N391SW

Part: GLOWSTRIP — DAMAGED (CABIN) · airframe 69,459 hrs · 55,930 cycles

RIGHT AFT GALLEY PHOTOLUMINESCENT STRIP DAMAGED. R & R STRIP IAW DWG.

Part: LENS — BROKEN (CABIN) · airframe 68,715 hrs · 55,445 cycles

RIGHT EMER EXIT OVERWING EXIT LIGHT LENS BROKEN. R & R LENS IAW AMM.

Part: ATTACH ANGLE — CRACKED (RT WING) · airframe 68,715 hrs · 55,445 cycles

RIGHT WING TE STRUCTURE RSS 545, INBD OF NR 2 AILERON HINGE, INTERCOSTAL WEB ATTACH ANGLE CRACKED. R & R ANGLE IAW DWG & SRM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 68,715 hrs · 55,445 cycles

SUPPORT ANGLE CRACKED AT BS 360, STRINGER 8R. R & R ANGLE IAW ARM.

Part: FAIRING — CRACKED (RT WING) · airframe 68,715 hrs · 55,445 cycles

RIGHT WING LOWER FIXED TE PANEL, OTBD OF NR 6 FLAP TRACK FAIRING CRACKED. R & R FAIRING IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 68,715 hrs · 55,445 cycles

FORWARD CARGO PIT UNDER FLOOR, SHEAR TIE ANGLE CORRODED, AT BS 500D, BETWEEN LBL 6 TO RBL 6. R & R SHEAR TIE IAW SRM & DWG.

Part: ATTACH FITTING — CORRODED (FUSELAGE) · airframe 68,715 hrs · 55,445 cycles

VERTICAL KEEL BEAM ATTACH CLIP CORRODED, AT BS 500D, LBL 6. R & R CLIP IAW SRM & DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,715 hrs · 55,445 cycles

L1 DOOR UPPER & LOWER HINGE CUT OUT DOUBLER CRACKED AT BS 305, STRINGER 10L. REPAIRED CUT OUT IAW EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 68,715 hrs · 55,445 cycles

SHEAR TIE ANGLE CORRODED, AT BS 500D, RBL 8. R & R SHEAR TIE IAW SRM & DWG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 68,715 hrs · 55,445 cycles

FORWARD CARGO PIT LT CLIP CRACKED AT BS 540. R & R CLIP IAW DWG & SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,715 hrs · 55,445 cycles

FUSELAGE SKIN CRACKED AT STATION 520, GND SERVICE CONNECT CUT OUT. REPAIRED SKIN IAW SRM.

Part: CREASE BEAM — DAMAGED (FUSELAGE) · airframe 68,715 hrs · 55,445 cycles

RIGHT CREASE BEAM WEB DAMAGED, BETWEEN BS 927 - 947. R & R WEB IAW DWG & SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 68,715 hrs · 55,445 cycles

RIGHT STUB BEAM LOWER FASTENER ANGLE CRACKED AT BS 616. REPAIRED ANGLE IAW EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 68,715 hrs · 55,445 cycles

FUSELAGE FLOORBEAM CORRODED, AT STATION 986, RBL 42 TO LBL 45. REPAIRED BEAM IAW SRM & EA.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 68,715 hrs · 55,445 cycles

RIGHT CREASE BEAM CORRODED AT STATION 970. REPAIRED BEAM IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 68,715 hrs · 55,445 cycles

FUSELAGE FLOORBEAM CORRODED AT STATION 986, LBL 34 - LBL 45. REPAIRED BEAM IAW SRM & EA.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 68,715 hrs · 55,445 cycles

PASSENGER LT CABIN FLOOR STRUCTURE SUPPORT CORRODED, AT BS 984, LBL 16. R & R SUPPORT IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 68,715 hrs · 55,445 cycles

RIGHT CREASE BEAM CORRODED AT BS 1002, STRINGER 17R. R & R CREASE BEAM IAW SRM & DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 68,715 hrs · 55,445 cycles

LEFT CREASE BEAM CORRODED, BETWEEN BS 986 - 992, STRINGER 17L. R & R CREASE BEAM IAW SRM & DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 68,715 hrs · 55,445 cycles

MAIN CABIN INTERCOSTAL ATTACH ANGLE CRACKED AT BS 277, STRINGER 10R. R & R INTERCOSTAL IAW DWG & SRM.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 68,715 hrs · 55,445 cycles

MAIN CABIN INTERCOSTAL ATTACH ANGLE CRACKED AT BS 290, STRINGER 10R. R & R ANGLE IAW DWG & SRM.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 68,715 hrs · 55,445 cycles

MAIN CABIN INTERCOSTAL ATTACH ANGLE CRACKED AT BS 289, STRINGER 11R. R & R ANGLE IAW DWG & SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 68,715 hrs · 55,445 cycles

LEFT STUB BEAM FRAME WEB INNER CHORD CRACKED, AT BS 639, WL 208. REPAIRED FRAME IAW EA.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 68,715 hrs · 55,445 cycles

FORWARD GALLEY DOOR SURROUND, FWD INTERCOSTAL WEB CRACKED, BETWEEN BS 277 - 291.5, STRINGER 14R. R & R INTERCOSTAL IAW SRM & EA.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 68,715 hrs · 55,445 cycles

LEFT MAIN CABIN CUSP WEB CORRODED AT BS 430, STRINGER 17L. REPAIRED WEB IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,715 hrs · 55,445 cycles

FORWARD ENTRY DOOR UPPER HINGE CUT OUT CRACKED AT BS 305, WL 258. REPAIRED CUT OUT IAW EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,715 hrs · 55,445 cycles

STRINGER CLIP CRACKED AT BS 908, STRINGER 8L. R & R CLIP IAW SRM & DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,715 hrs · 55,445 cycles

STRINGER CLIP CRACKED AT BS 360, STRINGER 8R. R & R CLIP IAW SRM & DWG.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 68,715 hrs · 55,445 cycles

RIGHT MAIN CABIN CUSP WEB CORRODED, AT BS 390. R & R CUSP WEB IAW DWG & SRM.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 68,715 hrs · 55,445 cycles

RIGHT CREASE BEAM CORRODED AT STATION 294 - 328. REPAIRED CREASE BEAM IAW SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 68,715 hrs · 55,445 cycles

R1 DOOR CUT OUT AFT FRAME STRUCTURE, T CHORD CRACKED AT BS 332, AT DOOR STOP NR 1. R & R T CHORD IAW SRM & DWG.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · airframe 68,715 hrs · 55,445 cycles

AFT CARGO VERTICAL ATTACH ANGLE CORRODED AT BS 794, STRINGER 28R. R & R ANGLE IAW SRM & DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 68,715 hrs · 55,445 cycles

CREASE BEAM CORRODED AT BS 320, RBL 58. R & R CREASE BEAM IAW SRM.

Part: SUPPORT — DAMAGED (TE FLAP) · airframe 68,715 hrs · 55,445 cycles

RIGHT WING NR 7 OTBD FLAP, INBD A FRAME SUPPORT, AFT INBD CORNER DAMAGED. R & R SUPPORT IAW SOPM.

Part: STRAP — CRACKED (FUSELAGE) · airframe 68,715 hrs · 55,445 cycles

E & E COMPARTMENT, LOWER CABIN FLOOR, STABILIZER STRAP CRACKED AT BS 328, RBL 32. REPAIRED STRAP IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 68,715 hrs · 55,445 cycles

RIGHT CREASE BEAM CORRODED AT STATION 970. REPAIRED BEAM IAW SRM.

Part: DOOR — DELAMINATED (FUSELAGE) · airframe 68,715 hrs · 55,445 cycles

FUSELAGE DOOR OTBD HINGE DELAMINATED AT BS 340, STRINGER 2R. REPAIRED DOOR IAW SRM.

Part: BULKHEAD — CRACKED (LT MLG WW) · airframe 68,715 hrs · 55,445 cycles

BULKHEAD VERTICAL WEB CRACKED, AT BS 663, LBL 33. REPAIRED WEB IAW EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 68,258 hrs · 55,148 cycles

LEFT EXIT SIGN LIGHT INOPERATIVE. R & R LIGHT ASSEMBLY IAW MM.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 66,125 hrs · 53,624 cycles

LEFT WING NR 2 SLAT TE WEDGE DELAMINATED AT THE OTBD END. R & R NR 2 SLAT IAW AMM.

Part: TAB — DAMAGED (LT AILERON) · airframe 66,125 hrs · 53,624 cycles

LEFT WING AILERON TAB DAMAGED ON THE UPPER SURFACE AT THE INBD END. R & R TAB IAW MM.

Part: SPAR — CRACKED (LT WING) · airframe 65,619 hrs · 53,295 cycles

LEFT WING REAR SPAR WEB CRACKED AT EACH FASTENER HOLE RSS 222.2, UPPER ROW, 4TH HOLE INBD. REPAIRED WEB IAW EA & ER.

Part: SPAR — CRACKED (LT WING) · airframe 65,619 hrs · 53,295 cycles

LEFT WING REAR SPAR UPPER CHORD CRACKED AT RSS 222.2. REPAIRED CHORD IAW ER & EA.

Part: SPAR — CRACKED (RT WING) · airframe 65,619 hrs · 53,295 cycles

RIGHT WING REAR SPAR UPPER CHORD CRACKED AT RSS 222.2. REPAIRED CHORD IAW ER & EA.

Part: LIGHT — LOOSE (CABIN) · airframe 64,593 hrs · 52,558 cycles

LEFT EEPLS LOOSE. SECURED EEPLS IAW SIP.

Part: LIGHT — LOOSE (CABIN) · airframe 64,593 hrs · 52,558 cycles

RIGHT EEPLS LOOSE. SECURED EEPLS IAW SIP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 63,472 hrs · 51,745 cycles

LEFT FWD GALLEY AREA EMERGENCY EXIT BULB INOPERATIVE. R & R BULB IAW MM.

Part: CROSSBEAM — CRACKED (CARGO DOOR) · airframe 63,472 hrs · 51,745 cycles

CROSSBEAM E T CHORD CRACKED ON FASTENER HOLE IN LOWER CORNER OF AFT END AFT CARGO COMPARTMENT DOOR. REPAIRED CHORD IAW EA.

Part: SKIN — CRACKED (LE SLAT) · airframe 63,472 hrs · 51,745 cycles

RIGHT WING LE KRUEGER FLAP SEAL DOOR SKIN CRACKED AT WBL 213. REPAIRED SKIN IAW EA.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 63,472 hrs · 51,745 cycles

STRINGER CHANNEL CRACKED AT BS 727, STRINGER 22L. R & R CHANNEL IAW SRM & DWG.

Part: FLAP — DELAMINATED (RT WING) · airframe 63,472 hrs · 51,745 cycles

RIGHT WING OTBD AFT FLAP DELAMINATED. REPAIRED AFT FLAP IAW SRM.

Part: FLAP — DELAMINATED (RT WING) · airframe 63,472 hrs · 51,745 cycles

RIGHT WING INBD FORE FLAP DELAMINATED. REPAIRED FORE FLAP IAW SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 63,472 hrs · 51,745 cycles

DOME CAP WEB CRACKED AT BS 1016, STRINGER 15R. REPAIRED WEB IAW SRM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 63,472 hrs · 51,745 cycles

LEFT WING INBD FORE FLAP UPPER SURFACE DELAMINATED. REPAIRED FORE FLAP IAW SRM.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 63,472 hrs · 51,745 cycles

SUPPORT ANGLE CORRODED AT BS 440 + 14, STRINGER 18R. R & R ANGLE IAW SRM & DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 63,472 hrs · 51,745 cycles

FRAME SHEAR TIE CORRODED AT BS 344, BETWEEN STRINGER 26R TO STRINGER 27R. R & R SHEAR TIE IAW SRM & DWG.

Part: FITTING — LOOSE (TE FLAP) · airframe 63,472 hrs · 51,745 cycles

LEFT WING OTBD FORE FLAP NR 2 CARRIAGE FITTING LOOSE. SECURED FITTING IAW MM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 63,472 hrs · 51,745 cycles

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

Part: WEB — CRACKED (FUSELAGE) · airframe 63,472 hrs · 51,745 cycles

WEB CRACKED BETWEEN BS 351 TO BS 360, BETWEEN STRINGER 28L TO STRINGER 28R. R & R WEB IAW SRM & DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 63,472 hrs · 51,745 cycles

WEB CRACKED BETWEEN BS 312 TO BS 318, BETWEEN STRINGER 28L TO STRINGER 28R. R & R WEB IAW SRM & DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 63,472 hrs · 51,745 cycles

ANGLE CRACKED AT BS 328, LBL 46. R & R ANGLE IAW SRM & DWG.

Part: BEARING — BROKEN (TE FLAP) · airframe 63,472 hrs · 51,745 cycles

LEFT WING NR 2 A FRAME FLAP TRACK CARRIAGE BEARING BROKEN. R & R BEARING IAW CMM.

Part: WEB — CRACKED (FUSELAGE) · airframe 63,472 hrs · 51,745 cycles

WEB CRACKED AT BS 303, BETWEEN STRINGER 27R TO STRINGER 28L. R & R WEB IAW SRM & DWG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 63,472 hrs · 51,745 cycles

CLIP CRACKED AT BS 320, STRINGER 21L. R & R CLIP IAW SRM & DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 63,472 hrs · 51,745 cycles

SUPPORT ANGLE CRACKED AT BS 540, RBL 1. R & R ANGLE IAW SRM & DWG.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 63,472 hrs · 51,745 cycles

INNER CHORD CRACKED AT BS 348.2, STRINGER 17L. R & R CHORD IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 63,472 hrs · 51,745 cycles

TIE CLIP CRACKED AT BS 927, STRINGER 20L. R & R TIE CLIP IAW SRM & DWG.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 63,472 hrs · 51,745 cycles

CHANNEL CRACKED AT BS 540, RBL 1. R & R CHANNEL IAW SRM & DWG.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 63,472 hrs · 51,745 cycles

Z STIFFENER CRACKED AT BS 1016, STRINGER 21R. REPAIRED Z STIFFENER IAW EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 63,472 hrs · 51,745 cycles

FRAME CORRODED AT BS 727D, BETWEEN STRINGER 26R TO STRINGER 27R. REPAIRED FRAME IAW SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 63,472 hrs · 51,745 cycles

STRINGER CORRODED AT BS 967, STRINGER 27L. REPAIRED STRINGER IAW SRM.

Part: STRUCTURE — CRACKED (LT WING) · airframe 63,472 hrs · 51,745 cycles

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

Part: SHEAR WEB — CRACKED (FUSELAGE) · airframe 63,472 hrs · 51,745 cycles

SHEAR WEB CRACKED AT BS 348.2, STRINGER 16L. REPAIRED WEB IAW EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 63,472 hrs · 51,745 cycles

FRAME CORRODED AT BS 807, BETWEEN STRINGER 27L TO STRINGER 26L. REPAIRED FRAME IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,472 hrs · 51,745 cycles

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

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 63,472 hrs · 51,745 cycles

CHANNEL CRACKED AT BS 540, LBL 1. R & R CHANNEL IAW SRM & DWG.

Part: SHEAR WEB — CRACKED (FUSELAGE) · airframe 63,472 hrs · 51,745 cycles

SHEAR WEB CRACKED AT BS 348.2, STRINGER 17L. REPAIRED WEB IAW EA.

Part: WEB — CRACKED (FUSELAGE) · airframe 63,472 hrs · 51,745 cycles

WEB CRACKED BETWEEN BS 312 TO BS 328, LBL 46. R & R WEB IAW SRM & DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 63,472 hrs · 51,745 cycles

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

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 63,472 hrs · 51,745 cycles

STIFFENER CRACKED BETWEEN BS 312 TO BS 328, RBL 32. R & R STIFFENER IAW SRM & DWG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 63,472 hrs · 51,745 cycles

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

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 63,472 hrs · 51,745 cycles

TIE CLIP CRACKED AT BS 787, STRINGER 21R. R & R TIE CLIP IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,472 hrs · 51,745 cycles

FUSELAGE FRAME CRACKED AT STATION 947.5, STRINGER 26R. REPAIRED FRAME IAW EA.

Part: FITTING — CRACKED (FUSELAGE) · airframe 63,472 hrs · 51,745 cycles

CLIP CRACKED AT BS 348.2, STRINGER 16L. R & R CLIP IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,472 hrs · 51,745 cycles

FRAME CRACKED AT BS 947.5, STRINGER 19L. R & R FRAME IAW SRM & DWG.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 63,472 hrs · 51,745 cycles

FLOORBEAM UPPER FLANGE CRACKED AT BS 328, BL 0. REPAIRED FLOORBEAM IAW SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 63,472 hrs · 51,745 cycles

TIE CLIP CRACKED AT BS 967, LBL 3. R & R TIE CLIP IAW SRM & DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 63,472 hrs · 51,745 cycles

WEB CRACKED AT BS 360, BL 0. R & R WEB IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 63,472 hrs · 51,745 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,472 hrs · 51,745 cycles

FRAME CRACKED AT BS 492.4, STRINGER 24R. R & R FRAME IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,472 hrs · 51,745 cycles

FUSELAGE SKIN CRACKED AT BS 344.5, STRINGER 17L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,472 hrs · 51,745 cycles

FUSELAGE SKIN CRACKED AT BS 340, STRINGER 17L. REPAIRED SKIN IAW EA.

Part: SUPPORT CHANNEL — CORRODED (FUSELAGE) · airframe 63,472 hrs · 51,745 cycles

FRAME SUPPORT CHANNEL CORRODED AT BS 787, BETWEEN STRINGER 19L TO STRINGER 25L. R & R CHANNEL IAW SRM & DWG.

Part: ANGLE — CRACKED (NR 1 NACELLE) · airframe 63,472 hrs · 51,745 cycles

ANGLE CRACKED LOCATED INTERNAL AREA ACCESS PANEL 5757L STRUT TORQUE BOX ENG NR 1. R & R ANGLE IAW SRM & DWG.

Part: ANGLE — CRACKED (NR 1 NACELLE) · airframe 63,472 hrs · 51,745 cycles

ANGLE CRACKED ON INTERNAL AREA ACCESS PANEL 5743L AFT STRUT FAIRING ENG NR 1. R & R ANGLE IAW SRM & DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 63,472 hrs · 51,745 cycles

RIGHT SIDE NLG WHEEL WEB CRACKED AT BS 251.6+4.5, WL 169.1. REPAIRED WEB IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,472 hrs · 51,745 cycles

FRAME CRACKED AT BS 500B, BETWEEN STRINGER 20R TO STRINGER 21R. REPAIRED FRAME IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,472 hrs · 51,745 cycles

FRAME CRACKED AT BS 500D, BETWEEN STRINGER 20L TO STRINGER 21L. REPAIRED FRAME IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,472 hrs · 51,745 cycles

FUSELAGE FRAME OTBD CHORD CRACKED AT STATION 727, STRINGER 18A, RT SIDE. REPAIRED FRAME CHORD IAW EA.

Part: DOOR — CRACKED (CABIN) · airframe 63,472 hrs · 51,745 cycles

AFT ENTRY DOOR LOWER HINGE CUT OUT OF THE FWD FRAME CRACKED. R & R DOOR IAW SRM.

Part: CROSSBEAM — CRACKED (CARGO DOOR) · airframe 63,472 hrs · 51,745 cycles

AFT CARGO DOOR CROSSBEAM CHORD CRACKED AT FWD END. REPAIRED CHORD IAW EA.

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 63,472 hrs · 51,745 cycles

MAIN WW PRESS DECK WEB CRACKED AT BS 664, LBL 45.5 - 5. REPAIRED WEB IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,472 hrs · 51,745 cycles

FUSELAGE FRAME OTBD CHORD CRACKED AT STATION 727, STRINGER 18A, LT SIDE. REPAIRED FRAME CHORD IAW EA.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 63,421 hrs · 51,712 cycles

FORWARD OTBD FLASHLIGHT INOPERATIVE. R & R BATTERY IAW MM.

Part: SIGN — BROKEN (CABIN) · airframe 62,837 hrs · 51,306 cycles

AFT GALLEY RT SIDE EXIT SIGN BROKEN. REPAIRED SIGN IAW EA.

Part: SLIDE — UNSECURE (L1 DOOR) · airframe 62,861 hrs · 51,318 cycles

L1 DOOR EMERGENCY EVAC SLIDE FELL OUT. REINSTALLED SLIDE IAW MM.

Part: ANGLE — CRACKED (RT WING) · airframe 62,618 hrs · 51,166 cycles

RT WING UPPER TE PANEL ANGLE CRACKED JUST OTBD OF THE NR 2 PYLON. R & R ANGLE IAW SRM.

Part: SKIN — CRACKED (LT WING) · airframe 62,541 hrs · 51,116 cycles

LT WING FIXED LE SKIN AT NR 1 SLAT INBD AUXILIARY TRACK CUTOUT CRACKED AT OTBD EDGE. REPAIRED SKIN IAW EA.

Part: FITTING — LOOSE (R1 DOOR) · airframe 62,541 hrs · 51,116 cycles

R1 DOOR EMERGENCY EVAC SLIDE TWO EACH GIRT BAR RETAINING CLIPS LOOSE. SECURED CLIPS IAW SRM.

Part: ATTACH BRACKET — CRACKED (LT WING) · airframe 62,541 hrs · 51,116 cycles

LT WING UPPER TE PANEL TO OTBD ENGINE STRUT ATTACH BRACKET CRACKED. R & R BRACKET IAW SRM.

Part: TRANSMISSION — CORRODED (TE FLAP) · airframe 62,230 hrs · 50,887 cycles

NR 2 FLAP TRANSMISSION CORRODED AT GIMBAL ATTACH AREAS. R & R NR 2 FLAP TRANSMISSION IAW AMM.

Part: CONTROLLER — FAULTY (WINDOW HEAT) · airframe 61,582 hrs · 50,397 cycles

DIVERSION/DECLARED EMERGENCY SPARKS INTO COCKPIT FROM WINDOW RT 1 ELECTRICAL CONNECTION, TOP RT OF WINDOW. R&R RT 1 WINDOW HEAT CONTROLLER IAW M/M.

Part: BUSHING — LOOSE (LT MLG DOOR) · airframe 60,849 hrs · 49,877 cycles

LEFT MLG INNER DOOR LOOSE AT FWD HINGE. REMOVED AND REPLACED INNER DOOR FWD HINGE BUSHINGS AND ATTACH BOLT PER MM.

Part: ROD — LOOSE (LT MLG DOOR) · airframe 60,849 hrs · 49,877 cycles

LEFT MLG INNER DOOR LOOSE AT CONTROL ROD. REMOVED AND REPLACED INNER DOOR SUPPORT ROD ASSEMBLY AND TRAMMELED PER MM.

Part: BRACKET — CRACKED (R2 DOOR) · airframe 60,849 hrs · 49,877 cycles

R2 DOOR EMERGENCY EVAC SLIDE BRACKETS CRACKED. REMOVED AND REPLACED BRACKETS PER AMM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 60,119 hrs · 49,367 cycles

FLASHLIGHT IN FWD GALLEY INOP. REMOVED AND REPLACED FWD OUTBOARD FLASHLIGHT BATTERY PER M/M.

Part: SLAT — BUCKLED (RT WING) · airframe 60,099 hrs · 49,354 cycles

NR 5 SLAT BUCKLED ON TOP EDGE. REF LOG PG 8626785. REMOVED AND REPLACED NR 5 SLAT PER AMM. PERFORMED RIGHT OPS CHECK PER AMM 27-81-00-825-018. POS 5 ROBBED PART P/N OFF/ON 65C26602-312A S/N OFF PA750 S/N ON PA862

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 59,438 hrs · 48,876 cycles

FOWARD EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER M/M.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 58,331 hrs · 48,035 cycles

FWD GALLEY EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER M/M.

Part: WIRE — DAMAGED (CABIN) · airframe 57,758 hrs · 47,603 cycles

L1 DOOR OVERHEAD EMERGENCY EXIT SIGN INOP. REPAIRED WIRE IAW SWPM AND AMM.

Part: LIGHT — WORN (CABIN) · airframe 57,758 hrs · 47,603 cycles

RT EEPLS BETWEEN ROW 17 TO ROW 19 WORN. REMOVED AND REPLACED EEPLS IAW AMM.

Part: LIGHT — BROKEN (CABIN) · airframe 57,758 hrs · 47,603 cycles

LT EEPLS BROKEN AT ROW 1. REMOVED AND REPLACED EEPLS IAW AMM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 57,758 hrs · 47,603 cycles

R2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW MT.

Part: FITTING — CRACKED (FUSELAGE) · airframe 57,758 hrs · 47,603 cycles

L1 DOOR AFT CUTOUT STRINGER FITTING CRACKED AT BS 360, STR 15L. REMOVED AND REPLACED FITTING IAW SRM AND DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,758 hrs · 47,603 cycles

L1 DOOR FUSELAGE SKIN CUTOUT UPPER FWD CORNER CRACKED. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,758 hrs · 47,603 cycles

AFT CARGO DOOR CUTOUT FORWARD LOWER CORNER SKIN CRACKED. REPAIRED SKIN IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 57,758 hrs · 47,603 cycles

FLOORBEAM CHANNEL CORRODED AT BS 772, LBL 3. REMOVED AND REPLACED CHANNEL IAW EA AND SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,758 hrs · 47,603 cycles

SKIN CRACKED BETWEEN BS 664 TO BS 672, LBL 31. REPAIRED SKIN IAW SRM & AMM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 57,758 hrs · 47,603 cycles

RT HORIZONTAL STABILIZER LOWER SKIN CRACKED. REPAIRED SKIN IAW EA.

Part: HOOK — LOOSE (R2 DOOR) · airframe 57,376 hrs · 47,313 cycles

R2 DOOR EMERGENCY EVAC SLIDE GIRT BAR STORAGE HOOK LOOSE. SECURED HOOK PER M/M.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 55,464 hrs · 45,882 cycles

DURING SCHEDULED SPV CHECK FOUND, STRINGER CRACKED AT BS 727A, STR 6R. REPAIRED STRINGER PER SRM.

Part: LIGHT — BROKEN (CABIN) · airframe 55,464 hrs · 45,882 cycles

DURING SCHEDULED SPV CHECK, FOUND RT OVERHEAD EMERGENCY EXIT BULLNOSE LIGHT BROKEN AT ROW 2. REMOVED AND REPLACED LIGHT PER MM.

Part: LIGHT — BROKEN (CABIN) · airframe 55,464 hrs · 45,882 cycles

DURING SCHEDULED SPV CHECK, FOUND RT OVERHEAD EMERGENCY EXIT BULLNOSE LIGHT BROKEN BETWEEN ROW 15 TO ROW 16. REMOVED AND REPLACED LIGHT PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,464 hrs · 45,882 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 847, STR 6L. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,464 hrs · 45,882 cycles

DURING SCHEDULED SPV CHECK, FOUND FORWARD WINDOW FRAME CORNER CRACKED AT BS 360+10. REPAIRED SKIN IAW EA.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 55,464 hrs · 45,882 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 887, STR 7L. REMOVED AND REPLACED TIE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,464 hrs · 45,882 cycles

DURING SCHEDULED SPV CHECK, FOUND LOWER AFT WINDOW FRAME CORNER CRACKED AT BS 440+10. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,464 hrs · 45,882 cycles

DURING SCHEDULED SPV CHECK, FOUND LOWER AFT WINDOW FRAME CORNER CRACKED AT BS 460+10. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,464 hrs · 45,882 cycles

DURING SCHEDULED SPV CHECK, FOUND WINDOW FRAME SKIN CRACKED AT BS 500B+10 UPPER FORWARD WINDOW FRAME CORNER. REPAIRED SKIN PER BAC DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,464 hrs · 45,882 cycles

DURING SCHEDULED SPV CHECK, FOUND WINDOW FRAME SKIN CRACKED AT BS 380+10, UPPER FORWARD WINDOW FRAME CORNER. REPAIRED SKIN PER EA.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 55,464 hrs · 45,882 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CORRODED AT BS 360+5, STR 11R. REPAIRED SPLICE PER SRM.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 55,464 hrs · 45,882 cycles

DURING SCHEDULED SPV CHECK, FOUND RT WINDOW FRAME CRACKED AT BS 420+10. REPAIRED FRAME PER TC.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 55,464 hrs · 45,882 cycles

DURING SCHEDULED SPV CHECK, FOUND RT WINDOW FRAME CRACKED AT BS 400+10. REPAIRED FRAME PER TC.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 55,464 hrs · 45,882 cycles

DURING SCHEDULED SPV CHECK, FOUND LT WINDOW FRAME CRACKED AT BS 500+10. REPAIRED FRAME PER TC.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 55,464 hrs · 45,882 cycles

DURING SCHEDULED SPV CHECK, FOUND LT WINDOW FRAME CRACKED AT BS 420+10. REPAIRED FRAME PER TC.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,464 hrs · 45,882 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 887, STR 2L. REMOVED AND REPLACED CLIP PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 55,464 hrs · 45,882 cycles

DURING SCHEDULED SPV CHECK, FOUND RT FRAME SHEAR TIE CRACKED AT BS 460+10. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 55,464 hrs · 45,882 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CRACKED AT BS 540, STR 10R. REMOVED AND REPLACED SPLICE PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 55,464 hrs · 45,882 cycles

DURING SCHEDULED SPV CHECK FOUND, STRINGER CRACKED AT BS 500D+12, STR 5R. REMOVED AND REPLACED STRINGER PER SRM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 54,611 hrs · 45,261 cycles

DURING SCHEDULED MV1 CHECK, FOUND LT EMERGENCY EXIT LIGHT BROKEN AT ROW 10. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: COVER — LOOSE (CABIN) · airframe 54,411 hrs · 45,101 cycles

DURING SCHEDULED MV1 CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT COVER LOOSE. SECURED COVER PER MM.

Part: ACTUATOR — FAULTY (FUEL CROSSFEED) · airframe 54,140 hrs · 44,892 cycles

DIVERSION - CROSS FEED FUEL VALVE OPEN LIGHT ILLUMINATED AND WOULD NOT GO OUT DURING FUEL BALANCE. REMOVED AND REPLACED CROSS FEED VALVE ACTUATOR PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,100 hrs · 44,863 cycles

DURING SCHEDULED RON CHECK, FOUND SKIN CRACKED AT BS 510.5A, STR 10L. REPAIRED SKIN PER EA.

Part: SIGN — BROKEN (CABIN) · airframe 53,975 hrs · 44,762 cycles

DURING SCHEDULED MV1 CHECK, FOUND R1 DOOR EMERGENCY EXIT SIGN ASSY BROKEN. REMOVED AND REPLACED SIGN ASSY. PER MM.

Part: LENS — LOOSE (CABIN) · airframe 53,908 hrs · 44,713 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND RT EEPLS LENS LOOSE. SECURED LENS PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 53,838 hrs · 44,666 cycles

R1 DOOR EMERGENCY EXIT LIGHT ASSY LOOSE. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SIGN — BROKEN (EMERGENCY LIGHTS) · airframe 53,460 hrs · 44,376 cycles

FWD GALLEY EMERGENCY EXIT SIGN COVER BROKEN. REMOVED AND REPLACED SIGN ASSY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,071 hrs · 44,076 cycles

DURING SCHEDULED 16Y CHECK, FOUND SKIN CRACKED AT BS 510C, BETWEEN STR 6L TO STR 13L. REPAIRED SKIN PER EO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,071 hrs · 44,076 cycles

DURING SCHEDULED 16Y CHECK, FOUND SKIN CRACKED BETWEEN BS 767 TO BS 807, BETWEEN STR 10L TO STR 14L. REPAIRED SKIN PER EO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,071 hrs · 44,076 cycles

DURING SCHEDULED 16Y CHECK, FOUND SKIN CRACKED BETWEEN BS 767 TO STR 807, STR 10L TO STR 14L. REPAIRED SKIN PER EO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,071 hrs · 44,076 cycles

DURING SCHEDULED 16Y CHECK, FOUND SKIN CRACKED AT BS 510, BETWEEN STR 10L TO STR 13L. REPAIRED SKIN PER EO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,071 hrs · 44,076 cycles

DURING SCHEDULED 16Y CHECK, FOUND SKIN CRACKED AT BS 490, RT UPPER FORWARD CORNER. REPAIRED SKIN PER EO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,071 hrs · 44,076 cycles

DURING SCHEDULED 16Y CHECK, FOUND SKIN CRACKED AT BS 510A, BETWEEN STR 10L TO STR 11L. REPAIRED SKIN PER EO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,071 hrs · 44,076 cycles

DURING SCHEDULED 16Y CHECK, FOUND SKIN CRACKED AT BS 510B, STR 13L. REPAIRED SKIN PER EO.

Part: SLAT — DELAMINATED (LT WING) · airframe 53,071 hrs · 44,076 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,071 hrs · 44,076 cycles

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

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 53,071 hrs · 44,076 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,071 hrs · 44,076 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,071 hrs · 44,076 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 663.75, STR 10R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,071 hrs · 44,076 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 5R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 53,071 hrs · 44,076 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO COMPT CHANNEL CORRODED AT BS 944, LBL 3. REPAIRED CHANNEL PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,071 hrs · 44,076 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 26L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,071 hrs · 44,076 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,071 hrs · 44,076 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 11L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,071 hrs · 44,076 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,071 hrs · 44,076 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 11R. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — DELAMINATED (FOREFLAP) · airframe 53,071 hrs · 44,076 cycles

DURING SCHEDULED 16Y CHECK, FOUND LT WING I/B FORE FLAP UPPER SURFACE DELAMINATED BETWEEN WBL 147 TO WBL 151. REPAIRED FORE FLAP PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 53,071 hrs · 44,076 cycles

DURING SCHEDULED 16Y CHECK, FOUND WEB CRACKED BETWEEN BS 277 TO BS 291, STR 14R. REMOVED AND REPLACED WEB PER SRM AND BAC DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 53,071 hrs · 44,076 cycles

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

Part: TAB — DELAMINATED (LT ELEVATOR) · airframe 53,071 hrs · 44,076 cycles

DURING SCHEDULED 16Y CHECK, FOUND LT ELEVATOR TAB DELAMINATED BETWEEN STA 41 TO STA 42. REPAIRED ELEVATOR TAB PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,071 hrs · 44,076 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 4L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: FLAP — DELAMINATED (LT WING) · airframe 53,071 hrs · 44,076 cycles

DURING SCHEDULED 16Y CHECK, FOUND LT WING O/B FORE FLAP DELAMINATED BETWEEN WBL 320.69 TO WBL 323.69. REPAIRED FORE FLAP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,071 hrs · 44,076 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 28R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: LENS — BROKEN (CABIN) · airframe 53,071 hrs · 44,076 cycles

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

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 53,071 hrs · 44,076 cycles

DURING SCHEDULED 16Y CHECK, FOUND SUPPORT ANGLE CRACKED AT BS 639, RBL 45.5. REMOVED AND REPLACED ANGLE PER SRM AND BAC DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,071 hrs · 44,076 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CRACKED AT BS 520, STR 21L. REPAIRED FRAME PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 53,071 hrs · 44,076 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 1006, BETWEEN STR 27L TO STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,071 hrs · 44,076 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 28L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,071 hrs · 44,076 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 11L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,071 hrs · 44,076 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 440, STR 20R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,071 hrs · 44,076 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 25R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,071 hrs · 44,076 cycles

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

Part: WEB — CRACKED (FUSELAGE) · airframe 53,071 hrs · 44,076 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO COMPT DOOR CUTOUT WEB CRACKED AT BS 794.3, STR 23R. REMOVED AND REPLACED WEB PER SRM AND BAC DWG.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 53,071 hrs · 44,076 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM CHORD CRACKED AT BS 727B, LBL 24.8. REPAIRED BEAM PER EO.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,071 hrs · 44,076 cycles

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

Part: SLAT — DELAMINATED (LT WING) · airframe 53,071 hrs · 44,076 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,071 hrs · 44,076 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 25L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: FITTING — WORN (GIRT BAR) · airframe 53,071 hrs · 44,076 cycles

DURING SCHEDULED 16Y CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE BOTH GIRT BAR FITTING WORN. REMOVED AND REPLACED FITTING PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,071 hrs · 44,076 cycles

DURING SCHEDULED 16Y CHECK, FOUND SKIN CRACKED AT BS 959, STR 17R. REPAIRED SKIN PER EO.

Part: FITTING — WORN (GIRT BAR) · airframe 53,071 hrs · 44,076 cycles

DURING SCHEDULED 16Y CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE BOTH GIRT BAR FITTING WORN. REMOVED AND REPLACED FITTING PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,071 hrs · 44,076 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 27L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,071 hrs · 44,076 cycles

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

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 53,071 hrs · 44,076 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CRACKED AT BS 294.5, STR 11R. REPAIRED SHEAR TIE PER EO.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 53,071 hrs · 44,076 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM CORRODED AT BS 947, BETWEEN LBL 21 TO RBL 5. REPAIRED BEAM PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,071 hrs · 44,076 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 26L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,071 hrs · 44,076 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 420, STR 28L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 53,071 hrs · 44,076 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 993.5, STR 17R. REPAIRED FRAME PER EO.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 53,071 hrs · 44,076 cycles

DURING SCHEDULED 16Y CHECK, FOUND FWD EMERGENCY EXIT FLASHLIGHT BATTERY INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,071 hrs · 44,076 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 663.75, STR 10L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,071 hrs · 44,076 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 10R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: BATTERY — BROKEN (FLASHLIGHT) · airframe 53,071 hrs · 44,076 cycles

DURING SCHEDULED 16Y CHECK, FOUND FWD EMERGENCY EXIT FLASHLIGHT BROKEN. REMOVED AND REPLACED BATTERY PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,071 hrs · 44,076 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 16L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,071 hrs · 44,076 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 420, STR 16R. REMOVED AND REPLACED CLIP PER SRM.

Part: DOUBLER — DELAMINATED (L1 DOOR) · airframe 53,071 hrs · 44,076 cycles

DURING SCHEDULED 16Y CHECK, FOUND L1 DOOR DOUBLER AFT UPPER EDGE OF EXTERNAL SURFACE DELAMINATED. REMOVED AND REPLACED DOUBLER PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 53,071 hrs · 44,076 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM CORRODED AT BS 328, LBL 28. REPAIRED BEAM PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,510 hrs · 43,658 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 511B, STR 2R. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,508 hrs · 43,656 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 509B, STR 2R. REPAIRED SKIN PER EA.

Part: LENS — BROKEN (R1 DOOR) · airframe 52,448 hrs · 43,612 cycles

R1 DOOR EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LIGHT & LENS ASSY PER MM.

Part: FLAP — DELAMINATED (LT WING) · airframe 52,222 hrs · 43,449 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,222 hrs · 43,449 cycles

DURING SCHEDULED HC2 CHECK, FOUND SKIN CRACKED AT BS 507C, STR 10L. REPAIRED SKIN PER EA.

Part: SLIDE — OUT OF LIMITS (R2 DOOR) · airframe 51,745 hrs · 43,111 cycles

R2 DOOR EMERGENCY EVAC SLIDE PRESSURE GAUGE OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MT.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,507 hrs · 42,924 cycles

DURING SCHEDULED CV CHECK, FOUND SKIN CRACKED BETWEEN BS 477 TO BS 487, STR 2R. REPAIRED SKIN PER SRM.

Part: FLAP — DELAMINATED (LT WING) · airframe 50,709 hrs · 42,318 cycles

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

Part: SIGN — LOOSE (CABIN) · airframe 50,652 hrs · 42,275 cycles

FWD GALLEY EMERGENCY EXIT SIGN COVER LOOSE. REMOVED AND REPLACED SIGN PER MM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 50,126 hrs · 41,907 cycles

DURING SCHEDULED 1/2D CHECK, FOUND AFT EMERGENCY FLASHLIGHT BATTERY VOLTAGE LOW. REMOVED AND REPLACED BATTERY PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 49,754 hrs · 41,631 cycles

DURING SCHEDULED MV3 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: WIRE — DAMAGED (CABIN) · airframe 49,608 hrs · 41,522 cycles

DURING SCHEDULED MV1 CHECK, FOUND OVERHEAD EMERGENCY EXIT LIGHT INOP AT ROW 1. REPAIRED WIRE PER WDM.

Part: LIGHT — BROKEN (CABIN) · airframe 49,318 hrs · 41,316 cycles

EMERGENCY EXIT KORRY LIGHT BROKEN. REMOVED AND REPLACED LIGHT PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,008 hrs · 41,090 cycles

DURING SCHEDULED HC2 CHECK, FOUND L2 DOOR LOWER FWD CORNER FUSELAGE SKIN CUTOUT CRACKED. REPAIRED SKIN PER SRM.

Part: SKIN — DELAMINATED (FOREFLAP) · airframe 49,008 hrs · 41,090 cycles

DURING SCHEDULED HC2 CHECK, FOUND RT WING I/B FORE FLAP UPPER SURFACE DELAMINATED. REMOVED AND REPLACED FOREFLAP PER MM.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 52,643 hrs · 44,955 cycles

DURING SCHEDULED 14Y CHECK, FOUND LT WING NR 1 L/E SLAT DELAMINATED AT LOWER SKIN. REPAIRED SLAT PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,937 hrs · 41,036 cycles

DURING SCHEDULED 14Y CHECK, FOUND RADIO ALTIMETER ANTENNA SKIN CUTOUT CRACKED AT BS 413, RBL 3. REPAIRED SKIN PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,937 hrs · 41,036 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,937 hrs · 41,036 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,937 hrs · 41,036 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,937 hrs · 41,036 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,937 hrs · 41,036 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,937 hrs · 41,036 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 867, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,937 hrs · 41,036 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 48,937 hrs · 41,036 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 8L. REMOVED AND REPLACED CLIP PER SRM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 47,543 hrs · 40,007 cycles

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

Part: LENS — BROKEN (CABIN) · airframe 47,323 hrs · 39,834 cycles

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

Part: FITTING — LOOSE (GIRT BAR) · airframe 45,931 hrs · 38,824 cycles

DURING SCHEDULED HC2 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING LOOSE. SECURED FITTING PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 45,750 hrs · 38,685 cycles

DURING SCHEDULED MV2 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 2 ABC. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 45,739 hrs · 38,676 cycles

DURING SCHEDULED MV2 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 2 ABC. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: GUSSET — CRACKED (NLG W/W) · airframe 42,554 hrs · 36,197 cycles

DURING SCHEDULED MV2 CHECK, FOUND NLG W/W GUSSETT CRACKED. REMOVED AND REPLACED GUSSETT PER SRM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 42,462 hrs · 36,115 cycles

DURING SCHEDULED 12Y CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: BEARING — WORN (ELEVATOR TAB) · airframe 43,462 hrs · 36,115 cycles

DURING SCHEDULED 12Y CHECK, RIGHT ELEVATOR FAILED FREE PLAY CHECK. REMOVED AND REPLACED ELEVATOR CONTROL ROD BUSHING, BEARING AND SLEEVE PER MM.

Part: GLOWSTRIP — WORN (CABIN) · airframe 42,227 hrs · 35,935 cycles

DURING SCHEDULED C3 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP WORN AT ROW 7 DEF. REMOVED AND REPLACED STRIP PER MM.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 35,366 hrs · 41,495 cycles

FWD INBOARD EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT BATTERY PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 41,321 hrs · 35,231 cycles

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

Part: LENS — LOOSE (CABIN) · airframe 41,259 hrs · 35,187 cycles

DURING SCHEDULED C2 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LIGHT LENS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 41,259 hrs · 35,187 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 1000, STR 5R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 40,366 hrs · 34,482 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT E&E COOLING EXHAUST PORT, BS 378.5, LBL 3. REPAIRED SKIN PER SWA EA.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 40,366 hrs · 34,482 cycles

DURING SCHEDULED C1 CHECK, FOUND AFT RIGHT EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 40,366 hrs · 34,482 cycles

DURING SCHEDULED C1 CHECK, FOUND LEFT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 38,706 hrs · 33,229 cycles

DURING SCHEDULED SERVICE CHECK, FOUND AFT CABIN INBD EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT BATTERY PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 38,561 hrs · 33,105 cycles

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

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 38,449 hrs · 33,008 cycles

DURING SCHEDULED C3 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 38,449 hrs · 33,008 cycles

DURING SCHEDULED C3 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: FAN BLADE — SHINGLED (NR 2 ENGINE) · airframe 37,695 hrs · 32,401 cycles

VIBRATION FELT THROUGHOUT FLIGHT - NOTICEABLY LOUD UPON LANDING DURING REVERSE THRUST OPERATIONS. FOUND SEVERAL FAN BLADES ON NR 2 ENGINE DAMAGED & SHINGLED. REMOVED AND REPLACED NR 2 ENGINE FAN BLADE SET PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 36,608 hrs · 31,508 cycles

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

Part: FITTING — CRACKED (FUSELAGE) · airframe 34,615 hrs · 29,984 cycles

DURING SCHEDULED C3 CHECK, FOUND FWD ENTRY DOOR UPPER HINGE BOX FITTING CRACKED. REMOVED AND REPLACED UPPER HINGE BOX PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 34,615 hrs · 29,984 cycles

DURING SCHEDULED C3 CHECK, FOUND OVERHEAD OVERWING EMERGENCY EXIT LIGHT ASSEMBLY LOOSE. SECURED LIGHT ASSEMBLY PER MM.

Part: FITTING — CORRODED (VERTICAL STAB) · airframe 34,016 hrs · 29,504 cycles

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

Part: FLOORBEAM — CRACKED (BS 178) · airframe 34,016 hrs · 29,504 cycles

DURING SCHEDULED D CHECK, FOUND FLOORBEAM WEB AT BS 178 TO BS 182, LBL 24 TO LBL 37, CRACKED. REMOVED AND REPLACED FLOORBEAM WEB SECTION PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,016 hrs · 29,504 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,016 hrs · 29,504 cycles

DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 303.9, STRINGER 16L, CRACKED. REPAIRED FRAME SECTION PER SB.

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,016 hrs · 29,504 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,016 hrs · 29,504 cycles

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

Part: STRINGER CLIP — CRACKED (BS 460) · airframe 34,016 hrs · 29,504 cycles

DURING SCHEDULED D CHECK, FOUND STRINGER CLIP AT BS 460, STRINGER 16R CRACKED. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 34,016 hrs · 29,504 cycles

DURING SCHEDULED D-CHECK, FOUND RT CREASE BEAM WEBS AT BS 360 TO BS 380, BS 500A TO BS 500B, CORRODED. REMOVED AND REPLACED CREASE BEAM WEBS PER SRM.

Part: SKIN — CRACKED (RT WING SLAT) · airframe 34,016 hrs · 29,504 cycles

DURING SCHEDULED D-CHECK, FOUND RT WING NR 6 L/E SLAT SKIN, CRACKED. REPAIRED NR 6 L/E SLAT SKIN PER SRM.

Part: FRAME — CRACKED (BS 907) · airframe 34,016 hrs · 29,504 cycles

DURING SCHEDULED D CHECK, FOUND FRAME AT BS 907, STRINGER 9L AND STRINGER 9R, CRACKED. REPAIRED FRAME SECTION PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 34,061 hrs · 29,504 cycles

DURING SCHEDULED D-CHECK, FOUND CREASE BEAM WEB AT BS 727B TO BS 942, RBL 68 TO RBL 57, CORRODED. REMOVED AND REPLACED CREASE BEAM WEB SECTIONS PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 34,016 hrs · 29,504 cycles

DURING SCHEDULED D-CHECK, FOUND CREASE BEAM WEB AT BS 460 TO BS 466, RBL 70, CORRODED. REMOVED AND REPLACED CREASE BEAM WEB PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 34,016 hrs · 29,504 cycles

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM AT BS 294, RBL 53, CORRODED. REPAIRED CHORD PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 34,016 hrs · 29,504 cycles

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM AT BS 270, RBL 11, CORRODED. REMOVED AND REPLACED CHORD PER SRM.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 33,941 hrs · 29,444 cycles

FWD ENTRY DOOR OVERHEAD EMERGENCY EXIT LIGHT LENS COVER MISSING. REPLACED LIGHT LENS PER MM.

Part: ACTUATOR — FAULTY (NLG) · airframe 32,553 hrs · 28,329 cycles

AIRTURN BACK, ON TAKEOFF, NOSE GEAR WOULD NOT RETRACT. RETURNED TO HOU WITH 3 GREEN GEAR LIGHTS. GEAR EXTENDED NORMALLY. REMOVED AND REPLACED NOSE GEAR RETRACT ACTUATOR PER MM.

Part: LANDING GEAR — MALFUNCTIONED (MAINS) · airframe 31,203 hrs · 27,281 cycles

AIR TURNBACK, NLG WOULD NOT RETRACT, RED UNSAFE ILLUMINATED. RECYCLED GEAR, SAME INDICATION. C/W NLG EXTENSION AND RETRACTION TEST PER MM, NO DEFECTS NOTED. REMOVED AND REPLACED M1214 AND M1215 CIRCUIT CARDS PER MM FOR COMPANY CONV.

Part: GIRT BAR — OUT OF ADJUST (ESCAPE SLIDE) · airframe 30,862 hrs · 27,006 cycles

DURING SCHEDULED C3 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: GIRT BAR — OUT OF ADJUST (ESCAPE SLIDE) · airframe 30,862 hrs · 27,006 cycles

DURING SCHEDULED C3 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: SLIDE — DISLODGED (FWD PAX DOOR) · airframe 30,102 hrs · 26,409 cycles

FWD ENTRY DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT OF THE CONTAINER. REINSTALLED SLIDE PER MM.

Part: FLAP — DELAMINATED (LT WING) · airframe 28,026 hrs · 24,728 cycles

DURING SCHEDULED C4 CHECK, FOUND LT INBD AFT T/E FLAP DELAMINATED. REMOVED AND REPLACED INBD AFT T/E FLAP PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 25,717 hrs · 22,897 cycles

DURING SCHEDULED 1/4D CHECK, FOUND LT WINDOW POST SKIN CRACKED BETWEEN NR 1 WINDOW UPPER OTBD CORNER AND NR 2 WINDOW UPPER FWD CORNER. REPAIRED SKIN PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 25,712 hrs · 22,889 cycles

DURING SCHEDULED 1/4D CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 178, WL 219 TO 234, RBL 17.1. REMOVED AND REPLACED VERTICAL BEAM WEB PER SRM.

Part: LENS — LOOSE (CABIN) · airframe 25,712 hrs · 22,889 cycles

DURING SCHEDULED 1/4D CHECK, FOUND EMERGENCY EXIT LENS LOOSE ON CEILING PANEL AT ROW 3. SECURED LENS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,416 hrs · 22,644 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EEPLS LIGHT INOP AT EMERGENCY EXIT ROW. REMOVED AND REPLACED EEPLS LIGHT PER MM.

Part: WIRE — BROKEN (CABIN) · airframe 24,864 hrs · 22,180 cycles

EEPLS WIRE BROKEN AT ROW 13. REMOVED AND REPLACED TRACK COVER AND REPAIRED WIRE PER MM.

Part: LENS — MISSING (ENTRY DOOR) · airframe 23,339 hrs · 20,901 cycles

DURING SCHEDULED C3 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EXIT LIGHT MISSING LENS. INSTALLED EMERGENCY EXIT LIGHT LENS PER MM.

Part: SLIDE — OUT OF ADJ (SERVICE DOOR) · airframe 23,339 hrs · 20,901 cycles

DURING SCHEDULED C3 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUSTMENT. ADJUSTED EMERGENCY EVAC SLIDE GIRT ASSY PER MM.

Part: SLIDE — OUT OF ADJ (ENTRY DOOR) · airframe 23,339 hrs · 20,901 cycles

DURING SCHEDULED C3 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE OUT OF ADJUSTMENT. ADJUSTED EMERGENCY EVAC SLIDE PER MM.

Part: WIRE — EXPOSED (CABIN) · airframe 22,938 hrs · 20,560 cycles

EEPLS WIRING EXPOSED & LENS MISSING AT OVERWING EXIT. SECURED WIRING & INSTALLED LENS PER MM.

Part: COVER — BROKEN (CABIN) · airframe 22,446 hrs · 20,153 cycles

DURING SCHEDULED C2 CHECK, FOUND EEPLS TRACK COVERS BROKEN AT ROWS 2 & 13. REMOVED AND REPLACED TRACK COVERS PER MM.

Part: COVER — MISSING (CABIN) · airframe 22,363 hrs · 20,080 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EEPLS TRACK COVER MISSING AT ROW 19. INSTALLED TRACK COVER PER MM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 20,815 hrs · 18,821 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BS 178 BULKHEAD CRACKED, LBL 5, WL 201 AND WL 199. REPAIRED BULKHEAD PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 20,807 hrs · 18,810 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BS 178 BULKHEAD BOTH LT AND RT SIDE CHORDS CRACKED, WL 207. REMOVED AND REPLACED BOTH CHORDS PER ACO.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 20,807 hrs · 18,818 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BS 178 BULKHEAD CRACKED, RBL 5. REPAIRED BULKHEAD PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 20,807 hrs · 18,810 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BS 178 BULKHEAD CRACKED RBL 5, WL 201. REPAIRED BULKHEAD PER SRM.

Part: COVER — MISSING (CABIN) · airframe 20,327 hrs · 18,390 cycles

EEPLS TRACK COVER MISSING AT ROW 2. INSTALLED TRACK COVER PER MM.

Part: LENS — LOOSE (CABIN)

DURING SCHEDULED C2 CHECK, FOUND LT EMERGENCY OVERWING EXIT LENS LOOSE. RESECURED LENS ASSY PER MM.

Part: FAN — OVER HEATED (E&E COMP)

DECLARED EMERGENCY LANDING, DURING FLIGHT A SMOKE/BURNING SMELL IN COCKPIT. DISCOVERED EQUIPMENT COOLING FAN OVERHEATED AND C/B TRIPPED. DEFERRED PER MEL AND DURING RON REMOVED AND REPLACED EQUIPMENT COOLING FAN PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING SCHEDULED 1/2D CHECK, FOUND FWD CABIN EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: POWER UNIT — INOPERATIVE (CABIN)

FWD OUTBD EMERGENCY FLASHLIGHT NOT CHARGING. REMOVED AND REPLACED FWD OUTBOARD FLASHLIGHT POWER UNIT PER MM.

Part: COFFEEMAKER — FAILED (CABIN)

FLIGHT ATTENDANTS REPORTED ACRID, ELECTRICAL TYPE FUMES AFTER TAKEOFF IN AFT GALLEY AREA. AIRCRAFT RETURNED TO PHX. REMOVED AND REPLACED NR 2 AFT COFFEEMAKER C/B AND BOTH AFT COFFEEMAKERS. RAN ENGS, BOTH PACKS SEVERAL DIFFERENT AFT GALLEY PWR CONFIGURATIONS. SMELL NO LONGER EXISTS.

Part: HSI — INOP (NR 1)

A/C DIVERTED TO LAS FOR NR 1 HEADING FLAG AND FROZEN COMPASS CARD. REPLACED HSI PER BOEING M/M.

Part: CUTOUT LIP — CRACKED (FUSELAGE)

DURING SCHEDULED C1 CHECK, FOUND GROUND PWR CUTOUT CRACKED AT AFT MIDDLE LIP THROUGH TO RIVET .125 INCH LONG. PERMANENTLY REPAIRED PER SWA RA NR 1-353-1899.

Part: JAMB — CRACKED (EXT POWER DOOR)

DURING SCHEDULED C-CHECK, FOUND EXTERNAL POWER DOOR JAMB CRACKED, 1.5 INCH LENGTH. REPAIRED PER SWA RA 1-353-1447.