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 UPS03841190Fitting · crackedINSPECTION TYPE: C1, RT FWD TYPE 1 DOOR HAS A CRACKED FITTING BELOW THE MOST FORWARD LOWER ST OP FITTING AT AFT FRAME OF THE FORWARD WEB SECTION REMOVED FITTING RT EMERGENCY EXIT DOOR LOWER CORNER. REMOVED RT EMERGENCY EXIT DOOR. LOCATED AND DRILLED NEW FAug 11, 2003 · N801UP · Doug DC873F · Emergency ExitsSDR UPS03841189Floorbeam · corrodedINSPECTION TYPE: C1, CORROSION ON FLOORBEAM UNDERSIDE AT STA 1680 LBL 43 REMOVED CORROSION IAW DC8 SRM 51-1-8. MATERIAL REMAINING 0.00 FROM .125 FOUND OUT OF LIMITS IAW DC8 SRM 53-2-0 FIG 1F. FABRICATED REPAIR ANGLE AND FILLER IAW DC8 SRM 53-2-0 FIG 1B ANAug 10, 2003 · N801UP · Doug DC873F · Fuselage Main, Floor BeamSDR UPS03841188Floorbeam · corrodedINSPECTION TYPE: C1, CORROSION ON FLOORBEAM UNDER SIDE AT STA 1660 LBL 38.5 REMOVED CORR IAW DC8 SRM 51-1-8. MAT'L REMAINING 0.00 FROM .125 FOUN D OUT OF LIMITS IAW DC8 SRM 53-2-0 FIG 1F. FABRICATED REPAIR AN GLE AND FILLERS IAW DC8 SRM 53-2-0 FIG 1B & TR Aug 10, 2003 · N801UP · Doug DC873F · Fuselage Main, Floor BeamSDR DHL2003873011Indicator · inoperativeSMOKE IN COCKPIT COMING FRON HYD PITCH TRIM AREA. CHECKED AREA FOUND LONGITUDINAL TRIM INDICATOR LIGHT PLATE BAD, ISOLATED WIRES AND DEFERRED LIGHT PLATE. SEE ITEM 7M PAGE 279774. LONGITUDINAL TRIM INDICATOR LIGHT PLATE IS INOPERATIVE. ITEM TRANSFERRED TO DAug 9, 2003 · N873SJ · Doug DC873F · Autopilot Trim IndicatorSDR DHL2003805575Frame · crackedLEFT WING CTR L/E FORMER CRACKED 1.000 AT STA XFS 385.250. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. PERFORMED STOP HOLE ON CRACK END IAW SRM 57-2-0 PG 9-10. FABRICATED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTAAug 8, 2003 · N805DH · Doug DC873F · Wing, Rib/BulkheadSDR DHL2003805563Skin · damagedINTERIM REPAIR ON RIGHT INBD FLAP UPPER SURFACES, STA XW.106.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG 1, SRM 57-7-1 PG 2, FIG 1. REMOVED PLATING WITH INTERIM REPAIR IAW SRM 51-1-21 PG 1. CLEANED, TREATED AND PRIMED INTERNAL AREA IAW SRM Aug 8, 2003 · N805DH · Doug DC873F · Trailing Edge FlapsSDR DHL2003805522Frame · crackedLEFT WING CTR L/E FORMER CRACKED 0.500 AT STA XFS 416.500. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. PERFORMED STOP HOLE ON CRACK END IAW SRM 57-2-0 PG 9-10. FABRICATED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTAAug 8, 2003 · N805DH · Doug DC873F · Wing, Rib/BulkheadSDR DHL2003805517Frame · crackedLEFT WING CTR L/E FORMER CRACKED 0.500 AT STA XS 461.372. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. PERFORMED STOP HOLE ON CRACK END IAW SRM 57-2-0 PG 9, 10. FABRICATED ANGLE DOUBLER IAW SRM 57-2-0 PG 9, 10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTAug 8, 2003 · N805DH · Doug DC873F · Wing, Rib/BulkheadSDR DHL2003805593Skin · corrodedRIGHT OUTER WING INBD L/E UPPER SKIN SURFACE CORRODED STA XFS 568.000 - 633.750 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-2-1 FIG 44. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 57-Aug 8, 2003 · N805DH · Doug DC873F · Wing, Plate/SkinSDR UPS03841186Fitting · crackedINSPECTION TYPE: C1, CABIN STA 857, L19R FITTING BEHIND INTERCOSTAL CRACKED. REMOVED FITTING FROM STA 857, L19R FOR REPLACEMENT, RECEIVED SUPPORT FITTING P/N 3779498-502. LOCATED AND DRILLED IAW DC8 SRM 51-3-2. IN STALLED NEW FITTING IAW DC8 SRM 51-1-20D.Aug 8, 2003 · N801UP · Doug DC873F · Fuselage Main, Attach FittingsSDR UPS03841184Frame · corrodedINSPECTION TYPE: C1, CORROSION ON FRAME FS 1340 S36L. REMOVED CORROSION IAW DC8 SRM 51-1-8, ORIG THICK 0.080, LOSS .020 REM. MATERIAL .060, FOUND OUT OF LIMITS IAW DC8 SRM 53-4-1, 51-2-0, & 53-2-0.FAB BED ANGLE REPAIR (7075-0, 0.080, PO 312487.0) IAW DC8 T/R NAug 8, 2003 · N801UP · Doug DC873F · Fuselage Main, FrameSDR DHL2003805591Frame · crackedLEFT WING CTR L/E FORMER CRACKED 0.500 AT STA XS 442.185. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. PERFORMED STOP HOLE ON CRACK END IAW SRM 57-2-0 PG 9-10. FABRICATED ANGLE DOUBLERS IAW SRM 57-2-0 PG 9-10 (2024-T3 0.032, 2024-T3 0.040). CLEANED, TREATED ANDAug 7, 2003 · N805DH · Doug DC873F · Wing SparSDR DHL2003805573Skin · corrodedLEFT WING CTR L/E CORRODED FROM STA XFS 297.500 - XFS 310.250 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-2-1 FIG 44. REMOVED FASTENERS IAW SRM 51-1-21 PG 1, SRM 51-1-20D PG 21. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 5Aug 7, 2003 · N805DH · Doug DC873F · Wing, Plate/SkinSDR DHL2003805533Plate · nickedLEFT WING INBD FLAP PLATING UPPER PART WITH 0.500 NICK AT XW 104.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG 1, SRM 57-7-1 PG 2, FIG 1. PERFORMED BLEND OUT ON PLATING FOUND OUT OF LIMITS (DEPTH 0.042, DIA 0.500) IAW SRM 57-2-0 PG 14. REMOVEAug 7, 2003 · N805DH · Doug DC873F · Trailing Edge FlapsSDR DHL2003805529Frame · crackedLEFT WING CTR L/E FORMER CRACKED 0.500 AT STA XFS 379.000. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. PERFORMED STOP HOLE ON CRACK END IAW SRM 57-2-0 PG 9-10. FABRICATED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTAAug 7, 2003 · N805DH · Doug DC873F · Wing, Rib/BulkheadSDR DHL2003805530Intercostal · crackedRIGHT WING CTR L/E INTERCOSTAL CRACKED 2.000, STA XS 454.976 - XS 461.372. REMOVED CRACKED INTERCOSTAL IAW SRM 51-1-21 PG 1. FABRICATED INTERCOSTAL IAW SRM 57-1-0 PG 1 SRM 57-3-3 PG 15. CLEANED, TREATED AND PRIMED INTERCOSTAL IAW SRM 51-1-8B. INSTALLED INTAug 7, 2003 · N805DH · Doug DC873F · Wing Miscellaneous StructureSDR DHL2003805516Frame · crackedLEFT WING CTR L/E FORMER CRACKED 0.500 AT STA XS 448.561. REMOVED FASTENERS IAW SRM 51-1-21 PG 1, PERFORMED STOP HOLE ON CRACK END IAW SRM 57-2-0 PG 9, 10. FABRICATED ANGLE DOUBLER IAW SRM 57-2-0 PG 9, 10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTAAug 7, 2003 · N805DH · Doug DC873F · Wing, Rib/BulkheadSDR DHL2003805515Frame · crackedLEFT WING CTR L/E FORMER CRACKED 0.500 AT STA XFS 347.750. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. PERFORMED STOP HOLE ON CRACK END IAW SRM 57-2-0 PG 9, 10. FABRICATED ANGLE DOUBLERS IAW SRM 57-2-0 PG 9, 10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INAug 7, 2003 · N805DH · Doug DC873F · Wing, Rib/BulkheadSDR DHL2003805502Frame · crackedRT WING CTR L/E FORMER 0.250 CRACKED, STA XFS 291.500. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. PERFORMED STOP HOLE ON CRACK END IAW SRM 57-2-0 PG 9-10. FABRICATED ANGLE DOUBLER (AL2024-T3 0.040) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED ANGLE DOUAug 7, 2003 · N805DH · Doug DC873F · Wing SparSDR UPS03841182Frame · corrodedINSPECTION TYPE: C1, MAIN CABIN LT SIDE AT STA 1140 FWD SIDE 4 INCH ABOVE CUSP FRAME HAS CORROSION. REMOVED CORROSION, AREA IS OUT OF LIMITS IAW DC8 SRM 53-2-0, FABRICATED REPAIR IAW DC8 SRM 53-2-0, ALODINED AND PRIMED IAW DC8 SRM 51-1- 8, AND INSTALLED REPAAug 7, 2003 · N801UP · Doug DC873F · Fuselage Main, FrameSDR UPS03841181Fitting · crackedINSPECTION TYPE: C1, AFT CARGO PIT AT FS 1140-1150 L35L INTERCOSTAL ATTACH FITTING IS CRACKED. VERIFIED CRACK IAW DYE PENETRANT TEST IAW DPS 4.707.1, REMOVED FITTIN G IAW DC8 SRM 51-1-20D, RECEIVED NEW FITTING P/N 3758497.1N PO NR 3541 22 LOCATED AND DRILLED Aug 7, 2003 · N801UP · Doug DC873F · Fuselage Main, Attach FittingsSDR UPS03841180Fitting · crackedINSPECTION TYPE: C1, AFT CARGO PIT AT FS 1140-1150 BETWEEN L32R-L33R INTERCOSTAL ATTACK F ITTING IS CRACKED VERIFIED CRACK IAW DYE PENETRANT TEST IAW DPS 4.707.1. REMOVED CRACKED FITTING IAW DC8 SRM 51-1-20D. REC'D, LOCATED, AND DRILLED NEW FIT TING IAW DC8Aug 7, 2003 · N801UP · Doug DC873F · Fuselage Main, Attach FittingsSDR UPS03841178Fitting · crackedINSPECTION TYPE: C1, AFT CARGO PIT AT FS 1150 L32 RT-L33 RT BANANA FITTING IS CRACKED. REMOVED (2) BANANA FITTINGS STA 1152 AND 1160 L33R-L30R. UPON FURTHER INSPECTION BANANA FITTING NOTED TO BE CRACKED. REC'D, LOCATED, AND DRILLED (2) BANANA FITTINGS IAW DCAug 7, 2003 · N801UP · Doug DC873F · Fuselage Main, Attach FittingsSDR UPS03841176Web · crackedINSPECTION TYPE: C1, STA 25 S21L CUSP CRACKED APPROX. 3 INCHES IN LENGTH. FABRICATED NEW CUSP WEB, MATERIAL ID .063 2024-T3, PO 415380.3, ALODIINED, PRIMED, INSTALLED NEW CUSP CHORD WEB AND PARTS REMVOED TO FOM IAW DAC DWG 5597646, DC8 SRM 51-1-8, 51-1-21, Aug 7, 2003 · N801UP · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL2003805559Frame · crackedRIGHT OUTER WING INBD L/E FORMER CRACKED 2.000, STA XFS 672.500 (UPPER PART). REMOVED FASTENERS IAW SRM 51-1-21 PG 1. STOP DRILLED CRACK IAW SRM 57-2-0 PG 9-10. FABRICATED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED ANGLE DOUBLER IAW Aug 6, 2003 · N805DH · Doug DC873F · Wing, Rib/BulkheadSDR DHL2003805562Frame · crackedRT OUTER WING INBD L/E FORMER CRACKED 1.000, STA XFS 660.000 (UPPER PART). REMOVED FASTENERS IAW SRM 51-1-21 PG 1. PERFORMED STOP HOLE ON CRACK END IAW SRM 57-2-0 PG 9-10. FABRICATED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED AREA IAAug 6, 2003 · N805DH · Doug DC873F · Wing, Rib/BulkheadSDR DHL2003805565Plate · damagedELONGATED HOLES IN UPPER PLATING OF LEFT WING CTR L/E STA XS 520.168. PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG 1, SRM 57-3-3 PG 12. REMOVED UPPER PLATING WITH ELONGATED HOLES IAW SRM 51-1-21 PG 1, SRM 51-3-0 PG 1, SRM 51-1-20D PG 21. FABRICATED NEW PLATING Aug 6, 2003 · N805DH · Doug DC873F · Wing, Plate/SkinSDR DHL2003805561Frame · crackedRIGHT OUTER WING INBD L/E SHOWS FORMER CRACKED 1.000, STA XFS 635.000 (UPPER PART). REMOVED FASTENERS IAW SRM 51-1-21 PG 1. PERFORMED STOP HOLE ON CRACK END IAW SRM 57-2-0 PG 9-10. FABRICATED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10. INSTALLED ANGLE DOUBLER WIAug 6, 2003 · N805DH · Doug DC873F · Wing, Rib/BulkheadSDR DHL2003805560Frame · crackedRT OUTER WING INBD L/E SHOWS FORMER CRACKED 1.000, STA XFS.641.250 (UPPER PART). REMOVED FASTENERS IAW SRM 51-1-21 PG 1. STOP DRILLED CRACK IAW SRM 57-2-0 PG 9-10. FABRICATED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED AREA AND ANGLE Aug 6, 2003 · N805DH · Doug DC873F · Wing, Rib/BulkheadSDR DHL2003805523Frame · crackedLEFT WING CTR L/E FORMER CRACKED 0.500 AT STA XS 478.897. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. PERFORMED STOP HOLE ON CRACK END IAW SRM 57-2-0 PG 9-10. FABRICATED AN ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSAug 6, 2003 · N805DH · Doug DC873F · Wing, Rib/BulkheadSDR DHL2003805590Frame · crackedRIGHT OUTER WING INBD L/E SHOWS FORMER CRACKED 1.000, STA XFS.635.000 (UPPER PART). REMOVED FASTENERS IAW SRM 51-1-21 PG 1. PERFORMED STOP HOLE ON CRACK END IAW SRM 57-2-0 PG 9-10. FABRICATED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMEAug 6, 2003 · N805DH · Doug DC873F · Wing, Rib/BulkheadSDR DHL2003805583Clip · crackedCRACKED CLIP IN LEFT WING TO FUSELAGE INTERNAL STRUCTURE, STA 640.000 BETWEEN S-23L AND S-24L. REMOVED CRACKED CLIP IAW SRM 51-3-0 PG 1, SRM 51-1-21 PG 1. FABRICATED NEW CLIP IAW SRM 53-2-0 FIG 1F. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED NEWAug 6, 2003 · N805DH · Doug DC873F · Wing Miscellaneous StructureSDR UPS03841177Seat Track · corrodedINSPECTION TYPE: C1, OBSERVER SEAT TRACK FWD AND AFT IS CORRODED AT MOUNTING POINTS REMOVED AND REPLACED SEAT TRACK IAW DC8 SRM 51-3-0Aug 6, 2003 · N801UP · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR UPS03841175Skin · crackedINSPECTION TYPE: C1, MAP OUT L1 UPPER FWD EXTERNAL DOUBLER FOR ENGINEERING MAPPED OUT DOUBLER, TRIPLER SIZE AND FASTENER PATTERN AND CHECKED THICKNESS .063 AND .080. CUT OUT CRACK IN SKIN IAW DC8 SRM 53-2-0 FIG 15TR 53-155.FABBED -17 DBLR -15 TPLR AND FILLAug 6, 2003 · N801UP · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS03841107Web · crackedINSPECTION TYPE:C2 LEFT UPPER CUSP IS CRACKED AT STA. 1180 LONG.21L NDT VERIFIED CRACKED AREA, CUTOUT DAMAGE BETWEEN STA. 1170 TO 1190, FABRICATED AND INSTALLED REPAIR DOUBLER AND SPLICES I.A.W. SRM. 53-2-5 FIG. 15Aug 5, 2003 · N874UP · Doug DC873F · Fuselage Miscellaneous StructureSDR IXXA0300054OUplock Switch · malfunctionedENROUTE FROM KLAX TO KTOL LANDING GEAR UPLATCH CHECK FAILED. CREW CYCLED GEAR UNTIL GOOD CHECK ACHIEVED. AIRCRAFT LANDED WITHOUT INCIDENT IN KTOL. MAINTENANCE INSPECTED SYSTEM CLEANED AND LUBRICATED RT MLG UPLATCH SYSTEM AND ASSOCIATED COMPONENTS. GEAR OPERATIAug 5, 2003 · N605AL · Doug DC873F · Landing Gear Position and WarningSDR IXXA0300053OProximity Switch · wornWHEN MLG WAS EXTENDED NO LEFT GEAR OR DOOR UNLATCHED LIGHTS NOTED.PERFORMED ABNORMAL PROCEDURE PER ATI COM, NO HELP. AFTER SEVERAL GEAR CYCLES ALL LIGHTS INDICATED NORMALLY. CREW LANDED WITHOUT INCIDENT IN KTOL.UPON INSEPCTION MAINTENANCE NOTED L/H MLG DOWNLATAug 5, 2003 · N603AL · Doug DC873F · Landing Gear Position and WarningSDR DHL2003805534Door Frame · crackedFWD SERVICE DOOR JAMB AFT LWR CORNER CRACKED 0.600 BETWEEN STA 185.000 AND STA 190.000, L-20R TO L-21R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-2-0 FIG 14 SHEET 2 PG 85-86. REMOVED FASTENERS IAW SRM 51-1-21 PG 1, SRM 51-1-20D PG 9. TRIMMED OUT DAMAAug 4, 2003 · N805DH · Doug DC873F · Fuselage Main, StructureSDR DHL2003805589Skin · corrodedLEFT OUTER WING INBD L/E CORRODED BETWEEN STA XFS 572.250 - XFS.603.750. PERFORMED MAJOR REPAIR IAW SRM 57-2-1 FIG 44. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-1 PG 11-12. TRIMMED Aug 4, 2003 · N805DH · Doug DC873F · Wing, Plate/SkinSDR DHL2003805582Plate · corrodedRIGHT INNER WING EXTENDED L/E SLOT UPPER PLATING CORRODED, STA XFS 207.000 AND XFS 220.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-2-1 FIG 38. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS Aug 4, 2003 · N805DH · Doug DC873F · Leading Edge DevicesSDR DHL2003805519Frame · crackedLEFT OUTER WING INBD L/E FORMER CRACKED 0.500 AT XFS 641.250. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. PERFORMED STOP HOLE ON CRACK END IAW SRM 57-2-0 PG 9, 10. FABRICATED ANGLE DOUBLER IAW SRM 57-2-0 PG 9, 10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. Aug 4, 2003 · N805DH · Doug DC873F · Wing, Rib/BulkheadSDR DHL2003805510Cargo Track · wornMAIN CARGO COMPT NR 7 CARGO TRACK LUG WORN (STA 289.000 - 329.000). TRIMMED OUT DAMAGED CARGO TRACK SECTION IAW SRM 53-2-3 PG 49-50. FABRICATED SPLICES (7075-T6 AL0.100, 0.125, 0.160) IAW SRM 53-2-3 PG 49-50. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INAug 4, 2003 · N805DH · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR DHL2003805526Frame · crackedRIGHT WING CTR L/E FORMER 1.000 CRACKED, STA XFS 467.323 (UPPER SECTION). REMOVED FASTENERS IAW SRM 51-1-21 PG 1. STOP DRILLED CRACK IAW SRM 57-2-0 PG 8. FABRICATED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED ANGLE DOUBLER IAW SRM 51-Aug 3, 2003 · N805DH · Doug DC873F · Wing, Rib/BulkheadSDR DHL2003805508Frame · crackedRIGHT WING CTR L/E FRAME 1.000 CRACKED, STA XFS 429.000 (LWR SECTION). REMOVED FASTENERS IAW SRM 51-1-21 PG 1. STOP DRILLED CRACK IAW SRM 57-2-0 PG 9-10. FABRICATED ANGLE DOUBLERS (2024-T3 0.040) 92024-T3 0.050) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED ANDAug 3, 2003 · N805DH · Doug DC873F · Wing SparSDR DHL2003805509Frame · crackedRT WING CTR L/E FRAME 1.000 CRACKED, STA XFS 454.976. 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 0.042) (2024-T3 0.050) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51Aug 3, 2003 · N805DH · Doug DC873F · Wing SparSDR DHL2003805507Frame · crackedRT WING CTR L/E FRAME 0.250 CRACKED, STA XFS 347.750. REMOVED FASTENERS IAW SRM 57-2-0 PG 9-10. FABRICATED ANGLE DOUBLER (2024-T3 0.040) (2024-T3 0.032) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER WITH NEW FAug 3, 2003 · N805DH · Doug DC873F · Wing SparSDR DHL2003805568Skin Panel · delaminatedLEFT WING T/E LWR PANEL EXTERNAL SKIN DELAMINATED (STA XW.5.000 - 90.000). REMOVED AND REPLACED PANEL ASSY ON LEFT WING T/E LWR PART STA XW 5.000 - 90.000 IAW SRM 51-3-0 PG 1.Aug 2, 2003 · N805DH · Doug DC873F · Wing, Plate/SkinSDR DHL2003805542Frame · crackedRIGHT OUTER WING OTBD L/E SHOWS FORMER CRACKED, STA XFS 822.500 (UPPER PART). REMOVED FASTENERS IAW SRM 51-1-21 PG 1. STOP DRILLED CRACK IAW SRM 57-2-0 PG 9. FABRICATED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED ANGLE DOUBLER IAW SRMJul 31, 2003 · N805DH · Doug DC873F · Wing, Rib/BulkheadSDR DHL2003805546Frame · crackedRIGHT WING OTBD L/E FORMER 0.500 CRACKED, STA XFS 747.500. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. PERFORMED STOP HOLE ON CRACK END IAW SRM 57-2-0 PG 9. FABRICATED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED ANGLE DOUBLER IAW SRM 51-1Jul 31, 2003 · N805DH · Doug DC873F · Wing, Rib/BulkheadSDR DHL2003805543Frame · crackedRIGHT WING OUTBD L/E FORMER 0.500 CRACKED AT STA XFS 760.000. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. PERFORMED STOP HOLE ON CRACK END IAW SRM 57-2-0 PG 9. FABRICATED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED ANGLE DOUBLER IAW SRM 5Jul 31, 2003 · N805DH · Doug DC873F · Wing, Rib/Bulkhead
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