AD 77-19-03

Airworthiness directive · Main Rotor Retention Straps · MD Helicopters 369D

Effective
September 27, 1977
Model
369D
Data sheet
TCDSH3WE
Registered aircraft
211 matched by model
Product
Aircraft · Rotorcraft
Amendment
39-3038

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

77-19-03 HUGHES HELICOPTERS: Amendment 39-3038. Applies to Hughes Model 369D helicopters, certificated in all categories, which have P/N 369D21200 main rotor hub serial numbers 0001 through 0178 installed.

Compliance required as indicated.

To prevent failure of the main rotor retention straps which can result in loss of a main rotor blade accomplish the following:

A. Before further flight after the effective date of the AD, visually inspect the lead leg of each main rotor retention strap pack, P/N 369D21210, at the inboard ends to determine if two adjacent metallic anti-fretting laminates P/N 369D21271-5, -51, -53 or -55, have been installed on the upper side of the lead leg of any strap pack.

(1) If two adjacent metallic anti-fretting laminates have been installed, visually inspect to determine if one or both are cracked or have been broken off where they extend from the hub.

(i) If no anti-fretting laminate is found cracked or broken, repeat the inspections in (1), above, at times in service not to exceed 25 hours. This repetitive inspection can be discontinued when the main rotor hub, P/N 369D21200, has been replaced by a serviceable hub having only one anti-fretting laminate on the upper side of the lead leg of each main rotor strap pack.

(ii) If any anti-fretting laminate is found cracked or broken, further visually inspect the main rotor retention strap laminates adjacent to the anti-fretting laminates.

(a) If any strap laminate is broken or cracked, replace the main rotor hub, P/N 369D21200, before further flight.

(b) If no strap laminate is cracked or broken, replace the main rotor hub, P/N 369D21200, within ten hours time in service.

(2) If the inspection reveals that only one metallic anti-fretting laminate has been installed on the upper lead leg of each strap pack no further action is required by this AD.

This amendment becomes effective September 27, 1977, for all persons except those to whom it was made effective by telegram dated August 12, 1977, which contained this amendment.

Affected TCDS · 1

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

Registered aircraft · 211

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
  • Hughes Helicopters207 aircraft
  • Summa4 aircraft
By year built
19762021
Registered aircraft by year built: 170 aircraft
19763
197727
197831
197927
198031
198136
198213
19881
20211

41 with no year recorded

By model

Aircraft

See all 211 aircraft