# Service difficulty reports: N800AY

A list on [N800AY](https://openairdocs.org/aircraft/N800AY.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 · 110 reports

- [SDR REXA2022080801790](https://openairdocs.org/sdr/REXA2022080801790.md): Linkage · sticking · Jul 27, 2022 · N800AY · Cndair CL6002B19 · Passenger/Crew Doors
  > MAIN CABIN DOOR JAMMED AND WILL NOT OPEN OPENED DOOR, PERFORMED INSPECTION & LUBRICATED LINKAGES. PASSENGER DOOR OPEN OPS CHECKS GOOD PER AMM 52-11-00
- [SDR REXA2022072801707](https://openairdocs.org/sdr/REXA2022072801707.md): Lamp · inoperative · Jul 20, 2022 · N800AY · Cndair CL6002B19 · Emergency Lighting
  > EMER LIGHT BULBS BURNED OUT R/R LIGHT BULBS IAW CRJ-200 ESPM 20-24-00. OPS CHECK GOOD.
- [SDR REXA2020092800657](https://openairdocs.org/sdr/REXA2020092800657.md): Cleat · cracked · Sep 25, 2020 · N800AY · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > CLEAT CRACKED COMMON TO EXTERNAL SERVICE PANEL. CA: REMOVED, LOCATED, DRILLED, AND INSTALLED NEW SERVICEABLE BRACKET, IAW CRJ200 SRM TASKS 51-42-06 AND 51-40-11.
- [SDR REXA2020092800658](https://openairdocs.org/sdr/REXA2020092800658.md): Bulkhead Web · corroded · Sep 23, 2020 · N800AY · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FS 280 WEB IS CORRODED BETWEEN RBL 9 AND LBL 9. CA: REPAIRED IAW BOMBARDIER REO 601R-53-11-926 REV B DATED 2006/05/10.
- [SDR REXA2020092800663](https://openairdocs.org/sdr/REXA2020092800663.md): Frame · corroded · Sep 23, 2020 · N800AY · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME AT FS 589 CORRODED BETWEEN STGR 24R AND STGR 24L. REMOVED AND REPLACED FRAME SECTOR, IAW CRJ 200 SRM 51-42-06 AND 51-42-21. LEAK CHECK OF MIX MANIFOLD CHECK GOOD. NO DEFECTS NOTED AT THIS TIME, IAW CRJ 200 AMM 21-20-00-790-801.
- [SDR REXA2020092800661](https://openairdocs.org/sdr/REXA2020092800661.md): Channel · corroded · Sep 20, 2020 · N800AY · Cndair CL6002B19 · Service Doors
  > SERVICE DOOR BOTTOM CHANNELS AT CENTER SPLICE ARE CORRODED. REPLACED CORRODED SPLICE ANGLES AT SERVICE DOOR BOTTOM CHANNELS, IAW EA NR CRJ252-10846, EA NR CRJ252-10847, CRJ200 SRM'S 51-40-11-00, 51-42-06, 51-42-13.
- [SDR REXA2020092800668](https://openairdocs.org/sdr/REXA2020092800668.md): Door Sill · corroded · Sep 16, 2020 · N800AY · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PAX DOOR FLOOR SILL ANGLE IS CORRODED BETWEEN FS 310 TO FS 349. REMOVED SERVICEABLE FLOOR SILL ANGLE. LOCATED AND DRILLED FLOOR SILL ANGLE, IAW CRJ200 SRM 51-40-11.
- [SDR REXA2020009280671](https://openairdocs.org/sdr/REXA2020009280671.md): Seat Track · corroded · Sep 15, 2020 · N800AY · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK SEGMENT AT RBL 9 BETWEEN FS 409+128 TO FS 559 IS CORRODED. REMOVED AND REPLACED FABRICATED SEAT TRACK, IAW CRJ 200 MM 53-01-11-400 -802 AND REO 601R-53-00-485.
- [SDR REXA2020092800669](https://openairdocs.org/sdr/REXA2020092800669.md): Floorbeam · corroded · Sep 15, 2020 · N800AY · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > DOUBLER ON TOP OF FLOOR BEAM CAP AT FS 319 AT RBL 5 IS CORRODED. REMOVED AND INSTALLED NEW FABBED DOUBLER PLATE, IAW CRJ 200 SRM 51-42-13.
- [SDR REXA2020101300662](https://openairdocs.org/sdr/REXA2020101300662.md): Bulkhead · cracked · Sep 14, 2020 · N800AY · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > INDICATION NOTED AT BL 0.00, WL 114, 3.7" IN LENGTH, FS 621 REAR PRESSURE BULKHEAD. REPAIRED 621 BULKHEAD AT BL 0.00 WL 114, IAW MHIRJ REO 601R-53-61-1285, REV E DATED 10/31/16. NO DEFECTS NOTED. THIS IS A MAJOR REPAIR.
- [SDR REXA2020092800667](https://openairdocs.org/sdr/REXA2020092800667.md): Intercostal · corroded · Sep 14, 2020 · N800AY · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PAX DOOR INTERCOSTAL DD4 CORRODED BETWEEN FS 320.163 AND FS 338.963. INSTALLED NEW INTERCOSTAL DD4 ON PAX DOOR BETWEEN FS 320.163 AND FS 338.963, IAW CRJ200 SRM'S 51-42-06 AND 51-42-21. AFTER REMOVING CORRODED INTERCOSTAL AT DD4, IAW CRJ200 SRM'S 51-42-06 A
- [SDR REXA2020092800666](https://openairdocs.org/sdr/REXA2020092800666.md): Skin · corroded · Sep 14, 2020 · N800AY · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PAX DOOR INNER SKIN HAS MULTIPLE AREAS OF CORROSION. REMOVED AND REPLACED PAX DOOR INNER SKIN, IAW CRJ200 SRM'S 51-42- 51-42-21, 51-42-10, 51-42-13 AND 51-42-22.
- [SDR REXA2020092800672](https://openairdocs.org/sdr/REXA2020092800672.md): Seat Track · corroded · Sep 13, 2020 · N800AY · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RIGHT SIDE SEAT RAIL SEGMENT NO 6 BETWEEN FS 499 TO FS 544 IS CORRODED. REMOVED, FABRICATED AND INSTALLED RIGHT SIDE SEAT RAIL SEGMENT AT FS 497 TO FS 544, IAW MHIRJ REO 601R-53-00-055 REV C DATED 2017-03-21 REPAIR B.
- [SDR REXA2020092800670](https://openairdocs.org/sdr/REXA2020092800670.md): Seat Track · corroded · Sep 13, 2020 · N800AY · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK SEGMENT AT LBL 9 BETWEEN FS 409+128 TO FS 559 IS CORRODED. REMOVED UNSERVICEABLE SEAT TRACK. FABRICATED AND INSTALLED SERVICEABLE SEAT TRACK 9 LBL 9 BETWEEN 409 + 128-559 (FS), IAW CRJ200 AMM 53-01-11-020-002/53-01-11-400-802 AND MHIRJ REO 601R-
- [SDR REXA2020092800665](https://openairdocs.org/sdr/REXA2020092800665.md): Angle · corroded · Sep 13, 2020 · N800AY · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PAX DOOR SURROUND STRUCTURE CAP ANGLE BETWEEN FS 319.70 AND FS 345 CORRODED ON MULTIPLE CROSS ANGLE. REMOVED AND REPLACED CAP ANGLE AT PAX DOOR SURROUND STRUCTURE FLOOR SILL, IAW CRJ 200 SRM 51-42-06.
- [SDR REXA2020101300660](https://openairdocs.org/sdr/REXA2020101300660.md): Frame · corroded · Sep 12, 2020 · N800AY · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME AT FS 605 CORRODED BETWEEN STGR 18R AND STGR 24L. BLENDED AREAS ON 605 FRAME LISTED ABOVE, IAW CRJ 200 SRM 51-21-06, 53-61-15, 53-00-00 & 51-25-00. NO DEFECTS NOTED, WITHIN LIMITS.
- [SDR REXA2020092800659](https://openairdocs.org/sdr/REXA2020092800659.md): Intercostal · corroded · Sep 12, 2020 · N800AY · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PAX DOOR INTERCOSTAL DD6 CORRODED BETWEEN FS 320.163 AND 338.963. REMOVED AND REPLACED DD6 INTERCOSTAL, IAW CRJ200 SRM 51-42-06 AND 51-42-21. NO DEFECTS NOTED.
- [SDR REXA2020092800664](https://openairdocs.org/sdr/REXA2020092800664.md): Strap · corroded · Sep 11, 2020 · N800AY · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > STRAP IS CORRODED BETWEEN LBL 36 TO LBL 27 AT FS 559. REMOVED AND REPLACED STRAP LOCATED BETWEEN LBL 36 TO LBL 27 AT FS 559, IAW CRJ 200 SRM 51-42-06 AND CRJ 200 SRM 51-40-11.
- [SDR REXA2019021280139](https://openairdocs.org/sdr/REXA2019021280139.md): Fairing · detached · Feb 8, 2019 · N800AY · Cndair CL6002B19 · Wing, Control Surfaces
  > ON DEPARTURES THROUGH 10,000 AIRCRAFT MADE A THUMP ASSOCIATED WITH A VIBRATION WHICH WAS FELT IN THE FLIGHT CONTROL, PERFORMED AN AIR RETURN TO DEPARTURE AND DISCOVERED RIGHT WING INBOARD FAIRING BROKEN/MISSING. REPLACED RH INBOARD FAIRING, OUTBOARD AND AFT F
- [SDR REXA2018111360197](https://openairdocs.org/sdr/REXA2018111360197.md): Battery Pack · inoperative · Nov 6, 2018 · N800AY · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY LIGHTS BATTERY PACK #1 IS DEAD/INOP REMOVED AND REPLACED EMERGENCY LIGHTS BATTERY PACK #1 IAW CRJ 200 AMM 33-51-04 OPS CHECK GOOD IAW CRJ 200 AMM 33-51-04-710-801 AAR AP 344
- [SDR REXA2018110601086](https://openairdocs.org/sdr/REXA2018110601086.md): Bulkhead · cracked · Nov 6, 2018 · N800AY · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > AFT PRESSURE BULKHEAD HAS A CRACK IN THE WEB UNDER LINER SUPPORT AT RBL 9.50 APPROX WL 78.5. DOT 262A001 REPAIRED AFT PRESSURE BULKHEAD IAW REO 601R-53-61-1285 AND REO # 601R-53-61-6758 AAR SM-139
- [SDR REXA2018110301079](https://openairdocs.org/sdr/REXA2018110301079.md): Torque Box · cracked · Nov 3, 2018 · N800AY · Cndair CL6002B19 · Engine Thrust Reverser
  > #1 ENGINE T/R TORQUE BOX CRACKED ARE HI- LITE FASTNER ON AFT FLANGE @ 6 O'CLOCK POSITION. REPAIRED CRACK IAW ENDEAVOR EA CRJ 254-07814 REV IR AAR SM-35
- [SDR REXA2018111321075](https://openairdocs.org/sdr/REXA2018111321075.md): Frame · cracked · Nov 2, 2018 · N800AY · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME BS 333 IS CRACKED JUST I/B OF STGR 2L, IN THE CABIN. REPAIRED FRAME 333 JUST I/B OF STRINGER 2L IAW CRJ 200 EA CRJ-253-07892 ARR-SM-107
- [SDR REXA2018111311077](https://openairdocs.org/sdr/REXA2018111311077.md): Drag Angle · cracked · Oct 31, 2018 · N800AY · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR AFT DRAG ANGLE IS CRACKED. REPAIRED PAX DOOR AFT DRAG ANGLE IAW BOMBARDIER REO 601R-52-11-513 TYPE 11 AAR SM-23
- [SDR REXA2018111381091](https://openairdocs.org/sdr/REXA2018111381091.md): Bracket · cracked · Oct 28, 2018 · N800AY · Cndair CL6002B19 · Wing, Attach Fittings
  > LEFT WING FRONT SPAR CENTER LEADING EDGE HAS CRACK ON CORNER REMOVED AND REPLACED LEFT WING FRONT SPAR CENTER LEADING EDGE BRACKET IAW CRJ 200 SRM 51-42-06
- [SDR REXA2018111381090](https://openairdocs.org/sdr/REXA2018111381090.md): Latch · cracked · Oct 28, 2018 · N800AY · Cndair CL6002B19 · Accessory Compartment Doors
  > UPPER NOSE COMPARTMENT DOOR HAS CRACK AT LATCH. REPAIRED CRACK ON UPPER NOSE COMPARTMENT DOOR IAW EA NO CRJ 253-07855 AAR SM-33
- [SDR REXA2018102801088](https://openairdocs.org/sdr/REXA2018102801088.md): Floor Support · corroded · Oct 28, 2018 · N800AY · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LH FLOOR LANDING AT LBL 9 HAS CORROSION BETWEEN FS 280 AND FS 260, IN THE FLT DECK. REMOVED AND REPLACED L/H FLOOR LANDING AT LBL9 BETWEEN FS 280 & FS 260 IAW CRJ 200 SRM 51-42-21 51-42-06 AAR SM-107
- [SDR REXA2018111381087](https://openairdocs.org/sdr/REXA2018111381087.md): Floor Support · corroded · Oct 28, 2018 · N800AY · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RH FLOOR LANDING AT RBL 9 HAS CORROSION BETWEEN FS 280 AND FS 260, IN THE FLT DECK. REMOVED AND REPLACED R/H FLOOR LANDING @RBL9 BETWEEN FS 280-FS260. I.A.W. CRJ-200 SRM 51-42-06 AND 51-42-21 AAR SM-107
- [SDR REXA2018111328178](https://openairdocs.org/sdr/REXA2018111328178.md): Frame · cracked · Oct 28, 2018 · N800AY · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME 605 IS CRACKED ON THE FWD SIDE JUST ABOVE AND BELOW STGR 9L, IN THE CARGO BAY. REPAIRED FRAME 605 AT STGR 9L IAW BOMBARDIER REO 601-53-61-5214 AAR AP-377
- [SDR REXA2018111371089](https://openairdocs.org/sdr/REXA2018111371089.md): Bracket · cracked · Oct 27, 2018 · N800AY · Cndair CL6002B19 · Wing, Attach Fittings
  > RH WING LEADING EDGE FRONT SPAR IB REFUEL BRACKET HAS A CRACK REMOVED AND REPLACED REFUEL BRACKET IAW CRJ 200 SRM 51-41-02 AND 51-42-06
- [SDR REXA2018111361080](https://openairdocs.org/sdr/REXA2018111361080.md): Attach Bracket · cracked · Oct 26, 2018 · N800AY · Cndair CL6002B19 · Wing, Attach Fittings
  > RIGHT WING L/E @ WS149.58 HAS CRACKED CORNER BRACKET REMOVED AND REPLACED RIGHT WING L/E CORNER BRACKET AT WS 149.58 IAW CRJ 200 SRM 51-41-02
- [SDR REXA2018102501094](https://openairdocs.org/sdr/REXA2018102501094.md): Seat Track · gouged · Oct 25, 2018 · N800AY · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LT SIDE SEAT RAIL STICK 5 GOUGED AND CORRODED MULTIPLE AREAS. REMOVED AND REPLACED NR 5 LT SEAT RAIL IAW AMM 53-01-11.
- [SDR REXA2018102501093](https://openairdocs.org/sdr/REXA2018102501093.md): Seat Track · gouged · Oct 25, 2018 · N800AY · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LT SIDE SEAT RAIL STICK 7 GOUGED AND CORRODED MULTIPLE AREAS. REMOVED AND REPLACE NR 7 LT SIDE RAIL IAW AMM 53-01-11.
- [SDR REXA2018111351085](https://openairdocs.org/sdr/REXA2018111351085.md): Floorbeam · cracked · Oct 25, 2018 · N800AY · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FLOOR ANGLE STRIP ON THE FWD SIDE OF BEAM 280 IS CRACKED IN 2 SPOTS, JUST I/B OF LBL 9 AND RBL 9, IN THE VERY FWD E & E BAY. REMOVED AND REPLACED FLOOR ANGLE IAW CRJ 200 SRM 51-42-21 AAR SM-107
- [SDR REXA2018111351081](https://openairdocs.org/sdr/REXA2018111351081.md): Seat Track · corroded · Oct 25, 2018 · N800AY · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LH FLOOR SEAT RAIL STICK 5 GOUGED AND CORRODED SEVERAL LOCATIONS. REMOVED AND REPLACED L/H FLOOR SEAT RAIL STICK # 5 IAW CRJ 200 AMM 53-01-11 AAR SM-107
- [SDR REXA2018111341096](https://openairdocs.org/sdr/REXA2018111341096.md): Seat Track · gouged · Oct 24, 2018 · N800AY · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LH SIDE SEAT RAIL STICK 1 GOUGED AND CORRODED MULTIPLE AREAS. REMOVED AND REPLACED SEAT RAIL IAW CRJ 200 AMM 53-01-11. AAR SM-58
- [SDR REXA2018111341083](https://openairdocs.org/sdr/REXA2018111341083.md): Seat Track · corroded · Oct 24, 2018 · N800AY · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RH SIDE SEAT RAIL STICK 2 GOUGED AND CORRODED MULTIPLE AREAS. REMOVED AND REPLACED SEAT RAIL IAW CRJ 200 AMM 53-01-11. AAR SM-58
- [SDR REXA2018111341082](https://openairdocs.org/sdr/REXA2018111341082.md): Seat Track · corroded · Oct 24, 2018 · N800AY · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LH FLOOR SEAT RAIL STICK 2 GOUGED AND CORRODED. REMOVED AND REPLACED L/H FLOOR SEAT RAIL STICK # 2 IAW CRJ 200 AMM 53-01-11
- [SDR REXA2018111323176](https://openairdocs.org/sdr/REXA2018111323176.md): Floor Support · corroded · Oct 23, 2018 · N800AY · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RH SIDE FLOOR SUPPORT HAS CORROSION FS559.00 REMOVED AND REPLACED RH SIDE FLOOR SUPPORT (STRAP) IAW CRJ 200 SRM 51-42-06
- [SDR REXA2018102201095](https://openairdocs.org/sdr/REXA2018102201095.md): Seat Track · gouged · Oct 22, 2018 · N800AY · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RT SIDE SEAT RAIL STICK 7 GOUGED AND CORRODED MULTIPLE AREAS. REMOVED AND REPLACED NR 7 RT SEAT RAIL IAW AMM 53-01-11.
- [SDR REXA2018111321084](https://openairdocs.org/sdr/REXA2018111321084.md): Floor Support · corroded · Oct 22, 2018 · N800AY · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LH SIDE FLOOR SUPPORT HAS CORROSION FS559.00 REMOVED AND REPLACED LH SIDE FLOOR SUPPORT IAW CRJ 200 SRM 51-42-06 AAR-R S/M4
- [SDR REXA2018111391092](https://openairdocs.org/sdr/REXA2018111391092.md): Seat Track · corroded · Oct 19, 2018 · N800AY · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LH SIDE SEAT RAIL STICK 5 CORRODED MULTIPLE AREAS. REMOVED AND REPLACED SIDEWALL SEAT TRACK L/H # 5 IAW CRJ 200 AMM 53-01-11
- [SDR REXA2018092400886](https://openairdocs.org/sdr/REXA2018092400886.md): Seal · missing · Sep 20, 2018 · N800AY · Cndair CL6002B19 · Emergency Equipment
  > FA PBE MISSING 1 SEAL. REPLACED FA PBE MISSING SEAL IAW AMM 25-60-00.
- [SDR REXA2018082970719](https://openairdocs.org/sdr/REXA2018082970719.md): Duct · displaced · Aug 27, 2018 · N800AY · Cndair CL6002B19 · Pneumatic Indicating System
  > RT 14TH DUCT WARNING MESSAGE. QRH COMPLETED. MESSAGE PERSISTED AFTER 40 SECONDS. RIGHT THRUST LEVER REDUCED TO IDLE. LANDING AT FLAPS 20, ON TOUCHDOWN. FOUND THE RT ENGINE COWL ICE, 14TH STG SUPPLY DUCT CLAMP ALIGNMENT OFF. INSTALLED THE SEAL, ALIGNED THE
- [SDR REXA2018040400299](https://openairdocs.org/sdr/REXA2018040400299.md): Fire Warning · false indication · Apr 4, 2018 · N800AY · Cndair CL6002B19 · Fire Detection
  > SMOKE TOILET EICAS & WARNING HEARD, FA CHECKED THE LAVATORY. NO SMOKE NOTED. MESSAGE & WARN WENT AWAY ON ITS OWN AFTER 60 SECONDS. PERFORMED OPS CHECK OF THE LAVATORY SMOKE DETECTION SYSTEM. OPS CHECKED GOOD. NO MESSAGES NOTED. ACFT OKAY FOR SERVICE.
- [SDR REXA2018022800171](https://openairdocs.org/sdr/REXA2018022800171.md): Flashlight · inoperative · Feb 28, 2018 · N800AY · Cndair CL6002B19 · Emergency Equipment
  > CO-PILOT`S FLASHLIGHT INOPERATIVE. REPLACED THE FLASHLIGHT IAW AMM 25-61-00, OPS CHECK GOOD.
- [SDR REXA2017091901015](https://openairdocs.org/sdr/REXA2017091901015.md): Battery · inoperative · Sep 19, 2017 · N800AY · Cndair CL6002B19 · Emergency Equipment
  > PILOT FLASHLIGHT BATTERY DEAD. R & R THE BATTERY IAW AMM 25-61-00. OPS TESTED GOOD.
- [SDR REXA2017042500547](https://openairdocs.org/sdr/REXA2017042500547.md): Oxygen Mask · no test · Apr 25, 2017 · N800AY · Cndair CL6002B19 · Crew Oxygen System
  > FIRST OFFICER`S OXYGEN MASK NOT TESTING CORRECTLY. REMOVED AND REPLACED THE OXYGEN MASK STOWAGE BOX AND OXYGEN MASK IAW AMM 35-11-15, AND AMM 35-11-12. OPS & LEAK CHECKED GOOD. SERVICED CREW OXYGEN IAW AMM 12-16-35 TO 1850 PSI.
- [SDR REXA2017021900257](https://openairdocs.org/sdr/REXA2017021900257.md): Battery Pack · discharged · Feb 19, 2017 · N800AY · Cndair CL6002B19 · Emergency Lighting
  > FOUND EMERGENCY LIGHT LEFT ON EMERGENCY LIGHTS INOPERATIVE. CHARGED THE BATTERY PACK AND PERFORMED OPS CHECK IAW AMM 33-51-00, OPS GOOD.
- [SDR REXA2016081101549](https://openairdocs.org/sdr/REXA2016081101549.md): Bulkhead · cracked · Aug 11, 2016 · N800AY · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > BRAKE CABLE PASSAGE HOLE IS CRACKED ON INBD SIDE AT BS 202.75 BL 23.71. CUT OUT DAMAGE, FABRICATED, AND INSTALLED A REPAIR IAW REO 601R-53-11-2941 AND REO 601R-53-11-563 TYPE 5 REV C. OPS CHECKED GOOD IAW AMM 32-45-00-710-801.

Next page: https://openairdocs.org/aircraft/N800AY/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 = 'N800AY' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N800AY/reports

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