# AD 92-16-12 R1: Tail Cone Vents - Type: Airworthiness directive - Status: Current - Products: Textron BAe.125 Series 1000B, BAe.125 Series 800A, BAe.125 Series 800A (C-29A), BAe.125 Series 800A (U-125), BAe.125 Series 800B, BH.125 Series 400A, BH.125 Series 600A, DH.125 Series 1A, DH.125 Series 1A-522, DH.125 Series 1A/R-522, DH.125 Series 1A/S-522, DH.125 Series 3A and 29 more - Effective: September 28, 1992 - Superseded by: Nothing supersedes this AD - Product type: Aircraft, Large airplane - Amendment: 39-8702 - Docket: 93-NM-157-AD - Registered aircraft: 111 may be affected, by airframe or engine model (OpenAirDocs) - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/2B64B9FFBC4ED07C86256A09005E29ED.0001 - DRS record last changed: January 21, 2026 - Page: https://openairdocs.org/ad/92-16-12-R1 ## The airworthiness directive 92-16-12 R1 BRITISH AEROSPACE: Amendment 39-8702. Docket 93-NM-157-AD. Revises AD 92-16-12, Amendment 39-8321. Applicability: Model DH/BH/HS/BAe 125 series airplanes, as listed in British Aerospace Service Bulletin SB.53-74-3193C&D, Revision 1, dated March 12, 1992; certificated in any category. NOTE 1: Model BAe 125-1000A airplanes are not affected by this AD. Compliance: Required within 4 months after the effective date of this AD, unless accomplished previously. To prevent fire in the tail cone, accomplish the following: (a) Install fluid vent masts on the undercarriage fairing, and plug certain existing vent holes, in accordance with British Aerospace Service Bulletin SB.53-74-3193C&D, dated January 7, 1992; or Revision 1, dated March 12, 1992. (b) 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 2: Information concerning the existence of approved alternative methods of compliance with this AD, if any, may be obtained from the Standardization Branch, ANM-113. (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) The installation shall be done in accordance with British Aerospace Service Bulletin SB.53-74-3193C&D, dated January 7, 1992; or British Aerospace Service Bulletin SB.53-74-3193C&D, Revision 1, dated March 12, 1992. (The issuance date of Revision 1 of this service bulletin appears only on page 1 of the document.) The incorporation by reference of the former service bulletin was approved previously by the Directorof the Federal Register, in accordance with 5 U.S.C. 552(a) and 1 CFR Part 51, as of September 28, 1992 (57 FR 38266, August 24,1992). The incorporation by reference of the latter service bulletin 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 British Aerospace, PLC, Librarian for Service Bulletins, P.O. Box 17414, Dulles International Airport, Washington, DC. 20041-0414. Copies may be inspected at the FAA, Transport Airplane Directorate, 1601 Lind Avenue SW., Renton, Washington; or at the Federal Register, 800 North Capitol Street, NW., suite 700, Washington, DC. (e) This amendment is effective on September 28, 1992. ## Affected data sheets (1) (OpenAirDocs) The type certificate data sheets whose models the AD names. - [TCDS A3EU](https://openairdocs.org/tcds/A3EU): Textron Aviation Inc.; names 39 of 50 models: HS.125 Series 3B/RB, HS.125 Series 401B, HS.125 Series 600A, HS.125 Series 600B/2, HS.125 Series 403A(C), HS.125 Series 600B/1, HS.125 Series 700A, DH.125 Series 1A/R-522… ## Registered aircraft it may apply to (OpenAirDocs) Matched by airframe and engine model; the AD's applicability may narrow it by serial number, part number or equipment. - Aircraft: 111 (111 by airframe model, 0 by engine model) - Makers: British Aerospace 80, Hawker Siddeley 11, Corporate Jets 8, Raytheon Corporate Jets 8, Raytheon 3, Hawker Beechcraft 1 Models with the most aircraft: - [British Aerospace BAE 125 SERIES 800A](https://openairdocs.org/model/british-aerospace-bae-125-series-800a): 61 aircraft (airframe model) - [British Aerospace HS 125-700A](https://openairdocs.org/model/british-aerospace-hs-125-700a): 14 aircraft (airframe model) - [Corporate Jets BAE 125-800A](https://openairdocs.org/model/corporate-jets-bae-125-800a): 8 aircraft (airframe model) - [Raytheon Corporate Jets BAE 125-800A](https://openairdocs.org/model/raytheon-corporate-jets-bae-125-800a): 8 aircraft (airframe model) - [Hawker Siddeley HS.125 SERIES 700A](https://openairdocs.org/model/hawker-siddeley-hs-125-series-700a): 7 aircraft (airframe model) - [British Aerospace BAE 125-800A](https://openairdocs.org/model/british-aerospace-bae-125-800a): 5 aircraft (airframe model) - [Hawker Siddeley BH.125-400A](https://openairdocs.org/model/hawker-siddeley-bh-125-400a): 2 aircraft (airframe model) - [Hawker Siddeley DH.125-3A/RA](https://openairdocs.org/model/hawker-siddeley-dh-125-3a-ra): 2 aircraft (airframe model) - [Raytheon BAE 125-800A](https://openairdocs.org/model/raytheon-bae-125-800a): 2 aircraft (airframe model) - [Hawker Beechcraft BAE 125-800B](https://openairdocs.org/model/hawker-beechcraft-bae-125-800b): 1 aircraft (airframe model) - [Raytheon HS 125-700A](https://openairdocs.org/model/raytheon-hs-125-700a): 1 aircraft (airframe model) All 12 models: https://openairdocs.org/ad/92-16-12-R1/models.md Every aircraft: https://openairdocs.org/ad/92-16-12-R1/aircraft.md Its text cites no advisory circulars or STCs. --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.