12.04.2015 Views

Operator Survey: Cessna Citation III

Operator Survey: Cessna Citation III

Operator Survey: Cessna Citation III

SHOW MORE
SHOW LESS

Create successful ePaper yourself

Turn your PDF publications into a flip-book with our unique Google optimized e-Paper software.

PILOT REPORT<br />

O<br />

perator <strong>Survey</strong>:<br />

<strong>Cessna</strong> <strong>Citation</strong> <strong>III</strong><br />

Although its break-in problems may appear to have<br />

been inordinate, the <strong>Cessna</strong> <strong>Citation</strong> <strong>III</strong> has earned<br />

a following as loyal as those of its two smaller<br />

predecessors.<br />

By ROBERT L. PARRISH<br />

November 1987 Document # 2515, 5 pages<br />

As a rule of thumb, business aircraft designers optimistically<br />

estimate that it will take from three to five years for a<br />

new airplane model to progress from drawing board to<br />

certification. Often the process is protracted when a manufacturer<br />

ventures onto technological grounds on which it<br />

has not previously trod. And it’s more common than not<br />

that refinements of the product will continue long after<br />

production units are placed into consumer use.<br />

That more or less presents a thumbnail history of <strong>Cessna</strong>’s<br />

“electric airplane,” the Model 650 <strong>Citation</strong> <strong>III</strong>.<br />

From a comfortable niche as a leader in the light business<br />

jet marketplace, <strong>Cessna</strong> in the fall of 1976 disclosed<br />

plans to step into the long-range, midsize arena<br />

with a 20,000-pound gross weight, eight- to 11-place<br />

turbofan airplane.<br />

It was nearly three years later, on May 30, 1979,<br />

that the first Model 650 prototype marked its maiden<br />

flight. A reported total of some $300 million and another<br />

three and a half years were invested in the program<br />

before the first production unit was rolled out in December<br />

1982, and it was not until the spring of 1983 that<br />

the first <strong>Citation</strong> <strong>III</strong> was delivered to a customer.<br />

Once deliveries began, however, <strong>Cessna</strong>’s Wichita<br />

assembly facilities turned out copies of the new model<br />

at a rate of better than three a month. By July 1985<br />

there were 80 of them in the field, and that figure had<br />

increased to 140 by July of this year. Those units had<br />

posted a cumulative total of more than 115,000 flight<br />

hours, averaging 1.24 hours per flight, and the hightime<br />

<strong>Citation</strong> <strong>III</strong> had accumulated over 3,050 flight<br />

hours as of July this year.<br />

PROMISES FULFILLED?<br />

A performance analysis, comparing the <strong>Citation</strong> <strong>III</strong> with<br />

other business jets in essentially the same gross weight<br />

class—the Dassault Falcon 20F, BAe 125-700 and<br />

Gates Learjet 55—was done by B/CA early on (B/CA,<br />

July 1983, page 40). That study indicated that in 28<br />

parameters evaluated, the Garrett TFE731-3B-100S turbofan-powered<br />

<strong>Cessna</strong> twin was judged as being<br />

above the average for the group as a whole in 20.<br />

To determine how well the Model 650 has measured<br />

up to <strong>Cessna</strong>’s design goals and whether its overall performance<br />

has continued to reflect what B/CA found in<br />

1983, a telephone survey was made recently of flight<br />

departments that collectively operate over 18 percent of<br />

the total <strong>Citation</strong> <strong>III</strong> fleet. The survey group encompassed<br />

flight department managers, pilots and maintenance<br />

specialists whose experience with the <strong>Citation</strong> <strong>III</strong><br />

ranged from more than four years to as little as six<br />

months.<br />

From the standpoint of utilization, these operators fly<br />

their <strong>Citation</strong> <strong>III</strong>s from 160 hours a year to more than<br />

1,200 hours annually. The group as a whole averaged<br />

about 650 <strong>Citation</strong> <strong>III</strong> flight hours yearly. That average,<br />

in the opinion of one operator, reflects a subtle change<br />

in corporate air transport activity. It is not that operations<br />

have shown a sharp increase, he said, but rather<br />

COPYRIGHT 1995 THE MCGRAW-HILL COMPANIES, INC. ALL RIGHTS RESERVED


P ilot<br />

Report<br />

that flight departments have fewer aircraft and now<br />

appear to be operating them more efficiently.<br />

Most members of the survey group claimed that for<br />

their given mission requirements they believe the <strong>Citation</strong><br />

<strong>III</strong> is the most suitable business jet on the market for<br />

the price—about $6.2 million B/CA equipped. And if<br />

they were called upon today to select a replacement or<br />

additional aircraft for the same type of air transportation<br />

needs, it would be a current model of the same aircraft.<br />

But for some, that would not have been the case<br />

as recently as six months ago.<br />

The reason given was that the <strong>Citation</strong> <strong>III</strong> is an aircraft<br />

on which full development has been (or is being) completed<br />

on the basis of experience gained through its use<br />

in the field. While there have been only two ADs<br />

against it—pertaining to potential electrical fires, which<br />

are not unique to the <strong>Cessna</strong> 650—there have been “a<br />

pot full of service bulletins,” several operators complained.<br />

<strong>Cessna</strong> marketing personnel acknowledged<br />

that well over 100 SBs and service letters have been<br />

disseminated during the <strong>Citation</strong> <strong>III</strong>’s brief history, but<br />

those officials stressed that few of them were mandated<br />

corrective actions and that the vast majority can be<br />

attributed to what the manufacturer regards as an ongoing<br />

product-improvement effort.<br />

Basic design objectives for the <strong>Citation</strong> <strong>III</strong> reportedly<br />

were to provide an executive aircraft with at least 50<br />

percent more internal living space, 20 percent more<br />

speed, some 40 percent greater range and nearly 40<br />

percent more useful load capability than those afforded<br />

by the earlier <strong>Citation</strong> II but with about the same<br />

level of fuel economy and better ability to conform to<br />

the most exacting FAR Part 36 noise standards. Mechanisms<br />

employed to accomplish the objectives included<br />

adaptation of a supercritical wing, greater use of<br />

lightweight composite materials and extensive electrical/computer<br />

applications to subsystems monitoring<br />

and control functions.<br />

The operators surveyed by B/CA agreed that targeted<br />

objectives have generally been met. But advanced<br />

technologies employed in the process were blamed for<br />

initially extracting exorbitant tolls in dispatch reliability.<br />

One flight department manager claimed, in fact, that<br />

during the first year his company flew the <strong>Citation</strong> <strong>III</strong>,<br />

the airplane spent 244 days in the shop undergoing<br />

systems modifications, service and repairs. Others complained<br />

not about any single major problem area but of<br />

continuing minor malfunctions and glitches that disrupted<br />

flight schedules and impeded effective utilization of<br />

the aircraft.<br />

A conglomerate profile of operations surveyed<br />

showed that the group as a whole varies somewhat<br />

from fleet-wide characteristics compiled by <strong>Cessna</strong>.<br />

The survey sample, for instance, reported higher average<br />

utilization of their equipment than that computed<br />

by the OEM.<br />

Average load factors—placed at better than 4.5—<br />

also were higher, as were en route cruise speeds,<br />

which were flight planned at an average of 450 knots.<br />

However, fuel flows—reported at overall average rates<br />

of between 1,400 and 1,450 pounds per hour—were<br />

lower than those contained in <strong>Cessna</strong> manuals.<br />

SYSTEMS SNAFUS<br />

By and large, the most aggravating and numerous of<br />

problems revealed by those surveyed were related to<br />

the <strong>Citation</strong> <strong>III</strong> flap, environmental conditioning and horizontal<br />

tail anti-icing systems, although the electrical<br />

and anti-ice/deice systems in general drew critical comments.<br />

At the same time, <strong>Cessna</strong>’s product-support<br />

efforts, in many cases extending beyond the 1,000-<br />

hour aircraft warranty period, merited almost unanimous<br />

praise.<br />

And a strong correlation can be made between the<br />

age of individual aircraft (as reflected by serial number)<br />

and the frequency and perceived severity of problems<br />

experienced. <strong>Cessna</strong> explained this by pointing out that<br />

as defects and potential shortcomings have been discerned<br />

at company-owned or company-authorized service<br />

centers, every effort has been made to incorporate<br />

fixes into the production process.<br />

All of the aircraft included in the users’ survey were<br />

configured in seven-passenger plus lavatory seating<br />

arrangement; about half were equipped with electronic<br />

flight instrument systems (EFIS), the majority Sperrymade<br />

since that is the primary optional installation, but<br />

with Bendix and Collins also represented; and some 60<br />

percent had a factory-installed APU. All aircraft prior to<br />

Serial Number 100 were equipped with Sundstrand<br />

air-cycle machines; one to provide cockpit environmental<br />

conditioning and a second identical machine to cool<br />

and heat the passenger cabin. From Serial Number<br />

100 on, those units have been replaced with larger,<br />

higher-capacity Hamilton Standard air-cycle machines.<br />

Several survey respondents indicated that the primary<br />

incentives to select the <strong>Citation</strong> <strong>III</strong> over competitive aircraft<br />

were acquisition cost, along with cabin space,<br />

promised operating economy, speed and range.<br />

Among nine executive jets listed in B/CA’s 1987 Planning<br />

and Purchasing Handbook that could be considered<br />

as market competitors, however, the <strong>Cessna</strong><br />

Model 650 was estimated as the third most expensive,<br />

when comparably equipped.<br />

In terms of certified ceiling, true airspeed and fuel<br />

flow, the <strong>Citation</strong> <strong>III</strong> equaled or exceeded the capabilities<br />

of most of that competition, on paper at least. From<br />

the real-world aspect, however, several of the operators<br />

expressed disappointment with the <strong>Citation</strong> <strong>III</strong>’s range<br />

COPYRIGHT 1995 THE MCGRAW-HILL COMPANIES, INC. ALL RIGHTS RESERVED


P ilot<br />

Report<br />

and second-segment climb abilities.<br />

“The aircraft manual claims the <strong>Citation</strong> <strong>III</strong> has a<br />

range of 2,540 nm with NBAA IFR reserve fuel,” noted<br />

one operator, “but I’d be uncomfortable in attempting<br />

any nonstop flight of more than 2,100 nm if I had much<br />

of a payload aboard.” He and several others suggested<br />

that from a practical standpoint an 1,800 nm maximum<br />

IFR range would be more reasonable for flight<br />

planning purposes. (B/ CA computed an NBAA IFR<br />

range of 2,094 nm with four passengers in our April<br />

1987 Handbook).<br />

Some of the more experienced <strong>Citation</strong> <strong>III</strong> operators<br />

also were critical of what they regard as the hot-day,<br />

high-altitude limitations of the aircraft. Said one: “A 95<br />

degrees F day in Denver is going to cost as much as<br />

4,000 pounds in useful load, and our company officers<br />

can get pretty upset when an airplane they bought for<br />

its speed and range cannot make either the East Coast<br />

or West Coast without having to land to refuel en<br />

route.”<br />

THE ATTRIBUTES<br />

Generally, though, crew satisfaction with the aircraft’s<br />

performance and handling characteristics far outweighed<br />

any dislikes expressed. Among features mentioned<br />

as best-liked were the <strong>Citation</strong> <strong>III</strong>’s:<br />

Speed and altitude capabilities— (a cruise of 0.81<br />

to 0.83 Mach and MMO of 0.851, with a 51,000-foot<br />

service ceiling and optimum flight altitudes of FL 370 to<br />

FL 450 achieved without step-climbing.<br />

Trouble-free, dependable powerplants—Surprisingly,<br />

not one operator interviewed by B/CA reported any<br />

significant engine problems.<br />

Operational flexibility—Thirty-minute missions were<br />

reportedly performed almost as economically as those<br />

of 1,000 to 1,500 nm, where the superior speed and<br />

stability of the aircraft were said to cause it to really<br />

shine.<br />

Operational simplicity—<strong>Operator</strong>s noted the ease<br />

with which the <strong>Citation</strong> <strong>III</strong> can be hand-flown with the<br />

autopilot and yaw damper disengaged, and one pilot<br />

remarked, “Start-up and shutdown procedures are so<br />

uncomplicated that I feel like I must be forgetting something.”<br />

Specific fuel consumption—Over 1,000-nm stages<br />

the <strong>Citation</strong> <strong>III</strong> will use about the same amount of fuel as<br />

the smaller <strong>Citation</strong> II because it will complete the trip in<br />

less time, several operators said.<br />

Speed margins and landing capabilities—<strong>Operator</strong>s<br />

like the broad latitude between the minimum speed<br />

and stall speed, and the invariably good landings that<br />

result from the trailing-link gear.<br />

Interior size and noise levels— Stand-up cabin<br />

room, spaciousness of the cockpit, the airplane’s quietness<br />

inside and out, and the overall level of interior<br />

decor and comfort are appreciated by <strong>Citation</strong> <strong>III</strong> operators.<br />

The APU, which in later units is certified for operation<br />

in flight.<br />

Separate environmental control units for the cockpit<br />

and cabin.<br />

Ample baggage space and weight capacity.<br />

Worth noting is the fact that the majority of operators<br />

contacted fell into one of two categories. Either their<br />

companies were traditional users of <strong>Cessna</strong> products<br />

and they had stepped up from smaller <strong>Citation</strong> models,<br />

or they had changed over from Learjet 20 or 30 series<br />

aircraft. In either case, both flight crews and passengers<br />

were pleased with the added space and comfort<br />

afforded by the <strong>Citation</strong> <strong>III</strong>. A flight department manager<br />

whose firm replaced two Gulfstream Is with <strong>Citation</strong><br />

<strong>III</strong>s, another who replaced a Sabreliner 60 and one<br />

who traded a Falcon 20 for the <strong>Citation</strong> <strong>III</strong> all reported<br />

that their passengers were less impressed by the cabin<br />

size than by the new aircraft’s low noise level and<br />

greater speed.<br />

THE DOWNSIDE<br />

Features of the <strong>Citation</strong> <strong>III</strong> cited as least liked included:<br />

Its inability to deliver the claimed transcontinental<br />

nonstop range— When pressed, most operators admitted<br />

the range is adequate for their typical stage lengths,<br />

but an added 500 nm of capability would greatly<br />

enhance the <strong>Citation</strong> <strong>III</strong>’s value, one contended.<br />

System and component problems—Difficulties with<br />

the heating and cooling system, hydraulic, pneumatic<br />

and fuel valve, connectors, anti-ice/ deice components<br />

and electrical wiring bundles, which allegedly are<br />

installed in a manner that impedes troubleshooting and<br />

service functions.<br />

Quality control and spare parts inventories at <strong>Cessna</strong>’s<br />

<strong>Citation</strong> service centers—Several operators<br />

charged that the centers lack uniformity in both procedures<br />

and quality. “I’ve dealt with almost every <strong>Citation</strong><br />

center in North America,” said one, “and while I’ve<br />

found the personnel at most of them to be obliging,<br />

their work has run the gamut from excellent to unsatisfactory.<br />

The only consistency I’ve seen is a common<br />

lack of needed spares in inventory.”<br />

Failure or malfunction of MEL dispatch items like<br />

flaps, certain instruments, stabilizer anti-ice blankets<br />

and valves—Noted the operator of an early production<br />

unit: “<strong>Cessna</strong> cannot have made any money on our aircraft<br />

because of the time and parts provided under warranty.<br />

At the same time, there has been a cost to us in<br />

having to dispatch another airplane to transport stranded<br />

passengers.”<br />

Unsatisfactory maintenance access to many critical<br />

COPYRIGHT 1995 THE MCGRAW-HILL COMPANIES, INC. ALL RIGHTS RESERVED


P ilot<br />

Report<br />

and short-lived components—A flight department manager<br />

reported that anti-ice pilot/slave valves on his aircraft<br />

were failing at about two-week intervals and to<br />

replace them required removal of the engine thrust<br />

reversers, a two-day job in itself.<br />

Difficulty in troubleshooting electrical system-related<br />

problems—Several of those operators interviewed<br />

attributed miscellaneous component difficulties to the<br />

electrical system, and one recalled taking his aircraft to<br />

the Wichita <strong>Citation</strong> service center three times before<br />

the cause of an instrument malfunction finally was isolated<br />

as a chafed wire bundle. “When they put the <strong>Citation</strong><br />

<strong>III</strong> together, it seems like they wanted it to stay just<br />

the way they built it,” said the maintenance chief of<br />

another operation.<br />

Remote location of the circuitbreaker box where<br />

the flight crew cannot get at it in flight—A pilot noted<br />

that the aircraft operators manual requires that the airplane<br />

be landed immediately if the circuit-breaker warning<br />

light illuminates. On one occasion, he said, a<br />

passenger cabin stereo set anomaly led to an aborted<br />

takeoff run, and on another a malfunction in the lavatory<br />

flushing system resulted in an unscheduled landing.<br />

Bleed-air performance and noise—<strong>Operator</strong>s cited<br />

the inadequate windshield defogging ability of the<br />

bleed-air system and noise created by the windshield<br />

fan, which can interfere with radio communication during<br />

critical phases of flight.<br />

A cruise climb rate that contrasts with the aircraft’s<br />

otherwise outstanding high-performance characteristics—<br />

In a head-to-head comparison between a Learjet<br />

35 and the <strong>Citation</strong> <strong>III</strong> on trips of an hour or less, the<br />

modest climb rate of the <strong>Citation</strong> <strong>III</strong> offsets its superior<br />

en route speed, claimed a manager whose department<br />

operates both models.<br />

Repeated APU failures—Several operators have<br />

experienced numerous APU breakdowns and feel that<br />

there is a need for correction of a suspected link<br />

between the APU and the air-cycle machines that precipitates<br />

failure of the latter.<br />

Despite the length of this squawk list, a surprising<br />

number of operators insisted that they had experienced<br />

relatively fewer serious problems with the <strong>Citation</strong> <strong>III</strong><br />

than they had anticipated, or than they had experienced<br />

with other aircraft models. The most potentially<br />

hazardous problem disclosed by the survey was one in<br />

which fuel unporting from the wing tanks to the forward<br />

fuselage tank could cause a nose-heavy condition on<br />

landing approach, under certain conditions.<br />

And virtually all of those contributing to the survey<br />

agreed on three points:<br />

(1) Overall, the <strong>Citation</strong> <strong>III</strong> meets or exceeds primary<br />

performance specifications contained in the AOM;<br />

(2) <strong>Cessna</strong> has been conscientious in its product-support<br />

efforts;<br />

(3) With time, the <strong>Citation</strong> <strong>III</strong> has become increasingly<br />

more reliable, even though some problems still may<br />

exist.<br />

Among those who have tracked the dispatch reliability<br />

rates most carefully, it was reported that mechanical<br />

situations have resulted more in flight schedule delays<br />

than in cancellations, and trip completion rates were<br />

computed in the 97 to 99.9 percent range.<br />

CESSNA’S SOLUTIONS<br />

What <strong>Cessna</strong> has done in response to specific complaints<br />

was relayed from <strong>Citation</strong> <strong>III</strong> program engineers<br />

by David W. Carter, director of marketing communications.<br />

A major effort and the subject of many of the SBs<br />

that have been issued, he disclosed, has focused on<br />

refinement of subsystems arrangement, maintenance<br />

accessibility and inspection schedules.<br />

One significant advance was a landing gear and<br />

brake modification program that permitted increased<br />

ramp, takeoff and landing weights. Another was<br />

improvement of the APU installation that reportedly has<br />

resulted in fewer problems both with that unit and the<br />

air-cycle machines. Another was re-engineering of the<br />

wing flap control and asymmetric brake systems that<br />

has minimized reports of flap freeze situations, <strong>Cessna</strong><br />

claimed.<br />

Still another was a change in air-cycle machine vendors<br />

and refinements to the earlier air-cycle units that<br />

are reported to have radically reduced unscheduled<br />

removals. In August, <strong>Cessna</strong> acknowledged that discussions<br />

were being held with prospective new suppliers of<br />

subsystem control valves. In addition, the vendor for the<br />

<strong>Citation</strong> <strong>III</strong> anti-ice/deice systems reportedly has made<br />

several significant improvements in its products.<br />

Plans also were in the mill in August to fine-tune the<br />

entire electrical system by redesigning some junction<br />

boxes and eliminating others, Carter revealed, and a<br />

“bagged” noise insulation modification has been made<br />

available for <strong>Citation</strong> <strong>III</strong> operators whose aircraft may<br />

need further silencing treatment.<br />

No changes are currently planned, however, for the<br />

aircraft’s unique hydraulic swage fittings or for conversion<br />

from the non-corrosive hydraulic fluid now used,<br />

according to Carter. Neither is there any project in process<br />

to change the windscreen bleed-air defogging<br />

mechanism.<br />

Carter indicated that <strong>Cessna</strong> engineers expressed surprise<br />

when informed that the bleed-air system and<br />

defogging fan in combination caused noise interference<br />

with radio communication. This complaint was mentioned<br />

by several of the operators interviewed, however,<br />

so it must be assumed that it has some validity.<br />

Most of the post-certification improvements devised<br />

COPYRIGHT 1995 THE MCGRAW-HILL COMPANIES ALL RIGHTS RESERVED


P ilot<br />

Report<br />

for the <strong>Citation</strong> <strong>III</strong>—with the notable exception of the<br />

air-cycle machines— can be retrofitted on early units,<br />

Carter said. In his opinion, that should enable those aircraft<br />

to be upgraded to a state of product maturity<br />

equal to that of current production units.<br />

<strong>Cessna</strong> has been aware of inadequacies in its service<br />

center structure and has been working hard to overcome<br />

them, Carter added. Efforts are underway now to<br />

both beef up parts inventories at the centers and to train<br />

their personnel to more effectively incorporate product<br />

improvements and modifications into <strong>Citation</strong> <strong>III</strong> inspection<br />

programs, he claimed.<br />

Several of B/CA’s survey respondents cautioned,<br />

however, that flight departments considering acquisition<br />

of a used Model 650 would be well-advised to investigate<br />

thoroughly the structural impact that some of the<br />

later modifications might have on earlier airframes and<br />

systems (those aircraft preceding serial number 50 or<br />

75).<br />

<strong>Cessna</strong> indicated that the <strong>Citation</strong> <strong>III</strong> had “reached<br />

full maturity” at or near completion of the 100th production<br />

unit and that it expects complaints to dwindle. But<br />

<strong>Cessna</strong>’s promise was that each will be given the same<br />

high level of product support as the company has<br />

attempted to provide in the past.<br />

Despite its rash of introductory hiccups, the <strong>Cessna</strong><br />

<strong>Citation</strong> <strong>III</strong> obviously has filled a market need. And as<br />

long as speed and ease of handling remain important<br />

to prospective customers, the <strong>Citation</strong> <strong>III</strong> should continue<br />

to enlarge upon its past success. B/CA<br />

COPYRIGHT 1995 THE MCGRAW-HILL COMPANIES ALL RIGHTS RESERVED

Hooray! Your file is uploaded and ready to be published.

Saved successfully!

Ooh no, something went wrong!