N37077

Part: ELEVATOR — DAMAGED (RIGHT)

INSPECTION FOUND IMPACT DAMAGE TO RT ELEVATOR TIP CAUSED BY HANGAR DOOR. A NEW ELEVATOR WAS INSTALLED IAW MM 27-30-09, PAGE 401. ELEVATOR OPERATION CHECKED GOOD IAW MM 27-30-03, PAGE 601.

Part: SKIN — CRACKED (RT WING)

INSPECTION FOUND A 2 INCH CRACK IN RT WING LEADING EDGE DROOP PANEL UPPER SKIN. TWO RIBS WERE REMOVED AND REPLACED. THE SKIN WAS REINFORCED WITH DOUBLER AND INSTALLED IAW SRM 57-10-00, FIGURE 55, 51-21-01, AND 51-31-01.

Part: RIB — CRACKED (NR 1 LE SLAT)

INSPECTION FOUND A .25 INCH CRACK IN NR 1 SLAT RIB. THE RIB WAS REMOVED AND REPLACED IAW SRM 51-31-01.

Part: SUPPORT — CORRODED (BS 1871)

INSPECTION FOUND FLOOR SUPPORT CORRODED IN MAIN DECK AT STA 1871 NEAR LAV E. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 53-70-00, 51-21-01, AND 51-31-01.

Part: HYD PUMP — LEAKING (NR 3 ENGINE)

THE HYDRAULIC SYSTEM 3 ELEVATOR OFF LIGHT CAME ON JUST PRIOR TO LANDING AT LGW. THE ELEVATOR FEEL CHANNEL LIGHT CAME ON AFTER LANDING. THE AIRCRAFT HAD LOST FLUID FROM THE NR 3 HYDRAULIC SYSTEM. MAINTENANCE FOUND THE NR 3 ENGINE DRIVEN RIGHT HYDRAULIC PUMP HOUSING LEAKING. THE HYDRAULIC PUMP WAS REMOVED AND REPLACED. THE NR 3 HYDRAULIC SYSTEM WAS SERVICED. LEAK AND OPERATIONAL CHECKS WERE GOOD.

Part: RELAY — INOPERATIVE (BATTERY PANEL)

THE GROUND REFUEL POWER, FUEL TANK FILL VALVE, AND BATTERY BUS SENSING CIRCUIT BREAKERS POPPED WHILE EN ROUTE FROM FCO TO EWR. THE BATTERY BUS OFF LIGHT ILLUMINATED AND THE FUEL FILL VALVES CLOSED. FUEL COULD NOT BE TRANSFERRED. THE AIRCRAFT WAS DIVERTED TO LGW WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE EMERGENCY DC POWER R2-24 CHARGER/BATTERY RELAY (ON PANEL INSTL - BATTERY) AT FAULT. THE R2-24 RELAY WAS REMOVED AND REPLACED. OPERATIONAL CHECKS WERE GOOD.

Part: SKIN — CRACKED (BS 1255/1308.5)

INSPECTION FOUND RT DOOR ACCESS CUTOUT SKIN CRACKED AT STA 1308.5 AND STA 1255. BOTH CRACKS WERE 1 INCH LONG. DOUBLERS WERE INSTALLED IAW SRM 53-00-01, FIGURE 4 AND SRM 51-35-01.

Part: SUPPORT — CORRODED (BS 1986)

INSPECTION FOUND CABIN FLOOR SUPPORT CORRODED AT BS 1986 LBL 27. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-21-01, 51-31-01 AND 53-60-01 FIGURE 1.

Part: SUPPORT — CORRODED (BS 1099)

INSPECTION FOUND T-ANGLE FLOOR SUPPORT CORRODED IN FORWARD CARGO COMPARTMENT AT STA 1099, RBL 20. THE CORRODED AREA WAS CUT OUT, REPAIR ANGLES WERE FABRICATED AND INSTALLED IAW SRM 53-00-01, PAGE 8 AND 51-21-01.

Part: SLAT — GOUGED (NR 6 LE SLAT)

INSPECTION FOUND RT NR 6 SLAT CHAFED AND GOUGED AT INBOARD END, 12 INCHES UP FROM L/E TIP. THE SLAT WAS REPAIRED IAW ECRA 5750-02573.

Part: HINGE ANGLE — CRACKED (LT TE FLAP)

INSPECTION FOUND A 5.5 INCH CRACK IN UPPER RADIUS OF LOWER AFT FAIRING 535JL INBOARD HINGE AT OUTBOARD LT FLAP INBOARD FACE. THE FAIRING WAS REMOVED AND THE CORRODED AREA OF SKIN WAS CUT OUT, FILLER AND DOUBLER WERE FABRICATED AND INSTALLED IAW DRAWING SKB 020118N00677 AND ECRA 5720-01558. THE CORRODED HINGE ANGLE WAS CUT OUT, A SPLICE AND DOUBLER WERE FABRICATED AND INSTALLED IAW DRAWING SKB 020118N00677. THE FAIRING WAS REINSTALLED IAW SRM 51-31-1.

Part: SUPPORT — CORRODED (BS 472)

INSPECTION FOUND CABIN FLOOR SUPPORT CORRODED AT STA 472 LBL 54. A FLOOR SUPPORT REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-00-01, 51-21-01, 51-31-01, 51-35-01 AND 53-60-01 FIGURE 1.

Part: SKIN — CORRODED (BS 1509-1521)

INSPECTION FOUND FUSELAGE SKIN CORRODED STA 1509-1521, XCW 25 TO XCW -25. SKIN DOUBLERS WERE FABRICATED AND INSTALLED IAW ECRA 5330-02465 AND SRM 51-31-01.

Part: DOUBLER — CRACKED (NR 3 PYLON)

INSPECTION FOUND BOTH INBOARD AND OUTBOARD FORWARD UPPER ATTACH DOUBLERS OF NR 3 PYLON AFT FAIRING 489AL CRACKED THROUGH. THE CRACKED DOUBLERS WERE REMOVED IAW SRM 51-30-01. NEW DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM'S 51-21-01, 51-31-01, AND 53-00-01.

Part: SUPPORT — CORRODED (BS 1900)

INSPECTION FOUND THE UPPER HORIZONTAL SURFACE OF FORWARD END FLOOR SUPPORT CORRODED AT STA 1900, RBL 57. THE CORRODED SECTION WAS REMOVED, A NEW SECTION WAS SPLICED IN IAW SRM 53-70-00, FIGURE 13.

Part: SKIN — CRACKED (NR 3 PYLON)

INSPECTION FOUND A .50 INCH CRACK ON LT AND RT CORNERS OF NR 3 ENGINE PYLON FORWARD END. THE CRACKED AREAS WERE CUT OUT. TWO EACH DOUBLERS, FILLERS, AND TRIPLERS WERE FABRICATED AND INSTALLED IAW SRM 54-00-01, FIGURE 2A.

Part: SKIN — DENTED (NR 4 LE FLAP)

INSPECTION FOUND THE RT WING NR 4 SLAT DENTED AT XORS 480. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 57-10-00, FIGURE 12.

Part: SKIN — GOUGED (BS 1581/1585)

INSPECTION FOUND FUSELAGE SKIN GOUGED IN TWO PLACES AT STRINGER 48R, B.S. 1581 AND 1585. THE GOUGES WERE REMOVED IAW SRM 53-00-01, FIGURE 1. TWO DOUBLERS, FILLER, AND A FINGER DOUBLER WERE FABRICATED AND INSTALLED IAW SRM 53-20-00, FIGURE 6.

Part: SUPPORT — CORRODED (BS 1986-2007)

INSPECTION FOUND FLOOR SUPPORT CORRODED AROUND FLOOR PANEL ATTACH HOLES FROM BS 1986 TO 2007, RBL 27. A NEW FLOOR SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 53-60-01 FIGURE 1, 51-31-01 AND 51-20-01.

Part: SUPPORT — CORRODED (BS 1986)

INSPECTION FOUND FLOOR SUPPORT CORRODED AT BS 1986, LBL 27. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-21-01, 51-31-01 AND 53-60-01, FIGURE 1.

Part: SUPPORT — CORRODED (BS 1882)

INSPECTION FOUND FLOOR SUPPORT CORRODED AT BS 1882, LBL 36. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-21-01, 51-31-01 AND 53-60-01, FIGURE 1.

Part: SUPPORT — CORRODED (BS 1963)

INSPECTION FOUND FLOOR SUPPORT CORRODED AT BS 1963, LBL 27. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-21-01, 51-31-01 AND 53-60-01, FIGURE 1.

Part: SUPPORT — CORRODED (BS 457)

INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 457, RBL 29. A NEW SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 51-21-01, 51-35-01 AND 53-11-01, FIGURE 1A.

Part: SKIN — CRACKED (BS 1308.5)

INSPECTION FOUND A 1 INCH CRACK IN INNER SKIN AT RT DOOR CUT-OUT SURROUNDING FRAME STRUCTURE, STA 1308.5, AT CABIN FLOOR. THE SKIN WAS REPAIRED BY FABRICATING AND INSTALLING A DOUBLER IAW SRM'S 51-21-01 AND 53-00-01, FIGURE 4.

Part: SKIN — DENTED (LT LE SLAT)

INSPECTION FOUND LT WING NR 1 LEADING EDGE SLAT DENTED ON LEADING EDGE NOSE STARTING 30 INCHES OUTBOARD OF XFS 145. THE DENTED AREA WAS CUT OUT AND DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 57-10-00, FIGURE 43.

Part: SKIN — CRACKED (BS 1255)

INSPECTION FOUND A 1 INCH CRACK IN INNER SKIN AT RT DOOR CUT-OUT SURROUNDING FRAME STRUCTURE, STA 1255, AT CABIN FLOOR. THE CRACK WAS STOP DRILLED. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-00-01, FIGURE 4, SRM 51-21-01, AND 51-35-01.

Part: SKIN — CRACKED (WS 810)

THE LT WING FIXED LEADING EDGE SKIN HAD A 2.5 INCH CRACK FROM LOWER EDGE RUNNING FORWARD AT APPROXIMATELY XORS 810. THE CRACKED AREA WAS REMOVED. DOUBLER, FILLERS, AND FASTENERS WERE INSTALLED IAW SRM 57-00-01.

Part: CLIP — CORRODED (BS 1501)

INSPECTION FOUND CLIP FROM RT WHEEL WELL PRESSURE PANEL TO FRAME CORRODED ON UPPER FORWARD FACE OF FLANGE AT STA 1501, SIX INCHES BELOW CABIN FLOOR. A NEW CLIP WAS FABRICATED AND INSTALLED IAW SRM 51-21-01, 51-31-01, 53-00-01, FIGURE 1 AND 53-14-01, FIGURE 11.

Part: SUPPORT — CORRODED (BS 472)

INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 472, LBL 54. TWO ANGLES, FILLER AND A FLOOR SUPPORT WERE FABRICATED AND INSTALLED IAW SRM 51-31-01, 51-21-01, 51-35-01 AND 53-60-01 FIGURE 1.

Part: HINGED PANEL — CRACKED (LT HORIZ STAB)

INSPECTION FOUND A .50 INCH CRACK AROUND FASTENER OF LT HORIZONTAL STABILIZER LOWER TRAILING EDGE HINGED PANEL AT STA XE 158. THE AREA WAS REPAIRED IAW SRM 51-70-00.

Part: BLKHD STIFFENER — CORRODED (CTR MLG WW)

INSPECTION FOUND CORROSION AROUND LOWER BOLT HOLE OF T-SHAPED VERTICAL STIFFENER AT CENTER WHEELWELL AFT FACE OF FORWARD BULKHEAD, XCW -15.0. THE STIFFENER WAS REMOVED AND REPLACED IAW SRM'S 51-10-00, 51-21-01, AND 51-31-01.

Part: SKIN — CORRODED (BS 1009-1029)

INSPECTION FOUND FUSELAGE SKIN CORRODED AT BS 1009 TO 1029, STRINGER 52. THE CORRODED AREA WAS CUT OUT. REPAIR DOUBLERS, FINGER DOUBLERS AND FILLER WERE INSTALLED IAW SRM 53-20-00, FIGURE 7.

Part: SKIN — CORRODED (BS 1049-1069)

INSPECTION FOUND CORROSION ON FUSELAGE SKIN AT BS 1049 TO 1069, STRINGER 52. THE CORRODED AREA WAS REMOVED. REPAIR DOUBLERS, FINGER DOUBLER AND FILLER WERE INSTALLED IAW SRM 53-20-00, FIGURE 7.

Part: FRAME — CORRODED (CTR MLG DOOR)

THE RT CENTER MLG DOOR AFT FRAME WAS FOUND CORRODED. THE AFT FRAME WAS REMOVED AND REPLACED IAW SRM'S 51-35-01 AND 51-35-02.