# N349PH: 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: 486
- Year built: 1997
- Type: Fixed wing multi engine
- Engine type: Turbo-prop
- Airworthiness: Standard, transport
- Airworthiness date: August 9, 2016
- Certificate issued: January 10, 2012
- Expires: January 31, 2028
- Mode S code: A3E00A
- Registered owner: [Bam Leasing LLC](https://openairdocs.org/faa-owner/BAM%20LEASING%20LLC)
- Location: [California, MD](https://openairdocs.org/faa-place/MD/California)
- Owner type: LLC
- Owner's area on the map: 38.2925° N, 76.5277° W: Placed by OpenAirDocs at the center of ZIP code 20619, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=349PH
- Page: https://openairdocs.org/aircraft/N349PH

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/N349PH/ads.md

## Information bulletins (advisory)

None matched.

## NTSB investigations

None matched to N349PH.

## 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 20000215016079I](https://openairdocs.org/incident/20000215016079I), Feb 15, 2000: Dhav DHC8202 (N349PH), Redmond, OR. (-23)Aircraft experienced elevator trim freezing @ flight level 230. Outside air temp was -40C. When aircraft decended trim became operable. Small amounts of…
- [Incident 20000208001839I](https://openairdocs.org/incident/20000208001839I), Feb 8, 2000: Dhav DHC8202 (N349PH), Victoria, Bc, CN. (-23) Aircraft experienced an autofeather on #2 engine shortly after rotation. Aircraft returned to the field without event. Maintenance discovered cannon plug…

## Service difficulty reports (220, 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 QXEA2008110401158](https://openairdocs.org/sdr/QXEA2008110401158), Oct 30, 2008: HYDRAULIC LINE. FAILED. PDX - ON DOING DAILY CHECKS, PERFORMED PTU TEST AND LOST ALL HYD ON THE NR 2 SYSTEM. HYDRAULIC FLUID IS ALL OVER ROWS 3/4/5 SEATS. ENGINE SHUTDOWN WITH IN 1 MIN
- [SDR QXEA2008102301140](https://openairdocs.org/sdr/QXEA2008102301140), Oct 20, 2008: PRESSURE SWITCH. MALFUNCTIONED. PDX- NR 2 ENG HYD PUMP CAUTION ILLUMINATED. CAUTION REMAINED ILLUMINATED THROUGHOUT LANDING. TAXI AND PARKING. NO LOSS OF HYD PRESS OR QTY. PERFORMED ALTERNATE 
- [SDR QXEA200800535](https://openairdocs.org/sdr/QXEA200800535), May 31, 2008: SWITCH. MALFUNCTIONED. PDX - FLIGHT 2193, AUTOFEATHER ARM LIGHT FLICKERING AND SHOWING AS "ARM" WITHOUT THE BUTTON BEING SELECTED. DURING CLIMB AND CRUISE. MAINTENANCE REPLACED THE AU
- [SDR QXEA200800234](https://openairdocs.org/sdr/QXEA200800234), Mar 3, 2008: SERVO. INOPERATIVE. PDX - FLIGHT 2122 - ENGINE "SURGE" NOISE INTERMITTENT ABOUT EVERY 5-6 MINUTES DURING CLIMB. RTF PDX MAINTENANCE FOUND NR 1 ENGINE IBV SERVO INOPERATIVE, REMOVED
- [SDR QXEA200800086](https://openairdocs.org/sdr/QXEA200800086), Jan 14, 2008: STRINGER CLIP. CORRODED. PDX - C1 CHECK - X466 AND STRINGER 31R SUSPECT CORROSION AT CLIP RADIUS. MAINTENANCE BLENDED OUT CORROSION, REMAINED WITHIN LIMITS, INSPECTED AND NO CRACKS NOTE
- [SDR QXEA2008OOO70](https://openairdocs.org/sdr/QXEA2008OOO70), Jan 14, 2008: SEAT TRACK. CORRODED. PDX - C1 CHECK - RIGHT OUTBOARD SEAT TRACK NR 10 HAS 2 SMALL AREAS OF CORROSION AT APPROX X310. MAINTENANCE REMOVED CORROSION, INSPECTED BLENDED AREA AND NO CRA
- [SDR QXEA200800097](https://openairdocs.org/sdr/QXEA200800097), Jan 14, 2008: SEAT TRACK. CORRODED. PDX - C1 CHECK - SUSPECT CORROSION AROUND 2 SKIN RIVETS X520 TO X522 BELOW SEAT TRACK NR 2. MAINTENANCE REMOVED RIVETS, BLENDED OUT CORROSION, INSPECTED, REMAIN
- [SDR QXEA200800096](https://openairdocs.org/sdr/QXEA200800096), Jan 14, 2008: SEAT TRACK. GOUGED. PDX - C1 CHECK - SEAT TRACK NR 5 IS GOUGED X476 TO X 486. MAINTENANCE BLENDED OUT GOUGE. INSPECTED, REMAINED WITHIN LIMITS AND NO CRACK NOTED. RESTORED FINISH T
- [SDR QXEA200800095](https://openairdocs.org/sdr/QXEA200800095), Jan 14, 2008: SEAT TRACK. GOUGED. PDX - C1 CHECK - SEAT TRACK NR 5 IS GOUGED X510 TO 520. MAINTENANCE BLENDED OUT GOUGE ON TRACK, INSPECTED REMAINED WITHIN LIMITS AND NO CRACKS NOTED. RESTORED F
- [SDR QXEA200800090](https://openairdocs.org/sdr/QXEA200800090), Jan 14, 2008: SEAT TRACK. CORRODED. PDX - C1 CHECK - RIVET HEADS ABOVE INNER SKIN ON WEB X528 TO X534 ON THE RIGHT SIDE BELOW SEAT TRACK 8/9 SUSPECT LIGHT CORROSION. MAINTENANCE REMOVED RIVETS AND
- [SDR QXEA200800081](https://openairdocs.org/sdr/QXEA200800081), Jan 14, 2008: SKIN. DENTED. PDX - C1 CHECK - SCRATCH AND SMALL DENT AT APPROXIMATELY STA X106.00 AND APPROXIMATELY 4 INCHES ABOVE PANEL 112BR RIGHT EXTERNAL FUSELAGE. MAINTENANCE BLENDED A
- [SDR QXEA200800092](https://openairdocs.org/sdr/QXEA200800092), Jan 14, 2008: SHEAR TIE. CORRODED. PDX - C1 CHECK - X545 STRINGER 31R SUSPECT CORROSION AT SKIN CLIP. MAINTENANCE REMOVED RIVETS AND BLENDED OUT CORROSION FROM CLIP, BLEND REMAINED WITHIN LIMITS,
- [SDR QXEA200800109](https://openairdocs.org/sdr/QXEA200800109), Jan 14, 2008: SUPPORT ANGLE. CORRODED. PDX - C1 CHECK - CORROSION UNDER AFT CARGO DOOR THRESHOLD SUPPORT ANGLE APPROXIMATELY STA X600 STRINGER 28L. MAINTENANCE REMOVED RIVETS BLENDED CORROSION, INSPE
- [SDR QXEA200800107](https://openairdocs.org/sdr/QXEA200800107), Jan 14, 2008: SKIN. CORRODED. PDX - C1 CHECK - SPOT OF CORROSION ON THE INNER SKIN AROUND RIVET HOLE FORWARD OF FRAME STA 201 OUTBOARD OF STRINGER 31L. MAINTENANCE REMOVED MINOR CORROSION, I
- [SDR QXEA200800105](https://openairdocs.org/sdr/QXEA200800105), Jan 14, 2008: SEAT TRACK. CORRODED. PDX - C1 CHECK - SUSPECT CORROSION AROUND RIVET ON VERTICAL FRAME SUPPORT FOR NR 4 SEAT TRACK AT STA X370.00 INBOARD OF STRINGER 31L BOTTOM MOST INBOARD RIVET. 
- [SDR QXEA200800100](https://openairdocs.org/sdr/QXEA200800100), Jan 14, 2008: SKIN. DENTED. PDX - C1 CHECK - FORE RUDDER HAS A 1/4 BY 1/2 DENT ON RIGHT SIDE 13 INCHES FROM TOP EDGE 4 INCHES FROM TRAILING EDGE. MAINTENANCE CUT OUT SKIN DAMAGE, INSPECTED
- [SDR QXEA200800099](https://openairdocs.org/sdr/QXEA200800099), Jan 14, 2008: SEAT TRACK. CORRODED. PDX - C1 CHECK - SEAT TRACK NR 11 AT X496 HAS A CORROSION PIT ON TOP ANGLE. MAINTENANCE BLENDED OUT THE CORROSION, INSPECTED, REMAINED WITHIN LIMITS WITH NO CRA
- [SDR QXEA200800098](https://openairdocs.org/sdr/QXEA200800098), Jan 14, 2008: SEAT TRACK. CORRODED. PDX - C1 CHECK - SUSPECT LIGHT CORROSION FORMING ON WEB TIE RIVET HEADS BELOW FLOOR AND SEAT TRACK. MAINTENANCE REMOVED RIVETS AND BLENDED OUT CORROSION, INSPEC
- [SDR QXEA200800082](https://openairdocs.org/sdr/QXEA200800082), Jan 14, 2008: SEAT TRACK. CORRODED. PDX - C1 CHECK - NR 4 SEAT TRACK HAS CORROSION AT CAMLOCK RECEPTACLE UNDER DRIP TRAY AT STA X240. MAINTENANCE REMOVED CORRODED SEAT TRACK AND INSTALLED NEW SEAT
- [SDR QXEA200800085](https://openairdocs.org/sdr/QXEA200800085), Jan 14, 2008: SEAT TRACK. CORRODED. PDX - C1 CHECK - SEAT TRACK NR 5 AT X468 HAS 2 CORROSION PITS ON INNER FLOORBOARD FLANGE. MAINTENANCE BLENDED OUT CORROSION, REMAINED WITHIN LIMITS, INSPECTED A
- [SDR QXEA200800110](https://openairdocs.org/sdr/QXEA200800110), Jan 14, 2008: SKIN. CORRODED. PDX - C1 CHECK - LAV SERVICE DOOR APERATURE AFT LOWER CORNER CORRODED AROUND FASTENER. MAINTENANCE REMOVED LAV SERVICE DOOR CUT OUT DAMAGED AREA, FABRICATED REP
- [SDR QXEA200800106](https://openairdocs.org/sdr/QXEA200800106), Jan 14, 2008: THRESHOLD. CORRODED. PDX - C1 CHECK - MAIN CABIN DOOR THRESHOLD HAS LIGHT CORROSION AT 5 EA NUTPLATES. MAINTENANCE REMOVED MCD THRESHOLD AND NUTPLATES. REMOVED LIGHT SURFACE CORROSI
- [SDR QXEA200800101](https://openairdocs.org/sdr/QXEA200800101), Jan 14, 2008: FLAP TRACK. CORRODED. PDX - C1 CHECK - RIGHT OUTBOARD FLAP NR 4 FLAP TRACK LOWER SIDE THERE ARE TWO AREAS OF ROLLER CHAFE DAMAGE WITH PITTING CORROSION IN BETWEEN. MAINTENANCE BLENDE
- [SDR QXEA200800111](https://openairdocs.org/sdr/QXEA200800111), Jan 14, 2008: SEAT TRACK. CORRODED. PDX - C1 CHECK - NR 1 SEAT TRACK WEB TO FRAME ANGLE CLIP IS CRACKED FORWARD SIDE OF FRAME 312. MAINTENANCE REMOVED AND INSTALLED NEW CLIP.
- [SDR QXEA200800108](https://openairdocs.org/sdr/QXEA200800108), Jan 14, 2008: INTERCOSTAL. CORRODED. PDX - C1 CHECK - CORROSION ON AVIONICS RACK INTERCOSTAL AT FS X202 TO FS 198.300 OUTBOARD OF STRINGER 31L. MAINTENANCE REMOVED CORROSION, INSPECTED, BLENDED ARE
- [SDR QXEA200800094](https://openairdocs.org/sdr/QXEA200800094), Jan 14, 2008: SEAT TRACK. CORRODED. PDX - C1 CHECK - SEAT TRACK NR 5 X447 TO X457 IS GOUGED. MAINTENANCE BLENDED OUT GOUGE ON SEAT TRACK, INSPECTED AND REMAINED WITHIN LIMITS, NO CRACKS NOTED. RES
- [SDR QXEA200800093](https://openairdocs.org/sdr/QXEA200800093), Jan 14, 2008: SEAT TRACK. CORRODED. PDX - C1 CHECK - SEAT TRACK 36 AT X545 HAS PIT OF CORROSION THAT IS OUT OF LIMITS AT .028 DEEP. MAINTENANCE REMOVED SEAT TRACK AND INSTALLED NEW SEAT TRACK.
- [SDR QXEA200800087](https://openairdocs.org/sdr/QXEA200800087), Jan 14, 2008: STRINGER CLIP. CORRODED. PDX - C1 CHECK - X468 AND STRINGER 31R SUSPECT CORROSION AT CLIP EDGE. MAINTENANCE BLENDED OUT CORROSION, REMAINED WITHIN LIMITS, INSPECTED AND NO CRACKS NOTED.
- [SDR QXEA200800079](https://openairdocs.org/sdr/QXEA200800079), Jan 14, 2008: SEAT TRACK. CORRODED. PDX - C1 CHECK - RIGHT OUTBOARD SEAT TRACK NR 10 HAS 2 SMALL AREAS OF CORROSION AT APPROX X310. MAINTENANCE BLENDED OUT CORROSION, WITHIN LIMITS AND NO CRACKS N
- [SDR QXEA200800083](https://openairdocs.org/sdr/QXEA200800083), Jan 14, 2008: SEAT TRACK. CORRODED. PDX - C1 CHECK - NR 2 SEAT TRACK HAS VERY LIGHT PITTING IN THE CHANNEL AT APPROXIMATELY X488. MAINTENANCE BLENDED THE PITTED AREA, REMAINED WITHIN LIMITS AND IN
- [SDR QXEA200800102](https://openairdocs.org/sdr/QXEA200800102), Jan 14, 2008: FLAP TRACK. CORRODED. PDX - C1 CHECK - RIGHT OUTBOARD FLAP NR 4 FLAP TRACK INBOARD SIDE LOWER SURFACE OF UPPER FLANGE. THERE IS PITTING CORROSION AT ROLLER CONTACT AREA. MAINTENANCE 
- [SDR QXEA200800091](https://openairdocs.org/sdr/QXEA200800091), Jan 14, 2008: SKIN. CORRODED. PDX - C1 CHECK - X534 AND STRINGER 31R SUSPECT CORROSION AT SKIN CLIP. MAINTENANCE REMOVED RIVETS AND BLENDED OUT CORROSION AT CLIP, REMAINED WITHIN LIMITS AND 
- [SDR QXEA200800084](https://openairdocs.org/sdr/QXEA200800084), Jan 14, 2008: SEAT TRACK. CORRODED. PDX -C1 CHECK - SEAT TRACK NR 3 HAS A CORROSION PIT IN THE CHANNEL AT X544. MAINTENANCE BLENDED THE AREA, REMAINED WITHIN LIMITS AND INSPECTED, NO CRACKS NOTED.
- [SDR QXEA200800080](https://openairdocs.org/sdr/QXEA200800080), Jan 14, 2008: SEAT TRACK. CORRODED. PDX - C1 CHECK - RIGHT OUTBOARD SEAT TRACK NR 10 IS CORRODED ON THE FRONT OUTBOARD CORNER AT APPROX X262. MAINTENANCE BLENDED OUT CORRODED AREA, WITHIN LIMITS A
- [SDR QXEA200800103](https://openairdocs.org/sdr/QXEA200800103), Jan 14, 2008: FLAP TRACK. DAMAGED. PDX - C1 CHECK - RIGHT OUTBOARD FLAP AREA NR 5 FLAP TRACK. THERE ARE TWO ROLLER CHAFE AREAS ON THE UPPER SURFACE. MAINTENANCE BLENDED AREA, INSPECTED, REMAINED 
- [SDR QXEA200800078](https://openairdocs.org/sdr/QXEA200800078), Jan 14, 2008: SEAT TRACK. CORRODED. PDX - C1 CHECK - RIGHT OUTBOARD SEAT TRACK NR 10 HAS A SMALL AREA OF CORROSION AT APPROX X330. MAINTENANCE BLENDED CORRODED AREA, WITHIN LIMITS AND NO CRACKS NO
- [SDR QXEA200800077](https://openairdocs.org/sdr/QXEA200800077), Jan 14, 2008: SEAT TRACK. CORRODED. PDX - C1 CHECK - RIGHT OUTBOARD SET TRACK NR 10 HAS SMALL AREA OF CORROSION AT APPROX X346. MAINTENANCE BLENDED CORRODED AREA, WITHIN LIMITS AND NO CRACKS NOTED
- [SDR QXEA200800076](https://openairdocs.org/sdr/QXEA200800076), Jan 14, 2008: SEAT TRACK. CHAFED. PDX - C1 CHECK - TOP OF RIGHT OUTBOARD SEAT TRACK NR 10 IS CHAFED AT APPROX X362. MAINTENANCE BLENDED CHAFED AREA, WITHIN LIMITS AND NO CRACKS NOTED. APPLIED AL
- [SDR QXEA200800075](https://openairdocs.org/sdr/QXEA200800075), Jan 14, 2008: SEAT TRACK. CORRODED. PDX - C1 CHECK - RIGHT OUTBOARD SEAT TRACK NR 10 HAS A SMALL AREA OF CORROSION AT APPROX X364. MAINTENANCE REMOVED CORROSION, INSPECTED BLENDED AREA, WITHIN LIM
- [SDR QXEA200800074](https://openairdocs.org/sdr/QXEA200800074), Jan 14, 2008: SEAT TRACK. GOUGED. PDX - C1 CHECK - RIGHT INBOARD SEAT TRACK NR 7 HAS APPROX .060 GOUGE ON THE OUTBOARD FLANGE AT APPROX X256. MAINTENANCE REMOVED TRACK AND INSTALL NEW TRACK.
- [SDR QXEA200800073](https://openairdocs.org/sdr/QXEA200800073), Jan 14, 2008: BRACKET. CRACKED. PDX - C1 CHECK - LT WING INBOARD LEADING EDGE LOWER OUTBOARD BRACKET CRACKED. MAINTENANCE REMOVED AND REPLACE LEADING EDGE BRACKET.
- [SDR QXEA200800072](https://openairdocs.org/sdr/QXEA200800072), Jan 14, 2008: FLOORBEAM. CORRODED. PDX - C1 CHECK - FLOORBOARD SUPPORT ANGLE CORRODED AT APPROX STA X599.00, Y26.00 RT TO Y31.00 RT, Y 0.00 TO Y 8.00 RT, Y 0.00 TO Y 6.00 LT. MAINTENANCE REMOVED 
- [SDR QXEA200800069](https://openairdocs.org/sdr/QXEA200800069), Jan 14, 2008: NUT PLATE. CORRODED. PDX - C1 CHECK - NUTPLATE AND MOUNTING SURFACE AT STA X599.00 Y21.00 LT IS CORRODED. MAINTENANCE REMOVED NUTPLATE AND REMOVED CORROSION. INSPECTED BLENDED AREA,
- [SDR QXEA200800068](https://openairdocs.org/sdr/QXEA200800068), Jan 14, 2008: SUPPORT ANGLE. CORRODED. PDX - C1 CHECK - SUPPORT ANGLE AT APPROX STA X600.00 AT DOOR THRESHOLD AREA HAS CORROSION ON NUTPLATES AND MOUNTING SURFACE. MAINTENANCE REMOVED SUPPORT ANGLE A
- [SDR QXEA200800067](https://openairdocs.org/sdr/QXEA200800067), Jan 14, 2008: SUPPORT ANGLE. CORRODED. PDX - C CHECK - SUPPORT ANGLE AT APPROXIMATELY STA X594.00 AT DOOR THRESHOLD AREA HAS CORROSION ON NUTPLATES AND MOUNTING SURFACE. MAINTENANCE REMOVED NUTPLATES
- [SDR QXEA200800066](https://openairdocs.org/sdr/QXEA200800066), Jan 14, 2008: SUPPORT ANGLE. CORRODED. PDX - C CHECK - SUPPORT ANGLE AT APPROX X586.00 AT DOOR THRESHOLD AREA HAS CORROSION ON NUTPLATES AND MOUNTING SURFACE. MAINTENANCE REMOVED NUTPLATES AND REMOVE
- [SDR QXEA200800065](https://openairdocs.org/sdr/QXEA200800065), Jan 14, 2008: SUPPORT ANGLE. CORRODED. PDX - C CHECK - SUPPORT ANGLE AT APPROX STA X569.00 AT DOOR THRESHOLD AREA HAS CORROSION ON NUTPLATES AND MOUNTING SURFACE. MAINTENANCE REMOVED NUTPLATES AND RE
- [SDR QXEA200800064](https://openairdocs.org/sdr/QXEA200800064), Jan 14, 2008: SUPPORT ANGLE. CORRODED. PDX - C CHECK - SUPPORT ANGLE AT APPROXIMATELY STA X553.00 AT DOOR THRESHOLD HAS CORROSSION ON NUTPLATES AND MOUNTING SURFACE. REMOVED NUTPLATES AND REMOVED COR
- [SDR QXEA200702046](https://openairdocs.org/sdr/QXEA200702046), Dec 30, 2007: SMOKE DETECTOR. MALFUNCTIONED. MFR - ON TAXI THE LAV SMOKE DETECTOR WENT OFF. RETURNED TO THE GATE AND RESET THE DETECTOR. MAINTENANCE COULD NOT DUPLICATE PROBLEM. OPERATIONAL CHECKS GOOD. AI
- [SDR QXEA200702043](https://openairdocs.org/sdr/QXEA200702043), Dec 30, 2007: ENGINE. MALFUNCTIONED. MFR - FLIGHT 2150 - SHORTLY AFTER TAKEOFF, THE LAV SMOKE DETECTOR WENT OFF. THE FLIGHT ATTENDANT CHECKED AND SAW NO SMOKE, BUT DID SMELL A HOT DUSTY SMELL. RETU

All 220: https://openairdocs.org/aircraft/N349PH/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/N349PH/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

---
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.