N254CA

Part: SIGN — BROKEN (ROW 5)

EMERGENCY EXIT SIGN AT ROW 5 IS BROKEN. REPLACED SIGN ASSY.

Part: BATTERY — DISCHARGED (CABIN)

AFT SECTION OF EMERGENCY LIGHTING IS INOPERABLE. REPLACED EMERGENCY BATTERY.

Part: SIGN — BROKEN (ROW 18)

EMERGENCY EXIT SIGN, ROW 8 IS BROKEN. REPLACED EXIT SIGN.

Part: PIN — NOT REMOVED (NLG)

NLG WILL NOT RETRACT. REMOVED THE DOWN LOCK SAFETY PIN FROM NLG.

Part: WIRE — BROKEN (CABIN)

FLOOR EMERGENCY LIGHT AT ENTRANCE DOES NOT WORK. REPAIRED BROKEN WIRE AT FLOOR LIGHT.

Part: LAMP — FAILED (CABIN)

FORWARD EMERGENCY LIGHT WILL NOT ILLUMINATE. REPLACED LAMP.

Part: BATTERY — DISCHARGED (CABIN)

EMERGENCY LIGHTS BY CABIN DOOR ARE INOPERABLE. REPLACED EMERGENCY BATTERY.

Part: SIGN — BROKEN (CABIN)

EMERGENCY EXIT SIGN AT ROW 8 BROKEN. REPLACED EXIT SIGN.

Part: FITTING — WORN (LT NACELLE)

DURING LEFT ENGINE CHANGE, FOUND THE INBOARD, FORWARD SUPPORT ROD, FORWARD ATTACH BEARING TO HAVE EXCESSIVE PLAY. REPLACED INBOARD, FORWARD NACELLE SUPPORT ROD FORWARD FITTING.

Part: FITTING — WORN (LT NACELLE)

DURING LEFT ENGINE CHANGE, FOUND THE MOST AFT, INBOARD NACELLE SUPPORT ROD ATTACH BEARING TO HAVE EXCESSIVE PLAY. REPLACED THE FITTING.

Part: FITTING — WORN (LT NACELLE)

DURING LEFT ENGINE CHANGE, FOUND THE SECOND FROM AFT NACELLE SUPPORT ROD ATTACH FITTING ON THE INBOARD SIDE TO HAVE EXCESSIVE PLAY AT THE BEARING. REPLACED THE FITTING.

Part: FITTING — WORN (LT NACELLE)

DURING LEFT ENGINE CHANGE, FOUND PLAY IN ONE BEARING OF THE INBOARD NACELLE SUPPORT ROD CLUSTER FITTING. REPLACED INBOARD NACELLE SUPPORT ROD CLUSTER FITTING.

Part: SIGN — BROKEN (CABIN)

EMERGENCY EXIT SIGN AT SEAT 5A IS BROKEN. REPLACED EXIT SIGN.

Part: FLAP TRACKS — ICE CONTAM (TE FLAPS)

FLAP DISAGREEMENT FAULT. CLEANED ICE BUILD UP FROM FLAP TRACKS.

Part: ROLLERS — WORN (LT TE FLAP)

FLAP DISAGREEMENT WARNING AFTER TAKEOFF. REPLACED WORN ROLLERS ON LEFT HAND OUTBOARD FLAP.

Part: SKIN — PUNCTURED (FUSELAGE)

AIRCRAFT RECEIVED DAMAGE FROM BAGGAGE CART. DAMAGE CONSISTS OF APPROXIMATELY 2 INCH LONG PUNCTURE AND DENT BETWEEN STRINGERS 16L AND 17L, JUST AFT OF FRAME 45. THE AIRCRAFT WAS FERRIED TO MCO FOR REPAIR. THE FUSELAGE SKIN WAS REPAIRED PER APPROVED EMBRAER REPAIR SCHEME SST1071/97 AND JRM 53-00-01, FIGURE 202.

Part: DE-ICE VALVE — LEAKING (WING)

RT BLEED AIR DUCT LEAK WARNING. REPLACED A LEAKING DE-ICE PRESSURE REGULATOR VALVE.

Part: FLOORBEAM — CORRODED (CABIN)

ON 4C TASK 5320-151-01I, THE CABIN FLOOR SUPPORT LT CROSSBEAM AT FRAME 33 WAS FOUND CORRODED. REPLACED PER SRM STANDARD PRACTICES.

Part: ANGLE — CORRODED (EXIT DOORWAY)

ON 4C TASK 5320-152-01I, THE LOWER ANGLE AT THE AFT EMERGENCY EXIT DOOR CUTOUT, WAS FOUND CORRODED. REPLACED PER SRM STANDARD PRACTICES.

Part: FLOORBEAM — CORRODED (CABIN)

ON 4C TASK 5320-152-01I, THE CABIN FLOOR SUPPORT RT CROSSBEAM AT FRAME 33 WAS FOUND CORRODED. REPLACED PER SRM STANDARD PRACTICES.

Part: SEAL — WORN (RT BLEED DUCT)

RT DUCT LEAK WARNING CAME ON AFTER TAKEOFF. REPLACED O-RING SEALS ON THE RT ENGINE BLEED AIR SUPPLY DUCT.

Part: HYDRAULIC PUMP — FAILED (LT ENGINE)

THE LEFT ENGINE HYDRAULIC PUMP FAILED DURING FLIGHT. REPLACED FAILED LEFT ENGINE HYDRAULIC PUMP.

Part: PRESS REGULATOR — LEAKING (RT DE ICE SYST)

RIGHT BLEED AIR DUCT LEAK WARNING CAME ON AFTER TAKEOFF. REPLACED THE RT DEICE SYSTEM PRESSURE REGULATOR.

Part: CONNECTOR — LOOSE (RT MLG)

LT ANTI-SKID INOP WARNING DURING TAXI. SECURED LOOSE WIRING CONNECTOR AT THE RT ANTI-SKID TRANSDUCER.

Part: ROLLER — MALFUNCTIONED (LT TE FLAP)

FLAP DISAGREEMENT AFTER TAKEOFF. REPLACED LEFT OUTBOARD FLAP ROLLERS, 4 EACH. OPERATIONAL CHECK GOOD.

Part: TRACKS — DIRTY (TE FLAPS)

FLAP DISAGREEMENT ON TAKEOFF, WOULD NOT RETRACT FULLY. INSPECTED FLAP SYSTEM, CLEANED TRACKS AND OPERATIONAL CHECK GOOD.

Part: STEERING — FAILED (NLG)

NOSE WHEEL STEERING FAILED. AIRCRAFT DEPARTED RUNWAY. COULD NOT DUPLICATE DISCREPANCY. WEIGHT ON WHEELS PROXIMITY SENSORS WERE REPLACED FOR TROUBLESHOOTING. AIRCRAFT FLIGHT CHECK SATISFACTORY.

Part: POTENTIOMETER — OUT OF ADJUST (NLG STEERING)

DURING TAXI AIRCRAFT PULLS HARD TO THE RIGHT. ADJUSTED NWS FEEDBACK POTENTIOMETER. TAXI CHECK SATISFACTORY.

Part: BATTERY — DISCHARGED (CABIN)

EMERGENCY FLOOR LIGHTING FORWARD OF ROW 4 IS INOPERATIVE. REPLACED EMERGENCY BATTERY. PART TOTAL CYCLES, 11,712.

Part: PUMP — LEAKING (RT HYD SYST)

BLUE (RT) HYDRAULIC SYSTEM LOW FLUID LEVEL WARNING DURING APPROACH. QUANTITY GAUGE INDICATED EMPTY. REPLACED THE RT ENGINE DRIVEN HYDRAULIC PUMP DUE TO INTERNAL LEAKAGE TO CASE DRAIN. PART TOTAL CYCLES, 5,227.

Part: SEPARATOR — CRACKED (LT WING)

LT BLEED AIR DUCT LEAK WARNING CAME ON AFTER TAKEOFF. REPLACED THE LT BLEED AIR WATER SEPARATOR.

Part: ANGLE — CRACKED (LT WING)

LEFT WING ROOT FAIRING ATTACH ANGLE IS CRACKED. REPLACED FAIRING ATTACH ANGLE.

Part: POTENTIOMETER — MALFUNCTION (NLG STEERING)

NOSE WHEEL STEERING DISCONNECT TEST DID NOT FUNCTION. REPLACED THE N.W.S. FEED-BACK POTENTIOMETER.

Part: ACTUATOR — DEFECTIVE (RT TE FLAP)

FLAP DISAGREEMENT WARNING WHEN FLAPS SELECTED UP AFTER TAKEOFF. REPLACED THE RT OUTBD FLAP ACTUATOR.

Part: RETRACT MECH — MALFUNCTIONED (TE FLAPS)

AFTER TAKEOFF, FLAP DISAGREEMENT WHEN FLAPS SELECTED UP. COULD NOT DUPLICATE. INSPECTED FLAP SYSTEM AND NO DEFECTS NOTED.

Part: ROLLER — WORN (FLAPS)

FLAP DISAGREEMENT WARNING WHEN FLAPS SELECTED UP. REPLACED THE LT AND RT OUTBD FLAP SECTIONS ROLLERS.

Part: TRACKS — DIRTY (TE FLAPS)

FLAP DISAGREEMENT WARNING AFTER TAKEOFF. CLEANED ICE AND SLUSH FROM OUTBD FLAP TRACKS. ACFT RETURNED TO SERVICE.

Part: PCU — DEFECTIVE (RT ENGINE)

RT ENGINE NP DROPPED TO 50 PERCENT; TORQUE CLIMBED TO 125 PERCENT. REPLACED THE PITCH CONTROL UNIT.

Part: WARNING LIGHT — ILLUMINATED (CARGO DOOR)

CARGO DOOR WARNING LIGHT ILLUMINATED DURING FLIGHT. DEFERRED DOOR WARNING SYSTEM AND AIRCRAFT CONTINUED SERVICE.

Part: ROLLER — WORN (TE FLAPS)

FLAP DISAGREEMENT WARNING WHEN FLAPS RETRACTED AFTER TAKEOFF. REPLACED THE OUTBD FLAP ROLLERS.

Part: SUPPORT — CRACKED (LT/RT WINGS)

THE FOLLOWING P/N WING SKIN SUPPORTS WERE FOUND CRACKED DURING INSPECTION TASK NR 5720-551/651-01I AT RIBS NR 15 AND NR 16. THE SKIN SUPPORTS WERE REPAIRED IAW AERODESIGN E.O. 1327-2. P/N: 120-17056-007, 3 EA; 120-17056-015, 4 EA; 120-17056-013, 1 EA; 120-17056-011, 1 EA; 120-17056-019, 1 EA; 120-17056-017, 1 EA; 120-17057-005, 1 EA.

Part: FUEL HEATER — LEAKING (LT ENGINE)

LEFT ENGINE FUEL TO OIL HEAT EXCHANGER IS LEAKING FUEL. REPLACED HEAT EXCHANGER.

Part: SWITCH — OUT OF ADJUST (RT WING)

SERVICE DOOR WARNING LIGHT ILLUMINATED. ADJUSTED FUEL SERVICE DOOR MICROSWITCH.