Douglas DC-8-71F

Service difficulty reports · 8,938

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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 = 'DC871F'
  ORDER BY difficulty_date DESC"

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SDR UPS06847673Finger Doubler · corrodedFOUND CORROSION UNDER FINGER DOUBLER FLT DECK SUBFLOOR STA -67 TO -80 RBL-20. FABRICATED AND INSTALLED FINGER DOUBLER FLT DECK SUB FLOOR STA -67 TO -80 RBL-20 IAW SRM 53-03-01, AND SRM 51-1-20D.Aug 1, 2006 · N700UP · Doug DC871F · Fuselage Main, StructureSDR UPS06847655Bulkhead · crackedINSPECTION TYPE:C2 AFT PRESSURE BULKHEAD CRACKED AT STA 1766 RBL 34 L11R CUT OUT DAMAGED AREA AT AFT PRESS BULKHEAD IAW SRM 53-2-5 FIG 14A. FABRICATED AND INSTALLED -9, -11,-13 AND -19 FILLERS,-15 AND -17 DOUBLERS AT STA 1766 RBL 34 L11R IAW SRM 53-2-5 FIAug 1, 2006 · N700UP · Doug DC871F · Fuselage Main, BulkheadSDR UPS06847634Finger Doubler · corrodedINSPECTION TYPE:C2 PILLOWED SKIN, POPPED RIVETS UNDER FINGER DOUBLER FLT DECK SUB-FLOOR STA-52 TO-67 RBL 20. REMOVED CORRODED FINGER DOUBLER, FABRICATED AND INSTALLED REPLACEMENT FINGER DOUBLER STA-52 TO-67 RBL20 IAW SRM 53-3-01 FIG 7, SRM 51-01- 08, SRM 51-0Aug 1, 2006 · N700UP · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS06847811Pressure Panel · corrodedINSPECTION TYPE:C2 CORROSION UNDER REPAIR STRAP AND UNDER DOUBLER ON RT W/W STA 900-904 RBL 50-56. REPAIRED DOUBLER AND STRAP AT STA 900-908, RBL 50-56 IAW SAA EA 008-5320-01-A0338, UPS EO DC8-5330-24908-A, BAC MSG 1-216936088-2, 1-216936088-4, 1-216936088-5,Jul 31, 2006 · N700UP · Doug DC871F · Fuselage Main, BulkheadSDR UPS06847653Support Angle · crackedINSPECTION TYPE:C2, LT WING IB FLAP STA 3 FLAP TRACK SUPPORT ANGLE CRACKED. REMOVED, FABRICATED AND INSTALLED ANGLE IAW SRM 51-1-20D, 51-1-21, 51-2-00, DWG 5643117.Jul 31, 2006 · N700UP · Doug DC871F · Wing, Attach FittingsSDR UPS06847623Skin · crackedINSPECTION TYPE:C2 FUSELAGE EXTERIOR SKIN CRACKED AT STA 1726 L17R. CUT OUT DAMAGED AREA AT STA 1726 L17R IAW SRM 53-02-00 FIG 7. FABRICATED AND INSTALLED REPAIR DOUBLER, FILLERS, AND FINGER DOUBLER AT STA 1726 L17R IAW SRM 51-02-00 FIG 7 AND SRM 51-1-20D.Jul 28, 2006 · N700UP · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS06847622Skin · crackedINSPECTION TYPE:C2 FUSELAGE EXTERIOR SKIN CRACKED AT STA 1726 L17L. CUT OUT DAMAGED AREA AT STA 1726 L17L IAW SRM 53-02-01-0. FABRICATED AND INSTALLED REPAIR DOUBLER AND FINGER DOUBLER AT STA 1726 L17L IAW SRM 53-02-01-0 FIG 7 AND SRM 51-1-20D.Jul 28, 2006 · N700UP · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS06847828Skin · dentedINSPECTION TYPE: C2 REMOVE STEEL DOUBLER FROM LWR FWD CORNER OF MAIN CARGO DOOR AND REPAIR IAW SRO8530027. REMOVED STEEL DOUBLERS, REMOVED AND REPLACED SKIN FROM FS 70-210, L21L-L31L, DUE TO EXISTING CUTOUT IS OUT OF TANGENT AREA. REINSTALLED DOUBLER. IAW SRMJul 25, 2006 · N700UP · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS06847343Hose · defectiveON CLIMBOUT HYDRAULIC QUANTITY DECREASED. AOM PROCEDURE WAS COMPLIED WITH AND RESERVOIR WAS NOT EMPTY. FOUND LT MAIN GEAR DOWNLOCK BUNGEE CYLINDER PRESSURE HOSE BROKEN. REPLACED WITH TEMPORARY HOSE REFERENCE GMM 3-24-1- D329494 ASSIGNED. R&R PRESS LINE WITHJul 18, 2006 · N744UP · Doug DC871F · Hydraulic System, MainSDR UPS06847338Wheel · corrodedCORROSION ON NR 5 MAIN LANDING GEAR AXLE - INNER WHEEL BEARING. CHROME W/SOME PITTING. R/R NR 5 MLG WHEEL & TIRE ASSY. IAW MM REF 32-40-01-2. BLENDED AREA APPLIED FR PRIMER TO BLENDED AREA; REINSPECT EVERY 70 DAYS PERM. REPAIR AT OR BEFORE C CK.Jul 16, 2006 · N744UP · Doug DC871F · Wheel/Ski/FloatSDR IXXA060457OTransmitter · failedDURING CRUISE FROM KTOL TO CYJT, CREW NOTICED THE HYDRAULIC PRESSURE DROPPED TO 2000 POUNDS OF PRESSURE. THE CREW ELECTED TO RETURN TO KTOL AND SAFELY LANDED. MAINTENANCE REPLACED THE HYDRAULIC PRESSURE TRANSMITTER. THE HYDRAULIC SYSTEM OPERATIONAL CHECK WAJul 15, 2006 · N825BX · Doug DC871F · Hydraulic Pressure IndicatorSDR UPS06847314Coalescer Bag · odorSTRANGE ODOR IN C/P. REMOVED AND REPLACED WATER SEPARATOR BAG ON LT & RT WATER SEPARATOR IAW DC8 MM 21-55-03-2. LEAK & OPS CHECK LT & RT WATER SEPARATORS IAW 21-00-00. LT CHECKS GOOD. RT WATER SEPARATOR LEAKS. REMOVED AND REPLACED O-RING IAW 21-55-03-2. Jul 11, 2006 · N715UP · Doug DC871F · Humidity Control SystemSDR UPS06847306Battery Pack · dischargedEMERGENCY LIGHTS WOULD NOT ILLUMINATE DURING TEST. REMOVED AND REPLACED EMERGENCY LIGHTS BATTERY PACK IAW AMM 33-50-01-2. OPS CHK GOOD.Jul 10, 2006 · N701UP · Doug DC871F · Emergency LightingSDR UPS06847301Fuse · blownINSPECTION TYPE:N/A SMOKE AND ELECTRICAL ODOR CAME FROM BEHIND ENGINEERS PANEL. ALL BACKGROUND LIGHTS ON F/E PANEL WENT OUT. REPLACED BLOWN FUSE (5AMP) OP'S CHECK NORMAL ON BACKGROUND LIGHTS PER WDM 33.Jul 7, 2006 · N750UP · Doug DC871F · Instrument PanelSDR UPS06847293Fuse · blownSMOKE & ELECTRICAL ODOR CAME FROM BEHIND ENGINEERS PANEL. ALL BACK GROUND LIGHTS ON F/E PANEL WENT OUT. REPLACED BLOWN FUSE-5 AMP. OP'S CHECK NORMAL ON BACKGROUND LIGHTS PER WDM 33.Jul 7, 2006 · N750UP · Doug DC871F · Electrical Power System WiringSDR UPS06847289Windshield · corrodedF/O RIGHT SIDE WINDSHIELD FRAME & PAN HAS SEVERE CORROSION & RUST FLAKING & PITTED. PREVIOUSLY REPORTED ON CNTL UPS06847280, HOWEVER A/C FERRIED TO SAT FOR FINAL REPAIR. THIS CLOSES FERRY DEFERRAL - D328628. C/W ULT THICKNESS CK AFTER BLENDING UP TO 35% OF Jul 4, 2006 · N772UP · Doug DC871F · Flight Compartment WindowsSDR UPS06847288Windshield · delaminatedINSPECTION TYPE:N/A, F/O FWD RIGHT SIDE WINDSHIELD DELAMINATED & WILL NOT DEFOG. REMOVED F/O'S RT SIDE WINDSHIELD. REPLACED F/O'S RIGHT SIDE WINDSHEILD PER MM 56-10-02-2. INSTALLED TAPE INSTEAD OF SEALER FOR ONE TIME FERRY FLT TO SAT FOR CNTL UPS06847280.Jul 3, 2006 · N772UP · Doug DC871F · Flight Compartment WindowsSDR UPS06847280Window Post · corrodedFOUND CORROSION ON F/O'S WINDSHIELD FRAME. UPS ENGINEERING REQUESTS METAL REMOVAL VERIFICATION AND CRACK DETECTION AFTER BLEND OUT. C/W ULT THICKNESS CK AFTER BLENDING UP TO 35 PERCENT OF MAT'L REMOVED IN BLENDED AREAS. C/W HFEC OF BLENDED AREAS, NO CRACKS Jul 3, 2006 · N772UP · Doug DC871F · Fuselage Main, StructureSDR UPS06847292Splice · crackedINSPECTION TYPE: C3, SPLICE FITTING CRACKED, STA 1562 L34R. REMOVED LONGERON 34R AT STA 1562 IAW SRM 51-1-21, FABRICATED AND INSTALLED 2EA SPLICE ANGLES, ATTACH CLIP AND SPLICE FITTING AT STA 1562 L34R IAW SRM 53-02-00-0 FIG 002, 53-04-01 FIG 051, DWG 5758577Jun 29, 2006 · N715UP · Doug DC871F · Fuselage Main, StructureSDR IXXA060456SSkin · damagedDURING PREFLIGHT INSPECTION FOUND AIRCRAFT SKIN DAMAGED ON THE RIGHT HAND SIDE BELOW THE LAV SERVICE DOOR. REPAIRED SKIN PER DC8 SRM 53-2-1.Jun 28, 2006 · N829BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA060454OLanding Gear · lack of lubeDURING TAKEOFF FROM KDFW THE AIRCRAFT FAILED THE GEAR UPLATCH CHECK. THE CREW PERFORMED THE UNSATISFACTORY UPLATCH CHECKLIST AND RECYCLED THE GEAR, AGAIN FAILING THE UPLATCH CHECK. THE CREW ELECTED TO RECYCLE THE GEAR AGAIN AND THE UPLATCH CHECK WAS SUCCESSFJun 27, 2006 · N829BX · Doug DC871F · Nose/Tail Landing GearSDR UPS06847256Gauge · unserviceableINSPECTION TYPE:N/A MAIN ENTRY DOOR EMERGENCY ESCAPE SLIDE PRESSURE GAUGE IS UNREADABLE. VERIFY IF SLIDE PRESSURE IS SERVICEABLE PER TC 0231, STEP 1D SLIDE PRESSURE IS SERVICEABLE PER TC 231, 1D.Jun 24, 2006 · N744UP · Doug DC871F · Escape SlideSDR UPS06847184Coalescer Bag · dirtyINSPECTION TYPE:N/A STRONG BURNING ODOR WHEN LEFT PACK OPERATED WITH MIX VALVE IN FULL COLD POSITION. REMOVED AND CLEANED LT PACK COALESCER BAG IAW MM 21-55-03-2. RAN PACK WITH NO ODOR NOTED. A/C OK TO CONTINUE.Jun 22, 2006 · N705UP · Doug DC871F · Humidity Control SystemSDR UPS06847169Relief Valve · stuckINSPECTION TYPE:N/A 100 MILES OUT OF SLC F/O NOTICED A LOSS OF HYDRAULIC QTY. CREW RAN CHECKLIST AND DECLARED AN EMERGENCY. LANDING WAS UNEVENTFUL. FOUND LT BOGIE SWIVEL UNLOCK CYC - RELIEF VALVE STUCK IN THE OPEN POSITION. REMOVED AND REPLACED LT RELIEF VJun 21, 2006 · N729UP · Doug DC871F · Hydraulic Pressure Relief Valve, MainSDR IXXA060451OAdi · faultyDURING CRUISE FROM KMIA THE CAPTAINS ADI DISPLAYED BOTH FLIGHT DIRECTOR AND GYRO FLAGS, FLAGS STAYED IN VIEW FOR APPROXIMATELY 1-2 MINUTES THEN WENT AWAY FOR APPROXIMATELY 5 MINUTES, THEN INTERMITTENTLY DISPLAYED AFTER THAT. THE CREW RETURNED TO KMIA AND LANDJun 21, 2006 · N825BX · Doug DC871F · Integrated Flight SystemSDR UPS06847136Oxygen Mask · inoperativeINSPECTION TYPE:N/A CAPT OXYGEN MASK INOP. REMOVED AND REPLACED CAPT'S 02 MASK PER MEL 35-10-00. OPS CK GOOD.Jun 16, 2006 · N755UP · Doug DC871F · Crew Oxygen SystemSDR UPS06847131Structure · damagedINSPECTION TYPE:N/A LOAD CREW REPORTED HOLE IN NR 3 BELLY COMPARTMENT FLOOR APPROX 4 FT FWD OF DOOR LEFT OF CENTER. COMPLIED WITH EO DC8-5320-8724 APPROX A. PERMANENT REPAIR WITHIN 30 DAYS. REPAIRED DAMAGED FLOOR PANEL IAW DC8 SRM 53-2-5, FIG 8A. THIS CLEARJun 15, 2006 · N755UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS06847132Battery · dischargedINSPECTION TYPE:PFLT EMERGENCY DISCHARGE LIGHTS INOP. EMERGENCY DISCHARGE SWITCH WAS FOUND IN ARMED POS DURING PREFLIGHT. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY ASSY IAW MM 33-50-00. CHECK'S OK.Jun 14, 2006 · N729UP · Doug DC871F · Emergency LightingSDR UPS06847121O-Ring · damagedNR 3 ENG OIL PRESSURE DROPPED TO 15 PSI AND LIGHT ILLUMINATED THEN WENT OUT WITH OIL QTY DECREASING TO 8 QTS INITIALLY THEN CONTINUED TO 6 QTS. INFLIGHT ENG SHUT DOWN ACCOMPLISHED IAW CHECKLIST. WINDMILL TIME 25 MINUTES W/ POSITIVE OIL PRESSURE. PER PILOT RJun 14, 2006 · N700UP · Doug DC871F · Turbine Engine Oil SystemSDR UPS06847099Fitting · crackedFOUND C3 LONGERON 15L STA 1734 END FITTING IS CRACKED. REMOVED AND REPLACED LONGERON END FITTING AT STA 1734 L15L IAW SRM 51-3-2 AND SRM 51-1-20D.Jun 8, 2006 · N715UP · Doug DC871F · Fuselage Main, Longeron/StringerSDR IXXA060216OTransceiver · faultyAPPROXIMATELY ONE HOUR INTO CRUISE FROM KMIA TO SKCL, THE WEATHER RADAR INDICATED WEAK SIGNAL THEN STARTED SPOKING AND SPOTTING. AT ONE HOUR AND TEN MINUETS INTO FLIGHT THE WEATHER RADAR WENT COMPLETELY GREEN. THE CREW ELECTED TO RETURN TO KMIA AND PERFORMEDJun 7, 2006 · N823BX · Doug DC871F · Weather Radar SystemSDR UPS06847050Escape Rope · dislodgedINSPECTION TYPE:N/A LEFT ESCAPE ROPE CAME UNSTOWED. RESTOWED LEFT ESCAPE TAPE AS PER DC8 MM 25-60-02-2.Jun 6, 2006 · N755UP · Doug DC871F · Emergency EquipmentSDR UPS06847052Battery Pack · dischargedINSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS ARE INOP. REMOVED AND REPLACED BATTERY PACK PER MM 33-50-01. OPS CHECKS GOOD.Jun 5, 2006 · N798UP · Doug DC871F · Emergency LightingSDR UPS06847308Skin · crackedHFEC INSP DETECTED A .250" CRACK ON THE LWR AFT CORNER OF THE FWD LT TYPE 1 EMERGENCY EXIT DOOR (FWD OF STA 680.500) SEE ATTACHED DRAWING FOR LOC. REPAIRED LT TYPE 1 EMERGENCY EXIT LWR AFT CORNER IAW SAA EA 008- 5320-01-A0237 AND UPS EO DC8-5320-24507-A.Jun 1, 2006 · N715UP · Doug DC871F · Emergency ExitsSDR UPS06847164Support Fitting · crackedINSPECTION TYPE:C3 INTERCOSTAL CRACKED AT STA 620-640 L33L, FOUND DURING FLOOR SUPPORT REPAIR. REPAIRED INTERCOSTAL TRACK SUPPORT FITTING IAW SAA EA NR 008-5340-01- A0234, UPS RAA NR DC8-53-20557, BAC MSG NR 1-198392632-1 DATED 6/6/06 BAC MSG NR 1-198392632-2Jun 1, 2006 · N715UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS06847047Structure · puncturedINSPECTION TYPE:N/A PINHOLE PUNCTURE PIT 33 STA 1240 LEFT SIDE. PERFORMED INTERIM REPAIR PER EO DC8-5320-8724 APPENDIX A.Jun 1, 2006 · N744UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS06847027Smoke Goggles · missingINSPECTION TYPE:N/A SMOKE GOGGLES MISSING AT 2ND OBS STATION. INSTALLED SMOKE GOGGLES 1 EA.Jun 1, 2006 · N798UP · Doug DC871F · Emergency EquipmentSDR UPS06847034Skin · damagedINSPECTION TYPE:C3 STA 370 L28R HAS AREA OF DEEP INDENTATION AND RIVET HEAD MISSING. CUT OUT DAMAGED AREA AT STA 370 L28R IAW SRM 53-02-01-0 FIG 007. FABRICATED AND INSTALLED 2EA FILLERS, DOUBLER, AND 4EA FINGER DOUBLERS AT STA 370 L28R IAW SRM 53-02-01-0 FIMay 31, 2006 · N752UP · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS06847032Doubler · crackedINSPECTION TYPE:C3 AFTER REMOVAL OF INTERNAL TRIPLER IN LT CTR L/E FOUND LONG INTERNAL SPLICE DOUBLER CRACKED BETWEEN PNL 522A & XFS 409 AFT END. REMOVED INTERNAL SPLICE DOUBLER AT STA XFS 409 IAW SRM 51-01-20D. FABRICATED AND INSTALLED INTERNAL DOUBLER AT SMay 28, 2006 · N715UP · Doug DC871F · Wing Miscellaneous StructureSDR UPS06847098Attach Fitting · crackedC3 ATTACH FITTING CRACKED AT STA 834.500 L22L . REMOVED CRACKED FITTING AT STA 834.500 IAW SRM 51-1-20D. FABRICATED AND INSTALLED ATTACH FITTING AT STA 834.500 IAW DWG 4753360, AND SRM 51-1-20D.May 26, 2006 · N715UP · Doug DC871F · Fuselage Main, Attach FittingsSDR UPS06847085Attach Fitting · crackedINSPECTION TYPE:C3 ATTACH FITTING CRACKED AT STA 822.500 L22R AFT SIDE. REMOVED AND REPLACED FITTING AT STA 822.500 L22R IAW SRM 51-1-20D AND SRM 51-03-02.May 26, 2006 · N715UP · Doug DC871F · Fuselage Main, Attach FittingsSDR UPS06847012Tripler · crackedINSPECTION TYPE:C3 INTERNAL TRIPLER BROKEN INSIDE LT CTR L/E LWR SURFACE, BETWEEN PANELS 522A & 520B AT XFS 409. REMOVED, FABRICATED AND INSTALLED DOUBLER AND TRIPLER IAW SRM 51-1-20D, 51-03-00, 57-03-00-0 FIG 13 AND DWG 5769589.May 26, 2006 · N715UP · Doug DC871F · Wing, Plate/SkinSDR IXXA06SMN168SDoubler · improperDURING ROUTINE C CHECK INSPECTION FOUND LEFT HAND OUTER WING INBOARD EXTENDED LEADING EDGE OUTER SKIN EXISTING REPAIR DOUBLER WITH DISSIMILAR MATERIAL BETWEEN STATION 585.000 AND STATION 591.250. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NUMBER 06260 DATED 0May 25, 2006 · N830BX · Doug DC871F · Wing, Plate/SkinSDR IXXA06SMN167SSkin · crackedDURING C CHECK, FOUND LEFT WING L/E SKIN CRACKED ON INBOARD AILERON, AT STATION XA 480.000. PERFORMED MAJOR REPAIR IAW DC-8 SRM 57-8-1 FIG 1. REMOVED DAMAGED SKIN IAW DC-8 SRM 57-1-0 PAGE 1, DC-8 SRM 51-1-21. FAB`D NEW SKIN IAW DC-8 SRM 57-8-1 FIG 1 ITEM E.May 25, 2006 · N830BX · Doug DC871F · AileronsSDR IXXA06SMN112SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT AFT BATHTUB FITTING CRACKED STATION 902.100 LONGERON 9 LEFT. REPLACED AFT BATHTUB FITTING ON MAIN CARGO COMPARTMENT AT STATION 902.100 LONGERON 9 LEFT IAW DC-8 SRM 51-1-20D, DC-8 SRM 51-1-23, DC-May 25, 2006 · N830BX · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS06847100Fitting · crackedFOUND CRACKED FITTING L21L LWR CUSP FS 1320 D-PIT. REMOVED CRACKED FITTING AT STA 1320 L21L IAW SRM 51-1-20D. FABRICATED AND INSTALLED REPLACEMENT FITTING IAW DWG 9755584, AND SRM 51-3-0, AND SRM 51-1-20D.May 25, 2006 · N715UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS06847151Longeron · crackedINSPECTION TYPE:C3 LONGERON 15R CRACKED AT STA 1734. REMOVED CRACKED LONGERON SPLICE AND END FITTING AT STA 1734 L15R IAW SRM 51-1-21. FABRICATED AND INSTALLED LONGERON SPLICE AND END FITTING AT STA 1734-1770 L15R IAW SRM 53-02-02 FIG 10.May 23, 2006 · N715UP · Doug DC871F · Fuselage Main, Longeron/StringerSDR UPS06847115Skin · corrodedAFTER REMOVAL OF D-PIT SCUFF PLATE TO FOM NDT INSPECTION, FOUND CORROSION ON FUSELAGE SKIN. CUT OUT DAMAGED SKIN AT STA 1400-1410 L33R IAW SRM 53-2-0 FIG 21. FABRICATED AND INSTALLED REPAIR FILLER, DOUBLER, AND TRIPLER AT STA 1400-1410 L33R IAW SRM 53-02-00 May 23, 2006 · N715UP · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS06847033Attach Angle · crackedINSPECTION TYPE:C3 AFT PRESSURE BULKHEAD ATTACH ANGLE CRACKED AT STA 1766 L6R. REMOVED CRACKED ANGLE AT STA 1766 L6R IAW SRM 51-1-21, FABRICATED AND INSTALLED ATTACH CLIP AT STA 1766 L6R IAW SRM 51-01-20D, AND DWG 5773844.May 23, 2006 · N715UP · Doug DC871F · Fuselage Main, BulkheadSDR UPS06846955Structure · missingPILOT'S SIDE WINDOW BOLT POSITION NR 58 PER MM 56-10-02-2 HAS NO FRAME STRUCTURE BEHIND IT. BOLT ALSO WAS LEFT OUT OF TORQUE SEQUENCE STEP 10 AND 11 DUE TO NO STRUCTURE. DEFERRED CAPTS SIDE WINDSHIELD UPPER OUTBOARD DEFLECTOR AS MISSING PER EO DC8-5610-24395May 23, 2006 · N702UP · Doug DC871F · Fuselage Main, Structure
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