AD 82-11-02

Airworthiness directive · Elevator and/or Trim Tab · Gulfstream Aerospace G-1159 and G-1159B

Effective
May 31, 1982
Models
G-1159, G-1159B
Data sheet
TCDSA12EA
Registered aircraft
25 matched by model
Product
Aircraft · Large airplane
Amendment
39-4384

Unofficial copy of the text in the FAA’s Dynamic Regulatory System. The FAA’s own copy is the authoritative one. DRS record last changed May 30, 2024.

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The airworthiness directive

82-11-02 GULFSTREAM AMERICAN CORPORATION (formerly Grumman American Corporation, Grumman Aerospace Corporation): Amendment 39-4384. Applies to Gulfstream American Models G-1159 and G-1159B series airplanes, certificated in all categories. Compliance required as indicated unless previously accomplished.

To prevent possible severe flutter of the elevator and/or elevator trim tab, accomplish the following:

A. Within the next 50 hours time in service after the effective date of this AD, and thereafter at intervals not to exceed 50 hours time in service until repairs are accomplished in accordance with paragraph B, inspect the left and right outboard elevator trim tab hinge fittings and left and right elevator rear spar for cracks in accordance with Gulfstream American Customer Bulletin No. 325, Amendment 1, dated March 26, 1982. If cracks are found, repair or replace the failed parts before further flight in accordance with Gulfstream American Customer Bulletin No. 315 datedApril 15, 1982.

B. Within 150 hours time in service after the effective date of this AD, unless already accomplished, accomplish the following in accordance with Gulfstream American Service Change No. 315 dated April 15, 1982:

(1) Remove the left and right elevator outboard trim tab hinge fittings, P/N 1159CSM20105-1, and replace with P/N 1159CSM20837.

(2) Remove the left and right elevator ribs, P/N 1159CS20420-1 and -2, and replace with ribs, P/N 1159RDC300-919 and -920.

(3) Inspect and repair, if necessary, the elevator rear spar.

C. Perform a mass balance inspection of the elevator in accordance with Gulfstream American Model G-1159 Maintenance Manual upon completion of repairs and installation of replacement parts.

D. Alternate means of compliance which provide an equivalent level of safety may be used when approved by the Chief, Atlanta Aircraft Certification Office.

E. Special flight permits may be issued in accordance with FAR 21.197 and 21.199 to operate airplanes to a base in order to comply with the requirements of this AD.

The manufacturer's specifications and procedures identified and described in this directive are incorporated herein and made a part hereof pursuant to 5 U.S.C. 552(a)(1).

All persons affected by this directive who have not already received these documents from the manufacturer may obtain copies upon request to Gulfstream American Corporation, P.O. Box 2206, Savannah, Georgia 31402.

These documents may be examined at the Atlanta Aircraft Certification Office, FAA, 3400 Norman Berry Drive, East Point, Georgia 30344.

This amendment becomes effective May 31, 1982.

Affected TCDS · 1

The type certificate data sheets for the models this AD names, matched by model and maker.

Registered aircraft · 25

Registered aircraft whose airframe or engine model this AD names. Matched by model only, so check each against the AD’s applicability.

By aircraft maker
  • Gulfstream Aerospace10 aircraft
  • Grumman9 aircraft
  • Grumman American Avn.4 aircraft
  • Gulfstream American2 aircraft
By year built
19671979
Registered aircraft by year built: 15 aircraft
19671
19684
19692
19701
19711
19731
19741
19751
19761
19771
19791

10 with no year recorded

By model

Aircraft

See all 25 aircraft