N919UP, cancelled Dec 4, 2007

Service difficulty reports · 92

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 = 'N919UP' AND deregistration_id = 'N919UP-2007-12-04'
  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 UPS07248886Slide · dislodgedFWD ENTRY ESCAPE SLIDE IS OUT OF CONTAINER. INSTALLED FORWARD ENTRY DOOR EVACUATION SLIDE IAW 25-60-14-2. OPS CHECK GOOD.Jan 19, 2007 · N919UP · Boeing 72730C · Escape SlideSDR UPS06248684Skin · cracked3 INCH CRACK ON FUSELAGE SKIN AT 10 O'CLOCK POSITION RUNNING FWD AND AFT AT STA 348.2, BETWEEN STRINGERS 5L & 6L. ADDITIONAL DISBONDING APPROXIMATELY 4 X 4 INCHES. C/W EO B727-5330-25585A TO FERRY A/C TO BFM 9014 D337794 ISSUED.Nov 14, 2006 · N919UP · Boeing 72730C · Fuselage Main, Plate/SkinSDR UPS06248513Slide · dislodgedFOUND DOOR SLIDE ON FLOOR. RE-INSTALLED ESCAPE SLIDE PER 25-60-14-2.Nov 7, 2006 · N919UP · Boeing 72730C · Escape SlideSDR UPS06248330Battery · inoperativeEMERGENCY EXIT LIGHTS ABOVE THE MAIN ENTRY DOOR AND ABOVE THE COCKPIT ENTRY DOOR ARE INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSY ON MAIN ENTRY DOOR PER MM 33-50-90-2. REMOVED AND REPLACED BATTERIES ON COCKPIT ENTRY DOOR. OPS CHECK GOOD.Oct 26, 2006 · N919UP · Boeing 72730C · Emergency LightingSDR UPS06247827Slide · dislodgedINSPECTION TYPE: NA ESCAPE SLIDE FELL OUT OF CASE ON MAIN ENTRY DOOR REPLACED ENTRY DOOR EVACUATION SLIDE IAW MM 25-60-14-2.Aug 28, 2006 · N919UP · Boeing 72730C · Escape SlideSDR UPS06247717Battery · inoperativeINSPECTION TYPE: N/A EMERGENCY EXIT LIGHTS DO NOT ILLUMINATE WITH SWITCH ON. REMOVED AND REPLACED EMERGENCY LIGHT BATTERIES. OPS CK NORMAL.Aug 17, 2006 · N919UP · Boeing 72730C · Emergency LightingSDR UPS06247529Battery · dischargedFOUND COCKPIT DOOR EMERGENCY EXIT LIGHT INOP. REPLACED BATTERIES AS REQUIRED.Jul 31, 2006 · N919UP · Boeing 72730C · Emergency LightingSDR UPS06246808Fairing · delaminatedDELAM ON L/AFT WING TO BODY FAIRING PANEL NR 3510 JUST AFT OF HYD SYS BAY REF EO B727-5350-24306. PERFORMED INTERIM REPAIR PER EO B727-5350-24306 STEP 6. DEFERRED FOR REPEAT INSPECTION EVERY 30 DAYS AND PERM BY C-CK. NR D 325051 ASSIGNED INSTALLATION OF PANMay 8, 2006 · N919UP · Boeing 72730C · Aerodynamic FairingsSDR UPS05245266Skin · corrodedINSPECTION TYPE: C, NR 2 ENG UPPER HORIZ FIREWALL SURFACE TO VERT FIN, LT, ANGLE HAS EVIDENCE OF CORROSION ON INNER SURFACE OF VERT FIN SKIN BETWEEN STA 1385 AND 1425 APPROX. SKIN REMOVED AND FOUND CORRODED O/S LIMITS, CHORD BETWEEN BS 1384 AND 1484 FOUND CORAug 6, 2005 · N919UP · Boeing 72730C · Vertical Stabilizer, Plate/SkinSDR UPS05245265Stiffener · corrodedLT MLG W/W, EVIDENCE OF CORROSION ON BS 870 VERTICAL STIFFENER AND ATTACH CLIP AT LB 145. CEILING AREA. REPAIR CARRIED OUT IAW SRM 51-30-2 & 51-10-2, 51-10-1.Aug 5, 2005 · N919UP · Boeing 72730C · Fuselage Miscellaneous StructureSDR UPS05245262Stiffener · corrodedRT MLG W/W, EVIDENCE OF CORROSION ON VERTICAL STIFFENER CEILING AREA BS 870 RBL 45. REPAIR CARRIED OUT IAW SRM 51-40-4.Aug 4, 2005 · N919UP · Boeing 72730C · Fuselage Miscellaneous StructureSDR UPS05245263Floorbeam · corrodedFLOORBEAM TOP CHORD CORROSION OUTSIDE LIMITS BS 328 RBL 12. REPAIR CARRIED OUT IAW SRM 53-10-8 & 51-10-2.Aug 3, 2005 · N919UP · Boeing 72730C · Fuselage Main, Floor BeamSDR UPS05245207Intercostal · corrodedINSPECTION TYPE:C, CORROSION ON INTERCOSTAL BS 294.5 - BS 312 LBL 33. INTERCOSTAL REPLACED IAW BOEING DWG 65-17593 AND SRM 51-30-02.Aug 3, 2005 · N919UP · Boeing 72730C · Fuselage Miscellaneous StructureSDR UPS05245205Support · corrodedINSPECTION TYPE:C FWD LAV PARTITION SUPPORT STRUCTURAL EXTRUSION CORRODED BS 302 - 344 DOOR THRESHOLD AREA. PARTITION SUPPORT STRUCTURE EXTRUSION REPLACED IAW SRM 51-10-2, 51-20- 2 & 51-30-2.Aug 2, 2005 · N919UP · Boeing 72730C · Fuselage Miscellaneous StructureSDR UPS05245261Skin · corrodedAREA OF CORROSION ON SKIN BS 355, BETWEEN STR 8 AND 10 LT. PAINT STRIP AREA IF REQUIRED, REMOVE CORROSION AND RECTIFY. REPAIR CARRIED OUT IAW SRM 51-10-1, 53-30-1 MM 25-21-2 AND AAAE EO 200 5-077-001 UPS ENGINEERING FILE NO. B727-5330-22744-A.Aug 1, 2005 · N919UP · Boeing 72730C · Fuselage Main, Plate/SkinSDR UPS05245264Attach Angle · corrodedRT SIDE AFT OF BS 294.5 FWD ATTACHMENT ANGLE OF NWW BOX HAS EVIDENCE OF CORROSION. WEB REPAIRED IAW SRM 51-40-2.Jul 31, 2005 · N919UP · Boeing 72730C · Fuselage Main, Attach FittingsSDR UPS05245206Web · corrodedINSPECTION TYPE:C RT SIDE AFT OF RT 294.5 FWD ATTACHMENT ANGLE OF NWW BOX AND RT HAS EVIDENCE OF CORROSION. REPAIR CARRIED OUT IAW SRM 51-10-6, 53-10-1 & 51-40-2.Jul 31, 2005 · N919UP · Boeing 72730C · Fuselage Miscellaneous StructureSDR UPS05243629Light · inoperativeL1 DOOR EMERGENCY LIGHT INOP. RESEATED BULB, OPS CHECK GOOD.Jan 6, 2005 · N919UP · Boeing 72730C · Emergency LightingSDR UPS04242069Fitting · crackedINSPECTION TYPE:C ON REMOVAL OF STR END FITTING AT BS 360 S17L FOUND STR END FITTING CRACKED & CORRODED. REPLACED STR END FITTING IAW SRM 51-30-02 & DRAWING 65-18420.Mar 17, 2004 · N919UP · Boeing 72730C · Fuselage Miscellaneous StructureSDR UPS04242070Fitting · crackedINSPECTION TYPE:C ON REMOVAL OF LOWER SKIN BETWEEN BS 259.5 - BS 360 S22 24L STRINGER END FITTING FOUND CRACKED AT BS 360 S22L. REPLACED STRINGER END FITTING IAW SRM 51-30-02 & DRAWING 65-18420.Mar 12, 2004 · N919UP · Boeing 72730C · Fuselage Miscellaneous StructureSDR UPS04242058Stringer · corrodedINSPECTION TYPE: C, ON REMOVAL OF FASTENER AT BS 340 APPROX S25R STRINGER FOUND TO BE CORRODED. REPAIR CARRIED OUT IAW SRM 53-10-3.Mar 11, 2004 · N919UP · Boeing 72730C · Fuselage Main, Longeron/StringerSDR UPS04242073Skin · corrodedINSPECTION TYPE:C ON REMOVAL OF SKIN PANEL AT BS 295.5 & BS 360 S19L - 24L UPPER SKIN UNDER FWD ENTRY DOOR FOUND TO BE EXCESSIVELY CORRODED. REPAIR CARRIED OUT IAW SRMO EO 2004-024-002 UPS ENG.Mar 10, 2004 · N919UP · Boeing 72730C · Fuselage Main, Plate/SkinSDR UPS04242072Door Frame · corrodedINSPECTION TYPE:C TAIL SKID DOOR RIGHT LWR FRAME IS CORRODED ON INNER SURFACE. REPLACED TAIL SKID DOOR IAW MM 32-71-61.Mar 9, 2004 · N919UP · Boeing 72730C · Landing Gear DoorsSDR UPS04242060Cargo Track · crackedINSPECTION TYPE: C, LEFT CARGO TRACK RAIL IN AFT CARGO BAY, VERY FWD SECTION TO BS 950 IS CRACKED. REF CPT 2643 FOR FABRICATION OF CARGO TRACK. REPAIRED CARGO TRACK IAW SRM 53-10-5 FIG 8.Mar 9, 2004 · N919UP · Boeing 72730C · Fuselage, Seat/Cargo Attach FittingsSDR UPS04242075Support · corrodedINSPECTION TYPE:C NR 12 SPOILER ACTUATOR SUPPORT CASTING HAS PITTING AND CORROSION UNDERNEATH THE BOLT HEADS. NR 12 SPOILER ACTUATOR SUPPORT CASTING REPLACED IAW MM 27-61-81, 27-61-01.Mar 8, 2004 · N919UP · Boeing 72730C · Drag Control ActuatorSDR UPS04242059Mount · corrodedINSPECTION TYPE: C, ENGINE NR 1 PYLON FWD MOUNT FITTING, BOTH FWD AFT LARGE AND AFT SMALL HOLES HAVE PITTING CORROSION. REPAIR CARRIED OUT IAW EO B727-5440-11592-A APPENDIX A.Mar 5, 2004 · N919UP · Boeing 72730C · Engine Mount SectionSDR UPS04242057Mount · corrodedINSPECTION TYPE: C, ENGINE NR 3 PYLON FWD MOUNT FITTING, BOTH FWD AND AFT LARGE AND FWD SMALL HOLES HAVE PITTING CORROSION. REPAIR CARRIED OUT IAW EO B727-5440-11592-A APPENDIX B.Mar 5, 2004 · N919UP · Boeing 72730C · Engine Mount SectionSDR UPS04242056Skin · bulgedINSPECTION TYPE:C SUSPECT CORROSION (SKIN BULGING) BETWEEN SKIN & FRAME AT BS 260 FROM STR 18L - S19L. REF N/R 740347, LOW FREQ EDDY CURRENT INSP CARRIED OUT AT BS 260 FR STR 18L TO 19L IN ACCORDANCE W/B727 NDT MAN 51-00-00 PART 6 FIG 5. SUSPECT MATERIAL LOSMar 4, 2004 · N919UP · Boeing 72730C · Fuselage Main, Plate/SkinSDR UPS03240251Torque Tube · looseINSPECTION TYPE:N/A ATB-AFTER T/O, LG RAISED AND RIGHT MAIN GEAR STAYED DOWN. RED GEAR LIGHT AND DOORS LIGHT REMAINED ON. GEAR CAME DOWN NORMALLY. REPLACED 6 EA SHEARED RIVETS ON UPLOCK TORQUE TUBE, OPS CHECKS GOOD PER MM 32-30-00.Mar 4, 2003 · N919UP · Boeing 72730C · Landing Gear Retraction/Extension SystemSDR UPS02239549Battery · dischargedCOCKPIT EMERGENCY EXIT LIGHT WILL NOT TEST. REPLACED BATTERIES, OPS CHECKS GOOD, BATTERIES IAW MM 33-50-01.Sep 30, 2002 · N919UP · Boeing 72730C · Emergency LightingSDR UPS02239530Contactor · dirtyEMERGENCY EXIT LIGHTS INOP. REMOVED LIGHT ASSY OVER CREW CABIN DOOR, CLEANED CONTACTS, OPS CK OK IAW MM 33-50-01.Sep 20, 2002 · N919UP · Boeing 72730C · Emergency LightingSDR UPS02238920Battery · dischargedINSPECTION TYPE:N/A, EMERGENCY LIGHT WEAK AT L1 DOOR. REPLACED BATTERIES, OPS CHECK GOOD.Jul 29, 2002 · N919UP · Boeing 72730C · Emergency LightingSDR UPS02238919Battery · dischargedINSPECTION TYPE:N/A, EMERGENCY LIGHT WEAK AT COCKPIT. REPLACED BATTERIES, OPS CHECK GOOD.Jul 29, 2002 · N919UP · Boeing 72730C · Emergency LightingSDR UPS02238737Light · not seatedINSPECTION TYPE:N/A EMERGENCY EXIT LIGHT ABOVE CABIN DOOR INOP. SEATED EXIT LIGHT ASSY OPS CHECKS GOODJul 2, 2002 · N919UP · Boeing 72730C · Emergency LightingSDR UPS02238641Battery · dischargedINSPECTION TYPE:PFLT FORWARD ENTRY DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM 33-50-01.Jun 17, 2002 · N919UP · Boeing 72730C · Emergency LightingSDR UPS02237755Light · inoperativeINSPECTION TYPE:IN FWD EXIT DOOR EMERGENCY LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY. OP CHECK GOOD IAW MM 33-50-01.Mar 3, 2002 · N919UP · Boeing 72730C · Emergency LightingSDR UPS02237516Cover · looseINSPECTION TYPE:PFLT CABIN EXIT LIGHT COVER OVER CABIN DOOR IS LOOSE. CHECK SECURITY OF EXIT LIGHT ASSY PER MAINT PRACTICES MM 33-50-01 AND INSTALLED LIGHT COVER, NO DEFECTS NOTED.Jan 24, 2002 · N919UP · Boeing 72730C · Emergency LightingSDR UPS02237439Light · not seatedINSPECTION TYPE:N/A EMERGENCY EXIT LIGHT ABOVE COCKPIT DOOR IS DIM, RESEATED LIGHT ASSY. OPS CHECKS GOOD PER MM 33-50-101.Jan 20, 2002 · N919UP · Boeing 72730C · Emergency LightingSDR UPS01236604Fairing · crackedINSPECTION TYPE:PFLT LT INBD FLAP LT OUTBD CANOE FIXED FAIRING HAS A CRACK ON AFT UPPER CORNER OF PREVIOUS REPAIR. DEFFERRED PER MMOCAug 5, 2001 · N919UP · Boeing 72730C · Trailing Edge FlapsSDR UPS01236163Actuator · leakingINSPECTION TYPE:N/A RIGHT MAIN GEAR DOOR OPENED ENROUTE GEAR HANDLE PLACED TO "UP" POSIT ION DOOR CLOSED GEAR HANDLE RETURNED TO "OFF" POSITION OPS NORMAL ****SUPPLEMENTAL MRR*** REMOVED AND REPLACED GEAR DOOR ACTUATOR R/H PER MM 32-32-81 ADJ TEST GROUND DJun 22, 2001 · N919UP · Boeing 72730C · Landing Gear Retraction/Extension SystemSDR UPS01235279Frame · crackedINSPECTION TYPE:C-CK, CRACK AT FUSELAGE FRAME BS 930 ABOVE STR 13L. CUT OUT DAMAGE SECTION OF FRAME BETWEEN STR 12L & 13L. INSTALLED FORMED ANGLE REPAIR, HEAT TREATED.Mar 5, 2001 · N919UP · Boeing 72730C · Fuselage Main, FrameSDR UPS01235278Stringer · corrodedINSPECTION TYPE:C-CK, STRINGER 18 LEFT CORRODED BETWEEN BS 440 TO BS 460. REMOVED CORROSION ON STRINGER FLANGE. FOUND OUT OF UNIT. INSTALLED STRINGER REPAIR.Feb 28, 2001 · N919UP · Boeing 72730C · Fuselage Main, Longeron/StringerSDR UPS01235402Fitting · crackedINSPECTION TYPE:C CHECK LT WING FRONT SPAR INTERIOR & LBBL 70.5 TERMINAL FITTING ATTACH V SHAPE FITTING TO UPPER SHOW CRACK MIGRATING FROM OB BOLT. REMOVED FITTING LT WING FRONT SPAR INTERIOR LBL 70.5 V SHAPE. INSTALLED LT WING UPPER FRONT SPAR CONER NEW FITFeb 26, 2001 · N919UP · Boeing 72730C · Wing, Attach FittingsSDR UPS01235399Duct · crackedINSPECTION TYPE:C CHECK NR 2 ENGINE INLET S DUCT INNER SKIN HAS CIRCUMFERENTIAL CRACKS. 1 EA 4 INCH CRACK 93 INCHES FROM AFT EDGE 4 OCLOCK. CUT OUT DAMAGED AREA. INSTALLED REPAIR.Feb 19, 2001 · N919UP · Boeing 72730C · Engine Air Intake SystemSDR UPS01235398Duct · crackedINSPECTION TYPE:C CHECK NR 2 ENGINE INLET S DUCT INNER SKIN HAS CIRCUMFERENTIAL CRACKS 2 EA APPX 100-104 INCH FROM AFT EDGE. 1 EA 7 INCH Y SHAPED CRACK & 1 EA 1.5 INCH CRACK APPX 4 OCLOCK. CUT OUT DAMAGED AREA. INSTALLED REPAIR. HEAT TREATED.Feb 19, 2001 · N919UP · Boeing 72730C · Engine Air Intake SystemSDR UPS01235284Intake Duct · crackedINSPECTION TYPE:C-CK, NR 2 ENG INLET S-DUCT INNER SKIN HAS APPROX 6 INCH CIRCUMFERENTIAL CRACK AT 4 O''CLK APPROX 30 INCHES AFT OF WHERE S-DUCT ATTACHES TO INLET. CUT OUT DAMAGED AREA APPROX 7 X 1 INCHES. PERFORMED NDT AND NO CRACK INDICATIONS. INSTALLED SKFeb 19, 2001 · N919UP · Boeing 72730C · Engine Air Intake SystemSDR UPS01235283Skin · crackedINSPECTION TYPE:C-CK, FUSELAGE SKIN HAS CORROSION BULGE AND APPROX 3 INCH LATERAL CRACK. REMOVED FASTENERS, REMOVED CORROSION. NDT INSP C/W CUT DAMAGE AREA AND INSTALL DOUBLER REPAIR AT FUSE SKIN.Feb 19, 2001 · N919UP · Boeing 72730C · Fuselage Main, Plate/SkinSDR UPS01235282Skin · corrodedINSPECTION TYPE:C-CK, LOW FREQ EDDY CURRENT INSP OF SKIN AT BS 441 BETWEEN STRG 18R & 19R HAS INDICATION OF CORROSION LOSS GREATER THAN 10 PERCENT. REMOVED EQUIPMENT TO ACCESS REPAIR, CUT DAMAGED AREA AND INSTALLED REPAIR PER EO -1371.Feb 19, 2001 · N919UP · Boeing 72730C · Fuselage Main, Plate/SkinSDR UPS01235221Duct · crackedINSPECTION TYPE:C-CK, NR 2 ENG INLET S-DUCT INNER SKIN HAS APPROX 3 INCH CIRCUMFERENTIAL CRACK APPROX 104 INCHES FROM AFT EDGE AT 3 O''CLOCK. CUT OUT DAMAGE AREA. INSTALLED REPAIR.Feb 19, 2001 · N919UP · Boeing 72730C · Nacelle/Pylon, Main FrameSDR UPS01235401Lap Joint · bulgedINSPECTION TYPE:C CK LAP JOINT 19RT HAS SKIN BULGE AT BS 620. CUT OUT DAMAGED SKIN LWR & UPPER AREA. INSTALLED REPAIR PART AT LAP JOINT STR 19 BS 620.Feb 18, 2001 · N919UP · Boeing 72730C · Fuselage Main, Plate/Skin
Back to N919UP, cancelled Dec 4, 2007