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2014-16-26: Time Limits/Maintenance Checks

FAA order 2014-16-26 is an airworthiness directive in force since October 1, 2014. The FAA's subject line: Time Limits/Maintenance Checks. It names Dassault FALCON 900: about 277 aircraft on the U.S. register today, though an order usually covers particular versions or serial numbers rather than every one. System: airframe structure.

What it applies to as the FAA lists it

Kind of product
Aircraft
Makes
Dassault Aviation
Models
Falcon 900EX
On this site
Dassault FALCON 900 277 registered

Dates and paperwork

In force since
October 1, 2014
Published
August 27, 2014 (signed August 7, 2014)
Docket
FAA-2014-0258
Replaced by
2019-24-11
Status
Historical
The FAA's document
Read the order on the FAA's site

The FAA's summary their words, unchanged

We are adopting a new airworthiness directive (AD) for certain Dassault Aviation Model FALCON 900EX airplanes. This AD was prompted by our determination to introduce a corrosion prevention control program, among other changes, to the maintenance requirements and airworthiness limitations. This AD requires revising the maintenance or inspection program, as applicable, to include the maintenance tasks and airworthiness limitations specified in the Airworthiness Limitations section of the airplane maintenance manual. We are issuing this AD to prevent reduced structural integrity and reduced controllability of the airplane.

The order itself the regulatory text, as published

Show the full text (6,577 characters)
Adoption of the Amendment Accordingly, under the authority delegated to me by the Administrator, the FAA amends 14 CFR part 39 as follows: PART 39--AIRWORTHINESS DIRECTIVES 0 1. The authority citation for part 39 continues to read as follows: Authority: 49 U.S. C. 106(g), 40113, 44701. Sec. 39.13 [Amended] 0 2. The FAA amends Sec. 39.13 by adding the following new airworthiness directive (AD): 2014-16-26 Dassault Aviation: Amendment 39-17950. Docket No. FAA- 2014-0258; Directorate Identifier 2013-NM-065-AD. (a) Effective Date This AD becomes effective October 1, 2014. (b) Affected ADs This AD affects AD 2002-23-20, Amendment 39-12964 (67 FR 71098, November 29, 2002); and AD 2010-26-05, Amendment 39-16544 (75 FR 79952, December 21, 2010). (c) Applicability This AD applies to Dassault Aviation Model FALCON 900EX airplanes, certificated in any category, serial numbers 1 through 96 inclusive, and serial numbers 98 through 119 inclusive. (d) Subject Air Transport Association (ATA) of America Code 05, Time Limits/ Maintenance Checks. (e) Reason This AD was prompted by our determination to introduce a corrosion prevention control program, among other changes, to the maintenance requirements and airworthiness limitations. We are issuing this AD to prevent reduced structural integrity and reduced controllability of the airplane. (f) Compliance Comply with this AD within the compliance times specified, unless already done. (g) Revision of Maintenance or Inspection Program Within 30 days after the effective date of this AD, revise the maintenance or inspection program, as applicable, to incorporate the information specified in Chapter 5-40, Airworthiness Limitations, DGT 113874, Revision 12, dated September 2012, of the Falcon 900EX Maintenance Manual. The initial compliance time for accomplishing the actions specified in Chapter 5-40, Airworthiness Limitations, DGT 113874, Revision 12, dated September 2012, of the Falcon 900EX Maintenance Manual, is within the applicable times specified in the maintenance manual, or 30 days after the effective date of this AD, whichever occurs later, except as provided by paragraphs (g)(1) through (g)(4) of this AD. (1) The term ``LDG'' in the ``First Inspection'' column of any table in the service information means total airplane landings. (2) The term ``FH'' in the ``First Inspection'' column of any table in the service information means total flight hours. (3) The term ``FC'' in the ``First Inspection'' column of any table in the service information means total flight cycles. (4) The term ``M'' in the ``First Inspection'' column of any table in the service information means months. (h) Terminating Action Accomplishing paragraph (g) of this AD terminates the requirements of AD 2002-23-20, Amendment 39-12964 (67 FR 71098, November 29, 2002); and paragraph (g)(1) of AD 2010-26-05, Amendment 39-16544 (75 FR 79952, December 21, 2010); for Dassault Aviation Model FALCON 900EX airplanes, serial numbers 1 through 96 inclusive, and serial numbers 98 through 119 inclusive. (i) No Alternative Actions and Intervals After accomplishing the revision required by paragraph (g) of this AD, no alternative actions (e.g., inspections) or intervals may be used unless the actions or intervals are approved as an alternative method of compliance (AMOC) in accordance with the procedures specified in paragraph (j)(1) of this AD. (j) Other FAA AD Provisions The following provisions also apply to this AD: (1) Alternative Methods of Compliance (AMOCs): The Manager, International Branch, ANM-116, Transport Airplane Directorate, FAA, has the authority to approve AMOCs for this AD, if requested using the procedures found in 14 CFR 39.19. In accordance with 14 CFR 39.19, send your request to your principal inspector or local Flight Standards District Office, as appropriate. If sending information directly to the International Branch, send it to ATTN: Tom Rodriguez, Aerospace Engineer, International Branch, ANM-116, Transport Airplane Directorate, FAA, 1601 Lind Avenue SW., Renton, WA 98057-3356; telephone 425-227-1137; fax 425-227-1149. Information may be emailed to: 9-ANM-116-AMOC-REQUESTS@faa.gov. Before using any approved AMOC, notify your appropriate principal inspector, or lacking a principal inspector, the manager of the local flight standards district office/certificate holding district office. The AMOC approval letter must specifically reference this AD. (2) Contacting the Manufacturer: For any requirement in this AD to obtain corrective actions from a manufacturer, the action must be accomplished using a method approved by the Manager, International Branch, ANM-116, Transport Airplane Directorate, FAA; or the European Aviation Safety Agency (EASA); or Dassault Aviation's EASA Design Organization Approval (DOA). If approved by the DOA, the approval must include the DOA-authorized signature. (k) Related Information Refer to Mandatory Continuing Airworthiness Information (MCAI) EASA Airworthiness Directive 2013-0051, dated March 4, 2013, for related information. This MCAI may be found in the AD docket on the Internet at http://www.regulations.gov/#!documentDetail;D=FAA-2014- 0258-0002. (l) Material Incorporated by Reference (1) The Director of the Federal Register approved the incorporation by reference (IBR) of the service information listed in this paragraph under 5 U.S.C. 552(a) and 1 CFR part 51. (2) You must use this service information as applicable to do the actions required by this AD, unless this AD specifies otherwise. (i) Chapter 5-40, Airworthiness Limitations, DGT 113874, Revision 12, dated September 2012, of the Falcon 900EX Maintenance Manual. The document revision level is identified only on the title page and page 2. (ii) Reserved. (3) For service information identifiedin this AD, contact Dassault Falcon Jet, P.O. Box [[Page 51080]] 2000, South Hackensack, NJ 07606; telephone 201-440-6700; Internet http://www.dassaultfalcon.com. (4) You may view this service information at the FAA, Transport Airplane Directorate, 1601 Lind Avenue SW., Renton, WA. For information on the availability of this material at the FAA, call 425-227-1221. (5) You may view this service information that is incorporated by reference at the National Archives and Records Administration (NARA). For information on the availability of this material at NARA, call 202-741-6030, or go to: http://www.archives.gov/federal-register/cfr/ibr-locations.html.

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 7, 2026. Connections as data: /graph/directive/2014-16-26.json · aircraft systems.