AD 66-13-04

Active

Pressure Control Static Air System

Key Information
66-13-04
Active
May 17, 1966
Not specified
Unknown
39-237
Applicability
["Aircraft"]
["Large Airplane"]
Learjet Inc.
23 24
Regulatory Text

66-13-04 LEARJET: Amdt. 39-237 Part 39 Federal Register May 17, 1966. Applies to Models 23 and 24 Airplanes.

Compliance required before further flight, unless already accomplished, except that the airplane may be flown to a base where the repair can be performed, provided the following restrictions are contained on a placard in clear view of the pilot:

"(a) No passengers may be carried.

"(b) Monitor the cabin pressure indicator for proper pressurization control. If automatic and/or manual control of the cabin pressure is not properly effective:

"(1) Turn air bleed off to shutoff bleed air.

"(2) Reduce power to reduce bleed air pressure as necessary.

"(3) Don oxygen masks.

"(4) Expedite descent to a safe altitude."

Modify the pressure control static air system in accordance with Lear Service Kit SK23/24-230 or an equivalent approved by the Chief, Engineering and Manufacturing Branch, FAA Central Region.

This directive effective upon publication in the Federal Register for all persons except those to whom it was made effective immediately by telegram dated May 10, 1966.

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References
This information is not available.
--- - Part 39
FAA Documents