Douglas DC-8-73

Service difficulty reports · 821

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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 = 'DC873'
  ORDER BY difficulty_date DESC"

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SDR DHL2004803511Rib · crackedLT OUTER WING OB L/E FORMER CRACKED 0.250 (UPPER PART) STA XFS. 835.000 REMOVED FASTENERS IAW SRM 51-1-21 PAGE 1 FABRICATED DOUBLER (2024T3 AL,0.032) IAW SRM 57-2-0 PAGES 9, 10. CLEANED TREATED AND PRIMED AREA AND DOUBLER IAW SRM 51-1-8B. INSTALLED DOUBLER IAMar 24, 2004 · N803DH · Doug DC873 · Wing, Rib/BulkheadSDR DHL2004803506Skin · crackedEXTERNAL FUSELAGE SKIN CRACKED 0.500 AT STA.1747.000,L15 TO L16R. PERFORMED MAJOR REPAIR IAW SRM 53-2-1 FIG. 7 REMOVED FASTENERS IAW SRM 51-1-21 PAGE 1 TRIMMED OUT DAMAGED AREA IAW SRM 53-2-1 PAGES 103, 104 FIG.7, SHEET 3. FABRICATED FILLER (7075T6 0.063) FINMar 24, 2004 · N803DH · Doug DC873 · Fuselage Main, Plate/SkinSDR DHL2004803508Rib · crackedLT OUTER WING OB L/E FORMER CRACKED 0.250 AT XFS 822.000 (UPPER PART). REMOVED FASTENERS IAW SRM 51-1-21 PG.1. FABRICATED DOUBLER (2024-T3 AL 0.032) IAW SRM 57-2-0 PG. 9-10. CLEANED, TREATED AND PRIMED AREA AND DOUBLER IAW SRM 51-1-8B. INSTALLED DOUBLER IAW Mar 24, 2004 · N803DH · Doug DC873 · Wing, Rib/BulkheadSDR DHL2004803507Rib · crackedLT OUTER WING OB. L/E FORMER CRACKED 0.250 AT XFS 760.000 (UPPER PART). REMOVED FASTENERS IAW SRM 51-1-21 PG.1. FABRICATED DOUBLER (2024-T3 AL 0.032) IAW SRM 57-2-0 PG.9-10. CLEANED, TREATED AND PRIMED AREA AND DOUBLER IAW SRM 51-1-8B. INSTALLED DOUBLER IAW Mar 24, 2004 · N803DH · Doug DC873 · Wing, Rib/BulkheadSDR DHL2004803513Structure · crackedRT WING OTBD AILERON L/E PLATING CRACKED 0.250 AROUND STA XA 646.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DC8 SRM 57-1-0 PG 1, DC8 SRM 57-8-01 FIG 4 PG 9. REMOVED CRACKED PLATING IAW DC8 SRM 51-1-21 PG 1. FABRICATED NOSE PLATING (2024-T3 0.032) IAW DCMar 23, 2004 · N803DH · Doug DC873 · AileronsSDR DHL2004803505Skin · damagedRIGHT INBOARD FLAP HAS INTERIM REPAIR ON UPPER FWD PLATING, STA XW 104.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DC8 SRM 57-1-0 PG 1, DC8 SRM 57-7-1 FIG 1. REMOVED PLATING WITH INTERIM REPAIR IAW DC8 SRM 57-1-0 PG 1, DC8 SRM 51-1-21 PG 1. FABRICATED NEMar 23, 2004 · N803DH · Doug DC873 · Trailing Edge FlapsSDR DHL2004803502Floorbeam · wornITEM REF. NR. 1122: MAIN CARGO COMPT. NR 7 FLOORBEAM LUGS WORN, STA. 1120.000. CUT OUT NR 7 FLOORBEAM DAMAGE SECTION IAW SRM 53-2-3 PG.17 FIG. 6D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW CHANNEL AND FLOORBEAM PLUG IAW SRM 51-3-0 PG.1, Mar 20, 2004 · N803DH · Doug DC873 · Fuselage Main, Floor BeamSDR DHL2004803516Frame · crackedVERTICAL STABILIZER L/E FORMER CRACKED 0.500 (LT SIDE) AT ZFS 86.000. PERFORMED STOP HOLE ON CRACK END AND FABRICATED ANGLE DOUBLER (ALCLAD 2024-T3AL 0.032) IAW SRM 55-2-0 PG 7-8. CLEANED, TREATED AND PRIMED AREA AND ANGLE DOUBLER IAW SRM 51-1-8B. INSTALLEDMar 19, 2004 · N803DH · Doug DC873 · Vertical Stabilizer, Spar/RibSDR DHL2004803510Frame · crackedVERTICAL STABILIZER L/E FRAME CRACKED 2.000 AT FS 98.000 (LT SIDE). PERFORMED STOP HOLE ON CRACK END AND FABRICATED ANGLE DOUBLER (ALCLAD 2024-T3 0.032) IAW SRM 55-2-0 PG 7-8. CLEANED, TREATED AND PRIMED AREA AND ANGLE DOUBLER IAW SRM 51-1-8B. INSTALLED ANGMar 19, 2004 · N803DH · Doug DC873 · Vertical Stabilizer, Spar/RibSDR DHL2004803509Frame · crackedVERTICAL STAB L/E FRAME CRACKED 2.000 AT STA 105.000 (RT SIDE). STOP HOLE ON CRACK END AND FABRICATED ANGLE DOUBLER (ALCLAD 2024-T3 0.032) IAW SRM 55-2-0 PG 7-8. CLEANED, TREATED AND PRIMED AREA AND ANGLE DOUBLER IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER IAWMar 19, 2004 · N803DH · Doug DC873 · Vertical Stabilizer, Spar/RibSDR DHL2004803500Seat Track · wornMAIN CARGO COMPT NR 2 FLOOR TRACK PLUG IN POOR CONDITION, STA 774.000. REMOVED PLUG AT STA 774.000 IAW DC8 SRM 51-3-0 PG 1. CLEANED, TREATED AND PRIMED AREA IAW DC8 SRM 51-1-8B. INSTALLED NEW TRACK PLUG IAW DC8 SRM 51-3-0 PG 1-2.Mar 19, 2004 · N803DH · Doug DC873 · Fuselage, Seat/Cargo Attach FittingsSDR DHL2004803501Seat Track · wornMAIN CARGO COMPT NR 6 FLOOR TRACK LUGS WORN, STA 1482.000. CUT OUT DAMAGED SECTION OF NR 6 FLOOR TRACK, STA 1482.000 IAW DC8 SRM 53-2-3 PG 17 FIG 6D. CLEANED, TREATED AND PRIMED AREA IAW DC8 SRM 51-1-8B. INSTALLED NEW CHANNEL AND TRACK PLUG IAW DC8 SRM 51-3Mar 19, 2004 · N803DH · Doug DC873 · Fuselage, Seat/Cargo Attach FittingsSDR DHL2004803504Seat Track · wornMAIN CARGO COMPT NR 6 FLOOR TRACK LUGS WORN STA 1580.000. CUT OUT WORN SECTION OF NR 6 FLOOR TRACK, STA 1580.000 IAW DC8 SRM 53-2-3 PG 17 FIG 6D. CLEANED, TREATED AND PRIMED AREA IAW DC8 SRM 51-1-8B. INSTALLED NEW CHANNEL AND TRACK PLUG IAW DC8 SRM 51-3-0 PMar 19, 2004 · N803DH · Doug DC873 · Fuselage, Seat/Cargo Attach FittingsSDR DHL2004803512Rib · crackedVERTICAL STABILIZER L/E FORMER CRACKED 0.500 STA. XFS 110.000 (LT SIDE). PERFORMED STOP HOLE ON CRACK END AND FABRICATED ANGLE DOUBLER (2024-T3AL 0.032) UAW SRN 55-2-0 PG. 7-8. CLEANED, TREATED AND PRIMED AREA AND ANGLE DOUBLER IAW SRM 51-1-8B. INSTALLED ANGLMar 19, 2004 · N803DH · Doug DC873 · Vertical Stabilizer, Spar/RibSDR DHL2004803503Seat Track · wornMAIN CARGO COMPT NR 6 FLOOR TRACK LUGS WORN, STA 1493.000. CUT OUT DAMAGED SECTION OF NR 6 FLOOR TRACK STA 1493.000 IAW DC8 SRM 53-2-3 FIG 6D, PG 17. CLEANED, TREATED AND PRIMED AREA IAW DC8 SRM 51-1-8B. INSTALLED NEW CHANNEL AND TRACK PLUG IAW DC8 SRM 51-3Mar 18, 2004 · N803DH · Doug DC873 · Fuselage, Seat/Cargo Attach FittingsSDR DHL2004802002Fuel Filter · contaminatedFUEL BYPASS LIGHT ILLUMINATED ON NR 1 ENGINE. PERFORMED ABNORMAL PROCEDURE, LIGHT DID NOT EXTINGUISH. ENGINE PARAMETERS NORMAL. CLEARED DESCENDING THRU 15,000. INSPECTED NR 1 ENGINE FUEL FILTER. FOUND SMALL NON-METALLIC DEBRIS. REMOVED AND REPLACED NR 1 Jan 25, 2004 · N802DH · Doug DC873 · Aircraft Fuel Filter/StrainerSDR DHL2004802001Fuel Filter · contaminatedDURING CRUISE FLIGHT AT FL 350, NR 4 ENGINE FLAMED OUT. SEVERAL ATTEMPTS TO RESTART, THE LAST AT FL 250 AT 300 KIAS WERE UNSUCCESSFUL. REMOVED AND REPLACED NR 4 ENGINE FUEL FILTER DUE TO CONTAMINATION IAW DC-8 M/M 73-11-10. PERFORMED VISUAL INSPECTION OF BOJan 4, 2004 · N802DH · Doug DC873 · Aircraft Fuel Filter/StrainerSDR DHL2003802015Bleed Valve · malfunctionedENGINE NR 3 AND 4 OVER PRESSURE LIGHTS ILLUMINATED AFTER BRAKE RELEASE DURING TAKEOFF ROLL. RTO PERFORMED. CONFERRED WITH MX AFTER LIGHTS EXTINGUISHED AND CONTINUED FLIGHT. NOTED BY MX NO REJECTED T/O INSPECTION REQUIRED DUE TO ZERO AIRSPEED AND MINIMAL BRDec 31, 2003 · N802DH · Doug DC873 · Compressor Bleed ValveSDR DHL2003802564Skin · delaminatedRIGHT WING T/E UPPER PANEL EXTERNAL SKIN DELAMINATED STA XW 5.000 - XW 33.000. REMOVED AND REPLACED RIGHT WING T/E UPPER PANEL (STA XW 5.000 - XW 33.000) IAW SRM 51-3-0 PG 1.Dec 13, 2003 · N802DH · Doug DC873 · Wing, Plate/SkinSDR DHL2003803016Duct · looseIMMEDIATELY AFTER GEAR RETRACTION THERE WAS A CONTINUOUS VIBRATION / SHUDDER AND LOUD NOISE IN THE NOSE AREA. NOISE AND SHUDDER STOPPED AT 500 FEET WHEN PACK WAS TURNED OFF FOR LANDING. RE-SECURED LOOSE ACM DUCT RT EXPANSION SIDE PER DACO M/M 21-55-1. ALSO Dec 13, 2003 · N803DH · Doug DC873 · Air Distribution SystemSDR DHL2003802567Skin · brokenLEFT INBD FLAP UPPER AFT SKIN BROKEN STA XW 2.000 CANT (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW ED EDU38-7, DWG U38-R07. REMOVED DAMAGED SKIN SEGMENT IAW SRM 51-1-21 PG 1. FABRICATED NEW SKIN SEGMENT IAW ED EDU38-7, DWG U38-R07. COUNTERSUNK NEW SKIN SEGMDec 12, 2003 · N802DH · Doug DC873 · Trailing Edge FlapsSDR DHL2003802565Skin · wornLEFT OUTBD FLAP L/E PLATING WORN STA XF 163.000- 213.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW ED EDU38-8, DWG U38-R08. REMOVED DAMAGED PLATING, RUB STRIPS AND RIBS IAW SRM 51-1-21 PG 1, SRM 51-3-0 PG 1, ED EDU38-8, DWG U38-R08. HEAT TREATED IAW SRM 51Dec 12, 2003 · N802DH · Doug DC873 · Trailing Edge FlapsSDR DHL2003802578Mechanism · crackedRIGHT WING INBD AILERON MANUAL REVERSION MECHANISM CRACKED. REMOVED AND REPLACED MANUAL REVERSION MECHANISM AT RIGHT WING INBD AILERON IAW MM 27-11-8 PG 401-404. PERFORMED ADJUSTMENT TEST, GOOD IAW MM 27-10-0 PAGES 510 THRU 515. SEE NR 1456 FOR OPS CHECK.Dec 11, 2003 · N802DH · Doug DC873 · Aileron Control SystemSDR DHL2003802566Fitting · crackedAFT CARGO COMPT FITTING WITH 0.500 CRACK AT STA 1280.000 L-35L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1. REMOVED CRACKED FITTING IAW SRM 51-1-20D PG 21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IN AFT CARGO Dec 10, 2003 · N802DH · Doug DC873 · Fuselage Miscellaneous StructureSDR DHL2003802576Hinge Fitting · crackedNR 6 LEFT AILERON HINGE FITTING CRACK. REMOVED NR 6 LEFT AILERON HINGE FITTING IAW MM 20-16-0 PG 208. REFER TO JC 8-27-11-026 FOR NEW NR 6 LEFT AILERON HINGE FITTING INSTALLATION.Dec 4, 2003 · N802DH · Doug DC873 · AileronsSDR DHL2003802573Skin Panel · delaminatedLEFT WING TO FUSELAGE NR 706 PANEL EXTERNAL SKIN DELAMINATED STA 912.000 - STA 980.000. REMOVED DELAMINATED PANEL IAW SRM 51-3-0 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. APPLIED LPS3 IAW SRM 51-1-8 PG 35-36. INSTALLED NEW PANEL ASSY ON LEFT Dec 4, 2003 · N802DH · Doug DC873 · Aerodynamic FairingsSDR DHL2003802553Skin · delaminatedRIGHT WING T/E UPPER PANEL EXTERNAL SKIN DELAMINATED, STA XW 5.000 - XW 47.000. REMOVED AND REPLACED PANEL ON RIGHT WING T/E STA XW 5.000 - XW 47.000 IAW SRM 51-3-0 PG 1.Dec 4, 2003 · N802DH · Doug DC873 · Wing, Plate/SkinSDR DHL2003802577Hinge Fitting · crackedNR 4 LT AILERON HINGE FITTING CRACK. REMOVED AND REPLACED NR 4 LT AILERON HINGE FITTING IAW MM 20-16-0 PG 208.Dec 3, 2003 · N802DH · Doug DC873 · AileronsSDR DHL2003802571Skin · delaminatedRIGHT WING CENTERWING 723 PANEL LOWER SKIN DELAMINATED STA 742.000. REMOVED AND REPLACED NR 723 PANEL ASSY ON RIGHT WING CENTERWING, STA 742.000 IAW SRM 51-3-0 PG 1.Dec 3, 2003 · N802DH · Doug DC873 · Wing, Plate/SkinSDR DHL2003802563Fitting · crackedAFT CARGO COMPT T-BOLT FITTING CRACKED 0.500 AT STA 1240.000. REMOVED CRACKED T-BOLT FITTING IAW SRM 51-1-20D PG 21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW T-BOLT FITTING IAW SRM 51-1-20D PG 9.Dec 2, 2003 · N802DH · Doug DC873 · Fuselage Miscellaneous StructureSDR DHL2003802568Door · crackedRIGHT WING OTBD SLOT UPPER DOOR CRACKED 3.000. REMOVED AND REPLACED UPPER DOOR ON RIGHT WING OTBD SLOT IAW MM 27-80-2 PG 201-203, SRM 51-3-0 PG 1, SRM 51-3-1 PG 2A. FOR OPS CHECK SEE NR 1456.Dec 2, 2003 · N802DH · Doug DC873 · Leading Edge DevicesSDR DHL2003802572Door Frame · wornWEAR DAMAGE TO THE RIGHT FUSELAGE FWD CTR SECTION LOWER CARGO COMPARTMENT DOOR JAMB AROUND STA 324.000, L-32R (MAJOR REPAIR). REMOVED FASTENERS. TRIMMED OUT THE DAMAGED SKIN. PERFORMED NDT INSPECTION IAW DC8 NDT SPM PART O6,10-01.001. CLEANED, TREATED AND Dec 2, 2003 · N802DH · Doug DC873 · Fuselage Main, StructureSDR DHL2003802555Skin · damagedLT OUTER WING CENTER EXTENDED L/E SLOT LWR PLATING ELONGATED HOLES AROUND STA XFS 526.000 (MAJOR REPAIR). REMOVED FASTENERS. TRIMMED OUT THE DAMAGED SKIN AREA IAW ED EDU38-2 AND DWG U38-R02. PERFORMED NDT INSPECTION IAW DC8 NDT SPM PART 06,10-01-001. CLEANDec 1, 2003 · N802DH · Doug DC873 · Leading Edge DevicesSDR DHL2003802570Skin · corrodedRIGHT MLG DOOR INTERNAL SKIN AFT PART CORRODED, STA 960.000. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 52-2-0 PG 20. TRIMMED OUT CORRODED AREA IAW SRM 52-2-0 PG 18. FABRICATED INTERNAL DOUBLER, FILLER IAW SRM 52-2-0 PG 18. CLEDec 1, 2003 · N802DH · Doug DC873 · Landing Gear DoorsSDR DHL2003802556Skin · damagedRIGHT WING EXTENDED L/E INBD VANE FWD OUTER PLATING ELONGATED HOLES AROUND STA XS 247.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW ED EDU38-3 AND DWG U38-R03. REMOVED FASTENERS, TRIMMED OUT THE DAMAGED SKIN AREA. PERFORMED NDT INSPECTION. CLEANED, TREATENov 30, 2003 · N802DH · Doug DC873 · Leading Edge DevicesSDR DHL2003802554Skin · damagedELONGATED HOLES IN RT WING EXTENDED L/E INBD VANE FORWARD PLATING AROUND STA XILD 7095 (MAJOR REPAIR). REMOVED FASTENERS. TRIMMED OUT THE DAMAGED SKIN AREA. PERFORMED NDT INSPECTION. CLEANED, TREATED AND PRIMED AREA. FABRICATED AND EXTERNAL REPAIR DOUBLERNov 30, 2003 · N802DH · Doug DC873 · Leading Edge DevicesSDR DHL2003802575Panel · crackedRIGHT ELEVATOR UPPER PANEL CRACK 0.250, STA XE 65.156 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 55-1-0 PG 1, SRM 55-4-1 PG 1, 2. REMOVED CRACKED UPPER PANEL FROM RT ELEVATOR STA XE 65.156 IAW SRM 51-1-21 PG 1, SRM 51-1-21A PG 1, 4. CLEANED, TREATED ANDNov 29, 2003 · N802DH · Doug DC873 · Elevator, Plate/SkinSDR DHL2003802574Rib · damagedRIGHT OUTBD STUB WING RIB HOLES ELONGATED STA XOLDO 67.750 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG 1, ATM 201846, DWG 9753297. REMOVED DAMAGED RIB IAW SRM 51-3-0 PG 1, SRM 51-1-21 PG 1, SRM 51-1-20D PG 21. FABRICATED RIB IAW ATM 201846, DWGNov 28, 2003 · N802DH · Doug DC873 · Leading Edge DevicesSDR DHL2003802549Angle · crackedRIGHT OUTBD STUB WING WEB REINFORCING ANGLE CRACK 2.000, STA XS 503.000. REMOVED CRACK REINFORCING ANGLE IAW SRM 51-1-21 PG 1. FABRICATED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER IAW SRM 51-Nov 28, 2003 · N802DH · Doug DC873 · Wing Miscellaneous StructureSDR DHL2003802544Door Frame · damagedFWD PASSENGER DOOR JAMB UPPER FWD CORNER INTERIM REPAIR, STA 25.000 L-9L TO L-10L (MAJOR REPAIR). PERFORMED MAJOR REPAIR, SERVICE REWORK DWG SRO 8530021, DWG 5750776. REMOVED INTERIM REPAIR. TRIMMED OUT AFFECTED AREA IAW SRM 53-2-0 FIG 15, SERVICE REWORK DWNov 27, 2003 · N802DH · Doug DC873 · Fuselage Main, StructureSDR DHL2003802540Door Frame · damagedAFT PASSENGER DOOR JAMB LWR FWD CORNER INTERIM REPAIR, STA 1620.000 L-21L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-2-0 FIG 18, SERVICE REWORK DWG SR08530021, DWG 5750776. REMOVED INTERIM REPAIR IAW SRM 51-1-20D PG 21. FABRICATED DOUBLER AND TRIPLERNov 26, 2003 · N802DH · Doug DC873 · Fuselage Main, StructureSDR DHL2003802538Frame · crackedRIGHT WING L/E LOWER FORMER CRACKED, STA XFS 423.000. REMOVED FASTENERS IAW SRM 51-1-21 PG 21. 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 ANGLE DOUBLER IAW SRM 51-1-Nov 25, 2003 · N802DH · Doug DC873 · Wing, Rib/BulkheadSDR DHL2003802550Bracket · crackedNR 1 ALT TANK FWD BOOSTER PUMP BRACKET CRACKED. REMOVED AND REPLACED CRACKED BRACKET ON NR 1 ALT TANK FWD BOOSTER PUMP IAW SRM 51-1-20D PG 1, SRM 51-1-21 PG 1.Nov 25, 2003 · N802DH · Doug DC873 · Wing Miscellaneous StructureSDR DHL2003802548Bracket · crackedNR 1 ALT TANK AFT BOOSTER PUMP BRACKET CRACKED. REMOVED AND REPLACED CRACKED BRACKET ON NR 1 ALT TANK AFT BOOSTER PUMP IAW SRM 51-1-20D PG 21, 9 AND SRM 51-1-21 PG 1.Nov 25, 2003 · N802DH · Doug DC873 · Wing Miscellaneous StructureSDR DHL2003802560Fitting · crackedUPPER CARGO COMPT FWD FITTING CRACK 1.500, STA 781.500 RBL 20. REMOVED CRACK FITTING FROM UPPER CARGO COMPT STA 781.500 RBL 20 IAW SRM 51-1-20D PG 21. FABRICATED NEW FITTING IAW ATM 201843 AND DWG 4751820. PERFORMED NDT INSPECTION IAW NDT SPM PART 08-00-02/Nov 24, 2003 · N802DH · Doug DC873 · Fuselage Miscellaneous StructureSDR DHL2003802557Fitting · crackedUPPER CARGO COMPT AFT FITTING CRACK 1.000, STA 742.250 RBL 20. REMOVED CRACKED FITTING FROM UPPER CARGO COMPT, STA 742.250 RBL 20 IAW SRM 51-1-20D PG 21. FABRICATED NEW FITTING IAW ATM 201844, DWG 4751820. PERFORMED NDT INSPECTION IAW NDT SPM PART 08-00-02/Nov 24, 2003 · N802DH · Doug DC873 · Fuselage Miscellaneous StructureSDR DHL2003802562Fitting · crackedUPPER CARGO COMPT AFT FITTING CRACK 1.000, STA 702.875 LBL 20. REMOVED CRACK FITTING FROM UPPER CARGO COMPT STA 702.875 LBL 20 IAW SRM 51-1-20D PG 21. FABRICATED NEW FITTING IAW ATM 201843 AND DWG 4751820. PERFORMED NDT INSPECTION IAW NDT SPM PART 08-00-02/Nov 24, 2003 · N802DH · Doug DC873 · Fuselage Miscellaneous StructureSDR DHL2003802561Fitting · crackedUPPER CARGO COMPT AFT FITTING CRACK 1.000, STA 798.000 RBL 20. REMOVED CRACK FITTING FROM UPPER CARGO COMPT STA 798.000 RBL 20 IAW SRM 51-1-20D PG 21. FABRICATED NEW FITTING IAW ATM 201844 AND DWG 4751820. PERFORMED NDT INSPECTION IAW NDT SPM PART 08-00-02/Nov 24, 2003 · N802DH · Doug DC873 · Fuselage Miscellaneous StructureSDR DHL2003802559Fitting · crackedUPPER CARGO COMPT AFT FITTING CRACK 1.000, STA 822.500 RBL 20. REMOVED CRACK FITTING FROM UPPER CARGO COMPT STA 822.500 RBL 20 IAW SRM 51-1-20D PG 21. FABRICATED NEW FITTING IAW ATM 201844 AND DWG 4751820. PERFORMED NDT INSPECTION IAW NDT SPM PART 08-00-02/Nov 24, 2003 · N802DH · Doug DC873 · Fuselage Miscellaneous StructureSDR DHL2003802558Fitting · crackedUPPER CARGO COMPT AFT FITTING CRACK 1.000, STA 822.500 LBL 20. REMOVED CRACK FITTING FROM UPPER CARGO COMPT STA 822.500 LBL 20 IAW SRM 51-1-20D PG 21. FABRICATED NEW FITTING IAW ATM 201843 AND DWG 4751820. PERFORMED NDT INSPECTION IAW NDT SPM PART 08-00-02/Nov 24, 2003 · N802DH · Doug DC873 · Fuselage Miscellaneous Structure
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