# Service difficulty reports: N215AG, cancelled May 7, 2022

A list on [N215AG, cancelled May 7, 2022](https://openairdocs.org/deregistered/N215AG-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.

Page 1 of 2 · 71 reports

- [SDR SWIA201642056](https://openairdocs.org/sdr/SWIA201642056.md): Door Sill · corroded · Mar 26, 2016 · N215AG · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > THE SERVICE DOOR LOWER SILL ANGLE HAS CORROSION. NEW LOWER SILL ANGLE FOR THE SERVICE DOOR INSTALLED IAW SRM.
- [SDR SWIA201642055](https://openairdocs.org/sdr/SWIA201642055.md): Angle · corroded · Mar 25, 2016 · N215AG · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > PASSENGER DOOR KICK ANGLE, STGR 18L HAS EVIDENCE OF CORROSION AROUND RIVETS AND NUTPLATES. INSTALLED NEW PAX DOOR KICK ANGLE IAW SRM.
- [SDR SWIA201642054](https://openairdocs.org/sdr/SWIA201642054.md): Floorbeam · corroded · Mar 25, 2016 · N215AG · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > FS 280 FWD FLOORBEAM ANGLE HAS CORROSION.IN BETWEEN LBL 9.0 AND RBL 9.0. REMOVED AND INSTALLED NEW SERVICEABLE FLOORBEAM ANGLE IAW SRM.
- [SDR SWIA201642053](https://openairdocs.org/sdr/SWIA201642053.md): Door Sill · corroded · Mar 24, 2016 · N215AG · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > SERVICE DOOR LOWER SILL HAS CORROSION. NEW SERVICE DOOR LOWER SILL INSTALLED IAW SRM.
- [SDR SWIA201642052](https://openairdocs.org/sdr/SWIA201642052.md): Panel · corroded · Mar 23, 2016 · N215AG · Cndair CL6002C10 · Passenger/Crew Doors
  > CORROSION ARROUND SCREW HOLES ON PASSENGER DOOR PANEL 832AL. PANEL REMOVED AND INSTALLED IAW SRM.
- [SDR SWIA201541401](https://openairdocs.org/sdr/SWIA201541401.md): Shutoff Valve · malfunctioned · Aug 20, 2015 · N215AG · Cndair CL6002C10 · Pneumatic Distribution System
  > LT BLEED OVERHEAT WARNING AT FL340. FOLLOWED QRH, FLT 3469, F/O: 08/20/2015 VISUALLY INSPECTED THE ACFT AND BLEED AIR DUCTS FOR DAMAGE OR LEAKS, NONE FOUND. C/W FIM PROCEDURES FOR BLEED AND ANTI-ICE DUCT LEAK, LEAK RUN EVENT TEST. NDC SHOWED FAULT HISTORY F
- [SDR SWIA201540679](https://openairdocs.org/sdr/SWIA201540679.md): Post · cracked · Jan 29, 2015 · N215AG · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > LT AND RT BL30 POSTS HAVE INDICATIONS NOTED AT TOP T SECTION. REPAIRED IAW REO.
- [SDR SWIA201540678](https://openairdocs.org/sdr/SWIA201540678.md): Structure · damaged · Jan 29, 2015 · N215AG · Cndair CL6002C10 · Fuselage Main, Structure
  > FORWARD RT CAP ANGLE BETWEEN STR 13 & 14 CUT. R & R RT SKIN PANEL FROM FS 202-193, BUTTSTRAP AT FS 202, STR 11-15 RT; RBL 13 & 14 INTERCOSTAL AT FW SIDE OF FS 202 BULKHEAD; STR 14R AT FS 202-193 IAW SRM.
- [SDR SWIA201540636](https://openairdocs.org/sdr/SWIA201540636.md): Frame · cracked · Jan 9, 2015 · N215AG · Cndair CL6002C10 · Fuselage Main, Frame
  > FOUND RT FS 220 FRAME TO BE CRACKED. C-CHECK, REMOVED RT FS 220 FRAME IAW SRM, FASTENERS REQUIRE PAINT AND PRIMER. REMOVED SIDE CONSOLE SUPPORT BRACKET FROM FS 220 UPPER FRAME SECTION IAW SRM. OK TO INSTALL PARTS. INSTALLED NEW SERVICABLE FRAME AT FS 220.00
- [SDR SWIA201540635](https://openairdocs.org/sdr/SWIA201540635.md): Frame · damaged · Jan 9, 2015 · N215AG · Cndair CL6002C10 · Fuselage Main, Frame
  > BS 235, FRAME HAS AN INDICATION NOTED IN RADIUS AT STR 13AL, LT APPROX, 250' LONG. FAILED NDT INSP, C-CHECK, REMOVED INTERCOSTAL BETWEEN FS 234 AND FS 250 AT STR 12L IAW SRMS REINSTALLED INTERCOSTALS BETWEEN FS 235 AND FS 250 AT STR 12L IAW SRMS. REMOVED LT F
- [SDR SWIA201540640](https://openairdocs.org/sdr/SWIA201540640.md): Frame · cracked · Jan 5, 2015 · N215AG · Cndair CL6002C10 · Fuselage Main, Frame
  > BS 235 FRAME HAS A CRACK INDICATION IN RADIUS AT STRINGER 13L.
- [SDR SWIA201440639](https://openairdocs.org/sdr/SWIA201440639.md): Frame · cracked · Dec 30, 2014 · N215AG · Cndair CL6002C10 · Fuselage Main, Frame
  > RIGHT BS 220 FRAME CRACKED. INSTALLED A NEW FRAME IAW SRM.
- [SDR SWIA201438966](https://openairdocs.org/sdr/SWIA201438966.md): Support Fitting · cracked · Jul 27, 2014 · N215AG · Cndair CL6002C10 · Wing, Landing Gear Attach Fittings
  > ONE CRACK FOUND AT OTBD FASTENER HOLE ON LT MLG ACTUATOR SUPPORT FITTING. C-CHECK. REPAIRED SUPPORT FITTING IAW REO.
- [SDR SWIA201438965](https://openairdocs.org/sdr/SWIA201438965.md): Support Fitting · cracked · Jul 27, 2014 · N215AG · Cndair CL6002C10 · Wing, Landing Gear Attach Fittings
  > ONE CRACK FOUND AT OTBD FASTENER HOLE ON RT MLG ACTUATOR SUPPORT FITTING. C-CHECK, REPAIRED SUPPORT FITTING IAW REO.
- [SDR SWIA201438983](https://openairdocs.org/sdr/SWIA201438983.md): Seat Track · corroded · Jul 19, 2014 · N215AG · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > RT SEAT TRACK BS 485-581 HAS MULTIPLE CORRODED AREAS. C-CHECK, R & R THE SEAT TRACK IAW REO AND AMM.
- [SDR SWIA201438982](https://openairdocs.org/sdr/SWIA201438982.md): Seat Track · corroded · Jul 19, 2014 · N215AG · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > RIGHT SEAT TRACK BS 581-685 HAS MULTIPLE CORRODED AREAS. C-CHECK, REMOVED AND REPLACED THE SEAT TRACK IAW REO AND AMM.
- [SDR SWIA201438981](https://openairdocs.org/sdr/SWIA201438981.md): Seat Track · corroded · Jul 19, 2014 · N215AG · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > RT SEAT TRACK BS 685-701 HAS MULTIPLE CORRODED AREAS. C-CHECK, REPLACED THE SEAT TRACK IAW REO.
- [SDR SWIA201438980](https://openairdocs.org/sdr/SWIA201438980.md): Seat Track · corroded · Jul 19, 2014 · N215AG · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > RT SEAT TRACK BS 379-482 HAS MULTIPLE CORRODED AREAS. C-CHECK, BLENDED DAMAGED AREAS, IAW REO.
- [SDR SWIA201438979](https://openairdocs.org/sdr/SWIA201438979.md): Seat Track · corroded · Jul 19, 2014 · N215AG · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > RT SEAT TRACK BS 482-573 HAS MULTIPLE CORRODED AREAS. C-CHECK, R & R THE SEAT TRACK IAW REO AND AMM.
- [SDR SWIA201438978](https://openairdocs.org/sdr/SWIA201438978.md): Seat Track · corroded · Jul 19, 2014 · N215AG · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > LEFT SEAT TRACK BS 379-485 HAS MULTIPLE CORRODED AREAS. C-CHECK, R & R THE SEAT TRACK IAW REO AND AMM.
- [SDR SWIA201438977](https://openairdocs.org/sdr/SWIA201438977.md): Seat Track · corroded · Jul 19, 2014 · N215AG · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > LEFT SEAT TRACK BS 485-572 HAS MULTIPLE CORRODED AREAS. C-CHECK, R & R THE SEAT TRACK IAW REO AND AMM.
- [SDR SWIA201438976](https://openairdocs.org/sdr/SWIA201438976.md): Seat Track · corroded · Jul 19, 2014 · N215AG · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > LT SEAT TRACK BS 572-674 HAS MULTIPLE CORRODED AREAS. C-CHECK, R & R THE SEAT TRACK IAW REO AND AMM.
- [SDR SWIA201438975](https://openairdocs.org/sdr/SWIA201438975.md): Seat Track · corroded · Jul 19, 2014 · N215AG · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > LT SEAT TRACK BS 674-711 HAS MULTIPLE CORRODED AREAS. C-CHECK, R & R THE SEAT TRACK IAW REO AND AMM.
- [SDR SWIA201438974](https://openairdocs.org/sdr/SWIA201438974.md): Seat Track · corroded · Jul 19, 2014 · N215AG · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > LT SEAT TRACK BS 711-762 HAS MULTIPLE CORRODED AREAS. C-CHECK, R & R THE SEAT TRACK IAW REO AND AMM.
- [SDR SWIA201438973](https://openairdocs.org/sdr/SWIA201438973.md): Seat Track · corroded · Jul 19, 2014 · N215AG · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > LEFT SEAT TRACK BS 784-860 HAS MULTIPLE CORRODED AREAS. C-CHECK, R & R THE SEAT TRACK IAW REO AND AMM.
- [SDR SWIA201438972](https://openairdocs.org/sdr/SWIA201438972.md): Seat Track · corroded · Jul 19, 2014 · N215AG · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > RT SEAT TRACK BS 674-718 HAS MULTIPLE CORRODED AREAS. C-CHECK, R & R THE SEAT TRACK IAW REO AND AMM.
- [SDR SWIA201438971](https://openairdocs.org/sdr/SWIA201438971.md): Seat Track · corroded · Jul 19, 2014 · N215AG · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > RIGHT SEAT TRACK BS 718-762 HAS MULTIPLE CORRODED AREAS. C-CHECK, R & R THE SEAT TRACK IAW REO AND AMM.
- [SDR SWIA201438970](https://openairdocs.org/sdr/SWIA201438970.md): Seat Track · corroded · Jul 19, 2014 · N215AG · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > RT SEAT TRACK BS 784-861 HAS MULTIPLE CORRODED AREAS. C-CHECK, R & R THE SEAT TRACK IAW REO AND AMM.
- [SDR SWIA201438969](https://openairdocs.org/sdr/SWIA201438969.md): Seat Track · corroded · Jul 19, 2014 · N215AG · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > LT SEAT TRACK BS 482-579 HAS MULTIPLE CORRODED AREAS. C-CHECK, REMOVED AND REPLACED THE SEAT TRACK IAW REO AND AMM.
- [SDR SWIA201438968](https://openairdocs.org/sdr/SWIA201438968.md): Seat Track · corroded · Jul 19, 2014 · N215AG · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > LT SEAT TRACK BS 579-685 HAS MULTIPLE CORRODED AREAS. C-CHECK, REMOVED AND REPLACED THE SEAT TRACK IAW REO AND AMM.
- [SDR SWIA201438967](https://openairdocs.org/sdr/SWIA201438967.md): Seat Track · corroded · Jul 19, 2014 · N215AG · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > RT SEAT TRACK BS 349-485 HAS MULTIPLE CORRODED AREAS. C-CHECK, R & R SEAT TRACK IAW REO AND AMM.
- [SDR SWIA201438985](https://openairdocs.org/sdr/SWIA201438985.md): Angle · dented · Jul 18, 2014 · N215AG · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > PAX DOOR CUTOUT FORWARD LOWER STRIKER DENTED ON OTBD ANGLE. C-CHECK, REPAIRED STRIKER IAW REO.
- [SDR SWIA201438984](https://openairdocs.org/sdr/SWIA201438984.md): Striker · dented · Jul 18, 2014 · N215AG · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR CUTOUT AFT LOWER STRIKER DENTED ON OTBD ANGLE. C-CHECK, REPAIRED STRIKER IAW REO.
- [SDR SWIA201438989](https://openairdocs.org/sdr/SWIA201438989.md): Floor Panel · cracked · Jul 17, 2014 · N215AG · Cndair CL6002C10 · Fuselage Floor Panel
  > FLOOR PANEL NR 222VZ IS CRACKED. C-CHECK, REPAIRED FLOOR PANEL IAW EA.
- [SDR SWIA201438988](https://openairdocs.org/sdr/SWIA201438988.md): Structure · cracked · Jul 17, 2014 · N215AG · Cndair CL6002C10 · Fuselage Main, Structure
  > BS 193, FWD EQUIPMENT BAY CRACKED LT SIDE. C-CHECK, REPAIRED IAW REO.
- [SDR SWIA201438987](https://openairdocs.org/sdr/SWIA201438987.md): Structure · cracked · Jul 17, 2014 · N215AG · Cndair CL6002C10 · Fuselage Main, Structure
  > BS 193, FWD EQUIPTMENT BAY CRACKED RT SIDE. C-CHECK, REPAIRED IAW EA.
- [SDR SWIA201438986](https://openairdocs.org/sdr/SWIA201438986.md): Floor Panel · cracked · Jul 17, 2014 · N215AG · Cndair CL6002C10 · Fuselage Floor Panel
  > COCKPIT FLOOR PANEL 221ELW IS CRACKED. C-CHECK, REPAIRED FLOOR PANEL IAW EA.
- [SDR SWIA201438991](https://openairdocs.org/sdr/SWIA201438991.md): Support Arm · chafed · Jul 16, 2014 · N215AG · Cndair CL6002C10 · Cargo/Baggage Doors
  > FWD CARGO DOOR FWD LOWER SUPPORT ARM IS CHAFED ON TOP SIDE. C-CHECK, REPAIRED STEPS 1-8 OF EA.
- [SDR SWIA201438990](https://openairdocs.org/sdr/SWIA201438990.md): Support Arm · chafed · Jul 16, 2014 · N215AG · Cndair CL6002C10 · Cargo/Baggage Doors
  > FWD CARGO DOOR AFT LOWER SUPPORT ARM IS CHAFED ON AFT FACE. C-CHECK, REPAIRED IAW EA.
- [SDR SWIA201438732](https://openairdocs.org/sdr/SWIA201438732.md): Linkage · disconnected · Jul 13, 2014 · N215AG · Cndair CL6002C10 · Service Doors
  > SERVICE DOOR DIFFICULT TO OPEN AND CLOSE. CONNECTED THE TELESCOPIC LINKAGE AND TESTED DOOR FOR OPERATION IAW AMM.
- [SDR SWIA201438519](https://openairdocs.org/sdr/SWIA201438519.md): Bulb · inoperative · Jul 2, 2014 · N215AG · Cndair CL6002C10 · Emergency Lighting
  > CEILING EMERGENCY LIGHT POD INOPERATIVE. REPLACED BULB. OPS CHECKED GOOD.
- [SDR SWIA201438295](https://openairdocs.org/sdr/SWIA201438295.md): Battery Pack · failed · Jun 22, 2014 · N215AG · Cndair CL6002C10 · Emergency Lighting
  > EMERGENCY LIGHT SWITCH IN ON POSITION ON F/A PANEL. EMERGENCY LIGHTING WILL NOT STAY ON WHEN TESTED. REPLACED NR 1, NR 2, NR 3, NR 4 ELBP IAW AMM.
- [SDR SWIA201437810](https://openairdocs.org/sdr/SWIA201437810.md): Seal · cut · May 28, 2014 · N215AG · Cndair CL6002C10 · Emergency Exits
  > OVERWING EXIT DOOR SEAL IS CUT. REPAIRED IAW REO.
- [SDR SWIA201335724](https://openairdocs.org/sdr/SWIA201335724.md): Relay · failed · Dec 22, 2013 · N215AG · Cndair CL6002C10 · Landing Gear Position and Warning
  > PROX SYS FAULT 2 STATUS MESSAGE APPEARED WHEN LDG WAS RETRACTED. FLT 3488 REPLACED RELAY K133 & PSEU. PN ON 8-953-04, SN ON 0267, PN OFF 8-953-03 & SN OFF A010.
- [SDR SWIA201335353](https://openairdocs.org/sdr/SWIA201335353.md): Skin · damaged · Nov 19, 2013 · N215AG · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN DAMAGED JUST FWD OF 1098 BETWEEN STRINGERS 16 & 17. CW REPAIR ON FUSELAGE SKIN JUST FWD OF FS 1098 BETWEEN STRINGERS 16 & 17 IAW REO.
- [SDR SWIA201333792](https://openairdocs.org/sdr/SWIA201333792.md): Control Unit · failed · Jun 26, 2013 · N215AG · Cndair CL6002C10 · Drag Control System
  > ENROUTE HYDRAULIC SYSTEM QUANTITY WENT TO ZERO. FLT#3493 REPLACED LT WING OTBD MFS CU IAW AMM 27-62-01. PN: 51200-11 SN ON: MAL1000 SN OFF: MAL-0205
- [SDR SWIA201333291](https://openairdocs.org/sdr/SWIA201333291.md): Detector · failed · Apr 23, 2013 · N215AG · Cndair CL6002C10 · Trailing Flap Position Indicating System
  > FLAPS FAIL CAUTION MESSAGE AND ZERO FLAP LANDING. (FLT 3475) REPLACED LEFT INBOARD FLAP INBOARD SKEW DETECTOR IAW AMM. P/N 5915549 S/N ON 0909 S/N OFF 0314.
- [SDR SWIA201333240](https://openairdocs.org/sdr/SWIA201333240.md): Skin · chafed · Apr 3, 2013 · N215AG · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > BELLY SKIN CHAFED NEAR FS 977 AND STR 27. (C-CHECK) REMOVED PREVIOUS REPAIR DOUBLER AT FS 977.00 STR 27 AND FABRICATED NEW DOUBLER IAW REO.
- [SDR SWIA201332760](https://openairdocs.org/sdr/SWIA201332760.md): Light · inoperative · Feb 4, 2013 · N215AG · Cndair CL6002C10 · Emergency Lighting
  > EMERGENCY OVERHEAD LIGHT OVER ROW 4 BURNED OUT. (FLT 3476) RELAMPED EMERGENCY LIGHT.
- [SDR SWIA201332729](https://openairdocs.org/sdr/SWIA201332729.md): Battery Pack · malfunctioned · Feb 1, 2013 · N215AG · Cndair CL6002C10 · Emergency Lighting
  > THREE OVERHEAD EMERGENCY LIGHTS DO NOT ILLUMINATE. (FLT 3462) RESET 3 ELBP'S.

Next page: https://openairdocs.org/deregistered/N215AG-2022-05-07/reports.md?page=2

## 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 = 'N215AG' AND deregistration_id = 'N215AG-2022-05-07'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N215AG-2022-05-07/reports

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