EFTA00609328.pdf

FAA 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 ENGINE MODEL ENGINE SERIAL NUMBER 800726 JT8D-219 P726122V TEST SPECIFICATIONS: MANUAL USED PIN 773128 REV.# 99 TYPE OF TEST: PRE-INDUCTION TEST LIMTS (CHECK ONE): X HEAVY MAINTENANCE OVERHAUL OTHER. DOES NOT ITEM OPERATION AND REFERENCED PROCEDURE ACCEPTED REJECTED APPLY I-oI F; 21 1 MAIN OIL PRESSURE it 3 21 2 MAIN OIL TEMPERATURE. 21 3 OIL CONSUMPTION. NS: 2I 4 BREATHER PRESSURE i A L1 5 MAXIMUM EXHAUST GAS TEMPERATURE (EGT) 44W, 6 EXHAUST GAS TEMPERATURE (EGT) SPREAD. r 42Pa 7 FRONT VIBRATION LIMITS. 7I 21 8 REAR VIBRATION LIMITS. IC, 0 21 9 TURBINE COOLING PRESSURE. sisn 21 10 MAXIMUM LOW COMPRESSOR SPEED. iii 11 MAXIMUM HIGH COMPRESSOR SPEED. I NL'? 12 E.P.R. vs. THRUST RELATIONSHIP. i. I 21 13 ACCELERATION TIME. NSW 14 ANTI-SURGE BLEED CHECK. t 71 .-”-. 21 15 AUTOMATIC RESERVE THRUST INCREMENT. SPEED DATA PLATE. F. OBSERVED: R.P.M.: 11,101 PERCENT: 90.66 % 21 18 in:P. 17 RE-STAMP OF DATA PLATE REQUIRED IF ENGINE QUALIFIES BASED ON WORK PERFORME NO X YES 18 COMMENTS: TAKE-OFF LIMIT TAKE-OFF - ACTUAL TAKE-OFF MARGIN RED LINE 590 °C (OBSERVED) 572 °C (OBSERVED) 18 °C EHM (for Pt7IPt2) 543 °C (CORRECTED) 542 °C (CORRECTED) 1 °C 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 . 26 °C 393 °C CIT 78 °F EGT 740 °F T7 TIME @ TEMP THRUST 1099 LBS CORR. EPR 1.031 CORRECTED DATA N1 % 26.22 N1 RPM 2,157 N1 2118 CORR. PT2 30.09 HGA Fn 1093 N2% 54.54 N2 RPM 6,681 N2 6561 PT2 AVG (CELL) 0.00 "H20 EGT 370 °C 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 1.381 4/4/2014 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 SIN: P726122V WO: 800725 CUST: FJ TURBINE POWER ZIA P,D , 26 497 °C CIT 78 °F EGT 927 °F T7 TIME @ TEMP 0 THRUST 14596 LBS CORR. EPR 1.650 CORRECTED DATA N1 % 81.96 N1 RPM 6,739 N1 6618 CORR. PT2 30.05 HGA Fn 15133 N2 % 92.29 I N2 RPM 11,304 N2 11101 PT2 AVG (CELL) -1.20 "H20 EGT 470 t 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 0.570 4/4/2014 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 CORRECTED DATA N1 % 26.37 N1 RPM 2,168 N1 2129 CORR. PT2 30.11 HGA Fn 1120 N2 % 54.78 N2 RPM 6,710 N2 6590 PT2 AVG (CELL) 0.00 "H20 EGT 366 °C TIMER Wf 971 PT7 31.04 HGA 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 CORR. Ps3/Pt2 1.393 OIL IN 209 °F 98 °C CORR. Ps4/Pt2 0.987 PS4 14.6 PSIA PS3 41.9 HGA OIL OUT 240 °F PCP 21.6 PSIA CELL TEMP 78 °F BAROMETER 30.11 "HG PS3 f 20.6 PSIA PCP RATIO 1.479 4/4/2014 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 26 °C 572 °C CIT 78 °F EGT 1062 °F T7 TIME © TEMP 0 THRUST 20556 LBS CORR. EPR 1.989 CORRECTED DATA N1% 92.39 N1 RPM 7,697 N1 7445 CORR PT2 30.03 HGA Fn 21118 N2 % 97.38 N2 RPM 11,928 N2 11708 PT2 AVG (CELL) -1.50 "H20 EGT 542 °C 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 0.555 4/4/2014 EFTA00609333 FJ TURBINE POWER,INC FAA REPAIR STATION F7JR192Y JT8D Page 24 MODEL JT8D-219 S/N P726122V W.O. 800725 CUSTOMER FJ TURBINE T7 COND TAKEOFF 1. 1084 F 2. 1101 F 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 . 26 °C 392 CC CIT 78 °F EGT 737 °F T7 TIME @ TEMP THRUST 1091 LBS CORR. EPR 1.030 CORRECTED DATA N1% 25.80 N1 RPM 2,121 N1 2083 CORR. PT2 30.11 HGA Fn 1084 N2 % 53.97 N2 RPM 6,611 N2 6492 PT2 AVG (CELL) 0.00 "H20 EGT 368 °C 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 1.473 4/4/2014 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