# Service difficulty reports: N951U, cancelled Jan 6, 2011

A list on [N951U, cancelled Jan 6, 2011](https://openairdocs.org/deregistered/N951U-2011-01-06.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 · 57 reports

- [SDR AALA20090609TUL41](https://openairdocs.org/sdr/AALA20090609TUL41.md): Seat Track · corroded · May 20, 2009 · N951U · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION BEYOND LIMITS ON SEAT TRACK NR 5. INSTALLED PLUG PER AARD 53-20-00-10.
- [SDR AALA20090609TUL44](https://openairdocs.org/sdr/AALA20090609TUL44.md): Support Angle · cracked · May 15, 2009 · N951U · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > NR 2 SEAT TRACK SUPPORT ANGLE CRACKED AT STATION 927 BELOW FLOORBEAM. REMOVED CRACKED ANGLE, INSTALLED NEW ANGLE PER SRM 51-01.
- [SDR AALA20090609TUL43](https://openairdocs.org/sdr/AALA20090609TUL43.md): Longeron · cracked · May 15, 2009 · N951U · Doug DC982 · Fuselage Main, Longeron/Stringer
  > LONGERON 20L CRACKED AT STATION 1003. STOP DRILLED CRACK AND INSTALLED DOUBLER PER AARD 53-10-00-18.
- [SDR AALA20090609TUL47](https://openairdocs.org/sdr/AALA20090609TUL47.md): Pressure Panel · cracked · May 14, 2009 · N951U · Doug DC982 · Fuselage Main, Bulkhead
  > CRACK IN RIGHT WHEEL WELL PRESSURE DECK AT STATION 990 IN AREA OF FUEL LINE SHROUD. STOP DRILLED CRACK, INSTALLED TITANIUM DOUBLER PER AARD 53-30-00-13.
- [SDR AALA20090512TUL49](https://openairdocs.org/sdr/AALA20090512TUL49.md): Battery Pack · discharged · Apr 29, 2009 · N951U · Doug DC982 · Emergency Lighting
  > CEILING EMERGENCY LIGHTS ARE INOP FROM SEAT 7 TO 16. REMOVED AND REPLACED BATTERY PACKS IN RT BIN PER MM 33-60-98-4.
- [SDR AALA20090512TUL38](https://openairdocs.org/sdr/AALA20090512TUL38.md): Skin · damaged · Apr 24, 2009 · N951U · Doug DC982 · Fuselage Main, Plate/Skin
  > LT ALT STATIC PORT, 7 INCH WAVINESS CHECK IS OUT OF LIMITS. INSTALLED DOUBLER PER SRM 51-30-2.
- [SDR AALA20090513TUL15](https://openairdocs.org/sdr/AALA20090513TUL15.md): Skin · dented · Apr 23, 2009 · N951U · Doug DC982 · Fuselage Main, Plate/Skin
  > DENT IN FUSELAGE STA 333 ABOVE LONG 23L. INSTALLED DOUBLER PER SRM 53-04 FIG 38.
- [SDR AALA20090513TUL14](https://openairdocs.org/sdr/AALA20090513TUL14.md): Skin · dented · Apr 23, 2009 · N951U · Doug DC982 · Fuselage Main, Plate/Skin
  > DENT IN FUSELAGE BETWEEN LONG 17L-18L. REPAIRED PER SRM 53-04 FIG 38 SHEET 30 VIEW P.
- [SDR AALA20090513TUL13](https://openairdocs.org/sdr/AALA20090513TUL13.md): Channel · cracked · Apr 23, 2009 · N951U · Doug DC982 · Fuselage Miscellaneous Structure
  > NOSE LANDING GEAR WHEEL WELL C-CHANNEL IS CRACKED AT SPRAY DEFLECTOR GUIDE LT SIDE. REPAIRED PER AARD 53-10-00-4 REPAIR NR 4.
- [SDR AALA20090513TUL10](https://openairdocs.org/sdr/AALA20090513TUL10.md): Skin · dented · Apr 22, 2009 · N951U · Doug DC982 · Fuselage Main, Plate/Skin
  > DENT IN FUSELAGE AT STA 254 AND LONG 18L-19L. INSTALLED DOUBLER PER SRM 53-04 FIG 12B.
- [SDR AALA20090513TUL11](https://openairdocs.org/sdr/AALA20090513TUL11.md): Cusp Web · cracked · Apr 21, 2009 · N951U · Doug DC982 · Fuselage Miscellaneous Structure
  > RT CUSP CRACKED UNDER NUMBER 5 SEAT TRACK. CUT OUT CRACKED AREA AND INSTALLED DOUBLER PER 53-20-00-16.
- [SDR AALA20090513TUL07](https://openairdocs.org/sdr/AALA20090513TUL07.md): Skin · corroded · Apr 21, 2009 · N951U · Doug DC982 · Fuselage Main, Plate/Skin
  > LT ALTERNATE STATIC PORT HAS CORROSION. INSTALLED NEW DOUBLER PER SRM 51-30-2.
- [SDR AALA20090513TUL09](https://openairdocs.org/sdr/AALA20090513TUL09.md): Skin · dented · Apr 16, 2009 · N951U · Doug DC982 · Fuselage Main, Plate/Skin
  > DENT IN FUSELAGE AT RT STA 355 ABOVE LONG 21R. COLD WORK DENT AND INSTALLED DOUBLER PER SRM 53-04 FIG 38.
- [SDR AALA20050807](https://openairdocs.org/sdr/AALA20050807.md): Oil System · leaking · Dec 8, 2005 · N951U · Doug DC982 · APU Oil System
  > ORD - COMING IN FOR LANDING AT ABOUT 2000 FEET SMELLED AN UNIDENTIFIED ODOR. AFTER LANDING FLIGHT ATTENDANTS INFORMED CREW OF A LITE HAZY SMOKE IN THE CABIN. SHUT OFF THE WING AND ENGINE ANTI-ICE AND THE SMOKE SUBSIDED. SUSPECT OIL LEAKING INTO APU INLET. R
- [SDR AALA20041036](https://openairdocs.org/sdr/AALA20041036.md): Battery Pack · inoperative · Oct 10, 2004 · N951U · Doug DC982 · Emergency Lighting
  > DFW - TAIL CONE EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK B527 FOR TAIL CONE EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION.
- [SDR AALA20041035](https://openairdocs.org/sdr/AALA20041035.md): Battery Pack · inoperative · Oct 10, 2004 · N951U · Doug DC982 · Emergency Lighting
  > DFW - AFT ENTRY OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK B527 FOR AFT ENTRY OVERHEAD EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.
- [SDR ZW0A0301302](https://openairdocs.org/sdr/ZW0A0301302.md): Frame · corroded · Jan 27, 2003 · N951U · Doug DC982 · Fuselage Main, Frame
  > DURING CHECK-C, IN THE AFT CARGO COMPT FOUND BULKHEAD FRAME CORRODED AT STRINGER 1320, RBL 6, LBL 40. REMOVED OLD FRAME AND REPLACED PER SPM 6-70-01.
- [SDR ZW0A0301104](https://openairdocs.org/sdr/ZW0A0301104.md): Bracket · cracked · Jan 17, 2003 · N951U · Doug DC982 · Cargo/Baggage Doors
  > DURING CHECK-C CRACKED BRACKET FOR LOWER AFT DOOR STOP FORWARD CARGO DOOR. REPLACED BRACKET PER SRM 52-03.
- [SDR ZW0A0301103](https://openairdocs.org/sdr/ZW0A0301103.md): Door Frame · cracked · Jan 16, 2003 · N951U · Doug DC982 · Cargo/Baggage Doors
  > DURING CHECK-C MAINT FORWARD CARGO DOOR FORWARD SIDE AT SECOND DOOR STOP FROM BOTTOM PIN AREA CRACKED. INSTALLED DOUBLER REPAIR PER SRM 52-05 PAGE 291.
- [SDR ZW0A0300811](https://openairdocs.org/sdr/ZW0A0300811.md): Bracket · corroded · Jan 13, 2003 · N951U · Doug DC982 · Fuselage Miscellaneous Structure
  > DURING CHECK-C MAINT FOUND FWD SERVICE DOOR AFT SILL BRACKET CORRODED, STA 197 AND RBL 53. REPLACED BRACKET PER DOUGLAS DRAWING 9911516 AND SPM 6-70-01 FASTENER SUBSTITUTION, 51-50-01 SRM.
- [SDR ZW0A0300810](https://openairdocs.org/sdr/ZW0A0300810.md): Web · corroded · Jan 13, 2003 · N951U · Doug DC982 · Fuselage Miscellaneous Structure
  > DURING CHECK-C MAINT IN THE FWD ENTRY FOUND CORROSION ON WEB, BELOW FLOOR AT STA 168 TO 200, LBL 54. CLEANED AREA OF CORROSION. CUT OUT AREA BEYOND LIMITS AND INSTALLED REPAIR PER SRM 53-01, PAGE 9.
- [SDR ZW0A0300809](https://openairdocs.org/sdr/ZW0A0300809.md): Fitting · corroded · Jan 13, 2003 · N951U · Doug DC982 · Emergency Equipment
  > DURING CHECK-C MAINT IN THE FWD CABIN AT THE FWD SERVICE DOOR WAY, FOUND SILL BRACKET (GIRT BAR FITTING) CORRODED AT STA 172, RBL 53. REMOVED AND REPLACED FITTING PER SPM 6-70-01.
- [SDR ZW0A0300808](https://openairdocs.org/sdr/ZW0A0300808.md): Floor Support · corroded · Jan 10, 2003 · N951U · Doug DC982 · Fuselage Miscellaneous Structure
  > DURING CHECK-C MAINT IN THE FWD CABIN, FOUND CORROSION ALONG THE FLOOR SUPPORT AT STA 148 TO 200, 8 INCHES LBL, UNDER NUMBER 5 FLOOR PANEL. INSTALLED NEW FLOOR SUPPORT PER SPM 6-70-01.
- [SDR ZW0A0300807](https://openairdocs.org/sdr/ZW0A0300807.md): Door Frame · cracked · Jan 10, 2003 · N951U · Doug DC982 · Fuselage Main, Structure
  > DURING CHECK-C MAINT FOUND CRACK IN LOWER DOOR BEAM AT LOWER HINGE CUTOUT. FWD SERVICE DOOR. REPLACED FRAME PER SRM SPM 6-70-01.
- [SDR ZW0A0300806](https://openairdocs.org/sdr/ZW0A0300806.md): Floor Support · corroded · Jan 10, 2003 · N951U · Doug DC982 · Fuselage Miscellaneous Structure
  > DURING CHECK-C MAINT FOUND CORROSION ALONG FLOOR SUPPORT AT STA 148 TO 200, 8 INCHES RBL, UNDER NUMBER 4 FLOOR PANEL. INSTALLED NEW FLOOR SUPPORT, FABRICATED FROM EXTRUSION PER SPM 6-70-01.
- [SDR ZW0A0300805](https://openairdocs.org/sdr/ZW0A0300805.md): Floor Support · damaged · Jan 8, 2003 · N951U · Doug DC982 · Fuselage Miscellaneous Structure
  > DURING CHECK-C MAINT FOUND CABIN FLOOR SUPPORT DAMAGED AT STA 905, LBL 12. REMOVED AND REPLACED FLOOR SUPPORT PER SPM 6-70-01.
- [SDR ZW0A0300804](https://openairdocs.org/sdr/ZW0A0300804.md): Floor Support · corroded · Jan 7, 2003 · N951U · Doug DC982 · Fuselage Miscellaneous Structure
  > DURING CHECK-C MAINT FOUND A CORRODED CABIN FLOOR SUPPORT CAP AT STA 1250, LBL 22 TO 44. REMOVED CORRODED CAP. CLEANED AREA AND FABRICATED AND INSTALLED NEW CAP PER SPM 6-70-01.
- [SDR ZW0A0300803](https://openairdocs.org/sdr/ZW0A0300803.md): Floor Support · corroded · Jan 7, 2003 · N951U · Doug DC982 · Fuselage Miscellaneous Structure
  > DURING CHECK-C IN THE CABIN A CORRODED FLOOR SUPPORT CAP WAS FOUND AT STA 1155, LBL 22 TO 44. REMOVED CORRODED CAP. CLEANED AREA AND INSTALLED NEW FABRICATED CAP PER SPM 6-70-01.
- [SDR ZW0A0300802](https://openairdocs.org/sdr/ZW0A0300802.md): Angle · cracked · Jan 6, 2003 · N951U · Doug DC982 · Fuselage Miscellaneous Structure
  > DURING CHECK-C IN THE NLG WHEEL WHEEL A CRACK WAS FOUND ON RT SIDE OF NOSE GEAR WHEEL WELL JUST ABOVE THE RT FWD NOSE GEAR DOOR FWD HINGE, 8 INCHES AFT OF STA 37 ON WHEEL WELL CUTOUT SUPPORT ANGLE ON THE RT SIDE. CRACK WAS THROUGH FASTENER. TWO STACKED DOUBL
- [SDR ZW0A0210203](https://openairdocs.org/sdr/ZW0A0210203.md): Control Cable · out of rig · Sep 29, 2002 · N951U · Doug DC982 · Leading Edge Slat Control System
  > WHEN FLAPS EXTENDED TO 15 DEGREES THE SLAT DISAGREE LIGHT ILLUMINATED. DURING APPROACH SLAT DISAGREE LIGHT CONTINUED TO INTERMITTENTLY CHANGE BETWEEN OFF AND DISAGREE. NO ASYMMETRY IN FLIGHT CONTROLS WAS NOTICED. RIGGED SLAT FOLLOW UP CABLES PER MM 27-81-02
- [SDR ZW0A0201002](https://openairdocs.org/sdr/ZW0A0201002.md): Cable · Jan 22, 2002 · N951U · Doug DC982 · Leading Edge Slat Control System
  > FOUND FLAP BUS TRAVEL CABLE BROKEN. REPLACED THE CABLE. CHECK-C 8-25-01 STL. --CLOSED--
- [SDR ZW0A0201001](https://openairdocs.org/sdr/ZW0A0201001.md): Cable · Jan 22, 2002 · N951U · Doug DC982 · Leading Edge Slat Control System
  > FOUND FLAP BUS TRAVEL CABLE BROKEN. REPLACED THE CABLE. CHECK-C 8-25-01 STL. ---CLOSED---
- [SDR TWAA0105602](https://openairdocs.org/sdr/TWAA0105602.md): Battery · discharged · Mar 28, 2001 · N951U · Doug DC982 · Emergency Lighting
  > THE COCKPIT EMERGENCY FLOOD LIGHTS WERE INOPERATIVE. REPLACED THE BATTERIES. CHECK-C 9-8-00 STL.
- [SDR TWAA0105601](https://openairdocs.org/sdr/TWAA0105601.md): Light · inoperative · Mar 28, 2001 · N951U · Doug DC982 · Emergency Lighting
  > THE AFT ACCESSORY COMPT EMERGENCY LIGHTS WERE INOPERATIVE. REPLACED THE LAMPS. CHECK-C 9-8-00 STL.
- [SDR TWAA0017603](https://openairdocs.org/sdr/TWAA0017603.md): Wire · worn · Nov 8, 2000 · N951U · Doug DC982 · Light System Wiring
  > THE FIRST CLASS FLOOR EGRESS LIGHTS WERE INOPERATIVE. REPAIRED WIRING, WORN DUE TO WEAR AND TEAR. CHECK-C 9-8-00 STL.
- [SDR TWAA0008602](https://openairdocs.org/sdr/TWAA0008602.md): Gyro · failed · May 31, 2000 · N951U · Doug DC982 · Attitude and Direction Data System
  > DURING CRUISE, F/O''S RMI AND CAPT''S HSI BECAME ERRATIC THEREAFTER VG NUMBER 1 FAILED AND WOULD NOT RESET. REPLACED VG (PN 19911-C1) (S/N 45145) AND DG (P/N 17265-2A) (S/N 55485). AC03 04-04-00 JFK.
- [SDR TWAA9911303](https://openairdocs.org/sdr/TWAA9911303.md): Intercostal · cracked · Aug 13, 1999 · N951U · Doug DC982 · Fuselage Miscellaneous Structure
  > DURING OP 16 MAINT CHECK, FOUND AFT CARGO COMPT TRACK SUPPORT INTERCOSTAL CRACKED AND CORRODED AT STA 1309, LONGERON 27R TO 28R. REMOVED INTERCOSTAL AND REPLACED PER SPM 6-70-01, PAGE 3.
- [SDR TWAA9911304](https://openairdocs.org/sdr/TWAA9911304.md): Support · corroded · Aug 11, 1999 · N951U · Doug DC982 · Fuselage Miscellaneous Structure
  > DURING OP 16 MAINT CHECK, FOUND CABIN FLOOR SUPPORT CORRODED AT STA 198, RBL 9 TO RBL44. FABRICATED ANGLE FROM 7075 T-6 PER SPM 6-70-01.
- [SDR TWAA9911302](https://openairdocs.org/sdr/TWAA9911302.md): Support · corroded · Aug 11, 1999 · N951U · Doug DC982 · Fuselage Miscellaneous Structure
  > DURING OP 16 MAINT CHECK, THE CABIN O/B FLOOR SUPPORT RAIL WAS CORRODED AT STA 160 TO 198 AT FWD GALLEY DOOR. REMOVED THE CORROSION BY REPLACEMENT OF THE PART PER SPM 6-70-01, SEALED AND USED 5/32 AD RIVETS.
- [SDR TWAA9911210](https://openairdocs.org/sdr/TWAA9911210.md): Support · corroded · Aug 10, 1999 · N951U · Doug DC982 · Fuselage Miscellaneous Structure
  > DURING OP 16 MAINT CHECK, FOUND CORROSION ON CABIN FLOOR SUPPORT, STA 200, OTBD OF CHAIR TRACK AT RBL 44. REMOVED AND REPLACED SUPPORT MEMBER PER SPM 6-70-01, PAGE 2.
- [SDR TWAA9911209](https://openairdocs.org/sdr/TWAA9911209.md): Intercostal · corroded · Aug 10, 1999 · N951U · Doug DC982 · Fuselage Miscellaneous Structure
  > DURING OP 16 MAINT CHECK, FOUND IN AFT CARGO COMPT AT STA 1212 TO 1216, INTERCOSTAL BETWEEN LONGERONS 29R AND 30 WITH CORROSION ON FOOT. REMOVED AND RELACED FOOT PER SPM 6-70-01.
- [SDR TWAA9911208](https://openairdocs.org/sdr/TWAA9911208.md): Seat Track · corroded · Aug 10, 1999 · N951U · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > DURING OP 16 MAINT CHECK, FOUND CORROSION ON CHAIR TRACK FLANGE, STA 1271 TO 1307, LBL 44. REPLACED CHAIR TRACK PER SPM 6-70-01.
- [SDR TWAA9911207](https://openairdocs.org/sdr/TWAA9911207.md): Seat Track · corroded · Aug 10, 1999 · N951U · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > DURING OP 16 MAINT CHECK, FOUND CORROSION ON CHAIR TRACK FLANGE AT STA 1212 TO 1250, LBL 44. REPLACED CHAIR TRACK PER SPM 6-70-01.
- [SDR TWAA9911203](https://openairdocs.org/sdr/TWAA9911203.md): Intercostal · corroded · Aug 4, 1999 · N951U · Doug DC982 · Fuselage Miscellaneous Structure
  > DURING OP 16 MAINT CHECK, FOUND STA 1212 TO 1216 LONGERON 29R INTERCOSTAL CORRODED. REMOVED CORROSION BY REPLACEMENT OF PART PER SRM 51-10-3.
- [SDR TWAA9816310](https://openairdocs.org/sdr/TWAA9816310.md): Battery Pack · discharged · Oct 11, 1998 · N951U · Doug DC982 · Emergency Lighting
  > DURING MAINT CHECK, FOUND EMERGENCY CEILING LIGHT INOP AT AFT LAVS. REPLACED BATTERY PACK. CHECK-C 7-28-98 MCI.
- [SDR TWAA9816309](https://openairdocs.org/sdr/TWAA9816309.md): Battery Pack · discharged · Oct 11, 1998 · N951U · Doug DC982 · Emergency Lighting
  > DURING MAINT CHECK, FOUND EMERGENCY CEILING LIGHT INOPERATIVE AT CABIN ROWS 9 AND 11. REPLACED BATTERY PACK. CHECK-C 7-28-98 MCI.
- [SDR TWAA9811802](https://openairdocs.org/sdr/TWAA9811802.md): Connector · shorted · Jul 22, 1998 · N951U · Doug DC982 · Hydraulic Pump, Auxiliary
  > DURING CHECK-C MAINTENANCE, WHILE OPERATING THE AUX HYD PUMP THE ELECTRICAL CONNECTOR ON THE PUMP SHORTED, BURNING THE CONNECTOR CONTACTS AND CAUSING A SMALL FIRE AT THE CONNECTOR. REPLACED THE AUX HYD PUMP CONN AND THE PUMP. (M)
- [SDR TWAA9809009](https://openairdocs.org/sdr/TWAA9809009.md): Hyd Fluid · lost · Jun 7, 1998 · N951U · Doug DC982 · Hydraulic System, Main
  > STL - FLT 203 - DURING TAKEOFF, LOST RT SYSTEM HYDRAULIC FLUID. REPLACED RT NOSE TIRE MFG PN 3910097-535 DUE TO TREAD CAP MISSING. CC-010 7-20-97 LAX. (X)
- [SDR TWAA9804103](https://openairdocs.org/sdr/TWAA9804103.md): Generator · worn · Mar 19, 1998 · N951U · Doug DC982 · AC Generator-Alternator
  > JFK - FLT 8703 - THE LEFT GEN FAILED, NO VOLTS OR FREQS. APU STARTED AND RAN NORMALLY FOR 30 MINUTES THEN APU GEN FAILED, NO VOLTS OR FREQS RETURNED TO JFK. THE LEFT GEN WAS DEFERRED PER MEL, AND THE APU GENERATOR CONTROL UNIT WAS REPLACED. IN FLIGHT, THE A
- [SDR TWAA9713905](https://openairdocs.org/sdr/TWAA9713905.md): Duct · cracked · Nov 27, 1997 · N951U · Doug DC982 · Pneumatic Distribution System
  > PBI - FLT 229 - DURING CLIMB, HAD A RECURRENCE OF TAIL COMPARTMENT HIGH LIGHT ILLUMINATION. LIGHT WENT OUT WITH POWER REDUCTION. REPAIRED RIGHT AND LEFT PACK Y DUCT MFG P/N 5953625-521. ACCOMPLISHED TAIL COMPARTMENT LEAK AND Y DUCT HIGH PRESSURE CHECKS. OP

Next page: https://openairdocs.org/deregistered/N951U-2011-01-06/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 = 'N951U' AND deregistration_id = 'N951U-2011-01-06'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N951U-2011-01-06/reports

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