# Service difficulty reports: N677UP, cancelled Jul 23, 2011

A list on [N677UP, cancelled Jul 23, 2011](https://openairdocs.org/deregistered/N677UP-2011-07-23.md).

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

Page 1 of 15 · 702 reports

- [SDR UPS08451589](https://openairdocs.org/sdr/UPS08451589.md): Duct · damaged · Jan 30, 2008 · N677UP · Boeing 747123F · Airfoil Anti/De-ice System
  > WITH 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 H
- [SDR UPS07451337](https://openairdocs.org/sdr/UPS07451337.md): Panel · delaminated · Dec 22, 2007 · N677UP · Boeing 747123F · Wing, Plate/Skin
  > RT 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.
- [SDR UPS07450936](https://openairdocs.org/sdr/UPS07450936.md): Tube · chafed · Oct 18, 2007 · N677UP · Boeing 747123F · Engine Oil Distribution (Airframe Furnished)
  > INSPECTION 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 DOW
- [SDR UPS07450898](https://openairdocs.org/sdr/UPS07450898.md): Intake · clogged · Oct 10, 2007 · N677UP · Boeing 747123F · Instrument Panel
  > LOUD 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 CH
- [SDR UPS07450805](https://openairdocs.org/sdr/UPS07450805.md): Lamp · inoperative · Oct 1, 2007 · N677UP · Boeing 747123F · Emergency Lighting
  > INSPECTION TYPE:N/A EMERGENCY LIGHT INOP L1 DOOR FWD. RELAMPED EMERGENCY LIGHT, OPS CHECK GOOD 747 MM 33-51-00.
- [SDR UPS07450804](https://openairdocs.org/sdr/UPS07450804.md): Light · inoperative · Oct 1, 2007 · N677UP · Boeing 747123F · Emergency Lighting
  > INSPECTION TYPE:N/A EMERGENCY LIGHT INOP MCD CEILING FWD OF CREW ENTRY STAIRS. OPERATION CHECKS NORMAL 747 MM 33-51-00.
- [SDR UPS07450346](https://openairdocs.org/sdr/UPS07450346.md): Panel · delaminated · Jul 27, 2007 · N677UP · Boeing 747123F · Wing, Plate/Skin
  > RT 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 PANE
- [SDR UPS06448663](https://openairdocs.org/sdr/UPS06448663.md): Stiffener · cracked · Nov 7, 2006 · N677UP · Boeing 747123F · Wing Miscellaneous Structure
  > INSPECTION 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.
- [SDR UPS06448692](https://openairdocs.org/sdr/UPS06448692.md): Skin · corroded · Nov 5, 2006 · N677UP · Boeing 747123F · Wing, Plate/Skin
  > INSPECTION 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,
- [SDR UPS06448689](https://openairdocs.org/sdr/UPS06448689.md): Spar · cracked · Oct 29, 2006 · N677UP · Boeing 747123F · Wing Spar
  > INSPECTION 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 ITE
- [SDR UPS06448508](https://openairdocs.org/sdr/UPS06448508.md): Stiffener · cracked · Oct 25, 2006 · N677UP · Boeing 747123F · Service Doors
  > INSPECTION 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.
- [SDR UPS06448485](https://openairdocs.org/sdr/UPS06448485.md): Stringer · cracked · Oct 25, 2006 · N677UP · Boeing 747123F · Fuselage Main, Longeron/Stringer
  > INSPECTION 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.
- [SDR UPS06448519](https://openairdocs.org/sdr/UPS06448519.md): Seat Track · corroded · Oct 24, 2006 · N677UP · Boeing 747123F · Fuselage, Seat/Cargo Attach Fittings
  > BS 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.
- [SDR UPS06448702](https://openairdocs.org/sdr/UPS06448702.md): Skin · cracked · Oct 21, 2006 · N677UP · Boeing 747123F · Passenger/Crew Doors
  > INSPECTION 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 REQUIR
- [SDR UPS06448697](https://openairdocs.org/sdr/UPS06448697.md): Frame · cracked · Oct 21, 2006 · N677UP · Boeing 747123F · Fuselage Main, Frame
  > INSPECTION 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 I
- [SDR UPS06448695](https://openairdocs.org/sdr/UPS06448695.md): Frame · cracked · Oct 21, 2006 · N677UP · Boeing 747123F · Fuselage Main, Frame
  > INSPECTION 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 REQUIRE
- [SDR UPS06448694](https://openairdocs.org/sdr/UPS06448694.md): Frame · cracked · Oct 21, 2006 · N677UP · Boeing 747123F · Fuselage Main, Frame
  > INSPECTION 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 R
- [SDR UPS06448621](https://openairdocs.org/sdr/UPS06448621.md): Skin · cracked · Oct 21, 2006 · N677UP · Boeing 747123F · Fuselage Main, Plate/Skin
  > INSPECTION 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.
- [SDR UPS06448620](https://openairdocs.org/sdr/UPS06448620.md): Web · corroded · Oct 21, 2006 · N677UP · Boeing 747123F · Passenger/Crew Doors
  > INSPECTION 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.
- [SDR UPS06448612](https://openairdocs.org/sdr/UPS06448612.md): Vertical Beam · cracked · Oct 21, 2006 · N677UP · Boeing 747123F · Fuselage Main, Structure
  > INSPECTION 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.
- [SDR UPS06448611](https://openairdocs.org/sdr/UPS06448611.md): Door Frame · cracked · Oct 21, 2006 · N677UP · Boeing 747123F · Fuselage Main, Structure
  > INSPECTION 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.
- [SDR UPS06448607](https://openairdocs.org/sdr/UPS06448607.md): Panel · cracked · Oct 21, 2006 · N677UP · Boeing 747123F · Fuselage Miscellaneous Structure
  > L1 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.
- [SDR UPS06448593](https://openairdocs.org/sdr/UPS06448593.md): Beam · cracked · Oct 21, 2006 · N677UP · Boeing 747123F · Fuselage Miscellaneous Structure
  > NR 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.
- [SDR UPS06448698](https://openairdocs.org/sdr/UPS06448698.md): Skin · cracked · Oct 20, 2006 · N677UP · Boeing 747123F · Fuselage Main, Plate/Skin
  > INSPECTION 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 SSID
- [SDR UPS06448682](https://openairdocs.org/sdr/UPS06448682.md): Floorbeam · corroded · Oct 20, 2006 · N677UP · Boeing 747123F · Fuselage Main, Floor Beam
  > INSPECTION 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.
- [SDR UPS06448669](https://openairdocs.org/sdr/UPS06448669.md): Floorbeam · corroded · Oct 20, 2006 · N677UP · Boeing 747123F · Fuselage Main, Floor Beam
  > INSPECTION 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.
- [SDR UPS06448662](https://openairdocs.org/sdr/UPS06448662.md): Skin · cracked · Oct 20, 2006 · N677UP · Boeing 747123F · Fuselage Main, Plate/Skin
  > INSPECTION 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
- [SDR UPS06448619](https://openairdocs.org/sdr/UPS06448619.md): Floorbeam · corroded · Oct 20, 2006 · N677UP · Boeing 747123F · Fuselage Main, Floor Beam
  > INSPECTION 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.
- [SDR UPS06448599](https://openairdocs.org/sdr/UPS06448599.md): Floorbeam · corroded · Oct 20, 2006 · N677UP · Boeing 747123F · Fuselage Main, Floor Beam
  > BS 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.
- [SDR UPS06448594](https://openairdocs.org/sdr/UPS06448594.md): Seat Track · corroded · Oct 20, 2006 · N677UP · Boeing 747123F · Fuselage, Seat/Cargo Attach Fittings
  > BS 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.
- [SDR UPS06448562](https://openairdocs.org/sdr/UPS06448562.md): Seat Track · corroded · Oct 20, 2006 · N677UP · Boeing 747123F · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION 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.
- [SDR UPS06448558](https://openairdocs.org/sdr/UPS06448558.md): Floorbeam · corroded · Oct 20, 2006 · N677UP · Boeing 747123F · Fuselage Main, Floor Beam
  > INSPECTION 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.
- [SDR UPS06448557](https://openairdocs.org/sdr/UPS06448557.md): Seat Track · corroded · Oct 20, 2006 · N677UP · Boeing 747123F · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION 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.
- [SDR UPS06448556](https://openairdocs.org/sdr/UPS06448556.md): Floorbeam · corroded · Oct 20, 2006 · N677UP · Boeing 747123F · Fuselage Main, Floor Beam
  > INSPECTION 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.
- [SDR UPS06448555](https://openairdocs.org/sdr/UPS06448555.md): Seat Track · corroded · Oct 20, 2006 · N677UP · Boeing 747123F · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION 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).
- [SDR UPS06448553](https://openairdocs.org/sdr/UPS06448553.md): Seat Track · corroded · Oct 20, 2006 · N677UP · Boeing 747123F · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION 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 FO
- [SDR UPS06448552](https://openairdocs.org/sdr/UPS06448552.md): Seat Track · corroded · Oct 20, 2006 · N677UP · Boeing 747123F · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION 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.
- [SDR UPS06448547](https://openairdocs.org/sdr/UPS06448547.md): Seat Track · corroded · Oct 20, 2006 · N677UP · Boeing 747123F · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION 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.
- [SDR UPS06448546](https://openairdocs.org/sdr/UPS06448546.md): Seat Track · corroded · Oct 20, 2006 · N677UP · Boeing 747123F · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION 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.
- [SDR UPS06448545](https://openairdocs.org/sdr/UPS06448545.md): Seat Track · corroded · Oct 20, 2006 · N677UP · Boeing 747123F · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION 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.
- [SDR UPS06448544](https://openairdocs.org/sdr/UPS06448544.md): Seat Track · corroded · Oct 20, 2006 · N677UP · Boeing 747123F · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION 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 1A
- [SDR UPS06448543](https://openairdocs.org/sdr/UPS06448543.md): Seat Track · corroded · Oct 20, 2006 · N677UP · Boeing 747123F · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION 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.
- [SDR UPS06448542](https://openairdocs.org/sdr/UPS06448542.md): Seat Track · corroded · Oct 20, 2006 · N677UP · Boeing 747123F · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION 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.
- [SDR UPS06448526](https://openairdocs.org/sdr/UPS06448526.md): Floorbeam · corroded · Oct 20, 2006 · N677UP · Boeing 747123F · Fuselage Main, Floor Beam
  > INSPECTION 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.
- [SDR UPS06448525](https://openairdocs.org/sdr/UPS06448525.md): Floor Support · corroded · Oct 20, 2006 · N677UP · Boeing 747123F · Fuselage Miscellaneous Structure
  > INSPECTION 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.
- [SDR UPS06448510](https://openairdocs.org/sdr/UPS06448510.md): Floor Panel · corroded · Oct 20, 2006 · N677UP · Boeing 747123F · Fuselage Floor Panel
  > BS 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.
- [SDR UPS06448476](https://openairdocs.org/sdr/UPS06448476.md): Cargo Track · corroded · Oct 20, 2006 · N677UP · Boeing 747123F · Fuselage, Seat/Cargo Attach Fittings
  > BS 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.
- [SDR UPS06448499](https://openairdocs.org/sdr/UPS06448499.md): Seat Track · corroded · Oct 20, 2006 · N677UP · Boeing 747123F · Fuselage, Seat/Cargo Attach Fittings
  > BS 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.
- [SDR UPS06448490](https://openairdocs.org/sdr/UPS06448490.md): Web · corroded · Oct 20, 2006 · N677UP · Boeing 747123F · Fuselage Miscellaneous Structure
  > BS 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.
- [SDR UPS06448489](https://openairdocs.org/sdr/UPS06448489.md): Floor Support · corroded · Oct 20, 2006 · N677UP · Boeing 747123F · Fuselage Miscellaneous Structure
  > BS 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.

Next page: https://openairdocs.org/deregistered/N677UP-2011-07-23/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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
```

This list as a web page: https://openairdocs.org/deregistered/N677UP-2011-07-23/reports

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