VIND |
AD 2.2 |
| ||
| |||||
| |||||
| |||||
| |||||
|
| ||||
|
| ||||
|
1. PCR and runway surface details: | |||
|
Type of aids, magnetic variation and type of supported operation for ILS/MLS, basic GNSS, SBAS and | |||
|---|---|---|---|
Aircraft Stand |
Procedure |
|
|
N11, N12, N13, N14, N15, N16
|
|
N17 and N18 |
The aircraft shall be pushed back onto TWY C1facing east and to be towed abeam aircraft standN17 and follow further instructions from ATC |
A16R, A16L, A14R and A14L |
The aircraft shall be pushed back onto TXL C2 facing west and to be towed abeam aircraft stand A16R and follow further instructions from ATC. |
A20R, A20L, A24L, A24R, A28L, A28R,A32R & A32L |
The aircraft shall be pushed back onto TXL C2 facing west and to be towed abeam respective aircraft stand and follow further instructions from ATC. |
W2 & W3 |
The aircraft shall be pushed back onto TWY B facing east abeam aircraft stand W3 and follow further instructions from ATC. |
A06, A08, A10, A12 |
The aircraft on stand, A10, A12 shall be pushed back onto TXL C2 facing west abeam aircraft stand A08 and follow further instructions from ATC.The aircraft on stand A06, A08 shall be pushed back onto TXL C2 facing west, & then pull forward abeam stand A08 and follow further instructions from ATC. |
Note:a) Refer Aircraft Parking/Docking Chart for aircraft stands’ suitability.b) Refer AD 2.23 for taxiway suitability.c) All aircraft stands are power-in, and pushback standsd) Simultaneous pushback via TXL C1, serving north stands, and TXL C2,serving south stands, is authorized only when a minimum spacing of threestand positions exists between the two aircraft.e) High power run up is only approved at the IAPP (facing east). Pushbackand towing for high power run up to be coordinated by aircraft operatorwith Airside Duty Manager at least 60 minutes in advance.f) Pushback from stands N17, N18, A10, A12, A14L and A14R not permittedwhile aircraft taxing to TXL-C2 from C5.g) Aircraft to exercise caution during simultaneous pushbacks fromcorresponding opposite stands on TXLC1 and TXLC22. Taxiing Procedures2.1 Mode of Operation - Westerly (RWY 28)2.1.1 Departing aircraft from Apron 1 will taxi via taxi-lane C1 or C2, C6 andturn right on taxiway A, A1 or A3 (holding point RWY 28).2.1.2 Arrival for Apron 1 on RWY 28 to vacate runway via A9 or RET A6, taxivia A, C5, C1 or C2 to the respective aircraft stand.2.1.3 Arriving / Departing aircraft for cargo apron to enter/exit the apron via L42.2 Mode of Operation - Easterly (RWY 10)2.2.1 Departing aircraft from Apron 1 will taxi via C1 or C2, C6 and turn left on taxiway A, A9 (holding point RWY 10).2.2.2 Arrival for Apron 1 on RWY 10 to vacate runway via A1 or A3, taxi via A,C5, C1 or C2 to the respective aircraft stand.2.2.3 Arriving / Departing aircraft for cargo apron to enter/exit the apron via L4Note:i) Aircraft taxiing on TWY C5 on to TWY C2, shall hold at IHPC5 when an aircraft is pushing back from N16, N17, or N18 facing west on C1 and will be instructed to resume taxi when pushing back aircraft commences pulling forward and reports crossing abeam N16.ii) Aircraft taxiing on TWY C5 on to TWY C1, shall hold at IHPC5 when an aircraft is pushing back from A10 or A12 facing west on C2 and will be instructed to resume taxi when pushing back aircraft reaches abeam A08.iii) Aircraft taxiing on TWY C5 on to TWY C1, shall hold at IHPC5 when an aircraft is pushing back from A14L or A14R facing west on C2 and will be instructed to resume taxi when pushing back aircraft commences pulling forward.iv) All arriving helicopters shall switch off their engines at IHP C5 and furtherfollow ATC instructions.v) When an aircraft is holding on TWY A3 at the Runway Holding Position (RHP), any aircraft taxiing on TWY A shall hold short of TWY A3 on TWY Avi) When an aircraft is holding on Taxiway A1, A3, A6, or A9, short of TWY A, the Runway 10-28 shall be considered occupied.vii) All departing helicopters shall pushback on respective taxi lane and tow up to IHP C6 (short of A) and further follow ATC instructions.viii) Startup of engines at idle power is permitted during pushback and on stands. However, startup of engines at idle power at aerobridge stands is permitted only after removal of aerobridge. Airlines/GHAs are responsibleto adhere to all ground precautions e.g. Wing Walkers/Traffic Marshallers, Ground Equipment, Vehicular Traffic on tail of the stand road etc. against jet blast/ingestion to ensure safety. Indian registered Aircraft should seek permission from AODM only to carry startup of engine/idle power engine run up on stand. However, ATC may be informed through RT in case of any emergency situation. During idle power engine run up, AME will take all ground precautions including switching on aircraft anti-collision lights, positioning of wing walkers and RT trained engineer to be available in in cockpit. In case of foreign registered aircraft, if pilot conducts idle power engine start/ run up, he will seek permission from ATCix) In case of APU failure, the aircraft may be permitted to start one or both starboard side engines at idle power on the stand with the aerobridge attached. Further, in case of APU failure, a cross-bleed start is permitted only after completion of pushback, pull forward (if applicable) and disconnection of Tug. No cross bleed is permitted at stand or during pushback. Pilots to inform ATC and take all ground precautions against jet blast before starting cross-bleed. Airlines/GHAs are responsible to adhere to all ground precautions to ensure safety. |
3. Low Visibility Procedures3.1 Purpose: The purpose of these procedures is to ensure safe and efficient operations ofaircraft, vehicle/equipment, and personnel during low visibility operations at Noida International Airport, Jewar.3.2 Scope: Every year due to low visibility conditions during the period from 15 DEC to 15 FEB, aircraft operators are not permitted to file Noida International airport as alternate airport, if the latest met forecasted general visibility isexpected to be below 550 M, at estimated time of use.When visibility is less than 550 M RVR, landings are not permitted at Noida International Airport since aerodrome is certified only for CAT-I ILS operations.LVTO, however, will be permitted up to RVR 350 m.3.3 Definitions:3.3.1 Low Visibility Procedures (LVP): Specific procedures applied at an aerodrome for the purpose of ensuring safe operations during Categories II and III approaches and/or low visibility take-offsNote: as per para 5.3 of Civil Aviation Requirement on All Weather Operations, an operator shall not conduct Take-off with RVR/Visibility less than standard CAT-I conditions of 550m RVR/800m Visibility unless low visibility procedures are enforced3.3.2 Safeguarding Procedures (SP): Safeguarding Procedures (SP) are instructions for relevant airport, departments, and airside operators to prepare ground services and facilities for low visibility operations in order that when LVP are implemented all Safeguarding procedures are complete.3.3.3 Low Visibility Take-off (LVTO): A term used in relation to flight operations referring to a take-off on RWY where the RVR is less than 400M.3.3.4 Visibility: The greatest distance at which a black object of suitable dimensions, situated near the ground, can be seen and recognized when observed against a bright background.The greatest distance at which lights in the vicinity of 1000 candelas can be seen and identified against an unlit background.3.3.5 Runway visual Range (RVR): The range over which the pilot of an aircraft on the centreline of a runway can see the runway surface marking or the lights delineating the runway or identifying its centre line.3.3.6 Instrument runway: One of the following types of runways intended for the operation of aircraft using instrument approach procedures:3.3.7 Instrument Approach Operations. An approach and landing using instruments for navigation guidance based on an instrument approach procedure. There are two methods for executing instrument approach operations:a) a two-dimensional (2D) instrument approach operation, using lateral navigation guidance only; andb) a three-dimensional (3D) instrument approach operation, using both lateral and vertical navigation guidance.Lateral and vertical navigation guidance refers to the guidance provided either by:a) a ground-based radio navigation aid; orb) computer-generated navigation data from ground-based, space-based, selfcontained navigation aids or a combination of these.Instrument approach operations shall be classified based on the designed lowest operating minima below which an approach operation shall only be continued with the required visual reference as follows:a) Type A: a minimum descent height or decision height at or above 75 m (250 ft); andb) Type B: a decision height below 75 m (250 ft).3.3.8 Precision approach runway, category I-A runway served by visual aids and nonvisualaid(s) intended for landing operations following an instrument approachoperation type B with a decision height (DH) not lower than 60 m (200 ft.) and either avisibility not less than 800 m or a runway visual range not less than 550 m.3.3.9 Precision approach runway, category II- A runway served by visual aids and nonvisual aid(s) intended for landing operations following an instrument approachoperation type B with a decision height (DH) lower than 60 m (200 ft) but not lower than 30 m (100 ft.) and a runway visual range not less than 300 m.3.3.10 Precision approach runway, category III- A runway served by visual aids and nonvisualaid(s) intended for landing operations following an instrument approachoperation type B with a decision height (DH) lower than 30 m (100 ft), or no decisionheight and a runway visual range less than 300 m or no runway visual range limitation.3.3.11 Decision Height: A specified altitude or height in a 3D instrument approach operation at which a missed approach must be initiated if the required visual reference to continue the approach has not been established. Note. -- Decision altitude (DA) is referenced to mean sea level and decision height (DH) is referenced to the threshold elevation.3.3.12 ILS Critical Area: An area of defined dimensions about the localizer and glide pathantennas where aircraft and vehicles are excluded during all ILS operations. The criticalarea is protected because the presence of vehicles / or aircraft inside its boundaries willcause unacceptable disturbance to the ILS signal-in-space3.3.13 ILS Sensitive Area: An area extending beyond the ILS critical area where the parkingand/or movement of vehicles, including aircraft, are controlled to prevent the possibilityof unacceptable interference to the ILS signal during ILS operations. The sensitive areais protected to provide protection against interferences cause by large moving objectsoutside the critical area but still normally within the airfield boundary |
3.3.14 Obstacle Free Zone: The airspace above the inner approach surface, inner transitional surface and balked landing surface and that portion of the strip bounded by these surfaces, which is not penetrated by any fixed obstacle other than of low mass and frangible mounting, required for air navigation purposes.3.4 Abbreviations: |
LVP |
Low Visibility Procedures |
SP |
Safeguarding Procedures |
DGCA |
Directorate General of Civil Aviation |
NIA |
Noida International Airport |
ATC |
Air Traffic Control |
ARFF |
Aircraft Rescue and Firefighting |
APOC |
Airport Operations Control |
TDZ |
Touch Down Zone |
RVR |
Runway Visual Range |
ILS |
Instrument Landing System |
SMR |
Surface Movement Radar |
ADAC |
Aerodrome Advisory Circular |
IAPP |
Isolated Aircraft Parking Position |
3.5 Criteria for implementation of LVP: |
Activity |
Criteria |
Responsibility |
Initiation of SafeguardingProcedures |
When RVR is less than1200m or visibility isforecasted to deteriorateto 800m or less and/ orcloud ceiling is 400ft andforecasted to fall to 200ft |
Information by ATC toApron Control, APOCand ARFF |
Implementing LVP |
Either TDZ, mid or endRVR is less than 800Mand/or the cloud ceiling isless than 200ft, andsafeguarding proceduresare complete |
ATC will ImplementLVP |
Note: Airport arrivals shall be suspended at RVR below 550m, and departures shall besuspended at RVR below350 M .3.6 Minimum Requirements for Aeronautical Ground Lights3.6.1 The following aeronautical ground lights shall be serviceable to the required standard to support CAT I operations on Runway 10/28 |
Runways | |
Runway 28 |
Runway 10 |
Runway Approach Lights |
Runway Approach Lights |
Runway Edge Lights |
Runway Edge Lights |
Runway End Lights |
Runway End Lights |
Runway Centre line lights |
Runway Centre line lights |
Stop Bar |
Stop Bar |
Threshold Lights |
Threshold Lights |
Wing bar Threshold |
Wing bar Threshold |
Runway Guard Lights |
Runway Guard Lights |
Sequence Flashing Lights |
Sequence Flashing Lights |
Touch Down Zone Lights |
|
RWY Side Row Barrettes |
|
Taxiways |
|
Centreline lights |
|
Intermediate Holding Position |
|
|
|
Edge Lights |
|
3.6.2 Maximum Switchover time: |
3.7 Roles and Responsibilities:3.7.1 Action by ATC:3.7.1.1 Inform APOC, Apron control and ARFF when meteorological criteria are met for visibility standby and initiating safeguarding procedures.3.7.1.2 Switch on all AGL and facilitate of runway, taxiway and apron. Facilitate Follow me for manoeuvring area and apron inspection to complete safeguarding procedures. |
3.7.1.3 When meteorological criteria are met and safeguarding procedures are completed, implement LVP and inform APOC apron control and ARFF.3.7.1.4 ATC shall Broadcast in ATIS regarding LVP is in force.3.7.1.5 Stop bar lights associated with runway shall be switched on all the time.3.7.1.6 Stop bar lights associated with taxiway shall be switched on after safeguard procedure is initiated.3.7.1.7 ATC shall not permit high power engine ground runup after the initiation of safeguarding procedures till termination of safeguarding procedures. In case high power engine runup is in progress the same shall be stopped and towed back torespective stand in coordination with APOC before implementing LVP.3.7.2 Action by Met office:3.7.2.1 Duty MET officer shall ensure timely dissemination of any change in visibility or RVR to tower supervisor when RVR less than 1200M or visibility is forecasted to deteriorate to 800M or less and or cloud ceiling is 400ft and forecasted to fall to 200ft3.7.2.2 The duty MET officer shall ensure that the RVR displays in ATC units, controltower and approach control are serviceable. He shall ensure that RVR/visibilityrecorders of TDZ, Mid and end position are serviceable.3.7.2.3 In case of unserviceability of RVR equipment, he shall depute a Met officer forsupplementing manual RVR.3.7.3 Action by DM Airside Operations:3.7.3.1 Once safeguarding procedures are initiated, inform Follow Me in coordination with electrical team to complete safeguarding procedures.3.7.3.2 Coordinate with ATC, APOC and Follow me for implementation of LVP.3.7.3.3 Inform APOC and ATC once safeguarding procedures are completed.3.7.3.4 Coordinate and facilitate MET officials as and when required for any unserviceability or manual reading of RVR.3.7.4 Action by Follow me:3.7.4.1 No vehicles shall enter manoeuvring area without serviceable VEELO.3.7.4.2 Ensure timely completion of safeguarding procedures as per checklist and report to DM Airside.3.7.4.3 Stop all maintenance works (civil, electrical and project) in airside and if work is inside manoeuvring area, clear all men and material.3.7.4.4 Ensure Safeguarding inspection along with Shift Engineer Electrical as per checklist.3.7.4.5 Shall ensure that all LVOP boards are switched ON.3.7.4.6 Ensure closure of portion of perimeter road leading to critical/sensitive areas.3.7.4.7 Ensure TWY & Apron lights inspection along with Electrical team at 02hrs intervals3.7.4.8 Ensure Stop bars lights associated with taxiway are switched ON during implementation of safeguard procedure3.7.5 Actions by ARFF:3.7.5.1 Once safeguarding procedures are initiated Shift In-charge ARFF shall position CFT at the pre-determined positions. The CFT shall remain at PDP till the safeguarding procedures are withdrawn PDP locations:a) PDP 01 - On ARFF access road leading to RWY 10/28b) PDP 02 - West of Isolated Aircraft Parking Positionc) PDP 03 - On access road abeam airside gate 23.7.6 Action by Shift Engineer electrical:3.7.6.1 Ensure joint AGL inspection along with Follow Me to complete safeguarding procedures and when required during LVP.3.7.6.2 Ensure AGL supply switch over to DG/UPS as per the compliance requirement in coordination with Follow Me and ATC.3.7.6.3 Ensure CCR is always manned during LVP and maintains two-way communication with Apron Control.3.7.6.4 Notify Duty Manager Airside in real time in case of any AGL unserviceability noticed3.7.7 Action by Duty Manager APOC:3.7.7.1 APOC shall inform Apron Control, ARFF, CCR, CISF and all stakeholders regarding LVP operations. APOC shall start planning of their resources accordingly and maintain two-way communication with ATC and Airside Operations3.7.8 Suspension criteria for Low Visibility Operations3.7.8.1 Low Visibility Procedures will not be implemented / suspended when any of the light/equipment mentioned in table below is un-serviceable or is not maintained as per the required standard: |
Aeronautical GroundLighting Facility |
Un-serviceability |
Restrictions |
Approach Lights |
More than 15% of all lights areunserviceable |
Suspend CAT-IOperations |
Any two consecutive lights or more areunserviceable | ||
Runway Edge lights |
Any two consecutive lights or more areunserviceable |
Suspend CAT-IOperations |
Any one of the two circuits serving thepower supplygoes unserviceable | ||
Runway centre line lights |
More than 15% of all lights areunserviceable |
Suspend CAT-IOperations |
Any two consecutive lights or more areunserviceable | ||
Runway End lights |
More than 25% of all Lights |
Suspend CAT-I Operations |
Two adjacent lamps | ||
Standby Generators |
Any of the generators is unserviceable |
Suspend CAT-IOperations |
3.7.8.2 Unserviceability of Aeronautical Ground Lights/ Equipment after Implementation of LVP:When any of the light/equipment mentioned in para 3.8.8. above becomes unserviceable or fails to meet the required standard during periods of LVP, ADC/SMC shall advise the aircraft accordingly and LVP shall be suspended and information to this effect shall be included in ATIS broadcast.3.7.8.3 LOW VISIBILITY TAKE-OFF (LVTO):LVTO pertains to take off when the RVR is below 400 m and is applicable whenever the reported RVR in any zone (touch-down/mid/roll-out RVR) is below 400 m. LVTO, however, will be permitted up to RVR 350 m only.3.7.8.4 The facilities and conditions of the undermentioned Table required will be as per the lowest RVR reported in any zone (e.g. if the RVR is 400M/300M/300M representing the three zones, then the 300 m will be the RVR for reckoning facilities and conditions of the undermentioned Table. |
Take-off RVR/ Visibility | |
Facilities |
RVR/VIS (Refer Note l)CAT A, B, C, & D |
Adequate Visual reference (Day Only)(Refer Note 1) |
500 M |
Runway edge lights or Runwaycentreline markings(Refer Note 2) |
400 M |
Note-1: Adequate Visual Reference means, that a pilot is able to continuously identify the take-off surface and maintain directional control.Note-2: For night operations at least, Runway edge lights or centre line lights and Runway end lights are available.Note-3: An operator shall not conduct low visibility take-offs in less than 400m RVR unless approved by DGCA.Note-4: An operator shall not conduct take-off with visibility / RVR less than Category-I conditions unless low visibility procedures are enforced.Note-5: The required RVR must be achieved for all relevant RVR reporting points (touchdown, mid-point and stop-end/rollout). The governing RVR shall be the lowest of the reported RVRs.3.7.8.5 Restrictions during LVTO:• TWY A1 & A9 will be used for entry onto the Runway.• Entry via TWY A3 will be prohibited during LVTO.• Intersection departures will be prohibited.• Only one pushback will be permitted from passenger apron or cargo apron when either TDZ / MID / END RVR is less than 400 M.• Follow me service shall be provided as per the request from flight crew or as instructed by ATC.• Only essential vehicles with transponders shall be permitted in the manoeuvring area when LVTO is in force.3.7.9 Suspension of LVTO:When any of the light/equipment mentioned in table below becomes unserviceable or fails to meet the required standard during periods of LVTO, ADC/SMC shall advise the aircraft accordingly and LVTO shall be suspended and information to this effect shall be included in ATIS broadcast |
AGL Facility |
Un-serviceability |
Effect / Restrictions /Remarks |
Runway Edge lights |
More than 15% of alllights are unserviceable. |
Suspend LVTO |
Runway End lights |
More than 15% of alllights are unserviceable |
Suspend LVTO. |
Runway centre linelights |
More than 15% of alllights are unserviceable |
No impact / restrictions forLVTO |
4 ISOLATED AIRCRAFT PARKING POSITION/ HIGH-POWER ENGINE RUN UP BAY |
StandDesignation |
Coordinates |
Surface |
PCR |
Elevation |
AircraftSuitability |
Location |
IAPP |
281053.284N0773527.093E |
Asphalt |
790/F/C/W/T |
649 FT |
Up toCodeLetter E |
West ofTWY A9and TWYjunction,facing west |
4.1 The Isolated Aircraft Parking Position is in power-in/pushback configuration.4.2 Fuel bowser will be used for re-fuelling4.3 While aircraft is parked on this position under unlawful interference or bomb threat, the left turn from taxiway A towards IAPP is not permitted.4.4 While aircraft is parked on this position under unlawful interference or bomb threat, the right turn from taxiway A9 towards IAPP is not permitted.4.5 High power engine run up shall not be authorized if IAPP is occupied by an aircraft under unlawful interference or bomb threat4.6 TWY A9 is not available while any aircraft is pushing back from IAPP on TWY A / TWY A9 facing west / south4.7 High power engine run up shall be approved only during periods of lean air traffic movements as per the discretion of ATC.4.8 Aircraft shall tow / taxi to TWY A9 and then will be pushed back via tow truck on IAPP facing east to carry out high power engine run up or as instructed by ATC.4.9 Follow me service shall be provided while the aircraft is towing to/from IAPP.4.10 High power engine run up shall be conducted only with prior approval from Apron Control |
S.No |
Designation |
PCR |
Surface |
Width(m) |
Shoulder(m) |
Suitability |
1 |
TWY A |
790/F/C/W/T |
Asphalt |
23 |
7.5 |
Code E |
2 |
TWY A1 |
1180/R/C/W/T |
Concrete |
23 |
7.5 |
Code E |
3 |
TWY A3 |
790/F/C/W/T |
Asphalt |
23 |
7.5 |
Code E |
4 |
TWY A6 |
555/F/C/W/T |
Asphalt |
23 |
7.5 |
Code E |
5 |
TWY A9 |
1180/R/C/W/T |
Concrete |
23 |
7.5 |
Code E |
6 |
TWY B |
1180/R/C/W/T |
Concrete |
23 |
7.5 |
Code E |
7 |
TXL C1 |
1180/R/C/W/T |
Concrete |
15 |
|
Code C |
8 |
TXL C2 |
1180/R/C/W/T |
Concrete |
15 |
|
Code C |
9 |
TWY C5 |
790/F/C/W/T |
Asphalt |
23 |
7.5 |
Code E |
10 |
TWY C6 |
790/F/C/W/T |
Asphalt |
23 |
7.5 |
Code E |
11 |
TWY L4 |
790/F/C/W/T |
Asphalt |
23 |
7.5 |
Code E |
2. Description of Equipment and Services2.1 Runway Visual Range (RVR)There are three forward scatter meters for RWY 28/10 to record RVR values. One forward scatter meter (FSM) is located each at touchdown zone, runway midpoint, and end of runway. RVR values always refer to Touchdown RVR (TDZ), Midpoint RVR(MID) and End RVR (END). |
|
1. Aerodrome Chart (22 January 2026) 2. Aircraft Parking/Docking Chart (22 January 2026) 3.Aircraft Parking/Docking Chart Cargo Apron (22 January 2026) 4. Aerodrome Obstacle Chart - Type A RWY 10 (22 January 2026) 5. Aerodrome Obstacle Chart - Type A RWY 28 (22 January 2026) 6. Aerodrome Obstacle Chart - Type B (22 January 2026) 7. Precision Approach Terrain Chart RWY 10 (22 January 2026) 8. Precision Approach Terrain Chart RWY 28 (22 January 2026) 9. ILS Critical and Sensitive Area Chart (22 January 2026) 10.TORA and LDA chart(22 January 2026) 11. Instrument Approach Chart - ILS OR LOC Y RWY 28, CAT II & CAT III (27 November 2025) 12. Instrument Approach Chart - ILS OR LOC Y RWY 10 (27 November 2025) 13. Instrument Approach Chart - RNP RWY 10 (27 November 2025) 14. Tabular Description 1 - RNP Procedure RWY 10 15. Tabular Description 2 - RNP Procedure RWY 10 16. Instrument Approach Chart - RNP RWY 28 (27 November 2025) |
VIND |
Procedure | ||
1 | ||
|
|