AD 91-21-09

Airworthiness directive · Air Induction System · Piper PA-24-260

Effective
November 29, 1991
Published
October 28, 1991
Issued
September 25, 1991
Model
PA-24-260
Data sheet
TCDS1A15
Registered aircraft
590 matched by model
Product
Aircraft · Small airplane
Amendment
39-8056
Docket
91-CE-41-AD

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

91-21-09 PIPER AIRCRAFT CORPORATION: Amendment 39-8056. Docket No. 91- CE-41-AD. Supersedes AD 91-02-06.

Applicability: Model PA-24-260 airplanes (serial number (S/N) 24-3642, S/N 24-4000 through 24-4255, S/N 24-4257 through 24-4782, and S/N 24-4784 through 24-4803) that are equipped with nonturbocharged fuel-injected engines, certificated in any category.

Compliance: Required within the next 100 hours time-in-service after the effective date of this AD, unless already accomplished.

To prevent inadvertent engine stoppage while flying in weather conditions conducive to induction system icing, accomplish the following:

(a) Modify the airplane by installing a manually controlled heated alternate air induction system in accordance with the instructions in either Piper Service Bulletin No. 861, dated May 4, 1987, or Supplemental Type Certificate SA2694CE.

(b) The installation of a manually controlled heated alternate air induction system does not constituteapproval for flight in icing conditions.

(c) Special flight permits may be issued in accordance with FAR 21.197 and 21.199 to operate the airplane to a location where the requirements of this AD can be accomplished.

(d) An alternative method of compliance that provides an equivalent level of safety may be approved by the Manager, Atlanta Aircraft Certification Office, 1669 Phoenix Parkway, Suite 210C, Atlanta, Georgia 30349. The request should be forwarded through an appropriate FAA Maintenance Inspector, who may add comments and then send it to the Manager, Atlanta Aircraft Certification Office.

(e) The modification required by this AD shall be done in accordance with Piper Service Bulletin No. 861, dated May 4, 1987. This incorporation by reference was approved by the Director of the Federal Register in accordance with 5 U.S.C. 552(a) and 1 CFR Part 51. Copies of Piper Service Bulletin No. 861, dated May 4, 1987, may be obtained from the Piper Aircraft Corporation, 2926 Piper Drive, Vero Beach, Florida 32960. Copies of the service bulletin may be inspected at the FAA, Central Region, Office of the Assistant Chief Counsel, Room 1558, 601 E. 12th Street, Kansas City, Missouri, or at the Office of the Federal Register, 1100 L Street, NW, Room 8401, Washington, DC.

Airworthiness Directive 91-21-09 supersedes Amendment 39-6849, AD 91-02-06.

This amendment (39-8056, AD 91-21-09) becomes effective on November 29, 1991.

Affected TCDS · 1

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

Registered aircraft · 590

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
  • Piper590 aircraft
By year built
19641978
Registered aircraft by year built: 517 aircraft
196451
1965130
1966156
196747
196830
196960
197011
197121
197210
19781

73 with no year recorded

By model

Aircraft

See all 590 aircraft