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B767 LIMITATION
B767 Operating Limitation
| Question | Answer |
|---|---|
| RUNWAY SLOPE | +- 2% |
| MAXIMUM OPERATING ALTITUDE | 43100 FT. pressure altitude |
| MAXIMUM TAKE OFF & LANDING ALTITUDE | 8400 FT. pressure altitude |
| MAXIMUM TAKE OFF &LANDING TAILWIND COMPONENT | 15 Knots |
| MINIMUM FLIGHT CREW | Pilot Copilot |
| TURBULENT AIR PENETRATION | 290 KIAS/.78 Mach |
| NAVIGATIONAL DISPLAY DOES NOT SUPPORT LATITUDES GREATER THAN | 87 North or South |
| MAX INFLIGHT DIFFERENCES CAPTAIN AND FIRST OFFICER ALTITUDE DISPLAY FOR RVSM | 200 FT. |
| MAX ON THE GROUND DIFFERENCES CAPTAIN AND FIRST OFFICER ALTITUDE DISPLAY FOR RVSM MAX DIFFERENCE BETWEEN CAPTAIN AND FO MAX DIFFERENCE BETWEEN CAPTAIN OR FO AND FIELD ELEVATION | SEA LEVEL 40 FT./75 FT. 5000 FT. 45 FT./75 FT. 10000 FT. 50 FT./ 75 FT. |
| MAXIMUM TAXI WEIGHT B767-200SF/BDSF300 | 352,200/413.000 |
| MAXIMUM TAKE OFF WEIGHT B767-200SF/300BDSF | 351,000/412,000 |
| MAXIMUM LANDING WEIGHT B767-200SF/300BDSF | 272.000*/326,000 *Wing fuel at landing must be 79,000 or less 283,00* *Wing fuel at landing must be 43,000 or less |
| MAXIMUM ZERO FUEL WEIGHT B767-200SF/300BDSF | 266,000/309,000 |
| MINIMUM INFLIGHT WEIGHT B767-200SF/300BDSF | 168,000/179,000 |
| TAKE OFF AUTOPILOT | 200 FT. |
| MINIMUM ENROUTE AUTOPILOT USE | 1000 FT. |
| USE AILERON TRIM WITH AUTOPILOT ENGAGED | DONT DO IT! |
| AUTOPILOT DISCONNECTED ON ALL APPROACHES (UNLESS APPROVED AUTO LAND) | 50 FT. |
| AUTO LAND MUST BE AUTHORIZED BY OPSPEC ISSUED TO? | ATI |
| MAXIMUM WIND SPEED FOR CAT 1 AUTOLAND | HEAD WING 25 KNOTS CROSS WING 25 KNOTS TAIL WING 15 KNOTS (10 KNOTS) |
| MAXIMUM ALLOWABLE CROSSWIND SPEED FOR CAT II OR CAT III AUTOLAND | 15 KNOTS |
| ENGINE | GE CF6-80A/A1/A2/C |
| ENGINE STARTING N2 LIMITS | 0 % PREFERABLE 0-20% PERMISSIBLE 21-30% FOR PURGING OR CLEAR A FIRE 31% OR MORE MAY RESULT GEARBOX DAMAGE ABOVE 20% LOGBOOK ENTRY REQUIRED |
| ENGINE STARTING CYCLE LIMITS | 1ST. AND 2ND. 5 MINUTES ON 1 1/2 OFF for each minute on. 3RD. AND 4TH. 5 MINUTES ON AND 10 OFF 5TH. 5 MINUTES ON |
| ENGINE N1 N2 LIMITS | N1 117.0% N2 110.5% |
| ENGINE MAXIMUM EGT LIMITS GE CF6-80A/A1/A2 STARTING (GROUND/INFLIGHT) TRANSIENT LIMITED | 870 C. LIMITED 40 SECONDS |
| ENGINE MAXIMUM EGT LIMITS GE CF6-80A/A1/A2 STARTING (GROUND/INFLIGHT) | 750 C. UNLIMITED |
| ENGINE MAXIMUM EGT LIMITS GE CF6-80A/A1/A2 TAKE OFF | 940 C. 5 MINUTES |
| ENGINE MAXIMUM EGT LIMITS GE CF6-80A/A1/A2 MAXIMUM CONTINUOS | 895 C. |
| ENGINE OIL MIN PRESSURE | 10 PSI |
| ENGINE OIL MAXIMUM OIL TEMPERATURE (CONTINUOUS) | 160 C, |
| ENGINE OIL MAXIMUM TEMPERATURE TIME LIMITED | 175 C. 15 MINUTES |
| MINIMUM OIL QUANTITY (dispatch) | 17 QUARTS |
| ENGINE IGNITION ON | Takeoff and landing |
| MINIMUM FUEL INFLIGHT BULK TEMPERATURE | 3 C. 5 F. ABOVE FUEL FREEZING POINT |
| MAXIMUM FUEL TEMPERATURE | 49 C. 120 F. |
| CENTER TANK | 22,050 POUNDS (CHECK ZERO FUEL WEIGHT LIMIT AND CG LIMIT) |
| FUEL IMBALANCE | 2500# MAIN TANK FUEL LOAD 48,000 # OR LESS |
| FUEL IMBALANCE LINEAR REDUCTION | 1500 # MAIN TANK FUEL LOAD 48,000# TO 79,000# |
| FUEL IMBALANCE | 1500 # MAIN THANK FUEL LOAD GREATER THAN 79,800 # |
| FUEL JETTISON | NOT ALLOWED WITH FLAPS POSITION 25 & 30 |
| FUEL PUMP CIRCUIT BREAKER | DO NOT RESET COYOTE! |
| FLAP EXTENSION MAX ALT | 20,000 FT. |
| CARGO DOOR OPERATION OPEN MAXIMUM WIND SPEED | 40 KNOTS |
| LONG RANGE NAVIGATION REQUIREMENT | ONE FLIGHT MANAGEMENT COMPUTER SYSTEM (FMCS) TWO CONTROL DISPLAY UNIT (CDU) OR MULTI PURPOSE CONTROL DISPLAY UNIT (MCDU) TWO INERTIAL REFERENCE UNITS (IRU) IN NAV MODE |
| REQUIRED FOR RNAV | 1 FMC 1 CDU 1 VHF OMNI-DIRECTIONAL RADIO VOR 1 DME OR GPS |
| LNAV WITH AUTOPILOT ENGAGED | FMC + GPS 0.13 NM, FMC ONLY 0.28 NM |
| LNAV WITH FLIGHT DIRECTOR | FMC + GPS 0,14 NM, FMC ONLY 0,28 NM |
| MANUAL CONTROL WITH MAP DISPLAY ONLY | FMC + GPS 0.81 NM, FMC ONLY 1.16 NM |
| TERRAIN ALERTING AWARENESS DISPLAY (TAAD) OFF | DISPATCHING WITH BOTH FMCs INOPERATIVE BOTH FMCs FAIL IN FLIGHT WHEN OPERATING QFE BELOW TRANSITION ALTITUDE |
| ICING CONDITION GROUND | 10 C. OR BELOW VISIBLE MOISTURE (VIS LESS 1 MILE, RVR LESS 5000) TEMPERATURE DEW POINT SPREAD 3 C. OR LESS |
| ICING CONDITION FLIGHT (CLIMB OR CRUISE) | FROM 10 C. TAT TO -40 C. SAT VISIBLE MOISTURE PRESENT OR ANTICIPATED |
| ICING CONDITION FLIGHT (DESCENT) | LESS THAN 10 C. TAT TO -40 C. SAT VISIBLE MOISTURE PRESENT OR ANTICIPATED |
| WING ANTI-ICE (DESCENT) AT OR BELOW 22,000 FT. | LESS THAN 10 C. TAT TO -40 C. SAT VISIBLE MOISTURE PRESENT OR ANTICIPATED |
| ICE CRYSTALS | ENGINE ANTI-ICE ON (EVEN BELOW -40 C. SAT) |
| CABIN PRESSURE DIFFERENTIAL | 9.1 P S I Max, 8.6 P S I Normal |
| MAXIMUM PRESSURE DIFFERENTIAL FOR TAKE OF AND LANDING | .125 P S I (236 FT. BELOW AIRPORT PRESSURE ALT) |
| HF RADIO DURING REFUELING | DO NOT OPERATE SILLY GOOSE! |
| WEATHER RADAR DO NOT OPERATE | IN A HANGAR 50 FT. OF ANY PERSONNEL OR FUEL SPILL |
| Boeing 767 200/300 wing span | 200/300 without winglets 156 feet 1 inch 300 with winglets 166 feet 11 inches |
| Boeing 767 length | 200 nose to tail length 159 feet 2 inches, 300 180 feet 3 inches |
| Boeing 767 300 turning radius at the wing (largest arc) | without winglets 123 feet with winglets 131 feet 4 inches |
| Boeing 767 200/300 minimum width of pavement for 180° Turn | 129 feet / 146 feet |
| Dry running of a center tank ( fuel pump (CTR L OR R FUEL PUMP message displayed on EICAS) | |
| Engine starting sequence verifications Max motoring (N2 <1% in 5 sec) Min N2 15% Min | 1) FUEL CONTROL switch run 2) FUEL spar and engine fuel valves lights illuminate temporarily 3) N1 rotation starts within 30 sec 4) EGT starts within 25 sec 5) engine operates within normal idle range within 2 minutes 6) Oil pressure at 10% at idle |
| Coast out check (vor) | VOR freq VOR IDENT IN FIX FOR BEARING AND DISTANCE PFD ON VOR DIAL FREQUENCY AND BEARING CHECK BEARIMG AND DISTANCE VERSUS FIX MAX DEVIATION 2° AND OR 2 MILES |
| VLO Gear up or down max speed | 270 knots |
| VFE Flaps extension speed | 240/250 knots |
| Normal engine indication after start | 2, 4, 6, 12 |
| Fuel configuration light | |
| Imbalance: B757 1800 lbs. B767 2000+/- 500 lbs Less 2200 lbs in either main tank Center tank pumps off with >1200 lbs | |
| Minimum crew oxigen pressure | 1100 psi, if below contact maintenance |
| Minimum hydraulic quantity | If RF is displayed call maintenance |
| ETOPS pre-departure check accomplishes within how many hours? | 4 |
| IRU maximum error | 2.5 NM |
Created by:
Gbaron
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