AD 63-27-03

Airworthiness directive · Landing Gear Retraction Motor Circuit · Piper PA-24 and PA-24-250

Effective
January 23, 1964
Published
December 24, 1963
Issued
December 17, 1963
Models
PA-24, PA-24-250
Data sheet
TCDS1A15
Registered aircraft
1,567 matched by model
Product
Aircraft · Small 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 November 21, 2025.

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The airworthiness directive

63-27-03 PIPER: Amdt. 661 Part 507 Federal Register December 24, 1963. Applies to All Models PA-24 and PA-24-250 Aircraft, Which Have 25 Ampere Circuit Breakers in the Landing Gear Retraction Motor Circuit.

Compliance required within the next 100 hours' time in service after the effective date of this AD.

Inadvertent tripping of the 25 ampere landing gear retraction circuit breaker has resulted in stoppage of the landing gear retraction mechanism in other than the fully extended position. Therefore, in order to eliminate this condition, with its associated hazard of partial-gear-down landing accidents, the 25 ampere circuit breaker in the landing gear retraction motor circuit must be replaced with a 30 ampere circuit breaker, Piper P/N 454661, or FAA approved equivalent.

(Piper Service Letter No. 356, dated March 31, 1961, pertains to this same subject.)

This directive effective January 23, 1964.

Affected TCDS · 1

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

Registered aircraft · 1,567

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
  • Piper1,567 aircraft
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19541971
Registered aircraft by year built: 1,332 aircraft
19541
19561
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1958203
1959345
1960263
1961216
1962139
1963109
196444
19652
19681
19691
19711

235 with no year recorded

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