N660CP

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 11,848 hrs · 9,253 cycles

RH OVERWING EMERGENCY LIGHTS INOP.

Part: BATTERY — DISCHARGED (CABIN) · airframe 11,562 hrs · 9,044 cycles

EMERGENCY EXIT SIGN/LIGHT AT LH OVERWING EXIT WILL NOT STAY LIT.

Part: FRAME — DENTED (FUSELAGE) · airframe 8,711 hrs · 6,827 cycles

INSPECTION REVEALED A DENT IN THE INBD CHORD OF THE FUSELAGE FRAME AT THIS LOCATION. THE SRM ALLOWS NO DENTS IN THIS AREA & THERE ARE NO SRM REPAIRS FOR SHEAR TIED FRAMES, SO A SERVICE REQUEST WAS RAISED INCLUDING A REQUEST TO ALLOW TO CONTINUE IN SERVICE AS IS BY ENGINEERING. DENT WAS ALLOWED FOR CONTINUED SERVICE AFTER REWORK AS A PERMANENT REPAIR.

Part: FRAME — DENTED (FUSELAGE) · airframe 8,711 hrs · 6,827 cycles

INSPECTION REVEALED A DENT IN THE INBD CHORD OF THE FUSELAGE FRAME AT THIS LOCATION. THE SRM ALLOWS NO DENTS IN THIS AREA & THERE ARE NO SRM REPAIRS FOR SHEAR TIED FRAMES, SO A SERVICE REQUEST WAS RAISED, INCLUDING A REPAIR SCHEME SUGGESTED BY ENGINEERING.

Part: FRAME — DENTED (FUSELAGE) · airframe 8,711 hrs · 6,827 cycles

INSPECTION REVEALED A DENT IN THE INBD CHORD OF THE FUSELAGE FRAME, PN 146A1285-70, AT THIS LOCATION. THE SRM ALLOWS NO DENTS IN THIS AREA & THERE ARE NO SRM REPAIRS FOR SHEAR TIED FRAMES, SO A SERVICE REQUEST WAS RAISED INCLUDING A REPAIR SCHEME SUGGESTED BY ENGINEERING.

Part: INTERCOSTAL — DEFORMED (FUSELAGE) · airframe 8,711 hrs · 6,827 cycles

DURING INSPECTION, DAMAGE WAS NOTED IN THE UPPER FLANGE OF THE INTERCOSTAL RUNNING BETWEEN BS 787 & BS 807 AT STRINGER 22L. FABRICATED & INSTALLED REPLACEMENT INTERCOSTAL.

Part: SHEAR TIE — DENTED (ZONE 100) · airframe 8,711 hrs · 6,827 cycles

INSPECTION REVEALED A DENT IN THE INBD CHORD OF THE FUSELAGE FRAME AT THIS LOCATION. THE SRM ALLOWS NO DENTS IN THIS AREA AND THERE ARE NOR SRM REPAIRS FOR SHEAR TIE FRAMES.

Part: FRAME — DENTED (FUSELAGE) · airframe 8,711 hrs · 6,827 cycles

INSPECTION REVEALED A DENT IN THE INBD CHORD OF THE FUSELAGE FRAME AT THIS LOCATION. THE SRM ALLOWS NO DENTS IN THIS AREA & THERE ARE NO SRM REPAIRS FOR SHEAR TIED FRAMES, SO A SERVICE REQUEST WAS RAISED INCLUDING A REQUEST TO ALLOW TO REMAIN IN SERVICE & A REPAIR SCHEME SUGGESTED BY ENGINEERING. FRAME WAS NOT ABLE TO BE REWORKED SO HAD TO BE REPAIRED.

Part: FRAME — DENTED (FUSELAGE) · airframe 8,711 hrs · 6,827 cycles

INSPECTION REVEALED A DENT IN THE INBD CHORD OF THE FUSELAGE FRAME AT THIS LOCATION. THE SRM ALLOWS NO DENTS IN THIS AREA & THERE ARE NO SRM REPAIRS FOR SHEAR TIED FRAMES, SO A SERVICE REQUEST WAS RAISED INCLUDING A REQUEST TO ALLOW TO CONTINUE IN SERVICE AS IS BY ENGINEERING. DENT WAS ALLOWED FOR CONTINUED SERVICE AFTER REWORK AS A PERMANENT REPAIR.

Part: FRAME — DENTED (ZONE 100) · airframe 8,611 hrs · 6,827 cycles

INSPECTION REVEALED A DENT IN THE INBD CHORD OF THE FUSELAGE FRAME AT THIS LOCATION. THE SRM ALLOWS NO DENTS IN THIS AREA AND THERE ARE NO SRM REPAIRS FOR SHEAR TIED FRAMES SO A SERVICE REQUEST WAS RAISED WITH MFG INCLUDING A REQUEST TO ALLOW TO CONTINUE IN SERVICE AS-IS BY ENGINEERING. DENT WAS ALLOWED FOR CONTINUED SERVICE AFTER REWORK AS A PERMANENT REPAIR.

Part: WARNING LIGHT — FALSE ACTIVATION (PAX DOOR) · airframe 6,852 hrs · 5,380 cycles

DURING TAKEOFF ROLL, FORWARD ENTRY DOOR LIGHT ILLUMINATED AT 80 KNOTS. REJECTED TAKEOFF, RETURNED TO GATE. INSPECTED AND TESTED FORWARD ENTRY DOOR IAW FAULT ISOLATION MANUAL 52-10-08. NO FAULTS FOUND. ACFT RELEASED FOR SERVICE. SUBSEQUENT FLIGHT REPORTED, NO DISCREPANCIES.

Part: INTERCOSTAL — CRACKED (ZONE 100) · airframe 6,404 hrs · 5,030 cycles

FOUND CRACK IN INTERCOSTAL NEXT TO FLOOR PANEL ATTACH NUTPLATE.

Part: FLOOR PANEL — CRACKED (ZONE 100) · airframe 6,404 hrs · 5,030 cycles

FLOOR PANEL FOUND CRACKED.

Part: FLOOR PANEL — CRACKED (ZONE 100) · airframe 6,404 hrs · 5,030 cycles

FLOOR PANEL FOUND CRACKED.

Part: DOWNLOCK SWITCH — OUT OF TOLERANCE (MLG) · airframe 5,904 hrs · 4,645 cycles

DURING CLIMB OUT, AFTER GEAR RETRACTION, FORWARD PANEL GEAR INDICATOR SHOWED RT MAIN GEAR STILL DOWN AND LOCKED. OVERHEAD GEAR INDICATOR SHOWED ALL 3 GEAR UP AND LOCKED. RETURNED TO DEPARTURE. LANDED UNEVENTFUL. FOUND RT GEAR PRIMARY DOWN LOCK PROXIMITY SWITCH RESISTANCE OUT OF TOLERANCE. REPLACED SWITCH. GEAR SWING, OPS CHECK OK. SUBSEQUENT FLIGHTS OK.

Part: COMPRESSOR BLADE — NICKED (NR 2 ENGINE) · airframe 2,423 hrs · 1,935 cycles

NR 2 ENG BIRD STRIKE AND INGESTION AT THE 9 O’CLOCK POSITION. BLOOD AND FEATHERS FOUND ON BLADES IN BYPASS PATH AND BOOSTER INLET. CONDITIONAL INSP COMPLIED WITH IAW AMM 05-51-18 AND 71-00-00. NO DEFECTS NOTED. ENGINE BORESCOPE INSP OF HIGH PRESSURE COMPRESSOR BLADES COMPLIED WITH. BLADES CHECKED GOOD WITH MINOR DEFECTS NOTED, ALL WITHIN LIMITS IAW MM 72-00-00.

Part: AUTOPILOT SYS — DISCONNECTED (ZONE 200) · airframe 1,454 hrs · 1,185 cycles

SPEED TRIM FAIL LIGHT ILLUMINATED AND YAW DAMPER WON'T ENGAGE DURING TAKEOFF. MADE UNEVENTFUL RETURN TO DEPARTURE AIRPORT. PERFORMED YAW DAMPER SYS TEST IAW AMM 22-23-00, NO DEFECTS NOTED. PERFORMED DFCS BITE PROCEDURE AND DFCS ADJUSTMENT/TEST IAW AMM 22-11-00 AND PERFORMED SPEED TRIM SYSTEM TEST IAW AMM 22-00-00, NO DEFECTS NOTED.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 533 hrs · 451 cycles

MULTIPLE BIRD STRIKES ON DEPARTURE, RETURNED TO AIRPORT. REPLACED F/O WINDSHIELD. REPLACED 5 RIVETS UNDER INBD STRAFE OF NR 2 ENGINE NOSE COWL. CLEANED MULTIPLE BIRD REMAINS FROM RT FUSELAGE NOSE AND TAIL OF ACFT. PERFORMED BIRD STRIKE INSP IAW AMM 05-51-18; NO ADDITIONAL DAMAGE NOTED.