SCHEDULE OF AIRWORTHINESS DIRECTIVES
Cessna 170 · Airworthiness Directives
Overview
This document is an Airworthiness Directive (AD) issued by the Civil Aviation Safety Authority (CASA) of Australia, specifically addressing safety concerns related to the Cessna 170 and other related models. The directive outlines the requirements for inspecting the horizontal stabiliser front spar for cracks, a critical safety issue that has been reported in various aircraft within the Cessna 170 and 172 series. The AD mandates compliance with specific inspection intervals and procedures to ensure the continued airworthiness of the affected aircraft. It serves as a crucial reference for pilots, maintenance personnel, and operators of these aircraft, emphasizing the importance of regular inspections to prevent potential failures.
- Inspect the horizontal stabiliser front spar for cracks as per Cessna Service Bulletin SEB94-8.
- Compliance with the inspection is required at intervals not exceeding 100 hours of time in service.
- The directive applies to Cessna 170, 172, 175, F172, and FR172 series aircraft, excluding Models 172R and 172S.
- Cracking issues have been reported due to improper ground handling practices.
- The directive aims to prevent structural failures in the horizontal stabiliser front spar.
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
- 2001
- Pages
- 1
- File size
- 13 KB
- Publisher
- services.casa.gov.au
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In this document
Applicability
The Airworthiness Directive applies to all Model 172 and 175 series aircraft, as well as all Reims Model F172 and FR172 series aircraft, with the exception of Models 172R and 172S and subsequent models.
Requirement
The directive requires a visual inspection of the horizontal stabiliser front spar for any signs of cracking. This inspection must be conducted in accordance with Cessna Service Bulletin SEB94-8.
Compliance
The compliance interval for the required inspection is set at no more than 100 hours of time in service. This ensures that any potential issues are identified and addressed promptly.
Background
The directive was issued in response to multiple reports of cracking in the horizontal stabiliser front spar, which could lead to severe structural failure. The issue has been linked to improper ground handling practices.
Effective Date
This Airworthiness Directive became effective on 22 March 2001, following its initial issue on 17 August 1995.
Safety notes
- Failure to comply with the inspection requirements may lead to severe structural failure of the aircraft.
Full document text
COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY SCHEDULE OF AIRWORTHINESS DIRECTIVES Cessna 170, 172, F172, FR172 and 175 Series Aeroplanes AIRWORTHINESS DIRECTIVE For the reasons set out in the background section, the CASA delegate whose signature appears below revokes Airworthiness Directive (AD) AD/CESSNA 170/59 and issues the following AD under subregulation 39.1 (1) of CAR 1998. The AD requires that the action set out in the requirement section (being action that the delegate considers necessary to correct the unsafe condition) be taken in relation to the aircraft or aeronautical product mentioned in the applicability section: (a) in the circumstances mentioned in the requirement section; and (b) in accordance with the instructions set out in the requirement section; and (c) at the time mentioned in the compliance section. AD/CESSNA 170/59 Amdt 1 Horizontal Stabiliser Front Spar 3/2001 Applicability: All Model 172 and 175 series aircraft, all Reims Model F172 and FR172 series aircraft; except Models 172R & 172S, and subsequent. Requirement: Visually inspect the horizontal stabiliser front spar for cracking in accordance with Cessna Service Bulletin SEB94-8. Compliance: At intervals not to exceed 100 hours time in service. This Airworthiness Directive becomes effective on 22 March 2001. Background: A number of instances of cracking of the horizontal stabiliser front spar have been reported. In July 1984 the Authority issued AAC 153-2 highlighting the problem. The most likely cause was incorrect ground handling; pushing down on the stabiliser to lift the nose wheel. However cracks continue to be reported and in one instance the spar was reported to have been completely severed. Reports have also been received of cracking of modified and reinforced spars, Cessna P/N 0532001-98. The intent of this Directive is not applicable to later Model 172 aircraft, and is amended accordingly. The original issue of this Airworthiness Directive became effective on 17 August 1995. David Alan Villiers Delegate of the Civil Aviation Safety Authority 24 January 2001 The above AD is notified in the Commonwealth of Australia Gazette on 21 February 2001.
What's in the Cessna 170 TCDS
A Type Certificate Data Sheet (TCDS) is the FAA's record of what an aircraft type was approved as. It is the source of truth for weights, seating, fuel and the rules the design was certified against. Expand any line to see what it means.
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