SCHEDULE OF AIRWORTHINESS DIRECTIVES
CESSNA P210N · Airworthiness Directives
Overview
This document is an Airworthiness Directive issued by the Civil Aviation Safety Authority of Australia, specifically addressing the Cessna 210 series aeroplanes. The directive focuses on the P210N model, particularly those with serial numbers ranging from P21000001 to P21000690 that do not incorporate Cessna Service Kit No. SK210-98B. The directive mandates checks and modifications to the engine and turbocharger installation to mitigate the risk of engine overheating and detonation due to excessively lean mixtures during high power operations. The compliance timeframe is set for within 200 hours of service after October 31, 1981. The document also outlines the background and rationale for the directive, emphasizing improvements in climb performance as a result of the required modifications.
- This directive applies to Cessna P210N series aircraft with specific serial numbers.
- Compliance is required within 200 hours of service after October 31, 1981.
- The directive aims to reduce engine overheating and detonation risks.
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Reference only, not for flight. Use the current approved manual for your aircraft. See terms, section 5.
Document
Source
Copy found at services.casa.gov.au. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type ·
- Airworthiness Directives
- Year ·
- 1981
- Pages ·
- 1
- File size ·
- 10 KB
- Copy found at ·
- services.casa.gov.au
What is the SCHEDULE OF AIRWORTHINESS DIRECTIVES?
The SCHEDULE OF AIRWORTHINESS DIRECTIVES is a airworthiness directives for the CESSNA P210N, dated 1981.
How many pages is the SCHEDULE OF AIRWORTHINESS DIRECTIVES?
The copy of the SCHEDULE OF AIRWORTHINESS DIRECTIVES on file runs 1 pages.
What year was the SCHEDULE OF AIRWORTHINESS DIRECTIVES published?
The SCHEDULE OF AIRWORTHINESS DIRECTIVES — the CESSNA P210N airworthiness directives on file — is dated 1981.
Common. More common than 99% of the aircraft models we track.
Most owners only have the POH. Here's the essential set for the CESSNA P210N.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins on file
- Type Certificate (TCDS)
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—In this document
Applicability
The directive applies specifically to the Cessna P210N series aircraft with serial numbers P21000001 to P21000690 that have not incorporated the specified Cessna Service Kit.
Compliance
Operators of the affected aircraft must comply with the directive within 200 hours of time in service after October 31, 1981.
Background
The directive was issued to address concerns regarding engine overheating and detonation risks due to lean fuel mixtures during high power operations. It has been amended to broaden the range of affected serial numbers and to enhance safety through additional modifications.
Summary written by AI from the source document. Check the original before relying on it. See which parts of Sprinkle are written by AI.
Safety notes
- Failure to comply with the directive may result in engine overheating and detonation.
Summary written by AI from the source document. Check the original before relying on it. See which parts of Sprinkle are written by AI.
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 210/50 Amdt 1 Engine and Turbocharger Installation - Checks and Modification 10/81 Applicability: Model P210N series with S/Nos. P21000001 to P21000690 not incorporating Cessna Service Kit No. SK210-98B. Document: 1. CESSNA SIL No. SE 81-35 and Supplement No. 1 or 2. FAA AD 81-15-05, Amendment No. 39-4168. Compliance: Within 200 hours time in service after 31 October, 1981. Background: This directive was originally issued to reduce the possibility of engine overheating and detonation caused by excessively lean mixtures during high power operation. It has been amended to increase the range of serial numbers of affected aircraft and to further reduce the possibility of detonation by additional modifications. Climb performance is also improved as the result of these modifications.










