Multiple aircraft equipment problems malfunctions during single engine approach. Training in progres...

Attributes
ACN	263630
Time
Date	199402
Day	Sun
Local Time Of Day	0601 To 1200
Place
Locale Reference	airport : orl
State Reference	FL
Altitude	agl bound lower : 200 agl bound upper : 500
Environment
Flight Conditions	VMC
Light	Daylight
Aircraft 1
Controlling Facilities	tower : orl
Operator	general aviation : personal
Make Model Name	Beechcraft Twin Piston Undifferentiated or Other Model
Operating Under FAR Part	Part 91
Flight Phase	descent : approach landing : go around
Flight Plan	IFR
Person 1
Affiliation	Other
Function	instruction : instructor oversight : pic
Qualification	pilot : instrument pilot : commercial pilot : atp
Experience	flight time last 90 days : 109 flight time total : 6600 flight time type : 100
ASRS Report	263630
Person 2
Affiliation	Other
Function	flight crew : single pilot instruction : trainee
Qualification	pilot : instrument pilot : commercial
Events
Anomaly	aircraft equipment problem : critical conflict : ground less severe other anomaly other other spatial deviation
Independent Detector	other flight crewa
Resolutory Action	flight crew : exited adverse environment flight crew : overcame equipment problem flight crew : declared emergency
Consequence	Other
Supplementary
Primary Problem	Aircraft
Air Traffic Incident	Pilot Deviation

Narrative:

Mr. X, owner pilot, was flying beech baron. Mr. Y, an instructor, was in right front seat. Pilot was flying well on a training flight (IFR) which included emergency procedures. Beech baron was on 12 mi final and announced to orlando executive tower that it intended to land straight in on runway 25 (VOR DME 25) with a simulated emergency, right engine was feathered. Was cleared to land. Owner pilot per training procedure lowered landing gear. Landing gear down lock lights did not come on. At approximately missed approach point at MDA, about 500 ft, we announced a missed approach. Left operating engine was advanced to takeoff power. Aircraft was maintained at vyse blue line indicated airspeed. We initially failed to climb, in fact, lost a couple hundred ft altitude when maintaining proper airspeed control. With landing gear extended and right engine feathered, aircraft was not climbing. Aircraft was flown under control to approximately 200 ft AGL 1/2 mi beyond departure end of runway 25. Decision was made to start right engine and climb out using both engines at takeoff power. Gear was not immediately retracted because of manual extension. Unable to move landing gear from down (unlocked) position. Did not know status of landing mechanism. Right engine unfeathering accumulator did not work. (Feathered engine procedure with unfeathering accumulator was tested satisfactorily at altitude of 5000 ft first). Started right engine using starter. Right engine operated normally and with both engines operating, flew to safe altitude, departed pattern. Tested system (landing gear) all normal. Cleared to land, normal safe landing. Emergency crash crews were not called for landing since all system normal at landing.

Original NASA ASRS Text

Title: MULTIPLE ACFT EQUIP PROBS MALFUNCTIONS DURING SINGLE ENG APCH. TRAINING IN PROGRESS. BUZZ JOB ON SURROUNDING TERRAIN IN PROX OF ATA OCCURS ON GAR. HAD BEEN CLRED TO LAND BUT WENT AROUND ACCOUNT POSSIBLE INVOLVEMENT WITH GEAR INDICATION.

Narrative: MR. X, OWNER PLT, WAS FLYING BEECH BARON. MR. Y, AN INSTRUCTOR, WAS IN R FRONT SEAT. PLT WAS FLYING WELL ON A TRAINING FLT (IFR) WHICH INCLUDED EMER PROCS. BEECH BARON WAS ON 12 MI FINAL AND ANNOUNCED TO ORLANDO EXECUTIVE TWR THAT IT INTENDED TO LAND STRAIGHT IN ON RWY 25 (VOR DME 25) WITH A SIMULATED EMER, R ENG WAS FEATHERED. WAS CLRED TO LAND. OWNER PLT PER TRAINING PROC LOWERED LNDG GEAR. LNDG GEAR DOWN LOCK LIGHTS DID NOT COME ON. AT APPROX MISSED APCH POINT AT MDA, ABOUT 500 FT, WE ANNOUNCED A MISSED APCH. L OPERATING ENG WAS ADVANCED TO TKOF PWR. ACFT WAS MAINTAINED AT VYSE BLUE LINE INDICATED AIRSPD. WE INITIALLY FAILED TO CLB, IN FACT, LOST A COUPLE HUNDRED FT ALT WHEN MAINTAINING PROPER AIRSPD CTL. WITH LNDG GEAR EXTENDED AND R ENG FEATHERED, ACFT WAS NOT CLBING. ACFT WAS FLOWN UNDER CTL TO APPROX 200 FT AGL 1/2 MI BEYOND DEP END OF RWY 25. DECISION WAS MADE TO START R ENG AND CLB OUT USING BOTH ENGS AT TKOF PWR. GEAR WAS NOT IMMEDIATELY RETRACTED BECAUSE OF MANUAL EXTENSION. UNABLE TO MOVE LNDG GEAR FROM DOWN (UNLOCKED) POS. DID NOT KNOW STATUS OF LNDG MECHANISM. R ENG UNFEATHERING ACCUMULATOR DID NOT WORK. (FEATHERED ENG PROC WITH UNFEATHERING ACCUMULATOR WAS TESTED SATISFACTORILY AT ALT OF 5000 FT FIRST). STARTED R ENG USING STARTER. R ENG OPERATED NORMALLY AND WITH BOTH ENGS OPERATING, FLEW TO SAFE ALT, DEPARTED PATTERN. TESTED SYS (LNDG GEAR) ALL NORMAL. CLRED TO LAND, NORMAL SAFE LNDG. EMER CRASH CREWS WERE NOT CALLED FOR LNDG SINCE ALL SYS NORMAL AT LNDG.

Data retrieved from NASA's ASRS site as of July 2007 and automatically converted to unabbreviated mixed upper/lowercase text. This report is for informational purposes with no guarantee of accuracy. See NASA's ASRS site for official report.

Multiple aircraft equipment problems malfunctions during single engine approach. Training in progress. Buzz job on surrounding terrain in proximity of air traffic area occurs on go around. Had been cleared to land but went around account possible involvement with gear indication.