Accident Cessna 172N N1571E,
ASN logo
ASN Wikibase Occurrence # 364087
 
This information is added by users of ASN. Neither ASN nor the Flight Safety Foundation are responsible for the completeness or correctness of this information. If you feel this information is incomplete or incorrect, you can submit corrected information.

Date:Sunday 12 January 1992
Time:10:40 LT
Type:Silhouette image of generic C172 model; specific model in this crash may look slightly different    
Cessna 172N
Owner/operator:K & M Aviation
Registration: N1571E
MSN: 17271049
Year of manufacture:1978
Total airframe hrs:9000 hours
Engine model:LYCOMING O-320-H2AD
Fatalities:Fatalities: 0 / Occupants: 3
Aircraft damage: Substantial
Category:Accident
Location:Show Low, AZ -   United States of America
Phase: En route
Nature:Private
Departure airport:Phoenix, AZ (KDVT)
Destination airport:Albuquerque, NM
Investigating agency: NTSB
Confidence Rating: Accident investigation report completed and information captured
Narrative:
THE PILOT SAID WHILE IN LEVEL CRUISE ON AN IFR FLIGHT THE ENGINE BEGAN TO LOOSE POWER DUE TO CARBURETOR ICE AND ATTEMPTS TO REMEDY THE SITUATION WERE UNSUCCESSFUL WITH THE ENGINE EVENTUALLY LOOSING ALL POWER. THE PILOT DECLARED AN EMERGENCY WITH ALBUQUERQUE CENTER AND WAS RADAR VECTORED TOWARD THE SHOW LOW AIRPORT. THE FLIGHT WAS INTERMITTENTLY IN CLOUDS DURING THE EMERGENCY DESCENT AND BROKE OUT AT A LOW ALTITUDE. THE AIRCRAFT HAD INSUFFICIENT ALTITUDE TO MAKE THE AIRPORT AND LANDED IN THE ONLY AVAILABLE LOCATION, A FIELD ABOUT 23 MILES FROM THE AIRPORT. DURING ROLL OUT, THE AIRCRAFT COLLIDED WITH A DITCH AND NOSED OVER. POST ACCIDENT EXAMINATION OF THE AIRCRAFT BY FAA INSPECTORS REVEALED THAT THE CARBURETOR HEAT BOX HAD SEPARATED FROM THE HEAT MUFF OF THE EXHAUST SYSTEM AND WAS HANGING LOOSE IN THE COWLING ATTACHED ONLY BY THE FABRIC HOSE. A METAL BAND WHICH ATTACHES THE CARB HEAT BOX TO THE MUFF HAD SEPARATED. CHAFFING ON THE COWLING IN THE AREA OF WHERE THE HEAT BOX WAS HANGING INDICATED IT HAD BEEN SEPARATED FOR SOME TIME. THE LAST 100 HOUR INSPECTION WAS ACCOMPLISHED 80 OPERATING HOURS PRIOR TO THE ACCIDENT.

Probable Cause: THE FAILURE OF THE CARBURETOR HEAT BOX ATTACH STRAPS WHICH ALLOWED THE CARBURETOR HEAT BOX TO SEPARATE FROM THE EXHAUST SYSTEM HEAT MUFF AND RENDERED THE CARBURETOR HEAT SYSTEM INOPERATIVE. THE ENGINE THEN LOST POWER DUE TO CARBURETOR ICE.

Accident investigation:
cover
  
Investigating agency: NTSB
Report number: LAX92LA089
Status: Investigation completed
Duration: 1 year and 7 months
Download report: Final report

Sources:

NTSB LAX92LA089

Location

Revision history:

Date/timeContributorUpdates
19-Mar-2024 09:18 ASN Update Bot Added

Corrections or additions? ... Edit this accident description

The Aviation Safety Network is an exclusive service provided by:
Quick Links:

CONNECT WITH US: FSF on social media FSF Facebook FSF Twitter FSF Youtube FSF LinkedIn FSF Instagram

©2024 Flight Safety Foundation

1920 Ballenger Av, 4th Fl.
Alexandria, Virginia 22314
www.FlightSafety.org