2023-11-07
final ruleAirworthiness Directives; Various Helicopters
Unsafe Condition: unsafe condition on these products.
Why matched: Airworthiness Directives; Various Helicopters
Brantly International, Inc. Airworthiness Directives
26 ADs indexed for Brantly International, Inc. aircraft.
Models
B-2
21 ADs
B-2A
21 ADs
B-2B
21 ADs
International, Inc.
2 ADs
International, Inc. Model B-2, B-2A, and B-2B
2 ADs
305
2 ADs
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
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
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
Various
1 AD
305
1 AD
B-2
1 AD
B-2A
1 AD
B-2B
1 AD
Recent ADs
2021-26-09 Recurring
final ruleAirworthiness Directives; Brantly Helicopters Industries U.S.A. Co., Ltd., and Brantly International, Inc., Helicopters
Unsafe Condition: cracking of the tail rotor (T/R) hub, which could result in loss of T/R control and subsequent loss of control of the helicopter.
Why matched: Airworthiness Directives; Brantly Helicopters Industries U.S.A. Co., Ltd., and Brantly International, Inc., Helicopters
2014-20-16
final ruleAirworthiness Directives; Brantly International, Inc. Helicopters
Unsafe Condition: Cracks or delamination in main rotor blades, particularly near the trailing edge, can lead to blade separation and loss of control.
Why matched: Airworthiness Directives; Brantly International, Inc. Helicopters
2006-12-07
final ruleAirworthiness Directives; Engine Components Inc. (ECi) Reciprocating Engine Cylinder Assemblies
Unsafe Condition: Cracks in the cylinder assemblies and possible engine failure caused by separation of a cylinder head.
Why matched: Airworthiness Directives; Engine Components Inc. (ECi) Reciprocating Engine Cylinder Assemblies
2006-08-07
final ruleAirworthiness Directives; Brantly International, Inc. Model B-2, B-2A, and B-2B Helicopters
Unsafe Condition: Fatigue cracking of the vertical shaft, potentially caused by misalignment, leading to shaft failure and subsequent loss of control of the helicopter.
Why matched: Airworthiness Directives; Brantly International, Inc. Model B-2, B-2A, and B-2B Helicopters
68-04-04 R2
final ruleAirworthiness Directives; BRANTLY Models B-2, B-2A, and B-2B Helicopters
Unsafe Condition: Failures of the tail rotor blade at the spar retention areas due to pitting corrosion and cracks detected through visual and dye penetrant inspections.
Why matched: Airworthiness Directives; BRANTLY Models B-2, B-2A, and B-2B Helicopters
81-17-01
final ruleAirworthiness Directives; BENDIX: Applies to Bendix Starting Vibrator Assemblies, Part Numbers 10-176485-121, -122, -241, -242; 10-382780-12, -24
Unsafe Condition: Loss of ignition due to grounding of both 'P' (Primary) leads within the starting vibrator.
Why matched: Airworthiness Directives; BENDIX: Applies to Bendix Starting Vibrator Assemblies, Part Numbers 10-176485-121, -122, -241, -242; 10-382780-12, -24
76-08-06
final ruleAirworthiness Directives; Brantly Model 305 Helicopters.
Unsafe Condition: Failure of the main rotor hub clevis bearing or torsion strap assemblies P/N C0976-1, D2225-1, or ESJ 74837/36NBC2048YZP due to deterioration, roughness, or metallic particles in the grease residue...
Why matched: Airworthiness Directives; Brantly Model 305 Helicopters.
72-21-02
final ruleAirworthiness Directives; BRANTLY Models B-2, B-2A and B-2B Helicopters
Unsafe Condition: Fatigue failure of the pylon outboard bearing shaft, Part Number 280-5 or 280-6.
Why matched: Airworthiness Directives; BRANTLY Models B-2, B-2A and B-2B Helicopters
71-17-05
final ruleAirworthiness Directives; BRANTLY ROTORCRAFT Models B-2, B-2A, and B-2B Rotorcraft
Unsafe Condition: Corrosion on the inner bore surface of the main rotor mast P/N 104-1 could impair structural integrity.
Why matched: Airworthiness Directives; BRANTLY ROTORCRAFT Models B-2, B-2A, and B-2B Rotorcraft
68-05-02
final ruleAirworthiness Directives; BRANTLY Models B-2, B-2A and B-2B Series, and 305 Helicopters
Unsafe Condition: Failure of the tail rotor drive shaft due to corrosion.
Why matched: Airworthiness Directives; BRANTLY Models B-2, B-2A and B-2B Series, and 305 Helicopters
67-09-02
final ruleAirworthiness Directives; BRANTLY Models B-2, B-2A, and B-2B Helicopters
Unsafe Condition: The Fafnir P/N 212K bearing installed on the upper main rotor mast may have insufficient service life and reliability.
Why matched: Airworthiness Directives; BRANTLY Models B-2, B-2A, and B-2B Helicopters
65-28-01
final ruleAirworthiness Directives; BRANTLY Model B-2 Series Helicopters
Unsafe Condition: Failure of the tail rotor blade grip at the outboard thrust bearing shoulder due to tool marks deeper than 0.010 inch or relief radius less than 0.020 inch.
Why matched: Airworthiness Directives; BRANTLY Model B-2 Series Helicopters
62-06-01
final ruleAirworthiness Directives; BRANTLY Model B-2 Helicopters
Unsafe Condition: Sudden movement of the seat backs to the full aft adjustment position due to the seat back adjustment wire P/N B2-334-32.
Why matched: Airworthiness Directives; BRANTLY Model B-2 Helicopters
62-05-02
final ruleAirworthiness Directives; BRANTLY All Model B-2 Helicopters
Unsafe Condition: Failure of the seals in the engine driven fuel pump due to excessively high temperature conditions in the engine compartment.
Why matched: Airworthiness Directives; BRANTLY All Model B-2 Helicopters
61-23-01
final ruleAirworthiness Directives; BRANTLY All Model B-2 Helicopters
Unsafe Condition: Bond separation between the skin and foam filler on the inboard end of the B2-248-53 and B2-248-53A main rotor blades and cracks around the root fitting in both upper and lower skins.
Why matched: Airworthiness Directives; BRANTLY All Model B-2 Helicopters
61-18-02
final ruleAirworthiness Directives; BRANTLY All Model B-2 Helicopters
Unsafe Condition: Limited tail rotor control due to insufficient directional control over a wider main rotor r.p.m. range.
Why matched: Airworthiness Directives; BRANTLY All Model B-2 Helicopters
61-16-04
final ruleAirworthiness Directives; BRANTLY Model B-2 Helicopters
Unsafe Condition: Failures of the right forward mount lug of the upper transmission case have occurred due to fatigue associated with undesirable pre-stress introduced during assembly procedures.
Why matched: Airworthiness Directives; BRANTLY Model B-2 Helicopters
61-11-02
final ruleAirworthiness Directives; All BRANTLY Model B-2 Helicopters
Unsafe Condition: Severe oil leaks from failure of the welded seam of the mixture heater oil jacket (Lycoming P/N 72396) on Lycoming VO-360 engines introduce a fire hazard and engine failure risk from oil starvation.
Why matched: Airworthiness Directives; All BRANTLY Model B-2 Helicopters
61-16-03
final ruleAirworthiness Directives; BRANTLY All B-2 Helicopters
Unsafe Condition: Improper seat installation allows the seat to slide forward of its normal position, causing interference with the collective control leading to restriction.
Why matched: Airworthiness Directives; BRANTLY All B-2 Helicopters