N677UP, cancelled Jul 23, 2011

Service difficulty reports · 702

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 = 'N677UP' AND deregistration_id = 'N677UP-2011-07-23'
  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 UPS08451589Duct · damagedWITH WING ANTI-ICE ON, LOUD THUMP HEARD ON LEFT SIDE LEFT WING LE OVHT LIGHT ILLUMINATED. CLOSED LEFT ISOLATION VLV, SHUTOFF NR 1 AND NR 2 BLEED. WING OVHT LIGHT WENT OUT. FOUND MAIN PNEU SUPPLY DUCT WITH DAMAGED FLANGES AND CLAMPS, 2 EA LOWER SKIN PANELS HJan 30, 2008 · N677UP · Boeing 747123F · Airfoil Anti/De-ice SystemSDR UPS07451337Panel · delaminatedRT WING UPPER INBD FIXED TRAILING EDGE PANEL DELAMINATED. REMOVED DISBONDED, DAMAGED SKIN FROM LEADING EDGE ACROSS PANEL TO LWR EDGE IAW 51-40-20. FABRICATED SKIN FILLER. REPLACED PANEL WITH SERVICEABLE PANEL.Dec 22, 2007 · N677UP · Boeing 747123F · Wing, Plate/SkinSDR UPS07450936Tube · chafedINSPECTION TYPE:N/A IFSD - CREW INFORMED FLIGHT CONTROL THAT THE OIL PRESSURE ON NR 1 ENG WAS RUNNING IN THE YELLOW BAND AND OCCASSIONALLY WAS HITTING THE RED LINE. IT WAS ALSO INDICATED THE OIL PRESSURE LIGHT WAS FLICKERING. CREW DELARED EMERGENCY, SHUT DOWOct 18, 2007 · N677UP · Boeing 747123F · Engine Oil Distribution (Airframe Furnished)SDR UPS07450898Intake · cloggedLOUD HUMMING SOUND HEARD 5 TIMES FROM FORWARD INSTRUMENT PANEL, FIRST TWO TIMES WITH STRONG ODOR OF HOT ELECTRONICS. CLEARED CLOGGED AIR INTAKES ON NR 1 AND NR 2 INS CDU'S. INSPECTED FORWARD INSTRUMENTAL PANEL AREA. PERFORMED EQUIPMENT COOLING TEST. ALL CHOct 10, 2007 · N677UP · Boeing 747123F · Instrument PanelSDR UPS07450805Lamp · inoperativeINSPECTION TYPE:N/A EMERGENCY LIGHT INOP L1 DOOR FWD. RELAMPED EMERGENCY LIGHT, OPS CHECK GOOD 747 MM 33-51-00.Oct 1, 2007 · N677UP · Boeing 747123F · Emergency LightingSDR UPS07450804Light · inoperativeINSPECTION TYPE:N/A EMERGENCY LIGHT INOP MCD CEILING FWD OF CREW ENTRY STAIRS. OPERATION CHECKS NORMAL 747 MM 33-51-00.Oct 1, 2007 · N677UP · Boeing 747123F · Emergency LightingSDR UPS07450346Panel · delaminatedRT WING LEADING EDGE, TOP FILLER PANELS OF NR 3 ENGINE 4 INCH X 10 INCH DELAMINATED. DISCOVERED ADDITIONAL DELAM OF INNER SKIN OPPOSITE EXTERIOR SOFT SPOT. REMOVED PANEL FROM AIRCRAFT XZ 1227688, TRIMMED AND PICKED UP HOLES IN NEW PANEL IAW INSTALLED NEW PANEJul 27, 2007 · N677UP · Boeing 747123F · Wing, Plate/SkinSDR UPS06448663Stiffener · crackedINSPECTION TYPE:C RIGHT WING REAR SPAR WEB WS 405 STIFFENER THE SECOND MOST UPPER HOLE FOUND CRACK RUNNING UP APPROX 1 INCH. RIGHT WING REAR SPAR WEB WS 405 STIFFENER UPPER PORTION REPAIRED AS PER SRM 51-40-04 FIG 3.Nov 7, 2006 · N677UP · Boeing 747123F · Wing Miscellaneous StructureSDR UPS06448692Skin · corrodedINSPECTION TYPE:C RIGHT WING WS 402 CORROSION REVEAL AT MATTING SURFACE BETWEEN CHORD AND EXTENSION SKIN (DEFECT FOUND AFTER EXTENSION SKIN LIFT UP) FOR CHORD REPAIR. CORROSION BLEND OUT 0.124" X 2" X 2" & 0.137" X 1.5" X 6" EXCEED SRM 57-30-01 FIG 1 LIMITS, Nov 5, 2006 · N677UP · Boeing 747123F · Wing, Plate/SkinSDR UPS06448689Spar · crackedINSPECTION TYPE:C RIGHT WING REAR SPAR UPPER CHORD HORIZONTAL FLANGE FOUND 1EA FASTENER CRACKED AT WS 410 APPROX 0.030" RUNNING AFT. RIGHT WING REAR SPAR UPPER CHORD HORIZONTAL FLANGE AT WS 410 APPROX AREA CRACKED HOLE A REPAIRED AS PER HX RS R57-22-35684 ITEOct 29, 2006 · N677UP · Boeing 747123F · Wing SparSDR UPS06448508Stiffener · crackedINSPECTION TYPE:C M/D L3 DOOR FWD LWR CORNER REVEAL ATTACH STIFFENER CRACK, CRACK LENGTH 3/8". L3 DOOR FWD LOWER CORNER REVEAL ATTACH STIFFENER REPLACED AND INSTALLED AS PER SRM 51-10-01 PG9 AND 51-30-02.Oct 25, 2006 · N677UP · Boeing 747123F · Service DoorsSDR UPS06448485Stringer · crackedINSPECTION TYPE:C FWD CARGO COMPT RT STRINGER 39R SUSPECT CRACKED AT STA 744 TO STA 745, CRACK LENGTH 1". FWD CARGO COMPT BS 740-770 STR 39R STRINGER REPAIRED AS PER SRM 53-10-03 FIG 1.Oct 25, 2006 · N677UP · Boeing 747123F · Fuselage Main, Longeron/StringerSDR UPS06448519Seat Track · corrodedBS 2040 TO BS 2150 RBL 89 SEAT TRACK BOTTOM FLANGE CORRODED. CORROSION BLEND OUT 0.035" BY 1.5" BY 2" EXCEED SRM LIMIT. SEAT TRACK REPLACED AS PER SRM 51-10-01 P9 JUST AT M/D RBL89 BETWEEN BS2040 AND 2150.Oct 24, 2006 · N677UP · Boeing 747123F · Fuselage, Seat/Cargo Attach FittingsSDR UPS06448702Skin · crackedINSPECTION TYPE:C M/D L3 DOOR EXTERIOR SKIN FOUND CRACKED AT CTR LOWER PORTION. CRACK LENGTH .875 INCH. M/D L3 DOOR EXTERIOR SKIN CTR LOWER PORTION REPAIRED WITH ZERO TIMED AT CRITICAL ROW FASTENER HOLES AS PER SRM 52-10-02 FIG 9 SUBSEQUENT INSPECTION REQUIROct 21, 2006 · N677UP · Boeing 747123F · Passenger/Crew DoorsSDR UPS06448697Frame · crackedINSPECTION TYPE:C LEFT BS 2231 FRAME FOUND CRACKED AT REVEAL AT 3EA LOCATIONS BETWEEN S23L & 25L. CRACK LENGTH .125" & .375" & .625". LEFT BS 2231 FRAME BETWEEN S23L - S25L REVEAL REPAIRED AS PER HX RS R53-00-35672 WORKING DETAIL REF NRC 51422. CONTINUED IOct 21, 2006 · N677UP · Boeing 747123F · Fuselage Main, FrameSDR UPS06448695Frame · crackedINSPECTION TYPE:C RIGHT BS 2231 FRAME FOUND CRACKED AT CHORD AT 2EA FASTENER LOCATION STR 24R & 25R. CRACK LENGTH 0.040" & 0.060". M/D BS 2231 FRAME CHORD REPAIRED AS PER HX RS R53-60-35673 REFER NRC 51427 FOR WORKING DETAIL. CONTINUED INSPECTION IS REQUIREOct 21, 2006 · N677UP · Boeing 747123F · Fuselage Main, FrameSDR UPS06448694Frame · crackedINSPECTION TYPE:C RIGHT BS 2231 FRAME FOUND CRACKED AT REVEAL AT 2EA LOCATIONS BETWEEN STR 24R & 25R. CRACK LENGTH .1875" & .5". M/D BS 2231 FRAME ATTACHED REVEAL REPAIRED AS PER HX RS R53-60-35673 REF NRC 51427 FOR WORKING DETAIL. CONTINUED INSPECTION IS ROct 21, 2006 · N677UP · Boeing 747123F · Fuselage Main, FrameSDR UPS06448621Skin · crackedINSPECTION TYPE-C M/D L3 UPPER HINGE EXT SKIN FOUND CRACKED. CRACK LENGTH .3750 INCH. M/D L3 DOOR UPPER HINGE EXT SKIN REPAIR IAW SRM 52-10-02 FIG 11 AND SB 747-52-2144.Oct 21, 2006 · N677UP · Boeing 747123F · Fuselage Main, Plate/SkinSDR UPS06448620Web · corrodedINSPECTION TYPE-C M/D L5 DOOR LOWER HINGE LOWER WEB FOUND CORRODED. CORROSION BLEND OUT 0.063 INCH X 1INCH X 1.5 INCHES EXCEED SRM LIMIT. HINGE WEB REPLACED AND INSTALLED IAW SRM 51-10-01 PG 9 AND 51-30-02.Oct 21, 2006 · N677UP · Boeing 747123F · Passenger/Crew DoorsSDR UPS06448612Vertical Beam · crackedINSPECTION TYPE-C M/D NR 5R MED FWD LOWER INTERIOR CORNER FOUND VERTICAL BEAM PREVIOUSLY CRACKED. CRACK LENGTH 1.2500 INCH, M/D NR 5R MED FWD LOWER VERTICAL BEAM REPAIRED IAW SRM 52-10-02 FIG 10.Oct 21, 2006 · N677UP · Boeing 747123F · Fuselage Main, StructureSDR UPS06448611Door Frame · crackedINSPECTION TYPE-C M/D L1 DOOR LOWER HINGE CUTOUT FRAME FOUND CRACKED. CRACK LENGTH .3750 INCH, M/D L1 DOOR LOWER HINGE CUTOUT FRAME REPAIRED IAW SRM 52-10-02 FIG 12.Oct 21, 2006 · N677UP · Boeing 747123F · Fuselage Main, StructureSDR UPS06448607Panel · crackedL1 DOOR FWD CUTOUT MID REVEAL PANEL FOUND CRACKED, CRACK LENGTH 3/8". L1 DOOR FWD CUTOUT MID REVEAL PANEL REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.Oct 21, 2006 · N677UP · Boeing 747123F · Fuselage Miscellaneous StructureSDR UPS06448593Beam · crackedNR 4R MED FWD LWR INTERIOR CORNER FOUND VERTICAL BEAM CRACK BEYOND STOP HOLE AND HORIZONTAL BEAM CRACKED, CRACK LENGTH 7/8" AND 1". NR 4R MED FWD LOWER INTERIOR VERT AND HORIZ BEAM REPAIRED AS PER SRM 52-10-02 FIG 10.Oct 21, 2006 · N677UP · Boeing 747123F · Fuselage Miscellaneous StructureSDR UPS06448698Skin · crackedINSPECTION TYPE:C AFT CARGO DOOR COMPT CUTOUT FWD HINGE MOST FWD LWR FASTENER HOLE FOUND CRACK AT SKIN RUNNING UP. CRACKED SKIN TRIMMED OFF. FILLER FABRICATED & INSTALLED WITH INITIAL REPAIR DOUBLERS AS PER HX RS R53-61-35676. CONTINUED INSPECTIONS PER SSIDOct 20, 2006 · N677UP · Boeing 747123F · Fuselage Main, Plate/SkinSDR UPS06448682Floorbeam · corrodedINSPECTION TYPE:C M/D BS 2040 RBL 60 FLOORBEAM FOUND CORROSION. CORROSION BLEND OUT 0.075" X 1/2" X 1" EXCEED SRM LIMIT. M/D BS 2040 RBL 60 FLOORBEAM REPAIRED AS PER RS R53-61-35674 AND UPS ENGINEERING FILE NUMBER 747-53-20364.Oct 20, 2006 · N677UP · Boeing 747123F · Fuselage Main, Floor BeamSDR UPS06448669Floorbeam · corrodedINSPECTION TYPE:C M/D BS 2140 RBL 85 FLOORBEAM FOUND CORRODED. CORROSION BLEND OUT 0.053" X 1" X 2" EXCEED SRM LIMIT. M/D BS 2140 RBL 45 TO RIGHT O/B MOST FLOORBEAM REPAIRED AS PER SRM 51-40-04 FIG 1.Oct 20, 2006 · N677UP · Boeing 747123F · Fuselage Main, Floor BeamSDR UPS06448662Skin · crackedINSPECTION TYPE:C FWD CARGO DOOR CUTOUT FWD HINGE MOST FWD LWR FASTENER HOLE FOUND CRACK AT SKIN RUNNING DOWN APPROX 0.040". FUSELAGE FWD CARGO DOOR CUTOUT FWD HINGE ATTACHED SKIN REPAIRED AS PER HX RS R53-21-35670. CONTINUED INSPECTION IS REQUIRED AS PER HX Oct 20, 2006 · N677UP · Boeing 747123F · Fuselage Main, Plate/SkinSDR UPS06448619Floorbeam · corrodedINSPECTION TYPE-C M/D BS 2260 RBL13-20 FLOORBEAM FOUND CORRODED. CORROSION BLEND OUT 0.023 INCH X 2 INCHES X 2 INCHES EXCEED SRM LIMIT. M/D BS 2260 LBL 8 TO RBL 66 FLOORBEAM REPAIRED IAW SRM 51-40-04 FIG 1.Oct 20, 2006 · N677UP · Boeing 747123F · Fuselage Main, Floor BeamSDR UPS06448599Floorbeam · corrodedBS 520 LBL 26-28 FLOORBEAM UPPER CHORD FOUND CORRODED. CORROSION BLEND OUT 0.054" BY 1" BY 2" EXCEED SRM 53-10-01 FIG 1 LIMITS. FLOORBEAM UPPER CHORD REPAIRED AS PER SRM 51-40-04 FIG 3 REFER NRC NR 50665 FOR WORKING DETAIL.Oct 20, 2006 · N677UP · Boeing 747123F · Fuselage Main, Floor BeamSDR UPS06448594Seat Track · corrodedBS 2190-2200 RBL89 SEAT TRACK FLANGE FOUND CORRODED. (BOTH SIDES) CORROSION BLEND OUT 0.035" BY 5/8" BY 10" EXCEED SRM LIMIT. BS 2150-2230 RBL89 SEAT TRACK REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02.Oct 20, 2006 · N677UP · Boeing 747123F · Fuselage, Seat/Cargo Attach FittingsSDR UPS06448562Seat Track · corrodedINSPECTION TYPE:C M/D BS 1800-1860 RBL75 SEAT TRACK FLANGE AND CROWN FOUND CORRODED. CORROSION BLEND OUT 0.036" BY 5/8" BY 1 3/4" EXCEED SRM LIMIT. M/D SEAT TRACK AT BS 1730-1870 RBL75 REPAIRED AS PER SRM 53-10-05 FIG 1A REFER NRC50940 FOR WORKING DETAIL.Oct 20, 2006 · N677UP · Boeing 747123F · Fuselage, Seat/Cargo Attach FittingsSDR UPS06448558Floorbeam · corrodedINSPECTION TYPE:C M/D BS 1920 RBL74 FLOORBEAM FOUND CORRODED. CORROSION BLEND OUT 0.090" BY 2" BY 2" EXCEED SRM LIMT. FLOORBEAM REPAIRED AS PER SRM 51-40-04 FIG 3 JUST AT M/D BS 1920 BETWEEN RBL33 TO RT MOST O/B.Oct 20, 2006 · N677UP · Boeing 747123F · Fuselage Main, Floor BeamSDR UPS06448557Seat Track · corrodedINSPECTION TYPE:C M/D BS1880-1910 RBL11 SEAT TRACK O/B FLANGE FOUND CORRODED. CORROSION BLEND OUT 0.021" BY 1/2" BY 10" EXCEED SRM LIMIT. SEAT TRACK REPLACED AS PER SRM 51-10-01 P9 JUST AT M/D RBL11 BETWEEN BS 1870 AND 1910.Oct 20, 2006 · N677UP · Boeing 747123F · Fuselage, Seat/Cargo Attach FittingsSDR UPS06448556Floorbeam · corrodedINSPECTION TYPE:C M/D BS 2000 RBL33-50 FLOORBEAM FOUND CORRODED. CORROSION BLEND OUT 0.086" BY 2" BY 10" EXCEED SRM LIMIT. FLOORBEAM REPAIRED AS PER SRM 51-40-04 FIG 3 JUST AT M/D BS 2000 BETWEEN RBL 33 AND RT MOST O/B.Oct 20, 2006 · N677UP · Boeing 747123F · Fuselage Main, Floor BeamSDR UPS06448555Seat Track · corrodedINSPECTION TYPE:C M/D BS1920 RBL33 SEAT TRACK O/B FLANGE FOUND CORRODED. CORROSION BLEND OUT 0.022" BY 1/2" BY 1" EXCEED SRM LIMIT. SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 33 JUST AT M/D RBL33 BETWEEN BS 1810 AND BS 1950 (REFER NRC NO.51784 FOR DETAIL).Oct 20, 2006 · N677UP · Boeing 747123F · Fuselage, Seat/Cargo Attach FittingsSDR UPS06448553Seat Track · corrodedINSPECTION TYPE:C M/D BS 1880-1900 RBL33 SEAT TRACK I/B FLANGE FOUND CORRODED. CORROSION BLEND OUT 0.045" BY 7/8" BY 1 1/8" EXCEED SRM LIMIT. SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 33 JUST AT M/D RBL 33 BETWEEN BS 1810 AND BS 1950 (REFER NRC NO.51784 FOOct 20, 2006 · N677UP · Boeing 747123F · Fuselage, Seat/Cargo Attach FittingsSDR UPS06448552Seat Track · corrodedINSPECTION TYPE:C M/D BS1813 RBL33 SEAT TRACK I/B FLANGE LOWER FACE FOUND CORRODED. CORROSION BLEND OUT 0.040" BY 7/8" BY 1.5" EXCEED SRM LIMIT. SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 33 JUST AT M/D RBL33 BETWEEN BS1810 AND BS 1950.Oct 20, 2006 · N677UP · Boeing 747123F · Fuselage, Seat/Cargo Attach FittingsSDR UPS06448547Seat Track · corrodedINSPECTION TYPE:C M/D BS 2132 LBL89 SEAT TRACK I/B FLANGE FOUND CORRODED. CORROSION BLEND OUT 0.035" BY 5/8" BY 1" EXCEED SRM LIMIT. M/D BS 2150-2230 LBL89 SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 1A.Oct 20, 2006 · N677UP · Boeing 747123F · Fuselage, Seat/Cargo Attach FittingsSDR UPS06448546Seat Track · corrodedINSPECTION TYPE:C M/D BS1800-1820 SEAT TRACK I/B FLANGE FOUND CORRODED. CORROSION BLEND OUT 0.057" BY 7/8" BY 1 7/8" EXCEED SRM LIMIT. M/D BS 1770-1830 LBL33 SEAT TRACK REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED WITH EXISTING SPLICE PER SRM 51-30-02.Oct 20, 2006 · N677UP · Boeing 747123F · Fuselage, Seat/Cargo Attach FittingsSDR UPS06448545Seat Track · corrodedINSPECTION TYPE:C M/D BS 2050-2130 LBL97 SEAT TRACK FLANGE FOUND CORRODED (BOTH SIDE). CORROSION BLEND OUT 0.035" BY 3/4" BY 1.5" EXCEED SRM LIMIT. M/D BS 2030-2150 LBL 98 SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 1A.Oct 20, 2006 · N677UP · Boeing 747123F · Fuselage, Seat/Cargo Attach FittingsSDR UPS06448544Seat Track · corrodedINSPECTION TYPE:C M/D BS2160 RBL 65 SEAT TRACK FLANGE FOUND CORRODED. CORROSION BLEND OUT 0.022" BY 1/2" BY 3" EXCEED SRM LIMIT. M/D BS 2110-2240 RBL 65 SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 1AOct 20, 2006 · N677UP · Boeing 747123F · Fuselage, Seat/Cargo Attach FittingsSDR UPS06448543Seat Track · corrodedINSPECTION TYPE:C M/D BS 2220-2240 RBL65 SEAT TRACK O/B FLANGE FOUND CORRODED. CORROSION BLEND OUT 0.026" BY 5/8" BY 20" EXCEED SRM LIMIT. M/D BS 2110-2240 RBL65 SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 1A REFER NRC 51776 FOR WORKING DETAIL.Oct 20, 2006 · N677UP · Boeing 747123F · Fuselage, Seat/Cargo Attach FittingsSDR UPS06448542Seat Track · corrodedINSPECTION TYPE:C M/D SEAT TRACK FLANGE FOUND CORRODED BOTH I/B AND O/B. CORROSION BLEND OUT 0.043" BY 3/4" BY 1.5" EXCEED SRM LIMIT. M/D BS1890-2030 LBL 33 SEAT TRACK REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.Oct 20, 2006 · N677UP · Boeing 747123F · Fuselage, Seat/Cargo Attach FittingsSDR UPS06448526Floorbeam · corrodedINSPECTION TYPE:C M/D BS 2280 LBL60-70 FLOORBEAM FOUND CORROSION. CORROSION BLEND OUT 0.045" X 1.5" 2" EXCEED SRM LIMIT. FLOORBEAM REPAIRED AS PER SRM 51-40-04 FIG 1, JUST AT M/D BS2280 BETWEEN LBL 50 AND LT MOST O/B.Oct 20, 2006 · N677UP · Boeing 747123F · Fuselage Main, Floor BeamSDR UPS06448525Floor Support · corrodedINSPECTION TYPE:C M/D BS 2208 RBL 93 FLOOR SUPPORT FOUND CORROSION. CORROSION BLEND OUT 0.020" BY 1/2" BY 1" EXCEED SRM LIMIT. M/D BS 2200-2220 RBL 93 FLOOR SUPPORT REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.Oct 20, 2006 · N677UP · Boeing 747123F · Fuselage Miscellaneous StructureSDR UPS06448510Floor Panel · corrodedBS 2180-2200 LBL99-100 FLOOR WEB FOUND CORROSION. M/D BS 2180-2200 LBL 99-100 FLOOR WEB REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.Oct 20, 2006 · N677UP · Boeing 747123F · Fuselage Floor PanelSDR UPS06448476Cargo Track · corrodedBS 1680 RBL86 TIE DOWN FTG FLANGE FOUND CORROSION. CORROSION BLEND OUT 0.033" BY 1/2" BY 1/2" EXCEED SRM LIMIT. TIE DOWN FTG PLATE REPLACED AS PER MM 20-51-01.Oct 20, 2006 · N677UP · Boeing 747123F · Fuselage, Seat/Cargo Attach FittingsSDR UPS06448499Seat Track · corrodedBS 2060-2080 RBL75 SEAT TRACK O/B FLANGE FOUND CORROSION. CORROSION BLEND OUT 0.030" BY 1/2" BY 1.5". SEAT TRACK REPLACED AS PER SRM 53-10-05 FIG 1A JUST AT M/D, RBL75 BETWEEN STA 2010 AND 2110.Oct 20, 2006 · N677UP · Boeing 747123F · Fuselage, Seat/Cargo Attach FittingsSDR UPS06448490Web · corrodedBS 2160-2180 LBL 97-100 FLOOR WEB FOUND CORROSION. CORROSION BLEND OUT 0.050" BY 5/8" BY 1" EXCEED SRM LIMIT. BS 2160-2180 LBL97-100 FLOOR WEB REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.Oct 20, 2006 · N677UP · Boeing 747123F · Fuselage Miscellaneous StructureSDR UPS06448489Floor Support · corrodedBS 1930 RBL 118 FLOOR SUPPORT FOUND CORROSION. CORROSION BLEND OUT 0.021" BY 1" BY 1" EXCEED SRM LIMIT. BS 1920-1940 RBL 118 FLOOR SUPPORT REPAIRED AS PER SRM 51-40-04 FIG 2.Oct 20, 2006 · N677UP · Boeing 747123F · Fuselage Miscellaneous Structure
Back to N677UP, cancelled Jul 23, 2011