# N363PH: 1998 Bombardier DHC-8-202

- Status: Valid registration
- Airframe: [Bombardier DHC-8-202](https://openairdocs.org/model/bombardier-dhc-8-202) (registry code 1390007, 40 seats)
- Engine: [Pratt & Whitney Canada PW123](https://openairdocs.org/engine/pratt-whitney-canada-pw123) (registry code 52129)
- 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: 520
- Year built: 1998
- Type: Fixed wing multi engine
- Engine type: Turbo-prop
- Airworthiness: Standard, transport
- Airworthiness date: July 22, 1998
- Certificate issued: October 13, 2011
- Expires: October 31, 2027
- Mode S code: A418BE
- Registered owner: [Wells Fargo Trust Co Na Trustee](https://openairdocs.org/faa-owner/WELLS%20FARGO%20TRUST%20CO%20NA%20TRUSTEE)
- Location: [Columbia, MD](https://openairdocs.org/faa-place/MD/Columbia)
- Owner type: Corporation
- Owner's area on the map: 39.2060° N, 76.8282° W: Placed by OpenAirDocs at the center of ZIP code 21045, 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=363PH
- Page: https://openairdocs.org/aircraft/N363PH

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): 130 in force

### Matched by airframe (Bombardier DHC-8-202)

- [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 2022-15-08](https://openairdocs.org/ad/2022-15-08): Information systems · Airbus A318-111, A318-112, A319-111 and 49 more. Effective Aug 12, 2022
- [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 2013-14-09](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 2011-24-10](https://openairdocs.org/ad/2011-24-10): Equipment/Furnishings · Bombardier DHC-8-201 and DHC-8-202. Effective Dec 16, 2011
- [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 2010-19-02](https://openairdocs.org/ad/2010-19-02): Fuel · Bombardier DHC-8-201, DHC-8-202, DHC-8-301 and 2 more. Effective Oct 18, 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

### Matched by engine (Pratt & Whitney Canada PW123)

- [AD 2013-15-08](https://openairdocs.org/ad/2013-15-08): First-stage PT blades · Pratt & Whitney Canada PW118A, PW118B, PW119B and 15 more. Effective Sep 17, 2013
- [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 2004-20-01](https://openairdocs.org/ad/2004-20-01): Bypass valve cover · Pratt & Whitney Canada PW123, PW123AF, PW123B and 10 more. Effective Nov 5, 2004
- [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 94-11-11](https://openairdocs.org/ad/94-11-11): Intercompressor Case · Pratt & Whitney Canada PW118A, PW123, PW124B and 2 more. Effective Jul 25, 1994
- [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 92-17-14](https://openairdocs.org/ad/92-17-14): Fuel Pump · Pratt & Whitney Canada PW123, PW124B, PW125B and 1 more. Effective Nov 18, 1992
- [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 91-24-03](https://openairdocs.org/ad/91-24-03): Turbomachinery Magnetic Chip Detector · Pratt & Whitney Canada PW123, PW124B, PW125B and 1 more. Effective May 26, 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

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

- [AD 2019-20-03](https://openairdocs.org/ad/2019-20-03) (historical): Information systems · Airbus A340-312, A340-313, A318-111 and 48 more. Effective Nov 19, 2019
- [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 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 136: https://openairdocs.org/aircraft/N363PH/ads.md

## Information bulletins (advisory)

None matched.

## NTSB investigations (2)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB ENG15IA024](https://openairdocs.org/ntsb/ENG15IA024), Jun 5, 2015: Bombardier DHC 8 (N363PH), Windsor Locks, CT, incident, minor damage. Probable cause: The arcing failure of the windshield heat power wire on the right windshield due to unknown reasons. Contributing to the severity of the fire was the lack of training or guidance provided to the crew…
- [NTSB SEA05LA184](https://openairdocs.org/ntsb/SEA05LA184), Aug 29, 2005: Bombardier DHC-8-202 (N363PH), Portland, OR, substantial damage. Probable cause: The failure of the flightcrew of the other airplane to maintain clearance while taxiing.

## FAA accident and incident reports (6)

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 20150621007989I](https://openairdocs.org/incident/20150621007989I), Jun 21, 2015: Bombardier Inc DHC-8-202 (N363PH), Canandaigua, NY, No damage. Canandaigua airport, NY (D38):commutair flight 770, a DH8, diverted and landed on runway 31 due to a fire in the lavatory and smoke in the cockpit. The pilot…
- [Incident 20150605008489I](https://openairdocs.org/incident/20150605008489I), Jun 5, 2015: Bombardier Inc DHC-8-202 (N363PH), Windsor Locks, CT, Minor damage. On June 5, 2015, about 1215 eastern daylight time (EDT), a Bombardier DHC-8-202 airplane, N363PH, had an in-flight cockpit fire during approach into Bradley…
- [Incident 20080918850919I](https://openairdocs.org/incident/20080918850919I), Sep 18, 2008: Dhav DHC8202 (N363PH), IN, No damage. (-23) An air carrier aircraft on an IFR flight plan at 14,000 feet MSL responded to a terminal collision advisory system (TCAS) resolution advisory (ra)…
- [Accident 20050829019919A](https://openairdocs.org/incident/20050829019919A), Aug 29, 2005: Dhav DHC8202 (N363PH), Portland, OR, Substantial damage. (-23) While taxiing for takeoff NWA5 struck HORIZON66. The impact resulted in substantial damage to the horizon DHC-8 aircraft. Horizon 66 was holding short of…
- [Incident 20010129000859I](https://openairdocs.org/incident/20010129000859I), Jan 29, 2001: Dhav DHC8202 (N363PH), Seattle, WA, Minor damage. (-23) Noise heard at rotation, notified enroute by yakima (ykm) tower metal had separated from aircraft (a/c). On descent in Seattle/Tacoma (sea) second noise…
- [Incident 20000223016089I](https://openairdocs.org/incident/20000223016089I), Feb 23, 2000: Dhav DHC8202 (N363PH), Redding, CA. (-23)Enroute @ flight level 210 elevator trim frozen. Trim was operable after landing. Maintenance lubed both screw jack assemblies.

## Service difficulty reports (206, 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 A8ZR20180924002](https://openairdocs.org/sdr/A8ZR20180924002), Jul 18, 2018: LIGHT. DEFECTIVE. RT FWD EMERGENCY EXIT DOOR, LT & RT UNDER WING EMERGENCY EXIT DOOR BETA LIGHTS P/N DSC543-1 FAILED BRIGHTNESS CHECK REF TASK CARD 3350/02 AND REPLACED REF AMM 3
- [SDR JJBA20171003002](https://openairdocs.org/sdr/JJBA20171003002), Oct 3, 2017: BULB. INOPERATIVE. AUTOFEATHER SELECT LIGHT EXTINGUISHED DURING TAKEOFF, CREW ABORTED AND RETURNED TO GATE. R & R TWO BULBS ON THE PROPELLER SELECT BUTTON. RAN ENGINGES AND TESTED
- [SDR JJBA20170925028](https://openairdocs.org/sdr/JJBA20170925028), Sep 18, 2017: SENSOR. MALFUNCTIONED. IN FLIGHT, AMBER AND RED NOSE GEAR LIGHTS ILLUMINATED AND GEAR COULD BE HEARD CYCLING. PULLED THE PSEU FAULT CODES AND WORKING WITH THE MANUFACTURER FOR TROUBLE
- [SDR JJBA20170826025](https://openairdocs.org/sdr/JJBA20170826025), Aug 26, 2017: SENSOR. OUT OF POSITION. NOSE GEAR DOOR LIGHT CYCLED DURING CLIMB AND HEARD THE DOOR OPEN AND CLOSE. PERFORMED GVI OF NLG DOOR SENSOR WIRING AND SENSOR AND SENSOR CONNECTOR. WIRING IS I
- [SDR JJBA20170810011](https://openairdocs.org/sdr/JJBA20170810011), Aug 10, 2017: SKIN. DAMAGED. RIGHT ENGINE LOWER COWL FOUND DAMAGED INSIDE AT AFT WALL CONE. REPLACED LOWER COWL.
- [SDR JJBA20170801005](https://openairdocs.org/sdr/JJBA20170801005), Aug 1, 2017: DOOR. CORRODED. MINOR CORROSION FOUND ON PAX DOOR SHELL. MINOR SURFACE CORROSION HAS BEEN REPAIRED.
- [SDR JJBA20170801003](https://openairdocs.org/sdr/JJBA20170801003), Aug 1, 2017: SKIN. CORRODED. CORROSION FOUND ON THE INTERIOR SKIN, BOTTOM AFT CORNER OF THE CARGO DOOR OPENING. REPAIR AS REQUIRED. CORROSION REMOVED AND AREA TREATED PRIMED AND PAINTED.
- [SDR JJBA20161101004](https://openairdocs.org/sdr/JJBA20161101004), Nov 1, 2016: BATTERY PACK. INOPERATIVE. EMERGENCY EXIT LIGHTS DO NOT TURN ON. REMOVED AND REPLACED BATTERIES.
- [SDR JJBA20161001001](https://openairdocs.org/sdr/JJBA20161001001), Oct 1, 2016: LIGHT. INOPERATIVE. EMERGENCY LIGHT NOT ILLUMINATING. R&R LIGHT.
- [SDR JJBA20160810008](https://openairdocs.org/sdr/JJBA20160810008), Aug 10, 2016: SMOKE DETECTOR. NO TEST. LAVATORY SMOKE DETECTOR WILL NOT TEST. R & R THE SMOKE DETECTOR, OPS CHECKED GOOD.
- [SDR JJBA20151218008](https://openairdocs.org/sdr/JJBA20151218008), Dec 18, 2015: BATTERY. DISCHARGED. EMERGENCY LIGHTS FLICKER ON & OFF BRIEFLY WHEN SELECTED ON BOTH FROM COCKPIT & FLIGHT ATTENDANT CONTROL PANEL. R & R EMER BATTERIES.
- [SDR JJBA20150622008](https://openairdocs.org/sdr/JJBA20150622008), Jun 22, 2015: UNKNOWN. SMOKE. UPDATE, SMOKE IN COCKPIT & CABIN. INSPECTED L/R AVIONICS & AC CB PANELS, WIRING, EQUIP, NR 1 & 2 RELAY PANELS, L/R TERMINAL BOARDS, GALLEY & LAVATORY, ASSOCIATE
- [SDR JJBA20050622008](https://openairdocs.org/sdr/JJBA20050622008), Jun 22, 2015: UNKNOWN. SMOKE. SMOKE IN COCKPIT & CABIN. INSPECTED L/R AVIONICS & AC CB PANELS, WIRING, EQUIPMENT 1 & 2 RELAY PANELS. L/R TERMINAL BOARDS, GALLEY & LAVATORY.
- [SDR JJBA20150605004](https://openairdocs.org/sdr/JJBA20150605004), Jun 5, 2015: CONTROLLER. MALFUNCTIONED. FIRST OFFICER'S TOP LT CORNER OF THE WINDSHIELD CAUGHT ON FIRE. R & R WINDSHIELD, WINDSHIELD HEAT CONTROLLER, WINDSHIELD HEAT WIRES & CONNECTIONS & UPPER SILL F
- [SDR JJBA20150422009](https://openairdocs.org/sdr/JJBA20150422009), Apr 22, 2015: SMOKE DETECTOR. FAULTY. LAVATORY SMOKE DETECTOR ACTIVATED DURING TAXI. NO EVIDENCE OF SMOKE PRESENT. R & R LAVATORY SMOKE DETECTOR.
- [SDR JJBA20150421017](https://openairdocs.org/sdr/JJBA20150421017), Apr 21, 2015: BATTERY. DISCHARGED. MOST AFT EMER LIGHT ON CEILING INOPERABLE. R & R BATTERY 3351 PS4.
- [SDR JJBA20150421016](https://openairdocs.org/sdr/JJBA20150421016), Apr 21, 2015: UNKNOWN. ODOR. LAVATORY SMOKE DETECTOR ACTIVATED & ODOR OF ELEC SMOKE PRESENT IN FLIGHT DECK DURING DESCENT. POWERED UP ALL ELEC EQUIP & PERFORMED ENG RUNS & BLEED SYS CHECK. 
- [SDR JJBA20150421008](https://openairdocs.org/sdr/JJBA20150421008), Apr 21, 2015: BATTERY. DISCHARGED. AFT CABIN EMER LIGHT INOPERABLE. R & R EMER BATTERY 3351PS4.
- [SDR JJBA20141026008](https://openairdocs.org/sdr/JJBA20141026008), Oct 26, 2014: SERVO VALVE. MALFUNCTIONED. NUMBER 2 ENG NH IS ABNORMALLY HIGH. THERE IS A LARGE SPLIT BETWEEN POWER LEVERS & ITT 85C OFF. NUMBER 2 IS HIGHER. R & R NR 2 ENG HBOV SERVO VLV & TRIMMED ENGS.
- [SDR JJBA20131104004](https://openairdocs.org/sdr/JJBA20131104004), Nov 4, 2013: BATTERY PACK. MALFUNCTIONED. ALL EMERGENCY LIGHTS COME ON THEN GO OUT. R & R ALL EMERGENCY BATTERIES.
- [SDR JJBA20130823014](https://openairdocs.org/sdr/JJBA20130823014), Aug 23, 2013: BATTERY PACK. DISCHARGED. EMERGENCY LIGHT POWER SUPPLIES DISCHARGED. R & R POWER SUPPLIES IAW AMM 33-51-00. OPS CHECKED SATISFACTORY.
- [SDR JJBA20130515001](https://openairdocs.org/sdr/JJBA20130515001), May 15, 2013: SHROUD. CRACKED. A CRACK WAS FOUND IN THE NR 1 EXHAUST FINGERNAIL PANEL 419CT. THE SHROUD WAS REPAIRED IAW A REPAIR DWG.
- [SDR JJBA20130422003](https://openairdocs.org/sdr/JJBA20130422003), Apr 22, 2013: SKIN. CRACKED. THE NR 1 LOWER ENGINE COWLING WAS FOUND WITH A FEW SMALL CRACKS AND MISSING RIVETS. THE CRACKS WERE REPAIRED AND THE RIVETS WERE REPLACED.
- [SDR JJBA20130422002](https://openairdocs.org/sdr/JJBA20130422002), Apr 22, 2013: FITTING. CRACKED. A CRACK WAS FOUND ON THE FWD CARGO DOOR TRACK FITTING DURING A HEAVY CHECK INSPECTION. THE FITTING WAS CHANGED.
- [SDR JJBA20130418012](https://openairdocs.org/sdr/JJBA20130418012), Apr 18, 2013: STRUCTURE. CORRODED. CORROSION WAS FOUND UNDER THE ATC TRANSPONDER ANTENNA.
- [SDR JJBA20130418005](https://openairdocs.org/sdr/JJBA20130418005), Apr 18, 2013: STRUCTURE. CORRODED. CORROSION WAS FOUND UNDER THE ATC TRANSPONDER ANTENNA.
- [SDR JJBA20130418004](https://openairdocs.org/sdr/JJBA20130418004), Apr 18, 2013: FAIRING. CRACKED. THE RT AILERON TIP FAIRING WAS FOUND CRACKED.
- [SDR JJBA201304160011](https://openairdocs.org/sdr/JJBA201304160011), Apr 16, 2013: ANGLE. CORRODED. CORROSION WAS FOUND ON THE LT AND RT AFT WING SPAR TO FUSELAGE CLOSING ANGLES.
- [SDR JJBA20130416006](https://openairdocs.org/sdr/JJBA20130416006), Apr 16, 2013: SEAT TRACK. CORRODED. THE RT FWD SEAT TRACK WAS FOUND CORRODED. THE SEAT TRACK WAS REPLACED.
- [SDR JJBA20130416011](https://openairdocs.org/sdr/JJBA20130416011), Apr 16, 2013: SEAT TRACK. CORRODED. MX FOUND THE RT FWD SEAT TRACK WITH CORROSION. THE SEAT TRACK WAS REPLACED.
- [SDR JJBA20130415010](https://openairdocs.org/sdr/JJBA20130415010), Apr 15, 2013: SKIN. CRACKED. A CRACK WAS FOUND IN THE SKIN OF THE TRAILING RUDDER LT SIDE CENTER TOP. THE CRACK WAS REPAIRED IAW APPROVED DATA.
- [SDR JJBA20130415008](https://openairdocs.org/sdr/JJBA20130415008), Apr 15, 2013: HINGE. CHAFED. CHAFING DAMAGE WAS FOUND ON THE UPPER VERTICAL RUDDER HINGE. THE HINGE WAS REPLACED.
- [SDR JJBA20130415007](https://openairdocs.org/sdr/JJBA20130415007), Apr 15, 2013: HINGE. CHAFED. CHAFING DAMAGE WAS FOUND ON THE VERTICAL RUDDER UPPER AND LOWER FAIL SAFE HINGES. THE CORROSION WAS TREATED IAW APPROVED DATA.
- [SDR JJBA20130206004](https://openairdocs.org/sdr/JJBA20130206004), Feb 6, 2013: BUSHING. INOPERATIVE. CREW REPORTED THAT THE LEFT MLG DOOR ANNUNCIATOR ON THE GEAR PANEL REMAINED ILLUMINATED AFTER GEAR UP CAUSING THE LANDING GEAR CAUTION LIGHT TO ILLUMINATE. GROU
- [SDR JJBA20130105001](https://openairdocs.org/sdr/JJBA20130105001), Jan 5, 2013: CONNECTOR. DISCONNECTED. DURING PRE FLIGHT CREW NOTED THAT THE CEILING EMERGENCY LIGHT AT ROW 3 WAS NOT ILLUMINATING AS REQUIRED. MX DISCOVERED THE CONNECTOR FOR THE LIGHT WAS UNPLUGGED
- [SDR JJBA20121224010](https://openairdocs.org/sdr/JJBA20121224010), Dec 24, 2012: LIGHT. INOPERATIVE. CREW OBSERVED THE FWD SECTION OF FLOOR EMERGENCY LIGHTS WAS NOT ILLUMINATING DURING A ROUTINE TEST. MX REPLACED THE LIGHT STRIP AND ALL OPS CHECKED WERE SATISFA
- [SDR JJBA20121223009](https://openairdocs.org/sdr/JJBA20121223009), Dec 23, 2012: POWER SUPPLY. FAILED. CREW OBSERVED MULTIPLE EMERGENCY FAILING TO ILLUMINATE DURING A ROUTINE TEST. MX R & R THE EMERGENCY LIGHT POWER SUPPLIES AND ALL OPS CHECKED WERE SATISFACTORY.
- [SDR JJBA20120717009](https://openairdocs.org/sdr/JJBA20120717009), Jul 17, 2012: LENS. DETACHED. DURING PREFLIGHT, CREW NOTICED THE EMERGENCY EXIT SIGN BY MAIN CABIN DOOR WAS INOPERATIVE. GROUND MX CREW FOUND THE LENS FOR THE EXIT SIGN HAD COME OFF. ATTACHE
- [SDR JJBA20120617004](https://openairdocs.org/sdr/JJBA20120617004), Jun 17, 2012: WARNING HORN. FAILED. DURING A FUNCTIONAL CHECK OF THE BETA WARNING HORN, THE MECHANIC OBSERVED AN OPS CHECK FAILURE. THE MECHANIC R & R THE BETA WARNING HORN ASSY AND PERFORMED ANOT
- [SDR JJBA20120517006](https://openairdocs.org/sdr/JJBA20120517006), May 17, 2012: BULB. INOPERATIVE. DURING PRE-FLIGHT, THE CREW NOTICED THE EMERGENCY LIGHTS IN THE CEILING BETWEEN ROWS 3 & 4 WERE INOPERATIVE. GROUND MX CREW R & R THE LIGHT BULBS. AN OPS CHECK 
- [SDR JJBA20120514005](https://openairdocs.org/sdr/JJBA20120514005), May 14, 2012: BATTERY PACK. NOT SEATED. DURING PRE-FLIGHT, CREW NOTICED THE EMERGENCY LIGHTS WERE NOT ILLUMINATING. RESEATED THE EMERGENCY LIGHT POWER SUPPLY BATTERIES AND POWERED DOWN ACFT. POWERED U
- [SDR JJBA20120430011](https://openairdocs.org/sdr/JJBA20120430011), Apr 30, 2012: LIGHT. MALFUNCTIONED. DURING PRE-FLIGHT CREW NOTICED 3 CEILING EMERGENCY LIGHTS WERE INOPERABLE. GROUND MX CREW PERFORMED AN OPS CHECK AND WERE UNABLE TO DUPLICATE THE PROBLEM. THE A
- [SDR JJBA20120310003](https://openairdocs.org/sdr/JJBA20120310003), Mar 10, 2012: POWER SUPPLY. INOPERATIVE. DURING THE PRE-FLIGHT INSPECTION, CREW NOTICED THE RED FORWARD EMERGENCY LIGHTS WERE NOT OPERATING. GROUND CREW REPLACED POWER SUPPLY UNIT PS6. OPS CHECK WAS PE
- [SDR JJBA2012022900014](https://openairdocs.org/sdr/JJBA2012022900014), Feb 26, 2012: BATTERY PACK. INOPERATIVE. DURING THE PRE-FLIGHT INSPECTION, CREW NOTICED THE RED EMERGENCY LIGHTS AT ROW 1C WERE NOT OPERATIVE. GROUND MX CREW RESEATED BATTERYS 3352 PS1/PS2. AN OPS CHEC
- [SDR JJBA2012020336301](https://openairdocs.org/sdr/JJBA2012020336301), Jan 31, 2012: BULB. INOPERATIVE. DURING TESTING PRIOR TO FLIGHT, THE CREW FOUND A FLOOR EMERGENCY LIGHT STRIP WITH 2 LIGHT BULBS INOPERATIVE. R & R THE EMERGENCY LIGHT STRIP. OPS CHECKED SATISF
- [SDR JJBA201110210011](https://openairdocs.org/sdr/JJBA201110210011), Oct 21, 2011: LIGHT. INOPERATIVE. FLIGHT CREW REPORTED THAT THE EMERGENCY LIGHTS NOT WORKING. R & R LIGHT. OPS CHECKED SATISFACTORY.
- [SDR JJBA363PH331478](https://openairdocs.org/sdr/JJBA363PH331478), Sep 22, 2011: LIGHT. MALFUNCTIONED. FLIGHT CREW REPORTED THAT THE FORWARD RED EMERGENCY LIGHT STRIP IS NOT WORKING. MX PERFORMED OPS CHECK, SATISFACTORY AND NO DEFECTS WERE NOTED.
- [SDR JJBA363PH331429](https://openairdocs.org/sdr/JJBA363PH331429), Aug 21, 2011: POWER SUPPLY. INOPERATIVE. FLIGHT CREW REPORTED EMERGENCY LIGHTS FLICKERED ON TAXI. MX CREW R & R POWER SUPPLY, PERFORMED OPS CHECK AND WAS SATISFACTORY.
- [SDR JJBA20110820001](https://openairdocs.org/sdr/JJBA20110820001), Aug 20, 2011: BULB. INOPERATIVE. MX FOUND ON A LINE CHECK F/A EMERGENCY LIGHT SWITCH BACK LIGHTING IN BOTH ON/OFF POSITIONS NOT WORKING. R & R BULB AND PERFORMED OPS CHECK. OPS CHECK WAS SATISF
- [SDR JJBA363PH331428](https://openairdocs.org/sdr/JJBA363PH331428), Aug 20, 2011: WIRE. BROKEN. FLIGHT CREW REPORTED THAT THE EMERGENCY LIGHT FLOOR LIGHT WERE FLICKERING IN FLIGHT. MX CREW REPAIRED A BROKEN WIRE AT ROW 3 OPS CHECK WAS SATISFACTORY.

All 206: https://openairdocs.org/aircraft/N363PH/reports.md

## STCs that may be installed (OpenAirDocs) (155, 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 (Bombardier DHC-8-202)

- [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 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 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 ST01255SE](https://openairdocs.org/stc/ST01255SE): Installation of a center console extended fairing. Metal Innovations Inc. dba MII Aero
- [STC ST02050NY](https://openairdocs.org/stc/ST02050NY): Installation of U.S. Customs Special Mission Modifications. Field Aviation East Limited
- [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 ST00213MC](https://openairdocs.org/stc/ST00213MC): Installation of means to disable ADS-B Out. Sierra Nevada Corporation
- [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 ST00089IB](https://openairdocs.org/stc/ST00089IB): Installation of SNC Mission Systems. Field Aviation East Limited
- [STC ST03354NY](https://openairdocs.org/stc/ST03354NY): Installation of the Dual Auxiliary Air Condintioning system. Field Aviation Company Inc
- [STC ST04783NY](https://openairdocs.org/stc/ST04783NY): Installation of the provisions for the Mark II Laser Airborne Depth Sounder (LADS) in the Standard Passenger Carrying Configuration. Field Aviation East 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 ST00428NY](https://openairdocs.org/stc/ST00428NY): 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 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 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 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
- [STC ST04324NY](https://openairdocs.org/stc/ST04324NY): Installation of the Honeywell Solid State Cockpit Voice Recorder (SSVR) system. Avmax Aviation Services Inc

All 155: https://openairdocs.org/aircraft/N363PH/stcs.md

## Related

- Other Bombardier DHC-8-202 aircraft: https://openairdocs.org/model/bombardier-dhc-8-202/aircraft.md
- The Pratt & Whitney Canada PW123 engine: https://openairdocs.org/engine/pratt-whitney-canada-pw123.md

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