N744UP, cancelled Mar 30, 2010

Service difficulty reports · 233

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 = 'N744UP' AND deregistration_id = 'N744UP-2010-03-30'
  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 UPS08851521Slide · inoperativeCREW ENTRY DOOR WAS OPENED AFTER SECURED FOR FLIGHT BY DE-ICE; ESCAPE SLIDE WAS PULLED FROM CASE. INSTALLED SLIDE IN CASE PER MM 25-60-01-2.Jan 22, 2008 · N744UP · Doug DC871F · Escape SlideSDR UPS08851459Warning System · malfunctionedINSPECTION TYPE:N/A ATB - AFTER ROTATION, MASTER WARNING LIGHT ALONG WITH BELLY DOOR ILLUMINATED. THE TOWER WAS INFORMED, RETURN FOR LANDING. LANDED IN THE SAME PATTERN WITHOUT ANY PROBLEMS AND TAXIED TO THE RAMP. OPENED AND CLOSED FWD BELLY DOOR, PIT 32, LJan 18, 2008 · N744UP · Doug DC871F · Door Warning SystemSDR UPS07851292Battery Pack · inoperativeNO EMERGENCY LIGHTS ON PREFLIGHT CHECK, COCKPIT INSTRUMENT FLOODS AND COCKPIT DOME. REMOVED AND REPLACED EMERGENCY BATTERY PACK. OPS CHECK NORMAL. REF DC8 MM 26-00.Dec 12, 2007 · N744UP · Doug DC871F · Emergency LightingSDR UPS07849112Floorbeam · corrodedINSPECTION TYPE:C2 CORROSION ON FLOORBEAM LOWER T-CAP EXFOLIATED STA -80 RBL 54. REMOVED OUT OF LIMITS CORROSION AT STA -80 RBL 57 IAW SRM 51-2-1. FABRICATED AND INSTALLED REPAIR PARTS AT STA -80 RBL 57 IAW SRM 51-2-1 FIG 1, AND TR 51-130.Jan 22, 2007 · N744UP · Doug DC871F · Fuselage Main, Floor BeamSDR UPS07848955Frame · corrodedINSPECTION TYPE:C2 AFTER REMOVAL OF CORROSION, FOUND CORROSION OUT OF LIMITS ON FRAME AT STA 1973, LT & RT. REMOVED FRAME SPLICE AT STA 1973 FWD OF TAIL NAV LIGHT IAW SRM 51-1-21. FABRICATED, AND INSTALLED REPAIR FRAME SPLICES AT STA 1973 LT & RT IAW SRM 51-Jan 14, 2007 · N744UP · Doug DC871F · Fuselage Main, FrameSDR UPS07848998Spar Cap · crackedINSPECTION TYPE:C3 POSSIBLE CRACK AT NR 4 ALT BETWEEN LWR FRT SPAR CAP FLANGE AND STRINGER 64 JUST OUTBOARD XRS428. REMOVED, FABRICATED AND INSTALLED SPAR CAP FLANGE IAW SRM 51-1-20D & DWG 3644046.Jan 6, 2007 · N744UP · Doug DC871F · Wing SparSDR UPS07848941Support Fitting · crackedINSPECTION TYPE:C2 SUPPORT FITTING CRACKED AT STA 980 RBL 24 4 INCHES BELOW CABIN SEAT TRACK. REMOVED AND REPLACED SUPPORT FITTING IAW SRM 51-1-20D AND 51-3-0.Jan 6, 2007 · N744UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS07848840Stiffener · crackedINSPECTION TYPE:C2 RADIOGRAPHIC INSP DETECTED A CRACK ON THE LT WING AT STA XRS437.00 VERTICAL STIFFENER IN THE LEADING EDGE. REMOVED REPAIR FROM VERTICAL STIFFENER IAW SRM 51-1-21. FABRICATED AND INSTALLED REPAIR DOUBLER, AND REPAIR ANGLE AT LT WING STA XRSJan 5, 2007 · N744UP · Doug DC871F · Wing Miscellaneous StructureSDR UPS07848845Skin · crackedINSPECTION TYPE:C2 LT HORIZ STAB L/E UPPER SKIN CRACKED AT STA XFS 60. CUT OUT DAMAGED AREA ON HORIZ STAB LT L/E UPPER SKIN AT STA XFS 60 IAW SRM 55-02-01-0 FIG 4. FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER ON LT HORIZ STAB L/E UPPER SKIN STA XFS 60 Jan 4, 2007 · N744UP · Doug DC871F · Horizontal Stabilizer, Plate/SkinSDR UPS07849091Pressure Panel · corrodedINSPECTION TYPE:C2 COCKPIT SUBFLOOR HORIZ PRESS PANEL STA -80 LBL 24 HAS EXFOLIATION CORROSION. REPAIRED COCKPIT SUBFLOOR HORIZ PRESS PANEL AT STA -80 LBL 24 IAW SAA EA 008-5330-01-A0608, UPS EO DC8-5330-26007-A, BAC SERVICE MSG 1-275991347, AND FAA FORM 8100Jan 3, 2007 · N744UP · Doug DC871F · Fuselage Floor PanelSDR UPS07849075Window Frame · corrodedINSPECTION TYPE:C2 RIGHT & LEFT WINDOW FRAME Z-ANGLES (CENTER WINDSHIELD) ARE CORRODED AND PITTED. REPAIRED CENTER WINDSHIELD Z-ANGLE IAW SAA EA 008-5310-01-A0570 UPS EO DC8-5310-25945-A, BAC MSG 1-269510850, AND FAA FORM 8100-9.Jan 3, 2007 · N744UP · Doug DC871F · Fuselage Main, StructureSDR UPS07848976Longeron · corrodedINSPECTION TYPE:C2 CORROSION OUT OF LIMITS ON LONGERON L35R STA 50-70. REMOVED LONGERON L35R AT STA 50-70 IAW SRM 51-1-21. FABRICATED AND INSTALLED LONGERON L35R AT STA 50-70 IAW DWG 3702969, AND SRM 51-1-21, AND 51-1-20D.Jan 3, 2007 · N744UP · Doug DC871F · Fuselage Main, Longeron/StringerSDR UPS07848975Fitting · corrodedINSPECTION TYPE:C2 CORROSION OUT OF LIMITS ON END FITTING AT STA 70 L35R. REMOVED AND REPLACED LONGERON END FITTING AT STA 70 L35R IAW SRM 51-1-21, AND SRM 51-1-20D.Jan 3, 2007 · N744UP · Doug DC871F · Fuselage Main, Longeron/StringerSDR UPS07848926Angle · crackedINSPECTION TYPE:C2 LEFT HORIZ STAB LEADING EDGE VERY INBOARD UPPER T-ANGLE CRACKED. CUT OUT DAMAGED AREA ON INBOARD UPPER T-ANGLE ON LT HORIZ STAB LEADING EDGE IAW SRM 51-1-21, RECEIVED, LOCATED, DRILLED UP AND INSTALLED T-ANGLE FITTING ON THE LEFT HORIZ STABJan 3, 2007 · N744UP · Doug DC871F · Horizontal Stabilizer Miscellaneous StructureSDR UPS07848838Longeron Splice · crackedINSPECTION TYPE:C2 C-PIT STA 1040 L31L, LONGERON SPLICE FITTING CRACKED. REMOVED AND REPLACED LONGERON SPLICE FITTING AT STA 1040 L31L IAW SRM 51-01-20D, 51-03-02.Jan 3, 2007 · N744UP · Doug DC871F · Fuselage Main, Longeron/StringerSDR UPS07849074Floorbeam · crackedINSPECTION TYPE:C2 FLOORBEAM VIEWED FROM A-PIT STA 240 LBL 36 HAS A 9 INCH CRACK. REPAIRED FLOORBEAM AT STA 240 LBL 36 IAW SAA EA008-5310-01-A00586 UPS RAA DC8-53-20605-A, BAC MSG 1-271080190, AND FAA FORM 8100-9.Jan 2, 2007 · N744UP · Doug DC871F · Fuselage Main, Floor BeamSDR UPS07849071Spar · crackedINSPECTION TYPE:C2 FOUND CRACK ON LOWER CENTER SPAR CHORD AND WEB JUST I/B OF XRS 255 NR 1 MAIN TANK. REPAIRED CRACKED SPAR CHORD AND WEB AT NR 1 MAIN TANK JUST I/B OF XRS 255 IAW SAA EA# 008-5710-01-A0595, UPS EO DC8-5710-25944-A, BAC SERV MSG NR 1-270145772Jan 2, 2007 · N744UP · Doug DC871F · Wing SparSDR UPS07848999Support · crackedINSPECTION TYPE:C3 A-PIT FWD BULKHEAD STA 70 RBL 24 SUPPORT FRAME CRACKED. REMOVED, FABRICATED AND INSTALLED REPLACEMENT FRAME SUPPORT IAW SRM 51-1-21, 51-1-20D AND DWG 5613064.Jan 2, 2007 · N744UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS07848977Boss · corrodedINSPECTION TYPE:C2 RIGHT MAIN LANDING GEAR RETRACT PIN BOSS ID CORRODED. RIGHT MLG RETRACT PIN BORE BOSS CORROSION IS OUT OF LIMITS IAW EO DC8-3230-0450-O. RIGHT MLG TO BE REMOVED AND REPLACED ON NRC 949517 AND TC 9132-3.Jan 2, 2007 · N744UP · Doug DC871F · Landing Gear Retraction/Extension SystemSDR UPS07848865Door Frame · crackedINSPECTION TYPE:C2 HFEC INSP DETECTED A .156" CRACK ON THE UPPER FWD CORNER OF THE B-PIT DOOR JAMB. CUT OUT DAMGED AREA AT THE UPPER FWD B-PIT DOOR JAMB IAW SRM 53-2-0 FIG 20. FABRICATED AND INSTALLED FILLERS, DOUBLER AND TRIPLER AT THE UPPER FWD B-PIT DOOR Dec 30, 2006 · N744UP · Doug DC871F · Fuselage Main, StructureSDR UPS07848827Intercostal · crackedINSPECTION TYPE:C2 L1 DOOR INTERCOSTAL CRACKED .625 INCH UPPER FWD CORNER OF DOOR. FABRICATED AND INSTALLED REPAIR ANGLE DOUBLER AT L1 DOOR UPPER FWD CORNER STA 25 L11L IAW SRM 52-02-00-0 FIG 002 AND SRM 51-01-21D.Dec 30, 2006 · N744UP · Doug DC871F · Passenger/Crew DoorsSDR UPS07848826Intercostal · crackedINSPECTION TYPE:C2 L1 DOOR INTERCOSTAL CRACKED 1.75 INCH, UPPER AFT CORNER OF DOOR. FABRICATED AND INSTALLED REPAIR ANGLE DOUBLER AT STA 70 LBL 60 L1 DOOR AFT CORNER INTERCOSTAL IAW SRM 52-02-00-0, AND SRM 51-01-08.Dec 30, 2006 · N744UP · Doug DC871F · Passenger/Crew DoorsSDR UPS07848846Shear Tie · crackedINSPECTION TYPE:C2 60 COMPT CEILING SHEARTIE BROKEN AT EOP RT SIDE STA 1795 L3R. REMOVED CRACKED SHEARTIE AT STA 1795 L3R IAW SRM 51-1-21. FABRICATED AND INSTALLED REPLACEMENT SHEARTIE AT STA 1795 L3R IAW DWG 5612148, AND SRM'S 51-03-02-0 FIG 55, AND 51-1-20Dec 29, 2006 · N744UP · Doug DC871F · Fuselage Internal Mounting StructureSDR UPS07848839Fitting · brokenINSPECTION TYPE:C2 END FITTING BROKEN AT STA 1770, L10L. REMOVED AND REPLACED END FITTING AT STA 1770, L10L IAW SRM 51-1-20D AND SRM 51-3-0.Dec 29, 2006 · N744UP · Doug DC871F · Fuselage Main, Longeron/StringerSDR UPS07848832Fitting · corrodedINSPECTION TYPE:C2 HEAVY CORROSION ON FITTING AT BASE OF APB CENTERLINE BEAM, LT SIDE L36 STA 1755-1766. REMOVED FABRICATED AND REPLACED FITTING AT L36 STA 1755-1766 IAW SRM 51-1-20D AND DWG 5753522.Dec 29, 2006 · N744UP · Doug DC871F · Fuselage Main, Attach FittingsSDR UPS07848819Seat Track · gougedINSPECTION TYPE:C2 SEAT TRACK SCALLOPS GOUGED AT STA 958 LBL 24 IN MAIN CABIN. CUT OUT DAMAGED AREA OF SEAT TRACK AT STA 958 LBL 24 IAW SRM 53-02-03 FIG 6D. INSTALLED SEAT TRACK PLUG REPAIR AT STA 958 LBL 24 IAW SRM 51-3-0.Dec 28, 2006 · N744UP · Doug DC871F · Fuselage, Seat/Cargo Attach FittingsSDR UPS07848820Rib · crackedINSPECTION TYPE:C2 LEFT WING UPPER LEADING EDGE RIB CRACKED AT XFS 659. STOP DRILLED CRACKED RIB AT WING STA XFS 659 IAW SRM 51-1-21, AND SRM 57-02-00. FABRICATED AND INSTALLED REPAIR DOUBLER AT WING STA XFS 659 IAW SRM 57-02-00, AND SRM 51-1-20D.Dec 27, 2006 · N744UP · Doug DC871F · Wing, Rib/BulkheadSDR UPS06848762Slide · brokenEMERGENCY ESCAPE SLIDE FELL OUT OF CONTAINER. SLIDE LANYARD TANG BROKEN. REMOVED AND REPLACED EVAC SLIDE CONTAINER IAW 25-60-01.Dec 12, 2006 · N744UP · Doug DC871F · Escape SlideSDR UPS06847672Lamp · inoperativeEMERGENCY EXIT LIGHT, DISARM CHECK LIGHT INTERMITTENT INOP. RELAMPED EMERGENCY EXIT LIGHT PER M/M 33-10-00. OPS CHECK GOOD.Aug 11, 2006 · N744UP · Doug DC871 · Emergency LightingSDR UPS06847343Hose · defectiveON CLIMBOUT HYDRAULIC QUANTITY DECREASED. AOM PROCEDURE WAS COMPLIED WITH AND RESERVOIR WAS NOT EMPTY. FOUND LT MAIN GEAR DOWNLOCK BUNGEE CYLINDER PRESSURE HOSE BROKEN. REPLACED WITH TEMPORARY HOSE REFERENCE GMM 3-24-1- D329494 ASSIGNED. R&R PRESS LINE WITHJul 18, 2006 · N744UP · Doug DC871F · Hydraulic System, MainSDR UPS06847338Wheel · corrodedCORROSION ON NR 5 MAIN LANDING GEAR AXLE - INNER WHEEL BEARING. CHROME W/SOME PITTING. R/R NR 5 MLG WHEEL & TIRE ASSY. IAW MM REF 32-40-01-2. BLENDED AREA APPLIED FR PRIMER TO BLENDED AREA; REINSPECT EVERY 70 DAYS PERM. REPAIR AT OR BEFORE C CK.Jul 16, 2006 · N744UP · Doug DC871F · Wheel/Ski/FloatSDR UPS06847256Gauge · unserviceableINSPECTION TYPE:N/A MAIN ENTRY DOOR EMERGENCY ESCAPE SLIDE PRESSURE GAUGE IS UNREADABLE. VERIFY IF SLIDE PRESSURE IS SERVICEABLE PER TC 0231, STEP 1D SLIDE PRESSURE IS SERVICEABLE PER TC 231, 1D.Jun 24, 2006 · N744UP · Doug DC871F · Escape SlideSDR UPS06847047Structure · puncturedINSPECTION TYPE:N/A PINHOLE PUNCTURE PIT 33 STA 1240 LEFT SIDE. PERFORMED INTERIM REPAIR PER EO DC8-5320-8724 APPENDIX A.Jun 1, 2006 · N744UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS05845624Skin · crackedNR 4 PYLON O/B SKIN CRACKED APPROX 1 INCH LONG OB SIDE APPROX 6 INCHES AFT OF FWD BOX BULKHEAD. ACCOMPLISHED INTERIM REPAIR PER EO DC8-5430-23086A. PERMANENT REPAIR WITHIN 10 FLT CYCLIES, D312151 ASSIGNED. ACCOMPLISHED PERMANENT REPAIR PER EO DC8-5430-23086Oct 17, 2005 · N744UP · Doug DC871F · Nacelle/Pylon, Plate/SkinSDR UPS04843586Fitting · crackedBATHTUB FITTING CRACKED AT STA 1200 L34R-L35R. FITTING HAD BEEN PREVIOUSLY REPLACED. REMOVED AND RETAINED SPLICE PLATES FROM CRACKED FITTINGS REF SRM 51-1-20D. CUT REPLACEMENT FITTING, DRILLED, TREATED, AND PRIMED PER SRM 53-2-0 FIG2D. REMOVED AND REPLACEDNov 29, 2004 · N744UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS04843574Web · corrodedTORQUE BOX WEB CORRODED BEYOND LIMITS AT STA 1200, LONG 36. REMOVED FASTENERS TO FOM REF SRM51-1-20D. REMOVED CORROSION REF SRM 53-2-0 FIG 1F. NDT VERIFIED MATERIAL RANGE 0.125" - 0.088" REF NDT SPM 04-00-06. FABRICATED REPAIR DOUBLER FROM SHT7075T6-.160" Nov 26, 2004 · N744UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS04843570Doubler · crackedRT WING L/E INTERNAL DOUBLER (AUX TANK) CRACKED AT STA.182.502. FABRICATED REPAIR DOUBLER FROM SHT7075T6/0.125 AND INSTALLED SAME PER SAA SK744-520, SRM 51-1-8, 51-1-26, 51-1-20D.Nov 24, 2004 · N744UP · Doug DC871F · Wing, Plate/SkinSDR UPS04843576Gusset · crackedGUSSET CRACKED AT STA 460 ABOVE LONG 31 R. REMOVED CRACKED GUSSET REF SRM 51-1-21. FABRICATED REPLACEMENT GUSSET FROM SHT7075T6/.080 REF DWG 9758907. INSTALLED SAME REF SRM 51-1-8, AND 51-1-20DNov 22, 2004 · N744UP · Doug DC871F · Fuselage Main, StructureSDR UPS04843571Skin · crackedEXTERNAL FUSELAGE SKIN CRACKED AT RT AFT HEAT EXCHANGER CUT OUT LOWER AFT CORNER. REPAIRED PER EO DC8-5330-4732-D.Nov 22, 2004 · N744UP · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS04843582Frame · corrodedSTA 70 FRAME CORRODED BEYOND LIMITS ABOVE LONG 21R. REMOVED CORROSION, TREATED AND PRIMED SITE PER SRM51-1-8. FABRICATED REPAIR DOUBLER FROM SHT7075O-.080 PER EO DC8- 5310-11728/DWGDC8-53A-011. HEAT TREAT TO T6 PER DPS7.00 INSTALLED REF SRM 51-1-20D, 51-1-8Nov 21, 2004 · N744UP · Doug DC871F · Fuselage Main, FrameSDR UPS04843566Shear Tie · crackedCRACKED SHEAR TIE AT LONG 21L STA 460. REMOVED, FABRICATED AND INSTALLED REPLACEMENT SHEAR TIE REF SRM 51-1-21, 51-1-8, 51-1-20D, 51-9-0 FIG 68A, DWG3750891, AND DPS7.00-1.Nov 20, 2004 · N744UP · Doug DC871F · Fuselage Main, StructureSDR UPS04843565Shear Tie · crackedSHEAR TIE CRACKED AT STA 440 LONG 21L. REMOVED, FABRICATED, AND INSTALLED. REPLACEMENT SHEAR TIE REF SRM 51-1-21, 51-1-8, 51-9-0 FIG 88A, 51-1-20D DWG3750891, AND DPS7.00-1.Nov 20, 2004 · N744UP · Doug DC871F · Fuselage Main, StructureSDR UPS04843598Attach Fitting · crackedINSPECTION TYPE: C3, INTERCOSTAL FRAME ATTACH FITTING CRACKED AT STA 1140 LONG 35L. REMOVED AND REPLACED FITTING REF SRM 51-1-21, 51-1-20D, 51-1-8 NDT-SPM06-10-01.001.Nov 19, 2004 · N744UP · Doug DC871F · Fuselage Main, Attach FittingsSDR UPS04843581Splice · crackedLONG 31R SPLICE FITTING CRACKED AT STA 1050. REMOVED AND REPLACED SPLICE FITTING REF SRM 51-1-20D, 51-1-8, 51-1-22, 51-3-2.Nov 19, 2004 · N744UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS04843579Rib · crackedLT WING CENTER L/E RIB CRACKED AT XW429 UPPER RIB. STOP DRILLED CRACK, NDT VERIFIED TERMINATION PER SPM 06-10-01.001. FABRICATED STACKED ANGLE REPAIR DOUBLERS FROM SHT7075T6/.040 AND .050 THICK REF SRM 57-3-1 FIG 4 ITEM C, 57-2-0 FIG2. INSTALLED PARTS REF SNov 19, 2004 · N744UP · Doug DC871F · Wing, Rib/BulkheadSDR UPS04843578Doubler · crackedRT WING L/E INTERNAL DOUBLER CRACKED AT DRAN HOLE, STA XFS329. FABRICATED REPLACEMENT DOUBLER FROM SHT7075T6/.090 PER SRM 57-3-0 FIG 12. TREATED AND PRIMED REF SRM 51-1-8. REMOVED AND REPLACED PART PER SRM 51-1-20D, 51-1-21.Nov 19, 2004 · N744UP · Doug DC871F · Leading Edge DevicesSDR UPS04843573Fitting · crackedSPLICE FITTING CRACKED AT STA 1270, LONG 34L. REMOVED AND REPLACED SPLICE FITTING REF SRM 51-1-8, 51-3-2, 51-1-20D.Nov 19, 2004 · N744UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS04843548Rib · crackedLEFT WING CENTER L/E RIB CRACKED AT XW408. STOP DRILLED CRACK, NDT VERIFIED REF SPM06-10-01.001. FABRICATE STACKED REPAIR ANGLES FROM SHT7075T6-.040 AND INSTALLED SAME REF SRM 57-2-0 FIG 1, 57-3-1 FIG 4, 51-1-8, 51-1-20D, 51-1-21.Nov 19, 2004 · N744UP · Doug DC871F · Wing, Rib/BulkheadSDR UPS04843547Rib · crackedC3 LT WING CENTER L/E RIB CRACKED AT UPPER AFT END STA XW398. STOP DRILLED CRACK NDT VERIFIED REF SPM06-10-01.001. FABRICATE STACKED REPAIR ANGLES FROM SHT7075T6-.040 AND INSTALLED SAME REF SRM 57-2-0 FIG2, 57-3-1, FIG4, 57-3-1 FIG2, 51-1-8.Nov 19, 2004 · N744UP · Doug DC871F · Wing, Rib/BulkheadSDR UPS04843544Rib · crackedRT WING O/B L/E RIB CRACKED NEAR XFS722.50. STOP DRILLED CRACK. NDT VERIFIED REF SPM06-10-01.001. FABRICATE REPAIR ANGLE FROM SHT7075T6-.063 AND INSTALLED SAME REF SRM 57-3-3, 57-2-0 FIG2, 51-1-8, 51-1-21.Nov 19, 2004 · N744UP · Doug DC871F · Wing, Rib/Bulkhead
Back to N744UP, cancelled Mar 30, 2010