# N360PH: 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: 515
- Year built: 1998
- Type: Fixed wing multi engine
- Engine type: Turbo-prop
- Airworthiness: Standard, transport
- Airworthiness date: April 24, 1998
- Certificate issued: February 11, 2023
- Expires: February 28, 2030
- Mode S code: A40D99
- Registered owner: [Umb Bank Na Trustee](https://openairdocs.org/faa-owner/UMB%20BANK%20NA%20TRUSTEE)
- Location: [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City)
- Owner type: Corporation
- Owner's area on the map: 40.6171° N, 111.6866° W: Placed by OpenAirDocs at the center of ZIP code 84121, within about 5 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=360PH
- Page: https://openairdocs.org/aircraft/N360PH

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/N360PH/ads.md

## Information bulletins (advisory)

None matched.

## NTSB investigations

None matched to N360PH.

## FAA accident and incident reports (2)

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 20160129001729I](https://openairdocs.org/incident/20160129001729I), Jan 29, 2016: Bombardier Inc DHC-8-202 (N360PH), Newark, NJ, No damage. On 1/29/2016 at approximately 15:40 EST flight 5008 returned to ewr and landed on rwy 29 after reporting an engine oil pressure problem. Further investigation…
- [Incident 20150302001789I](https://openairdocs.org/incident/20150302001789I), Mar 2, 2015: Bombardier Inc DHC-8-202 (N360PH), Newark, NJ, No damage. At 500 feet AGL the #2 prop feathered automatically. The autofeather system was armed at the time of the incident. The f.o. reported that the #2 engine torque…

## Service difficulty reports (249, 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 A8ZR20181113003](https://openairdocs.org/sdr/A8ZR20181113003), Nov 12, 2018: FIREWALL. CRACKED. ACCOMPLISHED DOUBLER INSTALLATION FOR CRACK ON UPPER FIREWALL WEB PN 85410554 OF #1 NACELLE RH IB SIDE AT XN 127.00 REF BOMBARDIER DEHAVILLAND RD 8-54-1565 ISSU
- [SDR A8ZR20181113002](https://openairdocs.org/sdr/A8ZR20181113002), Nov 12, 2018: STRUCTURE. CRACKED. ACCOMPLISHED REPLACEMENT OF CRACKED CLOSING MEMBER PN 85410449 OF NR 1 NACELLE RT IB SIDE FIREWALL REF RD 8-54-611 ISSUE 4 DTD 12 APR, 2001.
- [SDR A8ZR20181113001](https://openairdocs.org/sdr/A8ZR20181113001), Nov 12, 2018: FIREWALL. CRACKED. ACCOMPLISHED DOUBLER INSTALLATION FOR CRACK ON UPPER FIREWALL WEB PN 85410554 OF NO 1 NACELLE RT IB SIDE REF RD 8-54-3940 ISSUE 1 DTD 24 MAY, 2017.
- [SDR A8ZR20181106001](https://openairdocs.org/sdr/A8ZR20181106001), Nov 5, 2018: FIREWALL. CRACKED. ACCOMPLISHED DOUBLER INSTALLATION FOR CRACK ON UPPER FIREWALL WEB PN 85410554 OF NR 2 NACELLE RT OB SIDE REF RD 8-54-3940 ISSUE 1 DTD 24 MAY, 2017.
- [SDR A8ZR20181106002](https://openairdocs.org/sdr/A8ZR20181106002), Nov 5, 2018: STRUCTURE. CRACKED. ACCOMPLISHED REPLACEMENT OF CRACKED CLOSING MEMBER PN 85410449 OF NR 2 NACELLE RT OB SIDE FIREWALL REF RD 8-54-611 ISSUE 4 DTD 12 APR, 2001.
- [SDR A8ZR20180921002](https://openairdocs.org/sdr/A8ZR20180921002), Jul 12, 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 JJBA20170727030](https://openairdocs.org/sdr/JJBA20170727030), Jul 27, 2017: STRUCTURE. DAMAGED. FOUND DAMAGE ON FORE RUDDER AND TRAILING RUDDER. PERMANENT REPAIR OF RUDDER IAW EA 38-2017-116.
- [SDR JJBA20170525034](https://openairdocs.org/sdr/JJBA20170525034), May 25, 2017: PROXIMITY SWITCH. INOPERATIVE. LEFT MAIN GEAR UNSAFE AND LEFT DOOR ADVISORY ILLUMINATED DURING TAXI. R & R THE PSEU IAW AMM 32-61-00. OPS CHECKED GOOD. GEAR SWINGS PERFORMED MULTIPLE TIMES IA
- [SDR JJBA20170518031](https://openairdocs.org/sdr/JJBA20170518031), May 18, 2017: LINE. LEAKING. LT DOOR LIGHT ON GEAR PANEL REMAIN ILLUMINATED AFTER TAKEOFF AND GEAR UP. FOUND A LEAK ON THE NOSE GEAR DOWN RIDGE LINE, WHICH CAUSED AIR TO BE INTRODUCED INTO 
- [SDR JJBA20170427033](https://openairdocs.org/sdr/JJBA20170427033), Apr 27, 2017: CONNECTOR. UNSECURE. MAIN CABIN DOOR EMERGENCY EXIT SIGN INOPERATIVE. FOUND CONNECTOR BEHIND EMERGENCY EXIT SIGN NOT SECURE. SECURED CONNECTOR OPS CHECKED SAT.
- [SDR JJBA20170427032](https://openairdocs.org/sdr/JJBA20170427032), Apr 27, 2017: SWITCH. INOPERATIVE. EMERGENCY LIGHTS INOPERATIVE. R&R EMERGENCY LIGHT SWITCH OPS CHECK SAT.
- [SDR JJBA20170423030](https://openairdocs.org/sdr/JJBA20170423030), Apr 23, 2017: STRUCTURE. DAMAGED. LADDER PLATE UNDER FUEL PANEL 624AT DAMAGED. REPAIRED IAW RD 8-57-7814.
- [SDR JJBA20170423029](https://openairdocs.org/sdr/JJBA20170423029), Apr 23, 2017: SKIN. DENTED. DENT LOCATED ON LT FUSELAGE SKIN BETWEEN BS 270.5 - 291, STRINGERS 9 - 10P. REPAIRED IAW RD 8-53-15173.
- [SDR JJBA20170419022](https://openairdocs.org/sdr/JJBA20170419022), Apr 19, 2017: DECK PLATE. CHAFED. UPPER DECK ON LT NACELLE CHAFED THROUGH BY FINGERNAIL. DAMAGE CUT OUT.
- [SDR JJBA20170418020](https://openairdocs.org/sdr/JJBA20170418020), Apr 18, 2017: SUPPORT BRACKET. CRACKED. CENTER WING, RT T-DUCT SUPPORT BRACKET CRACKED. REPLACED.
- [SDR JJBA20170416018](https://openairdocs.org/sdr/JJBA20170416018), Apr 16, 2017: FLOOR SUPPORT. CORRODED. RT FLOOR SUPPORT CRACKED UNDER FLIGHT DECK FLOOR UNDER CONTROL COLUMN. REPLACED RT FLOOR SUPPORT.
- [SDR JJBA20170416016](https://openairdocs.org/sdr/JJBA20170416016), Apr 16, 2017: BRACKET. CRACKED. BAGGAGE DOOR COUNTERBALANCE CABLE AFT PULLEY BRACKET IS CRACKED. COUNTERBALANCE AFT CABLE REPLACED.
- [SDR JJBA20170414021](https://openairdocs.org/sdr/JJBA20170414021), Apr 14, 2017: FITTING. CORRODED. AFT RT KEEL STRINGER TENSION FITTING CORRODED. FITTING REPLACED.
- [SDR JJBA20170414019](https://openairdocs.org/sdr/JJBA20170414019), Apr 14, 2017: STIFFENER. CRACKED. CENTER WING, FD OF BLEED AIR T-DUCT, STIFFENER CRACKED. REPLACED, TREATED AND PRIMED.
- [SDR JJBA20170414015](https://openairdocs.org/sdr/JJBA20170414015), Apr 14, 2017: SKIN. DENTED. SMALL CRACK FOUND ON FWD SIDE OF BOTTOM BEAM OF PASSENGER DOOR SHELL. REMOVED CRACKED BEAM ASSEMBLY.
- [SDR JJBA20170412017](https://openairdocs.org/sdr/JJBA20170412017), Apr 12, 2017: SEAT TRACK. CORRODED. MINOR CORROSION FOUND ON BOTH FWD AND AFT OB LT SEAT RAILS. CORROSION REMOVED IAW RD 8-53-1342.
- [SDR JJBA20170410026](https://openairdocs.org/sdr/JJBA20170410026), Apr 10, 2017: BRACKET. DAMAGED. SMALL AREA OF SURFACE CORROSION FOUND ON FWD AND AFT PASSENGER DOOR STEP LOWER ANGLES AND UPPER AFT SUPPORT BRACKET. BRACKETS FOUND TO BE DAMAGED. BRACKETS REPL
- [SDR JJBA20170425025](https://openairdocs.org/sdr/JJBA20170425025), Apr 10, 2017: STRUCTURE. CORRODED. CORROSION FOUND ON UNDER FLOOR STRUCTURE LOCATED AT BS 222, RH31. WORK CARRIED OUT IN REFERENCE TO SRM 51-20-11 AND 51-20-36.
- [SDR JJBA20170410024](https://openairdocs.org/sdr/JJBA20170410024), Apr 10, 2017: STRUCTURE. CORRODED. CORROSION FOUND IN CABIN UNDER FLOOR LOCATIONS RT 31 X270.5 X291.4 X312.35 X333.3. WORK CARRIED OUT IN REFERENCE TO SRM 51-20-11 AND SRM 51-20-36.
- [SDR JJBA20170409027](https://openairdocs.org/sdr/JJBA20170409027), Apr 9, 2017: FRAME. CORRODED. SKIN DEFECT AT STRINGER 31S AND BS 201.150. POSSIBLE CORROSION BETWEEN SKIN AND STRINGER. THE FRAME WAS CORRODED BEYOND LIMITS.
- [SDR JJBA20170420023](https://openairdocs.org/sdr/JJBA20170420023), Apr 8, 2017: PANEL. DAMAGED. RT WING FUEL PANEL 624AT (IB PANEL) HAS 2 SCREW HOLES DAMAGED, DAMAGE ALSO CARRIED THROUGH TO THE LADDER PLATE. REPAIRED RD8-57-2673.
- [SDR JJBA20161216016](https://openairdocs.org/sdr/JJBA20161216016), Dec 16, 2016: DOOR. OUT OF ADJUST. EMERGENCY EXIT DOOR AT 2CD HAS A GAP. ADJUSTED DOOR PANEL AND RESET DOOR. NO DEFECTS NOTED.
- [SDR JJBA20161202006](https://openairdocs.org/sdr/JJBA20161202006), Dec 2, 2016: POWER SUPPLY. INOPERATIVE. EMERGENCY LIGHT ABOVE MAIN CABIN DOOR INOPERATIVE. R & R THE POWER SUPPLY.
- [SDR JJBA20161202005](https://openairdocs.org/sdr/JJBA20161202005), Dec 2, 2016: POWER SUPPLY. INOPERATIVE. EMERGENCY LIGHTS INOPERATIVE. R & R THE POWER SUPPLY.
- [SDR JJBA20161112015](https://openairdocs.org/sdr/JJBA20161112015), Nov 12, 2016: AUTOFEATHER SYS. MALFUNCTIONED. AUTOFEATHER DID NOT ARM DEPARTURE ROLL. PERFORMED OPERATIONAL CHECK ON AUTOFEATHER SYSTEM. OPS CHECKED GOOD.
- [SDR JJBA20161031003](https://openairdocs.org/sdr/JJBA20161031003), Oct 31, 2016: SWITCH. DIRTY. EMERGENCY LIGHTS WILL NOT EXTINGUISH BY FA PANEL WHEN ARMED. CLEANED EMERGENCY LIGHT SWITCH. OPS CHECK SAT. NO DEFECTS NOTED.
- [SDR JJBA20161006007](https://openairdocs.org/sdr/JJBA20161006007), Oct 6, 2016: BATTERY. INOPERATIVE. DURING L CHECK, EMERGENCY LIGHTS FOUND INOPERATIVE. R & R EMERGENCY BATTERIES, OPS CHECKED GOOD. NO OTHER DEFECTS NOTED.
- [SDR JJBA20160816012](https://openairdocs.org/sdr/JJBA20160816012), Aug 16, 2016: BATTERY. DISCHARGED. EMERGENCY LIGHT OVER MAIN CABIN DOOR NOT ILLUMINATING. R & R EMERGENCY BATTERIES OPS CK SAT NO DEFECTS NOTED AT THIS TIME. ADDITIONAL BATTERIES REMOVED PN 61-04
- [SDR JJBA20160622011](https://openairdocs.org/sdr/JJBA20160622011), Jun 22, 2016: ENGINE. SMOKE. SMOKE IN THE FLT DECK AFTER ENGINE START. R & R ACM, OPS CHECK FAILED. BORESCOPE INSPECTION-1 AREA WAS MOIST WITH OIL RESIDUE BUT NOT COLLECTIBLE AS A QUANTITY.
- [SDR JJBA20160525010](https://openairdocs.org/sdr/JJBA20160525010), May 25, 2016: SWITCH. OUT OF ADJUST. EMERGENCY LIGHTS WON'T EXTINGUISH USING FLIGHT ATTENDANT BUTTON. ADJUSTED FLIGHT ATTENDANT BUTTON BY ADJUSTING TWO SCREWS FOR THE SWITCH.
- [SDR JJBA20160428018](https://openairdocs.org/sdr/JJBA20160428018), Apr 28, 2016: INVERTER. INOPERATIVE. PRIMARY INVERTER FAIL WITH SMOKE ODOR. R & R PRIMARY INVERTER.
- [SDR JJBA20160128010](https://openairdocs.org/sdr/JJBA20160128010), Jan 28, 2016: HYDRAULIC LINE. DEFECTIVE. NUMBER 1 ENG HYD PUMP, CAUTION FLICKERING, FOLLOWED BY NR 1 HYD QTY, LOSING ALL PRESS DURING FLIGHT. R & R NR 1 ENG HYD RESERVOIR FILLER LINE.
- [SDR JJBA20151220009](https://openairdocs.org/sdr/JJBA20151220009), Dec 20, 2015: BATTERY PACK. DISCHARGED. EMERGENCY LIGHTS INOPERATIVE. R & R ALL EMER LIGHT BATTERY PACKS.
- [SDR JJBA20151119005](https://openairdocs.org/sdr/JJBA20151119005), Nov 19, 2015: UNKNOWN. MALFUNCTIONED. ON LANDING ROLLOUT WITH NR 2 ENG POWER LEVER AT DISK, THE TORQUE & RPM ADVANCED TO TAKEOFF POWER UN-COMMANDED. PERFORMED BETA BACKUP, OVERSPEED GOVERNOR, MINIMU
- [SDR JJBA20151029010](https://openairdocs.org/sdr/JJBA20151029010), Oct 29, 2015: WARNING SYSTEM. ACTIVATED. WITH LG DOWN & LOCKED, RECEIVED GEAR UNSAFE HORN AS WELL AS BOTH AMBER & RED GEAR UNSAFE LIGHTS, WHICH WERE ILLUMINATED. GEAR UNSAFE LIGHTS CYCLED 6 TIMES FROM 
- [SDR JJBA20150908002](https://openairdocs.org/sdr/JJBA20150908002), Sep 8, 2015: BATTERY. DISCHARGED. EMERGENCY LIGHTS FLICKER ON WHEN SELECTED, THEN GO OUT. R & R EMER BATTERY PS-2.
- [SDR JJBA20150724009](https://openairdocs.org/sdr/JJBA20150724009), Jul 24, 2015: POWER SUPPLY. INOPERATIVE. LOWER EMER LIGHTS IN THE CABIN ARE INOPERATIVE. R & R LIGHT POWER SUPPLY UNIT AT PS4. R & R EMER LIGHT SWITCH.
- [SDR JJBA20150722008](https://openairdocs.org/sdr/JJBA20150722008), Jul 22, 2015: BATTERY. DISCHARGED. EMERGENCY LIGHTS WILL NOT OPERATE FROM THE FLIGHT ATTENDANT STATION. R & R EMER BATTERIES PS-1, PS-2 & PS-6.
- [SDR JJBA20150717007](https://openairdocs.org/sdr/JJBA20150717007), Jul 17, 2015: RELAY. FAILED. FOUR EMER LIGHTS ARE INOPERATIVE. R & R 3351 K2 RELAY.
- [SDR JJBA20150716006](https://openairdocs.org/sdr/JJBA20150716006), Jul 16, 2015: WIRE. DISCONNECTED. FOUR EMER EXIT LIGHTS IN CABIN AREA ARE NOT ILLUMINATED. RE-PINNED WIRE ON FLIGHT ATTENDANT SWITCH.
- [SDR JJBA20150612007](https://openairdocs.org/sdr/JJBA20150612007), Jun 12, 2015: POWER SUPPLY. INOPERATIVE. CABIN EMER LIGHTS WILL NOT ILLUMINATE. R & R ELEC POWER SUPPLY AT PS2.
- [SDR JJBA20150530012](https://openairdocs.org/sdr/JJBA20150530012), May 30, 2015: BATTERY PACK. NOT SEATED. EMERGENCY LIGHTS NOT OPERATING PROPERLY. RACKED BATTERY PACK PS4.
- [SDR JJBA20150302001](https://openairdocs.org/sdr/JJBA20150302001), Mar 2, 2015: CONTROL UNIT. MALFUNCTIONED. NUMBER 2 ENG SHUTDOWN AT 500 FEET. AFTER NR 2 ENG SHUTDOWN PILOT HEARD PROP FEATHER ON ITS OWN. AUTO FEATHER WAS ARMED & UP TRIM LIGHT ILLUMINATED. NO FIRE INDI
- [SDR JJBA20150217004](https://openairdocs.org/sdr/JJBA20150217004), Feb 17, 2015: BATTERY. DISCHARGED. CABIN DOOR EXIT SIGN DOES NOT STAY ILLUMINATED WHEN TESTED. R & R POSITION ONE EMER LIGHT BATTERY.
- [SDR JJBA20150216002](https://openairdocs.org/sdr/JJBA20150216002), Feb 16, 2015: BATTERY. DISCHARGED. CEILING & UPPER SIDEWALL EMER LIGHTS INOPERABLE. R & R EMER LIGHT BATTERIES.

All 249: https://openairdocs.org/aircraft/N360PH/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/N360PH/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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