# N359PH: 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: 514
- Year built: 1998
- Type: Fixed wing multi engine
- Engine type: Turbo-prop
- Airworthiness: Standard, transport
- Airworthiness date: March 27, 1998
- Certificate issued: September 21, 2023
- Expires: September 30, 2030
- Mode S code: A40789
- Registered owner: [Bighorn Airways Inc](https://openairdocs.org/faa-owner/BIGHORN%20AIRWAYS%20INC)
- Location: [Sheridan, WY](https://openairdocs.org/faa-place/WY/Sheridan)
- Owner type: Corporation
- Owner's area on the map: 44.8325° N, 106.8963° W: Placed by OpenAirDocs at the center of ZIP code 82801, within about 13 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=359PH
- Page: https://openairdocs.org/aircraft/N359PH

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/N359PH/ads.md

## Information bulletins (advisory)

None matched.

## NTSB investigations

None matched to N359PH.

## 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 20170814017969I](https://openairdocs.org/incident/20170814017969I), Aug 14, 2017: Bombardier Inc DHC-8-202 (N359PH), Albany, NY, No damage. The pilot reported the aircraft took off and encountered the #2 engine unresponsive to power lever input and experienced torque fluctuations. This lead to the…
- [Incident 20110310003429I](https://openairdocs.org/incident/20110310003429I), Mar 10, 2011: Bombardier DHC-8-202 (N359PH), Newark, NJ, No damage. During climb, the aircraft experienced a left wing down aileron trim tab runaway. Aircraft did not respond to right wing down selection. The crew performed the…
- [Incident 20000209019549I](https://openairdocs.org/incident/20000209019549I), Feb 9, 2000: Dhav DHC8202 (N359PH), Seattle, WA. (-23)Aileron trim was observed by the crew to be moving left without any crew input. Crew pulled circuit beaker and continued the flight without further…

## Service difficulty reports (281, 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 A8ZR20180920001](https://openairdocs.org/sdr/A8ZR20180920001), Jul 10, 2018: LIGHT. DEFECTIVE. RT FWD EMERGENCY EXIT DOOR, LT & RT UNDER WING EMERGENCY EXIT DOOR BETA LIGHTS P/N 1971001 FAILED BRIGHTNESS CHECK REF TASK CARD 3350/02 AND REPLACED REF AMM 33
- [SDR JJBA20171011006](https://openairdocs.org/sdr/JJBA20171011006), Oct 11, 2017: BATTERY PACK. NO TEST. EMERGENCY LIGHTS WILL NOT TEST. REMOVED AND REPLACED LIGHT BATTERIES. OPS CHECKED SAT.
- [SDR JJBA20170919027](https://openairdocs.org/sdr/JJBA20170919027), Sep 18, 2017: BATTERY PACK. INOPERATIVE. LOWER EMERGENCY EXIT AT ROWS 2CD, 18AB, AND 18CD WILL NOT ILLUMINATE. R & R THE BATTERY PACK, OPS CHECKED GOOD IAW AMM 33-51-00, NO DEFECTS NOTED.
- [SDR JJBA20170918007](https://openairdocs.org/sdr/JJBA20170918007), Sep 11, 2017: VALVE. FAILED. NR 2 ENGINE POWER SURGING IN FLIGHT. DURING FLIGHT THERE WAS A 10-20 PERCENT POWER SPLIT BETWEEN LEVERS. LATER THE ENGINE BEGAN SURGING AGAIN +/-5 PERCENT, THE 
- [SDR JJBA20170814014](https://openairdocs.org/sdr/JJBA20170814014), Aug 14, 2017: FUEL CONTROL. MALFUNCTIONED. AIRCRAFT DECLARED AN EMERGENCY, RETURNED TO FIELD AND SHUT DOWN THE NR 2 ENGINE FOR THE TORQUE NOT RESPONDING. THE LANDING GEAR DID NOT EXTEND, THE CREW MANUALL
- [SDR JJBA20170808010](https://openairdocs.org/sdr/JJBA20170808010), Aug 8, 2017: BULB. NOT SEATED. OVERHEAD CENTER SECOND CEILING EMERGENCY LIGHT INOPERATIVE. SEATED THE BULB IN OVERHEAD EMERGENCY LIGHT.
- [SDR JJBA20170702003](https://openairdocs.org/sdr/JJBA20170702003), Jul 2, 2017: DOOR. OBSTRUCTED. ALTERNATE EXTENSION DOOR WAS NOT FULLY CLOSED SO MAIN GEAR DID NOT RETRACT. CREW REPORTED A TRASH BAG STUCK IN THE ALTERNAT EXTENTION DOOR AND DOOR WAS NOT FULL
- [SDR JJBA20170329003](https://openairdocs.org/sdr/JJBA20170329003), Mar 29, 2017: FLAP TRACK. DAMAGED. NR 5 LT FLAP TRACK HAS PITTING CORROSION BELOW ALLOWABLE LIMITS LISTED IN RD 8-57-989. NEW FLAP TRACK INSTALLED.
- [SDR JJBA20170328020](https://openairdocs.org/sdr/JJBA20170328020), Mar 28, 2017: FLAP. DAMAGED. DELAMINATION FOUND ON LEADING EDGE OF LT OB FLAP JUST INBOARD OF FLAP TRACK NR 4. DAMAGED AREA INJECTED AND CURED IAW SRM 51-70-00.
- [SDR JJBA20170325021](https://openairdocs.org/sdr/JJBA20170325021), Mar 25, 2017: RUDDER. DENTED. DENT ON RUDDER RT SIDE. REPAIRED DAMAGED LOCATION - DENT CUT OUT, DOUBLER AND FILLER FITTED.
- [SDR JJBA20170324019](https://openairdocs.org/sdr/JJBA20170324019), Mar 24, 2017: SPLICE. CRACKED. CRACK FOUND ON LT FRAME JOINT SPLICE ANGLE AT STN X136.8 (BEHIND LT FLIGHT DECK SIDEWALL PANEL). REPLACED DAMAGED PARTS IAW SRM 51-10-00.
- [SDR JJBA20172403017](https://openairdocs.org/sdr/JJBA20172403017), Mar 24, 2017: RIB. CRACKED. NR 1 NACELLE UPPER AFT DECK SECOND TO LAST RIB CRACKED IN THE CENTER. CRACKED RIBS REMOVED AND NEW ONES FABRICATED AND INSTALLED IAW SRM 51-10-00.
- [SDR JJBA20161105007](https://openairdocs.org/sdr/JJBA20161105007), Nov 5, 2016: BATTERY PACK. INOPERATIVE. NO EMERGENCY LIGHTS. R & R THE BATTERY PACK. OPS CHECKED GOOD.
- [SDR JJBA20160925012](https://openairdocs.org/sdr/JJBA20160925012), Sep 25, 2016: BATTERY. DISCHARGED. EMERGENCY LIGHTS ARE NOT WORKING. FOUND EMERGENCY BATTERIES DRAINED. R & R PS1, PS2, PS3, PS4, PS5, AND PS6 EMERGENCY LIGHT BATTERIES. OPS CHECK SATISFACTORY IA
- [SDR JJBA20160826018](https://openairdocs.org/sdr/JJBA20160826018), Aug 26, 2016: PUMP. INOPERATIVE. NR 1 PROP TORQUE LAGS P/L INPUTS. FLUCTUATES 50% WITH NO P/L INPUTS. R & R THE NR 1 ENGINE FUEL PUMP AND NR 1 ENGINE MFC IAW PWMM 72-01-40 PERFORMED OPS CHECK I
- [SDR JJBA20160813010](https://openairdocs.org/sdr/JJBA20160813010), Aug 13, 2016: LIGHT. INOPERATIVE. EMERGENCY EXIT LIGHT AT 18CD INOPERATIVE. R & R EMERGENCY LIGHT ASSY. OPS CHECK SATISFACTORY.
- [SDR JJBA20150217005](https://openairdocs.org/sdr/JJBA20150217005), Feb 17, 2015: BATTERY. DISCHARGED. FIRST CEILING EMER LIGHT INOPERABLE. R & R PS3, PS4, PS5 EMER LIGHT BATTERIES.
- [SDR JJBA20150104003](https://openairdocs.org/sdr/JJBA20150104003), Jan 4, 2015: BATTERY. DISCHARGED. EMERGENCY LIGHTS INOPERABLE. R & R EMER LIGHT BATTERY 3351 PS4.
- [SDR JJBA20141123012](https://openairdocs.org/sdr/JJBA20141123012), Nov 23, 2014: CONNECTOR. UNSECURE. OVERHEAD EMER LIGHTS AT ROW TWO INOPERABLE. SECURED PLUG AS REQUIRED.
- [SDR JJBA20140101001](https://openairdocs.org/sdr/JJBA20140101001), Jan 1, 2014: SOCKET. DIRTY. FIRST OVERHEAD EMERGENCY LIGHTS INOPERABLE. CLEANED SOCKET & RESEATED BULB.
- [SDR JJBA20131220004](https://openairdocs.org/sdr/JJBA20131220004), Dec 20, 2013: CONNECTOR. DISCONNECTED. EXIT DOOR THRESHOLD LIGHT FAILS TO ILLUMINATE. RECONNECTED CANNON PLUG ON LIGHT ASSEMBLY.
- [SDR JJBA20131028008](https://openairdocs.org/sdr/JJBA20131028008), Oct 28, 2013: BATTERY. INOPERATIVE. EXTERIOR LOWER EMERGENCY LIGHT INOPERATIVE. R & R EMERGENCY BATTERY PS2 IRW AMM 33-51-00. NO OTHER DEFECTS NOTED, OPS CHECKED SATISFACTORY.
- [SDR JJBA20131027007](https://openairdocs.org/sdr/JJBA20131027007), Oct 27, 2013: BULB. INOPERATIVE. SECOND CEILING EMERGENCY LIGHT INOPERATIVE. R & R CEILING LIGHT BULB. OPS CHECKED GOOD.
- [SDR JJBA20130527015](https://openairdocs.org/sdr/JJBA20130527015), May 27, 2013: CONNECTOR. UNSECURE. ONE FLOOR EMERGENCY LIGHT STRIP WAS FOUND INOPERATIVE. THE MECHANIC FOUND THE CONNECTOR PLUG UNSECURED.
- [SDR JJBA20130519017](https://openairdocs.org/sdr/JJBA20130519017), May 19, 2013: PUMP. MALFUNCTIONED. CREW REPORTED THAT THE NR 1 ENGINE LOST POWER AT CRUISE AND THEN STARTED SURGING. MX REPLACED THE NR 1 ENGINE MFC AND HP FUEL PUMP.
- [SDR JJBA20130505004](https://openairdocs.org/sdr/JJBA20130505004), May 5, 2013: ECU. UNKNOWN. DURING CRUISE FLIGHT, THE CABIN PRESSURE WARNING LIGHT ILLUMINATED. BOTH AUTO AND MANUAL SYS WERE INOPERATIVE. THE CREW DECLARED AND EMERGENCY AND ALSO REPORTED
- [SDR JJBA20130310004](https://openairdocs.org/sdr/JJBA20130310004), Mar 10, 2013: BULB. BURNED OUT. DURING PRE-FLIGHT CREW REPORTED THAT THE FORWARD CEILING EMERGENCY LIGHT WAS INOPERATIVE. R & R BULB.
- [SDR JJBA20130111005](https://openairdocs.org/sdr/JJBA20130111005), Jan 11, 2013: BULB. BURNED OUT. DURING A LINE CHECK INSPECTION, NOTICED THE FIRST CEILING EMERGENCY LIGHT WAS NOT ILLUMINATING DURING TESTING. REPLACED THE LIGHT BULB AND PERFORMED AN OPS CHEC
- [SDR JJBA20121118007](https://openairdocs.org/sdr/JJBA20121118007), Nov 18, 2012: AHRS. BROKEN. DURING CLIMB CREW REPORTED THE TAKE OFF HEADING MISMATCH SHOWED A DIFFERENCE FROM COPILOT SIDE. MX CREW R & R THE AHRS UNIT. OPS CHECK.
- [SDR JJBA20120930002](https://openairdocs.org/sdr/JJBA20120930002), Sep 30, 2012: CHECK VALVE. LEAKING. SHORTLY AFTER TAKEOFF, CREW REPORTED THAT THE NR 2 HYD PRESSURE AND QUANTITY FELL TO 0 AT ACCELERATION HEIGHT. THE CREW RETURNED TO THE FIELD SHUTDOWN THE ENGIN
- [SDR JJBA20120701006](https://openairdocs.org/sdr/JJBA20120701006), Jul 1, 2012: LANDING GEAR. MALFUNCTIONED. DURING NORMAL CRUISE FLIGHT THE CREW HAD THE NOSE GEAR CYCLE UNCOMMANDED. GROUND MX CREW INSPECTED THE PSEU FOR FAULTS AND RERACKED THE PSEU AND PERFORMED A SYS
- [SDR JJBA20120521007](https://openairdocs.org/sdr/JJBA20120521007), May 21, 2012: CONNECTOR. DISCONNECTED. DURING PRE-FLIGHT, CREW NOTICED THE EMERGENCY LIGHT BETWEEN ROWS 4 AND 5 WAS NOT ILLUMINATING. MX RECONNECTED CONNECTOR TO THE FLOOR EMERGENCY LIGHT. OPS CHECKE
- [SDR JJBA20120320009](https://openairdocs.org/sdr/JJBA20120320009), Mar 20, 2012: CONNECTOR. UNSECURE. DURING THE PRE-FLIGHT INSPECTION, IT WAS NOTICED THAT THE EXIT SIGN ABOVE THE MAIN CABIN DOOR WAS NOT ILLUMINATING WHEN INTENDED. ON FURTHER INVESTIGATION, FOUN
- [SDR JJBA2012010800001](https://openairdocs.org/sdr/JJBA2012010800001), Jan 8, 2012: CONNECTOR. UNSECURE. DURING PRE-FLIGHT INSPECTION, AIRCREW NOTICED THE RED EMERGENCY FLOOR LIGHTS AT ROW 1 INOPERATIVE. GROUND MX CREW RESECURED THE CONNECTOR FOR THE EMERGENCY LIGH
- [SDR JJBA201201040001](https://openairdocs.org/sdr/JJBA201201040001), Jan 4, 2012: BATTERY. DISCHARGED. CEILING EMERGENCY LIGHTS INOPERATIVE DURING CREW PREFIGHT INSPECTION, IAW MAINTENANCE CONTROL, CHARGED SYSTEM. OPS CHECKED SATISFACTORY.
- [SDR JJBA359331316](https://openairdocs.org/sdr/JJBA359331316), May 6, 2011: BATTERY. DISCHARGED. FLIGHT CREW REPORTED EMERGENCY CEILING LIGHTS AT GALLEY AND ROW 7 DO NOT ILLUMINATE. GROUND MX CREW R & R ALL EMERGENCY LIGHT BATTERIES. EMERGENCY LIGHTS TEST S
- [SDR JJBA359PH241292](https://openairdocs.org/sdr/JJBA359PH241292), Apr 16, 2011: GCU. INOPERATIVE. DURING FLIGHT, AIRCREW NOTICED THE EMERGENCY LIGHTS FLICKERED. MX CREW R & R THE RT AC GENERATOR CONTROL UNIT. PERFORMED OPS CHECK OF SYS, CHECKED UNSATISFACTOR
- [SDR JJBA359PH241289](https://openairdocs.org/sdr/JJBA359PH241289), Apr 14, 2011: CIRCUIT BREAKER. CRACKED. DURING FLIGHT, AIRCREW NOTICED THE EMERGENCY LIGHTS AND ENG INTAKE BY-PASS LIGHTS FLICKERING. GROUND MX CREW PERFORMED A DVI OF THE SECONDARY BUSS BARS, FOUND L
- [SDR JJBA359PH331285](https://openairdocs.org/sdr/JJBA359PH331285), Apr 10, 2011: LAMP. INOPERATIVE. DURING PREFLIGHT INSP, AIRCREW NOTICED SMOKE FROM TOP STEP OF AIRSTAIR DOOR. GROUND MX CREW R & R THE LIGHT BULB IN THE TOP STEP LIGHT ASSY. PERFORMED OPS CHECK
- [SDR JJBA359PH291283A](https://openairdocs.org/sdr/JJBA359PH291283A), Apr 8, 2011: PRESSURE SWITCH. INOPERATIVE. DURING TAXI, GROUND MX CREW NOTICED THE INBD SPOILER HYD CAUTION LIGHT ILLUMINATED. THE INBD SPOILER HYD LOW PRESSURE SWITCH WAS R & R. PERFORMED OPS CHECK ON E
- [SDR JJBA2011241283](https://openairdocs.org/sdr/JJBA2011241283), Apr 8, 2011: TRU. INOPERATIVE. AIRCREW NOTICED EMERGENCY LIGHTS FLICKERING IN FLIGHT. ACFT RETURNED TO FIELD. GROUND MX FOUND LT TRU COOLING FAN INOPERATIVE. LT TRU WAS R & R. OPS CHECK PERFO
- [SDR JJBA359PH291279](https://openairdocs.org/sdr/JJBA359PH291279), Apr 7, 2011: CONNECTOR. DIRTY. AFTER TAKEOFF, THE INBD ROLL SPOILER HYD PRESSURE CAUTION LIGHT ILLUMINATED. ACFT RETURNED TO FIELD. GROUND MX CREW CLEANED THE ROLL SPOILER CONNECTOR PLUG AND 
- [SDR JJBA2011241279](https://openairdocs.org/sdr/JJBA2011241279), Apr 7, 2011: RELAY. INOPERATIVE. DURING FLIGHT, AIRCREW NOTICED EMERGENCY LIGHTS AND ENGINE INTAKE BY-PASS DOOR LIGHTS FLICKERED. ACFT WAS FERRIED. GROUND MX CREW R & R THE 2413-K18 RELAY. OPS 
- [SDR JJBA2011331242](https://openairdocs.org/sdr/JJBA2011331242), Mar 13, 2011: PIN. INOPERATIVE. FLIGHT CREW REPORTED CABIN EMERGENCY LIGHTS WOULD NOT STOP FLICKERING DURING CLIMB OUT. MX CREW R & R PIN D ON CONNECTOR 3351-21. SYS CK SATISFACTORY.
- [SDR JJBA2011331241](https://openairdocs.org/sdr/JJBA2011331241), Mar 12, 2011: CONNECTOR. LOOSE. DURING CLIMB, THE ACFT CABIN EMERGENCY LIGHTS FLICKERED. ACFT RETURNED TO FIELD, GROUND MX FOUND LOOSE CONNECTOR PLUG AT RELAY PANEL. OPS CHECK WAS PERFORMED ON
- [SDR JJBA2011271237](https://openairdocs.org/sdr/JJBA2011271237), Mar 10, 2011: MOTOR. INOPERATIVE. DURING CLIMB, THE ACFT EXPERIENCED A LT WING DOWN AILERON TRIM TAB RUNAWAY. ACFT DID NOT RESPOND TO RT WING DOWN SELECTION. GROUND MX CREW FOUND A DEFECTIVE AIL
- [SDR JJBA2011331219](https://openairdocs.org/sdr/JJBA2011331219), Feb 24, 2011: LIGHT. MALFUNCTIONED. FLIGHT CREW REPORTED THAT THE EMERGENCY LIGHTS FLICKERED DURING THE FIRST PHASE OF FLIGHT. GROUND CREW PERFORMED OPERATIONAL CHECK AND NO DEFECT NOTED AT THIS T
- [SDR JJBA2011331205](https://openairdocs.org/sdr/JJBA2011331205), Feb 11, 2011: SWITCH. INOPERATIVE. DURING FLIGHT AIRCREW NOTICED ALL EMERGENCY LIGHTS FLICKERED. GROUND MX CREW R & R THE F/A LIGHT SWITCH. PERFORMED SYS OPS AND SYSTEM CKD SATISFACTORY. ACFT RET
- [SDR JJBA2011331201](https://openairdocs.org/sdr/JJBA2011331201), Feb 10, 2011: LIGHT. INOPERATIVE. WHILE PERFORMING A PREFLIGHT INSP, AIRCREW NOTICED ONE RED LIGHT INOP ON THE FWD EMERGENCY LIGHT STRIP. GROUND MX CREW R & R THE LIGHT STRIP AND PERFORMED OPS C
- [SDR JJBA2011331168](https://openairdocs.org/sdr/JJBA2011331168), Jan 11, 2011: CONTROL PANEL. CHAFED. DURING CLIMBOUT, AIRCREW NOTICED THE EMERGENCY LIGHTS FLICKERING. GROUND MX R & R THE EMERGENCY LIGHT RELAY BRACKET ASSY. OPS CHECK WAS PERFORMED, SYS CHECKED S

All 281: https://openairdocs.org/aircraft/N359PH/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/N359PH/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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