N982PS, cancelled May 30, 2013

Service difficulty reports · 43

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

Query with SQL
duckdb -csv -c "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"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR ZW0A0104504Longeron · crackedLONGERON 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.Jul 2, 2001 · N982PS · Doug DC931 · Fuselage Main, Longeron/StringerSDR ZW0A0104503Longeron · crackedLONGERON 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.Jul 2, 2001 · N982PS · Doug DC931 · Fuselage Main, Longeron/StringerSDR ZW0A0104502Longeron · crackedLONGERON 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.Jul 2, 2001 · N982PS · Doug DC931 · Fuselage Main, Longeron/StringerSDR ZW0A0104501Longeron · crackedLONGERON 6R CRACKED AT STATION 639 APROX .25 INCH. REPAIRED LONGERON PER SRM 53-02 FIG 18. LAST CHECK C 5-31-00 STL.Jul 2, 2001 · N982PS · Doug DC931 · Fuselage Main, Longeron/StringerSDR TWAA0017201Fuel Cell · overservicedON 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.Nov 2, 2000 · N982PS · Doug DC931 · Fuel StorageSDR TWAA0011301Battery · dischargedTHE 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.Jul 19, 2000 · N982PS · Doug DC931 · Emergency LightingSDR TWAA0008504Frame · crackedDURING 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.May 27, 2000 · N982PS · Doug DC931 · Fuselage Main, FrameSDR TWAA0008503Skin · gougedDURING 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 BALMay 27, 2000 · N982PS · Doug DC931 · Elevator, Plate/SkinSDR TWAA0008502Frame · crackedDURING 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.May 27, 2000 · N982PS · Doug DC931 · Fuselage Main, FrameSDR TWAA9902706Deck · crackedDURING 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.Feb 16, 1999 · N982PS · Doug DC931 · Fuselage Miscellaneous StructureSDR TWAA9902203Former · crackedDURING OP 16 MAINT CHECK, FOUND AFT ACCESSORY COMPT FORMER FOOT CRACKED AT STA 1059, LONGERON 15L. REPLACED FORMER FOOT PER SPM 6-70-01.Feb 7, 1999 · N982PS · Doug DC931 · Fuselage Main, FrameSDR TWAA9902202Former · crackedDURING 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.Feb 6, 1999 · N982PS · Doug DC931 · Fuselage Main, FrameSDR TWAA9902201Floorbeam · corrodedDURING 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.Feb 3, 1999 · N982PS · Doug DC931 · Fuselage Main, Floor BeamSDR TWAA9902005Skin · dentedDURING 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.Jan 29, 1999 · N982PS · Doug DC931 · Elevator, Plate/SkinSDR TWAA9901902Blkhd Stiffener · crackedDURING 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.Jan 24, 1999 · N982PS · Doug DC931 · Fuselage Main, BulkheadSDR TWAA9901903Blkhd Stiffener · crackedDURING 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.Jan 23, 1999 · N982PS · Doug DC931 · Fuselage Main, BulkheadSDR TWAA9901904Frame · damagedDURING 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.Jan 19, 1999 · N982PS · Doug DC931 · Fuselage Main, FrameSDR TWAA9901107Seat Track · corrodedDURING 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.Jan 19, 1999 · N982PS · Doug DC931 · Fuselage, Seat/Cargo Attach FittingsSDR TWAA9901109Stringer · crackedDURING OP 16 MAINT CHECK, FOUND STRINGER 2L CRACKED AT STA 200. NEW STRINGER INSTALLED FROM STA 148 TO 229, FACTORY SPLICE TO END.Jan 18, 1999 · N982PS · Doug DC931 · Fuselage Main, Longeron/StringerSDR TWAA9901108Stringer · crackedDURING OP 16 MAINT CHECK, FOUND STRINGER 4L CRACKED AT STA 200. NEW STRINGER INSTALLED FROM STA 148 TO 229, FACTORY SPLICE TO END.Jan 18, 1999 · N982PS · Doug DC931 · Fuselage Main, Longeron/StringerSDR TWAA9901006Longeron · crackedFOUND 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.Jan 14, 1999 · N982PS · Doug DC931 · Fuselage Main, Longeron/StringerSDR TWAA9901005Longeron · crackedDURING 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.Jan 14, 1999 · N982PS · Doug DC931 · Fuselage Main, Longeron/StringerSDR TWAA9901004Stringer · crackedDURING 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.Jan 14, 1999 · N982PS · Doug DC931 · Fuselage Main, Longeron/StringerSDR TWAA9900803Web · brokenDURING 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.Jan 12, 1999 · N982PS · Doug DC931 · Fuselage Miscellaneous StructureSDR TWAA9820202Membrane · crackedDURING 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.Dec 23, 1998 · N982PS · Doug DC931 · Fuselage Miscellaneous StructureSDR TWAA9820102Splice · misinstalledDURING 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.Dec 21, 1998 · N982PS · Doug DC931 · Fuselage Miscellaneous StructureSDR TWAA9803203Windshield · shatteredSDF - FLT 697 - FIRST OFFICERS WINDSHIELD SHATTERED INFLIGHT. MADE UNSCHEDULED LANDING AT ADF. REPLACED WINDSHIELD AND HEAT CONTROLLER. (M)Mar 5, 1998 · N982PS · Doug DC931 · Flight Compartment WindowsSDR TWAA9791002Battery Pack · dischargedSTL - 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)Aug 10, 1997 · N982PS · Doug DC931 · Emergency LightingSDR TWAA9788002Battery Pack · dischargedSTL - 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)Aug 1, 1997 · N982PS · Doug DC931 · Emergency LightingSDR TWAA9787001Power Supply · inoperativeDURING 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)Jul 31, 1997 · N982PS · Doug DC931 · Emergency LightingSDR TWAA9786002Power Supply · inoperativeSTL - 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)Jul 30, 1997 · N982PS · Doug DC931 · Emergency LightingSDR TWAA9784004Power Supply · inoperativeSTL - 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)Jul 26, 1997 · N982PS · Doug DC931 · Emergency LightingSDR TWAA9781002Switch · dirtySTL - 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.Jul 21, 1997 · N982PS · Doug DC931 · Emergency LightingSDR TWAA9775005Oil Tube · failedCMH - 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.Jul 5, 1997 · N982PS · Doug DC931 · Turbine Engine Oil SystemSDR TWAA9771004Battery Pack · dischargedSTL - DURING CRUISE EGRESS LIGHTS ILLUMINATED. REPLACED BATTERY PACK. PERFORMED OPERATIONAL TEST OF EGRESS LIGHTS. FOUND NORMAL. (M)Jun 20, 1997 · N982PS · Doug DC931 · Emergency LightingSDR TWAA9764002Battery Pack · dischargedSTL - 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)Jun 6, 1997 · N982PS · Doug DC931 · Emergency LightingSDR TWAA9741004Battery Pack · dischargedSTL - 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)Mar 20, 1997 · N982PS · Doug DC931 · Emergency LightingSDR TWAA9615001Power Supply · failedSTL - 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.Dec 4, 1996 · N982PS · Doug DC931 · Emergency LightingSDR 96ZZZM1534Connector · dirtySTL - 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.Oct 16, 1996 · N982PS · Doug DC931 · Emergency LightingSDR 96ZZZM1210Power Supply · inoperativeSTL - DURING CRUISE, EMERGENCY LIGHTS FLASHED ON AND OFF. REMOVED AND REPLACED POWER SUPPLY, MFG P/N 5822-2. OPERATIONAL CHECK NORMAL.Jul 10, 1996 · N982PS · Doug DC931 · Emergency LightingSDR 96ZZZM1206Battery Pack · dischargedSTL - DURING CRUISE, EMERGENCY EGRESS LIGHT ILLUMINATED. REMOVED AND REPLACED BATTERY PACK, MFG P/N 5822-2. OPERATIONAL CHECK NORMAL. (M)Jul 9, 1996 · N982PS · Doug DC931 · Emergency LightingSDR 95ZZZX3419Actuator · failedSTL - 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.Jul 10, 1995 · N982PS · Doug DC931 · Drag Control ActuatorSDR 95ZZZM307Actuator · failedSTL - 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)Jul 10, 1995 · N982PS · Doug DC931 · Drag Control Actuator
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