2026-21-04
final ruleAirworthiness Directives; Rolls-Royce Deutschland Ltd & Co KG Engines
Unsafe Condition: unsafe condition on these products.
Why matched: Airworthiness Directives; Rolls-Royce Deutschland Ltd & Co KG Engines
Engine Airworthiness Directives
2518 ADs indexed for Engine aircraft.
Models
Alliance Turbofan
21 ADs
Various
12 ADs
Various
4 ADs
24R46
4 ADs
24R46S
4 ADs
24W-46
4 ADs
24W-46S
4 ADs
TAE 125-02-99 and TAE 125-02-114 reciprocating engines
3 ADs
M601D-11
3 ADs
A-65-1
2 ADs
A-65-12
2 ADs
A-65-12F
2 ADs
A-65-12FJ
2 ADs
A-65-12J
2 ADs
A-65-14
2 ADs
A-65-14F
2 ADs
A-65-14FJ
2 ADs
A-65-14J
2 ADs
A-65-3
2 ADs
Alliance
2 ADs
24R46A (Army UC-61K)
2 ADs
24W-41A (Army UC-61A)
2 ADs
AEIO-320-E1B
2 ADs
AEIO-320-E2B
2 ADs
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
AEIO-320-D1B
1 AD
AEIO-320-D2B
1 AD
AEIO-320-E1A
1 AD
AEIO-320-E1B
1 AD
AEIO-320-E2A
1 AD
AEIO-320-E2B
1 AD
AEIO-360-B1B
1 AD
AEIO-360-B1D
1 AD
AEIO-360-B1F
1 AD
AEIO-360-B1F6
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
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
7GCAA
1 AD
A36
1 AD
DA 40
1 AD
Propeller governors
1 AD
SW205 (UH-1H)
1 AD
UH-1H
1 AD
Various
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
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
LTIO-540-J2BD
1 AD
Magnetos
1 AD
TIO-540-J2BD
1 AD
AIO-320-A1A
1 AD
AIO-320-A1B
1 AD
AIO-320-A2A
1 AD
AIO-320-A2B
1 AD
AIO-320-B1B
1 AD
AIO-320-C1B
1 AD
AIO-360-A1A
1 AD
AIO-360-A1B
1 AD
AIO-360-A2A
1 AD
Fuel Injectors
1 AD
IO-720-B1BD
1 AD
IO-720-D1CD
1 AD
Magnetos
1 AD
TIO-540-F2BD
1 AD
TIO-540-N2BD
1 AD
TIO-540-R2AD
1 AD
TH-1F
1 AD
UH-1B
1 AD
UH-1F
1 AD
UH-1H
1 AD
UH-1P
1 AD
TH-1F
1 AD
UH-1B
1 AD
UH-1F
1 AD
UH-1H
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
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
T206H
1 AD
T207A
1 AD
T210F
1 AD
T210G
1 AD
T210H
1 AD
T210J
1 AD
T210K
1 AD
T210L
1 AD
T210M
1 AD
T210N
1 AD
O-470-11
1 AD
O-470-11-CI
1 AD
O-470-11B
1 AD
O-470-11B-CI
1 AD
O-470-13
1 AD
O-470-13A
1 AD
O-470-15
1 AD
O-470-2
1 AD
O-470-4
1 AD
O-470-A
1 AD
GTSIO-520-L
1 AD
GTSIO-520-M
1 AD
GTSIO-520-N
1 AD
LTIO-540-J2B
1 AD
TSIO-520-AF
1 AD
TSIO-520-CE
1 AD
TSIO-520-P
1 AD
TSIOL-550-A
1 AD
TSIOL-550-C
1 AD
Turbochargers
1 AD
A-65-1
1 AD
A-65-12
1 AD
A-65-12F
1 AD
A-65-12FJ
1 AD
A-65-12J
1 AD
A-65-14
1 AD
A-65-14F
1 AD
A-65-14FJ
1 AD
A-65-14J
1 AD
A-65-3
1 AD
GO-300-A
1 AD
GO-300-B
1 AD
GO-300-C
1 AD
GO-300-D
1 AD
GO-300-E
1 AD
GO-300-F
1 AD
O-470-11
1 AD
O-470-11-CI
1 AD
O-470-11B
1 AD
O-470-11B-CI
1 AD
2A4-45-B2
1 AD
2A4-49-B2
1 AD
4AC-150
1 AD
4AC-176 Series
1 AD
4AC-199B2
1 AD
4AC-199B3
1 AD
4AC-199D2
1 AD
4AC-199D3
1 AD
4AC-199E2
1 AD
Magnetos
1 AD
AEIO-360-B1B
1 AD
AEIO-360-B1D
1 AD
AEIO-360-B1F
1 AD
AEIO-360-B1F6
1 AD
AEIO-360-B1G6
1 AD
AEIO-360-B2F
1 AD
AEIO-360-B2F6
1 AD
AEIO-360-B4A
1 AD
AEIO-360-H1A
1 AD
Reciprocating Engine Connecting Rods
1 AD
AEIO-320-D1B
1 AD
AEIO-320-D2B
1 AD
AEIO-320-E1A
1 AD
AEIO-320-E1B
1 AD
AEIO-320-E2A
1 AD
AEIO-320-E2B
1 AD
AEIO-360-B1B
1 AD
AEIO-360-B1D
1 AD
AEIO-360-B1F
1 AD
Reciprocating Engine Cylinder Assemblies
1 AD
24R40 (Army UC-86)
1 AD
24R40S
1 AD
24R9 (Army UC-61C)
1 AD
24R9S
1 AD
24W-40 (Army UC-61G)
1 AD
24W-40S
1 AD
24W-41 (Army UC-61)
1 AD
24W-41AS
1 AD
24W-41S
1 AD
24W-9 (Army UC-61F)
1 AD
24W-9S
1 AD
PC-203
1 AD
PX-203
1 AD
PY-203
1 AD
Auxiliary Power Units
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
IO-540-K1A5
1 AD
IO-540-K1B5
1 AD
IO-540-K1G5
1 AD
O-540-B2B5
1 AD
O-540-B2C5
1 AD
O-540-E4B5
1 AD
O-540-E4C5
1 AD
O-540-G1A5
1 AD
O-540-G2A5
1 AD
Carburetors
1 AD
O-235-C1C
1 AD
O-235-H2C
1 AD
O-235-L2A
1 AD
O-235-L2C
1 AD
O-235-N2C
1 AD
O-235-P1
1 AD
Carburetors
1 AD
O-540-L3C5D
1 AD
AEIO-320-D1B
1 AD
AEIO-320-D2B
1 AD
AEIO-320-E1A
1 AD
AEIO-320-E2A
1 AD
AEIO-360-A1A
1 AD
AEIO-360-A1B
1 AD
AEIO-360-A1B6
1 AD
AEIO-360-A1C
1 AD
AEIO-360-B1G6
1 AD
AEIO-360-H1A
1 AD
O-235-C2C
1 AD
O-235-H2C
1 AD
O-235-K2C
1 AD
O-235-L2C
1 AD
O-320-A2D
1 AD
O-320-D1D
1 AD
AEIO-320-D1B
1 AD
AEIO-320-D2B
1 AD
AEIO-320-E1A
1 AD
AEIO-320-E1B
1 AD
AEIO-320-E2A
1 AD
AEIO-320-E2B
1 AD
AEIO-360-B1B
1 AD
AEIO-360-B1D
1 AD
AEIO-360-B1F
1 AD
AEIO-360-B1F6
1 AD
IO-360-A1A
1 AD
IO-360-A1B
1 AD
IO-360-A1B6
1 AD
IO-360-A1B6D
1 AD
IO-360-A1C
1 AD
IO-360-A1D
1 AD
IO-360-A1D6
1 AD
IO-360-A1D6D
1 AD
IO-360-A2A
1 AD
IO-360-A2B
1 AD
AEIO-540-D4A5
1 AD
AEIO-540-D4B5
1 AD
AEIO-540-D4C5
1 AD
AEIO-540-D4D5
1 AD
AEIO-540-L1B5
1 AD
AEIO-540-L1B5D
1 AD
AEIO-540-L1D5
1 AD
HIO 540-A1A
1 AD
IO-540-A1A5
1 AD
IO-540-AA1A5
1 AD
35
1 AD
500A
1 AD
500B
1 AD
500S
1 AD
500U
1 AD
H35
1 AD
Hose Assemblies
1 AD
J35
1 AD
K35
1 AD
M35
1 AD
Arrius 2F
1 AD
Turn and Bank Indicators
1 AD
737-100 Series
1 AD
737-200 Series
1 AD
737-200C Series
1 AD
737-300 Series
1 AD
737-400 Series
1 AD
737-500 Series
1 AD
737-600 Series
1 AD
737-700 Series
1 AD
737-700C Series
1 AD
737-800 Series
1 AD
DC-10-10
1 AD
DC-10-10F
1 AD
DC-10-15
1 AD
DC-10-30
1 AD
DC-10-30F (KC-10A, KDC-10)
1 AD
DC-10-40
1 AD
DC-10-40F
1 AD
DC-8-11
1 AD
DC-8-12
1 AD
DC-8-21
1 AD
707-100 Long Body
1 AD
707-100B Long Body
1 AD
707-100B Short Body
1 AD
707-200
1 AD
707-300 Series
1 AD
707-300B Series
1 AD
707-300C Series
1 AD
707-400 Series
1 AD
720 Series
1 AD
720B Series
1 AD
TAE 125-01
1 AD
TAE 125-02-114
1 AD
TAE 125-02-99
1 AD
Various
1 AD
H75- 100
1 AD
M601E-11AS
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
Strobe Light Flash Tubes
1 AD
Recent ADs
2026-21-06
final ruleAirworthiness Directives; Pratt & Whitney Division Engines
Unsafe Condition: unsafe condition on these products.
Why matched: Airworthiness Directives; Pratt & Whitney Division Engines
2026-20-11
final ruleAirworthiness Directives; Rolls-Royce Deutschland Ltd & Co KG Engines
Unsafe Condition: unsafe condition on these products.
Why matched: Airworthiness Directives; Rolls-Royce Deutschland Ltd & Co KG Engines
2026-19-03
final ruleAirworthiness Directives; Safran Helicopter Engines, S.A. Engines
Unsafe Condition: The FAA is issuing this AD to address the unsafe condition on these products.
Why matched: Airworthiness Directives; Safran Helicopter Engines, S.A. Engines
2026-20-12
final ruleAirworthiness Directives; Engine Alliance Engines
Unsafe Condition: unsafe condition on these products.
Why matched: Airworthiness Directives; Engine Alliance Engines
2026-18-04 Recurring
final ruleAirworthiness Directives; Rolls-Royce Deutschland Ltd & Co KG Engines
Unsafe Condition: Sub-surface anomalies in the low-pressure compressor (LPC) blades could lead to blade failure.
Why matched: Airworthiness Directives; Rolls-Royce Deutschland Ltd & Co KG Engines
2026-17-08
final ruleAirworthiness Directives; Pratt & Whitney Division Engines
Unsafe Condition: Incorrect shot peening on high-pressure compressor (HPC) drum rotor disk assemblies.
Why matched: Airworthiness Directives; Pratt & Whitney Division Engines
2026-17-06
final ruleAirworthiness Directives; Rolls-Royce Deutschland Ltd & Co KG Engines
Unsafe Condition: Premature failure of certain lubrication/scavenge pumps causing engine in-flight shut-downs (IFSDs).
Why matched: Airworthiness Directives; Rolls-Royce Deutschland Ltd & Co KG Engines
2026-17-03
final ruleAirworthiness Directives; International Aero Engines AG Engines
Unsafe Condition: Certain 3rd stage high pressure compressor (HPC) rotor blades were susceptible to shroud wear and blade failure.
Why matched: Airworthiness Directives; International Aero Engines AG Engines
2026-18-52
final ruleAirworthiness Directives; Rolls-Royce Deutschland Ltd. & Co. KG Engines
Unsafe Condition: Non-conformances leading to low oil pressure events on low life oil pumps.
Why matched: Airworthiness Directives; Rolls-Royce Deutschland Ltd. & Co. KG Engines
2026-18-51
final ruleAirworthiness Directives; Rolls-Royce Deutschland Ltd. & Co. KG Engines
Unsafe Condition: Non-conformances leading to low oil pressure events on low life oil pumps.
Why matched: Airworthiness Directives; Rolls-Royce Deutschland Ltd. & Co. KG Engines
2026-16-08 Recurring
final ruleAirworthiness Directives; Rolls-Royce Deutschland Ltd & Co KG Engines
Unsafe Condition: Cracking of the intermediate pressure (IP) compressor variable inlet guide vanes (VIGVs) due to high-cycle fatigue propagation.
Why matched: Airworthiness Directives; Rolls-Royce Deutschland Ltd & Co KG Engines
2026-17-10
final ruleAirworthiness Directives; Lycoming Engines
Unsafe Condition: Piston pin failure resulting in metal particulate contamination in the engine oil and engine failure.
Why matched: Airworthiness Directives; Lycoming Engines
2026-15-03
final ruleAirworthiness Directives; Safran Helicopter Engines, S.A. (Type Certificate Previously Held by Turbomeca, S.A.) Engines
Unsafe Condition: unsafe condition on these products.
Why matched: Airworthiness Directives; Safran Helicopter Engines, S.A. (Type Certificate Previously Held by Turbomeca, S.A.) Engines
2026-16-13 Recurring
final ruleAirworthiness Directives; Pratt & Whitney Canada Corp. Engines
Unsafe Condition: Turbine exhaust frames manufactured from a certain material are less durable and more susceptible to developing cracks under thermal stress.
Why matched: Airworthiness Directives; Pratt & Whitney Canada Corp. Engines
2026-16-11
final ruleAirworthiness Directives; BRP-Rotax GmbH & Co KG (Formerly BRP-Powertrain GMBH & CO KG and Bombardier-Rotax GmbH) Engines and Various Aircraft
Unsafe Condition: The oil spray nozzle and certain screws were not installed on the propeller gearbox.
Why matched: Airworthiness Directives; BRP-Rotax GmbH & Co KG (Formerly BRP-Powertrain GMBH & CO KG and Bombardier-Rotax GmbH) Engines and Various Aircraft
2026-14-03
final ruleAirworthiness Directives; General Electric Company Engines
Unsafe Condition: Fuel leak caused by a defective fuel tube hose connecting the main fuel-oil heat exchanger.
Why matched: Airworthiness Directives; General Electric Company Engines
2026-14-06 Recurring
final ruleAirworthiness Directives; CFM International, S.A. Engines
Unsafe Condition: Accelerated high-pressure turbine (HPT) rotor stage 1 blade deterioration and airfoil distress in engines operating in the South Asia region.
Why matched: Airworthiness Directives; CFM International, S.A. Engines
2026-13-06 Recurring
final ruleAirworthiness Directives; Rolls-Royce Deutschland Ltd & Co KG Engines
Unsafe Condition: The main fuel hose assembly of the fuel manifold may exhibit softness, non-compliance, resistance, shrinkage, cracks, chafing, dents, kinks, necking, and degradation of the hose braid wire.
Why matched: Airworthiness Directives; Rolls-Royce Deutschland Ltd & Co KG Engines
2026-13-09 Recurring
final ruleAirworthiness Directives; Pratt & Whitney Canada Corp. Engines
Unsafe Condition: Circumferential cracks at the turbine exhaust frame external surface caused by thermal stress from engine starts.
Why matched: Airworthiness Directives; Pratt & Whitney Canada Corp. Engines