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Embraer Phenom 100

EMBRAER EMB-500 Phenom 100 · Pilot's Operating Handbook

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Overview

The document provides an overview of the Embraer EMB-500 Phenom 100, detailing its design, features, performance, and pilot feedback. It discusses the aircraft's advanced avionics, performance specifications, and some operational issues experienced by pilots, particularly with the braking system.

  • The Phenom 100 features the Prodigy avionics suite based on Garmin's G1000.
  • It has a maximum cruise speed of 390 knots and a range of 1,178 nautical miles.
  • The aircraft's maximum operating altitude is 41,000 feet.
  • Early models had issues with grabby brakes, which have since been improved.
  • The average equipped price of the Phenom 100 is $4.1 million.
  • The aircraft can seat 2 + 5/6 passengers.
  • It has a fuel capacity of 419 gallons.
  • The Phenom 100 has been involved in three accidents related to braking issues.

Document

Source

Originally published by aeroresourcesinc.com. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.

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Document details

Type
·
Pilot's Operating Handbook
Year
·
2012
File size
·
5.6 MB
Publisher
·
aeroresourcesinc.com
Language
·
en

Specifications & performance

Extracted from this document.

Specifications

Height (ft)
·
14 ft 3 in
Length (ft)
·
42 ft 11 in
Wingspan (ft)
·
40 ft 4 in
Wing area sq (ft)
·
202 sq ft
Fuel capacity (gal)
·
419 gal
Max ramp weight (lb)
·
110,516 lbs
Max useful load (lb)
·
3,384 lbs
Max landing weight (lb)
·
9,766 lbs
Max takeoff weight (lb)
·
110,472 lbs
Max zero fuel weight (lb)
·
8,444 lbs
Max payload full fuel (lb)
·
578 lbs

Performance

Max range (nm)
·
1,178 nm
Cruise speed (kt)
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390 kt
Cabin altitude (ft)
·
8,000 ft
Landing distance (ft)
·
2,699 ft
Takeoff field length (ft)
·
3,400 ft
Max operating altitude (ft)
·
41,000 ft

V-speeds

V1_KIAS
·
102 KIAS
V2_KIAS
·
107 KIAS
VR_KIAS
·
104 KIAS
VS_KIAS
·
100 KIAS
VIE_KIAS
·
127 KIAS
VIO_KIAS
·
180 KIAS
VSO_KIAS
·
77 KIAS
V_MO_KIAS
·
275 KIAS
V_MO_MACH
·
0.7 M
V_REF_KIAS
·
105 KIAS
VFE_10_DEG_KIAS
·
200 KIAS
VFE_26_DEG_KIAS
·
160 KIAS
VFE_36_DEG_KIAS
·
145 KIAS
VMC_LANDING_ICING_KIAS
·
97 KIAS
VMC_LANDING_NO_ICING_KIAS
·
86 KIAS

Weight & balance

Max ramp weight (lb)
·
110,516 lbs
Max landing weight (lb)
·
9,766 lbs
Max takeoff weight (lb)
·
110,472 lbs
Max zero fuel weight (lb)
·
8,444 lbs
About this document
What is the Embraer Phenom 100?

The Embraer Phenom 100 is a pilot's operating handbook for the EMBRAER EMB-500 Phenom 100, dated 2012.

Where does the Embraer Phenom 100 come from?

This copy of the Embraer Phenom 100 was originally published by aeroresourcesinc.com and is hosted on Sprinkle as a free, searchable reference copy.

What year was the Embraer Phenom 100 published?

The Embraer Phenom 100 — the EMBRAER EMB-500 Phenom 100 pilot's operating handbook on file — is dated 2012.

Documentation completeness
2/7

Most owners only have the POH. Here's the essential set for the EMBRAER EMB-500 Phenom 100.

More EMBRAER EMB-500 Phenom 100manuals & documents

In this document

Introduction

The Phenom 100 was announced in May 2005 as a new small business jet design from Embraer, featuring advanced avionics and a focus on safety and ease of maintenance.

Performance

The Phenom 100 boasts a maximum cruise speed of 390 knots, a range of 1,178 nautical miles, and a maximum operating altitude of 41,000 feet.

Braking System Issues

Early versions of the Phenom 100 experienced complaints about the braking system, which was described as grabby and difficult to modulate. Improvements have been made to enhance braking feel.

Pilot Feedback

Pilots generally appreciate the Phenom 100 for its comfort and performance, with many praising Embraer's support and warranty coverage.

Specifications

The document includes detailed specifications such as dimensions, weights, and capacities of the Phenom 100.

Accidents

The Phenom 100 has been involved in three accidents, all related to braking issues, with no serious injuries reported.

Safety notes

  • Early Phenom 100s had issues with grabby brakes that could lead to runway overruns.
  • Brake fail warnings were often triggered by system sensitivity, leading to potential loss of braking.
  • Pilots experienced false flap fail messages if flaps were down during power-up.
  • The aircraft has no reverse thrust, which can complicate landing situations.

Full document text

When the Phen om 100 was announced in May 2005 it caused a fair amount of excitement. It was a clean-sheet design from a company that previously focused on producing airliners, plus a sole busi- ness jet-the large-cabin Legacy 600. What would be Embraer's idea of a small busi- ness jet? For one, the cockpit features an avi- onics suite dubbed Prodigy, based on Garmin's popular G1000. The phenom's three-screen setup includes a keypad for data entry, and the entire panel has a clean, uncluttered look that reflects design goals aimed at reducing workload. Anybody with G1000 experience will have little dif- ficulty learning the Prodigy's knobology, something Embraer knew would appeal to step-up turbine pilots with backgrounds using Garmin equipment. Both the phenom 100 and its big brother, the phenom 300, are very much computerized airplanes, loaded with all sorts of sensors, processors, and diagnostic features. The idea is to use the latest dig- ital technology to make the airplane safer to fly and easier to maintain. Some in the industry have taken to calling the Phenoms "computers with wings." With an advertised maximum cruise speed of 390 knots, a maximum range of 1,178 nm, and a max operating altitude of 41,000 feet, the phenom 100 prom- ised performance similar to that of the Mustang's-but with a stronger ramp pres- ence, larger cabin dimensions, and an aft flushing lavatory. It also has a bigger price tag, which is now up to $4.1 million. Now that a few years have passed it's time to look over the phenom 100 expe- rience. Has the airplane lived up to its promise? ISSUES. Perhaps the biggest complaints about earlier versions of the Phenom 100 centered on the brakes. Simply put, they were grabby.And powerful, being designed for maximum braking. Pilots didn't like the way the airplane lurched while taxiing, and couldn't smoothly modulate braking. After landing, more problems would crop up. It was either maximum braking, swerving, or no braking if a pilot pumped the brakes in the conventional manner. The trouble here was that the digital, brake-by-wire brake control unit (BCD) would reset each time the pilot let off on the brakes, and it would be a critical microsecond or so before T-18 I AOPA PILOT November 2012 SPEC SHEET Embraer Phenom 100 AVERAGE EQUIPPED PRICE: $4.1 MilLION Powerplants I 2 Pratt & Whitney Canada PW617F-E, 1,695 Ibst ea, 1,820 Ibst @ Automatic Thrust Reserve (10 min. max) Length I 42 ft lln Wingspan I 40 ft 4 in Wing area I 202 sq ft Height 114 ft 3 in Wing loading 1133 sq ft Power loading 1 3.08 Ib/hp Seats I 2 + 5/6 Cabin length 111 ft Cabin width 15ft 1 in Cabin height 14ft 11 in Max ramp weight 110,516 Ib Max takeoff weight 110,472 Ib Max zero fuel weight I 8,444 Ib Max useful load I 3,384 Ib Max payload, full fuel I 578 Ib Max landing weight I 9,766 Ib Fuel capacity I 419 gal (2,806 Ibs) PERFORMANCE Takeoff field length, flaps 1 I 3,400 ft Cruise speed/range w/NBAA fuel rsv I @ Max cruise setting, 33,000 ft 390 kt/l,178 nm Cabin altitude at FL410, 8.3 dpsi I 8,000 ft Max operating altitude I 41,000 ft Landing distance, flaps 3 I 2,699 ft ONE OF THE BIGGEST gripes about early Phenom 100s were their grabby brakes. There was none of the pedal feel that most pilots are accustomed to. Instead of progressive pedal pressure resulting in gradually increased braking, the brake-by- wire system seemed to be designed for optimum braking-period. To many pilots, the braking felt like maximum braking, or none at all. A new brake control unit and a redesigned, less-taut spring system (above right) helps provide a more modulated, conventional pedal feel, like that of a hydraulic braking system using master cylinders to dole out brake pressure. LIMITING AND RECOMMENDED AIRSPEEDS V, (takeoff decision speed), flaps 1 I 102 KIA5 V R(rotation), flaps 1 /104 KIAS V MC'landing (icing conditions) I 97 KIAS V MC'landing (no icing conditions) I 86 KIAS V2 (takeoff safety speed), flaps 1 1 107 KIAS VFE(max flap extended) @10 degrees / 200 KIAS @26 degrees 1160 KIAS @36 degrees 1145 KIAS VlE (max gear extended) 1275 KIAS VlO (max gear operating) Extend 1180 KIAS Retract 1180 KIAS V REF(reference speed, final approach), flaps 2 1105 KIAS V MO(max operating speed, SL to 28,000 ft) 1 275 KIAS MMO(max Mach number, above 28,000 ft) / 0.7 M Vs, (stall, clean) 1100 KIAS Vso (stall, in landing configuration) I 77 KIAS For more information, see the website (www.embraerexecutivejets.com ). All specifications are based on manu- facturer's calculations. All performance figures are based on standard day, stan- dard atmosphere, sea level, gross weight conditions unless otherwise noted. THE PHENOM'S PANEL features Garmin's Prodigy adaptation of the GlOOOsystem (bottom). It is integrated with the Phenom's systems and displays synoptic pages on the central multifunction display (MFD). The center pedestal's clean look (below left) shows the FADEC thrust lever detents, flap switch, takeoff configuration test button, and parking brake-which also provides emergency backup braking. In case the primary electric pitch trim fails, a backup electric pitch trim can be used (below right). Embraer's new final assembly plant in Melbourne, Florida (far right) is now building Phenom 100s and 300s .. braking was again available. So some pilots, sensing an apparent 10ssof braking during the momentary reset time, kept pump- ing the brakes, only to experience another "loss" of braking. Meanwhile, the airplane stormed down the runway CPhenomshave no reverse thrust). Some pilots felt the brakes had failed completely, applied the emergency/parking brake, and blew the tires. Some simply ran off the end of the runway. This problem was fixed by soft- ware upgrades to the transmitters in the brake control units, giving the pedal assem- blya longer pedal throw, and installing less powerful return springs. Essentially, the brake system is now more like that of the

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much friendlier Phenom 300's. Now brake pressures are more linear, and braking is much more conventional in feel. The brake fix is available free of charge as a retrofit item. The current BCD fix is the fifth iter- ation, and everyone appears to be happy with the fix. - ~.. " .•--.--~_ '''f ~ '/I \ . '/ . \ I \, ---'..----:- /----'.,,---\,-.--' , / ••• _ •• ~ -"I!I - ~.........., ',"",;""-- .. . ~'-"""-----'" IIL- • '- ----- -... PHENOM 100 DEVELOPMENTS First half 2009 Second half 2009 First half 2010 Second half 2010 I First half 2011 • Lavatory rigid • TCAS I • Enhanced takeoff • Belted toilet door • Synthetic vision performance (additional • New armrest • New pax seat system reserve thrust • AHEAD (Aircraft • Electronic • Improved to improve field Health Analysis checklist synoptic pages performance and Diagnosis) • Automatic • TCAS II reversion to • TAWS A electronic standby • Radio altimeter Second half 2011 • Side-facing seat • SMS and email functionality • TCAS II 7.1 Then there were the "brake fail" annun- ciations. Usually, these happened because the system was extra-sensitive, and designed to sample voltage and pressure spikes and other anomalies so frequently- as often as 60 times per second-that minor transient fluctuations fooled the system into thinking that the brakes had truly failed. The drill was to pull the flap circuit breaker to reset the system and clear any faults,wait, then push it back in. Usually, the message went away.The new BCU has so far solved the problem. Another software-related issue had to do with the flap system. The system assumes that after shutdown the flaps would be put in the full up position. If the flap handle was moved to a flaps- down position while the airplane was depowered, pilots would get a "flap fail" message when they next turned on the battery masters. The Phenom flap sys- tem computer is always looking for signs of flap asymmetry, and powering up with flaps down would trigger a false alarm. A new flap control unit was developed and installed in the entire fleet by mid-2011, and the problem went away. The aft-cabin cooling fans were too loud, so a redesign that halved the fan speed dialed down the noise. Early phenom 100 bleed air pressure- regulating and shutoff valves (PRSOVs) would sometimes give false messages, saying that the valves were closed when they really were open. This problem was solved by modifying the PRSOVs' electric switch monitoring system. Having only one cabin seating option grated on some customers. That the seats were too wide and didn't articulate or swivel was another issue. Now Embraer offers a side-facing forward seat opposite the cabin entry door (a $53,302 option) and a belted lavatory seat ($48,334). Together that makes for a total of eight seats. To raise payload, a 330-pound increase in maximum zero fuel weight ($15,000) also will be made available. Also, in a big move, phenom 100s will have articulating and swiveling seats starting in mid-2013; essentially, these are the seats used in the Phenom 300. Because structural changes are involved, the new seats will not be ret- rofittable to earlier Phenom 100s. ACCIDENTS. According to NTSB records, phenom 100s have been involved in just three accidents as of mid-2012. All involve braking issues, which led to runway www.aopa.org/pllot AOPA PILOT I T-21 NEW FOR 2013 will be an optional side-facing seat across from the cabin entry door (above left), as seen in a photo taken at the new Melbourne assembly facility. The 1,695 Ibst Pratt & Whitney PW617 engines (above right) can go to 1,820 Ibst under its automatic power reserve (APR) mode in emergencies such as an engine failure after takeoff. overruns. A September 10, 2010, accident at Brenham Municipal Airport in Brenham, Texas, happened after the pilot received a "brake fail" warning after a takeoff from Tucson, Arizona. During the landing at Brenham Municipal the pilot reported "zero braking," applied the emergency brake, blew both tires, and then ran 'offthe side of the runway. No one was injured. During a landing at the Sedona, Arizona, airport on May 25, 2011,a Phenom 100 ran offthe end of Runway 21,which has a down- hill slope; hit a fence; and went down an embankment. Witnesses saw the airplane fishtailing at high speed as it went down the runway. Two on board received serious inju- ries, but three others were uninjured. On February 3, 2012,an "anti-skid brake failure" during a landing roll at the Campo Grande, Brazil, airport caused a Phenom 100's tire to rupture, but the pilot and two passengers were not injured. PILOT FEEDBACK. So much for the bad news-which is not bad at all in the grand scheme of things. Especially when you consider that Embraer has a warranty that covers everything-even brakes, tires, and scheduled and unscheduled maintenance- for five years. Add Pratt & Whitney's Eagle Service Plan (ESP) engine warranty plan, and you're covered for everything that wears out or breaks. T-22 I AOPA PILOT November 2012 Owners love the airplane. Dr. Michael Alper of Boston says that his Phenom 100 is comfortable and quiet and that Embraer's support has been "unbe- lievable." He uses his airplane to fly for business and pleasure, mostly across New England and to Canada and back. "I always wanted a jet," he said. "And this one's been phenomenal, pun intended. Yes, there have been growing pains, but Embraer always covered the expenses." Jay Obernolte keeps his Phenom 100 at the BigBear airport in Southern California. "It's a fantastic airplane," he said. "It doesn't look like an entry-level jet. It looks like a real jet, and I catch myself looking back at it before I close the hangar doors." Obernolte plans for 360 knots when flying near the airplane's maximum operating altitude ofFL41O, but says he can get 390 knots when flying in the low thirties. "It's a great weather airplane, too," Obernolte said. "It's good in ice, and that small wing handles turbulence very well. It's also easy to land. "If there are any shortcomings I'd say it was the airplane's contaminated-runway performance. Without any speed brakes;, spoilers, or reverse thrust, stopping dis- tances are really dramatically lengthened. Payload/range trade-off is another issue. With full fuel I only have 600 pounds of useful load; with the cabin full, I can only fly an hour. But that's a light-jet thing anyway. All light jets have compromised payload." Dr. Tiron Pechet of Bedford, Massachusetts, said, "What's not to like about the airplane? It's a joy to fly and it's nearly impossible to make anything less than perfect landings. It's well set up for workload is down. Now I can devote my attention to situational awareness and planning ahead. "Embraer's approach to maintenance took some getting used to. With the Citation I had a guy who did my radios, another guy for the engines, and so on. With Embraer I have a single point of con- Embraer's background making airliners has driven its business-jet design, manufac- turing, and maintenance philosophies. This approach, and the string of improvements over the years, have built customer loyalty. Soon, the tradition will be extended with the introduction of Embraer's Legacy 500 and Legacy 450 midsize and "mid-light" "What's not to like about the airplane? It's ajoy to :flyand it's nearly impossible to make anything less than perfect landings." single-pilot flying, although you have to develop a different way of thinking about pilot workload. "By tha~ I mean it's better. Before, when I flew a Citation I was all over the panel and doing all sorts of arithmetic for descent planning, for example. With the Phenom's Prodigy panel, moving maps, and the FADEC-controlled engines, my tact. One time I landed and had three CAS [crew alerting system] annunciations. I did a download from the airplane's CMC [central maintenance computer] and sent it to Embraer service representatives in Brazil. Before I could even get a rental car, they were towing the airplane into the hangar for repairs. All the problems were fixed that evening." jets, respectively. First flight of the Legacy 500 should happen before year-end. Before long, Embraer will have a full line of business jets. If they're all as successful as the Phenom 100, and the economy's antic- ipated upswing comes about, the company is in for a good ride. AOPA EMAIL tom.horne@aopa.org