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 DHL2003804540Skin · crackedITEM REF. N/R 2153 LH WING T/E UPPER SKIN WITH .5000 CRACK AT STA XW90.000 CORR: STOP DRILLED IAW SRM 57-2-0 FIG 2 FABRICATED DOUBLER ( 7075T6.050) 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 , SRM5Feb 10, 2003 · N804DH · Doug DC873F · Wing, Plate/SkinSDR UPS03840191Fitting · crackedINSPECTION TYPE: C1, RT WING STRINGER 51 END FITTING IS CRACKED OUTBOARD SIDE AT XRS 74. REMOVED AND REPLACED FITTING IAW DWG 3704841 AND SRM 51-1-20D.Feb 10, 2003 · N811UP · Doug DC873F · Wing, Attach FittingsSDR UPS03840182Fitting · crackedINSPECTION TYPE: C1, LT WING STRINGER 51 END FITTING IS CRACKED OUTBOARD OF XRS 74. REMOVED AND REPLACED FITTING IAW DWG 3704841 AND SRM 51-1-20D.Feb 10, 2003 · N811UP · Doug DC873F · Wing Main, Frame StructureSDR DHL2003804889Fitting · corrodedRT WING CTR L/E UPPER PART CORRODED, STA XW 257.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW EODHL 030106, ED-3212. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. REMOVED CORROSION ON RT WING CTR L/E UPPER PART IAW SRM 51-1-8B PG 17-18, FOUND OUT OF LIMITS IAW SRFeb 9, 2003 · N804DH · Doug DC873F · Wing, Attach FittingsSDR DHL2003804555Structure · corrodedRT WING CTR L/E UPPER PART CORRODED, STA. XW 257.000-XFS329.000 PERFORMED MAJOR REPAIR IAW EO DHL 030106 , ED-3212. REMOVED FASTNERS IAW 51-1-21 PG1 REMOVED CORROSION ON RT WING CTR L/E UPPERPART SRM51-18 PAGE 17-18. FOUND OUT OF LIMITS IAW SRM57-2-0 PAGE PGFeb 9, 2003 · N804DH · Doug DC873F · Leading Edge DevicesSDR DHL2003806003Detector1) LOWER CARGO COMPARTMENT SMOKE DETECTION SYSTEM SHOWS CODE AC7444/FALSE ALARM WITH MX INDICATOR. SYSTEM OK LIGHT ON.2) DEFERRED AC7444 IAW MEL 26-10-1)-B), PAGE 6.(ALL OTHER FAULTS ANNUNCIATED BY MX DISPLAY). DMI #11944. 3) REF. DMI #11944 LOWER CARGO COMFeb 9, 2003 · N806DH · Doug DC873F · Smoke DetectionSDR DHL2003804891Vane · damagedRT OUTBOARD SLOT VANE AT STA XOLDI6.224 HOLES ELONGATED (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW EODHL-030105,ED-3210. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. TRIMMED OUT THE DAMAGED SKIN SEGMENT IAW EODHL-030105, ED-3210. FABRICATED AN EXTERNAL REPAIR DFeb 8, 2003 · N804DH · Doug DC873F · Wing Miscellaneous StructureSDR DHL2003804884Vane · elongatedLT WING OUTBOARD VANE SLOT UPPER SKIN HOLE ELONGATED AT XOLDO 6.224 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW EODHL 030110, ED-3221. REMOVED FASTENERS IAW SRM 51-1-21 PG 1, TRIMMED OUT DAMAGED SKIN IAW EODHL 030110, ED-3221, FABRICATED A REPAIR DOUBLER (707Feb 8, 2003 · N804DH · Doug DC873F · Trailing Edge FlapsSDR DHL2003804876Vane · damagedSLOT VANE UPPER SKIN HOLES ELONGATED AT STA XS 247.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW EODHL 03112, ED-3217. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. TRIMMED OUT THE DAMAGED SKIN SEGMENT IAW EO DHL 030112, ED-3217. FABRICATED A REPAIR DOUBLER (70Feb 8, 2003 · N804DH · Doug DC873F · Leading Edge DevicesSDR DHL2003804669Skin · dentedRT ELEVATOR UPPER SKIN SURFACE DENTED ( STA. 44.907 - 50.000) PERFORMED MAJOR REPAIR IAW EO DHL 030102, ED-3219 . REMOVED FASTENERS IAW SRM 51-1-21 PG. 1 REMOVED DAMAGED SKIN SEGMENT IAW EO DHL 030102 , ED-3219. CLEANED TREATED AND PRIMED NEW SKIN INTERIOR Feb 8, 2003 · N804DH · Doug DC873F · Elevator, Plate/SkinSDR DHL2003804548Structure · damagedLT OUTER WING LEADING EDGE SHOWS ELONGATED HOLES, STA XW 485.000 PERFORMED MAJOR REPAIR IAW E.O. DHL030107, ED-3207. REMOVED SKIN SEGMENT IAW EO DHL 030107, ED-3207. FABRICATED DOUBLER (7075T6AL0.063 IAW EO DHL 030107 , ED - 3207. CLEANED , TREATED AND PRFeb 8, 2003 · N804DH · Doug DC873F · Leading Edge DevicesSDR DHL2003804547Frame · crackedSTA 1580 LONG 21 RT HAS A DAMAGED FRAME WITH .750 CRACK DUE TO PALLET LOADING DAMAGE ( MAJOR REPAIR) CORR: PERFORMED MAJOR REPAIR IAW SRM 53-2-0 PG. 20U-2V SHEET 2. REMOVED FASTNERS IAW SRM 51-1-21 PG.1 , SRM51-1-20D PG 21 , CUT OUT DAMAGED FRAME SEGMENT IAW Feb 8, 2003 · N804DH · Doug DC873F · Fuselage Main, FrameSDR UPS03840230Stringer Clip · crackedINSPECTION TYPE: C1, RIGHT WING STRINGER CLIP IS CRACKED AT STRINGER 73 AT XRS 50. REMOVED, FABRICATED, AND REPLACED CLIP IAW SAA SK 811-162.Feb 8, 2003 · N811UP · Doug DC873F · Wing Miscellaneous StructureSDR UPS03840190Fitting · crackedINSPECTION TYPE: C1, RT WING STRINGER 51 END FITTING IS CRACKED AT XRS 74 INBOARD SIDE. REMOVED AND REPLACED FITTING IAW DWG 3704841 AND SRM 51-1-20D.Feb 8, 2003 · N811UP · Doug DC873F · Wing, Attach FittingsSDR DHL2003804894Angle · corrodedVERT STAB AND RT FUSE- ATTACHING ANGLE CORRODED BETWEEN STA 1766.000 - STA 1800.382 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-2-5 PG 44A-44B, FIG 16A. REMOVED CORROSION ON ANGLE IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. CUTFeb 7, 2003 · N804DH · Doug DC873F · Vertical Stabilizer, Attach FittingsSDR DHL2003804892Angle · corrodedCORROSION ON JOINT ANGLE BETWEEN FUSELAGE AND VERTICAL STABILIZER, STA 1766.000, L-3L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-2-5 PG 44A-44B FIG 16A. REMOVED CORROSION ON ANGLE IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. CUFeb 7, 2003 · N804DH · Doug DC873F · Vertical Stabilizer, Attach FittingsSDR DHL2003804879Fairing · delaminatedRT WING NR 709 AFTER WING FUSELAGE FILLET EXTERNAL SKIN DELAMINATED STA 108.000 - STA 120.000. REMOVED DELAMINATED PANEL (RT WING STA 108.000 - 1120.000) IAW SRM 51-3-0 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B, INSTALLED NEW PANEL (FROM USA) IAFeb 7, 2003 · N804DH · Doug DC873F · Aerodynamic FairingsSDR DHL2003804663Panel · delaminatedLT WING NR 718 CENTERWING LOWER PANEL EXTERNAL SKIN DELAMINATED STA 730.000-STA 779.000 R & R NR 718 CENTERWING LOWER PANEL ON LT WING , STA 730.000-STA. 779.000 IAW SRM 51-3-0Feb 7, 2003 · N804DH · Doug DC873F · Fuselage Main, Plate/SkinSDR DHL2003804545Fitting · corrodedCORROSION ON FITTING ATTACHING ACTUATOR TO RUDDER AT STA. ZR61.156. PERFORMED MAJOR REPAIR IAW SRM55-1-0 PG. 1 , REMOVED FITTING IAW SRM 51-1-21 PG. 1 SRM 51-1-20D. PG. 21 REMOVED CORROSION IAW SRM 51-1-8 PGS. 17-18 FOUND OUT OF LIMITS IAW SRM 55-2-0 PAGE 12Feb 7, 2003 · N804DH · Doug DC873F · Rudder ActuatorSDR DHL2003804543Vane · delaminatedITEM REF. N/R: 0100 : LH WING REMOVAL AND INSTALLATION OF #3 FLAP VANE FOR DELAMINATION IN L/E (REF. N/R0097) CORR: R/R #3 FLAP VANE ON LH WING IAW M/M 27-51-14 PG. 201-203 FOR OPS CHECK SEE N/R0607Feb 7, 2003 · N804DH · Doug DC873F · Trailing Edge Flap Control SystemSDR DHL2003804887Fitting · crackedRT WING L/E ZEE PAN CRACKED 2.000 INCHES AT STA XW 223.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG 1. REMOVED FITTING ZEE PAN CRACKED IAW SRM 51-3-0 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING ZEE PAN ON RFeb 6, 2003 · N804DH · Doug DC873F · Wing, Attach FittingsSDR DHL2003804549Fitting · crackedRT ZEE PAN WING ZEE PAN FITTING CRACKED 2.00STA. XW 223.000 CORR: REMOVED FITTING ZEE PAN(CRACKED CONDITION)IAW SRM51-3-0 PG. 1 CLEANED , TREATED, & PRIMED AREA IAW SRM51-1-8B , INSTALLED NEW FITTING ZEE PAN ON RH WING L/E , STA. XW 233.000 IAW SRM51-3-0 PG. 1Feb 6, 2003 · N804DH · Doug DC873F · Wing Miscellaneous StructureSDR DHL2003804535Fitting · crackedITEM:REF. N/R 1558 - AFT CARGO COMPT.- "T" BOLT FITTING CRACKED .5000 , STA. 1240 , L32R CORR:REMEVED DAMAGED FITTING IAW SRM51-1-20D PG. 11 . CLEANED .TREATED , AND PRIMED IAW SRM51-1-8B. INSTALLED NEW FITTING WITH NEW FASTNERS IAW SRM51-1-20D PG. 9Feb 6, 2003 · N804DH · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS03840211Longeron · corrodedINSPECTION TYPE:C3 AFT PIT LONG 34R STA 1420-1440 CORRODED. REMOVED AND REPLACED LONGERON IAW DC8 SRM 51-1-20D AND 51-1-21.Feb 6, 2003 · N805UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS03840201Frame · corrodedINSPECTION TYPE: C3, AFT CARGO PIT AT FS 1000 ABOVE L33R FRAME IS CORRODED. REMOVED FRAME CAP IAW DC8 SRM 51-1-21 & 51-1-20D. LOCATED DRILLED AND DEBURRED NEW FRAME CAP 9755885-7 IAW DC8 SRM 51-1-21 & 51-1-20D. INSTALLED NEW FRAME CAP IAW DC8 SRM 51-1-21 &Feb 6, 2003 · N805UP · Doug DC873F · Fuselage Main, FrameSDR UPS03840197Longeron · dentedINSPECTION TYPE: C3, AFT PIT LONG 35 RT DENTED STA 1377. REMOVED AND REPLACED LONGERON IAW DC8 SRM 51-1-20D AND 51-1-21.Feb 6, 2003 · N805UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS03840170Fitting · crackedINSPECTION TYPE: C3, ALC STA 1490 L34R SPLICE FITTING CRACKED. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-1-20D.Feb 6, 2003 · N805UP · Doug DC873F · Fuselage Main, Attach FittingsSDR UPS03840168Fitting · crackedINSPECTION TYPE: C3, AFT CARGO PIT AT FS 1160 BETWEEN L33R-34R Z-FITTING IS CRACKED. REMOVED CRACKED FITTING. FABRICATED REPAIR DOUBLER & SHIM IAW DC8 SRM 53-2-0. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED NEW FITTING REPAIR DOUBLER AND SHIM IAW DFeb 6, 2003 · N805UP · Doug DC873F · Fuselage Main, Attach FittingsSDR IXXA0300013OControl Valve · failedAFTER TAKEOFF CREW NOTED DOORS NOT LATCHED LIGHT ILLUMINATED. CREW CYCLED LANDING GEAR AND LIGHT REMAINED ILLUMINATED. AFTER APPROX 30 MINUTES LIGHT EXTINGUISHED. AFTER AN UNEVENTFUL LANDING IN BFI MAINTENANCE INSPECTED SYSTEM AND DETERMINED PROBLEM IS INDIFeb 6, 2003 · N606AL · Doug DC873F · Landing Gear Door ActuatorSDR DHL2003804893Fitting · crackedAFT CARGO COMPT FITTING CRACKED 3.000 BETWEEN STA 1040.000 AND 1060.000 NEAR TO L-31R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1 AND FAX BOEING-SEV-LIM-03-00-0003H, DATE: JAN. 20, 2003. REMOVED CRACKED FITTING IAW SRM 51-1-20D PG 21. CLEANEDFeb 5, 2003 · N804DH · Doug DC873F · Fuselage Main, Attach FittingsSDR DHL2003804886Splice · crackedAFT CARGO COMPT SPLICE FITTING CRACKED AT STA 1320.000, L-31L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1 AND FAX BOEING SEU-LIM-03-00002H DATE JUN 20, 2003. REMOVED CRACKED FITTING IAW SRM 51-1-20D PG 21. CLEANED, TREATED AND PRIMED AREA IAWFeb 5, 2003 · N804DH · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL2003804541Fitting · crackedITEM REF. N/R 1308 AFT CARGO COMPT.- FITTING CRACKED @ STA 1320 , L31L (MAJOR REPAIR) CORR: PERFORMED MAJOR REPAIR IAW 53-1-0 PG 1 AND BOEING FAX SEU-LIM-03-0002H DATED JAN 20TH , 2003 REMOVED CRACKED FITTING IAW SRM 51-1-20D PG 21, CLEANED , TREATED AND PRIMEFeb 5, 2003 · N804DH · Doug DC873F · Fuselage Structure (General)SDR DHL2003804539Skin · wornITEM REF. N/R 2389 LH INBD FLAP UPPER SKIN CHAFFING WEAR AT STA. XW120.000 (MAJOR REPAIR) CORR.: PERFORMED MAJOR REPAIR IAW SRM57-1-0 PG. 1 SRM 57-7-1 PG. 2 FIG. 1 REMOVED DAMAGED SKIN IAW SRM51-1-21 PG. 1 , CLEANED , TREATED AND PRIMED AREA IAW SRM 51-1-8B FFeb 5, 2003 · N804DH · Doug DC873F · Trailing Edge Flap Control SystemSDR DHL2003804667Vane · crackedRT WING L/E INBD. VANE SHOWS HOLES ELONGATED , XS247.000 PERFORMED MAJOR REPAIR IAW EO DHL 030104 , ED-3208. REMOVED FASTNERS IAW SRM 51-1-21 PG. 1 TRIMMED OUT DAMAGED SKIN SEGEMENT IAW EA DHL 030104, ED-3208 FABRICATED REPAIR DOUBLER. A FILLER 7075T6 AL 0/0Feb 4, 2003 · N804DH · Doug DC873F · Wing Main, Frame StructureSDR UPS03840207Spar · crackedINSPECTION TYPE: C3, LT WING UPPER FRONT SPAR SHOWS EVIDENCE OF STRESS CORROSION AT APPROX ST A XRS 540. REMOVED CORROSION IAW DC8 SRM 51-1-8, FAB REPAIR STRAP AND FILLER IAW R EO G09022. ALODINED AND PRIMED REPAIR IAW DC8 SRM 51-1-8. INSTALLED REPAIR STRAFeb 4, 2003 · N805UP · Doug DC873F · Wing SparSDR UPS03840185Longeron · corrodedINSPECTION TYPE: C1, STATION 280-300 LONGERON 28L IS CORRODED BEYOND LIMITS. REMOVED LONGERON 28L FROM STATION 265 TO 290, FABRICATED AND INSTALLED LONGERON SECTION, INSTALLED 2 LONGERON SPLICES AND REPLACED 2 BATHTUB FITTINGS IAW DWG 9754913 AND SRM 53-2-2 Feb 4, 2003 · N811UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR DHL2003804882Intercostal · crackedLT WING CTR L/E INTERCOSTAL LWR PART WITH 3.000 INCH CRACK STA XFS 10.250 - 335.250. REMOVED DAMAGED INTERCOSTAL IAW SRM 51-1-21 PG 1. FABRICATED INTERCOSTAL ( 7075-T6AL 0.071) IAW SRM 57-2-0 PG 8-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED Feb 3, 2003 · N804DH · Doug DC873F · Leading Edge DevicesSDR DHL2003804553Skin · worn"A" CARGO DOOR LOWER EXT. SKIN SHOWS WEAR (FS.280.000-340.000) PERFORMED MAJOR REPAIR IAW SRM52-1-0 PG. 1 , SRM51-9-0 FIG 68A, SRM 52-4-1 PG. 2 FIG. 1. REMOVED DAMAGED SKIN FROM "A" CARGO DOOR IAW SRM51-1-21 PG. 1 , SRM51-1-20D PG. 21. FABRICATED NEW SKIN Feb 3, 2003 · N804DH · Doug DC873F · Cargo/Baggage DoorsSDR UPS03840204Fitting · crackedINSPECTION TYPE: C-1, LONGERON SPLICE FITTING CRACKED AT LONGERON 12L BETWEEN STA 300-320. REMOVED, FABRICATED AND REPLACED LONGERON SPLICE FITTING IAW SAA SK 811-748, UPS ENGINEERING FILE NUMBER DC8-53-20283, DWG 4613574 SRM 51-1-20D.Feb 3, 2003 · N811UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS03840203Skin · crackedINSPECTION TYPE: C1, TRIPLER/DOUBLER REPAIR DOES NOT CONFORM TO THE SRM, AT L-2 DOOR LOWER FORWARD CORNER AT STA 1620 AT LONG 20L. REMOVED PREVIOUS REPAIR, NDT VERIFIED NO CRACKS AT EXISTING CUTOUT. FABRICATED AND INSTALLED DOUBLER AND TRIPLER IAW DC8-5310-Feb 3, 2003 · N811UP · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS03840192Skin · damagedINSPECTION TYPE: C1, RADIOGRAPHIC (X-RAY) INSPECTION DETECTED AN INTERNAL DOUBLER REPAIR BETWEEN THE OUTER SKIN AND INTERNAL DOUBLER OF THE L-2 DOOR UPPER CORNER,THE SKIN HAS A CUTOUT APPROX 1.75 X .90. INTERNAL DOUBLER REPAIR IS CONDITION II, AT STA 1660 LONFeb 3, 2003 · N811UP · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS03840186Longeron · corrodedINSPECTION TYPE: C1, STA 1760 LONG 25L IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED AND REPLACED LONGERON SECTION AND INSTALLED SPLICES IAW SRM 53-2-2 FIG 10.Feb 3, 2003 · N811UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS03840184Splice · crackedINSPECTION TYPE: C1, STATION 300 TO 320 LONG 13L SPLICE FITTING IS CRACKED. REMOVED, FABRICATED AND REPLACED FITTING IAW SAA SK 811-747 AND SRM 51-1-20D.Feb 3, 2003 · N811UP · Doug DC873F · Fuselage Main, StructureSDR UPS03840173Intercostal · crackedINSPECTION TYPE:C1 INTERCOSTAL CRACKED ON BOTTOM SIDE AT STA 660 AT LONG 11L. REMOVED, FABRICATED AND INSTALLED REPLACEMENT INTERCOSTAL IAW DWG 5750540 AND SRM 51-1-20D.Feb 3, 2003 · N811UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS03840169Fitting · crackedINSPECTION TYPE: C3, AFT CARGO PIT AT FS 1040-1060 AT L28R SPLICE FITTING IS CRACKED. REMOVED CRACK FITTING. LOCATE NEW FITTING, DRILL EXISTING FASTENER HOLES AND DEBURRED IAW DC8 SRM 51-3-2. REMOVED LOWER FILLET PANEL FOR ACCESS IAW DC8 SRM 51-3-0. INSTAFeb 3, 2003 · N805UP · Doug DC873F · Fuselage Main, Attach FittingsSDR DHL2003804881Skin · crackedLT OUTBOARD FLAP UPPER SKIN SURFACE WITH 1.000 INCH CRACK BETWEEN STA XF 213.000 AND XF 169.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-2-5 PG 3-6. CUT OUT DAMAGED SKIN IAW SRM 57-2-5 PG 3-6. FABRICATED FILLER (2024-T3 0.020) AND SPLICE (2024-T3 0Feb 2, 2003 · N804DH · Doug DC873F · Trailing Edge FlapsSDR DHL2003804666Fitting · crackedAFT CARGO COMPT. SPLICE FITTING CRACKED 3.000 INCH BETWEEN STA. 1040.000-1060.000 , L31R. PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PAGE 1 AND FAX BOEING -SEU-LIM - 03-00003H DATE 20TH 2003. REMOVED CRACKED FITTING IAW SRM 51-1-20D PAGE 21. CLEANED , TREATED ANDFeb 2, 2003 · N804DH · Doug DC873F · Fuselage Main, Attach FittingsSDR DHL2003804558Skin · corrodedLT WING L/E UPPER SKIN CORRODED BETWEEN STA 422.750 AND XFS 427.000 PERFORMED MAJOR REPAIR IAW SRM57-2-1 PAGE 2 FIG. 38 REMOVED CORROSION ON L/E UPPER SKIN IAW SRM51-1-8 PG. 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-0 PG.16. CUT OUT CORRODED AREA IAW SRM 57-2-Feb 2, 2003 · N804DH · Doug DC873F · Wing, Plate/SkinSDR UPS03840205Fitting · crackedINSPECTION TYPE: C3, NR 1 ALT FUEL TANK STR 59 STA 408 END FITTING CRACKED INSIDE PNL 505B. REMOVED CRACKED FITTING PER DC8 SRM 51-1-20D. DRILLED, LOCATED AND DEBURRED NEW END FITTING IAW DC8 SRM 51-1-24. INSTALLED NEW END FITTING IAW DC8 SRM 51-1-20D AND 5Feb 1, 2003 · N805UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS03840199Fitting · crackedINSPECTION TYPE: C3, NR 4 ALT TANK STR 59 END FITTING CRACKED STA XW 428 INSIDE PNL 505B. REMOVED CRACKED FITTING, LOCATED AND DRILLED NEW FITTING IAW DC8 SRM 51-1-24. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D.Feb 1, 2003 · N805UP · Doug DC873F · Fuselage Miscellaneous Structure
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