Airworthiness Directive Schedule Aeroplanes Cessna 195 Series
Cessna 195 · Airworthiness Directives
Overview
This document is an Airworthiness Directive (AD) schedule specifically for the Cessna 195 series aircraft, issued by the Civil Aviation Authority of New Zealand on 28 November 2013. It outlines various airworthiness directives that are applicable to Cessna 195 aircraft manufactured under FAA Type Certificate No. A-790. The document serves as a reference for maintenance and compliance, ensuring that operators are aware of the necessary inspections and modifications required to maintain airworthiness. Each directive includes an effective date, indicating when compliance is required. The directives cover a range of components and systems, from rudder cables to electrical systems, ensuring comprehensive oversight of the aircraft's safety and operational integrity.
- The document is an Airworthiness Directive schedule for Cessna 195 series aircraft.
- It includes directives with effective dates ranging from 1950 to 2013.
- Key inspections include rudder cables, elevator spar webs, and wing spars.
- Compliance with electrical system directives is crucial for safety.
- Inspections of bladder fuel cells and aileron control systems are mandated.
Document
Source
Originally published by www.aviation.govt.nz. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type
- Airworthiness Directives
- Year
- 2013
- Pages
- 2
- File size
- 43 KB
- Publisher
- www.aviation.govt.nz
Common. Rarer than 1% of the aircraft models we track.
Most owners only have the POH. Here's the essential set for the Cessna 195.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins
- Type Certificate (TCDS)
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In this document
Rudder Cable Inspection
Directive *50-39-01 mandates an inspection of the rudder cables, effective from 25 November 1950. This inspection is crucial for ensuring the integrity and functionality of the rudder control system.
Elevator Spar Webs
Directive *51-11-02 requires inspections of the elevator spar webs, effective from 1 June 1951. This inspection is important for maintaining the structural integrity of the elevator.
Wing Spar Inspection
Directive *63-20-02 outlines the need for wing spar inspections, effective from 8 October 1963. Regular inspections are vital for ensuring the safety and performance of the wing structure.
Electrical System
Directive *79-08-03 addresses the electrical system, with an effective date of 6 June 1979. Compliance with this directive is essential for the safe operation of the aircraft's electrical components.
Bladder Fuel Cells
Directive *84-10-01 (R1) pertains to bladder fuel cells, effective from 5 July 1988. This directive ensures that the fuel storage system is inspected and maintained properly.
Full Flow Engine Oil Adapter
Directive *96-12-22 requires inspections of the full flow engine oil adapter, effective from 31 July 1996. This is critical for maintaining engine lubrication and performance.
Upper Shoulder Harness Adjusters
Directive *2004-19-01 mandates inspections of upper shoulder harness adjusters, effective from 1 November 2004, to ensure passenger safety.
Aileron Control System
Directive *2004-21-08 (R1) addresses the aileron control system, effective from 9 May 2013, ensuring the control surfaces are functioning correctly.
Mode S Transponders
Directive *2005-01-19 requires compliance with Mode S transponder standards, effective from 23 February 2005, for improved air traffic control communication.
Seat Rails and Roller Housing Inspections
Directive *2011-10-09 mandates inspections of seat rails and roller housing, effective from 17 June 2011, to ensure passenger safety and comfort.
Safety notes
- Operators must comply with the effective dates of each directive to maintain airworthiness.
- Failure to adhere to these directives may compromise aircraft safety.
Full document text
Issued 28 November 2013 Page 1 of 2 CAA of NZ Airworthiness Directive Schedule Aeroplanes Cessna 195 Series 28 November 2013 Notes: 1. This AD schedule is applicable to Cessna 195 series aircraft manufactured under FAA Type Certificate No. A-790. 2. The Federal Aviation Administration (FAA) is the National Airworthiness Authority (NAA) responsible for the issue of State of Design Airworthiness Directives (ADs) for these aircraft. State of Design ADs can be obtained directly from the FAA website at: Dynamic Regulatory System (faa.gov) 3. The date above indicates the amendment date of this schedule. 4. New or amended ADs are shown with an asterisk * Contents *50-39-01 Rudder Cable Inspection............................................................................................................. 2 *51-11-02 Elevator Spar Webs ...................................................................................................................... 2 *63-20-02 Wing Spar Inspection .................................................................................................................. 2 *79-08-03 Electrical System ........................................................................................................................ 2 *84-10-01 R1 Bladder Fuel Cells .................................................................................................................... 2 *96-12-22 Full Flow Engine Oil Adapter....................................................................................................... 2 *2004-19-01 Upper Shoulder Harness Adjusters .......................................................................................... 2 *2004-21-08 R1 Aileron Control System......................................................................................................... 2 *2005-01-19 Mode S Transponders .............................................................................................................. 2 *2011-10-09 Seat Rails and Roller Housing Inspections ............................................................................... 2 Aeroplanes Cessna 195 Series Issued 28 November 2013 Page 2 of 2 CAA of NZ *50-39-01 Rudder Cable Inspection Effective Date: 25 Novenber 1950 *51-11-02 Elevator Spar Webs Effective Date: 1 June 1951 *63-20-02 Wing Spar Inspection Effective Date: 08 October 1963 *79-08-03 Electrical System Effective Date: 06 June 1979 *84-10-01 R1 Bladder Fuel Cells Effective Date: 05 July 1988 *96-12-22 Full Flow Engine Oil Adapter Effective Date: 31 July 1996 *2004-19-01 Upper Shoulder Harness Adjusters Effective Date: 01 November 2004 *2004-21-08 R1 Aileron Control System Effective Date: 09 May 2013 *2005-01-19 Mode S Transponders Effective Date: 23 February 2005 *2011-10-09 Seat Rails and Roller Housing Inspections Effective Date: 17 June 2011
What's in the Cessna 195 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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