# Service difficulty reports: N528CA, cancelled Jun 26, 2019

A list on [N528CA, cancelled Jun 26, 2019](https://openairdocs.org/deregistered/N528CA-2019-06-26.md).

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

- [SDR ASOA20161206247](https://openairdocs.org/sdr/ASOA20161206247.md): Battery Pack · corroded · Dec 6, 2016 · N528CA · Cndair CL6002D24 · Emergency Lighting
  > EMERGENCY LIGHTS OUT IN GALLEY AND MID CABIN. REMOVED AND REPLACED BATTERY PACK ASSY PER AMM 33-51-04. OPS CHECKED GOOD, NO FURTHER DEFECTS NOTED.
- [SDR ASOA2014041810381](https://openairdocs.org/sdr/ASOA2014041810381.md): Lamp · burned out · Apr 17, 2014 · N528CA · Cndair CL6002B19 · Emergency Lighting
  > FWD ORANGE SEGMENT OF EMERGENCY FLOOR PATH LIGHTS INOPERATIVE. R & R EMERGENCY FLOOR PATH LIGHT FLEXIBLE LAMP NR 1 IAW AMM 33-51-01. OPS CHECK GOOD. SDR CLOSED.
- [SDR ASOA2014031010107](https://openairdocs.org/sdr/ASOA2014031010107.md): Light · inoperative · Mar 6, 2014 · N528CA · Cndair CL6002B19 · Emergency Lighting
  > CABIN FLOOR FORWARD MOST EMERGENCY LIGHT STRIP, ORANGE, INOPERATIVE. PERFORMED THE OPS TEST OF THE EMERGENCY FLOOD LIGHTS IAW AMM 33-51-00. OPS CHK GOOD.
- [SDR ASOA2013090608962](https://openairdocs.org/sdr/ASOA2013090608962.md): Connector · disconnected · Sep 3, 2013 · N528CA · Cndair CL6002B19 · Light System Wiring
  > EMERGENCY LIGHT STRIP ABOVE PAX DOOR DOES NOT ILLUMINATE. REINSTALLED CONNECTOR FOR EMERGENCY EXIT SIGN IAW AMM 33-51-01.
- [SDR ASOA2013050603474](https://openairdocs.org/sdr/ASOA2013050603474.md): Battery Pack · discharged · Apr 30, 2013 · N528CA · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY LIGHT AT ROW 5 INOPERATIVE. FOUND BATTERY PACK TO BE DISCHARGED. CHARGED BATTERY PACK. OPS CHECKED GOOD IAW AMM 33-51-00.
- [SDR ASOA2013050303472](https://openairdocs.org/sdr/ASOA2013050303472.md): Skin · damaged · Apr 22, 2013 · N528CA · Cndair CL6002B19 · Trailing Edge Flaps
  > RT OTBD FLAP DAMAGED ON T/E. 41" FROM INBD END, DAMAGE IS APPROX 10" L. COMPLIED WITH MAJOR REPAIR IAW REO 601R-57-53-041, REV A, DATED 2004/05/07. COMPLIED WITH EC/TC EO 600-57-0128 02.
- [SDR ASOA2013050303471](https://openairdocs.org/sdr/ASOA2013050303471.md): Floor Panel · dented · Apr 8, 2013 · N528CA · Cndair CL6002B19 · Fuselage Floor Panel
  > PRESSURE FLOOR SKIN HAS 1 EA DENT MEASURING 4.256" LONG X 1.980" WIDE X.015" DEEP AND HAS 5 EA GOUGES WITH MAX DAMAGE BEING.730" LONG X.062" WIDE X.008" DEEP WITH HIGH METAL AT FS 553 BETWEEN LBL 0 AND LBL 9 AND IS NOT WITHIN REPAIRABLE LIMITS IAW SRM 53-4
- [SDR ASOA2013050303470](https://openairdocs.org/sdr/ASOA2013050303470.md): Bulkhead · damaged · Apr 8, 2013 · N528CA · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > AT FS 621.00 BULKHEAD LBL 30 WL 135 THERE IS A DRILL START.150" WIDE.031" DEEP AND.150" FROM CENTER OF FIRE BLOCK HOLE/NUTPLATE AT.1562" TO CENTER OF DRILL START. COMPLIED WITH MAJOR REPAIR IAW REO 601R-53-61-4873, DATED 2013/04/11. COMPLIED WITH EC/TC RE
- [SDR ASOA2013050203469](https://openairdocs.org/sdr/ASOA2013050203469.md): Bushing · damaged · Apr 6, 2013 · N528CA · Cndair CL6002B19 · Horizontal Stabilizer Structure
  > LT BUSHINGS AT HORIZONTAL STAB HINGE ARE DAMAGED. REPAIRED IAW REO 601R-55-00-045 REV B, 2013/04/27. MAJOR REPAIR
- [SDR ASOA2013042503445](https://openairdocs.org/sdr/ASOA2013042503445.md): Intercostal · cracked · Apr 5, 2013 · N528CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS 621.00 CRACKED INTERCOSTAL STRINGER 13L,. REMOVED CRACKED INTERCOSTAL IAW SRM 51-42-21. LOCATED & DRILLED NEW INTERCOSTAL IAW SRM 51-40-11. INSTALLED INTERCOSTAL IAW SRM 51-42-21.
- [SDR ASOA2013042503444](https://openairdocs.org/sdr/ASOA2013042503444.md): Bulkhead · cracked · Apr 4, 2013 · N528CA · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FOUND REAR PRESSURE BULKHEAD WEB HAS INDICATION NOTED AT LBL 27.50 WL 130 APPROX.2" IN LENGTH 60 PERCENT FSH FAILED NDT INSPECTION. REPAIRED IAW REO 601R-53-61-1541.
- [SDR ASOA2013042503443](https://openairdocs.org/sdr/ASOA2013042503443.md): Bulkhead · cracked · Apr 3, 2013 · N528CA · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FOUND FS 559 BULKHEAD WEB RT SIDE HAS INDICATION NOTED APPROX.3" IN LENGTH 50 PERCENT FSH AT WL 59.10 INBD OF RBL 18.0. FAILED NDT INSPECTION. REPAIRED IAW REO 601R-53-41-260 AND REO 601R-53-41-260, REV E, DATED: 08/24/2010, REO 601R-53-41-609, REO 601R-53-
- [SDR ASOA2013042503442](https://openairdocs.org/sdr/ASOA2013042503442.md): Post · cracked · Apr 3, 2013 · N528CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FOUND FS 409.00+128 VERTICAL POST BL 0.00 RT SIDE HAS INDICATION NOTED AT AFT FLANGE RADIUS WL 69.0 APPROX.2" IN LENGTH 50 PERCENT FSH. FAILED NDT INSPECTION. REPAIRED LT & RT POST BL 0 FS 409+128 IAW SRM 51-42-06 & REO 601R-53-41-889.
- [SDR ASOA2013020702965](https://openairdocs.org/sdr/ASOA2013020702965.md): Circuit Card · unserviceable · Feb 3, 2013 · N528CA · Cndair CL6002B19 · Rudder Control System
  > UNCOMMANDED FULL RT RUDDER DEFECTION IN FLT ON A/P, NO EICAS MSG OVER POWERED, DISCONNECTED A/P AND YD, WERE ABLE TO RETRIM (ENROUTE, ACFT DIVERTED TO GSO DUE TO MX) R & R NR 1 AND NR 2 FCC CARDS IAW AMM 22-12-14, OPS CHECK GOOD IAW AMM 22-12-14 IOC REF 22-
- [SDR ASOA2012081702076](https://openairdocs.org/sdr/ASOA2012081702076.md): Switch · illuminated · Aug 13, 2012 · N528CA · Cndair CL6002B19 · Engine Thrust Reverser
  > LEFT THRUST REVERSER UNLOCK MESSAGE. EMERGENCY DECLARED. R & R STOW SWITCH IAW AMM 78-37-01. OPS CHECKED GOOD.
- [SDR ASOA201201674](https://openairdocs.org/sdr/ASOA201201674.md): Sensing Element · broken · May 22, 2012 · N528CA · Cndair CL6002B19 · Overheat Detection
  > LT 10TH DUCT IN FLIGHT FOLLOWED CHECK LIST IT DID NOT GO OUT. DELCARED EMERGENCY AND RETURNED TO ATC (AFTER T/O ACFT RETURNED TO DEPARTURE AFTER T/O -- EMERGENCY DECLARED AS A PRECAUTION) FOUND SENSING ELEMENT A48WK BROKEN. R & R SENSING ELEMENT A48WK IAW A
- [SDR ASOA201201237](https://openairdocs.org/sdr/ASOA201201237.md): Fitting · cracked · Apr 9, 2012 · N528CA · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > REAR PRESSURE BULKHEAD CRACKED AT MACHINE FITTING (LINTEL FITTING) AT CARGO DOOR CUTOUT. REPAIRED IAW REO 601R-53-61-1230, REV C.
- [SDR ASOA201201235](https://openairdocs.org/sdr/ASOA201201235.md): Pressure Blkhd · cracked · Apr 9, 2012 · N528CA · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > REAR PRESSURE BULKHEAD CRACKED AT RBL 36.20. REPAIRED IAW REO 601R-53-61-1285, REV D AND REO 601R-53-61-1285 REV D.
- [SDR ASOA201201219](https://openairdocs.org/sdr/ASOA201201219.md): Wire · broken · Apr 6, 2012 · N528CA · Cndair CL6002B19 · Light System Wiring
  > WIRE BROKEN ON EMERGENCY FLOOR TRACK LIGHTING AT FWD END. REPLACED CRIMP CONNECTOR ON RT FWD EMERGENCY LIGHT FLOOR STRIP LIGHTING WIRE IAW ESPM 20-17-00. OPS TESTED IAW AMM 33-51-00-710-801. OPS CHECKED GOOD.
- [SDR ASOA201101683](https://openairdocs.org/sdr/ASOA201101683.md): Connector · damaged · Sep 9, 2011 · N528CA · Cndair CL6002B19 · Light System Wiring
  > EMERGENCY LIGHTS INOPERATIVE, CENTER TWO SECTIONS AND FWD WHITE SECTION AT FLOOR POSITIONS. R & R FWD WHITE EMERG LIGHT SECTION IAW AMM 33-51-01-000-801 AND 33-51-01-400-801. FOUND 2 SETS OF CONNECTORS (MALE/FEMALE) NOT TERMINATED ON LIGHT STRIP INSTALLED
- [SDR ASOA201101559](https://openairdocs.org/sdr/ASOA201101559.md): Attach Fitting · cracked · Aug 22, 2011 · N528CA · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > CLIP AT FS 484.00, RBL 27 CRACKED. R & R A NEW CLIP AT FS 484.00, RBL 27 IAW SRM 51-42-21. THIS REPAIR IS CLASSIFIED AS A MINOR REPAIR.
- [SDR ASOA201101558](https://openairdocs.org/sdr/ASOA201101558.md): Beam · cracked · Aug 22, 2011 · N528CA · Cndair CL6002B19 · Fuselage Main, Structure
  > FS 280 TRANSVERSE BEAM CRACKED IN WEB OTBD OF RBL 9. THIS DISCREPANCY AND THE AFT J-ANGLES ON JOB 8784121, OP 159 IS BEING REPAIRED AS ONE IAW REO 601R-53-11-926.
- [SDR ASOA201101557](https://openairdocs.org/sdr/ASOA201101557.md): Floorbeam · cracked · Aug 22, 2011 · N528CA · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FS 280 TRANVERSE BEAM UPPER AFT J-ANGLE CRACKED OTBD OF LBL 9 AND RBL 9. REPAIRED IAW REO 601R-53-11-926 REV B.
- [SDR ASOA201101556](https://openairdocs.org/sdr/ASOA201101556.md): Angle · corroded · Aug 22, 2011 · N528CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PASSENGER DOOR CUTOUT LOWER ANGLE HAS CORROSION AROUND HOLE FOR PROXIMITY SENSOR. REMOVED CORROSION IAW SRM 51-21-06 AND FOUND THE REMOVED MATERIAL (0.003) WITHIN THE LIMIT IAW SRM 53-00-00 AND SRM 53-21-023.
- [SDR ASOA201101555](https://openairdocs.org/sdr/ASOA201101555.md): Angle · cracked · Aug 22, 2011 · N528CA · Cndair CL6002B19 · Cargo/Baggage Doors
  > CARGO DOOR FWD TRACK LOWER C-CHANNEL ANGLE CRACKED. R & R DAMAGED C-CHANNEL IAW SRM 51-41-06 & 51-41-04. REPAIR IS CLASSIFIED AS A MINOR REPAIR.
- [SDR ASOA201101554](https://openairdocs.org/sdr/ASOA201101554.md): Drag Angle · cracked · Aug 22, 2011 · N528CA · Cndair CL6002B19 · Passenger/Crew Doors
  > PASSENGER DOOR AFT DRAG ANGLE CRACKED. REPAIRE IAW REO 601R-52-11-513 AND REO NR 610R-52-11-513, REV A.
- [SDR ASOA201101553](https://openairdocs.org/sdr/ASOA201101553.md): Web · cracked · Aug 22, 2011 · N528CA · Cndair CL6002B19 · Passenger/Crew Doors
  > PASSENGER DOOR FWD WEB CRACKED AT 4TH RISER. REPAIRED IAW REO 601R-52-11-702.
- [SDR ASOA201101522](https://openairdocs.org/sdr/ASOA201101522.md): Door · none · Aug 17, 2011 · N528CA · Cndair CL6002B19 · Emergency Exits
  > LEFT EMERGENCY OVERWING EXIT FAILS FUNCTION TEST, FORCE TO OPERATE HANDLE EXCEEDS 40 LBS. PERFORMED FUNCT TEST OF THE LT EMERGENCY EXIT IAW AMM 52-21-00-720-801. FUNCTION TEST GOOD AT 35LBS.
- [SDR ASOA201101072](https://openairdocs.org/sdr/ASOA201101072.md): Attach Fitting · cracked · May 27, 2011 · N528CA · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > FS 625, OBLIQUE CLIP IS CRACKED. REMOVED CLIP IAW SRM 51-42-20. COMPLIED WITH EDDY CURENT INSP IAW NDTM 51-20-06, PART 1 53-00-096, PART 6 AND COMFIRMED CRACK. INSTALLED NEW CLIP IAW REO 601R-53-61-100 AND REO 601R-53-61-422.
- [SDR ASOA201101071](https://openairdocs.org/sdr/ASOA201101071.md): Doubler · cracked · May 27, 2011 · N528CA · Cndair CL6002B19 · Fuselage Main, Structure
  > LT SIDE FS 640.00 DOUBLER CRACKED AT CUTOUT RADIUS FOR ENGINE SUPPORT BEAM ATTACH POINT. REPAIRED.
- [SDR REXA201100128](https://openairdocs.org/sdr/REXA201100128.md): Warning System · activated · Feb 16, 2011 · N528CA · Cndair CL6002B19 · Landing Gear Position and Warning
  > GEAR DISAGREE NOSE DOOR WARNING NOSE GEAR NEVER CAME UP DEFERRED PER MEL 32-30-01.
- [SDR REXA201000234](https://openairdocs.org/sdr/REXA201000234.md): Connector · dirty · Oct 24, 2010 · N528CA · Cndair CL6002B19 · Fire Protection System Wiring
  > DURING CLIMB, PASSING 27000FT CARGO BOTTLE LOW CAUTION MESSAGE CAUTION MESSAGE EXTINGUISHED DESCENDING THROUGH 11000FT. REMOVED, CLEANED, RESECURED CONNECTOR ON CARGO BOTTLES, TEST GOOD PER CRJ AMM 26-20-00.
- [SDR REXA201000136](https://openairdocs.org/sdr/REXA201000136.md): Unknown · odor · Sep 10, 2010 · N528CA · Cndair CL6002B19 · Air Distribution System
  > FUMES IN COCKPIT/CABIN LED TO DIVERSION. APU OFF/BLEEDS ON ENGINES/SMELLED LIKE CIGARETTE BURNING/NO VISIBLE SMOKE. PERFORMED GROUND RUNS WITH BLEEDS ON ENGINES AND APU NO FUMES OR SMOKE NOTED. PER 71-00-00 OPS CHECKED 1 AND 2 PACKS PER 21-50-00 OPS GOOD.
- [SDR REXA201000092](https://openairdocs.org/sdr/REXA201000092.md): Selector Valve · malfunctioned · Jun 7, 2010 · N528CA · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > UPON CLIMBOUT AFTER THE CLIMB CHECK, HAD A GEAR DISAGREE MSTR WARNING. THE NOSE GEAR WAS THE ONE IN DISAGREEMENT. THE F/O START THE QRH, THE WARNING WENT AWAY. A/C RETURNED TO DTW AND MAINTENANCE REMOVED AND REPLACED THE NLG SELECTOR VALVE IAW AMM 32-20-00.
- [SDR COMA0760474](https://openairdocs.org/sdr/COMA0760474.md): Ecu · faulty · Jul 11, 2007 · N528CA · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLIGHT 5011 - FLAP FAIL CAUTION RECEIVED ON TAXI OUT. RETURNED TO GATE. REPLACED FECU. NO FURTHER DEFECTS.
- [SDR COMA0760261](https://openairdocs.org/sdr/COMA0760261.md): Windshield · cracked · Mar 15, 2007 · N528CA · Cndair CL6002B19 · Flight Compartment Windows
  > CAPTAIN'S WINDSHIELD INNER PANEL SHATTERED. PROCEEDED TO CVG WITHOUT INCIDENT. REPLACED CAPTAIN'S WINDSHIELD.
- [SDR COMA0760150](https://openairdocs.org/sdr/COMA0760150.md): Flap System · malfunctioned · Feb 6, 2007 · N528CA · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLIGHT 5115 - DURING YUL APPROACH RECEIVED A FLAP FAIL CAUTION MESSAGE. COMPLIED WITH AD 2006-12-21 FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (G) 1, 2, 3, (A, B, C). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES.
- [SDR COMA0760080](https://openairdocs.org/sdr/COMA0760080.md): Shaft · damaged · Jan 26, 2007 · N528CA · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLIGHT 5510 - FLAP FAIL MESSAGE AT 8 DEGREES. LANDED WITHOUT INCIDENT. PERFORMED EO 27-046 AD INCLUDING FLAP SHAFT REJUVENATION. NO FURTHER DEFECTS.
- [SDR COMA0660501](https://openairdocs.org/sdr/COMA0660501.md): Skin Panel · cracked · Aug 18, 2006 · N528CA · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR SECOND STEP DOWN FORWARD AND AFT SKINS CRACKED UNDER BRACKETS WHERE HAND RAILS STOW WHEN DOWN. AFT SKIN ALSO CRACKED THIRD STEP DOWN IN RADIUS OF TREAD/RISER. REMOVED DAMAGED AREAS OF PAX DOOR FORWARD AND AFT SKINS SECOND STEP, AND THIRD STEP AFT SK
- [SDR COMA0660103](https://openairdocs.org/sdr/COMA0660103.md): Generator · faulty · Jan 28, 2006 · N528CA · Cndair CL6002B19 · AC Generation System
  > FLIGHT 5104 - CLIMBING OUT OF AUS DURING GEAR RETRACTION, THE AIR DRIVE GENERATOR DEPLOYED, FLIGHT RETURNED TO THE FIELD. REPLACED THE ADG AUTO DEPLOY CONTROL PANEL.
- [SDR COMA0560199](https://openairdocs.org/sdr/COMA0560199.md): Window · cracked · Mar 21, 2005 · N528CA · Cndair CL6002B19 · Flight Compartment Windows
  > FLIGHT 5380 PILOTS SIDE WINDOW CRACKED. REPLACED PILOTS SIDE WINDOW.
- [SDR COMA0560072](https://openairdocs.org/sdr/COMA0560072.md): Hydraulic System · low · Jan 22, 2005 · N528CA · Cndair CL6002B19 · Hydraulic System, Main
  > FLIGHT 5045 - DURING APPROACH TO BOS, RECEIVED A GEAR DISAGREE FOLLOWED BY A HYDRAULIC NR 3 LOW PRESSURE CAUTION, CREW DECLARED AN EMERGENCY, FOLLOWED QRH AND LANDED WITHOUT INCIDENT. SERVICED THE NR 3 HYDRAULIC SYSTEM.
- [SDR COMA0460288](https://openairdocs.org/sdr/COMA0460288.md): Pitot Line · contaminated · Apr 23, 2004 · N528CA · Cndair CL6002B19 · Pitot/Static System
  > FLIGHT 5208 ABORTED TAKEOFF AT 75 KTS DUE TO INOPERATIVE STANDBY AIRSPEED INDICATION. PURGED WATER FROM THE STANDBY PITOT SYSTEM LINE.
- [SDR COMA0460058](https://openairdocs.org/sdr/COMA0460058.md): Control Unit · malfunctioned · Jan 14, 2004 · N528CA · Cndair CL6002B19 · Stabilizer Control System
  > FLIGHT 5710 STAB TRIM AND MACH TRIM DISENGAGED DURING T/O. REPLACED THE HSTCU.
- [SDR COMA0460009](https://openairdocs.org/sdr/COMA0460009.md): Engine · fluctuates · Dec 30, 2003 · N528CA · Cndair CL6002B19 · Engine (Turbine/Turboprop)
  > FLIGHT 5732 N1 AND N2 AND F/F FLUCTUATING. COULD NOT DUPLCIATE. GROUND RUNS WERE NORMAL AND SATISFACTORY.
- [SDR COMA0360420](https://openairdocs.org/sdr/COMA0360420.md): Warning Light · illuminated · Sep 21, 2003 · N528CA · Cndair CL6002B19 · Trailing Edge Flap Control System
  > DURING DECENT INTO DTW RECEIVED A FLAP FAIL CAUTION MESSAGE AT 20 DEGREE FLAP POSITION. COMPLIED WITH AD 98-20-01 FLAP CAUTION MESSAGE (FIRST EVENT) FLAP SYSTEM WAS RESET WITH NO FURHTER FLAP CAUTION MESSAGES.

## 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 = 'N528CA' AND deregistration_id = 'N528CA-2019-06-26'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N528CA-2019-06-26/reports

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