19960125002059I

Incident · Minor damage

FAA incident report · Boeing 737 2J8 · Wichita, KS · January 25, 1996

Date
January 25, 1996 · 14:30 local
Place
Wichita, KS
Airport
Wichita Mid-Continent
Phase of flight
Forced/Precautionary Landing
Operating rules
Air carrier (Part 121)
Operator
DALA
Damage
Minor damage
Aircraft
N235WA
Reported as
Boeing 7372J8
People aboard
88
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: delta flt 846 from ict to atl on 1/25/96 a/c B-737 number N235WA at gear retraction, on takeoff at ict, left main gear remained illuminated with gear up. Recycled gear, and as gear returned to up position "a" system hydraulic quantity began decreasing. Put gear back down prior to loss of all "a" hydraulic quantity. Uneventful flaps 15 landing. Towed to gate and pinned gear. Found ruptured hydraulic line on "a" system hydraulic side of left main gear retract actuator. Replaced line with temporary hydraulic line. Leak check good, removed gear pins and serviced hydraulic system reservoir. At engine start on 1/26/96 "a" system hydraulic system and serviced head pressure. Restarted engine and "a" hydraulic system checked normal. Delayed flight 846 departed.

As the FAA filed it

NARRATIVE: DELTA FLT 846 FROM ICT TO ATL ON 1/25/96 A/C B-737 NUMBER N235WA AT GEAR RETRACTION, ON TAKEOFF AT ICT, LEFT MAIN GEAR REMAINED ILLUMINATED WITH GEAR UP. RECYCLED GEAR, AND AS GEAR RETURNED TO UP POSITION "A" SYSTEM HYDRAULIC QUANTITY BEGAN DECREASING. PUT GEAR BACK DOWN PRIOR TO LOSS OF ALL "A" HYDRAULIC QUANTITY. UNEVENTFUL FLAPS 15 LANDING. TOWED TO GATE AND PINNED GEAR. FOUND RUPTURED HYDRAULIC LINE ON "A" SYSTEM HYDRAULIC SIDE OF LEFT MAIN GEAR RETRACT ACTUATOR. REPLACED LINE WITH TEMPORARY HYDRAULIC LINE. LEAK CHECK GOOD, REMOVED GEAR PINS AND SERVICED HYDRAULIC SYSTEM RESERVOIR. AT ENGINE START ON 1/26/96 "A" SYSTEM HYDRAULIC SYSTEM AND SERVICED HEAD PRESSURE. RESTARTED ENGINE AND "A" HYDRAULIC SYSTEM CHECKED NORMAL. DELAYED FLIGHT 846 DEPARTED.

Other reports on N235WA · 1

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