# Service difficulty reports: N295SK, cancelled Jan 18, 2017

A list on [N295SK, cancelled Jan 18, 2017](https://openairdocs.org/deregistered/N295SK-2017-01-18.md).

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

- [SDR CHQA20140908267](https://openairdocs.org/sdr/CHQA20140908267.md): Trunnion · corroded · Sep 8, 2014 · N295SK · Emb EMB135KL · Main Landing Gear Attach Section
  > DURING INSPECTION CORROSION WAS FOUND ON THE LT MLG FWD UPPER TRUNNION. THE TRUNNION WAS REPAIRED IAW ETD 2014-145-075943A.
- [SDR CHQA20140908266](https://openairdocs.org/sdr/CHQA20140908266.md): Trunnion · corroded · Sep 8, 2014 · N295SK · Emb EMB135KL · Main Landing Gear Attach Section
  > DURING INSPECTION CORROSION WAS FOUND ON THE RT MLG UPPER FWD TRUNNION. THE TRUNNION WAS REPAIRED IAW ETD 2014-145-075943A.
- [SDR CHQA20140827269](https://openairdocs.org/sdr/CHQA20140827269.md): Bracket · chafed · Aug 27, 2014 · N295SK · Emb EMB135KL · Emergency Exits
  > DURING INSPECTION THE LT EMER EXIT DOOR WAS FOUND TO BE CHAFED & BENT ON THE BRACKET ON THE AFT SIDE. THE DOOR WAS REPAIRED IAW ETD 2014-145-073270.
- [SDR CHQA20140827260](https://openairdocs.org/sdr/CHQA20140827260.md): Fitting · damaged · Aug 27, 2014 · N295SK · Emb EMB135KL · Ailerons
  > DURING INSPECTION THE LT AILERON PCA OTBD FITTING WAS FOUND TO HAVE AN ENLARGED HOLE. THE LT AILERON PCA OTBD FITTING WAS REPLACED IAW SRM 51-40-02.
- [SDR CHQA20140826265](https://openairdocs.org/sdr/CHQA20140826265.md): Bearing · corroded · Aug 26, 2014 · N295SK · Emb EMB135KL · Main Landing Gear Attach Section
  > DURING INSPECTION CORROSION WAS FOUND ON THE LT MLG UPPER AFT TRUNNION BEARING. THE TRUNNION BEARING WAS REPAIRED IAW ETD 2014-145-075943A.
- [SDR CHQA20140824271](https://openairdocs.org/sdr/CHQA20140824271.md): Skin · dented · Aug 24, 2014 · N295SK · Emb EMB135KL · Fuselage Main, Plate/Skin
  > DURING INSPECTION A DENT FROM STRIKE DAMAGE BETWEEN FRAME 70 - 72 & STRINGERS 13 - 14R WAS REPAIRED IAW ETD 2014-145-071479.
- [SDR CHQA20140826264](https://openairdocs.org/sdr/CHQA20140826264.md): Bearing · corroded · Aug 24, 2014 · N295SK · Emb EMB135KL · Main Landing Gear Attach Section
  > DURING INSPECTION CORROSION WAS FOUND ON THE RT MLG UPPER AFT TRUNNION BEARING. THE TRUNNION BEARING WAS REPAIRED IAW ETD 2014-145-075943.
- [SDR CHQA20140822263](https://openairdocs.org/sdr/CHQA20140822263.md): Floor Support · corroded · Aug 22, 2014 · N295SK · Emb EMB135KL · Fuselage Miscellaneous Structure
  > DURING INSPECTION THE CTR OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. THE CTR OMEGA BEAM WAS REPLACED IAW SRM 51-40-02.
- [SDR CHQA20140822261](https://openairdocs.org/sdr/CHQA20140822261.md): Repair · corroded · Aug 22, 2014 · N295SK · Emb EMB135KL · Fuselage Miscellaneous Structure
  > DURING INSPECTION A PREVIOUS REPAIR ON THE LT OMEGA BEAM FLOOR FLANGE AT FRAME 20 WAS FOUND TO BE CORRODED. THE FLANGE WAS REPAIRED IAW SRM 53-00-10.
- [SDR CHQA20140820270](https://openairdocs.org/sdr/CHQA20140820270.md): Skin · corroded · Aug 20, 2014 · N295SK · Emb EMB135KL · Fuselage Main, Plate/Skin
  > DURING INSPECTION CORROSION WAS FOUND ON THE SKIN AT FRAME 25 & STRINGERS 20 - 21L. THE SKIN WAS REPAIRED IAW SRM 53-22-01.
- [SDR CHQA20140820268](https://openairdocs.org/sdr/CHQA20140820268.md): Skin · damaged · Aug 20, 2014 · N295SK · Emb EMB135KL · Fuselage Main, Plate/Skin
  > DURING INSPECTION A LIGHTNING STRIKE REPAIR WAS COMPLETED ON NR 1 FRAME 27 - 28 AT STRINGER 21L & FRAME 28 AT STRINGER 18L - 19L. THE REPAIR WAS MADE IAW SRM 53-22-01.
- [SDR CHQA20140820262](https://openairdocs.org/sdr/CHQA20140820262.md): Repair · chafed · Aug 20, 2014 · N295SK · Emb EMB135KL · Fuselage Miscellaneous Structure
  > DURING INSPECTION A PREVIOUS REPAIR WAS FOUND TO BE CHAFED BELOW ACCESS DOOR 113EL. THE PREVIOUS REPAIR DOUBLER WAS REPLACED IAW SRM53-11-01.
- [SDR CHQA20130123042](https://openairdocs.org/sdr/CHQA20130123042.md): Support · corroded · Jan 23, 2013 · N295SK · Emb EMB135KL · Fuselage Miscellaneous Structure
  > DURING INSPECTION, CORROSION WAS FOUND ON SUPPORT WEB FOR AILERON TORQUE TUBE BETWEEN FRAME 13 AND 14 AND STRINGERS 21R AND 20R. THE AILERON TORQUES TUBE SUPPORT WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02.
- [SDR CHQA20130123041](https://openairdocs.org/sdr/CHQA20130123041.md): Fitting · cracked · Jan 23, 2013 · N295SK · Emb EMB135KL · Fuselage Main, Attach Fittings
  > DURING INSPECTION, A CRACK WAS FOUND IN THE SHEAR CLIP AT FRAME 66 BETWEEN STRINGERS 8L AND 9L. THE DAMAGED SHEAR CLIP WAS REPLACED IN ACCORDANCE WITH SRM 53-31-04 AND 51-40-02.
- [SDR CHQA20120309082](https://openairdocs.org/sdr/CHQA20120309082.md): Skin · cracked · Mar 9, 2012 · N295SK · Emb EMB135KL · Elevator, Plate/Skin
  > DURING INSPECTION, THE RIGHT ELEVATOR LEADING EDGE SKIN WAS FOUND TO BE CRACKED AT THE SERVO TAB CONTROL ROD AT STA YH 1310. A HIGH FREQUENCY EDDY CURRENT INSPECTION WAS CARRIED OUT WITH NO CRACK LIKE INDICATIONS FOUND. THE RIGHT ELEVATOR LEADING EDGE SKIN A
- [SDR CHQA20120308081](https://openairdocs.org/sdr/CHQA20120308081.md): Frame · cracked · Mar 8, 2012 · N295SK · Emb EMB135KL · 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 CHQA20120308080](https://openairdocs.org/sdr/CHQA20120308080.md): Frame · cracked · Mar 8, 2012 · N295SK · Emb EMB135KL · 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 CHQA20120308079](https://openairdocs.org/sdr/CHQA20120308079.md): Frame · cracked · Mar 8, 2012 · N295SK · Emb EMB135KL · Fuselage Main, Frame
  > DURING INSPECTION, THE RIGHT FRAME 23, JUST BEHIND THE RIGHT SILL NUMBER 1 WAS FOUND TO BE CRACKED. MAINTENANCE REPAIRED THE RIGHT FRAME 23 JUST BEHIND THE RIGHT SILL NUMBER 1 IN ACCORDANCE WITH ETD 2012-145-003386.
- [SDR CHQA20120308078](https://openairdocs.org/sdr/CHQA20120308078.md): Skin · gouged · Mar 8, 2012 · N295SK · Emb EMB135KL · Fuselage Main, Plate/Skin
  > DURING INSPECTION, FOUR GOUGES WERE FOUND ON THE LEFT SKIN PANEL BETWEEN FRAME 20 AND FRAME 22 BETWEEN STRINGERS 19L AND 17L. THE LEFT SKIN BETWEEN FRAME 20 AND FRAME 22, AND BETWEEN STRINGERS 19L AND 17L WAS REPAIRED IN ACCORDANCE WITH ETD 2012-145-003415.
- [SDR CHQA20120308077](https://openairdocs.org/sdr/CHQA20120308077.md): Skin · dented · Mar 8, 2012 · N295SK · Emb EMB135KL · Fuselage Main, Plate/Skin
  > DURING INSPECTION, MULTIPLE DENTS WERE FOUND ON THE RIGHT SKIN BETWEEN FRAME 3 AND FRAME 4, SIX INCHES ABOVE THE NOSE LANDING GEAR DOOR CUTOUT. A HIGH FREQUENCY EDDY CURRENT INSPECTION WAS PERFORMED WITH NO CRACK INDICATIONS FOUND. THE RIGHT SKIN BETWEEN FRA
- [SDR CHQA201100492](https://openairdocs.org/sdr/CHQA201100492.md): Battery · discharged · Dec 18, 2011 · N295SK · Emb EMB135KL · Emergency Lighting
  > DURING INSPECTION, THE LEFT FORWARD EXTERNAL EMERGENCY LIGHT, CEILING AISLE EMERGENCY LIGHT 1 AND COCKPIT FLOOD LIGHT WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE NUMBER 1 EMERGENCY BATTERY. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTE
- [SDR CHQA201100201](https://openairdocs.org/sdr/CHQA201100201.md): Shear Plate · corroded · May 30, 2011 · N295SK · Emb EMB135KL · Fuselage Miscellaneous Structure
  > DURING INSPECTION, CORROSION WAS FOUND ON THE LOWER FRAMES BAGGAGE DOOR SHEAR CLIP. THE DAMAGED AREA OF THE SHEAR CLIP WAS REMOVED AND A NEW SECTION WAS INSTALLED.
- [SDR CHQA201100200](https://openairdocs.org/sdr/CHQA201100200.md): Floor Support · damaged · May 30, 2011 · N295SK · Emb EMB135KL · Fuselage Miscellaneous Structure
  > DURING INSPECTION THE CENTER FUSELAGE III OMEGA BEAM WAS FOUND TO BE DAMAGED. THE OMEGA BEAM WAS REPAIRED IAW SRM 53-23-02-RE AND EMBRAER ETD 2011-145-100373.
- [SDR CHQA201100215](https://openairdocs.org/sdr/CHQA201100215.md): Floor Support · cracked · May 28, 2011 · N295SK · Emb EMB135KL · Fuselage Miscellaneous Structure
  > DURING INSPECTION A CRACK WAS FOUND ON THE CABIN FLOOR STRUCTURE RIGHT OMEGA BEAM FLANGE AT FRAME 47. THE CRACK WAS REPAIRED IN ACCORDANCE WITH SRM 53-23-02.
- [SDR CHQA201100214](https://openairdocs.org/sdr/CHQA201100214.md): Floor Support · cracked · May 28, 2011 · N295SK · Emb EMB135KL · Fuselage Miscellaneous Structure
  > DURING INSPECTION A CRACK WAS FOUND ON THE CABIN FLOOR STRUCTURE MID OMEGA BEAM FLANGE AT FRAME 47. THE CRACK WAS REPAIRED IN ACCORDANCE WITH SRM 53-23-02.
- [SDR CHQA201100213](https://openairdocs.org/sdr/CHQA201100213.md): Floor Support · cracked · May 28, 2011 · N295SK · Emb EMB135KL · Fuselage Miscellaneous Structure
  > DURING INSPECTION A CRACK WAS FOUND ON THE CABIN FLOOR STRUCTURE LEFT OMEGA BEAM FLANGE AT FRAME 47. THE CRACK WAS REPAIRED IN ACCORDANCE WITH SRM 53-23-02.
- [SDR CHQA201100051](https://openairdocs.org/sdr/CHQA201100051.md): Controller · inoperative · Mar 8, 2011 · N295SK · Emb EMB135KL · Cabin Pressure Controller
  > CREW REPORTED, AFTER TAKEOFF WERE UNABLE TO CONTROL THE CABIN ALTITUDE IN MANUAL MODE WHILE THE AUTO MODE WAS ON DEFERRAL. IT WAS REPORTED THAT THE CABIN ALTITUDE WAS CLIMBING AT APPROXIMATELY THE SAME RATE AS THE AIRCRAFT AT ALL SETTINGS. THE AIRCRAFT RETUR
- [SDR CHQA201100034](https://openairdocs.org/sdr/CHQA201100034.md): Light · inoperative · Feb 8, 2011 · N295SK · Emb EMB135KL · Emergency Lighting
  > DURING INSPECTION, THE LEFT AFT EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE LIGHT BULB IN THE LEFT AFT EMERGENCY EXIT LIGHT WITH NO FURTHER DEFECTS NOTED.
- [SDR CHQA200900212](https://openairdocs.org/sdr/CHQA200900212.md): Light · broken · Sep 30, 2009 · N295SK · Emb EMB135KL · Emergency Lighting
  > WHILE REMOVING FLOOR STRIP FOR REMOVAL OF GASPER FAN, THE FLOOR PROX LIGHT STRIP BROKE. THE LIGHT STRIP AT ROW 14A WAS REPLACED AND CHECKED NORMAL PER EMB AMM 33-50-12.
- [SDR CHQA200900095](https://openairdocs.org/sdr/CHQA200900095.md): Heater · shorted · Mar 31, 2009 · N295SK · Emb EMB135KL · Windshield/Door Rain/Ice Removal
  > FLIGHT 5323, MKE TO STL - DURING DESCENT INTO STL, AT AROUND 11,000 FT SMOKE WAS SMELLED AND SEEN IN THE COCKPIT. THE CREW FOUND THE SOURCE TO BE AT THE BASE OF THE FIRST OFFICER'S WINDSHIELD. THE APPROACH WAS EXPEDITED AND THE APPROPRIATE CHECK LISTS WERE F
- [SDR CHQA200900264](https://openairdocs.org/sdr/CHQA200900264.md): Proximity Switch · dirty · Jan 2, 2009 · N295SK · Emb EMB135KL · Landing Gear Position and Warning
  > IMMEDIATELY AFTER TAKEOFF THE CREW RECEIVED A LG AIR/GND FAIL EICAS MESSAGE. THE LANDING GEAR INDICATED 3 GREEN DOWN AND LOCKED WITH THE LEVER DOWN. THE QRH WAS FOLLOWED AND THE ACFT RETURNED AND LANDED WITHOUT INCIDENT. MX CLEANED AND INSPECTED THE LANDING
- [SDR CHQA200800173](https://openairdocs.org/sdr/CHQA200800173.md): Solenoid · faulty · Sep 1, 2008 · N295SK · Emb EMB135KL · Landing Gear Door Retract Section
  > FLIGHT 5325 ICT TO STL. THE FLIGHT CREW REPORTED A LOUD AIR SOUND FROM THE NLG AREA DURING FLIGHT. THE ACFT LANDED WITHOUT INCIDENT. MX INSPECTED THE ACFT AND FOUND THE NLG DOOR COMMAND CIRCUIT BREAKER TRIPPED. THROUGH FURTHER TROUBLESHOOTING, IT WAS FOUND
- [SDR CHQA200600134](https://openairdocs.org/sdr/CHQA200600134.md): Bulb · inoperative · Oct 16, 2006 · N295SK · Emb EMB135KL · Emergency Lighting
  > EMERGENCY LIGHT OVER WING EXIT INOPERATIVE. TESTED EMERGENCY LIGHT SYSTEM IAW EMB 140 MM 33-50-00. NO DEFECTS NOTED.
- [SDR CHQA200600096](https://openairdocs.org/sdr/CHQA200600096.md): Battery · misinstalled · Jul 31, 2006 · N295SK · Emb EMB135KL · Emergency Lighting
  > PROXIMITY EMERGENCY LIGHT STRIP ON CENTER AISLE FLOOR FRONT HALF NOT WORKING. FOUND BATTERY INSTALLED INCORRECTLY. INSTALLED BATTERY IAW EMB 140 MM 30-50-04. LIGHTS WORK SATISFACTORY.
- [SDR CHQA200600095](https://openairdocs.org/sdr/CHQA200600095.md): Connector · disconnected · Jul 30, 2006 · N295SK · Emb EMB135KL · Light System Wiring
  > LEFT OVERWING EMERGENCY LIGHT DOES NOT COME ON WHEN SWITCHED TO THE ON POSITION. FOUND LIGHT NOT PLUGGED IN. PLUGGED IN LIGHT AND OPS CHECK GOOD IAW EMB 140 MM 33-50-07.
- [SDR CHQA200600094](https://openairdocs.org/sdr/CHQA200600094.md): Battery · inoperative · Jul 27, 2006 · N295SK · Emb EMB135KL · Emergency Lighting
  > AFT HALF OF EMERGENCY LIGHT ON CEILING PANEL BETWEEN PASSENGER CABIN EMERGENCY EXIT INOPERATIVE. REMOVED AND REPLACED NR 3 EMERGENCY LIGHT BATTERY IAW EMB 140 MM 33-50-04. OPS CHECK GOOD.
- [SDR CHQA200500136](https://openairdocs.org/sdr/CHQA200500136.md): Bulb · burned out · Aug 4, 2005 · N295SK · Emb EMB135KL · Emergency Lighting
  > LEFT AFT EXTERIOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED BULB IAW EMB 140 MM 33-50-10. OPS CHECK GOOD.
- [SDR CHQA200500076](https://openairdocs.org/sdr/CHQA200500076.md): Warning System · false indication · Apr 7, 2005 · N295SK · Emb EMB135KL · Gust Lock Damper System
  > WHILE CRUISING AT FL350 BOTH AMBER GUST LOCK WARNING LIGHTS ILLUMINATED. THE QRH PROCEDURES WERE RUN, WHICH AT THE END STATED TO LAND AT THE NEAREST SUITABLE AIRPORT. DISPATCH AND MAINTENANCE CONTROL WERE CONTACTED ABOUT THE PROBLEM AND ADVISED THEM ABOUT TH
- [SDR CHQA200500064](https://openairdocs.org/sdr/CHQA200500064.md): Bulb · burned out · Mar 27, 2005 · N295SK · Emb EMB135KL · Emergency Lighting
  > LEFT HAND AFT OVERWING EMERGENCY EXIT LIGHT IS INOP. RELAMPED LEFT HAND AFT OVERWING EMERGENCY EXIT LIGHT. OPS CHECK GOOD IAW EMB 140 AMM 33-50-09.
- [SDR CHQA000565](https://openairdocs.org/sdr/CHQA000565.md): Battery · inoperative · Oct 7, 2004 · N295SK · Emb EMB135KL · Emergency Lighting
  > EMERGENCY EXIT LIGHTS ARE INOP. REMOVED AND REPLACED EMERGENCY BATTERY IAW EMB 140 AMM 33-50-09. OPS CHECK GOOD.
- [SDR CHQA200500010](https://openairdocs.org/sdr/CHQA200500010.md): Battery Pack · discharged · Jan 21, 2004 · N295SK · Emb EMB135KL · Emergency Lighting
  > LEFT HAND OVERWING FORWARD EMERGENCY LIGHT IS INOP. AISLE EGRESS LIGHT AND CABIN FLOOD LIGHTS ARE INOP. REMOVED AND REPLACED EMERGENCY EGRESS BATTERY PACK PER EMB 140 MM 33-50-04-5. OPS CHECK GOOD.

## 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 = 'N295SK' AND deregistration_id = 'N295SK-2017-01-18'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N295SK-2017-01-18/reports

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