HAWKER 400XP/

BEECHJET 400A
PILOT CLIENT GUIDE
Revision 0.1

FlightSafety International, Inc.

Marine Air Terminal, LaGuardia Airport
Flushing, New York 11371
(718) 565-4100
www.FlightSafety.com
 Courses for the Hawker 400XP/Beechjet 400A are taught at the following
FlightSafety Learning Centers:

FlightSafety International
Hawker Beechcraft Learning Center
9720 E. Central Avenue
Wichita, KS 67206
(316) 612-5300
(800) 488-3747
Fax (316) 612-5399

Farnborough Airport
Farnborough,
Hampshire,
GU14 6XA,
United Kingdom

Publication history:

Revision 0 . . . . . . . . . . . . . . . . . . . Mar 2014

Revision 0.1 . . . . . . . . . . . . . . . . . June 2014

Copyright © 2014 FlightSafety International, Inc.

Unauthorized reproduction or distribution is prohibited.
All rights reserved.
 CONTENTS

Chapter 1 INTRODUCTION

Chapter 2 INITIAL TRAINING

Chapter 3 RECURRENT TRAINING

Chapter 4 TEST STANDARDS

Chapter 5 HANDOUTS
 HAWKER 400XP/BEECHJET 400A CLIENT GUIDE

CHAPTER 1
INTRODUCTION

CONTENTS

WELCOME LETTER . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1-1

PRE-ATTENDANCE CHECKLIST . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1-3

TRAINING FACILITY FLOORPLAN . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1-4

Revision 0 FOR TRAINING PURPOSES ONLY 1-i

 WELCOME LETTER

Thank you for choosing FlightSafety International as your aircraft training provider! We are
committed to providing pilots with the finest training, service, and professionalism. The following
is a list of key personnel in our facility who will be happy to assist you with your training needs:
Customer Support Manager Gretchen Stroh 316-612-5307
Customer Service Representative Nik Woodward 316-612-5395
Program Manager Randy Siebert 316-612-5336
Program Manager Chris Laws 316-612-5318
Program Manager (Farnborough) Kim Knight +44 1252 554500
Director of Standards Lynn Heath 316-612-5304
Director of Training Dan Orlando 316-612-5303
Sales Manager Sabrina Wolf 316-612-5355
Assistant Center Manager Russ Axtell 316-612-5302
Center Manager Debbie Jones 316-612-5301
This Client Guide will serve as a syllabus of instruction for you during your training. Please keep
in mind that this is only a guide. The flow of material in ground school and the scenario depicted in
the simulator sessions are representative of the material to be presented. However, the actual flow
of material may not be in the exact order illustrated.
Please thoroughly review all information to ensure you are prepared for your training event.
Scheduled start times and simulator times are subject to change. For hotel and/or rental car
reservations, please contact Tobi Tenbrink (TTenbrink@HospitalityToo.com). In order to receive
the discounted rate, all reservations for FlightSafety need to be booked through Hospitality Too.
I would like to introduce you to our website: www.myFlightSafety.com. This website provides a
number of tools including pre-course study guides, eLearning courses, and much more! If you
happen to be a first time visitor to myFlightSafety.com, you will need your client identification
number. If you are not a first time visitor to myFlightSafety.com, you may login with your previous
username and password. In case of log in access issues (except for holidays), please contact our
center’s Customer Support Manager or Sales Manager at the number listed above.
During your stay, your instructor will brief you on the specific safety procedures associated with
your simulator training and the location of classroom exits. The training facility floor plan follows
after the next page.
Again, thank you for choosing FlightSafety International as your aircraft training provider!
Best regards,

Dan Orlando
Director of Training

9720 E. Central Avenue • Wichita, KS 67206

Tel: 316.612.5300 • 800.488.3747 • Fax 316.612.5399 • flightsafety.com
Farnborough Airport • Farnborough, Hampshire, GU14 6XA • United Kingdom
 HAWKER 400XP/BEECHJET 400A CLIENT GUIDE

PRE-ATTENDANCE CHECKLIST
Please be sure to bring:
Pilot license
Medical certificate
Valid passport or birth certificate with an original, raised seal and a Government-issued ID
Valid, current FAA letter of approval for foreign pilots seeking initial FAA ATP certification
(must be applied for 90 days prior to attendance)
Valid, current FAA ATP written test result for those seeking an ATP certificate
Pilot logbooks for pilots seeking initial jet type certification or U.S. ATP (for first jet type on an
FAA certificate or EASA applicant meeting the minimum required times)
Company or country specific training and/or checking paperwork if required by EASA member
states or other authorities. (135 training authorization, AOC documents)
Method of payment if required
Review of company specific SOP prior to arrival for class if required
Review of expanded procedures checklist prior to arrival if enrolled in a recurrent course
Bring your AFM, POM and checklist for revisions if attending a recurrent course.

NOTE: If you have any concerns about required documentation, please feel free to contact the learning
center CSR or program manager at the numbers listed on page 1-1.

PRE-ATTENDANCE
CHECKLIST
Revision 0 FOR TRAINING PURPOSES ONLY 1-3
 HAWKER 400XP/BEECHJET 400A CLIENT GUIDE

TRAINING FACILITY W

FLOORPLAN
CONFERENCE S N
ROOM 111
E

TO SIM BAYS
ENGINEERS MAIN FLOOR

CLASS-
GFS RM.108 ROOM
CLASS- 113
MFTD ROOM
110 CLASS-
ROOM
112
CLASS- CLASS-
ROOM ROOM
107 CLASS- CLASS- 114
CLIENT PARKING

ROOM ROOM
105 104
CLASS-
ROOM
CLASS- 116
ROOM
STORAGE

STORAGE
106 LIVE LEARNING
ROOM 103 CLASS-
ROOM
115
CLASS-
ROOM CLASS- GFS
101 ROOM PHONE RM.117
102 ROOM

NET. NET.
ADMIN. ADMIN.
CLASS- CLASS-
ROOM ROOM

ELEC.
RM.
PROD. STOR.
100 119
MKTG
MGR.
CLASS-
ROOM

PROD. CLIENT
120

MECH.
RECEPTION MKTG BUSINESS RM.
AREA-MAIN MGR. OFFICE
ENTRANCE
MAIN ENTRANCE-
UNLOCKED
DURING NORMAL
BUSINESS HRS.- CTR MGR'S CLIENT
RM
VENDING

AT OTHER TIMES ASSISTANT CLIENT ENTRANCE

WITH PASS CARD STUDY WITH PASS
OR USE DOOR CTR DOQ ROOM LITTLE HAWK CARD OR
BUZZER MGR BREAK AREA USE DOOR
CUSTOMER
SUPPORT BUZZER
CLASS-
ASST. ROOM
CTR MGR 121
135
OFFICE
DOT DOS
STORAGE

CSM FILE
ROOM
ADOT
ASST.
TO 2ND FL.
CLASSROOMS

CUST. MAIL RM. OSCC

ADOS
SUP.
TEAMMATE
RESOURCES
HAWKER

PREMIER

PISTON
BEECHJET

CLIENT PARKING
ADOT

ELE.
90/200

EASA
HAWKER
350
PM
4000

PM
987 PM

CONF. FACILITIES TNG.

PM

PM

PM

ROOM LUGGAGE COORD.

PM

ROOM
COORD.
PUBS

CLIENT
ENTRANCE
WITH PASS
CARD OR
USE DOOR
BUZZER

CLIENT PARKING GARAGE

Hawker Beechcraft Learning Center—Main Floor

1-4 FOR TRAINING PURPOSES ONLY Revision 0

 HAWKER 400XP/BEECHJET 400A CLIENT GUIDE

W
S N
E

SECOND FLOOR

TEAMMATE
LOUNGE

CLASS-
ROOM
201

INSTRUCTOR
ROOM
CONF.
RM INSTRUCTOR
ROOM
LOUNGE
TO THE

CLASS-
ROOM
202 ENRICH
MANG.

OFFICE
ADOP

PRMS
DIRECTOR SR. INST/
GFS OF MENTOR
RM. PROGRAMS
ELE.

203 OFFICE
HELP
DOP DESK

STATIONS
LOADING
IPAD
INSTRUCTOR

STORAGE
STORAGE

CLASS- CLASS- CLASS- CLASS-

ROOM ROOM ROOM ROOM CLASS-
213 211 209 207 ROOM
205
ELEC.

NETWORK

CLIENT
LOUNGE

CLASS- CLASS- CLASS- CLASS-

ROOM ROOM ROOM ROOM CLASSROOM CLASSROOM
214 212 210 208 206 204

Hawker Beechcraft Learning Center—Second Floor

Revision 0 FOR TRAINING PURPOSES ONLY 1-5

 HAWKER 400XP/BEECHJET 400A CLIENT GUIDE

W
S N
E

SIM AREA

C. C. C. C. LEAD C. C. C. C.
O. O. O. O. TECH / O. O. O. O.
SQT
OFFICE 22 BR
JEPP
VIEW

BR BR BR BR BR
26 25 24 23 GFS 21 20

KING AIR
350 PL21

HAWKER HAWKER
400XP 800XP HAWKER HAWKER HAWKER KING AIR BEECHJET
4000 900XP 750 C90GTi 400A

BARON/
BONANZA
G1000
ROOM
CONF.

BR BR BR CLIENT'S BR SPARES
17 16 15 QUIET RM ADMIN. BR BR BR BR
5 6 7 8 9
GFS
COMPUTER ROOM 14 SIM SIM
COMPUTER BREAK
ROOM BR ROOM TECH TECH COMPUTER ROOM
13 OFFICE OFFICE

BR BR BR BR
19 10 11 BR BR BR BR
12 SFTD 1 2 3 4

BR
18
BARON/ CONFERENCE
BONANZA ROOM 111
430/530

PREMIER KING AIR ENGINEERS

HAWKER KING AIR KING AIR KING AIR
I/IA C90B 800XP 350 350 PL21 200 GT
TO FIRST
FLOOR
OFFICES

Hawker Beechcraft Learning Center—Sim Area

1-6 FOR TRAINING PURPOSES ONLY Revision 0

 HAWKER 400XP/BEECHJET 400A CLIENT GUIDE

CHAPTER 2
INITIAL TRAINING

CONTENTS

INITIAL GROUND TRAINING CURRICULUM . . . . . . . . . . . . . . . . . . . . . . . 2-1

Summary/Overview . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-1
Technical/CRM Objectives. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-1
Equipment and Materials . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-1
Completion Standards . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-1

INITIAL FLIGHT TRAINING CURRICULUM . . . . . . . . . . . . . . . . . . . . . . . . 2-3

Summary/Overview . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-3
Prerequisites . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-3
Technical/CRM Objectives. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-3
Equipment and Materials . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-3
Completion Standards . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-3
Line Oriented Simulation Training (LOST) . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-3

INITIAL TRAINING SCHEDULE. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-4

Revision 0 FOR TRAINING PURPOSES ONLY 2-i

 HAWKER 400XP/BEECHJET 400A CLIENT GUIDE

INITIAL GROUND TRAINING CURRICULUM

SUMMARY/OVERVIEW
This segment of the course is designed to provide pilots with the necessary training to understand the
operation of aircraft systems, the use of the individual system controls, and the integration of aircraft
systems with operational procedures in order to sufficiently prepare them to enter the flight training
curriculum segment. At the end of the ground training curriculum segment the pilot will be able to
locate, identify, and operate all aircraft systems. The pilot will be able to perform normal, abnormal,
and emergency operating procedures. Additionally, the pilot will be able to demonstrate knowledge
of aircraft performance as well as systems and aircraft limitations.

TECHNICAL/CRM OBJECTIVES
Each day, topics will be covered from the Pilot Training Manual, Aircraft Flight Manual, Pilot’s
Operating Handbook, and avionics materials. Reading assignments will be given by the instructor
for the following day. Pilots will be introduced to, and will exercise in, the elements of Crew
Resource Management as part of the integration process including, but not limited to such elements
as: Situational Awareness and the Error Chain, Crew Concept, and Workload Assessment and Time
Management.

EQUIPMENT AND MATERIALS

Pilot Training Manual, Aircraft Flight Manual, Pilot’s Operating Manual, Client Guide, Avionics
Handouts, Pilot Checklist.

COMPLETION STANDARDS
The pilot must demonstrate adequate knowledge of the aircraft systems, limitations, performance,
and flight planning by successfully completing the written examination with a minimum of 80%
(FAA and Foreign Non-EASA), corrected to 100%, and 70% (EASA graded for each section).

Revision 0 FOR TRAINING PURPOSES ONLY 2-1

 HAWKER 400XP/BEECHJET 400A CLIENT GUIDE

INITIAL FLIGHT TRAINING CURRICULUM

SUMMARY/OVERVIEW
Simulator Training modules will provide instruction to develop the skills to maneuver the aircraft
with and without the automatic flight control system. The pilot will become familiar and proficient in
the use of normal, abnormal, and emergency checklist procedures and standard operating procedures.

PREREQUISITES
Review the aircraft normal procedure checklists, memory items, and limitations prior to the
simulator training.

TECHNICAL/CRM OBJECTIVES
Pilots will exercise in the elements of Crew Resource Management as part of the flight training
process including, but not limited to such elements as: Situational Awareness and the Error Chain,
Crew Concept, and Workload Assessment and Time Management.

EQUIPMENT AND MATERIALS

Pilot Training Manual, Aircraft Flight Manual, Pilot’s Operating Manual, Client Guide, Avionics
Handouts, Pilot Checklist.

COMPLETION STANDARDS
The pilot must demonstrate normal, abnormal, and emergency procedures and checklists in a timely
and sequentially correct manner, and perform all the maneuvers and procedures in accordance with
the applicable Practical Test Standards.

LINE ORIENTED SIMULATION TRAINING (LOST)

If applicable: “This training will facilitate transition from the fixed package of maneuvers in the
Flight Simulator Module to crew-oriented flying. Pilots accomplishing all of their training/checking
in a simulator (100%) will complete Line Oriented Simulation Training.”

Revision 0 FOR TRAINING PURPOSES ONLY 2-3

 HAWKER 400XP/BEECHJET 400A CLIENT GUIDE

INITIAL TRAINING SCHEDULE

DAY GROUND SCHOOL SIMULATOR
AIRCRAFT GENERAL
ELECTRICAL
1—THURSDAY LIGHTING (NONE)
MASTER WARNING
FUEL (8 HOURS)
FUEL
POWERPLANT
THRUST REVERSERS
2—FRIDAY FIRE PROTECTION
(NONE)
PNEUMATICS
AVIONICS (8 HOURS)
ICE & RAIN PROTECTION
AIR CONDITIONING
3—SATURDAY PRESSURIZATION (NONE)
HYDRAULICS
AVIONICS (8 HOURS)
4—SUNDAY (NONE) (NONE)
LANDING GEAR AND BRAKES
PERFORMANCE
5—MONDAY FLIGHT PLANNING (NONE)
APPROVED AFM
FLIGHT CONTROLS (8 HOURS)
AVIONICS
OXYGEN
WINDSHEAR
6—TUESDAY CRM
(NONE)
WEIGHT AND BALANCE
FLIGHT CONTROLS (8 HOURS)
AVIONICS
SYSTEMS REVIEW
7—WEDNESDAY EXAMINATION
(NONE)
CRITIQUE (8 HOURS)
CPT-GROUND SCHOOL TRAINED COCKPIT FAMILIARIZATION
AS CREW. CONDUCTED IN PREFLIGHT-EXPANDED
8—THURSDAY SIMULATOR. PROCEDURES/CHECKS
(4 HOURS SINGLE, 6 HOURS AS ENGINE START PROCEDURES
CREW) TAXI PROCEDURES

9—FRIDAY SESSION 1
PREFLIGHT
TRAINING HOURS AS CREW ENGINE START
1 HOUR BRIEF (NONE) TAXI
2 HOURS PILOT FLYING NORMAL TAKEOFF
2 HOURS PILOT NOT FLYING BASIC AIRCRAFT HANDLING
1 HOUR DEBRIEF NORMAL APPROACH AND LANDING
SESSION 2
PREFLIGHT AND START
10—SATURDAY MALFUNCTIONS
TRAINING HOURS AS CREW AIRWORK (STEEP TURNS, STALLS,
1 HOUR BRIEF (NONE) UNUSUAL ATTITUDE RECOVERY)
2 HOURS PILOT FLYING CABIN PRESSURIZATION
2 HOURS PILOT NOT FLYING EMERGENCY
1 HOUR DEBRIEF EMERGENCY DESCENT
NON-PRECISION APPROACH AND
LANDING

2-4 FOR TRAINING PURPOSES ONLY Revision 0

 HAWKER 400XP/BEECHJET 400A CLIENT GUIDE

INITIAL TRAINING SCHEDULE (Cont.)

DAY GROUND SCHOOL SIMULATOR
DAY 11—SUNDAY (NONE) (NONE)
SESSION 3
REJECTED TAKEOFF
AIRWORK
12—MONDAY EMERGENCY DESCENT
ENGINE MALFUNCTION
TRAINING HOURS AS CREW SINGLE ENGINE PRECISION
1 HOUR BRIEF (NONE) APPROACH
2 HOURS PILOT FLYING SINGLE ENGINE MISSED
2 HOURS PILOT NOT FLYING APPROACH
1 HOUR DEBRIEF AIRSTART
CIRCLING APPROACH AND
LANDING
ENGINE FAILURE ON TAKEOFF
SESSION 4
HIGH-HOT-HEAVY OPERATIONS
WINDSHEAR/MICROBURST ON
TAKEOFF AND APPROACH
EMERGENCY/ABNORMAL SYSTEMS
13—TUESDAY HYDRAULIC
TRAINING HOURS AS CREW
ELECTRICAL
1 HOUR BRIEF (NONE) AVIONICS
2 HOURS PILOT FLYING
POWERPLANT
2 HOURS PILOT NOT FLYING
RAW DATA ILS
1 HOUR DEBRIEF
SINGLE ENGINE TAKEOFF
SINGLE ENGINE APPROACH (NON-
PRECISION)
VISUAL APPROACH
NO-FLAP APPROACH AND LANDING
14—WEDNESDAY SESSION 5
TRAINING HOURS AS CREW ICING PROCEDURES &
1 HOUR BRIEF (NONE) OPERATIONS
2 HOURS PILOT FLYING COLD WEATHER OPERATIONS
2 HOURS PILOT NOT FLYING LOW VISIBILITY TAKEOFFS,
1 HOUR DEBRIEF APPROACHES, AND LANDINGS

15—THURSDAY
TRAINING HOURS AS CREW SESSION 6
1 HOUR BRIEF (NONE) CHECKRIDE PRACTICE/LOST
2 HOURS PILOT FLYING SCENARIO
2 HOURS PILOT NOT FLYING
1 HOUR DEBRIEF

16—FRIDAY (NONE) SESSION 7

PRACTICAL TEST
17—SATURDAY (NONE) PRACTICAL TEST

HOURS SUMMARY
GROUND SCHOOL SIMULATOR
6 HOURS BRIEFING
6 HOURS DEBRIEFING
52-54 HOURS
12 HOURS PILOT FLYING
12 HOURS PILOT NOT FLYING

Revision 0 FOR TRAINING PURPOSES ONLY 2-5

 HAWKER 400XP/BEECHJET 400A CLIENT GUIDE

CHAPTER 3
RECURRENT TRAINING

CONTENTS

RECURRENT GROUND TRAINING CURRICULUM . . . . . . . . . . . . . . . . . . 3-1

Summary/Overview . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3-1
Technical/CRM Objectives. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3-1
Equipment and Materials . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3-1
Completion Standards . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3-1

RECURRENT FLIGHT TRAINING CURRICULUM. . . . . . . . . . . . . . . . . . . . 3-3

Summary/Overview . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3-3
Prerequisites . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3-3
Technical/CRM Objectives. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3-3
Equipment and Materials . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3-3
Completion Standards . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3-3

RECURRENT TRAINING SCHEDULE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3-4

Revision 0 FOR TRAINING PURPOSES ONLY 3-i

 HAWKER 400XP/BEECHJET 400A CLIENT GUIDE

RECURRENT GROUND TRAINING CURRICULUM

SUMMARY/OVERVIEW
This segment of the course is designed to provide pilots with the necessary training to understand the
operation of aircraft systems, the use of the individual system controls, and the integration of aircraft
systems with operational procedures in order to sufficiently prepare them to enter the flight training
curriculum segment. At the end of the ground training curriculum segment the pilot will be able to
locate, identify, and operate all aircraft systems. The pilot will be able to perform normal, abnormal,
and emergency operating procedures. Additionally, the pilot will be able to demonstrate knowledge
of aircraft performance as well as systems and aircraft limitations.

TECHNICAL/CRM OBJECTIVES
Each day, topics will be covered from the Pilot Training Manual, Aircraft Flight Manual, Pilot’s
Operating Handbook, and avionics materials. Reading assignments will be given by the instructor
for the following day. Pilots will be introduced to, and will exercise in, the elements of Crew
Resource Management as part of the integration process including, but not limited to such elements
as: Situational Awareness and the Error Chain, Crew Concept, and Workload Assessment and Time
Management.

EQUIPMENT AND MATERIALS

Pilot Training Manual, Aircraft Flight Manual, Pilot’s Operating Manual, Client Guide, Avionics
Handouts, Pilot Checklist.

COMPLETION STANDARDS
The pilot must demonstrate adequate knowledge of the aircraft systems, limitations, performance,
and flight planning by successfully completing the written examination with a minimum of 80%.

Revision 0 FOR TRAINING PURPOSES ONLY 3-1

 HAWKER 400XP/BEECHJET 400A CLIENT GUIDE

RECURRENT FLIGHT TRAINING CURRICULUM

SUMMARY/OVERVIEW
Simulator Training modules will provide instruction to develop the skills to maneuver the aircraft
with and without the automatic flight control system. The pilot will become familiar and proficient in
the use of normal, abnormal, and emergency checklist procedures and standard operating procedures.

PREREQUISITES
Review the aircraft normal procedure checklists, memory items, and limitations prior to the
simulator training.

TECHNICAL/CRM OBJECTIVES
Pilots will exercise in the elements of Crew Resource Management as part of the flight training
process including, but not limited to such elements as: Situational Awareness and the Error Chain,
Crew Concept, and Workload Assessment and Time Management.

EQUIPMENT AND MATERIALS

Pilot Training Manual, Aircraft Flight Manual, Pilot’s Operating Manual, Client Guide, Avionics
Handouts, Pilot Checklist.

COMPLETION STANDARDS
The pilot must demonstrate normal, abnormal, and emergency procedures and checklists in a timely
and sequentially correct manner, and perform all the maneuvers and procedures in accordance with
the applicable Practical Test Standards.

Revision 0 FOR TRAINING PURPOSES ONLY 3-3

 HAWKER 400XP/BEECHJET 400A CLIENT GUIDE

RECURRENT TRAINING SCHEDULE

DAY GROUND SCHOOL SIMULATOR
PERFORMANCE
WEIGHT AND BALANCE
AVIONICS TRAINING HOURS AS CREW
NAV/ COMM 1 HOUR BRIEF
1 AIRCRAFT GENERAL 2 HOURS PILOT FLYING
ELECTRICAL 2 HOURS PILOT NOT FLYING
LIGHTING .5 HOUR DEBRIEF
MASTER WARNING
4 HRS
PERFORMANCE
WEIGHT AND BALANCE
AVIONICS
TRAINING HOURS AS CREW
FUEL
1 HOUR BRIEF
POWERPLANT
2 THRUST REVERSERS
2 HOURS PILOT FLYING
2 HOURS PILOT NOT FLYING
FIRE PROTECTION
.5 HOUR DEBRIEF
HYDRAULICS
LANDING GEAR/ BRAKES
4 HRS
PERFORMANCE
WEIGHT AND BALANCE
AVIONICS
TRAINING HOURS AS CREW
PRESSURIZATION
1 HOUR BRIEF
AIR CONDITIONING
3 ICE AND RAIN PROTECTION
2 HOURS PILOT FLYING
2 HOURS PILOT NOT FLYING
PNEUMATICS
.5 HOUR DEBRIEF
FLIGHT CONTROLS
OXYGEN
4 HRS

HOURS SUMMARY
GROUND SCHOOL SIMULATOR
3 HOURS BRIEFING
1.5 HOURS DEBRIEFING
12 HOURS
6 HOURS PILOT FLYING
6 HOURS PILOT NOT FLYING

3-4 FOR TRAINING PURPOSES ONLY Revision 0

 HAWKER 400XP/BEECHJET 400A CLIENT GUIDE

CHAPTER 4
TEST STANDARDS

CONTENTS

PRACTICAL TEST STANDARDS (PTS)

AND FLIGHT CREW LICENSING (FCL)
CERTIFICATION SPECIFICATIONS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4-1
Practical Test Standards (PTS) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4-1
Satisfactory Performance . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4-1
Unsatisfactory Performance . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4-1
Practical Test Standards Access . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4-1

FLIGHT CREW LICENSING (FCL)

CERTIFICATION SPECIFICATIONS—
PART FCL AND JAR FCL . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4-2
Pass Marks . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4-2
Flight Crew Standards Access . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4-2

Revision 0 FOR TRAINING PURPOSES ONLY 4-i

 HAWKER 400XP/BEECHJET 400A CLIENT GUIDE

PRACTICAL TEST STANDARDS (PTS)

AND FLIGHT CREW LICENSING (FCL)
CERTIFICATION SPECIFICATIONS
PRACTICAL TEST STANDARDS (PTS)
Course standards are in accordance with the appropriate Pilot Test Standards for the level of
the certificate.

SATISFACTORY PERFORMANCE
1. Perform the TASK in the specified AREA OF OPERATION within appropriate approved standards
(see below).
2. Demonstrate mastery of the aircraft with the successful outcome of each TASK never seriously
in doubt.
3. Demonstrate satisfactory proficiency and competency within the approved standards and single-
pilot competence if the aircraft is type certificated for single-pilot operations.
4. Demonstrate sound judgment and single pilot resource management (SRM)/crew resource
management (CRM).

UNSATISFACTORY PERFORMANCE
Consistently exceeding tolerances as stated in the TASK objective or failure to take prompt, corrective
action when tolerances are exceeded.

PRACTICAL TEST STANDARDS ACCESS

• Access the FAA Pilot Practical Test Standards page:
http://www.faa.gov/training_testing/testing/test_standards/
then click on or search the appropriate links for:
• Airline Transport Rating (ATP)
• Commercial Pilot
• Instrument Rating

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FLIGHT CREW LICENSING (FCL)

CERTIFICATION SPECIFICATIONS—
PART FCL AND JAR FCL
PASS MARKS
The applicant shall pass all required sections of the skill test or proficiency check and demonstrate
the flight test tolerance abilities outlined in the applicable Part FCL.

FLIGHT CREW STANDARDS ACCESS

• Access the EASA Flight Crew Standards page:

http://www.caa.co.uk/standardsdocuments

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 HAWKER 400XP/BEECHJET 400A CLIENT GUIDE

CHAPTER 5
HANDOUTS

CONTENTS

EMERGENCY MEMORY ITEMS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-1

OPERATING SYSTEMS AND LIMITATIONS. . . . . . . . . . . . . . . . . . . . . . . . . 5-7

ANNUNCIATORS. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-16

FLIGHT PROFILES . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-18

AMS-5000 MODE SELECT PANEL . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-57

TRIM CHECK . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-59

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 HAWKER 400XP/BEECHJET 400A CLIENT GUIDE

EMERGENCY MEMORY ITEMS

ENGINE FAILURE DURING TAKEOFF
(BELOW V1—TAKEOFF ABORTED)
1. Brakes .........................................................................................................APPLY
2. Thrust ............................................................................................................. IDLE
3. Thrust Reverser(s) .................................................................................. DEPLOY
4. Reverser Lights ........................................................................................ VERIFY
5. Reverse Thrust ............................................................................ AS REQUIRED
6. Speed Brakes ..........................................................................................EXTEND

ENGINE FAILURE DURING TAKEOFF

(ABOVE V1—TAKEOFF CONTINUED)
1. Nose Up Pitch Attitude at Rotation (VR) .................................. 13–15° DESIRED
2. Landing Gear (when positive climb established) .......................................... UP
3. Airspeed ...........................................................................................MAINTAIN V2

ENGINE FIRE

OR

1. Thrust (affected engine) ............................................................................... IDLE

If ENG FIRE PUSH switch remains illuminated:
2. Thrust Lever (affected engine) ...............................................................CUTOFF
3. Illuminated Engine Fire Switch .................................................................. PUSH
4. Either Fire Bottle Switch ............................................................................. PUSH

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 HAWKER 400XP/BEECHJET 400A CLIENT GUIDE

ENGINE FIRE DETECTOR FAILURE

OR

1. Engine Fire Procedures ................................................................... COMPLETE

2. Remaining Illuminated Engine Fire Bottle Switch ................................... PUSH

DUAL ENGINE FLAMEOUT

1. N2 ........................................................................................ VERIFY ABOVE 52%
2. Ignitions.............................................................................................................ON
If N2 is not above 52% or neither engine relights:
3. BATTERY .....................................................................................................EMER

ENGINE FAILURE IN LANDING CONFIGURATION

1. Thrust (operating engine) ........................................................... AS REQUIRED
2. Airspeed ......................................................................................................... VREF

INADVERTENT THRUST REVERSER DEPLOYMENT

DURING TAKEOFF (BELOW V1—TAKEOFF ABORTED)

OR

1. Brakes ........................................................................................................APPLY
2. Thrust ............................................................................................................. IDLE
3. Thrust Reversers ......................................................................... BOTH DEPLOY
4. Reverser Lights ........................................................................................ VERIFY
5. Reverse Thrust ............................................................................. AS REQUIRED
6. Speed Brakes .........................................................................................EXTEND

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INADVERTENT THRUST REVERSER DEPLOYMENT

DURING TAKEOFF (ABOVE V1—TAKEOFF CONTINUED)

OR OR

1. Emergency Stow Push-Switch (affected engine) ..................................... PUSH

2. Nose Up Pitch Attitude at Rotation (VR) ................................. 13–15° DESIRED
3. Landing Gear (when positive climb established) ......................................... UP
4. Airspeed ................................................................................................... V2 (MIN)
If reverser will not stow and lock:
5. THRUST LEVER (affected engine) ........................................................CUTOFF

INADVERTENT THRUST REVERSER DEPLOYMENT IN FLIGHT

(UNLOCK/DEPLOY ANNUNCIATOR ILLUMINATED)

OR OR

1. Emergency Stow Push-Switch (affected engine) ..................................... PUSH

2. Altitude ................................................................................ BELOW 30,000 FEET
3. Airspeed ......................................................................................BELOW 35 KIAS

INADVERTENT OVERSPEED
1. Thrust ............................................................................................................. IDLE
2. Speed Brakes ..........................................................................................EXTEND
If airplaneis in a nose-down attitude, initiate a wings-level pull-up without
exceeding structural limits (3.2g)

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LOSS OF AIRSPEED INDICATION

1. Autopilot ......................................................................................... DISCONNECT
2. Airspeed ...................................................... SLOW TO AND MAINTAIN 0.2 AOA
3. Thrust ............................................................................................ AS REQUIRED
4. Speed Brakes .............................................................................. AS REQUIRED
(SLOW TO 0.25 AOA WITH
SPEED BRAKES EXTENDED)

ELECTRICAL FIRE OR SMOKE

1. Oxygen Masks ............................................................................................... DON
2. Smoke Goggles ............................................................................................. DON
3. Mic Selectors ...................................................................................... OXY MASK
4. SPKR Switches ............................................................... ON OR DON HEADSET
5. INTPH Switch ...................................................................................................ON
6. Smoke Removal Procedures ...................................................... IF NECESSARY
If known source:
7. Faulted Circuits ..................................................................................... ISOLATE
If unknown source:
8. Battery .........................................................................................................EMER
9. Master Generator Switches .......................................................................EMER

ENVIRONMENTAL SYSTEM SMOKE OR ODOR

1. Oxygen Masks ............................................................................................... DON
2. Smoke Goggles ............................................................................................. DON
3. Mic Selectors ...................................................................................... OXY MASK
4. SPKR Switches ............................................................... ON OR DON HEADSET
5. INTPH Switch ...................................................................................................ON
6. Cabin Pressure Source .......................................................................... ISOLATE
SOURCE BY SELECTING L ENG OR R ENG

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SMOKE REMOVAL
1. Oxygen Masks ............................................................................................... DON
2. Smoke Goggles ............................................................................................. DON
3. Mic Selectors ...................................................................................... OXY MASK
4. SPKR Switches ............................................................... ON OR DON HEADSET
5. INTPH Switch ....................................................................................................ON

CABIN DECOMPRESSION

1. Oxygen Masks ............................................................................................... DON

2. Mic Selectors ...................................................................................... OXY MASK
3. SPKR Switches ............................................................... ON OR DON HEADSET
4. INTPH Switch ....................................................................................................ON

EMERGENCY DESCENT
1. Thrust ............................................................................................................. IDLE
2. Speed Brakes ..........................................................................................EXTEND
3. Autopilot ......................................................................................................... OFF
4. Initiate Moderate Bank ..........................................................................45° MAX

OVERPRESSURIZATION

1. Cabin Pressure Source .................................................................................. OFF

2. Oxygen Masks ............................................................................................... DON
3. Mic Selectors ..................................................................................... OXY MASK
4. SPKR Switches ............................................................... ON OR DON HEADSET
5. INTPH Switch ....................................................................................................ON

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 HAWKER 400XP/BEECHJET 400A CLIENT GUIDE

LOSS OF BOTH GENERATORS

AND

1. GEN FLD and START/GEN Circuit Breakers (AFT MAIN PANEL) ......... CHECK
2. Generator Reset (L and R) ............................................................RESET/NORM

PITCH TRIM RUNAWAY OR FAILURE

ROLL TRIM RUNAWAY OR FAILURE
RUDDER TRIM RUNAWAY OR FAILURE
1. Trim Interrupt/AP Disengage Switch ..................................... PUSH AND HOLD

POWER BRAKE FAILURE

1. Break safety wire and remove guard clip on emergency brake handle.
2. Emergency Brakes .............................................................. APPLY GRADUALLY

AUTOPILOT TRIM FAIL

AND

1. Trim Indicators............................................... CHECK FOR PROPER POSITION

FOR FLIGHT CONDITION
2. Trim Interrupt/AP Disengage Switch ......................................................... PUSH

AUTOPILOT OVERSPEED RECOVERY

1. Thrust ............................................................................................................. IDLE

FLIGHT DIRECTOR MALFUNCTIONS

1. Trim Interrupt/AP Disengage Switch ........................................................ PUSH

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 HAWKER 400XP/BEECHJET 400A CLIENT GUIDE

OPERATING SYSTEMS
AND LIMITATIONS
NOTE TO THE CLIENT:
We strongly recommend that you ar rive for your
Hawker 400XP/Beechjet 400A course familiar with
the aircraft limitations.

AIRSPEED LIMITATIONS
(INDICATED AIRSPEED OR INDICATED MACH)
Maximum Operating Airspeed (VMO) (S.L. to 8,000 ft) ...........................................................264
VMO (8,000 to 11,000 ft) ....................................................................264 to 320 (linear variation)
VMO (11,000 to 26,000 ft) .........................................................................................................320
Limiting Mach (MMO) (above 26,000 ft)..................................................................................0.78
Flap Extension and Operation (VFE/VFO) (Flaps 10° and 20°) .................................................200
Flap Operation (VFO) (Flaps 30°) ..............................................................................................170
Flaps Extended (VFE) (Flaps 30°) ..............................................................................................165
Landing Gear Normal Operation (VLO) ....................................................................................200
Landing Gear Extended (VLE) ...................................................................................................200
Landing Gear Emergency Operation (VLO)...............................................................................150
Landing Lights (VLL).................................................................................................................200
Speed Brakes (VSB) ....................................................................................................... NO LIMIT
Minimum Controllable Airspeed—Airborne (VMCA) (Flaps 0°) ................................................96
VMCA (Flaps 10° and 20°) ...........................................................................................................89
Minimum Controllable Airspeed—Ground (VMCG) (Flaps 0°, 10°, and 20°) ............................88
Windshield Wipers (VWW) (if installed) ....................................................................................200
Tire Limiting Speed (VTIRE).......................................................... 165 (true speed on the ground)

ENGINE LIMITATIONS
Engine Speeds
Takeoff N1 Fan .................................................................................................................. 104%
Takeoff N2 Fan .................................................................................................................... 96%
Idle N2 Turbine, Engine EFC ON .......................................................................52% minimum
Idle N2 Turbine, Engine EFC OFF, in non-icing conditions ...............................46% minimum

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 HAWKER 400XP/BEECHJET 400A CLIENT GUIDE

Engine Temperatures
Takeoff ITT ...................................................................................................................... 700°C
Starting ITT............................................................... 550°C to 600°C for 4 seconds maximum
600°C to 700°C for 2 seconds maximum
ITT for maximum continuous thrust ................................................................................ 680°C

Powerplant
• Pratt and Whitney JT15D-5
• 2965 lb of thrust at takeoff
• 2900 lb of thrust at maximum continuous thrust
• Fire bottle should read 580 to 600 psi at nominal ambient temperatures

Refer to Takeoff Thrust and Max Continuous Thrust setting charts in Section 5 of the AFM for
maximum allowable N1 for ambient conditions.

Normal oil pressure is 60 to 83 psi at N2 speeds above 60%. Oil pressure below 60 psi is undesirable
and should only be tolerated for the completion of the flight, preferably at a reduced power setting.
Under cold conditions, oil pressure may exceed 83 psi.

OPERATING CONDITIONS ENGINE OPERATING LIMITATIONS

OIL
THRUST TIME LIMIT ITT N2 TURBINE N1 FAN OIL PRESSURE
TEMPERATURE
SETTING (MINUTES) TEMPERATURE °C % RPM % RPM PSI
°C
TAKEOFF 5* 700 96 104 (2) 60–83 (3) 10–121
MAX
------- 680 96 104 (2) 60–83 (3) 10–121
CONTINUOUS
IDLE ------- ------- (4) ------- 40 (MIN) -40–121
STARTING ------- (1) ------- ------- (3) -40 (MIN)
TRANSIENT 135 (MAX)
(EXCEPT ------- 700 96 104 ------- (15 MIN
STARTING) OVER 121)
*NOTE: TAKEOFF RATINGS THAT ARE NORMALLY LIMITED TO FIVE MINUTES DURATION MAY BE USED FOR UP TO TEN
MINUTES FOR ONE-ENGINE-INOPERATIVE OPERATIONS

Engine Oil
Oil Temperature (takeoff and max continuous thrust) ............................................10° to 121°C
Oil Pressure (takeoff and max continuous thrust) ...................................................60 to 83 PSI
Minimum Oil Temperature for Starting ........................................................................... –40°C
Oil Pressure at Idle RPM ................................................................................ 40 PSI minimum

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Oil Limitations
Use synthetic type II oil as per Pratt and Whitney Service Bulletin 7001. Do not operate the engine
below the ADD mark on the dipstick. An accurate oil level can only be obtained 10 to 30 minutes
after engine shutdown.

The maximum permissible oil consumption rate of an engine during any flight is 0.5 quart/hour over
a 10-hour period or 1 quart in 4 hours.

Thrust Reverser Limitations

Full Reverse Cutoff Speed...................................................................................55 KIAS or above
Maximum Time for Continuous Reverse Thrust above reverse idle .............................. 30 seconds
Maximum Deployed Time during taxi operations ........................................................... 5 seconds
• Restricted to ground use only.
• Must not be used to back up the aircraft.
• Engine starts with the thrust reversers deployed are prohibited.
• The restow envelope is 30,000 feet or below and 135 KIAS or below.

ELECTRICAL SYSTEM LIMITATIONS

• Two 28V 400-amp starter/generators
• One 24V 40-amp/hour lead acid battery
• GPU requirements: 28VDC–1,000 to 1,500 amp
• During engine start: EFCs come online at 26% N2
• During engine start: starter disengages between 35% and 45% N2

Inverter Supplied (A.C.) Power

• Pitch trim position indicator
• AC Bus Shed indicator light
• Flap position indicator
• LH oil pressure gauge
• RH oil pressure gauge

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 HAWKER 400XP/BEECHJET 400A CLIENT GUIDE

Standby Power
• Standby Attitude Indicator
• Back lighting for Standby Attitude Indicator
• Back lighting for Standby Altimeter
• Back lighting for Standby Airspeed Indicator
• Back lighting for Magnetic Compass
• #1 ITT
• #1 RTU

External Power Assisted Start—Limited to three (3) cycles as follows

First Cycle: 30 Seconds ON .................................................................................... 5 Minutes OFF
Second Cycle: 30 Seconds ON ............................................................................. 15 Minutes OFF
Third Cycle: 30 Seconds ON ................................................................................ 60 Minutes OFF

Battery Start
Do not attempt battery start if battery voltage is below 22 volts.

Generator Assisted Start

Do not attempt to start the second engine until the generator load is below 150 amps.

Ground Operation
Maximum Generator Load.........................................................280 AMPS EACH GENERATOR

In-flight Operation
Both Generators Operating Up to 41,000 ft ...............................280 AMPS EACH GENERATOR
Both Generators Operating Above 41,000 ft..............................260 AMPS EACH GENERATOR
One Generator Operating Up to 29,000 ft ..................................................................... 400 AMPS
One Generator Operating Up to 29,000 ft (Icing Conditions) ....................................... 440 AMPS
TRANSIENT (Below 20,000 ft, 30 Seconds Maximum) .............................................. 525 AMPS
One Generator Operating From 29,000 ft to 41,000 ft .................................................. 280 AMPS
One Generator Operating Above 41,000 ft .................................................................... 260 AMPS

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 HAWKER 400XP/BEECHJET 400A CLIENT GUIDE

FUEL LIMITATIONS
Minimum Fuel Temperature............................................................................................. –40°C
Maximum Fuel Temperature ............................................................................................ +50°C
WINGS FUSLAGE TOTAL
UNUSABLE 7.16 1.19 8.35
USABLE 427.20 305.80 733.00
TOTAL 434.36 306.99 741.35

Approved Engine Fuels

• Commercial kerosene Jet A, Jet A-1, Jet B, JP-4, JP-5, JP-8, JP-8+100, and RP-3 (Chinese)
• Fuels not containing icing inhibitors must have MIL-I-27686D or MIL-I-85470 fuel system icing
inhibitor added in amounts of not less than 0.10% nor more than 0.15% by volume.

Fuel Crossfeed and Imbalance

• Takeoff is prohibited with partial wing fuel and fuel in the fuselage tanks.
• Fuel crossfeed with two engines operating is limited to level flight when less than 600 lb remains
in the tank supplying fuel.

HYDRAULIC SYSTEM
• Power brakes
• Flaps
• Landing gear
• Speed brakes
• Thrust reversers

Hydraulic System Limitations

• Use MIL-I-5606
• Max allowable leakage from any component is 1 drop per 25 cycles or 2 drops per minute in the
pressurized condition of 1,000 psi to 1,500 psi.
• LH or RH PUMP PRESS LO caution light comes on 15 seconds after pressure drops below 750 ± 100 psi.
• Hydraulic pressure relief valve should open at 1,850 psi.

Normal hydraulic system pressure ...................................................................... 1,350 to 1,550 psi

HYD LEVEL LO light................................................................................................... 0.6 gallons

Accumulator Pressure Gauge

Pre-charge pressure ...................................................................................................... 900 ± 50 psi

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 HAWKER 400XP/BEECHJET 400A CLIENT GUIDE

OXYGEN AND PRESSURIZATION

Fully Charged System ....................................................................................................... 1,850 psi
• Quick-donning masks and smoke goggles must be on board and accessible to the crew for
each flight.
• Passenger masks must be serviceable when passengers are carried.
• Masks drop automatically when cabin altitude exceeds 12,500 ± 500 feet.
• CABIN PRESSURE LO caution light illuminates when cabin altitude exceeds 9,500 ± 500 feet.
• CABIN PRESSURE HI caution light illuminates when cabin differential exceeds 9.1 psid.
• Maximum cabin differential is 9.1 psid.
• Emergency pressurization activates automatically if pressure in the ACM exceeds 53 psi or if the
temperature in the ACM exceeds 400° ± 10°F.

ICE AND RAIN PROTECTION LIMITATIONS

• The magnetic compass is erratic and unreliable when WINDSHIELD heat is selected to HIGH
and/or the side window defog blowers are selected.
• Ground operation of the wing heat is not permitted except for preflight checks and landing rollout.
• Do not select 30° flaps within 15 seconds of selecting 10° flaps.
• Operations using flaps greater than 10° are limited to 20 minutes after initial flap extension.
After 20 minutes, use 10° flaps for landing.

FLIGHT CONTROLS
• With speed brakes extended, do not extend flaps beyond 10° in flight.
• Selecting flaps beyond 10° or advancing thrust lever(s) beyond a predetermined value will retract
the speed brakes.

MISCELLANEOUS SYSTEMS
Tire Pressure:
Mains............................................................................................................................. 125 ± 5 psi
Nose .............................................................................................................................. 120 ± 5 psi

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 HAWKER 400XP/BEECHJET 400A CLIENT GUIDE

AVIONICS
Autopilot
• Approved for CAT 1 ILS approaches only.
• Must be off for takeoff and landing.
• Yaw damp must be off for takeoff and landing.
• Do not manually override in flight.
• Do not operate with a trim malfunction.
• Autopilot utilizes the emergency trim motor.
• Max airspeed for autopilot usage is unchanged from the aircraft maximum speed limit
(VMO / MMO).
• Do not use below 200 feet AGL.
• A pilot must be at the controls with seatbelt and shoulder harnesses fastened during autopilot
operations.
• Autopilot preflight check must be conducted and found satisfactory prior to each flight for which
it is to be utilized.
• Both AHRS are required for autopilot operations.
• NAV captures, including LOC, must be accomplished with an intercept angle of 90° or less.
• LOC/BC captures must be accomplished with an intercept angle of 70° or less.
• VREF +5 minimum for autopilot coupled approaches.
• Do not use 1/2 bank mode when conducting FMS based approaches.

EFIS
• Third attitude indicator and standby power must be operative for takeoff.
• MAP mode of navigation and checklist data on MFD are provided only as an aid and are not
approved as primary information.
• Pilot and copilot PFDs must be operative in the normal mode for takeoff.
• Pilot and copilot ADCs must be operative for takeoff.

Operational Limitations
• Trim system must be checked and operable prior to flight.
• Stall warning system must be checked and operable prior to flight.
• Thrust reversers must be checked in accordance with the procedures in section 4 of the AFM prior
to flight.
• Speed brakes must be operable prior to flight.
• Rudder boost must be operable and armed for all operations.
• Cockpit voice recorder self-test must be successfully accomplished prior to flight.
• Do not operate engine anti-ice during ground operations above 10°C except for preflight.
Windshield anti-ice system must be ON (LOW or HI) for all in-flight operations. Windshield heat
HI mode is prohibited during takeoff and landing.

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 HAWKER 400XP/BEECHJET 400A CLIENT GUIDE

• Do not operate anti-ice systems at RAT greater than 10°C unless in actual icing conditions, as
indicated by illumination of the ICING annunciator (if installed) or airframe ice accumulation.
• ECS OFF and engine anti-ice ON is prohibited.
• Freon A/C operation below 5°C is prohibited.
• Do not operate Freon A/C with Horizontal Stab Anti-ice ON.
• Do not operate Freon A/C with Horizontal Stab De-ice ON.
• Do not operate Freon A/C with Horizontal Stab De-ice Backup ON.

STRUCTURAL LIMITATIONS
Maximum Ramp Weight ................................................................................................ 16,300 lbs
Maximum Takeoff Weight .............................................................................................. 16,100 lbs
Maximum Landing Weight ............................................................................................ 15,700 lbs
Maximum Zero Fuel Weight ........................................................................................... 13,000 lbs
With Increased Gross Weight Mod Kit 128-5052 or RK-347 and subsequent:
Maximum Ramp Weight ................................................................................................ 16,500 lbs
Maximum Takeoff Weight .............................................................................................. 16,300 lbs

MANEUVERING LOAD FACTORS

Flaps 0° .....................................................................................................................–1.0 to +3.2 G
Flaps 10°, 20°, and 30° .................................................................................................0 to +2.0 G

TAKEOFF AND LANDING OPERATIONS

Airfield Operation (Pressure Altitude) ...............................................................UP TO 10,000 feet
Ambient Temperature .....................................................................................–40°C to ISA +35°C
Maximum Tailwind Component for Takeoff and Landing ................................................ 10 knots
Maximum Fuel Unbalance for Takeoff ............................................................................... 100 lbs
Maximum Fuel Unbalance for Landing............................................................................... 300 lbs

ENROUTE OPERATIONS
Ambient Air Temperature......................................................................... –65°C to ISA + 35°C
Maximum Fuel Unbalance..............................................................................................300 lbs
Yaw Damper .......................OPERABLE AND ON FOR FLIGHT IN ICING CONDITIONS,
OR FLIGHT ABOVE 28,000 FEET
Maximum Operational Altitude ................................................................................45,000 feet
Freon A/C Operation .....................................................................Prohibited above 18,000 feet
Extension of gear, flaps, or landing lights .....................................Prohibited above 20,000 feet

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 HAWKER 400XP/BEECHJET 400A CLIENT GUIDE

16 FT 5 IN

9 FT 4 IN 43 FT 6 IN

5 FT 1 IN
19 FT 3 IN
43 FT 2 IN
48 FT 5 IN

CURB TO CURB 40.4 FT

23.0 FT

17.13 FT

8.0 FT

Aircraft Dimensions and Turn Radius

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 HAWKER 400XP/BEECHJET 400A CLIENT GUIDE

ANNUNCIATORS
CABIN ALTITUDE EXCEEDS CABIN PRESSURE DIFFERENTIAL
9,500 FEET ± 500 FEET EXCEEDS 9.1 PSID

FAULT DETECTED WITHIN LOOP OR FAULT DETECTED WITHIN LOOP OR

CONTROLLER * CONTROLLER

WINDSHIELD TEMPERATURE WINDSHIELD TEMPERATURE

EXCEEDING 190°F * EXCEEDING 190°F

HORIZONTAL STABILIZER DE-ICE/ WING TEMPERATURE EXCEEDING

ANTI-ICE SYSTEM HAS FAILED 212°F OR 350°F

OIL PRESSURE BELOW 40 PSI OIL PRESSURE BELOW 40 PSI

FUEL PRESSURE BELOW 5 PSI FUEL PRESSURE BELOW 5 PSI

MAIN FLAP ASYMMETRY OF 5–7°

LESS THAN 11 GALLONS (77 LB) LESS THAN 11 GALLONS (77 LB)
REMAINING IN THE COLLECTOR TANK REMAINING IN THE COLLECTOR TANK

FUSELAGE TANK IS EMPTY AND TRANSFER FUSELAGE TANK IS EMPTY AND TRANSFER
PUMP PRESSURE BELOW 1.3 PSI PUMP PRESSURE BELOW 1.3 PSI

LESS THAN 225 LB REMAINING LESS THAN 225 LB REMAINING

IN THE MAIN WING TANK IN THE MAIN WING TANK

WING TANK PRESSURE WING TANK PRESSURE

EXCEEDING 3.5 ± .5 PSI EXCEEDING 3.5 ± .5 PSI

2.3 PSI DIFFERENTIAL SENSED ACROSS 2.3 PSI DIFFERENTIAL SENSED ACROSS
FUEL FILTER. FUEL BYPASSING FUEL FILTER. FUEL BYPASSING
PRIMARY FUEL FILTER PRIMARY FUEL FILTER

OIL FILTER ELEMENT IS CLOGGED, OIL FILTER ELEMENT IS CLOGGED,

OIL BYPASSING OIL FILTER OIL BYPASSING OIL FILTER

PUMP PRESSURE LESS THAN PUMP PRESSURE LESS THAN

750 ± 15 PSI FOR GREATER THAN 15 750 ± 15 PSI FOR GREATER THAN 15
SECONDS SECONDS

ENGINE EFC IS DISENGAGED ENGINE EFC IS DISENGAGED

STALL STICK SHAKER IS INOPERATIVE STALL STICK SHAKER IS INOPERATIVE

* EITHER ANNUNCIATOR MAY BE INSTALLED

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ANNUNCIATORS
GENERATOR IS INOPERATIVE/OFFLINE GENERATOR IS INOPERATIVE/OFFLINE

ONE OF THREE FEEDERS HAS FAILED, ONE OF THREE FEEDERS HAS FAILED,
BACKUP FEEDER HAS ACTIVATED BACKUP FEEDER HAS ACTIVATED

EM ERGEN C Y BU S FEEDER H AS
BATTERY RELAY HAS OPENED
LO ST POWER

INVERTER FAILED/OFFLINE INVERTER FAILED/OFFLINE

ENGINE INLET COWL TEMPERATURE ENGINE INLET COWL TEMPERATURE

BELOW 120°F BELOW 120°F

AIR CYCLE MACHINE HAS FAILED DUE

TO OVER TEMPERATURE (400°F) OR
OVER PRESSURE (53 PSI). EMERGENCY
ICE DETECTOR HAS FAILED
PRESSURIZATION HAS BEEN ACTIVATED.
ANNUNCIATOR WILL ILLUMINATE IF EMER
IS SELECTED ON THE ECS SELECTOR.

ONE OF FOUR TEMPERATURE

SENSORS IN THE TAIL EXCEEDING MAIN CABIN DOOR OR AFT BAGGAGE
350°F OR WING DE-ICE SHROUD DOOR UNLOCKED
DUCT EXCEEDING 3.5 ± .5 PSI

PITOT HEATER SWITCHES ARE NOT ON

DEFOG AIR EXCEEDING 200°F OR PITOT HEAT SYSTEM HAS FAILED
WITH SWITCHES SELECTED ON

CONDITIONED CABIN DUCT AIR HYDRAULIC RESERVOIR LEVEL BELOW

EXCEEDING 390°F 0.6 GALLONS

ANTI-SKID SYSTEM IS SELECTED OFF OR RUDDER BOOST IS SELECTED OFF OR

HAS FAILED HAS FAILED

ANY CONDITION WHERE THRUST ANY CONDITION WHERE THRUST

REVERSERS ARE UNLOCKED OR REVERSERS ARE UNLOCKED OR
DEPLOYED, EMER STOW SWITCHES DEPLOYED, EMER STOW SWITCHES
ARE ENABLED. PUSHING SWITCH(ES) ARE ENABLED. PUSHING SWITCH(ES)
PROVIDES HYDRAULIC PRESSURE TO PROVIDES HYDRAULIC PRESSURE TO
CLOSE REVERSER DOORS. CLOSE REVERSER DOORS.

RESTOW ENVELOPE: RESTOW ENVELOPE:

BELOW 30,000 FEET AND BELOW 135 KTS BELOW 30,000 FEET AND BELOW 135 KTS

* EITHER ANNUNCIATOR MAY BE INSTALLED

Revision 0 FOR TRAINING PURPOSES ONLY 5-17

 HAWKER 400XP/BEECHJET 400A CLIENT GUIDE

FLIGHT PROFILES

NOTE:
PRIOR TO TAKING ACTIVE RUNWAY: CLIMB
1. HEADING BUG—SET RUNWAY HEADING
2. F/D—CONFIRM HDG AND PTCH SELECTED 1. ACCELERATE TO CLIMB SPEED
3. CONFIRM ALT PRESELECTOR SET
4. LINEUP CHECKS — COMPLETE

"400' AGL"
1. FLAPS—UP
2. AFTER TAKEOFF CHECKLIST

"ROTATE"
"V1"
1. ROTATE 13°-15° *
1. PILOT—BOTH HANDS ON YOKE 2. RELEASE PITCH SYNC
2. PITCH SYNC—PUSH AND HOLD

AFTER TAKEOFF
1. POSITIVE RATE
2. GEAR—UP
3. LIGHTS—IN
"80 KNOTS" 4. YAW DAMP—ON

"AIRSPEED ALIVE"

TAKEOFF
1. LINE UP AND HOLD BRAKES
2. SET POWER TO APPROXIMATELY 90% N1
3. CHECK ENGINE INSTRUMENTS * CAUTION:
4. RELEASE BRAKES AND ADVANCE POWER ROTATING TO LESS THAN 10° CAN CAUSE A
TO TARGET N1 WING TIP STRIKE IN THE EVENT OF AN ENGINE
5. SET TAKEOFF POWER BY 80 KIAS FAILURE, WAKE TURBULENCE, THRUST
REVERSER DEPLOYMENT, OR FAILURE TO
OBTAIN PUBLISHED OBSTACLE CLEARANCE.

Takeoff—Normal

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 HAWKER 400XP/BEECHJET 400A CLIENT GUIDE

CALL OUTS NOTES

TAKEOFF
PM SHOULD SET T.O. THRUST BY 80 KIAS AND THEN MOVE
PF* “SET POWER” HIS OR HER HAND AWAY TO AVOID INJURY IN THE EVENT
PM** “POWER SET” OF A THRUST REVERSER DEPLOYMENT OR AN ABORT. PM
SHOULD NOT HAVE HIS OR HER HANDS ON THE THROTTLES
PF “CHECK”
UNTIL SETTING MCT.

AIRSPEED ALIVE
PM “AIRSPEED ALIVE” PF GLANCES AT HIS OR HER AIRSPEED INDICATOR
PF “CHECK” AND VERIFIES MOTION.

80 KNOTS
PM “80 KNOTS” THE PF SHOULD READ AND RESPOND FROM HIS OR HER
AIRSPEED INDICATOR. ANY DISCREPANCY IN EXCESS OF 10
PF “80” KNOTS SHOULD CALL FOR AN ABORT.

V1
PM “V1”

VR
PM “ROTATE” THE CALLOUT SHOULD BE “ROTATE,” NOT “VR.”

AFTER TAKEOFF
PM “POSITIVE RATE”
PF “GEARUPLIGHTSINYAWDAMPON” ONE WORDER
PM “GEARUPLIGHTSINYAWDAMPON”

400’ AGL
PM “400 FEET” (AFTER TAKEOFF, CHECKS SHOULD BE DONE BY
MEMORY AND VERIFIED WITH THE CHECKLIST AT A SAFE
PF “FLAPSUPAFTERTAKEOFF CHECKLIST” ALTITUDE AND TIME)

STANDARDS:
AIRSPEED ± 5 KNOTS (ROTATE AND CLIMB OUT)
*PF = PILOT FLYING
HEADING ± 5°
**PM = PILOT MONITORING
ALTITUDE ± 100 FEET
ROTATION ANGLE 15° ± 3

Revision 0 FOR TRAINING PURPOSES ONLY 5-19

 HAWKER 400XP/BEECHJET 400A CLIENT GUIDE

NOTE:
PRIOR TO TAKING ACTIVE RUNWAY:
1. HEADING BUG—SET RUNWAY HEADING
2. F/D—CONFIRM HDG AND PTCH SELECTED
3. CONFIRM ALT PRESELECTOR SET
4. LINEUP CHECKS — COMPLETE

ABORT
1. BRAKES—APPLY
2. THRUST—IDLE
3. THRUST REVERSER(S)—DEPLOY
ENGINE FAILURE 4. REVERSER LIGHTS—VERIFY
1. ENGINE FAILURE OR 5. REVERSE THRUST—AS REQUIRED
OTHER MALFUNCTION 6. SPEEDBRAKES—EXTEND
PRIOR TO V1

"80 KNOTS"

"AIRSPEED ALIVE"

TAKEOFF
1. LINE UP AND HOLD BRAKES
2. SET POWER TO APPROXIMATELY 90% N1
3. CHECK ENGINE INSTRUMENTS
4. RELEASE BRAKES AND ADVANCE POWER
TO TARGET N1
5. SET TAKEOFF THRUST BY 80 KIAS

NOTE:
IN CASE OF AN ENGINE FAILURE, THE PM WILL NOT
DIFFERENTIATE BETWEEN SIDES. IN CASE OF AN
ENGINE FIRE, THE PM WILL INDICATE THE ENGINE THAT
IS ON FIRE.

Takeoff—Rejected

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 HAWKER 400XP/BEECHJET 400A CLIENT GUIDE

CALL OUTS NOTES

TAKEOFF
PM SHOULD SET T.O. THRUST BY 80 KIAS AND THEN MOVE
PF* “SET POWER” HIS OR HER HAND AWAY TO AVOID INJURY IN THE EVENT
PM** “POWER SET” OF A THRUST REVERSER DEPLOYMENT OR AN ABORT. PM
SHOULD NOT HAVE HIS OR HER HANDS ON THE THROTTLES
PF “CHECK”
UNTIL SETTING MCT.

AIRSPEED ALIVE
PM “AIRSPEED ALIVE” PF GLANCES AT HIS OR HER AIRSPEED INDICATOR
PF “CHECK” AND VERIFIES MOTION.

80 KNOTS
PM “80 KNOTS”
PF “80”

ENGINE FAILURE
THE PF SHOULD READ AND RESPOND FROM HIS OR HER
“ABORT, ABORT, ABORT”** AIRSPEED INDICATOR. ANY DISCREPANCY IN EXCESS OF 10
KNOTS SHOULD CALL FOR AN ABORT.

ABORT
PF “SPEED BRAKES”
PM “TOWER, FLIGHT XXX ABORTING”

IN CASE OF AN ENGINE FIRE DURING

TAKEOFF, THE PM SHOULD IDENTIFY THE ENGINE AS THE
PF MAINTAINS DIRECTIONAL CONTROL. PM WILL CALL NO
REVERSE ON THE ___ ENGINE.
CAPTAIN WILL SECURE THE AIRCRAFT WHILE THE F.O.
ESCORTS THE PASSENGERS TO SAFETY.
*PF = PILOT FLYING
STANDARDS:
**PM = PILOT MONITORING
APPLY THE CONTROLS SMOOTHLY TO MAINTAIN
***EITHER PILOT CAN CALL ABORT
LONGITUDINAL ALIGNMENT ON THE CENTERLINE OF THE
RUNWAY. ABORT THE TAKEOFF…WHERE THE AIRPLANE
CAN BE SAFELY STOPPED ON THE REMAINING RUNWAY.
USE SPOILERS, THRUST REVERSER(S), SPEED BRAKES,
WHEEL BRAKES AS APPROPRIATE, MAINTAINING POSITIVE
CONTROL…TO A SAFE STOP.
EXECUTE…APPROPRIATE CHECKLIST.

Revision 0 FOR TRAINING PURPOSES ONLY 5-21

 HAWKER 400XP/BEECHJET 400A CLIENT GUIDE

NOTE:
PRIOR TO TAKING ACTIVE RUNWAY: 1,500' AGL
1. HEADING BUG—SET RUNWAY HEADING 1. ACCELERATE TO 170 KIAS
2. F/D—CONFIRM HDG AND PTCH SELECTED 2. COMPLETE ENGINE FAILURE
3. CONFIRM ALT PRESELECTOR SET CHECKLIST
4. LINEUP CHECKS—COMPLETE

400' AGL LEVEL OFF

1. ACCELERATE TO V2 + 10 KT
2. FLAPS—UP
3. AFTER TAKEOFF CHECKLIST
4. ACCELERATE TO 140 KIAS

"ROTATE"
CLIMB
1. ROTATE 13°-15° *
1. MAINTAIN 140 KIAS TO
2. RELEASE PITCH SYNC
1,500' AGL
"V1" 2. CONTINUE WITH PLANNED
TAKEOFF FLIGHT PATH
1. PILOT—BOTH HANDS ON YOKE
2. PITCH SYNC—PUSH AND HOLD

AFTER TAKEOFF
"80 KNOTS" 1. POSITIVE RATE—GEAR UP, LIGHTS IN,
YAW DAMP ON
2. MAINTAIN V2
3. CHECK POWER—TAKEOFF THRUST

"AIRSPEED ALIVE"

ENGINE FAILURE

TAKEOFF
1. LINE UP AND HOLD BRAKES
2. SET POWER TO APPROXIMATELY 90% N1
NOTE:
3. ENGINE INSTRUMENTS—CHECK
THE PM WILL NOT DIFFERENTIATE BETWEEN
4. RELEASE BRAKES AND ADVANCE POWER
ENGINES IN THE CASE OF AN ENGINE FIRE
TO TARGET N1
AFTER V1. NO ACTION SHOULD BE TAKEN
5. SET TAKEOFF THRUST BY 80 KIAS
BELOW 400' AGL.

* CAUTION:
ROTATING TO LESS THAN 10° CAN CAUSE A
WINGTIP STRIKE IN THE EVENT OF AN ENGINE
FAILURE, WAKE TURBULENCE, THRUST
REVERSER DEPLOYMENT, OR FAILURE TO
OBTAIN PUBLISHED OBSTACLE CLEARANCE.

Engine Failure During Takeoff Above V1 Takeoff

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 HAWKER 400XP/BEECHJET 400A CLIENT GUIDE

CALL OUTS NOTES

TAKEOFF
PM SHOULD SET T.O. THRUST BY 80 KIAS AND THEN MOVE
PF* “SET POWER” HIS OR HER HAND AWAY TO AVOID INJURY IN THE EVENT
PM** “POWER SET” OF A THRUST REVERSER DEPLOYMENT OR AN ABORT. PM
SHOULD NOT HAVE HIS OR HER HANDS ON THE THROTTLES
PF “CHECK”
UNTIL SETTING MCT.

AIRSPEED ALIVE
PM “AIRSPEED ALIVE” PF GLANCES AT HIS OR HER AIRSPEED INDICATOR
PF “CHECK” AND VERIFIES MOTION.

80 KNOTS
PM “80 KNOTS” THE PF SHOULD READ AND RESPOND FROM HIS OR HER
AIRSPEED INDICATOR. ANY DISCREPANCY IN EXCESS OF 10
PF “80” KNOTS SHOULD CALL FOR AN ABORT.

V1
PM “V1”

ENGINE FAILURE
PM “ENGINE FAILURE” THE PM WILL NOT DIFFERENTIATE BETWEEN SIDES.

VR
PM “ROTATE” THE CALLOUT SHOULD BE “ROTATE,” NOT “VR.”

AFTER TAKEOFF
PM “POSITIVE RATE”
ONE WORDER
PF “GEARUPLIGHTSINYAWDAMPON”
PM SHOULD ANNOUNCE ANY DEVIATIONS GREATER THAN
PM “GEARUPLIGHTSINYAWDAMPON”
± 10º OF HEADING OR ± 5 KIAS FROM VR
PM “V2 ± …”

400’ AGL
PM “400 FEET”
ONE WORDER
PF “ACCELERATING”
(AFTER TAKEOFF, CHECKS SHOULD BE DONE BY MEMORY
PM “V2 + 10” AND VERIFIED WITH THE CHECKLIST AT A SAFE ALTITUDE
AND TIME)
PF “FLAPSUPAFTERTAKEOFF CHECKLIST”

1500 FEET AGL

PM “1500 FEET, STANDING BY ENGINE
FAILURE CHECKLIST”

*PF = PILOT FLYING

**PM = PILOT MONITORING
***EITHER PILOT CAN CALL ABORT

Revision 0 FOR TRAINING PURPOSES ONLY 5-23

 HAWKER 400XP/BEECHJET 400A CLIENT GUIDE

PAST NOISE
SENSITIVE AREA
1. SET MCT
2. FLAPS—UP (IF USED)
3. COMPLETE AFTER
NOTE: TAKEOFF CHECKLIST
PRIOR TO TAKING ACTIVE RUNWAY:
1. HEADING BUG—SET RUNWAY HEADING
2. F/D—CONFIRM HDG AND PTCH SELECTED
3. CONFIRM ALT PRESELECTOR SET
4. LINEUP CHECKS—COMPLETE AT APPROPRIATE ALTITUDE *
1. DECREASE PITCH TO 5° - 10°,
IF SAFE TO DO SO *
2. REDUCE POWER TO
APPROXIMATELY 85% N1 *

"ROTATE"
"V1"
1. PIC—ROTATE 13°-15° †
1. PILOT—BOTH HANDS ON YOKE 2. RELEASE PITCH SYNC
2. PITCH SYNC—PUSH AND HOLD

MAINTAIN V2 + 10 KT

"80 KNOTS" AFTER TAKEOFF

1. POSITIVE RATE
2. GEAR—UP
3. LIGHTS—IN
4. YAW DAMP—ON
"AIRSPEED ALIVE"

TAKEOFF
1. LINE UP AND HOLD BRAKES
2. SET POWER TO APPROXIMATELY 90% N1
3. ENGINE INSTRUMENTS—CHECK
4. RELEASE BRAKES AND ADVANCE POWER * NOTE:
TO TARGET N1 SAFETY IS ALWAYS THE PRIMARY CONSIDERATION.
5. SET TAKEOFF THRUST BY 80 KIAS BEFORE REDUCING POWER OR CHANGING DECK
ANGLE. THE FLIGHT CREW SHOULD CONSIDER
OBSTACLES, AIRFIELD RESTRICTIONS, AND RISING
TERRAIN.

† CAUTION:
ROTATING TO LESS THAN 10° CAN CAUSE A
WINGTIP STRIKE IN THE EVENT OF AN ENGINE
FAILURE, WAKE TURBULENCE, THRUST
REVERSER DEPLOYMENT, OR FAILURE TO
OBTAIN PUBLISHED OBSTACLE CLEARANCE.

Noise Abatement Takeoff

5-24 FOR TRAINING PURPOSES ONLY Revision 0

 HAWKER 400XP/BEECHJET 400A CLIENT GUIDE

CALL OUTS NOTES

TAKEOFF
PM SHOULD SET T.O. THRUST BY 80 KIAS AND THEN MOVE
PF* “SET POWER”
HIS OR HER HAND AWAY TO AVOID INJURY IN THE EVENT
PM** “POWER SET” OF A THRUST REVERSER DEPLOYMENT OR AN ABORT. PM
PF “CHECK” SHOULD NOT HAVE THEIR HANDS ON THE THROTTLES
UNTIL SETTING MCT.

AIRSPEED ALIVE
PM “AIRSPEED ALIVE” PF GLANCES AT HIS OR HER AIRSPEED INDICATOR
PF “CHECK” AND VERIFIES MOTION.

80 KNOTS
PM “80 KNOTS” THE PF SHOULD READ AND RESPOND FROM HIS OR HER
AIRSPEED INDICATOR. ANY DISCREPANCY IN EXCESS OF 10
PF “80” KNOTS SHOULD CALL FOR AN ABORT.

V1
PM “V1”

VR
PM “ROTATE” THE CALLOUT SHOULD BE “ROTATE,” NOT “VR.”

AFTER TAKEOFF
PM “POSITIVE RATE”
PF “GEARUPLIGHTSINYAWDAMPON”
ONE WORDER
PM “GEARUPLIGHTSINYAWDAMPON”
PM “V2 + 10”

AT APPROPRIATE ALTITUDE
NOTE:
IN ANY NONSTANDARD PROCEDURE THE FLIGHT CREW
PM “DECREASE PITCH”
MUST MAINTAIN A HIGH DEGREE OF SITUATIONAL
PM “STANDING BY TO REDUCE POWER” AWARENESS. IN THIS CASE, LOOKING FOR TRAFFIC,
PF “POWER 85%” SCANNING FOR OBSTACLES, MAINTAINING AIRCRAFT
CONTROL, AND FOLLOWING THE FLIGHT PROFILE ALL
DISTRACTS THE CREW.

PAST NOISE SENSITIVE AREA

PF “SET MCT”
PF “FLAPSUPAFTERTAKEOFF CHECKLIST”

STANDARDS:
AIRSPEED ± 10 KNOTS (ROTATE AND CLIMB OUT)
*PF = PILOT FLYING
HEADING ± 10°
**PM = PILOT MONITORING
ALTITUDE ± 100 FEET
ROTATION DECK ANGLE 15° ± 3°

Revision 0 FOR TRAINING PURPOSES ONLY 5-25

 HAWKER 400XP/BEECHJET 400A CLIENT GUIDE

200 KIAS
1. PREPARE FOR TURN IN NOTE:
THE OPPOSITE DIRECTION TURNS WILL BE ACCOMPLISHED
THROUGH 180° OR 360°

BANK ESTABLISHED
1. 30° BANK, CHECK AIRSPEED
AND ALTITUDE TRENDS
2. 45° BANK ESTABLISHED

EXIT
1. ROLL OUT ON HEADING AND
ALTITUDE. REDUCE POWER
5% N1 TO MAINTAIN 200 KIAS

ENTRY
1. ADD APPROXIMATELY 5% N1
AS TURN IS STARTED
2. PITCH APPROXIMATELY 5° CHECK AIRSPEED AND
ALTITUDE TRENDS

NOTE: PILOT MAY ELECT TO

ROLLOUT AND STABILIZE ON
HEADING AND AIRSPEED OR
PROCEED TO ROLL INTO A
TURN IN THE OPPOSITE
DIRECTION

ROLLOUT
1. START ROLLOUT 10° BEFORE
ROLLOUT HEADING

MANEUVER SETUP
1. GEAR UP, FLAPS UP
2. TRIM AIRPLANE FOR
200 KIAS LEVEL FLIGHT
3. 75% N1, 5° PITCH

Steep Turns

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 HAWKER 400XP/BEECHJET 400A CLIENT GUIDE

CALL OUTS NOTES

MANEUVER SETUP
BRIEF THE MANEUVER. THE PM MAY NOT ASSIST THE PF
DURING TESTING/CHECKING.

ENTRY

BANK ESTABLISHED

ROLLOUT
NOTE:
TURNS WILL BE 360° UNLESS SPECIFIED OTHERWISE BY
THE INSTRUCTOR OR EXAMINER.

ENGINE FAILURE

EXIT

STANDARDS:
BANK ANGLE ± 5°
ALTITUDE ± 100 FEET
AIRSPEED ± 10 KNOTS
ROLLOUT ± 10° OF SPECIFIED HEADING OR ENTRY HEADING

Revision 0 FOR TRAINING PURPOSES ONLY 5-27

 HAWKER 400XP/BEECHJET 400A CLIENT GUIDE

BEGINNING OF MANEUVER STALL AND RECOVERY COMPLETION OF MANEUVER

1. THRUST - AS DIRECTED ANNOUNCE THE FIRST INDICATION OF AN 1. ACCELERATE TO 140 KIAS

2. FLAPS - 10° (BELOW 200 KIAS) IMPENDING STALL (SUCH AS STICK SHAKER) 2. FLAPS—UP
3. LEVEL OFF AT NEW ALTITUDE
1. AUTOPILOT—DISCONNECT AND HEADING
2. NOSE DOWN PITCH CONTROL—APPLY UNTIL STALL
WARNING IS ELIMINATED
3. NOSE DOWN PITCH TRIM—AS NEEDED
4. BANK—WINGS LEVEL
5. THRUST—MAX ALLOWABLE
6. SPEED BRAKE—RETRACT

NOTE: THE REDUCTION OF ANGLE OF ATTACK

REQUIRED TO INITIATE RECOVERY WILL LIKELY
RESULT IN ALTITUDE LOSS. THE AMOUNT OF
ALTITUDE LOSS WILL BE AFFECTED BY THE
OPERATIONAL ENVIRONMENT.

EXECUTION:

1. THE INSTRUCTOR SETS UP THE STALL SCENARIO

2. THE ENTRY ALTITUDE SHOULD BE CONSISTENT WITH THE EXPECTED OPERATIONAL
ENVIRONMENT FOR THE STALL CONFIGURATION
3. FOR TRAINING AND EVALUATION, THE MANEUVERS MAY BE ACCOMPLISHED WITH THE
AUTOPILOT ON OR OFF AS DIRECTED BY THE INSTRUCTOR
4. THE STANDARD IS BASED ON THE DEMONSTRATION OF PROPER RECOGNITION AND RECOVERY
FROM THE STALL

THE AIM OF THESE STALL PROFILES IS TO FAMILIARIZE THE PILOT WITH THE STALL CHARACTERISTICS AND TO TRAIN
RECOGNITION AND RECOVERY PROCEDURES IN ACCORDANCE WITH THE ATP PRACTICAL TEST STANDARDS IN FLIGHT
SIMULATOR TRAINING ONLY. THESE STALL PROFILES ARE NOT INTENDED FOR MAINTENANCE TEST
FLIGHTS OR AIRCRAFT TRAINING.

Approach to Stall—Takeoff Configuration (Simulator)

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 HAWKER 400XP/BEECHJET 400A CLIENT GUIDE

CALL OUTS NOTES

MANEUVER SETUP
BRIEF THE MANEUVER.

BEGINNING
PF* “SET POWER”
PF WILL SET APPROXIMATELY 50% N1
PM** “SPEED CHECKS, FLAPS SELECTED 10, TO START THE MANEUVER.
INDICATING 10"

STICK SHAKER
PF MUST ANNOUNCE THE STALL
PF “STALL!” (PRACTICAL TEST STANDARDS).
PF REDUCES ANGLE OF ATTACK, ROLLS WINGS LEVEL
PF “ADJUST POWER"
PF MUST MAKE THE INITIAL POWER SETTING TO AT
PM “MAX POWER SET” LEAST 90% AND PM MAY THEN ADJUST THE POWER TO
MAXIMUM WITHIN ENGINE LIMITATIONS.

BUG + 10 KNOTS
PF "FLAPS UP"
PM "FLAPS UP"
PF “REDUCE POWER”

STANDARDS:
PILOT MUST EXHIBIT KNOWLEDGE OF THE FACTORS
WHICH INFLUENCE STALL CHARACTERISTICS, INCLUDING
POWER SETTINGS, PITCH ATTITUDE AND BANK ANGLES.
*PF = PILOT FLYING ANNOUNCE THE FIRST INDICATION OF AN IMPENDING STALL
INITIATES A PROMPT RECOVERY BY REDUCING ANGLE OF
**PM = PILOT MONITORING
ATTACK MANAGEMENT OF THRUST AND LEVELING THE
WINGS PROMPTLY.
PILOT SHOULD MINIMIZE ALTITUDE LOSS AND MAINTAIN
RECOVERY HEADING WHILE RECONFIGURING THE
AIRCRAFT.

Revision 0 FOR TRAINING PURPOSES ONLY 5-29

 HAWKER 400XP/BEECHJET 400A CLIENT GUIDE

BEGINNING OF MANEUVER APPROACH AND RECOVERY COMPLETION OF MANEUVER

1. THRUST - AS DIRECTED ANNOUNCE THE FIRST INDICATION OF AN 1. LEVEL OFF AT NEW ALTITUDE
IMPENDING STALL (SUCH AS STICK SHAKER) AND HEADING

1. AUTOPILOT - DISCONNECT
2. NOSE DOWN PITCH CONTROL - APPLY UNTIL STALL
WARNING IS ELIMINATED
3. NOSE DOWN PITCH TRIM - AS NEEDED
4. BANK - WINGS LEVEL
5. THRUST - MAX ALLOWABLE
6. SPEED BRAKE - RETRACT

NOTE: THE REDUCTION OF ANGLE OF ATTACK

REQUIRED TO INITIATE RECOVERY WILL LIKELY
RESULT IN ALTITUDE LOSS. THE AMOUNT OF
ALTITUDE LOSS WILL BE AFFECTED BY THE
OPERATIONAL ENVIRONMENT.

EXECUTION:

1. THE INSTRUCTOR SETS UP THE STALL SCENARIO

2. THE ENTRY ALTITUDE SHOULD BE CONSISTENT WITH THE EXPECTED OPERATIONAL
ENVIRONMENT FOR THE STALL CONFIGURATION
3. FOR TRAINING AND EVALUATION, THE MANEUVERS MAY BE ACCOMPLISHED WITH THE
AUTOPILOT ON OR OFF AS DIRECTED BY THE INSTRUCTOR
4. THE STANDARD IS BASED ON THE DEMONSTRATION OF PROPER RECOGNITION AND RECOVERY
FROM THE STALL

THE AIM OF THESE STALL PROFILES IS TO FAMILIARIZE THE PILOT WITH THE STALL CHARACTERISTICS AND TO TRAIN
RECOGNITION AND RECOVERY PROCEDURES IN ACCORDANCE WITH THE ATP PRACTICAL TEST STANDARDS IN FLIGHT
SIMULATOR TRAINING ONLY. THESE STALL PROFILES ARE NOT INTENDED FOR MAINTENANCE TEST
FLIGHTS OR AIRCRAFT TRAINING.

Approach to Stall—Enroute

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 HAWKER 400XP/BEECHJET 400A CLIENT GUIDE

CALL OUTS NOTES

MANEUVER SETUP
BRIEF THE MANEUVER.

BEGINNING
PF WILL SET APPROXIMATELY 50% N1.
PF* “SET POWER”
PM MAY THEN SET ADJUST/TRIM POWER.

STICK SHAKER
PF MUST ANNOUNCE THE STALL
PF “STALL!”
(PRACTICAL TEST STANDARDS).

PF IMMEDIATELY REDUCES THE ANGLE OF ATTACK AND

ADVANCES THE THROTTLES TO AT LEAST 90% AND THE
PF “SET MAX POWER”
PM RAPIDLY ADJUSTS THE POWER TO MAXIMUM WITHIN
ENGINE LIMITATIONS.

BUG + 10 KNOTS
(AT BUG + 10 THE MANEUVER IS CONSIDERED COMPLETE
PF “REDUCE POWER”
AND THE PM MAY RETURN TO NORMAL DUTIES)

STANDARDS:
PILOT MUST EXHIBIT KNOWLEDGE OF THE FACTORS
WHICH INFLUENCE STALL CHARACTERISTICS, INCLUDING
*PF = PILOT FLYING POWER SETTINGS, PITCH ATTITUDE, AND BANK ANGLES.
ANNOUNCE THE FIRST INDICATION OF AN IMPENDING
STALL INITIATES A PROMPT RECOVERY MANAGEMENT OF
THRUST AND LEVELING THE WINGS.

Revision 0 FOR TRAINING PURPOSES ONLY 5-31

 HAWKER 400XP/BEECHJET 400A CLIENT GUIDE

BEGINNING OF MANEUVER STALL AND RECOVERY COMPLETION OF MANEUVER

1. THRUST - AS DIRECTED ANNOUNCE THE FIRST INDICATION OF AN 1. ACCELERATE TO 140 KIAS

2. FLAPS - 10° (BELOW 200 KIAS) IMPENDING STALL (SUCH AS STICK SHAKER) 2. FLAPS—UP
3. GEAR - DOWN (BELOW 200 KIAS) 3. LEVEL OFF AT NEW ALTITUDE
4. FLAPS - 30° (BELOW 170 KIAS) 1. AUTOPILOT - DISCONNECT AND HEADING
2. NOSE DOWN PITCH CONTROL - APPLY UNTIL STALL
WARNING IS ELIMINATED
3. NOSE DOWN PITCH TRIM - AS NEEDED
4. BANK - WINGS LEVEL
5. THRUST - MAX ALLOWABLE
6. 100 KIAS - FLAPS 10°
7. POSITIVE RATE - GEAR UP

NOTE: THE REDUCTION OF ANGLE OF ATTACK

REQUIRED TO INITIATE RECOVERY WILL LIKELY
RESULT IN ALTITUDE LOSS. THE AMOUNT OF
ALTITUDE LOSS WILL BE AFFECTED BY THE
OPERATIONAL ENVIRONMENT.

EXECUTION:

1. THE INSTRUCTOR SETS UP THE STALL SCENARIO

2. THE ENTRY ALTITUDE SHOULD BE CONSISTENT WITH THE EXPECTED OPERATIONAL
ENVIRONMENT FOR THE STALL CONFIGURATION
3. FOR TRAINING AND EVALUATION, THE MANEUVERS MAY BE ACCOMPLISHED WITH THE
AUTOPILOT ON OR OFF AS DIRECTED BY THE INSTRUCTOR
4. THE STANDARD IS BASED ON THE DEMONSTRATION OF PROPER RECOGNITION AND RECOVERY
FROM THE STALL

THE AIM OF THESE STALL PROFILES IS TO FAMILIARIZE THE PILOT WITH THE STALL CHARACTERISTICS AND TO TRAIN
RECOGNITION AND RECOVERY PROCEDURES IN ACCORDANCE WITH THE ATP PRACTICAL TEST STANDARDS IN FLIGHT
SIMULATOR TRAINING ONLY. THESE STALL PROFILES ARE NOT INTENDED FOR MAINTENANCE TEST
FLIGHTS OR AIRCRAFT TRAINING.

Approach to Stall—Landing Configuration (Simulator)

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 HAWKER 400XP/BEECHJET 400A CLIENT GUIDE

CALL OUTS NOTES

MANEUVER SETUP
BRIEF THE MANEUVER.

BEGINNING
PF* “FLAPS 10”
PM** “SPEED CHECKS, FLAPS SELECTED 10,
INDICATING 10"
PF “GEAR DOWN"
PM “SPEED CHECKS, GEAR DOWN"
PF WILL SET APPROXIMATELY 50% N1 TO START THE
PM “THREE GREEN, NO RED, VERIFY?"
MANEUVER, PM MAY THEN SET ADJUST POWER TO 50%.
PF “GEAR CHECKS THREE GREEN"
PF “FLAPS 30”
PM “SPEED CHECKS, FLAPS SELECTED 30,
INDICATING 30"
PF “TRIM POWER"

STICK SHAKER
PF “STALL!”
PF “SET MAX POWER"
PF “ADJUST POWER"
PF MUST ANNOUNCE THE STALL
PF “FLAPS 10” (PRACTICAL TEST STANDARDS).
PM “SPEED CHECKS, FLAPS SELECTED 10, PF MUST MAKE THE INITIAL POWER SETTING TO AT
INDICATING 10" LEAST 90% AND PM MAY THEN ADJUST THE POWER TO
MAXIMUM WITHIN ENGINE LIMITATIONS.
PF “POSITIVE RATE”
PF “GEARUPLIGHTSINYAWDAMPON”
PM “GEARUPLIGHTSINYAWDAMPON”

BUG + 10 KNOTS
PF "FLAPS UP"
PM "FLAPS SELECTED UP, INDICATING POWER"
PF “SET POWER 75%”

STANDARDS:
PILOT MUST EXHIBIT KNOWLEDGE OF THE FACTORS THAT
INFLUENCE STALL CHARACTERISTICS, INCLUDING POWER
SETTINGS, PITCH ATTITUDE, AND BANK ANGLES.
*PF = PILOT FLYING ANNOUNCE THE FIRST INDICATION OF AN IMPENDING STALL
INITIATES A PROMPT RECOVERY BY REDUCING ANGLE OF
**PM = PILOT MONITORING
ATTACK MANAGEMENT OF THRUST AND LEVELING THE
WINGS PROMPTLY.
PILOT SHOULD MINIMIZE ALTITUDE LOSS AND MAINTAIN
RECOVERY HEADING WHILE RECONFIGURING THE
AIRCRAFT.

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 HAWKER 400XP/BEECHJET 400A CLIENT GUIDE

INITIAL DESCENT LEVEL-OFF

1. CRUISE CONFIGURATION
2. AT EXPLOSIVE/RAPID DECOMPRESSION—
PILOT AND COPILOT DON OXYGEN MASKS
(5 SECONDS)
3. SWITCHES—MIC SELECTOR/OXY MASK/
MIC/SPKR SWITCHES—ON OR DON
HEADSET INTERPHONE SWITCH—ON
4. THRUST LEVERS—IDLE
5. AUTOPILOT—DISCONNECT
6. SPEEDBRAKES—EXTEND
1. INITIATE MODERATE BANK NOT 1. LEVEL-OFF AT ASSIGNED
TO EXCEED 45° OR SAFE ALTITUDE *
2. PITCH—INITIALLY 15° NOSE DOWN 2. RETRACT SPEEDBRAKES
CAUTION: 3. WINGS LEVEL 3. POWER—AS REQUIRED
DO NOT USE THE RED TRIM INT/AP 4. ACCELERATE TO VMO/MMO
DISCONNECT SWITCH TO DISCONNECT 5. MAINTAIN HEADING, OR AS REQUIRED
THE AUTOPILOT. THIS WILL DISCONNECT 6. RAPID DECOMPRESSION AND/OR * PILOTS SHOULD CONSIDER:
THE YAW DAMP WHICH COULD CAUSE AN EMERGENCY DESCENT CHECKLIST— 1. TERRAIN
AN UNCONTROLLABLE DUTCH ROLL AND PERFORM 2. MEA, MOCA, DIRECTION
POSSIBLE LOSS OF AIRCRAFT CONTROL OF FLIGHT
AT ALTITUDE. 3. WHETHER RADAR SERVICE
CAUTION: DO NOT CONTINUOUSLY IS BEING PROVIDED
SPIRAL DOWN THROUGH THE FLIGHT 4. RVSM AIRSPACE
LEVELS BENEATH YOU. CONSIDER THE
TRAFFIC BENEATH YOU.

Emergency Descent

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 HAWKER 400XP/BEECHJET 400A CLIENT GUIDE

CALL OUTS NOTES

EXPLOSIVE/RAPID DECOMPRESSION
PF*, PM** “MASKS”
PILOT AND COPILOT SHOULD DON THEIR MASKS IN LESS
PF “AUTOPILOT OFF”
THAN 5 SECONDS. *
PF “SPEEDBRAKES”

DESCENT
PF “ADVISE ATC”
PF “EMERGENCY DESCENT CHECKLIST”

* AVERAGE TIME OF USEFUL CONSCIOUSNESS

35,000 FEET ................... 1/2 TO 1 MINUTE
40,000 FEET ................... 15 TO 20 SECONDS
45,000 FEET ................... 9 TO 15 SECONDS

NOTE:
PASSENGER MASKS DO NOT PROVIDE AN ADEQUATE O2
FLOW ABOVE FL250.

OPERATION IN RVSM AIRSPACE

IN ANY RVSM AIRSPACE, ATTEMPT TO GET A REVISED ATC
CLEARANCE BEFORE DEVIATING FROM THE ASSIGNED
ROUTE OR FLIGHT LEVEL, IF AT ALL POSSIBLE.
IF UNABLE TO MAINTAIN ASSIGNED FLIGHT LEVEL:
*PF = PILOT FLYING • INITIALLY MINIMIZE DESCENT RATE TO THE EXTENT
**PM = PILOT MONITORING OPERATIONALLY FEASIBLE.
• TURN WHILE DESCENDING TO ACQUIRE AND
MAINTAIN A TRACK LATERALLY SEPARATED BY 30
NM FROM THE ORIGINALLY ASSIGNED ROUTE.
• FOR THE SUBSEQUENT LEVEL FLIGHT, CHOOSE A
LEVEL WHICH DIFFERS FROM THOSE NORMALLY
USED BY 500 FEET.

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 HAWKER 400XP/BEECHJET 400A CLIENT GUIDE

UNUSUAL ATTITUDES For nose high recoveries, if you think of the

maneuver as being similar to a lazy eight or
Definition per FAA AC 61-27C: An unusual a wingover, you’ll find it easy to fly. Roll the
attitude is any unexpected or inadvertent shortest direction to 45° of bank, hold 1 “g,” and
airplane attitude, which is not normally required the nose will slice down to the horizon.
for instrument flight.
For a nose low recovery in a steep bank or
There are many scenarios that can lead to an inverted condition, it is imperative to quickly
unusual attitude. While an unusual attitude roll the airplane to an upright attitude. Use your
is an emergency condition warranting swift skypointer! The skypointer always shows the
corrective action, recovery is not difficult if we quickest way to upright.
follow a few basic steps.
As a general rule if there are no flags on the
There is one important difference between ADI, it is probably telling the truth. These are
swept-wing jets like the beechjet and the piston- 360° gyros on Beechjets and Hawkers and are
powered, straight wing airplanes most of us flew generally dependable. Cross-check and recover.
to earn our instrument ratings. In a swept-wing,
transport category jet both the instruments and
the aerodynamics are different. We have three
CAUTION
independent groups of instruments—pilot’s, In the event of a PFD failure, DO NOT
copilot’s, and standby. Turbofan engines, DELAY recovery to reach for EFIS
mounted high on the aft fuselage above and reversionary switch (ESC); consider
transfering control to the other pilot.
behind the wing, are prone to compressor stalls Recovery using primary instruments
at low indicated airspeeds and high power will be easier and faster than if using
settings, especially if we aggressively push the the standby instruments.
nose over. That type of recovery is also hard on
the engines that do not have zero or negative
Use the “RECOGNIZE—CONFIRM—RECOVER”
“g” fuel and oil systems. It also could slam the
sequence to handle an unusual attitude or an “upset”
passengers into the ceiling and launch glasses,
situation in flight.
dishes, laptops, etc. flying about the cabin.
RECOGNIZE: Observe the Primary Flight
SKY POINTER Instruments for clues.

CONFIRM: Cross-check the ADI with the other

instruments prior to initiating recovery.
AIRSPEED
TREND RECOVER: Perform the appropriate
recovery procedure.

INCLINOMETER

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INTENTIONALLY LEFT BLANK

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 HAWKER 400XP/BEECHJET 400A CLIENT GUIDE

BALKED LANDING/GO-AROUND
1. APPLY TAKEOFF RATED THRUST
2. DEPRESS G.A. BUTTON
3. ABOVE 100 KIAS - FLAPS 10°
4. ROTATE TO GO-AROUND ATTITUDE (10°)
5. POSITIVE RATE—GEAR UP, LIGHTS IN,
AFTER CLEARING RUNWAY YAW DAMP ON
1. AFTER LANDING CHECKLIST 6. ABOVE 400' AGL—FLAPS UP
7. POWER, AS REQUIRED
8. AFTER TAKEOFF CHECKLIST
9. CLIMB TO APPROPRIATE ALTITUDE
TOUCHDOWN AND ROLLOUT
1. WHEEL BRAKES—APPLY
2. THRUST REVERSERS—DEPLOY
3. SPEED BRAKES—EXTEND

BEFORE PATTERN LANDING ASSURED

1. SLOW TO 200 KIAS 1. CHECKLIST COMPLETE
2. THRUST LEVERS—IDLE AT 50' AGL
3. 30° FLAP VREF AT 50' AGL
4. YAW DAMP OFF AT 50' AGL

PATTERN ENTRY
1. SLOW TO 170 KIAS (63% N1)
2. FLAPS—10°
3. 140 KIAS (63% N1)

15 SEC

ABEAM NUMBERS
1. GEAR—DOWN
2. BEFORE LANDING CHECKS
3. MAINTAIN 140 KIAS

FINAL TURN
NOTE:
APPROACH CHECKLIST SHOULD BE COMPLETE 1. 65% N1
PRIOR TO ENTERING THE TRAFFIC AREA. VREF 2. MAX BANK—30°
SHOULD BE COMPUTED FOR 30° FLAP LANDING
CONFIGURATION AND SET IN THE VR POSITION
IN THE VSPEEDS .
TIP
CALCULATE LANDING VREF (SUBTRACT 4 KNOTS FROM THE
ORIGINAL VREF FOR EACH 1,000 LB. OF FUEL BURNED.
THIS IS CALCULATED VREF). ADD 22 KNOTS TO CALCULATED
VREF FOR VAC. ADD 10 KNOTS TO CALCULATED VREF FOR
THE FLAPS 10° CONFIGURATION.

EXAMPLE: VREF AT TAKEOFF WAS 116 KNOTS

FUEL BURN= 1,250 LB. (-5 KNOTS)
116 - 5 + 10 = 121 LANDING VREF (PUT IN VR POSITION)
111 + 22 = 133 VAC (PUT IN V2 POSITION)

Normal Landing

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CALL OUTS NOTES

BEFORE PATTERN
THE APPROACH CHECKLIST SHOULD BE A SILENT
CHECKLIST OR PER COMPANY S.O.P. EXCEPT FOR
PF “APPROACH CHECKLIST” THE SPEEDS AND APPROACH BRIEF. (THE PM READS
PM “APPROACH CHECKLIST COMPLETE” THE CHECKLIST SILENTLY; WHEN ALL ITEMS ARE
COMPLETED, THE PM WILL ANNOUNCE “APPROACH
CHECKLIST COMPLETE.”)

PATTERN ENTRY
PF “FLAPS 10”
PM “SPEED CHECKS, FLAPS SELECTED 10, INDICATING 10”

ABEAM NUMBERS
PF “GEAR DOWN”
PM “SPEED CHECKS, GEAR DOWN, LIGHTS ON, USING THE “GEAR DOWN” CUE LEADS TO THE FLOW. THE
IGNITIONS ON” LANDING CHECKLIST SHOULD BE DONE QUICKLY FROM
MEMORY AND CONFIRMED WITH THE CHECKLIST IN ORDER
PM “THREE GREEN, NO RED, VERIFY?”
FOR THE PM TO HELP SCAN FOR TRAFFIC AND MONITOR
PF “THREE GREEN NO RED” THE APPROACH.
PF “LANDING CHECKLIST”

FINAL TURN
PF “ FLAPS 30”
PM “SPEED CHECKS, FLAPS SELECTED 30, INDICATING 30”
PM “TURNING FINAL, LANDING CHECKS COMPLETE”
“VREF ±…”

LANDING ASSURED
PM “50 FEET”

BALKED LANDING/GO-AROUND
PF “GOING AROUND”
PF “SET TAKEOFF POWER”
PM “100 KNOTS”
PF “FLAPS 10” A BALKED LANDING PROCEDURE IS THE SAME AS AN
PM “POSITIVE RATE” APPROACH TO LANDING STALL RECOVERY. I.E., 100 KTS,
FLAPS 10, POSITIVE RATE GEAR UP, ETC.
PF “GEARUPLIGHTSINYAWDAMPON”
PM “400 FEET”
PF “FLAPS UP, SET MCT, AFTER
TAKEOFF CHECKLIST”

TOUCHDOWN AND ROLLOUT

PF “SPEED BRAKES”
PM “SIX LIGHTS”
PM “SIXTY KNOTS”

AFTER CLEARING RUNWAY

PF “AFTER LANDING CHECKLIST”

*PF = PILOT FLYING

**PM = PILOT MONITORING

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 HAWKER 400XP/BEECHJET 400A CLIENT GUIDE

NOTE:
ONE-ENGINE-INOPERATIVE APPROACH AND LANDING
CHECKLIST SHOULD BE COMPLETE UP TO (BUT NOT BALKED LANDING/GO-AROUND
INCLUDING) FLAPS 10° PRIOR TO ENTERING THE
TRAFFIC AREA. CONFIRM VSPEEDS AND SET 1. APPLY TAKEOFF RATED THRUST
APPROPRIATELY. 2. DEPRESS G.A. BUTTON
3. ABOVE 100 KIAS—FLAPS 10°
4. ROTATE TO GO-AROUND ATTITUDE (10°)
5. POSITIVE RATE—GEAR UP, LIGHTS IN,
AFTER CLEARING RUNWAY YAW DAMP ON
1. AFTER LANDING CHECKLIST 6. CLIMB AT VAC TO 400' AGL
7. FLAPS—UP (IF REQUIRED)
8. AFTER TAKEOFF CHECKLIST
9. CLIMB AT 140 KIAS TO 1,500' AGL
TOUCHDOWN AND ROLLOUT 10. AFTER 1,500' AGL—CLIMB AT 170 KIAS
1. WHEEL BRAKES—APPLY
2. THRUST REVERSER—DEPLOY
3. SPEED BRAKES—EXTEND

* FLAPS 10° RECOMMENDED

BEFORE PATTERN LANDING ASSURED

1. FLAPS—30°, IF DESIRED *
1. SLOW TO 200 KIAS
2. THRUST LEVER—IDLE AT 50' AGL
3. VREF FOR CONFIGURATION AT 50' AGL
4. YAW DAMP OFF AT 50' AGL

PATTERN ENTRY
1. POWER TO 85% N1
2. FLAPS—10°
3. SLOW TO 170 KIAS

15 SEC

ABEAM NUMBERS
1. GEAR—DOWN
2. CONTINUE CHECKLIST
3. SLOW 140 KIAS (MIN)

FINAL TURN
1. MAX BANK—30°
2. 65% N1
3. VREF + 10 KT
TIP

CALCULATE LANDING VREF AS USUAL. ADD 22 KNOTS TO THIS

NUMBER FOR VAC. ADJUST FOR THE LANDING CONFIGURATION.

EXAMPLE: VREF AT TAKEOFF WAS 116 KNOTS, LANDING FLAPS 10°.

FUEL BURN= 1,250 LB. (-5 KNOTS)
116 - 5 + 10 = 121 LANDING VREF (PUT IN VR POSITION)
111 + 22 = 133 VAC (PUT IN V2 POSITION)

THE THRUST REVERSER ON THE INOPERATIVE ENGINE MAY BE

DEPLOYED TO AID IN AERODYNAMIC BRAKING AND DIRECTIONAL
CONTROL.

Engine Out Landing

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 HAWKER 400XP/BEECHJET 400A CLIENT GUIDE

CALL OUTS NOTES

PATTERN ENTRY
PF* “SET POWER” (85%) THE ONE-ENGINE-INOPERATIVE APPROACH CHECKLIST
AND THE BRIEFING SHOULD BE DONE WELL BEFORE
PF “FLAPS 10”
ENTERING THE PATTERN TO ALLOW THE PM TO MONITOR
PM** “SPEED CHECKS, FLAPS SELECTED 10, THE APPROACH. THE PM WILL CALL DEVIATIONS IN BANK
INDICATING 10" OR PITCH AND ESPECIALLY AIRSPEED.

ABEAM NUMBERS
PF “GEAR DOWN”
PM “SPEED CHECKS, GEAR DOWN, THE TENDENCY ON A SINGLE-ENGINE APPROACH IS TO
PM “THREE GREEN, NO RED, VERIFY?” HAVE EXCESSIVE AIRSPEED.
PF “THREE GREEN NO RED”

LANDING ASSURED
PF “FLAPS 30”*** WHERE THE LANDING RUNWAY LENGTH IS ADEQUATE,
THE CREW SHOULD PLAN TO LAND FLAPS 10° TO AVOID
PM “VREF ±…”
ABRUPT PITCH CHANGES SINGLE-ENGINE AND IN CASE OF
PM “50 FEET” A MISSED APPROACH.

TOUCHDOWN AND ROLLOUT

PF “SPEED BRAKES”
PM “SIX LIGHTS”
PM “SIXTY KNOTS”

AFTER CLEARING RUNWAY

CAUTION
PF “AFTER LANDING CHECKLIST” A SUCCESSFUL SINGLE-ENGINE GO-
AROUND AFTER SELECTING FLAPS 30°
IS HIGHLY UNLIKELY.

STANDARDS:
*PF = PILOT FLYING
AIRSPEED ± 5 KNOTS
**PM = PILOT MONITORING
HEADING ± 5°
***FLAPS 10 RECOMMENDED
ALTITUDE ± 100 FEET

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 HAWKER 400XP/BEECHJET 400A CLIENT GUIDE

BALKED LANDING/GO-AROUND
1. APPLY TAKEOFF RATED THRUST
2. DEPRESS G.A. BUTTON
3. ROTATE TO GO-AROUND ATTITUDE (10°)
4. POSITIVE RATE—GEAR UP, LIGHTS IN,
YAW DAMP ON
AFTER CLEARING RUNWAY 5. CLIMB TO 400' AGL
1. AFTER LANDING CHECKLIST 6. POWER, AS REQUIRED
7. AFTER TAKEOFF CHECKLIST
8. CLIMB TO APPROPRIATE ALTITUDE
TOUCHDOWN AND ROLLOUT
1. WHEEL BRAKES—APPLY
2. THRUST REVERSERS—DEPLOY
3. SPEED BRAKES—EXTEND

BEFORE PATTERN LANDING ASSURED

1. SLOW TO 200 KIAS 1. CHECKLIST COMPLETE
2. THRUST LEVERS—IDLE AT 50' AGL
3. ZERO FLAP VREF AT 50' AGL
4. YAW DAMP OFF AT 50' AGL

PATTERN ENTRY
1. SLOW TO 170 KIAS (63% N1)

15 SEC

ABEAM NUMBERS
1. GEAR—DOWN
2. BEFORE LANDING CHECKS
3. SLOW TO 140 KIAS (MIN)

FINAL TURN
1. 45% N1
NOTE: 2. MAX BANK—30°
APPROACH AND LANDING CHECKLIST SHOULD BE
COMPLETE UP TO LANDING GEAR PRIOR TO
ENTERING THE TRAFFIC AREA. VREF SHOULD BE
COMPUTED FOR ZERO FLAP LANDING CONFIGURATION TIP
AND SET IN THE VR POSITION IN THE VSPEEDS.
CALCULATE LANDING VREF (SUBTRACT 4 KNOTS FROM THE
ORIGINAL VREF FOR EACH 1,000 LB. OF FUEL BURNED.
THIS IS CALCULATED VREF). ADD 22 KNOTS TO CALCULATED
VREF FOR VAC. ADD 20 KNOTS TO CALCULATED VREF FOR
THE FLAPS 0° CONFIGURATION.

EXAMPLE: VREF AT TAKEOFF WAS 116 KNOTS

FUEL BURN= 1,250 LB. (-5 KNOTS)
116 - 5 + 20 = 131 LANDING VREF (PUT IN VR POSITION)
111 + 22 = 133 VAC (PUT IN V2 POSITION)

Zero Flap Landing

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CALL OUTS NOTES

BEFORE PATTERN
THE FLAPS 10° LANDING CHECKLIST SHOULD BE
A CHALLENGE AND RESPONSE CHECKLIST. READ
PF* “ZERO FLAP APPROACH AND LANDING CHECKLIST”
VERBATIM TO ENSURE COMMUNICATION AND ACCURACY.
(SPEEDS AND PROCEDURE)

PATTERN ENTRY
PF “POWER 63%”
PM** “POWER 63%”

ABEAM NUMBERS
PF “GEAR DOWN”
PM “SPEED CHECKS, GEAR DOWN, LIGHTS ON, USING THE “GEAR DOWN” CUE LEADS TO THE FLOW. THE
IGNITIONS ON”
LANDING PORTION OF THE CHECKLIST SHOULD BE DONE
PM “THREE GREEN, NO RED, VERIFY?” QUICKLY IN ORDER FOR THE PM TO HELP SCAN FOR
TRAFFIC.
PF “THREE GREEN NO RED”
PF “LANDING CHECKLIST”

FINAL TURN
PF “POWER 45%”
PM “POWER 45%”

BALKED LANDING/GO-AROUND
PF “GOING AROUND”
PF “SET TAKEOFF POWER”
PM “100 KNOTS” THE LANDING SELECT SWITCH MAY BE PLACED IN THE
PF “FLAPS 10” 10° POSITION. THE CREW SHOULD BE AWARE THAT THIS
WOULD CAUSE THE GEAR WARNING HORN TO SOUND
PM “POSITIVE RATE” CONTINUOUSLY IF THE FLAPS ARE SELECTED TO 10° WITH
PF “GEARUPLIGHTSINYAWDAMPON” THE GEAR RETRACTED.
PM “400 FEET”
PF “FLAPS UP, SET MCT, AFTER TAKEOFF CHECKLIST”

LANDING ASSURED
PM “50 FEET”
PM “VREF ±…”

TOUCHDOWN AND ROLLOUT

PF “SPEED BRAKES”
PM “SIX LIGHTS”
PM “SIXTY KNOTS”

ABEAM NUMBERS
PF “AFTER LANDING CHECKLIST”

STANDARDS:
*PF = PILOT FLYING AIRSPEED ± 5 KNOTS
**PM = PILOT MONITORING HEADING ± 5°
ALTITUDE ± 100 FEET

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 HAWKER 400XP/BEECHJET 400A CLIENT GUIDE

BALKED LANDING/GO-AROUND
1. APPLY TAKEOFF RATED THRUST
2. DEPRESS G.A. BUTTON
3. ROTATE TO GO-AROUND ATTITUDE (10°)
4. POSITIVE RATE—GEAR UP, LIGHTS IN
5. ABOVE 400' AGL—FLAPS UP
6. POWER, AS REQUIRED
7. AFTER TAKEOFF CHECKLIST
8. CLIMB TO APPROPRIATE ALTITUDE
AFTER CLEARING RUNWAY
1. AFTER LANDING CHECKLIST

TOUCHDOWN AND ROLLOUT

1. WHEEL BRAKES—APPLY
2. THRUST REVERSERS—DEPLOY
3. SPEED BRAKES—EXTEND

LANDING ASSURED
BEFORE PATTERN
1. BEFORE LANDING CHECKLIST—
1. SLOW TO 200 KIAS IN COMPLETE
CLEAN CONFIGURATION 2. THRUST LEVERS—IDLE AT 50' AGL
3. 10° FLAP VREF AT 50' AGL
4. YAW DAMP OFF AT 50' AGL

PATTERN ENTRY
1. SLOW TO 170 KIAS (63% N1)
2. FLAPS—10°
3. 140 KIAS (63% N1)
15 SEC

ABEAM NUMBERS
1. GEAR—DOWN
2. BEFORE LANDING CHECKS
3. MAINTAIN 140 KIAS (MIN)

FINAL TURN
NOTE:
APPROACH CHECKLIST SHOULD BE COMPLETE 1. 55% N1
BEFORE ENTERING THE TRAFFIC AREA. 2. MAX BANK—30°
VREF SHOULD BE COMPUTED FOR A 10° FLAP
LANDING CONFIGURATION AND SET IN THE VR
POSITION ON THE VSPEEDS.
TIP

CALCULATE LANDING VREF (SUBTRACT 4 KNOTS FROM THE

ORIGINAL VREF FOR EACH 1,000 LB. OF FUEL BURNED.
THIS IS CALCULATED VREF). ADD 22 KNOTS TO CALCULATED
VREF FOR VAC. ADD 20 KNOTS TO CALCULATED VREF FOR
THE FLAPS 0° CONFIGURATION.

EXAMPLE: VREF AT TAKEOFF WAS 116 KNOTS

FUEL BURN= 1,250 LB. (-5 KNOTS)
116 - 5 + 20 = 131 LANDING VREF (PUT IN VR POSITION)
111 + 22 = 133 VAC (PUT IN V2 POSITION)

10° Flap Landing

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 HAWKER 400XP/BEECHJET 400A CLIENT GUIDE

CALL OUTS NOTES

BEFORE PATTERN
THE FLAPS 10° LANDING CHECKLIST SHOULD BE
A CHALLENGE AND RESPONSE CHECKLIST. READ
PF* “FLAPS 10 APPROACH AND LANDING CHECKLIST”
VERBATIM TO ENSURE COMMUNICATION AND ACCURACY.
(SPEEDS AND PROCEDURE)

PATTERN ENTRY
PF “POWER 63%”
PM “POWER 63%”

ABEAM NUMBERS
PF “GEAR DOWN”
PM** “SPEED CHECKS, GEAR DOWN, LIGHTS ON, USING THE “GEAR DOWN” CUE LEADS TO THE FLOW.
IGNITIONS ON”
THE LANDING PORTION OF THE CHECKLIST SHOULD BE
PM “THREE GREEN, NO RED, VERIFY?” DONE QUICKLY IN ORDER FOR THE PM TO HELP SCAN
FOR TRAFFIC.
PF “THREE GREEN NO RED”
PF “LANDING CHECKLIST”

FINAL TURN
PF “POWER 55%”
PM “POWER 55%”
PM “LANDING CHECKLIST COMPLETE”

BALKED LANDING/GO-AROUND
PF “GOING AROUND”
PF “SET TAKEOFF POWER”
PM “100 KNOTS” THE LANDING SELECT SWITCH MAY BE PLACED IN THE
PF “FLAPS 10” 10° POSITION. THE CREW SHOULD BE AWARE THAT THIS
WOULD CAUSE THE GEAR WARNING HORN TO SOUND
PM “POSITIVE RATE” CONTINUOUSLY IF THE FLAPS ARE SELECTED TO 10° WITH
PF “GEARUPLIGHTSINYAWDAMPON” THE GEAR RETRACTED.
PM “400 FEET”
PF “FLAPS UP, SET MCT, AFTER TAKEOFF CHECKLIST”

LANDING ASSURED
PM “50 FEET”
PM “VREF ±…”

TOUCHDOWN AND ROLLOUT

PF “SPEED BRAKES”
PM “SIX LIGHTS”
PM “SIXTY KNOTS”

ABEAM NUMBERS
PF “AFTER LANDING CHECKLIST”

STANDARDS:
*PF = PILOT FLYING AIRSPEED ± 5 KNOTS
**PM = PILOT MONITORING HEADING ± 5°
ALTITUDE ± 100 FEET

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 HAWKER 400XP/BEECHJET 400A CLIENT GUIDE

NOTE:
PRIOR TO INITIATING THE APPROACH, SLOW THE AIRPLANE
TO 200 KIAS IN THE CLEAN CONFIGURATION. COMPLETE
THE APPROACH CHECKLIST UP TO FLAPS 10°, CONFIRM
V-SPEEDS AND SET APPROPRIATELY. THE APPROACH CHART
SHOULD BE REVIEWED AND THE APPROACH BRIEFING
SHOULD BE COMPLETED.
PROCEDURE TURN OUTBOUND
1. FLAPS—10°
2. AIRSPEED—SLOW TO
140 KIAS (MIN) (63% N1)

MARKER OUTBOUND
1. AIRSPEED—170 KIAS (65% N1)

PRIOR TO FIX
MISSED APPROACH 1. AIRSPEED—140 KIAS
2. ONE DOT FLY UP—GEAR DOWN
1. APPLY TAKEOFF RATED THRUST 3. LANDING CHECKLIST
2. DEPRESS G.A. BUTTON
3. ROTATE TO GO-AROUND ATTITUDE (10°)
4. ABOVE 100 KIAS—FLAPS 10°
5. POSITIVE RATE—GEAR UP, LIGHTS IN,
YAW DAMP ON
6. ABOVE 400' AGL—FLAPS UP GLIDESLOPE INTERCEPT
7. POWER, AS REQUIRED
8. AFTER TAKEOFF CHECKLIST 1. FLAPS—30°
9. CLIMB TO APPROPRIATE ALTITUDE 2. AIRSPEED—SLOWING TO
VREF (65% N1)

AT 50' AGL
1. AIRSPEED—VREF
2. THRUST LEVERS—IDLE AT 50' AGL
3. YAW DAMP—OFF AT 50' AGL

TOUCHDOWN AND ROLLOUT

1. WHEEL BRAKES—APPLY
2. THRUST REVERSERS—DEPLOY
3. SPEED BRAKES—EXTEND

ILS Approach and Missed Approach

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 HAWKER 400XP/BEECHJET 400A CLIENT GUIDE

CALL OUTS NOTES

PROCEDURE TURN
PF* “FLAPS 10”
PM** “SPEED CHECKS, FLAPS 10”

PRIOR TO FIX
PF “GEAR DOWN, LANDING CHECKS”
PM “SPEED CHECKS GEAR DOWN LIGHTS ON,
IGNITIONS ON”

GLIDESLOPE INTERCEPT
THE PM CALLS THE DISTANCE TO MINIMUMS, NOT “TO
PF "FLAPS 30" GO” OR “LEFT” ETC. “1000’, 500’, 300’, 100’, MINIMUMS, NO
PM “SPEED CHECKS, FLAPS 30" RUNWAY OR RUNWAY IN SIGHT.” PM SHOULD ANNOUNCE
DEVIATIONS IN GS OR LOC.

THRESHOLD
PM “50 FEET”
PM “VREF ±…”

TOUCHDOWN AND ROLLOUT

PF “SPEED BRAKES”
PM “SIX LIGHTS”
PM “SIXTY KNOTS”

MISSED APPROACH
PF “MISSED APPROACH”
PM “100 KNOTS”
PF “FLAPS 10” IN THE EVENT OF A MISSED APPROACH, THE NONFLYING
PILOT HAS A LARGE AMOUNT OF IMPORTANT TASKS TO
PM “FLAPS 10”
CONDUCT RAPIDLY. ANNOUNCE THE MISS “MINIMUMS, NO
PM “POSITIVE RATE” RUNWAY,” CALL SPEEDS, CALL POSITIVE RATE, ADJUST
PF “GEAR UP” THE POWER WHEN THE PF CALLS FOR IT, AND MONITOR
THE AIRCRAFT FLIGHT PATH FOR THE MISSED APPROACH.
PM “400 FEET”
PF “FLAPS UP, AFTER TAKEOFF CHECKLIST”

STANDARDS:
AIRSPEED ± 5 KNOTS
*PF = PILOT FLYING HEADING ± 5°
**PM = PILOT MONITORING NO MORE THAN ONE-QUARTER SCALE DEFLECTION OF
THE LOCALIZER OR GLIDESLOPE.
AVOID DESCENT BELOW DH BEFORE TRANSITIONING TO
EITHER A MISSED APPROACH OR A LANDING.

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 HAWKER 400XP/BEECHJET 400A CLIENT GUIDE

NOTE:
PRIOR TO INITIATING THE APPROACH, SLOW THE AIRPLANE
TO 200 KIAS IN THE CLEAN CONFIGURATION. COMPLETE
THE ONE-ENGINE-INOPERATIVE APPROACH AND LANDING
CHECKLIST UP TO FLAPS 10°, CONFIRM V-SPEEDS AND SET
APPROPRIATELY. THE APPROACH CHART SHOULD BE
REVIEWED AND THE APPROACH BRIEFING SHOULD BE
COMPLETED.
PROCEDURE TURN OUTBOUND
1. FLAPS—10°
2. AIRSPEED—SLOW TO
140 KIAS (MIN) (85% N1)

MARKER OUTBOUND
1. AIRSPEED—170 KIAS (85% N1)

PRIOR TO FIX
MISSED APPROACH
1. AIRSPEED—140 KIAS (MIN)
1. APPLY TAKEOFF RATED THRUST 2. ONE DOT FLY UP—GEAR DOWN
2. DEPRESS G.A. BUTTON 3. LANDING CHECKLIST
3. ABOVE 100 KIAS—FLAPS 10°
4. ROTATE TO GO-AROUND ATTITUDE (10°)
5. POSITIVE RATE—GEAR UP, LIGHTS IN,
YAW DAMP ON
6. CLIMB AT VAC TO 400' AGL
7. FLAPS—UP GLIDESLOPE INTERCEPT
8. AFTER TAKEOFF CHECKLIST
9. CLIMB AT 140 KIAS TO 1,500' AGL 1. AIRSPEED—SLOWING TO
10. AFTER 1,500' AGL, CLIMB AT 170 KIAS VREF + 10 KT (65% N1)

LANDING ASSURED
1. FLAPS—30° *
2. AIRSPEED—VREF FOR CONFIGURATION

AT 50' AGL
1. THRUST LEVER—IDLE
2. YAW DAMP—OFF
* WHEN LANDING ASSURED

** THE THRUST REVERSER ON THE INOPERATIVE

TOUCHDOWN AND ROLLOUT ENGINE MAY BE DEPLOYED TO AID IN AERODYNAMIC
BRAKING AND DIRECTIONAL CONTROL.
1. WHEEL BRAKES—APPLY
2. THRUST REVERSER—DEPLOY **
3. SPEED BRAKES—EXTEND

Single Engine and ILS Approach and Missed Approach

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 HAWKER 400XP/BEECHJET 400A CLIENT GUIDE

CALL OUTS NOTES

PROCEDURE TURN

WARNING
PF* “FLAPS 10”
PM** “SPEED CHECKS, FLAPS 10” A SUCCESSFUL SINGLE-ENGINE GO-
AROUND AFTER SELECTING FLAPS 30°
IS HIGHLY UNLIKELY.

PRIOR TO FIX
PF “GEAR DOWN, LANDING CHECKS”
PM “SPEED CHECKS GEAR DOWN LIGHTS ON,
IGNITIONS ON”

GLIDESLOPE INTERCEPT
THE PM CALLS THE DISTANCE TO MINIMUMS, NOT “TO
GO” OR “LEFT” ETC. “1000’, 500’, 300’, 100’, MINIMUMS, NO
PM “REF ± …”
RUNWAY OR RUNWAY IN SIGHT.” PM SHOULD ANNOUNCE
DEVIATIONS IN GS OR LOC.

LANDING ASSURED
PF “FLAPS 30”***
PM “VREF ±…”

TOUCHDOWN AND ROLLOUT

PF “SPEED BRAKES”
PM “THREE LIGHTS”
PM “SIXTY KNOTS”

MISSED APPROACH
PF “MISSED APPROACH”
PM “100 KNOTS”
IN THE EVENT OF A MISSED APPROACH, THE NONFLYING
PF “FLAPS 0 OR 10” (DEPENDING ON CONFIGURATION) PILOT HAS A LARGE AMOUNT OF CRITICAL TASKS TO
PM “FLAPS SELECTED …” CONDUCT RAPIDLY. ANNOUNCE THE MISS “MINIMUMS, NO
RUNWAY,” CALL SPEEDS, CALL POSITIVE RATE, ADJUST
PM “POSITIVE RATE”
THE POWER WHEN THE PF CALLS FOR IT, MONITOR THE
PF “GEAR UP” AIRCRAFT FLIGHT PATH FOR THE MISSED APPROACH, AND
PM “400 FEET” MONITOR AIRCRAFT CONTROL.

PF “FLAPS UP, AFTER TAKEOFF CHECKLIST”

STANDARDS:
AIRSPEED ± 5 KNOTS
*PF = PILOT FLYING HEADING ± 5°
**PM = PILOT MONITORING NO MORE THAN ONE-QUARTER SCALE DEFLECTION OF
***FLAPS 10° RECOMMENDED THE LOCALIZER OR GLIDESLOPE.
AVOID DESCENT BELOW DH BEFORE TRANSITIONING TO A
MISSED APPROACH OR A LANDING.

Revision 0 FOR TRAINING PURPOSES ONLY 5-49

 HAWKER 400XP/BEECHJET 400A CLIENT GUIDE

NOTE:
PRIOR TO INITIATING THE APPROACH, SLOW THE AIRPLANE TO
200 KIAS IN THE CLEAN CONFIGURATION. COMPLETE THE
APPROACH CHECKLIST UP TO FLAPS 10°, CONFIRM V-SPEEDS AND
SET APPROPRIATELY. THE APPROACH CHART SHOULD BE
REVIEWED AND THE APPROACH BRIEFING SHOULD BE COMPLETED.

PROCEDURE TURN
FAF OUTBOUND OUTBOUND
1. SLOW TO 170 KIAS 1. FLAPS—10°
2. 65% N1 2. AIRSPEED—SLOWING
TO 140 KIAS (MIN) (65% N1)

PRIOR TO THE FIX

1. AIRSPEED—140 KIAS (MIN)
MISSED APPROACH 2. ONE MILE FROM FAF—GEAR DOWN
1. APPLY TAKEOFF RATED THRUST 3. LANDING CHECKLIST
2. DEPRESS G.A. BUTTON
3. ROTATE TO GO-AROUND ATTITUDE (10°)
4. 100 KIAS—FLAPS 10°
AT THE FINAL FIX
5. POSITIVE RATE—GEAR UP, LIGHTS IN, 1. FLAPS—30°
YAW DAMP ON 2. AIRSPEED—SLOWING TO VREF
6. ABOVE 400' AGL—FLAPS UP 3. START TIME (IF REQUIRED)
7. POWER, AS REQUIRED
8. AFTER TAKEOFF CHECKLIST
9. CLIMB TO APPROPRIATE ALTITUDE
AT MDA
1. LEVEL OFF
2. MAINTAIN VREF (75% N1)

MINIMUMS AT VDP (RWY IN SIGHT)

1. CONTINUE DESCENT
2. 60% N1

AT MAP (RWY NOT IN SIGHT)

1. EXECUTE MISSED APPROACH

AT THRESHOLD
1. AIRSPEED—VREF
2. THRUST LEVERS—IDLE
3. YAW DAMP—OFF

TOUCHDOWN AND ROLLOUT

1. WHEEL BRAKES—APPLY
2. THRUST REVERSERS—DEPLOY
3. SPEED BRAKES—EXTEND

Non-Precision Approach and Missed Approach

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 HAWKER 400XP/BEECHJET 400A CLIENT GUIDE

CALL OUTS NOTES

PROCEDURE TURN OUTBOUND
PF* “FLAPS 10”
PM** “SPEED CHECKS, FLAPS 10”

PRIOR TO THE FIX

PF “GEAR DOWN, BEFORE LANDING CHECKS"
PM “SPEED CHECKS GEAR DOWN, LIGHTS ON, IGNITION ON"

AT THE FINAL FIX

PF “ FLAPS 30”
PF “START TIME”
PM “REF ± …”

AT MDA
THE PM CALLS THE DISTANCE TO MINIMUMS, NOT “TO
PM “MINIMUMS” GO” OR “LEFT” ETC. “1000’, 500’, 300’, 100’, MINIMUMS, NO
PM “VREF ±…” RUNWAY OR RUNWAY IN SIGHT.” PM SHOULD ANNOUNCE
DEVIATIONS IN GS OR LOC.

AT VDP RUNWAY IN SIGHT

PM “RUNWAY IN SIGHT”

AT MAP RUNWAY NOT IN SIGHT

PM “RUNWAY NOT IN SIGHT, MISSED APPROACH”
PM “100 KNOTS” IN THE EVENT OF A MISSED APPROACH, THE NONFLYING
PILOT HAS A LARGE AMOUNT OF CRITICAL TASKS TO
PF “FLAPS 10” CONDUCT RAPIDLY. ANNOUNCE THE MISS “MINIMUMS, NO
PM “POSITIVE RATE” RUNWAY,” CALL SPEEDS, CALL POSITIVE RATE, ADJUST
PF “GEAR UP” THE POWER WHEN THE PF CALLS FOR IT, MONITOR THE
AIRCRAFT FLIGHT PATH FOR THE MISSED APPROACH, AND
PM “400 FEET” MONITOR AIRCRAFT CONTROL.
PF “FLAPS UP, AFTER TAKEOFF CHECKLIST”

AT THRESHOLD
PM “50 FEET”
PM “VREF ± …”

TOUCHDOWN AND ROLLOUT

PF “SPEEDBRAKES”
PM “SIX LIGHTS”
PM “SIXTY KNOTS”

STANDARDS:
*PF = PILOT FLYING AIRSPEED ± 5 KNOTS
**PM = PILOT MONITORING ALTITUDE - 0' + 100'
BANK ANGLE NOT TO EXCEED 30˚

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 HAWKER 400XP/BEECHJET 400A CLIENT GUIDE

NOTE:
PRIOR TO INITIATING THE APPROACH, SLOW THE AIRPLANE TO
200 KIAS IN THE CLEAN CONFIGURATION. COMPLETE THE ONE-
ENGINE-INOPERATIVE APPROACH AND LANDING CHECKLIST UP
TO FLAPS 10° BEFORE STARTING THE APPROACH. CONFIRM
V-SPEEDS AND SET APPROPRIATELY. THE APPROACH CHART
SHOULD BE REVIEWED, AND THE APPROACH BRIEFING SHOULD
BE COMPLETED.

PROCEDURE TURN
FAF OUTBOUND OUTBOUND
1. SLOW TO 170 KIAS 1. FLAPS—10°
2. 85% N1 2. AIRSPEED—SLOWING TO
140 KIAS (MIN) (85% N1)

PRIOR TO THE FIX

1. AIRSPEED—140 KIAS (MIN)
MISSED APPROACH 2. ONE MILE FROM FAF—GEAR DOWN
1. APPLY TAKEOFF RATED THRUST 3. LANDING CHECKLIST
2. DEPRESS G.A. BUTTON
3. ABOVE 100 KIAS—FLAPS 10°
4. ROTATE TO GO-AROUND ATTITUDE (10°)
AT THE FINAL FIX
5. POSITIVE RATE—GEAR UP, LIGHTS IN, 1. AIRSPEED—SLOWING TO
YAW DAMP ON VREF + 10 KT (65% N1)
6. CLIMB AT VAC TO 400' AGL 2. START TIME (IF REQUIRED)
7. FLAPS—UP
8. CLIMB AT 140 KIAS TO 1,500' AGL
9. AFTER TAKEOFF CHECKLIST
AT MDA
10 AFTER 1,500' AGL, CLIMB AT 170 KIAS 1. LEVEL OFF
2. MAINTAIN VREF + 10 KT (85% N1)

MINIMUMS
AT VDP (RWY IN SIGHT)
1. CONTINUE DESCENT

AT MAP (RWY NOT IN SIGHT)

1. EXECUTE MISSED APPROACH

LANDING ASSURED
1. FLAPS—30° *
2. AIRSPEED—VREF FOR CONFIGURATION
3. THRUST LEVER—IDLE AT 50' AGL
4. YAW DAMP—OFF AT 50' AGL

TOUCHDOWN AND ROLLOUT * WHEN LANDING ASSURED

1. WHEEL BRAKES—APPLY
2. THRUST REVERSER—DEPLOY ** ** THE THRUST REVERSER ON THE INOPERATIVE
3. SPEED BRAKES—EXTEND ENGINE MAY BE DEPLOYED TO AID IN AERODYNAMIC
BRAKING AND DIRECTIONAL CONTROL.

Single Engine Non-Precision Approach and Missed Approach

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 HAWKER 400XP/BEECHJET 400A CLIENT GUIDE

CALL OUTS NOTES

PROCEDURE TURN OUTBOUND
PF* “FLAPS 10”
PM** “SPEED CHECKS, FLAPS 10”

PRIOR TO THE FIX

PF “GEAR DOWN, BEFORE LANDING CHECKLIST”
PM “SPEED CHECKS GEAR DOWN LIGHTS ON,
IGNITIONS ON”

AT THE FINAL FIX

WARNING
PM “REF ± …”***
A SUCCESSFUL SINGLE-ENGINE GO-
PF “START TIME” (IF REQUIRED)
AROUND AFTER SELECTING FLAPS 30°
IS HIGHLY UNLIKELY.

AT MDA
THE PM CALLS THE DISTANCE TO MINIMUMS, NOT “TO
PM “RUNWAY IN SIGHT…O’CLOCK” GO” OR “LEFT” ETC. “1000’, 500’, 300’, 100’, MINIMUMS, NO
PF “LANDING” RUNWAY OR RUNWAY IN SIGHT.” PM SHOULD ANNOUNCE
DEVIATIONS IN GS OR LOC.

AT VDP (RUNWAY IN SIGHT)

PM “RUNWAY IN SIGHT…O’CLOCK”
PF “LANDING”

AT MAP RUNWAY NOT IN SIGHT

PM “NO RUNWAY, MISSED APPROACH” IN THE EVENT OF A MISSED APPROACH, THE NONFLYING
PILOT HAS A LARGE AMOUNT OF CRITICAL TASKS TO
PM “POSITIVE RATE” CONDUCT RAPIDLY. ANNOUNCE THE MISS “MINIMUMS, NO
PF “GEAR UP” RUNWAY,” CALL SPEEDS, CALL POSITIVE RATE, ADJUST
THE POWER WHEN THE PF CALLS FOR IT, MONITOR THE
PM “400 FEET”
AIRCRAFT FLIGHT PATH FOR THE MISSED APPROACH AND
PF “FLAPS UP, AFTER TAKEOFF CHECKLIST” MONITOR AIRCRAFT CONTROL.

LANDING ASSURED
PM “50 FEET”
PM “VREF ± …”

TOUCHDOWN AND ROLLOUT

PF “SPEEDBRAKES”
PM “THREE LIGHTS”
PM “SIXTY KNOTS”

STANDARDS:
*PF = PILOT FLYING
AIRSPEED ± 5 KNOTS
**PM = PILOT MONITORING
ALTITUDE – 0’ + 100’
***REF +10
BANK ANGLE NOT TO EXCEED 30°.

Revision 0 FOR TRAINING PURPOSES ONLY 5-53

 HAWKER 400XP/BEECHJET 400A CLIENT GUIDE

PROCEDURE TURN OUTBOUND

1. FLAPS 10°
PRIOR TO FINAL FIX 2. AIRSPEED—SLOWING TO
140 KIAS (MIN) (65% N1)
1. APPROACH CHECKLIST—COMPLETE
2. VREF SET

FINAL APPROACH
RUNWAY IN SIGHT
FIX INBOUND
1. BEGIN 30° TURN APPROXIMATELY 1. FLAPS 20°
ONE MILE PRIOR TO RUNWAY 2. GEAR DOWN
2. MAXIMUM BANK ANGLE—30° 3. AIRSPEED—140 KIAS
3. MAINTAIN CIRCLING MINIMUMS 4. DESCEND TO CIRCLING
MINIMUMS

THRESHOLD
AFTER CLEARING TOUCHDOWN AND ROLLOUT
1. AIRSPEED—VREF
RUNWAY 1. WHEEL BRAKES—APPLY 2. THRUST LEVERS—IDLE AT 50' AGL
1. AFTER LANDING 2. THRUST REVERSERS—DEPLOY 3. YAW DAMP—OFF AT 50' AGL
CHECKLIST 3. SPEED BRAKES—EXTEND

TURN TO FINAL
1. ADJUST BANK ANGLE AS
15 SEC NECESSARY (30° MAX)
(MAXIMUM DISTANCE 2. BEGIN DESCENT AT A POSITION
FOR CATEGORY C) FROM WHICH TO MAKE A
NORMAL LANDING
3. 1,000 FPM MAXIMUM DESCENT
RATE
NOTE:
KEEP RUNWAY IN SIGHT
WHILE CIRCLING
FINAL
1. FLAPS—30°
15 SEC 2. SLOW TO VREF

ROLLOUT
1. BEGIN TIMING UPON COMPLETION
OF ROLLOUT (WINGS LEVEL)
2. MAINTAIN 140 KIAS (MAX)
3. MAINTAIN CIRCLING MINIMUMS

BASE LEG
MISSED APPROACH 1. AFTER 15 SECONDS, TURN ON
IF THE AIRCRAFT ENCOUNTERS IFR WHILE TO BASE LEG
CIRCLING, THE MISSED APPROACH SHOULD 2. MAXIMUM BANK ANGLE—30°
BE A CLIMBING TURN OVER THE CENTER OF 3. MAINTAIN CIRCLING MINIMUMS
THE AERODROME, RE-INTERCEPTING THE
ORIGINAL APPROACH COURSE, AND FLYING
THE MISSED APPROACH.

Circling Approach

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 HAWKER 400XP/BEECHJET 400A CLIENT GUIDE

CALL OUTS NOTES

PRIOR TO THE FINAL FIX

PF* “FLAPS 10, APPROACH CHECKLIST”

CAUTION
PM** “SPEED CHECKS, FLAPS SELECTED 10, THE CIRCLING APPROACH IS
INDICATING 10" CONSIDERED TO BE THE MOST
DANGEROUS TYPE OF APPROACH.

FINAL APPROACH FIX INBOUND

PF "FLAPS 20"
PM “SPEED CHECKS, FLAPS 20 INDICATING 20"
PF “GEAR DOWN, BEFORE LANDING CHECKLIST”
PM “SPEED CHECKS GEAR DOWN LIGHTS ON,
IGNITIONS ON”

RUNWAY IN SIGHT BEGIN TURN

PM “RUNWAY IN SIGHT”
PF “SET HEADING BUG”

ROLLOUT
PF “START TIME”

BASE LEG
PM “TIME, LOOKING FOR THE RUNWAY”
PM “RUNWAY IN SIGHT”
PF “I’M OUTSIDE”
PM “I’M INSIDE”

TURN TO FINAL
PF “LEAVING MINIMUMS"

FINAL

WARNING
PF “FLAPS 30”
PM “SPEED CHECKS, FLAPS 30” ONCE YOU DESCEND BELOW CIRCLING
MINIMUMS, YOU ARE ON A VISUAL
PM “REF ±…”“SINKING …(FPM)” APPROACH, AND ARE NOT GUARANTEED
ANY OBSTACLE CLEARANCE.

THRESHOLD
PM “50 FEET” ESPECIALLY DURING A CIRCLE, THE PM NEEDS TO
PM “VREF ± …” MONITOR AIRSPEED, ALTITUDE AND BANK ANGLE.

TOUCHDOWN AND ROLLOUT

PF “SPEEDBRAKES”
PM “SIX LIGHTS”
PM “SIXTY KNOTS”

STANDARDS:
*PF = PILOT FLYING AIRSPEED ± 5 KNOTS
**PM = PILOT MONITORING ALTITUDE – 0’ + 100’
BANK ANGLE NOT TO EXCEED 30°

Revision 0 FOR TRAINING PURPOSES ONLY 5-55

 HAWKER 400XP/BEECHJET 400A CLIENT GUIDE

NOTES

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 HAWKER 400XP/BEECHJET 400A CLIENT GUIDE

AMS-5000 MODE SELECT PANEL

VERTICAL MODES
VS
Used for “constant rate” climbs or descents. The
FD/AP are synched to the current vertical speed.
The VS knob and the PITCH SYNC button on
the yoke may be used to adjust the target VS.

LVL CHG
LATERAL MODES
Used for “constant speed” climbs or descents.
HDG The FD/AP are synched to the current IAS. The
IAS knob and the PITCH SYNC button on the
Commands the airplane to turn to the heading set
yoke may be used to adjust the target IAS.
with the HDG knob on the Course Heading Panel.
ALT
1/2 BANK
Commands the FD/AP to go into altitude hold
Commands one-half the maximum commanded mode. The PITCH SYNC button on the yoke
roll angle. Automatically comes on climbing may be used to adjust the target ALT.
through 18,500; You may overshoot desired
courses when using 1/2 BANK. NOTE
When you dial a new altitude into the
APPR preselector after you have captured an
altitude, the FD goes into ALT as a pro-
Arms the selected approach. For an FMS or tective feature.
localizer-based approach, this will automatically
capture the approach course and navigation source VNAV
(FMS or LOC) when capture conditions are met.
Enables VGP mode of the VNAV function. Commands vertical navigation mode (VNAV).
When the FMS computed VNAV path is
NAV captured, VPATH is annunicated for enroute
descents; VGP is annunciated only on the final
Couples the active NAV source and course to approach glide path segment of approaches
the autopilot. If not in position to immediately when the approach has been armed.
capture the course, NAV arms and the autopilot/
FD remain in HDG or ROLL until course SPEED
intercept and capture. Switches the “speed bug” between IAS or
Mach. Enables the pilot to “bug” a target Mach
speed— particularly useful for holding constant
Mach in LVL CHG mode.

FD OFF
Turns the flight director off. Removes all steering
and mode information from the PFD.
Revision 0 FOR TRAINING PURPOSES ONLY 5-57
 HAWKER 400XP/BEECHJET 400A CLIENT GUIDE

NOTES

5-58 FOR TRAINING PURPOSES ONLY Revision 0

 TRIM CHECK

PITCH TRIM
CONTINUITY CHECK
1 PF 2 PM
—PRESS HAT ONLY —PRESS HAT ONLY
—VERIFY NO PITCH/ROLL —VERIFY NO PITCH/ROLL
—RELEASE AT HORN (5 SEC) —RELEASE AT HORN (5 SEC)
3 PF 4 PM
—PUSH BARREL NOSE UP —PUSH BARREL NOSE DOWN
—VERIFY NO PITCH/ROLL —VERIFY NO PITCH/ROLL
—RELEASE AT HORN (5 SEC) —RELEASE AT HORN (5 SEC)
5 PF 6 PM
—PUSH BARREL LEFT & RIGHT —PUSH BARREL LEFT & RIGHT
—VERIFY NO PITCH/ROLL —VERIFY NO PITCH/ROLL
—NO HORN —NO HORN

PITCH TRIM TEST

1 PF 2 PM
Trim Check Card PF ......TRIM NOSE UP PM.....TRIM NOSE DOWN
PM PF
PM.....INTERRUPT PF ......INTERRUPT
Tearout Page —VERIFY TRIM STOPS —VERIFY TRIM STOPS

3 PF PM
PF ......TRIM NOSE DOWN
PM.....PITCH TRIM DISCONNECT
—VERIFY TRIM STOPS

4 PF PF PF
PF ......PITCH TRIM DISCONNECT TO EMER
PF ......PITCH TRIM EMERGENCY TO N. UP
PF ......PITCH TRIM EMERGENCY TO N. DN
—VERIFY TRIM ACTION

5 PF PF PF ......RETURN PITCH TRIM

EMERGENCY TO NORMAL
PF ......TRIM NOSE UP
PF ......PUSH SPEED TEST
—VERIFY TRIM RATE SLOWS

Continued on Next Page

FOR TRAINING PURPOSES ONLY

Revision 0 5-59 FOR TRAINING PURPOSES ONLY Revision 0
 ROLL TRIM
1 2
PM PF
PF PM.....TRIM RIGHT PM PF ......TRIM LEFT
PF ......INTERRUPT PM.....INTERRUPT
—VERIFY TRIM STOPS —VERIFY TRIM STOPS

3 PF 4 PF
PF PF ......TRIM RIGHT
PF ......RETURN ROLL TRIM
PF ......DISCONNECT
DISCONNECT TO NORMAL
—VERIFY TRIM STOPS

RUDDER TRIM
CONTINUITY CHECK
1 PF
—PUSH RUDDER
TRIM SWITCH
—VERIFY NO RUDDER TRIM
2 PF 3 PF
—TWIST RUDDER TRIM —TWIST RUDDER TRIM Trim Check Card
SWITCH LEFT SWITCH RIGHT
—VERIFY NO RUDDER TRIM —VERIFY NO RUDDER TRIM
Tearout Page
RUDDER TRIM TEST
1 PF 2 PF
PM PF ......TRIM LEFT PF PF ......TRIM RIGHT
PM.....INTERRUPT PF ......INTERRUPT
—VERIFY TRIM STOPS —VERIFY TRIM STOPS

3 PM PF ......TRIM 4
PF PF OR PM
LEFT OR RIGHT
—RETURN RUDDER
PM.....RUDDER TRIM
TRIM DISCONNECT
DISCONNECT
TO NORMAL
—VERIFY TRIM STOPS

SET ALL TRIMS FOR TAKEOFF

FOR TRAINING PURPOSES ONLY

FOR TRAINING PURPOSES ONLY

5-60 Revision 0
Revision 0