N794SW

Part: SUPPORT FRAME — CHAFED (FAIRING) · airframe 62,844 hrs · 36,876 cycles

FAIRING SUPPORT FRAME CHAFED BETWEEN BS 652 TO BS 674, LBL 27. R&R FRAME IAW DWG & SRM.

Part: SUPPORT FRAME — CHAFED (FAIRING) · airframe 62,844 hrs · 36,876 cycles

FAIRING SUPPORT FRAME CHAFED BETWEEN BS 652 TO BS 674, RBL 27. R&R FRAME IAW SRM AND DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 62,844 hrs · 36,876 cycles

INTERCOSTAL CRACKED BETWEEN BS 312 TO BS 328, RBL 30. R&R INTERCOSTAL PER SRM AND DWG.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 62,844 hrs · 36,876 cycles

CABIN SEAT TRACK CORRODED BETWEEN BS 480 TO BS 520, RBL 45. R&R SEAT TRACK PER SRM AND DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 62,844 hrs · 36,876 cycles

FLOOR PANEL SUPPORT FASTENER HOLE CORRODED AT BS 328+12, LBL 11. R&R PANEL BREAK PER SRM AND DWG.

Part: WEB — CORRODED (FUSELAGE) · airframe 62,844 hrs · 36,876 cycles

FLOOR WEB CORRODED AT BS 1019, RBL 6. R&R WEB PER SRM & DWG.

Part: INTERCOSTAL — DAMAGED (FUSELAGE) · airframe 62,844 hrs · 36,876 cycles

INTERCOSTAL DAMAGED BETWEEN BS 344 TO BS 360, RBL 51. REPAIRED INTERCOSTAL PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 62,844 hrs · 36,876 cycles

FLOORBEAM CORRODED AT BS 986, BETWEEN LBL 44 TO RBL 44. REPAIRED FLOORBEAM PER SRM AND EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 62,844 hrs · 36,876 cycles

FLOORBEAM CRACKED AT BS 328, RBL 20. REPAIRED FLOOR BEAM PER SRM & DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 62,844 hrs · 36,876 cycles

INTERCOSTAL CRACKED BETWEEN BS 294 TO BS 312, RBL 16. R&R INTERCOSTAL IAW SRM AND DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 62,844 hrs · 36,876 cycles

INTERCOSTAL CRACKED BETWEEN BS 312 TO BS 328, LBL 45. R&R INTERCOSTAL IAW SRM AND DWG.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 62,844 hrs · 36,876 cycles

R1 DOOR MOP SILL CORRODED AT BS 312, RBL 54. R&R MOPSILL IAW SRM AND DWG.

Part: STRAP — CORRODED (FUSELAGE) · airframe 62,844 hrs · 36,876 cycles

TENSION STRAP CORRODED AT BS 1016, RBL 4. R&R TENSION STRAP PER SRM AND DWG.

Part: FRAME — CHAFED (FUSELAGE) · airframe 62,844 hrs · 36,876 cycles

FRAME CHAFED AT BS 294.5, STR 3L. REPAIRED FRAME PER SRM.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 62,844 hrs · 36,876 cycles

L1 DOOR MOP SILL CORRODED AT BS 312, LBL 54. R&R MOPSILL PER SRM AND DWG.

Part: STRAP — CORRODED (FUSELAGE) · airframe 62,844 hrs · 36,876 cycles

TENSION STRAP CORRODED AT BS 1016, RBL 18. R&R TENSION STRAP PER SRM & DWG.

Part: STRAP — CORRODED (FUSELAGE) · airframe 62,844 hrs · 36,876 cycles

TENSION STRAP CORRODED AT BS 1016, LBL 4. R&R TENSION STRAP PER SRM & DWG.

Part: BULKHEAD — LOOSE (RT MLG WW) · airframe 62,844 hrs · 36,876 cycles

LOWER COMPOSITE BULKHEAD LOOSE AT BS 663, RBL 12. REPAIRED BULKHEAD IAW SRM.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 62,844 hrs · 36,876 cycles

AFT CARGO FLOOR TO AFT BULKHEAD SUPPORT ANGLE CORRODED AT BS 947, BETWEEN RBL 17 TO LBL 11. R&R SUPPORT IAW DWG & SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 62,844 hrs · 36,876 cycles

AFT CARGO DOORWAY LOWER THRESHOLD SUB WEB CORRODED BETWEEN BS 795 TO BS 847, RBL 20. R&R SUB WEB IAW SRM AND DWG.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 62,844 hrs · 36,876 cycles

AFT CARGO FLOOR INTERCOSTAL CORRODED AT BS 770, RBL 19. R&R INTERCOSTAL IAW DWG & SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 62,844 hrs · 36,876 cycles

AFT CARGO FLOOR SUPPORT STRINGER CORRODED AT BS 752, RBL 3. R&R STRINGER IAW SRM & DWG.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 62,844 hrs · 36,876 cycles

AFT CARGO FLOOR TRACK CORRODED BETWEEN BS 798 TO BS 820, RBL 15. R&R FLOOR TRACK IAW SRM AND EA.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 62,844 hrs · 36,876 cycles

AFT CARGO FLOOR PANEL SUPPORT STRINGER CORRODED AT BS 945, RBL 3. R&R SUPPORT IAW DWG & SRM.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 62,844 hrs · 36,876 cycles

AFT CARGO FLOOR TRACK CORRODED AT BS 727D+8, LBL 17. R&R TRACK / RAIL ASSEMBLY IAW SRM AND DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 62,844 hrs · 36,876 cycles

AFT CARGO LT FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 727A TO BS 847, LBL 20. R&R SUPPORT PER SRM AND DWG.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 62,844 hrs · 36,876 cycles

AFT CARGO RT FLOOR TO SIDEWALL SUPPORT SHIELD CORRODED BETWEEN BS 767 TO BS 787, RBL 20. R&R SHIELD IAW DWG AND SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 62,844 hrs · 36,876 cycles

AFT CARGO LT FLOOR TO SIDEWALL SUPPORT ANGLE UPPER AND LOWER SURFACES CORRODED BETWEEN BS 870 TO BS 880, LBL 8. R&R ANGLE PER SRM AND DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 62,844 hrs · 36,876 cycles

AFT CARGO FLOOR SUPPORT STRINGER CORRODED AT BS 727A+3, RBL 3. R&R STRINGER PER SRM & DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 62,844 hrs · 36,876 cycles

AFT CARGO FLOOR SUPPORT STRINGER CORRODED AT BS 727B+1, LBL 3. R&R STRINGER IAW SRM & DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 62,844 hrs · 36,876 cycles

AFT CARGO RT FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 727A TO BS 767, RBL 20. R&R SUPPORT IAW SRM & DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 62,844 hrs · 36,876 cycles

SIDEWALL TO BULKHEAD SUPPORT CORRODED AT BS 500D, LBL 22. R&R SUPPORT PER SRM AND DWG.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 62,844 hrs · 36,876 cycles

FRAME TO STRINGER INTERCOSTAL SUPPORT CRACKED AT BS 500D, STR 22L. R&R SUPPORT IAW SRM & DWG.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 62,844 hrs · 36,876 cycles

FLOOR TO SIDEWALL SHIELD CORRODED BETWEEN BS 420 TO BS 440, RBL 22. R&R SHIELD IAW SRM AND DWG.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 62,844 hrs · 36,876 cycles

FRAME TO STRINGER INTERCOSTAL SUPPORT CRACKED AT BS 500D, STR 19R. R&R SUPPORT PER SRM & DWG.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 62,844 hrs · 36,876 cycles

FRAME TO STRINGER INTERCOSTAL SUPPORT CRACKED AT BS 500D, STR 19L. R&R SUPPORT PER SRM AND DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 62,844 hrs · 36,876 cycles

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

Part: SHIELD — CORRODED (FUSELAGE) · airframe 62,844 hrs · 36,876 cycles

FORWARD CARGO BAY FLOOR TO SIDEWALL SHIELD CORRODED BETWEEN BS 497 TO BS 500A, RBL 22. R&R SHIELD IAW SRM & DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 62,844 hrs · 36,876 cycles

FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 500A TO BS 500D, RBL 22. R&R SUPPORT IAW SRM & DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 62,844 hrs · 36,876 cycles

RT LOWER COMPOSITE BULKHEAD UPPER SUPPORT ANGLE CRACKED AT BS 663. REPAIRED ANGLE EA AND ER.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 62,844 hrs · 36,876 cycles

LOWER COMPOSITE BULKHEAD VERTICAL SUPPORT ANGLE CRACKED AT BS 663, RBL 32. R&R ANGLE IAW SRM AND DWG.

Part: WINDOW — ARCED (COCKPIT) · airframe 62,642 hrs · 36,743 cycles

CAPTAIN'S FRONT WINDSHIELD (L1) ARCED IN FLIGHT. R&R CAPTAINS L1 WINDOW PER AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 62,415 hrs · 36,603 cycles

EMERGENCY LIGHTING BATTERY PACK FAILED CAPACITY CHECK AT ROW 17. R&R BATTERY PACK PER MM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 62,232 hrs · 36,477 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 61,978 hrs · 36,323 cycles

RT EMERGENCY AISLE LIGHT INOP AT ROW 13. RELAMPED LIGHT IAW AMM.

Part: SLIDE — LOOSE (R1 DOOR) · airframe 61,774 hrs · 36,182 cycles

R1 DOOR EVAC SLIDE PRESSURE LOOSE. REINSTALLED SLIDE IAW MT.

Part: BATTERY — NO TEST (EMERGENCY LIGHT) · airframe 60,285 hrs · 35,192 cycles

EMERGENCY LIGHT BATTERY FAILED A TEST AT M01675. R & R THE BATTERY IAW AMM.

Part: BUMPER — MISSING (R2 DOOR SLIDE) · airframe 60,285 hrs · 35,192 cycles

R2 DOOR SLIDE COVER AFT BUMPER MISSING. R & R THE BUMPER IAW AMM.

Part: BRACKET — CRACKED (R2 DOOR LINER) · airframe 60,285 hrs · 35,192 cycles

R2 DOOR LOWER LINER PAN AFT BRACKET CRACKED. R & R THE PAN IAW AMM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 59,096 hrs · 34,446 cycles

RT EXTERNAL EMERGENCY LIGHT INOP AT AFT CARGO DOOR. RELAMPED LIGHT PER AMM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 58,287 hrs · 33,947 cycles

L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR BUSTLE OUT OF POSITION. REPACKED SLIDE IAW MT.

Part: SIGN — LOOSE (CABIN) · airframe 58,026 hrs · 33,787 cycles

RT EMERGENCY EXIT SIGN LOOSE. SECURED SIGN PER CMM.

Part: GASKET — DAMAGED (LT WING) · airframe 57,523 hrs · 33,516 cycles

AIR TURNBACK, ON CLIMB OUT TOWER ADVISED OF FLUID COMING OUT OF LEFT SIDE OF AIRCRAFT. R&R LT WING SURGE TANK ACCESS PANEL 53BB GASKET IAW MM.

Part: O-RING — DAMAGED (HYDRAULIC SYS) · airframe 57,539 hrs · 33,527 cycles

AIR TURNBACK, CLIMBING OUT OF DEPARTURE CONTROL REPORTED THAT TOWER SAID WE HAD FLUID VENTING OFF LEFT SIDE OF AIRCRAFT. FOUND AUTO SLAT CONTROL MODULE B-NUT FITTING LEAKING HYDRAULIC FLUID. R&R O-RING PER SIP.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 57,452 hrs · 33,469 cycles

L2 DOOR AFT SIDE EXTERIOR EMERGENCY LIGHT INOP. RELAMPED LIGHT PER AMM.

Part: WINDOW — ARCED (COCKPIT) · airframe 57,392 hrs · 33,434 cycles

L2 SLIDING WINDOW ARCED. R&R WINDOW PER MM.

Part: SIGN — UNSECURE (CABIN) · airframe 3,389 hrs · 56,815 cycles

R2 DOOR EMERGENCY EXIT SIGN CAME OFF. INSTALLED SIGN PER MM.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 56,362 hrs · 32,808 cycles

EMERGENCY LIGHT FAILED CAPACITY CHECK. R & R THE BATTERY PACK IAW MM.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 56,362 hrs · 32,808 cycles

EMERGENCY LIGHT FAILED CAPACITY CHECK. R & R THE BATTERY PACK IAW MM.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 56,362 hrs · 32,808 cycles

EMERGENCY LIGHT FAILED A CAPACITY CHECK. R & R THE BATTERY PACK IAW MM.

Part: CREASE BEAM — CORRODED (BS 680-690) · airframe 56,362 hrs · 32,808 cycles

RIGHT CREASE BEAM CORRODED AT BS 680 - 690. REPAIRED THE CREASE BEAM IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 56,362 hrs · 32,808 cycles

LT INBOARD CREASE BEAM CORRODED BETWEEN BS 680 TO BS 690, LBL 55. R&R CREASE BEAM PER SRM AND DWG.

Part: LIGHT — DAMAGED (CABIN) · airframe 56,362 hrs · 32,808 cycles

MID CABIN OVERHEAD EXIT LIGHT DAMAGED. R & R LIGHT ASSY IAW MM.

Part: BULKHEAD WEB — CRACKED (BS 663) · airframe 56,362 hrs · 32,808 cycles

MLG W/W BULKHEAD WEB CRACKED AT BS 663, RBL 40.5 TO 45. / REPAIRED WEB IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,362 hrs · 32,808 cycles

RT FRAME WEB CRACKED AT BS 727, WL 200. REPAIRED WEB PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,362 hrs · 32,808 cycles

LOWER FRAME WEB INNER CHORD CRACKED AT BS 727, WL 200. REPAIRED CHORD PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,362 hrs · 32,808 cycles

LOWER BULKHEAD SKIN CRACKED AT BS 540, STR 22R. REPAIRED SKIN PER EA & ER.

Part: BULKHEAD — CRACKED (LT MLG WW) · airframe 56,362 hrs · 32,808 cycles

MAIN WHEEL WELL LOWER BULKHEAD CRACKED AT BS 663 LBL 34. REPAIRED BULKHEAD PER EA.

Part: LATCH — DIRTY (R2 DOOR) · airframe 56,362 hrs · 32,808 cycles

R2 DOOR ESCAPE SLIDE GIRT BAR LATCH STUCK. CLEANED LATCH IAW AMM.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 56,176 hrs · 32,680 cycles

LEFT OVERWING EMERGENCY EXIT LIGHT BULB INOPERATIVE. R & R THE BULB IAW MM.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 55,935 hrs · 32,536 cycles

LEFT OVERWING EMERGENCY EXIT LATCH LOWER EXIT SIGN LAMP INOPERATIVE. RELAMPED IAW AMM.

Part: SIGN — BROKEN (CABIN) · airframe 54,376 hrs · 31,599 cycles

RIGHT OVERWING FWD LOWER EMER EXIT SIGN BROKEN. R & R SIGN ASSEMBLY IAW AMM.

Part: SENSOR — FAULTY (NLG WW) · airframe 52,422 hrs · 30,438 cycles

AIR TURN BACK, AFTER GEAR RETRACTION NOSE GEAR GREEN & RED LIGHTS ILLUMINATED. NO OVERWEIGHT LANDING & NO EMER DECLARED. R & R NLG SENSOR IAW AMM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 50,388 hrs · 29,262 cycles

LEFT AFT FUSELAGE EMER LIGHT INOPERATIVE. RELAMPED IAW MM.

Part: LENS — LOOSE (CABIN) · airframe 50,189 hrs · 29,156 cycles

R2 DOOR LOWER EXIT LENS LOOSE. REPAIRED LENS IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 49,964 hrs · 29,018 cycles

TRANSVERSE FLOORBEAM AFT SEAT TRACK AFT FASTENER HOLE CRACKED AT BS 727B, RBL 24.75. REPAIRED SEAT TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 49,964 hrs · 29,018 cycles

FORWARD SEAT TRACK INBD FLANGE FWD & AFT FASTENER HOLE CRACKED AT BS 727B, RBL 45.5. REPAIRED SEAT TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 49,964 hrs · 29,018 cycles

FORWARD SEAT TRACK OTBD FLANGE AFT FASTENER HOLE CRACKED AT BS 727B, RBL 45.5. REPAIRED SEAT TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 49,964 hrs · 29,018 cycles

FORWARD SEAT TRACK OTBD FLANGE FWD & AFT FASTENER HOLE CRACKED AT BS 727B, LBL 45.5. REPAIRED SEAT TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 49,964 hrs · 29,018 cycles

AFT SEAT TRACK OTBD FLANGE FWD FASTENER HOLE CRACKED AT BS 727B, LBL 24.75. REPAIRED SEAT TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 49,964 hrs · 29,018 cycles

FORWARD SEAT TRACK INBD FLANGE FWD FASTENER HOLE CRACKED AT BS 727B, LBL 24.75. REPAIRED SEAT TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 49,964 hrs · 29,018 cycles

FORWARD SEAT TRACK INBD FLANGE AFT FASTENER HOLE CRACKED AT BS 727B, LBL 45.5. REPAIRED SEAT TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 49,964 hrs · 29,018 cycles

TRANSVERSE FLOORBEAM FWD SEAT TRACK FASTENER HOLE CRACKED AT BS 727B, RBL 24.75. REPAIRED SEAT TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 49,964 hrs · 29,018 cycles

FORWARD SEAT TRACK OTBD FLANGE AFT FASTENER HOLE CRACKED AT BS 727B, LBL 24.75. REPAIRED SEAT TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 49,964 hrs · 29,018 cycles

AFT SEAT TRACK INBD FLANGE FASTENER HOLE CRACKED AT BS 727B, LBL 45.5. REPAIRED SEAT TRACK IAW EA.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 49,964 hrs · 29,018 cycles

LEFT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STAB STATION 120.30, 19 INCHES FWD OF THE REAR SPAR. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 49,964 hrs · 29,018 cycles

LEFT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STAB STATION 120.30, 10 INCHES FWD OF THE REAR SPAR. REPAIRED SKIN IAW SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 49,964 hrs · 29,018 cycles

EMERGENCY BULLNOSE LIGHT INOPERATIVE AT ROW 8 DEF. REPAIRED LIGHT IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 49,964 hrs · 29,018 cycles

EMERGENCY BULLNOSE LIGHT INOPERATIVE AT ROW 3 DEF. REPAIRED LIGHT IAW MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 49,132 hrs · 28,545 cycles

LEFT OVERWING EMER EXT LIGHT INOPERATIVE. R & R BATTERY PACK IAW AMM.

Part: SLIDE — LOOSE (R2 DOOR) · airframe 46,126 hrs · 26,833 cycles

R2 DOOR EMERGENCY EVAC SLIDE LOOSE. SECURED SLIDE IAW MT.

Part: FILTER — FAULTY (NR 1 ENGINE) · airframe 44,748 hrs · 26,006 cycles

INFLIGHT SHUTDOWN/DIVERSION/DECLARED EMERGENCY, NR 1 ENGINE IN CRUISE HAD A BANG AND YAW SHORTLY AFTER LOW OIL PRESSURE LIGHT ILLUMINATED, ALL OTHER INDICATIONS NORMAL. WE SHUTDOWN NR 1 AND DIVERTED. AFTER LANDING, SOME OIL NOTED IN HOT EXHAUST AREAS F ENGINE (NOT FAN BYPASS FLOW AREA). PERFORMED FIM TASK 71-00-00-210 INSP AFTER ENGINE STALL OR POSSIBLE ENGINE STALL. NO DEBRIS NOTED OR DAMAGE NOTED IN FAN MODULE OR EXHAUST AREA. INSPECTED 3 EA SCAVENGE FILTERS & REPLACED OIL SUPPLY FILTER. NO DEBRIS NOTED.

Part: HYDRAULIC LINE — LOOSE (HYDRAULIC SYS) · airframe 43,207 hrs · 25,078 cycles

DIVERSION / DECLARED EMERGENCY - HYD A-SYS QTY LOSS. TIGHTENED NR 1 ENGINE HYD PUMP LINE AT PYLON. REMOVED AND REPLACED HYD A-SYS ENGINE DRIVEN PUMP PER MM.

Part: FITTING — LOOSE (GIRT BAR) · airframe 43,204 hrs · 25,075 cycles

FED EMERGENCY SLIDE PACK FWD GIRT BAR RETAINER CLIP IS LOOSE. REMOVED & REPLACED 2 EA FASTENERS, FED EMERGENCY SLIDE PACK FWD GIRT BAR RETAINER CLIP PER SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 43,204 hrs · 25,075 cycles

INTERCOSTAL BS 500D - 520 AT STR 25R IS CRACKED. REMOVED AND REPLACED CRACKED INTERCOSTAL BS 500D-520 STR 25R IAW SRM 51-10-02-0G-0 PARAGRAPH 9A.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 43,204 hrs · 25,075 cycles

ATTACH CLIP CRACKED AT BS 261 STR 8L. REMOVED AND REPLACED WITH NEW CLIP AT BS 261 STR 8L PER SRM 51-40-02.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,204 hrs · 25,075 cycles

LEFT COCKPIT FRAME WEB AT BS 235-8 WL232 IS CRACKED. REPAIRED COCKPIT LEFT FRAME BS 235.8 WL 232 IAW ER 12-03592 AND EA 1-753-21218 FACT AS A RESULT OF POST REPAIR INSPECTION

Part: FAIRING — CRACKED (FLAP TRACK) · airframe 43,204 hrs · 25,075 cycles

RIGHT WING 7 FAIRING 643BB CRACKED AT I/B AND O/B. REMOVED AND REPLACED FAIRING PER SOPM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,204 hrs · 25,075 cycles

FRAME CRACKED AT A/C ATTACH BRACKET BS 360 STR 8R. REPAIRED BS 360 FRAME AT STR 8R IAW EA 1-753-21158 AND ER 12-03582.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,204 hrs · 25,075 cycles

FUSELAGE FRAME CRACKED AT AIR CONDITIONING ATTACH BRACKET BS 827 STR 8-9L. PERFORMED REPAIR AT FUSELAGE FRAME AIR CONDITIONING ATTACH BRACKET BS 827 STR 8L-9L IAW EA 1-A53-12114, REV 2.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 43,204 hrs · 25,075 cycles

CORROSION ON PASSENGER CABIN FLOOR CREASE BEAM WEB AT BS 712 WL 208 RBL 65. CREASE BEAM WEB AT BS 712 WL 208 RBL 65 REPAIRED PER EA 1-753-21161.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,204 hrs · 25,075 cycles

FUSELAGE FRAME CRACKED AT AIR CONDITIONING ATTACH BRACKET BS 480 STR 8-9L. REPAIRED FRAME AT AIR CONDITIONING ATTACH BRACKET BS 480 STR 8-9L PER EA 1-A53-12114 REV 2.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,204 hrs · 25,075 cycles

FUSELAGE FRAME CRACKED AT AIR CONDITIONING ATTACH BRACKET BS 867 STR 8-9L. PERFORMED REPAIR FRAME CRACKED AT AIR CONDITIONING ATTACH BRACKET BS 867 STR 8-9L IAW EA 1-A53-12114 REV 2.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,204 hrs · 25,075 cycles

FRAME CRACKED AT A/C ATTACH BRACKET BS 440 STR 8R. PERFORMED REPAIR AT FRAME ATTACH BRACKET BS 440 STR 8R IAW EA 1-A53-12114 REV 2.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,204 hrs · 25,075 cycles

FUSELAGE FRAME CRACKED AT AIR CONDITIONING ATTACH. PERFORMED REPAIR FRAME CRACKED AT AIR CONDITIONING ATTACH BRACKET BS827 STR 8-9R IAW EA 1-A53-12114.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,204 hrs · 25,075 cycles

FUSELAGE FRAME CRACKED AT AIR CONDITIONING ATTACH BRACKET BS 907 STR 8-9L. REPAIRED BS 907 FRAME STR 8-9 LEFT IAW ER 12-03581 AND EA 1-753-212 06.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,204 hrs · 25,075 cycles

FUSELAGE FRAME CRACKED AT AIR CONDITIONING ATTACH BRACKET BS 500C STR 8-9L. REPAIRED FRAME BS 500C STR 8-9L PER EA 1-A53-12114 REV 2.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,204 hrs · 25,075 cycles

FUSELAGE FRAME CRACKED AT AIR CONDITIONING ATTACH BRACKET BS 400 STR 8-9L. REPAIRED FUSELAGE FRAME AT AIR CONDITIONING ATTACH BRACKET BS 400 STR 8-9 LEFT PER EA 1-A53-12114 REV 2.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 43,204 hrs · 25,075 cycles

CORROSION, PASSENGER CABIN FLOOR PANEL 242UF, HAS CORRODED INSERTS ALONG OUTBOARD AND AFT EDGES. REPLACED CORRODED INSERTS AND REPAIRED DAMAGE ON FLOOR PANEL 242UF IAW SRM 53-00-50-2R-1. 969U, 16NOV12.

Part: FLOOR PANEL — CORRODED (CABIN) · airframe 43,204 hrs · 25,075 cycles

CORROSION, PASSENGER CABIN FLOOR PANEL 241ABF HAS CORRODED AND MISSING INSERTS. REPLACED CORRODED / MISSING INSERTS AND REPAIRED DAMAGE ON FLOOR PANEL 241ABF IAW SRM 53-00-50-2R-6 969U 16NOV12.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 43,204 hrs · 25,075 cycles

BULKHEAD LOWER ATTACH ANGLE CRACKED BS 865, LBL 11. REMOVED AND REPLACED ANGLE IAW SRM.

Part: FLOORBOARD — PUNCTURED (CABIN) · airframe 43,204 hrs · 25,075 cycles

PAX FLOORBOARD 231JF HAS SEVERAL PUNCTURES IN LOWER SURFACE. PAX FLOORBOARD 231JF PUNCTURES TO LOWER SURFACE WERE REPAIRED PER SWA EA 1-A53-13206 DATED 8/16/2010, EA 1-753-21078 DATED 16-NOV-2012 AND ATS ER 12-03563 DATED 16-NOV-2012.

Part: FLOORBOARD — PUNCTURED (CABIN) · airframe 43,204 hrs · 25,075 cycles

PAX FLOORBOARD 231GF HAS PUNCTURE AT 11" FROM AFT, 10" FROM LEFT SIDE. REPAIRED BOARD PER EA AND ATS ER.

Part: STIFFENER — CORRODED (RT MLG WW) · airframe 43,204 hrs · 25,075 cycles

CORROSION UPPER SURFACE OF RIGHT W/W PRESSURE DECK AT BS 708, RBL 63-70, WL 202. REMOVED AND REPLACED STIFFENER IAW SRM.

Part: FLOORBOARD — DAMAGED (CABIN) · airframe 43,204 hrs · 25,075 cycles

PAX FLOORBOARD 231GF HAS PLIES PEELED UP AT 5" FROM FWD EDGE LEFT SIDE. REPAIRED BOARD PER EA.

Part: FLOORBOARD — PUNCTURED (CABIN) · airframe 43,204 hrs · 25,075 cycles

PAX FLOORBOARD 232GF HAS PUNCTURE AT 2.5" FROM FWD, 3" FROM LEFT SIDE. REPAIRED BOARD PER EA.

Part: WEB — CORRODED (FUSELAGE) · airframe 43,204 hrs · 25,075 cycles

AFT CARGO BAY VERTICAL WEB HAS CORROSION BS 847-850 RBL 18 WL 248. REMOVED AND REPLACED WEB PER BOEING DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 43,204 hrs · 25,075 cycles

AFT CARGO BAY FLOOR SUPPORT HAS CORROSION BS 727A+5 RBL 2.5. REPAIRED FLOOR SUPPORT IAW SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 43,204 hrs · 25,075 cycles

AFT CARGO BAY FLOOR SUPPORT HAS CORROSION BS 727B+3 LBL 12. REPAIRED FLOOR SUPPORT IAW SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 43,204 hrs · 25,075 cycles

AFT CARGO BAY FLOOR SUPPORT HAS CORROSION BS 767+6 LBL 2.5. REPAIRED AFT CARGO BAY FLOOR SUPPORT BS 767+6 LBL 2.5 PER EA 1-A53-4982 REV 3.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 43,204 hrs · 25,075 cycles

AFT CARGO BAY FLOOR SUPPORT HAS CORROSION BS 767+6 LBL 17. REPAIR AFT CARGO BAY FLOOR SUPPORT BS 767+6 LBL 17 IAW EA 1-A53-4982 REV 3.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 43,204 hrs · 25,075 cycles

AFT CARGO BAY RT FLOOR TO SIDEWALL HAS CORROSION BS 847-867 RBL 18. REMOVED AND REPLACED SUPPORT PER SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 43,204 hrs · 25,075 cycles

AFT CARGO BAY FLOOR SUPPORT WEB HAS CORROSION BS 727A-727B RBL 2.5. REMOVED CORROSION ON AFT CARGO BAY FLOOR SUPPORT WEB AT BS 727A-BS 727B RBL 2.5 IAW SRM 51-10-02.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 43,204 hrs · 25,075 cycles

AFT CARGO BAY INTERCOSTAL HAS CORROSION BS 727+8 LBL 6 - RBL 6 WL 150-154. REMOVED AND REPLACED INTERCOSTAL WEB IAW SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 43,204 hrs · 25,075 cycles

AFT CARGO BAY FLOOR SUPPORT HAS CORROSION BS 767+6 RBL 2.5. REPAIRED AFT CARGO BAY FLOOR SUPPORT BS 767+6 RBL 25 PER EA 1-A53-4982 REV 3.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 43,204 hrs · 25,075 cycles

AFT CARGO BAY VERTICAL BULKHEAD SUPPORT HAS CORROSION BS 947 LBL 9, WL 181. REMOVED AND REPLACED SUPPORT PER SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 43,204 hrs · 25,075 cycles

AFT CARGO BAY FLOOR SUPPORT WEB CORRODED BETWEEN BS 727A-727B, LBL 2.5. REMOVED AND REPLACED WEB IAW SRM AND DRAWING.

Part: WEB — CORRODED (FUSELAGE) · airframe 43,204 hrs · 25,075 cycles

AFT CARGO BAY VERTICAL WEB HAS CORROSION UNDER NUT PLATES BS 794-831 RBL 18 WL 151. REMOVED AND REPLACED ACB VERTICAL WEB BS 794-831 RBL 18 WL 151 IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 43,204 hrs · 25,075 cycles

AFT CARGO BAY FLOOR SUPPORT HAS CORROSION BS 727D+6 RBL 13. REMOVED AND REPLACED SUPPORT IAW SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 43,204 hrs · 25,075 cycles

AFT CARGO BAY FLOOR SUPPORT HAS CORROSION BS 727B+3 LBL 2.5. REMOVED AND REPLACED SUPPORT IAW SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 43,204 hrs · 25,075 cycles

AFT CARGO BAY FLOOR SUPPORT HAS CORROSION BS 767+6 RBL 8. REPAIRED AFT CARGO BAY FLOOR SUPPORT BS 767+6 RBL 8 PER EA 1-A53-4982 REV 3.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 43,204 hrs · 25,075 cycles

AFT CARGO BAY LT FLOOR TO SIDEWALL SUPPORT HAS CORROSION BS 727-847. REMOVED AND REPLACED SUPPORT PER SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 43,204 hrs · 25,075 cycles

AFT CARGO BAY RT FLOOR TO SIDEWALL SUPPORT HAS CORROSION BS 727-767. REMOVED AND REPLACED SUPPORT IAW SRM.

Part: STRAP — CORRODED (FLOOR PANEL) · airframe 43,204 hrs · 25,075 cycles

AFT CARGO BAY FLOOR PANEL SPLICE STRAP HAS CORROSION BS 727D+6. REMOVED AND REPLACED STRAP PER DWG SRM.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 43,204 hrs · 25,075 cycles

BS 481-488 RBL 21WL 156 HAS CORROSION UNDER NUT PLATES. REMOVED AND REPLACED INTERCOSTAL IAW ER EA.

Part: SEAL — WORN (LT HORIZ STAB) · airframe 43,204 hrs · 25,075 cycles

LEFT STAB FWD LOWER SLIDE SEAL IS WORN THROUGH. REMOVED AND REPLACED LEFT STAB FWD LOWER SIDE SEAL PER MM 53-31-31-000-801 AND MM 53-31-31-400-801.

Part: SEAL — WORN (RT HORIZ STAB) · airframe 43,204 hrs · 25,075 cycles

RIGHT HORIZONTAL STAB LOWER FWD SLIDE SEAL IS WORN THROUGH. REMOVED AND REPLACED, WITH SERVICEABLE UNIT, RT HORIZ STAB FWD LOWER SLIDE SEAL PLATE IAW AMM 53-31-31-000-801 AND AMM 53-31-31-400-801 7641U 28NOV12.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 43,204 hrs · 25,075 cycles

FWD CARGO BAY STRINGER 26RT BS 539 HAS CORROSION. REPAIRED FWD CARGO BAY STRINGER 26RT BS 539 PER ER 12-03650 AND EA 1-753-21211.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 43,204 hrs · 25,075 cycles

CORROSION, ON AFT CARGO BAY DOOR CUTOUT SUB THRESHOLD WEB, BS 795 TO 832. REMOVED AND REPLACED SUB THRESHOLD WEB BETWEEN BS 795 AND BS 847 P/N 146A8123U6. 89004U, 02DEC12.

Part: SEAL — WORN (LT HORIZ STAB) · airframe 43,204 hrs · 25,075 cycles

LEFT STAB FWD UPPER SLIDE SEAL IS WORN THROUGH. REMOVED AND REPLACED LEFT STAB FWD UPPER SLIDE SEAL IAW MM 53-31-000-801 AND MM 53-31-31-400-801.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 43,204 hrs · 25,075 cycles

FWD CARGO BAY SUB THRESHOLD WEB HAS CORROSION. REMOVED CORROSION ON SUB THRESHOLD WEB FWD CARGO BAY PER SRM 51-10-02. FOUND TO BE OUT OF LIMITS PER SRM 53-30-15-1A-1. REMOVED AND REPLACED SUB THRESHOLD WEB AT FWD CARGO BAY PER SRM 51-40-02.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 43,204 hrs · 25,075 cycles

FWD CARGO BAY STRINGER 25LT BS 539 HAS CORROSION. REPAIRED FWD CARGO BAY STRANGER 25 LT FROM 35 500D & 10, TO 520 + 15 IAW SRM 53-00-03-2R-1 FIG 205.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 43,204 hrs · 25,075 cycles

FWD CARGO BAY INTERCOSTAL CRACKED BS 450 LBL 24 WL 156. FABRICATED NEW PART IAW BOEING DWG 143A7505 TREATED, PRIMED DRILLED DEBURRED AND INSTALLED IAW B737 SRM 51-20-01-0G-0, 51-40-02.

Part: PLATE — CRACKED (LT WING) · airframe 43,204 hrs · 25,075 cycles

LEFT WING LOWER T/E WAFFLE PLATE CRACKED BETWEEN 3 FLAP TRACK AND SWING DOWN DOOR. REMOVED AND REPLACED PLATE PER SRM EA.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 43,204 hrs · 25,075 cycles

CORROSION FED CUTOUT THRESHOLD SUPPORT ZEE HAS CORROISON ON UPPER SURFACE WL 208 LBL 63 BS 319-339. REMOVED & REPLACED FED CUTOUT THRESHOLD SUPPORT ZEE WL 208 LBL 63 BS 319-339 IAW SRM 51-40-02 83802U 19NOV12.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 43,204 hrs · 25,075 cycles

CORROSION FED CUTOUT THRESHOLD SUPPORT C-CHANNEL HAS CORROISON ON UPPER SURFACE WL 208 LBL 60 BS 312-342. REMOVED & REPLACED FWD CUTOUT THRESHOLD SUPPORT C-CHANNEL WL 208 LBL 60 BS 312-342 IAW SRM 51-40-02 83802U 19NOV12.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 43,204 hrs · 25,075 cycles

CORROSION BS 986.5 FLOORBEAM HAS CORROSION ON PREVIOUSLY REPAIRED UPPER CHORD LBL 44 TO RBL 44 WL 208. CORROSION LIMITED TO REPLACEMENT UPPER T-CHORD ONLY. BS 986.5 FLOORBEAM HAS CORROSION ON PREVIOUSLY REPAIR UPPER T-CHORD LBL 44 TO RBL

Part: SUPPORT ANGLE — CRACKED (LT WING) · airframe 43,204 hrs · 25,075 cycles

LEFT WING UPPER T/E PANEL CTR AFT SUPPORT ANGLE CRACKED ABOVE 1 PYLON AFT TIP. REMOVED AND REPLACED RETAINER IAW SRM.

Part: SUPPORT ANGLE — CRACKED (RT WING) · airframe 43,204 hrs · 25,075 cycles

RIGHT WING UPPER T/E BULB SEAL SUPPORT ANGLE CRACKED ABOVE 2 PYLON AFT TIP. REMOVED AND REPLACED ANGLE IAW SRM.

Part: WEB — CRACKED (RT WING) · airframe 43,204 hrs · 25,075 cycles

RIGHT WING UPPER T/E PANEL WEB CRACKED I/B TRACK MAIN FLAPS. REMOVED AND REPLACED WEB IAW SRM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 43,204 hrs · 25,075 cycles

(LEFT WING) O/B AFT FLAP I/B UPPER SURFACE IS DELAMINATED. LEFT WING O/B AFT FLAP I/B UPPER SURFACE DELAMINATION WAS REPAIRED.

Part: SILL — CORRODED (FUSELAGE) · airframe 43,204 hrs · 25,075 cycles

MOPSILL CORRODED BETWEEN BS 294-328, RBL 53 RT. REMOVED AND REPLACED CORROSION PER SRM IAW NEW CHORD MAT PER DWG DRILLED PER SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 43,204 hrs · 25,075 cycles

BS 344-360 WL 208 BL 0 INTERCOSTAL CRACKED AT FASTENER HOLE. REMOVED AND REPLACED NEW INTERCOSTAL ITEM 7530286 REQ NUMBER 533561 P/N 141A5410-23 AT BS 344-360 WL 208 BL 0 IAW DWG 141A5400 SHEET 32 AND SRM 51-40-02.

Part: SILL — CORRODED (FUSELAGE) · airframe 43,204 hrs · 25,075 cycles

CORROSION ON AFT GALLEY DOOR MOP SILL, BS 947 TO 996 WL 208 TO 209. REMOVED AND REPLACED NEW AFT GALLEY DOOR MOPSILL IAW SRM 51-40-02.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 43,204 hrs · 25,075 cycles

BS 277-294 WL 208 RBL 2 INTERCOSTAL CRACKED AT AFT FASTENER HOLE. REMOVED AND REPLACED NEW INTERCOSTAL ITEM 141A541003 PO NUMBER 419533 AT BS 277-294 WL 208 RBL 2 IAW SRM 51-40-02 AND DWG 141A5400 SHEET 20.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 43,204 hrs · 25,075 cycles

BS 344-360 WL 208 LBL 10 INTERCOSTAL CRACKED AT AFT FASTENER HOLE. REMOVED AND REPLACED NEW INTERCOSTAL ITEM 25393 REQ NUMBER 533499 P/N 141A5410-22 AT BS 344-360 WL 208 LBL 10 IAW DWG 141A5400 SHEET 12 AND SRM 51-40-02.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,204 hrs · 25,075 cycles

BS 294 WL 208 RBL 53 FWD SERVICE DOOR FWD FRAME IS CRACKED AT FASTENER. REPAIRED FWD SERVICE DOOR FWD FRAME AT BS 294 WL 208 RBL 53 IAW SWA EA 1-753-21190.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 43,204 hrs · 25,075 cycles

BS 312-329 WL 208 RBL 32 INTERCOSTAL CRACKED AT FASTENER HOLES. REMOVED AND REPLACED NEW INTERCOSTAL ITEM 141A5410U12 PO NUMBER 419533 AT BS 312-329 WL 208 RBL 32 IAW DWG 141A5400 SHEET 39 AND SRM 51-40-02.

Part: COVER — CRACKED (EMERGENCY EXIT) · airframe 43,204 hrs · 25,075 cycles

LEFT OVERWING EXIT DOOR HANDLE COVER IS CRACKED. REPLACED LEFT OVERWING EXIT DOOR HANDLE COVER PER AMM 52-22-00, STEP 4B1F.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 43,204 hrs · 25,075 cycles

THE RT HORIZONTAL STABILIZER LWR SKIN HAS A .6 INCH CRACK AT STABILIZER STA 92.70 26 INCH FROM FWD SPAR. REPAIRED SKIN PER SRM.

Part: BEARING — LOOSE (TE FLAP) · airframe 43,204 hrs · 25,075 cycles

NR 8 CANOE FAIRING AFT ADJUSTMENT LINK BEARING LOOSE. REMOVED AND REPLACED 8 CANOE BEARING IAW MM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 43,204 hrs · 25,075 cycles

THE RT HORIZONTAL STABILIZER LWR SKIN HAS A 1.0 INCH CRACK AT STAB STA 92.70 17.5 INCH FROM FWD SPAR. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 43,204 hrs · 25,075 cycles

THE RIGHT HORIZ STAB LWR SKIN HAS A 1.0" CRACK AT STAB STA 92.70 9" FROM FWD SPAR. REPAIRED RIGHT HORIZ STAB LWR SKIN AT STAB STR 92.70, 9", 17.5" AND 26" FROM FWD SPAR PER SRM 55-10-01-2R-11

Part: WINDOW FRAME — CRACKED (COCKPIT) · airframe 43,204 hrs · 25,075 cycles

CAPTAIN'S NR 3 WINDOW FRAME IS CRACKED AT FWD EDGE 3 INCHES ABOVE FWD LOWER CORNER. REMOVED AND REPLACED CAPTAINS NR 3 WINDOW FRAME IAW SRM.

Part: LINK ASSY — LOOSE (TE FLAP) · airframe 43,204 hrs · 25,075 cycles

NR 7 CANOE FAIRING AFT ADJUSTMENT LINK BEARING IS LOOSE. REMOVED AND REPLACED NR 7 CANOE FAIRING AFT ADJUSTMENT LINK ASSY IAW AMM 27-51-28-000-804 AND AMM 27-51-28-400-804 ADJUSTMENT CHECKS GOOD IAW AMM 27-51-28-820-802.

Part: COVER — BROKEN (CABIN) · airframe 43,109 hrs · 25,016 cycles

R1 DOOR EMERGENCY EXIT LIGHT COVER BROKEN. REMOVED AND REPLACED LIGHT ASSY PER M/M.

Part: NUT PLATE — CRACKED (R1 DOOR) · airframe 41,336 hrs · 23,944 cycles

R1 DOOR EMERGENCY EVAC SLIDE AFT ATTACH POINT UPPER NUT PLATE CRACKED. REMOVED AND REPLACED PLATE PER SRM.

Part: CAP — MISSING (R2 DOOR) · airframe 41,336 hrs · 23,944 cycles

R2 DOOR EMERGENCY EVAC SLIDE COVER BUMPER AFT ENDCAP MISSING. INSTALLED COVER ASSY PER MM AND MT.

Part: BATTERY PACK — FAILED (CABIN) · airframe 39,175 hrs · 22,681 cycles

DURING SCHEDULED HC1 CHECK LT EMERGENCY EXIT LIGHT BATTERY PACK FAILED CAPACITY CHECK. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 39,175 hrs · 22,681 cycles

DURING SCHEDULED HC1 CHECK RT EMERGENCY EXIT LIGHT BATTERY PACK FAILED CAPACITY CHECK. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SLIDE — FRAYED (R2 DOOR) · airframe 36,802 hrs · 21,330 cycles

DURING SCHEDULED HC2 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE GIRT FRAYED. REMOVED AND REPLACED SLIDE PER MT.

Part: FITTING — CRACKED (CENTER WING BOX) · airframe 36,694 hrs · 21,256 cycles

DURING SCHEDULED 10Y CHECK, FOUND CENTER WING BOX SHEAR FITTING CRACKED BETWEEN BS 545 TO BS 549, RBL 14.5. REMOVED AND REPLACED FITTING PER SRM.

Part: FITTING — CRACKED (CENTER WING BOX) · airframe 36,694 hrs · 21,256 cycles

DURING SCHEDULED 10Y CHECK, FOUND CENTER WING BOX SHEAR FITTING CRACKED BETWEEN BS 547 TO BS 549, RBL 6.5. REMOVED AND REPLACED FITTING PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 36,694 hrs · 21,256 cycles

DURING SCHEDULED 10Y CHECK, FOUND FLIGHT COMPARTMENT FLOOR SUPPORT ANGLE CORRODED AT BS 260, BETWEEN LBL 10 TO RBL 10. REPAIRED FLOORBEAM PER AAR EA.

Part: FITTING — CORRODED (RT MLG TRUNNION) · airframe 35,344 hrs · 20,481 cycles

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

Part: FITTING — CORRODED (LT MLG TRUNNION) · airframe 35,344 hrs · 20,481 cycles

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

Part: LENS — LOOSE (CABIN) · airframe 34,670 hrs · 20,077 cycles

DURING SCHEDULED HC1 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE COVER LENS LOOSE. SECURED LENS PER EA.

Part: FASTENER — MISSING (GIRT BAR HOOK) · airframe 34,670 hrs · 20,077 cycles

DURING SCHEDULED HC1 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR HOOK FASTENER MISSING. INSTALLED HOOK ASSY PER SRM.

Part: LENS — LOOSE (CABIN) · airframe 34,226 hrs · 19,804 cycles

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

Part: SENSOR — FAULTY (TE FLAP) · airframe 34,037 hrs · 19,680 cycles

DIVERSION - AFTER TAKEOFF FLAPS DID NOT RAISE. FLAP LEVER WAS UP. LEFT FLAP AT POS 1 AND RT FLAP BETWEEN POS 1 & 2. WITH LED IN EXT POSITION DIVERT TO MCI. EXTEND LED USING ALT FLAP SWITCH, PER QRH. REMOVED AND REPLACED FLAP SKEW SENSOR NR 6 PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,750 hrs · 18,282 cycles

DURING SCHEDULED SPV CHECK, FOUND EMERGENCY EXIT BULLNOSE LIGHT INOP AT ROW 8. RELAMPED LIGHT PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 31,750 hrs · 18,282 cycles

DURING SCHEDULED SPV CHECK, FOUND AFT L1 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 31,701 hrs · 18,255 cycles

L1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. REPACKED SLIDE PER MT.

Part: BATTERY PACK — FAILED (CABIN) · airframe 30,234 hrs · 17,368 cycles

DURING SCHEDULED HC1 CHECK, RT EMERGENCY EXIT BATTERY PACK FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 30,234 hrs · 17,368 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,173 hrs · 17,328 cycles

DURING SCHEDULED 8Y CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 4. RELAMPED PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,173 hrs · 17,328 cycles

DURING SCHEDULED 8Y CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 30,120 hrs · 17,298 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM TEE CAP CORRODED AT BS 986, BETWEEN RBL 48 TO LBL 48, WL 208. REPAIRED BEAM PER SWA EA.

Part: COMPRESSOR — STALLED (NR 1 ENGINE) · airframe 28,115 hrs · 16,052 cycles

COMPRESSOR STALL ON NR 1 ENGINE, FLIGHT CREW REPORTED VIBRATION FOR THREE SECONDS AFTER STALL. REMOVED AND REPLACED NR 1 ENGINE PER MT.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 25,628 hrs · 14,549 cycles

DURING SCHEDULED HC1 CHECK, FOUND LT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT BS 129.5. REPAIRED SKIN PER SRM.

Part: HOOK — LOOSE (L1 DOOR GIRT BAR) · airframe 24,641 hrs · 13,972 cycles

L1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR HOOK LOOSE. SECURED HOOK PER MM.

Part: FAN — FAILED (E&E BAY) · airframe 23,444 hrs · 13,264 cycles

DECLARED EMERGENCY, CREW REPORTED STRONG ELECTRICAL ODOR IN CABIN. INSPECTED AIRCRAFT, FOUND GASPER FAN HAD FAILED. REMOVED AND REPLACED GASPER FAN PER MM.

Part: FLOORBEAM — CORRODED (BS 772) · airframe 22,715 hrs · 12,843 cycles

DURING SCHEDULED 8Y CHECK, FOUND AFT CARGO FLOORBEAM CORRODED AT BS 772, LBL 3. REPAIRED FLOORBEAM PER SWA EA.

Part: FLOOR SUPPORT — CORRODED (BS 755-779) · airframe 22,715 hrs · 12,843 cycles

DURING SCHEDULED 8Y CHECK, FOUND AFT CARGO FLOORBEAM CORRODED AT BS 755 TO BS 779, RBL 13. REPAIRED FLOORBEAM PER SRM.

Part: WINDOW — CRACKED (FLIGHT COMPT) · airframe 22,267 hrs · 12,600 cycles

DURING FLIGHT CAPTAIN'S L1 WINDOW ARCHED AND CRACKED. REMOVED AND REPLACED L1 WINDOW AND WINDOW HEAT CONTROLLER PER MM.

Part: SENSOR — FAULTY (LT WING TE FLAPS) · airframe 21,642 hrs · 12,237 cycles

DECLARED EMERGENCY/DIVERSION. T/E FLAPS POSITION NEEDLES SPLIT AT POSITION 2 WHEN FLAPS 5 SELECTED. LANDED WITH NO FURTHER PROBLEMS. REMOVED AND REPLACED NR 3 FLAP SKEW SENSOR AND CONNECTOR PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 20,886 hrs · 11,789 cycles

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

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 17,325 hrs · 9,786 cycles

DURING SCHEDULED MV3 CHECK, FOUND L2 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 15,911 hrs · 8,975 cycles

DURING SCHEDULED HC1 CHECK, CABIN EMERGENCY LIGHTING BATTERY PACKS FAILED TEST. REMOVED AND REPLACED 7 EACH BATTERY PACKS PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 13,482 hrs · 7,594 cycles

DURING SCHEDULED HC2 CHECK, FOUND FWD ENTRY DOOR EVACUATION SLIDE OUT OF ADJUST. REPOSITIONED SLIDE ASSY PER MM.

Part: COVER — CRACKED (EMERGENCY LIGHT) · airframe 11,768 hrs · 6,669 cycles

DURING SCHEDULED C2 CHECK, FOUND EEPLS COVER CRACKED THROUGH OUT CABIN. REMOVED AND REPLACED EEPLS COVERS.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 11,758 hrs · 6,661 cycles

L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM.

Part: SLIDE — UNSERVICEABLE (L1 DOOR) · airframe 10,690 hrs · 6,065 cycles

L1 DOOR EVACUATION SLIDE PRESSURE INDICATION LOW. REMOVED AND REPLACED SLIDE ASSY PER MM.

Part: LENS — MISSING (CABIN) · airframe 5,721 hrs · 3,299 cycles

DURING SCHEDULED C1 CHECK, FOUND EEPLS LENS MISSING AT ROW NR 1. INSTALLED LENS PER MM.

Part: BATTERY — WEAK (CABIN) · airframe 2,142 hrs · 1,289 cycles

DURING SCHEDULED C2 CHECK, FOUND AFT ENTRY DOOR & AFT CENTER AISLE EMERGENCYEXIT LIGHTS DIM. R&R BATTERY PACK PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 383 hrs · 215 cycles

DURING SCHEDULED SERVICE CHECK, FOUND LT OVERWING EXTERNAL EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 383 hrs · 215 cycles

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

Part: ROD — BROKEN (RT WING) · airframe 120 hrs · 76 cycles

AIR TURNBACK, AFTER FLAP RETRACTION, A/C REQUIRED 3 UNITS OF RT RUDDER AND 2 UNITS OF AILERON TRIM TO REMAIN STRAIGHT AND LEVEL. REMOVED AND REPLACED INBOARD AFT FLAP DRIVE ROD AND NR 6 FLAP TRACK FAIRING (P/N 113A9350) PER MM.