# Service difficulty reports: N881EA, cancelled Nov 15, 2012

A list on [N881EA, cancelled Nov 15, 2012](https://openairdocs.org/deregistered/N881EA-2012-11-15.md).

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

- [SDR ERAA20120062](https://openairdocs.org/sdr/ERAA20120062.md): Light · inoperative · Sep 11, 2012 · N881EA · Dhav DHC8106 · Emergency Lighting
  > ROW 1D UPPER EMERGENCY SIGN INOP. REMOVED AND REPLACED BAD LAMPS, OPS CHECK GOOD. OK FOR SERVICE AT THIS TIME.
- [SDR ERAA20120057](https://openairdocs.org/sdr/ERAA20120057.md): Warning System · false activation · Sep 3, 2012 · N881EA · Dhav DHC8106 · Landing Gear Position and Warning
  > GEAR FAILED TO RETRACT PROPERLY - BOTH MAIN "AMBER" ADVISORY LIGHTS ON, RED NOSEWHEEL LIGHT ILLUMINATED. JACKED AIRCRAFT AND PERFORMED OPERATIONAL CHECK OF THE RETRACTION AND EXTENSION SYSTEM IAW PSM 1-8-2 CH32-30-00, OPS CHECKED GOOD.
- [SDR ERAA20120049](https://openairdocs.org/sdr/ERAA20120049.md): Pressure Switch · faulty · Jun 27, 2012 · N881EA · Dhav DHC8106 · Rudder Control System
  > DEPARTURE IN ANC 07:45 NR 2 RUDDER HYDRAULIC LIGHT ILLUMINATED. REMOVED AND REPLACED NR 2 RUDDER LOW PRESSURE SWITCH AT RUDDER DAMPER ASSEMBLY AND OPS AND LEAK CHECKED GOOD ON GROUND IAW PSM 1-8-2 CH 27-20-00.
- [SDR ERAA20120042](https://openairdocs.org/sdr/ERAA20120042.md): Battery Pack · discharged · May 14, 2012 · N881EA · Dhav DHC8106 · Emergency Lighting
  > EMERGENCY LIGHT FOUND INOP ON PREFLIGHT. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACKS IAW DHC MM 33-52-00, OPS CHECK GOOD.
- [SDR ERAA20120033](https://openairdocs.org/sdr/ERAA20120033.md): Smoke Detector · no test · Mar 10, 2012 · N881EA · Dhav DHC8106 · Smoke Detection
  > NR 2 BAG SMOKE WARNING TEST FAILED. REMOVED AND REPLACED NR 2 AFT BAGGAGE SMOKE DETECTOR. OPS CHECK GOOD.
- [SDR ERAA201202160029](https://openairdocs.org/sdr/ERAA201202160029.md): Skin · cracked · Feb 16, 2012 · N881EA · Dhav DHC8106 · Wing, Plate/Skin
  > LT WING LIGHTNING STRIPS HAVE TWO CRACKS AT STA 178. REPLACED STRIPS.
- [SDR ERAA201202160028](https://openairdocs.org/sdr/ERAA201202160028.md): Skin · cracked · Feb 16, 2012 · N881EA · Dhav DHC8106 · Wing, Plate/Skin
  > RT WING LIGHTNING STRIP HAVE FOUR CRACKS BETWEEN STA YW 139.00 & YW 250.00. REPLACE STRIPS.
- [SDR ERAA201200027](https://openairdocs.org/sdr/ERAA201200027.md): Skin · cracked · Feb 14, 2012 · N881EA · Dhav DHC8106 · Nacelle/Pylon, Plate/Skin
  > LT NACELLE OUTBD NACELLE SKIN CRACKED AT STA ZN 0-00 AND ZN 130.00. REPLACED SKIN.
- [SDR ERAA201200026](https://openairdocs.org/sdr/ERAA201200026.md): Firewall · cracked · Feb 11, 2012 · N881EA · Dhav DHC8106 · Nacelle/Pylon, Bulkhead/Firewall
  > REPAIRED CRACK IN LT ENGINE NACELLE FIREWALL OUTBD SKIN IAW RD8-54-0651 PERMANENT REPAIR.
- [SDR ERAA201200025](https://openairdocs.org/sdr/ERAA201200025.md): Fastener · loose · Feb 11, 2012 · N881EA · Dhav DHC8106 · Empennage Structure
  > REPLACED 8 LOOSE FASTENERS WITH JOBOLTS IAW RD8-55-032.
- [SDR ERAA201200024](https://openairdocs.org/sdr/ERAA201200024.md): Stringer · corroded · Feb 11, 2012 · N881EA · Dhav DHC8106 · Fuselage Main, Longeron/Stringer
  > REPLACED SECTION OF CORRODED STRINGER 32R STA 281 IAW SRM 53-10-21.
- [SDR ERAA201200023](https://openairdocs.org/sdr/ERAA201200023.md): Flap Track · corroded · Feb 9, 2012 · N881EA · Dhav DHC8106 · Trailing Edge Flaps
  > REMOVED LIGHT SURFACE CORROSION ON LT NR 4 FLAP TRACK IAW RD8-57-988.
- [SDR ERAA201200022](https://openairdocs.org/sdr/ERAA201200022.md): Stringer · corroded · Feb 9, 2012 · N881EA · Dhav DHC8106 · Fuselage Main, Longeron/Stringer
  > REPAIRED CORROSION ON FUSELAGE STRINGER 31S AT X436 IAW RD8-53-3044.
- [SDR ERAA201200020](https://openairdocs.org/sdr/ERAA201200020.md): Skin Panel · corroded · Feb 8, 2012 · N881EA · Dhav DHC8106 · Fuselage Main, Plate/Skin
  > REPAIRED SKIN PANEL CORROSION ON WAFFLE DOUBLER OF SKIN PANEL STA X275 BETWEEN STR 32P - 32S BY BLENDING IAW RD8-53-12242.
- [SDR ERAA201200019](https://openairdocs.org/sdr/ERAA201200019.md): Skin Panel · corroded · Feb 8, 2012 · N881EA · Dhav DHC8106 · Fuselage Main, Plate/Skin
  > REPAIRED SKIN PANEL CORROSION AT STA X429 BETWEEN STRINGER 32P & 31S, CUT AWAY SKIN IAW RD8-53-12243 ISSUE 2 AND INSTALLED EXTERNAL DOUBLER.
- [SDR ERAA201200018](https://openairdocs.org/sdr/ERAA201200018.md): Skin Panel · corroded · Feb 8, 2012 · N881EA · Dhav DHC8106 · Fuselage Main, Plate/Skin
  > REPAIRED SKIN PANEL CORROSION AND DISBONDED DOUBLER STA X167 AT STRINGER 33, CUT AWAY SKIN IAW RD8-53-12241 AND INSTALLED EXTERNAL DOUBLER.
- [SDR ERAA201200017](https://openairdocs.org/sdr/ERAA201200017.md): Pin · corroded · Feb 8, 2012 · N881EA · Dhav DHC8106 · Main Landing Gear Attach Section
  > RIGHT MLG DRAG STRUT TO SHOCKSTRUT ATTACH PIN REPLACED DUE TO PITTING.
- [SDR ERAA201200016](https://openairdocs.org/sdr/ERAA201200016.md): Skin · corroded · Feb 8, 2012 · N881EA · Dhav DHC8106 · Fuselage Main, Plate/Skin
  > CORROSION AND SKIN DISBOND AT LOWER FUSELAGE STA X506.
- [SDR ERAA201200015](https://openairdocs.org/sdr/ERAA201200015.md): Attach Bolt · cracked · Feb 8, 2012 · N881EA · Dhav DHC8106 · Fuselage, Wing Attach Fittings
  > LEFT FUSELAGE TO WING ATTACH BOLT HEAD CRACKED.
- [SDR ERAA201200014](https://openairdocs.org/sdr/ERAA201200014.md): Stiffener · corroded · Feb 8, 2012 · N881EA · Dhav DHC8106 · Fuselage Miscellaneous Structure
  > CORROSION DAMAGE ON STIFFENER AT WEB STA 387.5. REPLACED STIFFENER.
- [SDR ERAA201200013](https://openairdocs.org/sdr/ERAA201200013.md): Rib · cracked · Feb 8, 2012 · N881EA · Dhav DHC8106 · Nacelle/Pylon, Frame/Spar/Rib
  > CRACKED RIB ON RT NACELLE FIREWALL ON INBD SIDE.
- [SDR ERAA201200012](https://openairdocs.org/sdr/ERAA201200012.md): Doubler · cracked · Feb 8, 2012 · N881EA · Dhav DHC8106 · Nacelle/Pylon, Bulkhead/Firewall
  > CRACKED DOUBLER ON LT NACELLE FIREWALL ON INBD SIDE.
- [SDR ERAA201200011](https://openairdocs.org/sdr/ERAA201200011.md): Stringer · cracked · Feb 8, 2012 · N881EA · Dhav DHC8106 · Nacelle/Pylon, Longeron/Stringer
  > TWO CRACKS ON LT NACELLE SKIN STRINGERS UNDER EXHAUST FINGERNAIL.
- [SDR ERAA201200010](https://openairdocs.org/sdr/ERAA201200010.md): Stringer · corroded · Feb 8, 2012 · N881EA · Dhav DHC8106 · Fuselage Main, Longeron/Stringer
  > CORROSION ON STRINGER 31R, STA 156 - 159.
- [SDR ERAA2012F00051](https://openairdocs.org/sdr/ERAA2012F00051.md): Stringer · corroded · Feb 8, 2012 · N881EA · Dhav DHC8106 · Fuselage Main, Longeron/Stringer
  > CORROSION ON STRINGER 31R, STA 156 - 159.
- [SDR ERAA201100004](https://openairdocs.org/sdr/ERAA201100004.md): Skin · dented · Apr 3, 2011 · N881EA · Dhav DHC8106 · Fuselage Main, Plate/Skin
  > LOWER FUSELAGE SKIN DENT BEYOND AIRWORTHY LIMITS, STA X290.5 ABOVE STR 26P APPROXIMATELY 0.3 INCH ABOVE EDGE OF BONDED WAFFLE. OBTAINED RD FROM MANUFACTURERS ENGINEERING DEPARTMENT FOR REPAIR DESIGN.
- [SDR ERAA201000005](https://openairdocs.org/sdr/ERAA201000005.md): Smoke Detector · intermittent · Oct 3, 2010 · N881EA · Dhav DHC8106 · Smoke Detection
  > SMOKE WARNING LIGHT CAME ON INTERMITTENTLY IN FLIGHT. (NO EVIDENCE OF SMOKE OR FIRE IN AFT CARGO COMPARTMENT.) REPLACED SMOKE DETECTOR IAW MM CHAPTER 26-12-01, OPS CK SATISFACTORY.
- [SDR V0XR201004280003](https://openairdocs.org/sdr/V0XR201004280003.md): Skin · dented · Apr 28, 2010 · N881EA · Dhav DHC8106 · Fuselage Main, Plate/Skin
  > (V0XR) DENT ON RT FUSELAGE AT 1.5 INCHES FWD OF STA X312.35 BETWEEN STR 7R AND 8R IS BEYOND LIMITS. REPAIRED DENT ON RT FUSELAGE. W/C 2182.
- [SDR V0XR201004280002](https://openairdocs.org/sdr/V0XR201004280002.md): Skin · cracked · Apr 28, 2010 · N881EA · Dhav DHC8106 · Wing, Plate/Skin
  > (V0XR) CRACK ON LT WING UPPER SKIN LADDER PLATE OTBD OF AFT CORNER UNDER PANEL 522AT AT WS YW 137.0. REPAIRED WING UPPER SKIN LADDER PLATE. W/C 5073.
- [SDR V0XR201004280001](https://openairdocs.org/sdr/V0XR201004280001.md): Shear Web · corroded · Apr 28, 2010 · N881EA · Dhav DHC8106 · Fuselage Miscellaneous Structure
  > (V0XR) LT REAR BAGGAGE FLOOR INBD OF AFT DOOR SILL IS CORRODED BEYOND LIMITS. REMOVED AND REPAIRED BAGGAGE COMPARTMENT FLOOR, SHEAR WEB. W/C 1082.
- [SDR V0XR201004260003](https://openairdocs.org/sdr/V0XR201004260003.md): Seat Track · corroded · Apr 26, 2010 · N881EA · Dhav DHC8106 · Fuselage, Seat/Cargo Attach Fittings
  > (V0XR) RT UPPER SEAT TRACK FR 46-52 CORRODED BEYOND LIMITS. R & R SEAT TRACK. W/C 1098.
- [SDR V0XR201004260002](https://openairdocs.org/sdr/V0XR201004260002.md): Seat Track · corroded · Apr 26, 2010 · N881EA · Dhav DHC8106 · Fuselage, Seat/Cargo Attach Fittings
  > (V0XR) LT SEAT TRACK DRIP RAIL CORRODED BEYOND LIMITS. R & R SEAT TRACK. W/C 2225.
- [SDR V0XR201004260001](https://openairdocs.org/sdr/V0XR201004260001.md): Seat Track · corroded · Apr 26, 2010 · N881EA · Dhav DHC8106 · Fuselage, Seat/Cargo Attach Fittings
  > (V0XR) RT SEAT TRACK RAIL FR 182.0 TO 424.12 CORRODED BEYOND LIMITS. R & R SEAT TRACK. W/C 1087.
- [SDR V0XR201004160002A](https://openairdocs.org/sdr/V0XR201004160002A.md): Gusset · corroded · Apr 16, 2010 · N881EA · Dhav DHC8106 · Fuselage Main, Structure
  > CTR GUSSET FR 59-61 IS CORRODED BEYOND LIMITS. R & R CTR GUSSET. W/C 1154. (V0XR)
- [SDR V0XR201004160001](https://openairdocs.org/sdr/V0XR201004160001.md): Seat Track · corroded · Apr 16, 2010 · N881EA · Dhav DHC8106 · Fuselage, Seat/Cargo Attach Fittings
  > LT SEAT TRACK FR 182-484 IS CORRODED BEYOND LIMITS. R &R LT SEAT TRACK.
- [SDR ERAA200900004](https://openairdocs.org/sdr/ERAA200900004.md): Controller · unreliable · Aug 5, 2009 · N881EA · Dhav DHC8106 · Cabin Pressure Controller
  > AIRCRAFT DEPRESSURIZED AT FL 230 AND EMERGENCY DESCENT WAS PERFORMED, AT 12,000 FEET PRESSURIZATION RETURNED TO NORMAL.
- [SDR ERAA200900003](https://openairdocs.org/sdr/ERAA200900003.md): Nut · loose · Jun 24, 2009 · N881EA · Dhav DHC8106 · Passenger/Crew Doors
  > WHILE ATTEMPTING TO DEPLANE PASSENGERS, FOUND THE MAIN CABIN DOOR STUCK CLOSED. PASSENGERS DEPLANED VIA ALTERNATE EXIT. FOUND JAM NUT ON UPPER END OF OVER CENTER GAS SPRING LOOSE (IPC 52-10-00 FIG 60, ITEM 90, PN D1N439M10X1, NUT AND ITEM 120, PN 8SC0156, GAS
- [SDR ERA2005F00009](https://openairdocs.org/sdr/ERA2005F00009.md): Plate · corroded · Nov 8, 2005 · N881EA · Dhav DHC8103 · Fuselage, Landing Gear Attach Fittings
  > FOUND WHILE AIRCRAFT UNDERGOING C1-CHECK, AWC 19810. CORROSION ON LT NLG TRUNNION PLATE BEYOND MFG LIMITS. REPLACED LT NLG TRUNNION PLATE IAW DWG. (K)
- [SDR ERA2005F00000](https://openairdocs.org/sdr/ERA2005F00000.md): Seat Track · corroded · Nov 1, 2005 · N881EA · Dhav DHC8103 · Fuselage, Seat/Cargo Attach Fittings
  > FOUND WHILE AIRCRAFT WAS UNDERGOING C1 CHECK, AWC 19412, FOUND LT FWD SEAT RAIL CORROSION BEYOND MFG LIMITS. REPAIRED IAW RO. (K)
- [SDR ERA2005F00001](https://openairdocs.org/sdr/ERA2005F00001.md): Skin · gouged · Oct 26, 2005 · N881EA · Dhav DHC8103 · Fuselage Main, Plate/Skin
  > FOUND WHILE AIRCRAFT UNDERGOING C1 CHECK, AWC 19438, FOUND GOUGE IN RT TOP SKIN AT STRINGER 3R BETWEEN FRAME YW207, STA YW137. REPAIRED IAW RO. (K)
- [SDR ERA2005F00002](https://openairdocs.org/sdr/ERA2005F00002.md): Skin · dented · Oct 25, 2005 · N881EA · Dhav DHC8103 · Fuselage Main, Plate/Skin
  > FOUND WHILE AIRCRAFT UNDERGOING C1 CHECK, AWC 19388. FOUND DENT UNDER RT ICE SHIELD BETWEEN FUSELAGE STRINGER 14S AND 15S AT STATION X323.1. REPAIRED IAW MFG RD.
- [SDR ERA2005F00003](https://openairdocs.org/sdr/ERA2005F00003.md): Plate · cracked · Oct 24, 2005 · N881EA · Dhav DHC8103 · Wing, Plate/Skin
  > FOUND WHILE AIRCRAFT UNDERGOING C1-CHECK, AWC 19419. FOUND CRACK IN RT IB LADDER PLATE BETWEEN STRINGER 4 AND 6 AT WING STA YW137. REPAIRED IAW RD. (K)
- [SDR ERAA200000001](https://openairdocs.org/sdr/ERAA200000001.md): Indicator · burned out · Nov 28, 2000 · N881EA · Dhav DHC8103 · Landing Gear Position and Warning
  > RIGHT MAIN GEAR GREEN (DOWN/LOCKED) LIGHT DID NOT COME ON UPON EXTENSION. ALTERNATE EXTENSION LIGHTS (3 GREEN) APPEARED NORMAL. VISUAL INSPECTION ALSO APPEARED NORMAL. MADE UNEVENTFUL LANDING. RELAMPED R/H MAIN LANDING GEAR DOWN/LOCKED LIGHT. OPERATIONAL CHECK
- [SDR 20000816AP011](https://openairdocs.org/sdr/20000816AP011.md): Switch · stuck · Jun 2, 2000 · N881EA · Dhav DHC8103 · Propeller Feathering/Reversing
  > AFTER TAKEOFF AUTOFEATHER SELECT SWITCH WILL NOT TURN OFF. RETURNED AND MADE UNEVENTFUL LANDING ANC. REPLACED AUTOFEATHER SELECT SWITCH, GROUND TEST GOOD. (M)
- [SDR 99ZZZM667](https://openairdocs.org/sdr/99ZZZM667.md): Packing · cut · Aug 31, 1999 · N881EA · Dhav DHC8103 · Engine Oil Cooler
  > OIL PRESS CAUTION LIGHT FLICKERED DURING CLIMB-OUT FROM CDV. NR 2 ENGINE OIL PRESS DROPPED TO ZERO IN CRUISE. SHUTDOWN NR 2 ENGINE AND MADE UNEVENTFUL LANDING AT ANC. OIL LEAK AT NR 2 ENGINE OIL COOLER INLET DUE TO CUT O-RING. ENGINE REPLACED DUE TO OIL ST
- [SDR 98ZZZM596](https://openairdocs.org/sdr/98ZZZM596.md): Smoke Detector · contaminated · Jul 1, 1998 · N881EA · Dhav DHC8103 · Smoke Detection
  > CARGO COMPARTMENT SMOKE DETECTOR WARNING AFTER TAKEOFF, FOR APPROX 3 MINUTES. MADE UNEVENTFUL PRECAUTIONARY LANDING AT ENG. CAUTION LIGHT WENT OUT PRIOR TO LANDING. CLEANED SMOKE DETECTOR ELECTRICAL CONNECTORS AND REPLACED FWD SMOKE DETECTOR. GROUND OPERAT
- [SDR 98ZZZX2420](https://openairdocs.org/sdr/98ZZZX2420.md): Pcu · inoperatiave · Jun 12, 1998 · N881EA · Dhav DHC8103 · Propeller Controlling System
  > NR 2 ENGINE PROPELLER RPM FLUCTUATING BETWEEN 1032 AND 1088. UNABLE TO CONTROL PROP RPM. SHUT DOWN ENGINE AND MADE UNEVENTFUL LANDING AT ANC. REPLACED NR 2 PCU, GROUND CHECKS GOOD.
- [SDR ERA96002](https://openairdocs.org/sdr/ERA96002.md): Spur Gear · failed · Jul 8, 1996 · N881EA · Dhav DHC8103 · Turbine Engine Accessory Drive
  > ENGINE NR 2 FLAME-OUT IN CRUISE AT 20,000 FT. SECURED ENGINE AND DIVERTED TO HOM. ENGINE NR 2 FUEL PUMP DRIVE SPUR GEAR FAILURE RESULTING IN LOSE OF FUEL AND OIL PRESSURE. POST-MOD SB 20195, ACCESSORY DRIVE SPUR GEAR REPLACEMENT, POST-MOD SB 21178, AGB BEAR

## 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 = 'N881EA' AND deregistration_id = 'N881EA-2012-11-15'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N881EA-2012-11-15/reports

---
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