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 DHLA201000088Frame · wornNR3 ENG LT T/R FRAME WORN AT 6.30 AND 7.30 O'CLOCK POS STA YN 203.000 PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 08-04-10, EVA D878-00353 REV IR DATED 07-15-10. REMOVED FASTENERS IAW SRM 51-1-21, SRM 51-3-0. CUT OUT DAMAGED AREA AND FABRICATED FRAME SEGMSDR DHLA201000085Skin · crackedRT WING TOP AFT PANEL PLATING CRACKED 4" STA XCW 69.500 PERFORMED MAJOR REPAIR IAW SRM 57-2-1 FIG 20, SHEET 1. REMOVED FASTENERS IAW SRM 51-3-0, SRM 51-1-20D. CUT OUT DAMAGED AREA + FABRICATED (-5) DOUBLER (7075"0" 0.160") + (-7) TRIPLER (7075"0" 0.125") + FISDR DHLA201000034Battery Pack · dischargedEMERGENCY EXIT LIGHTS INOP ON RISE CHECK DURING PRE-FLIGHT BY S/O. R & R EMERGENCY LIGHT BATT PACK IAW AMM 33-50-1. OPS CHECK NORMAL. ACFT WAS GROUNDED.SDR DHLA201000017Battery Pack · inoperativePRE-FLIGHT NR 1881- EMERGENCY LIGHTS WILL NOT TEST 2. R & R EMER RACK ASSY BATTERY GRD OP CK GOOD IAW MM REF 33-50-1. ACFT WAS GROUNDED.SDR 2010FA0000680Skin · dented(SPUY) RT OTBD FLAP T/E PANEL UPPER SKIN WITH (02 EA) DENTS AT STA XF 310.000 AND 320.000.SDR 2010FA0000679Longeron · corroded(SPUY) AFT ACCY COMPT L-34L CORRODED AT STA 1700.000 (CORRECTING SOURCE DOCUMENT: CPCP 5600-0551).SDR 2010FA0000678Cargo Track · broken(SPUY) MAIN CARGO COMPT - NR 4 SEAT TRACK LUG PLUG BROKEN (STA 140.000- 160.000).SDR 2010FA0000677Access Door · cracked(SPUY) CTR WING AUX TANK RT SIDE - NR 516 ACCESS DOOR FLANGE WITH (02 EA) CRACKS AROUND STA XCW 23000, S57 AND S58.SDR 2010FA0000676Cargo Track · corroded(SPUY) MAIN CARGO COMPT - NR 2 SEAT TRACK LUGS WORN AND CORRODED (STA 857.000- 880.000).SDR 2010FA0000675Vane · damaged(SPUY) LT WING - INBD VANE SLOT WITH ELONGATED HOLES AT STA XS 247.000.SDR 2010FA0000674Skin · corroded(SPUY) RUDDER LT SIDE PLATING CORRODED AT STA ZR 140.000.SDR 2010FA0000673Cargo Track · worn(SPUY) MAIN CARGO COMPT - NR 2 SEAT TRACK (03 EA) LUGS WORN AT STA 280.000.SDR 2010FA0000672Skin · dented(SPUY) LT HORIZ STAB - ELEVATOR UPPER PLATING DENTED 6" AT STA XE 90.000.SDR 2010FA0000671Access Door · cracked(SPUY) LT WING - NR505F ACCESS DOOR PLATING SURFACE UPPER PART CRACKED 1".SDR 2010FA0000670Skin · crackedNLG - LT AFT DOOR EXTERNAL SKIN CRACKED 1" AND WITH INTERIM REPAIR.SDR 2010FA0000669Fitting · cracked(SPUY) LT MLG WW, LT 24L, JOINT FITTNG LWR PART CRACKED .5" AT STA 879.000.SDR 2010FA0000668Fitting · corroded(SPUY) LT MLG WW - L-24L, JOINT FITTING LWR PART CORRODED AT STA 940.000.SDR DHLA201000059Skin · corrodedRT RUDDER SKIN CORRODED STA ZR159.094-168.656. PERFORMED MAJOR REPAIR IAW SRM 55-1-0 PG 1, SRM 55-6-1 FIG 1. REMOVED CORROSION IAW SRM 51-1-8, PG 17-18. FOUND OUT OF LIMITS IAW SRM 55-2-0 PG 12 FIG 6. REMOVED CORRODED PANEL PLATING IAW SRM 55-1-0 PG 1, SRM 5SDR DHLA201000035Seat Track · wornUPPER CARGO COMPT NR 2 TRACK LUGS WORN STA 1590.000-1615.000. PERFORMED MAJOR REPAIR IAW SRM 53-2-3 FIG 14, SHEET 1, PG 49-50. REMOVED WORN TRACK SEGMENT AND EXISTING SPLICES IAW SRM 53-1-0, PG 1, SRM 51-3-0. FABRICATED NEW TRACK SEGMENT (PN S2772660) IAW SSDR DHLA201000036Seat Track · wornUPPER CARGO COMPT. NR 2 TRACK LUGS WORN STA, 1550.000-1595.000. PERFORMED MAJOR REPAIR IAW SRM 53-2-3, FIG 14, SHEET 1-2, PG 49-50-51. REMOVED WORN TRACK SEGMENT AND EXISTING SPLICES IAW SRM 53-1-0 PG 1, SRM 51-3-0. FABRICATED NEW TRACK SEGMENT (PN S4889185)SDR DHLA201000063Skin · corrodedRT WING UPPER PLATING CORRODED STA XRS 76.869 S-9R. PERFORMED MAJOR REPAIR IAW SRM 57-2-1 FIG. 17. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-0 FIG. 7. CUT OUT DAMAGED AREA IAW SRM 57-2-1 FIG. 17. FABRICATED EXT DOUBLER (AL7075SDR DHLA201000060Longeron · corrodedFWD ACCY COMPT L-36 CORRODED STA 35.000. RESOLUTION: PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1, SRM 53-3-3 FIG. 2 SHEET 1 ITEM "A". REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. REMOVED CORRODED LONGERON IAW SRM 53-1-0 SDR DHLA201000058Frame · crackedMAIN CARGO COMPT. FRAME CRACKED 1" BS 220.000 L20-21R. PERFORMED MAJOR REPAIR IAW SRM 53-2-0 FIG 2 SHEET 2,6. REMOVED FRAME SEGMENT, ANGLE & SPLICE (EXISTING) IAW SRM 51-1-20D. FABRICATED NEW FRAME SEGMENT IAW SRM 53-2-0 FIG 2, SHEET 2, SRM 53-2-0 FIG 2 SHEETSDR DHLA201000061Skin · delaminatedNR 1 LT SPOILER PANEL DELAMINATED. R & R NR 1 LT SPOILER PANEL (REPAIRED CONDITION) IAW MM 27-61-1 PG 201-207. ADJUSTED GROUND SPOILER IAW MM 27-60-0, PG 509-510. REFER TO NR 218133 FOR OPS CHECK.SDR IXXA100031OConnector · dirtyDURING CLIMB OUT NR 4 BLEED AIR SHUTOFF VALVE CLOSED CONFIRMING NO BLEED FROM ENGINE. THE CREW CYCLED SWITCH SEVERAL TIMES AND MOVED THROTTLE WITH NO HELP. ON DESCENT NR 4 BLEED AIR SHUTOFF VALVE OPENED. THEY LANDED AT DEPARTURE WITHOUT FURTHER INCIDENT. MX INSDR DHLA201000064Angle · crackedNR 1 ENG PYLON LT UPPER ANGLE CRACKED .7500" STA YN 202.6. PERFORMED MAJOR REPAIR IAW FORM 8110-3 DATED 06-10-10, EVA D854-00335 REV IR DATED 05-13-10. REMOVED FASTENERS IAW SRM 51-1-21, SRM 51-1-20D. CUT OUT DAMAGED AREA IAW SMN DWG ED-5130 REV 01 DATED 05-07SDR DHLA201000062Frame · wornNR3 ENGINE T/R FIXED STRUCTURE FRAME WORN. STA YN 203.000 AT 7 O'COCK POS. PERFORMED MAJOR REPAIR IAW FORM 8110-3 DATED 06-10-10, EVA D878-00332 REV IR DATED 05-12-10. REMOVED FASTENERS IAW SRM 51-1-21, SRM 51-3-0. CUT OUT DAMAGED AREA IAW SMN DWG ED-5129 REVSDR DHLA201000056Longeron · crackedLT MLG W/W L-24L CRACKED 3" STA 902.000. PERFORMED MAJOR REPAIR IAW SRM 53-2-2 FIG. 5 SHEET 1,1,3,14,15,16,17,25,26,27 TR NR 53-123 DATED 05-15-01. REMOVED FASTENERS IAW SRM 51-1-20D. PERFORMED STOP HOLE AND DETAILED VISUAL INSP OF CRACKED END. NO CRACK FOUND.SDR IXXA100028OPin · brokenDURING CLIMBOUT, ON GEAR RETRACTION, THE CREW HEARD LOUD BANG, BOTH DOORS NOT LATCH LIGHT AND GEAR NOT LATCH LIGHT REMAINED ON. THEY RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. MX INSPECTED AND FOUND RT MLG RETRACT CYL ATTACH PIN BROKE. THEY REPLACED RETRSDR DHLA201000012Battery Pack · inoperativeEMERGENCY LIGHTING SYS WOULD NOT OPERATE DURING PREFLIGHT TEST. R & R BATTERY EMERGENCY RACK ASSY CHECK OPS GOOD IAW MM 33-11-0. ACFT WAS GROUNDED.SDR IXXA10SMN055SLongeron · corrodedDURING ROUTINE C-CHECK INSP, FOUND AFT ACCESSORY COMPARTMENT LONGERON 34 LT CORRODED AT STATION 1700.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED CORRODED LONGERON SEGMENT. FABRICATED STRAPS. CLEANED, TREATED, PRIMED AREA, STRAPS, AND NEW EXTRUSION. INSDR IXXA10SMN057SSeat Track · corrodedDURING ROUTINE C-CHECK INSP FOUND MAIN CARGO COMPARTMENT NR 2 SEAT TRACK LUGS WORN AND CORRODED AT STA 857.000 - 880.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. FABRICATED SPLICES. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALLSDR IXXA10SMN054SFlange · crackedDURING ROUTINE C-CHECK INSP FOUND CTR WING AUX TANK RT SIDE NR 516 ACCESS DOOR FLANGE WITH CRACKED AROUND STATION XCW 23000, STRINGER 57 AND STRINGER 58. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING ANGLES AND WEB TO GAIN ACCESS. REMOVED DASDR IXXA10SMN058SSeat Track · brokenDURING ROUTINE C-CHECK INSP FOUND MAIN CARGO COMPARTMENT NR 4 SEAT TRACK LUG PLUG BROKEN AT STA 140.000 -160.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED SEAT TRACK. REMOVED DAMAGED AREA. FABRICATED NEW SEAT TRACK SEGEMENT, SPLICES. CSDR IXXA10SMN053SSlot · damagedDURING ROUTINE C-CHECK INSPECTION FOUND LEFT WING INBOARD VANE SLOT WITH ELONGATED HOLES AT STATION XS 247.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED VANE SLOT. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO DISCREPANCY NOTED. FABRICSDR IXXA10SMN052SSkin · corrodedDURING ROUTINE C-CHECK INSPECTION FOUND RUDDER LEFT SIDE SKIN CORRODED AT STATION ZR 140.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN AND BONDED DOUBLER. BONDED PARTS AS NEEDED WITH HYSOL. CLEANED, TREATED, PRIMESDR DHLA201000010Fire Warning · activatedAFTER TAKEOFF, NR 1 ENGINE FIRE WARNING. (USING "A" LOOP) PERFORMED EMERGENCY PROCEDURES, FIRED BOTH BOTTLES. WARNING CONTINUED AFTER LANDING, PENDING; ACFT IS GROUNDED.SDR IXXA10SMN056SSeat Track · wornDURING ROUTINE C-CHECK INSP FOUND MAIN CARGO COMPARTMENT NR 2 SEAT TRACK LUGS ARE WORN AT STA 280.000. REMOVED DAMAGED FASTENERS AS NEEDED TO PERFORM RPAIR. REMOVED DAMAGED AREA. FABRICATED SEAT TRACK, SPLICES, SPLICES. CLEANED, TREATED, PRIMED AREA, AND REPSDR IXXA10SMN051SSkin · dentedDURING ROUTINE C-CHECK INSPECTION FOUND LEFT HORIZONTAL STABILIZER ELEVATOR UPPER SKIN DENTED AT STATION XE 90.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN, FINGER DOUBLER. BONDED PARTS AS NEEDED WITH HYSOL.SDR IXXA10SMN050SDoubler · crackedDURING ROUTINE C CHECK INSP, FOUND LT WING NR 505F ACCESS DOOR MATING SURFACE UPPER PART CRACKED. REMOVED CHANNEL AND FASTENERS. REMOVE DAMAGED AREA. PERFORMED NDT INSP. NO DISCREPANCY FOUND. FABRICATED EXTERNAL REPAIR DOUBLER, INTERNAL REPAIR DOUBLER, AND SDR IXXA10SMN049SSkin · crackedDURING ROUTINE C-CHECK INSP, FOUND LT NLG AFT DOOR EXTERNAL SKIN CRACKED. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED CRACKED SKIN. FABRICATED NEW SKIN. CLEANED, TREATED, PRIMED AREA AND REPAIR PART. INSTALLED NEW FASTENERS AND REPAIR PART IAW SRM CSDR DHLA201000009Skin · corrodedFUSELAGE SKIN CORRODED AT FS 25.25 AND LONGERON 33R . ACCOMPLISHED MAJOR REPAIR TO FUSE SKIN, FS 24.0 TO 70.0, L33R TO L36R IAW EVA D853-00327 & DWG D85300327-001-D. SEE NR 00007 FOR REPAIR DETAILS. REV IR DATED 4/8/10, DWG NO D85300327-001-D REV IR DATED 4/1SDR IXXA10SMN47SFitting · corrodedDURING C-CHECK INSP FOUND LT MLG WHEEL WELL JOINT FITTING LOWER PART CORRODED AT STA 940.000 LONGERON 24 LT. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. FABRICATED SPLICES, DOUBLER AND SHIMS. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. SDR IXXA10SMN048SFitting · crackedDURING ROUTINE C-CHECK INSP FOUND LT MLG WHEEL WELL JOINT FITTING LOWER PART CRACKED AT STA 879.000 LONGERON 24 LT. REMOVED CRACKED FITTING. FABRICATED NEW FITTING, SPLICES, DOUBLER, SHIMS. CLEANED, TREATED, AND PRIMED IAW SRM 51-1-8B. INSTALLED NEW FITTING SDR IXXA100027OUplock · failedDURING UPLATCH CHECK, GEAR NOT LATCH LIGHT CAME ON, CREW CYCLED THE GEAR AND GEAR NOT LATCH LIGHT REMAINED ON THE REMAINDER OF FLIGHT. THEY LANDED WITHOUT FURTHER INCIDENT. MX DEFERRED MAIN UPLATCH SYS, IAW MEL 32-16-01. MX FOUND THE LT AND RT MAIN GEAR ACTUATSDR IXXA100026OSwitch · defectiveDURING UPLATCH CHECK, GEAR NOT LATCH LIGHT CAME ON, THE CREW CYCLED GEARS AND THE GEAR NOT LATCH LIGHT REMAINED ON THE REMAINDER OF FLIGHT. THEY LANDED WITHOUT FURTHER INCIDENT. MX INSPECTED AND FOUND NLG UPLATCH OVER CTR MECHANISM BINDING, NOT GOING OVER CTRSDR IXXA100023OUplock · no testDURING "C" CHECK INSP TEST FLIGHT, GEAR UPLATCH CHECK FAILED AFTER TAKEOFF, THE CREW CYCLED GEAR AND UPLATCH CHECK FAILED A SECOND TIME WITH GEAR RED LIGHT STAYED ON. THEY RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. MX PERFORMED LANDING GEAR EXTENSION ASDR IXXA100022OWarning Light · illuminatedDURING CRUISE,THE CREW GOT UNSATISFACTORY UPLATCH CHECK, DOOR NOT LATCH LIGHT ILLUMINATED. THEY CYCLED GEAR, THE DOOR NOT LATCH LIGHT ILLUMINATED THEN GOES OUT INTERMITTENTLY DURING FLIGHT. THEY LANDED WITHOUT FURTHER INCIDENT. THE CREW DEFERRED DOOR LIGHT IAWSDR DHLA201000049Skin Panel · delaminatedNR 1 LT SPOILER EXTERNAL SKIN DELAMINATED 3". R & R NR 1 LT SPOILER PANEL (REPAIR CONDITION) IAW MM 27-61-1, PG 201-206. REFER TONR 225817 FOR OPS CHECK.SDR IXXA100020OGuide · misinstalledDURING TAKEOFF THE CREW USED EXCESSIVE DOWNWARD FORCE ON ELEVATOR. THEY REJECTED TAKEOFF AND RETURNED TO BLOCKS WITHOUT FURTHER INCIDENT. MX INSPECTED ELEVATORS AND FOUND CABLE GUIDE UNDER F/O`S FLOOR (FWD) NOT PROPERLY INSTALLED, BOLT ON CABLE SECTOR DRIVE RU
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