N4118K

CESSNA 208B · 2007 · Fixed-wing single-engine · 1 engine · 12 seats · Valid Registration

Registered owner: SOUTHERN AIRWAYS PACIFIC LLC, FL (owner ≠ operator)

Operators of this aircraft

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

OperatorRolePeriodBasis
Multi-Aero Inc. (MUIA)Certificate holderMatched by certificate designator

Accident & incident history

No NTSB accidents or incidents on file for this aircraft.

Maintenance disclosures

Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.

4 reports on file, 2014-11-18 – 2025-04-23.

SMOKE/FUMES/ODORS/SPARKS; WARNING INDICATION · 2025-04-23 Matched by certificate designator
ATA 2421

Part: GENERATOR — FAILED

AROUND 10K FEET 40 MILES FROM BRL, CREW HEARD LOUD BANG FOLLOWED BY SMELL OF SMOKE. FEW MINUTES LATER GEN OFF/STANDBY POWER ON CAME ON. CREW DECLARED EMERGENCY AND CONTINUED TO BRL.THE SMELL WENT AWAY ONCE FINISHED WITH THE CHECKLIST. LANDED SAFELY

Source: SDR 141A202504230001
AFFECT SYSTEMS · 2023-10-15 Matched by certificate designator
ATA 3242

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 18,478 hrs · 17,878 cycles

BRAKE FAILURE ON BOTH PILOT AND CO-PILOTS SIDE. BOTH BRAKE CALIPERS HAD BEEN REPLACED 2 DAYS PRIOR. THE CORRECTIVE ACTION FOR THIS INCIDENT WAS REMOVING TRAPPED AIR BY BACK BLEEDING BRAKE SYSTEM. THERE WAS NO PART OR COMPONENT FAILURE

Source: SDR 2023F00308
SMOKE/FUMES/ODORS/SPARKS · 2018-03-29 Matched by certificate designator
ATA 2435

Part: STARTER GEN — FAULTY (ENGINE) · airframe 10,672 hrs

CREW PERFORMED GATE RETURN DUE TO A BURNING ODOR. MAINTENANCE FOUND THE STARTER GENERATOR TO BE FAULTY. REPLACED THE STARTER GENERATOR WITH SERVICEABLE UNIT WITH NO FURTHER ISSUES.

Source: SDR MUIA2018002020001
FLUID LOSS · 2014-11-18 Matched by certificate designator
ATA 1230

Part: BRAKE CALIPER — LEAKING (RT MLG) · airframe 3,153 hrs · 4,410 cycles

RIGHT MAIN WHEEL BRAKE CYLINDER HAD PUCK LEAKING HYDRAULIC FLUID CAUSING THE BRAKE PEDAL TO GO TO THE FLOOR AND FAIL TO STOP AIRCRAFT.

Source: SDR MUIA2014112000001