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 DHL2005801002Fire Warning · activatedNR 2 ENGINE FIRE WARNING, THE CREW BLEW BOTH FIRE BOTTLES. AFTER STARTING ENG DURING PUSHBACK--HAD ENG NR 2 FIRE WARNING.COMPLETED EMER. CHECK LIST. FIRED BOTH BOTTLES--FIRE WARNING LIGHT AND BELL CONTINUED TO ACTUATE AFTER SHUTDOWN. R/R NR 2 ENG RT CORE FIRE Jan 26, 2005 · N801DH · Doug DC873F · Fire DetectionSDR DHL2004809530Longeron · corrodedAFT ACCY COMPT L-34 CORRODED STA 1694. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. TRIMMED OUT CORRODED LONGERON SEGMENT IAW SRM 53-2-2 FIG 8. FABRICATED STANDARD LONGERON SPLICE (AL7075-T6510.100) IAW SRM 53-2-2 FIJan 21, 2005 · N809DH · Doug DC873F · Fuselage Main, Longeron/StringerSDR DHL2004809523Structure · wornRT WING OUTBOARD FLAP UPPER FWD PLATING WORN, XF 227.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATE 01-19-05, DWG X32-R04 REV-A DATE 01-19-05. REMOVED FASTENERS IAW SRM 51-1-21 PG 1, SRM 51-3-0 PG 1. TRIMMED OUT DAMAGED PLATING SEGMENT Jan 20, 2005 · N809DH · Doug DC873F · Trailing Edge FlapsSDR DHL2004809524Pressure Panel · crackedMAIN CARGO COMPT MLG PRESSURE PANEL SKIN CRACKED STA 907.000 LBL 41. (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATE 01-19-05 DWG X32-R05 REV A DATE 01-19-05. REMOVED EXISTING REPAIR IAW DWG X32-R05, SRM 51-1-21 PG.1, SRM 51-3-0 PG.1. TRIMMED Jan 20, 2005 · N809DH · Doug DC873F · Fuselage Main, BulkheadSDR DHL2004809528Skin · corrodedLWR FUSELAGE EXTERIOR SKIN CORRODED AT STA 1690.000 (L-28L TO L-28R). PERFORMED MAJOR REPAIR. REMOVED FASTENERS IAW SRM 51-1-20D PG 21, SRM 51-1-21 PG 1, SRM 51-3-0 PG 1. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. Jan 20, 2005 · N809DH · Doug DC873F · Fuselage Main, Plate/SkinSDR DHL2005807001Crank Assy · brokenRUDDER NEEDS CONSTANT TRIM CHANGES WITH SPEED AND FLAP CHANGES. A MAXIMUM OF FOUR UNITS OF RIGHT RUDDER TRIM IS REQUIRED DURING APPROACH WITH FLAPS DOWN, TO ZERO TRIM ON RUDDER WITH FLAPS UP. FOUND TWO CRANKS BROKEN ON RIGHT WING GROUND SPOILER. REMOVED ANDJan 19, 2005 · N807DH · Doug DC873F · Drag Control SystemSDR DHL2005801001Bulb · burned outNR 14 SMOKE DETECTOR DOES NOT PRESS TO TEST. REMOVED AND REPLACED BULBS AT NR 14 SMOKE DETECTOR. OPS CHECK OK IAW MM 26-10-6. P/N 376.Jan 19, 2005 · N801DH · Doug DC873F · Smoke DetectionSDR DHL2004809526Panel · delaminatedAFT FUSELAGE 732 LWR PANEL EDGE UNBONDED AND DELAMINATED, STA 980.000 TO STA 1060.000. REMOVED DELAMINATED PANEL IAW SRM 51-3-0 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW PANEL ASSY IAW SRM 51-3-0.Jan 18, 2005 · N809DH · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS05843851Stop Fitting · crackedINSPECTION TYPE: C3, RIGHT STA 98 FLAP UPSTOP FITTING CRACKED. GAINED ACCESS TO REPAIR SITE. REMOVED & REPLACED FITTING REF SRM 51-3-0, 51-1-8, 51-1-21, 51-1-15. RESTORED REPAIR AREA.Jan 17, 2005 · N868UP · Doug DC873F · Trailing Edge FlapsSDR DHL2004809527Skin · delaminatedLT WING - REMOVE AND INSTALL NR 1 SPOILER FOR DELAMINATION ON UPPER SKIN, XW 5.000 TO XW 90.000. REMOVED AND REPLACED NR 1 SPOILER (O/H CONDITION) ON LT WING XW 5.000 TO XW 90.000 (LT WING) IAW MM 27-61-1 PG 201-205.Jan 17, 2005 · N809DH · Doug DC873F · Wing, Plate/SkinSDR DHL2004809529Fitting · crackedAFT CARGO COMPT SPLICE FITTING CRACKED 2.000 BETWEEN STA 1060.000 AND STA 1040.000, L-35R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1. REMOVED CRACKED SPLICE FITTING IAW DC8 SRM 51-1-21 PG 1, SRM 51-1-20D PG 21. CLEANED, TREATED AND PRIMED ARJan 17, 2005 · N809DH · Doug DC873F · Fuselage Main, Attach FittingsSDR DHL2004809525Fitting · crackedAFT CARGO COMPT RT TUNNEL FITTING CRACKED 2.000, STA 1220.000. REMOVED CRACKED FITTING IAW SRM 53-1-0 PG 1, SRM 51-1-20D PG 1, SRM 51-1-21 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D PG 9, SRM 51-3-0 PG 1, Jan 17, 2005 · N809DH · Doug DC873F · Fuselage Main, Attach FittingsSDR DHL2004809522Bracket · brokenLEFT OUTBOARD SLOT UPPER DOOR BRACKET BROKEN. REMOVED AND REPLACED BROKEN BRACKET TO OUTBOARD SLOT DOOR UPPER DOOR IAW MM 27-80-2 PG 201-202, MM 20-16-0 PG 201-208.Jan 17, 2005 · N809DH · Doug DC873F · Wing, Attach FittingsSDR DHL2004809521Bracket · crackedNR 4 ALT TANK AFT BOOSTER PUMP BRACKET CRACKED. REMOVED AND REPLACED AFT BOOSTER PUMP BRACKET (NR 4 ALT TANK) IAW SRM 51-1-20D PG 9, 21 SRM 51-3-1 PG 2A.Jan 17, 2005 · N809DH · Doug DC873F · Wing, Attach FittingsSDR DHL2005804002Wire · looseAFTER PUSHBACK MAIN CARGO DOOR SYS-B WOULD NOT TEST DURING DESCENT FORWARD CARGO DOOR PROXIMTY C/B POPPED. TRANSFERRED TO DMI 19261 PER MEL 52-2-1 CAT-C FOUND BROKE WIRE IN MCD HARNESS SHORTING OUT (B-SYS) WARNING. SECURED WIRE TO PREVENT SHORTING AND ITEM IJan 15, 2005 · N804DH · Doug DC873F · Door System WiringSDR DHL2004809519Skin · delaminatedLT FWD ADF SENSE ANTENNA PANEL INTERNAL SKIN DELAMINATED (STA 810.000-855.000). REMOVED LT FWD ADF SENSE ANTENNA PANEL IAW SRM 51-3-0 PG 1. CLEANED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW LT FWD ADF SENSE ANTENNA PANEL IAW SRM 51-3-0 PG 1.Jan 14, 2005 · N809DH · Doug DC873F · Fuselage Main, Plate/SkinSDR DHL2004809520Support · crackedB-CARGO DOOR RT ROLLER SUPPORT CRACKED. REMOVED B-CARGO DOOR IAW MM 52-32-1 PG 201. REMOVED AND REPLACED RT ROLLER SUPPORT IAW OHM 52-3-5 PG 1-2. REINSTALLED B-CARGO DOOR IAW MM 52-32-1 PG 201-203. OPS CHECKED GOOD IAW MM 52-30-0 PG 7-11.Jan 14, 2005 · N809DH · Doug DC873F · Cargo/Baggage DoorsSDR DHL2004809518Bracket · brokenLT WING TRACK ASSY BRACKET BROKEN, XW 104.000. REMOVED AND REPLACED BRACKET ON LT WING TRACK ASSY XW 104.000 IAW SRM 51-3-0 PG 1, SRM 51-1-27A PG 1-4.Jan 14, 2005 · N809DH · Doug DC873F · Wing, Attach FittingsSDR DHL2005804001Lamp · inoperativeNR 13 SMOKE DETECTOR WILL NOT TEST. RELAMPED NR 13 SMOKE DETECTOR IAW MM 26-10-6.Jan 14, 2005 · N804DH · Doug DC873F · Smoke DetectionSDR UPS05845002Fitting · corrodedCORROSION UNDER SMALL CHAFF PAD IN C-PIT TORQUE BOX STA 1200 L34R. REMOVED CORROSION FROM UNDER CHAFF PAD IAW SRM 51-1-8 53-2-0. CORROSION OUT OF LIMITS IAW SRM 53-2-0. FABRICATED REPAIR DOUBLER AND INSTALLED DOUBLER AT STA 1200 L34R IAW SRM 51-1-8 AND DWG Jan 13, 2005 · N807UP · Doug DC873F · Fuselage Main, Attach FittingsSDR UPS05843739Fitting · corrodedINSPECTION TYPE:C3, LONGERON SPLICE FITTING CORRODED BEYOND LIMITS, STA 1260 - 1280 L34L. REMOVED AND REPLACED SPLICE FITTING REF SRM 51-1-20D, 51-1-8.Jan 13, 2005 · N868UP · Doug DC873F · Fuselage Miscellaneous StructureSDR IXXA0500002OSensing Element · intermittentDURING CRUISE FROM KTOL THE FIRE WARNING LIGHT AND BELL CAME ON FOR THE NR 4 ENGINE. NO OTHER INDICATIONS WERE NOTED. CREW RETURNED AIRCRAFT TO KTOL AND LANDED WITHOUT INCIDENT. AN INSPECTION IS ON GOING. AS SOON AS THE INFORMATION IS AVAILABLE IT WILL BE Jan 13, 2005 · N602AL · Doug DC873F · Fire DetectionSDR UPS05843760Skin · crackedINSPECTION TYPE:C3, L1 DOOR LOWER HINGE CUTOUT CRACKED ON FRAME. REMOVED LOCAL INTERCOSTAL & SEAL RETAINER TO FOM. STOP DRILLED CRACK & VERIFIED PER NDT/SPM06-10-01.001. FAB REPAIR DOUBLER FROM SHT 2024T3-0 -.071. INSTALLED ALL PARTS REF SRM 52-3-1 FIG 1, Jan 11, 2005 · N868UP · Doug DC873F · Passenger/Crew DoorsSDR UPS05843746Skin · crackedINSPECTION TYPE:C3 FUSELAGE SKIN CRACKED AT STA 1350 L35R. CUT OUT DAMAGED SKIN, NDT VERIFIED, ALL DAMAGE REMOVED. FAB FILLER FROM SHT2024T3-.071 & DOUBLER FROM SHT2024T3-.080 REF SRM 51-9-0, 53-2-1 FIG 8, 53-4-0 FIG 21A, 53-4-1 FIG 16. INSTALLED REPAIR PERJan 11, 2005 · N868UP · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS05843641Light · inoperativeINSPECTION TYPE:N/A, F/O UNDERGLARE SHIELD EMERGENCY LIGHT INOP. RELAMPED WITH NEW LAMPS. OPS CHECK NORMAL.Jan 11, 2005 · N819UP · Doug DC873F · Emergency LightingSDR DHL2004809531Skin · damagedLT WING INBD FLAP UPPER SKIN DEFLECTED, XW 2.000 TO XW 91.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR. REMOVED DAMAGED PANEL PLATING IAW SRM 51-1-21 PG 1, SRM 51-3-0 PG 1. FABRICATED NEW PANEL PLATING (AL2024-T3 0.050) IAW BOEING MESSAGE 1-XW84N, DWG SEMAN EJan 10, 2005 · N809DH · Doug DC873F · Trailing Edge FlapsSDR UPS05843756Rib · crackedINSPECTION TYPE:C3, RT WING CENTER L/E RIB CRACKED AT XFS 335.25. NDT VERIFIED CRACK TERMINATES AT RIVET HOLE REF SPM06-10-01.001. FAB 2 STACKED REPAIR ANGLES FROM SHT 7075T6-.040. INSTALLED REPAIR PER SRM 57-3-3 FIG 5, 57-2-0 FIG 2, 51-1-8, 51-1-21, 51-1-2Jan 8, 2005 · N868UP · Doug DC873F · Wing, Rib/BulkheadSDR UPS05843934Fitting · crackedINSPECTION TYPE: C, CRACK SPLICE FITTING AFT CARGO STA 1040 - 1060, L31R. REMOVED AND REPLACED SPLICE FITTING STA 1040 - 1060, L31R IAW DC8 SRM 51-1-21D, SRM 51-1-8, SRM 51-1-20 AND 51-1-11.Jan 6, 2005 · N868UP · Doug DC873F · Fuselage Main, Attach FittingsSDR UPS05843856Fitting · corrodedINSPECTION TYPE:C3 LOWER NR 5 T-BOLT BACKUP FITTING CORRODED BEYOND LIMITS AT C-PIT TORQUE BOX. REMOVED AND REPLACED FITTING REF SRM 53-2-0 FIG 1F, 51-1-20D.Jan 6, 2005 · N868UP · Doug DC873F · Fuselage Main, Attach FittingsSDR UPS05843854Longeron · crackedINSPECTION TYPE: C3, LONGERON 35L CRACKED STA 1260-1280. REMOVED 2 CLIPS & 1 INTERCOSTAL AT STA 1270. REMOVED SPLICE FITTING AT STA 1350. REMOVED SPLICE FITTING AT STA 1270. REMOVED AND REPLACED LONGERON SECTION FROM 1270-1350. REINSTALLED ALL FOM PARTS. Jan 6, 2005 · N868UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR DHL2004809517Longeron · crackedAFT FUSELAGE L-17R CRACKED 3.000, STA 1766.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1, SRM 53-5-3 FIG 5 SHEET 1. REMOVED DAMAGED LONGERON IAW SRM 51-1-20D PG 21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. APPLIED PRC SEALANT TO Jan 6, 2005 · N809DH · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS05843778Clip · crackedINSPECTION TYPE:C3 CRACK INSIDE THE NR 4 -T- BOLT BACKUP FITTING STA 320 REMOVED FITTING TO FOM. FOUND BOTH ATTACH CLIPS CRACKED (-1 & -2). REMOVED & REPLACED BOTH ATTACH CLIPS AND RE-INSTALLED BACKUP FITTING REF SRM 51-1-20D, 51-3-0, 53-2-0 FIG 2D, 51-1Jan 6, 2005 · N868UP · Doug DC873F · Fuselage Main, Attach FittingsSDR UPS05843755Longeron · crackedINSPECTION TYPE:C3 LONGERON 34L CRACKED AT STA 1260-1280. REMOVED SPLICE AT STA 1270 L34L. REMOVED L34L FROM SPLICE AT STA 1350 TO STA 1270. FAB & INSTALL REPLACEMENT LONGERON SECTION FROM 3758593-1 BETWEEN STA 1270-1350 AND SPLICE FITTING AT STA 1270 REF SJan 6, 2005 · N868UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS05843751Fitting · crackedINSPECTION TYPE:C3, CRACKED BANANA FITTING AT STA 1160 LONGERON 33R. GAINED ACCESS TO FITTING. REMOVED AND REPLACED FITTING PER SRM 51-1-20D, 51-1-8, 51-3-0. RESTORED AREA TO ORIGINAL CONFIG.Jan 6, 2005 · N868UP · Doug DC873F · Fuselage Main, Attach FittingsSDR UPS05843736Longeron · crackedINSPECTION TYPE:C3, LONGERON 34R CRACKED STA 1260-1280. REMOVED SPLICE FITTINGS AT STA 270 & 1350. OPENED BELLY SKIN FROM L31 LT TO L31 RT TO FOM FROM STA 1300-1350. CLEANED, TREATED, PRIMED AREA. REMOVED AND REPLACED LONGERON 34R FROM STA 1270-1350. REINJan 6, 2005 · N868UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS05843735Fitting · crackedINSPECTION TYPE: C3, BANANA FITTING CRACKED AT STA 1200 LONGERON 26L. CUT WEB ABOVE L27L TO FOM FITTING REMOVAL. REMOVED AND REPLACED FITTING REF SRM 51-1-20D, 51-1-8. REPAIRED WEB REF DWG9751879 USING SHT2024-T3 /.020 PER SRM 53-2-0 FIG 1D, 51-1-21, 51-1-2Jan 6, 2005 · N868UP · Doug DC873F · Fuselage Main, Attach FittingsSDR IXXA0500003OInsulator · brokenDURING CRUISE FROM FJDG TO RJTY NR 2 ENGINE SHORT CIRCUIT LIGHT ILLUMINATED, NO ASSOCIATED FIRE WARNING OR BELL. FIRE WARNING WOULD NOT TEST. CREW PERFORMED A PRECAUTIONARY SHUTDOWN OF NR 2 ENGINE. SHORT CIRCUIT LIGHT EXTINGUISHED WITH ENGINE SHUTDOWN. CREJan 6, 2005 · N606AL · Doug DC873F · Fire DetectionSDR DHL2006873001Skin · damagedK-LOADER PUNCHED A GAPING HOLE IN THE SIDE OF THE A/C. REPAIRED DAMAGE IAW DOUGLAS SRM 53-2-1 FIG 7 P105-106 FAA FORM 8100-9 & SRM 53-2-2 P47-48, NO DEFECTS NOTED.Jan 5, 2005 · N873SJ · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS05843936Fitting · crackedINSPECTION TYPE: C, CRACKS AFT CARGO PIT STA 1240 L35L. REMOVE EXISTING PRODUCTION SPLICE AND FITTING AND STOP DRILL CRACKS. FAB AND INSTALL SPLICE ANGLE. FAB AND INSTALL FRAME FITTING IAW DC8-SRM 51-1-21, 51-1-20, SR ADD DC8 5320-6176-B, SAA TRAVELER 0073 Jan 5, 2005 · N868UP · Doug DC873F · Fuselage Main, Attach FittingsSDR UPS05843933Rib · crackedINSPECTION TYPE: C, NR 4 STUB WING INBOARD L/E RIB CRACKED AT L/E. REMOVED, FABBED, AND INSTALLED NR 4 INBOARD STUB WING TAPERED FLANGE IAW DC8 SRM 51-1-21, DWG 9753297, SRM 51-1-8 AND DC8 SRM 51-1-21A.Jan 5, 2005 · N868UP · Doug DC873F · Wing, Rib/BulkheadSDR UPS05843932Finger Doubler · corrodedINSPECTION TYPE: C, FINGER DOUBLER AT RBL 70 BETWEEN FS 879 - 902 HAS EXFOLIATION CORROSION. REMOVED AND REPLACED FINGER DOUBLER IAW DC8 SRM 51-1-21, DWG 5645332, AND DC8 SRM 51-1-8.Jan 5, 2005 · N868UP · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS05843876Floorbeam · crackedFLOORBEAM LOWER FWD FLANGE HAS A 4.00 INCH CRACK F/S 920 RBL 65.0. FLOORBEAM SPLICE SEGMENT REPAIRED FROM RBL 31.40 TO RBL 70.0 IAW SAA SK 868-105.Jan 5, 2005 · N868UP · Doug DC873F · Fuselage Main, Floor BeamSDR UPS05843852Fitting · corrodedINSPECTION TYPE:C3 TORQUE BOX FITTING CORRODED BEYOND LIMITS AT STA 1220 L30L. REMOVED AND REPLACED FITTING REF SRM 51-1-8, 51-1-21, 51-1-20D.Jan 5, 2005 · N868UP · Doug DC873F · Fuselage Main, Attach FittingsSDR DHL2004809516Fitting · crackedAFT FUSELAGE FITTING CRACKED 1.000, NEXT L-17R STA 1766.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1. REMOVED CRACKED FITTING IAW SRM 51-3-0 PG 1. CLEANED, TREATED AND PRIMED AREA AND NEW FITTING IAW SRM 51-1-8B. INSTALLED NEW FITTING IAWJan 5, 2005 · N809DH · Doug DC873F · Fuselage Main, Attach FittingsSDR DHL2004809515Fitting · crackedFWD CARGO COMPT SPLICE FITTING CRACKED 3.000, STA 600.000 TO STA 620.000 L-31L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1. REMOVED CRACKED SPLICE FITTING IAW SRM 51-1-20D PG 21. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED NEW SPLJan 5, 2005 · N809DH · Doug DC873F · Fuselage Main, Attach FittingsSDR UPS05843759Longeron · crackedINSPECTION TYPE:C3 LONGERON 15R CRACKED UNDER SHEAR TIE AT STA 1754. REMOVED END FITTING AND CLIP TO FOM. REMOVED DAMAGED SECTION OF L15R FROM APPROX STA 1745-1766. FAB REPLACEMENT LONGERON SECTION FROM S1616757, SPLICE STRAPS FROM SHT7075T6-.080, SPLICE FIJan 5, 2005 · N868UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS05843757Longeron · crackedINSPECTION TYPE:C3 LONGERON 14R CRACKED UNDER CLIP AT STA 1756. REMOVED DAMAGE SECTION OF L14R FROM APPROX STA 1745-1766. REMOVED SHEAR TIE, END FITTING TO FOM. FAB REPLACEMENT LONGERON SECTION FROM S1616757, 2 SPLICE STRAPS FROM SHT7075T6-.080, AND 1 SPLICJan 5, 2005 · N868UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS05843753Rib · crackedINSPECTION TYPE:C3, LT WING ATTACHMENT RIB CRACKED AT XW454. CUT OUT DAMAGE, VERIFIED PER NDT SPM06-10-01.001. FABRICATED REPAIR DOUBLER FROM SHT7075-0-.100 & FILLER FROM SHT7075T6-.090 REF DWG 9753297. HEAT TREAT TO T6 PER DPS7.00-1. INSTALLED REPAIR PER Jan 5, 2005 · N868UP · Doug DC873F · Wing, Rib/BulkheadSDR UPS05843740Longeron · crackedINSPECTION TYPE:C3 LONGERON 14L CRACKED UNDER SHEAR TIE AT STA 1756. REMOVED END FITTING, INTERNAL DOUBLER & CLIP. CUT & REMOVED LONGERON SECTION FROM 1747 - 1766. FAB REPLACEMENT LONGERON SECTION FROM S1616757, 2 STRAPS FROM SHT7075T6-.080, SPLICE FITTING Jan 5, 2005 · N868UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS05843738Longeron · crackedINSPECTION TYPE:C3 LONGERON 15L CRACKED AT SHEAR TIE STA 1754. REMOVED END FITTING, CLIP, LONGERON SECTION FROM 1744 - 1766. FAB REPLACEMENT LONGERON SECTION FROM S1616757, 2 STRAPS FROM SHT 7075T6-.080, SPLICE FITTING FROM S2645716. TREATED, PRIMED, INSTALJan 5, 2005 · N868UP · Doug DC873F · Fuselage Main, Longeron/Stringer
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