
- CRITICAL OPS TESTFLIGHT CODE MANUAL
- CRITICAL OPS TESTFLIGHT CODE FULL
- CRITICAL OPS TESTFLIGHT CODE CODE
The airplane landed long, using 2048 feet of runway before main gear touchdown, leaving 4453 feet remaining to stop the airplane. Touchdown airspeed was 137 KCAS, which was 12 knots faster than the scheduled Vref speed of 125 KCAS. Because the warning inhibit was selected ON per the normal checklist, there was no aural warning tone to inform the crew of the amber message indicating the loss of the Aux system.
CRITICAL OPS TESTFLIGHT CODE MANUAL
With the landing imminent, the PNF discontinued his review of the checklist at this point, failing to note step 18 requiring the manual deployment of the speed brakes. The PNF devoted his attention to completing the Left Hydraulic System (SYS) Failure-Loss of Pressure and Fluid checklist prior to landing and per step 14 selected Aux pump-ON, 16 seconds prior to Main Landing Gear (MLG) touchdown.Subsequent to that, an amber left side hydraulic quantity low crew alerting system (CAS) message illuminated when the airplane was inside the FAF. The PNF also selected the Landing Mode on the Cabin Pressure Controller.
CRITICAL OPS TESTFLIGHT CODE FULL
The pilot not flying (PNF) completed the before landing checklist to "include arming ground spoilers, warning inhibit, pumping up Brakes/Hydraulics/Brake Accumulator to 3000 psi" except for "selecting full flaps." Full flaps were to be selected at the PF's call for full flaps. The landing gear came down with an indication of three green lights and no red lights. As the airplane approached the virtual glide slope, the pilot flying (PF) called for the landing gear to be selected down and called for the landing checklist to be conducted.


The autopilot disengaged during two inflight maneuvers. However, write ups were noted with the number one flight management system, the elevator trim, and Mach trim. All inflight checks were found to be normal. The flight to the Marquette, Michigan, area was normal. Taxi, engine "run-ups", and takeoff were reported as normal.

CRITICAL OPS TESTFLIGHT CODE CODE
The airplane was registered to and operated by Gulfstream Aerospace Corporation under the provisions of 14 Code of Federal Regulations Part 91 as a maintenance test flight.The airplane incurred substantial left wing damage when the left main landing gear collapsed during the overrun. The two airline transport pilots and one passenger were not injured.

