N921UP, cancelled Aug 23, 2006

Service difficulty reports · 126

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 = 'N921UP' AND deregistration_id = 'N921UP-2006-08-23'
  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 UPS02239825Light · not seatedINSPECTION TYPE:PFLT EMERGENCY EXIT LIGHTS ABOVE CABIN ENTRY DOOR ARE VERY DIM. CHARGED BATTERY FOR 3 HRS, RESEATED LIGHT ASSY, GROUND CHECK GOOD.Oct 25, 2002 · N921UP · Boeing 727180C · Emergency LightingSDR UPS02239750Light · inoperativeEMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED CREW ENTRY DOOR EMERGENCY EXIT LIGHT ASSY. OPS CHECK GOOD MM 33-50-01.Oct 15, 2002 · N921UP · Boeing 727180C · Emergency LightingSDR UPS02238111Skin · corrodedINSPECTION TYPE:C CORROSION FOUND AT LAP SKINS BS 479 STRINGER 26R FASTENERS REMOVED IAW SRM51-30-02, UPUPER SKIN CUT OUT BETWEEN BS 47 2-485, NDT NDF, REPAIR PARTS FABRICATED IAW AND INSATLLED IAW EO B72 7-5330-16775.Apr 22, 2002 · N921UP · Boeing 727180C · Fuselage Main, Plate/SkinSDR UPS02238094Skin · crackedINSPECTION TYPE:C NR 3 KRUEGER FLAP ANTI ICE SKIN CRACKED 14 INCHES FROM I/B END. INSPECTED IAW NDTM PT 6 51-00-00 FIG 4, REPAIR CARRIED OUT IAW UPS EO B727-5750-3082-D.Apr 22, 2002 · N921UP · Boeing 727180C · Leading Edge DevicesSDR UPS02238102Seat Track · corrodedINSPECTION TYPE:C CORROSION FOUND ON SEAT TRACK O/B FLANGE AT BS 500 AT R/H O/B SEAT T RACK SEAT TRACK REPAIRED IAW SRM 53-10-5Apr 20, 2002 · N921UP · Boeing 727180C · Fuselage Main, StructureSDR UPS02238112Doubler · corrodedINSPECTION TYPE:C SUSPECT CORROSION BETWEEN FUSELAGE SKIN AND TOILET SERVICE PAN UPPER FLANGE, AFT SERVICE PAN. AREA PAINT STRIPPED, SERVICE PAN DE-RIVETED AND REMOVED, SKIN PANEL DE-RIVETED BETWEEN STR 17L-23L BS 1183 - 1150. INTERNAL DOUBLER AROUND PAN FOApr 18, 2002 · N921UP · Boeing 727180C · Fuselage Main, Plate/SkinSDR UPS02238103Skin · crackedINSPECTION TYPE:C SUSPECT CRACK IN FUSELAGE SKIN BS 310 S8 L/H AT FWD ENTRY DOOR FWD D OOR CUT OUT REPAIR CARRIED OUT IAW UPS EO B727-5340-1460Apr 18, 2002 · N921UP · Boeing 727180C · Fuselage Main, Plate/SkinSDR UPS01234998Fitting · brokenINSPECTION TYPE:IN OXYGEN BOTTLE ATTACHING HARDWARE BROKEN. *S/D* REMOVED AND REPLACED MS FITTING ON BLOWOUT LINE AND UPPER 02 BOTTLE CLAMP. REMOVED AND REPLACED 02 BOTTLE. LK CHECK GOOD.Feb 15, 2001 · N921UP · Boeing 727180C · Crew Oxygen SystemSDR UPS00234545Switch · inoperativeINSPECTION TYPE:N/A CO PILOTS EMERG 0XYGEN SWITCH FAILS TO FULLY CLOSE ***SUPPLEMENTAL MRR*** REPLACED CO-PILOTS REGULATION W/SERVICABLE RUGULATION AND REPLACED W ITH SERVICABLE BOTTLE. LEAKED CHECK OK OPS CHECK PER 727 MM CHPT 35- 11-31 AND 12-15-11Dec 13, 2000 · N921UP · Boeing 727180C · Crew Oxygen SystemSDR UPS00234250Motor · failedINSPECTION TYPE:C, O/B ALT FLAP MOTOR NOT RETRACTING FLAPS. REPLACED MOTOR IAW MM 27-51-141.Oct 26, 2000 · N921UP · Boeing 727180C · Trailing Edge Flap Control SystemSDR UPS00234247Shear Tie · crackedINSPECTION TYPE:C, FLOORBEAM SHEAR TIE CRACKED AT BS 318 AND LBL 4. REPAIR CARRIED OUT IAW SRM 51-40-2.Oct 18, 2000 · N921UP · Boeing 727180C · Fuselage Main, StructureSDR UPS00234246Shear Tie · crackedINSPECTION TYPE:C, FLOORBEAM SHEAR TIE CRACKED AT BS 312 RBL 24. REPAIR CARRIED OUT IAW SRM 51-40-2.Oct 18, 2000 · N921UP · Boeing 727180C · Fuselage Main, StructureSDR UPS00234257Flange · crackedINSPECTION TYPE:C, SUSPECT CRACK ON AFT O/B AND FWD FLANGES OF BS 930 FUSELAGE FITTING BETWEEN S18A AND S19 LT. REPAIR CARRIED OUT IAW UPS EO B727-5310-2611 APPENDIX 8.1Oct 16, 2000 · N921UP · Boeing 727180C · Fuselage Miscellaneous StructureSDR UPS00234249Fitting · corrodedINSPECTION TYPE:C, DUE TO EXCESSIVE CORROSION IN BS 940 LT FITTING FASTENER HOLES, REPLACE FITTING BS 940 LT. REPLACED IAW UPS EO B727-5310-4501 APPENDIX C.Oct 16, 2000 · N921UP · Boeing 727180C · Fuselage Main, Attach FittingsSDR UPS00234256Stiffener · crackedINSPECTION TYPE:C, KEEL BEAM AREA, HORIZ STIFFENER AT BS 900 IS CRACKED STIFFENER IS LOCATED ON INTERNAL SIDE OF LT KEEL BEAM WALL. REPAIR CARRIED OUT IAW SRM 51-30-2 DRG NR 65-28900 AND SMRO EO 2000-38-006 UPS ENGINEERING FILE NR 727-53-2293.Oct 14, 2000 · N921UP · Boeing 727180C · Fuselage Miscellaneous StructureSDR UPS00234255Stiffener · crackedINSPECTION TYPE:C, KEEL BEAM AREA (INTERNAL) HORIZ STIFFENER AT BS 900 APPROX IS CRACK ED AT SITE OF PREVIOUS REPAIR RT KEEL BEAM WALL. REPAIR CARRIED OUT IAW DRG NR 65-28900 AND SMRO EO 2000-38-006 UPS ENGINEERING FILE NR 727-53-2293.Oct 14, 2000 · N921UP · Boeing 727180C · Fuselage Miscellaneous StructureSDR UPS00234252Stiffener · crackedINSPECTION TYPE:C, KEEL BEAM AREA, HORIZ STIFFENER AT BS 900 IS CRACKED. STIFFENER IS LOCATED ON INTERNAL SIDE OF LT KEEL BEAM WALL. STIFFENER INSTALLED IAW DRG NR 65-18636 AND SRM 51-30-2.Oct 14, 2000 · N921UP · Boeing 727180C · Fuselage Miscellaneous StructureSDR UPS00234251Stiffener · crackedINSPECTION TYPE:C, KEEL BEAM AREA (INTERNAL) HORZ STIFFENER AT BS 900 APPROX IS CRACKED AT SITE OF PREVIOUS REPAIR RT KEEL BEAM WALL. STIFFENER INSTALLED IAW DRG 65-18636 AND SRM 51-30-2.Oct 14, 2000 · N921UP · Boeing 727180C · Fuselage Miscellaneous StructureSDR UPS00234248Mount · corrodedINSPECTION TYPE:C, ENGINE NR 3 FWD MOUNT PITTING CORROSION FWD IN BOTH I/B MOUNT HOLES. REPAIR CARRIED OUT IAW EO B7274401592.Oct 13, 2000 · N921UP · Boeing 727180C · Engine Mount SectionSDR UPS00234244Mount · corrodedINSPECTION TYPE:C, ENG NR 1 FWD MOUNT, PITTING CORROSION FOUND IN FWD BOLT HOLES I/B, O/B. REPAIR CARRIED OUT IAW EOJ NR B727-5440-11592.Oct 13, 2000 · N921UP · Boeing 727180C · Engine Mount SectionSDR UPS00234241Beam · crackedINSPECTION TYPE:C, CRACK FOUND AT BS 1183 BULKHEAD VERTICAL BEAM RBL 26.83 AT WL 259.5. REPAIR CARRIED OUT IAW APPENDIX D OF EO B727-5311-0631.Oct 13, 2000 · N921UP · Boeing 727180C · Fuselage Miscellaneous StructureSDR UPS00234254Flange · corrodedINSPECTION TYPE:C, EVIDENCE OF CORROSION TO S18A FLANGE (HORIZ) AT BS 870 LT. REPAIR CARRIED OUT IAW SRM 53-10-1 AND 51-30-2 AND SMRO EO 2000-38-003 AND EO B727-5330-3815 UPS ENGINEERING FILE NR 727-53-2292.Oct 12, 2000 · N921UP · Boeing 727180C · Fuselage Miscellaneous StructureSDR UPS00234243Skin · crackedINSPECTION TYPE:C, SKIN CRACKS AT BS 203.8 RT AT WL 18 AND WL 20. DAMAGE REPAIRED IAW SRM 53-30-3 FIG 3.Oct 12, 2000 · N921UP · Boeing 727180C · Fuselage Main, Plate/SkinSDR UPS00234242Bracket · crackedINSPECTION TYPE:C, ENGINE NR 3 THRUST REV O/B FAIRING MID SUPPORT BRACKET CRACKED. BRACKET REPLACE IAW MM 20-80-01.Oct 12, 2000 · N921UP · Boeing 727180C · Engine Thrust ReverserSDR UPS00234240Beam · crackedINSPECTION TYPE:C, FOUR CRACKS FOUND AT BS 1183 BULKHEAD VERTICAL BEAM LBL 26.83 AT WL 257 AND WL 260. REPAIR CARRIED OUT IAW APPENDIX D OF EO B727-5311-0631AND BOEING DRG 65C34406.Oct 12, 2000 · N921UP · Boeing 727180C · Fuselage Miscellaneous StructureSDR UPS00234228Skin · crackedINSPECTION TYPE:C, SKIN CRACK AT BS 243.7 WL 19 LT. CRACKED AREA OF SKIN CUT OUT IAW SRM 53-30-3 FIG 3. HFEC C/O IN ALL ACCESSED HOLES AND AROUND PERIFERY OF CUTOUT. POST FASTENER REMOVAL AND SKIN CUTOUT IAW B727 NDTM. NO DEFECTS FOUND IN FASTENER HOLES ANOct 12, 2000 · N921UP · Boeing 727180C · Fuselage Main, Plate/SkinSDR UPS00234229Structure · corrodedINSPECTION TYPE:C, BILGE IN SKIN (SUSPECT CORROSION) AT BS 1030 ABOVE STR 18 LT. GILL LINER REMOVED IAW MM 25-52-02. CORROSION ON EXTRUSION FOUND TO BE CORRODED AND OUTSIDE LIMITS SRM 53-30-01. NEW EXTRUSION INSTALLED IAW SRM 51-30-02. GILL LINER INSTALLEDOct 11, 2000 · N921UP · Boeing 727180C · Fuselage Main, StructureSDR UPS00233068Floor Support · crackedINSPECTION TYPE: C CARGO BAY FLOOR SUPPORT LONGTITUDINAL BEAMS CRACKED TWO PLACES, BS 2020, BL 0, BS 1988, LBL 30 FLOOR SUPPORT BEAMS REPAIRED IAW SRM 53-10-07Jun 23, 2000 · N921UP · Boeing 727180C · Fuselage Miscellaneous StructureSDR UPS99231117Link · corrodedINSPECTION TYPE: AD, RT MLG TRUNNION LINK HAS PITTING CORROSION ON FORWARD BEARING SURFACE. REPLACED TRUNNION LINK ASSEMBLY. INSTALLED IAW MM 32-11-01.Nov 8, 1999 · N921UP · Boeing 727180C · Main Landing Gear Attach SectionSDR UPS99231116Support · corrodedINSPECTION TYPE: AD, RT SUPPORT ASSEMBLY INBOARD FLAP TRACK FORWARD CORRODED. SUPPORT ASSEMBLY REPLACED IAW BOEING DRAWING NR 65 19297, SHEET 3, REV E.Nov 8, 1999 · N921UP · Boeing 727180C · Trailing Edge FlapsSDR UPS99231120Fitting · leakingINSPECTION TYPE:AD, FUEL LEAK AT RT WING BEHIND LANDING GEAR TRUNNION FITTING, ONLY STAINS. THIS MRR RESUBMITTED TO INCLUDE TRUNNION FITTING, FUEL LEAK REPAIRED IAW SMRO EO 99-35-001. TRUNNION FITTING REMOVED AND REPLACED DUE TO MECHANICAL DAMAGE.Nov 5, 1999 · N921UP · Boeing 727180C · Fuel StorageSDR UPS99231119Fitting · leakingINSPECTION TYPE:AD FUEL LEAK AT LT WING BEHIND LANDING GEAR TRUNNION FITTING. THIS MRR RESUBMIT TO INCLUDE TRUNNION FUEL LEAK. REPAIRED IAW SMRO EO 99-35-01 TRUNNION FITTING REMOVED AND REPLACED DUE TO MECHANICAL DAMAGE.Nov 5, 1999 · N921UP · Boeing 727180C · Fuel StorageSDR UPS99229625Angle · corrodedINSPECTION TYPE:C, CORROSION ON 'T' ANGLE ON FAIRING UNDER AIR CONDITIONING EQUIPMENT AT BS 700. REPAIRES IAW SRM 51-40-2 FIG 1.May 10, 1999 · N921UP · Boeing 727180C · Fuselage Miscellaneous StructureSDR UPS99229646Stringer · crackedINSPECTION TYPE:C, DURING ACCOMPLISHMENT OF RT 870 PARTIAL REPLACEMENT CRACK DISCOVERED AT FASTENER HOLE, LWR TANG, STR 13 AFT OF FITTING FLANGE. RT 870 FITTING REPLACED IAW UPS EO B727-5310-3056-B APPD E.May 8, 1999 · N921UP · Boeing 727180C · Fuselage Main, Longeron/StringerSDR UPS99229626Hinge · crackedINSPECTION TYPE:C, RIGHT O/B AILERON HINGE CASTING CRACKED AT WS 68605 APPROX (I/B CASTING I/B BALANCE BAY). REPLACED CASTING IAW DRG 65-19260.May 7, 1999 · N921UP · Boeing 727180C · Wing, Control Surface Attach FittingsSDR UPS99229627Frame · crackedINSPECTION TYPE:C, FRAME CRACKED SECOND FROM AFT AT MID TRACK ATTACH POINT ON AFT CARGO DOOR MOVABLE FAIRING. FRAME REPAIRED IAW SRM 51-40-3 FIG 1.May 6, 1999 · N921UP · Boeing 727180C · Fuselage Miscellaneous StructureSDR UPS99229651Skin · looseINSPECTION TYPE:C, VERTICAL STAB LT SIDE, SKIN LOOSE ADJACENT FASTENERS STR 57 AREA BELOW STAB GEARBOX FWD CUTOUT. REPAIR CARRIED OUT IAW SRM 55-30-5 FIG 4.May 5, 1999 · N921UP · Boeing 727180C · Vertical Stabilizer, Plate/SkinSDR UPS99229649Skin · delaminatedINSPECTION TYPE:C, UPPER RUDDER TAB RT SIDE HAS EVIDENCE OF DELAMINATION T/E AREA, AFT OF CENTER HINGE FITTINGS. REPAIRED IAW SRM 51-40-10 FIG 1.May 5, 1999 · N921UP · Boeing 727180C · Rudder, Tab StructureSDR UPS99229648Hinge · corrodedINSPECTION TYPE:C, RIGHT O/B AILERON TAB HINGES CORRODED. RIGHT O/B AILERON TAB HINGES REMOVED AND REPLACED IAW MM 27-10-41.May 5, 1999 · N921UP · Boeing 727180C · Aileron TabsSDR UPS99229647Casting · corrodedINSPECTION TYPE:C, RIGHT O/B AILERON TAB ROD HINGE CASTING CORRODED. HINGE CASTINGS REMOVED AND REPLACED IAW MM 27-10-41.May 5, 1999 · N921UP · Boeing 727180C · AileronsSDR UPS99229628Hinge · corrodedINSPECTION TYPE:C, RIGHT I/B AILERON CENTER HINGE FITTING CORRODED. REPLACED HINGE FITTING IAW MM 27-10-01.May 5, 1999 · N921UP · Boeing 727180C · AileronsSDR UPS99229645Bracket · crackedINSPECTION TYPE:C, ENG NR 3 THRUST REV O/B FAIRING MID SUPPORT BRACKET CRACKED. REPLACED BRACKET IAW SRM 51-30-02 AND MM 78-30-00.Apr 30, 1999 · N921UP · Boeing 727180C · Engine Thrust ReverserSDR UPS99229650Bracket · crackedINSPECTION TYPE:C, ON INSPECTION OF THE FWD CARGO BAY CEILING, CARGO DOOR UPLOCK RETAINING BRACKET FOUND CRACKED. REPLACED BRACKET IAW SRM 51-20-1 FIG 3.Apr 29, 1999 · N921UP · Boeing 727180C · Fuselage Miscellaneous StructureSDR UPS99229652Bracket · crackedINSPECTION TYPE:C, ENG NR 1 THRUST REV O/B FAIRING MID SUPPORT BRACKET CRACKED. REPLACED BRACKET IAW SRM 51-30-02 AND MM 78-30-00.Apr 28, 1999 · N921UP · Boeing 727180C · Engine Thrust ReverserSDR UPS99229643Bracket · crackedINSPECTION TYPE:C, SUSPECT CRACK ON LT ELEVATOR REAR SPAR ON BRACKET AT TAB ROD CUTOUT. CRACKED BRACKET REPLACED IAW DRAWING 65-25635.Apr 28, 1999 · N921UP · Boeing 727180C · Elevator StructureSDR UPS99229642Frame · damagedINSPECTION TYPE:C, MECHANICAL DAMAGE FOUND ON FIRST FASTENER HOLE BELOW FLOOR AT BS 825 .95 RT. AFTER CLEAN UP THIS HOLE IS OUTSIDE LIMITS PER EO B727-5310-5 474 PAGE 9. FRAME REPAIRED IAW B727-5310-5474 APPENDIX C REF SMRO EO 99-12-002 AND UPS EO B727-5310-Apr 28, 1999 · N921UP · Boeing 727180C · Fuselage Main, FrameSDR UPS99229624Seat Track · corrodedINSPECTION TYPE:C, TO FACILITATE REPAIR OF FRAME 783.95 LT, SEAT TRACK MUST BE REMOVED. ON REMOVAL, SEAT TRACK WAS FOUND TO BE CORRODED AT BS 770 LBL 62.5. NEW SEAT TRACK SECTION SPLICED IAW SRM 53-10-5 FIG 1.Apr 28, 1999 · N921UP · Boeing 727180C · Fuselage, Seat/Cargo Attach FittingsSDR UPS99229623Frame · damagedINSPECTION TYPE:C, MECHANICAL DAMAGE ON SECOND FASTENER HOLE ABOVE FLOOR AT BS 848.95 LT. ON CLEAN UP, HOLE WAS OUTSIDE LIMITS PER PAGE 9 OF EO B727-5310 -5474. REPAIR TO FRAME CARRIED OUT IAW EO B727-5310-5474 APPENDIX C REF SMRO EO 99-12-002 AND UPS EO B72Apr 28, 1999 · N921UP · Boeing 727180C · Fuselage Main, FrameSDR UPS99229621Frame · damagedINSPECTION TYPE:C, MECHANICAL DAMAGE FOUND ON SECOND FASTENER HOLE ABOVE FLOOR AT BS 783.95 LT. AFTER CLEAN UP, HOLE WAS OUTSIDE LIMITS PER EO B727-5310- 5474 PAGE 9. DAMAGED HOLE TAKEN TO 0.370 AND FREEZE PLUG INSTALLED IAW SRM 51-10- 7 REF SMRO EO 99-12-00Apr 28, 1999 · N921UP · Boeing 727180C · Fuselage Main, FrameSDR UPS99229644Bulkhead · crackedINSPECTION TYPE:C, CRACK ON RT KEEL BEAM BULK HEAD BS 930 WL 158. REPAIRED IAW SRM 51-40-2.Apr 26, 1999 · N921UP · Boeing 727180C · Fuselage Main, Bulkhead
Back to N921UP, cancelled Aug 23, 2006