# N841PH: Dehavilland DHC-8-102, registration cancelled 2004-03-03 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: March 3, 2004 - Exported to: Canada - Status when cancelled: Valid registration - Airframe: [Dehavilland DHC-8-102](https://openairdocs.org/model/dehavilland-dhc-8-102) (registry code 2809003) - Engine: [Pratt & Whitney Canada PW120](https://openairdocs.org/engine/pratt-whitney-canada-pw120) (registry code 52114) - Data sheets: [TCDS A13NM](https://openairdocs.org/tcds/A13NM), [TCDS E20NE](https://openairdocs.org/tcds/E20NE) (OpenAirDocs) - Serial number: 082 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-prop - Airworthiness: Standard, transport - Airworthiness date: June 29, 1987 - Certificate issued: November 23, 1999 - Last registry action: October 30, 2003 - Mode S code: AB84DD - Owner when cancelled: [US Bancorp Equipment Finance Inc](https://openairdocs.org/faa-owner/US%20BANCORP%20EQUIPMENT%20FINANCE%20INC) - Location: [Portland, OR](https://openairdocs.org/faa-place/OR/Portland) - Owner type: Corporation - Owner's area on the map: 45.4403° N, 122.7766° W: Placed by OpenAirDocs at the center of ZIP code 97223, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N841PH - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=841PH - Page: https://openairdocs.org/deregistered/N841PH-2004-03-03 From the FAA registry file of October 29, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe. ADs and bulletins for the Dehavilland DHC-8-102: https://openairdocs.org/model/dehavilland-dhc-8-102.md ## Service difficulty reports (37) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR SABA020061](https://openairdocs.org/sdr/SABA020061), May 18, 2002: LIGHT. INOPERATIVE. AIRCRAFT 881 ON FLIGHT 5190 FROM AGS TO CLT. DURING POST FLIGHT INSPECTION AFTER ARRIVAL IN CLT THE EMERGENCY LIGHT AT 1A WOULD NOT TEST. MAINTENANCE REMOVED AN - [SDR SABA020058](https://openairdocs.org/sdr/SABA020058), May 9, 2002: BULB. BURNED OUT. Ailrcraft 841 on flight 5032 PGV to CLT. During post-flight inspection at CLT a floor emergency light was found intermittently inoperative. Maintenance removed - [SDR SABA020055](https://openairdocs.org/sdr/SABA020055), Apr 29, 2002: LIGHT. INOPERATIVE. AIRCRAFT 841 ON FLIGHT 5012 FROM CLT TO TLH. DURING INSPECTION PRIOR TO DEPARTURE MAINTENANCE FOUND FLOOR EMERGENCY LIGHT AT ROW 6 INOPERATIVE. MAINTENANCE REMO - [SDR SABA020031](https://openairdocs.org/sdr/SABA020031), Mar 1, 2002: LIGHT. INOPERATIVE. AIRCRAFT 841 ON FLIGHT 5025 FROM CLT TO TLH. DURING PREFLIGHT FOR FIRST FLIGHT OF THE DAY, THE NR 2 OVERHEAD EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REMOVE - [SDR SABA020018](https://openairdocs.org/sdr/SABA020018), Feb 8, 2002: BULB. BURNED OUT. Aircraft 841 on flight 5027 from CLT to CVG. During preflight inspection the emergency floor lights had one bulb inop. No emergency procedures were involved. Ma - [SDR SABA020006](https://openairdocs.org/sdr/SABA020006), Jan 17, 2002: LIGHT. BLEW OUT. Flight 5027 from CLT to CVG: During preflight pilot found two foward emergency floor lights out. Maintenance remoned and replaced Bulbs. System ops checked good - [SDR SABA010047](https://openairdocs.org/sdr/SABA010047), Sep 7, 2001: LIGHT. INOPERATIVE. ACFT 841 ON FLIGHT 5057 TLH TO CLT. AFTER THE AIRCRAFT WAS PARKED AT THE GATE IN CLT THE FLOOR EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. NO EMERGENCY PROCE - [SDR SABA010032](https://openairdocs.org/sdr/SABA010032), Jul 24, 2001: BATTERY PACK. DISCHARGED. AIRCRAFT 841 ON FLIGHT 5025 TLH TO CLT. AFTER ARRIVING AT CLT THE FLOOR EMERGENCY LIGHTING WAS FOUND TO BE INOPERATIVE. NO EMERGENCY WAS DECLARED AND NO EMERGEN - [SDR SABA010027](https://openairdocs.org/sdr/SABA010027), Jun 28, 2001: TOWERSHAFT. FAILED. ACFT 841 ON FLIGHT 5028 FROM TLH TO CLT. DURING CLIMBOUT FROM TLH THE RIGHT ENGINE SHUTDOWN. AN INFLIGHT EMERGENCY WAS DECLARED. THE AIRCRAFT RETURNED TO TLH AN - [SDR SABA010021](https://openairdocs.org/sdr/SABA010021), Jun 10, 2001: SEQUENCE VALVE. LEAKING. AIRCRAFT 841 ON FLIGHT 5157 CVG TO CLT. AFTER TAKEOFF THE RIGHT SYSTEM FAILED WITH A NR 2 ISOLATION LIGHT ILLUMINATED. ALSO THE RIGHT MAIN GEAR DOOR FAILED TO C - [SDR SABA010013](https://openairdocs.org/sdr/SABA010013), May 7, 2001: HARNESS. FAULTY. AIRCRAFT 841 ON FLIGHT 5190 FROM AGS TO CLT. DURING CRUISE FLIGHT FOUR RED FLOOR EVACUATION LIGHT BULBS BECAME DIM AND UNUSABLE. NO INFLIGHT EMERGENCY WAS DECLA - [SDR QXEA9800083](https://openairdocs.org/sdr/QXEA9800083), Feb 23, 1998: LIGHT. INOPERATIVE. OVERHEAD EMERGENCY LIGHT INOP. MAINTENANCE REPLACED OVERHEAD EMERGENCY LIGHT ASSEMBLY, OP'S CHECK NORMAL AS PER DE HAVILLAND MM. - [SDR QXEA9700916](https://openairdocs.org/sdr/QXEA9700916), Dec 23, 1997: LAMP. FAILED. SEA- BAGGAGE SMOKE WARNING TEST NR 2 INOP. TEST NR 1 WORKS NORMAL. RELAMPED TEST CIRCUIT OF NR 2 SMOKE DETECTOR, OPERATIONAL CHECK GOOD. - [SDR QXEA9700631](https://openairdocs.org/sdr/QXEA9700631), Oct 4, 1997: WARNING. SOUNDED. EUG - ABORTED TAKEOFF. TAKE OFF WARNING SOUNDED DURING TAKEOFF ROLL. MAINTENANCE CONTROL HAD CREW CYCLE FLAPS FULL DOWN, THEN FULL UP, THEN SET TO 5 DEGREES. TA - [SDR QXEA9700572](https://openairdocs.org/sdr/QXEA9700572), Sep 17, 1997: CONNECTOR. MALFUNCTION. AUTOFEATHER ARM WILL NOT TEST. REPLACED CANNON PLUGS 9811-P13 AND P14, OPERATIONAL CHECKS GOOD FOR NR 1 AND NR 2 ENGINE AUTOFEATHER SYSTEM. - [SDR QXEA9700569](https://openairdocs.org/sdr/QXEA9700569), Sep 16, 1997: HARNESS. MALFUNCTION. PDX - UNABLE TO TEST AUTO FEATHER, NO ARM LIGHT DURING TEST. REPLACED NR 1 AND NR 2 TRUSS HARNESS FROM FIREWALL TO ECU. GROUND RAN, OPERATIONAL CHECK GOOD. - [SDR QXEA9700565](https://openairdocs.org/sdr/QXEA9700565), Sep 14, 1997: DETECTOR. MALFUNCTION. SEA - LAV SMOKE DETECTOR DOES NOT TEST. REPLACED SMOKE DETECTOR, OPERATIONAL CHECK GOOD. - [SDR QXEA9700549](https://openairdocs.org/sdr/QXEA9700549), Sep 5, 1997: TQ SIGNAL COND. MALFUNCTION. BOI - AUTO FEATHER WOULD NOT ARM. REPLACED NR 1 AND NR 2 TSCU'S AND RELAY 6121K5, OPERATIONAL CHECK GOOD. - [SDR QXEA9700521](https://openairdocs.org/sdr/QXEA9700521), Aug 28, 1997: SWITCH LIGHT. MALFUNCTION. SEA- AUTO FEATHER WOULD NOT SELECT WHEN THE BUTTON WAS DEPRESSED. THIS OCCURRED DURING THE BEFORE TAKEOFF CHECKLIST. REPLACED AUTO FEATHER SWITCH LIGHT ASSY, OP - [SDR QXEA9700516](https://openairdocs.org/sdr/QXEA9700516), Aug 26, 1997: SWITCH. MALFUNCTION. SEA- AUTO FEATHER FAILED TO ARM ON TAKEOFF. ABORTED TAKEOFF AND RETURNED TO GATE. SWAPPED TORQUE SIGNAL CONDITIONERS, CONFIRMED LAYSHAFT SWITCHES. CHECKED RELAY - [SDR QXEA9700503](https://openairdocs.org/sdr/QXEA9700503), Aug 17, 1997: WIRE. FAILED. ABORTED TAKEOFF, AUTO FEATHER WOULD NOT ARM TO TAKEOFF ROLL. REPAIRED WIRING AT THE POWER LEVER SWITCH. - [SDR QXEA9700466](https://openairdocs.org/sdr/QXEA9700466), Aug 8, 1997: RELAY. FAILED. PSC - 24 HOUR SYSTEM CHECK NR 1 ENGINE FAILS AUTO FEATHER CHECK. REPLACED 2161 K3 RELAY. COMPLIED WITH AUTO FEATHER AND POWER UPTRIM. OPERATIONAL CHECK GOOD. - [SDR QXEA9700231](https://openairdocs.org/sdr/QXEA9700231), Jun 5, 1997: LIGHT. INOPERATIVE. COCKPIT OVERHEAD EMERGENCY LIGHT INOP. REPLACED LIGHT ASSEMBLY, OPERATIONAL CHECK GOOD. - [SDR QXEA9700155](https://openairdocs.org/sdr/QXEA9700155), Apr 25, 1997: INDICATOR. INACCURATE. PDX- AFTER TAKEOFF THE RIGHT ROLL SPOILER PFCS INDICATION WAS INACCURATE. RETURNED TO THE FIELD. REPLACED THE PFCS INDICATOR. OPERATIONAL CHECKS GOOD. AIRCRAFT - [SDR QXEA9700085](https://openairdocs.org/sdr/QXEA9700085), Mar 21, 1997: BATTERY. DISCHARGED. PDX- AFT CABIN EMERGENCY CEILING LIGHT, LEFT EGRESS LIGHT, AND AFT EXIT SIGN LOCATOR SIGN ARE INOP. BATTERY PACK PS3 REPLACED AND LIGHTS OP CHECKED GOOD. AIRCRA - [SDR QXEA9700077](https://openairdocs.org/sdr/QXEA9700077), Mar 15, 1997: LIGHT. INOPERATIVE. COCKPIT EMERGENCY LIGHT IS INOP. LIGHT ASSY REPLACED AND LIGHT OPS CHECKED GOOD. - [SDR QXEA9700070](https://openairdocs.org/sdr/QXEA9700070), Mar 6, 1997: CONTROL BOX. MALFUNCTIONED. EMERGENCY LIGHT STAYS ON WHEN SELECTED OFF. EMERGENCY LIGHT CONTROL BOX REPLACED AND LIGHT OPS CHECKED GOOD. - [SDR QXEA9700046](https://openairdocs.org/sdr/QXEA9700046), Feb 10, 1997: CONTROL BOX. MALFUNCTION. EMERGENCY LIGHTS FLASH ON AND OFF INTERMITTENTLY WHEN SELECTED TO ARM. EMERGENCY LIGHT CONTROL BOX ASSY REPLACED AND LIGHTS OPS CHECKED GOOD. - [SDR QXEA9600112](https://openairdocs.org/sdr/QXEA9600112), Mar 19, 1996: LIGHT. INOPERATIVE. COCKPIT OVERHEAD EMERGENCY LIGHT IS INOP. COCKPIT OVERHEAD LIGHT REPLACED AND LIGHT OPS CHECKED GOOD. - [SDR QXEA9600107](https://openairdocs.org/sdr/QXEA9600107), Mar 13, 1996: LIGHT. MISINSTALLED. COCKPIT OVERHEAD EMERGENCY LIGHT IS ON BRIGHT WHEN IN THE MOUNTING BRACKET AND ENGINES ARE RUNNING. LIGHT DOESN'T COME ON WHEN EMERGENCY LIGHTS ARE TURNED ON. L - [SDR QXEA9600087](https://openairdocs.org/sdr/QXEA9600087), Feb 28, 1996: LIGHT. INOPERATIVE. PDX - COCKPIT EMERGENCY LIGHT IS INOPERATIVE. LIGHT REPLACED AND LIGHT OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. - [SDR QXEA9600076](https://openairdocs.org/sdr/QXEA9600076), Feb 26, 1996: LIGHT. INOP. COCKPIT PORTABLE LIGHT IS INOP. LIGHT AND HOLDER REPLACED AND LIGHT OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. - [SDR QXEA9500452](https://openairdocs.org/sdr/QXEA9500452), Dec 25, 1995: CONNECTOR. LOOSE PINS. BOI - EMERGENCY LIGHT BY FLIGHT ATTENDANT SEAT INOP. LIGHT CONNECTOR REPAIRED AND LIGHT OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. - [SDR QXEA9500128](https://openairdocs.org/sdr/QXEA9500128), Apr 25, 1995: EEL BULB. FAILED. GEG - RIGHT AFT UNDER WING EGRESS LIGHT INOP. REPLACED BULB AND LIGHT OPS CHECKED GOOD. AIRCRFT RETURNED TO SERVICE. - [SDR QXEA9500108](https://openairdocs.org/sdr/QXEA9500108), Apr 9, 1995: PBE UNIT. VACUUM LOSS. BOI - THE FLIGHT ATTENDANTS P.B.E. IS SOFT AND THE RED TAB IS EXTENDED. - [SDR QXEA9500107](https://openairdocs.org/sdr/QXEA9500107), Apr 7, 1995: PBE UNIT. VACUUM LOSS. BOI - THE P.B.E. IN THE CABIN STORAGE CLOSET IS FULL OF AIR. REPLACED P.B.E. WITH A SERVICEABLE UNIT. AIRCRAFT WAS RETURNED TO SERVICE. - [SDR QXEA9500002](https://openairdocs.org/sdr/QXEA9500002), Jan 2, 1995: ACTUATOR. INTERMITTENT. PDX - LT MLG RED UNSAFE LIGHT REMAINED ILLUMINATED AFTER GEAR EXTENSION. CREW SELECTED ALTERNATE EXTENSION AND GEAR CAME DOWN AND LOCKED. REPLACED LT MLG UPLOCK --- 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.