N227CK

ATA 5311

DURING AN EDDY CURRENT INSPECTION REQUIRED PER AD 2017-10-01, CRACKS WHERE FOUND IN THE BENDS BETWEEN THE VERTICAL FRAME AND FRAME FLANGE ON THE LEFT AND RIGHT SIDES OF FRAME 33. BOTH CRACKS ARE LOCATED BETWEEN STRINGERS 5L AND 6L AND STRINGERS 5R AND 6R. CRACKS TO BE REPAIRED PER DASSAULT FALCON ENGINEERING WITH DOA APPROVAL.

ATA 5330

CORROSION FOUND ON THE INSIDE OF THE SKIN ALONG THE SPOT WELDS ON THE RIGHT SIDE OF THE FORWARD FUSELAGE BETWEEN FUSELAGE FRAMES 7 AND 9, AND BETWEEN STRINGERS 20R-22R DURING ROUTINE INSPECTION. CORRODED MATERIAL REMOVED AND AN EXTERNAL SKIN PATCH INSTALLED PER DOCUMENT NO. 17-02 REV.A AND FAA FORM 8110-3.

ATA 5711

AIRCRAFT WAS LEAKING FUEL FROM AFT LT SIDE OF CENTER FUEL TANK AREA. FURTHER EXAMINATION REVEALED CRACK IN AFT LOWER CENTER WING SPAR CAP LEFT SIDE. DASSAULT FALCON JET HAS BEEN CONTACTED AND THEY HAVE PROVIDED A REPAIR.

ATA 7110

CRACK WAS FOUND DURING VISUAL INSPECTION OF UPPER LT ENGINE COWLING P/N MY20 551.30-2. CRACKS LOCATED IN THE SHEET METAL STRUT AT THE LOCATION OF THE BOLT WHICH SECURES THE ATTACH FITTING TO THE COWLING. REPAIRED CRACK IN ACCORDANCE WITH FAA FORM 8110-3 DATED 2/11/2010 AND DOCUMENT 96-43-3, REV A DATED 2/11/2010.

ATA 7200

RT ENGINE ROLLED BACK AND SHUTDOWN WHEN CAPTAIN ADVANCED THE POWER LEVERS. PILOT TAXIED BACK TO HANGAR. PERFORMED ENGINE RUNS AND PERFORMANCE CHECKS IAW GE MANUAL SEI-187. COULD NOT DUPLICATE PROBLEM. CHECKED ENGINE FUEL FILTERS AND CLEANED, PERFORMED OVERSPEED GOVERNOR BYPASS CHECK. PERFOMRED GENERAL INSPECTION OF ENGINE, FUEL SYSTEM AND CONTROLS. PERFORMED HIGH SPEED TAXI CHECKS. NO DEFECTS NOTED. AIRCRAFT TEST FLIGHT WAS PERFORMED WITH NO DEFECTS OR ABNORMAL OPERATIONS NOTED. (K)