# Service difficulty reports: N982PS, cancelled May 30, 2013

A list on [N982PS, cancelled May 30, 2013](https://openairdocs.org/deregistered/N982PS-2013-05-30.md).

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

- [SDR ZW0A0104504](https://openairdocs.org/sdr/ZW0A0104504.md): Longeron · cracked · Jul 2, 2001 · N982PS · Doug DC931 · Fuselage Main, Longeron/Stringer
  > LONGERON 5R AT STA 680 WAS CRACKED APPROX.25 INCH. REMOVED DAMAGED LONGERON 5R SECTION. REPLACED WITH P/N 2777922-4 PER SRM 53-02 FIG 18. CHECK-C 5-31-00 STL.
- [SDR ZW0A0104503](https://openairdocs.org/sdr/ZW0A0104503.md): Longeron · cracked · Jul 2, 2001 · N982PS · Doug DC931 · Fuselage Main, Longeron/Stringer
  > LONGERON 5R AT STA 699 WAS CRACKED APPROX.5 INCH. REMOVED DAMAGED LONGERON 5R AND REPLACED WITH P/N 2777922-4 PER SRM 53-02 FIG 18. CHECK-C 5-31-00 STL.
- [SDR ZW0A0104502](https://openairdocs.org/sdr/ZW0A0104502.md): Longeron · cracked · Jul 2, 2001 · N982PS · Doug DC931 · Fuselage Main, Longeron/Stringer
  > LONGERON 5R AT STATION 639 CRACKED APPROX.5 INCH. REMOVED DAMAGED LONGERON SECTION. REPLACED WITH DACO P/N 2777922-4 PER SRM 53-02 FIG 18. LAST CHECK C 5-31-00 STL.
- [SDR ZW0A0104501](https://openairdocs.org/sdr/ZW0A0104501.md): Longeron · cracked · Jul 2, 2001 · N982PS · Doug DC931 · Fuselage Main, Longeron/Stringer
  > LONGERON 6R CRACKED AT STATION 639 APROX.25 INCH. REPAIRED LONGERON PER SRM 53-02 FIG 18. LAST CHECK C 5-31-00 STL.
- [SDR TWAA0017201](https://openairdocs.org/sdr/TWAA0017201.md): Fuel Cell · overserviced · Nov 2, 2000 · N982PS · Doug DC931 · Fuel Storage
  > ON TAKEOFF FUEL WAS SEEN VENTING FROM THE RIGHT WING. FLIGHT RETURNED TO STL. FOUND EXCESS FUEL IN LT WING WHICH FILLED THE VENT BOX, AND THE VENT BOX EMPTIED ON TAKEOFF. DURING LATER CHECK FOUND A CHECK VALVE BYPASSING SOME FUEL FROM THE CENTER TO LT TANK.
- [SDR TWAA0011301](https://openairdocs.org/sdr/TWAA0011301.md): Battery · discharged · Jul 19, 2000 · N982PS · Doug DC931 · Emergency Lighting
  > THE EMERGENCY EXIT LIGHTS AT THE MOST FORWARD LT SIDE AND RT SIDE CABIN DOORS ILLUMINATED INTERMITTENTLY WITH THE SWITCH IN THE ARMED POSITION. REPLACED THE FWD EMERGENCY LIGHT BATTERY PACK. CHECK-C 5-31-00 STL.
- [SDR TWAA0008504](https://openairdocs.org/sdr/TWAA0008504.md): Frame · cracked · May 27, 2000 · N982PS · Doug DC931 · Fuselage Main, Frame
  > DURING CHECK-C, FOUND BELTING FRAME ABOVE STATION 408 CRACKED AT LONGERON 17 RT (TWO.375 INCH CRACKS). CUT OUT BELT RING AND REPAIRED PER SRM 5-3-03 FIG 32 AND ELMR 70752. CHECK-C 05-27-00 STL.
- [SDR TWAA0008503](https://openairdocs.org/sdr/TWAA0008503.md): Skin · gouged · May 27, 2000 · N982PS · Doug DC931 · Elevator, Plate/Skin
  > DURING OP-9, FOUND RT ELEVATOR GOUGED APPROXIMATELY.125 INCH DEEP AND.25 INCH LONG ON THE UPPER SURFACE APPROXIMATELY 51 INCHES O/B FROM THE CENTERLINE. MADE A DOUBLER REPAIR PER DC9 SRM 55-01 FIG 2. BALANCED CALCULATED METHOD PER DC9 SRM 55-20-1. NEW BAL
- [SDR TWAA0008502](https://openairdocs.org/sdr/TWAA0008502.md): Frame · cracked · May 27, 2000 · N982PS · Doug DC931 · Fuselage Main, Frame
  > DURING CHECK-C, FOUND BELT RING FRAME STATION 389 CRACKED AT LONGERON 17R.375 INCH CRACK. CUT OUT BELT RING AND REPAIRED PER SRM 53-03-FIG 32 AND ELMR 70752. CHECK-C 05-27-00 STL.
- [SDR TWAA9902706](https://openairdocs.org/sdr/TWAA9902706.md): Deck · cracked · Feb 16, 1999 · N982PS · Doug DC931 · Fuselage Miscellaneous Structure
  > DURING OP 16 MAINT CHECK, FOUND UPPER PRESSURE DECK AT APPROXIMATELY STA 47.8 WITH A CRACK ABOUT 4 INCHES LONG. CONFIRMED WITH EDDY CURRENT. REPLACED Y ANGLE PER SPM 6-70-01, DRAWING 9911500, AND SRM 51-60-0, PAGE 27 ITEM E.
- [SDR TWAA9902203](https://openairdocs.org/sdr/TWAA9902203.md): Former · cracked · Feb 7, 1999 · N982PS · Doug DC931 · Fuselage Main, Frame
  > DURING OP 16 MAINT CHECK, FOUND AFT ACCESSORY COMPT FORMER FOOT CRACKED AT STA 1059, LONGERON 15L. REPLACED FORMER FOOT PER SPM 6-70-01.
- [SDR TWAA9902202](https://openairdocs.org/sdr/TWAA9902202.md): Former · cracked · Feb 6, 1999 · N982PS · Doug DC931 · Fuselage Main, Frame
  > DURING OP 16 MAINT CHECK, FOUND CRACK IN AFT SIDE OF FORMER RING, STA 1087, LBL 10 IN. INSTALLED NEW FORMER RING FOOT PER STD PROCESS MANUAL 6-70-01.
- [SDR TWAA9902201](https://openairdocs.org/sdr/TWAA9902201.md): Floorbeam · corroded · Feb 3, 1999 · N982PS · Doug DC931 · Fuselage Main, Floor Beam
  > DURING OP 16 MAINT CHECK, FOUND SURFACE CORROSION ON FLOORBEAM AT STA 218 TO 237, BL 0. MECHANICALLY REMOVED CORROSION PER TWA STD PROCESS MANUAL. REPAIRED MEMBER PER SRM 53-01, PAGE 10.
- [SDR TWAA9902005](https://openairdocs.org/sdr/TWAA9902005.md): Skin · dented · Jan 29, 1999 · N982PS · Doug DC931 · Elevator, Plate/Skin
  > DURING OP 16 MAINT CHECK, FOUND DENT IN LEADING EDGE OF RT ELEVATOR, APPROXIMATELY 2.25 BY 2.5 INCH AND 0.180 INCH DEEP, LOCATED JUST O/B OF ELEVATOR DAMPER. REPLACED DAMAGED PANEL PER SPM 6-70-01.
- [SDR TWAA9901902](https://openairdocs.org/sdr/TWAA9901902.md): Blkhd Stiffener · cracked · Jan 24, 1999 · N982PS · Doug DC931 · Fuselage Main, Bulkhead
  > DURING OP 16 MAINT CHECK, FOUND IN AFT CARGO COMPT THE FWD PRESSURE BULKHEAD STIFFENER CRACKED IN CENTER APPROXIMATELY 1.5 INCH LOCATED 18.5 INCHES FROM BOTTOM OF BULKHEAD. REMOVED CRACKED STIFFENER AND INSTALLED NEW STIFFENER WITH HI-LOKS PER SRM 51-60-0.
- [SDR TWAA9901903](https://openairdocs.org/sdr/TWAA9901903.md): Blkhd Stiffener · cracked · Jan 23, 1999 · N982PS · Doug DC931 · Fuselage Main, Bulkhead
  > DURING OP 16 MAINT CHECK, IN AFT CARGO COMPT THE FWD PRESSURE BULKHEAD STIFFENER WAS CRACKED IN CENTER 26.5 INCHES FROM BOTTOM OF PRESSURE BULKHEAD. REMOVED CRACKED STIFFENER AND INSTALLED NEW STIFFENER WITH HI-LOKS PER SRM 51-60-0.
- [SDR TWAA9901904](https://openairdocs.org/sdr/TWAA9901904.md): Frame · damaged · Jan 19, 1999 · N982PS · Doug DC931 · Fuselage Main, Frame
  > DURING OP 16 MAINT CHECK, FOUND STA 980 FORMER PREVIOUSLY REPAIRED AT STRINGER 17R. REPAIRED FORMER PER SRM 53-03, PAGE 131 TO 132, SHEET 2, AND PAGE 133 SHEET 3, AND PAGES 135 AND 137.
- [SDR TWAA9901107](https://openairdocs.org/sdr/TWAA9901107.md): Seat Track · corroded · Jan 19, 1999 · N982PS · Doug DC931 · Fuselage, Seat/Cargo Attach Fittings
  > DURING OP 15 MAINT CHECK, FOUND CORROSION ON CHAIR TRACK AT STA 200 TO 237, RBL 22. REPLACED SEAT TRACK AT PREVIOUS SPLICE REPAIR WITH (P/N 5910820-3) PER SRM 53-05 FIG F.
- [SDR TWAA9901109](https://openairdocs.org/sdr/TWAA9901109.md): Stringer · cracked · Jan 18, 1999 · N982PS · Doug DC931 · Fuselage Main, Longeron/Stringer
  > DURING OP 16 MAINT CHECK, FOUND STRINGER 2L CRACKED AT STA 200. NEW STRINGER INSTALLED FROM STA 148 TO 229, FACTORY SPLICE TO END.
- [SDR TWAA9901108](https://openairdocs.org/sdr/TWAA9901108.md): Stringer · cracked · Jan 18, 1999 · N982PS · Doug DC931 · Fuselage Main, Longeron/Stringer
  > DURING OP 16 MAINT CHECK, FOUND STRINGER 4L CRACKED AT STA 200. NEW STRINGER INSTALLED FROM STA 148 TO 229, FACTORY SPLICE TO END.
- [SDR TWAA9901006](https://openairdocs.org/sdr/TWAA9901006.md): Longeron · cracked · Jan 14, 1999 · N982PS · Doug DC931 · Fuselage Main, Longeron/Stringer
  > FOUND LONGERON 6L CRACKED AT STA 658L AT FORMER TIE. CONFIRMED BY NTD. REMOVED DAMAGED SECTION AND REPLACED. SPLICED PER SRM 53-02, PG 48 FIG 18 AND PAGE 51.
- [SDR TWAA9901005](https://openairdocs.org/sdr/TWAA9901005.md): Longeron · cracked · Jan 14, 1999 · N982PS · Doug DC931 · Fuselage Main, Longeron/Stringer
  > DURING OP 16 MAINT CHECK, FOUND LONGERON 7L CRACKED AT STA 658L FORMER TIE. CONFIRMED BY NDT. REMOVED DAMAGED SECTION AND SPLICED IN NEW PER SRM 53-02, PG 48 FIG 18 AND PAGE 51.
- [SDR TWAA9901004](https://openairdocs.org/sdr/TWAA9901004.md): Stringer · cracked · Jan 14, 1999 · N982PS · Doug DC931 · Fuselage Main, Longeron/Stringer
  > DURING OP 16 MAINT CHECK, FOUND STRINGER 5L CRACKED ON BOTH SIDES OF FORMER STA 718. INSTALLED NEW STRINGER PIECE AND SPLICED PER SRM 53-02, FIG 18 PG 1.
- [SDR TWAA9900803](https://openairdocs.org/sdr/TWAA9900803.md): Web · broken · Jan 12, 1999 · N982PS · Doug DC931 · Fuselage Miscellaneous Structure
  > DURING OP 16 MAINT CHECK, FOUND MEMBRANE BELOW FLOOR PANEL BROKEN AT STA 959, LT SIDE OUTBOARD OF OUTBOARD CHAIR TRACK. INSTALLED WEB REPAIR PER SRM 53-01.
- [SDR TWAA9820202](https://openairdocs.org/sdr/TWAA9820202.md): Membrane · cracked · Dec 23, 1998 · N982PS · Doug DC931 · Fuselage Miscellaneous Structure
  > DURING OP 16 MAINT CHECK, FOUND CABIN MEMBRANE CRACKED APPROXIMATELY.75 INCH AT STA 984 RT SIDE. STOP DRILLED CRACK 0.250 HOLE. FABRICATED DOUBLER AND INSTALLED FASTENERS TYPICAL WEB REPAIR SRM 53-01 PG 3.
- [SDR TWAA9820102](https://openairdocs.org/sdr/TWAA9820102.md): Splice · misinstalled · Dec 21, 1998 · N982PS · Doug DC931 · Fuselage Miscellaneous Structure
  > DURING OP 16 MAINT CHECK, FOUND SPLICE ON FORMER NOT PER SRM AT STR 18L, STA 980. REMOVED OLD REPAIR AND INSTALLED NEW REPAIR PER SRM 53--03, FIG 32 SHEET 4 AND 5, PAGE 135 AND 136.
- [SDR TWAA9803203](https://openairdocs.org/sdr/TWAA9803203.md): Windshield · shattered · Mar 5, 1998 · N982PS · Doug DC931 · Flight Compartment Windows
  > SDF - FLT 697 - FIRST OFFICERS WINDSHIELD SHATTERED INFLIGHT. MADE UNSCHEDULED LANDING AT ADF. REPLACED WINDSHIELD AND HEAT CONTROLLER. (M)
- [SDR TWAA9791002](https://openairdocs.org/sdr/TWAA9791002.md): Battery Pack · discharged · Aug 10, 1997 · N982PS · Doug DC931 · Emergency Lighting
  > STL - FLT 10 - DURING LANDING, THE EMERGENCY FLOOR LIGHTING ILLUMINATED INTERMITTENTLY. REMOVED AND REPLACED BATTERY PACK, MFG P/N 5822-2, MANUFACTURED BY LUMINESCENT SYSTEMS INC. OPERATIONAL CHECK NORMAL. (M)
- [SDR TWAA9788002](https://openairdocs.org/sdr/TWAA9788002.md): Battery Pack · discharged · Aug 1, 1997 · N982PS · Doug DC931 · Emergency Lighting
  > STL - FLT 627 - EGRESS LIGHT ON INTERMITTENTLY IN AFT CABIN. REMOVED AND REPLACED BATTERY PACK MFG PN 5822-2, MANUFACTURED BY LUMINESCENT SYSTEMS INS. OPERATIONAL CHECK NORMAL. CHECK C 1-22-97 STL. (M)
- [SDR TWAA9787001](https://openairdocs.org/sdr/TWAA9787001.md): Power Supply · inoperative · Jul 31, 1997 · N982PS · Doug DC931 · Emergency Lighting
  > DURING CRUISE, THE EMERGENCY LIGHTS ILLUMINATED INTERMITTENTLY. REMOVED AND REPLACED POWER SUPPLY, MFG P/N 5822-2 MANUFACTURED BY LUMINESCENT SYSTEMS, INC CHECK C-1/22/97 STL. OPERATIONAL CHECK NORMAL. (M)
- [SDR TWAA9786002](https://openairdocs.org/sdr/TWAA9786002.md): Power Supply · inoperative · Jul 30, 1997 · N982PS · Doug DC931 · Emergency Lighting
  > STL - FLT 120 - DURING CRUISE, EGRESS LIGHT ILLUMINATED INTERMITTENTLY. REMOVED AND REPLACED POWER SUPPLY, MFG PN 5822-22, MANUFACTURED BY LUMINESCENT SYSTEMS, INC. OPS CHECK NORMAL. CHECK C - 1-22-97 - STL. (X)
- [SDR TWAA9784004](https://openairdocs.org/sdr/TWAA9784004.md): Power Supply · inoperative · Jul 26, 1997 · N982PS · Doug DC931 · Emergency Lighting
  > STL - FLT 338 - DURING CRUISE, EMERGENCY LIGHTS ILLUMINATED AT ROWS 19-22. REMOVED AND REPLACED POWER SUPPLY, MFG P/N 5822-2, MANUFACTURED BY LUMINESCENT SYSTEMS, INC. OPS CHECK NORMAL. CHECK C - 1-22-97 - STL. (X)
- [SDR TWAA9781002](https://openairdocs.org/sdr/TWAA9781002.md): Switch · dirty · Jul 21, 1997 · N982PS · Doug DC931 · Emergency Lighting
  > STL - FLT 568 - DURING PRE-FLIGHT EMERGENCY, LIGHTS AT ROWS 19-22 STAYED ON WITH SWITCH IN ARM POSITION. CYCLED ARM SWITCH, OPERATIONAL CHECK NORMAL. CHECK C - 1-22-97 - STL.
- [SDR TWAA9775005](https://openairdocs.org/sdr/TWAA9775005.md): Oil Tube · failed · Jul 5, 1997 · N982PS · Doug DC931 · Turbine Engine Oil System
  > CMH - FLT 677 - DURING CRUISE, LEFT ENGINE, SN 2151, LOST OIL PRESSURE AND OIL QUANTITY. ENGINE WAS SHUT DOWN IN-FLIGHT. CHANGED NR 6 BEARING TUBE. ENGINE RUN AND LEAK CHECK NORMAL. CHECK C - 1-22-97 - STL. ENGINE TOTAL TIME: 46,086 HOURS; 46,086 CYCLES.
- [SDR TWAA9771004](https://openairdocs.org/sdr/TWAA9771004.md): Battery Pack · discharged · Jun 20, 1997 · N982PS · Doug DC931 · Emergency Lighting
  > STL - DURING CRUISE EGRESS LIGHTS ILLUMINATED. REPLACED BATTERY PACK. PERFORMED OPERATIONAL TEST OF EGRESS LIGHTS. FOUND NORMAL. (M)
- [SDR TWAA9764002](https://openairdocs.org/sdr/TWAA9764002.md): Battery Pack · discharged · Jun 6, 1997 · N982PS · Doug DC931 · Emergency Lighting
  > STL - DURING CRUISE, EMERGENCY EGRESS LIGHTS ILLUMINATED. REMOVED AND REPLACED BATTERY PACK, MFG P/N 5822-2, MANUFACTURED BY LUMINESCENT SYSTEMS, INC. OPERATIONAL CHECK NORMAL. (M)
- [SDR TWAA9741004](https://openairdocs.org/sdr/TWAA9741004.md): Battery Pack · discharged · Mar 20, 1997 · N982PS · Doug DC931 · Emergency Lighting
  > STL - FLT 389 - DURING CRUISE, EGRESS LIGHTS AFT OF OVERWING EXITS ILLUMINATED. REPLACED BATTERY PACK, MFG PN 2013-1A. OPERATIONAL TEST OF EGRESS LIGHTS NORMAL. CHECK C - 1-22-97 - STL. (X)
- [SDR TWAA9615001](https://openairdocs.org/sdr/TWAA9615001.md): Power Supply · failed · Dec 4, 1996 · N982PS · Doug DC931 · Emergency Lighting
  > STL - FLT 517 - DURING CRUISE, EGRESS LIGHTS ILLUMINATED AT SEAT ROWS 1 TO 7. FOUND FAULTY POWER SUPPLY, MFG PN 5822-2. REPLACED POWER SUPPLY. EGRESS LIGHT OPERATION THEN CHECKED NORMAL. CHECK C - 11-13-95 - STL.
- [SDR 96ZZZM1534](https://openairdocs.org/sdr/96ZZZM1534.md): Connector · dirty · Oct 16, 1996 · N982PS · Doug DC931 · Emergency Lighting
  > STL - DURING APPROACH EGRESS LIGHTS IN AFT CABIN WOULD INTERMITTENTLY ILLUMINATE. FOUND DIRTY FLEX CABLE CONNECTOR, MFG P/N 5853-1. CLEANED CABLE CONNECTOR AND SECURED CONNECTOR. EGRESS LIGHT SYSTEM OPERATION CHECKED NORMAL.
- [SDR 96ZZZM1210](https://openairdocs.org/sdr/96ZZZM1210.md): Power Supply · inoperative · Jul 10, 1996 · N982PS · Doug DC931 · Emergency Lighting
  > STL - DURING CRUISE, EMERGENCY LIGHTS FLASHED ON AND OFF. REMOVED AND REPLACED POWER SUPPLY, MFG P/N 5822-2. OPERATIONAL CHECK NORMAL.
- [SDR 96ZZZM1206](https://openairdocs.org/sdr/96ZZZM1206.md): Battery Pack · discharged · Jul 9, 1996 · N982PS · Doug DC931 · Emergency Lighting
  > STL - DURING CRUISE, EMERGENCY EGRESS LIGHT ILLUMINATED. REMOVED AND REPLACED BATTERY PACK, MFG P/N 5822-2. OPERATIONAL CHECK NORMAL. (M)
- [SDR 95ZZZX3419](https://openairdocs.org/sdr/95ZZZX3419.md): Actuator · failed · Jul 10, 1995 · N982PS · Doug DC931 · Drag Control Actuator
  > STL - FLT 651 - DURING LANDING, SMOKE APPEARED IN COCKPIT. FOUND AUTO GROUND SPOILER ACTUATOR, MFG PN 1040T100-5, HAD OVERHEATED CAUSING SMOKE. REPLACED AUTO GROUND SPOILER ACTUATOR AND OPERATION CHECKED NORMAL. CHECK C - 8-16-94 - STL.
- [SDR 95ZZZM307](https://openairdocs.org/sdr/95ZZZM307.md): Actuator · failed · Jul 10, 1995 · N982PS · Doug DC931 · Drag Control Actuator
  > STL - DURING LANDING, SMOKE APPEARED IN COCKPIT. FOUND AUTO GROUND SPOILER ACTUATOR, MFG P/N 1040T100-5, HAD OVERHEATED CAUSING SMOKE. REPLACED AUTO GROUND SPOILER ACTUATOR AND OPERATION CHECKED NORMAL. (M)

## 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 = 'N982PS' AND deregistration_id = 'N982PS-2013-05-30'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N982PS-2013-05-30/reports

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