N940FR, cancelled Dec 3, 2012

Service difficulty reports · 39

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 = 'N940FR' AND deregistration_id = 'N940FR-2012-12-03'
  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 F3LA2012083100781Skin · dentedNR 1 ENGINE NOSE COWL INNER BARREL AT 9:30 POSITION HAS A DENT. REPAIRED IAW SRM 54-10-00, REPAIR 23, PARAGRAPH 2.A,B,C(1-3}, D, E(1 -2), F{1 -2), G AND H( 1-4).Aug 27, 2012 · N940FR · Airbus A319111 · Nacelle/Pylon, Plate/SkinSDR F3LA2012083100780Skin · dentedNR 1 ENGINE NOSE COWL INNER BARREL AT 9:00 POSITION HAS A DENT, REPAIRED IAW SRM 54-10-00, REPAIR 23, PARAGRAPH 2.A,B,C(1 -3), D, E(1 -2), F( 1-2), G AND H( 1-4).Aug 27, 2012 · N940FR · Airbus A319111 · Nacelle/Pylon, Plate/SkinSDR F3LA2012041000733Valve · inoperativeLEFT BRAKE PRESSURE INDICATION SHOWS ZERO PSI. R & R ALTERNATE BRAKE DIRECT DRIVE VALVE. OPS CHECK NORMAL REF AMM 32-43-35 PAGE BLOCK 401. TORQUE WRENCH F9TAB2197C CALIBRATION DUE 01/13. MEL CLEARED.Apr 4, 2012 · N940FR · Airbus A319111 · Landing Gear Brake SystemSDR F3LA2012021400710Epsu · failedCIDS 1 EPSU SYS TEST FAILS EPSU (10WL) FWD L/ DEU B (300RH1), R & R FAP DUE TO FAP NOT ACCEPTING CAM WRT AMM 23-73-12 PB 401. FAP LAYOUT SELECTION NOT CONFIGURED FOR CURRENT CABIN LAYOUT-CONT T/S. REINSTALLED ORIGINAL FAP IAW AMM 23-73-12 PB401 CLEANED AND TFeb 12, 2012 · N940FR · Airbus A319111 · Emergency LightingSDR F3LA2011110900688Light · malfunctionedEMERGENCY EXIT LIGHTS AND ESCAPE PATH LIGHTS REMAINED ON DURING FLIGHT WITH SWITCH IN "NORM" POSITION- AND FAP AMBER NOTE "CHECK PAX RELATED FUNCTIONS" TROUBLESHOT REF TSM 33-51-00-810-881. CHECKED EPSU BATTERIES FOR CONDITION AND SECURITY. OPS TEST NORMAL IAWNov 4, 2011 · N940FR · Airbus A319111 · Emergency LightingSDR F3LA2011091300671Relay · inoperativeEMERGENCY EXIT LIGHTS FLICKERING ON TAKEOFF ROLL. R & R RELAY (8WL) REF ASM 33-51-00. OPS TEST OF THE EMERGENCY LIGHTS TEST GOOD REF AMM 33-51-00-710-001.Sep 13, 2011 · N940FR · Airbus A319111 · Emergency LightingSDR F3LA2011083100666Power Supply · failedPATHWAY EMERGENCY LIGHTS ON & OFF INTERMITTENTLY, EMERGENCY EXIT LIGHT ACFT LT OVERWING EXIT ON THROUGHOUT NIGHT. R & R EPSU EMERGENCY POWER SUPPLY UNIT 11WL WITH SERVICEABLE PART IAW AMM 33-51-38 PB 401, OPS CHECK GOOD.Aug 30, 2011 · N940FR · Airbus A319111 · Emergency LightingSDR F3LA2010010500287Blanking Plate · corrodedDURING C3 C-CHECK INSP NOTED L2 DOOR AFT GIRT BAR BLANKING PLATE CORRODED. MX INSTALLED NEW L2 DOOR AFT GIRT BAR BLANKING PLATE IAW AMM 52-13-31-400-007.Jan 3, 2010 · N940FR · Airbus A319111 · Fuselage Miscellaneous StructureSDR F3LA2010010500286Blanking Plate · corrodedDURING C3 C-CHECK INSP NOTED L2 DOOR FWD GIRT BAR BLANKING PLATE CORRODED. MX INSTALLED NEW L2 DOOR FWD GIRT BAR BLANKING PLATE IAW AMM 52-13-31-400-007.Jan 3, 2010 · N940FR · Airbus A319111 · Fuselage Miscellaneous StructureSDR F3LA2010010500285Blanking Plate · corrodedDURING C3 C-CHECK INSP NOTED R2 DOOR AFT GIRT BAR BLANKING PLATE CORRODED. MX INSTALLED NEW R2 DOOR AFT GIRT BAR BLANKING PLATE IAW AMM 52-13-31-400-007.Jan 3, 2010 · N940FR · Airbus A319111 · Fuselage Miscellaneous StructureSDR F3LA2010010500284Blanking Plate · corrodedDURING C3 C-CHECK INSP NOTED R2 DOOR FWD GIRT BAR BLANKING PLATE CORRODED. MX INSTALLED NEW R2 DOOR FWD GIRT BAR BLANKING PLATE IAW AMM 52-13-31-400-007.Jan 3, 2010 · N940FR · Airbus A319111 · Fuselage Miscellaneous StructureSDR F3LA2010010500283Floor Panel · delaminatedDURING C3 C-CHECK INSP NOTED FLOOR PANEL 261EF TOP GLASS LAYER IS DELAMINATED AFT LT SIDE. MX REPAIRED FLOOR PANEL IAW EA A9-53R-31605.Jan 2, 2010 · N940FR · Airbus A319111 · Fuselage Floor PanelSDR F3LA2010010500282Floor Panel · corrodedDURING C3 C CHECK INSP NOTED AFT R2 DOOR THRESHOLD AREA FLOOR PANEL 262FF HAS CORROSION AROUND ATTACHMENT HOLES AND TOP SURFACE. MX REPLACED PANEL 262FF IAW ROUTINE TASK CARD C534103-2.Dec 28, 2009 · N940FR · Airbus A319111 · Fuselage Floor PanelSDR F3LA2010010500281Skin · gougedDURING C3 C-CHECK INSP, NOTED SKIN GOUGED IN 3 SPOTS BETWEEN FRAME 52 AND FRAME 51 BETWEEN STRINGER 1 RT AND STRINGER 2 RT. MX REPAIRED FUSELAGE SKIN IAW SRM 53-00-11, FIG 204.Dec 28, 2009 · N940FR · Airbus A319111 · Fuselage Main, Plate/SkinSDR F3LA2010010500280Floor Support · corrodedDURING C3 C-CHECK INSP NOTED FLOOR SUPPORT Y1292 FRAME 68 TO FRAME 69 OTBD FASTENER HOLE AT FRAME 68 CORRODED. MX REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-74-00, SRM 53-00-14, SRM 51-42-11, SRM 51-44-11 AND SRM 51-75-12.Dec 28, 2009 · N940FR · Airbus A319111 · Fuselage Miscellaneous StructureSDR F3LA2010010500279Plate · corrodedDURING C3 C-CHECK INSP NOTED R2 DOOR SILL PLATE INBD FASTENER HOLE FWD OF FRAME 68 IS CORRODED. MX REPAIRED FASTENER HOLE IAW SRM 53-41-14 FIGURE 201 REPAIR PRINCIPLE NR 5.Dec 28, 2009 · N940FR · Airbus A319111 · Fuselage Miscellaneous StructureSDR F3LA2009123100276Plate · corrodedDURING C-3 C-CHECK INSP NOTED LT AFT SHEAR PLATE IS CORRODED ON NUT PLATE HOLES. MX REMOVED AND REPLACED SHEAR PLATE IAW SRM 51-42-11, SRM 51-21-11, SRM 51-44-11, SRM 51-75-12 AND EO A0-53EO-31434.Dec 28, 2009 · N940FR · Airbus A319111 · Fuselage Miscellaneous StructureSDR F3LA2010010500278Floorbeam · corrodedDURING C3 C-CHECK INSP, NOTED FLOORBEAM CORRODED AFT CABIN AT FRAME 67 Y1295. MX REMOVED AND REPLACED FLOORBEAM IAW SRM 51-74-00, SRM 53-00-14, SRM 51-42-11, SRM 51-44-11 AND SRM 51-75-12.Dec 27, 2009 · N940FR · Airbus A319111 · Fuselage Main, Floor BeamSDR F3LA2010010200277Floorbeam · corrodedDURING C3 C-CHECK INSP NOTED FLOORBEAM CORRODED AFT CABIN AT FRAME 67 Y1295. MX REMOVED AND REPLACED FLOORBEAM IAW SRM 51-74-00, SRM 53-00-14, SRM 51-42-11, SRM 51-44-11 AND SRM 51-75-12.Dec 27, 2009 · N940FR · Airbus A319111 · Fuselage Main, Floor BeamSDR F3LA2009123100275Plate · corrodedDURING C-3 C-CHECK INSP, NOTED THE SHEAR PLATE CORRODED RT SIDE AFT CABIN UNDER GALLEY AT FRAME 70 Y1162. MX REMOVED AND REPLACED SHEAR PLATE IAW SRM 51-42-11 AND EO A0-53EO-31434.Dec 27, 2009 · N940FR · Airbus A319111 · Fuselage Miscellaneous StructureSDR F3LA2009090800164Line · chafedREFERENCE LOG PAGE 472314. CREW MADE AN AIR TURN BACK TO DEN DUE TO AN INDICATION FOR THE GREEN HYDRAULIC RESERVOIR LEVEL LOW. MAINTENANCE INSPECTED AND FOUND A GREEN HYDRAULIC SYSTEM PRESSURE PIPE WITH CHAFING DAMAGE AND A PIN HOLE. MAINTENANCE REMOVED AND RESep 5, 2009 · N940FR · Airbus A319111 · Hydraulic System, MainSDR F3LA2009082500137Seal · displacedFUEL TRANSFERRED TO RT WING TANK DURING CTR PUMP OPERATION. MX FOUND SEAL FROM AFT FUEL SURGE ACCESS PANEL HAD MIGRATED INTO THE RT WING FUEL PUMP SUCTION VALVE. MX REPLACED THE PUMP SUCTION VALVE (PN D2825006400200)AND FUEL SURGE VALVE SEAL (PN 5725054220000)Aug 21, 2009 · N940FR · Airbus A319111 · Aircraft Fuel Distribution SystemSDR F3LA2009072200108Hose · leakingREF LOG PAGES 475705 AND 475708. DURING CLIMB OUT, PILOTS RECEIVED A WARNING FOR "AIR ENGINE 1 AND 2 BLEED FAULT" AND MADE AN AIR RETURN TO DEPARTURE. MX REMOVED AND REPLACED THE PRESSURE SENSE LINE AND PERFORMED OPS CHECK.Jul 19, 2009 · N940FR · Airbus A319111 · Pneumatic Distribution SystemSDR F3LA200800463Floor Panel · damagedDURING C-CHECK INSP NOTED FWD PIT FLOOR PANEL 131CG DAMAGED. MAINT REPAIRED DAMAGE IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B)Jul 11, 2008 · N940FR · Airbus A319111 · Fuselage Floor PanelSDR F3LA200800462Floor Panel · damagedDURING C-CHECK INSP NOTED AFT PIT TRANSITION PANEL 151HE DAMAGED. MAINT REPAIRED DAMAGE IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B)Jul 11, 2008 · N940FR · Airbus A319111 · Fuselage Floor PanelSDR F3LA200800461Panel · damagedDURING C-CHECK INSP NOTED AFT PIT TRANSITION PANEL 151GE DAMAGED. MAINT REPAIRED DAMAGE IAW SRM 53-02-00, FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B)Jul 11, 2008 · N940FR · Airbus A319111 · Fuselage Miscellaneous StructureSDR F3LA200800460Floor Panel · damagedDURING C-CHECK INSP NOTED AFT PIT FLOOR PANEL 151CE DAMAGED. MAINT REPAIRED DAMAGE IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B)Jul 11, 2008 · N940FR · Airbus A319111 · Fuselage Floor PanelSDR F3LA200800459Floor Panel · damagedDURING C-CHECK INSP NOTED AFT PIT PANEL 152UG DAMAGED. MAINT REMOVED DAMAGED AREA, FILLED DAMAGED AREA IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B)Jul 11, 2008 · N940FR · Airbus A319111 · Fuselage Floor PanelSDR F3LA200800458Floor Panel · damagedDURING C-CHECK INSP NOTED AFT PIT PANEL 152WG DAMAGED. MAINT REMOVED DAMAGED AREA, FILLED DAMAGED AREA IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B)Jul 11, 2008 · N940FR · Airbus A319111 · Fuselage Floor PanelSDR F3LA200800457Floor Panel · damagedDURING C-CHECK INSP NOTED AFT PIT PANEL 151FE DAMAGED. MAINT REMOVED DAMAGED AREA, FILLED DAMAGED AREA IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B)Jul 11, 2008 · N940FR · Airbus A319111 · Fuselage Floor PanelSDR F3LA200800456Panel · damagedDURING C-CHECK INSP NOTED AFT PIT PANEL 151DE DAMAGED. MAINT REMOVED DAMAGED AREA, FILLED DAMAGED AREA IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B)Jul 11, 2008 · N940FR · Airbus A319111 · Fuselage Miscellaneous StructureSDR F3LA200800455Floor Panel · damagedDURING C-CHECK INSP NOTED AFT PIT PANEL 151PE DAMAGED. MAINT REMOVED DAMAGED AREA, FILLED DAMAGED AREA IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B)Jul 11, 2008 · N940FR · Airbus A319111 · Fuselage Floor PanelSDR F3LA200800454Panel · damagedDURING C-CHECK INSP, NOTED AFT PIT PANEL 161NF DAMAGED. MAINT REMOVED DAMAGED AREA, FILLED DAMAGED AREA IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B)Jul 11, 2008 · N940FR · Airbus A319111 · Fuselage Miscellaneous StructureSDR F3LA200800453Floor Panel · damagedDURING C-CHECK INSP AFT PIT PANEL 161BF DAMAGED. MIANT REMOVED DAMAGED AREA, FILLED DAMAGED AREA IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B)Jul 11, 2008 · N940FR · Airbus A319111 · Fuselage Floor PanelSDR F3LA200800452Floor Panel · damagedDURING C-CHECK INSP, NOTED AFT PIT PANEL 162EF DAMAGED. MAINT REMOVED DAMAGED AREA, FILLED DAMAGED AREA IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B)Jul 11, 2008 · N940FR · Airbus A319111 · Fuselage Floor PanelSDR F3LA200800451Floor Panel · damagedDURING C-CHECK INSP, NOTED AFT PIT PANEL 161CF DAMAGED. MAINT REMOVED DAMAGE AREA, FILLED DAMAGED AREA IAW SRM 53-02-00 FIGURE 204. UPON COMPETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B)Jul 11, 2008 · N940FR · Airbus A319111 · Fuselage Floor PanelSDR F3LA200800464Floor Panel · damagedDURING C-CHECK INSP NOTED FWD PIT PANEL 131EG DAMAGED. MAINT REPAIRED DAMAGE IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B)Jul 11, 2008 · N940FR · Airbus A319111 · Fuselage Floor PanelSDR F3LA200800003Epsu · inoperativeDURING PERFORMANCE OF EPSU (12WL) FUNCTIONAL TEST, THE MECHANIC NOTED A POWER SUPPLY FAULT ON THE MDCU. THE EPSU WAS REPLACED, IAW AMM 33-51-38 PB 401 AND OPERATIONS CHECKED OKAY. PART TOTAL TIMES AND TOTAL CYCLES WILL BE PROVIDED AT A LATER DATE. REFERENCEJan 10, 2008 · N940FR · Airbus A319111 · Emergency LightingSDR F3LA200600163Rib · failedDURING C-1 CHECK, INSPECTION REPORTED RT PYLON RIB 9 FAILED HEAT TREATMENT TEST. READINGS BELOW 200. ACCOMPLISHED MODIFICATION (INSTALLATION OF RIB REINFORCEMENT KIT) PER EA A9-54R-11704.Dec 10, 2006 · N940FR · Airbus A319111 · Nacelle/Pylon, Frame/Spar/Rib
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