N796SW

Part: COVER — OUT OF POSITION (L1 DOOR SLIDE) · airframe 65,190 hrs · 38,567 cycles

L1 DOOR VELCRO STRAP FELL FROM THE SLIDE WHEN FA MOVED THE GIRT BAR. / REPOSITIONED SAFETY FLAP COVER PER SIP.

Part: SEAL — CRACKED (RT HORIZ STAB) · airframe 64,792 hrs · 38,300 cycles

RIGHT HORIZONTAL STABILIZER FORWARD UPPER SLIDING SEAL CRACKED / REMOVED/REPLACED RIGHT HORIZONTAL STABILIZER FORWARD UPPER SLIDING SEAL PER AMM 53-31-31

Part: SEAL — CRACKED (LT WING) · airframe 64,792 hrs · 38,300 cycles

LEFT HORIZONTAL STABILIZER FORWARD UPPER SLIDING SEAL CRACKED / REMOVED AND REPLACED LEFT HORIZONTAL STABILIZER FORWARD UPPER SLIDING SEAL PER AMM 53-31-31

Part: SKIN — DENTED (FWD FUSELAGE) · airframe 63,820 hrs · 37,661 cycles

REFERENCE LOG PAGE # 0692466. BIRD STRIKE INSP. DAMAGE; DENT AT STA 186; JUST ABOVE STRINGER 24R LAP JOINT. / REF. LOG PAGE # 0692466; REPAIRED DAMAGE @ STA 186 JUST ABOVE STR 24R LAP JOINT IAW EA 190357 P1; P2 & IR; & SWA EA 1-753-34911 REV IR.

Part: BRACKET — OUT OF ADJUST (L2 DOOR SLIDE) · airframe 63,468 hrs · 37,427 cycles

L2 DOOR ESCAPE SLIDE OUT OF ADJUST. ADJUSTED GIRT BAR BRACKETS PER MM.

Part: HOOK AND LOOP — OUT OF ALIGNMENT (R2 DOOR) · airframe 63,229 hrs · 37,275 cycles

R2 DOOR SLIDE HOOK AND LOOP NOT ALIGNED. SECURED HOOK AND LOOP PER SIP.

Part: BALANCE WEIGHT — CORRODED (RUDDER) · airframe 62,778 hrs · 37,001 cycles

RUDDER COUNTERBALANCE WEIGHT CORRODED / REMOVED AND REPLACED RUDDER COUNTERBALANCE WEIGHT PER CMM 55-40-09

Part: SCUFF PLATE — CRACKED (AFT CARGO) · airframe 62,726 hrs · 36,969 cycles

AFT CARGO BAY FWD SCUFF PLATE IS CRACKED / RECIEVED NEW PART # 654A0004-97 TO BE INSTALLED ON CUSTOMER CARD # 753-140-00-02Y. 57006U 13JAN19

Part: SCUFF PLATE — CRACKED (AFT CARGO) · airframe 62,726 hrs · 36,969 cycles

AFT CARGO BAY AFT SCUFF PLATE IS CRACKED / RECIEVED NEW PART # 654A0004-169; TO BE INSTALLED ON CUSTOMER CARD # 753-140-00-02Y. 57006U 15JAN19

Part: SKIN — CORRODED (FUSELAGE) · airframe 62,726 hrs · 36,969 cycles

EXTERNAL SKIN UNDER DORSAL FIN CORRODED BETWEEN BS 847 TO BS 872, BETWEEN STR 2L TO STR 2R. REPAIRED SKIN IAW ER AND EA.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 62,726 hrs · 36,969 cycles

R1 DOOR STUB FRAME CUTOUT ANGLE CRACKED AT BS 294, WL 210. R&R ANGLE IAW DWG AND SRM.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 62,726 hrs · 36,969 cycles

RT MAIN WHEEL WELL STIFFENER CRACKED AT BS 663, BETWEEN RBL 8 TO RBL 31. R&R STIFFENER PER SRM AND DWG.

Part: NONE — OUT OF TOLERANCE (FWD CARGO) · airframe 62,726 hrs · 36,969 cycles

INTERCOSTAL SUPPORT IS OUT OF ROUND FASTENER HOLE AT FWD CARGO BAY BS500C LBL25 WL 157 / REMOVED CLIP PER SRM 51-40-02. LOCATED; DRILLED AND INSTALLED REPLACEMENT CLIP AT STA. 500L LBL 25 PER SRM 51-40-02 AND DWG 143A7505 91195U 1/6/19

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 62,726 hrs · 36,969 cycles

INTERCOSTAL CRACKED BETWEEN BS 1006 TO BS 1016, LBL 38. R&R INTERCOSTAL IAW SRM & DWG.

Part: SKIN — GOUGED (FUSELAGE) · airframe 62,726 hrs · 36,969 cycles

FUSELAGE SKIN GOUGED AT BS 1011, STR 14L. REPAIRED SKIN IAW ER AND EA.

Part: VAPOR BARRIER — CRACKED (FUSELAGE) · airframe 62,726 hrs · 36,969 cycles

RT VAPOR BARRIER CRACKED AT BS 663. REPAIRED BARRIER IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 62,726 hrs · 36,969 cycles

STRINGER CLIP CRACKED AT BS 360, STR 10L. R&R STRINGER CLIP PER SRM AND DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 62,726 hrs · 36,969 cycles

FORWARD CARGO BAY INTERCOSTAL SUPPORT ANGLE CRACKED AT BS 400, LBL 25. R&R ANGLE IAW SRM & DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 62,726 hrs · 36,969 cycles

FORWARD CARGO BAY INTERCOSTAL SUPPORT ANGLE CRACKED AT BS 500C, LBL 24. R&R ANGLE IAW SRM & DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 62,726 hrs · 36,969 cycles

FORWARD CARGO BAY AFT BULKHEAD TO FLOOR SUPPORT ANGLE CORRODED AT BS 500D, BETWEEN LBL 23 TO RBL 23. R&R ANGLE IAW SRM AND DWG.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 62,726 hrs · 36,969 cycles

FORWARD CARGO BAY ON AFT SHIELD CORRODED BETWEEN BS 494 TO BS 500A, RBL 23. R&R SHIELD IAW DWG AND SRM.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 62,726 hrs · 36,969 cycles

FORWARD CARGO BAY ON LOWER CHANNEL CORRODED AT BS 500A+12. R&R CHANNEL PER SRM AND DWG.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 62,726 hrs · 36,969 cycles

FORWARD CARGO BAY SUB THRESHOLD WEB CORRODED. R&R WEB IAW SRM AND DWG.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 62,726 hrs · 36,969 cycles

AFT CARGO BAY FORWARD BULKHEAD SUPPORT CRACKED AT BS 727, RBL 5. R&R SUPPORT PER SRM.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 62,726 hrs · 36,969 cycles

FORWARD CARGO BAY ON FORWARD SHIELD CORRODED BETWEEN BS 420 TO BS 440, RBL 23. R&R SHIELD IAW SRM & DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 62,726 hrs · 36,969 cycles

FORWARD CARGO BAY FLOOR TO SIDE WALL SUPPORT CORRODED BETWEEN BS 400 TO BS 500D, LBL 23. R&R SUPPORT IAW SRM AND DWG.

Part: GUSSET — CHAFED (FWD FUSELAGE) · airframe 62,726 hrs · 36,969 cycles

FOUND CHAFING ON S-27R TO FRAME GUSSET AT BS420 RBL6. MARKED / GUSSET AT STA. 420 RBL 6 OUT OF LIMITS DUE TO NO ALLOWABLE LIMITS IN SRM. REPAIRABLE BY REPLACEMENT PER SRM 51-10-02-0G-0; FABRICATED GUSSET OUT OF BAC 1493-856 7075T62 LOT #1249633 PER DWG. 143A1010. INSTALLED GUSSET PER SRM 51-40-02-0G-0 AND DWG. 143A8130. 91195U 12-28-18

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 62,726 hrs · 36,969 cycles

FORWARD CARGO BAY ON LOWER CHANNEL CORRODED AT BS 500+8. REPAIRED CHANNEL PER SRM AND DWG.

Part: SKIN — CHAFED (FUSELAGE) · airframe 62,726 hrs · 36,969 cycles

AFT CARGO COMPARTMENT FUSELAGE SKIN INTERNAL SURFACE CHAFED BETWEEN BS 754 TO BS 765, BETWEEN LBL 0 TO LBL 3. REPAIRED SKIN IAW ER AND EA.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 62,726 hrs · 36,969 cycles

AFT CARGO COMPARTMENT CARGO TRACK CORRODED BETWEEN BS 727+3 TO BS 887, RBL 13.5. R&R TRACK PER SRM AND DWG.

Part: SKIN — CHAFED (FUSELAGE) · airframe 62,726 hrs · 36,969 cycles

FUSELAGE SKIN INTERNAL SURFACE CHAFED BETWEEN BS 727E+7 TO BS 727E+18. 5, BETWEEN RBL 2 TO LBL 2. REPAIRED SKIN PER EA.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 62,726 hrs · 36,969 cycles

AFT CARGO COMPARTMENT FLOOR TO SIDEWALL SUPPORT SHIELD CORRODED BETWEEN BS 767 TO BS 794, RBL 20. R&R SHIELD IAW SRM AND DWG.

Part: SKIN — CHAFED (FUSELAGE) · airframe 62,726 hrs · 36,969 cycles

FUSELAGE SKIN INTERNAL SURFACE CHAFED AT BS 727E+5, RBL 17.5. REPAIRED SKIN PER EA.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 62,726 hrs · 36,969 cycles

AFT CARGO COMPARTMENT FLOOR TO SIDEWALL SUPPORT ZEE CORRODED BETWEEN BS 887 TO BS 947, RBL 20. R&R FLOOR SUPPORT IAW SRM & DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 62,726 hrs · 36,969 cycles

AFT CARGO COMPARTMENT FLOOR TO SIDEWALL SUPPORT ZEE CORRODED BETWEEN BS 867 TO BS 887, RBL 20. R&R FLOOR SUPPORT IAW SRM & DWG.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 62,726 hrs · 36,969 cycles

AFT CARGO COMPARTMENT INTERCOSTAL WEB CORRODED BETWEEN BS 847 TO BS 867, LBL 17. REPAIRED WEB IAW ER AND EA.

Part: FLOOR PANEL — CORRODED (AFT CARGO) · airframe 62,726 hrs · 36,969 cycles

***CORROSION*** AFT CARGO COMPARTMENT: FLOOR PANEL SPLICE HAS CORROSION; BS 727D+4; RBL 20 TO LBL 20; WL 156. / FLOOR PANEL SPLICE AT BS 727D+4 RBL 20 TO LBL 20; WL 156 HAS NO ALLOWABLE DAMAGE LIMITS IN SRM AND IS REPAIRABLE BY REPLACEMENT IAW SRM 51-10-02 NO SPLICE WAS REPLACED ON CARD JPANEL-141-CLOSE

Part: SHIELD — CORRODED (FUSELAGE) · airframe 62,726 hrs · 36,969 cycles

AFT CARGO COMPARTMENT FLOOR TO SIDEWALL SUPPORT SHIELD CORRODED BETWEEN BS 847 TO BS 867, RBL 20. R&R SHIELD IAW SRM AND DWG.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 62,726 hrs · 36,969 cycles

AFT CARGO COMPARTMENT AFT CARGO DOOR LOWER MAIN SILL INTERCOSTAL CORRODED BETWEEN BS 767 TO BS 787, RBL 20. R&R INTERCOSTAL PER SRM AND DWG.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 62,726 hrs · 36,969 cycles

AFT CARGO COMPARTMENT FLOOR TRACK CORRODED AT BS 727A, LBL 17. R&R FLOOR TRACK IAW SRM AND DWG.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 62,726 hrs · 36,969 cycles

AFT CARGO COMPARTMENT STRINGER CLIP CORRODED AT BS 727C, STR 27L. R&R CLIP PER SRM AND DWG.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 62,726 hrs · 36,969 cycles

AFT CARGO COMPARTMENT FLOOR TRACK CORRODED BETWEEN BS 887 TO BS 947, RBL 13. R&R TRACK IAW SRM AND DWG.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 62,726 hrs · 36,969 cycles

AFT CARGO COMPARTMENT AFT CARGO DOOR LOWER AUX SILL WEB CORRODED BETWEEN BS 767 TO BS 787, RBL 6. R&R WEB IAW SRM AND DWG.

Part: SPLICE — CORRODED (AFT CARGO) · airframe 62,726 hrs · 36,969 cycles

***CORROSION*** AFT CARGO COMPARTMENT: FLOOR PANEL SPLICE HAS CORROSION; BS 773; RBL 20 TO LBL 20; WL 158. / FLOOR PANEL SPLICE AT BS 773 RBL 20 TO LBL 20 WL 158 HAS NO ALLOWABLE DAMAGE LIMITS IN SRM AND IS REPAIRABLE BY REPLACEMENT IAW SRM 51-10-02. NEW SPLICE WAS REPLACED ON CARD JPANEL-141-CLOSE

Part: THRESHOLD WEB — CORRODED (AFT CARGO BAY) · airframe 62,726 hrs · 36,969 cycles

***CORROSION*** AFT CARGO COMPARTMENT: AFT CARGO DOOR THRESHOLD WEB HAS CORROSION; BS 794 TO BS 847; RBL 21 TO RBL 29; WL 165. / REMOVED AND REPLACED THRESHOLD WEB ACB CARGO DOOR AT BS 794 BS 874 RBL 21 TO RBL 29 WL 165 IAW SRM 51-40-02-0G-0 AND DWG 146A8340 59205U 05JAN19

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 62,726 hrs · 36,969 cycles

AFT CARGO COMPARTMENT FLOOR TO SIDEWALL SUPPORT ZEE CORRODED BETWEEN BS 727+3 TO BS 767, RBL 20. R&R SUPPORT IAW SRM AND DWG.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 62,726 hrs · 36,969 cycles

AFT CARGO COMPARTMENT STRINGER CLIP CORRODED AT BS 807, STR 27L. R&R STRINGER CLIP PER SRM AND DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 62,726 hrs · 36,969 cycles

AFT CARGO COMPARTMENT FLOOR TO SIDEWALL SUPPORT ZEE CORRODED BETWEEN BS 727+3 TO BS 847, LBL 20. REPAIRED SUPPORT PER SRM & DWG.

Part: SKIN — CORRODED (TAIL) · airframe 62,726 hrs · 36,969 cycles

***CORROSION*** WIDESPREAD SURFACE CORROSION ON EXTERNAL FUSELAGE SKIN UNDER DORSAL FIN STA 847 TO STA 888; STR2L-2R / EXTERNAL FUSELAGE SKIN UNDER DORSAL FIN STA 847 TO STA. 888 WAS REPAIRED IAW ATS ER# 18-06261 REV IR AND EA # 1-753-33974 REV IR

Part: SKIN — CORRODED (FUSELAGE) · airframe 62,726 hrs · 36,969 cycles

EXTERNAL FUSELAGE SKIN UNDER DORSAL FIN CORRODED BETWEEN BS 888 TO BS 1007, BETWEEN STR 2L TO STR 2R. REPAIRED SKIN IAW ER & EA.

Part: FLOOR PANEL — BROKEN (FWD CABIN) · airframe 62,726 hrs · 36,969 cycles

FWD CABIN FLOOR PANEL 221BF AFT O/B CORNER (TANG) BROKEN / FWD CABIN FLOOR PANEL 221BF WITH BROKEN (TANG) AT AFT O/B CORNER WAS REPLACED WITH A SERVICEABLE FLOOR PANEL DUE TO AMOUNT OF ALL DAMAGE PER SRM 51-10-02-0G-0 PARA 9.A.(1)

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 62,726 hrs · 36,969 cycles

FLOORBEAM CORRODED AT BS 986, BETWEEN RBL 45 TO LBL 45. REPAIRED FLOORBEAM IAW ER AND EA.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 62,726 hrs · 36,969 cycles

RT MOP SILL CORRODED AT BS 967, RBL 50. R&R MOP SILL PER SRM AND DWG.

Part: STRAP — CORRODED (FUSELAGE) · airframe 62,726 hrs · 36,969 cycles

AFT CABIN TENSION STRAP CORRODED AT BS 1016, LBL 3. R&R TENSION STRAP PER DWG AND SRM.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 62,726 hrs · 36,969 cycles

LT MOP SILL CORRODED BETWEEN BS 907 TO BS 986, LBL 45. R&R MOP SILL PER SRM AND DWG.

Part: WEB — CORRODED (FUSELAGE) · airframe 62,726 hrs · 36,969 cycles

AFT CABIN WEB CORRODED AT BS 986, LBL 35. R&R WEB PER DWG AND SRM.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 62,726 hrs · 36,969 cycles

INTERCOSTAL CORRODED AT BS 947+4, RBL44. R&R INTERCOSTAL PER SRM AND DWG.

Part: FLOOR PANEL — BROKEN (FWD CABIN) · airframe 62,726 hrs · 36,969 cycles

FWD CABIN FLOOR PANEL 221GF FWD O/B CORNER (TANG) BROKEN / FWD CABIN FLOOR PANEL 221GF WITH FWD O/B CORNER (TANG) BROKEN REPLACED WITH A SERVICEABLE FLOOR PANEL DUE TO AMOUNT OF ALL DAMAGE IAW SRM 51-10-02-0G-0 PARA 9.A.(11) 57543U 12DEC18

Part: FLOOR PANEL — BROKEN (AFT CABIN) · airframe 62,726 hrs · 36,969 cycles

AFT CABIN FLOOR PANEL 242XF BROKEN / DUE TO THE AMOUNT OF ALL DAMAGE; AFT CABIN FLOOR PANEL 242XF WAS REPLACED IAW SRM 51-10-02-0G-0 PARA 9A. 59400U 10DEC18

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 62,726 hrs · 36,969 cycles

FUSELAGE INTERCOSTAL CRACKED AT STA 277 TO STA 294.5, BL 0. R&R INTERCOSTAL PER SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 62,726 hrs · 36,969 cycles

THRESHOLD SUPPORT CORRODED BETWEEN BS 294.5+3 TO BS 328, RBL 57. REPAIRED SUPPORT IAW SRM AND DWG.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 62,726 hrs · 36,969 cycles

R1 DOOR MOPSILL CORRODED BETWEEN BS 312 TO BS 328+5, RBL 56. REPAIRED MOPSILL IAW SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 62,726 hrs · 36,969 cycles

FLOOR SUPPORT CORRODED BETWEEN BS 328 TO BS 344, LBL 12. REPAIRED SUPPORT IAW SRM.

Part: SUPPORT WEB — CRACKED (LT WING) · airframe 62,726 hrs · 36,969 cycles

LT WING UPPER T/E PANEL ABOVE PYLON AFT TIP LOWER BULB SEAL SUPPORT WEB IS CRACKED ON FWD FLANGE / REMOVED AND REPLACED LT WING UPPER T/E PANEL ABOVE PYLON AFT TIP LOWER BULB SEAL SUPPORT WEB P/N 115A2982-9 IAW. SRM 51-40-02 AND AIPC 57-50-00-25 88920U 16DEC18

Part: SUPPORT BEAM — CRACKED (RT WING) · airframe 62,726 hrs · 36,969 cycles

RT WING LOWER TRAILING EDGE SUPPORT BEAM FOR PANEL 661AB IS CRACKED / REMOVED AND REPLACED RT WING LOWER TRAILING EDGE SUPPORT BEAM FOR PANEL 661AB P/N . 115A3758-10 IAW SRM 51-40-02 AND AIPC 57-50-00-18. 88920U 26DEC18

Part: FLAP — DELAMINATED (RT WING) · airframe 62,726 hrs · 36,969 cycles

RT WING OUTBOARD AFT FLAP DELAMINATED ON LOWER AFT CORNER. REPAIRED AFT FLAP IAW WO.

Part: FLAP — DELAMINATED (LT WING) · airframe 62,726 hrs · 36,969 cycles

LT WING OUTBOARD AFT FLAP DELAMINATED ON LOWER AFT CORNER. REPAIRED AFT FLAP PER WO.

Part: BEAM — CRACKED (FWD SERVICE DOOR) · airframe 62,726 hrs · 36,969 cycles

DURING COMPLETION OF CCN:14079 FOUND FORWARD SERVICE DOOR LOWER BEAM TO BE CRACKED IN THE RADIUS ON THE INBOARD SIDE COMMON TO THE FORWARD MOST ATTACH POINT FOR THE DOOR HANDLE BOX ASSY. / REMOVED & INSTALLED SF DOOR LINER PER AMM 52-41-31-000-802 & AMM 52-41-31-400-802. DOOR REMOVED & INSTALLED ON CUSTOMER CARD 14079. ADJUSTED SF DOOR PER AMM 52-41-00-820-801. PERFORMED SF DOOR SYSTEM TEST PER AMM 52-41-00-700-801. SYSTEM TEST GOOD! VERIFIED SF DOOR INDICATION SENSOR ADJUSTMENT IS CORRECT PER AMM 52-71-11-820-801. (POS:SF;TAG NO.:499373;P/N OFF:141A6516-14;S/N OFF/ON:000789;P/N ON:141A6516-14M)

Part: VAPOR BARRIER — CRACKED (LT M,LG WW) · airframe 62,726 hrs · 36,969 cycles

LOWER COMPOSITE VAPOR BARRIER CRACKED AT BS 663, LBL 11. REPAIRED BARRIER IAW SRM.

Part: PRESSURE DECK — CRACKED (RT MLG WW) · airframe 62,726 hrs · 36,969 cycles

HORIZONTAL PRESSURE DECK WEB CRACKED AT BS 663, BETWEEN RBL 41 TO RBL 42. REPAIRED WEB PER SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 62,726 hrs · 36,969 cycles

RT WING NR 7 SLAT LOWER SURFACE CRACKED AROUND FASTENER AT ACTUATOR ATTACH POINT. REPAIRED NR 7 SLAT SKIN IAW SRM.

Part: STRAP — BROKEN (FLASHLIGHT) · airframe 62,629 hrs · 36,910 cycles

L2 DOOR FLASHLIGHT SAFETY STRAP BROKEN. R&R SECURITY STRAP PER MM & SIP.

Part: VAPOR BARRIER — CRACKED (RT MLG WW) · airframe 62,522 hrs · 36,846 cycles

RT WHEEL WELL VAPOR BARRIER WEB CRACKED AT 12 RBL. REPAIRED WEB PER SRM.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 60,944 hrs · 35,853 cycles

LT WING NR 3 SLAT UPPER SURFACE INBOARD CORNER DELAMINATED AT INBOARD LEADING EDGE. R&R NR 3 SLAT PER AMM.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 59,770 hrs · 35,118 cycles

RT HORIZONTAL STABILIZER RIB CRACKED AT STA 120.30, AFT OF FORWARD SPAR. REPAIRED RIB PER SRM.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 59,094 hrs · 34,683 cycles

STIFFENER EXTENSION CRACKED; STA 663; RBL 25.00. / REMOVED AND REPLACED PER 51-40-02 SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 59,094 hrs · 34,683 cycles

UPPER BEAM OF INTERCOSTAL BETWEEN STAS 344-360 CRACKED. (U22) / REMOVED AND REPLACED INTERCOSTAL BETWEEN STA 344-360 REF SRM 51-40-02.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 59,094 hrs · 34,683 cycles

CRACK NOTED IN THE UPPER BEAM OF INTERCOSTAL BETWEEN STAS 344-360; BL0. (U23) / REMOVED AND REPLACED INTERCOSTAL BETWEEN STA 344-360 REF SRM 51-40-02.

Part: SCUFF PLATE — CRACKED (FWD CARGO BAY) · airframe 59,094 hrs · 34,683 cycles

EXTENSIVE WEAR NOTED AT FWD STOP PIN RESTING POINT ON THE SCUFF PLATE OF FWD CARGO DOOR; RESULTING IN A CRACK. / REMOVED AND REPLACED PER AMM.53-11-02

Part: WINDOW — ARCED (COCKPIT) · airframe 58,847 hrs · 34,527 cycles

L2 COCKPIT WINDOW ELECTRICAL ARCED. R&R L2 WINDOW PR MT.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 58,143 hrs · 34,104 cycles

RIGHT OVERWING UPPER EMERGENCY EXIT LENS LOOSE. SECURED THE LENS IAW SIP.

Part: SHEAR TIE — DAMAGED (FUSELAGE) · airframe 57,510 hrs · 33,730 cycles

SHEAR TIE DAMAGED AT BS 380, BETWEEN STR 16L TO STR 17L. R&R SHEAR TIE PER ER & EA.

Part: ANGLE — CRACKED (LT MLG WW) · airframe 56,216 hrs · 32,951 cycles

AFT BULKHEAD UPPER CHORD ANGLE CRACKED AT BS 663, LBL 24. REPAIRED ANGLE IAW EA.

Part: STRINGER — CRACKED (LT WING) · airframe 56,216 hrs · 32,951 cycles

LT WING INBOARD UPPER LEADING EDGE STRINGER CRACKED. R&R STRINGER IAW DWG AND SRM.

Part: BULKHEAD — CRACKED (RT MLG WW) · airframe 56,216 hrs · 32,951 cycles

RT MAIN WHEEL WELL FORWARD MOISTURE BARRIER BULKHEAD CRACKED AT BS 663.75, RBL 16. REPAIRED BULKHEAD IAW EA.

Part: LENS — CRACKED (CABIN) · airframe 56,216 hrs · 32,951 cycles

RT WING EMERGENCY EXIT SIDEWALL LIGHT LENS CRACKED. R&R LENS IAW AMM.

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 56,216 hrs · 32,951 cycles

MAIN LANDING GEAR FORWARD PRESSURE BULKHEAD WEB CRACKED AT BS 663, RBL 35. REPAIRED WEB IAW SRM.

Part: BULKHEAD — CRACKED (LT MLG WW) · airframe 56,216 hrs · 32,951 cycles

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

Part: SKIN — CRACKED (LE SLAT) · airframe 56,216 hrs · 32,951 cycles

RT WING NR 8 SLAT LOWER NOSE SKIN CRACKED. REPAIRED SLAT SKIN IAW SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 56,216 hrs · 32,951 cycles

LT WING NR 4 SLAT LOWER NOSE SKIN AT ACTUATOR RIBS, CRACKED AT FASTENER HOLES. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 56,216 hrs · 32,951 cycles

RT WING NR 6 SLAT LOWER NOSE SKIN AT ACTUATOR RIBS CRACKED. REPAIRED SKIN IAW SRM.

Part: COVER — MISSING (CABIN) · airframe 53,986 hrs · 31,625 cycles

R1 DOOR EXIT LIGHT COVER MISSING. R & R LIGHT ASSEMBLY IAW MM.

Part: ACTUATOR — DEFECTIVE (FUEL SYSTEM) · airframe 53,550 hrs · 31,377 cycles

DIVERSION, CROSS FEED SELECTOR VLV WOULD NOT ACTUATE. LIGHT REMAINED OUT, FOUND CROSS FEED VLV CB POPPED. R & R CROSS FEED ACTUATOR IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 52,373 hrs · 30,714 cycles

RIGHT OVERWING FWD LOWER EMER EXIT LIGHT BULB AT FWD LAVATORY INOPERATIVE. R & R BULB IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 52,373 hrs · 30,714 cycles

FORWARD EMER EXIT LIGHT BULB AT FWD LAVATORY INOPERATIVE. R & R BULB IAW AMM.

Part: RETAINER — LOOSE (R1 DOOR) · airframe 51,993 hrs · 30,479 cycles

R1 DOOR EMER EVAC SLIDE GIRT BRACKET RETAINER LOOSE. SECURED RETAINER IAW SIP.

Part: RETAINER — LOOSE (L1 DOOR) · airframe 49,455 hrs · 29,008 cycles

L1 DOOR EMER EVAC SLIDE GIRT BAR RETAINER LOOSE. SECURED RETAINER IAW AMM.

Part: LIGHT — LOOSE (CABIN) · airframe 48,883 hrs · 28,683 cycles

EMERGENCY EXIT AT OVERWING ROW OVERHEAD LIGHT LOOSE. R & R LIGHT IAW MM.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 47,756 hrs · 28,051 cycles

FLIGHT DECK RT NR 1 WINDOW FRAME OTBD UPPER CORNER EDGE CUT OUT CRACKED. REPAIRED FRAME IAW ACO.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 47,756 hrs · 28,051 cycles

RIGHT NR 3 WINDOW FRAME CRACKED AT 2ND & 3RD HOLE FROM THE BOTTOM. REPAIRED FRAME IAW ACO.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 47,756 hrs · 28,051 cycles

LEFT NR 3 WINDOW FRAME CRACKED AT 2ND & 3RD HOLE FROM THE BOTTOM. REPAIRED FRAME IAW ACO.

Part: HMU — FAULTY (NR 2 ENGINE) · airframe 46,745 hrs · 27,471 cycles

NR 2 ENG THRUST SURGE DURING CLIMB. R & R NR 2 ENG HYDRO MECHANICAL UNIT IAW WORK INSTRUCTIONS.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 46,567 hrs · 27,354 cycles

LT HORIZONTAL STABILIZER LOWER SKIN CRACKED FWD OF REAR SPAR 3.75 INCHES OTBD OF STAB STATION 120.30. REPAIRED SKIN IAW SRM & EA.

Part: COVER — MISSING (CABIN) · airframe 46,276 hrs · 27,179 cycles

RT EMERGENCY EXIT DOOR OVERWING COVER MISSING. INSTALLED OVERWING EMERGENCY EXIT LIGHT COVER IAW MM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 45,195 hrs · 26,523 cycles

R1 DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT, DID NOT DEPLOY, STILL OPERATIONAL. REINSTALLED SLIDE IAW MT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 43,382 hrs · 25,432 cycles

LEFT OVERWING EXIT EXTERIOR EMERGENCY EXIT LIGHT INOP. REMOVED & REPLACED LEFT OVERWING EXIT EXTERIOR LIGHT BULB AS PER AMM 33-51-04-960-801. PERFORMED GOOD OP CHECK AS PER AMM 33-51-04-960-801. 89347U, 09FEB2013

Part: SCUFF PLATE — CRACKED (FUSELAGE) · airframe 43,382 hrs · 25,432 cycles

ACB, DOOR CUTOUT, AFT CORNER SCUFF PLATE CRACKED. ACB AFT CORNER SCUFF PLATE REPAIRED ON EA 1-A53-2076.

Part: CONNECTOR — BROKEN (CABIN) · airframe 43,382 hrs · 25,432 cycles

LEFT OWE LIGHT HAS BROKEN CONNECTOR. REMOVED AND REPLACED CONNECTOR AND PERFORMED GOOD OP CHECK AS PER SWPM 20-42-01 AND AMM 33-51-00-710-801.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 43,382 hrs · 25,432 cycles

BS 727B RBL 24.75 SPLICE STRAP OPEN FASTENER HOLES HAVE CRACKS AT BOTH FWD AND AFT INBD HOLES AND FWD OTBD HOLE (AS MARKED). REPAIRED BS 727B RBL 24.75 SPLICE STRAP OPEN FASTENER HOLES (BOTH FWD AND AFT INBOARD HOLES AND FWD OUTBOARD HOLE AS MARKED.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 43,382 hrs · 25,432 cycles

BS 727B LBL 24.75 SPLICE STRAP OPEN FASTENER HOLES HAVE CRACKS AT FWD INBD HOLE AND AFT OTBD HOLE (AS MARKED). REPAIRED SPLICE AT BS 727B, LBL 24.75 IAW EA 1-753-21686 AND ATS ER 13-01344.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 43,382 hrs · 25,432 cycles

BS 727B LBL 45.5 SPLICE STRAP OPEN FASTENER HOLES HAVE CRACKS AT BOTH FWD AND AFT OTBD HOLES AND AFT INBD HOLE (AS MARKED). REPAIRED BS 727B LBL 45.5 SPLICE STRAP OPEN FASTENER HOLES (BOTH FWD AND AFT OUTBOARD HOLES AND AFT INBOARD HOLES AS MARKED.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 43,382 hrs · 25,432 cycles

STRINGER CLIP CRACKED AT FASTENER HOLE BS 360 AT STR 8 RT. REMOVED CRACKED STRINGER CLIP BS 360 AT STR 8 RT IAW SRM 51-40-02 89273U 24JAN13. INSTALLED NEW STRINGER CLIP BS 360 AT STR 8 RT IAW SRM 51-40-02-0G-0.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 43,382 hrs · 25,432 cycles

FLOOR PANEL 242WF DELAMINATED ON CORNER (MARKED). REPAIRED DELAMINATION ON CORNER OF FLOOR PANEL 242WF IAW SRM 53-00-50-2R-9 AND SRM 53-00-50-2R-0. 969U 24JAN13. 6042C 24JAN13.

Part: FLOOR PANEL — PUNCTURED (FUSELAGE) · airframe 43,382 hrs · 25,432 cycles

FLOOR PANEL 241UF HAS 2 EA PUNCTURES (MARKED) AND MULTIPLE DENTS ON UPPER SURFACE. FLOOR PANEL 241UF WAS FOUND TO HAVE EXCESSIVE DAMAGE WHICH REQUIRED REPLACEMENT OF PART PER SRM 51-10-02-0G-0 PAR.9.A(1). FABRICATED FLOOR PANEL 241UF PER BOEING

Part: FLOOR PANEL — PUNCTURED (CABIN) · airframe 43,382 hrs · 25,432 cycles

PASSENGER CABIN FLOOR PANEL 231YF UPPER SURFACE PUNCTURED. PASSENGER CABIN FLOOR PANEL 231YF UPPER SURFACE. PUNCTURE WAS REPAIRED IAW SRM 53-00-50-2R-2. REF EA 1-A53-11895.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 43,382 hrs · 25,432 cycles

FLOOR PANEL 231UF AFT EDGE OF UPPER SURFACE IS DELAMINATED. (MARKED) FLOOR PANEL 231UF WAS FOUND TO HAVE EXCESSIVE DAMAGE WHICH REQUIRED REPLACEMENT OF PART PER SRM 51-10-02-0G-0 PAR 9.A.(1). FABRICATED FLOOR PANEL 231UF PER BOEING DWG 143A5.

Part: FLOOR PANEL — PUNCTURED (CABIN) · airframe 43,382 hrs · 25,432 cycles

FLOOR PANEL 242AF HAS PUNCTURE IN UPPER SURFACE (MARKED). FLOOR PANEL 242AF PUNCTURE IN UPPER SURFACE WAS REPAIRED IAW SRM 53-00-50-2R-0 REF EA 1-A53-11895.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,382 hrs · 25,432 cycles

FRAME CRACKED AT RAIL SUPPORT FITTING, BS 480, STR 8 LT. REPAIRED CRACKED FRAME AT RAIL SUPPORT FITTING, BS 480, STR 8 LT IAW EA 1-A53-121114.

Part: SEAL — CRACKED (LT HORIZ STAB) · airframe 43,382 hrs · 25,432 cycles

LEFT HORIZONTAL STAB LOWER SLIDE SEAL IS CRACKED AT UPPER END. REMOVED AND REPLACED LEFT HORIZ STAB LOWER SLIDE SEAL IAW MM 53-31-31-000-801 AND MM 53-31-31-400-801 STEP 3.C.(1)-(25),3.D.(1)-(3)

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,382 hrs · 25,432 cycles

FRAME CRACKED AT RAIL SUPPORT FITTING, BS 400, STR 8 RIGHT. REPAIRED CRACKS FRAME AT BS 411 STR 8 RT IAW EA 1-A53-12114 R2.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,382 hrs · 25,432 cycles

FRAME CRACKED AT RAIL SUPPORT FITTING, BS 867, STR 8 RIGHT. REPAIRED CRACKS FRAME AT BS 867 STR 8RT IAW EA 1-A53-12114.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 43,382 hrs · 25,432 cycles

LEFT HORIZONTAL STAB LOWER SKIN CRACKED, AT STAB STA 92.7 RIB CHORD O/B HOLES, 8" AFT OF DRAIN HOLE. REPAIRED CRACK AT LEFT HORIZONTAL STAB LOWER SKIN STAB STA 92.7 8" AFT OF DRAIN HOLE PER SRM 55-10-01-2R-11 REPAIR 11.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,382 hrs · 25,432 cycles

FRAME CRACKED AT RAIL SUPPORT FITTING, BS 400, STR 8 LEFT. REPAIRED FRAME AT BS 400 STR 8 LT PER EA1-A53-12114R2 7020U 25JAN13

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,382 hrs · 25,432 cycles

FRAME CRACKED AT RAIL SUPPORT FITTING, BS 747, STR 8 RT. REPAIRED FRAME AT BS 747, STR 8 RT PER EA 1-A53-12114 7020U 26JAN13.

Part: SEAL — CRACKED (LT HORIZ STAB) · airframe 43,382 hrs · 25,432 cycles

LEFT HORIZONTAL STAB UPPER SLIDE SEAL IS CRACKED AT LOWER END. REMOVED AND REPLACED LEFT HORIZ STAB UPPER SLIDE SEAL IAW MM 53-31-31-000-801 AND MM 53-31-31-400-801 STEP 3.C(1)-(27), 3.D.(1)-(3).

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,382 hrs · 25,432 cycles

FRAME CRACKED AT RAIL SUPPORT FITTING, BS 787, STR 8 RIGHT. REPAIRED FRAME BS 787 STR 8RT PER EA 1-A53-12114.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,382 hrs · 25,432 cycles

FRAME CRACKED AT RAIL SUPPORT FITTING, BS 360, STR 8 RIGHT. REPAIRED FRAME AT BS 360 STR 8 RT PER ER 13-01279 AND EA 1-753-21590.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 43,382 hrs · 25,432 cycles

LT HORIZONTAL STAB RIB AT STAB STA 92.7 IS CRACKED AT 2ND AND 3RD STIFFENERS. REPAIRED LT/HORIZONTAL STAB RIB AT STAB STA 92.7 PER SRM 55-10-09-2R-4. 4318C, 27JAN13

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,382 hrs · 25,432 cycles

FRAME CRACKED AT RAIL SUPPORT FITTING, BS 867, STR 8 LEFT. REPAIRED FRAME AT BS 867, STR 8 LEFT PER EA 1-A53-12114 7020U 24JAN13.

Part: SPLICE — CORRODED (FUSELAGE) · airframe 43,382 hrs · 25,432 cycles

CORROSION ON ACB FLOOR TRACK SPLICE AT STA 763 RBL13, WL 156. REMOVED AND REPLACED ACB FLOOR TRACK FROM BS 759 TO BS 887 DUE TO CORROSION PER SRM 53-00-53-2R-3 AND EA 1-A53-8210

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 43,382 hrs · 25,432 cycles

CORROSION ON ACB FLOOR TRACK AT STA 795 AND 847 RBL 14, WL 158. CORRODED AFT CARGO BAY FLOOR TRACK FOUND TO BE OUT OF LIMITS AT REPAIR SPLICE 763 DUE TO NO ESTABLISHED LIMITS AT REPAIR SPLICE, ACB FLOOR TRACK TO BE REPLACED FROM SPLICE AT BS

Part: ATTACH ANGLE — CRACKED (RT MLG) · airframe 43,382 hrs · 25,432 cycles

RIGHT REAR SPAR TO MLG BEAM STRUCTURE SUPPORT I/B BEAM (COMMON TO PANEL 651AT AND WING TO BODY FAIRING) FWD ATTACH ANGLE CRACKED. REMOVED AND REPLACED RIGHT REAR SPAR TO MLG BEAM STRUCTURE SUPPORT I/B BEAM FWD ATTACH SUPPORT ANGLE (COMMON TO PANEL 65

Part: WEB — CRACKED (RT WING) · airframe 43,382 hrs · 25,432 cycles

RT WING SUPPORT WEB (ABOVE PANEL 651GB) BULB SEAL I/B RETAINER CRACKED. REMOVED AND REPLACED RT WING SUPPORT WEB JUST ABOVE PANEL 651GB BULB SEAL I/B RETAINER ANGLE PER SRM 51-40-02-0G-0.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 43,382 hrs · 25,432 cycles

CORROSION ON UPPER SIDE OF FLOOR TO SIDEWALL SUPPORT STA 500C+12, RBL 23, WL 156. REMOVED CORROSION 1"X6" AREA, ORIGINAL THICKNESS .040, REMAINING THICKNESS .030, OUT OF LIMITS IAW SRM 53-00-53-1A-2, FABRICATED NEW FLOOR TO SIDEWALL SUPPORT

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 43,382 hrs · 25,432 cycles

CORROSION ON FLOOR TO SIDEWALL SUPPORT STA 867 - 887, RBL 21, WL 157. REMOVED CORROSION 1" X 4" AREA ORIGINAL THICKNESS .040. REMOVED .010 OUT OF LIMITS IAW SRM 53-00-53-1A-2. REMOVED FLOOR TO SIDEWALL SUPPORT IAW SRM 51-40-02. FABRICATED NEW

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 43,382 hrs · 25,432 cycles

CORROSION ON ACB SUB THRESHOLD STA 795-817, RBL 20-28 ,WL 157. REMOVED & REPLACED ACB SUB THRESHOLD WITH NEW DUE TO CORROSION 100% MATERIAL LOSS PER SRM 53-60-15-1A-1 FIG 103, SRM 51-40-02 & DWG 146A8340 BS 794-847 RBL 20-28 WL 157.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 43,382 hrs · 25,432 cycles

CORROSION ON FLOOR TO SIDEWALL SUPPORT STA 727D+5, -787, LBL 21, WL 156. CORROSION ON FLOOR TO SIDEWALL SUPPORT STA 727D + 5 787 LBL 21 WL 156 FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2. REMOVED AND REPLACED FLOOR TO SIDEWALL SUPPORT BS

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 43,382 hrs · 25,432 cycles

CORROSION ON FLOOR TO SIDEWALL SUPPORT STA 727D+5 - 766, RBL 21, WL 156. REMOVED AND REPLACED RIGHT SIDEWALL SUPPORT FROM BS 727 + TO BS 766 PER SRM 51-40-02 AND SRM 53-60-53-01-2

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 43,382 hrs · 25,432 cycles

CORROSION BS 312-328 WL 208 LBL 10 CORROSION ON FLOOR SUPPORT. REMOVED CORROSION ON FLOOR SUPPORT BS 312-328 LBL 10 WL 208 IN AREA OF 1"X.5"X.013. ORIGINAL THICKNESS .080 OUT OF LIMITS PER SRM 53-10-51-1A-1. REMOVED FLOOR SUPPORT AND IN

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 43,382 hrs · 25,432 cycles

BS 294-312 WL 208 RBL 19 INTERCOSTAL CRACKED. REPAIRED DAMAGED INTERCOSTAL STA 294-312, WL 208, RBL 19 IAW SRM 53-10-51-2R-6. 8464U 24JAN13.

Part: ATTACH BRACKET — CORRODED (GIRT BAR) · airframe 43,382 hrs · 25,432 cycles

CORROSION BS 344 WL 208 LBL 56 CORROSION ON GIRT BAR ATTACH BRACKET. REMOVED GIRT BAR ATTACH BRACKET AT BS 344 WL 208 LBL 56 AT AT FWD DOOR PER SRM 51-10-02-0G-0 STEP 9 AND REPLACED WITH NEW ENTRY PER SRM 51-10-02-0G-0 STEP 9.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 43,382 hrs · 25,432 cycles

CORROSION BS 312-328 WL 208 RBL 10 CORROSION ON FLOOR SUPPORT. REMOVED CORROSION ON FLOOR SUPPORT BS 312-328 WL 208 RBL 10 IN AREA OF 1"X.5"X.020" ORIGINAL THICKNESS .080, OUT OF LIMITS PER SRM 53-10-51-1A-1 REMOVED FLOOR SUPPORT AND INS

Part: ATTACH BRACKET — CORRODED (GIRT BAR) · airframe 43,382 hrs · 25,432 cycles

CORROSION BS 312 WL 208 LBL 56 CORROSION ON GIRT BAR ATTACH BRACKET. REMOVED CORRODED GIRT BAR ATTACH BRACKET AT BS 312 WL 208 LBL 56 FORWARD ENTRY DOOR AND INSTALLED NEW GIRT BAR ATTACH BRACKET PER SRM 51-10-02-0G-0 STEP 9.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 43,382 hrs · 25,432 cycles

CORROSION BS 294-312 WL 208 RBL 10 CORROSION ON FLOOR SUPPORT. REMOVED CORROSION ON FLOOR SUPPORT BS 294-312 RBL 10 IN AREA OF 1"X.5"X.018 ORIGINAL THICKNESS .080 OUT OF LIMITS PER SRM 53-10-51-1A. REMOVED FLOOR SUPPORT AND INSTALLED RE

Part: COVER — CRACKED (CABIN) · airframe 43,276 hrs · 25,366 cycles

ESCAPE PATH LIGHTING COVER STRIP AT 1 ABC IS CRACKED. INSTALLED NEW PIECE OF EGRESS TRACK COVER AT ROW 1, IAW AMM.

Part: LIGHT — CRACKED (CABIN) · airframe 43,260 hrs · 25,355 cycles

EEPLS STRIP AT 2 ABC CRACKED. REMOVED AND REPLACED EEPLS PER MM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 43,127 hrs · 25,268 cycles

AFT CARGO COMP RIGHT SIDE FLOOR STRUCTURE, Z ANGLE FROM STA 767 TO 780 HAS NUMEROUS AREAS OF CORROSION AS MARKED. BLENDED CORROSION ORIGINAL THICKNESS .050" REMOVED .010" REMAINING .040" FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2 REMOVED A

Part: SIGN — BROKEN (CABIN) · airframe 42,649 hrs · 24,976 cycles

R2 DOOR EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED SIGN PER MM.

Part: LIGHT — MISSING (CABIN) · airframe 42,618 hrs · 24,957 cycles

EEPLS MISSING. INSTALLED EEPLS PER MM.

Part: COVER — BROKEN (CABIN) · airframe 42,375 hrs · 24,812 cycles

FWD EEPLS COVER BROKEN. REMOVED AND REPLACED COVER PER MM.

Part: WINDOW FRAME — CRACKED (COCKPIT) · airframe 42,296 hrs · 24,759 cycles

L1 WINDOW CRACKED POST AT O/B UPPER CORNER. REPAIRED FRAME IAW EA.

Part: WINDOW FRAME — CRACKED (COCKPIT) · airframe 42,296 hrs · 24,759 cycles

L1 WINDOW FRAME POST CRACKED AT THE OUTBOARD UPPER CORNER. REPAIRED FRAME IAW EA.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 42,294 hrs · 24,758 cycles

LEFT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 129.5. REPAIRED SKIN PER SRM.

Part: BULKHEAD — CRACKED (RT MLG WW) · airframe 42,294 hrs · 24,758 cycles

RIGHT MLG W/W FWD BULKHEAD PANEL WEB CRACKED. REPAIRED WEB PER EA.

Part: SLIDE — UNWANTED DEPLOY (R1 DOOR) · airframe 41,148 hrs · 24,049 cycles

R1 DOOR EMERGENCY EVAC SLIDE INADVERTENTLY DEPLOYED. REMOVED AND REPLACED SLIDE IAW MT.

Part: COVER — BROKEN (CABIN) · airframe 40,020 hrs · 23,392 cycles

AFT CABIN EMERGENCY EXIT LIGHT TRACK COVER AT 10C BROKEN. REMOVED AND REPLACED COVER PER MM. (SUBMITTED AS A SUPPLEMENT, COULDN`T FIND ORIGINAL CONTROL NUMBER.)

Part: BATTERY PACK — FAILED (CABIN) · airframe 40,020 hrs · 23,392 cycles

BATTERY PACK M1670 FAILED TEST. REMOVED AND REPLACED BATTERY PACK PER MM. (SUBMITTED AS A SUPPLEMENT, COULDN`T FIND ORIGINAL CONTROL NUMBER.)

Part: BATTERY PACK — FAILED (CABIN) · airframe 40,020 hrs · 23,392 cycles

EMERGENCY LIGHT BATTERIES FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERY PACKS PER MM. (SUBMITTED AS A SUPPLEMENT, COULDN`T FIND ORIGINAL CONTROL NUMBER.)

Part: COVER — BROKEN (CABIN) · airframe 40,020 hrs · 23,392 cycles

AFT CABIN EMERGENCY EXIT LIGHT TRACK COVER AT 1C BROKEN. REMOVED AND REPLACED COVER PER MM. (SUBMITTED AS A SUPPLEMENT, COULDN`T FIND ORIGINAL CONTROL NUMBER.)

Part: COVER — BROKEN (CABIN) · airframe 40,020 hrs · 23,392 cycles

AFT CABIN EMERGENCY EXIT LIGHT TRACK COVER AT 2C BROKEN. REMOVED AND REPLACED COVER PER MM. (SUBMITTED AS A SUPPLEMENT, COULDN`T FIND ORIGINAL CONTROL NUMBER.)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 37,913 hrs · 22,146 cycles

DURING SCHEDULED MV1 CHECK, FOUND LT OVERHEAD EMERGENCY EXIT LIGHT INOP AT ROW 4. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: STIFFENER — CRACKED (CENTER WING BOX) · airframe 36,399 hrs · 21,280 cycles

DURING SCHEDULED 10Y CHECK, FOUND CENTER WING BOX STIFFENER CRACKED AT BS 540, LBL 15.40. REPAIRED STIFFENER PER EA.

Part: STIFFENER — CRACKED (CENTER WING BOX) · airframe 36,399 hrs · 21,280 cycles

DURING SCHEDULED 10Y CHECK, FOUND CENTER WING BOX STIFFENER CRACKED AT BS 540, LBL 32.40. REPAIRED STIFFENER PER EA.

Part: STIFFENER — CRACKED (CENTER WING BOX) · airframe 36,399 hrs · 21,280 cycles

DURING SCHEDULED 10Y CHECK, FOUND CENTER WING BOX STIFFENER CRACKED AT BS 540, RBL 32.40. REPAIRED STIFFENER PER EA.

Part: STIFFENER — CRACKED (CENTER WING BOX) · airframe 36,399 hrs · 21,280 cycles

DURING SCHEDULED 10Y CHECK, FOUND CENTER WING BOX STIFFENER CRACKED AT BS 540, RBL 15.04. REPAIRED STIFFENER PER EA.

Part: STIFFENER — CRACKED (CENTER WING BOX) · airframe 36,399 hrs · 21,280 cycles

DURING SCHEDULED 10Y CHECK, FOUND CENTER WING BOX STIFFENER CRACKED AT BS 540, RBL 54.60. REPAIRED STIFFENER PER EA.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 36,399 hrs · 21,280 cycles

DURING SCHEDULED 10Y CHECK, FOUND LT WING O/B AFT FLAP I/B TRAILING EDGE SKIN DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 36,399 hrs · 21,280 cycles

DURING SCHEDULED 10Y CHECK, FOUND CENTER WEB ANGLE CORRODED AT BS 270, BL 0. REPAIRED ANGLE PER EA.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 36,399 hrs · 21,280 cycles

DURING SCHEDULED 10Y CHECK, FOUND CENTER WEB ANGLE CORRODED AT BS 259, BL 0. REPAIRED ANGLE PER EA.

Part: STIFFENER — CRACKED (CENTER WING BOX) · airframe 36,399 hrs · 21,280 cycles

DURING SCHEDULED 10Y CHECK, FOUND CENTER WING BOX STIFFENER CRACKED AT BS 540, RBL 6.14. REPAIRED STIFFENER PER EA.

Part: STIFFENER — CRACKED (CENTER WING BOX) · airframe 36,399 hrs · 21,280 cycles

DURING SCHEDULED 10Y CHECK, FOUND CENTER WING BOX STIFFENER CRACKED AT BS 540, LBL 54.60. REPAIRED STIFFENER PER EA.

Part: STIFFENER — CRACKED (CENTER WING BOX) · airframe 36,399 hrs · 21,280 cycles

DURING SCHEDULED 10Y CHECK, FOUND CENTER WING BOX STIFFENER CRACKED AT BS 540, LBL 6.14. REPAIRED STIFFENER PER EA.

Part: MODULE — BROKEN (CABIN) · airframe 35,976 hrs · 21,028 cycles

DURING SCHEDULED MV1 CHECK, FOUND AFT EMERGENCY EXIT LIGHT COVER PANEL MODULE BROKEN. REMOVED AND REPLACED MODULE PER MM.

Part: LENS — MISSING (CABIN) · airframe 35,599 hrs · 20,813 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT EMERGENCY EXIT LIGHT LENS MISSING AT ROW 2. INSTALLED LENS PER MM.

Part: COVER — CRACKED (CABIN) · airframe 35,341 hrs · 20,657 cycles

DURING SCHEDULED HC2 CHECK, FOUND EEPLS COVER CRACKED BETWEEN ROW 13 TO ROW 22. REMOVED AND REPLACED COVER PER MM.

Part: COVER — CRACKED (CABIN) · airframe 35,341 hrs · 20,657 cycles

DURING SCHEDULED HC2 CHECK, FOUND EEPLS COVER CRACKED BETWEEN ROW 1 TO ROW 12. REMOVED AND REPLACED COVER PER MM.

Part: FITTING — CORRODED (LT MLG TRUNNION) · airframe 34,858 hrs · 20,349 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT MLG TRUNNION FITTING LUG FACES CORRODED. REPAIRED FITTING PER EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 34,023 hrs · 19,827 cycles

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

Part: BRACKET — LOOSE (GIRT BAR) · airframe 33,291 hrs · 19,398 cycles

DURING SCHEDULED SPV CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE GIRT BAR BRACKETS LOOSE. SECURED BRACKETS PER MM.

Part: BRACKET — LOOSE (GIRT BAR) · airframe 33,291 hrs · 19,398 cycles

DURING SCHEDULED SPV CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE GIRT BAR BRACKETS LOOSE. SECURED BRACKETS PER MM.

Part: LENS — MISSING (CABIN) · airframe 31,990 hrs · 18,575 cycles

DURING SCHEDULED CV CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHTS LENS MISSING. REMOVED AND REPLACED LENS ASSY PER MM.

Part: LENS — MISSING (CABIN) · airframe 31,764 hrs · 18,432 cycles

FWD EEPLS LENS MISSING. INSTALLED LENS PER MM.

Part: CABLE — LOOSE (L1 DOOR) · airframe 31,652 hrs · 18,357 cycles

L1 DOOR EVACUATION SLIDE CASE RETAINING CABLE LOOSE. SECURED CABLE ASSY PER MM.

Part: LIGHT — BROKEN (CABIN) · airframe 31,523 hrs · 18,275 cycles

R2 DOOR EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 31,355 hrs · 18,170 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 29,872 hrs · 17,303 cycles

DURING SCHEDULED 8Y CHECK, FOUND FRAME CRACKED AT BS 294, STR 17R. REPAIRED FRAME PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 29,872 hrs · 17,303 cycles

DURING SCHEDULED 8Y CHECK, FOUND RT CREASE BEAM CORRODED BETWEEN BS 947 TO BS 986. REMOVED AND REPLACED BEAM PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 29,872 hrs · 17,303 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOOR FRAME CORRODED AT BS 986, BETWEEN LBL 18 TO LBL 43. REPAIRED T-CAP PER SWA EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 29,872 hrs · 17,303 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM T-CAP CORRODED AT BS 986, BETWEEN RBL 6 TO LBL 6. REMOVED AND REPLACED T-CAP PER SRM.

Part: WIRE — LOOSE (CABIN) · airframe 29,901 hrs · 17,323 cycles

DURING SCHEDULED 8Y CHECK, FOUND FWD EEPLS LIGHT INOP. SECURED WIRE PER MM.

Part: FITTING — CORRODED (GIRT BAR) · airframe 29,871 hrs · 17,303 cycles

DURING SCHEDULED 8Y CHECK, FOUND L1 DOOR EVAC SLIDE GIRT BAR FWD FITTING CORRODED. REMOVED AND REPLACED FITTING ASSY PER MM.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 28,732 hrs · 16,614 cycles

DURING SCHEDULED HC1 CHECK, FOUND LT HORIZONTAL STABILIZER IN SPAR SKIN CRACKED AT BS 101, AFT OF FRONT SPAR. REPAIRED SKIN PER SRM.

Part: GASPER FAN — FAULTY (E&E BAY) · airframe 27,534 hrs · 15,888 cycles

AT FL 360 CREW REPORTED AN ELECTRICAL ODOR IN CABIN. TURNED OFF GASPER FAN ODOR DISSIPATED. REMOVED AND REPLACED GASPER FAN PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,003 hrs · 14,972 cycles

DURING SCHEDULED MV1 CHECK, FOUND EEPLS INOP AT ROW 1 ABC. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 25,226 hrs · 14,519 cycles

DURING SCHEDULED MV2 CHECK, FOUND EEPLS INOP AT ROW 5 ABC INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 24,886 hrs · 14,325 cycles

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

Part: ENGINE — FAILED (LEFT) · airframe 24,842 hrs · 14,297 cycles

INFLIGHT SHUTDOWN/DECLARED EMERGENCY. CLIMBING THROUGH FL 1000 AGL, NR 1 ENGINE FAILED. LOUD BANG, RPM ROLLED BACK, EGT ROSE. REMOVED AND REPLACED NR 1 ENGINE PER MT.

Part: BATTERY — FAILED (CABIN) · airframe 23,775 hrs · 13,675 cycles

DURING SCHEDULED HC1 CHECK, EMERGENCY EXIT BATTERY PACKS FAILED LONG TEST. R&R BATTERY PACKS PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 23,421 hrs · 13,464 cycles

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

Part: COVER — CRACKED (EMERGENCY LIGHT) · airframe 21,297 hrs · 12,216 cycles

DURING SCHEDULED HC2 CHECK, FOUND EEPLS COVER CRACKED AT ROW 1 ABC. REMOVED AND REPLACED EEPLS COVER PER MM.

Part: COVER — CRACKED (EMERGENCY LIGHT) · airframe 21,297 hrs · 12,216 cycles

DURING SCHEDULED HC2 CHECK, FOUND EEPLS COVER CRACKED AT ROW 20 ABC. REMOVED AND REPLACED EEPLS COVER PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 21,269 hrs · 12,199 cycles

FWD CABIN EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: COVER — MISSING (CABIN) · airframe 21,150 hrs · 12,139 cycles

EEPLS COVER MISSING AT ROW 11 ABC. INSTALLED COVER PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 20,957 hrs · 12,025 cycles

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

Part: SIGN — BROKEN (CABIN) · airframe 17,682 hrs · 10,177 cycles

R1 DOOR LOWER EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED SIGN PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 17,502 hrs · 10,078 cycles

EEPLS TRACK LOOSE AT FWD END. REMOVED AND REPLACED EEPLS SECTION PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 16,756 hrs · 9,665 cycles

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

Part: SLIDE — DISLODGED (L2 DOOR) · airframe 16,438 hrs · 9,474 cycles

L2 DOOR SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM.

Part: LIGHT — LOOSE (ROW 1 ABC) · airframe 13,921 hrs · 8,028 cycles

DURING SCHEDULED RON, FOUND EEPLS AT ROW 1 ABC, INOP. RECONNECTED LIGHT ASSEMBLY PER MM.

Part: COVER — MISSING (ROW 1 ABC) · airframe 13,921 hrs · 8,028 cycles

DURING SCHEDULED RON, FOUND EEPLS COVER AT ROW 1 ABC, MISSING. REMOVED AND REPLACED EPPLS COVER PER MM.

Part: COVER — CRACKED (ROW 2 ABC) · airframe 11,647 hrs · 6,773 cycles

DURING SCHEDULED HC2 CHECK, FOUND EEPLS COVER AT ROW 2 ABC, CRACKED. REMOVED AND REPLACED EEPLS COVER PER MM.

Part: SLIDE — WRONG PART (L2 DOOR) · airframe 11,316 hrs · 6,590 cycles

L2 DOOR EVACUATION SLIDE WOULD NOT ARM. FOUND INCORRECT SLIDE INSTALLED DURING MV2 CK ON THE PREVIOUS NIGHT TO THIS FLIGHT. REMOVED AND REPLACED SLIDE ASSY PER MM.

Part: LIGHT — LOOSE (FWD CABIN) · airframe 9,088 hrs · 5,329 cycles

EEPLS LOOSE IN FWD CABIN. SECURED EEPLS PER MM.

Part: SLIDE — DISLODGED (FWD ENTRY DOOR) · airframe 9,088 hrs · 5,329 cycles

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

Part: LIGHT — LOOSE (CABIN) · airframe 9,035 hrs · 5,302 cycles

EEPLS COMING LOOSE IN CABIN. SECURED EEPLS PER MM.

Part: COVER — EXPOSED (CABIN) · airframe 6,263 hrs · 3,761 cycles

DURING SCHEDULED PM CHECK, FOUND EEPLS WIRES EXPOSED AT ROW 11. REMOVED AND REPLACED EEPLS COVER PER MM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 4,684 hrs · 2,787 cycles

DURING SCHEDULED PM CHECK, FOUND FWD UPPER EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT BATTERY PER MM.

Part: COVER — CRACKED (CABIN) · airframe 4,684 hrs · 2,787 cycles

DURING SCHEDULED C4 CHECK, FOUND EEPLS COVER CRACKED AT ROW NR 1. REMOVED AND REPLACED COVER PER MM.

Part: SLIDE — OUT OF ADJUST (FWD SVC DOOR) · airframe 4,684 hrs · 2,787 cycles

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

Part: BEARING — WORN (NLG) · airframe 3,752 hrs · 2,212 cycles

DURING TAXI INTO GATE, NOTED RT NLG WHEEL ASSY HAVING EXESSIVE PLAY. DISCOVERED RT NLG TIRE INNER BEARING AND RACE WORN. REMOVED AND REPLACED BOTH NLG TIRE/WHEEL ASSY'S, ALSO REMOVED AND REPLACED NLG AXEL ASSY DUE TO OVERHEAT. ALL WORK PER MM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 2,748 hrs · 1,607 cycles

DURING SCHEDULED RON, FOUND EMERGENCY FLASHLIGHT INOP AT AFT CABIN LT SIDE. REMOVED AND REPLACED BATTERY PER MM.

Part: SLIDE — OUT OF TOLERANCE (ENTRY DOOR) · airframe 10 hrs · 8 cycles

FWD ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE ASSY PER MM.