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 VJ9800472Tee · corrodedTEE CAP, STA 600. 28L-28R, CORRODED. DRILLED. LOCATED, DEBURRED AND INSTALLED NEW TEE CAP IAW DC9 SRM 51-10-4, 51-30, 51-20 AND DC9 DWG 5010068.Sep 15, 1998 · N933VV · Doug DC932 · Fuselage Miscellaneous StructureSDR VJ9800444Skin · gougedSKIN AT FS 962, L25R, GOUGED BEYOND LIMIT IAW DC9 SRM 53-04, FIG 38. CUT OUT GOUGE, FABRICATED AND INSTALLED EXTERNAL AND FINGER DOUBLERS IAW DC9 SRM 53-04, FIG 38, 51-10-3 AND 51-30-2.Sep 15, 1998 · N911VV · Doug DC932 · Fuselage Main, Plate/SkinSDR VJ9800430Floor · corrodedCENTER PANEL UNDER NR 3 GALLEY AT FS 200.0 CORRODED BEYOND LIMIT. TREATED AREA, FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC9 SRM 51-10-3, 51-30-2 AND 53-01.Sep 15, 1998 · N936VV · Doug DC932 · Fuselage Floor PanelSDR MWEA98962Cover · looseMCO - FLT 90 - FORWARD ENTRY DOOR EVACUATION SLIDE COVER FELL OFF. REINSTALLED FWD ENTRY DOOR EVAC SLIDE COVER. (X)Sep 15, 1998 · N302ME · Doug DC932 · Emergency EquipmentSDR CALA9801778Skin · crackedINSPECTION FOUND TOP OF FUSELAGE AFT ADF LOOP ANTENNA MOUNTING SURFACE EXTERNAL SKIN CRACKED AT RT CENTER MOUNT HOLE, STA 259 LONGERON 1R, BL 0 AND AT RT MOUNT HOLE, STA 265, LONGERON 1R, BL 0. BOTH CRACKS WERE .375 INCH LONG. THE CRACKED AREAS OF SKIN WERE Sep 15, 1998 · N70542 · Doug DC932 · Fuselage Main, Plate/SkinSDR VJ9800557Skin · crackedA CRACK INDICATION AT COUNTER SUNK HOLE FOUND AT FS 194, L22L. CUT OUT CRACKED SECTION OF SKIN, FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW DC9 MM 51-00-0, SB 53-251 AND EO 12-5310-29-B1078.Sep 14, 1998 · N936VV · Doug DC932 · Fuselage Main, Plate/SkinSDR VJ9800389Slide · detachedDOOR SLIDE DISLODGED FROM GALLEY DOOR. REINSTALLED SLIDE IAW MM 25-00 AND PERFORMED REQUIRED INSPECTIONS.Sep 14, 1998 · N932VV · Doug DC932 · Emergency EquipmentSDR VJ9800380Power Supply · inoperativeRT AND LT EXIT SIGNS AT OVERWING DO NOT ILLUMINATE. REPLACED BATTERY POWER SUPPLY IAW MM 33-53.Sep 14, 1998 · N924VV · Doug DC932 · Emergency LightingSDR CALA9801752Fairing · delaminatedINSPECTION FOUND LT HORIZONTAL STABILIZER UPPER FAIRING DELAMINATED FROM AFT ATTACH POINT FORWARD. REMOVED PAN ON LOWER SURFACE AND REMOVED DELAMINATED HONEYCOMB. NEW HONEYCOMB WAS BONDED IN LOWER PAN AND THEN PAN WAS INSTALLED ON FAIRING AND BONDED IAW SRM 5Sep 14, 1998 · N70542 · Doug DC932 · Horizontal Stabilizer StructureSDR CALA9801751Fairing · delaminatedINSPECTION FOUND RT LOWER HORIZONTAL STABILIZER FAIRING DELAMINATED AT FWD END. THE DELAMINATED HONEYCOMB CORE, DOUBLER, AND PLATE WERE REMOVED. BONDED DOUBLER WITH HONEYCOMB CORE AND PLATE TO SKIN FAIRING IAW ECRA 5510-01317, SRM 51-70-2, 51-30-2.Sep 14, 1998 · N70542 · Doug DC932 · Horizontal Stabilizer StructureSDR CALA9801750Frame · gougedINSPECTION FOUND FRAME GOUGED AT STA 332, LONGERON 29L TO 30. A SPLICE AND PLATE REPAIR WAS INSTALLED IAW SRM 53-03, FIGURE 2A AND 51-10-2A.Sep 14, 1998 · N70542 · Doug DC932 · Fuselage Main, FrameSDR CALA9801749Fitting · gougedINSPECTION FOUND FLAP FITTING GOUGED AT AFT END OF LT WING AFT MOVEABLE VANE INBOARD TRACK STA XFLS 65.612 TO 69.125. THE FITTING WAS REMOVED AND REPLACED IAW SRM 51-30-2.Sep 14, 1998 · N70542 · Doug DC932 · Trailing Edge FlapsSDR CALA9801748Web · crackedINSPECTION FOUND THREE 2 INCH CRACKS ON NR 1 ENGINE PYLON INTERNAL WEB AT STA 1065. THE CRACKS WERE STOP DRILLED IAW SRM 51-10-1. A REPAIR WAS INSTALLED IAW SRM 51-10-3 AND 54-01, FIGURE 2.Sep 14, 1998 · N70542 · Doug DC932 · Nacelle/Pylon StructureSDR CALA9801747Tab · delaminatedINSPECTION FOUND TWO AREAS OF DELAMINATION ON UPPER SURFACE OF LT ELEVATOR CONTROL TAB BETWEEN THIRD AND OUTBOARD HINGES. THE DELAMINATED AREAS WERE TRIMMED OUT AND FILLER AND DOUBLER WERE INSTALLED IAW SRM 51-70-2.Sep 14, 1998 · N70542 · Doug DC932 · Elevator, Tab StructureSDR CALA9801746Skin · crackedINSPECTION FOUND A 1 INCH CRACK IN FUSELAGE SKIN AT STA 950, THREE INCHES BELOW LONGERON 14L. THE CRACKED AREA WAS REMOVED IAW SRM 53-04, FIGURE 38. A DOUBLER AND FILLER REPAIR WAS INSTALLED IAW SRM 51-10-3 AND 53-04, FIGURE 38.Sep 14, 1998 · N70542 · Doug DC932 · Fuselage Main, Plate/SkinSDR ABXA9800827Batteries · dischargedWHEN TESTING EMERGENCY LIGHTS, LIGHTS WENT FROM DIM TO OFF IN 5 SECS. REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERIES.Sep 14, 1998 · N982AX · Doug DC932 · Emergency LightingSDR VJ9800379Connector · dirtyNR 1 ENGINE B-LOOP LIGHT ILLUMINATED IN FLIGHT, A-LOOP OK. CLEANED ELECTRICAL CONNECTOR ON NR 1 ENGINE IAW MM 26-00, OPS CHECKED GOOD.Sep 13, 1998 · N967VV · Doug DC932 · Fire DetectionSDR VJ9800378Batteries · dischargedEMERGENCY LIGHTS ABOVE TAIL CONE SLIDE DIDN'T ILLUMINATE. REPLACED NICAD BATTERIES IN EMERGENCY BATTERY PACK, OPS CHECKED GOOD.Sep 13, 1998 · N923VV · Doug DC932 · Emergency LightingSDR VJ9800549Skin · corrodedFUSELAGE SKIN AT FS 579, L30, CORRODED. CUT OUT SECTION OF SKIN, FABRICATED AND INSTALLED EXTERNAL DOUBLER AND FINGER DOUBLERS IAW DC9 SRM 53-04 FIG 12B, 51-10-3, 51-30-1.Sep 12, 1998 · N911VV · Doug DC932 · Fuselage Main, Plate/SkinSDR VJ9800478Frame · crackedMAIN FRAME RT FS 966 CRACKED. REPLACED FRAME IAW AIRTRAN EO 12-5311-29-B1044 AND RES 981533.Sep 12, 1998 · N911VV · Doug DC932 · Fuselage Main, FrameSDR VJ9800410Control Cable · out of adjAFTER TAKEOFF, FLIGHT CREW WAS UNABLE TO RAISE GEAR HANDLE. AS PRECAUTIONARY MEASURE FLIGHT CREW ELECTED TO RETURN TO ATL MAINTENANCE BASE. ADJUSTED ANTI RETRACTION CABLE WHICH WAS FOUND TO BE OUT OF TOLERANCE IAW MM 32-23-1, PERFORMED GEAR SWING AND ALL CHESep 12, 1998 · N912VV · Doug DC932 · Landing Gear Retraction/Extension SystemSDR VJ9800377Manifold · inoperativeALL PASSENGER OXYGEN MASKS DEPLOYED WHEN CREW TURNED ON OXYGEN. REPLACED REGULATOR (P/N 900-002-007-6), (S/N 425). SUSEQUENTLY REPACKED MASKS AND PERFORMED OXYGEN MASK DROP AND ALL EXCEPT PASSENGER SEAT ROW 24DEF SUCESSFULLY DEPLOYED. REPLACED PASSENGER OXYSep 12, 1998 · N945VV · Doug DC932 · Passenger Oxygen SystemSDR TWAA9814704Windshield · crackedTHE CAPTAIN'S NR 1 WINDOW CRACKED WITH ARCING VISIBLE. FLIGHT RETURNED TO STL. REPLACED WINDOW. CHECK-C 3-2-98 STL.Sep 12, 1998 · N923L · Doug DC932 · Flight Compartment WindowsSDR VJ9800551Floorbeam · corrodedAFT RT LAV FLOORBEAM AT FS 996 CORRODED FROM FUSELAGE TO LAV ENTRANCE. REMOVED RT CABLE RUN AND RT O/B PULLEY TOWER. CUT OUT CORRODED SECTION, TREATED AREA, FABRICATED AND INSTALLED FLOORBEAM SPLICE, FLOORBEAM WEB, ATTACH ANGLE, ANGLES AND ATTACH ANGLE BRACKSep 11, 1998 · N911VV · Doug DC932 · Fuselage Main, Floor BeamSDR VJ9800550Z Section · corrodedAFT CABIN CENTER Z SECTION AT FS 945, RBL 2-20 AND LBL 2-20, CORRODED FROM BULKHEAD TO BULKHEAD. CORROSION OUT OF LIMIT IAW DC9 SRM 53-01, FIG 1. BROKE CABLE TENSION ON RUNS 129 AND 130 AND REMOVED CABLE BRACKETS. FABRICATED AND INSTALLED Z SECTION REPAIRS Sep 11, 1998 · N911VV · Doug DC932 · Fuselage Miscellaneous StructureSDR VJ9800471Chord · corrodedTEE CHORD HAS TONG CUT OFF AND CORROSION AT STA 996, L30. REMOVED TEE CHORD AT FS 996, L23L-29R, DRILLED DEBURRED, ALODINED, PRIMED AND INSTALLED NEW TEE CHORD IAW DC9 SRM 53-03, FIG 37A, SB 53-232.Sep 11, 1998 · N933VV · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA98961Cover · detachedFORWARD ENTRANCE DOOR EVACUATION SLIDE COVER FELL OFF. REINSTALLED EVACUATION SLIDE COVER.Sep 11, 1998 · N302ME · Doug DC932 · Emergency EquipmentSDR ABXA9800880Angle · crackedWHILE COMPLYING WITH C-INSPECTION, FOUND A CRACK IN THE NR 1 ENGINE PYLON UPPER ATTACH ANGLE AT FS 980. REPAIRED CRACK IAW DC9 SRM CHAPTER 53-04.Sep 11, 1998 · N903AX · Doug DC932 · Nacelle/Pylon StructureSDR ABXA9800826Membrane · crackedDURING C-CHECK, FOUND THE SUBFLOOR MEMBRANE CRACKED AT STATION 120 ABOVE THE AILERON LOAD FEEL CENTERING SPRING ON RIGHT SIDE. REPAIRED SUBFLOOR MEMBRANE IAW DC-9 SRM 53-01.Sep 11, 1998 · N939AX · Doug DC932 · Fuselage Miscellaneous StructureSDR ABXA9800825Spar Cap · corrodedDURING C-CHECK, FOUND RIGHT WING UPPER SPAR CAP CORRODED BEYOND LIMITS UNDER AND AROUND THE NUT PLATE JUST OUTBOARD OF RIGHT AILERON. REPAIRED IAW ABX REA D957-24791-MR.Sep 11, 1998 · N939AX · Doug DC932 · Wing SparSDR ABXA9800824Blkhd Stiffener · crackedDURING C-CHECK, FOUND STIFFENER CRACKED, RIGHT SIDE OF AFT PRESSURE BULKHEAD DOOR JAMB APPROXIMATELY 18 ABOVE FLOOR. REPLACED STIFFENER IAW DC-9 SRM 51-30-5 AND 51-30-2.Sep 11, 1998 · N939AX · Doug DC932 · Fuselage Main, BulkheadSDR ABXA9800823Longeron · crackedDURING C-CHECK, FOUND LONGERONS 17L AND 17R CRACKED AT STATION 965 AND 980. REPAIRED LONGERONS IAW DC-9 SRM 53-02.Sep 11, 1998 · N939AX · Doug DC932 · Fuselage Main, Longeron/StringerSDR ABXA9800822Longeron · crackedDURING C-CHECK, FOUND LONGERON 16R CRACKED AT STATION 965. REPAIRED LONGERON IAW DC-9 SRM 53-02.Sep 11, 1998 · N939AX · Doug DC932 · Fuselage Main, Longeron/StringerSDR ABXA9800821Fitting · crackedDURING C-CHECK, FOUND RIGHT OUTBOARD SPOILER TORSION BAR CENTER SUPPORT FITTING CRACKED. REPLACED FITTING IAW DC-9 SRM 51-30 AND 51-30-2.Sep 11, 1998 · N939AX · Doug DC932 · SpoilersSDR ABXA9800820Longeron · crackedDURING C-CHECK, FOUND LONGERON 4L CRACKED AT STATION 160. REPAIRED LONGERON IAW DC-9 SRM 53-02.Sep 11, 1998 · N939AX · Doug DC932 · Fuselage Main, Longeron/StringerSDR VJ9800554Skin · dentedTHE AFT VENTRAL STAIRS CONTAINED 27 DENTS TOO CLOSE TOGETHER IAW DC9 SRM 51-50-1, FIG 1-2A. REPLACED LOWER SKIN AND CORRODED FITTING IAW DC9 SRM 51-30-5, 51-30-0, 51-10-4 AND MM 52-63-0 PG 501.Sep 10, 1998 · N911VV · Doug DC932 · Entrance StairsSDR VJ9800553Floor · corrodedAFT GALLEY FLOOR PANEL CORRODED. REMOVED FLOOR PANEL, FABRICATED AND INSTALLED NEW HAT SECTIONS AND FLOOR PANEL IAW DC9 SRM 51-20-0, 51-30-2, 53-21-0, FIG 4 AND 51-10-3.Sep 10, 1998 · N911VV · Doug DC932 · Fuselage Floor PanelSDR VJ9800552Longeron · corrodedFORWARD PIT UNDER AUX TANK AT FS 579, L30, CORRODED. REPLACED L30 AT FS 579 IAW DC9 SRM 53-02 FIG 14.Sep 10, 1998 · N911VV · Doug DC932 · Fuselage Main, Longeron/StringerSDR VJ9800511Skin · corrodedAFT VENTRAL STAIRS HAD DENTS TOO CLOSE TOGETHER IAW DC9 SRM 51-50-1, FIG 1-2A. REPLACED LOWER SKIN AND CORRODED FITTING IAW DC9 SRM 51-30-5, 51-30-0, 51-10-4 AND MM 52-63-0, PG 501.Sep 10, 1998 · N911VV · Doug DC932 · Entrance StairsSDR VJ9800475Skin · corrodedLAP SEAM AT FS 200, L26L, CORRODED. CUT OUT AREA, FABRICATED AND INSTALLED REPAIR DOUBLERS AND FILLER IAW DC9 SRM 53-04, FIG 37.Sep 10, 1998 · N966VV · Doug DC932 · Fuselage Main, Plate/SkinSDR MWEA98960Battery Pack · dischargedFOUND RIGHT NACELLE EMERGENCY LIGHT INOP. MAINTENANCE REMOVED AND REPLACED RIGHT NACELLE EMERGENCY LIGHT BATTERY PACK.Sep 10, 1998 · N501ME · Doug DC932 · Emergency LightingSDR MWEA98959Battery Pack · dischargedTHE LEFT NACELLE EMERGENCY LIGHT FOUND INOP. MAINTENANCE REMOVED AND REPLACED BATTERY PACK FOR LEFT NACELLE EMERGENCY LIGHT.Sep 10, 1998 · N501ME · Doug DC932 · Emergency LightingSDR ABXA9800904Tab · crackedWHILE COMPLYING WITH C-INSPECTION, FOUND THE LEFT ELEVATOR GEAR TAB CRACKED. REPLACED LEFT ELEVATOR GEAR TAB IAW DC-9 SUPPLEMENTAL MAINTENANCE MANUAL CHAPTER 27-30-4.Sep 10, 1998 · N903AX · Doug DC932 · Elevator, Tab StructureSDR VJ9800555Seat Track · corrodedFOUND CORROSION AROUND FASTENER HOLES ON SEAT TRACK AT FS 917 TO 996 LT. REPLACED SEAT TRACK IAW DC9 SRM 53-01 FIG 1, 51-10-4, 51-30-1 AND 51-10-3.Sep 9, 1998 · N911VV · Doug DC932 · Fuselage, Seat/Cargo Attach FittingsSDR MWEA98958Cover · detachedTHE GALLEY SLIDE COVER FELL OFF. MAINTENANCE REINSTALLED GALLEY SLIDE.Sep 9, 1998 · N302ME · Doug DC932 · Emergency EquipmentSDR CALA9801686Bracket · corrodedINSPECTION FOUND SUPPORT BRACKET CORRODED AT STA 917, STRINGER 28L. THE BRACKET WAS REMOVED AND REPLACED IAW SRM 51-10-3, 51-10-4, AND 51-30-1.Sep 9, 1998 · N70542 · Doug DC932 · Fuselage Miscellaneous StructureSDR CALA9801685Hat Channel · crackedINSPECTION FOUND A 3 CRACK IN HAT CHANNEL AT FLOORBOARD PANEL, LT SIDE, STA 756. A NEW HAT CHANNEL SECTION WAS INSTALLED IAW SRM 53-05, PAGE 1 AND 51-30-2.Sep 9, 1998 · N70542 · Doug DC932 · Fuselage Miscellaneous StructureSDR ABXA9800879Skin · delaminatedWHILE COMPLYING WITH C-INSPECTION, FOUND THE RIGHT OUTBOARD SPOILER UPPER SURFACE DELAMINATED. REPLACED THE RIGHT OUTBOARD SPOILER PANEL IAW DC9 MM CHAPTER 27-61-01.Sep 9, 1998 · N903AX · Doug DC932 · SpoilersSDR VJ9800470Frame · crackedLT MLG WW FRAME CRACKED UPPER AFT END TRAPEZOID STA 718. REPLACED FRAME STA 718 IAW EO 12-5311-29-B1044.Sep 8, 1998 · N933VV · Doug DC932 · Fuselage Main, FrameSDR MWEA98956Slide · detachedTHE GALLEY SLIDE GIRT BAR FELL OFF DOOR. MTC REINSTALLED GALLEY SLIDE AND COVER.Sep 8, 1998 · N502ME · Doug DC932 · Emergency Equipment
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