# N449YV: 1996 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: 449
- Year built: 1996
- Type: Fixed wing multi engine
- Engine type: Turbo-prop
- Airworthiness: Standard, transport
- Airworthiness date: December 27, 1996
- Certificate issued: July 23, 2025
- Expires: July 31, 2032
- Mode S code: A56E46
- 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=449YV
- Page: https://openairdocs.org/aircraft/N449YV

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/N449YV/ads.md

## Information bulletins (advisory)

None matched.

## NTSB investigations (2)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB WPR09LA211](https://openairdocs.org/ntsb/WPR09LA211), Apr 21, 2009: De Havilland DHC-8 (N449YV), Phoenix, AZ, substantial damage. Probable cause: The failure of ramp personnel and the flight crew to maintain clearance from ground equipment while taxiing. Contributing to the accident was the improper positioning of the ground equipment.
- [NTSB FTW98LA353](https://openairdocs.org/ntsb/FTW98LA353), Jul 27, 1998: de Havilland DH-8-202 (N449YV), Telluride, CO, substantial damage. Probable cause: The inadequate chocks and inadequate chocking procedures by the operator. Factors were the unavailability of the parking brake and sloping terrain.

## FAA accident and incident reports (3)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Accident 20090420004609A](https://openairdocs.org/incident/20090420004609A), Apr 20, 2009: Dhav DHC8202 (N449YV), Phoenix, AZ, Substantial damage. (-23) Air suttle flt 2957, struck a ground power unit with right engine propeller while taxiing into gate B24 at Phoenix, AZ.
- [Incident 19990427020029I](https://openairdocs.org/incident/19990427020029I), Apr 27, 1999: Dhav DHC8202 (N449YV), Philipsburg, PA. On approach landing gear down light would not illuminate. Crew reactivated gear lever and reset, light illuminated. Trouble shooted after landing and found bad…
- [Accident 19980727030109A](https://openairdocs.org/incident/19980727030109A), Jul 27, 1998: Dhav DHC8202 (N449YV), Telluride, CO, Substantial damage. (.19) See NTSB #FTW98LA353

## Service difficulty reports (60, 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 HKGA20220314004](https://openairdocs.org/sdr/HKGA20220314004), Mar 13, 2022: SPACER. CRACKED. BLEED SYSTEM PRSOV SPACE MOUNTING EARS FOUND CRACKED. REMOVED SPACER, REPLACED CRACKED ANGLES P/N 85531139-101 & 85531139-105. RE-INSTALLED REPAIRED SPACER.
- [SDR MASA2010060300599](https://openairdocs.org/sdr/MASA2010060300599), Jun 3, 2010: CONTROL BOX. FAULTY. EMERGENCY AISLE LIGHT AT ROW 4-9 OUT. MX R2 EMERGENCY LIGHTING CONTROL BOX, BATTERY CHARGER 3 AND ALL BATTERY PACKS.
- [SDR MASA2010052300542](https://openairdocs.org/sdr/MASA2010052300542), May 23, 2010: POWER SUPPLY. INOPERATIVE. RIGHT FWD FUSELAGE EMERGENCY LIGHT INOP. REMOVED AND REPLACED NR 2 EMERGENCY LIGHT POWER SUPPLY AND BATTERY ASSY, EMERGENCY LIGHT SYS OPS CHECKED GOOD.
- [SDR MASA2010040100281](https://openairdocs.org/sdr/MASA2010040100281), Apr 1, 2010: WIRE. DAMAGED. FWD E-LIGHT TRACK OUT. REPAIRED WIRING.
- [SDR MASA2010032400245](https://openairdocs.org/sdr/MASA2010032400245), Mar 24, 2010: LIGHT. INOPERATIVE. RIGHT FWD EGRESS LIGHT INOP. RELAMPED EGRESS LIGHT.
- [SDR MASA2010030700190](https://openairdocs.org/sdr/MASA2010030700190), Mar 7, 2010: LIGHT. INOPERATIVE. F/A'S GREEN E-LIGHT SWITCH OUT. RELAMPED EMERGENCY LIGHT.
- [SDR MASA2008102500751](https://openairdocs.org/sdr/MASA2008102500751), Oct 25, 2008: LIGHT. MALFUNCTIONED. ASH FLT 2767 MRY - ALL EMERGENCY LIGHTS WILL SHUT OFF. MX RESET SYSTEM WITH THE CREW.
- [SDR MASA200700825](https://openairdocs.org/sdr/MASA200700825), Nov 28, 2007: SIGN. LOOSE. ASH FLT 2950 PHX, EXIT SIGN AT PAX DOOR LOOSE. SECURED SIGN ASSEMBLY.
- [SDR MASA200700812](https://openairdocs.org/sdr/MASA200700812), Nov 20, 2007: BOLT. LOOSE. ASH FLT 2960 - PHX - GRINDING NOISE IN THE PAX DOOR WHEN TRYING TO CLOSE IT. RESECURED UPPER OUTER ATTACH BOLT, OPS CHECK GOOD.
- [SDR MASA200700440](https://openairdocs.org/sdr/MASA200700440), Jul 18, 2007: LIGHT. MALFUNCTIONED. ASH 2843 PHX. EMERGENCY LIGHTS WILL NOT TURN OFF. MX RESET SYSTEM. NO FURTHER DEFECTS NOTED.
- [SDR MASA200700134](https://openairdocs.org/sdr/MASA200700134), Mar 4, 2007: UNKNOWN. ODOR. ASH 2855 PHX. LOUD NOISE, SMOKE AND SMOKY SMELL. MX PERFORMED HIGH POWERED MAINT RUN. SYSTEM OP CHECK GOOD AND COULD NOT DUPLICATE THE DISCREPANCY.
- [SDR MASA200602505](https://openairdocs.org/sdr/MASA200602505), Oct 30, 2006: WIRE. DAMAGED. ASH 2894 PHX. SMOKE COMING FROM D/C POWER PLUG. MX RE-WIRED THE DC ELECTRICAL SYSTEM.
- [SDR MASA200601972](https://openairdocs.org/sdr/MASA200601972), Jul 28, 2006: TORQUE SENSOR. FAULTY. ASH 6253 DRO. FLAP DRIVE CAUTION IN FLIGHT. THE AIRCRAFT WAS FERRIED TO PHX WHERE MAINTENANCE REMOVED AND REPLACED THE TORQUE SENSOR.
- [SDR MASA200601861](https://openairdocs.org/sdr/MASA200601861), Jul 15, 2006: CONNECTOR. CORRODED. ASH 6286 PHX - FLAP DRIVE CAUTION MESSAGE. MX FOUND THE FLAP DRIVE CONNECTOR CORRODED. MX CLEANED CORROSION AND SECURED CANNON PLUG.
- [SDR MASA200601678](https://openairdocs.org/sdr/MASA200601678), Jun 23, 2006: LIGHT. INOPERATIVE. ASH 6251 DRO. EMERGENCY EXIT LIGHT AT ROW 4 INOP. MX RELAMPED EXIT SIGN.
- [SDR MASA200600290](https://openairdocs.org/sdr/MASA200600290), Feb 1, 2006: STARTER GEN. MALFUNCTIONED. ASH 6209 PHX. NR 2 DC GENERATOR CAUTION LIGHT ON TAXI OUT. MX PLACED ON MEL. MX REPLACED GEN.
- [SDR MASA200600296](https://openairdocs.org/sdr/MASA200600296), Feb 1, 2006: GENERATOR. WARNING LIGHT. ASH 7077 PHX - RT AC GEN CAUTION LIGHT CAME ON DURING TAKEOFF ROLL. MAINTENANCE REMOVED AND REPLACED THE GEN. OPS CHECK GOOD.
- [SDR MASA200500804](https://openairdocs.org/sdr/MASA200500804), Oct 14, 2005: POWER UNIT. MALFUNCTIONED. NR 2 ENGINE HYD CAUTION. MAINTENANCE REMOVED AND REPLACED SPU AND SERVICED HYDRAULIC SYSTEM.
- [SDR MASA200500519](https://openairdocs.org/sdr/MASA200500519), Jul 5, 2005: GENERATOR. FAILED. NR 1 DC GEN LIGHT IN FLIGHT. NR 1 DC GENERATOR REPLACED.
- [SDR MASA200500352](https://openairdocs.org/sdr/MASA200500352), May 13, 2005: TSCU. MALFUNCTIONED. ASH 6106 PHX TO PSP. THE AIRCRAFT RETURNED TO THE GATE WHEN THE CREW REPORTED THAT THE NR 1 ENGINE/PROP TORQUE WENT TO 100 PERCENT TORQUE UNCOMMANDED WHEN ADVAN
- [SDR MASA200500159](https://openairdocs.org/sdr/MASA200500159), Feb 26, 2005: CONNECTOR. DIRTY. CLOSED/SUP - ASH 6322 PHX - EMERGENCY LIGHTS REMAIN ON WHEN BOTH LIGHT SWITCHES ON/ARM ARE IN THE OFF POSITION. PHX MAINTENANCE TROUBLESHOOTING WITH GJT MAINTEN
- [SDR MASA200400617](https://openairdocs.org/sdr/MASA200400617), Oct 31, 2004: LAMP. INOPERATIVE. THE AIRCRAFT RETURNED TO GATE WITH FORWARD SECTION OF EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE TROUBLESHOT AND RELAMPED THE SYSTEM. OPS CHECKED GOOD.
- [SDR MASA200400449](https://openairdocs.org/sdr/MASA200400449), Aug 12, 2004: INDICATOR. INOPERATIVE. THE CREW RETURNED THE AIRCRAFT TO THE GATE DUE TO THE LEFT SPOILER INDICATING OPPOSITE OF DEFLECTION. CONFIRMED THAT THE FAULT WAS AN INDICATION ERROR AND FERRI
- [SDR MASA200400076](https://openairdocs.org/sdr/MASA200400076), Feb 8, 2004: WIRE. LOOSE. CREW REPORTED THE EMERGENCY LIGHT FLOOR PATH LIGHTS INOPERATIVE. MECHANIC TIGHTENED LEADS ON EMERGENCY LIGHTS. OPS CHECK GOOD. NO PARTS USED.
- [SDR MASA200300420](https://openairdocs.org/sdr/MASA200300420), Oct 20, 2003: BATTERY. DISCHARGED. PHX-DRO CREW REPORTED F/A EMERGENCY FLASHLIGHT INOPERATIVE. MECHANIC REPLACED THE BATTERY.
- [SDR MASA200200012](https://openairdocs.org/sdr/MASA200200012), Oct 4, 2002: POWER SUPPLY. DURING LINE CHECK INSPECTION, THE #2 CABIN EMERGENCY LIGHT WOULD NOT ILLUMINATE. THE #2 EMERGENCY LIGHT POWER SUPPLY WAS REPLACED WITH NO FURTHER DEFECTS NOTED.
- [SDR M02121](https://openairdocs.org/sdr/M02121), Aug 12, 2002: CONNECTOR. LOOSE. RETURNED TO THE GATE. NR 2 ENGINE HAD SIGNIFICANT RPM DROP WHEN POWER LEVERS MOVED FROM DISK TO FLIGHT IDLE. MECHANIC SECURED LOOSE CONNECTOR PLUG. OPS CHECK GO
- [SDR M02022](https://openairdocs.org/sdr/M02022), Feb 9, 2002: POWER SUPPLY. INOPERATIVE. DURING ROUTINE MAINTENANCE, SEVERAL EMERGENCY EXIT LIGHTS FAILED TO ILLUMINATE. MECHANIC REPLACED THE NR2 EMERGENCY POWER SUPPLY. OPS CHECK GOOD. THE AIRCRAFT W
- [SDR 2002F00218](https://openairdocs.org/sdr/2002F00218), Nov 27, 2001: STRUT. DEFECTIVE. FLT NR 6253 - ON ARRIVAL IN DRO, THE CREW COULD ONLY GET THE PASSENGER DOOR TO OPEN ONE-THIRD OF THE WAY. MAINTENANCE REPLACED BOTH STRUTS. OPS CHECKS GOOD. (M)
- [SDR 2001F00442](https://openairdocs.org/sdr/2001F00442), Sep 17, 2001: BATTERY PACK. INOPERATIVE. FLT 6330 - PHX-BFL - DURING TAXI-OUT, THE CREW HAD A MAIN DOOR EMERGENCY EXIT SIGN, ROW 1D EMERGENCY EXIT SIGN AND OVERHEAD EMERGENCY LIGHT INOPERATIVE. THE AIR
- [SDR MASA01035](https://openairdocs.org/sdr/MASA01035), Apr 6, 2001: POWER SUPPLY. DISCHARGED. DURING ROUTINE MAINTENANCE DISCOVERED F/A''S GALLEY EMERGENCY EXIT, RIGHT FORWARD EMERGENCY EXIT AND CEILING FORWARD AFT LIGHTS INOPERATIVE. REMOVED AND REPLACE
- [SDR MASA01028](https://openairdocs.org/sdr/MASA01028), Mar 20, 2001: FUEL CONTROL. FAILED. FLT 6323 - GJT-PHX - RETURNED TO FIELD AFTER SHUTTING DOWN ENGINE NR 2 DUE TO NO RESPONSE TO POWER LEVER MOVEMENT. AFTER AN UNEVENTFUL LANDING MAINTENANCE WAS C
- [SDR MASA00170](https://openairdocs.org/sdr/MASA00170), Dec 12, 2000: BATTERY. DISCHARGED. FLT 6202 - FLG-PHX - DURING THE PRE-FLIGHT INSPECTION, THE CREW NOTICED THAT THE EMERGENCY EXIT LIGHTING AT ROW 1 C/D AND FLIGHT ATTENDANT JUMP SEAT WOULD NOT I
- [SDR MASA99133](https://openairdocs.org/sdr/MASA99133), Aug 10, 1999: BULB. MISSING. FLT 6230 - PHX-MTJ - DURING PREFLIGHT ACCEPTANCE CHECK, THE CREW REPORTED THE RIGHT SIDE EMERGENCY EXIT PLACARD LENSE WAS MISSING. MAINTENANCE REMOVED AND REPLA
- [SDR MASA98230](https://openairdocs.org/sdr/MASA98230), Dec 31, 1998: POWER SUPPLY. DISCHARGED. FLT 6251 - PHX-DRO - PRIOR TO DEPARTURE, CREW REPORTED THAT SEVERAL EMERGENCY LIGHTS WOULD NOT ILLUMINATE. MAINTENANCE REPLACED ALL THE EMERGENCY BATTERIES. AIR
- [SDR MASA98226](https://openairdocs.org/sdr/MASA98226), Dec 17, 1998: POWER SUPPLY. DISCHARGED. FLT 6230 - PHX-MTJ - AS AIRCRAFT TAXIED FROM THE GATE, THE FLIGHT ATTENDANT TESTED THE EMERGENCY LIGHTS AND THEY WERE INOPERATIVE. AIRCRAFT WAS RETURNED TO GATE
- [SDR MASA98222](https://openairdocs.org/sdr/MASA98222), Dec 10, 1998: BULB. FAILED. FLT 6230 - PHX-MTJ - PRIOR TO DEPARTURE, CREW REPORTED TWO OVERHEAD EMRGENCY LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED THE BULBS. OPS CHECKED GOOD. AIRCRAFT
- [SDR MASA98204](https://openairdocs.org/sdr/MASA98204), Nov 17, 1998: BULB. FAILED. DURING A ROUTINE LINE CHECK INSPECTION, MAINTENANCE PERSONNEL FOUND THE NR 2 CABIN OVERHEAD EMERGENCY EXIT LIGHT FAILED TO ILLUMINATE. REMOVED AND REPLACED BULB
- [SDR MASA98198](https://openairdocs.org/sdr/MASA98198), Nov 4, 1998: BULB. FAILED. FLT 6322 - PHX-GJT - WHILE THE AIRCRAFT WAS WAITING ON THE RAMP PRIOR TO DEPARTURE, PHX MAINTENANCE NOTICED THAT THE F/A'S EMERGENCY LIGHT SWITCH BACKLIGHTING W
- [SDR MASA98096](https://openairdocs.org/sdr/MASA98096), Apr 23, 1998: BULB. FAILED. DURING A ROUTINE SERVICE CHECK, MAINTENANCE NOTED SIX BURNED BULBS IN THE OVERHEAD CABIN CEILING EXIT LIGHT AT THE AIRSTAIR DOOR. THE BULBS WERE REPLACED. OPS C
- [SDR MASA98094](https://openairdocs.org/sdr/MASA98094), Apr 22, 1998: HYDRAULIC LINE. SPLIT. FLT 7544 - DEN-DRO - AFTER TAKEOFF, THE CREW RAISED THE FLAPS AND NOTICED THAT THE NR 1 HYDRAULIC SYSTEM WAS LOSING PRESSURE AND FLUID. DECLARED AN EMERGENCY AN
- [SDR MASA98082](https://openairdocs.org/sdr/MASA98082), Apr 13, 1998: BATTERY. DISCHARGED. FLT 7565 - SHR-GCC - CREW TESTED EMERGENCY LIGHTS AND THEY WOULD NOT ILLUMINATE. MAINTENANCE CHARGED BATTERIES, OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE
- [SDR MASA98075](https://openairdocs.org/sdr/MASA98075), Apr 9, 1998: BULB. FAILED. DURING ROUTINE MAINTENANCE INSPECTION, MAINTENANCE PERSONNEL FOUND THE CENTER OVERHEAD EMERGENCY EXIT SIGN DIM. THE BURNED OUT BULBS WERE REPLACED, OPS CHECK GO
- [SDR MASA98047](https://openairdocs.org/sdr/MASA98047), Mar 5, 1998: BULB. FAILED. FLT 7662 - DEN-MTJ - CREW REPORTED ONE BULB BURNED OUT AT ROW 3 EMERGENCY TRACK LIGHTING. MAINTENANCE ACTION WAS DEFERRED PER MEL 33-11. AIRCRAFT WAS RETURNED T
- [SDR MASA98032](https://openairdocs.org/sdr/MASA98032), Feb 18, 1998: FAN. FAILED. FLT 7565 - GCC-DEN - EN ROUTE TO DEN, PILOT RECEIVED AN AVIONICS FAN FAILED ANNUNC, WITH AN ELECTRICAL ODOR. DEN MAINTENANCE DEFERRED THE AVIONICS COOLING FAN P
- [SDR MASA98029](https://openairdocs.org/sdr/MASA98029), Feb 17, 1998: BULB. FAILED. FLT 7622 - HDN-DEN - IN DEN, CREW REPORTED THE PORTABLE EMERGENCY LIGHT WAS INOP. MAINTENANCE REMOVED AND REPLACED THE BULB. AIRCRAFT WAS RETURNED TO SERVICE. (
- [SDR MASA98006](https://openairdocs.org/sdr/MASA98006), Jan 9, 1998: GAS STRUT. WORN. FLT - 7580 - DEN-GJT - CREW FOUND THAT THE AIRSTAIR DOOR WAS DIFFICULT TO OPEN FROM THE INSIDE. MAINTENANCE REMOVED AND REPLACED THE GAS STRUT AND LUBRICATED TH
- [SDR MASA97260](https://openairdocs.org/sdr/MASA97260), Dec 18, 1997: LIGHT. BROKEN. DURING MAINTENANCE, THE AFT EMERGENCY FLOOR TRACK LIGHT SECTION WAS FOUND TO HAVE A BROKEN CONNECTOR. THE LIGHT STRIP WAS REMOVED AND REPLACED. OPS CHECK GOOD. 
- [SDR MASA97246](https://openairdocs.org/sdr/MASA97246), Dec 8, 1997: WIRE. BROKEN. DURING ROUTINE LINE INSPECTION, EMERGENCY FLOOR PATH LIGHTING HAD TWO RED LIGHTS THAT FAILED TO ILLUMINATE. MAINTENANCE FOUND A BROKEN WIRE AND REMOVED AND REPL
- [SDR MASA97197](https://openairdocs.org/sdr/MASA97197), Oct 24, 1997: BATTERIES. DISCHARGED. FLT 7453 - RAP-DEN - CREW REPORTED THE FIRST THREE OVERHEAD EMERGENCY LIGHTS WOULD NOT ILLUMINATE. THE AIRCRAFT WAS FERRIED TO DEN, WHERE MAINTENANCE REMOVED AN

All 60: https://openairdocs.org/aircraft/N449YV/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/N449YV/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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