N524SW

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 71,407 hrs · 67,061 cycles

INTERCOSTAL CRACKED, BETWEEN BS 482 - 482A, STRINGER 26L. R & R INTERCOSTAL IAW SRM & DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,407 hrs · 67,061 cycles

SKIN CRACKED AT BS 787+3, STRINGER 17L. REPAIRED SKIN IAW ER & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,407 hrs · 67,061 cycles

SKIN CRACKED AT BS 360+2, STRINGER 5R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,407 hrs · 67,061 cycles

SKIN CRACKED, BETWEEN BS 892.5 - 894, STRINGER 2L. REPAIRED SKIN IAW ER & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,407 hrs · 67,061 cycles

SKIN CRACKED, BETWEEN BS 346 - 347, STRINGER 2L. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,407 hrs · 67,061 cycles

SKIN CRACKED, BETWEEN BS 482A+4.5 - 482A+5.5, STRINGER 26L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,407 hrs · 67,061 cycles

SKIN CRACKED AT BS 360+2, STRINGER 6R. REPAIRED SKIN IAW SRM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 71,309 hrs · 66,958 cycles

AFT ENTRY EMER EXTERIOR LIGHT LOW. R & R BATTERY PACK ASSEMBLY IAW AMM.

Part: BATTERY — FAULTY (CABIN) · airframe 70,832 hrs · 66,405 cycles

L2 DOOR EMER EXIT LIGHT FAULTY. R & R BATTERY IAW MM.

Part: MODULE — FAULTY (LT MLG) · airframe 70,799 hrs · 66,367 cycles

LEFT MLG DID NOT EXTEND VIA GEAR HANDLE. USING EMER CHECKLIST LOWERED LT GEAR VIA EMER GEAR HANDLE. R & R LT MLG MODULAR PACKAGE IAW AMM.

Part: ACTUATOR — FAULTY (LT MLG) · airframe 70,669 hrs · 66,212 cycles

DECLARED EMER, UPON LG EXTENSION, LT MAIN GEAR UNSAFE LIGHT ILLUMINATED, RED. COMPLIED WITH CHECK LIST FOR MANUAL GEAR EXTENSION & UPON PULLING T HANDLE FOR LT GEAR, RECEIVED LT GEAR SAFE, GREEN, INDICATION. R & R LT MLG UPLOCK ACTUATOR IAW MM.

Part: ACTUATOR — FAULTY (LT MLG) · airframe 70,669 hrs · 66,212 cycles

LEFT MLG INDICATED UNSAFE, RED LIGHT ONLY, AFTER EXTENSION. HANDLE SEATED, NOSE LANDING RT MAIN INDICATED GREEN. ACCOMPLISHED QRH PROCEDURE & CYCLED LG ON SECOND EXTENSION ON ATTEMPT, LT MLG FULLY EXTENDED, WITH GREEN LIGHT APPROX 10 SECONDS AFTER OTHER TWO LG SHOWED SAFE. R & R MLG ACTUATOR IAW MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,660 hrs · 66,201 cycles

SKIN CRACKED AT BS 482+5, STRINGER 16L. REPAIRED SKIN IAW EA.

Part: LENS — LOOSE (EXIT SIGN) · airframe 70,136 hrs · 65,599 cycles

L1 DOOR EXIT SIGN LENS LOOSE. SECURED LENS IAW AMM.

Part: SKIN — CRACKED (RT WING) · airframe 70,063 hrs · 65,515 cycles

RIGHT WING LOWER FIXED LE SKIN CRACKED. REPAIRED SKIN IAW EA.

Part: LIGHT — FAULTY (CABIN) · airframe 70,011 hrs · 65,454 cycles

AFT EMER EXIT BULLNOSE LIGHT FAULTY. RELAMPED LIGHT IAW AMM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 69,867 hrs · 65,283 cycles

R1 DOOR EXIT SIGN LIGHT INOPERATIVE. R & R BATTERY IAW WDM & AMM.

Part: BRACKET — BROKEN (FLASHLIGHT) · airframe 69,867 hrs · 65,283 cycles

FORWARD LAVATORY WALL FLASHLIGHT BRACKET ASSEMBLY BROKEN ON OTBD POSITION. R & R BRACKET ASSEMBLY IAW CMM.

Part: SUPPORT BRACKET — CRACKED (RT SPOILER) · airframe 69,867 hrs · 65,283 cycles

RIGHT WING ACTUATOR GND SPOILER INBD SIDE SUPPORT BRACKET CRACKED. R & R BRACKET IAW SRM & DWG.

Part: SPAR — CORRODED (LT HORIZ STAB) · airframe 69,867 hrs · 65,283 cycles

LEFT HORIZONTAL STABILIZER REAR SPAR UPPER CHORD CORRODED BETWEEN STAB STATION 157.10 TO STAB STATION 166.30. R & R STABILIZER IAW AMM.

Part: SPAR — CORRODED (LT HORIZ STAB) · airframe 69,867 hrs · 65,283 cycles

LEFT HORIZONTAL STABILIZER REAR SPAR UPPER CHORD CORRODED BETWEEN STAB STATION 129 TO STAB STATION 138.7. R & R STABILIZER IAW AMM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 69,867 hrs · 65,283 cycles

FRAME WEB CRACKED AT BS 303.9 BETWEEN STRINGER 16L - 17L. REPAIRED WEB IAW ACO.

Part: FRAME — CRACKED (FUSELAGE) · airframe 69,867 hrs · 65,283 cycles

FUSELAGE FRAME CRACKED AT STATION 309.9, STRINGER 16L. REPAIRED FRAME IAW ACO.

Part: SKIN — DELAMINATED (RT ELEVATOR TAB) · airframe 69,867 hrs · 65,283 cycles

RIGHT ELEVATOR TAB INBD END DELAMINATED ON LOWER SURFACE. REPAIRED TAB IAW SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 69,867 hrs · 65,283 cycles

TIE CLIP CRACKED AT BS 747, STRINGER 23L. R & R TIE CLIP IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 69,867 hrs · 65,283 cycles

TIE CLIP CRACKED AT BS 727B, STRINGER 25L. R & R TIE CLIP IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 69,867 hrs · 65,283 cycles

TIE CLIP CRACKED AT BS 767, STRINGER 23L. R & R TIE CLIP IAW SRM & DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,867 hrs · 65,283 cycles

SKIN CRACKED BETWEEN BS 818 TO BS 875, BETWEEN STRINGER 18L TO 21L. REPAIRED SKIN IAW EO & EA.

Part: SUPPORT CHANNEL — CRACKED (FUSELAGE) · airframe 69,867 hrs · 65,283 cycles

SUPPORT CHANNEL CRACKED LOCATED ON LOWER SURFACE & FWD POSITION OF E1 - 3, EE COMPARTMENT. R & R CHANNEL IAW SRM & DWG.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 69,867 hrs · 65,283 cycles

BULKHEAD WEB CRACKED AT BS 227.8, LBL 14.5. REPAIRED WEB IAW EO & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,867 hrs · 65,283 cycles

FUSELAGE SKIN CRACKED BETWEEN BS 219 TO BS 235, BETWEEN STRINGER 18L TO 25L. REPAIRED SKIN IAW EO & EA.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 69,867 hrs · 65,283 cycles

BULKHEAD WEB CRACKED AT BS 227.8, RBL 14.5. REPAIRED WEB IAW EO & EA.

Part: WEB — CRACKED (FUSELAGE) · airframe 69,867 hrs · 65,283 cycles

WEB CRACKED BETWEEN BS 727A TO 727B, STRINGER 25L. R & R WEB IAW SRM & DWG.

Part: RIB — CRACKED (LT WING) · airframe 69,867 hrs · 65,283 cycles

LEFT WING RIB WEB LOWER CHORD CRACKED AT WBL 254, STRINGER 10. REPAIRED RIB IAW EO & EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 69,867 hrs · 65,283 cycles

FORWARD CARGO COMPARTMENT FRAME INNER CHORD CRACKED AT BS 420, STRINGER 26L. REPAIRED CHORD IAW EO & EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 69,867 hrs · 65,283 cycles

FORWARD CARGO COMPARTMENT FRAME WEB INNER CHORD CRACKED AT BS 482, STRINGER 26L. REPAIRED WEB IAW EO & EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 69,867 hrs · 65,283 cycles

FRAME WEB CRACKED AT BS 277, STRINGER 16R. REPAIRED FRAME IAW EO & EA.

Part: LUG — CORRODED (TE FLAP) · airframe 69,867 hrs · 65,283 cycles

RIGHT WING NR 5 FLAP TRACK AFT ATTACH POINT LUG CORRODED. REPAIRED LUG IAW CMM.

Part: WEB — CRACKED (FUSELAGE) · airframe 69,867 hrs · 65,283 cycles

WEB CRACKED AT BS 303.9 BETWEEN STRINGER 16L - 17L. REPAIRED WEB IAW ACO.

Part: FLAP TRACK — CORRODED (TE FLAP) · airframe 69,867 hrs · 65,283 cycles

LEFT WING NR 4 FLAP TRACK AFT ATTACH POINT LUG CORRODED. REPAIRED FLAP TRACK IAW CMM.

Part: SUPPORT ANGLE — CRACKED (L1 DOOR) · airframe 69,867 hrs · 65,283 cycles

L1 DOOR SUPPORT ANGLE CRACKED. R & R ANGLE IAW DWG & SRM.

Part: SPAR — CORRODED (LT HORIZ STAB) · airframe 69,867 hrs · 65,283 cycles

LEFT HORIZONTAL STABILIZER UPPER REAR SPAR BETWEEN STAB STATION 83.50 - 92.70 UPPER SURFACE TE CORRODED. R & R STABILIZER IAW AMM.

Part: SUPPORT ANGLE — CRACKED (RT PYLON) · airframe 69,867 hrs · 65,283 cycles

RIGHT PYLON SUPPORT ANGLE CRACKED AT WBL 198.6. R & R ANGLE IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 69,867 hrs · 65,283 cycles

TIE CLIP CRACKED AT BS 482B, STRINGER 8R. R & R TIE CLIP IAW SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 69,867 hrs · 65,283 cycles

TIE CLIP CRACKED AT BS 380, STRINGER 21L. R & R TIE CLIP IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 69,867 hrs · 65,283 cycles

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

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 69,867 hrs · 65,283 cycles

LEFT SIDE OF RACK E 1 EE COMPARTMENT SUPPORT ANGLE CRACKED. R & R ANGLE IAW SRM & DWG.

Part: FLAP TRACK — CORRODED (TE FLAP) · airframe 69,867 hrs · 65,283 cycles

LEFT WING NR 2 FLAP TRACK UPPER SURFACE CORRODED. R & R FLAP TRACK IAW AMM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 69,867 hrs · 65,283 cycles

TIE CLIP CRACKED AT BS 482A, STRINGER 8R. R & R TIE CLIP IAW SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 69,867 hrs · 65,283 cycles

TIE CLIP CRACKED AT BS 482B, STRINGER 6R. R & R TIE CLIP IAW SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 69,867 hrs · 65,283 cycles

TIE CLIP CRACKED AT BS 380, STRINGER 8R. R & R TIE CLIP IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 69,867 hrs · 65,283 cycles

TIE CLIP CRACKED AT BS 482B, STRINGER 7R. R & R TIE CLIP IAW SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 69,867 hrs · 65,283 cycles

TIE CLIP CRACKED AT BS 727B, STRINGER 4R. R & R TIE CLIP IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,867 hrs · 65,283 cycles

STRINGER CLIP CRACKED AT STATION 616, STRINGER 1. R & R CLIP IAW SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 69,867 hrs · 65,283 cycles

TIE CLIP CRACKED AT BS 727C, STRINGER 7R. R & R TIE CLIP IAW SRM.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 69,867 hrs · 65,283 cycles

FASTENER HOLE CUT OUT CRACKED AT BS 400, STRINGER 7L. REPAIRED CUT OUT IAW SRM.

Part: ANGLE — CRACKED (CARGO DOOR) · airframe 69,867 hrs · 65,283 cycles

AFT CARGO DOOR ANGLE CRACKED ON FWD LOWER CORNER. REPAIRED ANGLE IAW EA.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 69,867 hrs · 65,283 cycles

TIE CLIP CRACKED AT BS 400, STRINGER 7L. R & R TIE CLIP IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 69,867 hrs · 65,283 cycles

TIE CLIP CRACKED AT BS 887, STRINGER 15R. R & R TIE CLIP IAW SRM & DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 69,867 hrs · 65,283 cycles

INTERCOSTAL CRACKED BETWEEN BS 196.5 TO 203.8, RBL 5.5. REPAIRED INTERCOSTAL IAW EO & EA.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 69,867 hrs · 65,283 cycles

TIE CLIP CRACKED AT BS 907, STRINGER 8L. R & R TIE CLIP IAW SRM & DWG.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 69,867 hrs · 65,283 cycles

LOWER LOBE OF NOSE COMPARTMENT OUTER CHORD CORRODED AT BS 227.8, RBL 2. REPAIRED CHORD IAW EA.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 69,867 hrs · 65,283 cycles

TIE CLIP CRACKED AT BS 827, STRINGER 16R. R & R TIE CLIP IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 69,867 hrs · 65,283 cycles

TIE CLIP CRACKED AT BS 706, STRINGER 8L. R & R TIE CLIP IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 69,867 hrs · 65,283 cycles

ANGLE CRACKED AT BS 887 STRINGER 1L. R & R ANGLE IAW SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 69,867 hrs · 65,283 cycles

TIE CLIP CRACKED AT BS 867, STRINGER 15R. R & R TIE CLIP IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 69,867 hrs · 65,283 cycles

TIE CLIP CRACKED AT BS 827, STRINGER 15R. R & R TIE CLIP IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 69,867 hrs · 65,283 cycles

FRAME CRACKED AT BS 400, BETWEEN STRINGER 15L TO 16L. REPAIRED FRAME IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 69,867 hrs · 65,283 cycles

FRAME CRACKED AT BS 787, BETWEEN STRINGER 17R - 20R. REPAIRED FRAME IAW EO & EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 69,867 hrs · 65,283 cycles

AFT CARGO COMPARTMENT FRAME CRACKED AT BS 787, STRINGER 24L. REPAIRED FRAME IAW EO & EA.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 69,867 hrs · 65,283 cycles

TIE CLIP CRACKED AT BS 482, STRINGER 16R. R & R TIE CLIP IAW SRM & DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 69,867 hrs · 65,283 cycles

KEEL BEAM AREA MLG WW WEB CRACKED AT BS 711, BETWEEN LBL 6.50 TO RBL 6.50. R & R WEB IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 69,867 hrs · 65,283 cycles

FRAME CRACKED AT BS 827, BETWEEN STRINGER 18L - 20L. REPAIRED FRAME IAW EO & EA.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 69,867 hrs · 65,283 cycles

TIE CLIP CRACKED AT BS 482B, STRINGER 6L. R & R TIE CLIP IAW SRM & DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 69,867 hrs · 65,283 cycles

SUPPORT ANGLE CRACKED AT BS 360, STRINGER 10R. R & R ANGLE IAW SRM & DWG.

Part: SKIN — DEBONDED (LE SLAT) · airframe 69,867 hrs · 65,283 cycles

RIGHT WING NR 5 LE SLAT OTBD SKIN DISBONDED. R & R SLAT IAW MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 69,867 hrs · 65,283 cycles

FRAME CRACKED AT BS 794.3, BETWEEN STRINGER 23R - 24R. R & R FRAME IAW EO & EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 69,867 hrs · 65,283 cycles

FUSELAGE FRAME CRACKED AT STATION 947.5, STRINGER 19L. REPAIRED FRAME IAW SRM & EA.

Part: SUPPORT ANGLE — CRACKED (RT PYLON) · airframe 69,867 hrs · 65,283 cycles

RIGHT PYLON OTBD STRUT FAIRING SUPPORT ANGLE CRACKED AT STATION 278. R & R ANGLE IAW SRM & DWG.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 69,867 hrs · 65,283 cycles

BULKHEAD OTBD LOWER CHORD CRACKED AT BS 227.8, BETWEEN BL 0 TO RBL 1.5. REPAIRED CHORD IAW EO & EA.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 69,867 hrs · 65,283 cycles

TIE CLIP CRACKED AT BS 927, STRINGER 25R. R & R TIE CLIP IAW SRM & DWG.

Part: PLATE — CRACKED (FUSELAGE) · airframe 69,867 hrs · 65,283 cycles

RIGHT SIDE TRANSVERSAL SUPPORT PLATE CRACKED AT BS 540. R & R PLATE IAW SRM & DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 69,867 hrs · 65,283 cycles

SUPPORT ANGLE CRACKED AT STATION 787+3, STRINGER 18R. R & R ANGLE IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 69,867 hrs · 65,283 cycles

AFT CARGO COMPARTMENT FRAME CRACKED AT BS 786, STRINGER 24L. REPAIRED FRAME IAW EA.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 69,867 hrs · 65,283 cycles

FRAME SUPPORT CRACKED AT BS 420, STRINGER 10R. R & R SUPPORT IAW SRM & DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 69,867 hrs · 65,283 cycles

SUPPORT ANGLE CRACKED BETWEEN BS 887 - 907, RBL 45. R & R ANGLE IAW SRM & DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 69,867 hrs · 65,283 cycles

NUMBER 8 TRANSMISSION INTERNAL SUPPORT ANGLE CRACKED. R & R ANGLE IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 69,867 hrs · 65,283 cycles

FRAME CRACKED AT BS 947.5, STRINGER 19R. R & R FRAME IAW EO & EA.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 69,867 hrs · 65,283 cycles

RIGHT WING AFT FLAP INBD UPPER SKIN DELAMINATED. REPAIRED AFT FLAP IAW SRM & EA.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 69,867 hrs · 65,283 cycles

SUPPORT CRACKED AT BS 360, BETWEEN STRINGER 10L TO 12L. R & R SUPPORT IAW SRM & DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,867 hrs · 65,283 cycles

FUSELAGE SKIN CRACKED AT STATION 465.750, STRINGER 26L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (TE FLAP) · airframe 69,867 hrs · 65,283 cycles

RIGHT WING FORE FLAP OTBD UPPER SKIN CRACKED AT WBL 304.5. R & R FORE FLAP IAW SRM.

Part: TAB — DELAMINATED (RT ELEVATOR) · airframe 69,867 hrs · 65,283 cycles

RIGHT ELEVATOR TAB INBD END LE DELAMINATED. REPAIRED TAB IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,867 hrs · 65,283 cycles

FUSELAGE SKIN CRACKED AT STATION 444.750, STRINGER 26L. REPAIRED SKIN IAW EA.

Part: FLAP TRACK — CORRODED (TE FLAP) · airframe 69,867 hrs · 65,283 cycles

LEFT WING NR 2 FLAP TRACK CORRODED. R & R FLAP TRACK IAW AMM.

Part: PLATE — CRACKED (FUSELAGE) · airframe 69,867 hrs · 65,283 cycles

PLATE CRACKED BETWEEN BS 698 TO 727, RBL 63. R & R PLATE IAW SRM & DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 69,867 hrs · 65,283 cycles

AFT CARGO COMPARTMENT ANGLE CRACKED AT BS 927, STRINGER 25L. R & R ANGLE IAW SRM AND DWG.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 69,867 hrs · 65,283 cycles

FORWARD CARGO COMPARTMENT KEEL BEAM LOWER CHORD CORRODED BETWEEN BS 482B - 520, STRINGER 28L. REPAIRED CHORD IAW EO & EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 69,867 hrs · 65,283 cycles

FUSELAGE FRAME CRACKED AT STATION 947.5, STRINGER 19L. REPAIRED FRAME IAW SRM & EA.

Part: PLATE — CRACKED (FLAP FAIRING) · airframe 69,867 hrs · 65,283 cycles

LEFT WING FLAP TRACK FAIRING ACCESS 3501L PLATE CRACKED. REPLACED PLATE IAW DWG & SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 69,867 hrs · 65,283 cycles

FRAME CRACKED AT BS 827, STRINGER 19L. REPAIRED FRAME IAW EO & EA.

Part: STRAP — CRACKED (FUSELAGE) · airframe 69,867 hrs · 65,283 cycles

AFT CARGO COMPARTMENT BELOW MAIN DECK FLOOR STRUCTURE STRAP CRACKED BETWEEN BS 727B - 727C, LBL 24.5. R & R STRAP IAW SRM.

Part: ANGLE — CRACKED (L1 DOOR) · airframe 69,867 hrs · 65,283 cycles

L1 DOOR ANGLE CRACKED AT BS 312, BETWEEN STRINGER 16L - 17L. R & R ANGLE IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 69,867 hrs · 65,283 cycles

TIE CLIP CRACKED AT BS 767, STRINGER 21L. R & R TIE CLIP IAW SRM & DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 69,867 hrs · 65,283 cycles

FORWARD CARGO COMPARTMENT ANGLE CRACKED BETWEEN BS 380 TO 400, BL 0. R & R ANGLE IAW SRM & DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 69,867 hrs · 65,283 cycles

FLOOR STRUCTURE FWD CARGO COMPARTMENT ANGLE CRACKED BETWEEN BS 482B TO 520, BL 0. R & R ANGLE IAW SRM & DWG.

Part: TIE DOWN — CRACKED (CARGO BAY) · airframe 69,867 hrs · 65,283 cycles

FORWARD CARGO COMPARTMENT TRACK TIE DOWN CRACKED AT BS 460, RBL 13.80. REPAIRED TIE DOWN IAW SRM & DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 69,867 hrs · 65,283 cycles

AFT CARGO COMPARTMENT ANGLE CRACKED AT BS 727, BL 0. R & R ANGLE IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 69,867 hrs · 65,283 cycles

FUSELAGE FRAME CRACKED AT STATION 947.5, STRINGER 19R. REPAIRED FRAME IAW SRM & EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 69,867 hrs · 65,283 cycles

AFT CARGO COMPARTMENT FRAME CRACKED AT BS 787, STRINGER 19R. REPAIRED FRAME IAW EO & EA.

Part: WEB — CRACKED (FUSELAGE) · airframe 69,867 hrs · 65,283 cycles

WEB CRACKED BETWEEN BS 420 TO 440, STRINGER 26R. R & R WEB IAW SRM & DWG.

Part: SKIN — DELAMINATED (TAILCONE) · airframe 69,867 hrs · 65,283 cycles

TAIL CONE SKIN DELAMINATED AT BS 1156+14, RBL 7. REPAIRED TAIL CONE IAW AMM SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,867 hrs · 65,283 cycles

SKIN CRACKED AT BS 867+15.5, STRINGER 24R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,867 hrs · 65,283 cycles

SKIN CRACKED AT BS 787+12, STRINGER 23L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,867 hrs · 65,283 cycles

SKIN CRACKED AT BS 887+6.5, STRINGER 25L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,867 hrs · 65,283 cycles

SKIN CRACKED AT BS 867+13.5, STRINGER 25L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,867 hrs · 65,283 cycles

SKIN CRACKED AT BS 767+16.5, STRINGER 21L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,867 hrs · 65,283 cycles

SKIN CRACKED AT BS 767+16.5, STRINGER 24L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,867 hrs · 65,283 cycles

SKIN CRACKED AT BS 767+3.250, STRINGER 23L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,867 hrs · 65,283 cycles

SKIN CRACKED BETWEEN BS 827+14 TO BS 847, STRINGER 17L. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,867 hrs · 65,283 cycles

SKIN CRACKED AT BS 767+7, STRINGER 24L. REPAIRED SKIN IAW EO & EA.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 69,867 hrs · 65,283 cycles

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

Part: DRAG ANGLE — CRACKED (FAIRING) · airframe 69,867 hrs · 65,283 cycles

RIGHT WING TO BODY FAIRING DRAG ANGLE CRACKED AT BS 540, STRINGER 21R. REPAIRED ANGLE IAW SRM.

Part: ATTACH ANGLE — CRACKED (RT HORIZ STAB) · airframe 69,867 hrs · 65,283 cycles

RIGHT HORIZONTAL STABILIZER ATTACH ANGLE CRACKED ON LOWER CHORD OF THE CTR SECTION. R & R ANGLE IAW SRM & DWG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 69,867 hrs · 65,283 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,867 hrs · 65,283 cycles

SKIN CRACKED AT BS 747+5.250, STRINGER 25L. REPAIRED SKIN IAW EA.

Part: ANGLE — CRACKED (L1 DOOR) · airframe 69,867 hrs · 65,283 cycles

L1 DOOR AFT UPPER CORNER ANGLE CRACKED. R & R ANGLE IAW SRM & DWG.

Part: PLATE — CRACKED (VERTICAL STAB) · airframe 69,867 hrs · 65,283 cycles

VERTICAL STABILIZER LT FWD FIN, ACCESS PANEL 9501, PLATE CRACKED. R & R PLATE IAW SRM & DWG.

Part: ANGLE — CRACKED (L1 DOOR) · airframe 69,867 hrs · 65,283 cycles

L1 DOOR FWD UPPER CORNER ANGLE CRACKED. R & R ANGLE IAW SRM & DWG.

Part: SKIN — CRACKED (RT WING) · airframe 69,867 hrs · 65,283 cycles

RIGHT WING INBD FIXED LE SKIN CRACKED AT STATION 208. REPAIRED SKIN IAW EO & EA.

Part: SIGN — BROKEN (CABIN) · airframe 69,597 hrs · 64,966 cycles

L1 DOOR LOWER EMER EXIT SIGN BROKEN. R& R SIGN ASSEMBLY IAW MM.

Part: FLAP — DELAMINATED (LT WING) · airframe 69,085 hrs · 64,390 cycles

LEFT WING OTBD AFT FLAP DELAMINATED. R & R AFT FLAP IAW AMM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 68,376 hrs · 63,598 cycles

BULKHEAD WEB CRACKED AT BS 1016, STRINGER 15L. REPAIRED WEB IAW ER & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,376 hrs · 63,598 cycles

CHEM MILL SKIN CRACKED BETWEEN BS 798.5 TO BS 800.6, STRINGER 22L. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,376 hrs · 63,598 cycles

SKIN CRACKED AT BS 914, STRINGER 4L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,376 hrs · 63,598 cycles

CHEM MILL SKIN CRACKED BETWEEN BS 931 TO BS 931.7, STRINGER 22L. REPAIRED SKIN IAW ER & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,376 hrs · 63,598 cycles

SKIN CRACKED AT BS 360, STRINGER 1L. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,376 hrs · 63,598 cycles

CHEM MILL SKIN CRACKED AT BS 482A+4, STRINGER 16R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,376 hrs · 63,598 cycles

CHEM MILL SKIN CRACKED AT BS 393, STRINGER 15L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,021 hrs · 63,227 cycles

FUSELAGE SKIN CRACKED AT BS 385, STRINGER 15R. REPAIRED SKIN IAW EA.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 68,021 hrs · 63,227 cycles

LEFT EEPLS INOPERATIVE AT ROW 15. R & R BATTERY PACK IAW MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,021 hrs · 63,227 cycles

FUSELAGE SKIN CRACKED AT BS 400, STRINGER 14R. REPAIRED SKIN IAW EA.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 67,647 hrs · 62,861 cycles

RT EXTERNAL EMERGENCY LIGHT BULBS INOPERATIVE. R & R BULBS IAW MM.

Part: ACTUATOR — LEAKING (LT SPOILER) · airframe 67,338 hrs · 62,560 cycles

LT WING GND SPOILER INBD ACTUATOR LEAKING. R & R ACTUATOR IAW MM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 67,058 hrs · 62,261 cycles

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

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 67,058 hrs · 62,261 cycles

EXTERIOR EMERGENCY EXIT LIGHT AT AFT ENTRY DOOR INOPERATIVE. RELAMPED LIGHT IAW AMM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 67,058 hrs · 62,261 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,058 hrs · 62,261 cycles

FUSELAGE SKIN CRACKED AT BS 779.5, STRINGER 19L. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,058 hrs · 62,261 cycles

FUSELAGE SKIN CRACKED AT BS 759.5, STRINGER 19L. REPAIRED SKIN IAW ER & EA.

Part: FLAP — DELAMINATED (RT WING) · airframe 66,827 hrs · 62,013 cycles

RT WING OTBD TE FLAP DELAMINATED. R & R AFT FLAP IAW AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,148 hrs · 61,275 cycles

FUSELAGE SKIN CRACKED AT STA 747+16, STR 24L. REPAIRED SKIN IAW SRM.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 65,816 hrs · 60,948 cycles

RIGHT OVERWING VERTICAL EMERGENCY EXIT SIGN BULBS INOP. RELAMPED SIGN PER AMM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 65,816 hrs · 60,948 cycles

LEFT OVERWING EMERGENCY EXTERNAL LIGHT FWD BULB INOP. RELAMPED LIGHT PER AMM.

Part: WIRE — STRIPPED (CABIN) · airframe 65,816 hrs · 60,948 cycles

G-1 GALLEY EMERGENCY EXIT INDICATOR LIGHT WIRE STRIPPED OF INSULATION. REPAIRED WIRES PER SWPM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,816 hrs · 60,948 cycles

SKIN CRACKED AT BS 380, BETWEEN STR 15L TO STR 16L. REPAIRED SKIN IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,816 hrs · 60,948 cycles

FRAME CRACKED AT BS 380, BETWEEN STR 14L AND STR 15L. REPAIRED FRAME PER ER AND EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 65,816 hrs · 60,948 cycles

STRINGER CLIP CRACKED AT BS 380, STR 15L. REMOVED AND REPLACED CLIP IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,816 hrs · 60,948 cycles

FRAME CRACKED AT BS 380, BETWEEN STR 14L AND STR 15L. REPAIRED FRAME PER ER AND EA.

Part: LENS — CRACKED (EXTERIOR) · airframe 65,816 hrs · 60,948 cycles

FWD ENTRY DOOR EXTERIOR EMERGENCY SLIDE LIGHT LENS CRACKED. REMOVED AND REPLACED LENS PER AMM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 65,816 hrs · 60,948 cycles

APU UPPER SHROUD FWD BULKHEAD CRACKED AT RIGHT O/B LOWER CORNER ON FLANGE RADIUS. REPAIRED BULKHEAD IAW EA AND ER.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 65,816 hrs · 60,948 cycles

APU UPPER SHROUD CRACKED 9 INCHES AFT OF FWD BULKHEAD ON RT O/B FLANGE RADIUS. REPAIRED BULKHEAD IAW EA.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 65,816 hrs · 60,948 cycles

STRINGER SPLICE ANGLE CRACKED AT BS 360, STR 11R. REMOVED AND REPLACED SPLICE IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 65,816 hrs · 60,948 cycles

CREASE BEAM WEB CORRODED BETWEEN BS 807 TO BS 827, WL 208. REMOVED AND REPLACED WEB IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 65,816 hrs · 60,948 cycles

ANGLE CRACKED AT BS 819, RBL 20. REMOVED AND REPLACED ANGLE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,816 hrs · 60,948 cycles

FRAME CRACKED AT BS 348.2, STR 16L. REMOVED AND REPLACED ATTACH CLIP IAW SRM & DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 65,816 hrs · 60,948 cycles

STRINGER CLIP CRACKED AT BS 1006, STR 15R. REMOVED AND REPLACED CLIP IAW SRM.

Part: MOUNT — CORRODED (L1 DOOR) · airframe 65,816 hrs · 60,948 cycles

L1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR MOUNT CORRODED AT BS 344, LBL 59. REMOVED AND REPLACED MOUNT PER SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 65,816 hrs · 60,948 cycles

FLOOR SUPPORT ANGLE CORRODED AT BS 270, BETWEEN LBL 12 - RBL 12L. REMOVED AND REPLACED ANGLE PER SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 65,816 hrs · 60,948 cycles

STRINGER SPLICE CRACKED AT BS 360, STR 15L. REMOVED AND REPLACED SPLICE IAW SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 65,816 hrs · 60,948 cycles

STRINGER SPLICE CRACKED AT BS 360, STR 4L. REMOVED AND REPLACED SPLICE IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 65,816 hrs · 60,948 cycles

FLOORBEAM UPPER FLANGE CORRODED AT BS 270, LBL 12 - RBL 12. REMOVED AND REPLACED FLANGE PER SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 65,816 hrs · 60,948 cycles

INTERCOSTAL CRACKED AT BS 294, STR 7L. REMOVED AND REPLACED INTERCOSTAL IAW SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 65,816 hrs · 60,948 cycles

UPPER CLIP CRACKED AT BS 349, STR 16L. REMOVED AND REPLACED CLIP IAW SRM & DWG.

Part: MOUNT FITTING — CORRODED (L1 DOOR) · airframe 65,816 hrs · 60,948 cycles

L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR MOUNT CORRODED AT BS 313, LBL 55. REMOVED AND REPLACED FITTINGS PER SOPM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 65,816 hrs · 60,948 cycles

LOWER CLIP CRACKED AT BS 349, STR 16L. REMOVED AND REPLACED CLIP IAW SRM & DWG.

Part: STRAP — CRACKED (FUSELAGE) · airframe 65,816 hrs · 60,948 cycles

SPLICE STRAP CRACKED AT BS 360, STR 6R. REMOVED AND REPLACED STRAP PER SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 65,816 hrs · 60,948 cycles

SEAT TRACK CORRODED BETWEEN BS 986 TO BS 1016, RBL 18. REMOVED AND REPLACED SEAT TRACK PER SRM.

Part: SILL — CORRODED (FUSELAGE) · airframe 65,816 hrs · 60,948 cycles

AFT SERVICE DOOR MOPSILL CORRODED AT BS 976, RBL 48. REMOVED AND REPLACED MOPSILL PER SRM & DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 65,816 hrs · 60,948 cycles

FLOORBEAM UPPER CHORD CORRODED AT BS 986, BETWEEN BL 0 TO LBL 47. REPAIRED FLOORBEAM PER ER AND EA.

Part: PLATE — CORRODED (FUSELAGE) · airframe 65,816 hrs · 60,948 cycles

FLOOR PANEL 2465ZA GIRT BAR SUPPORT PLATE CORRODED. REMOVED AND REPLACED SUPPORT PLATE ASSY IAW SRM.

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 65,816 hrs · 60,948 cycles

PRESSURE WEB ABOVE MAIN WHEEL WELL CRACKED AT BS 665, RBL 33. REPAIRED WEB PER ER AND EA.

Part: ATTACH ANGLE — CORRODED (MLG WW) · airframe 65,816 hrs · 60,948 cycles

MAIN WHEEL WELL WEB ATTACH ANGLE CORRODED AT BS 688, RBL 64. REPAIRED ANGLE PER ER AND EA.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 65,816 hrs · 60,948 cycles

PRESSURE WEB ABOVE MAIN WHEEL WELL CRACKED AT BS 665, LBL 39. REMOVED AND REPLACED WEB IAW ER AND EA.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 65,816 hrs · 60,948 cycles

INTERCOSTAL CRACKED AT BS 304, STR 4L. REMOVED AND REPLACED INTERCOSTAL IAW SRM.

Part: DOUBLER — CRACKED (FLAP FAIRING) · airframe 65,816 hrs · 60,948 cycles

INTERNAL DOUBLER CRACKED I/B NR 6 FLAP TRACK FAIRING. REMOVED AND REPLACED DOUBLER PER SRM.

Part: ANGLE — CRACKED (TE FLAP) · airframe 65,816 hrs · 60,948 cycles

RIGHT WING "L" ANGLE CRACKED I/B NR 6 FLAP TRACK FAIRING. REMOVED AND REPLACED L-ANGLE PER SRM.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 65,816 hrs · 60,948 cycles

INTERCOSTAL CORRODED AT BS 716, LBL 62. REPAIRED INTERCOSTAL PER SRM.

Part: FAIRING — CRACKED (TE FLAP) · airframe 65,816 hrs · 60,948 cycles

NR 6 FLAP TRACK FAIRING FWD UPPER CORNER CRACKED. REPAIRED FAIRING PER EA.

Part: STRAP — CRACKED (FUSELAGE) · airframe 65,816 hrs · 60,948 cycles

STRAP CRACKED AT BS 304, STR 4L. REMOVED AND REPLACED STRAP IAW SRM.

Part: WEB — CORRODED (LT MLG WW) · airframe 65,816 hrs · 60,948 cycles

MAIN W/W WEB CORRODED AT BS 697, LBL 63. REMOVED AND REPLACED WEB PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,816 hrs · 60,948 cycles

SKIN CRACKED BETWEEN BS 436.5 TO BS 437, STR 2R. REPAIRED SKIN PER ER AND EA.

Part: LONGERON — CRACKED (LT WING) · airframe 65,816 hrs · 60,948 cycles

LEFT WING NR 1 PYLON INBD FLAP TORQUE TUBE CUTOUT LOWER LONGERON CRACKED. REMOVED AND REPLACED LONGERON PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,816 hrs · 60,948 cycles

FRAME OUTBOARD CHORD FWD FLANGE CRACKED AT BS 727, STR 18A LEFT. REPAIRED FRAME PER ER AND EA.

Part: FAIRING — CRACKED (NR 1 PYLON) · airframe 65,816 hrs · 60,948 cycles

LEFT WING NR 1 PYLON INBD SKIRT FAIRING HAS A SUSPECTED CRACK IN THE FWD UPPER CORNER. REPAIRED FAIRING PER EA.

Part: LINK — LOOSE (TE FLAP) · airframe 65,816 hrs · 60,948 cycles

LEFT WING NR 4 AFT FLAP TRACK AFT MAIN SUPPORT LINK BEARINGS LOOSE. REMOVED AND REPLACED LINK IAW SOPM AND MM.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 65,816 hrs · 60,948 cycles

INTERNAL DOUBLER CRACKED AT LOWER AFT CORNER OF EXTERNAL POWER DOOR CUTOUT. REPAIRED DOUBLER PER EA.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 65,816 hrs · 60,948 cycles

INTERNAL DOUBLER CRACKED UNDER LOWER HINGE OF EXTERNAL POWER DOOR AT CUTOUT. REPAIRED DOUBLER PER EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 65,816 hrs · 60,948 cycles

SHEAR TIE CORRODED AT BS 727C, BETWEEN STR 25L AND STR 26L. REPAIRED SHEAR TIE IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 65,816 hrs · 60,948 cycles

SHEAR TIE CORRODED AT BS 827, BETWEEN STR 27LEFT TO STR 27R. REPAIRED SHEAR TIE PER ER AND EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 65,816 hrs · 60,948 cycles

SHEAR TIE CORRODED AT BS 887, BETWEEN STR 27L AND STR 27R. REPAIRED SHEAR TIE PER ER AND EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 65,816 hrs · 60,948 cycles

SHEAR TIE CORRODED AT BS 867, BETWEEN STR 26R TO STR 27R. REMOVED AND REPLACED SHEAR TIE IAW SRM.

Part: STRAP — CORRODED (FUSELAGE) · airframe 65,816 hrs · 60,948 cycles

STRAP CORRODED BETWEEN BS 827 TO BS 847, RBL 19. REMOVED AND REPLACED STRAP IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,816 hrs · 60,948 cycles

FUSELAGE SKIN CRACKED BETWEEN BS 371 TO BS 372, STR 15R. REPAIRED SKIN PER ER AND EA.

Part: WEB — CRACKED (NLG WW) · airframe 65,816 hrs · 60,948 cycles

RIGHT NOSE WHEEL WELL WEB CRACKED AT BS 247, RBL 15.5. REPAIRED WEB PER ER & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,632 hrs · 60,752 cycles

THERE APPEARS TO BE A CRACK IN THE FUSELAGE ABOVE THE FWD CARGO DOOR AT APPROX STA 440 ABD SL 16R. TRANSFERRED FROM LOG PAGE 0008542862. REPAIRED PER SRM 53-00-01-2R-31 AND EA 1-553-21833.

Part: SKIN — CRACKED (LE SLAT) · airframe 65,307 hrs · 60,407 cycles

(REF LOG PAGE 8376971) SKIN TORN/CRACKED UNDER NR 4 SLAT FIXED LEADING EDGE. REPAIRED CRACKED FIXED LEADING EDGE BEHIND NR 4 SLAT IAW SRN 57-41-01 SRM 51-70-17, SRM 51-70-14 & SRM 20-50-05 ALL WORK ACCOMPLISHED ON N/R T176153. CLOSING # 84232

Part: RETAINER — CRACKED (RT WING) · airframe 65,307 hrs · 60,407 cycles

RIGHT WING LOWER TRAILING EDGE SEAL RETAINER IS CRACKED JUST O/B OF NR 2 PYLON. REPAIRED RT WING LWR T/E SEAL RETAINER JUST O/B OF NR 2 PYLON IAW EA 1-A53-301 (T176199).

Part: SKIN — CRACKED (LE SLAT) · airframe 65,307 hrs · 60,407 cycles

RIGHT WING FIXED LEADING EDGE BEHIND NR 4 SLAT HAS CRACK IN RADIUS OF ACTUATOR CUTOUT. REPAIRED CRACK ON RIGHT WING FIXED LEADING EDGE BEHIND NR 4 SLAT AT ACTUATOR RADIUS CUTOUT IAW SRM 57-41-01 & SRM 51-70-17.

Part: SKIN — CRACKED (LE SLAT) · airframe 65,307 hrs · 60,407 cycles

SKIN UNDER NR 4 SLAT CRACKED. REPAIRED SLAT IAW SRM.

Part: RETAINER — CRACKED (LT WING) · airframe 65,307 hrs · 60,407 cycles

LEFT WING LWR T/E SEAL RETAINER IS CRACKED JUST O/B OF THE NR 1 PYLON. REPAIRED LEFT WING LWR T/R SEAL RETAINER JUST O/B OF THE NR 1 PYLON IAW EA 1-A57-301 (T176185).

Part: ANGLE — CRACKED (RT WING) · airframe 65,307 hrs · 60,407 cycles

RIGHTT WING UPPER T/E PANEL I/B FWD ANGLE IS CRACKED. REMOVED AND REPLACED RIGHT WING UPPER T/E PANEL I/B FWD ANGLE IAW SRM 51-40-02-0G-0 PARA 7 AND 9.

Part: SKIN — CRACKED (LE SLAT) · airframe 65,296 hrs · 60,399 cycles

SKIN TORN ON LEADING EDGE O/B AUX TRACK APPROX 14" LONG. UPON FURTHER INVESTIGATION SKIN UNDER 4 SLAT WAS CRACKED NOT TORN ON THE FIXED LEADING EDGE. REPAIRED PER EA 1-557-7776. OK TO CONTINUE FOR 10 (TEN) CYCLES TRACK 81532.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,791 hrs · 59,883 cycles

FUSELAGE SKIN CRACKED BS 890, STR 18R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,761 hrs · 59,863 cycles

FUSELAGE SKIN CRACKED AT BS 981, STR 21L. REPAIRED SKIN PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 64,686 hrs · 59,815 cycles

STRINGER CLIP CRACKED AT BS 927, STR 26R. REMOVED AND REPLACED CLIP IAW DWG AND SRM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 64,686 hrs · 59,815 cycles

L1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK IAW AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,686 hrs · 59,815 cycles

FUSELAGE SKIN CRACKED AT BS 787+13, STR 22L. REMOVED AND REPLACED SKIN IAW SRM & AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,686 hrs · 59,815 cycles

FUSELAGE SKIN CRACKED AT BS 907+13, STR 21L. REPAIRED SKIN IAW AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,686 hrs · 59,815 cycles

FUSELAGE SKIN CRACKED AT BS 931, STR 25R. REPAIRED SKIN IAW SRM & AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,686 hrs · 59,815 cycles

FUSELAGE SKIN CRACKED AT BS 875, BETWEEN STR 24L TO STR 25L. REPAIRED SKIN IAW SRM & AMM.

Part: FLAP — CRACKED (LT WING) · airframe 64,039 hrs · 59,414 cycles

LEFT WING FORE FLAP CRACKED AT FITTING. REMOVED AND REPLACED FORE FLAP IAW AMM.

Part: TAB — DELAMINATED (RT ELEVATOR) · airframe 63,835 hrs · 59,285 cycles

RT ELEVATOR TAB DELAMINATED. REMOVED AND REPLACED TAB PER AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,243 hrs · 58,900 cycles

FUSELAGE SKIN CRACKED AT BS 787. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,069 hrs · 58,797 cycles

FUSELAGE SKIN CRACKED AT BS 793, STR 18L. REPAIRED SKIN IAW SRM.

Part: ADC — FAILED (COCKPIT) · airframe 62,892 hrs · 58,690 cycles

ON TAKEOFF AIRSPEED INDICATOR (CAPT'S SIDE) FAILED, AIR TURNBACK. REMOVED & REPLACED ADC IAW AMM.

Part: SKIN — CORRODED (CARGO DOOR) · airframe 60,603 hrs · 57,180 cycles

DURING SCHEDULED 20Y CHECK FOUND, AFT CARGO DOOR SKIN CRACKED BETWEEN BS 767 TO BS 794.3, BETWEEN STR 25R TO STR 26R. REPAIRED SKIN PER EA.

Part: AILERON — DELAMINATED (LT WING) · airframe 60,603 hrs · 57,180 cycles

DURING SCHEDULED 20Y CHECK FOUND, LT WING AILERON DELAMINATED AT L/E LOWER AREA. REPAIRED AILERON PER EO SRM AND EA.

Part: SKIN — CORRODED (FUSELAGE) · airframe 60,603 hrs · 57,180 cycles

DURING SCHEDULED 20Y CHECK FOUND, AFT CARGO COMPARTMENT SKIN CORRODED AT BS 818, BETWEEN STR 26R TO STR 27R. REPAIRED SKIN PER EO AND EA.

Part: FLAP — DELAMINATED (LT WING) · airframe 60,603 hrs · 57,180 cycles

DURING SCHEDULED 20Y CHECK FOUND, LT WING FORE FLAP DELAMINATED. REMOVED AND REPLACED FORE FLAP PER EA.

Part: SKIN — PUNCTURED (FOREFLAP) · airframe 60,603 hrs · 57,180 cycles

DURING SCHEDULED 20Y CHECK FOUND, LT WING FORE FLAP LOWER SKIN I/B PUNCTURED. REPAIRED FORE FLAP PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 60,603 hrs · 57,180 cycles

DURING SCHEDULED 20Y CHECK, FOUND WEB CRACKED AT BS 247, RBL 23. REPAIRED WEB PER ACO.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 60,603 hrs · 57,180 cycles

DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CORRODED AT BS 767, BETWEEN STR 26R TO STR 27R. REPAIRED SHEAR TIE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,603 hrs · 57,180 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 285 TO BS 315, STR 6R TO STR 9R. REPAIRED SKIN PER EO.

Part: WEB — CRACKED (FUSELAGE) · airframe 60,603 hrs · 57,180 cycles

DURING SCHEDULED 20Y CHECK, FOUND WEB CRACKED AT BS 247, RBL 17. REPAIRED WEB PER ACO.

Part: FITTING — CRACKED (FUSELAGE) · airframe 60,603 hrs · 57,180 cycles

DURING SCHEDULED 20Y CHECK, FOUND AFT CARGO COMPARTMENT FITTING CRACKED AT BS 727, STR 27L. REMOVED AND REPLACED FITTING PER SRM.

Part: LENS — MISSING (CABIN) · airframe 60,603 hrs · 57,180 cycles

DURING SCHEDULED 20Y CHECK, FOUND RT OVERHEAD EMERGENCY EXIT BULLNOSE LIGHT LENS MISSING AT ROW 9. INSTALLED LENS PER MM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 60,603 hrs · 57,180 cycles

DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CORRODED AT BS 482A, BETWEEN STR 27R TO STR 28R. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 60,603 hrs · 57,180 cycles

DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CORRODED AT BS 482B, BETWEEN STR 27R TO STR 28R. REMOVED AND REPLACED SEHAR TIE PER SRM.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 60,603 hrs · 57,180 cycles

DURING SCHEDULED 20Y CHECK FOUND, AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 880, RBL 8.10. REPAIRED CHANNEL PER EA.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 60,603 hrs · 57,180 cycles

DURING SCHEDULED 20Y CHECK FOUND, AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 772, LBL 3. REPAIRED CHANNEL PER EA.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 60,603 hrs · 57,180 cycles

DURING SCHEDULED 20Y CHECK FOUND, AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 860, RBL 8.10. REPAIRED CHANNEL PER EA.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 60,603 hrs · 57,180 cycles

DURING SCHEDULED 20Y CHECK FOUND, AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 727B+5, RBL 3. REPAIRED CHANNEL PER EA.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 60,603 hrs · 57,180 cycles

DURING SCHEDULED 20Y CHECK FOUND, AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 727B+5, RBL 8.10. REPAIRED CHANNEL PER EA.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 60,603 hrs · 57,180 cycles

DURING SCHEDULED 20Y CHECK FOUND, AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 772, LBL 8.10. REPAIRED CHANNEL PER EA.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 60,603 hrs · 57,180 cycles

DURING SCHEDULED 20Y CHECK FOUND, AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 727B+5, LBL 3. REPAIRED CHANNEL PER EA.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 60,603 hrs · 57,180 cycles

DURING SCHEDULED 20Y CHECK FOUND, AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 860, RBL 3. REPAIRED CHANNEL PER EA.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 60,603 hrs · 57,180 cycles

DURING SCHEDULED 20Y CHECK FOUND, AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 772, RBL 8.10. REPAIRED CHANNEL PER EA.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 60,603 hrs · 57,180 cycles

DURING SCHEDULED 20Y CHECK FOUND, CLIP ANGLE CRACKED AT BS 312, WL 181.37. REPAIRED ANGLE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,603 hrs · 57,180 cycles

DURING SCHEDULED 20Y CHECK FOUND, STRINGER CLIP CRACKED AT BS 747, STR 18L. REMOVED AND REPLACED CLIP PER SRM.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 60,603 hrs · 57,180 cycles

DURING SCHEDULED 20Y CHECK FOUND, AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 727B+5, LBL 8.10. REPAIRED CHANNEL PER EA.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 60,603 hrs · 57,180 cycles

DURING SCHEDULED 20Y CHECK FOUND, AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 772, RBL 3. REPAIRED CHANNEL PER EA.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 60,603 hrs · 57,180 cycles

DURING SCHEDULED 20Y CHECK FOUND, AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 860, LBL 3. REPAIRED CHANNEL PER EA.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 60,603 hrs · 57,180 cycles

DURING SCHEDULED 20Y CHECK FOUND, LT WING AFT FLAP DELAMINATED ON O/B SIDE LOWER SKIN. REPAIRED AFT FLAP PER SRM.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 60,603 hrs · 57,180 cycles

DURING SCHEDULED 20Y CHECK FOUND, AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 860, LBL 8.10. REMOVED AND REPLACED CHANNEL PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,603 hrs · 57,180 cycles

DURING SCHEDULED 20Y CHECK FOUND, STRINGER CLIP CRACKED AT BS 400, STR 27L. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — DAMAGED (HORIZ STAB) · airframe 60,603 hrs · 57,180 cycles

DURING SCHEDULED 20Y CHECK, FOUND LT HORIZONTAL STABILIZER SKIN MISSING MATERIAL BETWEEN STA 161.04 TO STA 170.34. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,603 hrs · 57,180 cycles

DURING SCHEDULED 20Y CHECK FOUND, FUSELAGE SKIN CRACKED AT BS R1 DOOR UPPER FWD CORNER BETWEEN BS 291.5 TO BS 303.9. REPAIRED SKIN PER SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 60,603 hrs · 57,180 cycles

DURING SCHEDULED 20Y CHECK, FOUND ANGLE CORRODED BETWEEN BS 294.5 TO BS 328 STR 17R. REMOVED AND REPLACED ANGLE PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 60,603 hrs · 57,180 cycles

DURING SCHEDULED 20Y CHECK FOUND, SHEAR TIE CRACKED AT BS 360, BETWEEN STR 13L TO STR 14L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 660,603 hrs · 57,180 cycles

DURING SCHEDULED 20Y CHECK FOUND, WEB CORRODED BETWEEN BS 727C TO BS 747, STR 17L. REMOVED AND REPLACED WEB PER SRM AND DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 60,603 hrs · 57,180 cycles

DURING SCHEDULED 20Y CHECK FOUND, CLIP ANGLE CRACKED AT BS 320, WL 181.37. REMOVED AND REPLACED ANGLE PER SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 60,603 hrs · 57,180 cycles

DURING SCHEDULED 20Y CHECK FOUND, CLIP ANGLE CRACKED AT BS 328, WL 181.37. REMOVED AND REPLACED ANGLE PER SRM.

Part: LENS — DELAMINATED (CABIN) · airframe 60,603 hrs · 57,180 cycles

DURING SCHEDULED 20Y CHECK FOUND, R1 DOOR EMERGENCY EXIT LIGHT LENS DELAMINATED. REMOVED AND REPLACED LENS PER MM.

Part: LENS — BROKEN (CABIN) · airframe 60,603 hrs · 57,180 cycles

DURING SCHEDULED 20Y CHECK FOUND, R2 DOOR EMERGENCY EXIT LENS BROKEN. REMOVED AND REPLACED LENS PER MM.

Part: LENS — LOOSE (CABIN) · airframe 60,208 hrs · 56,919 cycles

RT EMERGENCY EXIT LIGHT LOOSE. SECURED LENS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,208 hrs · 56,919 cycles

DURING SCHEDULED CV CHECK, FOUND SKIN CRACKED AT BS 950.5, STR 24R. REPAIRED SKIN PER SRM.

Part: SIGN — LOOSE (CABIN) · airframe 60,113 hrs · 56,850 cycles

RT OVERWING EXIT DOOR EMERGENCY EXIT SIGN LOOSE. SECURED LIGHT ASSY PER MM.

Part: FITTING — CORRODED (GIRT BAR) · airframe 59,908 hrs · 56,704 cycles

DURING SCHEDULED SPV CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE GIRT BAR FITTING PLATES CORRODED. REMOVED AND REPLACED FITTING PER MM.

Part: FITTING — CORRODED (EVAC SLIDE) · airframe 59,908 hrs · 56,704 cycles

DURING SCHEDULED SPV CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE GIRT BAR FITTING PLATES CORRODED. REMOVED AND REPLACED FITTING PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 59,908 hrs · 56,704 cycles

DURING SCHEDULED SPV CHECK, FOUND FWD CARGO COMPARTMENT FRAME CRACKED AT BS 482A, STR 22R. REMOVED AND REPLACED FRAME PER SRM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 59,452 hrs · 56,385 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT AFT EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: PLATE — CRACKED (R1 DOOR) · airframe 59,331 hrs · 56,297 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR HOOK ATTACH HOLES CRACKED. REPAIRED PLATE ASSY PER EA.

Part: SKIN — GOUGED (LE SLAT) · airframe 59,331 hrs · 56,297 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND RT WING NR 6 I/B SLAT CAN LOWER SURFACE GOUGED. REMOVED AND REPLACED SLAT CAN PER SRM.

Part: HINGE — LOOSE (AILERON TAB) · airframe 59,331 hrs · 56,297 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND RT WING AILERON CONTROL TAB NR 1 HINGE LOOSE. REMOVED AND REPLACED TAB ASSY PER MM.

Part: HINGE — LOOSE (AILERON TAB) · airframe 59,331 hrs · 56,297 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND RT WING AILERON CONTROL TAB NR 4 HINGE LOOSE. REMOVED AND REPLACED TAB ASSY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,897 hrs · 56,003 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED BETWEEN BS 802 TO BS 805, STR 20L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,897 hrs · 56,003 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 934.5, STR 24L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,897 hrs · 56,003 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 932, STR 24L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,897 hrs · 56,003 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 957, STR 21L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,897 hrs · 56,003 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED BETWEEN BS 842 TO BS 845, STR 24L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,897 hrs · 56,003 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 933, STR 23L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,897 hrs · 56,003 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 830, STR 23L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,816 hrs · 60,948 cycles

SKIN CRACKED AT BS 932, STR 24L. REPAIRED SKIN PER SRM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 58,738 hrs · 55,890 cycles

DURING SCHEDULED MV2 CHECK, FOUND EMERGENCY LIGHT BATTERY PACK INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,082 hrs · 56,123 cycles

DURING SCHEDULED MV1 CHECK, FOUND SKIN CRACKED AT BS 780, STR 18L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,608 hrs · 55,800 cycles

DURING SCHEDULED MV1 CHECK, FOUND SKIN CRACKED AT BS 937, STR 21R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,529 hrs · 55,033 cycles

DURING SCHEDULED MV1 CHECK, FOUND SKIN CRACKED AT BS 397, STR 16R. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 57,577 hrs · 55,067 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,529 hrs · 55,033 cycles

DURING SCHEDULED MV1 CHECK, FOUND SKIN CRACKED AT BS 403, STR 16R. REPAIRED SKIN PER SRM.

Part: LENS — BROKEN (CABIN) · airframe 57,163 hrs · 54,779 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,107 hrs · 54,095 cycles

DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 747+12, STR 23L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,107 hrs · 54,095 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 482B+15, STR 16L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,107 hrs · 54,095 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 747, STR 23L. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 56,107 hrs · 54,095 cycles

DURING SCHEDULED MV2 CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 56,107 hrs · 54,095 cycles

DURING SCHEDULED MV2 CHECK, FOUND L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,923 hrs · 53,979 cycles

DURING SCHEDULED MV1 CHECK, FOUND SKIN CRACKED AT BS 799, STR 24L. REPAIRED SKIN PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 55,641 hrs · 53,797 cycles

DURING SCHEDULED 18Y CHECK, FOUND LONGITUDINAL FLOORBEAM WEB CRACKED AT BS 713, LBL 24.5. REPAIRED WEB PER AAR EA.

Part: SLAT — DELAMINATED (RT WING) · airframe 55,718 hrs · 53,850 cycles

DURING SCHEDULED 18Y CHECK, FOUND RT WING NR 6 SLAT I/B AFT UPPER CORNER DELAMINATED. REPAIRED SLAT PER SRM.

Part: SLAT — DELAMINATED (RT WING) · airframe 55,641 hrs · 53,797 cycles

DURING SCHEDULED 18Y CHECK, FOUND RT WING L/E NR 4 SLAT O/B LOWER SURFACE DELAMINATED. REMOVED AND REPLACED SLAT PER MM.

Part: FITTING — CORRODED (HORIZ STAB) · airframe 55,641 hrs · 53,797 cycles

DURING SCHEDULED 18Y CHECK, FOUND LT HORIZONTAL STABILIZER FITTINGS LUG FACE CORRODED. REPAIRED FITTINGS PER SRM.

Part: SLAT — DELAMINATED (RT WING) · airframe 55,641 hrs · 53,797 cycles

DURING SCHEDULED 18Y CHECK, FOUND RT WING NR 4 SLAT O/B CORNER DELAMINATED. REPAIRED SLAT PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 55,641 hrs · 53,797 cycles

DURING SCHEDULED 18Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED BS 692, RBL 24.5. REPAIRED BEAM PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 55,641 hrs · 53,797 cycles

DURING SCHEDULED 18Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED BETWEEN BS 707 TO BS 714, BBL 0.07. REPAIRED WEB PER SRM.

Part: SLAT — DELAMINATED (RT WING) · airframe 55,641 hrs · 53,797 cycles

DURING SCHEDULED 18Y CHECK, FOUND RT WING NR 5 SLAT O/B AFT UPPER CORNER DELAMINATED. REPAIRED SLAT PER SRM.

Part: PLATE — CORRODED (GIRT BAR) · airframe 55,641 hrs · 53,797 cycles

DURING SCHEDULED 18Y CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR PLATE CORRODED. REMOVED AND REPLACED PLATE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,815 hrs · 53,267 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR UPPER HINGE CUTOUT, BETWEEN BS 303 TO BS 304, BETWEEN WL 259 TO WL 260. REPAIRED SKIN PER AAR EA.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 54,815 hrs · 53,267 cycles

DURING SCHEDULED SPV CHECK, FOUND AFT CARGO FLOOR LOWER FRAME ATTACH ANGLE CRACKED AT BS 794, RBL 8. REMOVED AND REPLACED ANGLE PER BAC DWG.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 54,815 hrs · 53,267 cycles

DURING SCHEDULED SPV CHECK, FOUND AFT CARGO DOOR CUTOUT FWD FRAME CRACKED AT O/B LOWER CORNER OF LOWER DOOR STOP FITTING. REPAIRED FRAME PER AAR EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,815 hrs · 53,267 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER AAR EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,815 hrs · 53,267 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR LOWER HINGE CUTOUT BS 303, WL 239.5. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,815 hrs · 53,267 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR LOWER HINGE CUTOUT CRACKED AT BS 304.5, WL 239.5. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 54,621 hrs · 53,138 cycles

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

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 54,624 hrs · 53,141 cycles

DURING SCHEDULED MV1 CHECK, FOUND SEVERAL EGRESS LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,000 hrs · 51,834 cycles

DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SRM.

Part: BATTERY PACK — FAULTY (CABIN) · airframe 52,187 hrs · 51,251 cycles

UPON ARRIVAL TO AIRCRAFT, EMERGENCY EXIT LIGHTS ON. REMOVED AND REPLACED BATTERY PACKS PER MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 52,024 hrs · 51,126 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,777 hrs · 50,938 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 764, STR 25L. REPAIRED STRINGER PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 51,268 hrs · 50,545 cycles

DURING SCHEDULED MV2 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 6 ABC. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 51,149 hrs · 50,444 cycles

DURING SCHEDULED MV2 CHECK, FOUND MID CABIN CENTER AISLE OVERWING EMERGENCY EXIT SIGN INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,007 hrs · 50,325 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 944, STR 24L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,995 hrs · 50,316 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 941, STR 23R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,995 hrs · 50,316 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 944, STR 24L. REPAIRED SKIN PER SWA EA.

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 50,825 hrs · 50,188 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT OVERWING EMERGENCY BATTERY PACK INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 50,445 hrs · 49,895 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE SKIN CORRODED AT BEAR STRAP BS 790, RBL 19. REPAIRED SKIN PER EA.

Part: SKIN — CORRODED (FUSELAGE) · airframe 50,445 hrs · 49,895 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 790, STR 25R. REPAIRED SKIN PER SRM.

Part: CHARGER — FAULTY (EMERGENCY LIGHTS) · airframe 50,445 hrs · 49,895 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT LT LOWER FUSELAGE EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED BATTERY CHARGER PER MM.

Part: SKIN — CRACKED (BS 847) · airframe 50,445 hrs · 49,895 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BEAR STRAP BS 847, RBL 15. REPAIRED SKIN PER ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,445 hrs · 49,895 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 294, STR 16R. REPAIRED FRAME PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,445 hrs · 49,895 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 413, LBL 3. REPAIRED SKIN PER ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,445 hrs · 49,895 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727, STR 14R. REPAIRED FRAME PER ER.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 50,445 hrs · 49,895 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER 26R CORRODED AT BS 480. REPAIRED STRINGER PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 50,445 hrs · 49,895 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 847, RBL 15, WL 150. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 50,445 hrs · 49,895 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CRACKED AT BS 360, LBL 13.5. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 50,445 hrs · 49,895 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 807, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 50,445 hrs · 49,895 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 827, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 50,445 hrs · 49,895 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 482B, STR 6R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 50,445 hrs · 49,895 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CRACKED AT BS 360, STR 15R. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 50,445 hrs · 49,895 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 847, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,445 hrs · 49,895 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 887, STR 25R. REPAIRED SKIN PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 50,445 hrs · 49,895 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT PRESSURE BULKHEAD WEB CRACKED AT BS 1016, STR 6L. REMOVED AND REPLACED WEB PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 50,445 hrs · 49,895 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER 5L CRACKED AT BS 1010. REPAIRED STRINGER PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 50,445 hrs · 49,895 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 312, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 50,445 hrs · 49,895 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CRACKED AT BS 360, STR 13R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 50,445 hrs · 49,895 cycles

DURING SCHEDULED 16Y CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 360 TO BS 380, LBL 70. REMOVED AND REPLACED WEB PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 50,445 hrs · 49,895 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 867, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 50,445 hrs · 49,895 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 15R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 50,445 hrs · 49,895 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SLAT — DELAMINATED (LT WING) · airframe 50,445 hrs · 49,895 cycles

DURING SCHEDULED 16Y CHECK, FOUND LT WING NR 1 L/E SLAT INBOARD T/E DELAMINATED. REPAIRED SLAT PER SRM.

Part: FITTING — CORRODED (GIRT BAR) · airframe 50,445 hrs · 49,895 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 50,445 hrs · 49,895 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 482B, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 50,445 hrs · 49,895 cycles

DURING SCHEDULED 16Y CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 807 TO BS 827, RBL 70. REMOVED AND REPLACED WEB PER SRM.

Part: FITTING — CORRODED (GIRT BAR) · airframe 50,445 hrs · 49,895 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 50,445 hrs · 49,895 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 50,445 hrs · 49,895 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 7R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 50,445 hrs · 49,895 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 867, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SKIN — DELAMINATED (T/E FLAP) · airframe 50,445 hrs · 49,895 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 50,445 hrs · 49,895 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 50,445 hrs · 49,895 cycles

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

Part: SKIN — CRACKED (L/E SLAT) · airframe 50,445 hrs · 49,895 cycles

DURING SCHEDULED 16Y CHECK, FOUND RT WING NR 6 L/E SLAT SKIN CRACKED AT OUTBOARD T/E. REPAIRED SLAT PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 50,445 hrs · 49,895 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 7L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 50,445 hrs · 49,895 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 50,445 hrs · 49,895 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 50,445 hrs · 49,895 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 50,445 hrs · 49,895 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 50,445 hrs · 49,895 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,445 hrs · 49,895 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 750, STR 18L. REPAIRED SKIN PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,445 hrs · 49,895 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,445 hrs · 49,895 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 482, STR 8R AND STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,445 hrs · 49,895 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 520, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,445 hrs · 49,895 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,445 hrs · 49,895 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 597, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,445 hrs · 49,895 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8R AND STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,445 hrs · 49,895 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727B, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,445 hrs · 49,895 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 482A, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,445 hrs · 49,895 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727B, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,445 hrs · 49,895 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8R. REPAIRED FRAME PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,445 hrs · 49,895 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 479, STR 23R. REPAIRED SKIN PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,445 hrs · 49,895 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,445 hrs · 49,895 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 277, STR 16L. REPAIRED FRAME PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 50,445 hrs · 49,895 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FLOORBEAM CORRODED AT BS 946, RBL 5. REPAIRED FLOORBEAM PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 50,445 hrs · 49,895 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 727B, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,445 hrs · 49,895 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8L. REPAIRED FRAME PER SWA EA.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 50,445 hrs · 49,895 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER 4L CRACKED AT BS 867. REPAIRED STRINGER PER SRM.

Part: DOOR FRAME — CRACKED (BS 440) · airframe 50,246 hrs · 49,721 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FWD CARGO DOOR CUTOUT, FWD FRAME CRACKED AT BS 440, LOWER STOP FITTING. REMOVED AND REPLACED FWD CARGO DOOR FWD FRAME PER SWA ACO.

Part: DOOR FRAME — CRACKED (AFT CARGO DOOR) · airframe 50,246 hrs · 49,721 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND AFT CARGO DOOR FRAME LOWER FWD CORNER CRACKED. REMOVED AND REPLACED AFT CARGO DOOR PER MM.

Part: DOOR FRAME — CRACKED (BS 492) · airframe 50,246 hrs · 49,721 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FWD CARGO DOOR CUTOUT, AFT FRAME CRACKED AT BS 492, LOWER STOP FITTING. REMOVED AND REPLACED FWD CARGO DOOR AFT FRAME PER SWA ACO.

Part: FRAME — CRACKED (BS 492 S17R) · airframe 50,246 hrs · 49,721 cycles

DURING SCHEDULED SPV CHECK, FOUND BELTFRAME CRACKED AT BS 492, STR 17R. REPAIRED FRAME PER SRM.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 49,655 hrs · 49,163 cycles

L2 DOOR EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 49,554 hrs · 49,058 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CREASED AT BS 426, STR 17R. REPAIRED SKIN PER SWA EA.

Part: GLOWSTRIP — WORN (CABIN) · airframe 48,619 hrs · 48,168 cycles

DURING SCHEDULED MV2 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP WORN BETWEEN ROW 4 DEF AND ROW 6 DEF. REMOVED AND REPLACED STRIP PER MM.

Part: SKIN — CRACKED (BS 970 S21L) · airframe 47,804 hrs · 47,361 cycles

DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 970, STR 21L. REPAIRED SKIN PER SRM.

Part: FITTING — CORRODED (RT WING) · airframe 47,765 hrs · 47,323 cycles

DURING SCHEDULED MV2 CHECK, FOUND RIGHT MLG WALKING BEAM OUTBOARD FWD STABILIZER FITTING CORRODED. REPAIRED FITTING PER SWA EA.

Part: FITTING — CORRODED (LT WING) · airframe 47,765 hrs · 47,323 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT MLG WALKING BEAM OUTBOARD FWD STABILIZER FITTING CORRODED. REPAIRED FITTING PER SWA EA.

Part: FITTING — CORRODED (RT WING) · airframe 47,765 hrs · 47,323 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT MLG AFT HANGER FITTING CORRODED. REMOVED AND REPLACED AFT FITTING PER SRM.

Part: SIGN — LOOSE (CABIN) · airframe 47,664 hrs · 47,228 cycles

RIGHT OVERWING EMERGENCY EXIT SIGN LOOSE. SECURED SIGN PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 47,515 hrs · 47,082 cycles

LEFT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 47,301 hrs · 46,874 cycles

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

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 46,631 hrs · 46,160 cycles

LEFT OVERWING EMERGENCY EXIT SIGN LENS LOOSE. SECURED SIGN LENS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 46,554 hrs · 46,076 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: SKIN — CRACKED (LT WING) · airframe 46,277 hrs · 45,783 cycles

DURING SCHEDULED 14Y CHECK, FOUND LT WING SKIN CRACKED AT LOWER SURFACE MID SPAR, OUTBOARD STRUT. REPAIRED SKIN PER EA.

Part: DOOR — BROKEN (COCKPIT) · airframe 46,277 hrs · 45,783 cycles

DURING SCHEDULED 14Y CHECK, FOUND FIRST OFFICER'S EMERGENCY ESCAPE ROPE ACCESS DOOR BROKEN. REMOVED AND REPLACED ACCESS DOOR PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 45,468 hrs · 44,911 cycles

DURING SCHEDULED C2 CHECK, FOUND LH EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 45,283 hrs · 44,709 cycles

L1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM.

Part: SKIN — CRACKED (BS 750) · airframe 44,929 hrs · 44,342 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 750, STR 18L. REPAIRED SKIN PER SRM.

Part: BRACKET — CRACKED (R2 DOOR SLIDE) · airframe 44,572 hrs · 43,992 cycles

DURING SCHEDULED C1 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE FWD ATTACH MOUNT BRACKET CRACKED. REMOVED AND REPLACED MOUNT BRACKET PER MM.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 44,222 hrs · 43,640 cycles

DURING SCHEDULED SERVICE CHECK, FOUND CABIN EMERGENCY LIGHT INOP AT ROW 20 DEF. RELAMPED LIGHT PER MM.

Part: LENS — BROKEN (AFT GALLEY) · airframe 43,599 hrs · 42,985 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND L2 DOOR EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LENS PER SRM.

Part: BALLAST — INOPERATIVE (EMERGENCY LIGHT) · airframe 43,079 hrs · 42,426 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 42,970 hrs · 42,308 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 258, STR 19L TO STR 22L. REPAIRED SKIN PER SRM.

Part: FITTING — CRACKED (NLG WW) · airframe 42,352 hrs · 41,661 cycles

DURING SCHEDULED RON CHECK, FOUND NLG ACTUATOR UPPER ATTACH FITTING GUSSET CRACKED. REMOVED AND REPLACED GUSSET PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 42,076 hrs · 41,352 cycles

DURING SCHEDULED SERVICE CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT BETWEEN ROWS 16 DEF AND 17 DEF, INOP. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 41,968 hrs · 41,232 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 787, STRINGER 25L, CRACKED. REPAIRED SKIN PER SRM.

Part: SLIDE — DAMAGED (R2 DOOR) · airframe 39,926 hrs · 39,231 cycles

R2 DOOR EVAC SLIDE HIGH PRESSURE INDICATION. REMOVED AND REPLACED R2 DOOR EVAC SLIDE PER MM.

Part: WINDOW POST — CRACKED (FUSELAGE) · airframe 39,456 hrs · 38,744 cycles

DURING SCHEDULED 1/4D CHECK, FOUND COCKPIT NR 1 WINDOW LT POST, OUTBOARD UPPER CORNER CRACKED. REPAIRED WINDOW POST PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 39,456 hrs · 38,744 cycles

DURING SCHEDULED 1/4D CHECK, FOUND MLG UPPER DECK BEADED WEB AT BS 665 TO BS 673, LBL 30 TO LBL 35, CRACKED. REPAIRED WEB PER SRM.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 39,456 hrs · 38,744 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM SUPPORT AT BS 660, BL 0, CRACKED. REPAIRED FLOORBEAM SUPPORT PER EA.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 36,958 hrs · 36,421 cycles

DURING SCHEDULED C4 CHECK, FOUND BOTH LEFT AND RIGHT HORIZ STAB SKIN CRACKED ON LOWER SURFACE AT REAR SPAR ATTACHMENT POINT, LEFT AND RIGHT AT STA 145 AND RT AT STA 152. REPAIRED SKIN PER SRM.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 36,860 hrs · 36,327 cycles

AFT CABIN LOWER EMEGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT BATTERY PER MM.

Part: BRACKET — LOOSE (FWD CABIN DOORS) · airframe 36,031 hrs · 35,586 cycles

DURING SCHEDULED C3 CHECK, FOUND BOTH FWD CABIN DOOR EMERGENCY EVAC SLIDE GIRT BAR ATTACH BRACKETS LOOSE. SECURED ATTACH BRACKETS PER MM.

Part: SLIDE — DEPLOYED (AFT SVC DOOR) · airframe 33,395 hrs · 33,096 cycles

DURING SCHEDULED A1 CHECK, AFT SVC DOOR EMERGENCY EVAC SLIDE INADVERTENTLY DEPLOYED. REMOVED AND REPLACED SLIDE PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 31,289 hrs · 31,120 cycles

DURING SCHEDULED D CHECK, FOUND FRAME FASTENER HOLES CRACKED ( 2 EA ) AT BS 827, BETWEEN STR 8R & 9R, AND BS 867, BETWEEN STR 8R & 9R. REPAIRED FRAMES PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 31,289 hrs · 31,120 cycles

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORRODED AT BS 986, RBL 21 & WL 208. REPAIRED FLOORBEAM PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 31,289 hrs · 31,120 cycles

DURING SCHEDULED D CHECK, FOUND FRAME CRACKED AT BS 360, BETWEEN STR 7L & 8L. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 31,289 hrs · 31,120 cycles

DURING SCHEDULED D CHECK, FOUND FRAME FASTENER HOLES CRACKED ( 2 EA ) AT BS 400, STR 8 L, AND BS 360, STR 8 L. REPAIRED FRAMES PER SRM.

Part: FRAME — CRACKED (FWD CABIN) · airframe 31,289 hrs · 31,120 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 294.5, WL 209 & RBL 55. REPAIRED FRAME PER BFG ER 01-0838.

Part: FRAME — CRACKED (FUSELAGE) · airframe 31,289 hrs · 31,120 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 188, STR 17L. REPAIRED FRAME PER SRM.

Part: CLIP — CRACKED (FUSELAGE) · airframe 18,880 hrs · 16,594 cycles

DURING SCHEDULED D CHECK, FOUND STR CLIPS CRACKED ( 4 EA ) AT BS 312, STR 24R, BS 663, STR 10L, BS 683, STR 4L, BS 1088, STR 17L. R&R STR CLIPS PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 31,289 hrs · 31,120 cycles

DURING SCHEDULED D CHECK, FOUND STRINGER CRACKED AT BS 312, STR 24R. REPAIRED STRINGER PER SRM.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 31,289 hrs · 31,120 cycles

DURING SCHEDULED D CHECK, FOUND STR SPLICE CRACKED AT BS 907, STR 4R. R&R STR SPLICE PER SRM.

Part: CLIP — CRACKED (FUSELAGE) · airframe 31,289 hrs · 31,120 cycles

DURING SCHEDULED D CHECK, FOUND STR CLIPS CRACKED ( 4 EA ) AT BS 887, STR 4L & 4R, BS 328, STR 24R, BS 663, STR 10R. R&R STR CLIPS PER SRM.

Part: CLIP — CRACKED (FUSELAGE) · airframe 31,289 hrs · 31,120 cycles

DURING SCHEDULED D CHECK, FOUND STR CLIPS CRACKED ( 2 EA ) AT BS 727, STR 2L & 2R. R&R STR CLIPS PER SRM.

Part: BRACKET — CORRODED (CABIN) · airframe 18,880 hrs · 16,594 cycles

DURING SCHEDULED D CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE FLOOR BRACKET CORRODED. R&R EVAC SLIDE FLOOR BRACKET PER SRM.

Part: LENS — OUT OF POSITION (CABIN) · airframe 31,198 hrs · 31,030 cycles

RT OVERWING EMERGENCY EXIT LIGHT LENS FELL OFF. SECURED EXIT LENS PER MM.

Part: COVER — LOOSE (CABIN) · airframe 31,115 hrs · 30,954 cycles

EEPLS COVER LOOSE. SECURED EEPLS COVER PER MM.

Part: WIRE — DISCONNECTED (CABIN) · airframe 31,078 hrs · 30,913 cycles

EEPLS INOP BETWEEN ROWS 12 & 15. RECONNECTED WIRES PER MM.

Part: WIRE — DISCONNECTED (CABIN) · airframe 31,067 hrs · 30,905 cycles

EEPLS INOP IN NUMEROUS PLACES. RECONNECTED WIRES PER MM.

Part: WIRE — DISCONNECTED (CABIN) · airframe 30,544 hrs · 30,369 cycles

EEPLS SEGMENT INOP. RECONNECTED EEPLS WIRES PER MM.

Part: COVER — LOOSE (CABIN) · airframe 30,544 hrs · 30,369 cycles

DURING SCHEDULED C1 CHECK, FOUND EEPLS COVER LOOSE AT AFT CABIN. Removed and replaced EEPLS COVER PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,544 hrs · 30,369 cycles

DURING SCHEDULED C1 CHECK, FOUND EEPLS INOP AT ROW 1 & ROW 2. RELAMPED EEPLS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,557 hrs · 30,387 cycles

DURING SCHEDULED C1 CHECK, FOUND EEPLS LIGHTS INOP IN VARIOUS LOCATIONS. Removed and replaced CONNECTOR BLOCK AND RECONNECTED WIRES PER MM.

Part: WIRE — BROKEN (CABIN) · airframe 30,498 hrs · 30,326 cycles

EEPLS WIRES BROKEN AT ROW 13. REPAIRED EEPLS WIRES PER MM.

Part: CAP — MISSING (CABIN) · airframe 30,306 hrs · 30,123 cycles

EEPLS END CAP MISSING ON FWD END. INSTALLED END CAP PER MM.

Part: LENS — MISSING (CABIN) · airframe 29,903 hrs · 29,726 cycles

EEPLS LENS MISSING AT ROW 7. INSTALLED LENS PER MM.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 29,734 hrs · 29,550 cycles

DURING SCHEDULED C4 CHECK, FOUND LT HORIZ STAB SKIN CRACK 3 LONG, 37 OUTBOARD OF FUSELAGE AT AFT SPAR FASTENER ROW. REPAIRED SKIN PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,734 hrs · 29,550 cycles

DURING SCHEDULED C4 CHECK, FOUND EEPLS INOP FROM ROW 19 AFT. SECURED CONNECTOR PER MM.

Part: WIRE — DISCONNECTED (CABIN FLOOR) · airframe 29,241 hrs · 29,074 cycles

FOUR EEPLS LIGHTS INOP AT ROW 20. SECURED EEPLS WIRING PER MM.

Part: SLIDE — OUT OF ADJ (CABIN) · airframe 29,087 hrs · 28,922 cycles

EVAC SLIDE GIRT ASSY ON 3 OF 4 DOORS ARE OUT OF ADJUSTMENT. READJUSTED EVAC SLIDE ASSY PER MM.

Part: WIRE — DAMAGED (CABIN) · airframe 28,872 hrs · 28,714 cycles

EEPLS INOP AT ROWS 1 & 15. REPAIRED EEPLS WIRING AND REPLACED TRACK COVERS PER MM.

Part: LENS — MISSING (CABIN) · airframe 28,864 hrs · 28,705 cycles

OVERHEAD EMERGENCY EXIT LIGHT LENS MISSING AT ROW 6. REPLACED LENS PER MM.

Part: WIRE — INOPERATIVE (CABIN FLOOR) · airframe 28,816 hrs · 28,646 cycles

DURING SCHEDULED C3 CHECK, FOUND EEPLS INOP AT ROWS 10 TO 15. RE-PINNED CONNECTOR WIRING PER MM.

Part: COVER — LOOSE (CABIN FLOOR) · airframe 28,816 hrs · 28,646 cycles

DURING SCHEDULED C3 CHECK, FOUND EEPLS TRACK COVER LOOSE AT ROW 7. SECURED TRACK COVER PER MM.

Part: COVER — LOOSE (CABIN) · airframe 27,931 hrs · 27,771 cycles

EEPLS TRACK COVER LOOSE. RESECURED TRACK COVERS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,815 hrs · 27,658 cycles

EEPLS INOP AT MID CABIN. RECONNECTED LIGHTS PER MM, OPS CK GOOD.

Part: SLIDE — DISCHARGED (SERVICE DOOR) · airframe 27,521 hrs · 27,374 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FWD SERVICE DOOR EVACUATION SLIDE PRESS IND LOW. REMOVED AND REPLACED SLIDE ASSY PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,502 hrs · 27,355 cycles

EEPLS INOP AT ROW 4. REPAIRED WIRING PER MM.

Part: BRACKET — BROKEN (GIRT BAR) · airframe 24,173 hrs · 27,031 cycles

DURING SCHEDULED C1 CHECK, FOUND FWD ENTRY DOOR EVACUATION SLIDE FWD GIRT BAR ATTACH BRACKET BROKEN AT CONTAINER. REPAIRED BRACKET TO CONTAINER PER SRM.

Part: BRACKET — LOOSE (GIRT BAR)

DURING SCHEDULED C4 CHECK, FOUND AFT ENTRY AND SERVICE DOOR EVACUATION SLIDE AFT GIRT BAR FLOOR BRACKETS LOOSE. TIGHTENED BRACKETS PER MM.

Part: LIGHT — INOPERATIVE (ROW 6)

EEPLS INOP AT ROW 6. RELAMPED PER MM.

Part: SKIN — BIRD STRIKE (FUSELAGE)

AIR TURNBACK, SEVERAL BIRD STRIKES DURING CLIMB OUT. C/W BIRD STRIKE INSPECTION AND FOUND DAMAGED NOSE RADOME, RADAR ANTENNA, NR 2 KRUGER FLAP BELL CRANK ARM, AND FUSELAGE SKIN STRUCTURE DAMAGED FWD OF E/E DOOR. NO ENGINE INGESTION NOTED. REMOVED AND REPLACED NOSE RADOME, RADAR ANTENNA, NR 2 KRUGER FLAP BELL CRACK ARM AND REPAIRED FUSELAGE SKIN STRUCTURE.

Part: LATCH — BROKEN (COCKPIT)

F/O'S EMERGENCY ESCAPE ROPE DOOR LATCH BROKEN. REMOVED AND REPLACED PANEL ASSY PER MM.

Part: BULKHEAD CHORD — CRACKED (BS 178)

DURING SCHEDULED 1/4D CHECK, FOUND BS 178 BULKHEAD RT CHORD CRACKED, RBL 28.5. REMOVED AND REPLACED RT CHORD PER SRM.

Part: GUSSET — CRACKED (SERVICE DOOR)

DURING SCHEDULED 1/4D CHECK, FOUND FWD SERVICE DOOR AFT LOWER STUB FRAME GUSSET CRACKED. REMOVED AND REPLACED STUB FRAME GUSSET PER SRM.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED 1/4D CHECK, FOUND THROUGH ULTRASONIC INSPECTION 3 EACH CRACKS AT BS 178 BULKHEAD, LBL 5 - RBL 5. REPAIRED BULKHEAD PER SRM.

Part: CASTING — CRACKED (NR 4 SPOILER)

DURING SCHEDULED 1/4D CHECK, FOUND CRACKED CASTING FOR NR 4 GROUND SPOILER ACTUATOR ATTACH FITTING. REPAIRED CASTING PER SWA RA NR 1-A57-0571.

Part: LIGHT — LOOSE (ROW 7, 11 & 19)

DURING SCHEDULED C2 CHECK, FOUND 3 EACH BULLNOSE EMERGENCY EGRESS LIGHTS LENSES LOOSE AT ROWS 7 ABC, 11 ABC, AND 19 ABC. SECURED LIGHT LENSES PER MM.

Part: LIGHT — DISCONNECTED (CABIN)

EMERGENCY ESCAPE FLOOR TRACK LIGHT, FWD SECTION INOP. RECONNECTED TRACK SECTION, OPS CHECKED GOOD PER MM.

Part: LIGHT — DETACHED (ROW 15)

EMERGENCY EXIT TRACK LIGHTING PULLED UP AT ROW 15. REPOSITIONED TRACK PER MM.

Part: LIGHT — INOPERATIVE (ROW 15-16)

EMERGENCY TRACK LIGHTS AT ROWS 14 TO 16 INOPERATIVE. DISCOVERED WIRING DISCONNECTED. RECONNECTED WIRING PER MM.

Part: LIGHT — INOPERATIVE (CABIN)

DURING FAA INSPECTING AIRCRAFT, FOUND EMERGENCY ESCAPE PATH LIGHTING INOP. FOUND LIGHT DISCONNECTED. RECONNECTED LIGHTS PER MM, OPS CK GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND FWD SECTION OF EMERGENCY EVACUATION FLOOR TRACK LIGHTING INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BULB — FAILED (CABIN)

DURING SCHEDULED A1 CHECK, FOUND EGRESS LIGHT NR 12 FROM THE FRONT INOP. RELAMPED PER M/M, OPS CHECK GOOD.

Part: LIGHT — LOOSE (CABIN)

DURING WALKAROUND CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTING STRIP ROW 12 LOOSE. RESECURED LOOSE EMERGENCY FLOOR LIGHT STRIP PER BOEING MM.

Part: BRACKET — CRACKED (PYLON)

DURING SCHEDULED C2 CHECK, FOUND NR 6 CANOE/PYLON AREA O/B SIDE ANGLE BRACKET CRACKED. REPAIRED PER BOEING SRM.

Part: BRACKET — CRACKED (RT LE FLAP)

DURING SCHEDULED C2 CHECK, FOUND K-FLAP MOST I/B SEAL BRACKET CRACKED. REPAIRED PER BOEING SRM.

Part: LIGHTS — INOPERATIVE (CABIN)

DURING SERVICE CHECK, FOUND EGRESS LIGHTING INOP AT ROW 13ABC. REPAIRED LOOSE WIRE CONNECTION AT ROW 13ABC PER BOEING MM. OPS CH'K GOOD.

Part: BALLAST — INOPERATIVE (CABIN)

DURING RON CHECK, FOUND LT EMERGENCY EXIT LIGHTS INOP. REPLACED BALLAST ALL PER BOEING M/M.

Part: SKIN — CRACKED (HORIZ STAB)

DURING SCHEDULED D-CHECK, FOUND INTERIM REPAIR ON RT HORIZ STAB LOWER SPAR SKIN. INSTALLED PERMANENT REPAIR PER BOEING SRM.

Part: SUPPORT — CORRODED (BS 482)

DURING SCHEDULED D-CHECK, FOUND BULKHEAD TO FLOOR SUPPORT CORRODED AT BS 482 FROM LBL 18 TO RBL 13. REPAIRED PER BOEING SRM.

Part: SUPPORT — CRACKED (BS 540)

DURING SCHEDULED D-CHECK, FOUND A FLOOR SUPPORT CRACK AT BS 540, BL 0 TO RBL 25, WL 208. REPLACED PER BOEING SRM.

Part: WINDSHIELD — CRACKED (LT COCKPIT)

IN FLIGHT, CAPTAIN'S NR 1 WINDSHIELD ARCED AND CRACKED, CAUSING RESTRICTED VISIBILITY. AIRCRAFT RETURNED TO MDW AND LANDED WITHOUT INCDENT. REPLACED WINDOW AND WINDOW HEAT CONTROLLER PER BOEING M/M.

Part: SLIDE — LOW PRESS (SERVICE DOOR)

DURING SCHEDULED RON CHECK, FOUND AFT SERVICE DOOR ESCAPE SLIDE PRESSURE LOW. REPLACED PER BOEING M/M.

Part: LIGHT — INOPERATIVE (CABIN)

DURING SCHEDULED CHECK, FOUND EMERGENCY EXIT LIGHT AT FWD ENTRY INOP. REPLACED LIGHT ASSEMBLY PER BOEING M/M.