AD 60-08-02

final rule
Data completeness: 60%

Airworthiness Directives; BOEING All Model 75 Series Aircraft

AD Number
60-08-02
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft Boeing Airplane Company, Wichita Division 75 (Army PT-13) Airworthiness Directives; BOEING All Model 75 Series Aircraft
aircraft Boeing Airplane Company, Wichita Division A75 (Army PT-13A, -13B, -13C) Airworthiness Directives; BOEING All Model 75 Series Aircraft
aircraft Boeing Airplane Company, Wichita Division A75J1 (Army PT-18) Airworthiness Directives; BOEING All Model 75 Series Aircraft
aircraft Boeing Airplane Company, Wichita Division A75L3 Airworthiness Directives; BOEING All Model 75 Series Aircraft
aircraft Boeing Airplane Company, Wichita Division A75L300 Airworthiness Directives; BOEING All Model 75 Series Aircraft
aircraft Boeing Airplane Company, Wichita Division A75N1 (Army PT-17, -17A, Navy N2S-1, -4) Airworthiness Directives; BOEING All Model 75 Series Aircraft
aircraft Boeing Airplane Company, Wichita Division B75 (Navy N2S-5) Airworthiness Directives; BOEING All Model 75 Series Aircraft
aircraft Boeing Airplane Company, Wichita Division B75N1 (Navy N2S-3) Airworthiness Directives; BOEING All Model 75 Series Aircraft
aircraft Boeing Airplane Company, Wichita Division D75N1 (Army PT-27) Airworthiness Directives; BOEING All Model 75 Series Aircraft
aircraft Boeing Airplane Company, Wichita Division E75 (Army PT-13D, Navy N2S-5, PT-13D/N2S-5) Airworthiness Directives; BOEING All Model 75 Series Aircraft

Unsafe Condition

Cracked fuselage longerons and fuselage diagonal bracing in the vicinity of the lower wing front spar attach fittings

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

Required Actions

Visually inspect the fuselage longerons and fuselage diagonal bracing for cracks near the lower wing front spar attach fittings. Repair or replace all cracked structural members in accordance with CAR 18.

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

Compliance Time

not later than June 1, 1960, and at each 100 hours' time in service thereafter

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

Affected Aircraft

Boeing Airplane Company, Wichita Division Model 75 Series Aircraft operated in Restricted Category with a gross weight exceeding 3,200 pounds

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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