Douglas DC-8-72F
Service difficulty reports · 257
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 = 'DC872F' 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 = 'DC872F' 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 IXXA201208300015Skin · corrodedDURING AN INSPECTION OF THE RT WING UPPER SKIN CORROSION WAS FOUND AT XRS 763.000 BETWEEN S-3 AND S-4. REMOVED CORROSION IAW SRM 51-1-8. FOUND OUT OF LIMITS IAW SRM 57-2-0. PERFORMED NDT INSPECTION IAW NDT SPM PART 06-10-01-0001. NO DISCREPANCY FOUND. PERFSDR IXXA20120813021ODuct · contaminatedON ENGINE START, A HOT MUSTY ODOR WAS PRESENT IN THE COCKPIT. AFTER ALL FOUR ENGINES WERE STARTED, THE ODOR EVENTUALLY WENT AWAY. REMOVED, CLEANED AND REINSTALLED AIR DUCTS IAW MM 20-11-0. PERFORMED ENGINES RUN UP AT GROUND IDLE. OPS AND LEAK CHECKED GOOD ISDR DHLA20120519801Skin · corrodedPOSSIBLE CORROSION FOUND AT FS 102 AND LONGERON 36.SDR IXXA20120416010OControl Valve · inoperativeRIGHT AIR CONDITIONING PACK INOPERATIVE. FOUND RT AIR CONDITIONING PACK FLOW CONTROL VALVE WILL NOT OPEN. R & R RT AIR CONDITIONING PACK FLOW CONTROL VALVE IAW MM 21-55-5. OPS AND LEAK CHECK GOOD.SDR IXXA11SMN069SAngle · corrodedDURING ROUTINE C-CHECK INSP FOUND AFT FUSELAGE RT UPPER PART ANGLE CORRODED AT STA 1660.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED ANGLE. FABRICATED NEW ANGLE, SPLICERS, FILLERS, AND TAPERED SHIMS. PERFORMED HEAT TREATMENT. CLEANED, TREASDR IXXA11SMN068SSkin · corrodedDURING ROUTINE C-CHECK INSP, FOUND RT WING OTBD INNER L/E FWD UPPER SKIN CORRODED AT STA XFS 710.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. PERFORMED NDT INSP. NO DISCREPANCY FOUND. FABRICATED REPAIR DOUBLER AND FILLER. CLEANED, TREATESDR IXXA11SMN067SLongeron · corrodedDURING ROUTINE C-CHECK INSP FOUND AFT ACCESSORY COMPARTMENT LONGERON 24 RT CORRODED AT STATION 1380.000 - 1400.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. FABRICATED LANGERON AND SPLICERS. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTSSDR IXXA11SMN066SFloorbeam · corrodedDURING ROUTINE C-CHECK INSP, FOUND AFT ACCESSORY COMPARTMENT FLOORBEAM UPPER FLANGE CORRODED AT STA 1420.000 RBL 52. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. FABRICATED ANGLE AND FILLER. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. ISDR IXXA11SMN065SFrame · corrodedDURING ROUTINE C-CHECK INSP, FOUND AFT ACCESSORY COMPARTMENT FRAME CORRODED AT STA 1440.000, LONGERON 36. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. FABRICATED FRAME SEGMENT AND ANGLES. PERFORMED HEAT TREATMENT. CLEANED, TREATED, PRIMED ARSDR IXXA20110331001Fitting · crackedDURING ROUTINE C-CHECK INSP FOUND AFT ACCESSORY COMPARTMENT AFT BATHTUB FITTING CRACKED AT STA 1530.000 LONGERON 34 RT. REMOVED CRACKED FITTING. INSTALLED NEW FITTING IAW SRM 51-1-20D, SRM 51-1-21 AND SRM 51-3-1.SDR IXXA11SMN0061SFitting · crackedDURING ROUTINE C-CHECK INSP FOUND MAIN CARGO COMPARTMENT RT FITTING AFT LOWER PART CRACKED AT STA 680.000 LONGERON 11 RT. REMOVED CRACKED FITTING. INSTALLED NEW FITTING IAW SRM 51-1-20D AND SRM 51-3-1.SDR IXXA11SMN0060SAngle · corrodedDURING ROUTINE C-CHECK INSP FOUND AFT FUSELAGE RT UPPER PART ANGLE CORRODED AT STA 1633.822. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. FABRICATED ANGLE, SPLICES, FILLERS AND TAPERED SHIMS. PERFORMED HEAT TREATMENT. CLEANED, TREATED, PRSDR IXXA11SMN0059SFitting · corrodedDURING ROUTINE C-CHECK INSP FOUND "D" CARGO DOOR JAMB FITTING CORRODED AT STA 1280.000, LONGERON 34 REMOVED CORRODED FITTING. CLEANED, TREATED AND PRIMED AREA. INSTALLED NEW FITTING IAW SRM 51-1-20D, SRM 51-1-8B, SRM 51-1-20D AND SRM 51-3-1.SDR IXXA11SMN0058SSkin · canningDURING ROUTINE C-CHECK INSP FOUND LT ELEVATOR LOWER SKIN OIL CANNING AT STATION 246.000, XH285.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN AND FINGER DOUBLERS. BONDED PARTS AS NEEDED. CLEANED, TREATED, PRIMESDR IXXA11SMN0057SSkin · canningDURING ROUTINE C-CHECK INSP FOUND LT ELEVATOR LOWER SKIN OIL CANNING AT STA XAR 0.000 - XE 132.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN AND FINGER DOUBLERS. BONDED PARTS AS NEEDED. CLEANED, TREATED, PRIMSDR IXXA11SMN0056SSkin · dentedDURING REOUTINE C-CHECK INSP FOUND LT INBD FLAP UPPER SKIN DENTED AT STA XW 104.000. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN. CLEANED, TREATED, PRIMED AREA AND REPARED PARTS. INSTALLED REPAR PARTS IAW SRM CHAPTER 57-7-1, FIG 1 ITEM "D", SRM 51-1-21, SRM SDR IXXA11SMN049SSupport Fitting · crackedDURING ROUTINE C-CHECK, FOUND RT MLG WHEEL WELL TRAPEZOIDAL SUPPORT FITTING CRACKED AT STA 902.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED WING FUSELAGE FILLETS AND ATTACH PARTS TO GAIN ACCESS TO OTD SPLICE FITTING. PERFORMED STOP HOLE AT CRACSDR IXXA11SMN054SSupport Fitting · corrodedDURING ROUTINE C-CHECK, INSP FOUND LT MLG WHEEL WELL TRAPEZOIDAL SUPPORT FITTING WEB CORRODED AT STA 885.000. REMOVED CORROSION. FOUND OUT OF LIMITS. PERFORMED NDT INSP. NO DISCREPANCY FOUND. FABRICATED REPAIR DOUBLERS. CLEANED, TREATED, PRIMED AREA AND RESDR IXXA11SMN050SFitting · crackedDURING ROUTINE C-CHECK INSP FOUND RT MLG WHEEL WELL FITTING CRACKED AT STATION 879.000, LONGERON 24 RT. REMOVED CRACKED FRAME FITTING. FABRICATED SPLICERS, SHIMS AND DOUBLERS. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FITTING AND REPAIR PSDR IXXA11SMN053SSkin · corrodedDURING ROUTINE C-CHECK INSP, FOUND NR 4 STUB WING L/E EXTERNAL SKIN CORRODED. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO DISCREPANCY FOUND. FABRICATED NEW SKIN, REPAIR DOUBLER AND FILLER. CLEANED, TREATED, PRSDR IXXA11SMN052SSkin · corrodedDURING ROUTINE C-CHECK INSP FOUND LT WING OTBD L/E LOWER EXTERNAL SKIN CORRODED AROUND FASTENERS AT STA XFS 878.750. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSP. NO DISCREPANCSDR IXXA110005OPressure Switch · defectiveDURING CRUISE NR 2 ENGINE OIL PRESSURE LIGHT CAME ON WITH GOOD QTY AND PRESSURE. THE CREW RETARDED THE THROTTLES TO IDLE, THE LIGHT REMAINED ON. THEY SHUTDOWN NR 2 ENGINE IAW ATI COM 3-15-07 AND LANDED IN WSAP WITHOUT FURTHER INCIDENT. MX DEFFERED THE OIL LSDR IXXA100051OController · defectiveDURING CRUISE AT FL360, NR 1 ENGINE FLAMED OUT. THE CREW ACCOMPLISHED QRH FLAME OUT/IN FLIGHT START CHECKLIST. ENGINE WOULD NOT START, THE CREW LANDED WITHOUT FURTHER INCIDENT. MX REPLACED THE MAIN ENGINE CONTROLLER. OPS CHECK GOOD IAW ERH 70.01, MM 73-21-10SDR IXXA100040OSmoke Detector · defectiveDURING CRUISE, LOWER CARGO AFT FIRE WARNING CAME ON, THE CREW DISCHARGED BOTH BOTTLES. THEY LANDED, WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED LOWER CARGO SMOKE DETECTOR, DIVERTER VALVE AND BOTH FIRE EXTINGUISHER BOTTLES. OPERATIONAL CHECK GOOD IAW MM 26.SDR IXXA10SMN014SSkin · crackedDURING ROUTINE C CHECK INSP FOUND LT ELEVATOR UPPER SKIN CRACKED AT STA XE 274.875. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED CRACKED SKIN. FABRICATED NEW SKIN AND FINGER DOUBLERS. BONDED PARTS AS NEEDED WITH HYSOL. CLEANED, TREATED, PRIMED AREA SDR IXXA10SMN013SSupport Fitting · crackedDURING ROUTINE C CHECK INSP FOUND RT OTBD FLAP OTBD HINGE SUPPORT FITTING CRACKED AT STA XF 339.7332. REMOVED CRACKED FITTING. CLEANED, TREATED, PRIMED AREA. INSTALLED NEW FITTING IAW SB 27-249 REV 1 DATED 07/15/90, DWG 5894377, SB 27-249, SRM 51-1-21, SRM 51-SDR IXXA10SMN012SSkin · dentedDURING ROUTINE C CHECK INSP, FOUND RT HORIZONTAL STABILIZER OTBD L/E HAS DENTS AT STATION XFS 216.250 AND XFS 222.500. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INS. NO CRACKS OR CORROSION NOTSDR IXXA10SMN011SSkin · corrodedDURING ROUTINE C CHECK INSP FOUND RT WING INBD L/E SLANT PANEL UPPER SKIN CORRODED AT STA XFS 70.000 - 160.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED CORROSION. FOUND OUT OF LIMITS. FABRICATED NEW SKIN, INTERNAL AND EXTERNAL DOUBLERS. CLEANESDR IXXA10SMN009SSkin · wornDURING ROUTINE C CHECK INSP FOUND LT INBD FLAP UPPER SKIN WORN AT STA XW 106.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN, INTERNAL AND EXTERNAL DOUBLERS. BONDED PARTS AS NEEDED WITH HYSOL. CLEANED, TREATED, PRSDR IXXA10SMN008SSkin · dentedDURING ROUTINE C CHECK INSP FOUND LT OTBD FLAP LOWER SKIN DENTED AT STA XF 104.000-115.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN, INTERNAL AND EXTERNAL DOUBLERS. BONDED PARTS AS NEEDED WITH HYSOL. CLEANED, TRSDR IXXA10SMN007SSkin · dentedDURING ROUTINE C CHECK INSP, FOUND LT OTBD FLAP LOWER SKIN DENTED AT STA XF 169.000-213.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN, INTERNAL AND EXTERNAL DOUBLERS. BONDED PARTS AS NEEDED WITH HYSOL. CLEANED, TSDR IXXA10SMN005SSkin · dentedDURING ROUTINE C CHECK INSP FOUND LT OTBD FLAP T/E LOWER SKIN HAS SEVERAL DENTS AT STA XF 380.000-404.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN, INTERNAL AND EXTERNAL DOUBLERS. BONDED PARTS AS NEEDED WITH HYSSDR IXXA10SMN004SSkin · crackedDURING ROUTINE C CHECK INSP FOUND LT INBD AILERON LOWER SKIN CRACKED AT STA XA 502.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED CRACKED SKIN. FABRICATED NEW SKIN. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. PERFORMED LT INBD AILERON BALANCE.SDR IXXA10SMN002SSkin · crackedDURING ROUTINE C CHECK INSP, FOUND VERTICAL STABILIZER L/E SKIN CRACKED AT STA ZFS 179.750. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA, PERFORMED EDDY CURRENT INSP. NO DISCREPANCY FOUND. FABRICATED INTERNAL, EXTERNAL DOUBLERS AND FILLESDR IXXA090080OContact · dirtyDURING APPROACH FOR LANDING WITH GEAR LOWERED RT MAIN GEAR LIGHT DID NOT ILLUMINATE. CREW CYCLED GEAR SEVERAL TIMES BEFORE GETTING A GEAR DOWN INDICATION, THEY LANDED WITHOUT FURTHER INCIDENT. MX INSPECTED THE RT MLG AND FOUND EXCESSIVE AMOUNT OF DIRT AND LUSDR IXXA090078OLanding Gear · lack of lubeDURING APPROACH, WITH GEAR LOWERED, RT MAIN GEAR LIGHT DID NOT ILLUMINATE. THE CREW CYCLED GEAR SEVERAL TIMES BEFORE GETTING GEAR DOWN INDICATION, THEY LANDED WITHOUT FURTHER INCIDENT. MX INSPECTED ALL SWITCHES ON THE RT MLG AND LUBED GEAR. OPS CHECK GOOD IASDR IXXA090051OConnector · defectiveDURING CRUISE, NR 1 ENGINE FIRE WARNING CAME ON, CREW SHUTDOWN NR 1 ENGINE AND DISCHARGED BOTH FIRE BOTTLES. RETURNED AND LANDED WITHOUT FURTHER INCIDENT. MX INSPECTED AND FOUND LOW RESISTANCE FROM NR 1 FIRE DETECTOR PIN L TO GROUND. MX REPLACED NR 1 FIRE DETESDR IXXA090049OFire Loop · defectiveDURING CRUISE, NR 1 ENGINE FIRE WARNING WENT OFF. THE CREW SHUT DOWN NUMBER ONE ENGINE AND DISCHARGED ONE BOTTLE. THE CREW LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED ALL FIRE LOOPS, NR 1 FIRE CONTROL UNIT AND ONE FIRE BOTTLE. OPERATIONAL CHECK GOSDR IXX2008F00088Actuator · defectiveFLIGHT ATN103/KWRI TO PANC - DURING CRUISE FROM KWRI BOTH PILOT`S AND COPILOT`S YOKE TRIM SWITCHES INOPERATIVE. THE CREW DIVERTED TO KTOL AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED RT LONG TRIM ACTUATOR, OPERATIONAL CHECK GOOD IAW 27-41-10. ACFT WAS SDR IXX2008F00064Skin · damagedDURING ROUTINE C CHECK INSPECTION, FOUND ELONGATED HOLES ON RT WING INBOARD SLOT VANE LEADING EDGE AT STATION XILD 7095.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED PLATING. FABRICATED NEW SKIN. CLEANED, TREATED AND PRIMED AREA AND RSDR IXX2008F00062Skin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER REPAIR RT WING OUTBOARD SLOT VANE LEADING EDGE AT STATION XOLDI 6.224. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK, NO CSDR IXX2008F00035Skin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER REPAIR RT WING OUTBOARD SLOT VANE LEADING EDGE AT STATION XOLDI 6.224. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK, NO CSDR IXX2008F00077Frame · crackedDURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT FRAME CLIP CRACK AT STATION XF 350.000 LONGERON 21. REMOVED CRACKED FRAME CLIP. FABRICATED FRAME CLIP. PERFORMED HEAT TREATMENT. PERFORMED NDT INSPECTION, NO CRACK NO CORROSION. CLEANED, TREASDR IXX2008F00050Fitting · crackedDURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT FRAME CLIP CRACK AT STATION XF 350.000 LONGERON 21. REMOVED CRACKED FRAME CLIP. FABRICATED FRAME CLIP. PERFORMED HEAT TREATMENT. PERFORMED NDT INSPECTION, NO CRACK NO CORROSION. CLEANED, TRSDR IXX2008F00066Door Frame · wornDURING ROUTINE C CHECK INSPECTION, FOUND EXTERIOR FUSELAGE "B" DOOR JAMB WORN AT STATION 503.000 LONGERON 27-28 RT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK, NO CORROSION FOUND. FABRICATED REPSDR IXX2008F00065Skin · crackedDURING ROUTINE C-CHECK INSPECTION, FOUND LT WING CRACKED ON LEADING EDGE UPPER SKIN AT STATION XCW 69.500. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK, NO CORROSION, FABRICATED DOUBLER, FILLER PLUSDR IXX2008F00058Door Frame · wornDURING ROUTINE C CHECK INSPECTION, FOUND EXTERIOR FUSELAGE "B" DOOR JAMB WORN AT STATION 503.000 LONGERON 27-28 RIGHT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK, NO CORROSION FOUND. FABRICATED SDR IXX2008F00029Skin · crackedDURING ROUTINE C CHECK INSPECTION, FOUND LT WING CRACKED ON LEADING EDGE UPPER SKIN AT STATION XCW 69.500. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK, NO CORROSION, FABRICATED DOUBLER, FILLER PLUSDR IXX2008F00080Stiffener · crackedDURING ROUTINE C-CHECK INSPECTION, FOUND RT WING TRAILING EDGE STIFFENER CRACKED AT STATION XW 19.000. REMOVED CRACKED STIFFENER. FABRICATED STIFFENER. PERFORMED NDT INSPECTION. NO CRACK, NO CORROSION FOUND. CLEANED, TREATED AND PRIMED AREA AND STIFFENER.SDR IXX2008F00063Skin · crackedDURING ROUTINE C CHECK INSPECTION, FOUND AFT FUSELAGE EXTERNAL SKIN HAS A CRACK AT STATION 1606.000-1604.000 LONGERON 10RT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. FABRICATED REPAIR DOUBLER, INTERNAL FINGER DOUBLER, AND FILLER.
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