# Service difficulty reports: N8926E, cancelled Nov 23, 2010

A list on [N8926E, cancelled Nov 23, 2010](https://openairdocs.org/deregistered/N8926E-2010-11-23.md).

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

- [SDR NWAA093359946](https://openairdocs.org/sdr/NWAA093359946.md): Web · buckled · Sep 24, 2009 · N8926E · Doug DC931 · Nacelle/Pylon Miscellaneous Structure
  > DURING ENGINE CHANGE FOUND PYLON VERTICAL WEB BUCKLED BETWEEN UPPER AND LOWER SPARS FOR AFT ENGINE MOUNT AT XN39.250. REPAIRED PER EA 99-216590.
- [SDR NWAA074359946](https://openairdocs.org/sdr/NWAA074359946.md): Skin · cracked · Dec 21, 2007 · N8926E · Doug DC931 · Fuselage Main, Plate/Skin
  > DURING "H" CHECK, FOUND CRACKS IN SKIN AT FORWARD PASSENGER ENTRY DOOR CUTOUT AT AFT DOOR STOPS NR 3 AND NR 4. REPAIRED PER EA 99-211049.
- [SDR NWAA072859946](https://openairdocs.org/sdr/NWAA072859946.md): Battery Pack · inoperative · Aug 16, 2007 · N8926E · Doug DC931 · Emergency Lighting
  > TAIL CONE PATH LIGHTS INOP. REPLACED BATTERY PACK. OPERATION CHECKS GOOD.
- [SDR NWAA072809946](https://openairdocs.org/sdr/NWAA072809946.md): Power Supply · inoperative · Aug 8, 2007 · N8926E · Doug DC931 · Emergency Lighting
  > TAIL COMPARTMENT EMERGENCY ESCAPE PATH LIGHTING INOP. REPLACED POWER SUPPLY.
- [SDR NWAA072799946](https://openairdocs.org/sdr/NWAA072799946.md): Battery Pack · inoperative · Jul 26, 2007 · N8926E · Doug DC931 · Emergency Lighting
  > AFT EMERGENCY CAT-WALK LIGHT OUT DURING EMERGENCY LIGHT CHECK. REPLACED BATTERY PACK.
- [SDR 0300749946](https://openairdocs.org/sdr/0300749946.md): Line · leaking · Apr 7, 2003 · N8926E · Doug DC931 · Hydraulic System, Main
  > ON CLIMB SHORTLY AFTER GEAR RETRACTION THE RIGHT HYDRAULIC PRESSURE BEGAN FLUCTUATING BY FLUID LOSS. THE THE LEFT HYDRAULIC SYSTEM LOST PRESSURE AND LOST FLUID. THE LANDING GEAR WAS LOWERED BY ALTERNATE METHOD. FLIGHT DIVERTED TO IND AND LANDED SAFELY. MAI
- [SDR 0200159946](https://openairdocs.org/sdr/0200159946.md): Web · cracked · Jan 14, 2002 · N8926E · Doug DC931 · Fuselage Main, Structure
  > During Hck in ATL, A crack was found in the lower outboard corner of the diagonal web in the L/H engine pylon just forward of the rear spar. Repaired per EA 99-185474.
- [SDR 0200139946](https://openairdocs.org/sdr/0200139946.md): Floorbeam · cracked · Jan 9, 2002 · N8926E · Doug DC931 · Fuselage Main, Floor Beam
  > DURING HCK IN ATL, A CRACK WAS FOUND IN THE UPPER VERTICLE FLANGE OF THE STATION 237 FLOORBEAM AT X=6. REPAIRED PER EA 99-185447.
- [SDR 0200149946](https://openairdocs.org/sdr/0200149946.md): Skin · corroded · Jan 8, 2002 · N8926E · Doug DC931 · Wing Miscellaneous Structure
  > During HCK in ATL, corrosion was found on the R/H wing upper skin doubler flange attachment holes for the fuel access door. Repaired per EA 99-185451.
- [SDR 9809329946](https://openairdocs.org/sdr/9809329946.md): Wire · broken · May 17, 1998 · N8926E · Doug DC931 · Light System Wiring
  > DURING LINE MAINTENANCE INSPECTION, FOUND EMERGENCY LIGHTS ON CATWALK ILLUMINATED WITH SWITCH IN OFF POSITION. REPAIRED BROKEN WIRING TO SPLICE NEAR TAILCONE BATTERY PACK. OPERATIONAL CHECK NORMAL.
- [SDR 9800229946](https://openairdocs.org/sdr/9800229946.md): Battery Charger · failed · Jan 5, 1998 · N8926E · Doug DC931 · Battery/Charger System
  > BATTERY CHARGER ANNUNCIATOR LIGHT ILLUMINATED AFTER TAKEOFF. FLIGHT WAS RETURNED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED BATTERY CHARGER AND MAIN BATTERY, OPERATIONAL CHECK NORMAL.
- [SDR 9720339946](https://openairdocs.org/sdr/9720339946.md): Bulkhead · corroded · Oct 11, 1997 · N8926E · Doug DC931 · Fuselage Main, Bulkhead
  > DURING LINE CHECK, FOUND CORROSION ON AFT PRESSURE BULKHEAD AT RADIAL NR 9 APPROXIMATELY 12 INCHES FROM OUTBOARD END. REPAIRED PER EA 99-152220.
- [SDR 9716369946](https://openairdocs.org/sdr/9716369946.md): Battery · discharged · Sep 1, 1997 · N8926E · Doug DC931 · Emergency Lighting
  > DURING PERIODIC CHECK, FORWARD SERVICE DOOR EVACUATION SLIDE FAILED BATTERY TEST. REPLACED SLIDE.
- [SDR 9707809946](https://openairdocs.org/sdr/9707809946.md): Downlock Switch · malfunctioned · Apr 17, 1997 · N8926E · Doug DC931 · Landing Gear Position and Warning
  > DURING APPROACH INTO MEM, THE RIGHT MAIN LANDING GEAR GREEN LIGHT DID NOT ILLUMINATE AFTER GEAR EXTENSION. RECYCLED GEAR AND NORMAL INDICATIONS WERE ACHIEVED. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED RIGHT MAIN GEAR DOWNLOCK SWITCH. OPERATION
- [SDR 9702769946](https://openairdocs.org/sdr/9702769946.md): Downlock Switch · failed · Feb 7, 1997 · N8926E · Doug DC931 · Landing Gear Position and Warning
  > DURING APPROACH, THE RIGHT MAIN LANDING GEAR GREEN LIGHT FAILED TO ILLUMINATE AFTER GEAR EXTENSION. RECYCLED GEAR AND NORMAL INDICATIONS WERE ACHIEVED. MAINTENANCE WAS UNABLE TO DUPLICATE PROBLEM ON GROUND. REPLACED THE RIGHT MAIN GEAR DOWNLOCK SWITCH AS A
- [SDR 9622509946](https://openairdocs.org/sdr/9622509946.md): Wire · broken · Oct 16, 1996 · N8926E · Doug DC931 · Light System Wiring
  > DURING LINE MAINTENANCE INSPECTION, FOUND FLOOR PROXIMITY EMERGENCY LIGHTS AT ROW 13 INOPERATIVE. MAINTENANCE FOUND BROKEN WIRE ON CONNECTOR UNDER SEAT. REPAIRED BROKEN WIRE, OPERATIONAL CHECK NORMAL.
- [SDR 9620589946](https://openairdocs.org/sdr/9620589946.md): Lights · loose · Sep 25, 1996 · N8926E · Doug DC931 · Emergency Lighting
  > DURING LINE MAINTENANCE INSPECTION, FOUND TAILCONE EMERGENCY LIGHT AND POWER SUPPLY LOOSE FROM BRACKET. REPLACED POWER SUPPLY AND BATTERIES, OPERATIONAL CHECK NORMAL.
- [SDR 9619499946](https://openairdocs.org/sdr/9619499946.md): Air Cycle Mach · overserviced · Sep 7, 1996 · N8926E · Doug DC931 · Cabin Cooling System
  > FLIGHT ATTENDANT REPORTED HAZE AND SMOKE IN CABIN AFTER TAKEOFF. FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND RIGHT AIR CYCLE MACHINE OVERSERVICED. DRAINED OIL TO PROPER LEVEL. ALSO CHANGED COALESCER BAGS. OPERATIONAL CHECK NORMAL
- [SDR 9616589946](https://openairdocs.org/sdr/9616589946.md): Battery Pack · malfunctioned · Jul 30, 1996 · N8926E · Doug DC931 · Emergency Lighting
  > DURING LINE MAINTENANCE INSPECTION, FOUND AFT OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED BATTERY PACK, OPERATIONAL CHECK NORMAL.
- [SDR 9608659946](https://openairdocs.org/sdr/9608659946.md): Power Supply · inoperative · Apr 15, 1996 · N8926E · Doug DC931 · Emergency Lighting
  > DURING LINE MAINTENANCE INSPECTION, FOUND TAIL COMPARTMENT EMERGENCY LIGHT POWER SUPPLY BROKEN. REPLACED POWER SUPPLY AND OPERATIONAL CHECK NORMAL.
- [SDR 9518499946](https://openairdocs.org/sdr/9518499946.md): Transducer · failed · Nov 17, 1995 · N8926E · Doug DC931 · Stall Warning System
  > DURING CLIMB, THE STALL WARNING SYSTEM ACTIVATED AND THE RED STALL LIGHT ILLUMINATED. FOLLOWED COCKPIT OPERATING MANUAL PROCEDURE AND SYSTEM MALFUNCTION CONTINUED. PULLED CIRCUIT BREAKER TO DEACTIVATE SYSTEM. FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDE
- [SDR 9519199946](https://openairdocs.org/sdr/9519199946.md): Seat Track · corroded · Nov 9, 1995 · N8926E · Doug DC931 · Fuselage, Seat/Cargo Attach Fittings
  > DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE RBL 44 SEAT TRACK AT FS 284. REPAIRED TRACK (P/N 2772660), PER EA 99-103090.
- [SDR 9519159946](https://openairdocs.org/sdr/9519159946.md): Skin · corroded · Nov 6, 1995 · N8926E · Doug DC931 · Fuselage Main, Plate/Skin
  > DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE FUSELAGE SKIN FS 94 TO 110 AT LONGERON 24L AND ON THE T-CAP, FS 110 BETWEEN LONGERONS 24L TO 27R. REPAIRED SKIN (P/N 991911509-85) AND T-CAP (P/N 5911400) PER EA 99-102691.
- [SDR 9519149946](https://openairdocs.org/sdr/9519149946.md): Longeron · corroded · Nov 6, 1995 · N8926E · Doug DC931 · Fuselage Main, Longeron/Stringer
  > DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON LONGERON 19L BETWEEN FS 541 TO 579. REPAIRED LONGERON (P/N 5920354-1), PER EA 99-103115.
- [SDR 9519139946](https://openairdocs.org/sdr/9519139946.md): Bulkhead Tee · corroded · Nov 3, 1995 · N8926E · Doug DC931 · Fuselage Main, Bulkhead
  > DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE FS 756 T-CAP AT LONGERON 30. REPAIRED T-CAP (P/N 3915182-502), PER EA 99-103092.
- [SDR 9519129946](https://openairdocs.org/sdr/9519129946.md): Web · cracked · Nov 2, 1995 · N8926E · Doug DC931 · Fuselage Miscellaneous Structure
  > DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND A CRACK IN THE FS 83 FLIGHT COMPARTMENT PRESSURE PANEL WEB, RIGHT SIDE. REPAIRED WEB (P/N 9910073), PER EA 99-103091.
- [SDR 9519119946](https://openairdocs.org/sdr/9519119946.md): Bulkhead Tee · cracked · Oct 30, 1995 · N8926E · Doug DC931 · Fuselage Main, Bulkhead
  > DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND A CRACK IN THE FS 996 AFT PRESSURE BULKHEAD FLOOR TEE AT RBL 34. REPAIRED TEE (P/N 5910163-139), PER EA 99-102944.
- [SDR 9519109946](https://openairdocs.org/sdr/9519109946.md): Frame · corroded · Oct 11, 1995 · N8926E · Doug DC931 · Fuselage Main, Frame
  > DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION IN THE FS 996 FRAME ANGLE AT THE T-CAP BETWEEN LONGERONS 26R TO 27R. REPAIRED PER EA 99-102943.
- [SDR 9515579946](https://openairdocs.org/sdr/9515579946.md): Longeron · corroded · Oct 10, 1995 · N8926E · Doug DC931 · Fuselage Main, Longeron/Stringer
  > DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION IN THE LONGERON 29L TO 30 FITTINGS AT FS 756. REPLACED FITTINGS PER SRM 51-05.
- [SDR 9519099946](https://openairdocs.org/sdr/9519099946.md): Intercostal · corroded · Oct 3, 1995 · N8926E · Doug DC931 · Fuselage Miscellaneous Structure
  > DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE FS 190 INTERCOSTAL ABOVE THE FORWARD STAIR CUTOUT. REPAIRED INTERCOSTAL (P/N 9957838-3), PER EA 99-102920.
- [SDR 9519089946](https://openairdocs.org/sdr/9519089946.md): Angle · corroded · Sep 30, 1995 · N8926E · Doug DC931 · Fuselage Miscellaneous Structure
  > DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE NOSE GEAR FORWARD LEFT DOOR JAMB INNER ANGLE FS 43. REPAIRED ANGLE PER EA 99-102962.
- [SDR 9515219946](https://openairdocs.org/sdr/9515219946.md): Fitting · cracked · Sep 30, 1995 · N8926E · Doug DC931 · Fuselage Miscellaneous Structure
  > DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CRACKS AND CORROSION IN THE FS 980 TO 996 FLOORBEAM END FITTINGS, LEFT AND RIGHT SIDES. REPLACED ALL FOUR FITTINGS PER SRM 51-01.
- [SDR 9515159946](https://openairdocs.org/sdr/9515159946.md): Fitting · corroded · Sep 27, 1995 · N8926E · Doug DC931 · Fuselage Miscellaneous Structure
  > DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION IN THE LONGERON 26L END FITTINGS AT FS 996. REPLACED FITTING PER SRM 51-01.
- [SDR 9518139946](https://openairdocs.org/sdr/9518139946.md): Skin · corroded · Sep 14, 1995 · N8926E · Doug DC931 · Fuselage Main, Plate/Skin
  > DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE FUSELAGE SKIN FS 746 BETWEEN LONGERON 20R TO 21R. REPAIRED SKIN (P/N 5911420-3), PER EA 99-102910.
- [SDR 9514139946](https://openairdocs.org/sdr/9514139946.md): Casting · cracked · Sep 7, 1995 · N8926E · Doug DC931 · Fuselage Miscellaneous Structure
  > DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND A CRACK IN THE ATTACH CASTING LOCATED AT FS 691, LEFT OF THE CENTER LINE IN THE LEFT MAIN LANDING GEAR WHEEL WELL. REPLACED CASTING PER SRM 51-01.
- [SDR 9514129946](https://openairdocs.org/sdr/9514129946.md): Casting · cracked · Sep 7, 1995 · N8926E · Doug DC931 · Fuselage Miscellaneous Structure
  > DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND A CRACK IN THE ATTACH CASTING BETWEEN THE FS 756 BULKHEAD AND LONGERON 29L IN THE LEFT MAIN LANDING GEAR WHEEL WELL. REPLACED CASTING PER SRM 51-03.
- [SDR 9519079946](https://openairdocs.org/sdr/9519079946.md): Spar Web · cracked · Sep 5, 1995 · N8926E · Doug DC931 · Horizontal Stabilizer, Spar/Rib
  > DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND A CRACK IN THE HORIZONTAL STABILIZER REAR SPAR WEB AT STA 104. REPAIRED WEB (P/N 9918401-103), PER EA 99-102688.
- [SDR 9513969946](https://openairdocs.org/sdr/9513969946.md): Bulkhead · corroded · Sep 5, 1995 · N8926E · Doug DC931 · Fuselage Main, Bulkhead
  > DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION BETWEEN THE LONGERON 29L AND 30 ATTACH CASTINGS AND THE FS 756 BULKHEAD. REPLACED BOTH CASTINGS PER SRM 51-01 AND DWG 3911418.
- [SDR 9513489946](https://openairdocs.org/sdr/9513489946.md): Fitting · cracked · Aug 28, 1995 · N8926E · Doug DC931 · Fuselage Miscellaneous Structure
  > DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND A CRACK IN THE RIGHT T-CAP TIE FITTING, FS 604 AT LONGERON 30. REPLACED FITTING PER SRM 51-01.
- [SDR 9513019946](https://openairdocs.org/sdr/9513019946.md): Skin · cracked · Aug 22, 1995 · N8926E · Doug DC931 · Fuselage Main, Plate/Skin
  > DURING ACCEPTANCE CHECK, FOUND SKIN CRACKED BETWEEN FS 148 AND 150, LONGERON 27L. FABRICATED DOUBLER AND INSTALLED PER EA 99-102752 AND SRM 53-04 FIG 8.
- [SDR 9512469946](https://openairdocs.org/sdr/9512469946.md): Fitting · cracked · Aug 10, 1995 · N8926E · Doug DC931 · Fuselage Miscellaneous Structure
  > DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND A CRACK IN THE LONGERON 25L END FITTING AT FS 110. REPLACED FITTING PER SRM 51-01.
- [SDR 9519059946](https://openairdocs.org/sdr/9519059946.md): Blkhd Web · corroded · Jul 13, 1995 · N8926E · Doug DC931 · Fuselage Main, Bulkhead
  > DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE FS 604 BULKHEAD WEB LOWER AFT EDGE. REPAIRED WEB (P/N 5914865-23), PER EA 99-92255.

## 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 = 'N8926E' AND deregistration_id = 'N8926E-2010-11-23'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N8926E-2010-11-23/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.
