# Service difficulty reports: N8409N

A list on [N8409N](https://openairdocs.org/aircraft/N8409N.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 · 54 reports

- [SDR REXA2015032900351](https://openairdocs.org/sdr/REXA2015032900351.md): Oxygen Mask · unsecure · Mar 29, 2015 · N8409N · Cndair CL6002B19 · Passenger Oxygen System
  > O2 MASK 6CD FELL FROM CEILING. PERFORMED INSPECTION OF PAX OXYGEN SYS & MASKS O2 GEN AT SEATS 6CD IAW AMM 05-51-35. REPACKED O2 MASKS AT SEATS 6CD IAW AMM 35-21-09. OPERATIONAL TEST OF PAX OXYGEN SYS DEPLOYMENT REQUIRES IAW AMM 35-20-00-710-802 & REF LOG PA
- [SDR REXA2015031900335](https://openairdocs.org/sdr/REXA2015031900335.md): Oxygen Mask · unsecure · Mar 19, 2015 · N8409N · Cndair CL6002B19 · Passenger Oxygen System
  > AFTER PUSHBACK. PAX O2 MASK AT SEAT 6CD DROPPED. ACFT GATE RETURNED & MX CALLED OUT. REPACKED MASK & DEFERRED SEAT FOR OPERATIONS CHECKS TO BE PERFORMED ON RON. PAX SEATS 6CD NEED OPERATIONS CHECK OF PAX OXY SYS, LOG PAGE 3175884-1 FOR PAX OXY MASK DEPLOYME
- [SDR REXA2015012600153](https://openairdocs.org/sdr/REXA2015012600153.md): Cable · out of position · Jan 26, 2015 · N8409N · Cndair CL6002B19 · Passenger/Crew Doors
  > PASSENGER DOOR CABLE OFF TRACK. ROUTED PAX DOOR POWER ASSIST CABLE AROUND PULLEY. PERFORMED OPERATIONS CHECK OF PAX DOOR POWER ASSIST CABLE IAW AMM 52-11-08. OPERATIONS CHECKED GOOD. OK FOR SERVICE.
- [SDR REXA2014110601115](https://openairdocs.org/sdr/REXA2014110601115.md): Priority Valve · malfunctioned · Nov 6, 2014 · N8409N · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > GEAR DISAGREE ON TAKEOFF NOSE GEAR UP HANDLE, HEARD THUNK, GEAR LOWERED THEN BACK UP & LOCKED. PERFORMED TROUBLESHOOTING OF NLG RETRACTION ISSUE IAW FIM 32-60-09. NO FAULTS RECORDED IN PSECU. PERFORMED FUNCTIONAL CHECK OF LG PRIORITY VLVS, NLG PRIORITY VLV
- [SDR REXA2014102900904](https://openairdocs.org/sdr/REXA2014102900904.md): Structure · damaged · Oct 26, 2014 · N8409N · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > MULTIPLE RIVETS HOLES BURNED & ELONGATED AT FS 409+16 STRINGER 18L. REPAIRED IAW SRM 53-00-31.
- [SDR REXA2014080900804](https://openairdocs.org/sdr/REXA2014080900804.md): Battery Pack · discharged · Aug 9, 2014 · N8409N · Cndair CL6002B19 · Emergency Locator Beacon
  > ELT BATTERY NEEDS TO BE REPLACED. R & R ELT BATTERY PACK IAW AMM 25-62-09. OPERATIONS CHECKED GOOD.
- [SDR REXA2014041300376](https://openairdocs.org/sdr/REXA2014041300376.md): Life Vest · unserviceable · Apr 13, 2014 · N8409N · Cndair CL6002B19 · Life Jacket
  > CAPTAIN`S LIFE VEST BAG TORN. R & R CAPTAIN`S LIFE VEST IAW AMM 25-61-03.
- [SDR REXA2014033000337](https://openairdocs.org/sdr/REXA2014033000337.md): Acm · seized · Mar 30, 2014 · N8409N · Cndair CL6002B19 · Cabin Cooling System
  > UPON REACHING GATE WE NOTICED THE SMELL OF SMOKE. SHUT DOWN APU & PACKS. PAXS ALSO NOTICED A BURNING SMELL. RECEIVED A SMOKE TOILET MASTER CAUTION. DEPLANED, HAZE THROUGHOUT ACFT. WHILE DOING WORK SCOPE FOR SMOKE & FUMES SMOKE TOILET MSG FOUND RT ACM SEIZ
- [SDR REXA2014021700211](https://openairdocs.org/sdr/REXA2014021700211.md): Battery · discharged · Feb 17, 2014 · N8409N · Cndair CL6002B19 · Emergency Equipment
  > CAPTAIN`S FLASHLIGHT INOPERATIVE. R & R CAPTAIN’S FLASHLIGHT BATTERY IAW CMM 25-60-02, OPERATIONS CHECKED GOOD.
- [SDR REXA2014020400179](https://openairdocs.org/sdr/REXA2014020400179.md): Seal · torn · Feb 4, 2014 · N8409N · Cndair CL6002B19 · Emergency Exits
  > RIGHT EMERGENCY EXIT SEAL TORN. R & R RT EMERGENCY EXIT SEAL IAW CRJ 200 AMM. OPERATIONS CHECK TO 409D WO 54226-10-0000-0001.
- [SDR REXA2014012000008](https://openairdocs.org/sdr/REXA2014012000008.md): Beam · chafed · Jan 18, 2014 · N8409N · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > AFT PRESS BULKHEAD VERTICAL BEAM AT BL 0 IS CHAFED. REPAIRED IAW REO 601R-53-61-1523.
- [SDR REXA201401130007](https://openairdocs.org/sdr/REXA201401130007.md): Bulkhead · gouged · Jan 10, 2014 · N8409N · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FUSELAGE STATION 621 BULKHEAD FWD FACE ABOVE FLOOR HAS MINOR SCREW GOUGES AT WL 86.5 TO WL 112.5, LBL 36.2 TO RBL 36.2. REPAIRED IAW REO 601R-53-61-2155.
- [SDR REXA2013092001741](https://openairdocs.org/sdr/REXA2013092001741.md): Container · torn · Sep 20, 2013 · N8409N · Cndair CL6002B19 · Life Jacket
  > CAPTAIN`S LIFE VEST BAG TORN. REPLACED LIFE VEST IAW AMM 25-61-03.
- [SDR REXA2013042300641](https://openairdocs.org/sdr/REXA2013042300641.md): Frame · corroded · Apr 23, 2013 · N8409N · Cndair CL6002B19 · Fuselage Main, Frame
  > LOWER FRAME SECTOR AT FS 333.00 CORRODED BEYOND LIMITS BETWEEN S-26R AND S-27. REPAIRED IAW EA CRJ253-01517 AND ASSOCIATED 8110-3.
- [SDR REXA2012052200758](https://openairdocs.org/sdr/REXA2012052200758.md): Connector · not seated · May 22, 2012 · N8409N · Cndair CL6002B19 · Light System Wiring
  > LIGHTED CABIN EMERGENCY EXIT SIGN NEAR THE BOTTOM OF THE SERVICE DOOR IS INOP. RESEATED CONNECTOR ON INVERTER NR 1 (PS1LY) IAW ESPM 20 AND OPS CHECKED EMERGENCY LIGHTING IAW AMM 33-51-00. NO FURTHER DEFECTS NOTED.
- [SDR REXA2012042700573](https://openairdocs.org/sdr/REXA2012042700573.md): Detector · defective · Apr 27, 2012 · N8409N · Cndair CL6002B19 · Trailing Flap Position Indicating System
  > FLAPS FAIL AT 20 ON APPROACH. FLAPS PDU1 CB BREAKER POPPED WHEN FLAPS 30 SELECTED AT 165 KNOTS AT 2500 FEET. REMOVED AND REPLACED SKEW DETECTION UNIT POWER SUPPLY IAW AMM 27-51-00. NO FIX.
- [SDR REXA2012033000380](https://openairdocs.org/sdr/REXA2012033000380.md): Bulkhead · cracked · Mar 29, 2012 · N8409N · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > AFT PRESSURE BULKHEAD, FS 621, FOUND CRACKED IN 3 PLACES AROUND THE LINTEL INSTALLATION. REPAIRED IAW BOMBARDIER REO 601R-53-61-1230.
- [SDR REXA2012021400226](https://openairdocs.org/sdr/REXA2012021400226.md): Cover · missing · Feb 14, 2012 · N8409N · Cndair CL6002B19 · Airfoil Anti/De-ice System
  > DIVERTED TO PIT FOR WING ANTI-ICE WARNING MESSAGE. INSTALLED HEAT COVER FOR STBY HEAT SENOR IAW AMM 30-12-12, OPS CHECK GOOD.
- [SDR REXA201200143](https://openairdocs.org/sdr/REXA201200143.md): Coalescer Bag · dirty · Jan 25, 2012 · N8409N · Cndair CL6002B19 · Humidity Control System
  > AIR RETURN FOR SMOKE TOILET-MSG ON TAKEOFF MSG REMAINED UNTIL SHORT FINAL NO SMOKE VISUALLY ONLY 2 PAX FROM 9 A&B REPORTED AN OILY /SMOKE SMELL CFR REPORTED NO SMOKE OR HEAT SIGNATURES. REMOVED AND REPLACED LT &RT COALESCER BAGS IAW AMM 21-51-13. PERFORMED O
- [SDR REXA201100676](https://openairdocs.org/sdr/REXA201100676.md): Battery · discharged · Oct 3, 2011 · N8409N · Cndair CL6002B19 · Emergency Lighting
  > ON COMING CREW REPORTED TO MOC THAT ALL FLOOR EMERGENCY AND EXITS LIGHTS WOULD NOT STAY ON DURING PRE-FLIGHT CHECKS. BATTERY SWITCH WAS IN THE OFF POSITION NOTED BY CREW BEFORE EXTERNAL POWER APPLIED. EXT AC POWER WAS APPLIED AND EMERGENCY BATTERIES RECHARGE
- [SDR REXA201100600](https://openairdocs.org/sdr/REXA201100600.md): Coffeemaker · dirty · Sep 16, 2011 · N8409N · Cndair CL6002B19 · Buffet/Galleys
  > FLIGHT ATTENDANT SMELLED BURNING COMING FROM GALLEY AREA EN ROUTE, TURNED OFF ALL ELECTRICAL SWITCHES AND FANS, SMELL WENT AWAY. CLEANED OFF BURNT COFFEE RESIDUE FROM HOT PLATE ON COFFEEMAKER, RAN COFFEE HOT PLATE, COULD NO LONGER SMELL BURNING SMELL REF GMM
- [SDR REXA201100475](https://openairdocs.org/sdr/REXA201100475.md): Sensing Element · failed · Jul 25, 2011 · N8409N · Cndair CL6002B19 · Pneumatic Indicating System
  > RT 14TH DUCT MASTER WARNING 8,000 FT RED INDICATION BETWEEN 14TH SOV AND WING/COWL VALVES. REMOVED AND REPLACED RT PYLON SENSING ELEMENT (A59WK) IAW AMM 36-21-04. VERIFIED PART EFFECTIVITY. OPS CHECK GOOD. OK FOR SERVICE.
- [SDR REXA201100373](https://openairdocs.org/sdr/REXA201100373.md): Doubler · corroded · Jun 9, 2011 · N8409N · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LT FLOOR SILL STRUCTURE BETWEEN FS 409+128 AND FS 559 HAS MINOR CORROSION ON SKIN DOUBLERS. REPAIRED IAW BOMBARDIER REO 601R-53-41-666 REV A AND BOMBARDIER SERVICE CORPORATION EO 601R-53-21521A.
- [SDR REXA201100372](https://openairdocs.org/sdr/REXA201100372.md): Doubler · corroded · Jun 9, 2011 · N8409N · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RT FLOOR SILL STRUCTURE BETWEEN FS 409+128 AND FS 559 HAS MINOR CORROSION ON SKIN DOUBLERS. REPAIRED IAW BOMBARDIER REO GREO 601R-53-41-666 REV A AND BOMBARDIER SERVICE CORP EO BSC EO 601R-53-21521A.
- [SDR REXA201100369](https://openairdocs.org/sdr/REXA201100369.md): Bulkhead · cracked · Jun 8, 2011 · N8409N · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > EXCESSIVE CRACKING AND CORROSION WAS FOUND ON THE FS 280 BULKHEAD. REPAIRED IAW BOMBARDIER REO 601R-53-11-926 REV B AND BOMBARDIER SERVICE CORP EO 601R-53-21476D.
- [SDR REXA201100366](https://openairdocs.org/sdr/REXA201100366.md): Hinge Fitting · gouged · Jun 7, 2011 · N8409N · Cndair CL6002B19 · Horizontal Stabilizer Structure
  > RIGHT STABILIZER ELEVATOR HINGE FITTING NR 2 AT BL 55.8865 IS GOUGED 0.400"L X 0.020" DEEP. REPAIRED IAW BOMBARDIER REO 601R-55-11-371.
- [SDR REXA201100350](https://openairdocs.org/sdr/REXA201100350.md): Structure · damaged · Jun 4, 2011 · N8409N · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > WHILE INCORPORATING REO 601R-53-42-059 STEP B(1) FOUND PREVIOUS 559 BULKHEAD REPAIR THAT WOULD INTERFERE WITH FUEL QUANTITY DOUBLER. REPAIRED IAW BOMBARDIER REO 601R-53-41-0476.
- [SDR REXA201100339](https://openairdocs.org/sdr/REXA201100339.md): Bulkhead · scratched · Jun 4, 2011 · N8409N · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FS 621 BULKHEAD HAS SCRATCH APPROXIMATELY.650" BELOW REINFORCING STRAP AT RBL 7 APPROX 0.003" DEEP. REPAIRED IAW BOMBARDIER REO 601R-53-61-2155.
- [SDR REXA201100338](https://openairdocs.org/sdr/REXA201100338.md): Structure · chafed · Jun 4, 2011 · N8409N · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS 621 HAS CHAFE DAMAGE AT RBL 18 AND RBL 36, WL 103.25. REPAIRED IAW BOMBARDIER REO 601R-53-61-2155.
- [SDR REXA201100337](https://openairdocs.org/sdr/REXA201100337.md): Bulkhead · chafed · Jun 4, 2011 · N8409N · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FS 621 BULKHEAD WEB HAS CHAFE DAMAGE (SCREW MARKS) AT LBL 18 AND LBL 27 APPROXIMATELY WL 103.25, MEASURED TO BE 0.003" DEEP. REPAIRED IAW BOMBARDIER REO 601R-53-61-2155.
- [SDR REXA201100336](https://openairdocs.org/sdr/REXA201100336.md): Structure · gouged · Jun 4, 2011 · N8409N · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS 621 HAS GOUGE.3" WIDE X.5" LONG BETWEEN RBL 27 AND RBL 36. REPAIRED IAW BOMBARDIER REO 601R-53-61-2155.
- [SDR REXA201100335](https://openairdocs.org/sdr/REXA201100335.md): Hinge Fitting · chafed · Jun 3, 2011 · N8409N · Cndair CL6002B19 · Elevator Structure
  > LT ELEVATOR CENTER HINGE FITTING (ELEVATOR SIDE) IS CHAFED APPROX 1.6" LONG X 0.025" DEEP (MAX) ON LOWER INBD EDGE. REPAIRED IAW EO 601R-55-21492 AND 8110-3 DATED MAY 29, 2011.
- [SDR REXA201100333](https://openairdocs.org/sdr/REXA201100333.md): Skin · damaged · Jun 2, 2011 · N8409N · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN DAMAGE BETWEEN FS 349 AND FS 364 S-16L AND S-17L WAS PREVIOUSLY REPAIRED IAW EO 601R-53-16616 AND WAS DEEMED TEMPORARY BY REO 601R-53-21-115. PERMANENTLY REPAIRED IAW REO 601R-53-21-115.
- [SDR REXA201100332](https://openairdocs.org/sdr/REXA201100332.md): Angle · chafed · Jun 2, 2011 · N8409N · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS 621 REINFORCING ANGLE AT WL 121.5 HAS CHAFE DAMAGE AT RBL 9 AND LBL 7. REPAIRED IAW SRM 53-61-19 AND SRM 53-00-00.
- [SDR REXA201100331](https://openairdocs.org/sdr/REXA201100331.md): Bulkhead · cracked · Jun 1, 2011 · N8409N · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FS 280 BULKHEAD CRACKED ON LT SIDE APPROX 20" FROM FLOOR 1.00" FROM O/B OF DOOR FRAME. REPAIRED IAW BOMBARDIER SERVICE CORPORATION EO 601R-53-21467A AND AUTHORIZED PER 8110-3 DATED MAY 31, 2011.
- [SDR REXA201100319](https://openairdocs.org/sdr/REXA201100319.md): Rib · corroded · May 27, 2011 · N8409N · Cndair CL6002B19 · Nacelle/Pylon, Frame/Spar/Rib
  > LEFT ENGINE PYLON OUTBOARD RIB HAS FRETTING DAMAGE 0.002" DEEP TO PRODUCTION RISER. REPAIRED IAW BOMBARDIER REO 601R-54-54-030 REV H.
- [SDR REXA201100327A](https://openairdocs.org/sdr/REXA201100327A.md): Rib · corroded · May 27, 2011 · N8409N · Cndair CL6002B19 · Nacelle/Pylon, Frame/Spar/Rib
  > LEFT ENGINE PYLON OUTBOARD RIB HAS FRETTING DAMAGE 0.002" DEEP TO PRODUCTION RISER. REPAIRED IAW BOMBARDIER REO 601R-54-54-030 REV H.
- [SDR REXA201100326A](https://openairdocs.org/sdr/REXA201100326A.md): Rib · corroded · May 27, 2011 · N8409N · Cndair CL6002B19 · Nacelle/Pylon, Frame/Spar/Rib
  > RIGHT ENGINE PYLON OUTBOARD RIB HAS FRETTING DAMAGE 0.002" DEEP TO PRODUCTION RISER. REPAIRED IAW REO 601R-54-54-030 REV H.
- [SDR REXA201100249](https://openairdocs.org/sdr/REXA201100249.md): Bulkhead · cracked · Apr 24, 2011 · N8409N · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > CRACK INDICATION AT 559 BULKHEAD WEB LBL 18.00 CRACK IS 1 INCH LONG. CRACK INDICATION AT RBL 18.00 CRACK IS.5 INCH LONG. CRACK INDICATION AT RBL 9.00 IS.25 INCH LONG. REPAIRED IAW BOMBARDIER REO 601R-53-41-260, REV E STEPS 1-14 AND REO 601R- 41-53-609 RE
- [SDR REX2008F00003](https://openairdocs.org/sdr/REX2008F00003.md): Acm · smoke · Jul 1, 2008 · N8409N · Cndair CL6002B19 · Cabin Cooling System
  > CAPTAIN REPORTS WHEN LEFT AIR CYCLE MACHINE (ACM) IS TURNED ON COCKPIT STARTED TO FILL WITH SMOKE. MAINTENANCE DISPATCH, PERFORMED ENG RUNS AND VERIFIED LT ACM FAILURE CAUSING SMOKE. LT ACM DEFERRED PER MEL 21-51-11. (S)
- [SDR REXA201100318](https://openairdocs.org/sdr/REXA201100318.md): Rib · corroded · May 27, 2008 · N8409N · Cndair CL6002B19 · Nacelle/Pylon, Frame/Spar/Rib
  > RIGHT ENGINE PYLON OUTBOARD RIB HAS FRETTING DAMAGE 0.002" DEEP TO PRODUCTION RISER. REPAIRED IAW REPAIRED IAW BOMBARDIER REO 601R-54-54-030 REV H.
- [SDR REXA200700012](https://openairdocs.org/sdr/REXA200700012.md): Unknown · unknown · Jan 28, 2007 · N8409N · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAPS FAILED AT ZERO DEGREES ON APPROACH. LANDING UNEVENTFUL. COMPLIED WITH AD2006-12-21, RESET FLAPS AND MONITORING FOR 72 HOURS.
- [SDR REXA200700002](https://openairdocs.org/sdr/REXA200700002.md): Coalescer Bag · contaminated · Jan 17, 2007 · N8409N · Cndair CL6002B19 · Humidity Control System
  > AIR RETURN FOR SMOKE IN COCKPIT. LANDING UNEVENTFUL. REMOVED AND REPLACED NR 2 COALESCER BAG IAW BOMBARDIER AEROSPACE AMM, RAN ENGINES AND APU, NO SMELL OR SMOKE NOTED.
- [SDR REX2006000110](https://openairdocs.org/sdr/REX2006000110.md): Flap System · malfunctioned · Dec 2, 2006 · N8409N · Cndair CL6002B19 · Trailing Edge Flap Control System
  > RECEIVED FLAPS FAIL INDICATION AT CRUISE. FOLLOWED QRH AND PERFORMED UNEVENTFUL FLAP ZERO LANDING. SYSTEM RESET AND PLACED ON 72 HOUR WATCH PER AD 2006-12-21.
- [SDR REXA200600107](https://openairdocs.org/sdr/REXA200600107.md): Flap System · malfunctioned · Nov 29, 2006 · N8409N · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAPS FAILED AT ZERO ON APPROACH. QRH FOLLOWED UNEVENTFUL LANDING. SYSTEM RESET AND PLACED ON 72 HOUR WATCH PER AD 2006-12-21.
- [SDR REXA200600099](https://openairdocs.org/sdr/REXA200600099.md): Warning Message · illuminated · Oct 28, 2006 · N8409N · Cndair CL6002B19 · Trailing Flap Position Indicating System
  > RECEIVED FLAP FAILURE MESSAGE ON APPROACH. QRH FOLLOWED UNEVENTFUL LANDING. SYSTEM RESET AND PLACED ON 72 HOUR WATCH PER AD 2006-12-21.
- [SDR REXA200600023](https://openairdocs.org/sdr/REXA200600023.md): Windshield · cracked · Feb 17, 2006 · N8409N · Cndair CL6002B19 · Flight Compartment Windows
  > AT 500 FT AGL ON APPROACH, CAPTAINS WINDSHIELD CRACKED. REMOVED AND REPLACED WINDSHIELD.
- [SDR REXA200500144](https://openairdocs.org/sdr/REXA200500144.md): Flap System · failed · Dec 5, 2005 · N8409N · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAPS FAILED AT 0 DEGREES. SYSTEM REST AND PLACED ON 72 HOUR WATCH PER AD 98-20-01.
- [SDR REX2005F00032](https://openairdocs.org/sdr/REX2005F00032.md): Control System · failed · May 28, 2005 · N8409N · Cndair CL6002B19 · Trailing Edge Flap Control System
  > (REF NR: 05071) FLAPS FAIL AT 11 DEGREES ON APPROACH. QRH FOLLOWED UNEVENTFUL LANDING. RESET FLAPS AND PLACED ON 72 HOUR WATCH IAW AD 98-20-01. (K)
- [SDR REXA03006](https://openairdocs.org/sdr/REXA03006.md): Overheat Loop · malfunctioned · Oct 10, 2003 · N8409N · Cndair CL6002B19 · Overheat Detection
  > 14TH STAGE BLEED AIR LIGHT IN FLIGHT, QRH FOLLOWED, UNEVENTFUL LANDING. MAINTENANCE REMOVED AND REPLACED THE RIGHT PYLON DETECTION LOOP. (M)

Next page: https://openairdocs.org/aircraft/N8409N/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 = 'N8409N' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N8409N/reports

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