SCHEDULE OF AIRWORTHINESS DIRECTIVES
Piper PA-36 Pawnee Brave · Airworthiness Directives
Overview
This document is a Schedule of Airworthiness Directives issued by the Civil Aviation Safety Authority of Australia, specifically addressing the Piper PA-36 Pawnee Brave series of aeroplanes. It outlines mandatory inspection requirements for the rudder spar, applicable to all models within a specified serial number range. The directive is crucial for maintaining airworthiness and ensuring the safety of the aircraft during operation. Compliance with the directive is required within a defined time frame and at specified intervals thereafter, emphasizing the importance of regular inspections for the rudder spar to prevent potential failures.
- Initial rudder spar inspection required within 100 hours after April 30, 1977.
- Subsequent inspections must occur at intervals not exceeding 100 hours.
- Applicable to all Piper PA-36 models with serial numbers 36-7360001 to 36-7760003.
- Compliance is mandatory for maintaining airworthiness.
- Document references Piper SB No. 518.
Summary written by AI from the source document. Check the original before relying on it. See which parts of Sprinkle are written by AI.
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 ·
- 1977
- Pages ·
- 1
- File size ·
- 9.5 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 Piper PA-36 Pawnee Brave, dated 1977.
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 Piper PA-36 Pawnee Brave airworthiness directives on file — is dated 1977.
Most owners only have the POH. Here's the essential set for the Piper PA-36 Pawnee Brave.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins on file
- Type Certificate (TCDS)
More Piper PA-36 Pawnee Bravemanuals & documents
- Piper PA-36 Pawnee Brave Model GuideModel Guide
- CUSTOMER SERVICE OWNER PUBLICATIONS CATALOGPilot's Operating Handbook
- DESIGN OF AGRICULTURE AIRCRAFT WITH SPRAYING MECHANISMPilot's Operating Handbook
- Pawnee Brave 20cc Instruction ManualChecklist
- Pawnee Brave 20cc Instruction ManualPilot's Operating Handbook
- Type Acceptance Report TAR 19/21B/27 – Piper PA-36 Pawnee BravePilot's Operating Handbook
- ATSB Transport Safety Report: Aviation Occurrence Investigation (Short) AO-2019-043Other Documents
- HARTZELL PROPELLER INC. SERVICE BULLETIN HC-SB-61-227 Propeller - Hub InspectionService Bulletins
- PIPER PA-36-300 Pawnee Brave with Lycoming IO540 EngineSystems Description
- RAPCO INC. FUEL PUMP APPLICATION GUIDEFlight Manual
- AIRCRAFT FUEL PUMP APPLICATION GUIDEV Speeds Reference
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In this document
Rudder Spar - Inspection
This section details the Airworthiness Directive AD/PA-36/17, which mandates an inspection of the rudder spar for all Piper PA-36 models with serial numbers ranging from 36-7360001 to 36-7760003. The initial inspection must be completed within 100 hours of time in service after April 30, 1977, and subsequent inspections are required at intervals not exceeding 100 hours until the rudder is replaced.
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 Piper PA-36 (Pawnee Brave) Series Aeroplanes AD/PA-36/17 Rudder Spar - Inspection 4/77 Applicability: All models with S/Nos. 36-7360001 to 36-7760003. Document: Piper SB No. 518. Compliance: Within 100 hours time in service after 30 April 1977 and thereafter at intervals not exceeding 100 hours time in service until rudder is replaced.