# Service difficulty reports: N8541D

A list on [N8541D](https://openairdocs.org/aircraft/N8541D.md).

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

- [SDR REXA2014071600702](https://openairdocs.org/sdr/REXA2014071600702.md): Cover · wrong part · Jul 16, 2014 · N8541D · Cndair CL6002B19 · Emergency Lighting
  > CREW REPORTS ARROW ON RT EMER EXIT COVER FOR OVERWING EXIT IS POINTING WRONG WAY. R & R RT EMER OVERWING EXIT LIGHT COVER IAW AMM 33-51-13.
- [SDR REXA2014070600675](https://openairdocs.org/sdr/REXA2014070600675.md): Light · inoperative · Jul 7, 2014 · N8541D · Cndair CL6002B19 · Emergency Lighting
  > PAX DOOR LOWER EMERGENCY LIGHT INOPERATIVE. REPLACED EMERGENCY LIGHT ASSEMBLY IAW AMM 33-51-19. OPS TESTED OK.
- [SDR REXA2013081201584](https://openairdocs.org/sdr/REXA2013081201584.md): Light · inoperative · Aug 12, 2013 · N8541D · Cndair CL6002B19 · Emergency Lighting
  > MOST FORWARD CEILING EMERGENCY FLOOD LIGHT INOPERATIVE.
- [SDR REXA2013080601558](https://openairdocs.org/sdr/REXA2013080601558.md): Recorder · no test · Aug 6, 2013 · N8541D · Cndair CL6002B19 · Audio/Video Monitoring
  > CVR WILL NOT TEST. REPLACED CVR IAW AMM 23-71-01. OPS TESTED GOOD.
- [SDR REXA2013071201350](https://openairdocs.org/sdr/REXA2013071201350.md): Recorder · no test · Jul 12, 2013 · N8541D · Cndair CL6002B19 · Audio/Video Monitoring
  > CVR WILL NOT TEST.
- [SDR REXA2013011000128](https://openairdocs.org/sdr/REXA2013011000128.md): Life Vest · unserviceable · Jan 10, 2013 · N8541D · Cndair CL6002B19 · Life Jacket
  > CAPTAINS LIFE VEST HAS A TEAR IN BAG. REMOVED AND REPLACED CAPTAINS LIFE VEST IAW AMM 25-61-03.
- [SDR REXA2012112701534](https://openairdocs.org/sdr/REXA2012112701534.md): Flap · bent · Nov 26, 2012 · N8541D · Cndair CL6002B19 · Trailing Edge Flaps
  > LEFT INBOARD FLAP TRAILING EDGE BENT. REPAIRED IAW SRM 57-52-00.
- [SDR REXA2012112701533](https://openairdocs.org/sdr/REXA2012112701533.md): Seat Track · corroded · Nov 26, 2012 · N8541D · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > NR 5 RIGHT SEAT TRACK CORRODED. REPAIRED IAW AMM 53-01-11.
- [SDR REXA2012112701532](https://openairdocs.org/sdr/REXA2012112701532.md): Seat Track · corroded · Nov 26, 2012 · N8541D · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > NR 4 RIGHT SEAT TRACK CORRODED. REPAIRED IAW AMM 53-01-11.
- [SDR REXA2012112701531](https://openairdocs.org/sdr/REXA2012112701531.md): Seat Track · corroded · Nov 26, 2012 · N8541D · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > NR 3 RIGHT SEAT TRACK CORRODED. REPAIRED IAW AMM 53-01-11.
- [SDR REXA2012112701530](https://openairdocs.org/sdr/REXA2012112701530.md): Seat Track · corroded · Nov 26, 2012 · N8541D · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > NR 2 RIGHT SEAT TRACK CORRODED. REPAIRED IAW AMM 53-01-11.
- [SDR REXA2012112701529](https://openairdocs.org/sdr/REXA2012112701529.md): Floorbeam · corroded · Nov 26, 2012 · N8541D · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FLOORBEAM CAP AT LBL 27 IN CARGO AREA IS CORRODED BETWEEN FS 560 AND FS 621. REPAIRED IAW BOMBARDIER REO 601R-53-61-3778.
- [SDR REXA2012112701528](https://openairdocs.org/sdr/REXA2012112701528.md): Floorbeam · corroded · Nov 26, 2012 · N8541D · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FLOORBEAM CAP AT LBL 9 IS CORRODED BETWEEN FS 560 AND FS 621. REPAIRED IAW BOMBARDIER REO 601R-53-61-3780.
- [SDR REXA2012112601707](https://openairdocs.org/sdr/REXA2012112601707.md): Hinge · worn · Nov 26, 2012 · N8541D · Cndair CL6002B19 · Passenger/Crew Doors
  > AIRCRAFT IN HEAVY CHECK FOUND PASSENGER DOOR HINGE WORN, DURING RELIABILITY CHECKS. REMOVED AND REPLACED PASSENGER DOOR HINGE IAW CRJ 200 SRM 52-10-31.
- [SDR REXA2012112501698](https://openairdocs.org/sdr/REXA2012112501698.md): Battery Pack · discharged · Nov 25, 2012 · N8541D · Cndair CL6002B19 · Emergency Lighting
  > GALLEY EMERGENCY LIGHT INOPERABLE NEXT TO SERVICE DOOR. REMOVED AND REPLACED BATTERY PACK IAW CRJ 200 AMM 33-51-04. OPS CHECK BATTERY PACK IAW CRJ 200 AMM 33-51-04. NO DEFECTS NOTED.
- [SDR REXA201100959](https://openairdocs.org/sdr/REXA201100959.md): Warning System · activated · Dec 10, 2011 · N8541D · Cndair CL6002B19 · Engine Oil Indicating System
  > DIVERTED DUE TO RT ENG OIL PRESSURE WARNING MSG. CREW SHUT DOWN NR 2 ENG AND HAD MINIMAL SMOKE IN THE CABIN. CREW DECLARED AN EMERGENCY AND LANDED SAFELY. THIS IS NOT A REPEAT ITEM BUT RT ENG WAS ON OIL CONSUMPTION WATCH.
- [SDR REXA201100447](https://openairdocs.org/sdr/REXA201100447.md): Control Unit · malfunctioned · Jul 16, 2011 · N8541D · Cndair CL6002B19 · Stabilizer Control System
  > AIR RETURN STAB CHANNEL 1 INOP SWAPPED FROM 8541 TO 8808. REMOVED AND REPLACED THE MOTOR CONTROL UNIT AND ACTUATOR IAW AMM 27-40-00.
- [SDR REXA201100437](https://openairdocs.org/sdr/REXA201100437.md): Indication Sys · malfunctioned · Jul 2, 2011 · N8541D · Cndair CL6002B19 · Fuel Quantity Indicator
  > ON CLIMBOUT FUEL IMBALANCE MESSAGE. MADE IT TO 1100 LBS. PER QRH SUSPECT FUEL LEAK. A/C DIVERTED INTO BOS FROM JFK - YHZ ROUTE. MAINTENANCE DEFERRED EICAS FUEL QUANTITY - SPR OPERATIVE - IAW MEL 28-41-01, DM-46539. DM CLEARED ON TL-203802-2011 OPS CHECK O
- [SDR REXA201100212](https://openairdocs.org/sdr/REXA201100212.md): Bulkhead · cracked · Mar 29, 2011 · N8541D · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > CRACK INDICATION AT LBL 18 CRACK IS 1.0625 INCH LONG. CRACK INDICATION AT RBL 18 CRACK IS.8125 INCH LONG. CRACK INDICATION AT RBL 9 OUTBOARD POST CRACK IS.5 INCH LONG. CRACK INDICATION AT RBL 9 INBOARD POST CRACK IS.625 INCH LONG. REPAIRED IAW BOMBARDIE
- [SDR REXA201100192](https://openairdocs.org/sdr/REXA201100192.md): Skin · dented · Mar 23, 2011 · N8541D · Cndair CL6002B19 · Trailing Edge Flaps
  > RIGHT INBOARD FLAP DENTED BETWEEN CANT FLAP STATION 79.062 AND CANT FLAP STATION 82.473 JUST FORWARD OF REAR SPAR ON THE UPPER SKIN. REPAIRED IAW BOMBARDIER SERVICE CORPORATION EO 601R-57-20992A AND 8110-3 DATED 3/23/11.
- [SDR REXA201000231](https://openairdocs.org/sdr/REXA201000231.md): Sill · corroded · Oct 30, 2010 · N8541D · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CARGO SILL PLATE CORRODED BEYOND LIMILTS. REMOVED CARGO SILL PLATE IAW CRJ200 SRM 51-42-06. LOCATED AND DRILL NEW SERVICEABLE CARGO SILL PLATE IAW CRJ 200 SRM 51-40-11. INSTALLED NEW SERVICEABLE CARGO SILL PLATE IAW BOMBARDIER REO 601R-53-61-593 REV A.
- [SDR REXA201000230](https://openairdocs.org/sdr/REXA201000230.md): Stiffener · cracked · Oct 30, 2010 · N8541D · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FOUND FS 409.00+128 VERTICAL POST AT RBL 18.00 I/B O/B SIDE HAS INDICATION NOTED APPROXIMATELY.200" IN LENGTH AT WL 69.0. REMOVED VERTICAL POST ASSEMBLY AT FS 409.00+128, RBL 18.00 IAW CRJ 200 SRM 51-42-06. LOCATED AND DRILLED NEW O/B POSTS IAW CRJ 200 SRM
- [SDR REXA201000229](https://openairdocs.org/sdr/REXA201000229.md): Stiffener · cracked · Oct 30, 2010 · N8541D · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FOUND FS 409.00+128 VERTICAL POST AT LBL 18.00 I/B O/B SIDE HAS INDICATION NOTED APPROXIMATELY.200" IN LENGTH AT WL 69.0. REMOVED VERTICAL POST ASSEMBLY AT FS 409.00+128, LBL 18.00 IAW CRJ 200 SRM 51-42-06. LOCATED AND DRILLED NEW IO/B POSTS IAW CRJ 200 SRM
- [SDR REXA201000015](https://openairdocs.org/sdr/REXA201000015.md): Unknown · odor · Feb 1, 2010 · N8541D · Cndair CL6002B19 · Air Distribution System
  > 2/1/10 FLIGHT 4022 MEM TO TYS ON TAKEOFF RWY9 AFTER 120 KIAS, RECEIVED A SMOKE TOILET MASTER CAUTION MESSAGE. THERE WAS A SMELL OF PETROLEUM OR DEICE FLUID IN THE FLIGHT DECK. AFTER ROTATION PF DECLARED AN EMERGENCY WITH MEM TOWER. MADE RIGHT TRAFFIC TO LAN
- [SDR REXA200700015](https://openairdocs.org/sdr/REXA200700015.md): Flap System · failed · Feb 2, 2007 · N8541D · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAPS FAIL AT ZERO DEGREES UPON APPROACH. LANDING UNEVENTFUL. COMPLIED WITH AD 2001-12-21 BY RESET AND MONITORING FOR 72 HOURS.
- [SDR REXA200600105](https://openairdocs.org/sdr/REXA200600105.md): Flap · malfunctioned · Nov 24, 2006 · N8541D · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAPS FAILED AT ZERO ON APPROACH. EMERGENCY DECLARED QRH FOLLOWED WITH UNEVENTFUL ZERO FLAP LANDING. SYSTEM RESET AND PLACED ON 72 HOUR WATCH PER AD 2006-12-21.
- [SDR REXA200600069](https://openairdocs.org/sdr/REXA200600069.md): Flap · malfunctioned · Jun 17, 2006 · N8541D · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAPS FAIL. MONITORING FLAPS FOR 72 HOURS PER AD 98-20-01.
- [SDR REXA200600029](https://openairdocs.org/sdr/REXA200600029.md): Trim System · malfunctioned · Mar 2, 2006 · N8541D · Cndair CL6002B19 · Elevator Control System
  > ON APPROACH TO DTW BOTH STAB TRIM CHANNELS AND MACH TRIM DISENGAGED AND WOULD NOT RESET. RECEIVED STAB TRIM AND MACH TRIM CAUTION MESSAGES. CONTROLS FELT HEAVY, FOLLWED QRH AND CONFIGURED FOR FLAPS 45 DEGREE APPROACH. DECLARED EMERGENCY AND HAD AN UNEVENTFU

## 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 = 'N8541D' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N8541D/reports

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