N199AN

Part: EEC — FAULTY (LT ENGINE) · airframe 57,749 hrs · 16,435 cycles

AIRCRAFT WAS GROUNDED: PILOT REPORTS AS THROTTLES WERE ADVANCED FOR TAKE OFF AND N1/EPR BUTTON ENGAGED, THE LEFT EEC AND LEFT ENGINE LIMITER ILLUMINATED/ N1/EPR WOULD NOT ENGAGE. MAINTENANCE REMOVED AND REPLACED LEFT ENGINE EEC SUPERVISORY AND LIMITER IAW AMM 73-21-07. RAN UP ENGINE, ALL INDICATIONS NORMAL. INTERROGATED THE EEC IAW AMM 73-21-00, NO FAULTS DISPLAYED, APPROVED FOR SERVICE.

Part: MECHANISM — LACK OF LUBE (L1 DOOR) · airframe 57,492 hrs · 16,359 cycles

AIRCRAFT NOT GROUNDED: MAINTENANCE REPORTS L1 PASSENGER DOOR OUT OF SEQUENCE. - HARD TO OPEN. MAINTENANCE OPERATED L1 DOOR AND LUBED HANDLE MECHANISM IAW AMM 52-11-01. DOOR OPERATES NORMALLY.

Part: FLASHLIGHT — INOPERATIVE (FWD CABIN) · airframe 57,256 hrs · 16,287 cycles

AIRCRAFT WAS NOT GROUNDED: FLASHLIGHT AT 2L WAS INOPERABLE. MAINTENANCE REPLACED FLASHLIGHT PER AMM 25-64-00.

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 57,142 hrs · 16,252 cycles

AIRCRAFT NOT GROUNDED: PILOT REPORTS SLIDE LIGHT AT L1 DOOR REPORTED INOPERATIVE, MAINTENANCE REPLACED L1 LIGHT ANNUNCIATOR ASSEMBLY IAW AMM 33-16-02. OPS CHECK OK.

Part: SKIN — CRACKED (TE FLAP) · airframe 57,045 hrs · 16,222 cycles

AIRCRAFT IN BASE MAINTENANCE: LEFT WING INBOARD TRAILING EDGE FLAP LEADING EDGE SURFACE GROOVED AND CRACKED ON THE OUTBOARD END. REPAIRED FLAP PER SRM 57-52-01 R2.

Part: SPLICE STRAP — CORRODED (VERTICAL STAB) · corrosion level 2 · airframe 57,045 hrs · 16,222 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON VERTICAL STABILIZER TIP UPPER AND LOWER SPLICE STRAPS. REPLACED SPLICE STRAPS PER SRM 51-40-02-0G.

Part: FLOOR SUPPORT — CRACKED (BS 460) · airframe 57,045 hrs · 16,222 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED FLOOR SUPPORT AT FR 460, RBL -30. REPLACED FLOOR SUPPORT PER AARD 51-00-05.

Part: STRAP — CRACKED (BS 1640) · airframe 57,045 hrs · 16,222 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED STRAP AT FR 1640, STRINGER 14L. REPLACED STRAP PER BOEING DRAWING #1468711 AND AARD 51-00-05-1.

Part: FLOOR SUPPORT — CRACKED (BS 1420-1440) · airframe 57,045 hrs · 16,222 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED FLOOR SUPPORT (INTERCOSTAL) AT FR 1420 TO FR 1440. REPLACED INTERCOSTAL PER BOEING PRINT 146N5180 AND AARD 51-00-05.

Part: FLOOR SUPPORT — CRACKED (BS 1200-1220) · airframe 57,045 hrs · 16,222 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED FLOOR SUPPORT (INTERCOSTAL) AT FR 1200 TO FR 1220. REPLACED INTERCOSTAL PER BOEING PRINT 146N5180 AND AARD 51-00-05.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,045 hrs · 16,222 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT WET AREA FLOOR DECK "Z" ANGLE BETWEEN BS 1680 AND BS 1720 AT LBL 53. REPLACED ANGLE PER 51-00-05-1.

Part: TIE DOWN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,045 hrs · 16,222 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON GALLEY TIE DOWN AT FR 1680. REPLACED GALLEY TIE DOWN PER 51-00-05.

Part: MOUNT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,045 hrs · 16,222 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LAVATORY MOUNT AT FR 1640, RBL-24. REPLACED LAVATORY MOUNT PER 51-00-05.

Part: TIE DOWN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,045 hrs · 16,222 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON GALLEY TIE DOWN AT FR 1720, LBL55. REPLACED GALLEY TIE DOWN PER 51-00-05.

Part: MOUNT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,045 hrs · 16,222 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LAVATORY MOUNT AT FR 1640, RBL-54. REPLACED LAVATORY MOUNT PER 51-00-05.

Part: FITTING — CORRODED (FUSELAGE) · airframe 57,045 hrs · 16,222 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT WET AREA GALLEY TIE DOWN FITTING AT BS 1720 AND LBL 55. REPLACED TIE DOWN FITTING PER 51-00-05-1.

Part: TIE DOWN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,045 hrs · 16,222 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON GALLEY TIE DOWN AT FR 1720, RBL-53. REPLACED GALLEY TIE DOWN PER 51-00-05.

Part: TIE DOWN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,045 hrs · 16,222 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON GALLEY TIE DOWN AT FR 1720, RBL-53. REPLACED GALLEY TIE DOWN PER 51-00-05.

Part: CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,045 hrs · 16,222 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT WET AREA FLOOR DECK HAT CHANNEL BETWEEN BS 1680 AND BS 1720 AT BL 0. REPLACED HAT CHANNEL PER 51-00-05-1.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,045 hrs · 16,222 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FLOOR SUPPORT AT FR 1640. REPLACED FLOOR SUPPORT PER 51-00-05.

Part: BRACKET — CORRODED (RT HORIZ STAB) · corrosion level 2 · airframe 57,045 hrs · 16,222 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON BONDING STRAP ATTACHMENT BRACKET ON THE RIGHT HAND HORIZONTAL STABILIZER BETWEEN STATION 297 AND STATION 298. REPLACED BRACKET PER SRM 51-40-02.

Part: STRAP — CORRODED (RT ELEVATOR) · corrosion level 2 · airframe 57,045 hrs · 16,222 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT HAND ELEVATOR OUTBOARD END CAP STRAP AT STATION 318. REPLACED STRAP PER SRM 51-10-02-0G.

Part: STRAP — CORRODED (LT ELEVATOR) · corrosion level 2 · airframe 57,045 hrs · 16,222 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT HAND ELEVATOR OUTBOARD END CAP STRAP AT STATION 318. REPLACED STRAP PER SRM 51-10-02-0G.

Part: BRACKET — CORRODED (LT HORIZ STAB) · corrosion level 2 · airframe 57,045 hrs · 16,222 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON BONDING STRAP ATTACHMENT BRACKET ON THE LEFT HAND HORIZONTAL STABILIZER BETWEEN STATION 297 AND STATION 298. REPLACED BRACKET PER SRM 51-40-02.

Part: PAN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,045 hrs · 16,222 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LOWER EDGE OF THE POTABLE WATER SERVICE PAN BETWEEN BS 347 AND BS 365, BETWEEN BS S21R AND S23R. REPLACED PAN PER SRM 51-40-02.

Part: GEARBOX — STICKING (ZONE 400) · airframe 56,957 hrs · 16,199 cycles

AIRCRAFT WAS GROUNDED: PILOT REPORTS DURING TAKEOFF, A/T FAILED TO FULLY ADVANCE THRUST OF LT ENGINE 1/2 KNOB WIDTH STAGGER. MAINTENANCE REMOVED AND REPLACED UPPER CONTROL GEARBOX IAW AMM 76-11-12. ALL RIGS AND OPS CHECKS GOOD.

Part: UNKNOWN — MALFUNCTIONED (AUTOTHROTLLE SYS) · airframe 56,931 hrs · 16,193 cycles

AIRCRAFT NOT GROUNDED: PILOT REPORTS DURING TAKEOFF, UPON AUTO-THROTTLE ENGAGEMENT, A/T FAIL TO FULLY ADVANCE TO COMMAND THRUST SETTING. BOTH THROTTLES STOPPED ABOUT 0.1 BELOW EPR COMMAND BUG. MAINTENANCE ACCOMPLISHED AMM TASK 22-32-00-735-002. THRUST MANAGEMENT SYSTEM. NO FAULTS NOTED. NO 30 DAY HISTORY. ACCOMPLISHED SATISFACTORY MCDP TEST 40 AUTOLAND 22-03-00-815-843. AIRCRAFT REMAINS LAND CAT3 STATUS.

Part: SEAM — LEAKING (RT WING) · airframe 55,830 hrs · 15,881 cycles

MAINTENANCE FOUND THE RT INBD WING AT RIB 7 AND 8, WITH FUEL SEEPING FROM SEAM, INBD PYLON OUT OF LIMITS. MAINTENANCE SCRAPED AND CLEANED THEN RESEALED THE SEAM. LEAK CHECKED IAW AMM 28-11-00 REV 116.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 55,338 hrs · 15,741 cycles

ROW 33 EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE INSPECTED THE CONNECTOR AND FOUND THE EMERGENCY LIGHT AT SEAT 33D INOPERATIVE AND REPLACED THE LIGHT. MAINTENANCE ALSO PERFORMED A TEST IAW CMM 25-20-79, SATISFACTORY.

Part: FSEU — FAULTED (FLAPS) · airframe 54,884 hrs · 15,604 cycles

DURING APPROACH, THE TRAILING EDGE FLAPS DISAGREED AT ABOUT 17DEG, FLAP HANDLE AT 20DEG. ACCOMPLISHED QRH CHECKLIST. FLAP / SLAT ELECTRONIC UNIT DISPLAYED CODE 305. ACCOMPLISHED FAULT ISOLATION MANUAL 27, ALL TESTED NORMAL. OPS TESTED OK, FLAP SYSTEM NORMAL IAW MM 27-51-00.

Part: INDICATOR — UNKNOWN (L4 DOOR) · airframe 54,083 hrs · 15,383 cycles

L4 DOOR ARMED INDICATOR WILL NOT PROTRUDE WITH DOOR ARMED. ACCOMPLISHED AN OPS CHECK ON THE L4 DOOR ARMED AND DISARMED. ALL OPERATIONS CHECK ARE NORMAL IAW AMM 52-71-00. OK FOR SERVICE.

Part: BOTTLE — LOW PRESSURE (L2 DOOR SLIDE) · airframe 54,028 hrs · 15,365 cycles

L2 DOOR SLIDE BOTTLE PRESSURE IN RED BAND. AIRCRAFT WAS GROUNDED. REPLACED L2 DOOR SLIDE IAW WORK CARD 25-94-34.

Part: CONTROLLER — MALFUNCTIONED (FLOW VALVE) · airframe 53,967 hrs · 15,348 cycles

DURING FLIGHT, THE RIGHT ENGINE BLEED OFF LIGHT ILLUMINATED. AN EMERGENCY WAS DECLARED AND RETURNED TO DEPARTURE. THE AIRCRAFT WAS GROUNDED. REPLACED RIGHT REVERSE FLOW VALVE CONTROLLER IAW AMM 36-11-18.

Part: GIRT BAR — DETACHED (L4 DOOR) · airframe 53,514 hrs · 15,244 cycles

GIRT BAR DETACHED AT THE L4 DOOR. REINSTALLED THE GIRT BAR. OPS CHECKED NORMAL IAW AMM 25-66-10.

Part: HANDLE — BROKEN (L2 DOOR) · airframe 53,444 hrs · 15,226 cycles

AIRCRAFT WAS NOT GROUNDED. 1 OF THE 2L PLASTIC DOOR GRIPS BROKE OFF. REPLACED 2L DOOR ASSIST HANDLE PER AMM 52-11-02.

Part: STRAP — CRACKED (FUSELAGE) · airframe 52,419 hrs · 14,947 cycles

THE AIRCRAFT IS IN BASE MAINTENANCE. FOUND A CRACK IN STABILIZATION STRAP. INSTALLED REPAIR DOUBLER AND FILLER PER SRM 53-00-51-2R-12.

Part: WEB — CRACKED (BS 1200-1220) · airframe 52,419 hrs · 14,947 cycles

CRACKED ATTACH ANGLE FOR THE AFT CARGO WEB BETWEEN BS 1200 TO 1220, BL 0, JUST BELOW CABIN FLOOR LINE. REPLACED THE WEB IAW SRM 51-00-05-1, AND DRAWING 146N5180.

Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY) · airframe 52,305 hrs · 14,912 cycles

AIRCRAFT WAS NOT GROUNDED. LAVATORY SMOKE ALARM ACTIVATED IN LAVATORY. ACCOMPLISHED RESET OF SMOKE DETECTOR IN LAV A IAW MM 26 14 -01.

Part: BATTERY — FAULTY (EMERGENCY LIGHTS) · airframe 52,305 hrs · 14,912 cycles

SEAT MOUNTED EMERGENCY LIGHTS FROM 9D TO 15D ARE VERY DIM. REMOVED AND REPLACED BATTERY PER MM 33-51-07. ALL OPERATIONS AND INDICATIONS NOW NORMAL.

Part: POWER SUPPLY — FAULTY (EMERGENCY LIGHTS) · airframe 52,305 hrs · 14,912 cycles

SEAT MOUNTED EMERGENCY LIGHTS FROM 9D TO 15D ARE VERY DIM. REMOVED AND REPLACED THE POWER SUPPLY IAW MM 33-51-07. L OPS NORMAL.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 52,085 hrs · 14,843 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY LIGHTS AT FIRST CLASS DID NOT TURN OFF AFTER POWER SHUT DOWN. MAINTENANCE REPLACED BATTERY CHARGER (CONTROL MODULE) PER AMM 33-51-07 AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: BATTERY — DISCHARGED (CABIN) · airframe 52,085 hrs · 14,843 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY LIGHTS AT FIRST CLASS DID NOT TURN OFF AFTER POWER SHUT DOWN. MAINTENANCE REPLACED BATTERY PER AMM 33-51-07 AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 52,070 hrs · 14,838 cycles

AIRCRAFT GROUNDED. SEAT 1E EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED LIGHT ASSFEMBLY AT ROW 1E PER AMM 33-51-00.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 52,067 hrs · 14,837 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY LIGHT INOPERABLE AT ROW 4R. MAINTENANCE REPLACED EMERGENCY LIGHT PER AMM 33-51-00.

Part: LIGHT — INOPERATIVE (ROW 4) · airframe 52,067 hrs · 14,837 cycles

NO EMERGENCY LIGHT, INOP AT ROW4R, REMOVED AND REPLACED EMERGENCY LIGHT IAW AMM 33-51-00.

Part: SENSOR — FAULTY (R1 DOOR) · airframe 51,829 hrs · 14,764 cycles

THE AIRCRAFT WAS NOT GROUNDED. SLIDE GIRT BAR ENGAGE LIGHT, DOOR 1R SLIDE LIGHT WOULD NOT ILLUMINATE WHEN DOOR ARMED. REMOVED AND REPLACED THE R1 DOOR MOUNTED GIRT BAR MAGNETIC SENSORS (SWITCHES) S10216 AND S10217 PER AMM 25-66-11. OPERATIONAL CHECK GOOD. (CLOSED)

Part: BOTTLE — LOW PRESSURE (R2 DOOR SLIDE) · airframe 51,617 hrs · 14,712 cycles

L2 DOOR SLIDE BOTTLE PRESSURE NEEDLE IS IN THE RED. REMOVED AND REPLACED THE SLIDE ASSEMBLY IAW AMM 25-94-34. OPS CHECKED GOOD. AIRCRAFT WAS GROUNDED.

Part: LENS — DAMAGED (EXIT SIGN) · airframe 51,461 hrs · 14,669 cycles

AIRCRAFT WAS NOT GROUNDED. EXIT SIGN LENS AT DOOR 4L BROKEN. REPLACED EXIT SIGN LENS IAW AMM 33-51-01.

Part: BATTERY — CORRODED (MEGAPHONE) · airframe 51,333 hrs · 14,640 cycles

AIRCRAFT WAS NOT GROUNDED. AFT CABIN MEGAPHONE BATTERIES APPEAR TO BE CORRODED. REMOVED AND REPLACED MEGAPHONE BATTERIES PER AMM 25-64-00. OPERATIONAL CHECK GOOD.

Part: MODULE — NOT SEATED (EMERGENCY LIGHT) · airframe 50,867 hrs · 14,515 cycles

SEAT MOUNTED EMERGENCY LIGHT AT SEAT 30D IS INOPERATIVE. RESEATED LIGHT MODULE IAW AMM 33-51-11. OPS CHECKED GOOD.

Part: LENS — DETACHED (EXIT SIGN) · airframe 50,519 hrs · 14,421 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY EXIT SIGN BY THE L1 DOOR HAS A DETACHED LENS COVER. REINSTALLED LENS COVER IAW AMM 33-51-00. OPERATIONAL CHECK GOOD.

Part: COVER — LOOSE (R2 DOOR) · airframe 50,424 hrs · 14,393 cycles

R2 DOOR EMERGENCY EVACUATION SLIDE COVER IS LOOSE. TIGHTENED COVER IAW AMM 52-11-02. OPERATIONAL CHECKED GOOD.

Part: BULB — UNSECURE (EMERGENCY LIGHT) · airframe 50,377 hrs · 14,385 cycles

EMERGENCY EXIT EXTERIOR SLIDE LIGHT AT L4 DOOR IS INOPERATIVE. SECURED THE BULB IAW AMM 33-51-06. OPERATIONAL CHECKED GOOD. AIRCRAFT WAS GROUNDED.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 50,310 hrs · 14,373 cycles

EMERGENCY EXIT LIGHT BY THE L2 DOOR HAS A MISSING LENS. INSTALLED A NEW LENS IAW AMM 25-60-00. OPERATIONAL CHECKED GOOD.

Part: PAWL — DISENGAGED (ZONE 800) · airframe 49,671 hrs · 14,205 cycles

AIRCRAFT WAS NOT GROUNDED. FORWARD SLIDE GIRT BAR ENGAGE LIGHT DOES NOT ILLUMINATE WHEN SLIDE IS ARMED DUE TO PAWL NOT ENGAGING. REINSTALLED GIRT BAR PAWL IAW AMM 25-66-01. OPERATIONAL CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 48,899 hrs · 13,987 cycles

AIRCRAFT NOT GROUNDED. SEAT MOUNTED EMERGENCY LIGHTS AT SEATS 9D THROUGH 15D ARE VERY DIM. REMOVED AND REPLACED BATTERY PACK M10952 IAW AMM 33-51-07. OPERATIONAL CHECK GOOD.

Part: DECK PLATE — CORRODED (BS 1712-1720) · corrosion level 2 · airframe 47,993 hrs · 13,752 cycles

FOUND CORROSION ON AFT DECK PLATE. INSTALLED DOUBLER PER AARD 53-60-51-3. AIRCRAFT IN BASE MAINTENANCE.

Part: LIGHT — DAMAGED (CABIN) · airframe 47,993 hrs · 13,752 cycles

EXIT LIGHT DAMAGED BETWEEN WINDOWS 23-24 RIGHT ON BOTTOM OF THE PANEL. INSTALLED SERVICEABLE LIGHT IAW AMM 33-51-10.

Part: SLIDING WINDOW — UNSECURE (COCKPIT) · airframe 47,430 hrs · 13,609 cycles

AIRCRAFT WAS NOT GROUNDED. DURING TAKEOFF ROLL THE CAPTAIN"S SLIDING WINDOW BECAME INCREASINGLY NOISEY. TAKEOFF ABORTED AT APPROXIMATELY 115 KNOTS. CREW DETERMINED THAT THE CAPTAIN"S WINDOW WAS NOT FULLY CLOSED.

Part: RELAY — INTERMITTENT (THRUST REVERSER) · airframe 44,231 hrs · 12,902 cycles

DURING CLIMB RT ENG GREEN THRUST REVERSER INDICATION REMAINED INTERMITTENT. DIVERTED, EMERGENCY DECLARED, AND LANDING UNEVENTFUL. R & R RT THRUST REVERSER STOW RELAY K27 IAW WDM 78-36-21. ACCOMPLISHED THRUST REVERSER OPERATIONAL TEST IAW AMM 78-31-00-5. SYS CHECKED NORMAL.

Part: BATTERY — DISCHARGED (CABIN) · airframe 44,196 hrs · 12,893 cycles

EMERGENCY LIGHTS ARE INOPERATIVE FOR SEAT ROWS 9 - 15. R & R BATTERY PACK & CHARGER ASSEMBLY IAW AMM 33-51-07. ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: CONTROL PANEL — FAULTY (WEATHER RADAR) · airframe 43,942 hrs · 12,838 cycles

AIR INTERRUPT, EMER DECLARED, LANDING UNEVENTFUL & ACFT OVERWEIGHT. DURING CLIMB, WEATHER RADAR FAILED. R & R RADAR TRANSCEIVER & RADAR CONTROL PANEL IAW AMM 34-43-01 & 34-43-02. PERFORMED OPERATIONAL CHECK IAW AMM 34-43-00. SYS CHECKED NORMAL. SEE ALSO AALA20150628004.

Part: TRANSCEIVER — FAULTY (WEATHER RADAR) · airframe 43,942 hrs · 12,838 cycles

AIR INTERRUPT, EMER DECLARED, LANDING UNEVENTFUL & ACFT OVERWEIGHT. DURING CLIMB, WEATHER RADAR FAILED. R & R RADAR TRANSCEIVER & RADAR CONTROL PANEL IAW AMM 34-43-01 & 34-43-02. PERFORMED OPERATIONAL CHECK IAW AMM 34-43-00. SYS CHECKED NORMAL. SEE ALSO AALA20150629003.

Part: DUCT — LEAKING (ZONE 400) · airframe 43,773 hrs · 12,802 cycles

AIR INTERRUPT, RETURNED, EMER LANDING WAS DECLARED. LANDING WAS UNEVENTFUL & ACFT WAS OVERWEIGHT. CREW REPORTED THAT THE RT ENG OVERHEAT LIGHT ILLUMINATED. FOUND HP6 DUCT SEALING SURFACE DAMAGED & LEAKING. REPLACED DUCT. AN OPERATIONAL & LEAK CHECK WAS ACCOMPLISHED WITH NO DEFECTS BEING NOTED.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 42,783 hrs · 12,576 cycles

FUSELAGE SKIN BETWEEN STATIONS 311 & 319 BELOW STRINGER 16 LT HAS LIGHTNING STRIKE DAMAGE. REPAIRED SKIN IAW 53-00-01-2R-3.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 39,907 hrs · 11,909 cycles

LT NR 3 DOOR EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR LT NR 3 DOOR EMERGENCY LIGHT, OPERATIONS CHECKED NORMAL.

Part: TRANSCEIVER — FAILED (WEATHER RADAR) · airframe 38,851 hrs · 11,660 cycles

SJU INFLIGHT MIA-BSB. CREW REPORTED WEATHER RADAR FAILED. EMERGENCY DECLARED FLIGHT DIVERTED SJU LANDED WITHOUT INCIDENT. REPLACED WEATHER RADAR TRANSCEIVER, SYSTEM GND CHECKED NORMAL OPERATION CLOSED.

Part: STRAP — CRACKED (FUSELAGE) · airframe 37,529 hrs · 11,341 cycles

AFT CARGO COMPARTMENT UPPER FLOOR BEAM SUPPORT STRAP CRACKED AT FRAME STATION 1340 & LBL 26. DRILLED 2 STOP HOLES AT THE END OF THE CRACK & INSTALLED REPAIR PLATE IAW AARD 53-60-51-4 & SRM 53-10-51-2R-1.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 37,529 hrs · 11,341 cycles

EXTERIOR FS SKIN HAS LIGHTNING STRIKE TO BS 1573 & STRINGER 27 + 1 RT. DRILLED OUT DAMAGE IAW SRM 53-00-01-2R-6. ACCOMPLISHED HFEC WITH NO CRACK NOTED. DRILLED FINAL HOLE SIZE & INSTALLED FASTENER IAW SRM 53-00-01-2R-6.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 37,529 hrs · 11,341 cycles

EXTERIOR FS SKIN HAS LIGHTNING STRIKE TO BS 1587 & STRINGER 27 RT. ACCOMPLISHED HFEC WITH NO CRACK NOTED. ACCOMPLISHED REPAIR IAW SRM 53-00-01-2R-2.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 37,529 hrs · 11,341 cycles

EXTERIOR FS SKIN HAS LIGHTNING STRIKE TO BS 1612.5 AT STINGER 27 RT. DRILLED OUT DAMAGE IAW SRM 53-00-01-2R-6. ACCOMPLISHED HIGH FREQUENCY EDDY CURRENT WITH NO CRACKS NOTED. DRILLED FINAL HOLE SIZE & INSTALLED FASTENER IAW SRM 53-00-01-2R-6.

Part: SKIN — DAMAGED (BS 1597.25) · airframe 37,529 hrs · 11,341 cycles

EXTERIOR SKIN HAS LIGHTNING STRIKE BS 1597.25 AT STRINGER 27 RT. DRILLED OUT DAMAGE IAW SRM 53-00-01-2R-6. ACCOMPLISHED HIGH FREQUENCY EDDY CURRENT WITH NO CRACKS NOTED. DRILLED FINAL HOLE SIZE & INSTALLED FASTENER IAW SRM 53-00-01-2R-6.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 37,529 hrs · 11,341 cycles

FS AT BS 580 BELOW FORWARD CARGO DOOR & STRINGERS 26 TO 27 RIGHT DAMAGED. INSTALLED DOUBLER REPAIR IAW EA B757-53-030739.

Part: COVER — MISSING (CABIN) · airframe 36,038 hrs · 10,993 cycles

EMERGENCY EXIT LIGHT ASSEMBLY AT RIGHT OVERWING HATCH 16F MISSING COVER. REPLACED COVER FOR EMERGENCY EXIT LIGHT ASSEMBLY AT RIGHT OVERWING HATCH 16F. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 33,415 hrs · 10,410 cycles

AFT RIGHT DOOR EXTERNAL EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR AFT RIGHT DOOR EXTERNAL EMERGENCY LIGHT, OPS CHECK NORMAL.

Part: TRANSMITTER — INOPERATIVE (HYDRAULIC SYS) · airframe 33,390 hrs · 10,405 cycles

MAN - CREW REPORTED RIGHT HYDRAULIC SYSTEM PRESSURE LIGHT ILLUMINATED. EMERGENCY DECLARED FLIGHT LANDED MAN WITHOUT INCIDENT. REPLACED QUANTITY TRANSMITTER. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: CONNECTOR — INOPERATIVE (EMERGENCY LIGHT) · airframe 32,966 hrs · 10,326 cycles

SEAT 33DEF SEAT MOUNTED EMERGENCY LIGHT WILL NOT TEST. RESEATED CONNECTOR AT 33DEF. OPS CHECKED NORMAL.

Part: SUPPORT FITTING — CORRODED (RT MLG TRUNNION) · airframe 32,682 hrs · 10,273 cycles

RIGHT MAIN GEAR FORWARD TRUNNION SUPPORT FITTING, CORROSION AT THE BORE EDGE OF THE UPPER INBOARD SUPPORT FITTING AND BUSHING. REPLACED BUSHING PER EA B757-57-022344.

Part: SUPPORT FITTING — CORRODED (RT MLG TRUNNION) · airframe 32,682 hrs · 10,273 cycles

RIGHT MAIN GEAR FORWARD TRUNNION SUPPORT FITTING, CORROSION AT THE BORE EDGE OF THE UPPER OUTBOARD SUPPORT FITTING AND BUSHING. REPLACE BUSHING PER EA B757-57-022344.

Part: SUPPORT FITTING — CORRODED (RT MLG TRUNNION) · airframe 32,682 hrs · 10,273 cycles

RIGHT MAIN GEAR FORWARD TRUNNION SUPPORT FITTING, CORROSION AT THE BORE EDGE OF THE LOWER OUTBOARD SUPPORT FITTING AND BUSHING. REPLACED BUSHING PER EA B757-57-022344.

Part: BUSHING — CORRODED (LT MLG TRUNNION) · airframe 32,682 hrs · 10,273 cycles

LEFT GEAR FORWARD TRUNNION INBOARD LOWER ATTACH BOLT BUSHING HAS CORROSION AND PITTING. REPLACED BUSHING PER EA B757-57-022344.

Part: BUSHING — CORRODED (LT MLG TRUNNION) · airframe 32,682 hrs · 10,273 cycles

LEFT GEAR FORWARD TRUNNION OUTBOARD LOWER ATTACH BOLT BUSHING HAS CORROSION AND PITTING. REPLACED BUSHING PER EA B757-57-022344.

Part: SUPPORT FITTING — CORRODED (RT MLG TRUNNION) · corrosion level 2 · airframe 32,682 hrs · 10,273 cycles

RIGHT MAIN GEAR FORWARD TRUNNION SUPPORT FITTING, CORROSION AT THE BORE EDGE OF THE LOWER INBOARD SUPPORT FITTING AND BUSHING. REPLACED BUSHING PER EA B757-57-022344.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 32,439 hrs · 10,218 cycles

DENT WITH A GOUGE ON THE RIGHT SIDE OF THE AIRCRAFT JUST BELOW FORWARD CARGO STATIONS 580 TO 600. INSTALLED REPAIR DOUBLER PER EA B757-53-021826.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,758 hrs · 9,670 cycles

EMERGENCY LIGHT ABOVE SEAT 10D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT ABOVE SEAT 10D. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,758 hrs · 9,670 cycles

EMERGENCY LIGHT ABOVE SEAT 34C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT ABOVE SEAT 34C. OPS CHECK NORMAL.

Part: LAMP — INOPERATIVE (CABIN) · airframe 24,388 hrs · 8,436 cycles

EMERGENCY LIGHTS AT SEAT ROW 18 INOPERATIVE. REPLACED LAMP AT SEAT ROW 18.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 24,388 hrs · 8,436 cycles

EMERGENCY LIGHT AT FORWARD ENTRY DOOR INOPERATIVE. REPLACED BATTERY PACK.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 24,388 hrs · 8,436 cycles

EMERGENCY LIGHTS IN FIRST CLASS SECTION INOPERATIVE. REPLACED BATTERY PACK.

Part: TRANSMITTER — INOPERATIVE (HYDRAULIC SYS) · airframe 23,128 hrs · 8,020 cycles

DFW - RIGHT HYDRAULIC QUANTITY WENT TO ZERO. EMERGENCY DECLARED, RETURNED DFW WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED RIGHT HYDRAULIC QUANTITY TRANSMITTER. SERVICED RIGHT HYDRAULIC QUANTITY TO FULL. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: LAMP — BURNED OUT (EMERGENCY LIGHTS)

DFW - LEFT NUMBER 4 EMERGENCY SLIDE LIGHT INOPERATIVE. REPLACED LAMP FOR LEFT NUMBER 4 EMERGENCY SLIDE LIGHT.

Part: LIGHT — INOPERATIVE (CABIN)

DFW - SEAT MOUNTED EMERGENCY LIGHT IN ROW 28 INOPERATIVE. REPLACED LAMP FOR SEAT MOUNTED EMERGENCY LIGHT IN ROW 28.

Part: LAMP — BURNED OUT (EMERGENCY LIGHTS)

DFW - RIGHT NUMBER 4 EMERGENCY SLIDE LIGHT INOPERATIVE. REPLACED LAMP AT RIGHT NUMBER 4 EMERGENCY SLIDE LIGHT.

Part: B-NUT — LOOSE (HYD LINE)

INFLIGHT LEFT HAND HYDRAULIC SYSTEM QUANTITY DROPPED TO .18. LANDED MCO WITHOUT INCIDENT. TIGHTENED LOOSE B-NUT ON LEFT HAND PRESSURE LINE TO ALT SHUTTLE VALVE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 21,594 hrs

TPA - EMERGENCY LIGHTS AT SEAT ROWS 16D TO 21D INOPERATIVE. REPLACED BATTERY PACK AT SEAT ROW 19DEF FOR EMERGENCY LIGHTS AT SEAT ROWS 16D TO 21D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (CABIN) · 20,995 cycles

LAX SEAT MOUNTED EMERGENCY LIGHTS AT AFT CABIN INOPERATIVE. REPLACED BATTERY PACK M10801 FOR INOPERATIVE EMERGENCY LIGHTS AT AFT CABIN. SYSTEM GROUND CHECKED NORMAL OPS.

Part: LAMP — MISSING (EMERGENCY LIGHTS) · airframe 20,004 hrs

MIA - EMERGENCY LIGHT AT SEAT 23D MISSING LAMP. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 23D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LENS — MISSING (EMERGENCY LIGHTS) · airframe 20,004 hrs

MIA - EMERGENCY LIGHT AT SEAT 23D MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 23D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: OVEN — DIRTY (GALLEY)

SJU INFLIGHT T1044/11JAN AUA TO BOS - FIRST CLASS GALLEY OVEN BEGAN SMOKING. SMELLED LIKE ORGANIC MATERIAL. OVEN TEMPERATURE WAS SET AT 175 AND THE OVERHEAT LIGHT DID NOT COME ON. THE NUMBER ONE AND NUMBER TWO FIRST CLASS OVENS WERE TURNED OFF AND THE CIRCUIT BREAKER PULLED. LANDED AT SJU WITHOUT INCIDENT. FOUND FOOD RESIDUE IN FIRST CLASS GALLEY OVEN. CLEANED OVEN. SYSTEM GROUND CHECKED NORMAL OPERATION FOR BOTH OVENS.

Part: LENS — INOPERATIVE (EMERGENCY LIGHT)

DFW - EMERGENCY PATH LIGHTING AT SEAT 15D IS MISSING LENS. REPLACED EMERGENCY PATH LIGHTING LENS AT SEAT 15D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BALLAST — INOPERATIVE (CABIN)

ORD - EMERGENCY LIGHT AT SEAT 18F OVERWING HATCH INOPERATIVE. REPLACED BALLAST FOR EMERGENCY LIGHT AT SEAT 18F OVERWING HATCH. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

RT AFT GALLEY DOOR EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK FOR RT AFT GALLEY DOOR EMERGENCY LIGHT. SYSTEM GROUND CHECKED. NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

SEAT MOUNTED AND EXIT DOOR EMERGENCY LIGHTS AFT OF OVERWING INOPERATIVE. REPLACED BATTERY PACKS IN AFT SECTION FOR SEAT MOUNTED AND EXIT DOOR EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — INOPERATIVE (ESCAPE SLIDE)

LT EMERGENCY SLIDE LEFT AFT OF WING AT STATION 1388 INOPERATIVE. FOUND PIN CONNECTOR D5526 PUSHED BACK. REPOSITIONED PIN BACK INTO CONNECTOR AND LOCKED EMERGENCY SLIDE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)