# N365PH: 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: 526
- Year built: 1998
- Type: Fixed wing multi engine
- Engine type: Turbo-prop
- Airworthiness: Standard, transport
- Airworthiness date: December 11, 1998
- Certificate issued: November 19, 2024
- Expires: November 30, 2031
- Mode S code: A4202C
- 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=365PH
- Page: https://openairdocs.org/aircraft/N365PH

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/N365PH/ads.md

## Information bulletins (advisory)

None matched.

## NTSB investigations

None matched to N365PH.

## FAA accident and incident reports

None matched to N365PH.

## Service difficulty reports (208, 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 JJBA2018061910007](https://openairdocs.org/sdr/JJBA2018061910007), May 10, 2018: WIRE. OUT OF POSITION. LEFT EMERGENCY EXIT FORWARD EMERGENCY LIGHT WAS UNSERVICEABLE. TROUBLESHOT AND FOUND WIRES IN CONNECTORS J12 ON SIDEWALL PANEL SWAPPED. SWAPPED WIRES BACK. OPS 
- [SDR JJBA20170714021](https://openairdocs.org/sdr/JJBA20170714021), Jul 14, 2017: PLATE. CRACKED. WING LADDER PLATE DAMAGED. REPAIRED IAW RD 8-57-7899.
- [SDR JJBA20170605005](https://openairdocs.org/sdr/JJBA20170605005), Jun 5, 2017: BATTERY PACK. DISCHARGED. FWD CENTER ISLE EMERGENCY LIGHT INTERMITTENT. CHARGED EMERGENCY LIGHT BATTERIES AND PERFORMED OPERATIONAL TEST OF EMERGENCY LIGHT SYSTEM. OPS CHECK SAT. NO OTHE
- [SDR JJBA20170324016](https://openairdocs.org/sdr/JJBA20170324016), Mar 24, 2017: PCU. INOPERATIVE. BOTH PROPELLERS RPM DROPPED FROM 1050-1020 DURING CLIMB WITH POWER AT 90% TORQUE. IN CRUISE SETTING PROPELLER RPM WOULD NOT DROP BELOW 925 AT 90% TORQUE. CRUISE
- [SDR JJBA20170130022](https://openairdocs.org/sdr/JJBA20170130022), Jan 30, 2017: LIGHT. INOPERATIVE. WD AND THIRD EMERGGENCY LIGHT INOPERATIVE. ADJUSTED THE LIGHT, OPS CHECKED GOOD. NO DEFECTS NOTED AT THIS TIME.
- [SDR JJBA20170114007](https://openairdocs.org/sdr/JJBA20170114007), Jan 14, 2017: ACM. FAILED. SMOKE IN THE AIRCRAFT. R & R THE ACM. OPS AND LEAK CHECK GOOD.
- [SDR JJBA20170113008](https://openairdocs.org/sdr/JJBA20170113008), Jan 13, 2017: BULB. INOPERATIVE. GREEN ADVISORY LIGHT, EMERGENCY SIGN INOPERATIVE. SECURED THE BULB OPS CHECKED GOOD.
- [SDR JJBA20161130001](https://openairdocs.org/sdr/JJBA20161130001), Nov 30, 2016: AHRS. INOPERATIVE. BOTH EADI DISPLAYED ERRONEOUS INFORMATION IN FLIGHT. R & R THE NR 1 AHRU, OPS CHECKED GOOD.
- [SDR JJBA20161128034](https://openairdocs.org/sdr/JJBA20161128034), Nov 28, 2016: DUCT. LOOSE. VISIBLE SMOKE IN THE CABIN. R & R FLEXIBLE CONNECTOR BETWEEN HEAT EXCHANGER AND ACM OPS CHECK SAT.
- [SDR JJBA20161026034](https://openairdocs.org/sdr/JJBA20161026034), Oct 26, 2016: UNKNOWN. SMOKE. DURING CLIMB OUT AT 3000 FT, CAPTAIN SMELLED SMOKE FOLLOWED BY VISUAL SMOKE COMING FROM THE UPPER CENTER DASH. OPS CHECK PERFORMED IAW AMM 30-41-00. WINDSHIELD 
- [SDR JJBA20160617008](https://openairdocs.org/sdr/JJBA20160617008), Jun 17, 2016: BATTERY. DISCHARGED. CENTER AISLE AND AFT EMERGENCY LIGHTS INOPERATIVE. R & R BATTERY PS3.
- [SDR JJBA20160214009](https://openairdocs.org/sdr/JJBA20160214009), Feb 14, 2016: LIGHT. INOPERATIVE. FOUR EMER LIGHTS ARE INOPERATIVE. OPERATIONAL CHECKED SATISFACTORY.
- [SDR JJBA20151229013](https://openairdocs.org/sdr/JJBA20151229013), Dec 29, 2015: SWITCH. STUCK. FLIGHT ATTENDANT EMER LIGHT SWITCH STUCK ON ASSEMBLY, NOT SECURE. R & R FLIGHT ATTENDANTS EMER LIGHT SWITCH & 6 EMER LIGHT BATTERIES.
- [SDR JJBA20150304002](https://openairdocs.org/sdr/JJBA20150304002), Mar 4, 2015: BATTERY PACK. DISCHARGED. CABIN CEILING EMER LIGHT NOT ILLUMINATING. R & R PS3 EMER LIGHT SUPPLY BATTERY PACK.
- [SDR JJBA20150129012](https://openairdocs.org/sdr/JJBA20150129012), Jan 29, 2015: BOLT. OUT OF ADJUST. PASSENGER DOOR WARNING LIGHT ILLUMINATED AT 12,000 FT & EXTINGUISHED AT 5,00 FT. DEFERRED IAW MEL. ADJUSTED ALL PAX DOOR STOP BOLTS. OPERATIONAL CHECK SATISFACT
- [SDR JJBA20141112005](https://openairdocs.org/sdr/JJBA20141112005), Nov 12, 2014: LIGHT. INOPERATIVE. EMERGENCY LIGHTS IN AFT CABIN & CTR CEILING INOPERABLE. R & R 3352-PS1.
- [SDR JJBA20141015005](https://openairdocs.org/sdr/JJBA20141015005), Oct 15, 2014: CIRCUIT BREAKER. TRIPPED. NUMBER 2 PITOT HEAT CAUTION LIGHT ILLUMINATED IN FLIGHT. RESET CB.
- [SDR JJBA20140711015](https://openairdocs.org/sdr/JJBA20140711015), Jul 11, 2014: BATTERY. DISCHARGED. OVERHEAD AFT EMER LIGHTS INOPERABLE. RECHARGED EMER LIGHT BATTERIES.
- [SDR JJBA20140704011](https://openairdocs.org/sdr/JJBA20140704011), Jul 4, 2014: SIGN. UNSECURE. EMERGENCY EXIT SIGN ABOVE MAIN CABIN DOOR LOOSE & KEEPS FALLING DOWN. SECURED EMER EXIT SIGN ABOVE MAIN CABIN DOOR.
- [SDR JJBA20140612004](https://openairdocs.org/sdr/JJBA20140612004), Jun 12, 2014: PUMP. FAILED. NUMBER 1 HYD PX WENT TO ZERO IN FLIGHT & NR 1 ENG HYD PX LIGHT ILLUMINATED. R & R NR 1 HYD PUMP.
- [SDR JJBA20140611005](https://openairdocs.org/sdr/JJBA20140611005), Jun 11, 2014: HYDRAULIC LINE. DAMAGED. NUMBER 1 HYD FLUID WENT TO ZERO IN FLIGHT. INSTALLED TEMP FLEX LINE & INSPECTED SYS.
- [SDR JJBA20140123013](https://openairdocs.org/sdr/JJBA20140123013), Jan 23, 2014: BATTERY. DISCHARGED. SEVERAL EMERGENCY LIGHTS INOPERABLE. R & R PSU BATTERIES PS3 & PS2.
- [SDR JJBA20140104002](https://openairdocs.org/sdr/JJBA20140104002), Jan 4, 2014: LIGHT. INOPERATIVE. ONE CEILING EMERGENCY LIGHT INOPERABLE. R & R LIGHT BULB.
- [SDR JJBA20121031009](https://openairdocs.org/sdr/JJBA20121031009), Nov 1, 2012: CONTROL UNIT. MALFUNCTIONED. CREW REPORTED THAT THE NR 2 ENGINE WAS SURGING 15 - 20 PERCENT TORQUE IN FLIGHT WITH THE PROPS AT 1050. DECLARED AN EMERGENCY AND RETURNED TO THE FIELD. MX TRAC
- [SDR JJBA20121022005](https://openairdocs.org/sdr/JJBA20121022005), Oct 22, 2012: PUMP. MALFUNCTIONED. DURING CLIMB CREW REPORTED THE NR 2 ENGINE WAS SURGING CAUSING THE ACFT TO YAW DURING THE SURGING. DECLARED AN EMERGENCY AND RETURNED THE FIELD. GROUND MX WAS A
- [SDR JJBA20120719011](https://openairdocs.org/sdr/JJBA20120719011), Jul 19, 2012: BATTERY PACK. DISCHARGED. DURING PRE-FLIGHT, CREW NOTICED THE MID CABIN EXIT SIGN WAS INOPERATIVE. GROUND MX CREW CHARGED THE BATTERIES WITH GROUND POWER, RESET THE SYSTEM, AND PERFORMED
- [SDR JJBA20120718010](https://openairdocs.org/sdr/JJBA20120718010), Jul 18, 2012: LIGHT. INOPERATIVE. DURING PRE-FLIGHT, CREW NOTICED THE LT CEILING EMERGENCY LIGHTS WERE INOPERATIVE. GROUND MX CREW RESET THE SYSTEM POWER AND PERFORMED AN OPS CHECK OF THE EMERGE
- [SDR JJBA20120716008](https://openairdocs.org/sdr/JJBA20120716008), Jul 16, 2012: BATTERY. INOPERATIVE. DURING PREFLIGHT, CREW NOTICED THAT ALL EMERGENCY LIGHTS WERE INOPERATIVE. GROUND MX CREW R & R ALL THE EMERGENCY LIGHT BATTERIES. AN OPERATIONAL CHECK PRODUCED
- [SDR JJBA20120704002](https://openairdocs.org/sdr/JJBA20120704002), Jul 4, 2012: SMOKE DETECTOR. DEFECTIVE. DURING CRUISE FLIGHT, CARGO SMOKE WARNING LIGHT ILLUMINATED IN THE COCKPIT. THE CREW DECLARED AN EMERGENCY AND RETURNED TO FIELD. MX CREW INSPECTED CARGO BAY AN
- [SDR JJBA20120307001](https://openairdocs.org/sdr/JJBA20120307001), Mar 4, 2012: BATTERY PACK. INOPERATIVE. DURING THE PRE-FLIGHT INSPECTION, CREW NOTICED CEILING EMERGENCY LIGHTS WERE NOT OPERATING. GROUND MX CREW R & R ALL SIX OF THE EMERGENCY LIGHT BATTERIES. AN OP
- [SDR JJBA2012010800101](https://openairdocs.org/sdr/JJBA2012010800101), Jan 8, 2012: BATTERY PACK. INOPERATIVE. DURING PRE-FLIGHT INSPECTION, AIRCREW NOTICED THE EMERGENCY EXIT LIGHT ABOVE MAIN CABIN DOOR WAS INOPERATIVE. GROUND MX CREW R & R THE PS1 EMERGENCY BATTERY PAC
- [SDR JJBA20110919001](https://openairdocs.org/sdr/JJBA20110919001), Sep 19, 2011: WIRE. DAMAGED. FLIGHT CREW REPORTED EMERGENCY LIGHT NOT WORKING. MX RESEATED WIRE INTO CONNECTOR. OPS CHECKED SATISFACTORY.
- [SDR JJBA365PH33013](https://openairdocs.org/sdr/JJBA365PH33013), Sep 6, 2011: LIGHT. BROKEN. MAINTENANCE CREW FOUND DURING AN "L" CHECK, EMERGENCY FLOOR STIP LIGHT AT SEAT 3BA AND 3ED BROKEN AND NOT WORKING. R & R LIGHT, OPS CHECKED SATISFACTORY.
- [SDR JJBA20110906001](https://openairdocs.org/sdr/JJBA20110906001), Sep 6, 2011: LIGHT. INOPERATIVE. EMERGENCY LIGHT , ROW 1, NOT ILLUMINATING. R & R LIGHT, OPS CHECKED SATISFACTORY.
- [SDR JJBA20110831001](https://openairdocs.org/sdr/JJBA20110831001), Aug 31, 2011: CONNECTOR. LOOSE. FLIGHT CREW REPORTED EMERGENCY EXIT FWD DOWN LIGHT NOT WORKING. RECONNECTED LOOSE CONNECTOR FOR THE EMERGENCY EXIT LIGHT FORWARD DOWN LIGHT ON THE CEILING. PERF
- [SDR JJBA365PH331453](https://openairdocs.org/sdr/JJBA365PH331453), Aug 31, 2011: CONNECTOR. UNSECURE. FLIGHT CREW REPORTED RED EMERGENCY LIGHT ON 2ND STRIP NOT ILLUMINATING AT ROW 1. MX CREW RESECURED PLUG PERFORMED OPS CHECK WAS SATISFACTORY.
- [SDR JJBA365PH331440](https://openairdocs.org/sdr/JJBA365PH331440), Aug 20, 2011: BATTERY. DISCHARGED. FLIGHT CREW REPORTED SEGMENTS OF THE EMERGENCY LIGHTS ARE NOT WORKING. MX CONTROL PERFORMED GROUND RUN TO RECHARGE BATTERIES. OPS CHECK WAS SATISFACTORY.
- [SDR JJBA365PH331373A](https://openairdocs.org/sdr/JJBA365PH331373A), Jul 6, 2011: BATTERY PACK. INOPERATIVE. FLIGHT CREW REPORTED EMERGENCY EXIT SIGN AT ROW 1 IS NOT WORKING. MX CREW R & R BATTERY PACK PS2. PERFORMED OPS CHECK AND OPS CHECK WAS SATISFACTORY.
- [SDR JJBA365PH331369](https://openairdocs.org/sdr/JJBA365PH331369), Jul 5, 2011: BULB. LOOSE. FLIGHT CREW REPORTED EMERGENCY LIGHT IN ROW 3, CEILING NOT WORKING. MX CREW RESEATED LIGHT BULB, OPS CHECK WAS SATISFACTORY.
- [SDR JJBA365PH331363](https://openairdocs.org/sdr/JJBA365PH331363), Jul 1, 2011: SWITCH. UNKNOWN. FLIGHT CREW REPORTED EMERGENCY EXIT SIGN ABOVE GALLEY AT ROW 1 IS NOT WORKING. MX CREW TESTED SWITCH AND OPS CHECK WAS SATISFACTORY.
- [SDR JJBA365PH321332](https://openairdocs.org/sdr/JJBA365PH321332), Jun 12, 2011: DOOR. UNKNOWN. FLIGHT CREW REPORTED LT MLG FAILED TO EXTEND ON APPROACH, USED ALTERNATE GEAR EXTENSION METHOD. GEAR EXTEND SUCCESSFULLY. MX CREW R & R MLG CENTER DOOR ASSY. PE
- [SDR JJBA365PH211298](https://openairdocs.org/sdr/JJBA365PH211298), May 19, 2011: ACM. ODOR. AFTER PUSHBACK, DURING TRANSITION FROM START/FEATHER TO MAXIMUM WITH THE CONDITION LEVERS, AIRCREW NOTICED A BURNED ODOR COMING THROUGH THE VENTS IN THE FLIGHT 
- [SDR JJBA2011331155](https://openairdocs.org/sdr/JJBA2011331155), Jan 8, 2011: CONNECTOR. LOOSE. DURING PREFLIGHT INSP, AIRCREW NOTICED THE 2 FWD FLOOR EMERGENCY LIGHTS INOPERATIVE. GROUND MX CREW CLEANED AND RESEATED CONNECTORS. OPS CHECK OF THE EMERGENCY 
- [SDR JJBA2010331138](https://openairdocs.org/sdr/JJBA2010331138), Dec 24, 2010: LIGHT. DEFECTIVE. DURING PREFLIGHT INSP, AIRCREW NOTICED FWD RED SECTION OF FLOOR EMERGENCY LIGHTS INOPERATIVE. GROUND MX CREW R & R THE FLOOR EMERGENCY LIGHT STRIP. PERFORMED EM
- [SDR JJBA2010261104](https://openairdocs.org/sdr/JJBA2010261104), Nov 28, 2010: CONNECTOR. DIRTY. DURING PREFLIGHT INSP, AIRCREW NOTICED THAT THE "SMOKE" WARNING LIGHT ILLUMINATED TRIGGERING THE "MASTER" WARNING LIGHT. GROUND CREW CLEANED THE CONNECTORS ON B
- [SDR JJBA2010321062](https://openairdocs.org/sdr/JJBA2010321062), Oct 21, 2010: BRAKE ASSY. LEAKING. FLIGHT CREW REPORTED THAT NR 2 HYD FLUID LEAKED OUT. MX CREW R & R NR 2 BRAKE ASSY AS REQUIRED, BLEED BREAKS AND OPS CHECK SATISFACTORY NO OTHER DEFECTS NOTED.
- [SDR JJBA201026944](https://openairdocs.org/sdr/JJBA201026944), Jul 18, 2010: SMOKE WARNING. FALSE ACTIVATION. SMOKE WARNING LIGHT ILLUMINATED IN FLT INTERMITTENT 1 SEC DURATION. MEL'ED UPON NORMAL LANDING. TROUBLESHOT SYSTEM AND FOUND NO DEFECTS.
- [SDR JJBA2010520992](https://openairdocs.org/sdr/JJBA2010520992), Jun 30, 2010: CHECK VALVE. NOT SEATED. CAPT STATED THAT 8730 WAS AT FL 185 AND INSTRUCTED BY ATC TO DESCEND TO FL 140. AT THIS TIME THE CREW HEARD A LOUD BANG AND THEN NOTICED THE CABIN CLIMB RATE MO
- [SDR JJBA201025765](https://openairdocs.org/sdr/JJBA201025765), Feb 8, 2010: BATTERY PACK. DISCHARGED. DURING PREFLIGHT, TRIED TO TEST EMERGENCY LIGHTS, DID NOT TEST. RECHARGED BATTERIES IAW MX CONTROL. TEST SATISFACTORY.
- [SDR QXEA200800178](https://openairdocs.org/sdr/QXEA200800178), Feb 11, 2008: SMOKE DETECTOR. NO TEST. SEA - FLIGHT 2059 - BAGGAGE SMOKE DETECTOR WARNING WILL NOT TEST. MAINTENANCE PLACED ON MEL 26-8A. AIRCRAFT RETURNED TO SERVICE. ON 2/14/08, THE SMOKE DETECTOR 

All 208: https://openairdocs.org/aircraft/N365PH/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/N365PH/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

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.