N935FR, cancelled Apr 12, 2017
Service difficulty reports · 31
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 = 'N935FR' AND deregistration_id = 'N935FR-2017-04-12' 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.
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 = 'N935FR' AND deregistration_id = 'N935FR-2017-04-12' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR F3LA2016062100051Engine · shutdownDURING CRUISE FLIGHT THE CREW NOTED, ECAM ENGINE 2 STALL WHICH WAS SOON FOLLOWED BY ENGINE 2 SHUTDOWN. THE CREW DECLARED EMERGENCY LANDING. MAINTENANCE R & R NR 2 ENGINE. REF WC MP71042-01 AND MP71042-02, REMOVAL AND INSTALLATION CARDS.
OPS CHECK GOOD.SDR F3LA2015040601127Unknown · malfunctionedFLAP JAM AT SLAT ONLY, FLAPS LOCKED. PERFORMED BITE TEST OF SFCC IAW AMM 27-51-00-740-002-A. PERFORMED 2 FULL FLAPS & SLATS CYCLES, NO DEFECTS NOTED. PERFORMED VISUAL INSPECTION OF THE FLAPS & SLATS, NO DEFECTS NOTED LP 893710.SDR F3LA2015020401104Battery Pack · dischargedLEFT EPSU BATTERY FAILS TEST. REPLACED LT EPSU IAW AMM 33-51-38 PB 401. OPERATIONS CHECKED NORMAL. LOG PAGE 843284.SDR F3LA2014082001054Battery · dischargedEPSU BATTERY 12WL FAILED THE TEST ON THE HEAVY SERVICE CHECK. R & R EPSU BATTERY 12WL IAW AMM 33-51-38-000-002-A & 33-51-38-400-002 A.SDR F3LA2014012700956Battery Pack · defectiveEMERGENCY LIGHT FAULT EPSU AFT LT & NO GREEN SYS OK LIGHT UPON TESTING. R & R AFT LT EPSU BATTERY IAW AMM 33-51-38 PB 401, OPERATIONS CHECKED GOOD.SDR F3LA2013121900951Wire Harness · brokenAIRCRAFT OUT OF SERVICE DUE TO C6 CHECK. EMERGENCY LIGHTING WIRING AT SEAT ROW 25L IS BROKEN. R & R EMERGENCY LIGHTING WIRING HARNESS IAW AMM 33-51-19. OPERATIONS CHECKED GOOD IAW AMM 33-51-00-710-001-A AT SEAT ROW 25L.SDR F3LA2011061400656Door · openLP 540215: AIR TURN BACK, FWD CARGO DOOR OPEN AFTER TAKEOFF "OVERWEIGHT LANDING". PLACED THE CARGO DOOR ON MEL 52-70-01H MDDR 1083274 AND PERFORMED INSPECTION RTS 1715 MCI LOCAL TIME.SDR F3LA2011020400598Line · leakingA/C REPORT LP NR605872: GREEN HYD SYS RESERVOIR LOW QUANTITY. GRAVITY EXTENSION OF LANDING GEAR APPARENT FLUID LEAKING FROM NR 1 ENGINE. UPON FURTHER INSP FOUND HYD LOW PRESSURE SWITCH TUBE LEAKING. REMOVED IN REF WITH AMM 29-11-49-000-005 AND INSTALLED HYDSDR F3LA2010072500515Floor Panel · damagedC-CHECK NON ROUTINE N0479, 6 EACH INSERTS PULLED OUT WITH SKIN DAMAGE. REPAIRED THE SKIN DAMAGE AT 6 EACH HOLE LOCATIONS USING PATCH METHOD IAW A319 SRM 53-02-00 PARA 8 A. INSTALLED INSERTS IAW AIRBUS PMS 01-05-72 PARA 5.SDR F3LA2010072500514Epsu · inoperativeC-CHECK NON ROUTINE N0769, L-1 AND R-1 LOWER DOOR INTERIOR EMERGENCY LIGHTS ARE INOP. REMOVED AND REPLACED EPSU ON (10WL) AND TEST GOOD IAW A319 AMM 33-51-38-PB 401.SDR F3LA2010072500513Panel · puncturedC-CHECK NON ROUTINE N0473, AFT CARGO FLOOR PANEL 151VG HAS 7 PUNCTURES. FABRICATED AND REPLACEMENT PANEL IAW MCG IRM 9701 REV G.SDR F3LA2010072500512Floor Panel · damagedC-CHECK NON ROUTINE N0649, AFT CARGO FLOOR PANEL 151FE HAS COMPOSITE DAMAGE ON BOTH SIDES. REPAIRED COMPOSITE DAMAGE IAW A319 SRM 53-02-00 PARA 5.SDR F3LA2010072500511Floor Panel · puncturedC-CHECK NON ROUTINE N0507, AFT CARGO FLOOR PANEL 151UG HAS 2 PUNCTURES AND 4 EACH DAMAGED PREVIOUS REPAIRS. FABRICATED AND REPLACED PANEL IAW MCG IRM 9701 REV G.SDR F3LA2010072500510Support · corrodedC-CHECK NON ROUTINE N0413, FRAME SUPPORT FROM 69 TO 70 STRINGER 23R BELOW SHEAR PLATE HAS 2 AREAS OF CORROSION TOTALING 2 SQUARE INCHES. REMOVED AND REPLACED FRAMES SUPPORT IAW A319 SRM 51-42-11 PARA 6 AND 7.SDR F3LA2010072500509Floor Panel · puncturedC-CHECK NON ROUTINE N0479, AFT CARGO FLOOR PANEL 151PE HAS A 2 EACH PUCTURES. REPAIR USING GLASS CLOH WET LAYUP IAW A319 SRN 53-00 PARA 8 B.SDR F3LA2010072500508Seat Track · corrodedC-CHECK: NON ROUTINE N0494, AFT CABIN SEAT TRACK Y1292 AT FRAME 68L HAS 2 AREAS OF CORROSION UPPER SURFACE. CORROTIONS OUT OF LIMITS IAW A319 SRM 53-00-14 FIG 102. REMOVED AND REPLACED SEAT TRACK Y1292 BETWEEN FRAMES 68L AND 69L.SDR F3LA2010072500507Panel · puncturedC-CHECK: NON ROUTINE AFT CARGO TRANSITION PANEL 151AE HAS 6 PUNCTURES. FABRICATED REPLACEMENT PANEL IAW MCG IRM 9701 PARA 13 REVISION G.SDR F3LA2010072500506Floorbeam · corrodedC-CHECK: NON ROUTINE N0410, AFT MAIN CABIN FLOORBEAM Y1292 AT FRAME 68R HAS 2 AREAS OF CORROSION. REMOVED AND REPLACED FLOORBEAM - Y1292 FROM FRAME 68R TO FRAME 69R IAW A319 SRM 51-42-11 PARA 7.SDR F3LA2010072500505Plate · corrodedC-CHECK: NON ROUTINE 0414, AFT CARGO DOORS SILL SHEET HAS 4 AREAS OF CORROSION MEASURING 4.5 SQUARE INCHES TOTAL. REMOVED CORROSION IAW A319 SRM 51-74-00 PARA 5.A (3). ALL AREAS WITHIN LIMITS IAW A319 SRM 51-73-11 PARA 1. B RE-PROTECTED AREAS IAW A319 SRM 51SDR F3LA2010072500504Battery · dischargedC-CHECK: NON ROUTINE N0074, FWD MEGAPHONE INOPERATIVE. REPLACED BATTERIES IN THE MEGAPHONE IAW A319 AMM 25-65-51-920-001. MEGAPHONE STILL INOPERATIVE, REMOVED AND REPLACED MEGAPHONE IAW A319 AMM 25-65-920-001 AND AMM 25-64-51-010-050 PARA. B (3) AND AMM 25-6SDR F3LA2010072500503Floor Panel · debondedC-CHECK: NON ROUTINE N0384, CABIN FLOOR PANEL 251AF DISBONDED. REPAIRED DISBOND ON FLOOR PANEL 251AF IAW A319 SRM 53-02-00 PARA 8. A, (2) FIG. 204.SDR F3LA2010072500502Floor Panel · debondedC-CHECK: NON ROUTINE N0383, CABIN FLOOR PANEL 252SF DISBONDED. REPAIRED DISBONDED SKIN AREA ON THE FLOOR PANEL 252SF USING FILLER METHOD. REPAIRED DISBONDED IAW A319 SRM 53-02-00 PARA 8. A, (2) FIG. 204.SDR F3LA2009080300124Control Unit · defectiveCREW MADE AN AIR RETURN, DUE TO THE ALTITUDE SELECTOR KNOB ON THE FLIGHT CONTROL UNIT BEING STUCK ON AN ALTITUDE, RENDERING THE AUTO-PILOT, AUTO-THRUST AND FLIGHT DIRECTORS TO AN UNAVAILABLE STATE. MX REMOVED AND REPLACED THE FLIGHT CONTROL UNIT AND PERFORMED SDR F3LA2009020900024Sill · corrodedDURING C3 C-CHECK, INSPECTION NOTED THE LEFT GALLEY FLOOR STRUCTURE AT FRAME 66 HAS TWO NUT PLATE HOLES CORRODED AFT OF GIRT BAR FITTING ADAPTER PLATE. MAINTENANCE TRIMMED OUT DAMAGED AREA, FABRICATED REPAIR ANGLE AND FILLER AND INSTALLED IN REFERENCE TO ENGISDR F3LA2009020900023Sill · corrodedDURING C3 C-CHECK, INSPECTION NOTED THE L2 DOOR SILL BEAM HAS TWO CORRODED NUT PLATE HOLES AT FRAME 68. MAINTENANCE TRIMMED OUT DAMAGED AREA, FABRICATED REPAIR ANGLE AND INSTALLED IAW SRM 53-41-14 FIGURE 201.SDR F3LA2009020900022Floorbeam · corrodedDURING C3 C-CHECK, INSPECTION NOTED THE LEFT AFT GALLEY FLOORBEAM Y1292 HAS CORROSION AROUND FASTENER HOLES BETWEEN FRAME 67 AND FRAME 68. MAINTENANCE REMOVED AND REPLACED FLOORBEAM IAW SRM 51-42-11, PARAGRAPHS 5 AND 7.SDR F3LA2009020900021Floor Panel · corrodedDURING C3 C-CHECK, INSPECTION NOTED FLOOR PANEL 262FF HAS CORROSION. MAINTENANCE REMOVED AND REPLACED FLOOR PANEL PER TASK CARD C534103-2.SDR F3LA200800275Coffeemaker · odorREFERENCE LOG PAGES 369125 AND 369126. DURING FLIGHT THE FA REPORTED A STRONG ODOR AND HEAT. MAINT RAN APU AND ENGINE (1) AND (2) AT IDLE WITH BOTH PACKS ON. MAINT VISUALLY INSPECTED CARGO PITS, FWD AVIONICS COMPARTMENTS AND FUSELAGE, AFT OF PRESSURE BULKHEADSDR F3LA200800001Flap System · out of alignmentDURING THE APPROACH, THE FLIGHT CREW RECEIVED AN ECAM MESSAGE THAT THE FLIGHT CONTROLS - FLAPS - WERE LOCKED DUE TO AN ALIGNMENT FAULT. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED UNEVENTFULLY. MAINTENANCE RESET THE WING TIP BREAK IN ACCORDANCE WITH AMSDR F3LA200700199Support Beam · corrodedDURING C-2 CHECK, INSPECTION REPORTED FR C-20 TOP SUPPORT BEAM IN LT FWD ELECTRICAL EQUIPMENT COMPARTMENT FRETTING. FOUND FITTING TO BE OUT OF LIMITS IAW AIRBUS DRAWING D53113988. PERFORMED HFEC OF FR C-20 INBD SUPPORT BEAM LUG ON NLG WHEEL WELL UPPER AFT LTSDR F3LA200600008Control System · failedDURING C-1 CHECK, MAINTENANCE REPORTED RT OVERWING EMERGENCY EXIT FAILED FUNCTION TEST (PER WORK CARD C522101-3, EMERGENCY ESCAPE SYSTEM FAILURE). ADJUSTED RT OVERWING EMERGENCY EXIT FLEXIBLE CONTROL ASSY IAW AMM 25-62-43-820-050. PERFORMED OPERATIONAL CHECK
Back to N935FR, cancelled Apr 12, 2017