Douglas DC-9-32

Service difficulty reports · 12,755

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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 aircraft_model_key = 'DC932'
  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 AT0000459Skin · crackedDURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND CRACK IN FORWARD ENTRY DOOR JAMB. INSTALLED FILLER, DOUBLER, AND TRIPLER IAW DC9 SRM 51-30-03, 51-10-03, AND SR09530252.Sep 11, 2000 · N832AT · Doug DC932 · Fuselage Main, Plate/SkinSDR AT0000445Skin · gougedDURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND VERTICAL STABILIZER RIGHT SKIN GOUGED BEYOND LIMITS. REMOVED AND REPLACED SKIN IAW DC9 SRM 51-10-02, 51-10-04, 51-30-01, 51-30-02, AND 51-30-05.Sep 11, 2000 · N832AT · Doug DC932 · Vertical Stabilizer, Plate/SkinSDR ABXA000448Pan · crackedEDDY CURRENT INSPECTION INDICATED CRACK ON OUTER PAN AT FORWARD STOP AT NR 5 BEAM ON AFT LOWER CARGO DOOR S/N ABX 47380. REPLACED AFT LOWER CARGO DOOR IAW DC9 SRM 52-03.Sep 11, 2000 · N900AX · Doug DC932 · Cargo/Baggage DoorsSDR AT0000405Meter · malfunctionedFOUND ELECTRICAL BURNING SMELL IN COCKPIT AND IN GALLEY AREA. REMOVED AND REPLACED LEFT AND RIGHT DC LOAD METERS.Sep 11, 2000 · N840AT · Doug DC932 · DC Power Distribution SystemSDR ABXA000445Fitting · crackedPYLON BULKHEAD SUPPORT UPPER FITTING WAS CRACKED AT FLOORBEAM 965, BUTT LINE 35 RIGHT. REPLACED FITTING IAW DC9 SRM 51-30-1 AND 51-30-5.Sep 8, 2000 · N900AX · Doug DC932 · Nacelle/Pylon, Attach FittingsSDR ABXA000444Fitting · crackedPYLON BULKHEAD SUPPORT LOWER FITTING WAS CRACKED AT FLOORBEAM 965, BUTT LINE 35 RIGHT. REPLACED FITTING IAW DC9 SRM 51-30-1 AND 51-30-5.Sep 8, 2000 · N900AX · Doug DC932 · Nacelle/Pylon, Attach FittingsSDR ABXA000443Fitting · crackedLEFT LOWER VENTRAL DOOR STOP FITTING WAS CRACKED. REPLACED FITTING IAW DC9 SRM 51-30-2 & 51-30-5.Sep 8, 2000 · N900AX · Doug DC932 · Fuselage Miscellaneous StructureSDR ABXA000442Angle · crackedAFT PRESSURE BULKHEAD RADIAL ATTACH ANGLE WAS CRACKED AT LONGERON 12 LEFT. REPLACED ANGLE IAW DC9 SRM.Sep 8, 2000 · N900AX · Doug DC932 · Fuselage Miscellaneous StructureSDR TWAA0014604Retainer · corrodedDURING OP 15 MAINT CHECK AT STA 996, RBL 0 TO 24 INCHES, THE TOP RT CAM LOCK RETAINER ON AFT SIDE OF BULKHEAD HAD HEAVY CORROSION UNDER IT. CUT OUT CORRODED T ANGLE WEB. SPLICED PER SRM 53-01 PAGE 10. PAINTED PER SRM 51-10-3. MADE WEB REPAIR PER SRM 51-70-Sep 8, 2000 · N931L · Doug DC932 · Fuselage Miscellaneous StructureSDR TWAA0014603Frame · crackedDURING OP 15 MAINT CHECK FORMER CASTING WAS CRACKED AT STA 658, LBL 58 INCHES. REMOVED AND REPLACED WITH NEW CASTING PER DOUGLAS DRAWING 9919615, TWA ARA 17117A, DOUGLAS DRAWING 5918374, AND DOUGLAS DRAWING 5910537.Sep 8, 2000 · N931L · Doug DC932 · Fuselage Main, FrameSDR AT0000404R1Ignition Switch · shortedDURING TAXI SMOKE CAME FROM BEHIND COCKPIT OVERHEAD PANEL. REMOVED AND REPLACED IGNITION SWITCH AND SYSTEM WIRING IAW DC9 MM 30-31-01, 30-41, 33-13, 24-31, 74-00, 73-00, AND 28-22.Sep 7, 2000 · N811AT · Doug DC932 · Ignition SwitchingSDR ABXA000441Frame · crackedFRAME AT STATION 1132 CRACKED IN RADIUS AT APPROX ONE AND ELEVEN O''CLOCK POSITIONS. REPLACED FRAMES IAW DC9 SRM 51-30-1, 51-30-5, AND 51-30-2.Sep 7, 2000 · N900AX · Doug DC932 · Fuselage Main, FrameSDR ABXA000440Frame · crackedCRACK/CORROSION IN FRAME FLANGE AT STATION 1038, RIGHT BUTT LINE 12, JUST AFT OF APU ENCLOSURE. REPLACED T-CAP IAW DC9 SRM 51-30-2 & 51-30-5.Sep 7, 2000 · N900AX · Doug DC932 · Fuselage Main, FrameSDR TWAA0014907Frame · corrodedDURING OP 15 MAINT CHECK, FOUND CORROSION AROUND FORMER FOOT ON MEMBRANE AT STA 408, LONGERON 18R AFT SIDE. REMOVED CORROSION PER SRM 51-10-03. REPLACED FORMER FOOT PER SPM 6-70-01 PAGE 3, PARAGRAPH 1, 2 A, B, C. TREATED PER SRM 51-10-8 PAGE 2 CHAPTER 3 PARSep 7, 2000 · N996Z · Doug DC932 · Fuselage Main, FrameSDR AT0000404Smoke · detectedFOUND SMOKE IN COCKPIT FROM BEHIND OVERHEAD PANEL. TROUBLESHOOTING IN PROGRESS.Sep 7, 2000 · N811AT · Doug DC932 · Electrical Power SystemSDR 0003179605Skin · crackedFUSELAGE EXTERIOR .25 INCH LONG CRACK 9 O''CLOCK POSITION AT NR 2 AFT DOOR STOP ADJUST HOLE. TRIMMED OUTER SKIN, CRACK REMOVED. FABRICATED DOUBLER AND FILLER. REPAIRED PER EA 96-179114 AND SRM 53-05 FIG 114. LOGPAGE 1491024.Sep 7, 2000 · N605NW · Doug DC932 · Fuselage Main, Plate/SkinSDR TWAA0013902Wire · damagedTHE FIRST CLASS CABIN EGRESS LIGHTS DID NOT ILLUMINATE WHEN SWITCH PLACED IN THE TEST POSITION. SPLICED THE LIGHT CABLE AT THE SIDE WALL, ROW 2. CHECK-C 1-12-00 STL.Sep 7, 2000 · N924L · Doug DC932 · Light System WiringSDR MWEA00778Bracket · crackedMKE - FOUND CABIN FLOOR SUPPORT BRACKET AT FS 680 AND BELOW SEAT TRACK NR 4 IS CRACKED. REMOVED, FABRICATED, DRILLED AND INSTALLED NEW BRACKET. (M)Sep 6, 2000 · N302ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA00779Rib · damagedMKE - FOUND LEFT ELEVATOR HAS TOOLMARKS ON 21ST LEADING EDGE RIB, INBOARD SIDE, UPPER FLANGE. REMOVED RIB, LOCATED, DRILLED, AND INSTLALED NEW RIB. (M)Sep 6, 2000 · N302ME · Doug DC932 · Elevator, Spar/RibSDR MWEA00780Rib · misdrilledMKE - FOUND LEFT ELEVATOR HAD A MISDRILLED HOLE IN THE 26TH LEADING EDGE RIB. REMOVED RIB AND ANGLE. FABRICATED ANGLE, LOCATED, DRILLED NEW RIB AND ANGLE. INSTALLED BOTH. (M)Sep 6, 2000 · N302ME · Doug DC932 · Elevator, Spar/RibSDR MWEA00782Web · crackedMKE - FOUND CRACKED SUB FLOOR OUTBOARD OF NR 4 SEAT TRACK AT FS 965. STOP DRILLED CRACK, FABRICATED DOUBLER, AND INSTALLED. (M)Sep 6, 2000 · N302ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA00775Shear Tie · crackedMKE - FOUND SHEAR TIE CRACKED AT FRAME FS 977, LONGERON R14. REMOVED AND FABRICATED NEW SHEAR TIE. LOCATED, DRILLED, AND INSTALLED. (M)Sep 6, 2000 · N302ME · Doug DC932 · Fuselage Main, StructureSDR MWEA00776Intercostal · corrodedMKE - FOUND CORROSION ON INTERCOSTAL BETWEEN FS 980 AND 996 AND LONGERON 27-28 RT. REMOVE INTERCOSTAL, SUPPORT STRAP AND BRACKET. FABRICATED INTERCOSTAL AND BRACKET. LOCATED, DRILLED, AND INSTALLED PARTS. (M)Sep 6, 2000 · N302ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA00777Shear Tie · misinstalledMKE - FOUND SHEAR TIE AT FS 908 HAD TWO EACH INSTALLED RIVETS WITH NO EDGE DISTANCE AT LONGERON R8. REMOVED, FABRICATED NEW SHEAR TIE SECTION AND SPLICE, LOCATED, DRILLED, AND INSTALLED. (M)Sep 6, 2000 · N302ME · Doug DC932 · Fuselage Main, StructureSDR MWEA00783Rudder · restrictedMKE - FLT 3 - DURING TAXI CHECK OF FLIGHT CONTROLS, THE RUDDER TRAVEL FELT RESTRICTED IN BOTH DIRECTIONS. MAINTENANCE COULD NOT DUPLICATE THIS DISCREPANCY. PERFORMED INSPECTION AND CHECK. (X)Sep 6, 2000 · N203ME · Doug DC932 · Rudder Control SystemSDR AT0000431Skin · dentedFOUND DENT AT BS 484. CUT OUT DENTED AREA, FABRICATED REPAIR FILLER, INTERNAL DOUBLER, AND INSTALLED IAW DC9 SRM 53-04 FIGURE 12C.Sep 6, 2000 · N805AT · Doug DC932 · Fuselage Main, Plate/SkinSDR ABXA000439Support Bracket · crackedAUX TANK VERTICAL SUPPORT WAS CRACKED AND CORRODED AROUND 3 NUT PLATES, STA 511, LEFT BUTT LINE 35. INSTALLED NEW VERTICAL SUPPORT ANGLE IAW DC9 SRM 51-30-1.Sep 6, 2000 · N900AX · Doug DC932 · Fuselage Miscellaneous StructureSDR ABXA000438Floorbeam · corrodedEXFOLIATION CORROSION ON FLOORBEAM TOP FLANGE AT BLIND RIVET AT STATION 465, RIGHT BUTT LINE 44. REPAIRED FLOORBEAM IAW DC9 SRM 53-05.Sep 6, 2000 · N900AX · Doug DC932 · Fuselage Main, Floor BeamSDR ABXA000437Vane · crackedRIGHT AFT MOVABLE VANE LOWER SKIN WAS CRACKED ON THE INBOARD AFT CORNER AND CURLED UP ON THE OUTER END. REPLACED VANE IAW DC9 MM.Sep 6, 2000 · N900AX · Doug DC932 · Trailing Edge FlapsSDR TWAA0014304Spar · crackedDURING OP 15 MAINT CHECK ON THE RT WING HAD A CRACK INDICATION ON REAR SPAR AT TOP HOLE FOR CENTER FLAP HINGE MOUNT AT STA XW251. REPAIRED HOLE PER DOUGLAS DRAWING JO6022.Sep 6, 2000 · N931L · Doug DC932 · Wing SparSDR TWAA0014303Angle · crackedDURING OP 15 MAINT CHECK, THE FUSELAGE TO WING TIE ANGLE WAS CRACKED AT STA 605, BETWEEN LONGERON 22L AND 23L. REPLACED WING TO FUSELAGE TIE ANGLE PER DOUGLAS DRAWING 5910068.Sep 6, 2000 · N931L · Doug DC932 · Fuselage Miscellaneous StructureSDR ABXA000436Attach Angle · crackedNR 2 ENGINE PYLON SUPPORT ANGLE CRACKED AT STA YN 156. REPAIRED CRACK IAW DC9 SRM DWG K05159.Sep 5, 2000 · N900AX · Doug DC932 · Nacelle/Pylon, Attach FittingsSDR 0003199613Skin · corrodedNUMEROUS AREAS OF CORROSION ON LEFT AND RIGHT WINGS. REPAIRED BY BLENDING, DOUBLERS, AND FASTENER REPLACEMENT. REPAIRED PER SRM 53-04 AND EA''S 96-178021, 96-178129, REFERENCE LOG PAGES DURING THE MONTH OF AUGUST 2000.Sep 4, 2000 · N613NW · Doug DC932 · Wing, Plate/SkinSDR TWAA0014906Skin · damagedDURING OP 15 MAINT CHECK ON RT WING T/E FLAP FOUND CORNER DAMAGED AT O/B END OF T/E. REPAIRED PER SRM 57-09, 51-70-1, 57-03 PAGE 7, AND 51-90-0 PARAGRAPH 6-1 PAGES 23 TO 25.Sep 4, 2000 · N996Z · Doug DC932 · Trailing Edge FlapsSDR CA001019029Bolt · missing(CAN) DURING WALK AROUND INSPECTION OF AIRCRAFT, LEFT HAND NOSE LANDING GEAR WHEEL ASSEMBLY, FOUND WITH ONE TIE BOLT MISSING. (TIE BOLT ATTACHES HUB HALVES TOGETHER) SUSPECT TIE BOLT CRACKED AND SEPARATED FROM WHEEL HUB. TIRE ASSEMBLY REPLACED AS PER MAINTENANSep 3, 2000 · Doug DC932 · Wheel/Ski/FloatSDR 0003279984Fuel Control · inoperativeDURING CLIMBOUT FROM MSP, THE RIGHT ENGINE EXPERIENCED SURGES AND FLUCUATING ENGINE PARAMETER READINGS. THE FLIGHT CREW FOLLOWED COM PROCEDURES, RETURNED TO MSP, AND LANDED WITHOUT INCIDENT. AN EMERGENCY WAS DECLARED ON APPROACH TO LANDING DUE TO RIGHT ENGINSep 3, 2000 · N984US · Doug DC932 · Fuel Control/Turbine EnginesSDR MWEA00774Computer · inoperativeFLT 306 - MKE - AT ROTATION, STALL WARNING ILLUMINATED, STICK SHAKER CAME ON, GLARESHIELD LIGHTS ILLUMINATED. WENT OFF AT TOUCHDOWN, CONFIGURATION CHANGE MADE NO DIFFERENCE. REMOVED AND REPLACED NR 1 AND NR 2 STALL WARNING COMPUTERS, S/N''S 842 AND 1410A. (Sep 2, 2000 · N301ME · Doug DC932 · Stall Warning SystemSDR MWEA00773Audio Panel · inoperativeMKE - FLT 270 - NR 1 AUDIO PANEL WOULD NOT ALLOW ANY AUDIO VIA SPEAKER OR HEAD PHONE ON NR 1 COMM. REMOVED AND REPLACED NR 1 AUDIO PANEL BECAUSE OF INOPERATIVE NR 1 VHF AUDIO SELECT SWITCH. (M)Sep 2, 2000 · N202ME · Doug DC932 · Data Transmission Auto CallSDR MWEA00781Smoke · detectedDFW - FLT 310 - SMOKE NOTED IN CABIN. INSPECTED APU AREA FOR LEAKS, NONE FOUND. POWERED UP AIRCRAFT, FOUND RIGHT AIR CONDITIONED PACK SWITCH ON IN AUTO WITH AN EXTERNAL AIR CONDITION UNIT PLUGGED INTO AIRCRAFT. NO SMOKE NOTED AFTER DISCONNECTING EXTERNAL AISep 1, 2000 · N206ME · Doug DC932 · Air Distribution SystemSDR ABXA000435Fitting · crackedFITTING (P/N 5912979-2) AT STA 604 BETWEEN LONGERON 23 RT AND LONGERON 22 RT CRACKED AT INBOARD BOLT HOLE. REPLACED FITTING IAW DC9 SRM 51-10-4 AND 51-30-1.Sep 1, 2000 · N900AX · Doug DC932 · Fuselage Miscellaneous StructureSDR TWAA0014905Skin · crackedDURING OP 15 MAINT CHECK, FOUND CRACK AT FWD ENTRY DOOR CUTOUT AT NUMBER 3 AFT STOP. REPAIRED PER SRM 53-05, FIG 114.Sep 1, 2000 · N996Z · Doug DC932 · Fuselage Main, Plate/SkinSDR TWAA0014307Spar · crackedDURING OP 15 MAINT CHECK, FOUND ON RT WING A CRACK APPROX .0625 INCH LONG ON REAR SPAR AT XW154, I/B FLAP HINGE LOWER O/B HOLE. CRACK CONTAINED PER NDT TWA 51-10-03 PART 6 HFEC. MADE REPAIR DOUBLER AND INSTALLED PER REPAIR DRAWING JO60271. REPAIR WORK IN COSep 1, 2000 · N931L · Doug DC932 · Wing SparSDR MWEA00771Intercostal · crackedMKE - FOUND INTERCOSTAL CRACKED AT FRAME STATION 945 LONGERON LEFT 6. REMOVED AND REPLACED INTERCOSTAL. (M)Aug 31, 2000 · N302ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA00770Intercostal · crackedMKE - FOUND INTERCOSTAL CRACKED BETWEEN STATION 294 TO 275 ON LEFT SIDE OF LONGERON NR 1. REMOVED AND REPLACED INTERCOSTAL. (M)Aug 31, 2000 · N302ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA00769Intercostal · misinstalledMKE - FOUND 9 OPEN HOLES IN INTERCOSTAL AT STATION 659-665 LONGERON 8 RIGHT. REMOVED AND REPLACED INTERCOSTAL. (M)Aug 31, 2000 · N302ME · Doug DC932 · Fuselage Miscellaneous StructureSDR ABXA000403Window · stuckCAPTAIN''''S CLEARVIEW WINDOW WILL NOT OPEN. FOUND WINDOW LINKAGE STICKING. OPERATED WINDOW SEVERAL TIMES. WINDOW OPENS NORMALLY AT THIS TIME.Aug 31, 2000 · N901AX · Doug DC932 · Flight Compartment WindowsSDR AT0000494Skin · crackedFOUND 2 EA CRACKS IN FUSELAGE UPPER NOSE SKIN. CUT OUT CRACKED AREA AND INSTALLED REPAIR DOUBLERS. IAW EO 12-5330-29-B1048, AD 96-11-11, SB 53-262AND DC9 SRM 53-31-0, 51-10-3, 51-30-01, 51-30-02Aug 30, 2000 · N805AT · Doug DC932 · Fuselage Main, Plate/SkinSDR MWEA00592Frame · tool damageMKE - TOOL MARK ON FRAME AT STATION 945 LONGERON LEFT 12. FABRICATED AND INSTALLED REPAIR PLATE, FILLER, ANGLE. (M)Aug 30, 2000 · N502ME · Doug DC932 · Fuselage Main, FrameSDR AT0000434Angle · corrodedFOUND CORROSION AT BS 120 ON LONGERON 28R AND BS 130 LONGERON 28 AT BAY DOOR LOCKING INDICATOR. REMOVED 1 T-ANGLE, 1 SUPPORT, FABRICATED NEW SUPPORT AND INSTALLED IAW DCI SRM 51-30-2.Aug 30, 2000 · N805AT · Doug DC932 · Fuselage Miscellaneous StructureSDR TWAA0014305Galley Track · corrodedDURING OP 15 MAINT CHECK, FOUND GALLEY TRACK NUMBER 1 AT STA 237 TO 247, LBL 44 INCHES, WAS CORRODED. REPLACED TRACK FROM STA 200 TO 301. INSTALLED SPLICE PER SRM 53-05 FIG 4F.Aug 30, 2000 · N931L · Doug DC932 · Fuselage, Seat/Cargo Attach Fittings
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