# Safran ARRIEL-1E - Type: Engine model (FAA registry) - Registry code: 59996 - Manufacturer (registry): SAFRAN - Model: ARRIEL 1E - Engine type: Turbo-shaft - Power: 626 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/safran-arriel-1e 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 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 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 Effective Mar 2, 2007 Historical (superseded or no longer in force): - [AD 2003-12-14](https://openairdocs.org/ad/2003-12-14) (historical): Axial Compressor · Turbomeca Arriel 1A, Arriel 1A1, Arriel 1A2 and 11 more.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 ## 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 (24) As reported by operators and repair stations, by the model named in the report. - [SDR HDNA20110718](https://openairdocs.org/sdr/HDNA20110718), Jul 18, 2011: MOTOR. BURNED. AT CRUISE FLIGHT, THE CREW SENSED A BURNING ODOR THAT WAS DETECTED IN THE AFT CABIN. AT THAT TIME THE AIRCRAFT WAS DIVERTING TO AIRPORT. THE PILOT TURNED OFF TH - [SDR LEU2008F00000](https://openairdocs.org/sdr/LEU2008F00000), Jul 15, 2008: CHIP DETECTOR. SHORTED. ON 7/15/2008 AIRCRAFT MADE A PRECAUTIONARY LANDING DUE TO ILLUMINATION OF A TAIL ROTOR CHIP CAUTION LIGHT. INSPECTION REVEALED A DEFECTIVE CHIP DETECTOR WHICH G - [SDR GVNA119695](https://openairdocs.org/sdr/GVNA119695), May 8, 2008: ACTUATOR. JAMMED. IN FLIGHT NR 2 ENGINE TRIM ACTUATOR FULLY RETRACTED, JAMMED, POPPED TRIM CIRCUIT BREAKER. AIRCRAFT LANDED USING MANUAL TRIM. REPLACED ACTUATOR. - [SDR N984ME9080](https://openairdocs.org/sdr/N984ME9080), Apr 23, 2008: PULLEY. CHAFED. AIR CONDITIONING DRIVE PULLEY BOLTS SHEARED AND THE PULLEY DETACHED FROM THE DRIVE. IT LOOKS LIKE THE BOLTS LOST TORQUE SLIGHTLY, BOLT HEADS WERE SAFETIED, THE - [SDR 907204142008](https://openairdocs.org/sdr/907204142008), Apr 14, 2008: WIRE. DAMAGED. THIS REPORT IS THE 3RD OCCURRENCE OF SMOKE/ODOR CAUSED BY AN ELECTRICAL DISCHARGE FAULT IN THE OVERHEAD CIRCUIT BREAKER PANEL. MECHANICS REPLACED THE APPROPRIAT - [SDR 907204092008](https://openairdocs.org/sdr/907204092008), Apr 9, 2008: WIRE. SHORTED. UPON LANDING, STRONG ACRID ODOR IN CABIN AND COCKPIT AREAS. MECHANIC CALLED IN AND UPON INSPECTION OF OVERHEAD CIRCUIT BREAKER PANEL, IT WAS DISCOVERED THAT THE - [SDR GVNA119127](https://openairdocs.org/sdr/GVNA119127), Mar 1, 2008: LATCH. LOOSE. DURING CRUISE FLIGHT AT 120 KTS, THE LT SLIDING CABIN DOOR CAME OPEN, SLID ALL THE WAY TO THE STOP AT A HIGH RATE OF SPEED AND POPPED OUT OF THE CENTER GUIDE RA - [SDR BAQA200700032](https://openairdocs.org/sdr/BAQA200700032), Sep 24, 2007: FITTING. CRACKED. TAILROTOR GEAR BOX MOUNT FITTING AT TOP OF VERTICAL FIN CRACKED AND TAIL ROTOR GEAR BOX MOUNTING STUD ROSSET FITTING LOOSE. - [SDR RMXA2007](https://openairdocs.org/sdr/RMXA2007), Sep 20, 2007: SKIN PANEL. CRACKED. DURING A SCHEDULED INSPECTION, SEVERAL CRACKS WERE FOUND ON THE TAILBOOM TOP SKIN PT NR1120-32052.11 AROUND THE ATTACHING RIVET HOLES ON THE AFT LT EDGE. - [SDR 984ME](https://openairdocs.org/sdr/984ME), Aug 27, 2007: COMPRESSOR. SEIZED. THE AIR-CONDITIONING COMPRESSOR SEIZED, THE DRIVE BELT CONTINUED TURNING, SMOKING UNTIL IT BROKE. - [SDR 304ME](https://openairdocs.org/sdr/304ME), Aug 2, 2007: DRIVE BELT. DETERIORATED. THE AIR CONDITIONING DRIVE BELT HAD CRACKS IN IT AT A BELT TOTAL TIME OF 359.3. THE LIFE LIMIT OF THIS BELT IS 1000 HOURS. - [SDR 910207192007](https://openairdocs.org/sdr/910207192007), Jul 19, 2007: FUEL TANK. LEAKING. HAD 3 OCCURRENCES OF FUEL ODOR IN CABIN. 5 MIN AFTER DEPARTURE, THERE WAS A STRONG FUEL ODOR IN CABIN. ODOR WOULD DISSIPATE AND THEN RETURN. UPON THE THIRD RECU - [SDR 061907](https://openairdocs.org/sdr/061907), Jun 14, 2007: CONTROL ARM. CRACKED. TAIL ROTOR CONTROL LEVER FOUND CRACKED - [SDR 07N101VU01](https://openairdocs.org/sdr/07N101VU01), May 23, 2007: TRANSMISSION. WARNING LIGHT. DURING CRUISE FLIGHT ENROUTE TO A LOCAL HOSPITAL FOR A PATIENT PICK UP, THE MAIN TRANSMISSION CHIP LIGHT ILLUMINATED. PERFORMED THE EMERGENCY PROCEDURE IAW THE - [SDR 0508079100](https://openairdocs.org/sdr/0508079100), May 8, 2007: TANK. CONTAMINATED. FOUND A -PIG MAT- IN THE MAIN FUEL TANK. - [SDR BAQA2007005](https://openairdocs.org/sdr/BAQA2007005), Jan 30, 2007: SKIN. CRACKED. A CRACK WAS FOUND AT THE TOP OF THE TAILBOOM VERTICAL FIN WHILE TROUBLESHOOTING A TAIL ROTOR VIBRATION ISSUE. THE CRACK WAS FOUND ON THE LT SIDE OF THE ACCESS S - [SDR EHA2004F00002](https://openairdocs.org/sdr/EHA2004F00002), Jul 3, 2004: WARNING LIGHT. ILLUMINATED. NR 1 AND NR 2 FUEL FILTER LIGHT ILLUMINATED DURING FLIGHT. THE NR 1 CAME ON FIRST, THEN THE NR 2 CAME ON A MINUTE LATER. PILOT LANDED AIRCRAFT, CALLED FOR MECHA - [SDR EHA2004F00001](https://openairdocs.org/sdr/EHA2004F00001), Mar 14, 2004: DRAIN VALVE. LEAKING. PILOT REPORTED EXCESSIVE FUEL SMELL AFTER STARTING NR 1 ENGINE PILOT SHUT DOWN ENGINE DURING RESTART OBSERVED LARGE AMOUNT OF FUEL POURING OVER ENGINE FROM THE - [SDR R7MR35484](https://openairdocs.org/sdr/R7MR35484), May 4, 2002: PRESSURE SWITCH. INOPERATIVE. PRESSURE SWITCH INOPERATIVE. FUEL PRESSURE LIGHT CAME ON. FOUND SWITCH TO BE PROBLEM. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. - [SDR R7MR35483](https://openairdocs.org/sdr/R7MR35483), Jan 7, 2002: PRESSURE SWITCH. INOPERATIVE. PRESSURE SWITCH, UNIT INOPERATIVE UPON INSTALLATION. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. - [SDR R7MR35482](https://openairdocs.org/sdr/R7MR35482), Jan 7, 2002: PRESSURE SWITCH. INOPERATIVE. PRESSURE SWITCH INOPERATIVE. FUEL PRESSURE WARNING LIGHT WILL NOT GO OUT. REPLACED WITH NEW, CORRECTED PROBLEM. - [SDR 20000413SH006](https://openairdocs.org/sdr/20000413SH006), Feb 24, 2000: IGNITOR. WORN. IGNITER PLUG WORN AT TIP. REMOVED AND REPLACED. (X) - [SDR 99ZZZX1385](https://openairdocs.org/sdr/99ZZZX1385), Sep 11, 1998: VALVE. MALFUNCTIONED. NR 2 ENGINE OIL PRESSURE LOW. REMOVED AND REPLACED. - [SDR 99ZZZX1386](https://openairdocs.org/sdr/99ZZZX1386), Sep 10, 1998: PUMP. FAILED. NR 2 ENGINE OIL PRESSURE LOW. REMOVED AND REPLACED. ## STCs that may be installed (OpenAirDocs) (2) 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 ## PMA parts (OpenAirDocs) (3) 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 - [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 --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.