82-11-03 R1: Elevator Pitch Trim Switch
FAA order 82-11-03 R1 is an airworthiness directive in force since October 12, 1982. The FAA's subject line: Elevator Pitch Trim Switch. It names Hawker Siddeley HS.125 SERIES 700A: about 7 aircraft on the U.S. register today, though an order usually covers particular versions or serial numbers rather than every one. System: flight controls.
What it applies to as the FAA lists it
- Kind of product
- Aircraft
- Makes
- Textron Aviation Inc.
- Models
- HS.125 Series 700A, HS.125 Series 700B
- On this site
- Hawker Siddeley HS.125 SERIES 700A 7 registered
Dates and paperwork
- In force since
- October 12, 1982
- 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 (1,415 characters)
82-11-03 R1 BRITISH AEROSPACE: Amendment 39-4383 as amended by Amendment 39- 4470. Applies to Model HS-125 Series 700 and all variants serial numbers 25/7001, 7007, 7010, 7013, 7020, 7022, 7025, 7028, 7031, and 7034, 7037, 7040, 7046; NA 0201 - NA 0240 inclusive certificated in all categories.
Compliance required within the next 100 hours time in service after the effective date of this AD. To prevent improper operation of the elevator pitch trim switch located in the control column handwheel, accomplish the following unless already accomplished.
1. Remount the elevator pitch trim switch in accordance with the accomplishment instructions of British Aerospace Service Bulletin HS-125 27-124 (2705) dated January 1, 1979.
2. Special flight permits may be issued in accordance with FAR 21.197 and 21.199 to operate airplanes to a base for the accomplishment of inspections and/or modifications required by this AD.
3. Alternate means of compliance which provide an equivalent level of safety may be used when approved by the Chief, Seattle Area Aircraft Certification Office, FAA Northwest Mountain Region.
The manufacturer's specifications and procedures identified and described in this directive are incorporated herein and made a part hereof pursuant to 5 U.S.C. 552(a)(1).
Amendment 39-4383 became effective May 31, 1982.
This amendment 39-4470 becomes effective October 12, 1982.
Related safety bulletins advice on the same designs, not orders
2015-09-29NM-15-24 · Landing Gear
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 November 6, 2026. Connections as data: /graph/directive/82-11-03 R1.json · aircraft systems.