# N351PH: 1997 Dehavilland DHC-8-202

- Status: Valid registration
- Airframe: [Dehavilland DHC-8-202](https://openairdocs.org/model/dehavilland-dhc-8-202) (registry code 2809007, 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: 490
- Year built: 1997
- Type: Fixed wing multi engine
- Engine type: Turbo-prop
- Airworthiness: Standard, transport
- Airworthiness date: December 30, 1997
- Certificate issued: November 19, 2024
- Expires: November 30, 2031
- Mode S code: A3E9D1
- 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=351PH
- Page: https://openairdocs.org/aircraft/N351PH

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 (Dehavilland 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/N351PH/ads.md

## Information bulletins (advisory)

None matched.

## NTSB investigations

None matched to N351PH.

## FAA accident and incident reports

None matched to N351PH.

## Service difficulty reports (245, newest 50)

As reported by operators and repair stations. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR A8ZR20180411002](https://openairdocs.org/sdr/A8ZR20180411002), Mar 9, 2018: SKIN. DENTED. DENT IN FUSELAGE BETWEEN STA 291.4 TO STA 312.35 & S8P TO S10P. EXTERNAL REPAIR DOUBLER INSTALLED REF RD 20-2018-048. REPAIR DOUBLER 7" X 10"
- [SDR A8ZR20180815001](https://openairdocs.org/sdr/A8ZR20180815001), Feb 26, 2018: FIREWALL. CRACKED. UPPER FIREWALL CRACKED, ON THE LT NACELLE STA 125.50.
- [SDR A8ZR20180411003](https://openairdocs.org/sdr/A8ZR20180411003), Jan 30, 2018: SKIN. DENTED. DENT ON RT FUSELAGE AT XSTA 729 & BETWEEN S17S AND S18S TO BE OUT OF LIMITS. EXTERNAL DOUBLER INSTALLED REF SRM 53-30-24 REV 6 REPAIR DOUBLER 10.5" X 5.7".
- [SDR A8ZR20180411001](https://openairdocs.org/sdr/A8ZR20180411001), Jan 30, 2018: SKIN. DENTED. DENT ON LT FUSELAGE AT XSTA 724 & BETWEEN S13P AND S14P TO BE OUT OF LIMITS. DENT REPAIRED IN REF 53-30-24 REV 6 REPAIR DOUBLER 12.5" X 6.2".
- [SDR JJBA20170325015](https://openairdocs.org/sdr/JJBA20170325015), Mar 25, 2017: ACM. FAILED. FA REPORTED TO CREW AT 1000FT, SMOKE FILLED THE CABIN. CREW TURNED OFF BLEEDS AND SMOKE DISSIPATED. R & R THE ACM, OPS CHECKED GOOD.
- [SDR JJBA20160909004](https://openairdocs.org/sdr/JJBA20160909004), Sep 9, 2016: BATTERY. DISCHARGED. EMERGENCY LIGHTS INOPERATIVE. R & R EMERGENCY BATTERIES, OPS CHECK SATISFACTORY. ADDITIONAL PARTS INCLUDE: 2X PN 61-0478-11, SN CA012, TT 5948.28, TC 6979; SN 0
- [SDR JJBA20160613006](https://openairdocs.org/sdr/JJBA20160613006), Jun 13, 2016: BATTERY PACK. INOPERATIVE. EMERGENCY EXIT LIGHTS INOPERATIVE. R & R THE BATTERY PACKS.
- [SDR JJBA20151001003](https://openairdocs.org/sdr/JJBA20151001003), Oct 1, 2015: SKIN PANEL. GOUGED. GOUGE IN FUSELAGE, BETWEEN LT ICE SHIELD & BETWEEN STRINGER 6 & 7, X291.40 & X312.35. REPAIRED DAMAGE IAW RD 8-53-14381.
- [SDR JJBA2014110500002](https://openairdocs.org/sdr/JJBA2014110500002), Nov 5, 2014: POWER SUPPLY. INOPERATIVE. EMERGENCY LIGHTS WILL NOT TEST. R & R THE POWER SUPPLIES IN POSITION 1, 2, 3 & 6.
- [SDR JJBA20140929010](https://openairdocs.org/sdr/JJBA20140929010), Sep 29, 2014: LIGHT. MALFUNCTIONED. EMERGENCY LIGHTS FLICKERING DURING TAKEOFF & THEN AGAIN ON LANDING. PERFORMED OPERATIONAL CHECK OF EMER LIGHTS, SATISFACTORY AT THIS TIME.
- [SDR JJBA20140626010](https://openairdocs.org/sdr/JJBA20140626010), Jun 26, 2014: CIRCUIT BREAKER. POPPED. AUTOFEATHER WILL NOT ARM. FOUND TORQUE CONNECTOR CB POPPED. RESET BREAKER & PERFORMED POWER RUNS.
- [SDR JJBA20140615006](https://openairdocs.org/sdr/JJBA20140615006), Jun 15, 2014: PSU. UNSECURE. PSU OVER SEAT 23A FELL. SECURED SEAT 23A PSU.
- [SDR JJBA20140613007](https://openairdocs.org/sdr/JJBA20140613007), Jun 13, 2014: POWER SUPPLY. DISCHARGED. EMERGENCY LIGHTS WILL NOT STAY ON. RAN NR 2 ENG TO CHARGE POWER SUPPLY.
- [SDR JJBA20140427005](https://openairdocs.org/sdr/JJBA20140427005), Apr 27, 2014: GLOWSTRIP. MISINSTALLED. EMERGENCY LIGHTS WILL TEST USING THE FLIGHT DECK SWITCH. FOUND GLOW STRIP TO LT EMERGENCY EXIT DOOR BACKWARDS. INSTALLED CORRECTLY, OPERATIONS CHECKED SATISFACT
- [SDR JJBA20140314003](https://openairdocs.org/sdr/JJBA20140314003), Mar 14, 2014: STRUT. CRACKED. FOUND 10 INCH CRACK IN SHOCK STRUT OF NLG. R & R NLG SHOCK STRUT.
- [SDR JJBA20131031010](https://openairdocs.org/sdr/JJBA20131031010), Oct 31, 2013: SEAT TRACK. CORRODED. LEFT FWD INBD SEAT RAIL CORRODED TO LIMITS. SPLICED IN NEW SECTION ON LT FWD SEAT RAIL AT STATION X262.0 IAW BOMBARDIER GENERIC 8-53-3074.
- [SDR JJBA20130721013](https://openairdocs.org/sdr/JJBA20130721013), Jul 21, 2013: LIGHT. INOPERATIVE. FORWARD EMERGENCY LIGHT INOPERATIVE. R & R LIGHT, OPS CHECKED SATISFACTORY.
- [SDR JJBA20130715011](https://openairdocs.org/sdr/JJBA20130715011), Jul 15, 2013: BATTERY. INOPERATIVE. RIGHT AFT EGRESS LIGHT, MID CABIN OVERHEAD EXIT SIGN AND AFT CEILING EMERGENCY LIGHTS INOPERATIVE. R & R EMERGENCY LIGHT BATTERY PS4 IRW AMM 33-51-00. OPS CHECK
- [SDR JJBA20130713008](https://openairdocs.org/sdr/JJBA20130713008), Jul 13, 2013: CONNECTOR. LOOSE. FWD EMERGENCY LIGHT NOT WORKING. RESEATED CONNECTOR. OPS CHECKED SATISFACTORY.
- [SDR JJBA20130227011](https://openairdocs.org/sdr/JJBA20130227011), Feb 27, 2013: LIGHT. INOPERATIVE. DURING PREFLIGHT CREW REPORTED THAT A SECTION OF THE FWD FLOOR EMERGENCY LIGHTING STRIP WAS INOPERATIVE. THE GROUND MX CREW R & R THE SECTION OF FLOOR EMERGENCY
- [SDR JJBA20120903001](https://openairdocs.org/sdr/JJBA20120903001), Sep 3, 2012: BATTERY. INOPERATIVE. DURING PREFLIGHT THE CREW NOTICED THE EMERGENCY EXIT SIGN OVER THE MAIN CABIN DOOR DID NOT ILLUMINATE UPON TESTING. GROUND MX CREW REPLACED THE EMERGENCY LIGHT 
- [SDR JJBA20120823002](https://openairdocs.org/sdr/JJBA20120823002), Aug 23, 2012: BATTERY. INOPERATIVE. DURING PRE-FLIGHT, CREW NOTICED THE EMERGENCY EXIT LIGHT ABOVE THE MAIN ENTRANCE DOOR WAS INOPERATIVE. GROUND MX R & R THE EMERGENCY LIGHT BATTERIES. AN OPS TES
- [SDR JJBA20120803001](https://openairdocs.org/sdr/JJBA20120803001), Aug 3, 2012: BATTERY. INOPERATIVE. DURING PRE-FLIGHT CREW NOTICED THE ROW 1 EMERGENCY EXIT LIGHT AND MAIN CABIN DOOR LIGHT INOPERATIVE. GROUND MX CREW RE-SEATED THE EMERGENCY LIGHT BATTERIES IN T
- [SDR JJBA20120730016](https://openairdocs.org/sdr/JJBA20120730016), Jul 30, 2012: BULB. INOPERATIVE. DURING PREFLIGHT CREW NOTICED THE SECOND CEILING EMERGENCY LIGHT WAS INOPERATIVE. R & R THE LIGHT BULB AN PERFORMED AN OPS CHECK WHICH PRODUCED A SATISFACTORY R
- [SDR JJBA20120326011](https://openairdocs.org/sdr/JJBA20120326011), Mar 26, 2012: BATTERY PACK. DISCHARGED. DURING THE PRE-FLIGHT INSPECTION, THE CREW NOTICED THE EMERGENCY LIGHTS FAILED TO ILLUMINATE. CHARGED THE EMERGENCY LIGHT BATTERIES IN REF WITH THE AMM CH 3351.
- [SDR JJBA2011113000101](https://openairdocs.org/sdr/JJBA2011113000101), Nov 30, 2011: BATTERY PACK. INOPERATIVE. FLIGHT CREW REPORTED THAT THE EMERGENCY CEILING LIGHTS IN ROW 1 & 7 WILL NOT TEST. MX R & R ALL BATTERIES. PERFORMED OPS CHECK SATISFACTORY.
- [SDR JJBA2011112800101](https://openairdocs.org/sdr/JJBA2011112800101), Nov 28, 2011: ACM. SMOKE. FLIGHT CREW REPORTED THAT THERE WAS SMOKE IN THE COCKPIT. MX DETERMINED THAT IT WAS THE ACM. R & R ACM & PERFORMED OPS CHECK. CHECKED SATISFACTORY, NO OTHER DEF
- [SDR JJBA2011112300001](https://openairdocs.org/sdr/JJBA2011112300001), Nov 23, 2011: BATTERY PACK. INOPERATIVE. FLIGHT CREW REPORTED THAT THE 1 AND 3 WHITE OVERHEAD EMERGENCY LIGHTS ARE NOT WORKING. MX R & R PS4 BATTERY , OPS CHECKED SATISFACTORY.
- [SDR JJBA351PH331343](https://openairdocs.org/sdr/JJBA351PH331343), May 30, 2011: LIGHT. INOPERATIVE. FLIGHT CREW REPORTED EMERGENCY AISLE PATH LIGHTS BY ROW 8 NOT WORKING. MAINTENANCE CREW REMOVED AND REPLACED EMERGENCY LIGHT STRIP BY ROW 8. PERFORMED OBSERVATI
- [SDR JJBA351PH331300](https://openairdocs.org/sdr/JJBA351PH331300), Apr 30, 2011: CONNECTOR. INOPERATIVE. DURING PREFLIGHT INSP, AIRCREW NOTICED THE EMERGENCY PATH LIGHTING AT ROW 1 WAS INOPERATIVE. GROUND MX CREW RESECURED THE CONNECTOR TO THE INOPERATIVE STRIP LIG
- [SDR JJBA2011241200](https://openairdocs.org/sdr/JJBA2011241200), Jan 29, 2011: BRUSH BLOCK. WORN. WHILE ACFT WAS ON CLIMB-OUT FOR A TEST FLIGHT BEING PERFORMED, THE RT BUSS FAILED. THE RT TRU, RT STALL WARNING AND RT ELEVATOR HORN HEAT ILLUMINATED. MX FOUND 
- [SDR JJBA2010611129](https://openairdocs.org/sdr/JJBA2010611129), Dec 1, 2010: TSCU. MALFUNCTIONED. FLIGHT CREW REPORTED THAT AUTOFEATHER DID NOT ARM ON TAKEOFF, FLIGHT CREW ABORTED TAKEOFF. MX CREW R & R TSCU AND RELAY 6121. PERFORMED OPS CHECK AND TEST FLIGH
- [SDR JJBA200953036](https://openairdocs.org/sdr/JJBA200953036), Nov 12, 2008: SKIN. GOUGED. DURING C-CHECK FOUND GOUGE IN FUSELAGE (JUST FWD OF STA X531.5 BETWEEN STRINGERS 21S AND 22S). REPAIRED IAW REPAIR DOCUMENT 08-53-08 REV.1, DAMAGE TOLERANCE ANA
- [SDR QXEA200700529](https://openairdocs.org/sdr/QXEA200700529), Apr 9, 2007: ECU. WARNING LIGHT. PDX FLIGHT NR 2200 ON TAXI OUT FOR DEPARTURE, DURING BETA BACKUP TEST NR 1 ECU CAUTION. MAINTENANCE RE-SET BETA LOCKOUT CIRCUIT BREAKER IAW FSM. OPERATIONAL CHE
- [SDR QXEA200700209](https://openairdocs.org/sdr/QXEA200700209), Feb 16, 2007: SWITCH. MALFUNCTIONED. SEA FLIGHT NR 2020 - ROLL SPOILER HYDRAULIC CAUTION LIGHT ILLUMINATED ON TAXI OUT. MASTER CAUTION UNABLE TO BE RESET. ALL HYDRAULIC INDICATIONS NORMAL. MAINTENA
- [SDR QXEA200700112](https://openairdocs.org/sdr/QXEA200700112), Jan 27, 2007: UNKNOWN. UNKNOWN. PDX FLIGHT NR 2125, LOUD SCRAPING THUD HEARD WHEN DISCONNECTING FROM TUG RAMP SAID NOSE WHEEL JERKED TO THE SIDE. MAINTENANCE COMPLIED WITH GENERAL VISUAL INSPE
- [SDR QXEA200603020](https://openairdocs.org/sdr/QXEA200603020), Nov 23, 2006: SMOKE DETECTOR. MALFUNCTIONED. SEA FLIGHT NR 2042, DURING CLIMB-OUT, LAV SMOKE DETECTOR WENT OFF FOR ABOUT 30 SECONDS. AIRCRAFT HAD JUST ENTERED AREA MODERATE TURBULENCE. MAINTENANCE PERFORME
- [SDR QXEA200602604](https://openairdocs.org/sdr/QXEA200602604), Oct 1, 2006: BULB. INOPERATIVE. PDX FLIGHT NR 2147, NR 1 AUXILIARY PUMP ADVISORY LIGHT INOP. MAINTENANCE COULD NOT DUPLICATE. AIRCRAFT RETURNED TO SERVICE.
- [SDR QXEA200602497](https://openairdocs.org/sdr/QXEA200602497), Sep 15, 2006: STOP FITTING. WORN. C4 YYC-AIRSTAIR DOOR CUTOUT STOP FITTINGS LOCATIONS WORN. REPAIRED IAW RD8-53-3933 AND RD8-51-103.
- [SDR QXEA200602420](https://openairdocs.org/sdr/QXEA200602420), Sep 13, 2006: CONNECTOR. UNKNOWN. PSC FLIGHT NR 2107 - ELECTRICAL SMELL IN COCKPIT WITH WINDSHIELD HEAT ON. MAINTENANCE REPLACED CONNECTOR AT 1.2 TERMINAL. OPERATIONAL CHECK GOOD. AIRCRAFT RETUR
- [SDR QXEA200602496](https://openairdocs.org/sdr/QXEA200602496), Sep 11, 2006: KEELBEAM. CORRODED. C4 YYC-LT KEEL BEAM TENSION FITTING AT STATION X204.50 HAS DEEP PITTING CORROSION AROUND BOLT HEAD. REPAIRED IAW SRM 51-40-11.
- [SDR QXEA200602086](https://openairdocs.org/sdr/QXEA200602086), Aug 20, 2006: WARNING LIGHT. FALSE INDICATION. PDX FLIGHT 2260, NR 1 ENGINE MANUAL CAUTION LIGHT. MAINTENANCE RESET CIRCUIT BREAKER. OPERATIONAL CHECK GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.
- [SDR QXEA200602073](https://openairdocs.org/sdr/QXEA200602073), Aug 9, 2006: SKIN. CRACKED. PDX C4 CRACK AT RIGHT HAND NACELLE FORWARD OUTBOARD SKIN CUTOUT CORNER FOR RIGHT HAND MAIN LANDING GEAR. REPAIRED IAW RD 8-54-873.
- [SDR QXEA200602081](https://openairdocs.org/sdr/QXEA200602081), Aug 7, 2006: STRUCTURE. CRACKED. PDX C4 .25 INCH CRACK ON LEFT HAND LOWER NACELLE FORWARD INBOARD CORNER. REPAIRED IAW RD 8-54-874.
- [SDR QXEA200602075](https://openairdocs.org/sdr/QXEA200602075), Aug 7, 2006: STRUT. SCRATCHED. PDX C4 NR 2 NACELLE UPPER OUTBOARD ENGINE SUPPORT STRUT LIGHTLY SCRATCHED ON FORWARD END FITTING INBOARD RIB, INBOARD OF BOLT HEAD. REPAIRED IAW HORIZON AIR EA 
- [SDR QXEA200602046](https://openairdocs.org/sdr/QXEA200602046), Aug 6, 2006: STOP FITTING. CHAFED. PDX - C4 CARGO DOOR APERATURE TOP AFT STOP FITTING CHAFED/WORN. REPAIRED IAW RD 8-53-104.
- [SDR QXEA200602043](https://openairdocs.org/sdr/QXEA200602043), Aug 6, 2006: STOP FITTING. CHAFED. PDX - C4 CARGO DOOR APERATURE TOP FORWARD STOP FITTING CHAFED/WORN. REPAIRED IAW RD 8-53-104.
- [SDR QXEA200602042](https://openairdocs.org/sdr/QXEA200602042), Aug 6, 2006: STOP FITTING. CHAFED. PDX - C4 CARGO DOOR APERATURE BOTTOM FORWARD STOP FITTING CHAFED/WORN. REPAIRED IAW RD 8-53-104.
- [SDR QXEA200602036](https://openairdocs.org/sdr/QXEA200602036), Aug 6, 2006: UNKNOWN. CORRODED. PDX - C4 MILD FRETTING CORROSION ON UNDERSIDE OF PANEL 261JT. REPAIRED IAW RD 8-53-3366 AND DHC-8-200 SRM 51-20-36.
- [SDR QXEA200602035](https://openairdocs.org/sdr/QXEA200602035), Aug 6, 2006: UNKNOWN. CORRODED. PDX- C4 MILD FRETTING CORROSION ON UNDERSIDE OF PANEL 261GT. REPAIRED IAW RD 8-53-3366 AND DHC-8-200 SRM 51-20-36.

All 245: https://openairdocs.org/aircraft/N351PH/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 (Dehavilland 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/N351PH/stcs.md

## Related

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

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