EXCLUSIVE JETS LLC

Operated by Exclusive Jets LLC (per NTSB report)

The airplane’s impact with birds during approach.

Part: SEAL — LEAKING (ZONE 800) · airframe 5,213 hrs · 3,506 cycles

UPON CLIMBING THROUGH FL310, WE HEARD LOUD WHISTLE FROM MAIN CABIN DOOR. THERE WAS NO LOSS OF CABIN PRESSURE AND THE PRESSURE DIFFERENTIAL REMAINED AT 7.5 PSI AND 4,000 CABIN ALTITUDE. PERFORMED CABIN PRESSURIZATION LEAK CHECK IAW AMM 21-30-TWO AREA THAT REQUIRED CLEANING AND SEALANT APPLIED AND DOOR SEAL ADJUSTMENT. PERFORMED REQUIRED CLEANING AND SEALANT APPLIED AND DOOR SEAL ADJUSTMENT. PERFORMED PRESSURIZATION TEST 3X.THE 2ND AND 3RD TIME TESTING RESULTS, PRODUCED NO NOISE IN CABIN AND THE DEFFERENTIALL PRESSURE WAS AT8.35. OK FOR SERVICE

Part: WHEEL — FAILED (ZONE 700)

LOST RIGHT MAIN INBOARD TIRE ASSEMBLY AFTER ROTATION FROM TJSJ.////// REPLACED RH MLG AND BOTH MAIN WHEEL ASSY.

Part: OUTFLOW VALVE — FAILED (ZONE 100) · airframe 15,801 hrs · 10,726 cycles

AFTER DEPARTURE FROM KSLC PASSING THROUGH 8000’, NOTICED THE CABIN WAS NOT PRESSURIZING.

Part: SEAL — WORN (ZONE 100) · airframe 2,411 hrs · 1,242 cycles

L BLEED LEAK RED CAS MESSAGE. RAN CHECKLIST AND LIGHT EVENTUALLY EXTINGUISHED. REMOVED AND REPLACED SEALS FOR BOTH PACK FLOW CONTROL VALVE. FOUND BLEED LEAK REPORT POINTS TO AREA AROUND LEFT-INTERMEDIATE VALVE. FOUND VALVE LEAKING REINSTALLED INBD CLAMP. PERFORMED OPS AND LEAK CHECK, CHECKS GOOD IAW AMM 36-11-05-04

Part: ELEC CONNECTOR — DIRTY (ZONE 700) · airframe 9,927 hrs · 7,665 cycles

LOWERED LANDING GEAR AND RH MAIN GEAR GREEN LIGHT DID NOT ILLUMINATE AND THE RED UNLOCKED LIGHT STAYED ILLUMINATED. COMPLIED WITH MAIN LANDING GEAR HYDRAULIC SYSTEMS- ADJUSTMENT/TEST IAW AMM 32-01 -00 REV 48 SWUNG GEAR 10 TIMES ALL INDICATIONS NORMAL CLEANED AND WIPED DOWN LANGING GEAR, REMOVED UPLOCK AND DOWNLOCK ELECTRICAL CONNECTOR, CLEANED AND INSPECTED OPS CHECK OF LANDING GEAR COMPLETE AND NO FAULTS FOUND.

Part: CONTACTOR — DIRTY (ZONE 100) · airframe 8,995 hrs · 7,035 cycles

AFTER ADVANCING TO TAKE OFF POWER GOT A BIG RUSH OF AIR AND A ACM OVERHEAT WITH MASTER CAUTION. CLEANED CONTACTOR FOLLOWED BY REINSTALLATION OF PT 038 SWITCH, OPS CHECK GOOD.

Part: GROMMET — INSTALLED (ZONE 800) · airframe 6,281 hrs · 4,322 cycles

DESCENDING FROM FL450 TO FL350, THROUGH 38000 FT, DOOR SEAL INDICATION FOLLOWED BY A LOUD NOISE AND CAB ALT WARNING IN SECONDS LATER. VISUALLY INSPECTED MAIN DOOR SEAL. NO DEFECTS OR OTHER DAMAGE WAS NOTED. INSPECTED SECONDARY SEAL. NO DAMAMGE NOTED. NOTED THE GROMMET SEAL BETWEEN THE DOOR AND THE FUSELAGE WAS NOT FULLY INSTALLED IN HINGE. REINSTALLED GROMMET CORRECTLY IAW CE525B M/M CH. 52-10-00. FLUSHED OUT MAIN DOOR SEAL WITH NITROGEN. SUPPLIED VACUUM TO REMOVE ANY MOISTURE. BLEW NITROGEN THROUGH THE MANIFOLD THAT SUPPLIES PRESSURE TO THE DOOR SEAL, NOTED A LITTLE BIT OF VAPOR CAME OUT. REMOVED AFT BAGGAGE TO GAINED ACCESS TO WATER TRAP FOR SUPPLY. CHECKED THAT LINES HAD NO BLOCKAGE AND WERE CLEAR. CLEANED OUT TRAP AND REINSTALLED IAW CE525B AMM 36-10-00. CLOSED UP AFT BAGGAGE. CABIN DOOR SEAL OPS CHECK GOOD

Part: BULB — BURNED OUT (ZONE 700) · airframe 4,412 hrs · 4,118 cycles

LANDING GEAR LIGHT MAIN DOES NOT ILLUMINATE IN FLIGHT AFTER SELECTING THE GEAR LEVER TO THE DOWN POSITION.

Part: CONTROL UNIT — INOPERATIVE (FIRE DETECT) · airframe 8,552 hrs · 7,095 cycles

RIGHT ENGINE FIRE LIGHT ILLUMINATE.

Part: ANTI-SKID SYS — UNSERVICEABLE (ZONE 700) · airframe 10,304 hrs · 6,986 cycles

ANTI-SKID LIGHT FLASHED JUST BEFORE LANDING, NO MAIN BRAKES, USED EMERGENCY BRAKE TO STOP.

Part: BULB — BURNED OUT (ZONE 700) · airframe 5,034 hrs · 3,392 cycles

RT MAIN GEAR INDICATOR LIGHT DID NOT ILLUMINATE WHEN LANDING GEAR SELECTED DOWN. FOLLOWED "GEAR WILL NOT EXTEND" CHECKLIST AND MANUALLY EXTENDED THE WITH THE EMERGENCY BLOWDOWN BOTTLE. UPON LANDING, EMERGENCY BRAKE WAS UTILIZED TO STOP ON THE RUNWAY.

Part: SEAL — FAILED (ZONE 400) · airframe 13,652 hrs · 9,562 cycles

CLIMBING THROUGH ABOUT 8000 FEET, LH ENGINE FIRE LIGHT ILLUMINATION, FOLLOWED BY THE AURAL WARNING. BOTH WENT AWAY AFTER 30 TO 45 SECONDS. INSPECTED ENGINE AND FOUND ALL THREE BLEED AIR DUCT WIGGINS FITTING SEALS BLOWN OUT.

Part: VALVE — FAILED (ZONE 200) · airframe 9,210 hrs · 5,705 cycles

ON TAKEOFF CLIMB PRESS FLUCTUATIONS UP TO 4300 ON THE RATE AND BACK DOWN AND BACK UP AGIN ACCOMPANIED WITH A ACM OVERHEAT: REMOVED AND REPLACED LH BILEVEL VALVE IAW AMM 21-11-00. OPS & LEAK CHECKED GOOD.

Part: BRACKET — BENT (ZONE 700) · airframe 8,460 hrs · 6,348 cycles

ON TAKEOFF AFTER RAISING THE GEAR THE NOSE GEAR DIDN'T RETRACT. NOSE GEAR LIGHT WAS ON AND THE UNLOCK LIGHT ALSO WAS ON. REMOVED THE DAMAGED LH AND RH NOSE UPLOCK BRACKETS AND INSTALLED NEW BRACKETS REMOVED THE DAMAGED NOSE UPLOCK SWITCH AND INSTALLED A NEW SWITCH REMOVED THE DAMAGED NOSE UPLOCK SWITCH AND INSTALLED A NEW SWITCH REMOVED THE DAMAGED NOSE UPLOCK EMERGENCY CABLE AND INSTALLED A NEW CABLE, NEW TURNBUCKLE AND A SERVICEABLE CLEVIS END PERFORMED SEVERAL LANDING GEAR RETRACT/EXTENSIONS. OPS CHECK GOOD AT THIS TIME PERFORMED SEVERAL LANDING GEAR RETRACT/EXTENSIONS. PERFORMED EMERGENCY LANDING GEAR EXTENSLON. OPS CHECK GOOD AT THIS TIME

Part: DOOR SEAL — WORN (ZONE 800) · airframe 3,814 hrs · 2,396 cycles

CREW STARTED DECENT FROM FL 450 TO FL 270, AT FL 350 THEY RECEIVED A CABIN DOOR SEAL CAS MESSAGE. CREW REFERRED TO EMERGENCY CHECKLIST E2 AND FOLLOWED TO PROCEED BELOW FL 310 WITH MASKED DON NORMAL. AT ABOUT FL 310 THEY RECEIVED A CABIN ALTITUDE CAS MESSAGE AND PROCEEDED TO DECLARE EMERGENCY AND REQUESTED TO DESCEND TO 15000 FEET. PROCEEDED TO DO THE EMERGENCY DESCENT MEMORY ITEMS AND THEN BACK IT UP WITH EMERGENCY CHECKLIST. A4 ON THE RED MESSAGE CHECK LIST. AS CREW LEVELED OFF THE CAS MESSAGE CLEARED AND PRESSURE WENT BACK TO NORMAL. PROCEEDED TO FLY SWF WHICH WAS THE INTENDED DESTINATION WITH NO FURTHER ISSUES ALONG THE FLIGHT. CORRECTIVE ACTION: REPOSITIONED CABIN ENTRY DOOR SEAL WARM AIR DUCT IAW CABIN DOOR SEAL PRESSURIZATION COMPONENTS WARM AIR DUCT ROUTING ATA 21-40. REMOVED AND REPLACED SECONDARY DOOR SEAL IAW 525B MM CH 52-10-00 OPS CHECKED GOOD. REPACKED O2 MASK IAW 525B MM 35-20-00

Part: CONTROLLER — FAILED (ZONE 100) · airframe 14,159 hrs · 9,638 cycles

PRESSURE CONTROLLER WENT BLANK IN FLIGHT. R & R PRESSURIZATION CONTROLLER.

Part: POWERPACK — FAILED (ZONE 100) · airframe 12,270 hrs · 9,586 cycles

DURING TAKE OFF ROLL JUST AFTER 80 KT CHECKS MASTER CAUTION / ANTISKID INOP ANNUNCIATION ILLUMINATED. REMOVED FAILED HYDRAULIC PACK ASSY AND INSTALLED NEW HYDRAULIC POWER PACK ASSY. BRAKE BLEEDING C/W WITH NO DISCREPANCIES NOTED AT THIS TIME. OPS AND LEAK CHECK C/W WITH NO DISCREPANCIES NOTED AT THIS TIME. WORK PERFORMED REF AMM 32-44-20 AND AMM 32-44-00.

Part: RADIO — MALFUNCTIONED (NR 1) · airframe 13,115 hrs · 8,964 cycles

AT APPROXIMATELY FL230 CLIMBING, ENROUTE TO FRG, EXPERIENCED TOTAL PASS OF COMMS WHERE BOTH SEATS AND BOTH RADIO 1 AND COULD NOT TRANSMIT AND/OR RECEIVE RADIO COMMUNICATIONS SQUELCH WAS INCREDIBLY LOUD AND EAR PIERCING. DID WHAT TROUBLESHOOTING THAT THEY COULD BEFORE SQUAWKING 7600. TURNED BACK TO SUA AND WAS ABLE TO ESTABLISH POOR COMMUNICATION WITH ATC, BUT ONLY FROM THE RIGHT SEAT. AN EMERGENCY WAS DECLARED. WENT INTO MX AND CND.

Part: DOOR SEAL — FAILED (ZONE 800) · airframe 14,125 hrs · 9,615 cycles

WHILE CLIMBING OUT OF OGS THROUGH ABOUT 20,000 FT, WE STARTED HEARING A LIGHT WHISTLE FROM THE CABIN. R&R MED PRIMARY AND SECONDARY SEALS.

Part: BYPASS SWITCH — FAILED (ZONE 400) · airframe 10,089 hrs · 6,737 cycles

DURING CLIMB I RECEIVED A CASS MESSAGE, FUEL FILTER BYPASS L. R&R LH FUEL FILTER AND FUEL FILTER BYPASS SWITCH.

Part: HOSE — FAILED (ZONE 200) · airframe 16,271 hrs · 12,342 cycles

THE YAW DAMPER AND AUTOPILOT DISCONNECTED. WE HAD A YELLOW IAS MISCOMPARE INDICATION. R&R #2 PITOT HOSE, R&R LH/RH STATIC DRAIN PACKINGS

Part: ACTUATOR — LOOSE (ZONE 700) · airframe 12,930 hrs · 8,475 cycles

LANDING GEAR WILL NOT RETRACT AFTER TAKEOFF ( RED GEAR UNLOCK LIGHT REMAIN ON) FOLLOWED WITH QRH PROBLEM REMAINED. RETURNED BACK TO RBD AIRPORT SAFELY.//////DISCOVERED LH MAIN LANDING GEAR ACTUATOR JAM NUT TO BE LOOSE PERFORMED ROD ENG ADJUSTMENT AND SECURED JAM NUT

Part: BRACKET — BENT (ZONE 700) · airframe 9,037 hrs · 6,233 cycles

IMMEDIATELY FOLLOWING TAKEOFF FROM KSYR, THE LANDING GEAR HANDLE WAS SELECTED UP. THE LANDING GEAR FAILED TO RETRACT, AND THE RED GEAR UNLOCKED LIGHT REMAINED ILLUMINATED. R&R NLG BRACKET ASSY WITH NEW BRACKET AND ADJUSTED AND SECURED LH MLG ACTUATOR LOCK NUT AND SAFETY WIRED

Part: PROXIMITY SENSOR — OUT OF ADJUST (ZONE 700) · airframe 3,181 hrs · 2,074 cycles

WOW FAIL GEAR WILL NOT RETRACT. PERFORMED OPERTIONAL TEST OF THE PROXIMITY SENSORS & ADJUSTED PROXIMITY SENSORS IAW AMM 32-61-00. OP CHECKED GOOD.

Part: PRESSURE SWITCH — FAILED (ZONE 400 FUEL) · airframe 15,793 hrs · 11,128 cycles

ON THE TAKEOFF ROLL PRIOR TO 80, THE R LO FUEL PRESS ILLUMINATED FOLLOWED IMMEDIATELY BY R FUEL BOOST LIGHT.

Part: ACM — FALSE INDICATION (ZONE 100) · airframe 10,893 hrs · 8,981 cycles

DURING TAKEOFF AT 100 FEET ACM OVERHEAT LIGHT ILLUMINATED ALONG WITH AN ODOR OF PLASTIC MELTING. TROUBLE SHOT AND COULD NOT DUPLICATE.

Part: OUTFLOW VALVE — FAILED (ZONE 100) · airframe 1,382 hrs · 953 cycles

CABI ALT HIGH CAS/DEPRESSURIZATION AT FL290. EXECUTED EMERGENCY PROCEDURES AND DIVERTED TO FXE. /R & R OUTFLOW VALVE.

Part: OUTFLOW VALVE — FAILED (ZONE 100) · airframe 1,382 hrs · 953 cycles

CABI ALT HIGH CAS/DEPRESSURIZATION AT FL290. R&R OUTFLOW VALVE.

Part: BRACKET — BENT (ZONE 700) · airframe 8,763 hrs · 5,980 cycles

AFTER TAKEOFF WITH THE GEAR HANDLE SELECTED IN UP POSITION THE GEAR UNLOCK LIGHT REMAINS ILLUMINATED. FOUND NOSE GEAR FORK MOUNTED UPLOCK ROLLER BRACKETS BENT DOWN OVER 1/16 OF AN INCH CAUSING IMPROPER TOO LITTLE CONTACT TO THE NOSE UPLOCK SWITCH, R & R BRACKET

Part: CONTROL VALVE — FAILED (ZONE 700) · airframe 10,879 hrs · 8,972 cycles

THE GEAR UNLOCK LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. REMOVED LANDING GEAR CONTROL VALVE P/N 71839-1 S/N 0110 AND INSTALLED OVERHAULED LANDING GEAR CONTROL VALVE P/N 71839-1 S/N 0111,

Part: UPLOCK SWITCH — FAILED (ZONE 700) · airframe 8,375 hrs · 6,983 cycles

GEAR UNLOCK LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. R & R LH MLG UPLOCK SWITCH

Part: SWITCH — DIRTY (THRUST REVERSERS) · airframe 10,696 hrs · 6,735 cycles

ON DEPARTURE AT 2000 FEET T/R LIGHT ARM, AND UNLOCKED CAME ON, WITH ASSOCIATED HYDRAULIC PRESSURE CAS MESSAGE. CLEANED AND INSPECTED TR SWITCHES, FUNCTION CHECK, NDF

Part: OIL COOLER — FAILED (LT ENGINE) · airframe 13,013 hrs · 8,893 cycles

RECEIVED RED OIL PRESSURE INDICATION (POINTER AND DIGITS) LEFT ENGINE IN FLIGHT. SHUT DOWN LEFT ENGINE, DECLARED AN EMERGENCY AND DIVERTED TO KCHS. FOLLOWED CHECKLIST PAGES D4 LOW OIL PRESSURE INDICATION, A2 ENGINE FAILURE/SHUTDOWN AND Y1 SINGLE ENGINE APPROACH AND LANDING. LANDED WITHOUT INCIDENT. REMOVED LEFT ENGINE OIL COOLER AND REPLACED WITH REPAIRED UNIT.

Part: ACM — OVERTEMP (ZONE 100) · airframe 9,013 hrs · 6,514 cycles

ACM OVHT AND EMERGENCY PRESSURIZATION ON TAKEOFF. R & R ACM.

Part: BYPASS VALVE — FAILED (ZONE 100) · airframe 7,277 hrs · 7,257 cycles

CABIN TEMPERATURE UNCONTROLLABLE. R&R LOW LIMIT BYPASS VALVE

Part: ELEC CONNECTOR — DIRTY (ZONE 700) · airframe 10,791 hrs · 8,922 cycles

NOSE GEAR WOULD NOT RETRACT, COMPLIED WITH ABNORMAL PROCEDURES CHECKLIST. CLEANED NLG UP-LOCK CONNECTOR PLUG ON UP-LOCK

Part: CABLE — OUT OF ADJUST (ZONE 700) · airframe 8,320 hrs · 6,950 cycles

DURING CLIMB OUT WE RETRACTED THE LANDING GEAR, THE UNLOCK LIGHT WOULD NOT EXTINGUISH. WE RAN THROUGH THE CHECKLIST DID ALL THE PROPER PROCEDURES AND UNLOCK LIGHT STAYED ILLUMINATED. FOUND GEAR BLOW DOWN CABLE INSTALLED ON AFT SIDE OF UPLOCK BRACKET CAUSING CONTACT WITH WHEEL WELL WHEN ACUATED. INSTALLED CABLE ON FORWARD SIDE OF BRACKET IAW AMM 32-30-08, OPS CHECK GOOD.

Part: HOOK — FAILED (ZONE 700) · airframe 2,554 hrs · 1,613 cycles

DESCENDING THROUGH FL 220 AT APPROX 230 KIAS, RECEIVED RED LANDING GEAR LIGHT FOLLOWED BY A RUMBLE SOUND AND THE AMBER HYD PRESS ON MESSAGE.//////////REMOVED FAILED PART NO: 6341356-1-1 REMOVED SERIAL NO: NSN. INSTALLED NEW UPLOCK HOOK ASSEMBLY IAW CESSNA 5258 MM CH.23-31-04. OPS CHECKS GOOD.

Part: MOUNT — WORN (ZONE 300) · airframe 6,311 hrs · 4,639 cycles

PITCH TRIM FREEZING IN CLIMB AND DESCENT FROM FL430. REMOVED AND REPLACED ELEVATOR TRIM SERVO MOUNT IAW AMM 27-30-02.

Part: UPLOCK SWITCH — FAILED (ZONE 700) · airframe 5,457 hrs · 3,584 cycles

AFTER TAKEOFF WE RETRACTED THE GEAR AND THE NOSE GEAR LIGHT REMAINED ILLUMINATED AND THE MAIN GEAR LIGHTS EXTINGUISHED. R & R NOSE GEAR UPLOCK SWITCH, OPS CHECK GOOD.

Part: WINDSHIELD — CRACKED (ZONE 200) · airframe 9,765 hrs · 6,675 cycles

WHILE DESCENDING ON THE ARRIVAL TO KELP, AT ABOUT FL240, THE LEFT WINDSHIELD OUTER LAYER CRACKED/SHATTERED.

Part: STATIC LINE — FAULTED (ZONE 100)

WE LOST THE CAPTAIN AND FO’S ALTITIMER, ALTITUDE SELECT AT NIGHT IN MOUNTAINOUS TERRAIN. PURGED PILOT AND COPILOT STATIC SYSTEM, FOUND PILOT SIDE FITTING ON THE MOISTURE DRAIN VALVE LOOSE.

Part: BRACKET — WORN (ZONE 700) · airframe 6,552 hrs · 9,352 cycles

ON RETRACTING THE MLG WE FELT AND HEARD A LOUD VIBRATION THAT SEEMED TO BE COMING FROM THE NOSE GEAR. IT WAS ACCOMPANIED BY THE GEAR UNSAFE LIGHT FLASHING IN RHYTHM WITH THE SOUND THAT EVENTUALLY EXTINGUISHED WITH THE HYDRAULIC ANNUNCIATOR. REPLACED NLG UPLOCK BRACKET, OPS CHECK GOOD

Part: ACTUATOR — FAILED (ZONE 700) · airframe 10,094 hrs · 7,379 cycles

DURING LANDING DROPPED THE LANDING GEAR AND RECEIVED A RED UNLOCK GEAR LIGHT ASSOCIATED WITH A GREEN LEFT MAIN LANDING GEAR LIGHT THAT DID NOT ILLUMINATE.///////R&R LH MLG ACTUATOR.

Part: UPLOCK SWITCH — OUT OF RIG (ZONE 700) · airframe 11,861 hrs · 7,761 cycles

GEAR SELECTED UP. GEAR WOULD NOT RETRACT….STILL HAD 3 GREEN, NO RED. SUCCESSFULLY RIGGED NLG UPLOCK SWITCH, OPERATIONAL CHECK GOOD

Part: ENGINE — FAILED (LEFT) · airframe 3,190 hrs · 1,799 cycles

AT APPROX 400 FEET WE HAD A LEFT ENGINE EXCEEDANCE WITH RED CAS MESSAGE, AND THE ENGINE WENT TO IDLE. ENGINE REMOVED FOR REPAIR

Part: VALVE — FAILED (RT ENGINE) · airframe 11,172 hrs · 8,791 cycles

DURING TAKE-OFF, APPLIED TAKE-OFF POWER, AND THE PRESSURIZATION CLIMB RATE WENT TO -1000 FPM. REMOVED AND REPLACED RT ENG BI LEVEL FLOW VALVE, OPS CHKD GOOD.

Part: UPLOCK — DAMAGED (ZONE 700) · airframe 2,421 hrs · 1,537 cycles

IN FLIGHT FROM APF TO 07FA AT 13,000 FT. FELT A BANG AND GOT “GEAR UNLOCKED” LIGHT. R & R DAMAGED RT MLG UPLOCK WITH A NEW UPLOCK ASSY, OPS CHECKED GOOD WITH NO DEFECTS NOTED AT THIS TIME. WORK PERFORMED !AW AMM 32·31-04.

Part: UNKNOWN — ODOR (CABIN) · airframe 6,291 hrs · 4,625 cycles

MASTER CAUTION ILLUMINATED ALONG WITH AURAL WARNING REFERENCED QRH. THEN GOT A BURNING SMELL THROUGHOUT THE AIRCRAFT, DECLARED AN EMERGENCY DIVERTED TO CHARLESTON INTERNATIONAL AIRPORT CHARLESTON. PERFORMED SEVERAL ENGINE RUNS WITH BLEEDS ON, CND.

Part: CONTROL VALVE — FAILED (ZONE 700) · airframe 5,895 hrs · 5,452 cycles

AFTER NORMAL LANDING FROM RIGHT SIDE APPLIED BRAKES, ANTI SKID LIGHT CAME ON AND BRAKES DID NOT ACTUATE. R & R ANTISKID CONTROL VALVE P/N ON 9912621-3, S/N ON 868, NEW & BLED BRAKE SYSTEM IAW