Douglas DC-9-32

Service difficulty reports · 12,755

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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 MWEA95121Girt Bar Latch · dirtyPILOT REPORTS GIRT BAR ON GALLEY SERVICE DOOR SLIDE HARD TO OPERATE. CLEANED AND LUBED GIRT BAR RELEASE. OPS CHECK GOOD. RETURNED A/C TO SERVICE.Jan 31, 1995 · N203ME · Doug DC932 · Emergency EquipmentSDR MWEA95120Slide Cover · fell offPILOT REPORTS GALLEY SERVICE DOOR EVACUATION SLIDE COVER FELL OFF. REINSTALLED SLIDE COVER AND RETURNED A/C TO SERVICE.Jan 31, 1995 · N203ME · Doug DC932 · Emergency EquipmentSDR ABXA9500179Panel · corrodedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND CORROSION ON THE RIGHT WING OUTBOARD TRAILING EDGE PANEL JUST FORWARD OF THE AILERON. REPLACED PANEL IAW DC-9 SRM CHAPTERS 51-30-1 AND 51-30-2.Jan 31, 1995 · N988AX · Doug DC932 · Wing, Plate/SkinSDR ABXA9500169Skin · corrodedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE FORWARD LOWER FUSELAGE SKIN FROM FS 229 TO FS 512, FROM LONGERON 18R TO 26R, HAD NUMEROUS AREAS OF CORROSION AND PREVIOUS REPAIRS. REPLACED SKIN FROM FS 229 TO FS 512 IAW ABX REA D953-10751-MR AND DC-9 SRM CHAPTJan 31, 1995 · N988AX · Doug DC932 · Fuselage Main, Plate/SkinSDR ABXA9500151Bulkhead Skin · dentedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND A DENT AND PUNCTURE IN AFT PRESSURE BULKHEAD SKIN, FORWARD FACE, BETWEEN LONGERON 29R AND 30R APPROXIMATELY EIGHT INCHES UP FROM TEE CAP. REPAIRED IAW DC-9 SRM CHAPTER 53-01, FIGURE 1, SHEET 2.Jan 31, 1995 · N988AX · Doug DC932 · Fuselage Main, BulkheadSDR 9502079984Longeron · corrodedDURING PERIODIC CHECK, FOUND CORROSION ON LONGERON 29L AT FS 522. REPLACED LONGERON PER EA 99-096876.Jan 31, 1995 · N984US · Doug DC932 · Fuselage Main, Longeron/StringerSDR 9502069984Fitting · crackedDURING PERIODIC CHECK, FOUND CRACK IN FORWARD CARGO DOOR NR 5 BEAM END FITTING. REPLACED FITTING PER SRM 51-30-5.Jan 31, 1995 · N984US · Doug DC932 · Cargo/Baggage DoorsSDR ABXA9500231Trap Panel · crackedDURING C-CHECK INSPECTION, THE RIGHT TRAPEZOIDAL PANEL WAS FOUND CRACKED BETWEEN THREE EACH BOLTS ON THE HORIZONTAL FLANGE JUST FORWARD OF THE FIXED SIDE BRACE ATTACH POINT. REPLACED PANEL IAW DC-9 SERVICE BULLETIN 53-182.Jan 30, 1995 · N902AX · Doug DC932 · Fuselage Miscellaneous StructureSDR ABXA9500189Spar Cap · corrodedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND CORROSION ON THE LEFT WING LOWER REAR SPAR TEE CAP AT STATION XRS 494.5. REPAIRED LEFT WING LOWER SPAR CAP IAW ABX REA D957-10793-MR.Jan 30, 1995 · N988AX · Doug DC932 · Wing SparSDR ABXA9500185Spar Cap · corrodedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND CORROSION ON THE RIGHT WING REAR SPAR LOWER TEE CAP FROM XRS 509 TO XRS 563. REPAIRED RIGHT WING REAR SPAR IAW ABX REA D957-10641-MR.Jan 30, 1995 · N988AX · Doug DC932 · Wing SparSDR ABXA9500184Panel · delaminatedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND CORROSION AND DELAMINATION ON THE LEFT WING TRAILING EDGE BONDED PANEL JUST FORWARD OF LEFT AILERON. REPLACED PANEL IAW DC-9 SRM 51-30-1 AND 51-30-2.Jan 30, 1995 · N988AX · Doug DC932 · Wing, Plate/SkinSDR ABXA9500193Floor Beam · corrodedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND CORROSION ON THE FLOOR BEAM AT FS 965 AT RBL 22. REPAIRED FLOOR BEAM IAW ABX REA D953-10811-MR.Jan 28, 1995 · N988AX · Doug DC932 · Fuselage Main, Floor BeamSDR MWEA95117Slide Cover · fell offPILOT REPORTS WHILE EN ROUTE TO MKE, THE GALLEY SERVICE DOOR SLIDE COVER FELL OFF. MECHANIC REINSTALLED SLIDE COVER, AND RETURNED A/C TO SERVICE.Jan 27, 1995 · N302ME · Doug DC932 · Emergency EquipmentSDR MWEA95116Eel Power Supply · inoperativePILOT REPORTED AT CRUISE, THE LAST 5 LIGHTS ON THE EMERGENCY FLOOR TRACK LIGHTING CAME ON DIMLY. PILOT TESTED SYSTEM, AND RESET BREAKER. UPON RETURN TO MKE, MECHANICS REPLACED AFT FLOOR TRACK LIGHTING BATTERY POWER SUPPLY. OPS CHECK GOOD, RETURNED A/C TO SEJan 27, 1995 · N204ME · Doug DC932 · Emergency LightingSDR ABXA9500226Fitting · damagedDURING C-CHECK INSPECTION, FOUND A DOUBLE DRILLED HOLE IN THE FITTING AT STA 897.0 AND RBL 54.5. REPAIRED FITTING IAW ABX REA D953-10844-MR.Jan 27, 1995 · N902AX · Doug DC932 · Fuselage Main, Floor BeamSDR ABXA9500225Floor Beam · damagedDURING C-CHECK INSPECTION, FOUND A DOUBLE DRILLED HOLE IN THE FLOOR BEAM AT STA 897.0 AND RBL 54.5. REPAIRED FLOOR BEAM IAW ABX REA D953-10844-MR.Jan 27, 1995 · N902AX · Doug DC932 · Fuselage Main, Floor BeamSDR ABXA9500204Longeron · crackedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND LONGERON 29L CRACKED AFT OF STATION 256 AND 351. REPLACED LONGERON 29L FROM FS 237 TO FS 522 IAW DC-9 SRM CHAPTERS 51-30-2 AND 51-30-5.Jan 27, 1995 · N988AX · Doug DC932 · Fuselage Main, Longeron/StringerSDR 95ZZZX1626Anti-Ice Valve · malfunctionATL/IAD - FLT 368 - AIRCRAFT RETURNED TO ATL DUE TO RIGHT FUEL HEAT STAYED ON CAUSING OIL TEMP TO EXCEED 120 DEGREES CENTIGRADE. REMOVED AND REPLACED NR 2 ANTI-ICE VALVE.Jan 27, 1995 · N901VJ · Doug DC932 · Fuel HeaterSDR 95ZZZW217Frame · crackedSTL - DURING OP-15, FOUND ONE INCH CRACK IN MAIN FRAME RIGHT SIDE, STATION 680, ABOVE STRINGER 15R. REPAIRED PER EMLR 65330. TOTAL CYCLES 78,720.Jan 27, 1995 · N996Z · Doug DC932 · Fuselage Main, FrameSDR 95ZZZW116Anti-Ice Valve · malfunctionedATL-IAD - FLT 368 - FLIGHT RETURNED TO ATL DUE TO RT FUEL HEAT STAYED ON CAUSING OIL TEMP TO EXCEED LIMITS PER MM 71-00. REMOVED AND REPLACED NR 2 FUEL ANTI-ICE VALVE.Jan 27, 1995 · N901VJ · Doug DC932 · Engine Fuel DistributionSDR 95ZZZW115Apu · malfunctionedIAD - FLT 469 - WHILE AT THE GATE, EXPERIENCED FUMES AND SMOKE TO A MARGINAL DEGREE DUE TO THE APU. PLACED APU ON MEL 49-1.Jan 27, 1995 · N915VV · Doug DC932 · Airborne Auxiliary Power Unit (APU) SystemSDR MWEA95115Switch · malfunctionedCAPTAIN'S FLIGHT DIRECTOR INOP. FOUND THAT WHEN EMERGENCY POWER SWITCH IS CYCLED, ALL CONTACTS WOULD NOT TOGGLE BACK TO THE OFF POSITION. REPLACED SWITCH.Jan 26, 1995 · N501ME · Doug DC932 · AC Generation SystemSDR ABXA9500223Splice · corrodedDURING C-CHECK INSPECTION, FOUND LEVEL II CORROSION ON LONGERON 30 SPLICE, FORWARD OF STA 560. REPLACED LONGERON 30 SPLICE IAW DC-9 SRM 53-02, FIGURE 14.Jan 26, 1995 · N902AX · Doug DC932 · Fuselage Miscellaneous StructureSDR ABXA9500197Skin · corrodedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND CORROSION ON A SKIN REPAIR ON AFT FUSELAGE SKIN FROM FS 996 TO FS 1034 AT LONGERON 23 LEFT. REPAIRED AFT FUSELAGE SKIN IAW ABX REA D953-10834-MR.Jan 26, 1995 · N988AX · Doug DC932 · Fuselage Main, StructureSDR ABXA9500163Frame · crackedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND A CRACK ON THE FUSELAGE FRAME 1132, LEFT SIDE BELOW CATWALK. REPLACED FRAME IAW DC-9 SRM CHAPTERS 51-30-2 AND 51-30-5.Jan 26, 1995 · N988AX · Doug DC932 · Fuselage Main, FrameSDR ABXA9500326Rib · corrodedDURING D-CHECK ACCEPTANCE INSPECTION WHILE PERFORMING DC-9 FLAP OFF WING INSPECTION ON THE LEFT FLAP, FOUND LEVEL II CORROSION ON THE OUTBOARD END RIB. REPLACED IAW DC-9 SRM 57-50-9.Jan 25, 1995 · N988AX · Doug DC932 · Trailing Edge FlapsSDR MWEA95114Eel Power Supply · inoperativeDURING A SERVICE CHECK, THE RIGHT SIDE NACELLE EMERGENCY LIGHT WAS FOUND INOP. REPLACED BATTERY POWER SUPPLY FOR THE RIGHT NACELLE LIGHT. OPERATIONAL CHECK WAS GOOD. AIRCRAFT RETURNED TO SERVICE.Jan 24, 1995 · N204ME · Doug DC932 · Emergency LightingSDR ABXA9500229Frame · crackedDURING C-CHECK INSPECTION, THE RIGHT FUSELAGE MAIN FRAME AT STA 718 WAS FOUND CRACKED IN THE RIGHT WHEELWELL. REPLACED RIGHT MAIN FRAME IAW SERVICE BULLETIN 53-131.Jan 24, 1995 · N902AX · Doug DC932 · Fuselage Main, FrameSDR ABXA9500228Floor Beam · crackedDURING C-CHECK INSPECTION, FOUND A FLOOR BEAM CRACKED WITH DOUBLE DRILLED HOLES AT STA 680, LBL 54.5. REPAIRED FLOOR BEAM IAW ABX REA D953-10828-MR.Jan 24, 1995 · N902AX · Doug DC932 · Fuselage Main, Floor BeamSDR ABXA9500172Skin · corrodedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND LEVEL II CORROSION ON AFT FUSELAGE LOWER SKIN FROM FS 802 TO FS 996, BETWEEN LONGERON 26 RIGHT TO 26 LEFT. REPLACE LOWER SKIN FROM FS 802 TO FS 996 IAW DC-9 SRM CHAPTERS 51-30-2 AND 51-30-5.Jan 24, 1995 · N988AX · Doug DC932 · Fuselage Main, Plate/SkinSDR 95ZZZX859Splice · crackedSTL - DURING OP-15, FOUND .25 INCH CRACK IN FORWARD CARGO BIN LONGERON 30 AND IN LONGERON SPLICE, STA 414. INSTALLED NEW SECTION OF LONGERON AND REPLACED SPLICE PLATE. AIRCRAFT TOTAL TIME: 70,380 HOURS; 78,720 CYCLES.Jan 24, 1995 · N996Z · Doug DC932 · Fuselage Main, Longeron/StringerSDR 95ZZZX858Longeron · crackedSTL - DURING OP-15, FOUND A .25 INCH CRACK IN LONGERON 8L, STA 718. REPAIRED PER SRM 53-02, FIGURE 2, PAGE 2A. AIRCRAFT TOTAL TIME: 70,380 HOURS; 78,720 CYCLES.Jan 24, 1995 · N996Z · Doug DC932 · Fuselage Main, Longeron/StringerSDR 95ZZZM349Frame · crackedUPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, A 1 INCH CRACK WAS FOUND IN THE AFT CARGO DOOR FRAME. STOP DRILLED CRACK. FABRICATED AND INSTALLED REPAIRS IAW DC9 SRM 52-03, 51-10-4, AND 51-30-5. N/R NR 027N1/0710.Jan 24, 1995 · N937VV · Doug DC932 · Fuselage Miscellaneous StructureSDR 95ZZZM348Frame · corrodedUPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, THE FRAME SEGMENT AT FS 560 AT LONGERON 28L WAS FOUND CORRODED. FABRICATED AND INSTALLED A NEW FRAME SEGMENT IAW DC9 SRM 51-10-2A, 51-10-4 AND 53-10-1. N/R NR 027N1/0633.Jan 24, 1995 · N937VV · Doug DC932 · Fuselage Main, FrameSDR 95ZZZM347Frame · corrodedUPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, CORROSION WAS FOUND UNDER THE NUTPLATES ON THE FLOOR FRAME AT FS 1019 PRESSURE DOME. FABRICATED AND INSTALLED PRESSURE DOME FLOOR FRAME REPAIRS IAW DC9 SRM 53-05 AND 51-10-3. N/R NR 027N1/0643.Jan 24, 1995 · N937VV · Doug DC932 · Fuselage Main, FrameSDR 95ZZZM346Frame · corrodedUPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, CORROSION WAS FOUND UNDER THE TEFLON STRIP ON THE UPPER FLOOR FRAMES AT FS 541. FABRICATED AND INSTALLED FRAME REPAIRS IAW DC9 SRM 53-03-2A, 51-10-3, AND 51-10-2A. N/R NR 027N1/0658.Jan 24, 1995 · N937VV · Doug DC932 · Fuselage Main, FrameSDR 95ZZZM344Frame · corrodedUPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, THE FRAME SEGMENT AT FS 522 AT LONGERON 28L WAS FOUND WITH CORROSION. FABRICATED AND INSTALLED A NEW FRAME SEGMENT IAW DC9 SRM 51-10-2A, 51-10-4, AND 53-10-1. N/R NR 027N1/0632.Jan 24, 1995 · N937VV · Doug DC932 · Fuselage Main, FrameSDR ABXA9500201Skin · corrodedDURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND LEVEL II CORROSION ON FUSELAGE SKIN FORWARD OF E AND E COMPARTMENT ENTRY DOOR BETWEEN LONGERON 28 RIGHT AND 29 RIGHT. REPAIRED IAW DC-9 SRM CHAPTER 53-01, FIGURE 4, SHEET 3.Jan 23, 1995 · N988AX · Doug DC932 · Fuselage Main, Plate/SkinSDR ABXA9500177Spar · corrodedDURING C-CHECK ACCEPTANCE INSPECTION, FOUND CORROSION ON THE LOWER FLANGE OF THE RIGHT WING LOWER REAR SPAR FROM XRS 488 TO XRS 560. REPAIRED RIGHT WING LOWER REAR SPAR IAW ABX REA D957-10795-MR.Jan 23, 1995 · N988AX · Doug DC932 · Wing SparSDR 95ZZZX861Longeron · crackedSTL - DURING OP-15, FOUND CRACK IN LONGERON 6R, STA 639 AND STA 658, APPROXIMATELY .1250 INCH TO .50 INCH. REPAIRED PER SRM 53-02 AND TWA STANDARD PRACTICES. AIRCRAFT TOTAL TIME: 70,380 HOURS; 78,720 CYCLES.Jan 23, 1995 · N996Z · Doug DC932 · Fuselage Main, Longeron/StringerSDR 95ZZZX5346Longeron · corrodedUPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, FOUND THE FWD CARGO LONGERON 30 WAS CORRODED OUT 25 PERCENT OF MATERIAL THICKNESS AT FS 508. REMOVED AND REPLACED LONGERON 30 FROM FS 503 TO FS 520 IAW DC9 SRM 51-40-4 AND SRM 51-30-05. N/R NR 0Jan 23, 1995 · N938VV · Doug DC932 · Fuselage Main, Longeron/StringerSDR 95ZZZX5349Skin · damagedUPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, FOUND THE REPAIR AT FS 125 TO FS 157 IS A NON-STANDARD REPAIR. FABRICATED AND INSTALLED NEW SKIN FILLERS AND DOUBLERS IAW DC9 SRM 53-04, FIG 12B, AND SRM 51-20-0. N/R NR 027A1/0234.Jan 22, 1995 · N938VV · Doug DC932 · Fuselage Main, Plate/SkinSDR 95ZZZM345Le Skin · crackedUPON A SCHEDULED INSPECTION AT AERO CORP INLAKE CITY, FLORIDA, THE VERTICAL STABILIZER L/E WAS FOUND WITH 5 CRACKED STIFFENERS. FABRICATED AND INSTALLED NEW STIFFENERS IAW DC9 SRM 55-02 AND MM 51-00. N/R NR027N1/0598.Jan 22, 1995 · N937VV · Doug DC932 · Fuselage, Stabilizer Attach FittingsSDR 95ZZZM343Longeron · crackedUPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, LONGERON 23 AT FS 200 WAS FOUND CRACKED. FABRICATED AND INSTALLED REPAIR MEMBERS IAW DC9 SRM 53-02, 51-10-3 AND 51-30-2.Jan 22, 1995 · N937VV · Doug DC932 · Fuselage Main, Longeron/StringerSDR ABXA9500230Bracket · crackedDURING C-CHECK INSPECTION, THE LEFT FLAP OUTBOARD HINGE ATTACH BRACKETS WERE FOUND CRACKED. REPLACED BRACKETS IAW DC-9 SRM 51-30-2, 51-30-1 AND 51-30-5.Jan 20, 1995 · N902AX · Doug DC932 · Trailing Edge FlapsSDR 95ZZZX865Press Reg Valve · malfunctionedATL/MDW - FLT 240 - RETURNED TO ATL DUE TO FLIGHT CREW COULD NOT PRESSURIZE AIRCRAFT IN AUTO OR MANUAL. REPLACED PRESSURIZED REGULATION VALVE FOR LEFT AIR CONDITIONING PACK AND SEGMENT.Jan 20, 1995 · N922VV · Doug DC932 · Pressure Regulator/Outflow ValveSDR 95ZZZX856Frame · crackedSTL - DURING OP-15, FOUND A ONE INCH CRACK IN RT MAIN FRAME, COMING FROM AFT LOWER HOLE ATTACHED TO TRAPEZOID PANEL. REPAIRED PER SSRM 53-60-102. AIRCRAFT TOTAL TIME: 70,380 HOURS: 78,720 CYCLES.Jan 20, 1995 · N996Z · Doug DC932 · Fuselage Main, FrameSDR 95ZZZW98Clamp · brokenMDW-ATL - FLT 245 - DURING CLIMB-OUT, THE LT ENGINE FIRE WARNING CAME ON, RETARDED POWER LEVER, LIGHT WENT OUT. RETURNED TO MDW. FOUND 13TH STAGE BLANKING CAP OFF, BROKEN CLAMP. REPLACED CAP AND CLAMP, ENGINE OPERATIONAL CHECK NORMAL.Jan 20, 1995 · N1269L · Doug DC932 · Pneumatic Distribution SystemSDR 95ZZZW97Hyd Pump · failedIAD-ATL - FLT 175 - FLIGHT EXPERIENCED A LT SYSTEM HYDRAULIC LOW PRESSURE LIGHT, 300 PSI AFTER PERFORMING THE GEAR UPLATCH CHECK. FLIGHT RETURNED TO IAD FOR REPAIRS. REMOVED AND REPLACED HYDRAULIC PUMP NR 1 ENGINE.Jan 20, 1995 · N904VJ · Doug DC932 · Hydraulic Pump (Electric/Engine), MainSDR 95ZZZX5352Angle · crackedUPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, FOUND THE MAIN CABIN COMPARTMENT AFT PRESSURE BULKHEAD ATTACH ANGLE IS CRACKED AT APPROXIMATELY 10 O'CLOCK POSITION, RT SIDE. FABRICATED AND INSTALLED PRESSURE BULKHEAD REPAIRS IAW DC9 SRM 53-05-Jan 19, 1995 · N938VV · Doug DC932 · Fuselage Main, Bulkhead
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