What happened
The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.
(-23) Aircraft lost hydraulic pressure in the "a" system during climbout from smo. The the "b" system overtemped (190C). Aircraft declared an emergency. Aircrew performed an emergency extension of the gear. On landing at lax, the emergency pneumatic brakes were utilized. No fuselage or wing damage. Acft towed to garratt aviation. Four souls deplane acft with no injuries. Long beach citation service center dispatched to make the repairs on the aircraft. The following components were changed: power transfer unit, pressure (ruptured) line from the left hydraulic filter to the ptu left engine hydraulic pump, auxiliary pump, left engine hydraulic pump, auxiliary pump, right side system "b" hydaulic reservoir, nose steering wheel roll pin (broken), and nitrogen bottle. A mechanical interruption summary report was submitted by netjet on 11/27/02, 18:15 central time. Coordinated info on 12-13-2002 with poi (cleveland, oh FSDO) who will relay to pmi.
As the FAA filed it
(-23) AIRCRAFT LOST HYDRAULIC PRESSURE IN THE "A" SYSTEM DURING CLIMBOUT FROM SMO. THE THE "B" SYSTEM OVERTEMPED (190C). AIRCRAFT DECLARED AN EMERGENCY. AIRCREW PERFORMED AN EMERGENCY EXTENSION OF THE GEAR. ON LANDING AT LAX, THE EMERGENCY PNEUMATIC BRAKES WERE UTILIZED. NO FUSELAGE OR WING DAMAGE. ACFT TOWED TO GARRATT AVIATION. FOUR SOULS DEPLANE ACFT WITH NO INJURIES. LONG BEACH CITATION SERVICE CENTER DISPATCHED TO MAKE THE REPAIRS ON THE AIRCRAFT. THE FOLLOWING COMPONENTS WERE CHANGED: POWER TRANSFER UNIT, PRESSURE (RUPTURED) LINE FROM THE LEFT HYDRAULIC FILTER TO THE PTU LEFT ENGINE HYDRAULIC PUMP, AUXILIARY PUMP, LEFT ENGINE HYDRAULIC PUMP, AUXILIARY PUMP, RIGHT SIDE SYSTEM "B" HYDAULIC RESERVOIR, NOSE STEERING WHEEL ROLL PIN (BROKEN), AND NITROGEN BOTTLE. A MECHANICAL INTERRUPTION SUMMARY REPORT WAS SUBMITTED BY NETJET ON 11/27/02, 18:15 CENTRAL TIME. COORDINATED INFO ON 12-13-2002 WITH POI (CLEVELAND, OH FSDO) WHO WILL RELAY TO PMI.