# Service difficulty reports: N690AE

A list on [N690AE](https://openairdocs.org/aircraft/N690AE.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 4 · 159 reports

- [SDR HNAA2026083100811](https://openairdocs.org/sdr/HNAA2026083100811.md): Warning Message · false activation · Aug 30, 2026 · N690AE · Emb EMB145LR · Central Warning
  > NR 2 BLEED VALVE FAILED MESSAGE AFTER AIR START WITH SLIGHT ODOR. RAN ENGINES NO BLEED VALVE FAIL MESSAGE ON EICAS. NO ODOR NOTICED. ACFT OK FOR SERVICE.
- [SDR HNAA2026082400746](https://openairdocs.org/sdr/HNAA2026082400746.md): Battery · inoperative · Aug 22, 2026 · N690AE · Emb EMB145LR · Emergency Lighting
  > ROW 4, 5, 6, & 7 EMERGENCY LIGHT FLOOR STRIPS INOPERATIVE. R & R NR 100 EMERGENCY LIGHT BATTERY PACK IAW AMM 33-50-04.
- [SDR HNAA2026080300641](https://openairdocs.org/sdr/HNAA2026080300641.md): Radar · failed · Aug 1, 2026 · N690AE · Emb EMB145LR · Weather Radar System
  > WING A/I FAIL MSG APPEARED ON EICAS IN ICING CONDITIONS, WING ANTI-ICING SYSTEM. OPS CHECK GOOD IAW AMM 30-00-00. A/C OK FOR SERVICE AT THIS TIME.
- [SDR HNAA2026062200551](https://openairdocs.org/sdr/HNAA2026062200551.md): Battery · inoperative · Jun 20, 2026 · N690AE · Emb EMB145LR · Emergency Lighting
  > ALL EMERGENCY LIGHTS CONNECTED TO #100 EMERGENY LIGHT BATTERY ARE INOP. R & R BATTERY IAW AMM 33-50-04-04
- [SDR HNAA2026031700220](https://openairdocs.org/sdr/HNAA2026031700220.md): Valve · odor · Mar 17, 2026 · N690AE · Emb EMB145LR · Air Distribution System
  > STRONG FUEL ODOR ENTERED COCKPIT, ON APU START SHORTLY AFTER TOUCHDOWN. APU AUXILIARY POWER UNIT R & R APU BLEED AIR VALVE IAW EMT-62T-40C14 AND CLEANED APU DRAIN LINES IAW AMM 49-19-00, OPS CHECKED GOOD, NO ODOR IN FLT DECK WITH APU ON CLEAR MEL 49-1.
- [SDR HNAA2026030200165](https://openairdocs.org/sdr/HNAA2026030200165.md): Gasket · leaking · Mar 2, 2026 · N690AE · Emb EMB145LR · APU Engine Fuel and Control
  > AMMAENDED: STRONG FUEL SMELL/ODOR ENTERED COCKPIT AND CABIN ON APU START HAS EXTENSIVE HISTORY - APU FAIL ON EICAS MESSAGE ALSO DISPLAYED MEL 02MAR26 11:53 GRR C06116 49-1 APU AUXILIARY POWER UNIT DFRL 04MAR26 08:46 SBY ENGINE PROGRAMS DEPARTM
- [SDR HNAA2026022500157](https://openairdocs.org/sdr/HNAA2026022500157.md): Apu · odor · Feb 24, 2026 · N690AE · Emb EMB145LR · Airborne Auxiliary Power Unit (APU) System
  > AFTER LANDING DURING APU START, JET FUEL SMELL IN FLT DECK AND IN CABIN FOR APPROX 20 SECONDS. APU AUXILIARY POWER UNIT FACT 25FEB26 04:09 PHL OPERATED APU AND ENGINES. NO JET FUEL SMELL PRESENT IN FLIGHT DECK AND CABIN IRT AMM 71-00-01. A/C OK FOR SE
- [SDR HNAA2026022400155](https://openairdocs.org/sdr/HNAA2026022400155.md): Unknown · odor · Feb 21, 2026 · N690AE · Emb EMB145LR · Air Distribution System
  > FUEL SMELL ENTERED COCKPIT AFTER APU START ON LANDING WITH PACKS 1 & 2 RUNNING INSPECTED E1 & E2 INLETS & DUCTS, NO DEFECTS NOTED. INPSECTED APU INLETS & EXHAUST & COWLING W/NO DEFECTS NOTED. RAN PACKS FOR 10-15 MINUTES W/NO ODOR NOTICED. OPS CHECK DONE IA
- [SDR HNAA2026021000114](https://openairdocs.org/sdr/HNAA2026021000114.md): Warning Message · false activation · Feb 9, 2026 · N690AE · Emb EMB145LR · Engine Fuel Indicating System
  > ON TAKE OFF ROLL 75 KNOTS, NR 1 ENGINE FUEL LOW TEMP. PERFORMED CONTINUITY & RESISTANCE TESTS ON ENGINE HARNESS W9 IAW RMM 73-31-00-900-801. NO DEFECETS NOTED. SUSPECT TRANSITORY CONDITION DUE TO EXTREME COLD CONDITIONS. PERFORMED MULTIPLE POWER RUNS WITH C
- [SDR HNAA2026012000012](https://openairdocs.org/sdr/HNAA2026012000012.md): Inverter · faulted · Jan 16, 2026 · N690AE · Emb EMB145LR · Emergency Lighting
  > CABIN EMERGENCY FLOOR STRIPS NOT ILLUMINATING FROM ROWS 3 TO 7. R & R EMERGENCY LIGHT DC/AC INVERTER 3 IRT AMM 3-50-11-000/400-801-A OPS CHECK GOOD OK FOR SERVICE
- [SDR HNAA2026012100036](https://openairdocs.org/sdr/HNAA2026012100036.md): Inlet · corroded · Dec 21, 2025 · N690AE · Emb EMB145LR · Turbine Engine Air Inlet Section
  > RIGHT ENGINE INLET HAS CORROSION ON THE INTERNAL LWR SIDE WHERE THE GENERATOR INLETS ARE LOCATED. RAR RH ENGINE INLET IAW EMB 145 AMM 71-60-01,
- [SDR HNAA2026012100050](https://openairdocs.org/sdr/HNAA2026012100050.md): Attach Fitting · worn · Dec 9, 2025 · N690AE · Emb EMB145LR · Wing, Attach Fittings
  > RIGHT AILERON DAMPER ATTACHMENT FITTING HOLE IS WORN. R & R RT AILERON DAMPER ATTACHMENT FITTING IAW EMB 145 SRM 51-40-02.
- [SDR HNAA2026012100049](https://openairdocs.org/sdr/HNAA2026012100049.md): Bracket · cracked · Dec 1, 2025 · N690AE · Emb EMB145LR · Fuselage Miscellaneous Structure
  > COCKPIT LH LATERAL BRACKET IS CRACKED. REMOVED AND INSTALLED NEW SERVICEABLE LH LATERAL BRACKET IN COCKPIT IAW EMB 145 SRM 51-20-03, 51-40-02
- [SDR HNAA2026012100048](https://openairdocs.org/sdr/HNAA2026012100048.md): Shear Tie · cracked · Nov 30, 2025 · N690AE · Emb EMB145LR · Fuselage Internal Mounting Structure
  > SHEAR CLIP IS CRACKED AT FRAME 16 BETWEEN STRINGERS 15R-16R. REMOVED AND REPLACED SHEAR CLIP AT FRAME 16 BETWEEN STRINGERS 15R-16R IAW EMB 145 SRM 51-40-02.
- [SDR HNAA2026012100047](https://openairdocs.org/sdr/HNAA2026012100047.md): Shear Tie · cracked · Nov 29, 2025 · N690AE · Emb EMB145LR · Fuselage Internal Mounting Structure
  > SHEAR CLIP IS CRACKED AT FRAME 15 BETWEEN STRINGERS 15R-16R. R & R SHEAR CLIP AT FRAME 15 BETWEEN STRINGERS 15R-16R. IAW EMB 145 SRM 51-40-02 AND PDT EO1-53-25-0454
- [SDR HNAA2026012100035](https://openairdocs.org/sdr/HNAA2026012100035.md): Floorbeam · corroded · Nov 29, 2025 · N690AE · Emb EMB145LR · Fuselage Main, Floor Beam
  > CORROSION ON SIDE OF STEP-UP CROSS FLOORBEAM AT FRAME 23 BETWEEN STRINGERS 21R-21L. R & R STEP-UP CROSS FLOORBEAM AT FR23 BTWN STGRS 21R-21L IAW EMB 145 SRM 51-40-02
- [SDR HNAA2026012100034](https://openairdocs.org/sdr/HNAA2026012100034.md): Gusset · corroded · Nov 29, 2025 · N690AE · Emb EMB145LR · Fuselage Main, Structure
  > CORROSION ON LH NR 1 BEAM GUSSET. R & R L/H # 1 BEAM GUSSET IAW EMB-145 SRM 51-40-02
- [SDR HNAA2026012100033](https://openairdocs.org/sdr/HNAA2026012100033.md): Floor Support · corroded · Nov 29, 2025 · N690AE · Emb EMB145LR · Fuselage Miscellaneous Structure
  > CORROSION ON LT OTBD NR 1 FLOOR SILL. R & R L/H OUTBD # 1 FLOOR SILL IAW EMB145 SRM 51-40-02.
- [SDR HNAA2026012100032](https://openairdocs.org/sdr/HNAA2026012100032.md): Door Sill · corroded · Nov 29, 2025 · N690AE · Emb EMB145LR · Fuselage Main, Structure
  > CORROSION ON SERVICE DOOR CUT-OUT FWD SILL. R & R THE SERVICE DOOR CUTOUT FWD SILL IAW EMB 145 SRM 51-40-02.
- [SDR HNAA2026012100031](https://openairdocs.org/sdr/HNAA2026012100031.md): Gusset · corroded · Nov 29, 2025 · N690AE · Emb EMB145LR · Fuselage Main, Attach Fittings
  > CORROSION IN GALLEY AREA ON RT FLOORBEAM GUSSET AT FRAME 18. REMOVED AND REPLACED GUSSET ON GALLEY AREA RT FLOORBEAM GUSSET AT FRAME 18 IAW EMB 145 SRM 51-40-02.
- [SDR HNAA2026012100030](https://openairdocs.org/sdr/HNAA2026012100030.md): Floor Support · corroded · Nov 29, 2025 · N690AE · Emb EMB145LR · Fuselage Miscellaneous Structure
  > CORROSION IN GALLEY AREA ON FWD DIGITAL. REPAIRED WITH DOUBLER IAW EMB-145 SRM 53-21-10
- [SDR HNAA2026012100029](https://openairdocs.org/sdr/HNAA2026012100029.md): Floorbeam · corroded · Nov 29, 2025 · N690AE · Emb EMB145LR · Fuselage Main, Floor Beam
  > CORROSION IN GALLEY AREA ON LT CROSS FLOORBEAM AT FRAME 18. R & R LT CROSS FLOORBEAM AT FRAME 18 IAW EMB145 SRM 51-40-02
- [SDR HNAA2026012100028](https://openairdocs.org/sdr/HNAA2026012100028.md): Floor Support · corroded · Nov 29, 2025 · N690AE · Emb EMB145LR · Fuselage Miscellaneous Structure
  > CORROSION ON PASSENGER DOOR ENTRY AFT FLOORBOARD SUPPORT. RAR SUPPORT IAW SRM 51-40-02
- [SDR HNAA2026012100027](https://openairdocs.org/sdr/HNAA2026012100027.md): Structure · corroded · Nov 29, 2025 · N690AE · Emb EMB145LR · Fuselage Main, Structure
  > LAV WASTE BUCKET IS CORRODED AT AFT OF THE WASTE DRAIN VALVE. REMOVED AND REPLACED LAV WASTE BUCKET IAW EMB 145 SRM 51-40-02.
- [SDR HNAA2026012100026](https://openairdocs.org/sdr/HNAA2026012100026.md): Seat Track · corroded · Nov 29, 2025 · N690AE · Emb EMB145LR · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON RT OTBD NR 2 SEAT TRACK. REMOVED AND REPLACED RT NR 2 OTBD SEAT TRACK IAW EMB 145 AMM 53-01-06.
- [SDR HNAA2026012100046](https://openairdocs.org/sdr/HNAA2026012100046.md): Shear Tie · cracked · Nov 26, 2025 · N690AE · Emb EMB145LR · Fuselage Internal Mounting Structure
  > SHEAR CLIP IS CRACKED AT FRAME 25 BETWEEN STRINGERS 15R-16R. REMOVED AND REPLACED SHEAR CLIP AT FRAME 25 BETWEEN STRINGERS 15R-16R IAW EMB 145 SRM 51-40-02.
- [SDR HNAA2026012100045](https://openairdocs.org/sdr/HNAA2026012100045.md): Shear Tie · cracked · Nov 26, 2025 · N690AE · Emb EMB145LR · Fuselage Internal Mounting Structure
  > SHEAR CLIP IS CRACKED AT FRAME 24 BETWEEN STRINGERS 15R-16R. REMOVED AND REPLACED SHEAR CLIP AT FRAME 24 BETWEEN STRINGERS 15R-16R IAW EMB 145 SRM 51-40-02
- [SDR HNAA2026012100025](https://openairdocs.org/sdr/HNAA2026012100025.md): Floorbeam · corroded · Nov 26, 2025 · N690AE · Emb EMB145LR · Fuselage Main, Floor Beam
  > CORROSION ON LT NR 2 FLOORBEAM ISLE AREA AT FRAME 29. REMOVED CORROSION ON LT NR 2 FLOORBEAM ISLE AREA AT FRAME 29 IAW EMB 145 SRM 51-10-03. BLEND OUT IS ACCEPTED AS PERMANENT REPAIR IAW ETD2025-145-933947 AND EO1-05-26-0006.
- [SDR HNAA2026012100024](https://openairdocs.org/sdr/HNAA2026012100024.md): Floor Support · corroded · Nov 26, 2025 · N690AE · Emb EMB145LR · Fuselage Miscellaneous Structure
  > CORROSION ON LT OTBD #2 FLOOR SILL. R & R L/H OTBD #2 FLOOR SILL IAW EMB 145 SRM 51-40-02.
- [SDR HNAA2026012100023](https://openairdocs.org/sdr/HNAA2026012100023.md): Seat Track · corroded · Nov 26, 2025 · N690AE · Emb EMB145LR · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON RH INBD NR 4 SEAT TRACK. REMOVED AND REPLACED RT INBD NR 4 SEAT TRACK IAW EMB 145 AMM 53-01-06.
- [SDR HNAA2026012100022](https://openairdocs.org/sdr/HNAA2026012100022.md): Gusset · corroded · Nov 26, 2025 · N690AE · Emb EMB145LR · Fuselage Main, Attach Fittings
  > CORROSION IN LAV AREA ON LH FLOORBEAM GUSSET. RAR LH FLOORBEAM GUSSET IN LAV IAW EMB 145 SRM 51-40-02.
- [SDR HNAA2026012100021](https://openairdocs.org/sdr/HNAA2026012100021.md): Gusset · corroded · Nov 26, 2025 · N690AE · Emb EMB145LR · Fuselage Main, Attach Fittings
  > CORROSION IN LAV AREA ON CENTER FLOORBEAM GUSSET. R & R CENTER FLOORBEAM GUSSET IN LAV IAW EMB 145 SRM 51-40-02.
- [SDR HNAA2026012100020](https://openairdocs.org/sdr/HNAA2026012100020.md): Gusset · corroded · Nov 26, 2025 · N690AE · Emb EMB145LR · Fuselage Main, Attach Fittings
  > CORROSION IN LAV AREA ON RH FLOORBEAM GUSSET. RAR RH FLOORBEAM GUSSET IN LAV IAW EMB 145 SRM 51-40-02.
- [SDR HNAA2026012100044](https://openairdocs.org/sdr/HNAA2026012100044.md): Shear Tie · cracked · Nov 24, 2025 · N690AE · Emb EMB145LR · Fuselage Internal Mounting Structure
  > SHEAR CLIP IS CRACKED AT FRAME 61 BETWEEN STRINGERS 6R-7R. REMOVED AND REPLACED SHEAR CLIP AT FRAME 61 BETWEEN STRINGERS 6R-7R IAW EMB 145 SRM 51-40-02.
- [SDR HNAA2026012100043](https://openairdocs.org/sdr/HNAA2026012100043.md): Spar · cracked · Nov 24, 2025 · N690AE · Emb EMB145LR · Wing Spar
  > RIGHT WING SPAR I LOWER FLANGE AT RIB 9 IS CRACKED. PERFORMED REPAIR OF RH WING SPAR I AT RIB 9 REPAIR PARTS IAW EMB 145 SRM 57-20-05 ITEM3, ETD2025-145-934133 AND EO1-57-25-0455.
- [SDR HNAA2026012100042](https://openairdocs.org/sdr/HNAA2026012100042.md): Spar · cracked · Nov 24, 2025 · N690AE · Emb EMB145LR · Wing Spar
  > LEFT WING SPAR I LOWER FLANGE AT RIB 9 IS CRACKED. PERFORMED REPAIR ON LT WING SPAR I LOWER FLANGE AT RIB 9 IAW EMB 145 SRM 57-20-05 ITEM 3, ETD2025-145-933843 AND EO1-57-25-0446.
- [SDR HNAA2026012100019](https://openairdocs.org/sdr/HNAA2026012100019.md): Door Sill · corroded · Nov 24, 2025 · N690AE · Emb EMB145LR · Fuselage Main, Structure
  > CORROSION ON CARGO DOOR CUTOUT LOWER SILL. REMOVED AND REPLACED CARGO DOOR CUTOUT LOWER SILL IAW EMB 145 SRM 51-40-02.
- [SDR HNAA2026012100018](https://openairdocs.org/sdr/HNAA2026012100018.md): Shear Tie · corroded · Nov 24, 2025 · N690AE · Emb EMB145LR · Fuselage Internal Mounting Structure
  > CORROSION ON CARGO DOOR CUT-OUT SHEAR CLIP AT FRAME 65. PERFORMED SPLICE REPAIR OF SHEAR CLIP AROUND CARGO DOOR CUTOUT AT FRAME 65 IAW EMB 145 SRM 53-31-04 ITEM 4D FIG 212 AND EO1-53-25-0445.
- [SDR HNAA2026012100041](https://openairdocs.org/sdr/HNAA2026012100041.md): Door Frame · cracked · Nov 23, 2025 · N690AE · Emb EMB145LR · Fuselage Main, Structure
  > CARGO DOOR LWR OUTBD FRAME PROFILE IS CHAFED AND CRACKED AT FWD END. REMOVED AND REPLACED CHAFED AND CRACKED CARGO DOOR LWR OUTBOARD FRAME PROFILE IAW EMB 145 SRM 51-40-02, 51-20-01, 51-20-03, 51-40-04, 51-40-06
- [SDR HNAA2026012100040](https://openairdocs.org/sdr/HNAA2026012100040.md): Door Frame · corroded · Nov 23, 2025 · N690AE · Emb EMB145LR · Fuselage Main, Structure
  > CARGO DOOR CORRODED AROUND FWD MOST 2 SCREW HOLES ON INBD LOWER FRAME PROFILE. R & R CARGO DOOR INBD LOWER FRAME PROFILE IAW EMB 145 SRM 51-40-02
- [SDR HNAA2026012100039](https://openairdocs.org/sdr/HNAA2026012100039.md): Access Door · cracked · Nov 23, 2025 · N690AE · Emb EMB145LR · Fuselage Main, Structure
  > COCKPIT UNDER FLOOR ACCESS HATCH CRACKED UNDER HINGE PIN ATTACH RING (HATCH SIDE). REPAIRED IAW EMB145 SRM 52-42-02-RE & 51-40-02, CPM 51-21-04 & 51-21-05.
- [SDR HNAA2026012100038](https://openairdocs.org/sdr/HNAA2026012100038.md): Skin · cracked · Nov 22, 2025 · N690AE · Emb EMB145LR · Fuselage Main, Plate/Skin
  > POSSIBLE SKIN CRACK AT FR 77 BTWN STGRS 3L-4L. REPAIRED SKIN CRACK AT FR 77 BTWN STGRS 3L-4L WITH INSTALLATION OF SKIN BUSHING IAW EMB145 SRM 53-32-01RE, ITEM 9, FIG. 213 AND EO1-53-26-0005.
- [SDR HNAA2026012100037](https://openairdocs.org/sdr/HNAA2026012100037.md): Skin · dented · Nov 21, 2025 · N690AE · Emb EMB145LR · Wing, Plate/Skin
  > RIGHT WING LEADING EDGE NR 2 HAS A DENT APPROX. 13" FROM OTBD EDGE. REPAIRED RH WING LEADING EDGE #2 DENT APPROX. 13" FROM OTBD EDGE IAW PIEDMONT EO1-57-25-0461, ETD2025-145-934265 AND EMB 145 SRM 57-40-00RE.
- [SDR HNAA2025101400701](https://openairdocs.org/sdr/HNAA2025101400701.md): Frame · corroded · Oct 12, 2025 · N690AE · Emb EMB145LR · Fuselage Main, Frame
  > AREA OF CORROSION AT FR22, STR16R. REPAIRED IAW EO1-53-25-0364
- [SDR HNA2025F00002](https://openairdocs.org/sdr/HNA2025F00002.md): Sensor · faulted · Apr 2, 2025 · N690AE · Emb EMB145LR · Engine Indicating System
  > N THE CLIMB FROM CLT E1 OIL TEMPERATURE WENT INTO THE RED FOR APPROXIMATELY 1 MINUTE THEN RETURNED TO NORMAL 20 PSI INCREASE INDICATION OIL PRESSURE, OIL TEMPERATURE WAS MAXED OUT AT 138 DEGREES TOP OIL TEMPERATURE. FACT 02APR25 19:28 CLT R+R'D #1 ENG O
- [SDR HNAA2025011500023](https://openairdocs.org/sdr/HNAA2025011500023.md): Window · no discrepancy · Jan 15, 2025 · N690AE · Emb EMB145LR · Flight Compartment Windows
  > BIRD STIRKE FO DV WINDOW DURING LANDING. CLEANED AREA, PERFORMED BIRD STRIKE INSPECTION IAW AMM 05-50-08. NO DEFECTS NOTED. AIRCRAFT OK FOR SERVICE.
- [SDR HNAA2024102901035](https://openairdocs.org/sdr/HNAA2024102901035.md): Heater · inoperative · Oct 26, 2024 · N690AE · Emb EMB145LR · Pitot/Static Anti-Ice System
  > TAT 2 HEAT INOP ON CLIMB OUT. FACT 26OCT24 10:33 ALB FOUND TAT 2 CB OPENED PERFORMED OPS CHECK IAW EMB 145 AMM TASK 30-33-00 AFTER CLOSING CB. BOTH TAT 1&2 SENSOR BECAME HOT OPS CHECK GOOD.
- [SDR HNAA2024102201015](https://openairdocs.org/sdr/HNAA2024102201015.md): Lamp · inoperative · Oct 21, 2024 · N690AE · Emb EMB145LR · Emergency Lighting
  > EMERGENCY LIGHT ON SERVICE DOOR HINGE INOP. RAR LAMP ASSY WITH RETAINED HARDWARE
- [SDR HNAA2023102300365](https://openairdocs.org/sdr/HNAA2023102300365.md): Unknown · unknown · Oct 22, 2023 · N690AE · Emb EMB145LR · Fuselage Structure (General)
  > MULTIPLE BIRDSTRIKES ON TAKE OFF. RETURNED TO FIELD. MX INSPECTED A/C FOR BIRDSTRIKE AND CLEANED AREA IAW AMM 05-50-25 NO DEFECTS NOTED AND ENGINE AND INLET INGESTION NOTED AT THIS TIME. A/C OK FOR SERVICE AT THIS TIME
- [SDR HNAA2023081700316](https://openairdocs.org/sdr/HNAA2023081700316.md): Unknown · unknown · Aug 17, 2023 · N690AE · Emb EMB145LR · Fuselage Miscellaneous Structure
  > HN00103352 CORROSION FOUND ON "0" FLOOR BEAM CAP BETWEEN FRM 36-26 REMOVED CORRODED FLOOR BEAM CAP AND INSTALLED NEW FLOOR GUSSET/ FLOOR BEAM CAP AT "0" BEAM FRM 26 TO FRM 36 IAW EMB 145 SRM 51-40-02-PR.

Next page: https://openairdocs.org/aircraft/N690AE/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 = 'N690AE' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N690AE/reports

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