# Service difficulty reports: N893EA, cancelled Feb 13, 2024

A list on [N893EA, cancelled Feb 13, 2024](https://openairdocs.org/deregistered/N893EA-2024-02-13.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 · 76 reports

- [SDR 7C7A2023100600051](https://openairdocs.org/sdr/7C7A2023100600051.md): Caution Panel · faulty · Oct 6, 2023 · N893EA · Dhav DHC8106 · Indicating/Recording System
  > MASTER CAUTION LIGHT NOT COMING ON. R/R CAUTION ADVISORY PANEL
- [SDR 7C7A2023062100038](https://openairdocs.org/sdr/7C7A2023062100038.md): Unknown · unknown · Jun 19, 2023 · N893EA · Dhav DHC8106 · Fuselage Structure (General)
  > BATTERY CABLE ATTACHED TO AIRFRAME GROUND LUG SHOWS EVIDENCE OF ARCING. DEHAVILLAND RD8-53-17986 HAS BEEN PROVIDED FOR A REPAIR TO THE NOSE COMPARTMENT DECK.
- [SDR 7C7A2023051800036](https://openairdocs.org/sdr/7C7A2023051800036.md): Oil Cooler · leaking · May 17, 2023 · N893EA · Dhav DHC8106 · Engine Oil Indicating System
  > NO 1 OIL PRESSURE LOW LIGHT. OIL LEAKING NO1 SIDE. FOUND O-RING ON R/H SIDE OF OIL COOLER CUT. R/R O-RINGS ON R/H SIDE OF OIL COOLER. LEAK AND OPS CHECK GOOD. ON RETURN FLIGHT BACK OIL CONTINUED TO LEAK AND IT WAS DISCOVERED THE OIL COOLER CORE IS AT FAULT WH
- [SDR 7C7A2023042600031](https://openairdocs.org/sdr/7C7A2023042600031.md): Unknown · unknown · Apr 26, 2023 · N893EA · Dhav DHC8106 · Wing, Plate/Skin
  > DISBOND ON R/H WING LOWER SKIN DOUBLER, BTW STA YW171-YW189 AND AT LEVEL OF REAR SPAR. REPAIRED IAW RD8-57-9809ISS1
- [SDR 7C7A2023042600030](https://openairdocs.org/sdr/7C7A2023042600030.md): Unknown · unknown · Apr 26, 2023 · N893EA · Dhav DHC8106 · Wing, Plate/Skin
  > DISBOND AND CORROSION ON L/H WING LOWER SKIN, BTW STA YW171-YW189 AND AT LEVEL OF REAR SPAR. REPAIRED IAW RD8-57-9810ISS1
- [SDR 7C7A2023042600029](https://openairdocs.org/sdr/7C7A2023042600029.md): Piston · unknown · Apr 26, 2023 · N893EA · Dhav DHC8106 · Main Landing Gear
  > L/H MLG LOWER PISTON TORQUE LINK BUSHING HAS INTERNAL CORROSION. REPLACED LOWER PISTON.
- [SDR 7C7A2023041300028](https://openairdocs.org/sdr/7C7A2023041300028.md): Unknown · unknown · Apr 13, 2023 · N893EA · Dhav DHC8106 · Fuselage Main, Floor Beam
  > L/H SEAT TRACK CORROSION BETWEEN STA X202 AND STA X215. REPAIRED PER DHC RD8-53-5623
- [SDR 7C7A2023040700026](https://openairdocs.org/sdr/7C7A2023040700026.md): Stiffener · corroded · Apr 7, 2023 · N893EA · Dhav DHC8106 · Fuselage Miscellaneous Structure
  > CARGO DOOR THRESHOLD AT STA X600 STIFFINER CORRODED. REPLACED PER DHC-8-100 SRM 51-42-05
- [SDR 7C7A2023040400022](https://openairdocs.org/sdr/7C7A2023040400022.md): Threshold · corroded · Apr 4, 2023 · N893EA · Dhav DHC8106 · Fuselage Floor Panel
  > PASSENGER DOOR THRESHOLD CORRODED/BLENDED BEYOND LIMITS. REPLACED PER DHC-8-100 SRM 51-42-05.
- [SDR 7C7A2023011730002](https://openairdocs.org/sdr/7C7A2023011730002.md): Relay · failed · Jan 13, 2023 · N893EA · Dhav DHC8106 · Air Collision Avoidance System
  > TCAS INOP DURING CRUISE, DEFERRED TCAS SYSTEM. REPLACED RELAY 3452-K6 FOR FIX
- [SDR 7C7A2022122100043](https://openairdocs.org/sdr/7C7A2022122100043.md): Pressure Switch · failed · Dec 21, 2022 · N893EA · Dhav DHC8106 · Hydraulic System, Main
  > "RUD FULL PRESS CAME ON INTERMITTENTLY" CHANGED 1&2 RUD FULL PRESS SWITCHES
- [SDR 7C7A2022121300038](https://openairdocs.org/sdr/7C7A2022121300038.md): Controller · failed · Dec 7, 2022 · N893EA · Dhav DHC8106 · Air Collision Avoidance System
  > TCAS FAIL. TCAS CONTROLLER WAS CHANGED
- [SDR 7C7A2022120700034](https://openairdocs.org/sdr/7C7A2022120700034.md): Processing Unit · failed · Dec 7, 2022 · N893EA · Dhav DHC8106 · Air Collision Avoidance System
  > TCAS FAILED.
- [SDR 7C7A2022081300025](https://openairdocs.org/sdr/7C7A2022081300025.md): Brake · smoke · Aug 13, 2022 · N893EA · Dhav DHC8106 · Brake
  > RAMP AGENTS NOTICED THAT THERE WAS SMOKE COMING OFF OF THE BRAKE WHILE OFF LOADING PASSENGERS. ONE OF THEM NOTICED A SMALL FLAME WHICH WAS QUICKLY EXTINGUISHED BY RAMP STAFF. BRAKES HAVE BEEN REMOVED AND SENT TO OVERHAUL FACILITY FOR INVESTIGATION OF CAUSE.
- [SDR 7C7A2021111100042](https://openairdocs.org/sdr/7C7A2021111100042.md): None · none · Nov 11, 2021 · N893EA · Dhav DHC8106 · Rudder Structure
  > GENIE LIFT CONTACTED LOWER AFT TRAILING RUDDER, BENDING RH&LH SKIN PANELS AND AFT CLOSING ANGLE.WC 55-2501.
- [SDR 7C7A2021102800038](https://openairdocs.org/sdr/7C7A2021102800038.md): None · none · Oct 27, 2021 · N893EA · Dhav DHC8106 · Main Landing Gear
  > DURING BUSHING REPLACEMENT ON R/H MLG SHOCK STRUT CYLINDER I/B TORQUE LINK LUG FOUND CORRODED.
- [SDR 7C7A2021102800037](https://openairdocs.org/sdr/7C7A2021102800037.md): None · none · Oct 26, 2021 · N893EA · Dhav DHC8106 · Elevator, Plate/Skin
  > L/H ELEVATOR UPPER SKIN OUTBOARD AREA HAS LOOSE RIVETS IN AREA YH139 AND YH145. REPAIRED WITH DOUBLER IAW RD8-55-3686.
- [SDR 7C7A2021102700036](https://openairdocs.org/sdr/7C7A2021102700036.md): None · none · Oct 24, 2021 · N893EA · Dhav DHC8106 · Nose/Tail Landing Gear Attach Section
  > CORROSION ON NLG TRUNNION PLATES (BOTH SIDES), IDENTIFIED AS PART OF GENERIC PERMANENT REPAIR FOR THIS CONDITION, AND REMOVED IAW RD8-53-3115.
- [SDR 7C7A2021102700035](https://openairdocs.org/sdr/7C7A2021102700035.md): None · none · Oct 24, 2021 · N893EA · Dhav DHC8106 · Rudder, Plate/Skin
  > DENTS ON TRAILING RUDDER R/H SKIN BETWEEN RIBS 4 - 5 & 19 - 20. REPAIRED IAW RD8-55-3680
- [SDR 7C7A2021102700034](https://openairdocs.org/sdr/7C7A2021102700034.md): None · none · Oct 24, 2021 · N893EA · Dhav DHC8106 · Fuselage Main, Plate/Skin
  > R/H FUSELAGE DENT AT STA X231.7 AND 0.30" ABOVE STRINGER 18S. REPAIRED IAW RD8-53-17249.
- [SDR 7C7A2021102700033](https://openairdocs.org/sdr/7C7A2021102700033.md): None · none · Oct 24, 2021 · N893EA · Dhav DHC8106 · Fuselage Main, Plate/Skin
  > R/H FUSELAGE SKIN DENT AT STA X194, 2 INCHES ABOVE STRINGER 31R. REPAIRED WITH RD8-53-17264.
- [SDR 7C7A2021102300032](https://openairdocs.org/sdr/7C7A2021102300032.md): None · none · Oct 23, 2021 · N893EA · Dhav DHC8106 · Nacelle/Pylon Structure
  > L/H NACELLE HORSE COLLARASSY, AFT LOWER ANGLE CRACKED ON OUTBOARD SIDE BETWEEN 9 - 10 O'CLOCK. REPAIRED IAW RD8-54-4461.
- [SDR 7C7A2021102300031](https://openairdocs.org/sdr/7C7A2021102300031.md): None · none · Oct 23, 2021 · N893EA · Dhav DHC8106 · Fuselage Structure (General)
  > R/H FUSELAGE DENT AT STA X178.20, ABOVE STRINGER 32R. REPAIRED IAW RD8-53-17264
- [SDR 7C7A2021102300030](https://openairdocs.org/sdr/7C7A2021102300030.md): None · none · Oct 23, 2021 · N893EA · Dhav DHC8106 · Trailing Edge Flaps
  > RH FLAP LOWER SKIN DAMAGEAT STA YW316.00. REPAIRED IAW RD8-57-9302
- [SDR 7C7A2021102300029](https://openairdocs.org/sdr/7C7A2021102300029.md): None · none · Oct 23, 2021 · N893EA · Dhav DHC8106 · Nacelle/Pylon Structure
  > L/H NACELLE HORSE COLLAR ASSY. FWD WEB FLANGE ON INBOARD SIDE CRACK BETWEEN 9 - 10 O' CLOCK. REPAIRED IAW RD8-54-4469
- [SDR 7C7A2021102200028](https://openairdocs.org/sdr/7C7A2021102200028.md): None · none · Oct 22, 2021 · N893EA · Dhav DHC8106 · Nacelle/Pylon Structure
  > L/H NACELLE HORSE COLLAR ASSY, FORWARD WEB FLANGE ON OUTBOARD SIDE, CRACK BTW 9 & 10 O'CLOCK. CRACK REMOVED BY CUTTOUT & ANGLE DOUBLER IAW RD8-54-4469
- [SDR 7C7A2021102200027](https://openairdocs.org/sdr/7C7A2021102200027.md): None · none · Oct 21, 2021 · N893EA · Dhav DHC8106 · Passenger Compartment Windows
  > R/H SIDE FORE RUDDER SKIN GOUGED/CUT BETWEEN RIBS 4 & 5. REPLACED SKIN DHC-8-100 SRM 55-40-28.
- [SDR 7C7A2021102200026](https://openairdocs.org/sdr/7C7A2021102200026.md): None · none · Oct 21, 2021 · N893EA · Dhav DHC8106 · Rudder, Plate/Skin
  > DENT BETWEEN RIBS 9 & 10 ON R/H SIDE OF TRAILING RUDDER, REPLACED SKIN DHC-8-100 SRM 55-40-28.
- [SDR 7C7A2021102200025](https://openairdocs.org/sdr/7C7A2021102200025.md): None · none · Oct 20, 2021 · N893EA · Dhav DHC8106 · Rudder, Plate/Skin
  > DENT ON LH SIDE TRAILING RUDDER BETWEEN RIBS 4 & 5 REPLACED SKIN DHC-8-100 SRM 55-40-28.
- [SDR 7C7A2021102200024](https://openairdocs.org/sdr/7C7A2021102200024.md): None · none · Oct 20, 2021 · N893EA · Dhav DHC8106 · Fuselage Main, Longeron/Stringer
  > CORROSION AT STRINGER 31R, AT STA 531 - 539, REPLACED DHC-8-100 SRM 51-40-07, 51-42-05 AND AMM 20-14-01.
- [SDR 7C7A2021102200023](https://openairdocs.org/sdr/7C7A2021102200023.md): None · none · Oct 19, 2021 · N893EA · Dhav DHC8106 · Fuselage Main, Longeron/Stringer
  > CORROSION ON STRINGER 31LH, SPLICE AT STA 531 REPLACED DHC-8-100 SRM 51-42-05, RD8-53-3044, DRAWING #85330220
- [SDR 7C7A2021102200022](https://openairdocs.org/sdr/7C7A2021102200022.md): None · none · Oct 19, 2021 · N893EA · Dhav DHC8106 · Fuselage Main, Floor Beam
  > CORROSIN ON RH INBD SEAT TRACK BETWEEN STA 564 - 600 REPLACED DHC-8-100 SRM 51-42-05, 51-40-10, DRAWING #85330469 RD8-53-4936
- [SDR 7C7A2021102200021](https://openairdocs.org/sdr/7C7A2021102200021.md): None · none · Oct 19, 2021 · N893EA · Dhav DHC8106 · Fuselage Main, Floor Beam
  > CORROSION ON LH INBD SEAT TRACK BTW STA 564 - 600 REPLACED DHC-8-100 SRM 51-42-05, RD8-53-1599, DRAWING #85330217
- [SDR 7C7A202110220020](https://openairdocs.org/sdr/7C7A202110220020.md): Window Frame · corroded · Oct 19, 2021 · N893EA · Dhav DHC8106 · Passenger Compartment Windows
  > CORROSION FOUND AT LH WINDOW #2 FRAME AT BOTTOM STA X302.4, REPLACED DHC-8-100 SRM 51-42-05.
- [SDR 7C7A2020032700022](https://openairdocs.org/sdr/7C7A2020032700022.md): Tail Cone · damaged · Mar 11, 2020 · N893EA · Dhav DHC8103 · Aerodynamic Fairings
  > FORWARD TAILCONE ASSEMBLY (P/N 85560061) HAS MULTIPLE AREAS OF BUBBLED PAINT AND SOFT COMPOSITE ALONG RIGHT SIDE OF FUSELAGE.
- [SDR 7C7A2020030500001](https://openairdocs.org/sdr/7C7A2020030500001.md): Skin · debonded · Mar 5, 2020 · N893EA · Dhav DHC8106 · Elevator, Plate/Skin
  > FOUND DURING PERFORMANCE OF MRB TASK CARD 5500/01. DISBOND AREA OF UPPER ELEVATOR SKIN.
- [SDR 7C7A2019091000512](https://openairdocs.org/sdr/7C7A2019091000512.md): Skin · dented · Sep 10, 2019 · N893EA · Dhav DHC8106 · Cargo/Baggage Doors
  > DENTS IN THE BAGGAGE DOOR OUTER SKIN P/N 85230002 BEYOND MFG LIMIT.
- [SDR 7C7A2019032000492](https://openairdocs.org/sdr/7C7A2019032000492.md): Inverter · failed · Mar 20, 2019 · N893EA · Dhav DHC8106 · AC Inverter
  > PRIMARY INVERTER FAILED.
- [SDR 7C7A2019030900490](https://openairdocs.org/sdr/7C7A2019030900490.md): Longeron · cracked · Mar 9, 2019 · N893EA · Dhav DHC8106 · Nacelle/Pylon, Longeron/Stringer
  > RCRACK IN LT NACELLE OB UPPER LONGERON 85410209 AT XN120.5. ECO 008.54-19.01, RD 8-54-4142, 7H-RW-32186.
- [SDR 7C7A2018070200452](https://openairdocs.org/sdr/7C7A2018070200452.md): Shutoff Valve · faulty · Jul 2, 2018 · N893EA · Dhav DHC8106 · Pneumatic Distribution System
  > DURING NR 2 ENGINE START, BLEED AIR CAME ON, A/C PRESSURIZED, AND SMELL OF FUMES IN COCKPIT. BLEED AIR SWITCHES NOT ON.
- [SDR 7C7A2018060500450](https://openairdocs.org/sdr/7C7A2018060500450.md): Skin · dented · Jun 5, 2018 · N893EA · Dhav DHC8106 · Elevator Tab Control System
  > THE LT ELEVATOR SPRING TAB WAS DENTED. REPLACED THE SKIN IAW SRM 51-42-05, AND 51-42-45
- [SDR 7C7A2018060400449](https://openairdocs.org/sdr/7C7A2018060400449.md): Skin · dented · Jun 4, 2018 · N893EA · Dhav DHC8106 · Fuselage Main, Plate/Skin
  > DENT FOUND ON THE LT SKIN AT BS 110 AND.3 INCHES ABOVE STRINGER 10L. REPAIRED IAW RD 8-53-15705 AND ECO 008-53-18.30.
- [SDR 7C7A2018060400448](https://openairdocs.org/sdr/7C7A2018060400448.md): Skin · dented · Jun 4, 2018 · N893EA · Dhav DHC8106 · Elevator Tab Control System
  > DENT ON ELEVATOR SPRING TAB AT XH 41. THE SKIN WAS REPLACED IAW RD 8-55-565.
- [SDR 7C7A2018053100447](https://openairdocs.org/sdr/7C7A2018053100447.md): Bracket · corroded · May 31, 2018 · N893EA · Dhav DHC8106 · Fuselage Miscellaneous Structure
  > PAX DOOR THRESHOLD AND BRACKET CORRODED. REPLACED IAW SRM 51-42-05.
- [SDR 7C7A2018053100446](https://openairdocs.org/sdr/7C7A2018053100446.md): Tab · dented · May 31, 2018 · N893EA · Dhav DHC8106 · Aileron Tabs
  > RIGHT AILERON TRIM TAB TRAILING EDGE WAS FOUND DENTED. REPAIRED IAW RD 8-57-112 AND WC 57-398.
- [SDR 7C7A2018053100445](https://openairdocs.org/sdr/7C7A2018053100445.md): Doubler · corroded · May 31, 2018 · N893EA · Dhav DHC8106 · Fuselage Miscellaneous Structure
  > TOILET INNER DOUBLER BETWEEN BS 203 - 222, STRINGER 27R WAS CORRODED. REPAIRED IAW RD 8-53-2103.
- [SDR 7C7A2018052500443](https://openairdocs.org/sdr/7C7A2018052500443.md): Skin · dented · May 25, 2018 · N893EA · Dhav DHC8106 · Fuselage Main, Plate/Skin
  > MULTIPLE DENTS ON FUSELAGE BELLY PANEL. RD8-53-15761 AND ECO 008.53-18.49.
- [SDR 7C7A201805150435](https://openairdocs.org/sdr/7C7A201805150435.md): Skin · dented · May 11, 2018 · N893EA · Dhav DHC8106 · Fuselage Main, Plate/Skin
  > THE BOTTOM FUSELAGE SKIN BETWEEN BS 240.5 - 270.5, STRINGERS 30S - 32S WAS DENTED. REMOVED THE DAMAGE AND REPAIRED IAW RD 8-53-15717 AND ECO 008.53-18.45.
- [SDR 7C7A2018052200441](https://openairdocs.org/sdr/7C7A2018052200441.md): Skin · damaged · May 10, 2018 · N893EA · Dhav DHC8106 · Fuselage Main, Plate/Skin
  > DAMAGE TO THE RH FUSELAGE SKIN PANEL. REPAIRED IAW RD 8-53-15756, AND ECO 008.53-18.48.
- [SDR 7C7A201805150436](https://openairdocs.org/sdr/7C7A201805150436.md): Angle · cracked · May 10, 2018 · N893EA · Dhav DHC8106 · Nacelle/Pylon Miscellaneous Structure
  > LEFT ENGINE HORSE-COLLAR RIGHT SIDE FORWARD ANGLE CRACKED. THE ANGLE WAS REPAIRED IAW RD 8-54-1736, AND ECO 008.51-17.01.

Next page: https://openairdocs.org/deregistered/N893EA-2024-02-13/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 = 'N893EA' AND deregistration_id = 'N893EA-2024-02-13'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N893EA-2024-02-13/reports

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