N388SW

Part: HOUSING — BROKEN (CABIN) · airframe 68,952 hrs · 55,590 cycles

G1 GALLEY EMER EXIT LIGHT HOUSING BROKEN. R & R LIGHT IAW AMM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 68,952 hrs · 55,590 cycles

LEFT CREASE BEAM WEB CORRODED BETWEEN BS 500A - 500B. R & R WEB IAW SRM.

Part: WIRE — DAMAGED (CABIN) · airframe 68,952 hrs · 55,590 cycles

RIGHT SIDE PAX CABIN EXIT LIGHT WIRES DAMAGED AT BS 616 CONNECTOR. REPAIRED WIRE IAW AMM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 68,952 hrs · 55,590 cycles

AFT CARGO PIT FRAME BOTTOM ANGLE CORRODED AT BS 84, STRINGER 27R. R & R ANGLE IAW SRM & DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,952 hrs · 55,590 cycles

FORWARD CARGO BAY STRINGER CLIP CRACKED AT BS 500D, STRINGER 19R. R & R CLIP IAW SRM & DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 68,952 hrs · 55,590 cycles

INTERCOSTAL WEB CRACKED AT BS 277, STRINGER 14R. R & R WEB IAW EA.

Part: INTERCOSTAL — DAMAGED (FUSELAGE) · airframe 68,952 hrs · 55,590 cycles

INTERCOSTAL DAMAGED, BETWEEN BS 947 - 952, BETWEEN STRINGER 11L - 12L. R & R INTERCOSTAL IAW SRM & DWG.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 68,952 hrs · 55,590 cycles

LEFT FLOORBEAM CRACKED AT BS 294.5, WL 208. REPAIRED FLOORBEAM IAW EA.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 68,952 hrs · 55,590 cycles

BUTT JOINT SPLICE STRAP CRACKED AT BS 360, STRINGER 3R. REPAIRED SPLICE IAW EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 68,952 hrs · 55,590 cycles

LONGITUDINAL FLOORBEAM LOWER CHORD CRACKED AT BS 662, RBL 24.8, CTR WING BOX. REPAIRED CHORD IAW EA.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 68,952 hrs · 55,590 cycles

STRINGER SPLICE CRACKED AT BS 360, STRINGER 4L. R & R CHANNEL IAW DWG & EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 68,952 hrs · 55,590 cycles

AFT CARGO COMPARTMENT SHEAR TIE CORRODED AT BS 727E, STRINGER 27L. REPAIRED SHEAR TIE IAW EA.

Part: CONNECTOR — MISSING (CABIN) · airframe 68,952 hrs · 55,590 cycles

G1 GALLEY EMER EXIT LIGHT CONNECTOR MISSING. R & R CONNECTOR ASSEMBLY IAW AMM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 68,952 hrs · 55,590 cycles

LEFT CUSP WEB CORRODED, BETWEEN BS 887 - 907. R & R CUSP WEB IAW DWG & SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 68,952 hrs · 55,590 cycles

LEFT CUSP WEB CORRODED, BETWEEN BS 727A - 727B. R & R CUSP WEB IAW SRM & DWG.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 68,952 hrs · 55,590 cycles

LEFT CUSP WEB CORRODED, BETWEEN BS 727C - 727D. R & R CUSP WEB IAW SRM & DWG.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 68,952 hrs · 55,590 cycles

RIGHT CUSP WEB CORRODED, BETWEEN BS 847 - 867. R & R CUSP WEB IAW DWG & AMM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 68,952 hrs · 55,590 cycles

LEFT CUSP WEB CORRODED BETWEEN BS 460 - 480. R & R CUSP WEB IAW SRM & DWG.

Part: FITTING — CORRODED (FUSELAGE) · airframe 68,952 hrs · 55,590 cycles

AFT PRESS BULKHEAD FWD STRINGER END FITTING CORRODED AT BS 1016, STRINGER 19L. R & R FITTING IAW EA.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 68,952 hrs · 55,590 cycles

LEFT BOTTOM OF CUSP WEB CORRODED, BETWEEN BS 380 - 400. R & R CUSP WEB IAW SRM & DWG.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 68,952 hrs · 55,590 cycles

RIGHT CUSP WEB CORRODED, BETWEEN BS 400 - 420. R & R CUSP WEB IAW SRM & DWG.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 68,952 hrs · 55,590 cycles

RIGHT CUSP WEB CORRODED, BETWEEN BS 332 - 344. R & R CUSP WEB IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 68,952 hrs · 55,590 cycles

SHEAR TIE CORRODED AT BS 847, BETWEEN STRINGER 27R - 27L. R & R SHEAR TIE IAW SRM & DWG.

Part: BAFFLE — CRACKED (FUSELAGE) · airframe 68,952 hrs · 55,590 cycles

AFT PRESS BULKHEAD BAFFLE PLATE CRACKED AT BS 1016, LBL 20. R & R BAFFLE PLATE IAW DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 68,952 hrs · 55,590 cycles

FORWARD GALLEY DOOR, AFT SURROUND STRUCTURE INTERCOSTAL T CHORD CRACKED AT TRIM RADIUS AT DOOR STOP. R & R T CHORD IAW EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 68,952 hrs · 55,590 cycles

SHEAR TIE CORRODED AT BS 767, BETWEEN STRINGER 26L - 27L. R & R SHEAR TIE IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 68,952 hrs · 55,590 cycles

AFT CARGO COMPARTMENT PREVIOUS SHEAR TIE CORRODED AT BS 807, BETWEEN STRINGER 27R - 27L. REPAIRED SHEAR TIE IAW EA.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 68,952 hrs · 55,590 cycles

AFT GALLEY DOOR CUT OUT, LOWER SILL CREASE BEAM INNER CHORD CORRODED ON UPPER SURFACE. R & R CREASE BEAM IAW SRM & DWG.

Part: STRAP — CRACKED (FUSELAGE) · airframe 68,952 hrs · 55,590 cycles

LEFT CREW O2 MASK BOX FORWARD MOUNT STRAP CRACKED AT BS 967, BETWEEN STR 3L TO STR 4L. R & R STRAP IAW SRM & DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,952 hrs · 55,590 cycles

R1 DOOR LOWER AFT CORNER SKIN CRACKED AT BS 328, STRINGER 17R. REPAIRED SKIN IAW SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 68,952 hrs · 55,590 cycles

LEFT WEB CRACKED AT BS 947 FWD LOWER CORNER OF AFT ENTRY DOOR, UPPER HINGE FITTING. R & R WEB IAW DWG & SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 68,952 hrs · 55,590 cycles

AFT CARGO COMPARTMENT STRINGER CLIP CORRODED, AT BS 787, STRINGER 26R. R & R CLIP IAW SRM & DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 68,952 hrs · 55,590 cycles

SHEAR TIE CORRODED AT BS 727E, BETWEEN STRINGER 26R - 27R. REPAIRED SHEAR TIE IAW EA.

Part: CREASE BEAM — CORRODED (L1 DOOR) · airframe 68,952 hrs · 55,590 cycles

L1 DOOR CREASE BEAM INNER CHORD CORRODED, BETWEEN BS 312 - 350, LBL 58. R & R CHORD IAW SRM & DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 68,952 hrs · 55,590 cycles

FORWARD GALLEY DOOR CUT OUT LOWER SILL, CREASE BEAM INNER CHORD, CORRODED AT BS 332, STRINGER 17R, ON UPPER SURFACE. R & R BEAM IAW SRM & DWG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 68,952 hrs · 55,590 cycles

L1 DOOR, UPPER HINGE CUT OUT FITTING CRACKED AT BS 303.9+2, STRINGER 10L. R & R FITTING IAW SRM & DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 68,952 hrs · 55,590 cycles

FORWARD GALLEY DOOR CUT OUT, FWD FRAME SUPPORT ANGLE CRACKED AT BS 291, STRINGER 11R. R & R ANGLE IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 68,952 hrs · 55,590 cycles

FRAME CRACKED AT BS 500D, BETWEEN STRINGER 21R - 22R. REPAIRED FRAME IAW EA.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 68,952 hrs · 55,590 cycles

R1 DOOR UPPER HINGE CUT OUT SUPPORT ANGLE CRACKED AT BS 291.50, STRINGER 9R. R & R ANGLE IAW SRM & DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 68,952 hrs · 55,590 cycles

FORWARD GALLEY DOOR CUT OUT FWD FRAME SUPPORT ANGLE CRACKED AT BS 291, STRINGER 12R. R & R ANGLE IAW SRM & DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 68,952 hrs · 55,590 cycles

FORWARD GALLEY DOOR CUT OUT, FWD FRAME SUPPORT ANGLE CRACKED AT BS 291, STRINGER 11R. R & R ANGLE IAW SRM & DWG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 68,952 hrs · 55,590 cycles

LONGITUDINAL FLOORBEAM ATTACHMENT CLIP CRACKED AT BS 639, RBL 45.5. R & R CLIP IAW SRM & DWG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 68,952 hrs · 55,590 cycles

L1 DOOR UPPER HINGE CUT OUT FITTING CRACKED AT BS 303.9+2, WL 259.88. R & R FITTING IAW SRM & DWG.

Part: INDICATOR — MALFUNCTIONED (COCKPIT) · airframe 68,520 hrs · 55,304 cycles

JUST PRIOR TO TOP OF DESCENT AT FL350 HEARD A NOISE, SOUNDED LIKE ARCING, FOLLOWED BY STRONG ODOR. DID NOT GET ANY APPRECIABLE SMOKE & SMELL DISSIPATED. R & R WEATHER INDICATOR IAW AMM.

Part: SUPPORT ANGLE — CRACKED (LT WING) · airframe 67,733 hrs · 54,784 cycles

LEFT WING LOWER LE SUPPORT STRUCTURE ANGLE, LOCATED INBD OF LE STATION 212, CRACKED. R & R ANGLE IAW DWG & SRM.

Part: FITTING — CORRODED (RT WING) · airframe 67,733 hrs · 54,784 cycles

RIGHT WING AFT MLG, SUPPORT BEAM FITTING INBD UPPER HOLE CORRODED, AROUND UPPER PART OF HOLE. R & R FITTING IAW EA.

Part: SKIN — CRACKED (LT WING) · airframe 67,733 hrs · 54,784 cycles

LEFT WING UPPER SKIN, 3RD FROM AFT FASTENER ROW HOLE AT APPROX RSS 168 CRACKED. REPAIRED SKIN IAW SRM & EA.

Part: SKIN — CRACKED (LT WING) · airframe 67,733 hrs · 54,784 cycles

LEFT WING UPPER SKIN, AFT MOST ROW, FASTENER HOLE AT APPROX RSS 253 CRACKED. REPAIRED SKIN IAW SRM & EA.

Part: SKIN — CRACKED (LT WING) · airframe 67,733 hrs · 54,784 cycles

LEFT WING UPPER SKIN, 3RD FROM AFT FASTENER ROW HOLE AT APPROX RSS 248 CRACKED. REPAIRED SKIN IAW SRM & EA.

Part: SKIN — CRACKED (RT WING) · airframe 67,733 hrs · 54,784 cycles

RIGHT WING TE UPPER SKIN AT RSS 253, FASTENER HOLE CRACKED. REPAIRED SKIN IAW SRM & EA.

Part: SKIN — CRACKED (RT WING) · airframe 67,733 hrs · 54,784 cycles

RIGHT WING UPPER SKIN AT TE, WING STATION RSS 264.5, FASTENER HOLE CRACKED. REPAIRED SKIN IAW SRM & EA.

Part: SKIN — CRACKED (LT WING) · airframe 67,733 hrs · 54,784 cycles

LEFT WING UPPER SKIN, 2ND FROM AFT FASTENER ROW HOLE AT APPROX RSS 270 CRACKED. REPAIRED SKIN IAW SRM & EA.

Part: SKIN — CRACKED (LT WING) · airframe 67,733 hrs · 54,784 cycles

LEFT WING UPPER SKIN AFT MOST ROW, FASTENER HOLE AT APPROX RSS 256 CRACKED. REPAIRED SKIN IAW SRM & EA.

Part: SKIN — CRACKED (RT WING) · airframe 67,733 hrs · 54,784 cycles

RIGHT WING STATION RSS 239.5, UPPER WING SKIN TE CRACKED. REPAIRED SKIN IAW SRM & EA.

Part: SKIN — CRACKED (LT WING) · airframe 67,733 hrs · 54,784 cycles

LEFT WING UPPER SKIN, AFT MOST ROW, FASTENER HOLE AT APPROX RSS 238 CRACKED. REPAIRED SKIN IAW SRM & EA.

Part: SKIN — CRACKED (RT WING) · airframe 67,733 hrs · 54,784 cycles

RIGHT WING UPPER SKIN AT STATION RSS 245 TE, FASTENER HOLE CRACKED. REPAIRED SKIN IAW SRM & EA.

Part: SKIN — CRACKED (RT WING) · airframe 67,733 hrs · 54,784 cycles

RIGHT WING UPPER SKIN AT TE, STATION RSS 267.5, FASTENER HOLE CRACKED. REPAIRED SKIN IAW SRM & EA.

Part: SKIN — CRACKED (LT WING) · airframe 67,733 hrs · 54,784 cycles

LEFT WING UPPER SKIN AFT MOST ROW, FASTENER HOLE AT APPROX RSS 263 CRACKED. REPAIRED SKIN IAW SRM & EA.

Part: WEB — CRACKED (RT WING) · airframe 67,733 hrs · 54,784 cycles

RIGHT WING RSS 219, UPPER HOLE IN WEB CRACKED. REPAIRED WEB IAW EA.

Part: SKIN — CRACKED (RT WING) · airframe 67,733 hrs · 54,784 cycles

RIGHT WING UPPER SKIN TE FASTENER HOLE AT RSS 263 CRACKED. REPAIRED SKIN IAW SRM & EA.

Part: SKIN — CRACKED (LT WING) · airframe 67,733 hrs · 54,784 cycles

LEFT WING UPPER SKIN, AFT MOST ROW, FASTENER HOLE AT APPROX RSS 249 CRACKED. REPAIRED SKIN IAW SRM & EA.

Part: SKIN — CRACKED (LT WING) · airframe 67,733 hrs · 54,784 cycles

LEFT WING UPPER SKIN, AFT MOST ROW, FASTENER HOLE AT APPROX RSS 248 CRACKED. REPAIRED SKIN IAW SRM & EA.

Part: FITTING — CRACKED (LT MLG) · airframe 67,733 hrs · 54,784 cycles

LEFT MLG SUPPORT BEAM, AFT FITTING CRACKED IN UPPER INBD HOLE. R & R FITTING IAW EA.

Part: STRUCTURE — CRACKED (LT WING) · airframe 67,733 hrs · 54,784 cycles

LEFT WING RSS 271, LOWER WAFFLE BOARD CRACKED. R & R WAFFLE BOARD IAW SRM & DWG.

Part: ATTACH ANGLE — CRACKED (LT WING) · airframe 67,733 hrs · 54,784 cycles

LEFT WING OTBD TE, OTBD FIRE BOX AFT INBD ATTACH ANGLE CRACKED. R & R ANGLE IAW SRM & DWG.

Part: SPAR — CRACKED (LT WING) · airframe 67,733 hrs · 54,784 cycles

LEFT WING REAR SPAR, UPPER CHORD SPLICE CRACKED AT UPPER INBD FASTENER HOLE, COMMON TO MLG SUPPORT BEAM AFT FITTING. REPAIRED CHORD IAW EA.

Part: SPAR — CRACKED (RT WING) · airframe 67,733 hrs · 54,784 cycles

RIGHT WING REAR SPAR UPPER CHORD, CRACKED IN UPPER INBD FASTENER HOLE, COMMON TO MLG SUPPORT BEAM AFT FITTING. REPAIRED CHORD IAW EA.

Part: SKIN — CRACKED (RT WING) · airframe 67,733 hrs · 54,784 cycles

RIGHT WING UPPER SKIN, CRACKED AT AFT SPAR FASTENER, STATION 175. REPAIRED SKIN IAW SRM & EA.

Part: SKIN — CRACKED (RT WING) · airframe 67,730 hrs · 54,783 cycles

RIGHT WING UPPER SKIN CRACKED AT AFT SPEED FASTENER, STATION 175. RT SKIN IAW EA.

Part: SKIN — CRACKED (RT WING) · airframe 67,733 hrs · 54,784 cycles

RIGHT WING UPPER SKIN CRACKED, AFT SPAR AFT FASTENER STATION 175. REPAIRED SKIN IAW SRM.

Part: LENS — LOOSE (EXIT SIGN) · airframe 66,901 hrs · 54,185 cycles

RIGHT LOWER OVERWING EXIT SIGN LENS LOOSE. SECURED LENS IAW AMM.

Part: LENS — LOOSE (CABIN) · airframe 66,901 hrs · 54,185 cycles

RIGHT OVERWING EXIT LIGHT COVER LENS LOOSE. SECURED LENS IAW AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,737 hrs · 54,063 cycles

FUSELAGE SKIN CRACKED AT FWD RT CORNER OF GND SERVICE ACCESS PANEL. REPAIRED SKIN IAW EA.

Part: SLAT — DELAMINATED (LT WING) · airframe 66,737 hrs · 54,063 cycles

NUMBER 2 LE SLAT OTBD UPPER CORNER DELAMINATED. R & R SLAT ASSEMBLY IAW MM.

Part: ACTUATOR — MALFUNCTIONED (LE FLAP) · airframe 66,389 hrs · 53,831 cycles

AIR TURN BACK, LE FLAPS TRANSIT LIGHT ILLUMINATED UPON FLAP RETRACTION. R & R 2 LE FLAP ACTUATOR IAW AMM 27-81-31.

Part: LENS — UNSECURE (CABIN) · airframe 66,213 hrs · 53,707 cycles

RIGHT OVERWING EMER EXIT LENS FELL OFF. REPAIRED LENS IAW AMM.

Part: COVER — MISSING (EXIT SIGN) · airframe 65,870 hrs · 53,483 cycles

LEFT OVERWING EMER EXIT SIGN COVER MISSING. INSTALLED COVER IAW SIP.

Part: LENS — LOOSE (CABIN) · airframe 63,653 hrs · 51,934 cycles

LEFT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. R & R LENS IAW MM.

Part: ANGLE — CRACKED (RT WING) · airframe 63,542 hrs · 51,862 cycles

RIGHT WING NR 6 FAIRING FLAP TRACK OTBD SIDE UPPER AREA ANGLE CRACKED. R & R ANGLE IAW SRM & DWG.

Part: ANGLE — CRACKED (RT WING) · airframe 63,542 hrs · 51,862 cycles

RIGHT WING NR 6 FAIRING FLAP TRACK INBD SIDE UPPER AREA ANGLE CRACKED. R & R ANGLE IAW SRM & DWG.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 63,542 hrs · 51,862 cycles

STRINGER SPLICE CRACKED AT BS 360, STRINGER 15L. R & R SPLICE IAW SRM & DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 63,542 hrs · 51,862 cycles

FRAME LOWER FLANGE CORRODED AT BS 328, BETWEEN STRINGER 27R TO STRINGER 28R. REPAIRED FRAME IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 63,542 hrs · 51,862 cycles

ANGLE CRACKED AT BS 360, STRINGER 20L. R & R ANGLE IAW SRM & DWG.

Part: PLATE — CRACKED (FUSELAGE) · airframe 63,542 hrs · 51,862 cycles

PLATE CRACKED AT BS 328, BETWEEN STRINGER 22R TO STRINGER 24R. REPAIRED PLATE IAW SRM.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 63,542 hrs · 51,862 cycles

SUPPORT BRACKET CRACKED AT BS 380, STRINGER 20L. R & R BRACKET IAW SRM & DWG.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 63,542 hrs · 51,862 cycles

SUPPORT BRACKET CRACKED AT BS 294.5, STRINGER 23L. R & R BRACKET IAW SRM & DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 63,542 hrs · 51,862 cycles

ANGLE CRACKED AT BS 328, STRINGER 20L. R & R ANGLE IAW SRM & DWG.

Part: STRAP — CRACKED (FUSELAGE) · airframe 63,542 hrs · 51,862 cycles

STRAP CRACKED AT BS 328, LBL 12. R & R STRAP IAW SRM & DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 63,542 hrs · 51,862 cycles

SUPPORT ANGLE CRACKED AT BS 312+9, STRINGER 20L. R & R ANGLE IAW SRM & DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 63,542 hrs · 51,862 cycles

SUPPORT ANGLE CRACKED AT BS 336, STRINGER 20L. R & R ANGLE IAW SRM & DWG.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 63,542 hrs · 51,862 cycles

ATTACHMENT CLIP CRACKED AT BS 348.2, STRINGER 15L. R & R CLIP IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,542 hrs · 51,862 cycles

FRAME INNER CHORD CRACKED AT BS 348.2, STRINGER 17L. REPAIRED CHORD IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,542 hrs · 51,862 cycles

FRAME OUTER CHORD CRACKED AT BS 348.2, STRINGER 16L. REPAIRED CHORD IAW EA.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 63,542 hrs · 51,862 cycles

ATTACH CLIP CRACKED AT BS 348.2, STRINGER 15L. R & R CLIP IAW SRM & DWG.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 63,542 hrs · 51,862 cycles

LONGITUDINAL FLOORBEAM CTR SECTION WEB CRACKED AT BS 713, RBL 24.8. REPAIRED WEB IAW EA.

Part: RIB — CRACKED (RT WING) · airframe 63,542 hrs · 51,862 cycles

RIGHT WING UPPER CHORD RIB CRACKED AT WBL 114 AT LEVEL OF STRINGER 2. REPAIRED CHORD IAW EA.

Part: FITTING — CRACKED (FUSELAGE) · airframe 63,542 hrs · 51,862 cycles

CLIP CRACKED AT BS 348.2, STRINGER 15L. R & R CLIP IAW SRM & DWG.

Part: STRAP — CRACKED (FUSELAGE) · airframe 63,542 hrs · 51,862 cycles

STRAP CRACKED AT BS 348.2+2, STRINGER 16L. R & R STRAP IAW SRM & DWG.

Part: RIB — CRACKED (LT WING) · airframe 63,542 hrs · 51,862 cycles

LEFT WING RIB UPPER CHORD CRACKED AT WBL 114, STRINGER 2. REPAIRED CHORD IAW EO & EA.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 63,542 hrs · 51,862 cycles

CHANNEL CRACKED AT BS 727, RBL 3. R & R CHANNEL IAW SRM & DWG.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 63,542 hrs · 51,862 cycles

LONGITUDINAL FLOORBEAM CTR SECTION WEB CRACKED AT BS 709, RBL 24.8. REPAIRED WEB IAW EA.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 63,542 hrs · 51,862 cycles

SUPPORT ANGLE CRACKED AT BETWEEN BS 927 TO BS 947.5, BL 0. R & R ANGLE IAW SRM & DWG.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 63,542 hrs · 51,862 cycles

CENTER WING BOX SEAT TRACK CRACKED AT BS 727B, LBL 45.57+1. REPAIRED SEAT TRACK IAW SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 63,542 hrs · 51,862 cycles

UPPER FLOORBEAM ANGLE CRACKED AT BS 540, BETWEEN BL 0 TO LBL 24.5. R & R ANGLE IAW SRM & DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,542 hrs · 51,862 cycles

FORWARD ENTRY DOOR AFT LOWER CUT OUT CORNER CRACKED AT BS 344, STRINGER 17L. REPAIRED CUT OUT IAW SRM.

Part: STRUCTURE — CRACKED (LT WING) · airframe 63,542 hrs · 51,862 cycles

LEFT WING LOWER CHORD CRACKED AT RRS 537, 806 TE AREA OF AILERON & CONTROL TAB. R & R CHORD IAW SRM & DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 63,542 hrs · 51,862 cycles

UPPER FLOORBEAM ANGLE OF WEB CRACKED BETWEEN BS 500D TO BS 520, BL 0. R & R WEB IAW SRM & DWG.

Part: ANGLE — CRACKED (VERTICAL STAB) · airframe 63,542 hrs · 51,862 cycles

VERTICAL STABILIZER ANGLE CRACKED AT ACCESS PANEL 9503. R & R ANGLE IAW SRM & DWG.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 63,542 hrs · 51,862 cycles

RIGHT HORIZONTAL STABILIZER ACCESS PANEL 9249R RIB CRACKED. R & R RIB IAW SRM & DWG.

Part: ANGLE — CRACKED (RT WING) · airframe 63,542 hrs · 51,862 cycles

RIGHT WING TE ANGLE CRACKED AT LEVEL RSS 533+13 INCHES. R & R ANGLE IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,542 hrs · 51,862 cycles

FRAME CRACKED AT BS 947.5, BETWEEN STRINGER 24R TO STRINGER 25R. R & R FRAME IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 63,542 hrs · 51,862 cycles

TIE CLIP CRACKED AT BS 727A, STRINGER 20L. R & R TIE CLIP IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,542 hrs · 51,862 cycles

FRAME CRACKED AT BS 500B, STRINGER 21R. REPAIRED FRAME IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,542 hrs · 51,862 cycles

FRAME CRACKED AT BS 520, STRINGER 21R. REPAIRED FRAME IAW SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 63,542 hrs · 51,862 cycles

TIE CLIP CRACKED AT BS 787, STRINGER 24R. R & R TIE CLIP IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,542 hrs · 51,862 cycles

FRAME INNER CHORD CRACKED AT BS 500B, STRINGER 21L. REPAIRED FRAME IAW SRM.

Part: PLATE — CRACKED (RT HORIZ STAB) · airframe 63,542 hrs · 51,862 cycles

RIGHT HORIZONTAL STABILIZER ACCESS PANEL 9226R PLATE CRACKED. R & R PLATE IAW SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 63,542 hrs · 51,862 cycles

WEB CORRODED BETWEEN BS 460 TO BS 480, STRINGER 17R. R & R WEB IAW SRM & DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 63,542 hrs · 51,862 cycles

ANGLE CRACKED BETWEEN BS 927 TO BS 947.5, BL 0. R & R ANGLE IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 63,542 hrs · 51,862 cycles

TIE CLIP CRACKED AT BS 947.5, STRINGER 25R. R & R TIE CLIP IAW SRM & DWG.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 63,542 hrs · 51,862 cycles

LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 663.75+7.5, RBL 25.8. REPAIRED BEAM IAW EA.

Part: CROSSBEAM — CRACKED (CARGO DOOR) · airframe 63,542 hrs · 51,862 cycles

AFT CARGO DOOR CROSSBEAM WEB CRACKED. REPAIRED WEB IAW EA.

Part: CROSSBEAM — CRACKED (CARGO DOOR) · airframe 63,542 hrs · 51,862 cycles

AFT CARGO DOOR CROSSBEAM E & D T CHORDS CRACKED. REPAIRED T CHORD IAW EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 63,542 hrs · 51,862 cycles

LONGITUDINAL FLOORBEAM UPPER CHORD AFT END CTR SECTION CRACKED AT BS 727B, LBL 45.5. REPAIRED CHORD IAW EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 63,542 hrs · 51,862 cycles

LONGITUDINAL FLOORBEAM CTR SECTION WEB CRACKED AT BS 708, RBL 24.8. REPAIRED WEB IAW EA.

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 63,542 hrs · 51,862 cycles

MAIN WW PRESS DECK WEB CRACKED AT BS 663.75, RBL 42. REPAIRED WEB IAW SRM.

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 63,542 hrs · 51,862 cycles

MAIN WW PRESS DECK WEB CRACKED AT BS 663.75+9.5, LBL 24.5 + 6.5. REPAIRED WEB IAW SRM.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 63,542 hrs · 51,862 cycles

CHORD CRACKED AT BS 727, STRINGER 18L. REPAIRED CHORD IAW EA.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 63,542 hrs · 51,862 cycles

CHORD CRACKED AT BS 727, STRINGER 18R. REPAIRED CHORD IAW EA.

Part: LENS — MISSING (CABIN) · airframe 63,396 hrs · 51,761 cycles

FORWARD ENTRY LOWER EMERGENCY EXIT LIGHT LENS MISSING. R & R LIGHT ASSEMBLY IAW AMM.

Part: GASPER FAN — FAULTY (AC BAY) · airframe 62,899 hrs · 51,443 cycles

AIR TURN BACK, SMELL OF ELECTRICAL BURNING IN MID CABIN, NO VISIBLE SMOKE. R & R GASPER FAN IAW MM.

Part: LENS — BROKEN (CABIN) · airframe 61,560 hrs · 50,473 cycles

ENTRY DOOR "EMERGENCY EXIT" LIGHT COVER BROKEN. R&R LENS IAW MM & SIP.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,816 hrs · 49,917 cycles

R2 DOOR LOWER HINGE SKIN CUTOUT CRACKED. REPAIRED SKIN PER EA.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 60,797 hrs · 49,905 cycles

R1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MT.

Part: SPINDLE — CORRODED (TE FLAP) · airframe 59,907 hrs · 49,263 cycles

LEFT WING NR 7 FLAP SPINDLE HAS EVIDENCE OF BASE METAL CORROSION AT THE LOWER SURFACE OF THE SPINDLE PORTION OF THE ROOT. REMOVED AND REPLACED RIGHT OTBOARD MIDFLAP INBOARD (NR 7) CARRIAGE PER MT #327-51-08.

Part: FASTENER — CRACKED (FUSELAGE) · airframe 59,635 hrs · 49,062 cycles

AFT PRESSURE BULKHEAD AT STATION 101B HAS TWO FASTENERS WITH CRACKS OUTBOARD OF STA 6L (MARKED). VERIFIED FROM FWD SIDE OF BULKHEAD. REPAIRED PER SRM 53-80-08-2R-7. THIS IS A CATEGORY B REPAIR. SEE SA-M 326 FACT AS A RESULT OF POST REPAIR INSPECTION.

Part: FASTENER — CRACKED (FUSELAGE) · airframe 59,635 hrs · 49,062 cycles

AFT PRESSURE BULKHEAD AT STATION 101B HAS TWO FASTENERS WITH CRACKS OUTBOARD OF STA 6L (MARKED). VERIFIED FROM FWD SIDE OF BULKHEAD. REPAIRED PER SRM 53-80-08-2R-7. THIS IS A CATEGORY B REPAIR. SEE SA-M 326

Part: FITTING — MISSING (FUSELAGE) · airframe 59,356 hrs · 48,867 cycles

STA 178 BULKHEAD RADOME CLOSE CLIP MISSING AT 3 O'CLOCK POSITION. INSTALLED CLIP IAW SRM.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 59,357 hrs · 48,867 cycles

BULKHEAD STIFFENER CRACKED AT BS 178, STR 17R. REMOVED AND REPLACED STIFFENER IAW EA.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 59,357 hrs · 48,867 cycles

LEFT EMERGENCY EXIT LIGHT FOR DOOR AND SIDEWALL INOP. REMOVED AND REPLACED BATTERY PACK IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 59,357 hrs · 48,867 cycles

RIGHT OVERHEAD EMERGENCY EXIT BULLNOSE LIGHT INOP AT ROW 15. RELAMPED LIGHT IAW AMM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 59,357 hrs · 48,867 cycles

STRINGER CRACKED AT BS 178, 17R. REPAIRED STRINGER IAW EA.

Part: SIGN — LOOSE (CABIN) · airframe 58,642 hrs · 48,317 cycles

R1 DOOR EMERGENCY EXIT SIGN LOOSE. REMOVED & REPLACED SIGN ASSY PER MM.

Part: SLIDE — LOW PRESSURE (L1 DOOR) · airframe 58,607 hrs · 48,291 cycles

L1 DOOR EMERGENCY EVAC SLIDE PRESSURE GAUGE LOW. REMOVED AND REPLACED SLIDE PER MT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 58,496 hrs · 48,207 cycles

RIGHT EEPLS INOP AT ROW 1. RELAMPED EEPLS IAW AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,496 hrs · 48,207 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 460+10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,496 hrs · 48,207 cycles

FUSELAGE SKIN CRACKED AT RIGHT BS 787+10 LOWER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN PER SERVICE BULLETIN.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,496 hrs · 48,207 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 520+10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,496 hrs · 48,207 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 887+10 UPPER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,496 hrs · 48,207 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 420+10 UPPER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW S/B.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,496 hrs · 48,207 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 440+10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,496 hrs · 48,207 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 500B+10 UPPER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,496 hrs · 48,207 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 727+10 LOWER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,496 hrs · 48,207 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 360+10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,496 hrs · 48,207 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 500B+10 UPPER FORWARD CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,496 hrs · 48,207 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 887+10 LOWER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,496 hrs · 48,207 cycles

FUSELAGE SKIN CRACKED AT LEFT BS 460+10 UPPER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN PER SERVICE BULLETIN.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,496 hrs · 48,207 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 460+10 UPPER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW S/B.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,496 hrs · 48,207 cycles

FUSELAGE SKIN CRACKED AT RIGHT BS 807+10 UPPER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN PER SERVICE BULLETIN.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,496 hrs · 48,207 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 400+10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,496 hrs · 48,207 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 420+10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW S/B.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,496 hrs · 48,207 cycles

FUSELAGE SKIN CRACKED AT LEFT BS 480+10 UPPER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN PER SERVICE BULLETIN.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,496 hrs · 48,207 cycles

FUSELAGE SKIN CRACKED AT LEFT BS 380+10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN PER SERVICE BULLETIN.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,496 hrs · 48,207 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 520+10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,496 hrs · 48,207 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 807+10 UPPER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,496 hrs · 48,207 cycles

FUSELAGE SKIN CRACKED AT RIGHT BS 807+10 FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN PER SERVICE BULLETIN.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,496 hrs · 48,207 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 867+10 UPPER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,496 hrs · 48,207 cycles

FUSELAGE SKIN CRACKED AT RIGHT BS 787+10 UPPER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN PER SERVICE BULLETIN.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,496 hrs · 48,207 cycles

FUSELAGE SKIN CRACKED AT RIGHT BS 807+10 UPPER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN PER SERVICE BULLETIN.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,496 hrs · 48,207 cycles

FUSELAGE SKIN CRACKED AT LEFT BS 440+10 UPPER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN PER SERVICE BULLETIN.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,496 hrs · 48,207 cycles

FUSELAGE SKIN CRACKED AT RIGHT BS 500C+10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN PER SERVICE BULLETIN.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,496 hrs · 48,207 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 500+10 UPPER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW S/B.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,496 hrs · 48,207 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 360+10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,496 hrs · 48,207 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 440+10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,496 hrs · 48,207 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 500A+10 UPPER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW S/B.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,496 hrs · 48,207 cycles

RIGHT FUSELAGE WINDOW CRACKED AT BS 400+10 UPPER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,496 hrs · 48,207 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 480+10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW S/B.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 58,496 hrs · 48,207 cycles

STRINGER CLIP CRACKED AT BS 887, STR 5R. REMOVED AND REPLACED CLIP IAW BAC DWG & SRM.

Part: WIRE — BROKEN (CABIN) · airframe 58,496 hrs · 48,207 cycles

G1 GALLEY EMERGENCY EXIT LIGHT WIRE BROKEN. REPAIRED WIRE IAW AMM.

Part: COVER — CRACKED (EXIT SIGN) · airframe 58,364 hrs · 48,104 cycles

FORWARD LAV EMERGENCY EXIT SIGN COVER CRACKED. REMOVED AND REPLACED COVER IAW AMM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 58,364 hrs · 48,104 cycles

R2 DOOR EMERGENCY ESCAPE SLIDE OUT OF POSITION. REMOVED AND INSTALLED SLIDE IAW MT.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 58,364 hrs · 48,104 cycles

LT WING NR 2 SLAT TRAILING EDGE WEDGE OUTBOARD END DELAMINATED. REPAIRED SLAT PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 58,364 hrs · 48,104 cycles

LONGITUDINAL FLOORBEAM CRACKED AT BS 616, LBL45. REPAIRED WEB IAW EA.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 58,364 hrs · 48,104 cycles

LT CREASE BEAM WEB CRACKED AT BS 616. REMOVED AND REPLACED WEB IAW SRM & DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 58,364 hrs · 48,104 cycles

AFT CARGO PIT FLOOR SUPPORT STA 825, RBL 8 CORRODED. REPAIRED FLOOR SUPPORT PER SRM & EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 58,364 hrs · 48,104 cycles

LONGITUDINAL FLOORBEAM CRACKED AT BS 727B, RBL 45.2. REPAIRED BEAM IAW EA AND AMM.

Part: PLATE — WORN (GIRT BAR) · airframe 58,364 hrs · 48,104 cycles

R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR FLOOR MOUNTS WORN. REMOVED AND REPLACED PLATES IAW MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,364 hrs · 48,104 cycles

SKIN CRACKED AT BS 947.5, WL 219. REPAIRED SKIN IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 58,364 hrs · 48,104 cycles

FRAME INNER CHORD CRACKED AT BS 616, STR 15L. REPAIRED CHORD IAW EA AND AMM.

Part: SKIN — TORN (CARGO DOOR) · airframe 58,364 hrs · 48,104 cycles

AFT CARGO DOOR SKIN PROTECTOR AT AFT UPPER CUTOUT TORN. REMOVED AND REPLACED SKIN PER SRM & BAC DRAWING.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,495 hrs · 47,444 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 767+8, STR 4R. REPAIRED SKIN IAW SRM AND EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,495 hrs · 47,444 cycles

DURING SCHEDULED OTS CHECK, FOUND LT SKIN CRACKED AT BS 420+6. REPAIRED SKIN IAW EA.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 57,420 hrs · 47,392 cycles

DURING SCHEDULED OTS CHECK, FOUND LT KEEL BEAM CORRODED BETWEEN BS 625 TO BS 727+14. REPAIRED KEEL BEAM PER EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 57,420 hrs · 47,392 cycles

DURING SCHEDULED OTS CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT IAW MM.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 57,420 hrs · 47,392 cycles

DURING SCHEDULED OTS CHECK, FOUND LT HORIZONTAL STABILIZER LOWER SKIN CRACKED BETWEEN STA 157 TO STA 147. REPAIRED SKIN IAW EA.

Part: CONNECTOR — LOOSE (CABIN) · airframe 57,420 hrs · 47,392 cycles

DURING SCHEDULED OTS CHECK, FOUND RT OVERHEAD EMERGENCY EXIT BULLNOSE LIGHT CONNECTOR LOOSE. SECURED CONNECTOR PER MM.

Part: LENS — LOOSE (CABIN) · airframe 56,540 hrs · 46,737 cycles

L1 DOOR EMERGENCY EXIT LOWER LIGHT LENS LOOSE. REPAIRED LENS IAW MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,186 hrs · 46,452 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 867+11, STR 4R. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,186 hrs · 46,452 cycles

DURING SCHEDULED MV1 CHECK, FOUND SKIN CRACKED AT BS 867+11, STR 4R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,186 hrs · 46,452 cycles

DURING SCHEDULED MV1 CHECK, FOUND SKIN CRACKED AT BS 747+8, STR 4R. REPAIRED SKIN PER SRM.

Part: LIGHT — MISSING (CABIN) · airframe 56,165 hrs · 46,436 cycles

L1 DOOR EMERGENCY EXIT LIGHT LENS MISSING. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SLIDE — FAILED (R1 DOOR) · airframe 55,701 hrs · 46,084 cycles

DURING SCHEDULED 2HC2 CHECK, R1 DOOR EMERGENCY EVAC SLIDE FAILED SLIDE DEPLOYMENT CHECK. REMOVED AND REPLACED SLIDE PER MM.

Part: FLAP — DELAMINATED (LT WING) · airframe 55,701 hrs · 46,084 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND LT WING O/B AFT FLAP DELAMINATED FROM I/B END. REMOVED AND REPLACED AFT FLAP PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,543 hrs · 45,222 cycles

DURING SCHEDULED RON CHECK, FOUND SKIN CRACKED ART BS 847+7.5, STR 4R. REPAIRED SKIN PER EA.

Part: COVER — MISSING (CABIN) · airframe 54,387 hrs · 45,109 cycles

RT OVERWING EMERGENCY EXIT LIGHT COVER MISSING. INSTALLED COVER PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 5,482 hrs · 44,872 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 817, STR 4R. REPAIRED SKIN PER EA.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 53,150 hrs · 44,132 cycles

DURING SCHEDULED 16Y CHECK, FOUND SUPPORT ANGLE CRACKED AT BS 294.5, STR 13L. REMOVED AND REPLACED ANGLE PER SRM AND BAC DWG.

Part: SLAT — DELAMINATED (LT WING) · airframe 53,150 hrs · 44,132 cycles

DURING SCHEDULED 16Y CHECK, FOUND LT WING NR 2 SLAT I/B END DELAMINATED. REPAIRED SLAT PER SRM.

Part: SLAT — DELAMINATED (RT WING) · airframe 53,150 hrs · 44,132 cycles

DURING SCHEDULED 16Y CHECK, FOUND RT WING NR 5 SLAT I/B END DELAMINATED. REPAIRED SLAT PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 53,150 hrs · 44,132 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM CRACKED AT BS 616, LBL 45.5. REPAIRED BEAM PER EO.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,150 hrs · 44,132 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CRACKED AT BS 328, BETWEEN STR 20R TO STR 21R. REPAIRED FRAME PER EO.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 53,150 hrs · 44,132 cycles

DURING SCHEDULED 16Y CHECK, FOUND FWD CARGO SUPPORT ANGLE OF FRAME CORRODED AT BS 500D, BETWEEN STR 27R TO STR 28R. REMOVED AND REPLACED ANGLE PER SRM AND BAC DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 53,150 hrs · 44,132 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO FRAME CORRODED AT BS 747, BETWEEN STR 26L TO STR 27L. REPAIRED FRAME PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 53,150 hrs · 44,132 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 747, BETWEEN STR 25R TO STR 26R. REPAIRED FRAME PER SRM.

Part: STIFFENER — CRACKED (CENTER WING BOX) · airframe 53,150 hrs · 44,132 cycles

DURING SCHEDULED 16Y CHECK, FOUND CENTER WING BOX STIFFENER CRACKED AT BS 663.75, RBL 6.15. REMOVED AND REPLACED STIFFENER PER ACO.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 53,150 hrs · 44,132 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO CHANNEL CORRODED AT BS 772, LBL 8.10. REPAIRED CHANNEL PER SRM.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 53,150 hrs · 44,132 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 944, RBL 3.0. REPAIRED CHANNEL PER EA.

Part: WEB — CORRODED (FUSELAGE) · airframe 53,150 hrs · 44,132 cycles

DURING SCHEDULED 16Y CHECK, FOUND WEB CORRODED BETWEEN BS 827 TO BS 847, RBL 62.50. REMOVED AND REPLACED WEB PER SRM AND BAC DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,150 hrs · 44,132 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CRACKED AT BS 294.5, STR 7R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,150 hrs · 44,132 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO COMPARTMENT FRAME ANGLE CRACKED AT BS 727E, BETWEEN STR 26L TO STR 27L. REPAIRED ANGLE PER SRM AND BAC DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,150 hrs · 44,132 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CRACKED AT BS 277, BETWEEN STR 9R TO STR 10R. REPAIRED FRAME PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,150 hrs · 44,132 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 1006, STR 9L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 53,150 hrs · 44,132 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO CHANNEL CORRODED AT BS 732D, RBL 8.10. REPAIRED CHANNEL PER EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 53,150 hrs · 44,132 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO FRAME CORRODED AT BS 767, BETWEEN STR 26L TO STR 27L. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,150 hrs · 44,132 cycles

DURING SCHEDULED 16Y CHECK, FOUND LT FRAME CRACKED AT BS 188. REPAIRED FRAME PER EA.

Part: LENS — BROKEN (CABIN) · airframe 53,150 hrs · 44,132 cycles

DURING SCHEDULED 16Y CHECK, FOUND RT EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LENS PER MM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 53,150 hrs · 44,132 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO COMPARTMENT FRAME CORRODED AT BS 787, BETWEEN STR 26L TO STR 27L. REPAIRED FRAME PER SRM.

Part: SUPPORT ANGLE — CRACKED (RT WING) · airframe 53,150 hrs · 44,132 cycles

DURING SCHEDULED 16Y CHECK, FOUND RT WING SUPPORT ANGLE UPPER SURFACE I/B SIDE CRACKED. REMOVED AND REPLACED ANGLE PER SRM AND BAC DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 53,150 hrs · 44,132 cycles

DURING SCHEDULED 16Y CHECK, FOUND FWD CARGO SHEAR TIE CORRODED AT BS 520, BETWEEN STR 28R TO STR 28L. REMOVED AND REPLACED SHEAR TIE PER SRM BAC DWG.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 53,150 hrs · 44,132 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 807, STR 27R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 53,150 hrs · 44,132 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 813, RBL 8.10. REPAIRED CHANNEL PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,150 hrs · 44,132 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 1121, STR 4L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: SLAT — DELAMINATED (RT WING) · airframe 53,150 hrs · 44,132 cycles

DURING SCHEDULED 16Y CHECK, FOUND RT WING NR 5 SLAT O/B END DELAMINATED. REPAIRED SLAT PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 53,150 hrs · 44,132 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO FRAME CORRODED AT BS 727D, BETWEEN STR 26L TO STR 27L. REPAIRED FRAME PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 53,150 hrs · 44,132 cycles

DURING SCHEDULED16Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986.5, LBL 43.5. REPAIRED BEAM PER SRM.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 53,150 hrs · 44,132 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED BETWEEN BS 907 TO BS 947.5, LBL 12.50. REPAIRED CHANNEL PER EA.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 53,150 hrs · 44,132 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 772, RBL 8.10. REPAIRED CHANNEL PER EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 53,150 hrs · 44,132 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO FRAME CORRODED AT BS 747, BETWEEN STR 26R TO STR 27R. REPAIRED FRAME PER SRM.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 53,150 hrs · 44,132 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO CHANNEL CORRODED AT BS 727B, STR 8.10. REPAIRED CHANNEL PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 53,150 hrs · 44,132 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO COMPARTMENT SHEAR TIE CORRODED AT BS 807, BETWEEN STR 26L TO STR 27L. REPAIRED FRAME PER SRM.

Part: SLAT — DELAMINATED (LT WING) · airframe 53,150 hrs · 44,132 cycles

DURING SCHEDULED 16Y CHECK, FOUND LT WING NR 3 SLAT O/B EDGE DELAMINATED. REPAIRED SLAT PER SRM.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 53,150 hrs · 44,132 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 897, RBL 8.10. REPAIRED CHANNEL PER EA.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 53,150 hrs · 44,132 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 915, LBL 8.10. REPAIRED CHANNEL PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 53,150 hrs · 44,132 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 727E, BETWEEN STR 26L TO STR 27L. REPAIRED FRAME PER SRM.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 53,150 hrs · 44,132 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED BETWEEN BS 927 TO BS 947.5, LBL 3. REPAIRED CHANNEL PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,150 hrs · 44,132 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 24R. REMOVED AND REPLACED CLIP PER SRM.

Part: DOOR FRAME — CRACKED (CARGO DOOR) · airframe 53,150 hrs · 44,132 cycles

DURING SCHEDULED 16Y CHECK, FOUND FWD CARGO COMPARTMENT DOOR CRACKED ON LOWER LATERAL AFT FRAME AT BS 489.90. REPAIRED FRAME PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 53,150 hrs · 44,132 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986.5, RBL 43.5. REPAIRED BEAM PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 53,150 hrs · 44,132 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO COMPARTMENT FRAME CORRODED AT BS 727D, BETWEEN STR 26R TO STR 27R. REPAIRED FRAME PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 53,150 hrs · 44,132 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 727E, BETWEEN STR 25R TO STR 26R. REPAIRED FRAME PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 53,150 hrs · 44,132 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO COMPARTMENT SHEAR TIE CORRODED AT BS 986.5, BETWEEN STR 27R TO STR 27L. REMOVED AND REPLACED SHEAR TIE PER SRM AND BAC DWG.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 53,150 hrs · 44,132 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED BETWEEN BS 927 TO BS 845, RBL 8.10. REPAIRED CHANNEL PER EA.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 53,150 hrs · 44,132 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 772, RBL 3. REPAIRED CHANNEL PER EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 53,150 hrs · 44,132 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 727E, BETWEEN STR 25R TO STR 26R. REPAIRED FRAME PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 53,150 hrs · 44,132 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CRACKED AT BS 328, STR 20R. REMOVED AND REPLACED STRINGER PER SRM.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 53,150 hrs · 44,132 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 772, LBL 3. REPAIRED CHANNEL PER EA.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 53,150 hrs · 44,132 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 772, LBL 12.50. REPAIRED CHANNEL PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,150 hrs · 44,132 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 5L. REMOVED AND REPLACED CLIP PER SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,150 hrs · 44,132 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 2R. REMOVED AND REPLACED CLIP PER SI.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 53,150 hrs · 44,132 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT PRESSURE BULKHEAD WEB CRACKED AT BS 1016, STR 15R. REPAIRED WEB PER SRM.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 53,150 hrs · 44,132 cycles

DURING SCHEDULED 16Y CHECK, FOUND BRACKET CRACKED AT BS 706, STR 11R. REMOVED AND REPLACED BRACKET PER SRM AND DWG.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 53,150 hrs · 44,132 cycles

DURING SCHEDULED 16Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 727B, RBL 45.5. REPAIRED BEAM PER EO.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,150 hrs · 44,132 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 8R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,150 hrs · 44,132 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 559, STR 16L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,150 hrs · 44,132 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 10R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 53,150 hrs · 44,132 cycles

DURING SCHEDULED 16Y CHECK, FOUND CREASE BEAM WEB CORRODED BETWEEN BS 727B TO BS 727C, RBL 62.50. REMOVED AND REPLACED WEB PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,150 hrs · 44,132 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 1. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,150 hrs · 44,132 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 10L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: LENS — BROKEN (CABIN) · airframe 53,150 hrs · 44,132 cycles

DURING SCHEDULED 16Y CHECK, FOUND FWD GALLEY EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LENS PER MM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 53,150 hrs · 44,132 cycles

DURING SCHEDULED 16Y CHECK, FOUND VERTICAL ANGLE CRACKED AT BS 328, LBL 45. REMOVED AND REPLACED ANGLE PER SRM AND BAC DWG.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 63,541 hrs · 51,862 cycles

AFT PRESS BULKHEAD CRACKED AT BS 1016, STRINGER 15R. REPAIRED BULKHEAD IAW SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 52,662 hrs · 43,767 cycles

DURING SCHEDULED MV2 CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LAMP PER MM.

Part: SIGN — LOOSE (CABIN) · airframe 52,615 hrs · 43,733 cycles

FWD GALLEY EMERGENCY EXIT SIGN LOOSE. SECURED SIGN PER MM.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 52,384 hrs · 43,552 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT WING NR 2 SLAT UPPER T/E WEDGE DELAMINATED. REMOVED AND REPLACED NR 2 SLAT PER MM.

Part: FLAP — DELAMINATED (RT WING) · airframe 52,384 hrs · 43,552 cycles

DURING SCHEDULED HC2 CHECK, FOUND RIGHT WING I/B AFT FLAP O/B TRAILING EDGE DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,188 hrs · 43,404 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 1000, STR 5R. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,495 hrs · 48,207 cycles

SKIN CRACKED AT BS 1000, STR 5R. REPAIRED SKIN PER EA AND SRM.

Part: VALVE — FAULTY (LT MLG) · airframe 51,279 hrs · 42,737 cycles

ON APPROACH LOWERED GEAR AND GOT AN UNSAFE RED LEFT GEAR LIGHT AND NO GREEN LEFT FEAR LIGHT. RAISED GEAR AND MANUALLY LOWERED GEAR AND GOT THREE GREEN GEAR LIGHTS. REMOVED AND REPLACED LT MLG PRIORITY MODULAR VALVE PER MM.

Part: LOGIC CARD — FAULTY (E&E BAY) · airframe 51,194 hrs · 42,667 cycles

LEFT MLG UNSAFE LIGHT IND. CYCLED THE GEAR LEVER AND INDICATION LIGHT GREEN. REMOVED AND REPLACED M986 LANDING GEAR LOGIC CARD PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 51,048 hrs · 42,548 cycles

DURING SCHEDULED MV2 CHECK, FOUND R1 DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.

Part: COVER — CRACKED (CABIN) · airframe 50,865 hrs · 42,411 cycles

DURING SCHEDULED HC1 CHECK, FOUND EEPLS COVER CRACKED AT ROW 21. REMOVED AND REPLACED COVER PER MM.

Part: SLIDE — UNSERVICEABLE (R2 DOOR) · airframe 48,937 hrs · 41,036 cycles

DURING SCHEDULED 14Y CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE PRESSURE GAUGE NEEDLE IN THE RED. REMOVED AND REPLACED SLIDE PER MM.

Part: FLAP — DELAMINATED (LT WING) · airframe 49,113 hrs · 41,141 cycles

DURING SCHEDULED 14Y CHECK, FOUND LT WING O/B FORE FLAP DELAMINATED I/B AFT EDGE. REMOVED AND REPLACED FORE FLAP PER MM.

Part: SIGN — DAMAGED (CABIN) · airframe 49,113 hrs · 41,141 cycles

DURING SCHEDULED 14Y CHECK, FOUND FWD EMERGENCY EXIT SIGN DAMAGED. REMOVED AND REPLACED SIGN PER MM.

Part: SUPPORT BRACKET — CRACKED (NLG WW) · airframe 49,113 hrs · 41,141 cycles

DURING SCHEDULED 14Y CHECK, FOUND NLG ACTUATOR SUPPORT BRACKET CRACKED AT CEILING BS 259, LBL 1. REMOVED AND REPLACED BRACKET PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 49,113 hrs · 41,141 cycles

DURING SCHEDULED CHECK, FOUND STRINGER CRACKED AT BS 500A, STR 8R. REPAIRED BRACKET PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,113 hrs · 41,141 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 400, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,113 hrs · 41,141 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 520, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,113 hrs · 41,141 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 727D, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,113 hrs · 41,141 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 500C, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,113 hrs · 41,141 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 380, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,113 hrs · 41,141 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 727B, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,113 hrs · 41,141 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 480, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,113 hrs · 41,141 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 827, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,113 hrs · 41,141 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 480, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,113 hrs · 41,141 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 727B, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,113 hrs · 41,141 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 440, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,113 hrs · 41,141 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 727D, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,113 hrs · 41,141 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 440, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,113 hrs · 41,141 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 500C, STR 8R. REPAIRED FRAME PER SWA EA.

Part: LENS — OUT OF POSITION (CABIN) · airframe 48,530 hrs · 40,740 cycles

DURING SCHEDULED 14Y CHECK, FOUND LT OVERWING EMERGENCY EXIT SIGN LENS OUT OF POSITION. INSTALLED SIGN PER MM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 47,390 hrs · 39,898 cycles

R2 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 47,045 hrs · 39,652 cycles

R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 47,034 hrs · 39,643 cycles

R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,164 hrs · 38,982 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SWA EA.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 44,008 hrs · 37,318 cycles

DURING SCHEDULED HC1 CHECK, FOUND L1 DOOR EMRGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: COVER — MISSING (CABIN) · airframe 42,762 hrs · 36,379 cycles

FWD CABIN EMERGENCY EXIT SIGN COVER MISSING. REMOVED AND REPLACED EXIT SIGN PER MM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 42,357 hrs · 36,090 cycles

DURING SCHEDULED 12Y CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,011 hrs · 35,836 cycles

DURING SCHEDULED SPV CHECK, FOUND AFT CARGO DOOR CUTOUT FWD FRAME CRACKED AT NR 5 DOOR STOP. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: STRINGER — CRACKED (BS 794 S26R) · airframe 42,011 hrs · 35,836 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER 26R CRACKED AT BS 794. REMOVED AND REPLACED STRINGER SECTION PER SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 42,011 hrs · 35,836 cycles

DURING SCHEDULED SPV CHECK, FOUND FWD CARGO DOOR CUTOUT AFT FRAME CRACKED AT NR 5 DOOR STOP. REMOVED AND REPLACED FRAME SECTION PER ACO.

Part: SHAFT — BROKEN (VBV MOTOR) · airframe 41,885 hrs · 35,734 cycles

WHILE CLIMBING OUT OF PHX ABOVE FL 250, NR 1 ENGINE WAS UNABLE TO REACH CLIMB N1 POWER SETTING WITH PMC OFF. THROTTLE WAS ALL THE WAY TO FWD STOP. REMOVED AND REPLACED BROKEN VBV MOTOR MAIN SHAFT PER MM.

Part: BATTERY — FAULTY (EMERGENCY LIGHT) · airframe 41,554 hrs · 35,458 cycles

DURING SCHEDULED MV1 CHECK, FOUND AFT CABIN EMERGENCY EXIT LIGHTS WILL NOT EXTINGUISH. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 41,280 hrs · 35,239 cycles

DURING SCHEDULED C2 CHECK, FOUND AFT CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY CHARGING BASE PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 41,280 hrs · 35,239 cycles

DURING SCHEDULED C2 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 41,202 hrs · 35,183 cycles

AFT CABIN LT EMERGENCY EXIT LIGHT FLICKERS. R&R BATTERY AND BATTERY CHARGER PER MM.

Part: CABLE — MISROUTED (SLIDE GIRT BAR) · airframe 35,315 hrs · 30,614 cycles

DURING SCHEDULED RON, FOUND L2 AND R2 DOOR EVAC SLIDE GIRT BAR CABLES MISROUTED. REROUTED CABLES PER MM.

Part: SLIDE — DISLODGED (L1 DOOR) · airframe 34,877 hrs · 30,263 cycles

L1 DOOR EVAC SLIDE FELL OUT, DID NOT DEPLOY. REINSTALLED L1 DOOR EVAC SLIDE PER MM.

Part: SLIDE — DISLODGED (L1 DOOR) · airframe 34,808 hrs · 30,211 cycles

L1 DOOR EVAC SLIDE FELL OUT, DID NOT DEPLOY. REINSTALLED L1 DOOR EVAC SLIDE PER MM.

Part: FITTING — CORRODED (VERTICAL STAB) · airframe 34,077 hrs · 29,629 cycles

DURING SCHEDULED D-CHECK, FOUND VERTICAL STAB FWD AND AFT BODY LUG FACE CORRODED. REPAIRED VERTICAL STAB PER ER.

Part: LAMP — INOPERATIVE (FUSELAGE) · airframe 34,077 hrs · 29,629 cycles

DURING SCHEDULED D-CHECK, FOUND RT AFT SERVICE DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 34,076 hrs · 29,628 cycles

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM AT BS 947.5, LBL 53.52, CRACKED. REPAIRED FLOORBEAM CHORD PER ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,076 hrs · 29,628 cycles

DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 348, LBL 60, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 34,076 hrs · 29,628 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN AT NR 1 COCKPIT WINDOW OUTBOARD UPPER CORNER, CRACKED. REPAIRED SKIN PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,076 hrs · 29,628 cycles

DURING SCHEDULED D-CHECK, FOUND FRAME CHORD AT RIGHT BS 616, WL 208, CRACKED. REPAIRED FRAME CHORD PER ER.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 34,076 hrs · 29,628 cycles

DURING SCHEDULED D-CHECK, FOUND CREASE BEAM AT BS 580, RBL 65, CRACKED. REMOVED AND REPLACED CREASE BEAM SECTION PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 34,076 hrs · 29,628 cycles

DURING SCHEDULED D-CHECK, FOUND SHEAR TIE AT BS 787, BETWEEN STRINGER 26R AND STRINGER 27R, CORRODED. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 34,076 hrs · 29,628 cycles

DURING SCHEDULED D-CHECK, FOUND FRAME WEB AT BS 986 TO BS 992, RBL 46, CORRODED. REMOVED AND REPLACED FRAME WEB SECTION PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 34,076 hrs · 29,628 cycles

DURING SCHEDULED D-CHECK, FOUND CREASE BEAMS AT BS 360 TO BS 380, RBL 70.5, BS 500 TO BS 500A, RBL 70.5, CORRODED. REMOVED AND REPLACED CREASE BEAM SECTIONS PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 34,076 hrs · 29,628 cycles

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM AT BS 294.5, RBL 45 TO RBL 51, CORRODED. REMOVED AND REPLACED FLOORBEAM SECTION PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 34,076 hrs · 29,628 cycles

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM AT BS 328, RBL 55 TO LBL 51, BS 344, LBL 55 TO BL 0, CORRODED. REMOVED AND REPLACED FLOORBEAM CHORDS PER SRM.

Part: FITTING — CORRODED (L1 DOOR GIRT BAR) · airframe 34,076 hrs · 29,628 cycles

DURING SCHEDULED D-CHECK, FOUND L1 DOOR EVAC SLIDE GIRT BAR FWD AND AFT MOUNT FITTINGS, CORRODED. REMOVED AND REPLACED L1 DOOR EVAC SLIDE GIRT BAR MOUNT FITTINGS PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 34,076 hrs · 29,627 cycles

DURING SCHEDULED D-CHECK, FOUND CREASE BEAM WEB AT BS 967 TO BS 986.5, RBL 49, CORRODED. REMOVED AND REPLACED CREASE BEAM WEB SECTION PER SRM.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 34,076 hrs · 29,628 cycles

DURING SCHEDULED D-CHECK, FOUND ZEE AT BS 270, BBL 11 TO LBL 11, CORRODED. REMOVED AND REPLACED ZEE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,076 hrs · 29,628 cycles

DURING SCHEDULED D-CHECK, FOUND FRAMES AT BS 747, STRINGER 8R AND STRINGER 8L, CRACKED. REMOVED AND REPLACED FRAME SECTIONS PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,076 hrs · 29,628 cycles

DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 360, STRINGER 8R, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,076 hrs · 29,628 cycles

DURING SCHEDULED D-CHECK, FOUND FRAMES AT BS 907, BS 867, BS 827, BS, 787, STRINGER 8L, BS 907, BS 867, BS 787, STRINGER 8R, CRACKED. REMOVED AND REPLACED FRAME SECTIONS PER SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 34,076 hrs · 29,628 cycles

DURING SCHEDULED D-CHECK, FOUND DOOR FRAME AT BS 303, STRINGER 16L, CRACKED. REPAIRED DOOR FRAME SECTION PER SB.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 34,076 hrs · 29,628 cycles

DURING SCHEDULED D-CHECK, FOUND CREASE BEAM WEB AT BS 872, RBL 60 TO RBL 67, CORRODED. REMOVED AND REPLACED CREASE BEAM WEB SECTION PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,076 hrs · 29,628 cycles

DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 400, STRINGER 8R, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 34,076 hrs · 29,628 cycles

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM AT BS 986.5, LBL 44, CORRODED. REMOVED AND REPLACED FLOORBEAM SECTION PER SRM.

Part: FLOOR PANEL — CRACKED (FUSELAGE) · airframe 34,076 hrs · 29,628 cycles

DURING SCHEDULED D-CHECK, FOUND FLOOR WEB AT RIGHT BS 188 TO RIGHT BS 196, WL 208, CRACKED. REMOVED AND REPLACED FLOOR WEB SECTION PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,076 hrs · 29,628 cycles

DURING SCHEDULED D-CHECK, FOUND FRAME AT RT BS 188, WL 208, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: BUSHING — WORN (RT ELEVATOR) · airframe 33,333 hrs · 29,019 cycles

ACFT VIBRATION FELT ABOVE 250 KNOTS. REMOVED AND REPLACED RT ELEVATOR TAB INBD HINGE ATTACH BUSHING AND BOLT PER MM.

Part: COVER — BROKEN (EMERGENCY LIGHT) · airframe 33,227 hrs · 28,938 cycles

DURING SCHEDULED A2 CHECK, FOUND EMERGENCY EXIT LIGHT COVER BROKEN AT ROW 11DEF. REMOVED AND REPLACED EMERGENCY EXIT LIGHT COVER PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 32,867 hrs · 28,650 cycles

DURING SCHEDULED C1 CHECK, FOUND L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM.

Part: LENS — MISSING (EMERGENCY SIGN) · airframe 32,867 hrs · 28,650 cycles

DURING SCHEDULED C1 CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT LENS MISSING. REPLACED LIGHT LENS PER MM.

Part: LIGHT — FAULTY (CABIN) · airframe 32,397 hrs · 28,290 cycles

EMERGENCY LIGHTS ILLUMINATED. REMOVED AND REPLACED LT AFT CABIN EMERGENCY LIGHT BASE PER MM.

Part: GIRT BAR — OUT OF ADJUST (ESCAPE SLIDE) · airframe 31,839 hrs · 27,831 cycles

DURING SCHEDULED C4 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: BUSHING — WORN (RT HORIZ STAB) · airframe 28,157 hrs · 24,905 cycles

DURING SCHEDULED C4 CHECK, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED HARDWARE AND BUSHING ON NR 1 TAB HINGE ATTACH POINT PER MM.

Part: FUSE — MALFUNCTIONED (HYD SYSTEM) · airframe 27,778 hrs · 24,593 cycles

AIR TURN BACK, AFTER TAKEOFF, LEADING EDGE DEVICES FAILED TO RETRACT. RESET B-SYSTEM L/E DEVICE HYD FUSES PER MM. OPS CK GOOD PER MM.

Part: PCU — LEAKING (LT MLG W/W) · airframe 26,861 hrs · 23,852 cycles

DECLARED EMERGENCY, DURING FLIGHT A HYD SYSTEM QTY DROPPED TO ONE-QUARTER WITH ASSOCIATED LOW PRESS LIGHT ILLUMINATED. TIGHTENED BOTTOM FLEX LINE ON AILERON PCU PER MM

Part: LANYARD — BROKEN (EVAC SLIDE) · airframe 26,559 hrs · 23,606 cycles

FWD ENTRY DOOR EMERGENCY EVAC SLIDE LANYARD CHAIN BROKEN. REMOVED AND REPLACED SLIDE PER MM.

Part: WEB — CRACKED (FUSELAGE) · airframe 25,855 hrs · 23,024 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BULKHEAD WEB CRACKED (2 EA) AT BS 178, LBL 5.4, WL 198 AND WL 201. REPAIRED WEB PER SRM.

Part: FLOORBEAM — CORRODED (FWD CARGO) · airframe 25,855 hrs · 23,024 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM CORRODED BETWEEN BS 500C PLUS 3 TO 500C PLUS 18, LBL 18. REMOVED AND REPLACED FLOORBEAM SECTION PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 25,855 hrs · 23,024 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BULKHEAD WEB CRACKED AT BS 178, RBL 5.4 7 WL 201. REPAIRED WEB PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 25,855 hrs · 23,024 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT SIDE OF EQUIPTMENT COOLING EXHAUST CUT OUT. REPAIRED SKIN PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 25,855 hrs · 23,024 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BULKHEAD WEB CRACKED (2 EA) AT BS 178, RBL 5.4, WL 201 AND WL 198. REPAIRED WEB PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,314 hrs · 22,601 cycles

DURING SERVICE CHECK, FOUND SEVERAL EEPLS LIGHTS INOP. REMOVED AND REPLACED EEPLS LIGHT ASSY'S PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 24,969 hrs · 22,269 cycles

EEPLS LOOSE AT MID CABIN. SECURED EEPLS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,856 hrs · 22,203 cycles

EEPLS INOP AT SEVERAL LOCATIONS IN CABIN. RELAMPED AND SECURED WIRING PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 24,293 hrs · 21,734 cycles

EEPLS LOOSE AT MID CABIN. REMOVED AND REPLACED EEPLS LIGHT ASSY PER MM.

Part: COVER — LOOSE (CABIN FLOOR) · airframe 24,166 hrs · 21,626 cycles

EEPLS COVER LOOSE AT AFT CABIN. SECURED COVER PER MM.

Part: WIRE — DISCONNECTED (CABIN) · airframe 23,903 hrs · 21,404 cycles

EEPLS INOP BETWEEN ROW 14 & ROW 12. RECONNECTED EEPLS WIRES PER MM.

Part: LENS — CRACKED (SERVICE DOOR) · airframe 23,611 hrs · 21,169 cycles

DURING SCHEDULED C3 CHECK, FOUND FWD SVC DOOR EMERGENCY EXIT LIGHT LENS CRACKED. R&R LIGHT LENS PER MM.

Part: PUMP — OVERHEATED (HYD SYSTEM) · airframe 23,372 hrs · 20,988 cycles

AIR TURNBACK. A SYSTEM HYD ELECTRIC PUMP OVERHEAT LIGHT ILLUMINATED. REMOVED AND REPLACED A HYD PUMP AND ELECTRICAL CONNECTOR PER MM. OPS CHECK GOOD.

Part: LIGHT — LOOSE (CABIN) · airframe 22,857 hrs · 20,576 cycles

EEPLS LOOSE AT MID CABIN. SECURED EEPLS PER MM.

Part: WIRE — BROKEN (CABIN) · airframe 22,664 hrs · 20,422 cycles

EEPLS WIRING BROKEN NEAR EMERGENCY EXIT ROW. REPAIRED WIRING PER MM.

Part: COVER — MISSING (CABIN) · airframe 22,664 hrs · 20,422 cycles

EEPLS TRACK COVER MISSING AT ROW 12. REPLACED TRACK COVER PER MM.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 22,553 hrs · 20,333 cycles

DURING SCHEDULED C2 CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED FLAP ASSY PER MM.

Part: COVER — MISSING (CABIN) · airframe 22,134 hrs · 19,979 cycles

EEPLS TRACK COVER MISSING AT MID CABIN. INSTALLED TRACK COVER PER MM.

Part: CABLE — MISROUTED (ESCAPE SLIDE) · airframe 21,596 hrs · 19,542 cycles

DURING SCHEDULED C1 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE CABLE MIS-ROUTED. ROUTED AFT SVC DOOR SLIDE CABLE PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 21,218 hrs · 19,219 cycles

EEPLS LOOSE AT ROW 15. RESECURED LIGHT ASSY PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 21,177 hrs · 19,184 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BS 178 BULKHEAD LT CHORD CRACKED, WL 207. REMOVED AND REPLACED CHORD SECTION PER ACO.

Part: WIRE — EXPOSED (CABIN) · airframe 20,512 hrs · 18,627 cycles

EEPLS HAS EXPOSED WIRING AT ROW 13. RESECURED LIGHT ASSY PER MM.

Part: SLIDE — DEPLOYED (PAX DOOR) · airframe 20,376 hrs · 18,507 cycles

FWD ENTRY DOOR EVACUATION SLIDE INADVERTENTLY DEPLOYED. REMOVED AND REPLACED SLIDE ASSY PER MM.

Part: WIRE — EXPOSED (CABIN)

EEPLS WIRING EXPOSED AT ROW 11. SECURED WIRING PER MM.

Part: WARNING SYS — ACTIVATED (COCKPIT)

ABORTED TAKEOFF, TAKEOFF WARNING HORN SOUNDED AND COULD NOT SILENCED BY CYCLING SPEED BRAKE HANDLE. SILENCED TAKEOFF WARNING HORN AFTER CYCLING FLAPS. UNABLE TO DUPLICATED WARNING INDICATION. NO DEFECTS NOTED.

Part: BUSHING — WORN (ELEVATOR TAB)

AIR TURNBACK, AIRFRAME VIBRATION DURING CLIMB. VIBRATION GREATER AT HIGHER SPEEDS. REMOVED AND REPLACED RT ELEVATOR OUTBOARD TAB HINGE BUSHINGS AND LT ELEVATOR INBOARD TAB HINGE BUSHINGS PER MM.

Part: LENS — BROKEN (SERVICE DOOR)

DURING SCHEDULED SERVICE CHECK, FOUND FWD SERVICE DOOR EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LENS ASSY PER MM.

Part: WIRE — LOOSE (ROW 1-4)

EEPLS INOP AT ROWS 1-4. RECONNECTED WIRING AND REPLACED LIGHTS AND MOLDING PER MM.

Part: WINDOW — LEAKING (COCKPIT)

AIR TURNBACK, AFTER REMOVED AND REPLACED NR 1 F/O WINDOW, TEMPORARY SPEED TAPE CAME LOOSE INFLIGHT (SPEED TAPE OK'D PER MX NOTE TX NR 23483). CLEANED SEALANT, RESEALED AND CURED PER MM.

Part: LIGHT — INOP (CABIN)

EMERGENCY ESCAPE FLOOR TRACK LIGHT INOP AT MID CABIN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SLIDE — DETACHED (PAX DOOR)

EMERGENCY ESCAPE SLIDE CAME OUT OF COVER ON FWD ENTRY DOOR (DID NOT DEPLOY, JUST CAME OUT OF BRACKET). REINSTALLED SLIDE ASSY PER MM.

Part: LIGHT — INOPERATIVE (CABIN)

DURING WALKAROUND CHECK, FOUND LOWER AFT EMERGENCY FLASHLIGHT INOP. REPLACED BATTERY PER BOEING MM.

Part: SKIN — DENTED (BS 967)

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN DENTED BELOW AFT ENTRY DOOR AT BS 967. REPAIRED PER BOEING SRM.