# Service difficulty reports: N290SK, cancelled Nov 21, 2018

A list on [N290SK, cancelled Nov 21, 2018](https://openairdocs.org/deregistered/N290SK-2018-11-21.md).

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

- [SDR UHLA201602120059](https://openairdocs.org/sdr/UHLA201602120059.md): Hand Rail · malfunctioned · Feb 12, 2016 · N290SK · Emb EMB145LR · Passenger/Crew Doors
  > PAX DOOR HANDRAILS DON'T STOW WITH DOOR CLOSED. CLEANED HANDRAIL ASSY, REPLACED ASSIST SPRINGS, OPS CHECKED GOOD.
- [SDR UHLA2015011400013](https://openairdocs.org/sdr/UHLA2015011400013.md): Cabin Pressure · malfunctioned · Jan 14, 2015 · N290SK · Emb EMB145LR · Cabin Pressure Control System
  > THE CREW REPORTED THAT THE CABIN ALTITUDE INDICATION WAS LOST ON CLIMB OUT WHILE THE AUTO PRESSURIZATION SYSTEM WAS DEFERRED. THE AIRCRAFT RETURNED TO FIELD AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE VERIFIED THE ELECTROPNUEMATIC VALVE WAS PROPERLY DEACT
- [SDR CHQA20141119337](https://openairdocs.org/sdr/CHQA20141119337.md): Elevator · cracked · Nov 19, 2014 · N290SK · Emb EMB145LR · Elevator Structure
  > DURING INSPECTION, THE LT ELEVATOR WAS FOUND TO BE CRACKED. THE ELEVATOR WAS REPAIRED IAW ETD 2014-145-097861.
- [SDR CHQA20141119334](https://openairdocs.org/sdr/CHQA20141119334.md): Structure · dented · Nov 19, 2014 · N290SK · Emb EMB145LR · Fuselage Miscellaneous Structure
  > DURING INSPECTION, A DENT WAS FOUND BETWEEN FRAME 19 & 20 & STRINGERS 19R & 20R. THE DENT WAS REPAIRED IAW SRM 53-21-01.
- [SDR CHQA20141115335](https://openairdocs.org/sdr/CHQA20141115335.md): Angle · corroded · Nov 15, 2014 · N290SK · Emb EMB145LR · Wing Miscellaneous Structure
  > DURING INSPECTION, CORROSION WAS FOUND ON THE ANGLE BRACKET IN THE RT WHEEL AREA AFT SIDE. THE PROFILE WAS REPLACED IAW SRM 51-40-02.
- [SDR CHQA20141114341](https://openairdocs.org/sdr/CHQA20141114341.md): Floor Support · corroded · Nov 14, 2014 · N290SK · Emb EMB145LR · Fuselage Miscellaneous Structure
  > DURING INSPECTION, THE RT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 59 & 61. THE BEAM WAS REPAIRED IAW ETD 2014-145-096615.
- [SDR CHQA20141114339](https://openairdocs.org/sdr/CHQA20141114339.md): Skin · cracked · Nov 14, 2014 · N290SK · Emb EMB145LR · Fuselage Main, Plate/Skin
  > DURING INSPECTION, THE FUSELAGE SKIN WAS FOUND TO BE CRACKED AT FRAME 75 BELOW STRINGER 2L. THE STRINGER WAS REPAIRED IAW ETD 2014-145-096626.
- [SDR CHQA20141114338](https://openairdocs.org/sdr/CHQA20141114338.md): Skin · cracked · Nov 14, 2014 · N290SK · Emb EMB145LR · Fuselage Main, Plate/Skin
  > DURING INSPECTION, THE FUSELAGE SKIN WAS FOUND TO BE CRACKED AT FRAME 75 ABOVE STRINGER 2L. THE STRINGER WAS REPLACED IAW SRM 51-40-02.
- [SDR CHQA20141114332](https://openairdocs.org/sdr/CHQA20141114332.md): Floor Support · corroded · Nov 14, 2014 · N290SK · Emb EMB145LR · Fuselage Miscellaneous Structure
  > DURING INSPECTION, THE CTR OMEGA BEAM WAS FOUND TO BE CORRODED ON A PREVIOUS REPAIR AT FRAMES 20 & 22. THE CTR OMEGA BEAM WAS REPLACED IAW SRM 51-40-02.
- [SDR CHQA20141113340](https://openairdocs.org/sdr/CHQA20141113340.md): Floor Support · corroded · Nov 13, 2014 · N290SK · Emb EMB145LR · Fuselage Miscellaneous Structure
  > DURING INSPECTION, THE RT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 53. THE BEAM WAS REPAIRED IAW SRM 51-40-02.
- [SDR CHQA20141113336](https://openairdocs.org/sdr/CHQA20141113336.md): Floorbeam · corroded · Nov 13, 2014 · N290SK · Emb EMB145LR · Fuselage Main, Floor Beam
  > DURING INSPECTION, THE LT FLOORBEAM WAS FOUND TO BE CORRODED ON A PREVIOUS REPAIR AT FRAME 20. THE BEAM WAS REPAIRED IAW SRM 53-00-10.
- [SDR CHQA20141113333](https://openairdocs.org/sdr/CHQA20141113333.md): Door Sill · corroded · Nov 13, 2014 · N290SK · Emb EMB145LR · Fuselage Miscellaneous Structure
  > DURING INSPECTION, THE SERVICE DOOR SILL WAS FOUND TO BE CORRODED. THE SILL WAS REPLACED IAW SRM 51-40-02.
- [SDR CHQA20140909248](https://openairdocs.org/sdr/CHQA20140909248.md): Switch · inoperative · Sep 9, 2014 · N290SK · Emb EMB145LR · Emergency Lighting
  > DURING INSPECTION THE FLIGHT ATTENDANT EMER LIGHT SWITCH WAS FOUND TO BE INOPERATIVE. REPLACED THE FLIGHT ATTENDANT CONTROL PANEL. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.
- [SDR CHQA20140601178](https://openairdocs.org/sdr/CHQA20140601178.md): Battery · discharged · Jun 1, 2014 · N290SK · Emb EMB145LR · Emergency Lighting
  > DURING INSPECTION, THE NR 4 EMER LIGHT BATTERY WAS REPORTED TO BE INOPERATIVE. MX REPLACED THE NR 4 EMER LIGHT BATTERY. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.
- [SDR CHQA20140601177](https://openairdocs.org/sdr/CHQA20140601177.md): Light · damaged · Jun 1, 2014 · N290SK · Emb EMB145LR · Emergency Lighting
  > DURING INSPECTION, THE RT AFT OVERWING EMERGENCY LIGHT WAS FOUND TO BE DAMAGED. MX REPLACED THE RT OVERWING EMERGENCY LIGHT HOUSING ASSEMBLY. OPS CHECKED GOOD WITH NO FURTHER DEFECTS NOTED.
- [SDR CHQA20140106003](https://openairdocs.org/sdr/CHQA20140106003.md): Light · inoperative · Jan 6, 2014 · N290SK · Emb EMB145LR · Emergency Lighting
  > DURING INSPECTION, THE LT OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. REPLACED THE BULB & ALL OPERATIONS CHECKED GOOD.
- [SDR CHQA20140105002](https://openairdocs.org/sdr/CHQA20140105002.md): Anti-Ice Valve · faulty · Jan 5, 2014 · N290SK · Emb EMB145LR · Airfoil Anti/De-ice System
  > CREW REPORTED THAT DURING CRUISE FLIGHT, IN ICING CONDITIONS, THEY RECEIVED A WING ANTI-ICE FAIL MESSAGE. THE CREW DIVERTED & LANDED WITHOUT FURTHER INCIDENT. REPLACED THE LT WING ANTI-ICE VLV. OPERATIONS CHECKED GOOD WITH NO FURTHER DEFECTS NOTED.
- [SDR CHQA20131123428](https://openairdocs.org/sdr/CHQA20131123428.md): Battery · discharged · Nov 23, 2013 · N290SK · Emb EMB145LR · Emergency Lighting
  > MULTIPLE EMERGENCY FLOOR STRIP LIGHTS WERE FOUND TO BE INOPERATIVE. REPLACED THE NUMBER TWO EMERGENCY BATTERY & ALL OPERATIONS CHECKED GOOD.
- [SDR CHQA20131002365](https://openairdocs.org/sdr/CHQA20131002365.md): Frame · damaged · Oct 2, 2013 · N290SK · Emb EMB145LR · Fuselage Main, Frame
  > DURING INSPECTION, A DAMAGED HOLE IN FRAME 26 BETWEEN STRINGERS 15R AND 16R WAS FOUND. THE DAMAGE WAS REPAIRED IAW ETD 2013-145-045443.
- [SDR CHQA20131001366](https://openairdocs.org/sdr/CHQA20131001366.md): Shear Tie · cracked · Oct 1, 2013 · N290SK · Emb EMB145LR · Fuselage Internal Mounting Structure
  > DURING INSPECTION, A CRACK WAS FOUND ON THE SHEAR TIE AT FRAME 26 BETWEEN STRINGERS 15 AND 16R. THE SHEAR TIE WAS REPLACED IAW ETD 2013-145-04543.
- [SDR CHQA20131001364](https://openairdocs.org/sdr/CHQA20131001364.md): Floor Support · corroded · Oct 1, 2013 · N290SK · Emb EMB145LR · Fuselage Miscellaneous Structure
  > DURING INSPECTION, CORROSION WAS FOUND ON THE REPAIR DOUBLER AT THE LT OMEGA FRAME 20. THE REPAIR DOUBLER WAS REPLACED IAW SRM 53-00-10.
- [SDR CHQA20131001363](https://openairdocs.org/sdr/CHQA20131001363.md): Frame · bent · Oct 1, 2013 · N290SK · Emb EMB145LR · Fuselage Main, Frame
  > DURING INSPECTION, FRAME 72 WAS FOUND TO BE BENT BETWEEN STRINGERS 15L AND 16L. THE FRAME WAS REPAIRED IAW ETD 2013-145-045154, REV B.
- [SDR CHQA20130226064](https://openairdocs.org/sdr/CHQA20130226064.md): Control Unit · faulty · Feb 26, 2013 · N290SK · Emb EMB145LR · Landing Gear Brake System
  > CREW REPORTED THAT ON LANDING, WITH THE BRAKES FULLY DEPRESSED, THE BRAKING WAS POOR BELOW 80 KNOTS. THE AIRCRAFT TAXIED TO THE GATE WITHOUT INCIDENT. MAINTENANCE REPLACED THE BRAKE CONTROL UNIT. OPERATIONAL AND TAXI CHECKS WERE GOOD WITH NO FURTHER DEFECTS
- [SDR CHQA20121215476](https://openairdocs.org/sdr/CHQA20121215476.md): Light · inoperative · Dec 15, 2012 · N290SK · Emb EMB145LR · Emergency Lighting
  > DURING INSPECTION, THE FLOOR PROXIMITY STRIP WAS FOUND TO BE INOPERATIVE. THE FLOOR PROXIMITY LIGHT STRIP WAS REPLACED. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.
- [SDR CHQA20120703223](https://openairdocs.org/sdr/CHQA20120703223.md): Skin · damaged · Jul 3, 2012 · N290SK · Emb EMB145LR · Fuselage Main, Plate/Skin
  > DURING INSPECTION, THREE CREASES WERE FOUND ON CENTER FUSELAGE, BETWEEN FRAME 19 AND FRAME 20 AND STRINGERS 1L AND 2L. THE CREASES ON CENTER FUSELAGE, BETWEEN FRAME 19 AND FRAME 20 AND STRINGERS 1L AND 2L WERE REPAIRED IN ACCORDANCE WITH ETD 2012-145-010111 RE
- [SDR CHQA20120703222](https://openairdocs.org/sdr/CHQA20120703222.md): Skin · damaged · Jul 3, 2012 · N290SK · Emb EMB145LR · Fuselage Main, Plate/Skin
  > DURING INSPECTION, THE RIGHT AFT FUSELAGE SKIN WAS FOUND TO BE DAMAGED AT FRAME 80 AND STRINGER 9L. THE RIGHT AFT FUSELAGE SKIN AT FRAME 80 AND STRINGER 9L WAS REPAIRED IN ACCORDANCE WITH ETD 2012-145-009769.
- [SDR CHQA201100299](https://openairdocs.org/sdr/CHQA201100299.md): Frame · corroded · Jul 25, 2011 · N290SK · Emb EMB145LR · Fuselage Main, Frame
  > DURING INSPECTION, CORROSION WAS FOUND ON THE LEFT CHANNEL FRAME AT FRAME 65 BETWEEN STRINGER 17L AND 18L. MAINTENANCE REPAIRED THE LEFT CHANNEL FRAME AT FRAME 65 BETWEEN STRINGERS 17L AND 18L IN ACCORDANCE WITH ETD 2011-145-102599 REVISION A.
- [SDR CHQA201100300](https://openairdocs.org/sdr/CHQA201100300.md): Frame · cracked · Jul 25, 2011 · N290SK · Emb EMB145LR · Fuselage Main, Frame
  > DURING INSPECTION, A CRACK WAS FOUND ON THE CHANNEL OF THE CARGO FRAME AT FRAME 66 BETWEEN STRINGER 17L AND 18L. MAINTENANCE REPAIRED THE CHANNEL CARGO FRAME AT FRAME 66 BETWEEN STRINGER 17L AND 18L IN ACCORDANCE WITH ETD 2011-145-102616.
- [SDR CHQA201100306](https://openairdocs.org/sdr/CHQA201100306.md): Beam · corroded · Jul 25, 2011 · N290SK · Emb EMB145LR · Fuselage Miscellaneous Structure
  > DURING INSPECTION, CORROSION WAS FOUND ON THE CARGO DOOR CUTOUT LOWER BEAM. MAINTENANCE REPLACED THE CARGO DOOR LOWER CUTOUT BEAM IN ACCORDANCE WITH SRM 51-40-02.
- [SDR CHQA201100305](https://openairdocs.org/sdr/CHQA201100305.md): Angle · corroded · Jul 25, 2011 · N290SK · Emb EMB145LR · Fuselage Miscellaneous Structure
  > DURING INSPECTION, THE CARGO DOOR CUT-OUT FORWARD LATERAL L-SHAPE WAS FOUND TO BE CORRODED. MAINTENANCE REPAIRED THE CARGO DOOR CUTOUT FORWARD LATERAL L-SHAPE IN ACCORDANCE WITH ETD2011-145-102611 REVISION A.
- [SDR CHQA201000209](https://openairdocs.org/sdr/CHQA201000209.md): Controller · inoperative · Nov 11, 2010 · N290SK · Emb EMB145LR · Cabin Pressure Control System
  > DURING CLIMB, CREW REPORTED CABIN ALTITUDE CLIMBING ABNORMALLY IN AUTO MODE. CREW DECLARED AN EMERGENCY & DESCENDED TO FL100, DIVERTED & LANDED WITHOUT INCIDENT. CREW DID NOT ATTEMPT USING MANUAL MODE, & OXYGEN MASKS WERE NOT DEPLOYED. MX CONFIRMED MANUAL M
- [SDR CHQA201000194](https://openairdocs.org/sdr/CHQA201000194.md): Connector · corroded · Oct 6, 2010 · N290SK · Emb EMB145LR · Ice/Rain Protection System Wiring
  > DURING CLIMB THE CREW REPORTED AN E1 ANTI-ICE FAIL MESSAGE AND THE E1 ANTI-ICE CIRCUIT BREAKER HAD TRIPPED. THE FLIGHT DIVERTED TO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE DEFERRED THE E1 ANTI-ICE VALVE AND RELEASED THE AIRCRAFT FOR SERVICE. MAINTENANCE
- [SDR CHQA201000190](https://openairdocs.org/sdr/CHQA201000190.md): Flap · malfunctioned · Oct 3, 2010 · N290SK · Emb EMB145LR · Trailing Edge Flap Control System
  > ON DESCENT INTO MKE, WHEN THE CREW EXTENDED FLAPS, THE RECEIVED A FLAP FAIL MSG WITH THE FLAPS STUCK AT ZERO DEGREES. THE FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED FIM TASK 27-51-00-810-804-A AND IT WAS FOUND TO BE A TRANSITORY CONDITION OF THE F
- [SDR CHQA200600097](https://openairdocs.org/sdr/CHQA200600097.md): Bulb · burned out · Aug 13, 2006 · N290SK · Emb EMB145LR · Emergency Lighting
  > EMERGENCY LIGHT NR 5 FLOOR STRIP AND LT WING FWD LIGHT INOPERATIVE. REMOVED AND REPLACED NR 5 FLOOR STRIP AND LT WING FWD BULB IAW MM 33-26-07. OPS CHECK GOOD.
- [SDR CHQA200600036](https://openairdocs.org/sdr/CHQA200600036.md): Engine · damaged · Mar 10, 2006 · N290SK · Emb EMB145LR · Engine (Turbine/Turboprop)
  > FLIGHT 7796 - ORD-BUF - SHORTLY AFTER SELECTING CLIMB THRUST, NR 2 ENGINE INDICATED AN ABNORMALLY HIGH ITT AND THE FUEL FLOW WAS SIGNIFICANTLY HIGHER THAN ENGINE NR 1. IMMEDIATELY REDUCED THRUST ON NR 2 ENGINE UNTIL ITT WAS BACK IN GREEN. DECIDED THE ENGINE
- [SDR CHQA200600006](https://openairdocs.org/sdr/CHQA200600006.md): Bulb · burned out · Jan 10, 2006 · N290SK · Emb EMB145LR · Emergency Lighting
  > LEFT OVERWING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED LEFT OVERWING EMERGENCY LIGHT BULB IAW EMB 145 MM 33-50-09. OPS CHECK GOOD.
- [SDR CHQA000570](https://openairdocs.org/sdr/CHQA000570.md): Bulb · burned out · Oct 19, 2004 · N290SK · Emb EMB145LR · Emergency Lighting
  > LT SIDE ADT EMERGENCY EXIT LIGHT IS INOPERATIVE. REMOVED AND REPLACED LT AFT EMERGENCY EXIT LIGHT BULB IAW EMB 145 AMM 33-50-10. OPS CHECK GOOD.
- [SDR CHQ00046](https://openairdocs.org/sdr/CHQ00046.md): Smoke Detector · activated · Nov 27, 2001 · N290SK · Emb EMB145 · Smoke Detection
  > LAV SMOKE DETECTOR WENT OFF WHEN DOING A/I TEST, THEN ON CLIMBOUT.

## 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 = 'N290SK' AND deregistration_id = 'N290SK-2018-11-21'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N290SK-2018-11-21/reports

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