N510AM

Part: CHARGER — INOPERATIVE (E&E BAY) · airframe 66,577 hrs · 34,679 cycles

DFW - CREW REPORTED BATTERY CHARGER LIGHT ILLUMINATED AND CIRCUIT BREAKER POPPED IN FLIGHT. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITH INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED BATTERY CHARGER AND BOTH BATTERIES. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: PORTABLE LIGHT — INOPERATIVE (CABIN) · airframe 66,017 hrs · 34,358 cycles

LEFT NUMBER 1 DOOR PORTABLE EMERGENCY LIGHT (B5-29) INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR LEFT NUMBER 1 DOOR PORTABLE EMERGENCY LIGHT. OPS CHECK NORMAL.

Part: BATTERY — DISCHARGED (CABIN) · airframe 65,800 hrs · 34,236 cycles

SEAT MOUNTED ESCAPE PATH LIGHTING FROM ROWS 21D TO 32D INOPERATIVE. REPLACED POWER SUPPLY AND BATTERY AT AB5-4 AT AFT GALLEY. OPS CHECK NORMAL.

Part: SWITCH — INOPERATIVE (APU) · airframe 65,551 hrs · 34,092 cycles

PHX - CREW REPORTED TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMUNATED. ACCOMPLISHED QRH PROCEDURES. EMERGENCY DECLARED FLIGHT RETURNED PHX LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED BOTH TEMPERATURE SWITCHES AND SEALS ON AUXILIARY POWER UNIT COOLING DUCT. SYSTEM, GROUND CHECK NORMAL OPERATION.

Part: PERISEAL — LEAKING (AC BAY) · airframe 65,446 hrs · 34,035 cycles

LAS - CREW REPORTED TAIL COMPARTMENT OVERHEAT LIGHT ILLUMINATED. EMERGENCY DECLARED FLIGHT RETURNED LAS LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND PERI SEALS LEAKING AT LEFT CONNECTOR ON LEFT PRESSURIZATION DUCT FROM HEAT EXCHANGER AND PERI SEALS LEAKING AT RIGHT CONNECTOR ON RIGHT PRESSURIZATION DUCT FROM HEAT EXCHANGER. REPLACED LEFT AND RIGHT PERI SEALS. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 63,504 hrs · 32,962 cycles

LONGERON 2 RIGHT CRACKED AFT OF STATION 1418. INSTALLED NEW SECTION OF LONGERON PER SRM 53-02-00.

Part: A/C PACK — DIRTY (AC BAY) · airframe 62,241 hrs · 32,224 cycles

JAX - INFLIGHT RWS-DFW. FLIGHT ATTENDANTS REPORTED ODOR IN AFT CABIN. EMERGENCY DECLARED FLIGHT DIVERTED JAX LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND COALESCER BAGS EXTREMELY DIRTY. ACCOMPLISHED PACK BURN. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: SHROUD — MISSING (CABIN)

EMERGENCY LIGHT AT SEAT 25D MISSING LENS SHROUD. REPLACED LENS SHROUD ON SEAT 25D.

Part: MODULE — MALFUNCTIONED (CABIN) · airframe 58,054 hrs · 29,962 cycles

FAILED SECTION 7 WORK CARD 5403 - SEAT MOUNTED ESCAPE PATH LIGHTING - DUAL FEED CHECK. REPLACED FLOOR PATH LIGHTING CONTROL MODULE AND 4 BATTERY PACKS.

Part: PUMP — FAILED (RT ENGINE) · airframe 58,000 hrs · 29,935 cycles

DFW - CREW REPORTED RIGHT ENGINE DRIVEN HYDRAULIC PUMP FAILED. RETURNED TO DFW WITHOUT INCIDENT. FOUND RIGHT ENGINE DRIVEN HYDRAULIC PUMP SHAFT SHEARED. REMOVED AND REPLACED RIGHT ENGINE DRIVEN HYDRAULIC PUMP. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 57,721 hrs · 29,773 cycles

EMERGENCY LIGHTS FAILED TO OPERATE IN FORWARD CABIN AND MID CABIN. REPLACED BATTERY PACK FOR FORWARD AND MID CABIN EMERGENCY LIGHTS.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 57,721 hrs · 29,773 cycles

EMERGENCY LIGHTS IN FORWARD AND MID CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS IN FORWARD AND MID CABIN.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 57,721 hrs · 29,773 cycles

EMERGENCY LIGHTS IN FORWARD AND MID CABIN AREAS INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT FORWARD AND MID CABIN AREAS.

Part: FUSE — BLOWN (HYDRAULIC SYS) · airframe 57,104 hrs · 29,431 cycles

DFW - AIRCRAFT EXPERIENCED RIGHT HYDRAULIC QUANTITY LOSS AND LANDING GEAR DOORS DAMAGED DURING LANDING DUE TO NO PRESSURE TO RETRACT ON LANDING. AIRCRAFT REMOVED FROM SERVICE. FOUND TWO BRAKE FUSES BLOWN AT LEFT WING SPAR. REPLACED HYDRAULIC FUSE AND HYDRAULIC AUXILIARY PUMP. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 56,266 hrs

ATL- EMERGENCY PATH LIGHTING FROM ROW 3 THRU ROW 20 INOPERATIVE. REPLACED BATTERY PACK IN THE FORWARD AND MID CABIN POSITIONS.

Part: DIAPHRAGM — CORRODED (ZONE 100) · airframe 55,714 hrs · 28,679 cycles

CORROSION ON DIAPHRAGM UNDER G-1 GALLEY DRAIN PAN. INSTALLED DOUBLER REPAIR PER AARD 53-20-00-16.

Part: SPAR — CORRODED (ZONE 300) · airframe 55,714 hrs · 28,679 cycles

03 PLANK BOLTS SEALANT LOOSE AND EMITTING RUST AT CENTER SPAR BOX RIGHT TOP SIDE. REMOVED 05 BOLTS, FOUND CORROSION IN BORES. REAMED HOLES TO REMOVE CORROSION. TREATED AND PRIMED BORES. MANUFACTURED AND INSTALLED 05 BUSHINGS IN ACCORDANCE WITH ESO 80559 DATED 10-14-08.

Part: MOUNT — CORRODED (ZONE 100) · airframe 55,714 hrs · 28,679 cycles

CORROSION ON TOP OF INBOARD GALLEY TIE DOWN. REPLACED INBOARD GALLEY MOUNT PER SRM 51-01-00.

Part: DIAPHRAGM — CORRODED (ZONE 100) · airframe 55,714 hrs · 28,679 cycles

CORROSION ON DIAPHRAGM UNDER G-1 GALLEY DRAIN PAN. INSTALLED DOUBLER REPAIR PER AARD 53-20-00-16.

Part: MOUNT — CORRODED (ZONE 100) · airframe 55,714 hrs · 28,679 cycles

CORROSION TOP OF FORWARD OUTBOARD GALLEY TIE DOWN FITTING. REPLACED FORWARD OUTBOARD OUTBOARD GALLEY MOUNT PER SRM 51-00-00.

Part: DIAPHRAGM — CORRODED (ZONE 100) · airframe 55,714 hrs · 28,679 cycles

CORROSION ON SUB FLOOR DIAPHRAM BETWEEN STATION 160-200. INSTALLED DOUBLER/DIAPHRAM DOUBLER BETWEEN STATION 160-200, RBL 42-57,PER AARD 53-20-00-16.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 55,714 hrs · 28,679 cycles

LEFT LOUVER BOX INBOARD FORWARD UPPER CORNER ATTACH ANGLE CRACKED. INSTALLED REPAIR DOUBLER ON ATTACH ANGLE PER SRM 53-01-00.

Part: FITTING — CORRODED (ZONE 100) · airframe 55,714 hrs · 28,679 cycles

CORROSION ON GALLEY TIE DOWN FITTING. REPLACED GALLEY TIE DOWN FITTING PER SRM 51-01-00.

Part: CUSP WEB — CORRODED (ZONE 100) · airframe 55,714 hrs · 28,679 cycles

CORROSION ON TOP OF SUBFLOOR CUSP FORWARD OF NR 6 SEAT TRACK. INSTALLED CUSP REPAIR DOUBLER PER AARD 53-20-00-16.

Part: SEAT TRACK — CORRODED (ZONE 100) · airframe 55,714 hrs · 28,679 cycles

SEAT TRACK NR 6 HAS CORROSION, STATION 214-220 RIGHT. INSTALLED NR 6 SEAT TRACK SPLICE PER SRM 53-05-00.

Part: CUSP WEB — CORRODED (ZONE 100) · airframe 55,714 hrs · 28,679 cycles

CORROSION ON CUSP STATION 218 UNDER G-2 GALLEY MOUNT. INSTALLED REPAIR DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (ZONE 100) · airframe 55,714 hrs · 28,679 cycles

CRACK IN CUSP STATION 219 RIGHT OUTBOARD OF NR 6 SEAT TRACK. INSTALLED NEW CUSP AT STATION 218 TO 237 RIGHT, PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (ZONE 100) · airframe 55,714 hrs · 28,679 cycles

CUSP ANGLE CORRODED STATION 160 RIGHT. REPLACED CUSP ANGLE FROM STATION 144 TO 227 PER SRM 53-05-00 AND ESO 80559 DATED 10/13/08.

Part: CUSP WEB — CORRODED (ZONE 100) · airframe 55,714 hrs · 28,679 cycles

RIGHT CUSP CORRODED. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: ANGLE — CORRODED (ZONE 100) · airframe 55,714 hrs · 28,679 cycles

CORROSION ON UNDERSIDE OF CUSP ANGLE BETWEEN STATION 204-218. REPLACED CUSP ANGLE.

Part: SHEAR TIE — CORRODED (ZONE 100) · airframe 55,714 hrs · 28,679 cycles

SHEAR TIE CORRODED IN AFT CARGO AT STATION 1287 LONGERON 29 LEFT. INSTALLED SHEAR TIE AND DOUBLER PER SRM 53-03-00.

Part: CYLINDER — DAMAGED (NLG) · airframe 55,714 hrs · 28,679 cycles

RETRACK CYLINDER STRUCK NOSE LANDING GEAR CASTING. INSTALLED NEW NOSE LANDING GEAR RETRACK CYLINDER.

Part: FLOOR PANEL — CORRODED (ZONE 100) · airframe 55,714 hrs · 28,679 cycles

CORROSION ON SUBFLOOR FORWARD OF NR 6 SEAT TRACK. CORROSION REMOVED AND INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: BOLT — MIGRATED (NLG) · airframe 55,714 hrs · 28,679 cycles

BOLT FOR NOSE LANDING GEAR RETRACK CYLINDER SCORED DUE TO MIGRATING EYE BOLT BUSHINGS. REPLACED BOLT AND BUSHINGS PER 32-32-06.

Part: SEAT TRACK — CORRODED (ZONE 100) · airframe 55,714 hrs · 28,679 cycles

NUMBER 3 SEAT TRACK CORRODED AT STATION 1176 TO 1180. INSTALLED SEAT TRACK SPLICE PER 53-05-00.

Part: BEAM — OUT OF LIMITS (FUSELAGE) · airframe 55,714 hrs · 28,679 cycles

MID CARGO DOOR LAMB BEAM DAMAGE OUT OF LIMITS. INSTALLED REPAIR DOUBLER PER AARD 53-10-00-3.

Part: BEAM — CORRODED (ZONE 100) · airframe 55,714 hrs · 28,679 cycles

AFT DOOR BEAM CORRODED. INSTALLED DOUBLER PER AARD 53-10-00-03.

Part: CUSP WEB — CORRODED (BS 1250-1309) · airframe 55,714 hrs · 28,679 cycles

BOTTOM OF CUSP CORRODED AT STATION 1308 TO 1309 LONGERON 18 RIGHT. CUSP SHEET REPLACED FROM STATION 1250 TO 1309 PER AARD 53-20-00-16.

Part: CUSP WEB — CRACKED (ZONE 100) · airframe 55,714 hrs · 28,679 cycles

3 INCH CRACK IN LEFT CUSP BETWEEN NR 1 AND NR 2 SEAT TRACK AT STATION 1295. NEW LEFT CUSP INSTALLED AT STATION 1250 TO 1309 PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (ZONE 100) · airframe 55,714 hrs · 28,679 cycles

CORROSION ON RIGHT CUSP AT STATION 1155 TO 1174. CORROSION REMOVED AND DOUBLER INSTALLED PER AARD 53-20-00-16.

Part: SKIN — SCRATCHED (ZONE 100) · airframe 55,714 hrs · 28,679 cycles

SCRATCHES IN SKIN AFT OF AFT CARGO DOOR MEASURING 8 INCHS BY 1.25 INCHES. INSTALLED EXTERNAL FUSELAGE DOUBLER AND FILLER PER SRM 53-05, FIG 80.

Part: MOUNT — CORRODED (ZONE 100) · airframe 55,714 hrs · 28,679 cycles

GALLEY TIE DOWN MOUNT CORRODED. REPLACED GALLEY FLOOR MOUNT.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 55,714 hrs · 28,679 cycles

RIGHT CUSP WEB CRACKED AT STATION 788. INSTALLED CUSP REPAIR PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 55,714 hrs · 28,679 cycles

RIGHT CUSP CORRODED AT STATION 826 TO 845. CUT OUT CORROSION AND INSTALLED CUSP REPAIR DOUBLER PER AARD 53-20-00-16/

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 55,714 hrs · 28,697 cycles

AFT UPPER CORNER OF WINDOW PANE IS CRACKED. DOUBLER INSTALLED PER AARD 53-10-00-25.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 55,714 hrs · 28,679 cycles

AFT UPPER CORNER OF WINDOW PAN IS CRACKED AT STATION 1041 LEFT SIDE. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 55,714 hrs · 28,679 cycles

FORWARD LOWER SIDE OF WINDOW PAN IS CRACKED AT AFT SIDE OF STATION 1022 RIGHT SIDE. INSTALLED REPAIR ANGLE PER AARD 53-40-00-25.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 54,640 hrs

LGA - EMERGENCY LIGHT AT SEAT ROW 13CDE INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT SEAT ROW 13CDE. SYSTEM GROUND CHECKED NORMAL OPERATION. (A)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

LGA - EMERGENCY LIGHTS FROM SEAT ROWS 22 TO 26 INOPERATIVE. REPLACED BATTERY PACK AT ROW 25 OVERHEAD BIN FOR EMERGENCY LIGHTS FROM SEAT ROWS 22 TO 26. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — LOOSE (CABIN)

DFW - EMERGENCY EXIT LIGHT AT LEFT FIRST CLASS GALLEY IS LOOSE. REPLACED LOWER EMERGENCY EXIT LIGHT ASSEMBLY AT LEFT FIRST CLASS GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LINE — LOOSE (APU)

SJC - INFLIGHT SMOKE IN CABIN. RETURNED TO SJC AND LANDED WITHOUT INCIDENT. FOUND APU LEAKING OIL. TIGHTENED LOOSE OIL LINE ON APU. REPLACED BOTH PACK SOCKS AND ACCOMPLISHED PACK BURN. REPLACED APU AT DFW PER WORK CARD 49 96 82. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

ATL - OVERWING EMERGENCY LIGHT ON LEFT AND RIGHT HAND SIDES INOPERATIVE. REPLACED BATTERY PACK FOR OVERWING EMERGENCY LIGHTS ON LEFT AND RIGHT HAND SIDES. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DEN - OVERHEAD EMERGENCY LIGHTS AT ROWS 13 TO 16 INOPERATIVE. REPLACED BATTERY PACK AT B5102 FOR OVERHEAD EMERGENCY LIGHTS AT ROWS 13 TO 16. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY — INOPERATIVE (EMERGNECY LIGHT)

PHX - DURING OVERNIGHT MAINTENANCE, FOUND AFT LEFT AND RIGHT OVERWING EXIT SIGNS INOPERATIVE. REPLACED AFT ELFT AND RIGHT OVERWING EXIT SIGN BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: HEATER — MALFUNCTIONED (CARGO BAY)

AUS - FLT 1171 - EN ROUTE HSV-DFW, ENCOUNTERED SMOKE IN FIRST CLASS CABIN AT 33,000 FEET. ACCOMPLISHED CABN FIRE/SMOKE CHECKLIST. DIVERTED AUS AND LANDED WITHOUT INCIDENT. REPLACED FORWARD CARGO COMPARTMENT HEATER. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (AFT AIRSTAIR)

DFW - DURING OVERNIGHT MAINTENANCE, AFT STAIRWAY SIDEWALL EMERGENCY EXIT LIGHTS INOPERATIVE. RECONNECTED FORWARD AFT TAIL CONE ON SIDEWALL EMERGENCY EXIT IGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT)

DFW - DURING OVERNIGHT MIANTENANCE, CEILING EMERGENCY EXIT LIGHTS BY AFT GALLEY DOOR INOPERATIVE. RESEATE CEILING EMERGENCY EXIT LIGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: HARNESS — INOPERATIVE (EMERGENCY LIGHT)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT IGHT AT 10D INOPERATIVE. REPLACED EMERGENCY LIGHT PIGTAIL ASSEMBLY AT SEAT 10D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: HARNESS — INOPERATIVE (EMERGENCY LIGHT)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT 7D INOPERATIVE. REPLACED EMERGENCY LIGHT PIGTAIL ASSEMBLY AT SEAT 7D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BATTERY — DISCHARGED (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS AT ROWS 27-29 AFT SERVICE OVERHEAD INOPERATIVE. REPLACED EMERGENCY EXIT LIGHTS BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BATTERY — LOOSE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, AFT GALLEY OVERHEAD EMERGENCY PATH LIGHTING AND ROW 28-30 EMERGENCY EXIT LIGHTS INOPERATIVE. RESEATED EMERGENCY EXIT LIGHTS BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (CABIN)

RDU - DURING OVERNIGHT MAINTENANCE, EMERGENCY PATH LIGHTING IN VENTRAL STAIRS AFT SIDEWALL INOPERATIVE. REPLACED EMERGENCY PATH LIGHTING ASSEMBLY IN VENTRAL STAIRS AFT SIDEWALL, SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, FOUND EMERGENCY PATH MARKING SEAT MOUNTED LIGHT INOPERATIVE ON SEAT ROW 3. REPLACED LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LAMP — MALFUNCTIONED (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT ROW 4E DIM. REPLACED EMERGENCY EXIT LIGHT AT SEAT 4E. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT FORWARD GALLEY CEILING INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT AT FORWARD GALLEY CEILING. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: TIEDOWN TRACK — CORRODED (BS 1140-1193)

TUL - FOUND LEFT TIEDOWN TRACK PLATE EARS CORRODED OVER LINEAR DISTANCE OF 53 INCHES. SUBSEQUENT E58-4, 0104877 AND 0104878 REQUIRED REMOVAL OF ENTIRE LEFT TIEDOWN TRACK IN AFT CARGO COMPT. REMOVED DAMAGED TIEDOWN AND REPLACED WITH NEW TRACK. (M)

Part: CHANNEL — CORRODED (BS 1320)

TUL - COROSION INSIDE AND OUTSIDE OF J-CHANNEL ON FORWARD SIDE OF STA 1320 FRAME ABOVE LONGERON 30. TREATED AND PRIMED, AND INSTALLED DOUBLER PER AARD 53-10-00-14. TST: 22,603.49 CYCLES: 12,253. (X)

Part: FAN — DEFECTIVE (ACM BAY)

MIA - FLT 1845 - EN ROUTE DCA/MIA DURING CRUISE, HOT ODOR AND LIGHT SMOKE NOTED IN CABIN. ACCOMPLISHED ABNORMAL PROCEDURES AND ODOR/SMOKE STOPPED WHEN GASPER RECIRCULATION FAN TURNED OFF. NO OTHER ABNORMAL INDICATIONS AND AIRCRAFT PROCEEDED TO MIA, LANDNG WITHOUT INCIDENT. REPLACED CABIN GASPER RECIRCULATION FAN. ACCOMPLISHED GROUND ENGINE RUN AND OPERATED BOTH PACKS AND FAN WITH NO DEFECTS, ODOR OR SMOKE NOTED. SYSTEMS GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — DEFECTIVE (CABIN)

SFO - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BY PAX SEAT ROWS 32 AND 33 INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT STRIP BY PAX SEAT ROWS 32 AND 33. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT STRIP — DEFECTIVE (CABIN)

DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHT STRIP AT AFT CABIN HAD LIGHTS UNDER EXIT PLACARD INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT STRIP AT AFT CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)