PMA Part #
(Replacement For OEM PN) |
Approval Means
Description |
PMA Holder |
| Model Eligibility |
Spring-Wing Fuel Tank Drain
(McDonnell Douglas 2381539)
|
Details Available
2381539 |
Details Available
|
|
McDonnell Douglas (DC-10-10, -30, -40, MD-11)
|
Bulkhead, Spinner Rear
(26313-000 and 23815-000)
|
Details Available
3A001-3 |
Details Available
|
|
Piper (PA-23-250, -E250, PA-24-260, PA-30 and PA-39.)
|
Propulsion System Installation
(238-1100)
|
Details Available
238-1100 |
Details Available
|
|
Airbus (A319-113,-114, A320-111, -211, -212)
|
Insulation Blanket Differential Pressure Switch
(238-1100)
|
Details Available
22M1027-113 |
Details Available
|
|
Airbus (A319-114, A320-111, -211, -212, -231)
|
Spring
(MDC 2381539)
|
Details Available
2381539 |
Details Available
|
|
McDonnell Douglas (DC-10-10,-10F, -30,-30F,-40, -40F,-15)
|
R/H Thrust Reverser
(Airbus 238-1106-501( ))
|
Details Available
238-1106-501( ) |
Details Available
|
|
Airbus (A320-111, -211)
|
Fan Reverser Inst'l
(Airbus 238-1104-501)
|
Details Available
238-1101-501( ) |
Details Available
|
|
Airbus (A320-111, -211)
|
L/H Thrust Reverser
(Airbus 238-1105-501( ))
|
Details Available
238-1105-501( ) |
Details Available
|
|
Airbus (A320-111, -211)
|
Demountable Power Plant
(Airbus 238-1103-501( ))
|
Details Available
238-1103-501( ) |
Details Available
|
|
Airbus (A320-111, -211)
|
Engine Buildup Assembly
(Airbus 238-1104-501( ))
|
Details Available
238-1104-501( ) |
Details Available
|
|
Airbus (A320-111, -211)
|
Propulsion System Installation
(Airbus 238-1100)
|
Details Available
238-1100 |
Details Available
|
|
Airbus (A319-113,-114 A320-111, -211, -212, A319-114, A320-111, -211, -212, -231)
|
Demountable Powerplant
(Airbus Industrie, 238-1103)
|
Details Available
238-1103 |
Details Available
|
|
Airbus (A320, -111, -211, -212, -231 A321, -111, -112. -131)
|
Engine Build Up
(Airbus Industrie, 238-1104)
|
Details Available
238-1104 |
Details Available
|
|
Airbus (A320, -111, -211, -212, -231 A321, -111, -112. -131)
|
LH Thrust Reverser
(Airbus Industrie, 238-1105)
|
Details Available
238-1105 |
Details Available
|
|
Airbus (A320, -111, -211, -212, -231 A321, -111, -112. -131)
|
Propulsion System Inst
(Airbus Industrie, 238-1100)
|
Details Available
238-1100 |
Details Available
|
|
Airbus (A320, -111, -211, -212, -231 A321, -111, -112. -131)
|
RH Thrust Reverser
(Airbus Industrie, 238-1106)
|
Details Available
238-1106 |
Details Available
|
|
Airbus (A320, -111, -211, -212, -231 A321, -111, -112. -131)
|
Thrust Reverser Installation
(Airbus Industrie, 238-1101)
|
Details Available
238-1101 |
Details Available
|
|
Airbus (A320, -111, -211, -212, -231 A321, -111, -112. -131)
|
Propulsion System Installation
(Airbus 238-1100-609)
|
Details Available
238-1100-609 |
Details Available
|
|
Airbus (A319-114, A320-111, -211, -212, -231)
|
Propulsion System Installation
(Airbus 238-1100-607)
|
Details Available
238-1100-607 |
Details Available
|
|
Airbus (A319-114, A320-111, -211, -212, -231)
|
Propulsion System Installation
(Airbus 238-1100-605)
|
Details Available
238-1100-605 |
Details Available
|
|
Airbus (A319-114, A320-111, -211, -212, -231)
|
Propulsion System Installation
(Airbus 238-1100-611)
|
Details Available
238-1100-611 |
Details Available
|
|
Airbus (A319-114, A320-111, -211, -212, -231)
|
Sensor T12
(GE Company 2381M33P01)
|
Details Available
509350-1 |
Details Available
|
|
GE Company TC E00078NE (GEnx1B54, GEnx1B58, GEnx1B64, GEnx1B67, GEnx1B70)
|
Spinner Bulkhead Assembly
(Piper Spinner Bulkhead asssembly 23815-000)
|
Details Available
W23815-000 |
Details Available
|
|
Piper (PA-23-250, (Ser. No. 27-2505 And Up), And All PA-23-250 with the Lycoming Turbocharger Installation PA-30 and PA-39 (All Ser. No.))
|
