N719SW

Part: HMU — FAULTY (NR 1 ENGINE) · airframe 74,516 hrs · 44,532 cycles

SUPPLEMENTAL INFORMATION, UPON SETTING TAKEOFF THRUST, NR 2 THRUST LEVER AT 89% N1, NR 1 THRUST LEVER GOT TO 84% N1 WITH THRUST LEVER MATCHED. PUSHED NR 1 THRUST LEVER UP TO APPROXIMATELY 86% N1, N1 DROPPED TO 83-84%, ABOVE 1000, NR 2 THRUST LEVER AT 94% N1, NR 1 THRUST LEVER PUSHED UP TO AS FAR AS 90% N1, NR 1 THRUST LEVER FIVE TO SIX THRUST LEVER KNOBS WIDTH SPLIT WITH NR 2. ABOVE 1000, THRUST LEVER SPLIT DECREASED TO 3 KNOBS WIDTH. CLIMB OUT ABOVE FL230, THRUST LEVER MATCHED, N1'S MATCHED. ALL NORMAL IN CRUISE. DESCENT APP AND LANDING. NO AUTO THROTTLES THROUGHOUT. NO EGT EXCEEDANCES. R&R NR 1 ENGINE HYDRO MECHANICAL UNIT PER MT.

Part: BATTERY — FAILED (CABIN) · airframe 73,515 hrs · 43,906 cycles

EMERGENCY LIGHT BATTERY FWD OF RT OVERWING EXIT FAILED CAPACITY CHECK. R&R EMERGENCY LIGHT BATTERY FWD OF RT OVERWING EXIT PER AMM 33-51-06.

Part: COVER — UNSECURE (EXIT SIGN) · airframe 71,342 hrs · 42,546 cycles

EMERGENCY EXIT SIGN COVER FELL OFF. ADJUSTED COVER PER SIP.

Part: BRACKET — LOOSE (R2 DOOR) · airframe 71,146 hrs · 42,409 cycles

R2 DOOR EVAC SLIDE GIRT BAR CLIP BRACKET LOOSE. SECURED BRACKET PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 71,146 hrs · 42,409 cycles

R1 DOOR EVAC SLIDE OUT OF ADJUST. REINSTALLED SLIDE ASSY PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 71,009 hrs · 42,319 cycles

R1 DOOR EVAC SLIDE OUT OF ADJUST. REINSTALLED SLIDE ASSY PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 70,535 hrs · 42,012 cycles

RT OVERWING DOOR EXIT LIGHT INOP. R&R LIGHT PER AMM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 70,345 hrs · 41,899 cycles

R1 DOOR SLIDE GAUGE OUT OF ADJUST. ADJUSTED SLIDE IAW MT.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 69,510 hrs · 41,334 cycles

LT OVERHEAD BIN EMERGENCY LIGHT INOP AT ROW 7. RECONNECTED CONNECTOR IAW WDM & AMM.

Part: POWER SUPPLY — FAILED (CABIN) · airframe 69,510 hrs · 41,334 cycles

EMERGENCY LIGHTS BATTERY FAILED TEST AT LOCATION M1675. R&R POWER SUPPLY IAW AMM.

Part: SIGN — DISCONNECTED (CABIN) · airframe 69,510 hrs · 41,334 cycles

R2 DOOR OVERHEAD EMERGENCY EXIT SIGN INOP. RECONNECTED SIGN PER AMM AND WDM.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 69,510 hrs · 41,334 cycles

BULKHEAD STIFFENER CRACKED AT BS 178, RBL 25. R&R STIFFENER IAW SRM & EA.

Part: PANEL — DAMAGED (E&E BAY) · airframe 69,510 hrs · 41,334 cycles

ELECTRONICS AND EQUIPMENT COMPARTMENT FLOOR PANEL COVER J-23 JUNCTION BOX DAMAGED ON FORWARD INBOARD CORNER. REPAIRED PANEL PER SRM AND DWG.

Part: BAFFLE — CRACKED (FUSELAGE) · airframe 69,510 hrs · 41,334 cycles

FORWARD CARGO BAFFLE CRACKED BETWEEN BS 400 TO BS 420, LBL 24. R&R BAFFLE IAW SRM & DWG.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 69,510 hrs · 41,334 cycles

FORWARD CARGO BAFFLE ATTACH CLIP CRACKED AT BS 400, LBL 24. R&R CLIP IAW SRM AND DWG.

Part: BAFFLE — CRACKED (FUSELAGE) · airframe 69,510 hrs · 41,334 cycles

FORWARD CARGO BAFFLE CRACKED BETWEEN BS 460 TO BS 480, LBL 24. R&R BAFFLE IAW DWG & SRM.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 69,510 hrs · 41,334 cycles

LT HORIZONTAL STABILIZER TRANS NR 2 RIB CRACKED AT STA 120.3. REPAIRED NR 2 RIB PER ER & EA.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 69,510 hrs · 41,334 cycles

AFT CARGO FLOOR SUPPORT Z-CHANNEL CORRODED BETWEEN BS 727+4 TO BS 767, RBL 24. R&R SUPPORT IAW SRM AND DWG.

Part: BAFFLE — CRACKED (FUSELAGE) · airframe 69,510 hrs · 41,334 cycles

FORWARD CARGO COMPARTMENT LT SIDE BAFFLE CRACKED BETWEEN BS 500A TO BS 500B. R&R BAFFLE IAW SRM & DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 69,510 hrs · 41,334 cycles

COCKPIT FLOOR SHEAR TIE CORRODED AT BS 224, LBL 40. R&R SHEAR TIE PER SRM AND DWG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 69,510 hrs · 41,334 cycles

RT OUTBOARD SEAT TRACK BOTTOM CORRODED BETWEEN BS 727C TO BS 727D+12, RBL 45. R&R SEAT TRACK PER SRM AND DWG.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 69,510 hrs · 41,334 cycles

GUSSET CRACKED AT BS 259.5, STR 8L. R&R GUSSET IAW SRM & DWG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 69,510 hrs · 41,334 cycles

SEAT TRACK CORRODED AT BS 874, LBL 24.5. R&R SEAT TRACK IAW SRM & DWG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 69,510 hrs · 41,334 cycles

LT OUTBOARD SEAT TRACK BOTTOM CORRODED AT BS 727B+13, LBL 45. R&R SEAT TRACK IAW SRM & DWG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 69,510 hrs · 41,334 cycles

RT OUTBOARD SEAT TRACK BOTTOM CORRODED BETWEEN BS 506 TO BS 515, RBL 45. R&R SEAT TRACK IAW SRM & DWG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 69,510 hrs · 41,334 cycles

RT OUTBOARD SEAT TRACK BOTTOM CORRODED AT BS 712, RBL 45. R&R SEAT TRACK IAW SRM & DWG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 69,510 hrs · 41,334 cycles

LT INBOARD SEAT TRACK BOTTOM CORRODED AT BS 462, LBL 24.5. R&R SEAT TRACK IAW DWG AND SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 69,510 hrs · 41,334 cycles

RT OUTBOARD SEAT TRACK BOTTOM CORRODED BETWEEN BS 380 TO BS 480, RBL 45. R&R SEAT TRACK IAW SRM AND DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 69,510 hrs · 41,334 cycles

SHEAR TIE CORRODED AT BS 667, RBL 69. R&R SHEAR TIE IAW SRM AND DWG.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 69,510 hrs · 41,334 cycles

LT MAIN WHEEL WELL HORIZONTAL PRESSURE WEB CRACKED AT BS 664, LBL 35. REPAIRED WEB IAW ER AND EA.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 69,510 hrs · 41,334 cycles

INTERCOSTAL CRACKED AT BS 304, LBL 26. R&R INTERCOSTAL PER SRM AND DWG.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 69,510 hrs · 41,334 cycles

LT HORIZONTAL STABILIZER TRANS NR 3 RIB CRACKED AT STA 120.3. REPAIRED RIB PER ER & EA.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 69,510 hrs · 41,334 cycles

RT HORIZONTAL STABILIZER TRANS RIB NR 3 CRACKED AT STAB STA 129.5. REPAIRED RIB IAW EA.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 69,510 hrs · 41,334 cycles

FORWARD CARGO LT FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 400 TO BS 500A+9.3. R&R SUPPORT IAW SRM & DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 69,510 hrs · 41,334 cycles

AFT CARGO LT FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 727 TO BS 847. REPAIRED SUPPORT IAW SRM AND DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 69,510 hrs · 41,334 cycles

FORWARD CARGO LT FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 500A+9.3 TO BS 500D. REPAIRED SUPPORT IAW SRM AND DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 69,510 hrs · 41,334 cycles

FORWARD CARGO INTERCOSTAL CRACKED BETWEEN BS 500 TO BS 500A, STR 26L. R&R BAFFLE IAW DWG & SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 69,510 hrs · 41,334 cycles

FORWARD CARGO RT FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 480+12.3 TO BS 500A. R&R SUPPORT IAW SRM AND DWG.

Part: SKIN — CORRODED (FUSELAGE) · airframe 69,510 hrs · 41,334 cycles

LT PACK AIR INLET DOOR SKIN CORRODED. REPAIRED SKIN IAW SRM AND EA.

Part: SKIN — CRACKED (LE SLAT) · airframe 69,510 hrs · 41,334 cycles

RT WING NR 7 LEADING EDGE SLAT LOWER SURFACE NOSE SKIN CRACKED AT FASTENER HOLE, FOR ACTUATOR ATTACH FITTING. REPAIRED SKIN IAW SRM.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 69,510 hrs · 41,334 cycles

L2 DOOR SLIDE GIRT FLAP OUT OF POSITION. REPOSITIONED SLIDE PER MT.

Part: FLAP TRACK — LOOSE (RT WING) · airframe 69,250 hrs · 41,168 cycles

RT WING INBOARD FLAP OUTBOARD FLAP TRACK FOUND LOOSE NR 6. R&R NR 6 FLAP TRACK PER AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 69,248 hrs · 41,167 cycles

RT OVERHEAD BIN EMERGENCY LIGHT INOP BETWEEN ROW 1 TO ROW 6. R&R BATTERY PACK PER AMM.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 69,172 hrs · 41,117 cycles

RT OVERWING EMERGENCY LIGHT INOPERATIVE. R & R THE BULB IAW AMM.

Part: ROD — BROKEN (TE FLAP) · airframe 68,834 hrs · 40,896 cycles

LT INBOARD AFT FLAP ACTUATING MECHANISM ROD BROKEN. R&R ROD IAW AMM AND EA.

Part: ROD — BROKEN (TE FLAP) · airframe 68,834 hrs · 40,896 cycles

RT WING INBOARD AFT FLAP ACTUATING MECHANISM ROD BROKEN. R&R ROD IAW AMM AND EA.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 68,827 hrs · 40,894 cycles

R1 DOOR EMERGENCY SLIDE FOUND OUT OF POSITION. REPOSITIONED THE SLIDE IAW MT.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 67,848 hrs · 40,258 cycles

R1 DOOR SLIDE OUT OF POSITON. REPOSITIONED THE SLIDE IAW MT.

Part: FLAP — DELAMINATED (LT WING) · airframe 67,735 hrs · 40,176 cycles

LT WING OUTBOARD AFT FLAP DELAMINATED AT INBOARD TRAILING EDGE. REPAIRED AFT FLAP PER SRM.

Part: SUPPORT FITTING — CORRODED (LT MLG TRUNNION) · airframe 67,285 hrs · 39,869 cycles

LT MAIN LANDING GEAR FORWARD TRUNNION LUG FACE SUPPORT FITTING CORRODED. REPAIRED FITTING PER EA.

Part: SUPPORT FITTING — CORRODED (RT MLG TRUNNION) · airframe 67,285 hrs · 39,869 cycles

RT MAIN LANDING GEAR FORWARD TRUNNION LUG FACE SUPPORT FITTING CORRODED. REPAIRED FITTING PER EA.

Part: DOOR — CRACKED (RT MLG) · airframe 67,285 hrs · 39,869 cycles

RT MAIN LANDING GEAR CENTER STRUT GEAR DOOR CRACKED. R&R DOOR PER MM.

Part: SIGN — UNSECURE (CABIN) · airframe 67,120 hrs · 39,775 cycles

RT LOWER EMERGENCY EXIT SIGN LIGHT FELL OFF. R&R LIGHT ASSEMBLY PER MM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 67,079 hrs · 39,744 cycles

R1 DOOR SLIDE OUT OF POSITION. REPOSITIONED THE SLIDE IAW MM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 66,417 hrs · 39,365 cycles

R1 DOOR SLIDE OUT OF POSITION. REPOSITIONED THE SLIDE IAW MT.

Part: LENS — LOOSE (CABIN) · airframe 66,307 hrs · 39,297 cycles

RT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER AMM.

Part: STIFFENER — BROKEN (BS 663) · airframe 65,817 hrs · 38,986 cycles

HORIZONTAL SUPPORT STIFFENER BROKEN AT BS. 663, RBL 12. R & R THE STIFFENER IAW SRM.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 65,817 hrs · 38,986 cycles

L2 DOOR SLIDE OUT OF POSITION. ADJUSTED THE SLIDE ASSY IAW MM.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 65,817 hrs · 38,986 cycles

EMERGENCY EXIT LIGHT M1673 BATTERY PACK FAILED TEST. R & R THE BATTERY PACK IAW MM.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 65,817 hrs · 38,986 cycles

EMERGENCY EXIT LIGHT M1672 BATTERY PACK FAILED TEST. R & R THE BATTERY PACK IAW MM.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 65,817 hrs · 38,986 cycles

EMERGENCY EXIT LIGHT M1675 BATTERY PACK FAILED TEST. R & R THE BATTERY PACK IAW MM.

Part: WEB — CRACKED (RT MLG WW) · airframe 65,817 hrs · 38,986 cycles

RT MAIN LANDING GEAR WHEEL WELL UPPER WEB CRACKED AT STA 663.75, RBL 43.80. REPAIRED WEB PER EA.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 65,817 hrs · 38,986 cycles

EMERGENCY EXIT LIGHT M1668 BATTERY PACK FAILED TEST. R & R THE BATTERY PACK IAW MM.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 65,817 hrs · 38,986 cycles

EMERGENCY EXIT LIGHT M1670 BATTERY PACK FAILED TEST. R & R THE BATTERY PACK IAW MM.

Part: BRACKET — CRACKED (BS 663) · airframe 65,817 hrs · 38,986 cycles

RIGHT MAIN GEAR WHEEL WELL BRACKET CRACKED AT BS 663, RBL 15.54. R & R THE BRACKET IAW SRM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 65,817 hrs · 38,986 cycles

R2 DOOR SLIDE OUT OF POSITION. ADJUSTED SLIDE ASSY IAW MM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 65,817 hrs · 38,986 cycles

R1 DOOR SLIDE OUT OF POSITION. ADJUSTED THE SLIDE ASSY IAW MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 65,785 hrs · 38,968 cycles

LEFT EMERGENCY LIGHT INOPERATIVE AT ROW 1. REPLACED THE LAMPS IAW AMM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 65,234 hrs · 38,630 cycles

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

Part: CRADLE — DAMAGED (FLASHLIGHT) · airframe 63,741 hrs · 37,770 cycles

FORWARD EMERGENCY FLASHLIGHT HOLDER IS DAMAGED. R & R HOLDER IAW SOPM.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 63,741 hrs · 37,770 cycles

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

Part: GUSSET — CRACKED (FUSELAGE) · airframe 63,741 hrs · 37,770 cycles

FORWARD BAY GUSSET CRACKED AT BS 500D, STR 19R. R & R GUSSET IAW SRM.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 63,741 hrs · 37,770 cycles

AFT CARGO BAY LOWER CHORD CORRODED BETWEEN BS 797 TO BS 803, RBL 20. REPAIRED CHORD IAW ER AND EA.

Part: WEB — CORRODED (FUSELAGE) · airframe 63,741 hrs · 37,770 cycles

AFT CARGO BAY LOWER VERTICAL WEB CORRODED BETWEEN BS 797 TO BS 807, WL 150. R & R WEB IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,741 hrs · 37,770 cycles

SKIN CORRODED AT BS 727D+10, BL0. REPAIRED SKIN IAW ER AND EA.

Part: FLOOR SUPPORT — CRACKED (BS 277-294) · airframe 63,741 hrs · 37,770 cycles

FLOOR SUPPORT CRACKED BETWEEN BS 277 TO 294, BL 0. R & R THE FLOOR SUPPORT IAW SRM.

Part: STRAP — CORRODED (FUSELAGE) · airframe 63,741 hrs · 37,770 cycles

AFT CARGO BAY FLOOR SPLICE STRAP CORRODED AT BS 772. R & R STRAP IAW SRM.

Part: SHEAR WEB — CRACKED (BS 986-1016) · airframe 63,741 hrs · 37,770 cycles

SHEAR WEB CRACKED BETWEEN BS 986 TO 1016, BETWEEN RBL 30 TO RBL 40. R & R SHEAR WEB IAW SRM.

Part: SUPPORT BEAM — CORRODED (FUSELAGE) · airframe 63,741 hrs · 37,770 cycles

GALLEY SUPPORT BEAM CORRODED AT BS 993, RBL 35. R & R BEAM IAW SRM AND ER.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 63,741 hrs · 37,770 cycles

AFT CARGO BAY FLOOR STRUCTURE T-ANGLE CORRODED AT BS 847, RBL 16. R & R T-ANGLE IAW SRM & DWG.

Part: ANGLE — CORRODED (BS 727D) · airframe 63,741 hrs · 37,770 cycles

FRAME REINFORCING ANGLE CORRODED AT BS 727D, STRINGER 25L. R & R THE ANGLE IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 63,741 hrs · 37,770 cycles

AFT CARGO BAY FLOOR STRUCTURE FLOORBEAM CORRODED BETWEEN BS 727 TO BS 727C, RBL 14. REPAIRED BEAM IAW SRM.

Part: STRINGER CLIP — CORRODED (BS 747) · airframe 63,741 hrs · 37,770 cycles

STRINGER CLIP CORRODED AT BS 747, STRINGER 26L. R & R THE STRINGER CLIP IAW SRM.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 63,741 hrs · 37,770 cycles

AFT CARGO BAY FLOOR STRUCTURE FLOORBEAM CHANNEL CORRODED AT BS 767+6, LBL 8. R & R CHANNEL IAW SRM & EA.

Part: SUPPORT — CORRODED (BS 500A-500D) · airframe 63,741 hrs · 37,770 cycles

FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 500A - 500D, RBL 24. R & R THE SUPPORT IAW SRM.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 63,741 hrs · 37,770 cycles

R1 DOOR MOP SILL INNER CHORD CORRODED BETWEEN BS 260 TO BS 360, RBL 57. R & R CHORD IAW SRM.

Part: STRINGER CLIP — CORRODED (BS 727A) · airframe 63,741 hrs · 37,770 cycles

STRINGER CLIP CORRODED AT BS 727A, STRINGER 25R. R & R THE STRINGER CLIP IAW SRM.

Part: FLOORBEAM — CRACKED (BS 328) · airframe 63,741 hrs · 37,770 cycles

FLOORBEAM UPPER TEE CRACKED AT BS 328, RBL 20. REPAIRED THE TEE IAW SRM.

Part: FLOOR SUPPORT — CORRODED (BS 727E) · airframe 63,741 hrs · 37,770 cycles

AFT CARGO BAY FLOOR SUPPORT CORRODED, AT BS 727E+16, STR. 25L. R & R THE FLOOR SUPPORT IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 63,741 hrs · 37,770 cycles

AFT CARGO BAY FLOOR STRUCTURE FLOORBEAM CORRODED BETWEEN BS 757 TO BS 857, RBL 14. REPAIR FLOORBEAM IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 63,741 hrs · 37,770 cycles

AFT CARGO BAY FLOOR STRUCTURE FLOORBEAM CORRODED AT BS 727D+6, LBL 3. R & R CHANNEL SRM & EA.

Part: CAP — CORRODED (FUSELAGE) · airframe 63,741 hrs · 37,770 cycles

AFT CARGO BAY FLOOR STRUCTURE FRAME SPLICE CAP CORRODED AT BS 787, STR 25R. R & R SPLICE CAP IAW SRM & DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 63,741 hrs · 37,770 cycles

AFT CARGO BAY FLOOR STRUCTURE FLOORBEAM CORRODED AT BS 727D+6, LBL 8. R & R CHANNEL IAW SRM & EA.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 63,741 hrs · 37,770 cycles

L1 DOOR THRESHOLD SUPPORT Z-ANGLE CORRODED AT BS 320, LBL 63. R & R Z-ANGLE IAW SRM AND DWG.

Part: SUPPORT — CORRODED (BS 727-847) · airframe 63,741 hrs · 37,770 cycles

AFT CARGO BAY FLOOR STRUCTURE FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 727 - 847, LBL 21. REPAIRED THE SUPPORT IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 63,741 hrs · 37,770 cycles

AFT CARGO BAY FLOOR STRUCTURE FLOORBEAM CORRODED AT BS 767+6, RBL 8. R & R FLOORBEAM IAW EA.

Part: SUPPORT ANGLE — CORRODED (BS 312-328) · airframe 63,741 hrs · 37,770 cycles

R1 DOOR MOPSILL THRESHOLD SUPPORT ANGLE CORRODED BETWEEN BS 312 - 328, RBL 57. REMOVED AND REPLACED THE SUPPORAT ANGLE IAW SRM AND DWG.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 63,741 hrs · 37,770 cycles

AFT CARGO BAY FLOOR STRUCTURE WASTE TANK COMPARTMENT BULKHEAD LOWER SUPPORT ANGLE CORRODED AT BS 847, LBL 18. R & R ANGLE IAW SRM.

Part: STRINGER CLIP — CORRODED (BS 747) · airframe 63,741 hrs · 37,770 cycles

STRINGER CLIP CORRODED AT BS 747, STRINGER 25L. R & R THE STRINGER CLIP IAW SRM.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 63,741 hrs · 37,770 cycles

AFT CARGO BAY FLOOR STRUCTURE FLOORBEAM CHANNEL CORRODED AT BS 767+6, LBL 12. R & R CHANNEL IAW SRM & EA.

Part: SHIELD — CORRODED (BS 767-787) · airframe 63,741 hrs · 37,770 cycles

AFT CARGO BAY FLOOR STRUCTURE SHIELD CORRODED BETWEEN BS 767 - 787, RBL 21. R & R THE SHIELD IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 63,741 hrs · 37,770 cycles

AFT CARGO BAY FLOOR STRUCTURE FLOORBEAM CORRODED BETWEEN BS 727 TO BS 727C, LBL 17. REPAIRED BEAM IAW SRM.

Part: STRINGER CLIP — CORRODED (BS 727E) · airframe 63,741 hrs · 37,770 cycles

STRINGER CLIP CORRODED AT BS 727E, STRINGER 26R. R & R STRINGER CLIP IAW SRM & DWG.

Part: WEB — CORRODED (FUSELAGE) · airframe 63,741 hrs · 37,770 cycles

AFT CARGO BAY FLOOR STRUCTURE WEB CORRODED BETWEEN BS 767 TO BS 787, RBL 6. R & R WEB ASSEMBLY IAW SRM.

Part: SHIELD — CORRODED (BS 492-500A) · airframe 63,741 hrs · 37,770 cycles

FLOOR SHIELD CORRODED BETWEEN BS 492 TO 500A, RBL 24. R & R SHIELD IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 63,741 hrs · 37,770 cycles

AFT CARGO BAY FLOOR STRUCTURE FLOORBEAM CORRODED AT BS 767+6, RBL 3. R & R FLOORBEAM IAW SRM.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 63,741 hrs · 37,770 cycles

AFT CARGO BAY FLOOR STRUCTURE FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 867 TO BS 887, RBL 21. R & R ANGLE IAW SRM.

Part: SHEAR WEB — CORRODED (BS 1016-1023) · airframe 63,741 hrs · 37,770 cycles

SHEAR WEB CORRODED BETWEEN BS 1016 - 1023, LBL 7. R & R THE SHEAR WEB IAW SRM.

Part: STRINGER CLIP — CORRODED (BS 727B) · airframe 63,741 hrs · 37,770 cycles

STRINGER CLIP CORRODED AT BS 727B, STRINGER 25L. R & R THE STRINGER CLIP IAW SRM & DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 63,741 hrs · 37,770 cycles

AFT CARGO BAY FLOOR STRUCTURE FLOORBEAM CHANNEL CORRODED AT BS 727D+6, RBL 8. R & R CHANNEL IAW SRM & EA.

Part: WEB — CORRODED (FUSELAGE) · airframe 63,741 hrs · 37,770 cycles

FORWARD CARGO BAY THRESHOLD SUPPORT WEB CORRODED AT BS 460+10, RBL 28. R & R WEB IAW DWG AND SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 63,741 hrs · 37,770 cycles

AFT CARGO BAY FLOOR STRUCTURE WEB CORRODED BETWEEN BS 727A TO BS 727B, LBL 21. R & R WEB IAW SRM AND DWG.

Part: SUPPORT — CORRODED (BS 500B-500D) · airframe 63,741 hrs · 37,770 cycles

FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 500B TO 500D, LBL 24. R & R THE SUPPORT IAW SRM.

Part: STRAP — CORRODED (FUSELAGE) · airframe 63,741 hrs · 37,770 cycles

AFT CARGO BAY FLOOR STRUCTURE DOORWAY, LOWER THRESHOLD INNER STRAP CORRODED BETWEEN BS 767 TO BS 847, RBL 17. R & R STRAP IAW SRM.

Part: SUPPORT — BROKEN (FUSELAGE) · airframe 63,741 hrs · 37,770 cycles

AFT BULKHEAD LOWER PANEL SUPPORT BROKEN AT BS 947, RBL 19. R & R SUPPORT IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 63,741 hrs · 37,770 cycles

AFT CARGO BAY FLOOR STRUCTURE FLOORBEAM CORRODED AT BS 727D+6, LBL 12. R & R CHANNEL IAW SRM & EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 63,741 hrs · 37,770 cycles

AFT CARGO BAY FLOOR STRUCTURE FLOORBEAM CORRODED AT BS 727D+6, RBL 14. REPAIRED BEAM IAW SRM.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 63,741 hrs · 37,770 cycles

UPPER CHORD CORRODED AT BS 986, BETWEEN RBL 43 TO LBL 50. REPAIRED CHORD IAW ER AND EA.

Part: STRINGER CLIP — CORRODED (BS 767) · airframe 63,741 hrs · 37,770 cycles

STRINGER CLIP CORRODED AT BS 767, STRINGER 25L. R & R THE STRINGER CLIP IAW SRM.

Part: STRINGER CLIP — CORRODED (BS 727A) · airframe 63,741 hrs · 37,770 cycles

STRINGER CLIP CORRODED AT BS 727A, STRINGER 25L. R & R THE STRINGER CLIP IAW SRM & DWG.

Part: FLOOR SUPPORT — CRACKED (BS 344-360) · airframe 63,741 hrs · 37,770 cycles

FLOOR SUPPORT CRACKED BETWEEN BS 344 TO 360, BL 0. R & R THE FLOOR SUPPORT IAW SRM.

Part: STRINGER CLIP — CORRODED (BS 727D) · airframe 63,741 hrs · 37,770 cycles

STRINGER CLIP CORRODED AT BS 727D, STRINGER 26R. R & R THE STRINGER CLIP IAW SRM & DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 63,741 hrs · 37,770 cycles

AFT CARGO BAY FLOOR STRUCTURE, FLOORBEAM CORRODED AT BS 727D+6, LBL 17. REPAIRED BEAM IAW SRM.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 63,741 hrs · 37,770 cycles

INTERCOSTAL CORRODED AT BS 950, RBL 55. R & R INTERCOSTAL IAW SRM AND DWG.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 63,741 hrs · 37,770 cycles

AFT CARGO BAY FLOOR STRUCTURE FLOORBEAM CHANNEL CORRODED AT BS 767+6, LBL 3. R & R CHANNEL IAW ER & EA.

Part: WEB — CORRODED (BS 727A-727B) · airframe 63,741 hrs · 37,770 cycles

AFT CARGO BAY FLOOR SUPPORT WEB CORRODED BETWEEN BS 727A - 727B, LBL 17. R & R WEB IAW DWG & SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 63,741 hrs · 37,770 cycles

AFT CARGO BAY FLOOR STRUCTURE FLOORBEAM CORRODED AT BS 727D+6, RBL 3. R & R CHANNEL IAW SRM & EA.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 63,741 hrs · 37,770 cycles

FRAME REINFORCING ANGLE CORRODED AT BS 727D, STR 25R. R & R ANGLE IAW SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 63,741 hrs · 37,770 cycles

AFT CARGO BAY FLOOR STRUCTURE FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 727 TO BS 767, RBL 21. R & R SUPPORT IAW SRM.

Part: WEB — CORRODED (BS 794-847) · airframe 63,741 hrs · 37,770 cycles

AFT CARGO BAY FLOOR STRUCTURE, DOORWAY LOWER THRESHOLD WEB CORRODED BETWEEN BS 794 - 847, BETWEEN RBL 20 - 28. R & R THE WEB IAW SRM AND DWG.

Part: STRAP — CORRODED (BS 1012) · airframe 63,741 hrs · 37,770 cycles

STRAP CORRODED AT BS 1012, RBL 3. R & R THE STRAP IAW SRM.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 63,741 hrs · 37,770 cycles

FORWARD CARGO BAY AFT LOWER BULKHEAD SUPPORT ANGLE CORRODED AT BS 500D, BETWEEN RBL 24 TO LBL 24. R & R ANGLE IAW SRM AND DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 63,741 hrs · 37,770 cycles

FLOORBEAM CORRODED, BETWEEN BS 927 TO BS 947, RBL 14. R & R FLOORBEAM IAW SRM.

Part: FRAME — CRACKED (BS 727) · airframe 63,741 hrs · 37,770 cycles

FRAME CRACKED AT BS 727, WL 200. REPAIRED THE FRAME IAW EA.

Part: TRACK — CORRODED (FUSELAGE) · airframe 63,741 hrs · 37,770 cycles

AFT CARGO BAY FLOOR TRACK CORRODED AT BS 945, LBL 3. R & R FLOOR TRACK IAW SRM.

Part: ANGLE — CRACKED (LT WING) · airframe 63,741 hrs · 37,770 cycles

LEFT WING TRAILING EDGE COVE SEAL RETAINING ANGLE CRACKED ABOVE NR 1 PYLON AFT TIP. R & R THE ANGLE IAW SRM.

Part: ATTACH ANGLE — CRACKED (LT WING) · airframe 63,741 hrs · 37,770 cycles

LT WING TRANSVERSE WEB TO MAIN FLAP PROGRAM ROLLER SUPPORT ARM ATTACH ANGLE CRACKED. R & R THE ATTACH ANGLE IAW SRM AND DWG.

Part: SKIN — CRACKED (RT WING SLAT) · airframe 63,741 hrs · 37,770 cycles

RIGHT WING HR 8 SLAT LEADING EDGE BULLNOSE SKIN CRACKED AT ACTUATOR ATTACH POINT. REPAIRED THE SKIN IAW SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 63,741 hrs · 37,770 cycles

RT WING NR 5 SLAT L/E BULLNOSE SKIN CRACKED AT ACTUATOR ATTACH POINT. REPAIRED SKIN IAW SRM.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 62,473 hrs · 37,013 cycles

LIGHT OVERWING EXIT SIGN SIDEWALL LIGHT INOPERATIVE. INSTALLED LIGHT IAW AMM.

Part: LENS — MISSING (CABIN) · airframe 62,227 hrs · 36,867 cycles

LEFT OVERWING, LOWER EMER EXIT LIGHT LENS MISSING. RELAMPED LIGHT ASSEMBLY IAW SIP.

Part: BATTERY PACK — FAILED (CABIN) · airframe 61,844 hrs · 36,632 cycles

EMERGENCY LIGHTING BATTERY PACK AT M01669 FAILED CAPACITY TEST. R & R BATTERY PACK IAW AMM.

Part: CIRCUIT CARD — FAULTY (NLG WW) · airframe 61,748 hrs · 36,580 cycles

AIR TURN BACK, NOSE GEAR WOULD NOT RETRACT AFTER TAKEOFF. R & R NOSE RETRACT PRESS FUSE CARD IAW AMM.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 59,964 hrs · 35,545 cycles

OVERWING EXIT SIGN INOPERATIVE. SECURED EMER LIGHT ASSEMBLY IAW MM.

Part: LATCH — DIRTY (R2 DOOR) · airframe 58,507 hrs · 34,711 cycles

R2 DOOR EMER EVAC SLIDE GIRT BAR FLOOR LATCH DIRTY. CLEANED LATCH IAW MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 57,487 hrs · 34,103 cycles

MID CABIN EMER LIGHT BATTERY PACK FAILED CAPACITY TEST. R & R BATTERY PACK IAW AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 57,487 hrs · 34,103 cycles

FORWARD ENTRY EMER LIGHT BATTERY PACK FAILED CAPACITY TEST. R & R BATTERY PACK IAW AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 57,487 hrs · 34,103 cycles

CEILING AFT ENTRY EMER LIGHT BATTERY PACK FAILED CAPACITY TEST. R & R BATTERY PACK IAW AMM.

Part: LENS — BROKEN (EXIT SIGN) · airframe 57,344 hrs · 34,024 cycles

R2 DOOR EMER EXIT SIGN LENS BROKEN. R & R SIGN ASSEMBLY IAW AMM.

Part: PRESSURE PANEL — CRACKED (MLG WW) · airframe 56,994 hrs · 33,809 cycles

VERTICAL PRESS WEB CRACKED AT BS 663. REPAIRED WEB IAW SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 56,994 hrs · 33,809 cycles

C2 DOOR CUT OUT SKIN EXTERNAL SURFACE CORRODED AT AFT LOWER CORNER. REPAIRED SKIN IAW SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 56,994 hrs · 33,809 cycles

C2 DOOR CUT OUT SKIN EXTERNAL SURFACE CORRODED AT FWD LOWER CORNER. REPAIRED SKIN IAW SRM.

Part: BULKHEAD — CRACKED (LT MLG WW) · airframe 56,994 hrs · 33,809 cycles

MLG PRESS BULKHEAD WEB CRACKED AT STATION 663, BETWEEN LBL 25 & 45. REPAIRED WEB IAW EA.

Part: SKIN — CRACKED (LE SLAT) · airframe 56,994 hrs · 33,809 cycles

RIGHT WING NR 6 SLAT NOSE SKIN CRACKED. REPAIRED SKIN IAW SRM.

Part: SIGN — MISSING (CABIN) · airframe 55,628 hrs · 33,012 cycles

RT EMERGENCY EXIT SIGN MISSING AT ROW 12. INSTALLED SIGN IAW MM.

Part: ACTUATOR — LEAKING (NR 1 SPOILER) · airframe 55,397 hrs · 32,867 cycles

HYD A SYS FAILURE. BOTH PUMPS LOW PRESSURE LIGHTS CAME ON & FLUID DRIPPING FROM APPROXIMATELY UNDER NR 2 SPOILER. R & R NR 1 GND SPOILER ACTUATOR IAW MM.

Part: SIGN — LOOSE (CABIN) · airframe 55,342 hrs · 32,837 cycles

OVERHEAD EMERGENCY EXIT SIGN OVERWING LOOSE. R & R SIGN ASSEMBLY IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 54,386 hrs · 3,227 cycles

RT EMERGENCY EVAC SLIDE LIGHT INOPERATIVE. RELAMPED LIGHT IAW AMM.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 54,231 hrs · 32,175 cycles

RT HORIZONTAL STABILIZER AT RIB STATION 92.7 - 11.750 BACK FROM FRONT SPAR CRACKED. REPAIRED RIB IAW EA.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 54,231 hrs · 32,175 cycles

RT NR 1 WINDOW FRAME ASSEMBLY CRACKED UPPER AFT CORNER. R&R FRAME IAW ACO.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 54,231 hrs · 32,175 cycles

RT HORIZONTAL STABILIZER AT RIB 92.7-20.750 BACK FROM FRONT SPAR CRACKED. REPAIRED RIB IAW EA.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 54,231 hrs · 32,175 cycles

LT NR 1 WINDOW FRAME ASSEMBLY CRACKED AT UPPER AFT CORNER. R&R FRAME IAW ACO.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 54,231 hrs · 32,175 cycles

LT NR 1 WINDOW FRAME CRACKED AT FASTENER HOLE. R&R FRAME IAW ACO.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 54,231 hrs · 32,175 cycles

RT NR 3 FLIGHT DECK WINDOW FRAME SECOND FASTENER HOLE FROM THE BOTTOM ALONG THE E-F POST CRACKED. R&R FRAME IAW SRM & DRAWING.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 54,231 hrs · 32,175 cycles

LT NR 3 WINDOW FRAME CRACKED AT THE SECOND LOWER CORNER FASTENER HOLE. R&R FRAME IAW SRM & DRAWING.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,231 hrs · 32,175 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,231 hrs · 32,175 cycles

FRAME CRACKED AT STATION 867, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,231 hrs · 32,175 cycles

FRAME CRACKED AT STATION 867, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,231 hrs · 32,175 cycles

FRAME CRACKED AT STATION 907, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,231 hrs · 32,175 cycles

FRAME CRACKED AT STATION 480, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,231 hrs · 32,175 cycles

FRAME CRACKED AT STATION 787, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,231 hrs · 32,175 cycles

FRAME CRACKED AT STATION 727D, STRINGER 8L. REPAIRED FRAME IAW EA 7 SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,231 hrs · 32,175 cycles

FRAME CRACKED AT STATION 827, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: STIFFENER — CRACKED (LT HORIZ STAB) · airframe 54,231 hrs · 32,175 cycles

LT HORIZONTAL STABILIZER STATION 92.70 RIB CRACKED IN VERTICAL STIFFENER & WEB 11 5/8" FROM FRONT SPAR & 1" FROM BOTTOM FLANGE. REPAIRED STIFFENER IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,231 hrs · 32,175 cycles

FRAME CRACKED AT STATION 747, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,231 hrs · 32,175 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,231 hrs · 32,175 cycles

STRINGER CLIP CRACKED AT STATION 360, STRINGER 8R. R&R CLIP IAW SRM & DRAWING.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,231 hrs · 32,175 cycles

FRAME CRACKED AT STATION 907, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 54,231 hrs · 32,175 cycles

LT HORIZONTAL STABILIZER STATION 92.70 VERTICAL RIB WEB CRACKED. REPAIRED WEB IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,231 hrs · 32,175 cycles

FRAME CRACKED AT STATION 440, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,231 hrs · 32,175 cycles

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

Part: STIFFENER — CRACKED (LT HORIZ STAB) · airframe 54,231 hrs · 32,175 cycles

LT HORIZONTAL STABILIZER STATION 92.70 VERTICAL RIB STIFFENER CRACKED. REPAIRED STIFFENER IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,231 hrs · 32,175 cycles

FRAME CRACKED AT STATION 480, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 54,231 hrs · 32,175 cycles

R1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW SWA MT.

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 53,608 hrs · 31,787 cycles

RIGHT MLG WHEEL WELL FORWARD VERTICAL PRESSURE WEB CRACKED AT BS 663.75, RBL 35. REPAIRED WEB IAW EA.

Part: SKATE ANGLE — CRACKED (VERTICAL STAB) · airframe 53,608 hrs · 31,787 cycles

RIGHT SIDE OF VERTICAL STAB SKATE ANGLE CRACKED. REPAIRED ANGLE IAW EA.

Part: POST — CRACKED (FUSELAGE) · airframe 53,608 hrs · 31,787 cycles

L1 WINDOW C/D POST CRACKED AT UPPER END. REPAIRED POST IAW EA.

Part: PRESSURE PANEL — CRACKED (RH MLG WW) · airframe 53,608 hrs · 31,787 cycles

RIGHT MLG WHEEL WELL FORWARD VERTICAL PRESSURE WEB CRACKED AT BS 663.75, RBL 40. REPAIRED WEB IAW EA.

Part: SIGN — LOOSE (EMERGENCY LIGHTS) · airframe 50,080 hrs · 29,598 cycles

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

Part: SKIN — CRACKED (HORIZ STAB) · airframe 49,207 hrs · 29,114 cycles

RT HORIZONTAL STABILIZER LOWER INSPAR SKIN CRACKED. REPAIRED SKIN PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 43,956 hrs · 26,015 cycles

DURING SCHEDULED 12Y CHECK, FOUND RT CREASE BEAM CORRODED BETWEEN BS 951 TO BS 992. REPAIRED BEAM PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 43,956 hrs · 26,015 cycles

DURING SCHEDULED 12Y CHECK, FOUND FLOORBEAM CORRODED AT BS 987, RBL 46. REPAIRED BEAM PER SRM.

Part: SIGN — CRACKED (CABIN) · airframe 43,956 hrs · 26,015 cycles

DURING SCHEDULED 12Y CHECK, FOUND FWD EMERGENCY EXIT SIGN CRACKED. REMOVED AND REPLACED SIGN PER MM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 43,956 hrs · 26,015 cycles

DURING SCHEDULED 12Y CHECK, FOUND RT CREASE BEAM CORRODED AT BS 986.5. REMOVED AND REPLACED WEB PER SRM AND BAC DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,956 hrs · 26,015 cycles

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

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 43,956 hrs · 26,015 cycles

DURING SCHEDULED 12Y CHECK, FOUND FLOORBEAM WEB CORRODED AT BS 1010, RBL 44. REPAIRED BEAM PER SRM AND BAC DWG.

Part: SIGN — DIRTY (CABIN) · airframe 43,956 hrs · 26,015 cycles

DURING SCHEDULED 12Y CHECK, FOUND R1 DOOR OVERHEAD EMERGENCY EXIT SIGN SOILED. CLEANED SIGN PER MM.

Part: SIGN — DIRTY (CABIN) · airframe 43,956 hrs · 26,015 cycles

DURING SCHEDULED 12Y CHECK, FOUND R2 DOOR OVERHEAD EMERGENCY EXIT SIGN SOILED. CLEANED SIGN PER MM.

Part: SIGN — CRACKED (CABIN) · airframe 43,956 hrs · 26,015 cycles

DURING SCHEDULED 12Y CHECK, FOUND AFT GALLEY EMERGENCY EXIT SIGN CRACKED. REMOVED AND REPLACED SIGN PER MM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 43,956 hrs · 26,015 cycles

DURING SCHEDULED 12Y CHECK, FOUND R1 DOOR CREASE BEAM CORRODED. REMOVED AND REPLACED BEAM PER SRM.

Part: LENS — MISSING (CABIN) · airframe 43,956 hrs · 26,015 cycles

DURING SCHEDULED 12Y CHECK, FOUND RT EMERGENCY EXIT LIGHT LENS MISSING AT ROW 13. INSTALLED LENS PER MM.

Part: FLAP — DELAMINATED (LT WING) · airframe 43,956 hrs · 26,015 cycles

DURING SCHEDULED 12Y CHECK, FOUND LT WING O/B AFT FLAP TRAILING EDGE I/B CORNER DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 43,956 hrs · 26,015 cycles

DURING SCHEDULED 12Y CHECK, FOUND AFT GALLEY OVERHEAD EMERGENCY EXIT SIGN LAMP INOP. RELAMPED PER MM.

Part: FLAP — DELAMINATED (RT WING) · airframe 43,956 hrs · 26,015 cycles

DURING SCHEDULED 12Y CHECK, FOUND RT WING O/B AFT FLAP CORNER DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.

Part: SIGN — DIRTY (CABIN) · airframe 43,956 hrs · 26,015 cycles

DURING SCHEDULED 12Y CHECK, FOUND L1 DOOR OVERHEAD EMERGENCY EXIT SIGN SOILED. CLEANED SIGN PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 43,956 hrs · 26,015 cycles

DURING SCHEDULED 12Y CHECK, FOUND LT MID CABIN EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SIGN — DIRTY (CABIN) · airframe 43,956 hrs · 26,015 cycles

DURING SCHEDULED 12Y CHECK, FOUND L2 DOOR OVERHEAD EMERGENCY EXIT SIGN SOILED. CLEANED SIGN PER MM.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · airframe 43,956 hrs · 26,015 cycles

DURING SCHEDULED 12Y CHECK, FOUND L1 DOOR CREASE BEAM ATTACH ANGLE CORRODED. REMOVED AND REPLACED ANGLE PER SRM.

Part: SLIDE — LOW PRESSURE (L2 DOOR) · airframe 43,956 hrs · 26,015 cycles

DURING SCHEDULED 12Y CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE PRESSURE LOW. REMOVED AND REPLACED SLIDE PER MM.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · airframe 43,956 hrs · 26,015 cycles

DURING SCHEDULED 12Y CHECK, FOUND R1 DOOR CREASE BEAM ATTACH ANGLE CORRODED. REMOVED AND REPLACED ANGLE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,956 hrs · 26,015 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 747, STR 8R. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,956 hrs · 26,015 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 400, STR 8R. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,956 hrs · 26,015 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 787, STR 8L. REPAIRED FRAME PER EA.

Part: FITTING — CORRODED (BIRT BAR) · airframe 43,956 hrs · 26,015 cycles

DURING SCHEDULED 12Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING CORRODED. REMOVED AND REPLACED FITTING PER SRM.

Part: FITTING — CORRODED (GIRT BAR) · airframe 43,956 hrs · 26,015 cycles

DURING SCHEDULED 12Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING CORRODED. REMOVED AND REPLACED FITTING PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 43,956 hrs · 26,015 cycles

DURING SCHEDULED 12Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 26R. REMOVED AND REPLACED CLIP PER SRM.

Part: SLIDE — LOW PRESSURE (L1 DOOR) · airframe 43,678 hrs · 25,837 cycles

L1 DOOR EMERGENCY EVAC SLIDE PRESSURE GAUGE LOW. REMOVED AND REPLACED SLIDE PER MT.

Part: SIGN — LOOSE (CABIN) · airframe 42,551 hrs · 25,148 cycles

OVERHEAD EMERGENCY EXIT SIGN LOOSE. SECURED SIGN PER MM.

Part: RIVET — LOOSE (L1 DOOR) · airframe 41,371 hrs · 24,418 cycles

DURING SCHEDULED MV2 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE CONTAINER GIRT BAR HOOK LOOSE. REMOVED AND REPLACED RIVETS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 40,969 hrs · 24,160 cycles

RIGHT EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BULB PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 38,923 hrs · 22,929 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT EMERGENCY EXIT LIGHT INOP AT ROW 5. RELAMPED PER MM.

Part: SIGN — LOOSE (CABIN) · airframe 37,063 hrs · 21,823 cycles

AFT GALLEY EXIT SIGN LOOSE. REMOVED AND REPLACED EXIT SIGN ASSY PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 36,868 hrs · 21,720 cycles

DURING SCHEDULED MV2 CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: GLOWSTRIP — LOOSE (CABIN) · airframe 36,207 hrs · 21,319 cycles

EEPLS PHOTOLUMINESCENT STRIP LOOSE AT ROW 8 DEF. SECURED STRIP PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 35,333 hrs · 20,793 cycles

DURING SCHEDULED MV1 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 23 ABC. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 33,391 hrs · 19,651 cycles

DURING SCHEDULED HC2 CHECK, AFT EMERGENCY EXIT LIGHTS BATTERY PACK FAILED THE CAPACITY TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 33,391 hrs · 19,651 cycles

DURING SCHEDULED HC2 CHECK, FWD CABIN EMERGENCY EXIT LIGHTS BATTERY PACK FAILED THE CAPACITY TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 33,391 hrs · 19,651 cycles

DURING SCHEDULED HC2 CHECK, CENTER CABIN EMERGENCY LIGHTS BATTERY PACK FAILED THE CAPACITY TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SHEAR TIE — CORRODED (BS 727A S24L) · airframe 29,928 hrs · 17,687 cycles

DURING SCHEDULED 8Y CHECK, FOUND SHEAR TIE CORRODED AT BS 727A, STR 24L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER — CORRODED (BS 727-727A S19L) · airframe 29,928 hrs · 17,687 cycles

DURING SCHEDULED 8Y CHECK, FOUND CASTING CORRODED AT BS 727 AND 727A, STR 19L. REPAIRED CASTING PER SWA EA.

Part: STRINGER CLIP — CORRODED (BS 727A S21L) · airframe 29,928 hrs · 17,687 cycles

DURING SCHEDULED 8Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 727A, STR 21L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CORRODED (BS 727A S25L) · airframe 29,928 hrs · 17,687 cycles

DURING SCHEDULED 8Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 727A, STR 25L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CORRODED (BS 727A S20L) · airframe 29,928 hrs · 17,687 cycles

DURING SCHEDULED 8Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 727A, STR 20L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER — CORRODED (BS 727-727B S24L) · airframe 29,928 hrs · 17,687 cycles

DURING SCHEDULED 8Y CHECK, FOUND STRINGER 24L CORRODED AT BS 727 TO BS 727B. REPAIRED STRINGER PER SWA EA.

Part: STRINGER CLIP — CORRODED (BS 727B S25L) · airframe 29,928 hrs · 17,687 cycles

DURING SCHEDULED 8Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 727B, STR 25L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CORRODED (BS 727A S22L) · airframe 29,928 hrs · 17,687 cycles

DURING SCHEDULED 8Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 727A, STR 22L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 29,928 hrs · 17,687 cycles

DURING SCHEDULED 8Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727A, STR 21L. REPAIRED FRAME SECTION PER SWA EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 29,928 hrs · 17,687 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986, RBL 42. REPAIRED FLOORBEAM PER SWA EA.

Part: HOOK — CORRODED (L1 DOOR) · airframe 29,928 hrs · 17,687 cycles

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

Part: HOOK — CORRODED (L1 DOOR) · airframe 29,928 hrs · 17,687 cycles

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

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 29,928 hrs · 17,687 cycles

DURING SCHEDULED 8Y CHECK, FOUND L2 DOOR CUTOUT, FWD LOWER FRAME CRACKED AT BS 295, STR 17R. REPAIRED FRAME SECTION PER SWA EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 29,928 hrs · 17,687 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 754, RBL 3. REPAIRED FLOORBEAM PER SWA EA.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 28,545 hrs · 16,894 cycles

DURING SCHEDULED HC2 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: HOOK — LOOSE (L1 DOOR SLIDE) · airframe 28,545 hrs · 16,894 cycles

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

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 28,545 hrs · 16,894 cycles

DURING SCHEDULED HC2 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: SLIDE — DISLODGED (L1 DOOR) · airframe 27,946 hrs · 16,545 cycles

DURING SCHEDULED RON CHECK, L1 DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REMOVED AND REPLACED SLIDE PER MM.

Part: CONTROLLER — FAILED (WINDSHIELD HEAT) · airframe 25,729 hrs · 15,293 cycles

DIVERSION, CLIMBING THROUGH 31,000 FT - R1 COCKPIT WINDSHIELD SHATTERED. REMOVED AND REPLACED R1 WINDSHIELD & HEAT CONTROLLER.

Part: MODULE — LEAKING (MLG WW) · airframe 24,119 hrs · 14,388 cycles

DECLARED EMERGENCY, A-SYSTEM HYDRAULIC FAILURE, QUANTITY LOSS. REMOVED AND REPLACED A-SYSTEM FILTER MODULE O-RING PER MM.

Part: STRIP — BROKEN (CABIN) · airframe 23,749 hrs · 14,167 cycles

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

Part: SLIDE — OUT OF ADJUST (L2 & R1 DOORS) · airframe 22,523 hrs · 13,458 cycles

DURING SCHEDULED MV2 CHECK, FOUND L2 AND R1 DOOR EVAC SLIDES OUT OF ADJUST. ADJUSTED L2 AND R1 DOOR EVAC SLIDES PER MM.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 17,468 hrs · 10,672 cycles

DURING SCHEDULED SERVICE CHECK, FOUND AFT ENTRY DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED EXIT LIGHT PER MM.

Part: WIRE — BROKEN (CABIN) · airframe 16,647 hrs · 10,217 cycles

EEPLS SECTION BROKEN. SECURED EEPLS STRIP, RELAMPED AND REPAIRED WIRING PER MM.

Part: FRAME — CRACKED (LT WING T/E) · airframe 16,646 hrs · 10,216 cycles

DURING SCHEDULED 5Y CHECK, FOUND LT WING T/E SUPPORT FRAME CRACKED, WBL 413.18. REPAIRED FRAME PER SWA EA.

Part: BUSHING — WORN (RT ELEVATOR) · airframe 16,326 hrs · 10,037 cycles

DURING SCHEDULED SERVICE CHECK, SWA SI 11075-55, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED RT ELEVATOR TAB HARDWARE AND BUSHING AT INBD HINGE ATTACH POINT.

Part: ENGINE — MAKING METAL (NR 1) · airframe 12,014 hrs · 7,491 cycles

DURING SCHEDULED C4 CHECK, FOUND METAL CHIPS AT NR 1 ENG AGB / TGB MAGNETIC CHIP DETECTOR, CHIPS EXCEED LIMITS GIVEN IN SWA TASK 4118. REMOVED AND REPLACED NR 1 ENG PER MM.

Part: COVER — BROKEN (CABIN) · airframe 12,014 hrs · 7,491 cycles

DURING SCHEDULED C4 CHECK, FOUND EEPLS COVERS BROKEN ( 26 EA ) IN CABIN. R&R COVERS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 7,522 hrs · 4,887 cycles

FWD SERVICE DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: RECEIVER — FAILED (NR 1 COMM)

APPROXIMATELY 10 MIN INTO FLIGHT, NR 1 COMM WOULD RECEIVE BUT NOT TRANSMIT, NR 2 WAS OK. PERFORMED AN AIR RETURN TO PHX. EVERY FREQ CHANGE (6 DIFF FREQ) TRIED. NR 1 COMM CONTINUED TO BE INOP AFTER LANDING, NR 1 COMM NOW WORKED. PERFORMED BITE CHECK OK OF BOTH NR 1, 2 COM, XCURS AND PSEU. AIR/GROUND BITE CHECKED. REMOVED AND REPLACED RECEIVER PER M/M. NR 1 RADIO OPS CHECKS AS PER MM.