N903FR, cancelled Feb 17, 2009

Service difficulty reports · 28

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 = 'N903FR' AND deregistration_id = 'N903FR-2009-02-17'
  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 F3LA200800587Power Supply · failedREFERENCE NON ROUTINE 104231. DURING EXIT CHECK, INSPECTION NOTED LT FORWARD EMERGENCY POWER SUPPLY UNIT FAILED EMERGENCY LIGHTS TEST. MX R&R LT FORWARD EMERGENCY POWER SUPPLY UNIT IN ACCORDANCE WITH THE REQUIREMENTS OF A319 AMM 33-51-38-400-001. UPON COMPLAug 25, 2008 · N903FR · Airbus A319112 · Emergency LightingSDR F3LA200800071Seal · corrodedDURING C5 C CHECK, MAINTENANCE REPORTED CORROSION FOUND ON RIGHT WING AILERON HINGE SEAL NEAR OUTBOARD HINGE LOCATION. MAINTENANCE REMOVED AND REPLACED AILERON SEAL IN ACCORDANCE WITH REQUIREMENTS OF A319 SRM 51-72-11 AND EA A9-57R-30062. TOUCH PAINTING PERFFeb 18, 2008 · N903FR · Airbus A319111 · AileronsSDR F3LA200800070Threshold · corrodedDURING C5 C CHECK, INSPECTION REPORTED LEVEL 1 CORROSION OF AFT CARGO PIT DOOR THRESHOLD AT EIGHTEEN (18) LOCATIONS AROUND ATTACHMENT HOLES AND ADJACENT TO THRESHOLD ITSELF. MAINTENANCE REMOVED CORROSION IN ACCORDANCE WITH REQUIREMENTS OF A319 SRM 51-74-00, PFeb 17, 2008 · N903FR · Airbus A319111 · Fuselage Miscellaneous StructureSDR F3LA200800057Profile · corrodedDURING C5 C CHECK, INSPECTION REPORTED CORROSION WAS FOUND ALONG THE ATTACHMENT HOLES OF THE AFT CARGO PIT PROFILE AT FRAME 58, FROM THE RIGHT TO THE LEFT SIDE. MAINTENANCE REMOVED AND REPLACED THE PROFILE, COMMON TO FRAME 58, IN ACCORDANCE WITH THE A319 AMM Feb 17, 2008 · N903FR · Airbus A319111 · Fuselage Miscellaneous StructureSDR F3LA200800056Profile · corrodedDURING A C5 C CHECK, INSPECTION REPORTED CORROSION WAS FOUND ALONG THE ATTACHMENT HOLES OF THE AFT CARGO PIT PROFILE AT FRAME 59, FROM THE RIGHT TO THE LEFT SIDE. MAINTENANCE REMOVED AND REPLACED THE PROFILE, COMMON TO FRAME 59, IN ACCORDANCE WITH THE A319 SRFeb 17, 2008 · N903FR · Airbus A319111 · Fuselage Miscellaneous StructureSDR F3LA200700047Connector · damagedMAINTENANCE REPORTED EPSU AFT L FAULTED. CLEANED AND INSPECTED PINS ON CONNECTOR TO EPSU AFT L POWER SUPPLY. PERFORMED EMERGENCY LIGHT TEST PER AMM 23-73-00-861-001 AND 33-51-38. OPS TEST GOOD.Apr 2, 2007 · N903FR · Airbus A319112 · Light System WiringSDR F3LA200600105Odor · detectedBLOCK TURNBACK IN CUN. FLIGHT ATTENDANTS REPORTED SMELL OF SMOKE IN FWD PASSENGER CABIN AREA (APPROXIMATELY ROW 6 AND FWD). MAINTENANCE PERFORMED INSPECTION OF AIRCRAFT MM 24-00-00-810-823. NO SMOKE ODOR OR DISCREPANCIES WERE FOUND. AIRCRAFT WAS RELEASED FSep 2, 2006 · N903FR · Airbus A319112 · Air Distribution SystemSDR F3LA200600102Epsu · failedDURING C-4 CHECK, INSPECTION REPORTED MID CABIN EPSU FAILED CAPACITY TEST. REPLACED 11WL MID CABIN EPSU. OPS CHECK GOOD IAW AMM 33-51-38, PB401.Aug 24, 2006 · N903FR · Airbus A319112 · Emergency LightingSDR F3LA200600101Battery Pack · failedDURING C-4 CHECK, INSPECTION REPORTED LT. MID CABIN EPSU 12WL FAILED CAPACITY TEST. REPLACED BATTERY PACK 12WL. OPS CHECK NORMAL IAW AMM 33-51-38, PB 401.Aug 24, 2006 · N903FR · Airbus A319112 · Emergency LightingSDR F3LA200600100Epsu · failedDURING C-4 CHECK, INSPECTION REPORTED FWD EMERGENCY POWER SUPPLY UNIT (EPSU) FAILED EMERGENCY LIGHTS CAPACITY TEST. REPLACED EPSU 10WL. OPS CHECK NORMAL PER AMM 33-51-38, PB 401.Aug 24, 2006 · N903FR · Airbus A319112 · Emergency LightingSDR F3LA200600095Slat Track · damagedDURING C-4 CHECK, INSPECTION REPORTED LT WING, NR 1 SLAT I/B SLAT TRACK CUTOUT DAMAGED. REMOVED DAMAGED AREAS AND PERFORMED HFEC INSPECTION. NO FAULTS OR CRACKS NOTED. APPLIED ALODINE TREATMENT EPOXY PRIMER AND PAINT TO AFFECTED AREAS. REFERENCE A319 SRM 5Aug 18, 2006 · N903FR · Airbus A319112 · Leading Edge DevicesSDR F3LA200600092Valve · corrodedLEFT HAND CABIN PRESSURE SAFETY VALVE (7HL) POSITION SWITCH STICKS AND IS CORRODED. NEW VALVE WAS INSTALLED PER AMM 21-31-52-400-001. BONDING CHECK PERFORMED ON BONDING STRAP PER AMM 20-28-00-912-004. CHECK WAS GOOD.Aug 18, 2006 · N903FR · Airbus A319112 · Cabin Pressure Control SystemSDR F3LA200600094Threshold · corrodedDURING C-4 CHECK, INSPECTION REPORTED MINOR CORROSION ON R1 DOOR THRESHOLD STRIP. FOUND R1 DOOR THRESHOLD STRIP TO BE OUT OF LIMITS PER SRM 51-70-00. FABRICATED AND INSTALLED REPLACEMENT R1 DOOR SILL COVER PER AIRBUS DWG B5 D53610197, SRM 51-27-00, SRM 51-44Aug 15, 2006 · N903FR · Airbus A319112 · Fuselage Miscellaneous StructureSDR F3LA200600093Threshold · corrodedDURING C-4 CHECK, INSPECTION REPORTED MINOR CORROSION ON L1 DOOR THRESHOLD STRIP. FOUND L1 DOOR THRESHOLD STRIP TO BE OUT OF LIMITS PER SRM 51-70-00. FABRICATED AND INSTALLED REPLACEMENT L1 DOOR SILL COVER PER AIRBUS DWG B5 D53610197, SRM 51-27-00, SRM 51-44Aug 15, 2006 · N903FR · Airbus A319112 · Fuselage Miscellaneous StructureSDR F3LA200600089Floor Support · corrodedFLOORBEAM FROM 68-69 LT SIDE, JUST INSIDE L-2 DOOR WAS CORRODED. NEW FLOORBEAM AND SPLICE ANGLE INSTALLED PER A319 SRM 51-42-11.Aug 10, 2006 · N903FR · Airbus A319112 · Fuselage Miscellaneous StructureSDR F3LA200600099Seat Track · corrodedDURING C-4 CHECK, INSPECTION REPORTED AFT FUSELAGE CABIN FLOOR STRUCTURE FR66, Y1292, CORRODED UNDER NUT CLIPS. BURNISHED CORROSION ON SEAT TRACK/STRUCTURE AT FR66 PER SRM 53-00-15, FIG 101, SECTION E-E, PAGES 101-104. UPON FURTHER INVESTIGATION, MORE CORROSAug 9, 2006 · N903FR · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR F3LA200600098Beam · corrodedDURING C-4 CHECK, INSPECTION REPORTED CORROSION AND HOLE THROUGH Y254 BEAM AT FR20 FWD ENTRY CENTER. FOUND CORRODED AREA TO BE OUT OF LIMITS PER SRM 53-11-14, FIG 104. CUT OUT AND REMOVED CORRODED SECTION FROM TOP FLANGE OF FLOOR SUPPORT PER SRM 53-11-14, FIAug 9, 2006 · N903FR · Airbus A319112 · Fuselage Main, StructureSDR F3LA200600097Floor Support · corrodedDURING C-4 CHECK, INSPECTION REPORTED LT SIDE FLOOR SUPPORT STRINGER NUT CLIPS AND NUT PLATES FOR ATTACHMENT OF FLOOR AND TRANS PANELS IN FWD CARGO COMPARTMENT CORRODED. REMOVED LT SIDE FLOOR SUPPORT STRINGER (TRANSITION PLATE) BETWEEN FR28 AND FR30 PER A319 Aug 9, 2006 · N903FR · Airbus A319112 · Fuselage Miscellaneous StructureSDR F3LA200600096Dummy Rail · corrodedDURING C-4 CHECK, INSPECTION REPORTED CORROSION IN FWD LAV AREA, FR16 AND Y503.2. DUMMY RAIL WAS FOUND TO BE OUT OF LIMITS PER SRM 53-11-14. REMOVED CORRODED DUMMY RAIL PER SRM 51-42-11. LOCATED AND DRILLED NEW DUMMY RAIL PER SRM 51-44-11 AND AIRBUS DWG B2 Aug 9, 2006 · N903FR · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR F3LA200600091Switch · corrodedRIGHT HAND CABIN PRESSURE SAFETY VALVE (GHL) FAILED OPERATION TEST. POSITION SWITCH WAS CORRODED. NO OPEN INDICATION ON ECAM. VALVE WAS REPLACED PER AMM 21-31-52-400-001.Aug 8, 2006 · N903FR · Airbus A319112 · Cabin Pressure Control SystemSDR F3LA200600090Guide Vane · crackedENGINE NR 1, 14 OUTLET GUIDE VANES DOUBLERS WERE CRACKED AND WERE OUT OF LIMITS. REPAIRED AND REPLACED PER AMM 72-23-00-400-008.Aug 6, 2006 · N903FR · Airbus A319112 · Turbine Engine Air Inlet SectionSDR F3LA200600011Engine · bird ingestionBIRD STRIKE TO NR 2 ENGINE ON APPROACH TO MKE. DUE TO N1/N2 ROLLBACK, DAMAGE WAS SUSPECTED AND AGENT NR 1 FIRE BOTTLE WAS DISCHARGED. AN EMERGENCY WAS DECLARED AND AIRCRAFT LANDED WITHOUT INCIDENT. A BORESCOPE OF THE NR 2 ENGINE WAS PERFORMED AND MAJOR DAMAMar 22, 2006 · N903FR · Airbus A319112 · Engine (Turbine/Turboprop)SDR F3LA200500041Fitting · corrodedINSPECTION REPORTED CORROSION IN FWD BORE FROM 4 O'CLOCK TO 7 O'CLOCK LT WING, RIB 5, LANDING FITTING. BORED OUT CORROSION PER SRM 57-26-13.Sep 7, 2005 · N903FR · Airbus A319112 · Wing, Landing Gear Attach FittingsSDR F3LA200500040Fitting · corrodedINSPECTION REPORTED CORROSION ON FWD FACE, FWD LUG, LT WING RIB 5, LANDING GEAR FITTING. MACHINED CORROSION ON LUG FACE PER SRM 57-26-13.Sep 7, 2005 · N903FR · Airbus A319112 · Wing, Landing Gear Attach FittingsSDR F3LA200500039Fitting · corrodedINSPECTION REPORTED CORROSION ON AFT FACE, FWD LUG, LT WING LANDING FITTING, RIB 5. MACHINED CORROSION PER SRM 57-26-13.Sep 7, 2005 · N903FR · Airbus A319112 · Wing, Landing Gear Attach FittingsSDR F3LA200500038Coffeemaker · odorAIR DIVERSION, SMOKE SMELL IN AFT GALLEY. DECLARED AN EMERGENCY. MX PERFORMED TSM TASK 24-00-00-810-823, FOUND AFT NR 2 COFFEEMAKER C/B'S POPPED ON REAR OF COFFEEMAKER. REMOVED AFT NR 1 COFFEEMAKER & INSTALLED INTO NR 2 POSITION, OPS NORMAL. NO ARCING OR DAug 15, 2005 · N903FR · Airbus A319112 · Buffet/GalleysSDR F3LA200500005Smoke · detectedON INBOUND TAXI, FLIGHT CREW REPORTED SMOKE IN CABIN. RAN ENGINES PER AMM 71-00-00-710-006. CYCLED AIR CONDITIONING PACKS. RAN APU. CYCLED APU BLEED AIR. INSPECTED CARGO BINS, E/E BAYS AND CABIN FOR SMOKE. NO FAULTS NOTED, COULD NOT DUPLICATE DISCREPANCYFeb 17, 2005 · N903FR · Airbus A319112 · Air Distribution SystemSDR F3LA200300126Skin · dentedDURING WALKAROUND, MAINTENANCE FOUND TWO SMALL DENTS AFT AND EVEN WITH FORWARD ENTRY DOOR, APPROXIMATELY 3 FT. AFT OF DOOR AT STA. 950, STR. 22L. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR IAW EA A9-53R-10127 AND SRM 53-00-11.Sep 6, 2003 · N903FR · Airbus A319111 · Fuselage Main, Plate/Skin
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