19970206045929A

Accident · Substantial damage

FAA accident report · Airbus A300 B4-605R · St Johns, AC · February 6, 1997

Date
February 6, 1997 · 14:40 local
Place
St Johns, AC
Airport
St Johns/V C Bird Antigua
Phase of flight
Final Approach
Operating rules
Air carrier (Part 121)
Operator
AALA
Damage
Substantial damage
Aircraft
N41063
NTSB investigation
NTSBDCA97LA027
Reported as
Airbus A300B4605R
Reported engine
GE CF680C2A5
People aboard
170
Fatal injuries
0
Pilot’s flight hours
19,000 total4,671 in this make and model

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.

(.4)The scheduled flight from san juan to the Antigua (anu) area was uneventful. During the VOR 07 approach, at about 2,500 feet AGL, the flight maneuvered to avoid TCAS traffic. The runway was in sight. The captain was flying the transport category airplane on final approach with 40 degrees of flaps. At 1,000 feet, on the final approach to landing, the first officer made the company procedural 1,000 foot verbal callout and the captain brought the power above idle. The crew stated that the airplane was slightly high at 1,000 feet and by 500 feet they were 'in the slot' with airspeed about 20 knots above the reference speed of 128 knots and decreasing. Flight recorder data indicated that during the final approach segment from about an altitude of 500 feet to the ground, the airspeed decreased from 143 knots to 135, the pitch attitude increased from 1/2-degree nose up to 9 degrees nose up, the descent rate decreased from 1,700 feet per minute (fpm) to 1,000 fpm, and the flight path angle decreased from 5.8 degrees to 2.7 degrees. The airplane contacted the runway on the main landing gear and bounced, at which time the airplane pitched nose up to about 11 degrees. The tail of t he airplane subseqently struck the runway and was substantially damaged. No anomlaies with the airplanes systems or engines were reported during the investigation. The airplane's aircraft operating manual described a "stabilized approach concept", but the airline did not provide specific procedures regarding crew actions, ro require a go-around, if an approach becomes unstabilized.

As the FAA filed it

(.4)THE SCHEDULED FLIGHT FROM SAN JUAN TO THE ANTIGUA (ANU) AREA WAS UNEVENTFUL. DURING THE VOR 07 APPROACH, AT ABOUT 2,500 FEET AGL, THE FLIGHT MANEUVERED TO AVOID TCAS TRAFFIC. THE RUNWAY WAS IN SIGHT. THE CAPTAIN WAS FLYING THE TRANSPORT CATEGORY AIRPLANE ON FINAL APPROACH WITH 40 DEGREES OF FLAPS. AT 1,000 FEET, ON THE FINAL APPROACH TO LANDING, THE FIRST OFFICER MADE THE COMPANY PROCEDURAL 1,000 FOOT VERBAL CALLOUT AND THE CAPTAIN BROUGHT THE POWER ABOVE IDLE. THE CREW STATED THAT THE AIRPLANE WAS SLIGHTLY HIGH AT 1,000 FEET AND BY 500 FEET THEY WERE 'IN THE SLOT' WITH AIRSPEED ABOUT 20 KNOTS ABOVE THE REFERENCE SPEED OF 128 KNOTS AND DECREASING. FLIGHT RECORDER DATA INDICATED THAT DURING THE FINAL APPROACH SEGMENT FROM ABOUT AN ALTITUDE OF 500 FEET TO THE GROUND, THE AIRSPEED DECREASED FROM 143 KNOTS TO 135, THE PITCH ATTITUDE INCREASED FROM 1/2-DEGREE NOSE UP TO 9 DEGREES NOSE UP, THE DESCENT RATE DECREASED FROM 1,700 FEET PER MINUTE (FPM) TO 1,000 FPM, AND THE FLIGHT PATH ANGLE DECREASED FROM 5.8 DEGREES TO 2.7 DEGREES. THE AIRPLANE CONTACTED THE RUNWAY ON THE MAIN LANDING GEAR AND BOUNCED, AT WHICH TIME THE AIRPLANE PITCHED NOSE UP TO ABOUT 11 DEGREES. THE TAIL OF T HE AIRPLANE SUBSEQENTLY STRUCK THE RUNWAY AND WAS SUBSTANTIALLY DAMAGED. NO ANOMLAIES WITH THE AIRPLANES SYSTEMS OR ENGINES WERE REPORTED DURING THE INVESTIGATION. THE AIRPLANE'S AIRCRAFT OPERATING MANUAL DESCRIBED A "STABILIZED APPROACH CONCEPT", BUT THE AIRLINE DID NOT PROVIDE SPECIFIC PROCEDURES REGARDING CREW ACTIONS, RO REQUIRE A GO-AROUND, IF AN APPROACH BECOMES UNSTABILIZED.

NTSB investigation

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

Other reports on N41063 · 3

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