AD 47-06-07

Airworthiness directive · Fire Extinguishing System · Boeing DC3-G102, DC3-G102A, DC3-G103A and 11 more

Models
DC3-G102, DC3-G102A, DC3-G103A, DC3-G202A, DC3A-S1C3G, DC3A-S1CG and 8 more
Registered aircraft
61 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

47-06-07 DOUGLAS: (Was Service Note 12 of AD-618-3, Supplement 1; Service Note 15 of AD-669-3, Supplement 1.) Applies to All DC3 Series Aircraft.

To be accomplished not later than the next periodic inspection, or in the case of scheduled air carrier aircraft, at the next major inspection.

Check the pull necessary to trip the trigger on the CO2 fire extinguishing system. If the trigger pull exceeds 50 pounds due to wear of the aluminum conduit covering the fire extinguisher release cable, this conduit must be replaced immediately. This procedure is to be repeated at each specified inspection period until such time as the aluminum cable conduit is replaced by stainless steel conduit.

(Douglas Service Bulletin DC3 No. 246 dated November 22, 1946, covers this same subject.)

Affected TCDS · 2

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

Registered aircraft · 61

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

By aircraft maker
  • Douglas61 aircraft
By year built
19361987
Registered aircraft by year built: 48 aircraft
19362
19371
19391
19404
19412
19428
19439
194416
19453
19491
19871

13 with no year recorded

By model

Aircraft

See all 61 aircraft