N184DN

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 134,281 hrs · 19,648 cycles

SHIP 184 EMERGENCY EXIT COVER DIFFUSER LENS DAMAGED OR MISSING. CORRECTIVE ACTION: SECURED EXIT SIGN COVER ABOVE SEAT 6C. CHKS GOOD (2976309)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 134,033 hrs · 19,602 cycles

SHIP 184 EMERGENCY EXIT COVER DIFFUSER LENS DAMAGED OR MISSING / LOCATIONS:801. CORRECTIVE ACTION: LENS REINSTALLED CHECKED SATISF (2937167)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 133,864 hrs · 19,576 cycles

SHIP 184 EMERGENCY EXIT SIGNS INOPERATIVE / LOCATIONS: 7D. CORRECTIVE ACTION: SECURED LENSES. OK TO CONTINUE. (2917873)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 133,507 hrs · 19,520 cycles

SHIP 0184 -DIV/DE- TO KEF DUE TO ACTIVE FUEL LEAK OUT LEFT-WING TANK VENT WITH CENTER FUEL BOOST PUMP SELECTED ON. CORRECTIVE ACTION: CONFIRMED FUEL JETTISON TRANSFER VALVE SHAFTS ALIGNED, TRANSFERRED FUEL FROM TANK TO TANK, NO LEAKS FOUND. (LP 4867524)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 133,132 hrs · 19,460 cycles

SHIP 184 1R DOOR SLIDE ARM LIGHT WILL NOT PUSH TO TEST; COMES ON AS NORMAL WHEN DOOR IS ARMED. CORRECTIVE ACTION: REMOVED AND REPLACED 1R DOOR SLIDE LIGHT PUSH TO TEST SWITCH; AS PER B767-300 AMM 52-73. (4683502)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 132,796 hrs · 19,412 cycles

SHIP 184 AFTER LANDING DURING TAXI AN OIL/ DIESEL SMELL DEVELOPED THROUGHOUT THE AIRCRAFT. CORRECTIVE ACTION: PER MCC REQUEST , C/W STEPS 1-4 ON MD LOG , REF B767-300 AMM 49- 52. NO OIL OR RESIDUE FOUND ON APU BLEED DUCT. CHKS NML. RAN PACKS @ BOTH FULL HOT +COLD WHILE RUNNING CHILLERS /IFE/OVENS . NO FUMES OR DEFECTS NOTED REF B767-300 AMM 21-51. INSPECTED ENG BLEED DUCTING. NO OIL OR RESIDUE FOUND . REF B767-300 AMM 36-11. A/C TAKEN OUT FOR HIGH POWER RUN. REF B767-300 AMM 71-00. NTF . R/R RECIRC FILTER PER B767-300 AMM 21-25. A/C OK FOR SVC . (4730331)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 132,594 hrs · 19,356 cycles

SHIP 184 FOUND NO.2 STRUT FWD UPR SPAR WEB CUTOUT CRACK AT NAC STA 188.00 AND 193.00. CORRECTIVE ACTION: THE CRACK AT NSTA 177 RBL 3, LENGTH 1.5" ; NSTA 175 RBL 1, LENGTH 0.5" AREA TRIMED OUT AND APPLY DOUBLER REPAIR WITH 2024T3 -0.125"CLAD ALUMINIUN SHEET AS PER PRI 687875-14 (2726621)

Part: NONE — NONE · airframe 132,230 hrs · 19,281 cycles

SHIP 184 PART OF OVERWING EXIT SIGN MISSING AT LEFT SIDE OVERWING. CORRECTIVE ACTION: LOCATED EMERGENCY EXIT LIGHT LENS IN CABIN AND REINSTALLED AS NECESSARY. OK FOR SVC. (9916812)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 132,592 hrs · 19,355 cycles

SHIP 184 DENT FOUND ON RT WING MAIN TRAILING EDGE FLAP LOWER SKIN. CORRECTIVE ACTION: RT WING MAIN TRAILING EDGE FLAP LOWER SKIN REPAIRED AS PER B767- 300 SRM 57-53-01-2R-1& SRM 51-70-10-2R-2 REPETITIVE INSP REQ (4070774)

Part: SIGN — DAMAGED (EMERGENCY LIGHTS) · airframe 131,236 hrs · 19,063 cycles

SHIP 184 R1 DOOR LOWER EXIT SIGN DAMAGED. CORRECTIVE ACTION: R/R EXIT LIGHT ASSY PER B767-300 AMM 33-51. (9616199)

Part: NONE — NONE · airframe 131,003 hrs · 19,022 cycles

SHIP 184 CREW REST EMER LTS INOP, CORRECTIVE ACTION: R/R CREW REST BATTERY FOR EMERG LIGHTS. CKS GOOD. IAW B767 AMM 33-51-01. OK FOR SVC (9616100)

Part: NONE — NONE · airframe 130,692 hrs · 18,970 cycles

SHIP 184 R/H AFT OVERWING ESCAPE HATCH STEP NOT STOWED, CORRECTIVE ACTION: RESTOWED OVERWING ESCAPE HATCH STEP PER B767 CMM 52-21-11 OK FOR SVC (8915756)

Part: NONE — NONE · airframe 130,602 hrs · 18,955 cycles

SHIP 184 FLOOR EMERGENCY LIGHTS INOP AT LOCATION 27A, 29A, & 36G. WIRES EXPOSED UNDER SEATS, CORRECTIVE ACTION: REMOVED AND REPLACED FUSES PER B767 WDM 33-51-31. OPERATIONAL CHECKS OK. (8915702)

Part: NONE — NONE · airframe 130,517 hrs · 18,942 cycles

AIRCRAFT 0184, EMERGENCY LIGHTS INOP SEATS 21-30 L AND R , CORRECTIVE ACTION: REPLACED EMERGENCY LIGHT BATTERY PACK AND CHARGER. LP 9014263

Part: NONE — NONE · airframe 130,472 hrs · 18,935 cycles

SHIP 184 F/O SIDE EXIT SIGN MESSING ON BULKHEAD BETWEEN BUSINESS AND COACH. CORRECTIVE ACTION: FOUND AND RESECURED (9014230)

Part: FUSE — INOPERATIVE · airframe 130,329 hrs · 18,917 cycles

SHIP 184 FOUND EMERGENCY ESCAPE PATH LIGHTING INOP ON ROWS 21 THROUGH 30 BOTH SIDES. CORRECTIVE ACTION: REPLACED PICO FUSES PER B767 WDM 33-51-31 OPS CHK NML. (9011353)

Part: NONE — NONE · airframe 130,112 hrs · 18,874 cycles

SHIP 184 FOUND EMERGENCY LIGHT SEAT 21-31 BOTH SIDES INOP, CORRECTIVE ACTION: R/R M9009 BATTERY CHARGER AND BATTERY REF B767 AMM 33-51. CKS NMLR (8949418)

Part: LIGHT — DETACHED · airframe 129,931 hrs · 18,835 cycles

SHIP 184 EXIT LIGHT FELL OFF 22F, CORRECTIVE ACTION: REINSTALLED EXIT LIGHT. OPS OK. (9207125)

Part: SIGN — INOPERATIVE · airframe 129,671 hrs · 18,800 cycles

SHIP 184 FOUND EXIT SIGN IN FLIGHT DECK INOP, CORRECTIVE ACTION: REPLACED BATTERY PER B767 AMM 33-51 OPS CHECK IS GOOD. (2266568)

Part: LIGHT — DAMAGED · airframe 129,615 hrs · 18,793 cycles

SHIP 184 EMERGENCY LIGHT AT SEAT 24F DAMAGED. CORRECTIVE ACTION: THIS ITEM WAS DEFERRED AS PER MEL 33-51-03A. (8835526)

Part: SWITCH — BROKEN · airframe 129,429 hrs · 18,760 cycles

SHIP 184 WHILE WORKING SVC. FWD ATTEND EMER LT SWITCH BROKEN. CORRECTIVE ACTION: R/R FWD ATTEND EMER LT SWITCH P/N: 2100-13 REF B767 WDM 33-51-11 AND PERFORMED EMERGENCY LT TEST REF. B767 AMM 33-51 OPS CHECK GOOD. (8406748)

Part: LIGHT — DAMAGED · airframe 129,333 hrs · 18,739 cycles

SHIP 184 EMERGENCY FLOOR LIGHTING DAMAGED OR INOPERATIVE / LOCATIONS:23F, CORRECTIVE ACTION: 23F EMERGENCY FLOOR LIGHT REPOSITIONED. DONE EMERGENCY LIGHT OPERATIONAL TEST PER B767-300 AMM 33-51-00, 23F EMERG LIGHT OK TO SERVICE. (2205337)

Part: GIRT BAR — DIRTY · airframe 129,229 hrs · 18,716 cycles

SHIP 184 DOOR 2L WOULD NOT ARM, CORRECTIVE ACTION: FOUND DEBRIS AROUND GIRT BAR, CLEANED DEBRIS AND OPS CHECKED DOOR IAW B767 25-66-01, OPS CHECKED GOOD, OK FOR SVC. (8824932)

Part: LIGHT — INOPERATIVE · airframe 129,180 hrs · 18,705 cycles

SHIP 184 DURING SERVICE CHECK FOUND EMERGENCY EXIT LIGHT ON ROW 39G INOP. CORRECTIVE ACTION: RESEATED CONNECTOR. OPS CHECK GOOD. (8824901)

Part: NONE — NONE · airframe 128,365 hrs · 18,514 cycles

SHIP 184 EMERGENCY EXIT LENS MISSING ABOVE SATS 12F,G, CORRECTIVE ACTION: REPLACED EMERGENCY EXIT LENS ABOVE SEAT 12F,G CKS NML (8256398)

Part: NONE — NONE · airframe 128,189 hrs · 18,470 cycles

SHIP 184 SLIDE INDICATOR LIGHT INOP OR DAMAGED. CORRECTIVE ACTION: PERFORMED OPERATION TEST B767-300 AMM 52-73. NO DEFECTS NOTED. (2039987)

Part: NONE — NONE · airframe 127,958 hrs · 18,424 cycles

SHIP 184 DURING EMERG LIGHTS CHK ALL ROWS AFT OF 30 ON RT SIDE OF A/C INOP. CORRECTIVE ACTION: REMOVED & REPLACED EMERGENCY LIGHT POWER SUPPLY M9010 PER B767- 300 AMM 33-51. (8096380)

Part: NONE — NONE · airframe 127,705 hrs · 18,369 cycles

SHIP 184 EMERG EXIT SIGN FELL OFF LEFT SIDE AT FL DIVIDER. CORRECTIVE ACTION: INSTALLED EMERGENCY EXIT COVER (7939562)

Part: NONE — NONE · airframe 127,577 hrs · 18,339 cycles

SEAT 23F EMERGENCY EXIT ISLE LIGHT INOP. RE TERMINATED CONNECTOR PER WDM 33-51-20 & SWPM CHAPT 20. CHECKS GOOD. (LP# 7939508)

Part: NONE — NONE · airframe 127,577 hrs · 18,339 cycles

SEAT 37B EMERGENCY EXIT ISLE LIGHT INOP. RE TERMINATED CONNECTOR PER WDM 33-51-20 & SWPM CHAPT 20. CHECKS GOOD. (LP# 7939510)

Part: NONE — NONE · airframe 127,577 hrs · 18,339 cycles

SEAT 38F EMERGENCY EXIT ISLE LIGHT INOP. RE TERMINATED CONNECTOR PER WDM 33-51-20 & SWPM CHAPT 20. CHECKS GOOD. (LP# 7939509)

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 127,128 hrs · 18,247 cycles

SHIP 184 EMERGENCY LIGHTS INOPERATIVE AT SEAT 1A, 2A AND 3A. CORRECTIVE ACTION: REPLACED EMERGENCY LIGHT POWER SUPPLY. SYSTEM OPERATION IS NORMAL. (LP 7832903)

Part: FAN — FAILED (RECIRCULATION) · airframe 126,360 hrs · 18,093 cycles

SHIP 0184 -DIVERTED TO BUF AND DECLARED AN EMERGENCY DUE TO ELECTRICAL ODOR IN FLIGHT DECK. CORRECTIVE ACTION: REPLACED LEFT RECIRCULATION FAN, VIBE MONITOR AND RECIRCULATION FILTERS.

Part: COMPUTER — MALFUNCTIONED (FLT CONTROLS) · airframe 126,091 hrs · 18,045 cycles

SHIP 184 -ATB - UNABLE TO ENGAGE ANY AUTOPILOT AFTER TAKEOFF. CORRECTIVE ACTION: TROUBLESHOT PER FIM. REPLACED CENTER FLIGHT CONTROL COMPUTER (FCC) AND THE TOTAL AIR TEMP (TAT) PROBE. AFDS TESTS PASSED.

Part: SKIN — OUT OF LIMITS (BS 1461-1502) · airframe 126,116 hrs · 18,049 cycles

DURING ROUTINE INSPECTIONS, EXISTING BLENDS WERE DISCOVERED ON THE FUSELAGE SKIN (PN 146T3231-1) BETWEEN BS 1461 AND BS 1502, AND BETWEEN S-28L AND S-31L. MULTIPLE BLENDS ARE OUT OF LIMITS PER SRM 53-00-01 ALLOWABLE DAMAGE AND REPAIRED PER SRM. (LP 1759113)

Part: PIN — LOOSE (WIRE HARNESS) · airframe 125,127 hrs · 17,805 cycles

EMERGENCY ESCAPE LIGHT AT SEAT 16G ARE INOPERATIVE. CORRECTIVE ACTION: REINSTALLED LOOSE PIN AT HARNESS GOING TO SIDEWALL PANEL. SYSTEM OPERATION IS NORMAL.

Part: FILTER — CONTAMINATED (RECIRCULATION) · airframe 124,899 hrs · 17,748 cycles

ATB/FUMES-DUE TO ODOR IN CABIN AND FLIGHT DECK AFTER T/O, LANDED OVERWEIGHT. NO EMERGENCY DECLARED. CORRECTIVE ACTION: COMPLIED WITH OVERWEIGHT LANDING INSPECTION AND NO-GO ODI TASKS. FOUND EVIDENCE OF HYD FLUID ON RT RECIRCULATION FILTER. FOUND DAMAGED HYDRAULIC LINE UNDER CABIN FLOOR PANEL NEAR ROW 22 CDE. REPAIRED LINE, REPLACED RECIRCULATION FILTERS, CLEANED AND RESTORED CABIN. AIRCRAFT RETURNED TO SERVICE.

Part: A/C PACK — CONTAMINATED (ECS) · airframe 124,517 hrs · 17,651 cycles

ODOR/SMELL BURNING SULFUROUS ODOR AFTER DEPART LAX AND GEAR DOOR OPEN FOR RETRACTION. ODOR QUICKLY CLEARED WITHIN 60 SEC. SAME ODOR WITH GEAR DOORS OPENING FIR GEAR EXTENSION FOR LANDING. AGAIN QUICKLY CLEARED 60 SEC. PERFORMED REMOVAL OF CONTAMINATION FROM THE AIR CONDITIONING AND PNEUMATIC SYSTEM PER B767 AMM 21-00-21. RAN ENGINES FROR 30MIN. NO ODORS IN FLIGHT DECK OR PASSENGER CABIN AT THIS TIME.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 124,492 hrs · 17,644 cycles

THE RIGHT SIDE CABIN EMERGENCY LIGHTS FROM SEAT 31 THROUGH 40 ARE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY PACK (M734) PER B767-300 AMM 33-51. OPERATIONAL CHECK IS NORMAL

Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 121,625 hrs · 17,207 cycles

ON SVC CK FOUND EMERGENCY SEAT LIGHTS INOPERATIVE ON RIGHT SIDE ROW 22 TO ROW 30 INOP FOUND SEATS 24 AND 26 WITH BROKEN WIRES WHICH TOOK OUT CHARGER POS M9009. REPLACED CHARGER SYSTEM OPERATION IS NORMAL.

Part: SKIN — CORRODED (LT WING) · airframe 119,934 hrs · 16,976 cycles

CORROSION LEVEL: 1 LT SKIN TOP OF WING FOR OVERWING FILL PORT HAS CORROSION AND PITTING C/W ERA 575716-14. (LP 0987059)

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 119,920 hrs · 16,970 cycles

UPPER CABIN STA 859.5 AT RIGHT OBD FLOOR TRACK HAS CORROSION ON FRAME STRAP DAMAGE OUT OF LIMITS REPAIRED PER ER/A 575453-14. (LP 0984632)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 119,939 hrs · 16,977 cycles

CORROSION LEVEL: 2 CORROSION ON THE UPPER SURFACE OF FLOOR SUPPORT, ON THE FWD SIDE OF FRAME 933, AT STR 20L REMOVED AND REPLACED SEAT TRACK SUPPORT (LP 0984690)

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 119,922 hrs · 16,972 cycles

CORROSION LEVEL: 2 LT FUSELAGE FRAME AT STA 933 HAS EXFOLIATION CORROSION AT STRINGER 20L. REPAIRED PER ERA 575548-14 (LP 0984597)

Part: SKIN — DAMAGED (FUSELAGE) · airframe 119,920 hrs · 16,970 cycles

LT STA 1809 EXTERIOR SKIN AT STRINGER 12L FOUR FASTENERS HAVE EXCESSIVE COUNTERSINKS AND PULLED THROUGH THE SKIN. REPAIRED PER ERA 575396-14. (LP 0981777)

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 119,922 hrs · 16,972 cycles

CORROSION LEVEL: 2 LT FUSELAGE FRAME AT STA 933 HAS EXFOLIATION CORROSION AT STRINGER 20L OUT OF LIMITS AND REPAIRED. (LP 0981642)

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 119,920 hrs · 16,970 cycles

CORROSION FOUND UNDER T CAP OF BULKHEAD AT NUTPLATE LOCATION. FS 1153 RBL 44 CORROSION FOUND TO BE OUT OF SRM LIMITS REPAIRED PER SRM 51-70-12. (LP 0975791)

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 119,920 hrs · 16,970 cycles

CORROSION LEVEL: 2 UPPER CABIN SEAT TRACK IS CORRODED IN MULTIPLE AREAS STA 1242-1439 RBL88. REPLACED SEAT TRACK. (LP 0963811)

Part: CONNECTOR — DEFECTIVE (CABIN) · airframe 119,920 hrs · 16,970 cycles

EMERGENCY LIGHTS AT SEATS 31F & 39F ARE INOPERATIVE. RE-TERMINATED EMERGENCY LIGHT CONNECTORS AT SEAT TO SIDEWALL. SYSTEM OPERATION IS NORMAL.

Part: ALTIMETER — MALFUNCTIONED (COCKPIT) · airframe 118,502 hrs · 16,773 cycles

CAPTAINS PRIMARY ALTIMETER FAILED IN FLIGHT FOR 5 MINUTES, TAPPED ON GLASS AND IT STARTED WORKING AGAIN. REPLACED CAPTAINS ALTIMETER.

Part: SKIN — DENTED (LT HORIZ STAB) · airframe 118,303 hrs · 16,743 cycles

DURING WALK AROUND FOUND DENT ON LEADING EDGE OF LEFT HORIZONTAL STAB DENT REQUIRES REPAIR PER SRM 51-70-10 REPAIR 4. DENT IS 7 FOOT FROM FUSELAGE.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 113,816 hrs · 16,153 cycles

DURING SERVICE FOUND FLIGHT DECK EMERGENCY INOPERATIVE. REPLACED ASSEMBLY SYSTEM OPERATION IS NORMAL.

Part: SEALANT — ERODED (WINDSHIELD) · airframe 112,061 hrs · 15,923 cycles

LEFT WINDSHIELD WEATHER SEAL ERODED. REPAIRED SEALANT.

Part: CONTACTOR — INOPERATIVE (EMERGENCY LIGHT) · airframe 109,916 hrs · 15,658 cycles

L1 DOOR EXTERNAL EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACED THE LIGHT CONTACTOR. SYSTEM OPERATION IS NORMAL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 109,900 hrs · 15,655 cycles

SLIDE INDICATOR LIGHT INOPERATIVE FORWARD TO MCO. REPLACED THE LAMP.

Part: FRAME — DAMAGED (BS 720) · airframe 105,593 hrs · 15,105 cycles

FRAME BS 720, BETWEEN STRINGERS 1 LT AND 1 RT HAS A NR 40 HOLE THAT NEEDS TO BE PLUGGED. INSTALLED RIVET IAW SRM 53-00-07.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHTS) · airframe 102,736 hrs · 14,755 cycles

EMERGENCY LIGHTS AT DOOR 2 LT AND RT ARE INOPERATIVE. MAINTENANCE RECONNECTED CONNECTOR, REPLACED THE BATTERY. SYSTEM OPS ARE NORMAL.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 94,582 hrs · 13,710 cycles

OVERHEAD CEILING EMERGENCY LIGHTS INOPERATIVE RT SIDE OF SEATS 22GF 26 GF AND 28GF. MX REPLACED BATTERY CHARGER. SYS OPS IS NORMAL.

Part: FITTING — CRACKED (RT WING) · airframe 93,936 hrs · 13,618 cycles

CRACK ON ONE FASTENER HOLE AT RT WING TOP OF FRONT SPAR LOAD FITTING MOST OTBD ROW LOWEST FASTENER HOLE. REPAIRED IAW PRI 512476-14AD, REV O AND ER/A 512476-14AD REV, ORIGINAL.

Part: FLOORBEAM — CRACKED (AFT CARGO) · airframe 93,936 hrs · 13,618 cycles

AFT CARGO FLOORBEAM BS 1197+88 , LBL 45 CRACKED. UPPER STRUCTURE REPAIRED IAW SRM 53-00-07, REPAIR 4 FIG 201, REV 91.02.

Part: STIFFENER — DAMAGED (NR 1 PYLON) · airframe 93,936 hrs · 13,618 cycles

ELONGATED FASTENER HOLES ON STIFFENER AT UPPER SPAR WEB LT SIDE. REPAIRED IAW PRI 511842-14AD REV 1 AND ER/A 511842-14AD, REV ORIG.

Part: SPLICE PLATE — MISMANUFACTURED (NR 2 PYLON) · airframe 93,936 hrs · 13,618 cycles

RING DOUBLER WITH TWO EXISTING HOLES LESS IAW DWG AT LT SIDE OF UPPER SPAR WEB ON NR 2 PYLON. REPAIRED IAW PRI 511844-14AD REV 1 AND ER/A 511844-14AD REV ORIG.

Part: UNKNOWN — ODOR (CABIN) · airframe 90,829 hrs · 13,196 cycles

ONE HOUR INTO FLIGHT LEFT PACK TEMP EICAS FOLLOWED BY PACK INOPERATIVE. LIGHT ON OVERHEAD PANEL BOTH EXTINGUISHED WITHIN 30 SECONDS WITHOUT ANY CREW ACTION. HOT METAL ODOR IN MID CABIN AT SAME TIME. THE LEFT PACK TEMP CONTROL VALVE WAS REPLACED. SYSTEM OPERATION IS NORMAL.

Part: FAILSAFE — CRACKED (BS 955.1) · airframe 90,661 hrs · 13,172 cycles

DURING ULTRASONIC INSPECTION, FOUND CRACK INDICATION ON FAILSAFE STRAP OF THE REAR SPAR BULKHEAD RT 955.1 AT 9 AND 4 O`CLOCK LOOKING OTBD. CRACK AREA REPAIRED AS PER ERA 503089-14AD REV ORIG DATED 05/25/12.

Part: FAILSAFE — CRACKED (BS 955) · airframe 90,661 hrs · 13,172 cycles

DURING ULTRASONIC INSPECTION, FOUND CRACK INDICATION ON FAILSAFE STRAP OF THE REAR SPAR BULKHEAD LT 955.1 AT 4 AND 9`OCLOCK LOOKING OTBD. CRACK AREA REPAIRED AS PER ERA 503090-14AD REV ORIG DATED 05/28/2012.

Part: CONNECTOR — DAMAGED (CABIN) · airframe 87,206 hrs · 12,716 cycles

EMERGENCY PATH LIGHT AT SEAT 22F IS INOPERATIVE. MAINTENANCE REPAIRED THE SEAT HARNESS CONNECTOR. SYSTEM OPERATION IS NORMAL. ATL/294719

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 84,416 hrs · 12,363 cycles

EMERGENCY LIGHT ASSY AT MID LAVATORY CROSSOVER AISLE IS INOPERATIVE. MX REPAIRED THE BROKEN WIRE BEHIND THE SIDE WALL PANEL AND REPLACED THE BATTER AND POWER SUPPLY. SYS OPS IS NORMAL.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 84,326 hrs · 12,350 cycles

FOUND DURING DRC EMERGENCY ESCAPE PATH MAKER ON MID LAVATORY TO BE INOPERATIVE. MX FOUND WIRING AT LAMP ASSY PINCHED AND REPLACED THE LIGHT ASSY.

Part: ANGLE — CRACKED (NR 2 PYLON) · airframe 83,179 hrs · 12,205 cycles

FOUND CLOSEOUT ANGLE ON NR 2 PYLON CRACKED WHILE CONDUCTING INSP IAW 1T204. CONDUCTED HFEC INSP OF BOLTS IAW EA 01-074944-12ADME04 AND ERA 485953-14AD. NO FURTHER DAMAGE NOTED. REPLACED CLOSEOUT ANGLE IAW DWG 311T3150.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 80,909 hrs · 11,905 cycles

EMERGENCY PATH LIGHT AT 22F AND 32F INOP. FWD TO MCO AND PLACARD IAW MEL 33-51-03A. ETOPS CATEGORY 'E': PROBLEMS WITH SYSTEMS CRITICAL TO ETOPS.

Part: STARTER — INOPERATIVE (NR 2 ENGINE) · airframe 79,697 hrs · 11,752 cycles

RT ENG FAILED TO START NO ROTATION. RTB REPLACED STARTER. CONFIRMED STARTER ASSY INOP. R & R STARTER ASSY IAW AMM 80-11-01-401. STARTER CONTROL VALVE IAW AMM 80-11-02-401. REMOVED AND INSTALLED. ALIGNED MAN OVERRIDE SOCKET. SERVICED STARTER WITH CRANKING IS OK. OK FOR SVC. PN 774860A4 S/N OFF 891127. ETOPS CATEGORY 'E': PROBLEMS WITH SYSTEMS CRITICAL TO ETOPS.

Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 79,618 hrs · 11,742 cycles

WORKING ETOPS A CK FOUND ROW 16AB EMERGENCY LIGHT INOP. REPAIRED BROKEN WIRES AT CONNECTOR. OPS CHECK GOOD.

Part: INDICATOR — FAILED (STANDBY AIRSPEED) · airframe 78,933 hrs · 11,654 cycles

STBY AIRSPEED INDICATOR FAILED. RESET AND SECURED ELECTRICAL AND PITOT-STATIC HOSES AT INDICATOR IAW AMM.

Part: PUMP — LEAKING (HYD SYSTEM) · airframe 76,419 hrs · 11,326 cycles

CENTER HYDRAULIC SYSTEM QTY LOW, SYS QTY AT .21. FOUND C2 ELEC PUMP TO BE LEAKING. REPLACED C2 ELECTRIC PUMP. SERVICED CENTER HYD LEAK AND OPN CHECK GOOD.

Part: CONTROLLER — MALFUNCTIONED (LT BLEED) · airframe 76,310 hrs · 11,311 cycles

LEFT BLEED NO OUTPUT PRESS UNABLE TO CROSSBLEED START ENG. FOUND LT ENG PRV INOP SWAPPED WITH HPSOV FWD TO MCO PER MEL 36-11-02 HPSOV LOCKED CLOSED. REMOVED AND REPLACED PRV CONTROLLER IAW MM.

Part: SENSOR — MALFUNCTIONED (RT AOA) · airframe 75,716 hrs · 11,240 cycles

ON TAXI OUT R AOA LIGHT ON AFTER ENG START. REPLACED R AOA SENSOR PER MM. OPS NML PER 30-32-00.

Part: CONNECTOR — NOT SEATED (BLEED AIR SYS) · airframe 75,429 hrs · 11,204 cycles

AFTER ENGINE START NO BLEED AIR FROM LEFT ENGINE WITH THE BLEED AIR VALVE SELECTED TO OPEN. RESEATED CONN ON LT ENG PRV AND HP CONT. CHECKED CONNECTIONS ON PRV AND HP VALVES. RAN LT ENG TO BLEED SHIFT AFTER UNLOCKING HPSOV DUE TO MSU. SEE NEXT ITEM. ENG BLEED OPS CHECK NORMAL PER AMM.

Part: ACTUATOR — LEAKING (HYD SYSTEM) · airframe 74,952 hrs · 11,145 cycles

CENTER HYDRAULIC SYSTEM WAS LOSING FLUID, ATB TO SVO. FOUND LCCA LEAKING.

Part: ENGINE — DEFECTIVE (NR 1) · airframe 74,826 hrs · 11,130 cycles

ENG FAILED EA 51-470869-12 REV B MGB OIL NOZZLES INSP. REPLACING NR 1 ENG. REPLACED NR 1 ENGINE PER TRANS 1T148.

Part: SKIN — DAMAGED (FS 1440) · airframe 71,936 hrs · 10,788 cycles

BLENDS TO SKIN FS 1440-1540 AND STR 28L-36L. DTA INSPECTION ADDED.

Part: WARNING MESSAGE — FALSE ACTIVATION · airframe 71,526 hrs · 10,739 cycles

CENTER ADP PRESS LIGHT AND EICAS MSG. PERFORMED RESET PER FIM. CENTER ADP OPS CKS OK.

Part: O-RING — CUT (HYD SYSTEM) · airframe 71,517 hrs · 10,738 cycles

FLIGHT 117 - DECLARED EMERGENCY INTO ATL DUE TO LOSS OF CENTER SYSTEM HYD QTY AND PRESS LOST. UNEVENTFUL LANDING AND TAXI. FOUND CUT O-RING ON CTR SYS LCCA FILTER BOWL. REPLACED SAME CKS OK.

Part: ENGINE — MAKING METAL (APU) · airframe 68,351 hrs · 10,337 cycles

APU AUTO SHUTDOWN AT DEPARTURE, DELAY TAKEN JFK WORKING MCO FOUND METAL ON CHIP DETECTOR. FOUND HEAVY METAL ACCUMULATION ON OIL CHIP DETECTORS. REMOVED AND REPLACED AP PER MM. OPS AND LEAK CHK OK. MCO AND PLACARD REMOVED.

Part: SWITCH — BROKEN (CABIN) · airframe 68,152 hrs · 10,313 cycles

CREW REPORTS CABIN OVERHEAD LIGHTS FLICKERING ON AND OFF THROUGH ENTIRE CABIN. PULLED C/BS ON P-33 PANEL TO STOP FLASHING RETURNED TO JFK FOR REPAIRS AFTER ISOLATED PROX BOX FAULTS CARD 06. REPLACED PSEU. OPS OK. FND SW S 527 P19 BROKEN. INSPECTED RT GEN FEEDER. ALL OK. INSPECTED WIRE ABOVE L1 DOOR PER BOEING . CKS OK. REPLACED PRESS SW S 527. TAXI A/C. UNABLE TO DUPLICATE ITEM.

Part: FRAME — CRACKED (FS 903 RBL 90) · airframe 67,075 hrs · 10,178 cycles

DURING CURRENT HMV, A CRACK WAS FOUND ON THE INNER CHORD LOWER END OF THE RHS FRAME SEGMENT AT FS 903.5 AND RBL 90. THE CRACK IS LOCATED AT WL 190, AND WAS LOCATED AT THE 0.25 IN RADIUS TRANSITION BETWEEN THE CHORD FLANGES. A BOEING APPROVED REPAIR AND FOLLOW UP REPETITIVE INSPECTIONS WERE SET UP PER ERA 460452-14AD.

Part: FRAME — CRACKED (FS 903 LBL 90) · airframe 67,075 hrs · 10,178 cycles

DURING CURRENT HMV, A CRACK WAS FOUND ON THE INNER CHORD LOWER END OF THE LBL 90 FRAME SEGMENT AT FS 903.5. THE CRACK WAS AT WL 190, AND WAS AT THE 0.25 INCH RADIUS TRANSITION BETWEEN THE CHORD FLANGES. A BOEING APPROVED REPAIR AND FOLLOW UP INSPECTIONS WERE INSTALLED PER 460453-14AD

Part: OVEN — BURNED (GALLEY) · airframe 65,674 hrs · 10,003 cycles

MARKS AROUND OVEN AFT GALLEY TOP RIGHT F/O SIDE. FWD TO MCO AND PLACARD PER MEL M25-20-01H DEFECT, CONFIRMED-SCORCH MARKS PRESENT AT DIVIDER WALL-SEAL. INSPECTED SATIS, HOWEVER, SEAL MATING SURFACE MISSING IN LOWER CORNER SECTION. NR 3 OVEN CONSIDERED AS INOP-CB PULLED AND COLLARED. REMOVED AND REPLACED A3 OVEN OPS NORMAL.

Part: STARTER — FAILED (LT ENGINE) · airframe 64,432 hrs · 9,853 cycles

NO N2 DURING LT ENGINE START. REPLACED AND TESTED LT ENG STARTER MOTOR PER MM CKS OK.

Part: COFFEEMAKER — LOOSE (GALLEY) · airframe 62,977 hrs · 9,678 cycles

ACRID SMELLING ODOR WAS PRESENT IN AFT GALLEY. REMOVED LT COFFEE MAKER AT GALLEY 413 LT SIDE AND FN D NBR 4 AND FWD COFFEE MAKER W/HOTPLATE RESISTANCE ASSY LOOSE AND OVER DRAIN COLLECTOR. CLEANED AREA. DEFECTIVE COFFEE MAKER REPLACED ETOPS CATEGORY (F): ANY OTHER EVENT DETRIMENTAL TO ETOPS.

Part: PUMP — FAILED (HYD SYSTEM) · airframe 62,921 hrs · 9,672 cycles

AFTER PUSHBACK RT ENG HYD PRIMARY PUMP EICAS MSG. FOUND FILTER DPI POPPED. REPLACED ENGINE DRIVEN PUMP AND ALL ASSOCIATED FILTERS PER AMM. NO DEBRIS FOUND IN ANY FILTER. LEAK AND PRESSURE CHECK OK.

Part: RECEPTACLE — ARCED (ELECTRICAL POWER) · airframe 61,351 hrs · 9,472 cycles

RAMP REPORTED ELECTRICAL ARCING VISIBLE AT EXTERNAL POWER RECEPTACLE. FOUND EXTERNAL POWER RECEPTACLE PIN DAMAGED. REPLACED RECEPTACLE.

Part: LENS — MISSING (SEATS 3F & 6B) · airframe 60,269 hrs · 9,326 cycles

SEAT MOUNTED ESCAPE PATH LIGHTING AT 3F AND 6B MISSING 1 WHITE LENS AND BOTH BULBS. RELAMPED AND REPLACED WHITE LENS AT SEATS 3F AND 6B. OPS CKS OK.

Part: WIRE — SHORTED (P64 PANEL) · airframe 56,681 hrs · 8,814 cycles

LOOSE WIRE UNDER COCKPIT SUNSHADE BY P6 PANEL CAUSED SPARK WHEN MOVED. CAPPED WIRE ON THE P64 PANEL WHICH ILLUMINATES P6 FLOOD CB PANEL.

Part: VALVE — UNSERVICEABLE (NR 1 ENGINE) · airframe 56,586 hrs · 8,800 cycles

ON CLIMBOUT LT STARTER CUTOUT EICAS PER QRH TURNED OFF LEFT ENG BLEED. ON DESCENT INTO BOM LT STARTER CUTOUT EICAS MESSAGE REAPPEARED WITH BLEED OFF, LANDED BOM. REPAIRED SHORT AT PIN 6 ON C/P AT LT START VALVE AND REPLACED START VALVE.

Part: PACKING — DAMAGED (RIGHT PYLON) · airframe 55,329 hrs · 8,615 cycles

RIGHT SYSTEM HYDRAULIC QUANTITY LOW. FOUND DELTA P PACKING BLOWN OUT ON HYD PRESSURE MODULE IN RT ENG STRUT. REPLACED DELTA P AND PACKINGS PER AMM, LEAK CHECK OK.

Part: HSI — MALFUNCTIONED (COCKPIT) · airframe 52,722 hrs · 8,249 cycles

ON ARRIVAL AT GATE CREW REPORTED A PUNGENT ODOR IN COCKPIT AND CAPT HSI BRIGHTNESS FLUCTUATING. ON INSPECTION NOTICED SIMILAR ODOR FROM CAPT FWD CONSOLE AND E/E EXHAUST AREA. REPLACED CAPT HSI AND CONFIRMED COOLING FLOW GAINED ACCESS TO EQUIP. COOLING SUPPLY FAN FOUND INLET GRILL CLOGGED. CLEANED GRILL AND INSTALLED NEW SUPPLY FAN PER MM. RETURNED A/C TO NORMAL, NO ODORS IN COCKPIT, OK FOR SERVICE.

Part: IRU — OUT OF ADJUST · airframe 52,697 hrs · 8,246 cycles

FMC WAS NOT PROVIDING GOOD NAV ORIENTATION IMMEDIATELY AFTER T/O. ALL DATA WAS OFF BY APPROX 300 MILES. UPON LANDING AT SNN POS SHOWED AIRCRAFT AT GATE IN HAM. RESET AND BITE CHECK OF BOTH FMCS, NO TROUBLE. CHECKED NAV DATA BASE FOR FMC, DATABASE CORRECT. CHECKED SENSORS AND READOUT ON FMC, CDU ALL OK. CHECKED ADCS, NO FAULT FOUND. REALIGNED IRU. NO FURTHER TROUBLE. FOUND A/C TO BE IN CORRECT WORKING ORDER.

Part: LIGHT — MISSING (CABIN) · airframe 51,050 hrs · 7,998 cycles

E-PATH LENS AND LIGHT BULB MISSING AT SEAT 10FG. REPLACED SAME, OPS NORMAL.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 49,761 hrs · 7,806 cycles

SEAT ROW 21 TO ROW 30 EMERGENCY ESCAPE PATH LIGHTS INOP. T/S FOUND POWER SUPPLY HAS BLOWN FUSE. REPLACED POWER SUPPLY. OPS CKD GOOD.

Part: PRESSURE SWITCH — FAILED (HYD SYSTEM) · airframe 46,997 hrs · 7,346 cycles

IR - AFTER T/O RT ENGINE PRIMERY HYD PUMP PRESS LIGHT CAME ON OVERHEAD AND EICAS. FLUID QUANTITIES OK. REPLACED S31 PRESSURE SWITCH, OPS CHECK/LEAK CHECK OK.

Part: TURBINE BLADES — DAMAGED (NR 2 ENGINE) · airframe 45,758 hrs · 7,125 cycles

FOUND 1 HPT FIRST STG BLADE WITH HOLE ON BORESCOPE. REPLACED NR 2 ENGINE.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 39,616 hrs · 6,111 cycles

EXISTING UNIDENTIFIED REPAIR AT DOOR STA 89 AND S8L WAS REMOVED AND NEW REPAIR PER SRM INSTALLED. ER/A 364286-14 REV B.

Part: WIRE — CHAFED (NR 1 ENGINE) · airframe 36,978 hrs · 5,673 cycles

LEFT PRV EICAS MSG AT 80 KTS. TAKEOFF DISCONTINUED. REPAIRED CHAFED WIRING TO TERM 3 OF PRV AND REPLACED TERM 1 TO PRV. ALSO REPLACED PRV. PERFORMED HI-PWR RUNUP. NOTE; PRV CONTROLLER ALSO REPLACED IN COURSE OF T/S.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 36,495 hrs · 5,592 cycles

ON L/O, FOUND EMERGENCY EXIT LIGHT IN COCKPIT INOP. LIGHT LOCATED JUST ABOVE COCKPIT DOOR. TRIED BATTERY PACK, NO HELP. REPLACED LIGHT ASSY.

Part: VIDEO UNIT — SHORTED (CABIN) · airframe 34,610 hrs · 5,279 cycles

DURING FLT ROCKWELL COLLINS PAX ENTERTAINMENT SYS BOX STARTED SMOKING. REPLACED PAT. ETOPS CATEGORY ''B'': DIVERSION OR TURNBACK

Part: CHILLER — MALFUNCTIONED (AFT GALLEY)

GALLEY 413 FAULT LIGHT CAME ON. SLIGHT ELECTRIC ODOR AFTER CHILLER SHUTDOWN. INSPECTED GALLEY (413) CHILLER, OPS OK. RAN FOR 45 MIN, NO FAULT AND DETECTED NO ELECTRIC ODOR BURN.

Part: ENTERTAIN SYS — FAILED (ROW 2CE)

IN FLIGHT, STRONG ELECTRICAL BURNING SMELL AND SLIGHT HAZE IN BUSINESS ELITE AREA HAD STRONG SMELL, DEPOWERED ENTERTAINMENT SYSTEM, SMELL WENT AWAY SLIGHTLY. REPOWERED SYSTEM AND SMELL RETURNED STRONG. SHUT SYSTEM DOWN WITH VCC/ADB SWITCHES, NO EFFECT. MAINTENANCE GAVE C/B'S TO PULL IN E AND E COMPT, SMELL AND HAZE DISSIPATED SLOWLY WITH SLIGHT SMELL LINGERING OVER 1C AND 2C. SUSPECT COMING OUT OF CENTER CEILING, FWD OF PROJECTOR. E AND E COMPARTMENT HAD NO SMELL OR HAZE WHEN OPENED. TWO HOURS AFTER C/B'S SHUTDOWN, SMELL COMPLETELY GONE. REPLACED AVU AND CABLES AT SEAT 2CE.

Part: SKIN — DAMAGED (BS 89)

THE FUSELAGE SKIN AT DOOR STATION 89 AND STRINGER 8L HAS A 1 X 2 CUTOUT. THE SKIN HAS BEEN REPAIRED WITH AN ALUMINUM DOUBLER PER THE GUIDELINES OF B767 SRM 53-00-01. ER/A 364286-14 WAS ISSUED TO DOCUMENT THE REPAIR AND TO ENSURE COMPLIANCE WITH THE SRM.

Part: SCAVENGE LINE — FAILED (NR 1 ENGINE)

LT ENGINE OIL QUANTITY DROPPED TO 4 QTS IN FIRST 2 HOURS. AIRCRAFT RETURNED TO JFK. ENGINE NR 1 SHUT DOWN AFTER LANDING. FOUND NR 4 BEARING SCAVENGE LINE DAMAGED. REPLACED SAME.

Part: LIGHT — CRACKED (CABIN)

EMERGENCY FLOOR LIGHT TRACK IN AFT LEFT BUSINESS AND AFT RIGHT/LEFT COACH IS CRACKED. REPLACED DAMAGED PORTIONS OF FLOOR TRACK.

Part: COFFEEMAKER — FAILED (AFT GALLEY)

STRONG ELECTRICAL SMELL IN AFT GALLEY, UNABLE TO ISOLATE. PULLED ALL C/B IN GALLEY, STRENGTH OF SMELL CYCLED. SUSPECT CHILLER. INSPECTED OVENS/CHILLERS/CM. STRONG SMELL COMING FROM NR 1CM F/O SIDE. REPLACED COFFEEMAKER, OPS CK OK.

Part: SLIDE SENSOR — OUT OF ADJUST (LEFT WING)

AT 270 KNOTS, LEFT WING SLIDE EICAS MESSAGE ILLUMINATED. FOUND PROXIMITY SENSOR 218 OUT OF ADJUSTMENT. ADJUSTED SAME. OPS CHECK NORMAL.

Part: COMPRESSOR — DAMAGED (NR 2 ENGINE)

DURING INSPECTION, FOUND FOD TO 2ND, 3RD, 5TH AND 6TH STAGE COMPRESSOR. REPLACED ENGINE, ROUTED TO SHOP.

Part: AIR DIST — SMOKE ODOR (FWD GALLEY)

DURING CRUISE, THE ON/OFF LIGHT ON CHILLER IN FWD GALLEY WAS FLICKERING. SMOKE COMING OUT OF VENT ABOVE CIRCUIT BREAKERS. ALL NORMAL WHEN GALLEY POWER SHUTDOWN. OPERATION OF FWD CHILLER FOUND NORMAL. OPENED AND CHECKED C/B PANEL IN FWD GALLEY AND FOUND ALL OK, NO EVIDENCE OF SMOKE OR BURNED WIRES. RETURNED TO SERVICE.

Part: WIRE — SHORTED (FWD CABIN 1C)

DURING CRUISE, HAD SMOKE AND SPARKS FROM UNDER F/C SEAT 1C. FOUND WIRE FOR SEAT ADJUSTMENT MOTOR CHAFED AND SHORTED. REPAIRED WIRE, OPERATION NORMAL.