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 UPS02839547Fitting · crackedINSPECTION TYPE:SPV R/H WHEEL WELL TRAP FITTING CRACKED AT FWD LWR BOLT HOLES,AT STA 855 RT. REMOVED STIFFNER, HFEC INSPECTED, VERIFIED TWO EACH CRACKS IN LWR TRAP FITTING, STOP DRILLED CRACKS I.A.W E.O. DC8-57-20059, AND SK 894-566,CRACKS TERMINATE AT STOPSDR UPS02839537Fitting · crackedINSPECTION TYPE: SP STA. 954 FITTING IS CRACKED CENTERLINE BETWEEN MAIN GEAR DOORS REMOVED AND REPLACED FITTING I.A.W. DWG. 4645516,AND SRM.51-1-20DSDR UPS02839536Fitting · crackedINSPECTION TYPE: SP STA. 934 FITTING IS CRACKED CENTERLINE BETWEEN MAIN GEAR DOORS REMOVED AND REPLACED FITTING I.A.W. DWG. 4646309,AND SRM. 51-1-20DSDR UPS02839534Fitting · crackedINSPECTION TYPE:SP STA 910 FITTING IS CRACKED CENTER LINE BETWEEN MAIN GEAR DOORS. REMOVED AND REPLACED FITTING IAW DWG 5616306 AND SRM 51-1-20D.SDR UPS02839533Fitting · crackedINSPECTION TYPE:SP STA 944 FITTING IS CRACKED CENTER LINE BETWEEN MAIN GEAR DOORS. REMOVED AND REPLACED FITTING IAW DWG 4645516, AND SRM 51-1-20D.SDR DHL2002801018Connector · defectiveNR 3 ENGINE B LOOP INOP. FOUND PIN B ON P1-7007 TO PIN B CONNECTOR P1-7001 GROUNDED. IT ONLY SHOWS WITH A MEGGER. REPLACED CONNECTOR P1-7007, SYS OPS CHECKS GOOD PER DC-8 M/M 26-10-0.SDR DHL2002873504Elevator · dentedITEM N/R: 0632 RT ELEVATOR LOWER EXTERNAL SKIN DEFLECTED (DENTED) XAR 0 TO XE 83.500 ( MAJOR REPAIR) CORR: PERFORMED MAJOR REPAIR IAW EO DHL 020901 , ED-3123 , AND EO SEMAN 2002735. REMOVED FASTNERS WITHIN REPAIR AREA IAW SRM51-1-21 PG. 1. TRIMMED OUT DAMAGED SDR DHL2002873503Elevator · dentedITEM N/R: 0693 RT. ELEVATOR UPPER EXTERNAL SKIN SHOWS SEVERAL DENTS ( XE132.000 TO XE141.250) ( MAJOR REPAIR) CORR: PERFORMED MAJOR REPAIR IAW E.O. DHL020902 ED-3122, EO SEMAN 2002736 REMOVED FASTNERS IAW SRM51-1-21A PG. 4. TRIMMED OUT DAMAGED SKIN SEGMENT IAWSDR DHL2002873502Skin · crackedLT WING L/E LOWER OUTER SKIN CRACKED .500, STA XW761. PERFORMED MAJOR REPAIR IAW EO DHL 020904, ED-3124, EO SEMAN 2002737. TRIMMED OUT DAMAGED OUTER SKIN IAW EO DHL020904, ED-3214, EO SEMAN 2002737. FABRICATED A REPAIR DOUBLER AND FILLER IAW ED DHL 020904, SDR DHL2002873501Skin · corrodedFUSELAGE EXTERNAL SKIN CORROSION, STA 280 L21L. PERFORMED MAJOR REPAIR IAW EO DHL 020903, ED-3125, EO SEMAN 2002738. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18 OUT OF LIMITS. FABRICATED A REPAIR DOUBLER, TWO FILLERS AND TWO INTERNAL FINGER DOUBLERS IAW EO DHSDR UPS02839436Smoke Detector · malfunctionedINSPECTION TYPE:N/A LOWER CARGO COMPARTMENT FIRE LIGHT CAME ON FOR ONE MINUTE THEN WENT OUT FWD B ON DISPLAY PANEL. PERFORM OPS CK TO LOWER CARGO SMOKE DETECTOR IAW DC-8 MM 26-18-01 ADJ &TEST OK TO CONTINUE NO FAULTS FOUND.SDR IXXA0200068OWarning System · malfunctionedAFTER TAKE OFF FROM BRO, THE LANDING GEAR DOOR NOT LATCHED LIGHT REMAINED ILLUMINATED FOLLOWING LANDING GEAR RETRACTION. THE FLIGHT CREW CYCLED THE GEAR AND THE LIGHT EXTINGUISHED. THE FLIGHT CONTINUED TO MEM FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTEDSDR DHL2002806013Fire Warning · malfunctionedWHEN NR 3 LOOP-B IS SELECTED MASTER FIRE WARNING LIGHT AND BELL ARE CONTINUOUSLY ACTUATED. LIGHT AND BELL ARE TERMINATED WHEN LOOP-A IS SELECTED. T/S RANG OUT EACH SECTION OF LOOP WITH METER AND NO DEFECTS NOTED. CLEANED AND RESECURED CONNECTORS AND SYS OPSSDR DHL2002873505Fitting · damagedLT MLG WW TRAPEZOIDAL PANEL SHOWS (04) 3/16 INCH DIA HOLES AT BS 902.000.SDR UPS02839386Angle · crackedINSPECTION TYPE:N/A VERTICAL ANGLE CRACKED LT MLG WHEEL WELL. LOCATED & DRILLED NEW ANGLE WA 18126. INSTALLED PER DC-8 SRM 51-1-20 & 51-1-21.SDR UPS02839385Angle · crackedINSPECTION TYPE:N/A UPPER INBD ANGLE CRACKED LT MLG WW. REMOVED ANGLE SENT TO MANUFACTURING WP 70050 LOCATED AND DRILLED NEW ANGLE W/CREF 18126 9-5-02 INSTALLED PER DC8 SRM 51-1-20 & 51-1-21.SDR UPS02839384Pressure Panel · crackedINSPECTION TYPE:N/A LEFT WHEEL WELL AFT FLAP ENCLOSURE, WEB ASSY ON AFT PORTION WHERE ACT RETRACTS IS CRACKED IN UPPER RADIUS. LOCATED & DRILLED NEW WEB FABRICATED NEW STIFFENER FOR SPOILER A PULLEY BRACKET ON I/B WEB PANEL, FABRICATED PER DC-8 SRM 51 W 18126SDR DHL2002873508Former · crackedITEM N/R 0716: LH WING OUTBD. LEADING EDGE .500 CRACK IN FORMER UPPER PART STA. XFS885.000CORR: REMOVED DAMAGED FORMER IAW SRM51-1-21 PG.1 FABRICATED NEW FORMER IAW SRM 57-2-0 PG. 9-10 CLEANED , TREATED , AND PRIMED IAW SRM 51-1-8B INSTALLED FORMER IAW SRM 57-SDR DHL2002873507Panel · crackedITEM N/R 0767: RT. WING T/E UPPER PANEL CRACKED 4" STA. XRS436.000 TO STA. XA475.000CORR: REMOVED AND REPLACED RT. WING T/E UPPER PANEL , STA XRS 436 TO XA475.000 IAW SRM 51-3-0SDR DHL2002801017Bulb1) #7 MAIN DECK CARGO SMOKE DET. WONT TEST2) ENTERED ON DMI #10282 IAW DHL MEL 26-6 (1) PLACARD INSTALLED G.MARTIN 211513) REF DMI #10282 #7 MAIN DECK CARGO SMOKE DET. WON'T TEST.4) RE-LAMPED TEST BULB AND OP CHECKS GOOD IAW DACO M/M 26-00. DMI 10282 CLESDR UPS02839248Fitting · crackedCRACK IN STEEL STRAP UNDER R/T ADF PNL. MILLED STEEL STRAP UNDER RT ADF (FWD) PANEL CRACKED AT STA 82.7 WHERE WING MEETS CENTER TANK BUT T L7ORT VERIFIED WITH EDDY CURRENT (SKI FITTING). R&R'D FITTING IAW DWG J060095 SRM 51-1-20D, 51-1-21,51-3-0 & 53-1-0. CSDR DHL2002806012Wire · shortedSMOKE DET SYS NOT TESTING PROPERLY. FOUND NR 3 SDU AT FAULT, NEW SDU INSTALLED, NO HELP. NR 3 SDU CONNECTOR STOWED SYSTEM OPS CHECK NORMAL. NR 3 SMOKE DETECTOR INOP. PULLED AND STOWED NR 3 SDU CONNECTOR DEFERRED. REMOVED AND REPLACED NR 3 MAIN DECK SMOKE SDR DHL2002805051Lamp · inoperativeNR 3 SMOKE DETECTOR WILL NOT TEST. REMOVED AND REPLACED LAMPS IN NR 3 SMOKE DETECTOR IAW MM 26-10-6. TESTS OK NOW.SDR UPS02839263Fitting · corrodedINSPECTION TYPE:C2 STA 680 AT LBL 63 CENTER WING BOX TO FRAME FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3642974, AND SRM 51-1-20D.SDR UPS02839103Light · inoperativeINSPECTION TYPE:N/A EMERGENCY LIGHTS DISARMED, WILL NOT ILLUMINATE. SUSPECT INOP BULB. RELAMPED EMERGENCY LIGHTS, DISARMED LIGHT. OPS CHECKS OK.SDR UPS02839094Attach Angle · crackedINSPECTION TYPE:PFLT RIGHT W/W AFT OPENING ATTACH ANGLE CRACKED. REMOVED ANGLE, DRILLED NEW ANGLE, INSTALLED NEW ANGLE IAW SRM 51-1-20D.SDR UPS02839092Stiffener · crackedINSPECTION TYPE:PFLT RT W/W UPPER INBOARD STIFFENER CRACKED. REMOVED ANGLE, INSTALLED NEW ANGLE IAW SRM 51-1-20.SDR UPS02839095Angle · corrodedINSPECTION TYPE:PFLT RIGHT W/W CORROSION FLAP WELL AREA. REPLACED ANGLE.SDR UPS02839093Pressure Panel · crackedINSPECTION TYPE:PFLT RT W/W UPPER WEB CRACKED STA XW 5.00 FERRY 9151 TO SDF REF D243078. REPAIRED WEB PER SRM 57-2-0 FIGURE 2A.SDR UPS02839074Web · crackedINSPECTION TYPE:PFLT RT WHEEL WELL FLAP SUPPORT WEB ANGLE CRACKED. FERRIED TO SDF FOR REPAIR PERMIT 9151, D243076. REMOVED FASTENERS IN DAMAGED WEB & SUPPORT BRACKET. REPAIRED WEB PER SRM 57-2-0 FIG 2A. REINSTALLED WEB.SDR UPS02839033Battery · dischargedINSPECTION TYPE:N/A, EMERGENCY EXIT LIGHTS DO NOT STAY ON. REMOVED AND REPLACED EMERGENCY LIGHTING BATTERY AND RELAY UNIT PER MM 33-50-01, OPS CHECK NORMAL.SDR UPS02839028Light · inoperativeINSPECTION TYPE:N/A, EMERGENCY EXIT LIGHT FAILED DURING PREFLIGHT. REMOVED AND REPLACED LIGHT ASSY.SDR UPS02839030Skin · corrodedINSPECTION TYPE:N/A, CORROSION FOUND AT FUSELAGE STATION 1680 STRINGER 28L IN FUSELAGE SKIN. REPAIRED CORROSION PER EO DC8-5330-17295-A IN SKIN PANEL.SDR UPS02839015Battery Pack · dischargedINSPECTION TYPE:N/A, EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK, LIGHTS CHECK NORMAL.SDR UPS02839262Fitting · crackedINSPECTION TYPE:C2 BATHTUB FITTING IS CRACKED AT STA 1160 AT LONG 34R. REMOVED, FABRICATED, AND REPLACED FITTING IAW DWG 3755841, AND SRM 53-2-0 FIG 2D.SDR UPS02839261Fitting · corrodedINSPECTION TYPE:C2 STA 320 BATHTUB FITTING IS CORRODED BEYOND LIMITS BETWEEN LONG 29L AND 30L. REMOVED AND REPLACED FITTING IAW DWG 3755822, AND SRM 53-2-0 FIG 2D.SDR UPS02839260Finger Doubler · corrodedINSPECTION TYPE:C2 STA. 8 TO -25 FINGER DOUBLER IS CORRODED BEYOND LIMITS AT RBL 60. REMOVED, FABRICATED, AND REPLACED FINGER DOUBLER IAW DWG 5612298, AND SRM 51-1-21, 51-1-20D.SDR UPS02839259Finger Doubler · corrodedINSPECTION TYPE:C2 STA -52 TO -67 FINGER DOUBLER AND WEB ARE CORRODED BEYOND LIMITS AT LBL 60. REMOVED FINGER DOUBLER, CUTOUT DAMAGE ON WEB, NDT VERIFIED NO CRACKS AT CUTOUT, FABRICATED AND INSTALLED FILLER, DOUBLER, AND FINGER DOUBLER IAW SR08530036.SDR UPS02839258Floorbeam · corrodedINSPECTION TYPE:C2 MAIN CABIN FLOORBEAM IS CORRODED BEYOND LIMITS AT STA 920 AT RBL 65. CUTOUT CORRODED SECTION OF FLOORBEAM, NDT VERIFIED NO CRACKS AT DAMAGE REMOVAL, FABRICATED AND INSTALLED FLOORBEAM SECTION IAW UPS ENGINEERING FILE NUMBER DC8-53-20237, ANSDR UPS02839257Skin · crackedINSPECTION TYPE:C2 RIGHT WING UPPER SKIN IS CRACKED AT XRS 74 AT STRINGER 9. CUTOUT DAMAGE, NDT VERIFIED NO CRACKS AT CUTOUT, FABRICATED AND INSTALLED FREEZE PLUG AND DOUBLER IAW SRM 57-2-1 FIG 10.SDR UPS02839256Skin · crackedINSPECTION TYPE:C2 RIGHT WING UPPER SKIN IS CRACKED AT XRS 74 AT STRINGER 11. CUTOUT DAMAGED AREA, NDT VERIFIED NO CRACKS AT CUTOUT, FABRICATED AND INSTALLED DOUBLER AND FREEZE PLUGS IAW SRM 57-2-1 FIG 10.SDR UPS02839254Fitting · corrodedINSPECTION TYPE:C2 STA 1660 FRAME TO CUSP FITTING IS CORRODED BEYOND LIMITS ABOVE LONG 21R. REMOVED, FABRICATED, AND REPLACED FITTING IAW DWG 4773161, AND SRM 51-1-20D.SDR COOSDR020226Fitting · crackedAFT ENTRANCE DOOR HAS A CRACKED FITTING.SDR COOSDR020225Fitting · crackedLOWER FUSELAGE STA Y640 CRACKED FITTING.SDR COOSDR020224Stiffener · crackedLEFT WING TRAILING EDGE AREA AT XRS407.000 CRACKED STIFFENER.SDR COOSDR020223Fitting · crackedLOWER FUSELAGE AT STA Y798 CRACKED FITTING.SDR COOSDR020222Fitting · crackedPAX CABIN AT STA Y781.500 CRACKED FITTING.SDR UPS02839264Pan · crackedINSPECTION TYPE:C2 LOWER RUDDER PANS ARE CRACKED AT 2ND AND 3RD HINGE FROM BOTTOM AT XE 77 AND XE 149. REMOVED, FABRICATED, AND REPLACED PANS IAW DWG 5656233, AND SRM 51-1-21, 51-3-0.SDR UPS02839251Skin · crackedINSPECTION TYPE:C2 R2 DOOR UPPER AFT CORNER SKIN IS CRACKED AT STA 1660 AT LONG 11R. CUTOUT CRACKED AREA, NDT VERIFIED NO CRACKS AT CUTOUT, FABRICATED AND INSTALLED DOUBLERS AND FILLERS IAW SRM 53-2-0 FIG 16.SDR DHL2002805050Indicator · faultyNR 1 ENGINE UNABLE TO DEVELOP THRUST ON TAKEOFF ABOVE 69 PERCENT. REMOVED AND REPLACED NR 1 ENG N1 IND PER 77-12-1, OPS CHECK GOOD PER JRH CHAP 11.
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