# Service difficulty reports: N8554A

A list on [N8554A](https://openairdocs.org/aircraft/N8554A.md).

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

- [SDR REXA2013032600592](https://openairdocs.org/sdr/REXA2013032600592.md): Control Cable · lack of lube · Mar 26, 2013 · N8554A · Cndair CL6002B19 · Power Lever
  > THRUST LEVERS ARE STIFF AND DIFFICULT TO MOVE THROUGH WHOLE RANGE OF MOTION. THRUST LEVERS ARE STIFFER MORE DIFFICULT TO MOVE AT CLIMB. LUBED BOTH LEFT & RIGHT AFT THROTTLE CONTROL CABLES IAW AMM 76-11-00. OPERATIONS CHECK GOOD FOR FRICTION TEST IAW AMM 76-
- [SDR REXA2013032600591](https://openairdocs.org/sdr/REXA2013032600591.md): Sign · cracked · Mar 26, 2013 · N8554A · Cndair CL6002B19 · Emergency Lighting
  > SERVICE DOOR EXIT SIGN CRACKED. REMOVED AND REPLACED EXIT SIGN IAW AMM 33-51-13. OK FOR SERVICE.
- [SDR REXA2013020300217](https://openairdocs.org/sdr/REXA2013020300217.md): Battery · discharged · Feb 3, 2013 · N8554A · Cndair CL6002B19 · Emergency Equipment
  > CAPTAIN FLASHLIGHT SEAL BROKE AND NO RED LIGHT. REMOVED AND REPLACED CAPTAIN'S FLASHLIGHT BATTERY AND SEAL IAW AMM 25-61-04. OK FOR SERVICE.
- [SDR REXA2012120701755](https://openairdocs.org/sdr/REXA2012120701755.md): Unknown · unknown · Dec 7, 2012 · N8554A · Cndair CL6002B19 · Smoke Detection
  > SMOKE TOILET, AFTER TAKEOFF, RAN QRH, RETURNED TO MSP. COMPLETED PA 21-009 AND PERFORMED MINIMUM WORK SCOPE FOR SMOKE TOILET, AFTER TAKEOFF. SUSPECT DEICE FLUID. OK FOR SERVICE.
- [SDR REXA2012112201520](https://openairdocs.org/sdr/REXA2012112201520.md): Skin · chafed · Nov 21, 2012 · N8554A · Cndair CL6002B19 · Trailing Edge Flaps
  > RIGHT INBOARD FLAP VANE UPPER SKIN AT TRAILING EDGE AT FLAP STATION 99 AND 104 CHAFED. REPAIRED IAW SRM 57-52-00/51-12-00.
- [SDR REXA2012081901273](https://openairdocs.org/sdr/REXA2012081901273.md): Bulb · inoperative · Aug 19, 2012 · N8554A · Cndair CL6002B19 · Emergency Lighting
  > OVERHEAD EMERGENCY EXIT FLOOD LIGHT INOPERATIVE AT SEAT 2C. REPLACED BULB IAW AMM 33-51-16. OPS CHECKS GOOD AT THIS TIME.
- [SDR REXA2012040200474](https://openairdocs.org/sdr/REXA2012040200474.md): Striker · damaged · Apr 2, 2012 · N8554A · Cndair CL6002B19 · Passenger/Crew Doors
  > DURING SERVICE CHECK PERFORMING INSPECTECTION OF DEF-059269 OF PASSENGER DOOR SEAL STRIKER FOUND DAMAGE TO LOWER REPAIRED AREA. REPAIRED DOOR SEAL STRIKER IAW REO 601R-53-22-033 PART IV. NO FURTHER DAMAGE NOTED.
- [SDR REXA2012030500333](https://openairdocs.org/sdr/REXA2012030500333.md): Control Wheel · loose · Mar 5, 2012 · N8554A · Cndair CL6002B19 · Aileron Control System
  > IN FLIGHT DURING CLIMB AND DESCENT, CAPT + F/O AILERONS IN TURNING THE YOKE FEEL NORMAL PRESSURE ASSOCIATED WITH A BANK. AT A CERTAIN POINT IN THE TURN, A CATCHING IS FELT AND THE NORMAL PRESSURE ASSOSIATED WITH A TURN IS LOST. HAPPENDS IN BOTH LEFT + RIGHT
- [SDR REXA2012030200321](https://openairdocs.org/sdr/REXA2012030200321.md): Aileron · out of adjust · Mar 2, 2012 · N8554A · Cndair CL6002B19 · Aileron Control System
  > AILERON CONTROL FELT STIFF ON FINAL. ADJ/OPC ON AILERON SYSTEM DONE IAW AMM 27-12-00. NO DEFECTS NOTED. OK FOR SVC.
- [SDR REXA2012021800261](https://openairdocs.org/sdr/REXA2012021800261.md): Aileron Sys · binding · Feb 18, 2012 · N8554A · Cndair CL6002B19 · Aileron Control System
  > CAPT'S YOKE, AILERON CONTROL SLIPS AND BINDS. INSPECTED CAPTAIN`S AILERON CABLE RUN, NO DEFECTS NOTED. CLEANED & LUBED BEHIND YOKE CABLE ASSY IAW AMM 27-00-00. OPS CHECKED GOOD.
- [SDR REXA2012021600236](https://openairdocs.org/sdr/REXA2012021600236.md): Strut · discharged · Feb 16, 2012 · N8554A · Cndair CL6002B19 · Nose/Tail Landing Gear Strut/Axle
  > GEAR DISAGREE MASTER WARNING AND NOSE DOOR OPEN MASTER WARNING BOTH ON CLIMBOUT WHEN SELECTING GEAR TO THE UP POSITION. SERVICED NOSE GEAR IAW AMM 12-12-32. ADJUSTED CENTERING PROX SWITCH IAW AMM 32-61-05. C/W PA 05-018B CKS GOOD. OK FOR SERVICE.
- [SDR REXA2012021200233](https://openairdocs.org/sdr/REXA2012021200233.md): Strut · underserviced · Feb 12, 2012 · N8554A · Cndair CL6002B19 · Nose/Tail Landing Gear Strut/Axle
  > GEAR DISAGREE MAST WARNING AND NOSE DOOR OPEN MAST. WARNING BOTH ON CLIMBOUT WHEN SELECTING GEAR TO THE UP POSITION. SERVICED NOSE GEAR IAW AMM 12-12-32. ADJUSTED CENTERING PROXIMITY SWITCH IAW AMM 32-61-05. COMPLIED WITH PA 05-018B, CHECKED GOOD, OK FOR S
- [SDR REXA2012021200228](https://openairdocs.org/sdr/REXA2012021200228.md): Link · faulty · Feb 12, 2012 · N8554A · Cndair CL6002B19 · Aileron Control System
  > AILERON CONTROLS BINDING WHEN APPLING LEFT PRESSURE INTON A TURN. FOUND LT/RT AILERON BACKLASH OUT OF TOLERANCE. REMOVED AND REPLACED LT/RT AILERON PCU LINKS IAW AMM 27-14-15. RIGGED LT/RT AILERONS IAW AMM 27-11-00. AILERON CONTROL SYS OPS CHECKS GOOD. OK
- [SDR REXA201200026](https://openairdocs.org/sdr/REXA201200026.md): Unknown · malfunctioned · Jan 1, 2012 · N8554A · Cndair CL6002B19 · Aileron Control System
  > IRREGULAR CONTROL FORCES. WHEN LEFT AILERON IS APPLIED IT FEELS LIKE A SECTION OF SLACK FOLLOWED BY A SECTION OF BINDING. ONLY OCCURS TO THE LEFT. DOES NOT OCCUR WITH HYDRAULICS OFF. CONTROL MOVEMENT DID CORRECTLY RESPOND TO APPLICATION. SET AILERON TRIM
- [SDR REXA201100832](https://openairdocs.org/sdr/REXA201100832.md): Control System · out of adjust · Nov 10, 2011 · N8554A · Cndair CL6002B19 · Aileron Control System
  > WHEN ROLLING THE AIRCRAFT TO THE LEFT THE CONTROLS FEEL LIKE THEY HAVE A SLIP IN THEM OR THAT SOMETHING IS BLOCKING THE MOVEMENT. ADJUSTED AILERON CONTROL SYSTEM IAW AMM 27-11-05. OPC GOOD.
- [SDR REXA201100606](https://openairdocs.org/sdr/REXA201100606.md): Light · misinstalled · Sep 18, 2011 · N8554A · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY LIGHTS (FLOOR STRIP) WILL NOT WORK FROM SEATS 6-9. CORRECTLY CONNECTED EMERGENCY FLOOR LIGHTS IAW GMM33-51-00. OPS CHECK GOOD, OK FOR SERVICE.
- [SDR REXA201100563](https://openairdocs.org/sdr/REXA201100563.md): Warning System · activated · Sep 3, 2011 · N8554A · Cndair CL6002B19 · Landing Gear Position and Warning
  > AIR RETURN FOR GEAR UP DISAGREE EMERGENCY DECLARED AND MX CURRENTLY INSPECTING FOR ISSUES.
- [SDR REXA201100534](https://openairdocs.org/sdr/REXA201100534.md): Coupling · damaged · Aug 17, 2011 · N8554A · Cndair CL6002B19 · Pneumatic Distribution System
  > ON CLIMBOUT FROM FWA RECEIVED A "L JET PIPE OVHT" MSG. CREW PERFORMED QRH AND MSG WENT OUT AT AROUND 70 PERCENT N1. RETURNED AND LANDED AT KFWA. MAINTENANCE INSPECTED JETPIPE FOR OVHT CONDITION, FOUND NONE. MAINTENANCE FOUND TERMINAL WIRE TO LOOP "B" BARE.
- [SDR REXA201100083](https://openairdocs.org/sdr/REXA201100083.md): Striker · damaged · Feb 3, 2011 · N8554A · Cndair CL6002B19 · Passenger/Crew Doors
  > PASSENGER DOOR SEAL STRIKER WAS FOUND DAMAGED. THE SEAL STRIKER HAD BEEN PREVIOUSLY REPAIRED PER BOMBARDIER REO 601R-53-22-033 TYPE I, BUT NOW THE SEALANT APPLIED PER FLAGNOTE 6 OF THE REO IS GONE. FERRY FLY FROM PIT TO MSP IAW STS ENGINEERING EA 09-2011-030
- [SDR REXA201000275](https://openairdocs.org/sdr/REXA201000275.md): Post · cracked · Nov 23, 2010 · N8554A · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS 409+128 LBL 18 VERTICAL POST OUTBOARD HALF IS CRACKED AT LOWER CORNER. COMPLIED WITH PERMANENT REPAIR BY REMOVING AND REPLACING OUTBOARD VERTICAL POST HALF AT FS 409+128 RBL 18.00 WITH SERVICEABLE P/N 601R32208-156 IAW CRJ 200 SRM 51-42-06 AND BOMBARDIER R
- [SDR REXA201000274](https://openairdocs.org/sdr/REXA201000274.md): Post · cracked · Nov 23, 2010 · N8554A · Cndair CL6002B19 · Fuselage Main, Structure
  > FS 409+128 RBL 18 VERTICAL POST OUTBOARD HALF IS CRACKED AT LOWER CORNER. COMPLIED WITH PERMANENT REPAIR BY REMOVING AND REPLACING OUTBOARD VERTICAL POST HALF AT FS 409+128 RBL 18.00 WITH SERVICEABLE P/N 601R32208-155 IAW SRM 51-42-06 AND REO 601R-53-41-889.
- [SDR REXA201000273](https://openairdocs.org/sdr/REXA201000273.md): Post · cracked · Nov 23, 2010 · N8554A · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS 559.00 LBL 18 VERTICAL POST IS CRACKED AT LOWER INBOARD CORNER. REMOVED AND REPLACED FS 559.00 LBL 18 VERTICAL POST IAW CRJ-200 SRM 51-42-06.
- [SDR REXA201000272](https://openairdocs.org/sdr/REXA201000272.md): Seat Track · corroded · Nov 23, 2010 · N8554A · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LT AND RT CABIN SIDEWALL SEAT TRACKS FROM FS 444.0 TO FS 495.0 ARE CORRODED. REMOVED AND REPLACED LT AND RT CABIN SIDEWALL SEAT TRACKS FROM FS 444.0 TO FS 495.0 IAW CRJ 200 AMM 53-01-11-000-802 AND 53-01-11-400-802.
- [SDR REXA201000271](https://openairdocs.org/sdr/REXA201000271.md): Seat Track · corroded · Nov 23, 2010 · N8554A · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LT AND RT CABIN SIDEWALL SEAT TRACK FROM FS 364 TO FS 409+18 ARE CORRODED. REMOVED AND REPLACED LT AND RT CABIN SIDEWALL SEAT TRACK FROM FS 364 TO FS 409+18 IAW CRJ 200 AMM 53-01-11-000-802 AND 53-01-11-400-802.
- [SDR REXA201000270](https://openairdocs.org/sdr/REXA201000270.md): Seat Track · corroded · Nov 23, 2010 · N8554A · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > CABIN SEAT TRACKS AT LBL 9.0 & RBL 9.0, FS 409+128 TO FS 559, ARE CORRODED. REMOVED AND REPLACED SEAT TRACKS AT LBL 9.0 & RBL 9.0, FS 409+128 TO FS 559, IAW CRJ 200 AMM 53-01-11-000-802 AND 53-01-11-400-802.
- [SDR REXA201000269](https://openairdocs.org/sdr/REXA201000269.md): Seat Track · corroded · Nov 23, 2010 · N8554A · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > CABIN SEAT TRACK WHERE SEAT MEETS LAV FLOORBOARD HAS MINOR CORROSION. REPLACED SEAT TRACK IAW CRJ 200 AMM 53-01-11-000-802 AND 53-01-11-400-802.
- [SDR REXA200900046](https://openairdocs.org/sdr/REXA200900046.md): Bulkhead · cracked · May 6, 2009 · N8554A · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > CRACK IN FWD PRESSURE BULKHEAD AROUND PARKING BRAKE CABLE AT FS 202.75, BL 23.71. (K)
- [SDR REXA200900045A](https://openairdocs.org/sdr/REXA200900045A.md): Switch · out of adjust · May 3, 2009 · N8554A · Cndair CL6002B19 · Nose/Tail Landing Gear
  > GEAR DISAGREE ON FINAL APPROACH. THE FINAL SIGN OFF WAS FOUND NOSE WHEEL CENTERING SWITCH OUT OF ADJ, IAW AMM 32-61-05. PERFORMED GEAR SWINGS. (K)
- [SDR REXA200900045](https://openairdocs.org/sdr/REXA200900045.md): Bulkhead · cracked · May 3, 2009 · N8554A · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > CRACK IN FORWARD PRESSURE BULKHEAD. AROUND PARKING BRAKE CABLE AT FS 202.75. LBL 23.71.
- [SDR REX2009F00007](https://openairdocs.org/sdr/REX2009F00007.md): Actuator · failed · Jan 20, 2009 · N8554A · Cndair CL6002B19 · Trailing Edge Flap Actuator
  > FLAPS FAIL AT ZERO ON APPROACH. RAI FLAP ACTUATOR IAW AMM 27-53-01.
- [SDR REX2009F00006](https://openairdocs.org/sdr/REX2009F00006.md): Actuator · failed · Jan 20, 2009 · N8554A · Cndair CL6002B19 · Trailing Edge Flap Actuator
  > FLAPS FAIL AT ZERO ON APPROACH. RAI FLAP ACTUATOR IAW AMM 27-53-01.
- [SDR REX2009F00005](https://openairdocs.org/sdr/REX2009F00005.md): Actuator · failed · Jan 20, 2009 · N8554A · Cndair CL6002B19 · Trailing Edge Flap Actuator
  > FLAPS FAIL AT ZERO ON APPROACH. RAI FLAP ACTUATOR IAW AMM 27-53-01.
- [SDR REX2009F00004](https://openairdocs.org/sdr/REX2009F00004.md): Actuator · failed · Jan 20, 2009 · N8554A · Cndair CL6002B19 · Trailing Edge Flap Actuator
  > FLAPS FAIL AT ZERO ON APPROACH. RAI FLAP ACTUATOR IAW AMM 27-53-01.
- [SDR REX2009F00003](https://openairdocs.org/sdr/REX2009F00003.md): Actuator · failed · Jan 20, 2009 · N8554A · Cndair CL6002B19 · Trailing Edge Flap Actuator
  > FLAPS FAIL AT ZERO ON APPROACH. RAI FLAP ACTUATOR IAW AMM 27-53-01.
- [SDR REX2009F00002](https://openairdocs.org/sdr/REX2009F00002.md): Actuator · failed · Jan 20, 2009 · N8554A · Cndair CL6002B19 · Trailing Edge Flap Actuator
  > FLAPS FAIL AT ZERO ON APPROACH. RAI FLAP ACTUATOR IAW AMM 27-53-01.
- [SDR REX2009F00001](https://openairdocs.org/sdr/REX2009F00001.md): Actuator · failed · Jan 20, 2009 · N8554A · Cndair CL6002B19 · Trailing Edge Flap Actuator
  > FLAPS FAIL AT ZERO ON APPROACH. RAI FLAP ACTUATOR IAW AMM 27-53-01.
- [SDR REX2009F00000](https://openairdocs.org/sdr/REX2009F00000.md): Actuator · failed · Jan 20, 2009 · N8554A · Cndair CL6002B19 · Trailing Edge Flap Actuator
  > FLAPS FAIL AT ZERO ON APPROACH. RAI FLAP ACTUATOR IAW AMM 27-53-01.
- [SDR REX2009F00021](https://openairdocs.org/sdr/REX2009F00021.md): Ecs · contaminated · Jan 14, 2009 · N8554A · Cndair CL6002B19 · Air Conditioning System
  > SHORTLY AFTER TAKE OFF RECEIVED SMOKE TOILET MSG WITH NO ABNORMAL ODORS OR ACTUAL SMOKE. QRH FOLLOWED AND RETURNED TO BASE WITH UNEVENTFUL LANDING. MX INSPECTED ACFT WITH NO DEFECTS FOUND, MSG RESULTED FROM RESIDUAL DE-ICE FLUID ENTERING THE ECS SYSTEM. GRO
- [SDR REX2008F00035](https://openairdocs.org/sdr/REX2008F00035.md): Hydraulic System · malfunctioned · Aug 7, 2008 · N8554A · Cndair CL6002B19 · Hydraulic System, Main
  > ON APPROACH INTO KCLE, WHEN GEAR WAS LOWERED THE AURAL "GEAR DISAGREE" WARNING WENT OFF WITH A RED NOSE GEAR INDICATION. CREW DECLARED AN EMERGENCY AND MANUALLY LOWERED THE GEAR. AN OTHERWISE NORMAL APPROACH AND LANDING WAS MADE AT KCLE. MAINTENANCE PERFORM
- [SDR REX2008F00025](https://openairdocs.org/sdr/REX2008F00025.md): Priority Valve · malfunctioned · Aug 1, 2008 · N8554A · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > ON APPROACH INTO KMSP, WHEN GEAR WAS LOWERED THE AURAL "GEAR DISAGREE" WARNING WENT OFF WITH A RED NOSE GEAR INDICATION. CREW DECLARED AN EMERGENCY AND MANUALLY LOWERED THE GEAR. AN OTHERWISE NORMAL APPROACH AND LANDING WAS MADE AT KMSP. MAINTENANCE MET THE
- [SDR REX2008F00004](https://openairdocs.org/sdr/REX2008F00004.md): Unknown · jammed · Jul 2, 2008 · N8554A · Cndair CL6002B19 · Elevator Control System
  > ON SHORT FINAL ELEVATOR CONTROL BECAME WHAT APPEARED TO BE "JAMMING" INTERMITTENTLY. ELEVATOR SYSTEM CHECKED GOOD ON GROUND. UPON FURTHER INSPECTION NOTICED VERTICAL STABILIZER VISOR PANELS DEFORMED. PANELS REMOVED, ELEVATOR ATTACHMENT POINTS, ATTACHMENT HA
- [SDR REX2008F00012](https://openairdocs.org/sdr/REX2008F00012.md): Door · open · Jun 26, 2008 · N8554A · Cndair CL6002B19 · Passenger/Crew Doors
  > PASSENGER DOOR MASTER WARNING DURING CLIMB. FOLLOWED QRH AND DECLARED AN EMERGENCY. NO LOSS IN CABIN PRESSURE AND DOOR REMAINED CLOSED. LANDING WAS UNEVENTFUL. EXTERIOR HANDLE APPEARED TO BE OPEN SLIGHTLY AS STATED BY EMERGENCY PERSONNEL (CFR). MAINTENANC
- [SDR REX2005F00018](https://openairdocs.org/sdr/REX2005F00018.md): Control System · failed · Jul 6, 2005 · N8554A · Cndair CL6002B19 · Trailing Edge Flap Control System
  > (REF NR: 05-085) FLAP FAILED ON APPROACH. RESET SYSTEM AND PLACED ON 72 HOUR WATCH IAW AD 98-20-01. (K)
- [SDR REXA02023](https://openairdocs.org/sdr/REXA02023.md): Computer · malfunctioned · Nov 22, 2002 · N8554A · Cndair CL6002B19 · Smoke Detection
  > ON APPROACH CREW RECEIVED A FALSE CARGO SMOKE WARNING RESULTING IN THE OPERATION OF THE EXTINGUISHING SYSTEM. UPON INVESTIGATION FOUND FIRE WARNING CONTROL COMPUTER TO BE MALFUNCTIONING. REMOVED AND REPLACED CONTROL SYSTEM OPERATES NORMALLY. (M)

## 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 = 'N8554A' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N8554A/reports

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