# N880EA: 1994 Dehavilland DHC-8-106, registration cancelled 2024-11-06

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: November 6, 2024
- Exported to: Kenya
- Status when cancelled: Valid registration
- Airframe: [Dehavilland DHC-8-106](https://openairdocs.org/model/dehavilland-dhc-8-106) (registry code 2809020)
- 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), [TCDS E20NE](https://openairdocs.org/tcds/E20NE) (OpenAirDocs)
- Serial number: 392
- Year built: 1994
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-prop
- Airworthiness: Standard, transport
- Airworthiness date: October 14, 2013
- Certificate issued: March 22, 2024
- Last registry action: March 22, 2024
- Mode S code: AC1E3A
- Owner when cancelled: [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 was based
- The mark today: https://openairdocs.org/aircraft/N880EA
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=880EA
- Page: https://openairdocs.org/deregistered/N880EA-2024-11-06

From the FAA registry file of November 7, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe.

ADs and bulletins for the Dehavilland DHC-8-106: https://openairdocs.org/model/dehavilland-dhc-8-106.md

## Service difficulty reports (77, newest 50)

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR 7C7A2023111900060](https://openairdocs.org/sdr/7C7A2023111900060), Nov 19, 2023: UNKNOWN. UNKNOWN. RIGHT FORWARD MAIN GEAR DOOR LINKAGE NOT CONNECTED TO DOOR.
- [SDR 7C7A2023110100057](https://openairdocs.org/sdr/7C7A2023110100057), Nov 1, 2023: SEAT TRACK. CORRODED. CORROSION ON L/H INBOARD COCKPIT SEAT TRACK. REPAIRED PER DHC-8-100 RD8-53-18096.
- [SDR 7C7A2023103100056](https://openairdocs.org/sdr/7C7A2023103100056), Oct 31, 2023: TRUNNION. CORRODED. CORROSION AT L/H NOSE LANDING GEAR TRUNNION PLATE, TRUNNION CAP MOUNTING BOLT HOLES. TRUNNION PLATE REMOVED AND REPLACED.
- [SDR 7C7A2023102700055](https://openairdocs.org/sdr/7C7A2023102700055), Oct 27, 2023: SEAT TRACK. CORRODED. R/H INBD SEAT TRACK CORRODED AT STA X598. REPLACED IAW DHC-8 RD8-53-4936
- [SDR 7C7A2023102400054](https://openairdocs.org/sdr/7C7A2023102400054), Oct 24, 2023: UNKNOWN. UNKNOWN. CORROSION ON L/H STEP ANGLE AT STA X600. REPLACED IAW DHC-8-100 SRM 51-42-05
- [SDR 7C7A2023102300053](https://openairdocs.org/sdr/7C7A2023102300053), Oct 23, 2023: COAMING. CRACKED. CARGO DOOR CUT OUT LOWER FWD COAMING CRACKED. REPLACED
- [SDR 7C7A2023101100052](https://openairdocs.org/sdr/7C7A2023101100052), Oct 12, 2023: UNKNOWN. UNKNOWN. L/H ELEVATOR SPRING TAB SKIN W/MULTIPLE DENTS. SKIN REPLACED PER DHC RD8-55-037.
- [SDR 7C7A2023090900050](https://openairdocs.org/sdr/7C7A2023090900050), Sep 9, 2023: CONTROLLER. FAILED. CABIN PRESS FAILURE @FL230 CABIN CLIMBED RAPIDLY AND DID NOT RESPOND TO QRH STEPS. CONTINUED FLIGHT UN-PRESSURIZED W/ CONTROLLER UNRESPONSIVE IN AUTO MODE. R/R 
- [SDR 7C7A2023040300022](https://openairdocs.org/sdr/7C7A2023040300022), Apr 3, 2023: ADC. FAILED. #2 ADC FAILS BRIEFLY AT ONE TO TWO MINUTE INTERVALS, MOST CONSISTENTLY IN CLIMB.
- [SDR 7C7A2023032100019](https://openairdocs.org/sdr/7C7A2023032100019), Mar 21, 2023: FMS. FAILED. FMS UNITS WENT INDEPENDENT. FMS SYNC LOSS. REPLACED #2 FMS
- [SDR 7C7A2022042600016](https://openairdocs.org/sdr/7C7A2022042600016), Apr 4, 2022: NONE. INTERMITTENT. DE-ICE PRESS LIGHT ILLUMINATED DE-ICE BOOTS CEASED OPERATION REMOVED AND REPLACED DE-ICE PRESS CAUTION LT. PRESSURE SWITCH. RAN ENGINES OPS CHECKED GOOD
- [SDR 7C7A2021060900016](https://openairdocs.org/sdr/7C7A2021060900016), Jun 9, 2021: THRESHOLD. CORRODED. STA X243 FWD EMERGENCY DOOR CUT OUT EDGE X2 CLEETS AND THRESHOLD PLATE CORREODED. REPAIRED SRM 51-42-05
- [SDR 7C7A2012060900015](https://openairdocs.org/sdr/7C7A2012060900015), Jun 9, 2021: SKIN. DAMAGED. DAMAGE ON THE RH FUSE FWD OF THE RH EMERGENCY EXIT 1" AVOVE 23 FWD STA X201 REPAIRED RD8-53-17031
- [SDR 7C7A2012060900014](https://openairdocs.org/sdr/7C7A2012060900014), Jun 9, 2021: SKIN. DAMAGED. EXTERNAL FUSELAGE RH SIDE STA X202 STR 21S SKIN NICKED REPAIRED RD8-53-4940
- [SDR 7C7A2021060900013](https://openairdocs.org/sdr/7C7A2021060900013), Jun 9, 2021: FLOORBEAM. CRACKED. STA X255 BELOW SERVICE DOOR LOWER CUT OUT FLOOR BEAM CRACKED REPAIRED SRM 51-42-05
- [SDR 7C7A2021060900012](https://openairdocs.org/sdr/7C7A2021060900012), Jun 9, 2021: SKIN. DAMAGED. RH EXT SKIN EDGE OF Y12 AND X115 RIVET LOOSE REPAIRED WITH RD 8-53-5099
- [SDR 7C7A2021060900011](https://openairdocs.org/sdr/7C7A2021060900011), Jun 9, 2021: THRESHOLD. CORRODED. UNDERFLOOR CABIN PAX DOOR THRESHOLD CORROSION FOUND, REPAIRED SRM 51-42-05
- [SDR 7C7A2021060900009](https://openairdocs.org/sdr/7C7A2021060900009), Jun 9, 2021: STRUCTURE. CORRODED. PASSENGER DOOR SHELL FWD AND AFT SIDE EDGES HAVE CORROSION REPAIRED IAW SRM 51-42-05.
- [SDR 7C7A2021060900008](https://openairdocs.org/sdr/7C7A2021060900008), Jun 9, 2021: SKIN. DENTED. PERMANENT REPAIR FOR DENT RH FUSE 85310016 X182 -X201 STR 20S. REPAIRED RD8-53-16442
- [SDR 7C7A2021060900007](https://openairdocs.org/sdr/7C7A2021060900007), Jun 9, 2021: SEAT TRACK. CORRODED. CORROSION FOUND OUT OF LIMITS ON LH INBD SEAT TRACK STA 564.5 - 597 REPAIRED RD8-53-1599
- [SDR 7C7A2021060900006](https://openairdocs.org/sdr/7C7A2021060900006), Jun 9, 2021: FLOOR SUPPORT. CORRODED. AT STATION X182 AT W/L Z100 ANGLE FLOOR SUPPORT FOUND CORRODED REPLACED ANGLE SRM 51-4205
- [SDR 7C7A2021051100005](https://openairdocs.org/sdr/7C7A2021051100005), May 12, 2021: SKIN. DENTED. R/H FUSELAGE, DENT FOUND ABOVE STR 23S AND FWD OF FR STA X 202.75. REPAIRED BY INSTALLING EXTERNAL PATCH IAW ECO 008.53-21.03
- [SDR 7C7A2021050600004](https://openairdocs.org/sdr/7C7A2021050600004), May 11, 2021: DOOR. GOUGED. NICK ON R/H EMERGENCY EXIT DOOR TYPE 2, 2.50" FROM FWD EDGE AND 25.00" FROM LOWER EDGE. REPAIRED IAW ECO 008.52-21.01. NO ICA
- [SDR 7C7A2021050500003](https://openairdocs.org/sdr/7C7A2021050500003), May 5, 2021: SKIN. DENTED. MULTIPLE DENTS ON FORE RUDDER. REPAIRED IAW RD 8-55-3616
- [SDR 7C7A2019120320523](https://openairdocs.org/sdr/7C7A2019120320523), Dec 2, 2019: SKIN. DENTED. LARGE DENT UNDER R/H FUSELAGE ICE SHIELD
- [SDR 7C7A2019110600517](https://openairdocs.org/sdr/7C7A2019110600517), Nov 6, 2019: SKIN. DENTED. DENT WITH SCRATCHES IN FUSELAGE SKIN 85311825-101 BEYOND MFG. LIMITS 2.0X1.6X0.11 SCRATCHES MAX DEPTH OF 0.01
- [SDR 7C7A2019090400511](https://openairdocs.org/sdr/7C7A2019090400511), Sep 4, 2019: FIREWALL. DAMAGED. #1 ENGINE FIREWALL CHAFED BY FIRE LOOP BRACKET. FIRE LOOP BRACKET MOUNTING HOLES IN FIREWALL ELONGATED.
- [SDR 7C7A2019071800508](https://openairdocs.org/sdr/7C7A2019071800508), Jul 17, 2019: CONTROL UNIT. INOPERATIVE. ON APPROACH AFTER GEAR WAS DOWN MOMENTARY GEAR WARNING HORN SOUNDED W/GEAR UNSAFE LIGHT (MOMENTARY 1 SEC OR LESS). HAPPENED TWO TIMES.
- [SDR 7C7A2019F00110](https://openairdocs.org/sdr/7C7A2019F00110), Jan 10, 2019: HYDRAULIC LINE. LEAKING. HAZE, POSSIBLE ELECTRICAL SMOKE IN THE CABIN, CAUSED RETURN FROM DEICE TO GATE. TURNED OUT TO BE HYDRAULIC LEAK IN HYDRAULIC LINE.
- [SDR 7C7A2018121900463](https://openairdocs.org/sdr/7C7A2018121900463), Dec 14, 2018: LIGHT. INOPERATIVE. AFT MOST EMERGENCY LIGHT INOP.
- [SDR 7C7A2018051424](https://openairdocs.org/sdr/7C7A2018051424), May 8, 2018: FITTING. CORRODED. CORROSION FOUND ON THE TOP OF LAVATORY CASTING AT BS 210, BETWEEN STRINGERS 25 - 27R. THE FITTING WAS REPLACED.
- [SDR 7C7A2018051400423](https://openairdocs.org/sdr/7C7A2018051400423), May 8, 2018: THRESHOLD. CORRODED. CORROSION FOUND ON PAX DOOR THRESHOLD. THE THRESHOLD WAS REPLACED.
- [SDR 7C7A2018051400422](https://openairdocs.org/sdr/7C7A2018051400422), May 8, 2018: SEAT TRACK. CORRODED. CORROSION FOUND ON THE RT INBD SEAT TRACK FROM BS 264 - 377. CORROSION REMOVED AND WITHIN LIMITS.
- [SDR 7C7A201805140421](https://openairdocs.org/sdr/7C7A201805140421), May 8, 2018: SEAT TRACK. CORRODED. CORROSION FOUND ON THE RIGHT INBD SEAT TRACK FROM BS 182 - 264. THE CORRIOSION WAS REMOVED, AND FOUND WITHIN LIMITS.
- [SDR 7C7A201805140420](https://openairdocs.org/sdr/7C7A201805140420), May 8, 2018: STEP. CORRODED. AIRSTAIR DOOR STEEP NOSING STEP CORRODED ON STEPS 1,3 & 4. PARTS REPLACED.
- [SDR 7C7A201805140419](https://openairdocs.org/sdr/7C7A201805140419), May 8, 2018: ATTACH FITTING. CORRODED. PAX DOOR SHELL LOWER ATTACHMENT POINTS CORRODED. ATTACHMENT FITTINGS REPAIRED IAW RD 8-52-647.
- [SDR 7C7A201805140418](https://openairdocs.org/sdr/7C7A201805140418), May 8, 2018: BRACKET. CORRODED. PAX DOOR STAIR, AFT UPPER BRACKET WAS FOUND CORRODED. REPLACED THE BRACKET.
- [SDR 7C7A201805140417](https://openairdocs.org/sdr/7C7A201805140417), May 8, 2018: DOOR FRAME. CORRODED. RIGHT FWD EMERGENCY EXIT DOOR FOUND CORRODED ON THE LOWER FRAME. REPLACED THE FRAME.
- [SDR 7C7A2018051400416](https://openairdocs.org/sdr/7C7A2018051400416), May 8, 2018: BRACKET. DAMAGED. PAX DOOR STAIR LOWER FWD ATTACHMENT BRACKET TO SHELL WAS FOURN CRACKED AND CORRODED. REPLACED THE BRACKET.
- [SDR 7C7A201805140415](https://openairdocs.org/sdr/7C7A201805140415), May 8, 2018: HINGE ARM. CORRODED. PAX DOOR HINGE ARMS CORRODED OUT OF LIMITS. BOTH HINGE ARMS REPLACED.
- [SDR 7C7A201805140414](https://openairdocs.org/sdr/7C7A201805140414), May 8, 2018: PLATE. CORRODED. PAX DOOR STRAIRCASE FWD AND AFT BACKING PLATED CORRODED. REPLACED THE PLATE.
- [SDR 7C7A2018050200402](https://openairdocs.org/sdr/7C7A2018050200402), May 2, 2018: INDICATION SYS. ACTIVATED. AUTOMATED ENGINE MONITORING SYSTEM HAS REPORTED OVER-TEMPERATURE IN DEPARTURE OUT OF YYC. EXCEEDED 816C FOR 104 SECONDS.
- [SDR 7C7A2018042400401](https://openairdocs.org/sdr/7C7A2018042400401), Apr 24, 2018: WIRE HARNESS. CHAFED. LEFT WING FSL-13 FAILED A FUNCTIONAL CHECK, WS 225 & 243. WIRE FOUND CHAFED IN THE CONDUIT. REPLACED WITH NEW INDICATOR HARNESS IAW AMM.
- [SDR 7C7A2018041700396](https://openairdocs.org/sdr/7C7A2018041700396), Apr 17, 2018: SKIN. DAMAGED. RT ELEVATOR ASSEMBLY TRAILING EDGE TOP SKIN AT STATIC DISCHARGE ATTACHMENT DAMAGED. REPAIRED IAW RD8-55- 064, D8-55-3182, AND ECO 008.55-18.03.
- [SDR 7C7A2018041600394](https://openairdocs.org/sdr/7C7A2018041600394), Apr 16, 2018: SEAT TRACK. CORRODED. CORROSION FOUND ON LEFT INBOARD SEAT TRACK FROM BS 182 - 302. LEFT INBOARD SEAT TRACK WAS REPLACED IAW RD8-53-3074.
- [SDR 7C7A2018040700387](https://openairdocs.org/sdr/7C7A2018040700387), Apr 7, 2018: SKIN PANEL. DAMAGED. PERMANENT REPAIR FOR DAMAGE ON THE LEFT HAND SIDE CENTER FUSELAGE SKIN PANEL(P/N 85320251) LOCATED BETWEEN FUSELAGE STATIONS X291.40 - X354.35 AND STRINGERS 26P
- [SDR 7C7A2018040700384](https://openairdocs.org/sdr/7C7A2018040700384), Apr 7, 2018: SKIN PANEL. DAMAGED. PERMANENT REPAIR FOR MULTIPLE DAMAGES ON FUSELAGE SKIN PANEL P/N 85320106 BETWEEN FUSELAGE STATIONS X202.75 - X370.80 AND STRINGERS 29P - 29S. THE REPAIR CONSIS
- [SDR 7C7A2018033100380](https://openairdocs.org/sdr/7C7A2018033100380), Mar 31, 2018: SKIN. DENTED. CENTER FUSELAGE LOWER SKIN DENTED BETWEEN BS 291.4 - 312.35, STRINGERS 29P - 32P. REPAIRED IAW RD8-53-15632, AND ECO 008.53-18.18.
- [SDR 7C7A2018033100379](https://openairdocs.org/sdr/7C7A2018033100379), Mar 31, 2018: PANEL. DAMAGED. SKIN BETWEEN BS 123 - 136.8, STRINGERS 30P - 32P DAMAGED. REPAIRED IAW RD8-53-15627, AND ECO 008.53-18.17.
- [SDR 7C7A2018033100378](https://openairdocs.org/sdr/7C7A2018033100378), Mar 31, 2018: SKIN. CORRODED. SKIN CORRODED BETWEEN BS 136.8 - 151.6, STRINGERS 29P - 31S, REPAIRED IAW RD8-53-15630, AND ECO 008.53-18.16.

All 77: https://openairdocs.org/deregistered/N880EA-2024-11-06/reports.md

## Other aircraft with N880EA

- [Cancelled 1997-10-03](https://openairdocs.org/deregistered/N880EA-1997-10-03): Cessna 425, S/N 4250080. Exported to Canada. Owner: [Eagle Aviation Inc](https://openairdocs.org/faa-owner/EAGLE%20AVIATION%20INC), [West Columbia, SC](https://openairdocs.org/faa-place/SC/West%20Columbia)

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