20010917029189A

Accident · Substantial damage

FAA accident report · Cessna 172R · Orlando, FL · September 17, 2001

Date
September 17, 2001 · 16:38 local
Place
Orlando, FL
Phase of flight
Fcd/Prec Ldg From Cruise
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N158RA
NTSB investigation
NTSBATL01LA110
Reported as
Cessna 172R
Reported engine
Continental IO360*
People aboard
2
Fatal injuries
0
Pilot’s flight hours
1,222 total635 in this make and model52 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.

(-23) At 6000 feet MSL, in cruise flight, on an IFR flight plan from orl to ocf, crew noticed oil pressure reading zero and low oil pressure light illuminated. The CFI decided to attempt return to Orlando executive airport, approximately 35 NM to the se. The crew overflew two nearby airports on their return to orl. At 3500 to 3000 feet MSL the engine seized. The CFI initially planned a forced landing to a busy highway. He changed his mind and landed in a marshy area adjacent to the highway substantially damaging the airplane. (.4) during cruise flight the engine lost oil pressure and the pilot continued to fly in an attempt to get back to his departure point, however the engine seized before the pilot could reach the departure point. The pilot made a forced landing into unsuitable terrain substantially damaging the airplane, however, the pilot and pilot rated passenger were not injured. Examination of the engine found the two bottom attachment screws for the upper (left) vacuum pump loose. Approximately one quart of oil was found in the engine and oil filter. The underside of the airplane was coated with oil from t he firewall to the tail mooring point. No anomalies were found with the oil pump or oil lines. A review of the airfrane maintenance logbooks revealed that the left vacuum pump and been removed and replaced on the same day of the accident prior to the accident flight. An oil leak test was performed on another 172R. The two lower nuts of the upper vacuum pump were loosened and the engine was run near full static RPM for five minutes. Oil began leaking from the vacuum pump as soon as the engine was started. After five minutes, the back of the engine, the lower cowling, engine accessories and the ground were partially covered with oil. According to the Cessna pilot operating handbook under emergency procedures, the pilot's should have landed at the nearest airport to inspect for the source of the loss of oil pressure.

As the FAA filed it

(-23) AT 6000 FEET MSL, IN CRUISE FLIGHT, ON AN IFR FLIGHT PLAN FROM ORL TO OCF, CREW NOTICED OIL PRESSURE READING ZERO AND LOW OIL PRESSURE LIGHT ILLUMINATED. THE CFI DECIDED TO ATTEMPT RETURN TO ORLANDO EXECUTIVE AIRPORT, APPROXIMATELY 35 NM TO THE SE. THE CREW OVERFLEW TWO NEARBY AIRPORTS ON THEIR RETURN TO ORL. AT 3500 TO 3000 FEET MSL THE ENGINE SEIZED. THE CFI INITIALLY PLANNED A FORCED LANDING TO A BUSY HIGHWAY. HE CHANGED HIS MIND AND LANDED IN A MARSHY AREA ADJACENT TO THE HIGHWAY SUBSTANTIALLY DAMAGING THE AIRPLANE. (.4) DURING CRUISE FLIGHT THE ENGINE LOST OIL PRESSURE AND THE PILOT CONTINUED TO FLY IN AN ATTEMPT TO GET BACK TO HIS DEPARTURE POINT, HOWEVER THE ENGINE SEIZED BEFORE THE PILOT COULD REACH THE DEPARTURE POINT. THE PILOT MADE A FORCED LANDING INTO UNSUITABLE TERRAIN SUBSTANTIALLY DAMAGING THE AIRPLANE, HOWEVER, THE PILOT AND PILOT RATED PASSENGER WERE NOT INJURED. EXAMINATION OF THE ENGINE FOUND THE TWO BOTTOM ATTACHMENT SCREWS FOR THE UPPER (LEFT) VACUUM PUMP LOOSE. APPROXIMATELY ONE QUART OF OIL WAS FOUND IN THE ENGINE AND OIL FILTER. THE UNDERSIDE OF THE AIRPLANE WAS COATED WITH OIL FROM T HE FIREWALL TO THE TAIL MOORING POINT. NO ANOMALIES WERE FOUND WITH THE OIL PUMP OR OIL LINES. A REVIEW OF THE AIRFRANE MAINTENANCE LOGBOOKS REVEALED THAT THE LEFT VACUUM PUMP AND BEEN REMOVED AND REPLACED ON THE SAME DAY OF THE ACCIDENT PRIOR TO THE ACCIDENT FLIGHT. AN OIL LEAK TEST WAS PERFORMED ON ANOTHER 172R. THE TWO LOWER NUTS OF THE UPPER VACUUM PUMP WERE LOOSENED AND THE ENGINE WAS RUN NEAR FULL STATIC RPM FOR FIVE MINUTES. OIL BEGAN LEAKING FROM THE VACUUM PUMP AS SOON AS THE ENGINE WAS STARTED. AFTER FIVE MINUTES, THE BACK OF THE ENGINE, THE LOWER COWLING, ENGINE ACCESSORIES AND THE GROUND WERE PARTIALLY COVERED WITH OIL. ACCORDING TO THE CESSNA PILOT OPERATING HANDBOOK UNDER EMERGENCY PROCEDURES, THE PILOT'S SHOULD HAVE LANDED AT THE NEAREST AIRPORT TO INSPECT FOR THE SOURCE OF THE LOSS OF OIL PRESSURE.

NTSB investigation

The NTSB’s investigation of this event, with its probable cause and findings. Matched to this report by N-number and date.