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CHI90FA146

1990-06-03 · GAYLORD, Michigan, United States · Fatal · 1 aircraft · Status: Completed

Airport GLR

Aircraft involved

Probable cause & findings

THE PILOT'S INADEQUATE AIRSPEED, WHILE MANEUVERING (TURNING) AFTER TAKEOFF, WHICH RESULTED IN A STALL/MUSH. FACTORS RELATED TO THE ACCIDENT WERE: THE PILOT'S IMPROPER PLANNING/DECISION, FAILURE TO MAINTAIN WEIGHT AND BALANCE LIMITS, AND ADVERSE WIND CONDITIONS.

Factual narrative

AFTER LNDG, THE PLT SEEMED CONCERNED ABOUT THE ACFT'S WT & ASKED THE ATTENDANT TO SVC THE FUEL TANKS THE BOTTOM OF THE TABS. AFTER LOADING WITH 3 PSGRS & BAGGAGE, HE TOOK OFF ON RWY 27. WINDS WERE RPRTD TO BE FM 260 DEG AT 20 GSTG 30 KTS; LOW LEVEL WIND SHEAR & TURBULENCE WERE RPRTD IN THE AREA. ACCORDING TO WITNESSES, THE ACFT SEEMED TO ACCELERATE SLOWLY &IT LIFTED OFF AFTER ROLLING ABOUT 1500 TO 2000 FT. THEY NOTED THAT IT WAS CLIMBING AT A SLOW RATE & TURNED LEFT (TO THE SOUTH, THEN EAST) AT 150 TO 200 FT AGL. ONE WITNESS NOTED THE ACFT'S NOSE WAS HIGHER THAN USUAL. ANOTHER RPRTD THE ACFTWAS 'STAGGERING: A SLOW PORPOISING MOTION NOT GAINING AIRSPEED.' THE ACFT THEN BANKED LEFT, DSCNDD & IMPACTED, RGT MAINGEAR 1ST ON A HDG OF 080 DEG. AFTER INPACT, FIRE ERUPTED, & THE ACFT SLID 105 FT & BURNED. NO PREIMPACT PART FAILURE OR MALFUNCTION WAS FND. THE ACFT WAS ESTD TO HAVE BEEN LOADED TO 3680 LBS WITH A CG OF 89.4 INCHES. THE CERT MAX GROSS WT WAS 3600 LBS; THE CG LIMITS WERE FROM 81.0 TO 87.7 INCHES. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12

Verbatim from NTSB's published report. Source file NTSB_1990_CHI90FA146.txt. Findings + structured fields enriched from FAA avall.mdb. Full investigation docket on data.ntsb.gov ↗.

Related research

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