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 UPS01836240Longeron · crackedINSPECTION TYPE:C2 AFT PIT LONGERON 34L CRACKED FS 1482-1487. REMOVED DAMAGED PART OF LONGERON, INSTALLED NEW PART OF LONGERON AND NEW SPLICE.Jun 29, 2001 · N851UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR RRXA11323Frame · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO FRAME AT STA.55 AND L24R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-20D, 51-1-11, 53-Jun 28, 2001 · N606AL · Doug DC873F · Fuselage Structure (General)SDR UPS01836350Longeron · crackedINSPECTION TYPE:C2 STA 1773 LONG 17R IS CRACKED. REPAIRED LONGERON IAW SRM 53-2-3 FIG 5.Jun 28, 2001 · N807UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR RRXA11379Fitting · crackedDURING A MAINTENANCE VISIT FOUND R/H WING CTR L/E STA XFS 404-400 FITTING CRACKED. *** CORRECTIVE ACTION *** REMOVED AND REPLACED FITTING IAW DWG # 5770409, SRM 51-1-20, 51-1-21 AND 51-1-21AJun 27, 2001 · N873SJ · Doug DC873F · Wing Main, Frame StructureSDR RRXA11378Fitting · crackedDURING A MAINTENANCE VISIT FOUND CPIT L31L SPLICE FITTING CRACKED. *** CORRECTIVE ACTION *** REMOVED AND REPLACED FITTING IAW SRM 51-1-20DJun 27, 2001 · N873SJ · Doug DC873F · Fuselage Main, StructureSDR RRXA11377Frame · crackedDURING A MAINTENANCE VISIT FOUND FRAME STA 55 L24L CRACKED. *** CORRECTIVE ACTION *** REMOVED DAMAGED AREA IAW SRM 53-3-3, FABRICATED AND INSTALLED REPLACEMENT PARTS IAW SRM 53-3-3 FIG 3, 51-1-21 AND 51-1-20D.Jun 27, 2001 · N873SJ · Doug DC873F · Fuselage Main, StructureSDR RRXA010056Pad · failedON DEPARTURE GEAR HANDLE UP NOSE GEAR HAD EXTREME NO ISE AS IF NOSE WHEELS WERE SPINNING AND RUBBING. ALSO HAD EXTREME VIBRATION, GEAR HANDLE PUT BACK DOWN, VIBRATION CONTINUED WITH GEAR DOWN, WHEN ACFT BANKED IN FLT NOSE GEAR HAD LOUD BANG. BOTH GEAR UP INDIJun 27, 2001 · N831AL · Doug DC873F · Landing Gear Brake SystemSDR UPS01836355Spar Cap · crackedINSPECTION TYPE:C2 RIGHT HORIZONTAL STAB UPPER FORMER/CAP IS CRACKED AT XFS 47.5. REMOVED AND REPLACED CAP IAW DWG 5654549 AND SRM 55-1-0, 51-1-20D, 51-1-21, 51-3-0.Jun 27, 2001 · N807UP · Doug DC873F · Horizontal Stabilizer, Spar/RibSDR UPS01836323Doubler · crackedINSPECTION TYPE:C2 RIGHT WING INTERNAL DOUBLER IS CRACKED AT XFS 597.5. REMOVED, FABRICATED AND REPLACED DOUBLER IAW DWG 5769600 AND SRM 51-1-20D, 51-1-21.Jun 27, 2001 · N807UP · Doug DC873F · Wing, Plate/SkinSDR UPS01836238Fitting · crackedINSPECTION TYPE:C2 AFT PIT STA 1240 BETWEEN L35R-L34R FITTING CRACKED. REMOVED CRACKED FITTING IAW DC8 SRM 51-1-20D, REC'D LOCATED AND DRILLED NEW FITTING IAW DC8 SRM 51-1-24 AND INSTALLED IAW DC8 SRM 51-1-20D.Jun 27, 2001 · N851UP · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL2001801008Flow Valve · failedAT CRUISE ALTITUDE IN BOTH AUTO AND MANUAL PRESSURIZATION AT ALL FLOW SETTINGS, CABIN CLIMBS AND DESCENDS UP TO 700 FPM AND WILL NOT STABILIZE AT CONSTANT PRESSURE LT MANIFOLD PRESSURE FLUCTUATES 3 PSI IN CRU.FOUND LT FLOW CONTROL VALVE TO INTERMITTENT/INOP INJun 27, 2001 · N801DH · Doug DC873F · Cabin Cooling SystemSDR RRXA11376Fitting · corrodedDURING A MAINTENANCE VISIT FOUND C PI BATH TUB FITTING STA 1180 L33R - L34R HAS LITE CORROSION. REMOVED BATH TUB IAW SRM 51-1-20D. REMOVED CORROSION, TREATED AND PRIMED IAW SRM 51-1-8 AND 53-2-0 FIG 1F. INSTALLED REPLACEMENT PARTS IAW SRM51-1-20 AND DWG 375Jun 26, 2001 · N873SJ · Doug DC873F · Fuselage Main, Attach FittingsSDR RRXA11373Rib · crackedDURING A MAINTENANCE VISIT FOUND R/H CTR L/E XFS 329.0 LWR WAS CRACKED. *** CORRECTIVE ACTION *** REMOVED AND REPLACED RIB AND REINSTALLED IAW SRM 51-1-20D AND DWG 5769530-54.Jun 26, 2001 · N873SJ · Doug DC873F · Wing Main, Frame StructureSDR RRXA11322Wedge · dentedDURING A MAINTENANCE VISIT FOUND DENTED DAMAGE TO L/H O/B FLAP T/E WEDGE AT STA.340-410, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-21.Jun 26, 2001 · N606AL · Doug DC873F · Wing StructureSDR UPS01836378Fitting · crackedINSPECTION TYPE:C2 STA 1690 LONG 33R END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4641326 AND SRM 51-3-1, 51-1-21.Jun 26, 2001 · N807UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS01836377Floorbeam · corrodedINSPECTION TYPE:C2 STA 1580 LBL 24 FLOORBEAM IS CORRODED BEYOND LIMITS. REPAIRED FLOORBEAM IAW 8110-3 APPROVED DH SK 807-644.Jun 26, 2001 · N807UP · Doug DC873F · Fuselage Main, Floor BeamSDR UPS01836362Skin · crackedINSPECTION TYPE:C2 RIGHT WING UPPER SKIN IS CRACKED AT XRS 79 AT STRINGER 15. REPAIRED SKIN IAW SRM 57-2-1 FIG 10.Jun 26, 2001 · N807UP · Doug DC873F · Wing, Plate/SkinSDR UPS01836361Skin · crackedINSPECTION TYPE:C2 RIGHT WING UPPER SKIN IS CRACKED AT XRS 79 AT STRINGER 9. REPAIRED SKIN IAW SRM 57-2-1 FIG 10.Jun 26, 2001 · N807UP · Doug DC873F · Wing, Plate/SkinSDR UPS01836360Skin · crackedINSPECTION TYPE:C2 RIGHT WING UPPER SKIN IS CRACKED AT XRS 74 STRINGER 10. REPAIRED SKIN IAW SRM 57-2-1 FIG 10.Jun 26, 2001 · N807UP · Doug DC873F · Wing, Plate/SkinSDR UPS01836359Skin · crackedINSPECTION TYPE:C2 RIGHT WING UPPER SKIN IS CRACKED AT STA XRS 79. REPAIRED SKIN IAW SRM 57-2-1 FIG 10.Jun 26, 2001 · N807UP · Doug DC873F · Wing, Plate/SkinSDR UPS01836354Seat Track · corrodedINSPECTION TYPE:C2 STA 1620 - 1660 SEAT TRACK IS CORRODED BEYOND LIMITS AT BL 0. REPAIRED SEAT TRACK IAW SRM 53-2-3 FIG 8A.Jun 26, 2001 · N807UP · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR UPS01836352Rib · crackedINSPECTION TYPE:C2 LEFT WING L/E UPPER RIB IS CRACKED AT XFS 678.75. REPAIRED RIB IAW SRM 57-2-0 FIG 2.Jun 26, 2001 · N807UP · Doug DC873F · Wing, Rib/BulkheadSDR UPS01836336Skin · corrodedINSPECTION TYPE:C2 RIGHT WING LOWER L/E SKIN IS CORRODED BEYOND LIMITS AT XFS 722. REPAIRED SKIN IAW SRM 57-2-0 FIG 2A.Jun 26, 2001 · N807UP · Doug DC873F · Wing, Plate/SkinSDR UPS01836335Skin · crackedINSPECTION TYPE:C2 RIGHT WING UPPER SKIN IS CRACKED AT XRS 105 AT STRINGER 14. REPAIRED SKIN IAW SRM 57-2-1 FIG 10.Jun 26, 2001 · N807UP · Doug DC873F · Wing, Plate/SkinSDR UPS01836331Frame · crackedINSPECTION TYPE:C2 STA 1680 FRAME IS CRACKED AT LONG 21R. REPAIRED FRAME IAW SRM 53-2-0 FIG 2.Jun 26, 2001 · N807UP · Doug DC873F · Fuselage Main, FrameSDR UPS01836330Doubler · brokenINSPECTION TYPE:C2 LEFT WING LOWER FRONT SPAR STRAP AND DOUBLER ARE BROKEN AT XS 520. REMOVED, FABRICATED AND REPLACED DOUBLER AND STRAP IAW SRM 57-2-1 FIG 14A.Jun 26, 2001 · N807UP · Doug DC873F · Wing SparSDR UPS01836328Fitting · crackedINSPECTION TYPE:C2 STA 1690 LONG 35R END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4641326 AND SRM 51-1-20D.Jun 26, 2001 · N807UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS01836327Skin · crackedINSPECTION TYPE:C2 LEFT WING L/E LOWER SKIN IS CRACKED AT XFS 597.5. REPAIRED SKIN IAW EO DC8-5720-4087.Jun 26, 2001 · N807UP · Doug DC873F · Wing, Plate/SkinSDR UPS01836326Fitting · crackedINSPECTION TYPE:C2 STA 320 BANANA FITTING IS CRACKED AT 27L. REMOVED AND REPLACED FITTING IAW DWG 3754041 AND SRM 51-1-20D, 51-1-21.Jun 26, 2001 · N807UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS01836324Fitting · crackedINSPECTION TYPE:C2 STA 1690 LONG 22L END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4641326 AND SRM 51-1-20D, 51-1-21.Jun 26, 2001 · N807UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS01836321Gusset · crackedINSPECTION TYPE:C2 STA 1240 UPPER GUSSET IS CRACKED AT LONG 34R. REMOVED, FABRICATED AND REPLACED GUSSET IAW DWG 9758507 AND SRM 53-1-0, 51-1-20D.Jun 26, 2001 · N807UP · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA11375Skin · crackedDURING A MAINTENANCE VISIT FOUND R/H WING L/E STA XFS 300 LWR SKIN CRACKED AT FASTENER HOLE. *** CORRECTIVE ACTION *** REPAIRED SKIN IAW 8110-3 APPROVED DH SK 873-883Jun 25, 2001 · N873SJ · Doug DC873F · Wing, Plate/SkinSDR RRXA11374Doubler · corrodedDURING A MAINTENANCE VISIT FOUND FUSELAGE BULGED, POSSIBLE INTERNAL CORROSION @ L21R STA 25 - 8. *** CORRECTIVE ACTION *** REMOVED FASTENER, REMOVED CORRODED DOUBLER. FABRICATED AND INSTALLED REPLACEMENT PART IAW DWG 561386-5613861 AND SRM 51-1-21-1 AND 51-Jun 25, 2001 · N873SJ · Doug DC873F · Fuselage Main, StructureSDR UPS01836379Spar Cap · crackedINSPECTION TYPE:C2 STA 855 LT WING REAR SPAR LOWER CAP IS CRACKED FROM XCW 0 TO XCW 10. REPAIRED SPAR IAW 8110-3 APPROVED DH SK 807-357.Jun 25, 2001 · N807UP · Doug DC873F · Wing SparSDR UPS01836358Longeron · crackedINSPECTION TYPE:C2 STA 940 - 960 LONG 24L IS CRACKED. REPAIRED LONGERON IAW SRM 53-2-2 FIG 5.Jun 25, 2001 · N807UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS01836357Skin · crackedINSPECTION TYPE:C2 STA 1600 AT LONG 20L FWD LOWER CORNER OF L-2 DOOR FUSELAGE SKIN IS CRACKED. REPAIRED SKIN IAW SRM 53-2-0 FIG 18.Jun 25, 2001 · N807UP · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS01836356Skin · crackedINSPECTION TYPE:C2 STA 160 LONG 10R FUSELAGE SKIN IS CRACKED AT FWD UPPER CORNER OF R-1 DOOR OPENING. REPAIRED SKIN IAW SRM 53-2-0 FIG 14.Jun 25, 2001 · N807UP · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS01836351Rib · crackedINSPECTION TYPE:C2 LEFT WING L/E LOWER RIB IS CRACKED AT XFS 397.75. REPAIRED RIB IAW SRM 57-2-0 FIG 2.Jun 25, 2001 · N807UP · Doug DC873F · Wing, Rib/BulkheadSDR UPS01836334Skin · crackedINSPECTION TYPE:C2 STA 1620 LONG 20R LOWER FWD CORNER SKIN IS CRACKED AT R-2 DOOR. REPAIRED SKIN IAW SRM 53-2-0 FIG 17.Jun 25, 2001 · N807UP · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS01836333Skin · crackedINSPECTION TYPE:C2 RIGHT WING L/E UPPER SKIN IS CRACKED AT XFS 572.5. REPAIRED SKIN IAW SRM 57-2-1 FIG 38.Jun 25, 2001 · N807UP · Doug DC873F · Wing, Plate/SkinSDR UPS01836332Web · crackedINSPECTION TYPE:C2 STA 354 CUSP MEMBRANE IS CRACKED AT LONG 21L. REPAIRED MEMBRANE IAW SRM 53-2-0 FIG 1B.Jun 25, 2001 · N807UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS01836329Skin · crackedINSPECTION TYPE:C2 RIGHT WING L/E UPPER SKIN IS CRACKED AT XFS 200. REPAIRED SKIN IAW SRM 57-2-0 FIG 2.Jun 25, 2001 · N807UP · Doug DC873F · Wing, Plate/SkinSDR UPS01836322Rib · crackedINSPECTION TYPE:C2 LEFT WING L/E LOWER RIB IS CRACKED AT XFS 341. REPAIRED RIB IAW SRM 57-2-0 FIG 2.Jun 25, 2001 · N807UP · Doug DC873F · Wing, Rib/BulkheadSDR UPS01836319Skin · crackedINSPECTION TYPE:C2 COMPLY WITH EO DC8-5330-12073-A, STA 25 LONG 10L FOUND TWO SKIN CRACKS AFTER DOUBLER WAS REMOVED. REPAIRED SKIN IAW SRM 53-2-0 FIG 15.Jun 25, 2001 · N807UP · Doug DC873F · Fuselage Main, Plate/SkinSDR RRXA11321Intercostal · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO INTERCOSTAL AT STA.355, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-21, 57-3-3, 51-1-20D.Jun 24, 2001 · N606AL · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA11320Angle · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO ANGLE AT D-PIT DOOR JAMB LOWER SEAL DEPRESSOR, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 5Jun 24, 2001 · N606AL · Doug DC873F · Fuselage Main, StructureSDR UPS01836353Skin · crackedINSPECTION TYPE:C2 FUSELAGE SKIN IS CRACKED AT STA 1766 AT LONG 15R. REPAIRED SKIN IAW SRM 53-2-1 FIG 7.Jun 24, 2001 · N807UP · Doug DC873F · Fuselage Main, Plate/SkinSDR RRXA11372Seat Track · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION ON SEAT TRACK MAIN CABIN STA 550-590 LBL48 - LBL63. *** CORRECTIVE ACTION *** REMOVED AND REPLACED CORRODED FASTENER IAW SRM51-3-0. SPLICED CORRODED SEAT TRACK IAW SRM 53-2-3 FIG 8A AND 51-3-0.Jun 23, 2001 · N873SJ · Doug DC873F · Fuselage Main, StructureSDR RRXA11371Rib · crackedDURING A MAINTENANCE VISIT FOUND L/H CENTER L/E @ XS461 RIB IS CRACKED AT UPPER SKIN END. *** CORRECTIVE ACTION *** STOP DRILLED CRACK PER SRM 57-2-0 FIG 2. NDT CRACK TERMINATED PER SPM 06-10-01.001. FABRICATED AND INSTALLED REPAIR PARTS PER SRM 57-2-0 FIGJun 23, 2001 · N873SJ · Doug DC873F · Fuselage Main, StructureSDR RRXA11370Fitting · corrodedDURING A MAINTENANCE VISIT FOUND C PIT BATH TUB FITTING AT STA 1160 L33R I/B TO 33R O/B HAS HEAVY CORROSION. REMOVED BATH TUB FITTING PER SRM 51-1-20D, REMOVED CORROSION ON BATH TUB FITTING MOUNT POINT. THICKNESS PER NDI SPM 04.00.06 FOUND TO BE WITHIN LIMITJun 23, 2001 · N873SJ · Doug DC873F · Fuselage Main, Attach Fittings
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