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2018-04-10: Landing Gear

FAA order 2018-04-10 is an airworthiness directive in force since April 12, 2018. The FAA's subject line: Landing Gear. It names Pilatus PC-7: about 19 aircraft on the U.S. register today, though an order usually covers particular versions or serial numbers rather than every one. System: landing gear.

What it applies to as the FAA lists it

Kind of product
Aircraft
Makes
Pilatus Aircraft Limited
Models
PC-7
On this site
Pilatus PC-7 19 registered

Dates and paperwork

In force since
April 12, 2018
Published
March 8, 2018 (signed February 16, 2018)
Docket
FAA-2017-1079
Status
Current
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 Pilatus Aircraft Limited Model PC-7 airplanes. This AD results from mandatory continuing airworthiness information (MCAI) issued by an aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI describes the unsafe condition as the brakes remaining activated after release of the brake pedal. We are issuing this AD to require actions to address the unsafe condition on these products.

The order itself the regulatory text, as published

Show the full text (4,429 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 AD: 2018-04-10 Pilatus Aircraft Limited: Amendment 39-19206; Docket No. FAA-2017-1079; Product Identifier 2017-CE-039-AD. (a) Effective Date This airworthiness directive (AD) becomes effective April 12, 2018. (b) Affected ADs None. (c) Applicability This AD applies to Pilatus Aircraft Limited Model PC-7 airplanes, manufacturer serial numbers 101 through 618, certificated in any category. (d) Subject Air Transport Association of America (ATA) Code 32: Landing Gear. (e) Reason This AD was prompted by mandatory continuing airworthiness information (MCAI) originated by an aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI describes the unsafe condition as the brakes remaining activated after release of the brake pedal. We are issuing this AD to prevent the brakes from remaining activated after the brake pedal has been released, which could lead to asymmetric braking and subsequent loss of control. (f) Actions and Compliance Unless already done, within the next 90 days after the effective date of this AD, modify the brake pedal interconnecting tie rods by removing the bonding straps and attachment hardware following sections A, B, and C of the Accomplishment Instructions in Pilatus Service Bulletin 32-028, dated September 20, 2017. (g) Other FAA AD Provisions The following provisions also apply to this AD: (1) Alternative Methods of Compliance (AMOCs): The Manager, Small Airplane Standards Branch, 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: Doug Rudolph, Aerospace Engineer, FAA, Small Airplane Standards Branch, 901 Locust, Room 301, Kansas City, Missouri 64106; telephone: (816) 329-4059; fax: (816) 329- 4090; email: doug.rudolph@faa.gov. Before using 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. (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, Small Airplane Standards Branch, FAA; or the Federal Office of Civil Aviation (FOCA), which is the aviation authority for Switzerland. (h) Related Information Refer to MCAI FOCA AD HB-2017-002, dated October 20, 2017, for related information. The MCAI can be found in the AD docket onthe internet at: https://www.regulations.gov/document?D=FAA-2017-1079-0002. (i) 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 the AD specifies otherwise. (i) Pilatus Service Bulletin 32-028, dated September 20, 2017. (ii) Reserved. (3) For service information identified in this AD, contact PILATUS Aircraft Ltd., Customer Technical Support (MCC), P.O. Box 992, CH-6371 Stans, Switzerland; phone: +41 (0)41 619 67 74; fax: +41 (0)41 619 67 73; email: aircraft.com">techsupport@pilatus-aircraft.com; internet: http://www.pilatus-aircraft.com. (4) You may view this service information at the FAA, Policy and Innovation Division, 901 Locust, Kansas City, Missouri 64106. For information on the availability of this material at the FAA, call (816) 329-4148. In addition, you can access this service information on the internet at http://www.regulations.gov by searching for and locating Docket No. FAA-2017-1079. (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 5, 2026. Connections as data: /graph/directive/2018-04-10.json · aircraft systems.