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 UPS00834563Bellcrank · damagedINSPECTION TYPE:N/A DURING DESCENT AT 340 KIAS, LOUD NOISE FROM NOSE WHEEL AREA. ALSO A CCOMPANIED BY MODERATE AIRFRAME VIBRATION. BOTH WENT AWAY WHEN GEAR CAME DOWN. ON BASE LEG, ANOTHER LOUD NOISE (THUD). REPLACED FWD NOSE GEAR DOOR TORQUE TUBE BELLCSDR RRXA001095Duct · failedCLIMBING THRU 12,000 FEET NR 2 ENGINE FIRE WARNING SOUNDED. SECURED ENGINE PER EWW QRH. UPON INSPECTION OF ENGINE FOUND HIGH STAGE BLEED DUCT CRACKED AT FLEX COUPLING. REMOVED AND REPLACED HIGH STAGE BLEED DUCT IAW DC-8 M/M CH 36-11-61 AND FIRE WARNING CHECSDR UPS00834552Unknown · odorINSPECTION TYPE:N/A BURNING SMELL IN COCKPIT DURING DEPARTURE NR 1 XFER RECTIFIER SHORTED DUE TO WATER INTRUSION DRIED OUT WATER AND DEFEREDSDR UPS00834551Slide · inoperativeINSPECTION TYPE:N/A ESCAPE SLIDE INOP REFERENCE M205259 ***SUPPLEMENTAL MRR*** R/R EVACUATION SLIDE & CONTAINER PER M/M 25-62-00. OPS CK NORMAL IN GERT BAR. THIS CLEARS M 205259. PLACARD REMOVED.SDR RRXA001089Computer · faultyDURING CRUISE FLIGHT AIRCRAFT REQUIRED 3 UNITS RIGHT RUDDER TRIM FOR COORDINATED FLIGHT DEPOWERED RUDDER TO MAINTAIN A/C CONTROL ACCOMPLISED QRH. REMOVED AND REPLACED YAW COMPUTER, OP'S CK'D GOOD IAW DC-8 M/M 22-11-1 AND 22-10-0. RT SPOILER SWIVEL LEAKING. SDR IXXA0000044Uplock · lack of lubeENROUTE FROM PDX TO TOL, AFTER T.O. THE GEAR DOOR WARNING LIGHT ILLUMINATED WITH THE GEAR RETRACTED. THE FLIGHT CREW CYCLED GEAR WITH THE DOOR WARNING INDICATION REMAINING THE SAME. THE FLIGHT RETURNED TO PDX FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED TSDR UPS00834541Battery Pack · inoperativeINSPECTION TYPE:PFLT EMERGENCY LIGHT INOP R/R BATTERY PACK ASSY PER MM 33-50-00SDR UPS00834536Coupling · leakingINSPECTION TYPE:N/A PIREP-FUEL LEAKING FROM RH WING ***SUPPLEMENTAL MRR*** FOUND GAMA COUPLING LEAKING RT INBD WING REPAIRED COUPLING NOTE: THIS WAS ON THE DAILY EXCP AGAINST 703 WHEN IT SHOULD HAVE BEE N TAIL 801 LOG PAGE ON THIS MRR IS ON 801 VOIDED THISSDR IXXA0000043Switch · misriggedGEAR FAILED UPLATCH CHECK. CYCLED SEVERAL TIMES FOLLOWED ATI DOOR WARNING CHECKLIST. FOUND INDICATION PROBLEM AND CONTINUED ACCORDING TO ATI CHECKLIST. 30 MIN LATER LIGHT WENT OUT. CREW LANDED UNEVENTLY AT DESTINATION. MAINTENANCE PERFORMED GEAR SWING AND COULSDR RRXA001085Switch · failedHAD SMOKE & BURNING SMELL IN COCKPIT COMING FROM OVERHEAD PANEL AROUND THE AREA OF THE #4 FIRE HANDLE. TURNED OFF ALL INSTRUMENT LIGHTING INPANEL. SMOKE STOPPED. SHORTLY THERE AFTER HAD STRONG BURNING SMELL. REMAINED, AND CREWW NEEDED TO WEAR O2 MASKS LASTSDR RRXA010514Structure · damagedDURING A MAINTENANCE VISIT FOUND SHEET METAL DAMAGE TO O/B T/E OF THE RT ELEVATOR, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED PART IAW DC-8 SRM 51-1-21 AND EO #00-306.SDR RRXA010512Skin · damagedDURING A MAINTENANCE VISIT FOUND SHEET METAL DAMAGE AFT CENTER OF THE "C" PIT DOOR, DAMAGE EXCEEDED LIMITATIONS IAAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR PER EO 00-306.SDR RRXA010511Structure · damagedDURING A MAINTENANCE VISIT FOUND DAMAGE TO THE SHEET METAL ON THE O/B T/E OF THE RT ELEVATOR, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 51-1-21 AND EO SDR RRXA003616Indicator · malfunctionedNO NOSE GEAR DOWN GREEN LIGHT WHEN GEAR WAS EXTENDED FOR LANDING, RAN EMERGENCY CHECK LIST AND LANDED WITHOUT INCIDENT.SDR RRXA003615Landing Gear · failedGEAR WOULD NOT RAISE AFTER T/O MECHANICAL GROUND SHIFT PROBLEM. JACKED AIRCRAFT. ACCOMPLISHED GEAR SWING IAW DC-8 MM 32-30-0. GEAR SWINGS NORMALLY IAW DC-8 MM 32-30-0. INSPECTED NOSE GEAR GROUND SHIFT AND OPS CHECKS GOOD IAW 32-23-1. LUBED NOSE GEAR & GROUND SDR RRXA003614Switch · out of adjWHEN LANDING GEAR WAS HYD LOWERED, NO NOSE GEAR DOWN GREEN & GEAR UNSAFE LIGHT STAYED ON. ADJUSTED DOOR SWITCH AND FOUND TO BE OK IAW DC-8 MM32-30-0.SDR RRXA003613Check Valve · misinstalledAFTER T/O UNABLE TO RAISE LANDING GEAR, NO MECHANICAL OR ELECT. GROUND SHIFT. SEPARATED INNER & OUTER NOSE STRUT. FOUND PISTON HEAD & RETURN CHECK VALVE INSTALLED UPSIDE DOWN. INSTALLED PISTON HEAD & CHECK VALVE CORRECTLY IAW DC-8 OHM 32-2-1. GROUND SHIFT CHESDR UPS00834471Warning Light · illuminatedINSPECTION TYPE: BTB - ABORTED TAKEOFF TWICE DUE MASTER WARNING LIGHT FLICKERED ON AND OFF AT 40 KTS.SDR RRXA003683Tire · failedON LANDING TIRES NR 3 & 4 BLEW. REMOVED AND INSPTED AXEL THREADS. REPLACED NR 3 & 4 WHEEL ASSEMBLIES IAW DC-8 MM 32-41-05. FOUND MLG ANTI-SKID INOP, TROUBLESHOT SYSTEM, FOUND BAD ANTI-SKID CONTROL VALVE. REMOVED AND REPLACED CONTROL VALVE IAW DC-8 MM 32-43-3SDR UPS00834352Indicator · failedINSPECTION TYPE:N/A, DURING BEFORE T/O CHECKLIST ON ELEVATOR CHECK FAILED. RETURN TO BLOCKS FOR MAINTENANCE INSPECTION. ELEVATOR FELT AS IF IT DID NOT MOVE AFTER SEVERAL ATTEMPTS. EPI SHOWED NO MOVEMENT. PERFORMED ELEVATOR POSITION INDICATION SYSTEM ADJ/TESDR RRXA003331Nose Cowl · dentedDURING A MAINTENANCE VISIT FOUND A DENT TO THE NR 2 ENGINE NOSE COWL AT 9 O'CLOCK POSITION, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 71-5-1 AND EO#00-262 WITH APPRSDR RRXA003330Panel · delaminatedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE WING PANEL O/B OF MLG AT STA XRS 76, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 SRM 51-3-0.SDR RRXA003333Seat Track · damagedDURING A MAINTENANCE VISIT FOUND A BROKEN SEAT TRACK LOCKING TAB NR 1 FROM LEFT TO RIGHT NR 5 BEAR CLAW UNDER BEAR CLAW, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IASDR RRXA003332Seat Track · damagedDURING A MAINTENANCE VISIT FOUND A BROKEN LUG AT NR 3 SEAT TRACK AT FWD PALLET STOP AT FS 80, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 51-3-0.SDR RRXA003842Fitting · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO CANTER BULKHEAD BRACKET AT STA. 1766 AND L3R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51SDR UPS00834420Fitting · crackedINSPECTION TYPE:C2, AFT LONGERON 29 RIGHT SPLICE FITTING CRACKED STA 1680. REMOVED AND REPLACED CRACKED FITTING PO 341342 (P/N 46413246502).SDR IXXA0000036Uplock Roller · lack of lubeEN ROUTE FROM IAH TO TOL, THE GEAR NOT LATCH LIGHT ILLUMINATED DURING THE LANDING GEAR UPLATCH CHECK. THE FLIGHT CREW CYCLED THE GEAR BUT THE WARNING INDICATION REMAINED THE SAME. THE FLIGHT CONTINUED TO TOL FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED SDR UPS00834260Line · leakingINSPECTION TYPE:N/A, COURIER''S O2 REGULATOR PROBLEM. *S/D* REPLACED BROKEN O2 LINE, OPS CK NORMAL.SDR UPS00834259Slide · inoperativeINSPECTION TYPE:N/A, ESCAPE SLIDE WILL NOT ARM. ATTACHED GIRT BAR.SDR UPS00834412Seat Track · corrodedINSPECTION TYPE:C2, SEAT TRACK FLANGE CORRODED BL 0 STA 1124. REPAIRED SEAT TRACK IAW REO G07703.SDR RRXA003837Vane · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO #1 FLAP VANE ABOVE I/B END, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 SRM 27-51-14.SDR UPS00834415Fitting · crackedINSPECTION TYPE:C2, FWD LONGERON 29R SPLICE FITTING CRACKED AT STA 1680. REMOVED AND REPLACED FITTING.SDR RRXA001073Thermocouple · malfunctionedNR 2 EGT ERRATIC IN CLIMB 620 - 1000 PRECAUTION ENGINE SHUT DOWN. REMOVED AND REPLACED 1 THERMOCOUPLE ASSY IAW MM 77-20-3. REMOVED AND REPLACED LEAD ASSY FROM EGT HARNESS HALF TO PYLON. REPAIRED WIRING IN PYLON. PERFORMED 35 MIN HIGH PWR RUN IAW DC-8 EWA RSDR RRXA003225Plate · damagedDURING A MAINTENANCE VISIT FOUND ELONGATED HOLE IN PLATE VERT STAB AT STA 1680 LEFT L/E, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.SDR RRXA003224Stiffener · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE STIFFENERS ON THE WEB BELOW HORIZ STAB. CONSTANT SECTION AT STA 1810 INSIDE ACC 60, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.SDR RRXA003223Sill · crackedDURING A MAINTENANCE VISIT FOUND A CRACK AND DOUBLE DRILLED HOLES TO THE R-1 DOOR SILL PLATE, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.SDR RRXA003222Frame · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE FRAME IN BEND RADIUS UNDER NUT PLATE A PIT AT STA 140 AND L36, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.SDR RRXA003221Intercostal · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE MID ACC COMPT INTERCOSTAL BETWEEN STA 660 - 680 AT L25L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.SDR RRXA003220Panel · delaminatedDURING A MAINTENANCE VISIT FOUND DELAMINATION TO THE WING T/E PANEL BETWEEN STA XRS 98 & 139, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.SDR RRXA003219Panel · delaminatedDURING A MAINTENANCE VISIT FOUND DELAMINATION TO THE T/E LWR PANEL AT STA XRS 219, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.SDR RRXA003218Panel · delaminatedDURING A MAINTENANCE VISIT FOUND DELAMINATION TO THE LWR WING T/E PANEL AT STA XRS 340, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.SDR RRXA003839Gusset · tool damageDURING A MAINTENANCE VISIT FOUND DRILL DAMAGE TO FRAME 120 TOP FWD CORNER OF CARGO DOOR, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-4, 53-2-0, 51-1-20D.SDR UPS00834414Fitting · crackedINSPECTION TYPE:C2, AFT CARGO COMPT FS 1200 FWD ATTACH FITTING CRACKED BETWEEN LONGERON 27 LT AND 28 LT. REMOVED CRACKED FITTING, FAB REPAIR ANGLES IAW DC8 SRM 53-2-0. ALODINED AND PRIMED IAW DC8 SRM 51-1-8, LOCATE NEW FITTING AND REPAIR ANGLES AND DRILL EXISDR UPS00834310Shear Tie · crackedINSPECTION TYPE:C2, CRACK IN SHEAR TIE FS 1360 BETWEEN LONGERON 32 TO 31 RIGHT. REMOVED DAMAGED SECTION OF SHEAR TIE, FABD NEW SHEAR TIE SECTION AND DOUBLER STRAP, ALODINED AND PRIMED, INSTALLED TIE SECTION AND DOUBLER STRAP.SDR UPS00834306Fitting · crackedINSPECTION TYPE:C2, AFT CARGO COMPT FS 1200 FWD ATTACH FITTING CRACKED BETWEEN LONG 27 RT AND 28 LT. REMOVED CRACKED FITTING, FAB REPAIR ANGLES IAW DC8 SRM 53-2-0. ALODINED, PRIMED, LOCATE NEW FITTING AND REPAIR ANGLE, DRILL EXISTING HOLES IAW DC8 SRM 51-1-8SDR UPS00834300Seat Track · wornINSPECTION TYPE:C2, SEAT TRACK E HAS WORN SCALLOPS 2 PLACES AT APPROX FS 160. BLENDED SEAT TRACK AT FS 150. BLENDOUT IS WITHIN LIMITS IAW DC8 SRM 53-2-3 FIG 12. CUT OUT HOLE FOR PLUG AT FS 160 IAW DC8 SRM 53-2-3 FIG 6D. ALODINED AND PRIMED IAW DC8 SRM 51-1SDR UPS00834298Seat Track · damagedINSPECTION TYPE:C2 MAIN CABIN SEAT TRACK AT FS 15080, SEAT TRACK ''A'' HAS 3 DAMAGED SCALLOPS. CUT OUT TRACK IAW DC8 SRM 53 FIG 6D, ALODINED AND PRIMED DRILLED CHANNEL PLUGS TO FIT IAW DC8 SRM 51-1-24, 53-2-3 FIG 6D. INSTALLED IAW DC8 SRM 51-3-0, 53-2-3 FIG SDR RRXA003239Access Panel · delaminatedDURING A MAINTENANCE VISIT FOUND DELAMINATION TO THE LT UPPER AILERON ACCESS PANEL, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.SDR RRXA003238Panel · delaminatedDURING A MAINTENANCE VISIT FOUND DELAMINATION TO THE LWR WING T/E PANEL FWD END BETWEEN STA XRS 340 & 419, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.SDR RRXA003237Panel · delaminatedDURING A MAINTENANCE VISIT FOUND DELAMINATION TO THE LWR WING T/E PANEL O/B OF FLAP ACTUATOR AT STA 419, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
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