AD 92-06-05 R1

final rule
Data completeness: 70%

BRITISH AEROSPACE Model DH/BH/HS/BAe 125, BAe 125-1000A Series Airplanes

AD Number
92-06-05 R1
Status
final_rule
Effective Date
Product Category
aircraft
Docket
91-NM-209-AD
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft Textron Aviation Inc. BAe.125 Series 1000B BRITISH AEROSPACE Model DH/BH/HS/BAe 125, BAe 125-1000A Series Airplanes
aircraft Textron Aviation Inc. BAe.125 Series 800A BRITISH AEROSPACE Model DH/BH/HS/BAe 125, BAe 125-1000A Series Airplanes
aircraft Textron Aviation Inc. BAe.125 Series 800A (C-29A) BRITISH AEROSPACE Model DH/BH/HS/BAe 125, BAe 125-1000A Series Airplanes
aircraft Textron Aviation Inc. BAe.125 Series 800A (U-125) BRITISH AEROSPACE Model DH/BH/HS/BAe 125, BAe 125-1000A Series Airplanes
aircraft Textron Aviation Inc. BAe.125 Series 800B BRITISH AEROSPACE Model DH/BH/HS/BAe 125, BAe 125-1000A Series Airplanes
aircraft Textron Aviation Inc. BH.125 Series 400A BRITISH AEROSPACE Model DH/BH/HS/BAe 125, BAe 125-1000A Series Airplanes
aircraft Textron Aviation Inc. BH.125 Series 600A BRITISH AEROSPACE Model DH/BH/HS/BAe 125, BAe 125-1000A Series Airplanes
aircraft Textron Aviation Inc. DH.125 Series 1A BRITISH AEROSPACE Model DH/BH/HS/BAe 125, BAe 125-1000A Series Airplanes
aircraft Textron Aviation Inc. DH.125 Series 1A-522 BRITISH AEROSPACE Model DH/BH/HS/BAe 125, BAe 125-1000A Series Airplanes
aircraft Textron Aviation Inc. DH.125 Series 1A/R-522 BRITISH AEROSPACE Model DH/BH/HS/BAe 125, BAe 125-1000A Series Airplanes

Unsafe Condition

Reduced structural integrity of the fuselage and subsequent decompression of the airplane due to the presence of washers or spotface under nuts on the nose landing gear bay sidewalls, or damage and cracks caused by nuts or washers.

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

Required Actions

Perform a visual inspection of the nose landing gear bay sidewalls to detect washers or spotface under nuts, and inspect for web damage caused by them. Blend out non-cracking damage prior to further flight. Conduct a dye penetrant or eddy current inspection for cracks on the sidewalls and repair any cracks as approved. Follow British Aerospace Service Bulletin 53-73, Revision 2.

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

Compliance Time

Prior to the accumulation of 4,000 landings, or within 60 days after the effective date of this AD (April 21, 1992), whichever occurs later.

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

Affected Aircraft

British Aerospace Model DH/BH/HS/BAe 125 series airplanes, except Model BAe 125-1000A series airplanes, certificated in any category.

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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