# Service difficulty reports: N882EA, cancelled Nov 20, 2013

A list on [N882EA, cancelled Nov 20, 2013](https://openairdocs.org/deregistered/N882EA-2013-11-20.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 · 68 reports

- [SDR ERAA201309170063](https://openairdocs.org/sdr/ERAA201309170063.md): Generator · defective · Sep 14, 2013 · N882EA · Dhav DHC8103 · AC Generator-Alternator
  > ACFT NR 2 GENERATOR FAILED. R & R NR 2 AC GENERATOR IAW MM 24-21-01. OPS AND LEAK CHECKED GOOD.
- [SDR ERAA201308260056](https://openairdocs.org/sdr/ERAA201308260056.md): Oil Cooler · defective · Aug 23, 2013 · N882EA · Dhav DHC8103 · AC Generator-Alternator
  > NR 2 AC GENERATOR HOT ANNUNCIATOR ILLUMINATED ON TAKEOFF. ENGINE OIL TEMP 110 DEGREES INDICATED. TAKEOFF ABORTED-NO FLIGHT. R & R NR 2 ENGINE OIL COOLER TEMPERATURE REGULATOR VALVE. GROUND RUN OPS AND LEAK CHECKED GOOD. OK FOR SERVICE.
- [SDR ERAA20130024](https://openairdocs.org/sdr/ERAA20130024.md): Light · inoperative · Feb 21, 2013 · N882EA · Dhav DHC8103 · Emergency Lighting
  > EMERGENCY LIGHT INOP AFT ROW CEILING. RELAMPED AS REQUIRED, OPS CHECK GOOD.
- [SDR ERAA20120132](https://openairdocs.org/sdr/ERAA20120132.md): Frame · cracked · Dec 8, 2012 · N882EA · Dhav DHC8103 · Fuselage Main, Frame
  > CRACK FOUND ON RIGHT FUSELAGE FRAME AT STATION X354 BETWEEN STATION 20S AND 33S.
- [SDR ERAA20120131](https://openairdocs.org/sdr/ERAA20120131.md): Skin Panel · gouged · Dec 8, 2012 · N882EA · Dhav DHC8103 · Fuselage Main, Plate/Skin
  > SKIN DAMAGE TO RIGHT FUSELAGE SKIN AT STATION X342 BETWEEN STRINGER 12S AND 13S. REPAIRED TO BOMBARDIER REPAIR DRAWING 8-53-2181.
- [SDR ERAA201212080130](https://openairdocs.org/sdr/ERAA201212080130.md): Skin · nicked · Dec 8, 2012 · N882EA · Dhav DHC8103 · Fuselage Main, Plate/Skin
  > NICK ON SKIN AT RIGHT FUSELAGE AT STATION X342 BETWEEN STRINGER 12S AND 13S. REPAIRED TO BOMBARDIER REPAIR DRAWING 853-2181.
- [SDR ERAA20120130](https://openairdocs.org/sdr/ERAA20120130.md): Seat Track · corroded · Dec 8, 2012 · N882EA · Dhav DHC8103 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION FOUND ON LEFT INBOARD SEAT TRACK. REPAIRED TO BOMBARDIER REPAIR DRAWING 8-53-3074.
- [SDR ERAA20120129](https://openairdocs.org/sdr/ERAA20120129.md): Frame · corroded · Dec 8, 2012 · N882EA · Dhav DHC8103 · Fuselage Main, Frame
  > FRAME FOUND CORRODED AT STATION X312 BETWEEN STRINGER 29P AND 30P AND 31P AND 32P. REPAIRED TO BOMBARDIER SRM 53-00-16.
- [SDR ERAA2120128](https://openairdocs.org/sdr/ERAA2120128.md): Seat Track · corroded · Dec 7, 2012 · N882EA · Dhav DHC8103 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION FOUND ON LEFT SEAT TRACK BETWEEN SAT X526 AND X 600. REMOVED AND REPLACED WITH NEW BY BOMBARDIER SRM 51-40-10.
- [SDR ERAA20120127](https://openairdocs.org/sdr/ERAA20120127.md): Access Panel · corroded · Dec 7, 2012 · N882EA · Dhav DHC8103 · Wing, Plate/Skin
  > RIGHT STRESS PANEL HAS CORROSION UNDER COUNTERSINK SCREW HOLES. REPLACED RIGHT STRESS PANEL 85711802-005.
- [SDR ERAA20120126](https://openairdocs.org/sdr/ERAA20120126.md): Access Panel · corroded · Dec 7, 2012 · N882EA · Dhav DHC8103 · Wing, Plate/Skin
  > LEFT STRESS PANEL HAS CORROSION UNDER COUNTERSINK SCREW HOLES. REPLACED LEFT STRESS PANEL P/N 85711802-005.
- [SDR ERAA20120124](https://openairdocs.org/sdr/ERAA20120124.md): Seat Track · corroded · Dec 6, 2012 · N882EA · Dhav DHC8103 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION FOUND ON RIGHT ONBOARD SEAT TRACK BETWEEN STATION X262 AND X526. REPAIRED USING BOMBARDIER REPAIR DRAWING 8-53-1339.
- [SDR ERAA201201223](https://openairdocs.org/sdr/ERAA201201223.md): Intercostal · corroded · Dec 6, 2012 · N882EA · Dhav DHC8103 · Passenger/Crew Doors
  > LIGHT SURFACE CORROSION FOUND AT STEP OF PASSENGER DOOR ENTRANCE. REPLACED INTERCOSTAL IN ACCORDANCE WITH BOMBARDIER SRM 52-10-00.
- [SDR ERAA20120122](https://openairdocs.org/sdr/ERAA20120122.md): Frame · corroded · Dec 6, 2012 · N882EA · Dhav DHC8103 · Fuselage Main, Frame
  > FRAME CORRODED AT STATION X446 BETWEEN STRINGERS 32S AND 33. FRAME REPLACED WITH NEW TO BOMBARDIER SRM 53-20-21.
- [SDR ERAA20120121](https://openairdocs.org/sdr/ERAA20120121.md): Spar · corroded · Dec 6, 2012 · N882EA · Dhav DHC8103 · Wing Spar
  > LEFT WING FRONT SPAR AT UPPER AND LOWER LEADING EDGE SEATS HAVE BARE METAL AND CORROSION. REPAIRED BETWEEN YW57 AND YW 139 TO BOMBARDIER REPAIR DRAWING 8-57-811.
- [SDR ERAA20120120](https://openairdocs.org/sdr/ERAA20120120.md): Seat Track · corroded · Dec 6, 2012 · N882EA · Dhav DHC8103 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION FOUND RIGHT SEAT TRACK BETWEEN STATION X264 AND X504. REPAIRED TO BOMBARDIER REPAIR DRAWING 8-53-1342.
- [SDR ERAA2120119](https://openairdocs.org/sdr/ERAA2120119.md): Seat Track · corroded · Dec 6, 2012 · N882EA · Dhav DHC8103 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION FOUND ON LEFT INBOARD SEAT TRACK BETWEEN STATION X285 AND X526. REPAIRED TO BOMBARDIER REPAIR DRAWING 8-53-1339.
- [SDR ERAA20120118](https://openairdocs.org/sdr/ERAA20120118.md): Frame · cracked · Dec 6, 2012 · N882EA · Dhav DHC8103 · Fuselage Main, Frame
  > FUSELAGE FRAME FOUND CRACKED AT X264.1 AND STR 21S AND INTERCOSTAL X264.4 CRACKED AT SEAT TRACK LEVEL. NEW FRAME REPLACED P/N 85320534-007.
- [SDR ERAA20120117](https://openairdocs.org/sdr/ERAA20120117.md): Bracket · cracked · Dec 6, 2012 · N882EA · Dhav DHC8103 · Passenger/Crew Doors
  > PASSENGER DOOR SHELL FORWARD LOWER BRACKET CRACKED. REPLACED BRACKET P/N 85210223-101 WITH NEW.
- [SDR ERAA2120116](https://openairdocs.org/sdr/ERAA2120116.md): Sill · corroded · Dec 4, 2012 · N882EA · Dhav DHC8103 · Cargo/Baggage Doors
  > AFT CARGO DOOR SILL FOUND WITH SURFACE CORROSION.
- [SDR ERAA20120115](https://openairdocs.org/sdr/ERAA20120115.md): Structure · corroded · Dec 4, 2012 · N882EA · Dhav DHC8103 · Passenger/Crew Doors
  > BARE METAL AND LIGHT SURFACE CORROSION AT LOWER SECTION OF INSIDE OF PASSENGER DOOR SHELL.
- [SDR ERAA20120114](https://openairdocs.org/sdr/ERAA20120114.md): Casting · corroded · Dec 4, 2012 · N882EA · Dhav DHC8103 · Fuselage Miscellaneous Structure
  > LAVATORY CASTING FOUND SLIGHTLY CORRODED. REPLACED CASTING P/N 85320980-105.
- [SDR ERAA20120113](https://openairdocs.org/sdr/ERAA20120113.md): Stop Fitting · worn · Dec 3, 2012 · N882EA · Dhav DHC8103 · Cargo/Baggage Doors
  > CARGO DOOR STOPS FOUND WORN. BLENDED STOPS IN ACCORDANCE WITH BOMBARDIER REPAIR DRAWING 8-53-104. P/NS 8533064,85332439, 85330365, 85330366, 85332440, 85330367
- [SDR ERAA2120112](https://openairdocs.org/sdr/ERAA2120112.md): Seat Track · corroded · Dec 1, 2012 · N882EA · Dhav DHC8103 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION FOUND ON RIGHT INBOARD SEAT TRACK BETWEEN STATIONS X182 AND X 262.
- [SDR ERAA20120111](https://openairdocs.org/sdr/ERAA20120111.md): Seat Track · corroded · Dec 1, 2012 · N882EA · Dhav DHC8103 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION FOUND ON LEFT OUTBOARD SEAT TRACK BETWEEN STATION X504 AND X545.
- [SDR ERAA2120110](https://openairdocs.org/sdr/ERAA2120110.md): Skin Panel · dented · Nov 29, 2012 · N882EA · Dhav DHC8103 · Vertical Stabilizer, Plate/Skin
  > DENT FOUND ON RIGHT STATION FORWARD BOTTOM VERTICAL STAB SKIN PANEL P/N 85530011 BETWEEN THE FRONT SPAR AND MIDDLE SPAR AT STIFFENER 85530107-105 BETWEEN RIBS TWO AND THREE.
- [SDR ERAA20120109](https://openairdocs.org/sdr/ERAA20120109.md): Fitting · corroded · Nov 27, 2012 · N882EA · Dhav DHC8103 · Fuselage Miscellaneous Structure
  > FITTING CORRODED BEYOND SRM LIMITS AT STA X531 AND STR 31P
- [SDR ERAA20120108](https://openairdocs.org/sdr/ERAA20120108.md): Skin Panel · gouged · Nov 26, 2012 · N882EA · Dhav DHC8103 · Emergency Exits
  > GOUGE DAMAGE TO THE RIGHT EMERGENCY DOOR OUTER SKIN PART NUMBER 85220030.
- [SDR ERAA20120107](https://openairdocs.org/sdr/ERAA20120107.md): Shear Web · corroded · Nov 24, 2012 · N882EA · Dhav DHC8103 · Fuselage Miscellaneous Structure
  > REMOVAL OF THE AFT CARGO SEAT TRACK REVEALED CORROSION UNDER THE RIGHT AFT CARGO TRACK AND DAMAGE TO THE SHEAR WEB P/N 85330431 BETWEEN X580.5 AND X600 STA 31S.
- [SDR ERAA20120106](https://openairdocs.org/sdr/ERAA20120106.md): Skin Panel · chafed · Nov 22, 2012 · N882EA · Dhav DHC8103 · Fuselage Main, Plate/Skin
  > VISUAL INSPECTION OF FUSELAGE PANEL P/N 85350327 REVEALED WEAR DAMAGE TO LOWER SURFACE OF THE PANEL.
- [SDR ERAA20120105](https://openairdocs.org/sdr/ERAA20120105.md): Nut Plate · stripped · Nov 22, 2012 · N882EA · Dhav DHC8103 · Trailing Edge Flaps
  > FUNCTIONAL CHECK OF THE LEFT NR 1 FLAP TRACK FASTENERS FAILED TORQUE CHECK. ON FLAP SUPPORT TRACK P/N 85780039. FAILED AT THREE LOCATIONS.
- [SDR ERAA20120104](https://openairdocs.org/sdr/ERAA20120104.md): Flap · delaminated · Nov 20, 2012 · N882EA · Dhav DHC8103 · Trailing Edge Flaps
  > DELAMINATION DAMAGE FOUND ON TRAILING EDGE FLAP ON LEFT WING P/N 85750233 AND P/N 85750245. TWO AREAS 1. 5.3" IN LENGTH 2. 7.1" IN LENGTH.
- [SDR ERAA20120103](https://openairdocs.org/sdr/ERAA20120103.md): Strap · cracked · Nov 19, 2012 · N882EA · Dhav DHC8103 · Wing Miscellaneous Structure
  > CRACKED LOWER REINFORCEMENT STRAPS ON LEFT WING STRINGER 12-16. PART NUMBER 85711248 AT YW197
- [SDR ERAA20120102](https://openairdocs.org/sdr/ERAA20120102.md): Plate · cracked · Nov 16, 2012 · N882EA · Dhav DHC8103 · Wing Miscellaneous Structure
  > CRACK AT RIGHT WING LADDER PLATE AT OUTBOARD OF YW139.2 AND STRINGER 4. PLATE P/N 85711069
- [SDR ERAA20120101](https://openairdocs.org/sdr/ERAA20120101.md): Skin Panel · scratched · Nov 16, 2012 · N882EA · Dhav DHC8103 · Fuselage Main, Plate/Skin
  > SCRATCH DAMAGE FOUND AT LOWER FUSELAGE SKIN PNL 8532016 BETWEEN FRAME STATION X222.0 -X-240.5 ALONG STR 32P. NO CRACK OR DISBOND BOUND.
- [SDR ERAA20120100](https://openairdocs.org/sdr/ERAA20120100.md): Attach Angle · cracked · Nov 15, 2012 · N882EA · Dhav DHC8103 · Wing Miscellaneous Structure
  > DURING INSPECTION OUTBOARD CLOSING ANGLES FOUND TO BE CRACKED. 34848 CYC SINCE INSTALLATION OF ANGLES. ONE CRACK ON EACH ANGLE ONE P/N 8530016-015 2.5 INCHES AND P/N 8530016-113 1.0 INCHES.
- [SDR ERAA20120099](https://openairdocs.org/sdr/ERAA20120099.md): Skin Panel · cracked · Nov 14, 2012 · N882EA · Dhav DHC8103 · Wing, Plate/Skin
  > CRACK AT RIGHT WING LADDER PLATE AT YW42.0 AND STR 4.
- [SDR ERAA20120076](https://openairdocs.org/sdr/ERAA20120076.md): Circuit Breaker · defective · Oct 4, 2012 · N882EA · Dhav DHC8103 · Hydraulic Pressure Indicator
  > NR 1 STANDBY HYDRAULIC GAUGE INDICATES PRESSURE WITH SWITCH SELECTED TO "NORMAL" (OFF) POSITION. INSTALLED SERVICEABLE A/C PUMP C/B IN RIGHT WHEEL A/C CONTACTOR BOX IAW DASH 8 MAINT MANUAL 24-21-09 AND OPS CHECKS OK IAW DASH 8 MAINT MANUAL 29-11-17, OPS CHECK
- [SDR ERAA20120059](https://openairdocs.org/sdr/ERAA20120059.md): Generator · defective · Sep 7, 2012 · N882EA · Dhav DHC8103 · AC Generator-Alternator
  > NR 1 AC GEN CAUTION LIGHT - NO LOAD LEFT SIDE. REMOVED AND REPLACED NR 1 AC GENERATOR IAW PSM 1-8-10, RUN UP CHECK GOOD. NO LEAKS FOUND, OK FOR SERVICE.
- [SDR ERAA20120038](https://openairdocs.org/sdr/ERAA20120038.md): Target · missing · Apr 19, 2012 · N882EA · Dhav DHC8103 · Landing Gear Position and Warning
  > "WT ON WHEELS" CAUTION LIGHT ILLUMINATED. INSTRUCTED BY OPS AND MAINTENANCE TO RETURN TO ANC. FOUND FAULT ON RIGHT NLG PROX SWITCH AND TARGET MISSING FROM LOWER GEAR KNEE. REPLACED TARGET ON RIGHT SIDE OF LOWER GEAR KNEE IAW MESSIER DOWTY CMM 32-20-01 CLEAR
- [SDR ERAA201200009](https://openairdocs.org/sdr/ERAA201200009.md): Drive Shaft · corroded · Feb 4, 2012 · N882EA · Dhav DHC8103 · Aileron Control System
  > ROLL CONTROL VERY STIFF. TENSIONED AILERON FUSELAGE CABLES AND LUBRICATED AILERION QUADRANT BEARINGS EXTERNALLY FOR TROUBLESHOOTING. OPERATIONAL CHECK FLIGHT-ROLL CONTROL CHECKS GOOD. 4 FEB 2012 REPLACE LT AND RT BEARINGS IN AILERON QUADRANT. REPLACED BEAR
- [SDR ERAA201200004](https://openairdocs.org/sdr/ERAA201200004.md): Battery Pack · weak · Jan 23, 2012 · N882EA · Dhav DHC8103 · Emergency Lighting
  > OVERHEAD AISLE EMERGENCY EXIT LIGHTS MID-CABIN WEAK. REMOVED AND REPLACED EMERGENCY BATTERY PACK IN AFT RIGHT POSITION IAW DHC-8 MAINTENANCE MANUAL 33-51-00. EMERGENCY LIGHTS OPS CHECK GOOD.
- [SDR ERAA201200001](https://openairdocs.org/sdr/ERAA201200001.md): Control Quadrant · dirty · Jan 7, 2012 · N882EA · Dhav DHC8103 · Aileron Control System
  > RETURNED TO ANC DUE TO VERY STIFF CONTROL YOKE MOVEMENT TO THE LEFT, OK UNTIL ABOUT 20 DEGREES PAST CENTER, ALSO SEEMS NORMAL ON GROUND, AIRSPEED OR CONFIGURATION DID NOT SEEM TO EFFECT IT. CLEANED AND LUBED L&R AILERON TERMINAL QUADRANTS, CHECKED RIG OF AILE
- [SDR ERAA201100011](https://openairdocs.org/sdr/ERAA201100011.md): Drag Brace · defective · Dec 24, 2011 · N882EA · Dhav DHC8103 · Landing Gear Retraction/Extension System
  > UNABLE TO EXTEND NOSE GEAR, MANUAL GEAR EXTEND COMPLETED UPON RETURN TO ANC. REMOVED AND REPLACED NLG DRAG BRACE IAW DASH 8 MAINTENANCE MANUAL 32-30-36 AND C/W GEAR SWING IAW DASH 8 MAINTENANCE MANUAL 32-30-00, OPS CHECKS OK.
- [SDR ERAA2012F00003](https://openairdocs.org/sdr/ERAA2012F00003.md): Selector · intermittent · Oct 26, 2011 · N882EA · Dhav DHC8103 · Landing Gear Selector
  > LANDING GEAR HANDLE AND RED NOSE GEAR LIGHT FLASHED 3 SEPARATE TIMES MIDFLIGHT AND NOSEGEAR WAS FELT HITTING GEAR DOORS ON 2 OF THESE OCCASIONS. REMOVED LANDING GEAR SELECTOR AND INSTALLED WITH REPAIRED UNIT IAW MM 32-30-05. OPS CHECKED NORMAL. OK FOR SERVI
- [SDR ERAA201100001](https://openairdocs.org/sdr/ERAA201100001.md): Actuator · fractured · Jan 4, 2011 · N882EA · Dhav DHC8103 · Drag Control Actuator
  > ON LANDING PILOT REPORTED TWO CAUTION LIGHTS, NR 1 HYD ISO VLV AND ROLL SPLR INBD HYD AND LOSS OF BRAKING. MAINTENANCE FOUND RIGHT, INBOARD ROLL SPOILER ACTUATOR HOUSING FRACTURED AROUND END CAP LEADING TO LOSS OF NR 1 HYDRAULIC SYSTEM FLUID. TOTAL TIME AND C
- [SDR V0XR201011020002](https://openairdocs.org/sdr/V0XR201011020002.md): Strut · corroded · Nov 2, 2010 · N882EA · Dhav DHC8103 · Fuselage Miscellaneous Structure
  > (V0XR) STRUT AT STR 31P, STA 531.5 IS CORRODED. R & R STRUT.
- [SDR V0XR201011020001](https://openairdocs.org/sdr/V0XR201011020001.md): Frame · corroded · Nov 2, 2010 · N882EA · Dhav DHC8103 · Fuselage Main, Frame
  > (V0XR) RT SIDE FRAME AT STA 510 IS CORRODED. R & R SPLICE IAW RD8-53-11498.
- [SDR V0XR201010290007](https://openairdocs.org/sdr/V0XR201010290007.md): Fitting · corroded · Oct 29, 2010 · N882EA · Dhav DHC8103 · Fuselage Main, Attach Fittings
  > (V0XR) JOINT FITTING AFT KEEL AT LT FRAME STN 531.5. R & R FITTING.
- [SDR V0XR201010290006](https://openairdocs.org/sdr/V0XR201010290006.md): Stringer · corroded · Oct 29, 2010 · N882EA · Dhav DHC8103 · Fuselage Main, Longeron/Stringer
  > (V0XR) CORROSION ON STRINGER AT STN 525.0 AT STR 32L. R & R STRINGER.

Next page: https://openairdocs.org/deregistered/N882EA-2013-11-20/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 = 'N882EA' AND deregistration_id = 'N882EA-2013-11-20'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N882EA-2013-11-20/reports

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