AD 89-23-14

final rule
Data completeness: 70%

Airworthiness Directives; MCDONNELL DOUGLAS HELICOPTER COMPANY (MDHC) Model 369 Series Helicopters

AD Number
89-23-14
Status
final_rule
Effective Date
Product Category
aircraft
Docket
89-ASW-26
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft MD Helicopters, Inc. 369 Airworthiness Directives; MCDONNELL DOUGLAS HELICOPTER COMPANY (MDHC) Model 369 Series Helicopters
aircraft MD Helicopters, Inc. 369A Airworthiness Directives; MCDONNELL DOUGLAS HELICOPTER COMPANY (MDHC) Model 369 Series Helicopters
aircraft MD Helicopters, Inc. 369D Airworthiness Directives; MCDONNELL DOUGLAS HELICOPTER COMPANY (MDHC) Model 369 Series Helicopters
aircraft MD Helicopters, Inc. 369E Airworthiness Directives; MCDONNELL DOUGLAS HELICOPTER COMPANY (MDHC) Model 369 Series Helicopters
aircraft MD Helicopters, Inc. 369F Airworthiness Directives; MCDONNELL DOUGLAS HELICOPTER COMPANY (MDHC) Model 369 Series Helicopters
aircraft MD Helicopters, Inc. 369FF Airworthiness Directives; MCDONNELL DOUGLAS HELICOPTER COMPANY (MDHC) Model 369 Series Helicopters
aircraft MD Helicopters, Inc. 369H Airworthiness Directives; MCDONNELL DOUGLAS HELICOPTER COMPANY (MDHC) Model 369 Series Helicopters
aircraft MD Helicopters, Inc. 369HE Airworthiness Directives; MCDONNELL DOUGLAS HELICOPTER COMPANY (MDHC) Model 369 Series Helicopters
aircraft MD Helicopters, Inc. 369HM Airworthiness Directives; MCDONNELL DOUGLAS HELICOPTER COMPANY (MDHC) Model 369 Series Helicopters
aircraft MD Helicopters, Inc. 369HS Airworthiness Directives; MCDONNELL DOUGLAS HELICOPTER COMPANY (MDHC) Model 369 Series Helicopters

Unsafe Condition

Fatigue failure of the control tubes could result in loss of control of the helicopter.

AI-generated summary from the source AD text. Verify against the official source before acting.

Required Actions

Inspect swaged ends of control tubes for cracks within 25 hours' time in service after the effective date and every 100 hours' time in service until paragraph (c) is completed. Replace cracked tubes with serviceable units before further flight. Inspect spare control tubes from inventory and reject cracked ones. Within 600 hours' time in service after the effective date, inspect and replace cracked tubes with FAA-approved -5 configuration parts or modify BASIC (BSC) tubes to the -5 configuration before reinstallation.

AI-generated summary from the source AD text. Verify against the official source before acting.

Compliance Time

Within 25 hours' time in service after the effective date of this AD, and at intervals of 100 hours' time in service until the requirements of paragraph (c) are accomplished

AI-generated summary from the source AD text. Verify against the official source before acting.

Affected Aircraft

MCDONNELL DOUGLAS HELICOPTER COMPANY (MDHC) Model 369 series helicopters with main rotor collective tube P/N 369A7009-BSC, longitudinal control tube P/N 369A7011-BSC, lateral control tube P/N 369A7012-BSC, and tail rotor control tube P/N 369A7007-BSC.

AI-generated summary from the source AD text. Verify against the official source before acting.

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

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