# Service difficulty reports: N953U, cancelled Jul 25, 2017

A list on [N953U, cancelled Jul 25, 2017](https://openairdocs.org/deregistered/N953U-2017-07-25.md).

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

- [SDR AALA20050066](https://openairdocs.org/sdr/AALA20050066.md): Battery Pack · inoperative · Jan 31, 2005 · N953U · Doug DC982 · Emergency Lighting
  > MSP - EMERGENCY LIGHTS AT AFT FLIGHT ATTENDANT AREA INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT AFT FLIGHT ATTENDANT AREA. SYSTEM GROUND CHECKED NORMAL OPERATION.
- [SDR ZW0A0304701](https://openairdocs.org/sdr/ZW0A0304701.md): Battery · inoperative · May 7, 2003 · N953U · Doug DC982 · Emergency Lighting
  > THE EMERGENCY OVERHEAD LIGHTS FROM ROWS 23 THRU 27, AND THE EMERGENCY OVERHEAD LIGHTS JUST FWD OF AFT TAIL CONE EXIT DOOR, WERE INOPERATIVE. REPLACED THE BATTERIES IN POWER SUPPLY B5-106 FOR ROWS 23 THRU 27, AND REPLACED THE BATTERIES IN POWER SUPPLY B5-28 FO
- [SDR ZW0A0303401](https://openairdocs.org/sdr/ZW0A0303401.md): Battery · inoperative · Mar 22, 2003 · N953U · Doug DC982 · Emergency Lighting
  > THE OVERHEAD EMERGENCY LIGHTS WERE INOPERATIVE FROM ROW 12 TO 17, AND FROM ROW 23 AFT INCLUDING IN TAIL COMPARTMENT. REPLACED BATTERIES FOR ROW 12 TO 17, AND RESEATED BATTERIES FOR ROW 23 AFT. CHECK-C 2-18-03 STL.
- [SDR ZW0A0301501](https://openairdocs.org/sdr/ZW0A0301501.md): Lamp · Feb 3, 2003 · N953U · Doug DC982 · Emergency Lighting
  > THE LEFT OVERWING EXTERIOR EMERGENCY LIGHT WAS INOPERATIVE. REPLACED THE LAMP. CHECK-C 2-8-02 STL. --CLOSED--
- [SDR ZW0A0211401](https://openairdocs.org/sdr/ZW0A0211401.md): Pressure Switch · failed · Nov 15, 2002 · N953U · Doug DC982 · Airfoil Anti/De-ice System
  > STRONG BURNING ODOR IN COCKPIT WITH AIR FOIL ANTI ICE ON. ODOR CEASED WHEN AIRFOIL ANTI ICE TURNED OFF. ACCOMPLISHED HANDBOOK PROCEDURE. MAINTENANCE REPLACED ANTICIPATOR, THERMOSTAT AND LOW PRESSURE SWITCH. CHECK-C 2-8-02 STL. --CLOSED--
- [SDR TWAA0101601](https://openairdocs.org/sdr/TWAA0101601.md): Power Supply · discharged · Jan 25, 2001 · N953U · Doug DC982 · Emergency Lighting
  > THE EGRESS LIGHTS FROM ROW 30 TO AFT LAVS COME ON WHEN SWITCH IS ARMED. REPLACED POWER SUPPLY. CHECK-C 3-21-00 MCI.
- [SDR TWAA0004309](https://openairdocs.org/sdr/TWAA0004309.md): Frame · cut · Mar 14, 2000 · N953U · Doug DC982 · Fuselage Miscellaneous Structure
  > DURING CHECK-C MAINT, CABIN WINDOW FRAMES WERE CUT APPROX 0.003 TO 0.005 DEEP ON LEFT SIDE FROM STA 256 TO 1271. BLENDED OUT DAMAGE PER ARA 16570A TO 63 MICRO FINISH. ALODINED AND PAINTED. REPLACED WINDOW BELT PANEL 9958156-1 AT STA 408 TO 313.
- [SDR TWAA0004308](https://openairdocs.org/sdr/TWAA0004308.md): Frame · scratched · Mar 14, 2000 · N953U · Doug DC982 · Fuselage Miscellaneous Structure
  > DURING CHECK-C MAINT, CABIN WINDOW FRAMES WERE CUT APPROX 0.003 TO 0.005 DEEP ON RT SIDE FROM STA 256 TO 1271. BLENDED OUT DAMAGE PER ARA 1670A TO 63 MICRO FINISH. AREA ALODINED AND TREATED.
- [SDR TWAA0004307](https://openairdocs.org/sdr/TWAA0004307.md): Door · damaged · Mar 14, 2000 · N953U · Doug DC982 · Emergency Exits
  > DURING CHECK-C MAINT, ALL FOUR OVERWING EMERGENCY EXIT DOORS HAD A DEEP SCRIBE LINE AROUND THE WINDOW FRAME. ON ALL FOUR EXITS, BLENDED OUT DAMAGE PER ARA 16570A TO 63 MICRO FINISH AND ALODINED.
- [SDR TWAA0004306](https://openairdocs.org/sdr/TWAA0004306.md): Skin · corroded · Mar 12, 2000 · N953U · Doug DC982 · Fuselage Main, Plate/Skin
  > DURING CHECK-C MAINT, THE BOTTOM OF FUSELAGE SKIN HAD RIVET HEADS STRESSED AND CRACKED, AND SKIN BULGED OUT FROM CORROSION AT AFT END OF NUMBER 1 VHF ANTENNA, STA 465 TO 484. REMOVED CORRODED ANTENNA SUPPORT. INSTALLED NEW INTERCOSTAL SUPPORT GUSSET AND CLIP
- [SDR TWAA0004304](https://openairdocs.org/sdr/TWAA0004304.md): Angle · corroded · Mar 8, 2000 · N953U · Doug DC982 · Fuselage Miscellaneous Structure
  > DURING CHECK-C MAINT, THE FWD SERVICE DOOR THRESHOLD UPPER CUSP ANGLE HAD CORROSION ON TOP AT STA 195, RBL 54 INCHES. CUT OUT DAMAGED CUSP AT STA 184 TO 203. REPLACED CUSP SECTION AND SPLICE PER 53-05, FIG 55. ALL PARTS REPAINTED.
- [SDR TWAA0003929](https://openairdocs.org/sdr/TWAA0003929.md): Skin · lightning strike · Mar 4, 2000 · N953U · Doug DC982 · Fuselage Main, Plate/Skin
  > DURING CHECK-C MAINT, FOUND STATIC BURN ON NUMBER 9 WINDOW FRAME, LEFT SIDE, UPPER FWD CORNER. INSTALLED NEW WINDOW BELT PANEL FROM STA 408 TO 313, LEFT SIDE, USING DRAWING 5911431 FOR FASTENER TYPE.
- [SDR TWAA0003904](https://openairdocs.org/sdr/TWAA0003904.md): Bulkhead · corroded · Mar 1, 2000 · N953U · Doug DC982 · Fuselage Main, Bulkhead
  > DURING CHECK-C MAINT, FOUND CORROSION ON BOTTOM FRAME OF AFT BULKHEAD DOOR. REPLACED BOTTOM DOOR CHANNEL PER SRM 51-01, SRM 51-30-4, SRM 51-30-2, SRM 51-30-3, 51-10-4. DOOR CHANNEL MFG PN 5910186-455.
- [SDR TWAA0003903](https://openairdocs.org/sdr/TWAA0003903.md): Bulkhead · cracked · Feb 28, 2000 · N953U · Doug DC982 · Fuselage Main, Bulkhead
  > DURING CHECK-C MAINT, FOUND CRACK AT TOP OF SUPPORT DOUBLER ON FWD FACE OF REAR BULKHEAD, STA 1338 BELOW LONGERON 1. REMOVED AND REPLACED EXISTING SUPPORT DOUBLER WITH NEW TWA PN 63-9879. PART SECURED TO BULKHEAD WITH MS20470AD-S RIVETS PER SRM 51-30-2, AND
- [SDR TWAA0003902](https://openairdocs.org/sdr/TWAA0003902.md): Floorbeam · corroded · Feb 28, 2000 · N953U · Doug DC982 · Fuselage Main, Floor Beam
  > DURING CHECK-C MAINT, MEMBRANE BELOW FLOOR STA 1140 TO 1180, LBL 48 TO 56, HAD CORROSION ON UPPER AND LOWER SURFACES. REMOVED CORROSION PER SRM 53-01, PAGE 18 FIG 4 SHEET 3, AND TWA STD PROCEDURES MANUAL 6-80-01 PAGE 1 TO 3. TREATED AND PRIMED PER SRM 51-10-
- [SDR TWAA0003303](https://openairdocs.org/sdr/TWAA0003303.md): Skin · damaged · Feb 21, 2000 · N953U · Doug DC982 · Cargo/Baggage Doors
  > DURING CHECK-C MAINT, THE AFT CARGO DOOR, FWD EDGE OF CARGO DOOR SKIN WAS DENTED MID WAY UP THE DOOR. CUT OUT DAMAGED AREA AND MADE INTERIOR DOUBLER PLUG. INSTALLED WITH SEALER PER SRM 52-03, PAGE 1 PARA 26, AND SRM 52-03 FIG 6.
- [SDR TWAA0003003](https://openairdocs.org/sdr/TWAA0003003.md): Longeron · corroded · Feb 20, 2000 · N953U · Doug DC982 · Fuselage Main, Longeron/Stringer
  > DURING CHECK-C MAINTENANCE, LONGERON 29L HAD CORROSION AT STA 370 TO 427. REMOVED CORRODED LONGERON STA 370 TO 484. INSTALLED NEW LONGERON. SPLICED PER SRM 53-02 FIG 18. INSTALLED HI-LOCKS PER SRM 51-30-5. INSTALLED RIVETS PER 51-30-2 OF THE SRM.
- [SDR TWAA0003002](https://openairdocs.org/sdr/TWAA0003002.md): Floorbeam · corroded · Feb 19, 2000 · N953U · Doug DC982 · Fuselage Main, Floor Beam
  > DURING CHECK-C MAINTENANCE, THE TOP OF FLOORBEAM STA 1322, LBL 40 IN, HAD CORROSION AT FLOOR PANEL HOLE. REMOVED CORROSION OF FLOOR BEAM PER SRM 51-10-3. REPAIRED FLOORBEAM PER SRM 53-05, FIG 20A.
- [SDR TWAA0002909](https://openairdocs.org/sdr/TWAA0002909.md): Tie Clip · cracked · Feb 17, 2000 · N953U · Doug DC982 · Rudder, Tab Structure
  > DURING CHECK-C MAINT, FOUND 8 DORSAL FIN FORMER TIE CLIPS CRACKED, 3 ON THE LT SIDE AND 5 ON THE RT SIDE. REPAIRED PER SSRM 55-30-102, PAGE 201, AND SRM 55-02 FIG 19.
- [SDR TWAA0003009](https://openairdocs.org/sdr/TWAA0003009.md): Rib · cracked · Feb 16, 2000 · N953U · Doug DC982 · Wing, Rib/Bulkhead
  > DURING CHECK-C MAINT, ON RT WING LE RIB STA XRS 418 WAS CRACKED AT AFT END. THE CRACKED ATTACH ANGLE WAS REMOVED FROM LE FORMER. NEW ANGLE AND DOUBLER WERE FABRICATED FROM 7075-0 AND HEAT TREATED TO 7075-T6. PARTS INSTALLED PER SRM 57-06A, PAGE 17 FIG 5 SHE
- [SDR TWAA0003008](https://openairdocs.org/sdr/TWAA0003008.md): Floorbeam · corroded · Feb 15, 2000 · N953U · Doug DC982 · Fuselage Main, Floor Beam
  > DURING CHECK-C MAINTENANCE, AFT CABIN FOUND CUTOUT IN MEMBRANE APPROXIMATELY 5 INCHES SQUARE INVOLVING A LIGHTENING HOLE OTBD OF NUMBER 1 TRACK, LT STA 1283 TO 1286. INSTALLED MEMBRANE DOUBLER PER SRM 53-05, FIG 96 SHEET 3.
- [SDR TWAA0003007](https://openairdocs.org/sdr/TWAA0003007.md): Floorbeam · corroded · Feb 15, 2000 · N953U · Doug DC982 · Fuselage Main, Floor Beam
  > DURING CHECK-C MAINTENANCE, FOUND AFT CABIN STA 1307 FLOOR LEVEL LT SIDE, ALL THE WAY OTBD, AN OLD REPAIR WAS FULL OF CORROSION. REMOVED CORROSION PER SPM 6-80-01. MADE FILLER 0.025 7075-T6. INSTALLED MEMBRANE DOUBLER PER SRM 53-05, SHEET 3 FIG 96.
- [SDR TWAA0003006](https://openairdocs.org/sdr/TWAA0003006.md): Floorbeam · cracked · Feb 15, 2000 · N953U · Doug DC982 · Fuselage Main, Floor Beam
  > DURING CHECK-C MAINTENANCE, FOUND CRACK IN AFT CABIN MEMBRANE, LEFT STA APPROX 1295, 2 INCHES INBD OF SIDEWALL, FLOOR LEVEL. REMOVED CORROSION PER SPM 6-80-01. INSTALLED MEMBRANE DOUBLER PER SRM 53-05, SHEET 3.
- [SDR TWAA0003005](https://openairdocs.org/sdr/TWAA0003005.md): Floorbeam · corroded · Feb 15, 2000 · N953U · Doug DC982 · Fuselage Main, Floor Beam
  > DURING CHECK-C MAINT IN THE AFT CABIN, AN OLD REPAIR INSTALLED WITH BLIND FASTENERS WAS ALSO SHOWING CORROSION ON LT STA 1287. REPAIR WAS INSTALLED EXTENDING FROM SIDEWALL INBOARD. REMOVED REPAIR. REMOVED CORROSION PER SRM 6-80-01. INSTALLED MEMBRANE DOUBL
- [SDR TWAA0003004](https://openairdocs.org/sdr/TWAA0003004.md): Floorbeam · cracked · Feb 15, 2000 · N953U · Doug DC982 · Fuselage Main, Floor Beam
  > DURING CHECK-C MAINTENANCE, IN THE CABIN FOUND A CRACKED MEMBRANE APPROX STA 1295, FLOOR LEVEL STRINGER 18L. INSTALLED MEMBRANE DOUBLER PER SRM 53-05, FIG 96 SHEET 3.
- [SDR TWAA0002709](https://openairdocs.org/sdr/TWAA0002709.md): Longeron · cracked · Feb 14, 2000 · N953U · Doug DC982 · Fuselage Main, Longeron/Stringer
  > DURING CHECK-C MAINT, LONGERON 4L WAS CRACKED AT STA 160. REPLACED LONGERON PER SRM 51-01 PAGE 1 FROM STA 151 TO 230.
- [SDR TWAA0003901](https://openairdocs.org/sdr/TWAA0003901.md): Floorbeam · cracked · Feb 2, 2000 · N953U · Doug DC982 · Fuselage Main, Floor Beam
  > DURING CHECK-C MAINT, FLOOR MEMBRANE WAS CRACKED AT STA 1293, JUST INBD OF LONGERON 18R. REPAIRED MEMBRANE PER SRM 53-05, FIG 96.
- [SDR TWAA0002304](https://openairdocs.org/sdr/TWAA0002304.md): Rib · cracked · Jan 31, 2000 · N953U · Doug DC982 · Wing, Rib/Bulkhead
  > DURING CHECK-C MAINTENANCE, THE RT WING LE RIB SRA XR5269 WAS CRACKED AT AFT END. REPLACED CRACKED CLIP PER SRM 51-01.
- [SDR TWAA0002303](https://openairdocs.org/sdr/TWAA0002303.md): Skin · damaged · Jan 28, 2000 · N953U · Doug DC982 · Trailing Edge Flaps
  > DURING CHECK-C MAINT, FOUND RT WING TE OF INBD FLAP WAS DINGED 18 IN FROM OTBD EDGE OF INBD FLAP. INSTALLED REPAIR DOUBLERS IN ACCORDANCE WITH SRM 51-70-1.
- [SDR TWAA9905701](https://openairdocs.org/sdr/TWAA9905701.md): Battery Pack · discharged · Apr 16, 1999 · N953U · Doug DC982 · Emergency Lighting
  > THE EMERGENCY EXIT SIGNS AT FWD SIDE OF BOTH FWD EMERGENCY EXIT DOORS WERE INOPERATIVE. REPLACED THE BATTERY PACK. CHECK-C 3-26-99 STL.
- [SDR TWAA9906310](https://openairdocs.org/sdr/TWAA9906310.md): Angle · cracked · Apr 5, 1999 · N953U · Doug DC982 · Vertical Stabilizer
  > DURING CHECK-C MAINT, FOUND A.1875 IN CRACK AT THE RT FWD DORSAL FIN ATTACH ANGLE AT STA 1421. REMOVED AND REPLACED ATTACH ANGLE PER SERVICE BULLETIN 53-223 PER MD9-AD-13.
- [SDR TWAA9905402](https://openairdocs.org/sdr/TWAA9905402.md): Angle · cracked · Apr 5, 1999 · N953U · Doug DC982 · Vertical Stabilizer
  > DURING CHECK-C MAINT, FOUND.1875 INCH CRACK AT THE RT FWD DORSAL FIN ATTACH ANGLE AT STA 1421. REMOVED AND REPLACED ATTACH ANGLE PER SB 53-223 AND PER MD9-AD-13.
- [SDR TWAA9905101](https://openairdocs.org/sdr/TWAA9905101.md): Angle · cracked · Apr 5, 1999 · N953U · Doug DC982 · Vertical Stabilizer
  > DURING CHECK-C MAINT, FOUND.1875 INCH CRACK AT THE RT FWD DORSAL FIN ATTACH ANGLE, STA 1421. REMOVED AND REPLACED ATTACH ANGLE PER SERVICE BULLETIN 53-223, AND PER MD9-AD-13.
- [SDR TWAA9906309](https://openairdocs.org/sdr/TWAA9906309.md): Angle · cracked · Apr 4, 1999 · N953U · Doug DC982 · Vertical Stabilizer
  > DURING CHECK-C MAINT, FOUND.1875 IN CRACK AT THE LT DORSAL FIN ATTACH ANGLE AT STA 1421. INSTALLED NEW ATTACH ANGLE PER SERVICE BULLETIN 53-223 AND SR09530162.
- [SDR TWAA9906308](https://openairdocs.org/sdr/TWAA9906308.md): Angle · cracked · Apr 4, 1999 · N953U · Doug DC982 · Elevator Structure
  > DURING CHECK-C MAINT, FOUND INSIDE ANGLE AT STA 1421, LT SIDE, WAS CRACKED. INSTALLED NEW ANGLE PER SRM 51-30-2 AND 51-30-5.
- [SDR TWAA9905403](https://openairdocs.org/sdr/TWAA9905403.md): Angle · cracked · Apr 4, 1999 · N953U · Doug DC982 · Vertical Stabilizer
  > DURING CHECK-C MAINT, FOUND.1875 INCH CRACK AT THE LT DORSAL FIN ATTACH ANGLE STA 1421. INSTALLED NEW ATTACH ANGLE PER SB 53-223 AND SRO9530162.
- [SDR TWAA9904903](https://openairdocs.org/sdr/TWAA9904903.md): Angle · cracked · Apr 4, 1999 · N953U · Doug DC982 · Vertical Stabilizer
  > DURING CHECK-C MAINT CHECK, FOUND.75 INCH CRACK AT THE LT DORSAL FIN ATTACH ANGLE AT STA 1421. INSTALLED NEW ATTACH ANGLE PER SVC BULLETIN 53-2234, SB 09530162.
- [SDR TWAA9906307](https://openairdocs.org/sdr/TWAA9906307.md): Angle · cracked · Apr 2, 1999 · N953U · Doug DC982 · Vertical Stabilizer
  > DURING CHECK-C MAINT, FOUND INSIDE ANGLE AT STA 1421 WAS CRACKED ON RT SIDE. INSTALLED NEW ANGLE AT STA 1421, PER SRM 51-10-4 AND 51-30-2.
- [SDR TWAA9903203](https://openairdocs.org/sdr/TWAA9903203.md): Air Dist · odor · Mar 2, 1999 · N953U · Doug DC982 · Air Distribution System
  > DURING PUSH BACK AND START OF RT ENGINE A BURN SMELL AND HAZE DEVELOPED IN THE AIRCRAFT. FOUND GLYCOL DRAINING FROM THE AFT FUSELAGE AREA. PERFORMED ENG RUNS AND APU TO CHECK FOR FUMES, NONE FOUND. CLEARED CABIN.
- [SDR TWAA9902901](https://openairdocs.org/sdr/TWAA9902901.md): Air Dist · smoke · Feb 23, 1999 · N953U · Doug DC982 · Air Distribution System
  > SMOKE WAS REPORTED IN CABIN AFTER AIR FOIL ANTI-ICE WAS TURNED ON. SUSPECT DEICER FLUID. COMPLETED PACK BURN OUT. CHECK-C 3-25-98 MCI.
- [SDR TWAA9816307](https://openairdocs.org/sdr/TWAA9816307.md): Housing · deformed · Oct 11, 1998 · N953U · Doug DC982 · Flight Compartment Equipment
  > FIRST OFFICER RT RUDDER PEDAL SEEMED TO BIND ON RUDDER PEDAL HOUSING. REPLACED FIRST OFF RUDDER PEDAL HOUSING. CHECK-C 3-25-98 MCI.
- [SDR TWAA9808202](https://openairdocs.org/sdr/TWAA9808202.md): Fire Loop · malfunctioned · May 22, 1998 · N953U · Doug DC982 · Fire Detection
  > IND - DLT 295 - DURING CRUISE, RT ENGINE FIRE WARNING CAME ON BOTH LOOPS. ACCOMPLISHED FLIGHT HAND BOOK PROCEDURES. REPLACED FIRE WARNING LOOPS MFG P/N 5958570-1. (M)
- [SDR TWAA9713601](https://openairdocs.org/sdr/TWAA9713601.md): Sensor · worn · Nov 18, 1997 · N953U · Doug DC982 · Landing Gear Position and Warning
  > MCO - FLT 328 - DURING LANDING, THE RIGHT MAIN LANDING GEAR RED LIGHT REMAINED ON WITH GEAR HANDLE IN THE DOWN POSITION. REMOVED AND REPLACED THE WORN RIGHT MAIN GEAR DOWNLOCK SENSOR, MFG 8-337-03, MANUFACTURED BY ELDEC CORPORATION. OPERATIONAL CHECK NORMAL.
- [SDR TWAA9780002](https://openairdocs.org/sdr/TWAA9780002.md): Gland Nuts · loose · Jul 17, 1997 · N953U · Doug DC982 · Cabin Cooling System
  > BOS - FLT 239 - SHORTLY AFTER TAKEOFF, TAIL COMPARTMENT HIGH TEMPERATURE LIGHT ILLUMINATED. RE-TORQUED GLAND NUTS ON CLAMPS ON BOTH HEAT EXCHANGERS. OPS CHECK NORMAL. OP-15 - 3-16-97 - JFK. (X)
- [SDR TWAA9750004](https://openairdocs.org/sdr/TWAA9750004.md): Oil Line · cracked · Apr 18, 1997 · N953U · Doug DC982 · Turbine Engine Oil System
  > ORD - FLT 102 - DURING DESCENT NR 2 ENGINE, S/N 1412, INDICATED LOW OIL QTY. SHUT DOWN ENGINE. REMOVED AND REPLACED CRACKED OIL LINE, MFG P/N 7938314-501. OPERATIONAL CHECK NORMAL. (M)
- [SDR TWAA9615102](https://openairdocs.org/sdr/TWAA9615102.md): Oven · failed · Dec 5, 1996 · N953U · Doug DC982 · Buffet/Galleys
  > STL - FLT 222 - DURING DESCENT, HAD ELECTRICAL ODOR IN AFT CABIN. PULLED CIRCUIT BREAKER FOR AFT GALLEY OVENS. FOUND OVEN, MFG PN 50381, WITH INTERNAL MALFUNCTION. REPLACED OVEN. OVEN OPERATION THEN CHECKED NORMAL. CHECK C-1D - 5-28-96 - JFK. (X)
- [SDR 97ZZZM105](https://openairdocs.org/sdr/97ZZZM105.md): Engine · failed · Sep 27, 1996 · N953U · Doug DC982 · Engine (Turbine/Turboprop)
  > FLT 224 - GJT - DURING CRUISE, NR 1 ENGINE SPOOLED DOWN. AIRCRAFT DIVERTED TO GJT FOR AN ENGINE CHANGE. (M)
- [SDR 96ZZZM1468](https://openairdocs.org/sdr/96ZZZM1468.md): Engine · failed · Sep 27, 1996 · N953U · Doug DC982 · Engine (Turbine/Turboprop)
  > GJT - DURING CRUISE NR 1 ENGINE, S/N 1407, SPOOLED DOWN. AIRCRAFT DIVERTED TO GJT, FOR AN ENGINE CHANGE.
- [SDR 96ZZZM1366](https://openairdocs.org/sdr/96ZZZM1366.md): Oven · smoking · Aug 13, 1996 · N953U · Doug DC982 · Buffet/Galleys
  > JFK - DURING CRUISE, GALLEY OVEN EMITTED SMOKE. SHUT DOWN OVEN. FOUND DEFECTIVE FAN MOTOR. REPLACED OVEN, MFG P/N 5316E. OVEN OPERATION THEN CHECKED NORMAL.
- [SDR 95ZZZW747](https://openairdocs.org/sdr/95ZZZW747.md): Eel Wire · out of position · May 14, 1995 · N953U · Doug DC982 · Emergency Lighting
  > MCI - DURING INVESTIGATION OF EMERGENCY LIGHT PROBLEMS, FOUND RUDDER CABLE B-1 BURNT. FOUND EMERGENCY LIGHT BATTERY PACK WIRE RUBBING ON RUDDER CABLE AT STA 1060. REPLACED RUDDER CABLE AND REPAIRED BATTERY PACK WIRE, CLAMPED WIRE TO CLEAR CABLE. RUDDER OPER

## 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 = 'N953U' AND deregistration_id = 'N953U-2017-07-25'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N953U-2017-07-25/reports

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