SE0UIENCE ro.IUMBER

SE0UIENCE ro.IUMBER 11111M110111111 6030187 ACTION CARD 166-CAV-AMO-2014 ROUTINE PROJECT 1999M weon:Itnet 737 Ratser 9( tat ra R 324471 w Qr iarAArr .) Wt.' 00i vP4B8 71 14 us COV COM 807 10.9%18 GIMES 482100 m.,..cemOci,A1Tha 'tweet AWR.9 at. NA icre NA YES S2 Ill.CrO,at DEG. La. 0£0 , YA.C4 REPAIt K: it 0 46 yrs 6) ..,41 3 1 floill y -2-4,-7 NECK VA.' MiC a1 0. *". O n , (" -7 DISCREPANCY. Customer request- perform test 5 engine runs RESOLUTION. PLUGS?... I `1 61 ire....1 Cron. Irkr.... C-orvdcir cr.rel 3r-rt..x.k_ ;n 3ro iliNC-- r eartenkr OAR. COirti , IttuelLS r2 1/4 ") CDT tapani 737 Ainn. a-rt-a2 MECH INS? 7.4",e ' Per"%c•-• „ze.-7,772 Sa ADeerg- 1O0O qc..[ oc -foci cror-t. ruiticA. Air CD° OX13€3e0( Pc r cot- r^stic c,.. Poc-x_r i:LS Li". 4 I.-X.- C.-kt.r.,....L 4:.A..... A a -lei Crel Al C.V. \ (..... hec .ic_. cr, VocAt-.. ci, f . ne.;) 9a - c_c_,..a.ton, e-e- _r c_ciocA;" =ALA 4.. ...te; :,41 737-ea> .,4) PIM "Tip 00:042.. -7-j.:,,p pr./kr 5/..4.) icio_sc—s-8, Cat-- 6.4.-:c, ,, 4 A , PART NUMBER REMOVED SERIAL NUMBER REMOVED PART NUMBER INSTALLED SERIAL NUMBER INSTALLED P.O. NUMBER ./ / --7...--7 ,-." , ..---7-e----/ ACC4106.4- PACE. Yes COIAJJX ANEOCA.LLC. anted Reati • Pap. I Off mein 7 111-2_ 28 aN 20IS EFTA00812370 ts:SCH F11! 1.) Operator: BOSCO AVIATION Serial No: 32806 (YD405) 737-BAWD) REVISION 20 RegNo. VP-CBS Date Lecget. 30-MAY-2017 Work Card No.: 270530-1-1 Workorder No.: WO 17O530C8B Due At DATE(DD/MMM/MY) HOURS CYCLES Accomplished Task No 9/04; L1gX3 Task Duce*don 170530-1-1 PERFORM TEST 5 — POWER ASSURANCE CHECK AS PER 8737 AMM TASK 71-00-00.700-813-F00. COMPLETE THE ATTACHED FORM ENGINE DATA AND RECORD SHEET FIGURE 501/71-00-00.990.803-F00 (SHEET 1 OF 2) AND RECORD IN THE ADDITIONAL DATA REQUIREMENTS SECTION, THE BAROMETRIC VALUE AT THE TIME OF RUN. P/N: S/N • LABOR HRS: COST: REPAIR STATION' CORRECTIVE ACTION: Pfr Pot 1b 5/ ES r afrift- fr__eveihded la 43 P.' _ AIn fn TASK I 00-_00 - 100 - - fop. TECHNICIAN SIGNATURE' INSPECTED BY: Z- ";;;;;C'esIC ,••Nti 24:J ,• 166-CAY-AMO-2014 KIND Of CERTIFICATE & NO • KIND OF CERTIFICATE & NO • 166-CAY-AMO-2014 30-MAY-2017 0 CAMP SYSTEMS 1 of 1 WID: 24560128.1 Total Pages • Initial . Return completed copy via email to EFTA00812371 Operator: aOsco AVIATION Work Card No.: 170530-2-2 Serial No: 32806 (YD405) Model: 737-8AWF31 REVISION 20 RegNo. VP-CBB Date Loggec: 30-MAY-2017 Workorder No.: WO 170530088 DATE(DD/PIMM(YTYY) Due At HOURS CYCLES Accomplished ul M ogi I Task No Task Description It.,VIS -le 4192 _1 170530-2-2 PERFORM ACCELERATION CHECK PER AMM TASK 71.00-00-700.824-F00 (TEST 8) CORRECTIVE ACTION' TECHNICIAN SIG INSPECTED BY: P/N: S/N: LABOR HRS: COST: REPAIR STATION' ( fr eer/A r 3 &Ca feito-n? ter: I PIFr Am AS I -00 -OO ••110O -•v34—A2,9 #s7-bnezt n71) .4m,1 :a y es- 3., etil KIND OF CERTIFICATE & NO.- 166-CAY-AMO-2014 KIND Of CERTIFICATE & NO.- 166-CAY-AMO-21114 30-MAY-2017 CD CAMP SYSTEMS 1 of I WID: 24560130-1 Total Pages- Initial Return completed copy via email to EFTA00812372 CAMP ,_CHEE.1 Operator: BOSCO AVIATION Work Card No.: 170530-3-3 I Serial No: 32806 (YD405) Model: 737-8AWB3 REVISION 20 RegNo. VP-C8B Date logged. Workorder No.: WO 170530am Due At DATE(DOMMM/YYYY) CYCUES ACcoallished Task No log*. Le Task Dosaiption 170530-3-3 POWER ASSURANCE CHECK AT ALL THREE SPEEDS (65, 70 AND 75% NI) P/N: LABOR HRS: COST: REPAIR STATION' CORRECTNEACToN: tot D ASS4Itaroce cingeeks- Per 8')3r) /1-rn in TECHNICIAN SIG INSPECTED BY: qt. oo -Po- loo -81 3 - Foo 30-MAV-2017 WID: 24560131.1 Return completed copy via email to afren 7 166-CM-A610-2014 ic KIND Of CERTIFICATE & NO • D"A t2 KIND OF CERTIFICATE & NO • 166-CAY-AMO-2014 0 CAMP SYSTEMS 1 of 1 Total Pages , Initial EFTA00812373 clif4P Insi•••••••Ier...„/- SERIAL: 32806 (YD405) DATE IN : UTC:5/30/2017 Work Order Tally Sheet Report REGNO : VP-C88 MODEL NAME : BB) 737-7001GW/-800/-900ER DATE OUT : UTC:5/30/2017 11:00:00 PM ICAO : KIND WORK ORDER C: WO 17053003B SERVICE CENTER : COMLUX MALTA LTD. ITEM NO DESCRIPTION TECHNICIAN 4 efrOPC 170530-1-1 ENGINE. PERFORM TEST 5- POWER ASSURANCE CHECK AS PER 8737 AMM TASK TECH : 71-0O.O0-700-813-F00. COMPLETE THE ATTACHED FORM ENGINE DATA AND RECORD SHEET FIGURE 501,71-00-00-990-803-F00 (SHEET 1 OF 2) AND RECORD IN THE ADDITIONAL DATA REQUIREMENTS SECTION. THE BAROMETRIC VALUE AT THE TIME OF RUN. 170530-2-2 ENGINE, PERFORM ACCELERATION CHECK PER AMM TASK 71.00.00-700.824-F00 (TEST 8) 170530-3-3 ENGINE. POWER ASSURANCE CHECK AT ALL THREE SPEEDS (85. 70 AND 75% NI) Srn t TECH u *CC* ./a Xfaree 7 - TECH : eiL—O-66O/O INSP : INSP INSP INSPECTOR v.-411? :747.2...-<?5- • 30MAY-2017 0 CAMP SYSTEMS 1 of 1 EFTA00812374 CFM56 ENGINES (CFM56-7) I 6s- g 7c 421 AirdtZEIA,S 1 737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL DATE 30 MAY -2-0 n AIRPLANE DA TA ENGINE DATA AIRPLANE NO. FUEL TYPE ENG ENGINE MODEL ENGINE 5/N HMI P/N -see--f-m- C. e (3 3£-r A POS VP- 71S..2-7/ 14:59v1.1s- TAM FUEL QUANTI T Y AZ p6k)mtp9vp.2v NO. 1 2 762,7/£3.3 f -3L ;`1,1 53 7 asshi-W13c5- -^—' "709'0 NO. 2 7'100 REMARK BARD PC.B.S.S ; 3D. pet. C TR 2 720 gE(... resi TA.,' o'veztt)cluirmiehrkPce. pQ L. Pcx. 2. Weir 07Y&10ceni i car ;4,2 et». TOT AL 2 7) b o ENGINE START DA TA START LEVER ADV. LIGNTUP STARTER MAX. TIME TO OIL ENG POS xN2 MOTORING TINE (SEC> INITIAL rc TIRE <SEC) CUTOUT CZN2/ EGT • < 'O MAX . FF IDLE <SEC> OTT TENS' PRESS I VIBRATION (UNITS) .713 58.3 s-30•tic:3 LS tg 3'! . 1 2 • 75' Sb s"15:3 659 fl 77 3O • 1 HYDRAULICS ADDITIONAL DATA REQUIREMENTS FT° Hy') HID SYS PRESS ENG SYS CITY (MOP En P05 s I a e _ TEST NO. 5 .- POVER ASSURANCE CHECK ENG OAT TARGET RECORDED VALUES POS OF (,)0) FN I '.142 EGI ' 75 k6.1 I,6 1 P 4•I S Se. 2 75 (2‘.f bbl R9•'( .5"433 1 -75- -71 1 -71. I 90.9 I, 17 2 7c '711 71.1 91.0 61C, I 7S" 761 -7E.1 q )-$ 41 tori 7$ 7b.i -lb 1 9). • 3. - _/S5 - EFFECTIVITY BBJ ALL Engine Data and Record Sheet Figure 501/71-00-00.990-803-F00 (Sheet 1 of 2) G4146$ S0006511TD0_VI 71-00-00 Page 507 D633A101-B8J Oct 15/2015 AGEING PIXOPRIZ~ • Cer•Vi ~Pei Wa" • he Fil•OWM OWak EFTA00812375 C A MP Andibl.••••••••"Ir Work Order Contents Report SERIAL: 32806 (YD40S) REGNO W-(38 MODEL NAME : EEO 737-7001GW/-800/-900ER DATE IN : UTC:30-May-2017 12:00 AM DATE OUT : UTC:30-May-2017 11:00 PM IOO : KIND WORK ORDER alt: WO 170530088 SERVICE CENTER : COMLUX MALTA LTD. WOMKCARD DESCRIPTION STATUS M 1705304-1 ENGINE, PERFORM TEST S - POWER ASSURANCE CHECK AS PER VP AMM TASK 71-0040-7C0-613-F00. OPEN COMPLETE DIE ATTACHED FOOT ENGINE DATA AND RECORD SHEET FIGURE 501771-00-00-990-803400 (SHEET 1 OF 2) AND RECORD IN THE ADDITIONAL DATA REQUIREMENTS SECTION, THE SAROVETRIC VALUE AT THE TIME OF RUN. 2.0 1705304-2 ENGINE, PERFORM ACCELERATION CITEOC PER AMM TASK 71-00-00-700424400 (TESTS) OPEN 3.0 170530-3-3 MINE, POWER ASSURANCE CHECK AT AU. THREE SPEEDS (65, 70 AND 75%01) OPEN Proparmt By: Approved By: Siwkhart &en& &Hart DM*: 30 Okay 2017 Date: 30-MAY-2017 CAMP SYSTEMS 1 at 1 EFTA00812376 L CFM56 ENGINES (CFM56-7) gifirosArAfc 737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL (b) Look at the inside surfaces of the fan cowl panels or thrust reverser as applicable for new fuel, oil or hydraulic stains. (c) Do the leak check again after you replace or repair the tubes, tube flanges. fittings or components. F. Put the Airplane Back to Its Usual Condition SUITASK 7140-0.410.013•00 WARNING: OBEY THE INSTRUCTIONS IN THE PROCEDURE TO CLOSE THE THRUST REVERSERS. IF YOU DO NOT OBEY THE INSTRUCTIONS. INJURIES TO PERSONS AND DAMAGE TO EQUIPMENT CAN OCCUR. (1) If they were opened, do this task: Close the Thrust Reverser (Selection), TASK 78-31-00-010.804-F00. SUBTASK 7140.00.410.014-F00 (2) Do this task: Close the Fan Cowl Panels. TASK 71-11-02-410-801-F00. TASK 71-00-00-700-813-F00 7. Test 5 - Power Assurance Check (Figure 503, Figure 504. and Figure 505) A. General END OF TASK (1) The Power Assurance Check is not a good test for performance analysis of the engine. Do not use only the Power Assurance Check to accept or reject an engine. The power assurance run is usually not sufficiently stable to accurately calculate the engine's health. You can get a more reliable performance analysis by doing a test cell operation or on-wing performance trend monitoring. (2) Do this test to make sure the engine will get takeoff power without the EGT or N2 at redline limits. For a specific %N1, this check will calculate the maximum EGT and the %N2 target values. This check can be done at one of three different N1 speeds: t is recommended that the initial check be done at 65% N1. If th e , is operator policy, men do a subsequent test at the higher N1 speeds. This procedure will also give the steps to adjust the EGT limit (make an altitude correction of the maximum EGT) when you operate the airplane at an airport above sea level. The actual EGT margin is based on the airplane route structure. B. References Reference Title (3) (4) (5) 24-22-00-860-811 71-00-00-700-819-F00 71-00-00-800-807-F00 73-21-00-700-808-F00 73-21-0D-740-803-F00 C. Tools/Equipment Reference Supply Electrical Power (P/B 201) Stop the Engine Procedure (Usual Engine Stop) (P/B 201) Start the Engine Procedure (Selection) (P/B 201) IDENT/CONFIG (P/8 501) EEC BITE TEST - RECENT FAULTS (P/B 501) Description STD-1122 Thermometer - Alcohol/Mercury (or equivalent meter meets task requirements) EFFECTIVITY BBJ ALL 71-00-00 Page 520 D633A101-BBJ Jun 15/2015 BOEING OROVRIETAPY .Cocrighe t'unp.c.thee Mot • See Me Dam lee delak EFTA00812377 L CFM56 ENGINES (CFM56.7) 0_4117E/ACC 737-600,70018001900 AIRCRAFT MAINTENANCE MANUAL D. Power Assurance Check SUBTASK 114040-970-00S-F00 CAUTION: DO NOT USE THE TOTAL TEMPERATURE INDICATION FROM THE AIRPLANE FOR THE AMBIENT AIR TEMPERATURE. THIS WILL PREVENT AN INCORRECT TRIM TARGET SELECTION. CAUTION: DO NOT PUT A MERCURY THERMOMETER ON THE AIRPLANE. MERCURY (FROM A BROKEN THERMOMETER) CAN CAUSE DAMAGE TO THE AIRPLANE COMPONENTS. (1) Use a thermometer, STD-1122 to get the ambient air temperature (OAT) in the shade of the nose wheel well. (a) Record the OAT on the data sheet. SUBTASK T14040470404-F00 (2) Use the OAT to get the %N1 Target speed, the Max EGT and Max %N2 for the applicable engine model and thrust rating (Figure 503, Figure 504. and Figure 505). NOTE: The 7826 and 7B26/B1 engine models are equivalent in thrust rating. The 7827 and e ngine models are equivalent in thrust rating. (a) Record the %N1 Target, Max EGT and Max %N2 on the data sheet. (b) To do a check of the thrust rating, refer to the Ident/Config page, do this task: IDENT/CONFIG. TASK 73-21-00-700-808-F00 1) Record the trim level for the N1 Modifier Adjustment used in the Test Results. SUBTASS 7tMMM04OtP00 (3) Do this task: Supply Electrical Power. TASK 24-22-00-860-811. SUBTASK 1140-00460401400 WARNING: MAKE SURE YOU OBEY ALL THE INSTRUCTIONS AND PRECAUTIONS WHEN YOU OPERATE AN ENGINE AT HIGH POWER. REFER TO THE ENGINE GROUND SAFETY PRECAUTIONS TASK. IF YOU DO NOT OBEY THE INSTRUCTIONS AND PRECAUTIONS, INJURIES TO PERSONS AND DAMAGE TO EQUIPMENT CAN OCCUR. (4) Do this task: Start the Engine Procedure (Selection), TASK 71-00-00-800-807-F00. (a) Make sure the BLEED 1 and BLEED 2 switches are in the OFF position. (b) Set the applicable GEN switch to the OFF position and release. NOTE: This will remove the load from the IDG, if it is not already removed. 1) Make sure the applicable GEN OFF BUS light comes on. (c) Let the engine become stable at the idle-power position for five minutes. SUBTASK T140.00440.0104,00 (5) Make sure that the applicable switches on the overhead panel. P5. are in the OFF position: (a) WING ANTI-ICE (b) ENG ANTI-ICE 1 or 2. SUBTASK 714040460-1 75400 (6) Make sure the PROBE HEAT "A" or "Be switch on the overhead panel, P5, is in the ON position. NOTE: For engine operation at high power, the EEC can go into Alternate Mode operation if neither pitot probe is heated. EFFECTIVITY 88J ALL 71-00-00 Page 521 0633A101-BBJ Jun 15/2015 SOONG PROANETARY - CoarAil QUngNWf AtoA. Ste EA 030* fre delas EFTA00812378 L CFM56 ENGINES (CFM56-7) gifiroreArc 737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL SUSTAIN( 71•00•00400411400 (7) Monitor all engine parameters. (a) Carefully monitor the EGT and N2 indications. SUBTASK 71-00•00469•165400 (8) Slowly move the applicable forward thrust lever to the N1 target speed that you got for the applicable MPA power level: (a) It is recommended that the 1ni is check e done at 65% N1. If that test fails. or if it is operator policy, then do a subsequent test at the higher N1 speeds. (b) If this is a subsequent check at a higher speed, make sure the engine runs at the idle-power position for a minimum of 10 minutes before you increase the engine speed again. SUBTASK 71•00-00410-034400 (9) Let the engine become stable at this power assurance target for a SUBTASK TI•40•06410496400 (10) arameters from the power assurance target on the data s ee . SUSTASK 7140-00-SWISAFOO (11) Slowly move the applicable forward thrust lever to the idle-power position. SUSTASK 7140404704$400 (12) When this check is complete. make a decision if an additional check is necessary as follows: (a) If the test was satisfactory, you can do one of these steps: 1) Do the above check again at the higher N1 speed; or, 2) Continue to the steps to stop the engine. BBJ 001-004, 006, 008-018, 020, 021, 023-026. 028-037.039, 040, 042, 043, 061, 064, 068, 070-072, 075. 076, 078, 079, 082, 083, 086, 087, 091-095, 097-099, 111-114, 116-119, 121, 122, 124, 125, 401, 404, 405, 407, 409, 410, 415417, 901-905 PRE SB 737.30A1063 a) Put the Probe Heat "A" and "B" switches on the overhead panel. P5, to the OFF position. BBJ 005, 007, 019, 022, 027, 038, 041, 062, 063, 066, 073, 077. 080, 085, 096, 120, 123, 126-399, 402, 403, 406, 408, 412.414, 418422, 906-999; BBJ 001-004, 006, 008-018, 020. 021, 023-026, 028-037, 039, 040, 042, 043, 061, 064, 068, 070-072, 075, 076, 078, 079, 082, 083, 086, 087, 091-095, 097-099, 111-114, 116-119, 121. 122, 124, 125, 401, 404, 405, 407, 409, 410, 415.417, 901-905 POST SB 737-30A1063 b) Put the Probe Heat "A" and "B" switches on the overhead panel, P5. to the AUTO position. BBJ ALL c) Do this task: Stop the Engine Procedure (Usual Engine Stop), TASK 71-00-00.700-819-F00. (b) If the test is not satisfactory, do the above check again at the higher N1 speed. EFFECTIVITY BBJ ALL IO633A101 -MU SOONG PRCORIETART • Ctenhi D kfrptainlind renri • $. US Wei S 444M 71-00-00 Page 522 Jun 15/2016 EFTA00812379 L CFM56 ENGINES (CFM56-7) Z I tirt7LFIAor 737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL (a) Use these steps to find if there is a positive or negative difference between the N1 target and the N1 record: 1) If the N1 target is more than the N1 record, there is a positive difference. 2) If the N1 target Is less than the N1 record, there is a negative difference. (b) For each 0.1% of positive difference In N1, 0.8 degrees C must be added to the EGT, and 0.03% must be added to the N2 value that you recorded during the test. (c) For each 0.1% of negative difference in N1, 0.8 degrees C must be subtracted from the EGT, and 0.03% must be subtracted from the N2 value that you recorded during the test. Table 503/71-00-00-993-925-F00 Adjustments for Difference between N1 Target and N1 Record Parameter EGT Correction Value/0.1 %N1 0.8 Degrees C N2 0.03% kT6 G 27/83) 5 rLE eg9 Yin LT (7cs-1 3,,,f 38r►`7`' (d) If the engine has been configured with 7BUI or higher version of the EEC software, use the data for the applicable rating in the table below to adjust the N2 margin (Table 504). NOTE: Table 504/71-00-00-993-932-F00 Rating NT Margin Adjustment" VI 7924 or 7824/3 1.2 792291 or 7822/381 1.3% 7822 or 7822/3 1.5% g-Theets-----/ 1.7% •[ ie adjustment is applicable to SAC and DAC engines. [2) N2 Margin (Adjusted) • Calculated N2 Margin - N2 Margin Adjustment (e) This is an Example Calculation for the MPA Test Table - 70% Nt of the 7620 engine for an OAT of 10 degrees C (Figure 504): BBJ ALL; AIRPLANES WITH SINGLE ANNULAR COMBUSTOR (SAC) ENGINES Table 505171-00.00-993-908-F00 FROM MPA TEST TABLE - 70% Ni. OAT OF 10 DEG C N1 TARGET = 69.4%. EGT MAX r6 DEG C. N2 MAX = 91.8% TEST DATA RECORDS. N1 RECORD = 69.7%, EGT RECORD = 695 DEG C N2 RECORD = 81% N1 TARGET < N1 RECORD, A NEGATIVE DIFFERENCE al DIFF = N1 RECORD - N1 TARGET = 69.7 - 69.4 = 0.3 EGT ADJ = EGT RECORD - (0.8/0.1)(N1 DIFF) = 695 - (0.8/0.1X0.3) = 692.6 DEG C N2 ADJ = N2 RECORD - (0.03/0.1XN1 DIFF) = 81% - (0.03/0.1X0.3) = 80.9% FIND EGTAND N2 MARGINS WITH THE VALUES OF EGTADJ AND N2 ADJ EGT MARGIN • EGT MAX - EGTADJ • 726 - 692.6 • 33.4 DEG C N2 MARGIN • N2 MAX • N2 ADJ • 91.8 - 80.9 • 10.9% EFFECTIVITY BBJ ALL D633A101-BBJ BCC PC PROGRETARY .Cysylip , Ova Mel Work • Sof Ode pne to, details 71-00-00 Page 523 Jun 15/2016 EFTA00812380 L CFM56 ENGINES (CFM56-7) gLATOSZAW 737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL BBJ ALL; AIRPLANES WITH SINGLE ANNULAR COMBUSTOR (SAC) ENGINES (Continued) Table 505/71-00-00-993-908-F00 (Continued) N2 Margin (Adjusted) = 10.9% (Calculated N2 Margin) - 1.7% (N2 Margin Adjustment) = 92%. I II12) ill Get the N2 margin adjustment from Table 504 (21 Adjust the N2 margin for engines configured with 7BUI or higher software. 88.1 ALL SUSTASK 11 40 40704 3/400 (2) To adjust the EGT margin for altitude. do these steps: (a) Find the Altitude Correction Adjustment for the applicable engine and altitude in the table. 1) Use the highest altitude on the airplane's route structure. 2) The EGT corrections shown are for takeoff worst case flight condition and Includes ambient temperature and altitude effects. 3) Linear interpolation is necessary for altitudes between the table values. (b) Subtract the altitude adjustment value from the calculated EGT margin. Table 506/71-00-00-993-911-F00 Altitude Adjustment Factors ALTITUDE ENGINE MODEL I I) FEET 7820 7622 7822/81 7824 7624/61 7826 7626/82 7827 7827161 7826/81 'CO 24 0 [repeated 3 times] 5 7 0 [repeated 3 times] 24 0 [repeated 3 times] 5 7 0 0 1000 24 0 [repeated 3 times] 6 7 0 0 2000 24 0 [repeated 3 times] 7 8 0 0 3000 24 0 [repeated 3 times] 7 8 0 0 4000 24 0 [repeated 3 times] 8 6 0 0 5000 24 0 [repeated 3 times] 5 4 0 0 6000 18 0 [repeated 3 times] 3 0 [repeated 3 times] 7000 12 0 [repeated 7 times] 8000 6 0 [repeated 7 times] 9000 0 [repeated 8 times] >9000 0 [repeated 8 times] LE . /3F. AND -76E RATINGS (c) To continue the same Examp e Calculation for altitude adjustment, assume the highest airport is at 4000 feet. BBJ ALL; AIRPLANES WITH SINGLE ANNULAR COMBUSTOR (SAC) ENGINES Table 507/71-00-00.993-912-F00 FOR A 7820. 4000 FT ALTITUDE. ALTITUDE ADJUSTMENT FACTOR = 24 EGT MARGIN ALT = EGT MARGIN - ALTITUDE ADJUSTMENT FACTOR EFFECTIVITY BBJ ALL 0633A101-BBJ scow pRopissusy.sopr o., Unpubli1W5 Wylt • St. lib Per 10,600. 3 71-00-00 Page 524 Jun 15/2016 EFTA00812381 CFM56 ENGINES (CFM56-7) cofirostsca 737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL BB./ ALL; AIRPLANES WITH SINGLE ANNULAR COMBUSTOR (SAC) ENGINES (Continued) Table 507/71-00-00.993-912-F00 (Continued) - 33.4 - 24 = 9.4 DEG C BB.) ALL SWUM 71.0.WM.OSNW (3) To adjust the EGT margin for N1 modifiers, do these steps: (a) Find the N1 Modifier Adjustment for the applicable engine model and trim level. 1) To find the trim level, do this task: IDENT/CONFIG, TASK 73-21-00-700-808-F00. (b) Add the adjustment to the calculated EGT margin. Table 508/71.00-00-993409-F00 N1 Modifier Adjustments ENGINE MODEL in TRIM 7820 7822 7822/81 7824 7824181 7826 7827 7827181 LEVEL 7828/61 nigarips 7928/82 0 [repeated 8 times] 1 2 [repeated 3 times] 1 1 6 3 2 3 [repeated 5 times] 8 5 3 4 5 [repeated 4 times] 10 8 4 6 6 7 [repeated 3 times] 12 11 5 7 8 [repeated 4 times] 14 15 6 8 9 10 [repeated 3 times] 15 18 7 10 11 [repeated 3 times] 12 17 _ 20 Ill APPLICABLE TO ALL /3. /3F. AND -7BE RATINGS (c) To continue the same Example Calculation for N1 Modifier, assume the trim level is 4. MU ALL; AIRPLANES WITH SINGLE ANNULAR COMBUSTOR (SAC) ENGINES Table 509/71.00.00-993-910-F00 FOR A 7B20 WITH TRIM LEVEL OF 4. N1 MODIFIER ADJUSTMENT = 6 EGT MARGIN MODIFIED = EGT MARGIN ALT -0. N1 MODIFIER ADJUSTMENT = 9.4 + 6 = 15.4 DEG C BBJ ALL SOBTASK 71•00•004704311400 (4) If the 65% N1 power assurance check is not satisfactory, do the test again at 70% Ni. (a) If the 70% N1 power assurance check is not satisfactory, do the test again at 75% N1. 1) If the 75% Ni power assurance check is not satisfactory, do this task: EEC BITE TEST - RECENT FAULTS, TASK 73.21-00-740.803-F00. EFFECTIVITY riALL D633A101-BBJ e0EiNCPROloctiCYNtt - ecorip t; inatai~vra . se. my rm rd 1.041. 71-00-00 Page 525 Jun 15/2016 EFTA00812382 L CFM56 ENGINES (CFM56-7) co_fronsc EFFECTIVITY MU AU. 737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL a) If you find and correct the cause, do the test again at the first power level that failed. b) If you do not find the cause, use your airline policy to make the decision if the engine must be replaced. END OF TASK 71-00-00 Page 526 D633A101-BBJ Jun 15/2016 !CCM 'Ronne rim • CayIr2 2 unputioaa WV\ - Sea OA 109* /W I'S.' EFTA00812383 L CFM56 ENGINES (CFM56-7) iZtdirOSZAW 737.600/70018001900 AIRCRAFT MAINTENANCE MANUAL SUBTASK 71-000007040$F00 (11) If the test is to get vibration data for an on-board fan trim balance, view the flight history data (TASK 71-00-00-750-802-F00 or TASK 71-00.00-750-806-F00 or TASK 71-00-00-750.805-F00 or TASK 71-00-00-750-804-F00 or TASK 71-00-00-750-803-F00). SUSTASK 7140-004110401-FCC (12) If the vibration indications for the fan and low pressure turbine rotor (N1) is more than 4.0 units or is less than 4.0 units with engine noise or rumble, do the fault isolation procedure for high engine vibration FfM 71-05 TASK 808. SUSTASK 71.0040410-002-F00 (13) If the vibration indications for the high pressure compressor and turbine (N2) is more than 3.0 units, do the fault isolation procedure for high engine vibration FIM 71-05 TASK 808. I. Put the Airplane Back to Its Usual Condition SWITASK 71.00-00-0804014T4 (1) If you installed the portable engine balancing system. COM-3932. remove the analyzer. SUSTASK 71404F010-02SF00 (2) If you installed the analyzer. COM-1562, do these steps to remove the analyzer: (a) (b) (c) Disconnect the analyzer, COM-1562 from the test box, SPL-2415. Do this step: open this access panel: Number Name/Location 117A Electronic Equipment Access Door Remove the test box, SPL-2415 from the flight compartment window and close the window. (d) Disconnect the test box, SPL-2415 from the front panel of the airborne vibration monitor (AVM) signal conditioner. (e) Remove the analyzer. COM-1562 from the flight compartment. (f) Do this step: Close this access panel: Number Name/Location 117A Electronic Equipment Access Door END OF TASK A. General (1) The acceleration check is a good test for transient performance analysis of the engine. (a) Do not use the test by itself to accept or reject an engine. (2) Do this test to make sure the engine has usual acceleration performance. B. References Reference Title 24-22-00-660-811 Supply Electrical Power (NB 201) 71-00.00.700.819-F00 Stop the Engine Procedure (Usual Engine Stop) (PM 201) EFFECTIVITY BBJ ALL 71-00-00 D633A101-BBJ 800,4 PRCPRIETARY . Cavyaga a arcaasaM at • ate O. ara kt deal* Page 550 Oct 15/2016 EFTA00812384 CFM56 ENGINES (CFM56-7) (Continued) Reference 71-00-00-800-805-F00 71-00-00-800-807-F00 73-21-00-740-803-F00 FIM 73-05 TASK 814 Fifirostsw 737-60017001800/900 AIRCRAFT MAINTENANCE MANUAL Title Engine Ground Safety Precautions (P/B 201) Start the Engine Procedure (Selection) (P/B 201) EEC BITE TEST- RECENT FAULTS (P/B 501) Engine is Slow to Accelerate - Fault Isolation C. Tools/Equipment Reference Description Thermometer - Alcohol/Mercury (or equivalent meter meets task requirements) Timer - Stop Watch, Accurate to 1 Second $TD-1122 STD-1139 D. Location Zones Zone Area 211 Flight Compartment - Left 212 Flight Compartment - Right 411 Engine 1 - Engine 421 Engine 2 - Engine E. Acceleration Check SUSTASK 714040470091400 CAUTION: DO NOT USE THE TOTAL TEMPERATURE INDICATION FROM THE AIRPLANE FOR THE AMBIENT AIR TEMPERATURE. THIS WILL PREVENT AN INCORRECT TRIM TARGET SELECTION. CAUTION: DO NOT PUT A MERCURY THERMOMETER ON THE AIRPLANE. MERCURY (FROM A BROKEN THERMOMETER) CAN CAUSE DAMAGE TO THE AIRPLANE COMPONENTS. (1) Use a thermometer, STD-1122 to get the ambient air temperature (OAT) in the shade of the nose wheel well. (a) Record the OAT on the data sheet. SUBTASK 710000470417400 (2) Use the OAT to get the N1 target speed and the N2 starting point: (a) (b) (c) For N1, use the MPA Test Table - 70% N1 Corrected Fan Speed (Figure 504). For N2, use the (Table 510). Record the N1 and N2 speeds for the OAT on the data sheet. SUBTASK 714040410.1.2.F00 (3) If not already done, do this task: Supply Electrical Power, TASK 24-22-00.860-811. SUBTASK 71-00404004.3400 WARNING: MAKE SURE THAT YOU OBEY ALL THE INSTRUCTIONS AND PRECAUTIONS WHEN YOU OPERATE AN ENGINE AT HIGH POWER. REFER TO THIS TASK: ENGINE GROUND SAFETY PRECAUTIONS ENGINE GROUND SAFETY PRECAUTIONS. TASK 71-00-00-800-805-F00. IF YOU DO NOT OBEY THE INSTRUCTIONS AND PRECAUTIONS, INJURIES TO PERSONS AND DAMAGE TO EQUIPMENT CAN OCCUR. (4) Do this task: Start the Engine Procedure (Selection), TASK 71-00-00.800.807-F00. EFFECTIVITY BBJ ALL 71-00-00 D633A101-BBJ 60ENCi PROPRIETARY • C; c, OIc,MfC ASH.. Sn IA NV* b *Ws Page 551 Oct 15/2016 EFTA00812385 L CFM56 ENGINES (CFM56-7) Son's 737-600/7001800/900 AIRCRAFT MAINTENANCE MANUAL (a) Make sure the BLEED 1 and BLEED 2 switches are in the OFF position. (b) Set the applicable GEN switch to the OFF position and release. NOTE: This will remove the load from the IDG, if it is not already removed. 1) Make sure the applicable GEN OFF BUS light comes on. (c) Let the engine become stable at the idle-power position for five minutes. SWAIM 714044450.1114400 (5) Make sure that the applicable switches on the overhead panel, P5, are in the OFF position: (a) WING ANTI-ICE (b) ENG ANTI-ICE 1 or 2. SUSTASK 71-0040460.145•PIN (6) Make sure the PROBE HEAT "A" or "B" switch on the overhead panel. P5, is in the ON position. NOTE: For engine operation at high power, the EEC can go into Alternate Mode operation if neither pilot probe is heated. 5VSTASK 714044-11.0.1.5400 (7) Monitor all engine parameters. (a) Carefully monitor the EGT and N2 indications. SUMS( 7140.00400-001-r-00 (8) To do the acceleration check with the N1 and N2 speeds, use a stopwatch. STD-1139 and do these thrust lever movements: (a) Slowly move the applicable forward thrust lever to 5% N1 speed more than the N1 target speed that you got from the MPA Test Table (70% N1) (Figure 504). (b) Mark the thrust lever position (control stand) with a piece of tape or pencil. 1) Minimize the amount of time spent at more than idle. (c) To decelerate, slowly move the applicable forward thrust lever back to the N2 starting point +/-0.3% (Table 510). (d) When the engine parameters are stable, quickly move the thrust lever to the marked position. (e) Start the stopwatch at the initial thrust lever movement. (1) Stop the stopwatch when N1 is at the N1 MPA target speed (not target + 5%). (g) Slowly move the applicable thrust lever back to the idle position. (h) Record the acceleration time on the data sheet. (i) If the test is performed above sea level. subtract 0.25 seconds for each 1000 feet altitude from the recorded acceleration time. 1) Record the adjusted acceleration time on the data sheet. (j) Make sure the adjusted acceleration time is less than 6.3 seconds. (k) If the adjusted acceleration time is not in the limits, do this task: Engine is Slow to Accelerate • Fault Isolation. FIM 73-05 TASK 814. 3VIITASK 7140-00460.1117-r00 (9) When the acceleration check is complete, do these tasks: EFFECTIVITY SBJ ALL 71-00-00 Page 552 D633A101-BBJ Oct 15/2016 BOEIC PROPFICAerr CwygtO tleptailv4 Wolk -6« 6* Part, anhis EFTA00812386 L CFM56 ENGINES (CFM56-7) cbsraPanno 737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL BBJ 001-004, 006, 008-018, 020, 021, 023-026, 028-037, 039, 040, 042, 043, 061, 064, 068, 070-072, 075, 076, 078, 079, 082, 083, 086, 087, 091-095, 097-099, 111-114, 116-119, 121, 122. 124, 125, 401, 404, 405, 407, 409, 410, 415-417, 901-905 PRE SB 737-30A1063 (a) Put the Probe Heat 'A' and "13" switches on the overhead panel. P5, to the OFF position. SEW 005, 007, 019, 022, 027, 038, 041, 062, 063, 066, 073, 077, 080, 085, 096, 120, 123, 126.399, 402, 403, 406, 408, 412-414, 418-422, 906-999; BBJ 001-004, 006, 008-018, 020, 021, 023-026, 028-037, 039, 040, 042, 043, 061. 064, 068, 070-072, 075iii 078, 079, 082, 083, 086. 087, 091-095, 097-099, 111-114, 116-119, 121, 122, 124, 125, 401, 404407, 409, 410, 415-417, 901.905 POST SB 737-30A1063 (b) Put the Probe Heat 'A" and "B" switches on the overhead panel. P5. to the AUTO position. BBJ ALL (c) Stop the Engine Procedure (Usual Engine Stop), TASK 71-00-00-700-819-F00 SMARM 71-00404150-4$8400 (1 0) Do this task: EEC BITE TEST - RECENT FAULTS, TASK 73-21-00-740-803-F00. SMMOK7I0040404040) (11) The table below shows the N2/OAT Acceleration Test data (Table 510): Table 510/71-00-00-993-882-F00 OAT Deg F (C) %N2 OAT Dog F (C) %N2 OAT Deg F (C) %N2 OAT Deg F (C) %N2 -40 (40) 65.0 1 (-17) 68.1 43 (6) 71.1 84 (29) 74.0 -38 (-39) 65.1 3 (-16) 68.3 45 (7) 71.3 86 (30) 74.2 -36 (-38) 65.3 5 (-15) 68.4 46 (8) 71.4 88 (31) 74.3 -35 (-37) 65.4 7 (-14) 68.6 48 (9) 71.5 90 (32) 74.4 -33 (-36) 65.5 91-13) 68.7 50(10) 71.7 91 (33) 74.5 -31 (-35) 65.7 10 (-12) 68.8 52 (11) 71.8 93 (34) 74.6 /29 (-34) 65.8 12 (-11) 69.0 54 (12) 71.9 95 (35) 74.8 -27 (-33) 66.0 14 (-10) 69.1 55 (13) 72.0 97 (36) 74.9 -26 (-32) 66.1 16 (-9) 69.2 57 (14) 72.2 99 (37) 75.0 -24 (-31) 66.2 18 (-8) 69.4 59 (15) 72.3 100 (38) 75.1 -22 (-30) 66.4 19 (-7) 69.5 61 (16) 72.4 102 (39) 75.3 -20 (-29) 66.5 21 (-6) 69.6 63 (17) 72.6 104 (40) 75.4 -18 (-28) 66.7 23 (-5) 69.7 64 (18) 72.7 106 (41) 75.5 -17 (-27) 66.8 25 (-4) 69.9 66 (19) 72.8 108 (42) 75.6 -15 (-26) 66.9 27 (-3) 70.0 68 (20) 72.9 109 (43) 75.7 -13 (-25) 67.1 28 (-2) 70.1 70 (21) 73.0 111 (44) 75.9 -11 (-24) 67.2 30 (-1) 70.3 72 (22) 73.2 113 (45) 76.0 -9 (-23) 67.4 32 (0) 70.4 73 (23) 73.3 115 (46) 76.1 -8 (-22) 67.5 34 (1) 70.5 75 (24 M23.. 117 (47) 76.2 -6 (-21) 67.6 36 (2) 70.6 77 (25) 73.5 118 (48) 76.3 -4 (-20) 67.8 37 (3) 70.8 79 (26) _ 73.7 120 (49) 76.5 EFFECTIVITY BBJ ALL 71-00-00 Page 553 0633A101-BBJ BOENO PROPRIETARY C04/19.4-DtARAARAneo WA% . Soo ale Po?. So *cab Oct 15/2016 EFTA00812387 L CFM56 ENGINES (CFM56-7) .__Bear/NC 737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL Table 510/71-00-00-993.882-F00 (Continued) OAT Deg F (CI %N2 OAT Deg F (C) %N2 OAT Deg F (C) %N2 OAT Deg F (C) %/42 -2 (-19) 67.9 39 (4) 70.9 81 (27) 73.8 122 (50) 76.6 0 (-18) 68.0 41 (5) 71.0 82 (28) 73.9 END OF TASK TASK 71.00-00-700-816-F00 10. Test 9 - Replacement Engine Test (Pretested) A. General (1) This test does the checks that are necessary when a new pretested engine is installed on an airplane. (2) A pretested engine is a complete engine, with or without the Boeing quick-engine-change (QEC) parts, that was operated satisfactorily in an approved test cell or if engine was previously removed for convenience or time staggering. (3) If the replacement engine was not pretested, do this procedure: Test 10 - Replacement Engine Test (Untested) to do a check of the engine installation and operation. (4) This procedure will do all the necessary checks for the Boeing QEC components on the engine. B. References Reference Title 24-11-00-700-802 24-11-00-700-803 26-11-00-710-801 29.11.00.860-804 30-21-00-710-801 38.00-00.860-801 36-11-04-400-801 71.00-03-600-803-F00 71-71-00-200-801-F® 73-21-00-700-804-F00 73-21-00-700-808-F00 73-21-00-700-809-F00 73.21.00-740.803-F00 73.21.00.800.801-F® 79-00-00-710-806-F00 C. Location Zones Zone Area Operational Test For Number 1 IDG (MB 501) Operational Test For Number 2 IDG (P/B 501) Engine Fire Detection - Operational Test (P/B 501) Hydraulic System A or B Pressurization with an Engine-Driven Pump (EDP) (P/B 201) Engine Cowl Anti-Icing - Operational Test (NB 501) Supply Pressure to the Pneumatic System (Selection) (NB 201) PRSOV Installation (NS 401) Depreservation of an Engine On-Wing (Task Selection) (P/B 201) Engine Vents and Drains Inspection (P/B 601) EEC TEST (P/B 501) IDENT/CONFIG (P/B 501) EEC Discretes Test (P/B 501) EEC BITE TEST - RECENT FAULTS (MB 501) Erase All EEC Faults (P/B 501) DMS Operational Check (P/B 601) 211 Flight Compartment - Left 212 Flight Compartment - Right 411 Engine 1 - Engine 421 Engine 2 - Engine FI EFFECTIVITY Irl ALL 0633A101-BBJ ROME PROPRIETARY. Cconhet 1,00.0..-es fon .Sceut. pew ice ckno i 71-00-00 Page 554 Oct 15/2016 EFTA00812388 L CFM56 ENGINES (CFM56-7) i?;Lfirostsec 737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL OAT XN1 TARGET MAX EGT - 'C ENGINE MODEL F-7> F 'C 10.57. 7827/81 7827 7826 826/81 7826/82 7824/81 7824 7822/81 7822 7820 -40 -40 58.6 443 461 465 501 503 524 553 -38 -39 58.7 446 464 468 504 506 527 556 -36 -38 58.8 450 468 472 508 510 531 560 -35 -37 58.9 453 471 475 511 513 534 563 -33 -36 59.1 456 474 478 514 516 537 566 -31 -35 59.2 460 478 482 518 520 541 570 -29 -34 59.3 463 481 485 521 523 544 573 -27 -33 59.4 466 484 488 524 526 547 576 -26 -32 59.5 470 488 492 528 530 551 580 -24 -31 59.7 473 4 491 495 531 533 554 583 -22 -30 59.8 476 4 494 498 534 536 557 586 -20 -29 59.9 480 4 498 502 538 540 561 590 -18 -28 60.0 483 4 501 505 541 543 564 593 -17 -27 60.2 486 4 504 508 544 546 567 596 -15 -26 60.3 490 4 508 512 548 550 571 600 -13 -25 60.4 493 4 511 515 551 553 574 603 -11 -24 60.5 496 4 514 518 554 556 577 606 -9 -23 60.6 498 4 516 520 556 558 579 608 -8 -22 60.7 501 5 519 523 559 561 582 611 -6 -21 60.9 503 5 521 525 561 563 584 613 -4 -20 61.0 506 5 524 528 564 566 587 616 -2 -19 61.1 508 5 526 530 566 568 589 618 0 -18 61.2 511 51 529 533 569 571 592 621 1 -17 61.3 513 51 531 535 571 573 594 623 3 -16 61.5 516 51 534 538 574 576 597 626 5 -15 61.6 518 5 536 540 576 578 599 628 7 -14 61.7 521 5 539 543 579 581 602 631 9 -13 61.8 524 5 542 546 582 584 605 634 10 -12 61.9 526 5 544 548 584 586 607 636 12 -11 62.0 528 546 550 586 588 609 638 14 -10 62.2 531 549 553 589 591 612 641 16 -9 62.3 533 551 555 591 593 614 643 18 -8 62.4 536 554 558 594 596 617 646 19 -7 62.5 538 556 560 596 598 619 648 21 -6 62.6 541 559 563 599 601 622 651 23 -5 62.7 543 561 565 601 603 624 653 25 -4 62.9 546 564 568 604 606 627 656 11- >APPLICABLE TO ALL /3, /3F, AND -7BE RATINGS EFFECTIVITY BBJ ALL MPA Test Table corrected Fan Speed) Figure 503/71-00-00-990-820-F00 (Sheet 1 of 6) D633A101-BBJ PlinPRIE PAY • encor thipvtinnsl ?Ws • See ilk :49e be Is GMM-1156640-00-A (MOD) GIS.SO IS SGOOMI785_V4 71-00-00 Page 527 Oct 15/2015 EFTA00812389 L CFM56 ENGINES (CFM56-7) Ofi ir4C7SZAW 737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL OAT 2N1 TARGET MAX EGT - C ENGINE MODEL r> 'F •C :0.52 7827/B1 7827 7826 826181 7826/82 7824/81 7824 7822/81 7822 7820 27 -3 63.0 548 566 570 606 608 629 658 28 -2 63.1 550 568 572 608 610 631 660 30 -1 63.2 552 570 574 610 612 633 662 32 0 63.3 555 573 577 613 615 636 665 34 1 63.4 557 5 575 579 615 617 638 667 36 2 63.5 559 5 577 581 617 619 640 669 37 3 63.7 561 5 579 583 619 621 642 671 39 4 63.8 563 5 581 585 621 623 644 673 41 5 63.9 565 583 587 623 625 646 675 43 6 64.0 567 585 589 625 627 648 677 45 1 64.1 570 588 592 628 630 651 680 46 8 64.2 572 590 594 630 632 653 682 48 9 64.3 574 592 596 632 634 655 684 50 10 64.4 576 594 598 634 636 657 686 52 11 64.6 578 596 600 636 638 659 688 54 12 64.7 579 597 601 637 639 660 689 55 13 64.8 581 599 603 639 641 662 691 57 14 64.9 583 601 605 641 643 664 693 59 15 65.0 585 603 607 643 645 666 695 61 16 65.1 586 604 608 644 646 667 696 63 17 65.2 588 606 610 646 648 669 698 64 18 65.3 590 608 612 648 650 671 700 66 19 65.4 592 610 614 650 652 673 702 68 20 65.6 594 612 616 652 654 675 704 70 21 65.7 596 614 618 654 656 677 706 72 22 65.8 598 616 620 656 658 679 708 73 23 65.9 600 618 622 658 660 681 710 75 24 66.0 602 620 624 660 662 683 712 77 25 66.1 604 622 626 662 664 685 714 79 26 66.2 606 624 628 664 666 687 716 81 27 66.3 608 626 630 666 668 689 718 82 28 66.4 611 I 629 633 669 671 692 721 84 29 66.5 613 631 635 671 673 694 723 86 30 66.6 615 633 637 673 675 696 725 88 31 66.8 617 635 639 675 677 698 727 90 32 66.9 619 637 641 677 679 700 729 91 33 67.0 621 639 643 679 681 702 731 P-7>APPLICABLE TO ALL /3, /3F, AND -7BE RATINGS rB -- EFFECTIVITY EtJ ALL GMM-1156641-00-A (MOD) Gan17 S00065417862/4 MPA Test Table Corrected Fan Speed) Figure 503/71-00 - - -F00 (Sheet 2 of 6) D633A101-BRU anetho PRognimr • coovent Chlft440•011.-n Fwr CHI peon I.. -leak 71-00-00 Page 528 Oct 15/2015 EFTA00812390 L CFM56 ENGINES (CFM56-7) gilift7SZAW 737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL OAT Oil TARGET MAX EGT - C ENGINE MODEL EC> 7827 7826 F 'C :0.5% 7827/840, 7826/B1 7824/B1 7824 7B22/B1 7822 7820 7826/82 93 34 67.1 623 641 645 681 683 704 733 95 35 67.2 625 643 647 683 685 706 735 97 36 67.3 628 646 650 686 688 709 738 99 37 67.4 630 648 652 688 690 711 740 100 38 67.5 632 650 654 690 692 713 742 102 39 67.6 634 652 656 692 694 715 744 104 40 67.7 637 655 659 695 697 718 747 106 41 67.8 639 657 661 697 699 720 749 108 42 67.9 641 659 663 699 701 722 751 109 43 68.0 643 661 665 701 703 724 753 111 44 68.1 645 663 667 703 705 726 755 113 45 68.2 647 665 669 705 707 728 757 115 46 68.4 649 667 671 707 709 730 759 117 47 68.5 651 669 673 709 711 732 761 118 48 68.6 653 671 675 711 713 734 763 120 49 68.7 655 673 677 713 715 736 765 122 50 68.8 657 675 679 715 717 738 767 7-7>APPLICABLE TO ALL /3, /3F, AND -7BE RATINGS EFFECTIVITY BBJ ALL MPA Test Table orrected Fan Speed) Figure 503/71-NgeFOO (Sheet 3 of 6) D633A101-BBJ HIE Mr; PW)PSIETAR? • C.,./ite ":0•Atail•ed No" • Sr. eue P.Oe m. '<Wit GMM-1156641 -00 -A O86614 500069 0787_1/ 4 71-00-00 Page 529 Oct 15/2015 EFTA00812391 L CFM56 ENGINES (CFM56-7) cafinansfc 737.600/700/800/900 AIRCRAFT MAINTENANCE MANUAL OAT XN1 TARGET MAX XN2 ENGINE MODEL N::› •F C ±0.5X 7827/81 7827 7826 826/82 7826/82 7824/81 7824 7022/81 7822 7820 -40 -40 58.6 79.8 7 79.7 80.3 80.9 81.5 81.6 81.9 -38 -39 58.7 80.0 8 79.9 80.5 81.1 81.7 81.8 82.1 -36 -38 58.8 80.1 8 80.0 80.6 81.2 81.8 81.9 82.2 -35 -37 58.9 80.3 8 80.2 80.8 81.4 82.0 82.1 82.4 -33 -36 59.1 80.5 8 80.4 81.0 81.6 82.2 82.3 82.6 -31 -35 59.2 80.6 8 80.5 81.1 81.7 82.3 82.4 82.7 -29 -34 59.3 80.8 8 80.7 81.3 81.9 82.5 82.6 82.9 -27 -33 59.4 80.9 80.8 81.4 82.0 82.6 82.7 83.0 -26 -32 59.5 81.1 81.0 81.6 82.2 82.8 82.9 83.2 -24 -31 59.7 81.3 81.2 81.8 82.4 83.0 83.1 83.4 -22 -30 59.8 81.4 81.3 81.9 82.5 83.1 83.2 83.5 -20 -29 59.9 81.6 81.5 82.1 82.7 83.3 83.4 83.7 -18 -28 60.0 81.7 81.6 82.2 82.8 83.4 83.5 83.8 -17 -27 60.2 81.9 81.8 82.4 83.0 83.6 83.7 84.0 -15 -26 60.3 82.0 81.9 82.5 83.1 83.7 83.8 84.1 -13 -25 60.4 82.2 82.1 82.7 83.3 83.9 84.0 84.3 -11 -24 60.5 82.4 82.3 82.9 83.5 84.1 84.2 84.5 -9 -23 60.6 82.5 5 82.4 83.0 83.6 84.2 84.3 84.6 -8 -22 60.7 82.7 7 82.6 83.2 83.8 84.4 84.5 84.8 -6 -21 60.9 82.8 8 82.7 83.3 83.9 84.5 84.6 84.9 -4 -20 61.0 83.0 0 82.9 83.5 84.1 84.7 84.8 85.1 -2 -19 61.1 83.2 2 83.1 83.7 84.3 84.9 85.0 85.3 0 -18 61.2 83.3 3 83.2 83.8 84.4 85.0 85.1 85.4 1 -17 61.3 83.5 5 83.4 84.0 84.6 85.2 85.3 85.6 3 -16 61.5 83.7 7 83.6 84.2 84.8 85.4 85.5 85.8 5 -15 61.6 83.8 8 83.7 84.3 84.9 85.5 85.6 85.9 7 -14 61.7 84.0 0 83.9 84.5 85.1 85.7 85.8 86.1 9 -13 61.8 84.2 2 84.1 84.7 85.3 85.9 86.0 86.3 10 -12 61.9 84.3 3 84.2 84.8 85.4 86.0 86.1 86.4 12 -11 62.0 84.5 5 84.4 85.0 85.6 86.2 86.3 86.6 14 -10 62.2 84.6 6 84.5 85.1 85.7 86.3 86.4 86.7 16 -9 62.3 84.8 8 84.7 85.3 85.9 86.5 86.6 86.9 18 -8 62.4 85.0 0 84.9 85.5 86.1 86.7 86.8 87.1 19 -7 62.5 85.1 1 85.0 85.6 86.2 86.8 86.9 87.2 21 -6 62.6 85.3 85.2 85.8 86.4 87.0 87.1 87.4 23 -5 62.7 85.5 • 85.4 86.0 86.6 87.2 87.3 87.6 25 -4 62.9 85.6 . 85.5 86.1 86.7 87.3 87.4 87.7 Ll_2>APPLICABLE TO ALL /3, /3F, AND -7BE RATINGS EFFECTIVITY BBJ ALL • MPA Test Table Corrected Fan Speed) Figure 503/71-00-00- -F00 (Sheet 4 of 6) D633A101-BBJ POCINGPROCCIETARv • cccr kNaitozis4ti F.se Mn pro Pe Mints GMM-1156642-00-A (MOD) kiat526 Sr/36W Ult./4 71-00-00 Page 530 Oct 15/2015 EFTA00812392 L CFM56 ENGINES (CFM56-7) ejLisrortivo 737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL OAT ZN1 TARGET MAX XN2 ENGINE MODEL F C 20.57. 7B27/B1 7827 7B26 m ir e26/91 7826/82 7824/61 7824 7822/B1 7622 7620 27 -3 63.0 85.8 85.7 86.3 86.9 87.5 87.6 87.9 28 -2 63.1 86.0 85.9 86.5 87.1 87.7 87.8 88.1 30 -1 63.2 86.1 86.0 86.6 87.2 87.8 87.9 88.2 32 0 63.3 86.3 86.2 86.8 87.4 88.0 88.1 88.4 34 1 63.4 86.5 86.4 87.0 87.6 88.2 88.3 88.6 36 2 63.5 86.6 86.5 87.1 87.7 88.3 88.4 88.7 37 3 63.7 86.8 86.7 87.3 87.9 88.5 88.6 88.9 39 4 63.8 87.0 86.9 87.5 88.1 88.7 88.8 89.1 41 5 63.9 87.1 87.0 87.6 88.2 88.8 88.9 89.2 43 6 64.0 87.3 • 87.2 87.8 88.4 89.0 89.1 89.4 45 7 64.1 87.4 87.3 87.9 88.5 89.1 89.2 89.5 46 8 64.2 87.6 . 87.5 88.1 88.7 89.3 89.4 89.7 48 9 64.3 87.8 . • 87.7 88.3 88.9 89.5 89.6 89.9 50 10 64.4 87.9 • • 87.8 88.4 89.0 89.6 89.7 90.0 52 11 64.6 88.1 88.0 88.6 89.2 89.8 89.9 90.2 54 12 64.7 88.3 88.2 88.8 89.4 90.0 90.1 90.4 55 13 64.8 88.4 88.3 88.9 89.5 90.1 90.2 90.5 57 14 64.9 88.6 88.5 89.1 89.7 90.3 90.4 90.7 59 15 65.0 88.8 88.7 89.3 89.9 90.5 90.6 90.9 61 16 65.1 88.9 88.8 89.4 90.0 90.6 90.7 91.0 63 17 65.2 89.1 89.0 89.6 90.2 90.8 90.9 91.2 64 18 65.3 89.2 . 89.1 89.7 90.3 90.9 91.0 91.3 66 19 65.4 89.4 89.3 89.9 90.5 91.1 91.2 91.5 68 20 65.6 89.6 8 89.5 90.1 90.7 91.3 91.4 91.7 70 21 65.7 89.7 8 89.6 90.2 90.8 91.4 91.5 91.8 72 22 65.8 89.9 8 89.8 90.4 91.0 91.6 91.7 92.0 73 23 65.9 90.0 89.9 90.5 91.1 91.7 91.8 92.1 75 24 66.0 90.2 ' 90.1 90.7 91.3 91.9 92.0 92.3 77 25 66.1 90.3 • • 90.2 90.8 91.4 92.0 92.1 92.4 79 26 66.2 90.5 90.4 91.0 91.6 92.2 92.3 92.6 81 27 66.3 90.6 90.5 91.1 91.7 92.3 92.4 92.7 82 28 66.4 90.8 • 90.7 91.3 91.9 92.5 92.6 92.9 84 29 66.5 90.9 • 90.8 91.4 92.0 92.6 92.7 93.0 86 30 66.6 91.1 9 91.0 91.6 92.2 92.8 92.9 93.2 88 31 66.8 91.3 9 91.2 91.8 92.4 93.0 93.1 93.4 90 32 66.9 91.4 9 91.3 91.9 92.5 93.1 93.2 93.5 91 33 67.0 91.6 9 91.5 92.1 92.7 93.3 93.4 93.7 FIMAPPLICABLE TO ALL /3, /3F AND -7BE RATINGS EFFECTIVITY BBJ ALL MPA Teat Table rected Fan Speed) Figure 503/71.-0700, 990M0 (Sheet 5 of 6) 0633A101-BBJ *NM PROpkirrpfre • ccpecht aPh.°+•O1a rvan ra. dosr, GMM-1156642-00-A (MOD) 1-145511S0006581789_1/4 71-00-00 Page 531 Oct 15/2015 EFTA00812393 L CFM56 ENGINES (CFM56-7) gifirostivo 737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL OAT 2N1 TARGET MAX XN2 ENGINE MODEL ' '? *F C ±0.5Z 7827/81 7827 7826 amit26/B1 7824/81 7824 7822/81 7822 7820 26/82 93 34 67.1 91.7 9 91.6 92.2 92.8 93.4 93.5 93.8 95 35 67.2 91.9 9 91.8 92.4 93.0 93.6 93.7 94.0 97 36 67.3 92.0 9 91.9 92.5 93.1 93.7 93.8 94.1 99 37 67.4 92.2 9 92.1 92.7 93.3 93.9 94.0 94.3 100 38 67.5 92.3 9 92.2 92.8 93.4 94.0 94.1 94.4 102 39 67.6 92.5 92.4 93.0 93.6 94.2 94.3 94.6 104 40 67.7 92.6 92.5 93.1 93.7 94.3 94.4 94.7 106 41 67.8 92.8 92.7 93.3 93.9 94.5 94.6 94.9 108 42 67.9 92.9 92.8 93.4 94.0 94.6 94.7 95.0 109 43 68.0 93.1 93.0 93.6 94.2 94.8 94.9 95.2 111 44 68.1 93.2 93.1 93.7 94.3 94.9 95.0 95.3 113 45 68.2 93.4 93.3 93.9 94.5 95.1 95.2 95.5 115 46 68.4 93.5 93.4 94.0 94.6 95.2 95.3 95.6 117 47 68.5 93.7 93.6 94.2 94.8 95.4 95.5 95.8 118 48 68.6 93.8 93.7 94.3 94.9 95.5 95.6 95.9 120 49 68.7 94.0 9 93.9 94.5 95.1 95.7 95.8 96.1 122 50 68.8 94.1 9 94.0 94.6 95.2 95.8 95.9 96.2 i -->APPLICABLE TO ALL /3, /3F AND -7BE RATINGS EFFECTIVITY BBJ ALL GMM-1156644 -00-A (MOD) Hans? $000656i 700_V4 MPA Test Table allalCorrected Fan Speed) Figure 503171-00-00.990.820-F00 (Sheet 6 of 6) 71-00-00 Page 532 D633A101-BBJ Oct 15/2015 tiOCING /*COMET/AY CON091. %TA 5.+IS ratwir losk EFTA00812394 L CFMS6 ENGINES (CFMS6.7) co sfi rOSZAW 737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL OAT XN1 TARGET MAX EGT - C ENGINE MODEL I > F C :0.57. 7827/81 7827 7626 826/B 7826/82 7B24/81 7824 7822/81 7822 7620 -40 -40 63.1 485 503 507 543 545 566 595 -38 -39 63.2 489 507 511 547 549 570 599 -36 -38 63.4 493 511 515 551 553 574 603 -35 -37 63.5 496 514 518 554 556 577 606 -33 -36 63.6 500 518 522 558 560 581 610 -31 -35 63.7 503 2 521 525 561 563 584 613 -29 -34 63.9 506 5 524 528 564 566 587 616 -27 -33 64.0 509 8 527 531 567 569 590 619 -26 -32 64.1 511 0 529 533 569 571 592 621 -24 -31 64.3 514 3 532 536 572 574 595 624 -22 -30 64.4 517 6 535 539 575 577 598 627 -20 -29 64.5 519 537 541 577 579 600 629 -18 -28 64.7 522 540 544 580 582 603 632 -17 -27 64.8 525 543 547 583 585 606 635 -15 -26 64.9 528 546 550 586 588 609 638 -13 -25 65.0 530 548 552 588 590 611 640 -11 -24 65.2 533 551 '555 591 593 614 643 -9 -23 65.3 536 554 558 594 596 617 646 -8 -22 65.4 538 556 560 596 598 619 648 -6 -21 65.6 541 559 563 599 601 622 651 -4 -20 65.7 543 561 565 601 603 624 653 -2 -19 65.8 546 564 568 604 606 627 656 0 -18 65.9 549 567 571 607 609 630 659 1 -17 66.1 551 569 573 609 611 632 661 3 -16 66.2 554 572 576 612 614 635 664 5 -15 66.3 557 575 579 615 617 638 667 7 -14 66.4 559 577 581 617 619 640 669 9 -13 66.6 561 579 583 619 621 642 671 10 -12 66.7 564 582 586 622 624 645 674 12 -11 66.8 566 584 588 624 626 647 676 14 -10 66.9 569 587 591 627 629 650 679 16 -9 67.1 571 589 593 629 631 652 681 18 -8 67.2 574 592 596 632 634 655 684 19 -7 67.3 576 594 598 634 636 657 686 21 -6 67.4 579 597 601 637 639 660 689 23 -5 67.6 581 599 603 639 641 662 691 25 -4 67.7 584 602 606 642 644 665 694 IT- T>APPLICABLE TO ALL /3, /3F, AND -78E RATINGS EFFECTIVITY BBJ ALL GMM-1156645 -00-A (MOD) 085094 SC008581791_94 PAPA Test Table , Corrected Fan Speed) Figure 504/71-00-00-990-821-F00 (Sheet 1 of 6) 0633A101-BBJ Karrtg. PROPRIC Mgt. • Ctsg-gS " tTo-tilshed gicek • Ste %. page S SSP 71-00-00 Page 533 Oct 15,2015 EFTA00812395 CFM56 ENGINES (CFM56-7) APOSZAllia 737-600/7001800/900 AIRCRAFT MAINTENANCE MANUAL OAT XN1 TARGET MAX EGT - C ENGINE MODEL 0::› .F 'C ±0.52 7827/81 7827 IIIIIII77026/81 7826 7824/81 826/82 7824 71322/B1 7822 7820 27 -3 67.8 586 604 608 644 646 667 696 28 -2 67.9 588 606 610 646 648 669 698 30 -1 68.1 591 609 613 649 651 672 701 32 0 68.2 593 611 615 651 653 674 703 34 1 68.3 595 613 617 653 655 676 705 36 2 68.4 598 616 620 656 658 679 708 37 3 68.6 600 618 622 658 660 681 710 39 4 68.7 602 620 624 660 662 683 712 41 5 68.8 605 623 627 663 665 686 715 43 6 68.9 607 625 629 665 667 688 717 45 7 69.0 609 627 631 667 669 690 719 46 8 69.2 611 6 629 633 669 671 692 721 48 9 69.3 613 6 631 635 671 673 694 723 50 10 69.4 616 6 634 638 674 676 697 726 52 11 69.5 618 6 636 640 676 678 699 728 54 12 69.6 621 639 643 679 681 702 731 55 13 69.8 623 641 645 681 683 704 733 57 14 69.9 625 643 647 683 685 706 735 59 15 70.0 627 645 649 685 687 708 737 61 16 70.1 630 648 652 688 690 711 740 63 17 70.2 632 650 654 690 692 713 742 64 18 70.4 634 652 656 692 694 715 744 66 19 70.5 637 655 659 695 697 718 747 68 20 70.6 639 657 661 697 699 720 749 70 21 70.7 641 659 663 699 701 722 751 72 22 70.8 644 662 666 702 704 725 754 73 23 70.9 646 664 668 704 706 727 756 75 24 71.1 648 666 670 706 708 729 758 77 25 71.2 651 669 673 709 711 732 761 79 26 71.3 653 671 675 711 713 734 763 81 27 71.4 655 673 677 713 715 736 765 82 28 71.5 657 675 679 715 717 738 767 84 29 71.7 660 678 682 718 720 741 770 86 30 71.8 662 680 684 720 722 743 772 88 31 71.9 664 682 686 722 724 745 774 90 32 72.0 666 684 688 724 726 747 776 91 33 72.1 668 686 690 726 728 749 778 FI-:›APPLICABLE TO ALL /3, /3F, AND -7BE RATINGS EFFECTIVITY BBJ ALL GMM-1156645 -00-A (MOD) 085423 SOX)6531792_V4 MPA Test Table A/ -82 Corrected Fan Speed) Figure 504/71-00-00-990 1-F00 (Sheet 2 of 6) D633A101-BBJ 'octal ntoppitiaqy . cooesu tiopast.teerb - 9w IS tar lm twat 71-00-00 Page 534 Oct 15/2015 EFTA00812396 L CFMS6 ENGINES (CFM56-7) gifiracess 737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL OAT 7.N1 TARGET MAX EGT - / ENGINE MODEL [ > F C 20.S7. 7827 7827/81 7826 826181 7824/81 7824 7822/B1 7822 7820 7826/82 93 34 72.2 670 688 692 728 730 751 780 95 35 72.3 673 6 691 695 731 733 754 783 97 36 72.5 675 6 693 697 733 735 756 785 99 37 72.6 677 6 695 699 735 737 758 787 100 38 72.7 679 6 697 701 737 739 760 789 102 39 72.8 681 699 703 739 741 762 791 104 40 72.9 684 702 706 742 744 765 794 106 41 73.0 686 704 708 744 746 767 796 108 42 73.1 688 706 710 746 748 769 798 109 43 73.3 690 708 712 748 750 771 800 111 44 73.4 692 710 714 750 752 773 802 113 45 73.5 695 713 717 753 755 776 805 115 46 73.6 697 715 719 755 757 778 807 117 47 73.7 699 717 721 757 759 780 809 118 48 73.8 701 719 723 759 761 782 811 120 49 73.9 703 7 721 725 761 763 784 813 122 50 74.1 705 7 723 727 763 765 786 815 ›APPLICABLE TO ALL /3, /3F, AND -78E RATINGS EFFECTIVITY BBJ ALL GMM -1156646-00-A (MOD) G86652 S00065817MV4 MPA Test Table issaver Corrected Fan Speed) Figure 504/71-00-00-990-821-F00 (Sheet 3 of 6) 71-00-00 Page 535 D633A101-BBJ Oct 15/2015 DOENG PRCPRIETARY • CoPrttP tflooti 041 hOostit • Stt nth PM, lot 'Wok EFTA00812397 L CFM56 ENGINES (CFM56-7) gLISPOSAIAW 737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL OAT ZN1 TARGET MAX 2N2 ENGINE MODEL 0::> ( C d3.5X 7827/61 7827 7826 826181 7826/82 7824/81 7824 7822/81 7822 7820 -40 -40 63.1 81.3 81 81.2 81.8 82.4 83.0 83.1 83.4 -38 -39 63.2 81.5 81 81.4 82.0 82.6 83.2 83.3 83.6 -36 -38 63.4 81.7 8 81.6 82.2 82.8 83.4 83.5 83.8 -35 -37 63.5 81.8 8 81.7 82.3 82.9 83.5 83.6 83.9 -33 -36 63.6 82.0 8 81.9 82.5 83.1 83.7 83.8 84.1 -31 -35 63.7 82.1 8 82.0 82.6 83.2 83.8 83.9 84.2 -29 -34 63.9 82.3 8 82.2 82.8 83.4 84.0 84.1 84.4 -27 -33 64.0 82.5 8 82.4 83.0 83.6 84.2 84.3 84.6 -26 -32 64.1 82.7 8 82.6 83.2 83.8 84.4 84.5 84.8 -24 -31 64.3 82.8 8 82.7 83.3 83.9 84.5 84.6 84.9 -22 -30 64.4 83.0 8 82.9 83.5 84.1 84.7 84.8 85.1 -20 -29 64.5 83.2 8 83.1 83.7 84.3 84.9 85.0 85.3 -18 -28 64.7 83.3 8 83.2 83.8 84.4 85.0 85.1 85.4 -17 -27 64.8 83.5 83 83.4 84.0 84.6 85.2 85.3 85.6 -15 -26 64.9 83.7 83 83.6 84.2 84.8 85.4 85.5 85.8 -13 -25 65.0 83.8 83 83.7 84.3 84.9 85.5 85.6 85.9 -11 -24 65.2 84.0 84 83.9 84.5 85.1 85.7 85.8 86.1 -9 -23 65.3 84.2 84 84.1 84.7 85.3 85.9 86.0 86.3 -8 -22 65.4 84.3 84 84.2 84.8 85.4 86.0 86.1 86.4 -6 -21 65.6 84.5 8 84.4 85.0 85.6 86.2 86.3 86.6 -4 -20 65.7 84.7 8 84.6 85.2 85.8 86.4 86.5 86.8 -2 -19 65.8 84.8 8'. 84.7 85.3 85.9 86.5 86.6 86.9 0 -18 65.9 85.0 8 84.9 85.5 86.1 86.7 86.8 87.1 1 -17 66.1 85.2 8 85.1 85.7 86.3 86.9 87.0 87.3 3 -16 66.2 85.3 8 85.2 85.8 86.4 87.0 87.1 87.4 5 -15 66.3 85.5 8- 85.4 86.0 86.6 87.2 87.3 87.6 7 -14 66.4 85.7 8. 85.6 86.2 84.8 87.4 87.5 87.8 9 -13 66.6 85.9 85 85.8 86.4 87.0 87.6 87.7 88.0 10 -12 66.7 86.0 86 85.9 86.5 87.1 87.7 87.8 88.1 12 -11 66.8 86.2 86 86.1 86.7 87.3 87.9 88.0 88.3 14 -10 66.9 86.4 86 86.3 86.9 87.5 88.1 88.2 88.5 16 -9 67.1 86.5 86 86.4 87.0 87.6 88.2 88.3 88.6 18 -8 67.2 86.7 8- 86.6 87.2 87.8 88.4 88.5 88.8 19 -7 67.3 86.9 86 86.8 87.4 88.0 88.6 88.7 89.0 21 -6 67.4 87.0 87 86.9 87.5 88.1 88.7 88.8 89.1 23 -5 67.6 87.2 8 87.1 87.7 88.3 88.9 89.0 89.3 25 -4 67.7 87.4 87 87.3 87.9 88.5 89.1 89.2 89.5 1-1-->APPLICA8LE TO ALL /3, /3F, AND -78E RATINGS EFFECTIVITY BBJ ALL MPA Test Table (Hillialla Corrected Fan Speed) Figure 504/71-00-00-990-821-F00 (Sheet 4 of 6) 0633A101-BBJ Boum; ononbETARy • COPr5IM Orput•Wel TPA- Re. tl11. pArr kntrinoll GMM-1156645-00-A (MOD) t14 )5 72 $0006f." • 714y4 71-00-00 Page 536 Oct 15/2015 EFTA00812398 L CFM56 ENGINES (CFMS6.7) gtfinsrArzAw 737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL OAT XN1 TARGET MAX XN2 ENGINE MODEL E:> F C t0.5% 7827/61 7827 mm 7826 7826/81 7826/82 7824/81 7824 7822/81 7022 7820 27 -3 67.8 87.5 87.4 88.0 88.6 89.2 89.3 89.6 28 -2 67.9 87.7 87.6 88.2 88.8 89.4 89.5 89.8 30 -1 68.1 87.9 87.8 88.4 89.0 89.6 89.7 90.0 32 0 68.2 88.0 87.9 88.5 89.1 89.7 89.8 90.1 34 1 68.3 88.2 88.1 88.7 89.3 89.9 90.0 90.3 36 2 68.4 88.4 4 88.3 88.9 89.5 90.1 90.2 90.5 37 3 68.6 88.5 5 88.4 89.0 89.6 90.2 90.3 90.6 39 4 68.7 88.7 7 88.6 89.2 89.8 90.4 90.5 90.8 41 5 68.8 88.9 9 88.8 89.4 90.0 90.6 90.7 91.0 43 6 68.9 89.1 1 89.0 89.6 90.2 90.8 90.9 91.2 45 7 69.0 89.2 89.1 89.7 90.3 90.9 91.0 91.3 46 8 69.2 89.4 89.3 89.9 90.5 91.1 91.2 91.5 48 9 69.3 89.6 89.5 90.1 90.7 91.3 91.4 91.7 50 10 69.4 89.7 89.6 90.2 90.8 91.4 91.5 91.8 52 11 69.5 89.9 89.8 90.4 91.0 91.6 91.7 92.0 54 12 69.6 90.1 90.0 90.6 91.2 91.8 91.9 92.2 55 13 69.8 90.2 90.1 90.7 91.3 91.9 92.0 92.3 57 14 69.9 90.4 90.3 90.9 91.5 92.1 92.2 92.5 59 15 70.0 90.5 90.4 91.0 91.6 92.2 92.3 92.6 61 16 70.1 90.7 90.6 91.2 91.8 92.4 92.5 92.8 63 17 70.2 90.9 90.8 91.4 92.0 92.6 92.7 93.0 64 18 70.4 91.0 90.9 91.5 92.1 92.7 92.8 93.1 66 19 70.5 91.2 91.1 91.7 92.3 92.9 93.0 93.3 68 20 70.6 91.4 91.3 91.9 92.5 93.1 93.2 93.5 70 21 70.7 91.5 91.4 92.0 92.6 93.2 93.3 93.6 72 22 70.8 91.7 91.6 92.2 92.8 93.4 93.5 93.8 73 23 70.9 91.8 91.7 92.3 92.9 93.5 93.6 93.9 75 24 71.1 92.0 91.9 92.5 93.1 93.7 93.8 94.1 77 25 71.2 92.2 9 92.1 92.7 93.3 93.9 94.0 94.3 79 26 71.3 92.3 9 92.2 92.8 93.4 94.0 94.1 94.4 81 27 71.4 92.5 9 92.4 93.0 93.6 94.2 94.3 94.6 82 28 71.5 92.6 92.5 93.1 93.7 94.3 94.4 94.7 84 29 71.7 92.8 92.7 93.3 93.9 94.5 94.6 94.9 86 30 71.8 92.9 92.8 93.4 94.0 94.6 94.7 95.0 88 31 71.9 93.1 93.0 93.6 94.2 94.8 94.9 95.2 90 32 72.0 93.3 93.2 93.8 94.4 95.0 95.1 95.4 91 33 72.1 93.4 93.3 93.9 94.5 95.1 95.2 95.5 APPLICABLE TO ALL /3, /3F, AND -7BE RATINGS EFFECTIVITY BBJ ALL GMM-1156648-00—A (MOD) H43591 SO)Ceas 795:14 MPA Test Table corrected Fan Speed) Figure 504/71-00-00-990-821-F00 (Sheet 5 of 6) 0633A101-BBJ SOCING PROPRIG /ARV Corvign c Unput40.1 Win. Ss. MI. Cwq• 71-00-00 Page 537 Oct 1512015 EFTA00812399 L. CFM56 ENGINES (CFM56-7) gifirarszaw 737-6001700/800/900 AIRCRAFT MAINTENANCE MANUAL OAT XN1 TARGET MAX XN2 ENGINE MODEL I---> F C z0.5X 7827/61 7827 7826 7B24/81 7824 7822/31 7822 7820 IIIIIIP7626/81 7826/82 93 34 72.2 93.6 93.5 94.1 94.7 95.3 95.4 95.7 95 35 72.3 93.7 93.6 94.2 94.8 95.4 95.5 95.8 97 36 72.5 93.9 93.8 94.4 95.0 95.6 95.7 96.0 99 37 72.6 94.0 93.9 94.5 95.1 95.7 95.8 96.1 100 38 72.7 94.2 94.1 94.7 95.3 95.9 96.0 96.3 102 39 72.8 94.4 94.3 94.9 95.5 96.1 96.2 96.5 104 40 72.9 94.5 94.4 95.0 95.6 96.2 96.3 96.6 106 41 73.0 94.7 94.6 95.2 95.8 96.4 96.5 96.8 108 42 73.1 94.8 94.7 95.3 95.9 96.5 96.6 96.9 109 43 73.3 95.0 94.9 95.5 96.1 96.7 96.8 97.1 111 44 73.4 95.1 95.0 95.6 96.2 96.8 96.9 97.2 113 45 73.5 95.3 95.2 95.8 96.4 97.0 97.1 97.4 115 46 73.6 95.4 95.3 95.9 96.5 97.1 97.2 97.5 117 47 73.7 95.6 95.5 96.1 96.7 97.3 97.4 97.7 118 48 73.8 95.8 95.7 96.3 96.9 97.5 97.6 97.9 120 49 73.9 95.9 95.8 96.4 97.0 97.6 97.7 98.0 122 50 74.1 96.1 96.0 96.6 97.2 97.8 97.9 98.2 F> APPLICABLE TO ALL /3, /3F, AND -78E RATINGS EFFECTIVITY 88J ALL GMM-1156648-00-A (MOD/ MPA Test TableaCorrected Fan Speed) Figure 504/71-00-00-990-821-F00 (Sheet 6 of 6) D633A101-BBJ rEINC•OAOPPICTAA, • Cqm gni - • AV.INKAml Oh* Se. Mk Oar Iry f.n.h I -14*AI SC1:06561 718_'/ 71-00-00 Page 538 Oct 15/2015 EFTA00812400 L. CFM56 ENGINES (CFM56.7) 1 gifirosna 737-600f700/800/900 AIRCRAFT MAINTENANCE MANUAL OAT XN1 TARGET MAX EGT - t ENGINE MODEL I > F t r0.5X 7827/81 7827 7826 7824/81 7826/81 7626/82 7626/82 7824 7822/81 7822 7820 -40 -40 67.6 516 5 534 538 574 576 597 626 -38 -39 67.8 519 5 537 541 577 579 600 629 -36 -38 67.9 522 5 540 544 580 582 603 632 -35 -37 68.0 525 5 543 547 583 585 606 635 -33 -36 68.2 527 545 549 585 587 608 637 -31 -35 68.3 530 548 552 588 590 611 640 -29 -34 68.5 533 551 555 591 593 614 643 -27 -33 68.6 536 554 558 594 596 617 646 -26 -32 68.7 538 556 560 596 598 619 648 -24 -31 68.9 541 559 563 599 601 622 651 -22 -30 69.0 544 562 566 602 604 625 654 -20 -29 69.2 547 565 569 605 607 628 657 -18 -28 69.3 549 567 571 607 609 630 659 -17 -27 69.4 552 570 574 610 612 633 662 -15 -26 69.6 555 573 577 613 615 636 665 -13 -25 69.7 558 576 580 616 618 639 668 -11 -24 69.8 560 578 582 618 620 641 670 -9 -23 70.0 563 581 585 621 623 644 673 -8 -22 70.1 565 583 587 623 625 646 675 -6 -21 70.3 568 586 590 626 628 649 678 -4 -20 70.4 570 588 592 628 630 651 680 -2 -19 70.5 573 591 595 631 633 654 683 0 -18 70.7 575 593 597 633 635 656 685 1 -17 70.8 578 596 600 636 638 659 688 3 -16 70.9 580 598 602 638 640 661 690 5 -15 71.1 583 601 605 641 643 664 693 7 -14 71.2 585 603 607 643 645 666 695 9 -13 71.3 588 5 606 610 646 648 669 698 10 -12 71.5 590 5 608 612 648 650 671 700 12 -11 71.6 593 5 611 615 651 653 674 703 14 -10 71.7 595 5 613 617 653 655 676 705 16 -9 71.9 598 5 616 620 656 658 679 708 18 -8 72.0 600 5 618 622 658 660 681 710 19 -7 72.1 603 6 621 625 661 663 684 713 21 -6 72.3 605 6 623 627 663 665 686 715 23 -5 72.4 608 6 626 630 666 668 689 718 25 -4 72.5 610 6 628 632 668 670 691 720 5-T>APPLICABLE TO ALL /3, /3F, AND -7BE RATINGS FEtB .EFFECTIVITY J ALL GMM-1156649-00-A (MOD) G85150 $000958179) V4 MPA Test Table Corrected Fan Speed) Figure 505/71-00.00-990$22-F00 (Sheet 1 of 6) D633A101-BEIJ BOEIN3 PROPRIETWV • Copotert %, .d real, . Suitt' ova b. MUM 71-00-00 Page 539 Oct 15/2015 EFTA00812401 L CFM56 ENGINES (CFM56.7) OLAVOSZAW 737-60017001800/900 AIRCRAFT MAINTENANCE MANUAL OAT XN1 TARGET MAX EGT - C ENGINE MODEL F-7> 'F t 10.5X 7827/81 7827 7826 826/81 7826/82 7824/81 7824 7822/81 7822 7820 27 -3 72.7 613 631 635 671 673 694 723 28 -2 72.8 615 633 637 673 675 696 725 30 -1 72.9 617 635 639 675 677 698 727 32 0 73.1 620 638 642 678 680 701 730 34 1 73.2 622 640 644 680 682 703 732 36 2 73.3 625 643 647 683 685 706 735 37 3 73.5 628 646 650 686 688 709 738 39 4 73.6 630 648 652 688 690 711 740 41 5 73.7 633 651 655 691 693 714 743 43 6 73.8 635 653 657 693 695 716 745 45 7 74.0 638 656 660 696 698 719 748 46 8 74.1 640 658 662 698 700 721 750 48 9 74.2 643 661 665 701 703 724 753 50 10 74.4 645 663 667 703 705 726 755 52 11 74.5 648 666 670 706 708 729 758 54 12 74.6 650 668 672 708 710 731 760 55 13 74.7 653 671 675 711 713 734 763 57 14 74.9 655 673 677 713 715 736 765 59 15 75.0 658 676 680 716 718 739 768 61 16 75.1 660 678 682 718 720 741 770 63 17 75.3 662 1 680 684 720 722 743 772 64 18 75.4 665 4 683 687 723 725 746 775 66 19 75.5 667 6 685 689 725 727 748 777 68 20 75.6 670 9 688 692 728 730 751 780 70 21 75.8 672 1 690 694 730 732 753 782 72 22 75.9 675 4 693 697 733 735 756 785 73 23 76.0 677 6 695 699 735 737 758 787 75 24 76.1 680 9 698 702 738 740 761 790 77 25 76.3 682 1 700 704 740 742 763 792 79 26 76.4 685 4 703 707 743 745 766 795 81 27 76.5 687 705 709 745 747 768 797 82 28 76.6 689 707 711 747 749 770 799 84 29 76.8 692 710 714 750 752 773 802 86 30 76.9 694 712 716 752 754 775 804 88 31 77.0 696 714 718 754 756 777 806 90 32 77.1 699 717 721 757 759 780 809 T-7>APPLICABLE TO ALL /3, /3F, AND -78E RATINGS EFFECTIVITY SEW ALL GMM-1156649-00-A (MOD) GMM-1156650-00-A (MOD) G85186 SC006511, 70/3_14 MPA Test Table orrected Fan Speed) Figure 505/7 - -F00 (Sheet 2 of 6) D633A101-BBJ DOCING PROPME TART. CarJM1 r thrbire. Wait • See Mn Per I., War. 71-00-00 Page 540 Oct 15/2015 EFTA00812402 L CFM56 ENGINES (CFM56-7) gLAMSZACC 737-60017001800/900 AIRCRAFT MAINTENANCE MANUAL OAT XN1 TARGET MAX EGT — 'C ENGINE MODEL ' l) F 'C e0.57. 7827/61 7827 7826 626161 7824/61 7824 7822/81 7822 7820 7826/82 91 33 77.3 701 719 723 759 761 782 811 93 34 77.4 703 721 725 761 763 784 813 95 35 77.5 706 724 728 764 766 787 816 97 36 77.6 708 726 730 766 768 789 818 99 37 77.8 710 728 732 768 770 791 820 100 38 77.9 712 730 734 770 772 793 822 102 39 78.0 715 7 733 737 773 775 796 825 104 40 78.1 717 7 735 739 775 777 798 827 106 41 78.2 720 7 738 742 778 780 801 830 108 42 78.4 722 7 740 744 780 782 803 832 109 43 78.5 724 7 742 746 782 784 805 834 111 44 78.6 726 7 744 748 784 786 807 836 113 45 78.7 729 7 747 751 787 789 810 839 115 46 78.8 731 7 749 753 789 791 812 841 117 47 79.0 733 7 751 755 791 793 814 843 118 48 79.1 735 7 753 757 793 795 816 845 120 49 79.2 737 755 759 795 797 818 847 122 50 79.3 739 7 757 761 797 799 820 849 il-->APPLICABLE TO ALL /3, /3F, AND -7BE RATINGS EFFECTIVITY BBJ ALL GMM-1156650-006-A (MOD) 086703 8000653 799_V4 MPA Test Table (Corrected Fan Speed) Figure 505/71-00-00.990-822-F00 (Sheet 3 of 6) 71-00-00 Page 541 0633A101-BBJ Oct 1512015 ICE1KPROPIKTARY•• CorrI9N fU.,cos.., win • See U%pi. to Snalb EFTA00812403 L CFM56 ENGINES (CFM56-7) gifiroszisec 737-600/7001800/900 AIRCRAFT MAINTENANCE MANUAL OAT XN1 TARGET MAX XN2 ENGINE MODEL 0::> F C 10.5X 7827/B1 7827 IIIIIIIII826/B1 7826 826/82 7824/81 7824 7822/81 7822 7820 -40 -40 67.6 82.7 82.6 83.2 83.8 84.4 84.5 84.8 -38 -39 67.8 82.9 82.8 83.4 84.0 84.6 84.7 85.0 -36 -38 67.9 83.1 83.0 83.6 84.2 84.8 84.9 85.2 -35 -37 68.0 83.2 83.1 83.7 84.3 84.9 85.0 85.3 -33 -36 68.2 83.4 8 83.3 83.9 84.5 85.1 85.2 85.5 -31 -35 68.3 83.6 8 83.5 84.1 84.7 85.3 85.4 85.7 -29 -34 68.5 83.7 8 83.6 84.2 84.8 85.4 85.5 85.8 -27 -33 68.6 83.9 83 83.8 84.4 85.0 85.6 85.7 86.0 -26 -32 68.7 84.1 8 84.0 84.6 85.2 85.8 85.9 86.2 -24 -31 68.9 84.3 8 84.2 84.8 85.4 86.0 86.1 86.4 -22 -30 69.0 84.4 8 84.3 84.9 85.5 86.1 86.2 86.5 -20 -29 69.2 84.6 8 84.5 85.1 85.7 86.3 86.4 86.7 -18 -28 69.3 84.8 8 84.7 85.3 85.9 86.5 86.6 86.9 -17 -27 69.4 85.0 8 84.9 85.5 86.1 86.7 86.8 87.1 -15 -26 69.6 85.1 85.0 85.6 86.2 86.8 86.9 87.2 -13 -25 69.7 85.3 85.2 85.8 86.4 87.0 87.1 87.4 -11 -24 69.8 85.5 85.4 86.0 86.6 87.2 87.3 87.6 -9 -23 70.0 85.7 85.6 86.2 86.8 87.4 87.5 87.8 -8 -22 70.1 85.8 85.7 86.3 86.9 87.5 87.6 87.9 -6 -21 70.3 86.0 8 85.9 86.5 87.1 87.7 87.8 88.1 -4 -20 70.4 86.2 86.1 86.7 87.3 87.9 88.0 88.3 -2 -19 70.5 86.3 86.2 86.8 87.4 88.0 88.1 88.4 0 -18 70.7 86.5 86.4 87.0 87.6 88.2 88.3 88.6 1 -17 70.8 83.7 86.6 87.2 87.8 88.4 88.5 88.8 3 -16 70.9 86.9 9 86.8 87.4 88.0 88.6 88.7 89.0 5 -15 71.1 87.0 0 86.9 87.5 88.1 88.7 88.8 89.1 7 -14 71.2 87.2 2 87.1 87.7 88.3 88.9 89.0 89.3 9 -13 71.3 87.4 4 87.3 87.9 88.5 89.1 89.2 89.5 10 -12 71.5 87.5 87.4 88.0 88.6 89.2 89.3 89.6 12 -11 71.6 87.7 87.6 88.2 88.8 89.4 89.5 89.8 14 -10 71.7 87.9 87.8 88.4 89.0 89.6 89.7 90.0 16 -9 71.9 88.1 8 88.0 88.6 89.2 89.8 89.9 90.2 18 -8 72.0 88.2 88.1 88.7 89.3 89.9 90.0 90.3 19 -7 72.1 88.4 88.3 88.9 89.5 90.1 90.2 90.5 21 -6 72.3 88.6 88.5 89.1 89.7 90.3 90.4 90.7 23 -5 72.4 88.7 8 88.6 89.2 89.8 90.4 90.5 90.8 25 -4 72.5 88.9 8 88.8 89.4 90.0 90.6 90.7 91.0 :APPLICABLE TO ALL /3, /3F, AND -7BE RATINGS EFFECTIVITY 138J ALL MPA Test Table Corrected Fan Speed) Figure 505171-00-00-990.822-F00 (Sheet 4 of 6) GMM-1156651 -00—A (MOD) H43125 S000666 1600_V4 71-00-00 Page 542 D633A101-B8.1 Oct 15/2015 KENO PROCIKTARY • Coorxili r unputathoo /irk. 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'Moog, for +Oak EFTA00812404 L CFM56 ENGINES (CFM56-7) gifirsen.a. 737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL OAT XN1 TARGET MAX XN2 ENGINE MODEL (--)- F C s0.5X 7827/81 7827 7826 LV Iyi 7826/82 7624/61 7624 7622/81 7822 7820 27 -3 72.7 89.1 89.0 89.6 90.2 90.8 90.9 91.2 28 -2 72.8 89.3 89.2 89.8 90.4 91.0 91.1 91.4 30 -1 72.9 89.4 89.3 89.9 90.5 91.1 91.2 91.5 32 0 73.1 89.6 89.5 90.1 90.7 91.3 91.4 91.7 34 1 73.2 89.8 89.7 90.3 90.9 91.5 91.6 91.9 36 2 73.3 89.9 9 89.9 90.4 91.0 91.6 91.7 92.0 37 3 73.5 90.1 90.0 90.6 91.2 91.8 91.9 92.2 39 4 73.6 90.3 90.2 90.8 91.4 92.0 92.1 92.4 41 5 73.7 90.4 90.3 90.9 91.5 92.1 92.2 92.5 43 6 73.8 90.6 90.5 91.1 91.7 92.3 92.4 92.7 45 7 74.0 90.8 9 90.7 91.3 91.9 92.5 92.6 92.9 46 8 74.1 90.9 9 90.8 91.4 92.0 92.6 92.7 93.0 48 9 74.2 91.1 9 91.0 91.6 92.2 92.8 92.9 93.2 50 10 74.4 91.3 9 91.2 91.8 92.4 93.0 93.1 93.4 52 11 74.5 91.4 9 91.3 91.9 92.5 93.1 93.2 93.5 54 12 74.6 91.6 9 91.5 92.1 92.7 93.3 93.4 93.7 55 13 74.7 91.8 91.7 92.3 92.9 93.5 93.6 93.9 57 14 74.9 91.9 91.8 92.4 93.0 93.6 93.7 94.0 59 15 75.0 92.1 92.0 92.6 93.2 93.8 93.9 94.2 61 16 75.1 92.3 92.2 92.8 93.4 94.0 94.1 94.4 63 17 75.3 92.4 92.3 92.9 93.5 94.1 94.2 94.5 64 18 75.4 92.6 92.5 93.1 93.7 94.3 94.4 94.7 66 19 75.5 92.8 92.7 93.3 93.9 94.5 94.6 94.9 68 20 75.6 92.9 92.8 93.4 94.0 94.6 94.7 95.0 70 21 75.8 93.1 93.0 93.6 94.2 94.8 94.9 95.2 72 22 75.9 93.2 93.1 93.7 94.3 94.9 95.0 95.3 73 23 76.0 93.4 93.3 93.9 94.5 95.1 95.2 95.5 75 24 76.1 93.6 93.5 94.1 94.7 95.3 95.4 95.7 77 25 76.3 93.7 9 93.6 94.2 94.8 95.4 95.5 95.8 79 26 76.4 93.9 9 93.8 94.4 95.0 95.6 95.7 96.0 81 27 76.5 94.1 94.0 94.6 95.2 95.8 95.9 96.2 82 28 76.6 94.2 94.1 94.7 95.3 95.9 96.0 96.3 84 29 76.8 94.4 94.3 94.9 95.5 96.1 96.2 96.5 86 30 76.9 94.5 94.4 95.0 95.6 96.2 96.3 96.6 88 31 77.0 94.7 94.6 95.2 95.8 96.4 96.5 96.8 90 32 77.1 94.9 94.8 95.4 96.0 96.6 96.7 97.0 11 >APPLICABLE TO ALL /3, /3F, AND -7BE RATINGS EFFECTIVITY rALL GMM-1156651-00-A (MOD) GMM-1156652-00-A (MOD) f4924$ St0O658IS0LV5 MPA Test Table guippiporrected Fan Speed) re Figu 505/7 a. 0 -F00 (Sheet 5 of 6) 71-00-00 Page 543 D633A101-BBJ Oct 15/2015 BOENG PROPRIETOR, • Ccvo Umob404•110"," , 5" UI. p. 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