# N367PH: 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: 511
- Year built: 1998
- Type: Fixed wing multi engine
- Engine type: Turbo-prop
- Airworthiness: Standard, transport
- Airworthiness date: December 2, 1998
- Certificate issued: November 19, 2024
- Expires: November 30, 2031
- Mode S code: A4279A
- Registered owner: [Bank Of Utah Trustee](https://openairdocs.org/faa-owner/BANK%20OF%20UTAH%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 is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=367PH
- Page: https://openairdocs.org/aircraft/N367PH

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/N367PH/ads.md

## Information bulletins (advisory)

None matched.

## NTSB investigations (1)

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 ERA09LA529](https://openairdocs.org/ntsb/ERA09LA529), Aug 29, 2009: Bombardier DHC-8-202 (N367PH), Sterling, VA, substantial damage. Probable cause: Undetermined.

## 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 20160221001749I](https://openairdocs.org/incident/20160221001749I), Feb 21, 2016: Bombardier Inc DHC-8-202 (N367PH), Dulles, VA, No damage. On 02/21/2016, at approximately 13:20 EST, a commutair DHC-8-202 aircraft flying as united express flight 4944 experienced a left engine failure and associated…
- [Incident 20160210001739I](https://openairdocs.org/incident/20160210001739I), Feb 10, 2016: Bombardier Inc DHC-8-202 (N367PH), Latham, NY, No damage. On 2/10/2016, at approximately 0855 EST, a commutair DHC-8-202 aircraft while flying as united express flight 4775, on departure from Albany international(alb)…
- [Incident 20021119033789I](https://openairdocs.org/incident/20021119033789I), Nov 19, 2002: Dhav DHC8202 (N367PH), Portland, OR. (-23) Horizon air flight 2056 rdm to sea diverted to Portland or. When they experienced smoke in cabin and cockpit. Maintenance at Portland or. Ran both…
- [Incident 20020107002819I](https://openairdocs.org/incident/20020107002819I), Jan 7, 2002: Dhav DHC8202 (N367PH), Seattle, WA. (-23) On flight 2331 from lewiston Idaho to Seattle Washington crew noted noise and vibration on approach to seatac. On postflight inspection crew noted that…

## Service difficulty reports (245, 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 A8ZR201809121005](https://openairdocs.org/sdr/A8ZR201809121005), Jul 19, 2018: SKIN. GOUGED. ACCOMPLISHED RE-SKIN ON AFT BAGGAGE DOOR UPPER SECTION THAT MEASURES 5.7" X 49.70" FOR GOUGES IN SKIN REF RD 8-52-029 ISSUE 2 DATED 2014-06-05.
- [SDR A8ZR20180911002](https://openairdocs.org/sdr/A8ZR20180911002), Jul 2, 2018: STRUCTURE. DENTED. ACCOMPLISHED DOUBLER REPAIR AT STA 315.80 & BETWEEN S30S AND S31S FOR DENT WITH CREASE REF EA 45-2018-080 REV ORIGINAL ISSUE DATED 06/20/2018.
- [SDR A8ZR20180911004](https://openairdocs.org/sdr/A8ZR20180911004), Jun 20, 2018: STRUCTURE. DENTED. ACCOMPLISHED DOUBLER REPAIR AT STA 213.8 & BETWEEN S16S AND S17S FOR DENT REF EA 48-2018-042 REV ORIGINAL ISSUE DATED 06/20/2018.
- [SDR A8ZR20180911001](https://openairdocs.org/sdr/A8ZR20180911001), Jun 6, 2018: TAIL CONE. DELAMINATED. ACCOMPLISHED COMPOSITE REPAIR ON LWR TAILCONE FWD AT TAIL BUMPER FOR DELAMINATION STA X806 & Z130.43 REF SRM 53-70-28 REV 6 DATED SEP 17, 2017.
- [SDR JJBA20171227004](https://openairdocs.org/sdr/JJBA20171227004), Dec 27, 2017: DOOR SILL. CORRODED. CORROSION FOUND ON THE AIR STAIR DOOR SILL. STRUCTURES TO ACCESS. AIR STAIR DOOR SILL BLENDED, TREATED AND PRIMED IAW 51-20-11 BLENDING, SRM 51-20-16 ALODINE AN
- [SDR JJBA20171020008](https://openairdocs.org/sdr/JJBA20171020008), Oct 20, 2017: LAMP. INOPERATIVE. FWD OVERHEAD EMERGENCY LIGHTS INOPERATIVE. . R & R THE LAMPS IAW AMM 33-00-00. OPS CHECKED GOOD.
- [SDR JJBA20170720024](https://openairdocs.org/sdr/JJBA20170720024), Jul 20, 2017: POWER SUPPLY. INOPERATIVE. CEILING EMERGENCY LIGHTS AT 1 AND 3 INOPERATIVE. R & R THE NR 3 BATTERY POWER UNIT, R & R NR 3 AND 6 EMERGENCY LIGHT BATTERY PACKS, OPS CHECKED.
- [SDR JJBA20170711017](https://openairdocs.org/sdr/JJBA20170711017), Jul 11, 2017: BATTERY PACK. INOPERATIVE. FIRST AND THIRD EMERGENCY OVERHEAD LIGHTS ARE INOPERATIVE. R & R THE BATTERY PACK. OPS CHECKED GOOD.
- [SDR JJBA20170701002](https://openairdocs.org/sdr/JJBA20170701002), Jul 1, 2017: POWER SUPPLY. INOPERATIVE. AFT & FWD CENTER AISLE EMERGENCY LIGHT INOPERATIVE. R & R POWER SUPPLY PS3. OPS CHECKED GOOD. NO DEFECTS NOTED AT THIS TIME.
- [SDR JJBA20170616012](https://openairdocs.org/sdr/JJBA20170616012), Jun 16, 2017: CONDITIONER. INOPERATIVE. AUTOFEATHER ARM REMAINS ILLUMINATED WHEN SELECTED OFF. R & R THE NR 2 TSCU. PERFORMED OPS CHECK OF AUTO FEATHER SYSTEM. OPS CHECKED SAT. REMOVED THE NR 1 TSCU F
- [SDR JJBA20170615011](https://openairdocs.org/sdr/JJBA20170615011), Jun 15, 2017: BATTERY PACK. DISCHARGED. EMERGENCY LIGHTS INOPERATIVE. SWITCH WAS FOUND IN THE ARM POSITION. R & R THE BATTERY PACK, OPS CHECKED SAT.
- [SDR JJBA20170206005](https://openairdocs.org/sdr/JJBA20170206005), Feb 6, 2017: DOOR. LACK OF LUBE. MAIN CABIN DOOR BINDING AND WOULD NOT OPEN. CLEANED AND LUBED. OPS CHECKED GOOD.
- [SDR JJBA20170120016](https://openairdocs.org/sdr/JJBA20170120016), Jan 20, 2017: LIGHT. NOT REPORTED. EMERGENCY LIGHT OVER CABIN DOOR HALF ILL. R & R THE BULBS, OPS CHECK SAT.
- [SDR JJBA20161228026](https://openairdocs.org/sdr/JJBA20161228026), Dec 28, 2016: BULB. INOPERATIVE. EMERGENCY LIGHT ABOVE CABIN DOOR INOPERATIVE. R & R THE BULB. OPS CHECKED GOOD.
- [SDR JJBA20161120025](https://openairdocs.org/sdr/JJBA20161120025), Nov 20, 2016: WINDSHIELD. CRACKED. FO`S WINDSHIELD CRACKED IN FLIGHT. DECLARED AN EMERGENCY AND DIVERTED. R & R THE WINDSHIELD AND PERFORMED AN OPS CHECK FOR THE WINDOW HEAT. OPS CHECKED GOOD. NO
- [SDR JJBA20161111019](https://openairdocs.org/sdr/JJBA20161111019), Nov 11, 2016: STRUT. FAILED. NR 2 PROPELLER OVERSPEED INFLIGHT. R & R THE NR 2 ENGINE SPRING STRUT.
- [SDR JJBA20161106010](https://openairdocs.org/sdr/JJBA20161106010), Nov 6, 2016: PIN. UNSECURE. EMERGENCY EXIT LIGHT NEXT TO FA SEAT NOT ILLUMINATING. FOUND PIN IN CONNECTOR NOT SECURE. SECURED WIRE IN CONNECTOR. OPS CHECK GOOD.
- [SDR JJBA20160930015](https://openairdocs.org/sdr/JJBA20160930015), Sep 30, 2016: SIGN. UNSECURE. EMERGENCY EXIT SIGN OVER MAIN CABIN DOOR FELL DOWN. RE-SECURED EXIT LIGHT ASSEMBLY. OPS CHECK SAT.
- [SDR JJBA20160406009](https://openairdocs.org/sdr/JJBA20160406009), Apr 6, 2016: FCU. MALFUNCTIONED. AFTER DE-ICING ON STARTUP THE NR 1 ENG OVER TORQUE TO 130%. R & R NR 1 FUEL CONTROL UNIT, FUEL PUMP PROP CONTROL UNIT & NR 1 ECU. FUEL PUMP PN 5008269J, SN 2720
- [SDR JJBA20160210002](https://openairdocs.org/sdr/JJBA20160210002), Feb 10, 2016: TSCU. FAILED. ON CLIMB OUT AT 400 - 500 FEET, THE NR 1 ENG FEATHERED UNCOMMANDED. LOST ALL TORQUE. THE CREW RAN THE CHECKLIST & SHUTDOWN THE ENG. INSPECTED THE NR 1 ENG WIRE 
- [SDR JJBA20150802001](https://openairdocs.org/sdr/JJBA20150802001), Aug 2, 2015: SMOKE DETECTOR. FAULTY. BAGGAGE SMOKE WARNING CAUTION CONTINUOUSLY ILLUMINATES & WILL NOT RESET. DEFERRED IAW MEL. R & R BOTH BAGGAGE COMPARTMENT SMOKE DETECTORS.
- [SDR JJBA20150528011](https://openairdocs.org/sdr/JJBA20150528011), May 28, 2015: BATTERY. INOPERATIVE. EMERGENCY BATTERY INOPERABLE. R & R EMER BATTERIES.
- [SDR JJBA20150525009](https://openairdocs.org/sdr/JJBA20150525009), May 25, 2015: BATTERY. NOT SEATED. EMERGENCY EXIT LIGHT OVER MAIN CABIN DOOR WILL NOT ILLUMINATE. RESEATED EMER BATTERIES.
- [SDR JJBA20150210014](https://openairdocs.org/sdr/JJBA20150210014), Feb 10, 2015: FLAP. DAMAGED. LEFT INBD ROLL SPOILER INBD & OTBD AFT CORNERS RUBBING ON OTBD FLAP. REPAIR OTBD FLAP.
- [SDR JJBA20150210013](https://openairdocs.org/sdr/JJBA20150210013), Feb 10, 2015: FLAP. GOUGED. RIGHT OTBD FLAP ON THE UPPER INBD SIDE HAS GOUGES. REPAIRED FLAP ON UPPER SIDE IAW RD 857-1022.
- [SDR JJBA20150131013](https://openairdocs.org/sdr/JJBA20150131013), Jan 31, 2015: CONNECTOR. LOOSE. CABIN OVERHEAD EMER LIGHTS 1 & 3 WILL NOT ILLUMINATE. FOUND CONNECTORS LOOSE ON PS2 EMER BATTERY. RE-SEATED CONNECTOR. OPERATIONS CHECK SATISFACTORY.
- [SDR JJBA20141205004](https://openairdocs.org/sdr/JJBA20141205004), Dec 5, 2014: LIGHT. INOPERATIVE. REAR AFT FLOOR EMER LIGHT INOPERABLE. R & R AFT REAR EMER FLOOR LIGHT BULB.
- [SDR JJBA20141205003](https://openairdocs.org/sdr/JJBA20141205003), Dec 5, 2014: WIRE. BROKEN. RED EMER LIGHT STRIP ON FLOOR AT SEAT 2C, D INOPERATIVE. FOUND BROKEN WIRE ON FWD PS2, SECURED.
- [SDR JJBA20141105001](https://openairdocs.org/sdr/JJBA20141105001), Nov 5, 2014: TORQUE LINK. DEFECTIVE. EXCESSIVE VIBRATION FELT IN TIRES ON TOUCH DOWN. R & R NR 2 MLG UPPER & LOWER TORQUE LINKS & PINS.
- [SDR JJBA20141016006](https://openairdocs.org/sdr/JJBA20141016006), Oct 16, 2014: WARNING SYSTEM. ACTIVATED. CABIN PRESS LIGHT ILLUMINATED ON DESCENT. DECLARED AN EMER TO DESCEND. DEFERRED IAW MEL.
- [SDR JJBA20141011004](https://openairdocs.org/sdr/JJBA20141011004), Oct 11, 2014: CONNECTOR. UNSECURE. EMERGENCY LIGHT AT 23C NOT ILLUMINATING. SECURED CONNECTOR.
- [SDR JJBA20140212006](https://openairdocs.org/sdr/JJBA20140212006), Feb 12, 2014: LIGHT. INOPERATIVE. CEILING EMERGENCY LIGHTS WILL NOT ILLUMINATE, HEATED CABIN.
- [SDR JJBA20140209005](https://openairdocs.org/sdr/JJBA20140209005), Feb 9, 2014: CONNECTOR. DISCONNECTED. EXIT SIGN BY FLIGHT ATTENDANT`S JUMP SEAT DOES NOT LIGHT UP. FOUND ELEC PLUG BEHIND LIGHT ASSEMBLY LOOSE, RECONNECTED.
- [SDR JJBA20140122009](https://openairdocs.org/sdr/JJBA20140122009), Jan 22, 2014: BATTERY. DISCHARGED. ONE FWD & SECOND TO LAST EMERGENCY LIGHT WILL NOT ILLUMINATE. CHARGED BATTERIES.
- [SDR JJBA20140121011](https://openairdocs.org/sdr/JJBA20140121011), Jan 21, 2014: BATTERY. DISCHARGED. EMERGENCY LIGHT AT RT FWD EMERGENCY EXIT & MAIN PAX DOOR OVERHEAD INOPERABLE. R & R EMERGENCY LIGHT BATTERIES PS1 & PS2 IRW DASH Q200 AMM 33-51-00.
- [SDR JJBA20131228009](https://openairdocs.org/sdr/JJBA20131228009), Dec 28, 2013: STRAP. BROKEN. EMERGENCY LIGHT STRAP BROKEN ON FLIGHT ATTENDANT`S FLASHLIGHT. R & R EMERGENCY FLASHLIGHT & STRAP.
- [SDR JJBA20131228008](https://openairdocs.org/sdr/JJBA20131228008), Dec 28, 2013: FLASHLIGHT. DEFECTIVE. RED LIGHT NOT BLINKING ON EMERGENCY FLASHLIGHT WHEN CHARGED. R & R FLASHLIGHT, OPERATIONS CHECKED SATISFACTORY.
- [SDR JJBA20131021006](https://openairdocs.org/sdr/JJBA20131021006), Oct 21, 2013: CONNECTOR. DISCONNECTED. EMERGENCY LIGHT BY AIRSTAIR DOOR NOT TESTING. CONNECTED CONNECTOR 351J19. OPS CHECKED GOOD.
- [SDR JJBA20130916009](https://openairdocs.org/sdr/JJBA20130916009), Sep 16, 2013: BOLT. LOOSE. PASSENGER DOOR WARNING LIGHT ILLUMINATED IN FLIGHT. TIGHTENED UPPER FWD AND AFT DOOR SHELL BOLTS. SEALED BOLT HEADS. PRESSURIZATION AND OPS CHECKED GOOD.
- [SDR JJBA20130702004](https://openairdocs.org/sdr/JJBA20130702004), Jul 2, 2013: SWITCH. INOPERATIVE. WHEN PILOT SELECTED EMERGENCY LIGHTS TO ARM AND F/A CYCLES TEST, THE LIGHTS REMAINED ILLUMINATED. REPLACED F/A EMERGENCY LIGHT SWITCH, OPS CHECKED SATISFACTORY.
- [SDR JJBA20130701002](https://openairdocs.org/sdr/JJBA20130701002), Jul 1, 2013: LIGHT. UNKNOWN. CREW REPORTED EMERGENCY LIGHTS ILLUMINATING IN FLIGHT. MX GROUND RAN AND PERFORMED AN OPS CHECK. ISSUE COULD NOT BE DUPLICATED.
- [SDR JJBA20130630034](https://openairdocs.org/sdr/JJBA20130630034), Jun 30, 2013: LIGHT. INOPERATIVE. DURING PREFLIGHT CREW REPORTED A SECTION OF THE FLOOR EMERGENCY LIGHTING WAS INOPERATIVE. MX REPLACED THE SECTION OF STRIP AND ALL OPERATIONAL TEST PRODUCED SAT
- [SDR JJBA20130527018](https://openairdocs.org/sdr/JJBA20130527018), May 27, 2013: HANDLE. LOOSE. THE BOTTOM HANDLE TO THE RT EMERGENCY EXIT DOOR CAME OFF. THE MECHANIC RESEATED THE HANDLE.
- [SDR JJBA20130504012](https://openairdocs.org/sdr/JJBA20130504012), May 4, 2013: BATTERY. INOPERATIVE. DURING PREFLIGHT CREW REPORTED THE FWD FLOOR PATH EMERGENCY RED LIGHTS WERE INOPERATIVE. MX SWAPPED BATTERY POSITIONS AND THE PROBLEM WAS CORRECTED.
- [SDR JJBA20130331016](https://openairdocs.org/sdr/JJBA20130331016), Mar 31, 2013: SEAL. LEAKING. DURING CRUISE CREW REPORTED A NR 1 OIL PRESSURE LOW LIGHT ILLUMINATED. THE OIL PRESSURE GAUGE WAS ERRATIC. DECLARED AN EMERGENCY AND MADE AN UNEVENTFUL LANDING 
- [SDR JJBA20130131021](https://openairdocs.org/sdr/JJBA20130131021), Jan 31, 2013: PUMP. FAILED. DURING FLIGHT, CREW REPORTED THE NR 2 ENG HYD PUMP CAUTION ILLUMINATED. THE NR 2 HYD PRESSURE SHOWED NO PRESSURE. GROUND MX CREW R & R THE ENGINE DRIVEN HYD PUM
- [SDR JJBA20130130018](https://openairdocs.org/sdr/JJBA20130130018), Jan 30, 2013: TRIM SYSTEM. BINDING. DURING CRUISE, CREW REPORTED THAT THE AUTO PILOT MISTRIM NOSE DOWN LIGHT ILLUMINATED AND THE AUTO PILOT DISENGAGED MANUALLY AND THE TRIM WAS REPORTED TO BE JAMM
- [SDR JJBA20130118011](https://openairdocs.org/sdr/JJBA20130118011), Jan 18, 2013: ENGINE. POWER LOSS. ON FINAL APPROACH, WHEN THE POWER LEVER WENT TO FLIGHT IDLE THE NR 2 ENGINE GAVE 20 PERCENT TORQUE. MX CREW RAN THE ENGINES AND DID NOT OBSERVE THE PROBLEM. ALL
- [SDR JJBA2012201207230](https://openairdocs.org/sdr/JJBA2012201207230), Jul 23, 2012: BATTERY PACK. INOPERATIVE. DURING PRE-FLIGHT CREW NOTICED THE OVERHEAD EMERGENCY CEILING LIGHTS AT POSITION 1 & 3 WERE INOPERATIVE. GROUND MX CREW R & R THE EMERGENCY LIGHT BATTERIES. AN 
- [SDR JJBA20120429012](https://openairdocs.org/sdr/JJBA20120429012), Apr 29, 2012: BATTERY PACK. INOPERATIVE. DURING PRE-FLIGHT CREW NOTICED THE FWD FLOOR EMERGENCY LIGHT STRIP WAS INOPERATIVE. GROUND MX CREW R & R THE PS6 BATTERY SUPPLY UNIT. A SATISFACTORY OPS CHECK W

All 245: https://openairdocs.org/aircraft/N367PH/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/N367PH/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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