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99-15-14

final rule

Airworthiness Directives; Sikorsky Aircraft-Manufactured Model CH-54B Helicopters

Unsafe Condition: Failure of the main gearbox second stage lower planetary plate (plate) due to fatigue cracking, which could lead to failure of the main gearbox and subsequent loss of control of the helicopter.

Effective: Aug 26, 1999 Category: aircraft Compliance: Within 100 hours TIS after the effective date for initial borescope inspection. Daily inspections...

Why matched: Airworthiness Directives; Sikorsky Aircraft-Manufactured Model CH-54B Helicopters

76-06-01

final rule

Airworthiness Directives; Sikorsky Models S-61L, S-61N, S-61NM, S-61R, S-62A, S-64A, S-64E, S-64F Helicopters, Including Military CH-3C, HH-3C, CH-3E, HH-3E, and CH-54B Helicopters

Unsafe Condition: Flaking chrome plating from the pistons of Model 66WAP200 and Model 66WAN200 hydraulic pumps with specified serial numbers could lead to hydraulic system contamination and failure.

Effective: Mar 24, 1976 Category: aircraft Compliance: Before the first flight each day and within 180 calendar days after the effective date of this AD.

Why matched: Airworthiness Directives; Sikorsky Models S-61L, S-61N, S-61NM, S-61R, S-62A, S-64A, S-64E, S-64F Helicopters, Including Military CH-3C, HH-3C, CH-3E, HH-3E, and CH-54B Helicopters