# Service difficulty reports: N8930E

A list on [N8930E](https://openairdocs.org/aircraft/N8930E.md).

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

- [SDR REXA2017090300959](https://openairdocs.org/sdr/REXA2017090300959.md): Battery Pack · inoperative · Sep 3, 2017 · N8930E · Cndair CL6002B19 · Emergency Lighting
  > OVERWING EMERGENCY EXIT SIGN WILL NOT ILLUMINATE. REMOVED AND REPLACED THE BATTERY PACKS 2 AND 3 IAW AMM 33-51-04. OPS CHECKED GOOD.
- [SDR REXA2017072800820](https://openairdocs.org/sdr/REXA2017072800820.md): Oxygen Mask · inoperative · Jul 28, 2017 · N8930E · Cndair CL6002B19 · Crew Oxygen System
  > FO OXYGEN MASK HARNESS IS NOT INFLATING. R&R FO'S O2 MASK IAW AMM 35-11-12,OP & LEAK CK GOOD.
- [SDR REXA2017061100700](https://openairdocs.org/sdr/REXA2017061100700.md): A/C Pack · malfunctioned · Jun 11, 2017 · N8930E · Cndair CL6002B19 · Cabin Cooling System
  > AT FL250, RT PACK BLOWING EXTREMELY HOT AIR THEN RT PACK HIGH TEMP CAUTION MESSAGE. RAN QRH, WENT AWAY ONCE BUT CAME BACK, SHUT THE PACK DOWN. CABIN PRESSURE STARTED TO RISE. STARTED DESCENT AND DIVERTED. PERFORMED OPS CHECK OF THE RT PACK IAW AMM 21-51-0
- [SDR REXA2017051800609](https://openairdocs.org/sdr/REXA2017051800609.md): Oxygen Mask · no test · May 18, 2017 · N8930E · Cndair CL6002B19 · Crew Oxygen System
  > OBSERVER'S OXYGEN MASK FLOWS CONTINUOUSLY DURING MASK TEST AT PREFLIGHT. INSTALLED A SERVICEABLE UNIT IAW AMM 35-11-12.
- [SDR REXA2017051600607](https://openairdocs.org/sdr/REXA2017051600607.md): Safety Wire · broken · May 16, 2017 · N8930E · Cndair CL6002B19 · Fire Bottle, Portable
  > FIRE EXTINGUISHER BOTTLE SAFETY WIRE BROKEN. WATER FIRE EXTINGUISHER BOTTLE REMOVED AND REPLACED IAW AMM 26-23-01.
- [SDR REXA2017042600550](https://openairdocs.org/sdr/REXA2017042600550.md): Connector · not seated · Apr 26, 2017 · N8930E · Cndair CL6002B19 · Landing Gear System Wiring
  > ON DEPARTURE, RECIEIVED A GEAR DISAGREE WARNING MESSAGE FOR THE NOSE GEAR. RAN QRH PROCUDURE RECEIVED 3 GEAR DOWN INDICATION. FOUND THE CONNECTOR ON NLG DOOR SELECTOR VALVE UNSEATED, SECURED AND PERFORMED MULTIPLE EXTENSION AND RETRACTIONS OF NOSE LANDING
- [SDR REXA2017030400315](https://openairdocs.org/sdr/REXA2017030400315.md): Battery Pack · inoperative · Mar 4, 2017 · N8930E · Cndair CL6002B19 · Emergency Locator Beacon
  > DURING OPS TEST OF THE ELT, FOUND THE BATTERY PACK FAILED. REMOVED AND REPLACED THE BATTERY PACK IAW AMM 25-62-09. OPS TESTED GOOD.
- [SDR REXA2016062001108](https://openairdocs.org/sdr/REXA2016062001108.md): Charger · defective · Jun 20, 2016 · N8930E · Cndair CL6002B19 · Emergency Lighting
  > LIGHTS ASSOCIATED WITH EMERGENCY BATTERY PACK NR 3 CAME ON, THEN IMMEDIATELY BEGIN TO EXTINGUISH WHEN SELECTED ON REPLACED EMERGENCY BATTERY, PN OFF AD-2013-1A, SN OFF 89255, PN ON 2013-1A, SN ON 103889 IAW AMM 33-51-04. NO FIX. REPLACED CHARGER ASSY, PN OFF
- [SDR REXA2016031000383](https://openairdocs.org/sdr/REXA2016031000383.md): Wire Harness · damaged · Mar 10, 2016 · N8930E · Cndair CL6002B19 · Landing Gear System Wiring
  > AFTER TAKEOFF, LG LEVER WAS SELECTED UP & A MASTER WARNING OCCURRED ALONG WITH A NOSE DOOR MSG & GEAR DISAGREE MSG. BOTH MAINS CAME UP BUT THE NOSE WHEEL DID NOT RETRACT. QRH PROCEDURES WERE ACCOMPLISHED & 3 GREEN INDICATION OCCURRED. AIR RETURN WITH SAFE
- [SDR REXA2015120801192](https://openairdocs.org/sdr/REXA2015120801192.md): Wire · damaged · Dec 8, 2015 · N8930E · Cndair CL6002B19 · Oxygen System Wiring
  > DURING O2 DROP, RT SIDE PSU OXYGEN DOORS FAILED TO OPEN. REPAIRED WIRES AT FWD RT OVERHEAD BIN IAW AMM 20-11-00 PGS 14 & 15. STEP OPERATIONAL TESTED OK IAW AMM 35-20-00.
- [SDR REXA2015120801191](https://openairdocs.org/sdr/REXA2015120801191.md): Fitting · cracked · Dec 8, 2015 · N8930E · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CLIP AT STRINGER L16 & AFT SIDE OF THE 621 BULKHEAD IS CRACKED. R & R CLIP IAW REO 601R-53-61-5265.
- [SDR REXA2015120801190](https://openairdocs.org/sdr/REXA2015120801190.md): Fitting · cracked · Dec 8, 2015 · N8930E · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CLIP AT STRINGER L14 & AFT SIDE OF THE 621 BULKHEAD IS CRACKED. R & R CLIP IAW SRM 51-42-21.
- [SDR REXA2015120801189](https://openairdocs.org/sdr/REXA2015120801189.md): Fitting · cracked · Dec 8, 2015 · N8930E · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CLIP AT STRINGER R13 & AFT SIDE OF THE 621 BULKHEAD IS CRACKED. REMOVED & REPLACED CLIP PN 601-35012-41, TAG B66968 IAW SRM 51-42-06 & 51-42-21. "
- [SDR REXA2015120801188](https://openairdocs.org/sdr/REXA2015120801188.md): Fitting · cracked · Dec 8, 2015 · N8930E · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CLIP AT STRINGER R14 & AFT SIDE OF THE 621 BULKHEAD IS CRACKED. R & R CLIP PN 601-35012-43, TAG B66967 IAW SRM 51-42-06 & 51-42-21.
- [SDR REXA2015120801187](https://openairdocs.org/sdr/REXA2015120801187.md): Fitting · cracked · Dec 8, 2015 · N8930E · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CLIP AT STRINGER R15 & AFT SIDE OF THE 621 BULKHEAD IS CRACKED. R & R CLIP PN 601-35012-45 TAG B66959 IAW SRM 51-42-06 & 51-42-21.
- [SDR REXA2015120801176](https://openairdocs.org/sdr/REXA2015120801176.md): Fitting · cracked · Dec 8, 2015 · N8930E · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CLIP AT STRINGER L13 & AFT SIDE OF THE 621 BULKHEAD IS CRACKED. R & R CLIP IAW SRM 51-42-21 & 51-42-50.
- [SDR REXA2015081600805](https://openairdocs.org/sdr/REXA2015081600805.md): Cable · defective · Aug 16, 2015 · N8930E · Cndair CL6002B19 · Light System Wiring
  > FLOOR TRACK EMER LIGHTS 2 - 5 INOPERATIVE. R & R FLOOR TRACK E LIGHT CABLE IAW AMM 33-51-01 & ESPM 20-17-10. OPERATIONS CHECKED GOOD AT THIS TIME.
- [SDR REXA2015050700468](https://openairdocs.org/sdr/REXA2015050700468.md): Light · disconnected · May 7, 2015 · N8930E · Cndair CL6002B19 · Emergency Lighting
  > AFT CABIN FLOOR LIGHTED EMER LIGHT INOPERATIVE. RECONNECTED AFT CABIN FLOOR LIGHTED EMER LIGHT. OPERATIONS CHECKED GOOD IAW AMM 33-51-01-04.
- [SDR REXA2014070800497](https://openairdocs.org/sdr/REXA2014070800497.md): Skin · gouged · Jul 3, 2014 · N8930E · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > GOUGE IN THE FUSELAGE SKIN BETWEEN FS 559+112 & FS 574, STRINGER 13R - 15R. REPAIRED IAW EA CRJ253-02723.
- [SDR REXA2014040600356](https://openairdocs.org/sdr/REXA2014040600356.md): Actuator · out of adjust · Apr 6, 2014 · N8930E · Cndair CL6002B19 · Passenger Compartment Equipment
  > SEAT 7D WILL NOT STAY IN THE UPRIGHT POSITION & BLOCKS EMERGENCY EXIT. ADJUSTED ACTUATOR AT SEAT 7D IAW AMM 25-20-00, ACFT OK FOR SERVICE.
- [SDR REXA2013111902263](https://openairdocs.org/sdr/REXA2013111902263.md): Life Vest · unserviceable · Nov 19, 2013 · N8930E · Cndair CL6002B19 · Life Jacket
  > FIRST OFFICER`S LIFE VEST HAS HOLE IN PACKAGE. R & R FIRST OFFICER`S LIFE VEST IAW AMM 25-61-03.
- [SDR REXA2013102301789](https://openairdocs.org/sdr/REXA2013102301789.md): Cover · cracked · Oct 23, 2013 · N8930E · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY LIGHT STRIP COVER IS CRACKED IN SEVERAL PLACES. R & R EMERGENCY LIGHT STRIP COVER WITH SERVICEABLE PART IAW AMM 33-51-01-400-808.
- [SDR REXA2013102101166](https://openairdocs.org/sdr/REXA2013102101166.md): Bulkhead Web · dented · Oct 19, 2013 · N8930E · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > AFT PRESSURE BULKHEAD HAS 8 SCREW INDENTATIONS ON FORWARD SIDE OF BULKHEAD. REPAIRED IAW REOS 601R-53-61-2155 AND 601R-53-61-1285.
- [SDR REXA2013102101165](https://openairdocs.org/sdr/REXA2013102101165.md): Bulkhead · cracked · Oct 19, 2013 · N8930E · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > AFT PRESSURE BULKHEAD CRACKED AROUND LINTEL FITTING. REPAIRED IAW REO 601R-53-61-1230.
- [SDR REXA2013072901393](https://openairdocs.org/sdr/REXA2013072901393.md): Container · torn · Jul 29, 2013 · N8930E · Cndair CL6002B19 · Life Jacket
  > F/A AND OBSERVERS LIFE VEST BAGS TORN. R & R F/A AND OBSERVERS LIFE VEST IAW AMM 25-61-03.
- [SDR REXA2013040100710](https://openairdocs.org/sdr/REXA2013040100710.md): Flashlight · inoperative · Apr 1, 2013 · N8930E · Cndair CL6002B19 · Emergency Equipment
  > FLIGHT ATTENDANT FLASHLIGHT INOPERABLE. REPLACED FLASHLIGHT BATTERY. OPERATIONS CHECK GOOD.
- [SDR REXA2013022100363](https://openairdocs.org/sdr/REXA2013022100363.md): Engine · malfunctioned · Feb 21, 2013 · N8930E · Cndair CL6002B19 · Engine (Turbine/Turboprop)
  > FLIGHT 3723, CREW REPORTED VIBRATION 2 CAUTION ON NR 1 ENGINE AND SHUT DOWN ENGINE DURING FLIGHT. DECLARED EMERGENCY AND LANDED SAFELY. REPLACED LT ENGINE ASSY AND AFT THRUST SHAFT IAW AMM 71-00-00-40-801. OPS AND LEAK CHECKED GOOD. ALL REQUIRED BRAKE IN RU
- [SDR REXA2012120201536](https://openairdocs.org/sdr/REXA2012120201536.md): Bulkhead · cracked · Nov 29, 2012 · N8930E · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > SEMI-PRESSURE BULKHEAD AT FS 559 FOUND CRACKED. REPAIRED IAW PA53-025 AND BOMBARDIER REO 601R-53-41-260 AND 601R-53-41-609.
- [SDR REXA2012082301288](https://openairdocs.org/sdr/REXA2012082301288.md): Container · damaged · Aug 23, 2012 · N8930E · Cndair CL6002B19 · Life Jacket
  > FIRST OFFICER’S LIFE BEST HAS SEVERAL HOLES IN BAG. REMOVED AND REPLACED FIRST OFFICER’S LIFE VEST IAW AMM 25-61-03.
- [SDR REXA2012082301287](https://openairdocs.org/sdr/REXA2012082301287.md): Lamp · inoperative · Aug 23, 2012 · N8930E · Cndair CL6002B19 · Emergency Lighting
  > FLT 4252, NR 3 CABIN EMERGENCY CEILING FLOOD LIGHT INOPERATIVE. REPLACED LAMP. OPS CHECKED GOOD IAW AMM 33-20-01. D
- [SDR REXA2012061000829](https://openairdocs.org/sdr/REXA2012061000829.md): Light · inoperative · Jun 10, 2012 · N8930E · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY EXIT CEILING FLOODLIGHT INOPERATIVE AT SEAT 10B. REMOVED AND REPLACED EMERGENCY FLOODLIGHT IAW AMM 33-51-16. OPS CHECKED GOOD. AIRCRAFT OK FOR SERVICE.
- [SDR REXA2012061000828](https://openairdocs.org/sdr/REXA2012061000828.md): Light · inoperative · Jun 10, 2012 · N8930E · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY EXIT CEILING FLOODLIGHT INOPERATIVE AT SEAT 4B. REMOVED AND REPLACED EMERGENCY FLOOD LIGHT IAW AMM 33-51-16. OPS CHECKED GOOD. AIRCRAFT OK FOR SERVICE.
- [SDR REXA2012041900536](https://openairdocs.org/sdr/REXA2012041900536.md): Ecu · malfunctioned · Apr 19, 2012 · N8930E · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAPS FAIL CAUTION, FLAPS AT 45. PERFORMED TROUBLESHOOTING PER BOMBARDIER FIM REV 39 IAW AD 2009-06-12 PARAGRAPH (H)(6)(I) AMOC DATED MARCH 27,2009 TR#27-012 PERAMOC DATED DECEMBER 18, 2009 AND PA AD27-052G CODES ARE AS FOLLOWS 72A 72B 12 1B 12 1A 131B 131A,
- [SDR REXA2012041700523](https://openairdocs.org/sdr/REXA2012041700523.md): Detection Sys · malfunctioned · Apr 17, 2012 · N8930E · Cndair CL6002B19 · Trailing Flap Position Indicating System
  > FLAP FAIL DUE TO SKEW DET BOX NOT RESET. PLACARD INSTALLED. PERFORMED T/S OF SKEW DETECTION FLAP FAIL IAW FIM 27-50-00 AND AMM 27-51-15 NOTED SKEW DETECTION WOULD NO RESET. R/R SKEW DETECTION UNIT IAW AMM 27-51-15 PERFORMED SEVERAL OPS CHECK IAW AMM 27-51-15
- [SDR REXA2012041600520](https://openairdocs.org/sdr/REXA2012041600520.md): Sdu · malfunctioned · Apr 16, 2012 · N8930E · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAPS FAIL AT 0. C/W PA AD 27-052G AND FIM 27-50-00. PERFORMED T/S PER BOMBERDIER FIM REV 39 IAW AD 2009-06-12 PARA CH (H)(6)(I), AMOC DATED MARCH 27 2009, TR# 27-012 PER AMOC DATED DEC 18,2009 AND PA AD 27-052G. INSPECTED FECU CODES FOUND TO BE MOST PROBAB
- [SDR REXA2012041200422](https://openairdocs.org/sdr/REXA2012041200422.md): Bulkhead · cracked · Apr 12, 2012 · N8930E · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > WHILE PERFORMING NDT OF PARKING BRAKE CABLE PASS THROUGH HOLE ON PRESSURE BULKHEAD AT FS 202.75 A CRACK WAS FOUND AT THE 3 O'CLOCK POSITION. REPAIRED IAW BOMBARDIER REO 601R-53-11-563.
- [SDR REXA2012033000451](https://openairdocs.org/sdr/REXA2012033000451.md): Aileron Sys · out of limits · Mar 30, 2012 · N8930E · Cndair CL6002B19 · Aileron Control System
  > LEFT AILERON SYSTEM NR 1 BACKLASH CHECK, OUT OF LIMITS. REMOVED AND REPLACED LEFT AILERON SYSTEM NR 1 PCO LINK IAW AMM 27-14-15, OPS CHECKED GOOD.
- [SDR REXA2012032300370](https://openairdocs.org/sdr/REXA2012032300370.md): Attach Bracket · corroded · Mar 21, 2012 · N8930E · Cndair CL6002B19 · Elevator Structure
  > LEFT ELEVATOR PCU ATTACH BRACKETS 1, 2, AND 3 AND HINGE ATTACH BRACKETS NR 1 AND 24.5 HAVE EVIDENCE OF CORROSION AROUND RIVET BUCKTAILS. REPAIRED IAW SRM 51-42-06 AND 51-42-13.
- [SDR REXA2012032300369](https://openairdocs.org/sdr/REXA2012032300369.md): Bulkhead · gouged · Mar 21, 2012 · N8930E · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FS 621 PRESSURE BULKHEAD WEB GOUGED ABOVE WL 73.5. REPAIRED IAW BOMBARDIER REO 601R-53-61-2155.
- [SDR REXA2012022600279](https://openairdocs.org/sdr/REXA2012022600279.md): A/C Pack · uncontrollable · Feb 26, 2012 · N8930E · Cndair CL6002B19 · Cabin Cooling System
  > AT THE GATE APU ON, RIGHT AFTER TURNED THE LEFT PACK ON TEMP STARTED RISING, COULD NOT CONTROL WITH AUTO OR MANUAL MODE. BURNING SMELL WITH POSSIBLY LIGHT SMOKE AND SMOKE WENT AWAY AFTER LEFT PACK OFF. FOUND LT PACK TO BE UNCONTROLLABLE IN AUTO AND MAN. ALS
- [SDR REXA201100995](https://openairdocs.org/sdr/REXA201100995.md): Warning System · false activation · Dec 20, 2011 · N8930E · Cndair CL6002B19 · Airfoil Anti/De-ice System
  > RT ANTI-ICE DUCT FUSELAGE OVERHEAT MSG IN FLIGHT. PERFORMED OPERATIONAL TEST OF WING ANTI-ICE DUCT SYSTEM IAW AMM 30-11-00, OPS CHECK GOOD NO DEFECTS AT THIS TIME.
- [SDR REXA201100754](https://openairdocs.org/sdr/REXA201100754.md): Beam · cracked · Nov 1, 2011 · N8930E · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS 280 TRANSVERSE BEAM CRACKED O/B OF LBL 9 AND RBL 9 AND RT UPPER J-ANGLE CRACKED O/B OF RBL 9. REPAIRED IAW BOMBARDIER REO 601R-53-11-926, BOMBARDIER SERVICE CORPORATION SR 601R-53-0110, SR 601R-53-0057B, AND SR 601R-53-0097A.
- [SDR REXA201100751](https://openairdocs.org/sdr/REXA201100751.md): Skin · dented · Oct 31, 2011 · N8930E · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > RT FUSELAGE SKIN IS DENTED FWD OF FS 700 BETWEEN S-20R AND S-22R. REPAIR IAW EA CRJ253-00184A AS AUTHORIZED BY 8110-3 DATED 10/31/11.
- [SDR REXA201100766](https://openairdocs.org/sdr/REXA201100766.md): Warning System · false activation · Oct 20, 2011 · N8930E · Cndair CL6002B19 · Fuel Pressure Indicator
  > L FUEL LO PRESS CAUTION MESSAGE. PERFORMED OPS CHECK OF FUEL WARNING SYSTEM IAW AMM 28-42-00. NO DEFECT NOTED OPS CHECK GOOD OK FOR SERVICE.
- [SDR REXA201100684](https://openairdocs.org/sdr/REXA201100684.md): Battery · discharged · Oct 6, 2011 · N8930E · Cndair CL6002B19 · Emergency Equipment
  > F/O FLASHLIGHT RED LIGHT NOT BLINKING. REMOVED AND REPLACED F/O'S FLASHLIGHT BATTERY IAW AMM 25-61-04. OPC GOOD. VERIFIED PARTS EFFECTIVITY.
- [SDR REXA201100682](https://openairdocs.org/sdr/REXA201100682.md): Secu · defective · Oct 5, 2011 · N8930E · Cndair CL6002B19 · Drag Control System
  > INBD GRND SPLR'S WILL NOT DEPLOY. REMOVED AND REPLACED SECU NR 1 AMM 27-61-05, OK FOR SERVICE.
- [SDR REXA201000102](https://openairdocs.org/sdr/REXA201000102.md): Ramp · corroded · Aug 5, 2010 · N8930E · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > SERVICE DOOR GALLEY CART RAMP CORROSION FOUND. REMOVED AND REPLACED GALLEY CART RAMP IAW SRM 51-41-02.
- [SDR REXA200600038](https://openairdocs.org/sdr/REXA200600038.md): Flap · malfunctioned · Mar 19, 2006 · N8930E · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAPS FAIL AT 20 DEGREES ON APPROACH. QRH FOLLOWED UNEVENTFUL LANDING. FLAPS RESET AND PLACED ON 72 HOUR WATCH PER AD 98-20-01

## 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 = 'N8930E' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N8930E/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.