35122 Federal Register / Vol. 61, No. 130 / Friday, July 5, 1996 / Rules and Regulations

(3) The appeal shall be filed in writing

within 30 days of the decision.

(4) The Corporation Ethics

Committee, at its discretion and after

determining that it is in the best

interests of the FDIC, may stay the effect

of the suspension and/or exclusion

pending conclusion of its review of the

matter.

(b) Reconsideration. (1) A suspended

and/or excluded contractor may submit

a request to the Ethics Counselor to

reconsider the suspension and/or

exclusion decision, reduce the period of

exclusion or terminate the suspension

and/or exclusion.

(2) Such requests shall be in writing

and supported by documentation that

the requested action is justified by:

(i) Reversal of the conviction or civil

judgment upon which the suspension

and/or exclusion was based;

(ii) Newly discovered material

evidence;

(iii) Bona fide change in ownership or

management;

(iv) Elimination of other causes for

which the suspension and/or exclusion

was imposed; or

(v) Other reasons the FDIC Ethics

Counselor deems appropriate.

(3) A request for reconsideration

based on the reversal of the conviction

or civil judgment may be filed at any

time.

(4) Requests for reconsideration based

on other grounds may only be filed

during the period commencing 60 days

after the Ethics Counselor’s decision

imposing the suspension and/or

exclusion. Only one such request may

be filed in any twelve month period.

(5) The Ethics Counselor’s decision on

a request for reconsideration is subject

to the review procedure set forth in

paragraph (a) of this section.

By order of the Board of Directors.

Dated at Washington, D.C., this 17th day of

June 1996.

Federal Deposit Insurance Corporation.

Robert E. Feldman,

Deputy Executive Secretary.

[FR Doc. 96–16510 Filed 7–3–96; 8:45 am]

BILLING CODE 6714–01–P

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. 94–NM–102–AD; Amendment

39–9679; AD 96–13–11]

RIN 2120–AA64

Airworthiness Directives; Airbus Model

A300 B2 and B4 Series Airplanes

AGENCY: Federal Aviation

Administration, DOT.

ACTION: Final rule.

SUMMARY: This amendment supersedes

an existing airworthiness directive (AD),

applicable to all Airbus Model A300 B2,

B4–100, and B4–200 series airplanes,

that currently requires supplemental

structural inspections to detect fatigue

cracking, and repair of cracked

structure. This amendment requires

revising the supplemental structural

inspection (SSID) program by changing

some of the inspection techniques,

changing some of the thresholds and

intervals for inspections, expanding the

area to be inspected for some of the

inspections, and revising the Fleet

Leader Program. This amendment is

prompted by a review of recent service

history and reports received from the

current SSID program required by the

existing AD. The actions specified by

this AD are intended to prevent reduced

structural integrity of these airplanes

due to fatigue cracking.

DATES: Effective August 9, 1996.

The incorporation by reference of

Airbus Industrie A300 Supplemental

Structural Inspection Document (SSID),

Revision 2, dated June 1994, as listed in

the regulations is approved by the

Director of the Federal Register as of

August 9, 1996.

The incorporation by reference of

Airbus Industrie A300 Supplemental

Structural Inspection Document (SSID),

dated September 1989, as listed in the

regulations, was approved previously by

the Director of the Federal Register as of

March 9, 1993 (58 FR 6703, February 2,

1993).

ADDRESSES: The service information

referenced in this AD may be obtained

from Airbus Industrie, 1 Rond Point

Maurice Bellonte, 31707 Blagnac Cedex,

France. This information may be

examined at the Federal Aviation

Administration (FAA), Transport

Airplane Directorate, Rules Docket,

1601 Lind Avenue, SW., Renton,

Washington; or at the Office of the

Federal Register, 800 North Capitol

Street, NW., suite 700, Washington, DC.

FOR FURTHER INFORMATION CONTACT: Phil

Forde, Aerospace Engineer,

Standardization Branch, ANM–113,

FAA, Transport Airplane Directorate,

1601 Lind Avenue, SW., Renton,

Washington 98055–4056; telephone

(206) 227–2146; fax (206) 227–1149.

SUPPLEMENTARY INFORMATION: A

proposal to amend part 39 of the Federal

Aviation Regulations (14 CFR part 39)

by superseding AD 93–01–24,

amendment 39–8478 (58 FR 6703,

February 2, 1993), which is applicable

to all Airbus Model A300 B2, B4–100,

and B4–200 series airplanes, was

published in the Federal Register on

January 31, 1996 (61 FR 3343). The

action proposed to continue to require

supplemental structural inspections to

detect fatigue cracking, and repair of

cracked structure. The action also

proposed to require revising the

supplemental structural inspection

program, including changing some of

the inspection techniques, changing

some of the thresholds and intervals for

certain inspections, expanding the area

to be inspected for some of the

inspections, and revising the Fleet

Leader Program.

Interested persons have been afforded

an opportunity to participate in the

making of this amendment. Due

consideration has been given to the two

comments received.

Support for the Proposal

Both commenters support the

proposed rule.

Conclusion

After careful review of the available

data, including the comment noted

above, the FAA has determined that air

safety and the public interest require the

adoption of the rule as proposed.

Cost Impact

The FAA estimates that

approximately 26 Model A300 series

airplanes of U.S. registry will be affected

by this AD.

The actions that are currently

required by AD 93–01–24 take

approximately 564 work hours per

airplane to accomplish, at an average

labor rate of $60 per work hour. Based

on these figures, the cost impact on U.S.

operators of the actions required by AD

93–01–24 is estimated to be $879,840, or

$33,840 per airplane.

Implementation of the inspections,

repairs, and replacements specified in

Revision 2 of the SSID into an operator’s

maintenance program is estimated to

require approximately 597 work hours

(including removal, inspection, and

installation work hours) per airplane per

year, at an average labor rate of $60 per
Federal Register / Vol. 61, No. 130 / Friday, July 5, 1996 / Rules and Regulations 35123

work hour. Based on these figures, the

cost impact on U.S. operators of the

proposed requirements of this AD is

estimated to be $931,320, or $35,820 per

airplane.

The cost impact figures discussed

above are based on assumptions that no

operator has yet accomplished any of

the requirements of this AD action, and

that no operator would accomplish

those actions in the future if this AD

were not adopted.

Regulatory Impact

The regulations adopted herein will

not have substantial direct effects on the

States, on the relationship between the

national government and the States, or

on the distribution of power and

responsibilities among the various

levels of government. Therefore, in

accordance with Executive Order 12612,

it is determined that this final rule does

not have sufficient federalism

implications to warrant the preparation

of a Federalism Assessment.

For the reasons discussed above, I

certify that this action (1) is not a

‘‘significant regulatory action’’ under

Executive Order 12866; (2) is not a

‘‘significant rule’’ under DOT

Regulatory Policies and Procedures (44

FR 11034, February 26, 1979); and (3)

will not have a significant economic

impact, positive or negative, on a

substantial number of small entities

under the criteria of the Regulatory

Flexibility Act. A final evaluation has

been prepared for this action and it is

contained in the Rules Docket. A copy

of it may be obtained from the Rules

Docket at the location provided under

the caption ADDRESSES.

List of Subjects in 14 CFR Part 39

Air transportation, Aircraft, Aviation

safety, Incorporation by reference,

Safety.

Adoption of the Amendment

Accordingly, pursuant to the

authority delegated to me by the

Administrator, the Federal Aviation

Administration amends part 39 of the

Federal Aviation Regulations (14 CFR

part 39) as follows:

PART 39—AIRWORTHINESS

DIRECTIVES

1. The authority citation for part 39

continues to read as follows:

Authority: 49 U.S.C. 106(g), 40113, 44701.

§ 39.13 [Amended]

2. Section 39.13 is amended by

removing amendment 39–8478 (58 FR

6703, February 2, 1993), and by adding

a new airworthiness directive (AD),

amendment 39–9679, to read as follows:

96–13–11 Airbus Industries: Amendment 39–

9679. Docket 94–NM–102–AD.

Supersedes AD 93–01–24, Amendment

39–8478.

Applicability: All Model A300 B2–1A, B2–

1C, B2K–3C, and B2–203 series airplanes,

and Model A300 B4–2C, B4–103, and B4–203

series airplanes; certificated in any category.

Note 1: This AD applies to each airplane

identified in the preceding applicability

provision, regardless of whether it has been

otherwise modified, altered, or repaired in

the area subject to the requirements of this

AD. For airplanes that have been modified,

altered, or repaired so that the performance

of the requirements of this AD is affected, the

owner/operator must request approval for an

alternative method of compliance in

accordance with paragraph (m) of this AD.

The request should include an assessment of

the effect of the modification, alteration, or

repair on the unsafe condition addressed by

this AD; and, if the unsafe condition has not

been eliminated, the request should include

specific proposed actions to address it.

Compliance: Required as indicated, unless

accomplished previously.

To prevent reduced structural integrity of

these airplanes due to fatigue cracking,

accomplish the following:

(a) Within one year after March 9, 1993

(the effective date of AD 93–01–24,

amendment 39–8478), incorporate a revision

into the FAA-approved maintenance

inspection program that provides for

supplemental maintenance inspections,

modifications, repair, or replacement of the

significant structural details (SSD) and

significant structural items (SSI) specified in

‘‘Airbus Industrie A300 Supplemental

Structural Inspection Document’’ (SSID),

dated September 1989 (hereafter referred to

as ‘‘the SSID’’).

(b) Within one year after the effective date

of this AD, replace the revision of the FAAapproved maintenance program required by

paragraph (a) of this AD with the inspections,

inspection intervals, repairs, and

replacements defined in ‘‘Airbus Industrie

A300 Supplemental Structural Inspection

Document’’ (SSID), Revision 2, dated June

1994 (hereafter referred to as ‘‘Revision 2 of

the SSID’’). Accomplish the actions specified

in the service bulletins identified in Section

6, ‘‘SB Reference List,’’ Revision 2 of the

SSID, at the times specified in those service

bulletins. The actions are to be accomplished

in accordance with those service bulletins.

(1) For airplanes that have exceeded the

threshold specified in any of the service

bulletins identified in Section 6, ‘‘SB

Reference List,’’ Revision 2 of the SSID:

Accomplish the actions specified in those

service bulletins within the grace period

specified in that service bulletin. The grace

period is to be measured from the effective

date of this AD.

(2) For airplanes that have exceeded the

threshold specified in any of the service

bulletins identified in Section 6, ‘‘SB

Reference List,’’ Revision 2 of the SSID, and

a grace period is not specified in that service

bulletin: Accomplish the actions specified in

that service bulletins within 1,500 flight

cycles after the effective date of this AD.

(c) If any cracked structure is detected

during the inspections required by either

paragraph (a) or (b) of this AD, prior to

further flight, permanently repair the cracked

structure in accordance with either paragraph

(c)(1), (c)(2), or (c)(3) of this AD.

Note 2: A permanent repair is defined as

a repair that meets the certification basis of

the airplane, and does not require additional

modification at a later date.

(1) The service bulletins listed in Section

6, ‘‘SB Reference List,’’ of the SSID [for

airplanes that are currently being inspected

in accordance with paragraph (a) of this AD];

or in accordance with a method approved by

the Manager, Standardization Branch, ANM–

113, FAA, Transport Airplane Directorate, if

a permanent repair is not specified in any of

these service bulletins. Or

(2) The service bulletins listed in Section

6, ‘‘SB Reference List,’’ of Revision 2 of the

SSID [for airplanes that are currently being

inspected in accordance with paragraph (b)

of this AD]; or in accordance with a method

approved by the Manager, Standardization

Branch, ANM–113, if a permanent repair is

not specified in any of these service

bulletins. Or

(3) Other permanent repair data meeting

the certification basis of the airplane which

is approved by the Manager, Standardization

Branch, ANM–113, or by the Direction

Gonorale de l’Aviation Civile (DGAC) of

France.

(d) For airplanes identified as Fleet Leader

Program (FLP) in Section 5, ‘‘Fleet Leader

Program,’’ of the SSID or Revision 2 of the

SSID: Inspect according to the instructions

and intervals specified in paragraph 4.4,

‘‘Adjustment of Inspection Requirements and

DSG,’’ of Section 4, or Section 9, as

applicable, of the SSID [for airplanes

inspected in accordance with paragraph (a) of

this AD], or Revision 2 of the SSID [for

airplanes inspected in accordance with

paragraph (b) of this AD], for each SSD.

(e) For the purpose of accomplishing

paragraphs (d), (f), (g), and (i) of this AD,

operators shall not use paragraph 6.2,

‘‘Complete RR Method,’’ of Section 9 of the

SSID to calculate inspection thresholds and

intervals.

(f) For Model A300–B2 and B2K–3C series

airplanes: For any SSD that has exceeded the

values of the threshold specified in

paragraph 6, ‘‘Inspection Threshold and

Intervals,’’ Section 9 of the SSID, inspect at

the time specified in either paragraph (f)(1)

or (f)(2) of this AD, as applicable.

(1) For airplanes inspected in accordance

with paragraph (a) of this AD: Inspect within

2,000 landings after March 9, 1993, in

accordance with the SSID. Or

(2) For airplanes inspected in accordance

with paragraph (b) of this AD: Inspect within

2,000 landings after the effective date of this

AD, in accordance with Revision 2 of the

SSID.

(g) For Model A300–B4 series airplanes:

For any SSD that has exceeded the values of

the threshold specified in paragraph 6,

‘‘Inspection Threshold and Intervals,’’

Section 9 of the SSID, inspect at the time

specified in either paragraph (g)(1) or (g)(2)

of this AD, as applicable.
35124 Federal Register / Vol. 61, No. 130 / Friday, July 5, 1996 / Rules and Regulations

(1) For airplanes inspected in accordance

with paragraph (a) of this AD: Inspect within

1,500 landings after March 9, 1993 [the

effective date of AD 93–01–24, amendment

39–8478]. Or

(2) For airplanes inspected in accordance

with paragraph (b) of this AD: Inspect within

1,500 landings after the effective date of this

AD.

(h) For airplanes identified as FLP in

Section 5, ‘‘Fleet Leader Program,’’ of the

SSID or Revision 2 of the SSID: Within one

year after the effective date of this AD, apply

the basic requirements given in Revision 2 of

the SSID.

(i) For airplanes that are subject to the

requirements of paragraph (b) of this AD, and

have exceeded the initial inspection

threshold specified in paragraph 4.4,

‘‘Adjustment of Inspection Requirements and

DSG,’’ of Section 4, or paragraph 6,

‘‘Inspection Threshold and Intervals,’’ of

Section 9, for each SSD: Perform the initial

inspection prior to the accumulation of the

number of flight cycles specified in

paragraph 7, ‘‘Additional Information,’’

Section 9, of Revision 2 of the SSID.

Note 3: Fatigue ratings are not applicable

to these allowances; therefore, no adjustment

is required.

Note 4: Paragraph (i) of this AD provides

the ‘‘grace’’ periods for those airplanes that

are new to the FLP or that have newly added

or revised SSID requirements in accordance

with paragraph (b) of this AD.

(j) The grace period provided by paragraph

(i) of this AD is also applicable to the

thresholds and/or repeat intervals for each

SSD for which the inspection interval or

threshold was reduced in accordance with

the requirements of paragraph (b) of this AD.

(k) For FLP airplanes identified in Section

5, ‘‘Fleet Leader Program,’’ of the SSID or

Revision 2 of the SSID that are listed in

Section 7, ‘‘SSI Limitation List,’’ of the SSID

[for airplanes that are currently being

inspected in accordance with paragraph (a) of

this AD] , or Revision 2 of the SSID [for

airplanes that are currently being inspected

in accordance with paragraph (b) of this AD]:

Inspect at intervals not to exceed the interval

specified for each SSI, in accordance with the

values given in Section 7, ‘‘SSI Limitation

List,’’ of the SSID or Revision 2 of the SSID,

as applicable.

(l) For all airplanes: All inspection results,

positive or negative, must be reported to

Airbus Industrie in accordance with either

paragraph (l)(1) or (l)(2) of this AD, as

applicable. Information collection

requirements contained in this regulation

have been approved by the Office of

Management and Budget (OMB) under the

provisions of the Paperwork Reduction Act of

1980 (44 U.S.C. 3501 et seq.) and have been

assigned OMB Control Number 2120–0056.

(1) For FLP airplanes, identified in Section

5, ‘‘Fleet Leader Program,’’ of the SSID or

Revision 2 of the SSID: Submit reports in

accordance with the instructions in

paragraph 5.2, ‘‘SSIP Inspection Reporting,’’

of Section 5, and paragraph 7.1, ‘‘General,’’

of Section 7 of the SSID [for airplanes that

are currently being inspected in accordance

with paragraph (a) of this AD]; or Revision

2 of the SSID [for airplanes inspected in

accordance with paragraph (b) of this AD].

(2) For all airplanes that are subject to

Section 6, ‘‘SB Reference List,’’ of the SSID:

Submit reports in accordance with the

instructions in the applicable service

bulletins identified in Section 6 of the SSID

[for airplanes that are currently being

inspected in accordance with paragraph (a) of

this AD]; or Revision 2 of the SSID [for

airplanes that are currently being inspected

in accordance with paragraph (b) of this AD].

(m) An alternative method of compliance

or adjustment of the compliance time that

provides an acceptable level of safety may be

used if approved by the Manager,

Standardization Branch, ANM–113, FAA,

Transport Airplane Directorate. Operators

shall submit their requests through an

appropriate FAA Principal Maintenance

Inspector, who may add comments and then

send it to the Manager, Standardization

Branch, ANM–113.

Note 5: Information concerning the

existence of approved alternative methods of

compliance with this AD, if any, may be

obtained from the Standardization Branch,

ANM–113.

Note 6: Alternative methods of compliance

previously granted for AD 93–01–24,

amendment 39–8478, continue to be

considered as acceptable alternative methods

of compliance with this amendment.

(n) Special flight permits may be issued in

accordance with sections 21.197 and 21.199

of the Federal Aviation Regulations (14 CFR

21.197 and 21.199) to operate the airplane to

a location where the requirements of this AD

can be accomplished.

(o) The actions shall be done in accordance

with Airbus Industrie Supplemental

Structural Inspection Document (SSID),

dated September 1989; or Airbus Industrie

A300 SSID, Revision 2, dated June 1994, as

applicable. Airbus Industrie A300 SSID,

Revision 2, dated June 1994, contains the

following list of effective pages:

Page No.

Revision

level

shown on

page

Date shown

on page

Record of revision 2 .............. Jun 94

Section 0:

O–LEP 1 ....... 2 .............. Jun 94.

O–TOC 1 ...... 2 .............. Jun 94.

Section 1:

1–LEP 1 ........ 2 .............. Jun 94.

1–TOC 1 ....... 1 .............. Mar 93.

1 .................... 1 .............. Mar 93.

2, 3 ............... 2 .............. Jun 94.

Section 2:

2–LEP 1 ........ 2 .............. Jun 94.

2–TOC 1 ....... 1 .............. Mar 93.

1, 2 ............... 1 .............. Mar 93.

3 .................... 2 .............. Jun 94.

Section 3:

3–LEP 1 ........ 2 .............. Jun 94.

3–TOC 1 ....... 2 .............. Jun 94.

1, 2 ............... 2 .............. Jun 94.

Section 4:

4–LEP 1 ........ 1 .............. Mar 93.

4–TOC 1 ....... 1 .............. Mar 93.

1–3, 7–9, 11–

16, 19, 24–

38, 40–46.

1 .............. Mar 93.

Page No.

Revision

level

shown on

page

Date shown

on page

4–6, 10, 17,

18, 20–23,

39.

0 .............. Sep 89.

Section 5:

5–LEP 1 ........ 2 .............. Jun 94.

5–TOC 1 ....... 2 .............. Jun 94.

1–48 .............. 2 .............. Jun 94.

Section 6:

6–LEP 1 ........ 2 .............. Jun 94.

6–TOC 1 ....... 1 .............. Mar 93.

1 .................... 1 .............. Mar 93.

2–4 ................ 2 .............. Jun 94.

Section 7:

7–LEP 1 ........ 1 .............. Mar 93.

7–TOC 1 ....... 1 .............. Mar 93.

1–10 .............. 1 .............. Mar 93.

Section 8:

8–LEP 1 ........ 1 .............. Mar 93.

8–TOC 1 ....... 1 .............. Mar 93.

1–5 ................ 1 .............. Mar 93.

Section 9:

9–LEP 1–6 .... 2 .............. Jun 94.

9–LEP 7–9 .... 2 .............. Jun 94.

9–TOC 1 ....... 1 .............. Mar 93.

1–3 ................ 1 .............. Mar 93.

4 .................... 2 .............. Jun 94.

526305/1–4 .......... 0 .............. Sep 89.

526305/5 .............. 1 .............. Mar 93.

526305/6 .............. 2 .............. Jun 94.

536101/1 .............. 0 .............. Sep 89.

536101/2 .............. 1 .............. Mar 93.

536101/3 .............. 2 .............. Jun 94.

536101/4 .............. 0 .............. Sep 89.

536110/1, 2 .......... 0 .............. Sep 89.

536110/3 .............. 1 .............. Mar 93.

536110/4 .............. 2 .............. Jun 94.

536110/5 .............. 0 .............. Sep 89.

536202/1 .............. 0 .............. Sep 89.

536202/2, 3 .......... 1 .............. Mar 93.

536202/4 .............. 2 .............. Jun 94.

536202/5–7 .......... 0 .............. Sep 89.

536204/1, 2 .......... 0 .............. Sep 89.

536204/3, 4 .......... 1 .............. Mar 93.

536204/5 .............. 2 .............. Jun 94.

536204/6, 7 .......... 0 .............. Sep 89.

536205/1, 2 .......... 0 .............. Sep 89.

536205/3 .............. 2 .............. Jun 94.

536205/4 .............. 1 .............. Mar 93.

536205/5 .............. 2 .............. Jun 94.

536205/6, 7 .......... 0 .............. Sep 89.

536206/1 .............. 0 .............. Sep 89.

536206/2, 3 .......... 1 .............. Mar 93.

536206/4 .............. 2 .............. Jun 94.

536206/5, 6 .......... 0 .............. Sep 89.

536207/1 .............. 0 .............. Sep 89.

536207/2 .............. 1 .............. Mar 93.

536207/3 .............. 2 .............. Jun 94.

536207/4–7 .......... 0 .............. Sep 89.

536225/1 .............. 0 .............. Sep 89.

536225/2 .............. 1 .............. Mar 93.

536225/3 .............. 2 .............. Jun 94.

536225/4–6 .......... 0 .............. Sep 89.

536301/1–3 .......... 0 .............. Sep 89.

536301/4 .............. 1 .............. Mar 93.

536301/5 .............. 0 .............. Sep 89.

536301/6 .............. 1 .............. Mar 93.

536301/7–9 .......... 2 .............. Jun 94.

536301/10 ............ 2 .............. Jun 94.

536311/1–3 .......... 0 .............. Sep 89.

536311/4 .............. 1 .............. Mar 93.

536311/5, 6 .......... 2 .............. Jun 94.
Federal Register / Vol. 61, No. 130 / Friday, July 5, 1996 / Rules and Regulations 35125

Page No.

Revision

level

shown on

page

Date shown

on page

536311/7 .............. 2 .............. Jun 94.

536355/1–4 .......... 0 .............. Sep 89.

536355/5 .............. 1 .............. Mar 93.

536355/6 .............. 2 .............. Jun 94.

536359/1 .............. 0 .............. Sep 89.

536359/2 .............. 1 .............. Mar 93.

536359/3 .............. 2 .............. Jun 94.

536365/1 .............. 0 .............. Sep 89.

536365/2 .............. 1 .............. Mar 93.

536365/3 .............. 2 .............. Jun 94.

536365/4 .............. 1 .............. Mar 93.

536367/1 .............. 0 .............. Sep 89.

536367/2 .............. 1 .............. Mar 93.

536367/3 .............. 2 .............. Jun 94.

536403/1 .............. 0 .............. Sep 89.

536403/2 .............. 1 .............. Mar 93.

536403/3 .............. 2 .............. Jun 94.

536403/4 .............. 0 .............. Sep 89.

536405/1–3 .......... 0 .............. Sep 89.

536405/4–5 .......... 1 .............. Mar 93.

536405/6 .............. 2 .............. Jun 94.

536405/7 .............. 0 .............. Sep 89.

536407/1–3 .......... 0 .............. Sep 89.

536407/4, 5 .......... 1 .............. Mar 93.

536407/6 .............. 2 .............. Jun 94.

536407/7 .............. 0 .............. Sep 89.

536415/1, 2 .......... 1 .............. Mar 93.

536415/3 .............. 2 .............. Jun 94.

536415/4 .............. 0 .............. Sep 89.

536502/1–4 .......... 0 .............. Sep 89.

536502/5, 6 .......... 1 .............. Mar 93.

536502/7–9 .......... 2 .............. Jun 94.

536502/10 ............ 2 .............. Jun 94.

536503/1, 2 .......... 0 .............. Sep 89.

536503/3, 4 .......... 1 .............. Mar 93.

536503/5 .............. 2 .............. Jun 94.

536503/6–10 ........ 0 .............. Sep 89.

536506/1, 2 .......... 0 .............. Sep 89.

536506/3, 4 .......... 1 .............. Mar 93.

536506/5 .............. 2 .............. Jun 94.

536506/6–11 ........ 0 .............. Sep 89.

536509/1, 2 .......... 0 .............. Sep 89.

536509/3 .............. 1 .............. Mar 93.

536509/4 .............. 2 .............. Jun 94.

536509/5 .............. 0 .............. Sep 89.

536510/1, 2 .......... 0 .............. Sep 89.

536510/3 .............. 1 .............. Mar 93.

536510/4 .............. 2 .............. Jun 94.

536510/5, 6 .......... 0 .............. Sep 89.

536521/1, 2 .......... 0 .............. Sep 89.

536521/3, 4 .......... 1 .............. Mar 93.

536521/5 .............. 2 .............. Jun 94.

536523/1 .............. 0 .............. Sep 89.

536523/2, 3 .......... 1 .............. Mar 93.

536523/4 .............. 2 .............. Jun 94.

536523/5, 6 .......... 0 .............. Sep 89.

536541/1 .............. 0 .............. Sep 89.

536541/2, 3 .......... 2 .............. Jun 94.

536541/4 .............. 2 .............. Jun 94.

536546/1 .............. 0 .............. Sep 89.

536546/2 .............. 1 .............. Mar 93.

536546/3 .............. 2 .............. Jun 94.

536546/4–6 .......... 0 .............. Sep 89.

536547/1 .............. 0 .............. Sep 89.

536547/2 .............. 1 .............. Mar 93.

536547/3 .............. 2 .............. Jun 94.

536547/4 .............. 0 .............. Sep 89.

536548/1, 2 .......... 0 .............. Sep 89.

536548/3, 4 .......... 1 .............. Mar 93.

536548/5 .............. 2 .............. Jun 94.

536548/6–8 .......... 1 .............. Mar 93.

Page No.

Revision

level

shown on

page

Date shown

on page

536596/1, 2 .......... 0 .............. Sep 89.

536596/3 .............. 1 .............. Mar 93.

536596/4 .............. 2 .............. Jun 94.

536596/5 .............. 0 .............. Sep 89.

536598/1, 2 .......... 0 .............. Sep 89.

536598/3, 4 .......... 1 .............. Mar 93.

536598/5 .............. 2 .............. Jun 94.

536598/6–9 .......... 0 .............. Sep 89.

536599/1 .............. 0 .............. Sep 89.

536599/2 .............. 1 .............. Mar 93.

536599/3–6 .......... 2 .............. Jun 94.

536599/7 .............. 2 .............. Jun 94.

536651/1, 2 .......... 0 .............. Sep 89.

536651/3, 4 .......... 1 .............. Mar 93.

536651/5 .............. 2 .............. Jun 94.

536652/1–3 .......... 0 .............. Sep 89.

536652/4 .............. 1 .............. Mar 93.

536652/5 .............. 2 .............. Jun 94.

536652/6 .............. 0 .............. Sep 89.

536704/1, 2 .......... 0 .............. Sep 89.

536704/3 .............. 1 .............. Mar 93.

536704/4 .............. 2 .............. Jun 94.

536704/5 .............. 0 .............. Sep 89.

546001/1 .............. 0 .............. Sep 89.

546001/2, 3 .......... 1 .............. Mar 93.

546001/4 .............. 2 .............. Jun 94.

546001/5–10 ........ 1 .............. Mar 93.

536014/1 .............. 0 .............. Sep 89.

536014/2, 3 .......... 1 .............. Mar 93.

536014/4 .............. 2 .............. Jun 94.

536014/5–7 .......... 0 .............. Sep 89.

556002/1 .............. 0 .............. Sep 89.

556002/2, 3 .......... 1 .............. Mar 93.

556002/4 .............. 2 .............. Jun 94.

556002/5–7 .......... 1 .............. Mar 93.

556003/1–4 .......... 0 .............. Sep 89.

556003/5, 6 .......... 1 .............. Mar 93.

556003/7 .............. 2 .............. Jun 94.

556003/8–10 ........ 1 .............. Mar 93.

556004/1, 2 .......... 0 .............. Sep 89.

556004/3 .............. 1 .............. Mar 93.

556004/4 .............. 2 .............. Jun 94.

576004/1 .............. 0 .............. Sep 89.

576004/2 .............. 1 .............. Mar 93.

576004/3 .............. 2 .............. Jun 94.

576004/4–6 .......... 0 .............. Sep 89.

576007/1 .............. 0 .............. Sep 89.

576007/2 .............. 1 .............. Mar 93.

576007/3 .............. 2 .............. Jun 94.

576007/4–6 .......... 0 .............. Sep 89.

576009/1 .............. 0 .............. Sep 89.

576009/2 .............. 1 .............. Mar 93.

576009/3 .............. 2 .............. Jun 94.

576009/4–6 .......... 0 .............. Sep 89.

576011/1 .............. 0 .............. Sep 89.

576011/2 .............. 1 .............. Mar 93.

576011/3 .............. 2 .............. Jun 94.

576011/4–6 .......... 0 .............. Sep 89.

576013/1–3 .......... 0 .............. Sep 89.

576013/4 .............. 1 .............. Mar 93.

576013/5–8 .......... 2 .............. Jun 94.

576013/9 .............. 2 .............. Jun 94.

576017/1 .............. 0 .............. Sep 89.

576017/2 .............. 1 .............. Mar 93.

576017/3 .............. 2 .............. Jun 94.

576017/4 .............. 0 .............. Sep 89.

576021/1 .............. 0 .............. Sep 89.

576021/2 .............. 1 .............. Mar 93.

576021/3 .............. 2 .............. Jun 94.

576021/4–6 .......... 0 .............. Sep 89.

576029/1, 2 .......... 0 .............. Sep 89.

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shown on

page

Date shown

on page

576029/3 .............. 1 .............. Mar 93.

576029/4 .............. 2 .............. Jun 94.

576029/5–7 .......... 0 .............. Sep 89.

576031/1 .............. 0 .............. Sep 89.

576031/2 .............. 1 .............. Mar 93.

576031/3 .............. 2 .............. Jun 94.

576031/4–6 .......... 0 .............. Sep 89.

576035/1 .............. 0 .............. Sep 89.

576035/2 .............. 1 .............. Mar 93.

576035/3 .............. 2 .............. Jun 94.

576035/4–6 .......... 0 .............. Sep 89.

576037/1 .............. 0 .............. Sep 89.

576037/2 .............. 1 .............. Mar 93.

576037/3–6 .......... 2 .............. Jun 94.

576037/7 .............. 2 .............. Jun 94.

576041/1–4 .......... 0 .............. Sep 89.

576041/5, 6 .......... 2 .............. Jun 94.

576047/1 .............. 0 .............. Sep 89.

576047/2–6 .......... 2 .............. Jun 94.

576051/1 .............. 0 .............. Sep 89.

576051/2 .............. 1 .............. Mar 93.

576051/3 .............. 2 .............. Jun 94.

576051/4–6 .......... 0 .............. Sep 89.

576062/1, 2 .......... 1 .............. Mar 93.

576062/3–5 .......... 2 .............. Jun 94.

576063/1–5 .......... 2 .............. Jun 94.

576064/1–6 .......... 2 .............. Jun 94.

576065/1–7 .......... 2 .............. Jun 94.

576067/1–3 .......... 2 .............. Jun 94.

576068/1–3 .......... 2 .............. Jun 94.

576070/1–7 .......... 2 .............. Jun 94.

This incorporation by reference of Airbus

Industrie SSID, dated September 1989, was

approved by the Director of the Federal

Register in accordance with 5 U.S.C. 552(a)

and 1 CFR part 51, as of March 9, 1993 (58

FR 6703, February 2, 1993). The

incorporation by reference of Airbus

Industrie SSID, Revision 2, dated June 1994,

is approved by the Director of the Federal

Register in accordance with 5 U.S.C. 552(a)

and 1 CFR part 51. Copies may be obtained

from Airbus Industrie, 1 Rond Point Maurice

Bellonte, 31707 Blagnac Cedex, France.

Copies may be inspected at the FAA,

Transport Airplane Directorate, 1601 Lind

Avenue, SW., Renton, Washington; or at the

Office of the Federal Register, 800 North

Capitol Street, NW., suite 700, Washington,

DC.

(p) This amendment becomes

effective on August 9, 1996.

Issued in Renton, Washington, on June 17,

1996.

Darrell M. Pederson,

Acting Manager, Transport Airplane

Directorate, Aircraft Certification Service.

[FR Doc. 96–15953 Filed 7–3–96; 8:45 am]

BILLING CODE 4910–13–U