AD 2024-08082
Published 2024-04-17 · 191 models · 87,814 US-registered tails affected · Federal Register
Airworthiness Directives; Various Airplanes Federal Register ↗
Abstract
The FAA is revising a notice of proposed rulemaking (NPRM) that applied to various airplanes modified with a certain configuration of the Garmin GFC 500 Autopilot System installed per Supplemental Type Certificate (STC) No. SA01866WI. This action revises the NPRM by removing airplane models from and adding airplane models to the applicability. The FAA is proposing this airworthiness directive to address the unsafe condition on these products. Since this action would expand the applicability for the required action as proposed in the NPRM, the agency is requesting comments on this SNPRM.
Applicability · by US fleet size
- PIPER PA-28-140 TCDS 2A13 4,260 tails
- CESSNA 172M TCDS 3A12 3,578 tails
- PIPER PA-28-181 TCDS 2A13 3,535 tails
- PIPER PA-28-180 TCDS 2A13 3,506 tails
- CESSNA 172N TCDS 3A12 3,138 tails
- CESSNA 172S TCDS 3A12 3,136 tails
- BEECH A36 TCDS 3A15 2,355 tails
- CESSNA 182P TCDS 3A13 2,100 tails
- CESSNA 172 TCDS 3A12 1,805 tails
- CESSNA 140 TCDS A-768 1,601 tails
- CESSNA 182Q TCDS 3A13 1,565 tails
- PIPER PA-28-161 TCDS 2A13 1,525 tails
- MOONEY M20J TCDS 2A3 1,407 tails
- CESSNA 182T TCDS 3A13 1,312 tails
- MOONEY M20C TCDS 2A3 1,257 tails
- PIPER PA-28R-200 TCDS 2A13 1,223 tails
- PIPER PA-24-250 TCDS 1A15 1,222 tails
- CESSNA 180 TCDS 5A6 1,178 tails
- TEXTRON AVIATION 172S TCDS 3A12 1,155 tails
- CESSNA 172P TCDS 3A12 1,110 tails
- CESSNA T206H TCDS A4CE 1,052 tails
- CESSNA 172K TCDS 3A12 1,026 tails
- PIPER PA-32-300 TCDS A3SO 993 tails
- BEECH F33A TCDS 3A15 978 tails
- PIPER PA-28-151 TCDS 2A13 961 tails
- BEECH V35B TCDS 3A15 913 tails
- PIPER PA-30 TCDS A1EA 877 tails
- CESSNA T182T TCDS 3A13 876 tails
- PIPER PA-28-235 TCDS 2A13 859 tails
- CESSNA 172L TCDS 3A12 858 tails
- CESSNA 177B TCDS A13CE 842 tails
- MOONEY M20E TCDS 2A3 829 tails
- CESSNA 177RG TCDS A20CE 788 tails
- CESSNA 172H TCDS 3A12 780 tails
- MOONEY M20K TCDS 2A3 771 tails
- CESSNA 172G TCDS 3A12 721 tails
- MOONEY M20F TCDS 2A3 721 tails
- CESSNA 172F TCDS 3A12 717 tails
- CESSNA R182 TCDS 3A13 706 tails
- CESSNA 172R TCDS 3A12 683 tails
- CESSNA R172K TCDS 3A17 653 tails
- PIPER PA-32-260 TCDS A3SO 650 tails
- CESSNA 172E TCDS 3A12 616 tails
- CESSNA 182S TCDS 3A13 606 tails
- PIPER PA-24-260 TCDS 1A15 590 tails
- PIPER PA-32R-301T TCDS A3SO 536 tails
- PIPER PA-28R-180 TCDS 2A13 535 tails
- PIPER PA-32R-300 TCDS A3SO 510 tails
- CESSNA 182R TCDS 3A13 487 tails
- CESSNA 182J TCDS 3A13 487 tails
- PIPER PA-28-236 TCDS 2A13 480 tails
- CESSNA 172D TCDS 3A12 471 tails
- CESSNA T210N TCDS 3A21 468 tails
- CESSNA TR182 TCDS 3A13 465 tails
- BEECH S35 TCDS 3A15 459 tails
- BEECH C23 TCDS A1CE 457 tails
- PIPER PA-32R-301 TCDS A3SO 456 tails
- RAYTHEON A36 TCDS 3A15 449 tails
- CESSNA 172RG TCDS 3A17 447 tails
- CESSNA 182 TCDS 3A13 446 tails
- CESSNA 177 TCDS A13CE 446 tails
- CESSNA 182M TCDS 3A13 432 tails
- BEECH V35 TCDS 3A15 425 tails
- CESSNA 182H TCDS 3A13 423 tails
- CESSNA 182K TCDS 3A13 413 tails
- CESSNA 182L TCDS 3A13 410 tails
- MOONEY M20R TCDS 2A3 399 tails
- CESSNA 182G TCDS 3A13 391 tails
- CESSNA 150 TCDS 3A19 387 tails
- CESSNA 182E TCDS 3A13 380 tails
- PIPER PA-28R-201T TCDS 2A13 368 tails
- TEXTRON AVIATION T206H TCDS A4CE 356 tails
- CESSNA 172I TCDS 3A12 353 tails
- PIPER PA-28R-201 TCDS 2A13 352 tails
- CESSNA U206G TCDS A4CE 347 tails
- PIPER PA-24 TCDS 1A15 346 tails
- TEXTRON AVIATION 182T TCDS 3A13 341 tails
- CESSNA 182N TCDS 3A13 336 tails
- CESSNA T210M TCDS 3A21 321 tails
- BEECH V35A TCDS 3A15 321 tails
- BEECH P35 TCDS 3A15 319 tails
- BEECH B36TC TCDS 3A15 307 tails
- CESSNA T210L TCDS 3A21 306 tails
- CESSNA 182F TCDS 3A13 294 tails
- BEECH 35-B33 TCDS A-777TCDS 3A15 290 tails
- BEECH 35 TCDS A-777TCDS 3A15 266 tails
- BEECH C35 TCDS A-777 258 tails
- PIPER PA-28RT-201T TCDS 2A13 255 tails
- PIPER PA-28-160 TCDS 2A13 253 tails
- MOONEY M20M TCDS 2A3 249 tails
- BEECH K35 TCDS 3A15 237 tails
- CESSNA 210L TCDS 3A21 235 tails
- BEECH 200 TCDS A24CE 234 tails
- CESSNA U206F TCDS A4CE 231 tails
- BEECH M35 TCDS 3A15 225 tails
- BEECH H35 TCDS 3A15 224 tails
- BEECH G35 TCDS A-777 224 tails
- BEECH J35 TCDS 3A15 221 tails
- CESSNA TU206G TCDS A4CE 206 tails
- PIPER PA-32RT-300T TCDS A3SO 205 tails
- PIPER PA-32RT-300 TCDS A3SO 201 tails
- BEECH F35 TCDS A-777 192 tails
- CESSNA 210 TCDS 3A21 188 tails
- BEECH 35-C33 TCDS A-777TCDS 3A15 185 tails
- PIPER PA-28RT-201 TCDS 2A13 179 tails
- BEECH C24R TCDS A1CE 176 tails
- BEECH A36TC TCDS 3A15 173 tails
- PIPER PA-32-301 TCDS A3SO 167 tails
- BEECH N35 TCDS 3A15 167 tails
- CESSNA 206H TCDS A4CE 159 tails
- BEECH 76 TCDS A29CE 155 tails
- BEECH B19 TCDS A1CE 145 tails
- BEECH D35 TCDS A-777 142 tails
- BEECH E35 TCDS A-777 141 tails
- BEECH 35-33 TCDS A-777TCDS 3A15 130 tails
- CESSNA 210M TCDS 3A21 128 tails
- BEECH 300 TCDS A24CE 126 tails
- CESSNA 210D TCDS 3A21 123 tails
- PIPER PA-28-150 TCDS 2A13 121 tails
- BEECH A23-24 TCDS A1CE 121 tails
- BEECH B24R TCDS A1CE 117 tails
- PIPER PA-28 TCDS 2A13 117 tails
- BEECH 35-C33A TCDS A-777TCDS 3A15 113 tails
- BEECH 36 TCDS 3A15 111 tails
- BEECH 77 TCDS A30CE 111 tails
- TEXTRON AVIATION T182T TCDS 3A13 94 tails
- MOONEY M20D TCDS 2A3 88 tails
- CESSNA TU206F TCDS A4CE 87 tails
- BEECH 35-A33 TCDS A-777TCDS 3A15 84 tails
- BEECH A23 TCDS A1CE 84 tails
- CESSNA 210N TCDS 3A21 83 tails
- RAYTHEON B36TC TCDS 3A15 82 tails
- PIPER PA-39 TCDS A1EA 82 tails
- PIPER PA-32-301T TCDS A3SO 81 tails
- CESSNA 210E TCDS 3A21 75 tails
- BEECH A23-19 TCDS A1CE 72 tails
- CESSNA T210F TCDS 3A21 65 tails
- CESSNA 500 TCDS A22CE 64 tails
- BEECH E33 TCDS 3A15 62 tails
- PIPER PA-28-201T TCDS 2A13 62 tails
- BEECH B23 TCDS A1CE 61 tails
- MOONEY M20S TCDS 2A3 58 tails
- CESSNA T182 TCDS 3A13 58 tails
- CESSNA 206 TCDS A4CE 55 tails
- CESSNA 210J TCDS 3A21 55 tails
- BEECH A23A TCDS A1CE 51 tails
- BEECH E33A TCDS 3A15 51 tails
- BEECH A24R TCDS A1CE 50 tails
- CESSNA 210K TCDS 3A21 50 tails
- CESSNA U206C TCDS A4CE 47 tails
- BEECH G33 TCDS 3A15 41 tails
- BEECH 19A TCDS A1CE 40 tails
- CESSNA 210G TCDS 3A21 39 tails
- CESSNA 210H TCDS 3A21 38 tails
- CESSNA 210F TCDS 3A21 34 tails
- COMMANDER 114TC TCDS A12SO 33 tails
- CESSNA U206E TCDS A4CE 31 tails
- CESSNA P206D TCDS A4CE 28 tails
- CESSNA T210K TCDS 3A21 26 tails
- CESSNA T210H TCDS 3A21 26 tails
- CESSNA T210G TCDS 3A21 25 tails
- CESSNA U206D TCDS A4CE 25 tails
- MOONEY M20 TCDS 2A3 23 tails
- CESSNA P172D TCDS 3A17 23 tails
- BEECH E33C TCDS 3A15 20 tails
- NEW PIPER PA-32R-301T TCDS A3SO 19 tails
- CESSNA T210J TCDS 3A21 19 tails
- CESSNA P206C TCDS A4CE 18 tails
- BEECH F33C TCDS 3A15 17 tails
- NEW PIPER PA-28-181 TCDS 2A13 16 tails
- NEW PIPER PA-28-161 TCDS 2A13 15 tails
- BEECH F33 TCDS 3A15 14 tails
- CESSNA 172Q TCDS 3A12 13 tails
- CESSNA TU206C TCDS A4CE 13 tails
- CESSNA P206E TCDS A4CE 9 tails
- NEW PIPER PA-32-301XTC TCDS A3SO 7 tails
- NEW PIPER PA-32R-301 TCDS A3SO 6 tails
- CESSNA TP206C TCDS A4CE 6 tails
- CESSNA TU206D TCDS A4CE 5 tails
- MOONEY INTERNATIONAL M20R TCDS 2A3 4 tails
- CESSNA TP206D TCDS A4CE 4 tails
- CESSNA TP206E TCDS A4CE 2 tails
- BEECH 33 2 tails
- CESSNA F177RG TCDS A26EU 2 tails
- BEECH 45 TCDS 5A3 2 tails
- CESSNA F172G TCDS A4EU 2 tails
- CESSNA FR172K TCDS A18EU 1 tails
- CESSNA F172H TCDS A4EU 1 tails
- AIR COMMAND COMMANDER 1 tails
- CESSNA F172M TCDS A4EU 1 tails
- CESSNA TU206E TCDS A4CE 1 tails
Federal Register text
Verbatim; the Federal Register publication is the legally binding document. Cite: 89 FR 27398. View on Federal Register ↗
[Federal Register Volume 89, Number 75 (Wednesday, April 17, 2024)] [Proposed Rules] [Pages 27398-27401] From the Federal Register Online via the Government Publishing Office [www.gpo.gov] [FR Doc No: 2024-08082]
======================================================================== Proposed Rules Federal Register ________________________________________________________________________ This section of the FEDERAL REGISTER contains notices to the public of the proposed issuance of rules and regulations. The purpose of these notices is to give interested persons an opportunity to participate in the rule making prior to the adoption of the final rules. ========================================================================
Federal Register / Vol. 89, No. 75 / Wednesday, April 17, 2024 / Proposed Rules
[[Page 27398]]
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2023-1990; Project Identifier AD-2023-00734-A] RIN 2120-AA64
Airworthiness Directives; Various Airplanes
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Supplemental notice of proposed rulemaking (SNPRM).
-----------------------------------------------------------------------
SUMMARY: The FAA is revising a notice of proposed rulemaking (NPRM) that applied to various airplanes modified with a certain configuration of the Garmin GFC 500 Autopilot System installed per Supplemental Type Certificate (STC) No. SA01866WI. This action revises the NPRM by removing airplane models from and adding airplane models to the applicability. The FAA is proposing this airworthiness directive to address the unsafe condition on these products. Since this action would expand the applicability for the required action as proposed in the NPRM, the agency is requesting comments on this SNPRM.
DATES: The FAA must receive comments on this SNPRM by June 3, 2024.
ADDRESSES: You may send comments, using the procedures found in 14 CFR 11.43 and 11.45, by any of the following methods: Federal eRulemaking Portal: Go to regulations.gov. Follow the instructions for submitting comments. Fax: (202) 493-2251. Mail: U.S. Department of Transportation, Docket Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New Jersey Avenue SE, Washington, DC 20590. Hand Delivery: Deliver to Mail address above between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. AD Docket: You may examine the AD docket at regulations.gov under Docket No. FAA-2023-1990; or in person at Docket Operations between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. The AD docket contains this SNPRM, any comments received, and other information. The street address for Docket Operations is listed above.
FOR FURTHER INFORMATION CONTACT: Christopher Withers, Aviation Safety Engineer, FAA, 1801 S Airport Road, Wichita, KS 67209; phone: (316) 946-4190; email: [email protected].