Years ago, following a "dive and drive" mishap, a major airline had to remind its pilots that a non-precision approach must be flown with great precision.
In my distant past, I think the U.S. Air Force must have lost a few airplanes to "dive and drive" because our evaluation criteria required crews be busted for even an inch of deviation below the MDA. For most limits we allowed momentary deviations with signs of a positive correction, but the MDA was a brick floor, none were allowed to go below it until the runway was sighted and the airplane was in a position to land.
Leveling off at the MDA can be problematic if there are distractions or turbulence. Keeping the airplane at the MDA until the runway is sighted is another issue. But the worst problem may be resisting the urge to descend when you spot the runway too far out. Why not bypass all this?
Flying a Continuous Descent Final Approach (CDFA) eliminates the MDA level off, puts the airplane in a position to land when the runway is sighted, and forces you to go around if the runway is not sighted before a normal visual descent point. It is easier to fly than a dive and drive approach and you don't need any special equipment. But technology does help.
It makes sense to use a CDFA on most non-precision approaches. About the only exceptions would be a circling approach or an approach where last minute maneuvering is required. And what about for U.S. approaches with the "Descent Angle NA" note? (For more about that caveat, see: Descent Angle NA.) With the caveats aside, it almost always makes sense to use a CDFA. Besides, it is mandatory in many parts of the world.
Note: The examples on this page are more than likely out of date. Many countries are adopting the CDFA technique and making changes as they fine tune. You need to check their AIP or the Jeppesen State pages to ensure you have the latest rules for any country.
Everything here is from the references shown below, with a few comments in an alternate color.
Figure: CDFA versus conventional approach, from Eddie's notes.
A continuous descent final approach is what you do for every straight-in ILS and what you attempt to do for every visual straight-in approach: you hit the glide path and start down on an angle that ends up in the touchdown zone of the runway. You can also do this when in instrument conditions flying a non-precision approach, which we are probably better off calling an "approach without vertical guidance."
[AC 120-108 §4.c] CDFA is a technique for flying the final approach segment of an NPA as a continuous descent. The technique is consistent with stabilized approach procedures and has no level-off. A CDFA starts from an altitude/height at or above the FAF and proceeds to an altitude/height approximately 50 feet (15 meters) above the landing runway threshold or to a point where the flare maneuver should begin for the type of aircraft being flown. This definition harmonizes with the ICAO and the European Aviation Safety Agency (EASA).
[ICAO Doc 8168, Vol I, Ch. 1, Definitions] CDFA: a technique, consistent with stabilized approach procedures, for flying the final approach segment of a non-precision instrument approach procedure as a continuous descent, without level-off, from an altitude/height at or above the final approach fix altitude/height to a point approximately 15 m (50 ft) above the landing runway threshold or the point where the flare manoeuvre should begin for the type of aircraft flown.
Some of us began our instrument jet experience without the benefit of an autopilot or flight director and flying an approach without vertical guidance was an invitation to making fatal mistakes. Even with the best technology, flying an approach without vertical guidance can be a problem:
Example: American Airlines 1572.
Example: Corporate Airlines 5966.
Example: Crossair 3597.
Example: Korean Air 2033.
[AC 120-108 §4] Controlled flight into terrain (CFIT) is a primary cause of worldwide commercial aviation fatal accidents. Unstabilized approaches are a key contributor to CFIT events. Present NPAs are designed with and without stepdown fixes in the final approach segment. Stepdowns flown without a constant descent will require multiple thrust, pitch, and altitude adjustments inside the final approach fix (FAF). These adjustments increase pilot workload and potential errors during a critical phase of flight. NPAs designed without stepdown fixes in the final segment allow pilots to immediately descend to the MDA after crossing the FAF. In both cases, the aircraft remains at the MDA until descending for the runway or reaching the missed approach point (MAP). This practice, commonly referred to as "dive and drive," can result in extended level flight as low as 250 feet above the ground in instrument meteorological conditions (IMC) and shallow or steep final approaches.
In some countries: yes. In other countries: it is recommended but not mandatory.
[ICAO Doc 8168, Vol I, ¶ 22.214.171.124]
Studies have shown that the risk of controlled flight into terrain (CFIT) is high on non-precision approaches. While the procedures themselves are not inherently unsafe, the use of the traditional step down descent technique for flying non-precision approaches is prone to error, and is therefore discouraged. Operators should reduce this risk by emphasizing training and standardization in vertical path control on non-precision approach procedures. Operators typically employ one of three techniques for vertical path control on non-precision approaches:
Of these techniques, the CDFA technique is preferred. Operators should use the CDFA technique whenever possible as it adds to the safety of the approach operation by reducing pilot workload and by lessening the possibility of error in flying the approach.
[EASA Air Operations, ¶CAT.OP.MPA.115] Approach flight technique — aeroplanes
(1) The continuous descent final approach (CDFA) technique shall be used for all non-precision approaches.
(2) Notwithstanding (1), another approach flight technique may be used for a particular approach/runway combination if approved by the competent authority. In such cases, the applicable minimum runway visual range (RVR):
(i) shall be increased by 200 m for category A and B aeroplanes and by 400 m for category C and D aeroplanes; or
(ii) for aerodromes where there is a public interest to maintain current operations and the CDFA technique cannot be applied, shall be established and regularly reviewed by the competent authority taking into account the operator’s experience, training programme and flight crew qualification.
[AC 120-108 §5] The FAA recommends CDFA for all of the following NPAs published with a vertical descent angle (VDA) or glideslope (GS):
[ICAO Doc 8168, Vol I, ¶ 126.96.36.199] Many Contracting States require the use of the CDFA technique and apply increased visibility or RVR requirements when the technique is not used.
Many countries do require CDFA techniques be used for flying approaches without vertical guidance, but the application of the technique is not consistent. Some countries list a CDFA approach with "CDFA" in the minimums section while others use "DA" or "DA/MDA" to signify such approaches. Even the countries that list "CDFA" are not consistent about the meaning. The only way to ensure you are following the rules of the host nation is to look it up in the country's Aeronautical Information Publication or the Jeppesen Airways Manual ATC pages.
If you have the equipment to fly an instrument approach, you have what you need to fly a continuous descent final approach. The more technology you have, however, the easier it will be to do that.
[AC 120-108 §6.a] CDFA requires no specific aircraft equipment other than that specified by the title of the NPA procedure. Pilots can safely fly suitable NPAs with CDFA using basic piloting techniques, aircraft flight management systems (FMS), and RNAV systems.
[AC 120-108 §6.b]
In the United States there is a stipulation in AC 120-108 requiring that you see a published angle on the chart. The presence of the angle varies with approach type and is also depicted differently between FAA and Jeppesen charts. There are four variations, described below.
Figure: Instrument approach procedure legend, from AC 120-108, appendix 1, figure 2.
[AC 120-108 §6.b]
[Jeppesen Airways Manual, Approach Chart Legend, 12 April 2013]
[Jeppesen Airways Manual, Approach Chart Legend, 12 April 2013]
Figure: KLAF RNAV(GPS) Rwy 28 profile view, from AL-200(FAA), 01 May 2014
On an FAA chart, an RNAV(GPS) will contain the glide slope angle in the profile view.
Figure: KLAF RNAV(GPS) Rwy 28 profile view, from Jeppesen Airways Manual, KLAF page 12-2, 16 Sep 11.
On a Jeppesen chart, an RNAV(GPS) will be depicted with glide feathers in the profile view.
Figure: KASH NDB Rwy 14 profile view, from AL-5036(FAA), 01 May 2014
On an FAA chart, a non-RNAV or RNAV without vertical guidance will contain the vertical descent angle in the profile view.
Figure: KASH NDB Rwy 14 profile view, from Jeppesen Airways Manual, KASH page 16-1, 31 Jan 14
On a Jeppesen chart, a non-RNAV or RNAV without vertical guidance will depict the vertical descent angle with a dotted gray line below the MDA in the profile view.
AC 120-108 does not impose a maximum vertical path angle, per se, but if you have OpSpec, MSpec, or LOA C073 you are already familiar with a VNAV DA(H) in lieu of MDA(H) provision that limits you to 3.77° (Category A, B, and C) or 3.5° (Category D and E). You really should adopt those limits for CDFA as well.
More about this: Vertical Navigation (VNAV).
[AC 120-108 §6.d] The VDA or GS is calculated from the FAF/precise final approach fix (PFAF) altitude to the threshold crossing height (TCH). The optimum NPA descent angle (VDA or GS) is 3.0 degrees. Descent angles are found in the following range when the optimum VDA is not possible: 2.75°–3.77° (IAPs w/≤ Category (CAT) C minimums), 2.75°–3.50° (IAPs w/CAT D/E minimums). On approaches with stepdown fixes, the goal is to publish a VDA that keeps the Vertical Path (VPATH) above the stepdown fix altitude. However, in some cases, the VDA is calculated from the stepdown fix altitude to the TCH.
The MDA, under most cases, is still an altitude you cannot go below. The CDFA technique adds an altitude pad to account for the aircraft's tendency to go below the altitude at which the missed approach is initiated, usually due to autopilot reaction time. The new altitude, that resulting from the addition of this pad to the MDA, is known as the Derived Decision Altitude (DDA).
[ICAO Doc 8168, Vol I, ¶ 188.8.131.52] An increment for the MDA/H may be prescribed by the operator to determine the altitude/height at which the vertical portion of the missed approach shall be initiated in order to prevent descent below the MDA/H. In such cases, there is no need to increase the RVR or visibility requirements for the approach. The RR and/or visibility published for the original MDA/H should be used.
[AC 120-108 §6.F] Pilots must not descend below the MDA when executing a missed approach from a CDFA. Operators should instruct their pilots to initiate the go-around at an altitude above the MDA (sometimes referred to as a DDA) to ensure the aircraft does not descend below the published MDA. Operators conducting approaches authorized by operations specification (OpSpec) C073, IFR Approach Procedures Using Vertical Navigation (VNAV), may use MDA as a DA.
C073 is now available also as a Letter of Authorization. These approaches, those with the "Only Authorized Operators" ball note, take into consideration the aircraft's momentary dip below the MDA.
More about this: Vertical Navigation (VNAV).
Some countries add the altitude pad into the approach minimums, pilots need not "double add." Examples below.
[G450 Airplane Flight Manual §1-22-20] Maximum demonstrated altitude loss for coupled go-around is 60 ft.
While some countries specify the method used to determine the DDA, most do not. In the case of a G450, pilots will add 60' to the MDA to determine the DDA.
The objective of CDFA is to leave the final approach fix fully configured, on speed, and ready to land. You should not have to destabilize the aircraft by making airspeed or trim adjustments when spotting the runway. GV and G550 pilots often withhold the last increment of flaps as a courtesy to faster moving aircraft, but if flying a CDFA in instrument conditions, it may be wiser to configure earlier.
Some aircraft allow a CDFA be flown with ILS-like indications so that procedures can be identical. Others may require adjustments, such as lowering the altitude select to field elevation. The closer CDFA procedures can be to an ILS, the better. Pilots simply follow the needles down to minimums, being mindful of the decision altitude. (In either case, pilots should consult their aircraft manuals and practice these procedures in a simulator until comfortable.)
The G450 can adhere to CDFA techniques by either:
While the first method prevents you from going below minimums if you attain visual contact, it increases your work load if you do. I recommend the second method, making sure both pilots understand it will be flown like an ILS.
[AC 120-108 §6.c]
If you don't have an FMS that does all this for you, or if you are flying an approach that prevents your FMS from doing all this for you, this table gives you an idea of what vertical descent rate you are going to need. If you don't have the table, you can approximate a 3° angle of descent by dividing your groundspeed by 2 and multiplying that by ten. A 120 knot ground speed, for example, yields 600 fpm.
You can check your progress during the approach by placing tick marks at each mile from the final approach fix to the missed approach point with the appropriate altitude. A 3° glide path should lose 318' every nautical mile. If, for example, the final approach fix altitude is 2,000 feet, you should be at 1,682' after one mile, 1,364' after two miles, 1,046' after three miles, and so on. You can figure these out during your approach briefing, marking each target on the approach plate.
[ICAO Doc 8168, Vol I, ¶ 184.108.40.206] This technique requires a continuous descent, flown either with VNAV guidance calculated by on-board equipment or based on manual calculation of the required rate of descent, without level-offs. The rate of descent is selected and adjusted to achieve a continuous descent to a point approximately 15m (50 ft) above the landing runway threshold or the point where the flare manoeuvre should begin for the type aircraft flown. The descent shall be calculated and flown to pass at or above the minimum altitude at any step down fix.
The CDFA places the aircraft right on glide path in a position to land in the touchdown zone of the runway. If the runway is sighted after this point, the aircraft will be too far down the runway to make that happen and a missed approach will be needed. This eliminates the judgment calls when sighting the runway early or late.
ICAO Doc 8168, Vol I, Part I, Amdt 3, ¶ 220.127.116.11] If the visual references required to land have not been acquired when the aircraft is approaching the MDA/H, the vertical (climbing) portion of the missed approach is initiated at an altitude above the MDA/H sufficient to prevent the aircraft from descending through the MDA/H. At not time is the aircraft flown in level flight at or near the MDA/H. Any turns on the missed approach shall not begin until the aircraft reaches the MAPt. Likewise, if the aircraft reaches the MAPt before descending to near the MDA/H, the missed approach shall be initiated at the MAPt.
ICAO Doc 8168, Vol I, Part I, Amdt 3, ¶ 18.104.22.168] It should be emphasized that upon reaching the MDA/H only two options exist for the crew: continue the descent below MDA/H to land with the required visual references in sight; or, execute a missed approach. There is no level flight segment after reaching the MDA/H.
Figure: Le Bourget VOR Rwy 07, from Jeppesen LFPB, pg. 33-1.
The Jeppesen State Rules and Procedures pages for France: "The operational minima published on French non-precision approach charts have been determined based on the assumption that these approaches are flown using CDFA flight technique unless otherwise stated by the Authority for a particular approach to a particular runway.
This approach has already added the altitude pad so you can fly it down to the posted DA (590'). There is no provision in the French ATC pages stating you may fly this approach using RNAV.
By the book, you would have to fly this using the VOR as your navigation source, estimate your descent rate to fly the given altitudes on the chart, and 590 feet. Is that the best way to fly this approach? Probably not.
As technique, if you have the technology, the following will probably be safer:
If you don't have the technology, you can determine your ground speed and compute an initial descent rate and a target altitude loss per nautical mile using the chart given above, Descent Table. Let's say you are moving along at 120 knots ground speed:
Figure: Geneva VOR DME Rwy 05, from Jeppesen Airways Manual, LSGG, pg. 13-1.
The Swiss do not specifically mention CDFA on their approach plates or in the State Rules and Procedures pages, but a DA is listed on the non-precision approaches and the ICAO recommended technique should be employed. The Swiss do, however, specifically allow GPS overlays for specific approaches, including this one:
This approach can be flown almost like an RNAV (GPS) approach in the U.S. with the exception that 60' should be added to the published DA. Both PFDs can be set to LRN data with the SFD showing VOR or one PFD to VOR data. Unlike flying a U.S. RNAV (GPS) approach, the Swiss ATC pages specifically require the ground based navaids be operational and used as the primary means of navigation. I would have the ground based navaids in view on a display with a CDI, either the copilot's or the standby system. This way you can fly the approach using the APPR button, once again treating it like an ILS.
Figure: Purdue University RNAV(GPS) Rwy 28, from Jeppesen Airways Manual, KLAF, pg. 12-2.
This approach gives you several options, depending on aircraft capability and crew training:
Figure: Nashua NDB Rwy 14, from Jeppesen Airways Manual, KASH, page 16-1.
Without C073 authorization, crews would have an MDA of 880' with a local altimeter setting, 920' without. They could elect to calculate a DDA and fly the approach using CDFA techniques. (A G450 would use 940' with the local altimeter setting, 980' without.)
With C073 authorization (OpSpec, MSpec, or LOA), crews can fly this approach using CDFA techniques down to the published MDA's, using them as DA's. (An authorized G450 would use 880' as a DA with the local altimeter setting, 920' without.)
More about this: Vertical Navigation (VNAV).
Figure: Hilo RNAV(GPS) Rwy 21, from Jeppesen Airways Manual, PHTO page 12-1.
There are at least three clues on the approach plate telling you a CDFA is not advisable:
Of course this begs the question: why?
Figure: Hilo Airfield Diagram, from Jeppesen Airways Manual, PHTO page 11-1, extract.
Looking at the airfield diagram we see three obstacles within a mile of the approach end of the runway that will required visual maneuvering at the last moment.
Figure: Aspen LOC DME-E, from Jeppesen Airways Manual, KASE page 11-1.
The approach contains the dotted gray line with a vertical descent angle given, 6.59°. The FAA version also has the requisite VDA depicted. Technically, you have what you need to fly this approach using a constant descent final approach, but it would be unwise. AC 120-108 suggests 3.77° is the maximum for a Category C aircraft.
There are many problems with such and approach, to name just a few:
The CDFA is meant to give you an unchanging flight path, laterally and vertically, from the final approach fix to the runway. Approaches like this are meant for low altitude maneuvering, making them unsuitable for CDFA techniques.
Advisory Circular 120-108, Continuous Descent Final Approach, 1/20/11, U.S. Department of Transportation
EASA Air Ops Annex 1 to VIII, European Aviation Safety Agency, October 2019
FAA-H-8083-15B, Instrument Flying Handbook, U.S. Department of Transportation, Flight Standards Service, 2012
FAA-H-8261-1A, Instrument Procedures Handbook, U.S. Department of Transportation, Flight Standards Branch, 2007
ICAO Doc 8168 - Aircraft Operations - Vol I - Flight Procedures, Procedures for Air Navigation Services, International Civil Aviation Organization, Sixth Edition, 2018
Gulfstream G450 Airplane Flight Manual, Revision 35, April 18, 2013
Jeppesen Airways Manual
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