AD 81-02-07

final rule
Data completeness: 70%

Airworthiness Directives; McDONNELL DOUGLAS DC-10 Series Airplanes

AD Number
81-02-07
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft The Boeing Company DC-10-10 Airworthiness Directives; McDONNELL DOUGLAS DC-10 Series Airplanes
aircraft The Boeing Company DC-10-10F Airworthiness Directives; McDONNELL DOUGLAS DC-10 Series Airplanes
aircraft The Boeing Company DC-10-15 Airworthiness Directives; McDONNELL DOUGLAS DC-10 Series Airplanes
aircraft The Boeing Company DC-10-30 Airworthiness Directives; McDONNELL DOUGLAS DC-10 Series Airplanes
aircraft The Boeing Company DC-10-30F (KC-10A, KDC-10) Airworthiness Directives; McDONNELL DOUGLAS DC-10 Series Airplanes
aircraft The Boeing Company DC-10-40 Airworthiness Directives; McDONNELL DOUGLAS DC-10 Series Airplanes
aircraft The Boeing Company DC-10-40F Airworthiness Directives; McDONNELL DOUGLAS DC-10 Series Airplanes

Unsafe Condition

Stress corrosion cracking of the upper and lower cargo door spool fitting attach bolts.

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

Required Actions

Inspect, lubricate, replace as necessary, and seal the cargo door latch spool fitting attach bolts in accordance with an approved method. For fuselages 1-125, compliance is required within 12 months after the effective date. For fuselage 126 and subsequent, compliance is required within 24 months after the effective date.

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

Compliance Time

within 12 months after the effective date of this AD (for fuselages 1-125) and within 24 months after the effective date of this AD (for fuselage 126 and subsequent)

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

Affected Aircraft

McDONNELL DOUGLAS DC-10 series airplanes certificated in all categories, including models DC-10-10, DC-10-10F, DC-10-15, DC-10-30, DC-10-30F (KC-10A, KDC-10), DC-10-40, DC-10-40F, with fuselages 1-125 and 126 and subsequent.

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

This site is not affiliated with or endorsed by the FAA. Always verify with official sources.

View Official Source ↗ Find More ADs for The Boeing Company DC-10-10

Related Airworthiness Directives

2008-06-21 R1

final rule

Airworthiness Directives; McDonnell Douglas Corporation Model DC- 10-10 and DC-10-10F Airplanes, Model DC-10-15 Airplanes, Model DC-10-30 and DC-10-30F (KC-10A and KDC-10) Airplanes, Model DC-10-40 and DC-10- 40F Airplanes, Model MD-10-10F and MD-10-30F Airplanes, and Model MD-11 and MD-11F Airplanes

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Effective: Dec 10, 2009 Category: aircraft

2003-17-07 R1

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Effective: Sep 24, 2003 Category: aircraft

99-08-22

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Airworthiness Directives; McDonnell Douglas Model DC-10 Series Airplanes and KC-10 (Military) Airplanes

Unsafe Condition: Rear Spar Cap Of Horizontal Stabilizer

Effective: May 21, 1999 Category: aircraft

99-06-08

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(Correction) Airworthiness Directives; McDonnell Douglas Model DC-10 and MD-11 Series Airplanes, and KC-10 (Military) Series Airplanes

Unsafe Condition: Forward Trunnion Bolt

Effective: Apr 16, 1999 Category: aircraft

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