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 ABXA9701892Skin · crackedLEFT WING LEADING EDGE AT STA XFS 354 CRACKED AT AFT UPPER END. REPAIRED IAW SRM 51-1-8 AND DWG K O 5056.SDR ABXA9701908Skin · crackedRT WING LEADING EDGE LOWER SURFACE CRACKED AT FASTENER HOLE XFS 572.5. INSTALLED DOUBLER AND FILLER IAW DC8 SRM 57-2-1.SDR ABXA9701861Skin · crackedRT WING LEADING EDGE LOWER SURFACE CRACKED AT FASTENER HOLE XFS 572.5. REPAIRED IAW SRM 57-2-1.SDR IXXA9800019Frame · corrodedDURING ROUTINE DCHECK INSPECTION, CORROSION WAS FOUND ON THE FUSELAGE FRAME SPLICE AT FUSELAGE STATION 270 BETWEEN LONGERONS 24 AND 25 LEFT. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION OF A REPAIR FILLER, AND NESTED REPAIR ANGLESSDR ABXA9701931Angle · crackedLEFT WING LEADING EDGE VERTICAL ANGLE AT THE OUTBOARD CORNER OF THE INBOARD SLAT AT STA XS 250.089 IS CRACKED AT THE LWR END. REPAIRED IAW DC8 SRM 51-1-21 AND 51-3-0.SDR ABXA9701882Angle · crackedLT WING LEADING EDGE VERTICAL ANGLE AT OUTBOARD CORNER OF THE INBOARD SLAT STA YS250.089 IS CRACKED AT LWR END. REPAIRED IAW SRM 51-1-21 AND 51-1-8.SDR IXXA9800025Longeron · corrodedDURING ROUTINE D-CHECK INSPECTION, CORROSION WAS FOUND ON LONGERON ONE AT FUSELAGE STATION 866. REPAIR ACCOMPLISHED CORROSION REMOVAL, FABRICATION AND INSTALLATION OF TWO REPAIR ANGLE DOUBLERS IN ACCORDANCE WITH FAA PER APPROVED DRAWING C88-R24 AND ENGINEERINSDR CKSA97559Fitting · crackedDURING ROUTINE CPCP INSPECTION, FOUND STRINGER END FITTINGS CRACKED S-34R AND S-34L STA1530 AFT SIDE. REMOVED END FITTINGS IAW DC8 SRM 51-1-20. INSTALLED NEW END FITTINGS IAW DC8 SRM 51-1-21. CORROSION TASK CARD NUMBER C5600-0551. NON-ROUTINE TASK CARD NUMSDR IXXA9800022Rib · crackedDURING ROUTINE D-CHECK INSPECTION, FOUND THE RIGHT WING LEADING EDGE RIB CRACKED AT STATION XFS 255. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION OF A REPAIR FILLER AND TWO REPAIR ANGLE DOUBLERS IN ACCORDANCE WITH FAA PER APPROVEDSDR IXXA9800020Spar Cap · crackedDURING ROUTINE D-CHECK INSPECTION, A CRACK WAS FOUND ON THE LOWER SPAR CAP STRAP AT STATION XW 475. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION OF AN INTERNAL REPAIR FILLER AND A REPAIR ANGLE IN ACCORDANCE WITH SERVICE REWORK DRASDR IXXA9800007Plating · corrodedDURING ROUTINE D-CHECK INSPECTION, CORROSION WAS FOUND ON THE LEFT HAND WING UPPER EXTERNAL PLATING BETWEEN STATIONS XRS 693 AND XFS 772.5 BETWEEN STRINGERS 2 AND 6. REPAIR ACCOMPLISHES CORROSION REMOVAL OF AFFECTED AREAS, FABRICATION AND INSTALLATION OF INTESDR ARWA971004Adi · malfunctionedCAPTS ADI INDICATES 6 DEGREE PITCH DOWN AND WHEN SELECTED TO NR 2 GYRO AGREES MOMENTARILY AND THEN INDICATES WORSE. REMOVED AND REPLACED CAPTS ADI AND RERACKED FD COMPUTER, OPS CHECKED NORMAL IAW MM 34-20-0.SDR ARWA971002Receiver · inoperativeDURING FINAL SEGMENT OF CLIMB, F/O'S RMI READS 180 DEGREE OPPOSITE FROM ALL OTHER INSTRUMENTS INCLUDING CAPTS HSI. REMOVED AND REPLACED NR 1 VOR/ILS RECEIVER, OPS CHECKED NORMAL IAW M/M 34-30-1.SDR IXXA9800028Plating · corrodedDURING ROUTINE D-CHECK INSPECTION, CORROSION WAS FOUND ON THE FUSELAGE EXTERNAL PLATING AT FUSELAGE STATION 181 ABOVE LONGERON 31 LEFT. REPAIR ACCOMPLISHED BY REMOVING DAMAGED AREA, FABRICATION AND INSTALLATION OF AN INTERNAL FILLER AND AN EXTERNAL REPAIR DOUSDR IXXA9800018Spar Web · corrodedDURING ROUTINE D-CHECK INSPECTION, CORROSION WAS FOUND ON THE RUDDER FRONT SPAR WEB DOUBLERS AT STATION ZR 163. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED DOUBLERS, FABRICATION AND INSTALLATION OF TWO NEW DOUBLERS IN ACCORDANCE WITH FAA DER APPROVED DRAWING C88-RSDR IXXA980010Doubler · corrodedDURING ROUTINE D CHECK INSPECTION, CORROSION WAS FOUND ON THE NOSE PRESSURE PANEL FINGER DOUBLER BETWEEN FUSELAGE STATION 188 AND 208. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION AN INTERNAL FILLER, ONE EXTERNAL REPAIR DOUBLER ANDSDR IXXA9800009Bulkhead Doubler · corrodedDURING ROUTINE D-CHECK INSPECTION, CORROSION WAS FOUND ON THE PRESSURE BULKHEAD FINGER DOUBLER BETWEEN FUSELAGE STATION 188 AN 208. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION OF AN INTERNAL FILLER, ONE EXTERNAL REPAIR DOUBLER, ASDR ARWA971001Link · wornAFTER T/O NOSE DOOR FLUTTERS, GEAR UP OR GEAR DOWN ATTEMPTED 8 GEAR RETRACTIONS CYCLES; NOSE GEAR DOOR CONTINUE TO FLUTTER, TRY YAWING POSITIVE AND NEGATIVE. FOUND LEFT NOSE GEAR DOOR LINK ASSY WITH PLAY AT INTERNAL MECHANISM R/R LT AND RT LINKS ASSY PER M.MSDR CKSA97545Regulator · leakingAT CRUISE, FOUND CREW SUPPLEMENTAL OXYGEN WAS BEING LOST. UNABLE TO LOCATE PROBLEM. DESCENDED TO 10,000 FT, CONTINUED TO CVG ADVISED OPERATION. FOUND REGULATOR AT BOTTLE ATTACH POINT LOOSE AND LEAKING. SERVICED OXYGEN AND LEAK CHECK GOOD.SDR ARWA970907Spin Brakes · out of adjustAFTER T/O GEAR UP, CLIMBING TO 3.000 STRONG VIBRATION COMING FROM NOSE GEAR, CK'D GEAR UP LATCH, CK'D OK, NO LIGHTS. RECYCLED GEAR TWICE, WITH GEAR DOWN THREE GREEN LTS. STILL STRONG VIBRATION, PERFORMED ABNORMAL CK LIST, VISUALLY CK'D NOSE GEAR DOWN AND LOCSDR TC8A97047Ballast · failedON APPROACH, SMOKE AND ACRID SMELL FROM FIRST OFFICER'S SIDE OF COCKPIT. FOUND BAD BALLAST. ENTERED ON DMI 7553 MEL 33-1, CAT C BALLAST ON ORDER.SDR IXXA9800021Plating · corrodedDURING ROUTINE D-CHECK INSPECTION, CORROSION WAS FOUND ON THE LEFT WING EXTERNAL UPPER PLATING AT STATION XRS 22.5. REPAIR ACCOMPLISHED CORROSION REMOVAL, FABRICATION AND INSTALLATION OF AN EXTERNAL REPAIR DOUBLER IN ACCORDANCE WITH FAA PER APPROVED DRAWING CSDR IXXA9800026Floorbeam · corrodedDURING ROUTINE D-CHECK INSPECTION, CORROSION WAS FOUND ON THE FLOORBEAM AT STATION 1520, BUTT LINE 45.O RIGHT. REPAIR ACCOMPLISHED BY REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION OF A REPAIR FILLER AND REPAIR ANGLE DOUBLERS IN ACCORDANCE WITH FAA PERSDR RRXA97274Floorbeam · corrosionPERFORMED FOLLOW-UP INSPECTION OF FLOORBEAM AT STA 1360 AND BL 58RT, FOUND CORROSION DAMAGE BEYOND LIMITATIONS IAW DC-8 SRM. REMOVED CORROSION DAMAGE, FABRICATED AND INSTALLED REPAIR FILLERS AND ANGLES IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH D19-R01 ANSDR CKSA97527Access Cover · unsecuredVERY LOUD NOISE HEARD COMING FROM NOSE GEAR AREA OF AIRCRAFT. RECYCLED NOSE GEAR, NO DIFFERENCE (INFLT) CONTINUED FLIGHT. LANDING GEAR DOWN AND LOCKED. FOUND RIGHT ACCESS COVER TO TURBO COMPRESSOR FLAPPING OFF ATTACHING SNAPS. RESECURED COVER, INSPECTED VISDR ABXA9701476Switch · corrodedDURING APPROACH, UPON GEAR EXTENSION RT MAIN LANDING GEAR GREEN LIGHT FAILED TO ILLUMINATE. CYCLED GEAR UP AND RED, UNSAFE LIGHT STAYED ON. CYCLED GEAR DOWN AND AFTER 20 SECONDS GREEN (SAFE) LIGHTS ILLUMINATED. CLEANED CORROSION FROM RIGHT MAIN LANDING GEARSDR ABXA9701469Spin Brake · wornAFTER GEAR RETRACTION, NOTED NOISE AND VIBRATION FROM NOSE WHEEL AREA. SIMILAR TO TIRES RUBBING AGAINST SPIN-DOWN BRAKES. RECYCLED GEAR AND NOISE AND VIBRATION STOPPED. REPLACED NOSE WHEEL SPIN-DOWN BRAKE ASSEMBLY IAW DC8 MM 32-00.SDR RRXA97258Centering Assy · malfunctionedAIR TURNBACK, ELEVATOR EXTREMELY STIFF IN FLIGHT AND VERY SLOW TO RESPOND TO INPUTS. REMOVED AND REPLACED ELEVATOR LOAD FEEL/CENTERING ASSEMBLY IAW MM 27-30-4. OPS CHECK NORMAL, NO DEFECTS NOTED.SDR ARWA970901Duct · looseUNABLE TO PRESSURISE ABOVE 1 PSI, 3 TC'S BLEEDS HIGH OUTFLOW HANDLE FULL UP AND LOCKED. DUMPED APPROXIMATELY 6.000 FUEL. FOUND EXHAUST DUCT OFF NR 3 T/C, REINSTALLED DUCT AND PRESSURIZED CABIN TO 4.5 PSI ON ENG RUN.SDR ABXA9701455Controller · overheatedUNIDENTIFIED ODOR IN THE COCKPIT. APPEARS TO BE SOMETHING SMOLDERING UNDER THE CENTER CONSOLE. REPLACED AUTOPILOT CONTROLLER IAW MM 22-10-2.SDR CKSA97478Connector · looseNOSE ON NOSE GEAR LIGHT DID NOT ILLUMINATE. CYCLED ONCE, STILL NO LIGHT. ON SHORT FINAL LIGHT ILLUMINATED. FOUND PIN IN NOSE DOWNLOCK SWITCH C/P PUSHED BACK. RE-SEATED PIN, SYSTEM CHECKED OK PER DC8 MM 32-60-0.SDR RRXA97223Mechanism · lack of lubeAT 0357Z ON TAKEOFF, AIRCRAFT MAIN CARGO DOOR LIGHT CAME ON. WOULD NOT PRESSURIZE PROPERLY WITH ALL T/C'S ON. RETURNED TO KCLT. SERVICED MAIN CARGO DOOR, LUBED DOOR LOCKS AND PINS, PERFORMED OPERATIONS CHECK MANUALLY AND ELECTRICALLY. NO DEFECTS NOTED.SDR TC8A97042Compressor · stalledNR 2 ENGINE COMPRESSOR STALL AT 80 KNOTS, ABORTED. EPR 1.87, EGT 550, N1 111.5.SDR IXXA9700120Fan · failedEN ROUTE, AN ELECTRICAL SMELL WAS SENSED IN THE COCKPIT WITH THE RIGHT RECIRCULATION FAN RUNNING. THE FAN WAS TURNED OFF FOR THE REMAINDER OF THE FLIGHT. MAINTENANCE DEFERRED THE RIGHT RECIRCULATION FAN AND RETURNED THE AIRCRAFT TO SERVICE.SDR TC8A97041Compressor · stalledNR 2 ENGINE COMPRESSOR STALL AT 90 KNOTS, - ABORTED. CHECKED PS4 AND MOISTURE TRAP IAW 73-20-3. CHECKED AIR FILTER ON FUEL CONTROL UNIT, HAD NO CONTAMINANTS. REPLACED O-RING AND INSTALLED FUEL FILTER IAW MM 73-20-2. PERFORMED FLAG CHECK OF PRBC VALVE, GROUSDR IXXA9700119Actuator · failedAFTER TAKEOFF UPON GEAR RETRACTION, THE DOORS LIGHT REMAINED ILLUMININATED AFTER THE UPLATCH CHECK. THE GEAR WAS RECYCLED SEVERAL TIMES WITH NO CHANGE IN WARNING STATUS. THE FLIGHT RETURNED TO HIK. MAINTENANCE REPLACED THE MAIN GEAR CONTROL VALVE, THE HYDRASDR IXXA9800033Plating · crackedDURING ROUTINE D-CHECK INSPECTION, A CRACK WAS FOUND ON THE RIGHT WING UPPER EXTERNAL PLATING AT STATION XRS 20 STRINGER 17. REPAIR ACCOMPLISHED BY REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION OF AN INTERNAL FILLER AND AN EXTERNAL REPAIR DOUBLER IN ASDR TC8A97038Seal · failedKMIA, TRIP NR 00447, UNABLE TO PRESSURIZE THE AIRPLANE. A VERY STRONG NOISE WAS COMING OUT OF THE AFT CARGO DOOR SEAL. AIRCRAFT RETURNED TO KMIA. REPAIRED MAIN CARGO DOOR SEAL LOWER AFT CORNER. CHECKED OK IAW MM 52-2-1, PERFORMED PRESSURIZATION CHECK, OK ISDR IXXA980009Skin · crackedDURING ROUTINE D CHECK INSPECTION, FOUND THE MAIN CARGO DOOR LOCK PIN ACTUATOR MOUNT ATTACHMENT SKIN TORN AND SEPARATED. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION AN INTERNAL FILLER AND AN EXTERNAL REPAIR DOUBLER IN ACCORDANCE SDR IXXA980011Angle · crackedDURING ROUTINE D CHECK INSPECTION, FOUND T ANGLE TO CENTER KEEL WEB CRACKED BETWEEN FUSELAGE STATION 971 AND 980. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION INTERNAL FILLER AND TWO ANGLE DOUBLERS IN ACCORDANCE WITH APPROVED DER SDR IXXA9800010Web · crackedDURING ROUTINE D-CHECK INSPECTION, FOUND A TEE ANGLE CRACKED ON THE CENTER KEEL BEAM WEB BETWEEN FUSELAGE STATION 971 AND 980. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION OF AN INTERNAL FILLER AND TWO ANGLE DOUBLERS IN ACCORDANCESDR IXXA980008Skin · gougedDURING ROUTINE D CHECK INSPECTION, FOUND THE RIGHT HAND OUTBOARD FLAP UPPER PLATING GOUGED AT STATION XF 226. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION AN INTERNAL FILLER AND AN EXTERNAL REPAIR DOUBLER IN ACCORDANCE WITH DER ASDR IXXA9800023Plating · corrodedDURING ROUTINE D-CHECK INSPECTION, CORROSION WAS FOUND ON THE RIGHT WING LEADING EDGE UPPER PLATING AT STATION XFS 291. REPAIR ACCOMPLISHED BY REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION OF INTERNAL FILLERS AND AN EXTERNAL REPAIR DOUBLER IN ACCORDANSDR IXXA9800008Plating · gougedDURING ROUTINE D-CHECK INSPECTION, FOUND THE RIGHT HAND OUTBOARD FLAP UPPER PLATING GOUGED AT STATION XF 226. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION AN INTERNAL FILLER AND AN EXTERNAL REPAIR DOUBLER IN ACCORDANCE WITH FAA DESDR IXXA890007Skin · gougedDURING ROUTINE D-CHECK INSPECTION, FOUND THE LEFT HAND OUTBOARD FLAP UPPER PLATING GOUGED AT STATION XF 415. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION OF AN INTERNAL FILLER AND AN EXTERNAL REPAIR DOUBLER IN ACCORDANCE WITH DER SDR ABXA9701289Pressure Web · corrodedNUMEROUS SHEARED FASTENERS AT PRESSURE PANEL, RT NLG TUNNEL AREA STA 160. REPAIRED IAW SRM 51-1-8 AND ABX REA D853-19564-MR.SDR IXXA980006Skin · crackedDURING ROUTINE D CHECK INSPECTION, A CRACK WAS FOUND ON THE LEFT WING LOWER LEADING EDGE PLATING AT STATION XFS 595. REPAIR ACCOMPLISHED STOP DRILLING ENDS OF CRACK, FABRICATION AND INSTALLATION OF AN EXTERNAL REPAIR DOUBLER IN ACCORDANCE WITH DER APPROVED DRSDR IXXA9800006Plating · crackedDURING ROUTINE D-CHECK INSPECTION, A CRACK WAS FOUND ON THE LEFT WING LOWER LEADING EDGE PLATING AT STATION XFS 595. REPAIR ACCOMPLISHED STOP DRILLING ENDS OF CRACK, FABRICATION AND INSTALLATION OF AN EXTERNAL REPAIR DOUBLER IN ACCORDANCE WITH FAA DER APPROVESDR IXXA980013Skin · corrodedDURING ROUTINE D CHECK INSPECTION, CORROSION WAS FOUND ON THE RIGHT RUDDER EXTERNAL PLATING BETWEEN STATIONS ZR145 TO ZR150. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION OF AN INTERNAL FILLER AND AN EXTERNAL REPAIR DOUBLER IN ACCOSDR IXXA9800012Plating · corrodedDURING ROUTINE D-CHECK INSPECTION, CORROSION WAS FOUND ON THE RUDDER EXTERNAL PLATING BETWEEN STATIONS ZR145 TO ZR150 RIGHT. REPAIR ACCOMPLISHED CORROSION REMOVAL, FABRICATION AND INSTALLATION OF AN INTERNAL FILLER AND AN EXTERNAL REPAIR DOUBLER IN ACCORDANC
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