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2008-24-02: Rear elevator control horn

FAA order 2008-24-02 is an airworthiness directive in force since December 30, 2008. The FAA's subject line: Rear elevator control horn. It names Maule M-4, Maule M-5, Maule M-6, Maule M-7, Maule MT-7, Maule MX-7, Maule MXT-7: about 1,329 aircraft on the U.S. register today across them, though an order usually covers particular versions or serial numbers rather than every one. System: flight controls.

What it applies to as the FAA lists it

Kind of product
Aircraft
Makes
Maule Aerospace Technology, Inc.
Models
Bee Dee M-4, M-4, M-4-180C, M-4-180V, M-4-210, M-4-210C, M-4-210S, M-4-220C, M-4-220S, M-4C, M-4S, M-4T, M-5-180C, M-5-200, M-5-210C, M-5-210TC, M-5-220C, M-5-235C, M-6-180, M-6-235, M-7-235, M-7-235A, M-7-235B, M-7-235C, M-7-260, M-7-260C, M-7-420A, M-7-420AC, M-8-235, MT-7-235, MT-7-260, MT-7-420, MX-7-160, MX-7-160C, MX-7-180, MX-7-180A, MX-7-180AC, MX-7-180B, MX-7-180C, MX-7-235, MX-7-420, MXT-7-160, MXT-7-180, MXT-7-180A
On this site
Maule M-4 207 registered
Maule M-5 364 registered
Maule M-6 81 registered
Maule M-7 275 registered
Maule MT-7 76 registered
Maule MX-7 192 registered
Maule MXT-7 134 registered

Dates and paperwork

In force since
December 30, 2008
Published
November 25, 2008 (signed November 10, 2008)
Docket
FAA-2008-0892
Status
Current
The FAA's document
Read the order on the FAA's site

The FAA's summary their words, unchanged

The FAA adopts a new airworthiness directive (AD) for certain Maule Aerospace Technology, Inc. M-4, M-5, M-6, and M-7 series and Model M-8-235 airplanes. This AD requires you to paint the top of the rear elevator control horn, the elevator control cable end attached to the top of the rear control horn, the bottom of the forward elevator control horn, and the elevator control cable end attached to the bottom of the forward control horn. This AD also requires you to insert a supplement into your maintenance program (maintenance manual). This AD results from two reports of accidents where reversed elevator control rigging was a factor. We are issuing this AD to reduce the likelihood of a mechanic rigging the elevator controls backwards, which could result in elevator movement in the opposite direction from control input. This condition could lead to loss of control.

The order itself the regulatory text, as published

Show the full text (5,540 characters)
2008-24-02 Maule Aerospace Technology, Inc.: Amendment 39-15742; Docket No. FAA-2008-0892; Directorate Identifier 2008-CE-049-AD. Effective Date (a) This AD becomes effective on December 30, 2008. Affected ADs (b) None. Applicability (c) This AD applies to the following airplane models and serial numbers that are certificated in any category: Model Serial Numbers Bee Dee M-4 All serial numbers M-4 All serial numbers M-4-180C All serial numbers M-4-180V 47001T through 47014T M-4-210 All serial numbers M-4-210C All serial numbers M-4-210S All serial numbers M-4-220C All serial numbers M-4-220S All serial numbers M-4C All serial numbers M-4S All serial numbers M-4T All serial numbers M-5-180C All serial numbers M-5-200 All serial numbers M-5-210C All serial numbers M-5-210TC All serial numbers M-5-220C All serial numbers M-5-235C All serial numbers M-6-180 8020C, 8043C, 8065C through 8067C M-6-235 7249C, 7356C, 7379C through 7444C, 7446C through 7450C, 7452C through 7459C, 7461C through 7466C, 7468C, 7469C, 7471C through 7475C, 7488C through 7514C, 7516C through 7522C M-7-235 4001C through 4132C, 12001C, 12002C M-7-235A 24001C M-7-235B 23001C through 23105C M-7-235C 25001C through 25106C M-7-260 26001C through 26021C M-7-260C 30001C through 30040C M-7-420A 35001C M-7-420AC 29001C, 29003C through 29007C M-8-235 15001C through 15006C MT-7-235 18001C through 18097C, 18099C, 18100C MT-7-260 27001C through 27014C MT-7-420 51001C, 51002C MX-7-160 19001C through 19046C MX-7-160C 34001C MX-7-180 11001C through 11097C MX-7-180A 20001C through 20064C MX-7-180AC 33001C through 33010C MX-7-180B 22001C through 22025C, 22027C MX-7-180C 28001C through 28027C MX-7-235 10001C through 10122C MX-7-420 13001C through 13003C MXT-7-160 17001C through 17008C MXT-7-180 14000C through 14125C MXT-7-180A 21001C through 21096C Unsafe Condition (d) This AD resultsfrom two reports of accidents where reversed elevator control rigging was a factor. We are issuing this AD to reduce the likelihood of a mechanic rigging the elevator controls backwards, which could result in elevator movement in the opposite direction from control input. This failure could lead to loss of control. Compliance (e) To address this problem, you must do the following, unless already done: Actions Compliance Procedures (1) Using yellow enamel paint, color code the following: (i) the top of the rear elevator control horn; (ii) the elevator control cable end attached to the top of the rear control horn; (iii) the bottom of the forward elevator control horn; and (iv) the elevator control cable end attached to the bottom of the forward control horn. Before the next time the elevator control cable is disconnected for any reason or within the next 12 calendar months after December 30, 2008 (the effective date of this AD), whichever occurs first. Follow Maule Aerospace Technology, Inc. Mandatory Service Bulletin No. 30, dated March 4, 2008. (2) Insert the following text into the rigging procedure section of your FAA-approved maintenance program (e.g. maintenance manual): CAUTION BEFORE FLIGHT WHENEVER ELEVATOR CABLES ARE RECONNECTED OR NEW CABLES INSTALLED: Always check operation of elevators after a cable reconnect by pulling back on the control and ascertain that the elevators are in the UP position. Before the next time the elevator control cable is disconnected for any reason or within the next 12 calendar months after December 30, 2008 (the effective date of this AD), whichever occurs first. Follow Maule Aerospace Technology, Inc. Mandatory Service Bulletin No. 30, dated March 4, 2008. You may insert a copy of this AD or you may insert the text located on the bottom of page 3 of Maule Aerospace Technology, Inc. Mandatory Service Bulletin No. 30, dated March 4, 2008, into the FAA-approved maintenance program (e.g. maintenance manual). Alternative Methods of Compliance (AMOCs) (f) The Manager, Atlanta Aircraft Certification Office (ACO), 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: Gerald Avella, Aerospace Engineer, One Crown Center, 1895 Phoenix Blvd., Suite 450, Atlanta, Georgia 30349; telephone: (770) 703-6066; fax: (770) 703-6097; e-mail: gerald.avella@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. Material Incorporated by Reference (g) You must use Maule Aerospace Technology, Inc. Mandatory Service Bulletin No. 30, dated March 4, 2008, to do the actions required by this AD, unless the AD specifies otherwise. (1) The Director of the Federal Register approved the incorporation by reference of this service information under 5U.S.C. 552(a) and 1 CFR part 51. (2) For service information identified in this AD, contact Maule Aerospace Technology, Inc., 2099 Georgia Highway 133 South, Moultrie, Georgia 31788; telephone: (229) 985-2045; fax: (229) 985- 2048; e-mail: engineering@mauleairinc.com; Internet: http:// www.mauleairinc.com. (3) You may review copies at the FAA, Central Region, Office of the Regional Counsel, 901 Locust, Kansas City, Missouri 64106; or 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/code_ of_federal_regulations/ibr_locations.html.

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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/2008-24-02.json · aircraft systems.