20251018015189A

Accident · Substantial damage

FAA accident report · Cessna L-19E · Phoenix, AZ · October 18, 2025

Date
October 18, 2025 · 13:48 local
Place
Phoenix, AZ
Airport
Phoenix Deer Valley
Phase of flight
Landing: Rollout
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N4584N
NTSB investigation
NTSBWPR26LA028
Reported as
Cessna L-19E
People aboard
2
Fatal injuries
0
Other injuries
0
Pilot’s certificate
Flight instructor
Pilot’s flight hours
2,300 total

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 10/18/2025 privacy data omittedCessna L-19E was departing grapevine 88AZ in-route to kdvt, pilot noticed he was giving full left rudder to stay in trim on climb-out. Pilot concluded his ruder was stuck in full right position. Pilot landed on main wheels and held the tail up until elevator lost authority due to low speeds. The tail came down and yawed hard left coming to rest 180 degrees from landing direction. Tail wheel was stuck 90 degrees to aircraft fore and aft direction, once tailwheel was disconnected from rudder controls, controls moved freely with no anomalies.

As the FAA filed it

ON 10/18/2025 ^PRIVACY DATA OMITTED^CESSNA L-19E WAS DEPARTING GRAPEVINE 88AZ IN-ROUTE TO KDVT, PILOT NOTICED HE WAS GIVING FULL LEFT RUDDER TO STAY IN TRIM ON CLIMB-OUT. PILOT CONCLUDED HIS RUDER WAS STUCK IN FULL RIGHT POSITION. PILOT LANDED ON MAIN WHEELS AND HELD THE TAIL UP UNTIL ELEVATOR LOST AUTHORITY DUE TO LOW SPEEDS. THE TAIL CAME DOWN AND YAWED HARD LEFT COMING TO REST 180 DEGREES FROM LANDING DIRECTION. TAIL WHEEL WAS STUCK 90 DEGREES TO AIRCRAFT FORE AND AFT DIRECTION, ONCE TAILWHEEL WAS DISCONNECTED FROM RUDDER CONTROLS, CONTROLS MOVED FREELY WITH NO ANOMALIES.

NTSB investigation

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

Other reports on N4584N · 2

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