19990304013389I

Incident · Minor damage

FAA incident report · Boeing 737200 · Kansas City, MO · March 4, 1999

Date
March 4, 1999 · 08:50 local
Place
Kansas City, MO
Airport
Kansas City International
Phase of flight
Final Approach
Operating rules
Air carrier (Part 121)
Operator
SWAA
Damage
Minor damage
Aircraft
N95SW
Reported as
Boeing 737200
People aboard
112
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.

On 3-4-99 at 0850, southwest airlines flight 500, a Boeing 737-200 declared an emergency landing while on approach into Kansas City International Airport. The pilot landed the aircraft safely and proceeded to the gate without further incident. The pilot reported that his trailing edge devices would not extend beyond 8 degrees. Alternate flap extension system was tried, but was of no help. His leading edge devices operated normal. Swa operations contacted their on call maintenance. Contract aviation maintenance (cam) found the r/h inboard flap torque shaft clearance door was broken and causing inteference with the flap jackscrew operation.. The door was removed per cdl 57-53-1 and is being tracked by #21019. The flaps were cycled processing of this report closes incident number CE99IACOO37.

As the FAA filed it

ON 3-4-99 AT 0850, SOUTHWEST AIRLINES FLIGHT 500, A BOEING 737-200 DECLARED AN EMERGENCY LANDING WHILE ON APPROACH INTO KANSAS CITY INTERNATIONAL AIRPORT. THE PILOT LANDED THE AIRCRAFT SAFELY AND PROCEEDED TO THE GATE WITHOUT FURTHER INCIDENT.THE PILOT REPORTED THAT HIS TRAILING EDGE DEVICES WOULD NOT EXTEND BEYOND 8 DEGREES. ALTERNATE FLAP EXTENSION SYSTEM WAS TRIED, BUT WAS OF NO HELP. HIS LEADING EDGE DEVICES OPERATED NORMAL. SWA OPERATIONS CONTACTED THEIR ON CALL MAINTENANCE. CONTRACT AVIATION MAINTENANCE (CAM) FOUND THE R/H INBOARD FLAP TORQUE SHAFT CLEARANCE DOOR WAS BROKEN AND CAUSING INTEFERENCE WITH THE FLAP JACKSCREW OPERATION.. THE DOOR WAS REMOVED PER CDL 57-53-1 AND IS BEING TRACKED BY #21019. THE FLAPS WERE CYCLED PROCESSING OF THIS REPORT CLOSES INCIDENT NUMBER CE99IACOO37.