Douglas DC-8-62F
Service difficulty reports · 1,163
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 = 'DC862F' 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 = 'DC862F' 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 IXXA060265SFrame · misdrilledDURING ROUTINE C CHECK FOUND FRAME FLANGE WITH A DOUBLE DRILLED HOLE AT STATION Y560 AT LONGERON 14 RIGHT. REPAIRED PER ALL PPLICABLE DATASDR IXXA060264SFrame · misdrilledDURING ROUTINE C CHECK FOUND FRAME FLANGE WITH A DOUBLE DRILLED HOLE AT STATION Y500 AT LONGERON 7 RIGHT. REPAIRED PER ALL APPLICABLE DATASDR IXXA060263SFrame · misdrilledDURING ROUTINE C CHECK FOUND FRAME FLANGE WITH A DOUBLE DRILLED HOLE AT STATION Y420 AT LONGERON 7 RIGHT. REPAIRED PER ALL APPLICABLE DATASDR IXXA060262SFrame · misdrilledDURING ROUTINE C CHECK FOUND FRAME FLANGE WITH A DOUBLE DRILLED HOLE AT STATION Y1120 AT LONGERON 7 LEFT. REPAIRED PER ALL APPLICABLE DATA.SDR IXXA060261SFrame · misdrilledDURING ROUTINE C CHECK FOUND FRAME FLANGE WITH A DOUBLE DRILLED HOLE AT STATION Y834 LONGERON 7 LEFT. REPAIRED PER ALL APPLICABLE DATA.SDR IXXA060260SFrame · misdrilledDURING ROUTINE C CHECK FOUND DOUBLE DRILLED HOLE IN FRAME FLANGE AT STATION 640, LONGERON 7 LEFT. REPAIRED PER ALL APPLICABLE DATASDR IXXA060259SFrame · misdrilledDURING ROUTINE C CHECK FOUND DOUBLE DRILLED HOLES AT STATION 600 AT LONGERONS 7 LEFT AND 14 LEFT. REPAIRED PER ALL APPLICABLE DATA.SDR IXXA060345SSupport Fitting · crackedDURING ROUTINE C CHECK, FOUND AIR CONDITIONING FLOORBEAM SUPPORT FITTING CRACKED AT STATION Y253, +X45, -Z1. REPLACED FITTING PER ALL APPLICABLE DATA.SDR IXXA060341SBoss · corrodedDURING ROUTINE C CHECK, FOUND RIGHT MAIN LANDING GEAR SHOCK STRUT RETRACT PIN BOSS INNER SURFACE CORRODED. REPAIRED PER ALL APPLICABLE DATA.SDR IXXA060340SBeam · crackedDURING ROUTINE C CHECK, FOUND UPPER TRANSVERSAL BEAM CRACKED AT STATION Y260 -X45. REPAIRED PER ALL APPLICABLE DATA.SDR IXXA060339SBeam · crackedDURING ROUTINE C CHECK, FOUND UPPER TRANSVERSAL BEAM CRACKED AT STATION Y260 +X45. REPAIRED PER ALL APPLICABLE DATA.SDR IXXA060328SFitting · corrodedDURING ROUTINE C CHECK, FOUND LONGERON 24 RIGHT END FITTING CORRODED AT STATION Y212. REPAIRED PER ALL APPLICABLE DATA.SDR IXXA060327SLongeron · corrodedDURING ROUTINE C CHECK, FOUND A CORRODED LONGERON AT STATION Y267 LONGERON 22 LEFT. REPAIRED PER ALL APPLICABLE DATA.SDR IXXA060326SSkin · dentedDURING ROUTINE C CHECK, FOUND SKIN DENTED AT STATION Y1287 BETWEEN LONGERONS 34 LEFT AND 35 LEFT. REPAIRED PER ALL APPLICABLE DATA.SDR IXXA060338SWeb · corrodedDURING ROUTINE C CHECK, FOUND WEB CORRODED AT STATION Y148, +X52, -Z11. REPAIRED PER ALL APPLICABLE DATA.SDR IXXA060337SWeb · corrodedDURING ROUTINE C CHECK, FOUND WEB CORRODED AT STATION Y169, +X52, -Z11. REPAIRED PER ALL APPLICABLE DATA.SDR IXXA060333SAngle · corrodedDURING ROUTINE C CHECK, FOUND ANGLE CORRODED AT STATION Y190 LONGERON 33 RIGHT. REPAIRED PER ALL APPLICABLE DATA.SDR IXXA060336SWeb · corrodedDURING ROUTINE C CHECK, FOUND WEB CORRODED AT STATION Y169, -X52 AND -X58, -Z11. REPAIRED PER ALL APPLICABLE DATA.SDR IXXA060335SSupport · corrodedDURING ROUTINE C CHECK, FOUND CEILING SUPPORT CORRODED AT STATION Y101, +X45. REPAIRED PER ALL APPLICABLE DATA.SDR IXXA060334SFitting · corrodedDURING ROUTINE C CHECK, FOUND LONGERON 27 RIGHT END FITTING CORRODED AT STATION Y270. REPAIRED PER ALL APPLICABLE DATA.SDR IXXA060257SLongeron · crackedDURING ROUTINE C CHECK FOUND A CRACKED LONGERON FROM STATION Y1580 TO Y1586 AT LONGERON 15 LEFT. REPAIRED LONGERON PER ALL APPLICABLE DATA.SDR IXXA060332SFloor Panel · crackedDURING ROUTINE C CHECK, FOUND FORWARD CARGO COMPARTMENT FLOOR PANEL CRACKED FROM STATION Y480 TO Y500. REPAIRED PER ALL APPLICABLE DATA.SDR IXXA060331SFitting · crackedDURING ROUTINE C CHECK, FOUND END FITTING CRACKED AT LONGERON 22 RIGHT STATION Y990. REPAIRED PER ALL APPLICABLE DATA.SDR IXXA060330SFitting · crackedDURING ROUTINE C CHECK, FOUND LONGERON 23 LEFT END FITTING CRACKED AT STATION Y990. REPAIRED PER ALL APPLICABLE DATA.SDR IXXA060401SSkin · dentedDURING ROUTINE C CHECK, FOUND LEFT WING INBOARD FLAP UPPER LEADING EDGE SKIN DENTED AT STATION XW58. REPAIRED SKIN PER ALL APPLICABLE DATA.SDR IXXA060400SSkin · dentedDURING ROUTINE C CHECK, FOUND LEFT WING INBOARD FLAP TRAILING EDGE SKIN DENTED FROM STATION XRS172 TO XRS220. REPLACED SKIN PER ALL APPLICABLE DATA.SDR IXXA060399SSkin · dentedDURING ROUTINE C CHECK, FOUND LEFT WING OUTBOARD AILERON UPPER SKIN DENTED AT STATION XW671. REPLACED PER ALL APPLICABLE DATA.SDR IXXA060398SSkin · tool damageDURING ROUTINE C CHECK, FOUND A DOUBLE HOLE IN THE LEFT WING OUTBOARD AILERON AT STATION XW698. REPLACED PER ALL APPLICABLE DATA.SDR IXXA060329SSeat Track · corrodedDURING ROUTINE C CHECK, FOUND TRACK CORRODED FROM STATION Y1000 TO Y1100, Z0, -X60. REPAIRED PER ALL APPLICABLE DATA.SDR IXXA060325SFitting · crackedDURING ROUTINE C CHECK, FOUND CRACKED FITTING ST STATION Y101, +X20. REPAIRED PER ALL APPLICABLE DATA.SDR IXXA060324SAngle · corrodedDURING ROUTINE C CHECK, FOUND ANGLE CORRODED IN THE LEFT SIDE NOSE LANDING GEAR TUNNEL AT STATION Y102. REPAIRED PER ALL APPLICABLE DATA.SDR IXXA060256SFitting · misdrilledDURING ROUTINE C CHECK FOUND A FITTING WITH A DOUBLE HOLE AT STATION 1740 BETWEEN LONGERONS 10 LEFT AND 11 LEFT. REPLACED FITTING PER ALL APPLICABLE DATA.SDR IXXA060255SFloor Panel · corrodedDURING ROUTINE C CHECK FOUND FLOOR PANEL CORRODED BETWEEN STATIONS Y1542 AND Y1580 AT -X40 AND +X40. REPLACED FLOOR PANEL PER ALL APPLICABLE DATA.SDR IXXA060254SFloor Panel · corrodedDURING ROUTINE C CHECK FOUND FLOOR PANEL CORRODED AND LOOSE FASTENERS BETWEEN STATION Y1520 AND Y1542 AND BETWEEN -X40 AND +X40. REPLACED FLOOR PANEL PER ALL APPLICABLE DATA.SDR IXXA060253SFloor Panel · corrodedDURING ROUTINE C CHECK FOUND FLOOR PANEL CORRODED, WITH LOOSE RIVETS AND A DOUBLE HOLE. REPLACED FLOOR PANEL PER ALL APPLICABLE DATA.SDR IXXA060221SFillet · delaminatedDURING ROUTINE C CHECK FOUND WING FILLET PANEL NUMBER 162V DELAMINATED. REPAIRED PANEL PER COOPESA EO COO-CMP-8-53-273-04 DATED 07/15/2004.SDR IXXA060397SRib · crackedDURING ROUTINE C CHECK, FOUND LEFT WING LEADING EDGE CAVITY RIB CRACKED AT STATION XFS842. REPAIRED PER ALL APPLICABLE DATA.SDR IXXA060396SRib · crackedDURING ROUTINE C CHECK, FOUND LEFT WING LEADING EDGE CAVITY RIB CRACKED AT STATION XFS780. REPLACED PER ALL APPLICABLE DATA.SDR IXXA060395SSkin · dentedDURING ROUTINE C CHECK, FOUND LEFT WING OUTBOARD FLAP UPPER SKIN DENTED AT STATION XF440. REPAIRED PER ALL APPLICABLE DATA.SDR IXXA060363SPanel · bulgedDURING ROUTINE C CHECK FOUND LEFT HAND HORIZONTAL STABILIZER TRAILING EDGE LOWER PANELS AT STATIONS ZR267.218, ZR276.531, AND ZR284.75 BULGED. REPAIRED PER ALL APPLICABLE DATA.SDR IXXA060322SSpar · corrodedDURING ROUTINE C CHECK FOUND VERTICAL STABILIZER RIGHT SIDE REAR SPAR INTERNAL AREA CORRODED AT STATION ZV299. REPAIRED PER ALL APPLICABLE DATA.SDR IXXA060321SPanel · bulgedDURING ROUTINE C CHECK, FOUND RUDDER LEFT SIDE AFT SKIN PANEL BULGED FROM STATION ZR100 TO ZR110. REPAIRED PER ALL APPLICABLE DATA.SDR IXXA060252SSkin · crackedDURING ROUTINE C CHECK FOUND SKIN CRACKED AT STATION 215 BETWEEN LONGERONS 15 LEFT AND 16 LEFT, (FORWARD ENTRANCE DOOR HOLD OPEN PIN CUTOUT). REPAIRED PER ALL APPLICABLE DATA.SDR IXXA060250SSkin · crackedDURING ROUTINE C CHECK FOUND SKIN CRACKED AND SHEARED FASTENERS AT STATION Y1589 BETWEEN LONGERONS 15 LEFT AND 17 LEFT. REPAIRED PER ALL APPLICABLE DATA.SDR IXXA060217SLongeron Splice · crackedDURING ROUTINE C CHECK FOUND A CRACKED LONGERON SPLICE BETWEEN STATION 600 AND 620 AT LONGERON 31 LEFT. REPLACED LONGERON SPLICE PER ALL APPLICABLE DATA.SDR IXXA060216SDoor Frame · crackedDURING ROUTINE C CHECK FOUND FORWARD CARGO COMPARTMENT DOOR FRAME CRACKED AT THE UPPER AFT CORNER. REPAIRED DOOR FRAME PER ALL APPLICABLE DATA.SDR IXXA060430SSkin · corrodedDURING ROUTINE C CHECK, FOUND RIGHT WING LEADING EDGE UPPER SKIN CORRODED FROM STATION XW257 TO XW260. REPAIRED PER ALL APPLICABLE DATA.SDR IXXA060429SSkin · corrodedDURING ROUTINE C CHECK, FOUND RIGHT WING UPPER IN BOARD PANEL (DIHEDRAL) SKIN, CORRODED. REPAIRED PER ALL APPLICABLE DATA.SDR IXXA060428SSkin · corrodedDURING ROUTINE C CHECK, FOUND RIGHT WING LEADING EDGE SKIN CORRODED AT STATIONS XFS -11.250 THRU XFS63.750. REPAIRED PER ALL APPLICABLE DATA.SDR IXXA060251SSeat Track · wornDURING ROUTINE C CHECK FOUND A SEAT TRACK WORN OUT OF LIMITS BETWEEN STATIONS Y400 AND Y420 AT -X45. REPLACED SEAT TRACK PER ALL APPLICABLE DATA.
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