N946CA

Part: PSEU — MALFUNCTIONED (E/E BAY) · airframe 13,476 hrs · 13,400 cycles

N.L.G. DID NOT RETRACT. REPLACED THE PSEU.

Part: COMPUTER — MALFUNCTIONED (STALL WARNING) · airframe 13,321 hrs · 13,230 cycles

STALL FAIL CAUTION DURING TAKE OFF. RESET THE STALL COMPUTER.

Part: ENGINE — FAILED (LEFT) · airframe 12,882 hrs · 12,777 cycles

LEFT ENGINE FAILED DURING CLIMB. TURBINE SEIZED. REMOVED AND REPLACED LEFT ENGINE.

Part: SEAL — TORN (CABIN DOOR) · airframe 12,678 hrs · 12,560 cycles

LOUD SQUEAL FROM CABIN DOOR. REPLACED DOOR SEAL.

Part: LIGHT — INOPERATIVE (ROW 4) · airframe 12,281 hrs · 12,157 cycles

OVERHEAD EMERGENCY LIGHT AT ROW 4 IS INOPERABLE. DEFERRED MAINT PER MEL.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 12,111 hrs · 11,979 cycles

VERTICAL J-ANGLE INSIDE CBP1 FS 280 LEFT HAND SIDE IS CRACKED. REMOVED DAMAGED ANGLE, FABRICATED NEW ANGLE AND INSTALLED IAW WVAC EO 601R-53-1363.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 12,111 hrs · 11,979 cycles

TOP OF FLOORBEAM CAPS LBL 27, LBL 9, RBL 27, RBL 9 AT FS 280 TO 409 CORRODED BEYOND LIMITS. INSTALLED NEW FLOORBEAM CAPS (P/N 601R31113-67) FROM FS 280 TO FS 409 IAW REO 601R-53-00-027 REV N/C DATED 4 NOV 97.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 12,111 hrs · 11,979 cycles

THE PASSENGER DOOR THRESHOLD ANGLE IS CORRODED AS WELL AS THE ANGLES FORWARD AND AFT OF THE MAIN ANGLE. PERFORMED A MAJOR REPAIR BY REPLACING CORRODED ANGLES BETWEEN FS 310 - FS 349 LBL 42 IAW WVAC EO 601R-53-1361.

Part: CLIP — CRACKED (FUSELAGE) · airframe 12,111 hrs · 11,979 cycles

BOTH CLIPS AT FS 280 - LBL 9 ARE CRACKED. REMOVED AND REPLACED CLIPS IAW WVAC EO 601R-53-1364.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 12,111 hrs · 11,979 cycles

FWD J-CHANNEL (P/N 600-34017-351) AT FS 280 CORRODED. REMOVED AND REPLACED FWD J-CHANNEL AT FS 280 IAW WVAC EO 601R-53-1367.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 12,111 hrs · 11,979 cycles

FOUND FLOOR MEMBER (P/N 600-34017-17) AT FS 280.0 TO BE CRACKED L/1 - .75 INCH TO THE RIGHT OF FLOOR SUPPORT RBL 9.0. REPAIRED FLOOR MEMBER AT FS 280.0 AND RBL 9.0 IAW WVAC EO 601R-53-1366.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 12,111 hrs · 11,979 cycles

ANGLE STIFFENER LOCATED AT THE FORWARD SIDE OF FS 280 AT LBL 9.0 WAS FOUND CRACKED. FABRICATED AND INSTALLED NEW ANGLE IAW WVAC EO 601R-53-1363.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 12,111 hrs · 11,979 cycles

SERVICE DOOR ANGLE IS CORRODED (P/N 601R38303-105). REMOVED AND REPLACED CORRODED THRESHOLD ANGLE IAW WVAC EO 601R-53-1360.

Part: CLIP — CRACKED (FUSELAGE) · airframe 12,111 hrs · 11,979 cycles

FOUND CLIPS AT FS 280 RBL 9 (P/N 601R31113-58) TO BE CRACKED. INSTALLED NEW CLIPS IAW WVAC EO 601R-53-1364.

Part: SKIN — DENTED (FUSELAGE) · airframe 12,111 hrs · 11,979 cycles

THE FUSELAGE SKIN HAS MULTIPLE DENTS BETWEEN FS 574.0 - FS 621.0 BETWEEN STR 29-23 LHS. PERFORMED A MAJOR REPAIR TO DENTED SKIN BETWEEN FS 574.0 - FS 621.0 STRI 20-23 LHS IAW WVAC EO 601R-53-1357.

Part: SEAL BRACKET — DENTED (PAX DOOR) · airframe 12,111 hrs · 11,979 cycles

SEAL STRIKER ON PASSENGER DOOR AT FS 310.00 AND 349.00 DAMAGED CONTACT WITH DOOR PINS. REPAIRED IAW REO 601R-52-11-008 REPAIR A.

Part: PLATE — CORRODED (FUSELAGE) · airframe 12,111 hrs · 11,979 cycles

FOUND TOP PLATES AT FS 349.00 TO BE CORRODED BEYOND LIMITS. REMOVED AND REPLACED CORRODED TOP PLATES IAW WVAC EO 601R-53-1362 A.

Part: DRAG BRACE — FAILED (NLG)

GEAR DISAGREE WARNING DURING TAKEOFF. REPLACED THE NLG DRAG BRACE ASSY.

Part: CONTROLLER — FAILED (E/E BAY)

LEFT HAND PITOT, STATIC AND AOA HEAT CAUTION MESSAGE. REPLACED THE LEFT ADSHC.

Part: WINDSHIELD — CRACKED (RT COCKPIT)

RIGHT WINDSHIELD CRACKED DURING FLIGHT AT 31,000 FEET, DESTINATION IAW. AIRCRAFT DIVERTED TO LIT. REPLACED RIGHT WINDSHIELD.

Part: WARNING — ACTIVATED (PAX DOOR)

CABIN DOOR LATCH MESSAGE ON EICAS. DEFERRED DOOR WARNING SYSTEM PER MEL.

Part: EXHAUST FRAME — CRACKED (RT ENGINE)

RIGHT HAND LOW OIL PRESSURE. REPLACED CRACKED EXHAUST FRAME.

Part: SMOKE DETECTOR — DAMAGED (CARGO COMPT)

CARGO SMOKE WARNING. REPLACED DAMAGED SMOKE DETECTOR IN CARGO COMPARTMENT.

Part: SENSOR LOOP — CHAFED (RT PYLON)

A 14TH STAGE BLEED AIR DUCT LEAK MESSAGE IFSD. REPLACED THE RT PYLON LEAK SENSOR LOOP.

Part: RETRACT MECH — MALFUNCTIONED (TE FLAPS)

FLAPS FAILED. RESET FLAP SYSTEM, AIRCRAFT RETURNED TO SERVICE.

Part: CLAMP — BROKEN (APU EXHAUST)

APU EXHAUST FINGER CLAMP HAS BROKEN AND CHAFED FINGERS. REPLACED CLAMP.

Part: SUPPORT — CRACKED (CARGO COMPT)

CARGO DOOR SLIDE BRACKET SUPPORT CRACKED. REPLACED SUPPORT.

Part: DAMPENER — LEAKING (LT ELEVATOR)

LEFT INBOARD ELEVATOR FLUTTER DAMPENER LEAKING. REPLACED FLUTTER DAMPENER.

Part: FRAME — CRACKED (BS 718)

FS 718 AND STR 11 (RHS), DISCOVERED DURING 24 MONTH INSPECTION TO HAVE A CRACK IN THE RADIUS EXTENDING BETWEEN THE SECOND AND THIRD FASTENER HOLE ABOVE STR 11 IN THE FLANGE, A CRACK IN THE FLANGE EXTNEDING THROUGH THE FIRST FASTENER HOLE, AND A CRACK IN THE DOUBLER ON THE AFT SIDE OF THE FRAME. FRAME FLANGE FS 718 REPAIRED IAW WVAC EO 601R-53-0067. DOUBLER ON AFT SIDE OF FRAME FS 718 REPAIRED IAW WVAC EO 601R-53-0069.

Part: BLANKET — DAMAGED (APU EXHAUST)

UPPER APU EXHAUST HEAT BLANKET HAS HOLES. REPLACED HEAT BLANKET.

Part: DUCT — WORN (APU EXHAUST)

APU EXHAUST SUPPORT DUCT ASSY IS WORN ON INBOARD SIDE. REPLACED DUCT.

Part: DUCT — BROKEN (APU EXHAUST)

APU EXHAUST DUCT HAS SEVERAL BROKEN TABS. REPLACED DUCT.

Part: BLANKET — DAMAGED (APU EXHAUST)

LOWER APU EXHAUST HEAT BRACKET HAS HOLES. REPLACED HEAT BLANKET.

Part: FRAME — CRACKED (BS 718)

FS 718 AND STR 11 (LHS) HAS A CRACK IN THE RADIUS EXTENDING BETWEEN THE FIRST AND SECOND FASTENER HOLE ABOVE STRINGER 11 IN THE FLANGE ATTACHING TO THE SKIN AND A CRACK IN THE DOUBLER ON THE AFT SIDE OF FRAME. FRAME FLANGE REPAIRED IAW WVAC EO 601R-53-0066. DOUBLER ON AFT SIDE OF FRAME REPAIRED IAW EO 601R-53-0068.

Part: COVER — BROKEN (CABIN)

FLOOR EMERGENCY LIGHT STRIP TOP COVER BROKEN. REPLACED COVER.

Part: BULKHEAD ANGLE — CRACKED (AFT PRESS BLKHD)

ANGLE BRACKET ON REAR PRESSURE BULKHEAD, LEFT AFT SIDE IS CRACKED. REPLACED ANGLE BRACKET.

Part: BUKKHEAD ANGLE — CRACKED (AFT PRESS BLKHD)

ANGLE BRACKET ON REAR PRESSURE BULKHEAD RIGHT AFT SIDE IS CRACKED. REPLACED ANGLE BRACKET.

Part: CONTROL HANDLE — FAILED (TE FLAPS)

AFTER LANDING RETRACTED FLAPS TO 30 DEGREES, FLAPS INDICATED 30 DEGREES BUT FLAP CAUTION MESSAGE APPEARED. COMPLIED WITH EO 27-045 AD EO 27-046 AD. REMOVED AND REPLACED FLAP HANDLE.

Part: DUCT — DETACHED (FUSELAGE)

DURING TAXI, AFTER NR 1 ENGINE START, COCKPIT FILLED WITH SMOKE. AIR DUCT BETWEEN LEFT HAND ACM AND HEAT EXCHANGER CAME OFF. REINSTALLED DUCT.

Part: LEVER — MALFUNCTIONED (TE FLAPS)

FLAPS FAIL CAUTION MESSAGE. REPLACED THE FLAP SELECTOR HANDLE.

Part: BPSU — MALFUNCTIONED (LT TE FLAP)

FLAPS FAILED AFTER TAKEOFF. REPLACED THE LEFT HAND BPSU.

Part: INDICATION — MALFUNCTIONED (TE FLAPS)

FLAPS FAIL MESSAGE. INSPECTED FLAPS PER AD 98-20-01. NO DEFECTS FOUND.

Part: CONNECTOR — LOOSE (CABIN)

AFT SECTION OF EMERGENCY FLOOR LIGHTING IS INOPERABLE. SECURED WIRING CONNECTOR BETWEEN LIGHT STRIPS.

Part: FECU — FAILED (TE FLAPS)

FLAPS FAIL MESSAGE PRESENT DURING LANDING. REPLACED RIGHT HAND BPSU AND FECU.

Part: INDICATION — MALFUNCTIONED (TE FLAPS)

FLAPS FAIL MESSAGE DURING LANDING. PERFORMED VISUAL INSPECTION OF FLAPS. PERFORMED SELF TEST, CYCLED FLAPS. COULD NOT DUPLICATE.

Part: FECU — FAILED (TE FLAPS)

FLAP FAIL MESSAGE DURING CRUISE FLIGHT. REPLACED THE FLAP ELECTRONIC CONTROL UNIT.

Part: ACTUATOR — FAILED (HORIZ STAB)

CONFIG TRIM WARNING. REPLACED THE HORIZONTAL TRIM ACTUATOR.

Part: DRAIN — NOISY (GALLEY)

NOISE FROM CABIN DOOR AREA. REPLACED THE GALLEY DRAIN ASSY.

Part: CIRCUIT BREAKERS — TRIPPED (DOOR WARN SYST)

CABIN DOOR, SERVICE DOOR AND CARGO DOOR WARNINGS. RESET CIRCUIT BREAKERS, CLEARED FAULTS FROM PSEU. SYSTEM TEST SATISFACTORY.

Part: WIRE HARNESS — DEFECTIVE (PAX DOOR WARNING)

CABIN DOOR WARNING DURING CRUISE AT 26,000 FEET, PERFORMED EMERGENCY DEPRESSURIZATION AS PER QRH LANDED SAFELY AT BMI. REPLACED DEFECTIVE SECTIONS OF DOOR WARNING WIRING HARNESS, WIRE NR MB20C22 AND WIRE NR MB67B22 AT CONNECTOR P1MB.

Part: LAMP — FAILED (CABIN)

AFT CABIN OVERHEAD EMERGENCY LIGHT INOPERABLE. REPLACED BULB.

Part: FECU — MALFUNCTION (TE FLAPS)

FLAPS FAILED AT 8 DEGREES. REPLACED THE FECU.

Part: OIL COOLER — FAILED (APU)

APU OIL TEMP CAUTION INDICATION. REPLACED THE OIL COOLER.

Part: WINDSHIELD — SHATTERED (LT COCKPIT)

PILOTS SIDE WINDSHIELD SHATTERED. REPLACED WINDOW.

Part: DEICE SYST — MALFUNCTIONED (WINGS)

WING OVERHEAT WARNING DURING TAKEOFF. DEFERRED NORMAL WING DE-ICE SYSTEM. AIRCRAFT CONTINUED SERVICE ON STANDBY SYSTEM.

Part: TARGET — LOOSE (LT MLG)

LT MLG DISAGREE MESSAGE ON EICAS AFTER LANDING GEAR RETRACTED. TIGHTENED LOOSE SENSOR TARGET ON LT MLG.

Part: HYDRAULIC PUMP — LEAKING (RT ENGINE)

AFTER REPLACEMENT OF ENGINE DRIVEN HYDRAULIC PUMP VALVE PLATE BOLTS AS IN VICKERS SERVICE BULLETIN 887055-29-01, HYDRAULIC PUMP LEAKAGE OCCURRED. DISCOVERED HOLE IN PUMP FLANGE O-RING RECESS. REPLACED HYDRAULIC PUMP.

Part: UNLOCK MESSAGE — ILLUMINATED (LT TR UNIT)

LEFT REVERSER UNLOCK MESSAGE ILLUMINATED. DEFER PER 78-30-1.

Part: DRAG BRACE — FAILED (NOSE GEAR)

UNABLE TO RETRACT GEAR ON TAKEOFF, UPON SELECTION OF GEAR UP, NOSE GEAR ONLY. REPLACED NOSE LANDING GEAR DRAG BRACE, OPERATIONAL CHECK GOOD.

Part: PCU — INOPERATIVE (LT FLT SPOILER)

WHITE FLIGHT SPOILER MESSAGE CAME ON AFTER LANDING. REPAIRED LT INBD FLIGHT SPOILER POWER CONTROL UNIT.

Part: SHAFT — BROKEN (LT TE FLAP)

FLAPS FAIL MESSAGE ON EICAS. FLAPS WILL NOT OPERATE. REPLACED DEFECTIVE FLEX DRIVE CABLE ON LEFT INBOARD FLAP.

Part: O-RING — CUT (NR 3 HYD SYST)

NR 3 HYDRAULIC SYSTEM LOST ALL FLUID IN CRUISE FLIGHT. REPLACED O-RING.

Part: SIDE WINDSHIELD — CRACKED (LT COCKPIT)

PILOT'S SIDE WINDSHIELD CRACKED. REPLACED WINDOW. PART TOTAL CYCLES, 1,663.

Part: DRAG BRACE — DEFECTIVE (NLG)

THE NOSE LANDING GEAR DID NOT RETRACT. REPLACED THE NLG DRAG BRACE ASSY.

Part: GEARBOX — BINDING (LT ENG)

THE LEFT ENGINE POWER LEVER IS BINDING AND CANNOT BE MOVED TO REVERSE THRUST POSITION. REPLACED THE THROTTLE CONTROL GEARBOX.

Part: BORESCOPE PLUG — BROKEN (LT ENGINE)

LEFT ENGINE N2 VIBRATION WARNING ON EICAS. REMOVED AND REPLACED THE LT ENGINE DUE TO FOD CAUSED BY A DEFECTIVE BORESCOPE PLUG, WHICH SEPERATED AND ENTERED THE ENGINE.

Part: AIR START VALVE — FAILED (RT ENGINE)

RIGHT ENGINE START MESSAGE ON EICAS. REPLACED THE RIGHT ENGINE START VALVE.

Part: FLAP INDICATION — MALFUNCTIONED (TE FLAPS)

FLAP FAULT MESSAGE ON EICAS, ZERO FLAPS LANDING. COULD NOT DUPLICATE PROBLEM. SYSTEM TEST NORMAL AND ACFT RETURNED TO SERVICE.

Part: LEAK SENSOR — DEFECTIVE (LT WING)

ANTI-ICE DUCT MESSAGE AFTER 20 MINUTES OF USE, EICAS INDICATED LT WING. STANDBY SYSTEM OPERATES NORMAL. REPLACED DUCT LEAK SENSORS 527WK, 519WK, 525WK, 515WK.