AMC5 CAT.OP.MPA.110 Aerodrome operating minima    

CAA ORS9 Decision No. 1

DETERMINATION OF RVR/CMV/VIS MINIMA FOR NPA, APV, CAT I — AEROPLANES

(a) Aeroplanes

The RVR/CMV/VIS minima for NPA, APV and CAT I operations should be determined as follows:

(1) The minimum RVR/CMV/VIS should be the highest of the values specified in Table 5 or Table 6.A, but not greater than the maximum values specified in Table 6.A, where applicable.

(2) The values in Table 5 should be derived from the formula below,

Required RVR/VIS (m) = [(DH/MDH (ft) x 0.3048)/tanα] — length of approach lights (m)

where α is the calculation angle, being a default value of 3.00° increasing in steps of 0.10° for each line in Table 5 up to 3.77° and then remaining constant.

(3) If the approach is flown with a level flight segment at or above MDA/H, 200 m should be added for category A and B aeroplanes and 400 m for category C and D aeroplanes to the minimum RVR/CMV/VIS value resulting from the application of Tables 5 and 6.A.

(4) An RVR of less than 750 m as indicated in Table 5 may be used:

    (i) for CAT I operations to runways with full approach lighting system (FALS), runway touchdown zone lights (RTZL) and runway centreline lights (RCLL);

    (ii) for CAT I operations to runways without RTZL and RCLL when using an approved head-up guidance landing system (HUDLS), or equivalent approved system, or when conducting a coupled approach or flight-director-flown approach to a DH. The ILS should not be published as a restricted facility; and

    (iii) for APV operations to runways with FALS, RTZL and RCLL when using an approved head-up display (HUD).

(5) Lower values than those specified in Table 5, for HUDLS and auto-land operations may be used if approved in accordance with Annex V (Part-SPA), Subpart E (SPA.LVO).

(6) The visual aids should comprise standard runway day markings and approach and runway lights as specified in Table 4. The CAA may approve that RVR values relevant to a basic approach lighting system (BALS) are used on runways where the approach lights are restricted in length below 210 m due to terrain or water, but where at least one cross-bar is available.

(7) For night operations or for any operation where credit for runway and approach lights is required, the lights should be on and serviceable except as provided for in Table 9.

(8) For single-pilot operations, the minimum RVR/VIS should be calculated in accordance with the following additional criteria:

    (i) an RVR of less than 800 m as indicated in Table 5 may be used for CAT I approaches provided any of the following is used at least down to the applicable DH:

      (A) a suitable autopilot, coupled to an ILS, MLS or GLS that is not published as restricted; or

      (B) an approved HUDLS, including, where appropriate, enhanced vision system (EVS), or equivalent approved system;

    (ii) where RTZL and/or RCLL are not available, the minimum RVR/CMV should not be less than 600 m; and

    (iii) an RVR of less than 800 m as indicated in Table 5 may be used for APV operations to runways with FALS, RTZL and RCLL when using an approved HUDLS, or equivalent approved system, or when conducting a coupled approach to a DH equal to or greater than 250 ft.

Table 4

Approach lighting systems

Class of lighting facility

Length, configuration and intensity of approach lights

FALS

CAT I lighting system (HIALS ≥720 m) distance coded centreline, Barrette centreline

IALS

Simple approach lighting system (HIALS 420 – 719 m) single source, Barrette

BALS

Any other approach lighting system (HIALS, MALS or ALS 210 - 419 m)

NALS

Any other approach lighting system (HIALS, MALS or ALS <210 m) or no approach lights

Note: HIALS: high intensity approach lighting system; MALS: medium intensity approach lighting system.

Table 5

RVR/CMV vs DH/MDH

DH or MDH Class of lighting facility

ft

 

FALS IALS BALS NALS

See (a)(4),(5),(8) above for RVR <750/800 m

RVR/CMV (m)

200

-

210

550

750

1000

1200

211

-

220

550

800

1000

1200

221

-

230

550

800

1000

1200

231

-

240

550

800

1000

1200

241

-

250

550

800

1000

1300

251

-

260

600

800

1100

1300

261

-

280

600

900

1100

1300

281

-

300

650

900

1200

1400

301

-

320

700

1000

1200

1400

321

-

340

800

1100

1300

1500

341

-

360

900

1200

1400

1600

361

-

380

1000

1300

1500

1700

381

-

400

1100

1400

1600

1800

401

-

420

1200

1500

1700

1900

421

-

440

1300

1600

1800

2000

441

-

460

1400

1700

1900

2100

461

-

480

1500

1800

2000

2200

481

 

500

1500

1800

2100

2300

501

-

520

1600

1900

2100

2400

521

-

540

1700

2000

2200

2400

541

-

560

1800

2100

2300

2500

561

-

580

1900

2200

2400

2600

581

-

600

2000

2300

2500

2700

601

-

620

2100

2400

2600

2800

621

-

640

2200

2500

2700

2900

641

-

660

2300

2600

2800

3000

661

-

680

2400

2700

2900

3100

681

-

700

2500

2800

3000

3200

701

-

720

2600

2900

3100

3300

721

-

740

2700

3000

3200

3400

741

-

760

2700

3000

3300

3500

761

-

800

2900

3200

3400

3600

801

-

850

3100

3400

3600

3800

851

-

900

3300

3600

3800

4000

901

-

950

3600

3900

4100

4300

951

-

1000

3800

4100

4300

4500

1001

-

1100

4100

4400

4600

4900

1101

-

1200

4600

4900

5000

5000

1201 and above

5000

5000

5000

5000

 

Table 6.A

CAT I, APV, NPA — aeroplanes

Minimum and maximum applicable RVR/CMV (lower and upper cut-off limits)

Facility/conditions

RVR/CMV

(m)

Aeroplane category

A

B

C

D

ILS, MLS, GLS, PAR, GNSS/SBAS, GNSS/VNAV

Min

According to Table 5

Max

1 500

1 500

2 400

2 400

NDB, NDB/DME, VOR, VOR/DME, LOC, LOC/DME, VDF, SRA, GNSS/LNAV with a procedure that fulfils the criteria in AMC4 CAT.OP.MPA.110, (a)(1)(ii)

Min

750

750

750

750

Max

1 500

1 500

2 400

2 400

For NDB, NDB/DME, VOR, VOR/DME, LOC, LOC/DME, VDF, SRA, GNSS/LNAV:

    — not fulfilling the criteria in in AMC4 CAT.OP.MPA.110, (a)(1)(ii), or

    — with a DH or MDH ≥1 200 ft

Min

1 000

1 000

1 200

1 200

Max

According to Table 5, if flown using the CDFA technique, otherwise an add-on of 200 m for Category A and B aeroplanes and 400 m for Category C and D aeroplanes applies to the values in Table 5 but not to result in a value exceeding 5 000 m.