N702DN

Part: SKIN — DAMAGED (FUSELAGE) · airframe 58,136 hrs · 5,021 cycles

(AIRCRAFT 7102, L/P 1421298) FOUND HOLE RH FX SKIN AREA AT APPROX. STA 1033 BETWEEN STR 36R AND 37R SKIN SURFACE (02 EA) WITH ABRASION. CORRECTIVE ACTION: DAMAGE TRIMMED OUT AND REPAIRED IAW DELTA ERA 583814AD REV ORIGINAL DUE TO CRACK FOUND ON BOTH 02 EA HOLES.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,136 hrs · 5,021 cycles

(AIRCRAFT 7102, L/P 1421291) LH FUSELAGE SKIN APPROX STA 1028 AND STA 1033 STR 37L FOUND 02EA HOLES SURFACE CRACK. CORRECTIVE ACTION: TRIMMED-OUT AND REPAIRED I.A.W DELTA PRI 583827-14AD REV 1 STEP 11D.

Part: SKIN — CRACKED (LE SLAT) · airframe 58,136 hrs · 5,021 cycles

(AIRCRAFT 7102, L/P 1421207) DURING HFEC OPEN HOLE INSPECTION ON RHW LE I/B SLAT NO.8 OUTER SKIN FASTENER HOLES, 04 HOLES AND 01EA HOLE FOUND WITH CRACK INDICATION ON THE SKIN SIDE AT LOC ISS 196 AND LOC ISS 183 RESPECTIVELY. CORRECTIVE ACTION: REPAIRED I.A.W DELTA PRI 583455-14 REV 0.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,136 hrs · 5,021 cycles

(AIRCRAFT 7102, L/P 1421303) RH FUSELAGE SKIN APPROX STA 1028 AND STA 1033 STR 37R FOUND 02 EA HOLE SURFACE CRACKS. CORRECTIVE ACTION: REPAIRED IAW DELTA PRI 583826-14AD REV 1 STEP 11D.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 58,136 hrs · 5,021 cycles

(AIRCRAFT 7102, L/P 1421246) DURING ULTRASONIC INSPECTION CARRIED OUT AT LH STA 1035 UNDERWING LONGERON, FOUND 01 EA FASTENER HOLE AT LOWER HOLE OF VERTICAL FLANGE WITH CRACK INDICATION. CORRECTIVE ACTION: REPLACEMENT WORK AND MODIFICATION PERFORMED IAW DELTA PRI 583827-14AD REV O ISSUE DATE:14 DEC 2019 & REV 1 ISSUE DATED:17 DEC 2019.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 58,136 hrs · 5,021 cycles

(AIRCRAFT 7102, L/P 1421274) DURING INSP ON LH CTR TANK FRONT SPAR LOWER CHORD AT STA 1035, FOUND 01EA O/B FASTENER HOLE WITH CRACK INDICATION. CORRECTIVE ACTION: SUMMARY: REPAIR PERFORMED BETWEEN LBL 67 AND LBL 95 PER B777-200 SRM 57-10-10-2R REPAIR 1.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 58,136 hrs · 5,021 cycles

(AIRCRAFT 7102, LP 1421293) DURING HFEC OPEN HOLE INSP ON RH CTR TANK FRONT SPAR LOWER CHORD AT STA 1035, FOUND 01EA O/B FASTENER HOLE WITH CRACK INDICATION. CORRECTIVE ACTION: REPAIRED PER B777-200 SRM 57-10-10-2R REPAIR 1.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 58,136 hrs · 5,021 cycles

(AIRCRAFT 7102, L/P 1421306) RH STA 1035 UNDERWING LONGERON, FOUND 01EA FASTENER HOLE AT O/B HOLE OF HORIZONTAL FLANGE WITH CRACK INDICATION. CORRECTIVE ACTION: CRACKED UNDERWING LONGERON REPLACEMENT WORK CARRIED OUT I.A.W DELTA PRI 583826-14AD REV 0 ISSUE.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 58,136 hrs · 5,021 cycles

(AIRCRAFT 7102, L/P 1421282) LH FX SKIN AREA AT APPROX. STA 1033, BETWEEN STR 36L AND STR 37L FOUND HOLE SURFACE (02 EA) WITH ABRASION DAMAGE (WITHIN TRIM LINE). CORRECTIVE ACTION: TRIMMED-OUT AND REPAIRED I.A.W DELTA ERA 583827-14AD REV ORIGINAL.

Part: SKIN — CRACKED (NR 7 SLAT) · airframe 58,099 hrs · 5,016 cycles

(AIRCRAFT 7102, L/P 1397351) DURING HFEC OPEN HOLE INSPECTION ON LHW LE I/B SLAT NO.7 OUTER SKIN FASTENER HOLES, 02EA HOLES FOUND WITH CRACK INDICATION ON THE SKIN SIDE AT LOC ISS 196 AS MARKED. CORRECTIVE ACTION: REPAIRED AS PER B777-200 SRM 57-43-01-2R-15.

Part: WIRE HARNESS — PINCHED (CABIN) · airframe 57,501 hrs · 4,972 cycles

(AIRCRAFT 7102, L/P 6124442) SEAT 42D INSEAT MONITOR STARTED SMOKING (NO FLAME) TURNED OFF MONITORS AT 42D,E,F. FOUND PANASONIC 42D SDU HARNESS PINCHED SHORTED BY SEAT PAN ARM. R/R 42D MONITOR 42D SDU HARNESS & 42D SEB FOR ELECTRICAL SHORT DAMAGE. R/R 42DEF 3 SEAT HARNESS & SPM AT 41D AS PRECAUTION.

Part: LENS — MISSING (CABIN) · airframe 56,683 hrs · 4,911 cycles

(AIRCRAFT 7102, L/P 5942430) WAC FOUND DOOR 3L UPPER EMER LENS COVER MISSING. R/R EXIT LIGHT BASE AND INST EXIT LIGHT LENS OVER L3 DOOR.

Part: LIGHT — DETACHED (ROW 49F) · airframe 54,617 hrs · 4,741 cycles

(AIRCRAFT 7102, L/P 0930919) EMERGENCY FLOOR LIGHTING DAMAGED OR INOPERATIVE / LOCATIONS:49F / ACARS TEXT: FRC 33520149F / INTERIOR. FOUND IT WAS DETACHED FROM ITS POSITION. REPOSITIONED FLOOR PROX LIGHT AT 49F. CHECKED OP AND OK.

Part: SIGN — UNSECURE (CABIN) · airframe 53,357 hrs · 4,632 cycles

(AIRCRAFT 7102, L/P 5172594) EXIT SIGN AT EXIT 3L HAS FALLEN OFF. RE-INSTALLED EXIT SIGN.

Part: LENS — DAMAGED (CABIN) · airframe 51,956 hrs · 4,521 cycles

EMERGENCY FLOOR LIGHTING DAMAGED OR INOPERATIVE / LOCATIONS:901 / INTERIOR. REINSTALLED RED LENS COVER. OPS NORMAL.

Part: LENS — DAMAGED (CABIN) · airframe 51,956 hrs · 4,521 cycles

EMERGENCY FLOOR LIGHTING DAMAGED OR INOPERATIVE / LOCATIONS:405 / INTERIOR. REINSTALLED WHITE LENS COVER. OPS NORMAL.

Part: LENS — DAMAGED (CABIN) · airframe 51,956 hrs · 4,521 cycles

EMERGENCY FLOOR LIGHTING DAMAGED OR INOPERATIVE / LOCATIONS:901 / INTERIOR. PREVIOUSLY COMPLIED WITH -901 LENSES CHECK GOOD.

Part: SOCKET — NOT SEATED (CABIN) · airframe 50,926 hrs · 4,432 cycles

EMERGENCY EXIT LIGHTS 10-11 INOP BC. RESEATED SOCKET ASSY AT 11CB RELAMPED 10BC.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 50,766 hrs · 4,418 cycles

FLOOR EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMP.

Part: LENS — DAMAGED (EMERGENCY LIGHT) · airframe 48,961 hrs · 4,266 cycles

SHIP 7102 EMERGENCY FLOOR LIGHTING DAMAGED OR INOPERATIVE. CORRECTIVE ACTION: REPLACED LENS (0330400).

Part: LIGHT — INOPERATIVE (SEAT 4C) · airframe 48,255 hrs · 4,204 cycles

SEAT 4C FLOOR EMERGENCY LIGHT INOPERATIVE. REMOVED & REPLACED THE EMERGENCY LIGHT ASSY & OPS CHECKED GOOD IAW AMM 33-50.

Part: MONITOR — CLOGGED (CABIN) · airframe 47,015 hrs · 4,100 cycles

DIV TO HND DUE TO SMOKE IN THE CABIN NOTICED IN BUSINESS CLASS. TROUBLESHOOTING FOUND SEAT 7A MONITOR COOLING HOLES CLOGGED. IFE SYSTEM DEFERRED PER MEL 23-37-01A-ATL REPLACED MONITOR.

Part: LENS — MISSING (EMERGENCY LIGHTS) · airframe 46,897 hrs · 4,089 cycles

RED EMERGENCY FLOOR LIGHTS MISSING AT THE L3 AND R3 DOORS. REPLACED RED EMERGENCY LIGHT COVERS.

Part: COVER — NOT REPORTED (EMERGENCY LIGHTS) · airframe 46,141 hrs · 4,022 cycles

EMERGENCY LIGHT DAMAGED OR INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHTING LENS COVER. (2984932)

Part: BLADE — TORN (ENGINE) · airframe 45,986 hrs · 4,007 cycles

DURING BORESCOPE INSPECTION, FOUND A TEAR IN THE 5TH STAGE HPC BLADE.

Part: BLADE — DAMAGED (NR 2 ENGINE) · airframe 46,029 hrs · 4,011 cycles

NR 2 ENGINE HAS DAMAGE TO STAGES 3, & 5 HPC BLADES THAT EXCEED AMM 72-00-00-290-803-H01 LIMITS. COMPLIED WITH ERA 557259-14 REV ORIG, SECTION I .

Part: SKIN — DENTED (FUSELAGE) · airframe 45,704 hrs · 3,987 cycles

FOUND GOUGE AND DENT BETWEEN WINDOWS 15 AND 16 RT SIDE ON CROWN BETWEEN S-1R AND S-2R. REF NRC 001 AND ERA 556793-14 REV ORIG FOR REPAIR INSTRUCTIONS.

Part: SKIN — PUNCTURED (HORIZONTAL STAB) · airframe 48,255 hrs · 4,204 cycles

PUNCTURE IN THE LEFT HORIZONTAL STAB UPPER SURFACE 20 INCHES AFT OF LEADING EDGE AND 24 INCHES FROM INBD EDGE AT FUSELAGE. INSTALLED A REPAIR IAW SRM 55-10-01, REPAIR 2.

Part: SKIN — DENTED (BS 665) · airframe 41,210 hrs · 3,566 cycles

LEFT FUSELAGE FOUND DENT FWD OF L2 DOOR AT BS 665, S26 - 27L. DENT AREA OF SKIN CUT OUT. REPAIRED IAW SRM 53-00-01, REPAIR 7, FIG 202.

Part: SKIN — SCRATCHED (R4 DOOR) · airframe 41,054 hrs · 3,553 cycles

FUSELAGE RT SIDE, FOUND A SCRATCH AFT OF R4 DOOR AT BS 2112,S-24R TO S-25R. REPAIRED IAW ER/A 543544-14 PRI REV 0.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,814 hrs · 1,609 cycles

DURING A MAINTENANCE VISIT, THE EMERGENCY ESCAPE PATH LIGHT AT SEAT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. SYSTEM OPERATION WAS NORMAL AFTER THE LIGHT ASSEMBLY WAS REPLACED.

Part: BULB — FAILED (MAP LIGHT) · airframe 19,400 hrs · 1,575 cycles

CAPTAIN`S OVERHEAD MAP LIGHT FLICKERS FROM FULL BRIGHT TO OFF. SMOKE AND BURNING ODOR OBSERVED. BULB REMOVED AND COVER REMOVED. REPLACED AND ADJUSTED MAP LIGHT ASSY. CHECKED 30 MINS AND NO SMOKE AND ODOR. OK FOR SERVICE.

Part: SOCKET — SHORTED (EMERGENCY LIGHT) · airframe 17,126 hrs · 1,376 cycles

MAINTENANCE FOUND EMERGENCY LIGHTS IN THE AFT SECTION OF BUSINESS CLASS INOPERATIVE. MAINTENANCE REPLACED SLIDE LIGHT SOCKET L33232 AND THE LIGHTS RETURNED TO NORMAL OPERATION. ETOPS CATEGORY 'E': PROBLEMS WITH SYSTEMS CRITICAL TO ETOPS

Part: FUSE — BLOWN (BATTERY PACK) · airframe 14,614 hrs · 1,148 cycles

DURING A MAINTENANCE VISIT, THE EMERGENCY PATH LIGHTS BETWEEN ROWS 10-14 WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE FUSE ON THE BATTERY PACK M33098. SYSTEM OPERATION CHECKED GOOD AFTER THE FUSE WAS REPLACED.

Part: STOP FITTING — FAILED (NR 4 SLAT TRACK) · airframe 14,368 hrs · 1,125 cycles

NR 4 SLAT INBD MAIN TRACK STOP FITTING FAILED TORQUE CK IAW EA 11-469704-03AD, ME 03.

Part: PUMP — FAILED (FUEL SYSTEM) · airframe 3,410 hrs · 241 cycles

AFTER FUEL BALANCING COMPLETE RT FWD FUEL BOOST PUMP LIGHT REMAINED ON. SHORTLY AFTER RT AFT FUEL BOOST PUMP ILLUMINATED. COMPLETED NON NORMAL PROCEDURE FOR FWD & AFT BOOST PUMP FAILS PER QAH. BOTH BOOST PUMP REPLACED VERIFICATION FLT C/W ON 11/26/08 FLT 185.

Part: ENGINE — MALFUNCTIONED (NR 1) · airframe 3,232 hrs · 230 cycles

PERFORMED EA 54-41523-14 ORIG REMOVED STARTER GEARSHAFT AND TGB REMOVED AND REPLACED. REMOVED AND REPLACED NEC TUBES AND BRACKETS FOR ACCESS. PERFORMED TEST NO FAULTS DRY MOTOR NO LEAKS COMPLETED EA 54-471523-14 ORG OPERATED NR 1 ENG PER 71-00-00-700-805 TEST 6 CKS GOOD.

Part: IDG — MALFUNCTIONED (NR 1) · airframe 2,490 hrs · 180 cycles

LT GEN DRIVE LIGHT ILLUMINATED WITH GEN OFF LIGHT ILLUM AFTER PUSHBACK SERVICED LT IDG. NO HELP. PLACED L GEN INOP PER MEL 24-11-01. MAINT ACTION C/W. REMOVED AND REPLACED LEFT IDG PER MM OPS CK OK MCO AND PLAC REMOVED.

Part: SAARU — UNSERVICEABLE (E/E) · airframe 4,597 hrs · 318 cycles

HAD SAARU FAILURE INBOUND TO BOMBAY. COULD NOT RESET. AWAITING PART FROM ATL. REMOVED AND REPLACED SAARU, P/N ON HG2040AD02 P/N OFF, HG2040AD03 S/N ON 99090394 S/N OFF 56016691 IAW MM 34-21-02-400-801. RELOADED SAARU SOFTWARE. OPS OK. ALL MSG ERASED. BOTH ENG EEC IDLE TO NORMAL. CARRIED OUT IDLE ENG R ON BOTH ENGINES. ALL PARAMETERS NORMAL.