N886GA

Part: SKIN — DENTED (BS 1380) · airframe 52,948 hrs · 36,474 cycles

DENT IN FUSELAGE SKIN AT BS 1380, LONGERON 2L HAS A GOUGE IN THE CENTER THAT IS FLOURESCING, FOUND DURING FPI. INSTALLED REPAIR IAW SRM 53-04-2, FIG 4, PARA 3.C.1.C.

Part: LONGERON SPLICE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 52,948 hrs · 36,474 cycles

IN TAILCONE AREA, LEFT SIDE AFT OF ACM THERE IS INTERGRANNULAR EXFOLIATION CORROSION BELOW LEFT ACM WALKWAY AT STA 1430 LONGERON 22 APPROX. REMOVED AND REPLACED LONGERON SPLICE IN TAILCONE AREA LEFT SIDE OF ACM, BELOW LEFT ACM WALKWAY AT STA 1430 LONGERON 22L IAW SRM 51-30-5.

Part: SENSE LINE — LOOSE (AC BAY)

TAIL COMPARTMENT, TEMP HIGH ANNUNCIATOR ILLUMINATED ON CLIMB THROUGH FL260. QRH 21.4 WAS RUN, ANNUNCIATOR EXTINGUISHED 1 MIN 45 SEC AFTER LT ENG THROTTLE WAS BROUGHT BACK TO IDLE. INSPECTED TAIL COMPARTMENT AREA & FOUND LT HIGH PRESS PNEUMATIC SENSE LINE LOOSE. TIGHTENED SENSE LINE AS REQUIRED. PERFORMED HIGH POWER ENG RUNS & NO DEFECTS WERE NOTED AT THIS TIME. ACFT OK FOR SERVICE IAW AMM 36-10-01.

Part: DOUBLER — CORRODED (FUSELAGE)

FORWARD LAVATORY SERVICE LANDING STATION 237 - 256, LONGERON 20L - 21L. REPAIRED FWD LAVATORY SERVICE DOOR CUT OUT DOUBLER IAW EA 40-2015-177 DATED 10 15 2015 M301 LOG PAGE 269131 ITEM 24, WO 1012158-1000.0011.

Part: SPOILER — DEFECTIVE (LEFT) · airframe 50,168 hrs · 35,021 cycles

WITH SPEED BRAKES EXTENDED AT 320 KTS ACFT HAS A MODERATE ROLL RATE TO THE RT. LESS NOTICEABLE AT 250 KTS, BUT ACFT STILL ROLLS RT. OPERATIONS CHECKED SPOILER ACTUATOR SYS IAW AM 27-61-02. FOUND LT FLIGHT SPOILER ON INBD SIDE TO BE BAD. R & R IAW LP 581290.

Part: CLAMP — DAMAGED (HEAT EXCHANGER) · airframe 50,102 hrs · 34,972 cycles

TAIL COMPARTMENT TEMP HIGH DURING CRUISE, AFTER TURNING ON AIRFOIL ANTI-ICE. FOUND NR 1 PACK CLAMP DAMAGED AT HEAT EXCHANGER. ITEM PLACED ON MEL 21-01 SIT 1 CAT C. M PROCEDURE COMPLIED WITH. PLACARDS INSTALLED. OK TO CONTINUE IAW MEL.

Part: ACM — SEIZED (AC BAY) · airframe 50,093 hrs · 34,966 cycles

SMOKE & HAZE ACCUMULATED IN THE CABIN FROM ROW 10 TO THE REAR OF THE ACFT. CRUISE ALTITUDE WAS 33000. FLIGHT TIME WAS 45 MIN INTO THE FLIGHT. IN CONJUNCTION WITH SMOKE & HAZE, FLIGHT ATTENDANTS REPORTED A STRONG BURNING SMELL, POSSIBLY AN OILY SMELL. PERFORMED CABIN ODOR & SMOKE TASK CARD 21-059-002. FOUND RT PRESS REGULATOR VLV NOT REGULATING & RT ACM SEIZED. R & R RT PRESS REGULATOR VLV IAW MM 21-31-01. R & R RT ACM IAW MM 21-51-01. PACK BURNOUT TASK CARD 21-059-008 ALSO PERFORMED. LT & RT PACK OPERATIONS & LEAK CHECKED GOOD.

Part: DUCT — BLOWN (AC BAY) · airframe 49,988 hrs · 34,902 cycles

JUST AFTER DEPARTURE THE CREW RECEIVED TAIL COMPARTMENT TEMP HIGH ANNUNCIATOR. THE CREW FINISHED THE MEMORY ITEMS & STARTED EXECUTING QRH 21.4 TAIL COMPARTMENT TEMP HIGH CHECKLIST. THE NEXT STEP AFTER THE MEMORY ITEMS IS TO PULL ONE THROTTLE BACK AT A TIME UNTIL THE LIGHT GOES OUT. IT DID NOT GO OUT AFTER PULLING THE LT THROTTLE BACK, INSTEAD THE LT OIL TEMP INCREASED & SPIKED AT 147C WITH THE ASSOCIATED CAUTION LIGHT. DECLARED AN EMER & RETURNED. THE TAIL COMPARTMENT TEMP HIGH ANNUNCIATOR WENT OUT BETWEEN 3 TO 5 MINUTES AFTER IT CAME ON. R & R SEE LOGPAGE 611960, FOUND INSULATION ON SENSOR CLEANED INSULATION SEE LOGPAGE 611958, FOUND & REPAIRED BLOWN DUCT ON ACM SEE LOGPAGE 611959. ALL SYS OPERATE NORMALLY AMM 21-51-00.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 49,976 hrs · 34,894 cycles

TAIL COMPARTMENT TEMP HIGH ANNUNCIATOR ON CLIMB OUT. COMPLIED WITH QRH. LIGHT OUT APPROX 2 MIN AFTER APU SHUTDOWN, DID NOT RETURN. REF WO 00260062-1 & WO 00260062-2. PERFORMED TASK CARD 21-059-005 & 21-059-010, NO FAULTS FOUND.

Part: ENGINE — OVERTEMP (NR 1) · airframe 49,946 hrs · 34,879 cycles

ON TAKEOFF NR 1 ENG OVER TEMP, 632 EGT FOR 25 SECONDS EPR 1.91 OAT 42C N1 92 N2 95 MAX POWER PACK ON. REF WO 00259024. R & R LT ENG. ACFT OK FOR SERVICE.

Part: ENGINE — OVERTEMP (LEFT) · airframe 49,933 hrs · 34,874 cycles

ON TAKEOFF LT ENG EGT 636 FOR APPROX 9 SEC N1 94% N2 97 & EPR 1.98 OAT 34C OIL TEMP WENT TO 136 DEGREE. DURING THE TAKEOFF ROLL THE CREW NOTED THE EGT ON THE LT ENG WENT TO 636 C FOR 9 SECONDS. THIS ACFT WAS ALREADY ON THE MTO PROGRAM & AT THIS TEMP IT WILL REQUIRE A BORESCOPE INSPECTION. DURING THE RETURN ATC DECLARED AN EMER FOR THE FLIGHT & ROLLED THE EMER EQUIP. WO 00258651 IAW POWER PLANT ENGINEERING, EXCURSION WAS DUE TO ELEVATED THRUST LEVELS. NO FURTHER ACTION REQUIRED.

Part: GROUND STUD — LOOSE (CABIN)

FORWARD ENTRY DOOR EMER LIGHT INOPERATIVE WITH SWITCH ON. COMES ON WITH FWD ENTRY DOOR LIGHT. FOUND GND STUD LOOSE ON LIGHT ASSEMBLY. SECURED GND STUD IAW SWPM 20-50-01. FUNCTION CHECKED GOOD IAW MM 33-53-00.

Part: LIGHT — INOPERATIVE (CABIN)

FORWARD ENTRY EMER LIGHTS INOPERATIVE. RELAMPED THREE EACH 43 LIGHT BULBS. BULBS ILLUMINATE ONLY WITH FWD ENTRY LIGHTS ON, REF LOG PAGE 553552 IAW AMM 33-53-01.

Part: SLIDE — UNSECURE (R1 DOOR) · airframe 49,803 hrs · 34,802 cycles

R1 SLIDE FELL OFF WHEN DOOR WAS OPENED. R & R R1 SLIDE IAW TASK CARD 25-058-017.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 49,551 hrs · 34,667 cycles

EMERGENCY EXIT FLOOR IDENTIFIER LIGHT AT ROW 25 DEF INOPERATIVE. RELAMPED IAW AMM 33-53-00. OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 49,551 hrs · 34,667 cycles

EMERGENCY EXIT FLOOR IDENTIFIER LIGHT AT ROW 24DEF REQUIRES RELAMP. RELAMPED IAW AMM 33-53-00. OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (TAILCONE) · airframe 49,516 hrs · 34,651 cycles

FOUND ON WAKE UP, TAIL CONE EMER CTR LIGHT INOPERATIVE. RELAMPED TAIL CONE EMER LIGHT. OPERATIONS CHECKED GOOD IAW AMM 33-53-01.

Part: NOSE COWL — CORRODED (RT ENGINE)

NUMBER 2 ENG NOSE COWL CORROSION BLEND OUT AT 6 O'CLOCK POSITION ON INNER LIP ATTACH POINT OUT OF LIMITS. R & R NR 2 ENG NOSE COWL IAW AMM 71-10-01.

Part: LIGHT — INOPERATIVE (CABIN)

EMERGENCY EXIT REMOVABLE LIGHT AT L1 DOOR INOPERATIVE. REPLACED BULB IAW AMM 33-53-00.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 49,461 hrs · 34,621 cycles

EMERGENCY EXIT REMOVABLE LIGHT AT L1 DOOR INOPERATIVE. REPLACED BULB IAW AMM 33-53-00.

Part: BATTERY PACK — DISCHARGED (AC BAY) · airframe 49,173 hrs · 34,467 cycles

EMERGENCY LIGHT BATTERY PACK IN TAIL SECTION INOPERATIVE. R & R EMER LIGHT BATTERY PACK IN TAIL SECTION IAW AMM 35-53-01. OPERATIONS CHECKED GOOD.

Part: TRIM MOTOR — FAILED (HORIZ STAB) · airframe 51,386 hrs · 35,562 cycles

AFTER TAKEOFF PRIMARY TRIM FAILURE. COMPLIED WITH QRH REPLACED PRIMARY LONGITUDINAL TRIM ACTUATOR MOTOR IAW AMM 27-40-01. REF LOG PG 537838 FOR OPERATIONS CHECK.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 49,134 hrs · 34,445 cycles

EXTERIOR EMER LIGHT WILL NOT ILLUMINATE. R & R BATTERY POWER SUPPLY FOR EXTERIOR EMER LIGHTS IAW AMM 33-53-00. OPERATIONS CHECKED GOOD.

Part: BATTERY — DISCHARGED (CABIN)

EMERGENCY EXIT SIGN IS INOPERATIVE AT RT FWD OVERWING EXIT. REPLACED BATTERIES IN RT FWD OVERWING EXIT SIGN IAW AMM 33-53-00, OPERATIONS CHECKED GOOD.

Part: SPAR — CRACKED (VERTICAL STAB)

VERTICAL STABILIZER LE BOLT HOLE CRACKED ON RT SIDE JUST ABOVE SPLICE AT STATION 52.267. FRONT SPAR CAP FLANGE OVERSIZED FASTENER HOLE TO .325" FOR DAMAGE REMOVAL, HFEC INSPECTED WITH NO DEFECTS NOTED IAW NDTSPM 06-10-01-003 NO CRACKS NOTED. FABRICATED FREEZE PLUG BUSHING, REPAIR STRAP & INSTALLED IAW DWG SG095500051.

Part: SKIN PANEL — CORRODED (RT WING)

RIGHT WING LOWER SKIN PANEL UPPER SURFACE CORRODED OUT OF LIMITS AT STATION XCW 114. REMOVED CORROSION DAMAGE & EXISTING MLG DOUBLER. FABRICATED TAPERED FILLER 2 X 4.5 INCHES. LOCATED, DRILLED & INSTALLED A REPLACEMENT MLG DOUBLER & REPAIR PARTS IAW SB MD80-57-239 REV 2 CONDITION 2B, DWG SR 09570085, & EA 15643.

Part: PAN — GOUGED (FUSELAGE)

FORWARD RT SERVICE DOOR JAMB PAN GOUGED, PERMANENT REPAIR. REPAIRED IAW STS EA 20-2014-060.

Part: SKIN — DENTED (RT ELEVATOR TAB)

RIGHT ELEVATOR CONTROL TAB DENTED OUT OF LIMITS ON UPPER SURFACE, STATION XHS 86. REMOVED DAMAGE, FABRICATED FILLER, DOUBLER & HOT BONDED IAW SRM 51-70-2 PARA 13 PAGE 64, BOND TESTED GOOD IAW NDTSPM 05-10-002.001. WEIGHT & BALANCED 2937 LBS ARM -12.90 WITHIN LIMITS IAW SRM 55-20-2 STEPS 11-12.

Part: CHANNEL — CRACKED (FUSELAGE)

KEEL BEAM INTERCOSTAL AT STATION 937 CRACKED IN 2 EA LOCATIONS. REPAIRED BEAM INTERCOSTAL CHANNELS AT STATION 937 IAW SRM 53-05 FIG 81.

Part: BEAM — CRACKED (L1 DOOR)

L1 DOOR INTERNAL BEAM IN NR 8 HOLE CRACKED. STOP DRILLED CRACK, FABRICATED & INSTALLED DOUBLER IAW SRM 52-05.

Part: BATTERY — DISCHARGED (FLASHLIGHT)

AFT FLIGHT ATTENDANT`S FLASHLIGHT BLINKING LIGHT IS DEAD. R & R BATTERY IAW MM 25-60-00.

Part: BATTERY — DISCHARGED (CABIN)

R1 DOOR EMERGENCY LIGHT INOPERATIVE. R & R ONE EACH BATTERY IN R1 DOOR EMERGENCY LIGHT IAW AMM 33-53-00, CHECKED GOOD.

Part: ENGINE — POWER LOSS (RIGHT)

AT APPROXIMATELY 1000 FT AGL, RT ENGINE LOST POWER, AND INDICATED APPROXIMATE IDLE CONDITIONS, NO OVERWIEGHT LANDING MADE 124,000 LBS.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION, MX REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYS WOULD NOT TEST. MX R & R POWER SUPPLY BATTERY PACK AND OPS CHECKED IAW AMM 33-50-00, SYSTEM OPS CHECKED NORMAL. ACFT RETURNED TO SERVICE.

Part: ENGINE — OVERTEMP (RIGHT)

CLIMBING THROUGH 12000FT EXPERIENCED A LOUD BANG AND SHUTTER. RIGHT ENGINE EGT EXCEEDED 700 AND ROLLED BACK THROTTLE IS BOUND FROM 2" TO IDLE FUEL LEVER IS LOCKED IN ON POSITION. REMOVED AND REPLACED RT ENGINE IAW TASK CARD R087101. OPS AND LEAK CHECKS GOOD. NO BINDING NOTED IN THROTTLE AND FUEL CUTOFF CONTROLS.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE POWER SUPPLY BATTERY PACK AND MADE ALL REQUIRED CORRECTIONS AND OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00, SYSTEM OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT HAS BEEN RETURNED TO SERVICE.

Part: SMOKE DETECTOR — FAULTY (CARGO BAY)

FLIGHT CREW REPORTED, CARGO DETECTION SYSTEM AUDIBLE ALARM AND MASTER CAUTION/MASTER WARNING ANNUNCIATORS WHILE IN CLIMB COMPLETED. QRH FOLLOWED. NO SIGNS OF FIRE. BOTH BOTTLES USED. MX REMOVED AND REPLACED ALL 4 AFT PIT SMOKE DETECTORS, BOTTLES, VALVES, MANIFOLD, AND SMOKE DETECTORS AND CONTROL PANEL. REPLACED CARGO DETECTION AND SUPPRESSION CONTROL PANEL. PERFORMED FIRE SUPPRESSION SYSTEM ADJ/TEST. NO DEFECTS NOTED. REF CMM 26-22-00. FOUND NO SIGNS OF HEAT STRESS, OUT FLOW VALVE AREA NO ABNORMALITIES NOTED. AFT TAIL AREA , APU, W/W AREAS CHECKED & NO EXCESSIVE FLUIDS NOTED. RAN PACKS & ANTICE SYSTEM NO LEAKS & SMOKEY ODORS NOTED. PER M/M 21-00-00, M/M 29-10-00 M/M 36-10-00.

Part: CUSP WEB — CORRODED (FUSELAGE)

REPAIR DOUBLER IS CORRODED ON CUSP WEB BETWEEN FS 1060 TO 1079 ON LEFT SIDE. REMOVED CORRODED DOUBLER, FABRICATED AND INSTALLED.

Part: CUSP WEB — CORRODED (FUSELAGE)

PASSENGER CABIN RT CUSP WEB CORRODED AT FS 1030. CUT OUT DAMAGED AREA, FABRICATED DOUBLER AND RING DOUBLER AND INSTALLED.

Part: CUSP WEB — CORRODED (FUSELAGE)

RIGHT CUSP WEB CORRODED AT STATION 636. REPAIRED CORRODED WEB.

Part: CUSP WEB — CORRODED (FUSELAGE)

PASSENGER CABIN RIGHT CUSP WEB CORREDED AT FS 389. REMOVED CORRODED CUSP, FABRICATED REPAIR DOUBLER AND INSTALLED.

Part: CUSP WEB — CORRODED (FUSELAGE)

PASSENGER CABIN RIGHT CUSP WEB CORRODED AT FS 1030. CUT OUT DAMAGED AREA, FABRICATED DOUBLER AND RIGHT DOUBLER INSTALLED.

Part: FRAME — GOUGED (FUSELAGE)

CABIN LEFT FRAME GOUGED AT STATION 1212 NEAR LONGEON 17L. REMOVED DAMAGED AREA, FABRICATED REPAIR ANGLE, FILLER, STRAP AND INSTALLED.

Part: SHEAR TIE — CORRODED (FUSELAGE)

AFT CARGO PIT SHEAR TIE CORRODED AT STATION 1174 BETWEEN LONGERON 30 AND 29L. REMOVED DAMAGED AREA, FABRICATED SHEAR TIE AND REPAIR.

Part: CUSP WEB — CORRODED (FUSELAGE)

RIGHT CUSP WEB CORRODED AT STATION 370. REPAIRED RIGHT CUSP WEB.

Part: FRAME — GOUGED (FUSELAGE)

CABIN LEFT FRAME GOUGED AT STATION 1231 NEAR LONGERON 17L. REMOVED DAMAGED AREA, FABRICATED REPAIR ANGLE, FILLER, STAMP AND INSTALLED.

Part: CUSP WEB — CORRODED (FUSELAGE)

CABIN LEFT CUSP WEB 3 AREAS OF CORROSION STATION 712 TO 786. CUT OUT DAMAGED AREAS, FABRICATED REPAIR FILLERS, RING DOUBLERS, REPAIR DOUBLERS AND INSTALLED.

Part: CUSP WEB — CRACKED (FUSELAGE)

CABIN LEFT CUSP WEB CRACKED AT STATION 810 LBL 55. CRACK MEASURES .400. CUT OUT CORROSION AND FABRICATED REPAIR DOUBLER DRILLED AND INSTALLED.

Part: SKIN — CHAFED (CARGO DOOR)

FWD CARGO DOOR EXTERNAL SKIN CHAFED OUT OF LIMITS AT FWD LOWER CORNER. CUT OUT DAMAGED AREA, FABRICATED, DOUBLER, FILLER, LOCATED AND INSTALLED.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE POWER SUPPLY BATTERY PACK AND MADE ALL REQUIRED CORRECTIONS AND OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00, SYSTEM OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT HAS BEEN RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN)

DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE BATTERIES IN THE BATTERY PACK AND RELAMPED, MADE ALL REQUIRED CORRECTIONS AND OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00, SYSTEM OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT HAS BEEN RETURNED TO SERVICE.

Part: SWITCH — DAMAGED (COCKPIT)

PILOT; ON DESCENT WITH WING LANDING LIGHTS AND NOSE LIGHT ON, ELECTRICAL FIRE WAS SMELLED & SEVERAL SECONDS LATER SMOKE WAS SEEN COMING FROM PANEL LIGHTS. LIGHTS WERE TURNED OFF AND NO MORE SMOKE SEEN. MX; DURING INSPECTION FOUND ARCING BEHIND NOSE LIGHT SWITCH. REMOVED LIGHT SWITCH (NOSE LIGHT) AND FOUND LOOSE TERMINAL AND POSSIBLE GROUNDING PROBLEM ON NOSE LIGHT SWITCH, REMOVED AND REPLACED SWITCH S1-9 (NOSE GEAR LANDING AND TAXI LIGHT P/N 8906K1269) IAW SWPM 20-20-03 OP'S CHECK NORMAL REF W/O 00177903 ITEM 6 FOR SDR.

Part: BATTERY — DISCHARGED (CABIN)

DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE BATTERIES IN THE POWER SUPPLY BATTERY PACK AND MADE ALL REQUIRED CORRECTIONS AND OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00, SYSTEM OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT HAS BEEN RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN)

DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE BATTERIES IN THE POWER SUPPLY BATTERY PACK AND MADE ALL REQUIRED CORRECTIONS AND OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00, SYSTEM OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT HAS BEEN RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN)

DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE BATTERIES IN THE POWER SUPPLY BATTERY PACK AND MADE ALL REQUIRED CORRECTIONS AND OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00, SYSTEM OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT HAS BEEN RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN)

DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE BATTERIES IN THE POWER SUPPLY BATTERY PACK AND MADE ALL REQUIRED CORRECTIONS AND OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00, SYSTEM OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT HAS BEEN RETURNED TO SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE POWER SUPPLY BATTERY PACK AND MADE ALL REQUIRED CORRECTIONS AND OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00, SYSTEM OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT HAS BEEN RETURNED TO SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE BATTERIES IN THE POWER SUPPLY BATTERY PACK AND MADE ALL REQUIRED CORRECTIONS AND OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00, SYSTEM OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT HAS BEEN RETURNED TO SERVICE.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT)

DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION, MAINTENANCE REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE REMOVED AND REPLACED THE BATTERIES IN POWER SUPPLY BATTERY PACK. AN OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00, OPS CHECKED NORMAL. AIRCRAFT RETURNED TO SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE POWER SUPPLY BATTERY PACK AND MADE ALL REQUIRED CORRECTIONS AND OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00, SYSTEM OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT HAS BEEN RETURNED TO SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE POWER SUPPLY BATTERY PACK AND MADE ALL REQUIRED CORRECTIONS AND OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00, SYSTEM OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT HAS BEEN RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (TAILCONE)

TAIL CONE EMERGENCY LIGHTS INOP. DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE BATTERIES IN THE POWER SUPPLY BATTERY PACK AND MADE ALL REQUIRED CORRECTIONS AND OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00, SYSTEM OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT HAS BEEN RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN)

ROW 32-33 EMERGENCY LIGHTS INOP. DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE BATTERIES IN THE POWER SUPPLY BATTERY PACK AND MADE ALL REQUIRED CORRECTIONS AND OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00, SYSTEM OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT HAS BEEN RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN)

LEFT SIDE LOWER SIDEWALL OVERWING EMERGENCY LIGHTS INOP. DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE BATTERIES IN THE POWER SUPPLY BATTERY PACK AND MADE ALL REQUIRED CORRECTIONS AND OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00, SYSTEM OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT HAS BEEN RETURNED TO SERVICE.

Part: TRUNNION — CORRODED (LT MLG)

CORROSION IN BORE OF LT MLG TRUNNION WHERE PIN MOUNTS FOR LT GEAR EXTEND/RETRACT ACTUATOR. REPAIRED PER EO 57-42-01 AND BOEING MSG WJE-11-0001-07B.

Part: BATTERY — DISCHARGED (CABIN)

DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE BATTERIES IN THE POWER SUPPLY BATTERY PACK AND MADE ALL REQUIRED CORRECTIONS AND OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00, SYSTEM OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT HAS BEEN RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN)

DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE BATTERIES IN THE POWER SUPPLY BATTERY PACK AND MADE ALL REQUIRED CORRECTIONS AND OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00, SYSTEM OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT HAS BEEN RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN)

DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE BATTERIES IN THE POWER SUPPLY BATTERY PACK AND MADE ALL REQUIRED CORRECTIONS AND OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00, SYSTEM OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT HAS BEEN RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN)

DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE BATTERIES IN THE POWER SUPPLY BATTERY PACK AND MADE ALL REQUIRED CORRECTIONS AND OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00, SYSTEM OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT HAS BEEN RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN)

DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE BATTERIES IN THE POWER SUPPLY BATTERY PACK AND MADE ALL REQUIRED CORRECTIONS AND OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00, SYSTEM OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT HAS BEEN RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN)

DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE EMERGENCY EXIT LIGHT ASSY AND BATTERIES IN THE POWER SUPPLY BATTERY PACK AND MADE ALL REQUIRED CORRECTIONS AND OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00, SYSTEM OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT HAS BEEN RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN)

DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE BATTERIES IN THE POWER SUPPLY BATTERY PACK AND MADE ALL REQUIRED CORRECTIONS AND OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00, SYSTEM OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT HAS BEEN RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN)

DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE BATTERIES IN THE POWER SUPPLY BATTERY PACK AND MADE ALL REQUIRED CORRECTIONS AND OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00, SYSTEM OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT HAS BEEN RETURNED TO SERVICE.

Part: UNKNOWN — ODOR (LAVATORY)

FLIGHT ATTENDANT REPORTED SMELL IN AFT LAV AND BACK WALL WAS HOT. MAINTENANCE PERSONNEL INSPECTED AFT LAV LIGHTING WIRING AND WATER HEATER AND RUN ALL SYSTEMS CHECKS, NO DEFECTS NOTED AT THIS TIME IAW AMM 38-00-00 AND 25-41-00. AIRCRAFT OK FOR RETURN TO SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE BATTERIES IN THE POWER SUPPLY BATTERY PACK. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00. THE AIRCRAFT HAS RETURNED TO SERVICE.

Part: ANGLE — BENT (BS 1245)

DURING BOW 1C/2C/S1/S2/S4, LT CUSP T-ANGLE BENT AT STA 1245. ADDRESSED AS REQUIRED.

Part: CUSP WEB — CORRODED (FUSELAGE)

DURING BOW 1C/2C/S1/S2/S4, LT CUSP HAS AREAS OF CORROSION. ADDRESSED AS REQUIRED.

Part: SEAT TRACK — CORRODED (FUSELAGE)

DURING BOW 1C/2C/S1/S2/S4, NR 2 SEAT TRACK HAS AREAS OF CORROSION. ADDRESSED AS REQUIRED.

Part: SHEAR TIE — CRACKED (BS 1451 L2R)

DURING BOW 1C/2C/S1/S2/S4, FOUND SHEAR TIE CRACKED AT STA 1451 LONG 2 RT. ADDRESSED AS REQUIRED.

Part: ANGLE — CORRODED (FUSELAGE)

DURING BOW 1C/2C/S1/S2/S4, 2 INCH ANGLE INBOARD OF RT TIEDOWN TRACK IS CORRODED. ADDRESSED AS REQUIRED.

Part: CARGO TRACK — CORRODED (BS 1212-1307)

DURING BOW 1C/2C/S1/S2/S4, TIEDOWN TRACK IN AFT CARGO FOUND CORRODED BEYOND MM LIMITS, RT SIDE FROM STA 1212 - 1307. ADDRESSED AS REQUIRED.

Part: CARGO TRACK — CORRODED (CARGO BAY)

DURING BOW 1C/2C/S1/S2/S4, LT AFT TIEDOWN TRACK CORRODED SEVERAL PLACES IN REAR CARGO. ADDRESSED AS REQUIRED.

Part: DIAPHRAGM — CORRODED (BS 160 SUBFLOOR)

DURING BOW 1C/2C/S1/S2/S4, CORROSION WAS FOUND ON SUBFLOOR AT STA 160, RBL 4 TO 15. ADDRESSED AS REQUIRED.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

DURING A ROUTINE OVERNIGHT SERVICE CHECK, INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE BATTERIES IN THE POWER SUPPLY BATTERY PACK. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00. THE AIRCRAFT HAS RETURNED TO SERVICE.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS)

DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE BATTERIES IN THE POWER SUPPLY BATTERY PACK. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00. THE AIRCRAFT HAS RETURNED TO SERVICE.

Part: INLET — CRACKED (HEAT EXCHANGER)

DURING SCHEDULED INSP, FOUND VERTICAL STABILIZER L/E AT HEAT EXCHANGER INLET IS CRACKED APPROX 6.5 INCHES LONG ON LT SIDE. FOUND TO BE OUT OF LIMITS IAW SRM 55-05 FIG 3. (K)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE POWER SUPPLY BATTERY PACK. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00. THE AIRCRAFT HAS RETURNED TO SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE POWER SUPPLY BATTERY PACK. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00. THE AIRCRAFT HAS RETURNED TO SERVICE.

Part: B-NUT — LOOSE (LT ENGINE)

DURING TAKEOFF ROLL THE LEFT ENGINE OIL PRESSURE LOW LIGHT CAME ON, OIL PRESSURE INDICATOR READING WAS 19 PSI AT 80 KNOTS. ABORTED TAKEOFF AND RETURNED TO GATE. MAINTENANCE DEPARTMENT PERSONNEL DISCOVERED A LOOSE B-NUT AT THE LOW OIL PRESSURE SWITCH AND ABOUT ONE QUART OF OIL IN THE COWL. THE B-NUT WAS TIGHTENED AND THE OIL QUANITY WAS CHECKED AND OIL ADDED AS REQUIRED. LEAK AND OPS CHECK GOOD, THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

DURING A ROUTINE OVERNIGHT SERVICE CHECK MAINTENANCE INSPECTION, SANFORD REPORTED THAT AN EMERGENCY LIGHT AT ROW 34 WOULD NOT TEST. SANFORD FURTHER REPORT THE REMOVAL AND INSTALLATION OF AN EMERGENCY LIGHTS POWER SUPPLY BATTERY PACK FOR THE AFFECTED ASSEMBLY. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-53-00. THE AIRPLANE HAS RETURNED TO SERVICE.