Douglas DC-8-73F

Service difficulty reports · 15,471

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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"

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SDR UPS06846076Spar Cap · crackedINSPECTION TYPE:C1 RT W/W FWD BULKHEAD STA 857 PRESSURE WEB LOWER ATTACH ANGLE CRACKED FROM RBL 24-33. REMOVED PRESS PANEL AND CUT OUT CRACKED AREA IAW SRM 51-1-21, AND 51-1-20D. FABRICATED AND INSTALLED -15 SPAR SECTION, -3, -5, AND -15 FILLERS, AND -14 STRJan 6, 2006 · N852UP · Doug DC873F · Fuselage Main, StructureSDR UPS06845974Fitting · crackedINSPECTION TYPE:C1 MAIN DECK STA 702 L13R SPLICE FITTING IS CRACKED ON O/B SIDE. REMOVED CRACKED FITTING IAW SRM 51-1-20C, FABRICATED AND INSTALLED SPLICE FITTING IAW DWG 3779978, AND SRM 51-1-8, AND 51-1-20D AT STA 702 L13RJan 6, 2006 · N852UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS06846113Fitting · crackedINSPECTION TYPE:C1 BATHTUB FITTING CRACKED IN C-PIT STA 1160 BETWEEN L35R AND L36. REMOVED FITTING, FABRICATED REPAIR ANGLES AND INSTALLED IAW SRM 53-02-00, 51-1-20D.Jan 5, 2006 · N852UP · Doug DC873F · Fuselage Main, Attach FittingsSDR UPS06846108Fitting · crackedINSPECTION TYPE:C1 CRACKED LATCH BACKUP FITTING IN AFT CARGO COMP TORQUE BOX STA 1185 OF DOOR CUTOUT AT FWD FASTENER OF 3RD LATCH. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D, 51-3-00.Jan 5, 2006 · N852UP · Doug DC873F · Fuselage Main, Attach FittingsSDR UPS06846077Fitting · crackedINSPECTION TYPE:C1 CRACKED BATHTUB FITTING IN AFT CARGO COMPT TORQUE BOX JUST I/B OF DOOR CUTOUT AT STA 1168. REMOVED AND REPLACED BATHTUB FITTING AT STA 1168 IAW SRM 51-1-21, 51-1-20D, AND SRM 51-03-02-0.Jan 5, 2006 · N852UP · Doug DC873F · Fuselage Main, Attach FittingsSDR UPS06845976Longeron · crackedINSPECTION TYPE:C1 LONG 10L IS CRACKED ON LWR SIDE AT CANTED WEB STA 1720 AT LWR NUT. CUT OUT DAMAGED AREA IAW SRM 53-2-2 FIG 11 FABRICATED AND INSTALLED REPAIR ANGLE AND FILLER AT STA 1720 L10L IAW SRM 53-2-2 FIG 11, SRM 51-1-8 AND SRM 51-1-20D.Jan 5, 2006 · N852UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS06845975Fitting · crackedINSPECTION TYPE:C1 CRACKED BATHTUB FITTING IN AFT CARGO TORQUE BOX STA 1195 FWD SIDE ACCESS HOLE I/B OF CENTER DOOR LATCH. REMOVED AND REPLACED BATHTUB FITTING AT STA 1195 L34R IAW SRM 51-3-2, 51-1-8 AND SRM 51-1-20D.Jan 5, 2006 · N852UP · Doug DC873F · Fuselage Main, Attach FittingsSDR UPS06846124Frame · corrodedINSPECTION TYPE:C1 CORROSION ON AFT CARGO COMP FRAME UPPER SURFACE STA 1060 BETWEEN LONGERON 28L AND 29L. FOUND CORROSION OUT OF LIMITS IAW SRM 53-2-0 FIG 1F, CUT OUT DAMAGED AREA IAW SRM 53-2-0 FIG 2. FABRICATED AND INSTALLED 2EA REPAIR ANGLES, LOCATED AND Jan 4, 2006 · N852UP · Doug DC873F · Fuselage Main, FrameSDR UPS06846115Frame · corrodedINSPECTION TYPE:C1 (EXFOLIATION) CORROSION ON AFT CARGO FRAME AROUND FASTENER HOLE STA 1060 ABOVE L30R. REMOVED DAMAGED AREA. FABRICATED SPLICES AND INSTALLED REPLACEMENT FRAME AND SPLICES IAW SRM 53-2-0 FIG 2, 51-1-20D AND 51-1-21.Jan 4, 2006 · N852UP · Doug DC873F · Fuselage Main, FrameSDR UPS06846112Fitting · crackedINSPECTION TYPE:C1 CRACKED FITTING IN AFT CARGO COMP BILGE STA 985 JUST O/B OF LONGERON 34R UNDER FWD END OF CARGO TRACK. REMOVED, FABRICATED AND INSTALLED FITTING, AT STA 985 L34R IAW SRM 51-1-20D AND SAA EA 008-5310-01-A0016.Jan 4, 2006 · N852UP · Doug DC873F · Fuselage Main, Attach FittingsSDR UPS06846110Skin · damagedINSPECTION TYPE:C1 LT UPPER AFT I/B SURFACE OF HORIZONTAL STAB HAS 3 CREASES. REMOVED, FABRICATED AND INSTALLED HORIZONTAL STAB SKIN PANELS 2 IAW DWG 5651747, SRM 51-1-21.Jan 4, 2006 · N852UP · Doug DC873F · Horizontal Stabilizer, Plate/SkinSDR UPS06846107Shear Tie · crackedINSPECTION TYPE:C1 CRACK ON SHEAR TIE FITTING IN AFT CARGO COMP AFT OF STA 1160 FRAME INSIDE POCKET BETWEEN L34R-L35R. REMOVED AND REPLACED SHEAR TIE FITTING IAW SRM 53-2-0 FIG 2D AND 51-1-20D.Jan 4, 2006 · N852UP · Doug DC873F · Fuselage Internal Mounting StructureSDR UPS06846106Frame · corrodedINSPECTION TYPE:C1 CORROSION ON AFT CARGO FRAME STA 1060 UPPER SURFACE IN 3 AREAS JUST ABOVE L31L AND L32L AROUND FASTENERS HOLES, ALSO ON LWR SURFACE OF UPPER FLANGE AROUND NUT PLATE ABOVE 32L. REMOVED AND REPLACED UPPER FRAME CAP IAW SRM 51-03-02, 51-1-21 AJan 4, 2006 · N852UP · Doug DC873F · Fuselage Main, FrameSDR UPS06845973Skin · crackedINSPECTION TYPE:C1 RT STA 1726 AT L17R, HAIRLINE CRACK IN THE SKIN AFT OF THE RIVET. CUT OUT DAMAGED AREA IAW SRM 53-02-01-0 FIG 007 FABRICATED AND INSTALLED FILLER, FINGER DOUBLER, AND REPAIR DOUBLER IAW SRM 53-02-01-0 FIG 007, 53-05.01-0 FIG 001, AND SRM 51Jan 2, 2006 · N852UP · Doug DC873F · Fuselage Main, Plate/SkinSDR DHL2005809005Handle · unsecureMASTER WARNING LIGHT CAME ON DURING TAKEOFF ROLL. FOUND "B" PIT HANDLE NOT STOWED, PER M/M 52-31-1, OPS CHECK GOOD.Dec 23, 2005 · N809DH · Doug DC873F · Cargo/Baggage DoorsSDR DHL2005805006O-Ring · leakingNR 1 ENGINE AT IDLE WHILE STARTING NR 4 ENGINE NR 1 ENGINE FLAMED OUT NORMAL INDICATIONS, REPEAT WRITE UP 12/15. PERFORMED DECAY CHECK ON NR 1 ENG FUEL FEED SUPPLY SYSTEM. NR 1 ENG FEED FAILED CHECK. REMOVED AND REPLACED O-RINGS ON FEED LINE BOOST PUMP TO FDec 20, 2005 · N805DH · Doug DC873F · Engine Fuel DistributionSDR UPS05845899Spar · crackedINSPECTION TYPE:SV LT WING REAR SPAR UPPER CAP AFT FLANGE IS CRACKED APPROX. 7".(XW736.5). REMOVED DAMAGE, FABRICATED, AND INSTALLED REPAIR IAW SAA SK 894-928513.Dec 19, 2005 · N894UP · Doug DC873F · Wing SparSDR UPS05845879Light · inoperativeEMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EMERGENCY BATTERY PACK PER MM 33-50-01-2. OPS CHECK GOOD.Dec 18, 2005 · N866UP · Doug DC873F · Emergency LightingSDR UPS05845884Battery · malfunctionedDURING FINAL APPROACH LOW CARGO COMPT FIRE LIGHT CAME ON AS SOON AS PACKS WERE TURNED OFF IT WENT AWAY. PERFORMED LOWER CARGO COMPT SMOKE DETECTION SYS T/S MM 26-18-00-1. REMOVED AND REPLACED BATTERIES ON DETECTORS FA1326, AC3305, AD6652, AD7666 SYS OK LIGHTDec 17, 2005 · N809UP · Doug DC873F · Smoke DetectionSDR DHL2005805005Engine · surgesAFTER ENG START ON NR1 WITH NORMAL INDICATIONS, DURING NR4 ENG STAT NR1 ENG SURGED THEN FAILED. DURING RESTART ATTEMPT NO FUEL FLOW. INSP FUEL FILTER NO CONTAMINATION NOTED. RAN NR1 ENG IAW JRH 11.8 CROSSFEEDING FROM NR2 MAIN TANK OPS NORM. SW BACK TO NR1 MDec 15, 2005 · N805DH · Doug DC873F · Engine (Turbine/Turboprop)SDR UPS05845881Battery Pack · inoperativeEMERGENCY BATTERY PACK NEEDS REPLACING. REPLACED BAT PACK EMERGENCY LIGHT. OPS NORMAL. OK TO CONTINUE.Dec 12, 2005 · N851UP · Doug DC873F · Emergency LightingSDR IXXA0500157OScrew · looseON TAKEOFF FROM KTOL TO KBFI GEAR HANDLE UP GEAR NOT LATCHED LIGHT STAYED ON. LANDING CYCLED DOWN THEN UP LIGHT WENT OUT. MAINTENANCE LUBED GEAR UP LATCHES AND INDICATOR SWITCHES, NO DEFECTS NOTED. MAINTENANCE FOUND A LOOSE SCREW ON RT DOOR UP LATCH PROXIMIDec 9, 2005 · N602AL · Doug DC873F · Landing Gear Position and WarningSDR UPS05845864Battery Pack · activatedEMERGENCY EXIT LIGHTS DIM. REMOVED AND REPLACED BATTERY PACK IAW MM 33-50-01.Dec 7, 2005 · N874UP · Doug DC873F · Emergency LightingSDR UPS05845862Light · inoperativeEMERGENCY LIGHTS DISARM CHECK LIGHT INOP. RELAMPED IAW 33-15-00-2. OPS CK GOOD.Dec 6, 2005 · N874UP · Doug DC873F · Emergency LightingSDR UPS05845853Window · jammedCAPT SLIDING WINDOW W/NOT OPEN. PER IMPACTS A/C STATUS SLIDING WINDOW JAMMED AND OVER CTR MECHANISM IS WORN TO A POINT OF CAUSING JAM PROBLEM. REMOVED AND REPLACED CAPT CLEARVIEW WINDOW ASSY IAW 56-10-03-4. ALTERNATE P/N USED PER EO DC8-5610-23421-A. WINDODec 6, 2005 · N852UP · Doug DC873F · Flight Compartment WindowsSDR DHL2005805004Engine · failedNR 3 ENGINE FAILED DURING TAXI IN. TROUBLESHOT NR 3 ENGINE PER MM 71-00-00. INSPECTED INLET AND EXHAUST PER MM 72-00-00, NO DEFECTS FOUND.Dec 5, 2005 · N805DH · Doug DC873F · Engine (Turbine/Turboprop)SDR DHL2005801015Battery Pack · inoperativeEMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED EMERGENCY BATTERY PACK IAW MM 33-50-1 CHECKED OPERATION OK.Dec 2, 2005 · N801DH · Doug DC873F · Emergency LightingSDR UPS05845849Wire · openN/A RT MAIN LANDING GEAR LIGHT DID NOT ILLUMINATE DURING LANDING. GEAR WAS DOWN. T/S. FOUND WIRE FROM RT GEAR SWITCH TO TERMINAL BLOCK OPEN. REMOVED AND REPLACED WIRE IAW SWP 20-00-00. OPS CK IAW AMM 32-60-00-2 (E) STEPS 1 TO 6. OPS CK OK ALL 3 GREEN OK.Nov 30, 2005 · N851UP · Doug DC873F · Landing Gear System WiringSDR UPS05845844Light · malfunctionedEMERGENCY EXIT LIGHT REMAINED ON IN FLIGHT, BREAKER POPPED, BREAKER RESET LIGHTS OPERATING NORMAL. OPS CK NORMAL ON GROUND PER MM 33-50-00, OK TO CONTINUE SERVICE.Nov 30, 2005 · N819UP · Doug DC873F · Emergency LightingSDR UPS05845845Fire Warning · illuminatedLOWER CARGO FIRE AMBER MX LIGHT CAME ON AFTER 4 HOURS OF FLIGHT (5 AND 11). PERFORMED ADJUSTMENT AND TEST PER DC-8 M/M 26-18-00-5, NO FAULTS FOUND IN MEMORY OR SIGNAL STRENGTH.Nov 29, 2005 · N808UP · Doug DC873F · Fire DetectionSDR UPS05845841Battery Pack · inoperativeEMERGENCY LIGHTS INOP; FAILS TEST BUT BATTERY SEEMS TO BE GOOD. INSTALLED REPAIRED BATTERY PACK IAW 33-50-01-2.Nov 29, 2005 · N852UP · Doug DC873F · Emergency LightingSDR DHL2005806004Connector · faultyDURING CLIMB-OUT, NR 3 ENG FIRE LIGHT AND FIRE WARNING BELL ACTIVATED INTERMITTENTLY THEN CAME ON STEADY. ENG FIRE CHECKLIST WAS ACCOMPLISHED. ENGINE FIRE LIGHT REMAINED ILLUMINATED. LOOP SWITCH WAS CHANGED. FOUND LOOP "B" ON NR 3 ENGINE TO BE FAULTY. DEFNov 28, 2005 · N806DH · Doug DC873F · Fire DetectionSDR DHL2005806003Switch · malfunctionedDURING CLIMB-OUT, NR 3 ENG FIRE LIGHT AND FIRE WARNING BELL ACTIVATED INTERMITTENTLY THEN CAME ON STEADY. ENG FIRE CHECKLIST WAS ACCOMPLISHED. ENGINE FIRE LIGHT REMAINED ILLUMINATED. LOOP SWITCH WAS CHANGED. FOUND LOOP "B" ON NR 3 ENGINE TO BE FAULTY. DEFNov 28, 2005 · N806DH · Doug DC873F · Fire DetectionSDR IXXA0500119OLink Rod · broken3 HOURS INTO FLIGHT, A POP WAS HEARD, FOLLOWED BY AIR NOISE AND VIBRATION FROM NOSE GEAR AREA. CREW RETURNED AIRCRAFT TO DEPARTURE AIRPORT AND LANDED WITH OUT INCIDENT. INSPECTION IS ON GOING. WHEN INFORMATION IS AVAILABLE IT WILL BE PROVIDED. UPON INSPECTINov 27, 2005 · N603AL · Doug DC873F · Landing Gear DoorsSDR IXXA0500116OPin · installedAFTER DEPARTURE FROM EDFH, NLG DID NOT RETRACT. FROM NGL INSPECTION WINDOW FOUND GROUND PIN STILL IN GEAR. RETURNED AIRCRAFT TO EDFH AND CREW LANDED WITHOUT INCIDENT. FOUND GROUND HANDLERS NOSE GEAR PIN INSTALLED. THE HANDLERS NOSE GEAR PIN WAS REMOVED, PENov 13, 2005 · N602AL · Doug DC873F · Landing Gear SystemSDR UPS05845753Skin · damagedFOUND PIT 31 DOOR HAS "CREASE" AT 2 O'CLOCK POSITION. COMPLIED WITH HFEC INSP OF AREA. NO CRACKS DETECTED DEFERRED PER EO DC8-5230-23256-A (D313697). COLD WORKED SKIN IAW DC8 SRM 51-01-04. VERIFIED NO CRACKS EXIST INTERNALLY AND EXTERNALLY. DAMAGE NO FALLS Nov 10, 2005 · N801UP · Doug DC873F · Cargo/Baggage DoorsSDR DHL2005805003Regulator Valve · malfunctionedON TAKEOFF NR 2 ENGINE OVERPRESS LIGHT ILLUMINATED. REJECTED T/O A/C WEIGHT 252000 IAS 20KTS OAT 13C PA 1000FT. DEFFERRED NR 2 HIGH PRESS 9TH STAGE REG & SO VALVE IAW MEL 36-1-5 SPEC PROC C/W NR 2 HS PRESS 9TH STAGE REG & SO CLOSED. DMI NR 23103 PLACARDS INSNov 4, 2005 · N805DH · Doug DC873F · Pneumatic Distribution SystemSDR UPS05845793Door Frame · crackedINSPECTION TYPE:C1 D-PIT TORQUE BOX FRAME AT L28R FS 1400 CRACKED WHERE LATCH MECHANISM ATTACHES. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR ANGLE DOUBLER IAW SRM 51-3-0, 53-2-0 FIG 1B, 51-1-21 AND 51-1-20D.Nov 3, 2005 · N813UP · Doug DC873F · Fuselage Main, StructureSDR UPS05845755Pressure Panel · corrodedFOUND LT NOSE TUNNEL, UPPER CEILING PRESSURE PANEL HAS 2 SHEARED RIVETS CRACKS AND BULGING CORROSION AT APPROX STA -32 LBL65. REMOVED EXISTING REPAIR FINGER DOUBLER, FINGER DOUBLER "T" FITTING AND 2 ATTACH FITTINGS. REMOVED CORRODED AREA. FABRICATED AND INSNov 1, 2005 · N813UP · Doug DC873F · Fuselage Main, BulkheadSDR UPS05845687Unknown · corrodedFOUND CORROSION IN LT W/W. AIRCRAFT BEING FERRIED NR 9157 TO SAA FOR REPAIR. CUT OUT CORROSION FROM EXTERNAL SKIN, AND FAB'D AND INSTALLED REPAIR PARTS FOR SKIN REPAIR. ALL WORK PERFORMED IAW SAA SK 840-727258 & UPS EO DC8-53-20523.Oct 27, 2005 · N840UP · Doug DC873F · Fuselage Structure (General)SDR UPS05845710Rib · crackedFOUND LT HORIZ STAB I/B L/E STA 141.250 RIB HAS CRACK ON LWR FLANGE ANGLE. STOP DRILLED CRACK, FABBED, AND INSTALLED REPAIR IAW DC-8 SRM 55-2-0 FIG 2 AND 3.Oct 26, 2005 · N813UP · Doug DC873F · Horizontal Stabilizer, Spar/RibSDR UPS05845709Rib · crackedFOUND LT HORIZONTAL STAB IB L/E STA XFS 47.5 RIB HAS 1/2" CRACK ON LOWER FLANGE ANGLE. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 55-2- 0 FIG 2 AND 3.Oct 26, 2005 · N813UP · Doug DC873F · Horizontal Stabilizer, Plate/SkinSDR UPS05845766Skin · corrodedINSPECTION TYPE:CI 2AE POPPED RIVET HEADS AT I/B LOWER SKIN OF RT ELEVATOR AND OBVIOUS INTERNAL CORROSION. REMOVED AND REPLACED SKIN IAW SRM 55-2-1 PAGE 23 & 24, 51-01-22, 55-2-1 FIG 8, 51-1-21, 51-1-21D AND 51-3-0.Oct 25, 2005 · N813UP · Doug DC873F · Elevator, Plate/SkinSDR UPS05845754Fitting · corrodedFOUND SEVERE CORROSION ON SPLICE FITTING AND AROUND FASTENERS AT BS 1570, RBL 20 AS MARKED. REMOVED AND REPLACED FITTING IAW SRM 51-3-0 AND 51-3-2.Oct 24, 2005 · N813UP · Doug DC873F · Fuselage Main, Attach FittingsSDR IXXA05SMN265SFitting · crackedDURING ROUTINE C CHECK INSPECTION, RT FLAP SUPPORT FITTING CRACKED AT STA. XW 410.000. REMOVED AND REPLACED RT FLAP LINK SUPPORT AT STA XW 410.000 IAW DC8 MM 27-51-12 PAGES 201-204. REFER TO N/R FOR OPS CHECK.Oct 24, 2005 · N829BX · Doug DC873F · Wing, Attach FittingsSDR UPS05845795Frame · crackedINSPECTION TYPE:C1 FUSELAGE FRAME IS CRACKED 2" LONG AT F/S 240 L36. CRACK IS IN RADIUS OF UPPER FLANGE. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR SPLICE, ANGLE AND SHEAR TIE CLIP IAW SRM 53-02-00-0, 51-3-2, 51-1-21, 53-4-1 AND 51-1-20D.Oct 23, 2005 · N813UP · Doug DC873F · Fuselage Main, FrameSDR UPS05845772Fitting · crackedINSPECTION TYPE:C1 A PIT DOOR FRAME FWD SPIDER IS CRACKED STA 280 L27R. REMOVED AND REPLACED SPIDER FITTING IAW SRM 51-1-20D, 51-1-21.Oct 23, 2005 · N813UP · Doug DC873F · Cargo/Baggage DoorsSDR UPS05845770Fitting · crackedINSPECTION TYPE:C1 A PIT A/C DOOR FRAME AFT SPIDER FITTING IS CRACKED L27R. REMOVED, FABRICATED AND INSTALLED SPIDER FITTING IAW 51-1-20D, 51-3-0, DWG 3754025.Oct 23, 2005 · N813UP · Doug DC873F · Cargo/Baggage DoorsSDR DHL2005806002Wire · damagedAFTER TAKEOFF DOORS NOT LATCH LIGHT ILLUMINATED AND REMAINED ON UPLATCH CHECK, GEAR NOT LATCHED LIGHT LIGHT ILLUMINATED AND NOSE WHEELGEAR EXTENDED LEFT MAIN GEAR ALTERNATE LIGHT ILLUMINATED INTERMITTENT. LUBRICATED NOSE GEAR UPLATCH REPAIRED WIRE AT MAIN GEAOct 22, 2005 · N806DH · Doug DC873F · Landing Gear System WiringSDR UPS05845797Web · corrodedINSPECTION TYPE:C1 COCKPIT SUBFLOOR STA -93 RBL 30 STATIC TUBE CONNECTING POINT PLATE HAS 4 SHEARED HEAD FASTENERS AND POSSIBLE CORROSION UNDER THE PLATE. REPAIRED IAW SAA SK 813-823093 AND UPS EO DC8-5310-23264-A.Oct 22, 2005 · N813UP · Doug DC873F · Fuselage Miscellaneous Structure
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