N825MH

Part: SWITCH — FAULTED (ZONE 800) · airframe 98,626 hrs · 18,382 cycles

R1 DOOR SLIDE ARMED LIGHT AT FWD F/A PANEL INOPERATIVE. R & R R1 DOOR ARMED STATUS LIGHT SWITCH ASSY AT FOWARD FAP PANEL. (1168017)

Part: LIGHT — INOPERATIVE (ZONE 800) · airframe 97,410 hrs · 18,209 cycles

SHIP 1801 1L SLIDE IS INOP. CORRECTIVE ACTION: R/R LIGHT BOARD ASSY PER B767 AMM 52-73 OPC CHECK GOOD. (7527434)

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 97,273 hrs · 18,191 cycles

ROW 41F-49F EMERGENCY LIGHTS ARE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK PER B767-400 AMM 32-51. OPERATIONAL CHECK IS NOW NORMAL. (LP #7542926)

Part: WINDOW — FAILED (ZONE 200) · airframe 96,309 hrs · 18,045 cycles

SHIP 1801 -DIV/DE- THE CREW DECLARED AN EMERGENCY WITH ATC AND DIVERTED THE AIRCRAFT TO SNN PER THE QRH, DUE TO THE F/O R3 SIDE WINDOW SHOWING INCREASING DAMAGE FROM HEAT. THE DAMAGE INCREASED RAPIDLY AND INCLUDED GLASS LAYER RIPPLING, DISCOLORATION, AND EXTREMELY HOT TO THE TOUCH. THE LANDING WAS OVERWEIGHT BUT OTHERWISE UNEVENTFUL. CORRECTIVE ACTION: MAINTENANCE REPLACED THE R3 WINDOW AND THE WINDOW HEAT CONTROL COMPUTER. THE WINDOW HEAT SYSTEM CHECKED GOOD AND THE AIRCRAFT RETURNED TO SERVICE. (LP #6661752)

Part: ELEC CONNECTOR — DISCONNECTED (ZONE 200) · airframe 96,309 hrs · 18,045 cycles

THE EMERGENCY LIGHTS FOR ROWS 50-52AB ARE INOPERATIVE. MAINTENANCE FOUND A CONNECTOR AT 52AB TO BE DISCONNECTED. THE WIRES WERE RECONNECTED AND THE OPERATIONAL CHECK WAS GOOD IAW B767-400 AMM 33-51. (LP #6661750)

Part: SKIN — DELAMINATED (ZONE 300) · airframe 100,128 hrs · 18,611 cycles

LEFT SIDE OF TAIL SHOWING PAINT LOSS OR DELAMINATION NEAR LEADING EDGE ON CAPTAINS SID. CORRECTIVE ACTION: FOUND LEFT SIDE OF TAIL DELAMINATION NEAR LEADING EDGE ON CAPTAINS SIDE AND PERFORMED INTERIM REPAIR AS PER ER/A 631907-14 (6716370)

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHTS) · airframe 92,682 hrs · 17,553 cycles

AIRCRAFT 1801, DURING SVC, FOUND ROWS 31-38 FG EMMERGENCY LIGHTS INOP. CORRECTIVE ACTION: FOUND CONNECTOR AT 32 FG DISCONNECTED. RESECURED. ALL OPS NML. (LP 5761218)

Part: SKIN — DAMAGED (LT NR 3 SLAT) · airframe 92,483 hrs · 17,520 cycles

SHIP 1801 FOUND LHW SLAT NO.3 IB INNER SURFACE WORN. CORRECTIVE ACTION: LHW SLAT NO.3 IB INNER SURFACE REPAIRED AS PER B767-400 SRM 57- 43-02-2R-1 & SRM 51-70-10-2R-4. FIG202(SHEET8) & SRM 51-70-10-2R (0351205)

Part: STIFFENER — CRACKED (FLOORBEAM) · airframe 92,483 hrs · 17,520 cycles

SHIP 1801 FOUND OUT FLOOR BEAM STIFFENER CRAKED AS BS246 BETWEEN LBL0 AND LBL30. CORRECTIVE ACTION: THE CRACKED STIFFENER AT STA 246 REMOVED AND REPLACED AS PER B767-400 SRM 51-40-02 (0349280)

Part: ROLLER TRAY — CRACKED (BS 1480) · airframe 92,483 hrs · 17,520 cycles

SHIP 1801 FOUND OUT AFT CARGO LH NO.1 ROLLER TRAY CRACKED AT BS1480. CORRECTIVE ACTION: THE CRACKED ROLLER TRAY APPLIED DOUBLER REPAIR AS PER B767-400 SRM 53-00-53-2R-1 (0346502)

Part: DOOR — FOD (L2) · airframe 92,385 hrs · 17,507 cycles

SHIP 1801 AFTER DEPARTUREFLT CREW REPORT DOOR 2L WONT ARMED. CORRECTIVE ACTION: REMOVED FOD. PERFORM OPS CHK. DOOR OPS NML. A/C OK FOR SVC (5644364)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 91,031 hrs · 17,322 cycles

SHIP 1801 EMERGENCY EXIT SIGN COVER LOOSE / LOCATIONS: 3. CORRECTIVE ACTION: EMERGENCY EXIT SIGN INTACT AT SAID LOCATION. GOOD FOR SVC. (0120392)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 90,945 hrs · 17,311 cycles

SHIP 1801 1L DOOR SHOWING OPEN. OPENED AND RESET 1L DOOR IAW AMM B767 52-11. DOOR AND INDICATIONS CHECK GOOD. (5071912)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 90,139 hrs · 17,201 cycles

SHIP 1801 - DIV - CREW REPORTED LOSS OF OIL FROM RIGHT ENGINE AT A RATE OF 1 QUART/30 MINUTES. OUT OF AN ABUNDANCE OF PRECAUTION, CREW DECIDED TO STOP SHORT. FLIGHT DIVERTED TO TPA. CORRECTIVE ACTION: REPLACED RIGHT ENGINE STARTER AND HYDRAULIC PUMP PER B767 AMM 72-64. NO FURTHER LEAKS FROM THOSE SEALS. FOUND OIL LEAKING FROM B AND C AND 6 O'CLOCK RECOUP DUCT. RAN ENGINE AT 80% N2 FOR 20 MINUTES, OIL CONSUMPTION WITHIN LIMITS. (LP 4535404)

Part: DISPLAY — SMOKE (ENTERTAIN SYS) · airframe 90,031 hrs · 17,185 cycles

SHIP 1801 -SMKE/FUME- PASSENGER ENTERTAINMENT SCREEN AT 40A SMOKING. CORRECTIVE ACTION: ITU REPLACED. (4511560)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 89,828 hrs · 17,153 cycles

SHIP 1801 NUMEROUS F/C RIGHT SIDE EMERGENCY LIGHTS INOP. CORRECTIVE ACTION: REPLACED OVHD BATTERY PACK M6756 PER B767 MM 33-51 ALL LIGHTS NOW ILLUMINATE (4598064)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 88,901 hrs · 17,027 cycles

SHIP 1801 FA CREW WEST FACILITY EMERGENCY LIGHT ON IN BUNK WITH ESCAPE HATCH. CORRECTIVE ACTION: R/R EMERGENCY EXIT LIGHT PER B767 AMM25-29. OPS CHECK GOOD. OK FOR SVC (4722565)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 88,734 hrs · 17,005 cycles

SHIP 1801 ON SVC CHK, FOUND EMERG LIGHT ON TEMP CONTROL PANEL & EMERG LIGHT AT ALT EXIT INOP IN LLCR. CORRECTIVE ACTION: R&R LLCR EMERGENCY POWER SUPPLY & BATTERY PER B767-400 AMM 25-29 . R&R BOTH LIGHTY ASSY PER B7676-400 AMM 25-29. OPS CHK GOOD (4722504)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 88,734 hrs · 17,005 cycles

SHIP 1801 FLIGHT ATTENDANTS REPORT WARM ELECTRICAL SMELL IN CREW REST COMPARTMENT. CORRECTIVE ACTION: FOUND HEATERS TO BE THE SOURCE OF ELEC SMELL. FWD TO MEL 21-66-02A. MEL PLACARD INSTALLED & "M" PROC C/W (4722506)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 88,667 hrs · 16,995 cycles

SHIP 1801 -DIV- DIVERTED TO IAD DUE TO ALL LAVS INOP. CORRECTIVE ACTION: FOUND LAV TANKS FULL. SERVICED LAV TANKS. OPS CHECKS GOOD. (4714274)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 88,239 hrs · 16,939 cycles

SHIP 1801 SLIDE INDICATOR LIGHT INOP OR DAMAGED / LOCATIONS:601. CORRECTIVE ACTION: POS 601 SLIDE INDICATOR LIGHT OK. (2755448)

Part: UNKNOWN — UNKNOWN · airframe 87,602 hrs · 16,847 cycles

SHIP 1801 - DIV - DUE TO UNRELIABLE AIRSPEED INDICATION. CORRECTIVE ACTION: R/R F/O ADM, C/W AUTOPILOT TEST AND PITOT STATIC TEST. (4159768)

Part: UNKNOWN — UNKNOWN · airframe 87,586 hrs · 16,844 cycles

SHIP 1801 -MISC/DE- CREW ELECTED DE DUE TO TE DISAGREE INDICATION DURING DESCENT. C/W QRH AND LANDED UNEVENTFULLY AT DESIRED FLAPS 20. CORRECTIVE ACTION: SUSPECTED FLAP OVERSPEED DUE TO AIRSPEED ISSUE. R/R F/O PITOT PROBE PER B767-400 AMM 34-11, OPS TEST NORMAL. FLAP SYSTEM TEST NORMAL.(4159753)

Part: NONE — NONE (SLIDE LIGHT) · airframe 87,088 hrs · 16,777 cycles

SLIDE INDICATOR LIGHT INOP OR DAMAGED / LOCATIONS: 1L. REPOSITIONED LAMP, SLIDE INDICATOR LIGHT WORKING NORMALLY. B767- 400 AMM 52-71. ITEM OK .

Part: TRACK — FOD (GIRT BAR) · airframe 86,955 hrs · 16,761 cycles

SHIP 1801 2L DOOR HARD TO ARM. CORRECTIVE ACTION: T/S PER FIM 52-11-00-815-804 B767-400. FOUND DEBRIS IN GIRT BAR TRACK AND LOCKING MECHANISM. CLEANED AND LUBRICATED PER B767-400 FIM 52-11-00-815-804. OPS CHK OK. (2574232)

Part: NONE — NONE (L2 DOOR) · airframe 86,820 hrs · 16,743 cycles

2L DOOR WILL NOT ARM. CORRECTIVE ACTION: CYCLED DOOR & ARMING LEVER AT 2L DOOR, ARMS NML OK FOR SVC.

Part: LANDING GEAR — DAMAGED (RIGHT) · airframe 92,483 hrs · 17,520 cycles

SHIP 1801 OUTBD OF RT MLG HAS BOLT PUNCTURE. CORRECTIVE ACTION: ARRIVAL PNL 651TB OUTBD OF RT MLG REPAIRED AS PER B767-400 SRM 57-51-01-2R-2. (9100304)

Part: DOOR — UNLATCHED · airframe 85,263 hrs · 16,507 cycles

SHIP 1801 AOM REPORT R3 DOOR UNLATCHED, CORRECTIVE ACTION: R/R R3 SLIDE PER A330 M/M 2566. CLOSED R3 DOOR PER A330 M/M 52-22 (9013994)

Part: NONE — NONE · airframe 85,050 hrs · 16,479 cycles

SHIP 1801 2R DOOR DOES NOT ARM CORRECTLY, CORRECTIVE ACTION: CYCLED DOOR AND ARMS PROPERLY NO TROUBLE FOUND. (9290388)

Part: NONE — NONE · airframe 84,956 hrs · 16,467 cycles

SHIP 1801 UNABLE TO ARM 2L DOOR AT DEPT. CORRECTIVE ACTION: FOUND OUTSIDE HANDLE NOT STOWED RECYCLED DOOR AND PERFORMED OPS TEST OF ARMING SYSTEM AS PER B767-400 AMM 52-12. OPS OK. (9290358)

Part: WARNING LIGHT — INOPERATIVE · airframe 84,607 hrs · 16,419 cycles

SHIP 1801 1R DOOR SLIDE, LIGHT BLINKS CONTINUALLY WITH DOOR ARMED. CORRECTIVE ACTION: SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0082:2500-0829/001 00583 PERFORMED OPS CHECK OF DOOR 1R SLIDE-RAFT ARMED WARNING SYSTEM REF B767 AMM 52-73-00. OPS NML. (2252853)

Part: GIRT BAR — DIRTY · airframe 84,511 hrs · 16,402 cycles

SHIP 1801 PRIOR TO PUSHBACK RT DOOR WOULDNT ARM, CORRECTIVE ACTION: REMOVED DEBRIS FROM GIRT BAR. OPN NORMAL (8762534)

Part: NONE — NONE · airframe 84,063 hrs · 16,323 cycles

SHIP 1801 SLIDE INDICATOR LIGHT INOP OR DAMAGED / LOCATIONS:01L. CORRECTIVE ACTION: RE-SEATED LIGHT ASSY, OPS CKS NML. REF B767 AMM 52-71. (2158216)

Part: NONE — NONE · airframe 83,626 hrs · 16,241 cycles

SHIP 1801 AT DEPT 2L DOOR WONT ARM. CORRECTIVE ACTION: REMOVED DEBRIS FROM DPPR FITTING DOOR ARMS NORMALLY (8844142)

Part: NONE — NONE · airframe 83,574 hrs · 16,232 cycles

SHIP 1801 SLIDE INDICATOR LIGHT INOP OR DAMAGED / LOCATIONS: L1, CORRECTIVE ACTION: NO FAULTS NOTED. INDICATION OPERATES NORMAL. (2101180)

Part: NONE — NONE · airframe 83,210 hrs · 16,163 cycles

SHIP 1801 FLT CREW STATES 2L DOOR WONT ARM. CORRECITIVE ACTION: CYCLED 2L DOOR HANDLE, ARMS NORMALLY OK FOR SVC PER B767-400 AMM 52-11 (8324952)

Part: NONE — NONE · airframe 83,043 hrs · 16,128 cycles

SHIP 1801 -DIV- TO ELP DUE LOW ENGINE OIL QUANTITY MESSAGE ON THE #2 ENGINE. CREW SHUTDOWN THE ENGINE WHEN OIL PRESSURE REACHED 16PSI. CORRECTIVE ACTION: FOUND #6 SCAVENGE OIL LINE LOOSE, INSPECTED AND RETORQUED. INSPECTED MCD AND OIL FILTER, NO DEFECTS NOTED. PERFORMED HIGH POWER RUN. LEAK CHECK OK. (8206280)

Part: NONE — NONE · airframe 82,613 hrs · 16,039 cycles

SHIP 1801 DURING INSPECTION FOUND LOWER AFT FAIRING FLAP DRIVE ASSEMBLY CLOSE-OUT PANEL WAS WITH DELAMINATION AND CRACK DAMAGE DAMAGE. REPAIRED PER SRM 51-70. (LP 1994929)

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHTS) · airframe 81,211 hrs · 15,718 cycles

SHIP 1801 FOUND EMERGENCY PATH LIGHTING AT ROW 37 AND 38G ARE INOPERATIVE. CORRECTIVE ACTION: FOUND CONNECTOR FOR POWER SUPPLY OFF AT ROW 38G AND RE-CONNECTED SYSTEM OPERATION IS NORMAL. (LP 7381608)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 80,586 hrs · 15,575 cycles

SHIP 1801 EMERGENCY LIGHTS FROM 6A TO L2 DOOR ARE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY BATTERY PACK. SYSTEM OPERATION IS NORMAL. (LP 7392902)

Part: SENSOR — FALSE INDICATION (FWD EQUIP BAY) · airframe 79,137 hrs · 15,226 cycles

FLIGHT 8824; MSP-HNL PERFORMED AN AIR TURN BACK DUE TO 'FWD EQUIP OVERHEAT' WARNING. CORRECTIVE ACTION: REPLACED LOW FLOW SENSOR AT FORWARD RACK AND FLIGHT DECK LOW FLOW SENSOR TS0163. SYSTEM OPERATION IS NORMAL.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 79,118 hrs · 15,221 cycles

CORROSION LEVEL: 2 CORROSION FOUND ON THE BOTTOM SURFACE OF THE STRINGER 39L , BETWEEN STA 1197+193 AND STA 1197+218 IN AFT CARGO. C/W ERA 585883-14 (LP 1543064)

Part: SKIN — CRACKED (FUSELAGE) · airframe 79,118 hrs · 15,221 cycles

LEFT UPPER FUSELAGE SKIN AT STA 1660 BETWEEN S3L AND S4L AS MARKED POINT FOUND CRACK. C/W ERA 586296-14 (LP 1543070)

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 79,118 hrs · 15,221 cycles

CORROSION LEVEL: 2 WING CENTER SECTION UPPER SURFACE AT STA 955 RBL 76 FOUND CORROSION C/W ERA 585848-14 (LP 1543055)

Part: SKIN — SCRATCHED (FUSELAGE) · airframe 79,118 hrs · 15,221 cycles

THE SCRATCH OF THE LH SIDE FUSELAGE SKIN AFT L-3 PASSENGER ENTRY DOOR AT STA 1537, BETWEEN S-21L AND S-22L FOUND OVER THE LIMIT. C/W ERA 38217-14 (LP 1540988)

Part: SPAR — CRACKED (VERTICAL STAB) · airframe 79,118 hrs · 15,221 cycles

THE AUXILIARY SPAR WEB AROUND THE SCREW HOLE WHERE IT ABOVE THE LH SIDE AUX SPAR CHORD AT APPROXIMATELY FSS 193 FOUND CRACK. REPAIRED PER ERA 585991-14 (LP 15411190)

Part: SKIN — DELAMINATED (VERTICAL STAB) · airframe 79,118 hrs · 15,221 cycles

LH SIDE INTERNAL SKIN OF THE VERTICAL STABILIZER FOUND DELAMINATION AT FSS 170 TO FSS 220. 19 NICH AFT OF THE AUX FRONT SPAR. REPAIRED PER ERA 585841-14 (LP 1540344)

Part: SKIN — DELAMINATED (VERTICAL STAB) · airframe 79,118 hrs · 15,221 cycles

LH SIDE VERTICAL STABILIZER SKIN BETWEEN AUX SPAR AND FRONT SPAR AT STA FSS 245 TO STA FSS 270 FOUND DELAMINATION. C/W ERA585841. (LP 1540341)

Part: SKIN — DELAMINATED (VERTICAL STAB) · airframe 79,118 hrs · 15,221 cycles

LH SIDE VERTICAL STABILIZER SKIN BETWEEN AUX SPAR AND FRONT SPAR AT STA FSS 220 TO STA FSS 245 FOUND DELAMINATION. REPAIRED PER ERA 585841-14 (LP 1540339)

Part: SKIN — CRACKED (FUSELAGE) · airframe 79,118 hrs · 15,221 cycles

RH SIDE FUSELAGE SKIN AT BS STA 1725.5, NEAR THE S-7R AS MARKED POINT FOUND CRACK. REPAIRED PER SRM 53-80-01 (LP 1540356)

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 79,118 hrs · 15,221 cycles

CORROSION LEVEL: 2 THE SHEAR TIE UPPER SURFACE AND VERTICAL SURFACE FOUND CORROSION IN AFT CARGO AT STA 1197+209, BETWEEN S-39R AND S-39L. FOUND OUT OF LIMITS. REPLACED SHEAR TIE. (LP 1538173)

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 79,118 hrs · 15,221 cycles

FWD GALLEY AREA FLOOR SUPPORT STRUCTURE AT STA246 RBL 63 FOUND CRACK ON LOWER WEB. REPAIRED PER ERA 586031-14. (LP 1536093)

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 79,118 hrs · 15,221 cycles

CORROSION LEVEL: 2 SEAT TRACK-CABIN SEAT TRACK AT STA 1480 RBL 54.75 FOUND CORROSION OUT OF LIMITS. REPLACED SEAT TRACK. (LP 1536081)

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 79,118 hrs · 15,221 cycles

CORROSION LEVEL: 2 THE SHEAR TIE UPPER SURFACE AND VERTICAL SURFACE FOUND CORROSION IN AFT CARGO AT STA1197+132,BETWEEN S-39R AND S- 39L FOUND OUT OF LIMITS. REPLACED SHEAR TIE. (LP 1533335)

Part: WEB — CRACKED (NR 2 PYLON) · airframe 79,118 hrs · 15,221 cycles

#2 ENG PYLON STRUT UPPER WEB I/B WIRING CUT OUT FOUND CRACKED AT NAC STA223 TO NAC STA235. (LP 1533329)

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 79,118 hrs · 15,221 cycles

CORROSION LEVEL: 2 THE SHEAR TIE UPPER SURFACE FOUND CORROSION IN AFT CARGO AT STA1197+231,BETWEEN S-39L AND S-39R OUT OF LIMITS. REPLACED SHEAR TIE. (LP 1533276)

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 79,118 hrs · 15,221 cycles

CORROSION LEVEL: 2 THE SHEAR TIE UPPER SURFACE FOUND CORROSION IN AFT CARGO AT STA1197+231,BETWEEN S-39L AND S-39R OUT OF LIMITS. REPLACED SHEAR TIE. (LP 1533285)

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 79,118 hrs · 15,221 cycles

CORROSION LEVEL: 2 THE SHEAR TIE UPPER SURFACE AND VERTICAL SURFACE FOUND CORROSION IN AFT CARGO AT STA1197+168,BETWEEN S-39R AND S-39 OUT OF LIMITS. REPLACED SHEAR TIE.

Part: WEB — CRACKED (NR 1 PYLON) · airframe 79,118 hrs · 15,221 cycles

NO.1 PYLON WIRE BUNDLE WEB CUTOUT AT NAC STA255 FOUND CRACK. C/W REPAIRED PER ERA585803-14 (LP 1533339)

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 79,118 hrs · 15,221 cycles

CORROSION LEVEL: 2 FOUND CORROSION ON THE UPPER SURFACE AND VERTICAL SURFACE OF THE SHEAR TIE IN AFT CARGO AT STA 1197+66,BETWEEN S- 39L AND S-38L. FOUND OUT OF LIMITS AND REPLACED SHEAR TIE. (LP 1532204)

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 79,118 hrs · 15,221 cycles

CORROSION LEVEL: 2 THE SHEAR TIE UPPER SURFACE AND VERTICAL SURFACE FOUND CORROSION IN AFT CARGO AT STA1197+132,BETWEEN S-38R AND S- 39R OUT OF LIMITS. REPLACED SHEAR TIE. (LP 1532538)

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 79,118 hrs · 15,221 cycles

CORROSION LEVEL: 2 FOUND CORROSION ON THE UPPER SURFACE AND VERTICAL SURFACE OF THE SHEAR TIE IN AFT CARGO AT STA 1197+66,BETWEEN S- 39L AND S-39R OUT OF LIMITS. REPLACED SHEAR TIE. (LP 1532460)

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 79,118 hrs · 15,221 cycles

CORROSION LEVEL: 2 FOUND CORROSION ON THE UPPER SURFACE AND VERTICAL SURFACE OF THE SHEAR TIE IN AFT CARGO AT STA 1197+88,BETWEEN S- 39R AND S-38R OUT OF LIMITS. REPLACED SHEAR TIE. (LP 1532432)

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 79,118 hrs · 15,221 cycles

CORROSION LEVEL: 2 FOUND CORROSION ON THE UPPER SURFACE AND VERTICAL SURFACE OF THE SHEAR TIE IN AFT CARGO AT STA 1197+88,BETWEEN S- 39R AND S-39L OUT OF LIMITS. REPLACED SHEAR TIE. (LP 1532474)

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 79,118 hrs · 15,221 cycles

CORROSION LEVEL: 2 THE SHEAR TIE UPPER SURFACE FOUND CORROSION IN AFT CARGO AT STA1263,BETWEEN S-39L AND S-39R OUT OF LIMITS. REPLACED SHEAR TIE. (LP 1532409)

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 79,118 hrs · 15,221 cycles

CORROSION LEVEL: 2 THE SHEAR TIE UPPER SURFACE AND VERTICAL SURFACE FOUND CORROSION IN AFT CARGO AT STA1197+110,BETWEEN S-38R AND S- 39R AND FOUND OUT OF LIMJITS. REPLACED THE SHEAR TIE. (LP 1532522)

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 79,118 hrs · 15,221 cycles

THE SHEAR TIE UPPER SURFACE AND VERTICAL SURFACE FOUND CORROSION IN AFT CARGO AT STA1197+168,BETWEEN S-39L AND S- 38L. LOG-PAGE UPDATED MEASURED THE CLEAN UP SHEAR TIE DEPTH IS 0.006" REMAIN THICKNESS IS 0.034" THE ORIGINAL THICKNESS IS 0.040" ALLOWABLE DAMAGE .IS 10% ORIGINAL THICKNESS AND FOUND OUT OF LIMIT AS PER B767-400 SRM 53-00-07 ALLOWABLE DAMAGE .2 RELEASE:59.00 DATE:19 DEC 19. REMOVED AND REPLACED THE SHEAR TIE AS PER B767-400 SRM 51-40-02 (1531454)

Part: STRUCTURE — CRACKED (NR 2 NACELLE) · airframe 82,181 hrs · 15,942 cycles

DURING INSPECTION STAG FOR MAINTENANCE H CHECK FOUND CRACK COMMON TO THE #2 PYLON UPPER SPAR WEB AT NAC STA 221.25-237 AT POWER FEEDER CABLE CUTOUT TO THE INBOARD FORWARD NUTPLATE. C/W ERA 585804-14. (LP 1531838)

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 79,118 hrs · 15,221 cycles

FOUND CORROSION ON THE UPPER SURFACE AND VERTICAL SURFACE OF THE SHEAR TIE IN AFT CARGO AT STA 1197+88,BETWEEN S- 39L AND S-38L. LOG-PAGE UPDATED MEASURED THE CLEAN UP SHEAR TIE DEPTH IS 0.007".REMAIN THICKNESS IS 0.033" THE ORIGINAL THICKNESS IS .0.040" ALLOWABLE DAMAGE IS .10% ORIGINAL THICKNESS AND FOUND OUT OF LIMIT AS PER B767-400 SRM 53-00-07 ALLOWABLE DAMAGE .2 RELEASE:59.00 DATE:19 DEC 19. AND REMOVED AND REPLACED THE SHEAR TIE AS PER B767-400 SRM 51-40 -02 RELEASE (1531429)

Part: SPAR — CRACKED (NR 2 NAC STRUT) · airframe 82,181 hrs · 15,942 cycles

DURING HEAVY CHECK A CRACK WAS NOTED ON STRUT #2 FWD UPPER SPAR. REFER TO ERA 585799-14AD. (LP 1528295)

Part: NONE — NONE · airframe 82,238 hrs · 15,958 cycles

DURING INSPECTION MAINTENANCE FOUND #1 PYLON FWD UPPER SPAR WEB A TNAC STATION 221.25-237.5 AT POWER FEEDER CABLE CUTOUT CRACKED. REPAIRED PER ERA 585803-14. (LP 1528007)

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 78,647 hrs · 15,159 cycles

EXT EMER LET @ DOOR 4L INOP C/A REP PWR SUPPLY & BATT PACK M739 REF B767-400 M/M 33-51. LT OPS CK GOOD. (6221800)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 78,501 hrs · 15,141 cycles

4L OVERHEAD EMERGENCY EXIT LIGHT AND EMERGENCY LIGHT OUTSIDE 4L DOOR INOP R/R BATTERY AND CHARGER IAW B767 AMM 33-51 AT 4R DOOR NO HELP R/R BATT PACK FOR 4L DOOR IAW B767-400 AMM 33-51 AND RELAMPED EXT LIGHT OPS CK GOOD (6389839)

Part: HEATER — ODOR (CABIN) · airframe 77,692 hrs · 15,017 cycles

IMMEDIATELY AFTER T/O F/A CALLED COCKPIT TO SAY THEY HAD A BURNING ODOR. INVESTIGATION FOUND L1 SUPPLEMENTAL HEAT VERY HOT. ODOR DISAPPEARED AFTER A FEW MINS. T/S C/O, SLIGHT ELECTRICAL SMELL NOTED FROM DOOR L1 SUPPLEMENTAL FLOOR HEATER. CONNECTOR AND WIRING INSPECTED WITH NIL FAULTS NOTED. L1 DOOR HEATER DEFERRED PER MEL 21-45-03, M PROC COMPLIED WITH, CBS D1 & D2 P36 PULLED AND COLLARED. PLACARD INSTALLED. AS A PRECAUTION BOTH PACKS RAN, RE-CIRC FANS, ALL LIGHTS IN GALLEY & FWD CABIN INSPECTED. GALLEY OVENS & CHILLERS, ALL IFE MONITORS CHECKED WITH NIL FAULTS NOTED. R/R L1 ENTRY DOOR HEATER PER B767-400 21-45 OPS CHK NML A/C OK FOR SVC PLACARD AND MEL RMVD. (LP6556016)

Part: HEATER — FAILED (PITOT HEAD) · airframe 76,117 hrs · 14,795 cycles

ATB - FIRST OFFICER PITOT HEAT FAILED AFTER TAKEOFF ROTATION. MAINTENANCE REPLACED PROBE AND SYSTEM OPERATION CHECKS NORMAL. AIRCRAFT RTS.

Part: UNKNOWN — ODOR (AFT GALLEY) · airframe 76,018 hrs · 14,782 cycles

SLIGHT ELECTRICAL BURNING ODOR DETECTED IN AFT GALLEY. DISSIPATED AFTER GALLEY LIGHTS WERE LOWERED REMOVED, CLEANED AND INSPECTED AFT GALLEY VENT FILTERS FLOW NORMAL. INSPECTED RECIRC. FAN FILTERS AND ASSOCIATED COMPONENTS. NO DEFECTS NOTED. NO ABNORMAL SMELLS NOTED NOTIFIED OPS CHECKED ALL AFT GALLEY COFFEEMAKERS NO DEFECTS NOTED.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 75,808 hrs · 14,750 cycles

SHIP 1801 - ATO - CREW REPORTED WINDSHEAR WARNING AT 70KTS AND EXECUTED REJECTED TAKE-OFF. CORRECTIVE ACTION: CREW TESTED WEATHER RADAR AND ALL CHECKED GOOD. CONTINUED IN DEPARTURE SEQUENCE AND PERFORMED NORMAL TAKE-OFF.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 75,201 hrs · 14,651 cycles

EXIT LIGHTS BY 4L DOOR INOPERATIVE. REPLACED BATTERY PACK. SYSTEM OPERATION IS NORMAL.

Part: RADAR — MALFUNCTIONED (WX SYSTEM) · airframe 73,934 hrs · 14,483 cycles

SHIP 1801 - ABORTED TAKEOFF AT 90 KNOTS DUE TO AUDIBLE WINDSHEAR. CORRECTIVE ACTION: REPLACED WEATHER RADAR TRANSCEIVER. PERFORMED HIGH ENERGY STOP INSPECTION.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 73,571 hrs · 14,430 cycles

DURING SERVICE VISIT IN ATL, HEAVY CORROSION FOUND ON BELLY SKIN AT STA 1081 C/W ERA 572350-14.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,571 hrs · 14,430 cycles

DURING SERVICE CHECK ON WALK AROUND FOUND TWO CRACKS ON LOWER SKIN JUST AFT OF MAIN GEAR DOOR, BELLY SKIN. REPAIRED DAMAGED SKIN IAW ERA 572350-14.

Part: SKIN — DENTED (BS 1551) · airframe 71,811 hrs · 14,182 cycles

FUSELAGE EXTERNAL SKIN WAS DENTED AT BS 1551, BETWEEN STRINGERS 23L AND 24L. THE DENT WAS OUT OF LIMITS. REPAIRED IAW SRM 53-00-01, AND ERA 568948-14.

Part: FLOORBEAM — CORRODED (BS 1439) · airframe 71,811 hrs · 14,182 cycles

FOUND THE CABIN FLOORBEAM LOWER TEE FASTENER HOLE CORRODED AT BS 1439, LBL 35. REPAIRED IAW ERA 568917-14.

Part: FAILSAFE — CRACKED (BS 955) · airframe 71,811 hrs · 14,182 cycles

DURING PERFORMANCE OF AMDS CARD 5312-01170-05, UT INSPECTION ON THE BS 955 FAILSAFE STRAP, FOUND A CRACK INDICATION. REPAIRED IAW 5312-01170-10A-02.

Part: FAILSAFE — CRACKED (BS 955) · airframe 71,811 hrs · 14,182 cycles

DURING PERFORMANCE OF AMDS CARD 5312-01170-05, HFEC OPEN HOLE AND HFEC SURFACE INSPECTION ON THE BS 955 FAILSAFE STRAP FOUND CRACKED. REPAIRED IAW ERA 568799-14.

Part: FAILSAFE — CRACKED (BS 955) · airframe 71,811 hrs · 14,182 cycles

DURING PERFORMANCE OF AMDS CARD 5312-01170-05, HFEC OPEN HOLE INSPECTION, ON THE BS 955 FAIL SAFE STRAP AT THE LWR OF THE THREE FASTENER HOLES FOUND LOWEST HOLE TO BE CRACK AT 2 O'CLOCK AND 7 O'CLOCK. C/W ERA 568799-14.

Part: SHEAR TIE — CORRODED (BS 1307) · corrosion level 2 · airframe 71,811 hrs · 14,182 cycles

AFT CARGO BAY SHEAR TIE WAS CORRODED AT BS 1307, STRINGERS 39L TO 39R. FOUND OUT OF LIMITS. REPLACED IAW SRM 53-00-07, AND 51-40-02.

Part: SHEAR TIE — CORRODED (BS 1285) · corrosion level 2 · airframe 71,811 hrs · 14,182 cycles

AFT CARGO BAY, FOUND TWO SHEAR TIES CORRODED AT BS 1285 BETWEEN STRINGER 39L AND 38R, FOUND OUT OF LIMITS AND REPLACED IAW SRM 51-40-02, AND 53-00-07.

Part: STIFFENER — CRACKED (BS 287) · airframe 71,811 hrs · 14,182 cycles

MFEC INSPECTION FOUND ONE CRACK, APPROXIMATELY 0.80 IN LENGTH ON THE NOSE WHEEL WELL LT VERTICAL STIFFENER AT BS 287, WL 159 TO WL 185. THE STIFFENER WAS REPAIRED.

Part: STIFFENER — CRACKED (BS 287) · airframe 71,811 hrs · 14,182 cycles

DURING AN MFEC INSPECTION, FOUND ONE CRACK APPROXIMATELY .0.80 IN LENGTH, ON THE NOSE WHEEL WELL RT VERTICAL STIFFENER AT BS 287, WL159 TO WL 185. REPAIRED.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHTS) · airframe 70,879 hrs · 14,055 cycles

DURING A SERVICE CHECK, FOUND THE EMERGENCY LIGHTS OUT AT 23R TO 27R. FOUND THE CONNECTOR AT SEAT 23FG DISCONNECTED. CONNECTED THE CONNECTOR AND OPS CHECKED GOOD.

Part: HANDLE — BROKEN (R3 DOOR ASSIST) · airframe 69,708 hrs · 13,885 cycles

EMERGENCY R3 DOOR HANDLE BROKEN. INSTALLED AN ASSIST HANDLE. CHECKED NORMAL. OK FOR SERVICE.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 69,160 hrs · 13,813 cycles

DURING A SERVICE CHECK, FOUND THE EMERGENCY LIGHT BENEATH THE STAIRS INOPERATIVE. ALL BULBS BURNED OUT. REPLACED THE BULBS IAW AMM 33-51 OPS NORMAL.

Part: DOOR FRAME — DIRTY (R4 DOORWAY) · airframe 68,975 hrs · 13,791 cycles

R4 DOOR SLIDE INDICATIOR INOPERATIVE. CLEANED DEBRI FROM DOOR FRAME SURROUNDING AND OPERATED DOOR, LIGHT WORKS OK, INDICATIONS ARE OK. ARMED AND DISARMED OK.

Part: BUSTLE — OUT OF ALIGNMENT (R4 DOOR) · airframe 68,902 hrs · 13,782 cycles

R4 DOOR INTERIOR FRAME APPEARS TO BE BENT. LOWER PART OF DOOR APPEARS TO BE DAMAGED. FOUND THE BUSTLE NOT ALIGNED WITH DOOR, ALIGNED THE BUSTLE, DOOR WORKS NORMAL. OK FOR SERVICE.

Part: LAMP — INOPERATIVE (ARMED INDICATOR) · airframe 68,829 hrs · 13,773 cycles

R4 DOOR SLIDE ARMED LIGHT INOPERATIVE. THE SLIDE ARMED LIGHT CHECKED. TROUBLESHOT IAW FIM 52-73, SSM 52-73, SM 32-09-01, AND SSM 32-09. REPLACED THE LAMP, OPS CHECKED OK. (3950481).

Part: GIRT BAR — OBSTRUCTED (R4 DOOR SLIDE) · airframe 68,829 hrs · 13,773 cycles

R4 DOOR WOULD NOT ARM. THE DOOR WAS INSPECTED AND DEBRIS FOUND OBSTRUCTING THE GIRT BAR FITTING. THE DEBRIS WAS REMOVED AND ARM/DISARM LEVER CYCLED MULTIPLE TIMES, NORMAL, OPERATES FREELY. SYSTEM SERVICEABLE.

Part: FUSE — INOPERATIVE (EMERGENCY LIGHTS) · airframe 68,201 hrs · 13,698 cycles

L2 EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED THE FUSE IN THE BATTERY PACK SUPPLY IAW WDM 33-51.

Part: LIGHT — INOPERATIVE (CREW REST) · airframe 67,633 hrs · 13,631 cycles

EMERGENCY EXIT SIGNS INOPERATIVE / LOCATIONS 900. ALL EMERGENCY LIGHTS AND SIGNS OPS NML AT THIS TIME. EXIT LIGHT IN CREW REST RELAMPED.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 67,287 hrs · 13,586 cycles

THE L3 DOOR EMERGENCY LIGHTS ARE INOPERATIVE. R & R THE POWER SUPPLY.

Part: TRUNNION — DAMAGED (FWD) · airframe 78,541 hrs · 15,146 cycles

FWD TRUNNION BEARING STRESS STRAP HOLE TOOLING DAMAGED. REPAIRED PER SECTION 1 ER/A 557794-14AD.

Part: PLENUM — CRACKED (AC BAY) · airframe 66,611 hrs · 13,505 cycles

FOUND PLENUM CRACKED. REPLACED LT PLENUM (FAN INLET DIFFUSER HOUSING) PER WORKCARD 2151-4303.

Part: LENS — DAMAGED (CABIN) · airframe 66,530 hrs · 13,495 cycles

FOUND ON SERVICE CHECK. INTERIOR EMERGENCY LIGHT LENS DAMAGED 2 EA LOC 603. REPLACED LENS.

Part: LIGHT — DAMAGED (CABIN) · airframe 66,530 hrs · 13,495 cycles

FOUND ON SERVICE CHECK. EMERGENCY LIGHT ASSY DAMAGED AT DOOR 1R. REPLACED LENS ASSY. OPS CK GOOD.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 65,907 hrs · 13,407 cycles

EMERGENCY LIGHT LENS MISSING FROM CONTROL PANEL. REPLACED THE LENS IAW AMM 33-51.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHTS) · airframe 60,640 hrs · 12,736 cycles

DURING SERVICE CHECK, FOUND EMERGENCY LIGHTS INOPERATIVE AND EXIT SIGNS AFT GALLEY OVERHEAD INOPERATIVE. FOUND HARNESS PLUG LOOSE UNDER SEAT 15FG. SECURED SAME AND FOUND C/P ON POWER SUPPLY M1210 LOOSE. SECURED SAME.

Part: SKIN — CORRODED (HORIZONTAL STAB) · airframe 54,228 hrs · 11,922 cycles

FOUND SURFACE CORROSION ON UPPER EXTERNAL SURFACE OF HORIZONTAL STABILIZER CENTER SECTION BETWEEN 1725-1809, RBL5. REPAIR IAW PRI 524542-14, REV 0, 1 & 2. PRI 524542-14, REV 0, 1 & 2.

Part: STRINGER — CORRODED (BS 1197) · airframe 54,228 hrs · 11,922 cycles

AFT CARGO BAY BETWEEN BS 1197+132-1197+154 S37R, FOUND CORRODED. REPAIRED IAW PRI 524527-14, REV 0 & REV 1. PRI 524527-14, REV 0 & REV 1.

Part: FAILSAFE — CRACKED (BS 955) · airframe 54,228 hrs · 11,922 cycles

HFEC OPEN HOLE INSPECTION CARRIED OUT, FOUND HOLE, ONE CRACK ON RT SIDE BS 955, FAILSAFE STRAP AT LOWER OF THE THREE FASTENER HOLES. REPAIRED IAW PRI 524525-14AD, REV O AND REV 1. PRI 524525-14AD, REV 0 AND REV 1.

Part: STRINGER — CORRODED (BS 1197) · airframe 54,228 hrs · 11,922 cycles

AFT CARGO BAY BETWEEN BS 1197+132 -1197+154 S39R, FOUND CORRODED. ACCOMPLISHED REPAIR IAW PRI 524527-14, REV 0 & REV 1. PRI 524527-14, REV 0 & REV 1.

Part: SKIN — CORRODED (BS 1197) · airframe 54,228 hrs · 11,922 cycles

AFT CARGO BAY BS 1197+185, S39R INNER SKIN FOUND BULGED. REPAIRED IAW PRI 524527-14, REV 0 & REV 1. PRI 524527-14, REV 0 & REV 1.

Part: FRAME — CRACKED (BS 1809 BULKHEAD) · airframe 54,228 hrs · 11,922 cycles

AFTER AN HFEC INSPECTION, FOUND A CRACK INDICATION ON BS 1809 BULKHEAD, RT FWD OUTER FRAME BETWEEN STRINGERS 6 - 7R. REPAIRED IAW SRM 53-80-08, REPAIR 9.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHT) · airframe 49,427 hrs · 11,305 cycles

ON SERVICE CHECK, FOUND EMERGENCY LIGHTS ON SEAT 30 A/B THRU 42 A/B INOPERATIVE. RT AND RT CHARGER AT SEAT 32 A/B, PN 0717-02-030, LIGHT CHECKED GOOD.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHT) · airframe 49,086 hrs · 11,265 cycles

EMGENCY LIGHT BATTERY PACK FAILED TEST IAW CHECK 74. R & R BATTERY PACK M1208 IAW AMM 33-51-07, OPS OK.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 46,724 hrs · 10,975 cycles

EMERGENCY LIGHTS AT ROW 20AB THRU 27AB ARE INOPERATIVE. BATTERY CHARGER REPLACED. SYSTEM OPS NORMAL.

Part: BATTERY — WEAK (EMERGENCY LIGHT) · airframe 45,931 hrs · 10,875 cycles

EMERGENCY EXIT SIGN NEAR 30AB/L3 DOOR DIM. MAINTENANCE FOUND BATTERY AT CHARGER M7236 WEAK AND REPLACED BATTERY. SYSTEM OPERATION IS NORMAL.

Part: POWER SUPPLY — DAMAGED (EMERGENCY LIGHTS) · airframe 44,695 hrs · 10,720 cycles

DURING OPS 6803, FOUND EMERGENCY PATH BATTERY MOUNT CAMLOCK BROKEN ON POWER SUPPLY M6758. REPLACED POWER SUPPLY. SYSTEM OPERATION IS NORMAL.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 44,695 hrs · 10,720 cycles

BATTERY PACK M732 FAILED AND REPLACED. SYS OPS NORMAL.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 44,688 hrs · 10,719 cycles

DURING OPS 6803 BATTERY PACKS M730 M6756 M736 M737 M738 FAILED. REPLACED. SYSTEM OPERATION IS NORMAL.

Part: MODULE — INOPERATIVE (CABIN) · airframe 44,385 hrs · 10,679 cycles

DURING DRC MAINTENANCE FOUND L1 R1 DOOR EMERGENCY LIGHTS INOPERATIVE. POWER SUPPLY MODULE AT L1 DOOR WAS REPLACED. SYSTEM OPERATION IS NORMAL.

Part: CONNECTOR — LOOSE (CABIN) · airframe 44,075 hrs · 10,637 cycles

EMERGENCY PATH LIGHTS AT ROWS 21-27 ARE INOPERATIVE. MAINTENANCE FOUND CONNECTOR D21160 LOOSE AND RE-SECURED. SYSTEM OPERATION IS NORMAL. ETOPS CATEGORY 'E': PROBLEMS WITH SYSTEMS CRITICAL TO ETOPS

Part: BATTERY — DISCHARGED (CABIN) · airframe 43,214 hrs · 10,531 cycles

ON DRC MAINTENANCE FOUND THE EMERGENCY LIGHTS AT ROW 30AB - 44AB HAD A BATTERY FAULT AND REPLACED THE BATTERY. SYSTEM OPERATION IS NORMAL.

Part: SOCKET — DIRTY (EXTERIOR) · airframe 42,540 hrs · 10,446 cycles

MAINTENANCE FOUND THE EMERGENCY ESCAPE LIGHTS AT DOOR 3L, THE AISLE EXIT SIGN, AND OUTSIDE FUSELAGE LIGHTS ALL TO BE DIM. AFTER CLEANING BULB AND SOCKET OUTSIDE OF DOOR L3 THE OPERATION OF THE LIGHTS WAS NORMAL.

Part: SKIN — DENTED (FS 1506-1514) · airframe 39,527 hrs · 10,062 cycles

FUSELAGE SKIN DENTED AT FS 1506 & 1514. REPAIRED IAW ERA 482800-14AD.

Part: SHUTOFF VALVE — MALFUNCTIONED (BLEED AIR SYS) · airframe 37,700 hrs · 9,843 cycles

AFTER T/O RECEIVED RT HPSOV EICAS MSG. UNABLE TO RESET. RETURN TO ATL DUE TO GATE AND CREW AVAILABILITY. FWD TO MCO /PLAC PER MEL 36-11-02 HPSOV LOCKED CLOSED NR 2 ENG (ODI 2010-D0925) (DL764101994).

Part: UNKNOWN — ODOR (CABIN) · airframe 35,455 hrs · 9,553 cycles

DIVERSION DUE TO ODOR IN AFT CABIN. MX IN PROGRESS.

Part: TURBINE — ODOR (APU) · airframe 35,445 hrs · 9,551 cycles

DURING THE PUSH BACK, SMOKE ENTERED THE CABIN. RETURN TO GATE. AMM 21-00-21-102-001. NO SMOKE OR OIL ODOR FELT IN THE CABIN. CAUSE OF SMOKE DETERMINED TO BE THE APU. LOSS OF OIL FROM APU NOTED.

Part: O-RING — LEAKING (SPOILER ACTUATOR) · airframe 31,504 hrs · 9,064 cycles

FLIGHT 130/27 ATB TO ATL - DUE TO CTR SYS HYD QUANTITY DROPPING. NO FURTHER INFO AT THIS TIME. FOUND O-RING LEAKING AT THE FILTER PLUG OF THE NR 4 SPOILER ACTUATOR. REPLACED O-RING, LEAK CKS OK.

Part: TRANSPONDER — FAILED (TCAS) · airframe 30,981 hrs · 9,003 cycles

MODE C REPORTED INOP BY BOTH GROUND AND TOWER. TCAS CHECKS GOOD. PERFORMED TEST OF BOTH ATC TRANSPONDERS. NO DEFECTS. ALL CHECKS NORMAL. OK FOR SERVICE, TESTED WITH ATC.

Part: WARNING MESSAGE — ILLUMINATED · airframe 30,603 hrs · 8,958 cycles

ACFT RTB AFTER CREW REPORTED YSM AND F/O DISPLAY TRU STATUS MESSAGES. CREW LEFT RUNWAY AND RETURNED TO GATE IN ORDER TO ATTEMPT RESET AND THEN PLACE ITEMS ON FLIGHT CREW PLACARD AS PER MCC TLX. THIS MSG COULD APPEAR IF ACFT ON BATTERY POWER ONLY FOR 1 MIN. ACFT DOWN POWERED MCDP MSG CLEARED AND STS M CLEARED. MCO AND PLACARD REMOVED.

Part: PSEU — MALFUNCTIONED (CARGO DOOR) · airframe 30,491 hrs · 8,945 cycles

NUMEROUS ABNORMAL CAUTION MSGS ON TAXI OUT. DOOR MSG BULK CARGO. CLEARED ALL MSG. REPLACED PSEU, BIT CK OK. NO ABNORMAL CAUTION MSG OK FOR SVC.

Part: UNKNOWN — MALFUNCTIONED (VHF SYSTEM) · airframe 26,037 hrs · 8,433 cycles

LEFT VHF PANEL STARTED DISPLAYING FAIL INTERMITTENTLY THEN CONTINUOUSLY. RESET CB, FAIL WENT AWAY BUT COULD NOT TRANSMIT OR RECEIVE ON VHF OR STACOM. RT VHF AND STACOM WAS ABLE TO RECEIVE BUT NOT TRANSMIT. AFTER 10 MIN, RT VHF COULD TRANSMIT ON A HANDFULL OF FREQUENCIES ACARS COULD RECEIVE, BUT NOT TRANSMIT. ACARS AND ATC INTERMITTENT. OPN OF ALL RADIOS NORMAL ON GROUND IN GRU. SWAPPED LT AND CENTER TRANSCEIVER AND LT AND CENTER RTPS AS PRE-CAUTION. CLEANED LT/RT VHF ANTENNA CONNECTORS. PERFORMED LIGHTNING STRIKE AND OVWT LDG INSPECTION ATC/VHF/SATOM/ACARS ALL TESTS NORMAL.

Part: CHARGER — INOPERATIVE (BS 841 LBL 94) · airframe 25,764 hrs · 8,399 cycles

BATTERY CHARGER M6759 STA 841 LBL 94 LIGHTS INOP AFTER 5 MINUTES. REMOVED AND REPLACED BATTERY CHARGER DURING HMV 1 AT TIMCO AT GSO ON NR 44973.

Part: CHARGER — INOPERATIVE (STA 401 RBL 95) · airframe 25,764 hrs · 8,399 cycles

BATTERY CHARGER M730 STA 401 RBL 95 LIGHTS INOP AFTER 5 MINUTES. REMOVED AND REPLACED BATTERY CHARGER OPS CK GOOD. REPLACED DURING HMV1 ON N/R 44971 AT TIMCO IN GSO.

Part: BATTERY — INOPERATIVE (BS 1545 RBL 53) · airframe 25,764 hrs · 8,399 cycles

BATTERY AT CHARGER M12 STA 1545 RBL 53 BATTERY WON`T CHARGE. REMOVED AND REPLACED BATTERY, DURING HMV1 AT TIMCO IN GSO ON NR 44981.

Part: CHARGER — INOPERATIVE (BS 1384 RBL 95) · airframe 25,764 hrs · 8,399 cycles

BATTERY CHARGER M734 STA 1384 RBL 95 LIGHTS INOP AFTER 5 MINUTES. REMOVED AND REPLACED BATTERY CHARGER M734 ON NR 44975, DURING HMV 1 AT TIMCO IN GSO.

Part: CHARGER — INOPERATIVE (BS 654A LBL 94) · airframe 25,764 hrs · 8,399 cycles

BATTERY CHARGER M7235 STA 654A PLUS 33 LBL 94 LIGHTS INOP AFTER 5 MINUTES. REMOVED AND REPLACED BATTERY CHARGER M7235 ON NR 44972, DURING HMV AT TIMCO IN GSO.

Part: CHARGER — INOPERATIVE (BS 1197 LBL94) · airframe 25,764 hrs · 8,399 cycles

BATTERY CHARGER M7236 STA 1197 PLUS 77 LBL 94 LIGHTS INOP AFTER 5 MINUTES. REMOVED AND REPLACED BATTERY CHARGER M7236 DURING HMV 1 AT TIMCO IN GSO ON NR 44974.

Part: CHARGER — INOPERATIVE (BS 284 LBL 53) · airframe 25,764 hrs · 8,399 cycles

BATTERY CHARGER M1208 STA 284 LBL 53 INOP. REMOVED AND REPLACE BATTERY CHARGER ON N/R 44980 DURING HMV1 AT TIMCO IN GSO.

Part: OVEN — UNSERVICEABLE (GALLEY) · airframe 25,626 hrs · 8,364 cycles

FAS REPORTED A SCREECHING SOUND WHEN STARTING FWD NR 1 OVEN. SUBSEQUENT HOT ELECTRICAL SMELL IN FWD GALLEY. FWD OVENS WERE SHUT OFF AND SMELL DISSIPATED. NR 1 OVEN IS BELIEVED TO BE SOURCE OF ODOR. PULLED FWD GALLEY U-33 CIRCUIT BREAKER AS PRECAUTION. RESET U-33 BREAKER FWD TO MCO NR 1 OVEN PER MEL 25-20-01H. NIS HNL - NDS 250007390. W/GALLEY PWR ON, ELECTRICAL SMELL NOTED. REPLACED NR 1 OVEN FWD GALLEY FOR PRECAUTION DUE TO HOT ELECTRIC SMELL AND SCRATCHING SOUND WHEN OVEN WAS TURNED ON OVEN CKS OK. MCO/PLAC REMOVED. ETOPS CATEGORY 'F': ANY OTHER EVENT DETRIMENTAL TO ETOPS.

Part: FAN — OVERHEATED (EQUIP COOLING) · airframe 24,491 hrs · 8,113 cycles

ELEC ODOR IN COCKPIT AT FLT 350 AND .80 MACH WITH EQUIP COOLING FAN STATUS MSG. REPLACED FWD EQUIP COOLING EXHAUST FAN PER M/M. MCO/PLAC RMVD.

Part: INDICATION SYS — MALFUNCTIONED (HYDRAULIC SYS) · airframe 21,923 hrs · 7,626 cycles

DURING TAXI FOR T/O, EICAS MESSAGE RT HYD QTY ON STATUS PAGE. RT HYD SYS IND 1.02. FWD TO MCO AND PLACARD PER MEL 29-33-02. PERFORM REP CK RT HYD QTY CKS FULL, NO MSGS AND NO DISCREPANCIES NOTED RT HYD QTY SYS NORMAL MCO/PLAC REMOVED.

Part: O-RING — LEAKING (SPOILER ACTUATOR) · airframe 21,411 hrs · 7,474 cycles

CTR HYD QTY DROPPED TO .29 INFLIGHT. MX IN WORK, FOUND NR 4 SPOILER LEAKING LEFT WING. SERVICE HYD SYSTEM. REPLACED O-RING ON NR 4 SPOILER ACTUATOR. LEAK CHECKED OK. CHECKED DIFFERENTIAL FILTER INDICATING ON CENTER ACMPS BOTH CHECK OK. CYCLED SPOILERS CONTROL SURFACES, NO FURTHER LEAK NOTED.

Part: START VALVE — MALFUNCTIONED (LT ENGINE) · airframe 19,774 hrs · 7,052 cycles

LEFT ENG START VLV WILL NOT OPEN. DEFERRED PER MEL 80-00-02, REPLACED NR 1 ENG START VLV, LEAK CHECK OK. OPS CHECKS OK.

Part: INDICATOR — FAULTY (COCKPIT) · airframe 19,531 hrs · 7,012 cycles

CENTER HYD QTY WENT TO ZERO AFTER ENGINE START. REPLACED HYD QTY MONITOR UNIT. CHECKS GOOD, MCO PLACARD REMOVED.

Part: CONNECTOR — NOT SEATED (NR 2 ENGINE) · airframe 19,143 hrs · 6,931 cycles

R BLEED OFF LIGHT WOULD NOT EXTINGUISH. BIT ASCTU FAULTED R SIDE 36-13205 DID NOT SHOW ON LEFT RESEATED CONNECTOR PRSOV. RAN ENGINE, ALL PNEU OPS NORMAL.

Part: BEARING — FAILED (RECIRC FAN) · airframe 15,676 hrs · 6,112 cycles

SMOKE FUMES IN THE CABIN. RT RECIRC FAN AND FWD IFE COOLING STATUS MESSAGE. ACCOMPLISHED SMOKE REMOVAL CHECKLIST AND SMOKE DISSIPATED. RT RECIRC FAN C/B POPPED INFLT. REPLACED FAN.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 13,159 hrs · 5,348 cycles

TWO OVERHEAD EXIT LIGHTS INOPERATIVE. RELAMPED SAME.

Part: COUPLER — FAILED (NR 2 HF SYSTEM) · airframe 13,151 hrs · 5,345 cycles

BOTH HF RADIOS UNABLE TO TRANSMIT, AUDIO OK. RESET C/B`S SEVERAL TIMES, NO HELP. REPLACED NR 2 HF COUPLER.

Part: ACTUATOR — CRACKED (NLG) · airframe 12,371 hrs · 5,099 cycles

ON PREFLIGHT FOUND NOSE GEAR RETRACT CYLINDER RAM CRACKED AT ROD END ATTACH POINT. REPLACED NOSE GEAR RETRACT CYCLINDER BORROWED FROM AA, S/N ON 00196, S/N OFF 00822, ASSY NR 273T4112-4.

Part: POWER SUPPLY — FAILED (EMERGENCY LIGHT) · airframe 9,884 hrs · 4,336 cycles

EMERGENCY LIGHTS ON SEATS 17AB THRU 25AB INOP. SEATS ONLY LEFT SIDE. FOUND PWR SUPPLY M 6759 AT FAULT. REPLACED SAME, CHECKS GOOD.

Part: POWER SUPPLY — OVERHEATED (SEAT 11 CDE) · airframe 9,429 hrs · 4,157 cycles

ENTERTAINMENT POWER UNIT UNDER SEAT 11D WARM TO THE TOUCH WITH NOTICEABLE ODOR. SHUTDOWN THE ENTERTAINMENT SYS UNIT UNDER 11D. REPLACED 11 CDE AVU LOADED SOFTWARE, CHECKS OK .

Part: GENERATOR — MALFUNCTIONED (NR 1 ENGINE) · airframe 6,663 hrs · 3,030 cycles

AT CRUISE L GEN CONT TRIPPED OCCURRED WHILE TRYING TO ELECTRICALLY OPEN EN CHANCED COCKPIT DOOR. STARTED APU THEN REFERRED TO QRH. RESET WAS SUCCESSFUL EXCEPT L BUS TIE REMAINED OPEN. GEN OPERATED NORMALLY FOR REMAINDER OF FLIGHT. ALL BITE ON BPCU L AND R GCUS, NO FAULTS. RESET LT BUS TIE. ACCOMPLISHED ENGINE RUN. ELEC LOADS AND VALUES NORMAL. APPLIED FULL ELEC LOAD. NO FURTHER TRIPS NOTED.

Part: PDU — FAULTY (L/E SLAT) · airframe 4,580 hrs · 2,196 cycles

ALTERNATE SLAT INBOARD ELECTRIC ACTUATOR POPPED C/B. REPLACED SLAT PDU INBD ELECT MOTOR. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 3,518 hrs · 1,828 cycles

THE 29AB EMERGENCY LIGHT INOP. INSTALLED BULBS AND LENS COVER, OPS CHECK GOOD.

Part: BPCU — FAULTY (E/E BAY) · airframe 1,929 hrs · 1,195 cycles

AT FL 370 LOST F/D - AUTOTHROTTLES AND A/P LATER WE GOT L/E SLAT DISAGREE CAUTION MSG ALONG WITH NUMEROUS ADVISORY MSGS. AILERON LOCKOUT AND STBY BUS OFF, ALSO NOTICED THAT DC STBY BUS C/B AND BUS DISTR C/B HAD POPPED AFTER LANDING. ONCE ON GROUND MTC RESET CBS, ALL MSGS CLEARED. INSPECTED BATTERY AND CHARGER, CKS OK. INSPECTED RELAYS K105-K109 CKS OK. BPCU SHOWED NO FAULTS. REPLACED BPCU AS PRECAUTIONARY. MTC FERRIED TO ATL ON 9936. REPLACED OVERHEAD PANEL, K109Â¥ K106 AND K104 RELAYS STDBY POWER FOR PRECAUTION.