N110DL

Part: WEDGE — DELAMINATED (T/E FLAP) · airframe 62,776 hrs · 29,907 cycles

AFT FLAP T/E WEDGE BONDED ASSY WAS FOUND DELAMINATED BEYOND THE SCOPE OF A LOCALIZED REPAIR. REPAIR PER ER/A 417896-14.

Part: IDG — LACK OF LUBE (NR 1 ENGINE) · airframe 57,040 hrs · 27,159 cycles

ON T/O ROLL, LT GEN DRIVE EICAS MSG CAME ON. ABORT T/O AT 100 KNTS. BPCU INDICATES SERVICE IDG. SERVICED IDG AND RAN ENGINE.

Part: SKIN — CORRODED (CENTER WING) · airframe 56,882 hrs · 27,092 cycles

CORROSION DAMAGE FOUND ON THE UPPER SURFACE OF THE CENTER WING SKIN AND IN THE UPPER SPAR CAP AT STA 955, RBL 70 - 90. IN NORDER TO VERIFY REMOVAL AND FACILITRATE A REPAIR THE LOWER CHORD OF THE RBL 74.81 FLOORBEAM WAS CUT FWD TO THE DAMAGE AND THE AFT SECTION REMOVED. THIS CHORD IS SPLICED IN AND THE BLENDED CORROSION AREAS ARE APPROVED AS ALLOWABLE DAMAGE. 396345-14.

Part: BULKHEAD — WORN (NR 1 PYLON) · airframe 56,882 hrs · 27,092 cycles

HOLE FOUND ELONGATED IN THE AFT BULKHEAD OF THE NR 1 PYLON ON THE LOWER FWD GSE HOLE (6TH FROM THE TOP). THE RIVET HOLES INSTALLED PER BOEING S/B 767-54-0010 WERE DOUBLE DRILLED. ADDITIONAL WEAR DAMAGE FOUND JUST BENEATH THE GSE HOLE. ER/A 396279-14.

Part: SKIN — PUNCTURED (BS 1197)

THE FUSELAGE SKIN WAS PUNCTURED BETWEEN FS 1197 & 1219 AND BETWEEN STRINGERS 36L & 38L. STRINGERS 36L & 37L WERE CRACKED AND THE O/B SKIN FLANGE OF STRINGER 38L WAS CRACKED. THE DAMAGED SKIN WAS CUT OUT WITH A 10 X 18 CUTOUT AND THE DAMAGED FLANGE OF STR 38L WAS TRIMMED OUT. THE STRINGERS WERE REPAIRED PER B767 SRM, THE SKIN WAS REPAIRED WITH AN EXTERNAL ALUM DOUBLER PER ER/A 368828-14, REV A.

Part: SLIDE — DEPLOYED (LT WING)

LT OVERWING SLIDE DEPLOYED IN FLIGHT PASSING THRU FL 12 OUT OF ATL. MTC OBSERVED LINKAGE ON DOOR RELEASE MECHANISM, FOUND THIRD LINKAGE FROM FORWARD EDGE BENT AND BROKEN, CAUSING CENTER TWO LATCHES TO RELEASE. FORWARD AND AFT LATCHES WERE FOUND INTACT WITH DOOR KEEPERS STILL IN PLACE. SLIDE AND DOOR WERE FOUND MISSING, AND FIVE SURROUNDING PANELS DAMAGED. SQUIBB WAS FOUND NOT FIRED AND SLIDE INFLATION BOTTLE EMPTY. (P/N 251205959) BROKEN LINAGE, (P/N BACT32G64-1072). REPLACED SAME.

Part: SLIDE — DETACHED (LT OVERWING)

PASSING 21,000 FT MSL, FLT ATTENDANTS COMPLAINED OF LOUD NOISE. ALSO, HAD EICAS MSG LT SLIDE DOOR AND OVERHEAD DISCREET EMERG DOORS. AIR TURNBACK TO ATL. FOUND LT OVERWING SLIDE PANEL AND SLIDE DEPARTED AIRCRAFT. SEVERAL SMALL ABRASIONS AROUND SURROUNDING AREA. REPLACED SLIDE, REPAIRED SURROUNDING AREA.

Part: DOOR — MISSING (LT SLIDE)

PASSING 12,000 FT, FLT ATTENDANT REPORTED LOUD NOISE. ALSO, HAD LT SLIDE DOOR EICAS MSG AND OVERHEAD DISCREET EMER DOORS. SLIDE HAD DEPARTED A/C WITH FAILURE OF DOOR. REPLACED DOOR SLIDE AND DAMAGED PANELS.

Part: SKIN — DELAMINATED (NR 3 LE SLAT)

THE UPPER SKIN ON THE NR 3 SLAT TRAILING EDGE WAS FOUND WITH A 3 X 4 DENTED/DELAMINATED AREA. THE DAMAGED SKIN WAS TRIMMED AWAY AND REPAIRED PER B767 SRM 57-43-02 AND DOCUMENTED PER ER/A 366773-14AD.

Part: OVEN — CONTAMINATED (GALLEY)

SHORTLY AFTER TAKEOFF, SMOKE OBSERVED FROM AFT GALLEY OVENS. COULD NOT DETERMINE SOURCE OF SMOKE, FOOD OR ELECTRICAL. FOUND BURNT SUBSTANCE IN CORNER OF LOWER LEFT OVEN IN AFT GALLEY. REPLACED OVEN ASSEMBLY AND NEW OVEN, OPS NORMAL.

Part: FLOORBEAM — CORRODED (BS 850)

CORROSION DAMAGE WAS FOUND ON THE UPPER CAP OF THE OVERWING LONGITUDINAL FLOORBEAM AT RBL 54, FROM BS 850 TO THE AFT END OF THE UPPER CAP AT APPROX BS 1000. THE UPPER CAP WAS REPLACED, BUT THE ORIGINAL EXTRUSION COULD NOT BE OBTAINED. REPAIRED PER ERA 332058-14.

Part: FLOORBEAM — CORRODED (BS 287)

CORROSION WAS FOUND ON THE UPPER SURFACE OF THE BS 287 FLOORBEAM UPPER CHORD. IN ADDITION, AN EXISTING REPAIR WAS ALSO LOCATED IN THE SAME AREA. REPAIRED PER ERA 332044-14.

Part: WEDGE — DELAMINATED (NR 1 LE SLAT)

DELAMINATION WAS FOUND ON THE NR 1 SLAT T/E WEDGE. DELAM AREA IS APPROX 4 IN DIAMETER. REPAIRED PER ERA 365245-14AD.

Part: SKIN — PUNCTURED (BS 422)

THE FUSELAGE SKIN AT FS 422 BETWEEN STRINGERS 21L AND 22L WAS PUNCTURED BY GROUND EQUIPMENT. THE FINAL SKIN CUTOUT WAS 6.5 BY 5. THE DAMAGE WAS REPAIRED WITH A SKIN DOUBLER. INSTALLED PER THE PROCEDURES OF THE B767 SRM AND DOCUMENTED PER ER/A 300885-14, REV B.

Part: UNION — BROKEN (ADP)

AFTER T/O, RETRACTED GEAR, RAISED FLAPS TO 5 DEG, THEN 1 DEG AND LOST HYD FLUID IN CTR SYS. FLAPS REMAINED AT 5 DEG, RAISED WITH ALT SYS. MTC FOUND UNION (P/N S270T230- 20) ON OUTLET OF ADP PUMP BROKEN. REPLACED WITH AS1582C10.

Part: CHECK VALVE — INOPERATIVE (RT PACK)

AFTER T/O, A/C WOULD NOT COOL. HOT AIR ENTERED PASSENGER CABIN AND COCKPIT UNABLE TO STOP HOT AIR ISOLATED BOTH SIDES, NO HELP. REPLACED RT PACK TRIM AIR CK VALVE (P/N 211102808) (MFG/NR 3202726-1) (S/N 2347).

Part: SKIN — DENTED (NR 1 SLAT)

THE NR 1 SLAT, TRAILING EDGE WEDGE WAS FOUND DENTED IN THE UPPER SKIN. THE DAMAGE WAS REPAIRED PER B767-200 SRM 51-70-10 FIG 9.

Part: FAN — FAILED (AC COMP)

DURING CRUISE, HAD ELECTRICAL BURNING ODOR IN CABIN. DEACTIVATED RECIRC FAN AND ODOR DISSIPATED. REPLACED RECIRC FAN, OPERATION NORMAL.

Part: TE WEDGE — DELAMINATION (NR 9/11 LE SLATS)

RT WING NR 9 AND NR 11 SLAT TRAILING EDGE WEDGES HAVE AREAS OF DELAMINATION. ACCOMPLISHED REPAIRS PER DL ERA 272145-14AD.

Part: FLAP — DELAMINATED (O/B FLAP LE)

NR 7 INTERM REPAIR TO L/E OF O/B FLAP JUST I/B OF THE NBR 8 FLAP DRIVE IS DELAMINATED.