Bell Airworthiness Directives

748 ADs indexed for Bell aircraft.

Models

Various 205 ADs 47B 79 ADs 47B3 72 ADs 206A 70 ADs Helicopter Textron 62 ADs 206B 61 ADs 47D 56 ADs 47D1 56 ADs 47G 50 ADs 206L 49 ADs 206L-1 49 ADs 205A-1 49 ADs 47H-1 48 ADs 47G-2 47 ADs 212 44 ADs 47J 42 ADs 206L-3 40 ADs 47G-2A 35 ADs 47G-3 35 ADs 47J-2 35 ADs 47G-2A-1 34 ADs 47G-3B-1 34 ADs 47G-3B-2 34 ADs 47G-4 34 ADs 47G-4A 34 ADs 47G-5 34 ADs 47G-3B 33 ADs 47G-3B-2A 33 ADs 47G-5A 33 ADs 47J-2A 33 ADs 47K 33 ADs 204B 32 ADs 47E 32 ADs 222 31 ADs 206B-1 30 ADs 222B 30 ADs Textron Canada Limited 29 ADs 206A-1 (OH-58A) 29 ADs 407 28 ADs 222U 28 ADs 205A 27 ADs 47 27 ADs 412 26 ADs 206L-4 25 ADs 214ST 25 ADs 214B 22 ADs 214B-1 22 ADs Helicopter Textron Canada Limited 20 ADs 430 20 ADs 205B 20 ADs 14-13 19 ADs 14-13-2 19 ADs 230 18 ADs 407 17 ADs Textron Inc 17 ADs Helicopter Textron Canada Model 222 15 ADs 412EP 15 ADs 429 13 ADs 427 12 ADs 429 12 ADs 505 12 ADs 412CF 9 ADs Helicopter Textron Canada 8 ADs 14-13-3 8 ADs Helicopter Textron Inc 7 ADs 206L 7 ADs 206L-1 7 ADs 206L-3 7 ADs 206L-4 7 ADs Helicopter Textron Canada Model 206A 6 ADs Helicopter Textron Canada Model 407 6 ADs 407 6 ADs 14-13-3W 6 ADs 206A 5 ADs 206L 5 ADs 222 5 ADs Various 5 ADs 204B 5 ADs 210 5 ADs 206B 5 ADs 212 5 ADs 412 5 ADs 412CF 5 ADs 412EP 5 ADs 430 4 ADs 505 4 ADs 206A 4 ADs 205A 4 ADs 205A-1 4 ADs 205B 4 ADs 205B 4 ADs 412 3 ADs 412CF 3 ADs 412EP 3 ADs AB412 3 ADs AB412 EP 3 ADs 204 3 ADs 204B 3 ADs Helicopter Textron Canada Limited Model 206A 3 ADs Helicopter Textron Canada Model 206A and 206B 3 ADs Helicopter Textron Canada Model 206L 3 ADs Various 3 ADs 206A-1 (OH-58A) 3 ADs 206B-1 3 ADs 427 3 ADs 210 3 ADs 205A-1 3 ADs 212 3 ADs 412 3 ADs 412CF 3 ADs 412EP 3 ADs 47 3 ADs 47B 3 ADs 47B3 3 ADs 47D 3 ADs 47D1 3 ADs 47E 3 ADs 47G 3 ADs 47G-2 3 ADs 47G-2A 3 ADs 47G-2A-1 3 ADs 47G-3 3 ADs 47G-3B 3 ADs 47G-3B-1 3 ADs 47G-3B-2 3 ADs 47G-3B-2A 3 ADs 47G-4 3 ADs 47G-4A 3 ADs 47G-5 3 ADs 47G-5A 3 ADs 47H-1 3 ADs 47J 3 ADs 47J-2 3 ADs 47J-2A 3 ADs 47K 3 ADs Fast Kat I (U.S. Army OH-13S) 3 ADs OH-13E 3 ADs OH-13H 3 ADs 412 2 ADs 412CF 2 ADs 412EP 2 ADs AB412 2 ADs AB412 EP 2 ADs TH-1F 2 ADs TH-1L 2 ADs UH-1A 2 ADs UH-1B 2 ADs UH-1E 2 ADs UH-1F 2 ADs UH-1H 2 ADs UH-1L 2 ADs UH-1P 2 ADs 206L-4 2 ADs 230 2 ADs 427 and Model 429 2 ADs Helicopter Textron Canada Inc 2 ADs Helicopter Textron Canada Limited Model 407 2 ADs Helicopter Textron Canada Limited Model 427 2 ADs Helicopter Textron Canada Model 206L-4 2 ADs Helicopter Textron Canada Model 427 2 ADs Helicopter Textron Canada Model 430 2 ADs crank for cracks 2 ADs crank for the control linkage in the vertical stabilizer 2 ADs helicopters and the determination that these same part-numbered fittings may be installed on various restricted category 2 ADs 206 2 ADs 206A 2 ADs 206B 2 ADs 206L 2 ADs 206L-1 2 ADs 206L-3 2 ADs 206L-4 2 ADs 222 2 ADs 222B 2 ADs 222U 2 ADs 230 2 ADs 407 2 ADs 427 2 ADs 430 2 ADs 206 2 ADs 430 2 ADs 204B 2 ADs 204B 2 ADs 205A 2 ADs Aircraft Corp 2 ADs Models 14-19-3A 2 ADs 204B 1 AD 205A 1 AD 205A-1 1 AD TH-1L 1 AD UH-1B 1 AD UH-1E 1 AD UH-1F 1 AD UH-1L 1 AD TH-1L 1 AD UH-1A 1 AD UH-1B 1 AD UH-1E 1 AD UH-1F 1 AD UH-1L 1 AD F.260 1 AD F.260B 1 AD F.260C 1 AD F.260D 1 AD F.260E 1 AD F.260F 1 AD S.205 - 18/F 1 AD S.205 - 18/R 1 AD S.205 - 20/F 1 AD S.205 - 20/R 1 AD 205A 1 AD 205A-1 1 AD 205B 1 AD 212 1 AD High Landing Gear Aft Crosstube Assembly 1 AD High landing gear forward crosstube assembly 1 AD A318-111 1 AD A318-112 1 AD A318-121 1 AD A318-122 1 AD A319-111 1 AD A319-112 1 AD A319-113 1 AD A319-114 1 AD A319-115 1 AD AW139 1 AD 212 1 AD 214B 1 AD 214B-1 1 AD 214ST 1 AD 412 1 AD 412CF 1 AD 412EP 1 AD 429 1 AD 430 1 AD A109 1 AD A109A 1 AD A109A II 1 AD A109C 1 AD A109E 1 AD A109K2 1 AD A109S 1 AD AB139 1 AD AB412 1 AD AB412 EP 1 AD AS-365N3 1 AD AS332L2 1 AD AW109SP 1 AD AW139 1 AD EC135P1 1 AD EC135P2 1 AD EC135P2+ 1 AD EC135T1 1 AD EC135T2 1 AD EC135T2+/EC635T2+ 1 AD EC225LP 1 AD MBB-BK 117 C-2 1 AD MD900 1 AD S-61L 1 AD S-61N 1 AD S-61NM 1 AD S-61R 1 AD S-70 1 AD S-70A 1 AD S-70C 1 AD S-70C(M) 1 AD S-70C(M1) 1 AD S-76A 1 AD S-76B 1 AD S-76C 1 AD S-76D 1 AD S-92A 1 AD 206 1 AD 206A 1 AD 206A-1 (OH-58A) 1 AD A109 1 AD A109A 1 AD A109A II 1 AD A109C 1 AD A109E 1 AD A109K2 1 AD A109S 1 AD 206A 1 AD 206B 1 AD 206L 1 AD 206L-1 1 AD 206L-3 1 AD 206L-4 1 AD 210 1 AD 212 1 AD 407 1 AD 412 1 AD 412CF 1 AD 412EP 1 AD 427 1 AD AB412 1 AD AB412 EP 1 AD BO-105A 1 AD BO-105C 1 AD BO-105LS A-1 1 AD BO-105LS A-3 1 AD BO-105S 1 AD EC135P1 1 AD EC135P2 1 AD EC135P2+ 1 AD EC135T1 1 AD EC135T2 1 AD EC135T2+/EC635T2+ 1 AD 205A 1 AD 205A-1 1 AD 205B 1 AD 212 1 AD 206A 1 AD 206B 1 AD 206L 1 AD 206L-1 1 AD 206L-3 1 AD 206L-4 1 AD 210 1 AD 212 1 AD 369D 1 AD 369E 1 AD 369F 1 AD 369FF 1 AD 369HE 1 AD 369HM 1 AD 369HS 1 AD 407 1 AD 412 1 AD 412CF 1 AD 412EP 1 AD 500N 1 AD AB412 1 AD AB412 EP 1 AD AS350B 1 AD AS350B1 1 AD AS350B2 1 AD AS350B3 1 AD AS350BA 1 AD AS350C 1 AD AS350D 1 AD AS350D1 1 AD AS355E 1 AD AS355F 1 AD AS355F1 1 AD AS355F2 1 AD AS355N 1 AD BO-105A 1 AD BO-105C 1 AD BO-105LS A-3 1 AD BO-105S 1 AD EC120B 1 AD EC130B4 1 AD EC135P1 1 AD EC135P2 1 AD EC135P2+ 1 AD EC135P3 1 AD EC135T1 1 AD EC135T2 1 AD EC135T2+ 1 AD EC135T3 1 AD MBB-BK 117 C-2 1 AD MBB-BK 117 D-2 1 AD R44 1 AD R44 II 1 AD R66 1 AD S-76A 1 AD S-76B 1 AD S-76C 1 AD 107-II 1 AD 1100 1 AD 204B 1 AD 205A 1 AD 205A-1 1 AD 205B 1 AD 206 1 AD 206A 1 AD 206A-1 1 AD 206A-1 (OH-58A) 1 AD 206B 1 AD 206B-1 1 AD 206L 1 AD 206L-1 1 AD 206L-3 1 AD 206L-4 1 AD 210 1 AD 212 1 AD 222 1 AD 222B 1 AD 222U 1 AD 230 1 AD 234 1 AD 269A 1 AD 269A-1 1 AD 269B 1 AD 269C 1 AD 269C-1 1 AD 269D 1 AD 280 1 AD 280C 1 AD 280F 1 AD 280FX 1 AD 305 1 AD 369 1 AD 369A 1 AD 369D 1 AD 369E 1 AD 369F 1 AD 369FF 1 AD 369H 1 AD 369HE 1 AD 369HM 1 AD 369HS 1 AD 407 1 AD 412 1 AD 412CF 1 AD 412EP 1 AD 427 1 AD 429 1 AD 430 1 AD 47 1 AD 47B 1 AD 47B3 1 AD 47D 1 AD 47D1 1 AD 47E 1 AD 47G 1 AD 47G-2 1 AD 47G-2A 1 AD 47G-2A-1 1 AD 47G-3 1 AD 47G-3B 1 AD 47G-3B-1 1 AD 47G-3B-2 1 AD 47G-3B-2A 1 AD 47G-4 1 AD 47G-4A 1 AD 47G-5 1 AD 47G-5A 1 AD 47H-1 1 AD 47J 1 AD 47J-2 1 AD 47J-2A 1 AD 47K 1 AD 480 1 AD 480B 1 AD 500N 1 AD 505 1 AD 600N 1 AD A109 1 AD A109A 1 AD A109A II 1 AD A109C 1 AD A109E 1 AD A109K2 1 AD A109S 1 AD A119 1 AD AB139 1 AD AB412 1 AD AB412 EP 1 AD AS-365N2 1 AD AS-365N3 1 AD AS332C 1 AD AS332C1 1 AD AS332L 1 AD AS332L1 1 AD AS332L2 1 AD AS350B 1 AD AS350B1 1 AD AS350B2 1 AD AS350B3 1 AD AS350BA 1 AD AS350C 1 AD AS350D 1 AD AS350D1 1 AD AS355E 1 AD AS355F 1 AD AS355F1 1 AD AS355F2 1 AD AS355N 1 AD AS355NP 1 AD AW109SP 1 AD AW119 MKII 1 AD AW139 1 AD AW169 1 AD AW189 1 AD B-2 1 AD B-2A 1 AD B-2B 1 AD BO-105A 1 AD BO-105C 1 AD BO-105LS A-1 1 AD BO-105LS A-3 1 AD BO-105S 1 AD CABRI G2 1 AD CH-47D 1 AD CH-54A 1 AD EC 155B 1 AD EC120B 1 AD EC130B4 1 AD EC130T2 1 AD EC155B1 1 AD EC225LP 1 AD F-28 1 AD F-28A 1 AD F-28C 1 AD F-28C-2 1 AD F-28C-2R 1 AD F-28F 1 AD F-28F-R 1 AD FH-1100 1 AD K-190A 1 AD K-225 1 AD K-240 1 AD K-600 1 AD MBB-BK 117 A-1 1 AD MBB-BK 117 A-3 1 AD MBB-BK 117 A-4 1 AD MBB-BK 117 B-1 1 AD MBB-BK 117 B-2 1 AD MBB-BK 117 C-1 1 AD MBB-BK 117 C-2 1 AD MBB-BK 117 D-2 1 AD MBB-BK 117 D-3 1 AD MD900 1 AD OH-13E 1 AD OH-13H 1 AD PZL W-3A 1 AD R22 1 AD R22 ALPHA 1 AD R22 BETA 1 AD R22 MARINER 1 AD R44 1 AD R44 II 1 AD R66 1 AD S-51 1 AD S-52 1 AD S-55 1 AD S-55B 1 AD S-55C 1 AD S-58A 1 AD S-58B 1 AD S-58BT 1 AD S-58C 1 AD S-58D 1 AD S-58DT 1 AD S-58E 1 AD S-58ET 1 AD S-58F 1 AD S-58FT 1 AD S-58G 1 AD S-58H 1 AD S-58HT 1 AD S-58J 1 AD S-58JT 1 AD S-61A 1 AD S-61D 1 AD S-61E 1 AD S-61L 1 AD S-61N 1 AD S-61NM 1 AD S-61R 1 AD S-61V 1 AD S-64A 1 AD S-64E 1 AD S-64F 1 AD S-70 1 AD S-70A 1 AD S-70C 1 AD S-70C(M) 1 AD S-70C(M1) 1 AD S-70M 1 AD S-76A 1 AD S-76B 1 AD S-76C 1 AD S-76D 1 AD S-92A 1 AD S62A 1 AD SA 3180-Alouette Astazou 1 AD SA 318B-Alouette Astazou 1 AD SA 318C-Alouette Astazou 1 AD SA-365C 1 AD SA-365C1 1 AD SA-365C2 1 AD SA-365N 1 AD SA-365N1 1 AD SA-366G1 1 AD SA.315B Alouette III 1 AD SA.316B Alouette III 1 AD SA.316C Alouette III 1 AD SA.319B Alouette III 1 AD SA330J 1 AD SA341G 1 AD SA342J 1 AD SE 3130-Alouette II 1 AD SE 313B-Alouette II 1 AD SE.3160 Alouette III 1 AD TH-1L 1 AD TH-28 1 AD UH-12 1 AD UH-12A 1 AD UH-12B 1 AD UH-12C 1 AD UH-12E 1 AD UH-12E-L 1 AD UH-12L 1 AD UH-12L4 1 AD UH-1E 1 AD UH-1L 1 AD AS-365N3 1 AD AS332L 1 AD AS332L1 1 AD AS332L2 1 AD AS350B2 1 AD AS350B3 1 AD EC135P1 1 AD EC135P2 1 AD EC135P2+ 1 AD EC225LP 1 AD 206A 1 AD 206B 1 AD 206L 1 AD 206L-1 1 AD 206L-3 1 AD 206L-4 1 AD 407 1 AD AS350B 1 AD AS350B1 1 AD AS350B2 1 AD AS350B3 1 AD AS350BA 1 AD AS350C 1 AD AS350D 1 AD AS350D1 1 AD EC130B4 1 AD A300 B2-1A 1 AD A300 B2-1C 1 AD A300 B2-203 1 AD A300 B2K-3C 1 AD A300 B4-103 1 AD A300 B4-203 1 AD A300 B4-2C 1 AD A300 B4-601 1 AD A300 B4-603 1 AD A300 B4-605R 1 AD A 1 AD A-2 1 AD A-3 1 AD A-4 1 AD A-5 1 AD A-5T 1 AD A-6 1 AD A-7 1 AD A-7T 1 AD A-9 1 AD 14-13 1 AD 14-13-2 1 AD 14-13-3 1 AD 14-13-3W 1 AD 14-19 1 AD 14-19-2 1 AD 204B 1 AD 205A 1 AD 205A-1 1 AD SW205A-1 1 AD TH-1L 1 AD UH-1A 1 AD UH-1B 1 AD UH-1E 1 AD UH-1F 1 AD UH-1H 1 AD UH-1L 1 AD AH-1S 1 AD HH-1K 1 AD TH-1F 1 AD TH-1L 1 AD UH-1A 1 AD UH-1B 1 AD UH-1E 1 AD UH-1F 1 AD UH-1H 1 AD UH-1L 1 AD UH-1P 1 AD HH-1K 1 AD TH-1F 1 AD TH-1L 1 AD UH-1A 1 AD UH-1B 1 AD UH-1E 1 AD UH-1F 1 AD UH-1H 1 AD UH-1L 1 AD UH-1P 1 AD HH-1K 1 AD SW204HP (UH-1B) 1 AD SW205A-1 1 AD TH-1F 1 AD TH-1L 1 AD UH-1A 1 AD UH-1B 1 AD UH-1E 1 AD UH-1F 1 AD UH-1H 1 AD UH-1L 1 AD UH-1P 1 AD 206B 206L 1 AD 206B and 206L 1 AD 206L-4 and 407 1 AD 212 and 412 1 AD 407 427 1 AD 407 and 427 1 AD HH-1K 1 AD Helicopter Textron Canada Limited Model 206A and 206B 1 AD Helicopter Textron Canada Limited Model 206L 1 AD Helicopter Textron Canada Model 206L-1 and 206L-3 1 AD Helicopter Textron Canada Model 407 and 427 1 AD Helicopter Textron Model 204B 1 AD Helicopter Textron Model 206A and 206B 1 AD Helicopter Textron Model 212 1 AD Helicopter Textron Model 47D1 1 AD and Agusta model 1 AD crank 1 AD crank assembly and elevator bell crank mount 1 AD crank of the elevator push rod that can cause failure of the elevator 1 AD crank with a life limit of 40 1 AD model 1 AD Various 1 AD 172 1 AD 172A 1 AD 172B 1 AD 172C 1 AD 172D 1 AD 172E 1 AD 172F (USAF T-41A) 1 AD 172G 1 AD 172H (USAF T-41A) 1 AD 407 1 AD 150G 1 AD 172H (USAF T-41A) 1 AD 180H 1 AD 182J 1 AD 182K 1 AD 185E 1 AD 188 1 AD 206A 1 AD 210F 1 AD 210G 1 AD 206 1 AD 206A 1 AD 206A-1 (OH-58A) 1 AD 206B 1 AD 206B-1 1 AD 206L 1 AD 206L-1 1 AD 206L-3 1 AD 206L-4 1 AD Auxiliary Fuel System 1 AD 205B 1 AD 412 1 AD 204B 1 AD 205A 1 AD 205A-1 1 AD 205B 1 AD 209/AH-1G 1 AD 210 1 AD 212 1 AD AH-1S 1 AD HH-1K 1 AD SW204 (UH-1B) 1 AD SW204HP (UH-1B) 1 AD SW205 (UH-1H) 1 AD SW205A-1 1 AD TH-1F 1 AD TH-1L 1 AD UH-1A 1 AD UH-1B 1 AD UH-1E 1 AD UH-1F 1 AD UH-1H 1 AD UH-1L 1 AD UH-1P 1 AD 222 1 AD 222B 1 AD 222U 1 AD AS355E 1 AD AS355F 1 AD AS355F1 1 AD AS355F2 1 AD BO-105A 1 AD BO-105C 1 AD BO-105LS A-1 1 AD BO-105LS A-3 1 AD BO-105S 1 AD MBB-BK 117 A-1 1 AD MBB-BK 117 A-3 1 AD MBB-BK 117 A-4 1 AD MBB-BK 117 B-1 1 AD TH-1L 1 AD UH-1A 1 AD UH-1B 1 AD UH-1E 1 AD UH-1F 1 AD UH-1H 1 AD UH-1L 1 AD 204B 1 AD 205A 1 AD 205A-1 1 AD 205B 1 AD 212 1 AD UH-1B 1 AD UH-1F 1 AD UH-1H 1 AD TH-1L 1 AD UH-1E 1 AD UH-1L 1 AD 222 1 AD 222B 1 AD 222U 1 AD 230 1 AD 204B 1 AD 205A 1 AD 205A-1 1 AD 205B 1 AD 210 1 AD 212 1 AD 214B 1 AD 214B-1 1 AD 412 1 AD 412CF 1 AD 412EP 1 AD AB412 1 AD AB412 EP 1 AD HH-1K 1 AD SW204 (UH-1B) 1 AD SW204HP (UH-1B) 1 AD SW205 (UH-1H) 1 AD TH-1F 1 AD TH-1L 1 AD UH-1A 1 AD UH-1B 1 AD UH-1E 1 AD UH-1F 1 AD UH-1H 1 AD UH-1L 1 AD UH-1P 1 AD 204B 1 AD 205A 1 AD 205A-1 1 AD 205B 1 AD 210 1 AD 212 1 AD 412 1 AD 412CF 1 AD 412EP 1 AD HH-1K 1 AD SW204 (UH-1B) 1 AD SW204HP (UH-1B) 1 AD SW205 (UH-1H) 1 AD SW205A-1 1 AD TH-1F 1 AD TH-1L 1 AD UH-1A 1 AD UH-1B 1 AD UH-1E 1 AD UH-1F 1 AD UH-1H 1 AD UH-1L 1 AD UH-1P 1 AD 204B 1 AD 205A 1 AD 205A-1 1 AD SW205 (UH-1H) 1 AD SW205A-1 1 AD TH-1F 1 AD TH-1L 1 AD UH-1A 1 AD UH-1B 1 AD UH-1E 1 AD UH-1F 1 AD UH-1H 1 AD UH-1L 1 AD UH-1P 1 AD 214B 1 AD 214B-1 1 AD 214ST 1 AD Various 1 AD 14-12F-3 1 AD 14-9 1 AD 14-9L 1 AD 300-W Pacemaker 1 AD CH 1 AD CH-300 Pacemaker 1 AD CH-400 Skyrocket 1 AD E Pacemaker 1 AD F Skyrocket 1 AD Pacemaker 31-42 1 AD 120 1 AD 140 1 AD 140A 1 AD 150 1 AD 150A 1 AD 150B 1 AD 150C 1 AD 150D 1 AD 150E 1 AD CH-300 Pacemaker 1 AD 280 1 AD 280C 1 AD 280F 1 AD B-2 1 AD B-2A 1 AD B-2B 1 AD F-28 1 AD F-28A 1 AD F-28C 1 AD Starting Vibrator Assemblies 1 AD 208 1 AD 310F 1 AD 310G 1 AD 310H 1 AD 310I 1 AD 310J 1 AD 310K 1 AD CL-215-1A10 1 AD CL-215-6B11 (CL-215T Variant) 1 AD CL-215-6B11 (CL-415 Variant) 1 AD HH-1K 1 AD SW204 (UH-1B) 1 AD SW204HP (UH-1B) 1 AD SW205 (UH-1H) 1 AD TH-1F 1 AD TH-1L 1 AD UH-1A 1 AD UH-1B 1 AD UH-1E 1 AD UH-1F 1 AD UH-1H 1 AD UH-1L 1 AD UH-1P 1 AD HH-1K 1 AD TH-1F 1 AD TH-1L 1 AD UH-1A 1 AD UH-1B 1 AD UH-1E 1 AD UH-1F 1 AD UH-1H 1 AD UH-1L 1 AD UH-1P 1 AD HH-1K 1 AD TH-1F 1 AD TH-1L 1 AD UH-1A 1 AD UH-1B 1 AD UH-1E 1 AD UH-1F 1 AD UH-1H 1 AD UH-1L 1 AD UH-1P 1 AD HH-1K 1 AD TH-1F 1 AD TH-1L 1 AD UH-1A 1 AD UH-1B 1 AD UH-1E 1 AD UH-1F 1 AD UH-1H 1 AD UH-1L 1 AD UH-1P 1 AD HH-1K 1 AD SW204HP (UH-1B) 1 AD SW205A-1 1 AD TH-1F 1 AD TH-1L 1 AD UH-1A 1 AD UH-1B 1 AD UH-1E 1 AD UH-1F 1 AD UH-1H 1 AD UH-1L 1 AD UH-1P 1 AD HH-1K 1 AD SW205A-1 1 AD TH-1F 1 AD TH-1L 1 AD UH-1A 1 AD UH-1B 1 AD UH-1E 1 AD UH-1F 1 AD UH-1H 1 AD UH-1L 1 AD UH-1P 1 AD 47D1 1 AD 47G 1 AD 47G-2 1 AD 47G-2A 1 AD 47G-2A-1 1 AD 47G-3 1 AD 47G-3B 1 AD 47G-3B-1 1 AD 47G-3B-2 1 AD 47G-3B-2A 1 AD 47G-4 1 AD 47G-4A 1 AD 47G-5 1 AD 47G-5A 1 AD OH-13H 1 AD 328-100 1 AD F.260 1 AD F.260B 1 AD F.260C 1 AD F.260D 1 AD F.260E 1 AD GTX 33 1 AD GTX 330 1 AD GTX 330D 1 AD GTX 33D 1 AD 47G 1 AD 47G-2 1 AD 47G-2A 1 AD 47G-2A-1 1 AD 47G-3 1 AD 47G-3B 1 AD 47G-3B-1 1 AD 47G-3B-2 1 AD 47G-3B-2A 1 AD UH-12D 1 AD HH-1K 1 AD TH-1F 1 AD TH-1L 1 AD UH-1A 1 AD UH-1B 1 AD UH-1E 1 AD UH-1F 1 AD UH-1H 1 AD UH-1L 1 AD UH-1P 1 AD HH-1K 1 AD TH-1F 1 AD TH-1L 1 AD UH-1A 1 AD UH-1B 1 AD UH-1E 1 AD UH-1F 1 AD UH-1H 1 AD UH-1L 1 AD UH-1P 1 AD HH-1K 1 AD SW204HP (UH-1B) 1 AD SW205A-1 1 AD TH-1F 1 AD TH-1L 1 AD UH-1A 1 AD UH-1B 1 AD UH-1E 1 AD UH-1F 1 AD UH-1H 1 AD UH-1L 1 AD UH-1P 1 AD HH-1K 1 AD SW204 (UH-1B) 1 AD SW204HP (UH-1B) 1 AD SW205 (UH-1H) 1 AD SW205A-1 1 AD TH-1F 1 AD TH-1L 1 AD UH-1A 1 AD UH-1B 1 AD UH-1E 1 AD UH-1F 1 AD UH-1H 1 AD UH-1L 1 AD UH-1P 1 AD HH-1K 1 AD SW204HP (UH-1B) 1 AD SW205A-1 1 AD TH-1F 1 AD TH-1L 1 AD UH-1A 1 AD UH-1B 1 AD UH-1E 1 AD UH-1F 1 AD UH-1H 1 AD UH-1L 1 AD UH-1P 1 AD HH-1K 1 AD SW204HP (UH-1B) 1 AD SW205A-1 1 AD TH-1F 1 AD TH-1L 1 AD UH-1A 1 AD UH-1B 1 AD UH-1E 1 AD UH-1F 1 AD UH-1H 1 AD UH-1L 1 AD UH-1P 1 AD 47B 1 AD 47B3 1 AD 47D 1 AD 47D1 1 AD 47E 1 AD 47G 1 AD 47G-3 1 AD 47H-1 1 AD OH-13E 1 AD AC32 1 AD AS332C 1 AD AS332C1 1 AD AS332L 1 AD AS332L1 1 AD AS332L2 1 AD CN-235 1 AD CN-235-100 1 AD CN-235-200 1 AD CN-235-300 1 AD HH-1K 1 AD SW204 (UH-1B) 1 AD SW204HP (UH-1B) 1 AD SW205 (UH-1H) 1 AD SW205A-1 1 AD TH-1F 1 AD TH-1L 1 AD UH-1A 1 AD UH-1B 1 AD UH-1E 1 AD UH-1F 1 AD UH-1H 1 AD UH-1L 1 AD UH-1P 1 AD

Recent ADs

2026-14-07 Recurring

final rule

Airworthiness Directives; Bell Textron Canada Limited Helicopters

Unsafe Condition: unsafe condition on these products.

Effective: Aug 21, 2026 Category: aircraft

Why matched: Airworthiness Directives; Bell Textron Canada Limited Helicopters

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2026-13-12

final rule

Airworthiness Directives; Bell Textron Canada Limited Helicopters

Unsafe Condition: The unsafe condition involves exceeding life limits on the main rotor (M/R) clevises, universal bearings, and universal to pitch link bolts, which could result in failure of these components and su...

Effective: Aug 11, 2026 Category: aircraft

Why matched: Airworthiness Directives; Bell Textron Canada Limited Helicopters

Technical illustration of a helicopter rotor hub assembly
Problem area Rotor system
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2026-12-04

final rule

Airworthiness Directives; Airbus SAS Airplanes

Unsafe Condition: Improper application of the fastener retorque process at the center wing box and belly fairing junctions could lead to insufficient clamping.

Effective: Jul 14, 2026 Category: aircraft

Why matched: Airworthiness Directives; Airbus SAS Airplanes

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2026-11-08

final rule

Airworthiness Directives; Airbus SAS Airplanes

Unsafe Condition: Double overcoating sealant was not applied during production on certain fasteners in the center wing box and belly faring junction for both left-hand and right-hand sides, and certain fasteners are...

Effective: Jul 9, 2026 Category: aircraft

Why matched: Airworthiness Directives; Airbus SAS Airplanes

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2026-10-04

final rule

Airworthiness Directives; Bell Textron Canada Limited Helicopters

Unsafe Condition: Chafing can occur at various locations on the electrical harnesses located in the aircraft instrument panel area.

Effective: Jun 25, 2026 Category: aircraft

Why matched: Airworthiness Directives; Bell Textron Canada Limited Helicopters

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2026-06-02

final rule

Airworthiness Directives; Bell Textron Canada Limited Helicopters

Unsafe Condition: Incorrectly installed lockwire on the stability and control augmentation system (SCAS) actuator jam nut could allow the actuator jam nut to loosen.

Effective: Apr 24, 2026 Category: aircraft Compliance: Within 50 flight hours after the effective date of this AD.

Why matched: Airworthiness Directives; Bell Textron Canada Limited Helicopters

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2026-05-51

final rule

Airworthiness Directives; Bell Textron Canada Limited Helicopters

Unsafe Condition: A failure of the hinge assembly on the aft movable ballast box assembly, which could allow the ballast weights to escape the ballast box and strike the tail rotor assembly.

Effective: Apr 16, 2026 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; Bell Textron Canada Limited Helicopters

Technical illustration of a helicopter rotor hub assembly
Problem area Rotor system
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2025-25-01 Recurring

final rule

Airworthiness Directives; Bell Textron Canada Limited Helicopters

Unsafe Condition: Cracked transmission oil check valve (part number 209-062-520-001) caused by incorrect torque application during assembly, potentially leading to degradation or loss of lubrication to the transmiss...

Effective: Jan 16, 2026 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; Bell Textron Canada Limited Helicopters

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2025-22-03

final rule

Airworthiness Directives; Bell Textron Canada Limited Helicopters

Unsafe Condition: Deformation and improper pin engagement in the knuckles of the door hinge on the aft movable ballast box assembly, which could allow the ballast weights to escape the ballast box and strike the tai...

Effective: Nov 20, 2025 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; Bell Textron Canada Limited Helicopters

Technical illustration of a helicopter rotor hub assembly
Problem area Rotor system
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2025-18-10

final rule

Airworthiness Directives; Bell Textron Canada Limited Helicopters

Unsafe Condition: A cracked mounting bracket on the oil cooler fan assembly housing can lead to failure of the drive shaft, loss of the tail rotor drive, and consequent loss of control of the helicopter.

Effective: Sep 25, 2025 Category: aircraft Compliance: Within 25 hours time-in-service or 30 days, whichever occurs first.

Why matched: Airworthiness Directives; Bell Textron Canada Limited Helicopters

Technical illustration of a helicopter rotor hub assembly
Problem area Rotor system
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2025-13-01

final rule

Airworthiness Directives; Bell Textron Canada Limited Helicopters

Unsafe Condition: Expandable blade bolts installed on the main rotor blade may not have received the correct heat treatment, which could result in stress corrosion cracking and failure of the main rotor blade assemb...

Effective: Jul 8, 2025 Category: aircraft Compliance: Within 30 hours time-in-service or 30 days, whichever occurs first.

Why matched: Airworthiness Directives; Bell Textron Canada Limited Helicopters

Technical illustration of a helicopter rotor hub assembly
Problem area Rotor system
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2025-07-01

final rule

Airworthiness Directives; Thommen Aircraft Equipment AG Digital Air Data Computers

Unsafe Condition: Occurrences of AC32 Digital ADCs that stopped functioning due to the power module failing at temperatures below -20 degrees Celsius.

Effective: May 15, 2025 Category: aircraft Compliance: Within 12 months after the effective date of this AD

Why matched: Airworthiness Directives; Thommen Aircraft Equipment AG Digital Air Data Computers

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2025-09-01 Recurring

final rule

Airworthiness Directives; Bell Textron Canada Limited Helicopters

Unsafe Condition: Possible chafing in certain locations between the basic and supplemental helicopter wiring and the structure, which could lead to a short to ground and command the engine to idle, resulting in loss...

Effective: May 13, 2025 Category: aircraft Compliance: Within 50 flight hours or 30 days, whichever occurs first.

Why matched: Airworthiness Directives; Bell Textron Canada Limited Helicopters

Technical illustration of an aircraft electrical generator and wiring assembly
Problem area Electrical system
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2025-09-03 Recurring

final rule

Airworthiness Directives; Bell Textron Canada Limited Helicopters

Unsafe Condition: Crack initiation at the main rotor (M/R) clevis neck or threaded area, leading to failure of the M/R pitch link, which could result in loss of control of the helicopter.

Effective: May 13, 2025 Category: aircraft Compliance: Within 12 months of effective date

Why matched: Airworthiness Directives; Bell Textron Canada Limited Helicopters

Technical illustration of a helicopter rotor hub assembly
Problem area Rotor system
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2025-06-51

final rule

Airworthiness Directives; Bell Textron Canada Limited Helicopters

Unsafe Condition: Deformation and/or improper pin engagement in the knuckles of the door hinge on the aft movable ballast box assembly, part number SLS-706-201-007, could lead to ballast weights escaping the ballast...

Effective: Apr 25, 2025 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; Bell Textron Canada Limited Helicopters

Technical illustration of a helicopter rotor hub assembly
Problem area Rotor system
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2024-20-07 Recurring

final rule

Airworthiness Directives; Various Helicopters

Unsafe Condition: Difficulty pulling the emergency float kit activation handle installed on the pilot cyclic, and deficiencies in the installation of the cables on the emergency float kits.

Effective: Dec 5, 2024 Category: aircraft Compliance: Within 50 flight hours

Why matched: Airworthiness Directives; Various Helicopters

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2024-16-19 Recurring

final rule

Airworthiness Directives; Bell Textron Inc. Helicopters

Unsafe Condition: Cracked tail boom attachment barrel nuts (barrel nuts) due to corrosion damage, high time in service, or hydrogen embrittlement, which can cause loss of torque on the associated bolt and subsequent...

Effective: Nov 8, 2024 Category: aircraft Compliance: Within 5,000 flight hours or 5 years, depending on the specific helicopter model and serial number.

Why matched: Airworthiness Directives; Bell Textron Inc. Helicopters

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2024-17-02

final rule

Airworthiness Directives; Bell Textron Inc. Helicopters

Unsafe Condition: Failure of the tail boom attachment structure, including fatigue cracking of tail boom attachment fittings, cap angles, longerons, and bolts.

Effective: Nov 8, 2024 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; Bell Textron Inc. Helicopters

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2024-15-10

final rule

Airworthiness Directives; Bell Textron Canada Limited Helicopters

Unsafe Condition: Fuel leakage discovered during fuel system crash impact testing activity. The fuel drain quick disconnect valve catches on the airframe cutout upon impact, resisting against the fuel bladder rotati...

Effective: Oct 21, 2024 Category: aircraft Compliance: Within the compliance times specified in Transport Canada AD CF-2023-51.

Why matched: Airworthiness Directives; Bell Textron Canada Limited Helicopters

Technical illustration of an aircraft fuel pump, filter, valve, and lines
Problem area Fuel system
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2024-19-17

final rule

Airworthiness Directives; Bell Textron Inc. and Various Restricted Category Helicopters

Unsafe Condition: The failure of a tension torsion (TT) strap, which can result in loss of a main rotor blade and subsequent loss of control of the helicopter.

Effective: Oct 11, 2024 Category: aircraft Compliance: Within 50 hours time-in-service (TIS)

Why matched: Airworthiness Directives; Bell Textron Inc. and Various Restricted Category Helicopters

Technical illustration of a helicopter rotor hub assembly
Problem area Rotor system
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