Document ID: chunk:federal_register_of_legislation:F2023C00696:body:0:p72
Version: federal_register_of_legislation:F2023C00696
Segment Type: other
Provision Reference: 
Character Range: 264529–271594

PC                                                                                                                                                      Headwind (KT)  LDR in Metres
A                                                                                                                                                       30             780            900         810   930
                                                                                                                                                        20             820            940         840   970
                                                                                                                                                        10             860            990         890   1020
                                                                                                                                                        0              900            1040        930   1070
                                                                                                                                                        –5             990            –           1020  –
B                                                                                                                                                       30             1220           1400        1250  1440
                                                                                                                                                        20             1270           1460        1610  1510
                                                                                                                                                        10             1330           1530        1370  1580
                                                                                                                                                        0              1400           1610        1440  1660
                                                                                                                                                        –5             1540           –           1590  –
C                                                                                                                                                       30             1570           1800        1610  1850
                                                                                                                                                        20             1640           1880        1690  1940
                                                                                                                                                        10             1710           1970        1760  2030
                                                                                                                                                        0              1800           2070        1850  2130
                                                                                                                                                        –5             1980           –           2040  –
  1. These figures apply only to aerodromes 0 to 500 FT.
  2. For operations at aerodromes between 500 and 2,500 FT the LDR is calculated by multiplying the figure obtained from the table by a factor of 1.2.
  3. For QNH below 997 HPa, multiply the LDR by a factor of 1.1.
  4. Interpolation is permitted between rows and columns (for similar conditions of temperature and runway status) for each aircraft PC.
  5. The table must not be used when the runway slope exceeds one percent down.

10.13.7         Letters of Agreement for LAHSO

10.13.7.1     A Letter of Agreement between the relevant ATS provider and any foreign military authority must be raised by the ATS unit following an initial request from the relevant military authority.

10.13.7.2     The Letter of Agreement must include, but is not limited to, the following items:
(a)         the specific aerodrome at which the Agreement is valid;
(b)         the ATC service provider bound by the Agreement;
(c)          foreign military authority bound by the Agreement;
(d)         a validity period;
(e)         the LAHSO procedures that are the subject of the Agreement;
(f)            a statement authorising active and/or passive participation by pilots of specified aircraft types and categories.

10.13.8         Runway Separation Minima

Minimum                                                                Application                                                                Conditions                                                                                                                                                                                                                                  Diagram
Take-off behind a preceding departing aircraft                         Fixed Wing Aircraft                                                        A departing aircraft must not be permitted to commence take-off until the preceding departing aircraft:
                                                                                                                                                    1. has crossed the up-wind end of the runway-in-use; or
                                                                                                                                                    2. has commenced a turn; or
                                                                                                                                                    3. is airborne and has reached a point at least 1 800 m (6 000 ft) ahead of the following aircraft, the runway is longer than 1 ,800 m (6 000 ft) and the distance can be readily determined; or
                                                                                                                                                    4. is airborne and has reached a point at least 600 m (2 000 ft) ahead of the following aircraft, and:
                                                                                                                                                       (a) the preceding aircraft has a MTOW of 7 000 kg or less; and
                                                                                                                                                       (b) the following aircraft has an MTOW of less than 2 000 kg; and
                                                                                                                                                       (c) the following aircraft is slower than the preceding aircraft; or
                                                                                                                                                    5. is airborne and has reached a point at least 600 m (2 000 ft) ahead of the following aircraft, and