# N807EX: 1991 Boeing DHC-8-102

- Status: Valid registration
- Airframe: [Boeing DHC-8-102](https://openairdocs.org/model/boeing-dhc-8-102) (registry code 1386002, 39 seats)
- 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) (De Havilland Aircraft of Canada Limited), [TCDS E20NE](https://openairdocs.org/tcds/E20NE) (Pratt & Whitney Canada Corp.) (OpenAirDocs)
- Serial number: 292
- Year built: 1991
- Type: Fixed wing multi engine
- Engine type: Turbo-prop
- Airworthiness: Standard, transport
- Airworthiness date: September 3, 1991
- Certificate issued: September 22, 2022
- Expires: September 30, 2029
- Mode S code: AAFC58
- Registered owner: [Frontera Flight Holdings Inc](https://openairdocs.org/faa-owner/FRONTERA%20FLIGHT%20HOLDINGS%20INC)
- Location: [Dover, DE](https://openairdocs.org/faa-place/DE/Dover)
- Owner type: Corporation
- Owner's area on the map: 39.1815° N, 75.4736° W: Placed by OpenAirDocs at the center of ZIP code 19901, within about 5 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=807EX
- Page: https://openairdocs.org/aircraft/N807EX

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.

## ADs that may apply (OpenAirDocs): 171 in force

### Matched by airframe (Boeing DHC-8-102)

- [AD 2026-11-06](https://openairdocs.org/ad/2026-11-06): Hardware; Standard practices/structures · De Havilland Aircraft of Canada DHC-8-101, DHC-8-102, DHC-8-103 and 9 more. Effective Jul 9, 2026
- [AD 2026-13-02](https://openairdocs.org/ad/2026-13-02): Navigation · Airbus Canada Limited Partnership 18, 49-46, 80-A and 555 more. Effective Jul 1, 2026
- [AD 2021-19-11](https://openairdocs.org/ad/2021-19-11): Flight controls · De Havilland Aircraft of Canada DHC-8-102, DHC-8-103, DHC-8-106 and 8 more. Effective Nov 18, 2021
- [AD 2019-12-17](https://openairdocs.org/ad/2019-12-17): Stabilizers · Bombardier DHC-8-102, DHC-8-103, DHC-8-106 and 5 more. Effective Aug 12, 2019
- [AD 2018-23-04](https://openairdocs.org/ad/2018-23-04): Engine Controls · Bombardier DHC-8-102, DHC-8-103, DHC-8-106 and 5 more. Effective Mar 15, 2019
- [AD 2018-20-12](https://openairdocs.org/ad/2018-20-12): Ice and rain protection · Bombardier DHC-8-102, DHC-8-103, DHC-8-106 and 5 more. Effective Nov 23, 2018
- [AD 2017-15-11](https://openairdocs.org/ad/2017-15-11): Landing Gear · Bombardier DHC-8-102, DHC-8-103, DHC-8-106 and 5 more. Effective Sep 5, 2017
- [AD 2017-08-02](https://openairdocs.org/ad/2017-08-02): Ignition · Bombardier DHC-8-102, DHC-8-103, DHC-8-106 and 5 more. Effective May 17, 2017
- [AD 2016-24-06](https://openairdocs.org/ad/2016-24-06): Ice and rain protection · Bombardier DHC-8-102, DHC-8-103, DHC-8-106 and 5 more. Effective Jan 12, 2017
- [AD 2016-24-01](https://openairdocs.org/ad/2016-24-01): Electrical Power · Bombardier DHC-8-102, DHC-8-103, DHC-8-106 and 5 more. Effective Dec 30, 2016
- [AD 2016-10-07](https://openairdocs.org/ad/2016-10-07): Electrical power · Bombardier DHC-8-102, DHC-8-103, DHC-8-106 and 5 more. Effective Jun 23, 2016
- [AD 2015-21-02](https://openairdocs.org/ad/2015-21-02): Electrical Power · Bombardier DHC-8-102, DHC-8-103, DHC-8-106 and 5 more. Effective Nov 24, 2015
- [AD 2015-14-03](https://openairdocs.org/ad/2015-14-03): Fuel · Bombardier DHC-8-102, DHC-8-103, DHC-8-106 and 5 more. Effective Aug 21, 2015
- [AD 2015-04-08](https://openairdocs.org/ad/2015-04-08): Landing Gear · Bombardier DHC-8-102, DHC-8-103, DHC-8-106 and 5 more. Effective Apr 27, 2015
- [AD 2013-15-06](https://openairdocs.org/ad/2013-15-06): Electrical Power · Bombardier DHC-8-102, DHC-8-103, DHC-8-106 and 5 more. Effective Oct 20, 2014
- [AD 2014-15-07](https://openairdocs.org/ad/2014-15-07): Wings · Bombardier DHC-8-102, DHC-8-103, DHC-8-106 and 5 more. Effective Sep 2, 2014
- [AD 2014-13-18](https://openairdocs.org/ad/2014-13-18): Instruments, Engine Controls · Bombardier DHC-8-102, DHC-8-103, DHC-8-106 and 5 more. Effective Aug 19, 2014
- [AD 2014-05-17](https://openairdocs.org/ad/2014-05-17): Fuel · Bombardier DHC-8-102, DHC-8-103, DHC-8-106 and 5 more. Effective May 2, 2014
- [AD 2013-22-04](https://openairdocs.org/ad/2013-22-04): Flight controls · Bombardier DHC-8-102, DHC-8-103, DHC-8-106 and 8 more. Effective Dec 5, 2013
- [AD 2013-16-12](https://openairdocs.org/ad/2013-16-12): Nacelles/pylons · Bombardier DHC-8-102, DHC-8-103 and DHC-8-106. Effective Sep 24, 2013
- [AD 2013-14-09](https://openairdocs.org/ad/2013-14-09): Landing gear · Bombardier DHC-8-101, DHC-8-102, DHC-8-103 and 6 more. Effective Sep 10, 2013
- [AD 2013-04-07](https://openairdocs.org/ad/2013-04-07): Electrical Power · Bombardier DHC-8-102, DHC-8-103, DHC-8-106 and 5 more. Effective Apr 9, 2013
- [AD 2012-15-16](https://openairdocs.org/ad/2012-15-16): Landing gear · Bombardier DHC-8-102, DHC-8-103, DHC-8-106 and 8 more. Effective Sep 12, 2012
- [AD 2012-04-08](https://openairdocs.org/ad/2012-04-08): Flight controls · Bombardier DHC-8-102, DHC-8-103, DHC-8-106 and 8 more. Effective Apr 10, 2012
- [AD 2012-05-07](https://openairdocs.org/ad/2012-05-07): Engine Controls · Bombardier DHC-8-102, DHC-8-103 and DHC-8-106. Effective Apr 4, 2012
- [AD 2011-21-08](https://openairdocs.org/ad/2011-21-08): Equipment/Furnishings · ATR - GIE Avions de Transport Régional ATR42-200, ATR42-300, ATR42-320 and 202 more. Effective Nov 23, 2011
- [AD 2011-21-04](https://openairdocs.org/ad/2011-21-04): Doors · Bombardier DHC-8-102, DHC-8-103, DHC-8-106 and 5 more. Effective Nov 16, 2011
- [AD 2011-09-12](https://openairdocs.org/ad/2011-09-12): Windows · Bombardier DHC-8-101, DHC-8-102, DHC-8-103 and 8 more. Effective Jun 6, 2011
- [AD 2011-01-09](https://openairdocs.org/ad/2011-01-09): Oxygen · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 290 more. Effective Feb 9, 2011
- [AD 2010-21-02](https://openairdocs.org/ad/2010-21-02): Landing gear · Bombardier DHC-8-101, DHC-8-102, DHC-8-103 and 9 more. Effective Nov 12, 2010
- [AD 2010-05-12](https://openairdocs.org/ad/2010-05-12): Wings · Bombardier DHC-8-102, DHC-8-103, DHC-8-106 and 2 more. Effective Apr 13, 2010
- [AD 2010-04-12](https://openairdocs.org/ad/2010-04-12): Landing Gear, Standard Practices/Structures, Doors, Fuselage, Nacelles/Pylons, Stabilizers and  Wings. · Bombardier DHC-8-101, DHC-8-102, DHC-8-103 and 6 more. Effective Apr 8, 2010
- [AD 2008-09-25 R1](https://openairdocs.org/ad/2008-09-25-R1): Fuel · Bombardier DHC-8-102, DHC-8-103, DHC-8-106 and 5 more. Effective Dec 10, 2009
- [AD 2009-21-03](https://openairdocs.org/ad/2009-21-03): APU full- authority digital controller (FADEC) · Bombardier DHC-8-101, DHC-8-102, DHC-8-103 and 10 more. Effective Nov 20, 2009
- [AD 2009-06-21](https://openairdocs.org/ad/2009-06-21): Fuselage spoiler cable · Bombardier DHC-8-102, DHC-8-103, DHC-8-106 and 8 more. Effective Apr 28, 2009
- [AD 2008-26-03](https://openairdocs.org/ad/2008-26-03): Electronic strike system of the cockpit doo · Cockpit door electro-mechanical strike (Jazz Air STC ST02014NY). Effective Apr 13, 2009
- [AD 2008-13-09](https://openairdocs.org/ad/2008-13-09): Fuel tank bonding jumpers · Bombardier DHC-8-102, DHC-8-103, DHC-8-106 and 5 more. Effective Sep 17, 2008
- [AD 2008-04-17](https://openairdocs.org/ad/2008-04-17): Observer utility light system · Bombardier DHC-8-102, DHC-8-103, DHC-8-106 and 8 more. Effective Apr 3, 2008
- [AD 2007-23-04](https://openairdocs.org/ad/2007-23-04): Elevator spring tab mechanism · Bombardier DHC-8-102, DHC-8-103, DHC-8-106 and 5 more. Effective Dec 11, 2007
- [AD 2007-21-16](https://openairdocs.org/ad/2007-21-16): Spolier cable · Bombardier DHC-8-102, DHC-8-103, DHC-8-106 and 5 more. Effective Nov 21, 2007
- [AD 2007-12-01](https://openairdocs.org/ad/2007-12-01): Main landing gear (MLG) shock strut · Bombardier DHC-8-101, DHC-8-102, DHC-8-103 and 6 more. Effective Jul 10, 2007
- [AD 2007-06-19](https://openairdocs.org/ad/2007-06-19): Main landing gear (MLG) and nose landing gear (NLG) handle assemblies for alternate release and  
 the MLG retaining plate. · Bombardier DHC-8-102, DHC-8-103, DHC-8-106 and 5 more. Effective Apr 27, 2007
- [AD 2007-04-22](https://openairdocs.org/ad/2007-04-22): Electrical cable harness assembly. · Bombardier DHC-8-102, DHC-8-103, DHC-8-106 and 5 more. Effective Apr 3, 2007
- [AD 2007-01-11](https://openairdocs.org/ad/2007-01-11): Flight compartment door · Bombardier DHC-8-101, DHC-8-102, DHC-8-103 and 9 more. Effective Mar 5, 2007
- [AD 2006-20-04](https://openairdocs.org/ad/2006-20-04): Inspection of chain assemblies of elevator trim system · Bombardier DHC-8-102, DHC-8-103, DHC-8-106 and 5 more. Effective Nov 2, 2006
- [AD 2006-17-17](https://openairdocs.org/ad/2006-17-17): Rivets on left and right control column torque tube assemblies · Bombardier DHC-8-102, DHC-8-103, DHC-8-106 and 8 more. Effective Sep 29, 2006
- [AD 2006-17-10](https://openairdocs.org/ad/2006-17-10): Fluorescent light tube assemblies of the cabin, lavatory, and sidewall · Bombardier DHC-8-102, DHC-8-103, DHC-8-106 and 5 more. Effective Sep 27, 2006
- [AD 2005-13-35](https://openairdocs.org/ad/2005-13-35): Flight idle stop · Bombardier DHC-8-101, DHC-8-102, DHC-8-103 and 6 more. Effective Sep 26, 2005
- [AD 2005-13-38](https://openairdocs.org/ad/2005-13-38): Longitudinal skin joints in the fuselage pressure shell · Bombardier DHC-8-101, DHC-8-102, DHC-8-103 and 6 more. Effective Aug 9, 2005
- [AD 2005-11-10](https://openairdocs.org/ad/2005-11-10): Brake shuttle valves · Bombardier DHC-8-102, DHC-8-103, DHC-8-106 and 5 more. Effective Jul 12, 2005

### Matched by engine (Pratt & Whitney Canada PW120)

- [AD 2015-20-03](https://openairdocs.org/ad/2015-20-03): Fuel nozzle and the fuel manifold flow adapter · Pratt & Whitney Canada PW120, PW121, PW121A and 6 more. Effective Nov 18, 2015
- [AD 2012-26-08](https://openairdocs.org/ad/2012-26-08): Propeller shafts · Pratt & Whitney Canada PW118, PW118A, PW118B and 20 more. Effective Feb 15, 2013
- [AD 2006-19-06](https://openairdocs.org/ad/2006-19-06): Propeller shaft · Pratt & Whitney Canada PW118, PW118A, PW118B and 14 more. Effective Sep 29, 2006
- [AD 2003-21-03](https://openairdocs.org/ad/2003-21-03): Low pressure rotor speed (NL) sensor · Pratt & Whitney Canada PW118, PW120, PW120A and 1 more. Effective Nov 20, 2003
- [AD 2003-16-04](https://openairdocs.org/ad/2003-16-04): Fuel heaters · Pratt & Whitney Canada PW118, PW118A, PW118B and 19 more. Effective Sep 10, 2003
- [AD 98-14-02](https://openairdocs.org/ad/98-14-02): Fuel Manifold Transfer Tubes · Pratt & Whitney Canada PW118, PW118A, PW118B and 17 more. Effective Aug 31, 1998
- [AD 97-17-05](https://openairdocs.org/ad/97-17-05): Gas Generator Case Drain Ports · Pratt & Whitney Canada PW118, PW118A, PW118B and 17 more. Effective Sep 9, 1997
- [AD 94-03-02](https://openairdocs.org/ad/94-03-02): High Pressure Turbine Disks · Pratt & Whitney Canada PW118, PW118A, PW120 and 5 more. Effective Feb 16, 1994
- [AD 92-01-08](https://openairdocs.org/ad/92-01-08): High Pressure Rotor · Pratt & Whitney Canada PW118, PW118A, PW120 and 5 more. Effective Jul 27, 1992
- [AD 91-06-02](https://openairdocs.org/ad/91-06-02): Turbomachinery Magnetic Chip Detector · Pratt & Whitney Canada PW118, PW118A, PW120 and 6 more. Effective Mar 29, 1991
- [AD 91-01-03](https://openairdocs.org/ad/91-01-03): Hydromechanical Fuel Control Units · Pratt & Whitney Canada JT15D-5, PW118, PW118A and 3 more. Effective Jan 7, 1991
- [AD 88-26-51](https://openairdocs.org/ad/88-26-51): High Pressure Turbine Components · Pratt & Whitney Canada PW118, PW118A, PW120 and 2 more. Effective Sep 22, 1989

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

- [AD 2014-06-08](https://openairdocs.org/ad/2014-06-08) (historical): Landing gear · Bombardier DHC-8-101, DHC-8-102, DHC-8-103 and 6 more. Effective Apr 14, 2014
- [AD 2012-14-04](https://openairdocs.org/ad/2012-14-04) (historical): Landing gear · Bombardier DHC-8-101, DHC-8-102, DHC-8-103 and 6 more. Effective Aug 27, 2012
- [AD 2006-12-16](https://openairdocs.org/ad/2006-12-16) (historical): Structural testing of the cockpit door · Bombardier DHC-8-102, DHC-8-103, DHC-8-106 and 5 more. Effective Jul 18, 2006
- [AD 74-08-09 R2](https://openairdocs.org/ad/74-08-09-R2) (historical): Waste Receptacles · Aero Spacelines 377, 377MG, 377SGT and 268 more. Effective Jul 29, 1996
- [AD 2014-14-02](https://openairdocs.org/ad/2014-14-02) (historical): O-ring seal · Pratt & Whitney Canada PW120, PW121, PW121A and 6 more. Effective Aug 15, 2014
- [AD 2012-11-14](https://openairdocs.org/ad/2012-11-14) (historical): Propeller shafts · Pratt & Whitney Canada PW118, PW118A, PW118B and 20 more. Effective Jul 20, 2012

All 177: https://openairdocs.org/aircraft/N807EX/ads.md

## Information bulletins (advisory)

None matched.

## NTSB investigations

None matched to N807EX.

## FAA accident and incident reports (3)

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 20030312007869I](https://openairdocs.org/incident/20030312007869I), Mar 12, 2003: Dhav DHC8102 (N807EX), Syracuse, NY, Minor damage. (-23) Approximately 10-15 miles out on approach to syr first officer smelled fumes in cockpit. After the smell grew worse the crew donned oxygen masks. At…
- [Incident 19991215034869I](https://openairdocs.org/incident/19991215034869I), Dec 15, 1999: Dhav DHC8102 (N807EX), Providence, RI, Minor damage. (-23) Allegheny flight 3637 struck a ramp boundary fence with the left wing while taxiing in a non-movement area at pvd. Visibility was marginal and the pilot…
- [Incident 19930108003989I](https://openairdocs.org/incident/19930108003989I), Jan 8, 1993: Dhav DHC8102 (N807EX), Lancaster, PA. Smell at cabin overheat light. Diverted to Lancaster. Found dirt and small plastic chips on reading light lens.

## Service difficulty reports (93, newest 50)

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 HNAA2017051000157](https://openairdocs.org/sdr/HNAA2017051000157), May 9, 2017: LAMP. INOPERATIVE. EMERGENCY LIGHTS ON CENTER FLOOR AT ROW 4 DO NOT ILLUMINATE. REPLACED THE BULBS.
- [SDR HNAA2017051000156](https://openairdocs.org/sdr/HNAA2017051000156), May 9, 2017: LAMP. INOPERATIVE. AFT EGRESS LIGHT ON RIGHT SIDE OF AIRCRAFT WILL NOT ILLUMINATE. R & R THE LAMP.
- [SDR HNAA2016112300357](https://openairdocs.org/sdr/HNAA2016112300357), Nov 23, 2016: LIGHT. INOPERATIVE. THIRD RED EMERGENCY FLOOR LIGHT IS INOPERATIVE AT ROW 4DF. REMOVED AND REPLACED THE EMERGENCY LIGHT. OPS CHECKED GOOD.
- [SDR HNAA2016112300356](https://openairdocs.org/sdr/HNAA2016112300356), Nov 23, 2016: BULB. INOPERATIVE. LEFT FORWARD EMERGENCY EGRESS LIGHT IS INOPERATIVE. REMOVED AND REPLACED THE BULB. OPS CHECKED GOOD.
- [SDR HNAA2016090700269](https://openairdocs.org/sdr/HNAA2016090700269), Sep 6, 2016: LIGHT. INOPERATIVE. 4TH FLOOR PATH EMERGENCY LIGHT INOPERATIVE. R & R BULB FOR 4TH FLOOR EMERGENCY LIGHT RESECURED LENS AND TRIM.
- [SDR HNAA2016090700272](https://openairdocs.org/sdr/HNAA2016090700272), Sep 4, 2016: B-NUT. LOOSE. AFTER OPENING GEAR DOORS OIL SPLASHED ON LEFT MAIN TIRE AND DRIPPING NOTED FROM GEAR DOORS ON NR 1 NACELLE. INSPECTED AND CLEANED AREA, FOUND ONE B-NUT ON ISOLA
- [SDR HNAA2016090700270](https://openairdocs.org/sdr/HNAA2016090700270), Sep 2, 2016: LIGHT. INOPERATIVE. ROW 1 HAS 2 ADJACENT RED EMERGENCY ESCAPE PATH LIGHTS INOPERATIVE. RELAMPED EMERGENCY PATH LIGHT, OPS CK GOOD OK FOR SERVICE.
- [SDR HNAA2016081100246](https://openairdocs.org/sdr/HNAA2016081100246), Aug 10, 2016: BULB. INOPERATIVE. EMERGENCY LIGHT SWITCH ON F/A PANEL DOES NOT ILLUMINATE. R & R THE BULB.
- [SDR HNAA2016041800109](https://openairdocs.org/sdr/HNAA2016041800109), Apr 15, 2016: BULB. INOPERATIVE. EMERGENCY LIGHT 8TH FROM FRONT OF ACFT INOPERATIVE. R & R BULB.
- [SDR HNAA2016021900045](https://openairdocs.org/sdr/HNAA2016021900045), Feb 19, 2016: BULB. INOPERATIVE. EMERGENCY LIGHT INOPERATIVE AT ROW 7. R & R THE BULBS. OPS CHECKED GOOD.
- [SDR HNAA2015112000343](https://openairdocs.org/sdr/HNAA2015112000343), Nov 20, 2015: UNKNOWN. ODOR. BURN ODOR IN FLIGHT DECK WITH NO POWER ON AIRCRAFT. MAINTENANCE POWER ACFT WITH APU FOR APPROXIMATELY 15 MINUTES. NO EVIDENCE OF ANY BURNING ODOR. OK FOR SERVIC
- [SDR HNAA2015072900239](https://openairdocs.org/sdr/HNAA2015072900239), Jul 29, 2015: BULB. INOPERATIVE. TWO RED FLOOR EMERGENCY LIGHTS ARE INOPERATIVE. R & R BULBS. OPS CHECKED GOOD.
- [SDR HNAA2015072900238](https://openairdocs.org/sdr/HNAA2015072900238), Jul 29, 2015: POWER SUPPLY. MALFUNCTIONED. CABIN EMERGENCY LIGHT SYS FLASHES ON/OFF INTERMITTENTLY DURING FLIGHT. INSPECTED EMERGENCY LIGHT SYS, SWITCHES AND CIRCUIT BREAKERS. NO DEFECTS NOTED. INSPECTED
- [SDR HNAA2015031300094](https://openairdocs.org/sdr/HNAA2015031300094), Mar 13, 2015: BULB. INOPERATIVE. FORWARD MOST EMERGENCY FLOOR PATH LIGHT IS INOPERATIVE. R & R BULB. OPS CHECKED GOOD.
- [SDR HNAA2015011400017](https://openairdocs.org/sdr/HNAA2015011400017), Jan 14, 2015: WIRE HARNESS. BURNED. DURING CRUISE, APPROXIMATELY 6,000 FT, NR 1 ECU CIRCUIT BREAKER TRIPPED WITH NR 1 FUEL CAUTION LIGHT ILLUMINATED. NR 1 TORQUE FELL TO 3.8. CONFIRMED LOSS OF POW
- [SDR HNAA2014122900388](https://openairdocs.org/sdr/HNAA2014122900388), Dec 29, 2014: SWITCH. FAILED. EMERGENCY LIGHTS FLICKER IN FLIGHT. R & R LIGHT SWITCH AT F/A PANEL. OPS CHECKED GOOD ON THE GROUND. OK FOR SERVICE.
- [SDR HNAA2014082200248](https://openairdocs.org/sdr/HNAA2014082200248), Aug 22, 2014: BATTERY PACK. FAILED. FORWARD TWO EMERGENCY LIGHTS ARE INOPERATIVE. R & R EMERGENCY LIGHT BATTERY. OPS CHECKED GOOD.
- [SDR HNAA2014062400187](https://openairdocs.org/sdr/HNAA2014062400187), Jun 21, 2014: ENGINE. OUT OF RIG. DURING CLIMBOUT WITH NR 1 POWER LEVER FULL. COULD NOT MAINTAIN CLIMB TORQUE. RIGGED NR 1 ENGINE. GROUND RAN ACFT. OPS CHECKED GOOD.
- [SDR HNAA2014061300179](https://openairdocs.org/sdr/HNAA2014061300179), Jun 13, 2014: SWITCH. OUT OF ADJUST. TAKEOFF WARNING HORN SOUNDED WHEN ADVANCING POWER LEVERS. RESET PARAMETERS, STILL SOUNDS. ADJUSTED NR 1 CONDITION LEVER SWITCH 3151-S3 IAW MM 76-10-13. OPS CHEC
- [SDR HNAA2014030300066](https://openairdocs.org/sdr/HNAA2014030300066), Feb 28, 2014: SMOKE DETECTOR. FALSE ACTIVATION. DURING APPROACH, SMOKE WARNING LIGHT ILLUMINATED BRIEFLY, APPROXIMATELY FIVE SECONDS. ALONG WITH THE MASTER WARNING. EXTINGUISHED BY THEMSELVES. NO SMOKE DETECT
- [SDR HNAA2014020300028](https://openairdocs.org/sdr/HNAA2014020300028), Feb 3, 2014: BULB. INOPERATIVE. BULBS ARE OUT IN EMERGENCY EXIT THRESHOLD LIGHT SIGN ON FORWARD LT SIDE. R & R BULBS. OPS CHECKED GOOD.
- [SDR HNAA2014020300027](https://openairdocs.org/sdr/HNAA2014020300027), Feb 3, 2014: COVER. BROKEN. EMERGENCY LIGHT COVER IS BROKEN AT ROW 4. R & R EMERGENCY LIGHT COVER. OPS CHECKED GOOD.
- [SDR HNAA2013122500637](https://openairdocs.org/sdr/HNAA2013122500637), Dec 25, 2013: DRAIN. CORRODED. CORROSION FOUND AT NOSE WATER DRAIN AT STA X167.00. REPAIRED IAW EA15-2013-525 AND EO8-53-13-0733.
- [SDR HNAA2013120600601](https://openairdocs.org/sdr/HNAA2013120600601), Dec 6, 2013: WARNING LIGHT. ILLUMINATED. AFTER ROTATION, NR 2 AC GENERATOR CAUTION LIGHT ILLUMINATED. AFTER THREE MINUTES, NR 2 AC GENERATOR HOT LIGHT ILLUMINATED. CYCLED GENERATOR OFF IAW CHECK LIST. 
- [SDR HNAA2013120400598](https://openairdocs.org/sdr/HNAA2013120400598), Dec 4, 2013: GENERATOR. FAILED. AFTER ROTATION, NR 2 AC GENERATOR CAUTION LIGHT ILLUMINATED. ABOUT 3 MINUTES LATER, NR 2 AC GENERATOR HOT CAUTION LIGHT ILLUMINATED. CYCLED GENERATOR OFF IAW CH
- [SDR HNAA2013092700518](https://openairdocs.org/sdr/HNAA2013092700518), Sep 27, 2013: RELAY. MALFUNCTIONED. REJECTED TAKEOFF DUE TO AUTO FEATHER FAILURE TO ARM. GROUND RAN ACFT, COULD NOT DUPLICATE. R & R ARM CONTROL RELAY 6121-K5 FOR POSITIVE MX ACTION. OPS CHECKED G
- [SDR HNAA2013081200458](https://openairdocs.org/sdr/HNAA2013081200458), Aug 12, 2013: SWITCH. INOPERATIVE. AT 300 FEET, BETA LOCKOUT CYCLED NR 2 PROPELLER. RETURNED TO FIELD. ACTIVATED BETA LOCKOUT SYS. BOTH BETA LOCKOUT SWITCHES MOVED TO ENABLE. R & R SWITCH 6141-S4
- [SDR HNAA2013080200440](https://openairdocs.org/sdr/HNAA2013080200440), Aug 2, 2013: TRANSCEIVER. FAILED. WEATHER RADAR IS INOPERATIVE. MESSAGE APPEARS IN LOWER RT, NO RETURNS PAINTED. R & R RADAR R/T IAW MM 34-41-04. OPS CHECKED GOOD.
- [SDR HNAA2013040300197](https://openairdocs.org/sdr/HNAA2013040300197), Apr 3, 2013: STARTER GEN. MALFUNCTIONED. NR 1 DEC GENERATOR HOT CAUTION LIGHT ILLUMINATED IN FLIGHT. R & R NR 1 DC STARTER GENERATOR. OPS CHECKED GOOD IAW 24-30-02R. OK FOR SERVICE.
- [SDR HNAA2013032200143](https://openairdocs.org/sdr/HNAA2013032200143), Mar 22, 2013: ANGLE. CRACKED. ANGLE FOUND CRACKED ON TOP OF FUSELAGE , UNDER CENTER PANEL 261 FT. R & R WITH NEW PART IAW SRM 51-42-05 AND SRM 51-40-10.
- [SDR HNAA2013032200142](https://openairdocs.org/sdr/HNAA2013032200142), Mar 22, 2013: BULB. FAILED. EMERGENCY FLOOR PATH LIGHT IS INOPERATIVE AT ROW 7. R & R BULB. OPS CHECKED GOOD.
- [SDR HNAA2012122701131](https://openairdocs.org/sdr/HNAA2012122701131), Dec 24, 2012: CONTROL BOX. MALFUNCTIONED. MASTER WARNING CHECK, FIRE DETECTION LIGHT ILLUMINATED INFLT FOR APPROX 2 MINUTES. NO OTHER INDICATIONS OF FIRE, SMOKE, OR OTHER ADV LIGHTS. R & R WARNING LIGHT
- [SDR HNAA2012111201037](https://openairdocs.org/sdr/HNAA2012111201037), Nov 12, 2012: LAMP. FAILED. F/A EMERGENCY LIGHT SWITCH IS NOT BACK ILLUMINATED. RELAMPED F/A EMERGENCY LIGHT SWITCH. OPS CHECKED GOOD
- [SDR HNAA2012080800907](https://openairdocs.org/sdr/HNAA2012080800907), Aug 8, 2012: BULB. FAILED. EMERGENCY LIGHT INOPERATIVE. R & R LAMP . OPS CHECKED GOOD IAW AMM 33-51-11.
- [SDR HNAA2012072500881](https://openairdocs.org/sdr/HNAA2012072500881), Jul 25, 2012: BULB. FAILED. EMERGENCY FLOOR LAMP IS INOPERATIVE AT 4TH RED LIGHT FROM REAR OF ACFT. R & R BULB AT 4TH AFT FLOOR EMERGENCY. OPS CHECKED GOOD.
- [SDR HNAA2012072500880](https://openairdocs.org/sdr/HNAA2012072500880), Jul 25, 2012: BULB. FAILED. EMERGENCY LIGHT BUTTON ON F/A PANEL WILL NOT COME ON. REMOVED BULB FROM EMERGENCY LIGHT BUTTON ON F/A PANEL. INSTALLED NEW BULB. OPS CHECKED GOOD.
- [SDR HNAA2012052900806](https://openairdocs.org/sdr/HNAA2012052900806), May 29, 2012: BATTERY. FAILED. FLOOR EMERGENCY LIGHTS ARE INOPERATIVE FROM ROW 4 TO ROW 7 AND 2 RED IN FRONT ARE OUT. R & R BATTERIES IAW 33-50-05R AND 33-50-03Q.
- [SDR HNAA2012050300762](https://openairdocs.org/sdr/HNAA2012050300762), May 3, 2012: LAMP. FAILED. DIM LEFT EMERGENCY EXIT EGRESS LIGHT. R & R LAMP. OPS CHECKED GOOD.
- [SDR HNAA2012030200634](https://openairdocs.org/sdr/HNAA2012030200634), Mar 2, 2012: RADOME. DAMAGED. POSSIBLE LIGHTNING STRIKE OR STATIC DISCHARGE ON APPROACH. NO VISIBLE STORMS IN THE AREA. NO LOSS OF INSTRUMENTS. MX FOUND NOSE CONE AND TAIL CONE DAMAGE FROM L
- [SDR HNAA2011081200246](https://openairdocs.org/sdr/HNAA2011081200246), Aug 7, 2011: PUMP. FAILED. NR 2 STANDBY HYD PUMP HOT CAUTION LIGHT ILLUMINATED, FOLLOWED THEN BY STANDBY PUMP CIRCUIT BREAKER POPPED. SWAP OVER TEMP SENSOR TO SPARE. NO FIX. SWAP BACK TO 
- [SDR HNAA2011051700141](https://openairdocs.org/sdr/HNAA2011051700141), May 14, 2011: SWITCH. INOPERATIVE. ABORTED TAKEOFF DURING TAKEOFF ROLL. AUTOFEATHER DID NOT ARM. R & R SWITCH 6121-S13. GROUND RUN OPS CHECKED GOOD IAW RUNUP MANUAL.
- [SDR HNAA2011051700138](https://openairdocs.org/sdr/HNAA2011051700138), May 13, 2011: SWITCH. INOPERATIVE. ABORTED TAKEOFF AUTOFEATHER WILL NOT ARM. CYCLED POWER LEVERS, OPS CHECKED NORMAL. R & R SWITCH 6121-S13. GROUND RUN, OPS CHECKED GOOD IAW RUNUP MANUAL.
- [SDR HNAA2011040300067](https://openairdocs.org/sdr/HNAA2011040300067), Mar 29, 2011: SMOKE DETECTOR. FALSE INDICATION. DURING CLIMB OUT, BAG BAY SMOKE DETECTOR CAUTION LIGHT ILLUMINATED WITH MASTER CAUTION WARNING. FIRE DEPT CLEARED ACFT WITH NO SMOKE OR FIRE INDICATIONS. SMOKE 
- [SDR HNAA2011021500022](https://openairdocs.org/sdr/HNAA2011021500022), Feb 4, 2011: UNKNOWN. ODOR. STRONG ODOR OF FUEL IN CABIN WITH NO AIR CONDITION RUNNING. INSPECTED APU BAY, NO FUEL LEAKS NOTED. GROUND RAN NR 2 ENGINE WITH BLEEDS ON, FUEL ODOR DECREASED, 
- [SDR HNAA2010092300221](https://openairdocs.org/sdr/HNAA2010092300221), Sep 23, 2010: LAMP. INOPERATIVE. EMERGENCY FLOOR PATH LIGHTS ARE INOP. FROM 5DF TO 6DF. R & R EMERGENCY FLOOR PATH LIGHT LAMP AT 5DF, ALL PATH LIGHT ILLUMINATED, THEN CLOSED ACCESS PANEL IAW 33
- [SDR HNAA2010063000162](https://openairdocs.org/sdr/HNAA2010063000162), Jun 10, 2010: BULB. INOPERATIVE. RT AFT FUSELAGE MOUNTED EMERGENCY LIGHT IS NOT WORKING. REMOVED LENS, R & R BULB, REINSTALLED LENS.
- [SDR HNAA2010063000161](https://openairdocs.org/sdr/HNAA2010063000161), Jun 7, 2010: SIGN. INOPERATIVE. EMERGENCY EXIT SIGN ABOVE F/A SEAT NOT WORKING. R & R POWER SUPPLY BASE 3351-PS2. OPS CHECKED GOOD.
- [SDR HNAA2010042700128](https://openairdocs.org/sdr/HNAA2010042700128), Apr 27, 2010: CONNECTOR. DIRTY. MAIN BATTERY HOT CAUTION LIGHT ILLUMINATED AFTER TAKEOFF AT APPROX 1000 FEET. INSPECTED MAIN BATTERY CONNECTOR PLUG AND WIRING, NO DEFECTS NOTED. CLEANED AND RE
- [SDR HNAA2009121500345](https://openairdocs.org/sdr/HNAA2009121500345), Dec 7, 2009: SPOILER. CRACKED. LOSS OF QUANTITY ON NR 1 HYD SYS AFTER SELECTION OF SPOILERS TO FLIGHT. NR 1 RUDDER ISO ILLUMINATED. NR 1 HYD QUANTITY AT 1/2 QUART. MECHANIC FOUND RT ROLL SPOI
- [SDR HNAA2009080900243](https://openairdocs.org/sdr/HNAA2009080900243), Jul 31, 2009: WARNING SYSTEM. FALSE ACTIVATION. AT FLO ON JULY 31, TAKEOFF WARNING HORN SOUNDED ON TAKEOFF ROLL. RESET ELEVATOR TRIM, OPS CHECK GOOD. FOLLOW UP: ON AUGUST 3 ROA MAINTENANCE PERFORMED TAKEOFF W

All 93: https://openairdocs.org/aircraft/N807EX/reports.md

## STCs that may be installed (OpenAirDocs) (151, first 50)

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 airframe (Boeing DHC-8-102)

- [STC ST00153IB](https://openairdocs.org/stc/ST00153IB): Installation of Static Line Provisions. Voyageur Aviation Corp
- [STC ST12461IB](https://openairdocs.org/stc/ST12461IB): Installation of Cockpit Voice Recorder with optional RIPS Upgrade. Mid- Canada Mod Center
- [STC ST00197IB](https://openairdocs.org/stc/ST00197IB): Installation of the Universal Quick Access Recorder (uQAR). Flight Data Technologies Inc
- [STC ST04328NY](https://openairdocs.org/stc/ST04328NY): The Manufacture and Installation of Exterior Placards, Labels and Signs is to be performed, installed. Libellule Monde Inc
- [STC ST03875NY](https://openairdocs.org/stc/ST03875NY): Installation of interior placards, signs and markings. Libellule Monde Inc
- [STC SA2622NM](https://openairdocs.org/stc/SA2622NM): Installation of Precise Flight Pulselite Control Unit in landing/taxi system. (767-200 B17) (DHC-8 101). Precise Flight Inc
- [STC ST00030IB](https://openairdocs.org/stc/ST00030IB): Installation of Test Tech ELT. APTOZ EHF
- [STC ST03885AT](https://openairdocs.org/stc/ST03885AT): Installation of an Avionica, Inc. avCM Cellular Module. Aircraft Systems and Manufacturing Inc
- [STC ST04559CH](https://openairdocs.org/stc/ST04559CH): Installation of L3Harris Aviation Products SRVIVR25 Model 7100 Cockpit Voice Recorder (CVR) System. Acron Aviation Inc
- [STC ST03472NY](https://openairdocs.org/stc/ST03472NY): Installation of the Cabin LED Lighting. Avmax Aviation Services Inc
- [STC ST02472AT](https://openairdocs.org/stc/ST02472AT): Installation of a mini Quick Access Recorder (QAR) model MKI, MKII, or MKIII. Aircraft Systems and Manufacturing Inc
- [STC ST03795NY](https://openairdocs.org/stc/ST03795NY): Installation of the TB44 Lithium-Ion Battery System. Avmax Aviation Services Inc
- [STC ST00079IB](https://openairdocs.org/stc/ST00079IB): Integration of Halon-free Portable Fire Extinguisher HAFEX. UMLAUT ENGINEERING GMBH
- [STC ST01909NY](https://openairdocs.org/stc/ST01909NY): Installation of Hawker 9750W0370-6 (24V 43Ah) sealed lead-acid batteries. Securaplane Technologies Inc
- [STC ST02028WI](https://openairdocs.org/stc/ST02028WI): Installation of Bighorn CASEVAC Interior System. Bighorn Airways Inc
- [STC ST03065NY](https://openairdocs.org/stc/ST03065NY): The installation of Dual Universal UNS-1F Flight Management System WAAS Up-grade. Field Aviation East Limited
- [STC ST00215IB](https://openairdocs.org/stc/ST00215IB): Installation of saf-Tglo ECO Photoluminescent Aisle Path Marking Systems. STG AEROSPACE GERMANY GmbH
- [STC ST03424CH](https://openairdocs.org/stc/ST03424CH): Certification of Automatic Dependent Surveillance - Broadcast (ADS-B) Out System with Rockwell Collins TDR-94/-94D Transponders. CMD Flight Solutions LLC
- [STC ST02311AT](https://openairdocs.org/stc/ST02311AT): Installation of Saf-T-Glo Inc photoluminescent floor proximity emergency escape path marking system (FPEEPMS). STG Aerospace Inc
- [STC ST04562NY](https://openairdocs.org/stc/ST04562NY): Installation of saf-Tglo® SuperSeal UltraLite-X (SSUL-X) Photoluminescent Floor Proximity Emergency Escape Path Marking Systems. STG AEROSPACE GERMANY GmbH
- [STC ST00109IB](https://openairdocs.org/stc/ST00109IB): Installation of the Flight Compartment Stowage Box. Infinion Certification Engineering Inc
- [STC ST04788NY](https://openairdocs.org/stc/ST04788NY): Installation of the Terrain Awareness and Warning System. Mid Canada Mod Center
- [STC ST00098IB](https://openairdocs.org/stc/ST00098IB): Introduction of ADS-B Out. STC Twenty One Limited
- [STC ST00886NY](https://openairdocs.org/stc/ST00886NY): Installation of Flight Deck Manual Stowage Box, in accordance with Aero Consulting Services Modification Data Summary Number B78600, Revision H, dated November 9, 2006, or later TCCA approved revision. B/E Aerospace Limited
- [STC ST00015NY](https://openairdocs.org/stc/ST00015NY): Installation of a Sundstrand Turbomach T-62T-40C7B gas turbine auxiliary power unit with a Lear Siegler Model 23088-002 DC starter-generator. Avmax Aviation Services Inc
- [STC ST01689WI](https://openairdocs.org/stc/ST01689WI): Installation of Crane Aerospace & Electronics SmartStem Wireless Tire Pressure Sensing System. ELDEC Corporation
- [STC SA1220NW](https://openairdocs.org/stc/SA1220NW): Installation of Universal flight data recorder. Honeywell International Inc
- [STC SA2916SO](https://openairdocs.org/stc/SA2916SO): Installation of dual TRA-67 Mode S transponder system. Honeywell International Inc
- [STC SA2917SO](https://openairdocs.org/stc/SA2917SO): Installation of CAS-81 TCAS II system. Honeywell International Inc
- [STC ST04667NY](https://openairdocs.org/stc/ST04667NY): Installation of the Honeywell MK VIII Enhanced Ground Proximity Warning System (EGPWS) Override Control. Field Aviation East Limited
- [STC SA9086SC-D](https://openairdocs.org/stc/SA9086SC-D): Recore of Hamilton Standard Heat Exchangers 778683-2 for Installation on deHavilland DHC-8 Series Aircraft and 778683-2 for Installation on Fokker F27 Mark 050 Aircraft, in accordance with Honeywell LORI Sealed Drawing List SDL3545-1, Revision C, dated 11 October 2005 or later FAA approved revision. Honeywell International Inc
- [STC SA9080SC-D](https://openairdocs.org/stc/SA9080SC-D): Replace 30E94-2 Sensing Element in Janitrol Valve 45E04-1 used on DHC-8 Oil Coolers 28E99-6 and 28E99-7 in accordance with Honeywell LORI Specification LR 0201-117 as reflected on Honeywell LORI Sealed Drawing List SDL3709-1, Revision A, dated 11 October 2005 or later FAA approved revision. Honeywell International Inc
- [STC ST04652NY](https://openairdocs.org/stc/ST04652NY): Installation of the ACSS TCAS 7.1. Avmax Aviation Services Inc
- [STC ST02722SE](https://openairdocs.org/stc/ST02722SE): Installation of LT-4098 series Integrated LED Display Panel and/or associated LT-2201 series LED Pushbutton Switches. Luma Technologies LLC
- [STC ST03261NY](https://openairdocs.org/stc/ST03261NY): Installation of Dual Universal UNS-1E Flight Management System WAAS Up-grade. Field Aviation East Limited
- [STC ST04177AT](https://openairdocs.org/stc/ST04177AT): Installation of a Talon Aerospace LED Replacement General Purpose Lamps. Aaxico Technical Services Inc
- [STC ST02448SE](https://openairdocs.org/stc/ST02448SE): Installation of a Supplemental Lighting System. Aviation Specialties Unlimited Inc
- [STC ST00782LA](https://openairdocs.org/stc/ST00782LA): Installation of Chadwick Helmuth Propeller Balance Monitoring System (Vibration Management System II, VMS II). Diagnostic Solution International LLC
- [STC ST01226NY](https://openairdocs.org/stc/ST01226NY): Installation of Environmental Control System Performance Improvement Modification. Cascade Aerospace Inc
- [STC ST10977SC](https://openairdocs.org/stc/ST10977SC): Installation of Dual Universal Avionics Flight Management Systems (FMS) with Global Positioning System (GPS). DAC International Inc
- [STC ST04480NY](https://openairdocs.org/stc/ST04480NY): Installation of the Traffic Collision Avoidance System (TCAS) II Version 7.1 and Elementary Surveillance (ELS) Transponder Upgrade. Genesys Certification Services Inc
- [STC ST02729NY](https://openairdocs.org/stc/ST02729NY): Sky Connect Tracking System to be installed. Honeywell International Inc
- [STC ST04449NY](https://openairdocs.org/stc/ST04449NY): Conversion of DHC-8-102/-103/-106 from passenger carrying aircraft into Package Freighter with a Class E Cargo Compartment. Voyageur Aerotech Inc
- [STC ST04445NY](https://openairdocs.org/stc/ST04445NY): Installation of the Collins TDR-94D Transponder / Traffic Collision Avoidance System (TCAS) 4100 Upgrade. Mid Canada Mod Center
- [STC ST02635LA](https://openairdocs.org/stc/ST02635LA): Modification to replace the existing Mode S Transponder system with the ACSS NXT-600 Mode S Transponder with ADS-B Out. Aviation Communication and Surveillance Systems (ACSS) LLC
- [STC SA01452CH](https://openairdocs.org/stc/SA01452CH): Installation of an air ambulance conversion kit. Med-Pac Inc
- [STC ST04372NY](https://openairdocs.org/stc/ST04372NY): Installation of saf-Tglo® SSUL23 Photoluminescent Aisle Path Marking System. STG Aerospace Ltd
- [STC ST01900WI](https://openairdocs.org/stc/ST01900WI): Heated (LH) Side Canopy Window Assembly replacement installation. Lee Aerospace Inc
- [STC ST04344NY](https://openairdocs.org/stc/ST04344NY): Installation of the Universal Avionics EFI-890R MFD. Avmax Aviation Services Inc
- [STC ST04340NY](https://openairdocs.org/stc/ST04340NY): Installation of TCAS 7.1 (ACAS II) upgrade of Prior Existing TCAS 7.0. Scandinavian Avionics Design ApS

All 151: https://openairdocs.org/aircraft/N807EX/stcs.md

## Related

- Other Boeing DHC-8-102 aircraft: https://openairdocs.org/model/boeing-dhc-8-102/aircraft.md
- The Pratt & Whitney Canada PW120 engine: https://openairdocs.org/engine/pratt-whitney-canada-pw120.md

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