# Service difficulty reports: N884EA

A list on [N884EA](https://openairdocs.org/aircraft/N884EA.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 · 95 reports

- [SDR 7C7A2025012300003](https://openairdocs.org/sdr/7C7A2025012300003.md): Wire Harness · inoperative · Jan 23, 2025 · N884EA · Dhav DHC8106 · Landing Gear System Wiring
  > "ALT GEAR IND FAIL" ANNUNCIATOR CAME ON IN FLIGHT. RIGHT MAIN ALT LIGHT WAS INOP.
- [SDR 7C7A2022121900039](https://openairdocs.org/sdr/7C7A2022121900039.md): Warning Message · illuminated · Dec 18, 2022 · N884EA · Dhav DHC8106 · Engine Air Intake System
  > #1 ENGINE INTAKE BYPASS DOOR OPEN LIGHT INTERMITTENT IN FLIGHT. OPEN LIGHT ILLUMINATES WHEN ADVISORY LIGHT TEST SWITCH MOVED TO ADVISORY
- [SDR 7C7A2022072100024](https://openairdocs.org/sdr/7C7A2022072100024.md): Brake Assy · corroded · Jul 21, 2022 · N884EA · Dhav DHC8106 · Brake
  > MAINTENANCE WAS TAXING AIRCRAFT BACK FROM ENGINE RUNS. WHEN THEY PARKED AT HANGER THE #1 BRAKE CAUGHT ON FIRE. FIRE WAS EXTINGUISHED BY MAINTENANCE TECHNICIANS. BRAKE WAS SENT TO OVERHAUL VENDOR TO DETERMINE WHAT THE CAUSE OF THE FIRE WAS. OVERHAUL FACILITY FO
- [SDR 7C7A2022061900022](https://openairdocs.org/sdr/7C7A2022061900022.md): Aileron · cracked · Jun 19, 2022 · N884EA · Dhav DHC8106 · Ailerons
  > R/H AILERON TOP STRINGER AT RIVET LINE 13 FROM INBOARD (APPROX YW 450) FOUND CRACKED. REPAIRED IAW DHC-8-100 RD8-57-052.
- [SDR 7C7A2022061600021](https://openairdocs.org/sdr/7C7A2022061600021.md): Rudder · dented · Jun 16, 2022 · N884EA · Dhav DHC8106 · Rudder, Plate/Skin
  > DENT ON FORE RUDDER L/H SIDE BETWEEN RIB 19 AND 20. REPAIRED WITH DOUBLER PATCH IAW DHC RD8-55-3763
- [SDR 7C7A2022060800020](https://openairdocs.org/sdr/7C7A2022060800020.md): Cargo Track · corroded · Jun 8, 2022 · N884EA · Dhav DHC8106 · Fuselage Main, Floor Beam
  > CARGO SEAT TRACK CORROSION BETWEEN STS X545 & X600
- [SDR 7C7A2022060700019](https://openairdocs.org/sdr/7C7A2022060700019.md): Skin Splice · dented · Jun 7, 2022 · N884EA · Dhav DHC8106 · Fuselage Main, Structure
  > FUSELAGE SKIN DENT STA 479 NEAR STR 32S. REPAIRED WITH DOUBLER IAW DHC-8-100 SRM 53-30-21.
- [SDR 7C7A2019022200489](https://openairdocs.org/sdr/7C7A2019022200489.md): Aileron · dented · Feb 22, 2019 · N884EA · Dhav DHC8106 · Ailerons
  > DENT RT AILERON TRAILING EDGE STA YW499.300. REPAIRED PER RD 8-57-8556, ECO 008.27-19-04, NDT REPORT (NO CRACK OR DISBOND INDICATION FOUND), 7H-RW-29504 AND 7H-NRW-5313.
- [SDR 7C7A2019022200488](https://openairdocs.org/sdr/7C7A2019022200488.md): Floor Support · corroded · Feb 22, 2019 · N884EA · Dhav DHC8106 · Fuselage Miscellaneous Structure
  > LH CABIN UNDER FLOOR STINGER RELACED DO TO CORROSION. FABRICATED STRINGER AND REPLACED CORRODED STRING. PREMIER WC 53-342 AND 7H-NRW-5673.
- [SDR 7C7A2019022000487](https://openairdocs.org/sdr/7C7A2019022000487.md): Skin · damaged · Feb 20, 2019 · N884EA · Dhav DHC8106 · Fuselage Main, Plate/Skin
  > MULTIPLE DAMAGE LOWER FUSELAGE SKIN PN:85320106. WC 53-337, 7H-RW-29516, 7H-NRW-5671, RD 8-53-16037, AND ECO 008.53-19.06.
- [SDR 7C7A2019021600486](https://openairdocs.org/sdr/7C7A2019021600486.md): Fitting · corroded · Feb 16, 2019 · N884EA · Dhav DHC8106 · Fuselage Main, Attach Fittings
  > TOILET DRAIN MACHINED FITTING CORRORED BEOND LIMITS. MACHINNED FITTING R&R. SEE PREMIER W/C 53-325 FOR DETIALS.
- [SDR 7C7A2019021500483](https://openairdocs.org/sdr/7C7A2019021500483.md): Skin · gouged · Feb 15, 2019 · N884EA · Dhav DHC8106 · Fuselage Main, Plate/Skin
  > GOUGE ON LOWER FUSE SKIN DAMAGE REPAIRED IAW RD 8-53-16047. SEE WC 53-366, 7H-RW-29520, 7H-NRW-5730, NDT REPORT, AND ECO 008.53-19.08.
- [SDR 7C7A2019021500482](https://openairdocs.org/sdr/7C7A2019021500482.md): Skin · damaged · Feb 15, 2019 · N884EA · Dhav DHC8106 · Fuselage Main, Plate/Skin
  > SKIN DAMAGED, REPAIRED IAW RD 8-53-15935. SEE WC 53-336, 7H-RW-29505, 7H-NRW-5670, NDT REPORT AND ECO 008.53-19.04.
- [SDR 7C7A2019021500481](https://openairdocs.org/sdr/7C7A2019021500481.md): Clamp · corroded · Feb 15, 2019 · N884EA · Dhav DHC8106 · Fuselage Main, Attach Fittings
  > DUCT CLAMP ATTACHEMENT TO STRINGER 30L CORRODED. SEE WC 53-319 FOR CORROSION REMOVAL.
- [SDR 7C7A2019021200479](https://openairdocs.org/sdr/7C7A2019021200479.md): Skin · damaged · Feb 12, 2019 · N884EA · Dhav DHC8106 · Fuselage Main, Plate/Skin
  > DENT AND SCRATCH ON L/H FUSELAGE SKIN, WC 53-351, 7H-RW-29519, 7H-NRW-5682, RD 8-53-16036, AND ECO 008.53-19.07.
- [SDR 7C7A2019021200478](https://openairdocs.org/sdr/7C7A2019021200478.md): Skin · damaged · Feb 12, 2019 · N884EA · Dhav DHC8106 · Fuselage Main, Plate/Skin
  > MULTIPLE DAMAGE RH LOWER FUSELAGE SKIN, WC53-333, 7H-RW-29284, 7H-NRW-5667, RD 8-53-16038, AND ECO 008.53-19.05.
- [SDR 7C7A2019021200477](https://openairdocs.org/sdr/7C7A2019021200477.md): Skin · damaged · Feb 12, 2019 · N884EA · Dhav DHC8106 · Fuselage Main, Plate/Skin
  > MULTIPLE DAMAGES LOWER FUSELAGE SKIN PN 85320106. PREMIER WC 53-332,7H-RW-29283, 7H-NRW-5666, RD 8-53-15959 AND ECO 008.53-19.02
- [SDR 7C7A2019020900476](https://openairdocs.org/sdr/7C7A2019020900476.md): Rudder · dented · Feb 9, 2019 · N884EA · Dhav DHC8106 · Rudder Structure
  > DENT LT FORE RUDDER RD 8-55-3260 AND ECO 008.27-19.01 FOR DETAILS.
- [SDR 7C7A2019020900475](https://openairdocs.org/sdr/7C7A2019020900475.md): Flap · dented · Feb 9, 2019 · N884EA · Dhav DHC8106 · Trailing Edge Flaps
  > RT OB FLAP DENT RD 8-57-8554 AND ECO 008.27-19.03.
- [SDR 7C7A2019020900474](https://openairdocs.org/sdr/7C7A2019020900474.md): Strap · corroded · Feb 9, 2019 · N884EA · Dhav DHC8106 · Fuselage Miscellaneous Structure
  > LT CABIN AT X539 AT STR 23 TO 25 STRAP CORROSION LEVEL 2 LOCAL. CORRODED STRAP REPLACED REMOVING ALL CORROSION.
- [SDR 7C7A2018060500451](https://openairdocs.org/sdr/7C7A2018060500451.md): Beta Switch · broken · Jun 5, 2018 · N884EA · Dhav DHC8106 · Propeller Controlling System
  > #1 PROP OVER TORQUE
- [SDR 7C7A2017063000330](https://openairdocs.org/sdr/7C7A2017063000330.md): Battery Pack · discharged · Jun 29, 2017 · N884EA · Dhav DHC8106 · Emergency Lighting
  > EMERGENCY LIGHT BY ROW 4A INOPERATIVE, R & R BAD EMERGENCY LIGHT BATTERY RECEPTACLE AND OPS CHECKED GOOD IAW MM 33-52-00.
- [SDR 7C7A2017021400285](https://openairdocs.org/sdr/7C7A2017021400285.md): Stringer · corroded · Feb 14, 2017 · N884EA · Dhav DHC8106 · Fuselage Main, Longeron/Stringer
  > CORROSION FOUND ON STR 24P AT STA X370.8.
- [SDR 7C7A2017021400284](https://openairdocs.org/sdr/7C7A2017021400284.md): Seat Track · corroded · Feb 14, 2017 · N884EA · Dhav DHC8106 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION FOUND ON LT IB SEAT TRACK BETWEEN STA X200.0 AND X262.0.
- [SDR 7C7A2017013100283](https://openairdocs.org/sdr/7C7A2017013100283.md): Rib · cracked · Jan 31, 2017 · N884EA · Dhav DHC8106 · Rudder, Spar/Rib
  > TRAILING RUDDER, CENTER HINGE, TOP LEADING EDGE RIB CRACKED
- [SDR 7C7A2017013100282](https://openairdocs.org/sdr/7C7A2017013100282.md): Strap · cracked · Jan 31, 2017 · N884EA · Dhav DHC8106 · Nacelle/Pylon Miscellaneous Structure
  > RT NACELLE AFT END HEAT SHIELD STRAP CRACKED.
- [SDR 7C7A2017013100281](https://openairdocs.org/sdr/7C7A2017013100281.md): Structure · cracked · Jan 31, 2017 · N884EA · Dhav DHC8106 · Engine Mount Section
  > RIGHT ENGINE HORSE COLLAR CRACKED ON OUTBOARD FWD SIDE LOWER ANGLE, INBOARD FWD LOWER SIDE ANGLE, FWD, OUTBOARD AFT LOWER ANGLE
- [SDR 7C7A2017013100280](https://openairdocs.org/sdr/7C7A2017013100280.md): Heat Shield · punctured · Jan 31, 2017 · N884EA · Dhav DHC8106 · Nacelle/Pylon Miscellaneous Structure
  > LT NACELLE HEAT SHIELD PUNCTURED.
- [SDR 7C7A2017013100279](https://openairdocs.org/sdr/7C7A2017013100279.md): Skin · cracked · Jan 31, 2017 · N884EA · Dhav DHC8106 · Nacelle/Pylon, Plate/Skin
  > LEFT NACELLE FWD DOOR CUT OUT FWD INBD CORNER CRACKED.
- [SDR 7C7A2017013100278](https://openairdocs.org/sdr/7C7A2017013100278.md): Strap · cracked · Jan 31, 2017 · N884EA · Dhav DHC8106 · Nacelle/Pylon Miscellaneous Structure
  > LEFT NACELLE OUTBOARD SKIN DISH PANEL STRAP CRACKED
- [SDR 7C7A2017013100277](https://openairdocs.org/sdr/7C7A2017013100277.md): Floorbeam · cracked · Jan 31, 2017 · N884EA · Dhav DHC8106 · Fuselage Main, Floor Beam
  > RIGHT FLOORBEAM CRACKED AT BS 253.4 OUTBOARD.
- [SDR 7C7A2016121100272](https://openairdocs.org/sdr/7C7A2016121100272.md): Battery Pack · inoperative · Dec 11, 2016 · N884EA · Dhav DHC8106 · Emergency Lighting
  > TWO EMERGENCY EXIT LIGHTS INOPERATIVE. R & R THE BATTERY PACK. ALL EMERGENCY LIGHTS OPS CHECKED GOOD
- [SDR 7C7A2016112700265](https://openairdocs.org/sdr/7C7A2016112700265.md): Battery · discharged · Nov 27, 2016 · N884EA · Dhav DHC8106 · Emergency Lighting
  > FWD OVERHEAD & RT EMERGENCY LIGHTS OUT. R&R EMERGENCY LIGHT BATTERY 3351-PS2 & AX EMERGENCY LIGHTS. OPS CHECK GOOD REF -8MM CH 33-52-00.
- [SDR 7C7A2016111000257](https://openairdocs.org/sdr/7C7A2016111000257.md): Floor Support · cracked · Oct 14, 2016 · N884EA · Dhav DHC8106 · Fuselage Miscellaneous Structure
  > CRACK DAMAGE TO THE LOWER FRONT FUSELAGE FLOOR SUPPORT AT BS 136.8. REPAIRED IAW RD 8-53-14815
- [SDR 7C7A2016072100250](https://openairdocs.org/sdr/7C7A2016072100250.md): Battery Pack · discharged · Jul 21, 2016 · N884EA · Dhav DHC8106 · Emergency Lighting
  > ROW 4 LEFT EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE BATTERY PACK.
- [SDR 7C7A20160114002](https://openairdocs.org/sdr/7C7A20160114002.md): Hydraulic Line · contaminated · Jan 12, 2016 · N884EA · Dhav DHC8106 · Hydraulic System, Main
  > NOSE GEAR FAILED TO EXTEND USING NORMAL GEAR EXTENSION. NOSE GEAR EXTENDED FOLLOWING COMPLETION OF ALTERNATE LANDING GEAR EXTENSION CHECKLIST. CAUSE DETERMINED TO BE AIR IN THE HYD LINE.
- [SDR 7C7A20151216101](https://openairdocs.org/sdr/7C7A20151216101.md): Duct · cracked · Dec 14, 2015 · N884EA · Dhav DHC8106 · Engine Cowling System
  > CRACK DAMAGE IN ATTACHMENT BRACKET ON STARTER GENERATOR INTAKE DUCT ASSEMBLY.
- [SDR 7C7A20150821070](https://openairdocs.org/sdr/7C7A20150821070.md): Battery · discharged · Aug 20, 2015 · N884EA · Dhav DHC8106 · Emergency Lighting
  > SEVERAL EMER EXIT LIGHTS IN THE CABIN DO NOT REMAIN ILLUMINATED WHEN THE EMER LIGHTS ARE SELECTED ON. R & R TOP BATTERY BOX IN WARDROBE FOR EMER LIGHTS. OPERATIONS CHECKED. R & R EMER BATTERY ALSO.
- [SDR 7C7A20150720069](https://openairdocs.org/sdr/7C7A20150720069.md): Strap · cracked · Jul 20, 2015 · N884EA · Dhav DHC8106 · Nacelle/Pylon Miscellaneous Structure
  > CRACK FOUND DURING ROUTINE INSPECTION ON THE INBD SIDE OF THE NACELLE NR 2 LANDING STRAP AT STATION XN64.0 & YN8.48.
- [SDR 7C7A201411140078](https://openairdocs.org/sdr/7C7A201411140078.md): Threshold · corroded · Nov 14, 2014 · N884EA · Dhav DHC8106 · Fuselage Miscellaneous Structure
  > PASSENGER DOOR OPENING THRESHOLD MEMBER CORROSION BEYOND BLEND LIMITS
- [SDR 7C7A2014111400077](https://openairdocs.org/sdr/7C7A2014111400077.md): Rib · cracked · Nov 14, 2014 · N884EA · Dhav DHC8106 · Fuselage Main, Bulkhead
  > RADAR BULKHEAD LT AND RT VERTICAL RIBS CRACKED AT TOP LOCATION
- [SDR ERAA201411120075](https://openairdocs.org/sdr/ERAA201411120075.md): Access Panel · corroded · Nov 12, 2014 · N884EA · Dhav DHC8106 · Wing, Plate/Skin
  > PANEL 624BT HAS CORROSION IN 2 COUNTERSINKS FOR PANEL BOLT HOLES
- [SDR ERAA201411120074](https://openairdocs.org/sdr/ERAA201411120074.md): Access Panel · corroded · Nov 12, 2014 · N884EA · Dhav DHC8106 · Wing, Plate/Skin
  > ACCESS PANEL 524CT HAS CORROSION IN TWO COUNTERSINKS.
- [SDR ERAA201411120073](https://openairdocs.org/sdr/ERAA201411120073.md): Access Panel · corroded · Nov 12, 2014 · N884EA · Dhav DHC8106 · Wing, Plate/Skin
  > ACCESS PANEL 524BT HAS CORROSION IN THREE COUNTERSINKS.
- [SDR ERAA201411120072](https://openairdocs.org/sdr/ERAA201411120072.md): Access Panel · corroded · Nov 12, 2014 · N884EA · Dhav DHC8106 · Wing, Plate/Skin
  > ACCESS PANEL 534AT HAS CORROSION IN 4 COUNTERSINKS.
- [SDR ERAA201411120071](https://openairdocs.org/sdr/ERAA201411120071.md): Strap · corroded · Nov 12, 2014 · N884EA · Dhav DHC8106 · Nacelle/Pylon Miscellaneous Structure
  > LEFT NACELLE TAIL CONE JOINT STRAP CORRODED
- [SDR ERAA201411120070](https://openairdocs.org/sdr/ERAA201411120070.md): Tee Fitting · corroded · Nov 12, 2014 · N884EA · Dhav DHC8106 · Fuselage Main, Attach Fittings
  > TEE FITTING UNDER PAX ENTRANCE FLOORBOARD. CORROSION AROUND ANCHOR NUT HOLE OUT OF LIMITS IAW SRM53-00-16
- [SDR ERAA201411120069](https://openairdocs.org/sdr/ERAA201411120069.md): Window Frame · corroded · Nov 12, 2014 · N884EA · Dhav DHC8106 · Fuselage Main, Structure
  > CORROSION REMOVAL NOT PERMISSIBLE AT THIS LOCATION IAW RD8-53-6323 FOR CABIN WINDOW FRAME
- [SDR 7C7A201411110068](https://openairdocs.org/sdr/7C7A201411110068.md): Angle · cracked · Nov 11, 2014 · N884EA · Dhav DHC8106 · Nacelle/Pylon Miscellaneous Structure
  > LEFT NACELLE FINGERNAIL REAR ANGLE CRACKED AND OUTBD MISSING RIVET. REPLACED ANGLE WITH NEW WC 4007
- [SDR ERAA20140023](https://openairdocs.org/sdr/ERAA20140023.md): Pump · overtemp · Apr 26, 2014 · N884EA · Dhav DHC8106 · Hydraulic Pump, Auxiliary
  > NUMBER 1 STBY PUMP HYD HOT LIGHT ILLUMINATED. WHEN NR 1 STBY PUMP SELECTED TO NORM IN FIGHT, HYD PRESS GRADUALLY DECREASED. WHEN PUMP IS CYCLED, PRESS ONLY INCREASES TO APPROX 800 PSI. NR 1 STBY PRESS INCREASED TO 2700 WHEN FLAPS SELECTED FOR LANDING WITH S

Next page: https://openairdocs.org/aircraft/N884EA/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 = 'N884EA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N884EA/reports

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