N365ES

CESSNA 172R · 1997 · Valid Registration

Registered owner: LAKEWOOD INVESTMENTS LLC, CA (owner ≠ operator)

Operators of this aircraft

Who operated this tail, and how firmly we know it.

No operator established for this aircraft.

Accident & incident history

No NTSB accidents or incidents on file for this aircraft.

Maintenance disclosures

R J · 2016-08-29 Unresolved
ATA 8520

CRANKSHAFT BROKE AT THE NR 4 CONNECTING ROD JOURNAL, SEPARATION OCCURRED AT THE NR 5 CHEEK COUNTING FROM THE FRONT OF CRANKSHAFT.

Source: SDR T22R R/O9856 · FAA SDRS
O · 1998-02-20 Unresolved
ATA 5412

DURING 100-HOUR INSPECTION, FOUND FIREWALL CRACKED AT THE LOWER LEFT COWL SHOCK MOUNT BELOW THE BATTERY BOX. VISIBLE PORTION OF CRACK WAS APPROXIMATELY .50 INCH LONG. AFTER CLOSER EXAMINATION FROM INSIDE THE CABIN, THE CRACK APPEARED TO BE ABOUT 3 INCHES LONG AND ORIGINATING FROM A RIVET HOLE. DOUBLER WAS FABRICATED AND INSTALLED ON INSIDE OF CABIN. CRACK DEVELOPED POSSIBLY FROM IMPROPER SHEET METAL PRACTICES AT MANUFACTURE.

Source: SDR 98ZZZX973 · FAA SDRS
O · 1998-02-20 Unresolved
ATA 5512

DURING 100-HOUR INSPECTION, FOUND 4 OF THE AN426 RIVETS SECURING THE UPPER HORIZONTAL STABILIZER SKIN PULLED COMPLETELY THROUGH ON THE LEFT SIDE. ALL OF THE REMAINING RIVETS BOTH LEFT AND RIGHT SIDE SHOWED SIGNS OF WORKING THESE RIVETS ARE INBOARD UNDER THE STABILZIER ROOT FAIRING. OLDER 172'S USE UNIVERSAL HEAD RIVETS WITH NO PROBLEMS OF WORKING. OBTAINED REPAIR PROCEDURE FROM CESSNA AND PROBLEM WAS CORRECTED.

Source: SDR 98ZZZX974 · FAA SDRS
O · 1997-12-30 Matched by certificate designator
ATA 2842

RIGHT FUEL QUANTITY GAUGE INOPERABLE. TRACED PROBLEM TO TRANSMITTER IN RT WING. PLASTIC FLOAT HAD SEPARATED FROM THE ARM AND WAS ALLOWING THE ARM TO SINK. FLOAT FAILED BECAUSE OF INADEQUATE CRIMP ON ARM WHICH ALLOWED THE RETAINING WASHER AND FLOAT TO COME OFF. THIS TRANSMITTER WAS INSTALLED ONLY 11.0 HOURS AGO. ANOTHER NEW TRANSMITTER WAS INSTALLED AND SYSTEM APPEARS TO OPERATE NORMALLY.

Source: SDR 98ZZZX164 · FAA SDRS
W · 1997-12-19 Matched by certificate designator
ATA 2215

DURING ROUTINE INSPECTION, FOUND AUTOPILOT SERVO CONTROL CABLE WRAPPED AROUND RT AILERON CONTROL CABLE. MM DOES NOT SHOW THESE CABLES CROSSED. INSPECTED CABLES FOR DAMAGE AND POSITIONED PROPERLY. AIRCRAFT WAS DELIVERED FROM THE MANUFACTURER WITH THIS CONDITION.

Source: SDR 98ZZZX163 · FAA SDRS
O · 1997-12-19 Matched by certificate designator
ATA 2842

PILOT COMPLAINED OF FLUCTUATING FUEL QUANTITY INDICATING GAUGE. TRACED PROBLEM TO BOTH LEFT AND RIGHT QUANTITY TRANSMITTERS GIVING ERRONEOUS OHM READINGS. REPLACED TRANSMITTERS AND SYSTEM OPERATES NORMALLY.

Source: SDR 98ZZZX165 · FAA SDRS