# AD 92-25-11: Hydraulic Accumulator

- 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: January 12, 1993
- Superseded by: Nothing supersedes this AD
- Product type: Aircraft, Large airplane
- Amendment: 39-8425
- Docket: 92-NM-153-AD
- Registered aircraft: 111 may be affected, by airframe or engine model (OpenAirDocs)
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/B171CFEDCD4A8B1486256A09005E337A.0001
- DRS record last changed: January 21, 2026
- Page: https://openairdocs.org/ad/92-25-11

## The airworthiness directive

92-25-11 BRITISH AEROSPACE: Amendment 39-8425. Docket No. 92-NM-153-AD.

Applicability: All Model DH/BH/HS/BAe 125 series airplanes, excluding Model BAe 125-1000A, certificated in any category.

Compliance: Required as indicated, unless accomplished previously.

To prevent rupture of the hydraulic accumulator, failure of one or more hydraulic systems, fire in the tailcone area, and possible structural damage to the aft fuselage, accomplish the following:

  (a) Within 6 months after the effective date of this AD, accomplish paragraphs (a)(1) and (a)(2) of this AD, in accordance with British Aerospace Service Bulletin SB.29-89-3269A, dated May 22, 1992.

  (1) Install a placard on the hydraulic box front cover, stating that accumulators must be charged with nitrogen.

  (2) Review the airplane maintenance records to confirm that the hydraulic accumulators are charged with nitrogen. If these records do not indicate that the accumulators are charged with nitrogen, prior to further flight, discharge the accumulators and recharge them with nitrogen.

  (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: 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 of the placard and the review, discharge and recharge of the accumulator shall be done in accordance with British Aerospace Service Bulletin SB.29-89-3269A, dated May 22, 1992. (NOTE: The issue date of that service bulletin is indicated only on "Page 1 of 7"; no other page of the document is dated.) 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 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 Office of the Federal Register, 800 North Capitol Street, NW., suite 700, Washington, DC.

  (e) This amendment becomes effective on January 12, 1993.

## 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/92-25-11/models.md
Every aircraft: https://openairdocs.org/ad/92-25-11/aircraft.md

Its text cites no advisory circulars or STCs.

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