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94-16-02: Stabilizer Forward Attach Fitting

FAA order 94-16-02 is an airworthiness directive in force since September 19, 1994. The FAA's subject line: Stabilizer Forward Attach Fitting. It names Luscombe 8 Silvaire, Luscombe T-8: about 1,445 aircraft on the U.S. register today across them, though an order usually covers particular versions or serial numbers rather than every one. System: airframe structure.

What it applies to as the FAA lists it

Kind of product
Aircraft
Makes
Don Luscombe Aviation History Foundation, Inc.
Models
8, 8A, 8B, 8C, 8D, 8E, 8F, T-8F
On this site
Luscombe 8 Silvaire 1,420 registered
Luscombe T-8 25 registered

Dates and paperwork

In force since
September 19, 1994
Docket
93-CE-27-AD
Status
Current
The FAA's document
Read the order on the FAA's site

The FAA's summary their words, unchanged

This amendment supersedes AD 79-25-05, which currently requires repetitively inspecting the existing aluminum vertical stabilizer forward attach fitting for cracks on Luscombe Model 8 series airplanes, and replacing any cracked parts. Steel fittings are now available that, when installed, will eliminate the need for repeated removal and inspection of the aluminum fitting, which could result in damage to the fastener holes. This action requires replacing the existing aluminum fitting with a steel vertical stabilizer forward attach fitting on Luscombe Model 8 series airplanes that have round-tipped vertical stabilizer installations. The actions specified by this AD are intended to prevent failure of the vertical stabilizer as a result of a cracked fitting, which could result in loss of control of the airplane.

The order itself the regulatory text, as published

Show the full text (2,650 characters)
94-16-02 LUSCOMBE: Amendment 39-8991; Docket No. 93-CE-27-AD. Supersedes AD 79-25-05, Amendment 39-3630. Applicability: Model 8 Series airplanes (all serial numbers) that have round-tipped vertical stabilizer installations, 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 failure of the vertical stabilizer as a result of a cracked fitting, which could result in loss of control of the airplane, accomplish the following: (a) Replace the vertical stabilizer forward attach fitting, Luscombe part number (P/N) 28415, P/N 28444, or P/N 28453, with either Luscombe P/N 28455 manufactured by the Don Luscombe Aviation History Foundation (DLAHF); a welded steel fitting manufactured by the Univair Aircraft Corporation, P/N U28444; or an FAA-approved equivalent part. Accomplish this replacement in accordance with the procedures included in DLAHF ServiceRecommendation #1, dated November 28, 1993. (b) Special flight permits may be issued in accordance with sections 21.197 and 21.199 of the Federal Aviation Regulations (14 CFR 21.197 and 21.199) to operate the airplane to a location where the requirements of this AD can be accomplished. (c) An alternative method of compliance or adjustment of the compliance time that provides an equivalent level of safety may be approved by the Manager, Los Angeles Aircraft Certification Office (ACO), 3229 E. Spring Street, Long Beach, California 90806. The request shall be forwarded through an appropriate FAA Maintenance Inspector, who may add comments and then send it to the Manager, Los Angeles ACO. NOTE: Information concerning the existence of approved alternative methods of compliance with this AD, if any, may be obtained from the Los Angeles ACO. (d) The replacement required by this AD shall be done in accordance with the Don Luscombe Aviation History Foundation Service Recommendation #1, dated November 28, 1993. 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 may be obtained from the Don Luscombe Aviation History Foundation, P.O Box 63581, Phoenix, Arizona. Copies 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, 800 North Capitol Street, NW., suite 700, Washington, DC. (e) This amendment (39-8991) supersedes AD 79-25-05, Amendment 39-3630. (f) This amendment becomes effective on September 19, 1994.

Related safety bulletins advice on the same designs, not orders

2017-06-05CE-17-14 · Main Landing Gear: Lower Leg Internal Corrosion
2014-02-13CE-14-09 · Luscombe Model 8A Fuel System
1997-05-15ACE-97-03 ·

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 5, 2026. Connections as data: /graph/directive/94-16-02.json · aircraft systems.