N188AN

Part: SLIDING WINDOW — BINDING (COCKPIT) · airframe 65,005 hrs · 16,403 cycles

AIRCRAFT WAS NOT GROUNDED: CAPTAINS WINDOW IS VERY DIFFICULT TO LOCK , UNLOCK AND OPEN/CLOSE. LUBED WINDOW LOCKCOMPONENTS AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 56-11-02.

Part: GCU — FAULTY · airframe 64,844 hrs · 16,344 cycles

AIRCRAFT WAS GROUNDED: PILOT REPORTS AT FL 380 LH ENGINE HAD 4 ABNORMAL INDICATIONS HAPPENING SIMULTANEOUSLY DUCT PRESS WENT ABOVE 60 PSI EGT, N2, N3 ALL WENT INTO YELLOW BAND AND WOULD HAVE EXCEEDED RED WITHOUT THROTTLE REDUCTION. FL 360 HAD REAT. BELOW FL 300 ALL INDICATIONS STAYED NORMAL. MAINTENANCE PERFORMED EEC BITE IAW FIM 73-21-00, NO FAULTS FOUND. PERFORMED TPU BITE OF LH ENG IAW FIM 75-32-00-301, FOUND FAULT CODE B3, TPU REPLACEMENT NECESSARY. REMOVED AND REPLACED LH ENG TPU SENSOR IAW AMM 75-32-15-404-012-R00. PERFORMED BVCU BITE OF LH ENG IAW FIM 75-32-00-301, FOUND FAULT CODE 74-7E (REPLACE BVCU). REMOVED AND REPLACED LH ENG BVCU IAW AMM 75-32-01, BITE TEST NORMAL. REMOVED AND REPLACED ENG 1 UPPER AND LOWER GCU IAW AMM 73-21-10. GENERATOR AND STATOR REMOVED AND REPLACED AND OPS CHECKED. ACCOMPLISHED DEDICATED GENERATOR TEST IAW AMM 73-21-08, STEP H. ALL CHECKS OK. NO LEAKS NOTED. (SEE SDR # AALA201912059004, AALA201912099051, AALA201912099052)

Part: GCU — FAULTY (LT ENGINE) · airframe 64,844 hrs · 16,344 cycles

AIRCRAFT WAS GROUNDED: PILOT REPORTS AT FL 380 LH ENGINE HAD 4 ABNORMAL INDICATIONS HAPPENING SIMULTANEOUSLY DUCT PRESS WENT ABOVE 60 PSI EGT, N2, N3 ALL WENT INTO YELLOW BAND AND WOULD HAVE EXCEEDED RED WITHOUT THROTTLE REDUCTION. FL 360 HAD REAT. BELOW FL 300 ALL INDICATIONS STAYED NORMAL. MAINTENANCE PERFORMED EEC BITE IAW FIM 73-21-00, NO FAULTS FOUND. PERFORMED TPU BITE OF LH ENG IAW FIM 75-32-00-301, FOUND FAULT CODE B3, TPU REPLACEMENT NECESSARY. REMOVED AND REPLACED LH ENG TPU SENSOR IAW AMM 75-32-15-404-012-R00. PERFORMED BVCU BITE OF LH ENG IAW FIM 75-32-00-301, FOUND FAULT CODE 74-7E (REPLACE BVCU). REMOVED AND REPLACED LH ENG BVCU IAW AMM 75-32-01, BITE TEST NORMAL. REMOVED AND REPLACED ENG 1 UPPER AND LOWER GCU IAW AMM 73-21-10. GENERATOR AND STATOR REMOVED AND REPLACED AND OPS CHECKED. ACCOMPLISHED DEDICATED GENERATOR TEST IAW AMM 73-21-08, STEP H. ALL CHECKS OK. NO LEAKS NOTED. (SEE SDR # AALA201912099050, AALA201912099051, AALA201912099052)

Part: STATOR — UNRELIABLE · airframe 64,844 hrs · 16,344 cycles

AIRCRAFT WAS GROUNDED: PILOT REPORTS AT FL 380 LH ENGINE HAD 4 ABNORMAL INDICATIONS HAPPENING SIMULTANEOUSLY DUCT PRESS WENT ABOVE 60 PSI EGT, N2, N3 ALL WENT INTO YELLOW BAND AND WOULD HAVE EXCEEDED RED WITHOUT THROTTLE REDUCTION. FL 360 HAD REAT. BELOW FL 300 ALL INDICATIONS STAYED NORMAL. MAINTENANCE PERFORMED EEC BITE IAW FIM 73-21-00, NO FAULTS FOUND. PERFORMED TPU BITE OF LH ENG IAW FIM 75-32-00-301, FOUND FAULT CODE B3, TPU REPLACEMENT NECESSARY. REMOVED AND REPLACED LH ENG TPU SENSOR IAW AMM 75-32-15-404-012-R00. PERFORMED BVCU BITE OF LH ENG IAW FIM 75-32-00-301, FOUND FAULT CODE 74-7E (REPLACE BVCU). REMOVED AND REPLACED LH ENG BVCU IAW AMM 75-32-01, BITE TEST NORMAL. REMOVED AND REPLACED ENG 1 UPPER AND LOWER GCU IAW AMM 73-21-10. GENERATOR AND STATOR REMOVED AND REPLACED AND OPS CHECKED. ACCOMPLISHED DEDICATED GENERATOR TEST IAW AMM 73-21-08, STEP H. ALL CHECKS OK. NO LEAKS NOTED. (SEE SDR # AALA201912059004, AALA201912099050, AALA201912099051)

Part: ROTOR — UNRELIABLE · airframe 64,844 hrs · 16,344 cycles

AIRCRAFT WAS GROUNDED: PILOT REPORTS AT FL 380 LH ENGINE HAD 4 ABNORMAL INDICATIONS HAPPENING SIMULTANEOUSLY DUCT PRESS WENT ABOVE 60 PSI EGT, N2, N3 ALL WENT INTO YELLOW BAND AND WOULD HAVE EXCEEDED RED WITHOUT THROTTLE REDUCTION. FL 360 HAD REAT. BELOW FL 300 ALL INDICATIONS STAYED NORMAL. MAINTENANCE PERFORMED EEC BITE IAW FIM 73-21-00, NO FAULTS FOUND. PERFORMED TPU BITE OF LH ENG IAW FIM 75-32-00-301, FOUND FAULT CODE B3, TPU REPLACEMENT NECESSARY. REMOVED AND REPLACED LH ENG TPU SENSOR IAW AMM 75-32-15-404-012-R00. PERFORMED BVCU BITE OF LH ENG IAW FIM 75-32-00-301, FOUND FAULT CODE 74-7E (REPLACE BVCU). REMOVED AND REPLACED LH ENG BVCU IAW AMM 75-32-01, BITE TEST NORMAL. REMOVED AND REPLACED ENG 1 UPPER AND LOWER GCU IAW AMM 73-21-10. GENERATOR AND STATOR REMOVED AND REPLACED AND OPS CHECKED. ACCOMPLISHED DEDICATED GENERATOR TEST IAW AMM 73-21-08, STEP H. ALL CHECKS OK. NO LEAKS NOTED. (SEE SDR # AALA201912059004, AALA201912099050, AALA201912099052)

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 64,607 hrs · 16,263 cycles

AIRCRAFT WAS NOT GROUNDED: SLIDE LIGHT AT 1R DOOR INOPERABLE. MAINTENANCE RELAMPED SLIDE LIGHT PER AMM 33-2000.

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 64,607 hrs · 16,263 cycles

AIRCRAFT WAS NOT GROUNDED: SLIDE LIGHT AT 1R DOOR INOPERABLE. MAINTENANCE RELAMPED SLIDE LIGHT PER AMM 33-2000.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 64,384 hrs · 16,191 cycles

AIRCRAFT WAS NOT GROUNDED: FORWARD CABIN SEAT MOUNTED EMERGENCY LIGHTS INOPERABLE 1E TO 4E. MAINTENANCE REPLACED BATTERY FOR EMERGENCY LIGHTS PER AMM 33-51-07 AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 64,384 hrs · 16,191 cycles

AIRCRAFT WAS NOT GROUNDED: AFT CABIN SEATS 26 TO 36 EMERGENCY LIGHTS INOPERABLE. MAINTENANCE REPLACED BATTERY FOR EMERGENCY LIGHTS PER AMM 33-51-07 AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 64,378 hrs · 16,189 cycles

AIRCRAFT WAS NOT GROUNDED: MID CABIN EMERGENCY LIGHTS WERE INOPERABLE AT SEATS 9D THROUGH 26D. REPLACED BATTERY PACK PER AMM 33-51-07.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 64,378 hrs · 16,189 cycles

AIRCRAFT WAS NOT GROUNDED: MID CABIN EMERGENCY LIGHTS WERE INOPERABLE AT SEATS 9D THROUGH 26D. REPLACED BATTERY PACK PER AMM 33-51-07.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 64,384 hrs · 16,191 cycles

AIRCRAFT WAS NOT GROUNDED: MID CABIN SEAT MOUNTED EMERGENCY LIGHTS INOPERABLE. MAINTENANCE REPLACED BATTERY FOR EMERGENCY LIGHTS PER AMM 33-51-07 AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 64,378 hrs · 16,189 cycles

AIRCRAFT WAS NOT GROUNDED: MID CABIN EMERGENCY LIGHTS WERE INOPERABLE AT SEATS 9D THROUGH 26D. REPLACED BATTERY PACK PER AMM 33-51-07.

Part: BLEED VALVE — FAILED (RT ENGINE) · airframe 63,291 hrs · 15,903 cycles

AIRCRAFT WAS GROUNDED: PILOT DECLARED EMERGENCY ON ACCOUNT OF RIGHT HAND BLEED FAULT. FLIGHT LANDED OVERWEIGHT WITHOUT INCIDENT. MAINTENANCE REPLACED R ENG PRSOV IAW AMM 36-11-09. RT ENG BLEED OPS CHECKS NORMAL IAW AMM 36-11-00-710-801.

Part: CONTACT — UNLOCKED (EMERGENCY LIGHT) · airframe 62,849 hrs · 15,781 cycles

AIRCRAFT NOT GROUNDED: MAINTENANCE REPORTS EMERGENCY LIGHT INOP AT SEAT12D. RELOCKED CONTACT ON SEAT TO WALL CONNECTOR IAW ESPM 20-42-01. OPS CHECKS NORMAL IAW AMM 33-51-00.

Part: TRACK — OUT OF ADJUST (L2 DOOR) · airframe 60,965 hrs · 15,223 cycles

ENTRY DOOR LATCH DOES NOT SECURE THE L2 DOOR CLOSED AND LOCKED. ADJUSTED THE UPPER TRACK. OPS CHECKED GOOD.

Part: PLATE — CORRODED (BS 1708-1720) · corrosion level 2 · airframe 60,599 hrs · 15,142 cycles

CORROSION ON THE AFT DECK PLATE BETWEEN BS 1708 AND 1720, LBL 53 TO RBL 53. REPAIRED THE AFT DECK PLATE IAW SRM 53-60-51-2R-18.

Part: SKIN — CRACKED (RT WING) · airframe 60,599 hrs · 15,142 cycles

AIRCRAFT IN BASE MAINTENANCE. CRACK INDICATION ON THE RIGHT WING UPPER SKIN AT THE DIAGONAL BRACE NR 4 FASTENER HOLE. REPAIRED RIGHT WING UPPER SKIN PER EA 281687.

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 60,599 hrs · 15,142 cycles

LEFTOVERWING FUEL PORT FAILED A RESISTANCE BONDING CHECK. DURING DISSEMBELY, DISCOVERED CORROSION ON THE UPPER AND LOWER LANDINGS OF THE WING SKIN BETWEEN LWS 469.5 - 479.5. REPLACED THE LT WING OVERWING FILL PORT IAW AMM 28-11-04-404.

Part: ACCESS DOOR — DETACHED (GRND AIR SUPPLY) · airframe 60,495 hrs · 15,111 cycles

GROUND AIR SUPPLY ACCESS DOOR FOUND MISSING FROM AIRCRAFT, BROKEN OFF AT HINGES. INSTALLED NEW DOOR PER AMM 52-49-04. AIRCRAFT WAS GROUNDED.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 59,574 hrs · 14,846 cycles

L2 DOOR EXIT SLIDE LIGHT IS INOPERATIVE. REPLACED THE LAMPS IAW AMM 33-51-06.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 59,574 hrs · 14,846 cycles

R4 DOOR EXIT SLIDE LIGHT IS INOPERATIVE. REPLACED THE LAMPS IAW AMM 33-51-06.

Part: BULB — LOOSE (EMERGENCY LIGHT) · airframe 57,275 hrs · 14,263 cycles

EMERGENCY EVACUATION SLIDE EXTERIOR LIGHT AT L2 DOOR IS INOPERATIVE. SECURED BULB IAW AMM 33-51-06. OPERATIONAL CHECKED GOOD.

Part: FAN — FAILED (RECIRCULATION) · airframe 57,259 hrs · 14,258 cycles

CAPTAIN REPORTED ELECTRICAL ODOR IN CABIN AFTER THE LEFT RECIRCULATION FAN FAILED. REMOVED AND REPLACED LEFT RECIRCULATION FAN IAW AMM 21-25-01. OPERATIONAL CHECKED GOOD. AIRCRAFT WAS GROUNDED.

Part: CONTROL PANEL — FAULTY (EMERGENCY LIGHTS) · airframe 57,012 hrs · 14,189 cycles

DURING PREFLIGHT, EMERGENCY LIGHTS WOULD NOT PROPERLY ARM. REMOVED AND REPLACED EMERGENCY LIGHT CONTROL PANEL IAW AMM 33-51-08. OPERATIONAL CHECKED GOOD.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 56,699 hrs · 14,091 cycles

AIRCRAFT WAS NOT GROUNDED. FLIGHT ATTENDANT EMERGENCY FLASHLIGHT AT R2 DOOR IS INOPERATIVE. REMOVED AND REPLACED FLASHLIGHT BATTERY IAW AMM 25-64-00. OPERATIONAL CHECK GOOD.

Part: TRANSCEIVER — FAULTY (VHF COMM) · airframe 56,676 hrs · 14,084 cycles

AIRCRAFT WAS NOT GROUNDED. MIA-LPB FLIGHT DIVERTED TO VVI ACCOUNT LEFT VHF RADIO FAILED. LANDING UNEVENTFUL. REMOVED AND REPLACED LEFT VHF RADIO TRANSCEIVER ASSEMBLY IAW AMM 23-12-01. OPERATIONAL CHECK GOOD.

Part: RESERVOIR — LOW PRESSURE (L4 DOOR) · airframe 56,312 hrs · 13,989 cycles

L4 DOOR EMERGENCY POWER RESERVOIR PRESSURE BELOW LIMITS. REMOVED AND REPLACED RESERVOIR ASSEMBLY IAW AMM 52-1130. OPS CHECKED GOOD.

Part: WIRE HARNESS — FAULTY (EMERGENCY LIGHT) · airframe 55,652 hrs · 13,822 cycles

EMERGENCY LIGHTS AT ROW 15 INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT WIRE HARNESS AT ROW 15 IAW ESO 90565. OPS CHECKED NORMAL.

Part: PAD — MISSING (RT ENGINE) · airframe 52,546 hrs · 13,069 cycles

RIGHT ENG VIBRATION, 3.1 TO 3.2, DURING CRUISE. THE FLIGHT DECLARED AN EMER & RETURNED WITHOUT FURTHER INCIDENT. ACFT WAS TAKEN OUT OF SERVICE. INSTALLED RT ENG CHOCKING PADS ON LP FAN BLADES, NR 4 & 16 IAW MCM 72-94-01. ACCOMPLISHED FAN TRIM BALANCE IAW MCM 71-95-25. ALL INDICATIONS WERE NORMAL.

Part: ENGINE — LEAKING (LEFT) · airframe 52,545 hrs · 13,068 cycles

LANDED, ACCOUNT LT ENG SHUT DOWN DUE TO OIL QTY DROPPING. EMER LANDING WAS DECLARED, UNEVENTFUL LANDING. SINGLE ENG TIME WAS 30 MINUTES. ACFT WAS REMOVED FROM SERVICE. R & R LT ENG IAW MCM CARD 71-94-01. ACCOMPLISHED ALL REQUIRED TESTS, GOOD FOR SERVICE.

Part: FLAP — WORN (RT WING) · airframe 51,998 hrs · 12,955 cycles

RIGHT INBD MAIN FLAP LE STRUCTURE WORN FROM CONTACT WITH THE FIXED WING STRUCTURE SHELF. ACCOMPLISHED FLUSH DOUBLER REPAIR IAW SRM 57-53-01-2R-2 & EA 253982 DATED 08 24 2015.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 50,672 hrs · 12,653 cycles

FIRST CLASS SEAT EMERGENCY LIGHT INOPERATIVE. R & R BATTERY PACK IAW AMM 33-51-07. PERFORMED OPERATIONAL CHECK IAW AMM 33-51-00. SYS CHECKED NORMAL.

Part: VALVE — FAULTY (LT ENGINE) · airframe 50,360 hrs · 12,576 cycles

AIR INTERRUPT, RETURNED & EMER DECLARED. LANDING UNEVENTFUL & ACFT WAS OVERWEIGHT. DURING CLIMB CREW REPORTED LT ENG HAS HIGH EXHAUST GAS TEMP. ANNUNCIATOR EXTINGUISHED AFTER RETARDING THE THROTTLE. R & R LT ENG HI STAGE PNEUMATIC VLV & HP6 AIR OUTLET DUCT IAW AMM 36-11-01. PERFORMED TEST NR 3 IP & HP COMPRESSOR AIR FLOW IAW TASK 71-00-00. SYS CHECKED NORMAL.

Part: LIGHT — UNSECURE (CABIN) · airframe 49,947 hrs · 12,475 cycles

EMERGENCY EXIT LIGHT AT FWD S MID LAVATORY IS INOPERATIVE. SECURED EMER EXIT LIGHT ASSEMBLY. PERFORMED OPERATIONAL CHECK IAW AMM 33-50-00. SYSTEM CHECKED NORMAL.

Part: WIRE — BROKEN (ZONE 700) · airframe 48,963 hrs · 12,239 cycles

ANTI-SKID MSG ON DESCENT. EMER DECLARED FLIGHT LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. FOUND BROKEN WIRE AT CONNECTOR D2046 NR 8 TRANSDUCER. REPAIRED WIRE AT CONNECTOR D2046. SYS GND CHECKED NORMAL OPERATION CLOSED.

Part: SIGN — INOPERATIVE (CABIN) · airframe 47,846 hrs · 11,962 cycles

AFT GALLEY RT 4 EXIT EMERGENCY SIGN INOPERATIVE. REPLACED AFT GALLEY RT NR 4 EMERGENCY EXIT SIGN. OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 47,188 hrs · 11,799 cycles

SEAT 14DEF ESCAPE PATH LIGHT INOPERATIVE. REPLACED LAMP FOR SEAT 14DEF ESCAPE PATH LIGHT. OPERATIONS CHECKED NORMAL.

Part: TRANSMITTER — INOPERATIVE (RT ENGINE) · airframe 46,055 hrs · 11,532 cycles

SJU INFLIGHT MIA-REC FLUCTUATING N3 ON THE RT HAND ENG ALONG WITH FLUCTUATING RT HAND BLEED PRESSURE. FLIGHT DIVERTED SJU LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED RT HAND EN N3 TACH TRANSMITTER. SYSTEM GROUND CHECKED NORMAL OPERATION CLOSED.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 43,155 hrs · 10,863 cycles

EMERGENCY EXIT SIGN AFT OF LEFT NUMBER 3 DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY EXIT SIGN AFT OF LEFT NUMBER 3 DOOR. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 43,155 hrs · 10,863 cycles

EXTERIOR EMERGENCY LIGHT AFT OF LEFT NUMBER 3 DOOR INOPERATIVE. REPLACED LAMP FOR EXTERIOR EMERGENCY LIGHT AFT OF LEFT NUMBER 3 DOOR. OPS CHECK NORMAL.

Part: INDICATOR — FAULTY (COCKPIT) · airframe 43,155 hrs · 10,863 cycles

MIA - CREW REPORTED SPLIT FLAP INDICATION. EMERGENCY DECLARED FLIGHT LANDED MIA WITHOUT INCIDENT. BITE FSEU WITH NO FAULTS NOTED. ALL FUNCTIONS CHECK NORMAL. REPLACED FLAP INDICATOR AS PRECAUTIONARY. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: CONTROL PANEL — SHORTED (COCKPIT) · airframe 42,439 hrs · 10,688 cycles

PTY INFLIGHT MIA-UIO. CREW REPORTED ELECTRICAL SPARKS IN FLIGHT DECK OVERHEAD PANEL. EMERGENCY DECLARED FLIGHT DIVERTED PTY LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED EXTERIOR LIGHTS CONTROL PANEL THAT HAD SHORTED. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: PILOT VALVE — INOPERATIVE (BLEED AIR SYS) · airframe 41,621 hrs · 10,492 cycles

BOS - CREW REPORTED RIGHT ENGINE HIGH STAGE LIGHT ILLUMINATED. EMERGENCY DECLARED FLIGHT RETURNED BOS LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED HIGH STAGE PILOT VALVE. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 41,397 hrs · 10,428 cycles

CENTER INTERCOSTAL FLOORBOARD SUPPORT ANGLE FROM STATIONS 1580 TO 1600 CRACKED. REMOVED AND REPLACED CENTER INTERCOSTAL SUPPORT ANGLE PER AARD 51-00-05.

Part: FLAP — CORRODED (RT WING) · corrosion level 3 · airframe 41,397 hrs · 10,428 cycles

CORROSION TO RIGHT INBOARD FLAP 31 INCHES FROM INBOARD END. INSTALLED PERMANENT HOT BONDED DOUBLER AS PER SRM 51-70-10-2R 4.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,397 hrs · 10,428 cycles

CORROSION ON LEFT GUTTER SUPPORT FROM STATIONS 1640 TO 1660, LEFT BUTTLINE 56. REMOVED AND REPLACED FORWARD GUTTER SUPPORT PER AARD 51-00-05.

Part: FLAP — CORRODED (RT WING) · corrosion level 3 · airframe 41,397 hrs · 10,428 cycles

CORROSION TO RIGHT INBOARD FLAP 21.5 INCHES FROM INBOARD END. INSTALLED PERMANENT HOT BONDED DOUBLER AS PER SRM 51-70-10-2R 4.

Part: SKIN PANEL — CORRODED (TE FLAP) · corrosion level 3 · airframe 41,397 hrs · 10,428 cycles

RIGHT INBOARD FLAP CORROSION BLEND AREA UNDER INTERIM REPAIR ALONG RIB LOCATED APPROXIMATELY 17.5 FROM INBOARD END OF UPPER INBOARD SKIN PANEL OUT OF LIMITS PER SRM 57-53-01-1A. INSTALLED PERMANENT HOT BONDED DOUBLER REPAIR SRM 51-70-10-2R 4 AND EA COMP-57-025207.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,397 hrs · 10,428 cycles

CORROSION ON LEFT GUTTER SUPPORT FROM STATIONS 1660 TO 1680, LEFT BUTTLINE 56. REMOVED AND REPLACED LEFT AFT GUTTER SUPPORT PER AARD 51-00-05.

Part: FLOOR SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,397 hrs · 10,428 cycles

CORROSION ON AFT DECK IN CABIN FROM STATIONS 1709 TO 1720, RIGHT BUTTLINE 41 TO LEFT BUTTLINE 53. INSTALLED DOUBLER REPAIR PER SRM 53-60-51-2R2.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 41,397 hrs · 10,428 cycles

CENTER INTERCOSTAL FLOORBOARD SUPPORT ANGLE IS CRACKED. REMOVED AND REPLACED CENTER INTERCOSTAL FLOORBOARD SUPPORT ANGLE PER AARD 51-00-05.

Part: CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,397 hrs · 10,428 cycles

HAT CHANNEL AT STATION 1716 CORRODED. REPLACED CHANNEL PER AARD 51-00-05-1.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 41,397 hrs · 10,428 cycles

FLOORBOARD SUPPORT ANGLE CRACKED FROM STATIONS 1520 TO 1540. REPLACED SUPPORT ANGLER PER SRM 51-00-5.

Part: STIFFENER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,397 hrs · 10,428 cycles

FLOOR STIFFENER (PIN BEAM) FROM STATIONS 1700 TO 1720 CORRODED. REPLACED STIFFENER PER AARD 51-00-05.

Part: CONNECTOR — UNSECURE (CABIN) · airframe 41,179 hrs · 10,383 cycles

EMERGENCY EXIT LIGHT AT SEAT 14D INOPERATIVE. SECURED CONNECTOR FOR EMERGENCY EXIT LIGHT AT SEAT 14D. OPS CHECK NORMAL.

Part: LIGHT — MISSING (EXTERIOR) · airframe 40,842 hrs · 10,319 cycles

RIGHT NUMBER 1 DOOR EXTERIOR EMERGENCY MISSING LAMP. REPLACED LAMP FOR RIGHT NUMBER 1 DOOR EXTERIOR EMERGENCY LIGHT, OPS CHECK NORMAL.

Part: FMC — INOPERATIVE (ZONE 100) · airframe 40,277 hrs · 10,210 cycles

CREW REPORTED FLIGHT CREW LOST ROUTE INFORMATION FROM BOTH FLIGHT MANAGEMENT COMPUTERS. EMERGENCY DECLARED FLIGHT LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT FLIGHT MANAGEMENT COMPUTER. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: SIGN — MISSING (CABIN) · airframe 39,773 hrs · 10,109 cycles

EMERGENCY EXIT SIGN IN LEFT NUMBER 4 DOOR POSITION MISSING. REPLACE EMERGENCY EXIT SIGN AND LIGHT ASSEMBLY. OPS CHECK NORMAL.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 39,364 hrs · 10,027 cycles

TWO INCH DENT IN FUSELAGE SKIN BETWEEN STATIONS 215 AND 223. INSTALLED DOUBLER PER EA B757-53-021376.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 36,536 hrs · 9,457 cycles

EMERGENCY LIGHT AT SEAT 1E INOPERATIVE. REPLACED LIGHT ASSEMBLY AT SEAT 1E. OPS CHECK NORMAL.

Part: COFFEEMAKER — MALFUNCTIONED (CABIN) · airframe 32,452 hrs · 8,564 cycles

ORD - FLIGHT ATTENDANT REPORTED, HEARD LOUD POP THEN SMOKE COMING FROM NUMBER 1 AND 2 COFFEEMAKERS. FLIGHT ATTENDANT PULLED THE BREAKERS FOR ALL THREE COFFEEMAKERS. SMOKE DISSIPATED AND FLIGHT CONTINUED WITHOUT FURTHER INCIDENT. REPLACED COFFEEMAKERS. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: LENS — MISSING (EMERGENCY LIGHTS) · airframe 31,918 hrs · 8,405 cycles

EMERGENCY LIGHT AT SIDE WALL SEAT ROW 17ABC HAS LENS MISSING. INSTALLED NEW LENS.

Part: MODULE — FAILED (EMERGENCY LIGHTS) · airframe 31,918 hrs · 8,405 cycles

EMERGENCY LIGHTS DIM FROM SEAT ROWS 16 TO 25. REPLACED MODULE & BATTERY PACK.

Part: LAMP — BURNED OUT (EMERGENCY LIGHTS) · airframe 31,918 hrs · 8,405 cycles

EMERGENCY LIGHT AT EXTERIOR LEFT NUMBER FOUR DOOR INOPERATIVE. REPLACED LAMP.

Part: WIRE — BROKEN (CABIN) · airframe 31,118 hrs · 8,199 cycles

EMERGENCY PATH LIGHT INOPERATIVE AT SEAT 31D. REPAIRED BROKEN WIRE IAW MM OPS CHECKED NORMAL, OK FOR SERVICE.

Part: ENGINE — FAILED (NR 1) · airframe 26,314 hrs

FLL INFLIGHT T2083/31MAR CAPTAIN REPORTED NUMBER ONE ENGINE OIL PRESSURE WENT TO ZERO AND THE NUMBER ONE ENGINE SPOOLED DOWN. CREW SHUT NUMBER ONE ENGINE DOWN. RETURNED TO FLL AND LANDED WITHOUT INCIDENT. REPLACED NUMBER ONE ENGINE ON 01 APR AT FLL. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

SFO - EMERGENCY LIGHT AT OVERHEAD LEFT OVERWING EXIT SIGN INOPERATIVE. REPLACED BATTERY PACK M10614 FOR EMERGENCY LIGHT AT OVERHEAD LEFT OVERWING EXIT SIGN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

ORD - EMERGENCY LIGHT AT RIGHT NUMBER TWO DOOR OVERWING EXIT INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT RIGHT NUMBER TWO DOOR OVERWING EXIT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS)

SFO - EMERGENCY LIGHT AT SEAT 36D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 36D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT)

SFO - EMERGENCY LIGHT AT SEAT 34D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 34D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CLAMP — LOOSE (VALVE)

BOS - INFLIGHT T96/14APR - LEFT ENGINE OVERHEAT INDICATION ILLUMINATED DURING CLIMB. RETURNED TO BOS AND LANDED WITHOUT INCIDENT. AIRCRAFT TAKEN OUT OF SERVICE. FOUND PRECOOLER CLAMPS LOOSE AND EVIDENCE OF AIR LEAKAGE AT PT6 VALVE. REPLACED PT6 VALVE DUCT AND TIGHTENED PRECOOLER CLAMPS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

TPA - EMERGENCY LIGHTS FROM SEAT ROW 26 TO AFT OF CABIN INOPERATIVE. REPLACED BATTERY PACK AT RIGHT NUMBER FOUR CEILING PANEL FOR INOPERATIVE EMERGENCY LIGHTS FROM SEAT ROW 26 TO AFT OF CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LENS — MISSING (CABIN)

DFW - EMERGENCY LIGHT AT SEAT 34D HAS MISSING LENS. REPLACED EMERGENCY LIGHT LENS AT SEAT 34D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LENS — MISSING (CABIN)

DFW - EMERGENCY LIGHT AT SEAT 1E MISSING LENS. REPLACED EMERGENCY LIGHT LENS AT SEAT 1E. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

DFW - EMERGENCY LIGHT AT SEAT 13D INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 13D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

DFW - EMERGENCY LIGHT AT SEAT 34D INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 34D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

DFW - EMERGENCY LIGHT AT SEAT 22D INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 22D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LENS — MISSING (CABIN)

DFW - EMERGENCY LIGHT AT SEAT 11D MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 11D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

DFW - EMERGENCY LIGHT AT SEAT 1E INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 1E. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

LAX - EMERGENCY LIGHTS ON RIGHT HAND SIDE FROM ROW 25 TO 36 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS ON RIGHT HAND SIDE FROM ROW 25 TO 36. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: IDG — LEAKING (RT ENGINE)

LAX - RIGHT GENERATOR DRIVE LIGHT AND EICAS MESSAGE ILLUMINATED DURING CRUISE. DISCONNECTED IDG. REPLACED RIGHT HAND IDG. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: IDG — LOW (RT ENGINE)

KOA - RIGHT GENERATOR DRIVE LIGHT AND EICAS MESSAGE ILLUMINATED. DISCONNECTED RIGHT GENERATOR DRIVE. SERVICED ENGINE IDG OIL TO FULL CHECKED FOR LEAKS. NONE FOUND. RAN ENGINE, NO LEAKS NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: COMPUTER — INOPERATIVE (FLT MANAGE)

INFLIGHT RIGHT FLIGHT MANAGEMENT COMPUTER FAIL LIGHT ILLUMINATED. LEFT FLIGHT MANAGEMENT COMPUTER KEYS FROZEN. LANDED LAX WITHOUT INCIDENT. REPLACED RIGHT FLIGHT MANAGEMENT COMPUTER AND PLACARD LEFT FLIGHT MANAGEMENT COMPUTER. SYSTEM GROUND CHECKED NORMAL OPERATION. *S/D* REPLACED LEFT FLIGHT MANAGEMENT COMPUTER. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

SFO - RIGHT HAND FUSELAGE OVERWING FORWARD EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK AT M10954 FOR RIGHT HAND OVERWING FORWARD EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT)

SFO EMERGENCY EXIT LIGHT AT SEAT 20D INOPERATIVE. FOUND LOOSE SIDE WALL CONNECTOR AT SEAT 20D. SECURED LOOSE CONNECTOR FOR EMERGENCY EXIT LIGHT AT SEAT 20D. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED)