Commonwealth legislation

AD/BEECH 36/45 - Inspection for Flight Control Interference with Wiring

In ForceCTH

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

3/10 complexity

Requires owners/operators of listed Beechcraft A36 and B36TC serial numbers to inspect for wiring that could interfere with flight controls and, if found, secure those components per Raytheon Mandatory Service Bulletin 27‑3232. Must be done within 25 flight hours; corrective action is required before further flight.

The measure responds to a reported incident where wiring entangled the flight control “T” column and temporarily disabled aileron and elevator control.

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AD/BEECH 36/45 - Inspection for Flight Control Interference with Wiring

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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY

SCHEDULE OF AIRWORTHINESS DIRECTIVES

View image in the official source Beechcraft 36 (Bonanza) Series Aeroplanes

AD/BEECH 36/45 Inspection for Flight Control Interference with Wiring

Applicability: This Directive is applicable to the following aircraft:

Model Serial Numbers

7/99 DM

A36 E-3058 through E-3156 inclusive, E-3158 through E-3170 inclusive, E-3172 through E-3177 inclusive, E-3180 through E-3185 inclusive, E-3187 through E-3198 inclusive, E-3200 and E-3202.

B36TC EA-594 through EA-610 inclusive, EA-613, EA-615, EA-616, EA-618, EA-619 and EA-621.

Requirement: Unless previously accomplished;

Inspect for interference or inadequate clearance between the flight control mechanism and any component located forward of the instrument in accordance with Raytheon Mandatory Service Bulletin (SB) 27-3232 dated March 1999.

2. If interference or inadequate clearance is found during the Requirement 1 inspection then secure all components clear of the flight control mechanisms in accordance with SB 27-3232.

Note 1. If Raytheon Safety Communiqué No 149 dated August 1998 or No 149 Rev 1 dated November 1998 has been carried out no further action is required.

Note 2. FAA AD 99-09-15 refers.

Compliance: 1. Within 25 hours time in service after 19 May 1999.

Prior to further flight after inspection.

This Airworthiness Directive becomes effective on 19 May 1999.

Background: There has been a reported incident were a Raytheon Beech Model 1900 aeroplane temporarily lost aileron and elevator control when the control column became restricted. Upon investigation the cause was found to be electrical/avionics wiring located forward of the instrument panel entangled in the flight control system “T” column.

Source text

Sourced from the Federal Register of Legislation (legislation.gov.au), CC BY 4.0.