AD 74-23-06

final rule
Data completeness: 70%

Airworthiness Directives; MCDONNELL DOUGLAS DC-8 Series Airplanes

AD Number
74-23-06
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft The Boeing Company DC-8-11 Airworthiness Directives; MCDONNELL DOUGLAS DC-8 Series Airplanes
aircraft The Boeing Company DC-8-12 Airworthiness Directives; MCDONNELL DOUGLAS DC-8 Series Airplanes
aircraft The Boeing Company DC-8-21 Airworthiness Directives; MCDONNELL DOUGLAS DC-8 Series Airplanes
aircraft The Boeing Company DC-8-31 Airworthiness Directives; MCDONNELL DOUGLAS DC-8 Series Airplanes
aircraft The Boeing Company DC-8-32 Airworthiness Directives; MCDONNELL DOUGLAS DC-8 Series Airplanes
aircraft The Boeing Company DC-8-33 Airworthiness Directives; MCDONNELL DOUGLAS DC-8 Series Airplanes
aircraft The Boeing Company DC-8-41 Airworthiness Directives; MCDONNELL DOUGLAS DC-8 Series Airplanes
aircraft The Boeing Company DC-8-42 Airworthiness Directives; MCDONNELL DOUGLAS DC-8 Series Airplanes
aircraft The Boeing Company DC-8-43 Airworthiness Directives; MCDONNELL DOUGLAS DC-8 Series Airplanes
aircraft The Boeing Company DC-8-51 Airworthiness Directives; MCDONNELL DOUGLAS DC-8 Series Airplanes

Unsafe Condition

Failure to maintain minimum N2 engine rotor speed at certain altitudes and airspeeds, and improper fuel pump operation during descent could lead to engine surge, flameout, or loss of engine power.

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

Required Actions

Revise the Airplane Flight Manual (AFM) to include new fuel management procedures requiring main tank pumps in boost and feed position before descent. Revise engine operation limitations to maintain a minimum N2 rotor speed of 62% at altitudes above 6,000 feet MSL and below 200 knots. Update emergency procedures for engine non-response to throttle advancement, including throttle advance, anti-ice off, airspeed increase, ignition override, bleed reduction, and electrical load removal.

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

Compliance Time

within 24 hours after receipt of this telegram

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

Affected Aircraft

McDonnell Douglas DC-8 series airplanes with Pratt and Whitney JT3D engines, including models DC-8-11, DC-8-12, DC-8-21, DC-8-31, DC-8-32, DC-8-33, DC-8-41, DC-8-42, DC-8-43, DC-8-51, and others as listed.

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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