# N436YV: 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: 436
- Type: Fixed wing multi engine
- Engine type: Turbo-prop
- Airworthiness: Standard, transport
- Airworthiness date: June 26, 1996
- Certificate issued: March 25, 2026
- Expires: March 31, 2033
- Mode S code: A53BA2
- 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=436YV
- Page: https://openairdocs.org/aircraft/N436YV

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/N436YV/ads.md

## Information bulletins (advisory)

None matched.

## NTSB investigations

None matched to N436YV.

## FAA accident and incident reports (1)

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 20020906024149I](https://openairdocs.org/incident/20020906024149I), Sep 6, 2002: Dhav DHC8202 (N436YV), Palm Springs, CA. (-23) A mesa airlines Dehavilland DHC-8-202, call sign ash 902 was being repositioned to Palm Springs airport from phoenix, AZ, when during descent the number…

## Service difficulty reports (58, 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 MASA2012022834501](https://openairdocs.org/sdr/MASA2012022834501), Feb 28, 2012: SMOKE WARNING. FALSE ACTIVATION. BAG SMOKE WARNING. MX INSPECTED AND NO DEFECTS WERE NOTED.
- [SDR MASA2012013194385](https://openairdocs.org/sdr/MASA2012013194385), Jan 31, 2012: HYDRAULIC LINE. LEAKING. AIRCRAFT EXPERIENCED NR 2 HYDRAULIC SYSTEM FLUID LOSS AFTER DEPARTURE FROM GYM EN ROUTE TO PHX. CAPTAIN DECLARED AN EMERGENCY AND RETURNED TO FIELD. CURRENTLY A
- [SDR MASA2011123064318](https://openairdocs.org/sdr/MASA2011123064318), Dec 27, 2011: BUTTON. STUCK. FLIGHT ATTENDANT PA BUTTON STUCK. CLEANED BUTTON.
- [SDR MASA2011111864047](https://openairdocs.org/sdr/MASA2011111864047), Nov 17, 2011: FLASHLIGHT. MISSING. FLIGHT DECK FLASHLIGHT MISSING. R2 FLASHLIGHT.
- [SDR MASA2011090603638](https://openairdocs.org/sdr/MASA2011090603638), Sep 5, 2011: LIGHT. INOPERATIVE. FLOOR TRACK LIGHTING DAMAGED AT ROW 7 & 8; R2 FLOOR TRACK LIGHTING.
- [SDR MASA2011082903581](https://openairdocs.org/sdr/MASA2011082903581), Aug 26, 2011: POWER SUPPLY. INOPERATIVE. LEFT FWD EGRESS LIGHT INOP. R2 E-LIGHT POWER SUPPLY.
- [SDR MASA2011082203529](https://openairdocs.org/sdr/MASA2011082203529), Aug 20, 2011: STRUT. UNKNOWN. PAX DOOR GAS STRUTS REQ CHANGED. PER MX GAS STRUTS ARE SERVICEABLE.
- [SDR MASA2011080803408](https://openairdocs.org/sdr/MASA2011080803408), Aug 5, 2011: LIGHT. INOPERATIVE. LEFT FWD EXTERIOR E-LIGHT INOP. RELAMPED EMERGENCY LIGHT.
- [SDR MASA2011080303394](https://openairdocs.org/sdr/MASA2011080303394), Aug 3, 2011: OIL COOLER. DEFECTIVE. ABNORMAL PWR NR 1 ENG OIL TEMP 120 C. R2 OIL COOLER.
- [SDR MASA2011052702876](https://openairdocs.org/sdr/MASA2011052702876), May 26, 2011: ROLLER. MISSING. CARGO DOOR LWR FWD ROLLER MISSING. INSTALLED ROLLER.
- [SDR MASA2011051602729](https://openairdocs.org/sdr/MASA2011051602729), May 15, 2011: LIGHT. INOPERATIVE. NR 2 T-HANDLE FIRE WARNING INDICATOR INOP. R2 HANDLE LAMP ASSY.
- [SDR MASA2011051102667](https://openairdocs.org/sdr/MASA2011051102667), May 9, 2011: BRAKE. DRAGGING. BRAKES DRAGGING. R2 NR 3 & 4 BRAKES.
- [SDR MASA2011051102666](https://openairdocs.org/sdr/MASA2011051102666), May 9, 2011: POTENTIOMETER. MALFUNCTIONED. NO FULL DEFLECT LWD AILERON TRIM. R2 TRIM TAB POTENTIOMETER.
- [SDR MASA2011050402602](https://openairdocs.org/sdr/MASA2011050402602), May 3, 2011: STATIC WICK. BROKEN. LT ELEVATOR STATIC WICK BROKEN. R2 STATIC WICK.
- [SDR MASA2011042502495](https://openairdocs.org/sdr/MASA2011042502495), Apr 23, 2011: FLOW DIVIDER. LEAKING. FUEL DRIPPING FROM GANG DRAIN AT NR 2 ENGINE. R2 FLOW DIVIDER.
- [SDR MASA2011041402397](https://openairdocs.org/sdr/MASA2011041402397), Apr 11, 2011: LIGHT. INOPERATIVE. UPPER AIRSTAIR DOOR LIGHT INOP. MX RELAMPED, OPS CHECK GOOD.
- [SDR MASA2011041402396](https://openairdocs.org/sdr/MASA2011041402396), Apr 11, 2011: BATTERY. DISCHARGED. FWD OVERHEAD E-LIGHT INOP. MX REMOVED AND REPLACED E-LIGHT BATTERY, OPS TEST GOOD.
- [SDR MASA2011041402395](https://openairdocs.org/sdr/MASA2011041402395), Apr 11, 2011: BATTERY. DISCHARGED. F/A'S FLASHLIGHT INOP. MX REPLACED BATTERY.
- [SDR MASA2011032902272](https://openairdocs.org/sdr/MASA2011032902272), Mar 26, 2011: ACTUATOR. FAULTY. NR 2 PROP SLOW TO COME OUT OF FEATHER. MX REMOVED AND REPLACED PROP ACTUATOR.
- [SDR MASA2011032902271](https://openairdocs.org/sdr/MASA2011032902271), Mar 26, 2011: BRAKE. LEAKING. NR 2 BRAKE LEAKING. MX REMOVED AND REPLACED BRAKE.
- [SDR MASA2011010601621](https://openairdocs.org/sdr/MASA2011010601621), Jan 4, 2011: ROD. BROKEN. MAIN DOOR AFT HANDRAIL ROD BROKEN. MX REPLACED HANDRAIL ROD, OPS NORMAL.
- [SDR MASA2010111001252](https://openairdocs.org/sdr/MASA2010111001252), Nov 9, 2010: BRAKE ASSY. LOOSE. NR 1 BRAKE ASSY LOOSE. MX REPLACED BRAKE.
- [SDR MASA2010082600920](https://openairdocs.org/sdr/MASA2010082600920), Aug 25, 2010: B-NUT. LOOSE. FUEL LEAK NR 1 ENG ON A-15 LEAK CHECK. MX TIGHTENED B-NUT ON WASTE FUEL RETURN LINE ON NR 1 ENG LEAK CHECK GOOD.
- [SDR MASA2010051700510](https://openairdocs.org/sdr/MASA2010051700510), May 17, 2010: BATTERY. DISCHARGED. DEAD EMERGENCY LIGHT BATTERY. MX R&R EMERGENCY LIGHT BATTERY OPS GOOD.
- [SDR MAS2008F00046](https://openairdocs.org/sdr/MAS2008F00046), Aug 18, 2008: ROD. BROKEN. ASH FLT 7098 - ASE-DEN - PASSENGER DOOR FWD SUPPORT ROD BROKEN. MAINTENANCE REMOVED AND REPLACED STRUT. OPS CHECK GOOD. (S)
- [SDR MASA200800104](https://openairdocs.org/sdr/MASA200800104), Feb 6, 2008: PRESSURE VALVE. MALFUNCTIONED. FLT 7075 - PASSENGER DOOR HARD TO OPEN. INFLATABLE DOOR SEAL NOT DEFLATING PROPLERLY. REPLACED PRESSURE VALVE, ELBOWS, AND TUBING. OPS CHECKED GOOD.
- [SDR MASA200700805](https://openairdocs.org/sdr/MASA200700805), Nov 15, 2007: CONTROLLER. MALFUNCTIONED. ASH FLT 7150 COD - PILOT REPORTED A RAPID DEPRESSURIZATION WITH O2 MASK DROP IN FLIGHT. REPLACED THE CABIN PRESSURE CONTROLLER
- [SDR MASA200700312](https://openairdocs.org/sdr/MASA200700312), Jun 8, 2007: CONTROL UNIT. MALFUNCTIONED. ASH 7106 DEN - EMERGENCY EXIT LIGHTS WILL NOT TURN ON FROM F/A'S PANEL. MX REPLACED THE PANEL CONTROL UNIT.
- [SDR MASA200700100](https://openairdocs.org/sdr/MASA200700100), Feb 13, 2007: SMOKE DETECTOR. FALSE ACTIVATION. ASH 7059 DEN - BAGGAGE COMPARTMENT SMOKE LIGHT ILLUMINATED ON GROUND. MX REMOVED AND REPLACED FWD SMOKE DETECTOR.
- [SDR MASA200601881](https://openairdocs.org/sdr/MASA200601881), Jul 17, 2006: CIRCUIT BREAKER. TRIPPED. ASH 7079 GJT - LT AND RT STALL WARNING CAUTION LIGHT. MX RESET C/B.
- [SDR MASA200601762](https://openairdocs.org/sdr/MASA200601762), Jul 3, 2006: POTENTIOMETER. OUT OF ADJUST. ASH 7039 DEN - AILERON TRIM REQUIRES FULL LEFT WING DOWN FOR LEVEL FLIGHT. THE AILERON POTENTIOMETER WAS ADJUSTED AND THE SYSTEM OPERATED NORMALLY.
- [SDR MASA200601122](https://openairdocs.org/sdr/MASA200601122), Apr 19, 2006: HOSE. LEAKING. LOSS OF NR 1 AND NR 2 HYD QTY AND PRESSURE DUE TO LEAK AT LT MLG. MAINTENANCE REMOVED AND REPLACED FLEX LINE AND SERVICED HYD.
- [SDR MASA200600608](https://openairdocs.org/sdr/MASA200600608), Mar 1, 2006: LAMP. INOPERATIVE. ASH 7066 DEN - NLG DOWN LOCK LIGHT NOT ILLUMINATED. MAINTENANCE RELAMPED THE NLG DOWN SWITCH LIGHT.
- [SDR MASA200400612](https://openairdocs.org/sdr/MASA200400612), Oct 29, 2004: WINDSHIELD. SPARKS. AIRCRAFT DIVERTED TO GJT DUE TO THE FIRST OFFICERS WINDSHIELD HEAT CAUSING SMOKE IN THE FLIGHT DECK. AIRCRAFT IS CURRENTLY AOG FOR A WINDSHIELD, SDR OPEN FOR FU
- [SDR 2002F00087](https://openairdocs.org/sdr/2002F00087), Sep 27, 2001: LIGHT. INOPERATIVE. FLT 6333 - AN EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE DETERMINED THE BULB WAS UNSERVICEABLE. THE BULB WAS REMOVED AND REPLACED AND OPS CHECKED GOOD. 
- [SDR MASA00145](https://openairdocs.org/sdr/MASA00145), Nov 10, 2000: LIGHT. BROKEN. FOUND NR 2 TRACK LIGHT PLASTIC HOUSING BROKEN DURNIG A ROUTINE INSPECTION. MAINTENANCE REMOVED AND REPLACED NR 2 TRACK LIGHT ASSEMBLY. OPS CHECK GOOD AND THE AI
- [SDR MASA00121](https://openairdocs.org/sdr/MASA00121), Oct 14, 2000: BATTERY PACK. DISCHARGED. FLT 6333 - BFL-PHX - THE PILOT REPORTED THAT THE MID CABIN OVERHEAD EMERGENCY EXIT SIGN WAS INOPERATIVE. MAINTENANCE REPLACED 6 BATTERY PACKS. OPS CHECKED GOOD 
- [SDR MASA00098](https://openairdocs.org/sdr/MASA00098), Aug 8, 2000: POWER SUPPLY. FAILED. DURING AN A-17 LINE CHECK INSPECTION, SEVERAL EMERGENCY EXIT LIGHTS WERE NOT ILLUMINATION DURING TEST. THE NR 1 AND NR 3 EMERGENCY POWER SUPPLIES WERE FOUND TO 
- [SDR MASA99016](https://openairdocs.org/sdr/MASA99016), Jan 28, 1999: LAMP. FAILED. DURING A ROUTINE MAINTENANCE INSPECTION, MAINTENANCE PERSONNEL FOUND THE NR 3 OVERHEAD EMERGENCY LIGHT WAS NOT ILLUMINATING. MAINTENANCE REPLACED THE BURNED OUT
- [SDR MASA99008](https://openairdocs.org/sdr/MASA99008), Jan 11, 1999: SMOKE DETECTOR. MALFUNCTIONED. FLT 6348 - PSP-PHX - AFTER DEPARTURE FROM PSP, CREW REPORTED A CARGO BAY SMOKE DETECTOR ANNUNCIATOR ILLUMINATED IN FLIGHT. AIRCRAFT RETURNED TO THE FIELD. NO EV
- [SDR MASA98184](https://openairdocs.org/sdr/MASA98184), Oct 5, 1998: TRIM. MALFUNCTIONED. FLT 5254 - DRO-PHX - AFTER DEPARTURE, CREW REPORTED UNABLE TO TRIM THE ELEVATOR AFTER REACHING FLIGHT ALTITUDE. THE CREW ELECTED TO RETURN TO DRO, AND EMERGENCY
- [SDR MASA98169](https://openairdocs.org/sdr/MASA98169), Sep 3, 1998: BATTERIES. DISCHARGED. DURING A ROUTINE MAINTENANCE CHECK, MAINTENANCE PERSONNEL FOUND THE PORTABLE EMERGENCY LIGHT TO BE DIM. MAINTENANCE REMOVED THE BATTERIES, DEEP CYCLED AND REINS
- [SDR MASA98097](https://openairdocs.org/sdr/MASA98097), May 1, 1998: BULB. FAILED. DURING ROUTINE MAINTENANCE, FOUND 'NORMAL SWITCH EMERGENCY LIGHT AT FLIGHT ATTENDANT'S PANEL WOULD NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE LIGHT BU
- [SDR MASA98026](https://openairdocs.org/sdr/MASA98026), Feb 11, 1998: LAMP. FAILED. FLT 7529 - DRO-DEN - UPON ARRIVAL IN DEN, CREW NOTICED LEFT FORWARD EMERGENCY EXIT LIGHT INOP. MAINTENANCE RESET LAMP, OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO 
- [SDR MASA98011](https://openairdocs.org/sdr/MASA98011), Jan 20, 1998: CABLE. WORN. FLT 7561 - SHR-DEN - UPON ARRIVAL IN DEN, THE AIRSTAIR DOOR WOULD NOT OPEN DUE TO THE CABLE BINDING. MAINTENANCE REMOVED AND REPLACED THE DOOR CABLE. AIRCRAFT W
- [SDR MASA98009](https://openairdocs.org/sdr/MASA98009), Jan 14, 1998: CABLE. OUT OF ADJ. FLT 7573 - GCC-SHR- AIRCRAFT LANDED IN SHR AND THE CREW HAD TROUBLE OPENING THE AIRSTAIR DOOR. MAINTENANCE LUBED CABLES AND PULLEYS. OPS CHECK GOOD, AIRCRAFT WA
- [SDR MASA98003](https://openairdocs.org/sdr/MASA98003), Jan 5, 1998: BULB. FAILED. DURING LINE CHECK INSPECTION, THE AFT OVERHEAD EMERGENCY LIGHT WOULD NOT ILLUMINATE. REMOVED AND REPLACED BULB, OPS CHECK GOOD. (M)
- [SDR MASA97275](https://openairdocs.org/sdr/MASA97275), Dec 24, 1997: BULB. FAILED. DURING MAINTENANCE INSPECTION, FOUND THE FLIGHT ATTENDANTS EMERGENCY LIGHT SWITCH WOULD NOT ILLUMINATE WHEN SELECTED ON. MAINTENANCE REMOVED AND REPLACED THE BU
- [SDR MASA97256](https://openairdocs.org/sdr/MASA97256), Dec 15, 1997: BULB. FAILED. FLT 7489 - CPR-DEN - CREW FOUND EMERGENCY OVERHEAD COCKPIT FLASHLIGHT INOP. MAINTENANCE REMOVED AND REPLACED BULB, OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO SERV
- [SDR MASA97248](https://openairdocs.org/sdr/MASA97248), Dec 8, 1997: LAMP. FAILED. DURING ROUTINE LINE INSPECTION, RIGHT FORWARD EMERGENCY EXIT UPPER 'EXIT' SIGN WAS DIM. MAINTENANCE REMOVED AND REPLACED THE BULBS. AIRCRAFT WAS RETURNED TO SER

All 58: https://openairdocs.org/aircraft/N436YV/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/N436YV/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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