N177AN

Part: FRAME — CRACKED (FUSELAGE) · airframe 58,822 hrs · 16,333 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED FRAME AT BS 1380 BETWEEN S23L TO S26L. REPLACED FRAME PER SRM 51-40-02.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,822 hrs · 16,333 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON L4 DOOR CUT OUT LOWER SILL ANGLE AT BS 1640. REPLACED ANGLE PER SRM 51-40-02. SUPPLEMENT TO CHANGE SECTION 7 CORROSION LEVEL TO REFLECT 2.

Part: STIFFENER — CORRODED (R4 DOOR SILL) · airframe 58,822 hrs · 16,333 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON R4 DOOR CUT OUT LOWER SILL STIFFENER BETWEEN BS 1320 AND BS 1322.

Part: STIFFENER — CORRODED (R4 DOOR SILL) · airframe 58,822 hrs · 16,333 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON R4 DOOR CUT OUT LOWER SILL STIFFENER BETWEEN BS 1348 AND BS 1350.

Part: STIFFENER — CORRODED (L1 DOOR FRAME) · airframe 58,822 hrs · 16,333 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON L1 DOOR CUT OUT LOWER SILL STIFFENER BETWEEN BS 333.45 AND BS 334.47. REPLACED STIFFENER PER SRM 51-40-02.

Part: STIFFENER — CORRODED (L1 DOOR SILL) · airframe 58,822 hrs · 16,333 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON L1 DOOR CUT OUT LOWER SILL STIFFENER BETWEEN BS 353 AND BS 354. REPLACED STIFFENER PER SRM 51-40-02.

Part: STIFFENER — CORRODED (L1 DOOR SILL) · airframe 58,822 hrs · 16,333 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON L1 DOOR CUT OUT LOWER SILL STIFFENER BETWEEN BS 346 AND BS 347. REPLACED STIFFENER PER SRM 51-40-02.

Part: STIFFENER — CORRODED (L1 DOOR SILL) · airframe 58,822 hrs · 16,333 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON L1 DOOR CUT OUT LOWER SILL STIFFENER BETWEEN BS 374.5 AND BS 377.7. REPLACED STIFFENER PER SRM 51-40-02.

Part: STIFFENER — CORRODED (L1 DOOR SILL) · airframe 58,822 hrs · 16,333 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON L1 DOOR CUT OUT LOWER SILL STIFFENER BETWEEN BS 363 AND BS 364. REPLACED STIFFENER PER SRM 51-40-02.

Part: FITTING — CORRODED (BS 1640) · airframe 58,822 hrs · 16,333 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON MAIN CABIN FLOOR LEFT HAND LAVATORY LOWER MOUNT PAD FITTING AT BS 1640 AND LBL 24. REPLACED FITTING PER SRM 51-40-02.

Part: MOUNT — CORRODED (LAVATORY) · airframe 58,822 hrs · 16,333 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON MAIN CABIN FLOOR RIGHT HAND LAVATORY LOWER MOUNT PAD FITTING AT BS 1640 AND RBL 24. REPLACED FITTING PER SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (BS 1640) · airframe 58,822 hrs · 16,333 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FLOOR SUPPORT AT BS 1640 AND RBL 24. REPLACED FLOOR SUPPORT PER SRM 51-40-02.

Part: MOUNT — CORRODED (GALLEY) · corrosion level 2 · airframe 58,822 hrs · 16,333 cycles

AIRCRAFT IN BASE VISIT: CORROSION, L=1.1", W=.6", D=0.045" ON AFT GALLEY MOUNT FITTING. REMOVED AND REPLACED GALLEY MOUNT FITTING IAW SRM 51-40-02.

Part: BATTERY PACK — NO TEST (EMEGENCY LIGHT) · airframe 58,234 hrs · 16,183 cycles

AIRCRAFT WAS NOT GROUNDED: SEAT MOUNTED EMERGENCY LIGHTS VERY DIM BETWEEN 19D AND 26D. MAINTENANCE REPLACED BATTERY PACK M10953 PER MM 33-51-07.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 57,727 hrs · 16,049 cycles

AIRCRAFT NOT GROUNDED: MAINTENANCE REPORTS R4 DOOR EXTERIOR SLIDE LIGHT IS INOPERATIVE. RELAMPED R4 DOOR EXTERIOR SLIDE LIGHT ASSY IAW AMM 33-51-06, OPS CHECKS NORMAL.

Part: SIGNAL COND UNIT — INACCURATE (VIBE MONITOR) · airframe 57,354 hrs · 15,947 cycles

AIRCRAFT WAS GROUNDED: PILOT REPORTS NR 1 ENGINE VIB IN YELLOW IN CRUISE. PERFORMED QRH, WITH AUTO THROTTLE OFF BOTH SIDES INCREASED WHEN THRUST WAS INCREASED. LEFT SIDE LEVEL 2.8 RIGHT SIDE 2.4. MAINTENANCE REMOVED AND REPLACED THE LT AND RT AVM SIGNAL CONDITIONERS IAW AMM 77-31-03. OPS CHECK NORMAL. SEE SDR AALA201905099008.

Part: FAN — OUT OF ADJUST (CABIN) · airframe 57,354 hrs · 15,947 cycles

AIRCRAFT WAS GROUNDED: PILOT REPORTS AT TOP OF CLIMB, EAI WAS TURNED OFF, DEVELOPED A STRONG ELEC SMELL. RIGHT CIRC FAN WAS TURNED OFF AND SMELL WENT AWAY. MAINTENANCE ACCOMPLISHED RT RECIRC FAN ADJ/TEST IAW AMM 21-25-00-5. OPS CHECKS GOOD.

Part: SIGNAL COND UNIT — INACCURATE (VIBE MONITOR) · airframe 57,354 hrs · 15,947 cycles

AIRCRAFT WAS GROUNDED: PILOT REPORTS NO1 ENGINE VIB IN YELLOW IN CRUISE. PERFORMED QRH, WITH AUTO THROTTLE OFF BOTH SIDES INCREASED WHEN THRUST WAS INCREASED. LEFT SIDE LEVEL 2.8 RIGHT SIDE 2.4. MAINTENANCE REMOVED AND REPLACED THE LT AND RT AVM SIGNAL CONDITIONERS IAW AMM 77-31-03. OPS CHECK NORMAL. SEE SDR AALA201905139008.

Part: CONNECTOR — OUT OF POSITION (CABIN) · airframe 56,578 hrs · 15,727 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY LIGHT WAS INOPERABLE AT SEAT 32DEF. MAINTENANCE REPOSITIONED LIGHT ASSEMBLY CONNECTOR, EMERGENCY LIGHT SEAT 32DEF AND PERFORMED SATISFACTORY OPERATIONAL CHECK PER AMM 33-51-00.

Part: ENGINE — MALFUNCTIONED (RIGHT) · airframe 56,363 hrs · 15,656 cycles

RIGHT ENGINE WOULD NOT SHUTDOWN WITH FUEL CUTOFF SWITCH, PULLED THE FIRE HANDLE TO SHUT DOWN THE ENGINE. THE AIRCRAFT WAS GROUNDED. MAINTENANCE CHECKED THE POWER AT CONNECTOR D1398P PIN 7 IAW WDM 71-51-22 28 AND CHECKED CONTINUITY FOR S10138 PIN 5 AND 6, BOTH CHECKED GOOD. ACCOMPLISHED A RIGHT ENGINE OPS RUN IAW AMM 71-00-00, AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: BATTERY — DEFECTIVE (EMERGENCY LIGHTS) · airframe 53,451 hrs · 14,865 cycles

SEAT MOUNTED EMERGENCY LIGHTS FROM ROWS 18 TO 25D VERY DIM. MAINTNENANCE TROUBLESHOT AND FOUND THE AFT BATTERY DEFECTIVE AND REPLACED IAW MM 33-51-07 AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: COVER — DETACHED (L4 DOOR) · airframe 53,370 hrs · 14,841 cycles

L4 DOOR ARMED AND DISARMED PANEL FELL OFF. MAINTENANCE ATTACHED THE ARM, DISARM PANEL AND PERFORMED SATISFACTORY OPS CHECK.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 52,530 hrs · 14,614 cycles

AIRCRAFT WAS GROUNDED. SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHTS IN THE FIRST CLASS AND EMERGENCY EXIT SIGNS BY THE L1 AND R1 DOORS ARE INOPERATIVE. REMOVED AND REPLACED BATTERY PACK AND CONTROL MODULE (AALA20170919005) AT M10798 PER AMM 33-51-07. OPERATIONAL CHECK GOOD.

Part: CONTROL MODULE — INOPERATIVE (CABIN) · airframe 52,530 hrs · 14,614 cycles

AIRCRAFT WAS GROUNDED. SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHTS IN THE FIRST CLASS AND EMERGENCY EXIT SIGNS BY THE L1 AND R1 DOORS ARE INOPERATIVE. REMOVED AND REPLACED BATTERY PACK (AALA20170919004) AND CONTROL MODULE AT M10798 PER AMM 33-51-07. OPERATIONAL CHECK GOOD.

Part: SIGN — MISSING (EMERGENCY LIGHTS) · airframe 52,506 hrs · 14,607 cycles

EMERGENCY EXIT SIGN AT THE R3 DOOR WAS MISSING. REPLACED THE SIGN ASSEMBLY IAW SWPM 20-30-12. OPERATIONAL CHECKED GOOD. AIRCRAFT WAS GROUNDED.

Part: LENS — MISSING (EXIT SIGN) · airframe 52,363 hrs · 14,575 cycles

AIRCRAFT WAS NOT GROUNDED. LEFT AFT DOOR EMERGENCY EXIT SIGN MISSING. REPLACED LEFT AFT DOOR EMERGENCY EXIT LIGHT ASSEMBLY COVER IAW AMM 33 51 01 013 002.

Part: LENS — DETACHED (EMERGENCY LIGHT) · airframe 52,345 hrs · 14,572 cycles

EMERGENCY EXIT SIGN IN THE FIRST CLASS SECTION HAS A DETACHED LENS. INSTALLED THE LENS. OPS CHECKED GOOD.

Part: LENS — MISSING (CABIN) · airframe 52,213 hrs · 14,534 cycles

AIRCRAFT WAS NOT GROUNDED. SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT AT SEAT 3E HAS A MISSING LENS COVER. REPLACED LENS COVER PER AMM 33-51-11. OPERATIONAL CHECK GOOD. (CLOSED)

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 51,766 hrs · 14,407 cycles

EMERGENCY EXIT SIGN BETWEEN THE L2 & R2 DOORS HAS A LOOSE LENS. SECURED THE LENS. OPS CHECKED GOOD.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 51,740 hrs · 14,398 cycles

EMERGENCY EXIT SIGN BETWEEN L2 AND R2 DOORS HAS A LOOSE LENS COVER. SECURED THE LENS COVER. OPS CHECKED GOOD.

Part: STRAP — LOOSE (L4 DOOR SLIDE) · airframe 51,398 hrs · 14,315 cycles

L4 DOOR EMERGENCY EVACUATION SLIDE COVER STRAP IS LOOSE. SECURED THE STRAP. OPS CHECKED GOOD.

Part: STRAP — DIRTY (R1 DOOR SLIDE) · airframe 51,398 hrs · 14,315 cycles

R1 DOOR EMERGENCY EVACUATION SLIDE ASSEMBLY ATTACH STRAP IS FULL OF DEBRIS. REMOVED DEBRIS. OPS CHECKED GOOD.

Part: LENS — DETACHED (EXIT SIGN) · airframe 51,370 hrs · 14,306 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY EXIT SIGN OVERHEAD FORWARD BETWEEN L1 AND R1 DOORS HAS A DETACHED LENS COVER. REINSTALLED LENS COVER. OPERATIONAL CHECK GOOD.

Part: LENS — DETACHED (EXIT SIGN) · airframe 51,328 hrs · 14,293 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY EXIT SIGN OUTSIDE THE COCKPIT DOOR ON THE CEILING HAS A DETACHED LENS COVER. INSTALLED LENS COVER. OPERATIONAL CHECK GOOD.

Part: LENS — DETACHED (CABIN) · airframe 51,321 hrs · 14,292 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY EXIT SIGN OUTSIDE THE COCKPIT DOOR ON THE CEILING HAS A DETACHED LENS COVER. INSTALLED LENS COVER. OPERATIONAL CHECK GOOD.

Part: BATTERY — FAILED (CABIN) · airframe 51,185 hrs · 14,257 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY EXIT LIGHTS AT R4/L4 DOORS AND SEAT MOUNTED ESCAPE PATH LIGHTS AT SEATS 26D-36D ARE VERY DIM. REMOVED AND REPLACED BATTERY PACK AT L4 DOOR IAW AMM 33-51-07. OPERATIONAL CHECK GOOD.

Part: LENS — DETACHED (CABIN) · airframe 50,710 hrs · 14,124 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY EXIT LIGHT BY L4 DOOR HAS A DETACHED LENS COVER. SECURED LENS COVER. OPERATIONAL CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 50,674 hrs · 14,113 cycles

AIRCRAFT WAS NOT GROUNDED. SEAT MOUNTED ESCAPE PATH LIGHTS AT SEATS 16DEF TO 25DEF ARE VERY DIM. REMOVED AND REPLACED BATTERY PACK IAW AMM 33-51-07. OPERATIONAL CHECK GOOD.

Part: WIRE HARNESS — DAMAGED (TE FLAP) · airframe 50,144 hrs · 13,967 cycles

AIRCRAFT WAS GROUNDED. EMERGENCY DECLARED. DURING APPROACH WHEN FLAPS 5 DEGREES SELECTED RECEIVED EICAS MESSAGE "TE FLAP ASYM" AND FLAPS STOPPED AT 2 DEGREES. FOUND DAMAGE TO #7 SKEW HARNESS AT CONNECTOR D8970. REPAIRED HARNESS IAW AMM 20-10-13 AND ACCOMPLISHED FSAM BIT CHECK AND SKEW SYSTEM TEST IAW AMM 27-51-00 AND 27-59-00. SYSTEM CHECKS NORMAL.

Part: MODULE — FAULTY (FLAP SYSTEM) · airframe 50,048 hrs · 13,945 cycles

DURING CLIMB RECIEVED, AN EICAS TRAILING EDGE FLAP ASYMMETRY INDICATION. EMERGENCY DECLARED. LANDING UNEVENTFUL. AIRCRAFT WAS GROUNDED. MAINTENANCE REMOVED AND REPLACED FLAP/SLAT ACCESSORY MODULE IAW 27-59-11-024-001-424-006. ACCOMPLISHED TRAILING EDGE FLAP SYSTEM OPS TESTED IAW AMM 27-59-00-715-059. SYSTEM CHECKED NORMAL.

Part: DECK PLATE — CORRODED (BS 1715) · corrosion level 2 · airframe 49,879 hrs · 13,906 cycles

AFT DECK PLATE UPPER SURFACE IS CORRODED AT BS 1715 AND RBL 48. REPAIRED THE DECK PLATE IAW SRM 53-60-51-2R-2.

Part: GCU — FAULTED (LEFT) · airframe 49,217 hrs · 13,742 cycles

DURING CRUISE THE LEFT AC BUS OFF LIGHT ILLUMINATED 5 HOURS INTO FLIGHT. QRH RESTORED SYSTEM. LEFT AC BUS OFF LIGHT ILLUMINATED AGAIN 7 HOURS INTO FLIGHT. LEFT GENERATOR RESET THE FAILED. LEFT BUS NOT RESTOREABLE. AIRCRAFT GROUNDED. EMERGENCY DECLARED. LANDING UNEVENTFUL. MAINTENANCE ACCOMPLISHED FIM 24-20-00-810-802. INSPECTED WIRING WITH NO DEFECTS FOUND. REMOVED AND REPLACED LEFT GENERATOR CONTROL UNIT IAW AMM 24-22-02. ACCOMPLISHED ENGINE RUN IAW AMM 71-00-00-5. SYSTEM CHECKS NORMAL.

Part: PACKING — LEAKING (HYD SYSTEM) · airframe 49,159 hrs · 13,727 cycles

DURING CRUISE CREW OBSERVED INDICATION OF RIGHT HYDRAULIC SYSTEM FLUID QUANTITY LOSS. EMERGENCY DECLARED. LANDING UNEVENTFUL. AIRCRAFT GROUNDED. MAINTENANCE FOUND THE PRESSURE SWITCH PACKING ON THE FILTER MODULE IN THE RIGHT PYLON LEAKING. REMOVED AND REPLACED THE PACKING AND ACCOMPLISHED LEAK CHECK. SYSTEM CHECKS NORMAL.

Part: TRANSMITTER — FAULTY (RT ENGINE) · airframe 48,762 hrs · 13,647 cycles

AIRCRAFT WAS GROUNDED. DURING TAKEOFF CREW NOTED EPR SPLIT WITH RT ENGINE NOT RESPONDING ACCOMPANIED BY A YAW TO THE RT. TAKEOFF ABORTED AT APPROXIMATELY 20 KNOTS. MAINTENANCE R & R THE RT ENGINE EPR TRANSMITTER IAW AMM 77-11-01 AND ACCOMPLISHED ENGINE RUN IAW AMM 71-00-00. OPS CHECK NORMAL.

Part: IDG — UNDERSERVICED (LT ENGINE) · airframe 47,837 hrs · 13,414 cycles

LEFT GEN DRIVE ILLUMINATED IN TAKEOFF ROLL, IN CLIMB 8,000 FT. WENT OUT BUT RETURNED AGAIN, 10,000 FT. LIGHT OUT BEFORE LANDING. THE FLIGHT DECLARED AN EMER & RETURNED WITHOUT FURTHER INCIDENT. PERFORMED FIM 24-20-00-810-802 & FOUND IDG UNDERSERVICED. PULLED SCAVENGE FILTER & INSPECTED FOR CONTAMINATION, NO DEBRIS FOUND. REPLACED FILTER IAW 24-11-02, SERVICED TO FULL. OPERATIONS CHECKED NORMAL, NO LEAKS OR FAULTS NOTED. THE ACFT WAS GNDED.

Part: LENS — CRACKED (CABIN) · airframe 46,592 hrs · 13,137 cycles

EMERGENCY IDENTIFIERS CRACKED AT R1 DOOR & R4 DOOR. REPLACED EXIT IDENTIFIERS AT R1 DOOR & R4 DOOR. OPERATION NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 45,419 hrs · 12,891 cycles

SEAT MOUNTED EMER LIGHTS IN FIRST CLASS ARE INOPERATIVE. R & R POWER SUPPLY & BATTERY. PERFORMED OPERATIONAL CHECK IAW AMM 33-51-00. SYS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 45,419 hrs · 12,891 cycles

SEAT MOUNTED EMER LIGHTS AT ROWS 16 - 25 ARE INOPERATIVE. R & R POWER SUPPLY & BATTERY. PERFORMED OPERATIONAL CHECK IAW AMM 33-51-00. SYS CHECKED NORMAL.

Part: MODULE — FAULTY (CABIN) · airframe 45,419 hrs · 12,891 cycles

SEAT MOUNTED EMER LIGHTS IN FIRST CLASS INOPERATIVE. R & R BATTERY MODULE FOR FIRST CLASS SEAT MOUNTED EMER LIGHTS. PERFORMED OPERATIONAL CHECK IAW AMM 33-51-07. SYS CHECKED NORMAL.

Part: GOVERNOR — FAULTY (FUEL FLOW) · airframe 44,575 hrs · 12,701 cycles

AFTER TAKEOFF LT ENG WAS STUCK AT TAKEOFF POWER & WOULDN’T RESPOND TO THROTTLE MOVEMENT. LT ENG EGT 792 & EPR STUCK AT 1.60. CREW CONDUCTED INFLIGHT SHUTDOWN OF LT ENG IAW QRH. THE SINGLE ENG TIME WAS 12 TO 15 MINUTES. EMERGENCY WAS DECLARED & LANDED WITHOUT INCIDENT. LT FUEL FLOW GOVERNOR WAS REPLACED IAW SIC 73-94-01 & ENG RUN WAS ACCOMPLISHED IAW SIC 71-92-01 WITH GOOD OPERATIONAL CHECK.

Part: SHIM — MIGRATED (LT MLG) · airframe 44,458 hrs · 12,677 cycles

SHIM MIGRATION AT LT MAIN GEAR FWD TRUNNION MOUNT CASTING, OTBD SIDE, FWD END. REPAIRED SHIM FOLLOWING INSTRUCTIONS OUTLINED IN EA 57-039202 DATED 3 31 2015.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 44,408 hrs · 12,659 cycles

EXTERIOR MOUNTED SLIDE ILLUMINATION LIGHT ADJACENT TO LT AFT PAX DOOR INOPERATIVE. RELAMPED EXTERIOR MOUNTED SLIDE ILLUMINATION LIGHT IAW AMM 33-51-06. SYS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 43,466 hrs · 12,455 cycles

EXTERIOR EMER EXIT LIGHT AT R4 DOOR IS INOPERATIVE. R & R LAMP. SYS CHECKED NORMAL.

Part: COVER — MISSING (EXIT SIGN) · airframe 42,820 hrs · 12,298 cycles

EMERGENCY LIGHT EXIT MARKER AT AFT RT DOOR MISSING COVER. REPLACED EMER EXIT SIGN IDENTIFIER. OPERATIONS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 41,662 hrs · 12,026 cycles

AFT LT DOOR EXTERIOR EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED BATTERY PACK. OPERATIONS CHECKED NORMAL.

Part: CONTROL PANEL — FAULTY (WEATHER RADAR) · airframe 40,279 hrs · 11,701 cycles

SJU CREW REPORTED WEATHER SYSTEM STATUS MESSAGE & WEATHER RADAR FAIL. FLIGHT LANDED SJU WITHOUT INCIDENT. REPLACED RADAR CONTROL PANEL, SYSTEM GND CHECKED NORMAL OPERATION CLOSED.

Part: DOUBLER — GOUGED (R4 DOOR) · airframe 39,362 hrs · 11,497 cycles

RT NR 4 DOOR INNER SKIN STRAP DOUBLER GOUGED THROUGH. ACCOMPLISHED DOUBLER REPAIR IAW EA COMP-52-031312.

Part: SKIN — CRACKED (LT WING) · airframe 39,360 hrs · 11,496 cycles

LT WING LE SKIN CRACKED AT FSS 438. REPAIRED LT WING LE SKIN AT FSS 438 IAW AARD 57-41-01.

Part: STRUCTURE — DAMAGED (RUDDER) · airframe 39,360 hrs · 11,496 cycles

RUDDER RT SIDE BETWEEN STATIONS 97 & 131 DAMAGED. ACCOMPLISHED BONDED REPAIR AT RUDDER RT SIDE FROM STATIONS 97 & 131 IAW SRM 51-70-04-0G.

Part: FRAME — DENTED (FUSELAGE) · airframe 39,360 hrs · 11,496 cycles

AFT CARGO COMPARTMENT FS FRAME IS DENTED AT STATION 1440 BETWEEN STRINGERS 25 & 26 LT. CUT OUT DAMAGE & INSTALLED J ANGLE REPAIR IAW SRM 53-00-27-2R-5 FIGURE 201, DETAIL I.

Part: DECK PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,481 hrs · 10,414 cycles

CORROSION ON AFT DECK PLATE STATIONS 1710 TO 1720 AND LEFT AND RIGHT BUTTLINES 52. REMOVED AND INSTALLED NEW AFT DECK PLATE PER BOEING DRAWING 146N8722.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 34,481 hrs · 10,414 cycles

CORROSION ON FLOOR SUPPORT, 39 INCHES RIGHT OF BUTTLINE 0, STATIONS 318 TO 324. REMOVED FLOOR SUPPORT AND INSTALLED NEW SUPPORT PER AARD 51-00-05-1.

Part: SHUTOFF VALVE — LOOSE (RT ENGINE) · airframe 33,662 hrs · 10,242 cycles

MIA INFLIGHT PUJ-JFK. CREW REPORTED RIGHT ENGINE BLEED LIGHT ILLUMUNATED ON TAKE OFF. FLIGHT DIVERTED MIA LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. TIGHTENED PRESSURE REGULATING SHUT-OFF VALVE AND SENSE LINE THAT WERE LOOSE. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: TRANSCEIVER — INOPERATIVE (WEATHER RADAR) · airframe 32,473 hrs · 10,009 cycles

JFK - CREW REPORTED WEATHER RADAR SYSTEM FAILED ON BOTH CAPTAIN AND FIRST OFFICERS SIDE. FLIGHT RETURNED JFK LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED WEATHER RADAR TRANSCEIVER. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 32,252 hrs · 9,973 cycles

AISLE EMERGENCY LIGHTS FROM ROWS 16 TO 36 INOPERATIVE. REPLACED BATTERY PACK AT CEILING LIGHT PANEL. OPS CHECK NORMAL.

Part: PLUG — MISSING (RT ENGINE) · airframe 31,597 hrs · 9,863 cycles

SNN - INFLIGHT-JFK-MAN. CREW REPORTED RIGHT ENGINE LOSS OF OIL PRESSURE AND QUANTITY. RIGHT ENGINE SHUTDOWN (SINGLE ENGINE TIME 80 MINS). EMERGENCY DECLARED FLIGHT DIVERTED SNN LANDED WITHOUT INCIDENT. FOUND GEARBOX CORE PLUG IN COWLING. RE-SECURED PLUG. REPLENISHED OIL SYSTEM. RAN ENGINE AND CHECKED FILTERS FOR DEBRIS. NONE FOUND. AIRCRAFT FERRIED TO JFK FOR PERMANENT REPAIR. REPLACED RIGHT ENGINE AT JFK ON 07/09/11. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: CONNECTOR — LOOSE (CABIN) · airframe 29,752 hrs · 9,484 cycles

EMERGENCY LIGHT AT SEAT 32 INOPERATIVE. RE-SECURED LOOSE CONNECTORS. OPS CHECK NORMAL.

Part: CONNECTOR — LOOSE (CABIN) · airframe 29,752 hrs · 9,484 cycles

EMERGENCY LIGHT AT SEAT 26 INOPERATIVE. RE-SECURED LOOSE CONNECTORS. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,606 hrs · 9,034 cycles

LEFT AFT EMERGENCY LIGHTS INOPERATIVE LAST TWO LIGHTS. REPLACED LAMP FOR LEFT AFT EMERGENCY LIGHTS. OPS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 26,158 hrs · 8,708 cycles

EMERGENCY AISLE AND EXIT LIGHTS IN FIRST CLASS AT DOOR INOPERATIVE. REPLACED BATTERY PACK.

Part: CONNECTOR — LOOSE (CABIN) · airframe 25,528 hrs · 8,552 cycles

EMERGENCY LIGHT AT SEAT ROW 1EF INOPERATIVE. FOUND LOOSE CONNECTOR. RE-SEATED CONNECTOR AT SEAT ROW 1EF.

Part: FMC — FAILED (COCKPIT) · airframe 24,751 hrs · 8,345 cycles

JFK - CREW REPORTED DUEL FLIGHT MANAGEMENT COMPUTER FAILURE. EMERGENCY DECLARED, LANDED JFK WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED RIGHT FLIGHT MANAGEMENT COMPUTER AND CROSS LOADED SOFTWARE AS PER MM34-61-00-2. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: HYDRAULIC LINE — LEAKING (NLG) · airframe 20,638 hrs

TUL INFLIGHT T1745/25APR ORD TO LAX - LEFT HYDRAULIC SYSTEM LOSS IN FLIGHT. DIVERTED TO TUL AND LANDED WITHOUT INCIDENT. FOUND NOSE GEAR DOOR ACTUATOR HYDRAULIC HOSE LEAKING. REPLACED NOSE GEAR DOOR ACTUATOR HYDRAULIC HOSE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT)

DFW - EMERGENCY LIGHT AT LEFT NUMBER FOUR DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT LEFT NUMBER FOUR DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHT)

DFW - EMERGENCY LIGHT PLACARD AT RIGHT FORWARD DOOR INOPERATIVE. REPLACED PLACARD FOR EMERGENCY LIGHT AT RIGHT FORWARD DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SHROUD — DAMAGED (EMERGENCY LIGHTS)

DFW - EMERGENCY LIGHT AT SEAT 23D HAS DAMAGED SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 23D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: FAN — INOPERATIVE (AIR CONDITIONING)

ORD INFLIGHT - FLIGHT ATTENDANT REPORTED ELECTRICAL SMELL/HAZE AFTER TAKEOFF. RETURNED TO ORD AND LANDED WITHOUT INCIDENT. DURING TAXI IN EQUIPMENT COOLING OVERHEAT LIGHT ILLUMINATED. REPLACED EQUIPMENT COOLING FAN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT)

DFW - EXTERNAL EMERGENCY LIGHT AT LEFT NUMBER FOUR DOOR INOPERATIVE. RELAMPED EXTERNAL EMERGENCY LIGHT AT LEFT NUMBER FOUR DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS)

DFW - EMERGENCY SLIDE LIGHT AT RIGHT NR 4 DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY SLIDE LIGHT AT RIGHT NR 4 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — INOPERATIVE (EMERGENCY LIGHT)

JFK - SEAT MOUNTED EMERGENCY LIGHTS AT SEAT 2B INOPERATIVE. FOUND SIDEWALL CONNECTOR LOOSE AT SEAT 2B. RECONNECTED CONNECTOR FOR SEAT MOUNTED EMERGENCY LIGHTS AT SEAT 2B. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

JFK - FORWARD CABIN FLOOR PROXIMITY EGRESS LIGHTS INOPERATIVE. REPLACED BATTERY PACK AND CHARGER FOR FORWARD CABIN FLOOR PROXIMITY EGRESS LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT)

ORD - EMERGENCY LIGHT AT SEAT 10D INOPERATIVE. SECURED LOOSE CONNECTOR FOR EMERGENCY LIGHT AT SEAT 10D. SYSTEM GROUND CHECKED NORMAL OPERATION.