N601DL

Part: ENGINE — MALFUNCTIONED (LEFT) · airframe 69,663 hrs · 36,182 cycles

ON CLIMB-OUT AT APPROX 8000, LEFT ENG EGT INCREASE INTO RED RADIAL MAX EGT OF 789. LEFT THROTTLE RETARD TO IDLE AFTER APPROX 2 MINUTES EGT WITHIN NORMAL LIMITS. THROTTLE ADVANCE BACK TO CLIMB POWER AND ALL ENGINES INDICATION ARE NORMAL. REPLACED NR 1 ENG PER TRANS 6T103.

Part: HYDRAULIC LINE — CRACKED (VERTICAL STAB) · airframe 59,182 hrs · 32,173 cycles

SLOW HYD LEAKING LEFT SYSTEM OVER 3 HRS QTY WENT FROM NORMAL TO 0.24 AT LANDING. FOUND SYS 1 RUDDER RET LINE LEAKING IN VERT FIN 2 BAYS ABOVE STAB COMPARTMENT REPLACED WITH APPROVED FLEX LINE LEAK, OPS CHECK NORMAL.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 58,226 hrs · 31,753 cycles

ONE LEFT DOOR EMERGENCY FLASHLIGHT NOT WORKING. REPLACED FLASHLIGHT ASSY.

Part: SWITCH — OUT OF ADJUST (THRUST REVERSER) · airframe 57,437 hrs · 31,370 cycles

ON INITIAL POWER APPLICATION FOR T/O LEFT ENGINE REVERSER LIGHT ILLUMINATED. WITH POWER REDUCED LIGHT EXTINGUISHED. DEACTIVATION PINS INST LOCKING T/REV IN FWD THRUST. ADJUSTED RIGHT SIDE CENTER PROX SWITCH.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 57,428 hrs · 31,368 cycles

DURING L/O CK FOUND R2 DOOR EXTERIOR EMERGENCY LIGHT INOP. RELAMPED CKS GOOD.

Part: SKIN — CORRODED (FS 740, S-28) · airframe 57,311 hrs · 31,311 cycles

FUSELAGE / SKIN / FS 715-740 / STRG. 28L-28R : CORROSION REPAIR AT LWR VHF ANTENNAL CUTOUT THE FUSLEAGE SKIN WAS FOUND WITH AREAS OF CORROSION AROUND THE LOWER VHF ANTENNA CUTOUT BETWEEN FS 715 & 740 AND BETWEEN STRINGERS 28L & 28R. THE CUTOUT WAS ENLARGED TO REMOVE THE CORROSION AND THE AREA REPAIRED WITH 2 EXTERNAL ALUMINUM REPAIR DOUBLERS PER ER/A 383860-14, REV A.

Part: SKIN — DENTED (FS 1711, S-15L) · airframe 57,311 hrs · 31,311 cycles

FUSELAGE / SKIN / FS 1711 / STRG. 14L-17L : DENT CUTOUT REPAIR THE FUSELAGE SKIN WAS FOUND WITH 2 DENTS AT FS 1711 BETWEEN STRINGERS 14L & 17L. THE DENTS WERE REMOVED WITH 2 SKIN CUTOUTS. THE CUTOUTS WERE REPAIRED WITH A SINGLE EXTERNAL ALUMINUM REPAIR DOUBLER PER ER/A 383877-14, REV A.

Part: SKIN — CORRODED (FUSELAGE) · airframe 57,311 hrs · 31,311 cycles

CUTOUT REPAIR, THE FUSELAGE SKIN WAS FOUND WITH SIGNS OF CORROSION AT AN EXISTING SKIN REPAIR. THE REPAIR WAS REMOVED AND ALL CORROSION DAMAGE REMOVED WITH A CUTOUT. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL REPAIR DOUBLER PER ER/A 383949-14, REV A.

Part: SKIN — LIGHTNING STRIKE (FUSELAGE) · airframe 57,311 hrs · 31,311 cycles

LIGHTNING STRIKE REPAIR, THE FUSELAGE CROWN SKIN WAS FOUND WITH A LIGHTNING BURN DAMAGE LOCATION AT FS 600 BETWEEN STRINGERS 2R & 3R. THE DAMAGE WAS REMOVED WITH A CUTOUT AND REPAIRED WITH 2 EXTERNAL REPAIR DOUBLERS PER ER/A 384019-14, REV A.

Part: SILL — CORRODED (FUSELAGE) · airframe 57,311 hrs · 31,311 cycles

CORROSION REPAIR, THE OUTBD CHORD OF THE LOWER SILL OF THE C1 DOOR CUTOUT WAS FOUND WITH SEVERAL AREAS OF CORROSION. THE OUTER CHORD AND WEB OF THE FS 620 OPENING FRAME WERE CUT AT STR 25R AND THE LOWER ENDS REMOVED TO ALLOW REMOVAL OF THE SILL CHORD. A NEW SILL CHORD WAS INSTALLED AND THE DOOR FRAME AND WEB SPLICED BACK IN WITH REPAIR ANGLES AND DOUBLERS PER ER/A 383863-14, REV B.

Part: SKIN — CORRODED (FUSELAGE) · airframe 57,311 hrs · 31,311 cycles

CORROSION REPAIR, CORROSION WAS FOUND ON THE FUSELAGE SKIN AT THE LOWER AFT VHF ANTENNA CUTOUT AT FS 1473 AND RBL 3. THE CUTOUT WAS ENLARGED TO REMOVE ALL DAMAGE AND REPAIRED WITH 2 EXTERNAL REPAIR DOUBLERS PER ER/A 383865-14, REV A.

Part: SKIN — GOUGED (FS 558, S-26L) · airframe 57,311 hrs · 31,311 cycles

FUSELAGE / SKIN / FS 558 / STRG. 26L : GOUGE CUTOUT REPAIR THE FUSELAGE SKIN WAS FOUND GOUGED JUST BELOW THE STRINGER 26L SKIN LAP JOINT AT FS 558. THE GOUGE WAS REMOVED WITH A CUTOUT IN THE SKIN. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER ER/A 383880-14, REV A.

Part: SKIN — LIGHTNING STRIKE (FUSELAGE) · airframe 57,311 hrs · 31,311 cycles

LIGHTNING STRIKE DAMAGE REPAIR, THE FUSELAGE SKIN AT FS 720 WAS FOUND WITH LIGHTNING DAMAGE AT STRINGER 3L. THE DAMAGE WAS REMOVED WITH A CUTOUT IN THE SKIN AND REPAIRED WITH AN EXTERNAL REPAIR DOUBLER PER ER/A 384001-14, REV A.

Part: SKIN — LIGHTNING STRIKE (FUSELAGE) · airframe 57,311 hrs · 31,311 cycles

LIGHTNING STRIKE DAMAGE REPAIR, THE FUSELAGE SKIN WAS FOUND WITH LIGHTNING STRIKE DAMAGE AT FS 478 AT THE STRINGER 4L SKIN LAP JOINT. THE DAMAGE WAS REMOVED WITH A CUTOUT AND REPAIRED WITH AN EXTERNAL REPAIR DOUBLER PER ER/A 383991-14, REV A.

Part: SKIN — LIGHTNING STRIKE (FUSELAGE) · airframe 57,311 hrs · 31,311 cycles

LIGHTNING STRIKE DAMAGE REPAIR, THE FUSELAGE SKIN WAS FOUND WITH LIGHTNING STRIKE DAMAGE AT FS 499, JUST ABOVE THE STRINGER 4R SKIN LAP JOINT. THE DAMAGE WAS REMOVED WITH A CUTOUT AND REPAIRED WITH AN EXTERNAL REPAIR DOUBLER PER ER/A 383992-14, REV A.

Part: SKIN — DENTED (FS 1420, S-29R) · airframe 57,311 hrs · 31,311 cycles

FUSELAGE / SKIN / FS 1420 / STRG. 28R-29L : DENT REPAIR THE FUSELAGE SKIN WAS FOUND WITH 2 DENTS NEAR FS 1420 BETWEEN STRINGERS 28R & 29L. THE DENTS WERE REMOVED WITH 2 CUTOUTS IN THE SKIN. THE CUTOUTS WERE REPAIRED WITH A SINGLE EXTERNAL ALUMINUM REPAIR DOUBLER PER ER/A 383884-14, REV A.

Part: SKIN — CORRODED (FS 1510, S28R) · airframe 57,311 hrs · 31,311 cycles

FUSELAGE / SKIN / FS 1510 / STRG. 28R-29R / AIRFONE ANTENNA CUTOUT : CORROSION REPAIR THE FUSELAGE SKIN AROUND THE AIRFONE ANTENNA CUTOUT AT FS 1510 BETWEEN STRINGERS 28R & 29R WAS FOUND CORRODED. THE CUTOUT WAS ENLARGED TO REMOVE THE CORROSION. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER ER/A 383850-14, REV A.

Part: CLIP — BROKEN (PAX DOOR SLIDE) · airframe 51,264 hrs · 28,433 cycles

L3 DOOR WILL NOT ARM. FOUND GIRT BAR CLIP BROKEN. REPLACED GIRT BAR.

Part: SKIN — DAMAGED (NR 7 SLAT) · airframe 50,868 hrs · 28,257 cycles

THE TRAILING EDGE WEDGE OF THE NR 7 SLAT WAS MODIFIED PER EO 6-59305-AD. ADDITIONAL DAMAGE TO THE SLAT WAS FOUND RESULTING IN THE REMOVAL OF SEVERAL FASTENERS THAT ATTACH THE T/E WEDGE TO THE SLAT INNER SURFACE. SEVERAL HOLES WERE OVERSIZED. REPAIRED PER ER/A 387806-14AD.

Part: PUMP — FAILED (LT ENGINE HYD) · airframe 49,581 hrs · 27,616 cycles

LT HYD QTY DECREASED TO 0 AND SYS PRESS LIGHT ILLUMINATED. EICAS MESSAGE L HYD SYS PRESS DISPLAYED AND RUDDER RATIO LIGHT. REPLACED LT ENGINE HYD OUT PRESSURE LINE AND LT ENGINE HYD PUMP. SERVICED LT SYSTEM AND RAN LT ENG ALL CHECK NORMAL. INSPECTED HYD FILTERS IN LT PYLON PRESSURE AND CASE DRAIN FILTERS, ALL CHECK OK.

Part: CONTROLLER — MALFUNCTIONED (EMERGENCY LIGHTS)

CABIN EMERGENCY EXIT LIGHT CAME ON INTERMITTENTLY. REPLACED CONTROL PANEL.

Part: WIRE — FAILED (LT WINDSHIELD)

STRONG FUMES IN COCKPIT. DIVERTED TO RDU. FOUND WIRING AT 1L FWD WINDSHIELD SMOKING. DEACTIVATED WINDOW HEAT SYS PER MEL 30-41-01A.

Part: LIGHT — FAILED (L2 DOOR)

L-2 EXTERIOR EMERGENCY LIGHT FAILED TO ILLUMINATE ON SYSTEM TEST. RELAMPED LIGHT ASSY, NOW CKS NORMAL.

Part: NR 1 EDP — FAILED (LT MLG WW)

DURING CRUISE, LT HYD QTY EICAS MSG AND RSVR LIGHT. QTY .16, AFTER 5 MINS LT SYSTEM PRESSURE MSG, FLAPS 20, LANDING MADE AND NO NOSE WHEEL STEERING. FOUND PRESSURE LINE FROM PTU CONTROL MODULE LEAKING. SECURED SAME, CKS OK. FOUND NR 1 EDP NOT PRODUCING PRESS AND METAL IN FILTER. REMOVED AND REPLACED NR 1 EDP, FLUSHED LINES, REPLACED FILTERS AND OPS CKS GOOD.