What happened
The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.
Bombardier CL-604 aircraft registration privacy data omitted, privacy data omitted departed from montreal-trudeau international airport in route to Fort Lauderdale executive airport. Passing through FL280 the LH windshield outer glass suddenly broke. There was no notable turbulence, OAT -34 degrees and no abnormal engine or pressurizations noted at the time of the break. Indicated air speed was 280 KIAS at the time of the break. Checklist for “broken outer ply” was executed from QRH-2. Limitations of staying clear of icing conditions were kept as well as remaining below 280 KIAS and 800 ft MSL. No injuries to captain, f/o or 6 passengers.
Broken LH windshield removed and replaced with a new windshield; ops check and leak check good. Ref’d CL-604 amm 56-11-01
Performed FOD inspection with no defect noted. Replaced 2 damaged fan blades with overhauled fan blades. All fan blades were removed, cleaned lubed and re-installed using blade plot provided by ge. Complied with engine runs and vibe checks in accordance with (iaw) maintenance manual with no further defects noted. All work accomplished iaw CF34BJ service manual SEI-780 rev 65 dated 02/01/2025.
As the FAA filed it
BOMBARDIER CL-604 AIRCRAFT REGISTRATION ^PRIVACY DATA OMITTED^, ^PRIVACY DATA OMITTED^ DEPARTED FROM MONTREAL-TRUDEAU INTERNATIONAL AIRPORT IN ROUTE TO FORT LAUDERDALE EXECUTIVE AIRPORT. PASSING THROUGH FL280 THE LH WINDSHIELD OUTER GLASS SUDDENLY BROKE. THERE WAS NO NOTABLE TURBULENCE, OAT -34 DEGREES AND NO ABNORMAL ENGINE OR PRESSURIZATIONS NOTED AT THE TIME OF THE BREAK. INDICATED AIR SPEED WAS 280 KIAS AT THE TIME OF THE BREAK. CHECKLIST FOR “BROKEN OUTER PLY” WAS EXECUTED FROM QRH-2. LIMITATIONS OF STAYING CLEAR OF ICING CONDITIONS WERE KEPT AS WELL AS REMAINING BELOW 280 KIAS AND 800 FT MSL. NO INJURIES TO CAPTAIN, F/O OR 6 PASSENGERS.
BROKEN LH WINDSHIELD REMOVED AND REPLACED WITH A NEW WINDSHIELD; OPS CHECK AND LEAK CHECK GOOD. REF’D CL-604 AMM 56-11-01
PERFORMED FOD INSPECTION WITH NO DEFECT NOTED. REPLACED 2 DAMAGED FAN BLADES WITH OVERHAULED FAN BLADES. ALL FAN BLADES WERE REMOVED, CLEANED LUBED AND RE-INSTALLED USING BLADE PLOT PROVIDED BY GE. COMPLIED WITH ENGINE RUNS AND VIBE CHECKS IN ACCORDANCE WITH (IAW) MAINTENANCE MANUAL WITH NO FURTHER DEFECTS NOTED. ALL WORK ACCOMPLISHED IAW CF34BJ SERVICE MANUAL SEI-780 REV 65 DATED 02/01/2025.