N451QS
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
7 reports on file, 2022-07-24 – 2024-06-27.
Part: BRAKE ASSY — DEGRADED (LT MLG) · airframe 2,100 hrs · 1,590 cycles
WHILE TAXING WHEN APPLYING THE RT BRAKE SIGNIFICANT SHUTTER FELT THROUGHOUT AIRPLANE. LT BRAKE OPS NORMALLY. WHILE PARKING ACFT HAD TO MAKE A RT TURN INTO SPOT. LOCKING & RELEASING OF RT MAIN BRAKE WAS SO PRONOUNCED THAT NOSE WAS LURCHING ACROSS RAMP IN TURN. WHILE SLOWING TO A STOP, THE AIRCRAFT ABRUPTLY JOLTED TO A STOP WITHOUT ADDITIONAL BRAKE PRESSURE APPLIED. PER MCC REQUEST, REMOVED OLD BCU DUE TO BRAKING ISSUES. INSTALLED MODIFIED BCU IAW AMM 32-41-01. PREPPED AND PERFORMED FUNCTIONAL CHECKS, CHECKS GOOD. PREPPED AND TAXIED AIRCRAFT AND CHECKS GOOD. BRAKING IS NORMAL AND SMOOTH. EMBRAER ENGINEERING PROVIDED ETD2024-P300-04956056 TO INSTALL -1 0. CLOSED AND SECURED AIRCRAFT.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 1,761 hrs · 1,351 cycles
ALL EMER LIGHTS ON WHEN EMER LIGHT SWITCH IN ARM POSITION. REPLACED BOTH #1 AND #2 BATTERY PACKS DUE TO NOT TURNING OFF WITH SWITCH I NTHE ARM POSITION. OPS CHECKED GOOD IAW AMM 33-52-01.
Part: BATTERY — FAULTED (EMERENCY LIGHTS) · airframe 1,725 hrs · 1,325 cycles
CABIN EMERGENCY LIGHTS ON IN FLIGHT WITH SWITCH IN ARM POSITION. REMOVED & REPLACED THE FWD BATTERY. REMOVED REPLACED THE AFT BATTERY IAW AMM 33·52·01·000·801·A/400 & JJ-52-01-400-801·A.
Part: CONTROL UNIT — DEFECTIVE (ZONE 100) · airframe 1,366 hrs · 1,055 cycles
RIGHT MLG BRAKE: ON LANDING ROLL AND TAXI IN, BRAKE CHATTER, GRABBING. SEEMS TO BE RIGHT SIDE, AS NOSE WOULD PULL RIGHT EACH TIME. COULD FEEL RIGHT TIRE CONSIDERABLY WARMER THAN LEFT. //SIGNOFF// PREFORMED NJA BLEEDING TASK CARD, REMOVED AND REPLACED BRAKE CONTROL UNIT , IAW EMB-505 M/M TASK 32-41-01-400·801-A. PERFORMED TAXI CHECK WITH NO DEFECTS NOTED, OPERATIONAL CHECKED SATISFACTORY.
Part: BATTERY — DEFECTIVE (ZONE 200) · airframe 1,286 hrs · 995 cycles
CABIN EMERGENCY LIGHTS BEGAN FLASHING IN CRUISE FLIGHT. RECEIVED MODIFIED EMERGENCY BATTERY P/N: 7450LS-00, S/N: 000915M. REMOVED AND REPLACED # 2 BATTERY PACK P/N: SAME, S/N: 005763 LOCATED IN THE LAV. USING GPU CHARGED PACK FOR THIRTY MINS. DISCONNECTED # 1 BATTERY IN THE COCKPIT. SET EMER SWITCH TO ARM AND VERFIED EMER LIGHTS WERE NOT FLASHING AND OFF. OPS CHECK GOOD. RECONNECTED # 1 BATTERY PACK CONNECTOR AND CHARGED PACKS FOR ANOTHER THIRTY MINS BEFORE SHUTTING DOWN GROUND POWER, APPLIED DATE,TIME, AIRPORT IDAND TECH STAMP ONTO BATTERY PACK. WORK DONE IAW PHENOM 300 M.M. 33-52-01 AND FIM 33-50-00.
Part: SENSOR — FAILED (ZONE 200) · airframe 1,261 hrs · 976 cycles
FUEL 2 FEED FAULT WHITE CAS: LEVEL FLIGHT AT FL 400, CAS DISPLAYED AND FUEL SYNOPTIC PAGE SHOWED YELLOW X OVER #2 EJECTOR PUMP AND GREEN #2 BOOST PUMP. REMOVE RH FUEL LOW PRESSURE SENSOR PN: 098C07-611, SN: 2514 AND INSTALLED NEW RH FUEL LOW PRESSURE SENSOR PN: 098C07-611, SN: 2950 IAW PHENOM 300 AMM 28-45-0L OPS CHECK GOOD.
Part: WARNING MESSAGE — ILLUMINATED · airframe 71 hrs · 54 cycles
FLAP FAIL YELLOW CAS: AT CRUISE WE RECEIVED THE FOLLOWING YELLOW CASS FLAP FAIL, PITCH TRIM BACKUP FAIL, SWAPS FAIL, YELLOW MAX SPD.