## ATTACHMENT B

## DRAFT-STATEMENT OF WORK

ENGINE MAINTENANCE SUPPORT

FAA-owned Pratt Whitney (P&W)

PT6A-60A

## C.1.1 INTRODUCTION

The Federal Aviation Administration has a continuing requirement for
engine maintenance of FAA-owned flight inspection aircraft consisting of
overhaul/repair in support of aircraft operating in various locations
throughout the world.

## C.1.2. BACKGROUND

\(a\) The FAA owned PTA-60A engines to be covered under a Power by the
Hours bases identified in the following chart. Appendix A exhibits the
status of the engines and their assigned location.

## C.1.3. SCOPE

The objective of this requirement is to acquire support of the FAA-owned
Pratt Whitney (P&W) engines cited in C.1.2 above and if needed on an
exception basis, drop-in maintenance, if ordered, for FAA customer and
other FAA engines. The P/H engines are maintained based on estimated
actual engine hours flown during each calendar month/year. Customer or
FAA engines not cited in C1.2 are maintained under a time and material
basis based on the required repair and at the negotiated labor rates
identified in the contract at time of maintenance. This support includes
Hot Section Inspections (HSI), overhaul (OH), Major Periodic Inspection
(MPI), Compressor Zone Inspection (CZI) (including test cell run),
Unscheduled Engine Maintenance, and implementation of recommended
Service Bulletins (SBs), Airworthiness Directives (ADs), engine
accessories, life-limited parts, contractor furnished loaned engines,
and applicable shipping, as required, to maintain airworthiness of
Federal Aviation Administration (FAA) flight inspection aircraft.
Preventative maintenance of P/H engines will be performed by FAA
personnel or by third party contractors.

## 

## C.1.4. DEFINITIONS

\(a\) [Airworthiness Directive (AD)]{.underline} - An AD is issued by
the Federal Aviation Administration in response to a safety-of-flight
problem occurring in-service for a specific type of aircraft. It is a
mandatory directive for commercial aircraft, which specifies the
conditions and limitations, if any, under which the aircraft type may
continue to be operated. The AD carries a compliance date plus flight
hours and/or cycles that must be complied with to maintain the FAA
Airworthiness Certificate (AC).

\(b\) [Bench Stock]{.underline} - Expendable items, which are not
requisitioned on an individual basis, but are bought in bulk when a
reorder level is reached.

\(c\) [Calibration]{.underline} - A comparison between two instruments,
one of which is a standard of known accuracy, to detect and correlate,
or adjust, any variation in the accuracy of the instrument being
compared.

\(d\) [Component]{.underline} - A separate identifiable part of an end
item which performs a function within the system or subsystem necessary
for the proper operation of that end item.

\(e\) [Compressor Zone Inspection (CZI)]{.underline} - (including test
cell run) - an inspection recommended at intervals of engine operation
per the light maintenance manual.

\(f\) [Contracting Officer's Technical Representative
(COTR)]{.underline} - the Contracting Officer may designate other
Government personnel to act as his or her authorized representative for
contract administration functions which do not involve changes to the
scope, price, schedule, or terms and conditions of the contract. The
designation will be in writing, signed by the Contracting Officer, and
will set forth the authorities and limitations of the representative(s)
under the contract. Such designation will not contain authority to sign
contractual documents, order contract changes, modify contract terms, or
create any commitment or liability on the part of the Government
different from that set forth in the contract.

\(g\) [Drop-in Maintenance]{.underline} - On a Time and material basis
for maintenance of other FAA or customer engines. The exact engine type
and overhaul schedule are unknown by the FAA prior to and at the time of
award and may vary throughout the life of this contract. This
maintenance is performed on a time-and-material basis under Section
B**,** (CLIN To be determined). Although there is no inherent incentive
to the contractor to minimize the turnaround time for drop-in
maintenance, the FAA is not bound by any other contract terms for
drop-in maintenance if it is not commensurate with similar P/H engine
maintenance turnaround times.

\(h\) [Engine Accessories]{.underline} - a mechanism or device employed
to facilitate or increase the effective use of the engine. Attachment 2,
Appendix B, exhibits the engine accessories covered under the P/H rate
(Section B, Item 1.0 & 2.0) when maintenance is performed at the
contractor's facility.

\(i\) [FAR]{.underline} - Federal Aviation Regulation

\(j\) [Flight Time Accounting]{.underline} - the time from the moment
the aircraft first moves under its own power for the purpose of flight
until the moment it comes to rest at the next point of landing.

\(k\) [Hot Section Inspection (HSI)]{.underline} - an inspection to
determine performance of HSI components, inner/outer combustion liner,
compressor turbine disk assembly, and small exit duct.

\(l\) [Inventoried Spare Engines]{.underline} - FAA-owned
repairable/serviceable engines.

\(m\) [Life Limited Parts]{.underline} - serviceable parts designated by
the item manufacturer as having limited life in use (either hours or
cycles). Such parts may be used since last overhaul and restored to a
condition meeting the established overhaul tolerances and limits. Such
parts must have sufficient time (hours and cycles) remaining to allow
use in service until the next major maintenance period is reached for
the engine in which installed or intended for installation.

\(n\) [Loan Engines]{.underline} - Contractor-owned serviceable engines
used on aircraft when FAA-owned serviceable spare engines are not
available.

\(o\) [Major Periodic Inspection (MPI)]{.underline} - an inspection
recommended at intervals of engine operation per the light maintenance
manual.

\(p\) [Overhaul]{.underline} - The disassembly, cleaning, inspection,
repair, rework, replacement of parts or components, reassemble and test
of any item or accessory in accordance with applicable technical
manuals, directives, or authorized manufacturer's publications to
provide an operationally safe, serviceable, and reliable item.

\(q\) (RESERVED)

\(r\) [Repair]{.underline} - the restoration or replacement of parts,
components, or material as necessitated by wear and tear, damage, or
failure of parts, or the like, in order to maintain the specific item or
material in efficient operating condition.

\(s\) [Repairable]{.underline} - an unserviceable item that can be
repaired and restored to a serviceable condition.

\(t\) [Replace]{.underline} - the replacement of items that are
determined to be beyond economical repair (IAW FAR 43).

\(u\) [Scheduled Maintenance]{.underline} - that maintenance which is
deemed necessary to be accomplished at prescribed intervals.

\(v\) [Service Bulletin (SB)]{.underline} - a document issued to all
customers recommending an inspection and possible repair to the engine.
SBs can carry a recommended time compliance by the manufacturer.

\(w\) [Serviceable]{.underline} - capable of meeting the requirement and
performing the function for which designed or modified, and meets all
test requirements established by the work specification.

\(x\) [Unscheduled Maintenance]{.underline} - maintenance, other than
scheduled (overhaul, HSI, MPI, CZI, etc.), that requires engine or major
module removal and repair at an authorized engine repair facility. This
requirement refers to unscheduled maintenance in two scenarios -
contractor responsibility and FAA responsibility. Maintenance required
due to contractor performed engine maintenance failures, distinguished
as those which would require the removal of an engine or major module,
is the contractor's responsibility and is covered under the P/H rate.
Maintenance required due to misuse by the FAA operator, incurrence of
FOD or Acts of God which are not repairable by the on-site FAA
maintenance staff, is the FAA's responsibility and is covered by a
separate contract line item.

\(y\) [AMS]{.underline} - FAA Acquisition Management System

\(z\) PHASE IN/OUT \-- Contractor shall provide 30 calendars prior and
post contract for a phase in and phase out of the contract performance
period at no additional cost. This time is for the administrative and
management needs to get in place the security paper work for personnel
employee identification, change in/out of badges, all administrative
things that have to take please so that on the start date/end date a
smooth conversion between going in and going out contractor\'s can be
accomplished.

## C.1.5. SCHEDULED MAINTENANCE

\(a\) The repair facility shall perform all scheduled maintenance
"except for preventative maintenance" overhaul of engines and
accessories, MPI, CZI, and HSI in compliance with SOW Paragraph
C1.8.0(e).

\(b\) If requested by the COTR, the contractor shall provide, at no
additional cost, an engine on loan for the FAA's use while the removed
engine undergoes overhaul, repair and/or MPI/CZI. Loan engines will only
be requisitioned by the FAA when FAA-owned serviceable spare engines are
not available.

## C.1.6. UNSCHEDULED MAINTENANCE

\(a\) Any unscheduled maintenance requiring engine removal/major module
removal for repair at an authorized facility, not including maintenance
resulting from operator misuse, acts of God, or incurrence of FOD, shall
be covered under the P/H rate.

\(b\) Unscheduled maintenance requirements, not cited in C.6(a) above,
and those resulting from misuse by the FAA operator, incurrence of FOD
and Acts of God which are not repairable by the on-site FAA maintenance
staff, are covered under Section B, Item 3.0.

\(c\) If requested by the COTR, the contractor shall provide an engine
on loan for the FAA's use while the removed engine undergoes overhaul or
repair. Loan engines will only be requisitioned by the FAA when
FAA-owned serviceable spare engines are not available.

\(d\) To ensure agreement between the contractor and the FAA concerning
the responsibility of unscheduled maintenance, the contractor shall
immediately notify the COTR on all actions which the contractor
determines not to be covered under the P/H program. The COTR will
inspect the damage and, if agreed, will authorize maintenance under
Section B, Item 3.0, or provide for disposition of the item.

## C.1.7 SERVICE BULLETINS

The repair facility shall incorporate Pratt & Whitney and Garrett
Service Bulletins in accordance with the following schedule:

\(a\) Recommended Service Bulletins. Recommended SBs shall be performed
concurrently with other work under the P/H rate as approved by the FAA.

\(b\) Optional Service Bulletins. Compliance is at the FAA's discretion.
The cost of parts and additional labor are chargeable to Section B,
(Item to be determined). Upon receipt of a request for estimate from the
COTR, the contractor is responsible for preparing and providing a cost
estimate for the additional labor and parts required to incorporate the
optional SB in relation to the prescribed standard hours. The FAA will
elect whether to enter into negotiations for the incorporation of the SB
based on this cost estimate and other factors and, if so, will authorize
performance after negotiations.

## C.1.8 CONTRACTOR QUALIFICATIONS

\(a\) All work performed under this requirement shall be performed by
Federal Aviation Administration (FAA) approved repair station
certificate holders that, at a minimum, hold the following ratings or
limited ratings:

Power plant Class 3 or Limited Rating for Pratt & Whitney PT6A-21
PT6A-41 and PT6A-135 engines. (Drop in maintenance requirements shall be
performed only by repair facilities holding FAA approved repair station
certificates for those engine types.)

\(b\) Under those ratings listed above, the repair station certificate
holder shall possess and maintain operations specification certification
that authorize the contractor to perform the following functions:

\(1\) Overhaul and internal repair of the PT6A-21 PT6A-41 and PT6A-135
engines engines.

\(2\) Overhaul and repair of basic engine accessories.

\(c\) The repair facility may subcontract other functions not authorized
by their operations specification certification to include:

\(1\) Repair and coating of internal engine components such as the vane
ring, ducts and liners.

\(2\) Repair and overhaul of other engine accessories not identified
above. Should a vendor who is not a certificated repair station perform
these subcontract functions, the repair facility must have a documented
system in place to determine the airworthiness of the article by either
inspection or test.

\(d\) Prior to award of a contract, the FAA will audit the repair
facility, at their facility, to ensure these quality standards are
available. The repair facility shall be subject to routine periodic
audits throughout the term of the contract to ensure these quality
standards are maintained and adhered to.

\(e\) The contractor shall comply with FAR, the FAA General Maintenance
Manual, the manufacturers' specifications, recommendations, and repair
instructions.

\(f\) Engine maintenance shall be performed at one location for each
engine type except for the subcontracted functions cited in subparagraph
(c) above.

## C.1.9. DELIVERABLES

\(a\) The contractor shall certify to the FAA, with supporting
documentation, that each engine and accessory overhaul, repair and
inspection was accomplished in compliance with the current
manufacturers' specifications, manuals, and/or operating specifications
in accordance with FAA instructions. The supporting documentation shall
be provided to the COTR at the following intervals:

\(1\) immediately following induction of engine

\(2\) immediately following completion of initial inspection

\(3\) immediately following completion of final inspection

\(b\) This documentation shall, at a minimum, contain the following
information:

(The contractor shall utilize the company's standard format, modifying
only as necessary to include elements cited herein which are not
otherwise included in the pre-existing format. The COTR shall review and
approve the format.)

\(1\) the FAA contract number (DTFAAC-08-D-\_\_\_\_\_\_\_\_), cited in
block 2, page 1 of this contract;

\(2\) Contractor issued work order identifying, by serial number,
component being overhauled;

\(3\) Dimensional check data;

\(4\) Replacement parts list;

\(5\) Repair data;

\(6\) Reassembly/test data;

\(7\) Rationale for determination of unserviceable condition, including
reference to overhaul/repair specifications;

\(8\) Complete status of life-limited components, as applicable;

\(9\) Summary of Airworthiness Directive compliance, as applicable;

\(10\) Summary of Service Bulletin compliance, as applicable;

\(11\) Documentation supporting any major repair and/or alteration, as
applicable;

\(12\) Maintenance Release returning the engine to service.

This needs to be incorporated into a Contractor Data Requirements List
(CDRL)

Appendix A

ENGINE STATUS REPORT

## 

<table>
<colgroup>
<col style="width: 9%" />
<col style="width: 8%" />
<col style="width: 5%" />
<col style="width: 10%" />
<col style="width: 5%" />
<col style="width: 8%" />
<col style="width: 11%" />
<col style="width: 5%" />
<col style="width: 8%" />
<col style="width: 8%" />
<col style="width: 7%" />
<col style="width: 10%" />
</colgroup>
<tbody>
<tr class="odd">
<td colspan="12"><strong>ENGINE STATUS REPORT BEECH 300</strong></td>
</tr>
<tr class="even">
<td colspan="12"><strong>MODEL: PT6A-60A</strong></td>
</tr>
<tr class="odd">
<td></td>
<td> </td>
<td> </td>
<td> </td>
<td> </td>
<td> </td>
<td> </td>
<td> </td>
<td> </td>
<td> </td>
<td> </td>
<td></td>
</tr>
<tr class="even">
<td>Data as of</td>
<td>01/02/08</td>
<td> </td>
<td> </td>
<td> </td>
<td> </td>
<td><table>
<colgroup>
<col style="width: 100%" />
</colgroup>
<tbody>
<tr class="odd">
<td> </td>
</tr>
</tbody>
</table></td>
<td colspan="3"><strong>NEXT MAINT DUE</strong></td>
<td> </td>
<td></td>
</tr>
<tr class="odd">
<td>ACFT</td>
<td>A/C Hours</td>
<td>POS</td>
<td>SERIAL NUMBER</td>
<td>TSO</td>
<td>TSHSI</td>
<td>TSN</td>
<td>Type</td>
<td>A/C Hr.</td>
<td>Eng. Hr.</td>
<td>TTG</td>
<td></td>
</tr>
<tr class="even">
<td>N66</td>
<td>10843.1</td>
<td>L/H</td>
<td>PCE95358</td>
<td>672.6</td>
<td>672.6</td>
<td>9753.9</td>
<td>O/H</td>
<td>15670.5</td>
<td>14581.3</td>
<td>4827.4</td>
<td></td>
</tr>
<tr class="odd">
<td> </td>
<td>10843.1</td>
<td>R/H</td>
<td>PCE95373</td>
<td>1543.6</td>
<td>1543.6</td>
<td>10630.6</td>
<td>O/H</td>
<td>14799.5</td>
<td>14587.0</td>
<td>3956.4</td>
<td></td>
</tr>
<tr class="even">
<td>N67</td>
<td>10039.1</td>
<td>L/H</td>
<td>PCE95407</td>
<td>1415.2</td>
<td>1415.2</td>
<td>8154.4</td>
<td>O/H</td>
<td>14123.9</td>
<td>12239.2</td>
<td>4084.8</td>
<td></td>
</tr>
<tr class="odd">
<td> </td>
<td>10039.1</td>
<td>R/H</td>
<td>PCE95362</td>
<td>2354.5</td>
<td>2354.5</td>
<td>10741.1</td>
<td>O/H</td>
<td>13184.6</td>
<td>13886.6</td>
<td>3145.5</td>
<td></td>
</tr>
<tr class="even">
<td>N68</td>
<td>10510.0</td>
<td>L/H</td>
<td>PCE95361</td>
<td>1948.0</td>
<td>1948.0</td>
<td>9087.1</td>
<td>OH</td>
<td>14062.0</td>
<td>12639.1</td>
<td>3552.0</td>
<td></td>
</tr>
<tr class="odd">
<td> </td>
<td>10510.0</td>
<td>R/H</td>
<td>PCE95277</td>
<td>3918.0</td>
<td>3918.0</td>
<td>9543.0</td>
<td>O/H</td>
<td>12092.0</td>
<td>11125.0</td>
<td>1582.0</td>
<td></td>
</tr>
<tr class="even">
<td>N69</td>
<td>8349.1</td>
<td>L/H</td>
<td>PCE95349</td>
<td>67.8</td>
<td>67.8</td>
<td>10422.2</td>
<td>O/H</td>
<td>13781.3</td>
<td>15854.4</td>
<td>5432.2</td>
<td></td>
</tr>
<tr class="odd">
<td> </td>
<td>8349.1</td>
<td>R/H</td>
<td>PCE95649</td>
<td>2121.6</td>
<td>2121.6</td>
<td>7613.7</td>
<td>O/H</td>
<td>11727.5</td>
<td>10992.1</td>
<td>3378.4</td>
<td></td>
</tr>
<tr class="even">
<td>N70</td>
<td>10639.4</td>
<td>L/H</td>
<td>PCE95326</td>
<td>1022.4</td>
<td>1022.4</td>
<td>9910.7</td>
<td>O/H</td>
<td>15117.0</td>
<td>14388.3</td>
<td>4477.6</td>
<td></td>
</tr>
<tr class="odd">
<td> </td>
<td>10639.4</td>
<td>R/H</td>
<td>PCE95323</td>
<td>4110.1</td>
<td>2161.0</td>
<td>10928.9</td>
<td>O/H</td>
<td>12029.3</td>
<td>12318.8</td>
<td>1389.9</td>
<td></td>
</tr>
<tr class="even">
<td>N71</td>
<td>11934.9</td>
<td>L/H</td>
<td>PCE95330</td>
<td>1756.7</td>
<td>1756.7</td>
<td>9889.3</td>
<td>O/H</td>
<td>15678.2</td>
<td>13632.6</td>
<td>3743.3</td>
<td></td>
</tr>
<tr class="odd">
<td> </td>
<td>11934.9</td>
<td>R/H</td>
<td>PCE95329</td>
<td>238.3</td>
<td>238.3</td>
<td>9307.6</td>
<td>O/H</td>
<td>17196.6</td>
<td>14569.3</td>
<td>5261.7</td>
<td></td>
</tr>
<tr class="even">
<td>N72</td>
<td>10717.5</td>
<td>L/H</td>
<td>PCE95331</td>
<td>2421.7</td>
<td>2421.7</td>
<td>8932.5</td>
<td>O/H</td>
<td>13795.8</td>
<td>12010.8</td>
<td>3078.3</td>
<td></td>
</tr>
<tr class="odd">
<td> </td>
<td>10717.5</td>
<td>R/H</td>
<td>PCE95478</td>
<td>2276.0</td>
<td>2276.0</td>
<td>9869.8</td>
<td>O/H</td>
<td>13941.5</td>
<td>13093.8</td>
<td>3224.0</td>
<td></td>
</tr>
<tr class="even">
<td>N73</td>
<td>10467.3</td>
<td>L/H</td>
<td>PCE95342</td>
<td>1207.7</td>
<td>1207.7</td>
<td>9672.3</td>
<td>O/H</td>
<td>14759.6</td>
<td>13964.6</td>
<td>4292.3</td>
<td></td>
</tr>
<tr class="odd">
<td> </td>
<td>10467.3</td>
<td>R/H</td>
<td>PCE95322</td>
<td>3601.8</td>
<td>3601.8</td>
<td>10420.6</td>
<td>O/H</td>
<td>12365.5</td>
<td>12318.8</td>
<td>1898.2</td>
<td></td>
</tr>
<tr class="even">
<td>N74</td>
<td>10780.9</td>
<td>L/H</td>
<td>PCE95319</td>
<td>1471.2</td>
<td>1471.2</td>
<td>9858.9</td>
<td>O/H</td>
<td>14809.7</td>
<td>13887.7</td>
<td>4028.8</td>
<td></td>
</tr>
<tr class="odd">
<td> </td>
<td>10780.9</td>
<td>R/H</td>
<td>PCE95336</td>
<td>00.0</td>
<td>00.0</td>
<td>5401.8</td>
<td>O/H</td>
<td>16280.9</td>
<td>10901.8</td>
<td>5500.0</td>
<td></td>
</tr>
<tr class="even">
<td>N75</td>
<td>10568.3</td>
<td>L/H</td>
<td>PCE95363</td>
<td>4286.5</td>
<td>683.0</td>
<td>11149.0</td>
<td>O/H</td>
<td>11781.8</td>
<td>12362.5</td>
<td>1213.5</td>
<td></td>
</tr>
<tr class="odd">
<td> </td>
<td>10568.3</td>
<td>R/H</td>
<td>PCE95345</td>
<td>214.4</td>
<td>214.4</td>
<td>8759.1</td>
<td>O/H</td>
<td>15853.9</td>
<td>14044.7</td>
<td>5285.6</td>
<td></td>
</tr>
<tr class="even">
<td>N76</td>
<td>11096.5</td>
<td>L/H</td>
<td>PCE95379</td>
<td>4474.1</td>
<td>702.0</td>
<td>10333.4</td>
<td>O/H</td>
<td>12122.4</td>
<td>11359.3</td>
<td>1025.9</td>
<td></td>
</tr>
<tr class="odd">
<td> </td>
<td>11096.5</td>
<td>R/H</td>
<td>PCE95334</td>
<td>1243.4</td>
<td>1243.4</td>
<td>9443.8</td>
<td>O/H</td>
<td>15353.1</td>
<td>13700.4</td>
<td>4256.6</td>
<td></td>
</tr>
<tr class="even">
<td>N77</td>
<td>12028.2</td>
<td>L/H</td>
<td>PCE95346</td>
<td>3027.0</td>
<td>3027.0</td>
<td>11020.4</td>
<td>O/H</td>
<td>14501.2</td>
<td>13493.4</td>
<td>2473.0</td>
<td></td>
</tr>
<tr class="odd">
<td> </td>
<td>12028.2</td>
<td>R/H</td>
<td>PCE95347</td>
<td>1690.8</td>
<td>1690.8</td>
<td><table>
<colgroup>
<col style="width: 100%" />
</colgroup>
<tbody>
<tr class="odd">
<td>10089.3</td>
</tr>
</tbody>
</table></td>
<td>O/H</td>
<td>15837.4</td>
<td>13898.5</td>
<td>3809.2</td>
<td></td>
</tr>
<tr class="even">
<td>N78</td>
<td>11382.3</td>
<td>L/H</td>
<td>PCE95339</td>
<td>4502.8</td>
<td>4502.8</td>
<td>11408.6</td>
<td>O/H</td>
<td>12379.5</td>
<td>12405.8</td>
<td>997.2</td>
<td></td>
</tr>
<tr class="odd">
<td> </td>
<td>11382.3</td>
<td>R/H</td>
<td>PCE95354</td>
<td>5162.2</td>
<td>5162.2</td>
<td>9149.3</td>
<td>O/H</td>
<td>11720.1</td>
<td>9487.1</td>
<td>337.8</td>
<td></td>
</tr>
<tr class="even">
<td>N79</td>
<td>11105.9</td>
<td>L/H</td>
<td>PCE95261</td>
<td>2041.6</td>
<td>2041.6</td>
<td>9197.0</td>
<td>O/H</td>
<td>14564.3</td>
<td>12655.4</td>
<td>3458.4</td>
<td></td>
</tr>
<tr class="odd">
<td> </td>
<td>11105.9</td>
<td>R/H</td>
<td>PCE95299</td>
<td>2628.7</td>
<td>2628.7</td>
<td>10995.4</td>
<td>O/H</td>
<td>13977.2</td>
<td>13866.7</td>
<td>2871.3</td>
<td></td>
</tr>
<tr class="even">
<td>N80</td>
<td>10607.7</td>
<td>L/H</td>
<td>PCE95352</td>
<td>921.8</td>
<td>921.8</td>
<td>9313.2</td>
<td>O/H</td>
<td>15185.9</td>
<td>13891.4</td>
<td>4578.2</td>
<td></td>
</tr>
<tr class="odd">
<td> </td>
<td>10607.7</td>
<td>R/H</td>
<td>PCE95340</td>
<td>2325.7</td>
<td>2325.7</td>
<td>10176.3</td>
<td>O/H</td>
<td>13782.0</td>
<td>13350.6</td>
<td>3174.3</td>
<td></td>
</tr>
<tr class="even">
<td>N81</td>
<td>11704.4</td>
<td>L/H</td>
<td>PCE95278</td>
<td>3018.4</td>
<td>3018.4</td>
<td>10003.2</td>
<td>O/H</td>
<td>14186.0</td>
<td>12484.8</td>
<td>2481.6</td>
<td></td>
</tr>
<tr class="odd">
<td> </td>
<td>11704.4</td>
<td>R/H</td>
<td>PCE95377</td>
<td>1202.6</td>
<td>1202.6</td>
<td>10289.6</td>
<td>O/H</td>
<td>16001.8</td>
<td>14587.0</td>
<td>4297.4</td>
<td></td>
</tr>
<tr class="even">
<td>N83</td>
<td>10710.6</td>
<td>L/H</td>
<td>PCE95318</td>
<td>1623.6</td>
<td>1623.6</td>
<td>9801.1</td>
<td>O/H</td>
<td>14587.0</td>
<td>13677.5</td>
<td>3876.4</td>
<td></td>
</tr>
<tr class="odd">
<td> </td>
<td>10710.6</td>
<td>R/H</td>
<td>PCE95650</td>
<td>4686.9</td>
<td>4686.9</td>
<td>8566.3</td>
<td>O/H</td>
<td>11523.7</td>
<td>9379.4</td>
<td>813.1</td>
<td></td>
</tr>
<tr class="even">
<td>N84</td>
<td>10788.6</td>
<td>L/H</td>
<td>PCE95300</td>
<td>2065.4</td>
<td>2065.4</td>
<td>10546.1</td>
<td>O/H</td>
<td>14223.2</td>
<td>13980.7</td>
<td>3434.6</td>
<td></td>
</tr>
<tr class="odd">
<td> </td>
<td>10788.6</td>
<td>R/H</td>
<td>PCE95380</td>
<td>994.8</td>
<td>994.8</td>
<td>9853.9</td>
<td>O/H</td>
<td>15293.8</td>
<td>14359.1</td>
<td>4505.2</td>
<td></td>
</tr>
<tr class="even">
<td colspan="11"><strong>OH due @ 5500 Hr - HSI On
Condition</strong></td>
<td></td>
</tr>
<tr class="odd">
<td colspan="11"><strong>SPARE ENGINES (R) repairable (S)
Serviceable</strong></td>
<td></td>
</tr>
<tr class="even">
<td>O/H DATE</td>
<td><strong> </strong></td>
<td><strong> </strong></td>
<td><strong> </strong></td>
<td><strong> </strong></td>
<td><strong> </strong></td>
<td><strong> </strong></td>
<td><strong> </strong></td>
<td><strong> </strong></td>
<td><strong> </strong></td>
<td><strong> </strong></td>
<td></td>
</tr>
<tr class="odd">
<td>7/07</td>
<td>S</td>
<td> </td>
<td>PCE95360</td>
<td>00.0</td>
<td>00.0</td>
<td>9372</td>
<td>O/H</td>
<td> </td>
<td>14872.0</td>
<td>5500.0</td>
<td></td>
</tr>
<tr class="even">
<td>STD AERO</td>
<td>R</td>
<td> </td>
<td>PCE95337</td>
<td>5454.0</td>
<td>5454.0</td>
<td>9302.6</td>
<td>OH</td>
<td> </td>
<td>9348.6</td>
<td>46.0</td>
<td></td>
</tr>
<tr class="odd">
<td>STD AERO</td>
<td>R</td>
<td> </td>
<td>PCE95333</td>
<td>5282.5</td>
<td>1403.9</td>
<td>9280.6</td>
<td>OH</td>
<td> </td>
<td>9498.1</td>
<td>217.5</td>
<td></td>
</tr>
<tr class="even">
<td>ATI</td>
<td>R</td>
<td> </td>
<td>PCE95314</td>
<td>5428.3</td>
<td>5428.3</td>
<td>9328.2</td>
<td>OH</td>
<td> </td>
<td>9399.9</td>
<td>71.7</td>
<td></td>
</tr>
<tr class="odd">
<td> </td>
<td> </td>
<td> </td>
<td> </td>
<td> </td>
<td> </td>
<td> </td>
<td> </td>
<td> </td>
<td> </td>
<td> </td>
<td></td>
</tr>
<tr class="even">
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
</tbody>
</table>