Airworthiness Directive Schedule
CESSNA 525-A Citation CJ2 · Airworthiness Directives
Overview
This document is an Airworthiness Directive (AD) schedule issued by the CAA of New Zealand, specifically addressing the Williams International FJ44 series engines. It applies to the FJ44-1A, FJ44-1AP, FJ44-2C, and FJ44-3A-24 engines installed on Cessna 525 and 525A aircraft. The directives outline mandatory inspections and compliance requirements for these engines to ensure safety and airworthiness. The document includes specific FAA ADs that detail the necessary inspections for various components of the engines, emphasizing the importance of adhering to the compliance timelines to maintain certification and operational safety.
- Applicable to Cessna 525 and 525A aircraft with Williams International FJ44 engines.
- Initial compliance for inspections required before issuing a New Zealand Certificate of Airworthiness.
- Repetitive inspections must follow the intervals specified in the FAA ADs.
- Specific FAA ADs detail inspections for disk posts, turbine blades, and high-pressure turbine disks.
- Effective date for all directives is 31 October 2024.
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 www.aviation.govt.nz. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type ·
- Airworthiness Directives
- Year ·
- 2024
- Pages ·
- 2
- File size ·
- 101 KB
- Copy found at ·
- www.aviation.govt.nz
What is the Airworthiness Directive Schedule?
The Airworthiness Directive Schedule is a airworthiness directives for the CESSNA 525-A Citation CJ2, dated 2024.
How many pages is the Airworthiness Directive Schedule?
The copy of the Airworthiness Directive Schedule on file runs 2 pages.
What year was the Airworthiness Directive Schedule published?
The Airworthiness Directive Schedule — the CESSNA 525-A Citation CJ2 airworthiness directives on file — is dated 2024.
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Most owners only have the POH. Here's the essential set for the CESSNA 525-A Citation CJ2.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins on file
- Type Certificate (TCDS)
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In this document
FAA AD 97-01-05 - Disk Posts and Turbine Blades - Inspection
This AD applies to FJ44-1A turbofan engines with serial numbers 1001-1179, 1196, and 1197, installed on Cessna Citation 525 series aircraft. Initial compliance is required before the issuance of a New Zealand Certificate of Airworthiness or at the next Review of Airworthiness (RA) or annual inspection, whichever comes first. Repetitive inspections must be conducted at specified intervals.
FAA AD 99-07-04 - High Pressure Turbine (HPT) Disk - Inspection
This directive is applicable to FJ44-1A turbofan engines installed on Cessna 525 series aircraft. Similar to AD 97-01-05, initial compliance is required before the issuance of a New Zealand Certificate of Airworthiness or at the next RA or annual inspection. Repetitive inspections are also mandated at specified intervals.
FAA AD 2022-13-15 - Turbine Section - Inspection
This AD covers FJ44-2A, FJ44-2C, FJ44-3A, and FJ44-3A-24 turbofan engines with specific serial numbers. Compliance is required before the issuance of a New Zealand Certificate of Airworthiness or at the next RA or annual inspection. Repetitive inspections must be performed at intervals not exceeding those specified in the FAA AD.
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
Issued 31 October 2024 Page 1 of 2 CAA of NZ Airworthiness Directive Schedule Engines Williams International FJ44 Series 31 October 2024 Notes: 1. This AD schedule is applicable to Williams International FJ44-1A, FJ44-1AP, FJ44- 2C and FJ443A-24 engines, manufactured under FAA Type Certificate (TC) No. E3GL and installed on Cessna 525 and 525A aircraft with a MCTOW below 5700kg. 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 * FAA AD 97-01-05 Disk Posts and Turbine Blades - Inspection ................................................................ 2 * FAA AD 99-07-04 High Pressure Turbine (HPT) Disk - Inspection ........................................................... 2 * FAA AD 2022-13-15 Turbine Section - Inspection ........................................................................................ 2 Engines Williams International FJ44 Series Issued 31 October 2024 Page 2 of 2 CAA of NZ * FAA AD 97-01-05 Disk Posts and Turbine Blades - Inspection Applicability: FJ44-1A turbofan engines, with S/N 1001-1179, 1196 and 1197, installed on, but not limited to, Cessna Citation 525 series aircraft. Compliance: Initial compliance required before the issue of a New Zealand Certificate of Airworthiness, or at the next Review of Airworthiness (RA), or at the next annual inspection, whichever is the sooner, unless previously accomplished. Repetitive inspections, if required, are to be accomplished at intervals not to exceed the times specified in the FAA AD. Effective Date: 31 October 2024 * FAA AD 99-07-04 High Pressure Turbine (HPT) Disk - Inspection Applicability: FJ44-1A turbofan engines, installed on but not limited to Cessna 525 series aircraft. Compliance: Initial compliance required before the issue of a New Zealand Certificate of Airworthiness, or at the next Review of Airworthiness (RA), or at the next annual inspection, whichever is the sooner, unless previously accomplished. Repetitive inspections, if required, are to be accomplished at intervals not to exceed the times specified in the FAA AD. Effective Date: 31 October 2024 * FAA AD 2022-13-15 Turbine Section - Inspection Applicability: FJ44-2A, FJ44-2C, FJ44-3A, and FJ44-3A-24 turbofan engines with an engine S/N identified in paragraph 1.A., Effectivity, of Williams International SB WISB-72-1032, Revision 2, dated June 4, 2020, with an installed high-pressure turbine (HPT) disk P/N 67093. Compliance: Initial compliance required before the issue of a New Zealand Certificate of Airworthiness, or at the next Review of Airworthiness (RA), or at the next annual inspection, whichever is the sooner, unless previously accomplished. Repetitive inspections, if required, are to be accomplished at intervals not to exceed the times specified in the FAA AD. Effective Date: 31 October 2024