N198AA

Part: PITOT LINE — FOD (FIRST OFFICER'S) · airframe 56,934 hrs · 16,232 cycles

AIRCRAFT WAS GROUNDED: PILOT REPORTS AT 80 KNOT SPEED CHECK, FOS SPEED INDICATED 37 KNOT. REJECTED TAKEOFF ABOVE 85 AND BELOW 100 KNOTS, AUTOBRAKE ENGAGED. MAINTENANCE FOUND DEBRIS IN F/O PITOT LINE AND ACCOMPLISHED AMM 34-11-00, OPS CHECK NORMAL. REPLACED ADC IAW AMM 34-12-01 AS A PRECAUTION, OPS CHECK NORMAL.

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 55,395 hrs · 15,798 cycles

AIRCRAFT WAS NOT GROUNDED: SEAT MOUNTED EMERGENCY LIGHTS WERE DIM 26-36D. MAINTENANCE REPLACED BATTERY PER AMM 33-51-07 AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 54,854 hrs · 15,640 cycles

AIRCRAFT IN BASE MAINTENANCE: RIGHT WING SKIN OVER-WING FUEL FILL PORT ADAPTER LANDING UPPER AND LOWER SURFACES CORRODED. REPAIRED PER SRM 57-20-01-2R-7 AND EA 292502.

Part: SIGN — DAMAGED (CABIN) · airframe 54,710 hrs · 15,593 cycles

AIRCRAFT WAS NOT GROUNDED: R1 DOOR LOWER AFT EXIT SIGN WAS DAMAGED. MAINTENANCE REPLACED SIGN PER AMM 33-51-01.

Part: FAN — DEFECTIVE (ZONE 100) · airframe 53,547 hrs · 15,273 cycles

JFK FLT 279 EN-ROUTE EDI - JFK. THE AIRCRAFT WAS GROUNDED SMOKE/FUMES/ODOR IN CABIN AIRCRAFT /L/ SIDE AFT VENT ONLY. FUMES DISSIPATED WITH LEFT RECIRC FAN SELECTED OFF PER STEP 9 OF THE QRH CHECKLIST (SMOKE, FIRE OR FUMES). RESEMBLED AN ACRID SMELL. (AFT GALLEY). MAINTENANCE ACCOMPLISHED ATBT SIC 05-96-70 SMOKE ODOR. REPLACED RECIRCULATION FAN BASED ON PILOT DEBRIEF AND PIREP. PUT AIRCRAFT IN THE AIR MODE FOR CHECK OF DOOR SUPPLEMENTAL HEATERS , OPERATION NORMAL. (REF AMM 21-45-00, 21-25-01, 25-32-00).

Part: COOLING FAN — DEFECTIVE (NR 1) · airframe 53,153 hrs · 15,178 cycles

SMOKE ODOR REPORTED IN THE CABIN. AFTER TROUBLESHOOTING, NO EMERGENCY WAS DECLARED. FLIGHT DIVERTED AND LANDED WITHOUT FURTHER INCIDENT. THE AIRCRAFT WAS GROUNDED. MAINTENANCE TROUBLESHOT SYSTEM AND FOUND FWD EQUIPMENT SUPPLY FAN NR 1 TO BE THE SOURCE OF THE ODOR. REMOVED AND REPLACED THE FWD EQ FAN IAW AMM 21-58-06, OPS CHECK ACCOMPLISHED IAW 5-96-70, OK FOR SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 52,527 hrs · 15,018 cycles

THE AIRCRAFT WAS NOT GROUNDED. SEAT MOUNTED EMERGENCY LIGHTS FROM SEAT 29D TO 36D ARE DIM. REPLACED BATTERY FOR AFT CABIN EMERGENCY LIGHTS PER AMM 33-51-07. OPERATIONS CHECK NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 52,520 hrs · 15,016 cycles

AIRCRAFT WAS NOT GROUNDED: SEAT MOUNTED EMERGENCY LIGHTS FROM SEAT 29D TO 36D WERE DIM. MAINTENANCE REPLACED BATTERY FOR AFT CABIN EMERGENCY LIGHT PER AMM 33-51-07. SEAT MOUNTED EMERGENCY LIGHTS 29D TO 36D AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 52,322 hrs · 14,959 cycles

EXIT LIGHT COVER IS MISSING AT THE R4 IN FRONT OF TRASH CONTAINER. REPLACED THE LIGHT ASSY IAW AMM 33-51-10.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 52,322 hrs · 14,959 cycles

L4 EXIT LIGHT COVER MISSING. REPLACED LIGHT IAW AMM 33-51-10.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 52,322 hrs · 14,959 cycles

L4 EXIT LIGHT COVER MISSING. REPLACED LIGHT IAW AMM 33-51-10.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 52,317 hrs · 14,957 cycles

SEAT 1E MISSING THE EMERGENCY LIGHT LENS ON THE ARM REST. REPLACED THE LENS. THE AIRCRAFT WAS GROUNDED.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 52,317 hrs · 14,957 cycles

SEAT 3E MISSING EMERGENCY AISLE LIGHT LENS AFT OF SEAT ARM REST. THE AIRCRAFT WAS GROUNDED. MAINTENANCE REPLACED MISSING LENS IAW AMM 33-51-11, AND PERFORMED A SATISFACTORY OPS CHECK.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 52,317 hrs · 14,957 cycles

SEAT 2E AISLE EMERGENCY LIGHT LENS MISSING AFT OF SEAT ARM REST. THE AIRCRAFT WAS GROUNDED. MAINTENANCE REPLACED THE LENS IAW AMM 33-51-11, AND PERFORMED A SATISFACTORY OPS CHECK.

Part: HANDLE — OUT OF ADJUST (L1 DOOR) · airframe 51,481 hrs · 14,728 cycles

L1 DOOR SLIDE ARMING INDICATOR DOES NOT POP OUT WHEN DOOR IS ARMED. ADJUSTED THE DOOR HANDLE IAW AMM 52-11-13. CHECKED OK.

Part: BATTERY — DISCHARGED (CABIN) · airframe 50,258 hrs · 14,417 cycles

AIRCRAFT WAS NOT GROUNDED. SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT AT SEAT 4E IS DIM. RECHARGED BATTERIES IAW AMM 33-51-07. OPERATIONAL CHECK GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 50,250 hrs · 14,415 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY ESCAPE PATH LIGHTS AT ROWS 26D THROUGH 32D ARE DIM. RECHARGED BATTERIES IAW AMM 33-51-07. OPERATIONAL CHECK GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 50,250 hrs · 14,415 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY ESCAPE PATH LIGHT AT SEAT 18D IS DIM. RECHARGED BATTERIES IAW AMM 33-51-07. OPERATIONAL CHECK GOOD.

Part: COVER — DETACHED (GIRT BAR) · airframe 50,136 hrs · 14,378 cycles

L4 DOOR GIRT BAR FLOOR ATTACHMENT COVER IS DETACHED. REINSTALLED THE COVER. OPERATIONAL CHECKED GOOD.

Part: LENS — MISSING (CABIN) · airframe 49,631 hrs · 14,044 cycles

AIRCRAFT WAS NOT GROUNDED. SIDEWALL EMERGENCY EXIT LIGHT LEFT FORWARD OVERWING HAS A MISSING LENS COVER. INSTALLED LENS COVER IAW AMM 33-51-11. OPERATIONAL CHECK GOOD.

Part: PANEL — UNSECURE (RAFT DOOR) · airframe 49,538 hrs · 14,207 cycles

FLIGHT ATTENDANT REPORTED THE LIFE RAFT DOOR PANEL IN MAIN CABIN CEILING IS NOT SECURE. SECURED THE PANEL ASSEMBLY. OPERATIONAL CHECKED GOOD.

Part: LENS — DETACHED (CABIN) · airframe 49,526 hrs · 14,204 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY ESCAPE PATH LIGHT AT BOTTOM OF SEAT 4E HAS A DETACHED LENS COVER. REPLACED LENS COVER IAW AMM 33-51-11. OPERATIONAL CHECK GOOD.

Part: SEAT — DAMAGED (CABIN) · airframe 49,159 hrs · 14,101 cycles

AIRCRAFT WAS NOT GROUNDED. R4 DOOR IS DIFFICULT TO OPEN DUE TO CONTACT WITH THE JUMPSEAT TRIM. REMOVED AND REPLACED FLIGHT ATTENDANT SEAT AT R4 DOOR. OPERATIONAL CHECK GOOD.

Part: BOTTLE — LOW PRESSURE (R2 DOOR) · airframe 48,402 hrs · 13,909 cycles

R2 DOOR SLIDE INFLATION RESERVOIR PRESSURE LOW. REMOVED AND REPLACED SLIDE IAW 25-94-34. OPERATIONAL CHECK GOOD.

Part: BOTTLE — LOW PRESSURE (L4 DOOR) · airframe 48,402 hrs · 13,909 cycles

L4 DOOR SLIDE INFLATION RESERVOIR PRESSURE LOW. REMOVED AND REPLACED SLIDE IAW 25-94-34. OPERATIONAL CHECK GOOD.

Part: BOTTLE — LOW PRESSURE (R4 DOOR) · airframe 48,402 hrs · 13,909 cycles

R4 DOOR SLIDE INFLATION RESERVOIR PRESSURE LOW. REMOVED AND REPLACED SLIDE IAW 25-94-34. OPERATIONAL CHECKED GOOD.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 46,476 hrs · 13,453 cycles

AIRCRAFT WAS IN BASE MX. TOP SURFACE OF AFT DECK WEB IS CORRODED, BETWEEN RBL 15 & RBL 29, FROM FS 1716 - 1720. REPAIRED WEB IAW SRM 53-60-51-2R-17.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 46,476 hrs · 13,453 cycles

AIRCRAFT WAS IN BASE MX. AFT DECK WEB IS CORRODED BETWEEN FS 1715 & 1720 AT LBL 45. REPAIRED WEB IAW AARD 53-60-51-3-3.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 46,476 hrs · 13,453 cycles

AIRCRAFT WAS IN BASE MX. MAIN CABIN AFT DECK WEB IS CORRODED AT FS 1715 & LBL 45. REPAIRED DECK IAW AARD 53-60-51-3 REPAIR 3.

Part: CONNECTOR — FAULTY (ZONE 400) · airframe 44,857 hrs · 13,081 cycles

AIR INTERRUPT, EMER DECLARED, LANDING UNEVENTFUL & ACFT OVERWEIGHT. DURING CRUISE, RECEIVED LT GEN & BUS OFFLINE INDICATION. R & R CONNECTOR PLUG D014J AT PYLON FIREWALL CONNECTORS IAW 20-23-01 & 20-63-02. ACCOMPLISHED IDG ADJUSTMENT & TEST IAW 24-11-00. OPERATIONAL CHECKED GOOD. SEE ALSO AALA20150930007.

Part: CONNECTOR — FAULTY (ELECTRICAL SYS) · airframe 44,857 hrs · 13,081 cycles

AIR INTERRUPT, EMER DECLARED, LANDING UNEVENTFUL & ACFT OVERWEIGHT. DURING CRUISE, RECEIVED LT GEN & BUS OFFLINE INDICATION. R & R CONNECTOR PLUGS D114P AT PYLON FIREWALL CONNECTORS IAW 20-23-01 & 20-63-02. ACCOMPLISHED IDG ADJUSTMENT & TEST IAW 24-11-00. OPERATIONAL CHECKED GOOD. SEE ALSO AALA2015100500.

Part: MODULE — FAILED (CABIN) · airframe 43,504 hrs · 12,790 cycles

AIRCRAFT AIR INTERRUPTED WITH SMOKE CONDITION IN FIRST CLASS CABIN. REPLACED SEAT MODULE ASSEMBLY UNIT 2A & B IAW CMM 25-25-423 WITH GOOD OPERATIONAL CHECKS.

Part: CONTROL UNIT — DEFECTIVE (ZONE 400) · airframe 42,086 hrs · 12,433 cycles

RETURNED & EMER DECLARED. LANDING UNEVENTFUL, ACFT NOT OVERWEIGHT. DURING CLIMB LT ENG EXHAUST GAS TEMPS INDICATED HIGH. PERFORMED BITE CHECK OF BVCU WHICH RETURNED FAULT CODE 7. R & R DEDICATED GEN IAW AMM 73-21-08 & DEDICATED GEN CONTROL UNIT B IAW AMM 73-21-10. PERFORMED ENG RUN. SYS CHECKED NORMAL.

Part: HYDRAULIC SYSTEM — LOW (ZONE 100) · airframe 41,976 hrs · 12,412 cycles

DIVERTED, EMER DECLARED. LANDING WAS UNEVENTFUL. ACFT WAS OVERWEIGHT. IN CRUISE RT HYD SYS SHOWED QTY LOSS. EVALUATION IN PROGRESS. FIELD TRIP ENROUTE. PLAN TO TROUBLESHOOT & PERFORM OVERWEIGHT LANDING INSPECTION. SERVICED RT HYD SYS IAW AMM 12-12-01. ACCOMPLISHED FIM 29-11-00-815-824. NO LEAKS NOTED NO FLUID TRANSFER AT THIS TIME. SYS CHECKED NORMAL.

Part: DOUBLER — DAMAGED (FUSELAGE) · airframe 41,354 hrs · 12,264 cycles

ACCOMPLISH PERMANENT REPAIR TO EXISTING DOUBLER. INSTALLED PERMANENT REPAIR DOUBLER IAW EA B757-53-036160.

Part: PANEL — GOUGED (TE FLAP) · airframe 41,354 hrs · 12,264 cycles

LEFT MAIN FLAP GOUGE IN THE LE PANEL. INSTALLED DOUBLER IAW SRM 57-53-01-2R-2 & EA B757-57-036154.

Part: MODULE — FAULTY (ANTI-SKID SYS) · airframe 41,249 hrs · 12,224 cycles

UNWANTED HYD FLUID TRANSFER FROM RT TO LT SYS. EMER DECLARED FLIGHT DIVERTED & LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. REPLACED LT & RT ANTI-SKID SHUTTLE VLV MODULES. SYS GND CHECKED NORMAL OPERATION CLOSED.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,599 hrs · 11,133 cycles

AFT CARGO COMPARTMENT, FLOOR NET ANCHOR SUPPORT LOWER SURFACE CORRODED FROM BODY STATIONS 1468 TO 1472, STRINGERS 29 TO 28 RIGHT. INSTALLED NEW CHORD AND 2 EACH CHANNELS PER SRM 51-40-02 AND DRAWING 146N5390.

Part: FRAME — DENTED (FUSELAGE) · airframe 36,599 hrs · 11,133 cycles

FRAME DENTED AT FRAME STATION 1460 LEFT SIDEWALL LEFT BUTTLINE 30. INSTALLED NESTED ANGLE REPAIR PER SRM 53-00-07-2R-5 FIG 201 DETAIL III.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 36,599 hrs · 11,133 cycles

MAIN CABIN LEFT CUSP ANGLE AT STATION 324 CRACKED. REMOVED DAMAGED AREA AND INSTALLED NESTED ANGLE REPAIR PER SRM 51-70-12-OG AND SRM 51-40-02.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 36,599 hrs · 11,133 cycles

FORWARD CARGO HAS DAMAGE ON CUTOUT EDGE JUST FORWARD OF CARGO DOOR. INSTALLED 3 EACH FASTENER PER SRM 51-40-02 AND EA B757-53-028788.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 35,971 hrs · 10,981 cycles

SEAT 36D EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED LAMP FOR SEAT 36D EMERGENCY EXIT LIGHT. OPS CHECK NORMAL.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 32,850 hrs · 10,302 cycles

LIGHTNING STRIKE FROM STATIONS 550 TO 600 AND STRINGER 3 TO 4 RIGHT. INSTALLED DOUBLER PER SRM 53-00-01 AND EA B757-53-021656.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 32,850 hrs · 10,302 cycles

LIGHTNING STRIKE FROM STATIONS 390 TO 417 AND STRINGERS 3 TO 5 RIGHT. INSTALLED DOUBLER PER SRM 53-00-01-2R AND EA B757-53-021708.

Part: WIRE HARNESS — INOPERATIVE (LT IDG) · airframe 32,406 hrs · 10,198 cycles

JFK - INFLIGHT BOS-MIA. CREW REPORTED LEFT AC BUSS FAILED. EMERGENCY DECLARED FLIGHT DIVERTED JFK LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT INTEGRATED DRIVE GENERATOR HARNESS CABLE. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,129 hrs · 10,137 cycles

LEFT NUMBER 2 DOOR EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR LEFT NUMBER 2 DOOR EMERGENCY LIGHT. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,129 hrs · 10,137 cycles

RIGHT NUMBER 2 DOOR EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR RIGHT NUMBER 2 DOOR EMERGENCY LIGHT. OPS CHECK NORMAL.

Part: TACH GENERATOR — FAULTY (LT ENGINE) · airframe 26,876 hrs · 9,105 cycles

JFK - CREW REPORTED LEFT ENGINE BLEED SURGE AND LEFT CENTER FUEL PUMP FAILED WITH RIGHT FORWARD FUEL PUMP ON PLACARD. FLIGHT RETURNED JFK LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED N3 TACHOMETER GENERATOR ON LEFT ENGINE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: INDICATOR — FAULTY (COCKPIT) · airframe 25,452 hrs · 8,733 cycles

FLAP INDICATOR DISPLAYED A SPLIT WHEN FLAPS SELECTED TO 15, 25 AND 30 DEGREES. CREW REPORTED THAT AFTER 5 TO 10 MINUTES INDICATORS WOULD AGREE. AN ALERT 8 WAS DECLARED. NO EICAS MESSAGE OR ANNUNCIATOR LIGHTS ILLUMINATED AT ANY TIME. FOUND FLAP INDICATOR FAULTY. REPLACED INDICATOR. ALL CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,029 hrs

BOS - ESCAPE PATH LIGHTING AT SEAT MOUNTED ROW 15 TO 26 AND FOUR EACH LOWER OVERWING EXIT SIGN LIGHTS INOPERATIVE. REPLACED LIGHT ASSEMBLY AT RIGHT FORWARD WING EMERGENCY DOOR.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 24,225 hrs · 8,339 cycles

CARGO FLOOR WEB CORRODED. REPAIRED IAW SRM 5-20-01-06.

Part: FLOOR PANEL — CORRODED (CARGO BAY) · corrosion level 2 · airframe 24,225 hrs · 8,339 cycles

CARGO FLOOR PANEL WEB CORRODED. REPAIRED IAW SRM.

Part: TRANS PANEL — CORRODED (CARGO BAY) · corrosion level 2 · airframe 24,225 hrs · 8,339 cycles

TRANSITION PANEL CORRODED AT AFT CARGO DOOR SILL. REPAIRED IAW SRM.

Part: LAMP — LOOSE (EMERGENCY LIGHT)

DFW - EXTERIOR EMERGENCY LIGHT AT RIGHT NUMBER ONE SLIDE INOPERATIVE. RESEATED LAMP. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT)

DFW - AFT CARGO DOOR MOUNTED EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR AFT CARGO DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: PLATE — MISSING (EMERGENCY LIGHT)

DFW - SEAT MOUNTED EMERGENCY LIGHT AT SEAT 31D MISSING FASTENER AND LENS. REPLACED FASTENER NUT PLATE AND LENS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: WIRE HARNESS — DAMAGED (EMERGENCY LIGHTS)

DFW - SEAT MOUNTED EMERGENCY LIGHT AT SEAT 16D INOPERATIVE. REPLACED SEAT HARNESS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

DFW - EMERGENCY LIGHTS AT RT OVERWING EXIT MARKER INOPERATIVE. REPLACED BATTERY PACK AT M10568 FOR EMERGENCY LIGHTS AT RT OVERWING EXIT MARKER. SYSTEM GROUND CHECKED NORMAL OPERATION. (A)

Part: LIGHT — DAMAGED (CABIN)

DFW - EMERGENCY LIGHT AT SEAT 31D DAMAGED. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT 31D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS)

DFW - EXTERIOR EMERGENCY LIGHT AT LEFT NR 1 DOOR INOPERATIVE. REPLACED LAMP FOR EXTERIOR EMERGENCY LIGHT AT LEFT NUMBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS)

DFW - EXTERIOR EMERGENCY LIGHT AT RIGHT NUMBER TWO DOOR INOPERATIVE. REPLACED LAMP FOR EXTERIOR EMERGENCY LIGHT AT RIGHT NUMBER TWO DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 19,400 hrs

JFK - EMERGENCY EXIT SIGN AT RIGHT NUMBER ONE DOOR INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY EXIT SIGN AT RIGHT NUMBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

ORD - EMERGENCY LIGHTS AT SEAT ROWS 16D TO 25D INOPERATIVE. REPLACED BATTERY PACK AT M10800 FOR EMERGENCY LIGHTS AT SEAT ROWS 16D TO 25D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SOCKET — INOPERATIVE (EMERGENCY LIGHTS) · airframe 19,039 hrs

ORD - EMERGENCY LIGHTS AT SEAT ROW 16D INOPERATIVE. REPLACED SOCKET AT SEAT ROW 16 FOR EMERGENCY LIGHTS AT SEAT ROWS 16D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 19,013 hrs

MIA - EMERGENCY LIGHT AT SEAT 30C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 30C. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

DFW - SEAT MOUNTED EMERGENCY LIGHTS AT SEAT ROWS 9 TO 15 INOPERATIVE. REPLACED BATTERY PACK AT SEAT ROW 9 FOR SEAT MOUNTED EMERGENCY LIGHTS AT SEAT ROWS 9 TO 15. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

DFW - SEAT MOUNTED EMERGENCY LIGHTS AT SEAT ROWS 26 TO 36 INOPERATIVE. REPLACED BATTERY PACK FOR SEAT MOUNTED EMERGENCY LIGHTS AT SEAT ROWS 26 TO 36. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SHROUD — MISSING (CABIN)

DFW - EMERGENCY LIGHT AT SEAT 33D HAS MISSING SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 33D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LENS — MISSING (CABIN)

DFW - EMERGENCY LIGHT AT SEAT 33D MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 33D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

TPA - EMERGENCY LIGHTS AT SEAT ROWS 26 TO 36 AND EXIT SIGN IN AFT GALLEY INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT SEAT ROWS 26 TO 36 AND EXIT SIGN IN AFT GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

MIA - FOUND EMERGENCY LIGHT AT SEAT 24D INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 24D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SIGN — BROKEN (CABIN)

DFW - EMERGENCY LIGHTS AT LEFT FORWARD OVERWING MARKER BASE ASSEMBLY IS BROKEN. REPLACED THE CABIN LEFT FORWARD OVERWING EXIT MARKER LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: GOVERNOR — INOPERATIVE (FUEL FLOW)

ORD INFLIGHT T1105/11JAN - ON CLIMB-OUT THROUGH 33000 FEET NOTICED AIRCRAFT NOT CLIMBING. LEVELED AT 34000 FEET AND PUSHED LEFT THROTTLE TO STOP. DID NOT RESPOND. LEFT ENGINE WAS PRODUCING 20 TO 30 PERCENT LESS POWER. ON RETUREN TO ORD LEFT ENGINE SEEMED OKAY. USED 5 TO 6 UNITS OF TRIM. LEFT ENGINE WAS NOT PRODUCING CLIMB POWER. LANDED ORD WITHOUT INCIDENT. AIRCRACT TAKEN OUT OF SERVICE AND ENGINEERING REQUESTED FLIGHT DATA RECORDER DOWNLOAD. REPLACED LEFT HAND FUEL FLOW GOVERNOR PER MM CARD 73 94 010. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — LOOSE (CABIN)

RNO - EMERGENCY LIGHTS AT ROWS 26 TO 33 INOPERATIVE. FOUND LOOSE PLUG AT SEAT 29. SECURED PLUG AT SEAT 29 FOR EMERGENCY LIGHTS AT ROWS 26 TO 33. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (CABIN)

SEAT MOUNTED EMERGENCY EXIT LIGHTS IN FIRST CLASS INOPERATIVE. REPLACED BATTERY PACK FOR SEAT MOUNTED EMERGENCY EXIT LIGHTS IN FIRST CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION.