SCHEDULE OF AIRWORTHINESS DIRECTIVES
Beechcraft C24R Sierra · Service Bulletins
Overview
This document is a Schedule of Airworthiness Directives issued by the Civil Aviation Safety Authority of Australia, specifically addressing safety concerns related to Beechcraft 19, 23, and 24 Series Aeroplanes. It highlights an important directive concerning the electric fuel boost pump for various models, including the Beechcraft C24R Sierra. The directive mandates compliance with the replacement of the electric fuel boost pump to prevent potential engine power loss due to fuel pressure issues. The document is crucial for maintenance personnel and operators of the affected aircraft models to ensure safety and compliance with aviation regulations.
- The directive applies to Beechcraft C24R Sierra 200, Serial No MC-96 through MC-795.
- Operators must comply with Beechcraft Service Bulletin No 2217 for pump replacement.
- Compliance is required before the next Maintenance Release after 11 August 1988.
- The issue is related to potential engine power loss due to fuel pressure loss.
- Improved fuel boost pumps are available on an exchange basis from Beech Aircraft Corporation.
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 ·
- Service Bulletins
- Year ·
- 1988
- Pages ·
- 1
- File size ·
- 11 KB
- Publisher ·
- services.casa.gov.au
What is the SCHEDULE OF AIRWORTHINESS DIRECTIVES?
The SCHEDULE OF AIRWORTHINESS DIRECTIVES is a service bulletins for the Beechcraft C24R Sierra, dated 1988.
How many pages is the SCHEDULE OF AIRWORTHINESS DIRECTIVES?
The copy of the SCHEDULE OF AIRWORTHINESS DIRECTIVES on file runs 1 pages.
Where does the SCHEDULE OF AIRWORTHINESS DIRECTIVES come from?
This copy of the SCHEDULE OF AIRWORTHINESS DIRECTIVES was originally published by services.casa.gov.au and is hosted on Sprinkle as a free, searchable reference copy.
What year was the SCHEDULE OF AIRWORTHINESS DIRECTIVES published?
The SCHEDULE OF AIRWORTHINESS DIRECTIVES — the Beechcraft C24R Sierra service bulletins on file — is dated 1988.
Most owners only have the POH. Here's the essential set for the Beechcraft C24R Sierra.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins on file
- Type Certificate (TCDS)
More Beechcraft C24R Sierramanuals & documents
- Beechcraft Musketeer A23 Maintenance ManualParts Catalog
- GROUND PROCEDURES Beech Sierra C24RPilot's Operating Handbook
- Supplemental Type CertificateWeight And Balance
- Airworthiness Directive Schedule Aeroplanes Beechcraft 23 and 24 Series (Musketeer, Sundowner and Sierra 200)Service Bulletins
- SCHEDULE OF AIRWORTHINESS DIRECTIVESAirworthiness Directives
- Beechcraft C24R Sierra Pilot's Operating HandbookPilot's Operating Handbook
- Beechcraft 180 and Sierra 200 Wiring Diagram ManualService Manual
- 1976 BEECHCRAFT C24R SIERRAAvionics Manual
- BEECHCRAFT SIERRAPilot's Operating Handbook
- Beechcraft C24R Sierra Pilot's Operating HandbookPilot's Operating Handbook
In this document
Applicability
The directive applies to several Beechcraft models, specifically Model A23-24 and A24 Musketeer Serial No MA-1 through MA-368; A24R Serial No MC-2 through MC-95; and C24R Sierra 200, Serial No MC-96 through MC-795.
Requirement
Operators are required to take action in accordance with Beechcraft Service Bulletin No 2217, which outlines the necessary steps for compliance with the directive.
Compliance
Compliance with this directive is required prior to the issue of the next Maintenance Release after 11 August 1988, ensuring that all affected aircraft are updated with the improved fuel boost pump.
Background
The background section explains that the manufacturer has received reports of engine power loss due to fuel pressure loss, which was caused by broken electric fuel boost pump vane material obstructing fuel flow. This directive aims to prevent such occurrences by mandating the replacement of the affected pumps.
Safety notes
- Failure to comply with this directive may result in engine power loss.
- Operators should ensure timely replacement of the electric fuel boost pump to maintain safety.
Full document text
COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY SCHEDULE OF AIRWORTHINESS DIRECTIVES Beechcraft 19, 23 and 24 Series Aeroplanes AD/BEECH 23/45 Electric Fuel Boost Pump 8/88 Applicability: Model A23-24 and A24 Musketeer Serial No MA-1 through MA-368; A24R Serial No MC-2 through MC-95; A24-R, B24R, and C24R Sierra 200, Serial No MC-96 through MC-795. Requirement: Action in accordance with Beechcraft Service Bulletin No 2217. Note: FAA AD 88-10-01 amendment 39-5904 refers. Compliance: Prior to the issue of the next Maintenance Release after 11 August 1988. Background: The manufacturer has received reports of engine power loss which resulted from loss of fuel pressure, caused by broken electric fuel boost pump vane material obstructing fuel flow in the engine driven pump. This AD requires the replacement of the electric fuel boost pump with a pump having improved vane material. Beech Aircraft Corporation are offering improved pumps on an exchange basis within a limited time period.