# N325UE: Jetstream JETSTREAM 4101

- Status: Valid registration
- Airframe: [Jetstream JETSTREAM 4101](https://openairdocs.org/model/jetstream-jetstream-4101) (registry code 1500501, 29 seats)
- Engine: [AiResearch TPE331 series](https://openairdocs.org/engine/airesearch-tpe331-series) (registry code 01514)
- Serial number: 41063
- Type: Fixed wing multi engine
- Engine type: Turbo-prop
- Airworthiness: Special flight permit
- Airworthiness date: July 24, 1995
- Mode S code: A382AA
- Registered owner: [Aircraft Propulsion Leasing LLC](https://openairdocs.org/faa-owner/AIRCRAFT%20PROPULSION%20LEASING%20LLC)
- Location: [Holland, OH](https://openairdocs.org/faa-place/OH/Holland)
- Owner type: LLC
- Owner's area on the map: 41.6289° N, 83.7496° W: Placed by OpenAirDocs at the center of ZIP code 43528, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=325UE
- Page: https://openairdocs.org/aircraft/N325UE

From the FAA registry file of October 24, 2026. ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination. The registry lists only the engine series, so ADs for every AiResearch TPE331 model are included.

## ADs that may apply (OpenAirDocs): 41 in force

### Matched by airframe (Jetstream JETSTREAM 4101)

None in force.

### Matched by engine (AiResearch TPE331 series)

- [AD 2018-22-01](https://openairdocs.org/ad/2018-22-01): Turbine Section · Honeywell International TPE331-10, TPE331-10N, TPE331-10R and 8 more. Effective Dec 10, 2018
- [AD 2018-17-15](https://openairdocs.org/ad/2018-17-15): Turbine Engine Combustion Section · Honeywell International TPE331-1, TPE331-10, TPE331-10AV and 39 more. Effective Oct 22, 2018
- [AD 2018-13-05](https://openairdocs.org/ad/2018-13-05): Turbine Engine Reduction Gear · Honeywell International TPE331-1, TPE331-10, TPE331-10AV and 18 more. Effective Jul 26, 2018
- [AD 2016-21-07](https://openairdocs.org/ad/2016-21-07): Fuel control drive · Honeywell International TPE331-1, TPE331-10, TPE331-10AV and 26 more. Effective Nov 28, 2016
- [AD 2016-18-17](https://openairdocs.org/ad/2016-18-17): Compressor impeller · Honeywell International TPE331-10, TPE331-10AV, TPE331-10GP and 22 more. Effective Nov 4, 2016
- [AD 2015-18-03](https://openairdocs.org/ad/2015-18-03): Engine propeller shaft coupling failures · Honeywell International TPE331-10, TPE331-10R, TPE331-10U and 8 more. Effective Nov 13, 2015
- [AD 2012-02-06](https://openairdocs.org/ad/2012-02-06): First stage turbine disks · Honeywell International TPE331-10, TPE331-10AV, TPE331-10GP and 12 more. Effective Mar 15, 2012
- [AD 2011-18-51 R1](https://openairdocs.org/ad/2011-18-51-R1): Main shaft bearing · Honeywell International TPE331-1, TPE331-10, TPE331-10A and 82 more. Effective Oct 19, 2011
- [AD 2009-17-05](https://openairdocs.org/ad/2009-17-05): First stage turbine disks · Honeywell International TPE331-10, TPE331-10A, TPE331-10AV and 20 more. Effective Sep 1, 2009
- [AD 2006-14-03](https://openairdocs.org/ad/2006-14-03): New flight cycle counting method for first, second, and third-stage turbine rotors · Honeywell International TPE331-1, TPE331-10, TPE331-10A and 48 more. Effective Aug 9, 2006
- [AD 2004-09-29](https://openairdocs.org/ad/2004-09-29): First Stage Turbine Disks · Honeywell International TPE331-10, TPE331-10A, TPE331-10AV and 20 more. Effective Jun 15, 2004
- [AD 2002-25-02](https://openairdocs.org/ad/2002-25-02): First stage compressors implellers · Honeywell International TPE331-10, TPE331-10A, TPE331-10AV and 35 more. Effective Jan 21, 2003
- [AD 2002-21-15](https://openairdocs.org/ad/2002-21-15): Second stage turbine stator inner seal support · Honeywell International TPE331-1, TPE331-2, TPE331-2UA and 9 more. Effective Nov 26, 2002
- [AD 2002-12-09](https://openairdocs.org/ad/2002-12-09): Spectrometric Oil Analysis Program (SOAP) Sampling of Oil and Filter, Gearbox Components · Honeywell International TPE331-11U, TPE331-12B, TPE331-12JR and 3 more. Effective Jul 3, 2002
- [AD 2001-21-02](https://openairdocs.org/ad/2001-21-02): Airplane Flight Manual--Electronic Engine Controls · Honeywell International TPE331-10N, TPE331-12B and TPE331-8. Effective Nov 19, 2001
- [AD 98-12-09](https://openairdocs.org/ad/98-12-09): Fuel Manifold · Honeywell International TPE331-10, TPE331-10A, TPE331-10AV and 29 more. Effective Aug 7, 1998
- [AD 98-04-15](https://openairdocs.org/ad/98-04-15): Turbine Stators · Honeywell International TPE331-1, TPE331-2, TPE331-2UA and 9 more. Effective Apr 27, 1998
- [AD 97-15-10](https://openairdocs.org/ad/97-15-10): Engine Inlet Ice Protection · Honeywell International TPE331-10, TPE331-10A, TPE331-10AV and 39 more. Effective Sep 22, 1997
- [AD 95-16-08](https://openairdocs.org/ad/95-16-08): Life Limited Turbine Components · Honeywell International TPE331-1, TPE331-10, TPE331-10A and 62 more. Effective Sep 5, 1995
- [AD 94-26-07](https://openairdocs.org/ad/94-26-07): Fuel Control Governor Drive · Honeywell International TPE331-10, TPE331-10A, TPE331-10B and 32 more. Effective Apr 18, 1995
- [AD 94-09-08](https://openairdocs.org/ad/94-09-08): Third Stage Stator Turbine Assemblies · Honeywell International TPE331-1, TPE331-2, TPE331-2UA and 7 more. Effective May 20, 1994
- [AD 93-15-11](https://openairdocs.org/ad/93-15-11): Propeller Pitch Control (PPC) Gasket · Honeywell International TPE331-1, TPE331-10, TPE331-10A and 58 more. Effective Sep 7, 1993
- [AD 92-26-08](https://openairdocs.org/ad/92-26-08): Third Stage Stator Assemblies · Honeywell International TPE331-1, TPE331-2, TPE331-2UA and 7 more. Effective Jul 15, 1993
- [AD 93-05-09](https://openairdocs.org/ad/93-05-09): Third Stage Turbine Stator Assemblies · Honeywell International TPE331-1, TPE331-2, TPE331-2UA and 9 more. Effective Jun 28, 1993
- [AD 93-02-01](https://openairdocs.org/ad/93-02-01): Stratoflex Fuel Manifold Assemblies · Honeywell International TPE331-10, TPE331-10A, TPE331-10B and 21 more. Effective Mar 18, 1993
- [AD 89-07-07 R1](https://openairdocs.org/ad/89-07-07-R1): Oil Scavenge Pump Assembly · Honeywell International TPE331-1, TPE331-10, TPE331-10R and 26 more. Effective Oct 30, 1989
- [AD 86-08-06 R1](https://openairdocs.org/ad/86-08-06-R1): Second Stage Turbine Rotor Assembly · Honeywell International TPE331-25AA, TPE331-25AB, TPE331-25DA and 7 more. Effective Dec 21, 1987
- [AD 84-10-06 R1](https://openairdocs.org/ad/84-10-06-R1): Fuel Pump Assemblies · Honeywell International TPE331-1, TPE331-10, TPE331-10B and 45 more. Effective Dec 26, 1984
- [AD 84-01-04](https://openairdocs.org/ad/84-01-04): Third Stage Turbine Wheels · Honeywell International TPE331-1, TPE331-1U, TPE331-1UA and 11 more. Effective Jan 25, 1984
- [AD 73-26-07 R3](https://openairdocs.org/ad/73-26-07-R3): Fuel Pump Shaft Internal Drive Splines · Honeywell International TPE331-1, TPE331-1U, TPE331-1UA and 39 more. Effective Jul 31, 1980
- [AD 78-25-08 R3](https://openairdocs.org/ad/78-25-08-R3): Turbine Rotor · Honeywell International TPE331-1, TPE331-1U, TPE331-1UA and 11 more. Effective Jun 12, 1980
- [AD 79-12-04](https://openairdocs.org/ad/79-12-04): Forged Third Stage Turbine Wheel Blade · Honeywell International TPE331-10. Effective May 10, 1979
- [AD 78-05-02](https://openairdocs.org/ad/78-05-02): Propeller Pitch Control Cam Follower Pin · Honeywell International TPE331-1, TPE331-1U, TPE331-1UA and 11 more. Effective Apr 5, 1979
- [AD 76-16-01](https://openairdocs.org/ad/76-16-01): Bearing Oil Transfer Tube · Honeywell International TPE331-1, TPE331-1U, TPE331-1UA and 11 more. Effective Aug 6, 1976
- [AD 75-10-05](https://openairdocs.org/ad/75-10-05): Torque Sensor Assembly Mounting Arm · Honeywell International TPE331-1, TPE331-2, TPE331-3U and 3 more. Effective Jul 11, 1975
- [AD 74-10-10](https://openairdocs.org/ad/74-10-10): Fuel Control Assembly Support Bracket · Honeywell International TPE331-1, TPE331-2, TPE331-3U and 2 more. Effective Jul 11, 1975
- [AD 74-24-05](https://openairdocs.org/ad/74-24-05): Propeller Pitch Control Sleeve Assembly · Honeywell International TPE331-3U, TPE331-3UW, TPE331-5 and 1 more. Effective Nov 26, 1974
- [AD 70-19-02](https://openairdocs.org/ad/70-19-02): High Speed Pinion Bearings · Honeywell International TPE331-1, TPE331-1U, TPE331-1UA and 3 more. Effective Feb 20, 1974
- [AD 71-05-07](https://openairdocs.org/ad/71-05-07): High Speed Pinion Assembly · Honeywell International TPE331-1, TPE331-1U, TPE331-1UA and 30 more. Effective Apr 8, 1972
- [AD 70-16-09](https://openairdocs.org/ad/70-16-09): High Speed Pinion Assembly · Honeywell International TPE331-3W
- [AD 70-04-04](https://openairdocs.org/ad/70-04-04): High Speed Pinion Retaining Nut · Honeywell International TPE331-1, TPE331-1U, TPE331-1UA and 3 more

### Historical (superseded or no longer in force)

- [AD 2018-02-14](https://openairdocs.org/ad/2018-02-14) (historical): Turbine Engine Combustion Section · Honeywell International TPE331-1, TPE331-10, TPE331-10AV and 38 more. Effective Feb 28, 2018
- [AD 2015-12-04](https://openairdocs.org/ad/2015-12-04) (historical): Fuel control unit (FCU) · Honeywell International TPE331-1, TPE331-10, TPE331-10AV and 26 more. Effective Jul 22, 2015
- [AD 2011-18-51](https://openairdocs.org/ad/2011-18-51) (historical): Main shaft bearing · Honeywell International TPE331-1, TPE331-10, TPE331-10A and 82 more
- [AD 2006-15-08](https://openairdocs.org/ad/2006-15-08) (historical): Woodward fuel control unit (FCU) assemblies · Honeywell International TPE331-1, TPE331-10, TPE331-10AV and 26 more. Effective Aug 24, 2006
- [AD 88-12-10](https://openairdocs.org/ad/88-12-10) (historical): Turbine Rotor · Honeywell International TPE331-10, TPE331-10R, TPE331-10U and 6 more. Effective Jun 6, 1988
- [AD 92-02-19 PL](https://openairdocs.org/ad/92-02-19-PL) (historical): Fuel Manifold Assembly Leak · Honeywell International TPE331-10, TPE331-10A, TPE331-10AV and 29 more
- [AD 91-04-02](https://openairdocs.org/ad/91-04-02) (historical): Third stage stator assembly · Honeywell International TPE331-1, TPE331-2, TPE331-2UA and 7 more
- [AD 90-21-01](https://openairdocs.org/ad/90-21-01) (historical): Third stage stator assembly · Honeywell International TPE331-1, TPE331-2, TPE331-2UA and 7 more

## Information bulletins (advisory) (4 in force)

- [SAIB NE-16-19](https://openairdocs.org/saib/NE-16-19): Turbine Engine Compressor Section  Stator Nozzle Distress. Issued Jul 22, 2016
- [SAIB NE-16-18](https://openairdocs.org/saib/NE-16-18): Power Lever  Loss of Power Control. Issued Jul 11, 2016
- [SAIB NE-06-70](https://openairdocs.org/saib/NE-06-70): . Issued Sep 25, 2006
- [SAIB NE-06-69](https://openairdocs.org/saib/NE-06-69): . Issued Sep 20, 2006

## NTSB investigations

None matched to N325UE.

## FAA accident and incident reports (2)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 20020822036899I](https://openairdocs.org/incident/20020822036899I), Aug 22, 2002: Jetair JETSTM4101 (N325UE), Newark, NJ. (-23) Flight crew aborted the takeoff twice. As per company procedures aircraft was returned to the gate. Maintenance adjusted a throttle micro switch.…
- [Incident 20020319004649I](https://openairdocs.org/incident/20020319004649I), Mar 19, 2002: Jetair JETSTM4101 (N325UE), Washington, DC. (-23) After aircraft arrived at the gate flight attendent attempted to open passenger door but could not. After several attempts by the crew from the outside…

## Service difficulty reports (43)

As reported by operators and repair stations. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR VTZA990185](https://openairdocs.org/sdr/VTZA990185), Jul 5, 1999: STARTER/GEN. MALFUNCTIONED. IAD/CHS - FLT 7311 - DURING CRUISE, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO LT GENERATOR DROPPED OFF-LINE. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEM
- [SDR VTZA98209](https://openairdocs.org/sdr/VTZA98209), Jun 2, 1998: BULB. FAILED. FLT 6199 - BDL-IAD - DURING LANDING, AIRCRAFT LANDED ON SCHEDULE WITH ONE DISCREPANCY WHICH WS NO RT MLG INDICATION. AIRCRAFT WENT TO GATE WITH NO FURTHER PROBL
- [SDR VTZA98167](https://openairdocs.org/sdr/VTZA98167), Apr 18, 1998: SMOKE DETECTOR. DIRTY. FLT 6302 - IAD-BOS - DURING CRUISE, EXPERIENCED A DISCREPANCY WITH THE POD SMOKE LIGHT ILLUMINATING. AIRCRAFT LANDED AT BOS AFTER DECLARING AN EMERGENCY. MAINTE
- [SDR VTZA98138](https://openairdocs.org/sdr/VTZA98138), Mar 19, 1998: SYMBOL GENERATOR. FAILED. FLT 6236 - BOS-BWI - DURING CRUISE, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO FO'S EFIS SCREENS WENT BLANK. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS
- [SDR VTZA98112](https://openairdocs.org/sdr/VTZA98112), Mar 9, 1998: SMOKE DETECTOR. FAILED. FLT 6371 - EWR-IAD - DURING TAXI, AIRCRAFT RETURNED TO GATE DUE TO BAGGAGE BAY SMOKE DETECTOR INOP, WOULD NOT TEST. AIRCRAFT WAS FERRIED TO IAD WHERE MAINTENANC
- [SDR VTZA97695](https://openairdocs.org/sdr/VTZA97695), Dec 14, 1997: SMOKE DETECTOR. FAILED. FLT 6497 - DET-IAD - DURING CRUISE, AIRCRAFT MADE AN UNSCHEDULED FLT DUE TO POD SMOKE WARNING LIGHT ILLUMINATED. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBL
- [SDR VTZA97659](https://openairdocs.org/sdr/VTZA97659), Dec 1, 1997: CONNECTOR. DIRTY. FLT 6356 - PWM-IAD - AIRCRAFT ABORTED TAKEOFF DUE TO RIGHT OIL PRESSURE WARNING LIGHT ILLUMINATED INTERMITTENTLY. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROB
- [SDR VTZA97663](https://openairdocs.org/sdr/VTZA97663), Nov 30, 1997: CONNECTOR. FAILED. FLT 6353 - IAD-TYS - AIRCRAFT MADE AN UNSCHEDULED LANDING AT IAD DUE TO NR 2 ENGINE IEC FAILED. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE 
- [SDR VTZA97626](https://openairdocs.org/sdr/VTZA97626), Nov 7, 1997: STARTER/GEN. FAILED. FLT 6211 - IAD-PVD - DURING CLIMB, AIRCRAFT MADE AN UNSCHEDULED LANDING AT IAD DUE TO RIGHT GENERATOR FAILED. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS
- [SDR VTZA97632](https://openairdocs.org/sdr/VTZA97632), Nov 6, 1997: DE-ICE BOOT. FAILED. FLT 6512 - IAD-LGA - DURING CLIMB, AIRCRAFT MADE AN UNSCHEDULED LANDING AT IAD DUE TO RIGHT PROP HEAT FAILED AND WARNING LIGHT ILLUMINATED. AIRCRAFT RETURNED TO
- [SDR VTZA97618](https://openairdocs.org/sdr/VTZA97618), Nov 4, 1997: CONNECTOR. LOOSE. IAD/BOS - FLT 6225 - DURING TAXI AT 1425 HOURS ON 11-4-97, AIRCRAFT RETURNED TO GATE DUE TO LT EGT FLUCTUATION AND IEC FELL OFF LINE. MAINTENANCE INSPECTED AND 
- [SDR VTZA97608](https://openairdocs.org/sdr/VTZA97608), Oct 27, 1997: FRICTION LEVERS. NOT SET. MHT/IAD - FLT 6574 - DURING TAKEOFF ON 10-27-97 AT 0640 HOURS, THE CREW EXPERIENCED A DISCREPANCY WITH THE TOCWS SYSTEM ACTIVATING. THE CREW ABORTED THE TAKEOFF
- [SDR VTZA97541](https://openairdocs.org/sdr/VTZA97541), Sep 12, 1997: SPEED TRANSDUCER. FAILED. FLT 6235 - IAD-CHO - DURING TAXI, AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS DUE TO ANTI-SKID LIGHT CYCLES ON AND OFF DURING TAXI. MAINTENANCE INSPECTED
- [SDR VTZA97259](https://openairdocs.org/sdr/VTZA97259), Apr 30, 1997: ENGINE. BIRD STRIKE. FLT 6212 - IAD-BDL - DURING APPROACH, MADE AN SCHEDULED LANDING AT BDL WITH ONE DISCREPANCY WHICH WAS BIRD STRIKE TO LEFT ENGINE. AIRCRAFT WENT TO GATE WITH NO 
- [SDR VTZA97253](https://openairdocs.org/sdr/VTZA97253), Apr 25, 1997: AIR DATA COMP. FAILED. IAD/CLE - FLT 6594 - DURING CLIMB-OUT AT 1230 HOURS ON 4-25-97, EXPERIENCED A FAILURE OF THE NR 1 AIR DATA COMPUTER. AIRCRAFT RETURNED TO IAD. MAINTENANCE INSPE
- [SDR VTZA97247](https://openairdocs.org/sdr/VTZA97247), Apr 23, 1997: DEICE MAT. FAILED. IAD/GSO - FLT 6321 - DURING CRUISE AT 1100 HOURS ON 4-23-97, MADE AN UNSCHEDLED LANDING AT CMH DUE TO RT PROP HEAT FAILED. AIRCRAFT WENT TO GATE WITH NO FURTHER
- [SDR VTZA97193](https://openairdocs.org/sdr/VTZA97193), Mar 20, 1997: FUEL CONTROL. OUT OF ADJUST. IAD/CHS - FLT 6483 - DURING LANDING AT 0920 HRS ON 3-20-97, MADE A SCHEDULED LANDING AT IAD WITH ONE DISCREPANCY WHICH WAS LT ENGINE TORQUE WENT TO -2.2 WITH LT
- [SDR VTZA97174](https://openairdocs.org/sdr/VTZA97174), Mar 13, 1997: SEAL. FAILED. EWR/BOS - FLT 6554 - DURING TAXI-OUT AT 1200 HRS ON 3-13-97, EXPERIENCED A PROBLEM WITH THE PASSENGER DOOR SEAL NOT INFLATING. AIRCRAFT RETURNED TO GATE AND CON
- [SDR VTZA97168](https://openairdocs.org/sdr/VTZA97168), Mar 6, 1997: OVERHEAT LOOP. FAILED. FLT 6264 - BTV-IAD - DURING APPROACH, MADE AN SCHEDULED LANDING AT IAD WITH ONE DISCREPANCY WHICH WAS LEFT ENGINE OVERHEAT LIGHT CAME ON DURING APPROACH. AIRCRA
- [SDR VTZA97136](https://openairdocs.org/sdr/VTZA97136), Feb 10, 1997: PWR DIST UNIT. FAILED. FLT 6445 - IAD-CHO - DURING TAXI-OUT, EXPERIENCED A RIGHT ENGINE NO START CONDITION. AIRCRAFT RETURNED TO THE GATE WHERE THE MAINTENANCE TECHNICIANS TROUBLESHOT
- [SDR VTZA97128](https://openairdocs.org/sdr/VTZA97128), Feb 3, 1997: FUEL CONTROL. OUT OF ADJUST. IAD-DAY - FLT 6292 - DURING LANDING, MADE A SCHEDULED LANDING WITH ONE DISCREPANCY WHICH WAS RT ENGIEN FLAMED OUT AFTER LANDING WHEN POWER LEVERS RETARDED. AIRC
- [SDR VTZA96461](https://openairdocs.org/sdr/VTZA96461), Dec 26, 1996: PDU. REQUIRED RESET. FLT 6280 - ORF-IAD - DURING CLIMB, AN UNSCHEDULED LANDING DUE TO LEFT ENGINE START CAPTION LIGHT ILLUMINATED. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS
- [SDR VTZA96453](https://openairdocs.org/sdr/VTZA96453), Dec 20, 1996: FUEL CONTROL. FAILED. FLT 6261 - IAD-EWR - ABORTED TAKEOFF DUE TO LEFT ENGINE WOULD ONLY MAKE 85 PERCENT TORQUE ON TAKEOFF ROLL. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. M
- [SDR VTZA96447](https://openairdocs.org/sdr/VTZA96447), Dec 19, 1996: ENGINE. LOW TORQUE. IAD-JFK - FLT 6577 - ABORTED TAKEOFF DUE TO NR 1 ENGINE WOULD ONLY MAKE 85 PERCENT TORQUE ON TAKEOFF ROLL. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. M
- [SDR VTZA96440](https://openairdocs.org/sdr/VTZA96440), Dec 13, 1996: TQ SIG COND. MALFUNCTIONED. FLT 6337 - IAD-EWR - ABORTED TAKEOFF DUE TO LEFT ENGINE WOULD ONLY MAKE 87 PERCENT TORQUE. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPE
- [SDR VTZA96425](https://openairdocs.org/sdr/VTZA96425), Dec 4, 1996: SWITCH. OUT OF ADJUST. FLT 6185 - IAD-RDU - ABORTED TAKEOFF DUE TO CONFIGURATION WARNING LIGHT ILLUMINATED. AIRCRAFT RETURNED TO GATE WITH NO FURHTER PROBLEMS. MAINTENANCE INSPECTED A
- [SDR VTZA97064](https://openairdocs.org/sdr/VTZA97064), Nov 15, 1996: IEC. MALFUNCTIONED. FLT 6198 - IAD-BDL - ABORTED TAKEOFF DUE TO RIGHT IEC FAILED. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE CLEARED IEC FAULT CODE 64. OPS CHE
- [SDR VTZA96388](https://openairdocs.org/sdr/VTZA96388), Sep 21, 1996: SWITCH STRIKER. OUT OF ADJUST. FLT 6395 - IAD-RIC - ABORTED TAKEOFF DUE TO BAGGAGE DOOR LIGHT ILLUMINATED. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE OPENED DMI 17799, M
- [SDR VTZA96373](https://openairdocs.org/sdr/VTZA96373), Sep 12, 1996: TO WARNING. ACTIVATED. FLT 6543 - EWR-IAD - ABORTED TAKEOFF DUE TO TAKEOFF CONFIGURATION WARNING. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED SYSTEM, NO 
- [SDR VTZA96361](https://openairdocs.org/sdr/VTZA96361), Sep 7, 1996: SWITCH. OUT OF ADJUST. IAD/EWR - FLT 6276 - DURING TAKEOFF AT 1945 HRS ON 9-7-96, ABORTED TAKEOFF DUE TO TAKEOFF CONFIGURATION WARNING. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCID
- [SDR VTZA96291](https://openairdocs.org/sdr/VTZA96291), Aug 6, 1996: PROP GOVERNOR. OUT OF ADJUST. JFK/BOS - FLT 6490 - DURING TAKEOFF AT 1930 HRS ON 8-6-96, MADE AN UNSCHEDULED LANDING DUE TO LT ENGINE WOULD ONLY OBTAIN 86 PERCENT TORQUE ON TAKEOFF ROLL. AIR
- [SDR VTZA96218](https://openairdocs.org/sdr/VTZA96218), Jun 8, 1996: GPU DOOR. NOT CLOSED. FLT NR 6270 - IAD-EWR - ABORTED TAKEOFF DUE TO GPU ACCESS DOOR LIGHT. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENT. MX INSPECTED AND CLOSED GPU ACCESS DOO
- [SDR VTZA96210](https://openairdocs.org/sdr/VTZA96210), Jun 3, 1996: LAV SERVICE DOOR. MISSING. FLT NR 6539 - BOS-EWR - DURING PREFLIGHT WALKAROUND, DISCOVERED THAT THE LAVATORY SERVICE DOOR WAS MISSING. MX OPENED DMI NR 17779 IAW MEL 52-4. MX LATER CLEARE
- [SDR VTZA96166](https://openairdocs.org/sdr/VTZA96166), Apr 23, 1996: DE-ICE LEAD. FAILED. FLT 6566 - ROC-JFK - ABORTED THE TAKEOFF, DUE TO THE LEFT PROP HEAT FAILING. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MX REPLACED THE LEFT PROP DE-I
- [SDR VTZA96158](https://openairdocs.org/sdr/VTZA96158), Apr 16, 1996: OIL TUBE. FAILED. IAD/EWR - FLT 6270 - DURING APPROACH AT 1315 HRS ON 4-16-96, SHUT DOWN RT ENGINE DUE TO OIL PRESSURE INDICATION LOST ON APPROACH. AN EMERGENCY DECLARED AND AIRC
- [SDR VTZA96151](https://openairdocs.org/sdr/VTZA96151), Apr 14, 1996: SWITCH. OUT OF ADJUST. IAD/LYH - FLT 6310 - DURING TAKEOFF TO LYH AT 1938 HRS ON 4-14-96, ABORTED TAKEOFF DUE TO MAIN BAGGAGE DOOR LIGHT ILLUMINATING DURING THE TAKEOFF ROLL. AIRCRAFT
- [SDR VTZA96114](https://openairdocs.org/sdr/VTZA96114), Mar 19, 1996: SWITCH. OUT OF ADJUST. FLT NR 6444 - BOS-IAD - ABORTED TAKEOFF DUE TO THE EMERGENCY EXIT DOOR WARNING ILLUMINATING DURING THE TAKEOFF ROLL. AIRCRAFT RETURNED TO GATE WITH NO FURTHER I
- [SDR VTZA96120](https://openairdocs.org/sdr/VTZA96120), Mar 14, 1996: SWITCH. DIRTY. FLT NR 6485 - IAD-JFK - ABORTED THE TAKEOFF DUE TO THE TAKEOFF CONFIGURATION WARNING SYSTEM ACTIVATING. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAI
- [SDR VTZA96080](https://openairdocs.org/sdr/VTZA96080), Feb 15, 1996: SWITCH. OUT OF ADJUST. FLT NR 6205 - IAD-MHT - DURING TAKEOFF, ABORTED THE TAKEOFF DUE TO THE EMERGENCY DOOR WARNING LIGHT ILLUMINATING DURING THE TAKEOFF ROLL. AIRCRAFT RETURNED TO G
- [SDR VTZA96048](https://openairdocs.org/sdr/VTZA96048), Dec 26, 1995: STARTER/GEN. FAILED. IAD/JFK - FLT 6171 - DURING TAKEOFF AT 1230 HRS ON 12-26-95, ABORTED TAKEOFF DUE TO LT GENERATOR FAILURE. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. M
- [SDR VTZA95298](https://openairdocs.org/sdr/VTZA95298), Sep 13, 1995: SMOKE DET. DIRTY. FLT NR 6417 - CHS-IAD - ABORTED TAKEOFF DUE TO THE VENTRAL BAGGAGE BAY SMOKE DETECTOR WARNING DURING THE TAKEOFF ROLL. AN EMERGENCY WAS DECLARED AND THE FIRE DE
- [SDR VTZA95213](https://openairdocs.org/sdr/VTZA95213), Jun 30, 1995: RELAY. FAILED. CHO/IAD - FLT 6270 - DURING CLIMB-OUT AT 100 HRS ON 6-30-95, THE LANDING GEAR WOULD NOT RETRACT WHEN SELECTED UP. AIRCRAFT PROCEEDED TO IAD AND LANDED AT IAD WI
- [SDR VTZA95212](https://openairdocs.org/sdr/VTZA95212), Jun 30, 1995: SWITCH. FAILURE. IAD/ORF - FLT 6462 - DURING TAKEOFF AT 1630 HRS ON 6-30-95, RETURNED TO IAD DUE TO THE LANDING GEAR NOT RETRACTING WHEN SELECTED UP. AIRCRAFT LANDED AT IAD WITH

## STCs that may be installed (OpenAirDocs) (20)

Approved for this aircraft's airframe or engine model, in force first, then newest. The registry doesn't record which STCs an aircraft has; its records do.

### Approved for the engine (AiResearch TPE331 series)

- [STC SE02538AK](https://openairdocs.org/stc/SE02538AK): Modification of Honeywell TPE331-12JR-702TT engine. TAE Aerospace (CTEC). Lists TPE331-12JR
- [STC SE03035AT](https://openairdocs.org/stc/SE03035AT): Installation of Royal Atlantic Aviation Engine Oil Filter Bypass Warning System, Kit P/N RAA2003-1-1. Reds Aircraft Service Inc. Lists TPE331-10N
- [STC SE00265AT](https://openairdocs.org/stc/SE00265AT): Install Ayres Fuel Manifold Purge Assembly Kit, P/N 21757-1 in accordance with "Installation Instructions - Ayres P/N 21757-1 Fuel Manifold Purge Assy-Kit" Dwg. No. 21757-1(1), Revision none, dated April 20, 1993, or later FAA approved revision. Thrush Aircraft Inc. Lists TPE331-1
- [STC SE2924SO](https://openairdocs.org/stc/SE2924SO): Installation of Garrett TPE-331-10 combustor and turbine in the TPE331-8 engine. National Flight Lakeland. Lists TPE331-8
- [STC SE01461NY](https://openairdocs.org/stc/SE01461NY): Propeller pitch control system modification. Hartzell HC-E4N-5D/D9690(B) propeller installed per STC SA01462NY. Not approved on serial numbers TC-398 through TC-418. Hartzell Propeller Inc. Lists TPE331-10UA
- [STC SE01604CH](https://openairdocs.org/stc/SE01604CH): Convert Honeywell TPE331-10AV-511B to a TPE331-10AV-511KA. National Flight Services, Inc. Lists TPE331-10AV
- [STC SE00229AT](https://openairdocs.org/stc/SE00229AT): Installation of Garrett TPE331-10 Combustor and Turbine in TPE331-6 engine. National Flight Services, Inc. Lists TPE331-6
- [STC SE00275AT](https://openairdocs.org/stc/SE00275AT): Installation of GarrettTPE331-10 combustor and turbine in the TPE331-5 engine. National Flight Services, Inc. Lists TPE331-5
- [STC SE00691CH](https://openairdocs.org/stc/SE00691CH): Modification of a turboprop engine to a turboshaft configuration by incorporation of AlliedSignal (Garrett) TSE331-3U turboshaft gearbox components and other associated changes. National Flight Services, Inc. Lists TPE331-10UA
- [STC SE383CH](https://openairdocs.org/stc/SE383CH): Modification of engines. National Flight Services, Inc. Lists TPE331-1
- [STC SE7547SW](https://openairdocs.org/stc/SE7547SW): Install Garrett P/N 865558-16 or865558-1E propeller pitch control cam. Peacock Joe N. Lists TPE331-25A
- [STC SE8029SW](https://openairdocs.org/stc/SE8029SW): Modify propeller pitch control, P/N 869130, by installing pitch control cam, Garrett P/N869386-1. Agri Jet Power, Inc. Lists TPE331-1
- [STC SE1725CE](https://openairdocs.org/stc/SE1725CE): Modification to replace torque pressure compensator with a plug for raw torque pressure indicating provision. Air Midwest, Inc. Lists TPE331-3UW
- [STC SE33WE](https://openairdocs.org/stc/SE33WE): Modification of: ( 1) Manual fuel valve and beta cams; (2) Fuel control linkage and propeller servo cam; and (3)Automatic control of bleed valve and engine starting functions; S/N P61801 only. Garrett Turbine Engine Company A Division of the Garrett Corporation. Lists TPE331-25D
- [STC SE35WE](https://openairdocs.org/stc/SE35WE): Modification of the fuel control, linkage to permit 75% r.p.m. for low ground idle. Garrett Turbine Engine Company Division of Garret Corporation. Lists TPE331-47
- [STC SE39WE](https://openairdocs.org/stc/SE39WE): Modification of the fuel control linkage to permit 75% r.p.m. for ground idle doe S/N 86001. Garrett Turbine Engine Company A Division of the Garrett Corporation. Lists TPE331-57
- [STC SE50WE](https://openairdocs.org/stc/SE50WE): One engine only. Modification of a Model TPE331-25DAL to. incorporate the engine components associated with a torque and temperature 1imitinq system in accordance with AiResearch Kit PIN 896642-1. An en9ine incorporating this kit is reidentified as a Model TPE331-25DALT . Garrett Turbine Engine Company Division of Garret Corporation. Lists TPE331-25DA
- [STC SE68WE](https://openairdocs.org/stc/SE68WE): Deletion of fireshield installation kit. West-Figueroa Trust. Lists TPE331-6
- [STC SE56WE](https://openairdocs.org/stc/SE56WE): Serial Numbers P-06012 AND P-06024: Installation of heated compressor inlet temperature sensor lines. AiResearch Manufacturing Company. Lists TPE331-5
- [STC SE38WE](https://openairdocs.org/stc/SE38WE): Modification of fuel control linkage to permit operation of 75% idle speed. S/N 61701 & 61702. Garrett Turbine Engine Company Division of Garret Corporation. Lists TPE331-55

## Related

- Other Jetstream JETSTREAM 4101 aircraft: https://openairdocs.org/model/jetstream-jetstream-4101/aircraft.md
- The AiResearch TPE331 series engine: https://openairdocs.org/engine/airesearch-tpe331-series.md

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