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FAA orders · airworthiness directive · current

2007-26-01: Vertical and horizontal stabilizer

FAA order 2007-26-01 is an airworthiness directive in force since January 22, 2008. The FAA's subject line: Vertical and horizontal stabilizer. It names Ayres Corporation S-2, Thrush Aircraft Inc S-2: about 346 aircraft on the U.S. register today across them, 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
Thrush Aircraft, Inc.
Models
S-2R, S2R-G1, S2R-G10, S2R-G5, S2R-G6, S2R-R1340, S2R-R1820, S2R-T11, S2R-T15, S2R-T34, S2R-T45, S2R-T65, S2R-T660, S2RHG-T34, S2RHG-T65
On this site
Ayres Corporation S-2 244 registered
Thrush Aircraft Inc S-2 102 registered

Dates and paperwork

In force since
January 22, 2008
Published
December 17, 2007 (signed December 10, 2007)
Docket
FAA-2007-28432
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 certain Thrush Aircraft, Inc. (Thrush) Model S2R series airplanes. This AD requires you to do repetitive visual inspections of the vertical and horizontal stabilizer attach fitting, attach fitting bolts, and the vertical fin aft spar for cracks or corrosion. This AD also requires immediate replacement of the vertical and horizontal stabilizer attach fittings and attach fitting bolts if cracked or corroded parts are found, and the inspection of the vertical fin aft spar with repair or replacement if cracks or corrosion are found. This AD requires the eventual replacement of the vertical and horizontal stabilizer attach fittings and attach fitting bolts if no corrosion or cracks are found as terminating action for the repetitive inspections. This AD results from reports of cracks in the empennage of Thrush S2R series airplanes. We are issuing this AD to detect and correct these cracks, which could cause the vertical stabilizer to lose structural integrity. This failure could lead to loss of control.

The order itself the regulatory text, as published

Show the full text (6,289 characters)
2007-26-01 Thrush Aircraft, Inc.: Amendment 39-15303; Docket No. FAA-2007-28432; Directorate Identifier 2007-CE-051-AD. Effective Date (a) This AD becomes effective on January 22, 2008. Affected ADs (b) None. Applicability (c) This AD applies to the following airplane models and serial numbers that are certificated in any category and are equipped with metal empennage part numbers (P/N) 40220 or 95400 (applies to serial numbers with or without a "DC'' suffix): Model Serial Numbers (1) S2R 1416R through 5100R (2) S2R-R1340 R1340-001 through R1340-035 (3) S2R-R1820 R1820-001 through R1820-036 (4) S2R-T11 T11-001 through T11-005 (5) S2R-T15 T15-001 through T15-044 and T27-001 through T27-044 (6) S2R-T34 6000 through 6049, T34-001 through T34-279, T36-001 through T36-279, T41-001 through T41-279, and T42-001 through T42-279 (7) S2RHG-T34 T34HG-101 through T34HG-107 (8) S2R-T45 T45-001 through T45-015 (9) S2R-T65 T65-001 through T65-018(10) S2RHG-T65 T65-001 through T65-018 and T65HG-011 through T65HG-019 (11) S2R-G1 G1-101 through G1-115 (12) S2R-G5 G5-101 through G5-105 (13) S2R-G6 G6-101 through G6-155 (14) S2R-G10 G10-101 through G10-168 (15) S2R-T660 T660-101 through T660-120 Unsafe Condition (d) This AD results from reports of cracks in the empennage of Thrush Aircraft, Inc., S2R series airplanes. We are issuing this AD to detect and correct these cracks, which could cause the vertical stabilizer to lose structural integrity. This condition could lead to loss of control. Compliance (e) To address this problem, you must do the following, unless already done: Actions Compliance Procedures (1) Perform a visual inspection of the vertical stabilizer attach fitting (P/N 40301-7), the horizontal stabilizer attach fitting (P/N 40303-1/-4/-7 or 95267-1), attachment bolt (P/N NAS1105-68), and the vertical fin aft spar (P/N 40261-24 or P/N 95253-1) for corrosion and cracks. Withinthe next 50 hours time-in-service (TIS) after January 22, 2008 (the effective date of this AD) and repetitively thereafter at intervals not to exceed 100 hours TIS. Follow Thrush Aircraft, Inc. Service Bulletin No. SB-AG-45, Revision B, dated June 1, 2007. (2) If corrosion or cracks are found in P/N 40301-7, 40303-1/-4/-7, 95267-1, NAS1105-68, 40261-24, or 95253-1 during any inspection required in paragraph (e)(1) of this AD: (i) Replace the vertical stabilizer attach fitting with new P/N 95266-3; the horizontal stabilizer attach fitting with new P/N 95267-5; and the attachment bolt with NAS6207-68; and (ii) If corrosion or cracks are found in the P/N 40261-24 or P/N 95253-1 vertical fin aft spar, repair in accordance with Thrush SB-AG-45, Revision B, or replace with a new P/N 40261-24 or new P/N 95253-1. Before further flight after any inspection where corrosion or cracks are found. This action terminates the repetitive inspections required in paragraph (e)(1) of this AD.Follow Thrush Aircraft, Inc. Service Bulletin No. SB-AG-45, Revision B, dated June 1, 2007. (3) If no corrosion or cracks are found in P/N 40301-7, 40303-1/-4/-7, 95267-1, NAS1105-68, 40261-24, or 95253-1 during any inspection required in paragraph (e)(1) of this AD: (i) Replace the vertical stabilizer attach fitting with new P/N 95266-3; the horizontal stabilizer attach fitting with new P/N 95267-5; and the attachment bolt with NAS6207-68; and (ii) Perform a visual inspection of the vertical fin aft spar (P/N 40261-24 or P/N 95253-1) for corrosion and cracks, and (iii) If corrosion or cracks are found in the P/N 40261-24 or P/N 95253-1 vertical fin aft spar, repair in accordance with Thrush SB-AG-45, Revision B, or replace with a new P/N 40261-24 or new P/N 95253-1. Within the next 2,000 hours TIS after January 22, 2008 (the effective date of this AD) or within 2 years after January 22, 2008 (the effective date of this AD), whichever occurs first. This action terminates the repetitive inspections required in paragraph (e)(1) of this AD. Follow Thrush Aircraft, Inc. Service Bulletin No. SB-AG-45, Revision B, dated June 1, 2007. Special Flight Permit (f) Under 14 CFR part 39.23, we are limiting the special flight permits authorized for this AD to ferry aircraft to a maintenance facility for inspection by the following conditions: (1) Hopper must be empty; (2) Vne reduced to 126 m.p.h. (109 knots); and (3) No flight into known turbulence. Alternative Methods of Compliance (AMOCs) (g) The Manager, 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: Cindy Lorenzen, Aerospace Engineer, ACE- 115A, Atlanta Aircraft Certification Office, One Crown Center, 1895 Phoenix Blvd., Suite 450, Atlanta, GA 30349; telephone: (770) 703- 6078; facsimile: (770) 703-6097; e-mail: cindy.lorenzen@faa.gov; or Mike Cann, Aerospace Engineer, ACE-117A, Atlanta Aircraft Certification Office, One Crown Center, 1895 Phoenix Blvd., Suite 450, Atlanta, Georgia 30349; telephone: (770) 703-6038; facsimile: (770) 703-6097; e-mail: michael.cann@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 (h) You must use Thrush Aircraft, Inc. Service Bulletin No. SB- AG-45, Revision B, dated June 1, 2007, 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 5 U.S.C. 552(a) and 1 CFR part 51. (2) For service information identified in this AD, contact Thrush Aircraft, Inc., P.O. Box 3149, 300 Old Pretoria Road, Albany, Georgia 31706-3149; telephone: 229-883-1440; facsimile: 229-436- 4856; or on the Internet at: http://www.thrushaircraft.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/2007-26-01.json · aircraft systems.