Airworthiness Directive Schedule Aeroplanes Beechcraft D18S (Expeditor)
Beechcraft Model 18 · Airworthiness Directives
Overview
This document is an Airworthiness Directive (AD) schedule specifically for the Beechcraft D18S aircraft, also known as the Expeditor. Issued on August 31, 2000, it outlines compliance requirements for various FAA Airworthiness Directives applicable to the D18S model. The document serves as a regulatory guide for ensuring the airworthiness of the aircraft, detailing necessary inspections and compliance measures that must be documented in the aircraft logbook. It is essential for operators and maintenance personnel to adhere to these directives to maintain safety and compliance with aviation regulations.
- The document is specifically for Beechcraft D18S aircraft.
- Compliance with FAA Airworthiness Directives is required before issuing a New Zealand Airworthiness Certificate.
- Repetitive inspections must be conducted at intervals specified in the FAA ADs.
- Each FAA AD must be certified in the aircraft logbook separately.
- The effective date for compliance is May 7, 1999.
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
- 2000
- Pages
- 2
- File size
- 21 KB
- Publisher
- www.aviation.govt.nz
Most owners only have the POH. Here's the essential set for the Beechcraft Model 18.
- 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
DCA/B18/1 Airworthiness Directive Compliance at Initial Airworthiness Certificate Issue
This section specifies that all Beechcraft D18S aircraft must comply with a series of FAA Airworthiness Directives before the issuance of a New Zealand Airworthiness Certificate. The directives cover various components such as the horizontal stabilizer spar, stabilizer attachment fittings, and fuel line modifications. Each FAA AD must be certified in the aircraft logbook separately, and repetitive inspections are required at specified intervals.
List of Applicable FAA Airworthiness Directives
The document lists several FAA Airworthiness Directives that are applicable to the Beechcraft D18S. These include directives related to the horizontal stabilizer spar (47-33-05), stabilizer spar replacement (47-33-06), and various other components such as the generator control box (48-13-01) and fuel line modification (59-18-02). Compliance with these directives is mandatory for maintaining airworthiness.
Safety notes
- Failure to comply with the listed FAA Airworthiness Directives may result in safety hazards and regulatory non-compliance.
Full document text
Issued 31 August 2000 Page 1 of 2 CAA of NZ Airworthiness Directive Schedule Aeroplanes Beechcraft D18S (Expeditor) 31 August 2000 Notes 1. This AD schedule is applicable to Beechcraft D18S aircraft, manufactured under Federal Aviation Administration (FAA) Type Certificate No. A-765. 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 DCA/B18/1 Airworthiness Directive Compliance at Initial Airworthiness Certificate Issue ................... 2 * DCA/B18/2 Cancelled .......................................................................................................................... 2 Aeroplanes Beechcraft D18S (Expeditor) Issued 31 August 2000 Page 2 of 2 CAA of NZ DCA/B18/1 Airworthiness Directive Compliance at Initial Airworthiness Certificate Issue Applicability: All Model D18S Requirement: Compliance with the following FAA Airworthiness Directives (as applicable) is required:- 47-33-05 - Horizontal stabilizer spar 47-33-06 - Stabilizer spar replacement 47-33-07 - Static selector valve 47-34-01 - Expansion type filler cap 47-34-02 - Tail cone drain holes 47-34-03 - Fuel cell seal 48-13-01 - Generator control box 48-34-01 - Stabilizer attachment fittings 49-29-02 - Rudder spring bushings 59-18-02 - Fuel line modification 65-03-01 - Gap seal strips 66-30-01 - Static pressure line 68-23-06 - Volpar tri-gear 72-16-02 R3 - Volpar nose gear fork 72-25-06 - Nose gear extension 75-27-09 R2 - Wing structure 77-19-07 - Control column assembly 78-10-01 - Lower rudder torque tube Note: Each part of this AD (each individual FAA AD) shall be certified in the aircraft log book separately. Compliance: Before issue of New Zealand Airworthiness Certificate. Repetitive inspections to be accomplished at intervals not exceeding the times specified in the FAA Airworthiness Directives Effective Date: 7 May 1999 * DCA/B18/2 Cancelled