- year period, however, the FAA conducted a sensitivity analys is to explore the effect of reducing the historical analysis period from 22 years to 10 years. As indicated in Appendix 14, using the 10

- year historical accident analysis period increases the estimated benefits of the final rule by approximately 17 percent

.

T he analysis conducted for the Regulatory Evaluation accompanying the SNPRM identified 149 pilot

- related accidents during the 22 year historical analysis period covering 1988 to 2009 for which the proposed rule would reduce the probability of their recu rrence

. The FAA Accident Investigation and Prevention Group (AVP) and FAA’s Flight Standards Service (AFS) subsequently determined that the more limited set of regulatory changes in this final rule address the causal factors (as determined by the NTSB) inv olved in nine of those 149 historical pilot

related accidents. For further explanation regarding the limited set of regulatory changes, please see Section I of the final rule preamble, “Overview of Final Rule.”

For example, on February 12, 2009, a Colga n Air, Inc. Bombardier DHC

- 8

- 400, operating as Continental Connection flight 3407, was on an instrument approach to Buffalo

- Niagara International Airport, Buffalo, New York, when it crashed into a residence in Clarence Center, New York, about five nautical miles northeast of the airport resulting in the death of everyone aboard and one person on the ground. The NTSB determined that the probable cause of this
accident was the pilot in command’s (PIC) inappropriate response to the activation of the stick
sha ker, which led to an aerodynamic stall from which the airplane did not recover. The PIC’s response was inappropriate because he pulled back on the control column rather than pushing it forward to reduce the angle of attack. As a result, the airplane’s pit ch increased and its airspeed decreased, resulting in the stall. A contributing factor was both pilots’ failure to monitor airspeed via their primary flight display and thus their failure to recognize the impending stick shaker onset as airspeed fell and pitch increased. The NTSB noted that the “failure of both pilots to detect this situation was the result of a significant breakdown in their monitoring responsibilities and workload management.” The PIC’s poor response suggests he was surprised14 by activa tion of the stick shaker. Another contributing factor was the crew’s lack of professionalism in failing to follow FAA sterile cockpit rules below 10,000 feet. The PIC had 3,379 hours total flying time and the second in command ( SIC ) 2,244 hours. Had the f lightcrew been required to complete the extended envelope training provisions required by this final rule, this accident would likely have been mitigated.

Also, on September 8, 1994 a USAir (now US Airways) Boeing 737

- 300, flight 427, crashed
while maneu vering to land at Pittsburgh International Airport, Pittsburgh, Pennsylvania. Flight 427 was operating as a scheduled domestic passenger flight from Chicago

- O'Hare International Airport, Chicago, Illinois, to Pittsburgh. The flight crew did not report an y problems with the airplane and radar data indicates that the closest other traffic was about 4.5 miles and 1,500 feet vertically separated from flight 427 at the time of the accident. About 6 miles northwest of the destination airport, the airplane ente red an uncontrolled descent and crashed near Aliquippa, Pennsylvania. All 132 people on board were killed, and the airplane was destroyed by impact forces and fire. The NTSB determined that the probable cause of the accident was a loss of
control of the a irplane resulting from the movement of the rudder surface to its limit. The rudder surface most likely deflected to its limit in a direction opposite to that commanded by the pilots as a result of a failed main rudder power control unit (PCU). The FAA has determined that the provisions regarding upset prevention and recovery training in this final rule may have prevented or mitigated this accident.

In addition, given the changes adopted in the final rule and the impact the training provisions
will have o n air carriers who provide training under an Advanced Qualification Program, the FAA has determined that two additional accidents, American 587 and Continental 1404, involved contributing factors that are addressed by the final rule.

On November 12, 200 1 an American Airlines A300

- 600, flight 587, crashed in a residential area of Belle Harbor, New York. The airplane accident occurred shortly after takeoff from John F. Kennedy International Airport, Jamaica, New York. All 260 people aboard the airplane a nd 5 people on the ground were killed, and the airplane was destroyed by impact forces and a post

crash fire. The NTSB found the probable cause of this accident to be the in

- flight separation of15 the vertical stabilizer as a result of the loads beyond ulti mate design caused by the SIC ’s unnecessary and excessive rudder pedal inputs. The rudder input was a reaction to wake
turbulence. Characteristics of the Airbus A300

- 600 rudder system design and elements of the
American Airlines Advanced Aircraft Maneuvering Program also contributed to the incorrect rudder pedal inputs. The NTSB found that the American Airlines Advanced Aircraft Maneuvering Program excessive bank angle simulator exercise could have caused the SIC to have an unrealistic and exagger ated view of the effects of wake turbulence; erroneously associate wake turbulence encounters with the need for aggressive roll upset recovery techniques; and develop control strategies that would produce a much different, and potentially surprising and

co nfusing, response if performed during flight. The provisions adding upset prevention and recovery training in this final rule may have mitigated this accident because the training delivers recovery strategies which focus on primary control inputs and early intervention strategies

. 7 Further, the provisions that require pilots to complete upset prevention and recovery training in a full flight simulator (FFS) with an instructor who has been trained on the specific motion and data limitations of the FFS, woul d mitigate the possibility of delivering negative training in
simulation. 8

On December 20, 2008, a Continental Airlines Boeing 737

- 500, flight 1404, departed the left side of runway 34R during takeoff from Denver International Airport, Denver, Colorado. At the time of the accident, visual meteorological conditions prevailed, with strong and gusty winds out
of the west. The NTSB reported that, as the airplane crossed the uneven terrain before coming to a stop; the airplane became airborne, resulting in a jarring impact when it regained contact with the ground. A post

- crash fire ensued and the airplane was substantially damaged. The PIC and 5 of the 110 passengers were seriously injured; the SIC , 2 cabin crewmembers, and 38 passengers
sustained minor in juries. The NTSB accident report revealed that before starting the takeoff roll
the PIC verbally repeated the wind speed and direction; however, during the takeoff rol l the PIC inconsistently applied cross wind correction. The NTSB found that the probabl e cause of the

7 A l l pilots have receive d training on wake turbulence from the early stages of flight training . Since wake turbulence can lead to an upset condition , the enhanced training required in this rule will reinforce earlier training by teaching pilots appropriate upset prevention and recovery techniques. 8 Appendix 15 provides a sens itivity analysis to determine the impact of removing the catastrophic Amer ican 587 accident from the benefits analysis for the 10 and 22 year historical accident analysis intervals.16 accident was the PIC’s ceased rudder input, which was needed to maintain directional control of the airplane, about 4 seconds before the excursion, when the airplane encountered a strong and gusty crosswind that exceeded the PIC’s training a nd experience. The FAA has determined that the expansion of existing requirements for training on crosswind maneuvers to include wind gusts in this final rule may have prevented or mitigated this accident.

American 587 and Continental 1404 were exclude d from the benefits estimates reported in the SNPRM because the SNPRM analysis assumed that the proposed rule would have no impact on the safety of flights operated by pilots trained using an Advanced Qualification Program ( AQP )

.

Following further review of existing AQP curriculums and the pilot training requirements
retained for the final rule , the agency has determined that the majority of the rule’s new pilot training maneuvers and procedures are not incorporated into existing AQPs used to train pilots ; therefore
, it is appropriate to include those two additional accidents in this analysis. For these 11 accidents, the NTSB investigations identified several specific areas of inadequate training that were either the probable cause or a contributing factor for many of these accidents. Of the 11 pilot

- related accidents, nine accidents involved one or more fatalities and two had no fatalities.

To determine the likely probability of effectiveness of the final rule in preventing the recurrence
of accidents si milar to the 11 accidents identified in the historic period, AVP undertook a multiple

- step process. The FAA recognizes that there are multiple rulemakings occurring in parallel with this final rule and there is some degree of overlap among them regarding t he
historical accidents used to estimate benefits. 9 Therefore, to account for the relationship of these new rules, AVP first rated the effectiveness of the entire suite of these rules in reducing the probability of the future recurrence of these accidents , using the scoring process of the Commercial Aviation Safety Team (CAST). 10 AVP used the NTSB recommendations along

9 Specifically, these parallel rulemakings are: Flightcrew Member Duty and Rest Rule (FDR); Pilot Certification and Qualification Requirements for A ir Carrier Operations Rule (FOQ); Flight Simulation Training Device Qualification Standards for Extended Envelope and Adverse Weather Event Training ( part 60) and Safety Management Systems for part 121 Certificate Holders (SMS). 10 The FAA evaluated these historical accidents in the context of the other rulemakings such that the sum of the probabilities for each accident across all these rules will not exceed one. Appendix 13 details the overlap of the probability for each accident in the parallel rules th at are published as a final rule.17 with its narrative descriptions, probable cause findings, identification of contributing factors, and other pertinent data to assign scores reflecting the likelihood that the collection of these rules could have prevented each accident in the final rule analysis interval.

AVP developed these scores using a Joint Implementation Monitoring Data Analysis Team (JIMDAT)

- like method because many of the issues surrounding these accidents are not clearly defined in the probable cause or contributing factors statements of the NTSB reports. The
JIMDAT

- like score, as applied to a specific historical accident, is based upon the likelihood that
the train ing, operational, and other changes these rules collectively require would have prevented the occurrence of that accident if they had been in place at the time it occurred. AVP used a sliding percentage scale of zero to 0.9 to describe the score assigned to each accident.

The second step of the process was to allocate the overall probability of effectiveness for the suite of new rules to each individual rule, so that the safety

- related benefits of each individual
rule

– which arise from the projected effectiveness of that specific rule in reducing the probability of future accidents

– could be estimated. AVP used the same zero to 0.9 sliding scale noted above to arrive at the final effectiveness ratings. In some cases , this effort to allocate the composite probability of effectiveness among individual rules is complicated by the ir
interrelatedness

. For instance, this final rule requires additional simulator training for pilots, while the upcoming p art 60 rule making wo uld establish the requirement s that simulator s be capable of providing the enhanced training capabilities required under this final rule. In that case
, the combined probability of effectiveness of the se two rule s was allocated roughly evenly
between this f inal rule and the p art 60 rule making

.

Table 2 shows probability of effectiveness for th is final rule for the 11 historical accidents that
were used as the basis for estimatin g its benefits
, and also reports important summary information regarding these accidents. Appendix 1 and Appendix 2 provide additional details of
the historical accidents

.18 Table 2 Selected Characteristics of 11 Historic Accidents (1988

- 2009)

Quantification of Safet y Benefits

This section describes the methodology the FAA used to quantify the safety benefits for the final rule. Appendix 3 identifies the specific provisions of this final rule that respond to the probable causes and contributing factors that the NTSB identified for each historic accident. Because many accidents were the result of multiple contributing factors, and the provisions of this final rule were developed to respond to these contributing factors, there are several cases where the
rule’s probabil ity of effectiveness for an historical accident is the result of the expected impacts of multiple provisions of the rule. For that reason, the FAA has not attempted to develop separate benefit estimates for each individual provision of this rule, and our q uantitative estimates of the rule’s benefits will be derived only for all of its provisions taken together. In addition, there are other provisions of the rule for which anticipated benefits can be described only in qualitative terms; these provisions will be discussed separately in a later section of this document.

The following provisions of the final rule are expected to have quantifiable safety benefits:

• Pilot monitoring (§§ 121.544, 121.409, Appendix H),

• Remedial training (§§ 121.415(h) and § 121.415 (i)),

• Extended envelope flight training maneuvers and procedures (§§ 121.423, 121.407(e), 121.424, 121.427(d)(1)(i), 121.433(e), Appendix E),

• Extended envelope ground training subjects (§§ 121.419(a)(2) and 121.427),

• Runway safety maneuvers and procedures (Appendices E and F), and19 • Crosswind maneuvers including wind gusts (Appendices E and F).

The benefits of avoiding the recurrence of an accident potentially include avoided fatalities, injuries, aircraft replacement or repair, loss of cargo for cargo plane accidents, property damage on the ground, and accident investigation costs. 11

In estimating the value of an averted future accident, we take the characteristics of the historic accidents as a starting point. No future accident is expected to have exactly the same causes or consequences as the historical accidents included in this analysis. Rather, this analysis uses these historical accidents to indicate the prevalence of accidents due to insufficient training in the past,
and uses this information as an indication of how frequently these same types of accidents might
occur in the future in the absence of this final rule.

The accident history is also used to inform our estimates of the likely severity of these types of potential future accidents, which is measured by the percent of passengers aboard the aircraft that were injured (fatal, serious, minor), the extent of physical damage to the aircraft involved, and the extent of any physical damage on the ground. This analysis then applies forward

- looking estimates of the value of preventing the recurrence of accidents of that same severity. For instance, the projected value of avoiding a hull loss during the future analysis period is not the
actual economic value of the aircraft hull that was lost in an hi storical accident, but is instead the estimated value of an aircraft that would be likely to be in use in the future.

In estimating benefit values for avoided fatalities and injuries, the FAA follows the Department of Transportation’s (DOT) recently

- issue d document “Revised Departmental Guidance 2013: Treatment of the Value of Preventing Fatalities and Injuries in Preparing Economic Analysis.” 12 That document estimates the value for preventing a fatality at $9.1 million (in 2012 dollars), while preventing a serious injury is valued at $1,264,900 (assumed to be the average of economic costs for severe, serious, and moderate injuries), and preventing a minor injury is

11 Avoided emergency response and environmental clean

- up costs might be included as other categories of benefits but at this time FAA does not have access to estimates of these cost categories. The FAA believes the magnitud e of the benefit categories to be relatively small in comparison to the other categories of benefits analyzed here. 12 Available at http://www.dot.gov/regulations/economic

- value s

- used

- in

- analysis20 estimated to have an economic value of $27,300. As recommended in the recent DOT guidance
doc ument identified above, these values are then escalated at 1.07 percent per year to reflect the effect of growth in real income levels on the value that society collectively places on avoiding accidental fatalities and injuries. See Appendix 4 for more det ails.

In estimating the number of fatalities and injuries avoided by preventing the occurrence of future accidents, we calculate the number of fatalities and serious and minor injuries as percentages of the number of people on board the aircraft involved in each historic accident. Table 3 shows this information for each historical accident. We then apply those percentages to the expected passenger count on a typical future flight. The average number of passengers per flight for part 121 passenger operation s during 2012 was 84 persons, and the average seating capacity of the aircraft they operated was 106 seats. 13 After allowing for three flight attendants (one for every 50 seats) and two flightcrew members, this procedure assumes there would have been 89 peo ple aboard a typical flight during 2012. For the single cargo plane accident (FedEx Flight 647) , this analysis includes the benefits of avoiding the two minor injuries that occurred in the actual historical accident. Any additional fatalities or injuries o n the ground that occurred in a historical accident are also included in the estimates, without adjustment.

13 Bureau of Transportation Statistics, Air Carrier Statistics, T

- 100 Segment Data (U.S. Carriers) for Jan

– Oct 2012. The listing of part 121 carriers can be found in Appendix 8.21 Table 3 Fatalities and Injuries as Percentages of People Onboard

* Details may not add to row or column totals due to rounding. Table 4 shows the forecasted number of fatalities and injuries that would be expected to result if an accident of the same severity as the historical accident recurred in 2012, and involved the typical airplane carrying 89 people. The 11 historical accidents resulted in a total of 601 fatalities, 48 serious injuries, and 137 minor injuries. In contrast, the method described above results in estimates of 44 fewer fatalities, 16 additional serious injuries, and 1 6 additional minor injuries from an identical number of simil arly severe potential future accidents. This discrepancy results because although the average number of people on board the aircraft involved in the historical accidents (90) is in line with the average future passenger load projected for this analysis (89 ), two of the historical accidents (American 587 and USAir 427) occurred on larger than average aircraft and were catastrophic. This means that the actual accident history shows higher fatalities than we assume would occur in the future without the final r ule. The decision to use expected future values for aircraft size and passenger counts is made because the FAA believes that the risk of a catastrophic accident is not specific to a certain size of aircraft. All FAA regulations require the same level of pi lot training and qualifications for all part 121 operations, regardless of the size of aircraft they typically operate, so that improving pilot training is expected to uniformly reduce the probability that aircraft of all sizes will be involved
in future a ccidents. Carrier Flt# Fatalities Serious Injuries Minor Injuries Total People Onboard Colgan 3407 100% 0% 0% 49 American 587 100% 0% 0% 260 American Eagle 4184 100% 0% 0% 68 USAir 427 100% 0% 0% 132 COMAIR 5191 98% 2% 0% 50 Northwest 1482 18% 23% 59% 44 Continental 1404 0% 5% 36% 115 FedEx 647 0% 0% 29% 7 Delta 1141 13% 24% 46% 108 Corporate 5966 87% 13% 0% 15 USAir 5050 3% 5% 29% 63 Total 65% 5% 15% 911 Onboard22 Our estimate of future benefit s incorporates information related to the rule’s expected impacts on the aviation system looking forward in order to appropriately value the reduction in future risks. However, as a test of the sensitivity of our benefits estimates using this approach, we also include an analysis assuming that the exact number of fatalities and injuries as actually occurred in each historical accident would occur in a potential future ac cident. The details and results of those calculations are in Appendix 5.

Table 4 Forecasted Fatalities and Injuries for Accidents

Table 5 below shows the estimated benefits from preventing the forecasted fatalities and injuries associated with the pot ential future recurrence of each of the 11 historical accidents. These estimated benefits have not yet been adjusted for the projected probability of effectiveness of the rule in preventing the recurrence of similar accidents in the future. Those adjustme nts are made in a later section. In addition, the benefits are projected to grow throughout the future analysis period, in order to account for projected growth in the airline industry.23 Table 5 Valuation of Forecasted Fatalities and Injuries for Accident s (2012 $)

An additional benefit from preventing future accidents is avoiding damage to the aircraft itself. Again, we take the approach of estimating benefits based on the replacement value of a “typical” aircraft expected to be in the future fleet. As indicated previously, the average seating capacity per passenger flight operating under part 121 in 2012 was 106 seats. 14 The FAA forecasts that seats per flight will grow by approximately 0.5 percent annually over the analysis period, which implies that th e average seating capacity of part 121 passenger aircraft is expected to average 112 by 2023, the midpoint of the benefits analysis period. 15 With a capacity of 117 seats, the Boeing B717

- 200 is the aircraft model in the current US fleet which is the closes t in size to average forecast size of 112 seats. 16 We therefore estimate the value of a passenger aircraft of average size, and of average age to be $10.5 million based on the current market value of a nine year old Boeing B717

- 200. We estimate the value o f a “typical” cargo aircraft to be $27.7 million, based on the market values of average

- aged Boeing B757

- 200, Airbus A300

- 600, and McDonnell Douglas MD

- 11, the most frequently used cargo airplanes used in part 121 operations. 17 Appendix 6 reports the detail s of these estimates.

In all eleven historical accidents used as the basis for this benefit analysis, the primary aircraft was destroyed. In one case (Northwest 1482 on December 3, 1990), a second aircraft was

14 Bureau of Transportation Statistics, Air Carrier Statis tics, T

- 100 Segment Data (U.S. Carriers) for Jan

– Oct 2012. 15 See Appendix 6, Table 1 for sources and methods. 16 Bureau of Transportation Statistics, Form 41, Schedule B

- 43, 2011. 17 Bureau of Transportation Statistics, Air Carrier Statistics, T

- 100 Segment Data (U.S. Carriers) for Jan

– Oct 2012

.24 involved and also sustained substantial damage, but was later repaired and placed back in service. For that accident, the damage to the second aircraft was valued at 13 percent of the average replacement value. 18

In the case of the single cargo plane accident used in the benefits analysis (Fed Ex Flight 647)
, preventing the destruction of the cargo and the resulting loss of its value is an additional benefit category. While the FAA is unaware of published estimates for the value of air cargo, we derived the average value per ton of air cargo by assessing the commodity flow value and commodity flow weight of goods transported by air using the U.S. Department of Transportation’s 2007 Freight Analysis Framework (FAF) Survey. 19 Because both weight and value of commodities typically shipped by air vary by shipment origin and destination, the average value of all shipments by air was used. An average cargo value per ton of $89 thousand (in 2012 dollars) was calculated by dividing the average value of commodities shipped by air over all origins and
destin ations by the corresponding average weight of an air freight shipment, and then adjusted to 2012 dollars using the change in the Gross Domestic Product deflator. The average amount of freight on a part 121 cargo

- only aircraft operation is approximately 25 tons. 20 Thus the value of the complete loss of the aircraft’s cargo on a typical flight is estimated to be $2.225 million in
2012 dollars.

In nine of the historical accidents, property damage on the ground was minimal because the
aircraft accident occurre d on or near the airport runway, in an undeveloped area such as a field,
or in the water. 21 However, the Colgan 3407 accident (February 12, 2009) destroyed one home on the ground, while the American 587 accident (November 12, 2001) destroyed four homes,

sev erely or substantially damaged four other homes and one boat (parked in a driveway), and also resulted in minor damage to a retail gasoline station and three additional homes. To estimate

18 “ Economic Values for FAA Investment and Regulatory Decisions, A Guide,” Oct. 3, 2007 by GRA , Incorporated, Table 5

- 4. 19 Freight Analysis Framework 2007, a joint survey conducted by the Census Bureau and BTS and updated every 5 years. ( http://www.bts.gov/publications/commodity_flow_s urvey/2007/state_summaries/ ) 20 Bureau of Transportation Statistics, Air Carrier Statistics, T

- 100 Segment Data (U.S. Carriers) for Jan

- Oct 2012. 21 It is worth noting that where the accident actually occurs and subsequently how much damage occurs on the g round for any future possible accident that this final rule prevents cannot be known with any level of certainty. In the absence of data or forecasts on where these types of crashes are likely to occur, we use the information on the actual ground damage ex perienced in the historical accidents.25 the value of avoiding similar damage to ground property by preventin g the recurrence of such an accident, the FAA used the 2012 median home value of $175,400. 22 Roughly 25 percent of a typical home’s value is associated with the land and would not be destroyed by an accident, so the value for a destroyed house structure used in this analysis is $131,600 (75 percent of $175,400). 23 The economic benefit from prevent ing severe or substantial damage to homes is in turn valued at 75 percent of this average structure value ($98,700); preventing minor damage (of homes and gas station) is estimated to result in benefits equal to 25 percent of structure value ($32,900). For completeness, we have also included an estimate of the value of a pre

- owned recreational boat to be $14,600. 24

FAA estimates a value of $10.7 million for the accident investigation costs associated with a catastrophic accident, and $0.6 million for the a ccident investigation costs associated with a non

catastrophic accident. 25 These values are derived from estimates of costs to NTSB, FAA, and private parties associated with historical accident investigations, adjusted to 2012 dollars using
the GDP deflato r.

Table 6 below shows these benefit calculations for preventing damage or destruction of aircraft hull values (primary and secondary aircraft), cargo value, property damage, and accident investigation costs applied to the 11 historic accidents. Again, no te that these benefits estimates are not yet adjusted to reflect the rule’s probability of effectiveness in preventing similar future
accidents.

22 Average of monthly U.S. Existing Home Median Sales Price from National Association of Realtors accessed at http://ycharts.com/indicators/s ales_price_of_existing_homes on April 4, 2013. 23 Davis, Morris A. and Jonathan Heathcote, 2007, "The Price and Quantity of Residential Land in the United States," Journal of Monetary Economics, vol. 54 (8), p. 2595

- 2620; data located at Land and Property V alues in the U.S., Lincoln Institute of Land Policy http://www.lincolninst.edu/resources/ accessed on April 4, 2013. Estimate is based on average aggregate U.S. quarterly values for Q4 2011 through Q3 2 012 for both CWS and FHFA sources. 24 Average price of a pre

- owned powerboat (with engine) in 2010 was $14,039 according to "Recreation Boating Stakeholders Growth Summit Industry Overview 2011" accessed at http://consensus.fsu.edu/Boat

Summit/pdfs/Recreational%20Boating%20Growth%20Summit%20Industry%20Overview.pdf on April 4, 2013. This value has been adjusted to 2012 value using the G DP deflator. 25 The estimated accident investigation cost s are the estimated costs of “Major” and “Air Carrier Weighted Average” investigations from “ Economic Values for FAA Investment and Regulatory Decisions, A Guide,” Oct. 3, 2007 by GRA for the FAA, Tab le 8

- 2.26 Table 6 Additional Categories of Benefits from Preventing Historic Accident (2012 $)

The next steps in e stimating the benefits of the final rule are to adjust the estimated benefits from preventing each accident by the probability of effectiveness of this rule in preventing the recurrence of that specific accident, and then to project those annualized benefi t values forward through the future analysis period. Table 7 displays the probability of effectiveness for each accident, along with the adjusted fatality and injury

- related benefits estimates, and other categories of benefits derived using the forecasting methods discussed above. Each of the entries in the two columns containing these adjusted benefits estimates is equal to the entry in Table 5 (fatalities and injuries) or Table 6 (other benefit categories) corresponding to a specific historical accident, multiplied by the estimated probability of effectiveness of the rule in preventing that
accident shown in Table 7. The bottom two rows of Table 7 show the total estimated benefits of the rule if it had been in place during the full 22 years of the accident history, and the estimated average annual benefit of the rule. Carrier Flt# Primary Secondary Total Colgan 3407 $10,500,000 $131,600 $10,700,000 $21,331,600 American 587 $10,500,000 $1,067,400 $10,700,000 $22,267,400 American Eagle 4184 $10,500,000 $10,700,000 $21,200,000 USAir 427 $10,500,000 $10,700,000 $21,200,000 COMAIR 5191 $10,500,000 $10,700,000 $21,200,000 Northwest 1482 $10,500,000 $1,365,000 $600,000 $12,465,000 Continental 1404 $10,500,000 $600,000 $11,100,000 FedEx 647 $27,700,000 $2,225,000 $600,000 $30,525,000 Delta 1141 $10,500,000 $600,000 $11,100,000 Corporate 5966 $10,500,000 $10,700,000 $21,200,000 USAir 5050 $10,500,000 $600,000 $11,100,000 Total $132,700,000 $1,365,000 $1,199,000 $2,225,000 $67,200,000 $204,689,000 Accident Investigation Costs Hull Damage Property Damage on

Ground Cargo Value27 Table 7 Single Year Benefits of Final Rule (2012 $)

The US airline industry has grown over time, and the FAA forecasts that the airline industry will continue to grow throughout the fore cast period. This projected increase in traffic is accompanied by an increase in the risk of future accidents under the baseline scenario, where this rule would not be adopted. To incorporate the effect of forecasted growth on the number of
future accident s prevented by the rule and the resulting economic benefits, we apply the FAA forecast of 2.1 percent annual growth in passenger enplanements to the estimates of benefits from avoided fatalities and injuries. 26 This accounts for the effects of projected inc reases in both overall flight activity and the typical number of passengers aboard each flight on the reduction in future fatalities expected to result from adopting this rule. Table 8 below shows the resulting growth in the estimated number of annual fata lities and injuries avoided due to the final rule. 27 We apply the 1.6 percent anticipated annual growth in commercial aircraft operations to the estimates of the other categories of benefits (avoided property damage and accident investigation costs), as the se categories of benefits are more closely related to the number of flights rather than

26 FAA Aerospace Forecasts 2013

- 2033, Table 10, U.S. Mainline Air Carriers Schedules Passenger Traffic, Average Annual Growth Rate (2013

- 2033) for Revenue Passenger Enplanements (System). 27 Due to rounding, using the information in Table 8 to calc ulate the benefits from avoided fatalities and injuries will result in a slightly different total than is presented below. Carrier Flt# Effectiveness Rating Benefits from Avoided Fatalities and Injuries Other Benefits Colgan 3407 20% $163,800,000 $4,266,320 American 587 25% $213,850,000 $5,566,850 American Eagle 4184 20% $161,980,000 $4,240,000 USAir 427 20% $161,980,000 $4,240,000 COMAIR 5191 15% $119,135,370 $3,180,000 Northwest 1482 50% $86,202,450 $6,232,500 Continental 1404 25% $1,803,275 $2,775,000 FedEx 647 35% $19,110 $10,683,750 Delta 1141 35% $47,930,820 $3,885,000 Corporate 5966 5% $35,795,740 $1,060,000 USAir 5050 50% $16,527,050 $5,550,000 $1,009,023,815 $51,679,420

$45,864,719 $2,349,065 Total benefit over 22 year history Per year benefit28 the number of people on a flight. 28 The projected future growth rates in passenger enplanements and the number of flights differ because the industry is moving toward la rger aircraft with higher load factors; therefore an increase in passenger demand can be met with a less than proportionate increase in the number of flights.

Table 8 Forecasted Growth in Fatalities and Injuries Avoided Due to Final Rule (2012 $)

As indicated previously, the unit values for fatalities and injuries avoided are escalated at 1.07 percent per year to account for growth in real incomes, in accordance with DOT guidance. 29 In the absence of information on how unit values for the other categor ies of benefits (aircraft hull damage, property damage on the ground, etc.) are likely to change in real terms over the future, the 2012 estimates of unit values for each other category of benefits are used throughout the future analysis period. Table 9 sh ows the results of these forecasting assumptions for each year
of the 10

- year benefit period for this rule, which extends from 2019 through 2028. To summarize, the annual benefits from avoided fatalities and injuries from the last row of Table 9
are escala ted by two factors: 1.07 percent per year to account for real income growth, and 2.1

28 FAA Aerospace Forecasts 2013

- 2033, p. 62. 29 “Revised Departmental Guidance 2013: Treatment of the Value of Preventing Fatalities and Injuries in Preparing Economic Analysis” available at http://www.dot.gov/regulations/economic

- values

- used

- in

- analysis29 percent per year to reflect growth in passenger enplanements. The other categories of benefits from the last row of Table 9 are escalated at 1.6 percent per year, to accou nt for future growth in the number of flights and the associated increase in accident risk exposure. In addition, Table 9 displays the present value of the benefits over the future analysis period when discounted at both the seven percent and three percen t rates recommended in OMB Circular A

- 4.

Appendix 5 presents calculations that parallel this analysis, but instead use the actual fatalities and injuries resulting from each historical accident as the basis for an alternative estimate of the
rule’s benef its. The calculations in Appendix 5 use the same 2012 estimates of property damage and accident investigation estimates as the central analysis, but do not incorporate any forecasted growth in industry

- wide flight activity.

Table 9
Total Benefits of Final Rule (2012 $)

* Details may not add to row or column totals due to rounding.

The total estimated benefit of the final rule over the analysis period is $689.2 million in 2012 dollars. This stream of benefits has a present value of $317.1 million when di scounted at seven percent and $488.7 million when discounted at three percent.30 These benefits estimates differ from those presented as part of the SNPRM for several reasons. On one hand, certain changes in the benefits estimation methodology acted to low er the estimated benefits of the final rule. The final rule has fewer training requirements and other provisions than the previously

- proposed version of the rule analyzed in the SNPRM; this results in lower benefits, because fewer accidents are judged to b e prevented by the final rule. Further, the effectiveness ratings used in the SNPRM represented the impact of this rule when considered in isolation, while the probability of effectiveness used here take into account the reductions in accident risk expect ed to result from other contemporaneous rulemakings that FAA is undertaking. Thus for the most part, the probability of effectiveness ratings assigned to the accidents that could have been mitigated by this final rule are lower than those used in the
SNPRM

.

The probability of effectiveness for USAir 427, which had an effectiveness rating of zero in the SNPRM, is the exception. USAir 427 crashed while maneuvering to land at Pittsburgh International Airport, Pittsburgh, Pennsylvania. 30 As part of the analy sis for the final rule, AVP

re

- evaluated the accidents to be included as the basis for the benefits estimates for the final rule. In doing so, AVP determined that the upset recovery and prevention training provisions in the final rule, together with the en hancements to simulators from the new part 60 rulemaking, may have prevented or mitigated the accident in such a way that the revised 20 percent probability of effectiveness was appropriate. Further, two additional accidents, American 587 and Continental
1 404, were added to the list of accidents used to develop the benefits estimates for the final rule when it was determined that the final rule would indeed improve the safety of flights operated by pilots trained using AQP. Finally, there have also been mo difications to the unit values used to estimate the various benefit categories. The most significant change is that DOT guidance now specifies that benefit cost analyses use an estimate of $9.1 million for the value of preventing a fatality, whereas at the time of the SNPRM, the DOT guidance specified $6.0 million as the Value of Statistical Life ( VSL ) to use in benefit cost analyses.

30 Appendix 1 and Appendix 2 provide additional d etails of the historical accidents

.31 On net, the methodology changes that acted to increase the estimated benefits outweighed the methodology changes that acted to reduce estimated benefits. As a result, the projected benefits for this final rule are higher than those estimated and reported in the SNPRM.

Qualitative Benefit Discussion

This section discusse s the benefits of the remaining provisions of the final rule in qualitative

terms:

• Fraud and falsification(§ 121.9)
,

• Personnel identified as flight attendants (§ 121.392)
,

• Proficiency checks for PICs (§ 121.441(a)(1)(ii)),

• Related aircraft differences training (§§ 121.400, 121.418, 121.434, 121.439, 121.441)
,

• Training equipment other than FSTDs approved under part 60 (§§ 121.408, 121.403(b)(2))
,

• Approval of FSTDs (§ 121.407)
,

• Communication records for domestic and flag operations (§ 121.711) , and

• Training for instructors and check airmen who serve in FSTDs (§§ 121.413 and 121.414 ).

Fraud and falsification (§ 121.9)

Although fraud is currently prohibited by criminal statute, the FAA has added language prohibiting fraud and falsification to part 121 to emphasize the importance of truthful statements. This provision prohibits fraudulent or intentionally false statements in, or a known omission from, any record or report that is kept, made, or used to show compliance with this part, or to exercise any privileges under this chapter

. This provision enhance s FAA enforcement options by allowing the agency to take certificate action or assess a civil penalty against a person for making
a fraudulent or intentional false statement

. This provision may contribute to safety of the aviation system although it is not possible to quantify or value that improvement.

Personnel identified as flight attendants (§ 121.392)32 This provision prohibits operators from identifying any person as a flight attendant if that person
has not completed all flight attendant training and qualification. Individuals who have not completed all flight attendant tra i ning and qualification requirements must be clearly identified (e.g. via an announcement, by wearing civilian clothes, or not wearing a uniform). This provision may reduce confus ion of passengers during an emergency situation on a flight who might otherwise presume that these individuals are fully qualified flight attendants. However FAA does not have access to any information that would allow for quantifying the safety benefit

o f this provision.

Proficiency checks for PICs (§ 121.441(a)(1)(ii) )

Currently, in accordance with §§ 121.433(d) and 121.441(a)(1), a PIC who serves on more than one aircraft type must complete either recurrent flight training or a proficiency check on each aircraft type every 12 months. T he final rule amends § 121.441(a)( 1) to require PICs who fly more than one aircraft type to receive a proficiency ch eck in each aircraft type flown every 12
months

. This amendment ensures PICs operating multiple aircraft types maintain proficiency on each aircraft type flown . However , th e FAA does not have access to any information that would allow for quantifying the safety benefit s of this provision.

Related aircraft differences training (§§ 121.400, 121.418, 121.434, 121.439, 121.441)

This provision formalizes the current practice of allowing carriers and their pilots to take credit for training or qualification events on one type of aircraft
, and apply that same credit to other aircraft types that have similar flight handling characteristics. This type of training credit is

current ly allowed in practice for some aircraft types, most notably the Boeing 757 and Boeing
767. N ew advances in fly

- by

- wire technology allow aircraft manufacturers to design aircraft with different models and aerodynamic airframes that are operated in the same way. The ability to transfer credit for previous training and qualification on existing aircraft types to different but related aircraft types that have similar flight handling characteristics could offer a significant cost savings to carriers when they a dd new aircraft types to their fleets. In this scenario, they will not need to develop completely new training programs or completely retrain the pilots flying the new33 aircraft types. In addition, there are long term training and qualification efficiencies for pilots who are qualified on more than one related aircraft type
, in the form of recurrent simulator training and qualification, as well as recency of experience requirements , operating experience requirements, and consolidation . Lowering the training cost s for air carriers to adopt new aircraft types will speed up the entry of newer aircraft types into the fleet
, which will also bring about social benefits from the reduced noise, emissions, and fuel usage that the newer aircraft types provide.

Training equipment other than FSTDs approved under part 60 (§§ 121.408, 121.403(b)(2))

Current regulations do not provide specific requirements for training equipment other than FSTDs, but the regulations genera lly require training equipment t o be adequat e. Section 121.408
states that t he FAA must approve training equipment (e.g. cockpit procedures trainers, door/exit trainers, water survival equipment, etc

. ) used to functionally replicate aircraft equipment required to be used as part of the approved trai ning program. As such, this provision enables the safety benefits from the regulations governing training on equipment other than FSTDs. It is not feasible to separately estimate the benefits of this specific provision.

Approval of FSTDs (§ 121.407)

Thi s provision conforms the requirements for evaluation, qualification, and maintenance of
FSTDs used in p art 121 to existing p art 60 requirements, by providing a reference to part 60 in part 121 and adding a new paragraph consistent with the § 121.423 requir e ment t o use an FSTD for extended envelope training. This provision therefore provides clarification regarding p art 60 requir ements that currently apply to p art 121 training. Compliance with new paragraph (e) of this provision is required 5 years and 120 days after the date of publication of the final rule in the Federal Register because the new extended envelope training required by § 121.423 is not required until such time.

Communication records for domestic and flag operations (§ 121.711)34 This provi sion clarifies the information that must be included in the record of communications between the pilot and aircraft dispatcher based on a legal interpretation of the current requirement in § 121.711. This provision also clarifies the recordkeeping requirem ent by defining “en route” for purposes of this section and applies the requirement to all flightcrew/dispatch communications made using a two

- way communication system required in
accordance with § 121.99.

Training for instructors and check airmen who serve in FSTDs (§§ 121.413, 121.414)

These final rule provisions will add some additional check airman (simulator) and flight instructor (simulator) initial, transition and recurrent training curriculum items to current requirements in existing §§ 121.413 and 121.414 to ensure comprehensive check airman and flight instructor understanding of new training tasks in the final rule and the limitations of simulation. When the FAA introduced the extended envelope requirements, we felt it was important to train s imulator instructors how to train pilots for these events. Instructors need to
understand the simulator control and possess the knowledge to be able to handle these new training requirements. This provision enables the safety benefits from the FSTD traini ng program by ensuring that the check airmen and flight instructors can adequately operate the FSTDs to achieve positive training outcomes. It is not possible to separately quantify the benefits of this individual provision.35 V . C OST ANALYSIS

The final rule costs w ill accrue from additional training requirements
, a low and high range for
the use of simulator time, ground school training facilities , and paperwork

. Th os e individuals affected by the new requirements include crew members (pilots and flight attendants) and aircraft dispatchers. The constant 2012 dollars and discounted 3 and 7 percent present value
costs are summarized in the Cost Summary section below.

General Cost Assumptions and Data Sources

T he assumptions and identification of key data sources to estimate costs are:

• The number of part 121 and 121/135 operators , and their pilots w ere obtained through the
FAA National Vital Information Subsystem (NVIS) database in February 2013

. 31

• NVIS only provides a total number for pilots and does not break out total pilots into pilots, check pilots and flight instructors

. We use the same assumptions as in the SNPRM that 4.0 percent of the total number of pilots are check pilots, and 2.0 percent of the total number of pilots are instructo rs.

• Using the FAA Aerospace Forecasts , for fiscal years 20 1 3

- 20 3 3 , the FAA estimated that the affected population of pilots would grow at approximately 0. 4 percent per year. 32

• In estimating simulator costs, we assume a full simulator; therefore, two pilots and one instructor will occupy a simulator during training. We assume operators will assign pilot s for training in the simulator based on availability and current training schedules

.

• Flight crewmembers undergoing initial, transition, upgrade, or recurren t training will train on one airplane group per training cycle.

• As in the SNRPM, the turnover rate of 5 percent covers pilot retirements and other pilot
attrition. 33

31 The National Vital Information Subsystem (NVIS) is a comprehensive Flight Standards Services (AFS) information system containing up

- to

- date information about operator s including the number of pilots. 32 FAA Aerospace Fo recasts 2013

- 2033. Table 30: Active Pilots by Type of Certificate, Airline Transport, 2012

- 2033. http://www.faa.gov/about/office _org/headquarters_offices/apl/aviation_forecasts/aerospace_forecasts/2013

- 2033/ Accessed March 2013.36 • The FAA conducted a survey of eight part 121 operators and estimated that annually 2.6

perc ent of the affected pilots will require upgrade training and annually 5.7 percent will require transition training.

• For part 121 operators, there is an average of two major groupings of aircraft types (equipment groups) per operator

. 34

• As in the SNPRM, we a ssume that check pilots and flight instructors earn 10 percent more
than line pilots.

C ost Estimate

The FAA analyzed the expected costs of the final rule over the 201 3 through 202 8 analysis
interval

. The major f actor driving the expected costs is the additional training tasks in sophisticated simulators . T he final rule adds training tasks, and therefore costs, to initial, transition, upgrade, and recurrent pilot training programs. Other cost driving factors include the high value of pilot’s time , ground school training, and additional paperwork.

Some p aperwork costs will begin on the effective date in 201 4 while other paperwork costs will begin one year before the 2019 compliance date

. The rest of the new paperwork costs start on the compliance date in 201 9 , and will continue to 2028, the end of the analysis interval. These
start dates are listed in the Estimated Paperwork Costs section.

This cost analysis estimate s the final rule costs by the objective group. 35 The cost model was computed annually a s follows: ( the number of pilots * fully burdened pilot wage * training hours) + (the number of pilots * ( simulator costs 36 +ground school costs )) + paperwork cost.

33 http://www.faa. gov/news/conferences_events/aviation_forecast_2010/agenda/media/GAF%20Jim%20Higgins%20 and%20Kent%20Love.pdf The University of North Dakota estimates that 2.12% of pilots have retired annually along with forecasting 2.94% pilot attrition (loss of medical, loss of certificate, career transfer) from 2009 to 2024. We rounded to three digits. 34 As of March 2013, the OAG Fleet Database reports an average of 1. 85 equipment groups per operator which we rounded up to two . The OAG Fleet Database defines an equipme nt group as major groupings of aircraft types. For example, B737 would include all of the B

- 737 variants. 35 An objective group is a grouping of related final rule sections. 36 Includes flight instructor’s fully burdened wages.37 Table 10 details the final rule provisions by objective grouping and provides the basis for the cost analysis

.

Table 10 Summary of Final Rule Requirements and When FAA Expects Costs to Accrue

The final rule will add paperwork costs to most of the objective group s listed in the T able 10

. Additionally, the final rule will add simulator and ground school costs to both extended envelope training objective group s

. However, the FAA has determined that the training and evaluation time required to complete the taxi and pre

- takeoff procedures w ould not take any longer than the time currently required to complete those maneuvers because
, the procedures are incorporated into the existing taxi and pre

- takeoff maneuver requirements. Moreover, since crosswind takeoff and landing are already required training tasks
, and gusty winds are merely one variable of th ese current requirement s , the agency does not believe any additional time is necessary to train and evaluate crosswind takeoffs and landings with gusts. Finally, the amended proficiency check

r equirement for PICs does not add simulator time during recurrent training because under existing regulation s PICs who fly multiple aircraft types must complete either a recurrent training or checking event on each aircraft type flown . Therefore, the recur rent training38 framework in place today contemplate s that a PIC could fulfill the recurrent training program requirements by completing a proficiency check on each aircraft type in which the PIC is qualified to serve. The following sections will discuss the development of parameters that form the basis for the final rule cost estimate. First, we will discuss our forecast of the annual number of pilots who will go through the additional initial, transition, upgrade and recurrent training required by the
final rule

. Next, we present the pilot’s hourly wages and the derivation of hourly employee
benefits. Then we list the part 121 operators affected by the final rule . Next, we discuss the
increase in t ime and cost the final rule adds to simulator and gro und school training programs for the extended envelope objective groupings

. W e then estimate the paperwork costs of revising pilot manuals, air carrier training courseware, and air carrier training programs for each of the objective groupings

. 37 Lastly, w e present a summary of the total costs.

There are other changes in the final rule that are either editorial or procedural. Some changes expand or clarify the intent of the final rule through reorganization, updating terminology, and clarifying procedures . These editorial or procedural changes will not impose any new requirements or costs.

Number of Pilots and Operators Affected by the Final Rule

In this section, we first estimate the number of pilots affected by the final rule. Then we discuss
the source and number of part 121 operators affected.

To estimate the number of flight crew members in the analysis interval w e begin with a 201 3 base
of 76,039 pilots who are employed by part 121 operators. As stated in the General Cost Assumptions and Data Sources section, we obtain the number of pilots from National Vital Information Subsystem ( NVIS ) . Appendix 9 lists the part 121 operators
, their pilots employed
, and if the operator trains their pilots under AQP

.

37 The Training Program is t he document that is submitted to the FAA for approval. It contains all the training requirements for that air carrier's crewmembers. Training courseware is the document that instructors teach from

— or the speaker's notes. This document is not FAA approve d, although the FAA can review the document at any time and require changes to be made.39 We apply the same estimate of check pilot s and flight instructor
, used in the SNPRM
, to calculate the adjusted pilot base. First, we estimate the number of check pilots by multiplying
the 201 3 base of 76,039 pilot s by 4.0 percent to arrive at 3,042 check pilots in 2013. Next we
estimate the number of flight instructor s by multiplying the 76,039 pilots by 2.0 percent to arrive at 1,521 flight instructor s in 2013. We then subtract ed the number of check pilots and instructor pilots from the 76,0 39 pilots to arrive at 71,476 pilots

.

We then estimate the number of pilots, check pilots and flight instructors who will undergo initial, upgrade, transition, and recurrent training in 2013. Next, we estimated the number of pilot s who will have to go th rough initial training.

Pilots who undergo initial training consist of newly hired pilots who replace pilots lost to
attrition (loss of medical certificate , loss of airman certificate, career transfer
, or retire ment )

. We estimate five percent of the to tal number of pilots would leave an operator through attrition. Pilots who undergo initial training are also new ly hire d pilots due to operator growth (fleet and route expansion and traffic growth ). Based on the FAA forecast, we expect the total number of part 121 pilots to increase by 0.4 percent annually.

We then estimated the number of newly hired pilots by multiplying the 2013 base of pilots
, check pilots, and flight instructors by 0.4 percent for growth and five percent for attrition

. These
calculations are displayed in the T able 11 below.

In addition, w e expect that annually 2.6 percent of the total pilots will go through upgrade training and annually 5.7 percent through transition training

. 38 Pilots who go through upgrade training do so because they are upgrading from a flight engineer to a first officer ( second in command) or a first officer to a captain (pilot in command) . Pilots who go through transition training do so because they are transitioning to another aircraft in an operator’s fleet. We estimated the number of pilots who would complete upgrade and transition training by

38 This expectation is based on a survey of 8 part 121 operators, and the FAA believes this data is representative of all part 121 operators.40 multiplying the 2013 base of pilots, check pilots, and flight instructors by 2.6 percent for upgrade training and 5.7 percent for transition training. These two calculations are displayed in the T able
11 below in the column labeled “Upgrade” and “Transition”.

Next, we calculated the remaining number of pilots by subtracting the pilots who left due to
attrition
, who completed upgrade training , and who completed transition training from the 2013 base of pilots, check pilots, and flight instructors

. The remaining pilots take recurrent training. Lastly, we estimated the number of pilots in 2014 by addin g the 2013 base of pilots, check pilots, and flight instructors to the number of pilo ts that would be added by growth

.

We repeated this process to estimate the number of pilots in the rest of the analysis interval (2014

- 2028) for pilots, check pilots, and flight instructors. The FAA notes that the final rule requires pilots to go through extended envelope simulator training every 24 months and extended envelope ground school training every 12 months and therefore must forecast pilots annually throughout t he analysis interval. T able 11 show s the se results :

Table 11 Pilot, Check Pilot and Flight Instructor Forecast41 * Details may not add to row or column totals due to rounding.

In order to estimate the paperwork costs for each part 121 operator affected by the final rule, the number of operators are necessary. We also need ed to determine which operators train their pilots under AQP and which ones train their pilots under the tra ditional training rules

. This
estimate is necessary because operators who train under AQP are required under § 121.909 , to complete an evaluation of their existing training program against the new requirements set forth
in this final rule to ensure these requirements are being met. Thus, operators training under AQP will have an additional paperwork burden that operators who train under traditional training rules
will not have.

The numbers o f part 121 operators were obtained through the FAA National Vital Information Subsystem (NVIS) database and are current as of February 2013 . The determination of the42 operators who train their pilots under AQP versus non

- AQP was provided the AFS

- 230, the Voluntary Safety Programs Branch of the FAA. 39

Appendix 9 shows th at there are 83 operators currently affected by the final rule ; 22 of the 83 operators train their pilots under AQP, while the remaining 61 operators train their pilots under

s ubpart s N and O.

Annual and Hourly Wages and Benefits

In this section, we disc uss the pilot wages the FAA used in the SNPRM, the reason for using those wages, and their source. We then discuss the wages the FAA uses in the final rule, the reason for using these wages, and their source

.

The proposed requirements of the SNPRM cont ained provisions, with different requir ements, for pilots in command (c aptains), second in command pilots (first officers), check pilots, flight engineers, and flight instructors. In addition, the SNPRM resulted in different training time
increases for pilots who operate turbojet airplanes and pilots who operate turboprop airplanes.
Therefore the SNPRM costs analysis required hourly wages for each of the se pilot categor ies

. For the SNPRM, the Flight Standards Services (AFS) of the FAA provided the ave rage hourly wages for each of these pilot categor ies . As stated in the General Cost Assumptions and Data
Sources section, for the SNPRM check pilots and flight instructors earn 10 percent more than pilots. For the SNPRM, the FAA multiplied the hourly pil ot wages, for each category of pilots, by a total 2009 benefit as a percentage of payroll from the Bureau of Labor Statistics (BLS) survey of employee benefits to arrive at a fully burdened hourly wage . Table 12 shows the pilot hourly wage s , the estimated hourly benefit s , and total hourly cost s, by pilot category, used in the
SNPRM

.

39 The FAA makes the determination that an operators can start train ing their pilots under AQP when the operator receives an FAA

- approved Phase IV Qualification letter.43 Table 12 SNPRM Pilot, Flight Engineer Hourly Wage & Benefit ( 2009 $)

The final rule does not contain different requirements for each of the pilot categories or turboje t or turboprop equipment types. The final rule requirements add the same amount of simulator and ground school training time to captains and first officers regardless of the aircraft they operate

.

In May 2012, BLS published the National Industry

- Specific Occupational Employment and Wage Estimates for Scheduled Air Transportation. The North American Industry Classification System ( NAICS ) code for Scheduled Air Transportation pilots is 481100. 40 The major group for pilots under the 481100 NAICS code is 53

- 2011. The FAA believes that the 53

- 2011 pilot survey is the appropriate wage to estimate the salary of the part 121 pilots, check pilots, and flight instructors affected by the final rule. 41 The BLS survey lists $128,760 as the annual mea n salary for a pilot. The cost analysis will use the annual mean salary of $128,760 for a pilot to estimate the additional costs the final rule adds for simulator and ground school training tasks.
The FAA notes that the survey lists the annual mean salar y range for pilots , by area in the continental United States, from $72,580 to $184,320.

BLS website for Scheduled Air Transportation pilots states “ Wages for some occupations that do not generally work year

- round, full time, are reported either as hourl y wages or annual salaries

40 The NAICS code is the standard used by Federal statistical agencies in classifying business establishments for the purpose of collecting, analyzing, and publishing statistical data related to the U.S. business economy. 41 BLS describes this survey as “Pilot and navigate the flight of fixed

- wing, multi

- engine aircraft, usually on scheduled air carrier routes, for the transport of passengers and cargo. Requires Federal Air Transport certificate and rating for specific aircraft type used. Includes regional, National, and international airline pilots and flight instructors of airline pilots.” http://www.bls.gov/oes/current/oes532011.htm Accessed April 2013.44 depending on how they are typically paid ” ; 42 BLS reports pilot wages as annual salaries because

p ilots do not work a 40 hour work week. The refore, the FAA used the Pro Pilot Compensation Salary Study

– 2012 compiled by ABCO Data Systems in Vienna, VA and estimated that pilots, who work for part 121 airlines, typically have their annual pay based on 80 hours per month. 43 The FAA divided the BLS annual mean salary by 80 hours per month to estimate the average hourly wage for a pilo t operating in part 121 service.

In addition, pilot benefits (such as health benefits, vacation, sick time, etc

. ) must be added to estimate the costs for this analysis. In Ma rch 2013 , BLS published their “ E mployer Costs for Employee Compensation” study of employee benefits . In Table A of the BLS study, they
estimated the total 20 12 benefit s, as a percentage of total compensation
, at 29.7 percent for private industry

. 44 The FAA accepts th e BLS 29.7 percen tage of total compensation to estimate
the value of benefits for pilots, check pilots, and flight instructors as an additional cost of this
final rule.

T echnical writers and flight instructor s are also necessary to complete the paperwork requirements of the final rule. In May 2012, BLS published the Na tional Industry

- Specific Occupational Employment and Wage Estimates for Scheduled Air Transportation. The NAICS
code for Scheduled Air Transportation technical writers is 27

- 3042. The FAA believes that the
27

- 3042 technical writer survey is the appropria te wage to estimate the salary of the part 121 technical writers affected by the final rule. 45 The BLS survey lists the mean hourly wage for a technical writer is $32.65. The cost analysis will use the annual mean hourly wage of $32.65 for
a technical wri ter to estimate the additional costs along with the total 20 12 benefit s of 29.7 percent discussed above. The survey lists the annual mean salary range, by area in the continental United States, for technical writers from $33,570 to $97,050.

Table 13 shows these results for pilots, check pilots, flight instructors and technical writers

.

42 http://www.bls.gov/oes/current/oes532011.htm#(4) 43 http://www.safetystanddown.com/wp

- content/uploads/2012/06/Salary

- study

- 6

- 12

- lyt_June.pdf Accessed April 2013. 44 http://www.bls.gov/news.release/pdf/ecec.pdf Accessed April 2013. 45 http://www.bls.gov/oes/current/oes273042.htm Accessed April 2013.45 Table 13 Mean Hourly Wages Plus Benefits ( 2012 $)

* Details may not add to row or column totals due to rounding.

Final Rule Simulator and Ground School Additional Time for Pilot s

Pilots must undergo two basic methods of training . This training includes flight training and ground school. In this section, we first discuss the method the FAA used to estimate the simulator training time th is final rule adds to curre nt pilot flight training requirements . We then
discuss the additional ground school training time the final rule adds

.

This regulatory evaluation will not attempt to estimate the existing practice relative to the new requirements. We base our estimate on the incremental time this final rule adds to the current regulatory requirements for captains and first officers who operate in part 121 service . To the extent industry current practices exceed the regulatory requirement s , we believe that the cost estimate will result in an over estimate of the actual compliance costs.

Under the assumption that existing facilities are optimized, 46 the final rule could result in additional capital and operating expenses to either build or expand training and sim ulator facilities for flight crewmembers. Rather than estimate the capital recovery costs over the life cycle of simulators and expansion of facilities, we estimated the rent of simulator services with a usage fee per pilot. As mentioned in the Backgroun d section, the FAA estimates the average cost of simulator session to be $500 an hour plus the cost of an instructor with two pilots in the
simulator.

46 R esponders to the NPRM and SNPRM confirmed that their existing training facilities, simulators, and ground school classes are op timized.46 Typically, simulator sessions are scheduled in four hour blocks. In the NRPM, the FAA
estimated the costs based on four

- hour simulator sessions. After analyzing the tasks prescribed in the technical report accompanying the SNPRM
, 47 we believe many of the simulator sessions
will last less than four hours. Therefore, in the SNPRM and final rule cost analysis, we estimat e the cost of the additional tasks the final rule requires for pilot s in the simulator rather than the
number of four hour simulator sessions.

When a pilot enters a simulator for training, the pilot must c omplete a prescribed number of
tasks. On October 26, 2009 the FAA conducted a simulator trial to determine the time necessary to perform the proposed recurrent proficiency check requirements . The agency collected data on the time it took to complete the recurrent proficiency check tasks proposed in the NPRM and then used this data to estimate the time required to complete the proficiency check requirements proposed in the SNPRM

.

For the final rule, the FAA conducted a second simulator trial to determine the time required to complete the additional final rule maneuvers and procedures in each curriculum. During the second simulator trial, two FAA pilots performed the extended envel ope flight training requirements. The FAA pilots serving as the pilot in command (PIC) and second in command pilot (SIC) both h eld ATP certificates and were current and qualified to operate the Airbus 330. The PIC was type rated. The SIC was not type rat ed. The Instructor Operating Station (IOS) operator had experience operating the Airbus 330 Level D simulator. All required checklists and procedures were completed in their entirety for each maneuver/procedure. All required Air Traffic Control (ATC) ins tructions and clearances were provided. The FAA expects task times to be comparable throughout the various aircraft fleets used in part 121 operations because we do not expect the differences in aircraft design to have an impact on task times.

The train ing time listed below represent the data collected during the second simulator trial and provides the estimated simulator time required to meet the extended envelope flight training

47 The Flightcrew Member Training and Qualification Review and Analysis Technical Report can be found in the docket for this rulemaking. The URL for the docket is http://www.regulations.gov/search/Regs/home.html#docketDetail?R=FAA

- 2008

- 0677

.47 requirements in the final rule. The FAA has reviewed both simulator trial s and revised the cost estimates for the training tasks required by the final rule. The full discussion of th e additional tasks the final rule adds to pilot training, along with an estimate of the time necessary to complete them, are listed in the preambl e and technical report in the federal docket. 48

The final rule add s simulator time for pilots to complete extended envelope training maneuvers
and procedures

. As noted previously, we determined the training and evaluation time required to complete the tax i and pre

- takeoff procedures, as well as crosswind maneuver with gusts, will not take any longer than the time required under existing regulations for completion. Also, the final rule requirement to include pilot monitoring during Line Oriented Flight Tra ining ( LOFT ) does not place any additional burden on operators who use advanced simulation training programs to train their pilots or substitute LOFT for recurrent proficiency check requirements because the requirement can be met during the ordinary course of any LOFT that is currently part of a part 121 operator’s training program.

T he final rule require s extended envelope training maneuvers and procedures for all pilots during initial, transition, and upgrade flight training and at least once every 24 months durin g recurrent flight training. At a minimum, a ll extended envelope training must take place in a Level C full flight simulator. 49 To account for these variables, the agency estimates the following ranges of
simulator time are required to meet the extended e nvelope training requirements. For the base

case cost estimate , we compute the average simulator time, for initial, upgrade, transition, and recurrent training, with the range of minutes listed in Table 14.

48 These reports may be found in the docket for this rulemaking. The URL for the docket is http://www.regulations.gov/search/Regs/home.html#docketDetail?R=FAA

- 2008

- 0677

. 49 The FAA n ote s that t he final rule provides deviation authority i n those instances in which a Level C or higher full flight simulator is unavailable

.48 Table 14 Additional Simulator Time from Final Rule (Minutes)

As stated in the Background section, the FAA did not include travel expenses in the final rule cost analysis for the additional simulator training time because the FAA believes operators can complete the new training requirements within the same amount of days as their current initial, upgrade, transition, or recurrent simulator and ground school training sessions . With regard to simulator training, w e a re assuming an additional 90

- 135 minutes for the initial extended envelope simulator training. If a n operator uses 4 hour simulator sessions (which is not required), it would take 6 days of training to get 24 hours. The operator could add 15

- 25 minutes to each simulator session and still finish in the same number of days. For transition
, upgrade, and recurrent simulator training we are assuming even less time for the extended envelope training, so again the same rationale applies. It is not efficient for the operator to use an extra day of training just for the additional simulator training time the final rule requires

. 50

In addition, t he final rule extended envelope ground training will be required for all pilots during initial, transition, and upgrade training and at least once every 1 2 months during recurrent ground school training. To account for these variables, the agency estimates the following amount of ground school time is required to meet the extended envelope training requirements.

50 Although industry informed us that simulators are typically rented in four

- hour blocks, simulator rental varies depending on the contract that the carrier has with the s imulator owner. We assume that air carriers will be able to rent only the time needed to complete the training required by the rule. In addition, many large operators have their own simulators and do not need to rent.49 Table 15 Additional Ground School Time from Final Rule

From the General Cost Assumptions and Data Sources section, 100 percent of the pilots will undergo distance learning for their ground school training. The costs for a pilot to undergo distance learning will be the same for the hours spent in a ground school class room but will not include transportation costs such as airfare, automobile mileage, hotel, facility usage fees, and per diems because of distance learning

.

The FAA believes that the additional simulator and ground school time this final rule requires can be conducted in an operator’s current training schedule without adding any additional travel
time. In the inter est of performing a robust cost benefit analysis, the FAA conducted a sensitivity analysis on the cost of pilots having to spend an extra day in simulator for the additional training tasks added by the final rule and determined that the benefits still exce ed the costs. The results of this sensitivity analysis can be found in Appendix 10.

Costs and Methodology for Final Rule Estimated Simulator Training Costs

We now discuss the methodology used to estimate the final rule costs for the additional simulato r training tasks required by th e final rule. A dditional simulator training costs are estimated by summing the cost of the additional time the final rule requires pilots to spend in the simulator plus the cost of the additional time simulator s are used. T he additional final rule cost for pilots in the simulator is estimated using fully burdened pilot wages from BLS. The cost for the additional time simulators are being used is estimated using hourly simulator costs based on
FAA data.50 The FAA estimate s th e additional time pilots spend in the simulator by multiplying the number of pilots by the additional time the final rule will require. We then multiply th e additional
simulator time by the fully burdened pilot ’ s hourly wage . An instructor will be needed for each additional simulator session with two pilots. The additional instructor time is multiplied by the flight instructors’ fully burdened wage. As mentioned in the General Cost Assumptions and
Data Sources section, the re are two pilots being trained for each simulator session. This
calculation is repeated for pilots who go through initial, upgrade, transition or recurrent training while taking into consideration that t here is one instructor for every two pilots in the simulator

. The FAA notes that pilots who go through initial, upgrade, or transition training would go through recurrent training in the following years of the analysis interval.

The FAA estimate s the cost of the simulator usage fees by multiplying the additional hours the
final rule requires for pilots to be in the simulator , with the $500 average hourly simulator cost

. 51 We perform these calculations for the additional time the final rule adds for pilots training in the
simulator and the additional ti me the simulator is being operated for both the low and high range of simulator times the FAA estimated for initial, upgrade, transition, or recurrent simulator training.

For the check pilots and flight instructors we calculate the incremental costs the final rule adds in a similar manner as we did for the pilots.

We then sum the initial ( attrition or growth) training cost s for pilots, check pilots, and flight
instructors with the transition, upgrade, and recurrent training costs to arrive at the t otal cost the final rule adds to part 121 operators for simulator training

. We perform this calculation for the both low and high range of simulator times. Lastly, we multiply the total costs, by year, by the three and seven percent present value series.

51 Hourly simulator costs provided by the FAA Flight Standards Service (AFS)

.51 T able 16 shows these results for the low and high range of time the FAA estimates the final rule
adds to the time pilots are in the simulator. 52 Appendix 11 shows the details by pilot, check pilot, and flight instructors in 2012 dollars

.

Table 16 Simula tor Training Costs

– Pilot Wages Plus Simulator Usage Time ( 2012 $)

* Details may not add to row or column totals due to rounding.

Estimated Costs and Methodology for Final Rule Ground School Training Tasks

We now discuss the FAA’s estimate of th e final rule’s additional ground school training costs to pilots, check pilots
, and flight instructors.

For the final rule, t he FAA re

- estimated the ground school cost analysis based on updated data and analysis that reflect the final rule requirements

.

The ground school costs consist s of the sum of the additional time the final rule requires for pilots , check pilots, and flight instructor s to be in initial, transition, upgrade , and recurrent ground school training

. The initial, transition, and upgrade training occurs only once while the recurrent training occurs annually.

For ground school training, the FAA continues to allo w training to be conducted in an environment other than a classroom by distance learning. An approved distance learning

52 See Table 14, Additional Simulator Time from Final Rule (Minutes).52 program e nsures the training will provide the students with the knowledge and cognitive skills to perform their required duties. As mentioned in the Background section, the agency assumes 100 percent of pilots w ill take advantage of distance learning and w ill not incur travel costs for the final rule ground school training

.

W e calculate the additional time pilots are in ground school training by multiplying the number of pilots
, with the additional ground school time
, and then their hourly wage

. We note that although operators do not incur travel costs from distance learning
, we still need to include the

cost of the additional time the final rule adds to pilo t s ’ ground school training regardless of whether the pilots are distance learning or lea rning in a classroom.

W e then sum the initial, transition, upgrade
, and recurrent ground school training costs to arrive
at a total cost. Next, we sum the pilot, check pilot, and flight instructor final rule ground school training costs . W e calculate th e final rule ground school training costs f or check pilots and flight
instructors in a similar manner as for pilots.

T able 17 shows the results of our calculation s for the estimate of total ground school training

costs. Appendix 1 1 shows the details by pilot, check pilot, and flight instructors in 2012 dollars

. Table 17
Ground School Costs ( 2012 $)

* Details may not add to row or column totals due to rounding.53 Estimated Paperwork Costs

The final rule adds paperwork in the curricu lums for part 121 operator training programs
, training courseware , and operating manuals. This section discusses the estimated costs , by objective groups of provisions, for the additional hours it takes to create the paperwork, along with the number of pages the final rule adds. The FAA notes that there is only a one

- time paperwork cost to respondents for each of the groups of provisions.

The FAA estimates no paperwork costs for the following groups of provisions:

• Fraud and falsification (§ 121.9)
,

• Related aircraft differences training (§§ 121.400, 121.418, 121.434, 121.439, 121.441)
,

• Proficiency checks for PICs (§ 121.441(a)(1)(ii))
, and

• Approval of FSTDs (§ 121.407)

.

The FAA assumed that air carriers will incur costs related to the paperwork burden for the following groups of provisions on the effective date of the final rule, which is 120 days after the publication of the rule:

• Personnel identified as flight attendants (§ 121.392)
,

• Communication records for domestic and flag operations (§ 121.711) , and

• Approval of Advanced Qualification Program (§ 121.909)

.

Although compliance with the provisions on qualification and training for instructors and check
airmen who serve in FSTDs (§§ 121.411, 121.412, 121.413, 121.414) is required 5 years after the effective date, the FAA believes that air carriers will start to accrue paperwork costs 4 years
after the effective date.

Air carriers will incur paperwork costs fo r the following groups of provisions five years and 120 days after the publication of the rule:

• Training equipment other than FSTDs approved under part 60 (§§ 121.403(b)(2), 121.408)
,

• Pilot monitoring (§§121.409,121.544, Appendix H)
,54 • Remedial training (§§ 121.415(h) and § 121.415(i)) , and

• Extended envelope flight training maneuvers and procedures (§§121.407(e),121.423, 121.424, 121.427(d)(1)(i), 121.433(e)), Extended envelope ground training subjects (§§ 121.419(a)(2), 121.427), Runway safety maneuvers and procedures (Appendices E and F) and Crosswind maneuvers including wind gusts (Appendices E and F).

The FAA estimated the paperwork costs for these provisions by multiplying the number of hours
the FAA estimates to update the training program, training co urseware, or operating manual by the hourly rate of the person responsible for the update , by the number of part 121 operators affected by the provision

. The Flight Standards Service (AFS) of the FAA provided average hourly times and the number of additional pages of paperwork the final rule will add. Table 18
summarizes the FAA’s cost estimate of the total paperwork requirement for each of the following groups of provisions.

The FAA estimates the total paperwork costs fo r the final rule will be about $ 8.2 million . T he following sections discuss each objective group of provisions, when the provisions will become effective, and their paperwork costs.

Fraud and falsification (§ 121.9)

Although f raud is current ly prohibited by criminal statute, the FAA has added language prohibiting fraud and falsification to part 121 to emphasize the importance of truthful statements. This provision p rohibits fraudulent or intentionally false statements in, or a known omission
fr om, any record or report that is kept, made, or used to show compliance with this part, or to exercise any privileges under this chapter. 53 Th is provision e nhances FAA enforcement options by allow ing the agency to take certificate action or assess a civil penalty against a person for making a fraudulent or intentional false statement

. Compliance with this provision is required

53 18 USC 1001is a criminal statute prohibiting fraud and intentional falsification in matters within the jurisdiction of the executive branch . Thi s regulation will allow the agency to pursue civil enforcement in instances in which a person has committed fraud or falsification.55 1 20 days after the date of publication of the final rule in the Federal Register. The FAA
estimates that there are no costs for th is provision.

Personnel identified as flight attendants (§ 121.392)

This provision prohibits operators from identifying any person as a flight attendant if that person has not completed all flight attendant training and qualification. Individuals who have not completed all flight attendant training and qualification requirements must be clearly identified (e.g. via an announcement, by wearing civilian clothes, or not wearing a uniform). This provision may reduce confusion of passengers during an emerg ency situation on a flight who might otherwise presume that these individuals are fully qualified flight attendants.

Operators must revise flight attendant manuals to reflect the new procedures. Compliance with this provision is required on the effecti ve date of the final rule, 120 days after the date of publication in the Federal Register. The FAA estimates that, for a certificate holder operating under part 121, one page of the content of the flight attendant operating manual will require
revision fo r each affected operator.

Proficiency checks for PICs (§ 121.441(a)(1)(ii))
Currently, in accordance with § § 121.433(d) and 121.441(a)(1) , a PIC who serves on more than one aircraft type must complete either recurrent flight training or a proficiency c heck on each aircraft type every 12 months . To ensure PICs operating multiple aircraft types maintain proficiency on each aircraft type, the final rule amends § 121.441(a)(1) by requiring PICs who fly more than one aircraft type to receive a proficiency c heck in each aircraft type flown at the existing 12

- month recurrent training interval

. T he FAA expects that any recurrent training program updates needed to reflect this change are minimal and are subsumed in the paperwork
costs for the collective amendments made to the recurrent training provisions in this final rule

. Compliance with new paragraph (a ) (1)(ii) of this provision is required 5 years and 120 days after
the date of publication of the final rule in the Federal Register , consistent with t he SNPRM

. The
FAA estimates that there are no costs for this provision.56 Related aircraft differences training (§§ 121.400, 121.418, 121.434, 121.439, 121.441)

Section 121.400 discusses the applicability and terms used in the final rule and adds no costs

.

T he remaining cost relieving provisions allow pilots
, who train in aircraft types that do not have a common type certificate
, to take credit for common tasks that pilots are already trained in. An example of this would be the Airbus airplanes that have cockpit commonality
, and through related aircraft difference training, these provisions could provide cost savings to operators.

Although air carriers are not required to seek a related aircraft designation as permitted by § 121.418(b), if they seek th e designation and receive it, it may provide relief from the training
, checking, and experience requirements in §§ 121.419, 121.424
, 121.425 , 121.427, 121.434,
121.439 and 121.44 1

. Lowering the cost for air carriers to adopt new aircraft types could speed up the entry of the newer aircraft types into the fleet

. However, the magnitude of any cost savings would be based on operator’s future actions and therefore we do not attempt to quantify
th e savings

.

These provisions are effective 120 days after the date of publication of the final rule in the Federal Register. The FAA estimates that there are no costs for these provisions.

Training equipment other than FSTDs approved under part 60 ( § § 121.403(b)(2) , 121.408)

Current regulations do not provide specific requirements for training equipment other than FSTDs, but the regulations generally require training equipment to be adequate. Section 121.408 states that the FAA must approve training equipment (e.g. cockpit pr ocedures trainers, door/exit trainers, water survival equipment, etc.) used to functionally replicate aircraft equipment required to be used as part of the approved training program. Compliance with this provision is required 5 years and 120 days after da te of publication of the final rule in the Federal Register. This provision will require an additional 5 pages in each air carrier’s General Operating manual. Section 121.403(b)(2) requires that operators provide the FAA with a list of all training devi c es or training aids that the certificate holder will use. Compliance with this provision is required 557 years and 120 days after date of publication of the final rule in the Federal Register. The FAA estimates that, for a certificate holder operating und er part 121, one page of the content of the air carrier’s approved training program will require revision for each affected operator.

Approval of FSTDs (§ 121.407)

This provision conforms the requirements for evaluation, qualification, an d maintenanc e of FSTDs used in part 121 to existing p art 60 requirements, by providing a reference to part 60 in part 121 and adding a new paragraph consistent with the require ment in § 121.423 to use an FSTD for extended envelope training. This provision therefore provides clarification regarding

p art 60 requirements that currently apply to p art 121 training. Compliance with new paragraph (e) of this provision is required 5 years and 120 days af ter date of publication of the final rule in the Federal Register, because the new extended envelope training required by § 121.423 is not required until such time. The FAA estimates that there are no compliance or paperwork costs for this provision.

Pil ot monitoring (§§ 121.409, 121.544, Appendix H)

Section 121.409 and Appendix H require training on pilot monitoring to be incorporated into existing requirement for scenario based training. Section 121.544 also establishes an operational requirement for p ilots to follow air carrier procedures regarding pilot monitoring.

These provisions reinforce active monitoring skills to the pilot not flying by requiring the inclusion of active pilot monitoring skills during line oriented flight training (LOFT). App endix
H currently requires all part 121 pilots in training to complete a four hour LOFT in a simulator

. The FAA believes that the active monitoring skills of this provision can be accomplished in the current four hour LOFT requirements. 54

54 Appendix H requires all pilots trained using advanced simulation to complete a qualification LOFT upon completion of init ial, transition, or upgrade training. Under existing regulations, LOFT may be substituted for recurrent flight training on an alternating basis, but it is not required.58 Compliance with pilot monitoring is required 5 years and 120 days after date of publication of the final rule in the Federal Register. The FAA estimates that §§ 121.544 and 121.409 will add 20 pages to each air carrier’s training courseware and one page to each air carri er’s approved training program.

Remedial training (§§ 121.415(h) and § 121.415(i))

These provisions require certificate holders to incorporate methods for remedial training and tracking for pilots who have experience d multiple failures or demonstrated performance deficiencies in the training or checking environment into approved training programs. Although the FAA expects that industry already addresses deficiencies in pilot performance in accordance with existing agency guidance, these final rule pro visions create a requirement for compliance. Examples of tracking include extra line checks, extra procedures, etc. to make sure the pilot
trains to his deficiencies.

In August 2010, Congress directed the FAA to ensure air carriers develop remedial training programs for flight crew members who have demonstrated performance deficiencies or experienced failures in the training environment. The final rule remedial training requirements are intended to reflect the congressional direction and existing agency guidance. 55 We assume
air carriers training under subparts N and O are already implementing the recommendations in the agency’s guidance material based on information received during FAA inspections in 2009 as part of the Call to Action to Enhance A irline Safety

. Also, since subpart Y already requires an AQP to include such a system , we assume no additional cost to carriers training under AQP. Therefore, we only estimate the paperwork costs for documenting this guidance.

Compliance with these prov isions is required 5 years and 120 days after the final rule is published. The FAA estimates that, for a certificate holder operating under part 121, 20 pages will be added to each air carrier’s courseware and one page to each air carrier’s training progr am.

Communication records for domestic and flag operations (§ 121.711)

55 SAFO 06015, Remedial Training for p art 121 Pilots.59 This provision clarifies the information that must be included in the record of communications between the pilot and aircraft dispatcher based on a legal interpretation of the cur rent requirement in § 121.711. This provision also clarifies the recordkeeping requirement by defining “en route” for purposes of this section and applies the requirement to all flight crew/dispatch communications made using a two

- way communication system required in accordance with § 121.99. It is current industry practice to record all en route communications as defined by the final rule. Compliance with this provision is required 120 days after date of publication of the final rule in the Federal Regis ter.

The FAA estimates that, for a certificate holder operating under part 121, one page will be added to each air carrier’s pilot operating manual and one page to each air carrier’s aircraft dispatcher operating manual.

Qualifications and Training f or i nstructors and check airm e n who serve in FSTDs (§§ 121.411, 121.412, 121.413, 121.414)

Sections 121.411 and 121.412 add simple technical changes, such as the deletion of obsolete dates, deletion of obsolete duty positions (such as flight navigator), and correction of terminology. These modifications do not affect costs.

Appendix H currently includes robust requirements for simulator training for check airmen and instructors. These final rule provisions will add some additional check airman (simula tor) and flight instructor (simulator) initial, transition and recurrent training curriculum items to current requirements in existing §§ 121.413 and 121.414 training to ensure comprehensive check airman and flight instructor understanding of new training tasks in the final rule and the limitations of simulation. When the FAA introduced the extended envelope requirements, we felt it was important to train simulator instructors on how to train pilots for these events. Although this requirement adds recurre nt training subjects to instructor training, the FAA believes the additional time can be incorporated into the time currently required to train check pilots and instructors. The addition of these minimal curriculum requirements will not require additional program hour requirements and therefore have minimal to no costs.60 Although compliance with this provision is required at 5 years and 120 days, the FAA believes that operators will start accruing paperwork costs 4 years after date of publication of the final rule in the Federal Register. The FAA estimates for a certificate holder operating under part 121, §§ 121.413 and 121.414 , these provisions will each add 40 pages to each air carrier’s training
courseware and two page s to each air carrier’s approved training program.

Extended envelope flight training maneuvers and procedures (§§ 121.407(e), 121.423, 121.424, 121.427(d)(1)(i), 121.433(e)), Extended envelope ground training subjects (§§ 121.419(a)(2), 121.427), Runway safety maneuvers and procedures (Appendices E and F) and Crosswind maneuvers including wind gusts (Appendices E and F).

Amendments to § 121.407 provide a reference in part 121 to part 60 and the new extended envelope training requirement in § 121.423, but does not add requirements ; there fore there is no paperwork cost.

Sections 121.419 and 121.427 revise current initial, transition, upgrade or recurrent ground training to include training for extended envelope flight training maneuvers and procedures, as well as additional training regarding runway safety and crosswind takeoffs and landings with gusts. The FAA estimates that, for a certificate holder operating under part 121, §§ 121.419 and 121.427 will add 20 pages to each air carrier's training courseware and one page, for each

pr ovision (two pages total) to each air carrier's approved training program.

Section 121.423 details new extended envelope flight training and provides the interval for recurrent training. The FAA estimates that, for a certificate holder operating under part 121, 20 pages will be added to each air carrier’s training courseware, one page to each air carrier’s approved training program, and 20 pages to each air carrier’s flightcrew operating manual.

Section 121.424 revises revise current initial, transit ion and upgrade flight training curriculum/courseware to include flight training and evaluation, as appropriate. The FAA estimates that, for a certificate holder operating under part 121, 20 pages will be added to each61 air carrier’s training courseware, o ne page to each air carrier’s approved training program, and 20 pages to each air carrier’s pilots operating manual.

Section 121.433 has paperwork included in the § 121.423 cost estimate.

Compliance with t he extended envelope training maneuvers and procedures as well as the crosswind maneuvers with gusts and runway safety procedures, is requir e d 5 years and 120 days after date of publication of the final rule in the Federal Register.

Approval of Qualification Standards Document for Operators with AQ P (§ 121.909)

Although the final rule does not mak e any changes to § 121.909
, when the new N and O training requirements are published, operators that use AQP will have to review their training programs to make sure they address the new N and O requiremen ts ( r ecovery from s tall, u pset r ecovery,
etc

. ) and possibly revise their Qualifications Standards Document during this process.

This is a cost that only applies to operators that use AQP for pilot training because they are the only ones who must meet the § 121.909 requirements. This provision does not apply to operators who train their pilots under a traditional N and O training program

.

The FAA estimates that, for a certificate using AQP to conduct training , this provision will add 5 pages to each air carrier’s Qu alification S tandards D ocument. For each of the 22 operators, i t will take an instructor 9.6 hours and a tech writer 40.0 hours to complete the 5 pages required for this provision.

Summary of Esti mate d Paperwork Costs by Objective Grouping

The FAA estimates the total paperwork costs for the final rule will be about $ 8.2 million in 2012
dollars . Table 18 shows the details of the number of pages required for each objective grouping
of final rule p rovision s , the estimated date that the FAA believes paperwork costs will start to62 accrue, the number hours required for each provision, the person conducting the paperwork review, their salary, and the total costs for each provision. 56 For some of these pro visions, technical writers and instructors will both be needed to complete the paperwork requirements. We have reflected the labor costs of the technical writers and instructors for these provisions in separate rows for the objective groupings in Table 18.

56 In most cases, because the actual implementation will vary by operator, the FAA used the date on which compliance is required to estimate paperwork costs.63 1
Table 18 2 Summary of Paperwork Requirements and Costs ( 2012 $) 3

4 * Details may not add to row or column totals due to rounding. 564 Cost Summary

From 201 3 to 202 8
, the FAA estimates the base case costs to air carriers for complying with the provisions of this final rule are $ 3 13

. 9 million in constant 2012 dollars. The present value of the base case is $1 4 9. 8 million when discounted at a 7 percent annual rate and $ 2 2 6

. 1 million when discounted at 3 percent. As mentioned earlier, we estimate the base case costs using the average of the range of simulator training times required by the final rule.

Table 19 summarizes the FAA estimate of the final rule low range costs.

Table 19
Total Costs

– Low (2012 $)

* Details may not add to row or column totals due to rounding.

Table 20 summarizes the FAA estimate of the final rule base case costs.65 Table 20
Total Costs

– Base Case (2012 $)

Table 2 1 summarizes the FAA estimate of the final rule high range costs.

Table 21
Total Costs

– High (2012 $)

* Details may not add to row or column totals due to rounding.66 V I

. BENEFIT COST SUMMARY

This final rule will increase safety and contribute significantly to reducing the frequency of
future aviation accidents. Phased

- in potential quantified benefits will accrue from the additional training initiatives and shown in Table 23 below

.

The final rule will also gene rate qualitative benefits
, by addressing NTSB safety recommendations related to crewmember training
, and requirements in the Airline Safety and
Federal Aviation Administration Extension Act of 2010 (the 2010 Act)

. 57

Under the 2010 Act, Congress directed the FAA to conduct rulemaking to ensure that all flightcrew members receive ground training and flight training in recognizing and avoiding stalls, recovering from stalls, recognizing and avoiding upset of an aircraft, and the proper techniques to recover from upset. The 2010 Act also directed the FAA to ensure air carriers develop remedial training programs for flight crew members who have demonstrated performance deficiencies or experienced failures in the training environment.

The changes in this fin al rule address the following NTSB recommendations:

• A

- 96

- 120 . Require 14 CFR p art 121 and 135 operators to provide training to flightcrews in the recognition of and recovery from unusual attitudes and upset maneuvers, including upsets that occur while the aircraft is being controlled by automatic flight control systems, and unusual attitudes that result from flight control malfunctions and

u ncommanded flight control surface movements.

• A

- 05

- 14 . Require all 14 Code of Federal Regulations p art 121 air carrier operators to establish programs for flight crewmembers who have demonstrated performance deficiencies or experienced failures in the trai ning environment that would require a review of their whole performance history at the company and administer additional oversight and training to ensure that performance deficiencies are addressed and corrected

• A

- 05

- 30 . Require all 14 Code of Federal Reg ulations p art 121 and 135 air carriers to incorporate bounced landing recovery techniques in their flight manuals and to teach these techniques during initial and recurrent training

57 Public Law 111

- 216.67 • A

- 07

- 44 . Require that all 14 Code of Federal Regulations p art s 91K, 121, and 135 operators establish procedures requiring all crewmembers on the flight deck to positively confirm and cross

- check the airplane’s location at the assigned departure runway before crossing the hold short line for takeoff. This required guidance shoul d be consistent with the guidance in Advisory Circular 120

- 74A and Safety Alert for Operators 06013 and 07003.

• A

- 10

- 22 . Require 14 Code of Federal Regulations (CFR) p art 121,135, and 91K operators and 14 CFR Part 142 training centers to develop and conduc t training that incorporates stalls that are fully developed; are unexpected; involve autopilot disengagement; and include airplane

- specific features, such as a reference speeds switch.

• A

- 10

- 23 . Require all 14 Code of Federal Regulations p art 121, 135, an d 91K operators of stick pusher

- equipped aircraft to provide their pilots with pusher familiarization Simulator training.

• A

- 10

- 111 . Require 14 Code of Federal Regulations p arts 121, 135, and 91 K operators to incorporate the realistic, gusty crosswind profiles developed as a result of Safety Recommendation A

- 10

- 110 into their pilot simulator training programs.

Table 2 2 shows a summary of the costs in 2012 dollars , 7 and 3 perce nt present value

. The total costs include increased training for pilots, check pilots and flight instructors along with
additional costs of more simulator time and paperwork for updating curriculums and operating
manuals.

Table 2 2 Range of Total Costs ( 2012 $ Millions ) From 2019 to 2028

Table 2 3 shows t he final rule’s present value (using a 7% discount rate) quantitative benefit estimate of $ 317.1 million exceeds the present value quantitative base case cost estimate of $ 149.8 million to operators training their pilots under part 121

.68 Table 2 3 Summary of Benefits and Costs (2012 $ Millions) From 2019 to 2028

Thus, the FAA concludes that the benefits of the final rule justify the costs.69 V I I

. APPENDICES70 Appendix 1

– Accident Descriptions 

## Colgan 3407 (1) Accident Information

2

- 12

- 2009 NTSB Report Number: DCA09MA027 COLGAN 3407 Part 121 Scheduled Domestic Flight Bombardier DHC

- 8

- 40 2 Fatalites

- 50 (2) Summary of NTSB accident narrative related to rulemaking. On February 12, 2009, about 2217 eastern standard time, a Colgan Air, Inc., Bombardier DHC

- 8

- 400, N200WQ, operating as Continental Connection flight 3407, was on an instrument approach to Buffalo

- Niagara International Airport, Buffalo, New York, when it crashed into a residence in Clarence Center, New York, about 5 nautical miles northeast of the airport. The 2 pilots, 2 flight attendants, and 4 5 passengers aboard the airplane were killed, one person on the ground was killed, and the airplane was destroyed by impact forces and a post

- crash fire. The flight was operating under the provisions of 14 Code of Federal Regulations Part 121. Night visual meteorological conditions prevailed at the time of the accident. (3) NTSB causal factors. The NTSB determined that the probable cause of the accident was the c aptain’s inappropriate response to the activation of the stick shaker, which led to an aerodyna mic stall from which the airplane did not recover. Other contributing factors are: 1. T he flight crew’s failure to monitor airspeed in relation to the rising position of the low speed cue

. 2. T he flight crew’s failure to adhere to sterile cockpit procedures

. 3. T he captain’s failure to effectively manage the flight

. 4. Colgan Air’s inadequate procedures for airspeed selection and management during approaches in icing conditions.71 

## American Airlines 587

(1) Accident Information

11/12/2001 NTSB Report Number: DCA02MA001 American Airlines 587 Part 121 Scheduled International Flight Airbus A

- 300 Fatalites

- 265 (2) Summary of NTSB accident narrative related to rulemaking. On November 12, 2001, about 0916:15 eastern standard time, American Airlines flight 587, an Airbus Industrie A300

- 605R, N14053, crashed into a residential area of Belle Harbor, New York, short ly after takeoff from John F. Kennedy International Airport, Jamaica, New York. Flight 587 was a regularly scheduled passenger flight to Las Americas International Airport, Santo Domingo, Dominican Republic, with 2 flight crewmembers, 7 flight attendants, and 251 passengers aboard the airplane. The airplane's vertical stabilizer and rudder separated in flight and were found in Jamaica Bay, about 1 mile north of the main wreckage site. The airplane's engines subsequently separated in flight and were found se veral blocks north and east of the main wreckage site. All 260 people aboard the airplane and 5 people on the ground were killed, and the airplane was destroyed by impact forces and a post

- crash fire. In the immediate vicinity of the impact area, four home s were destroyed, three homes received substantial damage, and three homes received minor damage. In addition, the in

- flight separation of the engines resulted in property damage where the engines came to rest. A gas station received minor damage as a

resu lt of the impact of the left engine, and a home and a boat (parked in the driveway) received severe damage as a result of the impact of the right engine. Flight 587 was operating under the provisions of 14 Code of Federal Regulations Part 121 on an instrum ent flight rules flight plan. Visual meteorological conditions prevailed at the time of the accident. (3) NTSB causal factors. The National Transportation Safety Board determines that the probable cause of this accident was the in

- flight separation of the vertical stabilizer as a result of the loads beyond ultimate design that were created by the first officer’s unnecessary and excessive rudder pedal inputs. Contributing to these rudder pedal inputs were characteristics of the Airbus A300

- 600 rudder system design and elements of the American Airlines Advanced Aircraft Maneuvering Program.72 

## American Eagle 4184

(1) Accident Information

10/31/1994 NTSB Report Number: DCA95MA001 American Eagle Airlines 4184 Part 121 Scheduled Domestic Flight ATR 72 68

- Fatal ities (2) Summary of NTSB accident narrative related to rulemaking. On October 31, 1994, American Eagle flight 4184 Chicago's O'Hare International Airport (ORD) to Indianapolis, Indiana (IND) at 1559 crashed at 41 o 5' 40" north latitude and 87 o 19' 20" west longitude (near Roselawn, IN) during a rapid descent after an uncommanded roll excursion. The airplane was in a holding pattern and was descending to a newly assigned altitude of 8,000 feet when the initial roll excursion occurred. The airpla ne was destroyed by impact forces; and the captain, first officer, 2 flight attendants and 64 passengers received fatal injuries. Flight 4184 was a regularly scheduled passenger flight being conducted under 14 Code of Federal Regulations, Part 121; and an instrument flight rules flight plan had been filed. (3) NTSB causal factors. The NTSB determined that the probable cause was t he loss of control, attributed to a sudden and unexpected aileron hinge moment reversal that occurred after a ridge of ice accreted beyond the deice boots while the airplane was in a holding pattern during which it intermittently encountered supercooled cloud and drizzle/rain drops, the size and water content of which exceeded those described in the icing certification envelop e. The airplane was susceptible to this loss of control, and the crew was unable to recover. Other contributing factors are: 1. The French Directorate General for Civil Aviation's (DGAC's) inadequate oversight of the ATR 42 and 72, and its failure to take th e necessary corrective action to ensure continued airworthiness in icing conditions. 2. The DGAC's failure to provide the FAA with timely airworthiness information developed from previous ATR incidents and accidents in icing conditions. 3. the Federal Aviation A dministration's (FAA's) failure to ensure that aircraft icing certification requirements, operational requirements for flight into icing conditions, and FAA published aircraft icing information adequately accounted for the hazards that can result from flig ht in freezing rain. 4. The FAA's inadequate oversight of the ATR 42 and 72 to ensure continued airworthiness in icing conditions. 5. ATR's inadequate response to the continued occurrence of ATR 42 icing/roll upsets which, in conjunction with information learned about aileron control difficulties during the certification and development of the ATR 42 and 72, should have prompted additional research, and the creation of updated airplane flight manuals, flightcrew operating manuals and training programs related to operation of the ATR 42 and 72 in such icing conditions.73 

## USAir 427 (1) Accident Information

09/08/1994 NTSB Report Number: DCA94MA076 USAir 427 Part 121 Scheduled Domestic Flight Boeing B

- 737

- 300 Fatalites

- 132 (2) Summary of NTSB accident narrative related to rulemaking. On September 8, 1994, about 1903:23 eastern daylight time, USAir (now US Airways) flight 427, a Boeing 737

- 3B7 (737

- 300), N513AU, crashed while maneuvering to land at Pittsburgh International Airport, Pittsburgh, Pennsylvania. Flight 427 was operating under the provisions of 14 Code of Federal Regulations Part 121 as a scheduled domestic passe nger flight from Chicago

- O'Hare International Airport, Chicago, Illinois, to Pittsburgh. The flight departed about 1810, with 2 pilots, 3 flight attendants, and 127 passengers on board. The airplane entered an uncontrolled descent and impacted terrain near Aliquippa, Pennsylvania, about 6 miles northwest of the destination airport. All 132 people on board were killed, and the airplane was destroyed by impact forces and fire. Visual meteorological conditions prevailed for the flight, which operated on an ins trument flight rules flight plan. (3) NTSB causal factors. The National Transportation Safety Board determines that the probable cause of the USAir flight 427 accident was a loss of control of the airplane resulting from the movement of the rudder surfac e to its blow

- down limit. The rudder surface most likely deflected in a direction opposite to that commanded by the pilots as a result of a jam of the main rudder power control unit servo valve secondary slide to the servo valve housing offset from its neu tral position and over

- travel of the primary slide.74 

## Comair 5191

(1) Accident Information

08/27/2006 NTSB Report Number: DCA06MA064 COMAIR 5191 Part 121 Scheduled Domestic Flight Bombardier CL

- 600

- 2B19 Fatalites

- 49 (2) Summary of NTSB accident narrative related to rulemaking. On August 27, 2006, about 0606:35 eastern daylight time, Comair flight 5191, a Bomb ardier CL

- 600

- 2B19, N431CA, crashed during takeoff from Blue Grass Airport, Lexington, Kentucky. The flight crew was instructed to take off from runway 22 but instead lined up the airplane on runway 26 and began the takeoff roll. The airplane ran off the e nd of the runway and impacted the airport perimeter fence, trees, and terrain. The captain, flight attendant, and 47 passengers were killed, and the first officer received serious injuries. The airplane was destroyed by impact forces and postcrash fire. The flight was operating under the provisions of 14 Code of Federal Regulations Part 121 and was en route to Hartsfield

- Jackson Atlanta International Airport, Atlanta, Georgia. Night visual meteorological conditions prevailed at the time of the accident. (3) NTSB causal factors. The National Transportation Safety Board determines that the probable cause of this accident was the flight crewmembers’ failure to use available cues and aids to identify the airplane’s location on the airport surface during taxi and their failure to cross

- check and verify that the airplane was on the correct runway before takeoff. Contributing to the accident were the flight crew’s non

- pertinent conversation during taxi, which resulted in a loss of positional awareness, and the F ederal Aviation Administration’s (FAA) failure to require that all runway crossings be authorized only by specific air traffic control (ATC) clearances.75 

## Northwest 1482 (1) Accident Information

12/03/1990 NTSB Report Number: DCA91MA010A NORTHWEST AIRLINES 1482 Part 121 Scheduled Domestic Flight DC

- 9 Fatalites

- 8 (2) Summary of NTSB accident narrative related to rulemaking. On December 3, 1990, at 1345 EST, Northwest Flight1482, a DC

- 9 (N3313L) a regular schedule flight to Pittsburg Pa, and Northwest Flight 299, a Boeing 727 (N278US) a regular schedule flight to Memphis, collided near the intersection of runway 09 /27 and 03C/21C in dense fog at Detroit Metropolitan/Wayne County Airport, Romulus, MI. At the time of the collision, theB

727 was on its takeoff roll, and the DC

- 9 had just taxied onto the active runway. The B

- 727 was substantially damaged, and DC

- 9 was d estroyed. Seven of the 40 passengers and 1 crewmember aboard the DC

- 9 received fatal injuries. (3) NTSB causal factors. The NTSB found the probable cause of the accident was the l ack of proper crew coordination, including virtual reversal of roles by th e DC

- 9 pilots, which led to their failure to stop taxiing & alert ground controller of their positional uncertainty in a timely manner before & after intruding onto the active runway

. Other contributing factors include: 1. Deficiencies in ATC services provide d by Detroit tower, including failure of ground controller to take timely action to alert local controller to possible runway incursion, inadequate visual observation, failure to use progressive taxi instructions in low

- vis conditions, & issuance of inappr opriate & confusing taxi instructions compounded by inadequate backup supervision for level of experience of staff on duty. 2. Deficiencies in surface markings, signage & lighting at a i rp or t & failure of FAA surveillance to detect or correct any of these defi ciencies; 3. Failure of northwest airlines to provide adequate cockpit resource management training to line aircrews. 4. Contributing to fatalities was inoperability of DC

- 9 inte rnal tailcone release mechanism. 5. Co ntributing to number & severity of injuries was failure of crew of DC

- 9 to properly execute the passenger evacuation.76 

## Continental 1404 (1) Accident Information

12

- 20

- 2008 NTSB Report Number: DCA09MA021 Continental 1404 Part 121 Scheduled Domestic Flight Boeing B

- 737

- 500 Fatalites

- 0 (2) Summary of NTSB accident narrative related to rulemaking. On December 20, 2008, about 1818 mountain standard time, Continental Airlines flight 1404, a Boeing 737

- 500, N18611, departed the left side of runway 34R during takeoff from Denver International Airport (DEN), Denver, Colorado. A postcrash fire ensued. The captain and 5 of the 110 passengers were seriously injured; the first officer, 2 cabin crewmembers, and 38 passengers received minor injuries; and 1 cabin crewmember and 67 passengers (3 of who m were lap

- held children) were uninjured. The airplane was substantially damaged. The scheduled, domestic passenger flight, operated under the provisions of 14 Code of Federal Regulations Part 121, was departing DEN and was destined for George Bush Interco ntinental Airport, Houston, Texas. At the time of the accident, visual meteorological conditions prevailed, with strong and gusty winds out of the west. The flight operated on an instrument flight rules flight plan. (3) NTSB causal factors. The NTSB foun d that the probable cause of the accident was t he captain’s ceased rudder input, which was needed to maintain directional control of the airplane, about 4 seconds before the excursion, when the airplane encountered a strong and gusty crosswind that exceede d the captain’s training and experience. Other contributing factors include: 1. An air traffic control system that did not require or facilitate the dissemination of key, available wind information to the air traffic controllers and pilots 2. 'Inadequate crosswi nd training in the airline industry due to deficient simulator wind gust modeling77 

## FedEx 647 (1) Accident Information

12

- 18

- 2003 NTSB Report Number: DCA04MA011 FEDEX 647 Part 121 Scheduled Domestic Flight Boeing MD

- 10

- 10F Fatalites

- 0 (2) Summary of NTSB accident narrative related to rulemaking. On December 18, 2003, about 1226 central standard time, Federal Express Corporation (FedEx) flight 647, a Boeing MD

- 10

- 10F (MD

- 10), N364FE, crashed while landing at Memphis International Airport (MEM), Memphis , Tennessee. The right main landing gear collapsed after touchdown on runway 36R, and the airplane veered off the right side of the runway. After the gear collapsed, a fire developed on the right side of the airplane. Of the two flight crewmembers and five nonrevenue FedEx pilots on board the airplane, the first officer and one nonrevenue pilot received minor injuries during the evacuation. The post

- crash fire destroyed the airplane ’ s right wing and portions of the right side of the fuselage. Flight 647 departed from Metropolitan Oakland International Airport (OAK), Oakland, California, about 0832 (0632 Pacific standard time) and was operating under the provisions of 14 Code of Federal Regulations (CFR) Part 121 on an instrument flight rules flight plan. (3) NTSB causal factors. The NTSB probable cause findings: 1) T he first officer failed to properly apply crosswind landing techniques to align the airplane with the runway centerline and to properly arrest the airplane ’ s descent rate (flare) before the a irplane touched down; and 2) the captain failed to adequately monitor the first officer ’ s performance and command or initiate corrective action during the final approach and landing.78 

## Delta 1141 (1) Accident Information

08

- 31

- 1988 NTSB Report Number: DCA88MA072 DELTA 1141 Part 121 Scheduled Domestic Flight Boeing B

- 727

- 232 Fatalites

- 14 (2) Summary of NTSB accident narrative related to rulemaking. About 0901 central daylight time on August 31, 1988, Delta Air Lines, Inc., flight 1141, crashed shortly after lifting off from runway 18L at the Dallas

- Fort Worth International Airport, Texas. The airplane , a Boeing 727

- 232, U.S. Registry N473DA, was a regularly scheduled passenger flight and was en route to Salt Lake City, Utah, with 101 passengers and 7 crewmembers. The flightcrew reported that the takeoff roll appeared to be normal in all respects, with no warning lights, audible warnings, or unusual engine instrument conditions. The captain stated that the rotation was initially normal, but as the main gear wheels left the ground he heard "two explosions." He said it felt as though the airplane was exper iencing "reverse thrust." The captain stated that the airplane began to "roll violently." The airplane struck the instrument landing system (ILS) localizer antenna array approximately 1,000 feet beyond the end of runway 18L, and came to rest about 3,200 fe et beyond the departure end of the runway. The flight was airborne approximately 22 seconds from liftoff to the first ground impact near the ILS localizer antenna. The airplane was destroyed by impact forces and the post

- crash fire. (3) NTSB causal factors. The NTSB probable cause findings: (1) T he Captain and First Officer's inadequate cockpit discipline which resulted in the flightcrew's attempt to takeoff without the wing flaps and slats properly configured; and (2) the failure of the takeoff configuration warning system to alert the crew that the airplane was not properly configured for the takeoff. Other contributing factors include: 1. Delta's slow implementation of necessary modifications to its operating procedures, manual's, che cklists, training, and crew checking programs which were necessitated by significant changes in the airline following rapid growth and merger. 2. 'The lack of sufficiently aggressive action by the FAA to have known deficiencies corrected by Delta and the lack of sufficient accountability within the FAA's air carrier inspection process.79 

## Corporate 5966 (1) Accident Information

10/19/2004 NTSB Report Number: DCA05MA004 CORPORATE 5966 Part 121 Scheduled Domestic Flight British Aerospace BAE

- J3201 Fatalites

- 13 (2) Summary of NTSB accident narrative related to rulemaking. On October 19, 2004, about 1937 central daylight time, Corporate Airlines (doing business as American Connection) flight 5966, a BAE Systems BAE

- J3201, N875JX, struck trees on fina l approach and crashed short of runway 36 at Kirksville Regional Airport (IRK), Kirksville, Missouri. The flight was operating under the provisions of 14 Code of Federal Regulations (CFR) Part 121 as a scheduled passenger flight from Lambert

- St. Louis Inte rnational Airport (STL), in St. Louis, Missouri, to IRK. The captain, first officer, and 11 of the 13 passengers were fatally injured, and 2 passengers received serious injuries. The airplane was destroyed by impact and a post

- impact fire. Night instrument meteorological conditions (IMC) prevailed for the flight, which operated on an instrument flight rules (IFR) flight plan. (3) NTSB causal factors. The pilots' failure to follow established procedures and properly conduct a non

- precision instrument appro ach at night in IMC, including their descent below the minimum descent altitude (MDA) before required visual cues were available (which continued un

- moderated until the airplane struck the trees) and their failure to adhere to the established division of d uties between the flying and nonflying (monitoring) pilot. Contributing to the accident was (1) the pilots' failure to make standard callouts and the current Federal Aviation Regulations that allow pilots to descend below the MDA into a region in which saf e obstacle clearance is not assured based upon seeing only the airport approach lights , (2) t he pilots' failure to establish and maintain a professional demeanor during the flight , and (3) the pilots’ fatigue likely contributed to their degraded performanc e.80 

## USAir 5050 (1) Accident Information

09

- 20

- 1989 NTSB Report Number: DCA89MA074 USAir 5050 Part 121 Scheduled Domestic Flight BOEING B

- 737

- 400 Fatalites

- 2 (2) Summary of NTSB accident narrative related to rulemaking. On September 20, 1989, USAir, Inc. flight 5050 was departing New York City's LaGuardia Airport, Flushing, New York, for Charlotte Douglas International Airport, Charlotte, North Carolina. As the first officer began the takeoff on runway 31, he felt the airplane drift left. The captain noticed the left drift also and used the nosewheel tiller to help steer. As the takeoff run progressed, the aircrew heard a "bang" and a continual rumbling noise. The captain then took over and rejected the takeoff but did not stop the airplane before running off the end of the runway into Bowery Bay. Instrument flight conditions prevailed at the time and the ru nway was wet. (3) NTSB causal factors. The captain's failure to exercise his command authority in a timely manner to reject the takeoff or take sufficient control to continue the takeoff, which was initiated with a mistrimmed rudder. Also causal was the captain's failure to detect the mistrimmed rudder before the takeoff was attempted.81 Appendix 2

– Historical Accidents82 Appendix 3 Historical Accidents Probable Cause(s), Contributing Factors, and Relevant Provisions of
Final Rule838485 Appendix 4

– Value of S tatistical Life (VSL)

Appendix 4, Table 1 Estimated Value of Preventing Fatalities and Injuries (2012 $ )

Appendix 4, Table 2 Estimated Value of Preventing Fatalities and Injuries (2012 $ )86 Appendix 5

– Fatalities, Injuries, and Quantified Benefit

- Sensitivity Analysis

Our estimate of future benefit s incorporates information related to the rule’s expected impacts on the aviation system looking forward in order to appropriately value the reduction in future risks. However, as a test of the sensitivity of our benefits estimates using this approach, we also include an analysis assuming that the exact number of fatalities and injuries as actually occurred in each historical accident would occur in a potential future accident. The details and results of
th e calculations for the sensitivity follow

. Appendix 5, Table 1 Actual Fatalities and Injuries from Historical Accidents

- Sensitivity Analysis

Append ix 5, Table 2 Valuation of Actual Fatalities and Injuries for Historical Accidents (2012 $) Sensitivity Analysis87 * Details may not add to row or column totals due to rounding.88 Appendix 5, Table 3 Single Year Benefits of Final Rule (Actual Fatalities and Injuries) (2012 $) Sensitivity Analysis

* Details may not add to row or column totals due to rounding. Appendix 5, Table 4 Total Benefits of Final Rule (Actual Fatalities and Injuries) (2012 $)

- Sensitivity Analysis

* Details may not add to row or column totals due to rounding.8990 Appendix 6
Table 1: Expected Value of a Typical Part 121 Passenger Aircraft During Benefits Period91 Appendix 6
Table 2 : Average Value of Most Frequently Used Cargo Aircraft (Jan

- Oct 2012 T

- 100 Segment Data for Part 121 Cargo Only Operations)92 Appendix 7 Unit Values for Benefit Analysis93 Appendix 8 Part 121 Carriers in T

- 100 Segment Data (US Carriers) (Jan 2012

- Oct 2012)94 Appendix 9
Part 121 and 121 /135 Pilot Employment February 201 395 Appendix 10 Sensitivity Analysis on Pilots Spending an Extra Day in Training

As a sensitivity analysis, the FAA estimated the travel cost s of pilots spending an extra day in simulator training for the additional tasks added by the final rule. Since t ravel costs incl ude hotel, airfare or automobile mileage, and per diems (meals, etc.)
, the airfare or automobile mileage has already occurred. Therefore, the only remaining travels costs are for the final rule are for hotel and per die m costs. The FAA notes that the pil ots ’ salary has already been
estimated and included in the costs above.

We used the same hotel and per diem costs we used in the SNPRM r egulatory e valuation. The
FAA notes that n o comments were received on our SNPRM estimates for hotel and per diem

costs

.

Based on the locations of the flight simulators and training centers, and the corresponding per diem rates for those locations, the FAA assumes that the weighted averages for lodging and meals are $92 and $44, respectively. 58 Per Diem cost (i.e., lodgi ng and meals) rates are based on rates established annually by the General Services Administration (GSA) for travelers on official Government business to use for their lodging, meals, and incidental expenses.

We estimated the additional day of travel co sts by taking the product of the number of pilots in simulator training with the sum of hotel and per diem . We perform this calculation for pilots in initial, upgrade, transition , and recurrent training and then sum the results.

The following table show s our cost estimate for an additional day in simulator training

.

58 Includes incidental expenses.96 Appendix 10
Table 1 : Cost of an Additional Day in Pilot Simulator Training

The FAA estimates the total travel cost for an extra day would be about $ 61.4 million in 2012
dollars ($ 29.4 million at a seven percent present value and $ 44.3 million at a three percent present value).

Even if pilots would have to travel an extra day for in order to complete the additional simulator training tasks the final rule adds, the final rule woul d be cost beneficial.97 Appendix 11 Low and High Estimated Simulator Costs by Pilot, Check Pilot, and Flight Instructor ( 2012 $ )

* Details may not add to row or column totals due to rounding.98 Appendix 12
Estimated Ground School Costs by Pilot, Check Pilot, and Flight Instructor ( 2012 $ )

* Details may not add to row or column totals due to rounding.99 Appendix 13
The Probability of Effectiveness Ratings of Overlapping Accidents For the Following Final Rules: Flightcrew Member Duty and Rest Requirements , The Pilot Certification and Qualification Requirements , and Qualification, Service, and Use of Crewmembers and Aircraft Dispatchers

The FAA notes that for future related final rules, the total probability of effectiveness will not exceed 100% for any accident.100 Appendix 14 Sensitivity Analysis on 10 Year Historical Accident Analysis Period for Benefits Estimation

The FAA reviewed accident data for U.S. certificate holders required to train under part 121 over
the 22

- year interval from 1988 through 2009. The objective of the analysis was to determine if an accident could have been prevented or mitigated by the trai ning provisions in the final rule. In 1988, Delta flight 1141, crashed shortly after lifting off from the runway at the Dallas

- Fort Worth International Airport (DCA88MA072). In their final report, the NTSB determined that
one causal factor for the accide nt was “ The captain and first officer’s inadequate cockpit discipline which resulted in the flightcrew’s attempt to takeoff without wing flaps and slats properly configured.” The FAA determined that the pilot monitoring training provisions in the
final rul e may have prevented or mitigated this accident. The FAA initiated the historical accident interval for the benefits analysis with this accident.

Over the next 22 year historical accident interval, the FAA identified accidents with casual
factors identifi ed by the NTSB that are addressed by the provisions in the final rule. The FAA cited these accidents based on pertinent accident causal factors, regardless of whether there were open NTSB recommendations associated with those accidents

.

We have explore d the effect of reduc ing the historical analysis period from 2 2 years to 10 years
here in response to comments disputing the use of a 2 2

- year time frame for accidents . These

comments stat e the accident rate has declined over time so using older accidents is not appropriate

. As a result of reducing the historical analysis period to 10 years from 2000 to 2009,
the number of relevant accidents is reduced from eleven to six. The 22

- year historical period had

an accident rate of 0.5 a ccidents per year
, while the 10 year historical period had a slightly higher
rate of 0.6 accidents per year

.101 Table 1 Accidents During 10 Year Period (2000

- 2009)

Table 2, below, is adapted from Table 7 of this regulatory evaluation to cover just thos e accidents that occurred during the 10 year historical period. Table 3 is similar to Table 9 of this regulatory evaluation and shows those single year benefits grown to account for industry growth and also displays the present value of the benefits over t he future analysis period when discounted at both the seven percent and three percent rates as recommended in OMB Circular
A

- 4. Using a 10

- year historical analysis period rather than the 22

- year period increases the
estimate d benefits by approximately 17 percent. The total estimated benefit of the final rule using the 10

- year historical analysis period is $ 803 million in 2012 dollars
, compared to $689 million when using the 22

- year historical analysis period . Th e stream of benefits estimated using
the 10

- year historical analysis period has a present value of $ 370 million when discounted at seven percent and $ 570 million when discounted at three percent
, compared to $317 million and $489 million respectively when estimated using the 22

- year historical analy sis period. Carrier Flt# Date State of Accident Aircraft Fatalities Serious Injury Minor Injury People on Board Effectiveness Rating for Final Rule
American 587 11/12/2001 NY A300B4-605R 265 0 0 260 0.25 FedEx 647 12/18/2003 TN MD-10-10F 0 0 2 7 0.35 Corporate 5966 10/19/2004 MO Jetstream 32 13 2 0 15 0.05 COMAIR 5191 8/27/2006 KY CRJ-100ER 49 1 0 50 0.15 Continental 1404 12/20/2008 CO B737-500 0 6 41 115 0.25 Colgan 3407 2/12/2009 NY DHC-8-402 50 0 0 49 0.20 10 Year Total 377 9 43 496102 Table 2 Single Year Benefits of Final Rule for 10 Year Period (2012 $)

Table 3
Total Benefits of Final Rule for 10 Year Period (2012 $) Carrier Flt# Effectiveness Rating Benefits from Avoided Fatalities and Injuries Other Benefits American 587 25% $213,850,000 $5,566,850 FedEx 647 35% $19,110 $10,683,750 Corporate 5966 5% $35,795,740 $1,060,000 COMAIR 5191 15% $119,135,370 $3,180,000 Continental 1404 25% $1,803,275 $2,775,000 Colgan 3407 20% $163,800,000 $4,266,320 $534,403,495 $27,531,920 $53,440,350 $2,753,192 Total benefit over 10 year history Per year benefit

Total Benefits Total Discounted at 7% Total Discounted at 3% 0 2012 1 2013 2 2014 3 2015 4 2016 5 2017 6 2018 7 2019 $66,586,953 $3,076,692 $69,663,645 $43,379,552 $56,643,510 8 2020 $68,717,985 $3,125,974 $71,843,959 $41,813,184 $56,713,621 9 2021 $70,908,550 $3,176,082 $74,084,632 $40,294,631 $56,778,462 10 2022 $73,172,734 $3,226,741 $76,399,475 $38,833,853 $56,848,849 11 2023 $75,505,580 $3,278,501 $78,784,081 $37,430,317 $56,913,620 12 2024 $77,914,525 $3,330,812 $81,245,337 $36,072,930 $56,985,479 13 2025 $80,408,150 $3,384,224 $83,792,374 $34,773,835 $57,062,607 14 2026 $82,975,142 $3,438,461 $86,413,603 $33,511,195 $57,128,033 15 2027 $85,623,197 $3,493,250 $89,116,447 $32,295,800 $57,203,847 16 2028 $88,353,957 $3,549,140 $91,903,097 $31,127,579 $57,274,010 Total $770,166,773 $33,079,877 $803,246,650 $369,532,876 $569,552,038 Year Calendar Year Benefits from Avoided Fatalities and Injuries Other Benefits Total Benefits103 Appendix 15 Sensitivity Analysis on Inclusion of AA 587 Accident in Historical Accident Analysis for Benefits Estimation

As explained in the “Accident Populatio n and Scoring” section of the RIA benefits and the “Background” section of the Preamble
, the accident involving American Airlines 587 was added to analysis of historical accidents subsequent to the NPRM. The AA 587 accident resulted in the deaths of all 260 people on board and an additional 5 people on the ground. The FAA Accident Investigati on and Prevention Group (AVP) assigned an effectiveness rating of 0.25 to this
accident.

Because this catastrophic accident was added to the benefits analysis for the final rule, the FAA feels it is worthwhile to present a sensitivity analysis exploring t he impact on the benefits estimates of not including that accident.

Table 1, below, is adapted from Table 7 of this regulatory evaluation but removes AA 587 from the calculations. Table 2 is similar to Table 9 of this regulatory evaluation and shows thos e single year benefits grown to account for industry growth and also displays the present value of the benefits over the future analysis period when discounted at both the seven percent and three percent rates as recommended in OMB Circular A

- 4.

Removin g AA 587 from the benefits analysis decreases the estimated benefits by approximately 26 percent. However, the benefits estimate without AA 587 still exceeds the costs of the final rule by a significant margin.104 Table 1
Sin gle Year Benefits of Final Rul e, Omitting AA 587 (2012 $)

Table 2
Total Benefits of Final Rule , Omitting AA 587 (2012 $) Carrier Flt# Effectiveness Rating Benefits from Avoided Fatalities and Injuries Other Benefits Colgan 3407 20% $163,800,000 $4,266,320 American Eagle 4184 20% $161,980,000 $4,240,000 USAir 427 20% $161,980,000 $4,240,000 COMAIR 5191 15% $119,135,370 $3,180,000 Northwest 1482 50% $86,202,450 $6,232,500 Continental 1404 25% $1,803,275 $2,775,000 FedEx 647 35% $19,110 $10,683,750 Delta 1141 35% $47,930,820 $3,885,000 Corporate 5966 5% $35,795,740 $1,060,000 USAir 5050 50% $16,527,050 $5,550,000 $795,173,815 $46,112,570 $36,144,264 $2,096,026 Total benefit over 22 year history Per year benefit

Total Present Value at 7% Present Value at 3% 0 2012 1 2013 2 2014 3 2015 4 2016 5 2017 6 2018 7 2019 $45,035,940 $2,342,309 $47,378,249 $29,502,436 $38,523,254 8 2020 $46,477,259 $2,379,828 $48,857,087 $28,434,825 $38,567,784 9 2021 $47,958,843 $2,417,976 $50,376,819 $27,399,952 $38,608,794 10 2022 $49,490,219 $2,456,542 $51,946,761 $26,404,539 $38,653,585 11 2023 $51,068,034 $2,495,948 $53,563,982 $25,448,248 $38,694,621 12 2024 $52,697,319 $2,535,772 $55,233,091 $24,523,492 $38,740,490 13 2025 $54,383,877 $2,576,435 $56,960,312 $23,638,529 $38,789,972 14 2026 $56,120,056 $2,617,727 $58,737,783 $22,778,512 $38,831,548 15 2027 $57,911,062 $2,659,438 $60,570,500 $21,950,749 $38,880,204 16 2028 $59,758,006 $2,701,987 $62,459,993 $21,155,200 $38,925,068 Total $520,900,615 $25,183,962 $546,084,577 $251,236,482 $387,215,320 Other Benefits Total Benefits

Year Calendar Year Benefits from Avoided Fatalities and Injuries105 As shown in Table 3 and 4 below, omitting AA 587 from the 10 year benefits history explored in Appendix 14 also does not impact the central conclusion that the e stimated benefits of the final rule exceed the costs by a wide margin.
Table 3 Single Year Benefits of Final Rule for 10 Year Period, Omitting AA 587 (2012 $)

Table 4
Total Benefits of Final Rule for 10 Year Period, Omitting AA 587 (2012 $) Carrier Flt# Effectiveness Rating Benefits from Avoided Fatalities and Injuries Other Benefits FedEx 647 35% $19,110 $10,683,750 Corporate 5966 5% $35,795,740 $1,060,000 COMAIR 5191 15% $119,135,370 $3,180,000 Continental 1404 25% $1,803,275 $2,775,000 Colgan 3407 20% $163,800,000 $4,266,320 $320,553,495 $21,965,070 $32,055,350 $2,196,507 Total benefit over 10 year history Per year benefit

Total Benefits Total Discounted at 7% Total Discounted at 3% 0 2012 1 2013 2 2014 3 2015 4 2016 5 2017 6 2018 7 2019 $39,941,132 $2,454,597 $42,395,729 $26,399,820 $34,471,967 8 2020 $41,219,398 $2,493,914 $43,713,312 $25,441,148 $34,507,288 9 2021 $42,533,374 $2,533,890 $45,067,264 $24,512,085 $34,539,551 10 2022 $43,891,509 $2,574,306 $46,465,815 $23,618,574 $34,575,213 11 2023 $45,290,830 $2,615,601 $47,906,431 $22,760,345 $34,607,606 12 2024 $46,735,798 $2,657,334 $49,393,132 $21,930,551 $34,644,343 13 2025 $48,231,559 $2,699,946 $50,931,505 $21,136,575 $34,684,355 14 2026 $49,771,329 $2,743,218 $52,514,547 $20,365,141 $34,717,367 15 2027 $51,359,722 $2,786,928 $54,146,650 $19,622,746 $34,756,735 16 2028 $52,997,726 $2,831,517 $55,829,243 $18,909,365 $34,792,784 Total $461,972,377 $26,391,251 $488,363,628 $224,696,350 $346,297,209 Year Calendar Year Benefits from Avoided Fatalities and Injuries Other Benefits Total Benefits