CRZ ALT CHANGED TO XXXXX | An altitude constraint added due to entering a new company route, a new destination airport, or selection of a new procedure conflicts with the cruise altitude, resulting in automatically raising the cruise altitude to match the highest waypoint altitude constraint in the mod plan, when not in active descent. | Clear the message. Verify MCP cruise altitude. |
CHECK ALT TGT | VNAV disengages while airplane is between MCP and FMC altitudes or VNAV button pressed while airplane is between MCP and FMC altitudes. | Clear the message. |
CYCLE IRS OFF–NAV | IRS is unable to complete alignment under current conditions. | Cycle IRS mode selector to “OFF” and back to “NAV.” |
DATA BASE INVALID | The automatic validity test of the permanent navigation database has failed. | Advise maintenance personnel to check the FMC and reload the database, as required. If desired, consider the use of the temporary nav database. |
DISCO INSRTD AFTR XXXXX (waypoint identifier) | A ROUTE DISCONTINUITY has been inserted into the flight plan due to undefined termination of a downpath leg or a triple waypoint BYPASS. | Select the RTE or RTE LEGS pages and modify the waypoints for a continuous route. |
DISCONTINUITY | Passing the last waypoint in the route prior to a ROUTE DISCONTINUITY (LNAV disengages) or pressing LNAV while in a discontinuity. | Select the RTE LEGS page. Enter the desired active waypoint into the box prompts. Correct any ROUTE DISCONTINUITY and EXECute. Reengage LNAV. |
DRAG REQ AFTER XXXXX | A waypoint speed constraint greater than 10 knots above the predicted speed exists at waypoint XXXXX. | Modify flight plan as required. Clear the message. |
END OF OFFSET | Two minutes prior to passing offset leg termination. | Confirm clearance. |
END OF ROUTE | LNAV engaged and passing the last waypoint in the route (LNAV disengages). | Select the RTE LEGS page. Enter the desired active waypoint into the dash prompts and EXECute. Reengage LNAV. |
ENG OUT SID MOD | An engine–out SID has been automatically inserted into the flight plan as a modification. | Clear the message. |
ENTER IRS POSITION | IRS in the alignment mode needs present position to complete alignment. Previous present position entry was not received back from the IRS. | Enter IRS present position into the scratchpad pad and line select 4R on the POS INIT page of the CDU. If present position was previously entered, overwrite displayed data. If necessary, enter present position directly into the IRS control /display unit. |
FMC APP/TUNE DISAGREE (U13.0) | An approach that utilizes FMC generated glide path is in the active flight plan but an approach navaid (ILS/GLS) has been tuned with G/S ON. | Confirm the tuned frequency and approach selected in the FMC are both consistent with the actual approach intended to be flown. Resolve tuning or approach selection inconsistency. Clear the message. |
FMC APP/TUNE DISAGREE (U14.0 and above) | An approach that utilizes FMC generated glide path is in the active flight plan but an approach navaid (ILS/GLS/LPV) has been tuned with G/S ON. | Confirm the tuned frequency and approach selected in the FMC are both consistent with the actual approach intended to be flown. Resolve tuning or approach selection inconsistency. Clear the message. |
FMC DISAGREE | During approach or on the ground, monitored parameters required for dual FMC operation are in disagreement. (Dual FMC as installed) Message will remain displayed until the condition has been resolved. The FMC does not check for mach and indicated airspeed miscompares on the ground. | Monitor FMCs closely. Both FMCs remain online. Limit approaches to single FMC only. If desired, revert to SINGLE FMC OPERATION in this section. |
FMC DISAGREE – VERTICAL | A vertical deviation, FMC Airspeed, or FMC Mach value disagreement between the FMCs by more than the allowed tolerance occurs and long enough that all attempts to resynchronize failed while the aircraft in a path descent. Message display is inhibited when in the Approach Nav environment. (dual FMC as installed) | Do not move the FMC source select switch. Monitor crossing altitudes to ensure compliance. |
FMC POS/RW DISAGREE | Position information is contradictory. | Refer to FMC Navigation Check Supplementary Procedure. |
FUEL DISAGREE | The totalizer fuel quantity and the FMC calculated fuel quantity disagree. Illuminates the FMC P/RST Light. Message displayed on Engine display. | Refer to FUEL DISAGREE non-normal checklist in the QRH. The Engine Display message will remain until the condition is no longer valid. |
GPS-L INVALID GPS-R INVALID | FMC is no longer receiving valid information from the displayed GPS system. | Clear the message. For ADS-B operations (if installed), when one GPS is invalid, ensure that the transponder selector is positioned to the side with the valid GPS. For dual GPS installations, if both GPS-L INVALID and GPS-R INVALID messages show, refer to FMC Navigation Check supplementary procedure. For single GPS installations, refer to FMC Navigation Check supplementary procedure |
INSUFFICIENT FUEL | FMC fuel at the destination is predicted to be less than 2000 lbs/900 kilograms. Scratchpad message shows for Active and Mod Flight Plan. Illuminates the FMC P/RST Light for Active and Mod Flight Plan. Message displayed on Engine display for the Active Flight Plan only. | Refer to INSUFFICIENT FUEL non-normal checklist in the QRH. The Engine Display message will remain until the condition is no longer valid. |
IRS MOTION | IRS has automatically restarted the alignment due to detection of excessive motion. | Clear message and attempt to reduce airplane movement, if practicable. |
IRS-(L or R) DRIFT | An FMC has detected that the IRS-(L or R) position or velocity data is unreasonable, and deselected IRS-(L or R) due to velocity divergence or position blunder checks. | Refer to FMC Navigation Check Supplementary Procedure. |
IRS POS/ORIGIN DISAGREE | Position information is contradictory. | Refer to FMC Navigation Check Supplementary Procedure. |
LNAV BANK ANGLE LIMITED | LNAV is engaged and the airplane is not on a lateral offset and is not near or in an orbit or hold and the airplane is within 5 minutes or less from an LNAV guided course change, and will exceed the airway/route boundaries for non-flyover turns less than or equal to 135 degrees due to performance limited bank angle. This message does not apply to fixed radius turns. | Review the LNAV course change. If course change exceeds airway/route boundary, consider flight plan change. |
MAX ALT FLXXX (flight level value) | Altitude intervention (as installed) attempt to raise cruise altitude when MCP altitude is above maximum altitude. | Clear the message. |
MISSED CAPTURE | Proper localizer capture maneuver was performed, but the AFDS did not capture. | Clear the message |
MODEL/ENG DATA INVALID | A valid performance database is not available. | Contact maintenance personnel. |
NAV DATA OUT OF DATE | Effectivity dates of nav database do not agree with date input from clock. | Check the IDENT page and reverse the dates for ACTIVE NAV DATA if required. |
NAV INVALID–TUNE XXXXX (navaid identifier) | FMC is unable to auto–tune or receive the navaid for a RNAV or VOR approach procedure. | Cross–check radios and manually tune the desired navaid. |
NO VNAV AFTER XXXXX, | The descent path is monitored independent of path construction for the following scenarios: – an “at”, “at or above”, “at or below” or “window” constraint is violated- a navigation data base gradient (vertical angle) is violated If a violation is detected and not resolved, VNAV will disconnect after the point of the violation. The alerting message is displayed one minute prior to the violation. | After sequencing waypoint XXXXX, VNAV INVALID – PERF logic applies: Pilot should reenter the CI using either the previous CI displayed or enter a new CI. Reengage VNAV when change has been EXECuted. |
OAT DISAGREE – DELETED | A check of entered OAT versus sensed OAT occurs after first engine start. A difference of +/- 6 degrees Celsius between the OAT value on the N1 LIMIT / TAKEOFF REF page and the engine temperature sensors. | Enter updated/corrected OAT on the N1 LIMIT page. |
OVERSPEED DISCONNECT | During path descent and above or below the speed restriction altitude, VNAV disengages when airspeed exceeds FMC speed restriction by more than 15 knots. | Manually reduce speed and reengage VNAV. |
PARTIAL ROUTE X LOADED | A route is loaded into the active/inactive RTE 1 or 2 flight plan buffer which references data not contained in any of the databases. | Clear the message. |
PERF DEFAULTS INVALID | Validity check of performance defaults database has failed. | Contact maintenance personnel. |
RESET MCP ALT | During the FMC cruise phase with VNAV engaged, when within 5 NM of the top-of-descent point without selecting a lower altitude on the AFDS MCP. | Select lower MCP altitude values as clearances permit. |
RTA UNACHIEVABLE | The RTA is not in the computed RTA window under current parameters. | Enter an achievable RTA or discontinue the RTA mode of navigation. Adjust parameters to meet the RTA. |
RW/APP TUNE DISAGREE | During approach, manual tuned approach frequency or channel does not match active flight plan. | Clear the message and select correct approach frequency. |
RW/APP CRS ERROR | During approach, MCP selected course does not match front course for the approach in the active flight plan. | Clear the message and select correct MCP course. |
SCANNING DME FAIL | Inputs from both frequency scanning DME radios have failed. | Clear the message and check position. Radio updating of FMC position is not available. |
SELECT MODE AFTER RTA | RTA mode has been discontinued due to sequencing of RTA waypoint or RTA waypoint has been removed from the flight plan. | Select alternate performance mode. (ECON, manual speed, etc.) |
SINGLE FMC OPERATION | The primary FMC has determined that the secondary FMC is not available. (Dual FMC as installed) | If the FMC source selector switch is in the “Normal” position, move to “BOTH ON L”. No action is required if the FMC source selector switch is already positioned to “BOTH ON L” or “BOTH ON R”. |
SW OPTIONS INVALID | The CRC performed during power up BIT on the current software options data base has failed, or the CRC of the software options data base that has been loaded via the data loader has failed. | Reload the FMC OPC software by maintenance. |
THRUST REQUIRED | Airplane is in an underspeed condition. | Clear the message. Increase airspeed to within 15 knots of speed target. |
UNABLE HOLD AIRSPACE | The lateral predicted hold path using the bank angle limit causes protected airspace to be exceeded. | Review the holding pattern. If holding pattern exceeds allowable holding airspace, consider flight plan change. |
UNABLE NEXT ALTITUDE | Unable to meet the next flight plan altitude constraint in a VNAV climb or descent. The message appears only with VNAV engaged. | Clear the message and review the prediction. For undershoot condition during climb, consider selection of MAX RATE CLB or MAX ANGLE CLB, or a different N1 limit as appropriate. |
UNABLE PROC AIRSPACE | Minimum procedure turn built by guidance exceeds the allowable excursion distance. | Modify flight plan as required. Clear the message. |
UNABLE YYY KTS AT XXXXX | Next waypoint speed restriction (speed YYY, at waypoint XXXXX) cannot be met. | Modify flight plan as required. Clear the message. |
UNABLE REQD NAV PERF–RNP (U13 and later) | FMC actual navigation performance is not sufficient for the displayed RNP. VT-BXD, VT-BXF, VT-BXG, VT-BXL UNABLE REQD NAV PERF-RNP message will be displayed if there is a divergence between IRU-L and IRU-R inertial altitude, or between IRS-L and IRS-R inertial vertical speed, when the aircraft is on an RNP-AR approach leg. | Refer to UNABLE REQD NAV PERF-RNP non-normal checklist in the QRH. Note: When on a procedure or airway without an RNP alerting requirement, the FMC Navigation Check supplementary procedure in SP11 can be used to verify position. VT-BXD, VT-BXF, VT-BXG, VT-BXL If a UNABLE REQD NAV PERF-RNP is shown during the RNP-AR approach, whether the lateral or vertical RNP are exceeded or not, do the Go-Around and Missed Approach Procedure unless suitable visual reference is established and maintained. |
USING RSV FUEL | FMC fuel at the destination is predicted to be less than the entered RESERVES fuel. Scratchpad message shows for Active and Mod Flight Plan. Illuminates the FMC P/RST Light for Active and Mod Flight Plan. Message displayed on Engine display for the Active Flight Plan only. | Refer to USING RSV FUEL non-normal checklist in the QRH. The Engine Display message will remain until the condition is no longer valid. |
VERIFY GW AND FUEL | Fuel data becomes invalid, PERF INIT fuel value is replaced with dashes. FMC uses last valid fuel quantity for performance predictions until manual entry is made. Shows if 30 minutes have elapsed since last manual entry. Does not show in descent with Vref selected. | Enter fuel weight on PERF INIT page 1/2. Periodic update of fuel weight is required to keep gross weight value current. |
VERIFY POS: FMC-FMC | Position information is contradictory. | Refer to FMC Navigation Check Supplementary Procedure. |
VERIFY POS: FMC-GPS | Position information is contradictory. | Refer to FMC Navigation Check Supplementary Procedure. |
VERIFY POS: FMC-RADIO | Position information is contradictory. | Refer to FMC Navigation Check Supplementary Procedure. |
VERIFY POS: IRS-FMC | Position information is contradictory. | Refer to FMC Navigation Check Supplementary Procedure. |
VERIFY POS: IRS-IRS | Position information is contradictory. | Refer to FMC Navigation Check Supplementary Procedure. |
VERIFY POS: IRS-RADIO | Position information is contradictory. | Refer to FMC Navigation Check Supplementary Procedure. |
VERIFY POSITION (on ground) | Position information is contradictory. | Clear message. Check accuracy of manually entered data. Crosscheck IRS, GPS and FMC positions. Manually re-align both IRS’s if needed. |
VERIFY RNP | Underlying RNP value is less than manually entered value. | Enter appropriate RNP. |
VERIFY TAKEOFF SPEEDS | A PERF INIT change has been made after takeoff speeds were specified. | On TAKEOFF REF page 1, accept previous V speeds, or reject previous V speeds and enter new V speeds. |
VERIFY TAKEOFF THRUST | With the Takeoff Thrust Auto Selection option enabled, the system determines that the selected takeoff thrust setting is not compatible with the engine thrust rating configuration. | Clear the message. Manually change takeoff thrust setting, or accept uplink of different thrust setting. |
VERIFY VERT RNP | During an active descent with navigation performance scales enabled, a manually entered vertical RNP is greater than the default vertical RNP. | Clear CDU message. Enter appropriate vertical RNP. |
VNAV DISCONNECT | The criteria for VNAV engagement is not satisfied (VNAV disengages). On approach, with VNAV engaged, the FCC has switched to LVL CHG. | Manually control the vertical path. |
VNAV INVALID-PERF | If the exception affects both the MOD and the ACT flight plan, the Cost Index (CI) will be replaced with box prompts on the PERF INIT page and the message will result. LNAV is still valid and can navigate the airplane laterally but VNAV will disconnect. Reference section 11.32 for further Software Exception Logic. | Pilot should reenter the CI using either the previous CI displayed or enter a new CI. Reengage VNAV when change has been EXECuted. |