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 UPS03840149Fitting · crackedINSPECTION TYPE:C1 MAIN CABIN FITTING IS CRACKED AT STA 680 FWD SIDE AT LONG 12R. REMOVED AND REPLACED FITTING IAW DWG 3779762, AND SRM 51-1-20D.Feb 1, 2003 · N811UP · Doug DC873F · Fuselage Main, Attach FittingsSDR UPS03840183Longeron · crackedINSPECTION TYPE: C1, STATION 1720 LONG 14R IS CRACKED. REMOVED CRACKED LONGERON, FABRICATED AND INSTALLED REPLACEMENT SECTION OF LONGERON AND INSTALLED REPAIR SPLICES IAW SRM 53-2-2 FIG 10 AND 11.Jan 31, 2003 · N811UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS03840151Clip · crackedINSPECTION TYPE: C1, STA 200 FRAME FORMER IS CRACKED ON I/B END BETWEEN LONG 32L AND 33L. REMOVED CRACKED FORMER CLIP, FABRICATED AND INSTALLED FORMER REPAIR CLIP IAW SRM 53-2-0 FIG 2A.Jan 31, 2003 · N811UP · Doug DC873F · Fuselage Main, StructureSDR DHL2003804878Cover · delaminatedLT WING JOINT FLAP COVER LOWER SKIN DELAMINATED. REMOVED AND REPLACED LT JOINT FLAP COVER IAW SRM 51-3-0 PG 1.Jan 30, 2003 · N804DH · Doug DC873F · Trailing Edge FlapsSDR DHL2003804544Link · crackedITEM REF. N/R: LH FLAP DRIVE LINK INNER BUSHING FLANGEPOINT "J" WITH .500 LONG CRACK IN IT. CORR: R/R LH FLAP DRIVE LINK @ STA. 219.99 IAW M/M 27-51-4 PG. 201 -204 REFERENCE N/R 0607 FOR OP'S CHECKJan 30, 2003 · N804DH · Doug DC873F · Trailing Edge Flap Control SystemSDR UPS03840233Skin · crackedINSPECTION TYPE: C1, REMOVE STEEL DOUBLER AT UPPER FWD CORNER OF THE L-1 FWD ENTRY DOOR AND REPAIR PER SRM 53-2-0 FIG 15 AT STA 25 LONG 10L. REMOVED EXISTING DOUBLER, CUTOUT DAMAGE, NDT VERIFIED NO CRACKS AT CUTOUT. FABRICATED AND INSTALLED DOUBLER, TRIPLERJan 30, 2003 · N811UP · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS03840163Skin · damagedINSPECTION TYPE: C1, STA 80 LONG 22L EXTERNAL DOUBLER HAS SEVERAL LOOSE CHERRY LOCK RIVETS. REMOVED DOUBLER AND FOUND BLIND FASTENERS UNDER DOUBLER WITH NO PITCH TO REPAIR DOUBLER HOLES, SHEAR TIE DRILLED THRU RADIUS, REMOVED DAMAGED SHEAR TIE, CUT OUT DAMAGJan 30, 2003 · N811UP · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS03840152Skin · crackedINSPECTION TYPE: C1, EXTERNAL FUSELAGE SKIN IS CRACKED AND CORRODED AT FASTENER HOLE AT STA 445 LONG 31L. CUTOUT DAMAGE, NDT VERIFIED NO CRACKS AT CUTOUT, FABRICATED AND INSTALLED DOUBLER, FILLER, AND FINGER DOUBLER IAW SRM 53-2-1 FIG 7.Jan 30, 2003 · N811UP · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS03840150Clip · crackedINSPECTION TYPE:C1 CLIP IS CRACKED AT STA 80 ABOVE LONG 30L. REMOVED, FABRICATED AND REPLACED CLIP IAW DWG 5613064 AND SRM 51-1-20D.Jan 30, 2003 · N811UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS03840148Fitting · crackedINSPECTION TYPE: C1, CRACKED FITTING BETWEEN STA 660 AND 680 AT LONGERON 11R IN MAIN CABIN. REMOVED AND REPLACED FITTING IAW DWG 5750540, AND SRM 51-1-20D.Jan 30, 2003 · N811UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS03840147Skin · crackedINSPECTION TYPE: C1, FUSELAGE SKIN IS CRACKED AT STA 1734 ABOVE LONG 16L. CUT OUT DAMAGE, NDT VERIFIED NO CRACKS AT CUTOUT. FABRICATED AND INSTALLED DOUBLER, FILLER, AND FINGER DOUBLERS IAW SRM 53-2-1 FIG 7.Jan 30, 2003 · N811UP · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS03840216Pan · crackedINSPECTION TYPE:C3, L2 LOWER FWD DOOR JAMB CORNER CRACKED TWO PLACES. FAB NEW SEAL RETAINER IAW DAC DWG 5751115. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. FAB PAN REPAIR DOUBLER IAW DAC DWG 5751040, ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED SEAL RETAJan 29, 2003 · N805UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS03840167Fitting · corrodedINSPECTION TYPE: C3, AFT CARGO PIT AT FS 1210 BETWEEN L33R-34R T-BOLT LATCH BACKUP FITTING IS CORRODED. REMOVED CORROSION IAW DC8 SRM 51-1-8. OUT OF LIMITS IAW DC8 SRM 53-2 -0. LOCATED, TRIMMED AND DRILLED UP FITTING 3754930-1 AND REPAIR FITTINGS 5894282-5Jan 29, 2003 · N805UP · Doug DC873F · Fuselage Main, Attach FittingsSDR DHL2003804538Doubler · crackedITEM REF. N/R: 1473 - LH WING CTR. L/E INNER DOUBLER UPPER PART WITH4.000 CRACK IN IT (STA XFS416.5000-429.000)CORR: REMOVED FASTNERS IAW SRM 51-1-21- PG. 1 REMOVED INNER DOUBLER IAW SRM51-1-21-PG 1 FABRICATED NEW INNER DOUBLER ( 7075T6AL.080) IAW SRM57-2-0 FIJan 28, 2003 · N804DH · Doug DC873F · Wing, Rib/BulkheadSDR UPS03840212Skin · crackedINSPECTION TYPE: C3, L1 DOOR UPPER FWD CORNER CRACKED BY CUTOUT, MARKED. FOUND WITH NDT ON SKIN MAT ID -17 DOUBLER 7075-T6 .063 PO 3874552 -15 DOUBLER 7075-T6 .080 PO 3958421 FILLER 7075-T6 .050 PO 3924131 IAW DC8 SRM 53-2-0. FAB DOUBLER TRIPER IAW DC8 SRM Jan 28, 2003 · N805UP · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS03840198Fitting · crackedINSPECTION TYPE: C3, CORROSION IN RT FWD UPPER CORNER OF RT MLG WHEEL WELL. REMOVED FITTING PN 3646772, REMOVED CORROSION FROM WEB IAW DC8 SRM 51-1-8, LESS THAN . 002 INCH, W/IN LIMITS IAW DC8 SRM 53-2-0. RECEIVED NEW FITTING P/N 3646772, LOCATED DRILL AND Jan 28, 2003 · N805UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS03840196Fitting · crackedINSPECTION TYPE: C3, LEFT WING FLAP HINGE SUPPORT FITTING AT STA XF 339 7332 CRACKED AT OUTBOARD SIDE JUST FWD OF FLAP FWD SPAR. REMOVED BASE FITTING, CENTER FITTING, SLIDER PANEL, OUTBOARD TRACK, CLOSURE PANELS AND SPRING PANEL IAW DC8 SRM 51-3-0. LOC AND Jan 28, 2003 · N805UP · Doug DC873F · Trailing Edge FlapsSDR DHL2003801002Smoke Detector1) #3 SMOKE DETECTOR MAIN CABIN WOULD NOT TEST. RELAMPED NO HELP.2) REMOVED AND REPLACED #3 SMOKE DETECTOR SYSTEM. OPS CHECKED OK IAW M/M 26-15-00.Jan 28, 2003 · N801DH · Doug DC873F · Smoke DetectionSDR DHL2003873001Smoke Detector · inoperativeLOWER CARGO SMOKE DETECTOR SYSTEM INOPERATIVE. MAINTENANCE MESSAGE AD1681 SHOWING. DEFERRED IAW MEL REF. 26-10-1-A1. CONTROL 11771 ASSIGNED. PLACARD INSTALLED.Jan 28, 2003 · N873SJ · Doug DC873F · Smoke DetectionSDR DHL2003804910Frame · crackedLT WING CTR L/E FORMER UPPER PART WITH 1.000 INCH CRACK AT STA XFS 460.250. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. STOP DRILLED CRACK IAW SRM 57-2-0 PG 9-10. FABRICATED DOUBLER ANGLE (2024-T3 AL0.040) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAJan 27, 2003 · N804DH · Doug DC873F · Leading Edge DevicesSDR DHL2003804911Frame · crackedLT WING- CTR L/E FORMER CRACKED 1.000, STA XFS 490.000. REMOVED FASTENERS IAW SRM 51-1-21 PG 1, STOP DRILLED CRACK AT STA XFS 490.000 IAW SRM 57-2-0 PG 9-10. FABRICATED ANGLE DOUBLER (2024-T3 AL0.040) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW Jan 27, 2003 · N804DH · Doug DC873F · Leading Edge DevicesSDR DHL2003804883Frame · crackedLT WING CTR L/E FORMER UPPER PART WITH 1.000 INCH CRACK AT STA XFS 496.250. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. STOP DRILLED CRACK AT STA XFS 496.250 IAW SRM 57-2-0 PG 9-10. FABRICATED DOUBLER ANGLE (2024-T3AL 0.040) IAW SRM 57-2-0 PG 9-10. CLEANED, TRJan 27, 2003 · N804DH · Doug DC873F · Leading Edge DevicesSDR DHL2003805002Engine · malfunctionedNR 1 ENGINE DID NOT SPOOL 240,100, LESS THAN 60 KTS, 3C, 16 FOOT, NORMAL. FOR INFORMATION ONLY PER GMM CHAP 8 SEC 8 PAGE 3.Jan 26, 2003 · N805DH · Doug DC873F · Engine (Turbine/Turboprop)SDR DHL2003804900Frame · crackedLT WING CTR L/E FORMER UPPER PART AT STA XFS 347.750 WITH 1.000 INCH CRACK. REMOVED FASTENERS IAW SRM 51-1-21 PG 1, STOP DRILLED CRACK IAW SRM 57-2-0 PG 9 - 10. FABRICATED DOUBLER ANGLE (2024-T3 AL0.040) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED DJan 25, 2003 · N804DH · Doug DC873F · Wing SparSDR DHL2003804899Frame · crackedLT WING CTR L/E FORMER LWR PART WITH CRACK AT STA XFS 297.500. STOP DRILLED CRACK IAW SRM 57-2-0 PG 9-10. FABRICATED DOUBLER ANGLE (2024-T3AL 0.040) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED DOUBLER ANGLE INNER SIDE IAW SRM 51-1-8B. INSTALLED DOUJan 25, 2003 · N804DH · Doug DC873F · Leading Edge DevicesSDR DHL2003804897Frame · crackedLT WING CTR L/E FORMER UPPER PART WITH 1.000 AT STA XFS 379.000. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. STOP DRILLED CRACK IAW SRM 57-2-0 PG 9-10. FABRICATED ANGLE DOUBLER (2024-T3 0.032) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW 51-1-8B. IJan 25, 2003 · N804DH · Doug DC873F · Leading Edge DevicesSDR DHL2003804902Frame · crackedLT WING CTR L/E FORMER UPPER PART WITH 1.000 INCH CRACK AT STA XFS 366.500. REMOVED FASTENERS IAW SRM 51-1-21 PG 1, STOP DRILLED CRACK IAW SRM 57-2-0 PG 9-10. FABRICATED ANGLE DOUBLER (2024-T3 AL0.040) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAWJan 25, 2003 · N804DH · Doug DC873F · Leading Edge DevicesSDR DHL2003804903Frame · crackedREMOVED FASTENERS IAW SRM 51-1-21 PG 1, STOP DRILLED CRACK IAW SRM 57-2-0 PG 9-10. FABRICATED ANGLE DOUBLER (2024-T3 AL0.040) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER WITH NEW FASTENERS ON LT WING CTR L/E Jan 25, 2003 · N804DH · Doug DC873F · Leading Edge DevicesSDR DHL2003804901Frame · crackedLT WING CTR L/E FORMER AT STA XFS 354.000 WITH 1.500 INCH CRACK. REMOVED FASTENERS IAW SRM 51-1-21 PG 1, STOP DRILLED CRACK IAW SRM 57-2-0 PG 9-10. FABRICATED DOUBLER ANGLE (2024-T3 AL0.040) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED DOUBLER ANGLE Jan 25, 2003 · N804DH · Doug DC873F · Leading Edge DevicesSDR DHL2003804518Frame · crackedLT WING I/B L/E FORMER CRACKED 1 IN STA XFS 603.750. REMOVED FASTNERS PER SRM 51-1-21 PG 1.STOP DRILLED CRACK PER SRM 57-2-0 PG 9-10.FABRICATED ANGLE DOUBLER (2024.T3 AL 0.032)PER SRM 57-2-0 PG 9-10.CLEANED TREATED AND PRIMED PER SRM 51-1-8B. INSTALLED ANGLJan 25, 2003 · N804DH · Doug DC873F · Leading Edge DevicesSDR DHL2003804875Web · crackedFUSE EXT - WEB LOWER PART CRACKED AT STA, 808.000 LBL 54.000. STOP DRILLED CRACK AT STA 808.000 LBL 54.000 IAW SRM 53-2-0, FABRICATED REINFORCEMENT (2024 T3 .040) IAW SRM 53-2-0 FIG 1B. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED REINFORCEMENT OJan 23, 2003 · N804DH · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS03840071Relay · inoperativeINSPECTION TYPE: PFLT, EMERGENCY EXIT LIGHTS WILL NOT CHECK. REMOVED AND REPLACED EMERGENCY LIGHTING BATTERY RELAY UNIT IAW MM 33-5 0-01. OPS CHECK NORMAL.Jan 23, 2003 · N810UP · Doug DC873F · Emergency LightingSDR DHL2003804770Cargo Track · wornMAIN CARGO TRACK WORN IN VARIOUS LOCATIONS . CUT OUT DAMAGED TRACKS IAW SRM 53-2-3 PG 17 , CLEANED , TREATED AND PRIMED AREA IAW SRM 51-1-8B INSTALLED NEW PLUGS AND CHANNEL OR INSTALLED NEW TRACK SECTION IAW SRM 53-2-3 PG. 49-50Jan 22, 2003 · N804DH · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR DHL2003804912Cargo Track · wornM/C COMPT CTR TRACK LUGS WORN FROM STA 1670.000 - STA 1710.000. REMOVED DAMAGED AREA FROM CTR TRACK IAW SRM 53-2-3 PG 49-50. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW TRACK SECTION AND REINSTALLED SPLICES IAW SRM 53-2-3 PG 49-50 AND 51Jan 21, 2003 · N804DH · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR DHL2003804904Cargo Track · wornMAIN CARGO COMPT NR 1 RT TRACK LUG WORN STA 1670.000 - STA 1770.000. REMOVED DAMAGED TRACK AREA IAW SRM 51-3-0 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW TRACK SECTION WITH NEW FASTENERS ON MAIN CARGO COMPT 1 RT TRACK STA 1670.000Jan 21, 2003 · N804DH · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR DHL2003804905Skin · delaminatedLT WING T/E TOP EXTERIOR SKIN SURFACE DELAMINATED (STA 5.000-47.000). CUT OUT DAMAGED AREA IAW SRM 57-2-3 PG 4 PAR 1. FABRICATED FILLER AND DOUBLER (7075-T6 AL0.032) IAW SRM 57-2-3 PG 4 PAR 11. CLEANED, TREATED AND PRIMED FILLER AND DOUBLER INNER SURFACE IAJan 21, 2003 · N804DH · Doug DC873F · Leading Edge DevicesSDR DHL2003804907Cargo Track · wornM/C COMPT NR 3 LT TRACK LUG WORN, STA 785.000. REMOVED NR 3 LT TRACK DAMAGED AREA IAW SRM 53-2-3 PG 17, SRM 51-3-0 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW CHANNEL AND PLUG IAW SRM 53-2-3 PG 17, SRM 51-3-0 PG 1.Jan 20, 2003 · N804DH · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR DHL2003804874Frame · crackedRT WING CTR L/E FORMER UPPER PART AT STA XFS 372.000 WITH .500. REMOVED FASTENERS IAW SRM 51-1-21 PG 1, STOP DRILLED .500 CRACK ON CENTER L/E FORMER UPPER PART IAW SRM 57-2-0 PG 9-10. FABRICATED A DOUBLER ANGLE 2024T3 AL.032 IAW SRM 57-2-0 PG 9-10. CLEANED,Jan 20, 2003 · N804DH · Doug DC873F · Leading Edge DevicesSDR DHL2003804502Frame · crackedRT WING CENTER L/E FORMER UPPER PART CRACKED 1/2 IN AT XFS 422.750. REMOVED FASTENERS PER SRM 51-1-21 PG 1. STOP DRILLED CRACK PER SRM 57-2-0 PG 9-10. FABRICATED ANGLE DOUBLER (2024-T3 AL 0.032) PER SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED PER SRM 5Jan 20, 2003 · N804DH · Doug DC873F · Leading Edge DevicesSDR UPS03840024Angle · corrodedINSPECTION TYPE: A, CORROSION IN RT FWD UPPER CORNER OF RIGHT MLG WHEEL WELL. FERRY TO TCO. REMOVED LITE SURFACE CORROSION, LESS THAN .002 INCH MATERIAL, W/IN LIMITS IAW DC8 SRM 53-2-0. ALODINED IAW DC8 SRM 51-1-8, OK TO PRIME. AFTER FURTHER INSPECTION, FJan 18, 2003 · N805UP · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL2003804668Door · crackedRT WING L/E OUTBD. SLOT DOORS SHOW .5000 CRACKS ON THREE SECTIONS BETWEEN STA. 435.789 - XS520.168 REMOVED DAMAGED L/E SLOT DOORS IAW MM 27-80-2 PG. 201-203 PERFORMED NEW HOLESAND COUNTERSUNK IAW SRM 51-1-22 FIG. 476 . INSTALLED NEW SLOT DOORS ON THE THREE SECJan 17, 2003 · N804DH · Doug DC873F · Wing StructureSDR DHL2003804517Frame · crackedRT WING CENTER L/E FORMER UPPER PART CRACKED 1/2 IN AT XFS 434.000. REMOVED FASTNERS PER SRM 51-1-21 PG 1.STOP DRILLED CRACK PER SRM 57-2-0 PG 9-10. FABRICATED REINFOCING ANGLE(2024.T3 AL 0.032)PER SRM 57-2-0 PG 9-10.CLEANED TREATED AND PRIMED PER SRM 51-1-8Jan 17, 2003 · N804DH · Doug DC873F · Leading Edge DevicesSDR DHL2003804511Frame · crackedRT WING CENTER L/E FORMER UPPER PART CRACKED AT XFS 454.000. REMOVED FASTNERS PER SRM 51-1-21 PG 1.STOP DRILLED CRACK PER SRM 57-2-0 PG 9-10. FABRICATED REINFOCING ANGLE (2024.T3 AL 0.032) PER SRM 57-2-0 PG 9-10.CLEANED TREATED AND PRIMED PER SRM 51-1-8B. INSJan 17, 2003 · N804DH · Doug DC873F · Leading Edge DevicesSDR DHL2003804510Frame · crackedRT WING CENTER L/E FORMER LOWER PART CRACKED AT 1/2 IN STA XFS 460.000. REMOVED FASTNERS PER SRM 51-1-21 PG 1.STOP DRILLED CRACK PER SRM 57-2-0 PG 9-10.FABRICATED REINFOCING ANGLE(2024.T3 AL 0.032)PER SRM 57-2-0 PG 9-10.CLEANED TREATED AND PRIMED PER SRM 51-1-Jan 17, 2003 · N804DH · Doug DC873F · Leading Edge DevicesSDR UPS03840072Fitting · corrodedINSPECTION TYPE: C-2, FORWARD PIT STA 140, BL45R AT CUSP, SUPPORT FITTING CORRODED. FABRICATED NEW PART IAW DAC DWG 5613430. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. LOCATED AND DRILLED IAW DAC DWG 5613430 AND DC8 SRM 51-1- 20. INSTALLED FITTING IAW DC8 SRJan 17, 2003 · N868UP · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL2003804665Vane · damagedRT OUTBD SLOT VANE AT STA XS 520.000 HOLES ELONGATED. PERFORMED MAJOR REPAIR IAW EO DHL 030101 , ED-3211. REMOVED FASTNERS IAW SRM 51-1-21 PG. 1, TRIMMED OUT DAMAGED SKIN SEGMENT IAW EO DHL 030101 , ED-3211 , FABRICATED REPAIR DOUBLER, A FILLER (7075T6AL-0.06Jan 16, 2003 · N804DH · Doug DC873F · Wing Main, Frame StructureSDR DHL2003804546Skin · corrodedITEM REF>: N/R: 0237 LH WING L/E UPPER SKIN CORRODED BETWEEN STA. XFS566.250 AND XFS585.000 ( MAJOR REPAIR)CORR: PERFORMED MAJORIAW SRM 57-2-1 PG. 2 REMOVED FASTNERS IAW SRM 51-1-21 PG. 1 REMOVED CORROSION ON LH WING UPPER SKIN ( STA. XFS566.250-585.000) IAW SJan 16, 2003 · N804DH · Doug DC873F · Wing, Plate/SkinSDR DHL2003804506Frame · crackedLT WING CENTER L/E FORMER CRACKED 1 INCH AT STA XFS 483.750 (UPPER). REMOVED FASTENERS PER SRM 51-1-21 PG 1. STOP DRILLED CRACK PER SRM 57-2-0 PG 9-10. FABRICATED REINFORCING ANGLE (2024-T3 AL 0.032) PER SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED PER Jan 16, 2003 · N804DH · Doug DC873F · Leading Edge DevicesSDR DHL2003804503Frame · crackedLT WING CTR L/E FORMER UPPER PART WITH 1 INCH CRACK AT STA XFS 416.500. REMOVED FASTENERS PER SRM 51-1-21 PG 1. STOP DRILLED CRACK PER SRM 57-2-0 PG 9-10. FABRICATED REINFORCEMENT ANGLE (2024-T3 AL 0.032) PER SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMEDJan 16, 2003 · N804DH · Doug DC873F · Leading Edge DevicesSDR DHL2003804500Frame · crackedRT WING L/E INNER FORMER CRACKED 1/2 IN AT XFS 598.000. REMOVED FASTNERS PER SRM 51-1-20D PG 21,STOP DRILLED CRACK PER SRM 57-2-0 PG 9-10.FABRICATED REINFOCING ANGLE(2024.T3 0.032. CLEANED, TREATED AND PRIMED PER SRM 51-1-8 B.INSTALLED REINFORCING ANGLE PER SJan 16, 2003 · N804DH · Doug DC873F · Leading Edge Devices
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