AD 60-24-01

Active

Fuel Pressure Relief Valve

Key Information
60-24-01
Active
December 13, 1960
Not specified
Unknown
N/A
Applicability
["Aircraft"]
["Large Airplane"]
Lockheed Martin Corporation
188A 188C
Regulatory Text

60-24-01 LOCKHEED: Amdt. 222 Part 507 Federal Register November 15, 1960. Applies to All 188 Aircraft.

Compliance required within 5,000 hours' time in service after the effective date of this directive.

To provide protection against possible over-pressurization of fuel tanks during refueling, the following modification is required unless already accomplished:

Install pressure relief overflow valves in each fuel tank. Lockheed overflow valves P/N 634114-7 or -9 are satisfactory for this purpose. (Lockheed Service Bulletin 188/SB-422 covers this subject.)

This directive effective December 13, 1960.

AD Assistant

Get AI-powered answers about this AD, check applicability, and find compliance steps.

Sign Up to Unlock
References
This information is not available.
--- - Part 39
FAA Documents