Douglas DC-8-71F
Service difficulty reports · 8,938
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 = 'DC871F' 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 = 'DC871F' 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 IXXA11SMN033SFitting · crackedDURING ROUTINE C-CHECK INSP FOUND MAIN CARGO COMPARTMENT BATHTUB FITTING CRACKED AT STA 857.000 LONGERON 8 LT. REMOVED CRACKED FITTING. CLEANED, TREATED AND PRIMED AREA. INSTALLED NEW FITTING IAW SRM 51-1-20D, SRM 51-18B, SRM 51-1-20D AND SRM 51-3-1 AND SRM SDR IXXA11SMN032SFitting · crackedDURING ROUTINE C-CHECK INSP, FOUND MAIN CARGO COMPARTMENT FORWARD FITTING CRACKED AT STA 857.000 LONGERON 19 RT. REMOVED CRACKED AFT FITTING. CLEANED AREA. INSTALLED NEW FITTING IAW SRM 51-1-20D, SRM 51-1-8B, SRM 51-1-20D AND SRM 51-3-1.SDR IXXA11SMN031SFitting · crackedDURING ROUTINE C-CHECK INSP FOUND MAIN CARGO COMPARTMENT AFT FITTING CRACKED AT STA 798.000 LONGERON 11 RT. REMOVED CRACKED AFT FITTING. CLEANED AREA. INSTALLED NEW FITTING IAW SRM 51-1-20D, SRM 51-1-8B, SRM 51-1-20D AND SRM 51-3-1.SDR IXXA110014SSkin · crackedDURING INSP FOR AD2008-26-07 AND SB DC8-57A102 FOUND LT WING LOWER SKIN CRACKED AT STRINGER 62 IN THE 14TH FASTENERS ROW OTBD FROM STA XW408 CENTERLINE PROPAGATING APPROX .300 FWD AND .050 AFT. REPAIR WAS ACCOMPLISHED IAW SRM 57-2-1 FIGURE 45 TR NUMBER 57-1SDR IXXA11SMN029SDoor Frame · crackedDURING ROUTINE C-CHECK INSP, FOUND FWD CARGO DOOR JAMB CRACKED AT STA FS 330.000 BETWEEN LONGERON 32 LT AND 33 LT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSP. NO DISCREPANCY FOUND. FABRICATED REPAIR TRIPLER, REPAIRSDR IXXA11SMN021SWeb · crackedDURING ROUTINE C-CHECK INSP FOUND RUDDER RIB WEB CRACKED AT STA ZR 106.00. REMOVED CRACKED WEB. FABRICATED NEW WEB. PERFORMED HEAT TREATMENT. CLEANED, TREATED, PRIMED AREA AND REPAIRED PARTS. APPLIED SEALANT TO FAYING SURFACES. PERFORMED RUDDER BALANCE. FOUNSDR IXXA11SMN027SWeb · crackedDURING ROUTINE C-CHECK INSP, FOUND RUDDER WEB LT SIDE CRACKED AT STA ZR 65.000. REMOVED CRACKED WEB. FABRICATED NEW WEB. PERFORMED HEAT TREATMENT. CLEANED, TREATED, PRIMED AREA AND REPAIRED PARTS. INSTALLED REPAIRED PARTS IAW SRM CHAPTER 55-2-3, FIG 5, SRM 55-SDR IXXA11SMN022SSkin · corrodedDURING ROUTINE C-CHECK INSP FOUND NR 1 ACCESSORY COMPARTMENT AIR CONDITIONING SKIN HAS CORROSION AT STA 70.000 LONGERON 33 RT AND LONGERON 34 RT. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. PERFORMED NDT INSP. NO DISCREPANCY FOUND. FABRISDR IXXA11SMN026SSkin · dentedDURING ROUTINE C-CHECK INSP FOUND RT WING OTBD AILERON LOWER SKIN HAS DENTS AT STA XA 678.000 - XA 752.000. REMOVED DAMAGE SKIN. FABRICATED NEW SKIN AND DOUBLER. BONDED PARTS AS NEEDED WITH HYSOL. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. PERFORMED WESDR IXXA11SMN025SSkin · dentedDURING ROUTINE C-CHECK INSP, FOUND RT WING OTBD FLAP UPPER SKIN SHOWS DENTS AT STA XF 380.000. REMOVED DAMAGE SKIN. FABRICATED NEW SKIN, INTERNAL AND EXTERNAL DOUBLERS. BONDED PARTS AS NEEDED WITH HYSOL. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALSDR IXXA11SMN024SSkin · dentedDURING ROUTINE C CHECK INSP FOUND RT WING OTBD FLAP UPPER SKIN SHOWS DENTS AT STA XF 408.343. REMOVED DAMAGE SKIN. FABRICATED NEW SKIN, INTERNAL AND EXTERNAL DOUBLERS. BONDED PARTS AS NEEDED WITH HYSOL. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALLSDR IXXA11SMN023SSkin · wornDURING ROUTINE C-CHECK INSP FOUND RT WING OTBD FLAP SKIN WORN AT STA XRS 162.263. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN. CLEANED, TREATED, PRIMED, PAINTED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS ANDSDR IXXA11SMN020SStringer · crackedDURING ROUTINE C-CHECK INSP, FOUND LT WING NR 1 MAIN FUEL TANK STR CRACKED AT STA XW 408.000 AND STR 60. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. PERFORMED STOP HOLE. PERFORMED NDT INSP. NO DISCREPANCY FOUND. FABRICATED SPLICES FITTING, EXTRUSION. CLSDR IXXA11SMN018SSupport Bracket · crackedDURING ROUTINE C-CHECK INSP FOUND NR 1 ENG THRUST REVERSER SUPPORT FRAME CRACKED AT STA YN 202.000 . REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. FABRICATED FRAME SEGMENT. CLEANED, TREATED, PRIMED AREA AND REPAIRED PARTS. INSTALLED NEW SDR IXXA11SMN017SSkin · crackedDURING ROUTINE C-INSP FOUND LT WING LOWER INNER SKIN CRACKED AROUND STRINGER 60 AT STA XW 408.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGE AREA. PERFORMED NDT INSP. NO DISCREPANCY FOUND. FABRICATED NEW SKIN, REPAIR DOUBLER AND FILLER. CSDR IXXA110008OInstrument Panel · unsecureDURING TAKEOFF ROLL AT 68 KTS THE F/O INSTRUMENT PANEL SLID OUT. THE TAKEOFF WAS ABORTED AND THE CREW RETURNED TO PARKING. MX SECURED THE F/O INSTRUMENT PANEL AND PERFORMED THE REJECTED TAKEOFF INSP. THE ACFT WAS RETURNED TO SERVICE IAW MM 31-10-2 AND MM 13SDR IXXA110010SStringer · crackedDURING ROUTINE B-CHECK INSP FOR ACCOMPLISHING AD 2008-26-07 FOUND LT WING AT STA XW 408.343 STR 60 CRACKED. MX PERFORMED FERRY FLIGHT INSP IAW GMM 3.117, FOR THE REPAIR.SDR IXXA11009SSkin · crackedDURING ROUTINE B-CHECK INSP FOR ACCOMPLISHING AD 2008-26-07 FOUND LT WING LOWER SKIN CRACKED AT STA XW408.343, STRINGER 60. MX PERFORMED FERRY FLIGHT INSP IAW GMM 3.117, FOR THE REPAIR.SDR IXXA110003SSkin · crackedDURING SKIN INSP FOR AD 2008-26-07, FOUND A .5 INCH CRACK ON LT WING LOWER SKIN AT STRINGER 58. MX PERFORMED INSP FOR FERRY FLIGHT FOR PERMANENT STORAGE IAW GMM 3.117.SDR U2RA449SPIM002Web · crackedFUSELAGE TAIL SECTION INTERIOR, FS 1817 TO FS 1823 UPPER WEB WITH 11" CRACK.SDR U2RA449SPIM001Skin · wornLT WING, T/E UPPER SURFACE, XRS 272 EXISTING REPAIR WITH WEAR.SDR IXXA100053SSkin · corrodedDURING ROUTINE B-CHECK, INSP FOUND CORROSION ON FUSELAGE SKIN AT STA 73 LONGERON 31 RT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED CORRODED SKIN. FABRICATED NEW SKIN. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REPSDR IXXA100049OUplock · out of adjustDURING CLIMBOUT, WHILE THE CREW PERFORMING CLIMB CHECK LIST, THE UP LATCH CHECK FAILED WITH RED DOOR LIGHT ON. THEY CYCLED THE GEARS WITH NO HELP. THEY RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. MX DEFERRED THE UPLATCH SYS IAW MEL 32-14-01 TO BE ACCOMPLISSDR IXXA100048OSwitch · out of adjustDURING CLIMBOUT,THE GEAR DOOR NOT LATCH LIGHT CAME ON. THE CREW CYCLED THE GEARS AND THE LIGHT REMAINED ON. THEY RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. MX ADJUSTED THE STRIKER SWITCH AND LUBED BOTH DOOR UPLATCH MECHANISMS. OPS CHECK GOOD IAW UAL MM SDR IXXA100046OSteering Sys · inoperativeDURING TAKEOFF, F/O HAD NO RESISTANCE IN RUDDER PEDAL AND NO NOSE WHEEL STEERING. THE CREW ABORTED TAKEOFF AND RETURNED TO BLOCKS WITHOUT FURTHER INCIDENT. MX INSPECTED THE F/O RUDDER PEDAL ASSY, OPS CHECK GOOD IAW MM 27-23-28, 27-20-03 AND 27-23-29. ACFT WAS SDR IXXA100035OPin · brokenAFTER TAKEOFF LANDING GEAR UNSAFE LIGHT CAME ON, THE CREW CYCLED GEAR LIGHT WENT OUT. ONE HR INTO FLIGHT DOOR NOT LATCH LIGHT CAME ON THEN WENT OUT, THE LANDING GEAR UNSAFE LIGHT REMAINED ON DURING FLIGHT. UPON GEAR EXTENSION, A LOUD BANG WAS HEARD, GOT (3) GRSDR IXXA10SMN037SFitting · crackedDURING ROUTINE C-CHECK INSP FOUND MAIN CARGO COMPARTMENT FITTING CRACKED AT STA 902.000 LONGERON 5 LT. REMOVED CRACKED FITTING. CLEANED, TREATED, AND PRIMED AREA.INSTALLED NEW FITTING IAW SRM 51-1-20D, SRM 51-1-8B, AND SRM 51-3-1.SDR 2010FA0000311Structure · cracked(SPUY) DURING ROUTINE C-CHECK INSPECTION, LT OTBD WING L/E INNER SECTION. LOWER PLATING CRACKED AT STA XFS 597.500.SDR 2010FA0000310Finger Doubler · corroded(SPUY) DURING ROUTINE C-CHECK INSP, FLIGHT COMPARTMENT - HORIZ PRESS PANEL (SUB FLOOR) FINGER DOUBLER CORRODED AT STA 58.000 AND LBL 19.SDR 2010FA0000309Angle · cracked(SPUY) DURING ROUTINE C-CHECK INSPECTION, AFT FUSELAGE INTERNAL SECTION- RING ANGLE CRACKED AT STA FS 1690.000 BETWEEN 30L AND L36.SDR 2010FA0000305Skin · damaged( SPUY) DURING ROUTINE C-CHECK INSPECTION, LT WING INBD FLAP - AFT UPPER SURFACE SKIN PANEL SHOWS SCRATCHES AND (05EA) DENTS (STA XW 1.000 - 91.000).SDR 2010FA0000304Skin · dented( SPUY) DURING ROUTINE C-CHECK INSPECTION, RT WING INBD FLAP - FWD UPPER SURFACE SKIN PANEL SHOWS DENTS ( STA XW 104.000-122.000)SDR 2010FA0000303Skin · dented( SPUY) DURING ROUTINE C-CHECK INSPECTION, RT WING OTBD FLAP - AFT LOWER SURFACE SKIN PANEL SHOWS INTERM REPAIR AND DENT ( STA XF375.00-415.00).SDR 2010FA0000301Hook · cracked( SPUY) DURING ROUTINE C-CHECK INSPECTION, FUSELAGE NOSE SECTION SKIN - FWD PASSENGER DOOR HOLD OPEN HOOK CRACKED .5" AT STA FS 15,000, L-16.SDR 2010FA0000300Doubler · worn(SPUY) DURING ROUTINE C-CHECK INSP, FUSELAGE NOSE SECTION, INTERNAL DOUBLER WORN AND BROKEN AT STA FS-156.00 (THRU NR 2 ACCESS DOOR. GROUND PNEU CONNECTION).SDR IXXA10SMN044SSkin · crackedDURING ROUTINE C-CHECK INSP FOUND FWD CARGO COMPARTMENT INTERNAL SKIN CORRODED AT STA FS 285.000 LONGERON 35 RT- LONGERON 36. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. PERFORMED NDT INSP. NO SDR IXXA10SMN043SFinger Doubler · corrodedDURING ROUTINE C-CHECK INSP FOUND FLIGHT COMPARTMENT HORIZONTAL PRESS PANEL (SUB FLOOR) FINGER DOUBLER CORRODED AT STA 58.000 LT BOTTOM LINE 19. REMOVED CORRODED DOUBLER. REMOVED DAMAGED AREA. FABRICATED DOUBLERS, SEGMENT PANEL, SPLICE. CLEANED, TREATED PRIMEDSDR IXXA10SMN42SSeat Track · crackedDURING ROUTINE C-CHECK INSP FOUND MAIN CARGO COMPARTMENT NR 5 SEAT TRACK LUG BROKEN AT STA 148.00-1570.000. REMOVED DAMAGED SEGMENT OF TRACK. REMOVED EXISTING FWD SPLICE HAT AND SPLICE PLATE. FABRICATED SPLICE HAT, AND SPLICE PLATE. CLEANED, TREATED AND PRIMEDSDR IXXA10SMN041SSeat Track · crackedDURING ROUTINE C CHECK INSP FOUND MAIN CARGO COMPARTMENT NR 4 SEAT TRACK LUG BROKEN AT STA 590.000. REMOVED DAMAGED SEGMENT OF TRACK. REMOVED EXISTING FWD SPLICE HAT AND SPLICE PLATE. FABRICATED SPLICE HAT, AND SPLICE PLATE. CLEANED, TREATED AND PRIMED AREA ANSDR IXXA10SMN040SAngle · crackedDURING ROUTINE C-CHECK INSP FOUND AFT FUSELAGE INTERNAL SECTION RING ANGLE CRACKED AT STA FS 1690.000 LONGERON 30, LT LONGERON 36. REMOVED CRACKED RING ANGLE. FABRICATED SPLICES. PERFORMED HEAT TREATMENT. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALLSDR IXXA10SMN038SFitting · crackedDURING ROUTINE C-CHECK INSP FOUND MAIN CARGO COMPARTMENT FITTING CRACKED AT STA 680.000 LONGERON 11 RT. REMOVED CRACKED FITTING. CLEANED, TREATED, AND PRIMED AREA. INSTALLED NEW FITTING IAW SRM 51-1-20D, SRM 51-1-8B, AND SRM 51-3-1.SDR IXXA10SMN039SFitting · crackedDURING ROUTINE C-CHECK INSP FOUND MAIN CARGO COMPARTMENT CTR WING FITTING CRACKED AT STA FS 702.000 LONGERON 21 RT AND LONGERON 20 RT. REMOVED CRACKED FITTING. CLEANED, TREATED, AND PRIMED AREA. INSTALLED NEW FITTING IAW SRM 51-1-20D, SRM 51-3-1, AND SRM 51-1-SDR IXXA10SMN035SSkin · misrepairedDURING ROUTINE C CHECK INSP FOUND LT WING OTBD FLAP AFT LOWER SKIN PANEL HAS IMPROPER REPAIR AT STA XF 304.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. FABRICATED NEW SKIN. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTASDR IXXA10SMN030SSkin · misrepairedDURING ROUTINE C-CHECK INSP FOUND RT WING OTBD FLAP FWD LOWER SKIN IMPROPER REPAIR AT STA XF 227.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO DISCREPANCY FOUND. FABRICATED NEWSDR IXXA10SMN036SSkin · misrepairedDURING ROUTINE C-CHECK INSP FOUND LT WING OTBD FLAP FWD UPPER SKIN HAS IMPROPER REPAIR AT STA XF 432.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN, INTERNAL AND EXTERNAL DOUBLERS. BONDED PARTS AS NEEDED WITH SDR IXXA10SMN034SSkin · misrepairedDURING ROUTINE C CHECK INSP, FOUND LT WING OTBD FLAP FWD LOWER SKIN HAS IMPROPER REPAIR AT STA XF 193.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN, INTERNAL AND EXTERNAL DOUBLERS. BONDED PARTS AS NEEDED WITHSDR IXXA10SMN033SSkin · dentedDURING ROUTINE C-CHECK INSP FOUND LT WING INBD FLAP AFT UPPER SURFACE SKIN HAS SCRATCHES AND DENTS AT STA XW 2.000 - 91.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN, INTERNAL AND EXTERNAL DOUBLERS. BONDED PARSDR IXXA10SMN032SSkin · dentedDURING ROUTINE C-CHECK INSP FOUND RT WING INBD FLAP FWD UPPER SURFACE SKIN HAS DENTS AT STA XW 104.000 - 122.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALLESDR IXXA10SMN031SSkin · misrepairedDURING C-CHECK INSP, FOUND RT WING OTBD FLAP AFT LOWER HAS IMPROPER REPAIR AT STA XF 375.000 - 415.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. FABRICATED NEW SKIN, INTERNAL AND EXTERNAL DOUBLERS. BONDED PARTS AS NEEDED WITH SDR IXXA10SMN046SSkin · brokenDURING ROUTINE C-CHECK INSP FOUND FUSELAGE NOSE SECTION INTERNAL DOUBLER WORN AND BROKEN AT STA FS -156.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSP. NO CRACKS OR CORROSION NOTED. FA
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