N934UP, cancelled May 10, 2007

Service difficulty reports · 60

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 = 'N934UP' AND deregistration_id = 'N934UP-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 UPS03240694Light · intermittentMAIN ENTRY DOOR EMERG LT INTERMITTENT. R/R LT ASSY & BATTERIES. OPS CK OK IAW MM 33-50-67. LT ASSY P/N ON/OFF 10-0067-9/10-0067-7. S/N ON/OFF S106/7432.May 14, 2003 · N934UP · Boeing 72721C · Emergency LightingSDR UPS03240693Battery · inoperativeCOCKPIT DOOR EMERG LT INOPERATIVE. R/R BATTERIES P/N S106. IAW MM 3307. OPS CK OKAY.May 14, 2003 · N934UP · Boeing 72721C · Emergency LightingSDR UPS03240053Panel · crackedINSPECTION TYPE: C, SUSPECT CRACK IN NLG WHEEL WELL STA 245 LT SIDE PANEL. REPAIR CARRIED OUT IAW SRM 51-40-2.Jan 14, 2003 · N934UP · Boeing 72721C · Fuselage Main, BulkheadSDR UPS03240055Spar · crackedINSPECTION TYPE: C, DURING REPLACEMENT OF RT O/B RIB FOR ELEVATOR STA 209.5 LWR REAR SPAR FOUND TO BE CRACKED BETWEEN TWO FASTENERS AT O/B EDGE OF SPAR. REPAIRED IAW SRM 55-10-5 FIG 1.Jan 10, 2003 · N934UP · Boeing 72721C · Elevator, Spar/RibSDR UPS03240050Bracket · crackedINSPECTION TYPE:C ON REMOVAL OF L/H ELEVATOR PCU BRACKET ON FRONT SPAR OF ELEVATOR FOU ND TO BE CRACKED POSITION SENSOR BRACKET ON L/H ELEV. FRONT SPAR REPLACED IAW MM 27-3 0-01 PG 410 STEP 4JJan 8, 2003 · N934UP · Boeing 72721C · Elevator Control SystemSDR UPS03240057Door · crackedINSPECTION TYPE:C WING LANDING GEAR DOOR R/H SIDE CRACK FOUND ON INSIDE OF DOOR REAR S PAR OF DOOR 19TH UP FROM BOTTOM OF DOOR CRACK IS ALONG BETWEEN 2 RIV ET HOLES REPAIR CARRIED OUT IAW SRM 51-40-2Jan 7, 2003 · N934UP · Boeing 72721C · Landing Gear DoorsSDR UPS03240056Fitting · crackedINSPECTION TYPE: C, CRACK INDICATION IN ONE HOLE BS 870 LT HOLE LOCATED 2ND FASTENER ROW FROM FWD EDGE OF FITTING TOP FASTENER HOLE OF LWR FITTING. REPAIRED IAW UPS EO B727-5310-3057-H.Jan 7, 2003 · N934UP · Boeing 72721C · Fuselage Main, Attach FittingsSDR UPS03240049Bracket · brokenINSPECTION TYPE:C FLAT BRACKET BROKEN ON FUSELAGE SKIN AT BS 740 AT INTERSECTION WITH STR. 17R NEW PLATE FABRICATED IAW SRM 51-20-01 FIG 7 INSTALLED IAW SRM 51-30-02Jan 7, 2003 · N934UP · Boeing 72721C · Fuselage Main, StructureSDR UPS03240066Elevator · crackedINSPECTION TYPE:C SUSPECT CRACK ON LH ELEVATOR REAR SPAR @ 2 ND HINGE FROM O/B @ TOP I /B CORNER DUE TO UNAVAILABILITY OF REAR SPAR REPLACEMENT KIT. REPLACED L/H ELE VATOR IAW MM 27-30-01Jan 6, 2003 · N934UP · Boeing 72721C · Elevator StructureSDR UPS03240065Fitting · crackedINSPECTION TYPE:C CRACK INDICATION IN 2 HOLES BS 950 L/H HOLES LOCATED ON ROWS 2ND FRO M FWD EDGE OF FITTING AND 2ND HOLES FROM BOTTOM OF SPLICE PLATE JUST BELOW STR. 6 L/H BS 950 BULKHEAD FITTING REPLACED IAW EO B727-5310-3012 & DRAWING 65C18332 AND 2MIJan 6, 2003 · N934UP · Boeing 72721C · Fuselage Main, StructureSDR UPS03240048Skin · corrodedINSPECTION TYPE: C, POPPED RIVET HEAD AT BS 1180 STR 7L DUE TO CORROSION. ALSO FURTHER SIGNS OF CORROSION ON STR 7L BETWEEN 1180 & 1150. LFEC INSP PERFORMED AT 1180 STR 7L, 10-15 PERCENT MATERIAL LOSS EVIDENT. CORRODED SKIN REMOVED APPROX 10 INCHES X 5 INCHJan 6, 2003 · N934UP · Boeing 72721C · Fuselage Main, Plate/SkinSDR UPS03240064Frame · crackedINSPECTION TYPE: C, SUSPECT CRACK ON LT HORIZONTAL STAB UPPER FRAME JUST I/B OF ELEVATOR RIB STA 173.21. REPAIR CARRIED OUT IAW SMRO EO 2003-001-004 UPS ENGINEERING FILE 727-55-20029.Jan 4, 2003 · N934UP · Boeing 72721C · Horizontal Stabilizer, Spar/RibSDR UPS01236766Light · defectiveINSPECTION TYPE:PFLT EXIT LIGHTS STAY ON IN ARMED POSITION. REPLACED LIGHT ASSEMBLYAug 30, 2001 · N934UP · Boeing 72721C · Emergency LightingSDR UPS01236257Frame · crackedINSPECTION TYPE:C CRACK INDICATION AT FRAME, FUSELAGE BS913.5 RIGHT SIDE. CRACK CONFIRMED BY NDT INSP. PART 6 51-00-00 STOP DRILL CRACK AT FRAME AT BS 913.5 B727-51-10-01 INSTALLED KIT REPAIR AS PER EO B727- 5310-1896-B APPENDIX C AT FRAM FUSELAGE BS 913Jun 28, 2001 · N934UP · Boeing 72721C · Fuselage Main, StructureSDR UPS01236261Bulkhead · crackedINSPECTION TYPE:C, RT WHEEL WELL FWD LOWER FRAME SHOWS CRACK DAMAGE AT BS 870 RBL 4.5. REMOVED FASTENERS AT DAMAGED AREA SRM 51-30-2, CUTOUT WEB DAMAGED AREA APPROX 1 X 1.5 INCH SRM 51-40-2 AT BS 870 RBL 4.5 HFEC INSP CUT OUT IAW M/M 51-00-00 PART 6 FIG 4. IJun 20, 2001 · N934UP · Boeing 72721C · Fuselage Main, BulkheadSDR UPS01236260Bulkhead · crackedINSPECTION TYPE:C RIGHT WHEEL WELL STA 870 BULKHEAD CRACK AT APU VALVE CUT OUT RBL4.5 STOP DRILL CRACK ON RH W/W STA 870 AT APU VALVE CUT OUT RBL45 STOP DRILL 1/4" SIVE AND NDT INSPECTION ACCOMPISHED HFEC AS PER PART6-51- 00-00 FIG4 INSTALL 3 DOUBLER REPAJun 20, 2001 · N934UP · Boeing 72721C · Fuselage Main, StructureSDR UPS01236259Frame · crackedINSPECTION TYPE:C, LEFT WW FRAME 930 HAS PREVIOUS REPAIR WITH STOP HOLE, BUT IS CONTINUING UPWARDS AFTER STOP HOLE FRAME BELOW FLOOR BS 930. PERFORMED HFEC INSP ON I/B FLANGE AS PER NDT MANUAL PART 6-51-00-01 FIG 4. CRACK AT 1/4 BOLTS HOLE APPROX .5 INCH DOWJun 20, 2001 · N934UP · Boeing 72721C · Fuselage Main, FrameSDR UPS01236258Web · crackedINSPECTION TYPE:C NOSE LANDING GEAR BAY RH SIDE WALL AT BS 266 HAS A CRACK INDICATION. REMOVED ACCESS PANEL #3125 AS PER SRMB727-51-30-2 CUT OUT DAMAGE AREA AS PER B727-51-40-2 APPROX 3.5"X1" ACCOMLPISHED NDT INSPECTION AND INSTALLED DOUBLER REPAIR AS PER Jun 20, 2001 · N934UP · Boeing 72721C · Fuselage Main, StructureSDR UPS01236256Web · crackedINSPECTION TYPE:C NOSE LANDING GEAR BAY LH SIDE AT BS 259 SIDE WALL HAS A CRACK INICATION. REMOVED ACCESS PANEL #3124 AND LOWER WEB TO GAIN ACCESS TO DAMAGE AREA, CUT OUT DAMAGE AREA APPROX 5"X1" AT NOSE LANDING GEAR BS259 AS PER B727 SRM51-40-2 ACCOMPLISHJun 20, 2001 · N934UP · Boeing 72721C · Fuselage Main, StructureSDR UPS00234570Landing Gear · faultyINSPECTION TYPE:N/A NOSE GEAR DID NOT EXTEND ON FIRST TRY. RECYCLED & NOSEGEAR EXTENDED. JACKED AIRCRAFT, HEATED NOSE WHEEL AREA TO REMOVE ICE. GREASED TRUNI ON, OVERCENTER KNUCKLE, GEAR DOORS. CYCLED GEAR SEVERAL TIMES.Dec 27, 2000 · N934UP · Boeing 72721C · Landing Gear Retraction/Extension SystemSDR UPS00232190Line · crackedAIR TURN BACK ON DELIVERY FLIGHT FROM C CHECK AT SNN . CREW EXPERIENCED TOTAL LOSS OF B SYSTEM HYD PRESS . PRESS LINE FROM NR 1 B PUMP TO B SYS PRESS MODULE FOUND FRACTURED AT SLEEVE PRESS LINE CANIBALIZED FROM A/C N912UP TO REPLACE FRACTURED PIPE LINE. HYD SApr 3, 2000 · N934UP · Boeing 72721C · Hydraulic System, MainSDR UPS00232144Support Bracket · crackedINSPECTION TYPE: C, ENGINE NR 1 THRUST REVERSER O/B FAIRING MID SUPPORT BRACKET CRACKED. BRACKET REPLACED AS PER MM 78-30-00Mar 21, 2000 · N934UP · Boeing 72721C · Engine Thrust ReverserSDR UPS00232142Support Bracket · crackedINSPECTION TYPE: C, LT WING, FIXED TE SUPPORT BRACKET CRACKED, AREA BELOW 37 SPOILER I/B HINGE. REPLACED BRACKET IAW SRM 51-30-02Mar 20, 2000 · N934UP · Boeing 72721C · Wing Miscellaneous StructureSDR UPS99228741Battery Pack · dischargedINSPECTION TYPE-N/A, EMER EXIT LIGHT OVER FWD ENTRY DOOR INOP. REMOVED AND REPLACED BATTERY PACK AND OPS CHECK NORMAL PER MM 33-50-01. A/C OK FOR SERVICE.Feb 17, 1999 · N934UP · Boeing 72721C · Emergency LightingSDR UPS98227730Skin · damagedINSPECTION TYPE:D WHILE REPLACEING BS 740 LT FITTING SEVERAL HOLES ON FUSELAGE SKIN COMMON TO FITTING FOUND DAMAGED. CARRIED OUT SKIN SPLICE REPAIR IAW EO 98-27-002 ENGINEERING FILE NR 5330-2071.Sep 11, 1998 · N934UP · Boeing 72721C · Fuselage Main, Plate/SkinSDR UPS98227780Balance Panel · corrodedINSPECTION TYPE-D, CORROSION ON NR 3 BALANCE PANEL LT HORIZ STAB. BALANCE PANEL REPLACED IAW MM 27-30-21.Sep 10, 1998 · N934UP · Boeing 72721C · Horizontal Stabilizer StructureSDR UPS98227777Balance Panel · corrodedINSPECTION TYPE-D, CORROSION ON NR 5 BALANCE PANEL LT HORIZ STAB. BALANCE PANEL REPLACED IAW MM 27-30-21.Sep 10, 1998 · N934UP · Boeing 72721C · Horizontal Stabilizer StructureSDR UPS98227732Rib · corrodedINSPECTION TYPE:D TENSION TIE RIB FWD AND AFT VERTICAL HOLES ARE PITTED. REPAIR CARRIED OUT IAW SRS EO 98-27-021 ENGINEERING FILE NO 727-55-0374.Sep 10, 1998 · N934UP · Boeing 72721C · Vertical Stabilizer, Spar/RibSDR UPS98227731Rib · corrodedINSPECTION TYPE:D TENSION TIE RIB ATTACH FITTINGS FWD AND AFT VERTICAL HOLES HAVE PITTING CORROSION. REPAIR CARRIED OUT IAW SRS EO 98-27-021 ENGINEERING FILE NR 727-55-0374.Sep 10, 1998 · N934UP · Boeing 72721C · Vertical Stabilizer, Spar/RibSDR UPS98227779Balance Panel · crackedINSPECTION TYPE-D, RT STAB NR 4 BALANCE PANEL CRACKED. BALANCE PANEL REPLACED IAW MM 27-30-21.Sep 8, 1998 · N934UP · Boeing 72721C · Horizontal Stabilizer StructureSDR UPS98227778Balance Panel · corrodedINSPECTION TYPE-D, RT STAB, LIGHT SURFACE CORROSION ON NR 5 BALANCE PANEL. BALANCE PANEL REPLACED IAW MM 27-30-21.Sep 8, 1998 · N934UP · Boeing 72721C · Horizontal Stabilizer StructureSDR UPS98227729Panel · corrodedINSPECTION TYPE:D LT WING BOLT ON FUEL TANK ACCESS PANELS ARE CORRODED PANELS NR 15 - NR 19. REPLACED PANELS IAW 28-12-11.Sep 3, 1998 · N934UP · Boeing 72721C · Wing, Plate/SkinSDR UPS98227728Panel · corrodedINSPECTION TYPE:D NR 1 FUEL TANK ACCESS PANEL CORRODED (FRONT SPAR) LT WING. REPLACED PANEL IAW 28-11-10.Sep 3, 1998 · N934UP · Boeing 72721C · Wing, Plate/SkinSDR UPS98227725Bracket · crackedINSPECTION TYPE:D FRAME BS 488 OUTER CHORD ATTACH BRACKET CRACKED AT MAIN CARGO SUPPORT FITTING (FWD SIDE OF FRAME). CARRIED OUT REPAIR IAW SRM 53-10-4 FIG 11.Sep 2, 1998 · N934UP · Boeing 72721C · Fuselage Miscellaneous StructureSDR UPS98227724Bracket · crackedINSPECTION TYPE:D LT OUTBD FLAP OUTBD SUPPORT RAMP STAY ROD REAR SPAR ATTACH BRACKET SUSPECT CRACKED. REPLACED SUPPORT BRACKET IAW SRM 51-30-2.Sep 1, 1998 · N934UP · Boeing 72721C · Trailing Edge FlapsSDR UPS98227723Web · crackedINSPECTION TYPE:D LT OUTBD AILERON FIXED WEIGHT BAY, INBOARD WEB IS CRACKED. REPAIRED IAW SRM 51-30-02.Sep 1, 1998 · N934UP · Boeing 72721C · AileronsSDR UPS98227722Casting · corrodedINSPECTION TYPE:D ON FURTHER INVESTIGATION OF NR 6 SPOILER LINKAGE SUPPORT CASTING MIGRATED REWORK SLEEVE REMOVED AND CORROSION FOUND IN REWORKED AREA. REPLACED SUPPORT CASTING IAW DRAWING NR 65-16216.Sep 1, 1998 · N934UP · Boeing 72721C · SpoilersSDR UPS98227721Rib · crackedINSPECTION TYPE:D CRACK AT NR 6 SLAT I/B TRACK O/B RIB. REPAIRED RIB IAW SRM 51-40-2.Sep 1, 1998 · N934UP · Boeing 72721C · Leading Edge DevicesSDR UPS98226343Bulb · failedCABIN ENTRY DOOR EMERGENCY EXIT 1 LIGHT INOP. RELAMPED, GROUND CHECKS OK.Apr 9, 1998 · N934UP · Boeing 72721C · Emergency LightingSDR UPS97224438Hose · leakingINSPECTION TYPE-N/A, LOSS OF HYDRAULIC SYSTEM 'B' FLUID AT 15,000 FT BOTH 1 AND 2 'B' PUMPS LOW PRESS LIGHTS CAME ON, QTY INDICATION 0. DECLARED EMERGENCY, COMPLIED WITH CHECKLISTS, LANDED WITHOUT FURTHER INCIDENT. FOUND NR 1 'B' PUMP PRESSURE LINE CHAFED THSep 16, 1997 · N934UP · Boeing 72721C · Hydraulic System, MainSDR UPS97224319Actuator · leakedINSPECTION TYPE-N/A, LOSS OF HYDS, GEAR EXTENDED MANUALLY. FOUND LEAK AT NR 5 LE SLAT ACTUATOR. REMOVED AND REPLACED ACTUATOR IAW MM 27-81-3 2, SERVICED HYDS, RAN ENGINES, CYCLED ALL FLT CONTROLS, CKD FOR LEAKS, OK FOR SERVICE.Aug 29, 1997 · N934UP · Boeing 72721C · Leading Edge Slat ActuatorSDR UPS205333Mid Spar · chafedWHILE IN FOR C-CHECK MAINTENANCE REPORTED, LT VENT FIN MID SPAR CHORD IS CHAFED AT ACCESS PNL 9601. REPAIRED AS REQUIRED PER UPS EO 727-55-0309.Jan 25, 1996 · N934UP · Boeing 72721C · Vertical StabilizerSDR UPS205319Wedge · corrodedWHILE IN FOR C-CHECK MAINTENANCE REPORTED, REMOVED AND REPLACED RT I/B MIDFLAP T/E WEDGE. REPLACED AS REQUIRED PER SRM 51-30-2.Jan 24, 1996 · N934UP · Boeing 72721C · Trailing Edge FlapsSDR UPS205332Rib · crackedWHILE IN FOR C-CHECK MAINTENANCE REPORTED, RT NR 2 ELEVATOR HINGE SUPPORT RIB IS CRACKED ON I/B UPPER FLANGE NEAR AFT END. REMOVED RT NR 2 ELEVATOR HINGE SUPPORT RIB IAW SRM 51-30-2.Jan 23, 1996 · N934UP · Boeing 72721C · Horizontal Stabilizer, Spar/RibSDR UPS205331Slat · crackedWHILE IN FOR C-CHECK MAINTENANCE REPORTED, NR 5 SLAT AFT LOWER CHORD O/B END CRACKED. REMOVED AND REPLACED NR 5 SLAT IAW MM 27-81-11.Jan 23, 1996 · N934UP · Boeing 72721C · Leading Edge DevicesSDR UPS205330Bonding Jumper · corrosionWHILE IN FOR C-CHECK MAINTENANCE REPORTED, NR 6 FLAP O/B LOWER BONDING JUMPER HAS CORROSION AROUND ATTACH BOLT UPPER END LOWER SURFACE. REMOVED AND REPLACED NR 6 K-FLAP IAW MM 27-81-01 AND 27-81-00.Jan 23, 1996 · N934UP · Boeing 72721C · Leading Edge DevicesSDR UPS205329Angle · crackedWHILE IN FOR C-CHECK MAINTENANCE REPORTED, NR 7 SLAT I/B TRACK I/B RIB SUPPORT ANGLE CRACKED. REPAIRED IAW 57-50-03, 51-30-2, OHM 57-51-41, MM 27-81-11 AND SRM 51-20-1.Jan 23, 1996 · N934UP · Boeing 72721C · Leading Edge DevicesSDR UPS205327Rod End · corrodedWHILE IN FOR C-CHECK MAINTENANCE REPORTED, RT WING O/B ROD END CLEVIS IS PITTED. REMOVED AND REPLACED RT WING O/B AILERON ROD END CLEVISES IAW MM 57-50-11 AND 27-10-00.Jan 23, 1996 · N934UP · Boeing 72721C · Aileron Control SystemSDR UPS205326Hinge Tab · corrodedWHILE IN FOR C-CHECK MAINTENANCE REPORTED, RT WING I/B AILERON TAB HINGES ARE CORRODED. REMOVED AND REPLACED RT WING I/B AILERON TAB HINGES IAW SRM 51-30-02 AND MM 51-10-0.Jan 23, 1996 · N934UP · Boeing 72721C · Aileron Tab Control SystemSDR UPS205328Hinge Fitting · corrodedWHILE IN FOR C-CHECK MAINTENANCE REPORTED, RT WING O/B AILERON CENTER HINGE FITTING PITTED AILERON SIDE. REMOVED AND REPLACED CENTER HINGE FITTING IAW 51-30-2 AND MM 27-10-31. ALSO, FOUND CRACKED RIB SUPPORT BRACKET. REMOVED AND REPLACED BRACKET IAW SRM 51-Jan 22, 1996 · N934UP · Boeing 72721C · Aileron Control System
Back to N934UP, cancelled May 10, 2007