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 UPS97822667Fitting · corrodedINSPECTION TYPE:D, INTERCOSTAL AT S-27R BETWEEN FS 70-80 IS CORRODED ON UPPER AND LOWER SIDES. REMOVED AND REPLACED STRINGER END FITTING IAW SRM 51-1-21, 51-1-20D (INTERCOSTAL WITHIN LIMITS).Mar 24, 1997 · N818UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS97822647Fitting · crackedINSPECTION TYPE:D, STA 680 STR 11R-END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-21 AND 53-01-0.Mar 24, 1997 · N818UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS97822589Rib · crackedINSPECTION TYPE-D, LT HORZ STAB L/E RIB AT STA FXS 47.5 IS CRACKED. FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM 55-2-0, 51-01-20, AND 51-1-8.Mar 24, 1997 · N818UP · Doug DC873F · Horizontal Stabilizer, Spar/RibSDR UPS97822582Fitting · crackedINSPECTION TYPE-D, AFT INTERCOSTAL SUPPORT FITTING CRACKED BETWEEN STA 822 TO 834 LONG 18L. REMOVED, FABRICATED AND REPLACED FITTING IAW SRM 51-1-20, DAC DWG NR 3779874, AND SRM 53-1-0.Mar 24, 1997 · N818UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS97822563Stringer · corrodedINSPECTION TYPE-D, STRINGER 25R HAS EXFOLIATION CORROSION AT FS 100. CORROSION IS FWD AND AFT OF FRAME. REMOVED, FABRICATED AND INSTALLED REPLACEMENT SECTION OF STRINGER IAW SRM 51-1-21, 53-4-1 AND 51-1-20D.Mar 24, 1997 · N818UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS97822560Seat Track · corrosionINSPECTION TYPE-D, STA 55 RBL 44 THE SEAT TRACK HAS HEAVY CORROSION. REMOVED, FABRICATED AND INSTALLED SECTION OF TRACK FS 50 TO 130 IAW SRM 53-2-3 FIG 6, AND 51-01-20.Mar 24, 1997 · N818UP · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR UPS97822533Fitting · crackedINSPECTION TYPE-D, LONGERON SPLICE FITTING CRACKED AT LONGERON 1 BETWEEN F/S 902-920. REMOVED AND REPLACED FITTING IAW SRM 51-1-20 AND 53-1-0.Mar 24, 1997 · N818UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS97822529Fitting · crackedINSPECTION TYPE: D. AFT INTERCOSTAL SUPPORT FITTING CRACKED AT STA 798 LONGERON 17L. REMOVED AND REPLACED FITTING PER SRM 51-1-21.Mar 24, 1997 · N818UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS97822771Intercostal · crackedINSPECTION TYPE:D, INTERCOSTAL CRACKED ABOVE AND BEHIND FWD ENTRY DOOR BAYONET. REMOVED DAMAGED INTERCOSTAL PER SRM 51-1-21. FABRICATED AND INSTALLED REPLACEMENT INTERCOSTAL PER SRM 53-1-0 AND 51-1-21.Mar 23, 1997 · N818UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS97822566Chord · corrosionINSPECTION TYPE-D, FS 70 CHORD ANGLE BETWEEN STR 30R AND 34R HAS HEAVY CORROSION ON FWD END. REMOVED DAMAGED SECTION OF CHORD, FABRICATED AND INSTALLED REPAIR SECTION IAW SRM 53-2-5 FIG 8C, SRM 51-1-20.Mar 23, 1997 · N818UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS97822595Web · crackedINSPECTION TYPE-D, MAIN CABIN FS 90 LBL 66 WEB MEMBRANE CUSP AREA CRACKED BEYOND LIMITS. TEMPORARY REPAIR INSTALLED. REMOVED EXISTING REPAIR, REMOVED DAMAGE, FABRICATED AND INSTALLED FILLER AND DOUBLER IAW UPS EO DC8-5330-2159-B.Mar 22, 1997 · N818UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS97822591Clip · crackedINSPECTION TYPE-D, INTERCOSTAL CLIP AT FS 1766 LONGERON 6L IS CRACKED. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT PART IAW SRM 51-1-0, 51-1-20, 51-9-0, 51-1-29D, AND 51-1-11.Mar 21, 1997 · N818UP · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA97084Frame · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION ON ANGLE AND POPPED RIVETS, AT Y=70 AND LONGERON 28 RIGHT. CUT AND REMOVED SECTION OF FRAME AT LONGERON 21 RIGHT TO 33 RIGHT, FABRICATED SPLICE DOUBLERS AND EXTERNAL DOUBLER AND SPLICED IN NEW SECTION OF FRAME IAW DMar 20, 1997 · N795FT · Doug DC873F · Fuselage Main, FrameSDR RRXA97082Web · crackedDURING A MAINTENANCE VISIT, FOUND FLOOR WEB CRACKED UNDER SECTION OF FLOOR TRACK, AT Y=640 AND X=-25. REMOVED DAMAGED AREA, FABRICATED REPAIR DOUBLER IAW FAA DER APPROVED COTNEY ENGINEERING SKETCH CO7-R22. TREATED AREA IAW DC-8 SRM 51-1-8 AND INSTALLED REPAIMar 20, 1997 · N795FT · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA97081Web · wornDURING A MAINTENANCE VISIT, FOUND RIGHT EXHAUST GATE INBD WEB AND UPPER ATTACH ANGLE WORN OUT OF LIMITATIONS. REMOVED ATTACH ANGLE AND WORN WEB. FABRICATED NEW WEB AND ATTACH ANGLE REPAIR AND INSTALLED IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH CO7-R23. Mar 20, 1997 · N795FT · Doug DC873F · Wing Miscellaneous StructureSDR RRXA97083Skin · damagedDURING A MAINTENANCE VISIT, FOUND FWD LT ENTRANCE DOOR OUTER SKIN DAMAGED AT UPPER EDGE AFT CORNER. REMOVED EXISTING REPAIR AND DAMAGED AREA, FABRICATED FILLER AND DOUBLER IAW FAA DER APPROVED COTNEY ENGINEERING SKETCH CO7-R21. INSTALLED REPAIR IAW DC-8 SRM Mar 17, 1997 · N795FT · Doug DC873F · Passenger/Crew DoorsSDR RRXA97074Connector · looseON GEAR EXTENSION INTO JFK, LAO AND LAT ANTI-SKID LIGHT ON IN F/W. MAINTENANCE FOUND LOOSE CANNON PLUG ON LEFT LANDING GEAR (ANTI-SKID CONTROL VALVE). CLEANED AND SECURED SAME, OPS CHECK NORMAL.Mar 15, 1997 · N791FT · Doug DC873F · Brake Anti-Skid SectionSDR UPS97822465Longeron · corrodedINSPECTION TYPE-C/CK, AFT ACCESS COMPTD BETWEEN STA 1680 AND 1690, L33R CORRODED. REMOVED AND REPLACED LONGERON SECTION IAW DC8 SRM 53-2-2 FIG 8.Mar 12, 1997 · N804UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR DHL97803003Box Assy · crackedNR 1 ALTERNATE LOW LEVEL LIGHT FLASHING. REPAIRED VENT BOX AND REINSTALLED.Mar 12, 1997 · N803DH · Doug DC873F · Fuel StorageSDR SRAA970305Fire Loop · chafedDURING FLIGHT, FOUND NR 3 ENGINE FIRE WARNING WILL NOT TEST. INSPECTED NR 3 ENGINE FIRE WARNING SYSTEM, FOUND LIGHT CHAFING ON AFT OUTBOARD FIRE LOOP. REPOSITIONED LOOP, SYSTEM OPS CHECKED GOOD IAW MM CH 26.Mar 7, 1997 · N874SJ · Doug DC873F · Fire DetectionSDR UPS97822557Fitting · crackedINSPECTION TYPE C-CK, FRAME TO CUSP FITTING AT STA 380 HAS A CRACK IN LEG, FRAME TO LOWER CUSP TO FLOORBEAM RT SIDE. REMOVED CUSP FITTING, FABBED NEW CUSP FITTING PER REO-02928 AND DAC DWG 3773479. ALODINED AND PRIMED FITTING IAW DC8 SRM 51-1-8. INSTALLED FMar 6, 1997 · N804UP · Doug DC873F · Fuselage Miscellaneous StructureSDR SRAA970304Batteries · dischargedPOST FLIGHT INSPECTION FOUND EMERGENCY EXIT LIGHTS WILL NOT OPERATE FROM BATTERIES. REMOVED AND REPLACED EMERGENCY EXIT LIGHTS BATTERIES, SYSTEM OPS CHECKED GOOD PER MM CH 33.Mar 6, 1997 · N873SJ · Doug DC873F · Emergency LightingSDR UPS97822552Floorbeam · corrodedINSPECTION TYPE C/CK, CABIN FLOORBEAM BOTTOM SIDE OF UPPER CHORD AT SEAT TRACK CRACKED AT FASTENERS. REMOVED FASTENERS, REMOVED CORROSION IAW DC8 SRM 51-1-8. PERFORMED DYE PEN TEST ON FLOORBEAM, FOUND NO CRACKS. ALODINED AND PRIMED IAW DC8 SRM 51 1 8. INSMar 5, 1997 · N804UP · Doug DC873F · Fuselage Main, Floor BeamSDR UPS97822469Floorbeam · corrodedINSPECTION TYPE-C/CK, CABIN FLOORBEAM STA 700 BOTTOM SIDE OF UPPER CHORD AT SEAT TRACK-G CRACK AT FASTENERS. REMOVED FASTENERS, REMOVED CORROSION IAW DC8 SRM 51-1-8. PERFORMED DYE PEN TEST ON FLOORBEAM, FOUND NO CRACKS. ALODINED AND PRIMED AREA IAW DC8 SRMMar 5, 1997 · N804UP · Doug DC873F · Fuselage Main, Floor BeamSDR UPS97822468Floorbeam · corrodedINSPECTION TYPE-C/CK, CABIN FLOORBEAM FS 900 AT SEAT TRACK B-UPPER CHORD CRACKED AND CORRODED AT FASTENERS LOWER SIDE. REMOVED BOLT FROM SEAT TRACK, REMOVED CORROSION AND ALODINED AND PRIMED IAW SRM 51-1-8 AND DREO 08-02908 AND INSTALLED BOLT IAW DC8 SRM D51-3Mar 5, 1997 · N804UP · Doug DC873F · Fuselage Main, Floor BeamSDR UPS97822454Floorbeam · corrodedINSPECTION TYPE-C/CK, CABIN FLOORBEAM FS 900 AT SEAT TRACK C, UPPER CHORD CRACKED AND CORRODED AT FASTENERS LOWER SIDE. REMOVED CORROSION DYE PEN AREA WITH NO CRACK NOTED IAW DC8 SRM D51-1- 8 AND MIL S 271F, ALODINED AND PRIMED IAW DC8 SRM 51-1-8D AND REO O 0Mar 5, 1997 · N804UP · Doug DC873F · Fuselage Main, Floor BeamSDR RRXA97071Compass · bindingDURING CRUISE, NR 2 COMPASS BINDING. FLIGHT TURN BACK TO KJFK.Mar 5, 1997 · N791FT · Doug DC873F · Magnetic CompassSDR UPS97822436Splice · crackedINSPECTION TYPE-C/CK, LONGERON SPLICE CRACKED AT 3 LT JUST FWD OF STA 1060. REMOVED CRACKED FITTING, CLEANED AREA, RECEIVED NEW SPLICE. INSTALLED NEW SPLICE FITTING IAW DC8 51-1-8 AND 51-1-20D.Mar 4, 1997 · N804UP · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL97806001Arrestor · defectiveNR 1 HF WILL NOT CHANNELIZE, TRANSMIT OR RECEIVE. REPLACED LIGHTING ARRESTOR, OPS CHECK GOOD.Mar 4, 1997 · N806DH · Doug DC873F · HF Communications SystemSDR UPS97822558Fitting · corrodedINSPECTION TYPE C-CK, BETWEEN STA 100 AND STA 120 LONG 27R CORRODED AT SKIN AREA. REMOVED CORRODED LONGERON END FITTING, HEAT TREATED FITTING IAW DAC DWG 4649643, TRIMMED, DRILLED NEW FITTING IAW DC8 SRM 51-1-24. ALODINED AND PRIMED IAW DC8 SRM 51-1-8 AND INMar 3, 1997 · N804UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS97822556Fitting · crackedINSPECTION TYPE C-CK, FLOORBEAM EXPANSION JOINT FITTING CRACKED WHERE ATTACHED TO SEAT TRA CK AFT ATTACH BOLT FS 759, RBL 24. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-3-0.Mar 3, 1997 · N804UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS97822555Fitting · crackedINSPECTION TYPE C-CK, FLOORBEAM EXPANSION JOINT FITTING CRACKED, FS 700, LBL 24. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-3-0.Mar 3, 1997 · N804UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS97822554Fitting · crackedINSPECTION TYPE C-CK, FLOORBEAM EXPANSION JOINT FITTING CRACKED, FS 749, LBL 24, FWD SIDE. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-3-0.Mar 3, 1997 · N804UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS97822553Fitting · crackedINSPECTION TYPE-C/CK, FLOORBEAM EXPANSION JOINT FITTING CRACKED FS 717, LBL 24, AFT SIDE. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-3-0.Mar 3, 1997 · N804UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS97822467Vane · elongated holesINSPECTION TYPE-C/CK, MISSING FASTENERS LEFT UPPER LEADING EDGE SLOT OUT BOARD END ABOVE NR 1 PYLON. REMOVED LEFT UPPER LEADING EDGE OUTBOARD SLOT VANE TO FOM. REMOVED DOUBLER AND FILLER, FABRICATED DOUBLER IAW REO 02867 REV A, ALODINED AND PRIMED ALL PARTMar 3, 1997 · N804UP · Doug DC873F · Trailing Edge FlapsSDR UPS97822466Floorbeam · corrodedINSPECTION TYPE-C/CK, FS 857 FLOORBEAM HAS FITTING CORROSION IN AREAS WHERE FLOORBOARDS CONTACT BEAM. BLENDED CORROSION IAW DC8 SRM D51-1-8. REMOVED PULLEY BRACKET, FABRICATED ANGLE AND FILLER IAW REO 02906, ALODINED AND PRIMED REPAIR ANGLE FILLER AND FLOORBMar 3, 1997 · N804UP · Doug DC873F · Fuselage Main, Floor BeamSDR UPS97822435Fitting · corrodedINSPECTION TYPE-C/CK, STA 340 RIGHT SIDE AT CUSP, CORROSION AROUND AND UNDER FRAME ATTACH FITTING. REMOVED WEB CUSP FITTING AND L-ANGLE TO GET ACCESS TO CORROSION. REMOVED CORROSION IAW DC8 SRM 51-1-8, ALODINED AND PRIMED IAW DC8 SRM 51-1-8, INSTALLED L-ANGLMar 3, 1997 · N804UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS97822434Angle · crackedINSPECTION TYPE-C/CK, NR 1 PYLON I/B DRAG ANGLE CRACKED EXTENDING APPROX .25 INCH PAST STOP DRILL HOLE. STOP DRILL END OF CRACK .250 AND POLISH TO 32 MICRO INCH FINISH. VERIFIED AND MARKED END OF CRACK UTILIZING HFEC. STOP DRILLED CRACK AS MARKED BY NOT VERMar 2, 1997 · N804UP · Doug DC873F · Nacelle/Pylon StructureSDR DHL97803001Ins · misalignedNR 2 INS CDU WENT BLANK WHILE INFLIGHT. MODE SWITCH PLACED IN THE ATT REF POSITION. NR 2 INS ALIGNED AND OPS CHECKED GOOD PER MM 34-44-0.Feb 26, 1997 · N803DH · Doug DC873F · Inertial Guidance SystemSDR DHL97803002Bushings · looseWHILE IN CRUISE, ATTEMPTED TO ADJUST POWER ON NR 3 ENGINE. T/L DID NOT MOVE, WHEN IT FINALLY DID, MOVED 1.5 . FELT AS IF DISCONNECTED FROM LINKAGE. NO ENGINE CONTROL AVAILABLE DURING REMAINING PORTION OF FLIGHT. ATTEMPTED TO MOVE T/L SEVERAL TIMES. AFTER Feb 25, 1997 · N803DH · Doug DC873F · Power LeverSDR RRXA97100Plating · corrodedDURING A MAINTENANCE VISIT, FOUND INNER SKIN CORROSION, AT Y=53 AND LONGERON 34R. AWAITING ON ZANTOP AND COTNEY ENGINEERING TO DETERMINE REPAIR PROCEDURE. *S/D* REMOVED DAMAGE SECTIONS FROM Y=47 AND LONGERON 35R. FABRICATED AND INSTALLED DOUBLERS IAW DER AFeb 24, 1997 · N795FT · Doug DC873F · Fuselage Main, Plate/SkinSDR RRXA97099Plating · corrosionDURING A MAINTENANCE VISIT, FOUND SKIN CORROSION ON TOP OF CENTER TANK, AT Y=780 & X=+8. AWAITING ON ZANTOP AND COTNEY ENGINEERING TO DETERMINE REPAIR PROCEDURE. *S/D* REMOVED DAMAGED SECTION, FABRICATED AND INSTALLED SPLICE REPAIR IAW DER APPROVED ENGINEERFeb 24, 1997 · N795FT · Doug DC873F · Wing, Center BoxSDR RRXA97098Skin · crackedDURING A MAINTENANCE VISIT, FOUND OUTER SKIN CRACKED, VERIFIED BY DYE PENE. INSPECTION, AT Y=130, RIGHT SIDE OF MAIN CARGO DOOR UPPER FWD CORNER. AWAITING ON ZANTOP AND COTNEY ENGINEERING TO DETERMINE REPAIR PROCEDURE. *S/D* REPAIRED CARGO DOOR JAMB SKIN BFeb 24, 1997 · N795FT · Doug DC873F · Fuselage Main, Plate/SkinSDR RRXA97097Floorbeam · misdrilledDURING A MAINTENANCE VISIT, FOUND MISDRILLED HOLE IN FLOOR SUPPORT, AT Y=560 AND X=-46. AWAITING ON ZANTOP AND COTNEY ENGINEERING TO DETERMINE REPAIR PROCEDURE. *S/D* REPAIRED FLOORBEAM BY FABRICATING AND INSTALLING 3 REINFORCEMENT ANGLES IAW DER APPROVED CFeb 24, 1997 · N795FT · Doug DC873F · Fuselage Main, Floor BeamSDR RRXA97068Skin · crackedDURING A MAINTENANCE VISIT, FOUND 3 SKIN CRACKS ON LEFT WING, LEADING EDGE AT XFS=422.750, BETWEEN PANELS 520B AND 522A. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW DER APPROVED COTNEY ENGINEERING SKETCH C07-R09.Feb 24, 1997 · N795FT · Doug DC873F · Wing, Plate/SkinSDR RRXA97067Frame · misdrilledDURING A MAINTENANCE, VISIT FOUND MISDRILLED HOLE IN FRAME AT Y=320 AND LONGERON 21 LEFT. REMOVED FASTENERS, CLEANED IAW DAC DC-8 SRM 51-1-21 AND 51-1-20D. FABRICATED AND INSTALLED REPAIR ANGLE AND SHIMS IAW DER APPROVED COTNEY ENGINEERING SKETCH C07-R12.Feb 24, 1997 · N795FT · Doug DC873F · Fuselage Main, FrameSDR RRXA97066Frame · misdrilledDURING A MAINTENANCE VISIT, FOUND MISDRILLED HOLE IN FRAME AT Y=340 AND LONGERON 21 LEFT. REMOVED FASTENERS, CLEANED. FABRICATED AND INSTALLED REPAIR IAW DER APPROVED COTNEY ENGINEERING SKETCH C07-R13 AND DAC DC-8 SRM 51-1-20D.Feb 24, 1997 · N795FT · Doug DC873F · Fuselage Main, FrameSDR RRXA97065Frame · misdrilledDURING A MAINTENANCE VISIT, FOUND MISDRILLED HOLE IN FRAME AT Y=1120 AND LONGERON 21 LEFT. REMOVED FASTENERS, CLEANED, TREATED AREA IAW DAC DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR ANGLE AND FILLER, IAW DER APPROVED COTNEY ENGINEERING SKETCH C07-R06 Feb 24, 1997 · N795FT · Doug DC873F · Fuselage Main, FrameSDR RRXA97064Frame · misdrilledDURING A MAINTENANCE VISIT, FOUND MISDRILLED HOLE IN FRAME AT Y=1400 AND LONGERON 21 LEFT. REMOVED FASTENERS, CLEANED AND TREATED AREA IAW DAC DC-8 SRM 51-1-8. FABRICATED AND INSTALLED ANGLE AND FILLER REPAIR IAW DER APPROVED COTNEY ENGINEERING SKETCH C07-R0Feb 24, 1997 · N795FT · Doug DC873F · Fuselage Main, FrameSDR RRXA97063Frame · misdrilledDURING A MAINTENANCE VISIT, FOUND MISDRILLED HOLE ON FRAME AT Y=1520 AND LONGERON 21 LEFT. REMOVED FASTENERS, CLEANED AND TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DER APPROVED COTNEY ENGINEERING SKETCH C07-R07 AND DAC DC-8 SRM 51Feb 24, 1997 · N795FT · Doug DC873F · Fuselage Main, Frame
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