Douglas DC-9-32

Service difficulty reports · 12,755

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Query with SQL
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 ABXA9500175Fitting · corrodedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND LEVEL II CORROSION ON WING TO FUSELAGE FITTING ON TOP OF CENTER WING SECTION, RIGHT SIDE, AT STATION XCW 58 AND FS 604. REPLACED FITTING IAW DC-9 SRM CHAPTERS 51-30-5 AND 51-20-0.Feb 11, 1995 · N988AX · Doug DC932 · Fuselage, Wing Attach FittingsSDR ABXA9500160Spar · crackedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE RIGHT WING REAR SPAR CRACKED AT INBOARD LOWER HOLE FOR INBOARD FLAP HINGE. REPAIRED ANGLE IAW ABX REA D957-10642-SB.Feb 11, 1995 · N988AX · Doug DC932 · Wing SparSDR ABXA9500183Skin · corrodedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE RIGHT FORWARD FUSELAGE SKIN HAD CORROSION AND A PREVIOUS REPAIR THAT WAS NOT IAW THE SRM, FROM FS 218 TO 256 AND BETWEEN LONGERON'S 14 AND 16 RIGHT. REPAIRED FUSELAGE SKIN IAW ABX REA D953-10849-MR.Feb 10, 1995 · N988AX · Doug DC932 · Fuselage Main, Plate/SkinSDR ABXA9500159Frame · gougedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND FUSELAGE FRAME GOUGED AT FS 362, BETWEEN LONGERON 29 AND 30R. REPAIRED FUSELAGE FRAME IAW ABX REA D953-10947-MR.Feb 10, 1995 · N988AX · Doug DC932 · Fuselage Main, FrameSDR MWEA95125Control Cable · corrodedPILOT REPORTS ROLL TENDANCY WHEN FLAPS ARE SELECTED TO 15 DEGREES. MECHANIC FOUND BROKEN FLAP BUS CABLE. FABRICATED NEW CABLE, INSTALLED AND RIGGED. OPS CHECK GOOD. RETURNED A/C TO SERVICE. CABLE WAS OF THE TYPE THAT HAS A CLEAR NYLON COATING. CABLE GETSFeb 9, 1995 · N602ME · Doug DC932 · Trailing Edge Flap Control SystemSDR CAL950113Radar Ind · inoperativeOKC - FLT 1468 - THE RADAR WENT INOPERATIVE AND WAS ACCOMPANIED BY A BURNING ODOR WHILE EN ROUTE TO OKC. THE RADAR WAS TURNED OFF AND THE ODOR SUBSIDED. THE FLIGHT WAS CONTINUED AND THE ACFT LANDED AT OKC WITHOUT INCIDENT. MAINTENANCE FOUND THE RADAR INDICAFeb 9, 1995 · N19504 · Doug DC932 · Weather Radar SystemSDR ABXA9500325Base · corrodedDURING D-CHECK ACCEPTANCE INSPECTION WHILE PERFORMING DC-9 FLAP OFF WING INSPECTION ON THE LEFT FLAP, FOUND LEVEL II CORROSION ON SPRING BASE. REPLACED IAW DC-9 OVERHAUL MANUAL 27-50-1.Feb 9, 1995 · N988AX · Doug DC932 · Trailing Edge FlapsSDR ABXA9500221Doubler · corrodedDURING C-CHECK INSPECTION, FOUND LEVEL II CORROSION ON AN INTERNAL DOUBLER UNDER LONGERON 26L AT STA 585. REPAIRED DOUBLER IAW ABX REA D953-10868-MR.Feb 9, 1995 · N902AX · Doug DC932 · Fuselage Miscellaneous StructureSDR ABXA9500220Intercostal · crackedDURING C-CHECK INSPECTION, FOUND A CRACK IN THE INTERCOSTALS BETWEEN STA 560 AND STA 579, BETWEEN LONGERONS 27 AND 28. REPAIRED INTERCOSTALS IAW ABX REA D953-10925-MR.Feb 9, 1995 · N902AX · Doug DC932 · Fuselage Miscellaneous StructureSDR ABXA9500162Longeron · crackedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND LONGERON 30 CRACKED AT FS 237. REPLACED LONGERON 30 FROM FS 237 TO FS 579, IAW DC-9 SRM CHAPTERS 51-30-2 AND 51-30-5.Feb 9, 1995 · N988AX · Doug DC932 · Fuselage Main, Longeron/StringerSDR 9502269951Skin · oil cannedDURING PERIODIC CHECK, FOUND OIL CANNING IN THE FUSELAGE SKIN FS 1056 - 1080 BETWEEN LONGERONS 17R - 18R. REPAIRED PER EA 99-096893.Feb 9, 1995 · N9347 · Doug DC932 · Fuselage Main, Plate/SkinSDR 9502019918Uplock Connector · dirtyDURING CLIMB-OUT FROM RST, THE LEFT MAIN LANDING GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR WAS RETRACTED. RECYCLED GEAR WITH SAME INDICATIONS. FLIGHT CONTINUED TO DESTINATION (MSP) AND NORMAL LANDING WAS ACCOMPLISHED. ADJUSTED THE LEFT MAIN GEAR DOOR ACTUATOFeb 9, 1995 · N940N · Doug DC932 · Landing Gear Position and WarningSDR 9502009918Uplatch Mech · out of adjustDURING CLIMB-OUT FROM MCI, THE LEFT MAIN LANDING GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR WAS RETRACTED. RECYCLED GEAR WITH SAME INDICATIONS. FLIGHT CONTINUED TO DESTINATION (MSP) AND NORMAL LANDING WAS ACCOMPLISHED. FOUND THE LEFT GEAR DOOR UPLATCH MECHANIFeb 9, 1995 · N940N · Doug DC932 · Landing Gear Position and WarningSDR 9502899923Pan · crackedDURING PERIODIC CHECK, FOUND CRACK IN FORWARD CARGO CUTOUT PAN AT THE LOWER FORWARD CORNER. REPAIRED PER EA 99-93849.Feb 8, 1995 · N927RC · Doug DC932 · Fuselage Miscellaneous StructureSDR 9501969925Fuel Door · jammedSLATS WOULD NOT RETRACT FULLY AFTER TAKEOFF AND SLAT DISAGREEMENT LIGHT ILLUMINATED. RECYCLED SLATS TWICE WITH NO HELP. FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. FOUND RIGHT WING FUELING PANEL DOOR JAMMED INTO SLAT. REPLACED DAMAGED LATCH ON FUELFeb 8, 1995 · N925US · Doug DC932 · Fluid Service DoorsSDR ABXA9500207Stiffener · corrodedDURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND LEVEL II CORROSION ON STIFFENER ON AFT FACE OF CANTED BULKHEAD 1089 AT LONGERON 6 LEFT. REPLACED STIFFENER IAW DC-9 SRM CHAPTER 51-30-2.Feb 7, 1995 · N988AX · Doug DC932 · Fuselage Main, BulkheadSDR ABXA9500206Stiffener · corrodedDURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND LEVEL II CORROSION ON STIFFENER ON AFT FACE OF CANTED BULKHEAD 1089 AT LONGERON 8 LEFT. REPLACED STIFFENER IAW DC-9 SRM CHAPTER 51-30-2.Feb 7, 1995 · N988AX · Doug DC932 · Fuselage Main, BulkheadSDR ABXA9500205Stiffener · corrodedDURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND LEVEL II CORROSION ON STIFFENER ON AFT FACE OF CANTED BULKHEAD 1089 AT LONGERON 11 LEFT. REPLACED STIFFENER IAW DC-9 SRM CHAPTER 51-30-2.Feb 7, 1995 · N988AX · Doug DC932 · Fuselage Main, BulkheadSDR ABXA9500186Frame · corrodedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND CORROSION ON THE FUSELAGE FRAME TEE AT FS 1089 BETWEEN LONGERON 11 AND 12 LEFT. REPAIRED TEE IAW ABX REA D953-10888-MR.Feb 7, 1995 · N988AX · Doug DC932 · Fuselage Main, FrameSDR ABXA9500157Angle · crackedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND A L ANGLE CRACKED ABOVE THE CENTER WING TANK AT FS 650 AND LBL 44. REPLACED ATTACH ANGLE IAW DC-9 SRM CHAPTERS 51-30-2 AND 51-30-5.Feb 7, 1995 · N988AX · Doug DC932 · Fuselage Miscellaneous StructureSDR 9502219951Longeron · crackedDURING PERIODIC CHECK, FOUND CRACKS IN LONGERON 17R AT FS 389 AND FS 408 AND IN LONGERON 17L AT FS 435. REPAIRED ALL THREE LOCATIONS PER EA 99-096899.Feb 7, 1995 · N9347 · Doug DC932 · Fuselage Main, Longeron/StringerSDR MWEA95123Water Line · rupturedDURING APPROACH TO MKE, PILOT WAS UNABLE TO MOVE GEAR HANDLE TO DOWN POSITION. HE EXTENDED GEAR USING EMERGENCY GEAR EXTENSION HANDLE AND PROCEDURES. GEAR EXTENDED, VERIFIED 3 GREEN. AFTER THE GEAR WAS EXTENDED THE FLAP HANDLE MOVED STIFFLY TO 15 POSITION WFeb 6, 1995 · N401ME · Doug DC932 · Water and Waste SystemSDR ABXA9500174Rib Cap · crackedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND A CRACK ON THE NR 2 ENGINE PYLON RIB CAP AT STATION YN 170. REPAIRED RIB CAP IAW ABX REA D954-10691-MR.Feb 6, 1995 · N988AX · Doug DC932 · Nacelle/Pylon StructureSDR CAL950345Bracket · brokenFLT NR 1859 - IAH - AFTER TAKEOFF TAIL COMPARTMENT TEMP HIGH LIGHT CAME ON, RETURNED TO IAH. 'NO' EMERGENCY WAS DECLARED. FOUND DUCT LEFT SIDE OF AIRCRAFT A-C BAY ATTACHMENT BROKEN. REPAIRED BRACKET PER DC-9 OVERHAUL MANUAL 20-10-9. OPS CHECK GOOD. (W)Feb 5, 1995 · N14534 · Doug DC932 · Air Distribution SystemSDR ABXA9500109Hinge · wornDURING COMPLIANCE OF AD 91-22-07, ASB 32-244, FOUND LEFT MAIN LANDING GEAR ARTICULATING DOOR BUSHING WORN ON OUTBOARD MAIN LANDING GEAR DOOR FOR WING MOUNTED HINGE. REPLACED HINGE IAW DC-9 OVERHAUL MANUAL 32-10-6.Feb 5, 1995 · N983AX · Doug DC932 · Landing Gear DoorsSDR ABXA9500090Hinge · wornDURING COMPLIANCE OF AD 91-22-07; ASB 32-244, FOUND RIGHT MAIN LANDING GEAR ARTICULATING DOOR BUSHING WORN ON THE OUTBOARD MAIN LANDING GEAR DOOR FOR THE WING MOUNTED HINGE. REPLACED HINGE IAW DC-9 OVERHAUL MANUAL 32-10-6.Feb 5, 1995 · N983AX · Doug DC932 · Landing Gear DoorsSDR ABXA9500082Hinge · wornDURING COMPLIANCE OF AD 91-22-07; ASB 32-244, FOUND RIGHT MAIN LANDING GEAR ARTICULATING DOOR BUSHING WORN ON OUTBOARD MAIN LANDING GEAR DOOR FOR WING MOUNTED HINGE. REPLACED HINGE IAW DC-9 OVERHAUL MANUAL 32-10-6.Feb 5, 1995 · N983AX · Doug DC932 · Landing Gear DoorsSDR ABXA9500081Bushing · wornDURING COMPLIANCE OF AD 91-22-07; ASB 32-244, FOUND RIGHT MAIN LANDING GEAR ARTICULATING DOOR SECONDARY LINKAGE FORK WORN AT THE DRIVE ROD. REPLACED BUSHING IAW DC-9 OVERHAUL MANUAL 32-10-6.Feb 5, 1995 · N983AX · Doug DC932 · Landing Gear Door Retract SectionSDR ABXA9500187Frame · corrodedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND CORROSION ON THE FUSELAGE FRAME AT FS 1121, UPPER PORTION OF -17 FRAME BETWEEN LONGERON 29 LEFT TO 29 RIGHT. REPAIRED FUSELAGE FRAME IAW ABX REA D953-10916-MR.Feb 4, 1995 · N988AX · Doug DC932 · Fuselage Main, FrameSDR 95ZZZX1623Flap · damagedAIRCRAFT WAS PORTED ON THE RAMP, CUSTOMERS WERE LOADING ONTO THE AIRCRAFT WHEN THE RIGHT TRAILING EDGE OF THE FLAP WAS STRUCK BY A BAGGAGE CART. APPROXIMATELY 20 INCHES OF THE TRAILING EDGE WAS BROKEN OFF.Feb 4, 1995 · N523MD · Doug DC932 · Trailing Edge FlapsSDR 95ZZZX1622Proximity Switch · defectiveATL/TPA - FLT 101 - RETURNED TO ATL DUE TO UPON RAISING LANDING GEAR, NOSE GEAR UNSAFE LIGHT REMAINED ON. RIGHT GEAR UNSAFE LIGHT REMAINED ON ALSO. REMOVED AND REPLACED PROXIMITY SWITCH BOX, PN 008-0004-004, SN OFF 254, SN ON 263. OPERATION SELF-TEST IAW VAFeb 4, 1995 · N914VV · Doug DC932 · Landing Gear Position and WarningSDR 9502159951Skin · oil cannedDURING PERIODIC CHECK, FOUND OIL CANNING IN FUSELAGE SKIN BETWEEN LOWER LEFT PYLON ATTACH ANGLE AND LONGERON 17L AT FS 1002 AND BETWEEN LONGERONS 17L - 18L AT FS 1015. REPAIRED BOTH PER EA 99-096893.Feb 4, 1995 · N9347 · Doug DC932 · Fuselage Main, Plate/SkinSDR BAXA9500218Skin · corrodedDURING C-CHECK INSPECTION FOUND CORROSION IN THE FUSELAGE SKIN LAP AT STA 813, LONGERON 26L FUSELAGE SKIN REPAIRED IAW ABX REA D953-10877-MR.Feb 3, 1995 · N902AX · Doug DC932 · Fuselage Main, Plate/SkinSDR ABXA9500224Skin · corrodedDURING C-CHECK INSPECTION, FOUND CORROSION ON THE FUSELAGE SKIN IN THE AREA OF THE NR 1 DOOR STOP OF THE AFT LOWER CARGO DOOR. REPAIRED FUSELAGE SKIN IAW ABX REA D953-10873-MR.Feb 3, 1995 · N902AX · Doug DC932 · Fuselage Main, Plate/SkinSDR ABXA9500164Fitting · crackedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND FUSELAGE FRAME FITTING CRACKED AT FS 1121. REPLACED FITTING IAW DC-9 SRM CHAPTERS 51-30-2, 51-30-5 AND 51-30-3.Feb 3, 1995 · N988AX · Doug DC932 · Fuselage Miscellaneous StructureSDR 95ZZZX870Separator Bags · dirtyATL/DFW - FLT 231 - AIRCRAFT RETURNED TO ATL DUE TO UNABLE TO PRESSURIZE IN AUTO OR IN MANUAL. REMOVE AND REPLACE WATER SEPARATOR BAGS AFTER T/S AND FINDING BAGS CLOGGED WITH ICE.Feb 3, 1995 · N923VV · Doug DC932 · Humidity Control SystemSDR ABXA9500239Tee Cap · corrodedDURING C-CHECK INSPECTION WHILE ACCOMPLISHING A.D. 90-18-03; S.B. 57-98, FOUND A CRACK AND CORROSION ON THE LEFT WING LOWER STA 58.5 TEE CAP. REPLACED TEE CAP IAW EA AD-57-03766-MR.Feb 2, 1995 · N902AX · Doug DC932 · Wing Miscellaneous StructureSDR ABXA9500238Tee Cap · corrodedDURING C-CHECK INSPECTION, WHILE ACCOMPLISHING A.D. 90-18-03; S.B. 57-98, FOUND A CRACK AND CORROSION ON THE LEFT WING LOWER TEE CAP AT STA XCW 58.5. RIGHT WING TEE CAP WAS ALSO REPLACED DUE TO DISCREPANCIES NOTED ON THE LEFT TEE CAP IAW EA AD-57-03766-MR.Feb 2, 1995 · N902AX · Doug DC932 · Wing Miscellaneous StructureSDR ABXA9500233Blkhd Tee · corrodedDURING C-CHECK INSPECTION, FOUND LEVEL II CORROSION ON THE STA 110 BULKHEAD LOWER TEE CAP. TEE CAP WAS REPAIRED IAW ABX REA D953-10867-MR.Feb 2, 1995 · N902AX · Doug DC932 · Fuselage Main, BulkheadSDR ABXA9500232Skin · corrodedDURING C-CHECK INSPECTION, FOUND LEVEL II CORROSION ON THE STA 110 FUSELAGE SKIN. REPAIRED FUSELAGE SKIN IAW ABX REA D953-10867-MR.Feb 2, 1995 · N902AX · Doug DC932 · Fuselage Main, Plate/SkinSDR ABXA9500219Tab · corrodedDURING C-CHECK INSPECTION, FOUND LEVEL II CORROSION ON THE RIGHT ELEVATOR GEAR TAB. REPLACED TAB IAW DC-9 M.M. 27-30-4.Feb 2, 1995 · N902AX · Doug DC932 · Elevator, Tab StructureSDR ABXA9500202Longeron · corrodedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND LEVEL II CORROSION ON LONGERON 27, RIGHT LOWER SURFACE, AFT OF FS 333. REPLACED LONGERON 27 RIGHT IAW DC-9 SRM CHAPTERS 51-30-2 AND 51-30-5.Feb 2, 1995 · N988AX · Doug DC932 · Fuselage Main, Longeron/StringerSDR ABXA9500180Skin · damagedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND AN IMPROPER REPAIR ON THE FUSELAGE EXTERIOR SKIN AT FS 889 AND LONGERON 21 RIGHT. REPAIRED SKIN IAW ABX REA D953-10806-MR.Feb 2, 1995 · N988AX · Doug DC932 · Fuselage Main, Plate/SkinSDR ABXA9500327Cap · corrodedDURING D-CHECK ACCEPTANCE INSPECTION WHILE PERFORMING DC-9 FLAP OFF WING INSPECTION ON THE LEFT FLAP, FOUND LEVEL II CORROSION ON LEADING EDGE NOSE CAP AT STA. XFLS 176. REPLACED IAW DC-9 SRM 57-50-9.Feb 1, 1995 · N988AX · Doug DC932 · Trailing Edge FlapsSDR ABXA9500324Spar · corrodedDURING D-CHECK ACCEPTANCE INSPECTION WHILE PERFORMING DC-9 FLAP OFF WING INSPECTION ON LEFT FLAP, FOUND LEVEL II CORROSION ON UPPER AFT SPAR AT STA. FLS. 114. BLENDED AND TREATED FOR CORROSION PER DC-9 SRM 581-10-3. REPAIRED SPAR PER DC-9 SRM 57-06.Feb 1, 1995 · N988AX · Doug DC932 · Trailing Edge FlapsSDR ABXA9500323Spar · corrodedDURING D-CHECK ACCEPTANCE INSPECTION WHILE PERFORMING DC-9 FLAP OFF WING INSPECTION ON LEFT FLAP, FOUND LEVEL II CORROSION ON LOWER AFT SPAR. BLENDED AND TREATED FOR CORROSION PER DC-9 SRM 51-10-3. REPAIRED SPAR IAW DC-9 SRM 57-06.Feb 1, 1995 · N988AX · Doug DC932 · Trailing Edge FlapsSDR ABXA9500227Skin · dentedDURING C-CHECK INSPECTION, FOUND A DENT ON THE FUSELAGE SKIN AT STA 218, LONGERON 17L. REPAIRED FUSELAGE SKIN IAW ABX REA D953-10854-MR.Feb 1, 1995 · N902AX · Doug DC932 · Fuselage Main, Plate/SkinSDR ABXA9500198Panel · delaminatedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND DELAMINATION ON THE RIGHT WING INBOARD GROUND SPOILER PANEL. REPLACED PANEL IAW DC-9 M.M. 27-62-1.Feb 1, 1995 · N988AX · Doug DC932 · SpoilersSDR ABXA9500087Skin · corrodedDURING OFF WING INSPECTION PROCEDURES FOUND LEVEL II CORROSION ON THE LEFT ELEVATOR TAB INBOARD LOWER SKIN. REPAIRED IAW DC-9 SRM 57.Feb 1, 1995 · N988AX · Doug DC932 · Elevator, Tab StructureSDR 9502109984Fitting · corrodedDURING PERIODIC CHECK, FOUND CORROSION IN AFT CARGO DOOR JAMB LOWER VERTICAL ATTACH FITTING, FS 945. REPLACED FITTING PER SRM 51-30-0.Feb 1, 1995 · N984US · Doug DC932 · Fuselage Miscellaneous Structure
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