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 VJ9800609Skin · dentedDENT AT FS 213.5L, L16-17, .023 X 1/2 DX=22, OUT OF LIMIT PER SRM 53-04, FIG 38, SHEET 10. COLD WORKED DENTS, VERIFIED NO CRACKS BY HFEC, FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC9 SRM 51-04, FIG 38 AND 51-10-2.Nov 3, 1998 · N937VV · Doug DC932 · Fuselage Main, Plate/SkinSDR VJ9800576Power Supply · inopLT OVERHEAD EMERGENCY LIGHT AT ROW 24 INOP. REPLACED BATTERY POWER SUPPLY IAW MM 33-51.Nov 3, 1998 · N903VJ · Doug DC932 · Emergency LightingSDR VJ9800637Support · corrodedDURING A SCHEDULED INSPECTION, THE FORWARD CABIN FLOORING SUPPORT STRUCTURE TEE CAP RUNNING DOWN THE CENTER LINE AT FS 237 WAS FOUND WITH CORROSION ON THE UPPER SURFACE AND AROUND FASTENER HOLES. REMOVED THE SUPPORT, FABRICATED AND INSTALLED A NEW SUPPORT IAWNov 2, 1998 · N947VV · Doug DC932 · Fuselage Miscellaneous StructureSDR VJ9800627Angle · crackedZ-ANGLE AT FS 160 TO 200 LT FOUND CRACKED AND MATERIAL MISSING. REMOVED, FABRICATED AND INSTALLED NEW Z-ANGLE IAW DC9 SRM 51-30-2, 51-30-8, 51-20-0, 51-10-4, 51-10-1.Nov 2, 1998 · N947VV · Doug DC932 · Fuselage Miscellaneous StructureSDR VJ9800626Support · corrodedFLOOR SUPPORT (60-2576) AT FS 200, T-CAP UPPER SURFACE AND FASTENER HOLES AT FS 160 TO 219 CORRODED. REMOVED, FABRICATED AND INSTALLED NEW FLOOR SUPPORT IAW DC9 SRM 51-10-3, 51-30-2, 51-10-4, 51-10-3 53-01, FIG 1.Nov 2, 1998 · N947VV · Doug DC932 · Fuselage Miscellaneous StructureSDR ABXA9800941Skin · crackedDURING C-CHECK, FOUND FUSELAGE SKIN AT RIGHT AFT NOSE GEAR DOOR HINGE CUTOUT STATION 100 CRACKED. REPAIRED SKIN IAW DC9 SRM 53-05.Nov 2, 1998 · N985AX · Doug DC932 · Fuselage Main, Plate/SkinSDR ABXA9800940Skin · crackedDURING C-CHECK, FOUND THE FORWARD LOWER CARGO COMPARTMENT DOOR EXTERIOR SKIN CRACKED IN SEVERAL PLACES AT THE DOOR PAN ATTACH RIVETS. REPAIRED DOOR SKIN IAW ABX REA D952-25273.Nov 2, 1998 · N985AX · Doug DC932 · Cargo/Baggage DoorsSDR ABXA9800939Bulkhead Frame · corrodedDURING C-CHECK, FOUND THE AFT PRESSURE BULKHEAD DOOR LOWER FRAME CORRODED. REPAIRED FRAME IAW DC9 SRM 51-30-2 AND 51-30-5.Nov 2, 1998 · N985AX · Doug DC932 · Nacelle/Pylon, Bulkhead/FirewallSDR ABXA9800938Longeron · crackedDURING C-CHECK, FOUND LONGERON 17R CRACKED AT PYLON BULKHEAD STATION 965. REPLACED LONGERON SECTION IAW DC9 SRM 51-30-2 AND 51-30-5.Nov 2, 1998 · N985AX · Doug DC932 · Fuselage Main, Longeron/StringerSDR ABXA9800937Bulkhead Fitting · crackedDURING C-CHECK, FOUND THE VENTRAL DOOR LOWER, LEFT STOP SUPPORT FITTING CRACKED. REPLACED FITTING IAW DC9 SRM 51-30-2 AND 51-30-5.Nov 2, 1998 · N985AX · Doug DC932 · Fuselage Main, BulkheadSDR ABXA9800936Rib · crackedDURING C-CHECK, FOUND FORWARD UPPER EDGE OF NR 1 PYLON RIB CRACKED INSIDE ACCESS PANEL AREA 8111. REPAIRED RIB IAW ABX DC9 SSRM DWG K05159.Nov 2, 1998 · N985AX · Doug DC932 · Nacelle/Pylon, Frame/Spar/RibSDR ABXA9800935Angle · crackedDURING C-CHECK, FOUND NR 2 PYLON TO FUSELAGE ATTACH ANGLE CRACKED BENEATH THE PYLON LEADING EDGE. REPLACED ANGLE IAW DC9 SRM 54-04.Nov 2, 1998 · N985AX · Doug DC932 · Nacelle/Pylon StructureSDR ABXA9800934Bulkhead Skin · crackedDURING C-CHECK, FOUND THE AFT SIDE OF THE AFT PRESSURE BULKHEAD SKIN CRACKED AT THE RIGHT SIDE OF VENTRAL DOOR CUTOUT APPROX 30 INCHES ABOVE FLOOR LINE. REPAIRED IAW DC9 SRM 53-05.Nov 2, 1998 · N985AX · Doug DC932 · Fuselage Main, BulkheadSDR VJ9800625Skin · corrodedRT WING LOWER SURFACE O/B TRAILING EDGE WING SKIN CORRODED AT XRS 509.5 - XRZ 531.7. REMOVED, FABRICATED AND INSTALLED NEW SKIN IAW DC9 SRM 51-20-0, 51-30-2, 57-31-3, 51-10-4, AND 51-30-9.Oct 31, 1998 · N947VV · Doug DC932 · Wing, Plate/SkinSDR VJ9800624Angle · corrodedNR 2 GALLEY ICE DRAWER CORRODED ON BEAM. REMOVED, FABRICATED AND INSTALLED NEW ANGLE IAW DC9 SRM 51-30-1, 51-10-3, 51-10-2.Oct 30, 1998 · N947VV · Doug DC932 · Buffet/GalleysSDR MWEA981031Pan · crackedFOUND CRACK ON FORWARD CARGO DOOR PAN FORWARD EDGE JUST BELOW FORWARD TORQUE TABLE. MTC FABRICATED AND INSTALLED DOUBLER.Oct 30, 1998 · N204ME · Doug DC932 · Cargo/Baggage DoorsSDR ABXA9800931Switch · defectiveWHEN LANDING GEAR WAS EXTENDED, GEAR DOOR OPEN LIGHT WOULD NOT EXTINGUISH. RECYCLED GEAR, LIGHT WOULD NOT GO OUT WITH GEAR IN THE UP POSTION. PERFORMED ABNORMAL PROCEDURE. LANDING WAS UNEVENTFUL. REPLACED RIGHT INBOARD GEAR DOWN SWITCH.Oct 30, 1998 · N902AX · Doug DC932 · Landing Gear Position and WarningSDR ABXA9801158Skin · crackedRIGHT MAIN LANDING GEAR DOOR HAD 2 CRACK ON LOWER SKIN SURFACE. REPAIRED UNIT IAW DC9 SRM.Oct 29, 1998 · N985AX · Doug DC932 · Landing Gear DoorsSDR VJ9800608Skin · corrodedFRAME BLENDED OUT IN RADIOUS 45 INCHES FROM AFT STAIRS, LT SIDE, AT FS 1089. FABRICATED AND INSTALLED TWO L-ANGLES REPAIRS IAW DC9 SRM 51-30-2, 51-10-3 AND 53-01, PG 10.Oct 28, 1998 · N937VV · Doug DC932 · Fuselage Main, Plate/SkinSDR MWEA981028Skin · damagedPREVIOUS REPAIR ON FORWARD CARGO BELLY SKIN AT STATION 565 DOES NOT MEET SRM REQUIREMENTS. MTC FABRICATED AND INSTALLED SKIN SPLICE REPAIR.Oct 28, 1998 · N202ME · Doug DC932 · Fuselage Main, Plate/SkinSDR MWEA981027Skin · corrodedFOUND CORROSION ON INTERIOR SKIN AT FS 579 BETWEEN LONGERON 29R AND 30R. MTC FABRICATED AND INSTALLED DOUBLER.Oct 28, 1998 · N202ME · Doug DC932 · Fuselage Main, Plate/SkinSDR VJ9800561Connector · failedLIGHT FOR EMERGENCY FLOOR PATH LIGHTING INOP AT ROW 10. REPAIRED FAULTY CONTACT, SYSTEM OPS CHECKED GOOD IAW MM 33-50.Oct 27, 1998 · N935VV · Doug DC932 · Emergency LightingSDR CALA9802004Megaphone · inopINSPECTION FOUND FORWARD MEGAPHONE INOPERATIVE. THE MEGAPHONE WAS REPLACED.Oct 27, 1998 · N14534 · Doug DC932 · Emergency EquipmentSDR VJ9800623Angle · corrodedRT NLG DOOR SEAL STRIKER ANGLE CORRODED FROM FWD TO AFT END. REPLACED ANGLE IAW DC9 SRM 51-10-1 AND 51-30-2.Oct 26, 1998 · N947VV · Doug DC932 · Landing Gear DoorsSDR MWEA981019Slide Cover · fell offFORWARD ENTRANCE DOOR EVACUATION SLIDE COVER FELL OFF. REINSTALLED FWD ENTRANCE DOOR EVACUATION SLIDE COVER.Oct 25, 1998 · N209ME · Doug DC932 · Emergency EquipmentSDR MWEA981018Slide Cover · fell offTHE FORWARD EMERGENCY DOOR SLIDE COVER FELL OFF. MTC REINSTALLED THE SLIDE COVER.Oct 25, 1998 · N209ME · Doug DC932 · Emergency EquipmentSDR MWEA981015Battery Pack · dischargedFOUND LEFT AND RIGHT FORWARD WING OVERHEAD EMERGENCY EXIT SIGN INOPERATIVE. MTC REMOVED AND REPLACED EMERGENCY BATTERY PACK.Oct 23, 1998 · N203ME · Doug DC932 · Emergency LightingSDR VJ9800620Skin · dentedFUSELAGE SKIN AT FS 218 TO 588R, L18-L27, DENTED. REPLACED SKIN IAW DC9 SRM 51-10-4, 51-10-3, 51-30-2, MM 34-10-0 AND AIRTRAN RES 191790 WITH DER APPROVAL BY DM BURCH NR NM1034.Oct 22, 1998 · N937VV · Doug DC932 · Fuselage Main, Plate/SkinSDR VJ9800619Mechanism · corrodedRT O/B SPOILER CAM ARM, TORSION ARM AND TORSION BAR AT XRS 307, SERRATION FOUND PITTED CORRODED. REPLACED TORSION BAR (3920944-503), CAM ARM ASSY ( 3923153-505) AND TORSION ARM (3920944-503) IAW DC9 MM 27-61-1 AND 27-61-6.Oct 22, 1998 · N937VV · Doug DC932 · Drag Control SystemSDR VJ9800607Skin · dentedDENT AT FS 171R-172R, L22-23, .009 X .0250 AND .009 X .0250, DEPTH .009, DX=28, CONDITION 1 B, TOO CLOSE TOGETHER PER DC9 SRM 53-04, FIG 38, SHEET 10, NOTE 3. COLD WORKED DENTS, VERIFIED NO CRACK BY HFEC, FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC9 SRM 51Oct 22, 1998 · N937VV · Doug DC932 · Fuselage Main, Plate/SkinSDR VJ9800606Skin · dentedDENT AT FS 945-966, L22R, .021X1.5, DEPTH .026 DX=58, OUT LIMIT IAW DC9 SRM 53-04, FIG 38, SHEET 10. COLD WORKED AREA, VERFIED NO CRACK BY HFEC, FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC9 SRM 53-04, FIG 38, 51-30-2 AND AIRTRAN RES 981842.Oct 22, 1998 · N937VV · Doug DC932 · Fuselage Main, Plate/SkinSDR VJ9800605Skin · dentedDENT AT FS 953.5-968, L25-26R, .070 X .125, DEPTH .090 DX=35, 0UT LIMIT PER DC9 SRM 53-04, FIG 38, SHEET 10, CONDITION B. COLD WORKED DENTS, CONFIRMED NO CRACK BY HFEC, FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC9 SRM 53-04, FIG 38 AND 53-04, FIG 3.Oct 22, 1998 · N937VV · Doug DC932 · Fuselage Main, Plate/SkinSDR VJ9800604Skin · dentedDENT AT FS 960.5. L25R, .012 X 1 AND .026 X 1.1, TOTAL DEPTH .014 AND .028, DX=71 AND 39 RESPECTIVELY, OUT OF LIMIT PER DC9 SRM 53-04, FIG 38, CONDITION 1 B. COLD WORKED DENT, VERIFIED NO CRACKS BY HFEC. FABRICATED AND INSTALLED REPAIR DOUBLER, SPLICE AND SHOct 22, 1998 · N937VV · Doug DC932 · Fuselage Main, Plate/SkinSDR VJ9800603Skin · dentedDENT AND BULGE IN AFT ENTRY DOOR SKIN AT FS 1092 AND 1097. .033 X 1/14 AND .106 X 3, TOO CLOSE TO EACH OTHER AND ARE OUT OF LIMIT IAW DC9 SRM 51-50-1, FIG 12A. REMOVED AND INSTALLED NEW SKIN IAW DC9 SRM 51-10-4, 51-30-2, 51-30-1.Oct 22, 1998 · N937VV · Doug DC932 · Fuselage Main, Plate/SkinSDR VJ9800602Torsion Bar · corrodedRT O/B SPOILER TORSION BAR SERRATION AT STA XRS307 PITTED CORROSION BEYOND LIMIT. REMOVED TORSION BAR AND REPLACED WITH SERVICEABLE PARTS. INSTALLED TORSION BAR ASSY AND CHECK SYSTEM IAW DC9 MM 27-61-6, OPS CHECKED GOOD IAW MM 27-61-6.Oct 22, 1998 · N937VV · Doug DC932 · Drag Control SystemSDR VJ9800595Skin · crackedA NON-CONFORMING REPAIR FOUND AT FS 464 TO 486, LBL 4.5 AND RBL 4.5. REMOVED ANTENNA DOUBLER, STOP DRILLED CRACKS, FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW DC9 SRM 53-01 FIG 1, 53-04 FIG 3B, 51-10-3, 51-10-4, 51-30-2 AND DOUGLAS DRAWING SRO 9530Oct 22, 1998 · N937VV · Doug DC932 · Fuselage Main, Plate/SkinSDR GTIA9800119Wire · looseACY - FLT 876A - LAST SIX EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE. FOUND WIRE DISCONNECTED. RECONNECTED WIRE, OPERATIONAL CHECK GOOD IAW 33-53-0. (M)Oct 22, 1998 · N12536 · Doug DC932 · Light System WiringSDR ABXA9800927Socket · inoperativeTHE GEAR DOOR OPEN LIGHT DID NOT ILLUMINATE WHEN THE LANDING GEAR LEVER WAS PUT IN THE DOWN POSITION DURING APPROACH. REPLACED THE GEAR DOOR OPEN LIGHT SOCKET.Oct 22, 1998 · N986AX · Doug DC932 · Landing Gear Position and WarningSDR VJ9800601Skin · dentedDENTS AT FS 157R, L18, FS 160R, L18-19, FS 161R, L19, FS 163R, L19. FOUND DENT AT FS 157R, L18 TO BE CONDITION 1B. CONFIRMIED NO CRACKS BY HFEC. REPETITIVELY INSPECT FOR CRACKS ANNUALLY OR AT C-CHECK PER DC9 SRM 53-04, FIG 38, SHEET 10.Oct 21, 1998 · N937VV · Doug DC932 · Fuselage Main, Plate/SkinSDR VJ9800600Skin · dentedDENTS AT FS 207R, L18-19, FS 210R, L19, AND FS 212R, L18, LESS THAN 3 INCHES APART AND OUT OF LIMIT IAW DC9 SRM 53-04, FIG 38, CONDITION 1 AND 2. DAMAGE REPAIRED IAW AIRTRAN RES 981791. HFEC INSPECTION ACCOMPLISHED AND NO CRACKS. REINSPECT CRACKS ANNUALLY OOct 21, 1998 · N937VV · Doug DC932 · Fuselage Main, Plate/SkinSDR VJ9800599Skin · dentedDENT AT FS 256R, L17R .045X1 DX=22. ADDITIONAL DENTS AT FS 250, L18-17, FS 252. L17, FS 253, L17, FS 256, L16-17, FS 258, L16, FS 260, L17, LESS THAN 3 INCHES APART AND OUT OF LIMIT IAW DC9 SRM 53-04, FIG 38. VERIFIED NO CRACKS BY HFEC. FABRICATED AND INSTALOct 21, 1998 · N937VV · Doug DC932 · Fuselage Main, Plate/SkinSDR VJ9800598Panel · corrodedCORROSION ALONG I/B EDGE PANEL 2017 FROM CENTER OF BELLY AT WHEEL WELL FS 756 TO THUMB NAIL PANEL AT FS 813. CORROSION AT FS 813 OUT OF LIMIT. FABRICATED AND INSTALLED DOUBLER REPAIR IAW DC9 SRM 51-10-3, 53-04, FIG 53 AND 53-01, FIG 3.Oct 21, 1998 · N937VV · Doug DC932 · Fuselage Main, Plate/SkinSDR VJ9800597Skin · dentedDENTS AT FS 927R AND 929R, L24, .053X2 DX=38, .029X2 DX=69, 0UT LIMIT IAW DC9 SRM 53-04, FIG 38. COLD WORKED DENTS, VERIFIED NO CRACKS BY HFEC, FABRICATED AND INSTALLED DOUBLER IAW DC9 SRM 53-04, FIG 38 AND 51-30-1.Oct 21, 1998 · N937VV · Doug DC932 · Fuselage Main, Plate/SkinSDR VJ9800596Skin · dentedDENTS AT FS 1109R AND 1116R, L22X.035X1, DX=29, .016 1/2 DX=32, CREASED AND OUT OF LIMIT IAW DC9 SRM 53-04, FIG 38. COLD WORKED DENT, PERFORMED HFEC TO VERIFY NO CRACKS, FABRICATED AND INSTALLED DOUBLERS IAW DC9 SRM 51-10-4, 53-01, FIG 2, 51-30-2.Oct 21, 1998 · N937VV · Doug DC932 · Fuselage Main, Plate/SkinSDR VJ9800556Battery · dischargedCOCKPIT ENTRANCE EMERGENCY EXIT LIGHT INOP. REPLACED POWER PACK BATTERIES, OPS CHECKED GOOD.Oct 21, 1998 · N966VV · Doug DC932 · Emergency LightingSDR CALA9801984Switch · inopTHE GEAR DOOR OPEN LIGHT REMAINED ILLUMINATED AFTER GEAR WAS EXTENDED FOR LANDING AT IAH. THE L/H AND R/H MLG DOORS WERE DAMAGED ON LANDING. MAINTENANCE REMOVED AND REPLACED THE L/H MLG DOOR SWITCH. BOTH L/H AND R/H MLG DOORS WERE REMOVED AND REPLACED IAW MM 3Oct 21, 1998 · N33506 · Doug DC932 · Landing Gear Position and WarningSDR VJ9800618Vane · corrodedLT WING CENTER FIXED VANE FLAP L/E CORRODED. REPLACED FIXED VANE IAW DC9 MM 27-51-3. FIT AND FAIRED, OPS CHECKED GOOD IAW DC9 MM 27-51-3.Oct 20, 1998 · N937VV · Doug DC932 · Wing Miscellaneous StructureSDR MWEA981013Battery Pack · dischargedFOUND THE RIGHT NACELLE EMERGENCY LIGHT INOPERATIVE. MTC REMOVED AND REPLACED BATTERY PACK.Oct 20, 1998 · N501ME · Doug DC932 · Emergency LightingSDR TWAA9816901Fuel Pump · failedNR 2 ENGINE HAD NO RESPONSE TO THROTTLE MOVEMENT. RETURNED TO BDL. ENGINE WAS SHUT DOWN ON APPROACH. REPLACED FUEL PUMP DUE TO HIGH STAGE FAILURE. CHECK-C 4-24-98 STL.Oct 19, 1998 · N932L · Doug DC932 · Engine Fuel PumpSDR MWEA981014Slide · looseUPON LANDING FORWARD PASSENGER EMERGENCY SLIDE CAME LOOSE. MTC REINSTALLED FORWARD PASSENGER EMERGENCY SLIDE.Oct 19, 1998 · N209ME · Doug DC932 · Emergency Equipment
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