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 IXXA9900028Fuel Filter · dirtyEN ROUTE FROM LAX TO TOL, THE NUMBER ONE ENGINE FLAMED OUT DURING CRUISE. THE FLIGHT CREW FOLLOWED COMPANY PROCEDURES AND CONTINUED TO TOL FOR AN UNEVENFULL LANDING. MAINTENANCE INSPECTED THE ENGINE AND PERFORMED THE NECESSARY TROUBLESHOOTING PROCEDURES IN ASDR UPS99831032Skin · crackedINSPECTION TYPE:SV, FWD LWR NOSE SKIN CREASED AND TORN STA -85 TO -80 L31L TO 28L CRACKED APRROX 15.0. REMOVED DAMAGE SECTION OF SKIN, FABBED DOUBLER, FILLER AND SPLICE DOUBLER IAW REO-06778, INSTALLED DOUBLER, FILLER AND SPLICE DOUBLER IAW DC8 SRM 51-1-20D, SDR UPS99831031Skin · crackedINSPECTION TYPE:SV, FWD LWR NOSE SKIN CREASE AND TORN STA -99 TO-93, L31R TO L28R. REMOVED DAMAGED SECTION OF SKIN AND DAMAGED FRAME, FABRICATED NEW SKIN SECTION AND DOUBLERS IAW REO -06765, LOCATED NEW FRAME SKIN SECTION AND DOUBLERS, DRILLED UP IAW DC8 SRM SDR UPS99830979Fasteners · missingINSPECTION TYPE:N/A, AFT RT EMERGENCY EXIT DOOR LWR EDGE HAS SEVEN MISSING FASTENERS. *S/D* REMOVED R5 DOOR, REPLACED NUT PLATE CHANNEL AND INSTALLED SCREWS IAW SRM 51-3-0. REINSTALLED DOOR REF LG 416910 ITEM 2.SDR RRXA991780Intercostal · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO INTERCOSTAL BETWEEN STA 980 TO STA 995 AND LONGERON 35 LEFT. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW INTERCOSTAL IAW DC-8 SSDR UPS99830966Battery Pack · dischargedEMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK. OPS CHECK GOOD.SDR IXXA9900025Ballast · odorEN ROUTE FROM TOL TO LAX, THE FLIGHT CREW SENSED AN ODOR IN THE COCKPIT. THE FLIGHT CREW EXTINGISHED THE OVERHEAD FLUORESCENT LIGHTING SYSTM AND THE ODOR SUBSIDED. THE FLIGHT CONTINUED TO LAX FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE LIGHTING SYSSDR UPS99830962Spar · crackedINSPECTION TYPE:C123, THE CENTER WING REAR SPAR LOWER CHORD WAS CRACKED AT XCW 0 TO XCW 2.5. STOP DRILLED CRACKS AND REPAIRED THE SPAR CHORD IAW DH SK718-583.SDR UPS99830906Battery Pack · dischargedEMERGENCY LIGHTS WILL NOT TEST. REPLACED EMERGENCY LIGHT BATTERY AND RELAY UNIT PER MM 33-50-01, LIGHTS TEST OK.SDR UPS99830905Battery Pack · dischargedEMERGENCY LIGHTS INOP. REPLACED EMERGENCY EXIT LIGHT BATTERY PACK AND OPS CHECK OK IAW MM 33-50-00.SDR UPS99830943Skin · crackedINSPECTION TYPE:SV 1 CRACK IN WING SKIN LT WING 18 I/B OF NR 1 PYLON. FABRICATED AND INSTALLED ALL BUSHINGS IAW REO 06799. FABBED STRAPS, SPLICES, DOUBLER, TRIPLER AND SKIN FILLER. CUT INTERNAL DOUBLER AND FABBED REPLACEMENT SEGMENT OF INTERNAL DOUBLER, TRISDR UPS99830871Battery Pack · dischargedINSPECTION TYPE:N/A, EMERGENCY LIGHTS DISARM CHECK FAILED. REPLACED DEAD BATTERY AND RELAY ASSY IAW MM 35-50-01, REPAIRED OPEN IN WIRE HVL9812R22 IN CHARGING CIRCUIT. REPAIRES OPEN AT SWITCH S1-3 27 A1 WIRE L9608A24. SYSTEM OPS NORMAL REF WDM 33-50-01.SDR RRXA991785Intercostal · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO INTERCOSTAL BETWEEN STA 520 TO STA 540 AND LONGERON 32 RIGHT. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW INTERCOSTAL IAW DC-8 SDR UPS99830874Skin · cracked1.5 INCH CRACK RIGHT WING LOWER SURFACE INB'D OF NR 3 PYLON. CRACK IS ON BOTH SIDES OF RIVET. REPAIRED AREA IAW SRM 57-2-1 FIG 35 AND SRM 57-2-1.SDR UPS99830868Window · jamedINSPECTION TYPE:N/A, F/O SLIDING WINDOW WILL NOT OPEN (JAMMED SHUT). ADJUSTED F/O WINDOW PER MM 56-10-03, OPS CHECK GOOD.SDR RRXA991781Frame · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FRAME AT STA 1280 AND LONGERON 35 LEFT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR SPLICE IAW DC-8 SRM 51-1-21. CORROSION DSDR IXXA900024Uplatch · dirtyEN ROUTE FROM LAX TO TOL, THE LANDING GEAR UNSAFE LIGHT ILLUMINATED DURING THE GEAR UPLATCH CHECK. THE FLIGHT CREW CYCLED THE GEAR AND THE WARNING INDICATION EXTINGUISHED. THE FLIGHT CONTINUED TO TOL FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE LANDSDR UPS99830839Fire Warning · activatedINSPECTION TYPE:N/A, NR 4 FIRE WARNING CAME ON AFTER SHUTTING DOWN ENGINES. RAN PROCEDURES AND DISCHARGED ONE FIRE BOTTLE. LIGHT WENT OUT AFTER 30 SECONDS AND TESTED NORMAL. REMOVED AND REPLACED FIRE BOTTLE ON RIGHT WING OUTBOARD POSITION PER 26-20-01. INSDR UPS99830919Fitting · crackedINSPECTION TYPE:C123, FITTING (P/N 5804007T6013) AT XRS 508, LT WING FOUND TO BE CRACKED. REMOVED, FABRICATED AND REPLACED THE FITTING IAW DWG 5804007 AND SRM 51-1-20D.SDR RRXA991783Bolt · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO CARGO DOOR T-BOLT BETWEEN STA 280 TO STA 340 AND LONGERON 29 RIGHT. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED NEW T-BOLT AND INSTALLED DC-8 SRM 5SDR RRXA991784Frame · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FRAME AT STA 1420 AND LONGERON 36. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR SPLICE IAW DC-8 SRM 53-2-0. CORROSION DAMAGESDR RRXA991515Lock · out of adjustAFTER GEAR RETRACTION, LOUD NOISE IN NOSE GEAR AREA, CYCLED GEAR NO HELP. ADJ NLG DOOR LOCKS, LUBED, INSPECTED SWUNG GEAR 3 TIMES. OPS CHECK GOOD AT THIS TIME.SDR UPS99830834Rib · crackedINSPECTION TYPE:C123 LT WING L/E RIB AT STA XFS340 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.SDR UPS99830756Battery Pack · dischargedINSPECTION TYPE:N/A, EMERGENCY LIGHTS DID NOT OPERATE WHEN TESTED. REMOVED AND REPLACED EMERGENCY BATTERY PACK ASSY PER M/M 33-50-01, OPS CHECK GOOD.SDR UPS99830757Light · inopINSPECTION TYPE:N/A, EMERGENCY LIGHTS WILL NOT DISARM. PERFORMED EMERGENCY LIGHT OPERATIONAL TEST IAW MM REF 33-50-01 PAGE 201, OPS CHECK GOOD.SDR UPS99830857Longeron · crackedINSPECTION TYPE:C123 LONGERON 35R IS CRACKED AT FS 1050. CUT OUT DAMAGED AREA AND SPLICED LONGERON IAW DH SK718-251.SDR UPS99830729Brake · inopINSPECTION TYPE:N/A, BTB - NUMBER 8 BRAKE STUCK. REMOVED AND REPLACED MAIN BRAKE ASSY PER MM 32-42-01.SDR RRXA991782Finger Doubler · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FINGER DOUBLER AT STA -25 AND BL 36L AND WL -9. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FINGER DOUBLER IAW DC-8 SRM 53-3-1.SDR UPS99830691Skin · cracked1 INCH CRACK LEFT WING LWR SURFACE (18 INCHES INBOARD NR 1 PYLON).SDR RRXA991775Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO LEFT WING, LEADING EDGE, TOP SKIN AT XFS=793. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGED SECTION, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED SDR RRXA991630Plank · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, HORIZONTAL STABILIZER, CENTER SECTION UPPER CENTER PLANK UPPER SURFACE AT RBL X30. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED PLANK IAW SB 55-SDR RRXA991521Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, HORIZONTAL STAB, CENTER SECTION, UPPER CENTER PLANK, UPPER SURFACE AT BL -30 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED PLANK IAW DC8 SBSDR UPS99830651Hyd Line · leakingINSPECTION TYPE:N/A, ATB-DISCOVERED HYD QTY LOSS. DECREASED TO AUX WITH ENGINE HYD PUMPS IN BYPASS. AFTER LANDING MX FOUND STAB TRIM HYDRAULIC MOTOR BRAKE RETURN LINE LEAKING. *S/D* INSTALLED INTERIM REPAIR (FLEX LINE) AT THE STAB TRIM HYD BRAKE PER GMM 3-SDR RRXA991776Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO LEFT WING, SKIN SECTION AT XW=693 AND BETWEEN STRINGERS 2 TO 4. CORROSION DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGED SECTION, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPASDR UPS99830795Fitting · crackedINSPECTION TYPE:C123, RT WING O/B SIDE OF THE STA XRS 74.9, THE STR 51 AFT END FITTING WAS CRACKED. REMOVED AND REPLACED THE FITTING IAW SRM 51-1-20D & 51-3-0.SDR 99ZZZX3809Fitting · crackedFITTING CRACKED MORE THAN 90 PERCENT OF FITTING AT FLAP ATTACH POINT, DEFECT NOTED DURING FLAP OVERHAUL. FLAP RECEIVED FOR OVERHAUL DUE TO AIRCRAFT IN D-CHECK.SDR UPS99830856Doubler · crackedINSPECTION TYPE:C123 RT WING LWR L/E SKIN DOUBLER AT XFS 305 IS CRACKED AT ACCESS PANEL 524B. REMOVED, FABRICATED, AND REPLACED THE DOUBLER IAW DWG 5641252 AND SRM 51-1-20D AND 51-1-21.SDR UPS99830789Clip · crackedINSPECTION TYPE:C123, RT WING L/E ABOVE AND FWD OF THE NR 3 PYLON CUTOUT STA FS 254.25, THE RIB FWD ATTACH CLIP WAS CRACKED. REMOVED, FABRICATED AND REPLACED THE CLIP IAW DWG 9753294 AND SRM 51-1-20D.SDR UPS99830788Rib · crackedINSPECTION TYPE:C123, RT WING L/E RIB AT FS 304.0 WAS CRACKED AT THE AFT UPPER END. STOP DRILLED THE CRACK AND REPAIRED THE RIB IAW SRM 57-2-0 FIG 2.SDR UPS99830787Doubler · crackedINSPECTION TYPE:C123, RT WING LWR L/E SKIN INTERNAL DOUBLER AT XS 520.168 WAS CRACKED AND A PIECE WAS BROKEN OFF. REMOVED, FABRICATED AND REPLACED THE DOUBLER IAW SRM 57-3-1 FIG 5 AND 51-3-0.SDR UPS99830786Rib · crackedINSPECTION TYPE:C123, RT WING L/E RIB AT XS 442.185 WAS CRACKED AT THE AFT UPPER END. STOP DRILLED THE CRACK AND REPAIRED THE RIB IAW SRM 57-2-0 FIG 2.SDR UPS99830785Rib · crackedINSPECTION TYPE:C123, RT WING L/E RIB AT XS 448.581 WAS CRACKED AT THE AFT UPPER END. STOP DRILLED THE CRACK AND REPAIRED THE RIB IAW SRM 57-2-0 FIG 2.SDR UPS99830784Rib · crackedINSPECTION TYPE:C123, RT WING L/E RIB AT XS 454.976 WAS CRACKED AT THE AFT UPPER END. REPAIRED THE RIB IAW SRM 57-2-0 FIG 2.SDR UPS99830783Angle · crackedINSPECTION TYPE:C123, RT WING L/E, INBOARD SIDE OF THE XS 520.168 RIB, THE SLOT AFT BLKHD VERTICAL ATTACH ANGLE WAS CRACKED AT THE BOTTOM. REMOVED, FABRICATED AND REPLACED THE ANGLE IAW DWG 9753297 AND SRM 51-1-20D.SDR UPS99830782Rib · crackedINSPECTION TYPE:C123, RT WING L/E RIB AT FS 297.5 WAS CRACKED AT THE AFT LWR END. STOP DRILLED THE CRACK AND REPAIRED THE RIB IAW SRM 57-2-0.SDR UPS99830781Rib · crackedINSPECTION TYPE:C123, RT WING L/E RIB AT FS 735 WAS CRACKED AT THE AFT LWR END. STOP DRILLED THE CRACK AND REPAIRED THE RIB IAW SRM 57-2-0.SDR UPS99830779Rib · crackedINSPECTION TYPE:C123, LT WING L/E RIB AT FS 835 WAS CRACKED AT THE AFT UPPER END. STOP DRILLED THE CRACK AND REPAIRED THE RIB IAW SRM 57-2-0.SDR UPS99830778Doubler · crackedINSPECTION TYPE:C123, LT WING L/E LWR SKIN DOUBLER AT FS 570.5 WAS CRACKED AT THE DRAIN HOLE. REMOVED, FABRICATED AND REPLACED THE DOUBLER IAW DWG 5769600 AND SRM 51-1-20D & 51-1-21.SDR UPS99830777Rib · crackedINSPECTION TYPE:C123, RT WING L/E RIB AT FS 335.25 WAS CRACKED AT THE AFT UPPER END. STOP DRILLED THE CRACK AND REPAIRED THE RIB IAW SRM 57-2-0.SDR UPS99830769Rib · crackedINSPECTION TYPE:C123, LT WING L/E RIB AT STA XFS 841.250 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.
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