NTSB ATL89FA182 — 1989-07-20 · RIDGELAND, South Carolina, United States

Aircraft involved

N4254L Cessna 172G Fatal

Probable cause & findings

IMPROPER PLANNING/DECISION BY THE PILOT-IN-COMMAND (PIC), WHICH RESULTED IN AN INADVERTENT STALL DURING TAKEOFF. FACTORS RELATED TO THE ACCIDENT WERE: THE EXCESSIVE GROSS WEIGHT AND IMPROPER LIFT-OFF BY THE PIC, THE PILOT/PASSENGER'S IMPROPER CREW COORDINATION REGARDING THE SPECIFIC INSTRUCTIONS THAT HE RECEIVED CONCERNING THE PAYLOAD LIMITATIONS, AND THE HIGH DENSITY ALTITUDE.

Factual narrative

TWO PLTS WERE SEATED AT THE CONTROLS. THE RIGHT FRONT SEAT PLT HAD RENTED THE ACFT; HE HAD 59 HRS TOTAL FLT TIME, OF WHICH, 3 HRS WAS IN THE CESSNA 172. THE LEFT FRONT SEAT PLT (NORMAL PSN FOR THE PIC) HAD 120 HRS OF FLT TIME, OF WHICH, 52 HRS WAS IN THE CESSNA 172. BEFORE RENTING THE ACFT, THE RIGHT FRONT SEAT PLT WAS TOLD OF THE ACFT'S LIMITED PAYLOAD & RWY LENGTH REQUIREMENTS DUE TO THE AUXILIARY FUEL CAPACITY. THE ACFT HAD BEEN REFUELED TO ITS CAPACITY AT THE EN ROUTE ARPT. DURING TAKEOFF FROM THE 3100 FT RWY, THE ACFT LIFTED OFF, SETTLED BACK ONTO RWY & LIFTED OFF AGAIN. THE ACFT CLIMBED WITH A STEEP NOSE HIGH ATTITUDE TO ABOUT 200 TO 250 FT, THEN IT ENTERED A STEEP DSCNT & CRASHED. THE WIND WAS RPRTD TO BE ALIGNED WITH THE RWY AT 10 KTS & THE TEMP WAS ABOUT 90 DEG. THE ACFT WAS ESTD TO HAVE BEEN LOADED ABOUT 120 LBS OVER ITS MAX WT LIMIT. NO PREIMPACT PART FAILURE OR MALFUNCTION OF THE ACFT WAS FOUND. DENSITY ALT WAS APRX 2100 FT. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12

Verbatim from NTSB's published report. Source file NTSB_1989_ATL89FA182.txt. Findings + structured fields enriched from FAA avall.mdb. Full investigation docket on data.ntsb.gov ↗.

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