# Service difficulty reports: N820AY

A list on [N820AY](https://openairdocs.org/aircraft/N820AY.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 3 · 112 reports

- [SDR REXA2022020900242](https://openairdocs.org/sdr/REXA2022020900242.md): Flange · corroded · Feb 8, 2022 · N820AY · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > IN C/W THE CRJ200 36 MO JOB CARD 53-170-500, DETAILED INSPECTION OF THE FLOOR SUPPORT STRUCTURE FROM 559.0+80 TO FS 621.0, CORROSION WAS FOUND AROUND MULTIPLE NUT PLATES IN THE FLANGES OF THE UPPER FLOOR SUPPORTS FROM FS 559.0+81.5 TO FS559.0+109.5 AT RBL9 & R
- [SDR REXA2021122001180](https://openairdocs.org/sdr/REXA2021122001180.md): Relay · inoperative · Dec 15, 2021 · N820AY · Cndair CL6002B19 · Emergency Lighting
  > AT GATE WITH AC POWER ON AIRCRAFT EMER LIGHTS ON STATUS COMES ON WHEN EMER LIGHTS ARE ARMED REMOVED AND REPLACED AC ESS BUS SENSE (K1XD) IAW CRJ-200 AMM 24-51-27. OPS TEST GOOD EMERGENCY LIGHTS ARE BACK IN WORKING ORDER.
- [SDR REXA2020092900675](https://openairdocs.org/sdr/REXA2020092900675.md): Battery · inoperative · Sep 21, 2020 · N820AY · Cndair CL6002B19 · Emergency Lighting
  > FWD EMERGENCY LIGHTS INOPERABLE. REMOVED AND REPLACED FWD EMERGENCY LIGHT BATTERY, IAW CRJ 200 AMM 33-51-04. P/N OFF AD-2013-1A S/N OFF 85293, P/N ON 2013-1ASMI S/N ON 12738. OPERATIONS CHECK GOOD.
- [SDR REXA2020012730050](https://openairdocs.org/sdr/REXA2020012730050.md): Battery Pack · inoperative · Jan 23, 2020 · N820AY · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY LIGHTS WILL NOT ILLUMINATE REMOVED AND REPLACED BATTERY PACK ASSEMBLY IAW CRJ 200 AMM 33-51-04 P/N ON/OFF AD-2013-1A S/N ON 85293 S/N OFF 177931
- [SDR REXA2019041100457](https://openairdocs.org/sdr/REXA2019041100457.md): Battery Pack · inoperative · Apr 11, 2019 · N820AY · Cndair CL6002B19 · Emergency Lighting
  > FOUND EMERGENCY LIGHTING INOP. REMOVED AND REPLACED BATTERY PACK #4 IAW CRJ 200 AMM 33-51-04. REMOVED AND REPLACED BATTERY CHARGER ASSEMBLY #4 IAW CRJ 200 AMM 33-51-05. OPS CHECK GOOD.
- [SDR REXA2019041020456](https://openairdocs.org/sdr/REXA2019041020456.md): Torque Box · cracked · Apr 2, 2019 · N820AY · Cndair CL6002B19 · Engine Thrust Reverser
  > LH THRUST REVERSER HAS A CRACK NEAR BLOCKER DOOR #9. REPAIRED LH THRUST REVERSER NEAR BLOCKER DOOR #9 IAW IAW REO 601R-78-30-26-16 AAR SM 33
- [SDR REXA2019041020454](https://openairdocs.org/sdr/REXA2019041020454.md): Plate · cracked · Apr 2, 2019 · N820AY · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CRACK IN FWD RADIUS OF CARGO STEP PLATE FOUND. REMOVED CRACK AND FOUND TO BE WITHIN LIMITS IAW CRJ 200 SRM 52-00-00 AAR AP 377
- [SDR REXA2019041000449](https://openairdocs.org/sdr/REXA2019041000449.md): Floor Support · corroded · Mar 30, 2019 · N820AY · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LBL 27 O/B LANDING HAS CORROSIN BETWEEN FS 605 AND FS 621, IN THE CARGO BAY. INSTALLED REPAIR STRAP IAW EA CRJ253-08726 REV. IR.
- [SDR REXA2019041030444](https://openairdocs.org/sdr/REXA2019041030444.md): Frame · corroded · Mar 30, 2019 · N820AY · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME 349 HAS CORROSION ON THE FWD AND AFT SIDE BETWEEN STGR 26L AND 26R, IN THE FWD E & E BAY. REMOVED/REPLACED LWR FRAME SECTOR 349 IAW CRJ 200 SRM 51-42-06 AND SRM 51-42-21 PERFORMED OPS TEST GOOD IAW CRJ 200 AMM 22-12-00-710-802 AAR SM 33
- [SDR REXA201904102948](https://openairdocs.org/sdr/REXA201904102948.md): Fitting · cracked · Mar 29, 2019 · N820AY · Cndair CL6002B19 · Cargo/Baggage Doors
  > CARGO DOOR I/B UPPER FWD BACK-UP FITTING IS CRACKED. REMOVED AND REPLACED CARGO DOOR 1B UPPER FWD BACK-UP FITTING IAW CRJ 200 SRM 51-42-10.
- [SDR REXA2019041025443](https://openairdocs.org/sdr/REXA2019041025443.md): Seat Track · corroded · Mar 25, 2019 · N820AY · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RIGHT HAND SEAT TRACK, STICK #2 HAS SEVERAL AREAS OF CORROSION. REMOVED/REPLACED WITH NEW SEAT TRACK IAW CRJ 200 AMM 53-01-11.
- [SDR REXA2019041024445](https://openairdocs.org/sdr/REXA2019041024445.md): Seat Track · corroded · Mar 24, 2019 · N820AY · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RIGHT HAND SEAT TRACK, STICK #6 HAS SEVERAL AREAS OF CORROSION. REMOVED AND REPLACED WITH NEW SEAT TRACK IAW AMM 53-01-11.
- [SDR REXA2019043102447](https://openairdocs.org/sdr/REXA2019043102447.md): Seat Track · corroded · Mar 21, 2019 · N820AY · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RIGHT HAND SEAT TRACK, STICK #4 HAS SEVERAL AREAS OF CORROSION. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-01-11.
- [SDR REXA2019041021446](https://openairdocs.org/sdr/REXA2019041021446.md): Seat Track · corroded · Mar 21, 2019 · N820AY · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LEFT HAND SEAT TRACK, STICK #2 HAS SEVERAL AREAS OF CORROSION. REMOVED AND REPLACED LT SEAT TRACK #2 PART #601R 31/032-21 IAW AMM 63-01-11.
- [SDR REXA2019041090453](https://openairdocs.org/sdr/REXA2019041090453.md): Spar · nicked · Mar 19, 2019 · N820AY · Cndair CL6002B19 · Nacelle/Pylon, Attach Fittings
  > 1 ENG PYLON FWD MOUNT AFT UPPER HOLE HAS TWO NICKS COMPLIED WITH BOMBARDIER REO 601R-54-51-193 DATED:3/15/2019 TO REMOVE NICK DAMAGE BY BLENDOUT, ROTOPEEN AND RESTORE FINISH (MATERIAL LOSS A:.325LX.325LX.175"W X.004" D). AAR SM 39
- [SDR REXA201904109442](https://openairdocs.org/sdr/REXA201904109442.md): Seat Track · corroded · Mar 19, 2019 · N820AY · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK ON TOP OF RBL 27 HAS CORROSION BETWEEN FS 559+80 AND FS 559+96, IN THE CARGO BAY. REMOVED/REPLACED SEAT TRACK IAW CRJ 200 AMM 53-00-49 AAR SM 58
- [SDR REXA201904109440](https://openairdocs.org/sdr/REXA201904109440.md): Intercostal · cracked · Mar 19, 2019 · N820AY · Cndair CL6002B19 · Engine Collector/Tailpipe/Nozzle
  > R/H ENGINE EXHAUST NOZZLE HAS BENT INTERCOSTAL BY O/B ACCESS PANEL INNER SECTION. REMOVED AND REPLACED WITH NEW INTERCOASTAL ON R/H ENGINE EXHAUST NOZZLE O/B INNER SECTION I.A.W. CRJ-200 BOMB CMM 20-42-06 AND CMM 20-42-20.
- [SDR REXA201904106441](https://openairdocs.org/sdr/REXA201904106441.md): Floor Support · cracked · Mar 16, 2019 · N820AY · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RH OVERWING ACCESS PNL SUPPORT BRACKET AT FS473.15 IS CRACKED. REMOVED AND REPLACED R/H OVERWING SUPPORT BRACKET @ F.S. 473.15 I.A.W. CRJ-200 SRM 51-42-06 AND 51-42-21.
- [SDR REXA2019041040452](https://openairdocs.org/sdr/REXA2019041040452.md): Bulkhead Web · gouged · Mar 14, 2019 · N820AY · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > REAR PRESSURE BULKHEAD IS GOUGED ON PREVIOUS REPAIR AT RBL 36.20. REMOVED AND REPLACED GOUGED TRIPLER IAW BOMBARDIER REO 601R-53-61-1285 REV. E REO 601R-53-61-6918. AAR SM 33
- [SDR REXA2019041040451](https://openairdocs.org/sdr/REXA2019041040451.md): Bulkhead Web · gouged · Mar 14, 2019 · N820AY · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > REAR PRESSURE BULKHEAD HAS GOUGE ON PREVIOUS REPAIR ON RBL18.00. REMOVED AND REPLACED GOUGED TRIPLER IAW REO 601R-53-61-1285 REV. E REO 601R-53-61-6918. AAR SM 33
- [SDR REXA2019041040450](https://openairdocs.org/sdr/REXA2019041040450.md): Bulkhead Web · gouged · Mar 14, 2019 · N820AY · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > REAR PRESSURE BULKHEAD IS GOUGED AT PREVIOUS REPAIR AT RBL27.50. REMOVED AND REPLACED GOUGED TRIPLER IAW BOMBARDIER REO 601R-53-61-1285 REV. E. REO 601R-53-61-6918. AAR SM 33
- [SDR REXA201904100436](https://openairdocs.org/sdr/REXA201904100436.md): Floorbeam · cracked · Mar 14, 2019 · N820AY · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > UNDER 262CRF AT RBL9 FS460 THERE IS A CRACKED ANGLE BRACKET. MARKED BY RED PENCIL. REMOVED CRACKED FITTING FS 460 RBL-9 AND INSTALLED NEW FITTING IAW CRJ 200 SRM 51-42-21 AAR SM 39
- [SDR REXA201904102439](https://openairdocs.org/sdr/REXA201904102439.md): Bulkhead Web · cracked · Mar 12, 2019 · N820AY · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > AFT PRESSURE BULKHEAD WEB HAS A CRACK AT BL 0 AND WL 111. REPAIRED CRACK IN AFT PRESSURE BULKHEAD IAW BOMBARDIER REO 601R-53-61-1285 REV. C.
- [SDR REXA201904100434](https://openairdocs.org/sdr/REXA201904100434.md): Bulkhead · gouged · Mar 11, 2019 · N820AY · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > REAR PRESSURE BULKHEAD FWD FACE IS GOUGED IN 2EA AREAS. BLENDED DAMAGE IAW CRJ 200 SRM TR51-41. MATERIAL LOSS OF.010 WITHIN LIMITS IAW BOMBARDIER REO 601R-53-61-2155 REV. A.
- [SDR REXA2019041090455](https://openairdocs.org/sdr/REXA2019041090455.md): Seat Track · corroded · Mar 9, 2019 · N820AY · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RH SIDEWALL SEAT TRACK STICK 3 HAS CORROSION SPOTS BETWEEN FS 409+16 THRU FS 409+112, IN THE CABIN. REMOVED/REPLACED SEAT TRACK IAW CRJ 200 AMM 53-01-11 AAR SM 58
- [SDR REXA2019041080433](https://openairdocs.org/sdr/REXA2019041080433.md): Angle · cracked · Mar 8, 2019 · N820AY · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > UNDER FLOORBOARD 262DRF AT RBL27 AT OR AROUND FS529.0 THERE IS A CRACKED ANGLE BRACKED. MARKED BY RED PENCIL. REPLACED CRACKED ANGLE UNDER FLOORBOARD AT RBL27 AND FS529 IAW CRJ 200 SRM 51-42-21. AAR SM 33
- [SDR REXA2019041070438](https://openairdocs.org/sdr/REXA2019041070438.md): Angle · cracked · Mar 7, 2019 · N820AY · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > AFT PRESURE BULKHEAD AFT FACE HAS ANGLE AT STR15 ON L/H HAS CRACK. REMOVED AND REPLACED WITH NEW L/H ANGLE ON AFT PRESSURE BULKHEAD AFT FACE AT STR15 IAW CRJ 200 SRM 51-42-06.
- [SDR REXA201904107437](https://openairdocs.org/sdr/REXA201904107437.md): Angle · cracked · Mar 7, 2019 · N820AY · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > AFT PRESURE BULKHEAD AFT FACE HAS ANGLE AT STR15 ON R/H HAS CRACK. REMOVED AND REPLACED WITH NEW R/H ANGLE ON AFT PRESSUR BULKHEAD AFT FACE AT STR 15 IAW CRJ 200 SRM 51-42-06. AAR SM 58
- [SDR REXA2019041050432](https://openairdocs.org/sdr/REXA2019041050432.md): Seat Track · corroded · Mar 5, 2019 · N820AY · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LEFT HAND SEAT TRACK, STICK #1 HAS SEVERAL AREAS OF CORROSION. REMOVED AND REPLACE SEAT TRACK IAW CRJ 200 AMM 53-01-11.
- [SDR REXA201904100435](https://openairdocs.org/sdr/REXA201904100435.md): Floorbeam · cracked · Mar 1, 2019 · N820AY · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > UNDER FLOORBOARD 261DLF BETWEEN LBL36 AND LBL27 AT OR AROUND FS484 THERE IS A CRACKED ANGLE BRACKET IN BOTH CORNERS. REPLACED CRACKED ANGLE AT LBL36 AT FS484 IAW REO #601R-53-41-059 AND ANGLE AT LBL27 AND FS484 IAW CRJ 200 SRM 51-42-21. AAR SM 33
- [SDR REXA2018122731269](https://openairdocs.org/sdr/REXA2018122731269.md): Vertical Beam · cracked · Dec 23, 2018 · N820AY · Cndair CL6002B19 · Fuselage Main, Structure
  > VERT BEAM RBL 18 AT FS 409+128 IS CRACKED LWR O/B FLANGE STARTING AT EDGE EXTENDING UP TO 1ST RIVET. COMPLETED REPAIR TO FS 128+ 128 RBL 18 O/B FLANGE IAW REO 601R-53-41-2410. REFERENCE CONTINUATION CARDS 114960 AND 114965 FOR DETAILS. THIS IS A MAJOR REPAIR
- [SDR REXA2018121901268](https://openairdocs.org/sdr/REXA2018121901268.md): Vertical Beam · cracked · Dec 19, 2018 · N820AY · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > VERT BEAM LBL 18.00 AT FS 409.0 +128 IS CRACKED LWROB FLANGE STARTING AT EDGE EXTENDING UP TO 1ST RIVET. COMPLETED PERMANENT REPAIR TO FS 409 +128 LBL 18 LWROB FLANGE IAW REO 601R-53-41-0056 REV F.
- [SDR REXA2018121901267](https://openairdocs.org/sdr/REXA2018121901267.md): Vertical Beam · cracked · Dec 19, 2018 · N820AY · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > VERT BEAM LBL 27.00 AT FS 409.0 +128 IS CRACKED LWROB FLANGE STARTING AT EDGE EXTENDING UP TO 1ST RIVET. COMPLETED REPAIR TO 409+128 VERT BEAM LBL 27 LWROB FLANGE IAW REO601R-53-41-0056 REV F.
- [SDR REXA2018122091266](https://openairdocs.org/sdr/REXA2018122091266.md): Vertical Beam · cracked · Dec 19, 2018 · N820AY · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > VERT BEAM RBL27.00 AT FS 409.0 +128 IS CRACKED LWRIB STAARTING AT EDGE EXTENDING UP TO POAST 1ST RIVET BUT DOESNT EXTEND ALL THE WAY UP TO 2ND RIVET COMPLETED PERMANENT REPAIR TO FS409+128 RBL 27 LWR IB FLANGE IAW REO 601R-53-41-0056 REV F SEE CONT CARD 1149
- [SDR REXA2018092000865](https://openairdocs.org/sdr/REXA2018092000865.md): Oxygen Mask · unwanted deploy · Sep 18, 2018 · N820AY · Cndair CL6002B19 · Passenger Oxygen System
  > LAV 02 MASK DEPLOYED. REPACKED 02 MAKS IAW AMM 35-21-03. NO DEFECTS NOTED AT THIS TIME.
- [SDR REXA2018082840717](https://openairdocs.org/sdr/REXA2018082840717.md): Oxygen Mask · unwanted deploy · Aug 24, 2018 · N820AY · Cndair CL6002B19 · Passenger Oxygen System
  > OXYGEN MASKS IN THE LAVATORY DROPPED. INSPECTED AND RESTOWED THE LAVATPRU OXYGEN MASKS IAW AMM 35-21-09.
- [SDR REXA2018052700424](https://openairdocs.org/sdr/REXA2018052700424.md): Battery Pack · discharged · May 27, 2018 · N820AY · Cndair CL6002B19 · Emergency Equipment
  > F/A FLASHLIGHT NOT CHARGING IN CRADLE. REMOVED AND REPLACED EMERGENCY FLASHLIGHT BATTERY PACK REF AMM 25-61-02 OPS CHECK GOOD.
- [SDR REXA2017091301002](https://openairdocs.org/sdr/REXA2017091301002.md): Charger · inoperative · Sep 13, 2017 · N820AY · Cndair CL6002B19 · Emergency Lighting
  > RIGHT AND LEFT OVERWING EMERGENCY LIGHTS ARE OUT, ALL EMERGENCY LIGHTS RUNNING OFF BATTERY PACK INOPERATIVE. REMOVED AND REPLACED THE BATTERY CHARGER ASSY IAW AMM 33-51-05. CHECKED GOOD.
- [SDR REXA2017020800188](https://openairdocs.org/sdr/REXA2017020800188.md): Lamp · inoperative · Feb 8, 2017 · N820AY · Cndair CL6002B19 · Emergency Lighting
  > DURING WALKAROUND, FOUND LEFT HAND AFT WING EMERGENCY LIGHT NOT ILLUMINATED. REPLACED THE LAMPS IAW AMM 33-51-21. OPS CHECKED GOOD.
- [SDR REXA2016120402367](https://openairdocs.org/sdr/REXA2016120402367.md): Floor Support · cracked · Dec 4, 2016 · N820AY · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > BS 621 - 625 FLOOR SUPPORT IS CRACKED. REMOVED AND REPLACED IAW SRM 51-42-06, 51-42-21 AND 51-42-22.
- [SDR REXA2016120302361](https://openairdocs.org/sdr/REXA2016120302361.md): Torque Box · cracked · Dec 3, 2016 · N820AY · Cndair CL6002B19 · Engine Thrust Reverser
  > NR 2 ENGINE THRUST REVERSER TORQUE BOX HAS CRACK FROM FASTENER HOLE AT 5 O’CLOCK POSITION. FOUND DURING FREEDOM OF MOVEMENT CHECK OF THRUST REVERSER. REPAIRED CRACK ON NR 2 THRUST REVERSER TORQUE BOX AT 5 O'CLOCK POSITION IAW REO 601R-78-30-2616.
- [SDR REXA2016120102350](https://openairdocs.org/sdr/REXA2016120102350.md): Seat Track · corroded · Dec 1, 2016 · N820AY · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > CABIN, LT SIDEWALL SEAT TRACK, STICK NR 4 HAS CORROSION AS MARKED. REMOVED AND REPLACED WITH NEW SEAT TRACK IAW AMM 53-01-11. REMOVED CORROSION, NO ALLOWABLE DAMAGE IAW SRM 51-21-06 AND 53-21-49.
- [SDR REXA2016113002368](https://openairdocs.org/sdr/REXA2016113002368.md): Floor Support · cracked · Nov 30, 2016 · N820AY · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > BS 621 - 625 FLOOR SUPPORT IS CRACKED. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-42-21 & 51-42-22
- [SDR REXA2016113002357](https://openairdocs.org/sdr/REXA2016113002357.md): Cargo Track · corroded · Nov 30, 2016 · N820AY · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > IN AFT CARGO AREA CARGO TRACK IS GOUGED AND CORRODED STA559+112 LBL9. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-00-49 AND REO 601R-53-00-485.
- [SDR REXA2016113002355](https://openairdocs.org/sdr/REXA2016113002355.md): Seat Track · corroded · Nov 30, 2016 · N820AY · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > CABIN, RT SIDEWALL SEAT TRACK, STICK NR 6 HAS CORROSION AS MARKED. REMOVED AND REPLACED SEAT RAIL IAW AMM-53-01-11. NO ALLOWABLE DAMAGE IAW SRM 53-21-49.
- [SDR REXA2016112802365](https://openairdocs.org/sdr/REXA2016112802365.md): Bulkhead · cracked · Nov 28, 2016 · N820AY · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > AFT PRESSURE BULKHEAD IS CRACKED AT LINTEL FITTING. REPAIRED AFT PRESSURE BULKHEAD AT LINTEL FITTING IAW REO 601R-53-61-1230 REV C.
- [SDR REXA2016112702358](https://openairdocs.org/sdr/REXA2016112702358.md): Web · cracked · Nov 27, 2016 · N820AY · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FWD E&E FLOOR IS CRACKED AT FS 193 ON LT. REPAIRED E&E FLOOR FS 193 LT SIDE IAW REO 601R-53-11-081.
- [SDR REXA2016112602366](https://openairdocs.org/sdr/REXA2016112602366.md): Doubler · gouged · Nov 26, 2016 · N820AY · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > IN AFT CARGO APB FWD FACE HAS FOUR REPAIRS THAT ARE GOUGED. REMOVED AND REPLACED OUTER DOUBLER (4 EA) AFT CARGO FWD APB PER REO 601R-53-61-1285.
- [SDR REXA2016112602356](https://openairdocs.org/sdr/REXA2016112602356.md): Seat Track · corroded · Nov 26, 2016 · N820AY · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > CABIN, RT SIDEWALL SEAT TRACK, STICK NR 7 HAS CORROSION AS MARKED. BLENDED NR 7 RT SEAT TRACK OUT OF LIMITS NO ALLOWABLE DAMAGE IAW AMM 53-01-11. REPLACED WITH NEW SEAT TRACK IAW AMM 53-01-11.
- [SDR REXA2016112302362](https://openairdocs.org/sdr/REXA2016112302362.md): Strip · chafed · Nov 23, 2016 · N820AY · Cndair CL6002B19 · Engine Cowling System
  > NR 2 ENG LOWER FAN COWL T/E IS CHAFED IS SEVERAL AREAS. REMOVED AND REPLACED T/E IAW CMM-71-14-01.

Next page: https://openairdocs.org/aircraft/N820AY/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 = 'N820AY' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N820AY/reports

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