N650AW
Service difficulty reports · 367
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 = 'N650AW' 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.
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 = 'N650AW' AND registry_match = 'registration' 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 AWXA200301161Floorbeam · corrodedMCN - MAJOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON Y1162 FLOORBEAM BETWEEN FR 68 AND FR 69. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED DAMAGED SECTION OF Y1162 FLOORBEAM FROM FR 68 TO FR 69; FABRISDR AWXA200301160Floor Support · corrodedDURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON THE UPPER SURFACE OF Y765 FLOOR SUPPORT AT FR 16. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED DAMAGED SECTION OF Y765 FLOOR SUPPORT FROM FR 12 TO FR 16; FABRICATED A NSDR AWXA200301159Floor Support · corrodedDURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON THE UPPER AND LOWER SURFACE OF UPPER LEG OF Y1162 LONGITUDINAL BEAM FR 68-69. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED Y1162 BEAM FROM FR 68 TO FR 69; FABRICATED A SDR AWXA200301155Floorbeam · corrodedDURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON UPPER SURFACE OF Y254 FLOORBEAM AT FR 20. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS, CUT OUT CORRODED SECTION OF Y254 FLOORBEAM AT FR 20; FABRICATED A FILLER AND 2 EACH REPAISDR AWXA200301154Track · corrodedMCN - MAJOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON AFT END OF Y503 DUMMY RAIL AT FR 16. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS, REMOVED AND REPLACED Y503 DUMMY RAIL AT FR 16 IAW A320 SRM 51-42-11 PG 23SDR AWXA200301153Plate · corrodedDURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON THE OUTBOARD RT AFT SHEAR PLATE AT Y1292, FORWARD OF FR 70. MAINTENANCE REMOVED CORRODED RT AFT SHEAR PLATE AT Y1292, FABRICATED A NEW REPLACEMENT SHEAR PLATE; INSTALLED REPAIR PART IAW A320 SRM 51-42-11 PGSDR AWXA200301152Floor Panel · corrodedDURING C-04 CHECK CORROSION WAS FOUND ON CABIN FLOOR PANEL 262FF. MAINTENANCE REMOVED AND REPLACED CORRODED CABIN FLOOR PANEL 262FF IAW AWA T/C C1D25310, ZONE 1D.SDR AWXA200301151Bracket · corrodedMCN - MINOR REPAIR - DURING C-04 CHECK CORROSION WAS FOUND ON FLOOR PANEL BRACKET (CONNECTING PLATE) AT Y1162. MAINTENANCE REMOVED CORRODED FLOOR PANEL CONNECTING PLATE AT Y1162, FABRICATED AND INSTALLED A NEW REPLACEMENT CONNECTING PLATE PER DWG D53670099. SDR AWXA200301150Floor Panel · corrodedDURING C-04 CHECK CORROSION WAS FOUND ON FLOOR PANEL TIE STRAP (CONNECTING PLATE) FROM Y765 TO Y254 AT FR 24. MAINTENANCE REMOVED CORRODED CONNECTING PLATE FROM Y765 TO Y254 AT FR 24, FABRICATED AND INSTALLED A NEW REPLACEMENT CONNECTING PLATE PER DWG D536700SDR AWXA200301166Skin · corrodedDURING C-04 CHECK PITTING CORROSION WAS FOUND ON THE NR 1 PYLON AFT FIXED FAIRING INBOARD SKIN AT LOWER AFT AREA. MAINTENANCE REMOVED NR 1 PYLON AFT FIXED FAIRING INBOARD SKIN; FABRICATED A NEW REPLACEMENT SKIN; INSTALLED REPAIR PART IAW A320 SRM 51-42-11 PG SDR AWXA200301168Seat Track · corrodedMCN - MAJOR REPAIR - DURING C-04 CHECK CORROSION WAS FOUND ON FORWARD END OF RT OUTBOARD PASSENGER SEAT TRACK AT Y1292, FR 12 TO FR 24. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED DAMAGED SECTION OF SEAT TRACK Y1292 FROMSDR AWXA200301164Floor Panel · corrodedDURING C-04 CHECK CORROSION WAS FOUND ON FLOOR PANEL 261 FF. MAINTENANCE REMOVED DAMAGED PORTION OF FLOOR PANEL; CLEANED AND PREPARED SURFACE; APPLIED FIBERGLASS BOND REPAIR IAW A320 SRM 53-02-00 PG 208-211 FIG 203.SDR AWXA200300584Control Unit · malfunctionedON TAKEOFF AT LAS EN ROUTE FOR CMH WITH THRUST SET TO FLEX, NR 2 WENT TO TOGA, AND NR 1 WENT TO FLEX OR REDUCED SETTING (10 O'CLOCK ON GAUGE). HAD ECAM MESSAGE NO FLEX TEMP SET, BUT FLEX WAS SET AT IDLE. UPPER ECAM POWER INDICATOR VARIED FROM TOGA TO CLIMB WISDR AWXA200201187Warning System · false activationEMERGENCY LANDING - FLT 0273 - ON APPROACH INTO IAH EN ROUTE FROM PHX SELECTED FLAP 3 WHEN RECEIVED ECAM FLIGHT CONTROL FLAPS FAULT ALONG WITH A FLIGHT CONTROL SLAT FAULT. CONFERRED WITH MAINTENANCE CONTROL AND FOLLOWED ECAM PROCEDURES, RECYCLED FLAPS FROM 2 TSDR AWXA200200595Computer · defectiveFLT 0185 - ON TAKEOFF ROLL THE NR 2 FLIGHT WARNING COMPUTER (FWC) FAULTED, REJECTED TAKEOFF AT LESS THAN 80 KTS. MAINTENANCE PLACED SYSTEM ON MEL 31-53-01, FOR FWC NR 2 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 2 FWC IAW AMM 31-52-00-0001. AIRCRSDR AWXA0001108Wire · brokenEMERGENCY LIGHT AT ROW 26 DID NOT ILLUMINATE DURING TEST. REPAIRED BROKEN WIRE AT SEAT 26 LEFTSDR AWXA0000333Apu · contaminatedCABIN HAD A MILD OILY SMELL ON THE TOP OF DESCENT WITH LOW POWER SETTINGS (HP VALVE OPEN). WASHED APU IAW CARD Z6D49301 AND F6D49303. RECOMMENDATION: MONITOR.
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