Douglas DC-8-62
Service difficulty reports · 2,778
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 = 'DC862' 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 = 'DC862' 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 ABXA9701284Longeron · crackedFORWARD WEB AT FS 960 TO 980, LONGERON 24 IS CRACKED. REPAIRED IAW DC-8 SRM 53-2-0.SDR ABXA9701283Frame · crackedCONTROL PEDESTAL FRAME CASTING CRACKED, LT AT BASE (FLOOR ATTACH POINT). REPAIRED IAW DC8 SRM 51-1-21 AND ABX REA D853-19823MR.SDR ABXA9701282Pressure Panel · corrodedFOUND CORROSION DAMAGE ON RT PRESSURE PANEL, UNDER PRODUCTION FINGER DOUBLERS WEB AT FS 159.5 TO FS 228. *S/D* REPAIRED IAW DC8 SRM 51-1-8 AND ABX REA D853-19564MR.SDR ABXA9701281Skin · crackedLOOSE RIVETS FOUND ON A DOUBLER AT FS 178 LT. WHEN REMOVED FOUND A 54 INCH CRACK AND AN 8 X 3.25 INCH CUTOUT IN THE FUSELAGE SKIN. INSTALLED DOUBLER AND FINGER DOUBLER IAW ABX REA D853-19550-MR.SDR IXXA980012Skin · corrodedDURING ROUTINE D CHECK INSPECTION, CORROSION WAS FOUND ON THE LEFT HORIZONTAL STABILIZER LEADING EDGE UPPER PLATING BETWEEN STATIONS XFS114 AND XFS178. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED AREAS, FABRICATION AND INSTALLATION OF INTERNAL FILLERS AND A EXTERSDR IXXA9800011Plating · corrodedDURING ROUTINE D-CHECK INSPECTION, CORROSION WAS FOUND ON THE LEFT HORIZONTAL STABILIZER LEADING EDGE UPPER PLATING BETWEEN STATIONS XFS114 AND XFS178. REPAIR ACCOMPLISHED CORROSION REMOVAL, FABRICATION AND INSTALLATION OF INTERNAL FILLERS AND AN EXTERNAL RSDR TC8A97035Engine · failedKLAX - TRIP NR 00398, NR 2 ENGINE STALL DURING TAKEOFF AT 60 KNOTS IAS. LOCKED OUT ENGINE AND PREPARED FOR 3 ENGINE FERRY PER GMM CHAP VIII AS REQUIRED. REMOVED ENGINE, SENT TO SHOP AND REINSTALLED NR 2 ENGINE. PERFORM TRIM RUN, OPS AND LEAK CHECKS GOOD IAWSDR TC8A97034Compressor · stalledREJECTED TAKEOFF DUE TO BIG BANG ENGINE NR 2 (STALL). INSPECTED PS3, PS4 AND PT2 LINES, NO DEFECTS NOTED. PERFORMED HIGH POWER RUN, NO DEFECTS NOTED. SWAPPED PRESSURE REGULATOR, HIGH STAGE BLEED AND CHECK VALVE IAW MM CHAPTER 36 FOR FURTHER TROUBLESHOOTING.SDR ABXA9701254Skin · wrinkledDURING C-CHECK, FOUND TOP LEFT SIDE OF RUDDER TO HAVE DENTS AND WRINKLED SKIN. REPLACED DAMAGED SKIN IAW DC8 SRM 51-1-21 AND DAC DWG 5655077-3.SDR ZIAA97020Track · chippedMCN - DURING SCHEDULED INSPECTION, FOUND LT WING, OUTBOARD FLAP, ICE BREAKER TRACK AT XFS345 BENT AND CHIPPED. REPAIRED DAMAGE IAW DER (COTNEY ENGINEERING) DWG C79-R04 AND DC8 SRM 51-1-8, 57-1-21. (M)SDR ZIAA97019Track · chippedMCN - DURING SCHEDULED INSPECTION, FOUND LEFT WING, OUTBOARD FLAP, ICE BREAKERS TRACK AT XFS415 BENT AND CHIPPED. REPAIRED DAMAGE IAW DER (COTNEY ENGINEERING) DWG C79-R04 AND DC8 SRM 51-1-8, 57-1-21. (M)SDR ZIAA97018Flap · chafedMCN - DURING SCHEDULED INSPECTION, RIGHT WING, OUTBOARD FLAP, UPPER SKIN, FOUND 2 CHAFFED THROUGH AREAS OF SURFACE DAMAGE: ONE 2.8 INCH BY 2.2 INCH AREA AT XFS 212, AND ONE 1.5 INCH BY 1.9 INCH AREA AT XFS 227. REPAIRED DAMAGED AREAS IAW DER (COTNEY ENGINEERISDR ZIAA97017Flap · chafedMCN - DURING SCHEDULED INSPECTION, RIGHT WING, INBOARD FLAP, UPPER SKIN, FOUND 2 CHAFFED THROUGH AREAS OF SURFACE DAMAGE ONE 2.2 INCH BY 1.7 INCH AREA AT XFS 90, AND ONE 2.2 INCH BY 2.1 INCH AREA AT XFS 105. REPAIRED DAMAGED AREAS IAW DER, COTNEY ENGINEERING,SDR ARWA970606Vertical Gyro · shortedF/O ADI INTERMITTENT FLAG ON ADI WHEN MANUVERING, RETURNED TO MIA FOR REPAIR. FOUND F/O'S VERTICAL GYRO EXTERNAL CASE SHORTED, 115V AT CASE. REMOVED AND REPLACED VERTICAL GYRO, OPS CHECK NORMAL IAW M/M 34-25-0.SDR ABXA9701225Panel · crackedRT WING PANEL 505F HAS CRACKS AT HOLES. REPAIRED IAW DC8 SRM 51-1-21 AND ABX REA D857-19555MR.SDR ABXA9701224Panel · crackedLT WING PANEL 505F HAS CRACKS AT HOLES. *S/D* REPAIRED PANEL IAW DC8 SRM 51-1-21 AND ABX REA D857-19566MR.SDR ZIAA97016Longereon · corrodedMCN - DURING SCHEDULED INSPECTION, FOUND LEVEL 2 CORROSION ON LONGERON NR 36 FROM FS 560 TO FS 570. REMOVED CORROSION AND REPAIRED IAW WITH DER APPROVED (COTNEY ENGINEERING) DWG NR C79-R01, AND DC8 SRM 51-1-8, 51-1-20D, 51-1-21. (M)SDR TC8A97032Pt2 Line · looseREJECTED TAKEOFF DUE TO NR 2 ENGINE STALLS AT 100 KTS. NR 2 ENGINE CHECKED AND FOUND PS4 FILTER CLOGGED AND PT2 LINE LOOSE. PS4 FILTER CLEANED AND PT2 LINE SECURED AS PER MM 75-30-2. ENGINE RUN CARRIED OUT, ALL CHECKS.SDR ZIAA97015Door Sill · damagedMCN - DURING SCHEDULED INSPECTION, FOUND TEMPORARY REPAIR INSTALLED ON NR 2 PIT DOOR SILL AREA AT FS 523. REMOVED TEMPORARY REPAIR AND INSTALLED PERMANENT REPAIR IAW WITH DACO ROD NR 97-06-25-04, AND DC8 SRM 51-1-8, 51-1-21, AND 51-2-20D. (M)SDR ZIAA97014Skin · crackedMCN - DURING SCHEDULED INSPECTION, FOUND FWD CREW ENTRY DOOR HOLD OPEN LATCH CUTOUT ON FUSELAGE SKIN WITH A .250 INCH CRACK. REPAIRED IAW WITH DER (COTNEY ENGINEERING) DWG C72-R01, AND DC8 SRM 51-1-8 AND 51-1-10. (M)SDR ARWA970605Proximity Switch · openON APPROACH LEFT MAIN LANDING GEAR GREEN LIGHT NOT ON. DOORS NOT LATCHED AND GEAR NOT LATCHED LIGHT ON. AIRCRAFT LANDING WITHOUT INCIDENT. REMOVED AND REPLACED LEFT GEAR DOWN PROXIMITY SWITCH. PERFORMED GEAR RETRACTION TEST I/A/W M/M 32-30-0. NO DEFECTS NSDR TC8A97031Fuel Control · malfunctionedREJECTED TAKEOFF DUE TO A BIG BANG ON THE LEFT SIDE OF AIRCRAFT. REMOVED AND REPLACED NR 1 FCU IAW 73-20-1, OPS AND LEAK CHECKED OK. PERFORMED HIGH SPEED TAXI'S AND NO DEFECTS AT THIS TIME, ENGINE PARAMETERS NORMAL.SDR ZIAA97013Pressure Web · crackedMCN - DURING SCHEDULED INSPECTION, FOUND 1.25 INCH CRACK AT FS 680, LOWER COMPARTMENT PRESSURE WEB, RT OUTBOARD LOWER CORNER. REPAIRED IAW DC8 SRM 53-2-5, PAGE 31-34. (M)SDR IXXA9700083Container · leakingSHORTLY AFTER TAKEOFF, CREW NOTICED FUMES ENTERING THE COCKPIT. FLIGHT ENGINEER WAS DISPATCHED TO INVESTIGATE MAIN CARGO DECK TO DETERMINE ORIGIN OF FUMES. THE FLIGHT ENGINEER CONFIRMED FUMES EMANATING FROM THE CARGO PALLET LOCATED IN THE NR 1 POSITION. CRESDR ARWA970604Cap · missingHYDRAULIC FAILURE IN CRUISE, HYD PRESS ZERO WITH MAIN PUMPS OR AUX PUMP, QUANTITY AND TEMP OK. FOUND MAIN HYD RESERVOIR CAP MISSING. REFILLED 15 GAL OF HYD FLUID. PERFORMED COMPLETE HYD POWER SYSTEM IAW MM 29-00. INSTALLED AND SAFETIED NEW CAP.SDR ARWA970601Battery Pack · dischargedMIA - FLT 615 - DURING PRE-FLIGHT INSPECTION, FOUND EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY PACK. SYSTEM OPS CHECK NORMAL IAW MM 33-50-1. AMENDMENT TO ORIGINAL ARWA970601. (X)SDR ABXA9701142O-Ring · deterioratedAFTER 50 MINUTES FLIGHT, LOST ONE-HALF QUANTITY OF GENERAL HYDRAULIC SYS. REPLACED O-RING AT LEFT HYDRAULIC PUMP. RESERVICED SYSTEM, OPS AND LEAK CHECKED GOOD.SDR TC8A97028Compressor · stalledAT 70 KNOTS, LOUD BANG AND BRIGHT FLASH NOTED ON LEFT SIDE. ENGINE INSTRUMENTS NORMAL, ABORTED TAKEOFF, RETURNED TO RAMP FOR INSPECTION. ACCOMPLISHED RUN-UP OF NR 1, 2, 3, 4 ENGINES IAW M/M 72-0 P/W. ALL ENGINES CHECK OK ON GROUND, NO DISCREPANCIES AT THIS SDR CKSA97314Door · not closedAFTER GEAR RETRACTION HEARD LOUD RUMBLE IN NOSE GEAR WELL. FOUND LEFT HAND NOSE GEAR DOOR OPEN. INSPECTED AREA, FOUND NO DEFECTS, CLOSED DOOR AND OPS CHECK GOOD.SDR CKSA97262Seal · rupturedLOST CABIN PRESSURIZATION AT FL290. CABIN RATE OF CLIMB WENT FROM 1000 TO 2000 FEET PER MINUTE. REGAINED CONTROL AT FL190. DESCENDED AIRCRAFT TO FL130 FOR FINAL CRUISE CEILING. CABIN STABILIZED AT 4000 FEET. LOUD NOISE ASSOCIATED WITH LOSE OF CABIN PRESSUSDR RRXA97182Floorbeam · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE ON FLOORBEAM, AT 1500 AND X=+36. TREATED AND REMOVED CORROSION FROM AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW FAA DER COTNEY ENGINEERING SKETCH C44-R57.SDR ARWA970505Fitting · corrodedMIA - DURING INSPECTION, FOUND RIGHT MLG WHEELWELL LONGERON 24, FS 940.000 SUPPORT FITTING HAS LEVEL 2 CORROSION UPPER AND LOWER AREAS. REMOVED AND DAMAGED FITTING PER SRM 51-3-0. REMOVED CORROSION FROM AREA IAW 51-1-8. TREATED AND PRIMED AREA IAW SRM 51-1-SDR ARWA970504Hinge · crackedDURING INSPECTION, FOUND BOTH MAIN L/G DOORS HINGE SUPPORT TOO MUCH PLAY AT KEEL BEAM. FOUND 4 INCH CRACK IN RT AND LT HINGE WITH EXCESSIVE WEAR. REMOVED AND REPLACED LT AND RT HINGES.SDR ARWA970503Support · crackedDURING INSPECTION, FOUND FWD AND AFT MAIN LANDING GEAR DOORS HINGE SUPPORTS CRACKED. FOUND NR 2, 7, 8, 9 TEE SUPPORTS CRACKED. REMOVED CRACKED SUPPORTS, CLEANED, TREATED AND PRIMED AREA. FABRICATED AND INSTALLED NEW SUPPORTS IAW DACO FAX ACTION NR 33065.SDR ARWA970502Fitting · corrodedMIA - DURING INSPECTION, FOUND LEFT WHEELWELL FORWARD AREA CENTER WING BOX OUTBOARD UPPER AREA SUPPORT FITTING AND AREA FORWARD HAVE LEVEL 2 CORRISION BEYOND LIMITS. REMOVED FASTENERS AND CORRODED MATERIAL. TREATED AND PRIMED AREA. FABRICATED AND INSTALLED SDR ARWA970501Floor Beam · crackedMIA - DURING INSPECTION, FOUND FS 920.000 FLOOR BEAM LT LOWER FORWARD AND AFT SIDE HAS LEVEL 2 CORROSION AND HAS CRACK. ALSO, THE AFT UPPER SIDE HAS LARGE AREA WITH CORROSION. REMOVED SECTION OF FLOOR BEAM AND SPLICE ANGLES IAW DACO FAC ACTION 330758/331021.SDR RRXA97181Frame · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE ON FRAME, AT Y=1530 BETWEEN LONGERONS 32R AND 36. *S/D* REMOVED CORRODED SECTION OF SPLICE FITTING AT Y=1530, IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR SPLICE DOUBLER IAW DC-8 SRM 53-2-5 FIGURE 8SDR TC8A97025Hydraulic Pump · failedLEFT ENGINE DRIVEN HYDRAULIC PUMP STUCK IN BYPASS. REMOVED AND REPLACED LEFT ENGINE DRIVEN HYDRAULIC PUMP IAW MM 29-10-12, OPS CHECKS NORMAL.SDR RRXA97103Fire Warning · malfunctionedFIRE BELL SOUNDED ACCOMPANIED BY MASTER FIRE WARNING LIGHT. NO LIGHT IN ANY FIRE LEVER WAS ILLUMINATED. TESTED ALL FIRE WARNING SWITCHES, NR 2 FIRE LIGHTS DID NOT ILLUMINATE. NR 2 WAS SHUT DOWN WITH ENG FIRE/DAMAGE CHECKLIST. BOTH FIRE BOTTLES WERE FIRED. SDR RRXA97132Plating · corrosionDURING A MAINTENANCE VISIT, FOUND CORROSION ON UPPER LEADING EDGE OF LEFT WING, AT XFS=32.75. *S/D* ATTACHED SCREW HOLES CORRODED BEYOND LIMITS, MATERIAL REMOVED WAS .001 TO .130. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 57-2-1 FIGURE 37.SDR RRXA97123Floorbeam · corrosionDURING A MAINTENANCE VISIT, FOUND LOWER AFT LEG OF TRANSVERSE FLOORBEAM SUPPORT CORRODED BEYOND LIMITATIONS, AT Y=902 AND X=-20 TO X-50. REMOVED CORROSION AND TREATED IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED SHIM AND STRAP REPAIR IAW DER APPROVED COTNEYSDR RRXA97106Frame · misdrilledDURING A MAINTENANCE VISIT, FOUND MISDRILLED HOLE IN CUSP RADIUS, AT Y=780 AND LONGERON 21R. *S/D* FABRICATED AND INSTALLED REPAIR IAW FAA DER COTNEY ENGINEERING SKETCH C44-R07.SDR RRXA97136Plating · gougedDURING A MAINTENANCE VISIT, FOUND AFT SIDE OF LT INBD FLAP GOUGED JUST ABOVE WEDGE AT Y=107 TO Y=117. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED REPAIR DOUBLER IAW DER APPROVED COTNEY ENGINEERING SKETCH C44-R02.SDR RRXA97135Frame · misdrilledDURING A MAINTENANCE VISIT, FOUND MISDRILLED HOLES IN FRAME RADIUS, AT Y=1120 AND ABOVE LONGERON 21L. FABRICATED AND INSTALLED REPAIR IAW DER APPROVED ENGINEERING SKETCH C44-R33.SDR RRXA97134Frame · misdrilledDURING A MAINTENANCE VISIT, FOUND MISDRILLED HOLE IN FRAME AND THUR HI-LOK, AT Y=760 AND LONGERON 18R. FABRICATED AND INSTALLED REPAIR IAW DER APPROVED COTNEY ENGINEERING SKETCH C44-R05.SDR RRXA97133Frame · misdrilledDURING A MAINTENANCE VISIT, FOUND MISDRILLED HOLES IN CUSP FITTING AND FRAME RADIUS, AT Y=300 AND LONGERON 21R. FABRICATED AND INSTALLED REPAIR ANGLE AND SHIMS IAW DER APPROVED ENGINEERING SKETCH C44-R24.SDR RRXA97131Frame · misdrilledDURING A MAINTENANCE VISIT, FOUND MISDRILLED HOLE IN FRAME RADIUS, AT Y=798 AND LONGERON 21L. PLUGGED HOLE WITH E RIVET. FABRICATED AND INSTALLED REPAIR IAW DER APPROVED ENGINEERING SKETCH C44-R54.SDR RRXA97130Frame · misdrilledDURING A MAINTENANCE VISIT, FOUND MISDRILLED HOLES IN FRAME RADIUS, AT Y=300 AND LONGERON 21L. FABRICATED AND INSTALLED REPAIR IAW DER APPROVED ENGINEERING SKETCH C44-R53.SDR RRXA97129Frame · misdrilledDURING A MIANTENANCE VISIT, FOUND MISDRILLED HOLES IN FRAME RADIUS, AT Y=920 AND LONGERON 19R. PLUGGED HOLE WITH E RIVETS. FABRICATED AND INSTALLED REPAIR ANGLE AND SHIMS IAW DER APPROVED ENGINEERING SKETCH C44-R52.SDR RRXA97127Frame · misdrilledDURING A MAINTENANCE VISIT, FOUND MISDRILLED HOLE THUR HI-LOK IN FRAME, AT Y=492 AND LONGERON 21R. FABRICATED AND INSTALLED REPAIR ANGLE AND SHIMS AND WEB IAW DER APPROVED ENGINEERING SKETCH C44-R50.
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