# Service difficulty reports: N516AE

A list on [N516AE](https://openairdocs.org/aircraft/N516AE.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 · 115 reports

- [SDR VNAA2026040950046](https://openairdocs.org/sdr/VNAA2026040950046.md): Skin · chafed · Mar 30, 2026 · N516AE · Cndair CL6002D24 · Ailerons
  > TEMP TO PERM DISPOSITION FOR BLENDED CHAFE DAMAGE TO THE LH IBD TRAILING EDGE LOWER SKIN PANEL EDGE MEMEBER.
- [SDR VNAA2026040920491](https://openairdocs.org/sdr/VNAA2026040920491.md): Skin · dented · Mar 30, 2026 · N516AE · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > DENT OF FUSELAGE. LOCATION FS 485
- [SDR VNAA2026040920489](https://openairdocs.org/sdr/VNAA2026040920489.md): Skin · dented · Mar 30, 2026 · N516AE · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > DENT OF FUSELAGE. LOCATION FS 409-421 STGR 19RH
- [SDR VNAA2026040920488](https://openairdocs.org/sdr/VNAA2026040920488.md): Skin · dented · Mar 30, 2026 · N516AE · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > DENT OF FUSELAGE. LOCATION FS 394-409 STGR 17RH (BELOW WINDOW 2 RH)
- [SDR VNAA2026040920487](https://openairdocs.org/sdr/VNAA2026040920487.md): Skin · dented · Mar 30, 2026 · N516AE · Cndair CL6002D24 · Passenger/Crew Doors
  > SKIN OUTER PAX DOOR HAS A DENT. LOCATION FS333, STRG 6-5LH.
- [SDR VNAA2026040920486](https://openairdocs.org/sdr/VNAA2026040920486.md): Skin · dented · Mar 30, 2026 · N516AE · Cndair CL6002D24 · Service Doors
  > DENT ON SERVICE DOOR SKIN, OUTER FS333, BETWEEN STRG14-13.
- [SDR VNAA2026040920126](https://openairdocs.org/sdr/VNAA2026040920126.md): Slat Track · chafed · Mar 27, 2026 · N516AE · Cndair CL6002D24 · Leading Edge Devices
  > RH WING SLAT 1 TRACK 1 WEAR ON UPPER SURFACE. LOCATION 14" FROM SLAT ATTACHMENT POINT.
- [SDR VNAA2026040920125](https://openairdocs.org/sdr/VNAA2026040920125.md): Slat Track · chafed · Mar 27, 2026 · N516AE · Cndair CL6002D24 · Leading Edge Devices
  > RH WING SLAT 2 TRACK 1 WEAR ON UPPER SURFACE. LOCATION 12.5" FROM SLAT ATTACHMENT POINT.
- [SDR VNAA2026040920123](https://openairdocs.org/sdr/VNAA2026040920123.md): Slat Track · chafed · Mar 27, 2026 · N516AE · Cndair CL6002D24 · Leading Edge Devices
  > LH WING SLAT 1 TRACK 1 HAS DAMAGE.
- [SDR VNAA2026040920127](https://openairdocs.org/sdr/VNAA2026040920127.md): Slat Track · gouged · Mar 27, 2026 · N516AE · Cndair CL6002D24 · Leading Edge Devices
  > RH SLAT 3 TRACK OBD HAS 3 SMALL GOUGES ON THE FLANGES OF THE TRACK UPPER SURFACE.
- [SDR VNAA2026040950052](https://openairdocs.org/sdr/VNAA2026040950052.md): Skin · damaged · Mar 27, 2026 · N516AE · Cndair CL6002D24 · Trailing Edge Flaps
  > DAMAGE ON SKIN LH OBD FLAP FS179.96 UPR BAY.
- [SDR VNAA2026040920559](https://openairdocs.org/sdr/VNAA2026040920559.md): Cradle · worn · Mar 27, 2026 · N516AE · Cndair CL6002D24 · Trailing Edge Flaps
  > R/H INBOARD FLAP, VANE ACTUATOR CRADLE ASSY, L/H INSIDE TRACK SHOWS WEAR.
- [SDR VNAA2026040920149](https://openairdocs.org/sdr/VNAA2026040920149.md): Crossbeam · corroded · Mar 27, 2026 · N516AE · Cndair CL6002D24 · Fuselage Main, Structure
  > CORROSION FOUND ON CROSSBEAM FS333 RH SIDE 5 IN FROM EDGE OF THE MEMBER P/N:SH670-32127-5.
- [SDR VNAA2026040920122](https://openairdocs.org/sdr/VNAA2026040920122.md): Slat Track · gouged · Mar 27, 2026 · N516AE · Cndair CL6002D24 · Leading Edge Devices
  > LH WING, SLAT 3 OBD TRACK HAS 4 MARKS IN TRACK UPPER SURFACES OF FLANGES.
- [SDR VNAA2026040920077](https://openairdocs.org/sdr/VNAA2026040920077.md): Floorbeam · corroded · Mar 27, 2026 · N516AE · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > DURING MAINTENANCE INTERGRANULAR CORROSION WAS FOUND ON BEAM LOCATED AT FLOOR SUPPORT STRUCTURE FS280. ALL CROSS THE UPPER SURFACE OF BEAM, WL72.5. ADJACENT FINDING OF CORROSION ON ANGLE CAPS LBL11.128 FS280 AND RBL11.128
- [SDR VNAA2026040920230](https://openairdocs.org/sdr/VNAA2026040920230.md): Door · corroded · Feb 27, 2026 · N516AE · Cndair CL6002D24 · Passenger/Crew Doors
  > MULTIPLE SPOTS OF BUBBLING/FLAKING PAINT IN INTERNAL PAX DOOR.
- [SDR VNAA2026040920076](https://openairdocs.org/sdr/VNAA2026040920076.md): Crossbeam · corroded · Feb 12, 2026 · N516AE · Cndair CL6002D24 · Fuselage Main, Structure
  > FS 280 CROSSBEAM HAS SIGNIFICANT CORROSION ACROSS THE UPPER SURFACES.
- [SDR VNAA2025052711101](https://openairdocs.org/sdr/VNAA2025052711101.md): Fairing · missing · May 24, 2025 · N516AE · Cndair CL6002C10 · Trailing Edge Flaps
  > RH INBOARD 2ND FLAP FAIRING MISSING, LOST IN FLIGHT / REMOVED WHAT WAS LEFT OF PANEL 686BB ON RH WING INBD FLAP IAW CRJ 700 AMM 57-51-84-000-802-A01.
- [SDR VNAA2024041711101](https://openairdocs.org/sdr/VNAA2024041711101.md): Pcu · faulted · Apr 13, 2024 · N516AE · Cndair CL6002C10 · Drag Control System
  > OB FLT SPLRS AND OB SPOILERONS CAUTION MSG IN FLIGHT / T/S PER CRJ 700 FIM 27-64-01-810-807-A01-PSA, FAULT DID NOT RETURN. OPS TEST GOOD IAW CRJ 700 AMM 27-64-00-710-801-A01. REMOVED AND REPLACED LH OB MFS PCU IAW CRJ700 AMM27-62-01-000/400-801-A01-PSA. OPS AN
- [SDR VNAA2023121811101](https://openairdocs.org/sdr/VNAA2023121811101.md): Compensator · unserviceable · Dec 15, 2023 · N516AE · Cndair CL6002C10 · Fuel Indicating System
  > AUTO XFLOW INHIB STATUS CLIMBING THRUGH 16000 FT. LOST LEFT FUEL TANK AND TOTAL FUEL INDICATION. / REMOVED AND REPLACED LH WING FUEL QUANITY PROBE 6 IAW CRJ AMM 28-41-09-000/400-801
- [SDR VNAA202204141111](https://openairdocs.org/sdr/VNAA202204141111.md): Track · broken · Apr 13, 2022 · N516AE · Cndair CL6002C10 · Engine Thrust Reverser
  > RH UPPER IB TRANSCOWL NYLON TRACK IS BROKEN. PERFORMED EA21-C7-78-710 AS TEMPORARY CORRECTIVE ACTION WITH EDDY CURRENT INSPECTION OF RH UPPER HINGE BEAM TRACK INSERT FASTENER HOLES IN ACCORDANCE WITH NDTM 51-20-006. NO CRACKS FOUND. PERFORMED REO 670-78-30-92
- [SDR VNAA202109281111](https://openairdocs.org/sdr/VNAA202109281111.md): Spoiler Sys · malfunctioned · Sep 25, 2021 · N516AE · Cndair CL6002C10 · Drag Control System
  > ON FINAL APPROACH INTO CLT, THE AIRCRAFT OB SPOILERONS AND OB FLIGHT SPOILERS FAILED. THE FLIGHT CREW DECLARED EMERGENCY, AND LANDED THE AIRCRAFT SAFELY. EMERGENCY VEHICLES ROLLED, HOWEVER THEY WERE NOT NEEDED AS THE CREW CANCELLED THE EMERGENCY ONCE THEY WERE
- [SDR VNAA202108191114](https://openairdocs.org/sdr/VNAA202108191114.md): Valve · stuck · Aug 18, 2021 · N516AE · Cndair CL6002C10 · Aircraft Fuel Distribution System
  > AFTER TAKE OFF FROM CLT THE CREW REPORTED A FUEL LEAK TO DISPATCH. THE CREW RETURNED THE FLIGHT TO CLT AND DECLARED A FUEL EMERGENCY. THEY LANDED SAFELY AND TAXIED TO THE GATE. THEY DID NOT LAND OVERWEIGHT. THE AIRCRAFT IS CURRENTLY IN MAINTENANCE. / CREW REPO
- [SDR VNAA202107211112](https://openairdocs.org/sdr/VNAA202107211112.md): Windshield · smoke · Jul 18, 2021 · N516AE · Cndair CL6002C10 · Flight Compartment Windows
  > SINGLE PUFF OF SMOKE FROM CENTER FRONT WINDSHIELD. PERFORMED GVI/DAMAGE CHECK OF WINDSHIELDS IAW CRJ 700 AMM 56-11-01-210-801-PSA AND OPS CHECKED WINDSHIELD HEAT IAW CRJ 700 AMM 30-41-06-710-801, NO SIGNS OF DAMAGE OR FAULTS FOUND.
- [SDR VNAA202107211111](https://openairdocs.org/sdr/VNAA202107211111.md): Windshield · unserviceable · Jul 18, 2021 · N516AE · Cndair CL6002C10 · Flight Compartment Windows
  > AFTER TAKEOFF THE CREW STARTED TO SEE SMOKE ALONG THE FLIGHT DECK WINDOWS. THEY DECLARED EMERGENCY AND TURNED AROUND TO RETURN TO CLT. CAPTAIN DID NOT SPECIFY WHETHER OR NOT THEY WERE OVERWEIGHT ON LANDING. PASSENGERS DID NOT BRACE. FLIGHT RETURNED TO E19 AND
- [SDR VNAA202104019993](https://openairdocs.org/sdr/VNAA202104019993.md): Stringer · corroded · Apr 1, 2021 · N516AE · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > REMOVED CORROSION AT F.S. 319 STR 27 MATERIAL LOST.001 FOUND WITHIN LIMITS IAW CRJ-700 SRM 53-21-06. TREAT AND PRIME IAW SRM 51-21-11 (LEVEL 2 CPCP)
- [SDR VNAA202104019994](https://openairdocs.org/sdr/VNAA202104019994.md): Drag Angle · corroded · Apr 1, 2021 · N516AE · Cndair CL6002C10 · Vertical Stabilizer
  > REPAIRED L/H DRAG ANGLE/AFT END @VERTICAL STABILIZER IAW BEMBARDRER REO 670-55-31-018
- [SDR VNAA202104019991](https://openairdocs.org/sdr/VNAA202104019991.md): Stringer · corroded · Apr 1, 2021 · N516AE · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > REPAIRED FRAME AT F.S. 517 BETWEEN STR 24L - 24R IAW EA21-C7-53-111. (LEVEL 2 CPCP) LEVEL 2 CORROSION.
- [SDR VNAA202104019992](https://openairdocs.org/sdr/VNAA202104019992.md): Stringer · corroded · Apr 1, 2021 · N516AE · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > BLEND OUT CORROSION IAW CRJ-700 SRM 51-21-06 AND EA 21-C7-53-139. RESTORED FINISH IAW CRJ-700 SRM 51-21-11, 51-25-01 & EA 21-C7-53-139. LEVEL 2 CORROSION.
- [SDR VNAA2021011810111](https://openairdocs.org/sdr/VNAA2021011810111.md): Unknown · odor · Jan 14, 2021 · N516AE · Cndair CL6002C10 · Air Distribution System
  > IN FLIGHT TOXIC ODOR WAS NOTICED MAKING IT DIFFICULT TO BREATH ODOR CONTINUED THROUGHOUT ENTIRE FLIGHT FLIGHT DECK ONLY. PRESSURIZED LT AND RT PACK WITH APU AND RT ENGINE, IAW CRJ 700 AMM 21-50-00-862-801-A02 AND 21-50-00-862-805-A01, NO ABNORMAL SMELL NOTED.
- [SDR VNAA202012181112](https://openairdocs.org/sdr/VNAA202012181112.md): Control Valve · abnormal · Dec 16, 2020 · N516AE · Cndair CL6002C10 · Engine Thrust Reverser
  > RTO-TAKING OFF RWY 6 IN ERI AT 40KTS THE CREW RECEIVED A RT THRUST REVERSER UNSAFE AMBER MESSAGE AND ABORTED TAKEOFF. CREW RETURNED TO GATE.
- [SDR VNAA202012071111](https://openairdocs.org/sdr/VNAA202012071111.md): Relay · abnormal · Dec 3, 2020 · N516AE · Cndair CL6002C10 · Engine Thrust Reverser
  > THE FLIGHT WAS TAKING OFF RWY 31 IN PIA AT 30KTS THE CREW RECEIVED A RT REVERSE UNSAFE CAUTION MESSAGE AND ABORTED TAKEOFF AND RETURNED TO GATE. DEF RT THRUST REVERSER SYSTEM, PER MEL 78-30-01 CAT C. M/FUNCTION C/W. DEACTIVATED THE RT THRUST REVERSER, IAW C
- [SDR VNAA202011191111](https://openairdocs.org/sdr/VNAA202011191111.md): Warning Message · illuminated · Nov 18, 2020 · N516AE · Cndair CL6002C10 · Engine Thrust Reverser
  > REJECTED TAKEOFF FOR A RT THRUST REV UNSAFE CAUTION MESSAGE AT THE VERY BEGINNING OF THE TAKEOFF ROLL, LESS THAN 10 KNOTS. AIRCRAFT EXITED THE RUNWAY WITHOUT ISSUE AND RETURNED TO GATE WHERE MAINTENANCE HAS BEEN CALLED TO INSPECT AND TO POTENTIALLY DEFER THE
- [SDR VNAA20201013111](https://openairdocs.org/sdr/VNAA20201013111.md): Loop · unsecure · Oct 10, 2020 · N516AE · Cndair CL6002C10 · Airfoil Anti/De-ice System
  > RESECURED BLEED LOOP AROUND RT WING ANTI-ICE VALVE. OPERATIONS AND LEAK CHECK GOOD, IAW CRJ 700 AMM 30-12-00-710-802-A02 AND AMM 36-21-00-710-801-A01.
- [SDR VNAA2020100211102](https://openairdocs.org/sdr/VNAA2020100211102.md): Seal · leaking · Sep 30, 2020 · N516AE · Cndair CL6002C10 · Air Distribution System
  > FOUL SMELL FROM VENT IN COCKPIT. PERFORMED GVI OF RT AC PACK. FOUND AIR LEAK ON HEAT EXCHANGER PERI-SEAL/CONNECTOR. REPLACED PERI-SEAL. OPERATIONS AND LEAK CHECK GOOD. NO FURTHER DEFECTS NOTED AT THIS TIME.
- [SDR VNAA2020091211101](https://openairdocs.org/sdr/VNAA2020091211101.md): A/C Pack · odor · Sep 11, 2020 · N516AE · Cndair CL6002C10 · Cabin Cooling System
  > OILY SMELL COMING FROM THE PACKS. INVESTIGATED OIL SMELL COMING FROM PACKS. COULD NOT REPLICATE PROBLEM. FOUND NO DEFECTS AT THIS TIME. OPS CHK OF A/C SYS SOURCING FROM APU & BOTH ENG ABOVE IDLE. NO ODORS DETECTED AT THIS TIME.
- [SDR VNAA2020091111102](https://openairdocs.org/sdr/VNAA2020091111102.md): Acm · failed · Sep 9, 2020 · N516AE · Cndair CL6002C10 · Cabin Cooling System
  > FOUL ODOR COMING FROM PACKS. TROUBLESHOT PER FIM. INSPECTED APU AND LOAD CONTROL VALVE, FOUND NO EVIDENCE OF OIL CONTAMINATION. RAN PACKS IN ALL BLEED CONFIGURATIONS WITH AND WITHOUT ENGINES AND DETERMINED SMELL TO BE PREVALENT WITH LT PACK. SUSPECT LT ACM
- [SDR VNAA2020060211101](https://openairdocs.org/sdr/VNAA2020060211101.md): Acm · failed · May 29, 2020 · N516AE · Cndair CL6002C10 · Cabin Cooling System
  > CABIN FILLED WITH SMOKE FOLLOWED BY RT PACK AUTO FAIL WHILE AT GATE. MAINTENANCE REMOVED AND REPLACED THE AIR CYCLE MACHINE.
- [SDR VNAA2019052511101](https://openairdocs.org/sdr/VNAA2019052511101.md): Windshield · cracked · May 25, 2019 · N516AE · Cndair CL6002C10 · Flight Compartment Windows
  > DURING CRUISE AT FL330, CA WINDSHIELD CRACKED. EMERGENCY DECLARED FOR PRIORITY DESCENT AND FLIGHT DIVERTED INTO CLT. CA STATED THE INNER LAYER OF THE WINDSHIELD PEELED OFF AND LANDED ON HIS LAP. FLIGHT LANDED ON RWY 18L IN CLT AND CANCELLED THE EMERGENCY AFTE
- [SDR VNAA2018100299904](https://openairdocs.org/sdr/VNAA2018100299904.md): Floor Support · corroded · Oct 2, 2018 · N516AE · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > PAX DOOR SURROUND STRUCTURE CENTER FLOORBOARD SUPPORT ANGLE AND SILL ANGLE HAS CORROSION AT SCREW HOLES. REMOVED AND REPLACED SILL ANGLE SH670-31875-3 IAW SRM 51-42-06-001-001-A01, AND 51-42-21-001-001-A01.
- [SDR VNAA2018100299903](https://openairdocs.org/sdr/VNAA2018100299903.md): Seat Track · corroded · Oct 2, 2018 · N516AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > RBL 9 FLOOR SEAT TRACK SEGMENTS FS 349 TO FS 485 AND FS 581 TO 683 ARE CORRODED. REMOVED SEAT TRACKS, FABRICATED NEW SEAT TRACKS AND INSTALLED IAW AMM 53-00-49 AND REO 670-53-00-343 REV M.
- [SDR VNAA2018100299902](https://openairdocs.org/sdr/VNAA2018100299902.md): Seat Track · cracked · Oct 2, 2018 · N516AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > LBL 9 FLOOR SEAT TRACK SEGMENTS FS 517 TO FS 581 AND FS 581 TO 683 ARE CORRODED. REMOVED SEAT TRACKS, FABRICATED NEW SEAT TRACKS AND INSTALLED IAW AMM 53-00-49 AND REO 670-53-00-343 REV M.
- [SDR VNAA2018100299901](https://openairdocs.org/sdr/VNAA2018100299901.md): Fitting · cracked · Oct 2, 2018 · N516AE · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > FS 280 CROSSBEAM TO RBL 9 FLOORBEAM T FITTING IS CRACKED ON IB SIDE. FABBED & REINSTALLED 2 EA NEW ATTACH ANGLES AT FS 280 RBL 9.0 IAW SRM 51-42-21-001-001-A01 AND REO 670-53-11-165 REV B.
- [SDR VNAA2017110411101](https://openairdocs.org/sdr/VNAA2017110411101.md): Warning System · activated · Nov 4, 2017 · N516AE · Cndair CL6002C10 · Autopilot System
  > CREW REPORTED AP LWD CAUTION MSG. CREW DIVERTED TO BMH. MAINTENANCE INSPECTED FLIGHT CONTROL CABLES NO DEFECTS NOTED. DEFERRED AUTO PILOT.
- [SDR SIMA20170914005](https://openairdocs.org/sdr/SIMA20170914005.md): Skin · damaged · Sep 14, 2017 · N516AE · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > DURING HEAVY MAINTENANCE, DAMAGE WAS FOUND TO THE EXTERIOR FUSELAGE SKIN BETEWEEN BS 969 AND 985, STRINGER 27L. REPAIRED THE SKIN IAW ERS-CR-53MR-2905.
- [SDR SIMA20170906008](https://openairdocs.org/sdr/SIMA20170906008.md): Crossbeam · cracked · Sep 6, 2017 · N516AE · Cndair CL6002C10 · Fuselage Main, Structure
  > FRAME BS 280 LT SIDE CROSSBEAM CRACKED ON FWD SIDE BELOW CENTER COCKPIT FLOORBOARD. A NEW CROSSBEAM WAS INSTALLED IAW SRM 51--42-06, SRM 51-42-10, AND SRM 51-42-13.
- [SDR SIMA20170107001](https://openairdocs.org/sdr/SIMA20170107001.md): Line · damaged · Jan 7, 2017 · N516AE · Cndair CL6002C10 · Hydraulic System, Main
  > DURING TAXI IN, LOST OF NOSE WHEEL STEERING HYDRAULIC SYSTEM NR 3 LOW PRESSURE AND ZERO QUANITY IN THE SYSTEM NR 3 RESEVOIR. REMOVED AND REPLACED THE REAR FLEXIBLE HYD HOSE FOR NLG RETRACT ACTUATOR IAW AMM 32-32-09. OPS AND LEAK CHECKED GOOD.
- [SDR SIMA20161107002](https://openairdocs.org/sdr/SIMA20161107002.md): Connector · loose · Nov 7, 2016 · N516AE · Cndair CL6002C10 · Light System Wiring
  > LAST TWO EMERGENCY DOME LIGHTS IN THE CABIN WILL NOT ILLUMINATE. FOUND LOOSE CONNECTOR ON EPSU 4. RE-SEATED CONNECTOR IAW ELECTRICAL STANDARD MTX PRACTICES. OPS CK GOOD. A/C OK FOR SERVICE
- [SDR SIMA20160504001](https://openairdocs.org/sdr/SIMA20160504001.md): Pcu · malfunctioned · May 4, 2016 · N516AE · Cndair CL6002C10 · Drag Control System
  > ON DESCENT, OTBD SPOILERONS, & OTBD FLIGHT SPOILERS", CAUTION MSGS. INTERROGATED MDC, FOUND, ROB MFS PCU FAILED PCU JAM. PERFORMED SPOST 1 RESET. PERFORMED OPERATIONS CHECK IAW ETN CR-27-093. OPERATIONS CHECKED GOOD. OPENED TDMI 516T2745 TA. R & R ROB MF
- [SDR SIMA20160406003](https://openairdocs.org/sdr/SIMA20160406003.md): Battery Pack · discharged · Apr 6, 2016 · N516AE · Cndair CL6002C10 · Emergency Lighting
  > EMERGENCY LIGHTS AFT OF FIRST CLASS INOPERATIVE. R & R EPSU BATTERY PACK & CHARGER NR 3 IAW WC 33-002. OPERATIONAL TESTED GOOD. BATTERY CHARGER ASSEMBLY PN 11-0049 & SN 12337.

Next page: https://openairdocs.org/aircraft/N516AE/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 = 'N516AE' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N516AE/reports

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