2. A DETRESFA ends when the:
(a) Aircraft successfully lands; or
(b) RCC advises of a successful rescue; or
(c) RCC advises of termination of SAR
activities. Cancel the DETRESFA by a message
addressed to the same stations as the DETRESFA
message.
i. A separate chronological record should be kept
on each ALERFA and DETRESFA together with a
chart which displays the projected route of the
aircraft, position reports received, route of
interceptor aircraft, and other pertinent information.
10-6-4. INFLIGHT CONTINGENCIES
a. If an aircraft over water requests weather, sea
conditions, ditching information, and/or assistance
from surface vessels, or if the controller feels that this
information may be necessary for aircraft safety, it
should be requested from the RCC. Also, an
appropriate AMVER SURPIC should be asked for if
requested by the aircraft or deemed beneficial by
control personnel.
NOTE-
The AMVER Center can deliver, in a matter of minutes, a
SURPIC of vessels in the area of a SAR incident, including
their predicted positions and their characteristics.
JO 7110.65S 2/14/08
10-6-3
Oceanic Emergency Procedures
b. In all cases of aircraft ditching, the airspace
required for SAR operations shall be determined by
the RCC. The ACC shall block that airspace until the
RCC advises the airspace is no longer required. An
International Notice to Airmen (NOTAM) shall be
issued describing the airspace affected.
c. The following actions will be taken in the event
an aircraft must make an emergency descent:
1. In the event an aircraft requests an emergency
descent:
(a) Issue a clearance to the requested altitude
if approved separation can be provided.
(b) Advise the aircraft of the traffic, and
request its intentions if traffic prevents an
unrestricted descent.
PHRASEOLOGY-
ATC ADVISES (aircraft identification) UNABLE TO
APPROVE UNRESTRICTED DESCENT.
TRAFFIC (traffic information).
REQUEST INTENTIONS.
2. In the event an aircraft is making or will make
an emergency descent without a clearance:
(a) Advise other aircraft of the emergency
descent.
PHRASEOLOGY-
ATC ADVISES (aircraft identification/all aircraft) BE
ALERT FOR EMERGENCY DESCENT IN THE VICINITY
OF (latitude/longitude) FROM (altitude/FL) TO
(altitude/FL).
(b) Advise other aircraft when the emergency
descent is complete.
PHRASEOLOGY(Aircraft identification/all aircraft) EMERGENCY
DESCENT AT (location) COMPLETED.
3. Upon notification that an aircraft is making an
emergency descent through other traffic, take action
immediately to safeguard all aircraft concerned.
4. When appropriate, broadcast by ATC communications, by radio navigation aids, and/or through
aeronautical communication stations/services an
emergency message to all aircraft in the vicinity of the
descending aircraft. Include the following information:
(a) Location of emergency descent.
(b) Direction of flight.
(c) Type aircraft.
(d) Route if appropriate.
(e) Altitude vacated.
(f) Other information.
EXAMPLE“Attention all aircraft in the vicinity of Trout, a northbound
D-C Ten on A-T-S Route Alfa Seven Hundred is making an
emergency descent from flight level three three zero.”
(Repeat as you deem appropriate.)
5. If traffic conditions permit, provide traffic
information to the affected aircraft.
6. Immediately after an emergency broadcast or
traffic information has been made, issue appropriate
clearances or instructions, as necessary, to all aircraft
involved.
10-6-5. SERVICES TO RESCUE AIRCRAFT
a. Provide standard IFR separation between the
SAR and the aircraft in distress, except when visual
or radar contact has been established by the search
and rescue aircraft and the pilots of both aircraft
concur, IFR separation may be discontinued.
b. Clear the SAR aircraft to a fixed clearance limit
rather than to the aircraft in distress, which is a
moving fix. Issue route clearances that are consistent
with that of the distressed aircraft.
c. Advise the rescue aircraft, as soon as
practicable, of any factors that could adversely affect
its mission; e.g., unfavorable weather conditions,
anticipated problems, the possibility of not being able
to approve an IFR descent through en route traffic,
etc.
d. Advise the appropriate rescue agency of all
pertinent information as it develops.
e. Forward immediately any information about the
action being taken by the RCC, other organizations,
or aircraft to the aircraft concerned.
f. Advise the aircraft operator of the current status
of the SAR operation as soon as practicable.
g. Since prompt, correct, and complete information is the key to successful rescue operations, ensure
that this information is swiftly and smoothly supplied
to those organizations actively engaged in rescue
operations.
JO 7110.65S 2/14/08
10-6-4
JO 7110.65S 2/14/08
10-7-1
Ground Missile Emergencies
Section 7. Ground Missile Emergencies
10-7-1. INFORMATION RELAY
When you receive information concerning a ground
missile emergency, notify other concerned facilities
and take action to have alerting advisories issued by:
a. EN ROUTE. Air carrier company radio stations for each VFR company aircraft which is or will
be operating in the vicinity of the emergency.
b. EN ROUTE. FSSs adjacent to the emergency
location.
c. TERMINAL. Relay all information concerning
a ground missile emergency to the ARTCC within
whose area the emergency exists and disseminate as
a NOTAM.
REFERENCE-
P/CG Term- Notice to Airmen.
10-7-2. IFR AND SVFR MINIMA
Reroute IFR and SVFR aircraft as necessary to avoid
the emergency location by one of the following
minima, or by greater minima when suggested by the
notifying official:
a. Lateral separation- 1 mile between the
emergency location and either of the following:
1. An aircraft under radar control and the
emergency location which can be accurately
determined by reference to the radar scope.
2. The airspace to be protected for the route
being flown.
b. Vertical separation- 6,000 feet above the
surface over the emergency location.
10-7-3. VFR MINIMA
Advise all known VFR aircraft which are, or will be,
operating in the vicinity of a ground missile
emergency, to avoid the emergency location by 1 mile
laterally or 6,000 feet vertically, or by a greater
distance or altitude, when suggested by the notifying
official.
10-7-4. SMOKE COLUMN AVOIDANCE
Advise all aircraft to avoid any observed smoke
columns in the vicinity of a ground missile
emergency.
10-7-5. EXTENDED NOTIFICATION
EN ROUTE
When reports indicate that an emergency will exist
for an extended period of time, a Notice to Airmen
may be issued.
JO 7110.65S 2/14/08
10-7-2
JO 7110.65S 2/14/08
11-1-1
General
Chapter 11. Traffic Management Procedures
Section 1. General
11-1-1. DUTY RESPONSIBILITY
a. The traffic management system mission is to
balance air traffic demand with system capacity to
ensure the maximum efficient utilization of the NAS.
b. It is recognized that the ATCS is integral in the
execution of the traffic management mission.
NOTE-
Complete details of traffic management initiatives and
programs can be found in FAAO JO_7210.3, Facility
Operation and Administration.
11-1-2. DUTIES AND RESPONSIBILITIES
a. Supervisory Traffic Management Coordinatorin-Charge (STMCIC) shall:
1. Ensure that an operational briefing is
conducted at least once during the day and evening
shifts. Participants shall include, at a minimum, the
STMCIC, Operations Supervisors (OS), Traffic
Management Coordinator(s) (TMC), and other
interested personnel as designated by facility
management. Discussions at the meeting should
include meteorological conditions (present and
forecasted), staffing, equipment status, runways in
use, AAR and traffic management initiatives (present
and anticipated).
2. Assume responsibility for TMC duties when
not staffed.
3. Ensure that traffic management initiatives are
carried out by Supervisory Traffic Management
Coordinator-in-Charge (STMCIC).
4. Where authorized, perform URET data
entries to keep the activation status of designated
URET Airspace Configuration Elements current.
5. Perform assigned actions in the event of a
URET outage or degradation, in accordance with the
requirements of FAA Order JO 7210.3, Facility
Operation and Administration, and as designated by
facility directive.
6. Ensure changes to restrictions based on the
Restrictions Inventory and Evaluation are implemented in a timely manner.
b. OS shall:
1. Keep the TMU and affected sectors apprised
of situations or circumstances that may cause
congestion or delays.
2. Coordinate with the TMU and ATCSs to
develop appropriate traffic management initiatives
for sectors and airports in their area of responsibility.
3. Continuously review traffic management
initiatives affecting their area of responsibility and
coordinate with TMU for extensions, revisions, or
cancellations.
4. Ensure that traffic management initiatives are
carried out by ATCSs.
5. Where authorized, perform URET data
entries to keep the activation status of designated
URET Airspace Configuration Elements current.
6. Perform assigned actions in the event of a
URET outage or degradation, in accordance with the
requirements of FAA Order JO 7210.3, Facility
Operation and Administration, and as designated by
facility directive.
7. Ensure changes to restrictions based on the
Restrictions Inventory and Evaluation are implemented in a timely manner.
c. ATCSs shall:
1. Ensure that traffic management initiatives
and programs are enforced within their area of
responsibility. Traffic management initiatives and
programs do not have priority over maintaining:
(a) Separation of aircraft.
(b) Procedural integrity of the sector.
2. Keep the OS and TMU apprised of situations
or circumstances that may cause congestion or
delays.
3. Continuously review traffic management
initiatives affecting their area of responsibility and
coordinate with OS and TMU for extensions,
revisions, or cancellations.
4. Where authorized, perform URET data
entries to keep the activation status of designated
URET Airspace Configuration Elements current.
JO 7110.65S 2/14/08
11-1-2 General
5. Perform assigned actions in the event of a
URET outage or degradation, in accordance with the
requirements of FAA Order JO 7210.3, Facility
Operation and Administration, and as designated by
facility directive.
JO 7110.65S 2/14/08
12-1-1
General Control
Chapter 12. Canadian Airspace Procedures
Section 1. General Control
12-1-1. APPLICATION
Where control responsibility within Canadian
airspace has been formally delegated to the FAA by
the Transport Canada Aviation Group, apply basic
FAA procedures except for the Canadian procedures
contained in this chapter.
NOTE-
In 1985, the U.S. and Canada established an agreement
recognizing the inherent safety of the ATC procedures
exercised by the other country. This agreement permits the
use of ATC procedures of one country when that country is
exercising ATC in the airspace over the territory of the
other country insofar as they are not inconsistent with, or
repugnant to, the laws and regulations or unique
operational requirements of the country over whose
territory such airspace is located. Accordingly, this
chapter was revised to include only those Canadian
procedures that must be used because of a Canadian
regulatory or unique operational requirement.
12-1-2. AIRSPACE CLASSIFICATION
a. Class A airspace. Controlled airspace within
which only IFR flights are permitted. Airspace
designated from the base of all controlled high level
airspace up to and including FL 600.
b. Class B airspace. Controlled airspace within
which only IFR and Controlled VFR (CVFR) flights
are permitted. Includes all controlled low level
airspace above 12,500 feet ASL or at and above the
minimum en route IFR altitude, (whichever is higher)
up to but not including 18,000 feet ASL. ATC
procedures pertinent to IFR flights shall be applied to
CVFR aircraft.
NOTE-
The CVFR pilot is responsible to maintain VFR flight and
visual reference to the ground at all times.
c. Class C airspace. Controlled airspace within
which both IFR and VFR flights are permitted, but
VFR flights require a clearance from ATC to enter.
d. Class D airspace. Controlled airspace within
which both IFR and VFR flights are permitted, but
VFR flights do not require a clearance from ATC to
enter, however, they must establish two-way
communications with the appropriate ATC agency
prior to entering the airspace.
e. Class E airspace. Airspace within which both
IFR and VFR flights are permitted, but for VFR flight
there are no special requirements.
f. Class F airspace. Airspace of defined dimensions within which activities must be confined
because of their nature, or within which limitations
are imposed upon aircraft operations that are not a
part of those activities, or both. Special use airspace
may be classified as Class F advisory or Class F
restricted.
g. Class G airspace. Uncontrolled airspace
within which ATC has neither the authority nor
responsibility for exercising control over air traffic.
12-1-3. ONE THOUSAND-ON-TOP
Clear an aircraft to maintain “at least 1,000_feet-on-
top” in lieu of “VFR-on-top,” provided:
a. The pilot requests it.
NOTE-
It is the pilot's responsibility to ensure that the requested
operation can be conducted at least 1,000 feet above all
cloud, haze, smoke, or other formation, with a flight
visibility of 3 miles or more. A pilot's request can be
considered as confirmation that conditions are adequate.
b. The pilot will not operate within Class A or
Class B airspace.
12-1-4. SEPARATION
Apply a lateral, longitudinal, or vertical separation
minimum between aircraft operating in accordance
with an IFR or CVFR clearance, regardless of the
weather conditions.
JO 7110.65S 2/14/08
12-1-2 General Control
12-1-5. DEPARTURE CLEARANCE/
COMMUNICATION FAILURE
a. Base controller action regarding radio failures
in Canadian airspace on the requirement for pilots to
comply with Canadian Airspace Regulations, which
are similar to 14 CFR Section 91.185; however, the
following major difference shall be considered when
planning control actions. Except when issued
alternate radio failure instructions by ATC, pilots will
adhere to the following: If flying a turbine-powered
(turboprop or turbojet) aircraft and cleared on
departure to a point other than the destination,
proceed to the destination airport in accordance with
the flight plan, maintaining the last assigned altitude
or flight level or the minimum en route IFR altitude,
whichever is higher, until 10 minutes beyond the
point specified in the clearance (clearance limit), and
then proceed at altitude(s) or flight level(s) filed in the
flight plan. When the aircraft will enter U.S. airspace
within 10 minutes after passing the clearance limit,
the climb to the flight planned border crossing
altitude is to be commenced at the estimated time of
crossing the Canada/U.S. boundary.
12-1-6. PARACHUTE JUMPING
Do not authorize parachute jumping without prior
permission from the appropriate Canadian authority.
NOTE-
Canadian regulations require written authority from the
Ministry of Transport.
12-1-7. SPECIAL VFR (SVFR)
NOTE-
Pilots do not have to be IFR qualified to fly SVFR at night,
nor does the aircraft have to be equipped for IFR flight.
a. Within a control zone where there is an airport
controller on duty, approve or refuse a pilot's request
for SVFR on the basis of current or anticipated IFR
traffic only. If approved, specify the period of time
during which SVFR flight is permitted.
b. Within a control zone where there is no airport
controller on duty, authorize or refuse an aircraft's
request for SVFR on the basis of:
1. Current or anticipated IFR traffic, and
2. Official ceiling and visibility reports.
c. Canadian SVFR weather minimums for:
1. Aircraft other than helicopters. Flight visibility (ground visibility when reported) 1 mile.
2. Helicopters. Flight visibility (ground visibility when available) 1/2 mile.
JO 7110.65S 2/14/08
13-1-1
User Request Evaluation Tool (URET) - En Route
Chapter 13. Decision Support Tools
Section 1. User Request Evaluation Tool
(URET) - En Route
13-1-1. DESCRIPTION
URET is an en route decision support tool that is used
by the sector team in performing its strategic planning
responsibilities. URET uses flight plan data, forecast
winds, aircraft performance characteristics, and track
data to derive expected aircraft trajectories, and to
predict conflicts between aircraft and between
aircraft and special use or designated airspace. It also
provides trial planning and enhanced flight data
management capabilities.
13-1-2. CONFLICT DETECTION AND
RESOLUTION
a. Actively scan URET information for predicted
aircraft-to-aircraft and aircraft-to-airspace alerts.
b. When a URET alert is displayed, evaluate the
alert and take appropriate action as early as practical,
in accordance with duty priorities.
c. Prioritize the evaluation and resolution of
URET alerts to ensure the safe, expeditious, and
efficient flow of air traffic.
NOTE-
URET alerts are based on radar separation standards.
Caution should be used when situations include
nonstandard formations.
d. When a URET alert is displayed and when
sector priorities permit, give consideration to the
following in determining a solution:
1. Solutions that involve direct routing, altitude
changes, removal of a flight direction constraint
(i.e.,_inappropriate altitude for direction of flight),
and/or removal of a static restriction for one or more
pertinent aircraft.
2. Impact on surrounding sector traffic and
complexity levels, flight efficiencies, and user
preferences.
e. When the URET Stop Probe feature is activated
for an aircraft, Conflict Probe for that aircraft shall be
restarted before transfer of control, unless otherwise
coordinated.
NOTE-
The requirement in subpara 13-1-2e does not apply to
aircraft entering airspace of a non-URET facility.
13-1-3. TRIAL PLANNING
a. When URET is operational at the sector and
when sector priorities permit, use the trial plan
capability to evaluate:
1. Solutions to predicted conflicts.
2. The feasibility of granting user requests.
3. The feasibility of removing a flight direction
constraint (i.e., inappropriate altitude for direction of
flight) for an aircraft.
4. The feasibility of removing a static restriction
for an aircraft.
13-1-4. URET-BASED CLEARANCES
When the results of a trial plan based upon a user
request indicate the absence of alerts, every effort
should be made to grant the user request, unless the
change is likely to adversely affect operations at
another sector.
13-1-5. THE AIRCRAFT LIST (ACL),
DEPARTURE LIST (DL) AND FLIGHT DATA
MANAGEMENT
a. The ACL shall be used as the sector team's
primary source of flight data.
b. Actively scan URET to identify automated
notifications that require sector team action.
c. When an ACL or DL entry has a Remarks
indication, the Remarks field of the flight plan shall
be reviewed. Changes to the Remarks field shall also
be reviewed.
d. Highlighting an entry on the ACL or DL shall
be used to indicate the flight requires an action or
special attention.
JO 7110.65S 2/14/08
13-1-2 User Request Evaluation Tool (URET) - En Route
e. The Special Posting Area (SPA) should be used
to group aircraft that have special significance
(e.g.,_aircraft to be sequenced, air refueling missions,
formations).
f. When URET is operational, sector teams shall
post flight progress strips for any nonradar flights.
g. When URET is operational, a flight progress
strip shall be posted for any flight plan not contained
in the Host Computer System.
h. When URET is operational, sector teams shall
post any flight progress strip(s) that are deemed
necessary for safe or efficient operations. The sector
team shall comply with all applicable facility
directives to maintain posted flight progress strips.
i. The URET Drop Track Delete option shall be
used in accordance with facility directives.
13-1-6. MANUAL COORDINATION AND
THE URET COORDINATION MENU
a. Where automated coordination with a facility is
not available (e.g., an international facility, a VFR
tower), use the URET Coordination Menu or a flight
progress strip to annotate manual coordination status,
in accordance with facility directives.
b. When the URET Coordination Menu is used
and the flight plan is subsequently changed, remove
the yellow coding from the Coordination Indicator
after any appropriate action has been taken.
13-1-7. HOLDING
For flights in hold, use URET Hold Annotations, a
flight progress strip, or a facility-approved worksheet to annotate holding instructions, in accordance
with facility directives.
13-1-8. RECORDING OF CONTROL DATA
a. All control information not otherwise recorded
via automation recordings or voice recordings shall
be manually recorded using approved methods.
b. When a point out has been approved, remove
the yellow color coding on the ACL.
c. When the URET Free Text Area is used to enter
control information, authorized abbreviations shall
be used. You may use:
1. The clearance abbreviations authorized in
TBL 13-1-1.
TBL 13-1-1
Clearance Abbreviations
Abbreviation Meaning
A Cleared to airport (point of intended landing)
B Center clearance delivered
C ATC clears (when clearance relayed through non-ATC facility)
CAF Cleared as filed
D Cleared to depart from the fix
F Cleared to the fix
H Cleared to hold and instructions issued
N Clearance not delivered
O Cleared to the outer marker
PD Cleared to climb/descend at pilot's discretion
Q Cleared to fly specified sectors of a NAVAID defined in terms of courses, bearings, radials,
or quadrants within a designated radius
T Cleared through (for landing and takeoff through intermediate point)
V Cleared over the fix
X Cleared to cross (airway, route, radial) at (point)
Z Tower jurisdiction
JO 7110.65S 2/14/08
13-1-3
User Request Evaluation Tool (URET) - En Route
2. The miscellaneous abbreviations authorized
in TBL 13-1-2.
3. The URET equivalents for control information symbols authorized in TBL 13-1-3.
4. Plain language markings when it will aid in
understanding information.
5. Locally approved abbreviations.
d. When the URET Free Text Area is used to enter
control information, the Free Text Area shall remain
open and visible. When no longer relevant, the
information entered into the Free Text Area shall be
updated or deleted.
e. Control information entered in the Free Text
Area shall be used for reference purposes only.
NOTE-
Information entered into the Free Text Area does not pass
on handoff and, if necessary, must be coordinated.
TBL 13-1-2
Miscellaneous Abbreviations
Abbreviation Meaning
BC Back course approach
CT Contact approach
FA Final approach
FMS Flight management system approach
GPS GPS approach
I Initial approach
ILS ILS approach
MA Missed approach
MLS MLS approach
NDB Nondirectional radio beacon approach
OTP VFR conditions-on-top
PA Precision approach
PT Procedure turn
RA Resolution advisory (Pilot-reported TCAS event)
RH Runway heading
RNAV Area navigation approach
RP Report immediately upon passing (fix/altitude)
RX Report crossing
SA Surveillance approach
SI Straight-in approach
TA TACAN approach
TL Turn left
TR Turn right
VA Visual approach
VR VOR approach
JO 7110.65S 2/14/08
13-1-4 User Request Evaluation Tool (URET) - En Route
TBL 13-1-3
URET Equivalents for Control Information Symbols
Abbreviation Meaning
T dir Depart (direction if specified)
↑Climb and maintain
↓Descend and maintain
CR Cruise
AT At
X Cross
M Maintain
/airway
Join or intercept (airway, jet route,
track, or course)
= While in controlled airspace
WICA While in control area
dir ECA Enter control area
dir OOCA Out of control area
dir ESA
Cleared to enter surface area.
Indicated direction of flight by
appropriate compass letter(s)
TSA alt
Through surface area and altitude
indicated direction of flight by
appropriate compass letter(s).
Maintain special VFR conditions
(altitude if appropriate) while in
surface area
250 K
Aircraft requested to adjust speed to
250 knots
-20 K
Aircraft requested to reduce speed
20 knots
+30 K
Aircraft requested to increase speed
30 knots
SVFR
Local Special VFR operations in the
vicinity of (name) airport are
authorized until (time). Maintain
special VFR conditions (altitude if
appropriate)
B4 Before
AF After or Past
/ Until
*instructions* Alternate instructions
REST Restriction
AOB At or Below
AOA At or Above
Abbreviation Meaning
- From-to (route, time, etc.)
(Alt)B(Alt)
Indicates a block altitude assignment.
Altitudes are inclusive, and the first
altitude shall be lower than the
second (Example 310B370)
V time
Clearance void if aircraft not off
ground by time
CL Pilot canceled flight plan
+info+
Information or revised information
forwarded
**alt**
Other than assigned altitude reported
Example: **50**
ARC mi. dir.
DME arc of VORTAC, TACAN, or
MLS
C freq.
Contact (facility) or (freq.), (time, fix,
or altitude if appropriate). Insert
frequency only when it is other than
standard
R Radar contact
R alt Requested altitude
R/ Radar service terminated
RX Radar Contact Lost
RV Radar vector
RVX Pilot resumed own navigation
HO Handoff completed
E Emergency
W Warning
P
Point out initiated. Indicate the
appropriate facility, sector, or
position.
FUEL Minimum fuel
EFC time Expect further clearance at (time)
- fix Direct to fix
FRC Full route clearance
IAF Initial approach fix
NORDO No Radio
PT Procedure turn
RLS Release
REQ Request
SI Straight in
JO 7110.65S 2/14/08
13-1-5
User Request Evaluation Tool (URET) - En Route
13-1-9. ACKNOWLEDGEMENT OF
AUTOMATED NOTIFICATION
a. The URET Inappropriate Altitude for Direction
of Flight (IAFDOF) feature shall be used in the
automatic mode (i.e., IAFDOF Manual shall remain
deselected) unless otherwise authorized in a facility
directive.
b. Completion of any required coordination for
IAFDOF shall be acknowledged on the ACL by
removing the IAFDOF coding.
c. Completion of appropriate coordination for an
Unsuccessful Transmission Message (UTM) shall be
acknowledged on the ACL by removing the UTM
coding.
d. Issuance of the Expect Departure Clearance
Time (EDCT) to the pilot or other control facility
shall be acknowledged on the DL by removing the
EDCT coding.
e. IAFDOF, UTM, or EDCT coding shall be
acknowledged only after the appropriate action has
been completed.
f. Send/acknowledge Host Embedded Route Text
(HERT) coding only after the appropriate clearance
has been issued to the pilot or otherwise coordinated.
Do not send/acknowledge HERT unless the sector
has track control for the flight or it has been otherwise
coordinated.
g. Remove ATC Preferred Route (APR) coding
only after the route has been checked and any
required action has been completed. Do not remove
APR coding unless the sector has track control or it
has been otherwise coordinated.
NOTE-
If coding is prematurely removed and the control of the
aircraft is transferred before completing the appropriate
action, the next sector may not receive the necessary APR
notification.
13-1-10. CURRENCY OF TRAJECTORY
INFORMATION
a. The sector team shall perform automation
entries in a timely manner.
NOTE1. Conflict probe accuracy requires timely updates of data
used to model each flight's trajectory. If this data is not
current, the aircraft entries and notification of probe
results for surrounding sectors and facilities, as well as the
subject sector, may be misleading.
2. Data used to model an individual aircraft's trajectory
includes route of flight, assigned and interim altitudes,
application/removal of an adapted restriction for that
flight, and aircraft type.
b. An exception to the requirement to enter or
update interim altitudes may be authorized for certain
ARTCC sectors if explicitly defined in an appropriate
facility directive.
NOTE-
URET accuracy in assigning alert notification is
dependent upon entry/update of a flight's interim altitude.
13-1-11. DELAY REPORTING
a. Adhere to all applicable delay reporting
directives while URET is operational.
b. Delay information shall be recorded. Delay
information may be automatically recorded via use of
the URET Hold Annotations Menu or manually on
flight progress strips or facility-approved worksheets, in accordance with the facility-defined
standard.
c. When using URET to automatically record
delay information, the URET hold annotations shall
be deleted when the aircraft is cleared from holding.
NOTE-
Delay information cannot be accurately recorded unless
URET hold annotations are deleted when the aircraft is
cleared from holding.
13-1-12. OVERDUE AIRCRAFT
Upon receipt of the URET overdue aircraft
notification, take appropriate actions set forth in
Chapter 10, Section 3, Overdue Aircraft.
NOTE-
URET overdue aircraft notification is based on radar track
data. Updating an aircraft's route of fight will remove the
overdue aircraft notification.
JO 7110.65S 2/14/08
13-1-6 User Request Evaluation Tool (URET) - En Route
13-1-13. USE OF GRAPHICS PLAN
DISPLAY (GPD)
a. Graphic depictions of flight trajectories may be
used only to aid in situational awareness and strategic
planning.
b. Do not use trajectory-based positions as a
substitute for radar track position.
c. Do not use trajectory-based altitude in lieu of
Mode C for altitude confirmation.
d. Do not use the GPD for radar identification,
position information, transfer of radar identification,
radar separation, correlation, or pointouts.
13-1-14. FORECAST WINDS
In the event that current forecast wind data are not
available, continue use of URET with appropriate
recognition that alert and trajectory data may be
affected.
13-1-15. INTERFACILITY CONNECTIVITY
In the event of a loss of connectivity to a neighboring
URET system, continue use of URET with
appropriate recognition that alert data may be
affected.
13-1-16. PRIMARY HOST OUTAGES
In the event of a primary HOST outage, URET data
may be used to support situational awareness while
the facility transitions to the backup RDP or nonradar
procedures.
NOTE-
Without primary system input, URET data cannot be
updated and becomes stale.
13-1-17. URET AIRSPACE
CONFIGURATION ELEMENTS
a. URET Airspace Configuration Elements are:
1. Special Activity Airspace (SAA).
2. Airport Stream Filters (ASF).
3. URET adapted restrictions.
b. Where assigned as a sector responsibility by
facility directive, the sector team shall update URET
Airspace Configuration Elements to reflect current
status.
c. For Airspace Configuration Elements designated as a sector responsibility, notify the operational
supervisor when the status of an Airspace Configuration Element has been modified in URET.
JO 7110.65S 2/14/08
13-2-1
Ocean21 - Oceanic
Section 2. Ocean21 - Oceanic
The following procedures are applicable to the
operation of the Ocean21 Oceanic Air Traffic Control
(ATC) System.
13-2-1. DESCRIPTION
a. The Ocean21 ATC System is utilized in
designated en route/oceanic airspace. Ocean21
includes both surveillance and flight data processing,
which provides the controllers with automated
decision support tools to establish, monitor and
maintain separation between aircraft, and aircraft to
airspace and terrain.
b. Ocean21 capabilities include:
1. MEARTS based radar surveillance
processing.
2. Conflict Prediction and Reporting.
3. Automatic Dependent Surveillance-
Broadcast (ADS-B).
4. Automatic Dependent Surveillance-
Contract (ADS-C).
5. Controller Pilot Data Link Communications
(CPDLC).
6. ATC Interfacility Data Communications
(AIDC).
7. Additional Decision Support Tools used
primarily for situational awareness.
8. Electronic Flight Data including Electronic
Flight Strips.
13-2-2. CONFLICT DETECTION AND
RESOLUTION
The controller shall use the most accurate information available to initiate, monitor, and maintain
separation.
a. Apply the following procedures in airspace
where conflict probe is being utilized as a decision
support tool:
1. Conflict Probe Results.
(a) Controllers shall assume that the conflict
probe separation calculations are accurate.
(b) Unless otherwise prescribed in subpara_a3, controllers shall utilize the results from
conflict probe to initiate and maintain the prescribed
separation minima.
2. Conflict Resolution.
(a) When a controller is alerted to a conflict,
which will occur in his/her sector, take the
appropriate action to resolve the conflict.
(b) The controller responsible for resolving a
conflict shall evaluate the alert and take appropriate
action as early as practical, in accordance with duty
priorities, alert priority, and operational
considerations.
(c) Unless otherwise specified in facility
directives, the controller shall take immediate action
to resolve any “red” conflicts.
3. Overriding Conflict Probe.
(a) Controllers shall not override conflict
probe except for the following situations:
(1) The application of a separation standard
not recognized by conflict probe listed in subpara_a8(a), or as identified by facility directive.
(2) When action has been taken to resolve
the identified conflict and separation has been
ensured, or
(3) Control responsibility has been delegated to another sector or facility, or
(4) Other situations as specified in facility
directives.
(b) Controllers shall continue to ensure that
separation is maintained until the overridden conflict
is resolved.
4. Use of Probe when Issuing Clearances. Utilize conflict probe results when issuing a clearance to
ensure that any potential conflict has been given
thorough consideration.
5. Use of Probe when Accepting Manual
Transfers. Prior to manually accepting an aircraft
transfer from an external facility ensure that the
coordinated flight profile is accurately entered,
conflict probe initiated and, if necessary, action is
taken to resolve any potential conflicts.
JO 7110.65S 2/14/08
13-2-2 Ocean21 - Oceanic
6. Trial Probe. The controller can utilize trial
probe to assess whether there are any potential
conflicts with a proposed clearance or when
performing manual coordination.
NOTE-
Once initiated, trial probe does not take into account any
changes made to the proposed profile or to any other flight
profile in the system. It is an assessment by conflict probe
of the current situation at the time the controller enters the
trial probe. A trial probe does not alleviate the controller
from performing a conflict probe when issuing a clearance
or accepting a transfer.
7. System Unable to Perform Conflict Probe for
a Specific Aircraft.
(a) If a flight's profile becomes corrupted,
conflict probe may not be able to correctly monitor
separation for that flight. Take the necessary steps to
correct an aircraft's flight plan when conflict probe
could not be performed.
(b) In addition, after verifying flight plan data
accuracy, utilize other decision support tools to
establish and maintain the appropriate separation
minima until such time that conflict probe can be
utilized.
8. Conflict Probe Limitations.
(a) Conflict Probe does not support the
following separation minima:
(1) Subpara 8-4-2a2 - Nonintersecting
paths.
(2) Subpara 8-4-2d - Intersecting flight
paths with variable width protected airspace.
(3) Subpara 8-4-3a - Reduction of Route
Protected Airspace, below FL 240.
(4) Subpara 8-4-3b - Reduction of Route
Protected Airspace, at and above FL 240.
(5) Subpara 8-4-4a1 - Same NAVAID:
VOR/VORTAC/TACAN.
(6) Subpara 8-4-4a2 - Same NAVAID:
NDB.
(7) Subpara 8-4-4c - Dead Reckoning.
(8) Para 8-5-4 - Same Direction.
(9) Para 8-6-3 - Temporary Moving
Airspace Reservations.
(10) Para 8-8-5 - VFR Climb and Descent.
(11) ZAN waiver 97-0-036 (30/40 DME).
b. Additional Decision Support Tools: These
support tools include: range/bearing, time of passing,
intercept angle, the aircraft situation display (ASD)
and electronic flight data.
1. The results provided by these additional
decision support/controller tools can be used by the
controller for maintaining situational awareness and
monitoring flight profile information, and for
establishing and maintaining separation standards
not supported by probe, or when probe is unavailable.
2. Under no circumstances shall the controller
utilize any of the additional decision support tools to
override probe results when the applicable separation
standard is supported by probe and none of the other
conditions for overriding probe apply.
13-2-3. INFORMATION MANAGEMENT
a. Currency of Information: The sector team is
responsible for ensuring that manually entered data is
accurate and timely. Ensure that nonconformant
messages are handled in a timely manner and that the
flight's profile is updated as necessary.
NOTE-
Conflict probe accuracy requires timely updates of data
used to model each flight's trajectory. If this data is not
current, the aircraft flight profile and probe results may be
misleading.
b. Data Block Management.
1. Ensure that the data block reflects the most
current flight information and controller applied
indicators as specified in facility directives.
2. Ensure that appropriate and timely action is
taken when a special condition code is indicated in the
data block.
c. Electronic Flight Strip Management.
1. Electronic flight strips shall be maintained in
accordance with facility directives and the following:
(a) Annotations. Ensure that annotations are
kept up to date.
(b) Reduced Separation Flags. Ensure the
flags listed below are selected appropriately for each
flight:
(1) M- Mach Number Technique (MNT).
(2) R- Reduced MNT.
JO 7110.65S 2/14/08
13-2-3
Ocean21 - Oceanic
(3) D- Distance-based longitudinal.
(4) W- Reduced Vertical Separation Minimum (RVSM).
(c) Degraded RNP. Select when an aircraft
has notified ATC of a reduction in navigation
capability that affects the applicable separation
minima.
(d) Restrictions. Ensure restrictions accurately reflect the cleared profile.
d. Queue Management.
1. Manage all sector and coordination queues in
accordance with the appropriate message priority and
the controller's priority of duties.
2. In accordance with facility directives, ensure
that the messages directed to the error queue are
processed in a timely manner.
e. Window/List Management.
1. Ensure that the situation display window title
bar is not obscured by other windows and/or lists.
NOTE-
The title bar changes color to denote when priority
information on the ASD is being obscured or is out of view.
2. In accordance with facility directives, ensure
that designated windows and/or lists are displayed at
all times.
13-2-4. CONTROLLER PILOT DATA LINK
COMMUNICATIONS (CPDLC)
a. Means of communication.
1. When CPDLC is available and CPDLC
connected aircraft are operating outside of VHF
coverage, CPDLC shall be used as the primary means
of communication.
2. Voice communications may be utilized for
CPDLC aircraft when it will provide an operational
advantage and/or when workload or equipment
capabilities demand.
3. When CPDLC is being utilized, a voice
backup shall exist (e.g., HF, SATCOM, Third party).
4. When a pilot communicates via CPDLC, the
response should be via CPDLC.
5. To the extent possible, the CPDLC message
set should be used in lieu of free text messages.
NOTE-
The use of the CPDLC message set ensures the proper
“closure” of CPDLC exchanges.
b. Transfer of Communications to the Next
Facility.
1. When the receiving facility is capable of
CPDLC communications, the data link transfer is
automatic and is accomplished within facility
adapted parameters.
2. When a receiving facility is not CPDLC
capable, the transfer of communications shall be
made in accordance with local directives and Letters
of Agreement (LOAs).
c. Abnormal conditions.
1. If any portion of the automated transfer fails,
the controller should attempt to initiate the transfer
manually. If unable to complete the data link transfer,
the controller should advise the pilot to log on to the
next facility and send an End Service (EOS) message.
2. If CPDLC fails, voice communications shall
be utilized until CPDLC connections can be
reestablished.
3. If the CPDLC connection is lost on a specific
aircraft, the controller should send a connection
request message (CR1) or advise the pilot via backup
communications to log on again.
4. If CPDLC service is to be canceled, the
controller shall advise the pilot as early as possible to
facilitate a smooth transition to voice communications. Workload permitting, the controller should also
advise the pilot of the reason for the termination of
data link.
5. Assume that all unanswered CPDLC messages have not been delivered. On initial voice
contact with aircraft, preface the message with the
following:
PHRASEOLOGY(Call Sign) CPDLC Failure, (message).
JO 7110.65S 2/14/08
13-2-4 Ocean21 - Oceanic
13-2-5. COORDINATION
In addition to the requirements set forth in Chapter 8,
Offshore/Oceanic Procedures, Section 2, Coordination, automated coordination shall constitute
complete coordination between Ocean21 sectors,
both internally and between sectors across adjacent
Ocean21 facilities, except:
a. When the aircraft is in conflict with another in
the receiving sector, or
b. When otherwise specified in facility directives
or LOA.
13-2-6. TEAM RESPONSIBILITIES -
MULTIPLE PERSON OPERATION
a. When operating in a multiple controller
operation at a workstation, ensure all ATC tasks are
completed according to their priority of duties.
b. Multiple controller operation shall be accomplished according to facility directives.
JO 7110.65S 2/14/08
Appendix A-1
Aircraft Information Fixed-Wing Aircraft
Appendix A. Aircraft Information Fixed-Wing Aircraft
TYPE ENGINE ABBREVIATIONS
P piston
T turboprop
J jet
CLIMB AND DESCENT RATES
Climb and descent rates based on average en route
climb/descent profiles at median weight between
maximum gross takeoff and landing weights.
SRS
SRS means “same runway separation;” categorization criteria is specified in para 3-9-6, Same Runway
Separation.
MANUFACTURERS
Listed under the primary manufacturer are other
aircraft manufacturers who make versions of some of
the aircraft in that group.
AIRCRAFT WEIGHT CLASSES
a. Heavy. Aircraft capable of takeoff weights of
more than 255,000 pounds whether or not they are
operating at this weight during a particular phase of
flight.
b. Large. Aircraft of more than 41,000 pounds,
maximum certificated takeoff weight, up to
255,000_pounds.
c. Small. Aircraft of 41,000 pounds or less
maximum certificated takeoff weight.
LAND AND HOLD SHORT OPERATIONS (LAHSO)
AIRCRAFT GROUP AND DISTANCE MINIMA
FAA Order 7110.118, Land and Hold Short
Operations, includes procedures and conditions for
conducting land and hold short operations at
designated airports. Appendix 1 to Order 7110.118
groups certain aircraft according to available landing
distance for LAHSO operations. Aircraft group
information for the purposes of Order 7110.118 is
incorporated in this Appendix under Performance
Information.
NOTE* Denotes single-piloted military turbojet aircraft or aircraft to receive the same procedural handling as a single-piloted
military turbojet aircraft.
*** Denotes amphibian aircraft.
+ Denotes aircraft weighing between 12,500 lbs. and 41,000 lbs. For Class B Airspace rules, these aircraft are “large,
turbine-engine powered aircraft.”
JO 7110.65S 2/14/08
Appendix A-2 Aircraft Information Fixed-Wing Aircraft
TBL A-1
Land and Hold Short Operations (LAHSO)
Aircraft Group/Distance Minima
Sea Level
-999
1,000-
1,999
2000-
2,999
3000-
3,999
4000-
4,999
5000-
5,999
6000-
6,999
7000-
7,000
Group 1 2500 2550 2600 2650 2700 2750 2800 2850
Group 2 &
Below
3000 3050 3100 3150 3200 3250 3300 3500
Group 3 &
Below
3500 3550 3600 3650 3700 3750 3800 3850
Group 4 &
Below
4000 4050 4100 4150 4200 4250 4300 4350
Group 5 &
Below
4500 4550 4600 4650 4700 4750 4800 4850
Group 6 &
Below
5000 5100 5200 5300 5400 5500 5600 5700
Group 7 &
Below
6000 6100 6200 6300 6400 6500 6600 6700
Group 8 &
Below
7000 7100 7200 7300 7400 7500 7600 7700
Group 9 &
Below
8000 8100 8200 8300 8400 8500 8600 8700
Group 10 Greater than 8000 feet
TBL A-1 is an air traffic control tool for identifying aircraft, by groups, that are able to land and hold short based
on the available landing distance. Air traffic managers shall utilize TBL A-1 for identifying aircraft by groups
that are able to land and hold short at their facility in accordance with FAA Order 7110.118, Land and Hold Short
Operations.
At locations requesting to utilize LAHSO with aircraft requiring greater than 8,000 feet of available landing
distance, air traffic managers shall coordinate with the appropriate Flight Standards' office and Air Traffic
Operations, Terminal Safety and Operations Support to obtain a letter of authorization approving LAHSO.
JO 7110.65S 2/14/08
Appendix A-3
Aircraft Information Fixed-Wing Aircraft
ADAM AIRCRAFT (USA)
Model Type
Designator
Description Performance Information
Number & Type Engines/
Weight Class
Climb
Rate (fpm)
Descent
Rate (fpm)
SRS
Cat.
LAHSO
Group
A-500, CarbonAero A500 2P/S II
AERMACCHI SpA (Italy)
(Also AGUSTA, SIAI-MARCHETTI)
Model Type
Designator
Description Performance Information
Number & Type Engines/
Weight Class
Climb
Rate (fpm)
Descent
Rate (fpm)
SRS
Cat.
LAHSO
Group
AMX AMX* 1J/S+ III
FN-333 Riviera*** FN33 1P/S I
MB-290TP Redigo L90 1T/S I
MB-326 M32 1J/S III
MB-339 M339* 1J/S III
SF-205-18F/20F S05F 1P/S I
SF-205-18R/20R/22R S05R 1P/S I
S-208 S208 1P/S I
S-211 S211 1T/S I
SF-260 A/B/C/D/E/F/M/W, Warrior F260 1P/S I
SF-260TP F26T 1T/S 1,800 1,100 I 3
SF-600A, SF-600TP Canguero F600 2T/S 2,100 II 4
AERONCA (USA- see Bellanca)
AERO SPACELINES (USA)
Model Type
Designator
Description Performance Information
Number & Type Engines/
Weight Class
Climb
Rate (fpm)
Descent
Rate (fpm)
SRS
Cat.
LAHSO
Group
Super Guppy,
Super Turbine Guppy
SGUP 4T/L 1,500 1,500 III 10
AEROSPATIALE (France)
(Also AEROSPATIALE/AERITALIA, ATR, ALENIA MORANE-SAULNIER, PZL-OKECIE, SOCATA, SUD, SUD-EST, TBM)
Model Type
Designator
Description Performance Information
Number & Type Engines/
Weight Class
Climb
Rate (fpm)
Descent
Rate (fpm)
SRS
Cat.
LAHSO
Group
ATR-42-200/300/320 AT43 2T/L 2,000 2,000 III 5
ATR-42-400 AT44 2T/L 2,000 2,000 III 5
ATR-42-500 AT45 2T/L 2,000 2,000 III 5
ATR-72 AT72 2T/L 2,000 2,000 III 6
JO 7110.65S 2/14/08
Appendix A-4 Aircraft Information Fixed-Wing Aircraft
Model Type
Designator
Description Performance Information
Number & Type Engines/
Weight Class
Climb
Rate (fpm)
Descent
Rate (fpm)
SRS
Cat.
LAHSO
Group
Rallye, Rallye Club, Super Rallye,
Rallye Commodore, Minerva (MS-880
to 894)
RALL 1P/S 750 750 I 3
SE-210 Caravelle S210 2J/L 2,300 2,000 III 8
SN-601 Corvette S601 2J/S+ 2,500 2,000 III 5
Tampico TB-9 TAMP 1P/S 600 700 I 2
TBM TB-700 TBM7 1T/S 1,700 1,500 I 5
Tabago TB10C/200 TOBA 1P/S 700 700 I 2
Trinidad TB-20/21 TRIN 1P/S 850 700 I 3
AIRBUS INDUSTRIES (International)
Model Type
Designator
Description Performance Information
Number & Type Engines/
Weight Class
Climb
Rate (fpm)
Descent
Rate (fpm)
SRS
Cat.
LAHSO
Group
A-300B2/4-1/2/100/200,
A-300C4-200
A30B 2J/H 3,500 3,500 III 8
A-300B4 - 600 A306 2J/H 3,500 3,500 III 7
A-310 (CC-150 Polaris) A310 2J/H 3,500 3,500 III 7
A-318 A318 2J/L 3,500 3,500 III
A-319, ACJ A319 2J/L 3,500 3,500 III 7
A-320 A320 2J/L 3,500 3,500 III 7
A-321 A321 2J/L 3,500 3,500 III
A-300ST Super Transporter, Beluga A3ST 2J/H III
A-330-200 A332 2J/H 3,500 3,500 III 8
A-330-300 A333 2J/H III 8
A-340-200 A342 4J/H 3,500 3,500 III 9
A-340-300 A343 4J/H III 9
A-340-500 A345 4J/H III 9
A-340-600 A346 4J/H III 9
A-380-800 A388 4J/H III 10
AIRCRAFT HYDRO-FORMING (USA)
(Also BUSHMASTER)
Model Type
Designator
Description Performance Information
Number & Type Engines/
Weight Class
Climb
Rate (fpm)
Descent
Rate (fpm)
SRS
Cat.
LAHSO
Group
Bushmaster 2000 BU20 3P/S+ 2,000 2,000 III 2
JO 7110.65S 2/14/08
Appendix A-5
Aircraft Information Fixed-Wing Aircraft
AIR TRACTOR, INC. (USA)
Model Type
Designator
Description Performance Information
Number & Type Engines/
Weight Class
Climb
Rate (fpm)
Descent
Rate (fpm)
SRS
Cat.
LAHSO
Group
AT-300/301/401 AT3P 1P/S 1,000 I 1
AT-302/400/402 AT3T 1T/S I
AT-501 AT5P 1P/S I
AT-502/503 AT5T 1T/S I
AT-602 AT6T 1T/S I
AT-802 AT8T 1T/S+ III
ANTONOV (Russia)
Model Type
Designator
Description Performance Information
Number & Type Engines/
Weight Class
Climb
Rate (fpm)
Descent
Rate (fpm)
SRS
Cat.
LAHSO
Group
An-2 AN2 1P/S I
An-8 AN8 2T/L III
An-12 AN12 4T/L III
An-70 AN70 4T/H III
An-74-100/200 AN72 2J/L III
An-124 Ruslan A124 4J/H III
An-140 A140 2T/L III
AVIATION DEVELOPMENT (USA)
Model Type
Designator
Description Performance Information
Number & Type Engines/
Weight Class
Climb
Rate (fpm)
Descent
Rate (fpm)
SRS
Cat.
LAHSO
Group
Alaskan Bushmaster ALBU 1P/S I
BEAGLE AIRCRAFT (UK)
(Also BEAGLE-AUSTER)
Model Type
Designator
Description Performance Information
Number & Type Engines/
Weight Class
Climb
Rate (fpm)
Descent
Rate (fpm)
SRS
Cat.
LAHSO
Group
A-109 Airedale AIRD 1P/S I
B-121 Pup PUP 1P/S 575 750 I 2
B-125 Bulldog BDOG 1P/S I
B-206 Basset BASS 2P/S 1,200 1,300 II 8
JO 7110.65S 2/14/08
Appendix A-6 Aircraft Information Fixed-Wing Aircraft
BEECH AIRCRAFT COMPANY (USA)
(Also CCF, COLEMILL, DINFIA, EXCALIBUR, FUJI, HAMILTON, JETCRAFTERS, RAYTHEON, SWEARINGEN, VOLPAR)
Model Type
Designator
Description Performance Information
Number & Type Engines/
Weight Class
Climb
Rate (fpm)
Descent
Rate (fpm)
SRS
Cat.
LAHSO
Group
1900 (C-12J) B190 2T/S+ 2,400 2,400 III 7
B300 Super King Air 350 B350 2T/S+ 3,000 3,000 III 7
100 King Air (U-21F Ute) BE10 2T/S 2,250 2,250 II 7
17 Stagger Wing (UC-43 Traveler,
YC-43 Traveler)
BE17 1P/S 1,375 1,375 I 2
Twin Beech 18/Super H18 BE18 2P/S 1,400 1,000 II 4
18 (turbine) B18T 2T/S 2,000 2,000 II
19 Musketeer Sport, Sport BE19 1P/S 680 680 I 1
200, 1300 Super King Air, Commuter
(C-12A to F, C-12L/R, UC-12, RC-12,
Tp101, Huron)
BE20 2T/S+ 2,450 2,500 III 7
23 Musketeer, Sundowner BE23 1P/S 740 800 I 2
24 Musketeer Super, Sierra BE24 1P/S 1,000 1,000 I 3
300 Super King Air BE30 2T/S+ 3,000 3,000 III 6
33 Debonair, Bonanza (E-24) BE33 1P/S 1,000 1,000 I 4
35 Bonanza BE35 1P/S 1,200 1,200 I 3
36 Bonanza (piston) BE36 1P/S 1,100 1,100 I 2
36 Bonanza (turbine) B36T 1/T/S I
400 Beechjet, Hawker 400 (T-1
Jayhawk, T-400)
BE40 2J/S+ 3,300 2,200 III 8
50 Twin Bonanza (U-8D/E/G, RU-8
Seminole)
BE50 2P/S 1,600 1,600 II 4
55 Baron (T-42 Chochise, C-55, E-20 BE55 2P/S 1,700 1,700 II 6
56 Turbo Baron BE56 2P/S II
58 Baron BE58 2P/S 1,730 1,730 II 6
60 Duke BE60 2P/S 1,600 1,600 II 8
65 Queen Air (U-8F Seminole) BE65 2P/S 1,300 1,300 II 5
70 Queen Air BE70 2P/S II
76 Duchess BE76 2P/S 1,500 1,500 II 4
77 Skipper BE77 1P/S 750 750 I 1
80 Queen Air (Zamir) BE80 2P/S 1,275 1,275 II
88 Queen Air BE88 2P/S II
95 Travel Air BE95 2P/S 1,250 1,250 II 5
99 Airliner BE99 2T/S 1,750 1,750 II 5
90, A90 to E90 King Air (T-44 V-C6) BE9L 2T/S 2,000 2,000 II 5
F90 King Air BE9T 2T/S 2,600 2,600 II 7
2000 Starship STAR 2T/S+ 2,650 2,650 III 7
Premier 1, 390 PRM1 2J/S+ 3,000 3,000 III
T34A/B, E-17 Mentor (45) T34P 1P/S 1,150 1,150 I 1
T-34C Turbo Mentor T34T 1T/S 1,100 1,000 I
T-6A Texan II TEX2* 1T/S I
U-21A/G, EU-21, JU-21, RU-21, Ute
(A90-1 to 4)
U21 2T/S 2,000 2,000 II
QU-22 (1074/1079) U22 1P/S I
JO 7110.65S 2/14/08
Appendix A-7
Aircraft Information Fixed-Wing Aircraft
BELLANCA AIRCRAFT (USA)
(Also AERONCA, CHAMPION, DOWNER, HINDUSTAN, NORTHERN)
Model Type
Designator
Description Performance Information
Number & Type Engines/
Weight Class
Climb
Rate (fpm)
Descent
Rate (fpm)
SRS
Cat.
LAHSO
Group
Aeronca Chief/Super Chief, Pushpak AR11 1P/S 500 500 I 1
Aeronca Sedan AR15 1P/S 500 500 I 2
14 Junior, Cruiseair,
Cruiseair Senior Cruisemaster
B14A 1P/S 1,030 1,030 I 1
14 Bellanca 260/A/B/C B14C 1P/S 1,500 I
17 Viking, Super Viking,
Turbo Viking
BL17 1P/S 1,100 1,100 I 1
19 Skyrocket BL19 1P/S I
8 Decathlon, Scout BL8 1P/S 1,000 1,000 I 2
Champion Lancer 402 CH40 2P/S 650 1,000 II
7 ACA/ECA Champ, Citabria, CH7A 1P/S 750 750 I 1
7 GCBC/KCAB Citabria CH7B 1P/S 1,100 1,100 I 1
T-250 Aries T250 1P/S I
BOEING COMPANY (USA)
(Also GRUMMAN, IAI, LOCKHEED-BOEING, MCDONNELL DOUGLAS, NORTHROP-GRUMMAN, ROHR)
Model Type
Designator
Description Performance Information
Number & Type Engines/
Weight Class
Climb
Rate (fpm)
Descent
Rate (fpm)
SRS
Cat.
LAHSO
Group
B-52 Stratofortress B52 8J/H 3,000 3,000 III
707-100 (C-137B) B701 4J/H 3,500 3,500 III 9
707-300(C-18, C-137C, E-8J-Stars,
EC-18, EC-137, KC-137, T-17)
B703 4J/H 3,500 3,500 III 9
717-200 B712 2J/L III 7
720 B720 4J/L 3,000 3,000 III 9
727-100 (C-22) B721 3J/L 4,500 4,500 III 7
727-200 B722 3J/L 4,500 4,500 III 7
727-100RE Super 27 R721 3J/L 4,300 4,300 III
727-200RE Super 27 R722 3J/L 4,300 4,300 III
737-100 B731 2J/L 3,000 3,000 III 7
737-200 (Surveiller, CT-43, VC-96) B732 2J/L 3,000 3,000 III 7
737-300 B733 2J/L 5,500 3,500 III 7
737-400 B734 2J/L 6,500 3,500 III 8
737-500 B735 2J/L 5,500 3,500 III 7
737-600 B736 2J/L 4,000 4,000 III 7
737-700, BBJ, C-40 B737 2J/L 4,000 4,000 III 8
737-800, BBJ2 B738 2J/L 4,000 4,000 III 7
737-900 B739 2J/L 4,000 4,000 III 8
747-100 B741 4J/H 3,000 3,000 III 10
747-200 (E-4, VC-25) B742 4J/H 3,000 3,000 III 10
747-300 B743 4J/H 3,000 3,000 III 10
747-400 (Domestic, no winglets) B74D 4J/H 3,000 3,000 III
747-400 (International, winglets) B744 4J/H 3,000 3,000 III 10
JO 7110.65S 2/14/08
Appendix A-8 Aircraft Information Fixed-Wing Aircraft
Model Type
Designator
Description Performance Information
Number & Type Engines/
Weight Class
Climb
Rate (fpm)
Descent
Rate (fpm)
SRS
Cat.
LAHSO
Group
747SR B74R 4J/H 3,000 3,000 III 10
747SP B74S 4J/H 3,000 3,000 III 9
757-200 (C-32) B752 2J/L 3,500 2,500 III 7
757-300 B753 2J/H 3,500 2,500 III 8
767-200 B762 2J/H 3,500 3,500 III 9
767-300 B763 2J/H 3,500 3,500 III 9
767-400 B764 2J/H 3,500 3,500 III 9
777-200 B772 2J/H 2,500 2,500 III 9
777-300 B773 2J/H 2,500 2,500 III 9
747SCA Shuttle Carrier BSCA 4J/H III
C-135B/C/E/K Stratolifter (EC-135,
NKC-135, OC-135, TC-135, WC-135)
C135 4J/H 2,000 2,000 III
C-17 Globemaster 3 C17 4J/H III
C-97 Stratofreighter C97 4P/L 2,500 3,000 III
KC-135A Stratotanker (J57 engines) K35A 4J/H 2,500 3,000 III
KC 135D/E Stratotanker (TF33
engines)
K35E 4J/H 5,000 3,000 III
KC 135R/T, C-135FR, Stratotanker
(CFM56 engines)
K35R 4J/H 5,000 3,000 III
KE-3 KE3 4J/H 3,500 3,500 III
RC-135 R135 4J/H 3,000 3,000 III
E-3A (TF33), E-B/C, JE-3, Sentry E3TF 4J/H 3,500 4,000 III
E-3A (CFM56), E-3D/F, Sentry E3CF 4J/H III
E6 Mercury E6 4J/H 3,500 3,500 III
E-767 E767 2J/H 2,500 2,500 III
75 Kaydet (PT-13, PT-17, PT-18,
PT-27, N2S)
ST75 1P/S 840 840 I
BOMBARDIER (Canada)
(Also CANADAIR)
Model Type
Designator
Description Performance Information
Number & Type Engines/
Weight Class
Climb
Rate (fpm)
Descent
Rate (fpm)
SRS
Cat.
LAHSO
Group
BD-100 Challenger 300 CL30 2J/S+ 3,500 3,500 III 7
BD-700 Global 5000 GL5T 2J/L 3,500 3,500 III 7
BD-700 Global Express, Sentinel GLEX 2J/L III 7
BRITISH AEROSPACE (BAe) (UK)
(Also AIL, AVRO, BAC, BUCURESTI, DE HAVILLAND, HANDLEY-PAGE, HAWKER-SIDDELEY, JETSTREAM, KANPUR,
MCDONNELL-DOUGLAS, RAYTHEON, SCOTTISH-AVIATION, VOLPAR)
Model Type
Designator
Description Performance Information
Number & Type Engines/
Weight Class
Climb
Rate (fpm)
Descent
Rate (fpm)
SRS
Cat.
LAHSO
Group
BAe 748 (Andover, C-91) A748 2T/L 2,500 2,000 III 5
ATP Advance Turboprop (ATP) ATP 2T/L 3,000 3,000 III 6
BAC-111 One-Eleven BA11 2J/L 2,400 2,400 III 7
JO 7110.65S 2/14/08
Appendix A-9
Aircraft Information Fixed-Wing Aircraft
Model Type
Designator
Description Performance Information
Number & Type Engines/
Weight Class
Climb
Rate (fpm)
Descent
Rate (fpm)
SRS
Cat.
LAHSO
Group
BAC-167 Strikemaster JPRO 1J/S III
BAe HS 125 Series 1/2/3/400/600 H25A 2J/S+ 2,500 2,000 III 6
BAe-125-700/800 (C-29, U-125) H25B 2J/S+ 3,000 4,000 III 7
BAe-125-1000 H25C 2J/S+ 3,000 4,000 III 7
BAe-146-100 Statesman B461 4J/L 3,500 3,500 III 7
BAe-146-200 Quiet Trader, Statesman B462 4J/L 3,500 3,500 III 7
BAe-146-300 B463 4J/L III 7
BAe-3100 Jetstream 31 (T.Mk.3) JS31 2T/S+ 2200 2200 III 5
BAe-3200 Jetstream Super 31 JS32 2T/S+ 2600 2600 III 5
BAe-4100 Jetstream 41 JS41 2T/S+ 2200 III 7
Harrier, Sea Harrier HAR* 1J/L 5,000 8,000 III
Hawk, T-45 Goshawk, CT-155 Hawk HAWK 1J/S+ III
Jetstream 1 JS1 2T/S+ 2,200 2,200 III
Jetstream 3 JS3 2T/S+ 2,200 2,300 III
Jetstream 200 JS20 2T/S+ 2,200 2,200 III
Nimrod N1M 4J/L III
RJ-70 RJ70 4J/L III 7
RJ-85 RJ85 4J/L III 7
RJ-100 RJ1H 4J/L III 7
Tornado TOR 2J/L III
BRITTEN NORMAN LTD. (A subsidiary of Pilatus Aircraft LTD.) (UK)
(Also AVIONS FAIREY, BAC, BUCURESTI, DE HAVILLAND, HAWKER-SIDDELEY, IRMA, PADC, ROMAERO, VICKERS)
Model Type
Designator
Description Performance Information
Number & Type Engines/
Weight Class
Climb
Rate (fpm)
Descent
Rate (fpm)
SRS
Cat.
LAHSO
Group
BN-2, BN-2A/B Islander, Defender,
Maritime Defender
BN2P 2P/S 1,250 1,250 II 1
BN-2T Turbine Islander,
Turbine Defender
BN2T 2T/S 1,500 1,500 II 1
Trident TRID 3J/L 3,000 3,000 III
BN-2A Mk3 Trislander TRIS 3P/S 1,200 1,000 III 2
VC-10 VC10 4J/H 1,900 2,000 III
Viscount VISC 4T/L 1,200 1,500 III 10
BUSHMASTER AIRCRAFT CORP. (USA—see Aircraft Hydro Forming)
CAMAIR AIRCRAFT CORP. (USA)
(Also RILEY, TEMCO)
Model Type
Designator
Description Performance Information
Number & Type Engines/
Weight Class
Climb
Rate (fpm)
Descent
Rate (fpm)
SRS
Cat.
LAHSO
Group
480 Twin Navion 480 TNAV 2P/S 1,800 2,000 II
JO 7110.65S 2/14/08
Appendix A-10 Aircraft Information Fixed-Wing Aircraft
CANADAIR BOMBARDIER LTD. (Canada)
Model Type
Designator
Description Performance Information
Number & Type Engines/
Weight Class
Climb
Rate (fpm)
Descent
Rate (fpm)
SRS
Cat.
LAHSO
Group
CL-41 Tutor (CT-114) CL41 1J/S III
CL-44 Forty Four CL44 4T/L III
CL-44-O Guppy CL4G 4T/L III
CL-66, CV-580 (CC-109
Cosmopolitan)
CVLT 2T/L 1,500 1,500 III
CL-600/Challenger 699/601/604
(CC-144, CE-144)
CL60 2J/L 2,250 3,000 III 8
CL-600 Regional Jet CRJ-100, RJ-100 CRJ1 2J/L III 7
CL-600, Regional Jet CRJ-200,
RJ-200
CRJ2 2J/L III 7
CL-600 Regional Jet CRJ-700 CRJ7 2J/L III 7
CL-600 Regional Jet CRJ-900 CRJ9 2J/L III 8
T-33, CT-133 Silver Star (CL-30) T33 1J/L 2,000 2,000 III
CESSNA AIRCRAFT COMPANY (USA)
(Also AVIONES-COLOMBIA, COLEMILL, DINFIA, ECTOR, FMA, FUJI, REIMS, RILEY, SUMMIT, WREN)
Model Type
Designator
Description Performance Information
Number & Type Engines/
Weight Class
Climb
Rate (fpm)
Descent
Rate (fpm)
SRS
Cat.
LAHSO
Group
A-37 Dragonfly (318D/E), OA-37 A37* 2J/S 3,370 3,000 III
120 C120 1P/S 640 640 I 1
140 C140 1P/S 640 640 I 3
150, A150, Commuter, Aerobat C150 1P/S 670 1,000 I 1
152, A152, Aerobat C152 1P/S 750 1,000 I 1
170 C170 1P/S 690 1,000 I 4
172, P172, R172, Skyhawk,
Hawk XP, Cutlass (T-41, Mescalero)
C172 1P/S 650 1,000 I 1
172RG, Cutlass RG C72R 1P/S 650 1,000 I 1
175, Skylark C175 1P/S 850 1,000 I 2
177, Cardinal C177 1P/S 850 1,000 I 2
177, Cardinal RG C77R 1P/S 850 1,000 I 2
180, Skywagon 180 (U-17C) C180 1P/S 1,130 1,130 I 2
182, Skylane C182 1P/S 890 1,000 I 2
R182, TR182 (Turbo) Skylane RG C82R 1P/S 890 1,000 I 2
185, A185 Skywagon, Skywagon 185,
AgCarryall (U-17A/B)
C185 1P/S 1,000 1,000 I 2
188, A188, T188 AgWagon, AgPickup
AgTruck, AgHusky
C188 1P/S 1,000 1,000 I 1
190 C190 1P/S 1,090 1,090 I 2
195 (LC-126) C195 1P/S 1,200 1,200 I
205 C205 1P/S 965 1,000 I 3
206, P206m T206m TP206, U206,
TU206, (Turbo) Super Skywagon,
(Turbo) Super Skyland, (Turbo)
Skywagon 206, (Turbo) Stationair,
Turbo Stationair 6
C206 1P/S 975 1,000 I 2
JO 7110.65S 2/14/08
Appendix A-11
Aircraft Information Fixed-Wing Aircraft
Model Type
Designator
Description Performance Information
Number & Type Engines/
Weight Class
Climb
Rate (fpm)
Descent
Rate (fpm)
SRS
Cat.
LAHSO
Group
206 (turbine) C06T 1/T/S I
207 (Turbo) Skywagon 207, (Turbo)
Stationair 7/8
C207 1P/S 810 1,000 I 2
207 (turbine) C07T 1T/S I
208 Caravan 1, (Super)
Cargomaster, Grand Caravan (C-98,
U27)
C208 1T/S 1,400 1,400 I 3
210, T210, (Turbo) Centurion C210 1P/S 900 1,000 I 2
P210 Pressurized Centurion P210 1P/S 1,000 1,000 I
P210 (turbine) C10T 1T/S I
T303 Crusader C303 2P/S 3,500 3,000 II 2
310, T310 (U-3, L-27) C310 2P/S 2,800 2,000 II 4
320 (Executive) Skyknight C320 2P/S 2,900 2,000 II 5
335 C335 2P/S 2,200 2,000 II 4
336 Skymaster C336 2P/S 1,340 1,340 II
337, M337, MC337, T337B/C/D/E/F/H
(Turbo)
Super Skymaster (O-2)
C337 2P/S 1,250 1,500 II 3
T337G, P337 Pressurized Skymaster P337 2P/S 1,250 1,500 II 3
340 C340 2P/S 2,900 2,000 II 4
401, 402, Utililiner, Businessliner C402 2P/S 2,500 2,000 II 3
402 (turbine) C02T 2T/S II
404 Titan C404 2P/S 2,600 2,000 II 5
404 (turbine) C04T 2T/S II
F406 Caravan 2, Vigilant F406 2T/S 1,850 II 6
411 C411 2P/S 2,800 2,000 II 4
414, Chancellor 414 C414 2P/S 2,300 2,000 II 6
414 (turbine) C14T 2T/S II
421, Golden Eagle, Executive
Commuter
C421 2P/S II 6
421 (turbine) C21T 2T/S II
425, Corsair, Conquest 1 C425 2T/S 3,500 2,500 II 5
441 Conquest, Conquest 2 C441 2T/S 4,200 3,000 II 6
5000 Citation, Citation 1 C500 2J/S 3,100 3,500 III 6
501 Citation 1SP C501 2J/S 4,300 3,000 III 6
525 Citationjet Citation CJ1 C525 2J/S 3,000 III 7
525A Citation CJ2 C25A 2J/S 3,870 III
525B Citation CJ3 C25B 2J/S+ III
526 Citationjet C526 2J/S 3,000 III
550, S550, 552 Citation 2/S2/Bravo
(T-47, U-20)
C550 2J/S+ 5,300 3,000 III 7
551 Citation 2SP C551 2J/S 5,300 3,000 III 5
560 Citation 5/5 Ultra/5Ultra Encore
(UC-35, OT-47, TR-20)
C560 2J/S+ 6,000 3,500 III 8
650 Citation 3/6/7 C650 2J/S+ 3,900 4,000 III 8
680 Citation Sovereign C680 2J/S+ III
750 Citation 10 C750 2J/S+ 3,500 3,500 III 9
AW CAW 1P/S I
JO 7110.65S 2/14/08
Appendix A-12 Aircraft Information Fixed-Wing Aircraft
Model Type
Designator
Description Performance Information
Number & Type Engines/
Weight Class
Climb
Rate (fpm)
Descent
Rate (fpm)
SRS
Cat.
LAHSO
Group
O-1, TO-1, OE, L-19, TL-19 Bird Dog
(305,321)
O1 1P/S 1,150 1,150 I
T37 (318A/B/C) T37* 2J/S 3,000 3,000 III
T-50 Bobcat (AT-8, AT-17, UC-78,
Crane)
T50 2P/S II
DC-6 CDC6 1P/S I
C-34/37/38/145/165, Airmaster CMAS 1P/S I
CHAMPION (USA-see Bellanca Aircraft)
CHRISTEN INDUSTRIES, INC. (USA)
(Also AVIAT)
Model Type
Designator
Description Performance Information
Number & Type Engines/
Weight Class
Climb
Rate (fpm)
Descent
Rate (fpm)
SRS
Cat.
LAHSO
Group
A-1 Huskey HUSK 1P/S 1,500 1,500 I
CIRRUS (USA)
Model Type
Designator
Description Performance Information
Number & Type Engines/
Weight Class
Climb
Rate (fpm)
Descent
Rate (fpm)
SRS
Cat.
LAHSO
Group
SR-20, SR-20 SRV, SRV SR20 1P/S I 1
SR-22 SR22 1P/S I 1
VK-30 Cirrus VK3P 1P/S I
COLEMILL (USA) (See BEECH, PIPER, CESSNA)
CONSTRUCCIONES AERONAUTICAS (CASA) (Spain)
(Also NURTANIO, NUSANTARA)
Model Type
Designator
Description Performance Information
Number & Type Engines/
Weight Class
Climb
Rate (fpm)
Descent
Rate (fpm)
SRS
Cat.
LAHSO
Group
C-212 Aviocar (T-12, TE-12, TR-12,
D-3, Tp89)
C212 2T/S+ 900 900 III 5
CURTISS-WRIGHT CORP. (USA)
Model Type
Designator
Description Performance Information
Number & Type Engines/
Weight Class
Climb
Rate (fpm)
Descent
Rate (fpm)
SRS
Cat.
LAHSO
Group
C-46 Commando (CW-20) C46 2P/L 600 700 III
JO 7110.65S 2/14/08
Appendix A-13
Aircraft Information Fixed-Wing Aircraft
DASSAULT-BREGUET (France)
Model Type
Designator
Description Performance Information
Number & Type Engines/
Weight Class
Climb
Rate (fpm)
Descent
Rate (fpm)
SRS
Cat.
LAHSO
Group
1150 Atlantic, Altantique 2 ATLA 2T/L III
Alpha Jet AJET 2J/S III
Falcon 10/100, Mystere 10/100 FA10 2J/S+ 2,300 1,600 III 8
Falcon 20/100, Mystere 20/200,
Gardian (HU-25, (T-11, TM-11)
FA20 2J/S+ 2,000 2,200 III 7
Falcon 50, Mystere 50 (T-16) FA50 3J/S+ 1,800 1,600 III 8
Falcon 900, Mystere 900 (T-18) F900 3J/L 2,000 1,700 III 8
Falcon 2000 F2TH 2J/S+ 2,500 1,500 III 8
Jaguar JAGR 2J/S+ III
Mirage 2000, Vajara MIR2 1J/S+ III
Mirage 3/5/50 (F-103) MIRA 1J/S+ III
Mirage F1 (C-14, CE-14) MRF1 1J/S+ III
Super Etendard ETAR 1J/S+ III
DEHAVILLAND (Canada/UK)
(Also AIRTECH, HAWKER-SIDDELEY, OGMA, RILEY, SCENIC)
Model Type
Designator
Description Performance Information
Number & Type Engines/
Weight Class
Climb
Rate (fpm)
Descent
Rate (fpm)
SRS
Cat.
LAHSO
Group
DHC-1 DHC1 1P/S 900 1,000 I 1
DHC-2 Mk1 Beaver (U-6, L-20) DHC2 1P/S 840 1,000 I 2
DHC-2 Mk3 Turbo Beaver DH2T 1T/S 1,220 1,000 I 2
DHC-3 Otter (U-1, NU-1, UC) DHC3 1P/S 750 1,000 I 1
DHC-3 Turbo Otter DH3T 1T/S I
DHC-4 Caribou (C-7, CV-2) DHC4 2P/S+ 1,350 1,000 III 5
DHC-5 (C-8, CV-7, CC-115, C-115) DHC5 2T/L 2,000 1,500 III 1
DHC-6 Twin Otter (UV-18, CC-138) DHC6 2T/S 1,600 1,800 II 4
DHC-7 Dash 7 (O-5, EO-5) DHC7 4T/L 4,000 4,000 III 2
DHC8 – 100 Dash 8 (E-9, CT-142,
CC-142)
DH8A 2T/L 1,500 1,500 III 4
DHC8 – 200 Dash 8 DH8B 2T/L 1,500 1,500 III 4
DHC8 – 300 Dash 8 DH8C 2T/L 1,500 1,500 III 5
DHC8 – 400 Dash 8 DH8D 2T/L 2,500 2,500 III
DH-104 Dove, Sea Devon DOVE 2P/S 1,420 1,420 II 4
DH-114 Heron HERN 4P/S+ 1,075 1,075 III 8
DIAMOND (Canada)
(Also HOAC)
Model Type
Designator
Description Performance Information
Number & Type Engines/
Weight Class
Climb
Rate (fpm)
Descent
Rate (fpm)
SRS
Cat.
LAHSO
Group
DA-20/22, DV-20 Katana,
Speed Katana
DV20 1P/S 525 500 I 2
DA-42 TwinStar DA42 2P/S 1,100 500 II 2
JO 7110.65S 2/14/08
Appendix A-14 Aircraft Information Fixed-Wing Aircraft
DORNIER GmbH (FRG)
(Also CASA, HINDUSTAN. Also see FAIRCHILD-DORNIER)
Model Type
Designator
Description Performance Information
Number & Type Engines/
Weight Class
Climb
Rate (fpm)
Descent
Rate (fpm)
SRS
Cat.
LAHSO
Group
228 D228 2T/S+ 2,000 2,000 III 2
328 D328 2T/S+ 2,000 2,000 III 7
27 DO27 1P/S 700 800 I 1
Do 28 A/B (Agur) DO28 2P/S 1,500 1,500 II
Do 28D/D-1/D-2, 128-2 Skyservant D28D 2P/S 1,000 - II 1
Do-28D-6, 128-6 Turbo Skyservant D28T 2T/S 1,500 - II 1
ECLIPSE AVIATION (USA)
Model Type
Designator
Description Performance Information
Number & Type Engines/
Weight Class
Climb
Rate (fpm)
Descent
Rate (fpm)
SRS
Cat.
LAHSO
Group
Eclipse 500 EA50 2J/S 1,725 3,000 III 4
EMBRAER (Brazil)
Model Type
Designator
Description Performance Information
Number & Type Engines/
Weight Class
Climb
Rate (fpm)
Descent
Rate (fpm)
SRS
Cat.
LAHSO
Group
CBA-123 Vector VECT 2T/S+ III
EMB-110/111 Bandeirante (C-95,
EC-95, P-95, R-95, SC-95)
E110 2T/S+ 1,500 1,500 III 7
EMB-120 Brasilia (VC-97) E120 2T/S+ 2,300 2,300 III 7
EMB-121 Xingu (VU-9, EC-9) E121 2T/S+ III
EMB-135, ERJ-135/140 E135 2J/L 2,410 2,030 III 7
EMB-145, ERJ-145 (R-99) E145 2J/L 2,350 2,190 III 7
EMB-145XR E45X 2J/L III 7
EMB-170/175 E170 2J/L III 7
EMB-190/195 E190 2J/L III 7
EXTRA (FRG)
Model Type Designator Description Performance Information
Number & Type Engines/
Weight Class
Climb
Rate (fpm)
Descent
Rate (fpm)
SRS
Cat.
LAHSO
Group
200 E200 1P/S 1,000 1,000 I
230 E230 1P/S 1,500 1,500 I
300, 350 E300 1P/S 2,500 1,500 I
400 E400 1P/S 1,500 1,500 I
500 E500 1T/S 1,800 1,800 I
JO 7110.65S 2/14/08
Appendix A-15
Aircraft Information Fixed-Wing Aircraft
FAIRCHILD DORNIER (USA/FRG)
(Also CONAIR, FAIRCHILD-HILLER, FLEET, FOKKER, KAISER, PILATUS, SWEARINGEN)
Model Type Designator Description Performance Information
Number & Type Engines/
Weight Class
Climb
Rate (fpm)
Descent
Rate (fpm)
SRS
Cat.
LAHSO
Group
228 D228 2T/S+ 2,000 2,000 III
328 D328 2T/S+ 2,000 2,000 III
328JET, Envoy 3 J328 2J/S+ III 6
728JET, Envoy 7 J728 2J/L III
FAIRCHILD INDUSTRIES (USA)
(Also CONAIR, FAIRCHILD-HILLER, FLEET, FOKKER, KAISER, PILATUS, SWEARINGEN)
Model Type Designator Description Performance Information
Number & Type Engines/
Weight Class
Climb
Rate (fpm)
Descent
Rate (fpm)
SRS
Cat.
LAHSO
Group
A-10, OA-10 Thunderbolt 2 A10* 2J/L 6,000 5,000 III
C-119, R4Q Flying Box Car (F-78) C119 2P/L 750 750 III 5
C-123 Provider C123 2P/L 890 1,000 III
F-27, FH-227 F27 2T/L 3,000 3,000 III 5
M-62 (PT-19/23/26, T-19 Cornell) FA62 1P/S 650 650 I
Pilatus/Peacemaker/Porter PC6P 1P/S 580 600 I
PC-6 Heli-Porter PC6T 1T/S 580 600 I
Merlin 2 SW2 2T/S 2,350 2,500 II 6
SA-226TB, SA-227TT Merlin 3,
Fairchild 300
SW3 2T/S+ 2,350 2,500 III 5
SA-226AC, SA-227AC/AT Metro,
Merlin 4, Expediter
SW4 2T/S+ 2,400 2,500 III 5
FOKKER BV (Netherlands)
(Also FAIRCHILD, FAIRCHILD-HILLER)
Model Type Designator Description Performance Information
Number & Type Engines/
Weight Class
Climb
Rate (fpm)
Descent
Rate (fpm)
SRS
Cat.
LAHSO
Group
F-27 Friendship, Troopship,
Maritime (C-31, D-2)
F27 2T/L 3,000 3,000 III
F-28, Fellowship F28 2J/L 4,650 2,000 III 7
50, Maritime Enforcer F50 2T/L 3,500 3,500 III 3
60 F60 2T/L 3,500 3,500 III
70 F70 2J/L 4,500 3,000 III
100 F100 2J/L 3,500 3,500 III 7
GAF (Australia)
Model Type Designator Description Performance Information
Number & Type Engines/
Weight Class
Climb
Rate (fpm)
Descent
Rate (fpm)
SRS
Cat.
LAHSO
Group
N2/22/24 Nomad, Floatmaster,
Missionmaster, Searchmaster
NOMA 2T/S 1,300 1,100 II 2
JO 7110.65S 2/14/08
Appendix A-16 Aircraft Information Fixed-Wing Aircraft
GATES LEARJET CORP. (USA)
(Also LEAR JET, LEARJET, SHIN MEIWA)
Model Type Designator Description Performance Information
Number & Type Engines/
Weight Class
Climb
Rate (fpm)
Descent
Rate (fpm)
SRS
Cat.
LAHSO
Group
23 LJ23 2J/S 4,500 4,000 III 8
24 LJ24 2J/S+ 4,500 4,000 III 7
25 LJ25 2J/S+ 4,500 4,000 III 9
28, 29 LJ28 2J/S+ 4,500 4,000 III 7
31 LJ31 2J/S+ 4,500 4,000 III 7
35, 36 (C-21, RC-35, RC-36, U-36) LJ35 2J/S+ 4,500 4,000 III 9
40 LJ40 2J/S+ III
45 LJ45 2J/S+ III
55 LJ55 2J/S+ 5,000 4,000 III 8
60 LJ60 2J/S+ 5,000 4,000 III 10
GENERAL DYNAMICS CORP. (USA)
(Also BOEING CANADA, CANADAIR, CANADIAN VICKERS, CONSOLIDATED, CONVAIR, FOKKER, GRUMMAN,
KELOWNA, LOCKHEED, LOCKHEED MARTIN, MITSUBISHI, SABCA, SAMSUNG, TUSAS)
Model Type Designator Description Performance Information
Number & Type Engines/
Weight Class
Climb
Rate (fpm)
Descent
Rate (fpm)
SRS
Cat.
LAHSO
Group
Canso/Catalina*** CAT 2P/S+ 600 600 III 7
Convair 240/340/440, Liner, HC-131 CVLP 2P/L 1,000 800 III 7
Convair 540/580/600/640 CVLT 2T/L 1,500 1,500 III 7
F-111, EF-111, (RF-111 Aardvark,
Raven
F111* 2J/L 5,000 5,000 III
F-16 A/B/C/D/N, NF-16, TF-16
Fighting Falcon, Netz, Barak, Brakeet
F16* 1J/L 8,000 5,000 III
F-16XL Fighting Falcon F16X* 1J/L III
Valiant VALI 1P/S 600 750 I
GREAT LAKES (USA)
Model Type Designator Description Performance Information
Number & Type Engines/
Weight Class
Climb
Rate (fpm)
Descent
Rate (fpm)
SRS
Cat.
LAHSO
Group
2T-1 Sport Trainer, Sport G2T1 1P/S 1,000 800 I
GROB (FRG)
Model Type Designator Description Performance Information
Number & Type Engines/
Weight Class
Climb
Rate (fpm)
Descent
Rate (fpm)
SRS
Cat.
LAHSO
Group
G109 Ranger (Vigilant) G109 1P/S 600 600 I 2
G115 A/B/C/D/E, Bavarian (Heron),
Tutoa
G115 1P/S 1,200 1,100 I
G-120 G120 1P/S 1,280 I
JO 7110.65S 2/14/08
Appendix A-17
Aircraft Information Fixed-Wing Aircraft
GRUMMAN AEROSPACE CORP. (USA)
(Also AERO MOD, AMERICAN GENERAL, GRUMMAN AMERICAN, GULFSTREAM AMERICAN
MID-CONTINENT, NORTHROP GRUMMAN, SERV-AERO)
Model Type Designator Description Performance Information
Number & Type Engines/
Weight Class
Climb
Rate (fpm)
Descent
Rate (fpm)
SRS
Cat.
LAHSO
Group
A-6, EA-6, KA-6 Intruder,
Prowler (G-128)
A6* 2J/L 7,500 5,000 III
AA1 Trainer,Tr2, T-Cat, Lynx AA1 1P/S 850 1,250 I 1
AA-5, Traveller, Cheetah Tiger AA5 1P/S 660 1,000 I 1
C-1, TF Trader (G-96) G96 2P/S+ III
C-2 Greyhound C2 2T/L 1,000 2,200 III
E-2, TE-2, Hawkeye, Daya E2 2T/L 2,690 3,000 III
F-3F (G-11/32), Replica F3F 1P/S I
F-6F Hellcat (G-50) HCAT 1P/S+ III
F-7F Tigercat (G-51) TCAT 2P/S+ III
F-9F Panther (G-79) F9F 1JS+ III
F-14 Tomcat F14* 2J/L 6,000 4,000 III
G-164 Ag-Cat, Super Ag-Cat G164 1P/S 1,500 1,500 I 1
G164 Turbo Ag-Cat G64T 1T/S 1,500 1,500 I 1
G-21 A/38/39 Goose (JRF)*** G21 2P/S 1,000 1,000 II
G-44 Widgeon (J4F)*** G44 2P/S 1,000 1,500 II 5
G-73 Mallard*** G73 2P/S+ 1,600 1,600 III 6
G-73T Turbo Mallard*** G73T 2T/S+ III
G-1159, G-1159B Gulfstream
2/2B/2SP (C-20J, VC-111)
GLF2 2J/L 5,000 4,000 III 8
GA-7 Cougar GA7 2P/S 1,600 1,500 II 1
HU-16, SA-16, UF Albatross
(G-64/111)***
U16 2P/S+ 1,500 1,500 III 4
OV-1, RV-1, AO-1 Mohawk (G-134) V1 2T/S+ 2,100 1,300 III
S-2, S2F, P-16 Tracker (G-89) S2P 2P/S+ III
S-2 Turbo Tracker S2T 2T/S+ III
X-29 (712) X29 1J/S+ III
GULFSTREAM AEROSPACE CORP. (USA)
(Also GRUMMAN, GRUMMAN AMERICAN, GULFSTREAM, GULFSTREAM AMERICAN, IAI)
Model Type Designator Description Performance Information
Number & Type Engines/
Weight Class
Climb
Rate (fpm)
Descent
Rate (fpm)
SRS
Cat.
LAHSO
Group
690 Jetprop Commander 840/900 AC90 2T/S 2,500 2,500 II
695 Jetprop Commander 980/1000 AC95 2T/S 2,500 2,500 II
AA-1 T-Cat, Lynx AA1 1P/S 850 1,250 I
AA-5 Traveler, Cheetah, Tiger AA5 1P/S 660 1,000 I
GA-7 Cougar GA7 2P/S 1,600 1,500 II
GAC 159-C, Gulfstream 1 G159 2T/S+ 2,000 2,000 III 7
G-1159, G-1159B/TT Gulfstream
2/2B/2SP/2TT
GLF2 2J/L 5,000 4,000 III
G-1159A Gulfstream 3/SRA-1,
SMA-3 (C20A/B/C/D/E)
GLF3 2J/L 5,000 4,000 III 8
JO 7110.65S 2/14/08
Appendix A-18 Aircraft Information Fixed-Wing Aircraft
Model Type Designator Description Performance Information
Number & Type Engines/
Weight Class
Climb
Rate (fpm)
Descent
Rate (fpm)
SRS
Cat.
LAHSO
Group
G-1159C Gulfstream 300/4/4SP/
400/SRA-4 (C-20F/G/H, S102,
Tp102, U-4)
GLF4 2J/L 5,000 4,000 III 8
G-1159D Gulfstream 5/500/550
(C-37)
GLF5 2J/L 5,000 4,000 III 7
HAMILTON AVIATION (USA)
(Also VOLPAR)
Model Type Designator Description Performance Information
Number & Type Engines/
Weight Class
Climb
Rate (fpm)
Descent
Rate (fpm)
SRS
Cat.
LAHSO
Group
Westwind 2/3 B18T 2T/S 2,000 2,000 II 1
Little Liner BE18 2P/S 1,400 1,000 II
T-28 Nomair T28 1P/S 2,500 2,500 I
HANDLEY PAGE (UK)
(Also BRITISH AEROSPACE, JETSTREAM, SCOTTISH AVIATION, VOLPAR)
Model Type Designator Description Performance Information
Number & Type Engines/
Weight Class
Climb
Rate (fpm)
Descent
Rate (fpm)
SRS
Cat.
LAHSO
Group
HP-137 Jetstream 1 JS1 2T/S+ 2,200 2,200 III
HP-137 Jetstream 200 (T.Mk1/2) JS20 2T/S+ 2,200 2,200 III
HELIO AIRCRAFT COMPANY (USA)
Model Type Designator Description Performance Information
Number & Type Engines/
Weight Class
Climb
Rate (fpm)
Descent
Rate (fpm)
SRS
Cat.
LAHSO
Group
H-391/392/395/250/295/700/800,
HT-295 Courier, Strato-Courier,
Super Courier (U-10)
COUR 1P/S 850 1,000 I 1
HST-550 Stallion (AU-24) STLN 1T/S 2,200 2,200 I 1
H-500 Twin Courier (U-5) TCOU 2P/S 1,250 1,500 II 1
HFB (FRG)
(Also MBB)
Model Type Designator Description Performance Information
Number & Type Engines/
Weight Class
Climb
Rate (fpm)
Descent
Rate (fpm)
SRS
Cat.
LAHSO
Group
HFB-320 Hansa HF20 2J/S+ 4,500 4,500 III 7
HOWARD (USA)
Model Type Designator Description Performance Information
Number & Type Engines/
Weight Class
Climb
Rate (fpm)
Descent
Rate (fpm)
SRS
Cat.
LAHSO
Group
