# N891EA: Dehavilland DHC-8-106

- Status: Valid registration
- Airframe: [Dehavilland DHC-8-106](https://openairdocs.org/model/dehavilland-dhc-8-106) (registry code 2809020, 44 seats)
- Engine: [Pratt & Whitney Canada PW121](https://openairdocs.org/engine/pratt-whitney-canada-pw121) (registry code 52124)
- 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: 335
- Type: Fixed wing multi engine
- Engine type: Turbo-prop
- Airworthiness: Standard, transport
- Airworthiness date: June 7, 2014
- Certificate issued: March 2, 2026
- Expires: March 31, 2033
- Mode S code: AC4970
- Registered owner: [Tvpx Ars Inc Trustee](https://openairdocs.org/faa-owner/TVPX%20ARS%20INC%20TRUSTEE)
- Location: [North Salt Lake, UT](https://openairdocs.org/faa-place/UT/North%20Salt%20Lake)
- Owner type: Corporation
- Owner's area on the map: 40.8386° N, 111.9179° W: Placed by OpenAirDocs at the center of ZIP code 84054, 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=891EA
- Page: https://openairdocs.org/aircraft/N891EA

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): 162 in force

### Matched by airframe (Dehavilland DHC-8-106)

- [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 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 2013-16-12](https://openairdocs.org/ad/2013-16-12): Nacelles/pylons · Bombardier DHC-8-102, DHC-8-103 and DHC-8-106. Effective Sep 24, 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 2012-05-07](https://openairdocs.org/ad/2012-05-07): Engine Controls · Bombardier DHC-8-102, DHC-8-103 and DHC-8-106. Effective Apr 4, 2012
- [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 2010-05-12](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
- [AD 2005-11-10](https://openairdocs.org/ad/2005-11-10): Brake shuttle valves · Bombardier DHC-8-102, DHC-8-103, DHC-8-106 and 5 more. Effective Jul 12, 2005

### Matched by engine (Pratt & Whitney Canada PW121)

- [AD 2015-20-03](https://openairdocs.org/ad/2015-20-03): Fuel nozzle and the fuel manifold flow adapter · Pratt & Whitney Canada PW120, PW121, PW121A and 6 more. Effective Nov 18, 2015
- [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 2003-21-03](https://openairdocs.org/ad/2003-21-03): Low pressure rotor speed (NL) sensor · Pratt & Whitney Canada PW118, PW120, PW120A and 1 more. Effective Nov 20, 2003
- [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 94-03-02](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 92-01-08](https://openairdocs.org/ad/92-01-08): High Pressure Rotor · Pratt & Whitney Canada PW118, PW118A, PW120 and 5 more. Effective Jul 27, 1992
- [AD 91-06-02](https://openairdocs.org/ad/91-06-02): Turbomachinery Magnetic Chip Detector · Pratt & Whitney Canada PW118, PW118A, PW120 and 6 more. Effective Mar 29, 1991
- [AD 91-01-03](https://openairdocs.org/ad/91-01-03): Hydromechanical Fuel Control Units · Pratt & Whitney Canada JT15D-5, PW118, PW118A and 3 more. Effective Jan 7, 1991
- [AD 88-26-51](https://openairdocs.org/ad/88-26-51): High Pressure Turbine Components · Pratt & Whitney Canada PW118, PW118A, PW120 and 2 more. Effective Sep 22, 1989

### Historical (superseded or no longer in force)

- [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 2014-14-02](https://openairdocs.org/ad/2014-14-02) (historical): O-ring seal · Pratt & Whitney Canada PW120, PW121, PW121A and 6 more. Effective Aug 15, 2014
- [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 168: https://openairdocs.org/aircraft/N891EA/ads.md

## Information bulletins (advisory)

None matched.

## NTSB investigations

None matched to N891EA.

## FAA accident and incident reports

None matched to N891EA.

## Service difficulty reports (87, 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 7C7A2025012300002](https://openairdocs.org/sdr/7C7A2025012300002), Jan 22, 2025: ELEC CONNECTOR. DIRTY. DISCREPANCY: #1 HYDRAULIC PUMP 'HOT CAUTION' LIGHT FLICKERING ON. CORRECTIVE ACTION: SWAPPED TO SECONDARY TEMP SENSOR ON #1 SPU AND REPLACED CANNON PLUG 2921-P1
- [SDR 7C7A2024112400010](https://openairdocs.org/sdr/7C7A2024112400010), Nov 24, 2024: DEICE SYSTEM. LOW PRESSURE. DEICE BOOT FAILURE OF TAIL RHS OUTBOARD SECTION 6 RIGHT HAND SIDE - INDICATION LIGHT DOES NOT ILLUMINATE DURING OPERATION IN AUTO NOR IN MANUAL
- [SDR 7C7A2024110700008](https://openairdocs.org/sdr/7C7A2024110700008), Nov 5, 2024: DEICE SYSTEM. LOW PRESSURE. #1 ENGINE INTAKE DEICE INOP
- [SDR 7C7A2023112200062](https://openairdocs.org/sdr/7C7A2023112200062), Nov 20, 2023: UNKNOWN. UNKNOWN. L/H AFT EMERGENCY "EXIT' SIGN DOES NOT ILLUMINATE. REPINNED CONNECTOR FOR LH AFT CABIN EMERGENCY EXIT LIGHT. OPS CHECKED OK. REF DHC-8-100 MM 20-45-06 AND 33-52
- [SDR 7C7A2023072700044](https://openairdocs.org/sdr/7C7A2023072700044), Jul 27, 2023: UNKNOWN. DETACHED. EMER EXIT PLACARD OVER MAIN CABIN ENTRY FELL OFF. RE-ATTACHED PER AMM 33-00
- [SDR 7C7A2023070200041](https://openairdocs.org/sdr/7C7A2023070200041), Jul 2, 2023: GENERATOR. FAILED. #2 AC GEN HOT CAUTION LIGHT CAME ON
- [SDR 7C7A2023050900033](https://openairdocs.org/sdr/7C7A2023050900033), May 9, 2023: CONTACTOR. FAILED. UN-COMMANDED ENGINE #1 MOTORING AFTER A DC BUSS CAUTION LIGHT. REPLACED A FAILED RELAY STUCK CLOSED.
- [SDR 7C7A2023041000027](https://openairdocs.org/sdr/7C7A2023041000027), Apr 10, 2023: CONTROL BOX. FAILED. EMERGENCY LIGHTS IN CABIN ILLUMINATED DURING TAXI WITH PROPELLERS IN MIN. REPLACED EMERGENCY LIGHT CONTROL BOX
- [SDR 7C7A2023031800018](https://openairdocs.org/sdr/7C7A2023031800018), Mar 18, 2023: CONTROL BOX. MALFUNCTIONED. EMERGENCY LIGHTS CONTINUOUSLY ON WITH EMER LIGHTS SWITCH IN ARM
- [SDR 7C7A2023031700017](https://openairdocs.org/sdr/7C7A2023031700017), Mar 17, 2023: BATTERY PACK. DISCHARGED. IN FLIGHT....EMERGENCY LIGHTS IN CABIN WOULD RANDOMLY COME ON FOR ABOUT 5 MINUTES THEN SHUT OFF.
- [SDR 7C7A2023030400015](https://openairdocs.org/sdr/7C7A2023030400015), Mar 4, 2023: SOLENOID VALVE. FAILED. ROLL SPLR OUTBD CAUTION LIGHT ILLUMINATED AFTER SELECTING "FLIGHT" OUTBD ROLL SPOILERS REMAINED DOWN AT IDLE WITH "FLIGHT" SELECTED. R/R R/H #1 ROLL SPOILER LIF
- [SDR 7C7A2023011980004](https://openairdocs.org/sdr/7C7A2023011980004), Jan 18, 2023: ANTENNA. FAILED. AFTER DEPARTING ANC CREW DISCOVERED #1 COM NOT WORKING. R&R #1 VHF COMM ANTENNA
- [SDR 7C7A2023010540001](https://openairdocs.org/sdr/7C7A2023010540001), Jan 4, 2023: HORN. FAILED. LEFT ELEVATOR HORN HEAT CAUTION LIGHT ON WHEN ELV HORN HEAT ON.
- [SDR 7C7A2022122800049](https://openairdocs.org/sdr/7C7A2022122800049), Dec 28, 2022: WARNING LIGHT. FALSE ACTIVATION. #1 STANDBY HYDRAULIC PUMP HOT LIGHT INTERMITTENTLY FLASHING ON TAXI. REPINNED IAW AMM 29-11-17.
- [SDR 7C7A2022122700044](https://openairdocs.org/sdr/7C7A2022122700044), Dec 24, 2022: PUMP. FAULTED. NR 1 STBY HYD PUMP HOT LIGHT INTERMITTENLY FLASHING ON TAXI. T/S STBY HYS PUMP, FOUND HARD FAULT ON STBY HYS PUMP OINS A/B OVERTEMP SWITCH MOVED TO PIN E/F OVER
- [SDR 7C7A2022120800033](https://openairdocs.org/sdr/7C7A2022120800033), Dec 7, 2022: AUTOPILOT SYS. FAILED. AFCS&AUTO PILOT FAIL IN FLIGHT
- [SDR 7C7A2022101900028](https://openairdocs.org/sdr/7C7A2022101900028), Oct 19, 2022: SEAT TRACK. CORRODED. CORROSION FOUND ON L/H INBOARD SEAT TRACK BTW STA X526 TO X592. REPLACED SEAT TRACK.
- [SDR 7C7A2022100300027](https://openairdocs.org/sdr/7C7A2022100300027), Oct 3, 2022: FRAME. CRACKED. FRAME CRACK @ STA X136 ABOVE STR 15A
- [SDR 7C7A2022100300026](https://openairdocs.org/sdr/7C7A2022100300026), Oct 3, 2022: SEAT TRACK. CORRODED. CORROSION R/H INBOARD SEAT TRACK BTW STA X526 - 600
- [SDR 7C7A2019080900509](https://openairdocs.org/sdr/7C7A2019080900509), Aug 9, 2019: LONGERON. CRACKED. CRACK DAMAGE TO RH NACELLE I/B UPPER NACELLE LONGERON P/N 85410209 AROUND EYE BOLT.
- [SDR 7C7A2019050910504](https://openairdocs.org/sdr/7C7A2019050910504), May 9, 2019: SKIN PANEL. DENTED. 2 DENTS ON LEFT HAND FUSELAGE BETWEEN STATION X277-X285 ABOVE AND BELOW STRINGER 11P. RD 8-53-16128 WAS ISSUED AND PROVIDES PREMANENT ALLOWANCE FOR MULTIPLE DEN
- [SDR 7C7A2019043000503](https://openairdocs.org/sdr/7C7A2019043000503), May 1, 2019: SKIN. SCRATCHED. SCRATCH IN BELLY FUSELAGE SKIN.
- [SDR 7C7A2019043050502](https://openairdocs.org/sdr/7C7A2019043050502), Apr 30, 2019: FLAP TRACK. CORRODED. CORROSION DAMAGE TO LEFT HAND #5 FLAP TRACK ASSEMBLY, INBOARD HALF
- [SDR 7C7A2019043040501](https://openairdocs.org/sdr/7C7A2019043040501), Apr 30, 2019: SKIN. DENTED. DENTS IN BOTTOM FUSELAGE SKIN
- [SDR 7C7A2019043024050](https://openairdocs.org/sdr/7C7A2019043024050), Apr 30, 2019: SKIN. DENTED. DENT ON L/H SKIN OF FORE RUDDER BTW RIB 11 - 12 AND AFT OF REAR SPAR
- [SDR 7C7A2019050900504](https://openairdocs.org/sdr/7C7A2019050900504), Apr 15, 2019: SKIN PANEL. DENTED. MULTIPLE DENTS IN FUSELAGE SKIN PANELS 85320281 AND 85320313.
- [SDR 7C7A2017080900334](https://openairdocs.org/sdr/7C7A2017080900334), Aug 9, 2017: CONTROL BOX. INOPERATIVE. EMERGENCY LIGHTS CONTROL BOX INOPERATIVE. REMOVED AND REPLACE THE EMERGENCY LIGHT CONTROL BOX IAW 33-51-00.
- [SDR 7C7A2017051000326](https://openairdocs.org/sdr/7C7A2017051000326), May 10, 2017: STRUCTURE. DAMAGED. FWD FUSELAGE ACCESS HOLE 122AR UPPER FWD CORNER SCREW HOLE ELONGATED.
- [SDR 7C7A2017050500325](https://openairdocs.org/sdr/7C7A2017050500325), May 5, 2017: PANEL. CHAFED. WEAR DAMAGE ON LT WING TO FUSELAGE PANEL ALONG THE LOWER EDGE.
- [SDR 7C7A2017050500324](https://openairdocs.org/sdr/7C7A2017050500324), May 5, 2017: SKIN. DENTED. VERTICAL STABILIZER, LT SKIN DENTED
- [SDR 7C7A2017050500323](https://openairdocs.org/sdr/7C7A2017050500323), May 5, 2017: SKIN. DENTED. DENTS ON LT NACELLE OUTBOARD COWLING 413AL
- [SDR 7C7A2017050300322](https://openairdocs.org/sdr/7C7A2017050300322), May 5, 2017: SKIN. DENTED. TWO DENTS ON FUSELAGE SKIN, ONE AT BS 324.5, 1.5 INCHES ABOVE STRINGER 4L AND ONE AT BS 324.5, 2.5 INCHES ABOVE STRINGER 4L.
- [SDR 7C7A2017050300321](https://openairdocs.org/sdr/7C7A2017050300321), May 4, 2017: PANEL. CORRODED. CORROSION IN COUNTERSINK SCREW HOLES OF STRESS PANEL.
- [SDR 7C7A2017050300320](https://openairdocs.org/sdr/7C7A2017050300320), May 4, 2017: STRINGER. CORRODED. ON RT FUSELAGE BETWEEEN STA X488.00 AND 532.00 STR 30S FOUND CORRODED.
- [SDR 7C7A2017050300319](https://openairdocs.org/sdr/7C7A2017050300319), May 4, 2017: SKIN. DENTED. MULTIPLE DENTS FOUND ON SKIN BTW STA X590 TO X600 & BTW STR 23S AND 24S.
- [SDR 7C7A2017050300318](https://openairdocs.org/sdr/7C7A2017050300318), May 3, 2017: SKIN. DENTED. DENT FOUND ON THE RT SKIN OF TRAILING RUDDER BETWEEN RIBS 22-23, AFT OF FRONT SPAR
- [SDR 7C7A2017050300317](https://openairdocs.org/sdr/7C7A2017050300317), May 3, 2017: SKIN. DENTED. DENT FOUND ON RT SKIN OF TRAILING RUDDER BTW RIBS 6-7 AT ONE INCH AFT OF REAR SPAR
- [SDR 7C7A2017050300316](https://openairdocs.org/sdr/7C7A2017050300316), May 3, 2017: SKIN. DENTED. DENT FOUND ON THE RT SKIN OF TRAILING RUDDER BETWEEN RIBS 6-7 ONE INCH AFT OF FRONT SPAR
- [SDR 7C7A2017050300315](https://openairdocs.org/sdr/7C7A2017050300315), May 3, 2017: SKIN. DENTED. DENT FOUND ON RT SKIN OF TRAILING RUDDER BETWEEN RIBS 5-6, 7 INCHES AFT OF FRONT SPAR
- [SDR 7C7A2017050300314](https://openairdocs.org/sdr/7C7A2017050300314), May 3, 2017: SKIN. DENTED. DENT FOUND ON LT SKIN OF TRAILING RUDDER BETWEEN RIBS 26-27 AND BETWEEN FRONT SPAR AND REAR SPAR
- [SDR 7C7A2017050300313](https://openairdocs.org/sdr/7C7A2017050300313), May 3, 2017: SKIN. DENTED. DENT FOUND ON LT SKIN OF TRAILING RUDDER BETWEEN RIBS 25-26, AFT OF REAR SPAR
- [SDR 7C7A2017050300312](https://openairdocs.org/sdr/7C7A2017050300312), May 3, 2017: SKIN. DENTED. DENT FOUND ON LTH TRAILING RUDDER BETWEEN RIBS 13-14, AT FRONT SPAR
- [SDR 7C7A2017050300311](https://openairdocs.org/sdr/7C7A2017050300311), May 3, 2017: SKIN. DENTED. DENT FOUND ON LT SKIN OF TRAILING RUDDER BETWEEN RIBS 7-8, AFT OF FRONT SPAR
- [SDR 7C7A2017050300310](https://openairdocs.org/sdr/7C7A2017050300310), May 3, 2017: STRAP. CHAFED. MAIN ENTRANCE, AFT FRAME STRAP CHAFED AT BS 252.3 AND FLOOR LEVEL 100.3
- [SDR 7C7A2017050300309](https://openairdocs.org/sdr/7C7A2017050300309), May 3, 2017: FRAME. CHAFED. LEFT FWD LOWER MAIN FRAME CHAFED.
- [SDR 7C7A2017042700308](https://openairdocs.org/sdr/7C7A2017042700308), Apr 27, 2017: TAB. DENTED. RIGHT ELEVATOR SPRING TAB BETWEEN YH6 AND YH16 DENTED.
- [SDR 7C7A2016090900254](https://openairdocs.org/sdr/7C7A2016090900254), Sep 7, 2016: ACTUATOR. DAMAGED. NR 1 ENGINE OIL PRESSURE DROPPED BELOW 40 PSI AND THE NR 1 ENGINE WAS SHUTDOWN. R & R THE NR 1 PROPELLER ACTUATOR DUE TO DOME PISTON SEALING SURFACE DAMAGED IAW
- [SDR 7C7A2016090600253](https://openairdocs.org/sdr/7C7A2016090600253), Sep 6, 2016: SEAL. FAILED. SHUT DOWN NR 1 ENGINE DUE TO LOW OIL PRESSURE, DETERMINED LEAK AT PROP SHAFT SEAL.
- [SDR 7C7A201506110052](https://openairdocs.org/sdr/7C7A201506110052), Jun 10, 2015: WIRE. DAMAGED. SCC-1430L AVIONICS COOLING FAN INOP. (FIRE/SMOKE INFLIGHT AIR TURNBACK). AVIONICS COOLING FAN DEFERRED AND THEN REPLACED WHEN AIRCRAFT RETURNED TO BASE. UPON FU
- [SDR 7C7A201505240050](https://openairdocs.org/sdr/7C7A201505240050), May 24, 2015: MOUNT BRACKET. CRACKED. CRACK DAMAGE TO I/B TRACK MOUNT IN 2 PLACES. WELDED REPAIR IAW BOMBARDIER RD 8-78-149.

All 87: https://openairdocs.org/aircraft/N891EA/reports.md

## STCs that may be installed (OpenAirDocs) (146, 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-8-106)

- [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 SA2622NM](https://openairdocs.org/stc/SA2622NM): Installation of Precise Flight Pulselite Control Unit in landing/taxi system. (767-200 B17) (DHC-8 101). Precise Flight 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 ST04559CH](https://openairdocs.org/stc/ST04559CH): Installation of L3Harris Aviation Products SRVIVR25 Model 7100 Cockpit Voice Recorder (CVR) System. Acron Aviation 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 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 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 ST03354NY](https://openairdocs.org/stc/ST03354NY): Installation of the Dual Auxiliary Air Condintioning system. Field Aviation Company Inc
- [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 ST00015NY](https://openairdocs.org/stc/ST00015NY): 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 SA2916SO](https://openairdocs.org/stc/SA2916SO): Installation of dual TRA-67 Mode S transponder system. Honeywell International Inc
- [STC SA2917SO](https://openairdocs.org/stc/SA2917SO): Installation of CAS-81 TCAS II system. 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 SA9086SC-D](https://openairdocs.org/stc/SA9086SC-D): Recore of Hamilton Standard Heat Exchangers 778683-2 for Installation on deHavilland DHC-8 Series Aircraft and 778683-2 for Installation on Fokker F27 Mark 050 Aircraft, in accordance with Honeywell LORI Sealed Drawing List SDL3545-1, Revision C, dated 11 October 2005 or later FAA approved revision. Honeywell International Inc
- [STC SA9080SC-D](https://openairdocs.org/stc/SA9080SC-D): Replace 30E94-2 Sensing Element in Janitrol Valve 45E04-1 used on DHC-8 Oil Coolers 28E99-6 and 28E99-7 in accordance with Honeywell LORI Specification LR 0201-117 as reflected on Honeywell LORI Sealed Drawing List SDL3709-1, Revision A, dated 11 October 2005 or later FAA approved revision. Honeywell International Inc
- [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 ST02173AK](https://openairdocs.org/stc/ST02173AK): Installation of required equipment for extended overwater operations. Corvus Airlines
- [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 ST04449NY](https://openairdocs.org/stc/ST04449NY): Conversion of DHC-8-102/-103/-106 from passenger carrying aircraft into Package Freighter with a Class E Cargo Compartment. Voyageur Aerotech 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

All 146: https://openairdocs.org/aircraft/N891EA/stcs.md

## Related

- Other Dehavilland DHC-8-106 aircraft: https://openairdocs.org/model/dehavilland-dhc-8-106/aircraft.md
- The Pratt & Whitney Canada PW121 engine: https://openairdocs.org/engine/pratt-whitney-canada-pw121.md

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