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 TWAA0017405Pan · corrodedDURING OP 15 MAINT CHECK ON THE AFT CARGO COMPT DOOR, THE FWD LOWER DOOR PAN AT STA 889 TO 937, AND RL 24 TO RL 29, HAD CORROSION. AFT CARGO DOOR ALSO HAD CORROSION ON BOTH FWD DOOR STOP ADJUSTMENT SCREWS, THE AFT DOOR JAMB STA 917 TO 935, THE INNER DOOR JAMBOct 30, 2000 · N996Z · Doug DC932 · Cargo/Baggage DoorsSDR MWEA001112Connector · corrodedON CLIMBOUT, FLIGHT CREW GOT BOTH STALL RECOGNITION LIGHTS ON. MAINTENANCE FOUND CORROSION ON BOTH LEFT AND RIGHT FLAP POSITION TRANSMITTER CONNECTORS. CLEANED RIGHT CONNECTOR. REMOVED AND REPLACED LEFT CONNECTOR.Oct 30, 2000 · N401ME · Doug DC932 · Elevator Control SystemSDR AT0000502Skin · crackedFOUND CRACKED EXTERIOR SKIN IN LOWER AFT DOOR JAMB CORNER OF FORWARD SERVICE DOOR. CUT OUT CRACKED SECTION, FABRICATED REPAIR DOUBLERS, SHIMS AND FILLERS. IAW DC9 SRM 51-10-2, 51-10-3, 51-10-4, 51-30-2, AND 51-30-5, DRAWING SR0953017C AND E.O. 095310-29-E14Oct 29, 2000 · N866AT · Doug DC932 · Fuselage Main, Plate/SkinSDR L1GA200000318Flange · crackedFLANGE CRACKED 1.75 INCHES (UNDER ACCESS PNL TO AFT BOOST PUMP, 1305A).Oct 29, 2000 · N17533 · Doug DC932 · Wing Miscellaneous StructureSDR L1GA200000317Jackscrew · wornHORIZONTAL STAB JACKSCREW WORN.Oct 28, 2000 · N33506 · Doug DC932 · Stabilizer Control SystemSDR TWAA0017404Floorbeam · corrodedDURING OP 15 MAINT CHECK IN THE RT AFT LAVATORY, AT STA 996 THE FLOORBEAM WAS CORRODED, 55 INCHES RBL, UNDER TOP FLANGE. FABRICATED AND INSTALLED REPAIR PER SRM 53-05, FIG 18.Oct 27, 2000 · N996Z · Doug DC932 · Fuselage Main, Floor BeamSDR TWAA0017215Floorbeam · corrodedDURING OP 15 MAINT CHECK AT RT AFT LAV AT STA 996, FLOORBEAM 8 PLACES HAD CORROSION ON TOP FLANGE. REMOVED THE CORROSION PER SPM 6-80-01. FABRICATED AND REPAIRED PER SRM 53-05, FIG 108.Oct 27, 2000 · N996Z · Doug DC932 · Fuselage Main, Floor BeamSDR TWAA0017214Angle · crackedDURING OP 15 MAINT CHECK THE AFT PRESSURE BULKHEAD ANGLE WAS CRACKED AT FASTENER TO L/E AND FASTENERS HAD TOOLING MARKS ABOVE LT DOOR JAMB FOR AFT AIRSTAIRS. BULKHEAD SKIN WAS NOT CRACKED UNDER ANGLE PER NDT PART L 51-00-3. REMOVED OLD PART AND MADE NEW PER Oct 27, 2000 · N996Z · Doug DC932 · Fuselage Miscellaneous StructureSDR TWAA0017213Skin · damagedDURING OP 15 MAINT CHECK FOUND FIELD SKIN REPAIR FWD OF STA 313, RL 24 TO 25. REPAIRED PER SRM 53-04, FIG 38.Oct 27, 2000 · N996Z · Doug DC932 · Fuselage Main, Plate/SkinSDR AT0000501Door Frame · crackedDURING A SCHEDULED INSPECTION, FOUND CRACK IN FORWARD CARGO COMPARTMENT DOOR JAMB. CUT OUT CRACKED SECTION AND INSTALLED REPAIR IAW EO 09-5310-29-E1482.Oct 26, 2000 · N807AT · Doug DC932 · Fuselage Main, StructureSDR AT0000499Frame · crackedDURING A SCHEDULED INSPECTION, FOUND CRACK AT BS 718 OVER WHEEL WELL END FRAME. REMOVED AND REPLACED MAIN FRAME AT BS 718 IAW EO 12-5311-29-B1044.Oct 26, 2000 · N807AT · Doug DC932 · Fuselage Main, FrameSDR AT0000498Door Frame · crackedDURING A SCHEDULED INSPECTION, FOUND FORWARD CARGO COMPARTMENT DOOR JAMB CRACKED. CUT OUT CRACKED SECTION AND INSTALLED REPAIR IAW EO 09-5310-29-E1482.Oct 26, 2000 · N807AT · Doug DC932 · Fuselage Main, StructureSDR GTIA000318Light · inoperativeDCA - FLT 72 - ONE WHITE PATH AISLE LIGHT INOPERATIVE, ROW 13. REPLACED LAMP AND LENS. OPS HECK OK IAW MM 33-53-01. THIS CLEARS DMI 121510-1, PLACARDS REMOVED. (M)Oct 26, 2000 · N12536 · Doug DC932 · Emergency LightingSDR TWAA0017212Intercostal · corrodedDURING OP 15 MAINT CHECK IN AFT CARGO COMPT FOUND CORROSION ON UNDER SIDE OF RL 29, STA 897 TO 917. REPLACED INTERCOSTAL PER DOUGLAS PRINT 5910158.Oct 26, 2000 · N996Z · Doug DC932 · Fuselage Miscellaneous StructureSDR TWAA0017211Longeron · crackedDURING OP 15 MAINT CHECK, FOUND LONGERON 17L WAS CRACKED AT STA 945. CRACK CONFIRMED BY NDT. REPLACED CRACKED LONGERON 17L AT STA 945 WITH NEW PER SRM 53-11-3, FIG 4 SHEET 3 PAGE 14. RE-INSTALLED RIVETS PER SRM 51-30-2. REINSTALLED HI-LOK PER SRM 51-30-5.Oct 26, 2000 · N996Z · Doug DC932 · Fuselage Main, Longeron/StringerSDR TWAA0017210Seat Track · corrodedDURING OP 15 MAINT CHECK, FOUND CORROSION ON SEAT TRACK AT STA 200, LBL 22. REPAIRED PER 53-05, PAGE 10L, FIG 4F SHEET 6.Oct 26, 2000 · N996Z · Doug DC932 · Fuselage, Seat/Cargo Attach FittingsSDR TWAA0017209Web · crackedDURING OP 15 MAINT CHECK IN THE AFT CARGO COMPT FOUND AT STA 889, LBL 45, A WEB CRACKED UNDER CABIN FLOOR TRACK FLANGE BETWEEN TIE BOLT AND RIVET. REPAIRED PER SRM 53-01, PAGE 9. STOP DRILLED CRACK, FABRICATED, PAINTED AND INSTALLED DOUBLER.Oct 26, 2000 · N996Z · Doug DC932 · Fuselage Miscellaneous StructureSDR L1GA200000316Skin · delaminatedLEFT I/B FLAP T/E DELAMINATED 5 INCHES.Oct 26, 2000 · N27509 · Doug DC932 · Trailing Edge FlapsSDR AT0000471Duct · blownEXPERIENCED PRESSURIZATION PROBLEM. CABIN ALTITUDE COULD NOT BE CONTROLLED MANUALLY, O2 MASK DEPLOYED. RETURNED TO ATL. REMOVED AND REPLACED HOSE ASSEMBLY FOR LOWER WATER SEPARATOR DUCT ON RIGHT PACK. REMOVED AND REPLACED HOSE ASSEMBLY FOR UPPER AIR CONDITOct 25, 2000 · N825AT · Doug DC932 · Cabin Pressure Control SystemSDR TWAA0017208Floor Support · corrodedDURING OP 15 MAINT CHECK FOUND CORROSION ON FLOOR SUPPORT AT STA 160, RBL 0 TO 53. FABRICATED NEW SUPPORT PER SRM 53-10-1 AND SPM 6-70-01 AND REPLACED. INSTALLED PER SRM 51-30 PAGE 18.Oct 25, 2000 · N996Z · Doug DC932 · Fuselage Miscellaneous StructureSDR WAA0017207Web · corrodedDURING OP 15 MAINT CHECK FOUND MEMBRANE CORRODED BETWEEN TRACKS 3 AND 4, STA 200 TO 218. REMOVED OLD MEMBRANE AND INSTALLED PER 53-01, PAGE 18. MANUFACTURED AND REPLACED PER SPM 6-70-1.Oct 25, 2000 · N996Z · Doug DC932 · Fuselage Miscellaneous StructureSDR TWAA0017206Floorbeam · corrodedDURING OP 15 MAINT CHECK AT STA 199, BETWEEN RBL 44 AND RBL 53, THE FLOOR WEB WAS CORRODED, JUST AFT OF SERVICE DOOR. REMOVED OLD MEMBRANE AND INSTALLED PER SRM 53-01, PAGE 18.Oct 25, 2000 · N996Z · Doug DC932 · Fuselage Main, Floor BeamSDR TWAA0017205Floorbeam · corrodedDURING OP 15 MAINT CHECK AT STA 180 BETWEEN RBL 44 AND 52, LEVEL ONE CORROSION WAS FOUND ON FLOOR WEB IN 2 LOCATIONS, WHERE FLOOR PANEL RUBBED ON WEB. REMOVED OLD WEB. MANUFACTURED NEW PER SPM 6-70-01. INSTALLED PER SRM 53-01, PAGE 18.Oct 25, 2000 · N996Z · Doug DC932 · Fuselage Main, Floor BeamSDR TWAA0017108Web · damagedDURING OP 15 MAINT CHECK, FOUND REPAIR TO FLOOR MEMBRANE NEEDED REPLACEMENT AT STA 205, RBL 0 TO 20. REMOVED OLD MEMBRANE. MANUFACTURED NEW PER 6-70-01. INSTALLED PER 53-01, PAGE 18.Oct 25, 2000 · N996Z · Doug DC932 · Fuselage Miscellaneous StructureSDR TWAA0017107Floor Support · corrodedDURING OP 15 MAINT CHECK, FOUND 37 INCHES OF FLOOR SUPPORT CORRODED BETWEEN STA 162 AND 200, RBL 43. REPLACED OLD SUPPORT WITH NEW. MADE PER SPM 6-70-1. INSTALLED PER SRM 51-30 PAGE 18.Oct 25, 2000 · N996Z · Doug DC932 · Fuselage Miscellaneous StructureSDR TWAA0017106Floor Support · corrodedDURING OP 15 MAINT CHECK, FOUND 11 INCH LONG SECTION OF FLOOR SUPPORT CORRODED AT STA 200 BETWEEN RBL 44 AND RBL 56, JUST AFT OF SERVICE DOOR. REMOVED OLD SUPPORT. NEW SUPPORT MADE PER SPM 6-70-01 AND SRM 53-10-01. INSTALLED PER SRM 51-30 P18.Oct 25, 2000 · N996Z · Doug DC932 · Fuselage Miscellaneous StructureSDR TWAA0017105Floor Support · corrodedDURING OP 15 MAINT CHECK, THE FLOOR SUPPORT WAS CORRODED AT RBL 0 TO 58 STA 200, AND AT BL 0 AT STA 160 TO 237. REMOVED OLD SUPPORTS. MADE NEW SUPPORTS PER SPM 6-70-01 AND SRM 53-10-1. INSTALLED PER SRM 51-30 PAGE 18.Oct 25, 2000 · N996Z · Doug DC932 · Fuselage Miscellaneous StructureSDR TWAA0017104Floor Panel · crackedDURING OP 15 MAINT CHECK, THE AFT CABIN FLOOR PANEL NUMBER 69 HAD AFT RT CORNER CRACKED AND CORRODED. FABRICATED NEW FLOOR PANEL PER SSRM 53-00-104.Oct 25, 2000 · N996Z · Doug DC932 · Fuselage Floor PanelSDR TWAA0017103Frame · corrodedDURING OP 15 MAINT CHECK, FOUND CORROSION ON FRAME AT STA 503, BETWEEN LONGERONS 28R TO 28L. REMOVED 2 FOOT SECTION OF FRAME AND INSTALLED NEW SECTION PER SRM 53-03, P4A.Oct 25, 2000 · N996Z · Doug DC932 · Fuselage Main, FrameSDR MWEA001110Harness · chafedWHEN GEAR LEVER WAS RAISED, SPARK CAME OUT BEHIND PANEL. FOUND CHAFING WIRE BEHIND GEAR HANDLE QUADRANT. REPOSITIONED WIRE BUNDLE AND SPLICED CHAFING WIRE.Oct 25, 2000 · N302ME · Doug DC932 · Instrument PanelSDR L1GA200000315Retainer · missingNR 2 MLG BOLT RETAINER MISSING .25 INCH X 1 INCH PIECE.Oct 23, 2000 · N14534 · Doug DC932 · BrakeSDR L1GA200000314Bolt · missingNR 2 BRAKE RETAINER BOLT MISSING.Oct 23, 2000 · N12508 · Doug DC932 · BrakeSDR TWAA0016810Splice · crackedDURING OP 15 MAINT CHECK AT STA 555, LONGERON 28L, FOUND A CRACK IN LONGERON SPLICES. INSTALLED NEW SPLICE PER SRM 53-02, FIG 18.Oct 23, 2000 · N996Z · Doug DC932 · Fuselage Miscellaneous StructureSDR TWAA0016809Seat Track · wornDURING OP 15 MAINT CHECK, NUMBER 3 CHAIR TRACK HAD WORN AREA AT STA 208 AND CORROSION AT STA 214 AND 233. REMOVED OLD TRACK AND FABRICATED NEW PER SRM 53-05, SPM 6-70-01, AND INSTALLED PER SRM 51-30.Oct 22, 2000 · N996Z · Doug DC932 · Fuselage, Seat/Cargo Attach FittingsSDR TWAA0016808Seat Track · corrodedDURING OP 15 MAINT CHECK, FOUND NUMBER 4 CHAIR TRACK CORRODED ON TOP BETWEEN STA 200 AND 218, RBL 44, 18 INCHES LONG. REMOVED OLD TRACK AND FABRICATED NEW TRACK PER SRM 53-05, SPM 6-70-01, AND INSTALLED PER SRM 51-30.Oct 22, 2000 · N996Z · Doug DC932 · Fuselage, Seat/Cargo Attach FittingsSDR TWAA0016807Skin · dentedDURING OP 15 MAINT CHECK, FOUND 3 DENTS ON FUSELAGE SKIN AT STA 207, BETWEEN LONGERON 16R AND 18R. DENTS 1 INCH BY 1.5 INCH BY 0.090 DEEP. INSTALLED FLUSH REPAIR PER SRM 53-04, FIG 33.Oct 22, 2000 · N996Z · Doug DC932 · Fuselage Main, Plate/SkinSDR TWAA0016501Skin · damagedTHE FUSELAGE SKIN WAS DAMAGED BY GROUND EQUIPMENT AFT OF THE FWD CARGO DOOR, LOWER LT CORNER AT STA 427. REPAIRED PER DOUGLAS DRAWING SRO9530117-7011 AND ARA 16859 AND EMLR 71243. CHECK-C 10-27-99 STL.Oct 22, 2000 · N998R · Doug DC932 · Fuselage Main, Plate/SkinSDR AT0000475Frame · corrodedFOUND VERTICAL STABILIZER LEADING EDGE UPPER KNEE CUP HAS CORROSION. REMOVED AND REPLACED VERTICAL STABILIZER LEADING EDGE HORSESHOE FORMER IAW DC9 SRM 51-10-02, 51-10-3, 51-10-4, 55-31-0 FIGURE 4.Oct 21, 2000 · N866AT · Doug DC932 · Vertical Stabilizer, Spar/RibSDR AT0000448R1Switch · inoperativeWHEN RIGHT LANDING LIGHT SWITCH WAS ACTIVATED FOR LANDING, SMOKE CAME FROM SWITCH. REMOVED VELCRO/ADHESIVE GLUE FROM BOTTOM OF LANDING LIGHT SWITCHES, REMOVED GLUE.Oct 21, 2000 · N825AT · Doug DC932 · Exterior LightingSDR AT0000448Switch · shortedWHEN RIGHT LANDING LIGHT SWITCH ACTIVATED FOR LANDING, SMOKE CAME FROM SWITCH. COULD NOT DUPLICATE, PULLED CIRCUIT BREAKER AND COLLARED.Oct 21, 2000 · N825AT · Doug DC932 · Exterior LightingSDR TWAA0016806Frame · crackedDURING OP 15 MAINT CHECK, FORMER REPAIR WAS CRACKED APPROX 2.5 INCH LONG, APPROX 3 INCHES UNDER RL 14, STA 980. REWORKED WITH MO 72J15. REMOVED CRACKED FORMER RT SIDE AT STA 908 AND INSTALLED NEW FORMER PER MO 72J14 AND DRAWING JO60119.Oct 20, 2000 · N996Z · Doug DC932 · Fuselage Main, FrameSDR MWEA001058Former · crackedFORMER UPPER RIGHT HAND SIDE OF APB AT STATION 996 IS CRACKED. MAINTENANCE REMOVED AND REPLACED FORMER.Oct 20, 2000 · N302ME · Doug DC932 · Fuselage Main, StructureSDR MWEA00858Gusset · corrodedWEB GUSSET CORRODED BELOW FIRST OFFICER''S CLEARVIEW WINDOW. REMOVED AND REPLACED GUSSET.Oct 20, 2000 · N302ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA00842Former · crackedFORMER AND UPPER OUTBOARD CLIP ON AFT PRESSURE BULKHEAD AT STATION 996 ARE CRACKED. REMOVED AND REPLACED FORMER AND CLIP.Oct 20, 2000 · N302ME · Doug DC932 · Fuselage Main, FrameSDR MWEA00841Clip · misdrilledAFT PRESSURE BULKHEAD, FORWARD SIDE STIFFENER ATTACH CLIP BY LONGERON 7 RIGHT, HAS ONE MISDRILLED HOLE. REMOVED AND REPLACED CLIP.Oct 20, 2000 · N302ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA00838Frame · crackedTOOL MARK ON AFT PRESSURE BULKHEAD FORMER DOUBLER, RIGHT FORWARD SIDE, OUTBOARD ATTACH POINT. REMOVED AND REPLACED FORMER AND CLIP.Oct 20, 2000 · N302ME · Doug DC932 · Fuselage Main, FrameSDR MWEA00859Intercostal · crackedCABIN INTERCOSTAL JUST FORWARD OF FLOORBEAM STATION 756 AND OUTBOARD OF SEAT TRACK NR 3 HAS A CRACK. REMOVED AND REPLACED INTERCOSTAL.Oct 20, 2000 · N302ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA00857Intercostal · crackedINTERCOSTAL CRACKED AT STATION 484 ATTACHMENT AT LONGERON 6 RIGHT. REMOVED AND REPLACED INTERCOSTAL.Oct 20, 2000 · N302ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA00856Intercostal · crackedINTERCOSTAL CRACKED AT INBOARD ATTACHMENT STATION 484, LONGERON 6 LEFT. REMOVED AND REPLACED INTERCOSTAL.Oct 20, 2000 · N302ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA00855Web · crackedCABIN SUBFLOOR OUTBOARD OF SEAT TRACK NR 4 AT STATION 756 IS CRACKED AND HAS LIGHT CORROSION AND MISSING FOUR FASTENERS. FABRICATED AND INSTALLED REPAIR DOUBLER.Oct 20, 2000 · N302ME · Doug DC932 · Fuselage Miscellaneous Structure
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