20250627008979I

Incident · Minor damage

FAA incident report · Cessna 340A · El Paso, TX · June 27, 2025

Date
June 27, 2025 · 13:45 local
Place
El Paso, TX
Airport
El Paso International Airport
Phase of flight
Landing: Rollout
Operating rules
General operating rules (Part 91)
Damage
Minor damage
Aircraft
N2696U
Reported as
Cessna 340A
Reported engine
Continental TSIO-520 series
People aboard
2
Fatal injuries
0
Other injuries
0
Pilot’s certificates
Commercial pilot, flight instructor, private pilot
Pilot’s flight hours
960 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.

During the landing roll and during the application of brakes the pilot felt a "pop" the acft then slid to a stop. Inspection of the lt landing gear revealed that the upper & lower torque links which maintains parallel alignment of the tire to the fuselage separated. This occurred as a result of the lower torque link being pulled over the outer washer, nut and cotter key, which, along with a bolt, secures the upper torque link to the lower. The tire then turned sideways perpendicular to the direction of travel after which the tire skidded to a stop. Examination of the failure revealed that Cessna service information letter ME83-37 which recommends replacement of the two outer washers with larger ones, on the main landing gear scissor assy (torque links) had not been complied with.

As the FAA filed it

DURING THE LANDING ROLL AND DURING THE APPLICATION OF BRAKES THE PILOT FELT A "POP" THE ACFT THEN SLID TO A STOP. INSPECTION OF THE LT LANDING GEAR REVEALED THAT THE UPPER & LOWER TORQUE LINKS WHICH MAINTAINS PARALLEL ALIGNMENT OF THE TIRE TO THE FUSELAGE SEPARATED. THIS OCCURRED AS A RESULT OF THE LOWER TORQUE LINK BEING PULLED OVER THE OUTER WASHER, NUT AND COTTER KEY, WHICH, ALONG WITH A BOLT, SECURES THE UPPER TORQUE LINK TO THE LOWER. THE TIRE THEN TURNED SIDEWAYS PERPENDICULAR TO THE DIRECTION OF TRAVEL AFTER WHICH THE TIRE SKIDDED TO A STOP. EXAMINATION OF THE FAILURE REVEALED THAT CESSNA SERVICE INFORMATION LETTER ME83-37 WHICH RECOMMENDS REPLACEMENT OF THE TWO OUTER WASHERS WITH LARGER ONES, ON THE MAIN LANDING GEAR SCISSOR ASSY (TORQUE LINKS) HAD NOT BEEN COMPLIED WITH.

Other reports on N2696U · 1

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