20000308003719I

Incident

FAA incident report · Lear 35A · Las Vegas, NV · March 8, 2000

Date
March 8, 2000 · 11:57 local
Place
Las Vegas, NV
Airport
Mc Carran International
Phase of flight
To Init Climb(1st Pwr Reduct)
Operating rules
Air taxi and commuter (Part 135)
Operator
O9IA
Aircraft
N45AE
Reported as
Lear 35A
People aboard
4
Fatal injuries
0
Pilot’s flight hours
4,954 total440 in this make and model131 in the last 90 days

From the FAA’s Accident/Incident Data System (AIDS), through its Aviation Safety Information Portal, as reported. The NTSB investigates accidents separately, and its record of an accident is the fuller one. The aircraft is matched to the registry by N-number and event date, checked against the reported make and model; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

What happened

The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.

On March 8, 2000 at approxiamately 1150 PST while departing las enroute to fch during inital climbout, crew indentified the cabin was not pressurizing normally and was climbing with the aircraft. Crew elected to return to las for precautionary landing. Troubleshooting revealed a "b" nut was disconnected on the venturi sense line for the flow control valva and venturi and in intermittent K2 relay on pcbi on the squat switch relay panel that prevented the safety valve from closing. All discrepancies were corrected and ground functional check completed successfully. Malfunction/defect report submitted by operator.

As the FAA filed it

ON MARCH 8, 2000 AT APPROXIAMATELY 1150 PST WHILE DEPARTING LAS ENROUTE TO FCH DURING INITAL CLIMBOUT, CREW INDENTIFIED THE CABIN WAS NOT PRESSURIZING NORMALLY AND WAS CLIMBING WITH THE AIRCRAFT. CREW ELECTED TO RETURN TO LAS FOR PRECAUTIONARY LANDING. TROUBLESHOOTING REVEALED A "B" NUT WAS DISCONNECTED ON THE VENTURI SENSE LINE FOR THE FLOW CONTROL VALVA AND VENTURI AND IN INTERMITTENT K2 RELAY ON PCBI ON THE SQUAT SWITCH RELAY PANEL THAT PREVENTED THE SAFETY VALVE FROM CLOSING. ALL DISCREPANCIES WERE CORRECTED AND GROUND FUNCTIONAL CHECK COMPLETED SUCCESSFULLY. MALFUNCTION/DEFECT REPORT SUBMITTED BY OPERATOR.

Other reports on N45AE · 1

Matched to the same aircraft by N-number and date.