N313WA

Part: WIRE HARNESS — BURNED (COCKPIT) · airframe 48,944 hrs · 33,474 cycles

JUST PRIOR TO T/O WHEN LANDING LIGHTS TURNED ON, SPARKS CAME FROM OVERHEAD PANEL. TURNED OFF LIGHTS SPARKS STOPPED. REPAIRED WIRE BUNDLE IN OVERHEAD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 41,532 hrs · 29,024 cycles

LWR EMERGENCY FLASHLIGHT AT AFT JUMPSEAT INOP. REPLACED BATTERY AND BRACKET.

Part: UPLOCK SENSOR — FAILED (NOSE GEAR) · airframe 40,274 hrs · 28,234 cycles

ON TAKEOFF SLC NOSE GEAR UNSAFE LIGHT ON RETRACTION. RED LIGHT STAYED ON. REPLACED NOSE UPLOCK SENSOR S846. PERFORMED GEAR SWING OPS CHECKED NORMAL.

Part: ENGINE — OVERHEATED (NR 2) · airframe 37,770 hrs · 26,574 cycles

ON T/O ROLL ABOUT 60-80 KTS, RT ENG EGT WENT FULL SCALE. HIGH WITH RED LIGHT ILLUMINATED. ABORTED T/O, PULLED THROTTLES BACK TO IDLE AND SHUT DOWN ENG. REPLACED NR 2 ENG.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 37,645 hrs · 26,486 cycles

A/C RTB, FLOOR EMERGENCY LIGHTS LAST 5 ROWS INOP. ALSO, LWR LIGHTS AT REAR DOOR INOP. FOUND DAMAGED CONNECTOR AT SEAT 28 DEF AND 2 BATTARY BASES INOP. REPLACED BASES AND REPAIRED CONNECTOR AT SEAT 28 DEF.

Part: FITTING — LEAKING (NR 1 ENGINE)

A SYSTEM HYDRAULIC SYSTEM DECREASED TO 1/4. INT LOW HYD LIGHT ON NR 1 ENG NR CAME ON STEADY ON TAXI IN. MONITORED VERY SLOW FLUID LOSS DURING 1/2 TO 1/4 WENT ABOVE 1/4 WITH GEAR EXTENSION. SECURED FITTING ON A SYSTEM FILTER MODULE, LEAK CHECKS GOOD.

Part: GENERATOR — FAILED (NR 1 ENGINE)

NR 1 ENGINE DRIVEN GENERATOR TRIPPED OFF ON CLIMBOUT. APU ON PREVIOUS MCO. REPLACED CSD.

Part: BULKHEAD — CRACKED (BS 178)

THE FS 178 BULKHEAD WEB WAS FOUND TO BE CRACKED IN 3 PLACES. THE LHS CHORD WAS ALSO FOUND CRACKED. THE SIDE CHORD WAS REPAIRED PER SB 737-53A1173 AND THE WEB WAS REPAIRED PER ERA 333649-14.

Part: SPAR — GOUGED (RT WING)

THE RIGHT WING REAR SPAR WAS GOUGED AT THE MLG BEAM AFT ATTACH FITTING. THE DAMAGE WAS REPAIRED AT MV PER ER/A 333653-14.

Part: BULKHEAD — CRACKED (BS 178)

THE FS 178 BULKHEAD WEB AND SIDE CHORD WERE FOUND CRACKED. THE DAMAGE WAS REPAIRED AT MV PER ERA 333649-14.

Part: STRINGER — CRACKED (BS 727)

THE LEFT STRINGER 18A WAS FOUND CRACKED AT FS 727. THE DAMAGE WAS FOUND AT MV AND REPAIRED PER ERA 333643-14.

Part: SKIN — GOUGED (BS 970)

THE FUSELAGE SKIN WAS GOUGED AT FS 970, ELEVEN INCHES BELOW THE R2 DOOR AT STRINGER 19L. THE DAMAGE WAS FOUND AT AMV AND REPAIRED PER ERA 333671-14.

Part: TARGET — BENT (CARGO DOOR)

AFT CARGO LIGHT ILLUMINATED AT APPROX 1000 FT MSL. FOUND TARGET BENT, REPOSITIONED SAME. CHECKS NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN)

ON LAYOVER INSP, FOUND SEVERAL SECTIONS OF FLOOR EMER EXIT LIGHTING WEAK. REPLACED 1 PWR SUPPLY RACK WITH BATTERY, SYS NOW OPS NML.

Part: BATTERY PACK — DISCHARGED (CABIN)

ON LAYOVER CK, FOUND SEVERAL SECTIONS OF CABIN FLOOR EMERG EXIT LIGHTING WEAK. REPLACED 2 BATTERY PACKS.

Part: OVEN — SMOKING (FWD GALLEY)

SMOKE OBSERVED COMING FROM FWD GALLEY INBD OVEN. TURNED OFF AND SMOKE CLEARED. PUT ON MCO C/N 549351002 BY SLC. ITEM CLEARED BY REPLACEMENT OF OVEN.

Part: WINDOW — CRACKED (RT COCKPIT)

FIRST OFFICER'S FORWARD WINDOW R1 OUTER PANE CRACKED IN-FLIGHT. LANDED SLC. REPLACED WINDOW PER MM.

Part: COFFEEMAKER — SMOKED (LT COCKPIT)

LOUD POP HEARD FROM AFT COFFEEMAKER FOLLOWED BY ELECTRIC SMOKE. REPLACED COFFEEMAKER CAPT SIDE AFT.

Part: SKIN CLIPS — CRACKED (FS FRAME 807)

DURING HMV, THE SKIN CLIPS WERE FOUND TO BE PITTED BETWEEN STRS 28L AND 28R. THE DAMAGED CLIPS WERE REMOVED AND A REPAIR WAS INSTALLED, ALL PER SRM 53-00-07 FIG 203.

Part: SKIN — DAMAGED (LT ELEV)

DURING HMV INSPECTION, FOUND EXISTING REPAIR IN POOR CONDITION ON LT ELEVATOR LOWER SURFACE T/E, 30 INCHES FROM O/B END. REPAIRED PER ERA 271896-14.

Part: SKIN — DAMAGED (LT ELEVATOR)

DURING HMV INSPECTION, FOUND LT ELEVATOR TOP SURFACE DAMAGE LOCATED 6 INCHES FROM TRAILING EDGE BETWEEN STATION 39 AND STATION 66.5. REPAIRED PER SRM 55-20-01 REF 51-70-17.

Part: SKIN — DAMAGED (LT ELEV)

FOUND DURING LETTER CHECK INSP, SMALL HOLE IN L/T ELEV, APPROX 24 INCHES FROM O/B END. REPAIRED PER SRM 51-70-05, WEIGHT ADDED IN REPAIR NEGLIGIBLE REBALANCE NOT REQUIRED PER SRM 51-60-04.

Part: SKIN — DELAMINATED (RUDDER)

DURING INSPECTION, FOUND RUDDER WITH NUMEROUS AREAS OF DELAMINATION ON OUTER SKIN. REPAIRED PER SRM 55-40-01.