AD 87-25-05

Airworthiness directive · Landing Gear Spindle · Columbia Helicopters 234

Effective
December 15, 1987
Model
234
Data sheet
TCDSH9EA
Registered aircraft
6 matched by model
Product
Aircraft · Rotorcraft
Amendment
39-5773

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

87-25-05 BOEING HELICOPTER COMPANY (BOEING VERTOL): Amendment 39-5773. Applies to Boeing Helicopter Model 234 series helicopters certificated in any category.

Compliance is required as indicated, unless already accomplished.

To prevent possible hazards in landing associated with a cracked aft landing gear spindle P/N 114L2322-5, -8, -9, or -11, accomplish the following:

(a) Within the next 25 hours' time in service after the effective date of this AD or before the accumulation of 1,200 hours' time in service, whichever comes later, remove from service aft landing gear spindles P/N's 114L2322-5 and -8 and replace with spindle P/N 114L2322-9 or -11. Removal and installation shall be accomplished in accordance with paragraph 3, "Accomplishment Instructions," Boeing Vertol Service Bulletin No. 234-32-1009, dated February 23, 1987.

(b) Remove from service spindle P/N 11402322-11 prior to the accumulation of 1,200 hours' time in service and spindle P/N 114L2322-9 prior to the accumulation of 3,500 hours' time in service.

(c) Upon submission of substantiating data by an owner or operator through an FAA maintenance inspector, the Manager, New York Aircraft Certification Office, FAA, New England Region, may adjust the compliance times specified in this AD.

The removal or installation of spindles shall be done in accordance with paragraph 3, Accomplishment Instructions, Boeing Vertol Service Bulletin No. 234-32-1009, dated February 23, 1987. This incorporation by reference was 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 Boeing Helicopter Company, Boeing Center, P.O. Box 16858, Philadelphia, Pennsylvania 19141. These documents may be examined at the Office of the Regional Counsel, FAA, Southwest Region, 4400 Blue Mound Road, Fort Worth, Texas, or the Office of the Federal Register, 1100 L Street, N. W., Room 8401, Washington, D.C.

This amendment 39-5773 supersedes AD 83-17-02, Amendment 39-4708. This amendment 39-5773 becomes effective December 15, 1987.

Affected TCDS · 1

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

Registered aircraft · 6

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
  • Boeing-Vertol6 aircraft
By year built
19811983
Registered aircraft by year built: 5 aircraft
19812
19821
19832

1 with no year recorded

By model

Aircraft