N523UP, cancelled Jul 7, 2010

Service difficulty reports · 146

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 = 'N523UP' AND deregistration_id = 'N523UP-2010-07-07'
  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 UPS08451372Cadc · malfunctionedINSPECTION TYPE:N/A ATB - RVSM - CAPTAINS ALTIMETER 1500' OF ALTITUDE AT 330, WENT TO ALT STATIC SOURCE. AS PER MM 34-11-00 AND 34-12-01 INSP NR 1 CADC AND PITOT STATIC SYS. DRAINED SOME WATER FROM STATIC LINES. REMOVED AND REPLACED NR 1 CADC PER MM 34-12-0Jan 3, 2008 · N523UP · Boeing 747200 · Air Data ComputerSDR UPS07450908Stringer · damagedSTR 45L DAMAGED. REMOVED STR 45L DAMAGE AS PER SRM 53-10-03. FABRICATED SPLICES FOR REPAIR AS PER SRM 53-10-03. INSTALLED NEW STRINGER AND SPLICES AS PER SRM 53-10-03.Oct 10, 2007 · N523UP · Boeing 747200 · Fuselage Main, Longeron/StringerSDR UPS07450412Fire Loop · damagedINSPECTION TYPE:N/A ON CLIMBOUT THE FWD PANEL FIRE DETECTION LIGHT WAS FLICKERING; NR 4 ENGINE NACELLE TEMP IND -A- WAS FLICKERING FROM 0 TO 9 AT SAME TIME & RATE AS FIRE DETECTION LIGHT. THIS IS INTERMITTENT; SELECTED LOOP-B. THE SYSTEM TEST AND WORKS. FOUJul 27, 2007 · N523UP · Boeing 747200 · Fire DetectionSDR UPS07450171Floor Panel · cracked3.5 INCH CRACK IN BULK CARGO COMPARTMENT FLOOR BETWEEN OBI BOXES. REPAIRED IAW SRM 51-40-02 FIG 1.Jul 15, 2007 · N523UP · Boeing 747200 · Fuselage Floor PanelSDR UPS07449325Light · inoperativeINSPECTION TYPE:N/A EMERGENCY LIGHTS INOP AT ESCAPE SLIDE DOOR FRAME AND EXIT SIGN ABOVE SLIDE. REMOVED AND REPLACED POWER SUPPLY MODULE FOR EXIT SIGN PER MM 33-51-04. EXIT SIGN OPS CHECKS NORMAL. LIGHTS IN ESCAPE DOOR FRAME STILL INOP. NEEDS MODULE X327, Mar 5, 2007 · N523UP · Boeing 747200 · Emergency LightingSDR UPS06448778Lock · damagedATB - NR 1 THRUST REVERSER UNLOCK LIGHT FLASHING DURING FLIGHT. NR 1 THRUST REVERSER DEFERRED AND LOCKED OUT M340031 ASSIGNED. NR 1 ENGINE SHUT DOWN AS A PRECAUTION. R & R NR 1 ENGINE THRUST REVERSER SYCN LOCK PER MM 78-34-12. #1 T/R AND OPS CHECKS GOOD PER Dec 17, 2006 · N523UP · Boeing 747200 · Engine Thrust ReverserSDR UPS06448292A/C Pack · odorINSPECTION TYPE:N/A NR 3 PACK OVERHEATS, ALSO BURNING SMELL. TRIPS RESET, TRIPPED AGAIN. NR 3 PACK AUTO FEATURE DEFERRED PER MEL 21-6-1, BYPASS VALVE GOES TO FULL HOT IN AUTO. R/R PACK TEMP CONTROLLER PER 21-62-06. OPS CK NORMAL. THIS CLEARS M336046.Oct 20, 2006 · N523UP · Boeing 747200 · Cabin Cooling SystemSDR UPS06448249Skin · corrodedINSPECTION TYPE: C FX BS 2180-2186 S46-47R EXISTING REPAIR REMOVE REQUIRE FOR CUTOUT EVALUATION. CORROSION BLEND OUT 0.048 INCH X 1INCH X .7500 INCH, FX BS 2180 TO BS 2193 STR 44R TO STR 48R AREA LAP AND BUTT JOINT SKIN REPAIRED IAW RS R53-61-35631 REPEAT INOct 3, 2006 · N523UP · Boeing 747283B · Fuselage Main, Plate/SkinSDR UPS06448211Vertical Beam · crackedINSPECTION TYPE-C NR 4L MED FWD LOWER CORNER VERTICAL BEAM FOUND CRACK APPROX 1 INCH LONG. NR 4L MED FWD LOWER CORNER VERTICAL BEAM REPAIRED IAW SRM 52-10-02 FIG 10.Sep 26, 2006 · N523UP · Boeing 747283B · Service DoorsSDR UPS06448207Vertical Beam · crackedINSPECTION TYPE-C NR 1R MED FWD LOWER CORNER VERTICAL BEAM FOUND CRACK APPROX 1.5 INCH LONG. NR 1R MED FWD LOWER CORNER VERTICAL BEAM REPAIRED IAW SRM 52-10-02 FIG 10.Sep 26, 2006 · N523UP · Boeing 747283B · Passenger/Crew DoorsSDR UPS06448206Vertical Beam · crackedINSPECTION TYPE-C NR 2L MED FWD LOWER CORNER VERTICAL BEAM FOUND CRACK APPROX .7500 INCH LONG. NR 2L MED FWD LOWER CORNER VERTICAL BEAM REPAIRED IAW SRM 52-10-02 FIG 10.Sep 26, 2006 · N523UP · Boeing 747283B · Passenger/Crew DoorsSDR UPS06448212Attach Fitting · corrodedINSPECTION TYPE-C CORROSION FOUND AT 1 FASTENER HOLE AT FRAME WEB ATTACH FITTING LOCATED AT BS 979 S38L. FWD CARGO COMPT BS979 S38L FRAME ATTACHED FTG REPLACED AND INSTALLED IAW SRM 51-10-01 PG 9 AND 51-30-02.Sep 23, 2006 · N523UP · Boeing 747283B · Fuselage Main, Attach FittingsSDR UPS06448208Fitting · corrodedINSPECTION TYPE-C FX LT BS 980 STR 38L UPPER AND LOWER DRAG SPLICE FITTINGS ATT BOLT HOLE AREA FOUND CORROSION. CORROSION BLEND OUT 0.092 INCH BY 1.5 INCH BY 3 INCH. FX LT BS 980 STR 38L UPPER AND LWR DRAG SPLICE FTGS REPLACED AND INSTALLED IAW SRM 51-10-01 Sep 23, 2006 · N523UP · Boeing 747283B · Fuselage Miscellaneous StructureSDR UPS06448182Stringer · crackedCRACK FOUND AT 1 FASTENER HOLE LOCATED AT BS 983 STR 38L APPROX 1" LONG RUNNING FORWARD AS MARKED. FX BS 970 TO BS 990 STR 38L STRINGER REPAIRED AS PER SRM 53-10-03 FIG 1.Sep 23, 2006 · N523UP · Boeing 747283B · Fuselage Main, Longeron/StringerSDR UPS06448209Vertical Beam · crackedINSPECTION TYPE-C M/D RT NR 5 DOOR INTERIOR FWD LWR CORNER VERTICAL BEAM FOUND CRACK, CRACK LENGTH 4.7500 INCH APPROX. M/D RT NR 5 DOOR INTERIOR FWD LOWER CORNER VERTICAL BEAM REPAIRED IAW SRM 51-10-02 FIG 10.Sep 22, 2006 · N523UP · Boeing 747283B · Passenger/Crew DoorsSDR UPS06448231Skin · crackedINSPECTION TYPE:C AFT CARGO DOOR CUTOUT FWD UPPER CORNER HINGE FAIRING COVERED AREA FOUND 1 CRACK AT SKIN AT THE MOST AFT HOLE APPROX 0.040" (CRACK LENGTH 0.040"). AFT CARGO DOOR CUTOUT FWD UPPER CORNER SKIN REPAIRED AS PER SRM 53-30-03 FIG 62. SUBSEQUENT INSep 21, 2006 · N523UP · Boeing 747283B · Fuselage Main, Plate/SkinSDR UPS06448210Door Frame · crackedINSPECTION TYPE-C M/D RT DOOR FRAME INTERIOR FACE AFT LWR CORNER AREA FOUND CRACKED, CRACK LENGTH 2.5 INCH APPROX. M/D R4 DOOR FRAME AFT LOWER CORNER AREA REPAIRED IAW SRM 52-10-02 FIG 10.Sep 21, 2006 · N523UP · Boeing 747283B · Fuselage Main, StructureSDR UPS06448239Frame · crackedINSPECTION TYPE:C NR 3 PYLON REAR UPPER ENG MT BULKHEAD O/B FWD FRAME FOUND CRACK AT UPPER PORTION, CRACK LENGTH 1.5". NR 3 PYLON REAR BULKHEAD O/B FWD FRAME REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.Sep 20, 2006 · N523UP · Boeing 747283B · Nacelle/Pylon, Plate/SkinSDR UPS06448233Skin · crackedINSPECTION TYPE:C FWD CARGO DOOR, DOOR EXTERNAL SKIN SURFACE FOUND DENT MARK AT STA 582, 6" TO LOWER EDGE, CRACK LENGTH 1/8". FWD CARGO DOOR EXTERNAL SKIN REPAIRED AT BS 582 6" ABOVE LOWER EDGE AREA AS PER SRM 52-00-03 FIG 4. SUBSEQUENT INSPECTION IS REQUIRESep 20, 2006 · N523UP · Boeing 747283B · Cargo/Baggage DoorsSDR UPS06448181Frame · crackedAPU COMPT BS 2675 LT WL325 FRAME FOUND CRACK AS MARKED, CRACK LENGTH .500 INCH. APU COMPT BS 2675 LT WL 325 FRAME REPAIRED AS PER SRM 51-40-03 FIG 1.Sep 20, 2006 · N523UP · Boeing 747283B · Fuselage Main, FrameSDR UPS06448180Frame · crackedEMP APU COMPT LT BS 2701 WL 315 FRAME FOUND CRACK AS MARKED, CRACK LENGTH .7500. APU COMPT LT BS 2701 WL 315 FRAME REPAIRED AS PER SRM 51-40-03 FIG 1.Sep 20, 2006 · N523UP · Boeing 747283B · Fuselage Main, FrameSDR UPS06448232Skin · crackedINSPECTION TYPE:C LT BS 980 STR 38L DRAG SLICE FTG AREA FOUND 1 FASTENER HOLE CRACKED AT FUSELAGE HOLE CRACKED AT FUSELAGE APPROX 1/8". FX BS 950 - BS 990 STR 37L - 39L SKIN. REPAIRED AS PER SRM 53-30-03 FIG 60. REPEAT INSPECTION IS REQUIRED AS PER SRM 53-3Sep 19, 2006 · N523UP · Boeing 747283B · Fuselage Main, Plate/SkinSDR UPS06448226Floorbeam · corrodedINSPECTION TYPE:C, RT B/G W/W UPPER PRESSURE FLOOR PANEL ATTACH ANGLE SOME AREA FOUND CORROSION AS MARK AT STA 1403, RBL 34 TO RBL 104. CORROSION BLEND OUT 0.030" BY 1/2" BY 4" EXCEED SRM 53-10-01 FIG 1 LIMITS, RBL 34-63 AND RBL 67-104 CORROSION. REMOVED ANSep 19, 2006 · N523UP · Boeing 747283B · Fuselage Main, Floor BeamSDR UPS06448179Intercostal · crackedN/G W/W TOP PANEL INTERNAL SIDE INTERCOSTAL AT BRAKE SNUBBER FOUND CRACK AS MARK AT STA 290 RBL 21, CRACK LENGTH 1/4". N/G W/W TOP PANEL INTERNAL SIDE INTERCOSTAL REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02Sep 19, 2006 · N523UP · Boeing 747283B · Fuselage Miscellaneous StructureSDR UPS06447744Chip Detector · damagedATB - OIL QTY ON NR 2 ENGINE DROPPED TO ZERO OIL PRESSURE DECREASING SHUT DOWN NR 2 ENGINE. LANDING WT 629.0. REPLACED NR 4 BEARING MAG PLUG PER MM 72-61-00.Aug 22, 2006 · N523UP · Boeing 747200 · Turbine Engine Oil SystemSDR UPS06447496Pump · leakingNR 4 HYD SYS LOST ALL FLUID, SYS INOP. FOUND HYD LEAK FROM NR 4 EDP BODY. REPLACED NR 4 HYD PUMP PER MM 29-11-05 & REPLACED CASE DRAIN & PRESS FILTERS PER MM 29-11-00. LEAK CHECK & OPS OK. HYD PWR INSP PER MM 29-00-00 OK.Jul 31, 2006 · N523UP · Boeing 747200 · Hydraulic Pump (Electric/Engine), MainSDR UPS06447304Indicator · activatedPBE PRESS IND IS EXTENDED. INSTALLED NEW PBE.Jul 9, 2006 · N523UP · Boeing 747200 · Emergency EquipmentSDR UPS05445857Link · crackedNR 4 ENGINE REAR MOUNT THRUST LINK FWD END LUG BORE LOWER AREA WITH CRACK INDICATION ( > 126 PERCENT FSH ) WHICH EXCEED LIMIT. NR 4 ENGINE REAR MOUNT THRUST LINK REPLACED PER 747 MM 71-21-03, REF EO NR B747-7120-22596-C APPENDIX I.Dec 6, 2005 · N523UP · Boeing 747283B · Engine Mount SectionSDR UPS05445856Link · crackedNR 3 ENGINE REAR MOUNT THRUST LINK FWD END LUG BORE UPPER AREA WITH CRACK INDICATION (90 PERCENT FSH ); AND AFT END LUG BORE UPPER AND LOWER AREA WITH CRACK INDICATION 60 PERCENT FSH AND 110 PERCENT FSH RESPECTIVELY. ALL EXCEED LIMIT. NR 3 ENGINE REAR MOUNT Dec 6, 2005 · N523UP · Boeing 747283B · Engine Mount SectionSDR UPS05445855Link · crackedNR 2 ENGINE REAR MOUNT THRUST LINK AFT END LUG BORE LOWER AREA WITH CRACK INDICATION 70 PERCEMT FSH WHICH EXCEED LIMIT. NR 2 ENGINE REAR MOUNT THRUST LINK REPLACED PER 747 MM 71-21-03 REF EO NR B747-7120-22596 APPENDIX G.Dec 6, 2005 · N523UP · Boeing 747283B · Engine Mount SectionSDR UPS05445854Link · crackedNR 1 ENGINE REAR MOUNT THRUST LINK FWD END LUG BORE UPPER AND LOWER AREA WITH CRACK INDICATION 60 PERCENT FSH AND 80 PERCENT FSH RESPECTIVELY. WHICH EXCEED LIMIT. NR 1 ENGINE REAR MOUNT THRUST LINK REPLACED PER 747 MM 71-21-03 REF EO NR B747-7120-22596 APPENDec 6, 2005 · N523UP · Boeing 747283B · Engine Mount SectionSDR UPS05445406Windshield · delaminatedINSPECTION TYPE:N/A F/O R1 WINDOW HAS CHIPPING AND CRACKING IN MAIN GLASS PLIES. COMPLETED R1 REMOVAL & INSTALLED NEW R1 REF TO MM 56-11-01 UP TO STEP 6.D. FIRST TORQUE COMPLETED. ITEM STEPS 6D THRU J NEED TO BE C/W. STEPS ARE FOR INSTALLATION OF SEALANT. Sep 12, 2005 · N523UP · Boeing 747200 · Flight Compartment WindowsSDR UPS05444404Skin · chafedEXTERIOR SKIN CHAFING MARK FOUND ABOVE STR 12L BS 2230. CHAFED AREA 0.016 INCH BY 3 INCH BY 1 INCH. SKIN REPAIRED AT BS 2220 TO BS 2240 BETWEEN S11L TO S12L AREA AS PER SRM 53-30-03 FIG 17 WITH ZERO TIMING AT CRITICAL ROW FASTENER CAT B REPAIR REPEAT INSP ATApr 23, 2005 · N523UP · Boeing 747283B · Fuselage Main, Plate/SkinSDR UPS05444426Frame · crackedNR 1 PYLON AFT BULKHEAD I/B FRAME ADJ TO UPPER SPAR FTG CRACKED APPROX .1875 RUNNING I/B AND O/B, CRACK LENGTH .1875. NR 1 PYLON AFT BULKHEAD I/B FRAME REPAIRED AS PER HX RS R54-53-35295 AND UPS EA ENGINEERING FILE NR 747-54-20051.Apr 14, 2005 · N523UP · Boeing 747283B · Nacelle/Pylon, Frame/Spar/RibSDR UPS05444422Frame · crackedNR 1 PYLON AFT BULKHEAD O/B FRAME ADJ TO UPPER SPAR FITTING FOUND CRACKED RUNNING I/B TO EDGE AND RUNNING O/B .9375 INCH LONG, (CRACK LENGTH .9375 ). NR 1 PYLON AFT BULKHEAD O/B FRAME REPAIRED AS PER HX RS NR R54-53-35295 AND UPS ENGINEERING FILE NR 747-54-20Apr 14, 2005 · N523UP · Boeing 747283B · Nacelle/Pylon, Frame/Spar/RibSDR UPS05444353Fitting · crackedINSPECTION TYPE:C RIGHT BS 1480 B/H NR 16 HOLE FOUND CRACK AT OUTER CHORD SPLICE FITTING RUNNING OUTBOARD APPROX 0.030 INCH LONG (CRACK LENGTH 0.030 INCH). RIGHT BS 1480 B/H NR 16 HOLE OVERSIZED TO 0.406 INCH & CRACK FREE AS PER EO B747-5310-10732.Apr 14, 2005 · N523UP · Boeing 747200 · Fuselage Main, BulkheadSDR UPS05444352Frame · crackedINSPECTION TYPE: C, RT BS 1480 BULKHEAD NR 11 HOLE FOUND CRACK AT BULKHEAD FRAME RUNNING AFT APPROX 0.040 INCH LONG (CRACK LENGTH .0625 INCH). RIGHT BS 1480 B/H NR 11 HOLE OVERSIZED TO 0.562 INCH & CRACK FREE AS PER EO B747-5310-10732.Apr 14, 2005 · N523UP · Boeing 747200 · Fuselage Main, FrameSDR UPS05444346Skin · crackedINSPECTION TYPE:C LT BS 1480 BHD NR 11 HOLE FOUND CRACK AT FUSELAGE SKIN THROUGH THICKNESS RUNNING FWD ( CRACK LENGTH 0.325 INCH ). BS 1480 LT STR 32 TO STR 34 AREA SKIN REPAIRED AS PER SB 747-53A2390 FIG 28Apr 14, 2005 · N523UP · Boeing 747200 · Fuselage Main, Plate/SkinSDR UPS05444334Splice · crackedINSPECTION TYPE:C RH BS 1480 B/H #18 HOLE FOUND CRACK AT WEB SPLICE PLATE RUNNING UP APPROX 0.080" LONG ( CRACK LENGTH 0.080" ) NR 18 BOLT HOLE OVERSIZED TO 0.532" AT SPLICE PLATE HFEC INSP C/OUT FOUND CRACK FREE BUSHING REPAIRED AS PER EO B747-5310-10732.Apr 14, 2005 · N523UP · Boeing 747283B · Fuselage Main, BulkheadSDR UPS05444333Bulkhead · crackedINSPECTION TYPE: C, RT BS 1480 B/H NR 7 HOLE FOUND CRACK AT FX, SKIN RUNNING AFT APPROX .0625 INCH LONG, CRACK LENGTH .0625. HOLE OVERSIZED TO 0.687" AS PER EO B747-5310-10732 AND BUSHING INSTALLED.Apr 14, 2005 · N523UP · Boeing 747283B · Fuselage Main, BulkheadSDR UPS05444425Frame · crackedNR 2 PYLON AFT BULKHEAD I/B FRAME ADJACENT TO UPPER SPAR FITTING FOUND CRACKED, CRACK LENGTH .375 AND .250. NR 2 PYLON AFT BULKHEAD I/B FRAME REPAIRED AS PER HX RS R54-53-35295 AND UPS EA ENGINEERING FILE NR 747-54-20051.Apr 13, 2005 · N523UP · Boeing 747283B · Nacelle/Pylon, Frame/Spar/RibSDR UPS05444421Frame · crackedNR 2 PYLON AFT BULKHEAD O/B FRAME ADJACENT TO UPPER SPAR FITTING FOUND CRACKED, (CRACK LENGTH .25 INCH AND .9375 INCH ). NR 2 PYLON AFT BULKHEAD O/B FRAME REPAIRED AS PER HX RS NR R54-53-35295 AND UPS ENGINERING FILE NUMBER 747-54-20051.Apr 13, 2005 · N523UP · Boeing 747283B · Nacelle/Pylon, Frame/Spar/RibSDR UPS05444399Shear Tie · crackedCOCKPIT BS 360 STR 1R FRAME SHEAR TIE CRACKED, CRACK LENGTH 1/2 INCH. COCKPIT BS 360 FRAME WEB REPAIRED AT BTN STR 1R AND STR 2R AREA AS PER HX RS R53-12-35290 AND UPS EO NR B747-5310-22086-A.Apr 12, 2005 · N523UP · Boeing 747283B · Fuselage Internal Mounting StructureSDR UPS05444398Frame · crackedCOCKPIT BS 360 FRAME STR 2R WEB CRACKED, CRACK LENGTH 9/16". COCKPIT BS 360 FRAME WEB REPAIRED AT BETWEEN STR 1R AND 2R AREA AS PER HX RS R53-12-35290 AND UPS EO NR B747-5310-22086A, REFER NRC 6590 FOR WORK DETAIL.Apr 12, 2005 · N523UP · Boeing 747283B · Fuselage Main, FrameSDR UPS05444335Stringer Clip · crackedINSPECTION TYPE:C COCKPIT - BS 360 S-8L FRAME/STR TIE CLIP CRACKED. ( CRACK LENGTH 0.5" ). COCKPIT BS 360 STR -8L TIE CLIP REPLACED AS PER SRM 51-10-01 P.9.Apr 12, 2005 · N523UP · Boeing 747283B · Fuselage Main, Attach FittingsSDR UPS05444428Fitting · corrodedU/D - STA 496 RBL 70 TOILET TANK TIE DOWN FTG CORROSION FOUND. CORROSION BLEND OUT 0.020" BY 1" BY 1". TIE DOWN FTG REPLACED AS PER SRM 51-10-01 PG 9.Apr 11, 2005 · N523UP · Boeing 747283B · Fuselage Main, Attach FittingsSDR UPS05444408Frame · crackedBS 480 FRAME S10AL STR CUTOUT CRACKED. CRACK LENGTH 3/4 INCH. BS 480 STR 10AL TO STR 12L FRAME REPAIRED AS PER SRM 53-10-04 FIG 22 REFER NRC 6374 FOR WORKING DETAIL.Apr 11, 2005 · N523UP · Boeing 747283B · Fuselage Main, FrameSDR UPS05444407Frame · crackedU/DECK BS480 STR 12L STR CUTOUT CRACKED. CRACK LENGTH 3/4 INCH. U/DECK BS480 STR 10AL TO STR 12L FRAME REPAIRED AS PER SRM 53-10-04 FIG 22.Apr 11, 2005 · N523UP · Boeing 747283B · Fuselage Main, FrameSDR UPS05444406Frame · crackedSTA 440 STR 10R FRAME CRACKED. U/DECK BS440 STR 10R FRAME REPAIRED AS PER SRM 53-10-04 FIG 11.Apr 11, 2005 · N523UP · Boeing 747283B · Fuselage Main, FrameSDR UPS05444405Frame · crackedBS440 LT FRAME, JUST BELOW U/D FLOORBEAM LWR CHORD, WEB CRACKED WL290, CRACK LENGTH 3/8 INCH. BS 440 LT FRAME WEB REPLACED BETWEEN STR 13L TO 16L AS PER SRM 51-10-01 PG 9.Apr 11, 2005 · N523UP · Boeing 747283B · Fuselage Main, Frame
Back to N523UP, cancelled Jul 7, 2010