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

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1 Airport Information For EV Printed on 06 ec 207 Page (c) SANERSON, INC., 207, ALL RIGHTS RESERVE jep= JeppView for Windows TZ-Elev: General 69 Information ft Lighting: Edge, ALS, Centerline, REIL, TZ Location: EU Communication ICAO/IATA: EV / HAJ Information Lat/Long: N ', E ' Elevation: 83 ft ATIS: At or below ft Out to 60 mi. Hannover Tower: Military Hannover Airport Use: Tower: Public20.75 Hannover aylight Savings: Tower: Observed Hannover UTC Conversion: Ground: -: = UTC e-icing Magnetic Ramp/Taxi: Variation: E e-icing Ramp/Taxi: Secondary Bremen Radar ACC: Military Bremen Fuel Types: Radar 00 ACC: Octane (LL), Jet A- Bremen Repair Types: Radar Major ACC: Airframe, Major Engine Customs: Yes Airport Type: IFR Landing Fee: Yes Control Tower: Yes Jet Start Unit: No LLWS Alert: No Beacon: Yes Sunrise: 075 Z Sunset: 509 Z Runway Information Runway: 09C Length x Width: 2559 ft x 74 ft Surface Type: asphalt TZ-Elev: 78 ft isplaced Threshold: 97 ft Stopway: 558 ft Runway: 09L Length x Width: 0499 ft x 48 ft Surface Type: concrete TZ-Elev: 67 ft Lighting: Edge, ALS, Centerline, REIL, TZ Runway: 09R Length x Width: 7677 ft x 48 ft Surface Type: concrete TZ-Elev: 72 ft Lighting: Edge, ALS, Centerline, REIL Runway: 27C Length x Width: 2559 ft x 74 ft Surface Type: asphalt TZ-Elev: 74 ft isplaced Threshold: 558 ft Stopway: 97 ft Runway: 27L Length x Width: 7677 ft x 48 ft Surface Type: concrete TZ-Elev: 79 ft Lighting: Edge, ALS, Centerline, REIL Runway: 27R Length x Width: 0499 ft x 48 ft Surface Type: concrete

2 Airport Information For EV Printed on 06 ec 207 Page 2 (c) SANERSON, INC., 207, ALL RIGHTS RESERVE jep= JeppView for Windows General TZ-Elev: 69 Information ft Lighting: Edge, ALS, Centerline, REIL, TZ Location: EU ICAO/IATA: Communication EV / HAJ Information Lat/Long: N ', E ' Elevation: 83 ft ATIS: At or below ft Out to 60 mi. Hannover Tower: Military Airport Hannover Use: Tower: Public aylight Hannover Savings: Tower: Observed UTC Hannover Conversion: Ground: -: = UTC Magnetic e-icing Ramp/Taxi: Variation: E e-icing Ramp/Taxi: Secondary Bremen Radar ACC: Military Fuel Bremen Types: Radar 00 ACC: Octane (LL), Jet A- Repair Bremen Types: Radar Major ACC: Airframe, Major Engine Customs: Yes Airport Type: IFR Landing Fee: Yes Control Tower: Yes Jet Start Unit: No LLWS Alert: No Beacon: Yes Sunrise: 075 Z Sunset: 509 Z Runway Information Runway: 09C Length x Width: 2559 ft x 74 ft Surface Type: asphalt TZ-Elev: 78 ft isplaced Threshold: 97 ft Stopway: 558 ft Runway: 09L Length x Width: 0499 ft x 48 ft Surface Type: concrete TZ-Elev: 67 ft Lighting: Edge, ALS, Centerline, REIL, TZ Runway: 09R Length x Width: 7677 ft x 48 ft Surface Type: concrete TZ-Elev: 72 ft Lighting: Edge, ALS, Centerline, REIL Runway: 27C Length x Width: 2559 ft x 74 ft Surface Type: asphalt TZ-Elev: 74 ft isplaced Threshold: 558 ft Stopway: 97 ft Runway: 27L Length x Width: 7677 ft x 48 ft Surface Type: concrete TZ-Elev: 79 ft Lighting: Edge, ALS, Centerline, REIL Runway: 27R Length x Width: 0499 ft x 48 ft Surface Type: concrete

3 , 2005, 20. ALL RIGHTS RESERVE. Printed from JeppView for Windows on 06 ec 207; Terminal chart data cycle ; Notice: After 4 ec 207, 0000Z, this chart may no longer be valid EV/HAJ.. ATIS *-ATIS AUG 0-P. GENERAL, GERMANY AIRPORT.BRIEFING.2. NOISE ABATEMENT PROCEURES.2.. NIGHT FLYING RESTRICTIONS Between LT, aircraft exceeding the noise limits pursuant to ICAO Annex 6, Volume, Chapter 3 are not permitted to operate. If any ACFT are to take-off or land between LT, a copy of the noise certificates shall be submitted in advance. Between LT, only the following ACFT movements and ACFT are permitted:. Take-offs and landings of turbo-jet ACFT with noise certificate in accordance ICAO with Annex 6, Chapter 3 or 4 which are more than 8 EPNdB below the limits laid down in ICAO Annex 6, Volume, Chapter 3, and a) which are usually scheduled for the APT of Hannover, or b) which are used for night airmail service of a universal service provider as defined in the Postal Universal Service Ordinance (PULV) if the night flight is required to meet the quality standard in accordance with Article 2, item 3 of the PULV (service provider shall prove this in advance to the airport), or c) which are operated by air carriers whose main base and maintenance facilities are in Hannover. 2. Take-offs and landings of turbo-jet cargo ACFT with noise certificate in accordance ICAO with Annex 6, Chapter 3 or 4, and a) which are more than 8 EPNdB below the limits laid down in ICAO Annex 6, Volume, Chapter 3, or b) all jet ACFT up to 2 KGS MTOW which are more than 5 EPNdB below the limits laid down in ICAO Annex 6, Volume, Chapter 3, as well as the following ACFT types: A300 CANAAIR RJ A30 ASH A39 FOKKER 70/00 A320 GULFSTREAM IV/V A32 LOCKHEE L0 - take-off only A330 C series A340 C 0 - take-off only BAe 46/AVRO RJ-series C 0-30 (all versions) - landing only B77 M B re-engined with 3 tay engines M 80 (all versions) - landing only B /400/500/600/700/800 M 90 B TUPOLEV 204 B757 B767 B Landings of ACFT not exceeding the limits pursuant to ICAO Annex 6, Volume, Chapter 3, operated by air carriers whose main base and maintenance facilities are in Hannover. 4. Take-offs and landings of ACFT with different means of propulsion in commercial and corporate air traffic complying with the provisions of ICAO Annex 6, Volume, Chapters 3, 4, 5, 6, (-4 dba), 8, 0 (-3 to -8 dba) or and/or Chapters III, IV 2.4, VII or X 2.4 of Noise Requirements for ACFT as well as landings of ACFT with different means of propulsion and noise certificate stationed at Hannover Airport in business air traffic. 5. Landings of delayed ACFT which are part of scheduled air services or regular air inclusive tours, which do not exceed the noise limits pursuant to ICAO Annex 6, Volume, Chapter 3 and which are scheduled to arrive at Hannover prior to 2300LT. 6. Landings of ACFT provably using the airport as alternate aerodrome for meteorological, technical or other safety reasons.

4 , 2005, 20. ALL RIGHTS RESERVE. Printed from JeppView for Windows on 06 ec 207; Terminal chart data cycle ; Notice: After 4 ec 207, 0000Z, this chart may no longer be valid EV/HAJ + 9 AUG 0-P. GENERAL, GERMANY AIRPORT.BRIEFING 7. Calibration flights conducted by FS eutsche Flugsicherung GmbH as far as necessary for maintaining flight safety. 8. Take-offs and landings in emergency cases. 9. Take-offs and landings in exceptional cases with special permission from the aviation supervision office of the "Niedersaechsisches Ministerium fuer Wirtschaft, Arbeit und Verkehr". Subject to further restrictions of this provision, between LT take-offs and landings by ACFT as listed below are only permitted on the northern RWYs 09L/27R. Exceptions for urgent technical, meteorological or operational reasons are possible. A300 LOCKHEE L0 A30 C 8-70-series A330 C 0 A340 M B re-engined with 3 tay engines M 80-series B M 90 B TUPOLEV 54 B TUPOLEV 204 B767 B777 and propeller-driven ACFT with more than 5.7t MTOW LOCAL FLYING RESTRICTIONS. Arrivals and departures immediately following one another as well as circling flights for ACFT over 5.7t MTOW and for ACFT up to 5.7t MTOW not complying with the conditions of ICAO Annex 6, Volume I, Chapter 3, 4, 5, 6 (-4 db [A]), 8, 0 (-3 to -8 db [A]) or pursuant to ICAO and/or LSL Chapters III, V, VI 2.4, VIII or X 2.4: Only permitted MON-FRI between LT and SAT between LT. 2. Arrivals and departures immediately following one another as well as circling flights for ACFT up to 5.7t MTOW complyingwith the conditions of ICAO Annex 6, Volume I, Chapter 3, 4, 5, 6 (-4 db [A]), 8, 0 (-3 to -8 db [A]) or pursuant to ICAO and/or LSL Chapters III, V, VI 2.4, VIII or X 2.4: Only permitted MON-SAT between LT and SUN, HOL between LT. 3. Arrivals and departures immediately following one another, not represented at the APT by an ACFT operator, are subject to permission by the "Luftaufsicht" at Hannover APT RUN-UP TESTS Run-up tests of jet engines shall be conducted exclusively in a noise suppression facility which is ready for operation. If the noise suppression facility is not ready for operation, run-up tests of jet engines may be conducted only from LT. Between LT as well as between LT run-up tests of jet engines may, however, also be conducted outside the noise suppression facility which is not ready for operation if required for urgent maintenance due to safety reasons shortly before a take-off after landing. This provision does not apply to idle test runs..3. LOW VISIBILITY PROCEURES ACFT will be guided onto RWY by Follow-me car. Enquiries via Ground.

5 , 2005, 207. ALL RIGHTS RESERVE. Printed from JeppView for Windows on 06 ec 207; Terminal chart data cycle ; Notice: After 4 ec 207, 0000Z, this chart may no longer be valid EV/HAJ 22 SEP 7 +, GERMANY.AIRPORT.BRIEFING.. GENERAL.4. AUXILIARY POWER UNIT (APU) To avoid additional noise and reduce further immissions, utilization of the APU shall be reduced to a minimum. This is the responsibility of the pilot. The APU shall be operated only: - To start the engines; 5 min prior to EOBT; at the earliest; - For necessary maintenance work on the ACFT; - If the stationary or mobile ground equipment of the APT is not available or suitable for certain ACFT types. In special cases, extended hours of operation for the APU may be granted by the APT duty officer (Tel : )..5. TAXI PROCEURES.5.. GENERAL uring the entire taxiing phase, ACFT shall maintain continuous radio contact with the control tower. Any instructions to change frequency shall be complied with without delay. To increase safety of RWYs RWY guard lights have been installed on both sides of CAT I holding positions of RWYs 09L/27R and 09R/27L, as well as of holding positions of RWY 09C/27C. On the apron, ACFT are permitted to taxi only at the minimum RPM required. TWYs A,, F and L on the apron are ACFT stand taxilanes with reduced minimum separation distances between taxilane centerlines and stationary objects. The separation distances between taxilane centerline and the red obstacle limitation lines are: - 56'/47.5m in the area of the parallel TWY F between positions 42 and 6 and L between postitions 4 an 27. The separation between the parallel guidelines is 256'/78m. - 39'/42.5m in the area of TWY. - 36'/4.5m in the area of taxilane A between positions 23 and '/38m in the area of positions and '/26m in the area of positions 2, 3 and 20. When entering positions to 20, the oversteering procedure shall be used. TWY B MAX wingspan 8'/36m, 59'/8m wheel base. TWY P MAX wingspan 56'/7m. TWY O MAX wingspan 66'/20m. TWY Q MAX wingspan 8 /36m. While taxiing to and from RWY 09L/27R pilots will need crossing-clearance for RWY 09C/27C, which is an active VFR daytime RWY. To avoid RWY incursions pilots are referred to the published hot spots on 0-9 page OPERATION OF B747-8/8F: - B747-8/8F may only take off from and land on RWY 09L/27R. - Taxiing on TWYs and the apron is only permitted under the guidance of a Follow-me car. The following TWYs shall be used: 0-P2 - To enter RWY 27R: TWY L and TWY M; - To enter RWY 09L: TWY L and TWY G; - To exit RWY 27R: TWY H, TWY G and TWY L or TWY G and TWY L; - To exit RWY 09L: TWY M and TWY L. B747-8/8F shall be parked on stand P or PARKING INFORMATION.6.. GENERAL On stands thru 28 and 40 thru 6, except R-stands push-back required. Stands thru 20, except A-stands equipped with visual docking guidance system. For stand graphic refer to 0-9 charts.

6 , 2005, 207. ALL RIGHTS RESERVE. Printed from JeppView for Windows on 06 ec 207; Terminal chart data cycle ; Notice: After 4 ec 207, 0000Z, this chart may no longer be valid EV/HAJ 22 SEP P3. GENERAL, GERMANY.AIRPORT.BRIEFING. TWY B not available for A320, A32 and H8 ACFT. A38 and A39 ACFT are not allowed to enter RWY 09R/27L via TWY B GENERAL AVIATION All ACFT will be guided by Follow-me. MAX wingspan 66'/20m between hangar, 2 and posn MAX wingspan 56'/7m in front of hangar 3. MAX wingspan 52'/6m on other parts of apron GENERAL AVIATION 2 MAX wingspan 49'/5m GENERAL AVIATION 3 MAX wingspan 8 /36m; ACFT with wingspan over 95 /29m will be towed. 2. ARRIVAL 2.. NOISE ABATEMENT PROCEURES 2... REVERSE THRUST Between LT reverse thrust, other than idle thrust, shall only be used to an extent necessary for safety reasons CAT II/III OPERATIONS RWY 09L/27R approved for CAT II/III operations, special aircrew and ACFT certification required OTHER INFORMATION FUEL SAVING AN NOISE REUCING ILS APPROACH PROCEURES (CONTINOUS 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 conducted 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 NM will be left for intercepting the glide path in level flight. This intermediate approach segment will serve to reduce speed. Intermediate approach altitude: 2000'. 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, 5 and 0NM 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-).

7 , 2005, 205. ALL RIGHTS RESERVE. Printed from JeppView for Windows on 06 ec 207; Terminal chart data cycle ; Notice: After 4 ec 207, 0000Z, this chart may no longer be valid EV/HAJ 30 JUN P4, GERMANY.AIRPORT.BRIEFING. 3. EPARTURE 3.. E-ICING 3... GENERAL The de-icing of ACFT will take place on defined de-icing areas (Ps), exclusively. These areas are located at the Western part of the apron. e-icing on other parking positions - with the exception of the regulation described below - is not permitted E-ICING AREAS The special areas assigned for the de-icing of ACFT are designated P and P2 (see 0-9A). In exceptional cases, de-icing may take place on the positions located in between. The actual de-icing position will be assigned by the de-icing operator. The de-icing of jet-propelled ACFT will be carried out with running engines and switched off auxiliary power units (APU). The same regulation applies for ACFT types ATR 42/72 with applied propeller brakes E-ICING A de-icing operation shall be reported to the de-icing operator in good time (30 min in advance prior to OFB/CTOT) under the phone number (05) however, when obtaining start-up clearance for the engines on frequency 2.95, at the least. The order of notifications has no influence on the actual de-icing sequence. This will be determined by ground control, exclusively. After start-up clearance/push-back, ACFT will be guided by ground control to the immediate vicinity of the de-icing areas. The ACFT will then be guided by a Follow-me car to a vacant de-icing position. After parking the ACFT on the de-icing area, the pilot will report on e-icing 30.6 together with his flight number. After the de-icing process has been completed, the pilot-in-command shall report "ready to taxi" to Ground. If the engines have to be started up again, this shall be reported to ground control. uring the de-icing process, the pilot shall maintain constant listening watch on the respective de-icing frequency. When the de-icing procedure has been completed, the de-icing code will be transmitted and the ACFT handed over by the deicing operator to the ground controller. Taxiing manoeuvres from the de-icing areas may only be carried out after express clearance by the ground controller and with the absolute minimum number of engine revolutions required, only. After de-icing has taken place, the de-icing areas shall be vacated as quickly as possible after receiving taxi clearance. All special services, such as the de-icing of the undercarriage or de-icing beneath the wings, will be conducted on the pads with engines switched off, only. The hands-on check will generally only be carried out by representatives of the air transport company concerned or by a crew member of the de-iced ACFT on the respective de-icing pad. A hands-on check shall be requested by the crew through a handling agent, only. On instructions from the de-icing operator, an ACFT may be towed to another position for the hands-on check or planned for another deicing position in the pre-planning stage already. If a hands-on check becomes necessary, the control tower shall be informed in time, but at the latest when requesting startup clearance. The employees of FHG and AGS (de-icing personnel) will not carry out these checks. ifferences of the above or in published Aeroplane eicing Plan mentioned procedures have to be granted by the airport operator.

8 , 2005, 207. ALL RIGHTS RESERVE. Printed from JeppView for Windows on 06 ec 207; Terminal chart data cycle ; Notice: After 4 ec 207, 0000Z, this chart may no longer be valid EV/HAJ 30 JUN P5, GERMANY 3. EPARTURE 3.2. TAXI PROCEURES ACFT may leave nose-in positions only by the aid of ACFT tractors. Reverse thrust or variable pitch propellers shall not be used..airport.briefing NOISE ABATEMENT PROCEURES The starting points for the take-off runs of 3200m in length are located at the level of the eastern edge of TWY N for landing direction 27 and at the level of the western edge of TWY H for landing direction 09. The starting points located 300m in front of THR 09L for take-offs in an eastern direction and 300m in front of THR 27R for take-offs in a western direction may only be used by ACFT requiring a take-off run exceeding 3200m for the forthcoming take-off START-UP, PUSH-BACK & TAXI PROCEURES START-UP Pilots shall obtain start-up approval on the appropriate frequency of GROUN PUSH-BACK PROCEURE ON MAIN APRON (STANS THRU 6) To receive push-back instructions from nose-in position, pilots are requested to contact the "Walkout Assistent" after they received approval to start their engines. This request shall only be made if the pilot is able to carry out the manoeuvre without delay. The "Walkout Assistent" will carry out the push-back procedure immediately after receiving the necessary clearance from apron control. To avoid delays, the engines shall be started during push-back TAXI PROCEURE To obtain taxi-out instructions after push-back or from a roll-out stand, pilots are instructed to request taxi clearance on the appropriate frequency of GROUN OTHER INFORMATION ATALINK EPARTURE CLEARANCE (CL) Temporal parameters: ti 25 min prior to EOBT for unregulated flights. 30 min prior to CTOT for ATFM regulated flights. tt min prior to EOBT for unregulated flights. 6 min prior to CTOT for ATFM regulated flights. t 5 min.

9 Printed from JeppView for Windows on 06 ec 207; Terminal chart data cycle ; Notice: After 4 ec 207, 0000Z, this chart may no longer be valid EV/HAJ BREMEN Radar (APP) MAY 83' 0-R Alt Set: hpa (IN on request) Trans level: By ATC Trans alt: ', GERMANY.RAAR.MINIMUM.ALTITUES NM 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 (000' above the highest obstacle within a radius of 8 km) and airspace structure (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 between AIRAC date NOV and AIRAC date MAR in order to meet required obstacle clearance at cold temperatures. COPENHAGEN EKK FIR (G) SWEEN ESAA FIR (G) NM BREMEN EWW FIR NM ALTITUE NOT PUBLISHE WUNSTORF WUN NB 265' 80NM 20NM ' NM Hannover BREMEN EWW FIR 2000 (200) 40NM 376' 3047' HW NB NIENBURG NIE VOR BUCKEBURG BYC NB 262' HA NB LEINE LE VOR ME 2474' ! " MUNICH EMM FIR LANGEN EGG FIR 3393' 2500 (2800) ' 80NM 2377' ! 2000 " ' 2933' ' CHANGES: Sectors & altitudes revised & established. 48' CELLE CEL NB BRAUN- SCHWEIG BRU NB 3 4 CONTOUR INTERVALS 20NM 900 (2200) 2500 (2600) 2800 () (300) (2400) (2200) 3052' 60 NM, 2005, 20. ALL RIGHTS RESERVE.

10 CHANGES: Chart reindexed; procedures renumbered & revised; coordinates., 207. ALL RIGHTS RESERVE. Printed from JeppView for Windows on 06 ec 207; Terminal chart data cycle ; Notice: After 4 ec 207, 0000Z, this chart may no longer be valid EV/HAJ *-ATIS JAN Alt Set: hpa (IN on request) 83' Trans level: By ATC Trans alt: '.Eff.2.Feb. ELNAT 4P [ELNA4P] 2, GITEX 4P [GITE4P] RWYS 27L/R ARRIVALS ELNAT 2R [ELNA2R] 2, GITEX 4R [GITE4R] RWYS 09L/R ARRIVALS, GERMANY.STAR. 200' MSA HW NB within 5 NM 4 CAUTION Intensive glider activities to be expected in the surrounding area of CEL. SPEE RESTRICTION MAX 250 KT below FL00 or as by ATC. Not applicable within airspace C. NIE NIENBURG 6.5 NIE N E R87^ (IAF Rwys 09L/R) ROBEG (WRB R-006/44.0) 87^ ^ N E ^ 268^ R85^ 8.9 R2^ CELLE 4 3 CEL N E LEINE LE (IAF Rwys 27L/R) 5.2 LE N E LE 244^ 7.3 HLZ NOT TO SCALE hlz 007^ 5.0 LE 5.0 GITEX 4R GITEX 4P ^ 30^ GITEX (7.3 HLZ R-203/24) 23 NORTA (34 WRB) 343^ TOLTA WARBURG 3.7 WRB N E ELNAT 2R ^ ELNAT ^ 3 005^ ELNAT 4P WERRA BRNAV equipment necessary. 2 Only for flights with requested FL above FL Between ELNAT & NORTA BRNAV equipment necessary. VERTICAL PLANNING INFORMATION Pilots should plan for possible descent clearance as follows: ELNAT 4P, GITEX 4P: at or below FL80 by LE. ELNAT 2R, GITEX 4R: at or below FL80 by ROBEG. ACTUAL ESCENT CLEARANCE AS IRECTE BY ATC.

11 Printed from JeppView for Windows on 06 ec 207; Terminal chart data cycle ; Notice: After 4 ec 207, 0000Z, this chart may no longer be valid EV/HAJ *-ATIS ' 0-2A Alt Set: hpa (IN on request) 83' Trans level: By ATC Trans alt: ' MSA HW NB within 5 NM 27 JAN 7.Eff.2.Feb. HEHLINGEN 6P (HLZ 6P) RWYS 27L/R ARRIVAL HEHLINGEN 6R (HLZ 6R) RWYS 09L/R ARRIVAL, GERMANY.STAR. LOST COMMS LOST COMMS LOST COMMS LOST COMMS In case of radio communication failure proceed to: HLZ 6R: NIE. COMMS LOST COMMS LOST COMMS LOST COMMS LOST SPEE RESTRICTION MAX 250 KT below FL00 or as by ATC. Not applicable within airspace C ^ HLZ 6P, 6R HLZ 6R: Clearance limit is CEL. 2 CAUTION Intensive glider activities to be expected in the surrounding area of CEL. 2 8^ 00^ N E N E HEHLINGEN 7.3 HLZ (IAF Rwys 27L/R) CELLE 3 CEL N E ^ 257^ 093^ 24 HLZ 6R 273^ (IAF Rwys 09L/R) NIENBURG 6.5 NIE N E VERTICAL PLANNING INFORMATION Pilots should plan for possible descent clearance as follows: HLZ 6P: at or below FL20 by HLZ, at or below FL70 by CEL. HLZ 6R: at or below FL0 by CEL. NOT TO SCALE at or below FL80 by NIE. ACTUAL ESCENT CLEARANCE AS IRECTE BY ATC. CHANGES: Chart reindexed; STARs renumbered; OSN STARs withdrawn., 207. ALL RIGHTS RESERVE.

12 CHANGES: Chart reindexed; STARs renumbered & withdrawn; coordinates., 207. ALL RIGHTS RESERVE. Printed from JeppView for Windows on 06 ec 207; Terminal chart data cycle ; Notice: After 4 ec 207, 0000Z, this chart may no longer be valid EV/HAJ *-ATIS JAN 7 0-2B Alt Set: hpa (IN on request) 83' Trans level: By ATC Trans alt: ' WARBURG 7P (WRB 7P) RWYS 27L/R ARRIVAL WARBURG 5R (WRB 5R) RWYS 09L/R ARRIVAL.Eff.2.Feb., GERMANY.STAR. 200' MSA HW NB within 5 NM NIE NIENBURG 6.5 NIE N E CELLE 3 CEL N E HW N E NOT TO SCALE (IAF Rwys 09L/R) ROBEG 007^ R87^ ^ 6.0 LE 268^ 088^ R20^ LEINE LE (IAF Rwys 27L/R) 5.2 LE N E WRB 5R UMKUK CAUTION Intensive glider activities to be expected in the surrounding area of CEL. 030^ 006^ 7 WRB 7P WARBURG 3.7 WRB N E SPEE RESTRICTION MAX 250 KT below FL00 or as by ATC. Not applicable within airspace C. VERTICAL PLANNING INFORMATION Pilots should plan for possible descent clearance as follows: at or below FL80 by LE. at or below FL80 by ROBEG. WRB 7P: WRB 5R: ACTUAL ESCENT CLEARANCE AS IRECTE BY ATC.

13 CHANGES: Chart reindexed; STAR WERRA R renumbered 2R; coordinates., 207. ALL RIGHTS RESERVE. Printed from JeppView for Windows on 06 ec 207; Terminal chart data cycle ; Notice: After 4 ec 207, 0000Z, this chart may no longer be valid EV/HAJ *-ATIS JAN 7 0-2C Alt Set: hpa (IN on request) 83' Trans level: By ATC Trans alt: ' WERRA P [WERAP] RWYS 27L/R ARRIVAL WERRA 2R [WERA2R] RWYS 09L/R ARRIVAL.Eff.2.Feb. 2 2, GERMANY.STAR. 200' MSA HW NB within 5 NM NIE 006^ R87^ 44 4 NIENBURG 6.5 NIE N E ^ 87^ CAUTION Intensive glider activities to be expected in the surrounding area of CEL. (IAF Rwys 09L/R) ROBEG ^ N E ^ 268^ R85^ LE CELLE 4 3 CEL N E LEINE LE (IAF Rwys 27L/R) 5.2 LE N E SPEE RESTRICTION MAX 250 KT below FL00 or as by ATC. Not applicable within airspace C NOT TO SCALE ^ TOLTA WARBURG 3.7 WRB N E WERRA 2R 5.5 (34 WRB) 325^ NORTA 24. WERRA 3 005^ WERRA P BRNAV equipment necessary. 2 Only for flights with requested FL below FL Between WERRA & NORTA BRNAV equipment necessary. VERTICAL PLANNING INFORMATION Pilots should plan for possible descent clearance as follows: WERRA P: at or below FL80 by LE. WERRA 2R: at or below FL80 by ROBEG. ACTUAL ESCENT CLEARANCE AS IRECTE BY ATC.

14 Printed from JeppView for Windows on 06 ec 207; Terminal chart data cycle ; Notice: After 4 ec 207, 0000Z, this chart may no longer be valid EV/HAJ *-ATIS ' SPEE RESTRICTION CEL (FL0-; K250-) - V460 (K220-) - V465 - ESIM ('+; K70+). RWY ROUTING 09L TRANSITION CEL 09L MAX 250 KT below FL00 or as by ATC. Not applicable within airspace C. CEL (FL0-; K250-) - V460 (K220-) - V465 - PIXEL ('+; K70+). CEL 09R 09R 83' NIE (FL80-; K250-) - V400 (K220-) - V460 - V465 - ESIM ('+; K70+). 09L NIE 09L MSA HW NB within 5 NM CAUTION Intensive glider activities to be expected in the surrounding area of CEL. NIE (FL80-; K250-) - V400 (K220-) - V460 - V465 - PIXEL ('+; K70+). NIE 09R 09R, GERMANY 0-2.Eff.2.Feb..RNAV.TRANSITION. Alt Set: hpa (IN on request) Trans level: By ATC Trans alt ' CELLE 3 CEL V4~~ 8^ 27 JAN 7 N E FL0 MAX 250 KT At or below FL0 V46~ ^. MAINTAIN transition track beyond end point, if no suceeding instruction (vector) is received. 2. Below FL00 clearance to altitude (QNH) above transition level may be issued. 3. If cleared for a "L" transition to final approach EXPECT instrument approach to RWY ~9L. 4. If cleared for a "R" transition to final approach EXPECT instrument approach to RWY ~9R. CEL ~9L, CEL ~9R Clearance limit MAX 220 KT Clearance limit NIENBURG 6.5 NIE N E At or below FL80 077^ 257^ CEL ~9L, ~9R NIE ~9L, ~9R 250 KT MAX 260^ KT MAX 80^ 4.4 V463 V464 V465 V46 V462 CEL ~9L, ~9R GPS- OR FMS-EQUIPPE AIRCRAFT BY ATC N E ^ [CEL~9] NIE ~9L, NIE ~9R [NIE~9] RNAV TRANSITIONS V475 V474 V473 V472 V49 V49~ PIXEL (FAF) COMMS LOST LOST COMMS LOST COMMS LOST COMMS LOST COMMS At or above ' Minimum 70 KT (FAF) LOST COMMS Before V465 NOT TO SCALE Continue transition until V465, turn RIGHT to NIE; alignment turn, follow standard instrument approach. MAX 220 KT. ESIM Beyond V465 At or above ' Minimum 70 KT LOST Turn RIGHT to NIE, alignment turn, follow standard instrument approach. MAX 220 KT. COMMS LOST COMMS LOST COMMS LOST COMMS LOST COMMS LOST CHANGES: Chart reindexed; procedures revised; coordinates. COMMS LOST COMMS, 207. ALL RIGHTS RESERVE.

15 Printed from JeppView for Windows on 06 ec 207; Terminal chart data cycle ; Notice: After 4 ec 207, 0000Z, this chart may no longer be valid EV/HAJ *-ATIS ' SPEE RESTRICTION CEL (FL70-; K250-) - V500 - V50 (K220-) - V502 - V565 - OINI ('+; K70+). RWY ROUTING 27L TRANSITION CEL 27L CHANGES: MAX 250 KT below FL00 or as by ATC. Not applicable within airspace C. CEL (FL70-; K250-) - V500 - V50 (K220-) - V502 - V565 - XAVER ('+; K70+). CEL 27R 27R 83' CAUTION 2 NIE (FL0-; K250-) - V502 (K220-) - V565 - OINI ('+; K70+). NIE 27L 27L NIE 27R 27R MSA HW NB within 5 NM Intensive glider activities to be expected in the surrounding area of CEL. NIE (FL0-; K250-) - V502 (K220-) - V565 - XAVER ('+; K70+). GPS- OR FMS-EQUIPPE AIRCRAFT BY ATC, GERMANY 0-2E.Eff.2.Feb..RNAV.TRANSITION. Alt Set: hpa (IN on request) Trans level: By ATC Trans alt '. MAINTAIN transition track beyond end point, if no succeeding instruction (vector) is received. 2. Below FL 00 clearance to altitude (QNH) above transition level may be issued. 3. If cleared for a "L" transition to final approach EXPECT instrument approach to RWY 27L. 4. If cleared for a "R" transition to final approach EXPECT instrument approach to RWY 27R. V5~ V5~~ 8^ CELLE 3 CEL 2 Clearance limit 00^ ^ MAX 220 KT 27 JAN 7 N E FL70 MAX 250 KT 80^ 08^ At or below 285^ 4.2 V565 V564 V563 V562 V56 V56~ NIE 27L, 27R Chart reindexed; procedures revised; coordinates. CEL 27L, CEL 27R NIE 27L, NIE 27R [CEL27] [NIE27] RNAV TRANSITIONS 077^ 257^ CEL 27L, 27R ^ V5~2 Clearance limit NIENBURG 6.5 NIE N E NIE 27L, 27R At or below 220 KT MAX FL0 250 KT MAX V59 V572 V573 V574 V575 V59~ OINI (FAF) N E (FAF) At or above ' Minimum 70 KT XAVER At or above ' Minimum 70 KT LOST COMMS COMMS LOST LOST COMMS LOST COMMS LOST COMMS LOST COMMS Before V565 Continue transition until V565, turn LEFT to CEL; alignment turn, follow standard instrument approach. MAX 220 KT. COMMS Beyond V565 LOST Turn LEFT to CEL, alignment turn, follow standard instrument approach. MAX 220 KT. LOST NOT TO SCALE COMMS LOST COMMS LOST COMMS LOST COMMS LOST COMMS LOSTCOMMS, 207. ALL RIGHTS RESERVE.

16 Printed from JeppView for Windows on 06 ec 207; Terminal chart data cycle ; Notice: After 4 ec 207, 0000Z, this chart may no longer be valid EV/HAJ 27 JAN 7, GERMANY 0-2F.Eff.2.Feb..RNAV.TRANSITION. *-ATIS ' Alt Set: hpa (IN on request) Trans level: By ATC Trans alt '. MAINTAIN transition track beyond end point, if no succeeding instruction (vector) is received. 2. Below FL00 clearance to altitude (QNH) above transition level may be issued. 3. If cleared for a "L" transition to final approach EXPECT instrument approach to RWY 27L. 4. If cleared for a "R" transition to final approach EXPECT instrument approach to RWY 27R. LE 27L, LE 27R [LE27] RNAV TRANSITIONS GPS- OR FMS-EQUIPPE AIRCRAFT BY ATC 200' MSA HW NB within 5 NM N E XAVER At or above ' Minimum 70 KT V59 V59~ (FAF) (FAF) OINI At or above ' Minimum 70 KT V572 V573 V574 V575 V ^ 5.6 V582 MAX 220 KT V583 V584 V ^ 268^ 00^ Clearance limit LEINE LE 5.2 LE N E At or below FL80 MAX 250 KT LOST COMMS LOST COMMS Before V585 LOST COMMS Beyond V585 SPEE RESTRICTION MAX 250 KT below FL00 or as by ATC. Not applicable within airspace C. LOST COMMS LOST COMMS LOST COMMS Continue transition until V585, turn RIGHT to LE; alignment turn, follow standard instrument approach. MAX 220 KT. Turn RIGHT to LE, alignment turn, follow standard instrument approach. MAX 220 KT. NOT TO SCALE LOST COMMS LOST COMMS LOST COMMS LOST COMMS LOST COMMS LOST COMMS LOST COMMS TRANSITION RWY LE 27L 27L LE 27R 27R ROUTING LE (FL80-; K250-) - V58 - V582 (K220-) - V585 - OINI ('+; K70+). LE (FL80-; K250-) - V58 - V582 (K220-) - V585 - XAVER ('+; K70+). CHANGES: Chart reindexed; procedures revised; coordinates., 207. ALL RIGHTS RESERVE.

17 Printed from JeppView for Windows on 06 ec 207; Terminal chart data cycle ; Notice: After 4 ec 207, 0000Z, this chart may no longer be valid EV/HAJ *-ATIS ' 27 JAN 7 ROBEG ~9L, ROBEG ~9R [ROBE~9] RNAV TRANSITIONS GPS- OR FMS-EQUIPPE AIRCRAFT BY ATC, GERMANY 0-2G.Eff.2.Feb..RNAV.TRANSITION. Alt Set: hpa (IN on request) Trans level: By ATC Trans alt '. MAINTAIN transition track beyond end point, if no succeeding instruction (vector) is received. 2. Below FL00 clearance to altitude (QNH) above transition level may be issued. 3. If cleared for a "L" transition to final approach EXPECT instrument approach to RWY ~9L. 4. If cleared for a "R" transition to final approach EXPECT instrument approach to RWY ~9R. (FAF) ESIM At or above ' Minimum 70 KT V475 V474 V473 V49 200' MSA HW NB within 5 NM HW N E V485 V484 V483 V V482 MAX 220 KT 270^ 6.0 V48 360^ V49~ (FAF) PIXEL At or above ' Minimum 70 KT Clearance limit ROBEG At or below MAX 250 KT At or below FL80 060^ 87^ 6.6 V48~ 007^ SPEE RESTRICTION MAX 250 KT below FL00 or as by ATC. Not applicable within airspace C. NOT TO SCALE LOST COMMS COMMS LOST COMMS LOST COMMS Before V485 Beyond V485 LOST COMMS LOST COMMS LOST COMMS LOST COMMS LOST COMMS LOST COMMS LOST LOST COMMS Continue transition until V485, turn LEFT to ROBEG; alignment turn, follow standard instrument approach. MAX 220 KT. Turn LEFT to ROBEG, alignment turn, follow standard instrument approach. MAX 220 KT. COMMS LOST COMMS LOST TRANSITION ROBEG ~9L ROBEG ~9R CHANGES: RWY 09L 09R ROBEG (FL80-; K250-) - V480 - V48 - V482 (K220-) - V485 - ESIM ('+; K70+). ROBEG (FL80-; K250-) - V480 - V48 - V482 (K220-) - V485 - PIXEL ('+; K70+). Chart reindexed; procedure revised; coordinates. ROUTING, 207. ALL RIGHTS RESERVE.

18 Printed from JeppView for Windows on 06 ec 207; Terminal chart data cycle ; Notice: After 4 ec 207, 0000Z, this chart may no longer be valid EV/HAJ *-ATIS ' 27 JAN 7 FLY THE TRANSITION AS CONTINUOUS ESCENT OPERATION (CO) GPS- OR FMS-EQUIPPE AIRCRAFT BY ATC, GERMANY 0-2H.Eff.2.Feb..RNAV.TRANSITION. Alt Set: hpa (IN on request) Trans level: By ATC Trans alt ' When cleared for "Transition and Profile" aim for a low noise continuous descent operation (CO) within the constraints as laid down in the procedure description. ESTA 3A [ESTA3A], ESTA 3E [ESTA3E] OBATU 3A [OBAT3A], OBATU 3E [OBAT3E] RNAV TRANSITIONS 200' MSA HW NB within 5 NM SPEE RESTRICTION MAX 250 KT below FL00 or as by ATC. Not applicable within airspace C. V463 V ^ 80^ ESTA 3A, 3E 4.0 V ^ 3. ESTA ^ At or above FL240 3 By ATC By ATC 44.4 OBATU 3A, 3E V49 V49~ NOT TO SCALE HW N E OBATU At or above FL ^ (FAF) PIXEL At or above ' Minimum 70 KT (FAF) 3 ESIM At or above ' Minimum 70 KT ESTA 3A, OBATU 3A 2 ESTA 3E, OBATU 3E TRANSITION ESTA 3A ESTA 3E OBATU 3A OBATU 3E RWY 09L 09R 09L 09R ESTA (FL240+) - V463 - V473 - V472 - ESIM ('+; K70+). ESTA (FL240+) - V463 - V473 - V472 - PIXEL ('+; K70+). OBATU (FL200+) - V463 - V473 - V472 - ESIM ('+; K70+). OBATU (FL200+) - V463 - V473 - V472 - PIXEL ('+; K70+). CHANGES: Chart reindexed; procedures renumbered; coordinates. ROUTING, 207. ALL RIGHTS RESERVE.

19 Printed from JeppView for Windows on 06 ec 207; Terminal chart data cycle ; Notice: After 4 ec 207, 0000Z, this chart may no longer be valid EV/HAJ 27 JAN 7, GERMANY 0-2J.Eff.2.Feb..RNAV.TRANSITION. *-ATIS ' Alt Set: hpa (IN on request) Trans level: By ATC Trans alt ' When cleared for "Transition and Profile" aim for a low noise continuous descent operation (CO) within the constraints as laid down in the procedure description. FLY THE TRANSITION AS CONTINUOUS ESCENT OPERATION (CO) GPS- OR FMS-EQUIPPE AIRCRAFT BY ATC TRANSITION RWY ROUTING 09L 09R 83' MSA HW NB within 5 NM 292^ HEHLINGEN HLZ 7.3 N E HLZ A, HLZ E RNAV TRANSITIONS 25.0 HLZ A, E V462 V49 V472 V49~ V563 27^ HLZ A HLZ E HLZ - V563 - V462 - V472 - ESIM ('+; K70+). HLZ - V563 - V462 - V472 - PIXEL ('+; K70+) By ATC ^ By ATC 096^ (FAF) PIXEL At or above ' Minimum 70 KT 083^ HLZ A 3. 2 HLZ E (FAF) 3 ESIM ' Minimum 70 KT At or above NOT TO SCALE SPEE RESTRICTION MAX 250 KT below FL00 or as by ATC. Not applicable within airspace C. CHANGES: STARs transferred; RNAV transitions established., 207. ALL RIGHTS RESERVE.

20 2 Printed from JeppView for Windows on 06 ec 207; Terminal chart data cycle ; Notice: After 4 ec 207, 0000Z, this chart may no longer be valid EV/HAJ *-ATIS ' 83' MSA HW NB within 5 NM 27 JAN 7, GERMANY 0-2K.Eff.2.Feb..RNAV.TRANSITION. Alt Set: hpa (IN on request) Trans level: By ATC Trans alt ' When cleared for "Transition and Profile" aim for a low noise continuous descent operation (CO) within the constraints as laid down in the procedure description. HLZ 3, HLZ 3L OBATU 3 [OBAT3], OBATU 3L [OBAT3L] RNAV TRANSITIONS FLY THE TRANSITION AS CONTINUOUS ESCENT OPERATION (CO) GPS- OR FMS-EQUIPPE AIRCRAFT BY ATC 280^ 23.8 HLZ 3, 3L 2 XAVER ' Minimum 70 KT At or above 276^ 4.3 V ^ 3.9 V59~ 265^ OINI V572 V573 OBATU HLZ 7.3 HEHLINGEN N E ^ 8. OBATU 3, 3L HLZ 3L, OBATU 3L HLZ 3, OBATU 3 SPEE RESTRICTION MAX 250 KT below FL00 or as by ATC. Not applicable within airspace C. (FAF) By ATC ^ 3. 27^ By ATC N E (FAF) ' Minimum 70 KT At or above TRANSITION HLZ 3 HLZ 3L 27R OBATU 3 OBATU 3L RWY ROUTING 27L 27L 27R HLZ (FL20+) - V573 - V572 - OINI ('+; K70+). HLZ (FL20+) - V573 - V572 - XAVER ('+; K70+). OBATU (FL0+) - V573 - V572 - OINI ('+; K70+). OBATU (FL0+) - V573 - V572 - XAVER ('+; K70+). At or above FL0 NOT TO SCALE At or above FL20 CHANGES: Chart reindexed; procedures renumbered & revised; coordinates., 207. ALL RIGHTS RESERVE.

21 Printed from JeppView for Windows on 06 ec 207; Terminal chart data cycle ; Notice: After 4 ec 207, 0000Z, this chart may no longer be valid EV/HAJ *-ATIS ' 27 JAN 7 FLY THE TRANSITION AS CONTINUOUS ESCENT OPERATION (CO) GPS- OR FMS-EQUIPPE AIRCRAFT BY ATC, GERMANY 0-2L.Eff.2.Feb..RNAV.TRANSITION. Alt Set: hpa (IN on request) Trans level: By ATC Trans alt ' When cleared for "Transition and Profile" aim for a low noise continuous descent operation (CO) within the constraints as laid down in the procedure description. KUGAV 3A [KUGA3A], KUGAV 3E [KUGA3E] TOLTA 3A [TOLT3A], TOLTA 3E [TOLT3E] WRB 3A, WRB 3E RNAV TRANSITIONS 200' MSA HW NB within 5 NM KUGAV At or above FL20 080^ 22.7 KUGAV 3A, 3E NOT TO SCALE V473 V ^ V472 (FAF) ESIM At or above ' Minimum 70 KT 083^ ^ By ATC By ATC PIXEL At or above ' Minimum 70 KT V49 (FAF) V49~ N E WARBURG WRB 3.7 WRB N E At or above FL200 WRB 3A, 3E 002^ TOLTA 3A, 3E 346^ 343^ 34.0 ROBEG At or above FL90 TOLTA At or above FL200 SPEE RESTRICTION MAX 250 KT below FL00 or as by ATC. Not applicable within airspace C. KUGAV 3A, TOLTA 3A, WRB 3A 2 KUGAV 3E, TOLTA 3E, WRB 3E TRANSITION KUGAV 3A KUGAV 3E TOLTA 3A TOLTA 3E WRB 3A WRB 3E RWY 09L 09R 09L 09R 09L 09R KUGAV (FL20+) - V473 - V472 - ESIM ('+; K70+). KUGAV (FL20+) - V473 - V472 - PIXEL ('+; K70+). TOLTA (FL200+) - ROBEG (FL90+) - V483 - V473 - V472 - ESIM ('+; K70+). TOLTA (FL200+) - ROBEG (FL90+) - V483 - V473 - V472 - PIXEL ('+; K70+). WRB (FL200+) - V483 - V473 - V472 - ESIM ('+; K70+). WRB (FL200+) - V483 - V473 - V472 - PIXEL ('+; K70+). CHANGES: Chart reindexed; procedures renumbered & revised; coordinates. ROUTING, 207. ALL RIGHTS RESERVE.

22 2 Printed from JeppView for Windows on 06 ec 207; Terminal chart data cycle ; Notice: After 4 ec 207, 0000Z, this chart may no longer be valid EV/HAJ *-ATIS ' 83' MSA HW NB within 5 NM 27 JAN 7, GERMANY 0-2M.Eff.2.Feb..RNAV.TRANSITION. Alt Set: hpa (IN on request) Trans level: By ATC Trans alt ' When cleared for "Transition and Profile" aim for a low noise continuous descent operation (CO) within the constraints as laid down in the procedure description. UPAT 3 [UPA3], UPAT 3L [UPA3L] VISKI 3 [VISK3], VISKI 3L [VISK3L] RNAV TRANSITIONS FLY THE TRANSITION AS CONTINUOUS ESCENT OPERATION (CO) GPS- OR FMS-EQUIPPE AIRCRAFT BY ATC 5.0 8^ ^ ^ VISKI XAVER 50.0 VISKI 3, 3L 276^ 4.3 V V59~ 265^ OINI V563 V572 UPAT By ATC ^ 3. 27^ By ATC 2 At or above FL220 N E UPAT 3L, VISKI 3L UPAT 3, VISKI 3 (FAF) ' Minimum 70 KT At or above (FAF) ' Minimum 70 KT At or above TRANSITION UPAT 3 UPAT 3L VISKI 3 VISKI 3L 27L 27R 27L 27R VISKI (FL220+) - V563 - V573 - V572 - OINI ('+; K70+). VISKI (FL220+) - V563 - V573 - V572 - XAVER ('+; K70+). V573 V57 At or above FL50 UPAT 3, 3L SPEE RESTRICTION MAX 250 KT below FL00 or as by ATC. Not applicable within airspace C. NOT TO SCALE RWY ROUTING UPAT (FL50+) - V57 - V573 - V572 - OINI ('+; K70+). UPAT (FL50+) - V57 - V573 - V572 - XAVER ('+; K70+). CHANGES: Chart reindexed; procedures renumbered & revised; coordinates., 207. ALL RIGHTS RESERVE.

23 CHANGES: Reissue., 207. ALL RIGHTS RESERVE. Printed from JeppView for Windows on 06 ec 207; Terminal chart data cycle ; Notice: After 4 ec 207, 0000Z, this chart may no longer be valid EV/HAJ BREMEN Radar ' MSA ARP 24 FEB Trans level: By ATC Trans alt: '. RNAV- or RNP- or A-RNP equivalent. 2. GPS required. 3. ME/ME, ME/ME/IRU not authorized., GERMANY 4. Contact BREMEN Radar IMMEIATELY after take-off. 5. SIs are also noise abatement procedures. Strict adherence within the limits of aircraft performance is mandatory. VAXEV W [VAXEW] VAXEV X [VAXEX] RNAV EPARTURES BY ATC.RNAV.SI. NOT TO SCALE SPEE RESTRICTION MAX 250 KT below FL00 or as by ATC. Not applicable within airspace C. V26 VAXEV W At or above 3200' VAXEV X At or above 3300' V262 VAXEV X ^ 237^ VAXEV W 0.7 VAXEV V26~ VAXEV W At or above 2300' MAX 20 KT These SIs require minimum climb gradients of VAXEV X: VAXEV W: 2.0% until passing ' due to airspace structure. 9.0% until passing ' due to airspace structure. Gnd speed-kt VAXEV X At or above 2200' MAX 200 KT 9.0% V/V (fpm) % V/V (fpm) If unable to comply advise Tower as soon as possbile. Initial climb clearance ' SI RWY ROUTING VAXEV W VAXEV X 27L 27R Cimb on 270^ track to 600', turn RIGHT direct to V26~, to V26, to V262, to VAXEV.

24 Printed from JeppView for Windows on 06 ec 207; Terminal chart data cycle ; Notice: After 4 ec 207, 0000Z, this chart may no longer be valid EV/HAJ BREMEN Radar ' 27 JAN 7 0-3B Trans level: By ATC Trans alt: '. 2..Eff.2.Feb., GERMANY Contact BREMEN Radar IMMEIATELY after take-off. SIs are also noise abatement procedures. Strict adherence within the limits of aircraft performance is mandatory. CELLE 8F (CEL 8F) CELLE 9G (CEL 9G) CELLE 6S (CEL 6S) CELLE 6Y (CEL 6Y) EPARTURES 200' MSA HW Lctr within 5 NM.SI. NIE NIENBURG 6.5 NIE N E SPEE RESTRICTION MAX 250 KT below FL00 or as by ATC. Not applicable within airspace C. 3 CELLE CEL N E ^ R34^ R35^ 4.2 HB (20^ BRG to HW) 357^ N E At HA 2.0 ME/ NIE R-32 or 600' whichever is later At 087^ 34^ CEL 8F HB 0.5 ME HA 2.0 ME ME HA N E HA 4.5 HB HA 2.0 ME CEL 6S 35^ HB 0.5 ME/ HA 2.0 ME or 600' whichever is later (NIE R-32) (3.95) HA 270^ 09^ 270^ 4 CEL 6Y CEL 9G ME HB (6.9) HB N E HA 320 HA N E HA 5.4 HB HA 8.8 HB HB 8.4 ME HA 7.2 ME 023^ NOT TO SCALE These SIs require minimum climb gradients of CEL 8F: 550' per NM (9.0%) until passing 3500' due to airspace structure. CEL 6S: 730' per NM (2.0%) until passing ' due to airspace structure. SI CEL 8F CEL 9G CEL 6S CEL 6Y RWY 27L 09R 27R 09L Initial climb clearance ' ROUTING After passing NIE R-8 B-RNAV equipment necessary. CHANGES: Gnd speed-kt ' per NM ' per NM If unable to comply advise Tower as soon as possible. Climb straight ahead to 0.5 ME WEST of HB/HA 2.0 ME or 600', whichever is later, turn RIGHT, intercept NIE R-35 inbound to 4.2 HB/20^ bearing to HW, turn RIGHT, 357^ track, when passing NIE R-8 turn RIGHT, intercept 087^ bearing to CEL. Climb straight ahead to HB 8.4 ME/HA 7.2 ME, turn LEFT, intercept 023^ bearing to CEL. Climb straight ahead to HA 2.0 ME/NIE R-32 or 600', whichever is later, turn RIGHT, intercept NIE R-34 inbound to 5.2 HA/4.5 HB, turn RIGHT, 357^ track, when passing NIE R-8 turn RIGHT, intercept 087^ bearing to CEL. Climb straight ahead to 7.5 HA/8.8 HBO, turn LEFT, intercept 023^ bearing to CEL. SIs renumbered & revised; coordinates; chart reindexed., 207. ALL RIGHTS RESERVE.

25 CHANGES: SIs withdrawn, transferred, renumbered & revised; coordinates., 207 ALL RIGHTS RESERVE. Printed from JeppView for Windows on 06 ec 207; Terminal chart data cycle ; Notice: After 4 ec 207, 0000Z, this chart may no longer be valid EV/HAJ BREMEN Radar These SIs require minimum climb gradients of 200' 550' per NM (9.0%) until passing 3500' due MULO 8F: to airspace structure. If unable to comply advise Tower as soon as possible. 83' 05^ 8^ MSA HW Lctr within 5 NM MULO 6G: 230' per NM (3.8%) until passing 2500' due to airspace structure. If unable to comply advise ATC upon start-up. MULO 6S: 730' per NM (2.0%) until passing ' due to airspace structure. If unable to comply advise Tower as soon as possible. (3.95) HA N E ME HA NIENBURG 6.5 NIE N E HA N E Trans level: By ATC Trans alt: '. Contact BREMEN Radar IMMEIATELY after take-off. 2. SIs are also noise abatement procedures. Strict adherence within the limits of aircraft performance is mandatory. Gnd speed-kt HA 5.4 HB 5.2 HA 4.5 HB 357^ R34^ 550' per NM OKOK R35^ 730' per NM HB 230' per NM HA 2.0 ME (NIE R-32) 27 JAN HLZ 29 34^ 0-3C ^ MULO 6S (20^ BRG to HW) MULO 5Y MULO 8 270^ 270^ 35^ MULO 6G MULO 8F N E N E HEHLINGEN 7.3 HLZ 094^ 6.5 PIGIR 0 R285^ (MULO 6G) 4.7 ME HB HB 0.5 ME HA 2.0 ME HA 2.0 ME/ NIE R-32 At or 600' whichever is later.eff.2.feb. MULO 8F MULO 6G MULO 6S MULO 5Y EPARTURES (MULO 5Y) 6.NM TO MULO 6.5NM TO MULO (6.9) HB N E SPEE RESTRICTION MAX 250 KT below FL00 or as by ATC. Not applicable within airspace C. HB 0.5 ME/ HA 2.0 ME At or 600' whichever is later, GERMANY NOT TO SCALE Initial climb clearance ' SI RWY ROUTING Climb straight ahead to 0.5 ME WEST of HB/HA 2.0 ME or 600', whichever is later, turn RIGHT, intercept NIE R-35 inbound to 4.2 HB/20^ bearing to HW, turn RIGHT, 357^ track, when passing NIE R-8 turn RIGHT, intercept HLZ R-285 inbound via OKOK to MULO. 27L MULO 8F Climb straight ahead to PIGIR, turn RIGHT, 094^ track MULO. 09R 27R MULO 6G MULO 6S Climb straight ahead to HA 2.0 ME/NIE R-32 or 600', whichever is later, turn RIGHT, intercept NIE R-34 inbound to 5.2 HA/4.5 HB, turn RIGHT, 357^ track, when passing NIE R-8 turn RIGHT, intercept HLZ R-285 inbound via OKOK to MULO..SI. To HA, turn RIGHT, 094^ bearing to MULO. 09L After passing 2500' B-RNAV equipment necessary. MULO 5Y

26 CHANGES: NIE SIs renumbered & revised; coordinates; chart reindexed., 207. ALL RIGHTS RESERVE. Printed from JeppView for Windows on 06 ec 207; Terminal chart data cycle ; Notice: After 4 ec 207, 0000Z, this chart may no longer be valid EV/HAJ BREMEN Radar NIE NIENBURG 6.5 NIE 83' N E JAN Eff.2.Feb. Trans level: By ATC Trans alt: '. Contact BREMEN Radar immediately after take-off. 2. SIs are also noise abatement procedures. Strict adherence within the limits of aircraft performance is mandatory. NIENBURG 7F (NIE 7F) NIENBURG 7G (NIE 7G) NIENBURG 9S (NIE 9S) NIENBURG Y (NIE Y) EPARTURES, GERMANY 200' MSA HW Lctr within 5 NM SPEE RESTRICTION MAX 250 KT below FL00 or as by ATC. Not applicable within airspace C..SI. R35^ R3^ R5^ NIE Y ME HA (3.95) HA N E NOT TO SCALE R34^ NIE 9S 34^ N E At NIE 7F HA 2.0 ME/ NIE R-32 or 600' whichever is later At NIE 7G 35^ HB 0.5 ME/ HA 2.0 ME or 600' whichever is later HA 2.0 ME (NIE R-32) 270^ 270^ HB 0.5 ME HA 2.0 ME 293^ 295^ HA.6 ME HB 2.9 ME HB 3. ME HA 2.0 ME ME HB (6.9) HB N E At HA.6 ME/ HB 2.9 ME or 600' whichever is later At HB 3. ME/ HA 2.0 ME or 600' whichever is later These SIs require minimum climb gradients Gnd speed-kt of NIE 7F: 550' per NM (9.0%) until passing 3500' 550' per NM NIE 9S: due to airspace structure. 730' per NM (2.0%) until passing ' 730' per NM due to airspace structure. If unable to comply advise Tower as soon as possible. Initial climb clearance ' SI RWY ROUTING NIE 7F 27L Climb straight ahead to 0.5 ME WEST of HB/HA 2.0 ME or 600', whichever is later, turn RIGHT, intercept NIE R-35 inbound to NIE. NIE 7G 09R Climb straight ahead to HB 3. ME/HA 2.0 ME or 600', whichever is later, turn LEFT, intercept NIE R-5 inbound to NIE. NIE 9S 27R Climb straight ahead to HA 2.0 ME/NIE R-32 or 600', whichever is later, turn RIGHT, intercept NIE R-34 inbound to NIE. NIE Y 09L Climb straight ahead to HA.6 ME/HB 2.9 ME or 600', whichever is later, turn LEFT, intercept NIE R-3 inbound to NIE.