AD 93-22-07

Airworthiness directive · Forward Cabin Door · Textron BAe.125 Series 800A, BAe.125 Series 800A (C-29A) and BAe.125 Series 800A (U-125)

Effective
December 20, 1993
Models
BAe.125 Series 800A, BAe.125 Series 800A (C-29A), BAe.125 Series 800A (U-125)
Data sheet
TCDSA3EU
Registered aircraft
84 matched by model
Product
Aircraft · Large airplane
Amendment
39-8731
Docket
93-NM-74-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 January 21, 2026.

On this page

The airworthiness directive

93-22-07 CORPORATE JETS LIMITED (FORMERLY BRITISH AEROSPACE): Amendment 39-8731. Docket 93-NM-74-AD.

Applicability: Model BAe 125-800A series airplanes, as listed in Corporate Jets Limited Service Bulletin SB.25-68-25A440A, dated August 19, 1992; certificated in any category.

Compliance: Required as indicated, unless accomplished previously.

To prevent the forward cabin door from closing during takeoff and landing, which could impede or hinder the ability of passengers and crew to exit through the main entrance door during an emergency evacuation, accomplish the following:

(a) Within 180 days after the effective date of this AD, replace the existing forward cabin door retainer catch assembly located in the upper luggage bay shelf with a new, improved forward cabin door retainer catch assembly, Modification No. 25A440A, in accordance with Corporate Jets Limited Service Bulletin SB.25-68-25A440A, dated August 19, 1992.

(b) As of the effective date of thisAD, no person shall install a catch assembly having part number 25-8DP1695 on any airplane.

(c) An alternative method of compliance or adjustment of the compliance time that provides an acceptable level of safety may be used if approved by the Manager, Standardization Branch, ANM-113, FAA, Transport Airplane Directorate. Operators shall submit their requests through an appropriate FAA Principal Maintenance Inspector, who may add comments and then send it to the Manager, Standardization Branch, ANM-113.

NOTE: Information concerning the existence of approved alternative methods of compliance with this AD, if any, may be obtained from the Standardization Branch, ANM-113.

(d) 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.

(e) The replacement shall be done in accordance with Corporate Jets Limited Service Bulletin SB.25-68-25A440A, dated August 19, 1992. 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 Corporate Jets, Inc., 22070 Broderick Drive, Sterling, Virginia 20166. Copies may be inspected at the FAA, Transport Airplane Directorate, 1601 Lind Avenue, SW., Renton, Washington; or at the Office of the Federal Register, 800 North Capitol Street, NW., suite 700, Washington, DC.

(f) This amendment becomes effective on December 20, 1993.

Affected TCDS · 1

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

Registered aircraft · 84

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
  • British Aerospace66 aircraft
  • Corporate Jets8 aircraft
  • Raytheon Corporate Jets8 aircraft
  • Raytheon2 aircraft
By year built
19841993
Registered aircraft by year built: 52 aircraft
19846
19855
19862
19874
19885
19897
19906
19911
19927
19939

32 with no year recorded

By model

Aircraft

See all 84 aircraft