BUSINESS AND GENERAL AVIATI RELOADABLE CUSTOMER DEFINITIS (RCD) All options must be completed, even if selected. Worksheets with blank entries will not be processed until all questionable selections are clarified. You can submit the completed worksheet to Honeywell Order Administration, via fax in USA (913-712-1335) or INTL (+420 234 625 777). Refer to the Product Description, Flight Safety Functions Enhanced Ground Proximity Warning System, Honeywell document 060-4564-001, for more information about each function. The relevant product description section numbers are listed in parentheses for the items below. NOTE 1: A/C type number is a 1 to 3-digit number used by the EGPWS model to define the installation. This number can be found using one following methods: Conducting a Level 3 Self-Test on the aircraft per Line Maintenance Manual MK V, MK VI, MK VII, MK VIII; Enhanced Ground Proximity Warning Systems, Honeywell document 060-4199-180. Examining EGPWS aircraft program pin wiring against the Interface Control Document for the Mark V Enhanced Ground Proximity Warning System (MKV EGPWS), Honeywell document 993-0976-401. Examining EGPWS aircraft program pin wiring against the Interface Control Document for the Mark VII Enhanced Ground Proximity Warning System (MKVII EGPWS), Honeywell document 993-1076-401. NOTE 2: MK VII aircraft types 3, 4, 5, 7 are generic, no windshear aircraft types that can be used with multiple airframes. For example, MK VII EGPWS A/C type 4 is a generic, Biz-Jet, no windshear configuration that may be used on Falcon, Gulfstream, Cessna and other OEM Biz-Jet aircraft. The RCD will not distinguish between aircraft models, only aircraft type numbers. If more than one aircraft model has EGPWS installed and is using a MK VII generic aircraft type, then multiple RCDs will be required. Complete the worksheet, listing all aircraft using the generic aircraft types, and send to Honeywell for evaluation. NOTE 3: the distance the GPS antenna is located, from the nose aircraft to the center antenna, rounded up to the nearest 5 foot. (i.e. If distance measured is 11 feet, then round up to 15 feet). NOTE 4: MK V EGPWS model is the following part numbers: 965-0976-XXX-XXX-XXX. MK VII EGPWS model is the following part numbers: 965-1076-XXX-XXX-XXX. (-XXX can be various 3-digit number sequences) NOTE 5: When selected the SmartRunway/SmartLanding functions can annunciate the Units of Measure for Distance Remaining Landing and Roll-out (4.2.4), Runway End (4.2.5), Approaching Short Runway INAIR (4.3.1), Insufficient Runway on Ground (4.3.3), Rejected Takeoff (4.3.7) and Distance Remaining (8.0) advisories. FIRST represents always for Short Runway, Insufficient Runway and Runway End, and the first callout only for sequential advisories. OTHER may be used to select specific advisories to be announced with the Unit of Measure. NOTE 6: The following table indicates for each function the type of message and whether the alert level is considered a caution or advisory message. Visual messages on the Terrain display can be selected for each aural annunciation except for the (8.0), RAAS (4.2.4 and 4.3.7) and the RAAS Runway End (4.2.5) callouts. Function (Product Description Reference paragraph) Type of Message Alert Level Approaching Short Runway In Air (4.3.2) Taxiway Landing (4.3.8) Monitor Landing Flaps (5.2.1) Monitor Excessive Approach Angle (5.2.2) Monitor Excessive Approach Speed (5.2.3) Monitor Unstable (5.2.4) Monitor (8.2) Altimeter Monitor Below Transition Altitude (6.2.1) SmartLandingTM Approaching Runway In Air (4.2.1) Approaching Short Runway In Air (4.3.1), Landing and Roll-out (4.2.4) Runway End (4.2.5) Page 1 of 9
BUSINESS AND GENERAL AVIATI RELOADABLE CUSTOMER DEFINITIS (RCD) Function (Product Description Reference paragraph) Altimeter Monitor Above Transition Altitude (6.2.2) Type of Message Alert Level SmartRunwayTM Approaching Runway On Ground (4.2.2) On Runway On Ground (4.2.3) Extended Holding On Runway (Initial and Repeat) (4.3.5) Insufficient Runway On Ground (4.3.3) Insufficient Runway On Ground (4.3.4), Rejected Takeoff (4.3.7) Taxiway Takeoff () (4.3.6.1) Taxiway Takeoff () (4.3.6.2) Takeoff Flap Configuration Monitor (7.2) Approaching Short Runway In Air (4.3.2) Taxiway Landing (4.3.8) Approaching Runway In Air (4.2.1) Approaching Short Runway In Air (4.3.1), Landing and Roll-out (4.2.4) Runway End (4.2.5) NOTE 7: The Monitor will be triggered when either the aircraft reaches the specified distance from the selected end runway or the specified percentage of runway remaining, depending on which provides the longer distance remaining. NOTE 8: When selected 450-550, the RAAS In Air advisory is suppressed between 550 feet and 450 feet above runway elevation to allow normal 500-foot altitude call outs and/or crew procedures without conflict. The option, 350450, will suppress the RAAS In Air advisory to allow the 400-foot altitude call outs in Airbus aircraft. Most aircraft should select 450-550. NOTE 9: RAAS Short and Insufficient Runway functions do not take into account aircraft performance factors such as aircraft weight, wind, runway conditions, slope, air temperature and altitude of airport. This information is intended to enhance the flight crew awareness by identifying that the runway length available may be marginal for the aircraft type. Nominal Runway Lengths: value rounded up to the nearest 100 ft (30 m). If advisory is turned, then leave blank. If available runway length is to always be annunciated, then enter ALWAYS. The RAAS algorithm processes distances in feet. If the operator selects the Meters option, and the nominal runway lengths listed are in meters, Honeywell will convert the meters value into feet using the formula (Feet = Meters x 3.280839895). When the advisories are triggered, the algorithm recalculates and provides distance advisories in meters. NOTE 10: If a function is enabled and the signals required for that function are failed or not available on the aircraft, then the function will be inoperative. For a Table of aircraft which support the Excessive Speed Monitor, Takeoff Flap Configuration Monitor and Altimeter Monitor see the Product Description 060-4564-001 Appendix H. NOTE 11: The operator/installer may use the COMMENTS block on page 10 or write freehand notes anywhere practical in the worksheet to communicate any instructions not specifically covered by current available selections. The operator/installer may append more than one worksheet if the number of separate aircraft types is greater than 9. Page 2 of 9
BUSINESS AND GENERAL AVIATI RELOADABLE CUSTOMER DEFINITIS (RCD) data by mouse clicking desired box, then typing the information requested or by selecting the appropriate radio button. Click on the Acrobat Text Select Tool icon if the worksheet appears unresponsive. Aircraft Operator RESET FORM Date (MM/DD/YYYY) Customer Name/Company Customer Phone/Fax/Email For Honeywell Use only Customer EGPWS P/N Purchase Order # EGPWS S/N Required Ship Date //////////////////////////////// OEM Aircraft Model Common Selections //////////////////////////////// G-IV OEM Aircraft TN or SN (leave blank for fleet) EGPWS Aircraft Type number (Note 1, 2) 79 MK V or MK VII EGPWS (Note 4) MK V GPS Antenna Location (Note 3) 15ft Select Distance Unit of Measure Set Distance Unit of Measure for and RAAS & Short Runway callouts only Feet Select Annunciation of Unit of Measure Optional annunciation of Units of Measure during advisory (Note 5) //////////////////////////////// Meters FIRST OTHER: Visual Messages on Terrain Display for Non-TSO Functions Enable Visual Messages //////////////////////////////// Enables Visual messages on the Terrain Display (Note 6) All Messages Non-routine Messages Only s Only None Page 3 of 9
BUSINESS AND GENERAL AVIATI RELOADABLE CUSTOMER DEFINITIS (RCD) /////////////////////////////////////////////////////// ///////////////////////// SMART LANDING Select Voice Gender (all aurals) Male Female Select Suppress Window 450-550 (ft) 350-450 (ft) ///////////////////////// (Note 8) (Note 8) Enable Approaching Runway in air (4.2.1) Select, Landing and Roll-out (4.2.4) 50% of Runway 1000 ft (300 m) 2000 ft (600 m) Enable Runway End advisory (4.2.5) Select Approaching Short Runway in air advisory (4.3.1) (Note 9) Select Short Runway in air (4.3.2) (Note 6,9) (Note 1) /////////////////////////////////////////////////////// RUNWAY AWARENESS AND ADVISORY SYSTEM (RAAS) Enable RAAS (Note 1, 8) TM Short Runway Length in air (ft or m) 4900ft Short Runway Length in air (ft or m) 4400ft 3000 ft (900 m) ALWAYS 4000 ft (1200 m) 5000 ft (1500 m) (enter Nominal Runway Runway Length table (enter Nominal Length in (enter Nominal Runway Runway Length Length in table (enter Nominal Enable Taxiway Landing (4.3.8) Select RAAS Enable/Inhibit discrete None Ground or 28V = Inhibit Ground or 28V = Enable Note: RAAS uses the same Enable/Inhibit discrete as Monitor and Takeoff Flap Configuration Monitor. Page 4 of 9
BUSINESS AND GENERAL AVIATI RELOADABLE CUSTOMER DEFINITIS (RCD) //////////////////////////////////////////////// STABILIZED APPROACH MITOR Enable Monitor (5.0) Select Voice Gender Select Monitor Enable/Inhibit discrete //////////////////////////////////////////////// Female Voice Male Voice None Ground or 28V = Inhibit Ground or 28V = Enable If both RAAS and Monitor Enable/Inhibit discrete are being activated, would you like the same discrete to apply to both? Enable Landing Flap Monitor (5.2.1) Upper Flap Gate Alert Lower Flap Gate Alert Flap Gate Maximum Altitude the the value value (in (in feet) feet) for for the the selected selected gates gates in table below. below. The upper Flap The Flap gate gate defines defines the the maximum maximum altitude altitude (AFE) (AFE) of the upper Stabilized Monitor Flap Flap gate. gate. 500 500 ft ft to to 1400 1400 ft, ft, typically typically is is 950 950 ft. ft. Approach Monitor The Flap gate gate defines defines the the lower The lower Flap the maximum maximum altitude altitude (AFE) (AFE) of Stabilized Approach Monitor Monitor Flap Flap gate. gate. 500 500 ft ft to to 1000 1000 ft, ft, typically typically is is 600 600 ft. ft. The The lower gate gate requires requires that that the the aircraft aircraft be be lined lined up up with with the the runway. runway. lower (Note 1) upper Flap gate (ft) AFE 950ft lower Flap gate (ft) AFE 600ft Enable Excessive Approach Angle Monitor (5.2.2) Enable Excessive Approach Speed Monitor (5.2.3) Checklist (Note 10) The required REFERENCE SPEED label was added to many MK V Biz-Jet aircraft types in -234 software release. It is NOT available with the MKVII EGPWS. Use the area below if more than one FMS type used. //////////////////////////////////////////////////////// Enable Altimeter Monitor (6.0) ALTIMETER MITOR //////////////////////////////////////////////////////// Female Voice Male Voice Enable Altimeter Monitor Below Transition Altitude (6.2.1) Enable Altimeter Monitor Above Transition Altitude (6.2.2) Select Voice Gender Page 5 of 9
BUSINESS AND GENERAL AVIATI RELOADABLE CUSTOMER DEFINITIS (RCD) //////////////////////////////////////////////////// Enable Monitor (8.0) (Note 7) Select Voice Gender Configure callout Distance (Long Runway) LG LANDING MITOR /////////////////////////////////////////////////// Female Voice Male Voice "Long Landing" callout callout "" "Deep callout "Deep Landing" Landing" callout Configure either from from the the Configure the the trigger trigger point point for for the the Long Landing Monitor Monitor to to be be measured measured either approach approach end end or or the the departure departure end end of the runway. runway. Departure Approach Distance from from selected selected end end in table below below (1 (1 to to 10,000 10,000 feet feet (3000 (3000 meters)). meters)). Distance Percentage (Short Runway) Percentage (%) (%) of of runway runway remaining remaining in table below. below. Percentage Percentage Remaining (0 (0 < <K K< < 1) 1) -- This This is is the the % % of of runway runway remaining remaining that that Percentage Remaining would trigger trigger the the aural aural ifif aircraft aircraft is is not not on on the the runway. runway. For For example, example, a a setting setting of of would 0.75 (75%) trigger the 0.75 (75%) would would trigger the aural aural ifif the the aircraft aircraft is is not not down down and and has has reached reached the point of of having having 75% 75% of the runway remaining. the point runway remaining. Distance Remaining (Long Runway) Configure the the trigger trigger point point for for the the Long Landing Distance Remaining Monitor to be Configure Monitor to be measured either either from from the the approach approach end end or or the the departure departure end end of the runway. runway. measured Departure Approach Distance from from selected selected end end in table below below (1 (1 to to 10,000 10,000 feet feet (3000 (3000 meters)). meters)). Distance Distance Remaining Percentage (Short Runway) Percentage Percentage (%) (%) of of runway runway remaining remaining in table below. below. Distance Remaining (0 (0 < <K K< < 1) 1) -- This This is is the the % % of of runway runway remaining remaining that that would would trigger the the Distance Callouts. For trigger Remaining Callouts. For example, example, a a setting setting of of 0.75 0.75 (75%) (75%) would trigger trigger the the Distance Remaining Callouts Callouts ifif the the aircraftpassed aircraft passedthe thepoint pointofof would having remaining. having 75% 75% of the runway runway remaining. (Note 1,7) Distance (ft or m) Percentage (%) (ft or m) Distance Remaining Percentage (%) 2000ft 75% 2000ft 75% Select Enable/Inhibit discrete Note: Monitor uses the same Enable/Inhibit discrete as RAAS and Takeoff Flap Configuration Monitor. RAAS must be activated to activate this Enable/Inhibit but RAAS functions do not need to be selected. Select the Enable/Inhibit discrete RAAS section of this worksheet. Page 6 of 9
BUSINESS AND GENERAL AVIATI RELOADABLE CUSTOMER DEFINITIS (RCD) /////////////////////////////////////////////////////// ///////////////////////// SMART RUNWAY TM /////////////////////////////////////////////////////// RUNWAY AWARENESS AND ADVISORY SYSTEM (RAAS) Enable Approaching Runway on ground (4.2.2) Enable On Runway on ground (4.2.3). Select Insufficient Runway Length on ground advisory (4.3.3) (Note 9) Select Short Runway on ground (4.3.4) (Note 6,9) (Note 1) Short Runway Length on gnd (ft or m) 4400ft Short Runway Length on gnd (ft or m) 3900ft ALWAYS enter Nominal Nominal Runway Runway Length Length in table ((enter Nominal Runway Runway Length Length in table (enter ( enter Nominal 60 90 60 90 Select Extended Holding time on runway, repeats (4.3.5) Enable Taxiway Take-off (4.3.6) Select Rejected Take-off (4.3.7) 50% of Runway 1000 ft (300 m) 2000 ft (600 m) 30 Select Extended Holding time on runway, initial (4.3.5) ///////////////////////// 120 180 240 300 120 180 240 300 3000 ft (900 m) 4000 ft (1200 m) 5000 ft (1500 m) Page 7 of 9
BUSINESS AND GENERAL AVIATI RELOADABLE CUSTOMER DEFINITIS (RCD) ////////////////////////////////////// Enable Takeoff Flap Configuration Monitor (7.0) Select Voice Gender Select Enable/Inhibit discrete TAKE FLAP CFIGURATI MITOR ////////////////////////////////////// Female Voice Male Voice Note: Takeoff Flap Configuration Monitor uses the same Enable/Inhibit discrete as RAAS and Monitor. RAAS must be activated to activate this Enable/Inhibit but RAAS functions do not need to be selected. Select the Enable/Inhibit discrete RAAS section of this worksheet. Flap Angle $QJOH SRVLWLRQ table below. below. the the value value (in (in degrees) degrees) for for the the Flap position in Minimum position, in in degrees degrees (0-50), (0-50), required required for for safe safe takeoff. takeoff. Minimum flap flap angle angle position, Maximum flap flap angle angle position, Maximum position, in in degrees degrees (0-50), (0-50), required required for for safe safe takeoff. takeoff. Note: Note: On On some some aircraft aircraft the the Flap Flap Handle Handle to to Flap Flap Angle Angle has has an an associated associated tolerance. tolerance. The The settings these tolerances. tolerances. settings entered entered below below should should account account for for these (Note 1) Takeoff Flap Angle Minimum Setting 0.5 Takeoff Flap Angle Maximum Setting 15.5 Flap Angle Checklist This monitor requires a digital ARINC 429 Flap Angle or Flap Discrete Word, Synchro (MK VII only) or Flap Position discrete as a source of Flap Angle. Example : CL-601/3A aircraft provide Flap Position discrete of 0 (all open), 20, 30 and 45. COMMENTS: Page 8 of 9
BUSINESS AND GENERAL AVIATI RELOADABLE CUSTOMER DEFINITIS (RCD) Reconfigure RCD Volume NO YES (if Yes, enter the values table RCD volume changes are available using procedure 060-4314-080 Data Gathering Test Procedure. Please contact your Honeywell Field Service Representative for assistance. Volume Setting in db 060-4314-080 Paragraph / Default level 2.2 2.2 Approaching Approaching Runway Runway On On Ground Ground -6dB 2.3 2.3 On On Runway Runway // Insufficient Insufficient Runway Runway On On Gnd Gnd -6dB 2.4 2.4 Extended Extended Holding Holding Initial Initial and and Repeated Repeated -6dB 2.5 Distance Remaining Rejected Rejected Takeoff Takeoff 2.5 2.6 2.6 Runway Runway End End 2.7 Taxiway Taxiway Takeoff Takeoff 2.7 +3dB 2.8 Approaching Approaching Runway Runway // Short Short Runway Runway in In Air Air 2.8-6dB 2.9 Distance Remaining -- Landing Landing 2.9 2.10 Taxiway Taxiway Landing 2.10 Landing 2.11 Flaps Flaps Flaps 2.11 Stabilized Approach Flaps 2.12 Stabilized Approach Too Too High High 2.12 2.13 Stabilized Approach Too Too Fast Fast 2.13 2.14 Stabilized Approach Unstable Unstable 2.14 2.15 Altimeter Altimeter Setting Setting 2.15 2.16 Takeoff Takeoff Flap Flap Monitor Monitor Flaps Flaps Flaps Flaps 2.16 2.17 Long Landing 2.17 2.17 2.17 Long Landing Distance Remaining AC-1 AC-2 AC-3 AC-4 AC-5 AC-6 AC-7 AC-8 AC-9 COMMENTS: Page 9 of 9