N910FR

Service difficulty reports · 87

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 = 'N910FR' 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 F3LA2010072700518Support · corrodedC-CHECK: NON ROUTINE N0449; UPON REMOVAL OF AFT CABIN LT SHEAR PLATE AT FRAME 68L TO 69L FOUND SUPPORT CORRODED. A/C IN C-CHECK CORROSION OUT OF LIMITS. REMOVED AND REPLACED SUPPORT IAW A319 SRM 51-72-11 PARA 1-7.Oct 8, 2010 · N910FR · Airbus A319112 · Fuselage Miscellaneous StructureSDR F3LA2010072700517Plenum · crackedPILOT REPORT: PACK NR 1 PRODUCING SMOKE AND FUMES AFTER NR 1 ENGINE START. AIRCRAFT RETURNED TO BLOCK, REMOVED AND REPLACED NR 1 PACK PLENUM CHAMBER, IAW AMM 21-52-22 PB 401.Oct 7, 2010 · N910FR · Airbus A319112 · Cabin Cooling SystemSDR F3LA2009050500085Battery Pack · failedDURING C5 C-CHECK, INSPECTION NOTED THAT THE EMERGENCY POWER SUPPLY UNIT AT POSITION 13WL FAILED THE CAPACITY CHECK. MAINTENANCE REMOVED FAILED BATTERY AND INSTALLED NEW, REFERENCE AMM 33-51-38-400-002. MAINTENANCE PERFORMED SATISFACTORY OPERATIONAL TEST, REApr 29, 2009 · N910FR · Airbus A319112 · Emergency LightingSDR F3LA2008121600725Unknown · smokePILOT REPORTED THAT THE DEICING CREW STARTED DEICING THE AIRCRAFT BEFORE CONTACT WITH THE COCKPIT CREW. SMOKE FILLED COCKPIT AND MID-CABIN. AN ALARM WAS RECEIVED FROM THE PARTICLE SENSORS IN THE AFT AND FORWARD CARGO AREA. PILOT TURNED OFF THE APU BLEED ANDDec 13, 2008 · N910FR · Airbus A319112 · Smoke DetectionSDR F3LA2008102700685Power Supply · failedLINE MAINTENANCE NOTED THAT MULTIPLE EMERGENCY LIGHTS FAILED TO ILLUMINATE IN CABIN. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY POWER SUPPLY UNIT AT POSITION 11WL IN ACCORDANCE WITH AMM 33-51-38-400-001. ALL EMERGENCY LIGHTS WORK NORMALLY.Oct 27, 2008 · N910FR · Airbus A319112 · Emergency LightingSDR F3LA200700301Uplock Hook · damagedDURING C4/S1 CHECK, INSPECTION REPORTED THAT UPON INSTALLATION OF THE L2 DOOR SLIDE, THE L2 DOOR HANDLE COULD BE MOVED INTO THE CLOSED POSITION BEFORE THE DOOR WAS IN THE HOLE. REMOVED AND REPLACED L2 DOOR UP-LOCK HOOK IAW 52-11-21-400-001, SUBTASK AMM 52-11-Oct 29, 2007 · N910FR · Airbus A319112 · Escape SlideSDR F3LA200700294Floor Support · corrodedDURING C4/S1 CHECK, INSPECTION REPORTED FLOORBEAM Y254 CORRODED ON UPPER SURFACE BETWEEN FRAMES 16 AND 18. FABRICATED AND INSTALLED FLOOR SUPPORT REPAIR PARTS IAW SRM 53-11-14, 51-47-00, 51-23-00, 51-75-12, 51-44-11, EAR 910-4551, AND EA A9-53R-12224.Oct 19, 2007 · N910FR · Airbus A319112 · Fuselage Miscellaneous StructureSDR F3LA200700292Floor Panel · corrodedDURING C4/S1 CHECK, INSPECTION REPORTED FLOOR PANEL 262FF CORRODED ON BOTTOM SIDE. REMOVED AND REPLACED FLOOR PANEL 262FF IAW WORK CARD CP753-36 AND AMM 53-42-12-PB401.Oct 19, 2007 · N910FR · Airbus A319112 · Fuselage Floor PanelSDR F3LA200700288Dummy Rail · corrodedDURING C4/S1 CHECK, INSPECTION REPORTED FLOORBEAM Y503.2 CORRODED ON UPPER SURFACE BETWEEN FRAMES 14 AND 16. DETERMINED CORROSION ON DUMMY RAIL Y503.2 TO BE OUT OF LIMITS IAW A319 SRM 53-11-14, FIG 106. REMOVED AND INSTALLED DUMMY RAIL Y503.2 IAW 51-42-11, AOct 19, 2007 · N910FR · Airbus A319112 · Fuselage Main, StructureSDR F3LA200700304Support · corrodedDURING C4/S1 CHECK, INSPECTION REPORTED SUPPORT FRAME AT FR70 CORRODED ON UNDERSIDE AT NUTPLATE CUTOUT, WHICH WAS FOUND AFTER REMOVAL OF THE SHEAR WEB. REMOVED SUPPORT FRAME AT LT SIDE OF FR70 IAW A319 SRM 51-42-11. DETERMINED TO BE OUT OF LIMITS IAW SRM 53-Oct 18, 2007 · N910FR · Airbus A319112 · Fuselage Miscellaneous StructureSDR F3LA200700299Blanking Plate · corrodedDURING C4/S1 CHECK, INSPECTION REPORTED CORROSION ON L1 DOOR GIRT BAR FITTING AFT BLANKING PLATE. REMOVED AND REPLACED L1 DOOR AFT GIRT BAR BLANKING PLATE IAW AMM 53-11-31-PB401.Oct 18, 2007 · N910FR · Airbus A319112 · Escape SlideSDR F3LA200700298Blanking Plate · corrodedDURING C4/S1 CHECK, INSPECTION REPORTED CORROSION ON L2 DOOR GIRT BAR FITTING BLANKING PLATE. REMOVED AND REPLACED L2 DOOR BLANKING PLATE IAW AMM 53-11-31-PB401.Oct 18, 2007 · N910FR · Airbus A319112 · Escape SlideSDR F3LA200700297Blanking Plate · corrodedDURING C4/S1 CHECK, INSPECTION REPORTED CORROSION ON R1 DOOR GIRT BAR FITTING AFT BLANKING PLATE. REPLACED R1 DOOR AFT GIRT BAR FITTING BLANKING PLATE IAW AMM 53-11-31-PB401.Oct 18, 2007 · N910FR · Airbus A319112 · Passenger/Crew DoorsSDR F3LA200700291Nut Plate · corrodedDURING C4/S1 CHECK, INSPECTION REPORTED CORROSION IN THE AFT OTBD NUTPLATE HOLE OF THE L2 DOOR SILL FWD GIRT BAR FITTING MOUNT PLATE. PERFORMED ROTO PROBE INSPECTION ON HOLE IAW NTM 51-10-01, PAGES 601-622 AND AND FOUND A CRACK BETWEEN RIVET HOLE AND FASTENEROct 18, 2007 · N910FR · Airbus A319112 · Fuselage Miscellaneous StructureSDR F3LA200700290Nut Plate · corrodedDURING C4/S1 CHECK, INSPECTION REPORTED CORROSION IN THE AFT OTBD NUTPLATE HOLE OF THE R2 DOOR SILL FWD GIRT BAR FITTING MOUNT PLATE. PERFORMED HFEC ON DAMAGED AREA IAW NTM 51-10-08, PAGES 601-608, AND FOUND NO DEFECTS. FABRICATED AND INSTALLED REPAIR DOUBLEOct 18, 2007 · N910FR · Airbus A319112 · Fuselage Miscellaneous StructureSDR F3LA200700313Support · corrodedDURING C4/S1 CHECK, INSPECTION REPORTED CORROSION AT FLOOR WEB NUTPLATE IN FWD CARGO COMPARTMENT, AFT RT CORNER, WHERE TRANSITION PANEL, AFT CARGO WALL AND FLOOR MEET. REMOVED CORRODED TRANSITION STRIP AT AFT BULKHEAD IAW SRM 51-42-11, PARA. 6. INSTALLED NEWOct 17, 2007 · N910FR · Airbus A319112 · Fuselage Miscellaneous StructureSDR F3LA200700312Floorbeam · corrodedDURING C4/S1 CHECK, INSPECTION REPORTED FLOORBEAM BETWEEN FRAME 68R AND 69R CORRODED. BLENDED CORRODED AREA AND FOUND FLOORBEAM TO BE OUT OF LIMITS IAW SRM 53-00-14, FIG 102. REMOVED AND INSTALLED FLOORBEAM IAW SRM'S 51-42-11, 51-44-00, AND 51-72-11.Oct 17, 2007 · N910FR · Airbus A319112 · Fuselage Main, Floor BeamSDR F3LA200700309Floor Panel · corrodedDURING C4/S1 CHECK, INSPECTION REPORTED FLOOR PANEL 222FF CORRODED ON LOWER SURFACE, FWD EDGE. REMOVED AND REPLACED FLOOR PANEL IAW AMM 53-12-12-PB401 AND WORK CARD CP753-12.Oct 17, 2007 · N910FR · Airbus A319112 · Fuselage Floor PanelSDR F3LA200700308Floor Panel · corrodedDURING C4/S1 CHECK, INSPECTION REPORTED FLOOR PANEL 221FF CORRODED ON LOWER SURFACE, FWD EDGE. REMOVED AND REPLACED FLOOR PANEL 221FF IAW AIRBUS AMM 53-12-12-400-001, 53-12-12-PB401, AND WORK CARD CP753-12.Oct 17, 2007 · N910FR · Airbus A319112 · Fuselage Floor PanelSDR F3LA200700307Floorbeam · corrodedDURING C4/S1 CHECK, INSPECTION REPORTED CABIN FLOORBEAM AT FR 69 RT CORRODED IN NUTPLATE HOLE. REMOVED AND REPLACED FLOORBEAM IAW SRM 53-00-14, FIG. 102, 51-42-11 AND 51-72-11.Oct 17, 2007 · N910FR · Airbus A319112 · Fuselage Main, Floor BeamSDR F3LA200700306Sill · corrodedDURING C4/S1 CHECK, INSPECTION REPORTED CORROSION IN R2 DOOR SILL NUTPLATE HOLE AT FR 66. BLENDED MATERIAL AT FWD END OF R2 DOOR SILL AND FOUND TO BE OUT OF LIMITS IAW SRM 53-41-14, FIG. 101. FABRICATED REPAIR FILLER IAW SRM 53-41-14, FIG. 201, REPAIR PRINCIOct 17, 2007 · N910FR · Airbus A319112 · Fuselage Miscellaneous StructureSDR F3LA200700305Floor Support · corrodedDURING C4/S1 CHECK, INSPECTION REPORTED FLOORBEAM BETWEEN FR 68 AND FR 69 AT Y1292, INBD AND AFT OF L1 DOOR FRAME, CORRODED. REMOVED AND REPLACED FLOORBEAM IAW SRM 51-42-11, PARA 7.Oct 17, 2007 · N910FR · Airbus A319112 · Fuselage Miscellaneous StructureSDR F3LA200700303Threshold · corrodedDURING C4/S1 CHECK, INSPECTION REPORTED L1 DOOR THRESHOLD STRIP CORRODED ON LOWER SURFACE. REMOVED AND REPLACED L1 DOOR THRESHOLD STRIP IAW AMM 53-12-12-400-001.Oct 17, 2007 · N910FR · Airbus A319112 · Fuselage Miscellaneous StructureSDR F3LA200700300Blanking Plate · corrodedDURING C4/S1 CHECK, INSPECTION REPORTED CORROSION ON R2 DOOR FWD AND AFT GIRT BAR PADS. REMOVED AND REPLACED FWD AND AFT R2 DOOR GIRT BAR BLANKING PLATES IAW AMM 52-13-31-PB401 AND 52-13-31-400-007.Oct 17, 2007 · N910FR · Airbus A319112 · Escape SlideSDR F3LA200700296Web · corrodedDURING C4/S1 CHECK, INSPECTION REPORTED CORROSION AT FWD CARGO COMPARTMENT FLOOR WEB NUTPLATES, RT SIDE WHERE TRANSITION PANEL AND FLOOR MEET, BETWEEN FR 28 AND FR 29. REMOVED AND REPLACED CORRODED TRANSITION STRIP IAW SRM 51-42-11 AND 51-44-11.Oct 17, 2007 · N910FR · Airbus A319112 · Escape SlideSDR F3LA200700295Web · corrodedDURING C4/S1 CHECK, INSPECTION REPORTED CORROSION AT FLOOR WEB NUTPLATE IN FWD CARGO COMPARTMENT AT FR 28, 6" INBD OF C1 DOOR CUTOUT. REMOVED AND REPLACED TRANSITION STRIP IAW SRM 51-42-11, 51-72-11 AND 51-21-11.Oct 17, 2007 · N910FR · Airbus A319112 · Fuselage Miscellaneous StructureSDR F3LA200700289Floorbeam · corrodedDURING C4/S1 CHECK, INSPECTION REPORTED FLOORBEAM AT FR67R CORRODED IN NUTPLATE HOLES. REMOVED AND REPLACED FLOORBEAM IAW SRM 51-42-11, PARA 5, AND 71-72-11.Oct 17, 2007 · N910FR · Airbus A319112 · Fuselage Main, Floor BeamSDR F3LA200700293Threshold · corrodedDURING C4/S1 CHECK, INSPECTION REPORTED R1 DOOR THRESHOLD STRIP CORRODED ON LOWER SURFACE. REMOVED AND REPLACED R1 DOOR THRESHOLD STRIP IAW MM 53-12-12-400-001.Oct 17, 2007 · N910FR · Airbus A319112 · Fuselage Main, Plate/SkinSDR F3LA200700287Shear Web · corrodedDURING C4/S1 CHECK, INSPECTION REPORTED SHEAR WEB AT FR 70L CORRODED. REMOVED AND REPLACED SHEAR PLATE IAW SRM 51-42-11 AND 51-72-11.Oct 17, 2007 · N910FR · Airbus A319112 · Fuselage Miscellaneous StructureSDR F3LA200700286Support · corrodedDURING C4/S1 CHECK, INSPECTION REPORTED SHEAR WEB AND SUPPORT PLATE AT FR70R BLOWN OUT FROM CORROSION. REMOVED AND REPLACED SHEAR PLATE SUPPORT IAW SRM 51-42-11, PARAGRAPHS 6, 7, AND 77, AND DWG D53474180.Oct 17, 2007 · N910FR · Airbus A319112 · Fuselage Miscellaneous StructureSDR F3LA200700302Wire Harness · damagedDURING C4/S1 CHECK, INSPECTION REPORTED R1 DOOR SLIDE ELECTRICAL HARNESS CAME FROM THE FACTORY PINCHED IN THE SLIDE ASSY, AND CANNOT BE ROUTED AS SHOWN IN AMM FIG 25-62-44-911-003, SHEET 404.2/3. REMOVED AND REPLACED DAMAGED R1 DOOR SLIDE IAW AMM 25-62-44-400Oct 16, 2007 · N910FR · Airbus A319112 · Equipment/Furnishings WiringSDR F3LA200700311Floorbeam · corrodedDURING C4/S1 CHECK, INSPECTION REPORTED CORROSION ON UPPER SURFACE OF FLOORBEAM Y254, BETWEEN FRAMES 16 AND 18. BLENDED 3 AREAS ON FLOOR SUPPORT Y254, ALL FOUND TO BE OUT OF LIMITS PER SRM 53-11-14-FIG 104. CUT OUT CORRODED UPPER CAP SECTION OF FLOOR SUPPORTOct 15, 2007 · N910FR · Airbus A319112 · Fuselage Main, Floor BeamSDR F3LA200700310Skin · dentedDURING C4/S1 CHECK, INSPECTION REPORTED A SMALL DENT IN THE LT FUSELAGE AT FR 15, STR30, AFT AND ABOVE 02 SERVICE DOOR. REMOVED PAINT FROM AREA IAW SRM 51-75-11 AND BLENDED AREA IAW SRM 51-73-00. DEPTH OF DENT IS .007, SIZE OF DENT IS .4" WIDE BY .5" LONG, 1Oct 15, 2007 · N910FR · Airbus A319112 · Fuselage Main, Plate/SkinSDR F3LA200600019Slide · inoperativeDURING C-3 CHECK, INSPECTION REPORTED LT AFT EPSU INDICATED EXTERNAL FAULT ON PTP DURING OPERATIONAL CHECK OF EMERGENCY LIGHTS AT L2 DOOR/ESCAPE SLIDE. REPLACED SLIDE RAFT ASSY AT L2 DOOR.Apr 25, 2006 · N910FR · Airbus A319112 · Emergency LightingSDR F3LA200600018Support · corrodedDURING C-3 CHECK, INSPECTION REPORTED SURFACE CORROSION ON SUPPORT CHANNEL FOR R-1 THRESHOLD AT ATTACH HOLE. BLENDED CORROSION ON SUPPORT CHANNEL, TREATED, PRIMED AND PAINTED PER EA A9-53R-11365.Apr 19, 2006 · N910FR · Airbus A319112 · Fuselage Miscellaneous StructureSDR F3LA200500017Smoke · detectedFLIGHT ATTENDANTS AND PASSENGERS REPORTED ODOR OF SMOKE ON FLIGHT FROM MZT TO DEN. FLIGHT CREW DECLARED AN EMERGENCY AND DIVERTED TO ELP. AIRCRAFT LANDED WITHOUT INCIDENT. TROUBLESHOT SMOKE IN CABIN PER MM 26-17-00-810-804, LAV SMOKE WARNING, NO DEFECTS NOTApr 25, 2005 · N910FR · Airbus A319112 · Air Distribution SystemSDR F3LA200400001Fan Blade · bentDURING CLIMBOUT, FLIGHT CREW REPORTED ABNORMAL NR 2 ENGINE NOISE (NO ABNORMAL ENGINE VIBRATION). FOUND FAN BLADES BENT DUE TO ICE INGESTION. REPLACED NR 2 ENGINE FAN BLADES PER MM 72-21-00-300-028, PERFORMED NR 2 ENGINE TRIM BALANCE PER MM 77-32-34-750-001 AJan 25, 2004 · N910FR · Airbus A319111 · Turbine Engine Compressor Section
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