JeppView for Windows. General Information. Runway Information. Communication Information. jep=jeppesen

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1 Airport Information For LIML Printed on ec 207 Page (c) SANERSON, INC., 207, ALL RIGHTS RESERVE jep= JeppView for Windows General Information ATIS: Linate Tower: 8.00 Location: MILAN ITA Linate Tower: At or below 4000 ft Out to 5 mi. ICAO/IATA: LIML / Linate Planning Tower: Lat/Long: N ', E ' Linate Ground: Elevation: 353 ft Milan Radar Approach: Milan Radar Approach: Milan Radar Approach: Airport Use: Public Milan Radar Approach: aylight Savings: Observed UTC Conversion: -:00 = UTC Magnetic Variation:.0 E Fuel Types: 00 Octane (LL), Jet A- Repair Types: Minor Airframe, Minor Engine Customs: Yes Airport Type: IFR Landing Fee: Yes Control Tower: Yes Jet Start Unit: No LLWS Alert: No Beacon: Yes Sunrise: 0652 Z Sunset: 540 Z Runway Information Runway: 7 Length x Width: 972 ft x 72 ft Surface Type: bitu TZ-Elev: 352 ft Runway: 8 Length x Width: 802 ft x 97 ft Surface Type: asphalt TZ-Elev: 353 ft Lighting: Edge, ALS, Centerline Runway: 35 Length x Width: 972 ft x 72 ft Surface Type: bitu TZ-Elev: 349 ft Runway: 36 Length x Width: 802 ft x 97 ft Surface Type: asphalt TZ-Elev: 345 ft Lighting: Edge, ALS, Centerline, TZ Communication Information

2 Airport Information For LIML Printed on ec 207 Page 2 (c) SANERSON, INC., 207, ALL RIGHTS RESERVE jep= JeppView for Windows General Information ATIS: Linate Tower: 8.00 Location: MILAN ITA Linate Tower: At or below 4000 ft Out to 5 mi. ICAO/IATA: LIML / Linate Planning Tower: Lat/Long: N ', E ' Linate Ground: Elevation: 353 ft Milan Radar Approach: Milan Radar Approach: Milan Radar Approach: Airport Use: Public Milan Radar Approach: aylight Savings: Observed UTC Conversion: -:00 = UTC Magnetic Variation:.0 E Fuel Types: 00 Octane (LL), Jet A- Repair Types: Minor Airframe, Minor Engine Customs: Yes Airport Type: IFR Landing Fee: Yes Control Tower: Yes Jet Start Unit: No LLWS Alert: No Beacon: Yes Sunrise: 0652 Z Sunset: 540 Z Runway Information Runway: 7 Length x Width: 972 ft x 72 ft Surface Type: bitu TZ-Elev: 352 ft Runway: 8 Length x Width: 802 ft x 97 ft Surface Type: asphalt TZ-Elev: 353 ft Lighting: Edge, ALS, Centerline Runway: 35 Length x Width: 972 ft x 72 ft Surface Type: bitu TZ-Elev: 349 ft Runway: 36 Length x Width: 802 ft x 97 ft Surface Type: asphalt TZ-Elev: 345 ft Lighting: Edge, ALS, Centerline, TZ Communication Information

3 , 2006, ALL RIGHTS RESERVE. Printed from JeppView for Windows on ec 207; Terminal chart data cycle ; Notice: After 4 ec 207, 0000Z, this chart may no longer be valid + 20-P 9 JUN 09 Eff.2.Jul AIRPORT.BRIEFING. GENERAL.. ATIS ATIS NOISE ABATEMENT PROCEURES.2.. REVERSE THRUST The use of reverse thrust at power higher than idle is allowed only in the event of proven safety/operational reasons RUN-UP TESTS Engine tests at high power are prohibited between LT, except for ACFT to be used immediately AUXILIARY POWER UNITS (APUs) Use of APU is allowed 30 minutes before departure, 5 minutes after arrival and 5 minutes at parking docks LOW VISIBILITY PROCEURES (LVP).3.. GENERAL LVP will be applied during CAT II/III and departure operations when - RVR reported at TZ is 550m or below, - ceiling is below 200' according to the local MET report, - the rapid detoriation of weather conditions recommends so. Pilots will be informed via ATIS and/or RTF when LVP are in force GROUN MOVEMENT For Low Visibility Taxi Routes refer to 20-9 charts GENERAL In case of failure of the Surface Movement Radar with RVR, measured on any available transmissometer, is below 400m only one ACFT movement at the time is allowed and Follow-me assistance always mandatory ARRIVAL Landing ACFT shall vacate the RWY preferentially via TWY K to the West Apron and only via TWY G to the North Apron. TWY J not available. ACFT shall report to Tower when the ILS sensitive area has been vacated (identified by the end of the green/yellow color coded TWY centerline lights) and when the assigned stand has been reached EPARTURE ACFT shall enter RWY 36 via TWY T only. TWY J not available. Holding bay RWY 36 not available. When RVR, measured on any available transmissometer, is below 400m, Follow-me assistance is mandatory on West Apron.

4 , 2006, ALL RIGHTS RESERVE. Printed from JeppView for Windows on ec 207; Terminal chart data cycle ; Notice: After 4 ec 207, 0000Z, this chart may no longer be valid + 20-P 9 JUN 09 Eff.2.Jul AIRPORT.BRIEFING. GENERAL.4. SURFACE MOVEMENT GUIANCE AN CONTROL SYSTEM.4.. OPERATION OF MOE S TRANSPONER WHEN ACFT IS ON GROUN.4... ACFT EQUIPPE WITH MOE S TRANSPONER From either push-back or taxi request, whichever is earlier: - Enter through the FMS or transponder control panel: - Flight Identification as specified in item 7 of ICAO flight plan form; or - In the absence of Flight Identification, the ACFT Registration; - Select XPR or its equivalent depending on the specifications of the installed model; - Select AUTO mode, if the function is available; - o not select the OFF or STAN BY functions; - Set the Mode A code assigned by ATC. After landing until at a stand: - Select XPR or its equivalent depending on the specifications of the installed model; - Select AUTO mode, if the function is available; - o not select the OFF or STAN BY functions; - Maintain the Mode A code assigned by ATC. On the movement area: - Select XPR or its equivalent depending on the specifications of the installed model; - Select AUTO mode, if the function is available; - o not select the OFF or STAN BY functions; - Set Mode A code to ACFT NOT EQUIPPE WITH MOE S TRANSPONER OR WITH UNSERVICEABLE MOE S TRANSPONER eparting ACFT maintain Mode A + C transponder OFF until line-up. Arriving ACFT set the Mode A + C transponder to OFF as soon as the RWY is vacated. On the movement area maintain Mode A + C transponder OFF for all the duration of displacement WARNING TCAS should be selected before entering the RWY, after receiving line-up clearance and should be deselected after vacating the RWY..5. RWY OPERATIONS.5.. PREFERENTIAL RWY SYSTEM Use RWY 36. MAX tailwind component 7 KT (dry RWY) or 5 KT (wet RWY). According to ENAC provision /OML dated , take-off operations from RWY 8 are permitted only when meteo conditions or safety reasons do not allow the use of the preferential RWY MINIMUM RWY OCCUPANCY TIME To minimize spacing between successive approaches, a special operational practice applies, unless otherwise instructed by Tower and with due respect to flight safety.

5 , 2006, 207. ALL RIGHTS RESERVE. Printed from JeppView for Windows on ec 207; Terminal chart data cycle ; Notice: After 4 ec 207, 0000Z, this chart may no longer be valid +. GENERAL.6. TAXI PROCEURES.6.. GENERAL ACFT with taxi allowance must switch on landing lights. TWY A MAX wingspan 8 /36m. 20-P2 3 NOV 7.Eff.9.Nov. TWY K centerline lights visible from RWY 8/36 to West apron only..airport.briefing. TWY K available for ACFT with MAX wingspan ICAO class C and MAX outer main gear wheel span ICAO class B. All ACFT not in compliance must inform Tower in advance. ACFT with a tail height above 30'/9m must inform Ground before entering TWY N. Any ACFT prior to taxi on the stretch of TWY N located along the extended RWY centerline of RWY 36 shall request and obtain specific ATC authorization RWY CROSSING PROCEURE ACFT which is required to cross or to taxi on active RWY will be issued instructions by the Ground controller, which will include a RWY holding position as a clearance limit, in which the ACFT will be required to hold short of the active RWY. When reaching the clearance limit specified in the taxiing instructions, the ACFT will be instructed to change frequency to Tower. After crossing RWY and having reported "RWY vacated" to the Tower controller, ACFT will be instructed to revert to Ground for further clearance. In the absence of further clearance it is essential that the ACFT does not proceed beyond the first position cleared of the RWY..7. PARKING INFORMATION Stands thru 5 equipped with visual docking guidance system, push-back required. On stands 3, 62, 64, 65, 67, 69 and 7 push-back required. On stands 5 thru 56 and areas GA and GA2, push-back or tow to get out compulsory for ACFT above MTOW 4000kg. Taxiing out with Follow-me or marshaller assistance allowed only as follows: - From area GA3 for all ACFT; - From area GA2 for ACFT with MTOW below 4000kg and for turboprop. Parking areas GA, GA2, GA3 and stands 5 thru 56 use of Follow-me car or marshalling service is always required from/to holding positions N/K and for all West apron ACFT movements..8. OTHER INFORMATION Aerodrome occasionally affected by terrain-induced wind shear phenomena, more frequently occurring from May to July, mostly originated by northern winds. Birds on maneuvering area and surroundings. A local anomaly in the earth magnetic field on the ground has been reported and measured on the area close to TZ RWY 36. In this area local magnetic North indication may vary considerably and may affect onboard settings. Some problems have been reported by M80 ACFT equipped with AHRS (Attitude Heading Reference System).

6 , 2006, 207. ALL RIGHTS RESERVE. Printed from JeppView for Windows on ec 207; Terminal chart data cycle ; Notice: After 4 ec 207, 0000Z, this chart may no longer be valid +.AIRPORT.BRIEFING. 2. ARRIVAL 2.. SPEE RESTRICTIONS Unless otherwise instructed by ATC pilots must comply with the following speed control: KT at or below FL KT when starting turn to intercept ILS LOC or appropriate VOR radial or when on ST-IN APCH at 2NM from THR KT when completing turn to intercept ILS LOC or when on ST-IN APCH at 9NM from THR KT at 7NM from THR. 20-P3 3 NOV 7.Eff.9.Nov CAT II/III OPERATIONS RWY 36 approved for CAT II/III operations, special aircrew and ACFT certification required RWY OPERATIONS MINIMUM RWY OCCUPANCY TIME After vacating RWY, ACFT shall not stop before having passed the holding line. Propeller and turbo propeller engine ACFT shall vacate the RWY as far as possible by TWY K if bound to West apron TAXI PROCEURE COMMUNICATION FAILURE Whenever an ACFT experiences a communication failure, it shall vacate the RWY and the ILS sensitive area via the appropriate TWY and wait on its first segment for the arrival of the Follow-me car in order to be guided to the stand PROVISIONS FOR GENERAL AVIATION ACFT ON WEST APRON Landing ACFT shall contact West Apron Coordination (3.775, Tel: ) to communicate the handler chosen to notify APT of departure before switching off engines: - Signature Flight Support on 3.40; - Sky Services on 3.9; - Universal Aviation Italy on 3.550; - Argos VIP Private Handling on 3.475; - Aviapartner. Pilots shall inform the selected handler of arrival time. Pilots shall wait for Follow-me or marshalling service on holding points N and K OTHER INFORMATION Arriving traffic is requested to provide Tower with indication of distance on final at first contact. uring VOR unavailability all radial values referred to VOR can be intended as bearings referred to LCTR of same value. uring TZO VOR unavailability all radial values referred to TZO VOR can be intended as bearings referred to TZO NB of same value.

7 , 2006, 207. ALL RIGHTS RESERVE. Printed from JeppView for Windows on ec 207; Terminal chart data cycle ; Notice: After 4 ec 207, 0000Z, this chart may no longer be valid +.AIRPORT.BRIEFING. 3. EPARTURE 3.. APT COLLABORATIVE ECISION MAKING (A-CM) PROCEURE 3... INTROUCTION APT Collaborative ecision Making (A-CM) procedure coordinates the turnaround process and is incorporated into the European Air Traffic Flow and Capacity Management (ATFCM). The procedure starts at EOBT -3 hours and is applied to all the operations until Take-Off. A-CM Milestone approach is mainly based on TOBT and TSAT. TOBT (Target Off-Block Time): 20-P4 27 OCT 7.Eff.9.Nov MILESTONES EOBT -3 HOURS (M) ATC flight plan will be checked against their APT Slot - Scheduled Off-Block Time (SOBT); other checks include the destination APT type of ACFT and registration marks. If they do not correspond, the flight will not enter the pre-departure sequence and an alert is risen on the local A-CM platform. AO/GH must take the appropriate actions to solve the alerts at the earliest possible. General Aviation Flights shall communicate their plans to operate on the APT in advance to SEA to allow SEA to publish SOBT on A-CM platform EOBT -2 HOURS (M2) TOBT is the time when the ACFT is planned to be "ready to move". For turnaround flights at EOBT -2 hours, the system will automatically generate a TOBT as follows: Flights not subject to turnaround will enter the pre-departure sequence with a TOBT=EOBT. In both cases, the AO/GH can input a manual TOBT that should comply with following rule: EOBT -5 minutes less than TOBT less than EOBT +5 minutes This rule applies only for flights without CTOT, for regulated flights the rule to apply is TOBT + EXOT less than CTOT. At EOBT -2 hours, a T-PI-t message will be sent to NMOC containing the TTOT TOBT -40 MINUTES: TSAT ISSUE TIME (M9) AO/GH is responsible to confirm TOBT at EOBT-40 minutes. TOBT must be coherent with EOBT, according to the {5 minutes window. FPL must be updated by AO/GH if EOBT is not consistent with TOBT. At TOBT -40 minutes, ENAV A-CM platform will issue a TSAT based on the last confirmed TOBT. TOBT must be updated by AO/GH for any change. Estimated time, calculated by an ACFT Operator/Ground Handler (AO/GH), when an ACFT will be "ready to move". TSAT (Target Start-Up Approval Time): Calculated time at which start-up clearance can be expected at the latest. TSAT includes all relevant parameters such as CTOT, variable taxiing time, etc. TOBT = ELT+EXIT+MTT - for inbound flights not yet landed TOBT = ALT+EXIT+MTT - for flights already landed TOBT = AIBT+MTT - for ACFT at the parking stand TOBT can be updated as often as desired until TSAT issue time, after that TOBT may be updated up to a maximum of 3 times, then the flight will lose priority in the pre-departure sequence. At EOBT -40 minutes, a T-PI-s message will be sent to NMOC containing TOBT, TTOT, TSAT.

8 , 2006, 207. ALL RIGHTS RESERVE. Printed from JeppView for Windows on ec 207; Terminal chart data cycle ; Notice: After 4 ec 207, 0000Z, this chart may no longer be valid + 20-P5 27 OCT 7.Eff.9.Nov. 3. EPARTURE.AIRPORT.BRIEFING ART (ACTUAL REAY TIME) (M2) eparting traffic must be "ready to move" within TOBT {5 minutes and must contact SEA Apron Unit (Tel: ) to obtain the ART. SEA Apron Operation Unit, after the check of "ready to move" status, will issue the ART and provide the pilot with the current TSAT. If the ACFT is not "ready to move" within TOBT +5 minutes, TOBT will be automatically deleted by A-CM platform. A new TOBT must be inserted in the platform within 5 minutes, otherwise a Flight Suspension Message (FLS) will be triggered by NMOC with the comment "SUSPENE BY EPARTURE APT. PLEASE SEN LA/CHG OR UPATE TOBT OF THE FLIGHT". (E.g.: TOBT=000, no ART within 005, no TOBT update to FLS at 00). To de-suspend the flight, a new TOBT not less than previous TOBT +5 minutes must be inserted into A-CM platform. It is still mandatory to send a LA message to the IFPS if TOBT deviates by 5 minutes or more from EOBT. If the flight is subject to a CTOT, at ART a PI message will be sent to NMOC in order to try to get an improvement. There is no need to request a REA message to get a CTOT improvement ASAT AN AOBT (M4/M5) Once the ART has been obtained, departing traffic shall contact, within TSAT {5 minutes, Ground LT or Tower LT. eparting traffic must thus keep a listening watch on the appropriate ATC frequency in order to receive a possible improvement. If an improved TSAT is available after ART, ATC will contact the departing traffic to notify the revised TSAT. ATC will issue the en-route clearance and approve start-up according to TSAT and current traffic situation. eparting traffic must leave the stand within ASAT +5 minutes. At AOBT, an A-PI message will be sent to NMOC containing latest TTOT. After sending A-PI, CTOT updates will be not received and it will be not possible to update Flight Plan. If traffic is unable to leave the stand ASAT +5 minutes, or must return to the stand, it must inform ATC on the appropriate frequency. ATC will remove the flight from the pre-departure sequence and a C-PI message will be sent to NMOC, that in turn issues a FLS message with the comment "SUSPENE BY EPARTURE APT. PLEASE SEN LA/CHG OR UPATE TOBT OF THE FLIGHT". In this case the process has to be started over with a new TOBT ACFT E-ICING REQUEST Every request for de-icing/anti-icing shall be forwarded to the own handling operator. ue to the influence that ACFT de-icing has on the sequencing process, it is highly advised to request ACFT de-icing at the latest at TOBT -40 minutes. e-icing requests submitted up to 25 minutes before TOBT will be sequenced in accordance with TOBT. e-icing requests submitted later than 25 minutes before TOBT will be inserted in the sequence in the first position available, in order to guarantee the priority of the flights who requested the service timely. e-icing request and relevant data will be published on ACM platform.

9 , 204, 207. ALL RIGHTS RESERVE. Printed from JeppView for Windows on ec 207; Terminal chart data cycle ; Notice: After 4 ec 207, 0000Z, this chart may no longer be valid TOBT: RULES AN RESPONSIBILITY - Responsibility for TOBT: AO/GH is responsible for correct update and coherence of TOBT. - TOBT Correction/eletion:.AIRPORT.BRIEFING. If TOBT is changed, the new TOBT must be at least 5 minutes later than the present time. If TOBT can no longer be met, it must be updated as soon as possible. - TOBT input: TOBT can be put into SEA A-CM platform available for all registered users through a web platform or mobile app. - An account to access A-CM platform can be obtained via: infoacdm@seamilano.eu A-CM PROCEURE SUSPENSION In case of A-CM system failure, the procedure will be suspended and: - "A-CM out of service" will be announced via ATIS; - NOTAM will be issued if the suspension lasts more than 2 hours; - AO/GH will be informed by Aerodrome Operator SEA; - A standard Taxi Time Scheme will be adopted; - REA messages can be asked to ATC to request a CTOT improvement. Operations will follow "NON A-CM EPARTURES PROCEURES" NON-A-CM EPARTURE PROCEURES - FAILURE OR SUSPENSION When "ready to move", all departing ACFT must contact SEA Apron Unit (Tel: ) to obtain ART clearance. ATC will manage departure sequence according to the "first call - first served" principle, and EOBT and CTOT tolerances as specified in AIP ENR COORINATION WITH THE NMOC A-CM platform establishes a permanent and fully automatic data exchange with NMOC (Network Manager Operations Center). This data transfer will enable highly accurate early predictions of landing and departure times. Furthermore, this will allow more accurate and efficient calculation of CTOT due to the use of local target take-off times. The following messages are used: - Flight Update Message (FUM); - Early eparture Planning Information Message (EPI); - Target eparture Planning Information Message (TPI); - ATC eparture Planning Information Message (API); - Cancel PI (C-PI). 20-P6 27 OCT 7.Eff.9.Nov. 3. EPARTURE The basic NMOC procedures continue to be applied CONTACTS ENAV: SEA: acdm.linate@enav.it infoacdm@seamilano.eu

10 , 204, 207. ALL RIGHTS RESERVE. Printed from JeppView for Windows on ec 207; Terminal chart data cycle ; Notice: After 4 ec 207, 0000Z, this chart may no longer be valid + 3. EPARTURE 3.2. E-ICING GENERAL e-icing takes place at stands 73 thru 76. Stand 73, 75 and 76 MAX wingspan 8'/36m..AIRPORT.BRIEFING. Stand 74 MAX wingspan 57'/48m PROCEURE ACFT operator/pilot of ACFT shall submit the request to the de-icing provider, through the company or the ramp agent attending the flight, at least 50 minutes before EOBT. No request will be accepted during taxiing. Pilot, at start-up, will report to Tower to have already agreed upon de-icing operations. For de-icing position expect Tower instructions to position via apron TWY. Follow-me car assistance on pilot s request. uring LVP marshaller will guide the ACFT to the de-icing position. 20-P7 27 OCT 7.Eff.9.Nov. Pilot in command shall report to Tower "ready to move" only after ground de-icing procedures have been completed. In case of snowfall, all ACFT will be automatically booked for de-icing/de-snowing treatment. If treatment is not needed, advise Tower ACFT ENGINES STATUS URING OPERATIONS Twin-engine ACFT: Both on idle power. Three-engine ACFT: Tail out, internal idle power. Four-engine ACFT: External out, internal idle power. Propeller ACFT: Propellers should be stopped when possible START-UP AN TAXI PROCEURES GENERAL All General Aviation departing ACFT shall follow approved A-CM procedure. At West apron not later than 5 minutes after ATC start-up clearance, ACFT pushing-back or taxiing will be performed START-UP At West apron ATC start-up clearance shall be requested when ACFT is, according to TSAT, at stand or within areas GA, GA2 or GA3; start-up is allowed with one engine at minimum power TAXIING AT WEST APRON - APRON SUBJECT TO SPECIAL PROCEURES Pilot shall request taxiing from ATC when ready to move. Q and Q2 occupancy time shall be reduced to the minimum. TWY K from West Apron to RWY 7/35 AY only. Pilots are requested to report leaving the West Apron on intermediate holding position N and K. Pilot shall require TWR permission to taxi before leaving the West Apron. ACFT can only move after receiving authorization. ACFT not equipped with APU or APU inoperative are allowed to set in motion by a single motor at minimum power within stands or parking areas.

11 , 207. ALL RIGHTS RESERVE. Printed from JeppView for Windows on ec 207; Terminal chart data cycle ; Notice: After 4 ec 207, 0000Z, this chart may no longer be valid + 20-P8 27 OCT 7.Eff.9.Nov..AIRPORT.BRIEFING. 3. EPARTURE 3.4. COMMUNICATION FAILURE Whenever an ACFT experiences a communication failure, it shall continue strictly on the assigned taxi route to the clearance limit and wait for the arrival of the Follow-me car in order to be guided back to the stand NOISE ABATEMENT PROCEURES Because of noise abatement requirements pilots are requested to strictly adhere to initial climb procedures within the limits of ACFT performance criteria. Compliance with the procedures below shall not be required in adverse weather conditions or for safety reasons. uring the initial climb phase pilots shall maintain the following parameters: a) Up to 500' QFE - Take-off power; - Take-off flap; - Climb at V 2 + 0/20 KT or as limited by body angle; b) At 500' QFE - Reduce thrust and climb V 2 + 0/20 KT until reaching 3000 QFE; c) At QFE - Accelerate smoothly to enroute climb speed with flap retraction RWY OPERATIONS MINIMUM RWY OCCUPANCY TIME Pilots shall comply with instructions to line-up without any delay. Line-up manoeuvre shall start immediately after the preceding departing ACFT has begun the take-off run or the landing traffic has passed the THR. As far as possible pre-flight checks should be completed before line-up. Any other checks following line-up shall be carried out as quickly as possible. Take-off run shall start immediately after take-off clearance. Prior to line-up, pilots must inform Tower if unable to comply.

12 Printed from JeppView for Windows on ec 207; Terminal chart data cycle ; Notice: After 4 ec 207, 0000Z, this chart may no longer be valid MILAN Radar (APP) ' FL95 FL80 ITALY FRANCE 50 FL45 270^ FL70 or TL if higher FL ^ SWITZERLAN 60 ITALY FL90 8 AUG 7 20-R VOR ME 60.RAAR.MINIMUM.ALTITUES. Alt Set: hpa. Minimum altitudes provide at least 000' obstacle clearance within 3NM from sector boundary until 40NM from RAAR antenna and within 5NM of the sector boundary beyond 40NM from RAAR antenna. 2. Chart only to be used for cross-checking of altitudes while under radar control. 3. Outside radar minimum altitude sectors shown on chart, MEAs will be used. 4. Minimum altitudes assigned by ATC include a correction for low temperatures. FL50 FL5 20^ 330^ FL00 UNUSUAL CONTOUR STAGGERING FL Milan (Linate) FL0 MARSEILLE LFMM FIR 2500 FL95 80^ FL80 FL50 FL30 FL FL00 FL FL0 FL90 FL ^ 30 SWITZERLAN ^ 2 FL70 or TL if higher SWITZERLAN LSAS FIR 50^ 20^ 060^ AUSTRIA ITALY VIENNA LOVV FIR ^ MILAN LIMM FIR ROME LIRR FIR CONTOUR INTERVALS Reissue., 207. ALL RIGHTS RESERVE.

13 FL Printed from JeppView for Windows on ec 207; Terminal chart data cycle ; Notice: After 4 ec 207, 0000Z, this chart may no longer be valid 20-2 ATIS NOV 4.Eff.3.Nov. Alt Set: hpa KALIK B [KALIB], KALIK RWY 36 RNAV ARRIVALS P-RNAV [KALI].RNAV.STAR. 20^ 0,00' MSA VOR 4200' within 5 NM (L) 2.25 N E TREZZO (H) TZO.8 N E SOROP N E R75^ IXER N E ML6~4 N E FL00 INVES 26 N E LIMBA N E FL90 32 ML6~3 N E NOGMO N E KALIK 28 KALIK B HOGS OVER IXER INVES LIMBA R75^ 23 R64^ 26 R75^ 32 FL00 30^ 332^ TZO KALIK N E R66^ 67 FL00 67/7 346^ 23/27 STAR KALIK B KALIK By ATC MAX 20 KT 26/30 MHA 6000 KALIK - NOGMO - LIMBA - IXER. KALIK - ML603 - INVES - ML604 - SOROP. STARs transferred; RNAV STARs established. 344^ 32/37 irect distance to Linate Apt from: SOROP 3 NM, 204. ALL RIGHTS RESERVE.

14 Printed from JeppView for Windows on ec 207; Terminal chart data cycle ; Notice: After 4 ec 207, 0000Z, this chart may no longer be valid ATIS NOV A.Eff.3.Nov. Alt Set: hpa KALIK C [KALIC] RWY 8 RNAV ARRIVAL P-RNAV BY ATC.RNAV.STAR. 20^ 0,00' MSA VOR 4200' within 5 NM (L) 2.25 N E TREZZO (H) TZO.8 N E TZO 345 N E ^ R70^ MHA ^ 5000 ML6~7 N E TOVSA N E ^ ML6~6 N E FL00 TZO 344^ 67 R66^ KALIK N E /7 FL00 346^ irect distance to Linate Apt from: TZO 2 NM KALIK - ML606 - TOVSA - ML607 - TZO. STARs transferred; RNAV STAR established., 204. ALL RIGHTS RESERVE.

15 320^ Printed from JeppView for Windows on ec 207; Terminal chart data cycle ; Notice: After 4 ec 207, 0000Z, this chart may no longer be valid ATIS MAY B.Eff.28.May. Alt Set: hpa LUSIL A [LUSIA] OINA 2A [OIN2A] OSKOR A [OSKOA] RWY 36 ARRIVALS CONVENTIONAL/P-RNAV 20^ 0,00' MSA VOR.STAR. 4200' within 5 NM OINA N E ^ LUSIL N E ^ 48 FL30 OINA 2A TREZZO (H) TZO.8 N E TZO 345 N E R32^ 206^ 27 FL40 2 FL00 LUSIL A 267^ OSKOR A OSKOR N E (L) 2.25 N E ^ ORI ORIO AL SERIO ORI N E ^ 5000 COOGNO CO N E irect distance to Linate Apt from: CO 7 NM STAR LUSIL A OINA 2A By ATC OSKOR A On 205^ bearing to ORI, 206^ bearing to CO. On TZO R-32 inbound to TZO, turn RIGHT, TZO R-75/75^ bearing to CO. Tabular description. On 267^ bearing to ORI, turn LEFT, 206^ bearing to CO., 204, 205. ALL RIGHTS RESERVE.

16 6000 R75^ 9 23 Printed from JeppView for Windows on ec 207; Terminal chart data cycle ; Notice: After 4 ec 207, 0000Z, this chart may no longer be valid ATIS MAY C.Eff.28.May. Alt Set: hpa OINA R [OIR] RWY 36 TRANSITION N, S RWY 36 ARRIVALS CONVENTIONAL/P-RNAV 20^ 0,00' MSA VOR.STAR. 4200' within 5 NM OINA N E ^ HOGS OVER IXER UNAP FL70 or TL if higher 69^ 27 MAX 280 KT MHA 6000 FL30 OINA R 23 R75^ 27/24 MHA 5000 MAX 20 KT MAX 20 KT 69^ 23/27 SARONNO (H) 3.7 N E N E SULUR N E FL00 R330^ 69^ 349^ (L) 2.25 N E ^ N, S N UNAP N E SOROP N E ML6~8 N E ^ 5000 IXER N E irect distance to Linate Apt from: SOROP 3 NM TRANSITION OINA R STAR N By ATC S On R-330 inbound/50^ bearing via SULUR to. On R-69/69^ bearing via UNAP to 35, turn LEFT, 085^ track to IXER, intercept R-75 inbound to SOROP. On R-69/69^ bearing to UNAP. Tabular description., 204, 205. ALL RIGHTS RESERVE.

17 Printed from JeppView for Windows on ec 207; Terminal chart data cycle ; Notice: After 4 ec 207, 0000Z, this chart may no longer be valid ATIS EC Eff.7.Jan. Alt Set: hpa LUSIL C [LUSIC] OINA C [OINC], OINA [OIN] OSBUL C [OSBUC], OSKOR C [OSKOC] RWY 8 ARRIVALS CONVENTIONAL/P-RNAV 20^ 0,00' MSA VOR.STAR. 4200' within 5 NM OINA N E ^ 32^ LUSIL N E FL30 R330^ 6000 OINA SULUR N E HOG OVER SARONNO 3.7 N E FL30 OINA C N E FL70 or TL if higher ROMUN N E R32^ 45^ 2.25 N E TREZZO TZO.8 N E TZO 345 N E R42^ 325^ 5 R069^ 249^ FL90 By ATC 27 FL40 2 FL00 ORI ORIO AL SERIO ORI 205^ LUSIL C 267^ OSKOR C N E /30 ORIN N E OSKOR N E MAX 280 KT MHA OSBUL C MAX 20 KT 69^ 322^ 349^ STAR LUSIL C OINA C OINA By ATC OSBUL C By ATC OSKOR C irect distance to Linate Apt from: 6 NM TZO 2 NM On 206^ bearing to ORI, turn RIGHT, 249^ bearing to TZO. On TZO R-32 inbound via ROMUN to TZO. On R-330 inbound/50^ bearing via SULUR to. On TZO R-42 inbound/322^ bearing via ORIN to TZO. On 267^ bearing to ORI, turn LEFT, 249^ bearing to TZO. PAR STAR replaced by OSBUL. OSBUL N E00 7.6, 2004, 205. ALL RIGHTS RESERVE.

18 Printed from JeppView for Windows on ec 207; Terminal chart data cycle ; Notice: After 4 ec 207, 0000Z, this chart may no longer be valid ATIS KALIK 2A 25 EC E.Eff.7.Jan. Alt Set: hpa OSBUL B [OSBUB] RWY 36 ARRIVALS [KALI2A], CONVENTIONAL/P-RNAV BY ATC 20^ 0,00' MSA VOR.STAR. 4200' within 5 NM TREZZO.8 TZO N E N E COOGNO CO N E TOVSA N E ^ ^ 099^ R66^ 22 PABRO N E VOGHERA 5.5 VOG N E ^ IBLUN N E FL90 8 OSBUL B 306^ OSBUL N E FL95 KALIK 2A 67 KALIK N E MHA FL00 MAX 230 KT 346^ 346^ 67/7 HOG OVER CO 40^ 5000 irect distance to Linate Apt from: CO 7 NM STAR KALIK 2A OSBUL B On TZO R-66 inbound to IBLUN, turn LEFT, intercept 339^ bearing via TOVSA to CO. On 306^ bearing via PABRO to CO. PAR STAR replaced by OSBUL. 320^, 204, 205. ALL RIGHTS RESERVE.

19 Printed from JeppView for Windows on ec 207; Terminal chart data cycle ; Notice: After 4 ec 207, 0000Z, this chart may no longer be valid ATIS TOP R RWY 8 TRANSITION ASTIG [ASTI], GEN RWY 8 ARRIVALS CONVENTIONAL/P-RNAV 22 MAY F.Eff.28.May. Alt Set: hpa MAX 20 KT MHA 6000 MAX 280 KT FL70 or TL if higher 20^ 0,00' MSA VOR.STAR. 4200' within 5 NM SARONNO (H) 3.7 N E N E ^ R82^ 349^ TORINO (H) TOP 4.5 N E TOP N E ^ 8 FL90 TOP R 29/34 VOG FL00 ASTIG N E FL90 ASTIG R266^ ^ R7^ (L) 2.25 N E VOGHERA (H) VOG N E VOG N E FL90 ML6~2 N E irect distance to Linate Apt from: 6 NM TRANSITION TOP R STAR ASTIG GEN Tabular description. GENOA (H) 2.8 GEN N E GEN 38 GEN N E On TOP R-086/086^ bearing to ASTIG. On VOG R-266 inbound/086^ bearing to VOG, turn LEFT, intercept R-82 inbound/002^ bearing to. On GEN R-35/VOG R-7 inbound via ML602 to VOG, intercept R-82 inbound/002^ bearing to. GEN 7 FL00 35^, 204, 205. ALL RIGHTS RESERVE.

20 Printed from JeppView for Windows on ec 207; Terminal chart data cycle ; Notice: After 4 ec 207, 0000Z, this chart may no longer be valid ATIS KALIK R [KAKR] KALMO R [KAOR] RWY 36 RNAV TRANSITION P-RNAV GEN R, IONA R [IOR] RWY 36 TRANSITIONS CONVENTIONAL/P-RNAV AMOXI 4H [AMOX4H] RWY 36 ARRIVAL CONVENTIONAL/P-RNAV 22 MAY G.Eff.28.May. Alt Set: hpa TREZZO (H) TZO.8 N E (L) 2.25 N E ^ 0,00' MSA VOR.STAR. 4200' within 5 NM HOGS OVER AMOXI IXER LIMBA R75^ 52 R75^ 23 R75^ 32 R75^ IXER N E /56 FL00 23/ FL90 32/37 LIMBA N E FL90 NOGMO N E GENOA (H) 2.8 GEN N E GEN 38 GEN N E ^ IONA N E AMOXI 4H 52 FL00 FL00 GEN R IONA R 37 FL00 AMOXI N E KALMO R 9 FL00 329^ 22 FL00 KALIK R TZO 290^ KALMO N E R66^ ^ MAH FL00 MAX 230 KT 67/7 KALIK N E TRANSITION GEN R On GEN R-048/048^ bearing to AMOXI. IONA R On R-75 inbound to AMOXI. KALIK R By ATC KALIK - AMOXI. KALMO R KALMO - AMOXI. STAR AMOXI 4H On R-75 inbound via NOGMO and LIMBA to IXER. AMOXI STAR renumbered; availability KALMO R; tabular description., 204, 205. ALL RIGHTS RESERVE.

21 Printed from JeppView for Windows on ec 207; Terminal chart data cycle ; Notice: After 4 ec 207, 0000Z, this chart may no longer be valid ATIS MAY H.Eff.28.May. Alt Set: hpa TOP R RWY 36 TRANSITION ASTIG J [ASTIJ], GEN J RWY 36 ARRIVALS CONVENTIONAL/P-RNAV 20^ 0,00' MSA VOR.STAR. 4200' within 5 NM (L) 2.25 N E TORINO (H) TOP 4.5 N E TOP N E ^ 8 FL90 TOP R 29/34 VOG FL00 ASTIG N E FL90 ASTIG J 5.5 VOGHERA (H) VOG N E VOG N E R266^ R7^ 6 FL90 ML6~2 N E HOG OVER VOG 72^ ^ TRANSITION TOP R STAR ASTIG J GEN J By ATC Tabular description. irect distance to Linate Apt from: VOG 32 NM GENOA (H) 2.8 GEN N E GEN 38 GEN N E On TOP R-086/VOG R-266 inbound/086^ bearing to ASTIG. On VOG R-266^ inbound/086^ bearing to VOG. On GEN R-35/VOG R-7 inbound via ML602 to VOG. GEN J 7 FL00 35^, 204, 205. ALL RIGHTS RESERVE.

22 Printed from JeppView for Windows on ec 207; Terminal chart data cycle ; Notice: After 4 ec 207, 0000Z, this chart may no longer be valid MILAN Radar OCT SI. SIs are also noise abatement routings. Strict adherence within the limits of aircraft performance is necessary. TOVSA 5C TREVI 6 [TOVS5C] [TREV6] RWY 8 EPARTURES 20^ 0,00' BERGAMO (H) 4.95 BEG BEG N E MSA VOR 4200' within 5 NM (L) 2.25 N E TREVI N E FL95 4 R87^ 386 LNE N E ^ 40^ 0^ 259^ 2.2 ( R-75) Turn at 840' but not before TREVI 6 COOGNO CO N E ^ 007^ 5000' TOVSA 5C 9 TOVSA N E ' These SIs require a minimum climb gradient of 395' per NM (6.5%) between 2.2 and 8. Gnd speed-kt ' per NM SI TOVSA 5C Climb on 75^ track, at 840', but not before 2.2, turn LEFT, 0^ track, intercept R-40 to CO, turn LEFT, 59^ bearing to TOVSA. TREVI 6 Climb on 75^ track, at 840', but not before 2.2, turn LEFT, 0^ track, intercept R-40 to CO, turn LEFT, intercept BEG R-87 inbound to TREVI. Communications., 204, 205. ALL RIGHTS RESERVE.

23 3 Printed from JeppView for Windows on ec 207; Terminal chart data cycle ; Notice: After 4 ec 207, 0000Z, this chart may no longer be valid (via MAL) MILAN Radar OCT A.SI. SIs are also noise abatement routings. Strict adherence within the limits of aircraft performance is necessary. LIMBA 5C [LIMB5C], MAL 8C RWY 8 EPARTURES 20^ 0,00' MALPENSA 364 MAL N E FL80 SARONNO 3.7 (H) N E MSA VOR 4200' within 5 NM 5 82^ 75^ (L) 2.25 N E ' 36^ 24^ 2500' MAL 8C 75^ 244^ LIMBA 5C 75^ LNE N E ' ' VOG VOG 055^ These SIs require minimum climb gradients of MAL 8C 322' per NM (5.3%) until leaving 2500'. LIMBA 5C 425' per NM (7%) until leaving. Gnd speed-kt ' per NM ' per NM ^ 2 32 LIMBA N E FL00 SI LIMBA 5C Intercept R-75 to LIMBA. 2 To LNE Lctr, 75^ bearing to LIMBA. MAL 8C Intercept R-75 to 4, turn RIGHT, 244^ track, when passing R-24 turn RIGHT, intercept 36^ bearing to MAL. 2 ALTERNATE INITIAL CLIMB (when unserviceable). Communications., 204, 205. ALL RIGHTS RESERVE.

24 Printed from JeppView for Windows on ec 207; Terminal chart data cycle ; Notice: After 4 ec 207, 0000Z, this chart may no longer be valid 20-3B 20^ MILAN Radar ,00' MSA VOR 4200' within 5 NM SIs are also noise abatement routings. Strict adherence within the limits of aircraft performance is necessary. NIKMO 9 MAY 7.Eff.25.May. NIKMO 6A [NIKM6A] RUVAB 5A [RUVA5A], RUVAB 5B [RUVA5B] RWY 36 EPARTURES RUVAB FL05.SI FL FL FL85 NIKMO 6A RUVAB 5B ^ RUVAB 5B 053^ 9 P-RNAV RORU 6000' ' ' 850' At but not before NIKMO 6A 020^ In order to avoid sensitive areas close to the airport, undue delay in joining R-340 (NIKMO 6A, RUVAB 5B)/ R-005 (RUVAB 5A) must be avoided. 352^ 340^ ^ 0 P-RNAV RUVAB 5A 2.25 N E ML468 ( R-005) 2.5 ( R-005) 2000' These SIs require minimum climb gradients of 547' per NM (9%). If unable to comply advise ATC at start-up and request to be cleared on a SI towards TZO. SI NIKMO 6A JET ONLY RUVAB 5A CONVENTIONAL (RNAV OVERLAY) RUVAB 5B By ATC JET ONLY NIKMO 6A, RUVAB 5B RUVAB 5A 608' per NM (0%) between and 4.0 / ML468. RNAV: RUVAB 5B established. Gnd speed-kt ' per NM ' per NM Climb on track, at 850', but not before, turn LEFT, intercept R-340 to 5.5, turn RIGHT, 020^ track, intercept R-352 to NIKMO. Climb on track, at 850', but not before, turn RIGHT, intercept R-005 to 4.0 /ML468, turn RIGHT RORU - RUVAB. (850'+) - ML468 (+) - RORU (6000'+) - RUVAB (FL05+). Climb on track, at 850', but not before, turn LEFT, intercept R-340 to 5.5, turn RIGHT, 020^ track, intercept R-352 to 4.0, turn RIGHT, intercept R-072 to RUVAB., 204, 207. ALL RIGHTS RESERVE.

25 Printed from JeppView for Windows on ec 207; Terminal chart data cycle ; Notice: After 4 ec 207, 0000Z, this chart may no longer be valid 20-3C 20^ MILAN Radar ,00' 9 MAY 7.Eff.25.May. SIs are also noise abatement routings. Strict adherence within the limits of aircraft performance is necessary. TZO 7C RWY 36 EPARTURE BY ATC COMPULSARY FOR TURBO PROP OR NON RNAV ONLY.SI. MSA VOR 4200' within 5 NM 4.0 ML468 ( R-005) 2800' 850' At but not before.5 MAX 220 KT 089^ 2.5 ( R-005) 2000' 2.25 N E R269^ TREZZO.8 TZO N E ^ 2 TZO 345 N E FL85 2 MHA ^ Climb in holding if at level lower than FL85. In order to avoid sensitive areas close to the airport, undue delay in joining R-005 must be avoided. This SI requires a minimum climb gradient of 486' per NM (8%) between and 4.0. TZO 7C transferred. Gnd speed-kt ' per NM Climb on track, at 850', but not before, turn RIGHT, intercept R-005 to 4.0, turn RIGHT, intercept TZO R-269 inbound to TZO., 207. ALL RIGHTS RESERVE.

26 Printed from JeppView for Windows on ec 207; Terminal chart data cycle ; Notice: After 4 ec 207, 0000Z, this chart may no longer be valid 20-3C MILAN Radar MAY 7.Eff.25.May. SIs are also noise abatement routings. Strict adherence within the limits of aircraft performance is necessary. ABSEM 5A TOVSA 5A [TOVS5A] RWY 36 EPARTURES 20^ 0,00' MSA VOR.SI. 4200' within 5 NM 80 KT 25^ bank MAX ' 850' At but not before ^ 050^ 005^ 30^ 500' ABSEM 5A 097^ 3.7 3^ 9 ABSEM 4000' ' 2.25 N E ^ TOVSA 5A ATGAM ' COOGNO CO N E ' These SIs require a minimum climb gradient of 456' per NM (7.5%) ABSEM 5A: between VOR and 2.5. between and 8.0. TOVSA 5A: Gnd speed-kt ABSEM 5A: In order to avoid sensitive areas close to the airport, undue delay in joining R-005 must be avoided ' per NM ^ 9 TOVSA 6000' TOVSA 5A: SI ABSEM 5A CONVENTIONAL (RNAV OVERLAY) TOVSA 5A Execute initial turn with a bank angle not higher than 20^. New chart (SIs transferred). Climb on track, at 850', but not before, turn RIGHT, intercept R-005 to 2.5, turn RIGHT, intercept R-20 to ABSEM. Climb on track, at 850', but not before, turn RIGHT, 30^ track to 8.0, turn RIGHT, intercept R-3 to ATGAM, turn RIGHT, intercept 48^ bearing to CO, turn RIGHT, 59^ bearing to TOVSA., 207. ALL RIGHTS RESERVE.

27 Printed from JeppView for Windows on ec 207; Terminal chart data cycle ; Notice: After 4 ec 207, 0000Z, this chart may no longer be valid 9 JUN MILAN Radar 26.3.RNAV.SI.(OVERLAY). SIs are also noise abatement routings. Strict adherence within the limits of aircraft performance is necessary. ABSEM 5A [ABSE5A] RWY 36 RNAV EPARTURE (OVERLAY 20-3C) 20^ 0,00' MSA VOR 4200' within 5 NM SARONNO 3.7 (H) N E ML N E MAX 80 KT ML N E ' 20^.9 005^ ML464 N E MAX 80 KT ML46.9 N E ABSEM N E ' (L) 2.25 N E ' This SI requires a minimum climb gradient of 456' per NM (7.5%) between VOR and ML462. Gnd speed-kt ' per NM (850'+) - ML46 - ML462 (2000'+) - ML463 (K80-) - ML464 (K80-) - ABSEM (4000'+). Reissue. In order to avoid sensitive areas close to the airport, undue delay in joining R-005 must be avoided., 204, 205. ALL RIGHTS RESERVE.

28 Printed from JeppView for Windows on ec 207; Terminal chart data cycle ; Notice: After 4 ec 207, 0000Z, this chart may no longer be valid 9 JUN E MILAN Radar SIs are also noise abatement routings. Strict adherence within the limits of aircraft performance is necessary. 8A 6 BY ATC, ALTERNATE FOR SI 8A RWY 36 EPARTURES 20^ 0,00' MSA VOR.SI. 4200' within 5 NM SARONNO (H) 3.7 N E N E FL85 6: In order to avoid sensitive areas close to the airport, undue delay in joining R-005 must be avoided. R099^ 279^ 8 N E ' ' ' 8A (L) 2.25 N E ^ ^ 6 8 N E ' ' ' 850' At but not before These SIs require minimum climb gradients of 8A 550' per NM (9%) between and ' per NM (8%) between and 4, then 334' per NM (5.5%). Gnd speed-kt ' per NM ' per NM ' per NM SI 8A 6 Reissue. Climb on track, at 850', but not before, turn LEFT, intercept R-340 to 8, turn LEFT, intercept R-099 inbound to. Climb on track, at 850', but not before, turn RIGHT, intercept R-005 to 8, turn LEFT, intercept R-099 inbound to., 204, 205. ALL RIGHTS RESERVE.

29 Printed from JeppView for Windows on ec 207; Terminal chart data cycle ; Notice: After 4 ec 207, 0000Z, this chart may no longer be valid MILAN Radar 26.3 SARONNO 3.7 (H) N E MAY F.Eff.28.May..SI. SIs are also noise abatement routings. Strict adherence within the limits of aircraft performance is necessary. TOVSA 5Z TREVI 5Z [TOVS5Z] [TREV5Z] RWY 8 EPARTURES TO BE PLANNE WHEN UNSERVICEABLE BERGAMO (H) 4.95 BEG BEG N E TREVI N E FL95 4 R87^ 20^ 6700' 5500' MSA LNE Lctr 2600' within 5 NM ILS ME (09.55) ILNT ILNT N E LNE N E ^ 38^ 0^ ILNT Turn at 840' but not before ILNT 0 23 TREVI 5Z None. COOGNO CO N E ' These SIs require minimum climb gradients of 395' per NM (6.5%) between ILNT and 23. Gnd speed-kt ' per NM ^ TOVSA 5Z 9 007^ TOVSA N E ' SI TOVSA 5Z Climb on 75^ bearing towards LNE, at 840', but not before ILNT, turn LEFT, 0^ track, intercept R-38 to CO, turn LEFT, 59^ bearing to TOVSA. TREVI 5Z Climb on 75^ bearing towards LNE, at 840', but not before ILNT, turn LEFT, 0^ track, intercept R-38 to CO, turn LEFT, intercept BEG R-87 inbound to TREVI., 204. ALL RIGHTS RESERVE.

30 Printed from JeppView for Windows on ec 207; Terminal chart data cycle ; Notice: After 4 ec 207, 0000Z, this chart may no longer be valid (via MAL) MILAN Radar MALPENSA 364 MAL N E FL G.SI. 22 MAY 5.Eff.28.May. SIs are also noise abatement routings. Strict adherence within the limits of aircraft performance is necessary. LIMBA 5Z [LIMB5Z], MAL 6Z RWY 8 EPARTURES TO BE PLANNE WHEN UNSERVICEABLE SARONNO 3.7 (H) N E ^ 6700' 5500' MSA LNE Lctr 2600' within 5 NM ILS ME (09.55) ILNT ILNT N E ^ 75^ 386 LNE N E ' 36^ 244^ MAL 6Z 75^ MAL 6Z 2000' LIMBA 5Z LIMBA 5Z ' 8 ILNT 6000' VOG VOG These SIs require minimum climb gradients of LIMBA 5Z 425' per NM (7%) until leaving. MAL 6Z 322' per NM (5.3%) until leaving 2500'. Gnd speed-kt ' per NM ' per NM SI LIMBA 5Z MAL 6Z irect distance from Linate Apt to: LNE 6 NM SI MAL 7 withdrawn ^ 098^ 3 LIMBA 30.7 ILNT N E FL00 To LNE, 75^ bearing to LIMBA. Intercept 75^ bearing to LNE, turn RIGHT, 244^ track, intercept 36^ bearing to MAL., 204, 205. ALL RIGHTS RESERVE.

31 Printed from JeppView for Windows on ec 207; Terminal chart data cycle ; Notice: After 4 ec 207, 0000Z, this chart may no longer be valid 20-3H MILAN Radar MAY 5.Eff.28.May. SIs are also noise abatement routings. Strict adherence within the limits of aircraft performance is necessary..si. NIKMO 5Z [NIKM5Z] RWY 36 EPARTURE JET ONLY CONVENTIONAL/P-RNAV TO BE PLANNE WHEN UNSERVICEABLE NIKMO N E ML5~4 20 ILNT N E FL ML5~6 25 ILNT N E009.9 FL35 ML5~3 5 ILNT N45 4. E FL85 20^ 6700' 5500' MSA LNE Lctr 2600' within 5 NM 352^ 72^ ML5~2 9.5 ILNT N E ' 5.5 ML5~ 4 ILNT N E ' ILS ME (09.55) ILNT ILNT N E ^ 386 LNE N E This SI requires a minimum climb gradient of 547' per NM (9%). If unable to comply advise ATC at start-up and request to be cleared on a TZO SI. On bearing from LNE to 9.5 ILNT, intercept 352^ bearing from LNE to NIKMO. RNAV: (800'+) - ML50 (800'+) - ML502 (5000'+) - ML503 (FL85+) - ML504 (FL05+) - ML506 (FL35+) - NIKMO. Availability. Gnd speed-kt ' per NM , 2007, 205. ALL RIGHTS RESERVE.

32 Printed from JeppView for Windows on ec 207; Terminal chart data cycle ; Notice: After 4 ec 207, 0000Z, this chart may no longer be valid 20-3J MILAN Radar MAY 5.Eff.28.May. SIs are also noise abatement routings. Strict adherence within the limits of aircraft performance is necessary. TZO 6Z RWY 36 EPARTURE TO BE PLANNE WHEN UNSERVICEABLE 20^ 6700' 5500' MSA LNE Lctr.SI. 2600' within 5 NM 5.5 ILNT N E ' MAX 220 KT 089^ 2 Climb in holding if at level lower than FL85. R269^ 45^ TREZZO (H).8 TZO N E TZO 345 N E FL ILNT.5 MHA ^ 800' ILS ME (09.55) ILNT ILNT N E ^ 386 LNE N E This SI requires a minimum climb gradient of 486' per NM (8%) until 5.5 ILNT. Gnd speed-kt ' per NM On bearing from LNE to 5.5 ILNT, turn RIGHT, intercept TZO R-269 inbound to TZO. MHA at TZO., 204, 205. ALL RIGHTS RESERVE.

33 Printed from JeppView for Windows on ec 207; Terminal chart data cycle ; Notice: After 4 ec 207, 0000Z, this chart may no longer be valid 20-3K MILAN Radar NOV 4.Eff.3.Nov. SIs are also noise abatement routings. Strict adherence within the limits of aircraft performance is necessary. ABSEM 5B TOVSA 5B [ABSE5B] [TOVS5B] RWY 36 EPARTURES TO BE PLANNE WHEN UNSERVICEABLE 20^ 6700' 5500' MSA LNE Lctr.SI. 2600' within 5 NM 4 ILNT 800' ^ 500' TREZZO TZO (H).8 TZO N E ILNT TOVSA 5B 850' At but not before.5 ILNT ILS ME (09.55)ILNT N E LNE N E ^ 30^ ^ ABSEM 5B 3^ 8 ME 2 48^ 9 At or above 2500' TOVSA 5B ATGAM N E ' ABSEM N E ' COOGNO CO N E ' These SIs require minimum climb gradients of ABSEM 5B 486' per NM (8%) until 4 ILNT. TOVSA 5B 456' per NM (7.5%) between.5 ILNT and 8 ME. Gnd speed-kt ' per NM ' per NM SI ABSEM 5B TOVSA 5B TOVSA 5B: In order to avoid sensitive areas close to the airport, first turn after take-off shall be performed with a bank angle not higher than 20^. SIs completely revised. TOVSA N E On bearing from LNE to 4 ILNT, turn RIGHT, intercept R-20 to ABSEM. Climb on bearing from LNE, at 850', but not before.5 ILNT turn RIGHT, 30^ track to 8 ME, turn RIGHT, intercept R-3 to ATGAM, turn RIGHT, intercept 48^ bearing to CO, turn RIGHT, 59^ bearing to TOVSA. 59^ ', 204. ALL RIGHTS RESERVE.

34 4 Printed from JeppView for Windows on ec 207; Terminal chart data cycle ; Notice: After 4 ec 207, 0000Z, this chart may no longer be valid 20-3L MILAN Radar NOV 4.Eff.3.Nov. SIs are also noise abatement routings. Strict adherence within the limits of aircraft performance is necessary. 5Z RWY 36 EPARTURE TO BE PLANNE WHEN UNSERVICEABLE SARONNO (H) 3.7 N E N E FL85 20^ 6700' 5500' MSA LNE Lctr.SI. 2600' within 5 NM R099^ 279^ 5.5 ILNT 2500' ILNT N E ' 4 ILNT 800' ILS ME (09.55)ILNT N E ^ 386 LNE N E This SI requires minimum climb gradients of 486' per NM (8%) until 5.5 ILNT, then 334' per NM (5.5%). Gnd speed-kt ' per NM ' per NM On bearing from LNE to 9.5 ILNT, turn LEFT, intercept R-099 inbound to. MSA., 204. ALL RIGHTS RESERVE.