AD 88-17-04

final rule
Data completeness: 70%

Airworthiness Directives; SCHWEIZER AIRCRAFT CORPORATION (MCDONNELL DOUGLAS HELICOPTER COMPANY, HUGHES HELICOPTERS, INC). Models 269A, TH-55A, 269A-1, 269B, and 269C Helicopter

AD Number
88-17-04
Status
final_rule
Effective Date
Product Category
aircraft
Docket
88-ASW-26
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft Schweizer Aircraft Corporation 269A Airworthiness Directives; SCHWEIZER AIRCRAFT CORPORATION (MCDONNELL DOUGLAS HELICOPTER COMPANY, HUGHES HELICOPTERS, INC). Models 269A, TH-55A, 269A-1, 269B, and 269C Helicopter
aircraft Schweizer Aircraft Corporation 269A-1 Airworthiness Directives; SCHWEIZER AIRCRAFT CORPORATION (MCDONNELL DOUGLAS HELICOPTER COMPANY, HUGHES HELICOPTERS, INC). Models 269A, TH-55A, 269A-1, 269B, and 269C Helicopter
aircraft Schweizer Aircraft Corporation 269B Airworthiness Directives; SCHWEIZER AIRCRAFT CORPORATION (MCDONNELL DOUGLAS HELICOPTER COMPANY, HUGHES HELICOPTERS, INC). Models 269A, TH-55A, 269A-1, 269B, and 269C Helicopter
aircraft Schweizer Aircraft Corporation 269C Airworthiness Directives; SCHWEIZER AIRCRAFT CORPORATION (MCDONNELL DOUGLAS HELICOPTER COMPANY, HUGHES HELICOPTERS, INC). Models 269A, TH-55A, 269A-1, 269B, and 269C Helicopter

Unsafe Condition

Cracks and surface defects in the aft cluster fittings (P/N 269A2234-3 and 269A2235-3) could result in loss of the tail boom support strut and tail boom, leading to loss of the helicopter.

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

Required Actions

Inspect aft cluster fittings for cracks and surface defects using specified procedures; install 'NO STEP' placards; replace cracked or non-compliant fittings before further flight; repeat inspections at intervals not exceeding 100 hours' time in service until compliance is achieved.

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

Compliance Time

Within the next 25 hours' time in service after the effective date of this AD, and repeat inspections at intervals not to exceed 100 hours' time in service from the previous inspections.

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

Affected Aircraft

Schweizer Aircraft Corporation Models 269A, TH-55A (all S/N's operated in civil use), 269A-1, 269B, and 269C (S/N's 0004 through 1289) helicopters.

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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