19970102008739I

Incident · Minor damage

FAA incident report · Piper PA-24-180 · Albuquerque, NM · January 2, 1997

Date
January 2, 1997 · 13:30 local
Place
Albuquerque, NM
Phase of flight
Fcd/Prec Ldg From Cruise
Operating rules
General operating rules (Part 91)
Damage
Minor damage
Aircraft
N6622P
Reported as
Piper PA24180
People aboard
3
Fatal injuries
0

From the FAA’s Accident/Incident Data System (AIDS), through its Aviation Safety Information Portal, as reported. The NTSB investigates accidents separately, and its record of an accident is the fuller one. The aircraft is matched to the registry by N-number and event date, checked against the reported make and model; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

What happened

The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.

Narrative: on January 2, 1997, a Piper PA24-180, N6622P departed santa fe, NM on a pleasure flight to return to santa fe. The private pilot elected to make a precautionary landing in mountainous terrain approximately 35 miles west of Albuquerque, NM. The landing was successful and minor damage to the left wing tip occurred when the aircraft struck brush on roll out. No injuries were sustained to the pilot or the two passengers. Follow-up investigation revealed the right exhaust pipe failed which allowed the hot gases to be directed onto a rubber boot that covers the right steering rod where it penetrates the firewall. M or d report to be submitted.

As the FAA filed it

NARRATIVE: ON JANUARY 2, 1997, A PIPER PA24-180, N6622P DEPARTED SANTA FE, NM ON A PLEASURE FLIGHT TO RETURN TO SANTA FE. THE PRIVATE PILOT ELECTED TO MAKE A PRECAUTIONARY LANDING IN MOUNTAINOUS TERRAIN APPROXIMATELY 35 MILES WEST OF ALBUQUERQUE, NM. THE LANDING WAS SUCCESSFUL AND MINOR DAMAGE TO THE LEFT WING TIP OCCURRED WHEN THE AIRCRAFT STRUCK BRUSH ON ROLL OUT. NO INJURIES WERE SUSTAINED TO THE PILOT OR THE TWO PASSENGERS. FOLLOW-UP INVESTIGATION REVEALED THE RIGHT EXHAUST PIPE FAILED WHICH ALLOWED THE HOT GASES TO BE DIRECTED ONTO A RUBBER BOOT THAT COVERS THE RIGHT STEERING ROD WHERE IT PENETRATES THE FIREWALL. M OR D REPORT TO BE SUBMITTED.

Other reports on N6622P · 1

Matched to the same aircraft by N-number and date.