JeppView for Windows. jep=jeppesen. Airport Information For EDDH Printed on 06 Dec 2017 Page 1. General Information. Runway Information

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1 Airport Information For EH Printed on 06 ec 2017 Page 1 (c) SANERSON, INC., 2017, ALL RIGHTS RESERVE jep= JeppView for Windows General Information Hamburg irect (Approach Control Radar): Bremen Radar Radar: Bremen Radar Radar: Location: EU ICAO/IATA: EH / HAM Lat/Long: N ', E ' Elevation: 53 ft Airport Use: Public aylight Savings: Observed UTC Conversion: -1:00 = UTC Magnetic Variation: 2.0 E Fuel Types: 100 Octane (LL), Jet A-1 Repair Types: Major Airframe, Major Engine Customs: Yes Airport Type: IFR Landing Fee: Yes Control Tower: Yes Jet Start Unit: No LLWS Alert: No Beacon: Yes Sunrise: 0720 Z Sunset: 1502 Z Runway Information Runway: 05 Length x Width: ft x 151 ft Surface Type: concrete TZ-Elev: 32 ft Lighting: Edge, ALS, Centerline, REIL isplaced Threshold: 978 ft Runway: 15 Length x Width: ft x 151 ft Surface Type: asphalt TZ-Elev: 53 ft Lighting: Edge, ALS, Centerline, REIL Runway: Length x Width: ft x 151 ft Surface Type: concrete TZ-Elev: 43 ft Lighting: Edge, ALS, Centerline, REIL, TZ isplaced Threshold: 512 ft Runway: 33 Length x Width: ft x 151 ft Surface Type: asphalt TZ-Elev: 35 ft Lighting: Edge, ALS, Centerline, REIL isplaced Threshold: 1463 ft Communication Information ATIS: At or below ft Out to 60 mi. Hamburg Tower: Hamburg Tower: Hamburg Ground: Hamburg Apron Ramp/Taxi: Hamburg Apron Ramp/Taxi:

2 Airport Information For EH Printed on 06 ec 2017 Page 2 (c) SANERSON, INC., 2017, ALL RIGHTS RESERVE jep= JeppView for Windows General Information Hamburg irect (Approach Control Radar): Bremen Radar Radar: Bremen Radar Radar: Location: EU ICAO/IATA: EH / HAM Lat/Long: N ', E ' Elevation: 53 ft Airport Use: Public aylight Savings: Observed UTC Conversion: -1:00 = UTC Magnetic Variation: 2.0 E Fuel Types: 100 Octane (LL), Jet A-1 Repair Types: Major Airframe, Major Engine Customs: Yes Airport Type: IFR Landing Fee: Yes Control Tower: Yes Jet Start Unit: No LLWS Alert: No Beacon: Yes Sunrise: 0720 Z Sunset: 1502 Z Runway Information Runway: 05 Length x Width: ft x 151 ft Surface Type: concrete TZ-Elev: 32 ft Lighting: Edge, ALS, Centerline, REIL isplaced Threshold: 978 ft Runway: 15 Length x Width: ft x 151 ft Surface Type: asphalt TZ-Elev: 53 ft Lighting: Edge, ALS, Centerline, REIL Runway: Length x Width: ft x 151 ft Surface Type: concrete TZ-Elev: 43 ft Lighting: Edge, ALS, Centerline, REIL, TZ isplaced Threshold: 512 ft Runway: 33 Length x Width: ft x 151 ft Surface Type: asphalt TZ-Elev: 35 ft Lighting: Edge, ALS, Centerline, REIL isplaced Threshold: 1463 ft Communication Information ATIS: At or below ft Out to 60 mi. Hamburg Tower: Hamburg Tower: Hamburg Ground: Hamburg Apron Ramp/Taxi: Hamburg Apron Ramp/Taxi:

3 , 2007, ALL RIGHTS RESERVE. Printed from JeppView for Windows on 06 ec 2017; Terminal chart data cycle ; Notice: After 14 ec 2017, 0000Z, this chart may no longer be valid EH/HAM +, GERMANY.AIRPORT.BRIEFING. 1. GENERAL 1.1. ATIS *-ATIS NOISE ABATEMENT PROCEURES Unless otherwise instructed by ATC, pilots should aim for a low noise continuous descent approach below FL 70 without level flight segment RWY USAGE RWY 33 shall be used for take-offs. Exceptions are permitted only if required by the traffic situation or for reasons of air traffic safety, especially due to weather and RWY conditions. Take-offs from RWY 15 and landings on RWY 33 are permitted only if required for reasons of air traffic safety, especially due to weather and RWY conditions LT 15 SEP P RWY 15 shall be used for landings. Exceptions are permitted only if the weather minima established for the IFR approach procedure to RWY 15 are not met and for reasons of air traffic safety as well as in exceptional traffic situations. Additional exceptions may be granted by the Aerodrome Control Tower in agreement with the competent local aeronautical authority NIGHT FLYING RESTRICTIONS JET-ACFT WITHOUT NOISE CERTIFICATION ACCORING TO ICAO ANNEX 16 - Take-offs and landings are not permitted between LT JET-ACFT WITHOUT NOISE CERTIFICATION ACCORING TO ICAO ANNEX 16, VOLUMEI, PART II, CHAPTER 2 - Take-offs are not permitted between LT. - Landings are not permitted between -0700LT. - elayed take-offs of scheduled air services and regular inclusive tour flights with scheduled times of departure before 2000LT are exempt from the night flight restrictions until LT if the delay was provably unavoidable JET-ACFT WITH NOISE CERTIFICATION ACCORING TO ICAO ANNEX 16, VOLUME I, PART II, CHAPTER 3, PROPELLER-RIVEN ACFT AN OTHER ACFT NOT COVERE IN PARAS AN Take-offs and landings are not permitted between LT. - elayed take-offs and landings of scheduled air services and regular inclusive tour flights with scheduled times of departure or arrival before 00LT are exempt from the night flight restrictions until 2400LT if the delay was provably unavoidable EXCEPTIONS Exempt from the restrictions mentioned in paras to are: - ACFT using Hamburg APT as alternate or emergency aerodrome for meteorological, technical or other safety reasons. - ACFT on disaster relief and medical assistance flights, SAR services or urgent police missions. - ACFT operated in the night airmail service of the eutsche Post AG, as specified in detail by the Hamburg Ministry of Economics. Additional exceptions from the regulations may be granted in individual cases, especially if required to avoid significant disturbances to air traffic or in cases of special public interest.

4 , 2007, ALL RIGHTS RESERVE. Printed from JeppView for Windows on 06 ec 2017; Terminal chart data cycle ; Notice: After 14 ec 2017, 0000Z, this chart may no longer be valid EH/HAM 15 SEP P1 1. GENERAL Requests shall be submitted - if possible, no later than 20LT - to: Behoerde fuer Umwelt und Energie Fluglaermschutz Neuenfelder Strasse Hamburg Tel.: , GERMANY.AIRPORT.BRIEFING. The ATC clearance does not include the exceptional permission from the noise abatement officer (Fluglaermschutzbeauftragter) required as stated above REVERSE THRUST Reverse thrust other than idle thrust shall only be used to an extent necessary for safety reasons RUN-UP TESTS Engine test runs outside the noise abatement hangar are permitted only after prior consent and in accordance with specific instructions by the aviation supervision office (Luftaufsicht) of the Hamburg Ministry of Economics, or Idle thrust test runs between LT are not covered by this regulation. The permission for a run-up-test from the Luftaufsichtsstelle does not include the necessary ATC taxi clearance. Engine test runs of rotorcraft: Engine test runs shall be reported to the traffic observer (Tel.: ) at the GAT. Engine test runs shall be conducted on Apron 4 between the western edge and the ACFT Stand Taxilane - V on an area provided for this purpose and marked by a white cross. Hover flights to this position are not allowed. The APT operator reserves the right to allocate another position if necessary. Compass calibration runs may be conducted on request on RWY 33 abeam TWY R and on the helipad West. If specially requested, compass calibration runs may be interrupted and ACFT requested to vacate its position if called upon to do so by the APT operator, the local air navigation services and/or the aviation supervision authority (Luftaufsicht) AUXILIARY POWER UNITS (APUs) ACFT shall shut down the APU directly after arriving at the ACFT stand, provided external power is available. At the pier positions, the central infrastructure for air conditioning and electricity shall be used. At remote stands, ACFT operators must request mobile devices from ground handling service providers. The APU shall remain turned off for the whole time at the ACFT stand. The APU may only be turned on 8 minutes (pier position) or 5 minutes (remote stand) before the last possible time to leave the ACFT stand. Exceptions from the prohibition on the use of the APU are issued by the central apron management service ( Apron on frequency or ) LOW VISIBILITY PROCEURES ACFT GUIANCE UNER CAT II/III OPERATIONS ACFT having landed are requested to report leaving the colour-coded section of the TWY in order to draw attention to the fact that the ACFT has left the ILS protection area. At CAT II/III intermediate holding positions and on additional TWY sections equipped with stop bars, the latter may, under no circumstances, be crossed when switched on. In apron areas with taxi guideline lighting (Apron 2, Y1 and Y3 only), ACFT will be guided by means of green centerline lights when CAT II/III operations are activated. In the apron areas without centerline lighting (Aprons 1 and 4, as well as parts of Apron 2), Follow-me cars will be assigned by Apron if required, or at the request of the pilot.

5 , 2007, ALL RIGHTS RESERVE. Printed from JeppView for Windows on 06 ec 2017; Terminal chart data cycle ; Notice: After 14 ec 2017, 0000Z, this chart may no longer be valid EH/HAM +, GERMANY.AIRPORT.BRIEFING. The intermediate holding position lights on apron 2 are operated in conjunction with the lighting for the taxi guidelines. The intermediate holding position lights consist of 5 yellow unidirectional underfloor lights. ACFT may cross these without special permission - unless they are expressly requested to hold SURFACE MOVEMENT GUIANCE AN CONTROL SYSTEM GENERAL Hamburg APT has installed an Advanced Surface Movement Guidance and Control System (A-SMGCS) using Mode S multilateration OPERATION OF MOE S TRANSPONERS WHEN ACFT IS ON GROUN ACFT operators shall ensure that Mode S transponders are able to operate when the ACFT is on ground. Pilots shall: 10 NOV P2 1. GENERAL Select AUTO mode and assigned Mode A code. If AUTO mode is not available, select ON (e.g. XPR) and assigned Mode A code shall be selected under the following conditions: - From the request for push-back or taxi, whichever is earlier; - After landing, continuously until ACFT is fully parked on stand; - When fully parked on stand, STBY shall be selected. Whenever ACFT is capable of reporting ACFT Ident (i.e. call sign used in flight), the ACFT ident should also be entered from request for push back or taxi, whichever is earlier (through the FMS or Transponder Control Panel). ACFT crew shall use the format for entry of the ACFT ident as defined in Item 7 of the ICAO flight plan. To ensure that performance of systems based on SSR frequencies (including airborne TCAS units and SSR radars) is not compromised, TCAS should not be activated before approaching the holding point. After landing, it shall be deselected after vacating the RWY TAXI PROCEURES GENERAL On aprons 1 and 2, ACFT may only taxi on or along the yellow guidelines and are permitted only at minimum thrust. B747 and larger ACFT will be guided by a Follow-me car. ACFT crossing RWY 33 via TWY B3 in direction TWY G, may only taxi along the yellow guidelines. Within the General Aviation area, the wingtip clearance on TWY Y4 is 10'/3m, on TWYs Y5 thru Y7 is 15'/4.5m. On apron 2, Follow-me car mandatory for ACFT with wingspan between 66'/20m and 98'/30m. Pilots taxiing between aprons 2 and 4 shall request clearance for crossing TWY G from Ground. Additional preceding holding positions are located on TWYs B3, B4, B5, G, B1, B6 and 1. If instructed by Apron/ Ground/ Tower, pilots shall stop at these points.

6 , 2007, ALL RIGHTS RESERVE. Printed from JeppView for Windows on 06 ec 2017; Terminal chart data cycle ; Notice: After 14 ec 2017, 0000Z, this chart may no longer be valid EH/HAM TWY T RESTRICTIONS 10 NOV 17 +, GERMANY.AIRPORT.BRIEFING. ACFT with a wingspan less than 213 /65 m may taxi through the gateway under their own power. ACFT permitted to taxi onto apron 6 under their own power will be requested to stop by a ground marking after passing through the gateway. The engines shall be turned off and the ACFT will subsequently be towed to its destination. ACFT wanting to leave apron 6 in the direction of TWY T will be towed up to the gateway. The engines may be turned on here and not earlier. After requesting and receiving a start-up/taxi clearance from Ground, ACFT may continue to taxi under their own power in accordance with instructions. ACFT with a wingspan of 213 /65m or more must wait in front of the gateway with the engines turned off. They will then be towed through the open gateway in the presence of a wing-walker TWY LIMITATIONS Apron 1 South of TWY B1 MAX wingspan 118'/36m. ACFT with a wingspan of more than 171'/52m may only use TWY B1 to vacate RWY 15/33 when guided by Follow-me vehicles. ACFT with MAX wingspan of 213'/65m may use TWY B1 to taxi onto RWY 15/33 without guidance. TWY B3 may only be used for crossing RWY 15/33. It cannot be used to enter RWY 15/33 for take-offs or to exit it after landings. TWY B5 is available only to ACFT with wingspan of up to but not including 118 /36m (ICAO code letter C). TWY U will be marked off by a gateway between TWY G and apron 5. The gateway has a width of 197 /60m and a height of 8 /2.43m AGL. ACFT with a wingspan of less than 118 /36m may taxi through the gateway under their own power. ACFT with a wingspan of 118 /36m or more shall stop in front of the gateway and turn off engines. They will then be towed to their destination. Eastern part of apron 2 including TWY Y4 MAX wingspan less than 98 /30m. TWYs Y5 and Y6 MAX wingspan 39'/12m. TWY Y7 MAX wingspan 95'/29m. 10-1P3 1. GENERAL TWY W MAX wingspan less than 79'/24m. TWY V MAX wingspan 94'/28.65m, a MAX length of 99'/30.3m and a landing gear width of MAX 16'/4.9m. Apron 4 MAX wingspan less than 94'/28.65m PARKING INFORMATION Stands 01A, 01, 01B, 02A, 02B, 03A, 03B thru 11 equipped with Visual ocking Guidance System. On stands 01A thru 43 and 81 thru 95A push-back required. On stands 01A thru 48, onboard APU must be switched off as long as power supply and fresh air are provided in return for extra fees TAXI-OUT/PUSH-BACK STANS 44 THRU 48 ACFT with a wingspan of more than 82'/25m must be pushed back from their positions. ACFT with a wingspan of less than 82'/25m may leave their positions under their own power OTHER INFORMATION Caution: Birds in vicinity of APT. For APT Collaborative ecision Making see ATC pages Germany.

7 , 2007, ALL RIGHTS RESERVE. Printed from JeppView for Windows on 06 ec 2017; Terminal chart data cycle ; Notice: After 14 ec 2017, 0000Z, this chart may no longer be valid EH/HAM 26 MAY P4, GERMANY.AIRPORT.BRIEFING. 2. ARRIVAL 2.1. CAT II/III OPERATIONS RWY approved for CAT II/III operations, special aircrew and ACFT certification required. In case of a long landing on RWY with subsequent vacating of RWY via TWY 1, ACFT will be guided from end of RWY to TWY 3, as an alternative by a follow-me car to the centerline lights TAXI PROCEURES Arriving ACFT will be passed by Tower to Apron and will taxi as instructed by Apron to the position assigned. Change-over will take place as early as possible, at the latest when reaching the boundary of responsibility. Parking of ACFT at all positions without Visual ocking Guidance System performed by marshaller OTHER INFORMATION FUEL SAVING AN NOISE REUCING ILS APPROACH PROCEURES (CONTINUOUS ESCENT APPROACH - CA) GENERAL For the purpose of fuel-saving and noise abatement during approach the following approach procedure is announced. It may be requested by the pilot or offered by the controller. It can be performed only in connection with an ILS approach PROCEURE - ACFT will be guided by the approach control unit by means of radar vectoring and will be cleared for a continuous descent to the intermediate approach altitude in such a way that after reaching this intermediate approach altitude on the localizer course, about 1NM will be left for intercepting the glide path in level flight. This intermediate approach segment will serve to reduce speed. Intermediate approach altitude: '. It is assumed that the continuous descent will be performed at a rate of 300ft/NM (descent angle approx. 3^), down to the cleared altitude. If, for specific reasons (e.g. separation, airspace structure, obstacles), altitudes above the intermediate approach altitude have to be initially assigned, these restrictions will be lifted early enough to allow a continuous descent at a rate of 300ft/NM. etails about the distance from touchdown will be transmitted to the pilot together with the clearance for descent and usually at 20, 15 and 10NM from touchdown. This should enable the pilot to correct the rate of descent as required. - In case of traffic situations allowing no CA (e.g. approaches of ACFT with different performance data), pilots will be informed by the notice NO CA POSSIBLE. In this case, approaches must be conducted according to the previous procedures NOISE ABATEMENT On approaches in accordance with the CA, pilots are also expected to use the approach techniques recommended for noise abatement in the vicinity of APTs (see AIR TRAFFIC CONTROL page GERMANY-1).

8 , 2007, ALL RIGHTS RESERVE. Printed from JeppView for Windows on 06 ec 2017; Terminal chart data cycle ; Notice: After 14 ec 2017, 0000Z, this chart may no longer be valid EH/HAM 26 MAY P5, GERMANY.AIRPORT.BRIEFING. 3. EPARTURE 3.1. START-UP, PUSH-BACK & TAXI PROCEURES START-UP GENERAL Pilots shall request start-up clearance from Ground. On initial radio contact the respective apron designation shall always be indicated. After clearance to start the engines, pilots will receive instruction to establish contact on the frequency of Apron GENERAL AVIATION APRONS On initial radio contact the taxilane shall be indicated additionally PUSH-BACK & TAXI "Nose-in positions" may only be left with push-back facility. Reverse thrust shall not be used. To obtain push-back instructions from a nose-in position, pilots must request permission from Apron. In order to avoid delays in taxiing, pilots are instructed to start engines during push-back. After completion of push-back, "ready to taxi" shall be reported to Apron. To obtain instructions for taxiing from a taxi-out position, pilots must request taxi clearance from Apron reporting "ready to taxi". On initial radio contact with Apron, pilots shall report position and RWY assigned. Permission for push-back or taxiing from a position may only be requested if the pilot can perform the manoeuvre immediately NOISE ABATEMENT PROCEURES The use of the noise abatement take-off and climb procedure NAP1 is recommended for all jet ACFT departures from Hamburg APT. Climb with MAX climb gradient to ': - Use the high lift devices TKOF configuration. - TKOF PWR reduction to climb PWR at 1500'. Automatic measuring equipment is used to MNT adherence.

9 Printed from JeppView for Windows on 06 ec 2017; Terminal chart data cycle ; Notice: After 14 ec 2017, 0000Z, this chart may no longer be valid EH/HAM BREMEN Radar (APP) Apt Elev 53' 7 APR R Alt Set: hpa (IN on request) Trans level: By ATC Trans alt: 5000', GERMANY.RAAR.MINIMUM.ALTITUES The MRVA (Minimum Radar Vectoring Altitude) is the lowest altitude which may be used for radar vectors for IFR flights taking into account the minimum safe height (1000' above the highest obstacle within a radius of 8 km) and airspace structure LUEBECK LUB VOR COPENHAGEN EKK FIR 40 (lower limit of the controlled airspace plus a buffer of 500'). Below the MRVA, IFR flights will normally be cleared on published IFR procedures only. Altitudes in brackets apply for the period from AIRAC date NOV until AIRAC date MAR in order to meet required obstacle clearance at cold temperatures LYE LCTR 1800 (2000) GT NB ELBE LBE VOR ME CHANGES: Sectors & altitudes revised. HAM VORTAC Hamburg (Hamburg) HOS NB (00) GERMANY NETHER- LANS 3500 FU NB POLAN 80 AMSTERAM EHAA FIR WARSAW EPWW FIR 80 GERMANY E(P)- NORHORN A E(P)- NORHORN B BREMEN EWW FIR LANGEN EGG FIR MUNICH EMM FIR 4118' 2000 BREMEN EWW FIR CONTOUR INTERVALS , 2009, ALL RIGHTS RESERVE.

10 Printed from JeppView for Windows on 06 ec 2017; Terminal chart data cycle ; Notice: After 14 ec 2017, 0000Z, this chart may no longer be valid EH/HAM 26 MAY Alt Set: hpa (IN on request) Trans level: By ATC Apt Elev 53 *-ATIS LUEBECK LUB ^ MHA 20 BOGMU 2A [BOGM2A] NOLGO 3A [NOLG3A] RARUP 3A [RARU3A] RIBSO 4A [RIBS4A] 2 Clearance Limit BOGMU 1^ ALL RWYS ARRIVALS BOGMU 2A 32 R258 TOPRA 078^.SPEE: MAX 250 KT BELOW FL100 OR AS BY ATC NOT APPLICABLE WITHIN AIRSPACE C RIBSO 4A 13 BRNAV and NON-RNAV equipped aircraft EXPECT RAAR vectors to 1 171^ ^ final approach. GPS/FMS equipped aircraft EXPECT respective TRANSITION on charts 10-2B to 10-2N. 316^ 110^ 2 263^ MHA RARUP 3A 17 R R051 R351 R ^ 2 277^ Finkenwerder EHI LOST LOST COMMS LOST COMMS COMMS LOST COMMS LOST COMMS LOST COMMS LOST COMMS LOST COMMS VERTICAL PLANNING INFORMATION RARUP Clearance Limit ELBE LBV 1 (IAF) LBV 290^ Pilots should plan for possible descent clearance of at or below by BOGMU, NOLGO, RARUP & RIBSO. 21 NOLGO 3A, GERMANY ACTUAL ESCENT CLEARANCE WILL BE AS IRECTE BY ATC. 006^ VO R NOLGO HA M ^ RIBSO R ^ 2 Clearance Limit.STAR. 5 Clearance Limit (208^ brg to 378 WSN) MHA Proceed from RARUP or NOLGO via HAM to LBV, from RIBSO via TOPRA to LBV, from BOGMU direct LBV. MHA MHA 028^ CHANGES: New format., ALL RIGHTS RESERVE.

11 Printed from JeppView for Windows on 06 ec 2017; Terminal chart data cycle ; Notice: After 14 ec 2017, 0000Z, this chart may no longer be valid EH/HAM 18 AUG B 028^ *-ATIS ^ MHA RIBSO H211 H215 Clearance Limit (208^ brg to 378 WSN) 138^ 122^ H H ^ 212^ ^ H214 H21~ H256 ANEXI MIN 170 KT H257 H258 By ATC 21 H~~2 Finkenwerder EHI 1004, GERMANY.RNAV.TRANSITION. Alt Set: hpa (IN on request) Trans level: By ATC Apt Elev 1. GPS- or FMS-equipped aircraft On downwind EXPECT vectors to final. 3. Speed restrictions on Transition are always mandatory unless cancelled by ATC. RIBSO 05 [RIB~5] RWY 05 RNAV TRANSITION USE OF RNAV TRANSITION ONLY WHEN CLEARE BY ATC.SPEE: MAX 250 KT BELOW FL100 OR AS BY ATC H AM V OR RIBSO (-) - H210 (K220) - H211 - H213 (K220) - H215 (K220) - H255 - ANEXI (K170+; +). CHANGES: None., ALL RIGHTS RESERVE.

12 Printed from JeppView for Windows on 06 ec 2017; Terminal chart data cycle ; Notice: After 14 ec 2017, 0000Z, this chart may no longer be valid EH/HAM RIBSO Clearance Limit 028^ *-ATIS (208^ brg to 378 WSN) H435 H ^ MHA RIBSO Apt Elev ^ 18 AUG ^ H432 H H455 H C Alt Set: hpa (IN on request) Trans level: By ATC 1. GPS- or FMS-equipped aircraft. H456 H43~ H457 H458, GERMANY.RNAV.TRANSITION On downwind EXPECT vectors to final. 3. Speed restrictions on Transition are always mandatory unless cancelled by ATC. RIBSO 15 [RIB15] RWY 15 RNAV TRANSITION USE OF RNAV TRANSITION ONLY WHEN CLEARE BY ATC.SPEE: MAX 250 KT BELOW FL100 OR AS BY ATC By ATC EVO MIN 170 KT H~~4 HAM V OR 21 H429 Optional 330^ 0 5 CHANGES: Reissue. Finkenwerder EHI H RIBSO (-) - H434 (K220) - H435 (K220) - H455 - EVO (K170+; +). 988, ALL RIGHTS RESERVE.

13 Printed from JeppView for Windows on 06 ec 2017; Terminal chart data cycle ; Notice: After 14 ec 2017, 0000Z, this chart may no longer be valid EH/HAM *-ATIS Apt Elev MAY Alt Set: hpa (IN on request) Trans level: By ATC 1. GPS- or FMS-equipped aircraft. 2. On downwind EXPECT vectors to final. 3. Speed restrictions on Transition are always mandatory unless cancelled by ATC. RIBSO [RIB] RWY RNAV TRANSITION USE OF RNAV TRANSITION ONLY WHEN CLEARE BY ATC.SPEE: MAX 250 KT BELOW FL100 OR AS BY ATC, GERMANY.RNAV.TRANSITION Clearance Limit RIBSO (208^ brg to 378 WSN) MHA 028^ 208^ 20 H62~ 16.6 RIBSO 076^ NOT TO SCALE 085^ H63~ 17.2 H631 Optional H~~6 HAM H632 V OR H634 H633 By ATC H635 H658 PISAS MIN 170 KT 138^ H ^ H656 H Finkenwerder EHI RIBSO (-) - H620 - H633 (K220) - H635 (K220) - H655 - PISAS (K170+; +). CHANGES: New format., ALL RIGHTS RESERVE.

14 Printed from JeppView for Windows on 06 ec 2017; Terminal chart data cycle ; Notice: After 14 ec 2017, 0000Z, this chart may no longer be valid EH/HAM 028^ 21 *-ATIS Clearance Limit RIBSO (208^ brg to 378 WSN) ^ MHA NOT TO SCALE 150^ H8~4 4.8 H8~5 Apt Elev ^ H8~6 H8~7 Finkenwerder EHI 26 MAY 17 H8~8 H8~9 H81~ H811 H~~ E Alt Set: hpa (IN on request) Trans level: By ATC 1. GPS- or FMS-equipped aircraft. 2. On downwind EXPECT vectors to final. 3. Speed restrictions on Transition are always mandatory unless cancelled by ATC. RIBSO 33 [RIB33] RWY 33 RNAV TRANSITION USE OF RNAV TRANSITION ONLY WHEN CLEARE BY ATC.SPEE: MAX 250 KT BELOW FL100 OR AS BY ATC By ATC, GERMANY.RNAV.TRANSITION. SOSAX MIN 170 KT H858 H857 0 H AM H812 V OR H813 H856 H RIBSO (-) - H804 (K220) - H815 (K220) - H854 - SOSAX (K170+; +). CHANGES: New format. H814 H815 H ^ 331^, ALL RIGHTS RESERVE.

15 Printed from JeppView for Windows on 06 ec 2017; Terminal chart data cycle ; Notice: After 14 ec 2017, 0000Z, this chart may no longer be valid EH/HAM STAE EHS ELBE LBV H256 *-ATIS H255 H257 Apt Elev SPEE: AHRENLOHE EHO UETERSEN Heist EHE ANEXI MIN 170 KT H258 H3 2. On downwind EXPECT vectors to final. 3. Speed restrictions on Transition are always mandatory unless cancelled by ATC. H2 26 MAY F Alt Set: hpa (IN on request) Trans level: By ATC 1. GPS- or FMS-equipped aircraft. BOGMU 05 [BOG~5] RARUP 05 [RAR~5] RWY 05 RNAV TRANSITIONS USE OF RNAV TRANSITION ONLY WHEN CLEARE BY ATC MAX 250 KT BELOW FL100 OR AS BY ATC By ATC Finkenwerder EHI H228 H~~2 H229 RARUP 05 H0 RARUP 05: H1 1004, GERMANY.RNAV.TRANSITION H227 Clearance Limit R051 WAHLSTET EHW RARUP BOGMU 250^ Clearance Limit (HAM R097) H225 NOT TO SCALE 167^ 16.3 MHA BOGMU ^ H ^ 1^ 277^ MHA ^ 5.0 H4 H5 H AM V OR TRANSITION BOGMU 05 RARUP 05 BOGMU (-) - H225 (K220) - H5 (K220) - H255 - ANEXI (K170+; +). RARUP (-) - H0 (K220) - H5 (K220) - H255 - ANEXI (K170+; +). CHANGES: New format., ALL RIGHTS RESERVE.

16 Printed from JeppView for Windows on 06 ec 2017; Terminal chart data cycle ; Notice: After 14 ec 2017, 0000Z, this chart may no longer be valid EH/HAM *-ATIS Apt Elev MAY G Alt Set: hpa (IN on request) Trans level: By ATC 1. GPS- or FMS-equipped aircraft. 2. On downwind EXPECT vectors to final. 3. Speed restrictions on Transition are always mandatory unless cancelled by ATC. BOGMU 15 [BOG15], RARUP 15 [RAR15] RWY 15 RNAV TRANSITIONS USE OF RNAV TRANSITION ONLY WHEN CLEARE BY ATC.SPEE: MAX 250 KT BELOW FL100 OR AS BY ATC, GERMANY.RNAV.TRANSITION H ^ 20 H ^ H457 H456 H458 EVO MIN 170 KT LBV ELBE LBV H414 H413 H412 By ATC H~~ HAM BOGMU ^ V OR ^ 13.8 R051 Clearance Limit BOGMU H417 RARUP 15 MHA ^ 314^ Clearance Limit RARUP (HAM R097) 097^ NOT TO SCALE 1^ MHA 277^ 0 5 Finkenwerder EHI TRANSITION BOGMU 15 CHANGES: RARUP 15 New format. 988 BOGMU (-) - H412 (K220) - H416 (K220) - H455 - EVO (K170+; +). RARUP (-) - H417 (K220) - H412 (K220) - H416 (K220) - H455 - EVO (K170+; +)., ALL RIGHTS RESERVE.

17 Printed from JeppView for Windows on 06 ec 2017; Terminal chart data cycle ; Notice: After 14 ec 2017, 0000Z, this chart may no longer be valid EH/HAM *-ATIS Apt Elev SPEE: 26 MAY H Alt Set: hpa (IN on request) Trans level: By ATC 1. GPS- or FMS-equipped aircraft. 2. On downwind EXPECT vectors to final. 3. Speed restrictions on Transition are always mandatory unless cancelled by ATC. BOGMU [BOG], RARUP [RAR] RWY RNAV TRANSITIONS USE OF RNAV TRANSITION ONLY WHEN CLEARE BY ATC MAX 250 KT BELOW FL100 OR AS BY ATC, GERMANY.RNAV.TRANSITION HAM BOGMU VBL R051^ LBV H658 PISAS MIN 170 KT H~~6 Clearance Limit 988 V OR MHA 138^ H634 By ATC BOGMU H611 H ^ 1^ H612 H6~~ H ^ ^ H656 H613 H655 H ^ R097^ RARUP 5.0 H ^ Clearance Limit RARUP LUBECK Blankensee EHL MHA 277^ TRANSITION BOGMU RARUP BOGMU (-) - H634 (K220) - H635 (K220) - H655 - PISAS (K170+; +). RARUP (-) - H600 (K220) - H611 (K220) - H615 (K220) - H655 - PISAS (K170+; +). CHANGES: New format., ALL RIGHTS RESERVE.

18 Printed from JeppView for Windows on 06 ec 2017; Terminal chart data cycle ; Notice: After 14 ec 2017, 0000Z, this chart may no longer be valid EH/HAM *-ATIS Apt Elev MAY J Alt Set: hpa (IN on request) Trans level: By ATC 1. GPS- or FMS-equipped aircraft. 2. On downwind EXPECT vectors to final. 3. Speed restrictions on Transition are always mandatory unless cancelled by ATC. BOGMU 33 [BOG33], RARUP 33 [RAR33] RWY 33 RNAV TRANSITIONS USE OF RNAV TRANSITION ONLY WHEN CLEARE BY ATC.SPEE: MAX 250 KT BELOW FL100 OR AS BY ATC MHA 1^, GERMANY.RNAV.TRANSITION ^ Optional H~~8 H82~ By ATC H821 LBVVBL H822 H R051 Clearance Limit BOGMU H829 H83~ SOSAX H831 MIN 170 KT H858 H H ^ BOGMU ^ H833 R097 NOT TO SCALE MHA 251^ RARUP RARUP Clearance Limit 277^ 0 5 TRANSITION BOGMU 33 RARUP 33 CHANGES: New format. H AM H856 V OR H855 H854 H ^ ^ H835 BOGMU (-) - H829 (K220) - H830 (K220) - H835 (K220) - H854 - SOSAX (K170+; +). RARUP (-) - H829 (K220) - H830 (K220) - H835 (K220) - H854 - SOSAX (K170+; +)., ALL RIGHTS RESERVE.

19 Printed from JeppView for Windows on 06 ec 2017; Terminal chart data cycle ; Notice: After 14 ec 2017, 0000Z, this chart may no longer be valid EH/HAM *-ATIS Apt Elev OCT K Alt Set: hpa (IN on request) Trans level: By ATC 1. GPS- or FMS-equipped aircraft. 2. On downwind EXPECT vectors to final. 3. Speed restrictions on Transition are always mandatory unless cancelled by ATC. NOLGO 05 [NOL~5] RWY 05 RNAV TRANSITION USE OF RNAV TRANSITION ONLY WHEN CLEARE BY ATC.SPEE: MAX 250 KT BELOW FL100 OR AS BY ATC, GERMANY.RNAV.TRANSITION H H ^ 5.0 H257 ANEXI MIN 170 KT H3 H4 H5 H258 H2 By ATC Finkenwerder EHI H~~2 228^ H H~ 9.3 MHA 310^ 006^ R186 H AM Clearance Limit NOLGO V OR NOLGO (-) - H0 (K220) - H5 (K220) - H255 - ANEXI (K170+; +). CHANGES: None., ALL RIGHTS RESERVE.

20 Printed from JeppView for Windows on 06 ec 2017; Terminal chart data cycle ; Notice: After 14 ec 2017, 0000Z, this chart may no longer be valid EH/HAM *-ATIS H455 USE OF RNAV TRANSITION ONLY WHEN CLEARE BY ATC.SPEE: MAX 250 KT BELOW FL100 OR AS BY ATC H H457 Apt Elev ^ 150^ By ATC H456 H458 EVO MIN 170 KT Finkenwerder EHI 20 H414 H~~4 27 OCT 17 H413 H L Alt Set: hpa (IN on request) Trans level: By ATC 1. GPS- or FMS-equipped aircraft. 2. On downwind EXPECT vectors to final. 3. Speed restrictions on Transition are always mandatory unless cancelled by ATC. NOLGO 15 [NOL15] RWY 15 RNAV TRANSITION H4~9 H4~7 H4~8 H4~6 At 220 KT 15.2 NOLGO 15 H4~5 H4~4 21 H4~3, GERMANY.RNAV.TRANSITION. Optional 331^ ^ R186 5 CHANGES: Reissue. HAM VOR MHA 006^ Clearance Limit NOLGO NOLGO (-) - H406 (K220) - H416 (K220) - H455 - EVO(K170+; +) , ALL RIGHTS RESERVE.

21 Printed from JeppView for Windows on 06 ec 2017; Terminal chart data cycle ; Notice: After 14 ec 2017, 0000Z, this chart may no longer be valid EH/HAM 26 MAY M Alt Set: hpa (IN on request) Trans level: By ATC *-ATIS Apt Elev 1. GPS- or FMS-equipped aircraft On downwind EXPECT vectors to final. 3. Speed restrictions on Transition are always mandatory unless cancelled by ATC. NOLGO [NOL] RWY RNAV TRANSITION USE OF RNAV TRANSITION ONLY WHEN CLEARE BY ATC.SPEE: MAX 250 KT BELOW FL100 OR AS BY ATC, GERMANY.RNAV.TRANSITION Finkenwerder EHI H6~7 H AM 1004 PISAS MIN 170 KT HAM Optional H~~6 MHA H6~8 By ATC H61~ H6~9 R ^ NOLGO NOLGO Clearance Limit H657 H658 H656 H612 H611 H ^ H ^ H H615 LUBECK Blankensee EHL 5 V OR 006^ NOLGO (-) - H611 (K220) - H615 (K220) - H655 - PISAS (K170+; +). CHANGES: New format., ALL RIGHTS RESERVE.

22 Printed from JeppView for Windows on 06 ec 2017; Terminal chart data cycle ; Notice: After 14 ec 2017, 0000Z, this chart may no longer be valid EH/HAM *-ATIS Apt Elev MAY N Alt Set: hpa (IN on request) Trans level: By ATC 1. GPS- or FMS-equipped aircraft. 2. On downwind EXPECT vectors to final. 3. Speed restrictions on Transition are always mandatory unless cancelled by ATC. NOLGO 33 [NOL33] RWY 33 RNAV TRANSITION USE OF RNAV TRANSITION ONLY WHEN CLEARE BY ATC.SPEE: MAX 250 KT BELOW FL100 OR AS BY ATC HAM, GERMANY.RNAV.TRANSITION CHANGES: H~~8 SOSAX MIN 170 KT R186 HA M H858 H857 VO R H856 H855 H854 H832 H833 H New format. By ATC Clearance Limit NOLGO MHA ^ 080^ ^ 331^ 5.0 NOLGO (-) - H832 (K220) - H835 (K220) - H854 - SOSAX (K170+; +). 241^ H835, ALL RIGHTS RESERVE.

23 Printed from JeppView for Windows on 06 ec 2017; Terminal chart data cycle ; Notice: After 14 ec 2017, 0000Z, this chart may no longer be valid EH/HAM 26 MAY P GIKOG FL250 FL190 SCHLESWIG ETNS HOHN ETNH Finkenwerder EHI KIEL Holtenau EHK VOR HAM FL150 H9~1 FL70 H9~2 FL150 H9~3 FL70 H9~5 FL70 EKERN FL250 FL H9~4 FL ANEXI 25 H213 MIN 170 KT H LUBECK Blankensee EHL FL250 FL EKERN 2A 190^ GIKOG 1A H9~~ *-ATIS Apt Elev TRANSITION EKERN 2A GIKOG 1A MICHAELSORF MIC, GERMANY.RNAV.TRANSITION. Alt Set: hpa (IN on request) Trans level: By ATC 1. GPS- or FMS-equipped aircraft. 2. When cleared for "transition and profile" aim for a low noise Continuous escent Approach (CA) within the constraints as laid down in the procedure description. EKERN 2A [EKER2A], GIKOG 1A [GIKO1A], MIC 2A [MIC2A] RWY 05 RNAV TRANSITIONS FLY THE TRANSITION AS CONTINUOUS ESCENT APPROACH (CA) USE OF RNAV TRANSITION ONLY WHEN CLEARE BY ATC.SPEE: MAX 250 KT BELOW FL100 OR AS BY ATC EKERN (FL250-; FL170+) - H902 (FL150-; +) - H903 (FL70+) - H213 - H257 (K220) - ANEXI (K170+; +). GIKOG (FL250-; FL190+) - H900 (FL150-; +) - H901 (FL70+) - H213 - H257 (K220) - ANEXI (K170+; +). MIC 2A MIC (FL250-; FL190+) - H904 (FL150-; +) - H905 (FL70+) - H213 - H257 (K220) - ANEXI (K170+; +). 162^ 40.0 MIC 2A ^ ^ ^ ^ CHANGES: New format., ALL RIGHTS RESERVE

24 Printed from JeppView for Windows on 06 ec 2017; Terminal chart data cycle ; Notice: After 14 ec 2017, 0000Z, this chart may no longer be valid EH/HAM 26 MAY Q, GERMANY.RNAV.TRANSITION. ANEXI MIN 170 KT H257 H911 FL H3 Finkenwerder EHI HA M VO R H9~7 FL H9~9 FL70 H9~6 FL150 H91~ FL150 H9~8 FL150 RAMAR FL210 FL ^ ^ 282^ ^ FL220 FL150 Alt Set: hpa (IN on request) Trans level: By ATC ^ RAMAR 1A.2 NOT TO SCALE FL240 FL BUMIL 1A.2 283^ NOT TO SCALE IRBO *-ATIS Apt Elev 53 2.When cleared for "transition and profile" aim for a low noise Continuous escent Approach (CA) within the constraints as laid down in the procedure description. FLY THE TRANSITION AS CONTINUOUS ESCENT APPROACH (CA) USE OF RNAV TRANSITION ONLY WHEN CLEARE BY ATC.SPEE: MAX 250 KT BELOW FL100 OR AS BY ATC TRANSITION BUMIL 1A IRBO 2A RAMAR 1A 1. GPS- or FMS-equipped aircraft. BUMIL 1A [BUMI1A], IRBO 2A [IRB2A] RAMAR 1A [RAMA1A] RWY 05 RNAV TRANSITIONS BUMIL (FL240-; FL170+) - H908 (FL150-; +) - H909 (FL70+) - H3 - H257 (K220) - ANEXI (K170+; +). IRBO (FL220-; FL150+) - H906 (FL150-; +) - H907 (FL70+) - H3 - H257 (K220) - ANEXI (K170+; +). RAMAR (FL210-; FL140+) - H910 (FL150-; +) - H911 (FL70+) - H3 - H257 (K220) - ANEXI (K170+; +). BUMIL IRBO 2A 306^ CHANGES: New format., ALL RIGHTS RESERVE.

25 CHANGES: New format., ALL RIGHTS RESERVE. Printed from JeppView for Windows on 06 ec 2017; Terminal chart data cycle ; Notice: After 14 ec 2017, 0000Z, this chart may no longer be valid *-ATIS GIKOG FL200 FL ^ GIKOG 2F Apt Elev H932 FL Alt Set: hpa (IN on request) Trans level: By ATC 1. GPS- or FMS-equipped aircraft. 2. When cleared for "transition and profile" aim for a low noise Continuous escent Approach (CA) within the constraints as laid down in the procedure description. SCHLESWIG ETNS HOHN ETNH TRANSITION EKERN 2F EKERN (FL180-; FL100+) - H931 (FL70+) - H458 (K220) - EVO (K170+; +). GIKOG 2F GIKOG (FL200-; FL140+) - H932 (FL150-; +) - H933 (FL100-; FL70+) - H458 (K220) - EVO (K170+; +). MIC 2F MIC (FL180-; FL130+) - H929 (FL150-; +) - H930 (FL100-; FL70+) - H934 - H458 (K220) - EVO (K170+; +)..2 EKERN FL FL100 H933 FL100 FL70 H931 FL70 HAM KIEL Holtenau EHK V OR H H EKERN 2F [EKER2F], GIKOG 2F [GIKO2F], MIC 2F [MIC2F] RWY 15 RNAV TRANSITIONS FLY THE TRANSITION AS CONTINUOUS ESCENT APPROACH (CA) USE OF RNAV TRANSITION ONLY WHEN CLEARE BY ATC.SPEE: MAX 250 KT BELOW FL100 OR AS BY ATC ^ 22.7 EKERN 2F ^ 7.8 4^ H93~ FL100 FL70 EVO MIN 170 KT H929 FL150.2 NOT TO SCALE MIC MICHAELSORF MIC FL180 FL RWY 15 RNAV TRANSITIONS MIC 2F 5^ EKERN 2F [EKER2F], GIKOG 2F [GIKO2F] MIC 2F [MIC2F] EH/HAM 26 MAY S, GERMANY.RNAV.TRANSITION.

26 Printed from JeppView for Windows on 06 ec 2017; Terminal chart data cycle ; Notice: After 14 ec 2017, 0000Z, this chart may no longer be valid EH/HAM 26 MAY T, GERMANY.RNAV.TRANSITION. H432 H458 H922 FL70 EVO MIN 170 KT Finkenwerder EHI H924 FL70 H928 FL70 H926 FL70 H V OR H AM H921 FL150 H H92~ FL150 AGATI FL220 FL170 H9 FL150 FL150 NOT TO SCALE H927 FL150 RAMAR FL170 FL120 IRBO FL270 FL200 *-ATIS Apt Elev ^ ^ ^ ^ 284^ RAMAR 2F ^ 330^ IRBO 2F BUMIL 2F 312^ NOT TO SCALE TRANSITION Alt Set: hpa (IN on request) Trans level: By ATC 1. GPS- or FMS-equipped aircraft. 2. When cleared for "transition and profile" aim for a low noise Continuous escent Approach (CA) within the constraints as laid down in the procedure description. AGATI 2F [AGAT2F], BUMIL 2F [BUMI2F] IRBO 2F [IRB2F]. RAMAR 2F [RAMA2F] RWY 15 RNAV TRANSITIONS FLY THE TRANSITION AS CONTINUOUS ESCENT APPROACH (CA) USE OF RNAV TRANSITION ONLY WHEN CLEARE BY ATC.SPEE: MAX 250 KT BELOW FL100 OR AS BY ATC AGATI 2F AGATI (FL220-; FL170+) - H920 (FL150+) - H921 (FL150-; +) - H922 (FL70+) - H432 - H458 (K220) - EVO (K170+; +). BUMIL 2F BUMIL (FL270-; FL190+) - H925 (FL150-; +) - H926 (FL70+) - H412 - H458 (K220) - EVO (K170+; +). IRBO 2F IRBO (FL270-; FL200+) - H9 (FL150-; +) - H924 (FL70+) - H412 - H458 (K220) - EVO (K170+; +). RAMAR 2F RAMAR (FL170-; FL120+) - H927 (FL150-; +) - H928 (FL70+) - H412 - H458 (K220) - EVO (K170+; +). BUMIL FL270 FL AGATI 2F ^ 345^ CHANGES: New format., ALL RIGHTS RESERVE

27 Printed from JeppView for Windows on 06 ec 2017; Terminal chart data cycle ; Notice: After 14 ec 2017, 0000Z, this chart may no longer be valid EH/HAM GIKOG FL250 FL ^ EKERN 2K 6.2 NOT TO SCALE H940 FL150 SCHLESWIG ETNS HOHN ETNH EKERN FL170 FL120 H942 FL150 *-ATIS Apt Elev MAY U, GERMANY.RNAV.TRANSITION. Alt Set: hpa (IN on request) Trans level: By ATC 1. GPS- or FMS-equipped aircraft. 2. When cleared for "transition and profile" aim for a low noise Continuous escent Approach (CA) within the constraints as laid down in the procedure description. 135^ EKERN 2K [EKER2K], GIKOG 1K [GIKO1K] MIC 2K [MIC2K] RWY RNAV TRANSITIONS FLY THE TRANSITION AS CONTINUOUS ESCENT APPROACH (CA) USE OF RNAV TRANSITION ONLY WHEN CLEARE BY ATC.SPEE: MAX 250 KT BELOW FL100 OR AS BY ATC GIKOG 1K ^ MICHAELSORF MIC FL ^ MIC 2K.9.2 V OR H AM TRANSITION EKERN 2K EKERN (FL170-; FL120+) - H942 (FL150-; +) - H943 (FL70+) - H952 - H658 (K220) - PISAS (K170+; +). GIKOG 1K GIKOG (FL250-; FL190+) - H940 (FL150-; +) - H941 (FL70+) - H632 - H658 (K220) - PISAS (K170+; +). MIC 2K MIC (FL180-; +) - H944 (FL70+) - H953 - H658 (K220) - PISAS (K170+; +). H941 FL70 H943 FL70 PISAS MIN 170 KT H952 H944 FL H632 H658 H ^ LUBECK Blankensee EHL ^ 228^ CHANGES: New format., ALL RIGHTS RESERVE

28 Printed from JeppView for Windows on 06 ec 2017; Terminal chart data cycle ; Notice: After 14 ec 2017, 0000Z, this chart may no longer be valid PISAS MIN 170 KT H951 H949 FL70 FL70 FASSBERG ETHS LUNEBURG EHG UELZEN EVU LUEBECK Blankensee EHL LUCHOW Rehbeck EHC 27 IRBO NOT TO SCALE NEUSTAT-GLEWE EAN V OR AGATI FL0 FL180 H95~ FL150 H AM H H612 H947 FL70 FL150 H945 FL RAMAR 2K FL220 FL150 RAMAR FL120 FL H946.2 FL150 FL190 FL130 AGATI 2K BUMIL 1K 13.3 H948 EH/HAM *-ATIS Apt Elev MAY 17 BUMIL 10-2V, GERMANY.RNAV.TRANSITION. Alt Set: hpa (IN on request) Trans level: By ATC 1. GPS- or FMS-equipped aircraft. 2. When cleared for "transition and profile" aim for a low noise Continuous escent Approach (CA) within the constraints as laid down in the procedure description. 228^ AGATI 2K [AGAT2K], BUMIL 1K [BUMI1K] IRBO 1K [IRB1K], RAMAR 2K [RAMA2K] 277^ ^ 318^ RWY RNAV TRANSITIONS FLY THE TRANSITION AS CONTINUOUS ESCENT APPROACH (CA) USE OF RNAV TRANSITION ONLY WHEN CLEARE BY ATC.SPEE: MAX 250 KT BELOW FL100 OR AS BY ATC 315^ TRANSITION AGATI 2K AGATI (FL0-; FL180+) - H950 (FL150-; +) - H951 (FL70+) - H612 - H658 (K220) - PISAS (K170+; +). BUMIL 1K BUMIL (FL190-; FL130+) - H946 (FL150-; +) - H947 (FL70+) - H658 (K220) - PISAS (K170+; +). IRBO 1K IRBO (FL220-; FL150+) - H948 (FL150-; +) - H949 (FL70+) - H612 - H658 (K220) - PISAS (K170+; +). RAMAR 2K RAMAR (FL120-; FL80+) - H945 (FL70+) - H658 (K220) - PISAS (K170+; +). IRBO 1K 012^ 316^ ^

29 Printed from JeppView for Windows on 06 ec 2017; Terminal chart data cycle ; Notice: After 14 ec 2017, 0000Z, this chart may no longer be valid EH/HAM V OR GIKOG FL250 FL H AM FL150 Finkenwerder EHI EKERN 164^ FL250 FL170 EKERN 1S 28.9 GIKOG 1S 150^ 48.8 H96~ NOT TO SCALE H961 FL70 H962 FL150 SOSAX MIN 170 KT H963 FL70 H965 FL70 FL220 FL150 H966 FL70 FL150.2 H831 LUBECK Blankensee EHL 151^.2 RAMAR FL140 FL H TRANSITION EKERN 1S EKERN (FL250-; FL170+) - H962 (FL150-; +) - H963 (FL70+) - H831 - H858 (K220) - SOSAX (K170+; +). GIKOG 1S GIKOG (FL250-; FL210+) - H960 (FL150-; +) - H961 (FL70+) - H811 - H858 (K220) - SOSAX (K170+; +). MIC 1S MIC (FL220-; FL150+) - H964 (FL150-; +) - H965 (FL70+) - H ^ 5.0 H811 *-ATIS Apt Elev Alt Set: hpa (IN on request) Trans level: By ATC 1. GPS- or FMS-equipped aircraft. 2. When cleared for "transition and profile" aim for a low noise Continuous escent MICHAELSORF MIC MIC 1S 205^ 21.1 H RAMAR 1S ^ 061^ 331^ 1004 NOT TO SCALE CHANGES: New format., ALL RIGHTS RESERVE. 26 MAY W, GERMANY.RNAV.TRANSITION. Approach (CA) within the constraints as laid down in the procedure description. EKERN 1S [EKER1S], GIKOG 1S [GIKO1S], MIC 1S [MIC1S] RAMAR 1S [RAMA1S] RWY 33 RNAV TRANSITIONS FLY THE TRANSITION AS CONTINUOUS ESCENT APPROACH (CA) USE OF RNAV TRANSITION ONLY WHEN CLEARE BY ATC.SPEE: MAX 250 KT BELOW FL100 OR AS BY ATC H858 (K220) - SOSAX (K170+; +). RAMAR 1S RAMAR (FL140-; FL90+) - H966 (FL70+) - H831 - H858 (K220) - SOSAX (K170+; +)

30 Printed from JeppView for Windows on 06 ec 2017; Terminal chart data cycle ; Notice: After 14 ec 2017, 0000Z, this chart may no longer be valid EH/HAM *-ATIS Apt Elev MAY X Alt Set: hpa (IN on request) Trans level: By ATC 1. GPS- or FMS-equipped aircraft., GERMANY.RNAV.TRANSITION. 2. When cleared for "transition and profile" aim for a low noise Continuous escent Approach (CA) within the constraints as laid down in the procedure description. BUMIL 2S [BUMI2S], IRBO 2S [IRB2S] RWY 33 RNAV TRANSITIONS FLY THE TRANSITION AS CONTINUOUS ESCENT APPROACH (CA) USE OF RNAV TRANSITION ONLY WHEN CLEARE BY ATC.SPEE: MAX 250 KT BELOW FL100 OR AS BY ATC SOSAX MIN 170 KT H858 3^ 3.4 H972 HA M VO R H971 H970 FL70 25 H968 FL H967 FL150 BUMIL FL160 FL H969 FL150 IRBO FL FL120 TRANSITION BUMIL 2S CHANGES: New format ^ IRBO 2S.2 BUMIL (FL160-; FL120+) - H967 (FL150-; +) - H968 (FL70+) - H971 - H858 (K220) - SOSAX (K170+; +). IRBO 2S IRBO (FL190-; FL120+) - H969 (FL150-; +) - H970 (FL70+) - H972 - H858 (K220) - SOSAX (K170+; +). 324^ 4.9 NOT TO SCALE 4.5 BUMIL 2S 293^, ALL RIGHTS RESERVE.

31 Printed from JeppView for Windows on 06 ec 2017; Terminal chart data cycle ; Notice: After 14 ec 2017, 0000Z, this chart may no longer be valid EH/HAM BREMEN Radar Apt Elev 53 Trans alt: Remain on Tower frequency until passing 2000, then contact BREMEN Radar. 2. SIs are also noise abatement procedures. Strict adherence within the limits of aircraft performance is mandatory. 3. Rwys, 05, 15: EXPECT close-in obstacles. 26 MAY AMLUH 9B, AMLUH 8C, AMLUH 8, AMLUH 8G EPARTURES.SPEE: MAX 250 KT BELOW FL100 OR AS BY ATC., GERMANY.SI. LUEBECK Blankensee EHL 114^ ELBE LBV GT 350 FU Finkenwerder EHI HOS 339 ME ALSTER (115.8) ALF ALF 117^ AMLUH 8G 358^ 5.2 ALF 331^ 151^ 229^ AMLUH 9B 5.5 ALF 5.0 ALF R ALF 4.1 ALF 162^ 4 AMLUH 8C 16.0 AMLUH ALF 089^ HAM AMLUH 29.8 V O R SI RWY AMLUH 9B AMLUH 8C 05 AMLUH 8 15 AMLUH 8G Initial climb clearance 5000 AMLUH 8 Climb straight ahead via FU to 5.5 ALF, turn LEFT, 089^ track, intercept This SI requires a minimum climb gradient LBV R114 to AMLUH. of To HOS (4.1 ALF), bearing to 5.2 ALF turn RIGHT, intercept 365 per NM (6.0%) until passing 2800 due to HAM R162 to AMLUH. airspace structure. Intercept 151^ bearing from GT to 8.2 ALF, turn LEFT, intercept LBV R114 to Gnd speed-kt AMLUH. 365 per NM Intercept 331^ bearing towards GT, at 3.0 ALF turn RIGHT, 358^ track, If unable to comply advise ATC prior to start-up. at 5.0 ALF turn RIGHT, intercept HAM R297 inbound to HAM, turn RIGHT, HAM R162 to AMLUH. CHANGES: New format., ALL RIGHTS RESERVE

32 Printed from JeppView for Windows on 06 ec 2017; Terminal chart data cycle ; Notice: After 14 ec 2017, 0000Z, this chart may no longer be valid CHANGES: New format., ALL RIGHTS RESERVE. BREMEN Radar Apt Elev BASUM (114.3 OSN R026) 22 WESER 378 WSN BREMEN EW 290^ 0 NIEEIN Trans alt: Remain on Tower frequency until passing 2000, then contact BREMEN Radar. 2. SIs are also noise abatement procedures. Strict adherence within the limits of aircraft performance is mandatory. 3. Rwys, 05, 15: EXPECT close-in obstacles. 202^ HAM ELBE LBV (LBV R175) [H1~5] 3 GT 5^ 5.0 ALF Finkenwerder EHI Initial climb clearance 5000 BASUM 4 This SI requires a minimum climb gradient Climb straight ahead to FU, 229^ bearing, intercept HAM R5 to of 38.1 HAM, turn LEFT, intercept LBV R206 to BASUM. 425 per NM (7.0%) until passing 2000 due to Intercept bearing towards HOS, at 3.8 ALF turn LEFT, intercept airspace structure. HAM R296, intercept LBV R064 inbound to LBV, turn LEFT, LBV R206 to BASUM. Gnd speed-kt Intercept 151^ bearing from GT to 5.0 ALF, turn RIGHT, intercept 255^ bearing towards WSN to 32.7 HAM, turn LEFT, 425 per NM intercept LBV R206 to BASUM. If unable to comply advise ATC prior to Intercept 331^ bearing towards GT, at ALF turn LEFT, start-up. intercept LBV R070 inbound to LBV, turn LEFT, LBV R206 to BASUM. 296^ GT BASUM 3B, BASUM 1C, BASUM 4, BASUM 1G EPARTURES SI RWY BASUM 3B BASUM 1C 05 BASUM 4 15 BASUM 1G 33.SPEE: MAX 250 KT BELOW FL100 OR AS BY ATC HAM HAM 7 206^ R064 R ^ ME ALSTER ALF FU BASUM 1G 25.0 HAM (115.8) ALF 350 FU 12 BASUM 3B ^ 229^ 331^ BASUM 1C 151^ [H153] ALF 3.8 ALF BASUM 4 255^ 2000 H AM HAM HOS 339 V OR BASUM 3B BASUM 1C BASUM 4 BASUM 1G EPARTURES 26 MAY A.SI. EH/HAM, GERMANY

33 Printed from JeppView for Windows on 06 ec 2017; Terminal chart data cycle ; Notice: After 14 ec 2017, 0000Z, this chart may no longer be valid EH/HAM 26 MAY B BREMEN Radar Apt Elev Trans alt: Remain on Tower frequency until passing 2000, then contact BREMEN Radar. 2. SIs are also noise abatement procedures. Strict adherence within the limits of aircraft performance is mandatory. 3. Rwys, 05, 15: EXPECT close-in obstacles. EKERN 8B, EKERN 8C, EKERN 9, EKERN 8G EPARTURES.SPEE: MAX 250 KT BELOW FL100 OR AS BY ATC.. EKERN 50.8, GERMANY.SI. NOT TO SCALE 25.0 HAM [H1~3] SI EKERN 8B 3 GT GT FU 350 FU 038^ EKERN 8B RWY EKERN 8C 05 EKERN 9 15 EKERN 8G 33 CHANGES: New format. 5.5 ALF ^ 3.0 ALF 358^ 229^ EKERN 8G 331^ 5.6 ALF 151^ ME ALSTER ALF (115.8)ALF HOS 339 8C EKERN 2.5 ALF 2.5 ALF ALF 4.1 ALF MSA HAM VOR Intercept 151^ bearing from GT, at 2.5 ALF or 1500, whichever is later, turn LEFT, intercept HAM R208 inbound to HAM, turn LEFT, HAM R344 to EKERN. 028^ EKERN 9 At or whichever is later Initial climb clearance R Climb straight ahead via FU to 5.5 ALF, turn RIGHT, intercept 038^ bearing to GT, 031^ bearing, intercept HAM R344 to EKERN. To HOS (4.1 ALF), bearing to 7.2 ALF, turn LEFT, intercept HAM R344 to EKERN. Intercept 331^ bearing towards GT, at 3.0 ALF turn RIGHT, 358^ track, at 5.6 ALF turn RIGHT, intercept 031^ bearing from GT, intercept HAM R344 to EKERN. 344^, ALL RIGHTS RESERVE.