AD 47-10-19

Airworthiness directive · Cabin Heater Fuel Solenoid Valve · Lockheed 49-46

Model
49-46
Data sheet
TCDSA-763
Registered aircraft
1 matched by model
Product
Aircraft · Large airplane

Unofficial copy of the text in the FAA’s Dynamic Regulatory System. The FAA’s own copy is the authoritative one. DRS record last changed May 30, 2024.

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The airworthiness directive

47-10-19 LOCKHEED: (Was Mandatory Note 21 of AD-763-3.) Applies to All Model 49 Serials Up to and Including 2088, Except as Noted.

Compliance required not later than 100 hours of operation after June 10, 1947.

(a) In each cabin heater installation, relocate and waterproof the fuel solenoid valve and replace and reroute the fuel pump bypass line.

(LAC Service Bulletin 49/SB-73 covers this same subject.)

(b) In zone 2 of each nacelle, install heat protective shield between propeller feathering line and cowl diaphragm. Applies to all serials up to and including 2082.

(LAC Service Bulletin 49/SB-150 covers this same subject.)

(c) In each outboard nacelle main junction box, replace existing mounting nuts (tinnerman) and PK screws with AN 366 nuts and NAS 221 screws.

(LAC Service Bulletin 49/SB-152 covers this same subject.)

(d) Drill one 1/4-inch drain hole on lower center line of spinner fairing lower panel assembly for each engine.

(LAC Service Instruction 49/SI-95 covers this same subject.)

Affected TCDS · 1

The type certificate data sheets for the models this AD names, matched by model and maker.

Registered aircraft · 1

Registered aircraft whose airframe or engine model this AD names. Matched by model only, so check each against the AD’s applicability.

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