N842FD

Part: LAMP — FAILED (ZONE 200) · airframe 56,434 hrs · 8,602 cycles

FOUND RT DOOR FWD EXIT SIGN - LAMP INOPERATIVE. AMM: 33-51-01-2 IAW AMM 33-51-01-2, REPLACED EXIT SIGN LAMPS, OPS TEST GOOD. OK TO CONTINUE. IAW AMM 33-51-01-2, REPLACED EXIT SIGN LAMPS, OPS TEST GOOD. OK TO CONTINUE.

Part: OIL SYSTEM — LEAKING (RT ENGINE) · airframe 55,160 hrs · 8,398 cycles

OIL QTY ON RIGHT ENGINE WENT TO 4 QTS ABOUT 3.5 HOURS INTO FLIGHT. EVENTUALLY DECREASED TO ZERO OIL QTY ABOUT 1.5 HOURS LATER. OIL PRESSURE DECREASED TO 35 IN DESCENT, NEVER ANY LOWER. NEVER GOT ANY EICAS MESSAGES OR SECONDARY INDICATIONS. REMOVED AND REPLACED AIR/OIL SEPARATOR PER AMM 79-21-13-4. DMS SENSOR TESTED GOOD PER AMM 71-00-00-5 TEST 18, AIR OIL SEPARATOR AND DMS SENSOR LEAK TEST GOOD PER AMM 71-00-00-5 TEST 5. A/C OKAY FOR SERVICE.

Part: SKIN — DELAMINATED (ZONE 600 FLAP) · airframe 51,767 hrs · 7,880 cycles

RH WING OB FLAP LWR SURFACE FOUND DENT WITH DISBOND AT 275 IN AWAY FROM OB, 10 IN AWAY TO AFT EDGE. REPAIRED RH WING OB FLAP LWR SURFACE DENT AT OTEF STA 251 AS PER B777 SRM 57-53-01-2R REPAIR 2, SRM 51-70-04-2R REPAIR 1 REV 46.3 AND EA: G-5750-T0380234 P1, TITLE: WING-FLIGHT SURFACES-RH OUTBD FLAP TE WEDGE DENT WITH DISBOND AT OTEF STA 251-SRM REPAIR-RSC TRACKING. DETAIL PLS REF TO WRI: 57508751, THIS IS A MAJOR REPAIR PER GMM 6-2-100.

Part: SKIN — DENTED (ZONE 100) · airframe 51,767 hrs · 7,880 cycles

DURING PERFORM E.A :G-5330-T0368078 - FUSELAGE - PLATES&SKINS - AFT FUSELAGE SKIN PANEL STA 1902.5 - 1907.5, STR 46R - 47R, THE DENT DAMAGE FOR CAT C INTERIM REPAIR WILL BE REPLACED BY CAT A OR B PERMANENT REPAIR. AFT FUSELAGE SKIN AT STA 1902.5-1907.5, STR 46R-47R REPAIRED AS PER B777 SRM 53-00-01-1A- 1, 51-70-01-0G, 51-20-01-0G, 53-00-01 REPAIR 3, 51-20-01-0G, 51-40-08-0G, 51-20-05-0G REV46.3 AND EA G-5330-T0368078 A P2,TITLE:FUSELAGE -PLATES & SKINS-AFT FUSELAGE SKIN PANEL STA 1902.5- 1907.5, STR 46R-47R, REPAIR FOR DENT DAMAGE. REFER TO WRI:53308508 FOR WORK DETAILS. THIS IS A MAJOR REPAIR PER GMM 6-2-100.

Part: BULB — FAILED (ZONE 200) · airframe 51,724 hrs · 7,873 cycles

SVC CK, (1EA) SUPRNMRY AREA OVERHEAD EMERGENCY LIGHT INOP. RE-LAMPED, REF B777 AMM: 33-50-00-2. EMERGENCY LT'S TEST SATIS, ITEM OK FOR SVC.

Part: WIRE HARNESS — DAMAGED (MLG STEERING) · airframe 50,113 hrs · 7,609 cycles

DURING TAXI OUT MAIN GEAR STEERING ALERT ON EICAS - FLASHED UP & DISAPPEARED DURING ONE OF FOUR TURNS TO RUNWAY. AFTER LINE UP & TOGA PRESSED - MAIN GEAR STEERING WARNING ANNUNCIATED. REJECTED TAKEOFF & RTB AT 40KTS. EICAS MAIN GEAR STEERING ANNUNCIATED AGAIN DURING ONLY ONE SUBSEQUENT TURN DURING RTB. STATUS MESSAGE REMAINED. REMOVED & REPLACED HARNESS W7244 PER AMM 32-11-30-4 & CMM 32-10-27. PERFORMED BELOW TESTS. ANTISKID/AUTOBRAKE CONTROL SYSTEM-SYS TEST IAW AMM 32-42-00-5, MLG STEERING SYSTEM-FUNCTION TEST IAW AMM 32-53-00-5, PROXIMITY SENSOR ELECTRONICS UNIT-SYS TEST IAW AMM 32-08-00-5, TIRE PRESSURE INDICATION SYS-FUNCTION CHECK IAW AMM 32-49-00-5, & TEST OF TRUCK TILT SENSOR IAW AMM 32-61-03-2.

Part: LIGHT — INOPERATIVE (N/A) · airframe 48,791 hrs · 7,405 cycles

POST-FLT INSP, R-1 DOOR OVRHD EMERGENCY LT INOP. RE-LAMPED, REF B777 AMM: 33-51-04-2. LT'S TEST SATIS, ITEM OK FOR SVC.

Part: NONE — NONE (N/A) · airframe 41,878 hrs · 6,364 cycles

POST-FLT INSP, R-1 EXTERIOR EMERGENCY LT INOP. RE-LAMPED, REF B777 AMM: 33-51-04-2. EMERGENCY LT'S TEST SATIS, ITEM OK FOR SVC.

Part: ANGLE — UNKNOWN (100) · airframe 41,583 hrs · 6,310 cycles

WHILE ACCOMPLISHING EA G-5710-T0366056A P2 RIGHT HAND LOWER CHORD INSTALLATION ON STEP (10.E), MENTIONED IN EA, FASTENER WET INSTALL WITH BMS 5-95 SEALANT (GENERAL PURPOSE SEALANT) COMPLIED WITH E.A # G-5710-T0366458.P2. TITLE : WING-BASIC WING STRUCTURE - CENTER WING RING CHORD , FRONT SPAR LOWER CHORD AND WEB , LEFT HAND AND RIGHT HAND UNDERWING LONGERON INSPECTION / MODIFICATION- DEVIATION TO SB777-57A0122 RB. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. (WRI:57-10/6158 AND SNRM N00609 FOR WORK DETAILS)

Part: ANGLE — UNKNOWN (100) · airframe 41,583 hrs · 6,310 cycles

WHILE ACOMPLISHING EA G-5710-T0366056A P1 LEFT HAND LOWER CHORD INSTALLATION ON STEP (10.E), MENTIONED IN EA, FASTENER WET INSTALL WITH BMS 5-95 SEALANT (GENERAL PURPOSE SEALANT). COMPLIED WITH E.A .# G-5710-T0366458.P1 TITLE: WING - BASIC WING STRUCTURE - CENTER WING RING CHORD , FRONT SPAR LOWER CHORD AND WEB , LEFT HAND AND RIGHT HAND UNDERWING LONGERON INSPECTION / MODIFICATION - DEVIATION TO SB 777-57A0122 RB. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. ( WRI : 57-10/6157 AND SNRM N00608 FOR WORK DETAILS )

Part: DOUBLER — UNKNOWN (ZONE 100) · airframe 41,583 hrs · 6,310 cycles

WHILE ACCOMPLISHING RIGHT HAND E.A.#G-5710-T0366056A P2 FOUND NEW FUSELAGE SKIN DOUBLER EXISTING HOLE AT STATION 998 STRINGER S-35R NEAR MILLED EDGE. COMPLIED WITH E.A.#G-5710-T0366458 P2 TITLE : WING - BASIC WING STRUCTURE - CENTER WING RING CHORD, FRONT SPAR LOWER CHORD AND WEB, LH AND RH UNDERWING LONGERON INSPECTION / MODIFICATION - DEVIATION TO SB 777 - 57A0122 RB. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — CRACKED (ZONE 100) · airframe 41,583 hrs · 6,310 cycles

DURING ACCOMPLISHMENT OF HIGH FREQUENCY EDDY CURRENT INSPECTION ON RIGHT HAND EXTERIOR FUSELAGE SKIN COMMON TO UNDERWING LONGERON FITTING, FOUND 01 EACH CRACK AROUND FASTENER HOLE AT STATION 1033 STRINGER 37R, APPROXIMATELY 1.0 INCH IN LENGTH, AS MARKED. COMPLIED WITH E.A.#G-5710-T0366056 A P2. TITLE : WING-BASIC WING STRUCTURE-RING CHORD, FRONT SPAR LOWER CHORD AND FRONT SPAR WEB-INSPECTION AND MODIFICATION- SB 77-57A0122RB. REPAIRED CLASSIFIED AS MAJOR PER 6-2-100.

Part: DOUBLER — UNKNOWN (ZONE 100) · airframe 41,583 hrs · 6,310 cycles

WHILE ACCOMPLISHING LEFT HAND E.A.#G-5710-T0366056A P1 FOUND NEW FUSELAGE SKIN DOUBLER EXISTING HOLE AT STATION 998 STRINGER S-35L NEAR MILLED EDGE COMPLIED WITH E.A.#G-5710-T0366458 P1 TITLE : WING - BASIC WING STRUCTURE - CENTER WING RING CHORD, FRONT SPAR LOWER CHORD AND WEB, LH AND RH UNDERWING LONGERON INSPECTION / MODIFICATION - DEVIATION TO SB 777 - 57A0122 RB. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: STRINGER — CRACKED (N/A) · airframe 41,583 hrs · 6,310 cycles

LOWER BULK CARGO COMPARTMENT STATION 1979 RIGHT BUTT LINE 49.5 STRINGER FOUND WITH CRACK AS MARKED. LOWER BULK CARGO COMPARTMENT STATION 1979 RIGHT BUTT LINE 49.5 CRACK STRINGER REPAIRED AS PER B777 SRM 53-70-53-2R FIGURE 202 REPAIR 2 FROM STATION 1946 TO STATION 1980.5 RIGHT BUTT LINE 49.5. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: STRINGER — CRACKED (N/A) · airframe 41,583 hrs · 6,310 cycles

LOWER BULK CARGO COMPARTMENT STATION 1937, RIGHT BUTT LINE 41.5 STRINGER FOUND WITH CRACK AS MARK. LOWER BULK CARGO COMPARTMENT STATION 1937 RIGHT BUTT LINE 41.5 CRACK STRINGER REPAIRED AS PER B777 SRM 53-70-53-2R FIGURE 202 REPAIR 2 FROM STATION 1924 TO STATION 1946 RIGHT BUTT LINE 41.5. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: TIRE — LEAKING (NR 1) · airframe 40,165 hrs · 6,087 cycles

TIRE PRESSURE EICAS. COMPLIED WITH EICAS PROCEDURES. EMERGENCY DECLARATION MADE BY ATC IN ORDER FOR US TO USE RUNWAY 36C TO LAND. FOUND NO VISUAL DEFECTS WITH TIRE. R&R'D #1 MLG TIRE/WHEEL ASSY PER AMM 32-45-01-4. OK FOR SERVICE.

Part: FAN — FAILED (RECIRCULATION) · airframe 39,657 hrs · 6,005 cycles

RH LOWER RECIRCULATION FAN IS CREATING VERY LOAD HUMING SOUND DURING OPERATION. FOUND R/H RECIRCULATION FAN INBOARD FILTER DEFORMED AND DRAWN DOWN INTO THE R/H RECIRCULATION FAN. REMOVED AND REPLACED R/H RECIRCULATION FAN REF M.M. 21-25-07-4, OPS CK NORMAL, REMOVED AND REPLACED R/H RECIRCULATION FAN FILTERS REF M.M. 21-25-08-4. ALSO C/W L/H RECIRCULATION FAN FILTER REPLACEMENT REF B777 M.M. 21-25-08-4, RECIRCULATION SYSTEM OPS CK NORMAL REF M.M. 21-25-00-5.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 35,607 hrs · 5,373 cycles

POST-FLT INSPECTION, L1 DOOR OVRHD EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMPS.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 35,607 hrs · 5,373 cycles

POST-FLT INSPECTION, L1 OVERHEAD EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMP IAW AMM 33-51-04-2. LIGHT TESTED SATISFACTORY, OK FOR SERVICE.

Part: BRAKE — OVERHEATED (NR 2) · airframe 35,526 hrs · 5,362 cycles

NR 2 BRAKE CAUSED OVERHEAT AND THERMAL OF NR 2 MAIN WHEEL ASSY. MPN: C20558000 POS: 2 SRL: 11467, REMOVED AND REPLACED NR 2 BRAKE PER 32-45-07-4 MAIN LANDING GEAR BRAKE REMOVAL/INSTALLATION. REMOVED AND REPLACED NR 2 BRAKE ASSY ON BLOCK IN THE BRAKE WAS ON FIRE. WHICH CAUSED NR 2 TIRE TO THERMAL. INSPECTED TRUCK AND AXLE ASSEMBLY WHEN BRAKE WAS REMOVED. NO DAMAGE OR SIGNS OF BURNING/SCORCHING FOUND.

Part: BRAKE ASSY — FIRE (NR 2) · airframe 35,526 hrs · 5,362 cycles

NR 2 BRAKE CAUSED OVERHEAT AND THERMAL OF NR 2 MAIN WHEEL ASSY. REMOVED AND REPLACED THE NR 2 BRAKE IAW 32-45-07-4.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 34,313 hrs · 5,187 cycles

MDIS 842 33-50 3495 18MAR20 MEM POST-FLT INSP L-1 EXTERIOR EMERGENCY LT INOP. FACT 18MAR20 07:12 MEM RE-LAMPED, REF B777 AMM: 33-51-04-2. EMERGENCY LT'S TEST SATIS, ITEM OK FOR SVC.

Part: UNKNOWN — MALFUNCTIONED (NLG STEERING) · airframe 32,059 hrs · 4,857 cycles

ON TAXI IN ATTEMPTED TO MAKE LEFT TURN TILLER BECAME EXTREMELY STIFF AND THE AIRCRAFT WAS SLOW TO TURN. STOPPED TURN COORDINATED WITH GROUND TO TAXI STRAIGTH AHEAD TO ANOTHER TAXI-WAY WAS ABLE TO MAKE NORMAL LEFT AT NEXT TAXI-WAY AND ALSO NORMAL LEFT TURN INTO THE PARKING SPOT. PERFORMED NOSE LANDING GEAR STEERING SYSTEM ADJUSTMENT/TEST IAW AMM32-51-00-5-0, NO DEFECT FOUND. SYSTEM WORKS PROPERLY AND CAPTAIN'S TILLER MOVES FREELY. PERFORMED GVI OF ALL STEERING CABLES FOR CONDITION. NO DEFECT FOUND. STILL NEED TO PERFORMED TAXI CHECK. TAXIED AIRCRAFT, NO ABNORMALITIES NOTICED EITHER RIGHT OR LEFT TURNS. A/C OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 29,729 hrs · 4,531 cycles

POST-FLT INSP, R1 DOOR EXTERIOR EMERGENCY EXIT LT INOP ON LIGHT TEST. RELAMPED, REF AMM 33-51-04-2. LT TESTS SATIS, ITEM OK FOR SVC.

Part: LAMP — INOPERATIVE (EXTERIOR LIGHT) · airframe 28,860 hrs · 4,397 cycles

POST-FLT INSP, R-1 DOOR OUTSIDE EMERGENCY LT INOP RE-LAMPED, REF B777 AMM: 33-51-04-2. EMERGENCY LT'S TEST SATIS, ITEM OK FOR SVC.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 28,860 hrs · 4,397 cycles

POST FLT INSP, R1 DOOR OUTSIDE EMERGENCY LIGHT INOP. RE-LAMPED, REF AMM 33-51-04-2. EMERGENCY LIGHTS TEST SATIS, ITEM OK FOR SVC.

Part: LAMP — INOPERATIVE (EXTERIOR LIGHT) · airframe 28,860 hrs · 4,397 cycles

POST-FLT INSPECTION, R-1 DOOR OUTSIDE EMERGENCY LIGHT INOPERABLE. RE-LAMPED, REF B777 AMM: 33-51-04-2. EMERGENCY LIGHTS TEST SATISFACTORY, ITEM OK FOR SERVICE.

Part: LAMP — INOPERATIVE (EXTERIOR LIGHT) · airframe 28,860 hrs · 4,397 cycles

POST-FLT INSPECTION, R-1 DOOR OUTSIDE EMERGENCY LIGHT INOPERABLE RE-LAMPED, REF B777 AMM 33-51-04-2. EMERGENCY LIGHTS TEST SATISFACTORY, ITEM OK FOR SERVICE.

Part: LAMP — NO TEST (EMERGENCY LIGHT) · airframe 28,860 hrs · 4,397 cycles

POST-FLT INSP, R-1 DOOR OUTSIDE EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMP IAW AMM: 33-51-04-2. EMERGENCY LIGHTS TESTED SATISFACTORY, OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 28,860 hrs · 4,397 cycles

POST FLT INSP, R1 DOOR OUTSIDE EMERGENCY LIGHT INOP. RE-LAMPED, REF AMM 33-51-04-2. EMERGENCY LIGHTS TEST SATIS, ITEM OK FOR SVC.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 28,860 hrs · 4,397 cycles

POST FLT INSP, R1 DOOR OUTSIDE EMERGENCY LIGHT INOP. RE-LAMPED, REF AMM 33-51-04-2. EMERGENCY LIGHTS TEST SATIS, ITEM OK FOR SVC.

Part: LAMP — INOPERATIVE (EXTERIOR LIGHT) · airframe 28,860 hrs · 4,397 cycles

POST-FLT INSP, R-1 DOOR OUTSIDE EMERGENCY LT INOP RE-LAMPED, REF B777 AMM: 33-51-04-2. EMERGENCY LT'S TEST SATIS, ITEM OK FOR SVC.

Part: LAMP — INOPERATIVE (EXTERIOR LIGHT) · airframe 28,860 hrs · 4,397 cycles

POST-FLT INSP, R-1 DOOR OUTSIDE EMERGENCY LT INOP RE-LAMPED, REF B777 AMM: 33-51-04-2. EMERGENCY LT'S TEST SATIS, ITEM OK FOR SVC.

Part: LENS — DETACHED (EMERGENCY LIGHT) · airframe 25,801 hrs · 3,946 cycles

L1 DOOR AFT EMERGENCY LENS DETACHED. COMPLIED WITH EA G-3350-T0336667, PART 3. INSTALLED THE LIGHT ASSY AND OPS CHECKED GOOD IAW MM 33-51-01-2.