N905UP, cancelled May 10, 2007

Service difficulty reports · 111

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 = 'N905UP' AND deregistration_id = 'N905UP-2007-05-10'
  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 UPS03241647Warning Light · illuminatedNR 3 ENG FUEL FILTER WARNING LIGHT ILLUMINATED.Dec 9, 2003 · N905UP · Boeing 72751C · Engine Fuel Indicating SystemSDR UPS02239943Pressure Panel · crackedINSPECTION TYPE:C SEVERAL CRACKS ON NLG WHEEL WELL PRESSURE WEB RHS FROM BS 260 DOWN 1 1" FROM CEILING AND 1" FWD OF THE AFT PRESSURE PANEL TP BS 279 6" BE LOW AFT PRESSURE PANEL DAMAGED AREAS REPAIRED IAW SRM51-40-2 FIG 1Nov 25, 2002 · N905UP · Boeing 72751C · Fuselage Main, StructureSDR UPS02239946Pressure Panel · crackedINSPECTION TYPE: C, NLG WHEEL WELL PRESSURE PANEL CRACKED AT BS 268, 3 INCHES DOWN FROM W/W CEILING. DAMAGED AREA CUTOUT IAW SRM 51-40-2 FIG 1 HFEC CONFIRMS A DEFECT FREE CONDITION, AREA REPAIR IAW SRM 51-40-2 F IG 1.Nov 21, 2002 · N905UP · Boeing 72751C · Fuselage Main, BulkheadSDR UPS02239949Bolt · crackedINSPECTION TYPE: C, DURING REMOVAL OF LT HAND TRUNNION LINK, THE LT MAIN GEAR AFT TRUNNION BOLT AND TRUNNION HOUSING FOUND SHEARED. ON REMOVAL OF LT MLG, AFT BEARING MOUNTING JOURNAL FOUND CRACKED & PIECE BROKEN OFF. END OF JOURNAL.BEARING RETAINING BOLT SHNov 19, 2002 · N905UP · Boeing 72751C · Main Landing Gear Attach SectionSDR UPS02239945Pressure Panel · crackedINSPECTION TYPE:C SUSPECT CRACK ON NLG CEILING AT BS 273 LBL14. HFEC CONFIRMS CRACK, DAMAGED ARE CUTOUT IAW SRM 51-40-02 FIG, HFEC CONFIRMS NDF. REPAIR CARRIED OUT SRM 51-40-02 FIG 1.Nov 19, 2002 · N905UP · Boeing 72751C · Fuselage Main, BulkheadSDR UPS02239944Pressure Panel · crackedINSPECTION TYPE:C CRACK ON NLG WHEEL WELL PRESSURE WEB @ BS 243.6 LHS 4" AFT FROM FWD PRESSURE PANEL. DAMAGED AREA CUT OUT IAW SRM 51-40-02 FIG1, HFEC AROUND CUTOUT NDF, REPAIR CARRIED OUT IAW SRM 51-40-02 FIG 1Nov 19, 2002 · N905UP · Boeing 72751C · Fuselage Main, StructureSDR UPS02239940Fitting · crackedINSPECTION TYPE:C SUSPECT CRACK ON L/H BS 910 FITTING REPAIR CARRIED OUT IAW EO B727-5310-1896-B APPENDIX BNov 18, 2002 · N905UP · Boeing 72751C · Fuselage Main, StructureSDR UPS02239937Fitting · crackedINSPECTION TYPE:C SUSPECT CRACK ON RH BS 910 FITTING REPAIR CARRIED OUT IAW EO B727-5310-1896-B APPENDIX BNov 18, 2002 · N905UP · Boeing 72751C · Fuselage Main, StructureSDR UPS02239938Pin · corrodedINSPECTION TYPE:C PITTING FOUND ON RT STAB INNER PINS. RT STAB INNER PIN REPLACED IAW MM 55-10-01.Nov 16, 2002 · N905UP · Boeing 72751C · Horizontal Stabilizer Miscellaneous StructureSDR UPS02239950Spar · crackedINSPECTION TYPE: C, DURING LFEC INSPECTION OR RT INBOARD MID FLAP REAR SPAR UPPER CHORD, A CRACK WAS FOUND AROUND A FASTENER HOLE. REPAIRED PER EO.B727-5750-3582.Nov 15, 2002 · N905UP · Boeing 72751C · Trailing Edge FlapsSDR UPS02239948Beam · crackedINSPECTION TYPE: C, DURING INSPECTION OF VERTICAL BEAM 17.8 RT, A CRACK WAS FOUND ON THE BEAM FLANGE. STOP CUT-OUT AT WL 273, BS 1183 REPAIR PARTS DRILLED OFF IAW EO B727-5310-11743. REPAIR ANGLES INSTALLED WET WITH SEALANT IAW EO B727-5310-11743 REPAIRNov 15, 2002 · N905UP · Boeing 72751C · Fuselage Main, StructureSDR UPS02239942Intercostal · crackedINSPECTION TYPE:C HORIZONTAL INTERCOSTAL CRACKED ON VERTICAL BEAM 17.8 L/H AT WL 283 1 183 BULKHEAD NEW INTERCOSTAL FABRICATED & INSTALLED PER BOEING DRAWING 65-16350 S HEET 6 & 65C15764 SH. 5 & SRM 51-30-2Nov 15, 2002 · N905UP · Boeing 72751C · Fuselage Main, StructureSDR UPS02239941Floorbeam · crackedINSPECTION TYPE:C BEAM TIE CRACKED ON FLOORBEAM LWR FLANGE BS 328 RBL 40. REPAIR PLATE FABRICATED AND FITTED AS PER ARM 53-10-8.Nov 14, 2002 · N905UP · Boeing 72751C · Fuselage Main, Floor BeamSDR UPS02239947Fitting · crackedINSPECTION TYPE: C&SI, WHILE CARRY OUT HFEC INSPECTION ON LT BS 950 FITTING. CRACK FOUND IN ROW 1 UP PER FASTENER HOLE, COMMON TO STR 9. DISCREPANT HOLE REPAIRED IAW SMRO EO 2002-061-003 UPS ENG. FILE NO. B727-5310-17956Nov 13, 2002 · N905UP · Boeing 72751C · Fuselage Main, Attach FittingsSDR UPS02238710Relay · failedINSPECTION TYPE:N/A EMERGENCY LIGHTS ABOVE COCKPIT DOOR ILLUMINATED IN FLIGHT WITH ARM SWITCH IN THE ARMED POSITION. REMOVED R70 RELAY. OPS CHECKS GOOD.Jun 28, 2002 · N905UP · Boeing 72751C · Emergency LightingSDR UPS01236733Stiffener · crackedINSPECTION TYPE:N/A RT MLG ACT BEAM SUPPORT PANEL. FWD STIFFENER CRACKED AT INBD HINGE. REPAIRED CRACKED STIFFENER RT MLG ACT BEAM SUPPORT PANEL PER B727 SRM 51-40-3Aug 30, 2001 · N905UP · Boeing 72751C · Fuselage Miscellaneous StructureSDR UPS01236532Slide · inoperativeINSPECTION TYPE:IN MAIN CABIN SLIDE INOP REF DEF M220206 FWD ENTRY SLIDE DEPLOYED. REPLACED SLIDE AND LATCH ASSY REF 25-60-14.Aug 5, 2001 · N905UP · Boeing 72751C · Escape SlideSDR UPS01236026Panel · crackedINSPECTION TYPE:C, 1 INCH CRACK ON PANEL, UPPER SURFACE OF WING, JUST FWD OF I/B AILERON ON RIGHT WING, I/B EDGE OF PANEL. REPAIRED PER SRM 51-40-2.May 31, 2001 · N905UP · Boeing 72751C · Wing, Plate/SkinSDR UPS01236033Skin · crackedINSPECTION TYPE:C, CRACK FOUND IN TRAILING EDGE SKIN ADJACENT NR 3 SPOILER PANEL HINGE INBOARD HINGE. CRACK REPAIRED IAW SRM.May 30, 2001 · N905UP · Boeing 72751C · SpoilersSDR UPS01235942Light · inoperativeINSPECTION TYPE:IN EMERGENCY LIGHTS UNARMED LIGHT INOP WHEN UNARMED AND PRESS TO TEST. RELAMPED AND FUNCTIONALLY CK GOOD AS PER 33-50.May 21, 2001 · N905UP · Boeing 72751C · Emergency LightingSDR UPS00234515Skin · crackedINSPECTION TYPE:C FOUND R/H OUTBRD FOREFLAP WITH A 3/8 INCH CRACK AT HINGE CUTOUT. REPLACED R/H OUTBRD FOREFLAP IAW M/M 27-51-11. OK PER SAMENov 26, 2000 · N905UP · Boeing 72751C · Leading Edge DevicesSDR UPS98227681Doubler · crackedINSPECTION TYPE-N/A, RIGHT WING AFT SPAR LOWER EDGE CORRIGATED DOUBLER CRACKED APROX 2 INCHES AT APROX WS 340 WBL 220. STOP DRILLED CRACK PER SRM 51-10-1 PG 6B.Sep 15, 1998 · N905UP · Boeing 72751C · Wing Miscellaneous StructureSDR UPS98227517Rib · crackedINSPECTION TYPE-D, ON REMOVAL OF NR 4 SLAT ACTUATOR EYE END BOLT FROM SLAT BOTH RIBS EITHER SIDE OF MOUNT POINT FOUND CRACKED. REPLACED RIBS IAW SRM AND DRAWING 657276, REINSTALLED NR 4 SLAT EYE BOLT IAW MM 27-81-32.Aug 14, 1998 · N905UP · Boeing 72751C · Wing, Rib/BulkheadSDR UPS98227488Bottle Pin · corrodedINSPECTION TYPE:D LT BS 750 BOTTLE PIN FOUND WITH LIGHT PITTING CORROSION. PIN REPLACED IAW MM 57-41-00.Aug 13, 1998 · N905UP · Boeing 72751C · Wing, Fuselage Attach FittingsSDR UPS98227574Stringer · corrodedINSPECTION TYPE:D STRINGER ON TOP OF NOSE WHEEEL WELL AT BL 0, BS 260 TO 277 IS CORRODED. STRINGER SECTION REPAIRED IAW SRM 53-10-3.Aug 12, 1998 · N905UP · Boeing 72751C · Fuselage Main, Longeron/StringerSDR UPS98227572Stringer · crackedINSPECTION TYPE:D SUSPECT CRACK ON STRINGER 23R AT STA 440. REPLACED PART WITH 69-14492-5 IAW SRM 51-30-2.Aug 12, 1998 · N905UP · Boeing 72751C · Fuselage Main, Longeron/StringerSDR UPS98227566Stringer · crackedINSPECTION TYPE-D, STRINGER 23L AT STATION 400 CRACKED AT FASTENER HOLE. STRINGER REPAIRED IAW SRM 53-10-3, FIG 1.Aug 12, 1998 · N905UP · Boeing 72751C · Fuselage Main, Longeron/StringerSDR UPS98227565Stringer · crackedINSPECTION TYPE-D, S21L HAS CRACK AT FASTENER HOLE AT STATION 380. STRINGER REPAIRED IAW SRM 53-10-3, FIG 1.Aug 12, 1998 · N905UP · Boeing 72751C · Fuselage Main, Longeron/StringerSDR UPS98227564Rib · crackedINSPECTION TYPE-D, CRACK ON RIB ATTACH TAB ON NR 13 STRINGER AT WING STATION 656.5 RT. REPAIR CARRIED OUT IAW UPS B727-5710-0314.Aug 12, 1998 · N905UP · Boeing 72751C · Wing, Rib/BulkheadSDR UPS98227561Rib · crackedINSPECTION TYPE-D, CRACK ON RIB ATTACH TAB ON NR 10 STRINGER AT WING STATION 656.5 RT. REPAIR CARRIED OUT IAW UPS EO B727-5710-0314 FIG 13.Aug 12, 1998 · N905UP · Boeing 72751C · Wing, Rib/BulkheadSDR UPS98227551Stringer · crackedINSPECTION TYPE-D, CRACK IN FASTENER HOLE AND FASTENER MISSING ON S21R AT BS 400. REPAIRED CRACK IAW SRM 51-10-3, FIG 2.Aug 12, 1998 · N905UP · Boeing 72751C · Fuselage Main, Longeron/StringerSDR UPS98227550Stringer · crackedINSPECTION TYPE-D, SUSPECT CRACK ON S22R FASTENER HOLE ST STA 380. REPAIRED CRACK IAW SRM 51-10-3 FIG 2.Aug 12, 1998 · N905UP · Boeing 72751C · Fuselage Main, Longeron/StringerSDR UPS98227549Stringer · crackedINSPECTION TYPE-D, CRACK AT FASTENER HOLE OF STRINGER 21R AT STATION 420. STRINGER REPAIRED IAW SRM 53-10-2, FIG 1, DETAIL 2.Aug 12, 1998 · N905UP · Boeing 72751C · Fuselage Main, Longeron/StringerSDR UPS98227548Stringer · brokenINSPECTION TYPE-D, STRINGER 23R BROKEN AT STA 420. STRINGER REPAIRED IAW SRM 53-10-2, FIG 1 DETAIL 2.Aug 12, 1998 · N905UP · Boeing 72751C · Fuselage Main, Longeron/StringerSDR UPS98227496Stringer · crackedINSPECTION TYPE:D, SUSPECT CRACK ON STRINGER 23R AT STA 440. REPLACED PART WITH 69-14492-5 IAW SRM 51-30-2.Aug 12, 1998 · N905UP · Boeing 72751C · Fuselage Main, Longeron/StringerSDR UPS98227573Frame · crackedINSPECTION TYPE:D CRACK ON UPPER FLANGE OF FRAME AT BS 420, BL 0. REPAIR CARRIED OUT ON UPPER FLANGE IAW SRM 51-40-3, FIG 1.Aug 11, 1998 · N905UP · Boeing 72751C · Fuselage Main, FrameSDR UPS98227518Frame · crackedINSPECTION TYPE-D, SLIDING FAIRING 2ND AFT FRAME HAS A CRACK AT THE UPPER SLIDING TRACK ATTACH POINT. CRACK STOP DRILLED PER SRM 51-10-1, REPAIRED FRAME IAW SRM 51-40-3 FIG 1.Aug 10, 1998 · N905UP · Boeing 72751C · Fuselage Main, FrameSDR UPS98227571Strap · crackedINSPECTION TYPE:D ON ACCOMPLISHMENT OF EDDY CURRENT INSPECTION OF RT E-F WINDOW POST PER EO B727-5310-0012, CRACKS FOUND ON 3 HOLES COMMON TO REPAIR STRAP. REPAIR CARRIED OUT IAW SRS ENGINEERING ORDER 98-24-012, REF UPS ENGINEERING FILE NUMBER 727-5310-2066.Aug 8, 1998 · N905UP · Boeing 72751C · Fuselage Miscellaneous StructureSDR UPS98227560Track · crackedINSPECTION TYPE-D, CARGO TRACK SECTION BS 1010 RT SIDE HAS SIZEABLE CRACK. RT FWD TRACK REPLACED IAW SRM 51-30-2.Aug 7, 1998 · N905UP · Boeing 72751C · Fuselage, Seat/Cargo Attach FittingsSDR UPS98227529Web · crackedINSPECTION TYPE-D, CRACK ON VERTICAL WEB ABOVE KEEL BEAM RBL BS 885 APPROX. VERTICAL WEB ABOVE KEEL BEAM REPAIRED IAW SRM 51-40-02.Aug 7, 1998 · N905UP · Boeing 72751C · Fuselage Miscellaneous StructureSDR UPS98227528Clip · crackedINSPECTION TYPE-D, WING CENTER SECTION FWD TANK FWD WALL SHEAR TIE CLIP CRACKED AT RBL 25. REPLACED SHEAR TIE CLIP IAW DRW 64-08333.Aug 7, 1998 · N905UP · Boeing 72751C · Wing Miscellaneous StructureSDR UPS98227527Clip · crackedINSPECTION TYPE-D, WING CENTER SECTION FWD TANK FWD WALL SHEAR TIE CLIP CRACKED AT LBL 25. REPLACED SHEAR TIE CLIP IAW DRAWING 64-08333.Aug 7, 1998 · N905UP · Boeing 72751C · Wing Miscellaneous StructureSDR UPS98227519Skin · corrodedINSPECTION TYPE-D, SUSPECT CORROSION BETWEEN SKIN AND CUSP ANGLE BS 1180 STR 17R. CORRODED SKIN AT BS 1180 STR 17R REPAIRED PER SRS EO 98-24-006 REF UPS ENGINEERING FILE NR 727-53-2063.Aug 7, 1998 · N905UP · Boeing 72751C · Fuselage Main, Plate/SkinSDR UPS98227499Fitting · corrodedINSPECTION TYPE:D, 9G BARRIER NET ATTACH FITTING ON FLOOR LBL 20 BETWEEN BS 360-380 HAS SEVERE CORROSION. 9G FITTING AT LBL 20 REPLACED IAW SRM 51-30-02.Aug 7, 1998 · N905UP · Boeing 72751C · Fuselage Miscellaneous StructureSDR UPS98227495Web · corrodedINSPECTION TYPE:D, COROSION ON WEB RBL 10 BS 830 APPROX. REPAIR CARRIED OUT IAW SRM 51-40-2.Aug 7, 1998 · N905UP · Boeing 72751C · Fuselage Miscellaneous StructureSDR UPS98227533Spindle · corrosionINSPECTION TYPE-D, SURFACE CORROSION IN BORE OF SPINDLE OF NR 3 FLAP TRACK CARRIAGE. FLAP TRACK CARRIAGE REPLACED REF OHM 57-58-11.Aug 6, 1998 · N905UP · Boeing 72751C · Trailing Edge FlapsSDR UPS98227492Web · crackedINSPECTION TYPE:D, ENGINE NR 1 THRUST REV AFT VERTICAL WEB SUSPECT CRACK AT 12 O'CLOCK POSITION AT HYD PIPE BRACKET ATTACH. REPAIR CARRIED OUT IAW SRM 51-40-2.Aug 6, 1998 · N905UP · Boeing 72751C · Engine Thrust ReverserSDR UPS98227563Angle · corrodedINSPECTION TYPE-D, CHORD ANGLE AT BS 740 LT (P/N 65-15940-24) HAS CORROSION ON O/B SECTION. CHORD REPAIRED IAW DRAWING 65C13724 AND SRS ENGINEERING ORDER 98-24- 004, REF UPS ENGINEERING FILE NUMBER 727-53-2064.Aug 5, 1998 · N905UP · Boeing 72751C · Fuselage Miscellaneous StructureSDR UPS98227544Bolt · corrodedINSPECTION TYPE-D, NR 5 FLAP TRACK ATTACH BOLT CORRODED. BOLT CHANGED IAW MM 27-51-31.Aug 5, 1998 · N905UP · Boeing 72751C · Trailing Edge FlapsSDR UPS98227576Panel · corrodedINSPECTION TYPE:D LT WING TANK FROMT SPAR ACCESS PANEL NR 1 CORRODED. PANEL REPLACED IAW MM 28-11-21.Aug 4, 1998 · N905UP · Boeing 72751C · Wing, Plate/Skin
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