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ASN Wikibase Occurrence # 135315
Last updated: 2 April 2020
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Date:26-OCT-2003
Time:14:19
Type:Silhouette image of generic M20T model; specific model in this crash may look slightly different
Mooney M20K
Owner/operator:Private
Registration: N1147N
C/n / msn: 25-0596
Fatalities:Fatalities: 0 / Occupants: 1
Other fatalities:0
Aircraft damage: Written off (damaged beyond repair)
Category:Accident
Location:San Diego, CA -   United States of America
Phase: Approach
Nature:Private
Departure airport:St. Johns, AZ (KSJN)
Destination airport:San Diego, CA (KMYF)
Investigating agency: NTSB
Narrative:
The airplane landed hard on a highway while attempting to perform a go-around from runway 28R. The pilot received a preflight weather briefing from 1120 to 1131 and was advised he could not file IFR into the destination airport due to the closure of the TRACON and the airport ATCT due to a major forest fire threatening the facilities. He was advised he "might be able to get in VFR." He filed IFR to an intersection located in the vicinity of his destination airport. Once the flight arrived in the general destination area, the pilot canceled his IFR clearance and flew visually to the airport. After attempting to land runway 28R, he applied power for a go-around. He retracted the flaps but left the landing gear down, and did not put the propeller control in the full forward position. As the pilot maneuvered during the go-around he turned into a tailwind situation and the airplane was unable to maintain a climb. The airplane descended to impact on a highway. A post crash fire erupted and consumed the airplane. The POH for the airplane states that the propeller control should be at a high rpm during landing. For a go-around procedure, the POH indicates that the pilot should apply power, retract the flaps to the takeoff position [10 degrees], and then retract the landing gear and remaining flaps once the airplane accelerates to 91 mph (77 knots) IAS. A post-accident inspection revealed that the propeller governor control arm was 3/8-inch from the low pitch stop. A METAR was issued at 1414 that noted the wind was from 070 degrees at 6 knots, gusting to 14 knots. No discrepancies were found duirng an examination of the engine.
Probable Cause: the pilot's failure to configure the airplane properly for the go-around which resulted in degraded climb performance, and his failure to maintain adequate airspeed which resulted in a stall. The tailwind was a contributing factor.

Sources:

NTSB: https://www.ntsb.gov/_layouts/ntsb.aviation/brief.aspx?ev_id=20031028X01819&key=1


Revision history:

Date/timeContributorUpdates
24-Dec-2014 19:28 Anon. Updated [Operator, Narrative]
21-Dec-2016 19:26 ASN Update Bot Updated [Time, Damage, Category, Investigating agency]
08-Dec-2017 20:00 ASN Update Bot Updated [Other fatalities, Departure airport, Destination airport, Source, Narrative]

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