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FAA orders · airworthiness directive · historical

2008-24-07: Airplane flight manual (AFM)

FAA order 2008-24-07 is an airworthiness directive in force since December 4, 2008. The FAA's subject line: Airplane flight manual (AFM). It names Eclipse Aerospace Inc EA500: about 30 aircraft on the U.S. register today, though an order usually covers particular versions or serial numbers rather than every one. System: engine.

What it applies to as the FAA lists it

Kind of product
Aircraft
Makes
Eclipse Aerospace, Inc.
Models
EA500
On this site
Eclipse Aerospace Inc EA500 30 registered

Dates and paperwork

In force since
December 4, 2008
Published
November 24, 2008 (signed November 17, 2008)
Docket
FAA-2008-1232
Replaced by
2011-06-06
Status
Historical
The FAA's document
Read the order on the FAA's site

The FAA's summary their words, unchanged

The FAA is adopting a new airworthiness directive (AD) for certain Eclipse Aviation Corporation (Eclipse) Model EA500 airplanes equipped with a Pratt and Whitney Canada, Corp. (PWC) PW610F-A engine. This AD requires you to incorporate operating limitations into Section 2, Limitations, of the airplane flight manual (AFM). This AD results from several incidents of engine surge. We are issuing this AD to prevent hard carbon buildup on the static vane, which could result in engine surges. Engine surges may result in a necessary reduction in thrust and decreased power for the affected engine. In some cases, this could result in flight and landing under single-engine conditions.

The order itself the regulatory text, as published

Show the full text (2,171 characters)
2008-24-07 Eclipse Aviation Corporation: Amendment 39-15747; Docket No. FAA-2008-1232; Directorate Identifier 2008-CE-070-AD. Effective Date (a) This AD becomes effective on December 4, 2008. Affected ADs (b) None. Applicability (c) This AD applies to Model EA500 airplanes, all serial numbers, that are: (1) Equipped with a Pratt and Whitney Canada, Corp. PW610F-A engine; and (2) Certificated in any category. Unsafe Condition (d) This AD is the result of several incidents of engine surge. We are issuing this AD to prevent hard carbon buildup on the static vane, which could result in engine surges. Engine surges may result in a necessary reduction in thrust and decreased power for the affected engine. In some cases, this could result in flight and landing under single-engine conditions. Compliance (e) Prior to further flight, unless already done, incorporate the following language into Section 2, Limitations, of your airplane flight manual (AFM): "Per AD 2008-24-07, LIMIT THE MAXIMUM OPERATING ALTITUDE TO 37,000 FEET (11277M) PRESSURE ALTITUDE.'' (1) A person holding at least a private pilot certificate as authorized by section 43.7 of the Federal Aviation Regulations (14 CFR 43.7) may insert the operating limitations into Section 2, Limitations, of the AFM. Make an entry into the aircraft logbook showing compliance with this portion of the AD in accordance with section 43.9 of the Federal Aviation Regulations (14 CFR 43.9). (2) You may incorporate paragraph (e) of this AD into Section 2, Limitations, of your AFM to comply with this AD. Alternative Methods of Compliance (AMOCs) (f) The Manager, Fort Worth Airplane Certification Office, FAA, has the authority to approve AMOCs for this AD, if requested using the procedures found in 14 CFR 39.19. Send information to Attn: Mitchell Soth, Aerospace Engineer, 2601 Meacham Blvd., Fort Worth, Texas 76137; telephone: (817) 222-5104; fax: (817) 222-5960. Beforeusing any approved AMOC on any airplane to which the AMOC applies, notify your appropriate principal inspector (PI) in the FAA Flight Standards District Office (FSDO), or lacking a PI, your local FSDO.

Related safety bulletins advice on the same designs, not orders

2012-05-08CE-12-30 · Wing, Fuselage Attach Fittings
2012-04-17CE-12-28 · Battery/Charger System
2012-01-24CE-12-13 · Ailerons

Source: FAA Dynamic Regulatory System, airworthiness directives. The FAA's document is the authority; the register counts are this site's, from the FAA register of October 8, 2026. Connections as data: /graph/directive/2008-24-07.json · aircraft systems.