# Service difficulty reports: N244CA, cancelled Aug 21, 2013 A list on [N244CA, cancelled Aug 21, 2013](https://openairdocs.org/deregistered/N244CA-2013-08-21.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR COMA9910035](https://openairdocs.org/sdr/COMA9910035.md): Skin · dented · Feb 18, 1999 · N244CA · Emb EMB120RT · Fuselage Main, Plate/Skin > DURING 1C INSPECTION, FOUND SMALL DENT IN FUSELAGE SKIN BETWEEN FS 6462.6 AND 6653.1 AND BETWEEN STRINGERS 19L AND 18L. REPAIRED DAMAGED AREA IAW EMB 120 SRM 53-00-01 PG 202-204. - [SDR COMA9910036](https://openairdocs.org/sdr/COMA9910036.md): Plate · dented · Feb 17, 1999 · N244CA · Emb EMB120RT · Nacelle/Pylon, Plate/Skin > DURING ENGINE REPLACEMENT, THE LEFT NACELLE CENTER PLATE SECTION WAS FOUND TO HAVE A DENT AND CHAFING DAMAGE ON THE AFT OUTBOARD SIDE. BOTH THE DENT AND CHAFING DAMAGE WERE REPAIRED PER AERODESIGN REPORT NR 3133-1, REV IR, 2-12-99. - [SDR COMA9910031](https://openairdocs.org/sdr/COMA9910031.md): Lens · missing · Feb 3, 1999 · N244CA · Emb EMB120RT · Emergency Lighting > EMERGENCY EXIT LIGHT COVER IS MISSING AT ROW 5. REPLACED LIGHT COVER. - [SDR COMA9910015](https://openairdocs.org/sdr/COMA9910015.md): Valve · malfunctioned · Jan 18, 1999 · N244CA · Emb EMB120RT · Compressor Bleed Valve > AIR CONDITIONING SYSTEM EMITS SMOKE. COULD NOT DUPLICATE DISCREPANCY. REPLACED THE RIGHT HAND ENGINE P2.5/3 SWITCHING VALVE FOR TROUBLESHOOTING. - [SDR COMA9810266](https://openairdocs.org/sdr/COMA9810266.md): Bulb · failed · Nov 11, 1998 · N244CA · Emb EMB120RT · Emergency Lighting > EMERGENCY FLOOR LIGHT AT ROW 5 INOPERABLE. REMOVED AND REPLACED BULB. - [SDR COMA9810128](https://openairdocs.org/sdr/COMA9810128.md): Roller · worn · May 25, 1998 · N244CA · Emb EMB120RT · Trailing Edge Flaps > FLAPS WOULD NOT RETRACT AFTER TAKEOFF. REPLACED FLAP ROLLERS AT LEFT HAND OUTBOARD FLAP. - [SDR COMA9810118](https://openairdocs.org/sdr/COMA9810118.md): Sensor · malfunctioned · May 12, 1998 · N244CA · Emb EMB120RT · Landing Gear Position and Warning > WHEN LANDING GEAR RETRACTED, THE NLG DOWN LIGHTS AND INTRANSIT LIGHTS REMAINED ON. REPLACED THE NLG DOWN LOCK PROXIMITY SENSOR. - [SDR COMA9810099](https://openairdocs.org/sdr/COMA9810099.md): Intransit Light · illuminated · Apr 9, 1998 · N244CA · Emb EMB120RT · Landing Gear Position and Warning > LEFT HAND MLG INTRANSIT LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. ENTERED DISCREPANCY IN DEFERRED MAINTENANCE LOG PER MEL. - [SDR COMA9810098](https://openairdocs.org/sdr/COMA9810098.md): Support · corroded · Apr 2, 1998 · N244CA · Emb EMB120RT · Fuselage Miscellaneous Structure > DURING 2C INSPECTION TASK 5310-131/132-01I, FOUND FLOOR SUPPORT-T AT FRAME 20R CORRODED BEYOND EMB LIMITS. REMOVED DAMAGED PART AND INSTALLED SERV PART IAW EMB-120 SRM, CHAPTER 51. - [SDR COMA9810097](https://openairdocs.org/sdr/COMA9810097.md): Sill · corroded · Apr 2, 1998 · N244CA · Emb EMB120RT · Fuselage Miscellaneous Structure > DURING 2C INSPECTION TASK 151/152-01Z, FOUND AFT EMERGENCY EXIT SILL AND PIN RECEPTACLES CORRODED BEYOND EMB LIMITS. REMOVED DAMAGED PARTS AND INSTALLED SERV PARTS IAW EMB-120 SRM, CHAPTER 51. - [SDR COMA9810096](https://openairdocs.org/sdr/COMA9810096.md): Support · corroded · Apr 2, 1998 · N244CA · Emb EMB120RT · Fuselage Miscellaneous Structure > DURING 2C INSPECTION TASK 5310-131/132 01I, FOUND FLOOR SUPPORT-T AT FRAME 20L CORRODED BEYOND EMB LIMITS. REMOVED DAMAGED PART AND INSTALLED SERV PART IAW EMB-120 SRM, CHAPTER 51. - [SDR COMA9810095](https://openairdocs.org/sdr/COMA9810095.md): Sill · corroded · Apr 2, 1998 · N244CA · Emb EMB120RT · Fuselage Miscellaneous Structure > DURING 2C INSPECTION TASK 5310-131/132 01I, FOUND FIRST LEFT FLOOR SILL CORRODED BYOND EMB LIMITS. REMOVED DAMAGED PART AND INSTALLED SERV PART IAW EMB-120 SRM, CHAPTER 51. - [SDR COMA9810094](https://openairdocs.org/sdr/COMA9810094.md): Sill · corroded · Apr 2, 1998 · N244CA · Emb EMB120RT · Fuselage Miscellaneous Structure > DURING 2C INSPECTION TASK 161/162-01Z, FOUND RIGHT CARGO FORWARD FLOOR SILL CORRODED BEYOND EMB LIMITS. REMOVED DAMAGED PART AND INSTALLED SERV PART IAW EMB-120 SRM, CHAPTER 51. - [SDR COMA9810093](https://openairdocs.org/sdr/COMA9810093.md): Support · corroded · Apr 2, 1998 · N244CA · Emb EMB120RT · Fuselage Miscellaneous Structure > DURING 2C INSPECTION TASK 5310-131/132 01I, FOUND FLOOR SUPPORT-T AT FRAME 16L CORRODED BEYOND EMB LIMITS. REMOVED DAMAGED PART AND INSTALLED SERV PART IAW EMB-120 SRM CHAPTER 51. - [SDR COMA9810092](https://openairdocs.org/sdr/COMA9810092.md): Support · corroded · Apr 2, 1998 · N244CA · Emb EMB120RT · Fuselage Miscellaneous Structure > DURING 2C INSPECTION TASK 5310-131/132 01I, FOUND FLOOR SUPPORT-T AT FRAME 16R CORRODED BEYOND EMB LIMITS. REMOVED DAMAGED PART AND INSTALLED SERV PART IAW EMB-120 SRM, CHAPTER 51. - [SDR COMA9810091](https://openairdocs.org/sdr/COMA9810091.md): Strap · corroded · Apr 2, 1998 · N244CA · Emb EMB120RT · Fuselage Miscellaneous Structure > DURING 2C INSPECTION TASK 5310-131/132 01I, FOUND FIRST RIGHT BUTT STRAP CORRODED BEYOND EMB LIMITS. REMOVED DAMAGED PART AND INSTALLED SERV PART IAW EMB-120 SRM CHAPTER 51. - [SDR COMA9810090](https://openairdocs.org/sdr/COMA9810090.md): Sill · corroded · Apr 2, 1998 · N244CA · Emb EMB120RT · Fuselage Miscellaneous Structure > DURING 2C INSPECTION TASK 5310-131/132 O1I, FOUND FIRST RIGHT FLOOR SILL CORRODED BYOND EMB LIMITS. REMOVED DAMAGED PART AND INSTALLED SERV PART IAW EMB-120 SRM, CHAPTER 51. - [SDR COMA9810089](https://openairdocs.org/sdr/COMA9810089.md): Strap · corroded · Apr 2, 1998 · N244CA · Emb EMB120RT · Fuselage Miscellaneous Structure > DURING 2C INSPECTION TASK 5310-131/01I, FOUND FIRST LEFT HAND BUTT STRAP CORRODED BEYOND EMB-LIMITS. REMOVED DAMAGED PART AND INSTALLED SERV PART IAW EMB-120 SRM CHAPTER 51. - [SDR COMA9810088](https://openairdocs.org/sdr/COMA9810088.md): Strap · corroded · Apr 2, 1998 · N244CA · Emb EMB120RT · Fuselage Miscellaneous Structure > DURING 2C INSPECTION TASK 5310-131/132 O1I, FOUND FIRST CENTER BUTT STRAP CORRODED BEYOND EMB LIMITS. REMOVED DAMAGED PART AND INSTALLED SERV PART IAW EMB-120 SRM CHAPTER 51. - [SDR COMA9710485](https://openairdocs.org/sdr/COMA9710485.md): Control Box · failed · Nov 30, 1997 · N244CA · Emb EMB120RT · Landing Gear Position and Warning > LEFT HAND MLG UNSAFE INDICATION DURING TAKEOFF. REPLACED THE LANDING GEAR CONTROL BOX. - [SDR COMA9710468](https://openairdocs.org/sdr/COMA9710468.md): Regulator Valve · failed · Nov 1, 1997 · N244CA · Emb EMB120RT · Pneumatic Distribution System > RT BLEED AIR DUCT LEAK WARNING ON. FOUND THE DRAIN CUP ON THE DE-ICE PRESSURE REGULATOR HAD FALLEN OFF. THIS ITEM IS RETAINED BY A WORN CLAMP. REINSTALLED DRAIN CUP. - [SDR COMA9710403](https://openairdocs.org/sdr/COMA9710403.md): Gear Control · failed · Sep 10, 1997 · N244CA · Emb EMB120RT · Landing Gear Selector > LANDING GEAR CONTROL WAS CYCLED 3 TIMES BEFORE GEAR RESPONDED. REPLACED THE LANDING GEAR CONTROL. - [SDR COMA9710402](https://openairdocs.org/sdr/COMA9710402.md): Tq Signal Cond · malfunction · Sep 9, 1997 · N244CA · Emb EMB120RT · Propeller Controlling System > AUTO FEATHER AURAL WARNING SOUNDED DURING TAKEOFF ROLL. REPLACED THE RIGHT ENGINE TORQUE SIGNAL CONDITIONER. - [SDR COMA9710352](https://openairdocs.org/sdr/COMA9710352.md): Bulb · failed · Aug 21, 1997 · N244CA · Emb EMB120RT · Landing Gear Position and Warning > RIGHT GEAR INDICATED UP ATER PLACING GEAR HANDLE DOWN. USED ELECTRICAL OVERRIDE, GEAR CONFIRMED DOWN, APPEARS TO BE AN INDICATION PROBLEM. REMOVED AND REPLACED ALL LANDING GEAR INDICATOR DOWN BULBS. PERFORMED SEVERAL GEAR SWINGS, NO DEFECTS NOTED. - [SDR COMA9710268](https://openairdocs.org/sdr/COMA9710268.md): Lockwasher · worn · May 17, 1997 · N244CA · Emb EMB120RT · Main Landing Gear Attach Section > DURING E-5 INSPECTION, FOUND LEFT MAIN GEAR OUTBOARD TRUNNION BEARING NUT TO BE LOOSE. REMOVED NUT AND FOUND LOCKWASHER INNER TAB TO BE SHEARED OFF. ALSO, NOTICED THAT LOCK WASHER WAS OUT OF ROUND AND APPEARED TO BE STRETCHTED IN AREA OF INNER TAB. REPLACED - [SDR COMA970150](https://openairdocs.org/sdr/COMA970150.md): Roller · dirty · Feb 15, 1997 · N244CA · Emb EMB120RT · Trailing Edge Flaps > FLAP DISAGREE WARNING AFTER TAKEOFF. REPLACED THE FLAP ROLLERS. - [SDR COMA9710096](https://openairdocs.org/sdr/COMA9710096.md): Pitchlock Screw · bent · Jan 30, 1997 · N244CA · Emb EMB120RT · Propeller Controlling System > ACTUATOR ASSEMBLY REMOVED FROM AIRCRAFT DUE TO FEATHER STOP TAB BEING FOUND DISPLACED. AIRCRAFT BROUGHT IN FOR SCHEDULED MAINTENANCE. UPON INITIAL RECEIVING INSPECTION THE FEATHER STOP TAB S/N S0561 WAS FOUND TO BE BENT APPROXIMATELY 0.125 INCH. PITCHLOCK S - [SDR COMA9710048](https://openairdocs.org/sdr/COMA9710048.md): Apu · malfunctioned · Jan 19, 1997 · N244CA · Emb EMB120RT · Airborne Auxiliary Power Unit (APU) System > AUXILIARY POWER UNIT START CYCLE HUNG AT 45 DEGREES, START CYCLE WAS ABORTED, DISCHARGED AUXILIARY POWER UNIT FIRE EXTINGUISHER AFTER REPORT OF FIRE. INSPECTED AUXILIARY POWER UNIT AND COMPARTMENT, NO DEFECTS NOTED. DEFERRED AUXILIARY POWER UNIT AND AUXILIAR - [SDR COMA9710041](https://openairdocs.org/sdr/COMA9710041.md): Tracks · dirty · Jan 17, 1997 · N244CA · Emb EMB120RT · Trailing Edge Flaps > FLAP DISAGREEMENT AFTER TAKEOFF. CLEANED AND INSPECTED FLAP TRACKS AND ROLLERS, OPERATIONAL CHECK GOOD. - [SDR COMA9710035](https://openairdocs.org/sdr/COMA9710035.md): Bushing · failed · Jan 15, 1997 · N244CA · Emb EMB120RT · Rudder Control System > WHEN CAPTAIN'S FEET CONTACT RUDDER PEDALS, PEDAL ADJUSTMENT WILL NOT HOLD. REPLACED BUSHING IN PEDAL ADJUSTMENT ASSEMBLY. - [SDR COMA9710127](https://openairdocs.org/sdr/COMA9710127.md): Pitchlock Screw · malfunctioned · Jan 12, 1997 · N244CA · Emb EMB120RT · Propeller Feathering/Reversing > PROPELLER ASSEMBLY REMOVED FROM AIRCRAFT FOR BLADE AND HUB MAJOR INSPECTION. UPON INITIAL RECEIVING INSPECTION, THE FEATHER STOP TABS S/N S0455 WERE FOUND DISPLACED APPROXIMATELY 0.125 INCH. PITCHLOCK SCREW WAS REMOVED FROM ASSEMBLY AND RETURNED TO MANUFACTU - [SDR COMA9610333](https://openairdocs.org/sdr/COMA9610333.md): Eec · out of adjust · Nov 19, 1996 · N244CA · Emb EMB120RT · Fuel Control/Turbine Engines > ON INITIAL CLIMBOUT, THE NR 1 ENGINE TORQUE FLUCTUATED FROM 92 PERCENT TO 100 PERCENT. WHEN POWER WAS REDUCED THE FLUCTUATION WAS FROM 72 PERCENT TO 90 PERCENT, OPERATION BECAME NORMAL SHORTLY. TRANSFERRED TO DEFERRED LIST CAT C, MEL 73-21-1, EXPIRES 11-29-9 - [SDR COMA9610279](https://openairdocs.org/sdr/COMA9610279.md): Indication · malfunctioned · Sep 14, 1996 · N244CA · Emb EMB120RT · Landing Gear Position and Warning > WHEN LANDING GEAR SELECTED TO RETRACT, BOTH THE GREEN DOWN AND RED INTRANSIT LIGHTS WERE ON. COULD NOT DUPLICATE DISCREPANCY. OPERATIONAL AND FUNCTIONAL CHECKS OF LANDING GEAR RETRACTION SYSTEM WERE NORMAL. - [SDR COMA9610258](https://openairdocs.org/sdr/COMA9610258.md): Control Unit · malfunction · Aug 23, 1996 · N244CA · Emb EMB120RT · Trailing Edge Flap Control System > FLAP CONTROL FAULT WARNING DURING TAKEOFF. REPLACED FLAP CONTROL BOX. - [SDR COMA9610155](https://openairdocs.org/sdr/COMA9610155.md): Tcas · malfunction · May 24, 1996 · N244CA · Emb EMB120RT · Air Collision Avoidance System > PILOT'S RED HEADING FLAG LIGHT ON ALONG WITH FAILURE OF TCAS. REPLACED THE AHC-85. PART TOTAL CYCLES, 13,044. - [SDR COMA9610150](https://openairdocs.org/sdr/COMA9610150.md): Radar · malfunctioned · May 20, 1996 · N244CA · Emb EMB120RT · Weather Radar System > RADAR DISPLAY IS ERRATIC AND ERRONEOUS. PLACED WEATHER RADAR SYSTEM ON DEFERRED MAINTENANCE LIST. ACFT RETURNED TO SERVICE. - [SDR COMA9610140](https://openairdocs.org/sdr/COMA9610140.md): Door Latch · broken · May 6, 1996 · N244CA · Emb EMB120RT · Landing Gear Door Retract Section > RIGHT MLG OUTBOARD DOOR HANGING OPEN AND WILL NOT CLOSE. REPLACED BROKEN LATCH ASSY. - [SDR COMA9610139](https://openairdocs.org/sdr/COMA9610139.md): Retract Mech · malfunctioned · May 2, 1996 · N244CA · Emb EMB120RT · Landing Gear Retraction/Extension System > LANDING GEAR WILL NOT RETRACT. ALL GREEN DOWN INDICATORS AND ALL RED INTRANSIT INDICATORS ARE ILLUMINATED. REVERSED THE NLG UPLOCK PROXIMITY SENSORS AND DEFERRED SYSTEM PER EMB SNL 032-0015. - [SDR COMA9610118](https://openairdocs.org/sdr/COMA9610118.md): Line · chafed · Mar 29, 1996 · N244CA · Emb EMB120RT · Hydraulic System, Main > HYDRAULIC FLUID DRIPPING FROM LEFT ENGINE NACELLE. REPAIRED CHAFED HYDRAULIC PRESSURE LINE UNDER ENGINE FIRE DECK. - [SDR COMA9610107](https://openairdocs.org/sdr/COMA9610107.md): Leak Sensor · defective · Mar 18, 1996 · N244CA · Emb EMB120RT · Pneumatic Indicating System > LEFT DUCT LEAK WARNING ACTIVATED DURING FLIGHT. REPLACED DUCT LEAK SENSOR IN LT WING ROOT. - [SDR COMA9610031](https://openairdocs.org/sdr/COMA9610031.md): Door Seal · loose · Jan 18, 1996 · N244CA · Emb EMB120RT · Cargo/Baggage Doors > CABIN PRESSURIZATION FAILED DURING FLIGHT. REPLACED CARGO DOOR SEAL WHICH HAD COME LOOSE. - [SDR COMA9610014](https://openairdocs.org/sdr/COMA9610014.md): Wheel · damaged · Jan 11, 1996 · N244CA · Emb EMB120RT · Wheel/Ski/Float > MECHANIC REMOVED TIRE FROM A/C DUE TO TIRE WORN TO LIMITS. DURING INSPECTION IN WHEEL SHOP, FOUND DAMAGE TO SUB ASSY AND KEY INSERTS ANTICIPATE BRAKE FAILURE. SUB ASSY HAS BEEN REMOVED FROM SERVICE AND SENT TO BFG FOR FURTHER INSPECTION AND EVALUATION. - [SDR COMA9511964](https://openairdocs.org/sdr/COMA9511964.md): Controller · defective · Sep 16, 1995 · N244CA · Emb EMB120RT · Cabin Pressure Controller > AFTER TAKEOFF, CABIN PRESSURE WAS RISING OUT OF CONTROL, SWITCHED TO MANUAL CONTROL WITH SAME RESULTS. AIRCRAFT RETURNED TO BHM. REPLACED THE ELECTRONIC PRESSURE CONTROLLER. - [SDR COM11858](https://openairdocs.org/sdr/COM11858.md): Hmu · defective · Apr 12, 1995 · N244CA · Emb EMB120RT · Fuel Controlling System > LEFT ENGINE STARTS, BUT WILL NOT ACCELERATE BEYOND MIN FLOW. REPLACED THE ENGINE HMU. - [SDR COM11790](https://openairdocs.org/sdr/COM11790.md): Lead · broken · Feb 15, 1995 · N244CA · Emb EMB120RT · Propeller/Rotor Anti-Ice/De-Ice System > RT PROPELLER ANTI-ICE IS INOP. REPLACED BROKEN DE-ICE LEAD. - [SDR COM11779](https://openairdocs.org/sdr/COM11779.md): Sensor · defective · Feb 11, 1995 · N244CA · Emb EMB120RT · Landing Gear Position and Warning > LANDING GEAR CONTROL COULD NOT BE SELECTED TO UP UNTIL OVERRIDE RELEASE WAS USED. REPLACED THE LEFT MLG WEIGHT ON WHEELS PROXIMITY SENSOR. - [SDR COM11763](https://openairdocs.org/sdr/COM11763.md): Rollers · worn · Feb 5, 1995 · N244CA · Emb EMB120RT · Trailing Edge Flaps > FLAP DISAGREEMENT WARNING, WHEN FLAPS SELECTED UP AFTER TAKEOFF. REPLACED THE LEFT OUTBD FLAP ROLLERS. ## 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 = 'N244CA' AND deregistration_id = 'N244CA-2013-08-21' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N244CA-2013-08-21/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.