# N805EX: 1990 Boeing DHC-8-102, registration cancelled 2018-06-29 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: June 29, 2018 - Exported to: Canada - Status when cancelled: Valid registration - Airframe: [Boeing DHC-8-102](https://openairdocs.org/model/boeing-dhc-8-102) (registry code 1386002) - 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: 228 - Year built: 1990 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-prop - Airworthiness: Standard, transport - Airworthiness date: September 6, 1990 - Certificate issued: January 8, 2018 - Last registry action: May 8, 2018 - Mode S code: AAF4EA - Owner when cancelled: [Wells Fargo Trust Co Na Trustee](https://openairdocs.org/faa-owner/WELLS%20FARGO%20TRUST%20CO%20NA%20TRUSTEE) - Location: [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City) - Owner type: Corporation - Owner's area on the map: 40.7558° N, 111.8843° W: Placed by OpenAirDocs at the center of ZIP code 84111, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N805EX - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=805EX - Page: https://openairdocs.org/deregistered/N805EX-2018-06-29 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 Boeing DHC-8-102: https://openairdocs.org/model/boeing-dhc-8-102.md ## Service difficulty reports (140, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR HNAA2017101000346](https://openairdocs.org/sdr/HNAA2017101000346), Oct 6, 2017: BULB. BURNED OUT. CABIN FLOOR EMERGENCY LIGHT THIRD RED LIGHT BULB INOPERATIVE AT SEAT 1DF. REMOVED & REPLACED THE BULB. - [SDR HNAA2017092900339](https://openairdocs.org/sdr/HNAA2017092900339), Sep 26, 2017: UNKNOWN. ODOR. CREW REPORTED AN ODD ODOR IN THE ACFT AROUND SEAT 5AC. DROPPED LT PSU AND CENTER AISLE PANEL INSPECTED, NO FAULTS FOUND. REINSTALLED PSU AND CENTER PANEL. OPS C - [SDR HNAA20170918316](https://openairdocs.org/sdr/HNAA20170918316), Sep 16, 2017: WARNING LIGHT. UNKNOWN. RIGHT AC BUSS CAUTION LIGHT ILLUMINATED DURING CLIMB OUT, WITH ASSOCIATED CAUTION LIGHTS. REMOVED AND REINSTALLED THE LT AC GCU FOR TROUBLESHOOTING. REPLACED RT - [SDR HNAA2017072500247](https://openairdocs.org/sdr/HNAA2017072500247), Jul 21, 2017: BATTERY. DISCHARGED. FWD RT EXTERNAL EMERGENCY LIGHT INOPERATIVE, GALLEY CEILING, RT FWD EMERGENCY EXIT TOP, NOT WORKING . CHANGED THE BATTERY AT 3351 PS2 LOCATION IAW AMM 33-51-00, - [SDR HNAA2017062800220](https://openairdocs.org/sdr/HNAA2017062800220), Jun 27, 2017: SENSOR. DIRTY. NR 1 ENGINE OIL TEMP WENT INTO THE HIGH YELLOW RANGE TOUCHING THE RED RANGE. CLEANED THE OIL TEMP GROUND TO ENGINE FLANGE. TEMP DROPPED 30 DEGREES C. OPS CHECKE - [SDR HNAA2017040300099](https://openairdocs.org/sdr/HNAA2017040300099), Apr 1, 2017: PROPELLER. POWER LOSS. DURING TAKE OFF ROLL, THE NR 2 PROPELLER RPM WAS 1137. R & R THE PCU IAW WC 61-10-10R. PERFORMED RIGGING IAW WC 76-00-01Q AND R & R THE NR 2 NP SENSOR IAW 72-01 - [SDR HNAA2017022400063](https://openairdocs.org/sdr/HNAA2017022400063), Feb 24, 2017: BULB. DIM. LOWER EMERGENCY LIGHT IS DIM BY ROW 4AC. REMOVED AND REPLACED THE BULBS. OPS CHECKED GOOD. - [SDR HNAA2017022400062](https://openairdocs.org/sdr/HNAA2017022400062), Feb 24, 2017: BULB. DIM. LOWER EMERGENCY LIGHT BY PAX DOOR IS DIM. REMOVED AND REPLACED THE BULBS. OPS CHECKED GOOD. - [SDR HNAA2017020800047](https://openairdocs.org/sdr/HNAA2017020800047), Feb 5, 2017: BULB. INOPERATIVE. EMERGENCY LIGHT AT 3DF IS INOPERATIVE. REMOVED AND REPLACED THE BULB. - [SDR HNAA2017011600019](https://openairdocs.org/sdr/HNAA2017011600019), Jan 16, 2017: INTERCOSTAL. CRACKED. LEFT INBOARD NACELLE INTERCOSTAL WAS FOUND CRACKED. FABRICATED REPLACEMENT INTERCOSTAL IAW EO8-54-17-0032 AND DRAWING 85410643. - [SDR HNAA2016123000351](https://openairdocs.org/sdr/HNAA2016123000351), Dec 30, 2016: INVERTER. ODOR. MODERATE ELECTRICAL ODOR IN COCKPIT AND GALLEY. ISOLATED TO SECONDARY INVERTER. - [SDR HNAA2016120700377](https://openairdocs.org/sdr/HNAA2016120700377), Dec 7, 2016: BULB. INOPERATIVE. 2ND AND 18TH FLOOR PATH EMERGENCY LIGHT IS INOPERATIVE. REMOVED AND REPLACED THE BULBS IN EMERGENCY FLOOR PATH LIGHTS. OPS CHECKED GOOD. - [SDR HNAA2016102600336](https://openairdocs.org/sdr/HNAA2016102600336), Oct 26, 2016: BATTERY PACK. MALFUNCTIONED. TWO ADJACENT RED FLOOR EMERGENCY LIGHTS ILLUMINATED, THEN EXTINGUISHED. REMOVED AND REPLACED BATTERY. OPS CHECKED GOOD. - [SDR HNAA2016082900263](https://openairdocs.org/sdr/HNAA2016082900263), Aug 26, 2016: BULB. INOPERATIVE. ROW 1, 4TH EMERGENCY LIGHT FROM THE FRONT IS OUT. R & R THE BULB. - [SDR HNAA2016071100214](https://openairdocs.org/sdr/HNAA2016071100214), Jul 8, 2016: BULB. INOPERATIVE. RIGHT AFT EXTERIOR EMERGENCY LIGHT BULB INOPERATIVE. R & R THE LIGHT BULB. - [SDR HNAA2015102700313](https://openairdocs.org/sdr/HNAA2015102700313), Oct 27, 2015: BRUSH BLOCK. DAMAGED. EMERGENCY LIGHTS FLICKERED IN FLIGHT WITH PROP HEAT ON AND OFF. R & R BOTH BRUSH BLOCKS, OPS CHECKED GOOD. - [SDR HNAA2015101900301](https://openairdocs.org/sdr/HNAA2015101900301), Oct 19, 2015: LIGHT. INTERMITTENT. EMERGENCY LIGHTS FLICKERING IN FLIGHT WITH PROP HEAT ON. INSPECTED AND CLEANED NR 2 CONNECTORS AT BRUSH BLOCK. SEATED EMERGENCY LIGHT BATTERIES AT PS1 AND PS2. - [SDR HNAA2015090900276](https://openairdocs.org/sdr/HNAA2015090900276), Sep 9, 2015: CONNECTOR. CORRODED. COULD NOT TRANSMIT NR 1 COM FROM EITHER SIDE. FOUND NR 1 VHF ANT AND CONN 2320-P4-1 CORRODED. R & R CONNECTOR PLU 2320-P4-1 AND NR 1 VHF ANTENNA. SYSTEM OPS CHE - [SDR HNAA2015090900275](https://openairdocs.org/sdr/HNAA2015090900275), Sep 9, 2015: ELECTRONIC UNIT. INOPERATIVE. COULD NOT TRANSMIT ON NR 1 COM FROM EITHER SIDE. R & R REMOTE ELECTRONIC UNIT IAW PB 23-15. OPS CHECKED GOOD, OK FOR SERVICE. - [SDR HNAA2015090400272](https://openairdocs.org/sdr/HNAA2015090400272), Sep 4, 2015: BULB. INOPERATIVE. 4TH EMERGENCY ESCAPE PATH FLOOR LIGHT IS INOPERATIVE. R & R BULB. OPS CHECKED GOOD. - [SDR HNAA2015060900191](https://openairdocs.org/sdr/HNAA2015060900191), Jun 9, 2015: SEAT TRACK. CORRODED. SEAT TRACK CORRODED ON INBD AFT FLOOR FLANGE AT FRAME BS 253.4. R & R SECTION OF DAMAGED SEAT TRACK IAW RD8-53-3074. - [SDR HNAA2015060900190](https://openairdocs.org/sdr/HNAA2015060900190), Jun 9, 2015: SEAT TRACK. CORRODED. SEAT TRACK CORRODED JUST FORWARD OF FRAME BS 222. REPAIRED THE SEAT TRACK IAW RD8-53-3074. - [SDR HNAA2015060900189](https://openairdocs.org/sdr/HNAA2015060900189), Jun 9, 2015: THRESHOLD. CORRODED. PASSENGER DOOR THRESHOLD HAS AREAS OF CORROSION NEXT TO SCREW HOLES. R & R PASSENGER DOOR THRESHOLD AND INSTALLED WITH NEW IAW DWG 85321241. - [SDR HNAA2015060900188](https://openairdocs.org/sdr/HNAA2015060900188), Jun 9, 2015: ATTACH FITTING. CORRODED. PASSENGER DOOR STRUTS LOWER ATTACH SHAFT HAS MINOR CORROSION RADIATING FROM FORWARD AND AFT ENDS. CLEANED AND TREATED MINOR CORROSION ON PASSENGER DOOR LOWER AT - [SDR HNAA2015060900187](https://openairdocs.org/sdr/HNAA2015060900187), Jun 9, 2015: SEAT TRACK. CORRODED. SEAT TRACK CORRODED ON INBD AFT FLOOR FLANGE AT FRAME BS 253.4. R & R SECTION OF DAMAGED SEAT TRACK IAW RD8-53-3074. - [SDR HNAA2015041000126](https://openairdocs.org/sdr/HNAA2015041000126), Apr 10, 2015: CONTROL BOX. MALFUNCTIONED. EMERGENCY LIGHTS START TO FLICKER AFTER TAKEOFF AND CONTINUED TO FLICKER TILL LANDING WITH PROP HEAT ON OR OFF. R & R F/A EMERGENCY LIGHT SWITCH AND EMERGENCY L - [SDR HNAA2015032500108](https://openairdocs.org/sdr/HNAA2015032500108), Mar 25, 2015: CONNECTOR. DAMAGED. WHEN PROP HEAT CYCLES TO NR 2 PROP A PHASE, EMERGENCY LIGHTS ILLUMINATED. INSPECTED AND FOUND CONNECTOR PLUG 3061-J4 AND CONNECTOR PLUG 3061-P5 WITH HIGH RESIST - [SDR HNAA2015031600098](https://openairdocs.org/sdr/HNAA2015031600098), Mar 16, 2015: MODULE. INOPERATIVE. EMERGENCY FLOOR PATH LIGHTS ARE INOPERATIVE AT ROW 9. R & R EMERGENCY FLOOR LIGHT MODULE AND REPAIRED BROKEN WIRE, AT SAID LOCATION. OPS CHECKED GOOD. - [SDR HNAA2015030200068](https://openairdocs.org/sdr/HNAA2015030200068), Mar 2, 2015: BRUSH BLOCK. MALFUNCTIONED. EMERGENCY LIGHTS FLICKERED WHEN PROP HEAT "A" PHASE ON. EITHER TIMER. R & R RT ENGINE BRUSH BLOCK DUE TO SUSPICIOUS. GROUND RAN AIRCRAFT. COULD NOT DUPLICATE EM - [SDR HNAA2015021600051](https://openairdocs.org/sdr/HNAA2015021600051), Feb 16, 2015: BULB. INOPERATIVE. EMERGENCY LIGHT IS INOPERATIVE AT ROWS 1AC-1DC. R & R THE BULB . OPS CHECKED GOOD. - [SDR HNAA2015021600048](https://openairdocs.org/sdr/HNAA2015021600048), Feb 16, 2015: UNKNOWN. SMOKE. APU BLEED AIR SMOKE NOTICED IN COCKPIT. INSPECTED APU AND BLEED, GROUND RAN ENGINE. RAN APU WITH BLEEDS SELECTED ON FOR OVER 30 MINUTES WITH NO SMOKE OR ODOR. C - [SDR HNAA2015021300043](https://openairdocs.org/sdr/HNAA2015021300043), Feb 13, 2015: FEEDER CABLE. ARCED. DC FEEDER CABLE DAMAGE FROM ARCING AT ROW 4 TERMINAL CONNECTION. R & R DC FEEDER CABLE. - [SDR HNAA2015012000023](https://openairdocs.org/sdr/HNAA2015012000023), Jan 20, 2015: LENS. MELTED. ODOR FOUND IN WARDROBE. WARDROBE COURTESY LIGHT LENS WAS FOUND TO BE MELTED. R & R BULB AND LENS IAW 25-28-00. OPS CHECKED GOOD. - [SDR HNAA2014122900389](https://openairdocs.org/sdr/HNAA2014122900389), Dec 29, 2014: LIGHT. MALFUNCTIONED. EMERGENCY LIGHTS FLICKERED ON INTERMITTENTLY IN FLIGHT. INSPECTED PROP HEAT LEADS AND BRUSH BLOCK. INSPECTED CIRCUIT BREAKER L3L AND L1. INSPECTED 9811J3 AND RE - [SDR HNAA2014122600382](https://openairdocs.org/sdr/HNAA2014122600382), Dec 26, 2014: BULB. INOPERATIVE. EMERGENCY LIGHT IS INOPERATIVE AT ROW 2. R & R BULB. OPS CHECKED GOOD. - [SDR HNAA2014121700366](https://openairdocs.org/sdr/HNAA2014121700366), Dec 17, 2014: UNKNOWN. UNKNOWN. EMERGENCY LIGHTS FLICKERED FIVE TIMES, 3-5 SECONDS EA ON CLIMB OUT, ALL ICING SYSTEMS SELECTED ON. OK FOR REST OF FLIGHT. REMOVED PANELS 412 AND 419AT. INSPECTE - [SDR HNAA2014112400335](https://openairdocs.org/sdr/HNAA2014112400335), Nov 24, 2014: CIRCUIT BREAKER. TRIPPED. RT PROPELLER HEAT A AND B PHASE IS INOPERATIVE, PROPELLER HEAT A AND B PHASE CIRCUIT BREAKER OUT. RESET THE CIRCUIT BREAKERS AND OPS CHECKED GOOD. - [SDR HNAA2014111000314](https://openairdocs.org/sdr/HNAA2014111000314), Nov 10, 2014: BULB. INOPERATIVE. THE 17TH EMERGENCY LIGHT, RED ARROW, IS INOPERATIVE AT ROW 7. R & R THE BULB. CHECKED GOOD. - [SDR HNAA2014081800238](https://openairdocs.org/sdr/HNAA2014081800238), Aug 18, 2014: BALLAST. FAILED. CABIN INTERIOR NORMAL LIGHTING SYSTEM, FOUND OVERHEAD BALLAST BURNED AT ROW 7DF. DEACTIVATED ASSOCIATED LIGHT SYS. PULLED AND COLLARED CIRCUIT BREAKERS R1, S1 A - [SDR HNAA2014081100228](https://openairdocs.org/sdr/HNAA2014081100228), Aug 11, 2014: BATTERY PACK. FAILED. TWO AFT EMERGENCY CEILING LIGHTS, FWD CEILING EMERGENCY LIGHT ALL OP EMERGENCY SIGNS MID CABIN COME ON, THEN GOES OUT. R & R ALL EMERGENCY LIGHT BATTERIES IAW 3 - [SDR HNAA2014052700164](https://openairdocs.org/sdr/HNAA2014052700164), May 27, 2014: ACTUATOR. FALSE INDICATION. NOSE RED UNSAFE AND GEAR HANDLE LIGHTS ILLUMINATED ON NORMAL GEAR EXTENSION. GEAR WARNING HORN SOUNDED, CYCLE GEAR AND RED UNSAFE LIGHT ILLUMINATED. USED ALTERN - [SDR HNAA2014040400120](https://openairdocs.org/sdr/HNAA2014040400120), Apr 4, 2014: INVERTER. ODOR. STRONG FISH ODOR IN COCKPIT, THROUGH ENTIRE FLIGHT. R & R SECONDARY INVERTER IAW MM 24-22-00. OPS CHECKED GOOD. - [SDR HNAA2014031900093](https://openairdocs.org/sdr/HNAA2014031900093), Mar 19, 2014: LINE. DISCONNECTED. BOTH NR 1 AND 2 ENGINES BLEED AIR CAUTION HOT LIGHT CYCLING ON & OFF DURING FLIGHT. ACFT WAS DEICED HEAVILY BEFORE FLIGHT. FOUND P3 LINE TO BLEED SWITCH DISCONN - [SDR HNAA2014022400055](https://openairdocs.org/sdr/HNAA2014022400055), Feb 24, 2014: UNKNOWN. ODOR. CREW REPORTED FUEL ODOR WITH APU BLEEDS ON. INSPECTED APU BAY, NO FUEL LEAKS NOTED. - [SDR HNAA2013122300632](https://openairdocs.org/sdr/HNAA2013122300632), Dec 23, 2013: LIGHT. WEAK. LEFT BETA EMERGENCY LIGHT IS WEAK/ DIM. R & R LT BETA EMERGENCY LIGHT IAW AMM 33-51-00. - [SDR HNAA2013122300631](https://openairdocs.org/sdr/HNAA2013122300631), Dec 23, 2013: LIGHT. WEAK. RIGHT AFT EMERGENCY EXIT BETA LIGHT IS WEAK/ DIM. R & R AFT EMERGENCY EXIT BETA LIGHT IAW H33-51-00. - [SDR HNAA2013030800116](https://openairdocs.org/sdr/HNAA2013030800116), Mar 8, 2013: TIMER. FAILED. AIRFRAME DEICE BOOTS ARE INOPERATIVE IN AUTO, FAST AND SLOW. OK IN MANUAL. R & R DEICE TIMER. OPS CHECKED GOOD IAW MM 30-10-00. OK FOR SERVICE. - [SDR HNAA2013012500011](https://openairdocs.org/sdr/HNAA2013012500011), Jan 25, 2013: CONTROL BOX. INOPERATIVE. EMERGENCY LIGHTS WILL NOT TURN ON. RERACKED EMERGENCY LIGHT CONTROL BOX. SYSTEM OPS CHECKED GOOD. OK FOR SERVICE. - [SDR HNAA2012122801133](https://openairdocs.org/sdr/HNAA2012122801133), Dec 28, 2012: HMU. MALFUNCTIONED. FUEL ODOR IN CABIN OFF ENGINE BLEEDS, SUSPECT NR 2 BLEED. R & R NR 2 ENGINE HMU AND FUEL PUMP IAW WC 73-20-01R AND 76-00-01Q. GROUND RAN, OPS CHECKED GOOD. - [SDR HNAA2012111601060](https://openairdocs.org/sdr/HNAA2012111601060), Nov 16, 2012: FRAME. CORRODED. FRAME CORRODED AND CRACKED. DOUBLER IS ALSO LIFTED. R & R FRAME SECTION AT BS 202 IAW EA 16-2012-013 AND DWG 85320004 AND EA 16-2012-014. All 140: https://openairdocs.org/deregistered/N805EX-2018-06-29/reports.md ## FAA accident and incident reports (4) 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 20030126000949I](https://openairdocs.org/incident/20030126000949I), Jan 26, 2003: Dhav DHC8102 (N805EX), Pittsburgh, PA. (-23) At 1137E on January 26, 2003, allegheny airlines flight #3569, a DH8 landed on runway 28R with #1 engine shut down for unknown reasons. Emergency was… - [Incident 19991111034089I](https://openairdocs.org/incident/19991111034089I), Nov 11, 1999: Dhav DHC8102 (N805EX), Pittsburgh, PA. (-23) On November 11, 1999 at 1820E, N805EX, a DHC-8, s/n 228, operating as "pcaa", flight #3832 aboarted takeoff. The aborted take off was at Pittsburgh… - [Incident 19990106005019I](https://openairdocs.org/incident/19990106005019I), Jan 6, 1999: Dhav DHC8102 (N805EX), Syracuse, NY. (-5)On Wednesday, January 6, 1999, at 0957 local, a Dehavilland DHC-8-100, N805EX operated by allegheny airlines, d/b/a us airways express, diverted to… - [Incident 19940530026389I](https://openairdocs.org/incident/19940530026389I), May 30, 1994: Dhav DHC8102 (N805EX), Philadelphia, PA, Minor damage. Over temp battery warning lights. Smoke in cabin. Diverted. Evacuated on runway. Internal failure battery monitor. --- 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.