N939FR, cancelled Aug 22, 2022

Service difficulty reports · 67

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 = 'N939FR' AND deregistration_id = 'N939FR-2022-08-22'
  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 F3LA2018112800479Hydraulic Line · leakingHYD G RSVR LO LVL. AIRCRAFT WAS GROUNDED DUE TO THIS DISCREPANCY. REMOVED AND REPLACED NR 1 ENG PRESSURE/SUCTION/RETURN LINE, REF AMM 29-11-49 PB401. NO LEAKS AT THIS TIME. OK TO CONTINUE. OPS CHECK GOOD. DUE TO LANDING GRAVITY EXTENSION MX PERFORMED LANDING GNov 23, 2018 · N939FR · Airbus A319112 · Hydraulic System, MainSDR F3LA2018090400420Door Frame · crackedFOUND CRACKS ON LT NR 1 EMERGENCY EXIT. LOCATED ON FWD AND AFT SEGMENTS AND ON THE FWD AND AFT SEGMENTS ON RT NR 1 EMERGENCY EXIT. ACCOMPLISHED OVERWING EMERGENCY EXIT LT AND RT DOOR FRAME OUTER FLANGE REPAIR PER EA A9-52R-34351 ON THE FWD AND AFT FRAME SEGMENAug 22, 2018 · N939FR · Airbus A319112 · Emergency ExitsSDR F3LA2018083000418Hydraulic Line · crimpedHYDRAULIC LINE IN THE RT AFT UPPER MLG WW WAS DAMAGED. REMOVED AND REPLACED THE HYD LINE IAW AMM 32-43-00-710-001-A, 32-43-00-870-002-A, 12-12-29-611-002-A, AND 20-23-11-300-001.Aug 19, 2018 · N939FR · Airbus A319112 · Hydraulic System, MainSDR F3LA2018083000417Hydraulic Line · rupturedHYDRAULIC LINE AT THE LT AFT UPPER MLG WW WAS RUPTURED. REMOVED RUPTURED ALTERNATE BRAKING HYDRAULIC LINE & REPLACED WITH NEW IAW AMM 20-23-11-911-001-A. PERFORMED BLEEDING OF ALTERNATE BRAKING SYSTEM IAW AMM 32-43-00-870-002-A, SUCCESSFUL OPS CHECK OF THEAug 19, 2018 · N939FR · Airbus A319112 · Hydraulic System, MainSDR F3LA2018083000419Floorbeam · corrodedDISCREPANCY: CORROSION AROUND HARD POINT, BEAM -Y765 FR66. CORRECTIVE ACTION: REFERENCE PEMCO N/R 2082N289 REMOVED AND REPLACED NEW FLOOR BEAM -Y765 IAW A319 SRM 51-72-11-911-001, 53-41-14-283-004 AND 51-21-11./END/Aug 17, 2018 · N939FR · Airbus A319112 · Fuselage Main, Floor BeamSDR F3LA2018082700409Floor Support · corrodedCORROSION FOUND ON THE RT FLOOR SUPPORT, -Y1292, FRAMES 66 - 68. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-42-11, 51-44-11, AND 53-41-14-283-004.Aug 17, 2018 · N939FR · Airbus A319112 · Fuselage Miscellaneous StructureSDR F3LA2018082700408Floor Support · corrodedLEFT FLOOR SUPPORT, Y1162 WAS CORRODED BETWEEN FRAMES 66 - 69. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11-911-001, AND 53-00-14-282-002.Aug 16, 2018 · N939FR · Airbus A319112 · Fuselage Miscellaneous StructureSDR F3LA2018082400402Floorbeam · corrodedDISCREPANCY: REFERENCE NR 2082N250, LH FLOORBEAM Y765 HAS CORROSION AT FR66. CORRECTIVE ACTION: REMOVED AND REPLACED AFT WET AREA FLOORBEAM AT FR66 LOC Y765 IAW A319 SRM 51-72-11-911-001, 53-00-14-282-002 AND 51-44-11./END/Aug 16, 2018 · N939FR · Airbus A319112 · Fuselage Main, Floor BeamSDR F3LA2018082400401Floorbeam · corrodedDISCREPANCY: REFERENCE NR 2082N247, RH AFT FLOORBEAM -Y1162 HAS CORROSION AROUND FASTENER HOLE FR68. CORRECTIVE ACTION: REMOVED AND REPLACED FLOORBEAM -Y1162 IAW A319 SRM 51-42-11, 51-44-11 AND 53-00-14-283-002 FR68./END/Aug 16, 2018 · N939FR · Airbus A319112 · Fuselage Main, Floor BeamSDR F3LA2018082300400Floor Support · corrodedLH FLOOR SUPPORT Y512 HAS CORROSION AROUND FASTENER HOLE FR66. REMOVED AND REPLACED FLOOR SUPPORT Y512 FR66 TO 70 IAW SRM 51-72-11-911-002, 53-00-14-283-002 AND 51-72-911-001./END/Aug 16, 2018 · N939FR · Airbus A319112 · Fuselage Miscellaneous StructureSDR F3LA2016100400063Door Frame · crackedRIGHT EMERGENCY OVERWING EXIT FWD AND AFT I/B FRAME HAS INDICATIONS OF CRACKS. REMOVED AND REPLACED IAW SRM 51-42-11.Sep 22, 2016 · N939FR · Airbus A319112 · Fuselage Main, StructureSDR F3LA2016100400062Door Frame · crackedLEFT EMERGENCY OVERWING EXIT AFT INBD DOOR FRAME HAS INDICATIONS OF CRACKS. REMOVED AND REPLACED EMERGENCY EXIT AFT DOOR FRAME IAW SRM 51-42-11.Sep 20, 2016 · N939FR · Airbus A319112 · Fuselage Main, StructureSDR F3LA2016100400064Floor Support · corrodedAFT CABIN FRAME 66+10 THROUGH 68+6 Y1292 FLOOR SUPPORT TOP FLANGE CORRODED AT MULTIPLE LOCATIONS. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-42-11.Sep 19, 2016 · N939FR · Airbus A319112 · Fuselage Miscellaneous StructureSDR F3LA2016091900059Floorbeam · corrodedAFT CABIN, FRAME 66, Y508 FLOORBEAM CORRODED AT MULTIPLE LOCATIONS. REMOVE CORROSION MAXIMUM DEPTH OF REWORK IS .016, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-14, FIG 001. REMOVED OLD BEAM AT Y508, FR 66 IAW SRM 52-42-11. LOCATED & DRILLED NEW FLOORBEAM, INSSep 10, 2016 · N939FR · Airbus A319111 · Fuselage Main, Floor BeamSDR F3LA2016091900058Floorbeam · corrodedCORROSION ON FLOORBEAM Y1292, FASTENER HOLE BETWEEN FRAME 20 AND FRAME 18. R & R FLOORBEAM AT Y1292, FRAME 12-24 IAW SRM 51-72-11-911 AND SRM 51-21-11.Sep 10, 2016 · N939FR · Airbus A319111 · Fuselage Main, Floor BeamSDR F3LA2016091900057Floorbeam · corrodedCORROSION ON FLOORBEAM Y1292 BETWEEN FRAME 17 AND FRAME 20. R & R FLOORBEAM AT Y1292, FRAME 17 AND FRAME 20 IAW SRM 51-72-11, 51-42-11, 51-44-11.Sep 10, 2016 · N939FR · Airbus A319112 · Fuselage Main, Floor BeamSDR F3LA2016091900056Floorbeam · corrodedAFT CABIN FRAME 67-FRAME 68, Y765, FLOORBEAM TOP FLANGE CORRODED AT MULTIPLE LOCATIONS. R & R AFT CABIN FLOORBEAM Y765 AT FRAME 67-FRAME 68 IAW SRM 51-72-11.Sep 10, 2016 · N939FR · Airbus A319111 · Fuselage Main, Floor BeamSDR F3LA2014091101069Structure · corrodedC6 CHECK. PAX CABIN FROM FRAME 69 - 70 RT - Y1292 HAS SURFACE CORROSION AT FIVE EACH MULTIPLE FASTENERS HOLES AT SKIN PLATE. R & R SKIN PLATE IAW EO A0-53EO-31434, SRM 51-42-11 PAR 6B 3 A-D PAR 13D 1-4.Sep 11, 2014 · N939FR · Airbus A319112 · Fuselage Miscellaneous StructureSDR F3LA2014081801053Battery · dischargedEPSU EMER LIGHTS BATTERY 12WL FAILED CAPACITY TEST ON TASK CARD A332204-02. R & R THE EPSU BATTERY ASSEMBLY IAW AMM 33-51-38-000-002A & 33-51-38-400-002A.Aug 18, 2014 · N939FR · Airbus A319112 · Emergency LightingSDR F3LA2014020701005Slide · low pressureDOOR R2 SLIDE PRESS LOW. R & R R2 DOOR ESCAPE SLIDE IAW AMM 25-62-44 PB 401.Feb 7, 2014 · N939FR · Airbus A319112 · Escape SlideSDR F3LA2013062100868Bleed Air Sys · odorODOR IN CABIN AT LOW ALTITUDES, BOTH TAKEOFF AND APPROACH (AROUND 10,000' AGL) STRONG ODOR AROUND ROW 20-22. RAN APU, ENGINE NR 1 AND ENGINE NR 2 AND COULD NOT DETECT AN ODOR. R & R RECIRCULATION FILTERS REF AMM 21-21-45, PB401. ACFT NEEDS OPS CHECK FLIGHT TJun 17, 2013 · N939FR · Airbus A319111 · Engine Bleed Air SystemSDR F3LA2012121900822Power Supply · inoperativeC-CHECK, EMERGENCY LIGHT SYS TEST FAILED FOR FWD EPSU 10WL. R & R EPSU IAW AMM 33-51-38-020-051-A. SYSTEM OPS GOOD IAW 33-51-38-740-050-B.Dec 17, 2012 · N939FR · Airbus A319111 · Emergency LightingSDR F3LA2012082300778A/C Pack · smokeECAM MESSAGE NR 2 PACK OVERHEAT, ON DEPARTURE CLIMBING THROUGH 11,000 F/A CALLED WITH INFO ON SMOKE IN CABIN (AFT), ODOR WAS NOTABLE BUT DISSIPATING. EMERGENCY DECLARED AIR TURN BACK ON LANDING ROLL OUT, ECAM MESSAGE APPEARED, ACTIONS COMPLETED.Aug 21, 2012 · N939FR · Airbus A319111 · Cabin Cooling SystemSDR F3LA2011051900646Floorbeam · corrodedC-CHECK: NON ROUTINE NR 1287; CORROSION ON UPPER SURFACE OF RT AFT ENTRY AREA, FLOORBEAM AT FR 68, RBL 48, FOUND TO BE OUT OF LIMITS. R & R FLOORBEAM AT FR 68, RBL 48 IAW SRM 51-24-00, PARA 6.May 19, 2011 · N939FR · Airbus A319111 · Fuselage Main, Floor BeamSDR F3LA2011501900645Floor Panel · delaminatedC-CHECK: CABIN FLOOR PANEL 241JF HAS DELAMINATION IN SEVERAL AREAS AND FOUND TO BE OUT OF REPAIRABLE LIMITS. R & R FLOOR PANEL 241JF IAW SRM 53-02-00, PB 101.May 13, 2011 · N939FR · Airbus A319111 · Fuselage Floor PanelSDR F3LA201151900644Floor Support · corrodedC-CHECK: CORROSION ON UPPER SURFACE OF RT AFT ENTRY AREA, FLOORBEAM AT FR 68, RBL 30. R & R FLOORBEAM AT FR 66-70, RBL 30 IAW SRM 51-74-00.May 13, 2011 · N939FR · Airbus A319111 · Fuselage Miscellaneous StructureSDR F3LA201151900643Shear Plate · crackedC-CHECK: NON ROUTINE NR1262; LT AFT LATERAL SHEAR PLATE IS CRACKED, FR69, STR 24. REPLACED LT AFT LATERAL SHEAR PLATE WITH NEW CONFIGURATION IAW EO A0-53EO-31434 AND IAW SRM 51-42-11-1- A, B, C.May 13, 2011 · N939FR · Airbus A319111 · Fuselage Miscellaneous StructureSDR F3LA201151900642Floorboard · damagedC- CHECK: NON ROUTINE NR1329: COCKPIT FLOORBOARD, 211GF SURFACE IS DAMAGED. FOUND DAMAGE TO FLOORBOARD 211GF BEYOND REPAIRABLE LIMITS. REPLACED FLOORBOARD IAW SRM 53-12-00, DIAGRAM 101.May 13, 2011 · N939FR · Airbus A319111 · Fuselage Floor PanelSDR F3LA2010071800471Computer · faultedREF: PILOT REPORT LOG PAGE 549851 ITEM 1. CLIMBING THROUGH FLIGHT LEVEL 380 ELAC NR 2 FAULTED, ACFT WENT INTO ALTERNATE LAW. AIR TURN BACK TO SMF. REPLACED NR 2 ELAC REF AMM 27-93-34 PAGE BLOCK 401, OPS CHECK GOOD. PERFORMED LAND CATAGORY III CAPABILITIES TESJul 15, 2010 · N939FR · Airbus A319111 · Flight Control SystemSDR F3LA2009122800272Fitting · out of adjustDURING LANDING THE FLIGHT CREW NOTED THE L2 DOOR SLIDING ARMING LEVER DISARMS IN FLIGHT AND APPEARS RELATED TO CABIN PRESSURE DIFFERENTIAL ABOVE 10000 FEET. MX ADJUSTED ESCAPE SLIDE RELEASE MECHANISM AFT GIRT BAR FITTING ADJUSTED TO CORRECT CLEARANCES AND PERDec 25, 2009 · N939FR · Airbus A319111 · Emergency EquipmentSDR F3LA2009122800271Fitting · out of adjustDURING CRUISE ALTITUDE, THE FLIGHT CREW NOTED THE L2 DOOR ARM LIGHT WAS ON AND INTERMITTENT. MX ADJUSTED THE GIRT BAR FITTING FOR THE L2 DOOR AND PERFORMED A TEST OF THE EMERGENCY ESCAPE SLIDE RELEASE MECHANISM IAW AMM 52-13-22-820-056 AND AMM 52-73-00-710-050Dec 25, 2009 · N939FR · Airbus A319111 · Emergency EquipmentSDR F3LA2009122200259Wire · brokenDURING C3 C-CHECK INSP NOTED SEAT ROW 10B AND 10C EMERGENCY EXIT LIGHT WIRE WAS BROKEN AT CONNECTOR OTBD SEAT LEG GOING TO FLOOR. MX REMOVED AND REPLACED EMERGENCY EXIT WIRE HARNESS IAW AMM 25-21-41-000-001 STEP 4A(2)(B), AMM 25-21-41-400-001 STEP 4D(1)(C) ANDec 18, 2009 · N939FR · Airbus A319111 · Light System WiringSDR F3LA2009122300266Sill · corrodedDURING C3 C-CHECK INSP, NOTED THE L2 DOOR SILL CORRODED AT FWD SPLICE IN AND AROUND THE FLOORBOARD ATTACH HOLE. MX REPAIRED DOOR SILL IAW SRM 53-41-14 AND EA A9-53R-31579.Dec 17, 2009 · N939FR · Airbus A319111 · Fuselage Miscellaneous StructureSDR F3LA2009122300265Floor Panel · corrodedDURING C3 C-CHECK INSP, NOTED MAIN CABIN FLOOR PANEL 261FF HAS CORROSION. MX REMOVED AND REPLACED FLOOR PANEL 261FF IAW AMM 53-42-12-400-002.Dec 16, 2009 · N939FR · Airbus A319111 · Fuselage Floor PanelSDR F3LA2009122200261Floorbeam · corrodedDURING C3 C-CHECK INSP NOTED A HOLE IN FLOORBEAM Y1292 JUST AFT OF LAVATORY D FROM FRAME 64 TO FRAME 66 AND WAS ALSO CORRODED. MX REMOVED AND REPLACED FLOORBEAM Y1292 IAW SRM 51-42-11 AND SRM 51-44-11.Dec 16, 2009 · N939FR · Airbus A319111 · Fuselage Main, Floor BeamSDR F3LA2009122200260Shear Plate · corrodedDURING C3 C-CHECK INSP NOTED THE RT SHEAR PLATE FROM FRAME 69 TO FRAME 70 WAS CORRODED. MX REMOVED AND REPLACED SHEAR PLATE IAW SRM 51-42-11, SRM 51-44-11 AND SRM 51-21-00.Dec 16, 2009 · N939FR · Airbus A319111 · Fuselage Miscellaneous StructureSDR F3LA2009122400270Plate · corrodedDURING C3 C-CHECK INSP NOTED THE ARMED PLATE FOR THE R2 DOOR WAS CORRODED. MX REMOVED AND REPLACED ARM PLATE IAW AMM 53-42-12-420-051.Dec 15, 2009 · N939FR · Airbus A319111 · Fuselage Miscellaneous StructureSDR F3LA2009122300269Strip · corrodedDURING C3 C-CHECK INSPECTION, NOTED THE THRESHOLD STRIP FOR PANEL 262EF IS CORRODED. MX REMOVED AND REPLACED STRIP IAW AMM 53-42-12-400-002.Dec 15, 2009 · N939FR · Airbus A319111 · Fuselage Miscellaneous StructureSDR F3LA2009122300268Plate · corrodedDURING C3 C-CHECK INSPECTION, NOTED ARMED PLATE FOR L2 DOOR IS CORRODED. MX REMOVED AND REPLACED ARMED PLATE ON L2 DOOR THRESHOLD IAW AMM 20-21-11, PB 201.Dec 15, 2009 · N939FR · Airbus A319111 · Fuselage Miscellaneous StructureSDR F3LA2009122300267Threshold · corrodedDURING C3 C-CHECK INSP, NOTED THRESHOLD STRIP FOR L2 DOOR THRESHOLD IS CORRODED. MX REMOVED AND REPLACED THRESHOLD STRIP IAW AMM 53-42-12-400-001.Dec 15, 2009 · N939FR · Airbus A319111 · Fuselage Miscellaneous StructureSDR F3LA2009122200263Floor Support · corrodedDURING C3 C-CHECK INSP NOTED UPON REMOVAL OF THE AFT GALLEY FLOOR CORROSION WAS FOUND AT Y1292 FRAME 66 TO FRAME 69. MX REMOVED AND REPLACED FLOOR SUPPORT Y1292 AT FRAME 66 TO FRAME 69 RT SIDE IAW SRM 51-42-11, SRM 51-21-00 AND EA A9-53T-30392.Dec 15, 2009 · N939FR · Airbus A319111 · Fuselage Miscellaneous StructureSDR F3LA2009122200262Floor Support · corrodedDURING C3 C-CHECK INSP NOTED UPON REMOVAL OF THE AFT GALLEY FLOOR CORROSION WAS FOUND AT FLOOR SUPPORT Y1292 FROM FRAME 66 TO FRAME 69. MX REPLACED FLOOR SUPPORT Y1292 AT FRAME 66 TO FRAME 69 LT SIDE IAW SRM 51-42-11 AND SRM 51-44-11.Dec 15, 2009 · N939FR · Airbus A319111 · Fuselage Miscellaneous StructureSDR F3LA2009021900028Hmu · failedPILOT REPORTED THAT THE NR 2 ENGINE FAILED ON DESCENT FROM FL 350, THE ENGINE RECOVERED AND FURTHER DESCENT, APPROACH AND LANDING WERE UNEVENTFUL ON TWO ENGINES. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE HYDRO MECHANICAL UNIT AND PERFORMED SATISFACTORYFeb 18, 2009 · N939FR · Airbus A319111 · Fuel Control/Turbine EnginesSDR F3LA2008111000711Bushing · out of positionREFERENCE LOG PAGE 420725. PILOT REPORTED THE FORWARD ENTRY DOOR L1 GUST LOCK WILL NOT ENGAGE. MAINTENANCE REINSTALLED BUSHING IN THE FORWARD ENTRY DOOR GUST LOCK MECHANISM IN ACCORDANCE WITH A319 AMM 52-11-11-730-050.Nov 9, 2008 · N939FR · Airbus A319111 · Passenger/Crew DoorsSDR F3LA200800405Floorboard · damagedDURING C-CHECK INSP NOTED AFT CARGO PIT FWD FLOORBOARD PANEL 151PE HAS A HOLE AT THE AFT LT EDGE. MAINT REMOVED DAMAGED AREA AND FILLED DAMAGED AREA IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)Jun 28, 2008 · N939FR · Airbus A319111 · Fuselage Floor PanelSDR F3LA200800406Panel · damagedDURING C-CHECK INSP, NOTED AFT CARGO PIT AFT LT HAND TRANSITION PANEL 161BF HAS A HOLE AT AFT TOP END. MAINT REPAIRED AND INSTALLED SERVICEABLE PANEL 161BF IAW SRM 53-42-44-400-001. COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)Jun 28, 2008 · N939FR · Airbus A319111 · Fuselage Miscellaneous StructureSDR F3LA200800407Panel · damagedDURING C-CHECK INSP NOTED AFT CARGO PIT FWD LT HAND LOWER TRANSITION PANEL 151AE HAS A HOLE AT FWD LOWER END. MAINT REPAIRED AND INSTALLED SERVICEABLE PANEL 151AE IAW SRM 53-42-14-400-001. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. Jun 28, 2008 · N939FR · Airbus A319111 · Fuselage Miscellaneous StructureSDR F3LA200800402Panel · damagedDURING C-CHECK INSP, NOTED AFT CARGO PIT AFT RT UPPER TRANSITION PANEL 162CF HAS SEVERAL HOLES AT AFT END. MAINT REPAIRED TRANSITION PANEL 162CF IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)Jun 24, 2008 · N939FR · Airbus A319111 · Fuselage Miscellaneous StructureSDR F3LA200800401Panel · damagedDURING C-CHECK INSP NOTED AFT CARGO PIT AFT LT UPPER TRANSITION PANEL 161CF HAS HOLES IN SEVERAL PLACED. MAINT REPAIRED TRANSITION PANEL 161CF IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)Jun 24, 2008 · N939FR · Airbus A319111 · Fuselage Miscellaneous StructureSDR F3LA200800400Panel · damagedDURING C-CHECK INSP, NOTED AFT CARGO PIT FWD LT UPPER TRANSITION PANEL 151FE HAS A HOLE AT FWD TOP CORNER. MAINT REPAIRED TRANSITION PANEL 151FE IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)Jun 24, 2008 · N939FR · Airbus A319111 · Fuselage Miscellaneous Structure
Back to N939FR, cancelled Aug 22, 2022