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2005 HQ Lear 45 Flightcheck 8 02 Lyt.Qxp

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2005 HQ Lear 45 Flightcheck 8 02 Lyt.Qxp FLIGHTCHECK Learjet 45: $9.84 mil, M.81, 9 seats, 2100 nm, up to FL510 Honeywell Primus 1000 with EICAS/EFIS, Universal UNS1C FMS, 2 Honeywell TFE731-20s giving 7000 lbs takeoff thrust. (L–R) Lacy and Learjet Dir of Flight Ops Bob Agostino perform low-speed maneuvers before By Clay Lacy their approach to ICT (Mid- ATP/CFII/Helo/Sea. Gulfstream Continent, Wichita KS). II/III/IV, Learjet and Citation series, HS125, Boeing 747 and 25 misc type ratings Learjet 45’s structural design includes a 47.78-ft wingspan and a 57.60-ft external length. Maximum operating altitude is FL510. A pair of Honeywell TFE731-20 engines power the light business jet, with each producing 3500 lbs of thrust. tomers. The original steer-by- craft in 1997 with RVSM certifi- wire system needed improve- cation following in 2000. ment and the brakes were not Bombardier began delivering ideal. Learjet 45s in 1998 and recently Bombardier has successfully delivered its 200th unit. List price addressed these concerns. I was of a Lear 45 is $9.84 million with looking forward to another first available delivery positions hen I flight tested the flight test of the aircraft and 6–8 months out. Bombardier Learjet learning about recent Learjet Learjet Dir of Public Relations W 45 five years ago the 45 product modifications. Dave Franson explains that the aircraft was in the middle of a design objective for the model 45 long, tough certification pro- Aircraft development was to maintain Learjet perfor- cess. In my opinion, the air- mance while eliminating the plane had some negatives. In The Learjet 45 program was problems of the Learjet 35 in terms of range and payload you launched in 1992 with first flight terms of handling characteristics could only board 3 to 4 passen- Oct 7, 1995—32 years to the day and maintainability. Today, the gers with full fuel, which was a after Bill Lear’s first flight of the 45 seats 8–9 passengers and flies concern to many potential cus- Learjet 23. FAA certified the air- further than any other aircraft in Photo courtesy Bombardier 102 PROFESSIONAL PILOT / August 2002 Photos by Grant McLaren (L–R) Learjet Dir of Flight Ops Agostino (L) looks on as Lacy holds an artificial ice shape used to test the aircraft’s aerodynamics during its FAA certification process. Agostino points out the Learjet 45’s external power connector port. Agostino explains the operation of the bizjet’s trailing link landing gear and brake-by-wire systems. its class. Certified to FAR Part 25, right side of the fuselage. Doors Our aircraft was equipped with Amendment 77, the 45 is type located on the forward outboard dual Universal Navigation UNS1C approved in 36 countries. side of each engine nacelle provide FMSs, Honeywell EGPWS, TCAS II earjet 45 originally had a access for oil servicing. and a MagnaStar digital phone sys- 19,500-lb MTOW but the man- The Learjet 45 is powered by 2 tem. Glareshield controls, much Lufacturer increased it to 20,500 Honeywell TFE731-20 turbofan like those on modern airliners, lbs, which was the weight of the air- engines producing 3500 lbs of were well thought out. The stan- craft I flew. After months of research thrust each. The turbofans are dard Honeywell Primus 1000 inte- and man-hours of paperwork, equipped with clamshell-type Dee grated avionics suite includes 4 Bombardier has won FAA certifica- Howard TR5045 thrust reversers. large 8 x 7-in EFIS screens. tion for a 21,500 MTOW for the Tandem, trailing-link main landing Learjet 45 with no added power or gear is fitted with carbon brakes Flying the Learjet 45 structural change requirements. guaranteed for 1100 landings. The 21,500-lb MTOW, APU- I was impressed with the 45’s After engine startup, which was equipped Learjet 45 will carry 7 spacious baggage compartment, straightforward, Agostino and I tax- passengers at 1400 lbs payload which passengers and crew can ied out for takeoff on 19R at ICT with full fuel, while a non-APU- access through a 33-in-wide (Mid-Continent, Wichita KS). Our equipped airplane transports 8 pas- hinged door on the port side. takeoff weight with 3610 lbs of sengers at 1600 lbs payload. This is Pressurized luggage capacity is 51 fuel and 2 passengers was 17,900 a significant and welcome im- cu ft with no C of G restrictions and lbs—or 87.3% of the aircraft’s provement over the original model there’s another 15 cu ft of internal 20,500-lb MTOW. 45. The latest gross weight im- luggage storage. The tailcone door, During taxi-out I was impressed provement should change the per- located aft of the right engine, pro- with the 45’s improved steer-by- ception that the Learjet 45 does not vides access to electrical, environ- wire system, which is smooth and have adequate range and payload. mental, hydraulic and engine fire responsive. For low-speed ground Bombardier is claiming a max IFR extinguishing system components. operations, 60° of steering authority range of 2102 nm. I’ve always liked the Learjet on either side of center is available. clamshell entry door and the model As groundspeed increases, maxi- Walkaround 45 offers a comfortable 30-in door mum wheel deflection is reduced width. Our flight test aircraft had a to zero. I tried a couple of 360s on The Learjet 45 is a relatively standard double club seating taxi-out and found that this air- compact aircraft with a length of arrangement, a spacious aft lav, a plane really turns tightly on the 57 ft 7 in, a 47 ft 9 in wingspan nice forward galley and a 10.4-in ground. and a height of 14 ft 2 in. The high flat panel forward-bulkhead- With V1, Vr and V2 of 105 kts, aspect ratio, fully cantilevered, mounted LCD screen for displaying 112 kts and 121 kts, respectively, swept-back wings with winglets are Air-show video and DVD inputs. we had a balanced field length of of riveted construction with the Cabin height, at 52 in from the 3714 ft at our weight. Agostino exception of the upper portion of flat floor, is adequate, although not suggested a standard climbout at the winglets, which utilize a hon- stand-up for most people. But I 270 kts to Mach 0.70. We climbed eycomb core bonded to the outer always remember what Bill Lear to FL330 with a couple of level- skin. said when people asked him why offs. Avionics racks, an oxygen service Learjets did not have stand-up cab- At FL330 I did a couple of 60° and a pressure gauge are accessed ins: “Remember, you can’t stand up bank turns. Agostino and I then through a forward nose door. in a Cadillac either.” tested the Learjet 45 roll disconnect Learjet Dir of Flight Ops Bob Access to the left seat is easy and system. In case of jamming, the Agostino pointed out the single- I was impressed with the Learjet ailerons may be disconnected from point refueling access door located 45’s flightdeck. It is larger than the the pilot control wheel. After dis- on the fuselage below the right Learjet 35 with better visibility. connection, bank angle is con- engine pylon. You can fuel the 45 Seats and armrests are comfortable, trolled from the pilot control wheel in approximately 7 min at up to 55- controls are within easy reach and I by the spoilerons. psi pressure. There’s also a gravity like the electrically adjustable rud- With Agostino holding his control fuel filler access door on the upper der pedals. wheel hard right, representing PROFESSIONAL PILOT / August 2002 103 no problem. In emergency braking mode you still have 92% of normal braking—even with an inoperative antiskid system. Our last landing was with maxi- Dawson city Anchorage mum braking and thrust reverse to a Whitehorse Chesterfield inlet Iqaluit turnoff on a taxiway about 1500 ft Juneau down the runway. Getting out of the airplane I checked the brakes Vancouver Quebec and detected no noticeable heat. Seattle Montreal The 45 truly has brake overkill. Portland Learjet 45 Diagnostic Product Boston Specialist Peter Levy hooked up a Wichita New York San Francisco laptop computer to the 45’s diag- Los Angeles Atlanta nostic system after the flight to show us how easy it is to download Havana information in real-time from vari- San Juan ous databases. This simple diagnos- tic procedure gives the operator a Cartagena Ranges from Managua Caracas great overview of the aircraft’s sys- • Los Angeles Panama city Georgetown tems on a spreadsheet. Levy • Wichita Medellin explained that these 2nd-generation • Atlanta Quito diagnostic capabilities allow Learjet 45 operators to reduce downtime and trim maintenance costs. Bombardier’s depiction of the Learjet 45’s operating radius from various US cities. System simplicity about 2/3 of the 18° max aileron wonderful. Our first approach to deflection, I turned my control stall was in clean configuration with The Learjet 45 features a cabin wheel hard left. It took me less than stick shaker at 103 kts and full aero- with an oval-shaped cross-section, half spoilers to fly level and I was dynamic stall at 97 kts. Aero- measuring 19 ft 9 in from the flight- able to roll the aircraft into a 45° dynamic buffet was gentle with no deck divider to the aft pressure bank in the opposite direction of pitch down or wing drop. With bulkhead. A simple fuel system ailerons using the spoileron roll dis- flaps 40 and gear down and a consists of 2600 lbs in wing tanks connect system.
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