Douglas DC-8-73F
Service difficulty reports · 15,471
Newest first. General aviation reporting is voluntary.
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 = 'DC873F' 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.
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 = 'DC873F' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR UPS04842120Fitting · crackedINSPECTION TYPE: C3, SUBFLOOR TO WEB FITTING IS CRACKED AT STA 925 AT LBL 63. REMOVED AND REPLACED FITTING IAW DWG 3649114 AND SRM 51-3-0, 51-1-20D.SDR UPS04842117Angle · crackedINSPECTION TYPE: C3, RT WING L/E STUBWING HAS VERTICLE ANGLE CRACKED AT XS 246.5. REMOVED, FABRICATED AND REPLACED ANGLE IAW DWG 9753295 AND SRM 51-1-20D, 51-3-0.SDR UPS04842116Stiffener · crackedINSPECTION TYPE: C3, LT WING I/B STUB WING HAS VERTICLE STIFFENER CRACKED AT LOWER END AT XS 256. REMOVED, FABRICATED AND REPLACED ANGLE IAW DWG 9753294 AND SRM 51-1-20D.SDR UPS04842114Rib · crackedINSPECTION TYPE: C3, RT WING L/E LOWER RIB IS CRACKED AT XOLDI 6.225. NDT VERIFIED CRACK TERMINATES AT FASTENER HOLE, FABRICATED AND INSTALLED REPAIR ANGLES IAW SRM 57-2-0 FIG 2.SDR UPS04842110Rib · crackedINSPECTION TYPE: C3, RIGHT WING O/B LEADING EDGE RIB IS CRACKED AT XFS 603.75. CRACK TERMINATES AT FASTENER HOLE, NDT VERIFIED CRACK TERMINATES AT FASTENER HOLE, FABRICATED AND INSTALLED REPAIR ANGLES IAW SRM 57-2-0 FIG 2.SDR UPS04842109Rib · crackedINSPECTION TYPE: C3, RIGHT WING L/E UPPER RIB IS CRACKED AT PNEUMATIC DUCT SUPPORT AT XFS 304. STOPDRILLED CRACK, NDT VERIFIED STOPDRILL TERMINATES CRACK, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 57-2-0 FIG 2.SDR UPS04842088Lamp · inoperativeEMERGENCY LIGHTS ABOVE COCKPIT DOOR INOP. RELAMPED, OPS CHECK OK.SDR UPS04842265Fitting · corrodedINSPECTION TYPE: C3, EVIDENCE OF CORROSION UNDER BOLTS AND BRACKET AT LT MLG. RETRACT ACTUATOR LOWER BOLTS ON UPPER MOUNT BRACKET. OVERSIZED FWD. UPPER MOUNT HOLE FOR RETRACT ACTUATOR,FABRICATED AND INSTALLED BUSHING IAW E.O. DC8-5740-1636SDR UPS04842264Fitting · corrodedINSPECTION TYPE: C3, EVIDENCE OF CORROSION UNDER FWD. UPPER BOLT OF RIGHT MAIN LANDING GEAR RETRACT ACTUATOR UPPER MOUNT BRACKET SPOT FACED LUG,OVERSIZED HOLE,FABBED AND INSTALLED FILLER AND REPLACE- MENT BUSHING IAW E.O. DC8-5740-1636SDR UPS04842236Finger Doubler · corrodedINSPECTION TYPE: C3, FINGER DOUBLER IS CORRODED BEYOND LIMITS AT STATION 82 LONG. 31R REMOVED,FABRICATED AND REPLACED FINGER DOUBLER IAW DWG. 5779916 AND SRM. 51-1-20D,51-1-21SDR UPS04842123Skin · corrodedINSPECTION TYPE: C3, RIGHT HORIZONTAL STAB L/E UPPER SKIN IS CORRODED BEYOND LIMITS AT XFS 91.25 TO XFS103.75, XFS 135-147, XFS 216-228. BLENDED OUT CORROSION, FABRICATED AND INSTALLED 3 REPAIR DOUBLERS IAW SRM 55-2-1 FIG 4.SDR UPS04842122Skin · corrodedINSPECTION TYPE:C3 LEFT HORIZONTAL STAB L/E UPPER SURFACE IS CORRODED BEYOND LIMITS XFS 153.75 TO XFS 161. BLENDED OUT CORROSION, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 55-2-1 FIG 4.SDR UPS04842115Rib · crackedINSPECTION TYPE: C3, RT WING LE LOWER RIB IS CRACKED AT XFS 335.25. CUT OUT DAMAGE, NDT VERIFIED STOPDRILL TERMINATES CRACK, FABRICATED AND INSTALLED REPAIR ANGLE AND FILLER IAW SRM 57-2-0 FIG 2.SDR UPS04842113Rib · crackedINSPECTION TYPE: C3, LT WING L/E UPPER RIB IS CRACKED AT XFS 810. STOPDRILLED CRACK, NDT VERIFIED STOPDRILL TERMINATES CRACK, FABRICATED AND INSTALLED REPAIR DOUBLERS IAW SRM 57-2-0 FIG 2.SDR UPS04842112Rib · crackedINSPECTION TYPE: C3, LEFT WING LEADING EDGE UPPER RIBS ARE CRACKED AT XFS 747.5 AND XFS 753.75. STOPDRILLED CRACKS, NDT VERIFIED STOPDRILLS TERMINATES CRACKS, FABRICATED AND INSTALLED REPAIR DOUBLERS IAW SRM 57-2-0 FIG 2.SDR UPS04842111Rib · crackedINSPECTION TYPE: C3, RT WING LEADING EDGE UPPER RIB IS CRACKED AT XFS 803.75. STOPDRILLED CRACK, NDT VERIFIED STOPDRILL TERMINATES CRACK, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 57-2-0 FIG 2.SDR UPS04842108Rib · crackedINSPECTION TYPE:C3 RIGHT WING L/E LOWER RIB IS CRACKED AT XS 429 AT I/B END OF SLOT HOUSING. STOPDRILLED CRACK, NDT VERIFIED STOPDRILL TERMINATES CRACK, FABRICATED AND INSTALLED DOUBLER IAW SRM 57-2-0 FIG 2.SDR UPS04842107Rib · crackedINSPECTION TYPE:C3 RIGHT WING L/E UPPER RIB IS CRACKED AT XFS 728.75. STOPDRILLED CRACK, NDT VERIFIED STOPDRILL TERMINATES CRACK, FABRICATED AND INSTALLED DOUBLERS IAW SRM 57-2-0 FIG 2.SDR UPS04842106Rib · crackedINSPECTION TYPE:C3 LEFT WING L/E UPPER RIB IS CRACKED AT XFS 304 AT PNEUMATIC DUCT SUPPORT. CUT OUT AND STOPDRILLED CRACKED AREA, NDT VERIFIED NO CRACKS AT STOPDRILLS AND CUTOUT, FABRICATED AND INSTALLED DOUBLER AND FILLER IAW SRM 57-2-0 FIG 2.SDR UPS04842262Skin · crackedINSPECTION TYPE: C3, RT WING CENTER LE. INNER SKIN IS CRACKED AT FASTENER HOLES XW408 TO XS520. REMOVED, FABRICATED AND REPLACED INNER SKIN AND DOUBLER IAW DWG. 5769759 AND 5769857 AND SRM. 51-1-20D,51-1-21SDR UPS04842165Skin · dentedINSPECTION TYPE:C3 FUSELAGE SKIN HAS A DENT AT STATION -48 LONG 20L. CUT OUT DAMAGE, FABRICATED FILLER, INSTALLED DOUBLER, FILLER AND FINGER DOUBLER IAW SRM 53-2-1 FIG 7.SDR UPS04842076Sliding Window · bindingINSPECTION TYPE:PFLT F/O'S SLIDING WINDOW WILL NOT OPEN. CYCLED WINDOW, OPS CHECKS NORMAL.SDR IXXA0400019OEngine · flamed outDURING FLIGHT AT 34.0 FL AT 88 PERCENT N1, RPM FLUXED APPROX. 8 PERCENT ROM 80 TO 88 PERCENT ON NR 1 ENGINE, ENGINE FLAMED OUT. DESCENDED TO FL250 ATTEMPTED RESTART WITH PMC ON ENG WOULD NOT RESTART, SECOND ATTEMPT WITH PMC OFF ENGINE RELIGHTED, CONTINUED REMASDR IXXA0400065SFlange · corrodedC-CHECK INSP MAIN CARGO COMP WEB, BEAM LOWER FLANGE CORRODED STA 960 RBL 58 - 64. REMOVED FASTENERS, CORROSION FOUND OUT OF LIMITS. REMOVED DAMAGED CORROSION AREA & SECTION OF FLANGE. FABBED FILLER & DOUBLER. PERFORMED NDT INSP, FABBED EXTERNAL REPAIR DOUBSDR IXXA0400056SSkin · corrodedDURING ROUTINE C-CHECK INSPECTION FOUND RT WING OB L/E OUTER SECTION UPPER SKIN SURFACE CORRODED, STA. XW 761.000. REPAIRS WERE ACCOMPLISHED BY REMOVING FASTENERS IAW SRM 51-1-20D PG. 21, SRM 51-3-0 PG. 1, SRM 51-1-21 PG. 1, REMOVED CORROSION IAW SRM 51-1-8 PGSDR IXXA0400055SSkin · corrodedDURING ROUTINE C-CHECK INSPECTION FOUND LT WING OB L/E OUTER SECTION LWR SKIN SURFACE CORODED, STA. XFS 710.000. REPAIRS WERE ACCOMPLISHED BY REMOVING FASTERNERS IAW DC8 SRM 51-120D PG. 21, SRM 51-1-21 PG. 1, SRM 51-3-0 PG.1, REMOVED CORROSION IAW SRM 51-1-8 PSDR IXXA0400054SSkin · corrodedDURING ROUTINE C-CHECK INSPECTION LT OB WING L/E IB SECTION LWR SKIN SURFACE CORRODED, STA XFS. 710.000. REPAIRS WERE ACCOMPLISHED IAW APPROVAL DOCUMENT, REMOVED FASTENERS, REMOVED CORROSION FOUND OUT OF LIMITS IAW SRM 57-2-1 PAGE 11 REMOVED DAMAGED AREA, PERFSDR IXXA0400053SSkin · corrodedDURING ROUTINE C-CHECK INSPECTION FOUND RT WING OB L/E INNER SECTION UPPER SKIN SURFACE CORRODED, STA XW 485.000. REPAIRS WERE ACCOMPLISHED IAW APPROVAL DOCUMENT DWG V22-R02, REMOVED FASTENERS IAW SRM 51-1-21 PAGE 1, 51-1-20D PAGE 21, 51-3-0 PAGE 1, REMOVED COSDR DHL2004807005Engine · malfunctionedWHILE SHUTTING DOWN NR 2 ENGINE DURING BLOCK IN, THE NR 3 ENGINE SHUT DOWN ON ITS OWN. GROUND RAN NR 2 AND NR 3 ENGINES, AND SHUT DOWN TWO TIMES, OPS CHECKED OK IAW CFM MM 71-00-00 AND JRH 13.1 AND 11.SDR IXXA0400039SJoint · crackedDURING ROUTINE C-CHECK INSPECTION RT WING INBD JOINT FLAP BRACE CRACKED. REPAIR IS ACCOMPLISHED BY PERFORMING MAJOR REPAIR IAW DC8 SRM 57-1-0 PAGE 1. REMOVED CRACKED JOINT FLAP BRACE IAW DC9 SRM 51-1-21 PAGE 1. CLEANED, TREATED, PRIMED AREA IAW DC8 SRM 51-1SDR UPS04842041Panel · inoperativeDURING TROUBLESHOOTING OF M277846 LANDING LIGHT INOP, MTC FOUND OVERHEAD LANDING LIGHT PANEL BURNED INTERNALLY AND WIRING SHORTED. OVERHEAD LIGHTING PANEL REMOVED & PLACED IN 5X STORES. REPLACED SWITCH 31-58, 51-59 & 51-61 AND ACCOMPANING WIRES TO DISCONNECTSDR DHL2004801004Latch · out of adjustCOCKPIT DOOR WILL NOT LATCH. ADJUSTED DOOR LATCH AS PER M/M 52-10-00, DOOR LATCHES NORMAL.SDR IXXA0400040SBulkhead · crackedDURING ROUTINE C-CHECK INSPECTION, LT FUSELAGE AFT PRESSURE BULKHEAD STRUCTURE HAS CRACK. REPAIR ARE ACCOMPLISHED BY PERFORMING MAJOR REPAIRS IAW SRM 53-2-5 FIG 9, AT STA. XW 130.00, IAW SRM 51-1-20D PAGE 21 PERFORMED CRACK END, SRM 53-2-5 PAGE 15-16 AND PERFSDR DHL2004809005Rib · crackedLEFT-HAND INBOARD FLAP UNDER JOINT PANEL THERE IS A .75 INCH CRACK OUTBOARD RIB LOWER CORD 40 INCHES FROM TRAILING EDGE. DEFERRED IAW GMM 3.5 CAT 1. REF BOEING SERVICE ENGINEERING TECH & FLEET SUPPORT LETTER DHL-CVG-04-00024H 15MAR04. ENTER AS DMI 16040E. SDR DHL2004809004Spar · crackedLT MLG WHEEL WELL FUSELAGE STA 931 FALSE SPAR STA 1.50 THE UPPER END OF CHANNEL HAS A .375 INCH CRACK IN RADIUS OF VERT LONG. DEFERRED IAW GMM 3.5 CAT 1. REF BOEING SERVICE ENGINEERING TECH & FLEET SUPPORT LETTER DHL-CVG-04-00024H 15MAR04. ENTER AS DMI 1604SDR DHL2004809003Fitting · crackedRIGHT-HAND WHEEL WELL STA 931 FALSE SPAR STA 1.50 FITTING IS CRACKED 1.50 INCH LONG FORWARD TO AFT. DEFERRED IAW GMM 3.5 CAT 1. REF BOEING SERVICE ENGINEERING TECH & FLEET SUPPORT LETTER DHL-CVG-04-00024H 15MAR04. ENTERED AS DMI 16041E. ONLY 2 REVENUE FLIGSDR UPS04842028Battery Pack · inoperativeEMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EMERGENCY BATTERY PACK IAW MM 33-50-01.SDR UPS04842022Battery Pack · inoperativeINSPECTION TYPE:P/S FOUND EMERGENCY BATTERY INOPERATIVE DURING PERIODIC SERVICE CHECK PARA 9C. REMOVED AND REPLACED EMERGENCY POWER SUPPLY BATTERY UNIT IAW AMM 33-50-01-2.SDR IXXA0400037SSkin · wornDURING ROUTINE C-CHECK INSPECTION RT OUTBD FLAP UPPER PLATING DOUBLER WORN OUT OF LIMITS (STA 226.000-333.000) MAJOR REPAIRS. REPAIR IS ACCOMPLISHED BY PERFORMING MAJOR REPAIRS IAW DC8 SRM 57-1-0 PG 1, DC8 SRM 57-7-1 FIG 4. REMOVED WORN PLATING IAW DC8 SRM 5SDR IXXA0400041SFrame · crackedDURING ROUTINE C-CHECK INSPECTION MAIN CARGO COMPT FRAME CRACKED 3 INCHES STAT. 1580.000, L-21R, MAJOR REPAIR. REPAIRS ARE ACCOMPLISHED BY PERFORMING IAW DC8 SRM 53-2-0 PAGE2 OF 2 FIG 2, REMOVED DAMAGED AREA IAW SRM 53-2-0 PAGES 2 OF 2 FIG. 2, FABRICATED FRAMSDR IXXA0400029SSkin Panel · damagedDURING ROUTINE C-CHECK INSPECTION RT WING INBD VANE SLOT UPPER SKIN HAS ELONGATED HOLES AT STA XS 247.000 (MAJOR REPAIR). REPAIR IS ACCOMPLISHED PERFORMED MAJOR REPAIR IAW DC8 SRM 57-1-0 PAGE 1, DC8 SRM 57-3-3 FIG 10 PAGE 22. REMOVED DETERIORATED SKIN IAW DCSDR IXXA0400045SSkin · crackedDURING A ROUTINE C-CHECK INSPECTION FOUND FWD FUSELAGE EXTERNAL SKIN HAS IMPROPER REPAIR IAW DWG V22-R19. REPAIR ACCOMPLISHED. TEMPORARY REPAIR WAS REMOVED. FABRICATION AND INSTALLATION OF FINGER DOUBLER FILLER AND DOUBLER IAW STRUCTURAL REPAIR MANUAL. CLEANEDSDR IXXA0400042SFloorbeam · corrodedDURING ROUTINE C-CHECK INSPECTION RT WING CENTER SECTION UPPER FLOORBEAM FLANGE CORRODED, STA. 980.000 RBL 10 INCHES. REPAIR ARE ACCOMPLISHED, PERFORMED MAJOR REPAIR IAW SRM 51-2-1 FIG. 1, REMOVED CORROSION FROM UPPER FLOORBEAM FLANGE, STA 980.000 RBL. 10 INCHSDR IXXA0400038SFloorbeam · corrodedDURING ROUTINE C-CHECK INSPECTION RT WING CTR FLOORBEAM FLANGE, STA 798.000 LBL 10 IAW DC8 SRM 51-1-8 PG 17-18, IAW DC8 SRM 53-2-0 PG 2M. REMOVED DAMAGED SECTION AND FABRICATED (7075-T651 0.250) IAW DC8 SRM 51-1-21 FIG 1. PERFORMED NDT INSP, CLEANED, TREATEDSDR IXXA0400034SSkin · damagedDURING ROUTINE C-CHECK INSPECTION RT WING OUTBOARD FLAP UPPER FORWARD PLATING INTERIM REPAIR BETWEEN STA XF 415.000 TO XF 440.00. REPAIR IS ACCOMPLISHED BY REPLACEMENT WAS ACCOMPLISHED IN ACCORDANCE WITH DC8 SRM CHAPTERS 57-1-0 PG 1, 57-7-1 FIG 4 TR 57-94, 51SDR IXXA0400032SSkin · damagedDURING ROUTINE INSPECTION RT OUTBOARD FLAP HAS INTERIM REPAIR ON UPPER PANEL (STA SF 415.000-440.000) MAJOR REPAIR. REPAIRS ARE ACCOMPLISHED BY PERFORMING MAJOR REPAIR IAW DC8 SRM 57-1-0 PG 1, DC8 SRM 57-7-4 FIG 4. REMOVED UPPER SKIN WITH INTERIM REPAIR ON ISDR IXXA0400030SHinge Fitting · crackedDURING ROUTINE C-CHECK INSPECTION RT WING INBD FLAP HINGE SUPPORT FITTING CRACKED 4 INCHES STA XW 97-906. REPAIRS ARE ACCOMPLISHED BY PERFORMING MAJOR REAIR IAW DC8 SRM 57-1-0 PAGE 1. REMOVED CRACKED FITTING IAW DC8 SRM 51-3-0 PAGE 1. CLEANED, TREATED AND PSDR UPS04841962Retainer · inoperativeRT MLG DOOR OPEN IN FLIGHT. POSSIBLE PROBLEM WITH DOOR RETRACT SYSTEM. FERRY TO SDF FOR REPAIR. RMVD RT MLG IB DOOR. RMVD ACCESS COVER FOR ALT INDICATOR SINKER PLATE. INSTALLED MLG DOOR ALT IND STRIKER PLATE. OK TO REINSTALL ACCESS COV ER. OK TO INSTALL SESDR DHL2004809002Windshield · crackedF/O'S WINDSHIELD CRACKED. REMOVED AND REPLACED F/O'S FORWARD SIDE WINDOW IAW DC8 M/M 56-10-2, NO LEAKS NOTED.SDR IXXA0400046SSkin · corrodedDURING A ROUTINE C CHECK INSPECTION FOUND RT HORIZONTAL STAB L/E SURFACE SHOWS CORROSION AND A 1 INCH CRACK. REPAIR ACCOMPLISHED. PERFORMED MAJOR REPAIR IAW DWG V22-R18. REMOVED FASTENERS , REMOVED CORROSION AND FOUND OUT OF LIMITS. REMOVED THE DAMAGED AREA IA
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