19980926039189A

Accident · Substantial damage

FAA accident report · Gruman HU-16 · Sedona, AZ · September 26, 1998

Date
September 26, 1998 · 09:45 local
Place
Sedona, AZ
Airport
Sedona Airport
Phase of flight
Roll-Out (Fixed Wing)
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N7025J
NTSB investigation
NTSBLAX98LA313
Reported as
Gruman HU16
People aboard
6
Fatal injuries
0
Pilot’s flight hours
4,500 total360 in this make and model65 in the last 90 days

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.

(.19)On September 26, 1998, at 0945 hours mountain standard time, a Grumman HU-16, N7025J, veered off runway 3 on the landing rollout at the Sedona, Arizona, airport. The aircraft sustained substantial damage. The private pilot/owner, two flight crewmember, and three passengers were not injured. Visual meteorological conditions existed for the personal flight and a visual flight rules (VFR) flight plan was filed. According to a federal aviation administration inspector from the scottsdale, Arizona, flight standards district office, reported winds at the time of the accident were 180 degrees at 9 knots gusting to 14 knots. He further reported that runway 21 was the active runway. (.4) the private pilot/owner seated in the right seat was type rated in the airplane. The second pilot in the left seat manipulating the flight controls, held an ATP and flight instructor certificates, but was not type rated in the airplane. The second pilot had a total of 1.9 hours in the airplane. Both pilots stated that they selected runway 3 for landing based on weather reports and that other airplanes were using that runway. During landing rollout, propeller reverse power was selected and the craft engine came in before the right engine, which caused the airplane to veer left, and braking was used to correct the heading. The propellers were brought out of reverse and the airplane continued to exit the left side of the runway and collapsed the nose gear. The manager of the FBO said they were advising runway 21 as the active runway. The pilot of another airplane said that he had just landed on runway 21 and that there were two other airplanes in the traffic pattern for runway 21 when the accident airplane landed on runway 3. He stated that winds were 130 degrees at 14 knots and the conditions in the pattern were turbulent. The pilot noted that after he landed the wind kept shifting direction from a southeasterly to northeasterly heading. No mechanical anomalies were found during an examination of the propeller reverse system or the braking system. (-23) on September 26, 1998, @ approximately 1000HOURS, mountain standard time, aircraft N7025J, s/n 131910, veered off runway 03 at Sedona Airport, AZ. Five occupants on board suffered no injuries, aircraft sustained substantial damage to nose landing gear, fuselage hull, left wing and float. PIC o ccupied right seat and SIC occupied left. Sedona Airport UNICOM reporting left traffic pattern to runway 21, aircraft landed runway 03. Meteorological conditions prevailed, winds reported 180 @ 9 KTS, gust 14 KTS.

As the FAA filed it

(.19)ON SEPTEMBER 26, 1998, AT 0945 HOURS MOUNTAIN STANDARD TIME, A GRUMMAN HU-16, N7025J, VEERED OFF RUNWAY 3 ON THE LANDING ROLLOUT AT THE SEDONA, ARIZONA, AIRPORT. THE AIRCRAFT SUSTAINED SUBSTANTIAL DAMAGE. THE PRIVATE PILOT/OWNER, TWO FLIGHT CREWMEMBER, AND THREE PASSENGERS WERE NOT INJURED. VISUAL METEOROLOGICAL CONDITIONS EXISTED FOR THE PERSONAL FLIGHT AND A VISUAL FLIGHT RULES (VFR) FLIGHT PLAN WAS FILED. ACCORDING TO A FEDERAL AVIATION ADMINISTRATION INSPECTOR FROM THE SCOTTSDALE, ARIZONA, FLIGHT STANDARDS DISTRICT OFFICE, REPORTED WINDS AT THE TIME OF THE ACCIDENT WERE 180 DEGREES AT 9 KNOTS GUSTING TO 14 KNOTS. HE FURTHER REPORTED THAT RUNWAY 21 WAS THE ACTIVE RUNWAY. (.4) THE PRIVATE PILOT/OWNER SEATED IN THE RIGHT SEAT WAS TYPE RATED IN THE AIRPLANE. THE SECOND PILOT IN THE LEFT SEAT MANIPULATING THE FLIGHT CONTROLS, HELD AN ATP AND FLIGHT INSTRUCTOR CERTIFICATES, BUT WAS NOT TYPE RATED IN THE AIRPLANE. THE SECOND PILOT HAD A TOTAL OF 1.9 HOURS IN THE AIRPLANE. BOTH PILOTS STATED THAT THEY SELECTED RUNWAY 3 FOR LANDING BASED ON WEATHER REPORTS AND THAT OTHER AIRPLANES WERE USING THAT RUNWAY. DURING LANDING ROLLOUT, PROPELLER REVERSE POWER WAS SELECTED AND THE CRAFT ENGINE CAME IN BEFORE THE RIGHT ENGINE, WHICH CAUSED THE AIRPLANE TO VEER LEFT, AND BRAKING WAS USED TO CORRECT THE HEADING. THE PROPELLERS WERE BROUGHT OUT OF REVERSE AND THE AIRPLANE CONTINUED TO EXIT THE LEFT SIDE OF THE RUNWAY AND COLLAPSED THE NOSE GEAR. THE MANAGER OF THE FBO SAID THEY WERE ADVISING RUNWAY 21 AS THE ACTIVE RUNWAY. THE PILOT OF ANOTHER AIRPLANE SAID THAT HE HAD JUST LANDED ON RUNWAY 21 AND THAT THERE WERE TWO OTHER AIRPLANES IN THE TRAFFIC PATTERN FOR RUNWAY 21 WHEN THE ACCIDENT AIRPLANE LANDED ON RUNWAY 3. HE STATED THAT WINDS WERE 130 DEGREES AT 14 KNOTS AND THE CONDITIONS IN THE PATTERN WERE TURBULENT. THE PILOT NOTED THAT AFTER HE LANDED THE WIND KEPT SHIFTING DIRECTION FROM A SOUTHEASTERLY TO NORTHEASTERLY HEADING. NO MECHANICAL ANOMALIES WERE FOUND DURING AN EXAMINATION OF THE PROPELLER REVERSE SYSTEM OR THE BRAKING SYSTEM. (-23) ON SEPTEMBER 26, 1998, @ APPROXIMATELY 1000HOURS, MOUNTAIN STANDARD TIME, AIRCRAFT N7025J, S/N 131910, VEERED OFF RUNWAY 03 AT SEDONA AIRPORT, AZ. FIVE OCCUPANTS ON BOARD SUFFERED NO INJURIES, AIRCRAFT SUSTAINED SUBSTANTIAL DAMAGE TO NOSE LANDING GEAR, FUSELAGE HULL, LEFT WING AND FLOAT. PIC O CCUPIED RIGHT SEAT AND SIC OCCUPIED LEFT. SEDONA AIRPORT UNICOM REPORTING LEFT TRAFFIC PATTERN TO RUNWAY 21, AIRCRAFT LANDED RUNWAY 03. METEOROLOGICAL CONDITIONS PREVAILED, WINDS REPORTED 180 @ 9 KTS, GUST 14 KTS.

NTSB investigation

The NTSB’s investigation of this event, with its probable cause and findings. Matched to this report by N-number and date.