# Service difficulty reports: N8587E

A list on [N8587E](https://openairdocs.org/aircraft/N8587E.md).

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

- [SDR REXA2013090301724](https://openairdocs.org/sdr/REXA2013090301724.md): Battery Pack · inoperative · Sep 3, 2013 · N8587E · Cndair CL6002B19 · Emergency Lighting
  > FOUND EMERGENCY LIGHTS ON LT AND RT FUSELAGE INOPERATIVE. REPLACED BATTERY PACK IAW AMM 33-51-04 AND OPS CHECKED GOOD.
- [SDR REXA2013090301723](https://openairdocs.org/sdr/REXA2013090301723.md): Pbe · punctured · Sep 3, 2013 · N8587E · Cndair CL6002B19 · Emergency Equipment
  > AFT PBE POUCH HAS HOLE PUNCTURE. INSTALLED SERVICEABLE PBE AS REQUIRED.
- [SDR REXA2013081101580](https://openairdocs.org/sdr/REXA2013081101580.md): Warning Light · false indication · Aug 11, 2013 · N8587E · Cndair CL6002B19 · Fire Detection
  > RT FIRE FAIL ILLUMUNTED IN FLIGHT FOR APPROX. 30 SECONDS ON 2 OCCASIONS AND THEN EXTINGUISHED. OPERATIONS CHECKED IAW AMM 26-11-00. NO FAULTS NOTED.
- [SDR REXA2013061000699](https://openairdocs.org/sdr/REXA2013061000699.md): Bulkhead · damaged · Jun 7, 2013 · N8587E · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > AFT PRESSURE BULKHEAD TOOLING DAMAGE BEHIND AN ISOLATOR AT LBL9 APPROX 24" ABOVE THE FLOOR, MEASURING.125" X 0.031" X 0.003" DEEP. REPAIRED IAW REO 601R-53-61-2155.
- [SDR REXA2013060600697](https://openairdocs.org/sdr/REXA2013060600697.md): Beam · chafed · Jun 4, 2013 · N8587E · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CENTER VERTICAL BEAM CHAFED ON THE AFT FACE, BL0 FS621 BULKHEAD, 0.005" DEEP AND 0.350" LONG. REPAIRED IAW REO 601R-53-61-1523.
- [SDR REXA2013052801029](https://openairdocs.org/sdr/REXA2013052801029.md): Flap · malfunctioned · May 28, 2013 · N8587E · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAPS FAIL CAUTION MESSAGE DURING AFTER START CHECKLIST WHILE MOVING FLAPS FROM ZERO TO 20 DEGREES ON THE GROUND. FLAPS STOPPED AT ZERO, OAT 14 DEGREES FAILED DURING EXTENSION. PERFORMED SDU RESET PROCEDURES, OPS CHECK GOOD IAW MEL PROCEDURES 27-51-14.
- [SDR REXA2013032800599](https://openairdocs.org/sdr/REXA2013032800599.md): Light · inoperative · Mar 28, 2013 · N8587E · Cndair CL6002B19 · Emergency Lighting
  > LEFT SIDE EXTERIOR EMERGENCY LIGHT INOPERABLE. REMOVED AND REPLACED EXTERIOR EMERGENCY LIGHT IAW AMM 33-51-21. OPERATIONS CHECKED GOOD.
- [SDR REXA2013012700195](https://openairdocs.org/sdr/REXA2013012700195.md): Battery · discharged · Jan 27, 2013 · N8587E · Cndair CL6002B19 · Emergency Equipment
  > CAPTAIN & COPILOT FLASHLIGHTS LED LT INOPERABLE. REMOVED AND REPLACED FLASHLIGHT BATTERIES IAW AMM 25-61-04.
- [SDR REXA2013012100172](https://openairdocs.org/sdr/REXA2013012100172.md): Actuator · failed · Jan 21, 2013 · N8587E · Cndair CL6002B19 · Trailing Edge Flap Actuator
  > ON FLIGHT 3895 (DTW TO ALB) RECEIVED FLAPS FAIL AT 0 ON APPROACH. AIRCRAFT DIVERTED TO GRB AND LANDED SAFELY. PERFORMED TROUBLESHOOT PER BOMBARDIER FIM REV 44 IAW AD 2009-06-12 PARA (H)(6)(I) AMOC DATED DEC 7 2012 AND PA AD27-052J. FAULT CODES HOW JAM ON L
- [SDR REXA2013011800070](https://openairdocs.org/sdr/REXA2013011800070.md): Skin · corroded · Jan 17, 2013 · N8587E · Cndair CL6002B19 · Wing, Plate/Skin
  > RIGHT WING LANDING FOR FUEL ACCESS PANEL 540BB BETWEEN WS 45 AND WS 65.75 PITTED FROM FRETTING AT INBOARD AND OUTBOARD EDGES MEASURING 0.007" DEEP. REPAIRED IAW BOMBARDIER REO 601R-57-21-030.
- [SDR REXA2013011500066](https://openairdocs.org/sdr/REXA2013011500066.md): Vane · chafed · Jan 12, 2013 · N8587E · Cndair CL6002B19 · Trailing Edge Flaps
  > LEFT INBOARD FLAP VANE INBOARD LEADING EDGE CHAFED. REMOVED AND REPLACED IAW SRM 57-52-00.
- [SDR REXA2013011500065](https://openairdocs.org/sdr/REXA2013011500065.md): Vane · chafed · Jan 12, 2013 · N8587E · Cndair CL6002B19 · Trailing Edge Flaps
  > LEFT INBOARD FLAP VANE CENTER LEADING EDGE CHAFED. REMOVED AND REPLACED IAW SRM 57-52-00.
- [SDR REXA2013011500064](https://openairdocs.org/sdr/REXA2013011500064.md): Vane · chafed · Jan 12, 2013 · N8587E · Cndair CL6002B19 · Trailing Edge Flaps
  > RIGHT INBOARD FLAP VANE CENTER LEADING EDGE CHAFED. REMOVED AND REPLACED IAW SRM 57-52-00.
- [SDR REXA2013011500063](https://openairdocs.org/sdr/REXA2013011500063.md): Vane · chafed · Jan 12, 2013 · N8587E · Cndair CL6002B19 · Trailing Edge Flaps
  > RIGHT INBOARD FLAP VANE INBOARD LEADING EDGE CHAFED. REMOVED AND REPLACED IAW SRM 57-52-00.
- [SDR REXA2012050100591](https://openairdocs.org/sdr/REXA2012050100591.md): Light · dirty · May 1, 2012 · N8587E · Cndair CL6002B19 · Emergency Lighting
  > FOUND 2 AFT CEILING EMERGENCY LIGHTS INOP, LIGHTS ADJACENT TO EACH OTHER. REMOVED AND CLEANED EMERGENCY LIGHT BULBS OPS CHECKS GOOD PER CRJ AMM 33-50-00. OK FOR SERVICE.
- [SDR REXA201200123](https://openairdocs.org/sdr/REXA201200123.md): Control Quadrant · faulty · Jan 15, 2012 · N8587E · Cndair CL6002B19 · Aileron Control System
  > UNUSUAL TENSION IN THE YOKE DURING AILERON INPUTS ONLY (WITH THE AUTO PILOT OFF). NOTICED AFTER DISCONNECTING AUTOPILOT FOR LANDING TENSION IN THE YOKE NOT AS NOTICEABLE ON THE GROUND. REMOVED AND REPLACED LT AFT THROTTLE QUADRANT SUB ASSY IAW AMM 27-11-10 R
- [SDR REXA201200111](https://openairdocs.org/sdr/REXA201200111.md): Aileron · binding · Jan 14, 2012 · N8587E · Cndair CL6002B19 · Aileron Control System
  > AILERON BINDING REQUIRES MORE PRESSURE THAN NORMAL TO OPERATE PREVIOUSLY WRITTEN UP 2 TIMES AML PG 2706520 AND 2206536. PERFORMED DVI ON AILERON CONTROL & AILERON TRIM SYSTEM. NO DEFECTS NOTED, SYSTEM OPS CHECKS WITHIN LIMITS IAW AMM 27-11-00. OK FOR SVC.
- [SDR REXA2012010800103](https://openairdocs.org/sdr/REXA2012010800103.md): None · none · Jan 8, 2012 · N8587E · Cndair CL6002B19 · Aileron Control System
  > AILERONS BINDING AND ARE HEAVIER THAN NORMAL. PERFORMED OPS CHECK OF AILERON IAW AMM 27-11-00. OPS CHECKED GOOD, NO ISSUES NOTED AT THIS TIME. OK FOR SERVICE.
- [SDR REXA20100086](https://openairdocs.org/sdr/REXA20100086.md): Warning System · activated · Jan 5, 2012 · N8587E · Cndair CL6002B19 · Landing Gear Position and Warning
  > FLT 4341 HAD AN GEAR UP DISAGREE OUTBOUND. A/C AIR RETURNED AND A/C WAS PLACED ON MEL. NO EMERGENCY DECLARED.
- [SDR REXA201200090](https://openairdocs.org/sdr/REXA201200090.md): Unknown · malfunctioned · Jan 3, 2012 · N8587E · Cndair CL6002B19 · Aileron Control System
  > FLIGHT CONTROLS REQUIRE GREATER THAN NORMAL FORCE TO MOVE AND AILERONS DO NOT SELF CENTER. PERFORMED OPS TEST OF AILERON CONTROL AND AILERON TRIM SYSTEM IAW AMM 27-11-00, NO DEFECTS NOTED. A/C OK FOR SERVICE.
- [SDR REXA201100991](https://openairdocs.org/sdr/REXA201100991.md): Quick Disconnect · disconnected · Dec 19, 2011 · N8587E · Cndair CL6002B19 · Landing Gear Brake System
  > HYDRAULIC QUICK DISCONNECT ON RT INBOARD LANDING GEAR FOUND DISCONNECTED. RE-SECURED RT INBOARD BRAKE QUICK DISCONNECT AS REQUIRED. OK FOR SVC.
- [SDR REXA201100776](https://openairdocs.org/sdr/REXA201100776.md): Inverter · inoperative · Oct 25, 2011 · N8587E · Cndair CL6002B19 · Emergency Lighting
  > REAR 3 EMERGENCY FLOOR LIGHT STRIPS INOP. REMOVED AND REPLACED NR 4 EMERGENCY LIGHT INVERTER IAW AMM 33-51-07. OP/C GOOD. PART EFFECTIVITY VERIFIED. OK FOR SERVICE.
- [SDR REXA201100058](https://openairdocs.org/sdr/REXA201100058.md): Skin · damaged · Jan 19, 2011 · N8587E · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > PUNCTURE (3.1 LONG X.16 IN WIDE REF) AND DENT (3.9 LONG X 2.7 WIDE X.24 IN DEEP REF) IN FUSELAGE SKIN AT FS 319.70 - 333 AND STR 24-25 LT. EDDY CURRENT WAS PERFORMED TO CONFIRM THERE WAS NO OTHER CRACK IN DISCREPANT AREA. TEMPORARY REPAIR AND FERRY FLY AIR
- [SDR REXA201000294](https://openairdocs.org/sdr/REXA201000294.md): Bulkhead · cracked · Dec 7, 2010 · N8587E · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FS 202.75 PRESSURE BULKHEAD IS CRACKED AT BRAKE CABLE PASS-THRU HOLE. REPAIRED IAW REO 601R-53-11-563 AND BSC STANDARD REPAIR 601R-53-0101A.
- [SDR REXA201000293](https://openairdocs.org/sdr/REXA201000293.md): Skin Panel · dented · Dec 7, 2010 · N8587E · Cndair CL6002B19 · Wing, Plate/Skin
  > LT WING LOWER SKIN BETWEEN WS 353.00 AND 389.00 HAS 5 DENTS. REPLACED SKIN PANEL IAW BOMBARDIER SERVICES ENGINEERING ORDER 601R-57-19981.
- [SDR REXA201000088](https://openairdocs.org/sdr/REXA201000088.md): Skin · damaged · May 21, 2010 · N8587E · Cndair CL6002B19 · Wing, Plate/Skin
  > A/C STRUCK TUG WHILE BEING MARSHALED, APPROXIMATELY 10 FEET FROM THE FINAL POSITION. DAMAGE OCCURRED AT CONTACT AT LT WING LEADING EDGE AT WS 380 AND CONTINUED AFT TO 5 LOCATIONS ON METALLIC LWR WING SKIN AND TWO ON THE LWR TRAILING EDGE FAIRING. PICTURES WI
- [SDR REXA200900037](https://openairdocs.org/sdr/REXA200900037.md): Proximity Sensor · misrigged · Mar 26, 2009 · N8587E · Cndair CL6002B19 · Landing Gear Position and Warning
  > ON CLIMBOUT, RECEIVED "GEAR DISAGREE" MESSAGE WITH "NOSE DOOR" AND "WOW STATUS MESSAGE" QRH FOLLOWED, RETURNED TO FIELD WITH UNEVENTFUL LANDING. MX INTERROGATED PSEU (PROXIMITY SYS ELECTRONIC UNIT) FOUND CODES FOR NOSE GEAR NR 2 WITH NO FURTHER DEFECTS. (K)
- [SDR REX2008F00044](https://openairdocs.org/sdr/REX2008F00044.md): Bpsu · malfunctioned · Aug 25, 2008 · N8587E · Cndair CL6002B19 · Trailing Edge Flap Control System
  > IN CRUISE AT FL 220 RECEIVED A FLAP FAIL CAUTION MESSAGE QRH FOLLOWED DECLARED EMERGENCY, DIVERT TO DTW FROM LEX LANDED WITHOUT INCIDENT IN DTW. TROUBLESHOT FLAP SYSTEM IAW BOMBARDIER FAULT ISOLATION MANUAL (FIM) AND ACFT MX MANUAL (AMM) R&R RT BRAKE POSITION
- [SDR REXA200600051](https://openairdocs.org/sdr/REXA200600051.md): Bpsu · failed · Apr 11, 2006 · N8587E · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAPS FAIL INDICATION ON APPROACH WHEN SELECTING FLAPS DOWN. QRH FOLLOWED UNEVETFUL LANDING. MAINTENANCE REMOVED AND REPLACED THE LEFT BRAKE POSITION SENSING UNIT (BPSU) IAW BOMBARDIER AMM AND PERFORMED OPERATIONAL CHECKS.
- [SDR REXA200600047](https://openairdocs.org/sdr/REXA200600047.md): Flap · malfunctioned · Apr 7, 2006 · N8587E · Cndair CL6002B19 · Trailing Edge Flap Control System
  > RECEIVED FLAPS FAIL MESSAGE AT GATE. SYSTEM WAS RESET AND PLACED ON A 72 HOUR WATCH PER AD 98-20-01.
- [SDR REX2005F00044](https://openairdocs.org/sdr/REX2005F00044.md): Proximity Switch · out of adjust · May 2, 2005 · N8587E · Cndair CL6002B19 · Landing Gear Position and Warning
  > (REF NR: 05-059) RECEIVED (GEAR DISAGREE) MESSAGE ON APPROACH. QRH FOLLOWED GEAR MANUALLY EXTENDED. EMERGENCY DECLARED UNEVENTFUL LANDING. ADJUSTED NOSE GEAR PROXIMITY SWITCH IAW AMM. GEAR SWINGS PERFORMED. (K)

## 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 = 'N8587E' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N8587E/reports

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