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"

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SDR MWEA00870Floorboard · tornCABIN FLOORBOARD E-6 HAS 2 SMALL TEARS IN UPPER SKIN AT ATTACH END. FABRICATED AND INSTALLED FLOORBOARD REPAIR.Oct 9, 2000 · N602ME · Doug DC932 · Fuselage Floor PanelSDR AT0000469Longeron · corrodedFOUND CORROSION ON LEFT LONGERON NR 20 AT THE OUTBOARD MEMBER SURFACE. CORROSION WAS OUT OF LIMITS, REMOVED CORRODED SECTION. FABRICATED AND INSTALLED LONGERON SPLICE AND STRAP IAW DC9 SRM 51-10-4, 51-10-3, 53-02 FIGURE 9A.Oct 7, 2000 · N866AT · Doug DC932 · Fuselage Main, Longeron/StringerSDR MWEA00880Warning Light · false indicationCREW REPORTED GEAR DOOR OPEN LIGHT CAME ON AFTER TAKEOFF AND GEAR HAD RETRACTED. AIRCRAFT RETURNED TO MKE FOR TROUBLESHOOTING AND REPAIRS. MAINTENANCE REPAIRED WIRING TO GEAR DOOR CAUTION SWITCH AND RIGHT GEAR UP LIMIT SWITCH.Oct 7, 2000 · N301ME · Doug DC932 · Landing Gear Position and WarningSDR AT0000468Floorbeam · corrodedFOUND FLOOR SUPPORT BEAM AT BS 1012 RBL 24 TO LBL 24 WAS CORRODED. MECHANICALLY REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. REMOVED LEFT AND RIGHT BEAM AND LOWER DOOR JAMB. FABRICATED AND INSTALLED NEW JAMB, PANELS AND ANGLES IAW DC9 SRM 51-30-2, 53-01 FOct 6, 2000 · N866AT · Doug DC932 · Fuselage Main, Floor BeamSDR AT0000466Skin · corrodedFOUND FLOOR BOARD NR 80 CORRODED ON SKIN. REMOVED CORROSION AND FOUND 3 CRACKS. REPAIRED SKIN, REMOVED AND INSTALLED HATS, AND REINSTALLED FLOOR BOARD IAW DC9 MM 53-20-1, DC9 SRM 53-21-0, 51-10-03, 51-30-2, 53-20-1.Oct 6, 2000 · N866AT · Doug DC932 · Fuselage Main, Plate/SkinSDR AT0000465Floor Panel · crackedFOUND FLOORBOARD NR 67 TEMPORARY PATCH INSTALLED. REMOVED FLOOR PANEL NR 67, FABRICATED REPAIR SKIN. REPLACED HAT CHANNELS AND INSTALLED REPAIR SKIN. REINSTALLED FLOOR PANEL IAW DC9 MM 53-20-1, DC9 SRM 51-10-3, 51-30-2.Oct 6, 2000 · N866AT · Doug DC932 · Fuselage Floor PanelSDR AT0000447Actuator · failedDURING GEAR EXTENSION, THE AMBER GEAR DOOR LIGHT WOULD NOT EXTINGUISH. CYCLED GEAR 3 TIMES WITH SAME RESULT. LIGHT FINALLY EXTINGUISHED PRIOR TO LANDING. LANDING WAS NORMAL. REPLACED RIGHT MAIN GEAR DOOR ACTUATING CYLINDER IAW 32-32-04.Oct 6, 2000 · N848AT · Doug DC932 · Landing Gear Door ActuatorSDR AT0000444Light · inoperativeAFT ENTRY LEFT EMERGENCY LIGHT OUT. SECURED GROUND WIRE AT AFT ENTRY DOOR EMERGENCY LIGHT IAW DC9 MM 20-50.Oct 6, 2000 · N836AT · Doug DC932 · Emergency LightingSDR AT0000474Floor Panel · corrodedFOUND FLOOR PANEL 4692 CORRODED AND HAT CHANNELS CRACKED. REMOVED FLOOR PANEL AND REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. FABRICATED, TREATED, AND INSTALLED NEW FLOOR PANEL AND HAT CHANNELS IAW DC9 MM 53-20-1 DC9 SRM 51-10-3.Oct 5, 2000 · N866AT · Doug DC932 · Fuselage Floor PanelSDR AT0000467Floor Panel · corrodedFOUND FLOOR BOARD NR 4695 WAS CORRODED. BLENDED OUT CORROSION, FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED HATS AND FABRICATED AND INSTALLED FLOOR PANEL IAW DC9 MM 53-20, DC9 SRM 53-01 FIGURE 1, 51-10-2, 51-10-4, 51-30-2, 53-20-1.Oct 5, 2000 · N866AT · Doug DC932 · Fuselage Floor PanelSDR ABXA000479Intercostal · crackedINTERCOSTAL AT LONGERON 29 LEFT CRACKED BETWEEN STATION 351 AND 370. REPLACED INTERCOSTAL (P/N 9957911-3AX) IAW DC9 SRM 51-30-2.Oct 5, 2000 · N901AX · Doug DC932 · Fuselage Miscellaneous StructureSDR TWAA0016010Finger Doubler · misinstalledDURING OP 15 MAINT CHECK, FOUND INTERCOSTAL FINGER DOUBLERS NOT PROPERLY INSTALLED AT STA 965, BETWEEN LONGERON 13R AND 14R. INSTALLED NEW FINGER DOUBLER OF 0.025 2024-T3, FILLER AND INTERNAL REPAIR DOUBLER PER SRM 53-04 PAGE 218X, FIGURE 38 SHEET 34.Oct 5, 2000 · N996Z · Doug DC932 · Fuselage Miscellaneous StructureSDR TWAA0016009Web · corrodedDURING OP 15 MAINT CHECK, FOUND FLOOR MEMBRANE CORRODED 8 INCHES INBD OF FWD GALLEY DRAIN PAN STA 152, AS SEEN FROM E AND E COMPT. CUT OUT CORRODED SECTION OF MEMBRANE. MADE AND INSTALLED REPAIR MEMBRANE PER SRM 51-70-4 FIG 1. MADE AND INSTALLED FLOOR SUPPOOct 5, 2000 · N996Z · Doug DC932 · Fuselage Miscellaneous StructureSDR TWAA0016005Longeron · crackedDURING OP 15 MAINT CHECK, FOUND LONGERON CRACKED AT STA 586, LONGERON 25R. REPLACED PART AND FASTENERS PER SRM 51-30-01 AND SPM 6-70-01.Oct 5, 2000 · N996Z · Doug DC932 · Fuselage Main, Longeron/StringerSDR MWEA00869Audio Panel · inoperativeAFTER TAKEOFF FROM KANSAS CITY, CREW WAS UNABLE TO TRANSMIT OR RECEIVE VOICE COMMUNICATIONS. MAINTENANCE REMOVED AND REPLACED CAPTAINS AUDIO CONTROL PANEL AND MICROPHONE.Oct 5, 2000 · N501ME · Doug DC932 · Data Transmission Auto CallSDR MWEA00868Sensor · inoperativeEN ROUTE FROM OMA TO DCA WHEN SELECTING THE AIRFOIL ICE PROTECTION SYSTEM ON, THE LEFT ICE PROTECTION TEMP HIGH ANNUNCIATOR ILLUMINATES. AIRCRAFT DIVERTED TO MKE FOR REPAIR. RAN AIRCRAFT TO CHECK TEMPS. CHECKED THERMAL SWITCH, ALL CHECKS GOOD. CHANGED ICE Oct 4, 2000 · N209ME · Doug DC932 · Pneumatic Distribution SystemSDR TWAA0016008Floor Support · corrodedDURING OP 15 MAINT CHECK FOUND FLOOR SUPPORT CORRODED AT STA 148 TO 160, RBL 34 INCHES. MADE AND INSTALLED NEW FLOOR SUPPORT PER SPM 6-70-01 PAGE 3. INSTALLED FASTENERS PER SRM 51-30-0. REF SRM 53-11-1 AND DOUGLAS PRINT 99100078.Oct 4, 2000 · N996Z · Doug DC932 · Fuselage Miscellaneous StructureSDR TWAA0016007Web · corrodedDURING OP 15 MAINT CHECK, FOUND FLOOR MEMBRANE CORRODED AT STA 156 TO 160, RBL 22 INCHES TO 33 IN. MADE AND INSTALLED NEW SECTION OF MEMBRANE PER SRM 51-70-4 FIG 2 PAGE 96. INSTALLED FASTENERS PER SRM 51-30-0. REF SRM 53-11-1 FIG 12.Oct 4, 2000 · N996Z · Doug DC932 · Fuselage Miscellaneous StructureSDR TWAA0016006Floor Support · corrodedDURING OP 15 MAINT CHECK, FOUND FLOOR SUPPORT CORRODED AT STA 148 TO 160, RBL 18 INCHES. MADE AND INSTALLED NEW FLOOR SUPPORT PER SPM 6-70-01 PAGE 3. INSTALLED FASTENERS PER SRM 51-30-0. REF SRM 53-11-1 FIG 12 AND DOUGLAS PRINT 9910078.Oct 4, 2000 · N996Z · Doug DC932 · Fuselage Miscellaneous StructureSDR AT0000490Panel · corrodedFOUND PANEL 1211 AT RIGHT WING LOWER LEADING EDGE HAS AREA OF CORROSION ON OUTER SURFACE. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS, FORMED REPAIR DOUBLER, TREATED, PRIMED AND INSTALLED. IAW DC9 SRM 51-10-3, 51-30-1, 51-30-2, 57-01 FIGURE 2A, FIGURE 1Oct 3, 2000 · N866AT · Doug DC932 · Wing, Plate/SkinSDR TWAA0016805Web · corrodedDURING OP 15 MAINT CHECK, THE MEMBRANE AT STA 897 TO 965, RT SIDE, HAD CORROSION BEYOND LIMITS AND CRACKED. REMOVED AND REPLACED MEMBRANE AT STA 897 TO 965 WITH NEW MEMBRANE FABRICATED IN SHOP AND SENT TO PAINT SHOP FOR PAINT. INSTALLED PER SRM 51-30-2. HI-Oct 3, 2000 · N996Z · Doug DC932 · Fuselage Miscellaneous StructureSDR ABXA000477Retainer · crackedUPPER FORWARD CORNER WINDOW RETAINER RING WAS CRACKED JUST AFT OF FRAME 598. REPAIRED RETAINER IAW DC9 SRM K07226.Oct 3, 2000 · N901AX · Doug DC932 · Fuselage Miscellaneous StructureSDR ABXA000476Longeron · crackedLONGERON 2 LEFT CRACKED AT FUSELAGE STA 200. INSTALLED NEW SECTION OF LONGERON FROM STATION 190 - 212 IAW DC9 SRM 53-02.Oct 3, 2000 · N901AX · Doug DC932 · Fuselage Main, Longeron/StringerSDR TWAA0015712Bulkhead · crackedDURING CHECK-C MAINT AN EDDY CURRENT CHECK OF THE BULKHEAD T-CAP SHOWED A CRACK APPROXIMATELY 1 INCH LONG IN RADIUS AT LONGERON 28L. INSTALLED NEW T-CAP PER SRM 53-03 FIG 37A AND BOEING DRAWING SERIES 5911425.Oct 3, 2000 · N929L · Doug DC932 · Fuselage Main, BulkheadSDR TWAA0015711Bulkhead · corrodedDURING CHECK-C MAINT, THE AFT PRESSURE BULKHEAD SKIN WAS CORRODED ALONG THE BOTTOM EDGE AT ''T'' CAP, STA 996 FROM LONGERON 27L TO 28R, 23 INCHES LONG BY 2.25 IN HIGH. REPAIRED PRESSURE BULKHEAD SKIN PER SRM 53-05 FIG 9.Oct 3, 2000 · N929L · Doug DC932 · Fuselage Main, BulkheadSDR TWAA0015705Web · corrodedDURING OP 15 MAINT CHECK MEMBRANE AT STA 897 TO 965 ON RT SIDE HAD CORROSION BEYOND LIMITS AND CRACKED. REMOVED AND REPLACED MEMBRANE AT STA 897 TO 965 WITH NEW MEMBRANE FABRICATED IN METAL SHOP AND SENT TO PAINT SHOP FOR PAINT. INSTALLED RIVETS PER SRM 51-3Oct 3, 2000 · N996Z · Doug DC932 · Fuselage Main, Floor BeamSDR AT0000437Battery · dischargedBATTERIES IN B5-27 WERE WEAK DUE TO INSUFFICENT CHARGING VOLTAGE. REMOVED AND REPLACED BATTERIES IN B5-27 AND CORRECTED INPUT VOLTAGE PROBLEM TO BATTERY PACK IAW DC9 MM 33-50.Oct 1, 2000 · N834AT · Doug DC932 · Emergency LightingSDR 0003749920Battery Pack · inoperativeDURING LINE CHECK, FOUND EMERGENCY LIGHTS IN COCKPIT, GALLEY, AND ENTRYWAY INOPERATIVE. MAINTENANCE RESEATED BATTERIES IN PACK B5-23. OPERATIONAL CHECK NORMAL.Oct 1, 2000 · N942N · Doug DC932 · Emergency LightingSDR AT0000424Battery · inoperativeAFT CEILING EMERGENCY LIGHTS DO NOT WORK. REMOVED AND REPLACED NICAD BATTERY IAW DC9 MM 33-53.Sep 30, 2000 · N849AT · Doug DC932 · Emergency LightingSDR L1GA200000311Jackscrew · corrodedDURING INSPECTION AT LEGEND AIRLINES FOUND THE HORIZONTAL JACK SCREW TO HAVE METAL SHAVINGS AND OUT OF LIMITS.Sep 30, 2000 · N12507 · Doug DC932 · Stabilizer Control SystemSDR L1GA200000310Doubler · corrodedLEFT WING MAIN LANDING GEAR DOUBLER ON THE UPPER SURFACE OF THE WING HAD EXFOLIATION AND DELAMINATION NOTED.Sep 29, 2000 · N14534 · Doug DC932 · Wing, Plate/SkinSDR TWAA0015509Frame · damagedDURING OP 15 MAINT CHECK, FOUND FORMER RING REPAIR NOT PER SRM AT STA 896, BETWEEN LONGERON 22L AND 23L. REPLACED FORMER RING PER DOUGLAS BLUE PRINT 9958214.Sep 28, 2000 · N996Z · Doug DC932 · Fuselage Main, FrameSDR TWAA0015508Frame · crackedDURING OP 15 MAINT CHECK, FOUND CRACK EMANATING FROM BENEATH REPAIR ON STA 718 FRAME CASTING, RT MAIN GEAR WHEEL WELL. REPLACED STA 718 CASTING RT, PER BLUE PRINT 9919647 AND INSTALLED HI-LOKS PER SRM 51-30-5, AND RIVETS PER SRM 51-30-2.Sep 28, 2000 · N996Z · Doug DC932 · Fuselage Main, FrameSDR TWAA0015507Frame · crackedDURING OP 15 MAINT CHECK FOUND FORMER TO WEB CORNER FRAME CRACKED AT STA 718, RBL 52 INCHES AFT SIDE. REPAIRED WEB PER SRM 53-01, FIG 2 AND REINSTALLED BRACKET PER SRM 53-30-5.Sep 28, 2000 · N996Z · Doug DC932 · Fuselage Main, FrameSDR 0003539941Bearing · damagedAUTOPILOT PORPOISING IN CRUISE, VIBRATION IN CABIN FLOOR, AND KNOCKING SOUND IN REAR. FLIGHT DECLARED AN EMERGENCY AS A PRECAUTION BUT LANDED AT MSP WITHOUT INCIDENT. MAINTENANCE FOUND FOLLOW-UP BALANCE LINKAGE BEARINGS TO RIGHT ELEVATOR CONTROL TAB BINDING.Sep 27, 2000 · N3324L · Doug DC932 · Elevator Control SystemSDR AT0000461Skin · corrodedFOUND CORROSION AROUND FASTENERS IN CENTER TANK LOWER SKIN. REPAIRED CORROSION IAW REO-L00271.Sep 26, 2000 · N832AT · Doug DC932 · Fuselage Main, Plate/SkinSDR AT0000460Frame · crackedDURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND FUSELAGE MAIN FRAME CRACKED AT RIGHT 737. REMOVED AND REPLACED FRAME IAW DC9 SB 53-131 REV 4.Sep 26, 2000 · N832AT · Doug DC932 · Fuselage Main, FrameSDR TWAA0015002Strap · damagedTHE RT PYLON RT AFT UPPER CAP STRAP AND RELATED STRUCTURE HAD OVERSIZED HOLES IN EXCESS OF THE NUMBER AUTHORIZED. REPAIRED PER EMLR 71221. UPPER CAP STRAP AND STRUCTURE REWORKED. CHECK-C 8-2-00 MCI.Sep 26, 2000 · N921L · Doug DC932 · Nacelle/Pylon StructureSDR MWEA00824Skin · dentedMKE - SMALL DENTS IN FUSELAGE SKIN BETWEEN STATIONS 218 AND 229 AT LONGERONS 16 TO 18 LEFT. FABRICATED AND INSTALLED REPAIR DOUBLER. (X)Sep 22, 2000 · N302ME · Doug DC932 · Fuselage Main, Plate/SkinSDR MWEA00823Seat Track · corrodedMKE - SEAT TRACK NR 3 HAD MODERATE CORROSION AT STA 200. REMOVED AND REPLACED SEAT TRACK. (X)Sep 22, 2000 · N302ME · Doug DC932 · Fuselage, Seat/Cargo Attach FittingsSDR MWEA00822Former · crackedMKE - CRACK IN OUTBOARD EDGE OF RIGHT SIDE APB FORMER AND DOUBLER, FORWARD SIDE. REMOVED AND REPLACED FORMER AND CLIP. (X)Sep 22, 2000 · N302ME · Doug DC932 · Fuselage Main, FrameSDR MWEA00821Frame · crackedMKE - FUSELAGE FRAME 484 CRACKED AROUND 2 EACH HI-LOCS AT LONGERON 6 LEFT. REMOVED AND REPLACED FRAME SECTION. (X)Sep 22, 2000 · N302ME · Doug DC932 · Fuselage Main, FrameSDR MWEA00820Frame · tool damageMKE - TOOL MARKS ON FRAME AT STA 945 BETWEEN LONGERONS 7 AND 8 RIGHT. REMOVED AND REPLACED FRAME SECTION. (X)Sep 22, 2000 · N302ME · Doug DC932 · Fuselage Main, FrameSDR MWEA00819Former · crackedMKE - CRACK ON APB FORMER AT LEFT OUTBOARD EDGE. REMOVED AND REPLACED FORMER. (X)Sep 22, 2000 · N302ME · Doug DC932 · Fuselage Main, FrameSDR MWEA00818Bulkhead · tool damageMKE - NUMEROUS TOOL MARKS ON FORWARD SIDE OF APB TEE, BETWEEN SHOVEL CLIPS 4 EACH LEFT TO 4 EACH RIGHT. (X)Sep 22, 2000 · N302ME · Doug DC932 · Fuselage Main, BulkheadSDR MWEA00817Former · crackedMKE - CRACK IN OUTBOARD EDGE OF RIGHT SIDE APB FORMER, FORWARD SIDE. REMOVED AND REPLACED FORMER. (X)Sep 22, 2000 · N302ME · Doug DC932 · Fuselage Main, FrameSDR MWEA00816Former · crackedMKE - CRACK IN OUTBOARD EDGE OF RIGHT SIDE APB FORMER AND DOUBLER, FORWARD SIDE. REMOVED AND REPLACED FORMER. (X)Sep 22, 2000 · N302ME · Doug DC932 · Fuselage Main, FrameSDR MWEA00815Former · crackedMKE - CRACK ON APB FORMER, AT LEFT OUTBOARD EDGE. REMOVED AND REPLACED FORMER. (X)Sep 22, 2000 · N302ME · Doug DC932 · Fuselage Main, FrameSDR MWEA00814Former · crackedMKE - CRACK ON APB FORMER DOUBLER, LEFT OUTBOARD EDGE. REMOVED AND REPLACED FORMER. (X)Sep 22, 2000 · N302ME · Doug DC932 · Fuselage Main, FrameSDR MWEA00831Connector · failedATW - FLT 431 - DURING CRUISE, DESCENT, AND APPROACH HEADINGS WOULD NOT STAY ALIGNED, SPLIT UP TO 15 DEGREES. REMOVED O-RING FROM FIRST OFFICERS RMI CONNECTOR. REPLACED NR 2 COMPASS RACK (INTERGRATED INSTRUMENT AMP). (M)Sep 22, 2000 · N205ME · Doug DC932 · Integrated Flight System
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