# Turbomeca ARRIEL-1D

- Type: Engine model (FAA registry)
- Registry code: 60048
- Manufacturer (registry): TURBOMECA
- Model: ARRIEL 1D
- Engine type: Turbo-shaft
- Power: 684 hp
- Data sheet: [TCDS E19EU](https://openairdocs.org/tcds/E19EU) (OpenAirDocs)
- Holder: Safran Helicopter Engines, S.A.S.
- Installed in: 0 registered aircraft
- Page: https://openairdocs.org/engine/turbomeca-arriel-1d

Model codes come from the FAA registry's reference file.

## ADs that may apply (OpenAirDocs)

Matched to this engine model by model name and maker. Each AD's applicability may narrow it by serial number, part number or equipment.

- [AD 2017-15-07](https://openairdocs.org/ad/2017-15-07): Fuel Control/Turbine Engines · Safran Helicopter Engines Arriel 1A1, Arriel 1A2, Arriel 1B and 9 more. Effective Aug 8, 2017
- [AD 2016-22-10](https://openairdocs.org/ad/2016-22-10): Centrifugal impeller · Turbomeca Arriel 1, Arriel 1A, Arriel 1A1 and 13 more. Effective Dec 6, 2016
- [AD 2016-11-09](https://openairdocs.org/ad/2016-11-09): Divergent rubbing between the piston shaft small diameter labyrinth and the rear bearing support · Turbomeca Arriel 1D and Arriel 1D1. Effective Jul 5, 2016
- [AD 2015-13-04](https://openairdocs.org/ad/2015-13-04): Engine accessory gearbox (AGB) · Turbomeca Arriel 1A1, Arriel 1A2, Arriel 1B and 16 more. Effective Sep 1, 2015
- [AD 2013-24-05](https://openairdocs.org/ad/2013-24-05): Free turbine module · Turbomeca Arriel 1A1, Arriel 1A2, Arriel 1B and 9 more. Effective Jan 28, 2014
- [AD 2013-08-22](https://openairdocs.org/ad/2013-08-22): Tachometer's unit cycle-counting feature · Turbomeca Arriel 1A1, Arriel 1A2, Arriel 1B and 9 more. Effective May 28, 2013
- [AD 2012-27-02](https://openairdocs.org/ad/2012-27-02): High gas generator speed (NG) rating vibration check · Turbomeca Arriel 1A1, Arriel 1A2, Arriel 1B and 9 more. Effective Feb 14, 2013
- [AD 2012-24-03](https://openairdocs.org/ad/2012-24-03): Gas generator rotating assembly · Turbomeca Arriel 1A, Arriel 1A1, Arriel 1A2 and 10 more. Effective Jan 7, 2013
- [AD 2010-19-06 R1](https://openairdocs.org/ad/2010-19-06-R1): Turbine disc · Turbomeca Arriel 1A, Arriel 1A1, Arriel 1B and 6 more. Effective Jan 17, 2012
- [AD 2010-10-09](https://openairdocs.org/ad/2010-10-09): 2nd stage turbine blades · Turbomeca Arriel 1B, Arriel 1D, Arriel 1D1 and 1 more. Effective Jun 21, 2010
- [AD 2009-08-08 R1](https://openairdocs.org/ad/2009-08-08-R1): PT Blades · Turbomeca Arriel 1B, Arriel 1D, Arriel 1D1 and 2 more. Effective May 7, 2010
- [AD 2010-02-01](https://openairdocs.org/ad/2010-02-01): Reduction Gear Box Intermediate Pinion · Turbomeca Arriel 1B, Arriel 1D and Arriel 1D1. Effective Feb 18, 2010
- [AD 2009-26-07](https://openairdocs.org/ad/2009-26-07): Reduction gearboxes (module M05) · Turbomeca Arriel 1A1, Arriel 1A2, Arriel 1B and 9 more. Effective Jan 12, 2010
- [AD 2007-02-17](https://openairdocs.org/ad/2007-02-17): Fuel leak at the level of start electro valve · Turbomeca Arriel 1A, Arriel 1A1, Arriel 1A2 and 12 more. Effective Mar 2, 2007
- [AD 2006-06-17](https://openairdocs.org/ad/2006-06-17): 2nd stage nozzle guide vanes (NGV2) · Turbomeca Arriel 1B, Arriel 1D and Arriel 1D1. Effective Apr 27, 2006
- [AD 2003-16-03](https://openairdocs.org/ad/2003-16-03): Second Stage Turbine Disk · Turbomeca Arriel 1A, Arriel 1A1, Arriel 1A2 and 10 more. Effective Sep 12, 2003
- [AD 2003-11-08](https://openairdocs.org/ad/2003-11-08): 2nd stage gas generator · Turbomeca Arriel 1B, Arriel 1D and Arriel 1D1. Effective Jul 3, 2003
- [AD 2003-03-12](https://openairdocs.org/ad/2003-03-12): Bleed Valve · Turbomeca Arriel 1A2, Arriel 1C, Arriel 1C1 and 12 more. Effective Mar 7, 2003
- [AD 2002-14-26](https://openairdocs.org/ad/2002-14-26): Containment Shield Rings · Turbomeca Arriel 1A, Arriel 1A1, Arriel 1B and 2 more. Effective Aug 6, 2002
- [AD 2000-20-01](https://openairdocs.org/ad/2000-20-01): Rear Bearing Oil Return System · Turbomeca Arriel 1A, Arriel 1A1, Arriel 1A2 and 9 more. Effective Oct 17, 2000
- [AD 94-25-08](https://openairdocs.org/ad/94-25-08): Gearboxes · Turbomeca Arriel 1A, Arriel 1A1, Arriel 1B and 2 more. Effective Jan 17, 1995
- [AD 91-24-02](https://openairdocs.org/ad/91-24-02): Main Rotor Drive Shaft · Turbomeca Arriel 1B, Arriel 1D and Arriel 1D1. Effective Feb 21, 1992

Historical (superseded or no longer in force):

- [AD 2017-04-51](https://openairdocs.org/ad/2017-04-51) (historical): Fuel Control/ Turbine Engines · Safran Helicopter Engines Arriel 1A1, Arriel 1A2, Arriel 1B and 9 more. Effective Mar 30, 2017
- [AD 2014-19-05](https://openairdocs.org/ad/2014-19-05) (historical): Engine accessory gearbox (AGB) · Turbomeca Arriel 1A1, Arriel 1A2, Arriel 1B and 16 more. Effective Nov 5, 2014
- [AD 2010-19-06](https://openairdocs.org/ad/2010-19-06) (historical): Gas generator · Turbomeca Arriel 1A, Arriel 1A1, Arriel 1B and 6 more. Effective Oct 6, 2010
- [AD 2009-12-51](https://openairdocs.org/ad/2009-12-51) (historical): Gearboxes (module M05) · Turbomeca Arriel 1A1, Arriel 1A2, Arriel 1B and 9 more. Effective Jul 15, 2009
- [AD 2009-08-08](https://openairdocs.org/ad/2009-08-08) (historical): Power turbine blades · Turbomeca Arriel 1B, Arriel 1D and Arriel 1D1. Effective Apr 29, 2009
- [AD 2008-07-01](https://openairdocs.org/ad/2008-07-01) (historical): Gas generator 2nd stage turbine blades · Turbomeca Arriel 1B, Arriel 1D, Arriel 1D1 and 1 more. Effective Apr 30, 2008
- [AD 2006-02-08 R1](https://openairdocs.org/ad/2006-02-08-R1) (historical): Gas generator 2nd stage turbine blades. · Turbomeca Arriel 1B, Arriel 1D, Arriel 1D1 and 17 more. Effective Sep 13, 2006
- [AD 2006-02-08](https://openairdocs.org/ad/2006-02-08) (historical): 2nd stage turbine blades · Turbomeca Arriel 1B, Arriel 1D, Arriel 1D1 and 1 more. Effective Feb 28, 2006
- [AD 2003-12-14](https://openairdocs.org/ad/2003-12-14) (historical): Axial Compressor · Turbomeca Arriel 1A, Arriel 1A1, Arriel 1A2 and 11 more. Effective Jul 25, 2003
- [AD 95-11-01](https://openairdocs.org/ad/95-11-01) (historical): Generator · Turbomeca Arriel 1A, Arriel 1A1, Arriel 1A2 and 6 more. Effective Jun 21, 1995

## Registered aircraft

None registered with this engine model now.

## NTSB investigations

None matched to aircraft with this engine model.

## FAA accident and incident reports

None matched to aircraft with this engine model.

## Service difficulty reports (252, newest 50)

As reported by operators and repair stations, by the model named in the report.

- [SDR CA190730021](https://openairdocs.org/sdr/CA190730021), Jul 29, 2019: SHOCK ABSORBER. FAILED. (CAN) PAINT WAS FOUND MISSING ON PART OF THE SHORT SHAFT ATTACHED TO THE ENGINE, SUSPECTED CONTACT WITH FIREWALL. SHAFT INSPECTED AND FOUND SERVICEABLE, PAINT T
- [SDR DCGA201708070362](https://openairdocs.org/sdr/DCGA201708070362), Aug 6, 2017: GEARBOX. FALSE INDICATION. PILOT EXPERIENCED A MAIN ROTOR GEARBOX CHIP LIGHT ENROUTE TO THE AIRPORT. MAINTENANCE EXAMINED THE SYSTEM CHIP DETECTORS AND ELECTRICAL SYSTEM AND FOUND NO CHIP
- [SDR CA130430022](https://openairdocs.org/sdr/CA130430022), Apr 25, 2013: BYPASS VALVE. FAILED. (CAN) WOULDN`T PRODUCE BYPASS INDICATION AT FUNCTION CHECK DURING A/C INSPECTION. LESS THAN 200 HRS. IN SERVICE FROM NEW. NOT AN AS355 BUT HAD NO CHOICE IN THE 
- [SDR ULXR201302060001](https://openairdocs.org/sdr/ULXR201302060001), Feb 5, 2013: LINE. LEAKING. HYDRAULIC LINE LEAKING AT SWAGGED FITTING.
- [SDR 2012FA0000520](https://openairdocs.org/sdr/2012FA0000520), Jul 10, 2012: COMPRESSOR. NOISY. INSTALLED MODULE 3, FRESH OUT OF OVERHAUL. DURING OPS CHECKS A LOUD "HOWLING" WAS OBSERVED. ENGINE WAS SHUTDOWN, REMOVED AND SENT TO MFG FOR FURTHER INVESTIGATI
- [SDR 2012FA0000354](https://openairdocs.org/sdr/2012FA0000354), Apr 13, 2012: STARFLEX. CRACKED. UPON PERFORMING (ALF) AFTER LAST FLIGHT INSPECTION, IAW MM 05-21-00-603. VISUAL INSPECTION OF THE MAIN ROTOR HEAD STARFLEX IT WAS DETERMINED THERE WAS A CRACK T
- [SDR MHI2011F00001](https://openairdocs.org/sdr/MHI2011F00001), Aug 18, 2010: COMPRESSOR BLADE. CRACKED. DURING FLIGHT ON 8/18/2010, THE PILOT NOTICED AN UNUSUAL NOISE IN HIS HEADSET. UPON LANDING AND SHUTDOWN OF THE ACFT IT WAS DISCOVERED THAT THERE WAS SIGNIGICAN
- [SDR CA091215002](https://openairdocs.org/sdr/CA091215002), Dec 8, 2009: WINDOW. DEPARTED. (CAN) AIRCRAFT ON DESCENT FROM 9000 FT ASL A VIBRATION ON THE LT FWD DOOR WINDOW SLIDER WAS NOTED BY THE PASSENGER WHO TRIED TO HOLD THE SLIDER FROM VIBERATING.
- [SDR CA090825004](https://openairdocs.org/sdr/CA090825004), Aug 21, 2009: BRACKET. CRACKED. THE RT UPPER REAR CORNER BRACKET UNDER THE ENG DECK FOUND CRACKED.
- [SDR CA090813010](https://openairdocs.org/sdr/CA090813010), Aug 4, 2009: PRESSURE SWITCH. FAILED. HYD PRESSURE CAUTION LIGHT STAYS ILLUMINATED AND WARNING HORN IS ON WHEN THERE IS NO HYD FAILURE. NEW PRESSURE SWITCH PN MA124-01, SN 4021 INSTALLED. 185.4 HOUR
- [SDR CA070831001](https://openairdocs.org/sdr/CA070831001), Jul 26, 2007: RING. LOOSE. (CAN) DURING ENGINE SHUTDOWN THE MAIN ROTOR BLADE DROOP STOP RING FELL DOWN THE MAST ASSY. THE HARDWARE HOLDING THE RING BRACKET ALL CAME OFF ALLOWING THE RING 
- [SDR CA070531007](https://openairdocs.org/sdr/CA070531007), Apr 25, 2007: VALVE. MALFUNCTIONED. (CAN) ASSEMBLY ON CONDITION. THIS UNIT WAS REMOVED SERVICEABLE FOR ANOTHER AIRCRAFT. A FUNCTIONAL CHECK WAS CARRIED OUT. FOLLOWING A RUN UP TO 100 PERCENT THE E
- [SDR CA070118010](https://openairdocs.org/sdr/CA070118010), Jan 18, 2007: BOLT. DAMAGED. (CAN) THIS IS (1) OF (2) BOLTS USED TO RETAIN THE HORIZONTAL STAB. TO THE TAIL BOOM OF THE HELICOPTER. THE THREADED SECTION OF THE BOLT AND THE NUT WERE FOUND M
- [SDR CA060710005](https://openairdocs.org/sdr/CA060710005), Jun 22, 2006: SHIM. MISINSTALLED. (CAN) DURING A 100 HR INSPECTION OF AN A-STAR IN THE FIELD, THE ENGINEER PERFORMING THE INSPECTION FOUND THAT THE T/R SERVO FRICTION/GUIDE SHIM (PAD) WAS INSTAL
- [SDR KBM2006F00171](https://openairdocs.org/sdr/KBM2006F00171), May 2, 2006: TRANSMITTER. READS LOW. OIL TRANSMITTER, OIL PRESSURE GAUGE READS ZERO, REMOVED AND REPLACED. (K)
- [SDR KBM2006F00174](https://openairdocs.org/sdr/KBM2006F00174), Apr 27, 2006: RADIO. INOPERATIVE. VHT SIDE TONE EXCESSIVELY LOUD, REMOVED AND REPLACED. (K)
- [SDR KBM2006F00177](https://openairdocs.org/sdr/KBM2006F00177), Apr 27, 2006: TRANSMITTER. MALFUNCTIONED. ENGINE TRANSMITTER, DROP TO ZERO, OTHER GAUGES ARE NORMAL. REMOVED AND REPLACED WITH NEW. (K)
- [SDR KBM2006F00193](https://openairdocs.org/sdr/KBM2006F00193), Apr 26, 2006: TRANSMITTER. READS LOW. ENGINE OIL TRANSMITTER, ENGINE OIL PRESSURE READS LOW, REMOVED AND REPLACED. (K)
- [SDR KBM2006F00158](https://openairdocs.org/sdr/KBM2006F00158), Apr 18, 2006: ENTERTAIN SYS. DISTORTED. DMP PLAYER, UNIT SOUNDS DISTORTED, REMOVED AND REPLACED. (K)
- [SDR KBM2006F00118](https://openairdocs.org/sdr/KBM2006F00118), Mar 13, 2006: PRESSURE SWITCH. INOPERATIVE. DIFF PRESSURE SWITCH, LOW AIR PRESSURE LIGHT FOR FDC FILTER CAME ON DURING HOVER, REMOVED AND REPLACED. (K)
- [SDR KBM2006F00119](https://openairdocs.org/sdr/KBM2006F00119), Mar 13, 2006: METER. INOPERATIVE. HOBBS METER, INOPERATIVE, REMOVED AND REPLACED. (K)
- [SDR KBM2006F00078](https://openairdocs.org/sdr/KBM2006F00078), Feb 17, 2006: BRUSHES. DEFECTIVE. DURING START FOUND SPARKS AT STARTER GEN. REMOVED AND REPLACED BRUSHES. (K)
- [SDR KBM2006F00079](https://openairdocs.org/sdr/KBM2006F00079), Feb 17, 2006: IGNITER. INOPERATIVE. AC HAS SLOW START. REMOVED AND REPLACED. (K)
- [SDR KBM2006F00080](https://openairdocs.org/sdr/KBM2006F00080), Feb 17, 2006: IGNITER. INOPERATIVE. AC HAS SLOW START, IGNITER, REMOVED AND REPLACED. (K)
- [SDR KBM2006F00084](https://openairdocs.org/sdr/KBM2006F00084), Feb 4, 2006: TRANSMITTER. READS LOW. SUSPECTED TORQUE TRANSMITTER READS LOW, REMOVED AND REPLACED. (K)
- [SDR KBM2006F00034](https://openairdocs.org/sdr/KBM2006F00034), Jan 3, 2006: BEARING. WORN. LAMINATED BEARINGS, BEARINGS ARE WORN. REMOVED AND REPLACED. (K)
- [SDR KBM2006F00031](https://openairdocs.org/sdr/KBM2006F00031), Dec 4, 2005: BUSHING SLEEVE. WORN. UNIT HAS WORN BUSHING SLEEVE, REMOVED AND REPLACED. (K)
- [SDR KBM2006F00032](https://openairdocs.org/sdr/KBM2006F00032), Dec 4, 2005: SHUTOFF VALVE. INOPERATIVE. FUEL SHUTOFF VALVE INOPERATIVE, REMOVED AND REPLACED. (K)
- [SDR KBM2006F00033](https://openairdocs.org/sdr/KBM2006F00033), Dec 4, 2005: SLEEVE. WORN. UNIT HAS WORN HOUSING SLEEVE. REMOVED AND REPLACED. (K)
- [SDR KBM2005F00356](https://openairdocs.org/sdr/KBM2005F00356), Nov 27, 2005: TRANSMITTER. FAILED. ENGINE OIL GAUGE DROPS TO ZERO. REMOVED AND REPLACED OIL PRESSURE TRANSMITTER. (K)
- [SDR KBM2005F00354](https://openairdocs.org/sdr/KBM2005F00354), Nov 25, 2005: BATTERY. WEAK. BATTERY WEAK, REMOVED AND REPLACED. (K)
- [SDR KBM2005F00355](https://openairdocs.org/sdr/KBM2005F00355), Nov 25, 2005: BATTERY. FAILED. SLOW START, REMOVED AND REPLACED BATTERY. (K)
- [SDR KBM2005F00353](https://openairdocs.org/sdr/KBM2005F00353), Nov 24, 2005: FCU. FAILED. SUSPECT HIGH SIDE FAILURE NTL GOVERNOR FUEL CONTROL UNIT. REMOVED AND REPLACED. (K)
- [SDR KBM2005F00342](https://openairdocs.org/sdr/KBM2005F00342), Nov 12, 2005: GYRO. SPINNING. DIRECTIONAL GYRO, UNIT SPINS IN FLIGHT, REMOVED AND REPLACED. (K)
- [SDR KBM2005F00333](https://openairdocs.org/sdr/KBM2005F00333), Nov 2, 2005: BATTERY. DISCHARGED. BATTERY, REMOVED DUE TO SLOW START. REMOVED AND REPLACED. (K)
- [SDR KBM2005F00318](https://openairdocs.org/sdr/KBM2005F00318), Oct 23, 2005: ICS BOX. INOPERATIVE. ICS BOX, UNIT INOPERATIVE. REMOVED AND REPLACED. (K)
- [SDR KBM2005F00317](https://openairdocs.org/sdr/KBM2005F00317), Oct 21, 2005: GYRO. INOPERATIVE. AG, UNIT INOPERATIVE. REMOVED AND REPLACED. (K)
- [SDR KBM2005F00315](https://openairdocs.org/sdr/KBM2005F00315), Oct 16, 2005: BEARING. FAILED. T/R HINGE LAMINATED BEARING HAD MULTIPLE CUTS IN RUBBER. REPLACED WITH NEW. (K)
- [SDR KBM2005F00314](https://openairdocs.org/sdr/KBM2005F00314), Oct 15, 2005: BOOT. WORN. MAIN ROTOR SWASHPLATE RUBBER BOOT WAS WORN. REPLACED WITH NEW UNIT. (K)
- [SDR KBM2005F00313](https://openairdocs.org/sdr/KBM2005F00313), Oct 13, 2005: CHIP DETECTOR. INOPERATIVE. CHIP DETECTOR, UNIT INOPERATIVE. REMOVED AND REPLACED. (K)
- [SDR KBM2005F00305](https://openairdocs.org/sdr/KBM2005F00305), Oct 6, 2005: STARTER GEN. FAILED. INTERNAL FAILURE- ARMATURE, REPLACED STARTER GEN WITH OFF UNIT. (K)
- [SDR KBM2005F00311](https://openairdocs.org/sdr/KBM2005F00311), Sep 30, 2005: RADIO. FAILED. VHF RADIO, UNIT DISPLAY BLANKS OFF AND UNREADABLE. REMOVED AND REPLACED. (K)
- [SDR KBM2005F00312](https://openairdocs.org/sdr/KBM2005F00312), Sep 30, 2005: GYRO. SPINNING. DIRECTIONAL GYRO, UNIT SPINS IN FLIGHT, REMOVED AND REPLACED. (K)
- [SDR KBM2005F00304](https://openairdocs.org/sdr/KBM2005F00304), Sep 28, 2005: RADIO. FAILED. VHF RADIO, UNIT FREQ IS TOO DIM TO READ, REMOVED AND REPLACED. (K)
- [SDR KBM2005F00303](https://openairdocs.org/sdr/KBM2005F00303), Sep 20, 2005: BEARING. SPINNING. CROSSBEAM, LAMINATED BEARING, SPINNING, REMOVED AND REPLACED. (K)
- [SDR KBM2005F00287](https://openairdocs.org/sdr/KBM2005F00287), Sep 19, 2005: BEARING. TORN. LAMINATED BEARING, UNIT RUBBER TORN, REMOVED AND REPLACED. (K)
- [SDR KBM2005F00288](https://openairdocs.org/sdr/KBM2005F00288), Sep 19, 2005: BRUSHES. INOPERATIVE. LT CONDENSER BLOWER INOPERATIVE, REMOVED AND REPLACED. (K)
- [SDR KBM2005F00289](https://openairdocs.org/sdr/KBM2005F00289), Sep 19, 2005: DRAIN VALVE. LEAKING. ENGINE FUEL START DRAIN VALVE LEAKING IN THE WEEPING HOLE, REMOVED AND REPLACED. (K)
- [SDR KBM2005F00269](https://openairdocs.org/sdr/KBM2005F00269), Sep 17, 2005: BLOWER MOTOR. READS HIGH. OIL TEMP RUNNING EXTREMELY HIGH. TROUBLESHOT REPLACED OIL COOLER BLOWER MOTOR WITH O/H UNIT. (K)
- [SDR KBM2005F00270](https://openairdocs.org/sdr/KBM2005F00270), Sep 16, 2005: RADIO. FAILED. VHF RADIO, DISPLAY BLANK OFF AND CAN`T TRANSMITT OR RECEIVE. REMOVED AND REPLACED VHF RADIO. (K)

All 252: https://openairdocs.org/engine/turbomeca-arriel-1d/reports.md

## STCs that may be installed (OpenAirDocs) (3)

Approved for this engine model: the STC's model list names it on its data sheet, or a series that includes it. In force first, then newest. The registry doesn't record which STCs an aircraft has.

- [STC SE00328AT](https://openairdocs.org/stc/SE00328AT): Installation of a P2 fuel control isolation valve kit. Bell Helicopter Textron Inc
- [STC SE00567AT](https://openairdocs.org/stc/SE00567AT): Install Aeronautical Accessories Torque Monitoring System. Bell Helicopter Textron Inc
- [STC SE1029GL](https://openairdocs.org/stc/SE1029GL): Installation of a fuel flow transducer. Shadin Company, Inc

## PMA parts (OpenAirDocs) (4)

Current parts manufacturer approvals (PMA): parts the FAA has approved companies to make as replacements or modifications. Each record lists its models as free text; OpenAirDocs matched them to this engine model on its data sheet, so check the FAA record before relying on it. Newest first.

- [1764469](https://drs.faa.gov/browse/excelExternalWindow/FCCF03532F2E39528625787000554BFA.0001): Filter Element Assembly. Purolator Facet Inc (formerly Facet Filter Products) · PMA PQ1207CE · Replaces Eurocopter (Turbomeca) PIN 9560166860… · Dec 9, 2009
- [CH34745](https://drs.faa.gov/browse/excelExternalWindow/77C23E3208488F308525703E006CB628.0001): Igniter Assembly. Champion Aerospace LLC · Replaces Turbomeca 9550175400 · Apr 20, 2003
- [Report No. AA-94025](https://drs.faa.gov/browse/excelExternalWindow/EA6EFCD6C4949E338525703B005844E7.0001): Torque Monitoring System. Bell Helicopter Textron Inc (formerly Aeronautical Accessories Inc) · Modification part · Oct 13, 1994
- [Report No. AA-93057](https://drs.faa.gov/browse/excelExternalWindow/0AD5DADF3AEB81F18525703B00584B70.0001): P2 Fuel Control Isolation Valve Kit. Bell Helicopter Textron Inc (formerly Aeronautical Accessories Inc) · Modification part · Sep 12, 1993

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