N621DL

Part: ATTACH FITTING — CRACKED (R4 DOOR) · airframe 73,150 hrs · 35,826 cycles

R4 DOOR AFT CLIPS 2EA CRACKED, C/W EO 06-465922-03 AD REV B ME02.

Part: STRINGER — DAMAGED (FS 1683 S13R) · airframe 73,150 hrs · 35,826 cycles

STRINGER 13R AT FS 1683 REPAIRED PER ERA 474693-14 REV ORIG. TOOLING DAMAGE

Part: SKIN — DAMAGED (FS1010 S2-3R) · airframe 70,377 hrs · 34,535 cycles

FUSELAGE/SKIN/FS 1010 - 1038, S-1 TO S-3R, LIGHTNING STRIKES TOO CLOSE TOGETHER FOR SRM REPAIRS, AND ONE REPAIR ON FS 1040 FRAME WHICH REQUIRED NON-SRM REPAIR. DAMAGE CUTOUT OUT, DOUBLERS INSTALLED.

Part: OIL SYSTEM — LOW (FLAP TRANMISSION) · airframe 69,565 hrs · 34,157 cycles

ON APPROACH INTO LGA AS WE WERE CONFIG FROM 20 TO 25 FLAPS, TE FLAP DISAGREE EICAS MSG. PERFORMED NON-NORMAL CHECKLIST AND AFTER SELECTING 20 WITH ALT SW POSITION AND ALTN SELECTED FOR POWER TE CAUTION LIGHT WENT OUT. LANDED AT JFK WITH 20 FLAPS. T/S PER FIM 27-51-00, NO FAULTS NOTED. DURING TE FLAP DRIVE TX INSPECTION FOUND OIL LEVEL LOW AT RT WING 2 OB TXS LOW. SVCD SAME AND PERFORMED TE FLAP TX SYS LUBE. OPS NORM, NO FAULTS.

Part: OIL CAP — MISSING (APU) · airframe 66,500 hrs · 32,834 cycles

WITH THE RT ENG GEN ON MCO AND THE APU RUNNING IN FLIGHT, THE CREW GOT AN APU LOW OIL QTY MESSAGE. LATER THE APU SHUT DOWN AND THE A/C WAS DOWN TO A SINGLE ELECTRICAL SOURCE. IDG REPLACEMENT AND APU T/S IN WORK OPEN COWLING SERVICED APU. RAN APU. FOUND OIL FITTING WITH A MISSING CAP. REPLACED MISSING CAP. RAN APU. FOUND NO LEAKS.

Part: ISOLATION VALVE — LEAKING (LT HYD SYSTEM) · airframe 66,212 hrs · 32,722 cycles

LEFT HYD SYS PRESS LIGHT .17 HYD FLUID IN RESEVIOR. FOUND LT SYSTEM EMPANAGE ISOLATION VALVE LEAKING. REPLACED VALVE PER AMM SERVICED LT HYD SYS CLEANED AFFECTED AREA OF HYD FLUID VALVE LEAK AND OPS CKS NORM.

Part: LIGHT — BROKEN (L2 DOOR) · airframe 65,570 hrs · 32,455 cycles

EMERGENCY EXIT LIGHT ASSY DAMAGED L2 DOOR. REPLACED L2 DOOR EXIT LIGHT ASSY.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 64,705 hrs · 32,099 cycles

A CRACK WAS FOUND IN THE L1 DOOR OPENING DOUBLER IN THE UPPER FORWARD CORNER. THE DAMAGED SKIN WAS CUT OUT AND A DOUBLER WAS INSTALLED.

Part: SKIN — DENTED (BS 589 S22-23L) · airframe 63,935 hrs · 31,831 cycles

THE FUSELAGE SKIN IS DENTED 3.25 INCH LONG AT BS 589 BETWEEN S22L AND S23L, NEAR A PREVIOUS REPAIR. DAMAGED SKIN WAS REMOVED AND A REPAIR DOUBLER WAS INSTALLED.

Part: FAN — FAILED (RIGHT) · airframe 60,221 hrs · 30,456 cycles

DURING DESCENT AT FL200, F/A ADVISED OF SMOKE SMELL IN CABIN. AT SAME TIME COCKPIT ALSO HAD A SULFUR ODOR. REPLACED RT RECIRC FAN FOR PRODUCING ODOR.

Part: FITTING — DAMAGED (NR 2 PYLON) · airframe 59,071 hrs · 30,028 cycles

REPAIR OF OVERSIZED HOLE IN NR 2 PYLON SIDE LINK FITTING. REPAIRED IAW VA 69201AD.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 56,105 hrs · 28,863 cycles

THE AFT END OF THE STRINGER 29R KEELBEAM WAS FOUND CORRODED AT FS 1400. THE BEAM WAS CUT AT FS 1390 AND THE AFT SECTION REMOVED. A NEW SECTION WAS INSTALLED AND SPLICED WITH STEEL REPAIR CHANNELS PER ER/A 087429-14, REV D.

Part: COFFEEMAKER — ODOR (GALLEY) · airframe 55,582 hrs · 28,656 cycles

LIGHT ELECTRICAL ODOR AT 2L DOOR AND GALLEY AREA F/A'S PULLED COFFEE AND OVEN C/B'S AND ODOR DISSIPATED//INSPECTED GALLEY AND SURROUNDING AREA FOR SOURCE RESET C/B'S RAN GALLEY EQUIPMENT NO DESCREPANCIES FOUND

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 51,632 hrs · 26,790 cycles

R4 DOOR EXT EMERGENCY LIGHT INOP. REPLACED POWER SUPPLY AND BATTERY. OPS CHECKS GOOD.

Part: DETECTOR — FAILED (OVERHEAT) · airframe 48,488 hrs · 25,308 cycles

FWD EQUIP COOLING OVERHEAT MSG. EQUIP COOLING SWITCH WILL NOT LATCH IN THE -ALTN- POSITION. REPLACED LOW FLOW SENSOR AND OVERHEAT DETECTOR

Part: ENGINE — FAILED (NR 2)

DURING DESCENT, RT ENGINE OIL QTY SHOWED 0. RT ENGINE OIL PRESS LIGHT CAME ON. ENGINE SHUTDOWN PER CHECK LIST. REPLACED ENGINE.

Part: FIRE LOOP — FAILED (NR 2 ENGINE)

AT 50 KTS TAKEOFF ROLL FIRE OVHT SYSTEM FAIL EICAS MESSAGE CAME ON RIGHT ENGINE FIRE LP 1 CAME ON. ABORTED TAKEOFF. RTB AT THE GATE FAIL LIGHT WENT OUT. REPLACED FIRE LOOP NB1 FOR RIGHT ENGINE AND REPAIRED DAMAGE TO LP-2 SHIELDED WIRING ON J SIDE OF FIREWALL CONNECTOR D1280 AND REPAIRED.

Part: FLOOR PANEL — CORRODED (CARGO COMPT)

DURING LETTER CHECK INSP, CORROSION FOUND AFT CARGO FLOOR LEFT SIDE AFT OF CARGO DOOR. REMOVED FLOOR PANEL AND CANTED WALL PANEL. REMOVED CORRODED AREA, MANUFACTURED REPLACEMENT SECTION. STARTED INSTALLATION OF REPLACEMENT SECTION, INSTALLED DOUBLER, INSTALLED FLOOR PANEL AND CANTED WALL PANEL REF SRM 53-60-53.