N200CD

Part: WINDOW FRAME — CRACKED (RT COCKPIT)

COPILOTS SIDE WINDOW LOWER STRUCTURAL BEAM IS CRACKED AT RT WINDSHIELD AFT BEAM. NORMAL OPS. (K)

Part: WINDOW FRAME — CRACKED (WINDSHIELD)

PILOT`S SIDE WINDOW LOWER STRUCTURAL BEAM IS CRACKED AT LT WINDSHIELD AFT BEAM. NORMAL OPERATIONS. (K)

Part: LANDING GEAR — MALFUNCTIONED (NLG) · airframe 26,568 hrs · 31,014 cycles

AFTER GEAR RETRACTION, BOTH RED AND GREEN A-SYSTEM NOSE LIGHTS REMAINED ILLUMINATED. PRESS TO TEST DISPLAYED ALL B-LIGHTS ON AND ONLY A-NOSE LIGHTS ON. ATTEMPTED TO CYCLE GEAR WITH NO RESPONSE. PERFORMED MANUAL ELECTRIC OVERRIDE QRH PROCEDURE SUCCESSFUL. REMOVED AND REPLACED A-HARNESS AND PROX SENSOR. CYCLED GEAR SEVERAL TIMES. OPS CHECKED GOOD. P/N ON 120-4125-001, S/N ON T99928.

Part: BOLT — BROKEN (LT MLG) · airframe 26,198 hrs · 30,451 cycles

UPON GEAR RETRACTION LEFT MAIN GEAR DOOR STAYED OPEN. RECYCLED GEAR AND IT STILL REMAINED OPEN. FOUND A BROKEN BOLT ON THE LEFT INBOARD FORWARD DOOR ACTUATOR ARM. INSTALLED A NEW BOLT. OPS CHECK GOOD.

Part: FCU — MALFUNCTIONED (T/E FLAP) · airframe 26,142 hrs · 30,360 cycles

ON TAKEOFF WE GOT THE FLAP AND ADVANCED SWS ON MAP AND CONTROL FAULT. ASYMMETRY AND DISAGREEMENT ON OVERHEAD FLAP PANEL AND FLAP DEG. INDICATOR WENT TO 0 DEGREES. ABORTED TAKEOFF. POWERED DOWN 5 MINUTES AND IT REPLICATED SAME PROBLEM AFTER POWER UP. RE-RACKED FLAP CONTROL BOX. SYSTEM FUNCTIONS NORMALLY. ALL WORK PERFORMED IAW EMB AMM 27-50-06.

Part: STRAP — OUT OF POSITION (PNEUMATIC VALVE) · airframe 26,113 hrs · 30,320 cycles

CLIMBING THROUGH 22,000 CABIN ALT LIGHT ON MAP. CABIN WOULD NOT RESPOND IN AUTO. SWITCH TO MANUAL, WOULD NOT RESPOND. AFTER ABOUT 30 SECONDS CABIN STARTED DESCENDING. DIVERTED FROM STS TO SFO.SECURED INSULATION ON AFT PRESSURE BULKHEAD AND REPOSITIONED BONDING STRAPS ON PNEUMATIC AND ELECTROPNEUMATIC VALVES. OPS CHECK GOOD.

Part: ENGINE — MALFUNCTIONED (LEFT) · airframe 26,050 hrs · 30,224 cycles

LEFT ENGINE LOST POWER INFLIGHT, PRECAUTIONARY ENGINE SHUT DOWN CHECK COMPLETED.REMOVED AND REPLACED LEFT ENGINE ASSY WITH SERVICEABLE UNIT. COMPLIED WITH ALL ITEMS ON ENGINE INSTALLATION CARD. NO DEFECTS NOTED. OPS CHECKS GOOD ON ENGINE RUNSPN ON: PW118 SN ON: 115424 SN OFF: 115238

Part: FRAME — CRACKED (LEFT NACELLE) · airframe 26,036 hrs · 30,202 cycles

LEFT NACELLE FRAME 1 CRACKED AT INBOARD TORSION MOUNT.REPLACED LEFT NACELLE FRAME 1 IAW SB120-54-0036 PART 2.

Part: FRAME — CRACKED (RIGHT NACELLE) · airframe 26,036 hrs · 30,202 cycles

RIGHT NACELLE FRAME 1 CRACKED AT OUTBOARD TORSION MOUNT.REPLACED RIGHT NACELLE FRAME 1 IAW SB120-54-0036 PART 2.

Part: SWIVEL — CORRODED (MLG DOOR) · airframe 26,036 hrs · 30,202 cycles

NOSE GEAR AFT DOORS RODS AND SWIVELS WORN AND CORRODED.REMOVED AND REPLACED NOSE LANDING GEAR AFT DOORS RODS AND SWIVELS WITH SERVICEABLE PARTS AS REQUIRED.

Part: STRINGER — CRACKED (FUEL BAY) · airframe 26,036 hrs · 30,202 cycles

CRACKED LOWER STRINGER IN FUEL BAY LEFT WING AT NR 2 FUEL ACCESS PANEL BAY AFT.REPAIRED IAW EMB120 SRM 57-20-03.

Part: STRINGER — CRACKED (LT WING FUEL BAY) · airframe 26,036 hrs · 30,202 cycles

CRACKED LOWER STRINGER IN FUEL BAY LEFT WING AT NR 2 FUEL ACCESS PANEL BAY FWD.REPAIRED IAW EMB120 SRM 57-20-03.

Part: STRINGER — CRACKED (FUEL PANEL) · airframe 26,036 hrs · 30,202 cycles

RIGHT MOST INBOARD FUEL PANEL FORWARD STRINGER CRACKED. REPAIRED IAW EMB120 SRM 57-20-03 AS OUTLINED.

Part: BEARING — CORRODED (RT WING TE FLAP) · airframe 26,036 hrs · 30,202 cycles

RIGHT NACELLE FLAP HINGE BEARINGS 2 EA. CORRODED AND WORN.REPLACED NACELLE FLAP WITH SERVICEABLE FLAP ASSEMBLY AS NEEDED.P/N: 120-40327-002 S/N OFF: 120212

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 25,683 hrs · 29,653 cycles

AURAL WARNING AND MAP LIGHT ILLUMINATED ON TAKEOFF WITH ABORT BELOW 80 KTS. RESET AURAL WARNING SYSTEM. OPS CHECK GOOD.

Part: BOOT — FAILED (STABILIZER) · airframe 24,649 hrs · 28,098 cycles

INBOARD STABILIZER AND INBOARD WING DEICE BOOTS FAILED AFTER TAKEOFF. RETURNED TO SEA. REMOVED AND REPLACED INBOARD STABILIZER AND WING EJECTOR VALVE WITH SERVICEABLE UNIT. OPS CHECK GOOD. PANEL CLOSED. S/N ON: N3503, S/N OFF: Q7401.

Part: WIRE — GROUNDED (FLAP ACTUATOR) · airframe 24,493 hrs · 27,894 cycles

ON APPROACH SELECTED FLAPS 25 THE RT OUTBOARD WENT 1 LIGHT BAR PAST FLAPS 25 AND CAUSED AN ASYMETRY. WE LANDED, PERFORMED THE QRH, THEN SELECTED FLAPS UP AND THE LT OUTBOARD DID NOT MOVE AND THE RT OUTBOARD WENT 2 LIGHT BARS UP AND CAUSED ANOTHER ASYMETRY. FOUND RT OUTBOARD FLAP ACTUATOR POTENTIOMETER WIPER WIRE GROUNDING TO AIRFRAME. ISOLATED TO SOLDER SLEEVE AT CANNON PLUG OF ACTUATOR. REPAIRED WIRING AND SOLDER SLEEVE W602-0023-22DR. OPS CHECK GOOD

Part: ACTUATOR — FAILED (TE FLAPS) · airframe 24,474 hrs · 27,865 cycles

RIGHT OUTBOARD FLAP GOES TO 45 DEGREES WHEN 25 DEGREES WAS COMMANDED. THERES NO INDICATION WITH THE OVERHEAD PANEL OR MAP. REPLACED RIGHT OUTBOARD ACTUATOR. OPS CHECK GOOD IAW RII 27-307 MM 27-50-09 PN ON 320200-1007 SN ON 221 SN OFF 774 REPLACED WIRE W201-0409-24 AS REQUIRED. OPS CHECK GOOD.

Part: ACTUATOR — FAILED (TE FLAPS) · airframe 24,409 hrs · 27,777 cycles

DURING SELECTION OF FLAPS 15 ON TAXI THE OUTBOARD PAIR WOULD ONLY EXTEND TO 1 LIGHT BAR. WE RECEIVED A CONTROL FAULT AND ASWS WARNING. WERE UNABLE TO EXTEND OR RETRACT THE OUTBOARD PAIR. QRH COULD NOT RESET FLAPS. REMOVED AND REPLACED LEFT OUTBOARD FLAP ACTUATOR PER MM 27-50-00. LEAK & OPS CHECKS GOOD.

Part: ACTUATOR — FAILED (TE FLAPS) · airframe 24,381 hrs · 27,734 cycles

DURING CRUISE FLIGHT, ''CONTROL FAUL'' FLAP WARNING INDICATOR ALONG WITH OUTBOARD PAIR OF FLAPS ILLUMINATED ON OVERHEAD PANEL. ADVANCED SWS AND FLAP LIGHTS ON MAP ILLUMINATED. COMPLIED WITH QRH PROCEDURE. SYSTEM WOULD NOT RESET. REMOVED AND REPLACED RIGHT OUTBOARD FLAP ACTUATOR IAW EMB MM 27-50-00 AND RII CARD 27-307. OPS CHECK GOOD.P/N: 320300-1007 S/N ON: 0779 S/N OFF: 0516

Part: CONNECTOR — CONTAMINATED (TE FLAPS) · airframe 24,381 hrs · 27,734 cycles

CONTROL FAULT IN OUTBOARD PAIR OF FLAPS DURING APPROACH WITH ASSOCIATED ''FLAP'' AND ''ADVANCED SWS'' ON MAP. ATTEMPTED TO RESET AS PER QRH WHICH WAS UNSUCCESSFUL. CLEANED MOISTURE FROM RIGHT OUTBOARD ACTUATOR CANNON PLUG. FLAP SYSTEM OPS CHECK GOOD.

Part: CONNECTOR — CONTAMINATED (TE FLAPS) · airframe 24,301 hrs · 27,632 cycles

ON DESCENT FLAP, ADVANCED SWS, CONTROL FAULT, OUTBOARD PAIR FLASHING. QRH WAS FOLLOWED BUT SYSTEM DID NOT RESET. FOUND MOISTURE IN CANNON PLUGS, CLEANED. USING PARKER FLAP TROUBLESHOOTING GUIDE, FOUND LEFT INBOARD FLAP SLOW TO EXTEND. REPLACED LEFT INBOARD ACTUATOR IAW 27-50-07 AND RII 27-307. CYCLED SEVERAL TIMES OPS CHECK GOOD WITH NO LEAKS NOTED.PN ON 320300-1005 SN ON 1107 SN OFF 1232

Part: LANDING GEAR — MALFUNCTIONED (LEFT) · airframe 24,228 hrs · 27,533 cycles

LEFT MAIN LANDING GEAR WOULD NOT RETRACT. SECURED LEFT GEAR INBOARD FOWARD DOOR. SWUNG GEAR, OPS CHECKS GOOD IAW MM 32-32-00.

Part: CONTROL UNIT — FAILED (TE FLAPS) · airframe 24,245 hrs · 27,557 cycles

DURING CRUISE FLIGHT, REEIVED 4 INDICATIONS: CONTROL FAULT, OUTBOARD FLAP PAIR SECOND SEGMENT FLASHING, MAP FLAP AND ADVANCED SWS CAPTIONS. QRH RESET UNSUCCESSFUL. REMOVED AND REPLACED FLAP CONTROL UNIT WITH SERVICEABLE UNIT. OPS CHECK NORMAL. S/N OFF 0230, ON 0105.

Part: ROD END — DAMAGED (RT MLG ACTUATOR) · airframe 23,474 hrs · 26,511 cycles

BOTH RIGHT MAIN ''''RED'''' DISAGREEMENT LIGHTS REMAINED ILLUMINATED AFTER GEAR WAS RETRACTED. RETURNED TO SFO. REPLACED RIGHT MLG RETRACTING ACTUATOR ROD END AND PIN IAW MM 32-32-10. OPS CHECKS GOOD.

Part: WARNING SYSTEM — FALSE INDICATION (COCKPIT) · airframe 22,718 hrs · 25,401 cycles

AFTER TAKEOFF SINGLE CHIME AURAL WARNING CHIMED CONTINUED WITH GEAR DOWN BUT STOPPED WHEN REACHING THE GATE. UNSCHEDULED LANDING. REPLACED AURAL WARNING UNIT IAW MM 315302, OPS CHECKS GOOD ON GROUND. (P/N 80055711) (S/N 0042) ON, (S/N 0086) OFF.

Part: RELAY — FAILED (LANDING GEAR)

LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. REMOVED AND REPLACED LANDING GEAR RELAY BOX IAW MM 32-31-02. GEAR SWING CHECKS GOOD.

Part: CABLE — CORRODED (CARGO DOOR)

DURING 2C INSPECTION TASK 813-01A, FOUND CARGO DOOR FORWARD INNER CABLE TO BE CORRODED. REMOVED CORRODED CABLE AND INSTALLED SERV CABLE IAW EMB120 MM.

Part: DISAGREE LIGHT — MALFUNCTIONED (RT MLG)

WHEN LANDING GEAR SELECTED UP, THE RIGHT HAND MLG DISAGREE LIGHTS REMAINED ON. COULD NOT DUPLICATE DISCREPANCY. LANDING GEAR RETRACT CHECKS NORMAL.

Part: DRAG BRACE — STIFF (LT MLG)

LEFT HAND MLG DID NOT DOWNLOCK DURING FREE FALL CHECK. RESHIMMED THE LANDING GEAR DRAG BRACE.

Part: PROX SENSOR — FALSE WARN (LT ELEVATOR)

TAKEOFF TRIM AURAL WARNING DURING TAKEOFF. REPLACED THE LT ELEVATOR TRIM PROXIMITY SENSOR.

Part: PROX SENSOR — FAILED (LT MLG)

AFTER TAKEOFF AND GEAR SELECTED UP, THE LEFT HAND MLG 'A' LIGHT REMAINED ON. LANDING GEAR DID NOT RETRACT UNTIL EMERGENCY SYSTEM WAS ACTIVATED. REPLACED THE LEFT HAND MLG DOWNLOCK PROXIMITY SENSOR.

Part: CYLINDER — CRACKED (NLG STEERING)

HYD LEAK COMING FROM NOSE GEAR STEERING AREA. REPLACED LEFT STEERING CYLINDER.

Part: ROLLER — WORN (LT TE FLAP)

LEFT OUTBOARD FLAP FAILS TO RETRACT WITH OTHERS. REPLACED LEFT OUTBOARD FLAP ROLLLRS, OPERATIONAL CHECK GOOD.

Part: ACTUATOR — INOPERATIVE (LT TE FLAP)

FLAP DISAGREEMENT UPON FLAP RETRACTION AFTER TAKEOFF. REPLACED LEFT OUTBOARD FLAP ACTUATOR OPERATIONAL CHECK GOOD. PART TOTAL CYCLES, 16,190.

Part: WIRE — CHAFED (LT BLEED AIR)

LT BLEED AIR DUCT LEAK WARNING CAME ON DURING CLIMB. REPAIRED CHAFED WIRING AT DUCT LEAK SENSOR.

Part: SKIN SUPPORT — CRACKED (FUSELAGE)

DURING 400FC INSPECTION, FOUND ONE RIVET AT FRAME 9 JUST BELOW RIGHT DIRECT WINDOW TO BE DEFORMED. FURTHER INSPECTION REVEALED SKIN SUPPORT TO BE CRACKED. REPLACED CRACKED SUPPORT.

Part: ROLLERS — WORN (RT TE FLAP)

FLAPS DISAGREEMENT WARNING AFTER TAKEOFF WHEN FLAPS SELECTED UP. REPLACED WORN ROLLERS AND TRACKS ON RT INBD FLAP.

Part: DOOR LATCH — BROKEN (ENGINE COWL)

OIL INSPECTION DOOR ON ENGINE COWLING WILL NOT STAY CLOSED. REPAIRED BROKEN SHEET METAL LATCH RETAINER.

Part: OAT PROBE HEAT — FAILED (NOSE)

OUTSIDE AIR TEMPERATURE PROBE HEAT IS INOPERATIVE. REPLACED THE TRUE AIR TEMP PROBE. PART TOTAL CYCLES, 12,082.

Part: LINES — FROZEN (LT/RT ENGINE)

LEFT AND RIGHT HYDRAULIC RESERVOIR LOW PRESS WARNINGS ILLUMINATED. THAWED THE FROZEN MOISTURE THAT WAS BLOCKING THE HYDRAULIC RESERVOIR BLEED AIR PRESSURIZATION LINES.

Part: SENSOR — MALFUNCTIONED (NLG)

NOSE LANDING GEAR INTRANSIT LIGHT REMAINED ON AFTER RETRACTION. COUD NOT DUPLICATE DISCREPANCY. REPLACED A-SYSTEM PROXIMITY SENSOR, WHILE TROUBLESHOOTING.

Part: CONTROL BOX — DEFECTIVE (NLG)

NOSE LANDING GEAR INTRANSIT LIGHT REMAINED ON AFTER GEAR RETRACTION. REPLACED THE LANDING GEAR CONTROL ASSY.

Part: RETRACT MECH — ICED UP (NLG)

NOSE LANDING, GEAR INTRANSIT LIGHTS REMAINED ON AFTER GEAR RETRACTION. REMOVED ICE FROM LANDING GEAR, RETRACT CHECKS NORMAL, AND ACFT RETURNED TO SERVICE.

Part: UPLOCK HOOK — LACK OF LUBE (LT MLG)

LT MLG WILL NOT RETRACT. FOUND UPLOCK HOOK ASSY TO BE BINDING. CLEANED AND LUBED UPLOCK ASSY AND SYSTEM OPERATES NORMALLY.

Part: UPLOCK — DIRTY (LT MLG)

WHEN LANDING GEAR SELECTED UP, LT MLG INTRANSIT LIGHTS REMAINED ON. CLEANED LT MLG UPLOCK, RETRACTION CHECK NORMAL AND ACFT RETURNED TO SERVICE.

Part: SEPARATOR — LEAKING (RT AIR FOIL)

RT DUCT LEAK WARNING ACTIVATED. REPLACED LEAKING AIR FOIL DE-ICE WATER SEPARATOR.

Part: WARNING LIGHT — ILLUMINATED (CARGO DOOR)

CARGO DOOR WARNING ILLUMINATED DURING FLIGHT. PLACED CARGO DOOR WARNING SYSTEM ON DEFERRED MAINTENANCE LIST.

Part: LINK ROD — FAILED (NLG)

AIRCRAFT ON APPROACH TO FPO, CREW SELECTED GEAR DOWN. THE MLG INDICATED DOWN AND LOCKED AND THE NLG INDICATED UNSAFE. MAINTENANCE INSPECTED THE NLG AND FOUND THE SECONDARY STRUT NOT TO BE FULLY LOCKED, GEAR SAFETY PIN COULD NOT BE INSTALLED. THE SAFETY PIN BUSHING ON THE LINK ROD HAD MIGRATED INTERFERING WITH THE SECONDARY STRUT. MAINTENANCE RESEATED BUSHING AND THE AIRCRAFT WAS FERRIED GEAR DOWN TO THE CLOSEST MAINTENANCE BASE FOR PERMANENT REPAIR. LINK ROD (P/N 20750), WAS REPLACED AND RETRACTION/EXTENSION CHECKS COMPLIED WITH.

Part: LATCH ASSY — BROKEN (LT NACELLE)

LEFT ENGINE INBD NACELLE LATCH IS BROKEN. REPLACED LATCH.

Part: SENSOR — DEFECTIVE (ELEV TRIM TAB)

TAKEOFF TRIM WARNING SOUNDED DURING TAKEOFF. REPLACED THE ELEVATOR TRIM TAB PROXIMITY SENSORS.

Part: REGULATOR — LEAKING (LT ENGINE)

LEFT ENGINE SECURED DURING FLIGHT DUE TO LOW OIL PRESSURE. REPLACED THE OIL PRESSURE REGULATOR FITTING P/N 3112525-01, PULLED OUT OF REGULATOR HOUSING. PWC SB 21186 REPLACES THIS WITH IMPROVED P/N 3117892-01 FITTING.

Part: SKIN SUPPORT — CRACKED (WINGS)

THE FOLLOWING P/N WING SKIN SUPPORTS WERE FOUND CRACKED DURING INSPECTION TASK 5720-551/651-01I AND 5720-552/652-01I AT WING RIBS NR 15, 16, 18 AND 21. THE SKIN SUPPORTS WERE REPLACED IAW AERODESIGN REPORT NR 1327-2. P/N: 120-17062-005, 2 EA; 120-17056-015, 4 EA; 120-17057-006, 2 EA; 120-17056-007, 12 EA; 120-17057-015, 1 EA; 120-17056-019, 2 EA; 120-17056-017, 2 EA; 120-17056-013, 2 EA; 120-17057-006, 1 EA.

Part: PROX SWITCH — REQUIRE ADJUST (LT MLG)

LEFT MAIN LANDING GEAR INTRANSIT LIGHTS REMAIN ON AFTER RETRACTION. ADJUSTED THE LEFT MLG UPLOCK PROXIMITY SWITCHES.

Part: VALVE — DEFECTIVE (LT MLG)

LEFT MLG DID NOT FULLY RETRACT, RED INTRANSIT LIGHTS REMAINED ON. REPLACED THE LANDING GEAR SOLENOID VALVE.

Part: FILTER — SUSPECT (LT ENGINE)

LEFT ENGINE FUEL FILTER WARNING CAME ON DURING FLIGHT. THE PROBLEMS CANNOT BE DUPLICATED AND VISUAL INSPECTION OF FILTERS INDICATED NO UNUSUAL DEBRIS. REPLACED THE FUEL FILTERS AND FUEL PRESSURE SWITCHES FOR TROUBLESHOOTING.

Part: ACTUATOR — OUT OF ADJUST (LT MLG)

AFTER LANDING GEAR RETRACITON, NLG AND LEFT MLG INTRANSIT LIGHTS REMAINED ON. ADJSUTED LEFT MLG RETRACT ACTUATOR AND ADJUSTED NLG PROXIMITY SENSORS.

Part: ACTUATOR — DEFECTIVE (LT MLG)

LEFT MLG INTRANSIT LIGHTS REMAINED ON AFTER RETRACTION. REPLACED THE LEFT MLG RETRACT ACTUATOR.

Part: UNSAFE IND — ACTIVATED (NLG)

NLG INDICATED UNSAFE AFTER LANDING GEAR RETRACTED. COULD NOT DUPLICATE NLG DISCREPANCY.

Part: DE-ICE LEAD — BROKEN (RT PROP)

RT PROPELLER DE-ICE FAILED. REPLACED BROKEN HEATER LEAD WIRE.

Part: HOOK ASSY — LACK OF LUBE (RT MLG)

RT MLG WILL NOT RETRACT. CLEANED AND LUBED RT MLG UPLOCK HOOK ASSY. FUNCTION CHECK OF LANDING GEAR SYSTEM SATISFACTORY.