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 DHL2006805513Door Frame · misrepairedFWD PASSENGER DOOR UPPER FWD JAMB CORNER REPAIR NOT IN ACCORDANCE WITH SR DWG 08530021 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8100-9 DATED 09-12-06, BOEING MESSAGE NR 1-225359431-2, SEMAN DWG ED43-13 DATED 09-12-06. REMOVED FASTENERS AND EXISTINSep 24, 2006 · N805DH · Doug DC873F · Fuselage Main, StructureSDR UPS06848038Battery Pack · inoperativeINSPECTION TYPE: N/A EMERGENCY EXIT LIGHTS INOPERATIVE. REMOVED AND REPLACED EMERGENCY BATTERY PACK ASSY. OPS TEST GOOD. REF MM CH 33-50-01.Sep 22, 2006 · N811UP · Doug DC873F · Emergency LightingSDR UPS06848006Sliding Window · lack of lubeCAPTAIN'S SLIDING WINDOW WILL NOT OPEN, IT IS BINDING ON TOP AND BOTTOM. LUBED CAPTAIN'S SLIDING WINDOW. OPS CHECK GOOD REF DC-8 MM CH 56-10- 03-5.Sep 19, 2006 · N894UP · Doug DC873F · Flight Compartment WindowsSDR DHL2006805510Skin · damagedLT INBD SLOT VANE HAS AN INTERIM REPAIR AT STA XS 250.089. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 09-05-06, EO NR AST060901 DATED 09-01-06. REMOVED EXISTING INTERIM REPAIR IAW SRM 51-1-21, SRM 51-1-20D. CUT OUT DAMAGED SECTION IAW EO NR AST060901.Sep 18, 2006 · N805DH · Doug DC873F · Leading Edge DevicesSDR DHL2006805509Skin · crackedLT ELEVATOR L/E LWR SKIN CRACKED AT STA XE 117.000. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 09-06-06, EO3 AST060902 DATED 09-06-06. REMOVED FASTENERS IAW SRM 51-1-21, SRM 51-3-0. CUT OUT DAMAGED SECTION IAW EO NR AST060902. PERFORMED NDT INSP IAW Sep 18, 2006 · N805DH · Doug DC873F · Elevator, Plate/SkinSDR DHL2006805508Skin · damagedLT OTBD SLOT VANE HAS AN INTERIM REPAIR AT STA XOLDI 6.225. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 09-07-06, EO NR AST060903 DATE 09-06-06. REMOVED INTERIM REPAIR IAW SRM 51-1-21, SRM 51-1-20D, SRM 51-3-0. TRIMMED OUT DAMAGED AREA IAW EO NR AST060Sep 18, 2006 · N805DH · Doug DC873F · Leading Edge DevicesSDR DHL2006805507Skin · damagedRT OTBD WING SLOT VANE HAS AN INTERIM REPAIR AT STA XOLD 6.224. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATE 09-07-06, EO NR AST060904 DATE 09-07-06. REMOVED INTERIM REPAIR IAW SRM 51-1-21, SRM 51-1-20D, SRM 51-3-0. TRIMMED OUT DAMAGED AREA IAW EO NR AST0Sep 18, 2006 · N805DH · Doug DC873F · Leading Edge DevicesSDR UPS06847986Line · leakingLOST HYD FLUID - DROPPED TO AUX - FOLLOWED BY MAIN SYSTEM PRESS FLUCTU ATIONS + - 1500 - 2000 PSI. DIVERT TO RICKENBACKER AFB (THIS INFO DIRE CTLY OFF LOGPAGE AS NOTED BY FLIGHT CREW). FOUND INBOARD HYD FLEX HOSE FROM NOSE GEAR RETRACT CYLINDER LEAKING. R/R HSep 13, 2006 · N819UP · Doug DC873F · Hydraulic System, MainSDR UPS06847979Wire · shortedINSPECTION TYPE: PFLT, CREW PREFLT - SMOKE IN COCKPIT. F/O'S SLIDING WINDOW ANTI-FOG WIRES SHORTED TO GROUND AT WINDOW FLEX CONDUIT AND C/B FAILED IN THE POWER CLOSED POS. WIRES & C/B REPLACED, SEE NRC 271362 - 271369 FOR DETAILS OF REPAIRS & CKS. ALL CHECKS GSep 12, 2006 · N840UP · Doug DC873F · Ice/Rain Protection System WiringSDR DHL2006801001Bleed Valve · warning lightENG (3) OVER PRESSURE LIGHTS ILLUMINATED ON TAKEOFF AT 67 PERCENT N1 RTO AT LESS THAN 60 KIAS LIGHT BRAKING. REPLACED NR 3 BLEED REG VALVE IAW DC-8 MM 36-12-1. OPS AND LEAKS CHECKS GOOD. RUN UP IAW JRH 12.2.Sep 12, 2006 · N801DH · Doug DC873F · Pneumatic Distribution SystemSDR UPS06847987Window · stuckCAPT'S WINDOW WILL NOT OPEN. REMOVED PIECE OF DEBRIS FROM UPPER TRACK, LUBRICATED WINDOW. OPS CK GOOD. OK FOR SERVICE.Sep 12, 2006 · N894UP · Doug DC873F · Flight Compartment WindowsSDR IXXA060602OEngine · overtempDURING TAKEOFF ROLL, NR 1 ENGINE OVER TEMPED TO 916 DEGREES AND CLIMBING, THE CREW ABORTED THE TAKE OFF AT 124 KNOTS AND RETURNED TO PARKING. MAINTENANCE INSPECTED THE ENGINE PER ALL APPLICABLE DATA, PERFORMED A POWER ASSURANCE RUN, ALL TARGETS ACHIEVED WITH NSep 9, 2006 · N602AL · Doug DC873F · Engine (Turbine/Turboprop)SDR DHL2006805506Angle · crackedAFT ACCY COMPT INTERNAL STRUCTURE "L" ANGLE CRACKED 2" STA 1660.000 LBL 50". REMOVED CRACKED "L" ANGLE IAW SRM 51-1-20D. FABRICATED NEW "L" ANGLE (AL7075T6 0.063") IAW SRM 53-2-0 PG 1. CLEANED, TREATED AND PRIMED AREA AND "L" ANGLE IAW SRM 51-1-8B. INSTALLSep 8, 2006 · N805DH · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL2006805517Skin · corrodedLT RUDDER SKIN CORRODED STA ZR 257.908 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 55-6-1 FIG 1 PG 2. REMOVED CORROSION IAW SRM 51-1-8. FOUND OUT OF LIMITS IAW SRM 55-2-0 PG 12. REMOVED CORRODED PANEL PLATING IAW SRM 55-1-0 PG.1, SRM 51-1-21. FABRICATESep 7, 2006 · N805DH · Doug DC873F · Rudder, Plate/SkinSDR DHL2006805504Fitting · crackedFWD CARGO COMPT FITTING CRACKED 1" STA 300.000 L-26L TO L-27L. PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1. REMOVED CRACKED FITTING IAW SRM 51-1-21, SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-21, SRM 5Sep 6, 2006 · N805DH · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS06847948Window · obstructedCAPTAIN'S EMERGENCY WINDOW WILL NOT FULLY OPEN. REMOVED TRIM ON L3 WINDOW AND DEFERRED PER GMM 3-6-10. WINDOW OPERATES NORMALLY. OK TO CONTINUE D332951.Sep 6, 2006 · N819UP · Doug DC873F · Flight Compartment WindowsSDR DHL2006805505Splice · crackedAFT ACCY COMPT AFT SPLICE FITTING 3" CRACK STA 1690.000 L-36. PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1. REMOVED CRACKED FITTING IAW SRM 51-1-21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D, SRM 51-3-0, SRM 51-Sep 5, 2006 · N805DH · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS06847937Battery · dischargedON PREFLIGHT, FOUND EMERGENCY LIGHTING INOP. REMOVED AND REPLACED EMERGENCY LIGHTING BATTERY PER MM 33-50-01-2, CHECKS OK.Sep 5, 2006 · N810UP · Doug DC873F · Emergency LightingSDR UPS06847949Hinge · lack of lubeCAPTAIN'S SLIDING WINDOW WILL NOT OPEN. LUBED UPPER WINDOW HINGE. SYSTEM GROUND CHECKED GOOD.Sep 2, 2006 · N894UP · Doug DC873F · Flight Compartment WindowsSDR DHL2006805503Skin · dentedRT WING INBD FLAP DENTED XW 106.000 (UPPER SKIN) MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW SRM 57-7-1 FIG 1 PG 2. REMOVED PLATING DIAW SRM 57-1-0 PG 1, SRM 51-1-21. FABRICATED NEW PLATING (AL2024T3 0.040") IAW SRM 57-7-1 FIG 1 PG 2 ITEM "D". CLEANED, TREATESep 1, 2006 · N805DH · Doug DC873F · Trailing Edge FlapsSDR IXXA060601OAnti-Skid Sys · failedDURING TAKEOFF, AFTER GEAR RETRACTION THE ANTISKID INOP LIGHT ILLUMINATED. THE CREW RECYCLED THE GEAR, RECYCLED THE ANTISKID SWITCH, RESET THE CIRCUIT BREAKERS, AND CYCLED THE PARKING BRAKE LEVER, ALL ACTIONS DID NOT EXTINGUISH THE ANTISKID INOP LIGHT. DUE TO Sep 1, 2006 · N603AL · Doug DC873F · Brake Anti-Skid SectionSDR DHL2006805502Frame · crackedRT WING CTR L/E LWR FORMER 1" CRACK STA XFS 360.000. REMOVED FASTENERS IAW SRM 51-1-20D, SRM 51-1-21. PERFORMED STOP HOLE AND FABRICATED (2) ANGLE DOUBLERS (AL7075T6 0.032") IAW SRM 57-2-0 PG 9,10. CLEANED, TREATED AND PRIMED AREA AND ANGLE DOUBLERS IAW SRMAug 31, 2006 · N805DH · Doug DC873F · Wing, Rib/BulkheadSDR DHL2006805501Frame · crackedRT WING CTR L/E UPPER FORMER HAS A CRACK OF 0.250" AT STA XFS 435.000. PERFORMED STOP HOLE AND FABRICATED (2EA) ANGLE DOUBLERS (AL7075T6 0.032") IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED AREA AND ANGLE DOUBLERS IAW SRM 51-1-8B. INSTALLED ANGLE DOUAug 31, 2006 · N805DH · Doug DC873F · Wing, Rib/BulkheadSDR DHL2006805500Frame · crackedRT WING CTR L/E UPPER FORMER 0.250" CRACK STA XFS 354.000. CORROSION, REMOVED FASTENERS IAW SRM 51-1-20D, SRM 51-1-21. PERFORMED STO HOLE AND FABRICATED (2EA) ANGLE DOUBLERS (AL7075T6 0.032") IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED AREA AND ANGLAug 31, 2006 · N805DH · Doug DC873F · Wing, Rib/BulkheadSDR UPS06847832Light · inoperativeINSPECTION TYPE: NA EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY PACK IAW MM 33-50-01, NO HELP. FOUND TERMINAL END SHORTED AND WIRE L619GA22. EMERGENCY LIGHT OPS TEST GOOD IAW MM 33-50-01.Aug 30, 2006 · N894UP · Doug DC873F · Emergency LightingSDR DHL2006805520Bulkhead · crackedAFT PRESSURE BLKD WEB FWD FACE HAS CRACKS OF 1.750" AND 1.500" APPROX AT STA 1766.000 L-10R TO L-11R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW AD90-16-05, S/B DC8 53-073, DWG SR08530007. REMOVED FASTENERS IAW SRM 51-1-21. CUT OUT DAMAGED SECTION AND FABRICAAug 26, 2006 · N805DH · Doug DC873F · Fuselage Main, BulkheadSDR UPS06847940Fitting · crackedINSPECTION TYPE:C3 END FITTING FOR STRINGER 51 OUTBOARD OF XRS 74 NR 2 MAIN TANK. REMOVED STRINGER END FITTING 51 AT STA XRS 74 NR 2 MAIN TANK IAW SRM 51-3-0. LOCATED, DRILLED UP AND INSTALLED END FITTING ON STRINGER 51 AT STA 74 NR 2 MAIN TANK IAW SRM 51-1-Aug 23, 2006 · N802UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS06847807Battery · dischargedEMERGENCY EXIT LIGHTS FADE OUT DURING TEST. A/C POWERED FOR 2.5 HRS AND BATTERY CHARGE WITH A/C POWER IAW DC8 AMM 33-50-01. CHECKED SERVICEABLE.Aug 23, 2006 · N814UP · Doug DC873F · Emergency LightingSDR UPS06847787Rib · crackedINSPECTION TYPE:C3 LT CENTER L/E UPPER RIB CRACKED AT XFS 460. STOP DRILLED CRACKED RIB AT LT L/E STA XFS 460 IAW SRM 57-02-00 FIG 2. FABRICATED AND INSTALLED REPAIR ANGLE AT LT L/E RIB STA XFS 460 IAW SRM 57-02-00 FIG 002.Aug 22, 2006 · N802UP · Doug DC873F · Leading Edge DevicesSDR UPS06847782Doubler · gougedINSPECTION TYPE:C1-3 STA 219 LT FLAP FOUND O/B VERT DOUBLER AND LWR ATTACH ANGLE GOUGED OUT OF LIMITS. REMOVED DAMAGED DOUBLER AND ATTACH ANGLE AT LT FLAP STA 219 IAW SRM 51-1-20D. FABRICATED AND INSTALLED REPLACEMENT REPAIR WEB, STRAP AND REPAIR ANGLE IAW DAug 22, 2006 · N806UP · Doug DC873F · Trailing Edge FlapsSDR IXXA060599OPressure Switch · faultyDURING DESCENT INTO KTOL NUMBER THREE ENGINE LOW OIL PRESSURE LIGHT ILLUMINATED. THE CREW PERFORMED A PRECAUTIONARY ENGINE SHUTDOWN PER ALL APPLICABLE DATA. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND A FAULTY LOW OIL PRESSURE WARNING SWITCH. MAug 22, 2006 · N602AL · Doug DC873F · Engine Oil PressureSDR UPS06847758Battery Pack · weakINSPECTION TYPE:N/A ON PRE-DEPARTURE CHECK FOUND EMERGENCY EXIT LIGHTS WEAK. REMOVED AND REPLACED EXIT LIGHT BATTERY PACK. TESTS OK.Aug 22, 2006 · N894UP · Doug DC873F · Emergency LightingSDR UPS06847743Battery Pack · inoperativeEMERGENCY LIGHTS WOULD NOT ILLUMINATE IN TEST. REMOVED AND REPLACED EMERGENCY LIGHTS BATTERY PACK PER AMM 33-50-01-2. OPS CHECK GOOD.Aug 21, 2006 · N851UP · Doug DC873F · Emergency LightingSDR UPS06847741Cusp Web · crackedRT CUSP WEB AT POS NR 2 CRACKED. REPAIRED IAW EO DC8-5330-2159.Aug 20, 2006 · N803UP · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL2006806004Fire Warning · illuminatedNR 1 ENGINE B-LOOP FIRE WARNING, BOTH FIRE BOTTLES DISCHARGED. FIRE LIGHT AND BELL CAME ON THROUGHOUT FLIGHT. ENGINE MAINTAINED OIL PRESSURE. PERFORMED TEST OF A AND B LOOP NR 1 ENG. PER DC-8 M/M 26-10-0. FOUND "A" LOOP RESISTANCE TOO LOW. B LOOP RESISTANCE Aug 20, 2006 · N806DH · Doug DC873F · Fire DetectionSDR UPS06847995Longeron · corrodedINSPECTION TYPE-C3 AFTER REMOVED FUSELAGE BELLY SKIN FROM FS -22 TO 70 L31L-L31R, FOUND LONGERON HAS HEAVY CORROSION AT STA 55 TO 70 L36. FABRICATED AND INSTALLED LONGERON AND END FITTING. IAW SRM 51-3-2 AND 51-1-20D.Aug 18, 2006 · N802UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS06847892Attach Angle · corrodedINSPECTION TYPE-C3 STA 857 RBL 53 UPPER HORIZONTAL ATTACH ANGLE, CENTER FUEL TANK, FWD BULKHEAD HAS EXFOLIATED CORROSION. REMOVED FABRICATED AND INSTALLED SHEAR WEB ANGLE RAT WHEEL WELL, FWD BULKHEAD (CENTER FUEL TANK), STA 857 RBL 53 IAW DRAWING NR 5644011, Aug 18, 2006 · N802UP · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL2006809519Skin · damagedRT WING CTR LE LWR EXTERNAL SKIN HAS AN INTERIM REPAIR AT STA XFS 422.750 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 07-12-06, EO NR AST060702 DATED 07-10-06. REMOVED FASTENERS FROM REPAIR AREA AND EXISTING DOUBLER IAW SRM 51-1-20D, SRMAug 17, 2006 · N809DH · Doug DC873F · Wing, Plate/SkinSDR DHL2006809522Skin · wornFUS EXT SKIN HAS WEAR OF 0.750" AND 0.500" APPROX AT STA 28.000 L-27L TO L-18L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110 DATED 07-14-06, EO AST060705 DATED 07-13-06. REMOVED FASTENERS IAW SRM 51-1-21, SRM 51-1-20D. CUT OUT DAMAGED SECTION IAWAug 17, 2006 · N809DH · Doug DC873F · Fuselage Main, Plate/SkinSDR DHL2006809521Doubler · crackedRT WING TOP PANEL NR 3 MAIN TANK ACCESS DOOR 505E, CRACK ON PREVIOUSLY REPAIRED DOUBLER CONTINUES 0.375" (STA XRS 107.000 - 139.000) MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 07-16-06, EO NR AST060707 DATED 07-15-06. REMOVED EXISTING INTAug 17, 2006 · N809DH · Doug DC873F · Wing, Plate/SkinSDR DHL2006809520Pressure Panel · corrodedFLT COMPT HORIZ PRESSURE PANEL CORRODED STA -12.000 RBL 30. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 07-16-06, EO NR AST060706 DATED 07-14-06. REMOVED CORROSION IAW SRM 51-1-8. FOUND OUT OF LIMITS IAW SRM 53-2-0. REMOVED FASTENERS FROM REPAIR AREA IAug 17, 2006 · N809DH · Doug DC873F · Fuselage Main, BulkheadSDR DHL2006809517Skin · corrodedITEM REF NR 058142: LT OUTER WING OTBD L/E UPPER SKIN CORRODED, STA XFS 742.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 07-14-06. REMOVED FASTENERS IAW SRM 51-1-21, SRM 51-1-20D. REMOVED CORROSION IAW SRM 51-1-8 PG. 17-18. FOUND OUT OFAug 17, 2006 · N809DH · Doug DC873F · Wing, Plate/SkinSDR DHL2006809523Vane · damagedRT INBD VANE SLOT HOLES ELONGATED STA XILD 7095. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 07-12-06, EO NR AST060701 DATED 07-07-06. REMOVED FASTENERS IAW SRM 51-1-21, SRM 51-3-0, SRM 51-1-20D. CUT OUT DAMAGED SECTION IAW EO NR AST060701. PERFORMED Aug 17, 2006 · N809DH · Doug DC873F · Trailing Edge FlapsSDR DHL2006809518Doubler · crackedRT WING CTR LE INTERNAL SPLICE DOUBLER 1.500" CRACK STA XFS 341.500 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 07-14-06, EO NR AST060704 DATED 07-12-06. REMOVED FASTENERS FROM REPAIR AREA IAW SRM 51-1-20D. CUT OUT DAMAGED SECTION IAW EAug 17, 2006 · N809DH · Doug DC873F · Wing, Plate/SkinSDR UPS06847894Longeron · corrodedINSPECTION TYPE-C3 STA.1766 LONGERON 28R CORRODED AND CRACKED. REMOVED DAMAGED SECTION OF LONGERON 28R FROM STA 1752 TO 1766 IAW SRM 53-02-02-0 FIG 10 AND SRM 51-01-21-0. FABRICATED LONGERON SECTION AND REPAIR STRAPS IAW SRM 53-05-03-0, AND SRM 53-02-02-0 FIAug 17, 2006 · N802UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS06847893Fitting · crackedINSPECTION TYPE-C3 STA 1766 LONGERON 28R END FITTING CORRODED. END FITTING FOUND TO BE CORRODED AND CRACKED. REMOVED AND REPLACED STA 1766 LONGERON 28R END FITTING IAW SRM 51-1-20D, AND SRM 51-03-02 -0.Aug 17, 2006 · N802UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS06847891Fitting · crackedINSPECTION TYPE-C3 STA 1760 LONGERON 14R END FITTING CRACKED. REMOVED AND REPLACED LONGERON END FITTING AT STA 1760 LONGERON 14R IAW SRM 51-01-21, SRM 51-03-00, AND SRM 51-01-20D.Aug 17, 2006 · N802UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS06847768Rib · crackedINSPECTION TYPE:C3 LEFT CENTER LEADING EDGE UPPER RIB CRACKED AT XFS 366. STOP DRILLED CRACK. FABRICATED AND INSTALLED 2 EA REPAIR DOUBLERS IAW SRM 57-3-3, 57-02-00, 51-1-21 AND 51-1-20D.Aug 17, 2006 · N802UP · Doug DC873F · Leading Edge DevicesSDR UPS06847871Skin · corrodedFOUND CORROSION BETWEEN SKIN AND DOUBLER AT L36 STA 1180, EXTERIOR BULGED. CUT OUT DAMAGED AREA AT STA 1180 L36 IAW SAA EA 008-5320-01-A0381. FABRICATED AND INSTALLED REPAIR PARTS AT STA 1180 L36 IAW SAA EA NR 008-5320-01-A0381, UPS RAA DC8-53-20581, DOUGLASAug 16, 2006 · N802UP · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS06847829Fitting · crackedINSPECTION TYPE: C3 STA.1690 LONGERON 26R END FITTING CRACKED. REMOVED AND REPLACED STA. 1690 LONGERON 26R END FITTING IAW SRM 51-1-20D,AND SRM 51-03-01-0.Aug 16, 2006 · N802UP · Doug DC873F · Fuselage Main, Attach Fittings
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