N943FR

Service difficulty reports · 45

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 = 'N943FR' AND registry_match = 'registration'
  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 F3LA2021041500032Megaphone · inoperativeDISCREPANCY, LP1239913 ITEM 2: AFT BULL HORN INOP. CORRECTIVE ACTION: REMOVED AND REPLACED AFT MEGAPHONE, OPS TEST GOOD. REF AMM 25-65--51-710-002-A. NOTE 1) THIS WAS FOUND DURING PRE BOARDING FOR FLIGHT 383. NOTE 2) TIME SINCE INSPECTION, IS THE LAST TIME THApr 15, 2021 · N943FR · Airbus A319112 · Emergency EquipmentSDR F3LA2021041500031Megaphone · inoperativeDISCREPANCY, LP1239913 ITEM 1: FWD BULL HORN INOP. CORRECTIVE ACTION: REMOVED AND REPLACED FWD MEGA PHONE BATTERIES, OPS TEST GOOD. REF AMM 25-65-51-970-001-A. NOTE 1 THIS WAS FOUND DURING PRE BOARDING FOR FLIGHT 383. NOTE 2 TIME SINCE INSPECTION, IS THE LASApr 15, 2021 · N943FR · Airbus A319112 · Emergency EquipmentSDR F3LA2021012800005Battery · failedEPSU BATTERY FAILED REMOVED AND REPLACED EPSU EMERGENCY POWER SUPPLY UNIT. OPERATIONS CHECK OK, IAW AMM 33-51-38-400-001-A.Jan 28, 2021 · N943FR · Airbus A319112 · Emergency LightingSDR F3LA2020021850011Tip Cap · damaged03/05/2020 SUPPLEMENT: REMOVED DAMAGED R/H WING TIP AND INSTALLED SERVICEABLE R/H WINGTIP IAW AMM 57-31-21-PB401. REMOVED PN D5735052101951A, SN 13572. REMOVED AND REPLACED R/H WINGTIP FENCH IAW AMM 57-31-22-PB401, PN D5735120000300A. SIGNIFICANT DAMAGE TO RH Feb 15, 2020 · N943FR · Airbus A319112 · Wing, Plate/SkinSDR F3LA2020012390003Fitting · crackedLOWER AFT FASTENER HOLE ON L/H FRAME 16 UPPER DOUBLE JOGGLE SHOWS CRACK INDICATIONS. REPAIRED L1 DOOR FRAME 16 UPPER DOUBLER JOGGLE HOLE 'D' IAW REPAIR DRAWING R53113041 (ISSUE E). REPAIR INSPECTION THRESHOLD 6800 FC WITH INTERVALS OF 4129 FC PER RDAS.Jan 9, 2020 · N943FR · Airbus A319112 · Fuselage Main, StructureSDR F3LA201909200116Pipe · crackedDISCREPENCY: PIPE P/N D2621012400400, CRACKED FIRE BOTTLE DISCHARGE LINE, NUMBER 1 ENGINE PYLON. REFERENCE IPC 26-21-06-01D ITEM 310. CORRECTIVE ACTION: REMOVED AND REPLACED PIPE NUMBER 1 ENGINE FIRE BOTTLE TUBE. PERFORMED LEAK CHECK AMM 26-21-49-400-002-A. Sep 17, 2019 · N943FR · Airbus A319112 · Extinguishing SystemSDR F3LA2018102900471Generator · leakingDISCREPANCY: REFERENCE LOG PAGE LP1090541 ITEM 1, IMMEDIATELY UPON TURNING ON APU BLEEN AND PACKS 1 AND 2, WE NOTICED AN OILY MUSTY SMELL ON FLIGHT DECK. ONE MINUTE LATER FLIGHT ATTENDANTS IN BACK CALLED TO INFORM US OF ODOR IN BACK OF AIRCRAFT, TRIED TO ISOLAOct 24, 2018 · N943FR · Airbus A319112 · AC Generator-AlternatorSDR F3LA2018062500359Power Supply · failedEPSU 10WL FAILED EPSU TEST. REMOVED AND REPLACED EPSU ASSEMBLY 10WL IAW AMM 33-51-38 PAGE BLOCK 401. OPERATIONAL CHECK GOOD.Jun 24, 2018 · N943FR · Airbus A319112 · Emergency LightingSDR F3LA2018013100285Floorbeam · corrodedCORROSION ON FLOORBEAM -Y765 AT FRAME 66. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-14-283-002. REMOVED AND REPLACED THE FLOORBEAM IAW SRM 51-42-11, 51-72-11-911-001, AND 51-44-11.Jan 25, 2018 · N943FR · Airbus A319112 · Fuselage Main, Floor BeamSDR F3LA2018013100284Floorbeam · corroded2 AREAS OF CORROSION ON FLOORBEAM -Y765 BETWEEN FR66 AND FR68. REMOVED AND REPLACED FLOORBEAM AT -Y765 BETWEEN FR66 AND FR68 IAW SRM 51-42-11, 53-00-14-283-002, 51-72-911-001 AND 51-44-11.Jan 23, 2018 · N943FR · Airbus A319112 · Fuselage Main, Floor BeamSDR F3LA2018013100282Floorbeam · corrodedFLOORBEAM Y512 HAS CORROSION AT FR66. REFERENCE NR 1832N291, REMOVED AND REPLACED FLOORBEAM Y512 FR67-64 IAW SRM 51-72-11-911-001, 53-00-14-283-002 AND 51-44-11.Jan 23, 2018 · N943FR · Airbus A319112 · Fuselage Main, Floor BeamSDR F3LA2018012900283Floorbeam · corrodedFLOORBEAM Y1292 HAS CORROSION AT FRAME 68. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-14-283-002. REMOVED AND REPLACED THE FLOORBEAM IAW SRM 51-72-11-911-001, 51-42-11, AND 51-44-11.Jan 23, 2018 · N943FR · Airbus A319112 · Fuselage Main, Floor BeamSDR F3LA2018012900281Floor Support · corrodedTHREE AREAS OF CORROSION ON THE FLOOR SUPPORT Y765 BETWEEN FRAMES 66 AND 68. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-42-11, 51-72-11-911-001, 53-00-14-283-002, AND 51-44-11.Jan 23, 2018 · N943FR · Airbus A319112 · Fuselage Miscellaneous StructureSDR F3LA2018012900280Floorbeam · corrodedCORROSION ON THE FLOORBEAM Y1162, FRAME 68. THE FLOORBEAM WAS FOUND TO BE OUT OF LIMITS IAW SRM 53-00-14-283-002. REMOVED AND REPLACED THE FLOORBEAM IAW SRM 51-72-11, 51-44-11, AND 51-72-11-911-001.Jan 23, 2018 · N943FR · Airbus A319112 · Fuselage Main, Floor BeamSDR F3LA2018012600279Floorbeam · corrodedCORROSION ON FLOORBEAM -Y1162 BY FRAME 68. REMOVED AND REPLACED THE FLOORBEAM IAW SRM 51-72-11, SRM 53-00-14, AND SRM 51-44-11.Jan 23, 2018 · N943FR · Airbus A319112 · Fuselage Main, Floor BeamSDR F3LA2018012600278Floorbeam · corrodedTWO AREAS OF CORROSION ON THE FLOORBEAM -Y1292 BY FRAME 66. REMOVED AND REPLACED THE FLOORBEAM IAW SRM 51-72-11, SRM 53-00-14, AND SRM 51-44-11.Jan 23, 2018 · N943FR · Airbus A319112 · Fuselage Main, Floor BeamSDR F3LA2016020200002Slide · failedEMERGENCY POWER SUPPLY UNIT TEST FAILED FOR L1 DOOR SLIDE. R & R L1 DOOR SLIDE IAW AMM 25-62-44-000-012A & AMM 25-62-44-400-007A. OPERATIONAL CHECKED GOOD.Jan 27, 2016 · N943FR · Airbus A319112 · Escape SlideSDR F3LA2016011100001Seal · damagedLOSS OF OIL QTY ON NR 2 ENG. QTY LESS THAN 2 PSI AT CRUISE. OIL PSI 0 ON APPROACH & LAND. OIL TEMP & PRESS WITH NR 2 ENG AT IDLE 28 PSI & 80 DEGREE C. TROUBLE SHOT, LEAK FOUND HYD PUMP PAD SEAL LEAKING. R & R SEAL ON THE HYD PUMP SHAFT IAW AMM 72-63-00-30Jan 6, 2016 · N943FR · Airbus A319112 · Turbine Engine Oil SystemSDR F3LA2015122201156Epsu · failedEMERGENCY POWER SUPPLY UNIT SYS TEST FAILED, CODE 10WL FWD LT. R & R EPSU 10WL. OPERATIONS TESTED GOOD IAW AMM 33-51-38 PB 401. REFERENCE LP 967286.Dec 19, 2015 · N943FR · Airbus A319112 · Emergency LightingSDR F3LA2015033001126Battery · dischargedEMERGENCY PATH LIGHTING BATTERY OF EPSU 10WL FAILED TEST DURING HEAVY SERVICE CHECK. R & R BATTERY OF EPSU 10WL. OPERATIONS CHECKED GOOD IAW AMM 33-51-38-000-002 & 33-51-38-400-002 LP 925756.Mar 27, 2015 · N943FR · Airbus A319112 · Emergency LightingSDR F3LA2018102900472Apu · leakingDISCREPANCY: REFERENCE LOG PAGE LP1090541 ITEM 1, IMMEDIATELY UPON TURNING ON APU BLEEN AND PACKS 1 AND 2, WE NOTICED AN OILY MUSTY SMELL ON FLIGHT DECK. ONE MINUTE LATER FLIGHT ATTENDANTS IN BACK CALLED TO INFORM US OF ODOR IN BACK OF AIRCRAFT, TRIED TO ISOLAOct 24, 2014 · N943FR · Airbus A319112 · APU Core EngineSDR F3LA2014090201061Floorbeam · corrodedAIRCRAFT DUE C 6 INSPECTION. DISCREPANCY, MAIN CABIN FLOORBEAM FRAME 68 Y1292 CORRODED TO 50% OF MATERIAL THICKNESS. R & R MAIN CABIN FLOORBEAM FRAME 68 Y1292 IAW SRM 51-42-11 PAR 5, 6 & 7 & SRM 51-49-00 TABLE 9. ACFT DUE OUT OF C CHECK SEPTEMBER 2, 2014.Sep 1, 2014 · N943FR · Airbus A319112 · Fuselage Main, Floor BeamSDR F3LA2014040101031Windshield · crackedWINDSHIELD CRACKED AT FL390, SEEMS TO BE OUTER PANE ONLY, NO FLUCTUATIONS IN PRESSURIZATION NOTED. R & R FIRST OFFICER`S WINDSHIELD IAW AMM 56-11-11-000-001 & AMM 56-11-11-400-001, OPERATIONS CHECKED GOOD. REPLACED WINDOW HEAT CONTROLLER SEE LOG PAGE 827954 Mar 28, 2014 · N943FR · Airbus A319112 · Flight Compartment WindowsSDR F3LA2012042300748Computer · malfunctionedECAM ON DESCENT: CIDS 1 AND 2 FAULT WITH UNCOMMANDED EMERGENCY LIGHTS FLICKERING CABIN LIGHTS LOSS OF CABIN COMMUNICATIONS. THIS WAS INTERMITTENT FOR ONLY A FEW MINUTES THEN WENT BACK TO NORMAL. TROUBLESHOT REPLACED CIDS DIRECTOR IAW AMM 23-73·34PB 401. OPS CApr 20, 2012 · N943FR · Airbus A319112 · Central WarningSDR F3LA2011122100695Unknown · odorAT 4000 FT AGL, F/A REPORTED A BURNING ODOR COMING FROM THE AFT LT LAV. TROUBLESHOT IAW TSM 24-00-00-810-823. NO DEFECTS NOTED. INSPECTED THE FOLLOWING AREAS, LAVATORY HOT WATER HEATERS, COFFEEMAKERS IN AFT GALLEY INCLUDING WIRING, LIVE TV COMPONENTS WHILE Dec 19, 2011 · N943FR · Airbus A319112 · Air Distribution SystemSDR F3LA2011052300651Shear Plate · corrodedC-CHECK: NON ROUTINE NR 33802; LT SHEAR PLATE AT FRAME 69-70 HAS CORROSION ON THE UPPER SURFACE. REMOVED AND REPLACED AHEAR PLATE IAW EO A0-53EO-31434 AND SRM 51-42-11.May 17, 2011 · N943FR · Airbus A319112 · Fuselage Miscellaneous StructureSDR F3LA2011052300650Shear Plate · corrodedC-CHECK: NON ROUTINE NR 33801; RT SHEAR PLATE AT FRAME 69 - 70 HAS UPPER SURFACE CORROSION. REMOVED AND REPLACED SHEAR PLATE IAW EO A0-53EO-31-434 AND SRM 51-42-11.May 17, 2011 · N943FR · Airbus A319112 · Fuselage Miscellaneous StructureSDR F3LA2011052300649Sill · corrodedC-CHECK: MAIN CABIN FRAME 66 -Y1500, AFT PASSENGER DOOR SILL BEAM HAS SURFACE CORROSION. REPARED DOOR SILL BEAM IAW SRM 53-41-14, FIG 201.May 17, 2011 · N943FR · Airbus A319112 · Fuselage Miscellaneous StructureSDR F3LA2011052300648Floorbeam · corrodedC-CHECK: CABIN FLOORBEAM AT FRAME 68, Y1292 HAS CORROSION. REMOVED AND REPLACED FLOORBEAM IAW SRM 53-00-14, FIG 102 ALSO SRM 51-42-11, PARA 5.May 17, 2011 · N943FR · Airbus A319112 · Fuselage Main, Floor BeamSDR F3LA2011052300647Floor Support · corrodedC-CHECK: NON ROUTINE NR 33820; CABIN FLOOR SUPPORT FRAME 67-69, -Y1292 HAS CORROSION. REMOVED AND REPLACED FLOORBEAM IAW SRM 53-00-14, FIG 102 ALSO SRM 51-42-11 PARA 5 A, D AND 6 B 1-8.May 17, 2011 · N943FR · Airbus A319112 · Fuselage Miscellaneous StructureSDR F3LA2009111300227Sill · corrodedREFERENCE NON ROUTINE C074186. DURING DEN C3 C-CHECK, INSPECTION NOTED CORROSION ON THE L2 DOOR SILL AT FRAME 66 IN FWD SPLICE AREA. MX PERFORMED MAJOR REPAIR IAW SRM 53-41-14, SRM 51-44-00, SRM 51-21-00 AND SRM 51-75-00.Nov 7, 2009 · N943FR · Airbus A319112 · Fuselage Miscellaneous StructureSDR F3LA2009111600230Floorbeam · corrodedDURING DEN C3 C-CHECK, INSP NOTED CORROSION ON THE FLOORBEAM Y1162.5 AT FRAME 68. MX REMOVED AND REPLACED THE FLOORBEAM IAW SRM 53-00-14, SRM 51-42-11, SRM 51-11-13, AND EA A9-53R-31489.Nov 6, 2009 · N943FR · Airbus A319112 · Fuselage Main, Floor BeamSDR F3LA2009111600229Floor Support · corrodedDURING DEN C3 C-CHECK, INSP NOTED CORROSION ON THE FLOOR SUPPORT Y1292 BETWEEN FRAME 64 AND FRAME 66. MX REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 53-00-14, SRM 51-42-11, SRM 51-11-13, SRM 51-44-11 AND AMM 20-28-00 PB 501.Nov 6, 2009 · N943FR · Airbus A319112 · Fuselage Miscellaneous StructureSDR F3LA2009111600228Floor Support · corrodedREFERENCE NON ROUTINE C073981. DURING DEN C3 C-CHECK, INSP, NOTED CORROSION IN THE AFT CABIN AREA ON THE FLOOR SUPPORT Y1292 BETWEEN FRAME 66 AND FRAME 68. MX REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 53-00-14, SRM 51-42-11 AND SRM 51-44-11.Nov 6, 2009 · N943FR · Airbus A319112 · Fuselage Miscellaneous StructureSDR F3LA2009111200226Floorbeam · corrodedREFERENCE NON ROUTINE C073982. DURING DEN C3 C-CHECK, INSP NOTED CORROSION ON FLOORBEAM LOCATED AT -Y1292 BETWEEN FRAME 67 AND FRAME 68. MX REPAIRED THE FLOORBEAM IAW SRM 51-73-11, SRM 51-44-11 AND EA A9-53R-31491.Nov 6, 2009 · N943FR · Airbus A319112 · Fuselage Main, Floor BeamSDR F3LA2008123000732Safety Valve · leakingPILOT RETURNED TO BLOCK DUE TO LOSS OF GREEN SYSTEM HYDRAULIC PRESSURE. MAINTENANCE REMOVED AND REPLACED LANDING GEAR SAFETY VALVE AND PERFORMED OPERATIONAL CHECK IAW A319 AMM 32-31-17 PB401 AND 32-31-00-710-005.Dec 28, 2008 · N943FR · Airbus A319112 · Hydraulic System, MainSDR F3LA200800504Hook · out of adjustDURING C-CHECK INSP, NOTED THE R2 DOOR INSIDE HANDLE CAN BE OPERATED WHILE DOOR IS NOT CLOSED. MAINT ADJUSTED THE R2 DOOR HOOK IAW AMM 52-11-21-400-001. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)Jul 20, 2008 · N943FR · Airbus A319112 · Service DoorsSDR F3LA200800503Torsion Bar · out of adjustDURING C-CHECK, INSP NOTED THE R2 DOOR WOULD NOT ARM WITH DOOR CLOSED AND LOCKED. THIS OCCURRED DURING OPERATION OF THE DOOR WHILE PERFORMING TASK CARD C528002-2. MAINT ADJUSTED TORSION BAR AND PERFORMED OPS CHECK IAW AMM 52-11-21-400-001 AND TASK CARD C5280Jul 20, 2008 · N943FR · Airbus A319112 · Service DoorsSDR F3LA200800502Floor Panel · delaminatedDURING C2 C-CHECK, INSPECTION NOTED THE TOP LAYER DELAMINATED ON FLOOR PANEL 251NF. MAINTENANCE REMOVED DELAMINATED LAYER AND APPLIED MYLAR PATCH IN ACCORDANCE WITH A319 SRM 53-02-00.Jul 17, 2008 · N943FR · Airbus A319112 · Fuselage Floor PanelSDR F3LA200800497Floor Panel · puncturedDURING C2 C CHECK, INSPECTION NOTED THE AFT PIT TRANSITION PANEL 161UG WAS PUNCTURED. MAINTENANCE RECORDED THAT THIS NON ROUTINE HAS THE PANEL NUMBER INCORRECTLY INDICATED. THE DAMAGED PANEL IS 151UG. MAINTENANCE REPAIRED DAMAGE TO PANEL 151UG IAW THE REQUIJul 15, 2008 · N943FR · Airbus A319112 · Fuselage Floor PanelSDR F3LA200800496Floor Panel · puncturedDURING C2 C CHECK, INSPECTION NOTED THE AFT PIT TRANSITION PANEL 151FE WAS PUNCTURED. MAINTENANCE REPAIRED DAMAGE IAW THE REQUIREMENTS OF A319 SRM 53-02-00, PARAGRAPH 8C FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (S)Jul 15, 2008 · N943FR · Airbus A319112 · Fuselage Floor PanelSDR F3LA200800495Floor Panel · puncturedDURING C2 C CHECK, INSPECTION NOTED THE AFT PIT TRANSITION PANEL 151DE WAS PUNCTURED. MAINTENANCE REPAIRED DAMAGE IAW THE REQUIREMENTS OF A319 SRM 53-02-00, PARAGRAPH 8C FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (S)Jul 15, 2008 · N943FR · Airbus A319112 · Fuselage Floor PanelSDR F3LA200800494Floor Panel · puncturedDURING C2 C-CHECK, INSPECTION NOTED THE AFT PIT TRANSITION PANEL 151BE WAS PUNCTURED. MAINTENANCE REPAIRED THE DAMAGE IAW THE REQUIREMENTS OF A319 SRM 53-02-00, PARAGRAPH 8C FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (SJul 15, 2008 · N943FR · Airbus A319112 · Fuselage Floor PanelSDR F3LA200800493Floor Panel · puncturedDURING C2 C CHECK, INSPECTION NOTED THE AFT PIT TRANSITION PANEL 151AE WAS PUNCTURED. MAINTENANCE REPAIRED THE DAMAGE IAW THE REQUIREMENTS OF A319 SRM 53-02-00, PARAGRAPH 8C FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (SJul 15, 2008 · N943FR · Airbus A319112 · Fuselage Floor PanelSDR F3LA200800492Floor Panel · puncturedDURING C2 C CHECK, INSPECTION NOTED THE AFT PIT TRANSITION PANEL 151UG WAS PUNCTURED. MAINTENANCE RECORDED THAT THIS IS EITHER A DUPLICATE WRITE-UP (161UG- NON ROUTINE C047467) OR SHOULD HAVE BEEN WRITTEN AS 152UG, WHICH HAD DAMAGE ALSO. THE DAMAGE REPAIR FOJul 15, 2008 · N943FR · Airbus A319112 · Fuselage Floor Panel
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