N925UP, cancelled Aug 23, 2006

Service difficulty reports · 105

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 = 'N925UP' AND deregistration_id = 'N925UP-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 UPS02239958Door · out of rigNOISE FROM NLG AREA DURING FLIGHT, WITH RED DOOR WARNING INDICATION. LEVEL AT FL260, MACH 0.82, 342 KIAS. HEARD LOUD THUMPING FROM FRONT OF AIRCRAFT WITH ASSCOCIATED RED 'DOORS' ANNUNCIATOR, SLOWED TO MACH 0.80 AND CONDITION WENT AWAY. PERFORMED NLG DOOR RIDec 4, 2002 · N925UP · Boeing 72731C · Landing Gear Door Retract SectionSDR UPS02237879Fitting · crackedINSPECTION TYPE:C CRACK AND CORROSION INDICATIONS FROM FASTENER HOLES AT BS 870L STR 13L TO STR 12L.Feb 28, 2002 · N925UP · Boeing 72731C · Fuselage Miscellaneous StructureSDR UPS02237819Stringer · crackedINSPECTION TYPE:C WHILE CARRYING OUT SKIN SPLICE AT L/H BS 740 FITTING STR 23L FOUND T O BE CRACKED STRINGER REPAIR CARRIED OUT IAW SRM 53-10-03Feb 26, 2002 · N925UP · Boeing 72731C · Fuselage Main, StructureSDR UPS02237872Support Fitting · crackedINSPECTION TYPE:C LH ELEVATOR, STA 46.50, ACTUATOR ATTACH SUPPORT FITTING, CRACK BETWE EN THREE FASTENER HOLES LH ELEVATOR REPLACED. REF. NRC 450554.Feb 25, 2002 · N925UP · Boeing 72731C · Elevator StructureSDR UPS02237822Rib · crackedINSPECTION TYPE:C LT WING, NR 3 SLAT, CRACK IN O/B RIB AT O/B TRACK, FWD TRACK ATTACH AREA. CRACK STOP DRILLED IAW SRM 51-10-1, REPAIR CARRIED OUT IAW SRM 57-50-3.Feb 25, 2002 · N925UP · Boeing 72731C · Leading Edge DevicesSDR UPS02237821Link · corrodedINSPECTION TYPE:C ON REMOVAL OF LT MLG TRUNNION LINK EXCESSIVE CORROSION WAS FOUND ON FWD SPLINED LOCKING SLEEVE. LT MLG TRUNNION LINK REPLACED IAW MM 32-11-01.Feb 25, 2002 · N925UP · Boeing 72731C · Main Landing Gear Attach SectionSDR UPS02237871Fitting · crackedINSPECTION TYPE:C LT BS 740 FITTING CRACKED IN 2 PLACES IN O/B FLANGE LOWER END. REPLACED LT FITTING IAW EO B727-5310-7477-G.Feb 21, 2002 · N925UP · Boeing 72731C · Fuselage Miscellaneous StructureSDR UPS02237869Keelbeam · crackedINSPECTION TYPE:C CRACK FOUND IN KEEL BEAM WEB FWD OF APU CUTOUT. CRACK REPAIRED IAW SRM ADDENDUM EO B727-5330-1995-B USING KIT P/N 65 -88832-2 AND BOEING DRG 65-88832 AND 65-22466.Feb 21, 2002 · N925UP · Boeing 72731C · Fuselage Main, KeelSDR UPS01236156Uplock · failedINSPECTION TYPE:N/A NOSE LANDING GEAR TOOK 4 CYCLES TO EXTEND MANUAL EXTENSION WAS NO HE LP. *S/D* REF WDM 32-64-01 REMOVED AND REPLACED WIRE BETWEEN S96 & S93. REMOVED AND ADJUSTED CORRECTLY. REMOVED AND REPLACED NLG LOCK ACT W/REF 32-33-11, PERFORMED NLGJun 20, 2001 · N925UP · Boeing 72731C · Landing Gear Retraction/Extension SystemSDR UPS00233659Stringer · corrodedINSPECTION TYPE:C, ON REMOVAL OF ATTACH BRACKET FASTENERS CORROSION FOUND ON STR 24L AT BS 740. STRINGER REPAIRED IAW SRM 53-10-3 FIG 1.Aug 22, 2000 · N925UP · Boeing 72731C · Fuselage Main, Longeron/StringerSDR UPS00233670Bolt · crackedINSPECTION TYPE:C, ENG NR 2 LEFT ADAPTER FITTING SUSPENSION LINK UPPER ADAPTER FITTING DUE CRACK IN TREADS. REPLACED BOLT IAW MM 71-21-12.Aug 17, 2000 · N925UP · Boeing 72731C · Engine Mount SectionSDR UPS00233669Bolt · crackedINSPECTION TYPE:C, ENG NR 2 LEFT ADAPTER FITTING SWING LINK BOLT FAILED NDI DUE CRACK IN THREADS. REPLACED BOLT IAW MM 71-21-12.Aug 17, 2000 · N925UP · Boeing 72731C · Engine Mount SectionSDR UPS00233668Bolt · crackedINSPECTION TYPE:C, ENG NR 2 RIGHT ADAPTER FITTING CONE BOLT ATTACH BOLT FAILED NDI DUE CRACK IN THREADS. REPLACED BOLT IAW MM 71-21-22.Aug 17, 2000 · N925UP · Boeing 72731C · Engine Mount SectionSDR UPS00233667Bolt · crackedINSPECTION TYPE:C, ENG NR 3 AFT LOWER CRANE BEAM SHOULDER BOLT FAILED NDI DUE CRACK COMING FROM SPLIT PIN HOLE. ALSO, CAD PLATING DAMAGED. NR 3 ENG AFT CRANE BEAM LOWER SHOULDER BOLT REPLACED IAW MM 71-21-03.Aug 17, 2000 · N925UP · Boeing 72731C · Engine Mount SectionSDR UPS00233666Bolt · crackedINSPECTION TYPE:C, ENG NR 3 FWD LOWER CRANE BEAM SHOULDER BOLT FAILED NDI DUE CRACK COMING FROM SPLIT PIN HOLE. ALSO, CAD PLATING DAMAGED. NR 3 ENG FWD CRANE BEAM LOWER SHOULDER BOLT REPLACED IAW MM 71-21-03.Aug 17, 2000 · N925UP · Boeing 72731C · Engine Mount SectionSDR UPS00233665Bolt · crackedINSPECTION TYPE:C, ENG NR 1 FWD UPPER CRANE BEAM SHOULDER BOLT FAILED NDI DUE CRACK COMING FROM SPLIT PIN HOLE. ALSO, CAD PLATING DAMAGED. ENG NR 1 FWD CRANE BEAM UPPER SHOULDER BOLT REPLACED IAW MM 71-21-03.Aug 17, 2000 · N925UP · Boeing 72731C · Engine Mount SectionSDR UPS00233664Bolt · crackedINSPECTION TYPE:C, ENG NR 1 AFT LOWER CRANE BEAM SHOULDER BOLT FAILED NDI DUE CRACK COMING FROM SPLIT PIN HOLE. ALSO, CAD PLATING DAMAGED. NR 1 ENG AFT CRANE BEAM LOWER SHOULDER BOLT REPLACED IAW MM 71-21-03.Aug 17, 2000 · N925UP · Boeing 72731C · Engine Mount SectionSDR UPS00233663Bolt · crackedINSPECTION TYPE:C, ENG NR 1 AFT UPPER CRANE BEAM SHOULDER BOLT FAILED NDI DUE CRACK COMING FROM SPLIT PIN HOLE. ALSO, CAD PLATING DAMAGED. NR 1 ENG AFT CRANE BEAM UPPER SHOULDER BOLT REPLACED IAW MM 71-21-03.Aug 17, 2000 · N925UP · Boeing 72731C · Engine Mount SectionSDR UPS00233662Web · crackedINSPECTION TYPE:C, AFT CARGO DOOR HINGE FWD WEB CRACKED AT INNER CORNER. FABRICATED WEB IAW DRW 69-19170. AFT CARGO DOOR FWD HINGE FWD WEB REPLACED IAW DRAWING 65-18625.Aug 17, 2000 · N925UP · Boeing 72731C · Fuselage Miscellaneous StructureSDR UPS00233661Web · crackedINSPECTION TYPE:C, AFT CARGO DOOR AFT HINGE FWD WEB CRACKED AT UPPER CORNER. AFT CARGO DOOR AFT HINGE FWD WEB REPLACED IAW DRW 65-18625.Aug 17, 2000 · N925UP · Boeing 72731C · Fuselage Miscellaneous StructureSDR UPS00233637Angle · corrodedINSPECTION TYPE:C, CRACK ON ANGLE BETWEEN SKIN AND RIB IN RIGHT WING L/E CAVITY AT O/B END OF NR 6 L/E FLAP. REPLACED ANGLE AND INSTALLED FASTENERS IAW SRM 51-30-02 AND BOLTS IAW OHM 20-50-01.Aug 17, 2000 · N925UP · Boeing 72731C · Wing Miscellaneous StructureSDR UPS00233658Bulkhead · corrodedINSPECTION TYPE:C EVIDENCE OF CORROSION UNDER RIVET HEAD ON BS 870 BULKHEAD I DOWN FROM PRES DECK, 42 INCHES RIGHT OF KEEL BEAM (RT WHEEL WELL). HFEC INSP OF THE CUTOUT PERIPHERY C/O NDF BULKHEAD REPAIRED IAW SRM 53-10-9 FIG 4.Aug 16, 2000 · N925UP · Boeing 72731C · Fuselage Main, BulkheadSDR UPS00233660Rib · crackedINSPECTION TYPE:C, NR 4 L/E SLAT 2 RIBS CRACKED OUTBOARD OF OUTBOARD TRACK. RIBS REPAIRED IAW SRM 57-50-3 FIG 9 & SRM 51-30-2.Aug 15, 2000 · N925UP · Boeing 72731C · Leading Edge DevicesSDR UPS00233657Bolt · crackedINSPECTION TYPE:C, ENG NR 2 FWD MOUNT CROSS STRUT AFT ATTACH BOLT FAILED NDI DUE BOLT CRACKED. NR 2 ENG FWD MOUNT CROSS STRUT AFT ATTACH BOLT REPLACED PER MM 71-21-1 2.Aug 15, 2000 · N925UP · Boeing 72731C · Engine Mount SectionSDR UPS00233656Firewall · crackedINSPECTION TYPE:C, SUSPECT CRACK ON WEB OVER ENGINE NR 2 HORIZONTAL FIRE WALL BS 1376 RT. HFEC C/O, CRACK CONFIRMED. FABRICATED AND INSTALLED WEB IAW DRAWING 657555.Aug 15, 2000 · N925UP · Boeing 72731C · Nacelle/Pylon, Bulkhead/FirewallSDR UPS00233655Bolt · crackedINSPECTION TYPE:C, ENGINE NR 2 FWD LEFT CONE BOLT HOUSING ATTACHMENT BOLTS, AFT UPPER BOLT FAILED NDI DUE BOLT CRACKED. ENG NR 2 FWD LEFT CONE BOLT HOUSING ATTACH BOLTS AFT UPPER REPLACED IAW MM 71-21-12.Aug 15, 2000 · N925UP · Boeing 72731C · Engine Mount SectionSDR UPS00233636Skin · corrodedINSPECTION TYPE:C, SUSPECT CORROSION BETWEEN SKIN AND INTERNAL STRUCTURE BS 1020 S17L. HFEC INSP C/O ON HOLES IN ABOVE AREA. NO DEFECT FOUND. CORROSION REMOVED IAW SRM 51-10-06 FROM SKIN AND FROM CUSP ANGLE SKIN CUTOUT BS 1020 S17L. REPAIRED AREA IAW SRM 5Aug 14, 2000 · N925UP · Boeing 72731C · Fuselage Main, Plate/SkinSDR UPS00233635Skin · corrodedINSPECTION TYPE:C, SUSPECT CORROSION BETWEEN SKIN AND STRUCTURE BS 1178 BETWEEN S7R & 9R. FASTENERS REMOVED, CORROSION FOUND TO BE OUT OF LIMITS. REMOVED DAMAGED SKIN BETWEEN BS 1183 - 1165 RT S7R - S9R IAW SRM 53-30-3. NDT INSP C/O. NO DEFECT FOUND. REPAAug 14, 2000 · N925UP · Boeing 72731C · Fuselage Main, Plate/SkinSDR UPS00233365Apu · overservicedINSPECTION TYPE:N/A, APU FIELD RELAY TRIPPED FLIGHT DECK FILLED WITH SMOKE. FOUND APU OVERSERVICED WITH OIL. RESERVICED APU PACKS, RUN ALL AND OPS CHECK NORMAL WITH NO SMOKE.Jul 12, 2000 · N925UP · Boeing 72731C · APU Cowling/ContainmentSDR UPS00231602Bulb · failedDURING ASE, COCKPIT EMERGENCY EXIT IND ONE FILAMENT INOP. RELAMPED EMERGENCY EXIT LIGHT IN COCKPIT FROM AIRCRAFT SPARE STOWAGE.Feb 11, 2000 · N925UP · Boeing 72731C · Emergency LightingSDR UPS99230638Spar · crackedINSPECTION TYPE:N/A, LT WING AFT FALSE SPAR LWR. CAP CRACKED BELOW I/B GROUND SPOILER ACTUATOR SUPPORT BRACKET AT TERMINATING END. DAMAGE APROX 1.25 INCHES IN LENGTH. *S/D* REPAIRED CRACK PER UPS EO B727-5750-11867-A, PARA 6A. CRACK STOP DRILLED IAW SRM 5Sep 19, 1999 · N925UP · Boeing 72731C · Wing SparSDR UPS99229832Light · looseINSPECTION TYPE:N/A, DURING TAKEOFF THE FLIGHT DECK EMERGENCY LIGHT FELL OFF MOUNT. REINSTALLED EMERGENCY EXIT LIGHT ASSY, OPS CHECKS NORMAL.Jun 13, 1999 · N925UP · Boeing 72731C · Emergency LightingSDR UPS99229608Out Flow Valve · stuckINSPECTION TYPE:SI, AIR TURNBACK AT 1945UTC DUE TO UNSATISFACTORY AIRCRAFT PRESSURIZATION. WHEN CLIMB THRUST SET, CARGO HEAT O'FLOW VALVE CLOSED, FULL MANUAL INCRASE ON MANUAL CONTROLLER. AIRCRAFT WAS ONLY ABLE TO MAINTAIN A CABIN ALTITUDE OF 8,000 AND DIFFEMay 14, 1999 · N925UP · Boeing 72731C · Pressure Regulator/Outflow ValveSDR UPS99229607Airstair · out of adjustINSPECTION TYPE:SI, AFT AIRSTAIR LIGHT ILLUMINATED IN FLT. VISUAL INSPECTION OF STAIR AREA SHOWED FLEXING OF DOOR ARMS INDICATIVE OF UNLOCK CONDITION. DOOR LIGHT WENT OUT WITH INITAIL FLAP SELECTION TO 2 DEGREES (POSSIBLE AIRFLOW CHANGE ON DOOR/STAIR AREA). May 14, 1999 · N925UP · Boeing 72731C · Passenger/Crew DoorsSDR UPS99229610Connector · dirtyINSPECTION TYPE:SI, AIR TURNBACK AT 0100 UTC UPON GEAR RETRACTION, GEAR LEVER WOULD NOT MOVE PAST OFF POSITION. ALSO, I/B ANTISKID RELEASE REMAINED ON IN FLIGHT WITH GEAR HANDLE IN DOWN/IN POSITION. REMOVED, CLEANED CONNECTOR AND RE-INSTALLED ANTISKID CONTROMay 13, 1999 · N925UP · Boeing 72731C · Landing Gear Position and WarningSDR UPS99229606Track · corrodedINSPECTION TYPE:SI (CORROSION C57-581-06.00-04) ON NR 6 FLAP TRACK AT SPOILER BEAM PAD. CORROSION ON SPOILER BEAM PAD IS OUT OF LIMITS IAW SRM 57-40-02. FLAP TRACK WAS REPLACED ON CID 888728.May 13, 1999 · N925UP · Boeing 72731C · Trailing Edge FlapsSDR UPS99229551Floorbeam · corrodedINSPECTION TYPE:SI, CORROSION ON STRAP ON FLOORBEAM UPPER CHORD LOWER SIDE BS 312, BL 0, WL 208. REPAIR TO BE ACCOMPLISHED ON CUSTOMER ID 888989.May 10, 1999 · N925UP · Boeing 72731C · Fuselage Main, Floor BeamSDR UPS99229561Fitting · corrodedINSPECTION TYPE:SI, CORROSION ON NR 7 FLAP TRACK FWD ATTACH FITTING. FITTING WAS REWORKED ON NRC NR 888956 AND REINSTALLED ON NRC NR 888744.May 7, 1999 · N925UP · Boeing 72731C · Trailing Edge FlapsSDR UPS99229562Fitting · corrodedINSPECTION TYPE:SI, CORROSION ON NR 8 FLAP TRACK FWD ATTACH FITTING. REWORKED FITTING PER ER 99-5226.May 6, 1999 · N925UP · Boeing 72731C · Trailing Edge FlapsSDR UPS99229517Chord · corrodedINSPECTION TYPE:SI, 740 UPPER CHORD CORRODED RBL 65-70 WL 202. REMOVED AND REPLACED CHORD SEGMENT RBL 53-55 TO RIGHT O/B END.May 3, 1999 · N925UP · Boeing 72731C · Fuselage Miscellaneous StructureSDR UPS99229515Skin · corrodedINSPECTION TYPE:SI, INTERIOR FUSELAGE SKIN AT STA 873-877 RT WL 261 ALONG EDGE OF 5-10R IS CORRODED. BLENDED CORROSION ON LOWER SKIN, HFEC FASTENER HOLES, FLAT PEENED THE BLENDED AREA. ALODINED AND PRIMED BLENDED AREA, FABRICATED REPAIR DOUBLER AND REPAIR FIApr 29, 1999 · N925UP · Boeing 72731C · Fuselage Main, Plate/SkinSDR UPS99229559Skin · corrodedINSPECTION TYPE:SI, CORROSION (C57-174-01-1B) ON INTERNAL 870 SKIN AT UPPER SPAR CHORD BS 870, RBL 61-64. REMOVED CORROSION PER SRM 57-30-1, FLAP PEENED AREA PER ER NR 99-5258, ALODINED AND PRIMED PER ER NR 99-5258.Apr 27, 1999 · N925UP · Boeing 72731C · Fuselage Main, Plate/SkinSDR UPS99229283Floorbeam · corrodedINSPECTION TYPE:SI CORROSION ON FLOORBEAM BS 312, LBL 3.5, WL 208. REMOVED AND REPLACED UPPER CHORD SEGMENT PER SRM 53-10-8 FIG 9.Apr 11, 1999 · N925UP · Boeing 72731C · Fuselage Main, Floor BeamSDR UPS99229375Stringer · corrodedINSPECTION TYPE:SI BS 851 STR 2 RT FOUND TO BE OUT OF LIMITS. REPAIRED PER SRM 53-10-3 CPCP.Apr 9, 1999 · N925UP · Boeing 72731C · Fuselage Main, Longeron/StringerSDR UPS99229286Stringer · crackedINSPECTION TYPE:SI CRACKS AROUND UPPER AND LOWER FASTENERS IN STRINGER 15R COMMON TO BS 400 FRAME. REPAIRED PER SRM 53-10-3.Apr 9, 1999 · N925UP · Boeing 72731C · Fuselage Main, Longeron/StringerSDR UPS99229281Seat Track · corrodedINSPECTION TYPE:SI CORROSION C53-224-01.05-01, ON FLANGE OF SEAT TRACK BS 740, LBL 25, WL 208, CUT OUT DAMAGED SECTION DUE TO THE EXTENT OF CORROSION. FABRICATED REPAIR PARTS (SEAT TRACK AND STRAPS). ALODINE, PRIMED AND INSTALLED REPAIR PARTS PER SRM 53-10-5Apr 9, 1999 · N925UP · Boeing 72731C · Fuselage, Seat/Cargo Attach FittingsSDR UPS99229280Doubler · corrodedINSPECTION TYPE:SI WHILE WORKING NRC 888366 (FUSE 123) LT 870 ACCESS COVER (PANEL) DOUBLER RING IS CORRODED LBL 58, BS 870, WL 180. AFTER THE CORROSION REMOVAL, THE DOUBLER RING WENT BEYOND THE SRM LIMITS. REMOVED DOUBLER RING AND FABRICATED A NEW ONE. ALODApr 9, 1999 · N925UP · Boeing 72731C · Fuselage Miscellaneous StructureSDR UPS99229278Stringer · corrodedINSPECTION TYPE:SI, CORROSION AT BS 806 STR 2 FOUND TO BE OUT OF LIMITS. REPAIRED SRM 53-10-3.Apr 9, 1999 · N925UP · Boeing 72731C · Fuselage Main, Longeron/StringerSDR UPS99229274Shear Tie · crackedINSPECTION TYPE:SI CRACKED SHEAR TIE AT BS 400 BETWEEN STR 14R AND STR 15R. REPLACED PER SRM 51-30-2.Apr 9, 1999 · N925UP · Boeing 72731C · Fuselage Miscellaneous StructureSDR UPS99229273Stringer · crackedINSPECTION TYPE:SI CRACKS AROUND UPPER FASTENER ON STR 16R COMMON TO BS 500 FRAME. REPAIRED PER SRM 53-10-3.Apr 9, 1999 · N925UP · Boeing 72731C · Fuselage Main, Longeron/Stringer
Back to N925UP, cancelled Aug 23, 2006