AD 81-01-01

Airworthiness directive · Propeller Deice Relay · Piper PA-31T and PA-31T1

Effective
February 27, 1981
Published
February 26, 1981
Issued
February 13, 1981
Models
PA-31T, PA-31T1
Data sheet
TCDSA8EA
Registered aircraft
151 matched by model
Product
Aircraft · Small airplane
Amendment
39-4051

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

81-01-01 PIPER: Amendment 39-4051. Applies to Piper PA-31T S/N 8120008, 8120009, 8120010, and 8120013, and Piper PA-31T1 airplanes S/N 8104007, 8104008, 8104009, 8104010, 8104011, 8104012, and 8104013. Compliance required as indicated, unless already accomplished.

To prevent loss of the propeller and intake lip deicing functions, comply as follows:

Prior to further flight in known icing conditions, inspect for proper propeller and intake lip deice power relay in accordance with Piper telegraphic form letter #31-28, dated December 22, 1980, or equivalent, approved by Chief, Engineering and Manufacturing Branch. If (P/N 484247) relay is installed, check to insure that correct D.C. relay PRD7DYD (24 VDC) is installed. If the latter relay is not installed, remove and install proper relay prior to further flight in known icing conditions.

This amendment is effective February 27, 1981, and was effective upon receipt by all recipients of the letter dated December 24, 1980.

Affected TCDS · 1

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

Registered aircraft · 151

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
  • Piper151 aircraft
By year built
19741984
Registered aircraft by year built: 114 aircraft
19742
19752
19766
197710
197824
197923
198020
198117
19824
19831
19845

37 with no year recorded

By model

Aircraft

See all 151 aircraft