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67-30-06: Engine Air Induction System

FAA order 67-30-06 is an airworthiness directive in force since December 22, 1967. The FAA's subject line: Engine Air Induction System. It names Piper PA-32 Cherokee Six, Lance and Saratoga: about 3,916 aircraft on the U.S. register today, though an order usually covers particular versions or serial numbers rather than every one. System: engine.

What it applies to as the FAA lists it

Kind of product
Aircraft
Makes
Piper Aircraft Inc.
Models
PA-32-300, PA-32S-300
On this site
Piper PA-32 Cherokee Six, Lance and Saratoga 3,916 registered

Dates and paperwork

In force since
December 22, 1967
Published
December 28, 1967 (signed December 22, 1967)
Docket
Unknown
Status
Current
The FAA's document
Read the order on the FAA's site

The order itself the regulatory text, as published

Show the full text (1,061 characters)
67-30-06 PIPER: Amdt. 39-508, Part 39, Federal Register November 8, 1967. Applies to Models PA-32-300, PA-32S-300 Series Airplanes. Serial Numbers 32-15, 32-40000 through 32- 40399. Compliance required within the next 50 hours' time in service after the effective date of this AD, unless already accomplished. To prevent the possibility of restricting air flow through the engine air induction system accomplish the following: (a) Replace the engine air inlet duct, Piper Part No. 457599 or 63633-50, with parts and per instructions contained in Piper Modification Kit 760159. (b) The compliance time may be adjusted up to a maximum of 10 hours to coincide with aircraft annual or 100-hour scheduled inspections. (c) Piper Service Bulletin No. 260 dated November 8, 1967, covers the same subject. Other means of compliance with the requirements of this directive may be utilized, if approved by the Chief, Engineering and Manufacturing Branch, Federal Aviation Administration, Southern Region. This amendment effective December 22, 1967.

Related safety bulletins advice on the same designs, not orders

2022-10-192022-20 · Wing Spar
2021-06-29AIR-21-10 · Wing, Attach Fittings (JASC 5740)
2021-03-30AIR-21-07 · WING SPAR, Verification of Correct Washers used with Wing Spar Attach Bolts
2018-11-21SW-18-31 · NAVIGATION, ATTITUDE, AND DIRECTION DATA SYSTEM
2015-12-02CE-11-12R1 · Wings - PA-28, PA-32, PA-34, and PA-44 Rear Spar Corrosion at Fuselage Attach Fitting

Source: FAA Dynamic Regulatory System, airworthiness directives. The FAA's document is the authority; the register counts are this site's, from the FAA register of October 30, 2026. Connections as data: /graph/directive/67-30-06.json · aircraft systems.