# Service difficulty reports: N836AY

A list on [N836AY](https://openairdocs.org/aircraft/N836AY.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 · 100 reports

- [SDR REXA2021061800418](https://openairdocs.org/sdr/REXA2021061800418.md): Light · inoperative · Jun 15, 2021 · N836AY · Cndair CL6002B19 · Emergency Lighting
  > RH EMERGENCY LIGHT FWD OF EMERGENCY EXIT DOOR INOP "R/R EMERGENCY LIGHT FWD OF EMERGENCY EXIT DOOR REF CRJ200 AMM 33-51-21 PN ON/OFF:GE1817 "
- [SDR REXA2021032200172](https://openairdocs.org/sdr/REXA2021032200172.md): Bulkhead Web · cracked · Mar 14, 2021 · N836AY · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FOUND 3 INDICATIONS: 1) FS 559 WEB O/B RBL 9 WL 58.7 APPROX 90% FSH.5"L; 2) FS 559 CAP ANGLE RADIUS RBL 18 APPROX 80% FSH.25"L; 3) FS 559 CAP ANGLE RADIUS LBL 18 APPROX 55% FSH.5"L FAILS NDT. REPAIRED FS 559 BULKHEAD WEB AND CAP ANGLE IAW ENDEAVOR EA P5302
- [SDR REXA2021032200170](https://openairdocs.org/sdr/REXA2021032200170.md): Hinge · cracked · Mar 14, 2021 · N836AY · Cndair CL6002B19 · Fuselage, Door Hinge
  > AFT BAGGAGE BAY DOOR STEP ASSY FWD HINGE ASSY FOUND CRACKED. REMOVED AND REPLACED FWD HINGE SECTOR IAW CRJ 200 SRM 51-42-06.
- [SDR REXA2021032200168](https://openairdocs.org/sdr/REXA2021032200168.md): Rib · corroded · Mar 14, 2021 · N836AY · Cndair CL6002B19 · Wing, Rib/Bulkhead
  > RH WING OB LEADING EDGE IB END RIB IS CORRODED. REMOVED AND REPLACED RIB IAW CRJ 200 SRM 51-42-06.
- [SDR REXA2021032200161](https://openairdocs.org/sdr/REXA2021032200161.md): Rib · corroded · Mar 14, 2021 · N836AY · Cndair CL6002B19 · Wing, Rib/Bulkhead
  > L/H REAR SPAR RIB AT WS 58.88 CORRODED LOWER FORWARD CORNER. REMOVED AND REPLACED RIB (CHANNEL) IAW CRJ 200 SRM 51-42-21 AND 51-42-06.
- [SDR REXA2021032200171](https://openairdocs.org/sdr/REXA2021032200171.md): Bulkhead · damaged · Mar 12, 2021 · N836AY · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > DURING INCORPORATION OF EO# P53025-559 BULKHEAD REPAIR, WHILE REMOVING/CUTTING EXISTING LOWER CAP ANGLE TECH DRILLED THROUGH SACRIFICIAL PLATE INTO 559.00 BULKHEAD (3 EA. LOCATIONS). "REPAIRED DRILL STRUTS AND MISDRILLED HOLE IN 559 BULKHEAD IAW CRJ 200 REO 6
- [SDR REXA2021032200162](https://openairdocs.org/sdr/REXA2021032200162.md): Spar · corroded · Mar 10, 2021 · N836AY · Cndair CL6002B19 · Wing Spar
  > R/H REAR SPAR RIB AT WS 58.88 CORRODED ON LOWER FORWARD CORNER. "REMOVED AND REPLACED R/H REAR SPAR RIB AT WS 58.88 IAW CRJ 200 SRMS 51-40-11 AND 51-42-20.REFERENCES FOR LINE ITEM #7 AS FOLLOWS: CRJ 200 SRM 51-40-11 AND 51-42-20 AND 51-77-00. "
- [SDR REXA2021032200164](https://openairdocs.org/sdr/REXA2021032200164.md): Retainer · cracked · Mar 5, 2021 · N836AY · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS 280.00 CLIP AT RBL 9 CRACKED. "REMOVED, LOCATED AND DRILLED AND INSTALLED NEW SERVICABLE CLIP IAW CRJ200 SRM 51-42-21 AND 51-40-11. "
- [SDR REXA2021032200166](https://openairdocs.org/sdr/REXA2021032200166.md): Seat Track · gouged · Mar 3, 2021 · N836AY · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RH SIDE SEAT RAIL BETWEEN FS 559+3 AND FS 559+60 ARE GOUGED AND NO CORROSION INHIBITOR VISABLE. FABBED AND REPLACED SEAT TRACK @ FS 559+3 TO 559+60 IAW MHIRJ REO 601R-53-00-055 AND CRJ 200 AMM 53-01-11-000/400-802.
- [SDR REXA2021032200167](https://openairdocs.org/sdr/REXA2021032200167.md): Seat Track · gouged · Mar 1, 2021 · N836AY · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RH SEAT RAIL AT FS 424.00 GOUGED AND NO CORROSION PREVENTATIVE. "REMOVED AND INSTALLED NEW FABBED RH SIDE SEAT RAIL AT FS424.00 IAW BOMBARDIER REO 601R-53-00-764 DATED 2019-10-11 AND CRJ 200 AMM'S 53-01-11-000/400-802. "
- [SDR REXA2021032200165](https://openairdocs.org/sdr/REXA2021032200165.md): Seat Track · gouged · Mar 1, 2021 · N836AY · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RH SIDE SEAT RAIL AT FS 409+112 GOUGED. "REMOVED AND REPLACED RH SIDE SEAT RAIL AT FS409+112 WITH NEW FABRICATED SEAT RAIL IAW BOMBARDIER REO 601R-53-00-055 REV C DATED 2017-03-21 REPAIR B AND CRJ 200 AMM'S 53-01-11-000/400-8802. "
- [SDR REXA2021032200163](https://openairdocs.org/sdr/REXA2021032200163.md): Floorbeam · corroded · Mar 1, 2021 · N836AY · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FS 280.00 FWD J ANGLE HAS MULTIPLE SPOTS OF CORROSION. "REMOVED AND REPLACED FS280 FWD J ANGLE IAW CRJ 200 SRM 51-42-21 & 51-42-06. "
- [SDR REXA2021032200160](https://openairdocs.org/sdr/REXA2021032200160.md): Bracket · corroded · Mar 1, 2021 · N836AY · Cndair CL6002B19 · Emergency Equipment
  > PAX DOOR POWER ASSIST PULLEY BRACKET CORRODED AT FASTENER HOLES. REMOVED AND REPLACED PAX DOOR ASSIST PULLEY BRACKET IAW CRJ 200 SRM 51-40-11 AND CRJ 200 AMM 20-21-00-810-801. REF MWC 8803621 OP 17.
- [SDR REXA2021032200169](https://openairdocs.org/sdr/REXA2021032200169.md): Rib · cracked · Feb 28, 2021 · N836AY · Cndair CL6002B19 · Wing, Rib/Bulkhead
  > RH WING O/B LEADING EDGE O/B END RIB IS CRACKED REMOVED, FABRICATED, AND INSTALLED RIB IAW CRJ 200 SRM 51-24-21 & 51-42-06
- [SDR REXA2021032200159](https://openairdocs.org/sdr/REXA2021032200159.md): Skin · dented · Feb 26, 2021 · N836AY · Cndair CL6002B19 · Wing, Plate/Skin
  > LH OUTBD FLAP BOTTOM SKIN DENTED BETWEEN FS 226.15 AND FS 223 APPROX. 3"" WIDE X 5"" LONG X.020"" DEEP. DENT IN SKIN TO BE.031 DEEP, OUT OF LIMITS IAW CRJ 200 SRM 57-53-00. REPAIRED L/H O/B FLAP F.S. 223 TO F.S. 226.15 IAW CRJ 200 SRM 57-53-00 REPAIR #3.
- [SDR REXA2019120251713](https://openairdocs.org/sdr/REXA2019120251713.md): Bulb · inoperative · Nov 25, 2019 · N836AY · Cndair CL6002B19 · Emergency Lighting
  > FWD OVERWING EMERGENCY EXIT BULB IS INOP REMOVED AND REPLACED BULB IAW AMM 33-51-21 OPS CHECK GOOD
- [SDR REXA2019051900727](https://openairdocs.org/sdr/REXA2019051900727.md): Skin · cracked · May 19, 2019 · N836AY · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN CRACKED 2 PLACES AT NOSE MLG CUTOUT RADIUS @ FS 235. REPAIRED PER CREO 601R-53-11-048 REV "D".
- [SDR REXA2019051900726](https://openairdocs.org/sdr/REXA2019051900726.md): Beam · cracked · May 19, 2019 · N836AY · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS 280 BEAM CRACKED ON LOWER SIDE OUT BOARD OF RBL 9 (TYP). REPAIRED PER GREO 601R-53-11-171 REV "D".
- [SDR REXA2019051700723](https://openairdocs.org/sdr/REXA2019051700723.md): Web · cracked · May 17, 2019 · N836AY · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FWD EQUIPMENT COMPARTMENT FLOOR-WEB CRACKED AT LT FS 191. REPAIRED PER GREO 601R-53-11-081.
- [SDR REXA2019051600725](https://openairdocs.org/sdr/REXA2019051600725.md): Floorbeam · corroded · May 16, 2019 · N836AY · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > SUPPLEMENTAL INFORMATION FS 621/ LBL27 FLOORBEAM FITTING IS CORRODED. REPAIRED FLOORBEAM.
- [SDR REXA2019051300717](https://openairdocs.org/sdr/REXA2019051300717.md): Skin · chafed · May 13, 2019 · N836AY · Cndair CL6002B19 · Engine Collector/Tailpipe/Nozzle
  > LT ENG EXHAUST NOZZLE EXT SKIN HAS FRETTING FROM CONTACT WITH PYLON SEAL. PERFORMED EXHAUST SKIN AND DOUBLER REPAIR IAW EA #CRJ254-08921 REV A.
- [SDR REXA2019051000722](https://openairdocs.org/sdr/REXA2019051000722.md): Intercostal · corroded · May 10, 2019 · N836AY · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > AVIONICS OPENING RT INTERCOSTAL IS CORRODED BEYOND SERVICABLE LIMITS. REPLACED PART WITH NEW PART.
- [SDR REXA2019050700724](https://openairdocs.org/sdr/REXA2019050700724.md): Door Sill · corroded · May 7, 2019 · N836AY · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LT CARGO FLOOR SILL FS 574-621 CORRODED OUT OF SRM LIMITS. REMOVED AND REPLACED SILL IAW SRM 51-42-06 AND REO 601R-53-61-1574.
- [SDR REXA2019050700719](https://openairdocs.org/sdr/REXA2019050700719.md): Support Bracket · cracked · May 7, 2019 · N836AY · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > RT MLG BAY, HYD LINE SUPPORT BRACKET ATTACHED TO PRESSURE FLOOR SKIN AT FS 528.0 RBL25 IS CRACKED. REMOVED AND REPLACED HYD LINE SUPPORT BRACKET IAW SRM 51-42-06.
- [SDR REXA2019050700718](https://openairdocs.org/sdr/REXA2019050700718.md): Angle · cracked · May 7, 2019 · N836AY · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > ANGLE CLIP ON THE I/B SIDE OF LBL 36 AT FS 484 IS CRACKED, IN THE CABIN BELOW THE FLOOR. REPAIRED ANGLE CLIP IAW REO 601R-53-41-059 REV B.
- [SDR REXA2019050500710](https://openairdocs.org/sdr/REXA2019050500710.md): Ring · chafed · May 5, 2019 · N836AY · Cndair CL6002B19 · Engine Cowling System
  > PANEL RACK. LEFT ENGINE CORE COWL PANEL TRAILING EDGE RUB STRIP WORN. REMOVED AND REPLACED CLOSER RING AND RUB STRIP IAW CMM 71-12-01 TASK 71-12-01-300-820-A01.
- [SDR REXA2019050300716](https://openairdocs.org/sdr/REXA2019050300716.md): Fitting · cracked · May 3, 2019 · N836AY · Cndair CL6002B19 · Flight Compartment Windows
  > LT WINDSHIELD SIDE POST BOTTOM O/B CLIP IS CRACKED, IN THE FLT DECK. REMOVED AND REPLACED LT WINDSHIELD O/B SIDE POST BOTTOM CLIP IAW SRM 51-42-21.
- [SDR REXA2019050300713](https://openairdocs.org/sdr/REXA2019050300713.md): Seat Track · corroded · May 3, 2019 · N836AY · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RIGHT HAND SIDE SEAT TRACK STICK #6 HAS CORROSION. REMOVED AND REPLACED RT SIDE SEAT TRACK STICK # 6 IAW AMM 53-01-11.
- [SDR REXA2019050300711](https://openairdocs.org/sdr/REXA2019050300711.md): Fitting · cracked · May 3, 2019 · N836AY · Cndair CL6002B19 · Flight Compartment Windows
  > RT WINDSHIELD SIDE POST BOTTOM O/B CLIP IS CRACKED, IN THE FLT DECK. REMOVED AND REPLACED RT WINDSHIELD SIDEPOST O/B CLIP IAW SRM 51-42-21.
- [SDR REXA2019050200712](https://openairdocs.org/sdr/REXA2019050200712.md): Intercostal · corroded · May 2, 2019 · N836AY · Cndair CL6002B19 · Service Doors
  > AFT EQUIPMENT BAY DOOR 2ND RIB IS BENT AND HAS BARE METAL SPOTS WITH PAINT FLAKING UP. REMOVED AND REPLACED UNSERVICEABLE WEB ON AFT ACCY BAY DOOR IAW SRM 51-42-06.
- [SDR REXA2019050200709](https://openairdocs.org/sdr/REXA2019050200709.md): Angle · chafed · May 2, 2019 · N836AY · Cndair CL6002B19 · Engine Collector/Tailpipe/Nozzle
  > RT ENG EXHAUST NOZZLE FWD T ANGLE EDGE MEMBER CHAFED IN SEVERAL AREAS. REPAIRED RT ENG EXHAUST NOZZLE FWD T ANGLE EDGE (LEADING EDGE) IAW CMM 78-11-00.
- [SDR REXA2019050200701](https://openairdocs.org/sdr/REXA2019050200701.md): Support Bracket · cracked · May 2, 2019 · N836AY · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LT OVERWING PNL SUPPORT BRACKET AT FS449.85 IS CRACKED. REMOVED AND REPLACED LT OVERWING PNL SUPPORT BRACKET (ANGEL) IAW SRM 51-42-06.
- [SDR REXA2019050100715](https://openairdocs.org/sdr/REXA2019050100715.md): Support · cracked · May 1, 2019 · N836AY · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > AC RECEPTACLE BOX CRACKED AT TOP ON FUSELAGE NEED MIRROR TO SEE, INSIDE ADG COMPARTMENT. REMOVED CRACKED BOX AND INSTALLED NEW A/C RECEPTACLE BOX IAW SRM 51-42-06 AND SRM 51-42-21.
- [SDR REXA2019050100714](https://openairdocs.org/sdr/REXA2019050100714.md): Track · corroded · May 1, 2019 · N836AY · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK ON TOP OF LBL 9 HAS CORROSION BETWEEN FS 559+80 AND FS 559+96, IN THE CARGO BAY. REMOVED AND REPLACED SEAT TRACK @LBL9 BETWEEN FS 559+80 TO FS 559+96 IAW AMM 53-01-11.
- [SDR REXA2019050100708](https://openairdocs.org/sdr/REXA2019050100708.md): Stringer · cracked · May 1, 2019 · N836AY · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > STR 3L IS CRACKED JUST AFT OF FRAME 280, IN THE CABIN. REMOVED AND REPLACED STR 3L AFT OF FRAME 280 IAW SRM 51-42-21.
- [SDR REXA2019050100706](https://openairdocs.org/sdr/REXA2019050100706.md): Bulkhead · chafed · May 1, 2019 · N836AY · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > AFT PRESSURE BULKHEAD HAS CHAFING AT 36INCHES FROM FLOOR UP ON RBL18. REPAIRED AFT PRESSURE BULKHEAD 36 ABOVE FLOOR @ RBL 18 IAW REO # 601R-53-61-6962.
- [SDR REXA2019050100705](https://openairdocs.org/sdr/REXA2019050100705.md): Bulkhead · chafed · May 1, 2019 · N836AY · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > AFT PRESSURE BULKHEAD HAS CHAFIN AT 36INCHES FROM FLOOR UP ON RBL36. REPAIRED AFT PRESSURE BULKHEAD 36 ABOVE FLOOR @ RBL 36 IAW REO #601R-53-61-6962.
- [SDR REXA2019050100704](https://openairdocs.org/sdr/REXA2019050100704.md): Bulkhead · chafed · May 1, 2019 · N836AY · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > AFT PRESSURE BULKHEAD HAS CHAFIN AT 36INCHES FROM FLOOR UP ON RBL27. REPAIRED AFT PRESSURE BULHEAD 36 ABOVE FLOOR @ RBL27 IAW REO #601R-53-61-6962.
- [SDR REXA2019050100703](https://openairdocs.org/sdr/REXA2019050100703.md): Seat Track · corroded · May 1, 2019 · N836AY · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK ON TOP OF LBL 9 HAS CORROSION BETWEEN FS 559+112 AND FS 574, IN THE CARGO BAY. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-00-49.
- [SDR REXA2019050100702](https://openairdocs.org/sdr/REXA2019050100702.md): Seat Track · corroded · May 1, 2019 · N836AY · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK ON TOP OF LBL 27 HAS CORROSION BETWEEN FS 559+80 AND FS 559+96, IN THE CARGO BAY. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-00-49.
- [SDR REXA2019042800699](https://openairdocs.org/sdr/REXA2019042800699.md): Skin Panel · gouged · Apr 28, 2019 · N836AY · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > SUPPLEMENTAL INFORMATION EXTERNAL LOWER SKIN PANEL HAS CORROSION AND SCRIBE MARKS IN NO DAMAGE ALLOWED AREAS FS 409+64 TO 409+90: STG 20L-23R. REPAIRED EXTERNAL LOWER SKIN ALONG PANELS 191AB AND 191BB FWD MATING SURFACE INCLUDING BELLY AND FASTENER HOLES IAW E
- [SDR REXA2019042800707](https://openairdocs.org/sdr/REXA2019042800707.md): Panel · damaged · Apr 28, 2019 · N836AY · Cndair CL6002B19 · Engine Cowling System
  > PANEL RACK. LEFT ENGINE COWL PANEL 432-AT TRAILING EDGE KNIFE EDGED. REMOVED AND REPLACED TRAILING EDGE ON PANEL 432AT IAW CMM 71-14-01.
- [SDR REXA2019042800700](https://openairdocs.org/sdr/REXA2019042800700.md): Attach Angle · cracked · Apr 28, 2019 · N836AY · Cndair CL6002B19 · Wing, Attach Fittings
  > LT WING L/E PNL ATTACH ANGLE CRACKED IN RADIUS AT WING TRANSITION SPLICE AREA, WS149.0. REMOVED AND REPLACED CRACKED ANGLE AT WS 149.0 ON LT WING IAW SRM 51-41-02.
- [SDR REXA2019012960067](https://openairdocs.org/sdr/REXA2019012960067.md): Lamp · inoperative · Jan 26, 2019 · N836AY · Cndair CL6002B19 · Emergency Lighting
  > DURING ROUTINE CHECK LH EMERGENCY LIGHT OUT (3RD BACK FROM FRONT OF AIRCRAFT). RELAMPED LH 3RD (GOING BACK) EMERGENCY LIGHT IAW AMM 33-51-21. OPC GOOD.
- [SDR REXA2018052000403](https://openairdocs.org/sdr/REXA2018052000403.md): Oxygen Mask · unwanted deploy · May 20, 2018 · N836AY · Cndair CL6002B19 · Passenger Oxygen System
  > O2 MASK IN LAV DOWN. REINSTALLED O2 MASK IAW AMM 35-21-09. NO FURTHER ISSUES NOTED.
- [SDR REXA2018050100330](https://openairdocs.org/sdr/REXA2018050100330.md): Outflow Valve · malfunctioned · Apr 28, 2018 · N836AY · Cndair CL6002B19 · Pressure Regulator/Outflow Valve
  > CABIN PRESSURE ALT WARNING DURING CLIMB THROUGH 10,000FT. CABIN ALTITUDE WAS GREATER THAN 10,000. FOLLOWED QRH, DESCENDED DOWN TO 10,000. COULDN'T GET CABIN ALT BELOW 8900 IN MAN MODE. PUSHED THE EMERGENCY DEPRESS IAW QRH. FOUND THE OVERBOARD EXHAUST SOV DE
- [SDR REXA2018042750314](https://openairdocs.org/sdr/REXA2018042750314.md): Flashlight Assy · inoperative · Apr 25, 2018 · N836AY · Cndair CL6002B19 · Emergency Equipment
  > DURING PREFLIGHT, FLIGHT ATTENDANT NOTICED THE FLASHLIGHT WAS INOPERATIVE. REMOVED AND REPLACED THE FLASHLIGHT AND HOLDER IAW CMM 25-60-02.
- [SDR REXA2017061300702](https://openairdocs.org/sdr/REXA2017061300702.md): Battery Pack · inoperative · Jun 13, 2017 · N836AY · Cndair CL6002B19 · Emergency Equipment
  > FA FLASHLIGHT NOT BLINKING. REMOVED & REPLACED THE BATTERY PACK IAW AMM 25-61-00. OPS CHECKED GOOD.
- [SDR REXA2017041400504](https://openairdocs.org/sdr/REXA2017041400504.md): Oxygen Bottle · empty · Apr 14, 2017 · N836AY · Cndair CL6002B19 · Portable Oxygen System
  > DURING WAKE-UP, NOTED FWD PORTABLE OXYGEN CYLINDER. HAD 0 PSI. INSTALLED NEW SERVICEABLE PORTABLE OXYGEN BOTTLE IAW AMM 35-31-01 AND T.S. 00340R1. OPS TESTED GOOD.
- [SDR REXA2017012100085](https://openairdocs.org/sdr/REXA2017012100085.md): Defibrillator · inoperative · Jan 21, 2017 · N836AY · Cndair CL6002B19 · Emergency Equipment
  > FA FOUND DEFIBRILLATOR INOPERATIVE. REPLACED DEFIBRILLATOR. ACFT OK FOR SERVICE.

Next page: https://openairdocs.org/aircraft/N836AY/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 = 'N836AY' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N836AY/reports

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