Performance Specification

Make	MERLIN	MERLIN	MERLIN	MERLIN
Model	300	IV	IV-A	IV-C
Serial Number	ORIGINAL	ORIGINAL	ORIGINAL	ORIGINAL
ENGINES
Number	2	2	2	2
Make	GARRETT	GARRETT	GARRETT	GARRETT
Model	TPE-331-10U-503G	TPE-331-10U-511G	TPE-331-10UA-511	TPE-331-11U-601G
Thrust LB Per Engine	0.00	0.00	0.00	0.00
Shaft HP Per Engine	900.00	840.00	840.00	1,000.00
Common TBO (hours)	5,400	5,400	5,400	3,600
FUSELAGE DIMENSIONS
Length	42.20	59.40	59.40	59.40
Height	16.80	16.70	16.70	16.70
Wing Span	47.90	46.30	46.30	57.00
TYPICAL CONFIGURATION
Crew	2	2	2	2
Passengers	7	14	14	14
Pressurization (psi)	7.00	7.00	7.00	7.00
WEIGHTS (LBS)
Max Ramp	12,600	12,560	12,560	14,600
Max Takeoff	12,500	12,500	12,500	14,500
Zero Fuel	13,130	8,320	8,320	13,100
Basic Operating	8,550	8,400	8,400	9,670
Max Landing	12,500	12,500	12,500	14,000
FUEL CAPACITY
Standard lbs/gal	4,342  /  648	3,712  /  544	3,645  /  544	4,342  /  648
Optional lbs/gal	0  /  0	0  /  0	0  /  0	0  /  0
TAKEOFF PERFORMANCE
SL ISA BFL (ft)	2,920	2,050	2,050	2,850
5000+20C BFL (ft)	4,100	5,028	5,028	4,900
LANDING PERFORMANCE
FAA Field Length	3,530	1,970	1,970	2,532
RANGE (NAUTICAL MILES)
Max Range (NBAA IFR)	2,025	1,815	1,580	2,040
CLIMB (SL ISA MTOW)
Normal (fpm)	2,650	2,400	2,400	2,440
Engine Out (fpm)	680	650	650	627
SPEEDS (KNOTS)
Vs (Clean)	106	0	0	0
Vso (Landing)	92	86	86	87
Normal Cruise TAS	265	260	260	261
Vmo (Max Operating) IAS	265	248	248	248