N392SW

Part: SIGN — LOOSE (EMERGENCY LIGHTS) · airframe 69,669 hrs · 56,168 cycles

RIGHT EMERGENCY EXIT SIGN LOOSE. SECURED THE SIGN IAW SIP.

Part: SLAT — DELAMINATED (LT WING) · airframe 69,240 hrs · 55,888 cycles

LEFT WING NR 2 SLAT UPPER OTBD L/E DELAMINATED. R & R NR 2 SLAT ASSY IAW AMM.

Part: SKIN — CRACKED (LE SLAT) · airframe 68,880 hrs · 55,629 cycles

LEFT WING NR 1 SLAT SKIN CRACKED AT LOWER AFT FASTENER ROW. R & R SLAT IAW MM.

Part: LOCK RING — MISSING (EMERGENCY EXIT) · airframe 68,880 hrs · 55,629 cycles

LEFT EMERGENCY EXIT HATCH FWD UPPER STOP MISSING LOCK RING. INSTALLED LOCK RING IAW AMM.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 68,864 hrs · 55,620 cycles

CEILING EMERGENCY EXIT LIGHT INOPERATIVE AT BS 616. INSTALLED D2978 CONNECTOR IAW AMM.

Part: CABLE — BROKEN (CABIN) · airframe 68,864 hrs · 55,620 cycles

AFT GALLEY LAVATORY B EMERGENCY EXIT LIGHT CABLE BROKEN. REPAIRED CABLE IAW AMM.

Part: FITTING — CORRODED (RT WING) · airframe 68,864 hrs · 55,620 cycles

RIGHT WING NR 5 FLAP TRACK, FORWARD SUPPORT FITTING, CORRODED ON BORE OF ATTACH FITTING ON MLG SUPPORT BEAM. REPAIRED FITTING IAW EA.

Part: FAIRING — CRACKED (TE FLAP) · airframe 68,864 hrs · 55,620 cycles

RIGHT WING NR 8 FLAP TRACK AFT FAIRING CRACKED. REPAIRED FAIRING IAW SRM.

Part: SKIN — CORRODED (RT WING) · airframe 68,864 hrs · 55,620 cycles

RIGHT WING UPPER SKIN CORRODED, BETWEEN WBL 70.5 & WBL 92.50 AT 19" AFT OF FORWARD EDGE SKIN PANEL. REPAIRED SKIN IAW EA.

Part: REVEAL — CRACKED (FUSELAGE) · airframe 68,864 hrs · 55,620 cycles

L2 DOOR CORNER REVEAL CRACKED AT BS 951, BETWEEN STRINGER 17L - 16L. R & R REVEAL IAW SRM & DWG.

Part: SPAR — CRACKED (LT WING) · airframe 68,864 hrs · 55,620 cycles

LEFT WING REAR SPAR WEB CRACKED, BETWEEN RSS 222 - 223. R & R WEB IAW SRM & DWG.

Part: SKIN — CRACKED (LT WING) · airframe 68,864 hrs · 55,620 cycles

LEFT WING INSPAR UPPER SKIN TE CRACKED AT RSS 268.0. REPAIRED SKIN IAW EA.

Part: SPLICE — CRACKED (RT WING) · airframe 68,864 hrs · 55,620 cycles

RIGHT WING REAR SPAR WEB SPLICE CRACKED IN FASTENER HOLE ON REAR SPAR RSS 223. REPAIRED SPLICE IAW EA.

Part: COVER — CRACKED (L1 DOOR) · airframe 68,864 hrs · 55,620 cycles

L1 DOOR ESCAPE SLIDE COVER CRACKED. REPAIRED COVER IAW EA.

Part: SKIN — CRACKED (RT WING) · airframe 68,864 hrs · 55,620 cycles

RIGHT WING UPPER SKIN ON REAR SPAR RSS 270 CRACKED. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (LT WING) · airframe 68,864 hrs · 55,620 cycles

LEFT WING INSPAR UPPER SKIN TE CRACKED AT RSS 267.0. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (RT WING) · airframe 68,864 hrs · 55,620 cycles

RIGHT WING UPPER SKIN ON REAR SPAR RSS 239 CRACKED. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (LT WING) · airframe 68,864 hrs · 55,620 cycles

LEFT WING INSPAR UPPER SKIN TE CRACKED AT RSS 251.5. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (LT WING) · airframe 68,864 hrs · 55,620 cycles

LEFT WING INSPAR UPPER SKIN TE CRACKED AT RSS 240. REPAIRED SKIN IAW EA.

Part: SPLICE — CRACKED (LT WING) · airframe 68,864 hrs · 55,620 cycles

LEFT WING REAR SPAR WEB SPLICE CRACKED AT RSS 223. REPAIRED SPLICE IAW EA.

Part: SUPPORT FITTING — CRACKED (RT WING) · airframe 68,864 hrs · 55,620 cycles

RIGHT WING AFT SUPPORT FITTING FASTENER HOLE CRACKED ON REAR SPAR AT RSS 222.5. R & R FITTING IAW SRM & DWG.

Part: LINK ASSY — CORRODED (RT MLG) · airframe 68,864 hrs · 55,620 cycles

RIGHT MLG SWING LINK HOLES CORRODED. REPAIRED SWING LINK IAW CMM.

Part: SUPPORT FITTING — CORRODED (TE FLAP) · airframe 68,864 hrs · 55,620 cycles

LEFT WING NR 4 INBD FLAP TRACK, FORWARD SUPPORT FITTING CORRODED AT WBL 66.5. REPAIRED FITTING IAW EA.

Part: LINK ASSY — CORRODED (LT MLG) · airframe 68,864 hrs · 55,620 cycles

LEFT MLG SWING LINK CORRODED ON HOLES. REPAIRED SWING LINK IAW CMM.

Part: FITTING — CRACKED (TE FLAP) · airframe 68,864 hrs · 55,620 cycles

LEFT WING NR 3 FAIRING INBD FLAP, OTBD TRACK INTERFACE FITTING CRACKED. R & R FITTING IAW SRM & DWG.

Part: ANGLE — CRACKED (TE FLAP) · airframe 68,864 hrs · 55,620 cycles

LEFT WING ANGLE CRACKED OTBD SIDE ON INBD FLAP OUTBOARD TRACK FAIRING 3 AT LEVEL OF WBL 198.6. R & R ANGLE IAW SRM & DWG.

Part: ANGLE — CRACKED (TE FLAP) · airframe 68,864 hrs · 55,620 cycles

RIGHT WING NR 6 FAIRING INBD FLAP, OTBD TRACK ANGLE CRACKED AT LEVEL OF WBL 198.6. R & R ANGLE IAW SRM & DWG.

Part: BRACKET — CRACKED (LT WING) · airframe 68,864 hrs · 55,620 cycles

LEFT WING PULLEY BRACKET CRACKED AT RSS 230.00. R & R BRACKET IAW SRM & DWG.

Part: SPLICE — CRACKED (RT WING) · airframe 68,864 hrs · 55,620 cycles

RIGHT WING REAR SPAR UPPER CHORD SPLICE CRACKED ON FASTENER HOLE AT RSS 222.5. REPAIRED CHORD IAW EA.

Part: SPLICE — CRACKED (LT WING) · airframe 68,864 hrs · 55,620 cycles

LEFT WING REAR SPAR UPPER CHORD SPLICED CRACKED AT RSS 222.5. REPAIRED SPLICE IAW EA.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 68,864 hrs · 55,620 cycles

FORWARD GALLEY DOOR INTERCOSTAL CRACKED AT BS 277, STRINGER 14R. REPAIRED INTERCOSTAL IAW EA.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 68,864 hrs · 55,620 cycles

FORWARD GALLEY DOOR INTERCOSTAL WEB CRACKED AT BS 277, STRINGER 14R. REPAIRED INTERCOSTAL IAW EA.

Part: FITTING — CRACKED (RT HORIZ STAB) · airframe 68,864 hrs · 55,620 cycles

RIGHT HORIZONTAL STABILIZER CTR SECTION IN TAIL COMPARTMENT, UPPER FITTING CRACKED AT BS 1121. R & R FITTING IAW SRM & DWG.

Part: PLATE — CRACKED (FUSELAGE) · airframe 68,864 hrs · 55,620 cycles

AFT CARGO COMPARTMENT FRAME PLATE CRACKED AT BS 794.3, STRINGER 25R. R & R PLATE IAW SRM & DWG.

Part: FLAP — DELAMINATED (LT WING) · airframe 68,864 hrs · 55,620 cycles

LEFT WING INBD AFT FLAP DELAMINATED. REPAIRED AFT FLAP IAW SRM.

Part: FITTING — CRACKED (LT WING) · airframe 68,864 hrs · 55,620 cycles

LEFT WING NR 4 SPOILER ACTUATOR INBD FITTING CRACKED. R & R FITTING IAW SRM & DWG.

Part: STIFFENER — CRACKED (TE FLAP) · airframe 68,864 hrs · 55,620 cycles

RIGHT WING NR 6 FAIRING INBD FLAP, OTBD TRACK CRACKED ON STIFFENER ON INTERNAL AREA AT WBL 183.40. R & R STIFFENER IAW SRM & DWG.

Part: SUPPORT ANGLE — CRACKED (RT WING) · airframe 68,864 hrs · 55,620 cycles

RIGHT WING TE SUPPORT ANGLE CRACKED ON WBL 92.5. REPAIRED ANGLE IAW EA.

Part: PLATE — CORRODED (R2 DOOR) · airframe 68,864 hrs · 55,620 cycles

R2 DOOR EMERGENCY EVAC SLIDE FLOOR MOUNTED PLATE ASSEMBLY ADAPTER CORRODED. R & R PLATE ASSEMBLY IAW AMM.

Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 68,864 hrs · 55,620 cycles

FORWARD GALLEY AREA SUPPORT FITTING CRACKED AT BS 348, STRINGER 16L. R & R FITTING IAW SRM & DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 68,864 hrs · 55,620 cycles

FUSELAGE FWD DOORWAY INTERCOSTAL CRACKED AT BS 277, STRINGER 10R. REPAIRED INTERCOSTAL IAW EA.

Part: FITTING — CRACKED (FUSELAGE) · airframe 68,864 hrs · 55,620 cycles

FORWARD ENTRY DOOR ANGLE CLIP CRACKED AT BS 312, STRINGER 8L. R & R CLIP IAW SRM & DWG.

Part: ANGLE — CRACKED (LT WING) · airframe 68,864 hrs · 55,620 cycles

LEFT WING ANGLE CRACKED INTERNAL CAVITY ON TE RSS 546. R & R ANGLE IAW SRM & DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 68,864 hrs · 55,620 cycles

LEFT MLG ANGLE CRACKED AT BS 695, CUT OUT AT LOWER FUSELAGE. R & R ANGLE IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,864 hrs · 55,620 cycles

SKIN CRACKED AT BS 951.5, BETWEEN STRINGER 15L - 16L. REPAIRED SKIN IAW EA.

Part: ANGLE — CRACKED (LT WING) · airframe 68,864 hrs · 55,620 cycles

LEFT WING TE ANGLE CRACKED ON WBL 184. R & R ANGLE IAW SRM & DWG.

Part: SKIN — DELAMINATED (FUSELAGE) · airframe 68,864 hrs · 55,620 cycles

TAIL CONE FUSELAGE SKIN DELAMINATED AT BS 1156+21, LBL 13. REPAIRED SKIN IAW SRM.

Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 68,864 hrs · 55,620 cycles

FORWARD GALLEY AREA SUPPORT CLIP CRACKED AT BS 348.20, STRINGER 11L. R & R CLIP IAW SRM & DWG.

Part: LENS — BROKEN (CABIN) · airframe 68,864 hrs · 55,620 cycles

AFT GALLEY AREA EMER EXIT LENS BROKEN. R & R LENS IAW AMM.

Part: LENS — BROKEN (CABIN) · airframe 68,864 hrs · 55,620 cycles

FORWARD GALLEY AREA LAVATORY EMER EXIT LIGHT LENS BROKEN. R & R LENS IAW AMM.

Part: FLASHLIGHT — BROKEN (CABIN) · airframe 68,864 hrs · 55,620 cycles

FORWARD GALLEY EMER FLASHLIGHT BASE BROKEN. R & R FLASHLIGHT ASSEMBLY IAW CMM.

Part: STRAP — BROKEN (FLASHLIGHT) · airframe 68,864 hrs · 55,620 cycles

AFT LT LAVATORY FLASHLIGHT STRAP BROKEN. R & R STRAP IAW CMM.

Part: GLOWSTRIP — DETERIORATED (CABIN) · airframe 68,864 hrs · 55,620 cycles

LEFT PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING STRIP DETERIORATED. R & R STRIP IAW AMM & DWG.

Part: LATCH — CRACKED (CARGO DOOR) · airframe 68,864 hrs · 55,620 cycles

RIGHT AFT CARGO COMPARTMENT, DOOR CHANNEL LATCH CRACKED, BETWEEN BS 787 - 807. REPAIRED LATCH IAW EA.

Part: GLOWSTRIP — DETERIORATED (CABIN) · airframe 68,864 hrs · 55,620 cycles

RIGHT PHOTO LUMINESCENT FLOOR PROXIMITY LIGHTING STRIP DETERIORATED. R & R STRIP IAW AMM & DWG.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 68,864 hrs · 55,620 cycles

AFT CARGO COMPARTMENT CHANNEL CRACKED BETWEEN BS 847 - 867, STRINGER 25R. R & R CHANNEL IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 68,864 hrs · 55,620 cycles

FRAME CRACKED AT BS 500B, BETWEEN STRINGER 20R - 21R. REPAIRED FRAME IAW EA.

Part: COVER — CRACKED (R1 DOOR) · airframe 68,864 hrs · 55,620 cycles

R1 DOOR EMER EVAC SLIDE COVER CRACKED. REPAIRED COVER IAW EA.

Part: LUG — BROKEN (LT SPOILER) · airframe 68,023 hrs · 55,084 cycles

LEFT WING INBD GND SPOILER LUG BROKEN. R & R SPOILER ASSEMBLY IAW MM.

Part: SKIN — CRACKED (L1 DOOR) · airframe 67,202 hrs · 54,507 cycles

L1 DOOR INTERIOR SKIN, JUST BELOW DOOR TORQUE TUBE CUT OUT FWD SIDE CRACKED. REPAIRED SKIN IAW EA.

Part: STRAP — CRACKED (FUSELAGE) · airframe 67,202 hrs · 54,507 cycles

FLOORBEAM WEB STRAP CRACKED AT BS 312. REPAIRED STRAP IAW SRM.

Part: COVER — BROKEN (CABIN) · airframe 66,206 hrs · 53,775 cycles

L1 BULKHEAD EMER EXIT LIGHT COVER BROKEN. R & R COVER IAW MM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 65,495 hrs · 53,279 cycles

RIGHT WING OTBD AFT FLAP DELAMINATED ON LOWER & UPPER SKIN JUST OTBD OF NR 7. R & R AFT FLAP IAW MM.

Part: SLIDE — LOW PRESSURE (L2 DOOR) · airframe 63,835 hrs · 52,129 cycles

L2 DOOR EMER EVAC SLIDE PRESS LOW. R & R SLIDE IAW MT.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 63,488 hrs · 51,885 cycles

Z ANGLE CRACKED BELOW L1 DOOR THRESHOLD PLATE. R & R ANGLE IAW SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 63,488 hrs · 51,885 cycles

L1 DOOR UPPER CUT OUT WEB CRACKED AT BS 338. R & R WEB IAW SRM & DWG.

Part: ACCESS PANEL — CRACKED (VERTICAL STAB) · airframe 63,488 hrs · 51,885 cycles

VERTICAL STABILIZER RETAINER PLATE ACCESS PANEL 9502 CRACKED. R & R PANEL IAW SRM & DWG.

Part: SUPPORT ANGLE — CRACKED (TE FLAP) · airframe 63,488 hrs · 51,885 cycles

RIGHT WING NR 6 FLAP TRACK FAIRING SUPPORT ANGLE CRACKED AT INBD UPPER SIDE INTERNAL AREA. REPAIRED ANGLE IAW SRM & DWG.

Part: STIFFENER — CRACKED (TE FLAP) · airframe 63,488 hrs · 51,885 cycles

LEFT WING NR 3 FLAP TRACK FAIRING STIFFENER CRACKED ON INBD LOWER SIDE. R & R STIFFENER IAW SRM & DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 63,488 hrs · 51,885 cycles

VERTICAL ANGLE CRACKED AT BS 328, RBL 38. R & R ANGLE IAW SRM & DWG.

Part: CROSSBEAM — CRACKED (CARGO DOOR) · airframe 63,488 hrs · 51,885 cycles

AFT CARGO DOOR FWD END OF THE CROSSBEAM E T CHORD CRACKED. REPAIRED E T CHORD IAW EO & EA.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 63,488 hrs · 51,885 cycles

TIE CLIP CRACKED AT BS 380, STRINGER 26R. R & R TIE CLIP IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 63,488 hrs · 51,885 cycles

TIE CLIP CRACKED AT BS 380, STRINGER 22L. R & R TIE CLIP IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,488 hrs · 51,885 cycles

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

Part: DUCT — CRACKED (FUSELAGE) · airframe 63,488 hrs · 51,885 cycles

DUCT ASSEMBLY CRACKED BETWEEN BS 294.5 TO 312, BETWEEN STRINGER 26R TO 26L. REPAIRED DUCT ASSEMBLY IAW EA.

Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 63,488 hrs · 51,885 cycles

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

Part: ANGLE — CRACKED (FUSELAGE) · airframe 63,488 hrs · 51,885 cycles

ANGLE CRACKED BETWEEN BS 294.5 TO 312, STRINGER 26L. R & R ANGLE IAW SRM & DWG.

Part: RIB — CRACKED (RT WING) · airframe 63,488 hrs · 51,885 cycles

RIGHT WING IN SPAR RIB WEB CRACKED AT WBL 198.60 AT LEVEL OF S 5. REPAIRED WEB IAW EA.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 63,488 hrs · 51,885 cycles

ANGLE CRACKED BETWEEN BS 887 TO 907, RBL 44. R & R ANGLE IAW SRM & DWG.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 63,488 hrs · 51,885 cycles

FLOOR SUPPORT CHANNEL CRACKED AT STATION 787 TO 807, RBL 18. R & R CHANNEL IAW SRM.

Part: RIB — CRACKED (RT WING) · airframe 63,488 hrs · 51,885 cycles

RIGHT WING RIB CRACKED AT STATION 135.5, BETWEEN STRINGER 2 & 3. REPAIRED RIB IAW EA.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 63,488 hrs · 51,885 cycles

ANGLE CRACKED AT BS 540, RT WING BODY FAIRING INTERNAL AREA. R & R ANGLE IAW SRM.

Part: RIB — CRACKED (RT WING) · airframe 63,488 hrs · 51,885 cycles

RIGHT WING RIB CRACKED AT STATION 114, BETWEEN STRINGER 2 & 3. REPAIRED RIB IAW EA.

Part: WEB — CRACKED (FUSELAGE) · airframe 63,488 hrs · 51,885 cycles

WEB CRACKED BETWEEN BS 947.5 TO 967, LBL 23. R & R WEB IAW SRM & DWG.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 63,488 hrs · 51,885 cycles

LONGITUDINAL FLOORBEAM CRACKED AT STATION 666, LBL 24.8. REPAIRED BEAM IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,488 hrs · 51,885 cycles

FRAME CRACKED AT BS 520, BETWEEN STRINGER 20R TO 21R. REPAIRED FRAME IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,488 hrs · 51,885 cycles

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

Part: SKIN — DELAMINATED (TAILCONE) · airframe 63,488 hrs · 51,885 cycles

TAIL CONE LOWER AREA SKIN DELAMINATED AT BS 1180, BL 0. REPAIRED SKIN IAW SRM.

Part: DOOR FRAME — CRACKED (GALLEY DOOR) · airframe 63,488 hrs · 51,885 cycles

FORWARD GALLEY DOOR AFT FRAME CRACKED AT BS 329, 14" FROM UPPER EDGE. REPAIRED FRAME IAW EO & EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 63,488 hrs · 51,885 cycles

FUSELAGE FRAME CORRODED AT STATION 500D, STRINGER 28L TO 28R. REPAIRED FRAME IAW SRM.

Part: STRAP — CRACKED (FUSELAGE) · airframe 63,488 hrs · 51,885 cycles

STRAP CRACKED BETWEEN BS 312 TO BS 344, LBL 45.6. R & R STRAP IAW SRM & DWG.

Part: THRESHOLD — CRACKED (FUSELAGE) · airframe 63,488 hrs · 51,885 cycles

R2 DOOR THRESHOLD WEB CRACKED BETWEEN STATION 986 TO 1006, RBL 38 TO 48. R & R WEB IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 63,488 hrs · 51,885 cycles

SHEAR TIE ANGLE CORRODED AT BS 500, BETWEEN STRINGER 26R TO 27R. R & R ANGLE IAW SRM & DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 63,488 hrs · 51,885 cycles

FUSELAGE WEB CRACKED AT STATION 500D, STRINGER 19L. R & R WEB IAW SRM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 63,488 hrs · 51,885 cycles

SUPPORT ANGLE CRACKED AT STATION 348.20, STRINGER 16L. R & R ANGLE IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,488 hrs · 51,885 cycles

FRAME CRACKED AT BS 520, BETWEEN STRINGER 21R TO 20R. REPAIRED FRAME IAW SRM.

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 63,488 hrs · 51,885 cycles

WHEEL WELL PRESS DECK WEB CRACKED AT BS 663.75+2", LBL 24.50+14.5". REPAIRED WEB IAW EO & EA.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 63,488 hrs · 51,885 cycles

SUPPORT ANGLE CRACKED AT BS 967, STRINGER 3L. R & R ANGLE IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,488 hrs · 51,885 cycles

FUSELAGE FRAME CRACKED AT STATION 787, STRINGER 25R. REPAIRED FRAME IAW SRM.

Part: PLATE — CRACKED (FUSELAGE) · airframe 63,488 hrs · 51,885 cycles

ACCESS PANEL 9508R PLATE CRACKED. R & R PLATE IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 63,488 hrs · 51,885 cycles

TIE CLIP CRACKED AT BS 947.5, STRINGER 26L. R & R TIE CLIP IAW SRM & DWG.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 63,488 hrs · 51,885 cycles

FORWARD CARGO DOOR CUT OUT FRAME WEB CRACKED AT BS 492, STRINGER 24R. R & R FRAME IAW SRM & DWG.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 63,488 hrs · 51,885 cycles

STRINGER 27L CORRODED AT STATION 1006. REPAIRED STRINGER IAW SRM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 63,488 hrs · 51,885 cycles

SUPPORT ANGLE CRACKED AT BS 947.5, STRINGER 25L. R & R ANGLE IAW SRM & DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 63,488 hrs · 51,885 cycles

FUSELAGE SHEAR TIE CORRODED AT STATION 1006, STRINGER 27L TO 27R. REPAIRED SHEAR TIE IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,488 hrs · 51,885 cycles

INTERCOSTAL CRACKED AT STATION 787, STRINGER 25R. R & R INTERCOSTAL IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 63,488 hrs · 51,885 cycles

FRAME CORRODED AT BS 767, BETWEEN STRINGER 27R TO 26R. REPAIRED FRAME IAW SRM.

Part: ACCESS PANEL — CRACKED (RT HORIZ STAB) · airframe 63,488 hrs · 51,885 cycles

RIGHT HORIZONTAL STABILIZER ACCESS PANEL 9223R CRACKED. R & R PLATE IAW SRM & DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 63,488 hrs · 51,885 cycles

SUPPORT ANGLE CRACKED AT STATION 962, STRINGER 25L. R & R ANGLE IAW SRM.

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 63,488 hrs · 51,885 cycles

MAIN WW PRESS DECK WEB CRACKED AT BS 663.75+9", LBL 24.50+15". REPAIRED WEB IAW EO & EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,488 hrs · 51,885 cycles

AFT FACE FRAME WEB CRACKED AT BS 492, STRINGER 24R. R & R FRAME IAW SRM & DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 63,488 hrs · 51,885 cycles

SUPPORT ANGLE CRACKED AT BS 957, STRINGER 25L. R &R ANGLE IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,488 hrs · 51,885 cycles

FORWARD FACE FRAME WEB CRACKED AT BS 492, STRINGER 24R. R & R FRAME IAW SRM & DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,488 hrs · 51,885 cycles

SKIN CRACKED AT BS 520+2, STRINGER 28R. REPAIRED SKIN IAW EO.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 63,488 hrs · 51,885 cycles

LONGITUDINAL FLOORBEAM CRACKED AT STATION 667, LBL 24.5. REPAIRED BEAM IAW EA.

Part: PLATE — CRACKED (FAIRING) · airframe 63,488 hrs · 51,885 cycles

LEFT WING TO BODY FAIRING ACCESS PANEL 3578L PLATE CRACKED. R & R PLATE IAW SRM.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 63,488 hrs · 51,885 cycles

RIGHT CHORD CRACKED AT BS 727, STRINGER 18A, FWD LOWER HOLE. REPAIRED CHORD IAW EA.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 63,488 hrs · 51,885 cycles

LEFT CHORD CRACKED AT BS 727, STRINGER 18A, FWD LOWER HOLE. REPAIRED CHORD IAW EA.

Part: LENS — FADED (CABIN) · airframe 62,788 hrs · 51,399 cycles

RIGHT OVERWING EMERGENCY LIGHT LENS COVER FADED. R & R COVER IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 62,161 hrs · 50,950 cycles

FWD ENTRY DOOR LOWER EMERGENCY EXIT LIGHT INOPERATIVE. R & R LIGHT ASSEMBLY IAW MM.

Part: ANGLE — CRACKED (RT WING) · airframe 61,953 hrs · 50,810 cycles

RT WING CRACKED VERTICAL ANGLE INBD & FWD OF NR 2 AILERON HINGE FITTING. R & R ANGLE IAW SRM.

Part: SKIN — CRACKED (LT WING) · airframe 61,953 hrs · 50,810 cycles

LT WING FIXED LE INBD OF PYLON AT FSS 197 CRACKED AT DEFLECTOR DOOR CUTOUT. REPAIRED CUTOUT IAW EA.

Part: WEB — CRACKED (NLG WW) · airframe 60,462 hrs · 49,692 cycles

NOSE WHEEL WELL CRACKED BETWEEN PANELS 3103R AND 3105R, BS259.5, WL 192R. REPAIRED WEB IAW SRM.

Part: FLAP — LOOSE (R1 DOOR) · airframe 60,350 hrs · 49,611 cycles

R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR FLAP LOOSE. SECURED FLAP IAW MM.

Part: ANGLE — CRACKED (RT MLG WW) · airframe 59,993 hrs · 49,349 cycles

L-ANGLE AT AFT I/B OF RIGHT WHEEL WELL CUTOUT CRACKED. REMOVED AND REPLACED L-ANGLE IAW SRM.

Part: WINDOW — CRACKED (COCKPIT) · airframe 59,598 hrs · 49,082 cycles

AT TOP OF DESCENT CAPTAIN'S L1 WINDOW SHATTERED WITH VISIBLE ARCED. REMOVED AND REPLACED WINDOW PER MM.

Part: LENS — CRACKED (EXIT SIGN) · airframe 59,462 hrs · 48,991 cycles

FLIGHT ATTENDANT REPORTS RIGHT OVERWING DOOR EXIT SIGN LENS CRACKED. REMOVED AND REPLACED SAID LENS PER MM.

Part: FLAP — DELAMINATED (RT WING) · airframe 59,433 hrs · 48,969 cycles

RIGHT I/B FORE FLAP LWR I/B SIDE HAS DELAMINATION. ACCOMPLISHED PERMANENT REPAIR 6"X6" ON RIGHT I/B FORE FLAP LWR I/B SIDE IAW B737 SRM 51-70-10 PAR 7 ,8, 9, 20, 22. APPLIED TOP COAT IAW B737 SRM 51-21-39.

Part: FITTING — CORRODED (TE FLAP) · airframe 59,433 hrs · 48,969 cycles

LEFT O/B FLAP INBOARD TRACK INSPAR ATTACH POINT HAS CORROSION IN BOLT HOLE AND CORRODED HARDWARE. REMOVED AND REPLACED: LEFT WING O/B FLAP, INBOARD TRACK, ATTACH FITTING IAW B737 SRM 51-40-02, 51-40-05, B737 AMM 28-11-00 AND B SOPM 20-50-03.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 59,433 hrs · 48,969 cycles

RIGHT O/B TRAILING EDGE FLAP HAS DELAMINATION ON LWR TRAILING EDGE. ACCOMPLISHED PERMANENT REPAIR 4" DIA ON RIGHT O/B AFT FLAP LWR SKIN TRAILING EDGE IAW B737 SRM 57-53-01, SRM 51-70- 10 REPAIR 2.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,372 hrs · 48,928 cycles

FUSELAGE SKIN CRACKED 7.00" AT VHF-3 ANTENNA ATTACH POINT, STA 727D+7.00" BETWEEN STR 27L AND 27R. COMPLIED WITH EA 1-353-21485.

Part: LENS — LOOSE (CABIN) · airframe 58,476 hrs · 48,250 cycles

RIGHT EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LIGHT PER MM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 57,785 hrs · 47,739 cycles

AFT I/B EMERGENCY FLASHLIGHT LIGHT INOP. REMOVED AND REPLACED BATTERIES IAW M/M.

Part: GASPER FAN — FAULTY (AC BAY) · airframe 57,725 hrs · 47,695 cycles

EN ROUTE AT 37,000FT, F/O AND CAPT SMELLED AN ACRID ODOR IN COCKPIT. FOUND GASPER FAN TO BE THE CAUSE. REMOVED AND REPLACED SAME PER MM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 57,672 hrs · 47,650 cycles

STRINGER CRACKED AT BS 460+16, STR 27R. REPAIRED STRINGER IAW EA AND SRM.

Part: STRUCTURE — DAMAGED (LE SLAT) · airframe 57,672 hrs · 47,650 cycles

RIGHT WING 6 SLAT I/B CAN DAMAGED FROM CONTACT WITH TRACK. REPAIRED SLAT CAN IAW SRM.

Part: DOOR FRAME — CRACKED (CARGO DOOR) · airframe 57,672 hrs · 47,650 cycles

FORWARD CARGO DOOR AFT LOWER EDGE FRAME CRACKED AT CUTOUT FOR LOWEST STOP FITTING. REMOVED AND REPLACED FRAME IAW SRM AND DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,672 hrs · 47,650 cycles

RIGHT FRAME INNER CHORD CRACKED AT STA 616. REPAIRED CHORD PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,672 hrs · 47,650 cycles

LEFT FRAME INNER CORD CRACKED AT BS 616. REPAIRED CHORD PER EA.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 57,672 hrs · 47,650 cycles

LEFT WING OUTBOARD AFT FLAP LOWER SKIN DELAMINATED. REMOVED & RE-INSTALLED AFT FLAP IAW AMM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,672 hrs · 47,650 cycles

FRAME CRACKED AT BS 500C, STR 21L. REPAIRED FRAME IAW EA AND EA.

Part: LENS — BROKEN (CABIN) · airframe 57,462 hrs · 47,485 cycles

AFT GALLEY EMERGENCY EXIT LENS ON WALL NEXT TO R2 DOOR BROKEN. REMOVED AND REPLACED LENS PER M/M.

Part: COVER — MISSING (EXIT SIGN) · airframe 57,135 hrs · 47,236 cycles

RT OVERWING EXIT SIGN COVER MISSING. INSTALLED RT OVERWING EXIT SIGN COVER IAW M/M.

Part: LENS — LOOSE (CABIN) · airframe 56,871 hrs · 47,035 cycles

RT OVERWING EMERGENCY EXIT LENS LOOSE. RE-SECURED LENS PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 56,788 hrs · 46,971 cycles

EMERGENCY EXIT LIGHTING STRIP LOOSE BETWEEN ROW 7 TO ROW 9. SECURED EEPLS IAW MM.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 56,685 hrs · 46,894 cycles

LT HORIZONTAL STABILIZER LOWER SURFACE STA 117.5 CRACKED. REPAIRED STABILIZER PER EA.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 56,686 hrs · 46,894 cycles

LT HORIZONTAL STABILIZER LOWER SURFACE, STA 145.0, CRACKED. REPAIRED STABILIZER PER EA.

Part: PUMP — FAULTY (NR 2 ENGINE) · airframe 56,181 hrs · 46,510 cycles

DIVERSION -- AT CRUISE N1 82 PERCENT - 84 PERCENT ENGINE NR 2 FLUCTUATES 0.3 PERCENT ALL OTHER PARAMETERS FOLLOW. REMOVED AND REPLACED FUEL PUMP AND MEC PER MT.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 55,795 hrs · 46,208 cycles

DURING SCHEDULED CV CHECK, FOUND RT EMERGENCY EXIT LIGHT INOPERATIVE. RELAMPED LIGHT PER MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 55,115 hrs · 45,665 cycles

L1 DOOR EMERGENCY EVAC SLIDE INADVERTANTLY FELL OUT, DID NOT DEPLOY. RE-INSTALLED SLIDE PER MT.

Part: FLAP — PUNCTURED (LT WING) · airframe 54,955 hrs · 45,542 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND LT WING I/B TRAILING EDGE FORE FLAP PUNCTURED. REMOVED AND REPLACED FORE FLAP ASSY PER MM.

Part: SPOILER — PUNCTURED (RT WING) · airframe 54,955 hrs · 45,542 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND RT WING I/B GROUND SPOILER NR 5 PUNCTURED. REMOVED AND REPLACED NR 5 SPOILER PER MM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 54,119 hrs · 44,878 cycles

L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: SLAT — CRACKED (LT WING) · airframe 54,049 hrs · 44,831 cycles

DURING SCHEDULED SPV CHECK, FOUND LT WING NR 1 SLAT CENTER OF SLAT, BOTTOM SIDE CRACKED. REPAIRED SLAT PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,049 hrs · 44,831 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT LT WINDOW BS 847+10. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,049 hrs · 44,831 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT LT WINDOW UPPER FORWARD CORNER, BS 480+10. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,049 hrs · 44,831 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 360, STR 14R. REPAIRED SKIN PER EA.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 54,049 hrs · 44,831 cycles

DURING SCHEDULED SPV CHECK, FOUND FWD FLIGHT ATTENDANT EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 54,049 hrs · 44,831 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 360, BETWEEN STR 14R TO STR 15R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,049 hrs · 44,831 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED BETWEEN BS 360 TO BS 540. REPAIRED SKIN PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,049 hrs · 44,831 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 827, STR 5R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,049 hrs · 44,831 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 5R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,049 hrs · 44,831 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 8R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,049 hrs · 44,831 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 5R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,049 hrs · 44,831 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 908, STR 5R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,049 hrs · 44,831 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 6R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,049 hrs · 44,831 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 827, STR 6R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,049 hrs · 44,831 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 7R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,049 hrs · 44,831 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 9R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,049 hrs · 44,831 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 6R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,049 hrs · 44,831 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 5R. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,049 hrs · 44,831 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 991, STR 8R. REPAIRED SKIN PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,049 hrs · 44,831 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 10L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,049 hrs · 44,831 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 10L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,049 hrs · 44,831 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 10L. REMOVED AND REPLACED CLIP PER SRM.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 54,049 hrs · 44,831 cycles

DURING SCHEDULED SPV CHECK, FOUND FWD LT EMERGENCY FLASHLIGHT HOLDER INOP. REMOVED AND REPLACED FLASHLIGHT ASSY PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,049 hrs · 44,831 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 10L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,049 hrs · 44,831 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 10L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,049 hrs · 44,831 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 4L. REMOVED AND REPLACED CLIP PER SRM.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 54,049 hrs · 44,831 cycles

DURING SCHEDULED SPV CHECK, FOUND LT EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT PER MM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 52,856 hrs · 43,891 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 907, BETWEEN STR 27R TO STR 27L. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,856 hrs · 43,891 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 22L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 52,856 hrs · 43,891 cycles

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

Part: WEB — CORRODED (FUSELAGE) · airframe 52,856 hrs · 43,891 cycles

DURING SCHEDULED 16Y CHECK, FOUND WEB CORRODED BETWEEN BS 927 TO BS 947, BETWEEN STR 25R TO STR 26R. REMOVED AND REPLACED WEB PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,856 hrs · 43,891 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME WEB CRACKED AT BS 303.9, STR 15L. REPAIRED WEB PER EO.

Part: FRAME — CORRODED (FUSELAGE) · airframe 52,856 hrs · 43,891 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 867, BETWEEN STR 27R TO STR 27L. REMOVED AND REPLACED FRAME PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,856 hrs · 43,891 cycles

DURING SCHEDULED 16Y CHECK, FOUND SKIN CRACKED BETWEEN BS 500A TO BS 500C, STR 1. REPAIRED SKIN PER EO.

Part: FRAME — CORRODED (FUSELAGE) · airframe 52,856 hrs · 43,891 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 500A, BETWEEN STR 28L TO STR 28R. REMOVED AND REPLACED FRAME PER SRM AND BAC DWG.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 52,856 hrs · 43,891 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM CHORD CRACKED AT BS 294.5, LBL 52.25. REPAIRED BEAM PER SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 52,856 hrs · 43,891 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 927, STR 25R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 52,856 hrs · 43,891 cycles

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

Part: WEB — CRACKED (FUSELAGE) · airframe 52,856 hrs · 43,891 cycles

DURING SCHEDULED 16Y CHECK, FOUND WEB CRACKED AT BS 247.7, RBL 24. REPAIRED WEB PER SRM.

Part: CROSSBEAM — CORRODED (FUSELAGE) · airframe 52,856 hrs · 43,891 cycles

DURING SCHEDULED 16Y CHECK, FOUND CROSS BEAM CORRODED AT BS 947.5, RBL 48. REPAIRED BEAM PER EO.

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,856 hrs · 43,891 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CRACKED AT BS 500C, BETWEEN STR 20R TO STR 21R. REPAIRED FRAME PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 52,856 hrs · 43,891 cycles

DURING SCHEDULED 16Y CHECK, FOUND WEB CRACKED AT BS 706, RBL 24.75. REMOVED AND REPLACED WEB PER SRM AND BAC DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,856 hrs · 43,891 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CRACKED AT BS 500D, BETWEEN STR 20L TO STR 21L. REPAIRED FRAME PER SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 52,856 hrs · 43,891 cycles

DURING SCHEDULED 16Y CHECK, FOUND WEB CORRODED AT BS 788, BETWEEN STR 25R TO STR 26R. REMOVED AND REPLACED WEB PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,856 hrs · 43,891 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CRACKED AT BS 767, BETWEEN STR 26R TO STR 27R. REPAIRED FRAME PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 52,856 hrs · 43,891 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 747, BETWEEN STR 26R TO STR 27R. REMOVED AND REPLACED FRAME PER SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 52,856 hrs · 43,891 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 927, STR 27L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,856 hrs · 43,891 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CRACKED AT BS 787, STR 25L. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,856 hrs · 43,891 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CRACKED AT BS 807, STR 25L. REPAIRED FRAME PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 52,856 hrs · 43,891 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 747, BETWEEN STR 27R TO STR 27L. REPAIRED SHEAR TIE PER SRM AND BAC DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 52,856 hrs · 43,891 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 887, BETWEEN STR 27R TO STR 27L. REMOVED AND REPLACED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,856 hrs · 43,891 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CRACKED AT BS 767, STR 25L. REPAIRED FRAME PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 52,856 hrs · 43,891 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 767, BETWEEN STR 25R TO STR 26L. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,856 hrs · 43,891 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 4L. REMOVED AND REPLACED CLIP PER SRM.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 52,856 hrs · 43,891 cycles

DURING SCHEDULED 16Y CHECK, FOUND STIFFENER CRACKED AT BS 639, LBL 45.50. REPAIRED STIFFENER PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,856 hrs · 43,891 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CRACKED AT BS 787, BETWEEN STR 26R TO STR 27R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,856 hrs · 43,891 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CRACKED AT BS 827, STR 25L. REPAIRED FRAME PER SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 52,856 hrs · 43,891 cycles

DURING SCHEDULED 16Y CHECK, FOUND RT WING NR 5 SLAT SKIN CRACKED AT WBL 229.75. REPAIRED SKIN PER SRM.

Part: STIFFENER — CRACKED (CARGO BAY) · airframe 52,856 hrs · 43,891 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO COMPARTMENT STIFFENER CRACKED AT BS 727D, BETWEEN STR 27L TO STR 27R. REMOVED AND REPLACED STIFFENER PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,856 hrs · 43,891 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 20L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: SKIN — DELAMINATED (FOREFLAP) · airframe 52,856 hrs · 43,891 cycles

DURING SCHEDULED 16Y CHECK, FOUND LT WING I/B FORE FLAP LOWER SURFACE DELAMINATED. REPAIRED FORE FLAP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,856 hrs · 43,891 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 21L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 52,856 hrs · 43,891 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM CORRODED AT BS 967, RBL 28. REPAIRED BEAM PER SRM.

Part: FITTING — CORRODED (GIRT BAR) · airframe 52,856 hrs · 43,891 cycles

DURING SCHEDULED 16Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING CORRODED. REMOVED AND REPLACED FITTING PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,856 hrs · 43,891 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 21L. REMOVED AND REPLACED CLIP PER SRM.

Part: STIFFENER — CRACKED (CARGO BAY) · airframe 52,856 hrs · 43,891 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO COMPARTMENT VERTICAL STIFFENER CRACKED AT BS 727, STR 27R. REPAIRED STIFFENER PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,856 hrs · 43,891 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 19L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,856 hrs · 43,891 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 21R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: FITTING — CORRODED (GIRT BAR) · airframe 52,856 hrs · 43,891 cycles

DURING SCHEDULED 16Y CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING CORRODED. REMOVED AND REPLACED FITTING PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,856 hrs · 43,891 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 907, STR 26R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,856 hrs · 43,891 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 1. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 52,856 hrs · 43,891 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CRACKED AT BS 967, STR 27L. REMOVED AND REPLACED STRINGER PER SRM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 52,856 hrs · 43,891 cycles

DURING SCHEDULED 16Y CHECK, FOUND LT WING I/B AFT FLAP LOWER SKIN DELAMINATED. REPAIRED AFT FLAP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,856 hrs · 43,891 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CRACKED AT BS 480, BETWEEN STR 27R TO STR 28R. REMOVED AND REPLACED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,856 hrs · 43,891 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 26L. REMOVED AND REPLACED CLIP PER BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,856 hrs · 43,891 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 5R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,856 hrs · 43,891 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 5L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,856 hrs · 43,891 cycles

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

Part: WEB — CRACKED (CARGO BAY) · airframe 52,856 hrs · 43,891 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO WEB CRACKED AT BS 771.5, STR 27R. REMOVED AND REPLACED WEB PER BAC DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,856 hrs · 43,891 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CRACKED AT BS 480, BETWEEN STR 27R TO STR 28R. REMOVED AND REPLACED FRAME PER BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,856 hrs · 43,891 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, BETWEEN STR 8R TO STR 9R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,856 hrs · 43,891 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 887, STR 4L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,856 hrs · 43,891 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 827, STR 25L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 52,856 hrs · 43,891 cycles

DURING SCHEDULED 16Y CHECK, FOUND SUPPORT ANGLE CRACKED AT BS 320.5, STR 20L. REMOVED AND REPLACED CLIP PER SRM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 52,856 hrs · 43,891 cycles

DURING SCHEDULED 16Y CHECK, FOUND SUPPORT ANGLE CRACKED AT BS 328, STR 20L. REMOVED AND REPLACED CLIP PER SRM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 52,856 hrs · 43,891 cycles

DURING SCHEDULED 16Y CHECK, FOUND SUPPORT ANGLE CRACKED AT BS 336.5, STR 20L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,856 hrs · 43,891 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 559, STR 11R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: SLAT — DELAMINATED (RT WING) · airframe 52,856 hrs · 43,891 cycles

DURING SCHEDULED 16Y CHECK, FOUND RT WING I/B EDGE NR 4 SLAT DELAMINATED. REPAIRED SLAT PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,856 hrs · 43,891 cycles

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

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 52,856 hrs · 43,891 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 4L. REMOVED AND REPLACED SPLICE PER SRM AND BAC DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 52,856 hrs · 43,891 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM CORRODED BETWEEN BS 947.5 TO BS 967, RBL 30. REPAIRED BEAM PER SRM AND BAC DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 52,856 hrs · 43,891 cycles

DURING SCHEDULED 16Y CHECK, FOUND SUPPORT ANGLE WEB CRACKED BETWEEN BS 685 TO BS 706, LBL 24.75. REMOVED AND REPLACED WEB PER SRM AND BAC DWG.

Part: SKIN — CORRODED (FUSELAGE) · airframe 52,856 hrs · 43,891 cycles

DURING SCHEDULED 16Y CHECK, FOUND SKIN CORRODED AT BS 871, BETWEEN STR 27R TO STR 27L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,900 hrs · 43,162 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 824, STR 19L. REPAIRED SKIN PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 51,515 hrs · 42,859 cycles

DURING SCHEDULED MV1 CHECK, FOUND OVERHEAD BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 12. RELAMPED BULB PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,383 hrs · 42,750 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR LOWER FWD CORNER. REPAIRED SKIN PER SRM.

Part: COMPRESSOR — STALLED (NR 1 ENGINE) · airframe 51,116 hrs · 42,569 cycles

ON ROLL OUT 60-80 KNOTS, LOUD BANG, COMPRESSOR STALL ON NR 1 ENGINE ALL INSTRUMENTS AFTER CLEARING APPEARED NORMAL. REMOVED AND REPLACED NR 1 ENGINE PER MT.

Part: SIGN — LOOSE (CABIN) · airframe 50,980 hrs · 42,465 cycles

LT OVERWING EMERGENCY EXIT SIGN LOOSE. RE-INSTALLED SIGN PER MM.

Part: FLAP — DELAMINATED (LT WING) · airframe 50,562 hrs · 42,165 cycles

DURING SCHEDULED HC1 CHECK, FOUND LT WING O/B AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.

Part: FLAP — DELAMINATED (LT WING) · airframe 50,562 hrs · 42,165 cycles

DURING SCHEDULED HC1 CHECK, FOUND LT WING O/B FORE FLAP DELAMINATED. REMOVED AND REPLACED FORE FLAP PER MM.

Part: BRACKET — CRACKED (EVAC SLIDE) · airframe 50,562 hrs · 42,165 cycles

DURING SCHEDULED HC1 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE FWD BRACKET CRACKED. REMOVED AND REPLACED BRACKET PER MM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 50,562 hrs · 42,165 cycles

DURING SCHEDULED HC1 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MT.

Part: LIGHT — NOT SEATED (CABIN) · airframe 50,524 hrs · 42,139 cycles

LT OVERWING EMERGENCY EXIT LIGHT INOP. RE-SEATED BULB INTO SOCKET PER MM.

Part: COVER — LOOSE (CABIN) · airframe 50,442 hrs · 42,079 cycles

LEFT OVERWING EMERGENCY EXIT LIGHT COVER LOOSE. REPAIRED COVER PER EA.

Part: LENS — LOOSE (CABIN) · airframe 50,434 hrs · 42,073 cycles

LEFT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. REMOVED AND REPLACED LENS PER MM.

Part: LENS — LOOSE (CABIN) · airframe 50,243 hrs · 41,937 cycles

LEFT OVERHEAD EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER EA.

Part: LENS — BROKEN (L1 DOOR) · airframe 49,281 hrs · 41,258 cycles

L1 DOOR EMERGENCY EXIT SIGN LENS BROKEN. REMOVED AND REPLACED LENS ASSY PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 48,862 hrs · 40,967 cycles

RT EEPLS STRIP LOOSE AT ROW 5. SECURED EEPLS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,844 hrs · 40,951 cycles

DURING SCHEDULED HC2 CHECK, FOUND R2 DOOR FRAME CUTOUT FWD LOWER CORNER CRACKED. REPAIRED SKIN PER SWA EA.

Part: FLAP — DELAMINATED (RT WING) · airframe 48,844 hrs · 40,951 cycles

DURING SCHEDULED HC2 CHECK, FOUND RT WING O/B AFT FLAP DELAMINATED AT O/B END. REMOVED AND REPLACED AFT FLAP PER MM.

Part: TRACK — DAMAGED (CABIN) · airframe 48,844 hrs · 40,951 cycles

DURING SCHEDULED HC2 CHECK, FOUND EEPLS TRACK DAMAGED BETWEEN ROW 11 TO ROW 12. REMOVED AND REPLACED EEPLS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,808 hrs · 40,219 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,808 hrs · 40,219 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SRM.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 46,966 hrs · 39,607 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CREASED AT BS 947, STR 25R. REPAIRED SKIN PER ER.

Part: DOOR — CRACKED (FWD ENTRY) · airframe 46,966 hrs · 39,607 cycles

DURING SCHEDULED 14Y CHECK, FOUND FWD ENTRY DOOR UPPER HINGE CUTOUT CRACKED. REPAIRED DOOR PER ER.

Part: DOOR — CRACKED (FWD ENTRY) · airframe 46,966 hrs · 39,607 cycles

DURING SCHEDULED 14Y CHECK, FOUND FWD ENTRY DOOR LOWER HINGE CUTOUT CRACKED. REPAIRED DOOR PER ER.

Part: STRINGER CLIP — CRACKED (BS 927 S8L) · airframe 46,966 hrs · 39,607 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER STRINGER CLIP CRACKED AT BS 927, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,966 hrs · 39,607 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 867, STR 9R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,966 hrs · 39,607 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,966 hrs · 39,607 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,966 hrs · 39,607 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,966 hrs · 39,607 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,966 hrs · 39,607 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,966 hrs · 39,607 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,966 hrs · 39,607 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,966 hrs · 39,607 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,966 hrs · 39,607 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,966 hrs · 39,607 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,966 hrs · 39,607 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,966 hrs · 39,607 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,966 hrs · 39,607 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8R AND STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,966 hrs · 39,607 cycles

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

Part: GLOWSTRIP — WORN (CABIN) · airframe 46,966 hrs · 39,607 cycles

DURING SCHEDULED HC1 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP WORN AT LH OVERWING EMERGENCY EXIT. R&R STRIP PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 45,434 hrs · 38,497 cycles

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

Part: CONTROL UNIT — FAULTY (T/E FLAP) · airframe 45,340 hrs · 38,424 cycles

ON APPROACH TO HOU L/E SLATS DID NOT EXTEND. REMOVED AND REPLACED FLAP CONTROL UNIT PER MM.

Part: CONTROL VALVE — FAULTY (L/E SLAT) · airframe 45,213 hrs · 38,325 cycles

AIR TURNBACK. DURING CLIMBOUT OF AMA WITH FLAP HANDLE UP AND T/E FLAPS UP NR 1 AND NR 6 L/E SLATS IN TRANSIT LIGHT ILLUMINATED. REMOVED AND REPLACED L/E SLAT CONTROL VALVE AND NR 2 L/E FLAP ACTUATOR PER MM.

Part: CONTROL VALVE — FAULTY (L/E SLAT) · airframe 45,212 hrs · 38,323 cycles

AIR TURNBACK. DURING CLIMBOUT OF DEN L/E TRANSIT LIGHT ILLUMINATED. NR 6 L/E SLAT DID NOT MOVE WHEN FLAPS RETRACTED. NO ROLL NOTED. REMOVED AND REPLACED L/E DEVICE CONTROL VALVE PER MM.

Part: SPOILER — CRACKED (NR 4 SPOILER) · airframe 44,680 hrs · 37,921 cycles

DURING SCHEDULED CABIN VISIT CHECK, FOUND LT WING NR 4 GROUND SPOILER OUTBOARD HINGE CRACKED. REMOVED AND REPLACED SPOILER PER MM.

Part: DOWNLOCK SENSOR — FAULTY (LT MLG) · airframe 43,523 hrs · 36,992 cycles

DECLARED EMERGENCY, LT MAIN LANDING GEAR LIGHT FLUCTUATED BETWEEN GREEN AND RED WITH NORMAL EXTENSION. R&R LT MAIN LANDING GEAR DOWN LOCK SENSOR PER MM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 42,251 hrs · 36,019 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER 26R CORRODED AT BS 442. REMOVED AND REPLACED STRINGER SECTION PER SRM.

Part: TORQUE TUBE — FAILED (RT ELEVATOR) · airframe 42,251 hrs · 36,019 cycles

DURING SCHEDULED SPV CHECK, RIGHT ELEVATOR BUSS LINKAGE FAILED CHECK. REMOVED AND REPLACED ELEVATOR OUTPUT TORQUE TUBE PER MM.

Part: WEB — CORRODED (FUSELAGE) · airframe 42,551 hrs · 36,019 cycles

DURING SCHEDULED SPV CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 827 TO BS 847, LBL 70. REMOVED AND REPLACED CREASE BEAM WEB PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 42,018 hrs · 35,825 cycles

DURING SCHEDULED SERVICE CHECK, FOUND R1 DOOR EMERGENCY EXIT SIDEWALL LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 41,585 hrs · 35,490 cycles

R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 41,328 hrs · 35,296 cycles

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

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 41,121 hrs · 35,135 cycles

DURING SCHEDULED C2 CHECK, FOUND R1 DOOR LOWER FRAME CRACKED AT LOWER AFT DOOR STOP. REMOVED AND REPLACED R1 DOOR PER MM.

Part: HINGE — CRACKED (PAX DOOR) · airframe 41,121 hrs · 35,135 cycles

DURING SCHEDULED C2 CHECK, FOUND FWD ENTRY DOOR UPPER HINGE BOX CRACKED. REMOVED AND REPLACED UPPER HINGE BOX PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 40,961 hrs · 35,016 cycles

DURING SCHEDULED SERVICE CHECK, FOUND BULL NOSE EMERGENCY EXIT LIGHT INOP AT ROW 1 DEF. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 40,961 hrs · 35,016 cycles

DURING SCHEDULED SERVICE CHECK, FOUND RT OVERWING EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 40,740 hrs · 34,829 cycles

L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHTS) · airframe 40,363 hrs · 34,530 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FWD CABIN CENTER AISLE OVERHEAD EXIT LIGHT INOP. SECURED CONNECTOR AT EMERGENCY EXIT LIGHT ASSY PER MM.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 40,234 hrs · 34,433 cycles

DURING SCHEDULED C1 CHECK, FOUND RT HORIZONTAL STAB SKIN CRACKED AT LOWER SURFACE, STA 70. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 39,764 hrs · 34,066 cycles

L2 DOOR EMERGENCY EXIT EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM.

Part: SKIN — CRACKED (RT WING LE) · airframe 39,296 hrs · 33,702 cycles

DURING SCHEDULED C4 CHECK, FOUND RIGHT WING L/E SKIN CRACKED AT WS 213. REPAIRED SKIN PER SWA EA.

Part: LIGHT — LOOSE (CABIN) · airframe 38,526 hrs · 33,092 cycles

L1 DOOR EMERGENCY EXIT LIGHT LOOSE. SECURED LIGHT PER MM.

Part: LINK — WORN (LT ELEVATOR) · airframe 38,296 hrs · 32,902 cycles

DURING SCHEDULED C3 CHECK, LT ELEVATOR TAB FAILED THE FREE PLAY CHECK. REMOVED AND REPLACED LT ELEVATOR TAB FWD SUPPORT LINKS AND HARDWARE PER MM.

Part: SKIN — DELAMINATED (RT WING) · airframe 38,296 hrs · 32,902 cycles

DURING SCHEDULED C3 CHECK, FOUND RT WING OTBD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.

Part: GASPER FAN — FAULTY (CABIN) · airframe 37,776 hrs · 32,480 cycles

STRONG SMOKE SMELL IN AFT CABIN AND COCKPIT. REMOVED AND REPLACED GASPER FAN PER MM.

Part: SKIN — DELAMINATED (RT WING FLAP) · airframe 35,547 hrs · 30,683 cycles

DURING SCHEDULED C4 CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED T/E AFT FLAP PER MM.

Part: BUSHING — WORN (LT ELEVATOR) · airframe 34,616 hrs · 29,984 cycles

DURING SCHEDULED C3 CHECK, LEFT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED NR 1 AND NR 2 TAB BUSHINGS PER MM.

Part: FITTING — CORRODED (VERTICAL STAB) · airframe 33,855 hrs · 29,340 cycles

DURING SCHEDULED D-CHECK, FOUND VERTICAL STAB FITTING LUGS CORRODED. REPAIRED VERTICAL STAB FITTING PER ER.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 33,855 hrs · 29,340 cycles

DURING SCHEDULED D-CHECK, FOUND FLOOR ZEE CHANNEL AT BS 270, RBL 10, CORRODED. REMOVED AND REPLACED FLOOR ZEE CHANNEL PER SRM.

Part: FITTING — CORRODED (HORIZONTAL STAB) · airframe 33,855 hrs · 29,340 cycles

DURING SCHEDULED D-CHECK, FOUND HORIZONTAL STAB FITTING LUGS, CORRODED. REPAIRED HORIZONTAL STAB PER ER AND SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,855 hrs · 29,340 cycles

DURING SCHEDULED D-CHECK, FOUND FRAME CHORDS AT RT AND LT BS 188, CRACKED. REPAIRED FRAME CHORDS PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 33,855 hrs · 29,340 cycles

DURING SCHEDULED D-CHECK, FOUND FLOOR WEB AT RT AND LT BS 188 TO BS 196, CRACKED. REMOVED AND REPLACED FLOOR WEB PER SRM.

Part: CREASE BEAM — CORRODED (CABIN FLOOR) · airframe 33,855 hrs · 29,340 cycles

DURING SCHEDULED D-CHECK, FOUND CREASE BEAM CORRODED AT BS 727A TO BS 727B, RT SIDE. REPAIRED CREASE BEAM PER SRM.

Part: FRAME — CORRODED (AFT CARGO) · airframe 33,855 hrs · 29,340 cycles

DURING SCHEDULED D-CHECK, FOUND AFT CARGO COMPARTMENT FUSELAGE FRAME CORRODED AT BS 747, LBL 7 TO LBL 11. REPAIRED FRAME PER SRM.

Part: FLOORBEAM — CORRODED (BS 344) · airframe 33,855 hrs · 29,340 cycles

DURING SCHEDULED D CHECK, FOUND FLOORBEAM CORRODED AT BS 344, LBL 21 TO RBL 1. REPAIRED FLOOR BEAM PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,855 hrs · 29,340 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 33,855 hrs · 29,340 cycles

DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 480, STRINGER 8L, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: FRAME — CRACKED (BS 787) · airframe 33,855 hrs · 29,340 cycles

DURING SCHEDULED D CHECK, FOUND FRAME AT BS 787, STRINGER 8R TO STRINGER 8L, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: STRUCTURE — CRACKED (BS 400-440) · airframe 33,855 hrs · 29,340 cycles

DURING SCHEDULED D CHECK, FOUND STRUCTURE AT BS 400 TO BS 440, STRINGER 8L, CRACKED. REMOVED AND REPLACED STRUCTURE SECTION PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,855 hrs · 29,340 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,855 hrs · 29,340 cycles

DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 727D, STRINGER 8R, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,855 hrs · 29,340 cycles

DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 294, STRINGER 7R, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 33,855 hrs · 29,340 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP AT BS 706, STRINGER 11L, CRACKED. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FITTING — CORRODED (HORIZONTAL STAB) · airframe 33,855 hrs · 29,340 cycles

DURING SCHEDULED D-CHECK, FOUND RIGHT HORIZONTAL STAB NR 6 ELEVATOR HINGE FITTING, CORRODED. REMOVED AND REPLACED HINGE FITTING PER ACO.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 33,855 hrs · 29,340 cycles

DURING SCHEDULED D-CHECK, FOUND FRAME WEB AT FWD ENTRY DOOR CUTOUT BS 303.9, STRINGER 16L, CRACKED. REMOVED AND REPLACED FRAME WEB SECTION PER SB AND SRM.

Part: STRINGER CLIP — CRACKED (BS 706) · airframe 33,855 hrs · 29,340 cycles

DURING SCHEDULED D CHECK, FOUND STRINGER CLIP AT BS 706, STRINGER 13R CRACKED. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 33,668 hrs · 29,182 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT BS 378.5, LBL 2.8, EQUIPMENT COOLING AIR EXHAUST CUTOUT, CRACKED. REPAIRED SKIN PER EA.

Part: STRUCTURE — DELAMINATED (LT FOREFLAP) · airframe 33,661 hrs · 29,175 cycles

DURING SCHEDULED C2 CHECK, FOUND LT WING INBOARD FOREFLAP DELAMINATED. REMOVED AND REPLACED FOREFLAP PER MM.

Part: STRUCTURE — CRACKED (L/E SLAT) · airframe 33,661 hrs · 29,175 cycles

DURING SCHEDULED C2 CHECK, FOUND LT WING NR 1 L/E SLAT, CRACKED. REPAIRED L/E SLAT PER EA.

Part: STRUCTURE — CRACKED (L/E SLAT) · airframe 33,661 hrs · 29,175 cycles

DURING SCHEDULED C2 CHECK, FOUND LT WING NR 2 L/E SLAT, CRACKED. REPAIRED L/E SLAT PER EA.

Part: SLIDE — UNSERVICEABLE (R1 DOOR) · airframe 33,642 hrs · 29,159 cycles

DURING SCHEDULED A1 CHECK, FOUND R1 DOOR EVAC SLIDE IND OUT OF LIMITS. REMOVED AND REPLACED R1 DOOR EVAC SLIDE PER MM.

Part: SLIDE — UNSERVICEABLE (R1 DOOR) · airframe 33,569 hrs · 29,103 cycles

DURING SCHEDULED A1 CHECK, FOUND R1 DOOR EVAC SLIDE LOW PRESSURE, IND. REMOVED AND REPLACED R1 DOOR EVAC SLIDE PER MM.

Part: LIGHT — WORN (FWD CABIN) · airframe 30,717 hrs · 26,846 cycles

DURING SCHEDULED C3 CHECK, FOUND EEPLS STRIP WORN AT ROW NR 3. REMOVED AND REPLACED EEPLS STRIP PER MM.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 29,809 hrs · 26,117 cycles

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

Part: CABLE — MISROUTED (AFT ENTRY DOOR) · airframe 27,981 hrs · 24,667 cycles

DURING SCHEDULED C4 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE GIRT CABLE MISROUTED. REROUTED CABLE PER MM.

Part: CABLE — DISCONNECTED (AFT SVC DOOR) · airframe 27,045 hrs · 23,909 cycles

DURING SCHEDULED C3 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE GIRT BAR LANYARD CABLE DISCONNECTED. CONNECTED CABLE PER MM.

Part: WEB — CRACKED (FUSELAGE) · airframe 25,740 hrs · 22,847 cycles

DURING SCHEDULED 1/4D CHECK, FOUND VERTICAL BEAM WEB CRACKED .25 INCH LONG AT BS 179, WL 227 AND LBL 17.1. REPAIRED WEB PER SRM.

Part: FLOORBEAM — CORRODED (AFT CARGO) · airframe 25,740 hrs · 22,847 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM CORRODED AT BS 767, LBL 6 AND LBL 10. REPAIRED FLOORBEAM PER SWA RA.

Part: ELEVATOR — DELAMINATED (RT HORIZ STAB) · airframe 25,740 hrs · 22,847 cycles

DURING SCHEDULED 1/4D CHECK, FOUND RT ELEVATOR DELAMINATED. REMOVED AND REPLACED RT ELEVATOR PER MM.

Part: SKIN — CRACKED (LT ELEVATOR) · airframe 22,394 hrs · 20,065 cycles

DURING SCHEDULED C2 CHECK, FOUND LT ELEVATOR UPPER SKIN CRACKED 1.5 INCH AT APPROX 12 INCHES FWD OF TAB, 46 INCHES OUTBD OF INBD SIDE OF ELEVATOR. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF ADJ (AFT SERVICE DOOR) · airframe 21,401 hrs · 19,246 cycles

DURING SCHEDULED C1 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE ASSY PER MM.

Part: SIGN — LOOSE (FWD PAX DOOR) · airframe 21,401 hrs · 19,246 cycles

DURING SCHEDULED C1 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EXIT SIGN LOOSE. SECURE SIGN PER MM.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 21,241 hrs · 19,121 cycles

FWD I/B EMERGENCY FLASHLIGHT INOP. REPLACED BATTERIES PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 20,774 hrs · 18,735 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BS 178 BULKHEAD, BOTH LT AND RT SIDE CHORDS CRACKED. REMOVED AND REPLACED SIDE CHORD SECTIONS PER ACO.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 20,518 hrs · 18,509 cycles

DURING SCHEDULED C4 CHECK, FOUND RT HORIZONTAL STAB LOWER SKIN CRACKED BETWEEN REAR SPAR AND NR 1 BALANCE PANEL. REPAIRED SKIN PER SRM.

Part: LIGHT — FAILED (COCKPIT)

ON FINAL APPROACH, RT MLG GREEN INDICATOR LIGHT FAILED TO ILLUMINATE. ABORTED THE APPOACH AND ALTERNATE GEAR EXTENSION WAS USED. REMOVED AND REPLACED RT MLG KORRY LIGHT ASSY. OPS CK GOOD.

Part: CLEVIS — CRACKED (RT MLG)

DURING SCHEDULED SERVICE CHECK, FOUND THROUGH ULTRASONIC INSPECTION, RT MLG WALKING BEAM ARM CLEVIS CRACKED ON AFT LUG. REMOVED AND REPLACED RT MLG BEAM ARM CLEVIS PER MM.

Part: SLIDES — SAGGING (FWD DOORS)

DURING SCHEDULED SERVICE CHECK, FOUND BOTH FWD DOOR EVACUATION SLIDE GIRT ASSY'S EXTENDING OUT OF LIMITS. ADJUSTED SLIDES PER MM.

Part: BATTERY — DISCHARGED (CABIN)

DURING SCHEDULED 1/2D CHECK, FOUND INTERIOR AND EXTERIOR OVERWING EXIT LIGHTS ILLUMINATED WHEN POWER IS TURNED OFF. REMOVED AND REPLACED LT AND RT BATTERY ASSY'S.

Part: FLOORBEAM — CORRODED (BS 328)

DURING SCHEDULED 1/2D CHECK, FOUND BS 328 FLOOR BEAM UPPER CHORD CORRODED IN NUMEROUS SCREW HOLES. REPAIRED BEAM PER SWA RA NR 1-353-2160.

Part: FRAME — CRACKED (SRVC DOORWAY)

DURING SCHEDULED 1/2D CHECK, FOUND FWD SERVICE DOOR LOWER CUT OUT FUSELAGE STUB FRAME CRACKED, BS 294. REPAIRED FRAME PER SRM.

Part: VALVE — FAILED (LT PACK)

EXTREMELY LOUD VIBRATION AT MID CABIN ACCOMPANIED BY THUMPING SOUND. FOUND LT TURBO FAN VALVE FAILED OPEN. SWAPPED LT AND RT TURBO FAN VALVES PER MM. OPS CHECK GOOD. NO VIBRATIONS OR OTHER IRREGULARITIES NOTED.

Part: ANGLE — CRACKED (LT A/C BAY)

DURING SCHEDULED C1 CHECK, FOUND INLET SUPPORT ANGLE CRACKED. REPAIRED PER SWA RA NR 1-A53-1876.

Part: ENGINE — BIRD STRIKE (NR 1)

AFTER TAKEOFF, EXPERIENCED BIRD STRIKE TO NR 1 ENGINE FOLLOWED BY VIBRATION. RETURNED TO SMF AND MADE AN UNEVENTFUL LANDING. REPLACED FAN BLADE SET, ACCOUSTIC PANELS AND CSD OIL COOLER PER BOEING M/M.

Part: VALVE — FAILED (NR 2 ENGINE)

DIVERTED TO OAK DUE TO NUMBER 2 ENGINE ANTI-ICE VALVE NOT OPENING. LANDED WITHOUT INCIDENT. REPLACED ANTI-ICE VALVE PER BOEING M/M.

Part: TRANSMITTER — MALFUNCTIONED (NR 1 ENGINE)

DIVERTED TO PHX DUE TO NR 1 ENGINE HIGH OIL TEMP AND MADE AND UNEVENTFUL LANDING. INSPECTED, UNABLE TO DUPLICATE PROBLEM. REMOVED AND REPLACED OIL TEMP TRANSMITTER AND INDICATOR AS A PRECAUTION PER BOEING M/M.

Part: NAV CONTL PNL — INOPERATIVE (NR 1)

NUMBER 1 VHF NAV SYSTEM BECAME INOPERATIVE, SWITCHING TO AUX, NO HELP. AIRCRAFT DIVERTED TO PHX AND MADE AN UNEVENTFUL LANDING. REPLACED BOTH NAV CONTROL PANELS AND NR 1 NAV RECEIVER PER BOEING M/M.

Part: AIR DISTR — ODOR (COCKPIT)

CREW NOTED JET FUEL SMELL IN COCKPIT EMITTING FROM AIR VENTS. INSPECTION PERFORMED, NO LEAKS NOTED PER BOEING M/M.

Part: SKIN — DAMAGED (AFT CARGO DOOR)

DURING SCHEDULED C4 CHECK, FOUND AFT CARGO DOOR SKIN CREASED AND OIL CANNING. REPAIRED PER BOEING SRM.

Part: OUTFLOW VLV — MALFUNCTIONED (CABIN)

AT 35,000 FEET, EXPERIENCED CABIN ALTITUDE ALERT WARNING. CREW WAS UNABLE TO CONTROL CABIN PRESSURE USING STANDBY OR MANUAL MODES. INITIATED EMERGENCY DESCENT TO 15,000 FEET WHERE CREW REGAINED CONTROL OF PRESSURE. AIRCRAFT MADE AN UNEVENTFUL LANDING AT SJC. INSPECTED AND PERFORMED PRESSURE CONTROL TEST WITH NO DEFECTS NOTED. REPLACED MAIN OUTFLOW VALVE, O/H PRESSURE CONTROL PANEL AND PRESSURE CONTROLLER PER BOEING M/M.