N19357

Part: CHARGER — INOPERATIVE (CABIN) · airframe 47,650 hrs · 44,404 cycles

THE AFT CENTER EMERGENCY LIGHT BATTERY PACK AND CHARGER WERE FOUND INOPERATIVE. THE BATTERY AND CHARGER WERE REPLACED IAW MM 33-51-51-201.

Part: SKIN — CRACKED (BS 727D BS 22L) · airframe 47,130 hrs · 44,149 cycles

INSPECTION FOUND A 2.5 INCH CRACK IN FUSELAGE SKIN AT STA 727D + 9.9, S22L. THE SKIN WAS REPAIRED IAW ECRA 5330-03580 AND A DIP WAS ISSUED TO REINSPECT THE AREA EVERY 9000 FLIGHT CYCLES PER PART 2 OF THE ECRA.

Part: SKIN — CORRODED (BS 967 S27L-27R) · airframe 46,710 hrs · 43,938 cycles

INSPECTION FOUND INSIDE SURFACE OF FUSELAGE SKIN PANEL CORRODED AT STA 967 BETWEEN S27L AND S27R. THE PANEL WAS REPAIRED IAW ECRA 5331-01246.

Part: SKIN — CRACKED (AFT CARGO DOOR) · airframe 42,397 hrs · 41,904 cycles

INSPECTION FOUND A .5 INCH CRACK AT LIGHTENING HOLE (3RD FROM TOP AND 1 FROM AFT EDGE OF DOOR) IN AFT CARGO DOOR INNER SKIN. A DOUBLER WAS INSTALLED IAW ECRA 5230-01740.

Part: SKIN — CRACKED (C-1 DOOR) · airframe 42,397 hrs · 41,904 cycles

INSPECTION FOUND A .5 INCH CRACK AT LIGHTENING HOLE (2ND ROW FROM TOP) IN C-1 DOOR INNER SKIN. A DOUBLER WAS INSTALLED IAW ECRA 5232-01053.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 42,397 hrs · 41,904 cycles

INSPECTION FOUND RIGHT O/B SEAT TRACK CORRODED AT STA 328-360. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 53-00-52.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 42,397 hrs · 41,904 cycles

INSPECTION FOUND FLOORBEAM UPPER CHORD CORRODED AT STA 328, LBL 29 TO RBL 58. THE FLOORBEAM UPPER CHORD WAS REPLACED IAW SRM 53-10-51.

Part: ANGLE — CORRODED (R-2 DOOR) · airframe 42,397 hrs · 41,904 cycles

INSPECTION FOUND R-2 DOOR ZEE ANGLE CORRODED AT STA 907-1006, RBL 0 TO RBL 45. THE ZEE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-02.

Part: FITTING — CORRODED (LT MLG) · airframe 42,397 hrs · 41,904 cycles

INSPECTION FOUND LT MLG UPLOCK FORWARD SUPPORT FRAME FITTINGS (2 EACH) CORRODED WITH BUSHINGS WORN AT STA 685, S17L. THE LUG FITTING WAS REWORKED TO REMOVE THE CORROSION AND SLEEVE AND BUSHINGS WERE INSTALLED IAW SRM 53-60-14.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 42,397 hrs · 41,904 cycles

INSPECTION FOUND MULTIPLE CRACKS IN STRINGER 16L AND 16R AT STA 540. THE CRACKS WERE 0.025 INCH LONG. CHANNELS WERE INSTALLED IAW ECRA 5310-03418.

Part: SPLICE — CRACKED (STRINGER) · airframe 42,397 hrs · 41,904 cycles

INSPECTION FOUND A .5 INCH CRACK IN STRINGER 4L SPLICE AT STA 907. THE STRINGER SPLICE WAS REMOVED AND REPLACED IAW SRM 51-10-02.

Part: SPLICE — CRACKED (STRINGER) · airframe 42,397 hrs · 41,904 cycles

INSPECTION FOUND A 0.65 INCH CRACK IN STRINGER 4R SPLICE AT STA 907. THE STRINGER SPLICE WAS REMOVED AND REPLACED IAW SRM 51-10-02.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 42,397 hrs · 41,904 cycles

INSPECTION FOUND G-1 GALLEY HOLD DOWN SEAT TRACK CORRODED AT STA 277-294.5 FROM BL 0 TO RBL 43. THE CORRODED SECTION OF TRACK WAS REMOVED AND A NEW SECTION OF TRACK WAS INSTALLED IAW SRM 53-00-52, FIGURE 202, REPAIR 1.

Part: CONNECTOR — SHORTED (APU FIRE LOOP) · airframe 42,397 hrs · 41,903 cycles

THE APU DET INOP LIGHT CAME ON WHILE CLIMBING THROUGH FL 180. THE APU FIRE WARNING LIGHT WITH FIRE BELL ACTIVATED WHILE CLIMBING THROUGH FL 330. THE APU FIRE BOTTLE WAS DISCHARGED AND THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND NO EVIDENCE OF FIRE. MAINTENANCE FOUND FIRELOOP CONNECTOR D984 SHORTED. THE CONNECTOR WAS REPLACED. THE APU AND PACKS WERE RUN AND OPERATIONAL CHECKS OF THE APU FIRE DETECTION SYSTEM WERE GOOD. THE APU FIRE BOTTLE WAS REPLACED IAW MM 26-22-11.

Part: SKIN — CRACKED (FUSELAGE) · airframe 41,734 hrs · 41,550 cycles

MAINTENANCE FOUND THE FUSELAGE SKIN DENTED AND CRACKED BETWEEN STA 500D + 10 AND 520, S12L. THE CRACK WAS 1.4 INCHES LONG. AN INTERIM REPAIR WAS INSTALLED IAW ECRA 5330-03361. A DIP WAS ISSUED TO PERFORM A PERMANENT REPAIR WITHIN 12 MONTHS.

Part: SKIN — CRACKED (NR 1 PYLON) · airframe 39,772 hrs · 40,520 cycles

INSPECTION FOUND A .5 INCH CRACK IN NR 1 ENGINE PYLON ACCESS PANEL NR 5727L CUTOUT. A REPAIR DOUBLER WAS INSTALLED IAW ECRA 5430-01230.

Part: CARGO TRACK — DAMAGED (FUSELAGE) · airframe 39,772 hrs · 40,520 cycles

INSPECTION FOUND IMPACT DAMAGE TO AFT BAGGAGE BIN LT TIE DOWN RAIL AT BS 787. REPLACED TIE DOWN RAIL IAW SRM 53-00-53.

Part: ATTACH FITTING — CORRODED (HORIZONTAL STAB) · airframe 39,772 hrs · 40,520 cycles

INSPECTION FOUND THE RT HORIZONTAL STABILIZER CENTER SECTION FORWARD UPPER LUG CORRODED AT AFT SIDE AROUND BUSHING. AN OVERSIZED BUSHING WAS INSTALLED IAW CMM 55-10-06 AND SRM 55-10-10.

Part: FITTING — GOUGED (RT SPOILER) · airframe 34,125 hrs · 37,517 cycles

INSPECTION FOUND RT WING AFT SPAR SPOILER FITTING GOUGED AT WS 133. THE SPOILER FITTING WAS REPLACED IAW ECRA 5750-03517 AND AMS EA 04-5750-0842.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 34,125 hrs · 37,517 cycles

INSPECTION FOUND A 1 INCH CRACK IN VERTICAL STIFFENER 18 INCHES ABOVE RT KEEL BEAM AT MAIN WHEEL WELL FORWARD BULKHEAD, STA 663, RBL 6. THE STIFFENER WAS REMOVED AND A NEW STIFFENER WAS INSTALLED IAW SRM 57-10-60 AND 51-10-01.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 34,116 hrs · 37,512 cycles

INSPECTION FOUND FLOORBEAM CORRODED ON UPPER SURFACE AROUND SCREW HOLES AT STA 967, RBL 27, LBL 6, AND LBL 27. REPAIR STRAPS AND SHIMS WERE INSTALLED IAW SRM 53-00-51, FIGURE 203, 51-20-01, AND 51-30-01.

Part: DOOR FRAME — CRACKED (CARGO DOOR) · airframe 34,116 hrs · 37,512 cycles

INSPECTION FOUND A 2.5 INCH CRACK IN AFT CARGO DOOR FORWARD FRAME SPLICE, THROUGH HOLE FOR TENSION PULLEY FOR COUNTER BALANCE MECHANISM, APPROXIMATELY 3.5 INCH FROM CENTERLINE OF DOOR. THE AFT CARGO DOOR WAS REMOVED AND THE FORWARD UPPER AND LOWER FRAME SECTIONS WERE REPLACED IAW SRM 51-40-2 AND 52-30-02. THE DOOR WAS REINSTALLED IAW CARD 03-5230-1-4003.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · airframe 34,117 hrs · 37,513 cycles

INSPECTION FOUND FORWARD CARGO COMPARTMENT AFT PRESSURE BULKHEAD RT PANEL LOWER ATTACH ANGLE CORRODED AT STA 500D, S26R. THE ATTACH ANGLE WAS REMOVED AND TWO REPAIR ANGLES WERE INSTALLED IAW SRM 51-70-12 AND 51-40-02.

Part: INTERCOSTAL — BENT (FUSELAGE) · airframe 34,117 hrs · 37,513 cycles

INSPECTION FOUND INTERCOSTAL IN FORWARD CARGO COMPARTMENT BENT ON UPPER SURFACE AT STA 440-460, S28R. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 34,117 hrs · 37,513 cycles

INSPECTION FOUND FLOOR SUPPORTS CORRODED AT STA 967-986.5, LBL 18 AND RBL 18. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-40-02.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 34,117 hrs · 37,513 cycles

INSPECTION FOUND A 1 INCH CRACK IN FLOOR SUPPORT INTERCOSTAL ANGLE AT STA 927-947, BL 0. REMOVED CRACKED ANGLE ON INTERCOSTAL AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-2.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 34,117 hrs · 37,513 cycles

INSPECTION FOUND RIGHT O/B MAIN CABIN SEAT TRACK CORRODED AT STA 540-727. THE CORRODED SECTION OF SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 53-00-52.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 34,117 hrs · 37,513 cycles

INSPECTION FOUND A .5 INCH CRACK IN FORWARD ENTRYWAY L-ANGLE AT FLOORBEAM AFT FLANGE ATTACH POINT, STA 344, LBL 10. THE L-ANGLE ON TOP OF INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-40-0.

Part: WEB — CORRODED (CARGO BAY) · airframe 34,117 hrs · 37,513 cycles

INSPECTION FOUND FORWARD CARGO COMPARTMENT DOOR OPENING LOWER SUPPORT PANEL (SILL WEB) CORRODED AT STA 440-490, S25R. THE SILL WEB WAS REMOVED AND A NEW SILL WEB WAS INSTALLED IAW SRM 51-40-5, 51-40-6, AND 51-40-8.

Part: WEB — CORRODED (FUSELAGE) · airframe 34,117 hrs · 37,513 cycles

INSPECTION FOUND FORWARD END OF FLOOR PAN CORRODED AT STA 986.5-1016, RBL 36-48. THE CORRODED FLOOR PAN WEB WAS REMOVED AND A NEW FLOOR PAN WEB WAS INSTALLED IAW SRM 51-10-2, 51-40-01, AND DRAWING 65C32677.

Part: BEARING — FROZEN (RT MLG) · airframe 34,117 hrs · 37,513 cycles

INSPECTION FOUND RT MLG SUPPORT BEAM HAD LOOSE BEARING HOUSING AND FROZEN BEARING AT MOUNT FITTING. REMOVED NR 5 FLAP TRACK WITH TRANSMISSION, REMOVED FITTING AND INSTALLED NEW BEARING. REINSTALLED NR 5 FLAP TRACK WITH TRANSMISSION. MAINTENANCE WAS PERFORMED IAW MM 27-51-71, PAGE 410-411 AND ECRA 5750-03524.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 34,117 hrs · 37,513 cycles

INSPECTION FOUND CHANNEL CORRODED AT L-1 DOOR THRESHOLD CUSP WEB, L18L. THE CHANNEL WAS REMOVED AND REPLACED IAW SRM 51-40-02.

Part: PAN — CORRODED (FUSELAGE) · airframe 34,117 hrs · 37,513 cycles

INSPECTION FOUND FLOOR PAN AT STA 1016 TO AFT PRESSURE BULKHEAD CORRODED AT BL 0 TO LBL 48. THE FLOOR PAN WAS REMOVED AND A NEW FLOOR PAN WAS INSTALLED IAW SRM 51-10-02, DRAWING 65-52878 AND DRAWING 65C32677.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 34,117 hrs · 37,513 cycles

INSPECTION FOUND A 3 INCH CRACK IN FORWARD CARGO COMPARTMENT FLOOR SUPPORT AT STA 500 ABOVE S27R. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-40-02 AND 51-40-03.

Part: RIB — WORN (HORIZ STAB) · airframe 34,117 hrs · 37,513 cycles

INSPECTION FOUND RT ELEVATOR CENTER BALANCE HAD WEAR MARKS ON I/B WALL (HOR STAB RIB) AT STA 66.54. THE WORN AREA WAS REMOVED IAW SRM 57-70-10, PARA 4B. FILLER AND DOUBLER WERE INSTALLED IAW SRM 51-70-10, PARA 5 & 9. REINSTALLED SEALS REMOVED FOR REPAIR IAW MM 27-31-41.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 34,116 hrs · 37,512 cycles

INSPECTION FOUND UPPER SURFACE OF FLOORBEAM CORRODED AT STA 986.5. THE CORRODED SECTION OF FLOORBEAM T-CAP WAS REMOVED AND A NEW SECTION WAS INSTALLED USING REPAIR STRAP AND ANGLES IAW SRM 51-40-00 AND ECRA 5310-03851.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 34,116 hrs · 37,512 cycles

INSPECTION FOUND A 1 INCH CRACK IN FORWARD ENTRYWAY INTERCOSTAL AT FLOORBEAM ATTACH AREA, STA 312, BL 0. THE INTERCOSTAL WAS REMOVED AND A NEW INTERCOSTAL WAS INSTALLED IAW SRM 51-40-02.

Part: SKIN — DENTED (SPOILER) · airframe 34,116 hrs · 37,512 cycles

INSPECTION FOUND LT WING NR 3 FLIGHT SPOILER DENTED ON TOP SURFACE. THE DENTED AREA WAS REMOVED AND A DOUBLER WAS INSTALLED IAW SRM 57-70-01, FIGURE 204 AND 51-20-01.

Part: SEAT TRACK — GOUGED (CABIN) · airframe 34,116 hrs · 37,512 cycles

INSPECTION FOUND LEFT O/B SEAT TRACK GOUGED AND WORN AT STA 480-520, LBL 46. THE DAMAGED SECTION OF SEAT TRACK WAS REMOVED AND A NEW SECTION OF TRACK WAS INSTALLED IAW SRM 53-00-52, 51-21-01, AND ECRA 5100-01844.

Part: FRAME — WORN (NR 2 PYLON) · airframe 34,116 hrs · 37,512 cycles

INSPECTION FOUND RT ENGINE PYLON FORWARD O/B UPPER CHORD WORN. THE CHORD WAS REPAIRED IAW ECRA 5440-01221 AND EA 04-5440-0836.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 34,116 hrs · 37,512 cycles

INSPECTION FOUND SEAT TRACK CORRODED AT STA 179-294, RBL 45. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK WAS INSTALLED IAW SRM 51-40-02.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 34,116 hrs · 37,512 cycles

INSPECTION FOUND THREE CREASES IN LT FUSELAGE EXTERIOR SKIN ALONG LAP SEAM AT STA 275, S19L. THE SKIN WAS REPAIRED IAW SRM 53-00-01.

Part: DOUBLER — GOUGED (FUSELAGE) · airframe 34,116 hrs · 37,512 cycles

INSPECTION FOUND FWD ENTRYWAY FLOORBEAM AFT FLANGE OUTER DOUBLE STACK REPAIR DOUBLER GOUGED IN RADIUS AND ON HORIZONTAL FLANGE AT STA 312, RBL 24. THE DOUBLER WAS REMOVED AND A REPAIR ANGLE WAS INSTALLED IAW SRM 53-10-51.

Part: INTERCOSTAL — BENT (FUSELAGE) · airframe 34,116 hrs · 37,512 cycles

INSPECTION FOUND AFT PIT DOOR CUTOUT LOWER INTERCOSTAL BENT AT FORWARD FRAME TO AFT FRAME, STA 794-849, LBL 24. THE INTERCOSTAL WAS REMOVED AND A NEW INTERCOSTAL WAS INSTALLED IAW SRM 51-40-2.

Part: SEAT TRACK — GOUGED (CABIN) · airframe 34,116 hrs · 37,512 cycles

INSPECTION FOUND LEFT O/B SEAT TRACK GOUGED AT STA 540-727, LBL 46. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK WAS INSTALLED IAW SRM 51-20-01 AND 51-40-00.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 34,116 hrs · 37,512 cycles

INSPECTION FOUND R-1 DOOR I/B CHORD O/B L-ANGLE CORRODED ON TOP AND BOTTOM SURFACES AT STA 312, S18R. THE L-ANGLE WAS REMOVED AND REPLACED IAW SRM 51-40-02 AND 51-10-02.

Part: SKIN — DENTED (SPOILER) · airframe 34,116 hrs · 37,512 cycles

INSPECTION FOUND LT WING NR 2 FLIGHT SPOILER DENTED ON LOWER SURFACE. THE DENTED AREA WAS REMOVED AND A DOUBLER WAS INSTALLED IAW SRM 57-70-01 AND MM 27-61-11.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 34,116 hrs · 37,512 cycles

INSPECTION FOUND A 1 INCH CRACK IN INTERCOSTAL UPPER FLANGE AT BS 380 - 400, LBL 23. THE INTERCOSTAL WAS REMOVED AND A NEW INTERCOSTAL WAS INSTALLED IAW SRM 53-30, 51-21-01, AND 51-40-02.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 34,116 hrs · 37,512 cycles

INSPECTION FOUND A .5 INCH CRACK IN STRINGER 28R AT STA 440. THE CRACKED SECTION OF STRINGER WAS CUT OUT AND A J-ANGLE REPAIR WAS INSTALLED IAW SRM 53-00-03.

Part: BEAM — GOUGED (PAX DOOR) · airframe 34,116 hrs · 37,512 cycles

INSPECTION FOUND L-1 DOOR INNER DOOR CHORD BEAM GOUGED IN UPPER TORQUE TUBE SLEEVE BAY AT STA 312. THE CHORD BEAM WAS REMOVED AND A NEW CHORD BEAM WAS INSTALLED IAW SRM 52-10-02 AND 51-30-02.

Part: WEB — DENTED (FUSELAGE) · airframe 34,116 hrs · 37,512 cycles

INSPECTION FOUND AFT CARGO DOOR AFT LOWER FRAME WEB DENTED AT STA 847. THE DENTED AREA WAS REMOVED AND A NEW REPAIR WEB WAS INSTALLED IAW SRM 51-70-13 AND 51-40-02.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 34,116 hrs · 37,512 cycles

INSPECTION FOUND FLOORBEAM CORRODED ON UPPER SURFACE AROUND SCREW HOLES AT STA 967, RBL 27, LBL 6, AND LBL 27. REPAIR STRAPS AND SHIMS WERE INSTALLED IAW SRM 53-00-51, FIGURE 203, 51-20-01, AND 51-30-01.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 34,116 hrs · 37,512 cycles

INSPECTION FOUND ANGLED FLOOR SUPPORT CORRODED AT AFT END AT STA 986.5-1006, RT SIDE. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-40-02.

Part: SKIN — DENTED (FUSELAGE) · airframe 34,116 hrs · 37,512 cycles

INSPECTION FOUND EXTERIOR FUSELAGE SKIN DENTED BELOW LAP SEAM AT STA 1010, S20R. THE DENTED AREA WAS CUT OUT AND A REPAIR PLATE WAS INSTALLED IAW SRM 53-00-01, FIGURE 202 AND 207.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 34,116 hrs · 37,512 cycles

INSPECTION FOUND GOUGES ON TOP OF SEAT TRACK AT STA 344-400, LBL 25. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 53-00-52.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 34,116 hrs · 37,512 cycles

INSPECTION FOUND FLOOR SUPPORT CORRODED AROUND SCREW HOLES AT STA 951, RBL 24 - 48. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-40-02.

Part: THRESHOLD — CORRODED (R2 DOOR) · airframe 34,116 hrs · 37,512 cycles

INSPECTION FOUND R-2 DOOR THRESHOLD CHORD CORRODED AT STA 977. THE R-2 DOOR THRESHOLD CHORD WAS REMOVED AND REPLACED IAW SRM 51-10-02.

Part: PAN — CORRODED (FUSELAGE) · airframe 34,116 hrs · 37,512 cycles

INSPECTION FOUND FLOOR PAN CORRODED AT STA 1016 TO AFT PRESSURE BULKHEAD, BL 0 TO RBL 48. THE FLOOR PAN WAS REMOVED AND A NEW FLOOR PAN WAS INSTALLED IAW SRM 51-10-02, DRAWING 65C32677, AND DRAWING 65-52878.

Part: FRAME — GOUGED (NR 1 PYLON) · airframe 34,116 hrs · 37,512 cycles

INSPECTION FOUND NR 1 ENGINE PYLON FORWARD O/B UPPER CHORD GOUGED. THE NR 1 ENGINE PYLON O/B UPPER CHORD WAS REPAIRED IAW ECRA 5440-01221 AND EA 04-5440-0836.

Part: STIFFENER — GOUGED (WING) · airframe 34,116 hrs · 37,512 cycles

INSPECTION FOUND VERTICAL T-SUPPORT (STIFFENER) ON AFT SPAR JUST I/B OF MLG SUPPORT BEAM O/B FITTING GOUGED AT WS 133. A NEW STIFFENER WAS INSTALLED IAW SRM 51-40-5 AND 51-40-6.

Part: SKIN — CREASED (BS 456)

INSPECTION FOUND THE RT FORWARD LOWER FUSELAGE SKIN CREASED AT STA 456, STRINGERS 29R-27R. THE SKIN WAS REPAIRED IAW ECRA 5330-02767.

Part: SKIN — DENTED (BS 480-500)

INSPECTION FOUND FUSELAGE SKIN DENTED AT STA 480-500B, STRINGER 19L. A REPAIR WAS INSTALLED IAW SRM 53-00-01.

Part: INTERCOSTAL — CORRODED (BS 950)

INSPECTION FOUND FLOORBEAM INTERCOSTAL CORRODED AT NUTPLATE HOLE BS 950 LBL 30. THE INTERCOSTAL WAS REPLACED IAW ECRA 5310-03413.

Part: FITTING — CRACKED (HORZ STAB)

INSPECTION FOUND A 3 INCH CRACK ON FITTING ATTACHED TO THE HORIZONTAL STABILIZER CENTER SECTION BOX. THE FITTING WAS REPLACED IAW SRM 51-40-02.

Part: WEB — CORRODED (BS 1121-1129)

INSPECTION FOUND CORROSION ON WEB BETWEEN STA 1121 AND 1129 LOOKING THROUGH APU INLET DUCT OPENING, RT SIDE TOP. THE WEB WAS REPAIRED IAW SRM 51-70-11.

Part: BEAM — CORRODED (BS 1104)

INSPECTION FOUND CORROSION ON RIGHT SIDEWALL BEAM OF APU BOX AT STA 1104. THE CORRODED SECTION WAS REMOVED, A NEW PART WAS FABRICATED AND INSTALLED IAW SRM 51-70-11.

Part: STRINGER — CRACKED (BS 500)

INSPECTION FOUND A .375 INCH CRACK IN STRINGER 16L AND A .375 INCH CRACK IN STRINGER 16R AT STA 500C. A REPAIR CHANNEL AND DOUBLER WERE INSTALLED AT EACH LOCATION IAW ECRA 5310-03418.

Part: FLOORBEAM — CORRODED (BS 312)

INSPECTION FOUND FLOORBEAM CORRODED AT NUT CLIP HOLES, STA 312. REPAIRED IAW SRM 53-10-51, FIGURE 205.

Part: FLOORBEAM — CORRODED (BS 344)

INSPECTION FOUND FLOORBEAM CORRODED AROUND NUT CLIP HOLES FROM BL 0 TO L-1 DOOR AT STA 344. THE CORRODED SECTION WAS REMOVED AND A NEW FLOORBEAM SECTION WAS FABRICATED AND INSTALLED IAW SRM 53-10-51.

Part: FLOORBEAM — CORRODED (BS 312-328)

INSPECTION FOUND FLOOR SUPPORT CORRODED AROUND NUTPLATE HOLES BETWEEN STA 312 AND 328 TO THE LEFT OF BL 0 AND TO THE RIGHT OF BL 0. THE FLOORBEAM SECTIONS WERE REMOVED, NEW FLOORBEAM SECTIONS WERE FABRICATED AND INSTALLED IAW ECRA 5310-03413 AND BOEING DRAWING 65-46812 AND 65-45834.

Part: FLOORBEAM — CORRODED (BS 294.5)

INSPECTION FOUND FLOORBEAM CORRODED AROUND NUTCLIP HOLES NEXT TO G-1 GALLEY TRACK AT STA 294.5. A FLOORBEAM UPPER CHORD WAS INSTALLED IAW SRM 53-10-51.

Part: SUPPORT — CRACKED (BS 380-400)

INSPECTION FOUND .25 INCH CRACKS IN FLOOR SUPPORT AT BL 0 BETWEEN STA 380 AND 400. A NEW FLOOR SUPPORT ANGLE WAS FABRICATED AND INSTALLED IAW SRM 53-30-51.

Part: FLOORBEAM — CORRODED (BS 328)

INSPECTION FOUND FLOORBEAM CORRODED ON RIGHT SIDE AT STA 328. THE FLOORBEAM WAS REPAIRED IAW SRM 53-10-51.

Part: INTERCOSTAL — CORRODED (BS 967-986)

INSPECTION FOUND FLOORBEAM INTERCOSTAL CORRODED ON NUTPLATE AT BS 967 TO 986, LBL 12. A REPAIR WAS FABRICATED AND INSTALLED IAW ECRA 5310-03413.

Part: INTERCOSTAL — CORRODED (BS 950)

INSPECTION FOUND FLOORBEAM INTERCOSTAL CORRODED AROUND NUTPLATE AT BS 950, LBL 45. A REPLACEMENT INTERCOSTAL WAS FABRICATED AND INSTALLED IAW ECRA 5310-03413.

Part: FAN — INOPERATIVE (LT PACK)

THE FLIGHT ATTENDANT REPORTED ODOR AND SMOKE IN CABIN DURING CRUISE. THE LT PACK WAS SECURED, THEN THE FORWARD LAV SMOKE DETECTOR ACTIVATED. THE RECIRCULATION FAN WAS TURNED OFF AND THE LEFT PACK WAS RESTORED TO OPERATION. THE FLIGHT CONTINUED WITHOUT FURTHER PROBLEM. MAINTENANCE FOUND THE RECIRCULATION FAN AT FAULT. THE FAN WAS REMOVED AND REPLACED AND OPERATION CHECKED GOOD.

Part: HYD PUMP — LEAKING (NR 1 ENGINE)

EWR - FLT 1556 - THE AIRCRAFT LOST A-SYSTEM HYDRAULIC FLUID ON APPROACH TO EWR. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 1 ENGINE DRIVEN HYDRAULIC PUMP AT FAULT. THE PUMP WAS REMOVED AND REPLACED. THE ENGINE WAS RUN AND LEAK CHECK WAS GOOD. (X)