N12064

Part: AIR BOX — CRACKED (PYLON) · airframe 102,012 hrs · 21,583 cycles

INSPECTION FOUND A 2 INCH CRACK IN LOWER CENTER PYLON AIR BOX WHERE THE PRECOOLER AIR DUCT ATTACHES (I/B SIDE). THE CRACKED AREA WAS CUT OUT AND A REPAIR WAS INSTALLED IAW SRM 54-20-00, FIGURE 19A.

Part: FLASHLIGHT — INOPERATIVE (CABIN)

INSPECTION FOUND TWO EACH EMERGENCY PORTABLE FLASHLIGHTS INOPERATIVE. THE FLASHLIGHTS WERE REPLACED AND TESTED IAW MM 25-60-00.

Part: SUPPORT — CORRODED (BS 1860 - 1889)

INSPECTION FOUND LAV SUPPORT CORRODED AT STA 1860-1889, BL 0. THE LAV SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-31-01.

Part: CHANNEL — CORRODED (CARGO BAY)

INSPECTION FOUND CENTER CARGO COMPARTMENT LEFT CHANNEL CORRODED UNDER OMNI ROLLERS. A NEW CHANNEL WAS INSTALLED IAW SRM 53-42-01.

Part: SPAR — CRACKED (HORIZONTAL STAB)

INSPECTION FOUND A 3 INCH CRACK IN LEFT HORIZONTAL STABILIZER PANEL SIDE UPPER CHORD. THE CHORD WAS REMOVED AND A REPAIR WAS INSTALLED IAW SRM 51-33-01.

Part: SUPPORT — CORRODED (BS 1850 - 1890)

INSPECTION FOUND LAV SUPPORTS CORRODED AT STA 1860-1887, RBL 47 AND AT STA 1850-1890, LBL 47. THE SUPPORTS WERE REMOVED AND NEW SUPPORTS WERE INSTALLED IAW SRM 51-31-01.

Part: FRAME — CORRODED (BS 1780 & 1841)

INSPECTION FOUND CENTER CARGO COMPARTMENT LOWER FRAME CORRODED AT STA 1780 BETWEEN LONGERON 50L - 50R AND AT STA 1841, L49R - 50L. THE CORRODED AREAS WERE TRIMMED OUT AND REINFORCED WITH SHEAR CLIPS AND SPLICES IAW SRM 53-30-00, FIGURES 9 AND 10, AND SRM 51-31-01.

Part: FRAME — CORRODED (BS 1660 - 1680)

INSPECTION FOUND CENTER CARGO COMPARTMENT LOWER FRAME CORRODED FROM STA 1660-1680, LONGERON 51L - 51R. THE CORRODED AREA WAS TRIMMED OUT AND REINFORCED WITH SHEAR CLIP AND SPLICE IAW SRM 53-30-00, FIGURE 10 AND SRM 51-31-01.

Part: SUPPORT — CORRODED (BS 460 - 515)

INSPECTION FOUND CABIN FLOORBEAM SUPPORT CORRODED BETWEEN STA 460 AND 515, LBL 33. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-31-01.

Part: SUPPORT — CORRODED (BS 785 - 789)

INSPECTION FOUND GALLEY FLOOR SUPPORT CORRODED BETWEEN STA 785 AND 789, RBL 47. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 53-70-00, FIGURE 13 AND 51-31-01.

Part: SUPPORT — CORRODED (BS 395 - 475)

INSPECTION FOUND FLOOR SUPPORT CORRODED AT UPPER LOBE CABIN FLOOR AT STA 395-457, RBL 28-33 AND STA 420-475, LBL 27. THE FLOOR SUPPORTS WERE REMOVED AND NEW SUPPORTS WERE INSTALLED IAW SRM 51-31-01.

Part: SUPPORT — CRACKED (BS 495 - 615)

INSPECTION FOUND FLOOR SUPPORT CRACKED AT UPPER LOBE CABIN FLOOR STA 495-615, RBL 14. THE CRACKED AREA OF FLOOR SUPPORT WAS TRIMMED OUT. A NEW SECTION WAS INSTALLED IAW SRM 51-31-01 AND 51-21-01.

Part: FRAME — CRACKED (NR 3 ENG COMP)

THE NR 3 ENGINE A AND B FIRELOOP LIGHTS ILLUMINATED AND THE FIRE HANDLE FLASHED AFTER TAKEOFF FROM HNL. CHECKLIST PROCEDURES WERE COMPLIED WITH AND THE AIRCRAFT WAS RETURNED TO HNL WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 3 ENGINE 13TH STAGE MANIFOLD CRACKED. THE NR 3 ENGINE IS BEING REMOVED AND REPLACED. *S/D* ENGINEERING FOUND THE COMPRESSOR REAR FRAME BOSS TO THE 14TH STAGE CDP CRACKED.

Part: CHANNEL — CRACKED (RT MLG WW)

INSPECTION FOUND A 1 INCH CRACK IN HORIZONTAL CHANNEL OF OUTBOARD AFT FAIRING AT RT MLG WHEEL WELL. THE CRACKED TEE WAS REMOVED AND A NEW TEE WAS INSTALLED IAW SRM 53-53-01, FIGURE 4, 51-21-01, AND 51-31-01.

Part: SKIN — DENTED (LT TE FLAP)

INSPECTION FOUND THE LT OUTBOARD TRAILING EDGE FLAP INBOARD SKIN DENTED AT LOWER FLAP 29 INCHES FROM INBOARD END. THE DENTED AREA WAS TRIMMED OUT AND REINFORCED WITH DOUBLER IAW SRM 57-10-00, FIGURE 7, 51-21-01, AND 51-31-01.

Part: SKIN — DENTED (BS 515-535)

INSPECTION FOUND FUSELAGE SKIN DENTED AT STA 515 TO 535, S28L. THE DENTED AREA WAS TRIMMED OUT AND REINFORCED WITH DOUBLER AND FINGER DOUBLER IAW SRM 53-20-00, FIGURE 6, 51-21-01, AND 51-31-01.

Part: LIGHT — INOP (SEAT 21B,34K,36B)

INSPECTION FOUND THE EMERGENCY EXIT LIGHT AT SEATS 21B, 34K, AND 36B INOPERATIVE. THE EMERGENCY LIGHT IN SEATS 21B, 34K, AND 36B WERE REPLACED IAW MM 33-50-00.

Part: SKIN — DENTED (BS 1942)

INSPECTION FOUND RT FUSELAGE SKIN DENTED AT STA 1942, STRINGERS 51-52. THE DENTED AREA WAS TRIMMED OUT AND REINFORCED WITH INNER AND OUTER DOUBLERS IAW SRM 53-20-00, FIGURE 6, 51-21-01, AND 51-31-01.

Part: DOUBLER — CRACKED (RT WING)

INSPECTION FOUND A 2.7 INCH CRACK AND DELAMINATION ON RT WING MLG SUPPORT DOUBLER. THE CRACKED AND DELAMINATED AREAS WERE TRIMMED OUT AND REINFORCED WITH DOUBLER AND FILLER IAW SRM 53-45-01, FIGURE 1, 51-21-01, AND ECRA 5730-01595.

Part: SEAT TRACK — CORRODED (BS 1289)

INSPECTION FOUND SEAT TRACK CORRODED AT STA 1289, RBL 107. THE CORRODED SECTION OF SEAT TRACK WAS REMOVED AND A NEW SECTION WAS INSTALLED IAW SRM 53-70-00, FIGURE 18 AND 51-21-01.

Part: DOOR — CRACKED (RT MLG)

INSPECTION FOUND A 1.75 INCH CRACK AT AFT LOWER CORNER OF RT MLG WHEEL WELL DOOR. THE AREA WAS REINFORCED WITH A DOUBLER IAW SRM 51-21-01 AND 51-35-02.

Part: FLOORBEAM — CRACKED (BS 1275)

INSPECTION FOUND A 1 INCH CRACK IN FLOORBEAM AT STA 1275, RBL 104. REPAIRED IAW ECRA 5316-01000.

Part: BATTERY PACK — DISCHARGED (CABIN)

THE EMERGENCY LIGHT SYSTEM IN A ZONE FAILED AFTER SIX MINUTES. THE BATTERY PACKS WERE REPLACED AND OPERATION CHECKED GOOD IAW MM 33-50-00.

Part: EXHAUST NOZZLE — CRACKED (NR 2 ENGINE)

INSPECTION FOUND A 5 CRACK IN #2 ENGINE EXHAUST NOZZLE. THE #2 ENGINE EXHAUST NOZZLE WAS REPLACED IAW MM 78-11-08.

Part: THRUST REVERSER — CRACKED (NR 2 ENGINE)

INSPECTION FOUND A CRACK ON INNER SKIN ADJACENT TO OPEN CLOSE ACTUATOR OF #2 ENGINE C DUCT RH. THE #2 ENGINE R/H THRUST REVERSER WAS REPLACED IAW MM 78-32-11.

Part: THRUST REVERSER — DELAMINATED (NR 2 ENGINE)

INSPECTION FOUND #2 ENGINE L/H THRUST REVERSER UPPER AFT SIDEWALL DELAMINATED. THE #2 ENGINE L/H THRUST REVERSER WAS REPLACED IAW MM 78-32-11.

Part: FASTENERS — SHEARED (NR 2 PYLON)

INSPECTION FOUND SIX FASTENER HEADS SHEARED AT LOWER AFT FACE OF NR 4 BANJO FITTING, NR 2 PYLON. THE FASTENERS WERE REMOVED AND REPLACED WITH NEW FASTENERS IAW SRM 51-42-00.

Part: BULKHEAD — HOLE (BS 2007)

INSPECTION FOUND A .5625 DIAMETER HOLE IN AFT PRESSURE BULKHEAD BETWEEN FLOOR SUPPORT BEAM AND LONGERON 41L AT STA 2007. REPAIRED IAW SRM 53-40-00.

Part: ANGLE — CORRODED (BS 2007)

INSPECTION FOUND FLOORBEAM HORIZONTAL ATTACHMENT ANGLE CORRODED AT THIRD FLOORBEAM RT FROM O/B SIDE, STA 2007, AFT CARGO LAV AREA. THE AREA WAS REPAIRED IAW SRM 53-40-00 FIGURE 16 PAGE 93.