AD 75-17-21

final rule
Data completeness: 70%

Airworthiness Directives; HAWKER SIDDELEY AVIATION, LTD Models DH-125 and BH-125 Airplanes

AD Number
75-17-21
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft Textron Aviation Inc. BH.125 Series 400A Airworthiness Directives; HAWKER SIDDELEY AVIATION, LTD Models DH-125 and BH-125 Airplanes
aircraft Textron Aviation Inc. BH.125 Series 600A Airworthiness Directives; HAWKER SIDDELEY AVIATION, LTD Models DH-125 and BH-125 Airplanes
aircraft Textron Aviation Inc. DH.125 Series 1A Airworthiness Directives; HAWKER SIDDELEY AVIATION, LTD Models DH-125 and BH-125 Airplanes
aircraft Textron Aviation Inc. DH.125 Series 1A-522 Airworthiness Directives; HAWKER SIDDELEY AVIATION, LTD Models DH-125 and BH-125 Airplanes
aircraft Textron Aviation Inc. DH.125 Series 1A/R-522 Airworthiness Directives; HAWKER SIDDELEY AVIATION, LTD Models DH-125 and BH-125 Airplanes
aircraft Textron Aviation Inc. DH.125 Series 1A/S-522 Airworthiness Directives; HAWKER SIDDELEY AVIATION, LTD Models DH-125 and BH-125 Airplanes
aircraft Textron Aviation Inc. DH.125 Series 3A Airworthiness Directives; HAWKER SIDDELEY AVIATION, LTD Models DH-125 and BH-125 Airplanes
aircraft Textron Aviation Inc. DH.125 Series 3A/R Airworthiness Directives; HAWKER SIDDELEY AVIATION, LTD Models DH-125 and BH-125 Airplanes
aircraft Textron Aviation Inc. DH.125 Series 3A/RA Airworthiness Directives; HAWKER SIDDELEY AVIATION, LTD Models DH-125 and BH-125 Airplanes
aircraft Textron Aviation Inc. DH.125 Series 400A Airworthiness Directives; HAWKER SIDDELEY AVIATION, LTD Models DH-125 and BH-125 Airplanes

Unsafe Condition

Rapid loss of cabin pressurization due to displacement of Hellerman type cabin pressure seal bungs.

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

Required Actions

Inspect all Hellerman type cabin pressure seal bungs for displacement within 50 hours time in service after the effective date. Rework as necessary per Maintenance Manual instructions and conduct a cabin leak rate check after reinstallation.

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

Compliance Time

within 50 hours time in service after the effective date of this AD

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

Affected Aircraft

HAWKER SIDDELEY AVIATION, LTD Models DH-125 and BH-125 airplanes certificated in all categories.

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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