20230323002869I

Incident · Substantial damage

FAA incident report · Cirrus Design SR20 · Phoenix, AZ · March 23, 2023

Date
March 23, 2023 · 10:50 local
Place
Phoenix, AZ
Airport
Phoenix Goodyear
Phase of flight
Climb
Operating rules
Pilot school (Part 141)
Operator
WIWS
Damage
Substantial damage
Aircraft
N837EF
Reported as
Cirrus Design SR20
Reported engine
Lycoming IO-390 series
People aboard
2
Fatal injuries
0
Other 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.

On 03-23-2023 at approximately 1037, a SR-20 departed Phoenix-Goodyear airport (gyr) under 14 CFR part 141 flight instruction. The aircraft was occupied by a certified flight instructor (CFI) and student pilot (sp). VMC conditions prevailed at the time of the incident. At 1050, following a loss of engine oil pressure, the CFI took control of the aircraft and executed an off-field emergency landing onto a farm road located approximately 4.1 miles southwest of the loop 202 and interstate 10 interchange. The aircraft landed safely with no injuries to personnel on board and without damage to the aircraft.

According to statement provided by the aircrew, all engine and engine oil parameters were normal during engine start, run-up, taxi, and takeoff. Flight operations quality assurance (foqa) data indicates that within 9 minutes of flight time, the engine began running rough and oil pressure rapidly dropped from 78 PSI to 0 PSI within 2 minutes.

An inspection of the aircraft following the off-field landing revealed oil covering the bottom of the fuselage and the engine compartment. The engine oil dipstick was tight and the engine was void of a measurable amount of oil. It was noted that the engine oil cooler pressure and return lines on the right side of the engine were “hand tight.”

One day prior to the incident, the aircraft was returned to service following a phase #2 (progressive) inspection conducted on 03-22-2023 at 14CFR part 145 repair station. During the phase #2 inspection, there was a squawk for the right magneto being out of time. Maintenance records show that the right magneto was retimed and signed off during the phase inspection. Following a review of pertinent maintenance records and subsequent interviews with maintenance personnel, there was no record of either the oil supply or return lines being loosened or removed to facilitate other maintenance (I.e. timing the right magneto). The engine at the time of this incident had 303.6 hours of service since overhaul.

As the FAA filed it

ON 03-23-2023 AT APPROXIMATELY 1037, A SR-20 DEPARTED PHOENIX-GOODYEAR AIRPORT (GYR) UNDER 14 CFR PART 141 FLIGHT INSTRUCTION. THE AIRCRAFT WAS OCCUPIED BY A CERTIFIED FLIGHT INSTRUCTOR (CFI) AND STUDENT PILOT (SP). VMC CONDITIONS PREVAILED AT THE TIME OF THE INCIDENT. AT 1050, FOLLOWING A LOSS OF ENGINE OIL PRESSURE, THE CFI TOOK CONTROL OF THE AIRCRAFT AND EXECUTED AN OFF-FIELD EMERGENCY LANDING ONTO A FARM ROAD LOCATED APPROXIMATELY 4.1 MILES SOUTHWEST OF THE LOOP 202 AND INTERSTATE 10 INTERCHANGE. THE AIRCRAFT LANDED SAFELY WITH NO INJURIES TO PERSONNEL ON BOARD AND WITHOUT DAMAGE TO THE AIRCRAFT.

ACCORDING TO STATEMENT PROVIDED BY THE AIRCREW, ALL ENGINE AND ENGINE OIL PARAMETERS WERE NORMAL DURING ENGINE START, RUN-UP, TAXI, AND TAKEOFF. FLIGHT OPERATIONS QUALITY ASSURANCE (FOQA) DATA INDICATES THAT WITHIN 9 MINUTES OF FLIGHT TIME, THE ENGINE BEGAN RUNNING ROUGH AND OIL PRESSURE RAPIDLY DROPPED FROM 78 PSI TO 0 PSI WITHIN 2 MINUTES.

AN INSPECTION OF THE AIRCRAFT FOLLOWING THE OFF-FIELD LANDING REVEALED OIL COVERING THE BOTTOM OF THE FUSELAGE AND THE ENGINE COMPARTMENT. THE ENGINE OIL DIPSTICK WAS TIGHT AND THE ENGINE WAS VOID OF A MEASURABLE AMOUNT OF OIL. IT WAS NOTED THAT THE ENGINE OIL COOLER PRESSURE AND RETURN LINES ON THE RIGHT SIDE OF THE ENGINE WERE “HAND TIGHT.”

ONE DAY PRIOR TO THE INCIDENT, THE AIRCRAFT WAS RETURNED TO SERVICE FOLLOWING A PHASE #2 (PROGRESSIVE) INSPECTION CONDUCTED ON 03-22-2023 AT 14CFR PART 145 REPAIR STATION. DURING THE PHASE #2 INSPECTION, THERE WAS A SQUAWK FOR THE RIGHT MAGNETO BEING OUT OF TIME. MAINTENANCE RECORDS SHOW THAT THE RIGHT MAGNETO WAS RETIMED AND SIGNED OFF DURING THE PHASE INSPECTION. FOLLOWING A REVIEW OF PERTINENT MAINTENANCE RECORDS AND SUBSEQUENT INTERVIEWS WITH MAINTENANCE PERSONNEL, THERE WAS NO RECORD OF EITHER THE OIL SUPPLY OR RETURN LINES BEING LOOSENED OR REMOVED TO FACILITATE OTHER MAINTENANCE (I.E. TIMING THE RIGHT MAGNETO). THE ENGINE AT THE TIME OF THIS INCIDENT HAD 303.6 HOURS OF SERVICE SINCE OVERHAUL.