N17087

ATA 5510

Part: BRACKET — CRACKED (HORIZONTAL STAB) · airframe 103,244 hrs · 22,441 cycles

CRACK IN RIGHT ANGLE BRACKET ON RIGHT HAND DETACHABLE SEGMENT OUTER SUPPORT ANGLE OF HORIZONTAL STABILIZER LEADING EDGE (23). CAP REPLACED PER SRM 51-71-00.

ATA 5313

Part: LONGERON — CRACKED (FUSELAGE) · airframe 103,244 hrs · 22,441 cycles

FORWARD STAB BAY LONGERON L5 CRACKED AT Y2014 APPROXIMATELY 3 INCHES FORWARD (3). REPAIRED LONGERON PER SRM 51-42-00.

ATA 2560

Part: MEGAPHONE — INOPERATIVE (CABIN)

BOTH MEGAPHONES INOP. ONE MEGAPHONE MOUTH RUBBER LOOSE. FWD AND AFT MEGAPHONES BATTERIES REPLACED. IN ONE MEGAPHONE THE MOUTH RUBBER WAS SECURED PER MM 25-60-00.

ATA 3350

Part: LIGHT — INOPERATIVE (ROW 5,9,21,29)

EMERGENCY LIGHT PARTLY INOP ON SEATS 5K, 9B, 21B, AND 29K. REPLACED LIGHT ASSEMBLIES ON SEATS PER MM 33-50-00.

ATA 3397

Part: WIRE — SHORTED (CABIN)

FORWARD ZONE A EMERGENCY LIGHTS INOP. DOOR 1L EXIT SIGN DISASSEMBLED AND WIRING FROM TERMINAL 1 FOUND SHORTED TO TERMINAL 2. DOOR EXIT SIGN WIRING RE-MADE. EMERGENCY LIGHT BATTERY CHARGER FITTED TO ZONE A. ALL DISTRIBUTED WIRING RE-MADE AND SYSTEM CHECKED PER MM 33-51-01 AND 33-55-00.

ATA 5753

Part: SKIN — PUNCTURED (RT TE FLAP)

INSPECTION FOUND A HOLE IN RT INBOARD FLAP LOWER SURFACE, FOUR INCHES FORWARD OF REAR SPAR. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 57-52-01, 51-30-00, AND 51-21-01.

ATA 5330

Part: SKIN — CRACKED (FUSELAGE)

INSPECTION FOUND FUSELAGE SKIN CRACKED AT LT AIR CONDITIONING BAY NR 1 DOOR AFT UPPER CORNER. THE CRACK WAS STOP DRILLED IAW SRM 53-30-00. REPAIR DOUBLERS WERE FABRICATED AND INSTALLED 53-30-00, FIGURE 3, PAGE 19.

ATA 5230

Part: ANGLE — CRACKED (CARGO DOOR)

INSPECTION FOUND A 6 AND 4 INCH CRACK WITH CORROSION IN AFT CARGO DOOR FORWARD LOWER MOUNT ANGLE FOR GILL LINER. THE ANGLE WAS REMOVED AND REPLACEMENT PARTS WERE FABRICATED AND INSTALLED IAW SRM 53-15-01 AND 51-31-01.

ATA 5320

Part: WEB — PUNCTURED (BS 1841)

INSPECTION FOUND PUNCTURES IN WEB PANEL AT STA 1841, LBL 38.5 TO 64. REPAIRS WERE FABRICATED AND INSTALLED IAW SRM 51-21-01 AND 53-00-01.

ATA 5350

Part: FITTING — GOUGED (TAIL CONE)

INSPECTION FOUND TAIL CONE RT LATCH HOOK FITTING WITH SUNK RIVETS AND A GOUGE JUST FORWARD OF INNER ACCESS DOOR ASSEMBLY AREA. THE DAMAGED AREA WAS REMOVED IAW SRM 51-31-01. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-52-01 AND 51-31-01.

ATA 5400

Part: ANGLE — CRACKED (NR 3 PYLON)

INSPECTION FOUND A .25 INCH CRACK IN L-ANGLE ON TOP OF NR 3 PYLON AT AFT END OF HEAT EXCHANGER. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-30-01 AND 54-11-02.

ATA 5753

Part: ANGLE — CRACKED (LT TE FLAP)

INSPECTION FOUND A 7 INCH CRACK IN ANGLE DOUBLER ON LT TRAILING EDGE FLAP HINGE PANEL 535JL. THE ANGLE DOUBLER WAS REMOVED. TWO DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 57-52-01 AND 51-30-01.