Flexjet, LLC

Operated by FLEXJET LLC (per NTSB report)

The control laws of the angle of attack limiter protection system, which precluded the system from disengaging during an approach in gusting wind conditions, limiting the flight crew’s ability to control the airplane’s pitch and resulting in a hard landing.

Operated by FLEXJET LLC (per NTSB report)

An unanticipated encounter with convective induced turbulence from developing cumulus clouds below the flight path, which produced strong updrafts and downdrafts.

Part: FCE — FAULTED (FLT CONTROLS) · airframe 7,152 hrs · 4,813 cycles

CREW REPORTS FCE2 CIRCUIT BREAKER POPS UPON POWERING ON AIRCRAFT. REPLACED FCE 2 WITH IAW AMM 27-05-01. SPOILER RIG AND OPS TEST SATISFACTORY IAW 27-60-00.

Part: ACM — OVERTEMP (ZONE 100) · airframe 18,351 hrs · 11,304 cycles

DIVERSION DUE TO PACK TEMP HIGH CAS WITH A HIGH PITCH WHISTLE FROM THE VENTS, A LIGHT BURNING ODOR AND RISING CABIN TEMPERATURE, NOTED WHILE EXECUTING A MISSED APPROACH AT KOXC. CREW CONTINUED TO KHPN. REPLACED AIR CYCLE MACHINE IAW BD 100 AMM 21-52-13. OPS CHECK AND LEAK CHECK GOOD IAW AMM 21-52-00.

Part: HYDRAULIC LINE — LEAKING (ZONE 100) · airframe 10,392 hrs · 5,436 cycles

AIR TURN BACK DUE TO LH HYD FAIL CAS AFTER TAKEOFF FROM KAUS, WITH ALL LEFT SYSTEM QUANTITY LOST; A LARGE AMOUNT OF HYDRAULIC FLUID WAS FOUND LEAKING ON THE GROUND AFTER LANDING. REPLACED RH SIDE STAY ACTUATOR RETURN LINE HOSE IAW GULFSTREAM G450 AMM 32-14-01. LEAK CHECK GOOD, NO DEFECTS NOTED.

Part: RADIO — FAULTED · airframe 7,838 hrs · 5,209 cycles

CREW REPORTS MULTIPLE HSDB FAULTS, GRD SPOILER FAIL CAS, AND YELLOW “X’S” ON ENGINE INSTRUMENTS. THIS AIRCRAFT IS ONE OF 17 EMBRAER PHENOM 300 AIRCRAFT IN THE FLEXJET FLEET THAT IS EQUIPPED WITH P/N 011-03177-10 XM RADIO AND AVIONICS SOFTWARE LOAD 18.10. IN THIS CONFIGURATION, THE RECEIVER CAN GO INTO RESET MODE WHEN IT RECEIVES CERTAIN PACKETS OF DATA FROM SIRIUS XM. DURING A XM RADIO RESET, IT DRAWS DOWN THE HSDB, RESULTING IN SOME OR ALL OF FOLLOWING CAS MESSAGES: HSDB FAULT, ENGINE NO DISPATCH, E2 TT0 HTR FAIL, GND SPLR FAIL. FURTHER, IT CAN DRIVE THE FOLLOWING GTC MESSAGES: GDL69 FAIL AND FAILED DATA PATH. LASTLY, THE FOLLOWING MFD ENGINE INDICATIONS MAY BE PRESENT: YELLOW X OVER E1 AND E2 OIL PRESSURE, YELLOW X OVER N1 AND N2 ENGINE, YELLOW X OVER LH AND RH ITT, YELLOW X OVER LFE VALUE. EMBRAER IS INVESTIGATING (CASE # EEJ-05526497). XM RADIO DISABLED AND PLACED ON MEL.

Part: POSITION UNIT — FAULTED (ZONE 100) · airframe 8,474 hrs · 5,787 cycles

DISCOVERED AIRCRAFT SUSCEPTIBLE TO HIGH SPEED DATA BUS (HSDB) ISSUE CAUSED BY A FAILURE OF THE XM RADIO RECEIVER. THIS AIRCRAFT IS ONE OF 17 EMBRAER PHENOM 300 AIRCRAFT IN THE FLEXJET FLEET THAT IS EQUIPPED WITH XM RADIO AND AVIONICS SOFTWARE LOAD 18.10. IN THIS CONFIGURATION, THE RECEIVER CAN GO INTO RESET MODE WHEN IT RECEIVES CERTAIN PACKETS OF DATA FROM SIRIUS XM. DURING A XM RADIO RESET, IT DRAWS DOWN THE HSDB, RESULTING IN SOME OR ALL OF FOLLOWING CAS MESSAGES: HSDB FAULT, ENGINE NO DISPATCH, E2 TT0 HTR FAIL, GND SPLR FAIL. FURTHER, IT CAN DRIVE THE FOLLOWING GTC MESSAGES: GDL69 FAIL AND FAILED DATA PATH. LASTLY, THE FOLLOWING MFD ENGINE INDICATIONS MAY BE PRESENT: YELLOW X OVER E1 AND E2 OIL PRESSURE, YELLOW X OVER N1 AND N2 ENGINE, YELLOW X OVER LT AND RT ITT, YELLOW X OVER LFE VALUE.

Part: POSITION UNIT — FAULTED (ZONE 100) · airframe 7,143 hrs · 4,738 cycles

DISCOVERED AIRCRAFT SUSCEPTIBLE TO HIGH SPEED DATA BUS (HSDB) ISSUE CAUSED BY A FAILURE OF THE XM RADIO RECEIVER. THIS AIRCRAFT IS ONE OF 17 EMBRAER PHENOM 300 AIRCRAFT IN THE FLEXJET FLEET THAT IS EQUIPPED WITH XM RADIO AND AVIONICS SOFTWARE LOAD 18.10. IN THIS CONFIGURATION, THE RECEIVER CAN GO INTO RESET MODE WHEN IT RECEIVES CERTAIN PACKETS OF DATA FROM SIRIUS XM. DURING A XM RADIO RESET, IT DRAWS DOWN THE HSDB, RESULTING IN SOME OR ALL OF FOLLOWING CAS MESSAGES: HSDB FAULT, ENGINE NO DISPATCH, E2 TT0 HTR FAIL, GND SPLR FAIL. FURTHER, IT CAN DRIVE THE FOLLOWING GTC MESSAGES: GDL69 FAIL AND FAILED DATA PATH. LASTLY, THE FOLLOWING MFD ENGINE INDICATIONS MAY BE PRESENT: YELLOW X OVER E1 AND E2 OIL PRESSURE, YELLOW X OVER N1 AND N2 ENGINE, YELLOW X OVER LH AND RH ITT, YELLOW X OVER LFE VALUE.

Part: POSITION UNIT — FAULTED (ZONE 100) · airframe 7,525 hrs · 5,094 cycles

DISCOVERED AIRCRAFT SUSCEPTIBLE TO HIGH SPEED DATA BUS (HSDB) ISSUE CAUSED BY A FAILURE OF THE XM RADIO RECEIVER. THIS AIRCRAFT IS ONE OF 17 EMBRAER PHENOM 300 AIRCRAFT IN THE FLEXJET FLEET THAT IS EQUIPPED WITH XM RADIO AND AVIONICS SOFTWARE LOAD 18.10. IN THIS CONFIGURATION, THE RECEIVER CAN GO INTO RESET MODE WHEN IT RECEIVES CERTAIN PACKETS OF DATA FROM SIRIUS XM. DURING A XM RADIO RESET, IT DRAWS DOWN THE HSDB, RESULTING IN SOME OR ALL OF FOLLOWING CAS MESSAGES: HSDB FAULT, ENGINE NO DISPATCH, E2 TT0 HTR FAIL, GND SPLR FAIL. FURTHER, IT CAN DRIVE THE FOLLOWING GTC MESSAGES: GDL69 FAIL AND FAILED DATA PATH. LASTLY, THE FOLLOWING MFD ENGINE INDICATIONS MAY BE PRESENT: YELLOW X OVER E1 AND E2 OIL PRESSURE, YELLOW X OVER N1 AND N2 ENGINE, YELLOW X OVER LH AND RH ITT, YELLOW X OVER LFE VALUE.

Part: POSITION UNIT — FAULTED (ZONE 100) · airframe 5,823 hrs · 4,051 cycles

DISCOVERED AIRCRAFT SUSCEPTIBLE TO HIGH SPEED DATA BUS (HSDB) ISSUE CAUSED BY A FAILURE OF THE XM RADIO RECEIVER. THIS AIRCRAFT IS ONE OF 17 EMBRAER PHENOM 300 AIRCRAFT IN THE FLEXJET FLEET THAT IS EQUIPPED WITH XM RADIO AND AVIONICS SOFTWARE LOAD 18.10. IN THIS CONFIGURATION, THE RECEIVER CAN GO INTO RESET MODE WHEN IT RECEIVES CERTAIN PACKETS OF DATA FROM SIRIUS XM. DURING A XM RADIO RESET, IT DRAWS DOWN THE HSDB, RESULTING IN SOME OR ALL OF FOLLOWING CAS MESSAGES: HSDB FAULT, ENGINE NO DISPATCH, E2 TT0 HTR FAIL, GND SPLR FAIL. FURTHER, IT CAN DRIVE THE FOLLOWING GTC MESSAGES: GDL69 FAIL AND FAILED DATA PATH. LASTLY, THE FOLLOWING MFD ENGINE INDICATIONS MAY BE PRESENT: YELLOW X OVER E1 AND E2 OIL PRESSURE, YELLOW X OVER N1 AND N2 ENGINE, YELLOW X OVER LH AND RH ITT, YELLOW X OVER LFE VALUE.

Part: POSITION UNIT — FAULTED (ZONE 100) · airframe 4,071 hrs · 2,941 cycles

DISCOVERED AIRCRAFT SUSCEPTIBLE TO HIGH SPEED DATA BUS (HSDB) ISSUE CAUSED BY A FAILURE OF THE XM RADIO RECEIVER. THIS AIRCRAFT IS ONE OF 17 EMBRAER PHENOM 300 AIRCRAFT IN THE FLEXJET FLEET THAT IS EQUIPPED WITH XM RADIO AND AVIONICS SOFTWARE LOAD 18.10. IN THIS CONFIGURATION, THE RECEIVER CAN GO INTO RESET MODE WHEN IT RECEIVES CERTAIN PACKETS OF DATA FROM SIRIUS XM. DURING A XM RADIO RESET, IT DRAWS DOWN THE HSDB, RESULTING IN SOME OR ALL OF FOLLOWING CAS MESSAGES: HSDB FAULT, ENGINE NO DISPATCH, E2 TT0 HTR FAIL, GND SPLR FAIL. FURTHER, IT CAN DRIVE THE FOLLOWING GTC MESSAGES: GDL69 FAIL AND FAILED DATA PATH. LASTLY, THE FOLLOWING MFD ENGINE INDICATIONS MAY BE PRESENT: YELLOW X OVER E1 AND E2 OIL PRESSURE, YELLOW X OVER N1 AND N2 ENGINE, YELLOW X OVER LH AND RH ITT, YELLOW X OVER LFE VALUE.

Part: POSITION UNIT — FAULTED (ZONE 100) · airframe 4,078 hrs · 2,995 cycles

DISCOVERED AIRCRAFT SUSCEPTIBLE TO HIGH SPEED DATA BUS (HSDB) ISSUE CAUSED BY A FAILURE OF THE XM RADIO RECEIVER. THIS AIRCRAFT IS ONE OF 17 EMBRAER PHENOM 300 AIRCRAFT IN THE FLEXJET FLEET THAT IS EQUIPPED WITH XM RADIO AND AVIONICS SOFTWARE LOAD 18.10. IN THIS CONFIGURATION, THE RECEIVER CAN GO INTO RESET MODE WHEN IT RECEIVES CERTAIN PACKETS OF DATA FROM SIRIUS XM. DURING A XM RADIO RESET, IT DRAWS DOWN THE HSDB, RESULTING IN SOME OR ALL OF FOLLOWING CAS MESSAGES: HSDB FAULT, ENGINE NO DISPATCH, E2 TT0 HTR FAIL, GND SPLR FAIL. FURTHER, IT CAN DRIVE THE FOLLOWING GTC MESSAGES: GDL69 FAIL AND FAILED DATA PATH. LASTLY, THE FOLLOWING MFD ENGINE INDICATIONS MAY BE PRESENT: YELLOW X OVER E1 AND E2 OIL PRESSURE, YELLOW X OVER N1 AND N2 ENGINE, YELLOW X OVER LH AND RH ITT, YELLOW X OVER LFE VALUE.

Part: RADIO — FAULTED · airframe 5,176 hrs · 3,692 cycles

CREW RECEIVED INTERMITTENT HSDB FAULTS IN FLIGHT. THIS AIRCRAFT IS ONE OF 17 EMBRAER PHENOM 300 AIRCRAFT IN THE FLEXJET FLEET THAT IS EQUIPPED WITH P/N 011-03177-10 XM RADIO AND AVIONICS SOFTWARE LOAD 18.10. IN THIS CONFIGURATION, THE RECEIVER CAN GO INTO RESET MODE WHEN IT RECEIVES CERTAIN PACKETS OF DATA FROM SIRIUS XM. DURING A XM RADIO RESET, IT DRAWS DOWN THE HSDB, RESULTING IN SOME OR ALL OF FOLLOWING CAS MESSAGES: HSDB FAULT, ENGINE NO DISPATCH, E2 TT0 HTR FAIL, GND SPLR FAIL. FURTHER, IT CAN DRIVE THE FOLLOWING GTC MESSAGES: GDL69 FAIL AND FAILED DATA PATH. LASTLY, THE FOLLOWING MFD ENGINE INDICATIONS MAY BE PRESENT: YELLOW X OVER E1 AND E2 OIL PRESSURE, YELLOW X OVER N1 AND N2 ENGINE, YELLOW X OVER LH AND RH ITT, YELLOW X OVER LFE VALUE. EMBRAER IS INVESTIGATING (CASE # EEJ-05526497). XM RADIO DISABLED AND PLACED ON MEL.

Part: RADIO — FAULTED · airframe 4,902 hrs · 3,443 cycles

CREW RECEIVED INTERMITTENT HSDB FAULTS ON GROUND. THIS AIRCRAFT IS ONE OF 17 AIRCRAFT IN THE FLEXJET FLEET THAT IS EQUIPPED WITH XM RADIO AND AVIONICS SOFTWARE LOAD 18.10. IN THIS CONFIGURATION, THE RECEIVER CAN GO INTO RESET MODE WHEN IT RECEIVES CERTAIN PACKETS OF DATA FROM SIRIUS XM. DURING A XM RADIO RESET, IT DRAWS DOWN THE HSDB, RESULTING IN SOME OR ALL OF FOLLOWING CAS MESSAGES: HSDB FAULT, ENGINE NO DISPATCH, E2 TT0 HTR FAIL, GND SPLR FAIL. FURTHER, IT CAN DRIVE THE FOLLOWING GTC MESSAGES: GDL69 FAIL AND FAILED DATA PATH. LASTLY, THE FOLLOWING MFD ENGINE INDICATIONS MAY BE PRESENT: YELLOW X OVER E1 AND E2 OIL PRESSURE, YELLOW X OVER N1 AND N2 ENGINE, YELLOW X OVER LH AND RH ITT, YELLOW X OVER LFE VALUE. EMBRAER IS INVESTIGATING (CASE # EEJ-05526497). XM RADIO DISABLED AND PLACED ON MEL.

Part: RADIO — FAULTED

CREW RECEIVED INTERMITTENT HSDB FAULTS IN FLIGHT. THIS AIRCRAFT IS ONE OF 17 EMBRAER PHENOM 300 AIRCRAFT IN THE FLEXJET FLEET THAT IS EQUIPPED WITH XM RADIO AND AVIONICS SOFTWARE LOAD 18.10. IN THIS CONFIGURATION, THE RECEIVER CAN GO INTO RESET MODE WHEN IT RECEIVES CERTAIN PACKETS OF DATA FROM SIRIUS XM. DURING A XM RADIO RESET, IT DRAWS DOWN THE HSDB, RESULTING IN SOME OR ALL OF FOLLOWING CAS MESSAGES: HSDB FAULT, ENGINE NO DISPATCH, E2 TT0 HTR FAIL, GND SPLR FAIL. FURTHER, IT CAN DRIVE THE FOLLOWING GTC MESSAGES: GDL69 FAIL AND FAILED DATA PATH. LASTLY, THE FOLLOWING MFD ENGINE INDICATIONS MAY BE PRESENT: YELLOW X OVER E1 AND E2 OIL PRESSURE, YELLOW X OVER N1 AND N2 ENGINE, YELLOW X OVER LH AND RH ITT, YELLOW X OVER LFE VALUE. IS INVESTIGATING (CASE # EEJ-05526497). XM RADIO DISABLED AND PLACED ON MEL.

Part: RADIO — FAULTED · airframe 3,962 hrs · 2,780 cycles

CREW RECEIVED INTERMITTENT HSDB FAULTS IN FLIGHT. THIS AIRCRAFT IS ONE OF 17 EMBRAER PHENOM 300 AIRCRAFT IN THE FLEXJET FLEET THAT IS EQUIPPED WITH P/N 011-03177-10 XM RADIO AND AVIONICS SOFTWARE LOAD 18.10. IN THIS CONFIGURATION, THE RECEIVER CAN GO INTO RESET MODE WHEN IT RECEIVES CERTAIN PACKETS OF DATA FROM SIRIUS XM. DURING A XM RADIO RESET, IT DRAWS DOWN THE HSDB, RESULTING IN SOME OR ALL OF FOLLOWING CAS MESSAGES: HSDB FAULT, ENGINE NO DISPATCH, E2 TT0 HTR FAIL, GND SPLR FAIL. FURTHER, IT CAN DRIVE THE FOLLOWING GTC MESSAGES: GDL69 FAIL AND FAILED DATA PATH. LASTLY, THE FOLLOWING MFD ENGINE INDICATIONS MAY BE PRESENT: YELLOW X OVER E1 AND E2 OIL PRESSURE, YELLOW X OVER N1 AND N2 ENGINE, YELLOW X OVER LH AND RH ITT, YELLOW X OVER LFE VALUE. EMBRAER IS INVESTIGATING (CASE # EEJ-05526497). XM RADIO DISABLED AND PLACED ON MEL.

Part: RADIO — FAULTED · airframe 8,277 hrs · 5,686 cycles

CREW REPORTS HSDB FAULT CAS MESSAGE DISPLAYED IN FLIGHT AND ON GROUND, ACCOMPANIED BY NUMEROUS OTHER CAS MESSAGES. THIS AIRCRAFT IS ONE OF 17 EMBRAER PHENOM 300 AIRCRAFT IN THE FLEXJET FLEET THAT IS EQUIPPED WITH P/N 011-03177-10 XM RADIO AND AVIONICS SOFTWARE LOAD 18.10. IN THIS CONFIGURATION, THE RECEIVER CAN GO INTO RESET MODE WHEN IT RECEIVES CERTAIN PACKETS OF DATA FROM SIRIUS XM. DURING A XM RADIO RESET, IT DRAWS DOWN THE HSDB, RESULTING IN SOME OR ALL OF FOLLOWING CAS MESSAGES: HSDB FAULT, ENGINE NO DISPATCH, E2 TT0 HTR FAIL, GND SPLR FAIL. FURTHER, IT CAN DRIVE THE FOLLOWING GTC MESSAGES: GDL69 FAIL AND FAILED DATA PATH. LASTLY, THE FOLLOWING MFD ENGINE INDICATIONS MAY BE PRESENT: YELLOW X OVER E1 AND E2 OIL PRESSURE, YELLOW X OVER N1 AND N2 ENGINE, YELLOW X OVER LH AND RH ITT, YELLOW X OVER LFE VALUE. EMBRAER IS INVESTIGATING (CASE # EEJ-05526497). XM RADIO DISABLED AND PLACED ON MEL.

Part: RADIO — FAULTED · airframe 7,710 hrs · 5,140 cycles

ON DEPARTURE CLIMB, CREW RECEIVED RECEIVED GROUND SPOILER FAIL, HSDB FAULT, AND ENGINE NO DISPATCH CAS ACCOMPANIED BY YELLOW X'S OVER ENG 2'S OIL PRESSURE AND TEMPERATURE INDICATORS. ALL CAS AND YELLOW X'S EXTINGUISHED AFTER A FEW SECONDS. THIS HAS HAPPENED THREE TIMES IN CRUISE. ON DESCENT, CREW RECEIVED THE SAME CAS MESSAGES AND NOTED ALL N1, ITT, AND OIL TEMP/PRESSURE INDICATIONS FOR BOTH ENGINES HAD YELLOW X'S. THIS AIRCRAFT IS ONE OF 17 EMBRAER PHENOM 300 AIRCRAFT IN THE FLEXJET FLEET THAT IS EQUIPPED WITH P/N 011-03177-10 XM RADIO AND AVIONICS SOFTWARE LOAD 18.10. IN THIS CONFIGURATION, THE RECEIVER CAN GO INTO RESET MODE WHEN IT RECEIVES CERTAIN PACKETS OF DATA FROM SIRIUS XM. DURING A XM RADIO RESET, IT DRAWS DOWN THE HSDB, RESULTING IN SOME OR ALL OF FOLLOWING CAS MESSAGES: HSDB FAULT, ENGINE NO DISPATCH, E2 TT0 HTR FAIL, GND SPLR FAIL. FURTHER, IT CAN DRIVE THE FOLLOWING GTC MESSAGES: GDL69 FAIL AND FAILED DATA PATH. LASTLY, THE FOLLOWING MFD ENGINE INDICATIONS MAY BE PRESENT: YELLOW X OVER E1 AND E2 OIL PRESSURE, YELLOW X OVER N1 AND N2 ENGINE, YELLOW X OVER LH AND RH ITT, YELLOW X OVER LFE VALUE. EMBRAER IS INVESTIGATING (CASE # EEJ-05526497). XM RADIO DISABLED AND PLACED ON MEL.

Part: RADIO — FAULTED · airframe 7,102 hrs · 4,773 cycles

CREW RECEIVED MULTIPLE CAS MESSAGES IN FLIGHT: HSDB FAULT, ENGINE NO DISPATCH, E2 TT0 HTR FAIL, AND GRND SPOILER FAULT. IN ADDITION, YELLOW ‘X’S” APPEARED OVER ENG 2 OIL PRES AND OIL TEMP. THIS AIRCRAFT IS ONE OF 17 EMBRAER PHENOM 300 AIRCRAFT IN THE FLEXJET FLEET THAT IS EQUIPPED WITH P/N 011-03177-10 XM RADIO AND AVIONICS SOFTWARE LOAD 18.10. IN THIS CONFIGURATION, THE RECEIVER CAN GO INTO RESET MODE WHEN IT RECEIVES CERTAIN PACKETS OF DATA FROM SIRIUS XM. DURING A XM RADIO RESET, IT DRAWS DOWN THE HSDB, RESULTING IN SOME OR ALL OF FOLLOWING CAS MESSAGES: HSDB FAULT, ENGINE NO DISPATCH, E2 TT0 HTR FAIL, GND SPLR FAIL. FURTHER, IT CAN DRIVE THE FOLLOWING GTC MESSAGES: GDL69 FAIL AND FAILED DATA PATH. LASTLY, THE FOLLOWING MFD ENGINE INDICATIONS MAY BE PRESENT: YELLOW X OVER E1 AND E2 OIL PRESSURE, YELLOW X OVER N1 AND N2 ENGINE, YELLOW X OVER LH AND RH ITT, YELLOW X OVER LFE VALUE. EMBRAER IS INVESTIGATING (CASE # EEJ-05526497). XM RADIO DISABLED AND PLACED ON MEL.

Part: RADIO — FAULTED · airframe 6,057 hrs · 4,218 cycles

CREW REPORTS INTERMITTENT HSDB FAULTS DURING FLIGHT. THIS AIRCRAFT IS ONE OF 17 EMBRAER PHENOM 300 AIRCRAFT IN THE FLEXJET FLEET THAT IS EQUIPPED WITH P/N 011-03177-10 XM RADIO AND AVIONICS SOFTWARE LOAD 18.10. IN THIS CONFIGURATION, THE RECEIVER CAN GO INTO RESET MODE WHEN IT RECEIVES CERTAIN PACKETS OF DATA FROM SIRIUS XM. DURING A XM RADIO RESET, IT DRAWS DOWN THE HSDB, RESULTING IN SOME OR ALL OF FOLLOWING CAS MESSAGES: HSDB FAULT, ENGINE NO DISPATCH, E2 TT0 HTR FAIL, GND SPLR FAIL. FURTHER, IT CAN DRIVE THE FOLLOWING GTC MESSAGES: GDL69 FAIL AND FAILED DATA PATH. LASTLY, THE FOLLOWING MFD ENGINE INDICATIONS MAY BE PRESENT: YELLOW X OVER E1 AND E2 OIL PRESSURE, YELLOW X OVER N1 AND N2 ENGINE, YELLOW X OVER LH AND RH ITT, YELLOW X OVER LFE VALUE. EMBRAER IS INVESTIGATING (CASE # EEJ-05526497). XM RADIO DISABLED AND PLACED ON MEL.

Part: RADIO — FAULTED · airframe 4,369 hrs · 3,121 cycles

ON AIRCRAFT POWER UP, CREW RECEIVED MOMENTARY GND SPOILER, HSDB, AND ENG NO DISP MESSAGES. FAULTS CLEARED WITHOUT CREW INTERVENTION WITHIN 1-2 SECONDS. FAULTS REOCCURRED APPROXIMATELY EVERY 20-30 MINUTES THROUGHOUT THE FLIGHT. ROUGHLY 95 MINUTES AFTER TAKEOFF, CREW RECEIVED ENG NO DISPATCH AND LOSS OF ENG #2 OIL PRESSURE AND TEMPERATURE INDICATION. ABOUT 9 MINUTES LATER, PTRIM NML FAIL CAS ILLUMINATED. ON DESCENT, CREW RECEIVED MOMENTARY E2 TTO HTR FAIL AND HSDB MESSAGES. THIS AIRCRAFT IS ONE OF 17 EMBRAER PHENOM 300 AIRCRAFT IN THE FLEXJET FLEET THAT IS EQUIPPED WITH XM RADIO AND AVIONICS SOFTWARE LOAD 18.10. IN THIS CONFIGURATION, THE RECEIVER CAN GO INTO RESET MODE WHEN IT RECEIVES CERTAIN PACKETS OF DATA FROM SIRIUS XM. DURING A XM RADIO RESET, IT DRAWS DOWN THE HSDB, RESULTING IN SOME OR ALL OF FOLLOWING CAS MESSAGES: HSDB FAULT, ENGINE NO DISPATCH, E2 TT0 HTR FAIL, GND SPLR FAIL. FURTHER, IT CAN DRIVE THE FOLLOWING GTC MESSAGES: GDL69 FAIL AND FAILED DATA PATH. LASTLY, THE FOLLOWING MFD ENGINE INDICATIONS MAY BE PRESENT: YELLOW X OVER E1 AND E2 OIL PRESSURE, YELLOW X OVER N1 AND N2 ENGINE, YELLOW X OVER LH AND RH ITT, YELLOW X OVER LFE VALUE. EMBRAER IS INVESTIGATING (CASE # EEJ-05526497). XM RADIO DISABLED AND PLACED ON MEL.

Part: RADIO — FAULTED

CREW RECEIVED INTERMITTED GND SPLR FAIL AND HSDB FAULT CAS MESSAGES DURING FLIGHT. ENG NO DISPATCH, E2 TTO HTR FAIL CAS, AND RIGHT OIL PRESSURE TEMP YELLOW X'S DISPLAYED ENTIRE FLIGHT. THIS AIRCRAFT IS ONE OF 17 AIRCRAFT IN THE FLEXJET FLEET THAT IS EQUIPPED WITH XM RADIO AND AVIONICS SOFTWARE LOAD 18.10. IN THIS CONFIGURATION, THE RECEIVER CAN GO INTO RESET MODE WHEN IT RECEIVES CERTAIN PACKETS OF DATA FROM SIRIUS XM. DURING A XM RADIO RESET, IT DRAWS DOWN THE HSDB, RESULTING IN SOME OR ALL OF FOLLOWING CAS MESSAGES: HSDB FAULT, ENGINE NO DISPATCH, E2 TT0 HTR FAIL, GND SPLR FAIL. FURTHER, IT CAN DRIVE THE FOLLOWING GTC MESSAGES: GDL69 FAIL AND FAILED DATA PATH. LASTLY, THE FOLLOWING MFD ENGINE INDICATIONS MAY BE PRESENT: YELLOW X OVER E1 AND E2 OIL PRESSURE, YELLOW X OVER N1 AND N2 ENGINE, YELLOW X OVER LH AND RH ITT, YELLOW X OVER LFE VALUE. EMBRAER IS INVESTIGATING (CASE # EEJ-05526497). XM RADIO DISABLED AND PLACED ON MEL.

Part: FCE — FAULTED (ZONE 100) · airframe 9,920 hrs · 6,740 cycles

P-TRIM NML FAIL DURING TRIM TESTS. REPLACED FCE 2 AND PERFORMED SUCCESSFUL RIGGING AND OPS CHECK. WORK COMPLETED IAW EMB 505 AMM 27-03-01 AND 27-60-00.

Part: FCE — FAULTED (ZONE 100) · airframe 12,870 hrs · 8,788 cycles

ON SHORT FINAL TO LAND, CREW RECEIVED AUTO PTRIM FAIL, GND SPLR FAIL, SWPS FAULT, AND SPOILER FAULT CAS. AIRCRAFT LANDED WITHOUT INCIDENT AT KTRI. REPLACED FCE NR 2 IAW AMM 27-03-01. OPS CHECKED GOOD.

Part: ACTUATOR — UNSERVICEABLE (ZONE 300) · airframe 500 hrs · 267 cycles

DURING FLIGHT, CYAN FCS NO DISPATCH CAS POSTED. CREW WAS ABLE TO CLEAR AND LANDED WITHOUT INCIDENT. DOWNLOADS INDICATED THAT THE REU DETECTED A FORCE FIGHT BETWEEN ELEVATOR ACTUATORS, I.E., ELEVATOR ACTUATORS FORCING IN OPPOSITE DIRECTIONS ON THE SAME SURFACE OF THE ELEVATOR. REPLACED LEFT EBHA ACTUATOR IAW GULFSTREAM G500 AMM 27-33-02. REMOVED AND REPLACED REU #7 IAW AMM 27-04-01.

Part: FLT CONTROLS — MULTIPLE FAIL · airframe 11,106 hrs · 7,806 cycles

DIVERTED DUE TO SWPS FAULT, FLAP FAIL, PTRIM BKP FAIL, AND SPOILER FAULT MESSAGES AT FL410. THE CREW RAN THE QRH AND DIVERTED TO KSFB. AIRCRAFT LANDED WITHOUT INCIDENT AT KSFB. REPLACED FCE #1 IAW AMM 27-03-01.

Part: MICROWAVE OVEN — ODOR (ZONE 900) · airframe 1,852 hrs · 1,070 cycles

DIVERTED DUE TO A STRONG ELECTRICAL BURNING SMELL IN THE COCKPIT DURING CRUISE, ISOLATED TO THE GALLEY MICROWAVE OVERHEATING. THE CREW DISCONTINUED MICROWAVE USE AND DIVERTED TO LIML. AIRCRAFT LANDED WITHOUT INCIDENT AT LIML. REPLACED MICROWAVE IAW AMM 25-32-02. TESTED SATISFACTORY.

Part: ACM — FAULTED (ZONE 100) · airframe 4,678 hrs · 2,632 cycles

DURING CRUISE, CREW RECEIVED PACK TEMP HIGH CAS, HEARD A SQUEAL NOISE, AND NOTICED A BURNT SMELL. AIRCRAFT LANDED WITHOUT INCIDENT AT KDPA. FOUND AIR CYCLE MACHINE SEIZED. REPLACED ACM. OPS AND LEAK CHECKS SATISFACTORY. WORK COMPLETED IAW CL350 AMM 21-52-13.

Part: FCE — FAULTED (ZONE 100) · airframe 12,147 hrs · 8,376 cycles

DESCENDING THROUGH FL340 RECEIVED GND SPLR FAIL, PTRIM NML FAIL, AND SPOILER FAULT. CREW RAN QRH AND LANDED WITHOUT INCIDENT. REPLACED FCE #2. ALL OPS CHECKS GOOD. WORK COMPLETED IAW EMB 505 AMM 27-03-01.

Part: SKIN — DAMAGED (ZONE 200) · airframe 17,582 hrs · 10,919 cycles

COMPLIED WITH THE REPAIR LOCATED ON THE RIGHT SIDE OF THE FUSELAGE BETWEEN FS 384 & FS 422 I.A.W. ENGINEERING DWG SA-CL300-20160-M01 REV. IR,

Part: FCE — FAULTED (ZONE 100) · airframe 12,135 hrs · 8,350 cycles

CREW RECEIVED FLAPS FAIL, SWPS FAULT, PITCH TRIM BACK UP FAIL, AND SPOILER FAULT IN FLIGHT. AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED FCE1 IAW AMM 27-03-01. COMPLIED WITH FLAP RIGGING IAW AMM 27-50-00. FLAP AND PITCH TRIM OPS CHECKS GOOD.

Part: FCE — UNSERVICEABLE (NR 2) · airframe 8,888 hrs · 6,193 cycles

CREW RECEIVED SPOILER FAIL CAS ON LANDING. REPLACED FCE #2. RIGGED FCE #2 AND PERFORMED OPERATIONAL CHECKS. NO FAULTS FOUND. WORK PERFORMED IAW EMB-505 AMM 27-03-01.

Part: FCE — UNSERVICEABLE (ZONE 100) · airframe 8,878 hrs · 6,187 cycles

CREW RECEIVED GND SPLR FAIL AND SPOILER FAIL CAS MESSAGES ON LANDING WHILE BRAKING. REPLACED #2 FCE IAW EMB-505 AMM 27-03-01. RIGGING AND OPS CHECKS GOOD.

Part: ANTI-ICE SYSTEM — NOISY (ZONE 500) · airframe 8,721 hrs · 5,446 cycles

CREW REPORTS LOUD CABIN SQUEALING NOISE DURING CLIMB BETWEEN 6000 FT AND 7000 FT DURING ENGINE AND WING ANTI ICE SELF-TEST. THE NOISE LASTED 5-10 SECONDS AND DISSIPATED ENTIRELY AFTER SELF-TEST CONCLUSION. DURING DESCENT, CREW TESTED ANTI-ICE AT DIFFERENT ALTITUDES AND CONFIGURATIONS AND CONCLUDED THAT NOISE WOULD ONLY PRESENT ITSELF WHEN ANTI-ICE ALL WAS ACTIVE BELOW 12,000 FT. NOISE BECAME MORE PROMINENT AT LOWER ALTITUDES AND WAS HEARD ONLY ON THE LEFT SIDE OF THE AIRCRAFT. REPLACED LH WING CENTER LEADING-EDGE PICCOLO TUBE. REPLACED LT WING INBOARD LEADING-EDGE ASSEMBLY. NO DEFECTS NOTED DURING AND LEAK CHECKS OF WING ANTI-ICE SYSTEM. WORK COMPLETED IAW 57-40-00 + 30-12-00.

Part: FCE — UNSERVICEABLE (NR 2) · airframe 6,878 hrs · 4,547 cycles

PRIOR TO THE DEPARTURE, CREW RECEIVED SWPS FAULT, PTRIM NML FAIL, GND SPLR FAIL CAS MESSAGES. YELLOW X APPEARED OVER SPOILER AND PITCH TRIM ON MFD. REPLACED FCE #2 IAW EMB-505 AMM 27-60-00. RIGGING AND OPS CHECKS GOOD.

Part: FCE — FAULTED (ZONE 100) · airframe 10,363 hrs · 7,252 cycles

DURING CRUISE, CREW RECEIVED GND SPLR FAIL CAS. AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED AND RIGGED FCE2. OPS CHECK GOOD. WORK PERFORMED IAW AMM 27-03-01.

Part: BRACKET — MISINSTALLED (ZONE 300) · airframe 10,216 hrs · 5,942 cycles

AIR TURN BACK DUE TO PITCH TRIM ACTUATION ON PILOT SIDE WORKED UNTIL REACHING 3.0 TRIM SETTING THEN STOPPED FUNCTIONING DURING TAKEOFF. PITCH TRIM WAS SET TO 5.3. CREW TRIED TO MOVE TWO TIMES WITH THE PILOT’S CONTROL TO NO AVAIL, THEN ACTIVATED CO-PILOT CONTROL AND MOVED THE TRIM SETTING TO UNDER 3.0. UNDER 3.0, THE PILOT TRIM WORKED NORMAL IN BOTH UP AND DOWN MOVEMENT. AIRCRAFT LANDED WITHOUT INCIDENT AT KTEB. FOUND RELAY MOUNT BRACKET NOT PROPERLY GROUNDED TO AIRCRAFT STRUCTURE. RE-BONDED TO AIRCRAFT STRUCTURE AND REPLACED RELAY K211. RE-RACKED JB3 AND VERIFIED PIN CONDITION AND RETENTION. WORK PERFORMED IAW WM 27-12-07 AND AMM 24-63-09. OPS CHECK GOOD AT THIS TIME.

Part: GLARE SHIELD — SMOKE (ZONE 200) · airframe 12,787 hrs · 8,674 cycles

DIVERTED TO KMRY DUE TO AN ELECTRICAL BURNING SMELL IN THE CABIN. DURING CRUISE, THE PIC NOTED A RED X APPEAR OVER COM2 WHICH THEN EXTINGUISHED AND REAPPEARED MULTIPLE TIMES SHORTLY THEREAFTER. THE CREW OBSERVED SMOKE EMANATING FROM THE GLARESHIELD PROMPTING THEM TO DON THEIR OXYGEN MASKS. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED GIA 2 IAW EMB 505 AMM 31-41-05. ALL FOLLOW-ON CHECKS PASSED.

Part: COFFEEMAKER — ODOR (ZONE 900) · airframe 560 hrs · 510 cycles

COFFEE POT OVER HEATED CAUSING STRONG BURNING SMELL IN FLIGHT. CREW PULLED AND COLLARED HOT JUG 1 AND 2 CIRCUIT BREAKERS. COFFEE POT WAS THEN SECURED IN AFT BAGGAGE AREA. REPLACED COFFEE POT IAW EMB-505 AMM 25-31-02. HOT JUG 1 AND 2 CIRCUIT BREAKERS RESET AIRCRAFT RETURNED TO NORMAL CONFIGURATION.

Part: ACM — FAULTED (ZONE 100) · airframe 17,328 hrs · 10,805 cycles

REJECTED TAKEOFF DUE TO PACK TEMP HIGH CAS, PACK FAIL CAS, AND VISIBLE SMOKE IN CABIN. CREW TAXIED BACK TO THE FBO WITHOUT INCIDENT. FOUND BROKEN BLADE ON ACM. REPLACED ACM AND PRECOOLER. PERFORMED OPS AND BLEED CHECKS. ALL CHECKS SATISFACTORY AT THIS TIME. WORK COMPLETED IAW CL 300 AMM 21-51-15, 21-52-13, 21-52-00.

Part: WINDSHIELD — SMOKE (ZONE 200) · airframe 12,722 hrs · 7,553 cycles

DURING CLIMB A SMALL AMOUNT OF SMOKE BEGAN EMANATING FROM THE LOWER LEFT CORNER OF THE CAPTAIN-SIDE WINDSHIELD NEAR THE CONTROL PANEL AREA. THE CREW OBSERVED THAT THE ODOR WAS METALLIC AND CONSISTENT WITH AN ELECTRICAL OR HEATING SOURCE AND IMMEDIATELY CEASED AFTER THE WINDSHIELD HEAT SYSTEM WAS DEACTIVATED. AIRCRAFT LANDED AT KMDW WITHOUT INCIDENT. REPLACED LEFT WINDSHIELD ASSEMBLY. PERFORMED SATISFACTORY WINDSHIELD ANTI-ICE CHECKS AND PRESSURIZATION LEAK CHECKS WITH NO FURTHER DEFECTS NOTED IAW BD-100 AMM 56-11-01.

Part: VHF COMM — SMOKE (ZONE 200) · airframe 17,786 hrs · 11,084 cycles

AIR TURN BACK DUE TO SMOKE IN CABIN DURING CLIMB BETWEEN 12000 AND 15000 FT. CREW NOTED THAT THE ODOR SEEMED TO BE COMING FROM BEHIND THE LT CIRCUIT BREAKER PANEL. AIRCRAFT LANDED WITHOUT INCIDENT AT KSFB. REPLACED THE NR 1 VHF 4000 IAW AMM 23-11-01. PERFORMED SATISFACTORY ELECTRICAL BONDING TEST IAW SPM 51-80-00. PERFORMED SATISFACTORY OPSL TEST OF THE NR 1 VHF IAW BD-100 23-11-00.

Part: FCE — FAULTED (ZONE 100) · airframe 4,727 hrs · 3,362 cycles

P TRIM NML FAIL CAS DISPLAYED. REPLACED FCE NR 2 IAW AMM 27-03-01. OPS CHECKS GOOD. NO FAULTS NOTED AT THIS TIME.

Part: FCE — FAULTED (NR 2) · airframe 7,215 hrs · 4,798 cycles

ON DECENT CREW RECEIVED GND SPLR FAIL AND PTRIM NML FAIL CAS MESSAGES. EXECUTED QRH, NO RESET POSSIBLE, LANDED ON BACK-UP TRIM. REPLACED #2 FCE IAW EMB 505 AMM 27-03-01. RIG AND OPERATIONAL CHECKS GOOD.

Part: RAM AIR TURB — FAULTED (ZONE 100) · airframe 2,201 hrs · 1,375 cycles

DURING CRUISE, CREW LOST TWO SMART PROBES. AN EMERGENCY WAS DECLARED & DECISION MADE TO CONTINUE TO THEIR DESTINATION: KDAL. ON APPROACH, TOWER NOTIFIED CREW THAT IT APPEARED THAT A PANEL WAS MISSING FROM THE NOSE SECTIONT. ACFT LANDED WITHOUT INCIDENT AT KDAL. FOUND THE RAT ATTEMPTED & FAILED TO DEPLOY. STOWAGE DOOR WAS FULLY OPEN, BUT RAT EGRESS BLOCKED WHEN A FAN BLADE CONTACTED THE EDGE OF THE DOOR OPENING. PERFORMED HIDDEN DAMAGE INSPECTION OF THE RAT BAY IAW AMM 05-41-00. FOUND DENT ON THE RAT DOOR LANDING SKIN NEAR DOOR SEAL FWD LOWER AREA. PERFORMED A PERMANENT REPAIR OF THE RAT DOOR LANDING SKIN NEAR DOOR SEAL FWD LOWER AREA IAW SRM 51-10-05, 51-10-03, 51-22-013, 51-22-04, & 51-22-05. PERFORMED RAT DOOR OPEN & CLOSING CHKS IAW AMM 24-23-00. NO DEFECTS NOTED. FOUND NICKS ON 1 RAT BLADE. REPLACED THE RAT WITH A REPAIRED UNIT IAW AMM 24-23-01. REPLACED RAT UPLOCK ASSLY IAW AMM 24-23-05. RIGGING, OPS TEST, FUNCTIONAL TEST ALL CHKD GOOD. PERFORMED RAT MANUAL-RELEASE HANDLE & CABLE ASSY ADJUST IAW AMM 24-23-07. PERFORMED RAT DEPLOYMENT ACTUATOR ADJUST IAW AMM 24-23-03. PERFORMED MULTIPLE RETRACTIONS & DEPLOYMENTS WITH NO DEFECTS.

Part: FCE — UNSERVICEABLE (NR 2) · airframe 7,196 hrs · 4,788 cycles

YELLOW X NOTED DURING PITCH TRIM MOVEMENT IN PRIMARY. REPLACED NR 2 FCE IAW AMM 27-03-01.

Part: FCE — UNSERVICEABLE (NR 2) · airframe 10,642 hrs · 7,475 cycles

SWPS FAULT, GNS SPLR FAIL, PTRIM NML FAIL, SPOILER FAULT CAS ILLUMINATED IN FLIGHT. REPLACED FCE # 2 IAW EMB 505 AMM 27-60-00. ALL OPS AND RIGGING PROCEDURES SATISFACTORY. NO DEFECTS NOTED AT THIS TIME.

Part: FCE — FAULTED (FLAP SYS) · airframe 11,330 hrs · 7,892 cycles

ON START UP, FLAP FAIL CAS ILLUMINATED AND FLAP INDICATOR ON MFD SHOWED YELLOW. CYCLED FLAPS AND MESSAGE REMAINED. REPLACED FCE 1 IAW EMB 505 AMM 27-03-01. RIGGING/OPS CHECK GOOD.

Part: FCE — FAULTED (FLAP SYS) · airframe 9,478 hrs · 6,459 cycles

FCE 2 CB POPPED WITH RELATED CAS MESSAGES. ATTEMPTED RESET WAS NOT SUCCESSFUL. REPLACED FLIGHT CONTROL ELECTRONIC (FCE) 2 IAW P300 AMM 27-3-01. OPS CHECK GOOD.

Part: FCE — FAULTED (FLAP SYS) · airframe 11,330 hrs · 7,892 cycles

DURING CRUISE, CREW RECEIVED SWPS FAULT, FLAPS FAIL, PTRIM BKP FAIL AND SPOILER FAULT. AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED FCE 1 IAW EMB 505 AMM 27-03-01. FCE 1 RIGGING / OPS CHECK GOOD AND NO CAS MESSAGE ILLUMINATED.

Part: FCE — FAULTED (FLAP SYS) · airframe 9,006 hrs · 6,266 cycles

DURING CRUISE, CREW RECEIVED SWPS FAULT, FLAP FAIL, PTRIM BKP FAIL AND SPOILER FAULT. THE FLAPS WERE RETRACTED AT THE 0 POSITION. CAS MESSAGES REMAINED ON FROM CRUISE, LANDING AND SHUTDOWN. REPLACED FCE #1 AND OPS/RIGGED TESTED WITH NO FURTHER DEFECTS IAW PHENOM 300 AMM 27-03-01.

Part: FCE — FAULTED (ZONE 100) · airframe 3,733 hrs · 2,644 cycles

WHILE DOING THE FLIGHT CONTROL CHECK AFTER STARTUP, GND SPOILER FAIL CAS. REPLACED FCE #2 IAW EMB 505 AMM TASK 27-03-01-400-801. RIGGING AND OPS CHECK SATISFACTORY AT THIS TIME.