N676UP, cancelled May 24, 2011

Service difficulty reports · 461

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Query with SQL
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 n_number = 'N676UP' AND deregistration_id = 'N676UP-2011-05-24'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR UPS08451591Skin · crackedLT O/B AILERON UPPER SKIN HAS .5" BPT CRACK 4" FWD T/E, 11' IB OF OB END. APPLIED SPEED TAPE PER SRM 51-40-09 FIG 1 TABLE 1 AND TABLE II. REINSPECT EVERY "A" CHECK. PERMANENT REPAIR AT NEXT "C" CHECK. TRANSFERRED TO D368106.Jan 30, 2008 · N676UP · Boeing 747123 · AileronsSDR UPS07451115Generator · inoperativeINSPECTION TYPE:N/A ATB FOR NR 3 BUSS TIE ON WITH FEEDER FAULT LT & CONST SPEED LIGHT. FIVE MIN LATER, CONST SPD LIGHT GEN 2 & GEN 4 W/LOSS OF BOOST PUMP IN TANKS 2 AND 3, NR 2 AFT, NR 3 FWD. NR 3 FAULT ANNUNCIATOR SHOWED GEN/FEEDER. INSPECTED FEEDERS IN PYNov 7, 2007 · N676UP · Boeing 747123 · Alternator-Generator DriveSDR UPS07451107Csd · overheatedIFSD, NR 2 ENG CSD HAD HIGH OIL TEMP. FLIGHT CREW TRIED TO DISCONNECT BUT COULDN'T. FOLLOWED CHECK LIST AND SHUT DOWN ENGINE. MX INSPECTED NR 2 ENG CSD AND FOUND THAT OIL HAD LEAKED OUT AND CSD OVERHEATED. CSD REMOVED AND REPLACED AND GEAR BOX INSPECTION Nov 6, 2007 · N676UP · Boeing 747123 · Alternator-Generator DriveSDR UPS07451082Connector · damagedEMERGENCY LIGHTS ABOVE R1 DOOR DO NOT WORK. FOUND TERMINAL END ON EXIT SIGN BROKEN. REPLACED PER BOEING SSWD 20-30-11. FUSE BLOWN ON POWER PACK MODULE. REPLACED MODULE X328 MM 33-51-04/2. ALSO, FOUND WIRES AT PLUG DC228 BROKEN. REPLACED PLUG PER BOEING SOct 23, 2007 · N676UP · Boeing 747123 · Light System WiringSDR UPS07450630Accumulator · leakingINSPECTION TYPE:N/A PILOT REPORT - BRAKES SLOW TO RESPOND, FOUND BRAKE ACCUMULATOR LOW DURING ATTEMPTED SERVICE. FOUND LARGE AMOUNT OF HYD FLUID ON NITROGEN SIDE OF ACCUMULATOR. REMOVED AND REPLACED BRAKE ACCUMULATOR PER MM 32-41-09. SERVICED, OPS CHECK GOOSep 10, 2007 · N676UP · Boeing 747123 · Landing Gear Brake SystemSDR UPS07449812Spar · brokenINSPECTION TYPE:C RIGHT HORIZONTAL STABILIZER UPPER REAR SPAR AND SPLICE PLATE INSP BROKEN BOLTS INDICATION REVEALED ON BOLT 6 & 29. RIGHT HORIZONTAL STAB UPPER REAR SPAR AND SPLICE PLATE BROKEN BOLTS 6 & 29 POSITION REPLACED (BOLTS P/N ON:BACB30US6K17 & BACBMay 13, 2007 · N676UP · Boeing 747123 · Horizontal Stabilizer StructureSDR UPS07449139Swivel · leakingINSPECTION TYPE:N/A COMPLETE LOSS OF HYD QTY IN FLIGHT, ON SYSTEM NR 4. NOTE: RESERVOIR NR 4 INDICATED 1 GALLON. FOUND RIGHT MAIN GEAR DOWNLOCK ACTUATOR FWD HOSE NEAR UPPER FITTING AT SWIVEL LEAKING. REMOVED AND REPLACED HOSE ASSY, SERVICED NR 4 HYD QTY PRFeb 7, 2007 · N676UP · Boeing 747123 · Hydraulic Reservoir, MainSDR UPS06448245Terminal · corrodedINSPECTION TYPE: N/A, SMOKE SMELLS, ABOUT 1:30 INTO FLIGHT. FOUND COPILOT WINDSCREEN CONNECTION AT LOWER RT SIDE SMOKING SECURED RT 1 OVERHEAD WINDOW HEAT, SMOKE STOPPED. FOUND R1 WINDOW HEAT POWER TERMINAL (A) LOOSE AT CORRODED. CLEANED, RETORQUED AT PERFORMOct 15, 2006 · N676UP · Boeing 747123 · Windshield/Door Rain/Ice RemovalSDR UPS06448035Light · weakINSPECTION TYPE: N/A EMERGENCY LIGHT ON CEILING ON MAIN DECK POS NR 1 IS VERY DIM. REMOVED AND REPLACED EMERGENCY CEILING LIGHT IAW MM 33-51-00. OPS CK GOOD. OK FOR SERVICE.Sep 21, 2006 · N676UP · Boeing 747123 · Emergency LightingSDR UPS06447998Skin · puncturedRT OB FLAP LWR SKIN APPX 1 INCH PUNCTURE. REMOVED DAMAGED AREA OF SKIN AND CORE PER SRM 51-40-06. DAMAGE REMOVED OKAY TO INSTALL REPAIR. DRYED AREA-INSTALLED REPAIR CORE AND STARTED CURE PER SRM 51-40-20. COMPLETED REPAIR PER SRM 51-40-20. REF LOG PAGE 566736Sep 13, 2006 · N676UP · Boeing 747123 · Trailing Edge FlapsSDR UPS06447934Module · inoperativeMAIN DECK EMERGENCY LIGHT IN CEILING AT STA 580R GOES OFF AFTER A FEW SECONDS OF TEST. REMOVED AND REPLACED CEILING LIGHT MODULE PER MM 33-51-07. OPS CHECK GOOD.Sep 5, 2006 · N676UP · Boeing 747123F · Emergency LightingSDR UPS06447932Light · inoperativeMAIN DECK EMERGENCY LIGHT IN CEILING AT STA 340R DOES NOT COME ON DURING TEST. PERFORMED LIGHT TEST W/LIGHT CHECKING GOOD ON GROUND.Sep 5, 2006 · N676UP · Boeing 747123F · Emergency LightingSDR UPS06447911Light · inoperativeINSPECTION TYPE: N/A MAIN DECK EMERGENCY LIGHT IN CEILING AT STA 58DL AND ENTRY DOOR AFT EMERGENCY LIGHT GO OFF AFTER A FEW SECONDS OF TEST. THESE LIGHTS ARE TIED TOGETHER IAW MM. SUSPECT CEILING LIGHT BATTERY PACK BAD. REMOVED AND REPLACED CEILING LIGHT MOSep 4, 2006 · N676UP · Boeing 747123 · Emergency LightingSDR UPS06447910Light · inoperativeINSPECTION TYPE: N/A EMERGENCY LIGHT IN CEILING (FWD OF STAIRS) ON MAIN CARGO DECK INOPERATIVE. MAIN DECK UPPER DOOR FRAME FWD EMERGENCY LIGHT IS TIED TO THIS LIGHT AND IS ALSO INOPERATIVE. REMOVED AND REPLACED CEILING LIGHT MODULE W/REF TO MM 33-51-07. OPS Sep 4, 2006 · N676UP · Boeing 747123 · Emergency LightingSDR UPS06447895Power Supply · inoperativeINSPECTION TYPE: ASE UPPER DECK DOOR FRAME EMEGENCY LIGHTS X 325 AND X 326 ARE INOP. REMOVED AND REPLACED UPPER DECK DOOR LIGHT POWER SUPPLY MODULE WITH REF TO MM 33-51-04. OPERATIONAL CHECK GOOD.Sep 4, 2006 · N676UP · Boeing 747123 · Emergency LightingSDR UPS06447541Floorbeam · crackedINSPECTION TYPE:C U/D BS440 FLOORBEAM WEB FOUND CRACKED AFTER UPPER CHORD REMOVED JUST AT LBL 4, CRACK LENGTH 1". U/D BS440 BETWEEN LBL24 AND RBL16 FLOORBEAM WEB REPAIRED AS PER SRM 53-10-07 FIG 11.Jul 25, 2006 · N676UP · Boeing 747123F · Fuselage Main, Floor BeamSDR UPS06447694Skin · crackedINSPECTION TYPE: C U/D FX SKIN AT BS 380 S6R REPAIR AREA FOUND 3 ADDITIONAL FASTENER HOLES CRACK AT OUTER SKIN. CRACK LENGTH 0.060" & 0.090" RESP. FX BS360-384 S6R OVERLAPPING SKIN REPAIRED AS PER RS R53-15-35543 ITEM D REFER NRC 7055 FOR WORKING DETAIL. PJul 21, 2006 · N676UP · Boeing 747123F · Fuselage Main, Plate/SkinSDR UPS06447676Reveal · crackedINSPECTION TYPE:C M/D BS 2231 FRAME INNER CHORD S25R-26R FOUND REVEAL CRACK AND PREVIOUSLY STOP DRILLED, CRACK LENGTH 1.5". REPAIR DOUBLER REINSTALLED AS PER RS R53-62-35534 CONTINUE THE REPETITIVE INSPECTION ARE REQUIRED PER RS R53-62-35534 AND UPS EO B747-5Jul 19, 2006 · N676UP · Boeing 747123F · Fuselage Miscellaneous StructureSDR UPS06447675Reveal · crackedINSPECTION TYPE:C M/D BS 2231 FRAME INNER CHORD S22L-S25L FOUND REVEAL CRACKED AT S22L AND S24L LOCATION AND PREVIOUSLY STOP DRILLED, CRACK LENGTH 1" AND 1.5". REPAIR DOUBLER REINSTALLED AND THE CRACK THAT ENDS AT A FASTENER HOLE OVERSIZED AS PER RS R53-62-35Jul 19, 2006 · N676UP · Boeing 747123F · Fuselage Miscellaneous StructureSDR UPS06447693Skin · crackedFX BS 340-380 S6R LAP SPLICE TOP ROW FASTENER HOLES FOUND CRACKS AT OUTER SKIN. FX BS340-360 S6R FASTENER REINSTALLED AS PER RS R53-15-35543 ITEM C. REFER NRC 7055 FOR WORKING DETAIL. FX BS360-384 S6R OVERLAPPING SKIN DOUBLERS ARE TO BE CONTINUE AT REPEAT IJul 14, 2006 · N676UP · Boeing 747123F · Fuselage Main, Plate/SkinSDR UPS06447681Frame · crackedINSPECTION TYPE:C FX BS340 FRAME FOUND 1 HOLE CRACK AT S6R LOCATION APPROX 0.030" LONG, CRACK LENGTH 0.030". FX BS 340 STR 6R AREA FRAME REPAIRED AS PER RS R53-15-35543 ITEM B AND UPS ENGINEERING FILE NR 747-53-20319.Jul 14, 2006 · N676UP · Boeing 747123F · Fuselage Main, FrameSDR UPS06447450Stringer · crackedINSPECTION TYPE:C FX BS 340-360 S6R FOUND FASTENER HOLES CRACK AT STRINGER (CRACK LENGTH 0.030 INCH). FX BS 340-375 STR 6R STRINGER REPAIRED AS PER SRM 53-10-03 FIG 3.Jul 14, 2006 · N676UP · Boeing 747123 · Fuselage Main, Longeron/StringerSDR UPS06447692Skin · crackedFX BS 360-380 S6R LAP SPLICE 6EA TOP ROW FASTENER HOLE FOUND CRACKS AT OUTER SKIN, CRACK LENGTH 1/16 APPROX. FX BS 340 TO BS 360 STR 6R FASTENER REINSTALLED AS PER RS R53-15-35543 ITEM C FX BS360-384 STR 6R OVERLAPPING SKIN REPAIRED AS PER RS R53-15-35543 ITEJul 13, 2006 · N676UP · Boeing 747123F · Fuselage Main, Plate/SkinSDR UPS06447660Floorbeam · corrodedBS 520 FLOORBEAM UPPER CHORD FOUND CORRODED. CORROSION BLEND OUT 0.030" BY 2" BY 3" EXCEED SRM 53-10-01 FIG 1 LIMIT AND U/D BS 520 FLOORBEAM UPPER CHORD REPAIRED AS PER HX RS NR R53-25-35537 REF NRC NR IB70247 FOR WORKING DETAIL AND REF UPS EO NR B747-5310-24Jul 13, 2006 · N676UP · Boeing 747123F · Fuselage Main, Floor BeamSDR UPS06447659Floorbeam · misdrilledBS 520 FLOORBEAM UPPER CHORD FOUND SHORT EDGE MARGIN AT LBL 76" TO LBL 78" APPROX. U/D BS 520 FLOORBEAM REPAIRED AS PER HX RS NR R53-25-35537 REFER NRC NR IB70247 FOR WORKING DETAIL AND REF UPS EO NR B747-5310-24843-A.Jul 13, 2006 · N676UP · Boeing 747123F · Fuselage Main, Floor BeamSDR UPS06447658Floorbeam · misdrilledBS 520 FLOORBEAM UPPER CHORD FOUND SHORT EDGE MARGIN FROM RBL 48 TO RBL 82. BS 520 FLOORBEAM REPAIRED AS PER HX RS NR R53-25-35537 REFER NRC NR IB70247 FOR WORKING DETAIL AND REF UPS EO NR B747-5310-24843-A.Jul 13, 2006 · N676UP · Boeing 747123F · Fuselage Main, Floor BeamSDR UPS06447480Frame · crackedINSPECTION TYPE:C RT BLG W/W STA 1438 FRAME ATT HOLE FOUND CRACKED RBL 116 WL 156, CRACK LENGTH 3/8". RT BLG W/W BS 1438 RBL 116 WL 152 TO WL 165 FRAME REPAIRED AS PER SRM 51-40-03 FIG 2.Jul 13, 2006 · N676UP · Boeing 747123F · Fuselage Main, FrameSDR UPS06447563Vertical Beam · crackedINSPECTION TYPE:C 1L MED FWD VERTICAL BEAM LOWER CORNER CRACK FOUND AS MARKED. CRACK LENGTH 1 INCH. 1L MED FWD VERTICAL BEAM LOWER CORNER REPAIRED AS PER SRM 52-10-02 FIG 10.Jul 12, 2006 · N676UP · Boeing 747123 · Fuselage Main, StructureSDR UPS06447562Vertical Beam · crackedINSPECTION TYPE:C 1R MED FWD VERTICAL BEAM LOWER CORNER FOUND CRACK. CRACK LENGTH 1 INCH. 1R MED FWD VERTICAL BEAM LOWER CORNER REPAIRED AS PER SRM 52-10-02 FIG 10.Jul 12, 2006 · N676UP · Boeing 747123 · Fuselage Main, StructureSDR UPS06447538Angle · crackedINSPECTION TYPE:C RT SIDE BS2231 FRAME AT STR25 FOUND 2 HOLES CRACKED AT INTERCOSTAL TO FRAME WEB ATTACHED T-ANGLE AREA. CRACK LENGTH 1/8". RT SIDE BS 2231 FRAME AT STR 25 FRAME WEB ATTACHED T-ANGLE REPLACED AS PER SRM 51-10-01 PG 9.Jul 12, 2006 · N676UP · Boeing 747123F · Fuselage Miscellaneous StructureSDR UPS06447491Splice Plate · corrodedINSPECTION TYPE:C FWD CARGO COMPT RT MAIN DECK FLOORBEAM LOWER CHORD SPLICE PLATE LOWER SURFACE FOUND SURFACE CORROSION AT STA 680 TO STA 700 RBL12. CORROSION BLEND OUT 0.019" BY 1/2" BY 1" EXCEED SRM LIMIT. FWD CARGO COMPT RT MAIN DECK FLOORBEAM LOWER CHORDJul 12, 2006 · N676UP · Boeing 747123F · Fuselage Main, Floor BeamSDR UPS06447662Floorbeam · damagedU/D RT BS 520 UPPER DECK FLOORBEAM FWD FLANGE 1 FASTENER HOLE FOUND OVAL AT RBL 70". U/D BS 520 FLOORBEAM REPAIRED AS PER HX RS NR R53-25-35537 REF NRC NR IB70247 FOR WORKING DETAIL AND REF UPS EO NR B747-5310-24843-A.Jul 11, 2006 · N676UP · Boeing 747123F · Fuselage Main, Floor BeamSDR UPS06447657Floorbeam · corrodedLT BS 520 UPPER DECK FLOORBEAM AFT FLANGE 5 FASTENER HOLES FOUND CRACK AND/OR CORROSION AT LBL 34, LBL 45, LBL 49, AND LBL 55" (CRACK LENGTH 0.060" , CORROSION BLEND OUT 0.075" X 1.5" X 2"). CORROSION EXCEED SRM 53-10-01 FIG 1 LIMITS, U/D BS 520 FLOORBEAM UPPJul 11, 2006 · N676UP · Boeing 747123F · Fuselage Main, Floor BeamSDR UPS06447635Floorbeam · damagedINSPECTION TYPE:C U/D RT BS 440 UPPER DECK FLOORBEAM FWD FLANGE 1 FASTENER HOLE FOUND OVAL AT RBL 48. U/DECK BS 440 LBL 68" TO RBL 68" FLOORBEAM UPPER CHORD REPAIRED AS PER SRM 53-10-07 FIG 14.Jul 11, 2006 · N676UP · Boeing 747123F · Fuselage Main, Floor BeamSDR UPS06447599Floorbeam · crackedINSPECTION TYPE:C U/D LEFT BS 520 UPPER DECK FLOORBEAM FWD FLANGE 1EA FASTENER HOLE FOUND CRACK AT LBL 45. CRACK LENGTH 0.030 INCH. U/D BS 520 FLOORBEAM UPPER CHORD FWD FLANGE AT LBL45 AREA HOLE OVERSIZED TO 0.326 INCH AND C/D WAS MEASURED MORE THAN 1.3 PER Jul 11, 2006 · N676UP · Boeing 747123 · Fuselage Main, Floor BeamSDR UPS06447560Floorbeam · corrodedINSPECTION TYPE:C U/D RIGHT BS 520 UPPER DECK FLOORBEAM FWD FLANGE 2EA FASTENER HOLE FOUND CORROSION AT RBL 21 & RBL 25. FASTENER HOLE OVERSIZED TO 0.342" AT RBL 21 AND 0.310" AT RBL 25 AS PER SRM 51-30-05 AS PER UPS EO B747-5310-23043 APP D WITHIN THE LIMITAJul 11, 2006 · N676UP · Boeing 747123 · Fuselage Main, Floor BeamSDR UPS06447559Floorbeam · corrodedINSPECTION TYPE:C U/D RIGHT BS 50 UPPER DECK FLOORBEAM AFT FLANGE 2EA FASTENER HOLE FOUND CORROSION AT RBL16 AND RBL 27. 0.310" & 0.326" OVERSIZED. FASTENER HOLE OVERSIZED TO 0.326" AT RBL 16 & 0.310" AT RBL 27 AS PER SRM 51-30-05 AS PER UPS EO B747-5310-2304Jul 11, 2006 · N676UP · Boeing 747123 · Fuselage Main, Floor BeamSDR UPS06447543Floorbeam · corrodedINSPECTION TYPE:C U/D RT BS 440 UPPER DECK FLOORBEAM AFT FLANGE 1 FASTENER HOLE FOUND CRACK AND CORROSION AT RBL7. CORROSION BLEND OUT 0.032" FASTENER HOLE OVERSIZED TO 0.310" AS PER SRM 51-30-05 AS PER UPS EO B747-5310-23043 APP D WITHIN THE LIMITATION.Jul 11, 2006 · N676UP · Boeing 747123F · Fuselage Main, Floor BeamSDR UPS06447542Floorbeam · corrodedINSPECTION TYPE:C U/D RT BS440 UPPER DECK FLOORBEAM FWD FLANGE 1 FASTENER HOLE FOUND CORROSION AT RBL24. CORROSION BLEND OUT 0.048". FASTENER HOLE OVERSIZED TO 0.326" AS PER SRM 51-30-05 AS PER UPS EO B747-5310-23043 APP D WITHIN THE LIMITATION.Jul 11, 2006 · N676UP · Boeing 747123F · Fuselage Main, Floor BeamSDR UPS06447540Floorbeam · damagedINSPECTION TYPE:C U/D BS440 MOST OF FLOORBEAM FASTENER HOLE FOUND SHORT EDGE BELOW 0.44" AS MARKED AT BETWEEN LBL 44 TO LBL 53 AND RBL 44 TO RBL 53 AREA. U/D BS 440 BETWEEN LBL68 TO RBL68 FLOORBEAM UPPER CHORD REPAIRED AS PER SRM 53-10-07 FIG 14 REFER NRC7031Jul 11, 2006 · N676UP · Boeing 747123F · Fuselage Main, Floor BeamSDR UPS06447539Strap · crackedINSPECTION TYPE:C U/D RT BS520 UPPER DECK FLOORBEAM FWD FLANGE AREA 1 FASTENER HOLE FOUND CRACK AT FLOOR CHORD STRAP AT RBL 35. CRACK LENGTH 0.030". STRAP REPLACED AND INSTALLED AS PER SRM 51-10-01 PG9 AND SRM 51-30-02.Jul 11, 2006 · N676UP · Boeing 747123F · Fuselage Main, Floor BeamSDR UPS06447477Shear Web · crackedFOUND BS 820-840 STR -10L STRINGER ATT SHEAR WEB BOTH END FOUND CRACK (CRACK LENGTH 1"). SHEAR WEB REPLACED AS PER SRM 51-10-01 PG 9.Jul 11, 2006 · N676UP · Boeing 747123F · Fuselage Main, StructureSDR UPS06447475Gusset · crackedRT BS 520 UPPER DECK FLOORBEAM FWD FLANGE AREA 2 FASTENER HOLES FOUND CRACK AT GUSSET AT RBL 35 AND RBL 39.5 (CRACK LENGTH 0.060"). U/DECK BS 820 RBL 31" TO RBL 40" GUSSET REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.Jul 11, 2006 · N676UP · Boeing 747123F · Fuselage Main, Floor BeamSDR UPS06447413Shear Web · crackedBS 820-840 STR -10R STRINGER ATT SHEAR WEB FWD END FOUND CRACKED, CRACK LENGTH 1/2". SHEAR WEB REPAIRED AS PER SRM 51-40-03 FIG 3.Jul 11, 2006 · N676UP · Boeing 747123F · Fuselage Miscellaneous StructureSDR UPS06447701Frame · crackedINSPECTION TYPE-C LT SIDE BS800 FRAME AT STR16 FOUND 1EA HOLE CRACKED AT FRAME STRAP APPROX .0625 INCH LONG RUNNING. CABIN LT SIDE BS800 FRAME ATTACH STRAP BETWEEN STR15L TI STR18L AREA REAIRED IAW RS R53-10-35541. CONTINUE INSPECTION AND SUPPLEMENTAL INSPECTJul 10, 2006 · N676UP · Boeing 747123 · Fuselage Main, FrameSDR UPS06447678Reveal · crackedINSPECTION TYPE:C M/D BS2231 BETWEEN S25L AND 26L REVEAL CRACK, CRACK LENGTH 0.8". M/D BS 2231 BETWEEN STR 25L-STR 26L REVEAL PANEL REPAIRED AS PER RS R53-62-35536 AND UPS EO B747-5310-24836-B.Jul 10, 2006 · N676UP · Boeing 747123F · Fuselage Miscellaneous StructureSDR UPS06447661Floorbeam · corrodedBS 520 LBL 33-47 FLOORBEAM FOUND CORROSION AS MARKED. CORROSION BLEND OUT 0.051" BY 1.5" BY 2" EXCEED SRM 53-10-01 FIG 1 LIMITS, AND U/D BS 520 FLOORBEAM UPPER CHORD REPAIRED AS PER HX RS NR R53-25-35537 REFER NRC NR IB70247 FOR WORKING DETAIL AND REF UPS EO Jul 10, 2006 · N676UP · Boeing 747123F · Fuselage Main, Floor BeamSDR UPS06447615Frame · crackedINSPECTION TYPE:C FWD CARGO COMPT - LT STA 980 STR39 FRAME FOUND CRACKED. CRACK LENGTH 1/2". FWD CARGO COMPT LT STA980 STR39 FRAME REPAIRED AS PER RS R53-10-35553 JUST BETWEEN STR36L AND STR40L AREA CONTINUE INSP IS REQUIRED AS PER RS R53-10-35553 AND UPS EO Jul 10, 2006 · N676UP · Boeing 747123 · Fuselage Main, FrameSDR UPS06447609Skin · corrodedRT BS 579 S44R LAP JOINT LOWEST FASTNENER HOLE FOUND CORROSION INDICATION AT OUTER SKIN AND INNER SKIN INTERFACE. CORROSION BLEND OUT AT INNER SKIN 0.009" BY 7/8" BY 1" AND OUTER SKIN 0.008" BY 3/4" BY 7/8". FX BS 565-622 BETWEEN STR 43R AND 45R OVERLAPPING Jul 10, 2006 · N676UP · Boeing 747123F · Fuselage Main, Plate/SkinSDR UPS06447473Floorbeam · corrodedBS 480 LBL 10- RBL 32 FLOORBEAM UPPER FACE FOUND CORRODED. CORROSION BLEND OUT 0.021" BY 1" BY 2" EXCEED SRM 53-10-01 FIG 1 LIMITS, U/D BS 480 LBL 10" - RBL 32" FLOOR SUPPORT REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.Jul 10, 2006 · N676UP · Boeing 747123F · Fuselage Main, Floor Beam
Back to N676UP, cancelled May 24, 2011