Douglas DC-8-73F
Service difficulty reports · 15,471
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 = 'DC873F' 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 = 'DC873F' 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 DHLA201100501Skin · corrodedRUDDER LT SIDE.- SKIN CORRODED (STA ZR 150.000 - 178.000). CA-PERFORMED MAJOR REPAIR IAW SRM 55-6-1, FIG 1. REMOVED LEVEL II CORROSION IAW SRM 51-1-8, PG 17-18. FOUND OUT OF LIMITS IAW SRM 55-2-0, FIG 6. REMOVED CORRODED PANEL PLATING IAW SRM 55-1-0 PG 1, SSDR DHLA201100046Skin · corrodedRUDDER LT SIDE.- SKIN CORRODED STA ZR 115.000 - 150.000 GALVANIC CORROSION. PERFORMED MAJOR REPAIR IAW SRM 55-6-1 FIG 1. REMOVED LEVEL II CORROSION IAW SRM 51-1-8, PG 17-18. FOUND OUT OF LIMITS IAW SRM 55-2-0, FIG. 6. REMOVED CORRODED PANEL PLATING IAW SRMSDR DHLA201100510Rib · crackedRT LWR SLOT DOOR NR 3 RIB CRACKED. REMOVED CRACKED RIB IAW SRM 51-1-21. CLEANED, TREATED & PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW RIB IAW SRM 51-1-21.SDR DHLA201100507Rib · crackedLT LWR SLOT DOOR, NR 3 RIB CRACKED. REMOVED CRACKED RIB IAW SRM 51-1-21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW RIB IAW SRM 51-1-21. REINSTALLED LT LWR SLOT DOOR IAW MM 27-80-2, PG 203-204.SDR DHLA201100050Rib · crackedRT WING L/E- INBD LWR SLOT DOOR NR 4 RIB CRACKED. REMOVED CRACKED NR 4 DOOR RIB IAW SRM 51-1-21. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED NEW RIB IAW SRM 51-1-21.SDR DHLA201100047Longeron Splice · crackedAFT FUS- L17L SPLICE FITTING CRACKED .2500" STA 1766.000. PERFORMED MAJOR REPAIR IAW SRM 53-1-0, PG 1. REMOVED CRACKED SPLICE FITTING IAW SRM 51-1-21, SRM 51-3-0. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW SPLICE FITTING IAW SRM 51-1-11SDR DHLA201100504Crank Assy · crackedRT OTBD SLOT CRANK CRACKED. REMOVED CRACKED RT OTBD SLOT CRANK IAW MM 27-80-2, PG 201. INSTALLED NEW RT OTBD SLOT CRANK AND REINSTALLED RT OTBD SLOT IAW MM 27-37-6, PG 1-2, MM 27-80-2, PG 201-203, SRM 51-1-21.SDR DHLA201100054Stiffener · crackedRUDDER L/E STIFFENER CRACKED 2" STA ZR 105.000. REMOVED CRACKED STIFFENER IAW SRM 51-1-21, SRM 51-3-0. FABRICATED STIFFENER IAW SRM 55-6-1 PG 4. HEAT TREATED STIFFENER FROM 2024"0" TO 2024T4 IAW SRM 51-1-1 PG 1-13-17. CLEANED, TREATED AND PRIMED AREA & STIFFESDR DHLA201100508Rib · crackedLT WING L/E -FORMER "L" ANGLE CRACKED 4" STA, XFS-23.750. REMOVED CRACKED FORMER IAW SRM 51-3-0 CLEANED TREATED & PRIMED AREA IAW SRM 51-1-8B INSTALLED NEW FORMER IAW SRM 51-3-0, SRM 51-3-1.SDR DHLA201100502Skin · corrodedRT RUDDER EXT SKIN CORRODED, STA ZR 140.750 (GALVANIC CORROSION). PERFORMED MAJOR REPAIR IAW SRM 55-6-1, FIG 1 REMOVED COROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 55-2-0 FIG. 6. REMOVED CORRODED PANEL PLATING IAW SRM 55-1-0 PG 1, SRM 51-1-21SDR DHLA201100053Skin · corrodedRT RUDDER EXT SKIN CORRODED STA ZR 168.656. PERFORMED MAJOR REPAIR IAW SRM 55-6-1, FIG 1. REMOVED LEVEL II CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 55-2-0 FIG 6. REMOVED CORRODED PANEL PLATING IAW SRM 55-1-0, PG 1, SRM 51-1-21. FABRICASDR DHLA201100045Support Angle · crackedRT NOSE WHEEL TUNNEL- SUPPORT ANGLE CRACKED STA -50.000. REMOVED SUPPORT ANGLE IAW SRM 51-3-0. FABRICATED SUPPORT ANGLE (AL2024T3 0.040") IAW SRM 53-2-0 PG 1. CLEANED, TREATED AND PRIMED SUPPORT ANGLE IAW SRM 51-1-8B. INSTALLED SUPPORT ANGLE IAW SRM 51-3-0 WSDR DHLA201100043Doubler · crackedRT INBD FLAP.- FLAP JOINT RIB ANGLE DOUBLER SHOWS (2EA) CRACKS 1" AND .5". REMOVED CRACKED ANGLE DOUBLER IAW SRM 51-1-21. FABRICATED NEW ANGLE DOUBLER (AL2024T3 0.063") IAW SRM 57-2-0 FIG. 2, SHEET 2, SRM 51-9-0 FIG. 68A. CLEANED, TREATED AND PRIMED AREA + ANGSDR DHLA201100506Tab · delaminatedRUDDER TAB DELAMINATED 1", STA ZRT 108.000 LT. CUT OUT DAMAGED AREA IAW SRM 55-2-2 PG 6-4. FABRICATED DOUBLER (AL2024T3 0.016") IAW SRM 55-6-1 PG 8. CLEANED + BONDED DOUBLER IAW SRM 51-1-9 PAR 1, 2, 3, 4. PERFORMED WEIGHT & BALANCE IAW SRM 51-4-7 PG 1-2.SDR DHLA201100503Tab · delaminatedLT ELEV CONTROL TAB DELAMINATED 2" STA XET 35.000. CUT OUT DAMAGED SKIN AREA IAW SRM 55-2-2, PAR 6. FABRICATED DOUBLER (2024T3 0.012") IAW SRM 55-4-0 PG 10. CLEANED AND BONDED DOUBLER IAW SRM 51-1-9, PAR 1-3, TR 51-142. CLEANED AND PAINTED IAW SRM 51-1-8B. PESDR DHLA201100051Skin · delaminatedNR 5 RT SPOILER DELAMINATED 4". CUT OUT DAMAGED AREA IAW SRM 57-2-3, PAR 23. FABRICATED DOUBLER & CORE IAW SRM 57-7-1, PG 15. CLEANED AND BONDED DOUBLER IAW SRM 51-1-9 PAR 1,2,4, TR 51-142. REINSTALLED NR 5 RT SPOILER IAW MM 27-61-1, PG 204-206.SDR DHLA201100042Skin · wornNR 4 ENG INLET NACELLE COWL UPPER SKIN WORN STA, YN 147.000 AT 12 O'CLOCK POS. PERFORMED MAJOR REPAIR IAW SRM 71-5-2, FIG 2, SHEET 1,2,3. REMOVED FASTENERS IAW SRM 51-1-21A. CUT OUT DAMAGED AREA & FABRICATED SKIN & SPLICE IAW SRM 71-5-2 FIG 2, SHEET 1,2,3. HSDR DHLA201100512Fitting · corrodedLEFT MLG WW PRESSURE PANEL AFT SIDE FITTING SHOWS INTERGRANULAR CORROSION AT BS 857.000. REMOVED LEVEL II CORROSION IAW SRM 51-1-8, PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. REMOVED CORRODED FITTING IAW SRM 51-1-21. CLEANED, TREATED AND PRIMED ARSDR DHLA201100052Hinge Fitting · wornVERTICAL STABILIZER REAR SPAR NR 1 HINGE FITTING SHOWS WEAR. STA ZR 103.000. PERFORMED MAJOR REPAIR IAW SRM 55-1-0 PG 1. REMOVED FITTING IAW M 20-16-0 PG 201-207. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. NDT INSPECTED NEW FITTING IAW NDT SPM PART 06-SDR DHLA201100044Frame · wornNR 2 ENG HALF THRUST REVERSER STRUCTURAL FWD FRAME SHOWS EXISTING WEAR DAMAGE STA YN 202.000. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 04-22-11, EVA D878-00401 REV IR DATED 04-06-11. REMOVED FASTENERS SRM 51-1-20D. CUT OUT DAMAGED AREA & FABRICATED NESDR DHLA201100509Skin · delaminatedLT WING T/E LOWER PANEL EXT SKIN DELAMINATED STA XF 339.000- 409.000. R & R LT WING T/E LOWER PANEL IAW SRM 51-3-0, 51-3-1.SDR DHLA201100505Door Frame · misrepairedREPAIR LOCATED ON C4 DOOR FRAME STA 1440.000, L 30R TO L 32R DOES NOT CONFORM , REMOVED REPAIR IAW SRM 51-1-21, SRM 51-1-20D. FABRICATED FILLER, DOUBLER, & TRIPLER IAW DWG ES D85300402-001-D, REV IR DATED 04-13-11. NDT INSPECTED CUT OUT AREA. NO CRACKS SDR DHLA201100511Skin · misrepairedSKIN MISREPAIRED. PERFORMED MAJOR REPAIR IAW FORM 8110-3, DATED 05-04-11, EVA D853-00403, REV IR DATED 04-11-11. REMOVED EXISTING REPAIR IAW SRM 51-1-21, SRM 51-1-20D. CUT OUT DAMAGED AREA, FABRICATED INTERNAL FILLER, EXTERNAL FILLER, INTERNAL DOUBLER, EXTERSDR IXXA110027OMec · defectiveAT THE TOP OF CLIMB OUT AT FLIGHT LEVEL 36,000 FT WHEN THROTTLES WERE PULLED BACK FROM CLIMB POWER TO CRUISE POWER NR 3 ENG MOMENTARILY COMPRESSOR STALLED. ALL OTHER ENGINES PARAMETERS WERE NORMAL AND NR 3 COMPRESSOR STALLED AGAIN 10 MINUTES LATER AT CRUISE WSDR U2RA485AML5571Inu · failedNR 1 INS SCREEN WENT BLANK, NR 1 INU FAILED. NR 2 INS WARNING FLAG FLASHING, NR 2 INU FAILED. INFORMATION REPORTED FROM FLIGHT CREW IS AS FOLLOWS. CREW DECLARED EMERGENCY. ON DESCENT FROM FL 260 TO 6000 WITHIN 75 MILES OF DESTINATION. THE NR 1 INS CDU WENT SDR IXXA110026OSensor · defectiveDURING CRUISE NR 3 ENG COMPRESSOR STALLED. CREW RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. MX REPLACED (CIT) SENSOR. OPS CHECK GOOD IAW CFM MM 73-21-20. ACFT WAS RETURNED TO SERVICE.SDR IXXA110024OWheel · dirtyDURING TAKE OFF ROLL THE CREW HAD NO DIRECTIONAL CONTROL OF AIRCRAFT, THE CREW ABORTED TAKEOFF AND THE AIRCRAFT CAME TO A REST WITH THE NOSE GEAR OFF THE RUNWAY. THE AIRCRAFT WAS TOWED BACK TO BLOCKS. MAINTENANCE ACCOMPLISHED REJECTED TAKEOFF INSPECTION, REPLASDR DHLA201100002Skin · crackedFUSELAGE SKIN CRACKED BETWEEN 2 FASTENERS AT FS 24.5, BETWEEN LONGERONS 31R AND 32R. ACCOMPLISHED FUSELAGE SKIN DOUBLER AND FILLER REPAIR IAW EVA D853-00398, REV IR, DWG NR D85300398-001-D REV IR, AND SRM CHAPTERS 51 & 53. FS 19.811 TO FS 42.5, LONGERON 31R SDR IXXA110020OProximity Switch · defectiveAFTER TAKEOFF, WHEN MLG RETRACTED THE DOOR NOT LATCH LIGHT REMAINED ON. THE CREW CYCLED MLG AND LIGHT REMAINED ON. THEY RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE LT MLG PROXIMITY SWITCH. OPERATIONAL CHECK GOOD IAW MM 32-60-0. AISDR IXXA110021OEngine · flamed outAFTER TAKEOFF, WHEN THROTTLES WERE RETARDED AT FL 37.0 NR 3 ENGINE FLAMED OUT. BEFORE THE CREW COULD ACCOMPLISH FLAME OUT CHECK LIST, THE ENG RELIT WITH NO PROBLEMS THE REMAINDER OF THE FLIGHT, LANDED WITHOUT FURTHER INCIDENT. MX ACCOMPLSHED TREE FAULT 51 WITHSDR IXXA110018OTarget · looseDURING CLIMBOUT, AFTER GEARS WAS RETRACTED THE DOOR NOT LATCH LIGHT REMAINED ON. THE CREW CYCLED THE GEARS, DOOR NOT LATCH LIGHT STILL REMAINED ON, AFTER ACCOMPLISHING UPLATCH CHECK LIGHT WENT OUT. THEY LANDED WITHOUT FURTHER INCIDENT. MX INSPECTED BOTH LT ASDR IXXA110012OSwitch · contaminatedAFTER TAKEOFF, WHEN GEAR WAS RETRACTED THE DOOR NOT LATCH LIGHT REMAINED ON. THE CREW CYCLED THE GEAR THE DOOR NOT LATCH LIGHT STILL REMAINED ON THE ALT GEAR DOOR LIGHT REMAINED OUT. ON DECENT THE LT ALT GEAR DOOR LIGHT MOMENTARILY FLASHED ON THEN OFF. THEY SDR DHLA201100020Longeron Splice · corrodedAFT CARGO COMPT- LONGERON SPLICE FITTING CORRODED STA 1260.000 - 1280.000 L35R EXFOLIATION PERFORMED MAJOR REPAIR IAW SRM 53-4-1 FIG 43A, SHEET 1, 3, 4. REMOVED CORROSION LEVEL II IAW SRM 51-1-8. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. REMOVED CORRODED FISDR DHLA201100015Skin · misrepairedREMOVED L/E SKIN WITH NON STANDARD REPAIRS & EXISTING DOUBLERS IAW SRM 51-1-21. FABRICATED NEW SKIN & DOUBLERS IAW SRM 57-3-3 FIG. 8 ITEM "A", "B". CLEANED, TREATED AND PRIMED AREA & REPAIR PARTS INNER FACE IAW SRM 51-1-8B. INSTALLED REPAIR PARTS IAW SRM 51-1-SDR DHLA201100014Skin · misrepairedREMOVED NON STANDARD REPAIR IAW SRM 51-3-0, SRM 51-1-20D. FABRICATED EXT REPAIR DOUBLER & INTERNAL DOUBLER IAW SRM 57-2-1A FIG. 1. HEAT TREATED INTERNAL DOUBLER IAW SRM 51-1-1 PG 1-13-17, DPS 7.00-1 REV "BL". CLEANED, TREATED AND PRIMED AREA & REPAIR PARTS IAWSDR DHLA201100040Longeron · misrepairedINSPECT EXISTING LONGERON SPLICE REPAIR AT FS 1723.000-1746.000, L26L FOR CONDITION, SECURITY. CONFORMITY WITH SRM 53-2-2. IF REPAIR CONFORMS, NOTE DETAILS ON NON ROUTINE. IF REPAIR DOES NOT CONFORM, R & R UTILIZING APPROVED DATA (REF REPAIR REPORT FI124). PSDR U2RA485ALM5291Pressure Switch · unreliableIN CRUISE NR 4 ENGINE LOW OIL PRESSURE LIGHT ON STEADY, ENGINE OIL PRESSURE INDICATOR 50 PSI . PERFORMED INFLIGHT ENGINE SHUTDOWN. WINDMILLING OIL PRESSURE 10 PSI.SDR DHLA201100029Seat Track · damagedMAIN CARGO COMPT.- NR 2 TRACK LUGS BROKEN (STA 1590.000 - 1650.000) PERFORMED MAJOR REPAIR IAW SRM 53-2-3, FIG 14, SHEET 1, PG 49-50. REMOVED FLOOR PANEL IAW SRM 51-3-0. REMOVED BROKEN TRACK SEGMENT & EXISTING SPLICES IAW SRM 51-3-0. CLEANED, TREATED AND PRIMSDR DHLA201100025Seat Track · damagedMAIN CARGO COMPT.- NR 6 TRACK LUGS WORN STA 180.000 - 210.000. PERFORMED MAJOR REPAIR IAW SRM 53-2-3, FIG 14, SHEET 1-2, PG 49-50. REMOVED DAMAGED TRACK SEGMENT & EXISTING SPLICES IAW SRM 53-1-0 PG 1, SRM 51-3-0. FABRICATED NEW TRACK SEGMENT IAW SRM 53-2-3 FISDR DHLA201100013Seat Track · brokenNR 2 SEAT TRACK LUGS BROKEN STA 1580.000 - 1540.000. PERFORMED MAJOR REPAIR IAW SRM 53-2-3 FIG. 14 SHEET 1,2 PG 49-51. REMOVED DAMAGED TRACK SEGMENT & EXISTING SPLICES IAW SRM 53-1-0 PG 1, SRM 51-3-0. FABRICATED NEW TRACK SEGMENT IAW SRM 53-2-3 PG 35-36, SRM SDR IXXA110007OControl Valve · defectiveDURING CRUISE, DOOR NOT LATCHED, RED LIGHT ON WITH GEAR UP. THE CREW RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. MX REPLACED LT MLG DOOR CONTROL VALVE. OPS CHECK GOOD IAW MM 32-32-7. ACFT WAS RETURNED TO SERVICE.SDR IXXA110006OUnknown · unknownDURING TAKEOFF ROLL, ACFT PULLED HARD LEFT. CREW WAS UNABLE TO MAINTAIN DIRECTIONAL CONTROL WITH FULL RT RUDDER. THEY ABORTED TAKEOFF AND RETURNED TO BLOCKS WITH OUT FURTHER INCIDENT. MX INSPECTED THE NOSE GEAR, WHEELS, BRAKES, NOSE WHEEL STEERING, NOSE STEESDR DHLA201100012Skin · misrepairedREMOVED PLATING WITH EXISTING NON STANDARD REPAIR IAW SRM 57-1-0 PG 1, SRM 51-1-21. FABRICATED NEW PLATING IAW SRM 57-3-3 FIG 8 ITEM "A", SRM 51-1-4. CLEANED, TREATED AND PRIMED AREA & NEW PLATING INNER FACE IAW SRM 51-1-8B. INSTALLED NEW PLATING IAW SRM 51-1-SDR DHLA201100011Skin · misrepairedREMOVED EXISTING REPAIR IAW SRM 51-1-21, SRM 51-1-20D. CUT OUT DAMAGED AREA & FABRICATED FILLER & DOUBLER IAW DWG ES-D85700391-001-D REV IR. VISUALLY INSPECTED CUT OUT AREA & REPAIR PARTS IAW NDT SPM PART 09, NDT SPM PART 06-10-01-001. NO CRACK, NO CORROSION FSDR DHLA201100010Skin · misrepairedREMOVED EXISTING NON STANDARD REPAIR IAW SRM 51-1-20D. FABRICATED REPAIR DOUBLER IAW SRM 53-2-0 FIG. 22A SHEET 2, 6, 12, 13, 14, 15 TR 53-170. NDT INSPECTED REPAIR DOUBLER IAW NDT SPM PART 8, SRM 53-2-0 FIG. 22 SHEET 12 ITEM 23 TR 53-170. NO CRACK FOUND. ENCLOSDR DHLA201100009Skin · misrepairedREMOVED NON STANDARD REPAIR & EXISTING SPLICES IAW SRM 51-1-21, SRM 51-1-20D. FABRICATED REPAIR DOUBLER & 2EA SPLICES IAW SRM 53-2-5 FIG. 15 SHEET 1-2, SRM 53-2-5 FIG. 15 SHEET 3, 4, 5 TR 53-179, SRM 53-4-1 FIG. 17A ITEM "A". HEAT TREATED REPAIR DOUBLER & SPLISDR DHLA201100003Skin · corrodedAFT LWR FUSELAGE SKIN CORRODED, STA 1690.000 L34R (INTERGRANULAR) PERFORMED MAJOR REPAIR IAW SRM 53-2-1 FIG. 7 SHEET 5, 23,24 TR 53-203 DATED 01-21-08. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS (LEVEL II) IAW SRM 53-2-0 PG 2P. CUT OUT CORRSDR DHLA201100037Skin · corrodedAFT CARGO COMPT INTERNAL SKIN CORRODED (STA 1260.000 - 1280.000 L35R) EXFOLIATION. PERFORMED MAJOR REPAIR IAW FORM 8110-3, DATED 02-27-2011, EVA D853-00396 REV DATED 02-10-11, DWG ED-5324 DATED 02-07-11. REMOVED EXISTING REPAIR IAW SRM 51-1-20D. REMOVED CORROSDR DHLA201100036Fitting · crackedRT WING TO FUS FAIRING. FITTING CRACKED 1" STA 920.000, L24R. PERFORMED MAJOR REPAIR IAW FORM 8110-3, DATED 02-28-11, EVA D853-00390 REV IR DATED 02-03-11, DWG ES-D85300390-001-D, REV B, DATED 2-15-11. REMOVED FASTENERS IAW SRM 51-1-20D. CUT OUT DAMAGED ARSDR DHLA201100032Skin · misrepairedR & R EXISTING REPAIR AT FS 1500.000, L21L. UTILIZING APPROVED DATA (REF REPAIR REPORT F087) PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 02-16-11, EVA D853-00392 DATED 02-02-11, SMN DWG ED-5308 DATED 01-22-11, JC EC-02377-001 WO 9960. REMOVED EXISTING REP
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