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.

SDR UPS99828974Ballast · failedINSPECTION TYPE-N/A, SMOKE IN FLT DECK, COMING FROM UNDER F/O'S GLARESHIELD. FOUND GLARESHIELD FLOOD LIGHTS, BALLAST (TRANSFORMER) BAD. REMOVED AND REPLACED BALLAST.Mar 12, 1999 · N866UP · Doug DC873F · Flight Compartment LightingSDR DHL9980733CTr Cowl · crackedAT C-CHECK, NR 1 ENGINE RT CORE COWL REAR UPPER REPAIR CRACKED. CUT OUT DAMGED SECTION OF INNER SKIN, FABRICATED REPAIR PER CFM 56 MM 78-31-10 AND INSTALLED PER DC-8 SRM 51-1-21A, 3 X 2.5.Mar 12, 1999 · N807DH · Doug DC873F · Engine Thrust ReverserSDR DHL9980727CFairing · crackedAT C-CHECK, LT FAIRING PANEL FRAME TO FUSELAGE AT LONGERON APPROX STA 1000 HAS FORMED ANGLE CRACKED AT LOWER SURFACE. STOP DRILLED END OF CRACK, FABRICATED ANGLE REPAIR AND INSTALLED PER SRM 51-21, 1 X 1 X 3.5.Mar 12, 1999 · N807DH · Doug DC873F · Aerodynamic FairingsSDR DHL99806001Regulator · failedALL OXYGEN QUANTITY IND WENT TO ZERO IN FLIGHT. PRESSURE INDICATION AT S/O STATION READ ZERO, BOTTLE PRESSURE READ NORMAL. CHECKED BOTTLE VALVE OPEN. REPLACED OXYGEN BOTTLE REGULATOR, OPS CHECKED NORMAL PER MM 35-10-3.Mar 12, 1999 · N806DH · Doug DC873F · Crew Oxygen SystemSDR UPS99829127Skin · corrodedINSPECTION TYPE:C123 STA 660 BTWN STR 35L TO 36, THE FUSELAGE SKIN IS CORRODED. REPAIRED AREA IAW DH SK 808-237.Mar 11, 1999 · N808UP · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS99829116Floorbeam · corrodedINSPECTION TYPE-C3, FLOORBEAM HAS HEAVY CORROSION ON THE UPPER FLANGE AT FS 1300, LBL 48. REPAIRED FLOORBEAM IAW DH SK808-870.Mar 11, 1999 · N808UP · Doug DC873F · Fuselage Main, Floor BeamSDR UPS99829106Seat Track · corrodedINSPECTION TYPE:C3 MAIN CABIN SEAT TRACK AT BL 0, FS 520 IS CORRODED BEYOND LIMITS. CUT OUT DAMAGED SECTION, FABRICATED AND REPLACED SEAT TRACK FS 450-590 IAW SRM 53-2-3.Mar 11, 1999 · N808UP · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR UPS99829105Floorbeam · corrodedINSPECTION TYPE:C3 FS 1580 AT LBL 48, THE FLOORBEAM UPPER FLANGE IS CORRODED BEYOND LIMITS. REPAIRED FLOORBEAM IAW DH SK808-839.Mar 11, 1999 · N808UP · Doug DC873F · Fuselage Main, Floor BeamSDR UPS99829075Web · corrodedINSPECTION TYPE-C123, STA 879 AT LBL 60, THE PRESSURE WEB IS CORRODED. REPAIRED AREA IAW DK SK808-444.Mar 11, 1999 · N808UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS99829070Fitting · crackedINSPECTION TYPE-C123, FLOORBEAM SUPPORT BACK-UP FITTING AT STA 280 AT STR 27R IS CRACKED. REMOVED, FABRICATED AND REPLACED FITTING IAW DWG 3754025 AND SRM 51-1-20D.Mar 11, 1999 · N808UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS99829068Skin · corrodedINSPECTION TYPE-C123, FUSELAGE SKIN (EXT) AT STA 660 BETWEEN STR 35L-36 IS CORRODED. REPAIRED AREA IAW DH SK 808-237.Mar 11, 1999 · N808UP · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS99829059Floorbeam · corrodedINSPECTION TYPE-C123, STA 1300 AT RBL 36, THE FLOORBEAM HAS HEAVY CORROSION. REPAIRED AREA IAW DH SK 808-576.Mar 11, 1999 · N808UP · Doug DC873F · Fuselage Main, Floor BeamSDR DHL9980761CSkin · damagedAT C CHECK, LEFT ELEVATOR T/E UPPER AREA AT STA XE 226 INTERM REPAIR ON SKIN. REMOVED REPAIR, CUT OUT DAMAGED AREA. FABRICATED REPAIR DOUBLER, PER EO 18R5521081 AND INSTALLED PER EO REBALANCED PER SRM 51-4-4. N/R 428Mar 11, 1999 · N807DH · Doug DC873F · Elevator, Plate/SkinSDR DHL9980758CBulkhead Angle · crackedAT C CHECK, UPPER CARGO COMPT AFT PRESS BULKHEAD RT FWD SIDE CEILING PANEL ATTACH ANGLE CRACKED. REMOVED AND REPLACED ANGLE AND INSTALLED PER SRM 51-1-21, 4.5 BY 1 BY 1. N/R 448Mar 11, 1999 · N807DH · Doug DC873F · Fuselage Main, BulkheadSDR DHL9980757CTr Cowl · brokenAT C CHECK, NR 4 ENG T/R HALF CORE COWL SIDEWALL FWD AREA AT 12 O'CLOCK SKIN DAMAGED. REMOVED AND INSTALLED SERVICABLE T/R HALF PER MM 78-30-0. N/R 520Mar 11, 1999 · N807DH · Doug DC873F · Engine Thrust ReverserSDR DHL9980723CPanel · damagedAT C-CHECK, LEFT WING LOWER L/E STA 515.7 O/B OF NR 1 SLOT SKIN IS BROKEN AWAY ALONG SCREW HOLES. REMOVED AND FABRICATED NEW PANEL PER SRM 51-3-0, 6 X 8.Mar 11, 1999 · N807DH · Doug DC873F · Wing, Plate/SkinSDR UPS99829104Seat Track · corrodedINSPECTION TYPE:C3 MAIN CABIN SEAT TRACK AT FS 1220, LBL 48 IS CORRODED BEYOND LIMITS. CUT OUT DAMAGE, FABRICATED AND REPLACED SEAT TRACK FS 1190-1290 IAW SRM 53-2-3.Mar 10, 1999 · N808UP · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR UPS99829079Angle · corrodedINSPECTION TYPE-C2, AFT PIT FLOORBEAM ATTACH ANGLE AT FS 1320 RBL10 CORRODED ON UPPER SURFACE. CUT OUT DAMAGED AREA AND FABRICATED ATTACH ANGLE AND SPLICE ANGLE IAW REO6375 AND DAC DWG 9887940.Mar 10, 1999 · N810UP · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL9980766CTr Unit · crackedAT C CHECK, NR 3 ENG I/B T/R FAN COWL FWD UPPER SEAL TRACK AT 12 O' CLOCK POSITION IS CRACKED. REMOVED DAMAGED MOUNTING METAL RETAINER SEAL AT NR 3 ENGINE I/B T/R AT 12 O' CLOCK POSITION. FABRICATED SEAL RETAINER 1.5 BY 4.0 AND INSTALLED PER SRM 51-1-21. N/Mar 10, 1999 · N807DH · Doug DC873F · Engine Thrust ReverserSDR DHL9980765CTr Unit · crackedAT C CHECK, NR 2 ENGINE RT T/R HALF TOP BLOCKER DOOR COWL CORE FIXTURE CRACKED. REMOVED DAMAGED FITTING. REMOVED REVERSER FIXED STRUCTURE. REMOVED NR 2 T/R I/B HALF. INSTALLED SERVICABLE T/R UNIT PER MM 78-30-0. N/R 384Mar 10, 1999 · N807DH · Doug DC873F · Engine Thrust ReverserSDR DHL9980760CSkin · corrodedAT C CHEK, LEFT HORIZONTAL STA L/E I/B LOWER AREA AT STA XFS 60 FOUND CORROSION UNDER SKIN SURFACE. CUT OUT DAMAGED SECTION, FABRICATED FILLER AND DOUBLER PER EO 18R5511080 AND INSTALLED PER SRM 51-1-8. N/R 426Mar 10, 1999 · N807DH · Doug DC873F · Horizontal Stabilizer, Plate/SkinSDR DHL9980759CSkin · corrodedAT C CHECK, LEFT HORIZONTAL STAB L/E UPPER AREA AT STA XFS 172.5, FOUND CORROSION UNDER SKIN SURFACE. CUT OUT DAMAGED AREA FABRICATED FILLERS AND REPAIR DOUBLER PER EO 18R5511079. INSTALLED FILLER S AND DOUBLER PER EO FILLER 4 BY 2 AND 1 BY 1, DOUBLER 5.75 Mar 10, 1999 · N807DH · Doug DC873F · Horizontal Stabilizer, Plate/SkinSDR DHL9980737CTr Cowl · crackedAT C-CHECK, NR 3 ENGINE I/B T/R TRANSLATING COWL OUTER ACCESS PANEL AT APPROX 7 O'CLOCK POSITION MOUNTING SURFACE HAS A CRACK. REMOVED DAMAGED MOUNTING SURFACE, FABRICATED NEW AND INSTALLED PER SRM 51-1-8.Mar 10, 1999 · N807DH · Doug DC873F · Engine Thrust ReverserSDR DHL9980736CTr Cowl · crackedAT C-CHECK, NR 2 ENGINE LT T/R HALF CORE COWL I/B SURFACE AFT LOWER AREA CRACKED. STOP DRILLED CRACK AND FABRICATED REPAIR DOUBLER PER SRM 51-1-20, 3 X 4.Mar 10, 1999 · N807DH · Doug DC873F · Engine Thrust ReverserSDR DHL9980735CTr Cowl · crackedAT C-CHECK, NR 2 ENGINE RT T/R HALF CORE COWL INNER SURFACE FWD AREA CRACKED. CUT OUT CRACKED AREA PER CFM 56 MM, FABRICATED DOUBLER AND INSTALLED PER CFM 56 MM 78-31-10, 4 X 3.Mar 10, 1999 · N807DH · Doug DC873F · Engine Thrust ReverserSDR DHL9980734CSkin · crackedAT C-CHECK, FOUND CRACK PROGRESSING THROUGH STEP HOLE AT STA 69.5 WW 5. CUT OUT DAMAGED SECTION OF SKIN AND FABRICATED FILLER 4 X 4' AND DOUBLER 9.75 X 6 PER SRM 57-2-0 AND 57-2-1.Mar 10, 1999 · N807DH · Doug DC873F · Wing, Plate/SkinSDR DHL9980755CSkin · wornAT C CHECK, LT O/B FLAP L/E I/B LOWER SECTION HAS FASTENER HOLES ELONGATED. FABRICATED DOUBLER PER SRM 57-2-0, 3.375 BY 2.5. N/R 267Mar 9, 1999 · N807DH · Doug DC873F · Trailing Edge FlapsSDR DHL9980754CSkin · dentedLEFT O/B FLAP AT T/E LOWER AREA O/B SECTION HAS DENT DAMAGE ON SURFACE STA XW 456.5. REMOVED DAMAGED SECTION. FABRICATED NEW SECTION AND INSTALLED PER SRM 51-1-21, 40 BY 10. N/R 261Mar 9, 1999 · N807DH · Doug DC873F · Trailing Edge FlapsSDR DHL9980742Bracket · brokenAT C-CHECK, LT WING FLAP VANE NR 4 O/B ATTACHING BRACKET AT L/E BROKEN. REMOVED AND REPLACED O/B ATTACH BRACKET PER MM 27-51-14.Mar 9, 1999 · N807DH · Doug DC873F · Trailing Edge FlapsSDR DHL9980741CPanel · crackedAT C-CHECK, LT WING T/E AREA INNER WING FLAP MECHANISM SUPPORT FITTING HAS UPPER PANEL WITH CRACK ON SURFACE. STOP DRILLED END OF CRACK, FABRICATED DOUBLER PER SRM 51-1-8 AND INSTALLED PER 51-1-21, 6.375 X 3.5.Mar 9, 1999 · N807DH · Doug DC873F · Trailing Edge FlapsSDR DHL9980740CAngle · crackedAT C-CHECK, LT O/B FLAP EXHAUST GATE CUTOUT AT I/B SECTION INTERIOR OF T/E HAS CRACK ON FORMED ANGLE. REMOVED DAMAGED T/E SECTION ON EXHAUST GATE CUTOUT, FABRICATED NEW SECTION AND NEW ANGLE AND INSTALLED PER SRM 51-1-20B, 8.5 X 26 AND 55 X 26.Mar 9, 1999 · N807DH · Doug DC873F · Trailing Edge FlapsSDR UPS99829069Seat Track · corrodedINSPECTION TYPE-C123, STA 1340 TO 1360 AT RBL 59, THE SEAT TRACK IS CORRODED OUT OF LIMITS. REPAIRED AREA IAW SRM 53-2-3.Mar 8, 1999 · N808UP · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR UPS99829072Seat Track · corrodedINSPECTION TYPE-C123, STA 150 TO 180 RBL 30, THE SEAT TRACK HAS HEAVY CORROSION. REPAIRED AREA IAW SRM 53-2-3 FIG 8A.Mar 7, 1999 · N808UP · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR UPS99829028Floorbeam · corrodedINSPECTION TYPE-C1, STA 1700 FLOORBEAM IS CORRODED OUT OF LIMITS AT LBL 24. REPAIRED AREA IAW DHC SK 811-528.Mar 7, 1999 · N811UP · Doug DC873F · Fuselage Main, Floor BeamSDR DHL9980769CVane · delaminatedAT C CHECK, LEFT WING NR 4 FLAP VANE IS DELAMINATED. REMOVED AND REPLACED VANE PER MM 27-51-14. N/R 42Mar 7, 1999 · N807DH · Doug DC873F · Trailing Edge FlapsSDR DHL9980768CTab · delaminatedAT C CHECK, LEFT WING AILERON TRIM TAB IS DELAMINATED. REMOVED AND REPLACED AILERON TAB AND RERIGGED PER MM 27-10-0. N/R 41Mar 7, 1999 · N807DH · Doug DC873F · Aileron TabsSDR DHL9980767CVane · delaminatedAT C CHECK, RT FLAP VANE FLAP PANEL NR 3 DELAMINATED. REMOVED VANE AND REPAIRED AND REINSTALLED PER MM 27-50-0..Mar 7, 1999 · N807DH · Doug DC873F · Trailing Edge FlapsSDR DHL9980764CTab · delaminatedAT C CHEK, RT ELEVATOR CONTROL TAB DELAMIANTED. REMOVED ELEVATOR TAB AND OVERHAULED AND INSTALLED PER MM 27-30-00. N/R 39Mar 7, 1999 · N807DH · Doug DC873F · Elevator, Tab StructureSDR DHL9980730CPanel · delaminatedAT C-CHECK, LT WING LOWER ACCESS PANEL NR 525 IS DELAMINATED. REMOVED PANEL AND REPAIRED PER SRM 51-3-0.Mar 7, 1999 · N807DH · Doug DC873F · Wing, Plate/SkinSDR DHL9980729CSkin · delaminatedAT C-CHECK, RT WING LOWER ACCESS PANEL NR 525 IS DELAMINATED. REMOVED AND REPAIRED PANEL, REINSTALLED PER SRM 51-3-0.Mar 7, 1999 · N807DH · Doug DC873F · Wing, Plate/SkinSDR DHL9980728CPanel · delaminatedAT C-CHECK, LT WING LOWER SURFACE T/E HINGED PANEL 710 DELAMINATED. REPAIRED AREA PER SRM 51-3-0.Mar 7, 1999 · N807DH · Doug DC873F · Wing, Plate/SkinSDR UPS99829131Skin · crackedINSPECTION TYPE:C123 FUSELAGE EXTERIOR SKIN AT STA 1748 STR 16L IS CRACKED. REPAIRED AREA IAW SRM 53-2-1 FIG 7.Mar 6, 1999 · N808UP · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS99829128Seat Track · corrodedINSPECTION TYPE:C123 SEAT TRACK BTWN STA 1660-1680 RBL 59 HAS HEAVY CORROSION. REPAIRED AREA IAW SRM 53-2-3.Mar 6, 1999 · N808UP · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR UPS99829125Skin · crackedINSPECTION TYPE:C3 FUSELAGE SKIN IS CRACKED AT FS 1746, LONGERON 16R. CUT OUT DAMAGED AREA, AND REPAIRED IAW SRM 53-2-1 FIG 7.Mar 6, 1999 · N808UP · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS99829101Seat Track · corrodedINSPECTION TYPE:C3 SEAT TRACK AT FS 1440, LBL 44 IS CORRODED BEYOND LIMITS. CUT OUT DAMAGED SECTION, FABIRCATED, AND INSTALLED SEAT TRACK IAW EO DC8-5320-5167C AND SRM 53-2-3 FIG. 8A.Mar 5, 1999 · N808UP · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR UPS99829061Fitting · crackedINSPECTION TYPE-C123, STA 1040 TO 1060 AT STR 35R, THE STR SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3750545 AND SRM 51-1-20D.Mar 5, 1999 · N808UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS99829030Floorbeam · corrodedINSPECTION TYPE-C1, STA 1700 AT RBL 24, THE FLOORBEAM FLANGE HAS HEAVY CORROSION. REPAIRED AREA IAW DHC SK 811-080.Mar 5, 1999 · N811UP · Doug DC873F · Fuselage Main, Floor BeamSDR RRXA99132Net · out of positionUNABLE TO PRESSURIZE AIRCRAFT AT 14,000 FEET AIRCRAFT CABIN CLIMBING AT 1100 FEET PER MINUTE BOTH PAX MAX FLOW AND MAX TEMP. DUMPED 18,000 LBS OF FUEL AND RETURNED TO KDAY. FOUND CARGO NET STRAP/BUCKLE ASSY HANGING FROM ACFT WITH DOOR CLOSED CAUSING GAP BETWMar 5, 1999 · N831AL · Doug DC873F · Cargo CompartmentsSDR RRXA99130Manifold · failedCLIMBING THROUGH FL350, NR 1 EGT GAUGE INTERMITTENTLY AND RAPIDLY OSCILLATED SEVERAL TIMES PLUS/MINUS 400 DEG FROM APPROXIMATELY 760DEG AVERAGE. THIS RESULTED IN A PRECAUTIONARY SHUTDOWN OF THE NR 1 ENGINE. AFTER SHUTDOWN, INTERMITTENTLY WENT FULL SCALE DEFLMar 4, 1999 · N961R · Doug DC873F · Engine Temperature Indicating SystemSDR UPS99829117Support · corrodedINSPECTION TYPE:C3 FLOORBEAM SUPPORT AT FS 1220 IS CORRODED OUT OF LIMITS. REMOVED, FABRICATED, AND REPLACED SUPPORT IAW DWG 9754002 AND SRM 51-1-20D.Mar 3, 1999 · N808UP · Doug DC873F · Fuselage Miscellaneous Structure
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