# Service difficulty reports: N282SK, cancelled Oct 9, 2019

A list on [N282SK, cancelled Oct 9, 2019](https://openairdocs.org/deregistered/N282SK-2019-10-09.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

- [SDR UHLA201606010290](https://openairdocs.org/sdr/UHLA201606010290.md): Gate · out of adjust · Jun 1, 2016 · N282SK · Emb EMB145LR · Passenger/Crew Doors
  > MAIN CABIN DOOR HAS LARGE GAP AT TOP SEAL. RED ALIGN MARKS SLIGHTLY OFF. ADJUSTED MAIN CABIN DOOR FOLDING FLAP IAW AMM 52-10-01.
- [SDR UHLA201605170245](https://openairdocs.org/sdr/UHLA201605170245.md): Spring · broken · May 17, 2016 · N282SK · Emb EMB145LR · Passenger/Crew Doors
  > NR 3 AIRSTAIR STEP SPRING BROKE. R & R SPRING IAW AMM 52-10-07.
- [SDR UHLA201605160248](https://openairdocs.org/sdr/UHLA201605160248.md): Wire · damaged · May 16, 2016 · N282SK · Emb EMB145LR · Door System Wiring
  > GALLEY SERVICE DOOR INDICATES OPEN WHEN SECURED CLOSED AND VERIFIED CLOSED. REPAIRED WIRE ON DOOR HARNESS IAW SRPM.
- [SDR CHQA20140424123](https://openairdocs.org/sdr/CHQA20140424123.md): Proximity Switch · faulty · Apr 24, 2014 · N282SK · Emb EMB145LR · Landing Gear Position and Warning
  > CREW REPORTED THAT THEY RECEIVED A LG AIR & GND FAIL MSG IN FLIGHT. THE CREW RETURNED TO FIELD & LANDED WITHOUT INCIDENT. FOUND THE NLG WEIGHT ON WHEELS SWITCH TO BE FAULTY. THE SWITCH WAS SWAPPED WITH THE LT MLG DOWNLOCK PROXIMITY SWITCH & DEFERRED. THE D
- [SDR CHQA20140418111](https://openairdocs.org/sdr/CHQA20140418111.md): Strut · underserviced · Apr 18, 2014 · N282SK · Emb EMB145LR · Nose/Tail Landing Gear Strut/Axle
  > CREW REPORTED THAT AFTER TAKEOFF THEY RECEIVED A LG AIR & GND FAIL MSG. THE CREW RETURNED TO FIELD & LANDED WITHOUT INCIDENT. THE ACFT WAS FOUND SAFE FOR FERRY FLIGHT & FLEW TO KCMH FOR REPAIR. REPACKED THE NOSE LG STRUT. OPERATIONAL CHECKS WERE GOOD WITH
- [SDR CHQA20140407109](https://openairdocs.org/sdr/CHQA20140407109.md): Wire Harness · faulty · Apr 7, 2014 · N282SK · Emb EMB145LR · Landing Gear System Wiring
  > CREW REPORTED THAT AFTER TAKEOFF, THEY RECEIVED A LG AIR & GND FAIL MSG & THAT THE LG DID NOT RETRACT. THE CREW ELECTED TO RETURN TO FIELD & LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE LEFT-HAND WEIGHT ON WHEELS PROXIMITY SWITCH NUMBER 1, THE RIGHT HAN
- [SDR CHQA20140331099](https://openairdocs.org/sdr/CHQA20140331099.md): Electronic Unit · faulty · Mar 31, 2014 · N282SK · Emb EMB145LR · Landing Gear Position and Warning
  > CREW REPORTED THAT AFTER TAKEOFF, THEY RECEIVED A LG AIR & GND FAIL MSG & THAT THE LG DID NOT RETRACT. THE CREW ELECTED TO RETURN TO FIELD & LANDED WITHOUT INCIDENT. THE WEIGHT ON WHEELS PROXIMITY SWITCHES WERE INSPECTED WITH NO DEFECTS NOTED. THE ACFT WAS
- [SDR CHQA20140324092](https://openairdocs.org/sdr/CHQA20140324092.md): Proximity Switch · faulty · Mar 24, 2014 · N282SK · Emb EMB145LR · Landing Gear Position and Warning
  > CREW REPORTED THAT AFTER TAKEOFF THEY RECEIVED A LG AIR & GND FAIL MESSAGE & THAT THE LG WOULD NOT RETRACT. THE CREW RETURNED TO FIELD & LANDED WITHOUT INCIDENT. THE ACFT WAS FOUND SAFE FOR FERRY FLIGHT & WAS FERRIED TO KCMH FOR REPAIR. REPLACED BOTH RT MLG
- [SDR CHQA20131212445](https://openairdocs.org/sdr/CHQA20131212445.md): Windshield · cracked · Dec 12, 2013 · N282SK · Emb EMB145LR · Flight Compartment Windows
  > CREW REPORTED THAT DURING CLIMB, THE CAPTAIN`S WINDSHIELD CRACKED. THE CREW DECLARED AN EMERGENCY & RETURNED TO FIELD. MX REPLACED THE LT WINDSHIELD. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.
- [SDR CHQA20130904337](https://openairdocs.org/sdr/CHQA20130904337.md): Wire · inoperative · Sep 4, 2013 · N282SK · Emb EMB145LR · Light System Wiring
  > DURING INSPECTION, A WIRE WAS FOUND TO BE BROKEN IN AN EMERGENCY LIGHT. MX REPLACED THE LIGHT AND NO FURTHER DEFECTS HAVE BEEN NOTED.
- [SDR CHQA20130705257](https://openairdocs.org/sdr/CHQA20130705257.md): Inverter · inoperative · Jul 5, 2013 · N282SK · Emb EMB145LR · Emergency Lighting
  > DURING INSPECTION, RT EMERGENCY EXIT SIGN FOUND TO BE INOPERATIVE. MX FOUND NR 5 INVERTER TO INOPERATIVE AND REPLACED IT, OPS CHECKED GOOD.
- [SDR CHQA20130627234](https://openairdocs.org/sdr/CHQA20130627234.md): Windshield · cracked · Jun 27, 2013 · N282SK · Emb EMB145LR · Flight Compartment Windows
  > CREW REPORTED THAT DURING CLIMB OUT, THE F/O WINDOW CRACKED. THE CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. THE ACFT WAS FERRIED. MX REPLACED THE RT WINDSHIELD. LEAK CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.
- [SDR CHQA20130623231](https://openairdocs.org/sdr/CHQA20130623231.md): Sign · inoperative · Jun 23, 2013 · N282SK · Emb EMB145LR · Emergency Lighting
  > DURING INSPECTION, THE EMERGENCY EXIT SIGN ABOVE THE SERVICE DOOR WAS FOUND TO BE INOPERATIVE. MX REPLACED THE SIGN AND OPS CHECKED GOOD. NO FURTHER DEFECTS WERE NOTED.
- [SDR CHQA20130623230](https://openairdocs.org/sdr/CHQA20130623230.md): Battery · inoperative · Jun 23, 2013 · N282SK · Emb EMB145LR · Emergency Lighting
  > DURING INSPECTION, THE FIRST THREE EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MX REPLACED THE NR 2 BATTERY. OPS CHECKED GOOD AND NO FURTHER DEFECTS WERE NOTED.
- [SDR CHQA20130409108](https://openairdocs.org/sdr/CHQA20130409108.md): Antenna · failed · Apr 9, 2013 · N282SK · Emb EMB145LR · Visual Omnirange (VOR) System
  > DURING APPROACH, CREW REPORTED ILS 1 AND 2 ERRATIC. DIVERTED AND LANDED WITHOUT INCIDENT. VOR/ILS STABILIZER ANTENNA 1 AND 2 WERE REPLACED. OPS CHECKED GOOD.
- [SDR CHQA20130406109](https://openairdocs.org/sdr/CHQA20130406109.md): Fitting · cracked · Apr 6, 2013 · N282SK · Emb EMB145LR · Fuselage Miscellaneous Structure
  > MAINTENANCE FOUND A CRACK IN THE SHEAR CLIP IN FRAME 28 BETWEEN STRINGERS 15R AND 16R. A REPLACEMENT SHEAR CLIP WAS FABRICATED AND INSTALLED IN ACCORDANCE WITH SRM 51-20-01 AND SRM 51-40-02.
- [SDR CHQA20130314079](https://openairdocs.org/sdr/CHQA20130314079.md): Light · inoperative · Mar 14, 2013 · N282SK · Emb EMB145LR · Emergency Lighting
  > CREW REPORTED THAT THE FIRST THREE EMERGENCY LIGHT PROXIMITY STRIPS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE FORWARD FLOOR EMERGENCY LIGHTING STRIP. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.
- [SDR CHQA20121103405](https://openairdocs.org/sdr/CHQA20121103405.md): Sign · inoperative · Nov 3, 2012 · N282SK · Emb EMB145LR · Emergency Lighting
  > DURING INSPECTION, THE EMERGENCY EXIT SIGN ABOVE SEAT 12F WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY EXIT SIGN AT ROW 12, OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.
- [SDR CHQA20120516172](https://openairdocs.org/sdr/CHQA20120516172.md): Beam · corroded · May 16, 2012 · N282SK · Emb EMB145LR · Fuselage Miscellaneous Structure
  > DURING INSPECTION, THE CENTER FUSELAGE I RIGHT BEAM AT FRAME 22 WAS FOUND TO BE CORRODED. THE CENTER FUSELAGE RIGHT BEAM WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02.
- [SDR CHQA20120516171](https://openairdocs.org/sdr/CHQA20120516171.md): Frame · cracked · May 16, 2012 · N282SK · Emb EMB145LR · Fuselage Main, Frame
  > DURING INSPECTION, FRAME 66 WAS FOUND TO BE CRACKED UNDER THE LOWER BEAM. FRAME 66, UNDER THE LOWER BEAM, WAS REPAIRED IN ACCORDANCE WITH ETD 2012-145-007135.
- [SDR CHQA20120514177](https://openairdocs.org/sdr/CHQA20120514177.md): Skin · damaged · May 14, 2012 · N282SK · Emb EMB145LR · Fuselage Main, Plate/Skin
  > DURING INSPECTION, A SKIN BURN FROM A LIGHTNING STRIKE WAS FOUND ON THE RIGHT FUSELAGE SKIN BETWEEN FRAME 30 AND FRAME 31 AT STRINGER 16R. THE RIGHT FUSELAGE SKIN BETWEEN FRAME 30 AND FRAME 31 AT STRINGER 16R WAS REPAIRED IN ACCORDANCE WITH SRM 53-22-01.
- [SDR CHQA20120514176](https://openairdocs.org/sdr/CHQA20120514176.md): Skin · burned · May 14, 2012 · N282SK · Emb EMB145LR · Fuselage Main, Plate/Skin
  > DURING INSPECTION, A SKIN BURN FROM A LIGHTNING STRIKE WAS FOUND ON THE RIGHT FUSELAGE SKIN BETWEEN FRAME 24 AND FRAME 25 AT STRINGER 18R. THE RIGHT FUSELAGE SKIN BETWEEN FRAME 24 AND FRAME 25 AT STRINGER 18R WAS REPAIRED IN ACCORDANCE WITH SRM 53-22-01.
- [SDR CHQA20120514175](https://openairdocs.org/sdr/CHQA20120514175.md): Shear Plate · corroded · May 14, 2012 · N282SK · Emb EMB145LR · Fuselage Miscellaneous Structure
  > DURING INSPECTION, THE FORWARD AND AFT L-SHAPES ON THE CARGO DOOR CUTOUT WERE FOUND TO BE CORRODED. THE FORWARD AND AFT L-SHAPES ON THE CARGO DOOR CUTOUT WERE REPAIRED IN ACCORDANCE WITH ETD 2012-145-006943.
- [SDR CHQA20120514174](https://openairdocs.org/sdr/CHQA20120514174.md): Shear Plate · corroded · May 14, 2012 · N282SK · Emb EMB145LR · Fuselage Miscellaneous Structure
  > DURING INSPECTION, THE FORWARD AND AFT L-SHAPES ON THE CARGO DOOR CUTOUT WERE FOUND TO BE CORRODED. THE FORWARD AND AFT L-SHAPES ON THE CARGO DOOR CUTOUT WERE REPAIRED IN ACCORDANCE WITH ETD 2012-145-006943.
- [SDR CHQA20120514170](https://openairdocs.org/sdr/CHQA20120514170.md): Frame · cracked · May 14, 2012 · N282SK · Emb EMB145LR · Fuselage Main, Frame
  > DURING INSPECTION, THE RIGHT FRAME 10 WAS FOUND TO BE CRACKED. THE RIGHT FRAME 10 WAS REPLACED. THE NEW PART WAS INSTALLED WITH A SOLID RIVET IN ACCORDANCE WITH SRM 51-40-02.
- [SDR CHQA20120514169](https://openairdocs.org/sdr/CHQA20120514169.md): Frame · cracked · May 14, 2012 · N282SK · Emb EMB145LR · Fuselage Main, Frame
  > DURING INSPECTION, THE LEFT FRAME 10 WAS FOUND TO BE CRACKED. THE LEFT FRAME 10 WAS REPLACED. THE NEW PART WAS INSTALLED WITH A SOLID RIVET IN ACCORDANCE WITH SRM 51-40-02.
- [SDR CHQA20120514168](https://openairdocs.org/sdr/CHQA20120514168.md): Floor Support · corroded · May 14, 2012 · N282SK · Emb EMB145LR · Fuselage Miscellaneous Structure
  > DURING INSPECTION, THE CENTER FUSELAGE I LEFT INBOARD OMEGA BEAM HAD AN EXISTING REPAIR THAT WAS FOUND TO BE CORRODED AT FRAME 20. THE CENTER FUSELAGE I LEFT INBOARD OMEGA BEAM AT FRAME 20 WAS REPAIRED IN ACCORDANCE WITH SRM 53-00-10.
- [SDR CHQA20120514167](https://openairdocs.org/sdr/CHQA20120514167.md): Beam · corroded · May 14, 2012 · N282SK · Emb EMB145LR · Fuselage Miscellaneous Structure
  > DURING INSPECTION, THE CARGO DOOR CUTOUT LOWER BEAM WAS FOUND TO BE CORRODED. THE LOWER BEAM ON THE CARGO DOOR CUTOUT WAS REPLACED. THE NEW PART WAS INSTALLED WITH A SOLID RIVET IN ACCORDANCE WITH SRM 51-40-02.
- [SDR CHQA20120513166](https://openairdocs.org/sdr/CHQA20120513166.md): Floor Support · cracked · May 13, 2012 · N282SK · Emb EMB145LR · Fuselage Miscellaneous Structure
  > DURING INSPECTION, THE CENTER FUSELAGE III RIGHT OMEGA BEAM ANGLE WAS FOUND TO BE CRACKED. THE CENTER FUSELAGE III RIGHT OMEGA BEAM ANGLE WAS REPAIRED IN ACCORDANCE WITH SRM 53-23-02.
- [SDR CHQA20120513165](https://openairdocs.org/sdr/CHQA20120513165.md): Floor Support · cracked · May 13, 2012 · N282SK · Emb EMB145LR · Fuselage Miscellaneous Structure
  > DURING INSPECTION, THE CENTER FUSELAGE III RIGHT OMEGA BEAM ANGLE WAS FOUND TO BE CRACKED. THE CENTER FUSELAGE III RIGHT OMEGA BEAM ANGLE WAS REPAIRED IN ACCORDANCE WITH SRM 53-23-02.
- [SDR CHQA20120513164](https://openairdocs.org/sdr/CHQA20120513164.md): Floor Support · cracked · May 13, 2012 · N282SK · Emb EMB145LR · Fuselage Miscellaneous Structure
  > DURING INSPECTION, THE CENTER FUSELAGE III LEFT OMEGA BEAM ANGLE WAS FOUND TO BE CRACKED. THE CENTER FUSELAGE III LEFT OMEGA BEAM ANGLE WAS REPAIRED IN ACCORDANCE WITH SRM 53-23-02.
- [SDR CHQA20120513163](https://openairdocs.org/sdr/CHQA20120513163.md): Floor Support · cracked · May 13, 2012 · N282SK · Emb EMB145LR · Fuselage Miscellaneous Structure
  > DURING INSPECTION, THE CENTER FUSELAGE III LEFT OMEGA BEAM ANGLE WAS FOUND TO BE CRACKED. THE CENTER FUSELAGE III LEFT OMEGA BEAM ANGLE WAS REPAIRED IN ACCORDANCE WITH SRM 53-23-02.
- [SDR CHQA20120322087](https://openairdocs.org/sdr/CHQA20120322087.md): Light · inoperative · Mar 22, 2012 · N282SK · Emb EMB145LR · Emergency Lighting
  > DURING INSPECTION, THE HAND RAIL EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE HAND RAIL EMERGENCY LIGHT BULB. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.
- [SDR CHQA201100396](https://openairdocs.org/sdr/CHQA201100396.md): O-Ring · leaking · Oct 2, 2011 · N282SK · Emb EMB145LR · Pneumatic Distribution System
  > CREW REPORTED, RECEIVED A BLEED 1 LEAK MESSAGE DURING CLIMB. THE AIRCRAFT RETURNED TO KCLE AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE O-RINGS AT JOINTS 13, 15, 17, 19, AND 23 IN THE BLEED 1 SYSTEMS. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DE
- [SDR CHQA201000170](https://openairdocs.org/sdr/CHQA201000170.md): Clamp · loose · Aug 29, 2010 · N282SK · Emb EMB145LR · Cabin Pressure Control System
  > WHILE CLIMBING OUT OF MKE, THE CREW NOTICED THAT THE CABIN ALTITUDE RATE WAS THE SAME AS THE AIRCRAFT. THE AIRCRAFT WAS LEVELED AT 13,000FT WITH A DIFFERENTIAL PRESSURE OF 1.9 IN AUTO MODE. THE FLIGHT DESCENDED TO 12,000FT WITH 8,000FT INDICATED FOR CABIN AL
- [SDR CHQA201000169](https://openairdocs.org/sdr/CHQA201000169.md): Controller · faulty · Aug 28, 2010 · N282SK · Emb EMB145LR · Cabin Pressure Controller
  > WHILE CLIMBING OUT OF MKE, THE CREW REPORTED THAT AT AROUND 14,000FT THE CABIN ALTITUDE WAS NEARING 10,000FT WITH AUTO PRESSURIZATION. THE AIRCRAFT DESCENDED TO 10,000FT FOLLOWED THE QRH AND RETURNED TO MKE WHERE THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTEN
- [SDR CHQA201000137](https://openairdocs.org/sdr/CHQA201000137.md): Wire · broken · Jul 8, 2010 · N282SK · Emb EMB145LR · Light System Wiring
  > DURING INSPECTION, A FLOOR PROXIMITY LIGHT STRIP WAS FOUND TO HAVE BROKEN WIRES. MAINTENANCE REPLACED THE FLOOR PROXIMITY LIGHT STRIP IAW EMB 145 AMM 33-50-12.
- [SDR CHQA201000136](https://openairdocs.org/sdr/CHQA201000136.md): Wire · missing · Jul 7, 2010 · N282SK · Emb EMB145LR · Light System Wiring
  > DURING INSPECTION, THE EMERGENCY EXIT DOOR LIGHTED PROXIMITY LIGHT STRIP WAS FOUND TO BE MISSING WIRES. MAINTENANCE REPLACED THE PROXIMITY PHOTO-LUMINESCENT LIGHT STRIP IAW EMB 145 AMM 33-50-12.
- [SDR CHQA200900120](https://openairdocs.org/sdr/CHQA200900120.md): Light · inoperative · May 2, 2009 · N282SK · Emb EMB145LR · Emergency Lighting
  > DURING INSPECTION THE FLOOR PROXIMITY LIGHTS 6, 7, AND 8 WERE FOUND TO BE INOPERATIVE WHEN TESTED. THE NR 8 FLOOR PROXIMITY LIGHT STRIP WAS REPLACED AND LIGHTS 6, 7, AND 8 OPERATED NORMALLY IAW AMM 33-50-12.
- [SDR CHQA200900086](https://openairdocs.org/sdr/CHQA200900086.md): Battery Pack · discharged · Mar 20, 2009 · N282SK · Emb EMB145LR · Emergency Lighting
  > DURING INSPECTION MAINTENANCE FOUND THE FLOOR LIGHT STRIPS 6, 7, AND 8 INOPERATIVE WHEN TESTING THE EMERGENCY LIGHT SYSTEM. THE NR 4 EMERGENCY LIGHT BATTERY WAS REPLACED AND THE EMERGENCY LIGHTS OPERATED NORMALLY.
- [SDR CHQA200900035](https://openairdocs.org/sdr/CHQA200900035.md): Switch · malfunctioned · Jan 26, 2009 · N282SK · Emb EMB145LR · Cabin Cooling System
  > WITH PACK 2 ON DEFERRAL AND E2 ANTI-ICE BLEED SECURED OPEN AND T/O POWER TAKEOFF WAS REQUIRED. AFTER DEPARTURE PACK NR 1 SHUTDOWN DUE TO OVERHEAT. THE QRH WAS FOLLOWED, BUT THE PACK WAS STILL SHUTTING DOWN. THE FLIGHT RETURNED TO THE FIELD AND LANDED WITHOU
- [SDR CHQA200800134](https://openairdocs.org/sdr/CHQA200800134.md): Indication Sys · malfunctioned · Jul 8, 2008 · N282SK · Emb EMB145LR · Hydraulic Indicating System
  > FLIGHT 3043, LGA TO IND. DURING CLIMBOUT OF LGA THE FLT CREW RECEIVED A HYDRAULIC 1 LOW QUANTITY EICAS MESSAGE. THE HYDRAULIC QUANTITY INDICATED AT THE TOP OF THE YELLOW RANGE. THIRTY MINUTES LATER THE QTY INDICATION HAD DROPPED TO JUST BELOW ONE THIRD OF T
- [SDR CHQA200600142](https://openairdocs.org/sdr/CHQA200600142.md): Ecu · failed · Dec 27, 2006 · N282SK · Emb EMB145LR · Trailing Edge Flap Control System
  > FLIGHT 3163 - BOS-ROC - CLIMBING OUT AT APPROXIMATELY FL200, RECEIVED "FLAP FAIL" AND "SPS ADVANCED". FLAPS STUCK AT 0 DEGREES, HIGH SPEED LANDING IN BOS. DECLARED AN EMERGENCY, LANDED UNEVENTFULLY. MAINTENANCE REMOVED AND REPLACED FLAP ELECTRONIC CONTROL U
- [SDR CHQA200600030](https://openairdocs.org/sdr/CHQA200600030.md): Wire · broken · Feb 28, 2006 · N282SK · Emb EMB145LR · Emergency Lighting
  > AIRSTAIR EMERGENCY LIGHT CONNECTION (BLUE RUBBER ONE) HAS A BROKEN WIRE. REPAIRED AIRSTAIRS LIGHT WIRE IAW EMB 145 MM 20-21-00. OPS CHECK GOOD AT THIS TIME.
- [SDR CHQA200500108](https://openairdocs.org/sdr/CHQA200500108.md): Odor · detected · Jun 7, 2005 · N282SK · Emb EMB145LR · Air Distribution System
  > FLIGHT 3049 DCA-GSO - AFTER TAKEOFF, CAPTAIN AND FIRST OFFICER DETECTED A BURNING ODOR IN THE COCKPIT AND CABIN. CYCLED BOTH BLEED SYSTEMS AND ODOR WENT AWAY. MAINTENANCE RAN BOTH ENGINES AND CYCLED BOTH BLEED VALVES. NO ODORS NOTED AT THIS TIME. OPS CHECK

## 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 = 'N282SK' AND deregistration_id = 'N282SK-2019-10-09'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N282SK-2019-10-09/reports

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