# Service difficulty reports: N266SK, cancelled May 23, 2018

A list on [N266SK, cancelled May 23, 2018](https://openairdocs.org/deregistered/N266SK-2018-05-23.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 · 65 reports

- [SDR UHLA201507300614](https://openairdocs.org/sdr/UHLA201507300614.md): Apu · fire · Jul 30, 2015 · N266SK · Emb EMB145LR · Airborne Auxiliary Power Unit (APU) System
  > WHILE APPROACHING THE GATE, THE CREW DISCHARGED THE APU FIRE BOTTLES AFTER A CONFIRMED APU FIRE. THE APU WAS R & R.
- [SDR UHLA2015022200118](https://openairdocs.org/sdr/UHLA2015022200118.md): None · none · Feb 22, 2015 · N266SK · Emb EMB145LR · Standard Practices/Structures
  > THE CREW REPORTED THAT THEY SUSPECTED A FUEL LEAK IN THE RT WING TANK DURING FLIGHT. THE CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE RT WING SURFACES AND PERFORMED OPS CHECKS OF THE FUEL SYSTEM WITH NO LEAKS OR DEFECTS NOTED
- [SDR CHQA20141119328](https://openairdocs.org/sdr/CHQA20141119328.md): Light · inoperative · Nov 19, 2014 · N266SK · Emb EMB145LR · Emergency Lighting
  > DURING INSPECTION, THE EMER FLOOR PROXIMITY LIGHT STRIP AT ROW 6 WAS FOUND TO BE INOPERATIVE. THE LIGHT WAS REPLACED. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.
- [SDR CHQA20140829255](https://openairdocs.org/sdr/CHQA20140829255.md): Floor Support · corroded · Aug 29, 2014 · N266SK · Emb EMB145LR · Fuselage Miscellaneous Structure
  > DURING INSPECTION THE RT OMEGA BEAM WAS FOUND TO BE CORRODED BETWEEN FRAME 59 & 60. THE BEAM WAS REPLACED IAW ETD 2014-145-073053.
- [SDR CHQA20140829253](https://openairdocs.org/sdr/CHQA20140829253.md): Floor Support · corroded · Aug 29, 2014 · N266SK · Emb EMB145LR · Fuselage Miscellaneous Structure
  > DURING INSPECTION CORROSION WAS FOUND ON THE CTR OMEGA BEAM AT FRAME 20. THE OMEGA BEAM WAS REPLACED IAW SRM 51-40-02.
- [SDR CHQA20140828252](https://openairdocs.org/sdr/CHQA20140828252.md): Skin · chafed · Aug 28, 2014 · N266SK · Emb EMB145LR · Cargo/Baggage Doors
  > DURING INSPECTION THE CARGO DOOR INNER SKIN WAS FOUND TO HAVE CHAFE MARKS ON THE LOWER AFT END. THE SKIN WAS REPLACED IAW SRM 51-40-02.
- [SDR CHQA20140827254](https://openairdocs.org/sdr/CHQA20140827254.md): Firewall · cracked · Aug 27, 2014 · N266SK · Emb EMB145LR · Fuselage Main, Bulkhead
  > DURING INSPECTION THE APU FIREWALL WAS FOUND TO BE CRACKED UNDER THE UPPER LT SUPPORT ROD. THE APU FIREWALL WAS REPAIRED IAW SRM 53-32-13.
- [SDR CHQA20140826256](https://openairdocs.org/sdr/CHQA20140826256.md): Doubler · corroded · Aug 26, 2014 · N266SK · Emb EMB145LR · Fuselage Miscellaneous Structure
  > DURING INSPECTION THE LT OMEGA BEAM REPAIR DOUBLER ON THE INBD SIDE WAS FOUND TO BE CORRODED AT FRAME 20. THE REPAIR DOUBLER WAS REPLACED IAW SRM 53-00-10.
- [SDR CHQA20140826250](https://openairdocs.org/sdr/CHQA20140826250.md): Seat Track · corroded · Aug 26, 2014 · N266SK · Emb EMB145LR · Fuselage, Seat/Cargo Attach Fittings
  > DURING INSPECTION CORROSION WAS FOUND ON THE CTR OMEGA BEAM SEAT TRACK FROM FRAME 25 - 30. THE SEAT TRACK WAS REPLACED IAW AMM 53-01-06.
- [SDR CHQA20140826249](https://openairdocs.org/sdr/CHQA20140826249.md): Seat Track · corroded · Aug 26, 2014 · N266SK · Emb EMB145LR · Fuselage, Seat/Cargo Attach Fittings
  > DURING INSPECTION CORROSION WAS FOUND ON THE LT OMEGA BEAM SEAT TRACK FROM FRAME 25 THROUGH FRAME 30. THE SEAT TRACK WAS REPLACED IAW AMM 53-01-06.
- [SDR CHQA20140825251](https://openairdocs.org/sdr/CHQA20140825251.md): Profile · corroded · Aug 25, 2014 · N266SK · Emb EMB145LR · Cargo/Baggage Doors
  > DURING INSPECTION CORROSION WAS FOUND ON THE LOWER PROFILE ON THE CARGO DOOR. THE PROFILE WAS REPLACED IAW SRM 51-40-02.
- [SDR CHQA20140518150](https://openairdocs.org/sdr/CHQA20140518150.md): Flap · malfunctioned · May 18, 2014 · N266SK · Emb EMB145LR · Trailing Edge Flap Control System
  > DURING APPROACH, THE FLIGHT CREW RECEIVED A FLAP FAIL MSG ON THE EICAS DISPLAY. AFTER RUNNING THE CHECKLIST IN THE QRH, AN EMERGENCY WAS DECLARED & A SUCCESSFUL LANDING WAS COMPLETED. RESET THE FLAP SYS & THE MSG CLEARED. NO FURTHER DEFECTS HAVE BEEN NOTED.
- [SDR CHQA20140430128](https://openairdocs.org/sdr/CHQA20140430128.md): Inverter · inoperative · Apr 30, 2014 · N266SK · Emb EMB145LR · Emergency Lighting
  > DURING INSPECTION, THE FWD CABIN COCKPIT ENTRANCE EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. REPLACED THE FWD CLOSET INVERTER. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.
- [SDR CHQA20140429127](https://openairdocs.org/sdr/CHQA20140429127.md): Transceiver · faulty · Apr 29, 2014 · N266SK · Emb EMB145LR · Weather Radar System
  > CREW REPORTED THAT THE WEATHER RADAR WAS INOPERATIVE. THE CREW DIVERTED THE ACFT & LANDED WITHOUT INCIDENT. REPLACED THE WEATHER RADAR RECEIVER & TRANSMITTER ASSEMBLY. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.
- [SDR CHQA20140218062](https://openairdocs.org/sdr/CHQA20140218062.md): Battery · discharged · Feb 18, 2014 · N266SK · Emb EMB145LR · Emergency Lighting
  > DURING INSPECTION, BOTH OVERWING EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MX REPLACED THE NR 4 EMERGENCY BATTERY & ALL OPERATIONAL CHECKS WERE GOOD.
- [SDR CHQA20140116016](https://openairdocs.org/sdr/CHQA20140116016.md): Battery · discharged · Jan 16, 2014 · N266SK · Emb EMB145LR · Emergency Lighting
  > DURING INSPECTION, THE AFT OVERWING EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. REPLACED THE NR 4 EMERGENCY BATTERY. OPERATIONS CHECKED GOOD WITH NO FURTHER DEFECTS NOTED.
- [SDR CHQA20140102001](https://openairdocs.org/sdr/CHQA20140102001.md): Battery · discharged · Jan 2, 2014 · N266SK · Emb EMB145LR · Emergency Lighting
  > DURING INSPECTION, THE RT & LT AFT OVERWING EMERGENCY EXIT LIGHTS WERE FOUND TO BE INOPERATIVE. REPLACED THE NR 4 EMERGENCY LIGHT BATTERY. OPERATIONS CHECKED GOOD WITH NO FURTHER DEFECTS NOTED.
- [SDR CHQA20131219457](https://openairdocs.org/sdr/CHQA20131219457.md): Warning System · false activation · Dec 19, 2013 · N266SK · Emb EMB145LR · Landing Gear Position and Warning
  > CREW REPORTED THAT ON APPROACH THEY RECEIVED AN AURAL WARNING FOR LG. ALL THREE GEAR INDICATED DOWN & LOCKED. THE CREW DID A GO AROUND & ON THE SECOND APPROACH THE AURAL MESSAGE REPEATED. AGAIN, ALL THREE GEAR INDICATED DOWN & LOCKED & THERE WERE NO EICAS I
- [SDR CHQA20131210444](https://openairdocs.org/sdr/CHQA20131210444.md): Battery Pack · discharged · Dec 10, 2013 · N266SK · Emb EMB145LR · Emergency Lighting
  > THE AFT EXTERIOR LT & RT FUSELAGE LIGHTS FAILED TO ILLUMINATE. MX REPLACED THE NR 4 EMERGENCY LIGHT BATTERY PACK & ALL OPERATIONS CHECKED GOOD.
- [SDR CHQA20131016370](https://openairdocs.org/sdr/CHQA20131016370.md): Duct · disconnected · Oct 16, 2013 · N266SK · Emb EMB145LR · Air Distribution System
  > CREW REPORTED THAT DURING CLIMB THERE WAS SMOKE IN THE CABIN AROUND SEAT 9A. DECLARED AND EMERGENCY AND RETURNED TO FIELD, LANDED WITHOUT INCIDENT. MAINTENANCE FOUND AIR CONDITIONING DUCT DISCONNECTED AND PRODUCING CONDENSATION INSIDE CABIN. DUCT RECONNECTE
- [SDR CHQA20130822329](https://openairdocs.org/sdr/CHQA20130822329.md): Frame · damaged · Aug 22, 2013 · N266SK · Emb EMB145LR · Fuselage Main, Frame
  > DURING INSPECTION, A HOLE WAS FOUND ON THE RT SIDE OF FRAME 65 BETWEEN STRINGERS 12R AND 13R. THE FRAME WAS REPAIRED IAW ETD 2013-145-032262.
- [SDR CHQA20130822328](https://openairdocs.org/sdr/CHQA20130822328.md): Support · cracked · Aug 22, 2013 · N266SK · Emb EMB145LR · Fuselage Miscellaneous Structure
  > DURING INSPECTION, A CRACK WAS FOUND IN THE RT INBD OMEGA BEAM SUPPORT AT FRAME 47 AND 48. THE OMEGA BEAM SUPPORTS WERE REPLACED IAW SRM 51-40-02.
- [SDR CHQA20130822327](https://openairdocs.org/sdr/CHQA20130822327.md): Channel · corroded · Aug 22, 2013 · N266SK · Emb EMB145LR · Fuselage Miscellaneous Structure
  > DURING INSPECTION, CORROSION WAS FOUND ON THE REPAIR DOUBLER OF LT OMEGA FRAME 20. THE DOUBLER WAS REPLACED IAW SRM 53-00-10.
- [SDR CHQA20130822326](https://openairdocs.org/sdr/CHQA20130822326.md): Frame · bent · Aug 22, 2013 · N266SK · Emb EMB145LR · Fuselage Main, Frame
  > DURING INSPECTION, FRAME 72 WAS FOUND BENT AT STRINGER 16R. FRAME REPAIRED IAW ETD 2013-145-032192-A.
- [SDR CHQA20130820320](https://openairdocs.org/sdr/CHQA20130820320.md): Battery Pack · inoperative · Aug 20, 2013 · N266SK · Emb EMB145LR · Emergency Lighting
  > DURING INSPECTION, NR 4 AND 5 EMERGENCY LIGHTS FOUND TO BE INOPERATIVE. REPLACED BATTERY PACK AND OPS CHECKED GOOD.
- [SDR CHQA20130621226](https://openairdocs.org/sdr/CHQA20130621226.md): Battery Pack · inoperative · Jun 21, 2013 · N266SK · Emb EMB145LR · Emergency Lighting
  > DURING INSPECTION, OVERWING EMERGENCY EXIT LIGHTS WERE FOUND TO BE INOPERATIVE. MX REPLACED THE NR 4 EMERGENCY LIGHT BATTERY. OPS CHECKED GOOD WITH NO FURTHER DEFECTS NOTED.
- [SDR CHQA20130509163](https://openairdocs.org/sdr/CHQA20130509163.md): Battery · discharged · May 9, 2013 · N266SK · Emb EMB145LR · Emergency Lighting
  > DURING INSPECTION, THE AFT OVERWING EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE NUMBER 4 EMERGENCY LIGHT BATTERY. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.
- [SDR CHQA20130222061](https://openairdocs.org/sdr/CHQA20130222061.md): Connector · corroded · Feb 22, 2013 · N266SK · Emb EMB145LR · Engine Control System Wiring
  > CREW REPORTED THAT ON TAKEOFF THEY SELECTED THE CLIMB THRUST RATING AND THE MODE AUTOMATICALLY REVERTED TO T/O THRUST MODE. THE CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED CORROSION FROM THE PINS ON RESISTOR MODULES A7055 AND A705
- [SDR CHQA20130114014](https://openairdocs.org/sdr/CHQA20130114014.md): Bleed Valve · faulty · Jan 14, 2013 · N266SK · Emb EMB145LR · Compressor Bleed Valve
  > CREW REPORTED THAT DURING FLIGHT THEY RECEIVED A BLEED 2 VALVE FAIL MESSAGE ALONG WITH A BLEED 2 VALVE CLOSED MESSAGE. DUE TO WEATHER RESTRICTIONS THE FLIGHT DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE ENGINE 2 BLEED VALVE. OPERATIONAL CH
- [SDR CHQA20121210469](https://openairdocs.org/sdr/CHQA20121210469.md): Ecu · faulty · Dec 10, 2012 · N266SK · Emb EMB145LR · Trailing Edge Flap Control System
  > CREW REPORTED, FLAP FAIL MESSAGE ON APPROACH TO KRHI. THE CREW RETURNED TO FIELD IN KMKE AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE FLAP ELECTRONIC CONTROL UNIT. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.
- [SDR CHQA20121209459](https://openairdocs.org/sdr/CHQA20121209459.md): Ecu · faulty · Dec 9, 2012 · N266SK · Emb EMB145LR · Trailing Edge Flap Control System
  > CREW REPORTED, RECEIVED A FLAP FAIL MESSAGE AFTER GEAR RETRACTION. THE CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE RESET THE FLAPS AND A FLAP LOW SPEED MESSAGE APPEARED. THE ITEM WAS DEFERRED. THE DEFERRAL WAS CLEARED ON 12/10/2012 BY R
- [SDR CHQA20120906312](https://openairdocs.org/sdr/CHQA20120906312.md): Fitting · corroded · Sep 6, 2012 · N266SK · Emb EMB145LR · Fuselage Miscellaneous Structure
  > DURING INSPECTION, CORROSION WAS FOUND ON SHEAR CLIP AT FRAME 10 BETWEEN STRINGER 21R AND 20R. THE SHEAR CLIP AT FRAME 10 WAS REPLACED IN ACCORDANCE WITH SRM 53-12-04 AND 51-40-02.
- [SDR CHQA20120906311](https://openairdocs.org/sdr/CHQA20120906311.md): Skin Splice · corroded · Sep 6, 2012 · N266SK · Emb EMB145LR · Fuselage Main, Plate/Skin
  > DURING INSPECTION, CORROSION WAS FOUND IN THE CIRCUMFERENTIAL SKIN SPLICE BETWEEN FRAMES 14 AND 16 AND STRINGERS 21L TO 20R. THE SKIN SPLICE WAS REPAIRED IN ACCORDANCE WITH SRM 53-00-02.
- [SDR CHQA20120904320](https://openairdocs.org/sdr/CHQA20120904320.md): Stringer · corroded · Sep 4, 2012 · N266SK · Emb EMB145LR · Fuselage Main, Longeron/Stringer
  > DURING INSPECTION, CORROSION WAS FOUND ON STRINGER 21R FROM FRAME 8 TO FRAME 13. THE STRINGER 21R AT FRAME 8 TO FRAME 13 WAS REPLACED IN ACCORDANCE WITH SRM 51-20-02.
- [SDR CHQA20120904317](https://openairdocs.org/sdr/CHQA20120904317.md): Web · corroded · Sep 4, 2012 · N266SK · Emb EMB145LR · Fuselage Miscellaneous Structure
  > DURING INSPECTION, CORROSION WAS FOUND ON THE RIGHT WEB ASSEMBLY BETWEEN FRAMES 12 AND 13. THE RIGHT WEB ASSEMBLY BETWEEN FRAMES 12 AND 13 WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02.
- [SDR CHQA20120904319](https://openairdocs.org/sdr/CHQA20120904319.md): Stanchion · corroded · Sep 4, 2012 · N266SK · Emb EMB145LR · Fuselage Miscellaneous Structure
  > DURING INSPECTION, CORROSION WAS FOUND ON THE RIGHT STANCHION AT FRAMES 11 AND 12. THE RIGHT STANCHION BETWEEN FRAMES 11 AND 12 WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02.
- [SDR CHQA20120904318](https://openairdocs.org/sdr/CHQA20120904318.md): Stanchion · corroded · Sep 4, 2012 · N266SK · Emb EMB145LR · Fuselage Miscellaneous Structure
  > DURING INSPECTION, CORROSION WAS FOUND ON THE RIGHT STANCHION AT FRAMES 12 AND 13. THE RIGHT STANCHION BETWEEN FRAMES 12 AND 13 WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02.
- [SDR CHQA20120904316](https://openairdocs.org/sdr/CHQA20120904316.md): Web · corroded · Sep 4, 2012 · N266SK · Emb EMB145LR · Fuselage Miscellaneous Structure
  > DURING INSPECTION, CORROSION WAS FOUND ON THE RIGHT WEB ASSEMBLY BETWEEN FRAMES 11 AND 12. THE RIGHT WEB ASSEMBLY BETWEEN FRAMES 11 AND 12 WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02.
- [SDR CHQA20120828315](https://openairdocs.org/sdr/CHQA20120828315.md): Skin Splice · corroded · Aug 28, 2012 · N266SK · Emb EMB145LR · Fuselage Main, Plate/Skin
  > DURING INSPECTION, CORROSION WAS FOUND ON THE CIRCUMFERENTIAL SKIN SPLICE BETWEEN FRAMES 60 AND 61 AND STRINGERS 20R AND 21R. THE SKIN SPLICE WAS REPAIRED IN ACCORDANCE WITH ETD 2012-145-012305.
- [SDR CHQA20120828313](https://openairdocs.org/sdr/CHQA20120828313.md): Fitting · cracked · Aug 28, 2012 · N266SK · Emb EMB145LR · Fuselage Miscellaneous Structure
  > DURING INSPECTION, THE SHEAR FOOT AT FRAME 68 BETWEEN STRINGERS 6L AND 7L WAS FOUND TO BE CRACKED. THE SHEAR CLIP WAS REPLACED AND INSTALLED IN ACCORDANCE WITH SRM 53-31-04.
- [SDR CHQA20120828310](https://openairdocs.org/sdr/CHQA20120828310.md): Threshold · corroded · Aug 28, 2012 · N266SK · Emb EMB145LR · Fuselage Miscellaneous Structure
  > DURING INSPECTION, CORROSION WAS FOUND AT THE SCREW HOLES ON THE SERVICE DOOR THRESHOLD. MAINTENANCE REPLACED THE SERVICE DOOR SILL IN ACCORDANCE WITH SRM 53-20-10.
- [SDR CHQA20120816314](https://openairdocs.org/sdr/CHQA20120816314.md): Skin · dented · Aug 16, 2012 · N266SK · Emb EMB145LR · Fuselage Main, Plate/Skin
  > DURING HEAVY MAINTENANCE A PREVIOUSLY DAMAGED SECTION OF SKIN AFT OF THE PASSENGER DOOR NEAR FRAME 19-20 AND STRINGER 12L -13L WAS REPAIRED IN ACCORDANCE WITH ETD 2011-145-03683A CLOSING DMI 591816/3 AND 591816/1.
- [SDR CHQA20120609187](https://openairdocs.org/sdr/CHQA20120609187.md): Battery Pack · discharged · Jun 9, 2012 · N266SK · Emb EMB145LR · Emergency Lighting
  > DURING INSPECTION, THE EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE NR 3 EMERGENCY LIGHT BATTERY. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.
- [SDR CHQA20120321085](https://openairdocs.org/sdr/CHQA20120321085.md): Battery · discharged · Mar 21, 2012 · N266SK · Emb EMB145LR · Emergency Lighting
  > DURING INSPECTION, THE LEFT AND RIGHT OVERWING EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE NUMBER 4 EMERGENCY LIGHT BATTERY. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.
- [SDR CHQA201200027](https://openairdocs.org/sdr/CHQA201200027.md): Coupling · defective · Jan 27, 2012 · N266SK · Emb EMB145LR · Pneumatic Distribution System
  > CREW REPORTED DURING CLIMB THEY RECEIVED A BLEED 1 LEAK MESSAGE. AFTER FOLLOWING THE QUICK REFERENCE HANDBOOK THE MESSAGE CLEARED. DUE TO SINGLE BLEED OPERATIONS, CREW DECIDED TO DIVERT. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED A COUPLING
- [SDR CHQA201100410](https://openairdocs.org/sdr/CHQA201100410.md): Connector · disconnected · Oct 22, 2011 · N266SK · Emb EMB145LR · Light System Wiring
  > DURING INSPECTION, THE RIGHT FORWARD WING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE FOUND THE CONNECTOR DISCONNECTED FROM THE LIGHT ASSEMBLY. THE CONNECTOR WAS REATTACHED AND OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.
- [SDR CHQA201100397](https://openairdocs.org/sdr/CHQA201100397.md): Warning System · malfunctioned · Oct 4, 2011 · N266SK · Emb EMB145LR · Drag Control System
  > CREW REPORTED THAT ON DESCENT, RECEIVED A SPOILER FAIL MESSAGE ON THE EICAS. THE CREW FOLLOWED THE QUICK REFERENCE HANDBOOK AND DISCOVERED THAT THEIR LANDING DISTANCE WOULD BE LONGER PER THE QUICK REFERENCE HANDBOOK AND THEY DID NOT HAVE THE CORRECT VAPP AND
- [SDR CHQA201100041](https://openairdocs.org/sdr/CHQA201100041.md): Connector · corroded · Feb 23, 2011 · N266SK · Emb EMB145LR · Engine Control System Wiring
  > CREW REPORTED THAT AFTER TAKEOFF THE THRUST MODE WOULD NOT CHANGE FROM TAKEOFF MODE. THE CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND CORROSION ON CONNECTOR P0885. THE CORROSION WAS CLEANED AND THE CONNECTOR WAS RE-CONNECTED. OPERA
- [SDR CHQA201100030](https://openairdocs.org/sdr/CHQA201100030.md): Shutoff Valve · faulty · Feb 3, 2011 · N266SK · Emb EMB145LR · Pneumatic Distribution System
  > CREW RETURNED TO FIELD DUE TO A BLEED 2 VALVE FAIL MESSAGE ON EICAS. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE E2 PRSOV AND HIGH STAGE PRESSURE SWITCH WITH NO FURTHER DEFECTS NOTED.
- [SDR CHQA201100002](https://openairdocs.org/sdr/CHQA201100002.md): Connector · dirty · Jan 3, 2011 · N266SK · Emb EMB145LR · Communications System Wiring
  > AFTER TAKEOFF THE CREW REPORTED THAT THE COMM 2 RMU WAS BLANKED OUT AND THE BACK-UP HEAD COULD NOT BE TUNED AND THAT COMM 1 WAS SWITCHING BETWEEN ACTIVE AND TUNING FREQUENCIES. THE AIRCRAFT RETURNED TO IAH AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT

Next page: https://openairdocs.org/deregistered/N266SK-2018-05-23/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 = 'N266SK' AND deregistration_id = 'N266SK-2018-05-23'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N266SK-2018-05-23/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.