N16310

Part: FRAME — CORRODED (BS 227) · airframe 61,199 hrs · 32,806 cycles

INSPECTION FOUND BULKHEAD FORWARD SIDE LOWER FRAME CORRODED AT STA 227, LBL 5. A REPAIR WAS INSTALLED IAW ECRA 5311-01294.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 61,199 hrs · 32,806 cycles

INSPECTION FOUND A 1 INCH CRACK THROUGH SECOND FASTENER HOLE IN NOSE WHEEL WELL TOP CENTER ACTUATOR BEAM STIFFENER, STA 229.8. A NEW STIFFENER WAS INSTALLED IAW SRM 51-40-02.

Part: WEB — CRACKED (FUSELAGE) · airframe 61,199 hrs · 32,806 cycles

INSPECTION FOUND A 6 INCH CRACK APPROXIMATELY 6 INCHES AFT OF FORWARD BULKHEAD IN NOSE WHEEL WELL TOP CENTER ACTUATOR SUPPORT BEAM WEB AT STA 233.8. THE WEB WAS REMOVED AND A NEW WEB WAS INSTALLED IAW SRM 51-40-02.

Part: SKIN — CORRODED (FUSELAGE) · airframe 61,199 hrs · 32,806 cycles

INSPECTION FOUND SKIN UNDER NR 1 DME ANTENNA CORRODED AT STA 460-480, S26L TO S26R. THE SKIN WAS REPAIRED IAW ECRA 5331-01289.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,199 hrs · 32,806 cycles

INSPECTION FOUND A 0.61 INCH CRACK IN FUSELAGE SKIN AT L-2 DOOR FORWARD LOWER CORNER ON DOOR TORQUE TUBE ACCESS, STA 947.5-967, S14L. REPAIRED IAW ECRA 5331-01288.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 61,199 hrs · 32,806 cycles

INSPECTION FOUND A 1 INCH CRACK IN C-1 DOOR HANDLE CUTOUT IN FORWARD UPPER CORNER OF SKIN. FILLER AND DOUBLER WERE INSTALLED IAW SRM 52-00-01.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 61,199 hrs · 32,806 cycles

INSPECTION FOUND LEFT KEEL BEAM CORRODED AT STA 500D-520, S28L. THE CORRODED SEGMENT OF KEEL BEAM WAS REMOVED AND REPLACED IAW SRM 53-60-12.

Part: SKIN — CRACKED (BS 947-967) · airframe 61,199 hrs · 32,806 cycles

INSPECTION FOUND A 1 INCH CRACK IN FUSELAGE SKIN AT R-2 FORWARD LOWER CORNER ON DOOR LOWER TORQUE TUBE ACCESS, STA 947.5-967, S14R TO S15R. REPAIRED IAW SRM 53-60-01, FIGURE 201, PAGE 201.

Part: SKIN — CRACKED (STA) · airframe 55,273 hrs · 29,930 cycles

INSPECTION FOUND A 2.8 INCH CRACK IN EXTERIOR FUSELAGE SKIN JUST AFT OF FRAME STA 727E ABOVE S23R. A REPAIR WAS INSTALLED IAW ECRA 5330-03375 AND A DIP WAS ISSUED TO COMPLETE A REPAIR ASSESSMENT WITHIN 12 MONTHS AND PROVIDE REPAIR/INSPECTION THRESHOLDS. THE REPAIR IS ACCEPTABLE FOR 12 MONTHS.

Part: KEELBEAM — WORN (FUSLEAGE) · airframe 55,272 hrs · 29,930 cycles

LEFT KEEL BEAM UPPER SURFACE OF OUTBOARD FLANGE WORN INTO BY NUT PLATES AT STATION 716, 720, AND 723. REPAIRED IN ACCORDANCE WITH EC/RA 5311-01206 AND EC/RA 5311-01207.

Part: STIFFENER — CORRODED (BULKHEAD) · airframe 55,273 hrs · 29,930 cycles

LOWER LT SIDE OF APB STIFFENER CORRODED. INSTALLED NEW STIFFENER PER BOEING DRAWING 65C28106.

Part: SKIN — CORRODED (FUSELAGE) · airframe 55,273 hrs · 29,930 cycles

APB SKIN CORROSION AT BL 0, 6 INCHES ABOVE Y-ATTACH CHORD. REPAIRED PER BOEING DRAWING 65C28106.

Part: FRAME — CORRODED (BULKHEAD) · airframe 55,273 hrs · 29,930 cycles

CORROSION ON BS 1016 PRESSURE CHORD. INSTALLED NEW CHORD PER SRM 53-80-08.

Part: SKIN — CRACKED (AFT CARGO DOOR) · airframe 55,272 hrs · 29,930 cycles

AFT CARGO DOOR HAS PREVIOUS REPAIR REQUIRING REPLACEMENT. REMOVED DAMAGE, FABRICATED DOUBLER, TREATED PRIMED AND INSTALLED NEW DOUBLER PER EC/RA 5232-01049.

Part: STIFFENER — CORRODED (BULKHEAD) · airframe 55,273 hrs · 29,930 cycles

STIFFENER ON LWR RT SIDE OF APB IS CORRODED AT RBL 1. INSTALLED NEW STIFFENER PER BOEING DRAWING 65C28106.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 55,273 hrs · 29,930 cycles

STRINGER 26 RT IS CORRODED AT STA 1006-1016. INSTALLED NEW STRINGER PER SRM 51-10-02.

Part: SKIN — CRACKED (L1 DOOR) · airframe 55,272 hrs · 29,930 cycles

L1 DOOR CRACK FOUND ON INNER SKIN AFT EDGE ON NR 6 STOP PIN CUTOUT FROM THE TOP. REPAIRED CRACK PER EC/RA 5210-01798.

Part: SKIN — CRACKED (NR 1 SLAT) · airframe 55,273 hrs · 29,930 cycles

NR 1 SLAT LOWER SKIN CRACKED AT TWO RIVETS FWD OF I/B AUX TRACK. REPAIRED SLAT SKIN PER SRM 57-43-01.

Part: BRACKET — CRACKED (FLAP TRACK FAIR) · airframe 55,273 hrs · 29,930 cycles

INSPECTION FOUND RIGHT WING NR 6 FLAP TRACK FAIRING HORSE COLLAR BRACKET BENT AND CRACKED. THE CRACK WAS 1 INCH LONG. THE HORSE COLLAR BRACKET WAS REMOVED AND REPLACED IAW SRM 51-10-02.

Part: SKIN — CRACKED (NR 3 SLAT) · airframe 55,273 hrs · 29,930 cycles

INSPECTION FOUND A 1 INCH CRACK IN THE NR 3 SLAT LOWER SKIN AT O/B MAIN TRACK. A REPAIR WAS INSTALLED IAW SRM 57-43-01.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 55,273 hrs · 29,930 cycles

INSPECTION FOUND FLOORBEAM UPPER T-CAP CORRODED AT STA 328, RBL 12 TO RBL 58. A NEW SECTION OF FLOORBEAM WAS INSTALLED IAW SRM 53-10-51.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 55,273 hrs · 29,930 cycles

INSPECTION FOUND SEAT TRACK CORRODED AT STA 892, RBL 24.5. THE CORRODED SECTION OF SEAT TRACK WAS REMOVED AND A NEW SECTION WAS INSTALLED IAW SRM 53-00-52, FIGURE 204.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 55,273 hrs · 29,930 cycles

INSPECTION FOUND R-1 DOOR THRESHOLD Z-ANGLE CORRODED AT STA 277-360, S17R. THE Z-ANGLE WAS REPLACED IAW SRM 51-10-2, FIGURE 101.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,273 hrs · 29,930 cycles

LT MAIN FRAME CRACKED. REPAIRED PER ECRA 5311-01158.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,273 hrs · 29,930 cycles

INSPECTION FOUND A 1 INCH CRACK IN THE LT AND RT FRAME AT STA 616. THE FRAME WAS REPAIRED IAW ECRA 5311-01158.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,273 hrs · 29,930 cycles

RT MAIN FRAME CRACKED. INSTALLED DOUBLER PER ECRA 5311-01158.

Part: FLOOR SUPPORT — CORRODED (FUSLEAGE) · airframe 54,421 hrs · 29,492 cycles

INSPECTION FOUND FORWARD GALLEY FLOOR SUPPORT CORRODED BETWEEN STA 312 AND 344 BELOW L-1 DOOR. REPAIRED IAW ECRA 5321-01186.

Part: SUPPORT ANGLE — CRACKED (NACELLE) · airframe 54,421 hrs · 29,492 cycles

INSPECTION FOUND A 3 INCH CRACK IN SUPPORT ANGLE AT RT NACELLE STA 363.65 ON I/B SIDE RADIUS. A NEW SUPPORT ANGLE WAS INSTALLED IAW SRM 54-50-71 AND 51-40-02.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 54,421 hrs · 29,492 cycles

INSPECTION FOUND FORWARD GALLEY FLOORBEAM CORRODED AT STA 328. THE CORRODED SECTION OF FLOORBEAM WAS CUT OUT AND A REPAIR WAS INSTALLED IAW SRM 51-70-12.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 54,421 hrs · 29,492 cycles

INSPECTION FOUND FORWARD GALLEY FLOORBEAM CORRODED AT STA 344. THE FLOORBEAM WAS REPAIRED IAW SRM 51-70-12.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 54,421 hrs · 29,492 cycles

INSPECTION FOUND AFT GALLEY FLOOR TRACK CORRODED AT STA 947.5. A NEW SEAT TRACK WAS INSTALLED IAW SRM 53-00-52 AND ECRA 5321-01189.

Part: BRACKET — CORRODED (FUSELAGE) · airframe 54,421 hrs · 29,492 cycles

INSPECTION FOUND RT DIAGONAL SUPPORT BRACKET CORRODED AT STA 992-1018. THE SUPPORT BRACKET WAS REPLACED IAW MM 51-21-31 AND SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 54,421 hrs · 29,492 cycles

INSPECTION FOUND LT DIAGONAL FLOOR SUPPORT BEAM CORRODED AT FS 1006-1010. THE FLOOR SUPPORT BEAM WAS REPLACED IAW SRM 51-40-02.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,421 hrs · 29,492 cycles

INSPECTION FOUND A 1.9 INCH CRACK IN FUSELAGE SKIN AT BS 767, S21R. THE SKIN WAS REPAIRED IAW ECRA 5330-03090 AND 53-00-01.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 54,421 hrs · 29,492 cycles

INSPECTION FOUND FORWARD GALLEY FLOORBEAM CORRODED AT STA 344. REPAIRED IAW SRM 51-70-12.

Part: SILL — CORRODED (FUSELAGE) · airframe 54,421 hrs · 29,492 cycles

INSPECTION FOUND THE L-1 DOOR LOWER SILL CHORD CORRODED AT BS 318, LBL 57. THE AREA WAS REPAIRED IAW ECRA 5321-01186.

Part: OVEN — MALFUNCTIONED (FWD GALLEY) · airframe 53,109 hrs · 28,829 cycles

SMOKE IN FLIGHT DECK. REMOVED AND REPLACED OVEN.

Part: SKIN — DEBONDED (RUDDER) · airframe 51,651 hrs · 28,047 cycles

INSPECTION FOUND LT RUDDER T/E SKIN DISBONDING IN THIRD LAYER OF EXISTING REPAIR 28 INCHES FROM LOWER END. A REPAIR WAS INSTALLED IAW ECRA 5540-01163.

Part: SKIN — CRACKED (C-2 DOOR) · airframe 51,650 hrs · 28,046 cycles

INSPECTION FOUND A 1/2" CRACK IN C-2 DOOR SKIN AT UPPER CORNER OF THE CUTOUT FOR THE DOOR HANDLE. HANDLE EXCEEDS TRAVEL IN CLOSING DIRECTION ALSO. A DOUBLER WAS INSTALLED IAW SRM 52-00-01. THE DOOR HANDLE WAS REMOVED AND REPLACED IAW SRM 51-10-2.

Part: SPAR — CORRODED (HORIZONTAL STAB) · airframe 45,929 hrs · 25,109 cycles

INSPECTION FOUND LT HORIZONTAL STABILIZER UPPER SPAR CHORD (AFT SPAR O/B END) CORRODED AT STA 305. REPAIRED IAW ECRA 5510-01553.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 45,929 hrs · 25,109 cycles

INSPECTION FOUND STRINGER 27L CORRODED ON O/B SIDE AT STA 500C. THE CORRODED SECTION OF STRINGER WAS REMOVED AND A REPAIR WAS INSTALLED USING DOUBLERS AND FILLER IAW SRM 53-00-03, PAGE 207.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 45,929 hrs · 25,109 cycles

INSPECTION FOUND A 2 INCH CRACK AT RIVET IN ANTENNA CHANNEL AT STA 727D, BL 0. A NEW ANTENNA CHANNEL WAS INSTALLED IAW SRM 51-10-2.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 45,929 hrs · 25,109 cycles

INSPECTION FOUNDA 3 INCH CRACK IN STRINGER 8R AT STA 500C. THE STRINGER WAS REPAIRED IAW ECRA 5310-04074.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 45,929 hrs · 25,109 cycles

INSPECTION FOUND FLOOR SUPPORTS CORRODED FIVE INCHES AFT OF STA 767 AT RBL 3 AND LBL 3. THE CORROSION WAS REMOVED AND REPAIRS WERE ACCOMPLISHED IAW ECRA 5320-01603A.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 45,929 hrs · 25,109 cycles

INSPECTION FOUND RIGHT I/B SEAT TRACK CORRODED AT STA 727E, RBL 19. THE CORRODED AREA WAS CUT OUT AND A REPAIR WAS INSTALLED IAW SRM 53-00-52, FIGURE 204.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 45,929 hrs · 25,109 cycles

INSPECTION FOUND A 1INCH CRACK IN FLOOR SUPPORT AT STA 540, RBL 1.0. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-10-02.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 45,929 hrs · 25,109 cycles

INSPECTION FOUND UPPER CHORD OF FLOORBEAM CORRODED AT STA 986. THE FLOORBEAM WAS REPAIRED IAW ECRA 5310-03851, REV A.

Part: SKIN — CRACKED (BS 767)

INSPECTION FOUND A 1.5 INCH CRACK IN FUSELAGE SKIN AT STA 767, TWO INCHES ABOVE L23R AND A 1.25 INCH CRACK WAS FOUND AT STA 767, TWO INCHES ABOVE L24R. DOUBLER REPAIRS WERE INSTALLED AT EACH CRACK LOCATION IAW SRM 53-00-01, FIGURE 201.

Part: SKIN — CRACKED (COCKPIT)

INSPECTION FOUND A .25 INCH CRACK IN L-1 COCKPIT WINDOW FRAME SKIN. A REPAIR WAS INSTALLED IAW ECRA 5330-02710.

Part: FLOORBEAM — CORRODED (BS 1006)

INSPECTION FOUND FLOORBEAM CORRODED AT STA 1006, LBL 20 TO RBL 20. A NEW UPPER T-FLANGE WAS SPLICED IN IAW SRM 53-00-51.

Part: FLOORBEAM — CORRODED (BS 328)

INSPECTION FOUND FORWARD CABIN FLOORBEAM AT STA 328 CORRODED FROM 29 LEFT OF CENTER TO AIRCRAFT CENTERLINE. THE FLOORBEAM WAS REPAIRED IAW SRM 53-10-51.

Part: SUPPORT — CORRODED (CARGO COMPT)

INSPECTION FOUND FLOOR SUPPORT CORRODED INBOARD OF DOOR IN AFT PIT. A NEW SECTION OF FLOOR SUPPORT WAS SPLICED IN IAW SRM 53-00-53.

Part: SUPPORT — CORRODED (BS 1006-1016)

INSPECTION FOUND LT AFT LAV FLOOR SUPPORT CORRODED AT STA 1006 TO 1016. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-10-02.

Part: INTERCOSTAL — CORRODED (BS 966-986)

INSPECTION FOUND INTERCOSTAL CORRODED AT STA 966 TO 986, RBL 15. AN INTERCOSTAL WAS FABRICATED AND INSTALLED IAW ECRA 5310-03347 AND SRM 51-10-02.

Part: SUPPORT — CORRODED (BS 986-1006)

INSPECTION FOUND RT AFT LAV FLOOR SUPPORT ANGLE CORRODED AT STA 986 TO 1006. THE SUPPORT ANGLE WAS REPAIRED IAW SRM 51-10-02.

Part: CHANNEL — CORRODED (BS 990)

INSPECTION FOUND LT AFT LAV U-CHANNEL CORRODED AT BS 990. A NEW U-CHANNEL WAS INSTALLED IAW SRM 51-10-02.

Part: SUPPORT — CORRODED (BS 1006-1016)

INSPECTION FOUND RT AFT LAV FLOOR SUPPORT ANGLE CORRODED AT STA 1006 TO 1016. THE SUPPORT ANGLE WAS REPLACED IAW SRM 51-10-02.

Part: SUPPORT — CORRODED (BS 986-1006)

INSPECTION FOUND LT AFT LAV FLOOR SUPPORT ANGLE CORRODED AT STA 986 TO 1006. A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-10-2.

Part: SUPPORT — CORRODED (BS 307)

INSPECTION FOUND FORWARD LAV LT SIDE AFT WALL FLOOR SUPPORT CORRODED AT STA 307. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-10-02.

Part: SUPPORT — CORRODED (BS 294.5-312)

INSPECTION FOUND FORWARD PASSENGER CABIN FLOOR SUPPORT CORRODED FROM STA 294.5 TO 312, 13 RIGHT OF CENTER AND 15 RIGHT OF CENTER. REPAIRS WERE FABRICATED AND INSTALLED IAW ECRA 5310-03347.

Part: SUPPORT — CRACKED (BS 328-344)

INSPECTION FOUND A 1.5 INCH CRACK AT ONE END OF FLOOR SUPPORT IN FORWARD CABIN ON LT SIDE, WITH CORROSION AT OTHER END, STA 328 TO 344. THE FLOOR SUPPORT WAS REPAIRED IAW SRM 51-70-12.

Part: SUPPORT — CRACKED (BS 327)

INSPECTION FOUND A .75 INCH CRACK AT AFT END OF FLOOR SUPPORT ON LT SIDE OF FORWARD CABIN NEAR STA 327, 13 INBOARD OF DOOR. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-70-11.

Part: FLOORBEAM — CORRODED (BS 312)

INSPECTION FOUND FORWARD CABIN FLOORBEAM CORRODED AROUND SCREW HOLES AT STA 312, FROM R-1 DOOR TO 10 LEFT OF CENTER. THE FLOORBEAM WAS REPAIRED IAW SRM 53-10-51.

Part: SUPPORT — CORRODED (BS 328-344)

INSPECTION FOUND FORWARD CABIN FLOOR SUPPORT CORRODED BETWEEN STA 328 AND 344, 11 RIGHT OF CENTER. THE FLOOR SUPPORT WAS REPAIRED IAW ECRA 5310-03347.

Part: FLOORBEAM — CORRODED (BS 294.5/344)

INSPECTION FOUND FORWARD CABIN FLOORBEAM CORRODED AROUND SCREW HOLES AT STA 294.5 AND STA 344. THE FLOORBEAM WAS REPAIRED IAW SRM 53-10-51.

Part: SUPPORT — CORRODED (BS 294.5-312)

INSPECTION FOUND FORWARD PASSENGER CABIN FLOOR SUPPORT CORRODED FROM STA 294.5 TO 312, 11 LEFT OF CENTER. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-10-2.

Part: FLOORBEAM — CORRODED (BS 947.5)

INSPECTION FOUND FLOORBEAM CORRODED AT STA 947.5, LBL 3 TO 8. THE CORRODED AREA WAS CUT OUT AND A REPAIR WAS INSTALLED IAW SRM 53-00-51.

Part: SKIN — CRACKED (NR 5 LE SLAT)

INSPECTION FOUND A .125 INCH CRACK JUST INBOARD OF ACTUATOR, IN LOWER SKIN OF RT WING NR 5 SLAT PANEL. A DOUBLER WAS INSTALLED IAW ECRA 5750-01159.