N926UP, cancelled Sep 19, 2007

Service difficulty reports · 254

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 = 'N926UP' AND deregistration_id = 'N926UP-2007-09-19'
  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 UPS06248770Light · inoperativeEMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERIES AND OPS CK IAW MM 33-50-01-5.Dec 15, 2006 · N926UP · Boeing 72731C · Emergency LightingSDR UPS06248392Light · inoperativeFOUND EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERIES AND OPERATIONAL CHECK PER MM 33-50-01-5 CKS NORMAL.Nov 1, 2006 · N926UP · Boeing 72731C · Emergency LightingSDR UPS06247166Battery Pack · dischargedINSPECTION TYPE:N/A EMERGENCY EXIT LIGHT INOP AT CABIN DOOR. REPLACED BATTERY PACK PER MM 33-50-90-2.Jun 21, 2006 · N926UP · Boeing 72731C · Emergency LightingSDR UPS06247165Light · inoperativeINSPECTION TYPE:N/A EMERGENCY LIGHT INOP AT COCKPIT DOOR. REMOVED AND REPLACED LIGHT ASSY, OPS CHECK NORMAL.Jun 21, 2006 · N926UP · Boeing 72731C · Emergency LightingSDR UPS05245892Hydraulic System · leakingINSPECTION TYPE:N/A ATB - HYD QTY AFTER TAKEOFF WENT TO 2.0 GALS AFTER FLAP RETRACTION QTY HELD STEADY AT 2.3 GALS. FOUND ASYS QTY LOW, SERVICED TO PROPER LEVEL PER M/M 12-12-00-2. CHECKED L/E SLAT ACTUATOR AND FLAP POW'S FOR LEAKS, NONE FOUND. NO OTHER LEADec 23, 2005 · N926UP · Boeing 72731C · Hydraulic System, MainSDR UPS05245846Light · inoperativeONE LAMP INOP IN EMERGENCY EXIT LIGHT AT L1 DOOR. RELAMPED OK FOR SERVICE.Nov 26, 2005 · N926UP · Boeing 72731C · Emergency LightingSDR UPS05245464Slide · inoperativeINSPECTION TYPE:N/A L-1 DOOR SLIDE INOP. REMOVED AND REPLACED SLIDE ASSY PER 25-60-14, THIS CLEARS M310071.Sep 18, 2005 · N926UP · Boeing 72731C · Escape SlideSDR UPS05244731Skin · corrodedC NDI HAS MATERIAL LOSS INDICATION AT S19 RT BS 441, SKIN CUT OUT AND REPAIR IN CONJUNCTION WITH NRC 792106 LAP REPAIR.Jun 15, 2005 · N926UP · Boeing 72731C · Fuselage Main, Plate/SkinSDR UPS05244729Bushing · damagedENGINE NR 3 FWD MOUNT AFT O/B HOLE REPAIR BUSHING DAMAGED. BUSHING REPLACED IAW UPS EO B727-5440-11592-A.Jun 14, 2005 · N926UP · Boeing 72731C · Nacelle/Pylon Miscellaneous StructureSDR UPS05244728Structure · corrodedENG NR 1 FWD MOUNT BOTH O/B HOLES HAVE PITTING CORROSION ON REPAIR BUSHINGS. BUSHINGS REPLACED IAW UPS EO B727-5440-11592-A.Jun 14, 2005 · N926UP · Boeing 72731C · Nacelle/Pylon Miscellaneous StructureSDR UPS05244725Skin · crackedCRACK IN FUSELAGE SKIN BS 355 BETWEEN S26L AND 27L. REPAIR CARRIED OUT IAW SRM 53-30-3 AND 51-10-2.Jun 13, 2005 · N926UP · Boeing 72731C · Fuselage Main, Plate/SkinSDR UPS05244732Fitting · crackedCLEAT CRACKED O/B OF S26R AT BS 600 LWR SECTION OF CLEAT ADJACENT TO S 26. REMOVED DAMAGED CLEAT IAW SRM 51-30-2. FABRICATED CLEAT IAW SRM 51-20-1. INSTALLED CLEAT IAW SRM 51-30-2.Jun 12, 2005 · N926UP · Boeing 72731C · Fuselage, Stabilizer Attach FittingsSDR UPS05244727Support Bracket · crackedENG NR 3 THRUST REVERSER O/B FAIRING MID SUPPORT BRACKET CRACKED. BRACKET REPLACED IAW SRM 51-30-2.Jun 11, 2005 · N926UP · Boeing 72731C · Engine Thrust ReverserSDR UPS05244726Support Bracket · crackedENG NR 1 THRUST REVERSER O/B FAIRING MID SUPPORT BRACKET CRACKED. BRACKET REPLACED IAW SRM 51-30-2.Jun 11, 2005 · N926UP · Boeing 72731C · Engine Thrust ReverserSDR UPS05244733Skin · crackedCRACK ON SKIN AT FWD ENTRY DOOR UPPER FWD AREA (BETWEEN S6 AND S 7L) OF CUT OUT. REPAIR CARRIED OUT IAW EO B727-5330-1460 OPTION 1.Jun 10, 2005 · N926UP · Boeing 72731C · Fuselage Main, Plate/SkinSDR UPS05244730Support Bracket · crackedNR 2 LE FLAP ACTUATOR O/B SUPPORT BRACKET CRACKED AT UPPER FWD CORNER. BRACKET FABRICATED AND REPLACED IAW SRM 51-20-1, 51-30-02 AND DRAWING 65 -16269.Jun 10, 2005 · N926UP · Boeing 72731C · Trailing Edge Flap ActuatorSDR UPS05244738Hinge · crackedINSPECTION TYPE:C SUSPECT CRACK ON LEFT O/B AILERON I/B TAB HINGE ASSY LWR HALF. HFEC CARRIED OUT ON SUSPECT AREA IAW B727 NDTM 51-00-00 PT6 FIG 4, CRACK CONFIRMED. FWD HINGE HALF REPLACED IAW SRM 51-30-02. APPLIED CIC TO EXPOSED AREA IAW SRM 51-10-02.Jun 7, 2005 · N926UP · Boeing 72731C · AileronsSDR UPS05244737Skin · debondedINSPECTION TYPE:C RT ELEVATOR TAB DISBONDED AT LOWER SURFACE 24 INCHES O/B OF INNER EDGE, AT LOWER SURFACE 3 INCHES FROM O/B EDGE 2 SUSPECT AREA RT UPPER OUTER CORNER AND RT UPPER INNER CORNER. REMOVED ELEVATOR TAB IAW MM 27-30-11. REPAIRED TAB IAW SRM 51-40Jun 7, 2005 · N926UP · Boeing 72731C · Elevator, Tab StructureSDR UPS05244736Skin · corrodedINSPECTION TYPE:C LT ELEVATOR TAB UPPER SKIN CORRODED 5 INCHES FROM O/B END. REMOVED CORROSION IAW SRM 51-10-01, BLENDOUT FOUND TO BE OUT OF LIMITS IAW SRM 55-20-01. REMOVED TAB IAW MM 27-30-11. TAB UPPER SKIN REPAIRED IAW SRM 51-40-20. TAB REPAINTED IAW MJun 7, 2005 · N926UP · Boeing 72731C · Elevator, Tab StructureSDR UPS05244735Lap Joint · corrodedINSPECTION TYPE:C SUSPECT CORROSION AT LAP JOINT S19R BETWEEN BS 390 AND 441 AREA BETWEEN BS 390 AND 441 PAINT STRIPPED IAW MM 51-20-01. AREA REINSPECTED, COROSION FOUND EVIDENT CONTINUE OPEN UP AND REPAIR IAW APPX C OF EO B727-5330-0509. REMOVED CORROSION IJun 7, 2005 · N926UP · Boeing 72731C · Fuselage Main, Plate/SkinSDR UPS04243150Actuator · brokenINSPECTION TYPE:N/A ON APPROACH RIGHT MAIN UPLOCKED LIGHT GEAR DOOR LIGHT REMAINED ON. RECYCLED ONCE, LIGHTS STILL ON, MANUALLY CRANKED RIGHT GEAR DOWN. REPLACED RIGHT MLG LOCK ACTUATOR, PERFORMED MAIN GEAR EXTENSION AND RETRACTION ADJ/TEST W/R/T MM 32-32-00Sep 22, 2004 · N926UP · Boeing 72731C · Landing Gear ActuatorSDR UPS04243022Light · malfunctionedFLT STA EMERGENCY LIGHT WAS COMING ON IN FLT IN ARM POST. REMOVED AND REPLACED EMERGENCY LIGHT ASSY IAW 33-50-00. OPS CHECK GOOD.Aug 25, 2004 · N926UP · Boeing 72731C · Emergency LightingSDR UPS04242900Switch · inoperativeEMERGENCY EXIT LIGHTS INOPERATIVE, COCKPIT DOOR. TURNED BATTERY SWITCH ON PLACED EMERGENCY LIGHT SWITCH TO ARMED, LIGHT CHECKS GOOD.Aug 13, 2004 · N926UP · Boeing 72731C · Emergency LightingSDR UPS04242550Light · inoperativeEMERGENCY EXIT LIGHTS NOT OPERATING. RESEATED EMERGENCY LIGHT ASSY, OPS CHECK NORMAL.Jun 9, 2004 · N926UP · Boeing 72731C · Emergency LightingSDR UPS04242205Flap Track · crackedINSPECTION TYPE: C, NR 6 FLAP TRACK FAIRING I/B TRACK IS CRACKED. FAIRING TRACK REPLACED IAW SRM 51-30-02.Apr 7, 2004 · N926UP · Boeing 72731C · Trailing Edge FlapsSDR UPS04242181Casting · crackedINSPECTION TYPE: C, RIGHT O/B FLAP I/B FLAP TRACK FAIRING HAS CRACKED CASTING/BRACKET. CRACKED BRACKET REMOVED IAW SRM 51-30-02 & STOP DRILLED IAW SRM 51-10-1. REPAIR SECTION FABRICATED IAW SRM 51-40-3 & INSTALLED IAW SRM 51-40-3.Apr 7, 2004 · N926UP · Boeing 72731C · Trailing Edge FlapsSDR UPS04242260Angle · corrodedINSPECTION TYPE:C LT 950 FITTING LWR SPLICE ANGLE HAS SUSPECT CORROSION UNDER THE ANGLE. ANGLE WAS ALSO FOUND CORRODED AFTER REMOVAL. ANGLE REPLACED AND BS 950 REPAIR CARRIED OUT IAW SRM 51-20-1 AND SMRO EO 2004-027-002. UPS ENGINEERING FILE NR B727-5310-203Apr 6, 2004 · N926UP · Boeing 72731C · Fuselage Miscellaneous StructureSDR UPS04242241Door Frame · crackedINSPECTION TYPE:C LWR FWD CARGO DOOR CUTOUT FRAME, CRACK INDICATION IN AREA NR 4 FWD DOOR STOP. REPAIR CARRIED OUT IAW SMRO EO 2004-027-01 UPS ENGINEERING FILE NR B727-5310-20302-AApr 6, 2004 · N926UP · Boeing 72731C · Fuselage Main, StructureSDR UPS04242206Frame · corrodedINSPECTION TYPE: C, FUSELAGE FAIRING 3430 HAS EXTENSIVE CORROSION TO THE FORMED FRAME HOLDING THE ANCHOR NUTS (FWD SIDE OF FAIRING). REPAIR CARRIED OUT IAW SRM 53-10-01, 51-20-01, 51-10-02 & 51-30-02.Apr 6, 2004 · N926UP · Boeing 72731C · Aerodynamic FairingsSDR UPS04242204Beam · corrodedINSPECTION TYPE: C, RT HORIZONTAL STABILIZER UPPER TRAILING EDGE BEAM HAS CORROSION AFT OF BALANCE PANEL BAYS. BEAM REPLACED IAW SRM 51-30-2 AND DRG NR 65-22987.Apr 6, 2004 · N926UP · Boeing 72731C · Horizontal Stabilizer StructureSDR UPS04242180Floorbeam · crackedINSPECTION TYPE: C, FLOORBEAM FOUND CRACKED AT BS 328, RBL 44. REPAIR CARRIED OUT IAW SRM 53-10-8.Apr 6, 2004 · N926UP · Boeing 72731C · Fuselage Main, Floor BeamSDR UPS04242219Drum · corrodedINSPECTION TYPE:C LEFT I/B MIDFLAP O/B AFT FLAP ACTUATING DRUM CORRODED. DRUM REPLACED IAW MM 27-51-01.Apr 5, 2004 · N926UP · Boeing 72731C · Trailing Edge Flap Control SystemSDR UPS04242179Floorbeam · crackedINSPECTION TYPE: C, FLOORBEAM FOUND CRACKED AT BS 344 LBL 24. REPAIR CARRIED OUT IAW SRM 51-20-1 FIG 7.Apr 5, 2004 · N926UP · Boeing 72731C · Fuselage Main, Floor BeamSDR UPS04242178Floorbeam · crackedINSPECTION TYPE: C, FLOORBEAM FOUND CRACKED AT BS 328 RBL 24. REPAIR CARRIED OUT IAW SRM 53-10-8.Apr 5, 2004 · N926UP · Boeing 72731C · Fuselage Main, Floor BeamSDR UPS04242223Rib · crackedINSPECTION TYPE:C NR 3 L/E SLAT, CRACK AT ACTUATOR ATTACH RIB (O/B RIB). REPAIR CARRIED OUT IAW SRM 51-30-02, 51-30-03, 57-50-03 & MM 28-81-11 & 27-00-00.Apr 3, 2004 · N926UP · Boeing 72731C · Leading Edge DevicesSDR UPS04242220Rib · crackedINSPECTION TYPE:C NR 2 L/E SLAT CLOSURE RIB AT INBOARD END OF SLAT CRACKED. REPAIR CARRIED OUT IAW SRM 51-30-02, 51-20-1 & MM 20-10-05.Apr 3, 2004 · N926UP · Boeing 72731C · Leading Edge DevicesSDR UPS04242177Skin · crackedINSPECTION TYPE:C NR 4 K-FLAP HAS CRACK ON INNER ANTI-ICE SKIN AROUND RIVET HOLE I/B OF O/B ACTUATION LINKAGE FOR BULLNOSE. REPAIR CARRIED OUT IAW SRM 51-30-2, 57-50-3.Apr 3, 2004 · N926UP · Boeing 72731C · Leading Edge DevicesSDR UPS02239194Stiffener · corrodedINSPECTION TYPE:C LOWER END OF STIFFENER AT WS 210, R/H WING REAR SPAR, IS CORRODED STIFFENER REPLACED IAW SMRO EO 2002-044-006, REF. UPS ENGINEERING FI LE NO. 727-57-20060.Aug 17, 2002 · N926UP · Boeing 72731C · Wing Main, Frame StructureSDR UPS02239191Web · crackedINSPECTION TYPE:C CRACK FOUND IN NLG FWD L/H PRESSURE WEB AT BS 235 APPROX. CRACK REMOVED IAW SRM 51-40-2. HFEC INSPECTION CONFIRMED CRACK REMOV AL. REPAIR PARTS FABRICATED AND REPAIR INSTALLED IAW SRM 51-40-2, FI G. 1.Aug 15, 2002 · N926UP · Boeing 72731C · Fuselage Main, StructureSDR UPS02239120Pressure Panel · crackedINSPECTION TYPE:C SUSPECT CRACK IN NLG FWD LT PRESS WEB AT BS 243.7. CRACKED AREA REMOVED IAW SRM 51-40-2 FIG 1. HFEC C/O ON THE ABOVE AREA INSP CARRIED OUT IAW B727 NDTM PT 6 51-00-00 FIG 4. RESULT CRACK REMOVED BY CUT OUT, FABRICATED DOUBLER & FILLER IAW Aug 15, 2002 · N926UP · Boeing 72731C · Fuselage Main, BulkheadSDR UPS02239168Skin · crackedINSPECTION TYPE:C CRACK IN ANTI-ICE SKIN AT 5TH BAY O/B ON NO.4 KRUEGER FLAP. ANTI-ICE SKIN FOUND TO BE OUT OF LIMITS IAW SRM ADDENDIUM EO NO. B72 7-5750-3082-D. ANTI ICE SKIN REPLACED IAW DRAWING NO.65-16225 + SRM 51-30-02.Aug 14, 2002 · N926UP · Boeing 72731C · Leading Edge DevicesSDR UPS02239166Skin · crackedINSPECTION TYPE:C #3 LE FLAP ANTI-ICE SKIN CRACKED AT MIDDLE O/B RIVET 3RD BAY FROM O/ B REPAIR CARRIED OUT IAW SRM ADDENDUM EO # B727-5750-3082Aug 14, 2002 · N926UP · Boeing 72731C · Leading Edge DevicesSDR UPS02239165Skin · crackedINSPECTION TYPE:C RIVET PULLED THROUGH ANTI-ICE SKIN AT #4 KRUEGER FLAP AT 8TH BAY O/B SKIN REPAIRED IAW SRM ADDENDUM EO # B727-5750-3082Aug 14, 2002 · N926UP · Boeing 72731C · Leading Edge DevicesSDR UPS02239199Spar · corrodedINSPECTION TYPE:C SUSPECT CRACK ON RT WING REAR SPAR UPPER CHORD AT APPROX WS 198 AND WS 194. UPPER CHORD HORIZONTAL FLANGE BLENDED TO REMOVE DAMAGE AT WS 196, WS 201 AND WS 205 IAW SRM 51-10-6. ADDITIONAL CORROSION FOUND AT 3 FASTENER LOCATION BETWEEN WS 17Aug 14, 2002 · N926UP · Boeing 72731C · Wing SparSDR UPS02239119Web · crackedINSPECTION TYPE:C LIGHTENING HOLE IN AFT AIRSTAIR TORQUE BOX AT BS 1243 RHS IS CRACKED WEB REPAIR CARRIED OUT IAW SRM 51-10-4Aug 14, 2002 · N926UP · Boeing 72731C · Fuselage Main, StructureSDR UPS02239167Doubler · crackedINSPECTION TYPE:C SUSPECT CRACK AT FASTNER BESIDE REPAIR AT NLG WHEEL WELL LEFT FWD PR ESS WEB AT BS 269.5 REPAIR DOUBLER REMOVED IAW SRM 51-30-2 NDT CARRIED OUT CRACK CONFIRM ED & END OF CRACK MARKED. DOUBLER AND FILLERS FABRICATED AND INSTALL ED IAW SRM Aug 13, 2002 · N926UP · Boeing 72731C · Fuselage Main, StructureSDR UPS02239197Web · crackedINSPECTION TYPE:C CRACKS FOUND IN NLG W/WELL PRESSURE WEB AT BS 269.5, 4" BELOW THE CE ILING ON THE R/H PRESSURE WEB AREA. NEW WEB AND DOUBLERS FABRICATED AND INSTALLED IAW DRAWING 65-18414Aug 13, 2002 · N926UP · Boeing 72731C · Fuselage Main, StructureSDR UPS02239190Skin · corrodedINSPECTION TYPE:C CORROSION FOUND AT LAP JOINT S4L. LFEC INSPECTION CARRIED OUT FROM B S 360 TO BS 440. MATERIAL LOSS INDICATION FROM BS 440 TO BS 411 APPR OX. 20% - 30%. CORRODED INTERNAL DOUBLER ALSO FOUND TO BE DISBONDED. DOUBLER REMOVED IAW SRM 51-30-2. Aug 13, 2002 · N926UP · Boeing 72731C · Fuselage Main, Plate/SkinSDR UPS02239187Stiffener · crackedINSPECTION TYPE:C SUSPECT CRACK ON AFT PRESSURE BULKHEAD VERTICAL BEAM LT AT W/L 264 APPROX LBL 26.83. HFEC INSPECTION CONFIRMED CRACK. CRACK STOP DRILLED IAW EO B727-5311-0631 STEP 3. HEFC INSPECTION CONFIRMED CRACK CONTAINED. AREA REPAIRED IAW B727-5311-Aug 13, 2002 · N926UP · Boeing 72731C · Fuselage Miscellaneous StructureSDR UPS02239115Stiffener · crackedINSPECTION TYPE:C WING TO BODY FAIRING 3409 HAS A CRACKED FWD FRAME STIFFENER ANGLE. FABRICATED AND INSTALLED NEW STIFFENER IAW SRM 53-50-1 FIG 4 AND SRM 51-2 0-1 FIG 7.Aug 13, 2002 · N926UP · Boeing 72731C · Aerodynamic Fairings
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