N707SA

Part: CONTROLLER — FAULTY (CABIN PRESSURE) · airframe 72,072 hrs · 43,180 cycles

AIR TURNBACK, CABIN ALTITUDE WARNING ON AT 27000 FT. CABIN ALTITUDE REACHED 10000. PSID READING IN AMBER BAND. CABIN ALTITUDE SHOWING 40000. NO PAX MASK DEPLOYMENT. R & R NR 2 CABIN PRESSURE CONTROLLER IAW AMM.

Part: SIGN — BROKEN (CABIN) · airframe 70,762 hrs · 42,340 cycles

MID CABIN OVERHEAD EXIT SIGN BRACKET BROKEN. R&R SIGN IAW MM.

Part: SIGN — LOOSE (CABIN) · airframe 70,519 hrs · 42,181 cycles

MID CABIN CEILING EMERGENCY EXIT SIGN LOOSE. SECURED SIGN PER SIP.

Part: COVER — UNSECURE (R1 DOOR) · airframe 70,478 hrs · 42,151 cycles

R1 DOOR SLIDE MANUAL DISPLAY HANDLE EXPOSED. SECURED COVER PER AMM.

Part: SIGN — LOOSE (CABIN) · airframe 70,430 hrs · 42,122 cycles

CEILING OVERWING EXIT SIGN LOOSE. SECURED SIGN IAW AMM.

Part: SCUFF PLATE — CRACKED (FWD ENTRY DOOR () · airframe 70,128 hrs · 41,932 cycles

FWD ENTRY DOOR AFT CORNER THRESHOLD CRACKED 2' IN CENTER @ RADIUS. / R&R'D FWD ENTRY AFT CORNER THRESHOLD PER AMM 53-11-01.

Part: BATTERY PACK — FAILED (CABIN) · airframe 70,128 hrs · 41,932 cycles

ONE EMERGENCY LIGHTING BATTERY PACK FAILED CAPACITY TEST (M10669). R&R BATTERY PACK PER AMM.

Part: BRACKET — LOOSE (R1 DOOR) · airframe 69,904 hrs · 41,798 cycles

R1 DOOR GIRT BAR BRACKET LOOSE. ADJUSTED BAR CLIP PER SIP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 69,815 hrs · 41,738 cycles

R1 DOOR EXIT LIGHT BULB INOP. RELAMPED LIGHT PER AMM.

Part: WIRE — OUT OF POSITION (CABIN) · airframe 69,815 hrs · 41,738 cycles

FORWARD LAV AFT WALL EMERGENCY EXIT WIRING OUT OF POSITION. REPAIRED WIRE PER SWPM AND WDM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 69,815 hrs · 41,738 cycles

R2 DOOR SLIDE EMERGENCY LIGHT INOP. R&R BATTERY PER AMM.

Part: BATTERY PACK — DISCHARGED (COCKPIT) · airframe 69,815 hrs · 41,738 cycles

FLIGHT DECK DOME EMERGENCY EXIT LIGHT INOP. R&R BATTERY PACK PER AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 69,815 hrs · 41,738 cycles

RT AISLE EMERGENCY LIGHT INOP AT ROW 16. RELAMPED LIGHT IAW MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 69,815 hrs · 41,738 cycles

RT AISLE EMERGENCY LIGHT INOP BETWEEN ROW 16 TO ROW 19. R&R BATTERY PER AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 69,815 hrs · 41,738 cycles

FORWARD SERVICE UPPER EMERGENCY EXIT LIGHT INOP. R&R BATTERY PACK PER AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 69,815 hrs · 41,738 cycles

LT AISLE EMERGENCY EXIT LIGHT INOP AT ROW 4. R&R BATTERY PACK PER AMM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 69,815 hrs · 41,738 cycles

L2 DOOR SLIDE UPPER EMERGENCY LIGHT INOP. R&R BATTERY PER AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 69,815 hrs · 41,738 cycles

RT OVERWING ESCAPE EMERGENCY LIGHT BULB INOP AT ROW 16. RELAMPED LIGHT IAW MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 69,815 hrs · 41,738 cycles

AFT CENTER AISLE EMERGENCY LIGHT INOP. R&R BATTERY PER AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 69,815 hrs · 41,738 cycles

L1 DOOR SLIDE EMERGENCY EXIT LIGHT INOP. R&R BATTERY PACK PER AMM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 69,815 hrs · 41,738 cycles

R2 DOOR EMERGENCY LOWER LIGHT INOP. R&R BATTERY PER AMM.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 69,815 hrs · 41,738 cycles

RT AFT EMERGENCY CHARGER INOP. RECONNECTED CONNECTORS PER AMM.

Part: NONE — CRACKED (MAIN CABIN) · airframe 69,815 hrs · 41,738 cycles

CRACKED BREAK PANEL STA 540; BLO-LBL 25; WL 208. / REMOVED DAMAGED PANEL BREAK AND LOCATED; DRILLED AND INSTALLED NEW PANEL BREAK BS 540; BL 0 - LBL 25 WL 208 PER SRM 51-40-02-0G-0 AND SRM 51-40-05-0G-0 56546U 11-02-2018

Part: BULKHEAD — CRACKED (LT MLG WW) · airframe 69,815 hrs · 41,738 cycles

BULKHEAD VERTICAL WEB CRACKED AT BS 663, LBL 50. REPAIRED WEB IAW DWG & SRM.

Part: BAFFLE — CRACKED (FUSELAGE) · airframe 69,815 hrs · 41,738 cycles

FORWARD CARGO BAY FLOOR TO SIDEWALL BAFFLE CRACKED BETWEEN BS 500B TO BS 500C, RBL 21. R&R BAFFLE PER SRM & DWG.

Part: STRAP — DETERIORATED (OVERWING EXIT) · airframe 69,815 hrs · 41,738 cycles

RT OVERWING EXIT ESCAPE STRAP ASSEMBLY DETERIORATED. R&R STRAP ASSEMBLY IAW AMM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 69,815 hrs · 41,738 cycles

RT CREASE BEAM WEB UPPER SURFACE CORRODED AT BS 721, RBL 65. REPAIRED WEB PER SRM & DWG.

Part: STRAP — CORRODED (MAIN CABIN) · airframe 69,815 hrs · 41,738 cycles

***CORROSION*** ON CABIN FRAME STRAP AT STA 540 STR 9R / CORROSION ON CABIN FRAME STRAP BS 540 STR 9R REWORKED IAW EA# 1-753-33598 REV IR & ER #18-04774 REV IR.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 69,815 hrs · 41,738 cycles

LT OVER WING EMERGENCY EXIT DOOR LOWER SILL CORRODED BETWEEN BS 616 TO BS 639. REPAIRED SILL PER EA & ER.

Part: FITTING — CRACKED (FUSELAGE) · airframe 69,815 hrs · 41,738 cycles

CLIP CRACKED AT BS 649.96, RBL 40.93. R&R CLIP IAW SRM AND DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 69,815 hrs · 41,738 cycles

FLOORBEAM WEB CORRODED BS 259, BETWEEN LBL 16 TO RBL 3. REPAIRED WEB PER ER AND EA.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 69,815 hrs · 41,738 cycles

SEAT TRACK CORRODED BETWEEN BS 540 TO BS 727B, LBL 45. R&R SEAT TRACK IAW SRM AND DWG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 69,815 hrs · 41,738 cycles

CABIN SEAT TRACK CORRODED BETWEEN BS 540 TO BS 727B, RBL 45. R&R SEAT TRACK IAW SRM AND DWG.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 69,815 hrs · 41,738 cycles

L1 DOOR CUT OUT FRAME CRACKED AT BS 312. REPAIRED FRAME PER EA & ER.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 69,815 hrs · 41,738 cycles

FLOORBEAM UPPER FORWARD CHORD CORRODED AT BS 259, BETWEEN LBL 13 TO RBL 5. REPAIRED CHORD IAW EA AND ER.

Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 69,815 hrs · 41,738 cycles

FORWARD SIDE OF BULKHEAD WEB CORRODED AT BS 1088, BETWEEN RBL 20 TO RBL 25. REPAIRED WEB IAW ER AND EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 69,815 hrs · 41,738 cycles

FLOORBEAM UPPER AFT CHORD CORRODED AT BS 259, BETWEEN LBL 11 TO RBL 3. REPAIRED CHORD PER ER AND EA.

Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 69,815 hrs · 41,738 cycles

AUXILIARY POWER UNIT INLET CUTOUT BULKHEAD CORRODED AT BS 1088, BETWEEN RBL 22 TO RBL 31. R&R L ANGLE PER SRM AND DWG.

Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 69,815 hrs · 41,738 cycles

AUXILIARY POWER UNIT INLET CUTOUT BULKHEAD CORRODED AT BS 1088, BETWEEN RBL 22 TO RBL 31. R&R T ANGLE PER SRM AND DWG.

Part: SEAL — CRACKED (RT HORIZ STAB) · airframe 69,815 hrs · 41,738 cycles

RT HORIZ STAB UPPER SLIDE SEAL IS CRACKED / REMOVED AND REPLACED RT HORIZONTAL STAB UPPER SLIDE SEAL IAW AMM 53-31-31-400-802 84036U 11OCT18 AND AMM 53-31-31-000-802 84036U 11OCT18

Part: FLAP — CRACKED (TE FLAP) · airframe 69,815 hrs · 41,738 cycles

RT WING, OUTBOARD AFT FLAP, INBOARD AFT CORNER CRACKED. REPAIRED AFT FLAP PER SRM.

Part: BEAM — CRACKED (FWD SERVICE DOOR) · airframe 69,815 hrs · 41,738 cycles

DURING COMPLETION OF CCN: 14079 FOUND FORWARD SERVICE DOOR #4 (LOWER) BEAM TO BE CRACKED COMMON TO THE HANDLE BOX ASSY FORWARD MOST ATTACH POINT AT THE INBD FASTENER HOLE. / FWD SERVICE DOOR #4 (LOWER) BEAM CRACKED COMMON TO THE HANDLE BOX ASSY FWD MOST ATTACH POINT AT THE INBD FASTENER HOLE WAS REPAIRED ON CUSTOMER P.O. 0520055-CKR.

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 69,815 hrs · 41,738 cycles

HORIZONTAL PRESSURE DECK CRACKED AT BS 665, LBL 32. REPAIRED DECK PER ER AND EA.

Part: PRESSURE DECK — CRACKED (FUSELAGE) · airframe 69,815 hrs · 41,738 cycles

HORIZONTAL PRESSURE DECK CRACKED AT BS 673, RBL 41.5. REPAIRED DECK IAW EA.

Part: SKIN — CORRODED (AFT CARGO BAY) · airframe 69,815 hrs · 41,738 cycles

AFT CARGO DOOR INNER SKIN HAS MULTIPLE AREAS OF CORROSION 2' UP FROM LOWER EDGE OF DOOR / AFT CARGO DOOR INNER SKIN WAS REPAIRED ON CUST. PO# 0520047-AFR

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 69,815 hrs · 41,738 cycles

AFT CARGO BAY, RT FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 727 TO BS 767, RBL 23. R&R SUPPORT IAW SRM AND DWG.

Part: SEAL — CRACKED (RT WING) · airframe 69,815 hrs · 41,738 cycles

RIGHT WING TRAILING EDGE CURVED SEAL RETAINER ABOVE #2 PYLON AT FWD SIDE OF TRANSVERSE WEB CRACKED / REMOVED AND REPLACED RT WING T/E PANEL SEAL RETAINER JUST ABOVE #2 PYLON; FWD SIDE OF TRANSVERSES WEB PER SRM 51-40-02-0G-0; AND IPC 57-50-00-25 FOR FASTENER CALL OUT.

Part: PLATE — CRACKED (LT WING) · airframe 69,815 hrs · 41,738 cycles

LT WING TRAILING EDGE WIGGLE PLATE AT INBOARD SIDE OF PANEL 551EB CRACKED. R&R WIGGLE PLATE PER SRM.

Part: SEAL — CRACKED (RT WING) · airframe 69,815 hrs · 41,738 cycles

RIGHT WING TRAILING EDGE SEAL RETAINER ABOVE #2 PYLON AFT SIDE OF TRANSVERSE WEB CRACKED / REMOVED AND REPLACED RIGHT WING TRAILING EDGE SEAL RETAINER ABOVE #2 PYLON AFT SIDE OF TRANSVERSE WEB IAW SRM 51-40-02-0G FASTENERS IAW AIPC 57-50-00-25 89813U 10-12-18

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 69,815 hrs · 41,738 cycles

AFT CARGO BAY, LT FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 727D TO BS 787, LBL 23. R&R SUPPORT IAW SRM & DWG.

Part: PLATE — CRACKED (LT WING) · airframe 69,815 hrs · 41,738 cycles

LT WING TRAILING EDGE WIGGLE PLATES CRACKED BETWEEN RSS 297 INBOARD TO THE NR 3 FLAP TRACK. R&R WIGGLE PLATE IAW SRM.

Part: ATTACH FITTING — CRACKED (LT WING) · airframe 69,815 hrs · 41,738 cycles

LEFT WING LOWER TRAILING EDGE PANEL AFT ATTACH BEAM BROKEN BELOW #5 SPOILER PANEL / REMOVED AND REPLACED LEFT WING LOWER TRAILING EDGE PANEL AFT ATTACH BEAM BELOW #5 SPOILER IAW SRM 51-40-02-0G-0 84036U 16OCT18

Part: SHIELD — CORRODED (FUSELAGE) · airframe 69,815 hrs · 41,738 cycles

AFT CARGO BAY, SHIELD FORWARD OF CARGO DOOR CORRODED BETWEEN BS 767 TO BS 787, RBL 23. R&R SHIELD PER SRM & DWG.

Part: PLATE — CRACKED (RT WING) · airframe 69,815 hrs · 41,738 cycles

RT WING TRAILING EDGE WIGGLE PLATE AT INBOARD SIDE OF PANEL 651EB CRACKED. R&R WIGGLE PLATE PER SRM.

Part: SEAL — CRACKED (L/H HORIZ. STAB.) · airframe 69,815 hrs · 41,738 cycles

LT STAB UPPER SLIDE SEAL IS CRACKED / REMOVED LT STAB UPPER SLIDE SEAL IAW MM 53-31-31-000-802 STEP 2.D.(2);(3);(5); 2.E. 5942R 11OCT18. INSTALLED A NEW SLIDE SEAL FOR LT HORIZ STAB IAW MM 53-31-31-400-802 STEPS 3.D.; 3.E.

Part: ACCESS PANEL — DELAMINATED (LT WING) · airframe 69,815 hrs · 41,738 cycles

#1 ENGINE PYLON ACCESS PANEL 431ER IS DISBANDED AT LWR FWD CORNER. / REPLACED #1 ENGINE PYLON ACCESS PANEL 431ER WITH NEW LOCATED FASTENER HOLE'S RESTORED FINISH PER SRM 51-40-02-0G-1 SRM 51-20-07-0G-0 DRAWING 311A2531 & AMM 51-21-99-300-801 INSTALLATION OF PANEL TO BS ACCOMPLISHED ON CUST: CARD JPANEL-431-CLOSE

Part: GUSSET — CRACKED (FUSELAGE) · airframe 69,815 hrs · 41,738 cycles

FORWARD CARGO BAY GUSSET CRACKED AT BS 500D, STR 19R. R&R GUSSET PER SRM & DWG.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 69,815 hrs · 41,738 cycles

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

Part: SUPPORT PLATE — CORRODED (FUSELAGE) · airframe 69,815 hrs · 41,738 cycles

FORWARD CARGO BAY RT FLOOR TO SIDEWALL SUPPORT PLATE CORRODED BETWEEN BS 500A TO BS 500D, RBL 22. R&R SUPPORT IAW SRM AND DWG.

Part: WEB — CORRODED (FUSELAGE) · airframe 69,815 hrs · 41,738 cycles

FORWARD CARGO BAY SUB THRESHOLD WEB CORRODED BETWEEN BS 440 TO BS 492, RBL 23. R&R WEB PER SRM & DWG.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 69,815 hrs · 41,738 cycles

FORWARD CARGO BAY, SHIELD CORRODED BETWEEN BS 492 TO BS 500, RBL 23. R&R SHIELD IAW SRM AND DWG.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 69,815 hrs · 41,738 cycles

FORWARD CARGO BAY GUSSET CRACKED AT BS 500D, STR 19L. R&R GUSSET PER SRM & DWG.

Part: SPLICE STRAP — CORRODED (FWD CARGO BAY) · airframe 69,815 hrs · 41,738 cycles

FWD CARGO BAY FLOOR SPLICE STRAP AT BS 420+10 RBL10 TO LBL10 HAS AREAS OF CORROSION / RECEIVED NEW FWD CARGO BAY FLOOR SPLICE STRAP FOR B.S. 5420+10 ON PO #709593. FOR PART'S TRACKING ONLY

Part: FLOOR SPLICE — CRACKED (AFT CARGO BAY) · airframe 69,815 hrs · 41,738 cycles

AFT CARGO BAY FLOOR SPLICE STRAP AT BS767 IS CRACKED ON OUTBOARD END / RECEIVED A NEW ACB FLOOR SPLICE STRAP FOR B.S. 767 ON PO# 696266. FOR PARTS TRACKING ONLY.

Part: VAPOR BARRIER — CRACKED (FUSELAGE) · airframe 69,815 hrs · 41,738 cycles

RT LOWER VAPOR BARRIER CRACKED AT BS 663, BETWEEN RBL 10 TO RBL 15. REPAIRED BARRIER IAW SRM.

Part: LENS — BROKEN (CABIN) · airframe 68,889 hrs · 41,164 cycles

RT OVERWING EMERGENCY EXIT LENS BROKEN. R&R LENS PER SIP.

Part: SUPPORT CHANNEL — BROKEN (RT AC BAY) · airframe 68,635 hrs · 40,995 cycles

RIGHT A/C BAY AFT VAPOR BARRIER WALL CROSS BRACE SUPPORT CHANNEL BROKEN AT INBOARD END / R&R RIGHT A/C BAY; AFT VAPOR BARRIER WALL CROSS BRACE SUPPORT CHANNEL REF SRM 51-40-02; AMM 51-21-22; AMM 51-21-91.

Part: BULKHEAD WEB — CRACKED (BS 663) · airframe 66,999 hrs · 39,957 cycles

BULKHEAD WEB CRACKED BETWEEN RBL 6.14 TO RBL 15.54, BS 663. REPAIRED THE BULKHEAD SRM.

Part: ATTACH BRACKET — BROKEN (FUSELAGE) · airframe 66,740 hrs · 39,798 cycles

KEEL BEAM PANEL 192E-FWD LEFT ATTACH BRACKET BROKEN OFF. / REMOVED AND REPLACED THE LEFT FWD KEEL BEAM ATTACH BRACKET UNDER PANEL 192 E PER SRM 51-40-02.

Part: WINDOW — ARCED (COCKPIT) · airframe 66,713 hrs · 39,782 cycles

CAPTAINS L1 WINDOW HEAT INOP, IT ARCED ON CLIMBOUT. R&R WINDOW PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 66,643 hrs · 39,737 cycles

R1 DOOR OVERHEAD EMERGENCY EXIT FLOOD LIGHT BULB INOP. RELAMPED LIGHT PER MM.

Part: COVER — DEFECTIVE (CABIN) · airframe 65,781 hrs · 39,223 cycles

L1 DOOR EMERGENCY EXIT LIGHT COVER MISSING RED ARROW. R&R COVER PER AMM.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 64,630 hrs · 38,524 cycles

BATTERY PACK FAILED CAPACITY TEST AT POSITION M01670. R & R THE BATTERY PACK IAW AMM AND DWG.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 64,630 hrs · 38,524 cycles

BATTERY PACK FAILED CAPACITY TEST AT POSITION M01672. R & R THE BATTERY PACK IAW AMM AND DWG.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 64,630 hrs · 38,524 cycles

BATTERY PACK FAILED CAPACITY TEST AT POSITION M01668. R & R THE BATTERY PACK IAW AMM AND DWG.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 64,630 hrs · 38,524 cycles

BATTERY PACK FAILED CAPACITY TEST AT POSITION M01673. R & R THE BATTERY PACK IAW AMM AND DWG.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 63,739 hrs · 38,002 cycles

FORWARD EMERGENCY EXIT LENS MISSING. INSTALLED LENS IAW SIP.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 63,275 hrs · 37,716 cycles

L1 DOOR OVERHEAD EMERGENCY EXIT LIGHT INOPERATIVE. REPAIRED THE WIRE IAW WDM.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 63,275 hrs · 37,716 cycles

R2 DOOR LOWER SILL WEB CORRODED BETWEEN BS 951 TO BS 993, RBL 55. R & R WEB IAW SRM.

Part: SHEAR WEB — CORRODED (FUSELAGE) · airframe 63,275 hrs · 37,716 cycles

SHEAR WEB CORRODED BETWEEN BS 986 TO BS 1006, RBL 45. R & R SHEAR WEB IAW SRM.

Part: STRAP — CORRODED (FUSELAGE) · airframe 63,275 hrs · 37,716 cycles

SHEAR WEB STRAP CORRODED AT BS 1010, LBL 6. R & R STRAP IAW SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 63,275 hrs · 37,716 cycles

R1 DOOR THRESHOLD SUPPORT CORRODED. R & R SUPPORT IAW SRM.

Part: FLOORBEAM — CORRODED (BS 328) · airframe 63,275 hrs · 37,716 cycles

FLOORBEAM UPPER SURFACE CORRODED AT BS 328, BETWEEN RBL 50 TO 60. R & R FLOORBEAM IAW SRM.

Part: FLOORBEAM — CORRODED (BS 986) · airframe 63,275 hrs · 37,716 cycles

FLOORBEAM SPLICE CORRODED AT BS 986, BETWEEN RBL 25 TO 45. REPAIRED FLOORBEAM IAW EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 63,275 hrs · 37,716 cycles

FLOORBEAM CORRODED AT BS 967, RBL 28. REPAIRED FLOORBEAM IAW SRM & EA.

Part: FLAP TRACK — DAMAGED (LT WING FLAP) · airframe 63,275 hrs · 37,716 cycles

LEFT WING INBOARD FLAP INBOARD AFT FLAP TRACK PLATING DAMAGED. R & R THE AFT FLAP TRACK IAW AMM.

Part: SIDEWALL SUPPORT — CORRODED (BS 727D-767) · airframe 63,275 hrs · 37,716 cycles

AFT CARGO BAY RIGHT FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 727D - 767. R & R THE SIDEWALL SUPPORT IAW SRM AND DWG.

Part: ATTACH BRACKET — CRACKED (LT WING) · airframe 63,275 hrs · 37,716 cycles

LEFT WING OUTBOARD NO STEP PANEL WEB TO DEFLECTOR ROLLER RIB ATTACH BRACKET CRACKED. R & R THE ATTACH BRACKET IAW DWG & SRM.

Part: WEB — CORRODED (THRESHOLD) · airframe 63,275 hrs · 37,716 cycles

AFT CARGO BAY SUB THRESHOLD WEB CORRODED. R & R WEB SRM.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 63,275 hrs · 37,716 cycles

AFT CARGO BAY INTERCOSTAL CORRODED BETWEEN BS 767 TO BS 787, STR 27R. R & R INTERCOSTAL IAW SRM.

Part: FITTING — CORRODED (RT MLG TRUNNION) · airframe 62,894 hrs · 37,496 cycles

RIGHT MAIN LANDING GEAR FORWARD TRUNNION SUPPORT FITTING LUG CORRODED. R & R FITTING IAW EA.

Part: SUPPORT FITTING — CORRODED (RT MLG TRUNNION) · airframe 62,894 hrs · 37,496 cycles

RT MLG FORWARD TRUNNION SUPPORT FITTING LUG FACE CORRODED. R & R FITTING IAW EA.

Part: FITTING — CORRODED (LT MLG TRUNNION) · airframe 62,894 hrs · 37,496 cycles

LEFT MAIN LANDING GEAR FORWARD TRUNNION SUPPORT FITTING LUG CORRODED. R & R FITTING IAW EA.

Part: SUPPORT FITTING — CORRODED (LT MLG TRUNNION) · airframe 62,894 hrs · 37,496 cycles

LEFT MLG FORWARD TRUNNION SUPPORT FITTING LUG FACE CORRODED. R & R FITTING IAW EA.

Part: COVER — BROKEN (CABIN) · airframe 61,247 hrs · 36,551 cycles

R2 DOOR EMER EXIT LIGHT COVER BROKEN. R & R BATTERY PACK IAW MM.

Part: COVER — BROKEN (CABIN) · airframe 61,247 hrs · 36,551 cycles

R2 DOOR EMER EXIT LIGHT COVER BROKEN. R & R LIGHT ASSEMBLY IAW MM.

Part: LENS — MISSING (CABIN) · airframe 60,499 hrs · 36,120 cycles

EMERGENCY AISLE BULLNOSE LIGHT LENS MISSING. INSTALLED LENS IAW MM.

Part: COVER — MISSING (EXIT SIGN) · airframe 59,365 hrs · 35,461 cycles

EMERGENCY EXIT LIGHT COVER MISSING NEXT TO REAR SERVICE DOOR. INSTALLED SIGN IAW MM.

Part: LENS — LOOSE (CABIN) · airframe 59,001 hrs · 35,248 cycles

FORWARD ENTRY LOWER EMER EXIT LENS LOOSE. SECURED LENS IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 58,337 hrs · 34,872 cycles

R1 DOOR EMER EXIT LAMP INOPERATIVE. RELAMPED LAMP IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 58,337 hrs · 34,872 cycles

L1 DOOR EMER EXIT LAMP INOPERATIVE. RELAMPED LAMP IAW AMM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,758 hrs · 33,985 cycles

STRINGER CLIP CRACKED AT BS 348.2 STRINGER 14L. R & R CLIP IAW SRM & DWG.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 56,758 hrs · 33,985 cycles

CENTER WING BOX ZEE STRINGER UPPER FLANGE CRACKED AT BS 540 RBL 40. REPAIRED FLANGE IAW SRM & EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,758 hrs · 33,985 cycles

FRAME CRACKED AT BS 520, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,758 hrs · 33,985 cycles

FRAME CRACKED AT BS 500A STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,758 hrs · 33,985 cycles

FRAME CRACKED AT BS 706 STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,758 hrs · 33,985 cycles

FRAME CRACKED AT BS 727B STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,758 hrs · 33,985 cycles

FRAME WEB CRACKED AT BS 727D, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,758 hrs · 33,985 cycles

FRAME CRACKED AT BS 747 STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,758 hrs · 33,985 cycles

FRAME CRACKED AT BS 827 STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,758 hrs · 33,985 cycles

FRAME WEB CRACKED AT BS 500A, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,758 hrs · 33,985 cycles

FRAME CRACKED AT BS 500C STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,758 hrs · 33,985 cycles

FRAME CRACKED AT BS 787 STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,758 hrs · 33,985 cycles

FRAME CRACKED AT BS 907 STRINGER 8R. REPAIRED FRAME IAW EA.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 56,758 hrs · 33,985 cycles

LEFT NR 3 WINDOW FRAME E-F POST 2ND FASTENER HOLE FROM BOTTOM CRACKED. REPAIRED FRAME IAW ACO.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 56,758 hrs · 33,985 cycles

MAIN WW SPAR VERTICAL PRESS WEB CRACKED AT BS 663 LBL 40. REPAIRED WEB IAW SRM.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 56,758 hrs · 33,985 cycles

RIGHT NR 1 WINDOW FRAME OTBD UPPER CORNER CRACKED. REPAIRED FRAME IAW ACO.

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 56,758 hrs · 33,985 cycles

MAIN WW SPAR VERTICAL PRESS WEB CRACKED AT BS 663 RBL 40. REPAIRED WEB IAW SRM.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 56,758 hrs · 33,985 cycles

RIGHT NR 3 WINDOW FRAME E-F POST 2ND FASTENER HOLE FROM BOTTOM CRACKED. REPAIRED FRAME IAW SI.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,430 hrs · 33,799 cycles

BULKHEAD SKIN CRACKED AT BS 540 BETWEEN STRINGER 22R TO 23R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,430 hrs · 33,799 cycles

BULKHEAD SKIN CRACKED AT BS 540 BETWEEN STRINGER 22L TO 23L. REPAIRED SKIN IAW EA.

Part: BRACKET — BROKEN (EXIT SIGN) · airframe 54,889 hrs · 32,925 cycles

CTR EMERGENCY EXIT SIGN BRACKET BROKEN. R & R LIGHT ASSEMBLY IAW MM.

Part: FAIRING — CRACKED (LT WING) · airframe 52,425 hrs · 31,473 cycles

LEFT WING NR 3 AFT CANOE FAIRING CRACKED. REPAIRED FAIRING IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 52,425 hrs · 31,473 cycles

SEAT TRACK CRACKED AT STA 727B, LBL 45.5. REPAIRED SEAT TRACK IAW AAR EA AND EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 52,425 hrs · 31,473 cycles

SEAT TRACK CRACKED AT STA 727B, RBL 45.5. REPAIRED SEAT TRACK IAW AAR EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 52,425 hrs · 31,473 cycles

SEAT TRACK CRACKED AT STA 727B, RBL 24.75. REPAIRED SEAT TRACK IAW AAR EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 52,425 hrs · 31,473 cycles

SEAT TRACK CRACKED AT STA 727B, LBL 24.75. REPAIRED SEAT TRACK IAW AAR EA.

Part: LENS — BROKEN (CABIN) · airframe 50,297 hrs · 30,158 cycles

FORWARD LAVATORY EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LENS IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 49,522 hrs · 29,680 cycles

L1 DOOR EMERGENCY LIGHT INOP. REMOVED AND REPLACED LIGHT IAW AMM.

Part: SIGN — LOOSE (CABIN) · airframe 49,359 hrs · 29,590 cycles

OVERHEAD EMERGENCY EXIT SIGN LOOSE AT ROW 11. SECURED SIGN PER MM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 48,460 hrs · 29,068 cycles

FWD LT EMERGENCY LIGHT BATTERY CHARGER INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY CHARGER PER MM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 48,460 hrs · 29,068 cycles

EMERGENCY LIGHT BATTERY CHARGER INOP. REMOVED AND REPLACED CHARGER PER MM.

Part: BATTERY — FAILED (CABIN) · airframe 48,460 hrs · 29,068 cycles

LT EMERGENCY EXIT LIGHT BATTERY FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERY PER MM.

Part: BATTERY — FAILED (CABIN) · airframe 48,460 hrs · 29,068 cycles

RT EMERGENCY EXIT LIGHT BATTERY FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERY PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 48,299 hrs · 28,966 cycles

DURING SCHEDULED MV1 CHECK, FOUND L1 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 48,252 hrs · 28,938 cycles

DURING SCHEDULED RON CHECK, FOUND L1 DOOR AFT EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LAMP PER MM.

Part: LENS — MISSING (CABIN) · airframe 47,767 hrs · 28,661 cycles

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

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 46,380 hrs · 27,858 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT AFT EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.

Part: LENS — MISSING (CABIN) · airframe 45,543 hrs · 27,349 cycles

LT OVERHEAD EMERGENCY EXIT BULLNOSE LIGHT LENS MISSING AT ROW 1. INSTALLED LENS PER MM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 43,802 hrs · 26,315 cycles

DURING SCHEDULED 12Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986, RBL 5. REPAIRED BEAM PER SRM.

Part: CONNECTOR — CRACKED (CABIN) · airframe 43,802 hrs · 26,315 cycles

DURING SCHEDULED 12Y CHECK, FOUND RT EEPLS CONNECTOR CRACKED AT ROW 13. REMOVED AND REPLACED CONNECTOR PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 43,802 hrs · 26,315 cycles

DURING SCHEDULED 12Y CHECK, FOUND L1 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BULB PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 43,802 hrs · 26,315 cycles

DURING SCHEDULED 12Y CHECK, FOUND R2 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BULB PER MM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 43,802 hrs · 26,315 cycles

DURING SCHEDULED 12Y CHECK, FOUND FLOORBEAM UPPER T CAP CORRODED AT BS 987, RBL 39. REPAIRED BEAM PER ER AND EA.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 43,802 hrs · 26,315 cycles

DURING SCHEDULED 12Y CHECK, FOUND FWD CARGO COMPARTMENT LT Z-ANGLE CORRODED BETWEEN BS 420 TO BS 440. REMOVED AND REPLACED Z-ANGLE PER SRM.

Part: SIGN — BROKEN (CABIN) · airframe 43,802 hrs · 26,315 cycles

DURING SCHEDULED 12Y CHECK, FOUND FWD LAV, AFT O/B LOWER WALL EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED SIGN PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,802 hrs · 26,315 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 360, STR 8R. REPAIRED FRAME PER EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 43,802 hrs · 26,315 cycles

DURING SCHEDULED 12Y CHECK, FOUND FLOORBEAM UPPER T-CAP CORRODED AT BS 987, BETWEEN RBL 6 TO LBL 5. REPAIRED BEAM PER ER AND EA.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 43,802 hrs · 26,315 cycles

DURING SCHEDULED 12Y CHECK, FOUND FWD CARGO COMPARTMENT LT Z-ANGLE CORRODED BETWEEN BS 400 TO BS 420. REMOVED AND REPLACED Z-ANGLE PER SRM.

Part: HOOK — BROKEN (GIRT BAR) · airframe 43,802 hrs · 26,315 cycles

DURING SCHEDULED 12Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE LT GIRT BAR HOOK BROKEN. REMOVED AND REPLACED HOOK PER MT.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 43,802 hrs · 26,315 cycles

DURING SCHEDULED 12Y CHECK, FOUND FLOORBEAM WEB CRACKED BETWEEN BS 986 TO BS 1016, RBL 38.5. REMOVED AND REPLACED WEB PER BAC DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 43,802 hrs · 26,315 cycles

DURING SCHEDULED 12Y CHECK, FOUND AFT CARGO COMPARTMENT ZEE ANGLE CORRODED BETWEEN BS 727 TO BS 767, RBL 22. REPAIRED ZEE ANGLE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 43,802 hrs · 26,315 cycles

DURING SCHEDULED 12Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 10R. REMOVED AND REPLACED CLIP PER SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 43,802 hrs · 26,315 cycles

DURING SCHEDULED 12Y CHECK, FOUND AFT CARGO COMPARTMENT Z-ANGLE CORRODED BETWEEN BS 767 TO BS 787, RBL 22. REPAIRED Z-ANGLE PER SRM AND BAC DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 43,802 hrs · 26,315 cycles

DURING SCHEDULED 12Y CHECK, FOUND RT CREASE BEAM CORRODED BETWEEN BS 960 TO BS 987. REMOVED AND REPLACED BEAM PER SRM AND BAC DWG.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 43,811 hrs · 26,321 cycles

DURING SCHEDULED 12Y CHECK, FOUND LT EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 43,802 hrs · 26,315 cycles

DURING SCHEDULED 12Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 1. REMOVED AND REPLACED CLIP PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 43,802 hrs · 26,315 cycles

DURING SCHEDULED 12Y CHECK, FOUND FLOORBEAM CORRODED BETWEEN BS 296 TO BS 325, RBL 52. REPAIRED BEAM PER SRM AND BAC DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 43,802 hrs · 26,315 cycles

DURING SCHEDULED 12Y CHECK, FOUND FLOORBEAM CORRODED BETWEEN BS 897 TO BS 1006, LBL 55. REPAIRED BEAM PER SRM AND BAC DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 43,802 hrs · 26,315 cycles

DURING SCHEDULED 12Y CHECK, FOUND FLOORBEAM CORRODED BETWEEN BS 967 TO BS 987, LBL 50. REPAIRED BEAM PER SRM AND BAC DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,802 hrs · 26,315 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 292, STR 17R. REPAIRED FRAME PER SRM.

Part: FUSE — BLOWN (CABIN) · airframe 43,185 hrs · 25,959 cycles

DURING SCHEDULED CV CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE LIGHT INOP. REMOVED AND REPLACED FUSE PER MM.

Part: ENGINE — FAILED (NR 2) · airframe 38,651 hrs · 23,204 cycles

ABORTED TAKEOFF/RETURN TO GATE. AFTER SETTING T/O THRUST HEARD A LOUD BANG FROM NR 2 ENGINE ABORTED T/O AT 40 KNOTS. NR 2 ENGINE FAILED AND NO ENGINE INDICATION RETURNED TO GATE. FOUND METAL IN REAR OF NR 2 ENGINE TAIL PIPE. REMOVED AND REPLACED NR 2 ENGINE ASSY PER MT.

Part: COVER — MISSING (CABIN) · airframe 38,380 hrs · 23,042 cycles

R2 EMERGENCY EXIT DOOR LIGHT COVER MISSING. REPLACED LIGHT ASSY PER MM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 37,731 hrs · 22,641 cycles

DURING SCHEDULED 10Y CHECK, FOUND FLOORBEAM TEE CAP CRACKED AT BS 540, RBL 1. REPAIRED BEAM PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 37,731 hrs · 22,641 cycles

DURING SCHEDULED 10Y CHECK, FOUND FLOORBEAM TEE CAP CRACKED AT BS 540, LBL 1. REPAIRED BEAM PER SRM.

Part: SKIN — CRACKED (LT WING) · airframe 37,731 hrs · 22,641 cycles

DURING SCHEDULED 10Y CHECK, FOUND LT WING L/E SKIN CRACKED AT I/B END. REPAIRED SKIN PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 37,731 hrs · 22,641 cycles

DURING SCHEDULED 10Y CHECK, FOUND SHEAR TIE CRACKED AT BS 540, RBL 6. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 37,731 hrs · 22,641 cycles

DURING SCHEDULED 10Y CHECK, FOUND SHEAR TIE CRACKED AT BS 540, LBL 32. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 37,731 hrs · 22,641 cycles

DURING SCHEDULED 10Y CHECK, FOUND SHEAR TIE CRACKED AT BS 540, RBL 32. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 37,731 hrs · 22,641 cycles

DURING SCHEDULED 10Y CHECK, FOUND SHEAR TIE CRACKED AT BS 540, RBL 40. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 37,731 hrs · 22,641 cycles

DURING SCHEDULED 10Y CHECK, FOUND SHEAR TIE CRACKED AT BS 540, LBL 15. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 37,731 hrs · 22,641 cycles

DURING SCHEDULED 10Y CHECK, FOUND SHEAR TIE CRACKED AT BS 540, LBL 40. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 37,731 hrs · 22,641 cycles

DURING SCHEDULED 10Y CHECK, FOUND SHEAR TIE CRACKED AT BS 540, LBL 6. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 37,731 hrs · 22,641 cycles

DURING SCHEDULED 10Y CHECK, FOUND SHEAR TIE CRACKED AT BS 540, RBL 15. REPAIRED SHEAR TIE PER SRM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 37,683 hrs · 22,614 cycles

DURING SCHEDULED HC1 CHECK, AFT GALLEY RT BATTERY PACK FAILED LONG TEST. R&R BATTERY PACK PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 37,683 hrs · 22,614 cycles

DURING SCHEDULED HC1 CHECK, FWD GALLEY LT BATTERY PACK FAILED LONG TEST. R&R BATTERY PACK PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 35,206 hrs · 21,147 cycles

DURING SCHEDULED HC2 CHECK, RT MID CABIN EMERGENCY BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 32,784 hrs · 19,718 cycles

DURING SCHEDULED HC1 CHECK, LT OVERWING EMERGENCY BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,758 hrs · 19,140 cycles

DURING SCHEDULED MV2 CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 31,758 hrs · 19,140 cycles

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

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 30,290 hrs · 18,330 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986.5, LBL 5. REPAIRED FLOORBEAM PER SWA EA.

Part: FITTING — CORRODED (L1 DOOR) · airframe 30,290 hrs · 18,330 cycles

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

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 30,290 hrs · 18,330 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986.5, RBL 5. REPAIRED FLOORBEAM PER SRM.

Part: LENS — CRACKED (EXTERIOR) · airframe 30,290 hrs · 18,330 cycles

DURING SCHEDULED 8Y CHECK, FOUND LEFT OVERWING EMERGENCY EXIT EXTERIOR LIGHT LENS CRACKED. REMOVED AND REPLACED LIGHT LENS PER MM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 30,290 hrs · 18,330 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CRACKED AT BS 947, LBL 15. REPAIRED FLOORBEAM PER SWA EA.

Part: FLOORBEAM — CORRODED (BS 967) · airframe 30,290 hrs · 18,330 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 967, LBL 5 TO RBL 28. REPAIRED FLOORBEAM PER SWA EA.

Part: FLOORBEAM — CORRODED (BS 967) · airframe 30,290 hrs · 18,330 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 967, LBL 41. REPAIRED FLOORBEAM PER SRM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 27,295 hrs · 16,569 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,781 hrs · 16,292 cycles

DURING SCHEDULED MV2 CHECK, FOUND EMERGENCY EXIT BULLNOSE LIGHT INOP AT ROW 19 ABC. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 26,480 hrs · 16,112 cycles

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

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 26,193 hrs · 15,957 cycles

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

Part: WINDOW — CRACKED (COCKPIT) · airframe 25,681 hrs · 15,672 cycles

AIR TURNBACK/DECLARED EMERGENCY, L5 COCKPIT WINDOW CRACKED AND SEPARATED FROM AIRCRAFT. REMOVED AND REPLACED R L5 COCKPIT WINDOW PER MM.

Part: STRIP — WORN (CABIN) · airframe 23,336 hrs · 14,321 cycles

DURING SCHEDULED MV2 CHECK, FOUND EEPLS STRIPS WORN AT ROWS 1 DEF & 3 DEF. REMOVED AND REPLACED EEPLS STRIPS PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 22,303 hrs · 13,744 cycles

DURING SCHEDULED RON FOUND R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM.

Part: BLADE — FOD (NR 2 ENGINE) · airframe 22,178 hrs · 13,672 cycles

AIR TURNBACK, DURING CLIMBOUT NOTICED A CONTINUOUS VIBRATION ON AIRCRAFT AND NR 2 ENGINE, VIBRATION METER AT 3 3/4. REDUCED POWER AND VIBRATION DECREASED. REMOVED AND REPLACED NR 2 ENGINE FAN BLADES NR 21 AND NR 9, PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,605 hrs · 13,333 cycles

AFT GALLEY OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED EMERGENCY EXIT OVERHEAD LIGHT PER MM.

Part: SKIN — CRACKED (RT WING FOREFLAP) · airframe 20,937 hrs · 12,963 cycles

DURING SCHEDULED HC2 CHECK, FOUND RT WING OUTBOARD FOREFLAP L/E, CRACKED. REPAIRED L/E FOREFLAP PER EA.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 20,937 hrs · 12,963 cycles

DURING SCHEDULED HC2 CHECK, FOUND EMERGENCY EXIT LIGHTS INOP AT FWD GALLEY, ROW 11 DEF, AND ROW 16 ABC. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERIES PER MM.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 20,488 hrs · 12,731 cycles

FWD ENTRY DOOR MISSING EMERGENCY LIGHT LENS COVER. INSTALLED LIGHT LENS COVER PER MM.

Part: LINE — CRACKED (NR 2 SPOILER) · airframe 18,615 hrs · 11,692 cycles

DECLARED EMERGENCY, ENGINE NR 1 'A' HYD LOW PRESS LIGHT ILLUMINATED, 'A' SYSTEM LEVEL DROPPED TO ZERO. FOUND, HOLE IN HYD DOWN LINE AT NR 3 SPOILER AUTUATOR. REMOVED AND REPLACED HYD LINE PER MM.

Part: COVER — CRACKED (CABIN) · airframe 15,473 hrs · 9,877 cycles

EEPLS COVER CRACKED AT ROW NR 1. REMOVED AND REPLACED EEPLS COVER PER MM.

Part: SLIDE — OUT OF ADJUST (AFT ENTRY DOOR) · airframe 14,572 hrs · 9,370 cycles

AFT ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: FITTING — WORN (LT ELEVATOR) · airframe 14,532 hrs · 9,345 cycles

DURING SCHEDULED PM CHECK, SWA SI 11038-55, FOUND LT ELEVATOR TAB NR 1, NR 2 AND NR 3 ATTACH LUGS WORN. REMOVED AND REPLACED LEFT ELEVATOR ATTACH LUGS PER MM.

Part: FITTING — WORN (RT ELEVATOR) · airframe 14,532 hrs · 9,345 cycles

DURING SCHEDULED PM CHECK, SWA SI 11038-55, FOUND RT ELEVATOR TAB NR 2, NR 3 AND NR 4 ATTACH LUGS WORN. REMOVED AND REPLACED RT ELEVATOR TAB ATTACH LUGS PER SWA EA

Part: SLIDE — LOOSE (FWD ENTRY DOOR) · airframe 11,467 hrs · 7,558 cycles

FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT BAR LOOSE. SECURED GIRT BAR PER MM.

Part: RIB — CRACKED (LT KRUEGER FLAP) · airframe 9,052 hrs · 6,105 cycles

DURING SCHEDULED C1 CHECK, FOUND LT WING L/E OUTBD KRUEGER FLAP RIB CRACKED AT THIRD RIB FROM OUTBD END. REMOVED AND REPLACED KRUEGER FLAP PER MM.

Part: SLIDE — LOOSE (SERVICE DOOR) · airframe 6,947 hrs · 4,848 cycles

WHILE PROVISIONING FOUND FWD SERVICE DOOR EVACUATION SLIDE FALLING OUT OF CONTAINER. REINSTALLED SLIDE ASSY PER MM.

Part: SEAL — LEAKING (PAX DOOR) · airframe 6,067 hrs · 4,381 cycles

DIVERSION- CABIN WOULD NOT PRESSURIZE AFTER TAKEOFF. FWD ENTRY DOOR HAS LARGE PRESS LEAK. DIVERTED TO PHX. INSPECTED FWD ENTRY DOOR SEALS AND ASSOCIATED FRAME AREAS, C/W PRESS LEAK CHECK. NO DEFECTS NOTED PER MM.

Part: SLIDE — DISLODGED (PAX DOOR) · airframe 5,862 hrs · 4,257 cycles

FWD ENTRY DOOR EVACUATION SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE ASSY PER MM.

Part: SLIDES — SAGGING (DOORS)

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

Part: HINGE — CRACKED (ELEV TAB)

DURING SCHEDULED SPECIAL CHECK, FOUND RT ELEVATOR TAB MAST FITTING HAS A .125 INCH LONG CRACK ON UPPER OUTBD FLANGE RADIUS. REMOVED AND REPLACED RT ELEVATOR TAB ASSY.

Part: LIGHT — LOOSE (COCKPIT)

ELECTRIC LOW PRESSURE CHECK LIGHT ILLUMINATED IN FLIGHT AND WOULD NOT GO OUT. RETURNED TO MDW. TIGHTENED CORY LIGHT BASE, OPS CK OK PER MM.