20011126032799I

Incident

FAA incident report · Boeing 737-214 · Salt Lake City, UT · November 26, 2001

Date
November 26, 2001 · 21:13 local
Place
Salt Lake City, UT
Airport
Salt Lake City International
Phase of flight
Normal Cruise
Operating rules
Air carrier (Part 121)
Operator
BJNA
Aircraft
N457TM
Reported as
Boeing 737214
People aboard
90
Fatal injuries
0

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.

(-23) At flight level 310, enroute from houston (iah) to elko (eko), the hydraulic quantity gage dropped from 2 gallons to 1 gallon indicated. The hydraulic "a" system pumps were turned off. Quantity continued to drop to zero and within 5 minutes the "b" system failed. Both "a" and "b" system pressure gages were observed dropping to zero simultaneously. An emergency was declared and the aircraft diverted into Salt Lake City (slc). Maintenance found a hole chaffed through a hydraulic hard line near the #1 engine. Both hydaulic pumps were changed due to an open circuit on the #1 pump solenoid which allowed the pumps to run dry. Also, the pressure regulator in the hydraulic reservoir was replaced which allowed the "b" system to deplete.

As the FAA filed it

(-23) AT FLIGHT LEVEL 310, ENROUTE FROM HOUSTON (IAH) TO ELKO (EKO), THE HYDRAULIC QUANTITY GAGE DROPPED FROM 2 GALLONS TO 1 GALLON INDICATED. THE HYDRAULIC "A" SYSTEM PUMPS WERE TURNED OFF. QUANTITY CONTINUED TO DROP TO ZERO AND WITHIN 5 MINUTES THE "B" SYSTEM FAILED. BOTH "A" AND "B" SYSTEM PRESSURE GAGES WERE OBSERVED DROPPING TO ZERO SIMULTANEOUSLY. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT DIVERTED INTO SALT LAKE CITY (SLC). MAINTENANCE FOUND A HOLE CHAFFED THROUGH A HYDRAULIC HARD LINE NEAR THE #1 ENGINE. BOTH HYDAULIC PUMPS WERE CHANGED DUE TO AN OPEN CIRCUIT ON THE #1 PUMP SOLENOID WHICH ALLOWED THE PUMPS TO RUN DRY. ALSO, THE PRESSURE REGULATOR IN THE HYDRAULIC RESERVOIR WAS REPLACED WHICH ALLOWED THE "B" SYSTEM TO DEPLETE.

Other reports on N457TM · 3

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