N675UP, cancelled Jul 19, 2010

Service difficulty reports · 387

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 = 'N675UP' AND deregistration_id = 'N675UP-2010-07-19'
  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 UPS05445843Battery · dischargedEMERGENCY LIGHT OVER THE FLT DECK STAIRS INOP (LOW BATTERY). REMOVED AND REPLACED EMERGENCY LIGHT ASSY IAW MM 33-51-00, OPS NORMAL.Nov 27, 2005 · N675UP · Boeing 747123 · Emergency LightingSDR UPS05444912Indication Sys · malfunctionedNR 3 ENG N2 REACH 112 PERCENT DURING DEPARTURE. THRUST REVERSE LEVERS IDLE AND N2 WAS 10 PERCENT OR HIGHER THAN OTHER ENGS. NR 3 ENG SHUTDOWN AND RETURNED TO FIELD. DUMPED FUEL AND DECLARED EMERGENCY. ATB, INTERCHANGED ENG NR 2 AND 3 N2 INDS. ENG GRND RUN UPJul 17, 2005 · N675UP · Boeing 747123F · Engine RPM Indicating SystemSDR UPS05444888Web · crackedNLG RT SIDE WEB FOUND CRACKED AT STA 300 WL 150. CRACK LENGTH 0.25 IN. NLG W/W RHS SIDE WEB REPAIRED AT BS 300 WL 150 AREA AS PER SRM 53-10-04 FIG 116.Jul 12, 2005 · N675UP · Boeing 747123F · Fuselage Miscellaneous StructureSDR UPS05444468Floorbeam · damagedFLOORBEAM AT STA 1800 HAS ELONGATED HOLES. A/C OOS AND WILL REQUIRE MX FERRY (9127) TO SAT. INSTALLED FREEZE PLUG AT STA 1800 LBL 99 IN FLOORBEAM IAW SA SK 675-800542.May 15, 2005 · N675UP · Boeing 747123 · Fuselage Main, Floor BeamSDR UPS05444027Control Module · intermittentINSPECTION TYPE:N/A EMERGENCY LIGHT CONTROL SWITCH INTERMITTENT FOR EMERGENCY LIGHTS. REMOVED AND REPLACED EMERGENCY LIGHTS CONTROL MODULE AS PER MM 33-51-09, OPS CHECKS OK.Mar 4, 2005 · N675UP · Boeing 747123 · Emergency LightingSDR UPS05443829Stringer · crackedBS 1560 - 1580 AFT RHS WINDOW FORGING REMOVED FOUND STRINGER CORROSION CRACKED. CORROSION BLEND OUT 0.040" BY 1" BY 5" EXCEED SRM LIMIT. NEW STRINGER SEGMENT AND SPLICE ANGLE INSTALLED AS PER SRM 51-40-04 FIG 3. STRINGER SEGMENT AND SPLICE ANGLE REWORKED REJan 13, 2005 · N675UP · Boeing 747123F · Fuselage Main, Longeron/StringerSDR UPS05443828Stringer · corrodedBS 980 - 1000 AFTER LT WINDOW FORGING REMOVED FOUND STR CORROSION CRACKED. CORROSION BLEND OUT 0.060" BY 1" BY 3" EXCEED SRM LIMIT. NEW STRINGER SEGMENT AND SPLICE ANGLE INSTALLED AS PER RS R-53-41-35234 AND ENGINEERING FILE NUMBER : 747-53-20213.Jan 13, 2005 · N675UP · Boeing 747123F · Fuselage Main, Longeron/StringerSDR UPS05443827Stringer · corrodedBS 1560 TO 1580 AFT LT WINDOW FORGING REMOVED FOUND STR CORROSION. CORROSION BLEND OUT 0.040 INCH BY 1" BY 5" EXCEED SRM LIMIT. NEW STRINGER SEGMENT AND SPLICE ANGLE INSTALLED AS PER RS R-53-61-35239 AND ENGINEERING FILE NUMBER : 747-53-20222.Jan 13, 2005 · N675UP · Boeing 747123F · Fuselage Main, Longeron/StringerSDR UPS05443826Stringer · crackedBS 1438 TO 1460 AFT RT WINDOW FORGING REMOVED FOUND STR CORROSION CRACKED. CORROSION BLEND OUT 0.100" BY 1" BY 5" EXCEED SRM LIMIT. NEW STRINGER SEGMENT, REPAIR STRAP AND SPICE ANGLE INSTALLED AS PER RS R-53-41-35248 AND ENGINEERING FILE NUMBER : 747-53-2022Jan 13, 2005 · N675UP · Boeing 747123F · Fuselage Main, Longeron/StringerSDR UPS05443825Stringer · crackedBS 1220 TO 1240 AFT RT WINDOW FORGING REMOVED FOUND STR CORROSION CRACKED. CORROSION BLEND OUT 0.080" BY 1" BY 5" EXCEED SRM LIMIT. NEW STRINGER SEGMENT, SPLICE ANGLE AND REPAIR STRAP INSTALLED AS PER RS R-53-41-35245 AND ENGINEERING FILE NUMBER : 747-53-202Jan 13, 2005 · N675UP · Boeing 747123F · Fuselage Main, Longeron/StringerSDR UPS05443815Stringer · crackedBS 1020 TO 1040 AFT RT WINDOW FORGING REMOVED FOUND STR CORROSION CRACKED. CORROSION BLEND OUT 0.100 BY 1 BY 10 INCHES EXCEED SRM LIMIT. ALL REPAIR PARTS AND NEW STRINGER SEGMENT INSTALLED AS PER RS R-53-41-35252 AND ENGINEERING FILE NUMBER : 747-53-20221.Jan 13, 2005 · N675UP · Boeing 747123F · Fuselage Main, Longeron/StringerSDR UPS05443814Stringer · corrodedBS 1080 TO BS 1100 AFT RT WINDOW FORGING REMOVED FOUND STR CORROSION CRACKED. CORROSION BLEND OUT 0.100" BY 1" BY 5" EXCEED SRM LIMIT. ALL REPAIR PARTS AND NEW STRINGER SEGMENT INSTALLED AS PER RS R-53-41-35252 AND ENGINEERING FILE NUMBER : 747-53-20221.Jan 13, 2005 · N675UP · Boeing 747123F · Fuselage Main, Longeron/StringerSDR UPS05443804Stringer · corrodedINSPECTION TYPE:C M/D BS 1580 TO BS 1600 AFT RT WINDOW FORGING REMOVED FOUND STRINGER CORROSION CRACKED. CORROSION BLEND OUT 0.100 X 1 X 10 EXCEED SRM LIMIT. STRINGER SEGMENT AND SPLICE ANGLE REWORKED REFER COMPONENT WORK PROCESS CARD SEQUENCE NR HE70480-1, Jan 13, 2005 · N675UP · Boeing 747123 · Fuselage Main, Longeron/StringerSDR UPS05443803Stringer · corrodedINSPECTION TYPE:C BS 1560 TO BS 1580 AFT RT WINDOW FORGING REMOVED FOUND STRINGER CORROSION CRACKED. CORROSION BLEND OUT 0.060 X 1 X 7 INCH, EXCEED SRM LIMIT. FLAP PEEN CARRIED OUT AS PER SRM 51-10-07 AND SOPM 20-10-03, STRINGER SEGMENT AND SPLICE ANGLE REWOJan 13, 2005 · N675UP · Boeing 747123 · Fuselage Main, Longeron/StringerSDR UPS05443717Skin · corrodedINSPECTION TYPE:C, CORROSION INDICATOR REVEALED ON FUSELAGE UPPER SKIN AT BS 1820 TO BS 1825 STR 46L. CORROSION BLEND OUT 0.035 X 2 X 2 INCHES EXCEED SRM LIMIT. OVER LAPPING SKIN REPLACED AS PER SRM 53-30-03 FIG 17 AND REPAIR DOUBLER AND FILLER INSTALLED AS Jan 12, 2005 · N675UP · Boeing 747123 · Fuselage Main, Plate/SkinSDR UPS05443695Fitting · crackedINSPECTION TYPE:C RT WING BS 1241 UPPER REAR SPAR SIDE-TO-BODY KICK FITTING AREA FOUND CRACK AT TERMINAL FITTING NR 2 HOLE. HOLE REPAIRED AS PER SB 747-57A2314.Jan 11, 2005 · N675UP · Boeing 747123F · Wing, Fuselage Attach FittingsSDR UPS05443819Frame · crackedBS 940, S25L FRAME I/B CHORD FOUND CRACK. M/D BS 940 FRAME AT S-25L, FRAME REPAIRED PER RS R-53-22-35244 AND EO B747-5310-21670-A.Jan 10, 2005 · N675UP · Boeing 747123F · Fuselage Main, FrameSDR UPS05443833Floor Panel · corrodedSTA 1020 TO 1110, BTN L11" AND R11" FLR METAL PNL SKIN FOUND CORROSION. FLOOR PANEL REPAIRED AS PER RS R53-20-35251 AND EO B747-5320-21675-A AND THIS METAL PANEL NEED REPLACEMENT WITHIN 18 MONTHS OR 1000 CYCLES WHICHEVER OCCURS FIRST. CORROSION BLEND OUT DEJan 9, 2005 · N675UP · Boeing 747123F · Fuselage Floor PanelSDR UPS05443832Floor Panel · corrodedSTA 1170 TO 1250, BTN L11 AND R11 FLR METAL PNL SKIN FOUND CORR. METAL FLOOR PANEL REPAIRED AS PER RS R53-20-35251 AND EO B747-5320- 21675-A AND THIS METAL PANEL NEED REPLACEMENT WITHIN 18 MONTHS OR 1000 CYCLES WHICHEVER OCCURS FIRST. CORROSION BLEND OUT DEPJan 9, 2005 · N675UP · Boeing 747123 · Fuselage Floor PanelSDR UPS05443802Seat Track · corrodedINSPECTION TYPE:C M/D - BS 1180 RBL 97 I/B SEAT TRACK SUPPORT FOUND CORRODED. CORROSION BLEND OUT 0.050 X 1 X 1 INCH, EXCEED SRM LIMIT. SEAT TRACK REPAIR PARTS FABRICATED PER SRM 53-10-05 FIG 34.Jan 9, 2005 · N675UP · Boeing 747123 · Fuselage, Seat/Cargo Attach FittingsSDR UPS05443801Seat Track · corrodedINSPECTION TYPE:C - BS 1160 - 1220 RBL 97 SEAT TRACK I/B FLANGE FOUND CORRODED. CORROSION BLEND OUT 0.050 X 1 X 2 INCH. SEAT TRACK CUT OFF AT BS 1070 RBL 98 AS PER SRM 51-10-01. REPROTECTED AS PER SRM 51-10-02. SEAT TRACK REPAIR PARTS FABRICATED PER SRM 53Jan 9, 2005 · N675UP · Boeing 747123 · Fuselage, Seat/Cargo Attach FittingsSDR UPS05443772Web · crackedINSPECTION TYPE:C - R3 DOOR LOWER WEB CRACKED AT LOWER GATE PUSH ROD CUTOUT. LOWER WEB REPAIRED AS PER SRM 51-40-02 FIG 1.Jan 9, 2005 · N675UP · Boeing 747123 · Passenger/Crew DoorsSDR UPS05443667Seat Track · corrodedINSPECTION TYPE:C - BS 1000 LBL 33 O/B SEAT TRACK FLANGE CORRODED. M/D BS 990 - 1000 LBL 33 SEAT TRACK REPAIR PARTS FABRICATED AS PER SRM 53-10-05 FIG 1A. CORROSION BLEND OUT 0.050 X 1 X 1 INCH EXCEED SRM LIMIT.Jan 9, 2005 · N675UP · Boeing 747123 · Fuselage, Seat/Cargo Attach FittingsSDR UPS05443659Floorbeam · corrodedINSPECTION TYPE:C - FLOORBEAM BS 340 LBL 11 - 39 UPPER CHORD CORRODED. REPAIR PARTS FABRICATED AS PER SRM 53-10-07 FIG 23. CORROSION BLEND OUT 0.050 X 2 X 2 INCHES EXCEED SRM LIMIT.Jan 9, 2005 · N675UP · Boeing 747123 · Fuselage Main, Floor BeamSDR UPS05443654Seat Track · corrodedINSPECTION TYPE:C - BS 520 - 540 LBL 46 SEAT TRACK CORRODED AS MARKED. U/D BS 520 - 560 LBL 46 SEAT TRACK REPAIR PARTS FABRICATED AS PER SRM 53-10-05 FIG 6. CORROSION BLEND OUT 0.060 X 1 X 1 INCHES EXCEED SRM LIMIT.Jan 9, 2005 · N675UP · Boeing 747123 · Fuselage, Seat/Cargo Attach FittingsSDR UPS05443653Seat Track · corrodedINSPECTION TYPE:C U/D - BS 480 LBL 46 SEAT TRACK CORRODED AS MARKED. U/D BS 480 - 500 LBL 46 SEAT TRACK REPAIR PARTS FABRICATED AS PER SRM 53-10-05 FIG 6. CORROSION BLEND OUT 0.050 X 1 X 2 INCHES EXCEED SRM LIMIT.Jan 9, 2005 · N675UP · Boeing 747123 · Fuselage, Seat/Cargo Attach FittingsSDR UPS05443650Seat Track · corrodedBS 480 - 500 RBL 66 SEAT TRACK CORRODED AS MARKED. SEAT TRACK PART FABRICATED AS PER SRM 51-10-01 PG 9. CORROSION BLEND OUT 0.050 X 2 X 2 INCHES EXCEED SRM LIMIT.Jan 9, 2005 · N675UP · Boeing 747123 · Fuselage, Seat/Cargo Attach FittingsSDR UPS05443812Stringer · crackedBS 1482 - 1485, STR 13R, STRINGER END FOUND CRACK. STRINGER REPAIRED PER RS 53-41-35250 AND ENGINEERING FILE NUMBER 747-53-20214.Jan 8, 2005 · N675UP · Boeing 747123 · Fuselage Main, Longeron/StringerSDR UPS05443808Stringer · crackedBS 1480 - 1485, S6L, STRINGER END FOUND CRACKED. STRINGER REPAIRED PER RS R53-41-35249 AND ENGINEERING FILE NUMBER 747-53-20215.Jan 8, 2005 · N675UP · Boeing 747123F · Fuselage Main, Longeron/StringerSDR UPS05443773Stringer · crackedINSPECTION TYPE:C - BS 736 - 738, S23R STRINGER END FOUND CRACK. M/D BS 736 TO BS 738 S-23R STRINGER END REPAIRED AS PER RS 53-61-35230 AND ENGINEERING FILE NUMBER 747-53-20204.Jan 8, 2005 · N675UP · Boeing 747123 · Fuselage Main, Longeron/StringerSDR UPS05443730Stiffener · crackedINSPECTION TYPE:C - BS 1080 RBL 99 BELOW FLOOR STIFFENER FOUND CRACKED. M/D BS 1080 RBL 99 BELOW FLOOR STIFFENER REPLACED IAW SRM 51-10-01 PAGE 9.Jan 8, 2005 · N675UP · Boeing 747123 · Fuselage Miscellaneous StructureSDR UPS05443726Intercostal · crackedINSPECTION TYPE:C M/D - BS 1220 RBL 118 BELOW FLOOR INTERCOSTAL WEB FOUND CRACKED. WEB REPAIR PER SRM 51-40-02 FIG 1.Jan 8, 2005 · N675UP · Boeing 747123 · Fuselage Miscellaneous StructureSDR UPS05443720Stringer · crackedINSPECTION TYPE:C M/D - STR END BS 739 S-8L CRACKED. CRACKED STRINGER REPAIRED PER RS 53-21-35238 AND ENGINEERING FILE NUMBER 747-53-20206.Jan 8, 2005 · N675UP · Boeing 747123 · Fuselage Main, Longeron/StringerSDR UPS05443716Frame · crackedINSPECTION TYPE:C - BS 960, S8R, FRAME FOUND CRACK. FRAME REPAIRED PER SRM 53-10-04 FIG 54.Jan 8, 2005 · N675UP · Boeing 747123 · Fuselage Main, FrameSDR UPS05443714Frame · crackedINSPECTION TYPE:C - FRAME BS 760 STR CUTOUT CRACKED AT S-6L AND S-7L. M/D BS 760 BETWEEN STR 6L AND STR 7L FRAME REPAIR CARRIED OUT IAW SRM 53-10-04 FIG 54.Jan 8, 2005 · N675UP · Boeing 747123 · Fuselage Main, FrameSDR UPS05443712Frame · crackedINSPECTION TYPE:C - BS 740, BETWEEN S7 - 8R, FRAME FOUND CRACK. M/D BS 740 BETWEEN STR 7R AND STR 8R FRAME REPAIR CARRIED OUT IAW SRM 53-10-04 FIG 54.Jan 8, 2005 · N675UP · Boeing 747123 · Fuselage Main, FrameSDR UPS05443711Frame · crackedINSPECTION TYPE:C - BS 760, BETWEEN STR 5 - 8R, FRAME FOUND CRACK. M/D BS 760 BETWEEN STR 5R AND STR 8R FRAME REPAIR CARRIED OUT IAW SRM 53-10-04 FIG 54.Jan 8, 2005 · N675UP · Boeing 747123 · Fuselage Main, FrameSDR UPS05443678Spar · crackedINSPECTION TYPE:C, RIGHT WING UPPER REAR SPAR SIDE-OF-BODY SPLICE PLATE FITTING CRACK FOUND AT HOLE NR 5 RUNNING FWD APPROX 0.060 INCH AND AFT APPROX .125 INCH. PLS REFER ATTACH FIG. HOLE REPAIRED AS PER S/B 747-57A2314.Jan 8, 2005 · N675UP · Boeing 747123 · Wing SparSDR UPS05443676Splice · crackedINSPECTION TYPE: C, RIGHT WING STA 1241 UPPER REAR SPAR SIDE - OF - BODY SPLICE PLATE AREA FOUND HOLE NR 3 CRACKED AT WING UPPER SKIN AND INTERNAL SPLICE FITTING APPROX 0.040 INCH REFER ATTACHED SKETCH. HOLE REPAIRED AS PER SB 747-57A2314.Jan 8, 2005 · N675UP · Boeing 747123 · Wing Main, Frame StructureSDR UPS05443666Stringer · crackedINSPECTION TYPE:C - STRINGER END BS 990 S-7L CRACKED. STRINGER REPAIRED PER SRM 53-10-03 FIG 2.Jan 8, 2005 · N675UP · Boeing 747123 · Fuselage Main, Longeron/StringerSDR UPS05443665Stringer · crackedINSPECTION TYPE:C - STRINGER END BS 990 S-9L CRACKED. STRINGER REPAIRED PER SRM 53-10-03 FIG 2.Jan 8, 2005 · N675UP · Boeing 747123 · Fuselage Main, Longeron/StringerSDR UPS05443660Stringer · crackedINSPECTION TYPE:C U/D - BS 680, S9R, STRINGER END FOUND CRACK. STRINGER REPAIRED PER SRM 53-10-03 FIG 2.Jan 8, 2005 · N675UP · Boeing 747123 · Fuselage Main, Longeron/StringerSDR UPS05443658Frame · crackedINSPECTION TYPE:C, FWD CARGO COMPT - SUPPORT FRAME WEB SURFACE FOUND CRACKED AT STA 880 BETWEEN STRINGER 37L TO STRINGER 38L. SUPPORT FRAME REPAIRED PER SRM 53-10-04 FIG 52.Jan 8, 2005 · N675UP · Boeing 747123 · Fuselage Main, FrameSDR UPS05443657Stringer · crackedINSPECTION TYPE:C U/D - BS 620, S9R, STRINGER END FOUND CRACK. STRINGER REPAIR PER SRM 53-10-03 FIG 2.Jan 8, 2005 · N675UP · Boeing 747123 · Fuselage Main, Longeron/StringerSDR UPS05443656Stringer · crackedINSPECTION TYPE:C U/D - BS 560, S9R, STRINGER END FOUND CRACK. STRINGER REPAIR PER SRM 53-10-03 FIG 2.Jan 8, 2005 · N675UP · Boeing 747123 · Fuselage Main, Longeron/StringerSDR UPS05443655Stringer · crackedINSPECTION TYPE:C - BS 640, S9R, STRINGER END FOUND CRACK. STRINGER REPAIR PER SRM 53-10-03 FIG 2.Jan 8, 2005 · N675UP · Boeing 747123 · Fuselage Main, Longeron/StringerSDR UPS05443652Stringer · crackedINSPECTION TYPE:C - BS 736 - 738, S8R, STRINGER END FOUND CRACK. STRINGER REPAIRED PER SRM 53-10-03 FIG 2.Jan 8, 2005 · N675UP · Boeing 747123 · Fuselage Main, Longeron/StringerSDR UPS05443824Stringer · crackedSTR END BS 1476 S-6L CRACKED. CRACKED STRINGER REPAIRED PER RS R53-41-35242 AND ENGINEERING FILE NUMBER : 747-53-20217.Jan 7, 2005 · N675UP · Boeing 747123F · Fuselage Main, Longeron/StringerSDR UPS05443817Stringer · crackedSTR END BS 1003 S-3L CRACKED. STRINGER REPAIRED PER RS R-53-41-35231 AND ENGINEERING FILE NUMBER 747-53-20216.Jan 7, 2005 · N675UP · Boeing 747123F · Fuselage Main, Longeron/StringerSDR UPS05443811Stringer · crackedSTR END BS 1485 S-8L CRACKED. STRINGER REPAIRED PER RS 53-1-35249 AND ENGINEERING FILE NUMBER 747-53-20215.Jan 7, 2005 · N675UP · Boeing 747123F · Fuselage Main, Longeron/Stringer
Back to N675UP, cancelled Jul 19, 2010