N140LL

Part: DUCT — CRACKED (TEMP SENSOR) · airframe 81,648 hrs · 29,512 cycles

WHILE ATTEMPTING TO REMOVE AND REPLACED FAN DUCT TEMP SENSOR FOUND CRACKS IN MOUNTING FLANGE . WELDED AND REPAIRED THE DUCT.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 79,762 hrs · 29,047 cycles

EMERGENCY AISLE LIGHTS ARE INOPERATIVE. REPLACED M737 POWER SUPPLY AND BATTERY PACK. SYSTEM OPERATION IS NORMAL.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 79,756 hrs · 29,044 cycles

STRINGER 38R AT STATION 1540 HAS CORROSION. C/W ERA 558968-14.

Part: SKIN — CORRODED (FUSELAGE) · airframe 79,756 hrs · 29,044 cycles

FUSELAGE SKIN CORRODED FWD OF FS 1582 AT LAV SERVICE PANEL C/W ERA 558970-14.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 79,756 hrs · 29,044 cycles

STRINGER 38L AT STATION 1540 HAS CORROSION. C/W ERA 559163-14.

Part: SKIN — CORRODED (FUSELAGE) · airframe 79,756 hrs · 29,044 cycles

CORROSION ON SKIN JUST FWD OF TAIL SKID FAIRING. REPAIRED IAW ERA 558947-14.

Part: SKIN — CORRODED (LAV PAN) · airframe 79,765 hrs · 29,048 cycles

DURING A C-CHECK, FOUND CORROSION COMMON TO THE LAV PAN ASSY LOCATED AT BS 1582. THE THE SKIN WAS REPAIRED IAW ER/A 558970-14 AND THE TWO LAV SUPPORT FITTINGS WERE REPAIRED IAW ER/A 558996-14.

Part: UNKNOWN — ODOR (COCKPIT & CABIN) · airframe 79,243 hrs · 28,914 cycles

AFTER TAKEOFF, THERE WAS AN OILY, DIRTY SOCK ODOR IN THE COCKPIT. ODOR DISSIPATED AFTER ABOUT 6000 FT, BUT CAME BACK DURING APPROACH AT ABOUT 6000 FT. ODOR WAS ALSO IN FRONT OF CABIN. INSPECTED, AND FOUND NO EXTERNALS LEAKS. REPLACED RECIRCULATION FAN FILTERS. SYSTEM OPERATION IS NORMAL.

Part: ACM — INOPERATIVE (AC BAY) · airframe 78,552 hrs · 28,673 cycles

CREW REPORTS ACID SMELL IN CABIN. LEFT PACK ACM INOPERATIVE AND REPLACED. SYSTEM OPERATION IS NORMAL.

Part: WIRE — BROKEN (CABIN) · airframe 78,552 hrs · 28,673 cycles

EMERGENCY LIGHT AT SEAT 39GF IS INOPERATIVE. MAINTENANCE FOUND BROKEN WIRE AND REPAIRED. SYSTEM OPERATION IS NORMAL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 78,382 hrs · 28,618 cycles

EMERGENCY LIGHTS AT ROW 27AB ARE INOPERATIVE. MAINTENANCE REPLACED THE LAMPS. SYSTEM OPERATION IS NORMAL.

Part: LIGHT — INOPERATIVE (R2 DOOR) · airframe 78,351 hrs · 28,609 cycles

R2 DOOR INDICATION ON FLIGHT ATTENDANT PANEL INOPERATIVE. RELAMPED SLIDE ARMED LIGHT. SYSTEM OPERATION IS NORMAL.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 73,080 hrs · 27,369 cycles

DURING SERVICE CHECK, FOUND EMERGENCY EXIT SIGN IN FIRST CLASS GALLEY INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK CHARGER, M735, AND BATTERY. SYSTEM OPERATION IS NORMAL.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 70,732 hrs · 26,813 cycles

RT AFT RED EMERGENCY EXIT LIGHT IS INOPERATIVE. MAINTENACE REPAIRED SPLICE AT FLOOR. SYSTEM CHECKS NORMAL.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 67,568 hrs · 26,063 cycles

FOUND THREE EMERGENCY LIGHTS AT C2 AND 4R DOOR WOULD NOT SHUTOFF. MAINTENANCE REPLACED LIGHT BATTERY POWER SUPPLY M733. SYSTEM OPS ARE NORMAL.

Part: FITTING — CRACKED (LT WING) · airframe 65,409 hrs · 25,541 cycles

CRACK INDICATION ON LT WING AFT PITCH LOAD FITTING OTBD TENSION BOLT HOLE COMMON TO THE WING LOWER SKIN JOB ACCOMPLISHED IAW PRI 5128354-14AD REV O AND ER/A 512834-14AD REV ORIGINAL.

Part: FRAME — CORRODED (BS 368 S19-20R) · airframe 65,409 hrs · 25,541 cycles

FRAME BS 368 BETWEEN S19 & 20R CORRODED. FRAME REPAIRED IAW ERA 512836-14, REV ORIGINAL.

Part: STRINGER — CORRODED (BS 1300 S35L) · airframe 65,409 hrs · 25,541 cycles

AFT CARGO STRINGER AT BS 1300 S35L FOUND CORRODED. STRINGER REPAIRED IAW ERA 512829-14 REV ORIGINAL.

Part: FITTING — CRACKED (RT WING) · airframe 65,409 hrs · 25,541 cycles

OPEN HOLE HFEC INSPECTION FOUND CRACK AT AFT O/B FASTENER HOLE ON RT WING UPPER LINK PITCH LOAD FITTING. CRACK REPAIRED PER ERA 512832-14 REV ORIGINAL.

Part: SKIN — CORRODED (BS 1540-1562) · airframe 65,409 hrs · 25,541 cycles

FUSELAGE SKIN AT BS 1540-1562 S27-29L. REPAIRED IAW ERA 513442-14, REV ORIGINAL.

Part: ANGLE — CRACKED (RT WING) · airframe 65,409 hrs · 25,541 cycles

RT WING L/E CAVITY AT APRROX 685 FRONT SPAR LT ANGLE FOUND CRACKED. NEW ANGLE FABRICATED AND INSTALLED IAW ERA 513480-14, REV ORIGINAL.

Part: STRINGER — CORRODED (BS 1315 S39L) · airframe 65,409 hrs · 25,541 cycles

AFT CARGO BS 1315, S39L, STRINGER FOUND CRACKED THROUGH FROM CORROSION. STRINGER & STRINGER SPLICE REPAIRED IAW ERA.

Part: FRAME — CRACKED (BS 883.5) · airframe 65,409 hrs · 25,541 cycles

CRACK FOUND ON RT BS 883.5 FRAME INNER CHORD. REPAIR TO FRAME ACCOMPLISHED IAW WC 5311-01195-09-02B.

Part: FRAME — CRACKED (BS 903.5) · airframe 65,409 hrs · 25,541 cycles

CRACK FOUND ON RT SIDE BS 903.5 FRAME INNER CHORD. DURING HFEC INSPECTION. REPAIRED FRAME IAW CARD 5311-01195-09-03B.

Part: FRAME — CRACKED (BS 903.5) · airframe 65,409 hrs · 25,541 cycles

CRACK FOUND ON LT SIDE BS 903.5 FRAME INNER CHORD DURING HFEC INSPECTION. REPAIR TO FRAME CARRIED OUT IAW WC 5311-01195-09-03A.

Part: FRAME — CORRODED (BS 1562) · airframe 65,409 hrs · 25,541 cycles

FUSELAGE FRAME FOUND CORROSION AT STA 1562, S39L AREA. FRAME REPAIRED IAW ERA.

Part: FAILSAFE — CRACKED (BS 955) · airframe 65,409 hrs · 25,541 cycles

DURING HFEC FOUND CRACK AT BS 955 FAILSAFE STRAP. REPAIR CARRIED OUT IAW ERA 512806-14AD.

Part: FAILSAFE — CRACKED (BS 955) · airframe 65,409 hrs · 25,541 cycles

FOUND CRACK ON RT SIDE BS 955 FAIL SAFE STRAP DURING HFEC OPEN HOLE INSPECTION. REPAIRED IAW ERA 512807-14.

Part: LONGERON FITTING — CRACKED (BS 783) · airframe 65,409 hrs · 25,541 cycles

DURING HFEC INSPECTION FOUND CRACK AT RT BS 783 LONGERON FITTING. RT LONGERON FITTING REPLACED AND ACCOMPLISHED EAJIC WC EA 01-499898-03, ME04, OPN 0401.

Part: SEAT TRACK — CORRODED (BS 347) · airframe 65,409 hrs · 25,541 cycles

CABIN SEAT TRACK AT FS 347, RBL 55 - CORRODED. REPLACED SEAT TRACK IAW SRM 51-40-02, REV 91-02. (REJECTED DOES NOT MEET SDR REQUIRMENTS) NRC 220-058

Part: FRAME — CORRODED (BS 1131) · airframe 65,409 hrs · 25,541 cycles

CABIN FRAME BS 1131, BL 0 FOUND CORRODED. FRAME REPAIRED IAW SRM 53-00-07, FIG 201, REPAIR 1, REV 91.02.

Part: FRAME — CORRODED (BS 412 S15-16R) · airframe 65,409 hrs · 25,541 cycles

BS 412 FRAME BETWEEN S15 & 16R FOUND CORRODED OUT OF LIMITS. REPAIRED IAW SRM 53-00-07, FIG 201 REPAIR 1 REV 91-02.

Part: FLOORBEAM — CORRODED (BS 347) · airframe 65,409 hrs · 25,541 cycles

CABIN FLOORBEAM AT FS 347, RBL 41-52 FOUND CORRODED. FLOORBEAM UPPER CHORD REPAIRED IAW SRM 53-00-51, FIGURE 201, REPAIR 1. REV 91-02.

Part: LIGHT — MISSING (CABIN) · airframe 64,671 hrs · 25,345 cycles

LEFT AFT WALL MOUNTED RED EMERGENCY LIGHT MISSING. MX REPLACED LIGHT ASSEMBLY.

Part: SPAR — CRACKED (NR 2 PYLON) · airframe 64,247 hrs · 25,234 cycles

DURING PSV DISCOVERED NR 2 PYLON FWD UPPER SPAR WEB CRACKED AT OTBD DRAIN HOLE. C/W TIME LIMITED REPAIR IAW ERA 508041-14, REV 0. ACCOMPLISH REPETITIVE INSPECTION AT 50,000 FLT CYCLES AND THEREAFTER AT 12,000 FLT CYCLES.__(ERA 508041-14R0)

Part: FITTING — DAMAGED (RT WING) · airframe 62,388 hrs · 24,808 cycles

DURING LONGERON FITTING REPLACEMENT FOUND SEVERAL FASTENERS HAVING SEM IF DRILLED FROM EXISTING HOLES ON ACFT. SEM CONDITION FOUND ACCEPTABLE IAW ERA 513468-14 AD, REV ORIGINAL.

Part: FITTING — CRACKED (LT WING) · airframe 62,388 hrs · 24,808 cycles

LEFT WING PITCH LOAD FITTING, ONE FASTENER HOLE FOUND CRACKED. FITTING CRACKED HOLE REPAIRED IAW ERA 512832-14, REV ORIGINAL.

Part: WIRE — DAMAGED (CABIN) · airframe 61,790 hrs · 24,674 cycles

RED EMERGENCY ESCAPE PATH LIGHTS NEAR L2 DOOR ARE INOPERTIVE. MAINTENANCE REPAIRED WIRE AND SECURED LIGHT. SYSTEM OPS NML.

Part: STRUCTURE — CORRODED (NLG WW) · airframe 58,438 hrs · 23,937 cycles

CHORD IN NOSE WHEEL WELL IN AFT CORNER BEHIND NOSE STEERING CHECK VALVE CORROSION C/W IAW ERA 491891-14 ORG.

Part: CIRCUIT BREAKER — TRIPPED (COCKPIT) · airframe 51,617 hrs · 22,413 cycles

LEFT FWD FUEL PUMP LOW PRESS LIGHT ILLUM. RESET GND SERVICE BUS C/B B7 ON P33 PANEL. PUMP OPS NORMAL.

Part: COFFEEMAKER — ODOR (AFT GALLEY) · airframe 50,480 hrs · 22,179 cycles

F/A`S REPORTED AN ELECTRICAL ODOR IN AFT GALLEY. ODOR DISSIPATED WHEN CHILLER AND BUN WARMER WERE TURNED OFF. FOUND AFT GALLEY NR 4 COFFEE MAKER HOT PLATE COIL BAD, FWD TO NEF 253.08. C/B PULLED SECURED.

Part: SWITCH — SHORTED (RADIO) · airframe 50,336 hrs · 22,144 cycles

CO-PILOT YOLK RADIO SWITCH INOP. REPLACED F/O YOKE PTT SWITCH. SWITCH OPS CKS NORMAL.

Part: TIRE — FOD (LT NLG WHEEL) · airframe 50,119 hrs · 22,088 cycles

ON PUSHBACK RAMP NOTICED A BOLT IN THE LT NOSE TIRE. REPLACED LT NOSE WHEEL ASSY PER AMM. SPACER INSTALLED AND PRESS CKD.

Part: TEE FITTING — CRACKED (NR 2 PYLON) · airframe 48,179 hrs · 21,572 cycles

THE CLOSEOUT TEE AT THE MIDSPAR FITTING ON THE NR 2 PYLON WAS FOUND CRACKED. AN ER/A WAS ISSUED TO REPLACE THE CLOSEOUT TEE AND COMPLETE AD MANDATED INSPECTIONS.

Part: DOOR — MISSING (NR 2 NACELLE) · airframe 47,836 hrs · 21,484 cycles

FOUND NR 2 ENG INBD AFT NACELLE STRUT ACCESS DOOR MISSING. FORWARD TO MCO PER CDL 54-53-02.

Part: CONTROLLER — FAILED (TEMP) · airframe 45,266 hrs · 20,816 cycles

ON TAXI OUT FLT DECK TEMP, AFT CABIN TEMP, MID CABIN TEMP, FWD CABIN TEMP CAUTION MSG ILLUMINATED. REPLACED ZONE TEMP CONTROLLER PER M/M. OPS CHK NORMAL. ACFT RTB.

Part: LINK — UNKNOWN (T/E FLAP) · airframe 45,077 hrs · 20,771 cycles

T/E FLAP 3-10 LINKS REPAIRED IAW EA 01-076248-12, ME07, ME08, ME09, ME10, ME11, ME12.

Part: LINE — FAILED (HYD SYSTEM) · airframe 44,467 hrs · 20,623 cycles

DURING PUSHBACK RIGHT HYD SYS WENT TO ZERO RETURNED TO GATE FOR REPAIRS. REPLACED ACMP HYD PRESSURE LINE.

Part: DOOR — MISSING (NR 2 PYLON) · airframe 43,461 hrs · 20,363 cycles

FOUND BY MTC ON PDC WALK AROUND FOUND NUMBER 2 ENGINE PYLON INBOARD NACELLE STRUT ACCESS DOOR MISSING FWD TO CDL PER 54-53-03 NEEDS DOOR MFG 311T3065-127. REPLACED ACCESS DOOR, MCO/PLACARD REMOVED.

Part: TURBINE WHEEL — DAMAGED (NR 1 ENGINE) · airframe 43,324 hrs · 20,331 cycles

SECOND STAGE HPT DAMAGE FOUND DURING DURING BORO OP 5067. REPLACED NR 1 ENG PER RC DECK XMITTER 76X1T148, RAN ENG PER DECK, OPS AND LEAK CHECKS OK.

Part: SHUTOFF VALVE — INOPERATIVE (LT ENGINE) · airframe 42,845 hrs · 20,222 cycles

LEFT ENG BLEED VALVE WOULD NOT OPEN. REPLACED LEFT PRSOV IAW AMM. LEFT ENG PRSOV OPS CKS GOOD.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 41,994 hrs · 19,991 cycles

DURING HMV, FOUND STA 287 FLOORBEAM CORRODED 18 INCHES FROM BL 0 RT. CAUSE OF CORROSION WAS ENVIRONMENTAL. DAMAGE WAS REPAIRED PER SRM 53-00-51D. CORROSION WAS FOUND DURING HMV ROUTINE INSPECTION.

Part: HEAT SHIELD — UNKNOWN (PYLON) · airframe 41,994 hrs · 19,991 cycles

LT AND RT PYLON INBD STRUT FAIRING MID AND AFT PANEL HEAT SHIELD REPAIRED IAW EA 01-097116-03, ME01, ME02.

Part: BARREL NUT — MISSING (VERTICAL STAB) · airframe 41,994 hrs · 19,991 cycles

JOINT BARREL NUT /BOLT ASSY OF VERTICAL FIN MISSING, REPLACED IAW EA 01-074297-12, ME05.

Part: APU — MALFUNCTIONED (APU BAY) · airframe 39,831 hrs · 19,189 cycles

APU SHUTDOWN IMMEDIATLY WHEN PACKS WERE TURNED OFF PRIOR TO ENG START. APU DID NOT RESTART UNTIL 3RD ATTEMPT. APU OPS NORMAL AFTER RESTART ELEC AND AIR OKAY NO HISTORY.

Part: PIN — MISSING (OVERWING SLIDE) · airframe 39,081 hrs · 18,879 cycles

WHILE WORKING EO 01-453956-03 ME 01 DISCOVERED LT OVERWING SLIDE DOOR ACTUATOR ROD DISCONNECTED AT FWD UPPER LATCH. REINSTALLED SAME.

Part: COUPLING — CRACKED (RT ENGINE) · airframe 36,799 hrs · 17,952 cycles

FUEL LEAK COMING FROM RT ENGINE AREA. FOUND RT ENGINE FUEL FEED TUBE COUPLING BROKEN. REPLACED SAME.

Part: ENGINE — FAILED (NR 2) · airframe 35,561 hrs · 17,407 cycles

INFLIGHT SHUTDOWN OF RIGHT ENGINE. CLIMBING THROUGH FL 260 WITH ALL ENG INDICATIONS NORMAL AND POWER AT CLIMB SETTING, ACFT SHUDDERED VIOLENTLY WITH LOUD BANG. RIGHT ENG HAD FAILED. ACCOMPLISHED ENGINE FAILURE CHECKLIST AND RETURNED TO TPA. PASSENGER REPORTED FLAMES COMING FROM RIGHT ENG. ENGINE INDICATIONS AT TIME OF FAILURE SHOWED NO N1, N2 OR EPR INDICATIONS. FUEL FLOW WAS ZERO AND ENG WAS COMPLETELY INOP AT TIME THAT CHECKLIST WAS ACCOMPLISHED. REPLACED ENGINE.

Part: SWITCH — BURNED (COCKPIT) · airframe 33,009 hrs · 16,079 cycles

CREW REPORTED SMOKE FROM THE GEAR HANDLE AREA AND GPS FAIL. PULLED GPWS C/BS AND SMOKE WENT AWAY. FOUND GPWS TERRAIN OVERRIDE SWITCH BAD. REPLACED SAME.

Part: COMPRESSOR — STALLED (NR 1 ENGINE) · airframe 32,254 hrs · 15,707 cycles

ON T/O NR 1 ENG COMPRESSOR STALLED AT 500 FT AGL, COMPLETED CHECKLIST PER QRH RETURNED FOR LANDING RSW. MAX EGT 850C FOR APPROX 1 MIN 30 SECS. ENG SHUTDOWN BY CREW. REPLACED NR 1 ENG PER TRANS 1T148.

Part: EEC — DEFECTIVE (NR 2 ENGINE) · airframe 31,612 hrs · 15,390 cycles

ON DESCENT INTO FLL RT ENGINE SURGED. EGT WENT INTO YELLOW. BOROSCOPE PER FIM 71005-00 ALL OK. EEC AND PT2 PROBE REPLCD C/W ALL INSP PER FIM 71-05-00. ENGINE RUN PER PFHB 6-7-4-14 AND T/O PWR CHECK ALL OK.

Part: FAN — INOPERATIVE (CABIN) · airframe 31,347 hrs · 15,248 cycles

AT CRUISE, SUDDEN ODOR IN COCKPIT THAT SMELLS LIKE FAULTY LIGHT BALLAST AND SEEMS TO BE STRONGEST NEAR/UNDER GLARESHIELD. TURNED OFF ALL LIGHTS. MAINTENANCE NEEDS TO CHECK ODOR IN CARGO AND E/E. OPERATED BALLAST FOR ALL COCKPIT LIGHTING PER FLIGHT CREW ODOR CAME FIRST FOLLOWED BY FWD EXHAUST FAN STATUS. C/B PULLED & COLLARED FWD TO MCO & PLACARD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 30,362 hrs · 14,740 cycles

EMERGENCY LIGHTS AT SEATS 1AB THRU 12AB AND 13FG THRU 21FG WILL NOT ILLUMINATE. REPLACED BATTERY PACK M9008, LIGHTS CHECK GOOD.

Part: SMOKE DETECTOR — ACTIVATED (CABIN) · airframe 25,262 hrs · 12,230 cycles

3R, 2R, 2L SMOKE DETECTORS WENT OFF IN FLIGHT, NO SIGN OF SMOKE, LIGHT SMELL (FLIGHT ATTENDANTS DESCRIBED AS SLIGHT ELECTRICAL SMELL). RAN ALL GALLEY EQPT, TURNED ON ALL CABIN LIGHTS, RAN PACKS WITH ENG AIR DOORS CLOSED AND NO SMOKE OR ELECTRICAL SMELL IN ANY AREA. CLEANED CABIN TEMP SENSOR FILTERS, LAV VENT FILTER AND RAN ENGS TO HIGH POWER PER PFHB WITH PACKS ON. UNABLE TO DUPLICATE. REPLACED SMOKE DETECTOR.

Part: SKIN — PUNCTURED (FS 654-720)

THE FUSELAGE SKIN WAS TORN AND GOUGED BY GROUND EQUIPMENT BETWEEN FS 654 + 44 AND FS 654 + 66 AND BETWEEN STRINGERS 34R AND 35R. THE DAMAGED SKIN WAS REMOVED WITH A 10 X 20 CUTOUT. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 367677-14.

Part: SELECTOR — MALFUNCTIONED (LANDING GEAR)

DURING GEAR EXT HAD 3 GREEN DOWNLOCK LIGHTS WITH GEAR DISAGREE AND TAIL SKID LIGHTS. EXECUTED MISSED APPROACH REVIEWED POM PROCEDURES. ON SECOND APPROACH SHORT FINAL INDICATIONS RETURNED TO NORMAL. NORMAL LANDING AND ROLLOUT. REPLACED THE LANDING GEAR SELECTOR HANDLE ASSY PER M/M, ALL INDICATIONS CHECK GOOD.

Part: SKIN — CORROSION (BS 686)

CORROSION WAS FOUND ON THE FUSELAGE SKIN UNDER THE LT FORWRD AIRFONE ANTENNA AT STA 686 FROM STR 35L TO 36L. THE DAMAGE RESULTED IN A CUTOUT MEASURING 6.75 BY 2.75. A DOUBLER WAS INSTALLED AND APPROVED PER FAA/DER FORM 8110-3, DER DESIGNATION SO-775, DTD 7-25-97.

Part: ENGINE — FAILED (NR 1)

ON TAKEOFF PASSING 400 FT, AGL LEFT ENG COMPRESSOR STALLED. THROTTLE REDUCED TO IDLE AND RETURN FOR LANDING, MAX EGT 697 DEGREE. FOUND ENG AT FAULT. REPLACED NR 1 ENGINE.

Part: BATTERY PACK — DISCHARGED (CABIN)

FOUND FLOOR TRACK LIGHTS INOPERATIVE. BOTH LT AND RT SIDES FROM ROW 34 AFT. REPLACED BATTERY PACK 9010. SYSTEM OPERATION NORMAL.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

ON PREFLIGHT, F0UND 2 EMERGENCY TRACK LIGHT STRIPS INOP. MTC FOUND L9028, L9021, L9007, L9010, L9008, L9011, L9022 AND L9030 ALL INOP. REPLACED BATTERY POWER SUPPLY M9008, OPERATION NOW NORMAL.

Part: EEL ASSY — MISSING (CABIN)

EMERGENCY PATH LIGHTS MISSING SEATS 25B AND 25G. REPLACED MISSING LIGHT ASSY, OPN OK.

Part: COOLING FAN — FAILED (E/E BAY)

ON CLIMBOUT, HAD ELECTRICAL BURNING SMELL IN COCKPIT AND FWD EQUIPMENT COOLING FAN C/B TRIPPED, RETURNED JAX. REPLACED COOLING FAN, OPERATION NORMAL.

Part: COMPRESSOR — STALLED (NR 2 ENGINE)

ON CLIMBOUT AT 500, NR 2 ENGINE HAD COMPRESSOR STALL, AND EGT OVERTEMP TO 735 DEGREES. REDUCED ENGINE POWER AND RETURNED TO JFK. ENGINE WAS REPLACED AND ROUTED TO SHOP. ETOPS UNSCHEDULED ENGINE REMOVAL.

Part: COFFEE MAKER — FAILED (FWD GALLEY)

DURING CRUISE, FORWARD GALLEY COFFEE MAKER STARTED TO POP AND EMIT SMOKE AND ELECTRICAL BURNING ODOR. SHUTOFF POWER, ODOR QUICKLY STOPPED. FOUND BURNED WIRES ON NR 2 COFFEE MAKER. REPLACED UNIT, OPERATION NORMAL.