# Service difficulty reports: N216AG, cancelled May 7, 2022 A list on [N216AG, cancelled May 7, 2022](https://openairdocs.org/deregistered/N216AG-2022-05-07.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR SWIA2018051544683](https://openairdocs.org/sdr/SWIA2018051544683.md): Angle · corroded · Apr 27, 2018 · N216AG · Cndair CL6002C10 · Fuselage Miscellaneous Structure > SERVICE DOOR LOWER SILL ANGLE HAS SEVERAL SPOTS OF CORROSION. REMOVED AND REPLACED THE DOOR LOWER SILL ANGLE IAW SRM. - [SDR SWIA2018051544682](https://openairdocs.org/sdr/SWIA2018051544682.md): Door Sill · corroded · Apr 25, 2018 · N216AG · Cndair CL6002C10 · Fuselage Miscellaneous Structure > GALLEY SERVICE DOOR SURROUND STRUCTURE, LOWER SILL HAS CORROSION BEHIND FWD AND AFT FITTINGS. INSTALLED A NEW DOOR SILL IAW SRM. - [SDR SWIA2018051544681](https://openairdocs.org/sdr/SWIA2018051544681.md): Window Frame · cracked · Apr 23, 2018 · N216AG · Cndair CL6002C10 · Fuselage Main, Structure > INTERNAL 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. - [SDR SWIA2018051544680](https://openairdocs.org/sdr/SWIA2018051544680.md): Channel · corroded · Apr 22, 2018 · N216AG · Cndair CL6002C10 · Fuselage Miscellaneous Structure > CORROSION FOUND ON TCAS OMNIDIRECTIONAL ANTENNA CHANNEL BETWEEN BS 295 - 310, STRINGER 27. REMOVED AND REPLACED THE CHANNEL IAW SRM. - [SDR SWIA2018051544679](https://openairdocs.org/sdr/SWIA2018051544679.md): Stringer · corroded · Apr 22, 2018 · N216AG · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer > CORROSION FOUND ON STRINGER 26L BETWEEN BS 295 - 310 AROUND THE STAND OFF. REPLACED THE STRINGER. - [SDR SWIA2018051544678](https://openairdocs.org/sdr/SWIA2018051544678.md): Frame · corroded · Apr 22, 2018 · N216AG · Cndair CL6002C10 · Fuselage Main, Frame > CORROSION FOUND ON THE FRAME AT BS 319.7, BETWEEN STRINGERS 26L AND 26R. REPLACED THE FRAME SECTION IAW REO. - [SDR SWIA2018051544677](https://openairdocs.org/sdr/SWIA2018051544677.md): Stringer · corroded · Apr 22, 2018 · N216AG · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer > CORROSION FOUND ON STRINGER 27 BETWEEN BS 319.7 AND 333. REMOVED AND REPLACED THE STRINGER SECTION IAW SRM. - [SDR SWIA2018051544676](https://openairdocs.org/sdr/SWIA2018051544676.md): Intercostal · corroded · Apr 22, 2018 · N216AG · Cndair CL6002C10 · Fuselage Miscellaneous Structure > CORROSION FOUND ON THE INTERCOSTAL BETWEEN BS 349 - 364 STRINGER 27R. REPLACED THE INTERCOSTAL IAW SRM. - [SDR SWIA201540899](https://openairdocs.org/sdr/SWIA201540899.md): Bracket · cracked · Mar 2, 2015 · N216AG · Cndair CL6002C10 · Wing, Attach Fittings > WELDED 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 ROLLE - [SDR SWIA201540898](https://openairdocs.org/sdr/SWIA201540898.md): Floor Support · corroded · Mar 1, 2015 · N216AG · Cndair CL6002C10 · Fuselage Miscellaneous Structure > RIGHT 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 - [SDR SWIA201540897](https://openairdocs.org/sdr/SWIA201540897.md): Floor Support · corroded · Mar 1, 2015 · N216AG · Cndair CL6002C10 · Fuselage Miscellaneous Structure > RIGHT 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. SUBM - [SDR SWIA201540896](https://openairdocs.org/sdr/SWIA201540896.md): Floor Support · corroded · Mar 1, 2015 · N216AG · Cndair CL6002C10 · Fuselage Miscellaneous Structure > RIGHT 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 S - [SDR SWIA201440426](https://openairdocs.org/sdr/SWIA201440426.md): Frame · cracked · Dec 18, 2014 · N216AG · Cndair CL6002C10 · Fuselage Main, Frame > FRAME BS 220 CRACKED. REPAIRED IAW SRM. - [SDR SWIA201440425](https://openairdocs.org/sdr/SWIA201440425.md): Frame · cracked · Dec 18, 2014 · N216AG · Cndair CL6002C10 · Fuselage Main, Frame > FRAME BS 235 CRACKED. REPAIRED IAW SRM. - [SDR SWIA201440424](https://openairdocs.org/sdr/SWIA201440424.md): Frame · cracked · Dec 18, 2014 · N216AG · Cndair CL6002C10 · Fuselage Main, Frame > BS 235 FRAME CRACKED. REPAIRED IAW SRM. - [SDR SWIA2014112540165](https://openairdocs.org/sdr/SWIA2014112540165.md): Frame · cracked · Nov 18, 2014 · N216AG · Cndair CL6002C10 · Fuselage Main, Frame > BS 220 FRAME FOUND CRACKED. REPAIRED IAW SRM. - [SDR SWIA2014112540164](https://openairdocs.org/sdr/SWIA2014112540164.md): Frame · cracked · Nov 18, 2014 · N216AG · Cndair CL6002C10 · Fuselage Main, Frame > FOUND BS 235 FRAME TO BE CRACKED. REPAIRED THE FRAME IAW SRM. - [SDR SWIA2014112540163](https://openairdocs.org/sdr/SWIA2014112540163.md): Frame · cracked · Nov 18, 2014 · N216AG · Cndair CL6002C10 · Fuselage Main, Frame > BS 235 FRAME CRACKED. REPAIRED IAW SRM. - [SDR SWIA201439243](https://openairdocs.org/sdr/SWIA201439243.md): Battery Pack · failed · Sep 3, 2014 · N216AG · Cndair CL6002C10 · Emergency Lighting > NR 3 ELBP DOESN'T HOLD A CHARGE. R & R NR 3 BATTERY PACK IAW AMM. OPS CHECKED GOOD. - [SDR SWIA201437807](https://openairdocs.org/sdr/SWIA201437807.md): Connector · failed · May 24, 2014 · N216AG · Cndair CL6002C10 · Light System Wiring > EMERGENCY LIGHT POD NR 5 IS INOPERATIVE. RESECURED EMERGENCY LIGHT ELECTRICAL CONNECTOR. - [SDR SWIA201335138](https://openairdocs.org/sdr/SWIA201335138.md): Channel · corroded · Oct 31, 2013 · N216AG · Cndair CL6002C10 · Wing Miscellaneous Structure > TE 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. - [SDR SWIA201335139](https://openairdocs.org/sdr/SWIA201335139.md): Seat Track · corroded · Oct 29, 2013 · N216AG · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings > REPLACE 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. - [SDR SWIA201335141](https://openairdocs.org/sdr/SWIA201335141.md): Hinge · chafed · Oct 13, 2013 · N216AG · Cndair CL6002C10 · Passenger/Crew Doors > PAX DOOR PIANO HINGE DOOR CHAFED. C-CHECK BLENDED CHAFE ON PAX DOOR PIANO HINGE DOOR SIDE IAW REO. - [SDR SWIA201335140](https://openairdocs.org/sdr/SWIA201335140.md): Hinge · chafed · Oct 13, 2013 · N216AG · Cndair CL6002C10 · Passenger/Crew Doors > PAX DOOR PIANO HINGE FS CHAFED. C-CHECK BLENDED CHAFE ON PAX DOOR LUGS FS SIDE IAW REO. - [SDR SWIA201335144](https://openairdocs.org/sdr/SWIA201335144.md): Crossbeam · cracked · Oct 11, 2013 · N216AG · Cndair CL6002C10 · Fuselage Miscellaneous Structure > FS280.00 CROSSBEAM CRACKED AT LBL 11. C-CHECK REPAIR TO BE ACCOMPLISHED IAW SERVICE BULLETIN. - [SDR SWIA201335143](https://openairdocs.org/sdr/SWIA201335143.md): Fitting · chafed · Oct 11, 2013 · N216AG · Cndair CL6002C10 · Landing Gear Doors > RT MLG DOOR CHAFED. C-CHECK REPLACED RT MLG DOOR FITTING IAW REO & SRM. - [SDR SWIA201335142](https://openairdocs.org/sdr/SWIA201335142.md): Fitting · chafed · Oct 11, 2013 · N216AG · Cndair CL6002C10 · Landing Gear Doors > LT MLG DOOR CHAFED. C-CHECK REPLACED LT MLG DOOR FITTING IAW REO & SRM. - [SDR SWIA201333176](https://openairdocs.org/sdr/SWIA201333176.md): Light · inoperative · Apr 3, 2013 · N216AG · Cndair CL6002C10 · Emergency Lighting > NR 4 REAR EMERGENCY OVERHEAD LIGHT IS BURNED OUT. (FLT 3454) RELAMPED EMERGENCY LIGHT. - [SDR SWIA201232466](https://openairdocs.org/sdr/SWIA201232466.md): Light · inoperative · Dec 26, 2012 · N216AG · Cndair CL6002C10 · Emergency Lighting > ROW 7 EMERGENCY OVERHEAD LIGHT BURNED OUT. (FLT 3471) RELAMPED EMERGENCY LIGHT. - [SDR SWIA201230788](https://openairdocs.org/sdr/SWIA201230788.md): Wire · disconnected · May 23, 2012 · N216AG · Cndair CL6002C10 · Light System Wiring > EXIT SIGN OVER SERVICE DOOR DOES NOT ILLUMINATE WHEN TESTING EMERGENCY LIGHTS. (FLT 3459) CONNECTED WIRE AT SPLICE IN REFERENCE TO AMM. - [SDR SWIA201230202](https://openairdocs.org/sdr/SWIA201230202.md): Light · inoperative · Mar 25, 2012 · N216AG · Cndair CL6002C10 · Emergency Lighting > NR 4 OVERHEAD EMERGENCY LIGHT IS OUT. (SERVICE) RELAMPED EMERGENCY LIGHT. - [SDR SWIA201128908](https://openairdocs.org/sdr/SWIA201128908.md): Light · inoperative · Dec 15, 2011 · N216AG · Cndair CL6002C10 · Emergency Lighting > AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 3451) RELAMPED EMERGENCY LIGHT. - [SDR SWIA201128397](https://openairdocs.org/sdr/SWIA201128397.md): Connector · disconnected · Oct 21, 2011 · N216AG · Cndair CL6002B19 · Light System Wiring > SERVICE DOOR EMERGENCY EXIT LIGHT IS OUT. (FLT 3477) RECONNECTED SERVICE DOOR EMERGENCY LIGHT CONNECTOR. - [SDR SWIA201127740](https://openairdocs.org/sdr/SWIA201127740.md): Light · inoperative · Sep 14, 2011 · N216AG · Cndair CL6002C10 · Emergency Lighting > AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 3471) RELAMPED EMERGENCY LIGHT. - [SDR SWIA201127702](https://openairdocs.org/sdr/SWIA201127702.md): Light · inoperative · Sep 13, 2011 · N216AG · Cndair CL6002C10 · Emergency Lighting > OVERHEAD EMERGENCY LIGHT OVER ROW 16 BURNED OUT. (FLT 3482) RELAMPED EMERGENCY LIGHT. ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql 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 ``` This list as a web page: https://openairdocs.org/deregistered/N216AG-2022-05-07/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.