# Service difficulty reports: N885EA, cancelled Jul 23, 2025

A list on [N885EA, cancelled Jul 23, 2025](https://openairdocs.org/deregistered/N885EA-2025-07-23.md).

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

Page 1 of 2 · 63 reports

- [SDR 7C7A2025021300006](https://openairdocs.org/sdr/7C7A2025021300006.md): Torque Sensor · malfunctioned · Feb 12, 2025 · N885EA · Dhav DHC8106 · Trailing Flap Position Indicating System
  > FLAP DRIVE CAUTION LIGHT ILLUMINATED AFTER TAKEOFF W/FLAPS SELECTED 5 DEGREES.
- [SDR 7C7A2024111200009](https://openairdocs.org/sdr/7C7A2024111200009.md): Generator · warning light · Nov 10, 2024 · N885EA · Dhav DHC8106 · DC Generating System
  > #2 DC GEN CAUTION LIGHT ILLUMINATED. RESET FAILED.
- [SDR 7C7A2024071100004](https://openairdocs.org/sdr/7C7A2024071100004.md): Sequence Valve · faulted · Jul 11, 2024 · N885EA · Dhav DHC8106 · Landing Gear Retraction/Extension System
  > LH INBOARD REAR MLG DOOR OPENED IN FLIGHT. REPLACED LH MLG SOLENOID SEQUENCE VALVE AND AFT LH MLG INBOARD DOOR.
- [SDR 7C7A2023110400058](https://openairdocs.org/sdr/7C7A2023110400058.md): Relay · failed · Nov 4, 2023 · N885EA · Dhav DHC8106 · Electrical Power System
  > FIRE PROTECTION PANEL INOP. R/R RELAY X-D4N OPS CHECK GOOD
- [SDR 7C7A2023081900049](https://openairdocs.org/sdr/7C7A2023081900049.md): Sensor · faulty · Aug 19, 2023 · N885EA · Dhav DHC8106 · Engine Oil System (Airframe Furnished)
  > #2 OIL PRESSURE GAUGE SHOWED LOW MOMENTARILY THEN CAME BACK UP. EMERGENCY WAS DECLARED AND RETURNED TO ANC. R/R#2 OIL PRESSURE SENSOR SWITCH.
- [SDR 7C7A2023081800048](https://openairdocs.org/sdr/7C7A2023081800048.md): Smoke Detector · intermittent · Aug 18, 2023 · N885EA · Dhav DHC8106 · Smoke Detection
  > LAV SMOKE DETECTOR INTERMITTENTLY CHIRPS FOR NOT REASON (LAV WASN'T ON FIRE)
- [SDR 7C7A2023062700040](https://openairdocs.org/sdr/7C7A2023062700040.md): Master Caution · erratic · Jun 27, 2023 · N885EA · Dhav DHC8106 · Flight Compartment Lighting
  > CAUTION LIGHT PANEL LIGHTS RANDOMLY TURNING ON AND OFF DURING TEST. WHEN #2 ENG RUNNING AND #2 ENG OFF, #1 ENG CAUTION LIGHTS THAT SHOULD BE ON WERE NOT. WHEN UNIT WARMED UP, MULTIPLE CAUTION LIGHTS FAIL INTERMITTENTLY. DZUS FASTENERS ARE TO SHORT.
- [SDR 2023F00007](https://openairdocs.org/sdr/2023F00007.md): Spu · faulted · Dec 29, 2022 · N885EA · Dhav DHC8106 · Hydraulic System, Main
  > #2 STBY HUD PRESSURE IS 0 PSI. R&R #2 SPU IAW DHC-8 100 AMM 29-11-17. LEAK AND OPS CHECK FAILED SEE ITEM 3 FOR CONTINUED MAINTENANCE. C/W BLEED LEAK AND OPS CHECK OK.
- [SDR 7C7A2022122000042](https://openairdocs.org/sdr/7C7A2022122000042.md): Spu · failed · Dec 20, 2022 · N885EA · Dhav DHC8106 · Hydraulic Power Accumulator, Main
  > NO.2 STBY HYDRAULIC PRESSURE INDICATES ZERO WHEN ON. NO ASSOCIATED CAUTION LIGHTS. REPLACED #2 STANDBY POWER UNIT
- [SDR 7C7A2022212100037](https://openairdocs.org/sdr/7C7A2022212100037.md): Pump · warning light · Dec 12, 2022 · N885EA · Dhav DHC8106 · Hydraulic System, Main
  > 7H-DIS-27219 #2 ENG HYD PUMP CAUTION LIGHT CAME ON INTERMITTENTLY. FOLLOWED THE QEH.
- [SDR 7C7A2022031700012](https://openairdocs.org/sdr/7C7A2022031700012.md): Skin · corroded · Mar 17, 2022 · N885EA · Dhav DHC8106 · Fuselage Main, Plate/Skin
  > CORROSION DAMAGE ON CENTER FUSELAGE RH TOP SKIN PANEL ASSEMBLY PN 85320282 BETWEEN X291.40 -X312.35 AND STR. 1-2S. REF. 008.53-22.07
- [SDR 7C7A2022031700011](https://openairdocs.org/sdr/7C7A2022031700011.md): Skin · damaged · Mar 17, 2022 · N885EA · Dhav DHC8106 · Ailerons
  > DAMAGE TO LH AILERON SPRING TAB LOWER SKIN. REF. 008.27-22.02
- [SDR 7C7A2022031700010](https://openairdocs.org/sdr/7C7A2022031700010.md): Skin · cracked · Mar 17, 2022 · N885EA · Dhav DHC8106 · Ailerons
  > CRACK DAMAGE ON RH AILERON LOWER SKIN PANEL PN 85740055 AT TAB HINGE STATIONS YW 442.50 AND YW471.50 ALONG THE REAR SPAR. REF 008.27-22.01
- [SDR 7C7A2022031700009](https://openairdocs.org/sdr/7C7A2022031700009.md): Shear Web · corroded · Mar 17, 2022 · N885EA · Dhav DHC8106 · Fuselage Miscellaneous Structure
  > CORROSION DAMAGE TO BAGGAGE DOOR SURROUND SHEAR WEB PN 85330431 BETWEEN X545 - X564.50 OUTBOARD OF Y-19.23. REF 008.53-22.06
- [SDR 7C7A2022031700008](https://openairdocs.org/sdr/7C7A2022031700008.md): Frame · chafed · Mar 17, 2022 · N885EA · Dhav DHC8106 · Fuselage Main, Frame
  > CHAFE DAMAGE TO THE CENTER FUSE FRAME X253.40 PN 85320575. REF 008.53-22.03
- [SDR 7C7A2022031700007](https://openairdocs.org/sdr/7C7A2022031700007.md): Strap · corroded · Mar 17, 2022 · N885EA · Dhav DHC8106 · Fuselage Miscellaneous Structure
  > CORROSION DAMAGE TO THE INNER CAP STRAPS PN 8533501 STRAPS AT FRAME AT X618 BETWEEN STR. 20S-22S. REF. 008.53-22.12
- [SDR 7C7A2022031700006](https://openairdocs.org/sdr/7C7A2022031700006.md): Frame · damaged · Mar 17, 2022 · N885EA · Dhav DHC8106 · Fuselage Main, Frame
  > MULTIPLE SCRATCH DAMAGE TO FRAME CAP REINFORCING STRAPS PN 85333501-139/-137/-134 AT X636.0 AND BETWEEN STR. 21S-23S. REF. 008.53-22.09
- [SDR 7C7A2022031700005](https://openairdocs.org/sdr/7C7A2022031700005.md): Skin · cracked · Mar 17, 2022 · N885EA · Dhav DHC8106 · Ailerons
  > CRACK DAMAGE TO UPPER SKIN PANEL PN 85740016 OF RH AILERON ASSY. PN 85740002-003 AT YW 491 ALONG THE FRONT SPAR. REF. 008.27-22.03
- [SDR 7C7A2022031700004](https://openairdocs.org/sdr/7C7A2022031700004.md): Strap · chafed · Mar 17, 2022 · N885EA · Dhav DHC8106 · Fuselage Structure (General)
  > CHAFE DAMAGE TO TOP STRAP PN 85322331 OF BOTTOM FRAME ASSEMBLY PN 8533086 AT X510 BETWEEN STR. 23S AND 24S. REF. 008.53-22.05
- [SDR 7C7A2022031700003](https://openairdocs.org/sdr/7C7A2022031700003.md): Frame · chafed · Mar 17, 2022 · N885EA · Dhav DHC8106 · Fuselage Structure (General)
  > CHAFE DAMAGE TO THE CENTER FUSELAGE FRAME X253.40 PN 85320575. REF. 008.53-22.03
- [SDR 7C7A2022031700002](https://openairdocs.org/sdr/7C7A2022031700002.md): Frame · chafed · Mar 17, 2022 · N885EA · Dhav DHC8106 · Fuselage Structure (General)
  > CHAFE DAMATE TO RH FRAME X531.50 PN 85330133 INBD FLANGE TO STRAP PN 85322331-179 AT STR. 23S. REF. ECO 008.53-22.04
- [SDR 7C7A2021100100019](https://openairdocs.org/sdr/7C7A2021100100019.md): Door · dented · Oct 12, 2021 · N885EA · Dhav DHC8106 · Passenger/Crew Doors
  > GROUND DAMAGE TO AIRSTAIR DOOR SKIN. PN 85210003-001. ACCEPTABLE ALLOWANCE FOR 300 HRS UNTIL PERMANENT REPAIR IS REQUIRED. IAW ECO 008.52-21.03
- [SDR 7C7A2018081700017](https://openairdocs.org/sdr/7C7A2018081700017.md): Windshield · cracked · Aug 17, 2021 · N885EA · Dhav DHC8106 · Flight Compartment Windows
  > FIRST OFFICERS WINDSHIELD CRACKED
- [SDR 7C7A2019112620522](https://openairdocs.org/sdr/7C7A2019112620522.md): Pseu · abnormal · Nov 22, 2019 · N885EA · Dhav DHC8106 · Landing Gear Door Retract Section
  > ALL GEAR DOORS OPENED AFTER GEAR EXTENSION. DOOR LIGHTS WERE OFF. CAME BACK ON, DOORS ARE OPEN.
- [SDR 7C7A2019010600472](https://openairdocs.org/sdr/7C7A2019010600472.md): Threshold · corroded · Jan 6, 2019 · N885EA · Dhav DHC8106 · Fuselage Miscellaneous Structure
  > PAX DOOR THRESHOLD CORROSION. PART REPLACED AT W/C 53-356.
- [SDR 7C7A2019010300471](https://openairdocs.org/sdr/7C7A2019010300471.md): Skin · nicked · Jan 3, 2019 · N885EA · Dhav DHC8106 · Fuselage Main, Plate/Skin
  > NICKS ON FUSELAGE SKIN AT STA X370.8 ON STR 29S. ECO 008.53-18.54 C/W.
- [SDR 7C7A2018123100470](https://openairdocs.org/sdr/7C7A2018123100470.md): Skin · dented · Dec 31, 2018 · N885EA · Dhav DHC8106 · Fuselage Main, Plate/Skin
  > MULTIPLE DENTS LH FUSELAGE SKIN STA X270.5-X291.4 & BTW STR 8P-9P. ECO 008.53-18.55.
- [SDR 7C7A2018123100469](https://openairdocs.org/sdr/7C7A2018123100469.md): Skin · nicked · Dec 31, 2018 · N885EA · Dhav DHC8106 · Fuselage Main, Plate/Skin
  > BLENDING OF NICKS AT STA X250.00 ABOVE STR 33. ECO 008.53-18.58.
- [SDR 7C7A2018123100468](https://openairdocs.org/sdr/7C7A2018123100468.md): Skin · nicked · Dec 31, 2018 · N885EA · Dhav DHC8106 · Fuselage Main, Plate/Skin
  > SEVERAL NICKS ON FUSELAGE SKIN BTW X377-396 & BTW STR 30-32P
- [SDR 7C7A2018123100467](https://openairdocs.org/sdr/7C7A2018123100467.md): Skin · dented · Dec 31, 2018 · N885EA · Dhav DHC8106 · Fuselage Main, Plate/Skin
  > MULTIPLE DENTS LH FUSE STA 103-110 BTW STIFF 11-12. ECO 008.53-18.57.
- [SDR 7C7A2018123100466](https://openairdocs.org/sdr/7C7A2018123100466.md): Skin · dented · Dec 31, 2018 · N885EA · Dhav DHC8106 · Fuselage Main, Plate/Skin
  > DENT RH FUSE AT STA X109. ECO 008.53-18.56
- [SDR 7C7A2018123100465](https://openairdocs.org/sdr/7C7A2018123100465.md): Skin · dented · Dec 31, 2018 · N885EA · Dhav DHC8106 · Passenger/Crew Doors
  > DENT ON MED. ECO 008.52-18.11.
- [SDR 7C7A2018102600455](https://openairdocs.org/sdr/7C7A2018102600455.md): Lug · broken · Sep 27, 2018 · N885EA · Dhav DHC8106 · Spoilers
  > BROKEN LUG.
- [SDR 7C7A2018090700454](https://openairdocs.org/sdr/7C7A2018090700454.md): Beam · cracked · Sep 7, 2018 · N885EA · Dhav DHC8106 · Fuselage Main, Structure
  > BEAM IN NOSE WHEEL WELL CRACKED BEYOND GENERIC RD ALLOWANCES.
- [SDR 7C7A2018020500366](https://openairdocs.org/sdr/7C7A2018020500366.md): Light · inoperative · Feb 5, 2018 · N885EA · Dhav DHC8106 · Emergency Lighting
  > EMERGENCY EXIT BACKLIGHTING OVER AIRSTAIR INOP.
- [SDR 7C7A2018013000359](https://openairdocs.org/sdr/7C7A2018013000359.md): Inverter · failed · Jan 30, 2018 · N885EA · Dhav DHC8106 · AC Inverter
  > STRONG ODOR EMANATING FROM THE COCKPIT. REPLACED THE INVERTER.
- [SDR 7C7A2017101300338](https://openairdocs.org/sdr/7C7A2017101300338.md): Plate · damaged · Oct 13, 2017 · N885EA · Dhav DHC8106 · Wing, Plate/Skin
  > RIGHT WING LADDER PLATE UNDER FUEL PANEL 624BT, HAD 3 SCREW HOLES ELONGATED. REPAIRED IAW ECO 008.57-17.03.
- [SDR 7C7A2017101300337](https://openairdocs.org/sdr/7C7A2017101300337.md): Skin · damaged · Oct 13, 2017 · N885EA · Dhav DHC8106 · Fuselage Main, Plate/Skin
  > DAMAGE TO FUSELAGE SKIN AT BS 322 AND BETWEEN STRINGERS 29R AND 30R. REPAIRED IAW ECO 008.53-17.29.
- [SDR 7C7A2017082600335](https://openairdocs.org/sdr/7C7A2017082600335.md): Battery Pack · inoperative · Aug 26, 2017 · N885EA · Dhav DHC8106 · Emergency Lighting
  > LOWER EMERGENCY EXIT DOOR LIGHT INOPERATIVE, REMOVED AND REPLACED BATTERY POWER SUPPLY BOX
- [SDR 7C7A2016121600273](https://openairdocs.org/sdr/7C7A2016121600273.md): Window Frame · corroded · Dec 16, 2016 · N885EA · Dhav DHC8106 · Fuselage Main, Structure
  > AT BS 302, WINDOW FRAME CORRODED. REPLACED IAW SRM 51-40-05.
- [SDR 7C7A2016120500269](https://openairdocs.org/sdr/7C7A2016120500269.md): Stringer · corroded · Dec 5, 2016 · N885EA · Dhav DHC8106 · Fuselage Main, Longeron/Stringer
  > STRINGER 31L BETWEEN BS 467 & 510 CORRODED. REPAIRED IAW SRM AND RD8-53-1834.
- [SDR 7C7A2016120500268](https://openairdocs.org/sdr/7C7A2016120500268.md): Threshold · corroded · Dec 5, 2016 · N885EA · Dhav DHC8106 · Fuselage Miscellaneous Structure
  > PAX DOOR THRESHOLD CORRODED. REMOVED AND REPLACED AND REPAIRED SUPPORT OF THRESHOLD REF. RD8-53-8421 AND SRM WC 53-136
- [SDR 7C7A2016112900267](https://openairdocs.org/sdr/7C7A2016112900267.md): Skin · dented · Nov 29, 2016 · N885EA · Dhav DHC8106 · Fuselage Main, Plate/Skin
  > DENT DAMAGE TO LT FUSELAGE SKIN UNDER THE ICE SHIELD. REPAIRED IAW RD8-53-14891.
- [SDR 7C7A2016112900266](https://openairdocs.org/sdr/7C7A2016112900266.md): Skin · dented · Nov 29, 2016 · N885EA · Dhav DHC8106 · Passenger/Crew Doors
  > DENT TO THE PAX DOOR BEYOND SRM LIMITS. REPAIRED IAW RD8-52-1475
- [SDR 7C7A2016112500264](https://openairdocs.org/sdr/7C7A2016112500264.md): Light · inoperative · Nov 25, 2016 · N885EA · Dhav DHC8106 · Emergency Lighting
  > R FWD OUTSIDE EMERGENCY LIGHT OUT. REPLACED BULB, OPS CHECK GOOD.
- [SDR 7C7A2016112400263](https://openairdocs.org/sdr/7C7A2016112400263.md): Firewall · damaged · Nov 24, 2016 · N885EA · Dhav DHC8106 · Engine Cowling System
  > CHAFING DAMAGE TO LOWER COWLING DECKING. REPAIRED WITH PATCH IAW 8-71-1196 AND ECO008-54-16-07
- [SDR 7C7A2016071200249](https://openairdocs.org/sdr/7C7A2016071200249.md): Firewall · damaged · Jul 12, 2016 · N885EA · Dhav DHC8106 · Nacelle/Pylon, Bulkhead/Firewall
  > RIGHT FIREWALL HAS ACRING DAMAGE, DISCOVERED DURING INSPECTION IAW SB 8-24-92. REPAIR BY CUTTING OUT DAMAGE HFEC INSPECTION AND INSTALLATION OF PATCH IAW 54-3825
- [SDR 7C7A2016042501](https://openairdocs.org/sdr/7C7A2016042501.md): Door · dented · Apr 25, 2016 · N885EA · Dhav DHC8106 · Passenger/Crew Doors
  > DENT DAMAGE TO PAX DOOR. TEMP ALLOWANCE IAW RD 8-52-1466 ISSUE 1.
- [SDR 7C7A2016010801](https://openairdocs.org/sdr/7C7A2016010801.md): Battery Pack · discharged · Jan 7, 2016 · N885EA · Dhav DHC8106 · Emergency Lighting
  > ROW 4 EXIT LIGHTS FLICKERED DURING FLIGHT, ALL EXIT LIGHTS ILLUMINATED BRIEFLY. MOSTLY OVERHEAD LIGHT AT 4. R & R PS2 BATTERY PACK FOR ROW 4. OPERATIONS CHECKED GOOD.
- [SDR 7C7A20151123097](https://openairdocs.org/sdr/7C7A20151123097.md): Oil Cooler · leaking · Nov 21, 2015 · N885EA · Dhav DHC8106 · Engine Oil Cooler
  > APPROX 1 HR INTO THE FLIGHT, THE MASTER WARNING LT INTERMITTENTLY FLASHED. A COUPLE MINUTES LATER WE NOTICED NR 1 ENG OIL PRESS FLUCTUATIONS, 60-45 APPROX, WE FEATHERED THE ENG & THIS HELPS THE FLUCTUATIONS. WE HAD A MOMENTARILY NR 1 ENG OIL PRESS LT BUT IT

Next page: https://openairdocs.org/deregistered/N885EA-2025-07-23/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
WHERE n_number = 'N885EA' AND deregistration_id = 'N885EA-2025-07-23'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N885EA-2025-07-23/reports

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