SCHEDULE OF AIRWORTHINESS DIRECTIVES
CESSNA T-210 · Airworthiness Directives
Overview
This document is a Schedule of Airworthiness Directives specifically for the Cessna 210 series aeroplanes, including the P210 and T210 models. It outlines the requirements for the installation of an alternator ground strap, which is critical for ensuring the safety and airworthiness of the aircraft. The directive applies to a specific range of serial numbers and mandates compliance within a specified time frame. It is intended for aircraft owners, maintenance personnel, and operators to ensure that their aircraft meet safety regulations and standards set by the Civil Aviation Safety Authority of Australia.
- The directive applies to Cessna 210, P210, and T210 models within specific serial number ranges.
- Compliance is required within 100 hours of service after March 31, 1982.
- Ground straps must be installed each time an engine is reinstalled in the aircraft.
Document
Source
Originally published by services.casa.gov.au. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type
- Airworthiness Directives
- Year
- 1982
- Pages
- 1
- File size
- 9.8 KB
- Publisher
- services.casa.gov.au
Most owners only have the POH. Here's the essential set for the CESSNA T-210.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins
- Type Certificate (TCDS)
More CESSNA T-210manuals & documents
- WINGS - MODEL 210 CARRY-THRU SPAR ONE-TIME CORROSION INSPECTIONService Manual
- WINGS - MODEL 210 CARRY-THRU SPAR ONE-TIME CORROSION INSPECTIONMaintenance Manual
- T210 Aircraft CheckoutPilot's Operating Handbook
- Runway excursion involving Cessna T210, VH-DQIOther Documents
- Cessna T206/T207/T210 Modified STCSystems Description
- AIRWORTHINESS DIRECTIVEAirworthiness Directives
- SCHEDULE OF AIRWORTHINESS DIRECTIVESAirworthiness Directives
- MANDATORY service bulletinService Bulletins
- Slick Service Bulletin No. SB 1-84Service Bulletins
- SEB88-3 - Cessna Flyer AssociationService Bulletins
- Type Certificate Data SheetType Certificate
- Supplemental Type Certificate for CESSNA T-210Supplemental Type Certificate
In this document
Applicability
The directive applies to all Cessna 210, P210, and T210 models with specific serial numbers ranging from 21058783 to 21062666, excluding 21062650 and 21062662, as well as P21000001 to P21000026 and T210-0001 to T210-0454.
Compliance Requirements
Compliance with the directive is required within 100 hours of time in service after March 31, 1982. Additionally, every time an engine is installed in an aircraft, the ground strap must be checked and installed if omitted during the initial compliance.
Background Information
The compliance requirements have been amended due to reports from the industry indicating that ground straps were being omitted during engine reinstallations. This amendment aims to enhance safety by ensuring that all installations are completed correctly.
Safety notes
- Failure to comply with the installation of the alternator ground strap may compromise aircraft safety.
Full document text
COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY SCHEDULE OF AIRWORTHINESS DIRECTIVES Cessna 210 Series Aeroplanes AD/CESSNA 210/43 Amdt 1 Alternator Ground Strap - Installation 9/82 Applicability: All model 210/P210/T210 with S/Nos. 21058783 to 21062666 except 21062650 and 21062662, P21000001 to P21000026, T210-0001 to T210-0454. Document: 1. Cessna SIL SE79-59; or 2. FAA AD 79-25-07. Compliance: 1. Within 100 hours time in service after 31 March 1982. 2. Each time an engine is installed in an aircraft following initial compliance. Background: Compliance has been amended by item 2 due to reports from industry that ground straps are being omitted from refitment on engine reinstallations.