# Service difficulty reports: N672UP, cancelled Jul 19, 2010

A list on [N672UP, cancelled Jul 19, 2010](https://openairdocs.org/deregistered/N672UP-2010-07-19.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 10 · 474 reports

- [SDR UPS08451374](https://openairdocs.org/sdr/UPS08451374.md): Engine · power loss · Jan 4, 2008 · N672UP · Boeing 747123 · Engine (Turbine/Turboprop)
  > INSPECTION TYPE:N/A IFSD - AT FL360 AT CRUISE NR 3 ENG ROLLED BACK, CHECK FUEL PANEL ENG HAD PRESS VIA X FEED. ENG STILL ROLLING BACK. PLACED IGN TO FLT START, TEMP STARTED TO OVERTEMP. SHUT ENG DOWN. DESCENDED TO 28000. DID INFLIGHT RESTART AND ENG START
- [SDR UPS07451230](https://openairdocs.org/sdr/UPS07451230.md): Hose · burned · Dec 1, 2007 · N672UP · Boeing 747123 · Propeller/Rotor Anti-Ice/De-Ice System
  > INSPECTION TYPE:A CK DURING INSPECTION OF EO FOUND WATER DRAIN TUBE CRUSHED AND BURNED. ALSO, FOUND EVIDENCE OF BURNED INSULATION BLANKET REF EO B747-3670-27749B. ORDERED NEW HOSE ON REQ A940808. WORKING WITH ENG ON INSULATION. REPLACE HOSE ASSY PER B747-3
- [SDR UPS07450701](https://openairdocs.org/sdr/UPS07450701.md): Power Supply · inoperative · Sep 20, 2007 · N672UP · Boeing 747123 · Emergency Lighting
  > INSPECTION TYPE:N/A CREW SERVICE DOOR EMERGENCY SLIDE LIGHT INOP. REMOVED & REPLACED POWER SUPPLY MODULE X327 REF WD 33-51-12 AND MM 33-51-04, OPS CHECK GOOD.
- [SDR UPS07450049](https://openairdocs.org/sdr/UPS07450049.md): Water Separator · cracked · Jun 26, 2007 · N672UP · Boeing 747123 · Humidity Control System
  > ATB - AFTER T/O, NR 3 PACK WOULD NOT OPERATE. ZERO AIRFLOW. NO FUNCTION. SWITCHES AND C/B'S RECYCLED. TRIED IN MAN/AUTO. NO HELP. NOTE: ISOLATION A BLEED VALVES OPEN WITH NORMAL DUCT PRESSURE. T/S PERFORMED. FOUND NR 3 PACK WATER SEPARATOR FROZEN UP. W
- [SDR UPS07449798](https://openairdocs.org/sdr/UPS07449798.md): Panel · cracked · May 14, 2007 · N672UP · Boeing 747123 · Wing, Plate/Skin
  > LEFT WING LOWER T/E PANEL HAS 5 FT CRACK. A/C IS OOS. [SUP 05-21-07] REMOVED PANEL FROM A/C. SENT TO SHEETMETAL SHOP. PANEL REINSTALLED IAW EO B747-5720-6416E.
- [SDR UPS07449324](https://openairdocs.org/sdr/UPS07449324.md): Door · malfunctioned · Mar 5, 2007 · N672UP · Boeing 747123 · Landing Gear Door Retract Section
  > NOSE GEAR DOORS OPENING DURING FLIGHT. REMOVED AND REPLACED NOSE GEAR DOOR SEQUENCE VALVE. OPS CHECK NORMAL. OK FOR CONTINUED SERVICE.
- [SDR UPS07449286](https://openairdocs.org/sdr/UPS07449286.md): Unknown · unknown · Mar 3, 2007 · N672UP · Boeing 747123 · Brake
  > DURING LANGING GEAR ROLL AT APPROX 95 KNOTS APPLIED MAXIMUM BRAKING EFFORT (BRAKE PEDALS PUSHED TO END OF THROW) AND THE ANTI SKID DID NOT CYCLE. ACCOMPLISHED HYD BRAKE SYS. ADJ/TEST MM 32-41-00. NO FAULT NOTED. ALL SATISFACTORY. CHECKED CABLE TENSIONS PE
- [SDR UPS07449282](https://openairdocs.org/sdr/UPS07449282.md): Brake · stiff · Mar 2, 2007 · N672UP · Boeing 747123 · Brake
  > BTB - APPLIED MAX BRAKING EFFORT AT 15 KNOTS GROUND SPEED. A/C CAME TO A SLOW GENTLE STOP. BRAKE PEDAL TRAVEL AND RESISTANCE IS INCONSISTANT WITH NORMAL BRAKING FEEL. T/S HYD BRAKE SYS IAW MM 32-41-00. CLEANED AND LUBED CABLE QUADRANTS. OPS CHECK NORMAL.
- [SDR UPS07449269](https://openairdocs.org/sdr/UPS07449269.md): Brake · failed · Mar 1, 2007 · N672UP · Boeing 747123 · Landing Gear Brake System
  > INSPECTION TYPE:N/A BTB - BRAKES BOTTOMED OUT DURING TAXI. BLED BRAKE SYS IAW 32-41-00. CK'D CABLE TENSION IAW AMM 32-41-00, PG 501. CABLE TENSION CKS GOOD. TAXIED A/C BRAKES OPERATE NORMAL IAW AMM 32-41-00 PG 1. OK FOR SERVICE.
- [SDR UPS07449236](https://openairdocs.org/sdr/UPS07449236.md): Battery Pack · inoperative · Feb 23, 2007 · N672UP · Boeing 747123 · Emergency Lighting
  > INSPECTION TYPE:N/A AFT EMERGENCY LIGHT IN MAIN ENTRY DOOR INOP. RELAMP, NO HELP. REMOVED AND REPLACED BATTERY PACK PER CHAPTER 33. OPS CHECKS OK.
- [SDR UPS07449117](https://openairdocs.org/sdr/UPS07449117.md): Skin · punctured · Jan 31, 2007 · N672UP · Boeing 747123 · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C FX- BS 203 RBL 3" EXTERIOR SKIN FOUND PUNCTURED, CRACK LENGTH 1/2". FX EXTERIOR SKIN REPAIRED AS PER SRM 53-30-03 FIG 1, JUST BETWEEN BS 195 AND 208 STR -1L AND STR -1R.
- [SDR UPS07449013](https://openairdocs.org/sdr/UPS07449013.md): Seat Track · corroded · Jan 23, 2007 · N672UP · Boeing 747123 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION TYPE:C FWD CARGO COMPT SEAT TRACK FOUND CORROSION AT STA 980 LBL 25. FWD CARGO COMPT BS 930 TO BS 980 LBL 25 AREA TRACK REPAIRED AS PER SRM 53-10-05 FIG 5.
- [SDR UPS07449012](https://openairdocs.org/sdr/UPS07449012.md): Stringer · cracked · Jan 22, 2007 · N672UP · Boeing 747123 · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE:C AFT OF BULK CARGO COMPT STR 32R BETWEEN BS 2200 TO BS 2220 FOUND 1EA HOLE CRACK AS MARKED (AFTER SKIN TRIMMED OFF) CRACK LENGTH.125 INCH. AFT OF BULK CARGO COMPT BETWEEN BS 2181 TO BS 2220 STR 32R REPAIRED AS PER SRM 53-10-03 FIG 1.
- [SDR UPS07449086](https://openairdocs.org/sdr/UPS07449086.md): Stringer · cracked · Jan 21, 2007 · N672UP · Boeing 747123 · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE:C LEFT SIDE BS 460 STR 15 STRINGER FASTENER HOLE CRACK FOUND RUNNING TO UPPER EDGE AND RUNNING DOWNWARD APPROX.25 INCH, CRACK LENGTH.5 INCH. M/D LEFT BS 460 STR 15L STRINGER REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.
- [SDR UPS07449085](https://openairdocs.org/sdr/UPS07449085.md): Stringer · corroded · Jan 15, 2007 · N672UP · Boeing 747123 · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE:C M/D AFTER BS 1800-1820 RIGHT WINDOW FORGING REMOVED FOUND STR 22R AFTER END CORRODED. CORROSION BLEND OUT 0.080 X.5 X 2 INCHES EXCEED SRM LIMIT. M/D BS 1740-1960 STR 22R STRINGER REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02
- [SDR UPS07449083](https://openairdocs.org/sdr/UPS07449083.md): Stringer · corroded · Jan 15, 2007 · N672UP · Boeing 747123 · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE:C M/D AFTER BS 1920 TO BS 1940 RIGHT WINDOW FORGING REMOVED, STR 22R FOUND CORROSION AS MARKED. CORROSION BLEND OUT 0.040 X.5 X 3 INCHES EXCEED SRM LIMIT. M/D BS 1740-1960 STR 22R STRINGER REPLACED AND INSTALLED AS PER SRM 51-10-01 AND 51-30
- [SDR UPS07449082](https://openairdocs.org/sdr/UPS07449082.md): Stringer · corroded · Jan 15, 2007 · N672UP · Boeing 747123 · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE:C M/D AFTER BS 1760-1780 RIGHT WINDOW FORGING REMOVED FOUND STR 22R FWD END CORRODED AS MARKED. CORROSION BLEND OUT 0.039 X 1 X 3 INCHES EXCEED SRM LIMIT. M/D BS 1740-1960 STR 22R STRINGER REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 5
- [SDR UPS07449151](https://openairdocs.org/sdr/UPS07449151.md): Stringer · cracked · Jan 11, 2007 · N672UP · Boeing 747123 · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE:C AFT OF BULK CARGO COMPT - FX STRINGER FOUND CRACK AT BS 2177 STR 28 RIGHT AS MARKED. CRACK LENGTH 1.25 INCH. AFT OF BULK CARGO COMPT FX STRINGER S28R AT BS 2177 AREA REPAIRED AS PER RS R53-62-35735 AND UPS ENGINEERING FILE NR 747-53-20377.
- [SDR UPS07449114](https://openairdocs.org/sdr/UPS07449114.md): Stringer Clip · corroded · Jan 11, 2007 · N672UP · Boeing 747123 · Fuselage Main, Attach Fittings
  > INSPECTION TYPE:C AFT CARGO COMPT - STRINGER CLIP FOUND CORRODED AT STA1860 S43R INSIDE OF TORQUE BOX. CORROSION BLEND OUT 0.040 X.5 X.5 INCH EXCEED SRM LIMIT. STRINGER CLIP REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02.
- [SDR UPS07449100](https://openairdocs.org/sdr/UPS07449100.md): Support Fitting · cracked · Jan 11, 2007 · N672UP · Boeing 747123 · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C FWD CARGO COMPT AFT FIXED STOP SUPPORT FITTING LWR SURFACE FOUND CRACK AT STA 980 RBL 45. CRACK LENGTH 2 INCHES. FWD CARGO COMPT AFT FIXED STOP SUPPORT FITTING REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02.
- [SDR UPS07449088](https://openairdocs.org/sdr/UPS07449088.md): Fitting · cracked · Jan 11, 2007 · N672UP · Boeing 747123 · Fuselage Main, Attach Fittings
  > INSPECTION TYPE:C FWD CARGO COMPT AFT FIXED STOP SUPPORT FITTING LOWER SURFACE FOUND CRACK AT STA 980 LBL 45. CRACK LENGTH 4 INCHES. FWD CARGO COMPT BS 980 LBL 45 AFT FIXED STOP SUPPORT FITTING REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.
- [SDR UPS07449081](https://openairdocs.org/sdr/UPS07449081.md): Angle · corroded · Jan 11, 2007 · N672UP · Boeing 747123 · Fuselage Main, Attach Fittings
  > INSPECTION TYPE:C AFT CARGO COMPT STA 1480 BULKHEAD LOWER ANGLE FOUND CORRODED AT LBL 25. CORROSION BLEND OUT 0.053 X.5 X 2 INCHES EXCEED SRM LIMIT. ANGLE REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02.
- [SDR UPS07449080](https://openairdocs.org/sdr/UPS07449080.md): Angle · corroded · Jan 11, 2007 · N672UP · Boeing 747123 · Fuselage Main, Attach Fittings
  > INSPECTION TYPE:C AFT CARGO COMPT STA 1480 BULKHEAD LOWER ANGLE FOUND CORRODED AT RBL 25. CORROSION BLEND OUT 0.060 X.5 X 3 INCHES EXCEED SRM LIMIT. ANGLE REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02.
- [SDR UPS07449079](https://openairdocs.org/sdr/UPS07449079.md): Floorbeam · corroded · Jan 11, 2007 · N672UP · Boeing 747123 · Fuselage Main, Floor Beam
  > INSPECTION TYPE:C AFT CARGO COMPT - LEFT FLOORBEAM LOWER SURFACE FOUND SURFACE CORROSION AT STA 1820 LBL 42 TO LBL 45 ANCHOR NUT AREA. CORROSION BLEND OUT 0.041 X 2 X 3 INCHES EXCEED SRM LIMIT. AFT CARGO COMPT - LEFT FLOORBEAM REPAIRED AT BS 1820 LBL 20 TO L
- [SDR UPS07449063](https://openairdocs.org/sdr/UPS07449063.md): Fitting · cracked · Jan 11, 2007 · N672UP · Boeing 747123F · Nacelle/Pylon, Main Frame
  > NR 3 PYLON FWD B/H I/B HANGER FTG AREA FASTENER REMOVED UPPERR HOLE AT T/R SYNC LOCK MOD HFEC INSP FOUND WITH CRACK INDICATION, CRACK LENGTH 0.030". NR 3 PYLON FWD BULKHEAD CHORD REPLACED AS PER SRM 51-10-01 P9.
- [SDR UPS07449059](https://openairdocs.org/sdr/UPS07449059.md): Stringer · cracked · Jan 11, 2007 · N672UP · Boeing 747123F · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE:C AFT OF BULK CARGO COMPT, FX STRINGER FOUND CRACK AT BS 2177 S46R AS MARKED, CRACK LENGTH 2". FX BS 2150 TO BS 2185 STR 46R STRINGER REPAIRED AS PER SRM 53-10-03 FIG 1.
- [SDR UPS07449034](https://openairdocs.org/sdr/UPS07449034.md): Skin · corroded · Jan 11, 2007 · N672UP · Boeing 747123F · Fuselage Main, Plate/Skin
  > AFT BULK CARGO COMPT FX SKIN FOUND CORRODED BTN BS 2200 TO BS 2220 STR 33R TO 34R AS MARKED. CORROSION BLEND OUT 0.035" BY 1/2" BY 4" EXCEED SRM LIMIT. FX BS 2193 TO BS 2217 BTN STR 31R TO STR 34R SKIN REPAIRED AS PER SRM 53-30-03 FIG 17.
- [SDR UPS07449010](https://openairdocs.org/sdr/UPS07449010.md): Cargo Track · corroded · Jan 11, 2007 · N672UP · Boeing 747123 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION TYPE:C M/D BS 2040-2060 RBL12 TIE DOWN TRACK FLANGE AREA LWR FACE FOUND CORROSION AS MARKED. M/D BS 2030-2130 RBL 11-33 TIE DOWN TRACK REPAIRED AS PER SRM 53-10-05 FIG 14.
- [SDR UPS07449008](https://openairdocs.org/sdr/UPS07449008.md): Beam · cracked · Jan 11, 2007 · N672UP · Boeing 747123 · Passenger/Crew Doors
  > INSPECTION TYPE:C LT MED NR 4 FWD VERTICAL BEAM INTERIOR LOWER CORNER FOUND CRACKED. LT MED NR 4 FWD VERTICAL BEAM LOWER CORNER AREA REPAIRED AS PER SRM 52-10-02 FIG 10.
- [SDR UPS07449006](https://openairdocs.org/sdr/UPS07449006.md): Floor Support · cracked · Jan 11, 2007 · N672UP · Boeing 747123 · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C AFT CARGO COMPT FLOOR SUPPORT FOUND CRACKED AT STA 1775 RBL 40. AFT CARGO COMPT FLOOR SUPPORT REPAIRED AS PER SRM 51-40-03 FIG 1, JUST AT STA 1775 RBL 40 AREA.
- [SDR UPS07449004](https://openairdocs.org/sdr/UPS07449004.md): Support Fitting · cracked · Jan 11, 2007 · N672UP · Boeing 747123 · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C FWD CARGO COMPT AFT FIXED STOP SUPPORT FITTING LOWER SURFACE FOUND CRACK AT STA 980 RBL 25. CRACK LENGTH 2 INCHES. FWD CARGO COMPT AT BS 980 RBL 25 AFT FIXED STOP SUPPORT FITTING REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51
- [SDR UPS07448983](https://openairdocs.org/sdr/UPS07448983.md): Splice · corroded · Jan 11, 2007 · N672UP · Boeing 747123 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION TYPE:C M/D RBL 11 SEAT TACK I-BEAM BS 1740-1760 LWR SPLICE CORRODED. M/D BS 1740-1760 RBL 11 SEAT TRACK I-BEAM LWR SPLICE REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02.
- [SDR UPS07448988](https://openairdocs.org/sdr/UPS07448988.md): Frame · cracked · Jan 11, 2007 · N672UP · Boeing 747123 · Nacelle/Pylon, Frame/Spar/Rib
  > INSPECTION TYPE:C NR 2 PYLON UPPER WING CAVITY O/B FRAME AT NAC STA 237 TOP CORNER AREA CRACKED AS RED MARKED. NR 2 PYLON AT NAC STA 237 O/B FRAME REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND SRM 51-30-02.
- [SDR UPS07448986](https://openairdocs.org/sdr/UPS07448986.md): Tie Clip · cracked · Jan 11, 2007 · N672UP · Boeing 747123 · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C M/D BS 1960 STR 3L FRAME ATT TIE CLIP FOUND CRACK. M/D BS 1960 STR 3L FRAME ATT TIE CLIP REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02.
- [SDR UPS07448973](https://openairdocs.org/sdr/UPS07448973.md): Stringer · corroded · Jan 11, 2007 · N672UP · Boeing 747123 · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE:C AFT CARGO COMPT STRINGER FOUND CORRODED AT STA1640 S40R. AFT CARGO COMPT BS 1632 TO BS 1648 STR 40R STRINGER REPAIRED AS PER SRM 53-10-03 FIG 1.
- [SDR UPS07448967](https://openairdocs.org/sdr/UPS07448967.md): Shear Tie · cracked · Jan 11, 2007 · N672UP · Boeing 747123 · Fuselage Internal Mounting Structure
  > INSPECTION TYPE:C AFT CARGO COMPT - BELOW FLOOR BILGE AREA SUPPORT FRAME SHEAR TIE FOUND CRACKED AT STA 1740 STR 44L TO STR 47L (3EA). AFT CARGO COMPT BS 1740 BETWEEN STR -43L TO STR 47L AREA SHEAR TIE REPAIRED AND TIE CLIPS 5EA REPLACED AS PER SRM 53-10-04 F
- [SDR UPS07448959](https://openairdocs.org/sdr/UPS07448959.md): Seat Track · corroded · Jan 11, 2007 · N672UP · Boeing 747123 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION TYPE:C M/D BS 980 RBL 11 SEAT TRACK O/B FLANGE FOUND CORROSION. M/D BS 950-1000 RBL 11 SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 14.
- [SDR UPS07448958](https://openairdocs.org/sdr/UPS07448958.md): Seat Track · corroded · Jan 11, 2007 · N672UP · Boeing 747123 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION TYPE:C M/D BS 1850 LBL 33 SEAT TRACK I/B FLANGE FOUND CORRODED. M/D BS 1830-1870 LBL 33 SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 1A.
- [SDR UPS07448952](https://openairdocs.org/sdr/UPS07448952.md): Intercostal · deformed · Jan 11, 2007 · N672UP · Boeing 747123 · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C AFT OF BULK CARGO COMPT FX FRAME INTERCOSTAL WEB FOUND DEFORMED BETWEEN BS 2220 AND BS 2240 STR 40R AS MARKED. AFT OF BULK CARGO COMPT FX FRAME INTERCOSTAL WEB REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02 JUST AT BS 22
- [SDR UPS07448935](https://openairdocs.org/sdr/UPS07448935.md): Web · cracked · Jan 11, 2007 · N672UP · Boeing 747123 · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE:C M/D BS 820-840 STR 10R STRINGER ATT WEB FWD CORNER AREA FOUND CRACK. M/D BS 820-840 STR 10R STRINGER ATT WEB FWD CORNER AREA REPAIRED AS PER SRM 51-40-02 FIG 1.
- [SDR UPS07448934](https://openairdocs.org/sdr/UPS07448934.md): Web · cracked · Jan 11, 2007 · N672UP · Boeing 747123 · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE:C M/D BS 820-840 STR 10L STRINGER ATT WEB FWD CORNER AREA FOUND CRACK. M/D BS 820-840 STR 10L STRINGER ATT WEB FWD CORNER AREA REPAIRED AS PER SRM 51-40-02 FIG 1.
- [SDR UPS07448933](https://openairdocs.org/sdr/UPS07448933.md): Stringer · cracked · Jan 11, 2007 · N672UP · Boeing 747123 · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE:C AFT OF BULK CARGO COMPT - FX STRINGER FOUND CORROSION CRACK AT BS 2177 STR 48 RT AS MARKED. AFT OF BULK CARGO COMPT - FX STRINGER 48R REPAIRED AS PER SRM 53-10-03 FIG 1, JUST BETWEEN BS 2150 AND 2185 AREA.
- [SDR UPS07449099](https://openairdocs.org/sdr/UPS07449099.md): Seat Track · corroded · Jan 10, 2007 · N672UP · Boeing 747123 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION TYPE:C FWD CARGO COMPT RIGHT SIDE SEAT TRACK LWR SURFACE FOUND CORROSION AT STA 957 TO 964 RBL 45. CORROSION BLEND OUT 0.045 X.5 X 7 INCHES EXCEED SRM LIMIT. SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 5, JUST AT RBL 45 BETWEEN BS 930 AND 967.
- [SDR UPS07449098](https://openairdocs.org/sdr/UPS07449098.md): Stringer · corroded · Jan 10, 2007 · N672UP · Boeing 747123 · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE:C BULK CARGO COMPT STRINGER FOUND CORRODED AT STA 2150 TO 2160 S31L. CORROSION BLEND OUT 0.080 X.375 X 1.5 INCH EXCEED SRM LIMIT. STRINGER 31L REPAIRED AS PER SRM 53-10-03 FIG 2, JUST BETWEEN BS 2156 AND BS 2170.
- [SDR UPS07449078](https://openairdocs.org/sdr/UPS07449078.md): Support Fitting · cracked · Jan 10, 2007 · N672UP · Boeing 747123 · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C LEFT BLG ACTUATOR UPPER SUPPORT FITTING I/B LUG BORE FOUND CRACKED. CRACK LENGTH 0.25 INCH. LEFT BLG ACTUATOR UPPER SUPPORT FITTING REPLACED IAW UPS EO B747-5340-0994-D APP 8.4 TO 8.6.
- [SDR UPS07449077](https://openairdocs.org/sdr/UPS07449077.md): Longeron · corroded · Jan 10, 2007 · N672UP · Boeing 747123 · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE:C L/G - RIGHT WLG W/W OVERWING LONGERON WEB UPPER SURFACE AT BS 1258-1261 FOUND CORROSION AND CRACKED. CORROSION BLEND OUT 0.055 X.5 X 3 INCHES EXCEED SRM LIMIT. L/G - RIGHT WLG W/W OVERWING LONGERON WEB REPLACED AT BS 1254-1264 AS PER SRM 5
- [SDR UPS07449062](https://openairdocs.org/sdr/UPS07449062.md): Floor Support · cracked · Jan 10, 2007 · N672UP · Boeing 747123F · Fuselage Miscellaneous Structure
  > FOUND RBL117 FLR SUPPORT BS 1525-1535 CRACKED, CRACK LENGTH 7/8". BS 1525-1535 RBL117 FLOOR SUPPORT REPAIRED AS PER SRM 51-40-04 FIG 2.
- [SDR UPS07449029](https://openairdocs.org/sdr/UPS07449029.md): Plate · corroded · Jan 10, 2007 · N672UP · Boeing 747123 · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C M/D - BS 1760 FLOOR SUPPORT PLATE RBL 50-55 CORRODED. CORROSION BLEND OUT 0.045 X.5 X 1 INCH EXCEED SRM LIMIT. SUPPORT PLATE REPLACED AS PER SRM 53-40-00.
- [SDR UPS07449016](https://openairdocs.org/sdr/UPS07449016.md): Floor Support · corroded · Jan 10, 2007 · N672UP · Boeing 747123 · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C M/D BS 2152 LBL100 FLOOR SUPPORT FOUND CORRODED. CORROSION BLEND OUT 0.050 X.5 X 1 INCH EXCEED SRM LIMIT. FLOOR SUPPORT REPAIRED AS PER SRM 51-40-04 FIG 2, JUST AT LBL 100 BETWEEN BS 2130 AND 2160.
- [SDR UPS07449015](https://openairdocs.org/sdr/UPS07449015.md): Seat Track · corroded · Jan 10, 2007 · N672UP · Boeing 747123 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION TYPE:C M/D BS 2040-2140 RBL 98 SEAT TRACK CROWN ATT BOLTS AREA FOUND CORRODED. CORROSION BLEND OUT 0.070 X.75 X 3 INCHES EXCEED SRM LIMIT. SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 1A, JUST AT RBL 98 BETWEEN BS 2090 AND 2150.

Next page: https://openairdocs.org/deregistered/N672UP-2010-07-19/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 = 'N672UP' AND deregistration_id = 'N672UP-2010-07-19'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N672UP-2010-07-19/reports

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