# Service difficulty reports: N883EA, cancelled May 23, 2025

A list on [N883EA, cancelled May 23, 2025](https://openairdocs.org/deregistered/N883EA-2025-05-23.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 · 88 reports

- [SDR 7C7A2023080300045](https://openairdocs.org/sdr/7C7A2023080300045.md): Computer · failed · Aug 3, 2023 · N883EA · Dhav DHC8106 · Autopilot System
  > ON ILS 7L INTO PANC @ X 1000' WITH AIRCRAFT ON DUAL APP A/C VEERED OFF TO THE RIGHT QUICKLY THEN SEEMED TO TRY AND CORRECT, BUT DISCONNECTED AUTOPILOT AT THAT POINT. REPLACED #2 FLIGHT GUIDANCE COMPUTER
- [SDR 7C7A2023051100035](https://openairdocs.org/sdr/7C7A2023051100035.md): Lens · detached · May 11, 2023 · N883EA · Dhav DHC8106 · Emergency Lighting
  > EMERGENCY EXIT SIGN ABOVE AIR STAIR DOOR FELL DOWN
- [SDR 7C7A2023040300023](https://openairdocs.org/sdr/7C7A2023040300023.md): Adc · failed · Apr 3, 2023 · N883EA · Dhav DHC8106 · Navigation System
  > DADC DATA INVALID MSG. ON #1 ADC
- [SDR 7C7A2022113000031](https://openairdocs.org/sdr/7C7A2022113000031.md): Selector Valve · inoperative · Nov 30, 2022 · N883EA · Dhav DHC8106 · Landing Gear Retraction/Extension System
  > LANDING GEAR FAILED TO EXTEND, HAD TO EXTEND MANUALLY. CREW DECLARED AN EMERGENCY. REPLACED LANDING GEAR SELECTOR VALVE.
- [SDR 7C7A2022112800030](https://openairdocs.org/sdr/7C7A2022112800030.md): Warning Light · illuminated · Nov 28, 2022 · N883EA · Dhav DHC8106 · Landing Gear Position and Warning
  > CREW ATTEMPTED TO LOWER THE LANDING GEAR, RED IN TRANSIT LIGHTS CAME ON BUT NONE OF THE GEAR LOWERED. MANUAL GEAR EXTENSION PERFORMED.
- [SDR 7C7A2022040100014](https://openairdocs.org/sdr/7C7A2022040100014.md): None · none · Mar 29, 2022 · N883EA · Dhav DHC8106 · Fuselage Main, Floor Beam
  > L/H SEAT TRACK ON CARGO AREA FOUND CORRODED.
- [SDR 7C7A2022040100013](https://openairdocs.org/sdr/7C7A2022040100013.md): None · none · Mar 29, 2022 · N883EA · Dhav DHC8106 · Fuselage Structure (General)
  > SEVERAL CORROSION SPOTS ON SKIN BTW STA X 487-510 BTW STR 31S-31P (INTERNAL).
- [SDR 7C7A2020031100002](https://openairdocs.org/sdr/7C7A2020031100002.md): Power Supply · inoperative · Mar 7, 2020 · N883EA · Dhav DHC8106 · Emergency Lighting
  > EMERGENCY LIGHTS ON IN ARM POSITION
- [SDR 7C7A2019032500494](https://openairdocs.org/sdr/7C7A2019032500494.md): Skin · dented · Mar 9, 2019 · N883EA · Dhav DHC8106 · Spoilers
  > DENTS ON BOTTOM SKIN LT OUTBOARD GROUND SPOILER.
- [SDR 7C7A2019032500493](https://openairdocs.org/sdr/7C7A2019032500493.md): Plate · cracked · Feb 28, 2019 · N883EA · Dhav DHC8106 · Wing Miscellaneous Structure
  > CRACK ON RT WING LADDER PLATE AT YW 137.0 JUST FORWARD OF STRINGER 6. P/N: 85711069.
- [SDR 7C7A2017072300331](https://openairdocs.org/sdr/7C7A2017072300331.md): Smoke Detector · defective · Jul 23, 2017 · N883EA · Dhav DHC8106 · Smoke Detection
  > AFTER START UP A SMOKE LIGHT ILLUMINATED AND WOULD NOT GO OUT. FOUND THE NR 2 CARGO SMOKE DETECTOR STAYS IN TEST MODE. OPEN
- [SDR 7C7A2017042500307](https://openairdocs.org/sdr/7C7A2017042500307.md): O-Ring · split · Apr 25, 2017 · N883EA · Dhav DHC8106 · Hydraulic System, Main
  > NR 1 HYDRAULIC ISOLATION VALVE LIGHT ON. FLAPS STOPPED DURING RETRACTION AT 4 DEGREES, REMOVED AND REPLACED THE 1 HYD PRESSURE MANIFOLD ASSY IAW MM 29-10-31, BLEED SYSTEM COMPLIED WITH. PERFORMED AN OPS CHECK OF THE NR1 HYD SYSTEM, OPS CHECKED GOOD. FOUND TH
- [SDR 7C7A2017040600303](https://openairdocs.org/sdr/7C7A2017040600303.md): Stringer · corroded · Apr 6, 2017 · N883EA · Dhav DHC8106 · Fuselage Main, Longeron/Stringer
  > CORROSION ON STRINGER 31L, BS 222.
- [SDR 7C7A2017040400302](https://openairdocs.org/sdr/7C7A2017040400302.md): Skin · corroded · Apr 4, 2017 · N883EA · Dhav DHC8106 · Fuselage Main, Plate/Skin
  > CORROSION UNDER BELLY ANTENNA.
- [SDR 7C7A2017033100300](https://openairdocs.org/sdr/7C7A2017033100300.md): Stringer · corroded · Apr 1, 2017 · N883EA · Dhav DHC8106 · Fuselage Main, Longeron/Stringer
  > CORRODED STRINGER.
- [SDR 7C7A2017032800299](https://openairdocs.org/sdr/7C7A2017032800299.md): Stringer · corroded · Mar 28, 2017 · N883EA · Dhav DHC8106 · Fuselage Main, Plate/Skin
  > CORROSION DAMAGE TO STRINGER 31. BLENDED AND REPAIR IAW RD8-53-15145 AND ECO008.53-17.16
- [SDR 7C7A2017031800298](https://openairdocs.org/sdr/7C7A2017031800298.md): Skin Panel · dented · Mar 18, 2017 · N883EA · Dhav DHC8106 · Fuselage Main, Plate/Skin
  > REPAIR FOR DENT, SCRATCH DAMAGE TO EXTERIOR LOWER FUSELAGE SKIN. REPAIRED IAW RD8-53-15090, RD8-53-15104, RD8-53-15115 AND ECO008.53-17.11
- [SDR 7C7A2017031600297](https://openairdocs.org/sdr/7C7A2017031600297.md): Skin · dented · Mar 16, 2017 · N883EA · Dhav DHC8106 · Fuselage Main, Plate/Skin
  > DENTS ON SKIN BETWEEN BS 167 - 182, ABOVE AND BELOW STRINGER 24L. REPAIRED IAW RD8-53-15109 AND ECO008.53-17.13
- [SDR 7C7A2017031500296](https://openairdocs.org/sdr/7C7A2017031500296.md): Frame · chafed · Mar 15, 2017 · N883EA · Dhav DHC8106 · Fuselage Main, Frame
  > CHAFE DAMAGE TO LT MACHINED FRAME (P/N 85320575) AT X253.4 AND BETWEEN STR 23P & 24P. REPAIRED IAW RD 8-53-15102 AND ECO008.53-17.12.
- [SDR 7C7A2017031300295](https://openairdocs.org/sdr/7C7A2017031300295.md): Skin · damaged · Mar 13, 2017 · N883EA · Dhav DHC8106 · Fuselage Main, Plate/Skin
  > DENT AND SCRATCH DAMAGE TO RT FUSELAGE SKIN, AFT AND BELOW ICE SHIELD. REPAIRED IAW RD 8-53-15089 AND ECO008.53-17-11.
- [SDR 7C7A2017031100294](https://openairdocs.org/sdr/7C7A2017031100294.md): Skin Panel · dented · Mar 11, 2017 · N883EA · Dhav DHC8106 · Cargo/Baggage Doors
  > DENT DAMAGE REPAIRED TO AFT CARGO DOOR IAW RD8-52-1509 AND ECO008.52-17-01
- [SDR 7C7A2017031100293](https://openairdocs.org/sdr/7C7A2017031100293.md): Skin Panel · damaged · Mar 11, 2017 · N883EA · Dhav DHC8106 · Elevator, Plate/Skin
  > LOOSE FASTENERS AT UPPER ELEVATOR HORN TOP SKIN REPAIRED IAW RD8-553035 AND ECO008.55-17.02.
- [SDR 7C7A2017031100292](https://openairdocs.org/sdr/7C7A2017031100292.md): Doubler · corroded · Mar 11, 2017 · N883EA · Dhav DHC8106 · Fuselage Main, Plate/Skin
  > CORROSION DAMAGE TO AFT CARGO DOOR SKIN DOUBLER. REPAIRED IAW RD8-53-15082 AND ECO008.53-17.06.
- [SDR 7C7A2017031000289](https://openairdocs.org/sdr/7C7A2017031000289.md): Skin Panel · dented · Mar 10, 2017 · N883EA · Dhav DHC8106 · Fuselage Main, Plate/Skin
  > DENT DAMAGE TO LT FUSELAGE SKIN. REPAIRED IAW RD8-53-15088 AND ECO 008.53-17.10.
- [SDR 7C7A2017031000258](https://openairdocs.org/sdr/7C7A2017031000258.md): Skin Panel · dented · Mar 10, 2017 · N883EA · Dhav DHC8106 · Fuselage Main, Plate/Skin
  > DENT DAMAGE TO THE LT SIDE FUSELAGE SKIN REPAIRED IAW RD 8-53-15085 AND ECO008.53-17.09.
- [SDR 7C7A2017030800287](https://openairdocs.org/sdr/7C7A2017030800287.md): Skin Panel · dented · Mar 8, 2017 · N883EA · Dhav DHC8106 · Fuselage Main, Plate/Skin
  > DENT DAMAGE TO FUSELAGE SKIN PANEL 85310533 STA X123 STR 24S AND 25S. REPAIRED IAW ECO 008.53-17-05.
- [SDR 7C7A2017030700286](https://openairdocs.org/sdr/7C7A2017030700286.md): Skin · dented · Mar 7, 2017 · N883EA · Dhav DHC8106 · Fuselage Main, Plate/Skin
  > DENT DAMAGE TO THE FUSELAGE SKIN PANEL BETWEEN BS 291.4 AND 312.35, STRINGER 1-2R. REPAIRED IAW RD 8-53-15073 WC 53-123.
- [SDR 7C7A201502220013](https://openairdocs.org/sdr/7C7A201502220013.md): Panel · corroded · Feb 21, 2015 · N883EA · Dhav DHC8106 · Wing, Plate/Skin
  > RIGHT STRESS PANEL 624AT ONE COUNTERSINK CORRODED, REPAIRED WITH A BUSHING IAW RD 8-57-2673.
- [SDR 7C7A201502220012](https://openairdocs.org/sdr/7C7A201502220012.md): Panel · corroded · Feb 21, 2015 · N883EA · Dhav DHC8106 · Wing, Plate/Skin
  > LEFT STRESS PANEL 521AT 9EA COUNTERSINKS CORRODED. REPAIRED IAW RD 8-57-4240.
- [SDR 7C7A201502220011](https://openairdocs.org/sdr/7C7A201502220011.md): Bolt · corroded · Feb 21, 2015 · N883EA · Dhav DHC8106 · Fuselage, Wing Attach Fittings
  > LT AND RT REAR SPAR WING/FUSELAGE JOINT BOLTS CORRODED. REPLACED THE BOLTS IAW AMM.
- [SDR 7C7A201502220010](https://openairdocs.org/sdr/7C7A201502220010.md): Stringer · corroded · Feb 21, 2015 · N883EA · Dhav DHC8106 · Fuselage Main, Longeron/Stringer
  > CORROSION ON STRINGER 31P AT BS 354. SPLICED STRINGER IAW RD 8-53-2499.
- [SDR 7C7A201502220009](https://openairdocs.org/sdr/7C7A201502220009.md): Frame Splice · corroded · Feb 21, 2015 · N883EA · Dhav DHC8106 · Fuselage Main, Frame
  > CORROSION SPOTS UNDER COCKPIT AREA ZONE 121-122. REPAIRED CORROSION; REPLACED HORIZONTAL STIFFNER, REPLACED FRAME, REPLACED 4 FRAME LEGS.
- [SDR 7C7A201502220008](https://openairdocs.org/sdr/7C7A201502220008.md): Cargo Track · corroded · Feb 21, 2015 · N883EA · Dhav DHC8106 · Fuselage, Seat/Cargo Attach Fittings
  > RT INBD CARGO TRACK CORRODED, REWORKED THE CARGO TRACK IAW RD 8-53-784 AND 8-53-4936.
- [SDR 7C7A201502220007](https://openairdocs.org/sdr/7C7A201502220007.md): Web · corroded · Feb 21, 2015 · N883EA · Dhav DHC8106 · Fuselage Miscellaneous Structure
  > BAGGAGE FLOOR WEB CORRODED AT SEVERAL PLACES, DOUBLER WEB INSTALLED SRM REPAIR.
- [SDR 7C7A201502220006](https://openairdocs.org/sdr/7C7A201502220006.md): Cargo Track · corroded · Feb 21, 2015 · N883EA · Dhav DHC8106 · Fuselage, Seat/Cargo Attach Fittings
  > LT INBD CARGO TRACK CORRODED. REPLACED THE CARGO TRACK IAW WC 1062 RD 8-53-4472
- [SDR 7C7A201502220005](https://openairdocs.org/sdr/7C7A201502220005.md): Threshold · corroded · Feb 21, 2015 · N883EA · Dhav DHC8106 · Fuselage Miscellaneous Structure
  > CORROSION AT PAX DOOR THRESHOLD. BEYOND LIMITS PART REPLACED WC 1050
- [SDR ERAA201410310066](https://openairdocs.org/sdr/ERAA201410310066.md): Generator · defective · Oct 30, 2014 · N883EA · Dhav DHC8106 · AC Generator-Alternator
  > NUMBER 1 AC GEN CAUTION LIGHT ILLUMINATED ON TAKEOFF ROLL. TAKEOFF EJECTED. R & R NR 1 AC GENERATOR IAW DHC-8 PPBM 71-00-02. OPERATIONS & LEAK CHECKED GOOD. OK FOR SERVICE.
- [SDR ERAA20140050](https://openairdocs.org/sdr/ERAA20140050.md): Inverter · failed · Aug 19, 2014 · N883EA · Dhav DHC8106 · AC Inverter
  > DURING PREFLIGHT WITH ENGS COLD 1ST OFFICER NOTED ELEC SMOKE ON THE FLIGHT DECK & HEARD 115 VOLT BUSS TIE CB POP. FOUND SECONDARY INVERTER BURNT UP. REPLACED INVERTER & GND TESTED GOOD.
- [SDR ERAA201408010047](https://openairdocs.org/sdr/ERAA201408010047.md): Actuator · cracked · Jul 31, 2014 · N883EA · Dhav DHC8106 · Drag Control Actuator
  > NUMBER 1 HYD ISO VLV, ROLL SPOILER INBD, FLAP POWER CAUTION LIGHTS WITH LESS THAN MIN NR 1 HYD FLUID. FLAPS REMAINED AT 5 DEGREES. FOUND RT INBD ROLL SPOILER ACTUATOR HOUSING CRACKED. R & R INBD ROLL SPOILER ACTUATOR IAW MM 27--14-05. RIGGING NOT AFFECTED,
- [SDR ERAA20140044](https://openairdocs.org/sdr/ERAA20140044.md): Actuator · leaking · Jun 25, 2014 · N883EA · Dhav DHC8106 · Drag Control Actuator
  > HYDRAULIC FLUID LEAKING FROM DRAIN HOLES ON WING FLAP FAIRINGS WITH NR 2 ENG RUNNING. R & R LT OTBD ROLL SPOILER ACTUATOR IAW MM 27-14-05. RIGGED IAW 27-14-00. LEAK & OPS CHECKED GOOD.
- [SDR ERAA201406230043](https://openairdocs.org/sdr/ERAA201406230043.md): Wire · damaged · Jun 22, 2014 · N883EA · Dhav DHC8106 · Flight Control System Wiring
  > SPOILER 2 PUSH OFF SWITCH LIGHT CAME ON IN FLIGHT. VERIFIED PROBLEM ON RT WING BY DISCONNECTING 2700-P4 & THEN 9811-J172, IT WENT AWAY. RAN NEW WIRE FROM 9811-J172 TO 2762-S6 TO E2 REPLACED. GND TEST GOOD IAW MM 27-19-00.
- [SDR ERAA20140009](https://openairdocs.org/sdr/ERAA20140009.md): Ahrs · inaccurate · Mar 23, 2014 · N883EA · Dhav DHC8106 · Integrated Flight System
  > NR 1 ADI SHOWING INCORRECT PITCH & ROLL INFORMATION. ADI PITCH & ROLL MISMATCH MESSAGES DISPLAYED ON 802 DISPLAY. R & R NR 1 AHRU IAW 34-20-06, OPERATIONS NORMAL.
- [SDR ERAA201309300066](https://openairdocs.org/sdr/ERAA201309300066.md): Rod End · out of adjust · Sep 27, 2013 · N883EA · Dhav DHC8106 · Landing Gear Door Actuator
  > LEFT GEAR DOOR INTERMITTENTLY STAYS OPEN ON GEAR RETRACTION. ADJUSTED LEFT FWD GEAR DOOR ACTUATOR ROD END IAW MM 32-10-36. GEAR SWING C/W IAW MM 32-30-00. OK FOR SERVICE.
- [SDR ERAA201309270065](https://openairdocs.org/sdr/ERAA201309270065.md): Unknown · odor · Sep 26, 2013 · N883EA · Dhav DHC8106 · Air Distribution System
  > F/A REPORTED ODOR OF "HOT OIL" ON DECENT. INSPECTED IAW FAULT ISOLATION 72-00-02. ENGINE OIL LEVELS CHECKED GOOD, NO STANDING OIL NOTED. ACM LEVELS CHECK OK. RAN UP NR 1 AND NR 2 ENGINE BLEEDS ON. NO DEFECTS NOTED, COULD NOT DUPLICATE. OK FOR SERVICE AT THI
- [SDR ERAA201309130061](https://openairdocs.org/sdr/ERAA201309130061.md): Power Supply · defective · Sep 12, 2013 · N883EA · Dhav DHC8106 · Emergency Lighting
  > EMEGENCY LIGHTS INOPERATIVE AT SIDE KICK PANELS AT ALL EMERGENCY EXITS. R & R NR 3 POWER SUPPLY UNIT AS REQUIRED WITH AN INSPECTED UNIT. OPS CHECKED GOOD. WORK DONE IAW MM SECTION 33-51-00.
- [SDR ERAA201309120060](https://openairdocs.org/sdr/ERAA201309120060.md): Battery Pack · discharged · Sep 11, 2013 · N883EA · Dhav DHC8106 · Emergency Lighting
  > EMERGENCY LIGHTS NOT ILLUMINATED. R & R BATTERY PACK AT STA X500. OPS CHECKED GOOD.
- [SDR ERAA20130058](https://openairdocs.org/sdr/ERAA20130058.md): Proximity Sensor · out of rig · Sep 5, 2013 · N883EA · Dhav DHC8106 · Landing Gear Door Retract Section
  > LT MAIN GEAR DOOR CAUTION LIGHT STAYED ON WITH GEAR RETRACTION. VISUALLY CHECKED GEAR DOOR WAS OPEN. COMPLIED WITH TROUBLESHOOTING IAW MM SECTION 32-00-00. RIGGED UPLOCK PROXIMITY SENSOR IAW SECTION 32-30-26. OPS CHECK ON GROUND FOUND GOOD. OPS CHECK FLIGHT
- [SDR ERAA20130046](https://openairdocs.org/sdr/ERAA20130046.md): Bracket · cracked · Jul 1, 2013 · N883EA · Dhav DHC8106 · Fuselage Main, Attach Fittings
  > NLG UPLOCK ACTUATOR ATTACH BRACKET CRACKED. REMOVED FITTING, REINSTALLED BRACKET IAW RD 8-53-3805. OK FOR SERVICE.
- [SDR ERAA201306280042](https://openairdocs.org/sdr/ERAA201306280042.md): Battery · weak · Jun 27, 2013 · N883EA · Dhav DHC8106 · Emergency Lighting
  > RIGHT FORWARD EXTERIOR EMERGENCY LIGHT INOP. R & R BATTERY 3351P2 IAW MM 33-52-00. OPS CHECKS NORMAL. OK FOR SERVICE.
- [SDR ERAA201306280041](https://openairdocs.org/sdr/ERAA201306280041.md): Connector · failed · Jun 27, 2013 · N883EA · Dhav DHC8106 · Light System Wiring
  > LEFT FWD EXTERIOR EGRESS EMERGENCY LIGHT INOPERATIVE. FOUND CONNECTOR DISCONECTED AND WIRE DISCONNECTED FROM CONNECTOR SOCKET. INSTALLED NEW SOCKET, CONNECTED CONNECTORS IAW MM 20-45-09 CHECKED NORMAL. OK FOR SERVICE.

Next page: https://openairdocs.org/deregistered/N883EA-2025-05-23/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 = 'N883EA' AND deregistration_id = 'N883EA-2025-05-23'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N883EA-2025-05-23/reports

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