EFTA00609328.pdf

FAA REPAIR REPAIR STATION # FTJR192Y TEST CELL RESULTS W. O.: 800725 MODEL: JT8D-219 ESN: P726122V EFTA00609328 F. J. Turbine Power, Inc. DATE TESTED: 4-Apr-14 FAA Approved Repair Station F7JR192Y Form Q 009 - 1/5/04 Engine Work Card: NT 5001A 7/22/11 ENGINE WORK CARD WARNING: This routine work form does not in any way supersede the OEM's manual requirements. This form is intended to be used in conjunction with the OEM's manuals. TITLE: ENGINE TEST RESULTS - JT8D-200 WORK ORDER 800726 ENGINE MODEL JT8D-219 ENGINE SERIAL NUMBER P726122V TEST SPECIFICATIONS: TEST LIMTS MANUAL USED PIN 773128 REV.# 99 TYPE OF OTHER. TEST: PRE-INDUCTION (CHECK ONE): X HEAVY MAINTENANCE OVERHAUL ITEM OPERATION AND REFERENCED PROCEDURE ACCEPTED REJECTED DOES NOT APPLY 1 MAIN OIL PRESSURE I-o 21 it I F; 3 2 MAIN OIL TEMPERATURE. 21 3 OIL CONSUMPTION. 21 NS: 4 BREATHER PRESSURE 2 I i A 5 MAXIMUM EXHAUST GAS TEMPERATURE (EGT) L1 44W, 6 EXHAUST GAS TEMPERATURE (EGT) SPREAD. r 42Pa 7 FRONT VIBRATION LIMITS. 7I 8 REAR VIBRATION LIMITS. 21 IC, 9 TURBINE COOLING PRESSURE. 21 sisn 0 10 MAXIMUM LOW COMPRESSOR SPEED. iii 21 11 MAXIMUM HIGH COMPRESSOR SPEED. NL'? I 12 E.P.R. vs. THRUST RELATIONSHIP. i. I 13 ACCELERATION TIME. 21 NSW 14 ANTI-SURGE BLEED CHECK. 71 t .-”-. 15 AUTOMATIC RESERVE THRUST INCREMENT. 21 18 SPEED DATA PLATE. OBSERVED: R.P.M.: 11,101 PERCENT: 90.66 % F. 2 in:P. 1 17 RE-STAMP OF DATA PLATE REQUIRED IF ENGINE QUALIFIES BASED ON WORK PERFORME NO X YES 18 COMMENTS: TAKE-OFF LIMIT TAKE-OFF RED LINE 590 °C (OBSERVED) 572 °C (OBSERVED) - ACTUAL TAKE-OFF 18 MARGIN °C °C EHM (for Pt7IPt2) 543 °C (CORRECTED) 542 °C (CORRECTED) 1 CIT: 78 ° F EFTA00609329 FJ TURBINE POWER, INC FAA #F7JR192Y JT8D-200 ENGINE TEST FROM PAGE 26 THIS DATA HAS BEEN CORRECTED BY USING CORRECTED PT2 PER CMS TABLE NO. 1424 EQUATION 2 (CURVE 1891-2) MODEL: JT8D-219 SIN: P726122V WO: 800725 CUST: FJ TURBINE POWER i.b . CIT 26 78 °C °F EGT 393 740 °C °F T7 TIME @ TEMP THRUST 1099 LBS CORR. EPR 1.031 N1 % N2% CORRECTED N1 Fn N2 EGT DATA °C 26.22 N1 RPM 2,157 2118 CORR. PT2 30.09 HGA 1093 54.54 N2 RPM 6,681 6561 PT2 AVG (CELL) 0.00 "H20 370 TIMER Wf 972 PT7 31.01 HGA MAIN FUEL 29 PSIG TSFC 0.889 MAIN OIL 45 PSIG FUEL FLOW 1005 PPH VIBRATION BREATHEF 0.1 "HG COMP 0.1 FUEL IN 81 °F TURB 0.4 CORR. Ps3/Pt2 1.387 OIL IN 154 °F 68 °C CORR. Ps4/Pt2 0.995 P641 14.7 PSIA PS3 41.7 HGA OIL OUT 168 °F PCP 20.3 JPSIA CELL TEMP 78 °F BAROMETER 30.09 "HG PS3 20.5 PSIA PCP RATIO 4/4/2014 1.381 EFTA00609330 FJ TURBINE POWER, INC FAA #F7JR192Y JT8D-200 ENGINE TEST FROM PAGE 26 THIS DATA HAS BEEN CORRECTED BY USING CORRECTED PT2 PER CMS TABLE NO. 1424 EQUATION 2 (CURVE 1891-2) MODEL: JT8D-219 CIT 26 78 °F EGT SIN: P726122V WO: 800725 CUST: 497 927 °C °F T7 TIME @ TEMP 0 THRUST 14596 FJ TURBINE POWER ZIA P,D , LBS CORR. EPR 1.650 N1 % N2 % CORRECTED N1 Fn N2 EGT DATA t 81.96 N1 RPM 6,739 6618 CORR. PT2 30.05 HGA 15133 92.29 I N2 RPM 11,304 11101 PT2 AVG (CELL) -1.20 "H20 470 TIMER Wf 7370 PT7 49.59 HGA MAIN FUEL 25 PSIG TSFC 0.487 MAIN OIL 47 PSIG FUEL FLOW 7611 PPH VIBRATION BREATHEFj 0.5 'HG COMP 0.8 FUEL IN 79 °F TURB 0.5 CORR. Ps3/Pt2 5.468 OIL IN 185 °F 85 °C CORR. Ps4/Pt2 13.409 PS4 197.9 PSIA PS3 164.3 HGA OIL OUT 288 °F PCP 112.8 PSIA CELL TEMP 78 °F BAROMETER 30.11 "HG PS3 80.7 PSIA PCP RATIO 4/4/2014 0.570 EFTA00609331 FJ TURBINE POWER, INC FAA #F7JR192Y JT8D-200 ENGINE TEST FROM PAGE 26 THIS DATA HAS BEEN CORRECTED BY USING CORRECTED PT2 PER CMS TABLE NO. 1424 EQUATION 2 (CURVE 1891-2) MODEL: JT8D-219 S/N: P726122V WO: 800725 CUST: FJ TURBINE POWER L L. 26 °C 389 °C CIT 78 °F EGT 734 °F T7 TIME © TEMP 0 THRUST 1127 LBS CORR. EPR 1.031 N1 % N2 % N1 N2 CORRECTED N1 Fn N2 EGT DATA °C 26.37 RPM 2,168 2129 1120 54.78 RPM 6,710 6590 366 TIMER Wf 971 MAIN FUEL 29 PSIG TSFC 0.867 MAIN OIL 44 PSIG FUEL FLOW 1005 PPH VIBRATION BREATHEFJ 0.1 "HG COMP 0.1 FUEL IN 80 °F TURB 0.5 OIL IN 209 °F 98 °C PS4 14.6 PSIA PS3 41.9 HGA OIL OUT 240 °F CELL TEMP 78 °F BAROMETER 30.11 "HG 4/4/2014 CORR. PT2 30.11 PT2 AVG (CELL) PT7 HGA 0.00 31.04 CORR. Ps3/Pt2 CORR. Ps4/Pt2 "H20 HGA 1.393 0.987 PCP 21.6 PSIA PS3 f 20.6 PSIA PCP RATIO 1.479 EFTA00609332 FJ TURBINE POWER, INC FAA #F7JR192Y JT8D-200 ENGINE TEST FROM PAGE 26 THIS DATA HAS BEEN CORRECTED BY USING CORRECTED PT2 PER CMS TABLE NO. 1424 EQUATION 2 (CURVE 1891-2) MODEL: JT8D-219 SIN: P726122V WO: 800725 CUST: FJ TURBINE POWER 1 -A CIT 26 78 °C °F EGT 572 1062 °C °F T7 TIME © TEMP 0 THRUST 20556 LBS CORR. EPR 1.989 N1% N2 % N1 N2 CORRECTED N1 Fn N2 EGT DATA °C 92.39 RPM 7,697 7445 CORR PT2 30.03 HGA 21118 97.38 RPM 11,928 11708 PT2 AVG (CELL) -1.50 "H20 542 TIMER Wf 10815 PT7 59.74 HGA MAIN FUEL 21 PSIG TSFC 0.512 MAIN OIL 47 PSIG FUEL FLOW 11163 PPH VIBRATION BREATHEF 0.5 "HG COMP 0.8 FUEL IN 79 °F TURB 0.8 CORR. Ps3/Pt2 6.901 OIL IN 187 °F 86 °C CORR. Ps4/Pt2 17.789 PS4 262.4 PSIA PS3 206.7 HGA OIL OUT 307 °F PCP 145.9 PSIA CELL TEMP 78 °F BAROMETER 30.11 "HG PS3 101.8 PSIA PCP RATIO 4/4/2014 0.555 EFTA00609333 FJ TURBINE POWER,INC FAA REPAIR STATION F7JR192Y JT8D Page 24 MODEL JT8D-219 S/N P726122V W.O. 800725 CUSTOMER FJ TURBINE 1. 2. T7 1084 1101 F F COND TAKEOFF 3. 1054 F CALCULATED AVG. 1063 F 4. 1059 F 5. 1093 F 6. 991 F EGT SPREAD EGT LO eig! EGT HI Ile! -00- EGT SPREADI/O -0- 7. 1066 F CHN216 CHN217 8. 1053 F DATE 04/04/14 EFTA00609334 FJ TURBINE POWER, INC FAA #F7JR192Y JT8D-200 ENGINE TEST FROM PAGE 26 THIS DATA HAS BEEN CORRECTED BY USING CORRECTED PT2 PER CMS TABLE NO. 1424 EQUATION 2 (CURVE 1891-2) MODEL: JT8D-219 SIN: P726122V WO: 800725 CUST: FJ TURBINE POWER f .D L . CIT 26 78 °C °F EGT 392 737 CC °F T7 TIME @ TEMP THRUST 1091 LBS CORR. EPR 1.030 N1% N2 % CORRECTED N1 Fn N2 EGT DATA °C 25.80 N1 RPM 2,121 2083 CORR. PT2 30.11 HGA 1084 53.97 N2 RPM 6,611 6492 PT2 AVG (CELL) 0.00 "H20 368 TIMER Wf 898 PT7 31.00 HGA MAIN FUEL 29 PSIG TSFC 0.828 MAIN OIL 44 PSIG FUEL FLOW 929 PPH VIBRATION BREATHEFI 0.1 "HG COMP 0.1 FUEL IN 80 °F TURB 0.3 CORR. Ps3/Pt2 1.380 OIL IN 224 °F 107 °C CORR. Ps4/Pt2 0.987 PS4 14.6 PSIA PS3 41.5 HGA OIL OUT 249 °F PCP 21.5 PSIA CELL TEMP 78 °F BAROMETER 30.11 "HG PS3 20.4 PSIA PCP RATIO 4/4/2014 1.473 EFTA00609335 F.J. TURBINE POWER, INC FAA #F7JR192Y ENGINE TEST PAGE 27 MODEL JT8D-219 S/N P726122V W.O. 800725 CUSTOMER FJ TURBINE BLEED VALVE SCHEDULE MIN LIMIT 67.7 CHN223 PS4 -.20 PSIG MAX LIMIT 73.2 CHN224 PS3 6.10 PSIG OPEN O 69.6 CHN225 PS3 42.6 HGA CLOSED O 70.2 CHN226 DATE 04/04/14 EFTA00609336 MODEL JT8D-219 S/N P726122V W.O. 800725 CUSTOMER FJ TURBINE ACCELERATION TIME CHECK N2 RPM PERCENT 95.91 PERCENT RPM 0 10 20 30 40 50 60 70 80 90 100 DATE 04/04/14 TIME 5:0 TIME OF DAY 10:18:48 PAGE 30 EFTA00609337