# N437YV: 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)
- Data sheets: [TCDS A13NM](https://openairdocs.org/tcds/A13NM) (De Havilland Aircraft of Canada Limited) (OpenAirDocs)
- Serial number: 437
- Type: Fixed wing multi engine
- Engine type: Turbo-prop
- Certificate issued: May 23, 2014
- Expires: May 31, 2027
- Mode S code: A53F59
- Registered owner: [Wells Fargo Trust Co Na Trustee](https://openairdocs.org/faa-owner/WELLS%20FARGO%20TRUST%20CO%20NA%20TRUSTEE)
- Location: [Columbia, MD](https://openairdocs.org/faa-place/MD/Columbia)
- Owner type: Corporation
- Owner's area on the map: 39.2060° N, 76.8282° W: Placed by OpenAirDocs at the center of ZIP code 21045, 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=437YV
- Page: https://openairdocs.org/aircraft/N437YV

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): 117 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

### 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

All 122: https://openairdocs.org/aircraft/N437YV/ads.md

## Information bulletins (advisory)

None matched.

## NTSB investigations

None matched to N437YV.

## FAA accident and incident reports

None matched to N437YV.

## Service difficulty reports (54, 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 HKGA20220314003](https://openairdocs.org/sdr/HKGA20220314003), 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 V0XR413Y050411003](https://openairdocs.org/sdr/V0XR413Y050411003), May 4, 2011: STRINGER. CORRODED. FWD FUSELAGE STA 182.00, FLIGHT COMPARTMENT UNDER FLOOR, RT SIDE, S31R CORRODED, REPLACED STR 31R FROM STA 123-201 IAW RD8-53-1243.
- [SDR V0XR413Y050411001](https://openairdocs.org/sdr/V0XR413Y050411001), May 4, 2011: SKIN. CORRODED. FWD FUSELAGE, STA 167.00 TO 182.00 BETWEEN STR 30 AND 31 LT, FOUND CORROSION ON SKIN. REPAIRED CORRODED SKIN FROM STA167.00 TO 182.00 BETWEEN STR 30 AND 31 LT I
- [SDR V0XR413Y042911001](https://openairdocs.org/sdr/V0XR413Y042911001), Apr 29, 2011: SEAT TRACK. CORRODED. CORROSION ON SEAT TRACK BEAM AT STA 182 TO STA 264, RT CTR BEAM. REMOVED RT CTR BEAM SUPPORT IAW RD8-53-3074 AND REPLACED IAW SRM 51-40-07.
- [SDR MASA2010051800518](https://openairdocs.org/sdr/MASA2010051800518), May 18, 2010: FLAP. MALFUNCTIONED. FLAPS WOULD NOT DEPLOY FOR LANDING, FLIGHT CREW PERFORMED A GO-AROUND AND LANDED WITH NO FLAPS. MX RESET SYSTEM, OPS CHECKS GOOD.
- [SDR MASA2010040100303](https://openairdocs.org/sdr/MASA2010040100303), Apr 1, 2010: BATTERY. DISCHARGED. ONE (1) FLIGHT DECK FLASHLIGHT INOP. REPLACED BATTERY.
- [SDR MASA2008111400774](https://openairdocs.org/sdr/MASA2008111400774), Nov 14, 2008: STRUT. BROKEN. ASH FLT 2896 PHX-DRO. PASSENGER DOOR AFT SUPPORT STRUT BROKEN. MX REMOVED AND REPLACED AFT SUPPORT STRUT.
- [SDR MASA200800344](https://openairdocs.org/sdr/MASA200800344), Apr 27, 2008: SPU. LEAKING. ASH FLT 2743 - PHX-PSP - DECLARED AN EMERGENCY AND RETURNED TO FIELD DUE TO NR 2 HYDRAULIC SYSTEM COMPLETE FLUID LOSS. REMOVED AND REPLACED NR 2 SPU.
- [SDR MASA200800266](https://openairdocs.org/sdr/MASA200800266), Mar 28, 2008: SPU. MALFUNCTIONED. ASH FLT 2950 PHX-GJT. NR 2 HYDRAULIC QUANTITY LOSS IN FLIGHT. AC DECLARED AND EMERGENCY AND DIVERTED TO GJT. CHANGED NR 2 SPU.
- [SDR MASA200700885](https://openairdocs.org/sdr/MASA200700885), Dec 14, 2007: TSCU. MALFUNCTIONED. ASH FLT 2849 PHX - AUTO FEATHER ON LIGHT ILLUMINATED IN FLIGHT NR 2 NOT FEATHERING. CHANGED NR 2 TSCU.
- [SDR MASA200700655](https://openairdocs.org/sdr/MASA200700655), Sep 29, 2007: BLEED VALVE. MALFUNCTIONED. ASH FLT 2962 PHX-GYM - AFTER 1 ENGINE START COCKPIT FILLED WITH SMOKE AFTER BLEED ON. REMOVED AND REPLACED HPV, P2.5 SWITCH VALVE, AND IBV. CLEANED GAS GEN, ICC
- [SDR MASA200700654](https://openairdocs.org/sdr/MASA200700654), Sep 28, 2007: UNKNOWN. SMOKE. ASH FLT 2851 PHX-YUM - PILOT REPORTED SMOKE IN THE FLIGHT DECK AND CABIN AFTER ENGINE START. INSPECTED A/C SYSTEM, OIL LEVEL GOOD, ENGINE RUNS GOOD, NO DEFECTS 
- [SDR MASA200700560](https://openairdocs.org/sdr/MASA200700560), Sep 7, 2007: VALVE. ACTIVATED. ASH FLT 2849 PHX. AFTER ENGINE START FLIGHT DECK FOGS UP WITH AN ODOR. MX REMOVED AND REPLACED NR 1 ENGINE P2.5 SWITCHING VALVE.
- [SDR MASA200700204](https://openairdocs.org/sdr/MASA200700204), Apr 14, 2007: DOOR. OUT OF RIG. ASH 2904 GJT. MAIN CABIN DOOR HARD TO OPEN FROM INSIDE AND OUTSIDE. MX RIGGED THE DOOR, OPS NORMAL.
- [SDR MASA200700195](https://openairdocs.org/sdr/MASA200700195), Apr 7, 2007: STRUCTURE. DISLODGED. ASH 2745 PHX. TRIM UNDER GALLEY EMERGENCY EXIT DOOR FELL OFF. MX SECURED THE TRIM.
- [SDR MASA200700003](https://openairdocs.org/sdr/MASA200700003), Jan 1, 2007: UNKNOWN. UNKNOWN. ASH 2905 PHX. CAPTAIN REPORTED FLAPS FAILED TO MOVE ON APPROACH INTO GJT FROM 15 DEGREES TO 35 DEGREES. MX INSPECTED SYSTEM AND PERFORMED NUMEROUS OPERATIONAL C
- [SDR MASA200602652](https://openairdocs.org/sdr/MASA200602652), Dec 2, 2006: INDICATOR. FAULTY. ASH 2904 GJT. RIGHT INBOARD ROLL SPOILER WOULD NOT DEPLOY. MX REMOVED AND REPLACED PFCS INDICATOR.
- [SDR MASA200602395](https://openairdocs.org/sdr/MASA200602395), Oct 5, 2006: SPU. MALFUNCTIONED. ASH 2896 PHX. NR 2 HYDRAULIC SYSTEM WENT TO ZERO PRESSURE AND QTY. MX REMOVED AND REPLACED THE O-RING AND SPU.
- [SDR MASA200602265](https://openairdocs.org/sdr/MASA200602265), Sep 11, 2006: PUMP. MALFUNCTIONED. ASH 2792 LAS. THE AIRCRAFT LANDING WITH NR 2 HYD SYSTEM WENT TO ZERO PRESSURE AND QTY IN FLIGHT. MX REMOVED EDP AND DOOR SEQ VALVE.
- [SDR MASA200602231](https://openairdocs.org/sdr/MASA200602231), Sep 6, 2006: FLAP. OUT OF RIG. ASH 2896 PHX. FLAPS WILL NOT EXTEND BEYOND 15 DEGREES. MX IS CURRENTLY TROUBLESHOOTING. MX PERFORMED FLAP RIG, SYSTEM CHECK GOOD.
- [SDR MASA200500931](https://openairdocs.org/sdr/MASA200500931), Nov 21, 2005: TIRE. FAILED. ASH 6372 PHX, NR 4 TIRE BLEW. MAINTENANCE REPLACED THE NR 3 AND NR 4 MLG TIRES.
- [SDR MASA200500560](https://openairdocs.org/sdr/MASA200500560), Jul 18, 2005: BRAKE ASSY. FAILED. ASH 6934 PSP. CREW REPORTED RT BRAKES FAILED DURING TAXI AND RT OB MLG TIRE FLAT. MX REPLACED THE #4 BRAKE.
- [SDR MASA200500524](https://openairdocs.org/sdr/MASA200500524), Jul 7, 2005: PRESSURE VALVE. MALFUNCTIONED. ASH 6259 PSP, THE AIRCRAFT DECLARED AN EMERGENCY ON ITS WAY INTO PHX WITH A PAX DOOR WARNING MESSAGE. MAINTENANCE REPLACED THE PASSENGER DOOR PRESSURE VALVE.
- [SDR MASA200400490](https://openairdocs.org/sdr/MASA200400490), Sep 1, 2004: LAMP. INOPERATIVE. ASH 6203 PHX-FLG, ON F/A'S PANEL EMERGENCY GREEN LIGHT WILL NOT ILLUMINATE. PHX LINE MX RELAMPED AND OPS CHECKED GOOD.
- [SDR MAS2002F00003](https://openairdocs.org/sdr/MAS2002F00003), Jun 7, 2002: LIGHT. INOPERATIVE. FORWARD EMERGENCY EGRESS LIGHT ON LEFT AT PAX DOOR, INOPERATIVE MECHANIC REPLACED BULB. OPS CHECKS GOOD.
- [SDR 2002F00202](https://openairdocs.org/sdr/2002F00202), Jan 31, 2002: POWER SUPPLY. DISCHARGED. DURING OVERNIGHT MAINTENANCE, DISCOVERED THAT SEVERAL EMERGENCY LIGHTS WOULD NOT ILLUMINATE. REPLACED THE NR 2 POWER SUPPLY. OPS CHECK GOOD. THE AIRCRAFT WAS RE
- [SDR 2001F00650](https://openairdocs.org/sdr/2001F00650), Sep 14, 2001: POWER SUPPLY. DISCHARGED. FLT 6389 - PHX-YUM - DURING TAXI-OUT, THE CREW HAD AN OVERHEAD EMERGENCY LIGHT INOPERATIVE AND THE MAIN DOOR EMERGENCY EXIT SIGN INOPERATIVE. THE PROBLEM WAS TR
- [SDR 2001F00438](https://openairdocs.org/sdr/2001F00438), Sep 14, 2001: BATTERY. DISCHARGED. FLT 6389 - PHX-YUM - DURING TAXI-OUT, THE CREW HAD AN OVERHEAD EMERGENCY LIGHT INOPERATIVE AND THE MAIN DOOR EMERGENCY EXIT SIGN INOPERATIVE. MAINTENANCE TROUBL
- [SDR MASA00178](https://openairdocs.org/sdr/MASA00178), Dec 21, 2000: HOUSING. CRACKED. DURING OVERNIGHT MX IT WAS DISCOVERED THAT THE NR3 EMERGENCY ESCAPE PATH LIGHTING HOUSING WAS CRACKED. REMOVED AND REPLACED NR3 EMERGENCY ESCAPE PATH LIGHTING. 
- [SDR MASA00171](https://openairdocs.org/sdr/MASA00171), Dec 13, 2000: POWER SUPPLY. DISCHARGED. DURING THE PREFLIGHT INSPECTION, THE CREW NOTICED THE EMERGENCY EXIT SIGN LIGHT OVER THE PAX DOOR INOPERATIVE. THE AIRCRAFT WAS FERRIED TO GRAND JUNCTION WERE M
- [SDR MASA00154](https://openairdocs.org/sdr/MASA00154), Nov 21, 2000: LAMP. BURNED OUT. FLT 6202 - FLP-PHX - MAINTENANCE DISCOVERED THE AFT OVERHEAD EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACED THE BURNED OUT BULB. OP CHECKS GOOD. THE AIRCRAFT
- [SDR MASA99128](https://openairdocs.org/sdr/MASA99128), Aug 1, 1999: BATTERY PACK. DISCHARGED. FLT 6393 - PHX-YUM - THE CAPTAIN REPORTED THAT EMERGENCY CABIN LIGHT INOPERATIVE. MAINTENANCE REPLACED ALL THE BATTERY PACK FOR LIGHT. OPS CHECK GOOD. THE AIRCR
- [SDR MASA99038](https://openairdocs.org/sdr/MASA99038), Mar 4, 1999: CHIME. MALFUNCTIONED. FLT 6255 - PHX-DRO - PRIOR TO DEPARTURE, PILOT REPORTED THE EMERGENCY CALL CHIME AND LIGHT INOPERATIVE. THE DISCREPANCY WAS DEFERRED PER MEL 23-3. AIRCRAFT WAS 
- [SDR MASA99007](https://openairdocs.org/sdr/MASA99007), Jan 8, 1999: DOOR STRUT. BENT. PHX/PSP - FLT 8345 - PRIOR TO DEPARTURE. CREW REPORTED THE PASSENGER DOOR WOULD NOT CLOSE COMPLETELY. MAINTENANCE REPLACED THE DOOR STRUTS, OPS CHECKED GOOD. AI
- [SDR MASA98220](https://openairdocs.org/sdr/MASA98220), Dec 7, 1998: POWER SUPPLY. INOPERATIVE. FLT 6389 - PHX-YUM - DURING PREFLIGHT INSPECTION, CREW REPORTED THAT THE EMERGENCY LIGHT SWITCH HAD BEEN LEFT IN THE ON POSITION OVERNIGHT AND ALL THE POWER SUP
- [SDR MASA98217](https://openairdocs.org/sdr/MASA98217), Dec 1, 1998: POWER SUPPLY. INOPERATIVE. DURING A ROUTINE SERVICE CHECK, MAINTENANCE PERSONNEL FOUND THE EMERGENCY EXIT LIGHTS EXTINGUISHING IMMEDIATELY AFTER BEING TURNED ON. MAINTENANCE REMOVED AND R
- [SDR MASA98214](https://openairdocs.org/sdr/MASA98214), Nov 30, 1998: AIR DISTRIBUTION. ODOR. PHX/DRO - FLT 6255 - AIRCRAFT WAS 15 MILES OUT FROM DRO WHEN THE CREW SMELLED AN ELECTRICAL SMELL IN THE COCKPIT. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE 
- [SDR MASA98186](https://openairdocs.org/sdr/MASA98186), Oct 9, 1998: LIGHT. INOPERATIVE. FLT 5293 - PHX-YUM - PRIOR TO DEPARTURE, CREW NOTICED ONE OVERHEAD EMERGENCY LIGHT INOP. MAINTENANCE RESECURED LOOSE CONNECTION, OPS CHECK GOOD. AIRCRAFT WAS RE
- [SDR MASA98158](https://openairdocs.org/sdr/MASA98158), Aug 22, 1998: LIGHT. INOPERATIVE. FLT 5228 - PHX-YUM - ON PREFLIGHT, CREW FOUND THE PORTABLE EMERGENCY LIGHT INOP. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT. AIRCRAFT WAS RETURNED TO 
- [SDR MASA98149](https://openairdocs.org/sdr/MASA98149), Jul 27, 1998: LIGHT. INOPERATIVE. FLT 5183 - PHX-TEX - DURING PREFLIGHT CHECK, CREW NOTICED THE HAND HELD EMERGENCY LIGHT WAS INOP. MAINTENANCE REMOVED AND REPLACED THE HAND HELD EMERGENCY LIGHT
- [SDR MASA98126](https://openairdocs.org/sdr/MASA98126), Jun 16, 1998: BULB. FAILED. DURING ROUTINE MAINTENANCE, PORTABLE EMERGENCY LIGHT WOULD NOT ILLUMINATE. REMOVED AND REPLACED BULB, OPS CHECK GOOD. (M)
- [SDR MASA98115](https://openairdocs.org/sdr/MASA98115), May 27, 1998: COVER PLATE. DAMAGED. DUE TO THE OTHER AIRCRAFT BEING NOTED WITH FORE RUDDER LOWER RIB END CAP AND/OR COVER PLATE DAMAGE. A/C'S RUDDER WAS INSPECTED WHILE THE A/C WAS INSPECTED DURIN
- [SDR 98ZZZM510](https://openairdocs.org/sdr/98ZZZM510), May 27, 1998: RIB. CRACKED. DUE TO THE OTHER AIRCRAFT BEING NOTED WITH FORE RUDDER LOWER RIB END CAP AND/OR COVER PLATE DAMAGE. A/C'S RUDDER WAS INSPECTED WHILE THE A/C WAS INSPECTED DURIN
- [SDR MASA98071](https://openairdocs.org/sdr/MASA98071), Apr 5, 1998: BULB. FAILED. DURING ROUTINE MAINTENANCE, FOUND PORTABLE EMERGENCY LIGHT WOULD NOT ILLUMINATE. REMOVED AND REPLACED BULB, OPS CHECK GOOD. (M)
- [SDR MASA98030](https://openairdocs.org/sdr/MASA98030), Feb 18, 1998: POWER SUPPLY. FAILED. FLT 7592 - DEN-GJT - DURING DEN PREFLIGHT CHECK, PILOT NOTICED TWO FLOOR TRACK LIGHTS WERE INOP. MAINTENANCE REMOVED AND REPLACED THE BATTERIES AND TRACK LIGHTI
- [SDR 98ZZZM329](https://openairdocs.org/sdr/98ZZZM329), Feb 18, 1998: LIGHT. FAILED. FLT 7592 - DEN-GJT - DURING DEN PREFLIGHT CHECK, PILOT NOTICED TWO FLOOR TRACK LIGHTS WERE INOP. MAINTENANCE REMOVED AND REPLACED THE BATTERIES AND TRACK LIGHTI
- [SDR MASA97236](https://openairdocs.org/sdr/MASA97236), Nov 28, 1997: PLACARD. TORN. DURING ROUTINE MAINTENANCE, FOUND 'LIFT HERE' PLACARD ON RIGHT AFT EMERGENCY EXIT, INTERIOR CABIN PANEL WAS HALF PEELED OFF AND TORN. IT WAS SUSPECTED A PASSENG
- [SDR MASA97208](https://openairdocs.org/sdr/MASA97208), Nov 5, 1997: STRUT. BROKEN. AIRSHUTTLE 7450 - DEN-RAP - WHILE IN DEN, THE CREW FOUND THAT THE CABIN DOOR WOULD NOT CLOSE. MAINTENANCE REMOVED AND REPLACED THE DOOR STRUT. OPS CHECK GOOD. A
- [SDR MASA97164](https://openairdocs.org/sdr/MASA97164), Sep 25, 1997: BULBS. FAILED. DURING A ROUTINE LINE CHECK INSPECTION, MAINTENANCE FOUND OVERHEAD EMERGENCY EXIT BULBS WERE BURNED OUT. THE BULBS WERE REPLACED AND THE AIRCRAFT WAS RETURNED T
- [SDR MASA97143](https://openairdocs.org/sdr/MASA97143), Sep 2, 1997: SIGN. LOOSE. DURING A ROUTINE LINE CHECK, MAINTENANCE FOUND THE EMREGENCY EXIT SIGN AT ROW 4 HAD FALLEN OFF. MAINTENANCE RESECURED THE EMERGENCY EXIT SIGN. AIRCRAFT WAS RETU

All 54: https://openairdocs.org/aircraft/N437YV/reports.md

## STCs that may be installed (OpenAirDocs) (143, 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 143: https://openairdocs.org/aircraft/N437YV/stcs.md

## Related

- Other Dehavilland DHC-8-202 aircraft: https://openairdocs.org/model/dehavilland-dhc-8-202/aircraft.md

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