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 UPS03840454Pressure Panel · corrodedINSPECTION TYPE: C1, LT NOSE WHEEL WELL TUNNEL, PRESSURE WEB IS CORRODED BEYOND LIMITS OUTBOARD OF HEAT EXCHANGER SUPPORT BRACKET AT STA -68 AT APPROX LBL 64. CUT OUT DAMAGED AREA, NDT VERIFIED NO CRACKS AT CUTOUT. FABRICATED AND INSTALLED FILLER, SPLICE, DApr 15, 2003 · N808UP · Doug DC873F · Fuselage Floor PanelSDR IXXA0300032OWarning Light · illuminatedDURING CLIMB FROM KEWR TO KTOL GEAR RETRACTION DOOR NOT LATCHED LIGHT STAYED ILLUMINATED. CREW USED MAIN GEAR ISOLATION SWITCHES SELECTED TO LT AND LATCH LIGHT WENT OUT. RT SELECTED LATCHED LIGHT STAYED ON AND THE ALTERNATE MAIN LANDING GEAR DOOR LIGHTS REMAApr 15, 2003 · N606AL · Doug DC873F · Landing Gear Position and WarningSDR DHL2003807005Smoke Detector · malfunctionedLOWER CARGO LIGHT ILLUMINATED. RESET LOWER CARGO SMOKE DETECTOR PER SMM 26-15-0.Apr 15, 2003 · N807DH · Doug DC873F · Smoke DetectionSDR DHL2003801031Frame · crackedLT WING CTR L\E FORMER CRACKED 1.000 INCH AT XS 454.000. REMOVED FASTENERS IAW SRM 51-121 PG 1. FABRICATED REINFORCING ANGLE (2024-T3 AL0.040) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED REINFORCING ANGLE WITH NEW FASTENEApr 14, 2003 · N801DH · Doug DC873F · Leading Edge DevicesSDR DHL2003801048Skin · elongatedLT WING CTR L/E UPPER SKIN SURFACE HAS ELONGATED HOLES BETWEEN STA XFS 410.250 AND XOLDI 6.225 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-2-1 FIG 38. FABRICATED DOUBLER (7075-T6 AL0.063) IAW SRM 57-2-1 FIG 38. CLEANED, TREATED AND PRIMED DOUBLER INNEApr 14, 2003 · N801DH · Doug DC873F · Wing, Plate/SkinSDR DHL2003801076Intercostal · crackedFWD CARGO COMPT PRESSURE BULKHEAD INTERCOSTAL CRACKED 1.500 AT STA 640.000, LBL-40. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. STOP DRILLED CRACK AT STA 640.000, LBL-40 IAW SRM 53-2-0 FIG 1B. FABRICATED DOUBLER (2024-T3 AL0.050) IAW SRM 53-2-0 FIG 1B. CLEANEDApr 14, 2003 · N801DH · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS03840636Skin · crackedINSPECTION TYPE: C1, HFEC INSP. OF L-1 DOOR FWD. UPPER CORNER DETECTED A CRACK COMING FROM THE EDGE OF THE CUTOUT EXTENDING FWD AND UP APPROX. 2.375 INCHES AT STA. 25 LONG. 10L REMOVED EXISTING REPAIR, CUTOUT DAMAGED AREA, NDT VERIFIED NO CRACKS AT CUTOUTApr 14, 2003 · N808UP · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS03840614Structure · crackedINSPECTION TYPE: C1, UPPER LT SIDE OF RUDDER LE. AREA HAS A 1.5 INCH CRACK AT ZR 298.1255 3.5 INCHES FWD. OF HINGE LINE STOP DRILLED CRACK, FABRICATED AND INSTALLED DOUBLER,CALCULATED RUDDER BALANCE,CALCULATED IN LIMITS AND UPDATED TAG WITH NEW MOMENT OF Apr 14, 2003 · N808UP · Doug DC873F · Rudder StructureSDR UPS03840613Longeron · crackedINSPECTION TYPE: C1, AFT FUSELAGE INSIDE 60 HOLE LONG. 17R IS CRACKED AT STA. 1776 APPROX REMOVED,FABRICATED AND REPLACED LONGERON IAW SRM. 53-5-0,51-1-20D AND DWG. 5649327Apr 14, 2003 · N808UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS03840480Stringer Clip · crackedINSPECTION TYPE: C1, STATION 1153 AT LONGERON 19R INSIDE HOLE HAS A CRACKED STRINGER CLIP. REMOVED AND REPLACED CLIP IAW DWG. 4750419 AND SRM. 51-1-20DApr 14, 2003 · N808UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS03840453Finger Doubler · corrodedINSPECTION TYPE:C1 STA 960-980 AT LBL 66 FINGER DOUBLER IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED AND REPLACED FINGER DOUBLER IAW DWG 5645332 AND SRM 53-1-0, 53-2-0 FIG 1F, 51-1-21.Apr 14, 2003 · N808UP · Doug DC873F · Fuselage Main, Plate/SkinSDR DHL2003801043Skin · wornFWD PASSENGER DOOR- EXTERNAL SKIN AROUND HANDLE SHOWS WEAR OUT OF LIMITS (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 52-1-0 PG 1. FABRICATED NEW SKIN (2024-T6 AL0.050) IAW SRM 52-3-1 PG 2. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED NEW SKIN Apr 13, 2003 · N801DH · Doug DC873F · Passenger/Crew DoorsSDR UPS03840682Spar · crackedINSPECTION TYPE: C1, HFEC HOLE INSPECTION DETECTED A CRACK ON THE RT WING FORWARD LOWER SPAR BETWEEN STA. XFS 515-XFS 526.76 IN HOLE NR 8 (PG. 15 OF E.O. DC8-5710-14184-D) COINED 10 EA. HOLES IN CONDITION 1, COLD WORKED 1 HOLE IN CONDITION 2 NDT VERIFIED NOApr 13, 2003 · N808UP · Doug DC873F · Wing SparSDR UPS03840676Fitting · crackedINSPECTION TYPE: C1, STA. 45-70 AT APPROX. LBL. 48 AT OVERHEAD IN AC BAY HAS A CRACKED FITTING. REMOVED,FABRICATED AND INSTALLED FITTING IAW DWG. 5890314,AND SRM 51-1-20D,51-3-0Apr 13, 2003 · N808UP · Doug DC873F · Fuselage Main, Attach FittingsSDR UPS03840662Skin · gougedINSPECTION TYPE: C1, LT WING IB. FLAP OB. LOWER SKIN IS GOUGED BEYOND LIMITS APPROX 25 INCHES AFT OF LE. BETWEEN XW101 TO XW 115. REMOVED, FABRICATED AND REPLACED SKIN IAW DWG 5652281,AND SRM. 51-1-21,51-3-0Apr 13, 2003 · N808UP · Doug DC873F · Trailing Edge FlapsSDR UPS03840481Longeron · crackedINSPECTION TYPE: C2, AT STA. 1723 CANTED FRAME, LONG.14L IS CRACKED. CUT OUT DAMAGED LONG. SECTION FABRICATED AND REPLACED LONGERON SECTION I.A.W. SRM. 53-2-03 FIG. 10Apr 13, 2003 · N808UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS03840477Bracket · crackedINSPECTION TYPE: C1, RT LONGERON 6R FWD OF PRESSURE BULKHEAD AT STA 1766 BRACKET IS BROKEN REMOVED,FABRICATED AND REPLACED BRACKET I.A.W. DWG.5773844 AND SRM. 51-1-20DApr 13, 2003 · N808UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS03840448Bulkhead · crackedINSPECTION TYPE: C1, MAIN CABIN AFT PRESSURE BULKHEAD IS CRACKED AT STA 1766 RBL 35 AT APPROX 66 INCHES ABOVE FLOOR LEVEL. CUT OUT DAMAGED AREA, NDT VERIFIED NO CRACKS AT CUTOUT. FABRICATED AND INSTALLED FILLER IAW SRM 53-2-5 FIG 14A, FOUND TO BE WITHIN RANGApr 13, 2003 · N808UP · Doug DC873F · Fuselage Main, BulkheadSDR DHL2003804002Smoke Detector · malfunctionedNR 2 SMOKE DETECTOR INOPERATIVE. MEL 26-6-1 DMI 12559 CAT-C PLACARD INSTALLED. REFER TO DMI 12559. NR 2 SMOKE DETECTOR INOPERATIVE. REMOVED AND REPLACED NR 2 SMOKE DETECTOR AS PER M/M 26-10-5. OPS CHECKED GOOD. THIS CLEARS DMI 12559.Apr 13, 2003 · N804DH · Doug DC873F · Smoke DetectionSDR DHL2003801046Skin · damagedLT WING CTR L/E UPPER SKIN HAS ELONGATED HOLES BETWEEN STA XOLDI 6.225 AND XS 466.651 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG 1 AND SRM 57-3-3 FIG 5. REMOVED DAMAGED CTR L/E UPPER SKIN IAW SRM 51-1-21 PG 1. FABRICATED NEW SKIN (7075-T6 AL0.Apr 12, 2003 · N801DH · Doug DC873F · Wing, Plate/SkinSDR DHL2003801045Skin · damagedLT WING CTR L/E UPPER SKIN SURFACE HAS ELONGATED HOLES BETWEEN STA XFS 379.000 AND 385.250 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-2-1 FIG 3. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. FABRICATED DOUBLER (7075-T6 AL0.063) IAW SRM 57-2- FIG 38. CLEANApr 12, 2003 · N801DH · Doug DC873F · Wing, Plate/SkinSDR DHL2003801055Skin · damagedLT WING CTR L/E UPPER SKIN SURFACE HAS ELONGATED HOLES BETWEEN STA XFS 341.500 AND 347.750 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-2-1 FIG 38. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. FABRICATED DOUBLER (7075-T6 AL0.063) IAW SRM 57-2-1 FIG 38. CLEApr 12, 2003 · N801DH · Doug DC873F · Wing, Plate/SkinSDR DHL2003801044Skin · damagedLT WING CTR L/E UPPER SKIN HOLES ELONGATED, XFS 335.250 TO XFS 335.250 TO XFS 341.500 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-2-1 PG 1. FABRICATED DOUBELR (7075-T6 AL0.063) IAW SRM 57-2-1 FIG 38. CLEANED, TREATED AND PRIMED INNER SURFACE IAW SRM 5Apr 12, 2003 · N801DH · Doug DC873F · Wing, Plate/SkinSDR UPS03840615Stiffener · crackedINSPECTION TYPE: C1, RIGHT WHEEL WELL AT STA. XW 5 AFT T-CAP STRUT FOR TE. IS CRACKED REMOVED,FABRICATED AND REPLACED STIFFENER I.A.W. 9887427,AND SRM. 51-1-20DApr 12, 2003 · N808UP · Doug DC873F · Wing Miscellaneous StructureSDR UPS03840473Fitting · crackedINSPECTION TYPE: C1, RIGHT WHEEL WELL OUTBOARD STA. 940 UPPER BEAM FITTING IS CRACKED AT LONG. 24R REMOVED AND REPLACED FITTING I.A.W. DWG 4619810,AND SRM. 51-1-20DApr 12, 2003 · N808UP · Doug DC873F · Fuselage Main, StructureSDR UPS03840451Skin · crackedINSPECTION TYPE: C1, REMOVE L2 UPPER AFT CORNER STEEL DOUBLER PER EO DC8-5330-12073-H STA 1660 LONG 10L. REMOVED EXISTING REPAIR, NDT VERIFIED NO CRACKS AT EXISTING CUTOUT. FABRICATED DOUBLER AND TRIPLER, REINSTALLED FILLER AND INSTALLED DOUBLER, TRIPLER ANApr 12, 2003 · N808UP · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS03840450Skin · crackedINSPECTION TYPE:C1 LT FUSELAGE SKIN IS DENTED AT STA 300 AT LONG 20L. REWORKED DENT, FOUND WITHIN LIMITS, NDT VERIFIED A .375 INCH CRACK AT DENTED AREA. CUT OUT DAMAGE, NDT VERIFIED NO CRACKS AROUND CUTOUT. FABRICATED AND INSTALLED DOUBLER FILLER AND FINGERApr 12, 2003 · N808UP · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS03840449Skin · crackedINSPECTION TYPE:C1 TWO STOP DRILLED HOLES ON OUTER SKIN AT STA 400 LONG 30R. REMOVED EXISTING REPAIR, CUTOUT DAMAGE, NDT VERIFIED NO CRACKS AT CUTOUT, FABRICATED AND INSTALLED DOUBLER, FILLER AND FINGER DOUBLERS IAW SRM 53-2-1 FIG 7.Apr 12, 2003 · N808UP · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS03840447Rib · crackedINSPECTION TYPE: C1, RT WING L/E UPPER RIB IS CRACKED AT FASTENER END AT XFS 826.750. STOP DRILLED CRACK, NDT VERIFIED STOP DRILL TERMINATES CRACK, FABRICATED AND INSTALLED STACK ANGLE DOUBLER REPAIR IAW SRM 57-2-0 FIG 2.Apr 12, 2003 · N808UP · Doug DC873F · Leading Edge DevicesSDR UPS03840547Frame · crackedINSPECTION TYPE: C3, FWD ACCESSORY COMPARTMENT AT STA 55 & L24L FRAME IS CRACKED. REMOVED DAMAGED FRAME SECTION IAW DC8 SRM 51-1-21. MAT ID 7075-0 .07 1 PO 401846.1 FABBED AND LOCATED FRAME SECTION AND SPLICES IAW DC8 S RM 53-2-0, 51-2-24. ALODINED AND PRIApr 11, 2003 · N819UP · Doug DC873F · Fuselage Main, FrameSDR UPS03840457Frame · crackedINSPECTION TYPE: C3, FWD ACCESSORY COMPARMENT AT STA 55 & L24L FRAME IS CRACKED. REMOVED DAMAGED FRAME SECTION IAW DC8 SRM 51-1-21. HEAT TREATED FRAME SECTION AND SPLICES IAW TPS-1003 REV A. FABBED AND LOCATED FRAME SECTION AND SPLICES IAW DC8 SRM 53-2-24. Apr 11, 2003 · N819UP · Doug DC873F · Fuselage Main, FrameSDR DHL2003801036Skin · crackedLT OUTBOARD AILERON NOSE PLATING WITH TWO CRACKS OF 1.000 AND 0.500 INCH BETWEEN STA XA 674.000 AND 752.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-8-1 PG 9 FIG 4. REMOVED DAMAGED NOSE PLATING SKIN IAW SRM 51-1-21 PG 1. FABRICATED NEW SKIN (2024-TApr 10, 2003 · N801DH · Doug DC873F · AileronsSDR DHL2003801041Structure · crackedLT WING- LT AILERON T/E CRACKED 0.500 INCH BETWEEN STA XA 715.000 AND XA 780.000. REMOVED AILERON T/E (CRACKED) IAW SRM 51-1-21A PG 3-4. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED NEW T/E (2024-T3 AL0.020) IAW SRM 57-8-1 PG 8. CLEANED, TRApr 10, 2003 · N801DH · Doug DC873F · AileronsSDR DHL2003801075Skin · crackedLT WING LT AILERON T/E CRACKED 0.500 INCH BETWEEN STA XA 622.00 AND STA XA 662.000. REMOVED AILERON T/E (CRACKED) IAW SRM 51-1-21A PG 3-4. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED NEW T/E (2024-T3 AL0.020) IAW SRM 57-8-1 PG 8. CLEANED, Apr 10, 2003 · N801DH · Doug DC873F · AileronsSDR UPS03840635Spar · crackedINSPECTION TYPE: C-3, WHEN INSPECTING LWR FRONT SPAR ON RT WING, FOUND PREVIOUSLY REPAIRED HOLES TO EXCEED LIMITATIONS CALLED OUT IN EO. FABBED & INSTALLED RPR BUSHINGS FOR HOLES 3,5,&11. FABBED RPR ANGLES J060232-53/56/58/60.LOCATED, DRILLED, AND STRESApr 10, 2003 · N819UP · Doug DC873F · Wing SparSDR UPS03840424Wire Harness · chafedNUMEROUS INTERMITTENT FIRE WARNING ON NR 4 ENGINE INFLIGHT. PERFORMED ENG FIRE SEVERE DAMAGE CHECKLIST AND SECURED ENGINE. RECEIVED BOTH LIGHT AND FIRE BELL. INSPECTED FIRE WARNING HARNESS AND FOUND RT CORE CHAFED. REPAIRED WIRE PER EOM-2000-16032-A, GROUNDApr 10, 2003 · N814UP · Doug DC873F · Fire Protection System WiringSDR DHL2003801049Frame · crackedNLG W/W DOOR FORMER CRACKED 1.000 STA 93.000 (LT). REMOVED FORMER CRACKED IAW SRM 51-1-21 PG 1. FABRICATED FORMER (2024-T3 AL0.063) IAW SRM 52-5-1 PG 1-4. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED FORMER ON NLG W/W DOOR STA 93.000 IAW SRM 51-1Apr 9, 2003 · N801DH · Doug DC873F · Landing Gear DoorsSDR DHL2003801042Skin · crackedEXTERNAL FUSE CRACKED 1.000 INCH STA 1743.000 - STA 1746.000 BETWEEN L-16R AND L-17R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-2-1 FIG 7. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. CUT OUT DAMAGED AREA IAW SRM 53-2-1 FIG 7. CLEANED, TREATED AND PRIMEDApr 9, 2003 · N801DH · Doug DC873F · Fuselage Main, Plate/SkinSDR DHL2003801035Skin · crackedLT INBOARD STUB WING LWR SURFACE DOUBLER WITH 0.500 INCH CRACK IN STA XFS 260.250 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-2-1A PG 3 FIG 1. REMOVED DAMAGED DOUBLER IAW SRM 51-1-21 PG 1. FABRICATED NEW DOUBLER (7075-T6 AL0.080) IAW SRM 57-2-1A PG 3 Apr 9, 2003 · N801DH · Doug DC873F · Wing, Plate/SkinSDR DHL2003801032Frame · crackedLT WING CTR L/E FORMER WITH 2.000 INCH CRACK AT STA XOLDI 6.225. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. STOP DRILLED 2.000 CRACK ON LT WING CTR L/E IAW SRM 57-2-0 PG 9-10. FABRICATED A DOUBLER ANGLE (STEEL-301 0.25H-0.032) IAW SRM 57-2-0 PG 9-10. CLEANED,Apr 9, 2003 · N801DH · Doug DC873F · Leading Edge DevicesSDR DHL2003801062Frame · crackedLT WING- CTR L/E FORMER CRACKED 0.500 INCH AT XFS 372.750. REMOVED FASTENERS IAW SRM 51-1-21 PG 1 AND SRM 51-1-20D PG 21. STOP DRILLED CRACK IAW SRM 57-2-0 PG 9-10. FABRICATED REINFORCING ANGLE (2024-T3 AL0.032) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED ANDApr 9, 2003 · N801DH · Doug DC873F · Wing SparSDR DHL2003801060Frame · crackedLT WING CTR L/E FORMER CRACKED 0.500 INCH AT XFS 354.000. REMOVED FASTENERS IAW SRM 51-1-21 PG 1 AND SRM 51-1-20D PG 21. STOP DRILLED CRACK IAW SRM 57-2-0 PG 9-00. FABRICATED REINFORCING ANGLE (2024-T3 AL0.032) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND Apr 9, 2003 · N801DH · Doug DC873F · Leading Edge DevicesSDR IXXA0300031OProximity Switch · out of adjustDURING CLIMB FROM KTOL TO KMCO THE CREW RAISED GEAR DOOR AND THE NOT LATCHED LIGHT STAYED ILLUMINATED. GEAR WAS RECYCLED, LEFT LIGHT WENT OUT AND RIGHT LIGHT STAYED ON. MAINTENANCE REMOVED RIGHT MAIN LANDING GEAR DOOR PROXIMITY SWITCH AND BRACKET. FABRICATApr 9, 2003 · N606AL · Doug DC873F · Landing Gear Position and WarningSDR IXXA0300030OWire Harness · dirtyAFTER TAKEOFF IN CLIMBOUT FROM BDL TO EWR, NR 3 EGT REACHED 999 AND WAS ERRATIC. CREW DIVERTED TO TOL DUE TO NO MAINTENANCE IN EWR. CREW ARRIVED IN TOL WITH AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE THERMOCOUPLE WIRING HARNESS FOR CRACKS AND NO DEFECApr 9, 2003 · N605AL · Doug DC873F · Engine EGT/TIT Indicating SystemSDR DHL2003801079Cargo Track · wornMAIN CARGO COMPT. NR 6 TRACK LUGS WORN (STA. 280.000 - STA. 321.000) REMOVED NR 6 TRACK DAMAGED SEGMENT IAW SRM 53-2-3 PG.49-50. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW TRACK SEGMENT IAW SRM 53-2-3 PG. 49-50.Apr 8, 2003 · N801DH · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR DHL2003801037Skin · crackedLT WING- LT INBOARD STUB WING UPPER SKIN CRACKED 5.000 INCHES AT STA XS 250.000. REMOVED DAMAGED LT INBOARD STUB WING UPPER SKIN IAW SRM 51-1-21 PG 1 AND SRM 51-1-20D PG 21. FABRICATED NEW SKIN (7075-T6 AL0.063) IAW SRM 57-7-3 PG 11. CLEANED, TREATED AND PRApr 8, 2003 · N801DH · Doug DC873F · Wing, Plate/SkinSDR DHL2003801054Frame · crackedRT WING CTR L/E FORMER WITH 0.500 INCH CRACK IN STA XFS 466.500. 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 IAW SRM 51-1-Apr 8, 2003 · N801DH · Doug DC873F · Leading Edge DevicesSDR DHL2003801063Frame · crackedRT WING CTR L/E FORMER WITH 0.500 INCH CRACK IN STA XFS 410.250. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. STOP DRILLED CRACK AT STA XFS 410.250 IAW SRM 57-2-0 PG 9-10. FABRICATED DOUBLER ANGLE (2024-T3 AL0.032) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PApr 8, 2003 · N801DH · Doug DC873F · Wing SparSDR DHL2003801057Skin · damagedLT WING CTR L/E UPPER SKIN HOLES ELONGATED BETWEEN XS 484.895 AND XS 520.168 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG 1, SRM 57-3-3 PG 12, FIG 4. REMOVED SKIN WITH HOLES ELONGATED IAW SRM 57-3-3 PG 12, FIG 4 AND SRM 51-1-21 PG 1. FABRICATED Apr 8, 2003 · N801DH · Doug DC873F · Wing, Plate/SkinSDR DHL2003801053Frame · crackedRT WING CTR L/E FORMER WITH 0.500 INCH CRACK IN 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 IAW SRM 51-1-Apr 8, 2003 · N801DH · Doug DC873F · Leading Edge Devices
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