N1217A

Part: APU — MALFUNCTIONED · airframe 90,585 hrs · 23,177 cycles

APU INOP(<P>TRANSFER TO MDDR # 105254 IAW DDG 49-11-01A CAT C&NBSP;</P><P>LP 1047299 M8 APU BITE OPS CHECK GOOD&NBSP; IAW AMM 49-61-05 AND 49-11-00 THIS CLEARED MDDR 105254 PLACARD REMOVED&NBSP;</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (CABIN PRESSURE) · airframe 90,590 hrs · 23,178 cycles

CABIN ALT AUTO 1(<P><SPAN>PERFORMED / AUTO 1 CABIN PRESSURE CONTROLLER BITE TEST PASSED MSG SELF CLEARED PER AMM / 21-31-00</SPAN></P>)

Part: APU — MALFUNCTIONED · airframe 90,533 hrs · 23,162 cycles

APU INOP TWO START ATTEMPS(<P>C/W FIM49-11 FT 958 BITE TEST MSG CLEARED APU STARTED THIRD ATTEMP AND OPS NORMAL<BR /></P>)

Part: OIL SYSTEM — LOW (APU) · airframe 90,544 hrs · 23,164 cycles

AFTER LANDING ATTEMPTED TO START APU TWICE, APU FAULT ANNUNCIATED BOTH TIMES.(<P>APU OIL FOUND TO BE LOW, SERVICED TO FULL IAW AMM 12-13-01. ACCOMPLISHED BITE TEST OF APU IAW FIM 49-11-00 F/T 815, OPS CHECK NORMAL AT THIS TIME. 3RD ATTEMPT SUCCESSFUL.</P>)

Part: PITOT TUBE — OVERHEATED (AUX) · airframe 90,526 hrs · 23,160 cycles

AFTER R ENG STARTED L AUX PITOT EICAS AND OVRHD LIGHT INDICATIONS DISPLAYED&NBSP;(<P>T/S PER FIM 30-31 FT 804 REMOVED AND REPLACED LH AUX PITOT TUBE AS PER AMM 34-11-01 LEAK CHECK PER AMM 34-11-00 LEAK CHECK OK&NBSP;</P>)

Part: UNKNOWN — MALFUNCTIONED (APU) · airframe 90,484 hrs · 23,146 cycles

APU WOULD NOT START WITH APU FAULT EICAS MESSAGE. PERFORMED FIM 49-11 APU BITE PROCEDURE " START ABORTED " MESSAGE PRESENT ON. STARTS 2 AND 3. REASON MESSAGE " SEE MAINTENANCE MANUAL" NO NUMERIC MINI FLAGS DISPLAYED. PER FIM 49-11. THIS IS FROM A STORES FAULT FROM THE PAST. CLEARED MEMORY PER FIM 49-11-00. APU START OPS CHECK GOOD. NO FURTHER MX ACTION REQUIRE AT THIS TIME.

Part: SOFTWARE — INACCURATE (EICAS) · airframe 90,355 hrs · 23,104 cycles

APU OIL QTY IND INOP. UPDATE EICAS SOFTWARE IAW AMM 31-00-00. CHECK OIL QTY IND, FOUND OK.

Part: SOFTWARE — FAULTY (CREW O2) · airframe 90,355 hrs · 23,104 cycles

CREW OXYGEN PRESSURE INDICATION INOP ON EICAS. CREW OXYGEN SYSTEM PRESSURE, PERFORMED TROUBLE SHOOTING TO OXYGEN. INSTALLED EICAS SOFTWARE 317E-B26-022-A5 IAW AMM 31-41-02. THIS CLEARED MDDR.

Part: CLAMP — LOOSE (OIL BULB) · airframe 90,355 hrs · 23,104 cycles

NO.2 ENGINE O/B SIDE, N.6 BEARING OIL BULB LINE CLAMP LOOSE.(<P>INSTALLED OIL SUPPLY LINE CLAMP PER B767 AMM 20-11-00.</P>)

Part: SMOKE DETECTOR — NO TEST (E/E BAY) · airframe 90,355 hrs · 23,104 cycles

EQUIPMENT COOLING SMOKE DETECTOR WILL NOT TEST.(<P>REMOVED AND REPLACED EQUIP. COOL SMOKE DETECTOR PER B767 SSM 21-28-02. OPS CHECK GOOD.</P>)

Part: WARNING MESSAGE — ACTIVATED (EXHAUST FAN) · airframe 90,279 hrs · 23,081 cycles

FWD EQUIPMENT EXHAUST FAN NR 1 EICAS MESSAGE.

Part: RADAR — MALFUNCTIONED (WX SYS) · airframe 90,279 hrs · 23,081 cycles

F/O TERRAIN WILL NOT DISPLAY WHEN SELECTED. PERFORMED AN OPS TEST OF THE WEATHER RADAR SYSTEM. FOUND NO DEFECTS IAW AMM 34-43-00.

Part: UNKNOWN — MALFUNCTIONED (FUEL SYSTEM) · airframe 90,184 hrs · 23,045 cycles

ABOUT A 1700LBS SPLIT DEVELOPED BETWEEN THE 2 MAIN TANKS DURING THE FLIGHT BURN ON GAUGES/ CDU PROG P8 APPEARED IDENTICAL. T/S PER FIM 28-41 FAULT TREE 838 AND FAULT TREE 847 SYSTEM OK. MCC ADVISED.

Part: STATUS MESSAGE — FALSE ACTIVATION (COCKPIT) · airframe 90,080 hrs · 23,011 cycles

CABIN ALT AUTO 1 STATUS MESSAGE. PERFORMED TEST OF CABIN ALT AUTO 1 IAW AMM 21-31-00, OPS CHECK GOOD AT THIS TIME.

Part: REGULATOR VALVE — MALFUNCTIONED (BLEED AIR SYS) · airframe 90,014 hrs · 22,990 cycles

STATUS MESSAGE: LEFT ENGINE PRV. REMOVED AND REPLACED LEFT ENGINE PRESSURE REGULATING VALVE IAW AMM 36-11-18. ENGINE BITE CHECK GOOD IAW AMM 36-11-00.

Part: ELBOW — MISSING (BLEED AIR SYS) · airframe 90,014 hrs · 22,990 cycles

LEFT ENG HIGH PRESSURE SHUT OFF VALVE MISSING ELBOW/ UNION. R&R REPLACED LEFT ENG HIGH PRESSURE SHUT -OFF VALVE ELBOW / UNION IAW AMM 36-11-18 OPS CHECK GOOD, NO DEFECTS NOTED AT THIS TIME.

Part: STATUS MESSAGE — FALSE ACTIVATION (COCKPIT) · airframe 89,993 hrs · 22,983 cycles

AFT EQ EXH FAN2 STATUS MSG. CYCLED AFT EQ EXH FAN2 CIRCUIT BREAKER IAW AMM 20-60-01. OPS CHECK OF EXHAUST FAN2 GOOD PER FIM 21-58-02. OK FOR SERVICE.

Part: APU — SHUTDOWN (APU BAY) · airframe 89,964 hrs · 22,971 cycles

APU AUTO SHUTDOWN. TRANSFER TO MDDR 99918 IAW MEL 49-11-01A CAT C DUE DATE 01 OCT 18.

Part: CHARGER — INOPERATIVE (APU) · airframe 89,946 hrs · 22,965 cycles

APU COLD START UNSUCCESSFUL -50 SAT FL 390 1ST ATTEMPT UNSUCCESSFUL, -42 SAT FL 350 AND & ERD ATTEMPTS UNSUCCESSFUL. REMOVED AND REPLACED APU BATTERY PER AMM 24-31-04, OPS CHECK OK. P/N 018550-000, S/N 063627. REMOVED AND REPLACED APU BATTERY CHARGER PER AMM 24-31-05 OPS CHECK GOOD.

Part: PIN — BROKEN (WINDOW HEAT) · airframe 89,948 hrs · 22,966 cycles

LT SIDE WINDOW EICAS MESSAGE MULTIPLE TIMES IN FLIGHT AND ON TAXI ASSOCIATED WITH L SIDE WINDOW HEAT INOP. REPLACED BROKEN PIN NR 3 ON CONNECTOR D05872P. OPS CHECK GOOD IAW SWPM 20-60-00.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 89,942 hrs · 22,964 cycles

AFTER TAKEOFF EICAS MSG L SIDE WINDOW. PERFORMED WINDOW HEAT RESISTANCE TEST IAW AMM 30-41-00, FOUND TO BE WITHIN LIMITS. PERFORMED BITE TEST OF WINDOW IAW FIM 30-41 FT 804, NO FAULTS NOTED AT THIS TIME.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 89,942 hrs · 22,964 cycles

ON TAKE OFF EICAS MSG L SIDE WINDOW. PERFORMED OPERATIONAL TEST OF WINDOW ANTI ICE SYSTEM. OPS CHECK GOOD IAW AMM 30-41-00, NO FAULTS NOTED.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 89,942 hrs · 22,964 cycles

APU FAULT CAUTION EICAS MSG AFTER ATTEMPTING TO START APU. AFTER LANDING FOLLOWED QRH AND APU FAILED TO START ON 2ND ATTEMPT. PERFORMED APU BITE PROCEDURES PER FIM 49-11 FT 958, NO FAULTS NOTED. ACCOMPLISHED OPS CHECK GOOD AT THIS TIME.

Part: WINDOW — MALFUNCTIONED (COCKPIT) · airframe 89,932 hrs · 22,962 cycles

PASSING FL 180 A LOUD BANG WAS HEARD FOLLOWED BY THE HANDLE MOVING ON THE R2 WINDOW. THE INDICATOR WAS BETWEEN OPEN/CLOSED. R&R R2 WINDOW AND ACCOMPLISHED ADJUSTMENT PER AMM 56-11-02. PRESSURIZED AIRCRAFT PER AMM 21-31-00. NO LEAKS NOTED.

Part: UNKNOWN — MALFUNCTIONED (APU) · airframe 89,931 hrs · 22,961 cycles

APU WONT START, MADE 3 ATTEMPTS. APU FAULT LIGHT AND EICAS MESSAGE DISPLAYED. PERFORMED APU BITE PROCEDURE IAW FIM 49-11 FT 950, NO FAULTS NOTED. OPS NORMAL.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 89,909 hrs · 22,951 cycles

APU FAULT ON START ATTEMPT AFTER LANDING. PERFORMED FIM 49-11-FT 958 NO FAULTS NOTED START NORMAL.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 89,891 hrs · 22,945 cycles

SHORTLY AFTER STARTING DECENT FROM FL390 EICAS MSG L STRUT DUCT LEAK. QRH PROCEDURES COMPLETE. PERFORMED FIM TASK 26-18, NO DISCREPACIES. GROUND PERFORMED OPS CHECK OF STRUT DUCT DETECTION IAW AMM 36-10-00, NO FAULTS OR OTHER DISCREPANCIES FOUND.

Part: SWITCH — INOPERATIVE (COCKPIT) · airframe 89,891 hrs · 22,945 cycles

CABIN ALTITUDE ALERT SWITCH OUT. REMOVED AND REPLACED CABIN ALTITUDE ALERT SWITCH IAW AMM 33-38-00. OPS CHECK OK.

Part: WARNING SYSTEM — FALSE INDICATION (COCKPIT) · airframe 89,879 hrs · 22,940 cycles

APU FAULT ON 2 ATTEMPTS AFTER LANDING REPEAT WRITE UP. ACCOMPLISHED APU BITE CHECK FOUND AC START CIRCUIT FAULT. PERFORMED APU OPS CK IAW AMM 49-11-00. OPS CKS GOOD AT THIS TIME.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 89,866 hrs · 22,935 cycles

APU FAULT WHEN START ATTEMPTED AFTER LANDING. ACCOMPLISHED APU BITE CHECK IAW FIM 49-11 FAULT TREE 958. NO FAULTS NOTED AND ACCOMPLISHED APU OPS CHECK IAW AMM 49-11-00. OPS CHECK GOOD AT THIS TIME.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 89,857 hrs · 22,932 cycles

APU FAULT ON LANDING. PERFORMED APU CONTROLLER BITE CHECK IAW AMM 49-11-00. NO FAULTS FOUND, OPS CHECK GOOD.

Part: PROBE — DEFECTIVE (PITOT/STATIC SYS) · airframe 89,852 hrs · 22,931 cycles

LEFT AUX PITOT MSG AND EICAS AFTER RIGHT ENGINE START. REMOVED AND REPLACED STATIC LT SIDE AUX PROBE IAW AMM 34-11-01. PERFORMED OPS AND LEAK CHECK IAW AMM 30-31-00. OPS CHECK NORMAL AT THIS TIME.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 89,852 hrs · 22,931 cycles

STARTING APU ON GROUND RECEIVED APU FAULT. PERFORMED APU OPERATIONAL CHECK ON GROUND, APU OPERATED NORMAL IAW AMM 49-11-00. PERFORMED APU BITE PER FIM 49-11, PASSED NO FAULTS NOTED AT THIS TIME.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 89,852 hrs · 22,931 cycles

LT SLIDE WINDOW EICAS MSG. PERFORMED OPS CKS, TEST GOOD. NO MSG IAW AMM 30-41-00.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 89,836 hrs · 22,926 cycles

APU FAULT AFTER 3 ATTEMPTS. PERFORMED APU OPS CHECK OF THE APU IAW AMM 49-11-00. APU BITE PROCEDURES IAW FIM 4-11 FT 958 FOUND A/C START CIRCUIT MGS ON ECU /LRU SUMMARY RESET. MEMORY RAN APU COULD NOT DUPLICATED, A/C OK FOR SERVICES.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 89,846 hrs · 22,929 cycles

LEFT SIDE WINDOW EICAS MESSAGE. PERFORMED FIM 30-41 FAULT TREE 804, TEST AND BITE CHECK GOOD, WDM 30-41-12/D0898A PIN 17-18 RESIST 337.8 OHM PINS 13-14 RESIST 341.4 OHM WITHIN LIMITS. GROUND PINS 3,4,5 CHECK GOOD HEATER ELEMENTS PINS 11 & 16 CHECK GOOD TO GROUND. PERFORMED OPERATIONAL CHECK IAW 30-41-00. OPS CHECK GOOD.

Part: SOFTWARE — INCORRECT (COCKPIT) · airframe 89,817 hrs · 22,918 cycles

WEATHER RADAR FAIL MESSAGE ON BOTH EHSI'S. DUE TO CENTER SYMBOL GENERATOR HAVING INCORRECT SOFTWARE.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 89,817 hrs · 22,918 cycles

LT CTR FUEL PUMP MSG FLIGHT ON DESCENT. PERFORMED OPERATIONAL TEST OF THE ENGINE FUEL FEED SYSTEM IAW AMM 28-22-00. OPS CHECKS GOOD. NO DEFECTS NOTED AT THIS TIME.

Part: FRAME — CRACKED (FUSELAGE) · airframe 89,815 hrs · 29,217 cycles

MAIN CABIN LT FRAME HAS 0.600 CRACK AT INBD CHORD TRANSITION RADIUS. REPAIRED IAW BSB 76753A0209.

Part: SKIN — DENTED (FUSELAGE) · airframe 89,815 hrs · 22,917 cycles

LOCATED DENT FUSELAGE SKIN STA 1450, STR 49R-20R. COMPLIED WITH FAS EA 18174 REV-IR AT FUSELAGE SKIN STA 1450 STR 19R-20R.

Part: WIRE — BROKEN (HYDRAULIC PUMP) · airframe 89,815 hrs · 22,917 cycles

WIRE BROKEN ON NR 2 ENG HYD PUMP APPROX 3 INCHES FROM CONNECTOR DV349. R&R HARNESS IAW AMM 71-00-00.

Part: FRAME — CRACKED (FUSELAGE) · airframe 89,815 hrs · 22,917 cycles

MAIN CABIN LT FRAME BS 903 HAS A 0.6 LONG CRACK AT INBD CHORD TRANSITION RADIUS. REPAIRED IAW EO 6753A038 PART 9.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 89,815 hrs · 22,917 cycles

APU FIRE LP2 MESSAGE ON EICAS. REMOVED M686 CLEARED CONDUCTS AND REINSTALLED. PERFORMED SATISFACTORY OP'S CHECK DONE IAW SWPM 20-10-04 AND AMM 26-11-0-715.

Part: DETECTOR — DETACHED (CARGO BAY) · airframe 89,815 hrs · 22,917 cycles

AFT CARGO DET MESSAGE ON EICAS. FOUND DETACHED AROUND 66011644-DC AND RECONNECTED. PERFORMED SATISFACTORY OPS CHECK DONE SWPM 20-20-11 AND AMM 26-11-715.

Part: FRAME — CRACKED (FUSELAGE) · airframe 89,815 hrs · 22,917 cycles

MAIN CABIN FRAME BS 883, STR 20R SIDE INBD CHORD TRANSITION RADIUS HAS A CRACK 0.600 LONG. REPAIRED IAW BSB 53.40209 FIG10.

Part: FRAME — CRACKED (FUSELAGE) · airframe 89,815 hrs · 22,917 cycles

MAIN CABIN RT FRAME BS 903 HAS A 0.400 LONG CRACK AT INBD CHORD TRANSITION RADIUS. REPAIRED IAW BSB 53A0209 FIG18.

Part: STRUCTURE — DENTED (FUSELAGE) · airframe 89,815 hrs · 22,917 cycles

LOCATED 2EA DENTS AT FUSELAGE STA 618, FWD CARGO DOOR CUTOUT AFT LWR SIDE BTWN 32R-33R. WORK ACCOMPLISHED ON FAS EA 18175-PI & EA 18175 IR.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 89,815 hrs · 2,291 cycles

EMPENAGE STA 1809.5 BULKHEAD FWD FACE, LEFT HORIZONTAL CHORD LBL 28.5 CRACKED ON LWR SIDE OF CHORD. REPAIRED EMPANAGE STA 1809.5 BULKHEAD FWD FACE, LEFT INNER HORIZONTAL CHORD LBL 28.5 LWR SIDE OF CHORD IAW SRM 53-80-08-2R-10 EO 6753A030 REV 12 FIGURE 7.

Part: FIRE LOOP — OUT OF POSITION (NR 1 ENGINE) · airframe 89,815 hrs · 22,917 cycles

NR 1 ENG FIRE FIRE DETECTION LOWER LOOP IS RUBBING ON LOOP SUPPORT TUBING AT 12:00 POSITION (BIFURCATION AREA BELOW ACCESSORY GEAR BOX). INSTALLED NR 1 ENG FIRE DETECTION LOWER LOOP AND ENSURED THERE IS A PROPER SPACING BETWEEN THE FIRE DETECTION LOOP AND SUPPORT TUBE ASSEMBLY. NO DAMAGE NOTED ON FIRE DETECTION ELEMENT. DONE IAW AMM 26-11-02-264-131.

Part: GUIDE PLATE — BENT (THRUST REVERSER) · airframe 89,815 hrs · 22,917 cycles

NR 1 ENG OUTBD UPPER GUIDE PLATE FOR V BAND LATCHING MECHANISM BENT. REMOVED AND REPLACED NR 1 ENG O/B T/R UPPER GUIDE PLATE IAW AMM 70-50-00.

Part: SHIM — MIGRATED (TE FLAP) · airframe 89,815 hrs · 22,917 cycles

SHIM MIGRATED AT RIGHT WING OUTBOARD FLAP TO ROAR SPAR, INBOARD FLAP FITTING. APPLIED TORQUE CHECK CHECK AT RIGHT WING O/B FLAP I/B FITTING ATTACHING BOLT IAW SRM 51-40-04. 51-20-12.

Part: CONTROLLER — FAILED (BLEED AIR SYS) · airframe 89,815 hrs · 22,917 cycles

NR 2 ENG PRV CONTROLLER FAILED. PNUEMATIC HEALTH CHECK (PRESS NOT BTWN 47.65 AND 90 PSI. R&R NR 2 ENG PRV CONTROLLER OP & LK CHECK SATISFACTORY IAW AMM 361119 AND 710000. PASSED CHK PSI TASK CARD 6736A005-2.

Part: OUTFLOW VALVE — FAULTY (CABIN PRESSURE) · airframe 89,815 hrs · 22,917 cycles

OUTFLOW VALVE INDICATION NOT OPERATING SMOOTHLY. TROUBLESHOT OUTFLOW INDICATION IAW SSM 21-31-01. R&R CABIN PRESSURE SELECTOR ASSY & CABIN OUTFLOW VALVE IAW AMM 21-31-03 AND 21-31-01. PERFORMED SATISFACTORY OPS CHECKS IAW AMM 21-31-01 & 21-31-03.

Part: DUCT — TORN (APU) · airframe 89,815 hrs · 22,917 cycles

APU COOLING FAN DUCT IS TORN AT THE ATTACHMENT POINT TO THE COOLING FAN. REMOVED AND REPLACED APU COOLING FAN DUCT IAW AMM 49-51-03.

Part: SKIN — DENTED (FUSELAGE) · airframe 89,815 hrs · 22,917 cycles

LOCATED 2EA DENTS AT FUSELAGE SKIN STA 1376, 23R-24R. COMPLIED WITH FAS EA 18178-REV AT FUSELAGE SKIN STA1376, BTWN STA 23R-24R.

Part: MONITOR — DEFECTIVE (VIBRATION SYS) · airframe 89,815 hrs · 22,917 cycles

ENG VIB BITE MESSAGE ON EICAS. REMOVED AND REPLACED ENG VIB MONITOR IAW 77-31-03.

Part: FASTENER — WORN (NR 2 EXHAUST) · airframe 89,815 hrs · 22,917 cycles

NR 2 ENG EXHAUST SLEEVE WEAR PAD NR 5 FROM TOP TO BOTTOM IS LOOSE/MISSING HARDWARE INBD SIDE. REMOVED AND REPLACED HARDWARE AT NR 2 ENG EXHAUST SLEEVE I/B SIDE WEAR PAD NR 5 FROM TOP. DONE IAW AMM70-50-00.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 89,817 hrs · 22,918 cycles

LT SIDE WINDOW, MSG CLEARED. C/W QRH, 10 MIN LATER TURNED AND LEFT LT SIDE WINDOW SWITCH OFF. PER QRH PERFORMED OPS CHECK OF FLIGHT COMPARMENT WINDOW ANTI ICE SYSTEM IAW AMM 30-41-00. OPS CHECK GOOD, NO DEFECTS NOTES AT THIS TIME.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 89,804 hrs · 22,911 cycles

APU FAULT ON START UP AFTER LANDING. SUSPECT COLD SOAK. RAN APU SEVERAL TIMES ON GROND IAW AMM 49-11-00 LOADED AND UNLOADED, OPS CHECK OK. APU COLD SOAK REQUIRED IN ORDER TO CONFIRM PROPER OPERATION IN FLT (COLD SOAK START).

Part: STATUS MESSAGE — FALSE ACTIVATION (COCKPIT) · airframe 89,783 hrs · 22,903 cycles

CABIN ALTITUDE AUTO 1 STATUS MESSAGE ON LANDING. PERFORMED BITE CHECK IAW FIM 21-31 FT 803. FAULT CLEARED WITHOUT RETURNING.

Part: WARNING MESSAGE — FALSE ACTIVATION (COCKPIT) · airframe 89,800 hrs · 22,910 cycles

CABIN ALT AUTO 1 STATUS MSG. PERFORMED BITE TEST OF AUTO 1 CABIN PRESSURE CONTROLLER , NO FAULTS NOTED ON CONTROLLER, NO FAULTS NOTED AT THIS TIME AS PER AMM 21-31-00.

Part: UNKNOWN — MALFUNCTIONED (APU) · airframe 89,775 hrs · 22,899 cycles

AFTER LANDING APU WOULD NOT START, 3 ATTEMPTS FAILED. PERFORMED APU BITE CHECK IAW AMM 49-61-05/201, APU STARTING 49-11-00-802-002, OPS CHECKED GOOD.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 89,753 hrs · 22,893 cycles

CTR RT FUEL PUMP EICAS MESSAGE ON TAKE OFF ROLL. REJECTED T/O. TRANSFERRED FUEL TO WINGS IAW AMM 28-26-00 ACCOMPLISHED. OPS CHECK ON CENTER PUMP IAW AMM 28-22-00 OPS CHECK GOOD AT THIS TIME.

Part: STARTER — INOPERATIVE (APU) · airframe 89,691 hrs · 22,871 cycles

APU COLD SOAK START UNSUCCESSFUL AFTER 3 ATTEMPTS SAT -50, FL 370. REMOVED AND REPLACED APU STARTER AS PER AMM 49-41-01. OPS AND LEAK CHECK OK.

Part: SLIDING WINDOW — SCRATCHED (COCKPIT) · airframe 89,669 hrs · 22,865 cycles

RT NR 2 WINDOW HAS SCRATCHES IN LINE OF SIGHT. REMOVED AND REPLACED RT NR 2 SLIDING WINDOW IAW AMM 56-11-02-004-001 AND 56-11-02-404-026. ALL OPS CHECKS AND ADJUSTMENTS GOOD.

Part: STATUS MESSAGE — FALSE ACTIVATION (COCKPIT) · airframe 89,602 hrs · 22,840 cycles

CABIN ALT AUTO 1 STATUS MESSAGE DISPLAYED. PERFORMED BITE CHECK ON CABIN ALT AUTO - 1 CONTROLLER UNIT IAW AMM 21-31-01. NO FAULT FOUND ON THE CONTROLLER.

Part: IDG — INOPERATIVE (RT ENGINE) · airframe 89,459 hrs · 22,777 cycles

RIGHT IDG INOPERATIVE. REMOVED AND REPLACED THE IDG IAW AMM 24-11-01, AND AMM 24-22-02.

Part: IDG — INOPERATIVE (NR 2 GENERATOR) · airframe 89,353 hrs · 22,742 cycles

NR 2 GENERATOR INOPERATIVE EICAS MESSGAE, NO RESET. NNC COMPLETE. REMOVED AND REPLACED THE IDG IAW AMM 24-11-01. PERFORMED A LEAK AND OPS CHECK IAW AMM 24-11-0.

Part: TUBE — CLOGGED (CONTROL VALVE) · airframe 89,299 hrs · 22,721 cycles

DUCT PRESSURE TO LOW FOR START, APU RUNNING, PACKS OF 22PSI ONCE STARTER ENGAGES DROPS TO 8 PSI, N2 MOTORS TO LESS THAN 10%. PERFORMED FIM 49-11 FAULT TREE 977, FOUND DEBRIS IN THE SURGE CONTROL VALVE SUPPLY TUBE. REMOVED THE DEBRIS, NO FURTHER FAULTS FOUND.

Part: START VALVE — STUCK (RT ENGINE) · airframe 89,201 hrs · 22,683 cycles

RIGHT ENGINE START VALVE STUCK OPEN. REMOVED AND REPLACED THE NR 2 ENGINE START VALVE IAW AMM 80-11-02, LEAK CHECKED OK.

Part: WARNING MESSAGE — FALSE ACTIVATION (TEMP) · airframe 89,199 hrs · 22,682 cycles

AFT CABIN TEMP EICAS MESSAGE. PERFORMED A BITE CHECK OF THE ZONE TEMP CONTROLLER IAW AMM 21-61-03, NO FAULTS NOTED.

Part: WARNING MESSAGE — FALSE ACTIVATION (APU) · airframe 89,186 hrs · 22,676 cycles

APU FAULTED. PERFORMED AN APU BITE IAW FIM 49-11, FAULT TREE 958, NO DEFECTS NOTED. PERFORMED AN APU OPS CHECK IAW AMM 49-11-00 TWO TIMES, NO FAULTS NOTED, OPS CHECKED GOOD.

Part: RELAY — FAILED (BOOST PUMP) · airframe 89,199 hrs · 22,682 cycles

LT AFT BOOST PUMP EICAS MESSAGE. REMOVED & REPLACED THE GFI RELAY IAW SWPM 20-30-00. PERFORMED AN OPS CHECK IAW AMM 28-22-00, OPS NORMAL.

Part: STARTER — FAILED (LT ENGINE) · airframe 89,178 hrs · 22,673 cycles

LEFT ENGINE DID NOT START. REMOVED AND REPLACED THE STARTER ASSY IAW AMM 80-11-01. OPS CHECKED OK.

Part: WARNING MESSAGE — FALSE ACTIVATION (APU) · airframe 89,147 hrs · 22,660 cycles

APU FAULT EICAS MESSAGE ON TWO START ATTEMPTS AFTER LANDING. EGT NEVER ABOVE 775 AND RPM NEVER ABOVE 28. UNABLE TO DUPLICATED START NORMAL IAW AMM 49-21-00.

Part: VALVE — FAILED (APU) · airframe 89,079 hrs · 22,635 cycles

APU BLEED AIR DROPS TO 6 PSI WITH PACKS ON. REMOVED AND REPLACED APU VALVE IAW AMM 36-11-10. OPS CHECK GOOD. REMOVED AND REPLACED FLOW MODULE SERIAL 2023, PART 490050 IAW AMM 49-53-00 OPS CHECKS GOOD.

Part: APU — FAULTED · airframe 89,049 hrs · 22,623 cycles

APU FAULT, NO START. ACCOMPLISHED AN OPS CHECK IAW AMM 49-11-00, AND ACCOMPLISHED AN ECU CHECK IAW AMM 49-61-05. RAN APU, CHECKED NORMAL, NO FAULTS.

Part: LIGHT — INOPERATIVE (SPAR VALVE) · airframe 88,966 hrs · 22,589 cycles

RIGHT ENGINE SPAR VALVE LIGHT INDICATION INOPERATIVE. R & R THE RT SPAR VALVE LIGHT ASSY, OPS CHECKED OK.

Part: VALVE — UNKNOWN (RT ENGINE) · airframe 88,949 hrs · 22,582 cycles

RIGHT ENGINE SPAR VALVE FAILED TO ILLUMINATE UPON ENGINE START. PERFORMED OPS CHECKS OF ENG SPAR VALVE IAW 28-22-11 AND RAN ENG AT IDLE IAW AMM 71-00-00. OPS CHECK NORMAL AT THIS TIME. INBD FLT CREW ALSO REPORTED OPS CHECKS NORMAL. THIS CLEARS MDDR. DISPATCH JL0319Z.&NBSP;</P>)

Part: RADAR — UNKNOWN (WX SYSTEM) · airframe 88,898 hrs · 22,564 cycles

WEATHER RADAR INOPERATIVE. RESET THE CIRCUIT BREAKERS, PERFORMED OPS CHECKS IAW AMM 34-43-00, OPS CHECKED GOOD, NO DEFECTS NOTED AT THIS TIME

Part: SEAL — TORN (FAN CASE) · airframe 88,853 hrs · 22,546 cycles

NR 2 ENGINE FAN CASE SEAL TORN ABOUT 4 INCHES AT THE 6 O'CLOCK POSTION. REPAIRED THE FAN CASE SEAL IAW AMM 72-33-00.

Part: PRESSURE SWITCH — FAULTED (SHUTOFF VALVE) · airframe 88,853 hrs · 22,546 cycles

LEFT PRSOV LOW PRESSURE SWITCH FAULTY. REMOVED AND REPLACED THE SHUTOFF VALVE IAW AMM 36-11-09. OPS CHECKED NORMAL.

Part: PRIORITY VALVE — MALFUNCTIONED (LEFT) · airframe 88,853 hrs · 22,546 cycles

LEFT PRV DOES NOT INDICATE OPEN. REMOVED AND REPLACED THE VALVE AND OPS CHECKED NORMAL IAW AMM 36-11-18.

Part: BOOT — TORN (APU BLEED VALVE) · airframe 88,853 hrs · 22,546 cycles

APU SURGE BLEED VALVE BOOT TORN. REMOVED AND REPLACED THE BLEED VALVE BOOT IAW AMM 49-53-01.

Part: BOLT — MISSING (ENGINE) · airframe 88,853 hrs · 22,546 cycles

FOUND A BOLT AND BUSHING MISSING ON THE NR 2 ENGINE 11TH STAGE COOLING AIR TUBES AT THE 4 O'CLOCK POSITION. INSTALLED THE BOLT IAW AMM 75-24-03.

Part: PRIORITY VALVE — MALFUNCTIONED (RIGHT) · airframe 88,853 hrs · 22,546 cycles

RIGHT PRSOV WILL NOT INDICATE OPEN. REMOVED AND REPLACED THE PRSOV IAW AMM 36-11-09.

Part: IGNITER — FOULED (APU) · airframe 88,853 hrs · 22,546 cycles

APU IGNITER PLUG FOULED. REMOVED AND REPLACED THE IGNITER PLUG IAW 49-41-02. OPS CHECKED NORMAL.

Part: O-RING — WORN (CONTROLLER) · airframe 88,853 hrs · 22,546 cycles

HIGH PRESSURE CONTROLLER O RING AT FITTING IS WORN(<P>REMOVED AND REPLACED O RING AT ENG 2 HPSOV. OPS CHECK NORMAL IAW AMM 36-11-08</P>)

Part: PRESSURE SWITCH — FAILED (ANTI ICE SYSTEM) · airframe 88,757 hrs · 22,506 cycles

RIGHT ENGINE TAI VALVE STATUS MESSAGE IN FLIGHT WITH ENG ANTI-ICE ON. REPLACED THE PRESSURE SWITCH S525. CHECKED GOOD IAW AMM 30-21-01, & 30-21-03.

Part: WARNING LIGHT — FALSE ACTIVATION (CABIN TEMP) · airframe 88,668 hrs · 22,480 cycles

AFT CABIN TEMP INOPERATIVE. HTC AND MESSAGE RESET IN FLT, NO FAULTS ON TEMP CONTROL BOX IAW AMM 21-51-00.

Part: TERMINAL — BROKEN (PRV) · airframe 88,152 hrs · 22,328 cycles

DURING A TEST, THE LT PRV FAILED, TROUBLESHOT IAW WDM 36-11-61. FOUND WIRE W3312-007-18 BROKEN OFF AT TERMINAL. REPLACED THE TERMINAL TO WIRE STUD.

Part: RADAR — MALFUNCTIONED (WX SYS) · airframe 88,144 hrs · 22,323 cycles

LEFT RADAR STABILIZATION PRESENTS STREAKS DURING CRUISE AND DESCENT. RADAR CHECKED NORMAL IAW FIM 34-43 FAULT TREE 805. CHECKED BOTH LT AND RT TRANSCEIVERS, NO FAULTS FOUND.

Part: CONTROL VALVE — FAILED (RT A/C PACK) · airframe 87,972 hrs · 22,264 cycles

RIGHT PACK TEMP EICAS ILLUMINATED INTERMITTENTLY DURING CLIMB OUT, LIGHT OUT IN STANDBY. REMOVED AND REPLACED THE RT ACM TEMP CONTROL VALVE OPS & LEAK CHECKED GOOD IAW AMM 21-51-12.

Part: CONTROLLER — MALFUNCTIONED (RT ENGINE BLEED) · airframe 87,940 hrs · 22,253 cycles

RT ENGINE BLEED OFF EICAS MESSAGE NUMEROUS TIMES DURING DECENT. REMOVED & REPLACED IAW AMM. OPS CHECKED GOOD.

Part: WARNING LIGHT — FALSE ACTIVATION (APU) · airframe 87,928 hrs · 22,249 cycles

APU AUTO SHUTDOWN, GENERATOR FILTER SHOWS ON BITE. PERFORMED BITE TEST IAW FIM 49-11-A26, EGT NR 2 FAULT SHOWS. REPAIRED EGT 2 WIRE HARNESS IAW SWPM 20-10-115 AND WDM 49-14-11, SYSTEM OPS CHECKED OK.

Part: TERMINAL — BROKEN (VALVE) · airframe 87,914 hrs · 22,245 cycles

LEFT ENGINE PRV, FOUND A BROKEN GROUND TERMINAL. REPAIRED THE WIRE AND REPLACED TERMINAL LUG AT PRV LT IAW SWPM 20-30-00. OPS CHECKED GOOD IAW 36-11-18-501.

Part: CONTROL VALVE — MALFUNCTIONED (A/C PACK TEMP) · airframe 87,914 hrs · 22,245 cycles

RIGHT PACK TEMP MESSAGE, EXTINGUISHES WITH STBY -B. REMOVED AND REPLACED THE A/C PACK TEMP CONTROL VALVE IAW 21-51-12, OPS CHECKED GOOD.

Part: SENSOR — MALFUNCTIONED (APU) · airframe 87,914 hrs · 22,245 cycles

APU FAILED AUTO SHUTDOWN DURING ENGINE START. TROUBLESHOT IAW FIM 49-11 F/T 970, REMOVED AND REPLACED THE APU PA SENSOR. OP CHECKED GOOD IAW AMM 49-61-04.

Part: STARTER — LEAKING (APU) · airframe 87,760 hrs · 22,195 cycles

APU INOPERATIVE DUE TO AN OIL LEAK. LOCATED LEAK TO BE COMING FROM STARTER. R & R STARTER MOTOR IAW 49-41-01. RAN APU FOR 30 MINUTES IAW 49-11-00, NO FAULTS NOTED, NO LEAKS NOTED AT THIS TIME.

Part: WARNING MESSAGE — FALSE ACTIVATION (APU OIL) · airframe 87,755 hrs · 22,193 cycles

APU QUANTITY STARTED AND OPERATED APU BY 30 MINUTES WITH PNEUMATIC & SUPPLY ON MONITOR FOR LEAKS, NO LEAKS NOTED. CHECKED OIL QTY AGAIN NO OIL LOSS NOTED. PERFORMED APU BITE TEST, CHECKED FLAGS, NO FAULTS NOTED IAW AMM 12-13-04 AND AMM 49-11-00 FIM 49-11FT 958.

Part: TRANSCEIVER — FAILED (WX RADAR SYS) · airframe 87,699 hrs · 22,177 cycles

RIGHT WEATHER RADAR FAILED. REPLACED THE WEATHER RADAR R/T IAW AMM 34-43-01. OPS CHECKED GOOD.

Part: BATTERY — INOPERATIVE (APU) · airframe 87,718 hrs · 22,182 cycles

APU WILL NOT START. APU FAULT DISPLAYED. R & R THE APU BATTERY AND CHARGER IAW AMM 24-31-04.

Part: LIGHT — LOOSE (APU) · airframe 87,718 hrs · 22,182 cycles

APU FAIL LIGHT MODULE INOPERATIVE. REMOVED APU LIGHT LEN CAP FOR INSPECTION CONDITIONS AND PROPER CONTACT, OPS CHECKED NORMAL IAW AMM 33-16-02.

Part: CONNECTOR — MISROUTED (APU ECU) · airframe 87,718 hrs · 22,182 cycles

APU ECU FAULTY, EGT HARNESS CIRCUIT NR 2 FAULT LATCHED ON. FOUND HARNESS CONNECTORS FOR EGT CIRCUITS 1 AND 2 CROSSED. CORRECTED THE CONNECTORS IAW SWPM 20-10-11. OPS CHECKED NORMAL.

Part: CHARGER — FAULTED (APU) · airframe 87,718 hrs · 22,182 cycles

APU BATTERY CHARGER IS FAULTY. R & R APU BATTERY CHARGER IAW AMM 24-31-05.

Part: WARNING MESSAGE — FALSE ACTIVATION (EXHAUST FAN) · airframe 87,697 hrs · 22,176 cycles

STATUS MESSAGE FOR THE NR 2 AFT EQUIPMENT EXHAUST FAN. CLEARED THE STATUS MESSAGE IAW FIM 21-26 FT 806 BLKS 1,3,20,41. OPS CHECKED NORMAL.

Part: ECU — MALFUNCTIONED (APU) · airframe 87,660 hrs · 22,164 cycles

WHILE PERFORMING APU MAINTENANCE, THE APU INDICATORS FOR EGT AND RPM WERE ZERO WHILE APU WAS RUNNING. REMOVED AND REPLACED ECU IAW AMM 49-61-05, OPS CHECKED NORMAL.

Part: APU — FAULTED · airframe 87,643 hrs · 22,159 cycles

DURING APU START ATTEMPT ON GROUND, FIRST ATTEMPT, APU FAULT DISPLAYED. SECOND ATTEMPT, APU FAULT DISPLAYED.

Part: GFI — MALFUNCTIONED (FUEL SYSTEM) · airframe 87,645 hrs · 22,160 cycles

LEFT FWD FUEL PUMP INOP. RESET GFI, PERFORMED OPS CHECKS IAW AMM 28-22-00. GFI DID NOT POP AGAIN, OPS CHECK NORMAL AT THIS TIME THIS CLEARS MDDR 81440.

Part: WARNING LIGHT — ILLUMINATED (FUEL PUMP) · airframe 87,643 hrs · 22,159 cycles

LEFT FWD FUEL PUMP LOW PRESSURE LIGHT ILLUMINATED.

Part: ECU — FAULTED (APU) · airframe 87,543 hrs · 22,130 cycles

APU FAULT EICAS. REMOVED AND REPLACED APU ECU IAW AMM 49-61-05, OPS CHECKED GOOD.

Part: APU — MALFUNCTIONED · airframe 87,543 hrs · 22,130 cycles

APU FAULT, APU WOULD NOT START. APU STARTED ON FIRST ATTEMPT IAW AMM 49-11-00 PERFORMED APU ECU SELF AND BITE TEST IAW AMM 49-61-05. PREVIOUS FAULT EGT 2 CIRCUIT AND MINI FLAG. NO DEFECTS NOTED. MEMORY CLEARED FAULTS REMOVED. OPS CHECKED GOOD IAW AMM 49-11-00.

Part: CONNECTOR — DIRTY (TEMP CONTROL) · airframe 87,532 hrs · 22,126 cycles

RIGHT TEMP CONTROL INOPERATIVE. ACCOMPLISHED PROCESS AND TEST IAW AMM 21-51-12-01-055. CLEANED AND RECONNECTED THE ELECTRICAL CONNECTOR TWICE ON RIGHT PACK TEMP CONTROL VALVE. BITE ON RT PACK TEMP CONTROL NO FAULTS CLEARED.

Part: CONNECTOR — LOOSE (SHUTOFF VALVE) · airframe 87,503 hrs · 22,115 cycles

LEFT ENGINE OFF, BLEED OFF EICAS MESSAGES DISPLAYED NUMEROUS TIMES DURING DECENT, AT HIGH ALTITUDE AND DURING APPROACH BELOW 3000 FT. FOUND THE PRSOV CONNECTOR M22 LOOSE. TIGHTENED THE CONNECTOR AND CHECKED GOOD IAW AMM 36-11-04.

Part: WARNING MESSAGE — FALSE ACTIVATION (WX RADAR SYS) · airframe 87,403 hrs · 22,084 cycles

DURING CLIMB OUT, SWITCHED TO WEATHER RADAR AND RECIEVED A WXR FAIL ON EHSI. PERFORMED SYSTEM TEST IAW AMM 34-43-00, OPS CHECKED GOOD.

Part: O-RING — LEAKING (CHIP DETECTOR) · airframe 87,333 hrs · 22,063 cycles

FOUND OIL LEAKING FROM APU METAL CHIP DETECTOR. R & R THE O-RING ON APU METAL CHIP DETECTOR IAW 49-27-04.

Part: INDICATION SYS — UNKNOWN (DUCT PRESSURE) · airframe 87,333 hrs · 22,063 cycles

LEFT DUCT PRESSURE SURGES 10 PSI TO 40 PSI WHEN ENGINE ANTI-ICE SELECTED. PERFORMED OPERATIONAL CHECK, NO DEFECTS NOTED IAW AMM 30-21-00.

Part: WARNING MESSAGE — FALSE ACTIVATION (DUCT PRESSURE) · airframe 87,285 hrs · 22,045 cycles

DURING CRUISE FL390, THERE WAS A DUCT PRESSURE SPLIT LT 45 RT 20. OPS CHECKED AIR CONDITIONING PRESSURIZATION SYSTEM IAW AMM 21-51-00, NO DEFECTS NOTED.

Part: THERMOCOUPLE — FAILED (NR 2 EGT) · airframe 87,103 hrs · 21,981 cycles

MAINTENANCE MESSAGE FOR APU BITE. PERFORMED A BITE CHECK, AND ECU FAULTED, EGT FAULTED, EGT NR 2 CIRCUIT. R & R THE NR 2 EGT UPPER THERMOCOUPLE IAW 49-71-01. BITE CHECK PASSED, CIRCUIT BREAKER CHECKED NORMAL.

Part: SOFTWARE — INCORRECT (FMC) · airframe 87,065 hrs · 21,969 cycles

TO OPERATE WX RADAR MUST CYCLE SWITCH ON EFIS PANEL, ON, OFF, & ON, THEN SELECT WX RADAR. FOUND INCORRECT SOFTWARE IN LT & RT FMC. INSTALLED 995-0191-010 SOFTWARE IAW AMM 34-22-00. OPS CHECKED GOOD.

Part: UNKNOWN — MALFUNCTIONED (WETHER RADAR) · airframe 87,063 hrs · 21,968 cycles

WX RADAR FAILED ON CLIMB OUT. PERFORMED OPERATIONAL CHECK IAW AMM 34-43-00 OPS CHECK NORMAL.

Part: SOFTWARE — FAULTY (EICAS) · airframe 87,061 hrs · 21,967 cycles

EICAS STATUS PAGE DISPLAYS APU OIL ADD. UPDATED EICAS SOFTWARE PER AMM 31-41-02. OPS GOOD.

Part: PUMP — NOT REPORTED (FUEL) · airframe 87,060 hrs · 21,966 cycles

CIRCUIT BREAKER, RIGHT FUEL OVERRIDE PUMP. REMOVED AND REPLACED R/H OVERRIDE PUMP IAW AMM 28-22-05, AND 28-22-05-404-078-022. OPS CHECKED GOOD IAW AMM 28-31-00.

Part: VALVE — WARNING MESSAGE (LT ENGINE) · airframe 87,060 hrs · 21,966 cycles

RIGHT ENGINE PRIORITY VALVE EICAS MESSAGE RECEIVED AFTER ENGINE START. DISAPPEARED AFTER 5 MINUTES. REMOVED AND REPLACED THE RT ENGINE PRIORITY VALVE IAW AMM 36-11-18. CHECKED OK.

Part: WEB — CORRODED (BS 1219) · corrosion level 2 · airframe 87,038 hrs · 21,962 cycles

AFT CARGO BAY, THE WEB WAS FOUND CORRODED. THE WEB WAS TRIMMED & WEB REPAIRED IAW EN1076-17, REV-.

Part: INTERCOSTAL — WORN (RT NACELLE) · airframe 87,038 hrs · 21,962 cycles

RT ENGINE, RT CORE COWL PRESSURE RELIEF DOOR SURROUNDING INTERCOSTAL FOUND WORN. INTERCOSTAL REMOVED AND REPLACED IAW SRM 51-40-02, REV 103.

Part: FAIRING — DAMAGED (NR PYLON) · airframe 87,038 hrs · 21,962 cycles

NR 1 PYLON FAIRING ASSY, HAD ONE ELONGATED HOLE OUTBOARD AFT FAIRING ASSY. REPAIRED IAW EN1048-17, REV.

Part: RUB STRIP — WORN (RT NACELLE) · airframe 87,038 hrs · 21,962 cycles

RIGHT ENGINE, LT CORE COWL INTERIOR SURFACE AFT UPPER EDGE RUB STRIP FOUND WORN. RUB STRIP WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 103.

Part: ADAPTER — WORN (LT NACELLE) · airframe 87,038 hrs · 21,962 cycles

LEFT ENGINE, RT CORE COWL INTERIOR SURFACE HOLD OPEN ROD STOW PIN SUPPORT BRACKET & ADAPTER WERE FOUND WORN. THE HOLD OPEN ROD STOW PIN BRACKET AND ADAPTER WERE REMOVED AND REPLACED IAW SRM 51-40-02, REV 103.

Part: RUB STRIP — WORN (LT NACELLE) · airframe 87,038 hrs · 21,962 cycles

LEFT ENGINE, RT CORE COWL FAIRING ASSY INTERIOR SURFACE AFT UPPER EDGE RUBSTRIP FOUND WORN. THE RUBSTRIP WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 103.

Part: CHANNEL — WORN (LT NACELLE) · airframe 87,038 hrs · 21,962 cycles

LEFT ENGINE, LT CORE COWL INTERIOR SURFACE MOST AFT HAT CHANNEL HAD TWO EXISTING REPAIR ANGLE DOUBLERS FOUND WORN, LOCATED 19 INCHES & 30.3 INCHES FROM LOWER EDGE. THE CHANNEL WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 103.

Part: BUTT JOINT — CORRODED (BS 434) · corrosion level 2 · airframe 87,038 hrs · 21,962 cycles

FWD CARGO BAY, BS 434 BETWEEN STRINGERS 35L AND 35R, BUTT SPLICE FOUND CORRODED. THE BUTT SPLICE WAS REMOVED & REPLACED IAW SRM 51-40-02, REV.103.

Part: RUB STRIP — DAMAGED (RT NACELLE) · airframe 87,038 hrs · 21,962 cycles

RIGHT ENGINE, RT CORE COWL EXTERIOR SURFACE FWD EDGE SEVERAL WEAR STRIP WITH COATING FRETTED & CRACKED.THE WEAR STRIP WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 103.

Part: CHANNEL — WORN (RT NACELLE) · airframe 87,038 hrs · 21,962 cycles

RIGHT ENGUNE, LT CORE COWL INTERIOR SURFACE MOST AFT HAT CHANNEL HAD ONE EXISTING REPAIR ANGLE DOUBLER WORN, LOCATED 6 INCHES FROM LOWER EDGE. THE HAT CHANNEL WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 103.

Part: WEB — CRACKED (BS 1197.66) · airframe 87,038 hrs · 21,962 cycles

AFT CARGO AT BS 1197+66, LBL 41, WL 120 STIFFENER TO WEB HAD TWO RIVETS SHEARED AND WEB CRACKED. THE WEB WAS TRIMMED & REPAIRED IAW EN1078-17, REV-.

Part: ROD END — WORN (COMPRESSOR) · airframe 87,038 hrs · 2,196,275 cycles

RIGHT ENGINE COMPRESSOR CASE AT THE 9 O'CLOCK POSITION, TCC DUCT THREE SUPPORT RODS FOUND TO HAVE ROD END PLAY.

Part: CONNECTOR — CORRODED · airframe 87,038 hrs · 21,962 cycles

ELECTRICAL CONNECTOR FOUND CORRODED. THE CONNECTOR WAS REMOVED & REPLACED IAW SWPM 20-61-00, REV 64, AND FOUND SATISFACTORY.

Part: STRINGER SPLICE — CORRODED (BS 434) · corrosion level 2 · airframe 87,038 hrs · 21,962 cycles

BS 434, STRINGER SPLICE 38R CORRODED. THE STRINGER SPLICE REMOVED & REPLACED IAW SRM 51-40-02, REV.103.

Part: DRIP TRAY — TORN (NR 2 ENGINE) · airframe 87,038 hrs · 21,962 cycles

RIGHT ENGINE AT THE 2 O'CLOCK POSITION, THE STRUT TO ENGINE FUEL HOSE DRIP SHIELD FOUND TORN.

Part: SEAL — CRACKED (RT NACELLE) · airframe 87,038 hrs · 21,962 cycles

RIGHT ENGINE, LT CORE COWL FAIRING ASSY FLIPPER DOOR SEAL FOUND CRACKED. THE SEAL WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 103.

Part: BYPASS SWITCH — NO TEST (LT ENGINE FUEL) · airframe 87,038 hrs · 2,196 cycles

LEFT ENGINE FUEL FILTER BYPASS SWITCH FAILED AN OPS TEST. THE BYPASS SWITCH WAS REMOVED AND REPLACED IAW AMM 73-34-01, REV 120. OPS TESTED IAW AMM 73-34-01 REV 120, AND FOUND SATISFACTORY.

Part: FRAME — WORN (LT NACELLE) · airframe 87,038 hrs · 21,962 cycles

LEFT ENGINE, RT CORE COWL AFT ZEE FRAME HAS ONE EXISTING REPAIR ANGLE DOUBLER WORN, LOCATED 12 INCHES FROM LOWER EDGE. THE FRAME WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 103.

Part: SEAL — CRACKED (RT NACELLE) · airframe 87,038 hrs · 21,962 cycles

RIGHT ENGINE, RT CORE COWL FAIRING ASSY FLIPPER DOOR SEAL FOUND CRACKED. THE SEAL WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 103.

Part: COOLING FAN — SCRATCHED (FWD CARGO) · airframe 87,038 hrs · 21,962 cycles

FWD CARGO BAY RT AIR COOLING FAN FWD FLANGE FOUND WITH DEEP SCRATCHES. REMOVED AND REPLACED THE COOLING FAN IAW AMM 21-58-06, REV 120. OPS TEST CARRIED OUT IAW AMM 21-58-06, REV 120, AND FOUND SATISFACTORY.

Part: STRINGER SPLICE — CORRODED (BS 434) · corrosion level 2 · airframe 87,038 hrs · 21,962 cycles

FWD CARGO AT BS 434, STRINGER SPLICE 37L CORRODED. THE STRINGER SPLICE WAS REMOVED & REPLACED IW SRM 51-40-02, REV.103.

Part: STOP — WORN (RT NACELLE) · airframe 87,038 hrs · 21,962 cycles

RIGHT ENGINE, LT CORE COWL INTERIOR SURFACE MOST AFT HAT CHANNEL HAD ONE STOP FOUND WORN. THE HAT FRAME STOP REMOVED AND REPLACED IAW SRM 51-40-02, REV 103.

Part: LONGERON — WORN (RT NACELLE) · airframe 87,038 hrs · 21,962 cycles

RIGHT ENGINE, RT CORE COWL INTERIOR SURFACE LOWER MOST AFT LONGERON FOUND WORN. LONGERON REMOVED AND REPLACED IAW SRM 51-40-02, REV 103.

Part: RIVET — SHEARED (LT NACELLE) · airframe 87,038 hrs · 21,962 cycles

LEFT ENGINE, RT CORE COWL FWD LOWER SECTION FOUND SEVERAL RIVETS SHEARED. THE RIVETS WERE REMOVED AND REPLACED IAW SRM 51-40-02, REV 103.

Part: SKIN — WORN (RT NACELLE) · airframe 87,038 hrs · 21,962 cycles

RIGHT ENGINE, LT CORE COWL FAIRING SKIN UPPER AFT CUTOUT SECTION INTERIOR SURFACE FOUND WORN. THE SKIN WAS REPAIRED IAW SRM 54-423-01-2R-5, REPAIR 5 , REV 103.

Part: SEAL — CRACKED (RT NACELLE) · airframe 87,038 hrs · 21,962 cycles

RIGHT ENGINE, RT CORE COWL FAIRING ASSY AFT UPPER EDGE STRIP SEAL FOUND CRACKED. THE SEAL WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 103.

Part: FRAME — WORN (RT NACELLE) · airframe 87,038 hrs · 21,962 cycles

RT ENGINE, RT CORE COWL AFT ZEE FRAME REPAIR ANGLE DOUBLER & FILLER FOUND WORN. REMOVED AND REPLACED IAW SRM 51-40-02, REV 103.

Part: SEAL — TORN (NR 2 NACELLE) · airframe 87,038 hrs · 21,962 cycles

NR 2 ENGINE, RT FAN COWL LOWER EDGE MOST FWD AND SECOND FROM FWD SEALS FOUND TORN. REMOVED AND REPLACED IAW AMM 70-50-00, REV 120.

Part: BULKHEAD WEB — DENTED (BS 1582) · airframe 87,038 hrs · 21,962 cycles

AFT CABIN, AFT PRESSURE BULKHEAD BS 158 DENTED. TRIMMED & REPAIRED IAW SRM 53-80-08, REPAIR 2, DETAIL I, REV 103.

Part: DOOR FRAME — CORRODED (BS 923.7) · corrosion level 2 · airframe 87,038 hrs · 21,962 cycles

L2 DOOR CUTOUT BS 923.7, WL 200.73 FOUND THE DOOR FRAME WEB CORRODED. TRIMMED THE AREA & REPAIRED IAW EN 1071-17, REV-.

Part: DUCT — WORN (PRECOOLER) · airframe 87,038 hrs · 21,962 cycles

RT ENG, RT CORE COWL PRECOOLER EXIT DUCT LIP FOUND WORN. REPAIRED IAW SB 71-032 REV 2.

Part: FEEDER CABLE — CHAFED · airframe 87,038 hrs · 21,962 cycles

FWD STRUT, TWO FEEDER WIRES FOUND CHAFED. THE FEEDER WIRES PROTECTED WITH TEFLON TAPES IAW SWPM 20-10-13, REV 64, AND FOUND SATISFACTORY.

Part: RIVET — SHEARED (LT NACELLE) · airframe 87,038 hrs · 21,962 cycles

LEFT ENGINE, RT CORE COWL EXTERIOR SURFACE PRECOOLER ASSY FOUND RIVET SHEARED. THE RIVET WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 103.

Part: FIRESHIELD — DAMAGED (RT NACELLE) · airframe 87,038 hrs · 21,962 cycles

RIGHT ENG, RT CORE COWL INTERIOR SURFACE FIRESHIELD FOUND WITH TWO HOLES. REPAIRED IAW SRM 54-42-01-2R-6, REPAIR 6, REV 103.

Part: SKIN — CORRODED (BS 1263) · corrosion level 2 · airframe 87,038 hrs · 21,962 cycles

AFT CARGO, BS 1263, STRINGER 37-38R, BILGE AREA INNER SURFACE SKIN CORRODED. AREA TRIMMED OUT & REPAIRED IAW EN 1069-17, REV-.

Part: RUB STRIP — WORN (LT NACELLE) · airframe 87,038 hrs · 21,962 cycles

LEFT ENGINE, RT CORE COWL FAIRING ASSY AFT UPPER EDGE STRIP SEAL FOUND CRACKED. THE RUBSTRIP WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 103.

Part: TEE FITTING — CORRODED (BS 1219) · corrosion level 2 · airframe 87,038 hrs · 21,962 cycles

AFT CARGO, BS 1219, WL 124.43, LBL 44 - RBL 44, FOUND THE TEE FITTING FOUND MULTIPLE AREAS OF SURFACE CORROSION. THE TEE FITTING WAS REMOVED & REPLACED IAW SRM 51-40-02, REV.103.

Part: SUPPORT — WORN (RT NACELLE) · airframe 87,038 hrs · 21,962 cycles

RIGHT ENGINE, RT CORE COWL PRESSURE RELIEF DOOR ASSY INTERIOR SURFACE UPPER LANYARD ATTACHING SUPPORT FOUND WORN. REMOVED AND REPLACED IAW AMM 71-11-09, REV 120. LATCH CHECKED IAW AMM 71-11-09, REV 120, FOUND SATISFACTORY.

Part: SEAL — CRACKED (RT NACELLE) · airframe 87,038 hrs · 21,962 cycles

RIGHT ENGINE, LT CORE COWL FAIRING ASSY AFT UPPER EDGE STRIP SEAL FOUND CRACKED. THE SEAL WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 103.

Part: SEAL — CRACKED (LT NACELLE) · airframe 87,038 hrs · 21,962 cycles

LEFT ENGINE, LT CORE COWL FAIRING ASSY AFT UPPER EDGE STRIP SEAL FOUND CRACKED. THE SEAL WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 103.

Part: SKIN — CORRODED (BS 1583.5-1610) · airframe 87,038 hrs · 21,962 cycles

RIGHT AFT LOWER FUSELAGE SKIN BS 1583.5 - 1610, STRINGER 36R, FOUND THE LAP JOINT AREA CORRODED. THE CORROSION WAS REMOVAL & REPAIRED IAW EN 1020-17, REV-.

Part: FRAME — DAMAGED (RT NACELLE) · airframe 87,038 hrs · 21,962 cycles

RIGHT ENGINE, RT CORE COWL INTERIOR SURFACE AFT LOWER CORNER FOUND FASTENER HOLE ELONGATED ON SUPPORT TEE & HAT FRAME. REAMED TO NEXT SIZE AND A NEW FASTENER INSTALLED IAW SRM 51-40-02, REV 103.

Part: ROD END — WORN (START DUCT) · airframe 87,038 hrs · 21,962 cycles

RIGHT ENGINE, AT THE 10 O'CLOCK POSITION, STARTER DUCT SUPPORT ROD INBD ROD END FOUND DAMAGED.

Part: RUB STRIP — WORN (LT NACELLE) · airframe 87,038 hrs · 21,962 cycles

LEFT ENGINE, LT CORE COWL INTERIOR SURFACE AFT UPPER EDGE RUB STRIP FOUND WORN. THE RUB STRIP WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 103.

Part: ADAPTER — WORN (RT NACELLE) · airframe 87,038 hrs · 21,962 cycles

RT ENGINE, LT CORE COWL INTERIOR SURFACE HOLD OPEN ROD STOW PIN SUPPORT BRACKET & ADAPTER FOUND WORN. THE BRACKET AND ADAPTER WERE REMOVED AND REPLACED IAW SRM 51-40-02, REV 103.

Part: STRUCTURE — ERODED (NR 2 NACELLE) · airframe 87,038 hrs · 21,962 cycles

NR 2 ENGINE, LT FAN COWL FOUND ERODED. THE FAN COWL WAS REPAIRED IAW SRM 54-22-01, REPAIR 4, REV 103.

Part: SKIN — CORRODED (BS 955) · corrosion level 2 · airframe 87,038 hrs · 21,962 cycles

CORROSION FOUND ON THE SKIN, LBL 3 TO RBL 3, BS 955. THE CORROSION WAS REMOVED & REPAIRED IAW EN 1022-17, REV-.

Part: BLADE — NICKED (RT ENGINE FAN) · airframe 87,038 hrs · 21,962 cycles

RIGHT ENGINE, NR 31 FAN BLADE L/E FOUND WITH ONE NICK.

Part: FRAME — CRACKED (RT NACELLE) · airframe 87,038 hrs · 21,962 cycles

RIGHT ENGINE, LT CORE COWL INTERIOR SURFACE UPPER SECOND FRAME FROM AFT, FOUND CRACKED. THE FRAME WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 103.

Part: RUB STRIP — WORN (LT NACELLE) · airframe 87,038 hrs · 21,962 cycles

LEFT ENGINE, RT CORE COWL INTERIOR SURFACE UPPER AFT EDGE WEAR STRIP FOUND WORN. THE WEAR STRIP WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 103.

Part: SKIN — CORRODED (BS 430) · corrosion level 2 · airframe 87,038 hrs · 21,962 cycles

FWD CARGO BAY SKIN CORRODED UNDER STRINGER 36R, BS 430. THE SKIN WAS TRIMMED & REPAIRED IAW EN 1043-17, REV-.

Part: SEAL — DETACHED (RT ENGINE FAN) · airframe 87,038 hrs · 21,962 cycles

RIGHT ENGINE FAN CASE L/E SEAL UPPER PORTION, FOUND DETACHED.

Part: SEAL — TORN (LT NACELLE) · airframe 87,038 hrs · 21,962 cycles

LEFT ENGINE, LT CORE COWL INTERIOR SURFACE UPPER FWD EDGE SEAL FOUND TORN. THE SEAL WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 103.

Part: RIVET — LOOSE (LT NACELLE) · airframe 87,038 hrs · 21,962 cycles

LEFT ENGINE, LT CORE COWL FWD LOWER SECTION FOUND SEVERAL RIVETS LOOSE. THE RIVETS WERE REMOVED AND REPLACED IAW SRM 51-40-02, REV 103.

Part: STRINGER SPLICE — CORRODED (BS 434) · corrosion level 2 · airframe 87,038 hrs · 21,962 cycles

FWD CARGO BAY AT BS 434 STRINGER SPLICE 39R CORRODED. THE STRINGER SPLICE WAS REMOVED & REPLACED IAW SRM 51-40-02, REV.103.

Part: ADAPTER — WORN (RT NACELLE) · airframe 87,038 hrs · 21,962 cycles

RIGHT ENGINE, RT CORE COWL INTERIOR SURFACE HOLD OPEN ROD STOW PIN SUPPORT BRACKET &;ADAPTER FOUND WORN. REMOVED AND REPLACED IAW SRM 51-40-02, REV 103.

Part: ADAPTER — WORN (NR 2 NACELLE) · airframe 87,038 hrs · 21,962 cycles

NR 2 ENGINE, RT FAN COWL INTERIOR SURFACE HOLD OPEN ROD STOW PIN ADAPTER AND FITTING FOUND WORN, LOCATED AT FWD LOWER SECTION. REMOVED AND REPLACED IAW SRM 51-40-02 REV 103.

Part: BONDING JUMPER — DIRTY · airframe 87,038 hrs · 21,962 cycles

LEFT INBD MAIN FUEL TANK FUELING SHUTOFF VALVE BONDING RESISTANCE CHECK FOUND OUT OF TOLERANCE. THE BONDING JUMPER WAS REMOVED, CLEANED & INSTALLED IAW AMM 20-11-00, REV 120. BONDING RESISTANCE CHECK CARRIED OUT IAW AMM 28-22-11, REV 120 AND FOUND SATISFACTORY.

Part: ANGLE — CRACKED (LT NACELLE) · airframe 87,038 hrs · 21,962 cycles

LEFT ENGINE, RT CORE COWL FAIRING ASSY INTERIOR SURFACE AFT ANGLE FOUND CRACKED. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 103

Part: STRINGER SPLICE — CORRODED (BS 434) · corrosion level 2 · airframe 87,038 hrs · 21,962 cycles

BS 434, STRINGER SPLICE 38L CORRODED. THE STRINGER SPLICE WAS REMOVED & REPLACED IAW SRM 51-40-02, REV.103.

Part: RUB STRIP — CRACKED (LT NACELLE) · airframe 87,038 hrs · 21,962 cycles

LEFT ENGINE, LEFT CORE COWL EXTERIOR SURFACE FWD EDGE SEVERAL WEAR STRIP FOUND THE COATING FRETTING & CRACKED. THE WEAR STRIP WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 103.

Part: SHEAR PIN — WORN (NR 2 NACELLE) · airframe 87,038 hrs · 21,962 cycles

NR 2 ENGINE, RT FAN COWL LOWER MOST FWD AND AFT SHEAR PIN FOUND WORN. THE SHEAR PIN WAS REMOVED AND REPLACED IAW AMM 70-50-00, REV 120.

Part: LONGERON — WORN (RT NACELLE) · airframe 87,038 hrs · 21,962 cycles

RIGHT ENGINE, LT CORE COWL INTERIOR SURFACE LOWER AFT LONGERON FOUND WORN. THE LONGERON WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 103.

Part: BONDING JUMPER — DIRTY · airframe 87,038 hrs · 21,962 cycles

LEFT OTBD MAIN FUEL TANK FUELING SHUTOFF VALVE BONDING RESISTANCE CHECK, FOUND OUT OF TOLERANCE. THE BONDING JUMPER WAS REMOVED, CLEANED & INSTALLED IAW AMM 20-11-00, REV 120. A ELECTRICAL BONDING RESISTANCE CHECK PERFORMED IAW AMM 28-22-11, REV 120, AND FOUND SATISFACTORY.

Part: STRINGER SPLICE — CORRODED (BS 434) · corrosion level 2 · airframe 87,038 hrs · 21,962 cycles

BS 434, STRINGER SPLICE 37R CORRODED. THE STRINGER SPLICE WAS REMOVED & REPLACED IAW SRM 51-40-02, REV.103.

Part: SKIN — CRACKED (RT NACELLE) · airframe 87,038 hrs · 21,962 cycles

RIGHT ENGINE, RT CORE COWL SKIN UPPER AFT CUTOUT SECTION FOUND CRACKED. REPAIRED IAW SRM 54-42-01-2R-4, REPAIR 4, REV 103.

Part: SKIN — CRACKED (RT NACELLE) · airframe 87,038 hrs · 21,962 cycles

RIGHT ENGINE, LT CORE COWL SKIN UPPER AFT CUTOUT SECTION FOUND CRACKED. THE SKIN CUTOUT WAS REPAIRED IAW SRM 54-423-01-2R-4, REPAIR 4, REV 103.

Part: SKIN — CORRODED (BS 1582) · airframe 87,038 hrs · 21,962 cycles

LEFT AFT LOWER FUSELAGE SKIN BS 1582, STRINGER 26L, FOUND THE LAP JOINT AREA CORRODED. THE CORROSION WAS REMOVED IAW EN 1040-17, REV-.

Part: FEEDER CABLE — CHAFED · airframe 87,038 hrs · 21,962 cycles

FWD STRUT FEEDER WIRES FOUND WITH CHAFED. THE FEEDER WIRES PROTECTED WITH TEFLON TAPE IAW SWPM 20-10-13, REV 64, AND FOUND SATISFACTORY.

Part: RIVET — SHEARED (LT NACELLE) · airframe 87,038 hrs · 21,962 cycles

LEFT ENGINE, RT CORE COWL INTERIOR SURFACE MOST AFT HAT FRAME SPLICE ANGLE HAD ONE ATTACHING RIVET FOUND SHEARD. THE RIVET WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 103.

Part: RUB STRIP — CRACKED (RT NACELLE) · airframe 87,038 hrs · 21,962 cycles

RIGHT ENGINE, LT CORE COWL EXTERIOR SURFACE FWD EDGE SEVERAL WEAR STRIP FOUND COATING FRETTED & CRACKED. THE WEAR STRIP WAS REMOVED AND REPLACED IAW SRM 51-40-02 REV 103.

Part: CONNECTOR — CORRODED · airframe 87,038 hrs · 21,962 cycles

D5930J ELECTRICAL CONNECTOR FOUND CORRODED. THE CONNECTOR WAS REMOVED & REPLACED IAW SWPM 20-61-00, REV 64, AND FOUND GOOD.

Part: STRUCTURE — DAMAGED (LT NACELLE) · airframe 87,038 hrs · 21,962 cycles

LEFT ENGINE, RT CORE COWL INTERIOR SURFACE AFT LOWER CORNER FOUND FASTENER HOLE ELONGATED ON SUPPORT TEE & HAT CHANNEL. REPAIRED IAW SRM 51-40-02 , REV 103.

Part: BONDING JUMPER — DIRTY · airframe 87,038 hrs · 21,962 cycles

APU DC FUEL PUMP MOTOR HOUSING AND REAR SPAR BONDING RESISTANCE CHECK FOUND OUT OF LIMITS. THE APU DC PUMP BONDING JUMPER WAS REMOVED, CLEANED, AND INSTALLED IAW AMM 20-11-00, REV 120, AND BONDING RESISTANCE CHECKED IAW AMM 28-25-01, REV 120. FOUND SATISFACTORY.

Part: RETAINER — CRACKED (NR 2 NACELLE) · airframe 87,038 hrs · 21,962 cycles

NR 2 ENGINE, RT FAN COWL INTERIOR SURFACE UPPER AFT EDGE SEAL RETAINER FOUND CRACKED. THE SEAL RETAINER WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 103.

Part: RUB STRIP — CRACKED (LT NACELLE) · airframe 87,038 hrs · 21,962 cycles

LEFT ENGINE, RT CORE COWL EXTERIOR SURFACE FWD EDGE SEVERAL WEAR STRIP FOUND COATING FRETTED & CRACKED. THE WEAR STRIP WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 103.

Part: SHEAR PIN — WORN (NR 1 NACELLE) · airframe 87,038 hrs · 21,962 cycles

NR 1 ENGINE, RT FAN COWL LOWER MOST FWD SHEAR PIN FOUND WORN. THE SHEAR PIN WAS REMOVED AND REPLACED IAW AMM 70-50-00, REV 120.

Part: FRAME — CRACKED (RT NACELLE) · airframe 87,038 hrs · 21,962 cycles

RIGHT ENGINE, LT CORE COWL INTERIOR SURFACE UPPER SECOND FRAME FROM AFT, FOUND CRACKED. THE FRAME WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 103.

Part: RIVET — SHEARED (LT NACELLE) · airframe 87,038 hrs · 21,962 cycles

LEFT ENGINE, LT CORE COWL INTERIOR SURFACE UPPER AFT EDGE WEAR STRIP ATTACHING RIVET FOUND SHEARED. THE RIVET WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 103.

Part: STRINGER — CORRODED (BS 434) · corrosion level 2 · airframe 87,038 hrs · 21,962 cycles

FWD CARGO BAY, BS 434, STRINGER 36R CORRODED. REPAIRED IAW SRM 53-30-03, REPAIR 1, DETAIL III, REV 103, & EN 1043-17, REV-.

Part: PSEU — MALFUNCTIONED · airframe 87,038 hrs · 21,962 cycles

GROUND CREW CALL HORN ALWAYS ON, DOES NOT TO CUT OFF WHEN AIRCRAFT IN AIR MODE, DURING EQUIPMENT COOLING LOW FLOW DETECTOR CHECK. PSEU REMOVED, REPLACED AND TESTED IAW AMM 32-09-04, REV 120A, AND FOUND SATISFACTORY.

Part: FRAME — WORN (RT NACELLE) · airframe 87,038 hrs · 21,962 cycles

RT ENGINE, LT CORE COWL INTERIOR SURFACE SECOND ZEE FRAME FROM FWD ONE EXISTING REPAIR ANGLE DOUBLER FOUND WORN. FRAME REMOVED AND REPLACED IAW SRM 51-40-02, REV 103.

Part: RIVET — LOOSE (RT NACELLE) · airframe 87,038 hrs · 21,962 cycles

RIGHT ENGINE, LT CORE COWL INTERIOR SURFACE AFT UPPER PLATE FOUND RIVET LOOSE. THE LOOSE RIVET WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 103.

Part: ADAPTER — WORN (NR 1 NACELLE) · airframe 87,038 hrs · 21,962 cycles

NR 1 ENGINE, RT FAN COWL INTERIOR SURFACE HOLD OPEN ROD STOW PIN ADAPTER FOUND WORN. THE ADAPTER WAS REMOVED AND REPLACED IAW AMM 70-50-00, REV 120.

Part: SEAL — TORN (RT NACELLE) · airframe 87,038 hrs · 21,962 cycles

RIGHT ENGINE, LT CORE COWL INTERIOR SURFACE UPPER FWD EDGE SEAL FOUND TORN. THE SEAL WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 103.

Part: SKIN — CORRODED (BS 1582-1614) · airframe 87,038 hrs · 21,962 cycles

LEFT AFT LOWER FUSELAGE AT SKIN BS 1582 - 1614, STRINGER 36L FOUND BUTT AND LAP JOINT AREA CORRODED. THE CORROSION WAS REMOVED & REPAIRED IAW EN 1020-17, REV-.

Part: FRAME — WORN (RT NACELLE) · airframe 87,038 hrs · 21,962 cycles

RIGHT ENGINE, RT CORE COWL INTERIOR SURFACE SECOND ZEE FRAME FROM FWD FOUND WORN. THE AREA WAS CLEANED UP AND FOUND WITHIN LIMIT IAW SRM 54-42-02-1A-1, FIG 101, NOTE B, DETAIL 1, REV 103.

Part: CONNECTOR — WORN (LT A/C PACK) · airframe 87,038 hrs · 2,196 cycles

LEFT PACK COMPRESSOR OUTLET TEMP SENSOR TS41 FOUND THE ELECTRICAL CONNECTOR D00688 WORN. THE ELECTRICAL CONNECTOR WAS REMOVED AND REPLACED IAW WDM 21-51-12, REV 26. OPS CHECKED IAW 21-51-14, REV 120, AND FOUND SATISFACTORY.

Part: ADAPTER — WORN (LT NACELLE) · airframe 87,038 hrs · 21,962 cycles

LEFT ENGINE, LT CORE COWL INTERIOR SURFACE HOLD OPEN ROD STOW PIN SUPPORT BRACKET & ADAPTER WERE FOUND WORN. REMOVED AND REPLACED IAW SRM 51-40-02, REV 103.

Part: DOOR — WORN (RT NACELLE) · airframe 87,038 hrs · 21,962 cycles

RIGHT ENGINE, RT CORE COWL PRESSURE RELIEF DOOR SKIN INTERIOR EDGES FOUND WORN. RELIEF DOOR REMOVED AND REPLACED IAW AMM 71-11-09, REV 120. LATCH CHECK CARRIED OUT IAW AMM 71-11-09, REV 120. FOUND SATISFACTORY.

Part: STRUCTURE — ERODED (NR 2 NACELLE) · airframe 87,038 hrs · 21,962 cycles

NR 2 ENGINE, RT FAN COWL FOUND ERODED. THE NR 2 ENGINE FAN COWL WAS REPAIRED IAW SRM 54-22-01, REPAIR 4, REV 103.

Part: TEE FITTING — CORRODED (BS 1197) · corrosion level 2 · airframe 87,038 hrs · 21,962 cycles

AFT CARGO, BS 1197+132, WL 124.43, LBL 44 - RBL 44, FOUND THE TEE FITTING WITH MULTIPLE AREAS OF CORROSION ON THE ANCHOR NUT ATTACHMENT AREA. THE TEE FITTING WAS REMOVED & REPLACED IAW SRM 51-40-02, REV.103.

Part: RUB STRIP — WORN (LT NACELLE) · airframe 87,038 hrs · 21,962 cycles

LEFT ENGINE, LT CORE COWL INTERIOR SURFACE UPPER AFT EDGE WEAR STRIP FOUND WORN. THE WEAR STRIP WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 103.

Part: CHANNEL — CRACKED (RT NACELLE) · airframe 87,038 hrs · 21,962 cycles

RIGHT ENGINE, RT CORE COWL FAIRING AFT UPPER SECTION CHANNEL FOUND CRACKED. CHANNEL REMOVED AND REPLACED IAW SRM 51-40-02, REV 103.

Part: HOUSING — DAMAGED (RT NACELLE) · airframe 87,038 hrs · 21,962 cycles

RT ENGINE, LT CORE COWL AFT KEEPER HOUSING PIN ATTACHING HOLE FOUND ELONGATED & PIN WORN. REMOVED AND REPLACED IAW SRM 51-40-02, REV 103.

Part: SKIN — WORN (RT NACELLE) · airframe 87,038 hrs · 21,962 cycles

RIGHT ENGINE, RT CORE COWL FAIRING SKIN UPPER AFT CUTOUT SECTION INTERIOR SURFACE FOUND WORN. REPAIRED IAW SRM 54-42-01-2R-5, REPAIR 5, REV 103.