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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.

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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

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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

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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

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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

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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

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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

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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

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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

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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