N107DL

Part: SKIN — CORRODED (FUSELAGE) · airframe 67,030 hrs · 32,242 cycles

CORROSION FOUND ON THE FUSELAGE SKIN AT APPROX FS 1323 BETWEEN S-39R AND 39L. DAMAGE REPAIRED WITH DOUBLER/TRIPLER ARRANGEMENT VIA ERA 091295-14 REV B.

Part: SILL — CORRODED (FS) · airframe 67,030 hrs · 32,242 cycles

ER/A 091340-14, C2 DOOR LOWER SILL WAS FOUND WITH CORROSION LOCATED ON THE INNER CHORD UPPER FLANGE AT FS 1270-1279. ADDITIONAL CORROSION WAS FOUND ON THE WEB AT FS 1279.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHT) · airframe 66,519 hrs · 32,010 cycles

EMERGENCY EXIT SIGNS INOP AT RT AND LT OVERWING EXIT DOORS. REPLACED EMERGENCY PWR SUPPLY BATTERIES AT M737, M732 PER M/M, NOW OPS NORMAL.

Part: FITTING — CORRODED (LT WING TE FLAP) · airframe 66,208 hrs · 31,862 cycles

THE INBOARD SUPPORT BEAM FOR THE INBOARD FLAP ON THE LT WING WAS FOUND WITH CORROSION IN THE FLAP ATTACH HOLES. THE CORROSION WAS REMOVED BY OVERSIZING THE HOLES. ALUMINUM REPAIR BUSHINGS WERE FABRICATED AND INSTALLED IN THE HOLE BORES. THE REPAIR WAS ACCOMPLISHED PER ER/A 088453-14.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 60,046 hrs · 28,692 cycles

RELAMPED R2 EXTERIOR EMERGENCY LIGHT.

Part: FRAME — CRACKED (FUSELAGE) · airframe 59,587 hrs · 28,449 cycles

DURING INSPECTION OF THE 1809 BULKHEAD PER S/B 767-53-0078 R.2, CRACKS WERE FOUND IN THE LT AND RT CHORDS REQUIRING PERMANENT MODIFICATION (SPLICING IN NEW SECTION OF CHORD PER THE SERVICE BULLETIN). ER/A 397806-14AD.

Part: SKIN — CORRODED (FUSELAGE) · airframe 56,646 hrs · 27,196 cycles

SKIN CORROSION WAS FOUND AT FS 786 AT STRINGER 38L AND WAS REMOVED WITH A 3 X 3 INCH CUTOUT. THE CUTOUT WAS NEAR AN EXISTING REPAIR FOR A 2 X 3 INCH REPAIR BETWEEN STRINGER 39L & 39R. THE EXISTING REPAIR WAS REMOVED AND BOTH CUTOUTS REPAIRED WITH AN ALUMINUM DOUBLER AND TRIPLER INSTALLED PER ER/A 378224-14, REV B.

Part: HANDLE — STUCK (COCKPIT) · airframe 56,618 hrs · 27,182 cycles

WHEN GEAR SELECTED DOWN GEAR DISAGREE LIGHT AND EICAS MESSAGE ILLUMINATED. ON APPROACH GEAR TOO LOW AURAL ANNOUNCED. FOUND GEAR HANDLE STUCK SLIGHTLY UP FROM DOWN DETENT PUSHED HANDLE DOWN, MESSAGE CLEARED AND AMBER GEAR LIGHT EXTINGUISHED. REMOVED AND REPLACED THE LANDING GEAR CONTROL LEVER MODULE PER MM, CKS OK.

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 55,671 hrs · 26,775 cycles

ALL LEFT SIDE EXTERIOR EMERGENCY LIGHTS INOP. REPLACED BATTERY PACKS M736 AT M738. RELAMPED FWD SLIDE LIGHT, EMERGENCY LIGHTS CHECK GOOD PER M/M.

Part: HOSE — LEAKING (LT MLG)

ON DEPARTURE, UNABLE TO RETRACT LT MAIN LANDING GEAR. RETRACTION OF OTHER GEAR NORMAL. WITH HANDLE IN UP MODE, HAD GREEN LT MAIN LIGHT AND AMBER GEAR LIGHT AND AMBER DOOR LIGHT. EICAS GEAR DISAGREE AND GEAR DOOR MSG'S. FOUND LT GEAR LEVELING CYLINDER RETURN LINE LEAKING. REPLACED LINE. LEAK CHECKED SATISFACTORY. RESET FUSE PER M/M 32-32-19-4-00.

Part: FITTING — CRACKED (LT WING)

A CRACK WAS FOUND IN THE LHS KICKLOAD FITTING IN THE INBD HOLE ON THE OUTER WING SIDE. THE HOLE WAS REAMED TO REMOVED THE CRACK INDICATION. FINAL REWORKED HOLE DIAMETER IS 0.947. REF NPRM 98-NM-278-AD. REWORKED PER ERA 333356-14AD.

Part: SKIN — CORRODED (BS 955-977)

CORROSION ON WING CENTER SECTION UPPER SKIN AT FS 955-977 BETWEEN RBL 54-74, ERA 333344-14 REV A.

Part: SKIN — CORRODED (CENTER WING)

CORROSION ON CENTER WING SKIN UPPER SURFACE AT SPLICE STRINGER U-17 FROM RBL 74 TO RBL 94, ERA 333346-14 REV A.

Part: SKIN — DENTED (BS 1540)

TWO DENTS FOUND DURING HMV, ON THE LOWER LOBE FUSELAGE SKIN AFT OF THE L2 DOOR OPENING AT STA 1555 AND 1560 BETWEEN STRINGERS 21L AND 22L. EXTERNAL DOUBLER/TRIPLER INSTALLED PER ER/A 333345-14 REV A.

Part: SKIN — GOUGED (BS 1260)

GOUGE IN THE LHS SKIN PANEL BETWEEN BS 1241 TO 1285 AND S22L TO S25L REQUIRED REWORK. REWORKED AND REPAIRED PER ERA 333352-14, REV. A.

Part: ACTUATOR — FAILED (RT MLG)

ON T/O FROM MCO, RT LANDING GEAR DID NOT RETRACT. DIVERTED TO ATL WITH ALL GEAR DOWN. REPLACED RT MLG SIDE BRACE LOCK ACTUATOR.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

RT OVERWING EGRESS LIGHTS INOP. REPLACED BATTERY POWER SUPPLY, CKS GOOD.

Part: SKIN — CRACKED (NR 2 PYLON)

NACELLES, NR 2 PYLON, TORQUE BOX, INBD STRUT SKIN, ACCESS CUTOUT: REPAIR FOR CRACK. THE NR 2 PYLON TORQUE BOX SKIN WAS FOUND WITH A CRACK IN THE UPPER AFT CORNER OF THE ACCESS CUTOUT AT NAC STA 231. THE CRACK WAS STOP DRILLED ON A TIME-LIMITED BASIS WITH A REPAIR DOUBLER INSTALLED WITHIN 10 DAYS. FURTHER TORQUE BOX MODIFICATIONS/REINFORCEMENTS ARE TO BE ACCOMPLISHED AT NEXT HMV VISIT. THE REPAIR WAS ACCOMPLISHED PER ER/A 364868-14.

Part: WEDGE — DELAMINATED (NR 5 LE SLAT)

NR 5 LEADING EDGE SLAT T/E WEDGE WAS FOUND WITH DELAMINATION ON THE UPPER SURFACE MEASURING 3 X 5. REPAIR PER ERA 364831-14AD.

Part: BATTERY PACK — DISCHARGED (CABIN)

EMERGENCY TRACK LIGHTING DIM IN COACH CABIN WITH SWITCH IN THE ARMED POSITION. REPLACED THE 9009 AND 9010 BATTERY PACKS, OPERATIONAL CHECK NORMAL.

Part: DOUBLER — CORRODED (BS 1445-1448)

THE FUSELAGE LT SIDE BULK CARGO DOOR INTERNAL BEARSTRAP SURROUND DOUBLER WAS FOUND WITH CORROSION BETWEEN FS 1445 AND 1448, JUST OUTBOARD AND ABOVE THE LOWER SILL OUTER CHORD ATTACHMENT. THE DOUBLER WAS BLENDED AND REINFORCED WITH A SHEET METAL DOUBLER. REV. B TO ERA PROVIDES FAA APPROVAL.

Part: SKIN — CORRODED (BS 1370)

THE FUSELAGE SKIN AT F.S.1370 AND STR 39R WAS FOUND CORRODED. THE SKIN WAS CUT OUT AND REPAIRED WITH A DOUBLER. REV. A TO ER/A PROVIDES FAA APPROVAL.

Part: SKIN — CORRODED (BS 676 BL0)

THE FUSEALGE SKIN WAS FOUND CORRODED AT F.S. 676 BETWEEN STR'S 39L AND 39R. THE DAMAGE WAS CUT OUT AND REINFORCED WITH A DOUBLER. REV A TO ERA PROVIDES FAA APPROVAL.

Part: LENS — MISSING (CABIN)

FROM CDL RED TRACK LIGHT EXIT LENS MISSING FROM RT OVERWING EXIT. REPLACED LENS AND BULB, OPN NORMAL.

Part: FAIRING — MISSING (LT WING)

ON ARRIVAL, FOUND FAIRING PANEL 195CL MISSING AND PANEL 195DL LEFT WING DAMAGED. INSPECTED AIRCRAFT FOR ADDITIONAL DAMAGE. REPLACED PANELS PER ERA 359898-14. REPAIRED FUSLAGE DAMAGE BETWEEN FS 1219 AND FS 1241 AND ABOVE S-22 AND S-23 PER SRM.

Part: SKIN — DELAMINATED (NR 12 LE FLAP)

NR 12 SLAT T/E WEDGE HAS TEMPORARY REPAIR 7 INCHES FROM O/B END. N/R NR 896, CHANGED WEDGE PER CMM 57-43-41. N/R NR 7738, T/E WEDGE DENTED 40 INCHES FROM O/B END UPPER SURFACE. CHANGED WEDGE PER CMM 57-43-41. REPAIRS ACCOMPLISHED AT SHOP VISIT.