# Service difficulty reports: N536EA

A list on [N536EA](https://openairdocs.org/aircraft/N536EA.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 · 73 reports

- [SDR VNAA2025081111102](https://openairdocs.org/sdr/VNAA2025081111102.md): Unknown · odor · Aug 8, 2025 · N536EA · Cndair CL6002C10 · Air Distribution System
  > BURNING SMELL OBERSEVRED IN THE FLIGHTDECK WHILE AIRPLANE WAS COLD AND DARK WITH GROUND POWER ATTACHED TO AIRPLANE BUT NOT AVAIL. BOTH PACKS OFF. RECRIC FANS ON. LOW PRESSURE AIR NOT ATTACHED. / T/S PER FIM 21-21-00-810-806-A01. NO ABNORMAL SMELL/SMOKE IN COC
- [SDR VNAA2025030611101](https://openairdocs.org/sdr/VNAA2025030611101.md): Door · open · Mar 5, 2025 · N536EA · Cndair CL6002C10 · Doors
  > GROUND COMMUNICATIONS PANEL LEFT OPEN / REMOVED REMAINDER OF HINGE AND REPLACED DOOR ASSY IAW CRJ700 AMM 52-45-31-000/400-801-A01.
- [SDR VNAA2024120411101](https://openairdocs.org/sdr/VNAA2024120411101.md): Acm · unserviceable · Dec 2, 2024 · N536EA · Cndair CL6002C10 · Air Distribution System
  > SMOKE IN COCKPIT AND CABIN WHEN ENGINE WAS SHUT OFF. PILOTS SAID SMELLS LIKE €ŒPACK RELATED SMOKE ISSUE€?. THE LOCATION OF THE SMOKE WAS LOCATED IN BOTH THE COCKPIT AND THE CABIN. THE SOURCE OF THE SMOKE WAS THE LH ACM. THE DURATION OF THE SMOKE LASTED NO MO
- [SDR VNAA2024082811101](https://openairdocs.org/sdr/VNAA2024082811101.md): Wire Harness · faulted · Aug 27, 2024 · N536EA · Cndair CL6002C10 · Landing Gear System Wiring
  > NOSEWHEEL STEERING FAILED COULD NOT RESET IN THE AIR OR ON THE GROUND. / REMOVED AND REPLACED THE NOSEWHEEL STEERING HARNESS IAW CRJ 700 AMM 32-21-01-000/400-803. BITE GOOD. OPS TEST GOOD.
- [SDR VNAA202304261111](https://openairdocs.org/sdr/VNAA202304261111.md): Window · cracked · Apr 25, 2023 · N536EA · Cndair CL6002C10 · Flight Compartment Windows
  > LH WINDOW HEAT CAUTION MSG CYCLED SWITCH MSG CLEARED,BUT SPARKS CAME FROM TERMINAL AND WINDOW BEGAN SHATTERING. REMOVED AND REPLACED LH FLIGHT COMPARTMENT SIDE WINDOW IAW CRJ-700 AMM 56-12-01-000/400-801-A01-PSA. OPS TEST AND LEAK CK GOOD.
- [SDR VNAA202310040012](https://openairdocs.org/sdr/VNAA202310040012.md): Support Angle · corroded · Apr 10, 2023 · N536EA · Cndair CL6002C10 · Vertical Stabilizer
  > BELLY FAIRING SUPPORT ANGLE IS CORRODED AT FS939.00 STGR 27.
- [SDR VNAA202310040011](https://openairdocs.org/sdr/VNAA202310040011.md): Door · gouged · Apr 10, 2023 · N536EA · Cndair CL6002C10 · Vertical Stabilizer
  > FWD CARGO DOOR LOWER OUTER SEAL RETAINER IS GOUGED AND BENT AT SEVERAL LOCATIONS.
- [SDR VNAA202310040010](https://openairdocs.org/sdr/VNAA202310040010.md): Door · chafed · Apr 10, 2023 · N536EA · Cndair CL6002C10 · Vertical Stabilizer
  > FORWARD BAGGAGE BAY DOOR INNER SKIN IS CHAFED AT (2EA) LOCATIONS.
- [SDR VNAA202310040009](https://openairdocs.org/sdr/VNAA202310040009.md): Drag Angle · cracked · Apr 10, 2023 · N536EA · Cndair CL6002C10 · Vertical Stabilizer
  > LH AFT VERTICAL STAB DRAG ANGLE SUSPECTED POSSIBLE CRACK
- [SDR VNAA202310040008](https://openairdocs.org/sdr/VNAA202310040008.md): Door · chafed · Apr 10, 2023 · N536EA · Cndair CL6002C10 · Doors
  > RH OVERWING EMERGENCY EXIT DOOR OUTER SKIN HAS THREE GOUGED AREAS ON EDGE OF THE SKIN AT THE UPPER MID SECTION OF THE DOOR
- [SDR VNAA202310040007](https://openairdocs.org/sdr/VNAA202310040007.md): Stringer · corroded · Apr 10, 2023 · N536EA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STRINGER 26L IS CORRODED BETWEEN FS 310.00 AND 333.00.
- [SDR VNAA202310040006](https://openairdocs.org/sdr/VNAA202310040006.md): Frame · corroded · Apr 10, 2023 · N536EA · Cndair CL6002C10 · Fuselage Main, Frame
  > UPON REMOVAL OF FRAME SECTION 319 FOUND EXCESSIVE CORROSION ON ATTACH FLANGE REQUIRES REPAIR
- [SDR VNAA202310040005](https://openairdocs.org/sdr/VNAA202310040005.md): Hinge · worn · Apr 10, 2023 · N536EA · Cndair CL6002C10 · Passenger/Crew Doors
  > DURING INSTALLATION OF THE PASSENGER DOOR, FOUND EXCESSIVE DOOR PLAY AT THE HINGE ATTACHMENT POINT WITH NEW PIN INSTALLED.
- [SDR VNAA202327030004](https://openairdocs.org/sdr/VNAA202327030004.md): Door · unknown · Mar 27, 2023 · N536EA · Cndair CL6002C10 · Fuselage Main, Frame
  > IS67052110200 IMPROVED CORROSION RESISTANCE OF PHASE IV PAX DOOR, REQUIRES COMPLETION.
- [SDR VNAA202327030003](https://openairdocs.org/sdr/VNAA202327030003.md): Door · unknown · Mar 27, 2023 · N536EA · Cndair CL6002C10 · Fuselage Main, Frame
  > SB 670BA-52-042 PAX DOOR MODIFICATION TO THE INSTALLATION OF ACCESS PANELS AND COVERS, REQUIRES COMPLETION.
- [SDR VNAA202327030002](https://openairdocs.org/sdr/VNAA202327030002.md): Stringer · corroded · Mar 27, 2023 · N536EA · Cndair CL6002C10 · Fuselage Main, Frame
  > STRINGER 25R IS CORRODED IN MULTIPLE LOCATIONS BETWEEN FS 280.00 AND 333.00.
- [SDR VNAA202327030001](https://openairdocs.org/sdr/VNAA202327030001.md): Frame · corroded · Mar 27, 2023 · N536EA · Cndair CL6002C10 · Fuselage Main, Frame
  > FRAME AT FS 310.00 IS CORRODED BETWEEN STGR 24L AND 26R.
- [SDR VNAA202210299990](https://openairdocs.org/sdr/VNAA202210299990.md): None · corroded · Oct 19, 2022 · N536EA · Cndair CL6002C10 · Aircraft Structures
  > C.O. 10315122 JOB21031511, OP 90 AFT CARGO DOOR SILL PLATE HAS MINOR CORROSION WITH ATTENTION TO BE AROUND THE CARGO DOOR STOP FITTINGS CORRECTIVE ACTION:. REMOVED AND REPLACED AFT CARGO SILL PLATE IAW CRJ700 SRM 51-42-06-001-001-A01, 51-42-13-001-00
- [SDR VNAA202203241111](https://openairdocs.org/sdr/VNAA202203241111.md): Engine · vibration · Mar 22, 2022 · N536EA · Cndair CL6002C10 · Engine (Turbine/Turboprop)
  > 5206/22MAR CLT-LFT TAIL 536 ENGINE VIBE WARNING, FOLLOWED QRH, UNABLE TO CLIMB FURTHER. RETURNING TO CLT. EMERGENCY DECLARED 0235Z ENGINE VIBE WENT UP TO 2.0 LANDED OVERWEIGHT, BUT WITHOUT FURTHER/OTHER ISSUE 70.4 - 70 LANDING WEIGHT. L ENGINE VIB WENT TO 2.0
- [SDR VNAA202203081115](https://openairdocs.org/sdr/VNAA202203081115.md): Proximity Sensor · out of rig · Mar 6, 2022 · N536EA · Cndair CL6002C10 · Landing Gear Position and Warning
  > SHORTLY AFTER TAKE OFF THE CREW RECEIVED A GEAR DISAGREE MESSAGE. THEY RAN THE QRH AND RETURNED TO DAY. CLIMB GEAR DISAGREE WARNING RAN QRC/QRH MESSAGE EXTINGUISHED RTF. INITIAL MSG APPEARED AROUND 600 FT WITH A PROX SYS 1 FAULT S MSG. THEY WERE NOT OVERWEIGH
- [SDR VNAA202203081111](https://openairdocs.org/sdr/VNAA202203081111.md): Wire Harness · unserviceable · Mar 3, 2022 · N536EA · Cndair CL6002C10 · Landing Gear Position and Warning
  > RETURN TO FIELD FOR GEAR DISAGREE ON TAKEOFF. EMERGENCY DECLARED. CONTINUED TROUBLESHOOTING GEAR DISAGREED MASTER WARNING IAW CRJ 700 FIM 32-61-05-810-828 B1-007412. REMOVED AND REPLACED WOW CENTER HARNESS ASSY (RH) IAW CRJ 700 AMM 32-61-05-000/400-805. RIGGIN
- [SDR VNAA202108121111](https://openairdocs.org/sdr/VNAA202108121111.md): Panel · scratched · Aug 10, 2021 · N536EA · Cndair CL6002C10 · Fuselage Main, Structure
  > DURING ROUTINE OPERATIONS, MAINTENANCE DISCOVERED MULTIPLE SCRATCHES TO THE ADG PANEL (P/N CC670-33109-3). THE PANEL IS FABRICATED FROM 2024-T42.100€? AND IS MILLED DOWN TO.058€? IN THE DAMAGED AREA. THE REPORTED SCRATCH DEPTHS ARE 0.003€? €“ 0.007€? /
- [SDR SIMA2020010821604](https://openairdocs.org/sdr/SIMA2020010821604.md): Skin · cracked · Dec 16, 2019 · N536EA · Cndair CL6002C10 · Passenger/Crew Doors
  > PASSENGER DOOR AFT SIDE SKIN HAS MULTIPLE CRACKS AT THE DOOR ASSIST MOTOR SUPPORT WEB-C/A-REMOVED AND REPLACED PASSENGER DOOR AFT SKIN IAW SRM 51-42-06.
- [SDR SIMA2019122411003](https://openairdocs.org/sdr/SIMA2019122411003.md): Stringer · corroded · Dec 11, 2019 · N536EA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STR 25R IS CORRODED BETWEEN FS 280.00 AND 293.00-C/A-REMOVED AND REPLACED STR 25R BETWEEN FS280 AND FS-293 IAW SRM 51-42-06.
- [SDR SIMA2019122010001](https://openairdocs.org/sdr/SIMA2019122010001.md): Floorbeam · corroded · Dec 10, 2019 · N536EA · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > LH CROSSBEAM AT FS 280.00 IS CORRODED IN NUMEROUS AREAS BEWTEEN DRIP TRAY AND THE UPPER L ANGLE.-C/A-COMPLETED LH FS280.00 CROSSBEAM INSTALLATION IAW SRM 53-11-10 AND 51-42-06
- [SDR SIMA2019122010002](https://openairdocs.org/sdr/SIMA2019122010002.md): Floorbeam · corroded · Dec 10, 2019 · N536EA · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > RH CROSSBEAM AT FS 280.00 IS CORRODED IN NUMEROUS AREAS BEWTEEN DRIP TRAY AND THE UPPER L ANGLE.-C/A-RH FS280.00 CROSSBEAM INSTALLATION IAW SRM 53-11-10 AND 51-42-06
- [SDR SIMA2019122309006](https://openairdocs.org/sdr/SIMA2019122309006.md): Floorbeam · cracked · Dec 9, 2019 · N536EA · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > LH CENTER COCKPIT FLOOR BEAM AT BL12.00 IS CRACKED, LOCATED JUST FWD OF CROSSBEAM AT FS280.OO-C/A-REPAIRED L/H CENTER COCKPIT FLOOR BEAM AT BL 12.00 JUST FWD OF FS 280.-00 IAW SRM 53-11-43 AND ETN CR-53-088.
- [SDR SIMA2019122309008](https://openairdocs.org/sdr/SIMA2019122309008.md): Floorbeam · cracked · Dec 9, 2019 · N536EA · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > RH CENTER COCKPIT FLOOR BEAM AT BL12.00 IS CRACKED, LOCATED JUST FWD OF CROSSBEAM AT FS280.OO-C/A-REPAIRED R/H CENTER COCKPIT FLOOR BEAM AT BL 12.00 JUST FWD OF FS 280.-00 IAW SRM 53-11-43 AND ETN CR-53-088.
- [SDR SIMA2019122309007](https://openairdocs.org/sdr/SIMA2019122309007.md): Angle · cracked · Dec 9, 2019 · N536EA · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR HAS A CRACK ON THE AFT ANGLE, ON PREVIOUS REPAIR-C/A-REPAIRED AFT DRAG ANGLE IAW SRM 52-11-04-201-002-A01.
- [SDR SIMA2019082219006](https://openairdocs.org/sdr/SIMA2019082219006.md): Indication Sys · unknown · Aug 19, 2019 · N536EA · Cndair CL6002C10 · Engine Oil Temperature
  > AT LEVEL OFF 13,000' 0 LEFT OIL TEMP WENT AMBER AND RED. WENT IDLE, TEMP WENT BACK AMBER, THEN WENT 147-149 AFTER 10 MIN TEMP STAYED 135 TO 137. TAXI, TAFF, CLIMB NORMAL OPS. CHECKED IAW FIM 79-30-00-810-810 RAR #1 ENGINE OIL LEVEL/OIL TEMPERATURE SENSOR IA
- [SDR SIMA201902198002](https://openairdocs.org/sdr/SIMA201902198002.md): Hydraulic System · contaminated · Feb 18, 2019 · N536EA · Cndair CL6002C10 · Hydraulic System, Main
  > GEAR DISAGREE WARNING AFTER GEAR RETRACTION ON T/O-C/A-T/S AND FOUND B CODE B1-0060112 IN THE MDC FOUND A LARGE AMOUNT OF AIR IN THE #3 HYD SYSTEM PERFORMED BLEEDING OF THE #3 HYD SYSTEM IAW CRJ 700 AMM 29-10-00 OPT'S CHECKED LANDING GEAR IAW CRJ 700 AMM 32-30
- [SDR SIMA201902043001](https://openairdocs.org/sdr/SIMA201902043001.md): Sensor · out of adjust · Feb 3, 2019 · N536EA · Cndair CL6002C10 · Landing Gear Position and Warning
  > PROX SYS FAULT STATUS MSG. AFTER X-LIST FOR GEAR DISAGREE WARNING MSG. GEAR DISAGREE WARNING MSG. AFTER T/0.-C/A-FOUND NG CENTRD #2 SNSR/OUT-OF-RIG/REASON-FAR 007412. C/W CRJ-700 FIM 32-61-05-810-828. ADJUSTED PX37 SENSOR IAW CRJ-700 AMM 32-61-05. PERFORMED OP
- [SDR SIMA2018101211002](https://openairdocs.org/sdr/SIMA2018101211002.md): Unknown · smoke · Oct 11, 2018 · N536EA · Cndair CL6002C10 · Air Distribution System
  > CABIN FILLED W/ SMOKE WITH BOTH ENGINES OFF. SMELL OF ELECTRICALSMOKE. -C/A-PERFORMED OPS CHECK OF CAIN INTERNAL LIGHTS IAW AMM 33-21-01 AND 33-2-09 OPS CHECKS GOOD NO DEFECTS NOTED PERFORMED OPS CHECK OF PACK SYSTEM IAW AMM 21-51-00 OPS CHECK GOOD NO DEFECTS
- [SDR SIMA201806186005](https://openairdocs.org/sdr/SIMA201806186005.md): Manifold · failed · Jun 16, 2018 · N536EA · Cndair CL6002C10 · Landing Gear Steering System
  > DECLARED AN EMERGENCY, NOSE WHEEL STEERING INOPERATIVE. R & R THE NLG STEERING MANIFOLD IAW AMM 32-51-50. OPS CHECKED GOOD
- [SDR SIMA20180320006](https://openairdocs.org/sdr/SIMA20180320006.md): Circuit Board · damaged · Mar 20, 2018 · N536EA · Cndair CL6002C10 · Air Distribution System
  > STRONG ELECTRICAL BURNING ODOR IN THE FLIGHT DECK, ON ARRIVAL AT AC GPU WAS PLUGGED IN WITH BATTERY SWITCH OFF. REMOVED LT DCPC AND INSPECTED FOR DAMAGE TO THE BACK AND FACE OF BOARD. CLEANED AND REASSEMBLED IAW CMM 24-63-10. REINSTALLED THE LT DCPC IAW AMM
- [SDR SIMA20180318002](https://openairdocs.org/sdr/SIMA20180318002.md): Pcb · burned · Mar 18, 2018 · N536EA · Cndair CL6002C10 · Battery/Charger System
  > WHEN FO FIRST ARRIVED AT THE ACFT, NOTICED THE BATTERY MASTER SWITCH WAS LEFT ON. ELECTRICAL ODOR WAS PRESENT. GPU PLUGGED IN BUT NOT SELECTED. REMOVED AND REPLACED THE MAIN BATTERY AND APU BATTERY. ALL OPS CHECKED GOOD. REMOVED AND REPLACED THE LEFT DCPC
- [SDR SIMA2017101111002](https://openairdocs.org/sdr/SIMA2017101111002.md): Tire · failed · Oct 9, 2017 · N536EA · Cndair CL6002C10 · Tire
  > NR 2 TIRE TREAD SEPARATION, LEFT MAIN GEAR FLAT. REMOVED AND REPLACED THE NR 2 MAIN WHEEL ASSY IAW WORKCARD 32-002.
- [SDR SIMA20170810002](https://openairdocs.org/sdr/SIMA20170810002.md): Fan · failed · Aug 10, 2017 · N536EA · Cndair CL6002C10 · Central Display
  > STRONG BURNED ELECTRICAL LIKE ODOR WHEN ENTERING COCKPIT. DETERMINED SMELL COMING FROM AVIONICS DISPLAY FAN 2. REMOVED AND REPLACED DISPLAY SUPPLY FAN NR 2 IAW AMM 21-24-12. OPS CHECKED GOOD.
- [SDR SIMA20170730001](https://openairdocs.org/sdr/SIMA20170730001.md): Light · intermittent · Jul 30, 2017 · N536EA · Cndair CL6002C10 · Emergency Lighting
  > EMERGENCY LIGHTS ON STATUS INTERMITTENT, EVEN WITH EMERGENCY LIGHTS SWITCH OFF. PERFORMED AND OPERATIONAL TEST OF THE EMERGENCY LIGHTS IAW AMM 33-51-00, OPS CHECKED GOOD.
- [SDR SIMA20170320003](https://openairdocs.org/sdr/SIMA20170320003.md): Bulb · inoperative · Mar 20, 2017 · N536EA · Cndair CL6002C10 · Emergency Lighting
  > LT EXTERIOR OVERWING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE BULB IAW 33-51-15. OPS CHECKED ALL EXTERIOR EMERGENCY LIGHTS, OPS CHECKED GOOD.
- [SDR SIMA20170206001](https://openairdocs.org/sdr/SIMA20170206001.md): Target · out of adjust · Feb 6, 2017 · N536EA · Cndair CL6002C10 · Landing Gear Position and Warning
  > GEAR DISAGREE, LANDING GEAR LEVER UP AFTER TAKE OFF. TROUBLESHOT TO RT NLG CENTERING PROX TARGET (PX37) AND HARDWARE. REPLACED HARDWARE WITH SERVICEABLE AND ADJUSTED TARGET IAW AMM32-61-05. OPS CHECK AND GEAR SWINGS GOOD.
- [SDR SIMA20161020005](https://openairdocs.org/sdr/SIMA20161020005.md): Frame · corroded · Oct 20, 2016 · N536EA · Cndair CL6002C10 · Fuselage Main, Frame
  > FRAME BS 319.7 IS CORRODED BETWEEN STRINGERS 25L AND 26R. REPAIRED THE FRAME IAW ERS-CR-53MR-2365.
- [SDR SIMA20161020006](https://openairdocs.org/sdr/SIMA20161020006.md): Frame · corroded · Oct 20, 2016 · N536EA · Cndair CL6002C10 · Fuselage Main, Frame
  > FRAME BS 310 IS CORRODED BETWEEN STRINGERS 24L AND 26R. REPAIRED THE FRAME BS 310 IAW ERS-CR-53MR-2366.
- [SDR SIMA20161020004](https://openairdocs.org/sdr/SIMA20161020004.md): Frame · corroded · Oct 20, 2016 · N536EA · Cndair CL6002C10 · Fuselage Main, Frame
  > FRAME BS 295 IS CORRODED BETWEEN STRINGERS 25L AND 25R. REPAIRED THE FRAME IAW ERS-CR-53MR-2367.
- [SDR SIMA20161019006](https://openairdocs.org/sdr/SIMA20161019006.md): Stand Off · cracked · Oct 19, 2016 · N536EA · Cndair CL6002C10 · Nacelle/Pylon Miscellaneous Structure
  > LEFT UPPER TRANSCOWL FWD STANDOFF CRACKED. REMOVED AND REPLACED THE STANDOFF IAW ETN-CR-54-015R1 AND SRM 51-42-14 & 51-42-21.
- [SDR SIMA20161019003](https://openairdocs.org/sdr/SIMA20161019003.md): Drag Angle · cracked · Oct 19, 2016 · N536EA · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR AFT SIDE DRAG ANGLE HAS A 1.25 INCH CRACK. DRAG ANGLE REPAIRED IAW SRM 52-11-04
- [SDR SIMA20161019004](https://openairdocs.org/sdr/SIMA20161019004.md): Stand Off · cracked · Oct 19, 2016 · N536EA · Cndair CL6002C10 · Nacelle/Pylon Miscellaneous Structure
  > RT UPPER TRANSCOWL FWD INBD STANDOFF CRACKED. REPLACED THE STANDOFF IAW ETN-CR-54-015R1.
- [SDR SIMA20161019005](https://openairdocs.org/sdr/SIMA20161019005.md): Stand Off · cracked · Oct 19, 2016 · N536EA · Cndair CL6002C10 · Nacelle/Pylon Miscellaneous Structure
  > LT UPPER TRANSCOWL AFT STANDOFF CRACKED. REMOVED AND REPLACED STANDOFF IAW ETN-CR-54-015R1 AND SRM 51-42-14 & 51-42-21.
- [SDR SIMA20160809001](https://openairdocs.org/sdr/SIMA20160809001.md): Cable · malfunctioned · Aug 9, 2016 · N536EA · Cndair CL6002C10 · Passenger/Crew Doors
  > CABIN DOOR HARD TO OPEN. R & R MAIN DOOR ICE BRAKE CABLE IAW AMM 52-11-15. OPS CHECKED GOOD.
- [SDR SIMA20141102004](https://openairdocs.org/sdr/SIMA20141102004.md): Pitot Line · contaminated · Nov 2, 2014 · N536EA · Cndair CL6002C10 · Pitot/Static System
  > 10 KT SPLIT BETWEEN CAPTAIN & FIRST OFFICER`S AIRSPEED INDICATIONS DURING APPROACH. INSPECTED DRAIN LINES FOR CONTAMINATION. FOUND WATER IN NR 1 PITOT DRAIN LINE. REMOVED WATER IAW MM 34-11-00. OPERATIONS CHECKED GOOD. NO PRIOR PIREPS NOTED. ACFT ELIGIBL

Next page: https://openairdocs.org/aircraft/N536EA/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 = 'N536EA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N536EA/reports

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