Airbus Helicopters Deutschland GmbH Airworthiness Directives

191 ADs indexed for Airbus Helicopters Deutschland GmbH aircraft.

Models

MBB-BK 117 C-2 40 ADs BO-105C 38 ADs EC135T1 36 ADs EC135P1 35 ADs BO-105A 34 ADs MBB-BK 117 A-3 29 ADs EC135P2 28 ADs EC135P2+ 28 ADs EC135T2 28 ADs EC135T2+/EC635T2+ 28 ADs MBB-BK 117 A-4 27 ADs BO-105S 26 ADs MBB-BK 117 B-1 26 ADs MBB-BK 117 A-1 25 ADs MBB-BK 117 D-2 25 ADs MBB-BK 117 C-1 24 ADs MBB-BK 117 B-2 23 ADs BO-105LS A-3 15 ADs EC135P3 14 ADs EC135T3 14 ADs BO-105LS A-1 10 ADs MBB-BK 117 D-3 10 ADs EC135P1 7 ADs EC135P2 7 ADs EC135P2+ 7 ADs EC135P3 7 ADs EC135T1 7 ADs EC135T2 7 ADs EC135T3 7 ADs EC135T2+ 6 ADs EC635T2+ 6 ADs MBB-BK 117 C-2 6 ADs MBB-BK 117 D-2 6 ADs MBB-BK 117 D-3 3 ADs EC135T2+/EC635T2+ 2 ADs MBB-BK 117 A-3 2 ADs MBB-BK 117 A-4 2 ADs MBB-BK 117 B-1 2 ADs MBB-BK 117 B-2 2 ADs MBB-BK 117 C-1 2 ADs AS350B 2 ADs AS350B1 2 ADs AS350B2 2 ADs AS350B3 2 ADs AS350BA 2 ADs AS350D 2 ADs AS355E 2 ADs AS355F 2 ADs AS355F1 2 ADs AS355F2 2 ADs AS355N 2 ADs AS355NP 2 ADs EC130B4 2 ADs EC130T2 2 ADs EC135P1 2 ADs EC135P2 2 ADs EC135P2+ 2 ADs EC135P3 2 ADs EC135T1 2 ADs EC135T2 2 ADs EC135T2+/EC635T2+ 2 ADs EC135T3 2 ADs MBB-BK 117 C-2 2 ADs MBB-BK 117 D-2 2 ADs AB139 1 AD AW139 1 AD EC135P1 1 AD EC135P2 1 AD EC135P2+ 1 AD EC135T1 1 AD EC135T2 1 AD EC135T2+/EC635T2+ 1 AD MBB-BK 117 C-2 1 AD S-92A 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 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 BO-105A 1 AD BO-105C 1 AD BO-105LS A-3 1 AD BO-105S 1 AD MBB-BK 117 A-1 1 AD AS-365N2 1 AD AS-365N3 1 AD AS332C 1 AD AS332C1 1 AD AS332L 1 AD AS332L1 1 AD EC 155B 1 AD EC120B 1 AD EC155B1 1 AD MBB-BK 117 D-3 1 AD SA-365N 1 AD SA-365N1 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 AS-365N2 1 AD AS-365N3 1 AD AS332C 1 AD AS332C1 1 AD AS332L 1 AD AS332L1 1 AD AS332L2 1 AD EC 155B 1 AD EC155B1 1 AD EC225LP 1 AD A319-111 1 AD A319-112 1 AD A319-113 1 AD A319-114 1 AD A319-115 1 AD A319-131 1 AD A319-132 1 AD A319-133 1 AD A319-151N 1 AD A319-153N 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 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

Recent ADs

2026-10-20

final rule

Airworthiness Directives; Airbus Helicopters Deutschland GmbH Helicopters

Unsafe Condition: Excessive vibrations in-flight due to an incorrect installation of the angular ball bearing of the control ring assembly.

Effective: Jul 9, 2026 Category: aircraft

Why matched: Airworthiness Directives; Airbus Helicopters Deutschland GmbH Helicopters

2026-09-08

final rule

Airworthiness Directives; Airbus Helicopters Deutschland GmbH (AHD) Helicopters

Unsafe Condition: A certain part-numbered standard MS18027 type hook may be subject to localized yielding in the mating threads when assembled to higher assembly torques.

Effective: Jun 17, 2026 Category: aircraft

Why matched: Airworthiness Directives; Airbus Helicopters Deutschland GmbH (AHD) Helicopters

2026-08-51

final rule

Airworthiness Directives; Airbus Helicopters Deutschland GmbH (AHD) Helicopters

Unsafe Condition: A crack on the rotor hub-shaft, which was detected after crew reported increased vibration of the helicopter.

Effective: May 14, 2026 Category: aircraft

Why matched: Airworthiness Directives; Airbus Helicopters Deutschland GmbH (AHD) Helicopters

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

2026-06-04

final rule

Airworthiness Directives; Airbus Helicopters Deutschland GmbH

Unsafe Condition: Certain bolts installed on the horizontal control rods of the flight controls were not dye penetrant inspected for cracks during manufacturing and thus are subject to bolt failure.

Effective: Apr 30, 2026 Category: aircraft Compliance: Within the compliance times specified in EASA AD 2022-0228, unless already done.

Why matched: Airworthiness Directives; Airbus Helicopters Deutschland GmbH

Technical illustration of an aircraft flight control surface and actuator
Problem area Flight controls

2026-05-04

final rule

Airworthiness Directives; Airbus Helicopters Deutschland GmbH (AHD) Helicopters

Unsafe Condition: Main rotor head (MRH) having the same part number (P/N) and serial number (S/N) as another MRH due to incorrect modification instructions where the modified part S/N was not re-identified, which co...

Effective: Apr 17, 2026 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; Airbus Helicopters Deutschland GmbH (AHD) Helicopters

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

2026-02-01

final rule

Airworthiness Directives; Airbus Helicopters Deutschland GmbH Helicopters

Unsafe Condition: Reports of ruptured and deformed flexible couplings. The unsafe condition, if not addressed, could result in cracks and extensive deformation of flexible couplings.

Effective: Feb 26, 2026 Category: aircraft Compliance: Within 50 flight hours after the effective date.

Why matched: Airworthiness Directives; Airbus Helicopters Deutschland GmbH Helicopters

2026-02-12 Recurring

final rule

Airworthiness Directives; Airbus Helicopters Deutschland GmbH (AHD) Helicopters

Unsafe Condition: excessive wear on the bearing bolts connecting the cardan ring and the control ring assembly

Effective: Feb 17, 2026 Category: aircraft Compliance: within 830 hours time-in-service (TIS) since new accumulated by the bearing bolt, or within 10 ho...

Why matched: Airworthiness Directives; Airbus Helicopters Deutschland GmbH (AHD) Helicopters

2026-03-02 Recurring

final rule

Airworthiness Directives; Airbus Helicopters Deutschland GmbH (AHD) Helicopters

Unsafe Condition: Fatigue crack in the ring frame X9227, part numbers L535H2120301, L535H2120303, or L535H2120304, which could lead to loss of the tail rotor and consequent loss of control of the helicopter.

Effective: Feb 17, 2026 Category: aircraft Compliance: Within 12 months of the effective date of this AD.

Why matched: Airworthiness Directives; Airbus Helicopters Deutschland GmbH (AHD) Helicopters

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

2025-25-11

final rule

Airworthiness Directives; Airbus Helicopters Deutschland GmbH Helicopters

Unsafe Condition: Damage to the threaded part of the affected hoist hook and the threads of the affected hook nut due to galling.

Effective: Feb 6, 2026 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; Airbus Helicopters Deutschland GmbH Helicopters

2025-16-02

final rule

Airworthiness Directives; Airbus Helicopters Deutschland GmbH

Unsafe Condition: significant wear of the spherical bearings of the control rod assembly and pitch link assembly

Effective: Jan 12, 2026 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; Airbus Helicopters Deutschland GmbH

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

2025-25-05

final rule

Airworthiness Directives; Airbus Helicopters Deutschland GmbH (AHD) Helicopters

Unsafe Condition: Crack found on the fork lever of the mixing lever assembly, which could result in failure of the fork lever and consequent loss of control of the helicopter.

Effective: Dec 31, 2025 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; Airbus Helicopters Deutschland GmbH (AHD) Helicopters

2025-20-06

final rule

Airworthiness Directives; Airbus Helicopters Deutschland GmbH Helicopters

Unsafe Condition: Reports of airspeed and altitude indication errors due to air from the air conditioning system (ACS) condenser outlets affecting the static ports during flight.

Effective: Dec 23, 2025 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; Airbus Helicopters Deutschland GmbH Helicopters

2025-18-12

final rule

Airworthiness Directives; Airbus Helicopters Deutschland GmbH Helicopters

Unsafe Condition: Reports of momentary direct current (DC) power interruption in flight of both essential busses.

Effective: Oct 29, 2025 Category: aircraft Compliance: Within 50 flight hours

Why matched: Airworthiness Directives; Airbus Helicopters Deutschland GmbH Helicopters

2025-18-04 Recurring

final rule

Airworthiness Directives; Airbus Helicopters Deutschland GmbH Helicopters

Unsafe Condition: Failure of the hoist boom assembly, which could lead to in-flight loss of the hoist load and consequent injury to occupants.

Effective: Oct 21, 2025 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; Airbus Helicopters Deutschland GmbH Helicopters

2025-14-04

final rule

Airworthiness Directives; Airbus Helicopters Deutschland GmbH Helicopters

Unsafe Condition: over-torqued swashplate bolts on helicopters in service and in production, which could lead to damage to the swashplate bolts and to the threads of the bearing ring and control ring of the swashpla...

Effective: Jul 30, 2025 Category: aircraft Compliance: Within 50 hours time-in-service or 30 days, whichever occurs first.

Why matched: Airworthiness Directives; Airbus Helicopters Deutschland GmbH Helicopters

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

2025-13-06

final rule

Airworthiness Directives; Airbus Helicopters Deutschland GmbH Helicopters

Unsafe Condition: A broken control rod of the yaw actuator can lead to loss of control of the helicopter.

Effective: Jul 18, 2025 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; Airbus Helicopters Deutschland GmbH Helicopters

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

2025-04-10

final rule

Airworthiness Directives; Airbus Helicopters Deutschland GmbH Helicopters

Unsafe Condition: Occurrences of emergency off switches, part of the warning unit, were reported to have mechanical failures, particularly getting stuck in intermediate positions or having an untimely change of stat...

Effective: Mar 24, 2025 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; Airbus Helicopters Deutschland GmbH Helicopters

2024-25-51 Recurring

final rule

Airworthiness Directives; Airbus Helicopters Deutschland GmbH Helicopters

Unsafe Condition: A worn tail rotor actuator bolt could result in failure of a tail rotor actuator bolt, loss of tail rotor control, and subsequent loss of control of the helicopter.

Effective: Jan 17, 2025 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; Airbus Helicopters Deutschland GmbH Helicopters

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

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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