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 DHL2001806520Floor Support · crackedC-CHECK - FWD. CARGO COMPARTMENT FLOOR PANEL SUPPORTING ANGLE CRACKED 3 INCHES, STA. 220.00 L-33 R.REMOVED DAMAGED AREA IAW SRM 53-2-0 PAGE 11. FABRICATED DOUBLER IAW SRM 53-2-0 PAGE 11. INSTALLED DOUBLER IAW SRM 53-2-0 PAGE 11. STATUS-CLOSED.Mar 14, 2001 · N806DH · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA11040Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO LH WING CENTER LE UPPER SKIN AT STA XOLDI 6.225 TO XFS422.75, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSMar 13, 2001 · N602AL · Doug DC873F · Wing, Plate/SkinSDR RRXA11039Spar Cap · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO RH AUX TANK UPPER SPAR CAP AT STA XFS32.5-XFS142, 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-Mar 13, 2001 · N602AL · Doug DC873F · Wing Main, Frame StructureSDR DHL2001806638Diffuser · crackedC-CHECK, LT WING L/E ANTI-ICE DIFFUSER 1 INCH CRACK AT LOWER PART STA AFS 766.500 - XFS 766.950.Mar 13, 2001 · N806DH · Doug DC873F · Airfoil Anti/De-ice SystemSDR DHL2001806600Fitting · crackedC-CHECK - RT REAR PRESSURE BULKHEAD TEE FITTING SHOWS CRACK OF 3 INCH WITH STOP DRILL. FABRICATED REINFORCEMENT ANGLE IAW SRM 51-1-8B FIG 1B. TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED REINFORCEMENT ANGLE IAW SRM 53-2-0 FIG 1B. STATUS-CLOSED.Mar 13, 2001 · N806DH · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL2001806581Diffuser · crackedC-CHECK - LT WING ANTI-ICE DIFFUSER UPPER PART HAS A 1 INCH CRACK AT STA XFS 728.720. PERFORMED STOP DRILL AND FABRICATED REINFORCING ANGLE IAW SRM 57-2-0 FIG 2. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED REINFORCING ANGLE IAW SRM 57-2-0 FIG 2. Mar 13, 2001 · N806DH · Doug DC873F · Airfoil Anti/De-ice SystemSDR DHL2001806575Diffuser · crackedC-CHECK - LT WING L/E ANTI-ICE DIFFUSER HAS A 1/2 INCH CRACK AT LWR PART STA XFS 747.500. PERFORMED STOP HOLE AND FABRICATED DOUBLER IAW SRM 57-2-0 FIG 2. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED DOUBLER IAW SRM 57-2-0 FIG 2. STATUS-CLOSED.Mar 13, 2001 · N806DH · Doug DC873F · Airfoil Anti/De-ice SystemSDR DHL2001806574Diffuser · crackedC-CHECK - LT WING L/E ANTI-ICE DIFFUSER 1 INCH CRACK AT LWR. PART STA XFS 728.750. PERFORMED STOP HOLE AND FABRICATED DOUBLER IAW SRM 57-2-0 FIG 2. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B AND INSTALLED DOUBLER IAW SRM 57-2-0 FIG 2. STATUS-CLOSED.Mar 13, 2001 · N806DH · Doug DC873F · Airfoil Anti/De-ice SystemSDR DHL2001806570Rib · crackedC-CHECK - LT WING LE RIB UPPER PART 1 INCH CRACK AT STA XFS 860. PERFORMED STOP DRILL AND FABRICATED DOUBLERS IAW SRM 57-2-0 FIG 2. CLEANED, TREATED & PRIMED IAW SRM 51-1-8B, PAGES 1-12, 13. INSTALLED DOUBLER IAW SRM 57-2-0 FIG 2. STATUS-CLOSED.Mar 13, 2001 · N806DH · Doug DC873F · Wing, Rib/BulkheadSDR DHL2001806569Rib · crackedC-CHECK - LH WING L/E RIB UPPER PART 1/2 INCH CRACK AT STA XFS 822. PERFORMED STOP DRILL AND FABRICATED DOUBLER IAW SRM 57-2-0 FIG 2. CLEANED, TREATED & PRIMED IAW SRM 51-1-8, PAGES 12, 13. INSTALLED DOUBLER IAW SRM 57-2-0 FIG 2. STATUS-CLOSED.Mar 13, 2001 · N806DH · Doug DC873F · Wing, Rib/BulkheadSDR DHL2001806566Rib · crackedC-CHECK - LT WING LE RIB UPPER PART 1/2 INCH CRACK AT STA XFS 803.730. PERFORMED STOP HOLE AND FABRICATED DOUBLERS IAW SRM 57-2-0 PAGE 9, 10. CLEANED, TREATED & PRIMED IAW SRM 51-1-8B, PAGES 1-12, 13. INSTALLED DOUBLER IAW SRM 57-2-0 PAGE 9/10. STATUS-CLOSEDMar 13, 2001 · N806DH · Doug DC873F · Wing, Rib/BulkheadSDR DHL2001806565Diffuser · crackedC-CHECK - LT WING LE ANTI-ICE DIFFUSER LOWER PART 1-1/2 INCH CRACK AT STA XFS 728. PERFORMED STOP HOLE AND FABRICATED DOUBLER IAW SRM 57-2-0 FIG 2. CLEANED, TREATED & PRIMED IAW SRM 51-1-8B. INSTALLED DOUBLER IAW SRM 57-2-0 FIG 2. STATUS-CLOSED.Mar 13, 2001 · N806DH · Doug DC873F · Airfoil Anti/De-ice SystemSDR DHL2001806564Diffuser · crackedC-CHECK - LT WING LE ANTI-ICE DIFFUSER LOWER PART 1/2 INCH CRACK AT STA XFS 760-250. PERFORMED STOP HOLE AND FABRICATED DOUBLER IAW SRM 57-2-0 FIG 2. CLEANED, TREATED & PRIMED IAW SRM 51-1-8B. INSTALLED DOUBLER IAW SRM 57-2-0 FIG 2. STATUS-CLOSED.Mar 13, 2001 · N806DH · Doug DC873F · Airfoil Anti/De-ice SystemSDR DHL2001806563Rib · crackedC-CHECK - LH WING L/E RIB UPPER PART 1 INCH CRACK AT STA XFS 766.500. PERFORMED STOP HOLE AND FABRICATED DOUBLER IAW SRM 57-2-0 PAGES 9. 10. CLEANED, TREATED & PRIMED IAW SRM 51-1-8B PAGES 1-12, 13. INSTALLED DOUBLER IAW SRM 57-2-0 PAGES 9, 10. STATUS-CLOSMar 13, 2001 · N806DH · Doug DC873F · Wing, Rib/BulkheadSDR DHL2001806562Diffuser · crackedC-CHECK - LT WING LE ANTI-ICE DIFFUSERS 1-1/2 INCH CRACK AT UPPER PART STA XFS 745.950. PERFORMED STOP HOLE AND FABRICATED DOUBLER IAW SRM 57-2-0 FIG 2. CLEANED, TREATED & PRIMED IAW SRM 51-1-8B PAGES 1-12, 13. INSTALLED DOUBLER IAW SRM 57-2-0 FIG 2. STATUMar 13, 2001 · N806DH · Doug DC873F · Airfoil Anti/De-ice SystemSDR DHL2001806561Diffuser · crackedC-CHECK - LT WING LE ANTI-ICE DIFFUSER LWR PART 1/2 INCH CRACK AT STA XFS 766.250. PERFORMED STOP HOLE AND FABRICATED DOUBLER IAW SRM 57-2-0 FIG 2. CLEANED, TREATED & PRIMED IAW SRM 51-1-8B PAGES 1-12, 13. INSTALLED DOUBLER IAW SRM 57-2-0 FIG 2. STATUS-CLOMar 13, 2001 · N806DH · Doug DC873F · Airfoil Anti/De-ice SystemSDR DHL2001806557Diffuser · crackedC-CHECK - LT WING LE ANTI-ICE DIFFUSER, 1 INCH CRACK AT UPPER PART STA XFS 766.500 - XFS 766.950. PERFORMED STOP HOLE. AND FABRICATED DOUBLER IAW SRM 57-2-0 FIG 2. CLEANED, TREATED & PRIMED IAW SRM 51-1-8B. INSTALLED DOUBLER IAW SRM 57-2-0 FIG 2. STATUS-Mar 13, 2001 · N806DH · Doug DC873F · Airfoil Anti/De-ice SystemSDR DHL2001806555Rib · crackedC-CHECK - WING LE RIB UPPER PART 1 INCH CRACK AT STA 803.730. PERFORMED STOP HOLE AND FABRICATED DOUBLERS IAW SRM 57-2-0 P1, 9, 10. CLEANED, TREATED & PRIMED IAW SRM 51-1-8B PAGES 1-12, 13. INSTALLED DOUBLERS IAW SRM 57-2-0 PAGE 10. STATUS-CLOSEDMar 13, 2001 · N806DH · Doug DC873F · Wing, Rib/BulkheadSDR DHL2001806549Floor Support · crackedC-CHECKED - MAIN CARGO 2 INCH CRACK IN CENTRAL WING FLOOR D STA 866.00. CUT OUT DAMAGED AREA OF FLOOR PANEL D AT STA 866.00, FABRICATED FILLER & DOUBLER ANGLES IAW SRM 53-2-3 PAGE 39, 40. CLEANED, TREATED, & PRIMED IAW SRM 51-1-8B. INSTALLED FILLER & DOUBMar 13, 2001 · N806DH · Doug DC873F · Cargo CompartmentsSDR DHL2001806545Angle · corrodedC-CHECK - AFT FUSELAGE EXTERIOR-UPPER PART VERTICAL STABILIZER TO FUSELAGE ANGLE SHOWS CORROSION, STA FS 000 RT SIDE.CORRECTIVE ACTION - REMOVED LEVEL I CORROSION FROM AFT FUSELAGE EXTERIOR UPPER PART VERTICAL STABILIZER TO FUSELAGE ANGLE STA FS 000 RH IAW SRMMar 13, 2001 · N806DH · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL2001806503Fitting · crackedRT HORIZONTAL STABILIZER, LE INTERIOR LWR FITTING CRACKED 1 IN AT STA XFS 60.REMOVED CRACKED FITTING AT STA. XFS.60 OF RT HORIZONTAL STAB LE INTERIOR IAW SRM 51-1-20D PAGE 21. CLEANED, TREATED, & PRIMED AREA IAW SRM 51-1-8 PAGE 12-13. INSTALLED NEW FITTING IMar 13, 2001 · N806DH · Doug DC873F · Horizontal Stabilizer StructureSDR RRXA010019Inu · failedNR 1 INS FAILED WENT ATT MODE. TRANSFERRED TO DMI LIST AS CONTROL D-9272201-1175 CAT: D MEL 3420 ATA 3410 DUE DATE 11JUL01 PLACARD INSTALLED. REMOVED AND REPLACED NR 1 INU PERFORMED OPERATIONAL CHECK IAW SUPPLEMENTAL MANUAL CHECK GOOD. THIS CLEARS DMI D9Mar 13, 2001 · N831AL · Doug DC873F · Inertial Guidance SystemSDR DHL2001806603Skin · crackedC-CHECKED - LT WING L/E LWR SKIN SURFACE CRACKED 1/2 INCH AT STA XFS 585. CUT OUT DAMAGED AREA OF LT WING L/E LWR SKIN XFS 585 AND FABRICATED FILLER AND DOUBLER IAW SRM 57-2-0 FIG 2. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED FILLER AND DOUBLEMar 12, 2001 · N806DH · Doug DC873F · Trailing Edge FlapsSDR DHL2001806573Rib · crackedC-CHECK - LT WING L/E RIB UPPER PART 1/2 INCH CRACK AT STA XFS 660. PERFORMED STOP DRILL AND FAVRICATE REINFORCING ANGLE IAW SRM 53-2-0 FIG 2. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED REINFORCING ANGLE IAW SRM 57-2-0 FIG 2. STATUS-CLOSED.Mar 12, 2001 · N806DH · Doug DC873F · Wing, Rib/BulkheadSDR DHL2001806568Rib · crackedC-CHECK - LT WING LE RIB UPPER PART 1 INCH CRACK AT STA XFS 822.500. PERFORMED STOP DRILL AND FABRICATED DOUBLER IAW SRM 57-2-0 FIG 2. CLEANED, TREATED & PRIMED IAW SRM 51-1-8B, PAGES 1-12, 13. INSTALLED DOUBLER IAW SRM 57-2-0 FIG 2. STATUS-CLOSED.Mar 12, 2001 · N806DH · Doug DC873F · Wing, Rib/BulkheadSDR DHL2001806558Rib · crackedC-CHECK - LT WING LE RIB 1 INCH CRACK AT UPPER PART STA XFS 822.500. PERFORMED STOP DRILL AND FABRICATED DOUBLER IAW SRM 57-2-0 FIG 2. CLEANED, TREATED & PRIMED IAW SRM 51-1-8B PAGES 1-12, 13. INSTALLED DOUBLER IAW SRM 57-2-0 FIG 2. STATUS-CLOSED.Mar 12, 2001 · N806DH · Doug DC873F · Wing, Rib/BulkheadSDR DHL2001806547Floor Support · crackedC-CHECK - MAIN CARGO 1 INCH CRACK IN CENTRAL WING FLOOR ''D'' STA 878.000. CUT OUT DAMAGED AREA OF FLOOR PANEL ''D'' AT STA 878 FABRICATED FILLER AND DOUBLER IAW SRM 53-2-3 PAGE 39/40 CLEANED, TREATED & PRIMED IAW SRM 51-1-8B PAGE 1-12. INSTALLED FILLER ANDMar 12, 2001 · N806DH · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL2001806535Floor Support · crackedC-CHECK - FWD CARGO COMPART. FLOOR SUPPORT ANGLE CRACKED 1 INCH AT STA 600. L-35LT. PERFORMED STOP DRILL IAW SRM 53-1-0 FIG 1B. FABRICATED REINFORCING ANGLE IAW SRM 53-2-0 FIG 1B. INSTALLED REINFORCING ANGLE IAW SRM 53-2-0 FIG 1B. STATUS-CLOSED.Mar 12, 2001 · N806DH · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA11023Door Frame · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO RT WW DOOR FRAME AT STA 883, 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 53-2-0 FIG2B, DWG 5616306, DC-8 SRM 53-1-01Mar 11, 2001 · N602AL · Doug DC873F · Fuselage Main, StructureSDR DHL2001806637Rib · crackedC-CHECK, LT WING L/E RIB LWR PORT .5 INCH CRACK AT STA XFS 642 - 250.Mar 11, 2001 · N806DH · Doug DC873F · Wing, Rib/BulkheadSDR DHL2001806609Rib · crackedC-CHECK - LT WING L/E RIB UPPER PART HAS A 1/2 INCH CRACK AT STA XFS 747.000. PERFORMED STOP DRILL AND FABRICATED REINFORCING ANGLE IAW SRM 57-2-0 FIG 2 CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INBSTALLED REINFORCING ANGLE IAW SRM 57-2-0 FIG 2. STATMar 11, 2001 · N806DH · Doug DC873F · Wing, Rib/BulkheadSDR DHL2001806580Rib · crackedC-CHECK - LT WING L/E RIB UPPER PART HAS A 1/2 INCH CRACK AT STA XFS 041.950.PERFORMED STOP DRILL AND FABRICATED DOUBLER IAW SRM 57-2-0 FIG 2. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED REINFORCING ANGLE IAW SRM 57-2-0 FIG 2. STATUS-CLOSED.Mar 11, 2001 · N806DH · Doug DC873F · Wing, Rib/BulkheadSDR DHL2001806579Rib · crackedC-CHECK - LT WING L/E RIB UPPER PART HAS A 1 INCH CRACK AT STA XFS 841.250. PERFORMED STOP DRILL AND FABRICATED REINFORCING ANGLE IAW SRM 57-2-0 FIG 2. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED REINFORCING ANGLE IAW SRM 57-2-0 FIG 2. STATUS-CMar 11, 2001 · N806DH · Doug DC873F · Wing, Rib/BulkheadSDR DHL2001806578Rib · crackedC-CHECK - LT WING L/E RIB UPPER PART HAS A 1 INCH CRACK AT STA XFS 822.950. PERFORMED STOP DRILL AND FABRICATED REINFORCING ANGLE IAW SRM 57-2-0 FIG 2. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED REINFORCING ANGLE IAW SRM 57-2-0 FIG 2. STATUS-CMar 11, 2001 · N806DH · Doug DC873F · Wing, Rib/BulkheadSDR DHL2001806577Rib · crackedC-CHECK - LT WING L/E RIB UPPER PART HAS A 1/2 INCH CRACK AT STA XFS 785.250. PERFORMED STOP DRILL AND FABRICATED REINFORCING ANGLE IAW SRM 57-2-0 FIG 2. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED REINFORCING ANGLE IAW SRM 57-2-0 FIG 2. STATUSMar 11, 2001 · N806DH · Doug DC873F · Wing StructureSDR DHL2001806576Rib · crackedC-CHECK, LT WING L/E RIB LOWER PART HAS A 1/2 INCH CRACK AT STA XFS 803.750.PERFORMED STOP DRILL AND FABRICATED REINFORCING ANGLE IAW SRM 57-2-0 FIG 2. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED REINFORCING ANGLE IAW SRM 57-2-0 FIG 2. STATUS-CMar 11, 2001 · N806DH · Doug DC873F · Wing, Rib/BulkheadSDR DHL2001806567Rib · crackedC-CHECK - LT WING LE RIB UPPER PART 1 INCH CRACK AT STA XFS 785.800. PERFORMED STOP DRILL AND FABRICATED REINFORCING ANGLE IAW SRM 57-2-0 FIG 2. CLEANED, TREATED & PRIMED IAW SRM 51-1-8B, AND INSTALLED REINFORCING ANGLE IAW SRM 57-2-0 FIG 2. STATUS-CLOSED.Mar 11, 2001 · N806DH · Doug DC873F · Wing, Rib/BulkheadSDR DHL2001806556Rib · crackedC-CHECK - LT WING LE RIB UPPER PART 1 INCH CRACK AT STA XFS 785.800. PERFORMED STOP DRILL AND FABRICATED REINFORCING ANGLE IAW SRM 57-2-0 FIG 2. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B AND INSTALLED REINFORCING ANGLE IAW SRM 57-2-0 FIG2. STATUS-CLOSEDMar 11, 2001 · N806DH · Doug DC873F · Wing, Rib/BulkheadSDR UPS01835408Floorboard · corrodedINSPECTION TYPE:C2 FLOORBOARD STA 1040 BETWEEN RAILS E & F CORRODED REPAIRED AREA IAW DC8 SRM 53-2-3Mar 11, 2001 · N808UP · Doug DC873F · Fuselage Floor PanelSDR RRXA010018Tire · blownON LANDING, TOWER REPORTED SMOKE OF RIGHT MLG NR 8 TIRE BLEW, NR 3 TIRE DAMAGED UPON LANDING. NO SECONDARY CAUTION LIGHT OR ANTI SKID LIGHT ILLUMINATED. TRANSFERRED TO DMI LIST AS CONTROL C-9272181-1171 CAT: C MEL 3101 ATA 3245 DUE DATE 23MAR01 PLACARD INSTAMar 11, 2001 · N831AL · Doug DC873F · TireSDR RRXA11031Longeron · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO LONGERON AT STA 35-55 AND L26R, 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, 51-Mar 10, 2001 · N602AL · Doug DC873F · Fuselage Main, StructureSDR DHL2001806536Floor Support · crackedC-CHECK - FWD CARGO COMPARTMENT LT FLOOR SUPPORT ANGLE CRACKED 3 INCH AT STA 520.00 L-33L TO L34L. STOP DRILLED AND FABRICATED DOUBLER AND INSTALLED IAW SRM 53-2-5 PAGE 6M. STATUS-CLOSED.Mar 10, 2001 · N806DH · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL2001806533Angle · crackedC-CHECK - VERT. STAB. LE INNER RIB REINFORCING ANGLE CRACKED 1/2 INCH ZF 86.000 RT. REMOVED CRACK REINFORCING ANGLE IAW SRM 51-1-21 PAGE 1. FABRICATED ANGLE IAW SRM 55-1-1 FIG 2. CLEANED, TREATED AND PRIMED IAW SRM 5-1-8B. INSTALLED ANGLE IAW SRM 51-1-21 PAGMar 10, 2001 · N806DH · Doug DC873F · Vertical StabilizerSDR DHL2001806506Floor Support · crackedC-CHECK - FWD CARGO COMPARTMENT FLOOR SUPPORT ANGLE CRACKED 1 INCH AT STA. 220 L-35 LT CORRECTIVE ACTION: PERFORMED STOP HOLE. FABRICATED REINFORCING ANGLE AND INSTALLED IAW SRM 53-2-3 FIG 10. STATUS-CLOSED.Mar 10, 2001 · N806DH · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA010017Engine · failedAFTER 1 HR INFLT NOTICED N2 DROPPED +0 2 PERCENT N1 EGT FUEL FLOW NORMAL QTS CKD OTHER GAUGES OIL QTY AT 6 QTS AND DROPPING OIL PRESS 40 PSI, RETARDED THE THROTTLE AND PERFORMED A PRECAUTIONARY SHUTDOWN AS PER QRH. WHEN OIL QTY DROP TO 20 PRESS BETWEEN 20-25 Mar 10, 2001 · N870TV · Doug DC873F · Engine (Turbine/Turboprop)SDR DHL2001806607Control Valve · misinstalledC-CHECK - RT FWD TANK, LEVEL CONTROL VALVE ELECTRICAL PLUG IMPROPERLY SAFETIED. SAFETIED PROPERLY LEVEL CONTROL VALVE ELECT PLUG (RT FWD TANK) IAW MM 20-18-0 PAGE 201-215. STATUS-CLOSED.Mar 9, 2001 · N806DH · Doug DC873F · Fuel Transfer ValveSDR DHL2001806590Floor Panel · crackedC-CHECK - COCKPIT - 682 FLOOR PANEL SUPPORT ANGLES LWR EDGE CRACKED 1/2 INCH AT STA -12.000. PERFORMED STOP HOLE IAW SRM 53-2-0 FIG 1B. FABRICATED REINFORCING ANGLE IAW SRM 53-2-0 FIG 1B. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED REINFORCING ANMar 9, 2001 · N806DH · Doug DC873F · Fuselage Floor PanelSDR DHL2001806544Structure · crackedC-CHECK 0- TAIL CONE INTERIOR PART, SIDE, RT AT STA 1920, SHOWS 1/2 INCH CRACK AND RIVETS LOOSE IN ELEVATOR TORQUE TUBE PROTECTOR. REMOVED FASTENERS IAW SRM 51-1-21 PAGE 1. PERFORMED STOP HOLE IAW SRM 53-2-0 FIG 1B. FABRICATED DOUBLER IAW SRM 53-2-0 FIG 1Mar 9, 2001 · N806DH · Doug DC873F · Elevator StructureSDR DHL2001806543Floor Panel · crackedC-CHECKED - FLIGHT COMPARTMENT #676B FLOOR PANEL SKIN CRACKED. PERFORMED STOP HOLE IAW SRM 53-2-3 FIG 10. FABRICATED DOUBLER IAW SRM 53-2-3 FIG 10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED DOUBLER USING NEW FASTNERS IAW SRM 51-1-21 PAGE 1. Mar 9, 2001 · N806DH · Doug DC873F · Fuselage Floor PanelSDR DHL2001806542Floor Panel · crackedC-CHECK - FLIGHT COMPARTMENT 676C FLOOR PANEL SKIN CRACKED. PERFORMED STOP HOLE IAW SRM 53-2-3 FIG 10. FABRICATED DOUBLER IAW SRM 53-2-3 FIG 10, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED DOUBLER IAW SRM 53-2-3 FIG 10. STATUS-CLOSED.Mar 9, 2001 · N806DH · Doug DC873F · Fuselage Floor Panel
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