Douglas DC-8-71F

Service difficulty reports · 8,938

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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 = 'DC871F'
  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 UPS00833952Skin · crackedINSPECTION TYPE:C123, RT WING LOWER SKIN I/B OF NR 4 PYLON AND I/B OF MOLD LINE DOUBLER HAS APPROXIMATELY 1 INCH CRACK IN SKIN. FABED AND INSTALLED INTERNAL DOUBLER, TRIPLER AND FILLERS IAW REO-G07 605. ALODINED AND PRIMED IAW DC8 SRM 51-1-8.Sep 9, 2000 · N798UP · Doug DC871F · Wing, Plate/SkinSDR RRXA003748Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE FILLET ATTACH POINTS BETWEEN STA 1100-1080 AND L29R TO L30R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED PART IAW DC-Sep 8, 2000 · N500MH · Doug DC871F · Fuselage Main, Plate/SkinSDR RRXA003747Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE FILLET ATTACH POINTS BETWEEN STA 1140-1147 AT L27R TO L29R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED PART IAW DC-8Sep 8, 2000 · N500MH · Doug DC871F · Fuselage Main, Plate/SkinSDR RRXA003746Doubler · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE RT FILLET AND FASTENERS UNDER SKIN PANEL BETWEEN STA 1080 TO 1090 AND L30R TO L29R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED ANDSep 8, 2000 · N500MH · Doug DC871F · Fuselage Main, Plate/SkinSDR RRXA003745Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE AROUND SCREW HOLES ON THE LT FILLET SKIN BETWEEN STA 1120-1146 L26L TO L29L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. BLENDED CORROSION IAW DC-8 SSep 8, 2000 · N500MH · Doug DC871F · Fuselage Main, Plate/SkinSDR RRXA003740Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE EXTERIOR FWD. TOILET SERVICE PANEL AT STA 100, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 SRM 53-2-0 FIG 1F.Sep 8, 2000 · N500MH · Doug DC871F · Fuselage Main, Plate/SkinSDR RRXA003134Intercostal · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE INTERCOSTAL BETWEEN STA 1380 - 1400 AND LBL -18 WATERLINE -35, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 51-1-24, 5Sep 8, 2000 · N8076U · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS00833872Fitting · crackedINSPECTION TYPE:C123, MAIN CABIN LONG END FITTING CRACK BETWEEN STA 900 AND STA 920 AND L10L. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-1-20D.Sep 8, 2000 · N798UP · Doug DC871F · Fuselage Miscellaneous StructureSDR RRXA003760Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE AND A CRACK TO THE PRESS PANEL BETWEEN STA 834 & 857 L/H FROM O TO +69, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRSep 7, 2000 · N500MH · Doug DC871F · Fuselage Main, Plate/SkinSDR RRXA003754Stiffener · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE STIFFENER BETWEEN STA 960 TO 980 X=0 TO +25 Z=8, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED NEW PART AND INSTALLED IAW DC-8 SRM 51-1Sep 7, 2000 · N500MH · Doug DC871F · Fuselage Main, Plate/SkinSDR RRXA003753Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE SKIN & FINGER DOUBLER AT STA 879 TO 902 X=+45 TO +69 Z=8", DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED PART IAW DC-8 Sep 7, 2000 · N500MH · Doug DC871F · Fuselage Main, Plate/SkinSDR RRXA003752Frame · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE BETWEEN FRAMES AT STA 1560 TO 1580 AND L21R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED PART IAW DC-8 SRM 51-1-21, 53-2-0 FSep 7, 2000 · N500MH · Doug DC871F · Fuselage Main, FrameSDR UPS00833963Intercostal · crackedINSPECTION TYPE:C123, IN FWD LWR CARGO COMPT STA 580 - 600 L33R INTERCOSTAL IS BENT CRACKED AND GOUGED. REMOVED INTERCOSTAL, FABBED NEW INTERCOSTAL, ALODINED AND PRIMED. INSTALLED IAW DC8 SRM 51-1-8, 51-1-21, 51-1-20D & DAC DWG 5753650.Sep 7, 2000 · N798UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS00833962Fitting · corrodedINSPECTION TYPE:C123, STA 360 L33R FITTING ON FRAME HAS CORROSION. REMOVED CORROSION IAW 51-1-8 FOUND TO BE OUT OF LIMITS IAW 53-2-0. LOCATE NEW FITTING P/N 4759281-503 AND DRILLING EXISTING HOLES IAW DC8 SRM 51-1-20D, INSTALLED FITTING IAW 51-1-20D.Sep 7, 2000 · N798UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS00833956Fitting · corrodedINSPECTION TYPE:C123, STA 350 L36 FITTING HAS CORROSION GEN AND RECD RFTS 798UP-11-21713 W/ REO G07628. TRIMMED OUT CORROSION IAW REO G07628, ALODINED AND PRIMED IAW DC8 SRM 51-1-8.Sep 7, 2000 · N798UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS00833703Battery Pack · inoperativeINSPECTION TYPE:P/F, ON PREFLIGHT LIGHTS DO NOT COME ON DURNIG TEST. REMOVED AND REPLACED EMERGENCY BATTERY PACK. OPS CHECK GOOD.Sep 7, 2000 · N779UP · Doug DC871F · Emergency LightingSDR UPS00833969Fitting · corrodedINSPECTION TYPE:C123, AFT LOWER PIT TRANVERSE FLOORBEAM END FITTING HAS CORROSION FS 1220 BL 64L. REMOVED CORROSION IAW 51-1-8, FOUND TO BE OUT OF LIMITS IAW DC8 SRM 53-2 -0, REMOVED FITTING IAW DC8 SRM 51-1-20 & 51-3-0, RCVD LOCATED AND DRILLED FITTING IAW DSep 6, 2000 · N798UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS00833968Fitting · crackedINSPECTION TYPE:C123, AFT LWR CARGO COMPT STA 1180 L33R FITTING CRACKED. REMOVED FITTING IAW 51-1-20D, RECEIVED NEW FITTING P/N 3755841-501N PO SP0470 579 RECEIVED DOOR JAMB FITTING DOUBLERS 3755841-5U, LOCATED AND DRILLED NEW FITTING DOUBLERS IAW DC8 SRM 51Sep 6, 2000 · N798UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS00833967Fitting · corrodedINSPECTION TYPE:C123, AFT LWR CARGO COMPT STA 1180 L35R FITTING HAS CORROSION. REMOVED CORRODED FITTING, FABED REPAIR ANGLES IAW DC8 SRM 53-2-0, ALODINED AND PRIMED IAW DC8 SRM 51-1-8 AND INSTALLED NEW FITTING AND REPAIR ANGLES IAW DC8 SRM 51-1-20D.Sep 6, 2000 · N798UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS00833951Fitting · crackedINSPECTION TYPE:C123, NWW LT NLG DOOR RETRACT ACTUATOR SUPPORT FITTING HAS 5 INCH CRACK ON FWD END LHS ABOVE PANEL NR 696. REPAIRED AREA IAW REO G07656.Sep 6, 2000 · N798UP · Doug DC871F · Fuselage, Landing Gear Attach FittingsSDR UPS00833948Fitting · crackedINSPECTION TYPE:C123, STA 680, L10R SPLICE FITTING CRACKED. REMOVED CRACKED FITTING AND REPLACED IAW DAC DWG 3779762 & 5615718.Sep 6, 2000 · N798UP · Doug DC871F · Fuselage Miscellaneous StructureSDR RRXA003136Angle · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE BLEED AIR CONNECTOR DOOR LANDING AT THE RT RAM AIR INLET, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 53-2-0.Sep 6, 2000 · N8076U · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS00833874Frame · corrodedINSPECTION TYPE:C123, THE AFT CARGO COMPT STA 1160 - 1220 L35L - L36 AREA FRAME UPPER SURFACE HAS CORROSION SEVERAL PLACES. REMOVED CORR IAW DC8 SRM 51-1-8, FOUND TO BE OUT OF LIMITS IAW DC8 SRM 5 3-2-0. GEN AND RECD RFTS N798UP REO G07632. FAB DOUBLER AND Sep 6, 2000 · N798UP · Doug DC871F · Fuselage Main, FrameSDR UPS00833828Frame · corrodedINSPECTION TYPE:C123, AFT PIT FS 1380 FRAME CORRODED AT LONGERON 36. REMOVED DAMAGED AREA ACQUIRED MAT ID FOR REPAIR ANGLE DOUBLER STRIP FILLER, FABBED REPAIR PARTS AND HEAT TREATED REPAIR ANGLE, ALODINED AND PRIMED REPAIR PARTS SEALED AND INSTALLED.Sep 6, 2000 · N798UP · Doug DC871F · Fuselage Main, FrameSDR UPS00833827Fitting · crackedINSPECTION TYPE:C123, STA 680L7R SPLICE FITTING CRACKED. REMOVED CRACKED FITTING IAW DC8 SRM 51-1-20D AND 51-3-0, RECEIVED NEW FITTING (P/N 3779762-501), DRILLED IAW DC8 SRM 51-1-24, INSTALLED IAW DC 8 SRM 51-1-20D, 51-1-21 AND 51-3-0.Sep 6, 2000 · N798UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS00833826Fitting · crackedINSPECTION TYPE:C123, STA 680 L5R SPLICE FITTING CRACKED. REMOVED CRACKED FITTING IAW DC8 SRM 51-3-0 AND 51-1-24, LOCATED AND DRILLED NEW FITTING IAW DAC DWG 3779762, INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D, 51-1-21 AND 51-3-0 FITTING (P/N 3779762-501).Sep 6, 2000 · N798UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS00833825Fitting · crackedINSPECTION TYPE:C123, STA 680 L4R SPLICE FITTING CRACKED. REMOVED CRACKED FITTING IAW DC8 SRM 51-3-0 & 51-1-24, LOCATED AND DRILLED NEW FITTING (P/N 3779762-501) IAW DAC DWG 3779762, INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D, 51-1-21 AND 51-3-0.Sep 6, 2000 · N798UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS00833794Fitting · crackedINSPECTION TYPE:C123, IN THE AFT LOWER CARGO COMPT STA 1150 L35R, FITTING IS CRACKED. REMOVED FITTING IAW DC8 SRM 51-1-20D, LOCATED AND DRILLED NEW FITTING IAW DC8 SRM 51-1-24, FABRICATED DOUBLERS IAW DC8 SRM 53-2-0, ALODINED AND PRIMED IAW DC8 SRM 51-1-8, INSep 6, 2000 · N798UP · Doug DC871F · Fuselage Main, Attach FittingsSDR UPS00833702Battery Pack · dischargedINSPECTION TYPE:P/F, EMERGENCY LIGHTING INOP. FOUND SOCKET NR 11 CONNECTOR P1-1345 BAD. REPLACED PER WDM 33-50-01 PG 1. REPLACED BATTERY PACK DUE TO LOW VOLTAGE. SYSTEM OPS CHECKS NORMAL PER MM 33-50-01.Sep 6, 2000 · N705UP · Doug DC871F · Emergency LightingSDR RRXA003744Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE SKIN AND POPPED RIVETS AT STA 25 L21R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED PART IAW DC-8 SRM 51-1-21 AND 53-2Sep 5, 2000 · N500MH · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS00833964Intercostal · corrodedINSPECTION TYPE:C123, FLC INTERCOSTAL CORRODED BTW STA 70R, 71R AND L33R. REMOVED CORROSION FOUND TO BE OUT OF LIMITS IAW DC8 SRM 51-1-8 & 53-2-0. FABED FILLER AND ANGLE DOUBLER IAW DC8 SRM 53-2-0. ALODINED AND PRIMED INSTALLED IAW DC8 SRM 53-2-0 & 51-1-8.Sep 5, 2000 · N798UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS00833955Fitting · corrodedINSPECTION TYPE:C123, FITTING CORRODED BEYOND LIMITS. REPLACED FITTING IAW DC8 SRM 51-1-20D.Sep 5, 2000 · N798UP · Doug DC871F · Fuselage Main, Attach FittingsSDR UPS00833824Longeron · crackedINSPECTION TYPE:C123, LONGERON 16L CRACKED AT FS 1774. REPLACED LONGERON 16L FS 1774 IAW DC8 SRM 51-1-20D, 51-1-21 & 51-3-0.Sep 5, 2000 · N798UP · Doug DC871F · Fuselage Main, Longeron/StringerSDR UPS00833819Intercostal · crackedINSPECTION TYPE:C123, INTERCOSTAL CRACKED AT STA 150 & L10RT. REMOVED INTERCOSTAL IAW DC8 SRM 51-1-20D, FABED NEW IAW DAC DWG 56157 00, ALODINED AND PRIMED IAW 51-1-8.Sep 5, 2000 · N798UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS00833796Fitting · crackedINSPECTION TYPE:C123, AFT LOWER PIT TRANSVERSE FLOORBEAM END FITTING CRACKED BETWEEN BOLT HOLES FS 1160 BL 66R AT FWD UPPER CORNER OF C-PIT DOOR. REMOVED TRANSVERSE FLOORBEAM END FITTING IAW DC8 SRM 57-1-20D END FITTING FOUND TO BE CRACKED RCVD. ORDERED NEW Sep 5, 2000 · N798UP · Doug DC871F · Fuselage Main, Attach FittingsSDR UPS00833960Skin · crackedINSPECTION TYPE:C123, LWR FUSELAGE LONG 34 LT SIDE END FTG AT STA 780 IS CRACKED. REMOVED AND REPLACED END FITTING IAW DC8 SRM 51-1-24 51-1-20D.Sep 4, 2000 · N798UP · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS00833959Fitting · crackedINSPECTION TYPE:C123, NR 1 PYLON FWD OF FWD V-BLOCK SUPPORT FTG FOR PYLON PLANK PNL IS CRACKED P/N 5756790-1. REMOVED CRACKED V-FITTING IAW DC8 SRM 51-1-20D & 51-3-0. INSTALLED FWD V-BLOCK IAW DC8 SRM 51-1-20D & 51-3-0. LEAK CHECK OF FWD V-BLOCK TO BE PERFOSep 4, 2000 · N798UP · Doug DC871F · Wing, Nacelle/Pylon Attach FittingsSDR UPS00833876Fitting · crackedINSPECTION TYPE:C123, FRAME SECTION 680R L14R HAS A CRACKED FITTING ON AFT SIDE OF INTERCOSTAL. REMOVED CRACKED FITTING, FABED FITTING IAW DAC DWG 2651707, ALODINED AND PRIMED IAW DC8 SRM 51-1-8, INSTALLED WITH HI-LOKS IAW DC8 SRM 51-1-20D.Sep 4, 2000 · N798UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS00833843Longeron · corrodedINSPECTION TYPE:C123, INNER LIP OF STR 8L CORRODED (EXFOLIATION) AT STA 80 & 9G NET FTG DOT I777. REMOVED DAMAGED LONGERON L8L FROM STA 70 - 100 MACHINED NEW LONGERON IAW DAC DWG 5610118, LOCATED AND DRILL UP NEW LONGERON IAW DC8 SRM 51- 1-24, ALODINED AND PRSep 4, 2000 · N798UP · Doug DC871F · Fuselage Main, Longeron/StringerSDR UPS00833793Frame · corrodedINSPECTION TYPE:C123, FRAME LIP CORRODED (EXFOLIATION) AT STA 55, BETWEEN STR 2L-5L DOT I769. REMOVED GILLINER SUPPORT FOR ACCESS TO CORROSION REMOVED CORROSION IAW DC8 SRM 51-1-8, REMOVAL HAS FRAME OUT OF LIMITS. REMOVED DAMAGE SECTION OF FRAME IAW DC8 SRM Sep 4, 2000 · N798UP · Doug DC871F · Fuselage Main, FrameSDR UPS00833800Fitting · crackedINSPECTION TYPE:C123, FRAME STA 740R L13R HAS A CRACKED FITTING ON AFT SIDE. REMOVED CRACKED FITTING IAW DC8 SRM 51-1-20. RECEIVED NEW FITTING P/N 4 751643-1, DRILLED NEW FITTING IAW DAC DWG 4751643, INSTALLED IAW DC8 SRM 51-3-0 & DC8 SRM 51-1-21D.Sep 4, 2000 · N798UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS00833723Skin · damagedINSPECTION TYPE:C123 RIGHT WING L/E UPPER SKIN IS DAMAGED BEYOND LIMITS AT XFS 397.750. REPAIRED SKIN IAW DC8-5720-7767-A.Sep 4, 2000 · N729UP · Doug DC871F · Wing, Plate/SkinSDR UPS00833816Fitting · crackedINSPECTION TYPE:C123, FITTING CRACKED. INSTALLED NEW FITTING AT FS 680 RT L11 IAW DC8 SRM 51-1-20D AND 51-3-0.Sep 3, 2000 · N798UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS00833743Intercostal · crackedINSPECTION TYPE:C123, STA 370 LONG 33L INTERCOSTAL IS CRACKED. REMOVED, FABRICATED, AND REPLACED INTERCOSTAL IAW DWG 5750726, AND SRM 51-1-21.Sep 2, 2000 · N729UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS00833741Fitting · corrodedINSPECTION TYPE:C123, STA 300 LONG 34L BATHTUB FITTING IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED FITTING IAW DWG 3755822, AND SRM 53-2-0 FIG 2D.Sep 2, 2000 · N729UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS00833869Skin · corrodedINSPECTION TYPE:C123, CORROSION IN FASTENER HOLE THROUGH FUSELAGE SKIN STA 1030 L23R. REMOVED CORROSION FOUND TO BE OUT OF LIMITS IAW DC8 SRM 53-2-0 MAT ID FOR EXTERNAL DOUBLER .140 7075-T6 PO 283708 MAT ID FOR FINGER DOUBLER .050 7075-T6 PO 332573 IAW DC8 SRSep 1, 2000 · N798UP · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS00833788Angle · crackedINSPECTION TYPE:C123, LEFT WING L/E VERTICAL ANGLE IS CRACKED AT XS250. REMOVED, FABRICATED AND REPLACED ANGLE IAW DWG 9753297, AND SRM 51-1-20D.Sep 1, 2000 · N729UP · Doug DC871F · Wing Miscellaneous StructureSDR UPS00833762Angle · crackedINSPECTION TYPE:C123, STA 1770 LONG 19R SUPPORT ANGLE IS CRACKED. REMOVED, FABRICATED, AND REPLACED ANGLE.Sep 1, 2000 · N729UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS00833753Doubler · crackedINSPECTION TYPE:C123, RIGHT WING L/E LOWER INTERNAL DOUBLER IS CRACKED AT STA XFS.347.75. REMOVED, FABRICATED, AND REPLACED DOUBLER IAW DWG 5769589, AND SRM 51-1-20D, 51-1-21.Sep 1, 2000 · N729UP · Doug DC871F · Wing, Plate/SkinSDR UPS00833744Doubler · crackedINSPECTION TYPE:C123, LEFT WING L/E LOWER INTERNAL DOUBLER IS CRACKED AT XFS 360.25. REMOVED, FABRICATED, AND REPLACED DOUBLER IAW 5769589, AND SRM 51-1-20D, 51-1-21.Sep 1, 2000 · N729UP · Doug DC871F · Wing, Plate/Skin
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