N119DL

Part: CAP — CRACKED (HYD MODULE) · airframe 56,793 hrs · 27,889 cycles

CENTER HYDRAULIC SYSTEM DUMPED ALL FLUID WHILE MOVING FLAPS TO 15 DEGREES ON TAXI OUT SLC. FOUND CAP CRACKED AND SEPARATED FROM MODULE ON UPPER PART ABOVE HANDLE ON RT GND CHECKOUT MODULE. REPLACED RT CHECKOUT MODULE. LK AND OP CK GOOD. REMOVED, INSPECTED AND REPLACED BOTH CTR ELEC PUMP CASE DRAIN AND SYSTEM FILTERS. NO METAL FOUND.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,305 hrs · 27,162 cycles

THE LOWER AFT CORNER OF THE L1 DOOR CUTOUT WAS FOUND WITH A CRACK IN THE SKIN AND UNDERLYING BEARSTRAP AT FS 340. THE CRACK WAS REMOVED WITH A 4 X 5 INCHES CUTOUT THROUGH BOTH MEMBERS. THE CUTOUT WAS REPAIRED WITH 3 EXTERNAL ALUMINUM REPAIR DOUBLERS PER ER/A 090194-14, REV A.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,305 hrs · 27,162 cycles

CRACK REPAIR THE LOWER AFT CORNER OF THE L1 DOOR CUTOUT WAS FOUND WITH A CRACK IN THE SKIN AND UNDERLYING BEARSTRAP. THE CRACK WAS REMOVED WITH A 5 X 4 INCHES CUTOUT THROUGH BOTH LAYERS. THE CUTOUT WAS REPAIRED WITH 3 EXTERNAL ALUMINUM REPAIR DOUBLERS PER ER/A 090194-14.

Part: BULKHEAD — BIRD STRIKE (FUSELAGE) · airframe 54,408 hrs · 26,646 cycles

THE WEB OF THE FWD PRESSURE BULKHEAD AT FS 132.5 WAS PUNCTURED AS A RESULT OF A BIRD STRIKE BETWEEN LBL 10.6 & 16. THE VERTICAL BEAMS AT LBL 10.6 & 16 WERE DENTED. THE DAMAGED AREA OF WEB WAS REMOVED WITH A CUTOUT AND THE DENTED FLANGES OF THE BEAMS TRIMMED OUT. THE WEB WAS REPAIRED WITH AN ALUMINUM REPAIR DOUBLER AND THE FLANGES WITH ALUMINUM REPAIR ANGLES PER ER/A 087969-14, REV A.

Part: SUPPORT BEAM — CORRODED (LT WING) · airframe 53,242 hrs · 26,105 cycles

WING LT INBD FLAP OUTBD SUPPORT BEAM NR 3 SUPPORT : CORROSION IN AFT ATTACH HOLE BORES. THE AFT 4 ATTACH HOLES FOR THE OUTBD SUPPORT BEAM AT THE INBD FLAP ATTACH LOCATION WERE FOUND CORRODED. THE HOLES WERE REAMED TO REMOVE CORROSION, HFEC INSPECTED, OVERSIZED FOR AND INSURANCE CUT, AND BUSHED WITH ALUMINUM BUSHINGS TO RESTORE ORIGINAL HOLE SIZE. THE REPAIR WAS ACCOMPLISHED PER ER/A 385378-14.

Part: SUPPORT BEAM — CORRODED (LT WING) · airframe 53,242 hrs · 26,105 cycles

WING LT INBD FLAP OUTBD SUPPORT BEAM NR 3 SUPPORT : FWD FLAP ATTACH HOLE CORROSION, THE 2 FWD FLAP ATTACH HOLES ON THE OUTBD SUPPORT BEAM NR 3 SUPPORT FOR THE INBD FLAP LOCATION WERE FOUND CORRODED. THE CORROSION WAS REMOVED BY OVERSIZING THE BORES, HFEC INSPECTING, OVERSIZING FOR AN INSURANCE CUT, AND INSTALLING ALUMINUM BUSHINGS TO RESTORE THE PROPER HOLE SIZE. THE REPAIR WAS ACCOMPLISHED PER ER/A 385394-14.

Part: SUPPORT BEAM — CORRODED (T/E FLAP) · airframe 53,242 hrs · 26,105 cycles

WING / LT / INBD FLAP / INBD SUPPORT BEAM / SUPPORT NR 4 : FLAP ATTACH HOLE CORROSION THE LT INBD FLAP INBD SUPPORT BEAM WAS FOUND WITH CORROSION IN THE AFT INBD AND AFT OUTBD ATTACH LUG HOLES. THE HOLES WERE REAMED TO REMOVE CORROSION, HFEC INSPECTED, OVERSIZED, AND ALUMINUM BUSHINGS INSTALLED TO RESTORE THE AREA. THE REPAIR WAS ACCOMPLISHED IAW ER/A 385379-14.

Part: SMOKE — DETECTED (CABIN) · airframe 50,079 hrs · 24,590 cycles

AFTER T/O SMOKE IN MID CABIN WITH SMOKE DETECTOR GOING OFF IN MID CABIN. RETURNED TO LAND. LT PACK TRIPPED AND LT ENG BLEED LIGHT ILLUMINATED. ON GROUND SMOKE DISSIPATED. COMPRESSOR WASH NUMBER 1 ENGINE. AFTER WASH - RUN ENG 5 MINS AT IDLE, RUN PACKS/CYCLE A/I SYS. RUN ENG AT PWR ABOVE 60 N1 FOR 5 MIN-R PACKS/CYCLE A/I SYS. TO PREVENT ATB OR RTO DUE TO SMOKE/OD IN CABIN. PERFORMED ENG WASH PER 72-00-00-7-G-00.

Part: BEAM — CRACKED (L/E SLAT) · airframe 49,243 hrs · 24,184 cycles

NR 5 LEADING EDGE SLAT NOSE BEAM WAS FOUND DAMAGED AT STA 439. REPAIR PER ER/A 402159-14.

Part: SWITCH — MALFUNCTIONED (COCKPIT) · airframe 48,967 hrs · 24,044 cycles

DURING THE BOARDING OF FLIGHT 706 FROM SEA/ATL CREW REPORTED SMOKE IN THE COCKPIT. CAUSE OF SMOKE WAS FOUND TO BE THE RT AFT FUEL PUMP SWITCH IN P5 PANEL. REPLACED SWITCH ASSY, PART WAS REPLACED.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 47,699 hrs · 23,413 cycles

FOUND ON L/O CHECK, DOOR R1 EXT EMERGENCY SLIDE LIGHT INOP. REPLACED LIGHT ASSY, CHECK GOOD.

Part: BOTTLE — DISCHARGED (ESCAPE SLIDE) · airframe 45,214 hrs · 22,234 cycles

ON LAYOVER FOUND RT WING OVERWING SLIDE BOTTLE PRESS LOW. REPLACED BOTTLE.

Part: SKIN — CRACKED (BS 1197)

SKIN CRACKED AT VHF ANTENNA CUTOUT AT STA 1197 + 99 AND BL 0. DAMAGE REMOVAL RESULTED IN A RECTANGULAR CUTOUT MEASURING 3 I/B-O/B BY 14 FWD/AFT. ER/A 334036-14 REV A.

Part: MEGAPHONE — BROKEN (CABIN)

ON L/O, FOUND FWD CLOSET MEGAPHONE BROKEN. REPLACED MEGAPHONE.

Part: OVEN — DIRTY (GALLEY)

ACRID FUMES IN COCKPIT AND CABIN COULD NOT ISOLATE. POSSIBLY STRONGER IN FWD GALLEY AND FC AREA. INSPECTED E & E, ALL CARGO COMPARTMENTS, NOTHING FOUND. REMOVED ALL FC GALLEY OVENS AND COFFEEMAKERS, NOTHING FOUND. CHECKED OVERHEAD AREA OF FC CABIN, NOTHING FOUND. RAN BOTH ENGS AT CRZ POWER FOR 20 MINS WITH BOTH PACKS ON, NO TROUBLE FOUND. REMOVED DIRTY FOOD TRAYS FROM FC OVENS.

Part: RETRACT MECH — MALFUNCTIONED (RT MLG)

RT MAIN GEAR REMAINED EXTENDED AFTER T/O, ALT GEAR EXTENSION WORKED OK. MTC IN WORK ON GEAR RETRACTION AT TOC. NO NOTICEABLE DAMAGE TO GEAR. GEAR PINS INSTALLED FOR MTC.

Part: SKIN — DELAMINATED (LT SLATS)

UPPER SKINS ON THE TRAILING EDGE WEDGES OF THE NR 9, 10, AND 12 SLATS WERE FOUND WITH DELAMINATED AREAS. REPAIRED PER ERA 365048-14AD.

Part: LIGHT — INOPERATIVE (LT OVERWING)

FOUND ON LAYOVER, LT OVERWING EMERGENCY LIGHTS INOP. RELAMPED, CHECKS GOOD.

Part: KEEL BEAM — CORRODED (BS 917)

LT KEEL BEAM HAD CORROSION AT STA 917. REPAIRED PER ERA 330983-14.

Part: SEAT TRACKS — CRACKED (BS 786)

SEAT TRACKS AT LBL AND RBL 54 WERE FOUND CRACKED IN THE VERTICAL WEB OF THE UPPER CHORD AT FS 786. REPAIRED PER ERA330946-14.

Part: FLOORBEAM — PUNCTURED (BS 287)

A NEW UPPER TEE CHORD WAS ADDED TO THE BEAM EXTRUSION PER SRM. DURING ACCOMPLISHMENT THE FLOORBEAM WEB WAS PUNCTURED. REPAIRED PER ERA 330971-14.

Part: FLOORBEAM — CORROSION (BS 1480)

CORROSION WAS FOUND ON THE UPPER CAP AT FS 1480 AT LBL 30 AND ENTIRE RT SIDE. REPAIRED PER ERA330975-14.

Part: FLOORBEAM — CRACKED (BS 246)

FS 246 FLOORBEAM WEB WAS FOUND WITH VERT CRACK APPROX 3 LONG AT RBL 20. THE OVERLYING STIFFENER WAS ALSO CRACKED. REPAIRED PER ERA 330992-14.

Part: FRAME — CRACKED (BS 544)

FORWARD CARGO COMPARTMENT STA 544 FRAME UPPER CHORD HAD AN 8 INCH CRACK IN THE RADIUS OF THE HORIZONTAL FLANGE AT RBL 16. REPLACED FLANGE.

Part: WEDGE — DELAMINATED (NR 9 LE SLAT)

THE NR 9 LEADING EDGE SLAT TRAILING EDGE WEDGE WAS FOUND TO HAVE THE UPPER SKIN DELAMINATED 4 FROM THE T/E AND 34 FROM THE INB'D END. THE DAMAGE AREA MEASURES 6 FWD-AFT AND 5.5 INBD-OUTBD. THE TRAILING EDGE WEDGE IS M/F 0.016 5052-H38 FACE SHEETS WITH A METALLIC HONEYCOMB CORE PER BMS 4-6, TYPE 4.1-25. VISUAL AND COIN TAP INSP PER 1-65079-12AD, OPN 0302 TO DETERMINE EXTENT OF DAMAGE; TRIM BACK DISBONDED FACT SHT, VISUALLY INSPECT; REPAIR PER B767-300 SRM, 57-43-02, FIG 201; TAPER FWD AND SIDE EDGES FOR AE SMOOTHNESS.

Part: SENSOR — OUT OF ADJUST (RT MLG)

AFTER T/O OUT OF ATL, GEAR HANDLE FAILED TO COME UP. ACARS DID NOT SENSE AIRBOURN AND LATER GOT TAIL SKID LIGHT, RETURN TO ATL. SHIMMED TRUCK TILT SENSORS S245/S246 ON RT MLG. RAN GEAR CHECKS, OK. SENSORS S238/S260 OK ON LT MLG.

Part: IDG — REQD SERVICE (NR 2 ENGINE)

LOST LEFT ENG GEN AT ABOUT 200 FT AFTER T/O, LOST RT GEN AT APPROX 1,000 FT. RETURNED TO BOS. RT IDG BPCU FAULTS LOW OIL PRESS, IDG HI DELTA TEMP/IDG/PMG WIRING PER 24-20-00. FOUND RT DPI EXTENDED, REQUIRES IDG REPLACEMENT. CHECKED SERV OK. FWD TO MCO AND PLA, LEFT GEN BPCU FAULTS/IDG HI DELTA TEMP/UNDER FREQ/IDG/PMG WIRING PER 24-20-00. CHECKED LEFT IDG DPI NOT EXTENDED. CHECKED FILTER, OK. FOUND IDG UNDERSERVICED. SERV SAME, LEAK CHECK AND OPS CKS NORMAL. NO LEAKS FOUND.

Part: HYD LINE — CHAFED (NR 1 ENGINE)

L HYD QTY EICAS MSG. LT ENG HYD QTY 0.46 RF. LT ENG PRIMARY AND DEMAND PUMPS OFF. REPLACED HYDRAULIC LINE AT #1 ENGINE HYDRAULIC PUMP. SYSTEM CHECKS NORMAL.

Part: MEC — MALFUNCTIONED (NR 2 ENGINE)

TAKEOFF ABORTED AT 80 KTS, RT ENG ONLY 88 PERCENT, N1 ACC WAS ALSO SLOW. REPLACED RT ENG, MEC LEAK CHECKED PERFORMED, ENG RUN PER PFHB AND ALL IND NORMAL.

Part: BULB — FAILED (CABIN)

DURING L/O, FOUND AFT RT DOOR EMERGENCY LIGHT INOP AND LT WING SLIDE LIGHT INOP. RELAMPED BOTH, CKS GOOD.

Part: TRUNNION — FRACTURED (LT MLG)

AFTER ARRIVAL AT GATE WHILE AIRCRAFT WAS MOTIONLESS, THE LEFT MAIN LANDING GEAR TRUNNION OUTER CYLINDER FRACTURED AT THE AFT TRUNNION BORE. THE LOWER 180 OF THE AFT END SEPARATED REMOVING A 6 INCH LONG PIECE. INITIAL VISUAL EXAMINATION REVEALS SEVERE CORROSION PRESENT IN THE CHAMBER UNDER THE SEALED BUSHING FLANGE. THE LANDING GEAR TRUNNION WAS REPLACED. THIS IS THE FIRST OCCURANCE OF THIS TYPE OF FAILURE ON DALA 767 AIRCRAFT.

Part: WEDGE — DELAMINATION (NR 4 TE FLAP)

FOUND DURING J-2 LETTER CHECK, DELAMINATION AREA ON LOWER SKIN OF NR 4 FLAP T/E WEDGE. REPAIRED PER SRM 51-70-07, AND PAINTED AREA.