N416FX

EMBRAER S A EMB-545 · 2017 · Fixed-wing multi-engine · 2 engines · 11 seats · Valid Registration

Registered owner: FLEXJET LLC, OH (owner ≠ operator)

Operators of this aircraft

Who operated this tail, and how firmly we know it.

OperatorRolePeriodBasis
Flexjet, LLC (J7SA)Certificate holder—Matched by certificate designator

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, 2004-09-21 – 2025-02-18.

WARNING INDICATION · 2025-02-18 Matched by certificate designator
ATA 2431

Part: SHAFT — SHEARED (NR 2 GENERATOR) · airframe 7,570 hrs · 4,881 cycles

DIVERTED DUE TO GEN 2 BUS OFF CAS AND RELATED MESSAGES WHILE CLIMBING THROUGH FL430. THE SIC RAN THE CHECKLIST AND ATTEMPTED TO RESET THE GENERATOR, BUT THE ISSUE PERSISTED. THE CREW DESCENDED TO FL310, DECLARED AN EMERGENCY, AND DIVERTED TO KRDU. AIRCRAFT LANDED WITHOUT INCIDENT. FOUND #2 GENERATOR SHAFT SHEARED. REPLACED #2 GENERATOR WITH CUSTOMER-SUPPLIED NEW GENERATOR IAW EMB-550 AMM 24-31-01. OPS CHECK GOOD

Source: SDR J7SA2025022100434
OTHER · 2022-08-23 Matched by certificate designator
ATA 5600

Part: NONE — NONE · airframe 4,928 hrs · 3,252 cycles

DURING DESCENT, LEFT SIDE COCKPIT WINDOW CRACKED. CREW DECLARED EMERGENCY AND LANDED SAFELY AT KAUS. NO LOSS OF PRESSURIZATION, NO INJURIES, ONE PASSENGER ON BOARD. REPLACED LEFT SIDE COCKPIT WINDOW IAW EMB 550 AMM 56-12-00. LEAK AND OPS CHECK GOOD. THIS IS THE THIRD SUCH INCIDENT WHERE A POST-AD 2022-25-07 HAS FAILED ON A FLEXJET AIRCRAFT, THE OTHER TWO ARE: (1) N430FX PILOT SIDE FAIL 11/24/2021 2350.3 TSN 1460 CSN; (2) N423FX RIGHT SIDE 05/05/2022 3273.4 TSN AND 2060 CSN.

Source: SDR J7SA2022082600328
OTHER · 2021-02-18 Matched by certificate designator
ATA 3350

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 3,619 hrs · 2,424 cycles

DISCOVERED EMERGENCY LIGHTS FAILED. REMOVED AND REPLACED BOTH FWD AND AFT EMERGENCY POWER SUPPLIES IAW EMB 550 AMM 33-51-01. OPS CHECK GOOD. PN 6450LS-00; SN FWD 001166; SN AFT 001878.

Source: SDR J7SA2021022500278
WARNING INDICATION · 2021-01-16 Matched by certificate designator
ATA 3350

Part: BATTERY PACK — FAULTED (EMERGENCY LIGHTS) · airframe 3,524 hrs · 2,361 cycles

EMERGENCY LIGHT BATTERY FAULT CAS MESSAGE DISPLAYED. REMOVED AND REPLACED FWD AND AFT EMERGENCY LIGHT BATTERY PACKS, IAW EMB 550 AMM 33-51-01. OPERATIONS CHECK GOOD. LEFT RACK P/N OFF/ON: 6450LS-00; S/N OFF: 000675, S/N ON: 002273. C FLOOR P/N OFF/ON: 6450LS-00; S/N OFF: 000832; S/N ON: 001154.

Source: SDR J7SA2021012600267
OTHER · 2020-11-23 Matched by certificate designator
ATA 3350

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 3,308 hrs · 2,236 cycles

DISCOVERED EMERGENCY LIGHTS REMAIN ON IN ARMED POSITION. REMOVED AND REPLACED FWD AND AFT EMERGENCY BATTERIES, IAW LEGACY 450/500 AMM 33-51-01. OPERATIONS CHECK GOOD AT THIS TIME. FWD P/N OFF/ON: 6450LS-00, S/N OFF: 000897, S/N ON: 000832. AFT P/N OFF/ON: 6450LS-00, S/N OFF: 002269, S/N ON: 00675.

Source: SDR J7SA2020112400243
WARNING INDICATION · 2005-02-13 Matched by certificate designator
ATA 3600

Part: CLAMP — LOOSE (RT PYLON) · airframe 3,440 hrs · 2,640 cycles

CREW ADVISED, THE RIGHT PYLON OVERHEAT ILLUMINATED IN CLIMB AT FL 17.0 WITH NAC AND ANTI-ICE SELECTED TO THE OFF POSITION. CREW REDUCED RIGHT ENGINE N1 TO 75 PERCENT FOR 1 MINUTE THEN TO IDLE FOR 2 MINUTES. CAS MESSAGE WOULD NOT EXTINGUISH. CREW FOLLOWED ACFT CHECKLIST AND SHUTDOWN ENGINE IN FLIGHT. NO PAX ON BOARD. FOUND CLAMP UNDER RT PYLON LP DUCT NEAR S-144 OVERHEAT SWITCH NOT SECURE, LEAKING AIR. SECURED CLAMP AND RAN ENGINES AT POWER, NO LEAKS NOTED. OPS CHECK GOOD.

Source: SDR 4511302132005
WARNING INDICATION · 2004-09-21 Matched by certificate designator
ATA 3230

Part: CABLE — MALADJUSTMENT (MLG FREEFALL SYS) · airframe 3,093 hrs · 2,382 cycles

LT AND RT GEAR IN TRANSIT LIGHTS REMAINED ILLUMINATED AFTER GEAR EXTENSION. THE FREEFALL CONTROL LEVER WAS BUMPED OUT OF ITS NORMAL (UP) POSITION AND WHEN THE GEAR WAS SELECTED DOWN AND IT COMPLETED ITS CYCLE THE MAIN LANDING GEAR INBOARD DOOR FREEFALL CABLE WOULD NOT ALLOW THE IB MLG DOOR UPLOCK SWITCH TO SEND A CLOSE SIGNAL, BECAUSE IT WAS ADJUSTED TO TIGHT. PROPER ADJUSTMENT OF CABLE IAW MM 32-33-02. (EA09200403107)

Source: SDR WVE2004F00023