N965CA
Registered owner: HYANNIS AIR SERVICE INC, MA (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| HYANNIS AIR SERVICE INC. (HYIA) | Certificate holder | — | Matched by certificate designator |
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
ON APPROACH INTO DTW RECEIVED GEAR DISAGREE AFTER SELECTING GEAR DOWN, BOTH MLG FAILED TO EXTEND. EMERGENCY DECLARED, QRH FOLLOWED, A/C LANDED SAFELY AT DTW. REMOVED AND REPLACED MLG SELECTOR VALVE. OPS CHECK GOOD.
RIGHT I/B FLAP VANE LEADING EDGE FOUND TO HAVE CHAFE DAMAGE. REPLACED THE RIGHT I/B FLAP VANE LEADING EDGE IAW CRJ 200 SRM.
FS 559.0 BULKHEAD WEB FOUND TO BE CRACKED. REPAIRED IAW REO 601R-53-41-260 AND DEVIATION REO 601R-53-41-609.
FS 280 BULKHEAD WEB AT LBL 11 TO LBL 13 IS CORRODED. REPAIRED BULKHEAD WEB AT FS 280 PER SRM 53-11-19.
FS 280 FLOOR SUPPORT CROSSBEAM AT LBL 9 TO RBL 9 IS CORRODED. REPAIRED CROSSBEAM PER SRM 51-42-06.
LT UPPER WEB-ENG SUPPORT BEAM ASSEMBLY CRACKED. COMPLIED WITH REPAIR TO UPPER WEB-ENG SUPPORT. BEAM ASSEMBLY BETWEEN BL27.5 AND 36.2 PER REO601R-53-51-569. (S)
RT SIDE FUSELAGE FRAME DOUBLER AT FS 640.00 IS CRACKED. COMPLIED WITH MODIFICATION K601R360094 AT FS 640 IAW S/B 601R-53-061. (S)
PRESSURE FLOOR SKIN AT STA 460 BETWEEN LBL 9 AND RBL 9 IS CRACKED. REPAIRED PRESSURE FLOOR SKIN WEB AT FS 460.00 WITH TEMPORARY REPAIR PER REO 601R-53-41-103 REV D. (S)
PASSENGER DOOR CUTOUT AIRFRAME SIDE FWD LOWER CORNER EXISTING REPAIR IS DAMAGED. REPAIRED PASSENGER DOOR CUTOUT AIRFRAME SIDE LOWER FWD CORNER PER CRJ REO 601R-53-21-180 REV (A) AND SR99-5140-0001 SECTION 1. (S)
RT INTERNAL SKIN DOUBLER AT STA 640 IS CRACKED. FABRICATED PARTS AT STA 640 IAW CRJ REO 601R-53-61-506. (S)
LT INTERNAL SKIN DOUBLER AT STA 640 IS CRACKED. FABRICATED PARTS AT STA 640 IAW CRJ REO 601R-53-61-506. (S)
LT SIDE FUSELAGE FRAME DOUBLER AT FS 640.00 IS CRACKED. COMPLIED WITH MODIFICATION K601R36009-R AT FS 640 IAW S/B 601R-53-061. (S)
RT UPPER WEB-ENG SUPPORT BEAM ASSEMBLY CRACKED. COMPLIED WITH REPAIR TO UPPER WEB-ENG SUPPORT. BEAM ASSEMBLY BETWEEN BL 27.5 AND 36.2 PER REO601R-53-61-569. (S)
FLIGHT 9422. DURING LINE CHECK FOUND ROW 2-5 EMERGENCY FLOOR LIGHTS INOP. REMOVED AND REPLACED FLOOR EMERGENCY LIGHT STRIP. (A)
FLIGHT 5326 - EMERGENCY LIGHTS NOT WORKING FROM ROW 9 AFT. REPLACED NR 4 INVERTER. NO FURTHER DEFECTS.
FLIGHT 5027 - THE AFT EMERGENCY EXIT FLOOR LIGHTS FAILED TO TEST. DEFERRED PER MEL 33-51-01-6.
FLIGHT 5103- RECEIVED RIGHT COWL ANTI-ICE MESSAGE WHEN ANTI-ICE SELECTED ON. RETURNED TO JFK, LANDED WITHOUT INCIDENT. REPLACED PRESSURE RELIEF VALVE. NO FURTHER DEFECTS.
FLIGHT 5479 - FLOOR MOUNTED EMERGENCY STRIP BEHIND ROW 8A IS INOP. REPLACED BATTERY PACK NR 4. NO FURTHER DEFECTS.
FORWARD PRESSURE BULKHEAD CRACKED AT PARKING BRAKE CABLE. REPAIRED IAW REO 601R-53-11-563.
REAR PRESSURE BULKHEAD CRACKED AROUND LINTEL FITTING. PERFORMED PERMANENT REPAIR TO AFT PRESSURE BULKHEAD IAW REO 601R-53-11-563.
FLIGHT 4988 - DURING TAKEOFF ROLL THE RIGHT ENGINE ITT INDICATED 905C, ABORTED TAKEOFF AND RETURNED TO THE GATE. REPLACED THE RIGHT ENGINE ASSEMBLY.
FLIGHT 5389 - HYD PUMP 1B CIRCUIT BREAKER POPPED WHILE STARTING NR 1 ENGINE. RETURNED TO GATE. RESET BREAKER, PERFORMED OPS CHECK, NO FURTHER DEFECTS.
DURING FS 559 INSPECTION FOUND SEMI-BULKHEAD CRACKED AT RBL 18. STOP DRILLED CRACK AND INSTALLED DOUBLER IAW REO 601R-53-41-353.
FLIGHT 5342 - RECEIVED ANTI-ICE DUCT WARNING MESSAGE IN FLIGHT. FOLLOWED QRH AND DIVERTED TO GSO. FLIGHT LANDED WITHOUT INCIDENT. REPLACED THERMAL SWITCH WIRE AT LEFT WING STATION 250. NO FURTHER DEFECTS.
FLIGHT 5206 - RECEIVED A FLAP FAIL CAUTION MESSAGE DURING BGR APPROACH AT 30 DEGREE FLAP SETTING. 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.
FLIGHT 5206 - RECEIVED A FLAP FAIL CAUTION MESSAGE DURING BGR APPROACH AT 30 DEGREE FLAP SETTING. REPLACED THE LEFT INBOARD FLAP INBOARD ACTUATOR.
FLIGHT 5206 - RECEIVED A FLAP FAIL CAUTION MESSAGE DURING BGR APPROACH AT 30 DEGREE FLAP SETTING. REPLACED THE LEFT OUTBOARD FLAP INBOARD ACTUATOR.
FLIGHT 5323 - DURING CLIMBOUT RECEIVED AN ANTI-ICE DUCT CAUTION MESSAGE, FLIGHT RETURNED TO CVG. REPAIRED CHAFED WIRING ON THE LEFT WING LEADING EDGE AT STA 330.25 AND 377.40.
DURING INSPECTION OF THE ENGINE SUPPORT BEAM IAW EO 53-021 (AD 2004-10-03) FOUND CRACK AT LOCATION FS 640, LBL 9.0, WL 119.12 (UPPER BOX BEAM SKIN).PERFORMED REPAIR IAW REO 601R-53-61-345.
FLIGHT 5063 - DURING CLIMBOUT OF GSO RECEIVED A CABIN DOOR OUTER HANDLE CAUTION MESSAGE, FLIGHT RETURNED TO THE FIELD. RE-RIGGED THE CABIN DOOR PRESSURE VALVE VENT FLAP.
FLIGHT 5063 - AFTER TAKEOFF FROM GSO RECEIVED A CABIN DOOR OUTER HANDLE CAUTION MESSAGE, FLIGHT RETURNED TO THE FIELD. DEFERRED THE CABIN DOOR INDICATION PER MEL 52-70-01-1.
FLIGHT 5285 - RECEIVED A FLAP FAIL CAUTION MESSAGE AT ZERO DEGREES DURING TAXI AT DCA. REPLACED THE FLAP ELECTRONIC CONTROL UNIT.
FLIGHT 5719 - FLAP FAIL MESSAGE AT GATE. COMPLIED WITH AD 98-20-01 FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (B) 1, 2, 3 (A, B, C AND E). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES.
FLIGHT 5450 - FLAP FAIL CAUTION MESSAGE. FLAPS WILL NOT COME OUT OF ZERO POSITION. FOUND LEFT SIDE FLAP SYSTEM OUT OF RIG. MECHANICALLY AND ELECTRICALLY RIGGED LEFT SIDE FLAP SYSTEM.
FLIGHT 5049 - FLAP FAIL MESSAGE ON GROUND AT 0 DEGREES. COMPLIED WITH AD 98-20-01 FLAP CAUTION MESSAGE FIRST EVENT, MAINTENANCE ACTION, PARAGRAPH (B) 1, 2, 3, (A, B, C AND E). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES.
FLIGHT 5381 - DURING PUSHBACK RECEIVED A FLAP FAIL CAUTION MESSAGE AT 20 DEGREES, FLIGHT RETURNED TO THE GATE. COMPLIED WITH AD 98-20-01 FLAP CAUTION MESSAGE FIRST EVENT MAINTENANCE ACTION, PARAGRAPH (B) 1, 2, 3, (A, B, C AND E). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES.
FLIGHT 5701 - EN ROUTE BTV-ATL RECEIVED A CABIN DOOR LATCH CAUTION MESSAGE, FLIGHT DIVERTED TO SYR. ADJUSTED ROD-END OF CABIN DOOR LATCH ROLLER ASSEMBLY.
FLIGHT 5093 - DURING CLIMB-OUT OF EVV RECEIVED A LEFT ENGINE COWL A/ICE CAUTION MESSAGE, FLIGHT RETURNED TO EVV. REPLACED THE LEFT ENGINE COWL ANTI ICE PRESSURE SWITCH.
FLIGHT 5701- PILOT'S WINDSHIELD SHATTERED. REPLACED WINDSHIELD.
FLIGHT 5850 - RECEIVED A FLAP FAIL CAUTION MESSAGE AFTER LANDING WHEN FLAPS WERE SELECTED TO 20 DEGREES. COMPLIED WITH AD 98-20-01 FLAP CAUTION MESSAGE "FIRST EVENT" MAINTENANCE ACTION PARAGRAPH (B) 1,2,3 (A,B,C AND E). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES.
FLIGHT 5565 - EMERGENCY FLOOR LIGHTING INOPERATIVE FROM ROWS 2 THROUGH 5. CLEANED CONTACTORS ON EMERGENCY FLOOR TRACK LIGHT STRIP.
FLIGHT 5387 - EMERGENCY LIGHTS ROW 1-5 INOPERABLE. RESECURED LIGHT STRIP.
FLIGHT 5858 - FLAPS FAIL CAUTION. ADJUSTED THE RIGGING OF THE RT BPSU.
FLIGHT 5105 - LT 14TH STAGE DUCT WARNING. REPLACED THE PYLON DUCT LEAK SENSING ELEMENT.
FS 280 HAS CORROSION ON WEB AT BL AFT SIDE AND CRACKS LOCATED OUTBOARD OF LBL/RBL 9. REPAIRED IAW REO 601R-53-11-136.
RT WING PLANK AT VS 148 IS CRACKED. IAW EO 57-020.
CARGO CAP WEB AT LIGHTING HOLE IB SIDE CRACKED FROM EXCESSIVE STRESS.IAW SRM 51-42-06, 51-42-13.
CARGO FLOOR CAP CRACKED. IAW SRM 51-42-06, 51-42-13, 51-42-21 AND 51-42-26.
FS 574 LEFT HAND SIDE HAS TWO CORRODED FASTENERS AT 8 POSITION ABOVE FLOOR. REPAIRED IAW REO 601R-53-61-1135.
FS 280 HAS CORROSION ON WEB AT CBP WALLS. REPAIRED IAW REO 601R-53-11-584.
FLIGHT 5405 RUDDER FLUTTER DURING FLIGHT. REPLACED THE YAW DAMPNER ACTUATOR.
FLIGHT 5005 LEFT THRUST REVERSER UNLOCKED CAUTION. SECURED AND DEFERRED MAINT ON T/R PER MEL.
FLIGHT 5244 RT ENGINE, HIGH OIL TEMP. FOUND OIL SYSTEM OVERSERVICED - DRAINED OIL TO NORMAL LEVEL.
FLIGHT 5704 GEAR DISAGREE WARNING WHEN GEAR EXTENDED. REPLACED HYDRAULIC PUMP 3A.
FLIGHT 5843 STAB TRIM, MACH TRIM AND AUTO PILOT NOSE DOWN CAUTION MESSAGE. REPLACED THE HSTA.
FLIGHT 5554 LT AOA, LT STATIC, LT PITOT HEAT CAUTION.RESET C/B, COULD NOT DUPLICATE PROBLEM, SYSTEM TEST NORMAL.
FLIGHT 5748 ONE SEGMENT OF EMERGENCY FLOOR LIGHTING IS INOP. REPAIRED WIRE SPLICE AT ROW 8.
FLIGHT 5789 FLAPS FAIL MESSAGE WHEN SELECTED 30 DEGREES.RESET FLAP SYSTEM AND DEFERRED MAINT. PER AD 98-20-01.
FLIGHT 5789 FLAS FAIL MESSAGE WHEN SELECTED TO 30 DEGREES.RESET FLAP SYSTEM AND DEFERRED MAINT. PER AD 98-20-01.
FLIGHT 9471 R/H ENGINE HIGH OIL TEMP.REPLACED THE ENGINE LUBE PUMP BYPASS CHECK VALVE.
FLAPS FAILED CAUTION AT 30 DEGREES.REPLACED THE FECU.
FLIGHT 5160 FLAPS FAILED AT 45 DEGREES DURING LANDING.RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01.
FLIGHT 5124 DURING BLEED AIR TRANSFER, COCKPIT FILLED WITH SMOKE AFTER LANDING WHILE TAXIING TO THE GATE.SECURED R/H COOLING PACK AND DEFERRED MAINT PER MEL.
CRACK FOUND ON L/H LOWER WING PLANK AT PANEL 550BB.REPAIRED I/A/W 601R-57-21-030.
CRACK FOUND ON R/H LOWER WING PLANK AT PANEL 650BB.REPAIRED I/A/W 601R-57-21-030.
CRACK FOUND ON L/H LOWER WING PLANK AT PANEL 550AB.REPAIRED I/A/W 601R-57-21-030.
CRACK FOUND ON R/H LOWER WING PLANK AT PANEL 650DB.REPAIRED I/A/W 601R-57-21-030.
CRACK FOUND ON R/H LOWER WING PLANK AT PANEL 650 AB.REPAIRED I/A/W 601R-57-21-030.
FLIGHT 5773 LOUD SQUEAL FROM SERVICE DOOR AREA. CABIN DOOR WITNESS MARKS NOT ALIGNED.FOUND STAIR HANDRAIL NOT STOWED PROPERLY DUE TO BENT PIN RETAINING BRACKET. REPOSITIONED BRACKET.
FLIGHT - R/H WING OVERHEAT FLOW LINE IS MISSING DURING WING OVERHEAT TEST.REPLACED R/H WING OVERHEAT SENSOR.
FLIGHT #5650. DURING DESCENT INTO SRQ RECEIVED A FLAP FAIL CAUTION MESSAGE WITH FLAPS AT 20 DEGREES.REPLACED THE BRAKE AND POSITIONING SENSING UNIT.
FLIGHT #5073. DURING APPROACH INTO TLH RECEIVED A FLAP FAIL CAUTION MESSAGE WITH FLAPS AT ZERO DEGREES.REPLACED THE FLAP ELECTRONIC CONTROL UNIT.
FLIGHT #5073. DURING APPROACH INTO TLH RECEIVED A FLAP FAIL CAUTION MESSAGE WITH FLAPS AT ZERO DEGREES.REPLACED THE POWER DRIVE UNIT.
DURING APPROACH INTO CVG, THE FLAP CAUTION MESSAGE ACTIVATED WHEN FLAPS WERE SELECTED TO 45 DEGREES.REPLACED THE FLAP ELECTRONIC CONROL UNIT.
CRACKS FOUND IN ENGINE SUPPORT BEAM LOWER WEB BETWEEN F.S. 640.0 - 625.30 ON LEFT HAND AND RIGHT HAND SIDES.REPAIRED CRACKS I/A/W REO 601R-53-61-366 REV B AND WVAC E.O.'S 601R-53-2560-1A AND 601R-53-2545B.
LEFT HAND MLB AFT TRUNION BUSHING MIGRATED .030.S/B 601R-32-054 MAIN LANDING GEAR SYSTEM - INSPECTION REPLACEMENT OF THE LEFT HAND AFT TRUNNION BUSHING INSPECTION AND RECERTIFICATION INCORPORATED.
RIGHT HAND WING INBOARD FLAP INBOARD LEADING EDGE VANE CAP IS CHAFED .020. REMOVED CHAFED VANE CAP AND INSTALLED NEW SERVICEABLE VANE CAP IAW WVAC EO 601R-57-2009.
RIGHT HAND SIDE FRAME AND DOUBLER AT F.S. 718.0 BETWEEN STR'S 11 AND 12 IS CRACKED.REPAIRED CRACKED 718 FRAME AND DOUBLER IAW REO 601R-53-61-193 REV A.
PAX DOOR SKIN REPAIR AT F.S. 310.00 IS DAMAGED. REPAIRED PAX DOOR SKIN REPAIR AT 310.00 IAW WVAC EO 601R-53-2006.
STALL FAIL CAUTION MESSAGE DURING TAKE OFF. RESET STALL COMPUTER.
STALL FAIL AND CONFIG SPOILER WARNING DURING T/O. RESET STALL COMPUTER.
STALL FAIL AND CONFIG WARNING DURING TAKEOFF. REPLACED THE AOA TRANSDUCER.
DURING LANDING GEAR EXTENSION, NLG REMAINED UP. COULD NOT DUPLICATE. ALL EXTENSION AND RETRACTION CHECKS NORMAL.
WHEEL ASSEMBLY WAS REMOVED FROM AIRCRAFT FOR TIRE CHANGE. FOUND WHEEL WAS CRACKED AT SPOKE AREA. MARKED LOT NR 1550.
EMERGENCY FLOOD LIGHT AT CABIN DOOR IS INOPERABLE. SECURED LOOSE WIRE AT LIGHT.
STALL FAIL MESSAGE. COULD NOT DUPLICATE. SYSTEM CHECK NORMAL.
CO-PILOTS CONTROL YOKE HAS A SLIPPING FEEL WHEN MOVED LEFT OR RIGHT. RETORQUED THE CONTROL YOKE NUT TO M/M SPECIFICATIONS.
FLAPS FAILED MESSAGE. REPLACED THE LEFT WING NR 3 AND NR 4 FLAP ACTUATORS.
FLAPS FAIL CAUTION MESSAGE. REPLACED THE RIGHT BPSU.
FLAPS FAILED AT 20 DEGREES DURING APPROACH. RESET FLAP SYSTEM PER AD 98-20-01.
RIGHT HAND THRUST REVERSER UNLOCK MESSAGE. DEACTIVATED AND DEFERRED THE RIGHT HAND THRUST REVERSER.
FLAPS FAILED AT 8 DEGREES DURING APPROACH. RESET FLAP SYSTEM PER AD 98-20-01.
EMERGENCY LIGHT IN CEILING ABOVE ROW 5 IS INOPERABLE. REMOVED AND REPLACED BULK.
FLAPS FAILED AFTER LANDING. RESET FLAP SYSTEM PER AD 98-20-01.
FS 718, STR 11 RHS AFT DOUBLER CRACKED. REPAIRED CRACKED DOUBLER AT FS 718.0 STR 11 RHS IAW WVAC EO 601R-53-0099.
FS 718.0, STRI 11 LHS FRAME FLANGE CRACKED AND AFT SIDE OF FRAME DOUBLER CRACKED. REPAIRED CRACKED FRAME FLANGE AND CRACKED DOUBLER AT FS 718.0 STRI 11 LHS IAW WVAC EO 601R-53-0098 AND WVAC EO 601R-53-0100A.
FS 718 STR 11 RIGHT AND LEFT SIDE DOUBLERS CRACKED. ALSO, FRAME AT FS 718 LT SIDE HAS 2 INCH CRACK. REPAIRED FRAME AT FS 718 LT SIDE AND DOUBLERS ON RT AND LT SIDE IAW WVAC EO 601R-53-0098, 601R-53-0099 AND 601R-53-0100A.
DURING INCOMING INSPECTION OF AIRCRAFT FOR EXTERNAL DAMAGE NOTICED THAT FUSELAGE SKIN WAS NICKED AT FS 310 STR 16 BY DOOR LATCH PIN. SKIN WAS BLENDED IAW BOMBARDIER REO 601R-53-21-160.
CVG - FLT 9600 - RIGHT ENGINE OIL PRESSURE FLUCTUATING BETWEEN 35 PSI AND 55 PSI. SERVICED OIL TANK TO PROPER LEVEL. (X)
FLOOR EMERGENCY EXIT LIGHTS WILL NOT COME ON. REPLACED BATTERY AT NR 3 POSITION.
FLAPS FAILED AFTER LANDING. REPLACED THE FECU.
FLAPS FAILED AFTER LANDING. REPLACED THE FECU.
EMERGENCY FLOOR LIGHTING INOPERABLE FROM ROW 9 TO ROW 13. CONNECTED LOOSE WIRING, SYSTEM OPERATION NORMAL.
EMERGENCY FLOOR LIGHTING AFT OF ROW 8 IS INOPERABLE. DISCONNECTED AND RECONNECTED LIGHT STRIP SYSTEM, OPERATION NORMAL.
EMERGENCY FLOOR PATH LIGHTING AFT OF ROW 8 IS INOPERABLE. RECONNECTED STRIP LIGHTING, SYSTEM TEST NORMAL.
FLAPS FAILED AT 24 DEGREES DURING APPROACH. REPLACED THE LEFT HAND BPSU.
SEVERAL EMERGENCY FLOOR LIGHTS ARE INOP. REPAIRED BROKEN WIRE AT ROW 5.
EMERGENCY EXIT SIGN AT GALLEY SERVICE DOOR IS BROKEN. REPLACED EXIT SIGN.
FLAPS FAILED WHEN SELECTED FOR LANDING APPROACH. REPLACED THE LEFT HAND WING NR 5 FLAP FLEX DRIVE CABLE. CABLE WAS CORRODED AND BROKEN.
SOME OF THE EMERGENCY FLOOR LIGHTS ARE INOP. SECURED LOOSE WIRING CONNECTOR AT TRACK LIGHTING.
FLIGHT SPOILERS CAUTION MESSAGE. REPLACED THE NR 2 SECU.
DURING TAKEOFF, CONFIG WARNING, SPOILERONS CAUTION MESSAGE. REPLACED THE NR 1 SECU.
AFTER LIFT OFF, 7 UNITS OF ROLL TRIM NEEDED TO REMAIN LEVEL. FLAPS FAILED DURING RETRACTION. THE LEFT OUTBOARD FLAP, INBOARD ACTUATOR FAILED CAUSING STRUCTURAL DAMAGE AND DEFORMATION OF THE FLAP ASSY. REPLACED ACTUATOR AND FLAP ASSY.
LEFT AND RIGHT EXTERIOR FORWARD EMERGENCY LIGHTS INOPERATIVE. DEFERRED FORWARD EXTERIOR EMERGENCY LIGHTS IN ACCORDANCE WITH MEL 33-51-2.
LANDING GEAR DISAGREE WARNING. NLG DID NOT RETRACT. REPLACED THE NLG WEIGHT ON WHEELS PROXIMITY SENSOR.
RT ENGINE FOD DURING TAKEOFF. ITT EXCEEDED LIMITS. REPLACED RIGHT HAND ENGINE.
NEW INOP MESSAGE DURING FLIGHT. STEERING INOP ON GROUND. REPLACED THE ELECTRO HYDRAULIC SERVO VALVE.
SPOILERON FAULT MESSAGE. REPLACED NR 1 SECU. PART TOTAL CYCLES, 3,204.
STALL FAIL MESSAGE ON EICAS. RESET THE STALL WARNING COMPUTER AND AIRCRAFT RETURNED TO SERVICE.