N109DL

Part: BATTERY — INOPERATIVE (CABIN) · airframe 63,202 hrs · 30,332 cycles

ON LAYOVER FOUND EMERGENCY LIGHTS AT EXTERIOR L2 AND OVERWING SLIDE INOP ON LT SIDE. REPLACED BATTERY PACK AND CHARGER PER M/M. OPS CHECK OK.

Part: FRAME — CRACKED (FUSELAGE) · airframe 61,718 hrs · 29,592 cycles

THE FWD, OUTER CHORD OF THE FS 1809.5 WAS FOUND WITH A 5 INCH CRACK ALONG THE RADIUS NEAR STRINGER 7R. THE CRACK IS OUTSIDE THE AREA ADDRESSED BY BAC S/B 767-53-0078 AND AD 2001-09-13. THE CRACKED SECTION OF CHORD WAS CUTOUT AND REMOVED. A FILLER SECTION WAS INSTALLED, AND THE CHORD REPAIRED WITH 3 ALUMINUM REPAIR ANGLES PER ER/A 383735-14, REV A.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 57,469 hrs · 27,494 cycles

FLIGHT DECK EMERGENGY EXIT LIGHT FAILED TO ILLUM WITH OVHD EMERGENCY LIGHT SW ON ALL CABIN EMERGENCY LIGHTS WORK NORMAL. REPLACED EMERGENCY LIGHT ASSY OPS CKS GOOD.

Part: FAN — INOPERATIVE (LEFT CARGO AREA) · airframe 57,073 hrs · 27,325 cycles

STRONG ODOR AND IRRITATING FUMES IN COCKPIT AT FL370. DECLARED EMERGENCY, O2 MASK ON, RETURNED TO CVG . LT RECIRCULATION FAN INOP, MESSAGE CAME ON DURING DESCENT. FOUND LT RECIRCULATION FAN INOP UPON ARRIVAL. PULLED AND COLLARED LT RECIRCULATION FAN C/B ON P-36 PANEL. INSPECTED LT RECIRCULATION FAN, FOUND NO FIRE DAMAGE IN DISTRIBUTION AREA. FWD TO MCO AND PLC PER MEL 21-25-01A.

Part: BATTERY PACK — INOPERATIVE (SLIDE LIGHT) · airframe 56,426 hrs · 27,058 cycles

LT LOWER WING SLIDE LIGHT INOP. REPLACED BATTERY PACK M738.

Part: OUTFLOW VALVE — FAILED (AFT) · airframe 56,182 hrs · 26,948 cycles

AT FL240 GOT CABIN PRESS AUTO CTL 2 EICAS MSG AND CABIN ALT EICAS MSG. BITE FAULTED NR 2 AC MOTOR. REPLACED OUTFLOW VALVE.

Part: TURBINE — DAMAGED (NR 1 ENGINE)

NR 1 ENG HIGH VIBS 5.0 N-2 WITH HUM AND VIBRATION. FOUND DAMAGE TO TURBINE. REPLACING ENGINE.

Part: ENGINE — FAILED (NR 1)

NR 1 ENG SLOW TO ACCELERATE, SEVERAL RED LINES. REPLACED ENGINE.

Part: VSI — FAILED (LT COCKPIT)

CAPTAINS VSI BLANKED AFTER BLUE SPARK OCCURED UNDER AND BEHIND CAPTAINS CLOCK PANEL. REPLACED VSI.

Part: SKIN — DENTED (BS 632)

FUSELAGE SKIN WAS FOUND WITH A GOUGE LOCATED AT BS 632 BETWEEN STRINGERS 30R AND 31R. REPAIRED PER ERA 331774-14 REV B.

Part: BULKHEAD — DAMAGED (NR 2 PYLON)

BULKHEAD AT NAC STA 163.5 ON THE RT OF PYLON HAD TOOLING DAMAGE THAT NECESSITATED PART REPLACEMENT. NO REPLACEMENT PART AVAILABLE, A NEW PART WAS FABRICATED. PART FABRICATED PER ERA 331773-14.

Part: SKIN — CORRODED (CENTER WING)

CORROSION WAS FOUND AROUND SEVERAL FASTENER HOLES WHERE THE FWD AND AFT CTR WING UPR SKIN ATTACHES TO STGR U-17 BETWEEN LBL 74 AND LBL 90. A SECTION AFT OF THE AFT UPPER WING SKIN WAS REMOVED. REPAIRED PER ERA 331767-14.

Part: WEDGE — DENTED (NR 7 LE SLAT)

THE RT WING NR 7 SLAT WAS FOUND WITH A 5 X 2.5 X .025 DENT ON THE LOWER SURFACE THE TRAILING EDGE WEDGE. THE DENT WAS REPAIRED PER THE B767 SRM 57-43-02 AND DOCUMENTED PER ER/A364235-14AD.

Part: INVERTER — FAILED (E/E COMP)

HAD STATIC INVERTER MSG ON EICAS FOLLOWED BY SMELL OF SMOKE. A/C DIVERTED INTO BIS. STATIC INVERTER WAS REPLACED AND FLT CONTINUED ON TO PDX.

Part: TR UNIT — FAILED (RADAR COMPT)

RADAR FAILED IN FLIGHT. R/T FAULT DISPLAYED. REPLACED TRANSCVR. OPS. CHECK NORMAL.

Part: FAN — FAILED (AC COMP)

ON APPROACH, THE LT RECIRC FAN EICAS MSG CAME ON WITH SOME SMOKE IN THE CABIN. AFTER TURNING THE FAN OFF, THE SMOKE DISSIPATED. FWD TO MCO AND PLAC PER MEL 21-25-01A. FAN WAS REPLACED, OPERATION NORMAL.

Part: LE SKIN — GOUGED (RT ELEV)

DURING LETTER CHECK, FOUND RT O/B ELEVATOR WITH GOUGE IN L/E SKIN. REPAIRED PER SRM 55-20-02.

Part: COWL — DENTED (NR 2 ENGINE)

DENT IN NOSE LIP SKIN AT 7 O/C POSITION. REPAIRED PER SRM 54-11-01 FOR NR 2 ENGINE INTAKE COWL.

Part: CORNER — DAMAGED (NR 1 TE FLAP)

FOUND DURING LETTER CHECK, NR 1 FLAP UPPER INBD CORNER DAMAGED. REPAIRED PER SRM 57-53-01 PAINTED AREA LT WING.

Part: TE WEDGE — DAMAGED (NR 1 TE FLAP)

FOUND DURING LETTER CHECK NR 1 FLAP DAMAGED 2 PLACES AT T/E EDGE LOWER SURFACE I/B OF NR 1 FLAP FAIRING. REPAIRED PER SRM 57-53-01, PAINTED AREA LT WING.

Part: LE SKIN — DAMAGED (NR 1 TE FLAP)

FOUND DURING LETTER CHECK NR 1 FLAP DAMAGE AT L/E JUST AFT OF NR 1 FLAP FAIRING. REPAIRED PER SRM 57-53-01 PAINTED AREA LT WING.