October 24, 2006 Rev. 4, December 11, 2007 ASB-MBB-BK117-60-121 Page 1 of 17 1. PLANNING 1.A. Effectivity 1.A.1. Helicopters affected: All MBB-BK117 C-1 with Turbomeca engine Arriel 1E2. 1.A.2. Components affected: FCU without modification TU 358 by Turbomeca *). 1.A.3. Spare Parts affected: FCU without modification TU 358 by Turbomeca *).
NOTE *) Modification of a FCU i.a.w. TU 358 is either retrofitted with Turbomeca Service Bulletin No. 292 73 0358 or installed by T urbomeca before new supply of a FCU. In both cases the accomplishment of TU 358 is confirmed by an entry in the log card of the FCU by Turbomeca. 1.B. Reason EUROCOPTER performed the ”MAX N1 Check” i.a.w. MM, Appendix E prior to delivery on each helicopter at an altitude (PA) of about 10000 ft. This test was successful for every delivered helicopter. During supplementary testings “MAX N1 CHECK” at EUROCOPTER at maximum certification altitude a few MBB-BK117 C-2 helicopters could not reach the specified N1 power threshold value. As the same engine is used on the helicopter MBB BK117 C-1, this problem may also occur on these helicopter models. After a first analysis, the suspected root cause is an engine acceleration limitation due to a delivered fuel flow lower than the engine fuel flow demand to achieve the OEI rating at high altitude. The fuel flow is limited by the FCU acceleration law in those cases. Therefore it is anticipated, that this limitation could potentially occur at altitudes higher than 10000 ft depending on the engine and FCU characteristics. As a conservative measure TURBOMECA and EUROCOPTER have decided that take-off, landing and HIGE/HOGE higher than 10000 ft or level flight above 13000 ft requires a dedicated mandatory check. If your operation requires to perform flights in altitudes higher than the above mentioned values, a ”MAX N1 CHECK” according to this Alert Service Bulletin has to be performed. Date: October 24, 2006 Rev. 4, December 11, 2007 

# ALERT SERVICE BULLETIN MBB-BK117

No. ASB-MBB-BK117-60-121 Subject: Power Plant – Power Control – Accomplishment of “MAX N1 CHECK”October 24, 2006 Rev. 4, December 11, 2007 ASB-MBB-BK117-60-121 Page 2 of 17 1.C. Description Mandatory check of engine power rating for take-off, landing and HIGE/HOGE in Pressure altitude higher than 10000 ft or level flight above 13000 ft, and if necessary, limitation of the maximum permissible flight altitude.
1.D. Compliance
EFFECTIVITY FCUs without modification TU 358 by Turbomeca. 1.D.1. If starting, landing and hovering procedures in or out of ground effect are accomplished up to pressure altitudes of a maximum of 10000 ft and mission flights are accomplished in pressure altitudes up to a maximum of 13000 ft, proceed i.a.w. section 2.B.2 of this Alert Service Bulletin. 1.D.2. If starting, landing and hovering procedures in or out of ground effect in pressure altitudes higher than 10000 ft or mission flights in pressure altitudes which are higher than 13000 ft are to be accomplished, a maintenance check flight i.a.w. section 2.B.1 of this Alert Service Bulletin must be performed once in order to verify the availability of the OEI rating of the engines. This maintenance check flight must be performed before the next mission flight. 1.D.3. If the engine and/or the FCU, and/or engine module 2 and/or the engine module 3 is replaced, the accomplishment of this Alert Service Bulletin must be repeated i.a.w. section 2.B.1 of this Alert Service Bulletin. 1.D.4. Accomplishment of this Alert Service Bulletin must be repeated with the Periodical Inspection (600 Fh).
EFFECTIVITY Helicopters on which Alert Service Bulletin MBB-BK117-60-121 has already been accomplished before Revision 04 and then modification TU 358 was installed. 1.D.5. After accomplishment of TU 358 on the FCUs of the two engines, the helicopters are no longer affected by Alert Service Bulletin MBB BK117-60-121 and the measures i.a.w. Section 2.B.6, 2.B.7 and 2.B.8 are to be accomplished.
1.E. Approval The technical content of this document is approved under the authority of DOA No. EASA.21J.034.
1.F. Manpower Requirement (not applicable)
1.G. Material, Cost and Availability (not applicable)
1.H. Special Tools (not applicable)October 24, 2006 Rev. 4, December 11, 2007 ASB-MBB-BK117-60-121 Page 3 of 17 1.I. Mass and Moment (not applicable)
1.J. Reference – FLM MBB-BK 117 C-1 – FLM MBB-BK 117 C-1C

1.K. Other Publications affected – FLM MBB-BK 117 C-1 (see appendix) – FLM MBB-BK 117 C-1C (effective for MBB-BK117 C-1C, S/N 7511, distributed separately)

. – MM MBB BK 117 C
1.L. Electrical Load Data (not applicable)

2. ACCOMPLISHMENT INSTRUCTIONS
2.A. Inspections Required (not applicable)
2.B. Work Procedure 2.B.1. Accomplishment of ”MAX N1 CHECK”: EFFECTIVITY For starting, landing and hovering procedures in or out of ground effect and for mission flights in pressure altitudes up to a maximum of 18000 ft.
NOTE Expect climbing during collective pull.
NOTE The “MAX N1 Check” is to be performed as a maintenance check flight by a qualified pilot. A second crew member is recommended to support parameter observation.
NOTE If the ”MAX N1 CHECK” is not successful in the chosen Pressure Altitude, accomplish the ”MAX N1 CHECK” in the next lower Pressure Altitude.

2.B.1.1. Accomplish ”MAX N1 CHECK”: (a) Set bleed air consumers to off. (b) Reduce electrical loads as much as possible, but generators remain on.October 24, 2006 Rev. 4, December 11, 2007 ASB-MBB-BK117-60-121 Page 4 of 17 (c) Establish level flight (approx. 65 KIAS) at AEO condition in 17500 ft PA. (d) Switch VARTOMS to MAN mode and trim to NRo=102%. (e) Reduce engine not to be tested to IDLE condition and trim rotor speed to NRo=101 %.
CAUTION DO NOT STAY WITHIN THE 2.5 MIN OEI RATING FOR MORE THAN 10 SEC. AND DO NOT UNDERSHOOT ROTOR RPM. IF MORE THAN 10 SECONDS OF 2.5 MIN OEI RATING HAS BEEN USED, RECORD THIS EVENT I.A.W. THE FLIGHT MANUAL. CAUTION IF THE TEST IS REPEATED ON THE SAME ENGINE, A “COOL DOWN TIME” OF AT LEAST 1 MINUTE AT OEI MCP LEVEL OR BELOW SHOULD BE OBSERVED BEFORE TO PERFORM A FURTHER “MAX N1 CHECK” ATTEMPT. (f) Maintain airspeed (approx. 65 KIAS) and pull collective pitch lever up to power setting n N1=1,3 % (2,5 min OEI-limit) and verify N1 increase up to value of ”N1 TACHO CHECK TABLE” of FLM MBB BK117 C-1 or FLM MBB BK117 C-1C and check rotor RPM. (g) When N1 limit is reached, the rotor speed must not drop below 98 %. (h) Note the value of N1 of the respective engine if the N1 limit is not reached. 2.B.1.2. If the OEI rating is reached, proceed i.a.w. section 2.B.3 of this Alert Service Bulletin. 2.B.1.3. If the OEI rating is not reached, starting, landing and hovering procedures in or out of ground effect up to a pressure altitude of a maximum of 10000 ft and mission flights in pressure altitudes up to a maximum of 13000 ft may be accomplished, proceed i.a.w. section 2.B.2 of this Alert Service Bulletin or with the next possible “MAX N1 CHECK” in a lower altitude. EFFECTIVITY For starting, landing and hovering procedures in or out of ground effect and for mission flights in pressure altitudes up to a maximum of 16000 ft.
NOTE Expect climbing during collective pull.
NOTE The “MAX N1 Check” is to be performed as a maintenance check flight by a qualified pilot. A second crew member is recommended to support parameter observation.
NOTE If the ”MAX N1 CHECK” is not successful in the chosen Pressure Altitude, accomplish the ”MAX N1 CHECK” in the next lower Pressure Altitude. 2.B.1.4. Accomplish ”MAX N1 CHECK”: (a) Set bleed air consumers to off.October 24, 2006 Rev. 4, December 11, 2007 ASB-MBB-BK117-60-121 Page 5 of 17 (b) Reduce electrical loads as much as possible, but generators remain on. (c) Establish level flight (approx. 65 KIAS) at AEO condition in 15500 ft PA. (d) Switch VARTOMS to MAN mode and trim to NRo=102 %. (e) Reduce engine not to be tested to IDLE condition and trim rotor speed to NRo=101 %.
CAUTION DO NOT STAY WITHIN THE 2.5 MIN OEI RATING FOR MORE THAN 10 SEC. AND DO NOT UNDERSHOOT ROTOR RPM. IF MORE THAN 10 SECONDS OF 2.5 MIN OEI RATING HAS BEEN USED, RECORD THIS EVENT I.A.W. THE FLIGHT MANUAL. CAUTION IF THE TEST IS REPEATED ON THE SAME ENGINE, A “COOL DOWN TIME” OF AT LEAST 1 MINUTE AT OEI MCP LEVEL OR BELOW SHOULD BE OBSERVED BEFORE TO PERFORM A FURTHER “MAX N1 CHECK” ATTEMPT. (f) Maintain airspeed (approx. 65 KIAS) and pull collective pitch lever up to power setting n N1=1,3 % (2,5 min OEI-limit) and verify N1 increase up to value of ”N1 TACHO CHECK TABLE” of FLM MBB BK117 C-1 or FLM MBB BK117 C-1C, and check rotor RPM. (g) When N1 limit is reached, the rotor speed must not drop below 98 %. (h) Note the value of N1 of the respective engine if the N1 limit is not reached. 2.B.1.5. If the OEI rating is reached, starting, landing and hovering procedures in or out of ground effect and mission flights up to pressure altitudes of a maximum of 16000 ft may be accomplished, proceed i.a.w. section 2.B.2 of this Alert Service Bulletin. 2.B.1.6. If the OEI rating is not reached, starting, landing and hovering procedures in or out of ground effect up to a pressure altitude of a maximum of 10000 ft and mission flights in pressure altitudes up to a maximum of 13000 ft may be accomplished, proceed i.a.w. section 2.B.2 of this Alert Service Bulletin or with the next possible “MAX N1 CHECK” in a lower altitude.October 24, 2006 Rev. 4, December 11, 2007 ASB-MBB-BK117-60-121 Page 6 of 17 EFFECTIVITY For starting, landing and hovering procedures in or out of ground effect and for mission flights in pressure altitudes up to a maximum of 13000 ft.
NOTE Expect climbing during collective pull.
NOTE The “MAX N1 Check” is to be performed as a maintenance check flight by a qualified pilot. A second crew member is recommended to support parameter observation. 2.B.1.7. Accomplish ”MAX N1 CHECK”: (a) Set bleed air consumers to off. (b) Reduce electrical loads as much as possible, but generators remain on. (c) Establish level flight (approx. 65 KIAS) at AEO condition in 12500 ft PA. (d) Switch VARTOMS to MAN mode and trim to NRo=102 %. (e) Reduce engine not to be tested to IDLE condition and trim rotor speed to NRo=101 %.
CAUTION DO NOT STAY WITHIN THE 2.5 MIN OEI RATING FOR MORE THAN 10 SEC. AND DO NOT UNDERSHOOT ROTOR RPM. IF MORE THAN 10 SECONDS OF 2.5 MIN OEI RATING HAS BEEN USED, RECORD THIS EVENT I.A.W. THE FLIGHT MANUAL. CAUTION IF THE TEST IS REPEATED ON THE SAME ENGINE, A “COOL DOWN TIME” OF AT LEAST 1 MINUTE AT OEI MCP LEVEL OR BELOW SHOULD BE OBSERVED BEFORE TO PERFORM A FURTHER “MAX N1 CHECK” ATTEMPT. (f) Maintain airspeed (approx. 65 KIAS) and pull collective pitch lever up to power setting n N1=1,3 % (2,5 min OEI-limit) and verify N1 increase up to value of ”N1 TACHO CHECK TABLE” of FLM MBB BK117 C-1 or FLM MBB BK117 C-1C, and check rotor RPM. (g) When N1 limit is reached, the rotor speed must not drop below 98 %. (h) Note the value of N1 of the respective engine if the N1 limit is not reached. 2.B.1.8. If the OEI rating is reached, starting, landing and hovering procedures in or out of ground effect and mission flights up to pressure altitudes of a maximum of 13000 ft may be accomplished. Proceed i.a.w. section 2.B.2 of this Alert Service Bulletin. 2.B.1.9. If the OEI rating is not reached, starting, landing and hovering procedures in or out of ground effect up to a pressure altitude of a maximum 10000 ft and mission flights in pressure altitudes up to a maximum of 13000 ft may be accomplished. Proceed i.a.w. section 2.B.2 of this Alert Service Bulletin.October 24, 2006 Rev. 4, December 11, 2007 ASB-MBB-BK117-60-121 Page 7 of 17 2.B.2. Affixing of placard: 2.B.2.1. Copy page 8 of this Alert Service Bulletin. 2.B.2.2. Choose placard (1, Figure 1) corresponding to the maximum permissible Pressure Altitude and cut out. 2.B.2.3. Using a transparent adhesive tape, affix placard (1, Figure 1) to a place in the cockpit which can easily seen by the pilot. 2.B.3. Copy the flight manual pages attached to this Alert Service Bulletin, cut out and insert behind the affected FLM pages. 2.B.4. After accomplishment of the “MAX N1 CHECK”, fill out copy of reply form sheet from page 17 and send to ECD and Turbomeca. 2.B.5. Confirm accomplishment of this Alert Service Bulletin by an entry in the historical record of the helicopter.
EFFECTIVITY After accomplishment of modification TU 358 on both engines. 2.B.6. If affixed, remove placard (1, Figure 1) from helicopter. 2.B.7. Remove the flight manual pages enclosed with this Alert Service Bulletin from FLM. 2.B.8. Removal of the possibly affixed placard and removal of the flight manual pages must be confirmed by an entry in the helicopter‘s historical record.
2.C. Conclusions (not applicable)

3. MATERIAL INFORMATION (not applicable)October 24, 2006 Rev. 4, December 11, 2007 ASB-MBB-BK117-60-121 Page 8 of 17 Placard for Maximum Pressure Altitude Figure 1 

### Maximum altitude for take-off, landing and HOGE is 

## 10000 ft PA Maximum operating altitude is 

## 13000 ft PA

Maximum operating altitude is 

## 16000 ft PA Maximum operating altitude is 

## 13000 ft PA

1 Placard
Choose placard corresponding to the maximum permissible flight altitude and cut out. Using a transparent adhesive tape, affix placard to a place in the cockpit which can be easily seen by the pilot. ASB-MBB BK117-60-121

ASB-MBB BK117-60-121 ASB-MBB BK117-60-121 1

1

1October 24, 2006 Rev. 4, December 11, 2007 ASB-MBB-BK117-60-121 Page 9 of 17October 24, 2006 Rev. 4, December 11, 2007 ASB-MBB-BK117-60-121 Page 10 of 17October 24, 2006 Rev. 4, December 11, 2007 ASB-MBB-BK117-60-121 Page 11 of 17October 24, 2006 Rev. 4, December 11, 2007 ASB-MBB-BK117-60-121 Page 12 of 17October 24, 2006 Rev. 4, December 11, 2007 ASB-MBB-BK117-60-121 Page 13 of 17October 24, 2006 Rev. 4, December 11, 2007 ASB-MBB-BK117-60-121 Page 14 of 17October 24, 2006 Rev. 4, December 11, 2007 ASB-MBB-BK117-60-121 Page 15 of 17October 24, 2006 Rev. 4, December 11, 2007 ASB-MBB-BK117-60-121 Page 16 of 17October 24, 2006 Rev. 4, December 11, 2007 ASB-MBB-BK117-60-121 Page 17 of 17 

# Telefax

To Eurocopter Deutschland GmbH Customer Service FAX 0049 906714111

Date:__________ Signature:___________________ Alert Service Bulletin MBB BK117-60-121 ”MAX N1 CHECK” has been accomplished. Reply form sheet for accomplishment of the “MAX N1 CHECK”:

Please copy page! The original page remains in the ASB! In order to clearly determine the reason why the OEI rating has not been reached in higher Pressure Altitudes, it is necessary to report the data mentioned below to ECD and Turbomeca. In case of further problems contact ECD or Turbomeca field representative!

Helicopter S/N: “MAX N1 CHECK” accomplished in Pressure Altitude: ft, successful engine LH yes / no –– N1-Value ft, successful engine RH yes / no –– N1-Value ft, successful engine LH yes / no –– N1-Value

LH engine S/N: RH engine S/N: LH FCU S/N: RH FCU S/N: To Turbomeca Local TM Field Representative

ft, successful engine RH yes / no –– N1-Value ft, successful engine LH yes / no –– N1-Value ft, successful engine RH yes / no –– N1-Value % % %

% % %

# Alert letter

OPERATOR SUPPORT 40220 Tarnos – France Tél. (33) (0) 5 59 74 40 00 Télex 570 042 Fax (33) (0) 5 59 64 74 98 Technical Support Department Fax (33) (0) 5 59 74 45 34

JSV/BF/MD 

## Service Letter No. 2495/06/AR1E/29 Subject: ARRIEL 1 E2. Engine power ratings availability at high altitude. Bordes, October 23, 2006

SIEGE SOCIAL ET DIRECTION GENERALE : 64511 Bordes Cedex – France Tél. (33) 5 59 12 50 00 – Télex 560 928 – Fax (33) 5 59 53 15 12 TURBOMECA - Brevets Szydlowski – Société Anonyme au capital de 38.553.056 Euros – Registre du Commerce et des Sociétés Pau B 338 481 955 1/2 

### A L E R T

L E T T E R A L E R T

L E T T E R 

# To the attention of maintenance personnel and crews

Dear Madam, Sir, The MBB BK117 C-2 (EC145) Master Servicing Manual (MSM) tasks 05-60-00 or MBB BK117 C-1 Maintenance Manual (MM), appendix E "MAX N1 check" aims to check the availability of the ARRIEL 1 E2 engine OEI 2.5-min rating. The OEI 2.5-min rating is designed to be used with one engine inoperative during take-off, landing or hover in / out-off ground effect (HIGE / HOGE). EUROCOPTER performs this “MAX N1 check” prior delivery on each helicopter at an altitude (PA pressure altitude) of about 10.000 ft. This test was successful for every delivered helicopter. During supplementary testing at EUROCOPTER at maximum certification altitude a few MBB BK117 C-2 helicopters failed this test. Therefore it is anticipated, that this behaviour could potentially occur at altitudes higher than 10.000 ft depending on the engine and FCU characteristics. After a first analysis, the suspected root cause is an engine acceleration limitation due to a delivered fuel flow lower than the engine fuel flow demand to achieve the OEI 2.5-min rating at high altitude. The fuel flow is limited by the FCU acceleration law in this case. As a conservative measure TURBOMECA and EUROCOPTER have decided that take-off, landing and hover HIGE / HOGE higher than 10000 ft or level flight above 13000 ft require a mandatory dedicated check. Should you require to perform operations in altitudes higher than the above mentioned values, a “MAX N1 check” according to ECD Alert Service Bulletin MBB BK117 C-2-71A-003 or MBB BK117-60-121 has to be performed successfully prior to operate at the desired altitude.Alert Letter No. 2495/06/AR1E/29

2/2 

### A L E R T

L E T T E R A L E R T

L E T T E R If the "N1 max" check is not successful, please contact your local TURBOMECA field representative and continue to operate according to the ECD Alert Service Bulletin. TURBOMECA is putting the highest priority in order to define a corrective action, which will allow recovering the initial whole flight envelope. Pending the results of the further analyses in progress, we would like to highlight that the engine or FCU exchange will not allow fixing the issue. We will keep you informed of the results of the analyses, and appropriate corrective action. Please do not hesitate to contact us if you require any other information.

J-S. VIGNES Technical Support Department