N216AG, cancelled May 7, 2022

Service difficulty reports · 35

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 = 'N216AG' AND deregistration_id = 'N216AG-2022-05-07'
  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 SWIA2018051544683Angle · corrodedSERVICE DOOR LOWER SILL ANGLE HAS SEVERAL SPOTS OF CORROSION. REMOVED AND REPLACED THE DOOR LOWER SILL ANGLE IAW SRM.Apr 27, 2018 · N216AG · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA2018051544682Door Sill · corrodedGALLEY SERVICE DOOR SURROUND STRUCTURE, LOWER SILL HAS CORROSION BEHIND FWD AND AFT FITTINGS. INSTALLED A NEW DOOR SILL IAW SRM.Apr 25, 2018 · N216AG · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA2018051544681Window Frame · crackedINTERNAL STRUCTURE OF THE FLIGHT CONTROL COMPARTMENT CANOPY RIGHT SIDE HAS A FRAME CRACKED. REMOVED AND REPLACED THE FRAME ON THE WINDSHIELD SUPPORT CANOPY STRUCTURE IAW SRM.Apr 23, 2018 · N216AG · Cndair CL6002C10 · Fuselage Main, StructureSDR SWIA2018051544680Channel · corrodedCORROSION FOUND ON TCAS OMNIDIRECTIONAL ANTENNA CHANNEL BETWEEN BS 295 - 310, STRINGER 27. REMOVED AND REPLACED THE CHANNEL IAW SRM.Apr 22, 2018 · N216AG · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA2018051544679Stringer · corrodedCORROSION FOUND ON STRINGER 26L BETWEEN BS 295 - 310 AROUND THE STAND OFF. REPLACED THE STRINGER.Apr 22, 2018 · N216AG · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SWIA2018051544678Frame · corrodedCORROSION FOUND ON THE FRAME AT BS 319.7, BETWEEN STRINGERS 26L AND 26R. REPLACED THE FRAME SECTION IAW REO.Apr 22, 2018 · N216AG · Cndair CL6002C10 · Fuselage Main, FrameSDR SWIA2018051544677Stringer · corrodedCORROSION FOUND ON STRINGER 27 BETWEEN BS 319.7 AND 333. REMOVED AND REPLACED THE STRINGER SECTION IAW SRM.Apr 22, 2018 · N216AG · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SWIA2018051544676Intercostal · corrodedCORROSION FOUND ON THE INTERCOSTAL BETWEEN BS 349 - 364 STRINGER 27R. REPLACED THE INTERCOSTAL IAW SRM.Apr 22, 2018 · N216AG · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA201540899Bracket · crackedWELDED ANGLE BRACKET IN LT FUEL TANK AT SLAT 1-3 ROLLER BOX IS CRACKED AT TOP AND BOTTOM OF BRACKET, MARKED. C-CHECK, ANGLE BRACKET IN LT FUEL TANK AT SLAT 1-3, ROLLER BOX REPAIRED REF STS EA. COMPLIED WITH VISUAL CHECK OF THE LT WING FUEL TANK SLAT 1-3 ROLLEMar 2, 2015 · N216AG · Cndair CL6002C10 · Wing, Attach FittingsSDR SWIA201540898Floor Support · corrodedRIGHT FLOOR SILL IS CORRODED AT FS 777. C-CHECK, RO 3/13/15, REMOVED CORROSION ON RT FLOOR SILL AT FS 777.00, REF SRM. REMAINING MATERIAL THICKESS IS .126" IAW NDT. NO MATERIAL LOST. RESTORED FINISH TO A023 REF SRM BECAUSE THIS WAS IN A NO DAMAGE AREA IAW Mar 1, 2015 · N216AG · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA201540897Floor Support · corrodedRIGHT FLOOR SILL IS CORRODED AT FS 769. C-CHECK, REMOVED CORROSION ON RT FLOOR SILL AT FS 769.00, REF SRM. REMAINING MATERIAL THICKESS IS .126" IAW NDT. NO MATERIAL LOST. RESTORED FINISH TO A023, REF SRM. BECAUSE THIS WAS IN A NO DAMAGE AREA IAW SRM. SUBMMar 1, 2015 · N216AG · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA201540896Floor Support · corrodedRIGHT FLOOR SILL IS CORRODED AT FS 711.00. C-CHECK, REMOVED CORROSION ON RT FLOOR SILL REF SRM. REMAINING MATERIAL THICKESS IS .129" IAW NDT. NO MATERIAL LOST. RESTORED FINISH TO A023 REF SRM. BECAUSE THIS WAS IN A NO DAMAGE AREA IAW SRM, SUBMITTED TO SMar 1, 2015 · N216AG · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA201440426Frame · crackedFRAME BS 220 CRACKED. REPAIRED IAW SRM.Dec 18, 2014 · N216AG · Cndair CL6002C10 · Fuselage Main, FrameSDR SWIA201440425Frame · crackedFRAME BS 235 CRACKED. REPAIRED IAW SRM.Dec 18, 2014 · N216AG · Cndair CL6002C10 · Fuselage Main, FrameSDR SWIA201440424Frame · crackedBS 235 FRAME CRACKED. REPAIRED IAW SRM.Dec 18, 2014 · N216AG · Cndair CL6002C10 · Fuselage Main, FrameSDR SWIA2014112540165Frame · crackedBS 220 FRAME FOUND CRACKED. REPAIRED IAW SRM.Nov 18, 2014 · N216AG · Cndair CL6002C10 · Fuselage Main, FrameSDR SWIA2014112540164Frame · crackedFOUND BS 235 FRAME TO BE CRACKED. REPAIRED THE FRAME IAW SRM.Nov 18, 2014 · N216AG · Cndair CL6002C10 · Fuselage Main, FrameSDR SWIA2014112540163Frame · crackedBS 235 FRAME CRACKED. REPAIRED IAW SRM.Nov 18, 2014 · N216AG · Cndair CL6002C10 · Fuselage Main, FrameSDR SWIA201439243Battery Pack · failedNR 3 ELBP DOESN'T HOLD A CHARGE. R & R NR 3 BATTERY PACK IAW AMM. OPS CHECKED GOOD.Sep 3, 2014 · N216AG · Cndair CL6002C10 · Emergency LightingSDR SWIA201437807Connector · failedEMERGENCY LIGHT POD NR 5 IS INOPERATIVE. RESECURED EMERGENCY LIGHT ELECTRICAL CONNECTOR.May 24, 2014 · N216AG · Cndair CL6002C10 · Light System WiringSDR SWIA201335138Channel · corrodedTE PANEL 581AB MOUNTING GANG CHANNEL IS CORRODED & BROKEN. C-CHECK R & R GANG CHANNEL PN B0204044-3-12-6M PO NR T000024490 FOR TE PANEL 581AB IAW SRM.Oct 31, 2013 · N216AG · Cndair CL6002C10 · Wing Miscellaneous StructureSDR SWIA201335139Seat Track · corrodedREPLACE RT SIDE SEAT TRACK FS457-00 TO 483.00, SEAT TRACK CORRODED. C-CHECK REPLACED RT SIDE SEAT TRACK AT FS457.00 TO FS 483.00 IAW SRM & REO.Oct 29, 2013 · N216AG · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA201335141Hinge · chafedPAX DOOR PIANO HINGE DOOR CHAFED. C-CHECK BLENDED CHAFE ON PAX DOOR PIANO HINGE DOOR SIDE IAW REO.Oct 13, 2013 · N216AG · Cndair CL6002C10 · Passenger/Crew DoorsSDR SWIA201335140Hinge · chafedPAX DOOR PIANO HINGE FS CHAFED. C-CHECK BLENDED CHAFE ON PAX DOOR LUGS FS SIDE IAW REO.Oct 13, 2013 · N216AG · Cndair CL6002C10 · Passenger/Crew DoorsSDR SWIA201335144Crossbeam · crackedFS280.00 CROSSBEAM CRACKED AT LBL 11. C-CHECK REPAIR TO BE ACCOMPLISHED IAW SERVICE BULLETIN.Oct 11, 2013 · N216AG · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA201335143Fitting · chafedRT MLG DOOR CHAFED. C-CHECK REPLACED RT MLG DOOR FITTING IAW REO & SRM.Oct 11, 2013 · N216AG · Cndair CL6002C10 · Landing Gear DoorsSDR SWIA201335142Fitting · chafedLT MLG DOOR CHAFED. C-CHECK REPLACED LT MLG DOOR FITTING IAW REO & SRM.Oct 11, 2013 · N216AG · Cndair CL6002C10 · Landing Gear DoorsSDR SWIA201333176Light · inoperativeNR 4 REAR EMERGENCY OVERHEAD LIGHT IS BURNED OUT. (FLT 3454) RELAMPED EMERGENCY LIGHT.Apr 3, 2013 · N216AG · Cndair CL6002C10 · Emergency LightingSDR SWIA201232466Light · inoperativeROW 7 EMERGENCY OVERHEAD LIGHT BURNED OUT. (FLT 3471) RELAMPED EMERGENCY LIGHT.Dec 26, 2012 · N216AG · Cndair CL6002C10 · Emergency LightingSDR SWIA201230788Wire · disconnectedEXIT SIGN OVER SERVICE DOOR DOES NOT ILLUMINATE WHEN TESTING EMERGENCY LIGHTS. (FLT 3459) CONNECTED WIRE AT SPLICE IN REFERENCE TO AMM.May 23, 2012 · N216AG · Cndair CL6002C10 · Light System WiringSDR SWIA201230202Light · inoperativeNR 4 OVERHEAD EMERGENCY LIGHT IS OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.Mar 25, 2012 · N216AG · Cndair CL6002C10 · Emergency LightingSDR SWIA201128908Light · inoperativeAFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 3451) RELAMPED EMERGENCY LIGHT.Dec 15, 2011 · N216AG · Cndair CL6002C10 · Emergency LightingSDR SWIA201128397Connector · disconnectedSERVICE DOOR EMERGENCY EXIT LIGHT IS OUT. (FLT 3477) RECONNECTED SERVICE DOOR EMERGENCY LIGHT CONNECTOR.Oct 21, 2011 · N216AG · Cndair CL6002B19 · Light System WiringSDR SWIA201127740Light · inoperativeAFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 3471) RELAMPED EMERGENCY LIGHT.Sep 14, 2011 · N216AG · Cndair CL6002C10 · Emergency LightingSDR SWIA201127702Light · inoperativeOVERHEAD EMERGENCY LIGHT OVER ROW 16 BURNED OUT. (FLT 3482) RELAMPED EMERGENCY LIGHT.Sep 13, 2011 · N216AG · Cndair CL6002C10 · Emergency Lighting
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