N373SW

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,333 hrs · 57,898 cycles

SKIN CRACKED AT BS 500D+4, STRINGER 2R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,333 hrs · 57,898 cycles

SKIN CRACKED AT BS 400+17, STRINGER 2L. REPAIRED SKIN IAW EA.

Part: ANGLE — CRACKED (LT WING) · airframe 69,814 hrs · 57,496 cycles

LEFT WING TE SEAL BULKHEAD LOWER ANGLE CRACKED AT WBL 209. R & R ANGLE IAW SRM.

Part: SUPPORT FITTING — CORRODED (LT WING) · airframe 69,814 hrs · 57,496 cycles

LEFT WING REAR SPAR AFT MLG BEAM SUPPORT FITTING CORRODED AT WBL 222. R & R FITTING IAW DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,814 hrs · 57,496 cycles

SKIN CRACKED AT BS 484, STRINGER 2R. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,814 hrs · 57,496 cycles

FUSELAGE SKIN CRACKED AT BS 804, STRINGER 1L. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,814 hrs · 57,496 cycles

FUSELAGE SKIN CRACKED AT BS 803, STRINGER 2R. REPAIRED SKIN IAW SRM.

Part: SPAR — CORRODED (LT WING) · airframe 69,814 hrs · 57,496 cycles

LEFT WING UPPER REAR SPAR CHORD CRACKED AT APPROX RSS 217. REPAIRED CHORD IAW EA & ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,814 hrs · 57,496 cycles

FUSELAGE SKIN CRACKED BETWEEN BS 500C+15.5 - 500C+16.6, STRINGER 2R. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,814 hrs · 57,496 cycles

SKIN CRACKED, BETWEEN BS 810 - 811.4, STRINGER 2R. REPAIRED SKIN IAW SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 69,814 hrs · 57,496 cycles

R2 DOOR LIGHT INOPERATIVE AT ROW 23. R & R LIGHT IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 69,814 hrs · 57,496 cycles

LEFT AFT TWO OVERHEAD BIN LIGHTS INOPERATIVE AT ROW 23. R & R LIGHT IAW AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,814 hrs · 57,496 cycles

FUSELAGE SKIN CRACKED, BETWEEN BS 500 - 500B+2, BETWEEN STRINGER 1R - 2R. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,814 hrs · 57,496 cycles

FUSELAGE SKIN CRACKED AT BS 500, STRINGER 1R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (R1 DOOR) · airframe 69,807 hrs · 57,494 cycles

R1 DOOR SKIN UPPER HINGE CUT OUT UPPER AFT CORNER CRACKED. R & R R1 DOOR IAW MM.

Part: LENS — BROKEN (CABIN) · airframe 68,747 hrs · 56,672 cycles

L2 DOOR EMER LIGHT LENS BROKEN. R & R LIGHT ASSEMBLY IAW AMM.

Part: STRAP — CRACKED (FUSELAGE) · airframe 68,747 hrs · 56,672 cycles

FLOOR STABILIZER STRAP CRACKED AT BS 320, LBL 10. R & R STRAP IAW SRM & DWG.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 68,747 hrs · 56,672 cycles

AFT CARGO FWD BULKHEAD PANEL SUPPORT CRACKED AT BL 0, WL166. R & R SUPPORT IAW SRM & DWG.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 68,747 hrs · 56,672 cycles

AFT LT KEEL BEAM CORRODED AT BS 720, LBL 7. REPAIRED KEEL BEAM IAW SRM.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 68,747 hrs · 56,672 cycles

AFT RT KEEL BEAM CORRODED AT BS 720, RBL 7. REPAIRED KEEL BEAM IAW SRM.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 68,747 hrs · 56,672 cycles

AFT CARGO RT VERTICAL STIFFENER CRACKED AT BS 727, RBL 6.3. R & R STIFFENER IAW DWG & SRM.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 68,747 hrs · 56,672 cycles

AFT CARGO LT VERTICAL STIFFENER CRACKED AT BS 727, LBL 6.3. R & R STIFFENER IAW DWG & SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 68,747 hrs · 56,672 cycles

SHEAR TIE CRACKED AT BS 360, BETWEEN STRINGER 14R TO 15R. REPAIRED SHEAR TIE IAW SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 68,747 hrs · 56,672 cycles

L1 DOOR LOWER HINGE LOWER FITTING CRACKED AT FUSELAGE CUT OUT. R & R FITTING IAW EA.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 68,747 hrs · 56,672 cycles

R1 DOOR CUT OUT SURFACE LOWER SILL WEB CORRODED AT FWD DRAIN HOLE. REPAIRED WEB IAW SRM.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 68,747 hrs · 56,672 cycles

RIGHT AFT CARGO BAY DOOR SUPPORT UPPER AFT CORNER SKIN CRACKED. REPAIRED DOOR IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,747 hrs · 56,672 cycles

SKIN CRACKED BETWEEN BS 500B+14 TO 500B+15, STRINGER 15R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,747 hrs · 56,672 cycles

SKIN CRACKED BETWEEN BS 868.5 - 874.25, STRINGER 1. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,747 hrs · 56,672 cycles

SKIN CRACKED BETWEEN BS 500B+6 TO 500B+7, STRINGER 16L. REPAIRED SKIN IAW SRM & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,747 hrs · 56,672 cycles

SKIN CRACKED BETWEEN BS 385 TO 386, STRINGER 15R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,747 hrs · 56,672 cycles

SKIN CRACKED BETWEEN BS 500B+4.5 TO 500B+15, STRINGER 15R. REPAIRED SKIN IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 68,747 hrs · 56,672 cycles

FRAME CRACKED AT BS 360, STRINGER 20R. REPAIRED FRAME IAW EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 68,747 hrs · 56,672 cycles

CENTER WING BOX LONGITUDINAL FLOORBEAM LOWER CHORD CRACKED AT BS 600, RBL 24.8. REPAIRED CHORD IAW EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 68,747 hrs · 56,672 cycles

CENTER WING BOX LONGITUDINAL FLOORBEAM LOWER CHORD FWD MOST FASTENER HOLE CRACKED AT BS 600, LBL 24.8. REPAIRED CHORD IAW EA.

Part: STRAP — CORRODED (FUSELAGE) · airframe 68,747 hrs · 56,672 cycles

AFT CARGO COMPARTMENT SURROUND DOUBLER STRAP CORRODED AT BS 787, BETWEEN STRINGER 25R - 26R. REPAIRED STRAP IAW EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 68,747 hrs · 56,672 cycles

FLOORBEAM UPPER CHORD T SECTION CORRODED AT BS 967, RBL 27. REPAIRED T SECTION IAW SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 68,747 hrs · 56,672 cycles

STRINGER SPLICE CRACKED AT BS 908, STRINGER 4R. R & R SPLICE IAW EA.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 68,747 hrs · 56,672 cycles

AFT CARGO COMPARTMENT FAIL SAFE STRAP LOWER SURFACE ANGLE CORRODED AT BS 807 FRAME AFT FACE 6:00 POSITION. REPAIRED ANGLE IAW SRM & EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 68,747 hrs · 56,672 cycles

FLOORBEAM CORRODED AT BS 986, BETWEEN RBL 15 - 44. REPAIRED BEAM IAW SRM.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 68,747 hrs · 56,672 cycles

TOP FLANGE OF ZEE L2 THRESHOLD CORRODED. R & R FLANGE IAW DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 68,747 hrs · 56,672 cycles

FUSELAGE FRAME CRACKED AT STATION 520, STRINGER 22L. REPAIRED FRAME IAW SRM.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 68,747 hrs · 56,672 cycles

LOWER FLANGE OF ZEE L2 THRESHOLD CORRODED. R & R FLANGE IAW DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 68,747 hrs · 56,672 cycles

FRAME CRACKED AT BS 520, BETWEEN STRINGER 20L TO 2IL. REPAIRED FRAME IAW EA & DWG.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 68,747 hrs · 56,672 cycles

LONGITUDINAL FLOORBEAM VERTICAL WEB ATTACH ANGLE CRACKED AT BS 727B, RBL 45. R & R ANGLE IAW DWG & SRM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 68,747 hrs · 56,672 cycles

LONGITUDINAL FLOORBEAM CRACKED AT STATION 676 - 686, RBL 24. REPAIRED BEAM IAW EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 68,747 hrs · 56,672 cycles

FLOORBEAM CORRODED AT BS 328, RBL 25. REPAIRED FLOORBEAM IAW SRM.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 68,747 hrs · 56,672 cycles

R1 CHORD CORRODED BETWEEN BS 291 - 332. R & R CHORD IAW SRM.

Part: TRIM PANEL — CORRODED (FUSELAGE) · airframe 68,747 hrs · 56,672 cycles

R1 DOOR FWD CUT OUT FRAME LOWER TRIM CORRODED. REPAIRED CUT OUT IAW SRM & DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 68,747 hrs · 56,672 cycles

FLOORBEAM CORRODED AT BS 312, RBL 35. REPAIRED FLOORBEAM IAW SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 68,747 hrs · 56,672 cycles

STRINGER SPLICE CRACKED AT BS 908, STRINGER 4L. R & R IAW EA.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 68,747 hrs · 56,672 cycles

STRINGER SPLICE CRACKED AT BS 908, STRINGER 5L. R & R SPLICE IAW EA.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 68,747 hrs · 56,672 cycles

R1 DOOR LOWER SILL NUTPLATE ANGLE CORRODED. R & R ANGLE IAW SRM & DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 68,747 hrs · 56,672 cycles

L2 DOOR CUT OUT THRESHOLD SUPPORT CORRODED ON UPPER SURFACE. REPAIRED CUT OUT IAW SRM & DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,747 hrs · 56,672 cycles

SKIN CRACKED BETWEEN BS 960 TO 963, STRINGER 5R. REPAIRED SKIN IAW SRM.

Part: PRESSURE DECK — CRACKED (FUSELAGE) · airframe 68,747 hrs · 56,672 cycles

MAIN WW PRESS DECK CRACKED BETWEEN BS 664 TO 675, LBL 34.50. REPAIRED DECK IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 68,747 hrs · 56,672 cycles

LEFT FUSELAGE FRAME CRACKED AT STATION 727, STRINGER 18A. REPAIRED SEAT TRACK IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 68,747 hrs · 56,672 cycles

RIGHT FUSELAGE FRAME CRACKED AT STATION 727, STRINGER 18A. REPAIRED SEAT TRACK IAW EA.

Part: SKIN — CRACKED (LE SLAT) · airframe 68,747 hrs · 56,672 cycles

RIGHT WING NR 5 SLAT SKIN CRACKED AT LOWER SIDE AFT ROW FASTENERS AT INBD AUXILIARY TRACK. REPAIRED SKIN IAW SRM.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 67,788 hrs · 56,051 cycles

AFT CABIN EMER FLASHLIGHT INOPERATIVE. R & R FLASHLIGHT ASSEMBLY IAW MM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 67,768 hrs · 56,038 cycles

FORWARD GALLEY EMER FLASHLIGHT INOPERATIVE. R & R BATTERY IAW AMM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 67,672 hrs · 55,967 cycles

FUSELAGE SKIN CORRODED AT BS 227 RBL 8. REPAIRED SKIN IAW EA.

Part: DOUBLER — DELAMINATED (LE SLAT) · airframe 66,644 hrs · 55,231 cycles

LEFT WING NR 2 SLAT OTBD TE DOUBLER WEDGE UPPER CORNER REPAIR DELAMINATED. REPAIRED DOUBLER IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,644 hrs · 55,231 cycles

FUSELAGE SKIN CRACKED BETWEEN BS 307 TO BS 307.5, STRINGER 2L. REPAIRED SKIN IAW SRM.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 66,644 hrs · 55,231 cycles

AFT PRESS BULKHEAD Z STIFFENER CRACKED AT BS 1016, STRINGER 15L. REPAIRED Z STIFFENER IAW EA.

Part: SKIN — CORRODED (FUSELAGE) · airframe 66,644 hrs · 55,231 cycles

AFT CARGO COMPARTMENT EQUIPMENT BAY SKIN CORRODED AT BS 1006, BETWEEN STRINGER 27L TO 27R. REPAIRED SKIN IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,644 hrs · 55,231 cycles

FRAME CRACKED AT BS 348.2, BETWEEN STRINGER 13L TO STRINGER 17L. R & R FRAME IAW EA.

Part: PRESSURE DECK — CRACKED (RT MLG WW) · airframe 66,622 hrs · 55,217 cycles

MLG WW PRESS DECK BEADED WEB CRACKED AT STATION 665, RBL 18. REPAIRED WEB IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,622 hrs · 55,217 cycles

FUSELAGE SKIN CRACKED AT STATION 480, STRINGER 1. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,622 hrs · 55,217 cycles

FUSELAGE SKIN CRACKED AT STATION 480, STRINGER 2L. REPAIRED SKIN IAW SRM.

Part: SLIDE — UNSECURE (R2 DOOR) · airframe 66,622 hrs · 55,217 cycles

R2 DOOR SLIDE PARTIALLY FELL OUT OF CONTAINER. R & R SLIDE IAW MT.

Part: SLIDE — LOW PRESSURE (L2 DOOR) · airframe 66,210 hrs · 54,947 cycles

L2 DOOR EMERGENCY EVAC SLIDE PRESS INDICATOR LOW. R & R SLIDE IAW MT.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 66,045 hrs · 54,833 cycles

CTR CABIN OVERHEAD EMERGENCY EXIT LIGHT INOPERATIVE. R & R BATTERY PACK IAW AMM.

Part: HINGE — BROKEN (LT SPOILER) · airframe 65,401 hrs · 54,398 cycles

LT WING NR 4 SPOILER HINGE BROKEN. R & R SPOILER IAW MM.

Part: SKIN — CRACKED (LE SLAT) · airframe 64,908 hrs · 54,041 cycles

RT WING NR 5 SLAT HAS SMALL SKIN CRACKED AT LOWER SIDE, AFT ROW FASTENERS AT INBD AUXILIARY TRACK. REPAIRED SLAT IAW SRM.

Part: ANGLE — CRACKED (RT AILERON) · airframe 64,908 hrs · 54,041 cycles

RT WING AILERON BALANCE BAY ANGLE CRACKED AT INBD SIDE OF NR 2 HINGE. R & R ANGLE IAW SRM.

Part: CONNECTOR — BROKEN (CABIN) · airframe 64,542 hrs · 53,763 cycles

FWD ENTRY EXIT LIGHT ON LOWERED CEILING STRUCTURE CONNECTOR BROKEN. R&R CONNECTOR IAW SWPM.

Part: PUMP — FAULTY (HYDRAULIC SYS) · airframe 64,542 hrs · 53,763 cycles

AIR TURNBACK, TOTAL LOSS OF B SYSTEM HYDRAULIC FLUID DURING FLAP RETRACTION, AFTER TAKEOFF. R&R NR 2 ELECTRIC HYDRAULIC PUMP NR 2 ENGINE HYDRAULIC PUMP NR 7 HYDRAULIC PUMP NR 7. SPOILER ACTUATOR IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 64,542 hrs · 53,763 cycles

RT AFT OVERHEAD BIN EMERGENCY LIGHT INOPERATIVE AT ROW 23. RELAMPED LIGHT IAW AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,542 hrs · 53,763 cycles

FS SKIN CRACKED BETWEEN BS 522.5 TO BS 527.25 STRINGER 1R. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,542 hrs · 53,763 cycles

FS SKIN CRACKED BETWEEN BS 914.5 TO BS 916.5, STRINGER 10R. REPAIRED SKIN IAW ER & EA.

Part: LENS — MISSING (EXIT SIGN) · airframe 64,375 hrs · 53,642 cycles

FWD UPPER EMERGENCY EXIT SIGN LOWER RT LIGHT LENS MISSING. R&R LIGHT IAW MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 64,259 hrs · 53,551 cycles

RT1 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. R&R BATTERY PACK HOUSING IAW M/M.

Part: SLIDE — LOOSE (R1 DOOR) · airframe 63,970 hrs · 53,344 cycles

R1 DOOR EMERGENCY EVAC SLIDE LOOSE. SECURED SLIDE IAW MM.

Part: STRAP — CRACKED (FUSELAGE) · airframe 63,073 hrs · 52,706 cycles

STRAP CRACKED AT BS 312+14" AND LEVEL RBL 24 UNDER FLOOR STRUCTURE E/E COMPARTMENT. R & R STRAP IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 63,073 hrs · 52,706 cycles

CRACK ON TIE CLIP LOCATED ON BST 380 AT LEVEL STR 22 LT. REPLACED TIE CLIP LOCATED ON BS 380 AT LEVEL STR 22L FWD CARGO COMPARTMENT IAW B737-300 SRM 51-10-02 ITEM 8, SRM 51-40-02 AND DWG 65-46525.

Part: PLATE — CRACKED (EMERGENCY EXIT) · airframe 63,073 hrs · 52,706 cycles

CRACK ON STOP PLATE BRG (4EA) OF EMERGENCY EXIT RT. REPLACED STOP PLATE BRG (4EA) AT EMERGENCY EXIT RT IAW SRM 51-10-02.

Part: WEB — CRACKED (NLG WW) · airframe 63,073 hrs · 52,706 cycles

RIGHT SIDE OF THE NLG W/W AROUND FASTENER HEAD CRACKED IN WL 169.1 AND BS 243.7+3.5. REPAIRED WEB IAW SRM.

Part: PRESSURE PANEL — CRACKED (NLG WW) · airframe 63,073 hrs · 52,706 cycles

RIGHT SIDE OF THE NLG W/W AROUND FASTENER HEAD CRACKED IN WL=169.2 AND BS 243.7+2.5. REPAIRED WEB IAW SRM.

Part: SHEAR WEB — CORRODED (FUSELAGE) · airframe 63,073 hrs · 52,706 cycles

CORROSION ON SHEAR WEB LOCATED BETWEEN BST 727E TO BST 747 AT LEVEL STR 17LT. REPLACED SHEAR WEB LOCATED BETWEEN BS 727E TO BS 747 AT LEVEL S-17L IAW SRM B737-300 51-40-02 AND DWG 65-46822, 51-10-02 ITEM 8.

Part: WEB — CRACKED (NLG WW) · airframe 63,073 hrs · 52,706 cycles

RIGHT SIDE OF THE NLG W/W AROUND FASTENER HEAD CRACK IN WL=169.1 AND BS 243.7+4.5. REPAIRED WEB IAW SRM.

Part: WEB — CRACKED (NLG WW) · airframe 63,073 hrs · 52,706 cycles

LT SIDE OF THE NLG W/W AROUND FASTENER HEAD CRACK IN WL 169.1+3.5. REPAIRED WEB IAW SRM.

Part: WEB — CRACKED (NLG WW) · airframe 63,073 hrs · 52,706 cycles

LEFT SIDE OF THE NLG W/W AROUND FASTENER HEAD CRACK IN BS 251.6 AND WL 169.1+10.5. REPAIRED WEB IAW SRM.

Part: WEB — CRACKED (NLG WW) · airframe 63,073 hrs · 52,706 cycles

LT SIDE OF NLG W/W AROUND FASTENER HEAD CRACK IN WL 169.1 AND BS 243.7+2.5. REPAIRED WEB IAW SRM.

Part: WEB — CRACKED (NLG WW) · airframe 63,073 hrs · 52,706 cycles

LEFT SIDE OF THE NLG W/W AROUND FASTENER HEAD CRACKED IN BS 251.6 AND WL169.1+11.5. REPAIRED WEB IAW SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 63,073 hrs · 52,706 cycles

CRACK INDICATION FOUND ON STRINGER SPLICE CHANNEL LOCATED STR 15L AND BS 360. REPLACED STRINGER SPLICE CHANNEL LOCATED STR 15L AND BETWEEN BS 348 TO BS 367 IAW SRM B737-300 51-10-02 PART 8 51-40-02 AND DRAWING 65-61777.

Part: SUPPORT ANGLE — CRACKED (RT PYLON) · airframe 63,073 hrs · 52,706 cycles

SUPPORT ANGLE CRACKED ON STRUCTURE OF OTBD SIDE OF PYLON RT ENG NR 2 WBL 198.6 AND FRONT SPAR INTERNAL CAVITY PYLON STRUT TORQUE BOX. R & R ANGLE IAW SRM AND DWG.

Part: SUPPORT ANGLE — CRACKED (NR 1 PYLON) · airframe 63,073 hrs · 52,706 cycles

SUPPORT ANGLE CRACKED AT STRUCTURE I/N SIDE OF PYLON LEFT ENG NR 1 WBL 183.4 AND AT LEVEL OF FRONT SPAR INTERNAL CAVITY PYLON STRUT TORQUE BOX. REPLACED ANGLE IAW SRM AND DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 63,073 hrs · 52,706 cycles

ANGLE CRACKED AT ENTRY DOOR SURROUND INTERNAL STRUCTURE BS 303.9+6, STR 8L. REPLACED ANGLE IAW SRM AND DWG.

Part: SHEAR TIE — CRACKED (ZONE 100) · airframe 63,073 hrs · 52,706 cycles

CRACK ON SHEAR TIE AT THE AFT LOWER CORNER OF THE FWD ENTRY DOOR SURRROUND INTERNAL STRUCTURE BETWEEN STR 15L AND STR 17L. REPLACED SHEAR TIE IAW SRM.

Part: BEARING — LOOSE (TE FLAP) · airframe 63,073 hrs · 52,706 cycles

LOOSE BEARINGS (2E/A) LOCATED AT FWD LOWER POSITION ON O/B MID FLAP CARRIAGE 7. REMOVED AND REPLACED (2E/A) BEARINGS LOCATED AT FWD LOWER POSITION ON O/B MIDFLAP CARRIAGE 7 RIGHT WING IAW CMM 57-53-36.

Part: BUSHING — CORRODED (LT WING TE FLAP) · airframe 63,073 hrs · 52,706 cycles

RUSTED ON BUSHING AND BOLT OF SAFETY LINK LOCATED AT OTBD FLAP CARRIAGE NR 2 LT WING. REMOVED AND REPLACED BUSHING AND BOLT IAW CMM 57-53-22 STEP 1.D (4) (5); 1B (5 )(B) 7).

Part: BUSHING — CORRODED (TE FLAP) · airframe 63,073 hrs · 52,706 cycles

RUSTED ON BUSHING AND BOLT OF SAFETY LINK LOCATED ON O/B MID FLAP CARRIAGE 7. REMOVED AND REPLACED BUSHING AND BOLT OF SAFETY LINK LOCATED ON O/B MIDFLAP CARRIAGE 7 IAW CMM 57-53-22 STEP 1.D.(4)(5),1.B.(5)(B)7).

Part: SHEAR TIE — CRACKED (BS 303) · airframe 63,073 hrs · 52,706 cycles

CRACK ON SHEAR TIE AT THE FWD ENTRY DOOR SURROUND STRUCTURE BS 303.9+6 INCH, STRINGER 15L. REPLACED SHEAR TIE IAW SRM 51-10-02 PAGE 8 AND 51-40-02 DWG.

Part: BEARING — DAMAGED (TE FLAP) · airframe 63,073 hrs · 52,706 cycles

MISSING MATERIAL LOCATED ON SPINDLE BEARING AND THRUST BEARING OF OUTBOARD FLAP TRACK CARRIAGE NR 2 LEFT WING. REMOVED AND REPLACED SPINDLE BEARING AND THRUST BEARING AT OUTBOARD FLAP TRACK CARRIAGE NR 2 LEFT WING IAW CMM 57-53-36.

Part: ANGLE — CRACKED (LT WING) · airframe 63,073 hrs · 52,706 cycles

CRACK ON ANGLE LOCATED AT WS 517.757 TRAILING EDGE AREA. REPLACED REPAIR ANGLE LOCATED AT WX 517.757 TRAILNG EDGE AREA LEFT WING IAW SRM B737-300 51-10-02 PART 8 51-40-02 AND DWG 65-46460.

Part: STRAP — BROKEN (RT WING) · airframe 63,073 hrs · 52,706 cycles

BROKEN STRAP AT WING STATION 530 REAR AREA ON RT WING WINGLET SUPPORT STRUCTURE INTERNAL FUEL TANK. REPLACED STRAP IAW SRM AND DWG.

Part: ANGLE — CRACKED (RT WING) · airframe 63,073 hrs · 52,706 cycles

CRACK ON ANGLE LOCATED AT LEVEL OF RSS 533, INTERNAL STRUCTURE OF AILERON TAB RIGHT WING. REPLACED ANGLE IAW SRM 51-40-02, SRM 51-10-02 ITEM 8 AND DWG NR65-46460.

Part: SHEAR TIE — CORRODED (BS 500) · airframe 63,073 hrs · 52,706 cycles

CORROSION ON SHEAR TIE LOCATED AT FRAME BS 500 BETWEEN STR 28L TO STR 28R FWD CARGO COMPARTMENT. REPLACED SHEARTIE LOC AT FRAME BS 500 BETWEEN STR 28L TO STR 28R FWD CARGO COMPARTMENT IAW SRM B737-300 51-10-02 ITEM 8 51-40-02 AND DWG 65-465.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 63,073 hrs · 52,706 cycles

CRACK ON TIE CLIP LOCATED AT BS 787 AND S-23R AFT CARGO COMPARTMENT. REPLACED TIE CLIP LOCATED AT BS 787 AND S-23R AFT CARGO COMPARTMENT IAW SRM B737-300 51-10-02 ITEM 8 51-40-02 AND DWG 65-46550.

Part: PLATE — BROKEN (FUSELAGE) · airframe 63,073 hrs · 52,706 cycles

BROKEN PLATE BETWEEN BS 787 AND 793.5 AND STR 22R AND STR 25R CARGO COMPARTMENT. R & R PLATE IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 63,073 hrs · 52,706 cycles

CRACK ON TIE CLIP LOCATED AT BS 727A AND S-25L AFT CARGO COMPARTMENT. REPLACED ON TIE CLIP LOCATED AT BS 727A AND S-25L AFT CARGO COMPARTMENT IAW SRM B737-300 51-10-02 ITEM 8 51-40-02 AND DWG 65-46595.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,073 hrs · 52,706 cycles

FRAME CRACKED AT BS 500D, BETWEEN STR 20R AND STR 21R. REPAIRED FRAME IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 63,073 hrs · 52,706 cycles

ANGLE CRACKED AT BS 344, BETWEEN STR 8L AND 9L. R & R ANGLE IAW SRM AND DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 63,073 hrs · 52,706 cycles

CRACK ON WEB LOCATED ON BS 500A STR 26R FLOOR STRUCTURE OF FWD CARGO COMP. REPLACED WEB LOCATED ON BS 500A STR 26R TO BS 500B FLOOR STRUCTURE OF FWD CARGO COMPARTMENT IAW SRM B737-30 51-10-02, 51-40-02 AND DRAWING 69-41473.

Part: SPINDLE — FLAKING (TE FLAP) · airframe 63,073 hrs · 52,706 cycles

FLAKED THERMAL COATING ON CARRIAGE SPINDLE NR 8. R & R SPINDLE ASSY NR 8 IAW AMM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 63,073 hrs · 52,706 cycles

FRAME CORRODED AT BS 500 AND LEVEL STR 26R CARGO DOOR CUT OUT. REPAIRED FRAME IAW EA.

Part: SPINDLE — CRACKED (TE FLAP) · airframe 63,073 hrs · 52,706 cycles

LT WING OTBD T/E FLAP OTBD SPINDLE CARRIAGE CRACKED. R & R SPINDLE ASSY IAW AMM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 63,073 hrs · 52,706 cycles

CRACK ON TIE CLIP LOCATED AT BS 927 AND S-19L AFT CARGO COMPARTMENT. REPLACED TIE CLIP LOCATED AT BS 927 AND S-19L AFT CARGO COMPARTMENT IAW B737-300 SRM 51-10-02, ITEM 8 SRM 51-40-02 AND DRAWING NR 65-46559.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 63,073 hrs · 52,706 cycles

CORROSION ON SHEAR TIE ANGLE LOCATED ON BS 827 STR 27R AFT CARGO COMP. REPLACED SHEAR TIE ANGLE LOCATED ON BS 827 STR 27R AFT CARGO COMP IAW SRM B737-300 51-10-02 ITEM 8 SRM B737-300 51-40-02 AND DRAWING 65-46552.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,073 hrs · 52,706 cycles

SKIN CRACKED AT BS 360, STR 1R. REPAIRED SKIN PER EA.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 63,073 hrs · 52,706 cycles

CRACK ON SUPPORT ANGLE LOCATED AT BS 380 AND BETWEEN STR 25L RO STR 26L FWD CARGO COMPARTMENT. REPLACED SUPPORT ANGLE AND FASTENERS LOCATED AT BS 380 AND BETWEEN STR 25L TO STR 26L FWD CC IAW B737-300 DWG 69-18388 SRM 51-40-02.

Part: FLAP — DELAMINATED (LT WING) · airframe 63,073 hrs · 52,706 cycles

DELAMINATED O/B AFT FLAP AT LEVEL FLAP TRACK FAIRING NR 1 LEFT WING. REMOVED AND REPLACED AFT FLAP ON CARD.

Part: FRAME — CORRODED (FUSELAGE) · airframe 63,073 hrs · 52,706 cycles

FRAME CORRODED AT BS 500C, BETWEEN STR 28R AND STR 27R. REPAIRED FRAME IAW SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 63,073 hrs · 52,706 cycles

TIE CLIP CRACKED AT BS 947.5, STR 26R. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 63,073 hrs · 52,706 cycles

CRACK ON HOLE (2EA) OF STRINGER 15L LOCATED BS 380+8.5" FWD PAX CABIN. REPAIRED STRINGER 15L LOCATED BETWEEN BS 380 TO BS 400 FWD PAX CABIN IAW SDRM B737-300 53-00-03 REPAIR 1 DETAIL VII. THIS REPAIR IS CATEGORY "A" REPAIR.

Part: FLAP — DELAMINATED (RT WING) · airframe 63,073 hrs · 52,706 cycles

DELAMINATION ON INBOARD EDGE OF OUTBOARD AFT FLAP RIGHT WING. REMOVED AND REPLACED O/B AFT FLAP RIGHT IAW AMM 27-51-39 STEPS ARE DOCUMENTED ON 357-335-02-02R AND MT 327-51-06 STEP 6E

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 63,073 hrs · 52,706 cycles

SHEAR TIE CRACKED AT BS 380, BETWEEN STR 14L TO STR 15L. REPAIRED SHEAR TIE IAW SRM.

Part: GUSSET — CRACKED (VERTICAL STAB) · airframe 63,073 hrs · 52,706 cycles

CRACK ON GUSSET LOCATED FIN STA 136.30 INTERNAL AREA VERTICAL STABILIZER. REPLACED GUSSET LOCATED FIN STA 136.30 INTERNAL AREA VERTICAL STABILIZER IAW SRM B737-300 51-10-02 ITEM 8 AND DWG 65-47401.

Part: COVER — BROKEN (EMERGENCY EXIT) · airframe 63,073 hrs · 52,706 cycles

BROKEN COVER OF EMERGENCY EXIT HANDLE LEFT SIDE. REPLACED COVER OF EMERGENCY EXIT HANDLE LEFT SIDE IAW AMM 52-21-12.

Part: ANGLE — CRACKED (RT WING) · airframe 63,073 hrs · 52,706 cycles

CRACK ON ANGLE LOCATED BS 540 AND AT LEVEL WBL 71.24 RIGHT WING. REPLACED ANGLE LOCATED BST 540 AT LEVEL WBL 71-24 RIGHT WING IAW SRM B737-300 51-10-02 PART 8 AND DRAWING 69-38865.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,073 hrs · 52,706 cycles

FUSELAGE SKIN CRACKED AT BS 907+14, STR 25R. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,073 hrs · 52,706 cycles

CRACK ON FUSELAGE SKIN LOCATED BS 380+7.5" AND STR 15L UPPER LOBE L=0.500" APPROX. REPAIRED FUSELAGE SKIN CHEM-MILL BETWEEN BSTA 375 TO BSTA 395 AND BETWEEN STR 14L TO STR 16L IAW EA 1-353-21615.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,073 hrs · 52,706 cycles

FUSELAGE SKIN CRACKED AT BS 967+4, STR 21L. REPAIRED SKIN IAW EO.

Part: PLATE — CRACKED (VERTICAL STAB) · airframe 63,073 hrs · 52,706 cycles

CRACK ON PLATE LOCATED AT ACCESS PANEL N. 9501 LEFT FWD FIN VERTICAL STABILIZER. REPLACED PLATE LOCATED AT ACCESS PANEL N. 9501 LEFT FWD FIN VERTICAL STABILIZER IAW SRM B737-300 51-10-02 ITEM 8 AND DRAWING N. 65-48249 AND SRM B737-300 51-40-02.

Part: MOUNT BOLT — LOOSE (R1 DOOR) · airframe 62,708 hrs · 52,441 cycles

FWD SERVICE DOOR ESCAPE SLIDE AFT MOUNT BOLT LOOSE. SECURED BOLT & BRACKET IAW M/M. OP'S CHECKS GOOD.

Part: COVER — UNSECURE (EXIT SIGN) · airframe 62,155 hrs · 52,033 cycles

LEFT MID CABIN EMERGENCY EXIT SIGN COVER FELL OFF. INSTALLED COVER PER MM.

Part: ACTUATOR — CRACKED (RT SPOILER) · airframe 61,026 hrs · 51,192 cycles

RIGHT WING NR 9 GROUND SPOILER CRACKED. REMOVED AND REPLACED ACTUATOR PER M/M.

Part: LENS — MISSING (CABIN) · airframe 60,493 hrs · 50,801 cycles

RT OVERHEAD BULLNOSE EMERGENCY EXIT LIGHT LENS MISSING AT ROW 8. REMOVED AND REPLACED LENS PER M/M.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,490 hrs · 50,800 cycles

SKIN CRACKED AT BS 392.5, STR 1L. REPAIRED SKIN PER SRM.

Part: LIGHT — LOOSE (CABIN) · airframe 60,159 hrs · 50,559 cycles

RIGHT EEPLS LOOSE AT ROW 8. SECURED EEPLS PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 59,239 hrs · 49,866 cycles

DURING SCHEDULED CV CHECK, FOUND RT EMERGENCY EXIT DOOR LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 58,083 hrs · 48,981 cycles

DURING SCHEDULED 18Y CHECK FOUND, STRINGER CLIP CRACKED AT BS 616, STR 5L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 58,083 hrs · 48,981 cycles

DURING SCHEDULED 18Y CHECK FOUND, STRINGER CLIP CRACKED AT BS 400, STR 8R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 58,083 hrs · 48,981 cycles

DURING SCHEDULED 18Y CHECK FOUND, STRINGER CLIP CRACKED AT BS 685, STR 4L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 58,083 hrs · 48,981 cycles

DURING SCHEDULED 18Y CHECK FOUND, STRINGER CLIP CRACKED AT BS 727B, STR 7R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 58,083 hrs · 48,981 cycles

DURING SCHEDULED 18Y CHECK FOUND, STRINGER CLIP CRACKED AT STA, 440 STR 1. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 58,083 hrs · 48,981 cycles

DURING SCHEDULED 18Y CHECK FOUND, STRINGER CLIP CRACKED AT 727D, STR 5R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 58,083 hrs · 48,981 cycles

DURING SCHEDULED 18Y CHECK FOUND, STRINGER CLIP CRACKED AT BS 727A, STR 7R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 58,083 hrs · 48,981 cycles

DURING SCHEDULED 18Y CHECK FOUND, STRINGER CLIP CRACKED AT BS 727A, STR 4R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 58,083 hrs · 48,981 cycles

DURING SCHEDULED 18Y CHECK FOUND, STRINGER CLIP CRACKED AT BS 727C, STR 5R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 58,083 hrs · 48,981 cycles

DURING SCHEDULED 18Y CHECK FOUND, STRINGER CLIP CRACKED AT BS 727D, STR 6R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 58,083 hrs · 48,981 cycles

DURING SCHEDULED 18Y CHECK FOUND, STRINGER CLIP CRACKED AT BS 597 STR 8R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 58,083 hrs · 48,981 cycles

DURING SCHEDULED 18Y CHECK FOUND, STRINGER CLIP CRACKED AT BS 616 STR 2L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 58,083 hrs · 48,981 cycles

DURING SCHEDULED 18Y CHECK FOUND, STRINGER CLIP CRACKED AT BS 727C, STR 6R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 58,083 hrs · 48,981 cycles

DURING SCHEDULED 18Y CHECK FOUND, STRINGER CLIP CRACKED AT BS 727C, STR 4R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 58,083 hrs · 48,981 cycles

DURING SCHEDULED 18Y CHECK FOUND, STRINGER CLIP CRACKED AT 639, STR 2L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 58,083 hrs · 48,981 cycles

DURING SCHEDULED 18Y CHECK FOUND, STRINGER CLIP CRACKED AT BS 500D, STR 5R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 58,083 hrs · 48,981 cycles

DURING SCHEDULED 18Y CHECK FOUND, STRINGER CLIP CRACKED AT BS 360 STR 5L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 58,083 hrs · 48,981 cycles

DURING SCHEDULED 18Y CHECK FOUND, STRINGER CLIP CRACKED AT BS 639, STR 2R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 58,083 hrs · 48,981 cycles

DURING SCHEDULED 18Y CHECK FOUND, STRINGER CLIP CRACKED AT BS 727C, STR 2L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 58,083 hrs · 48,981 cycles

DURING SCHEDULED 18Y CHECK FOUND, STRINGER CLIP CRACKED AT BS 727A, STR 8L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 58,083 hrs · 48,981 cycles

DURING SCHEDULED 18Y CHECK FOUND, STRINGER CLIP CRACKED AT BS 747, STR 4L. REMOVED AND REPLACED CLIP PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 58,084 hrs · 48,981 cycles

DURING SCHEDULED 18Y CHECK FOUND, SHEAR TIE CORRODED AT BS 847, BETWEEN STR 27L TO STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,084 hrs · 48,981 cycles

DURING SCHEDULED 20Y CHECK FOUND, SKIN CRACKED AT BS 500C+4, STR 10R. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,084 hrs · 48,981 cycles

DURING SCHEDULED 18Y CHECK FOUND, SKIN CRACKED BETWEEN BS 416-417.5, STR 15R. REPAIRED SKIN PER EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 58,083 hrs · 48,981 cycles

DURING SCHEDULED 18Y CHECK, FOUND CORROSION ON SHEAR TIE BS 787 STR 26-27R. REPAIRED PER SRM.

Part: SHEAR TIE — CORRODED (BS 787 S25-26R) · airframe 58,083 hrs · 48,981 cycles

DURING SCHEDULED 18Y CHECK, FOUND CORROSION ON SHEAR TIE BS 787 STR 25-26R. REPAIRED PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 58,084 hrs · 48,981 cycles

DURING SCHEDULED 18Y CHECK, FOUND SHEAR TIE CORRODED AT BS 727E, BETWEEN STR 25L TO STR 26L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 58,084 hrs · 48,981 cycles

DURING SCHEDULED 18Y CHECK, FOUND FRAME CRACKED AT BS 500B, BETWEEN STR 20L TO STR 21L. REPAIRED FRAME PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,084 hrs · 48,981 cycles

DURING SCHEDULED 18Y CHECK, FOUND SKIN CRACKED BETWEEN BS 945.25 TO BS 946.75, STR 23R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,084 hrs · 48,981 cycles

DURING SCHEDULED 18Y CHECK, FOUND SKIN CRACKED AT BS 752, STR 4L. REPAIRED SKIN PER ACO AND BAC DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,084 hrs · 48,981 cycles

DURING SCHEDULED 18Y CHECK, FOUND SKIN CRACKED AT BS 800, STR 4L. REPAIRED SKIN PER ACO AND BAC DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,084 hrs · 48,981 cycles

DURING SCHEDULED 18Y CHECK, FOUND SKIN CRACKED AT BS 727D+12, STR 4R. REPAIRED SKIN PER ACO AND BAC DWG.

Part: WEB — CORRODED (FUSELAGE) · airframe 58,084 hrs · 48,981 cycles

DURING SCHEDULED 18Y CHECK, FOUND AFT CARGO DOOR THRESHOLD CLOSE OUT WEB CORRODED BETWEEN BS 794 TO BS 867, BETWEEN RBL 21 TO RBL 28. REPAIRED WEB PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,084 hrs · 48,981 cycles

DURING SCHEDULED 18Y CHECK, FOUND SKIN CRACKED AT BS 727C+3, STR 4L. REPARIED SKIN PER ACO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,084 hrs · 48,981 cycles

DURING SCHEDULED 18Y CHECK, FOUND SKIN CRACKED AT BS 811, STR 4L. REPAIRED SKIN PER ACO.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 58,084 hrs · 48,981 cycles

DURING SCHEDULED 20Y CHECK, FOUND CRACKED TIE CLIP BS 663 AND 10R. REPAIRED CHANNEL PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,084 hrs · 48,981 cycles

DURING SCHEDULED 18Y CHECK, FOUND SKIN CRACKED AT BS 717A+14.5, STR 4L. REPARIED SKIN PER ACO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,084 hrs · 48,981 cycles

DURING SCHEDULED 18Y CHECK, FOUND SKIN CRACKED AT BS 727B+3, STR 4L. REPAIRED SKIN PER ACO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,084 hrs · 48,981 cycles

DURING SCHEDULED 18Y CHECK, FOUND SKIN CRACKED AT BS 717A+13, STR 4L. REPAIRED SKIN PER ACO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,084 hrs · 48,981 cycles

DURING SCHEDULED 18Y CHECK, FOUND SKIN CRACKED AT BS 807, STR 4L. REPAIRED SKIN PER ACO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,084 hrs · 48,981 cycles

DURING SCHEDULED 18Y CHECK, FOUND SKIN CRACKED AT BS 727D+6, STR 4L. REPAIRED SKIN PER ACO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,084 hrs · 48,981 cycles

DURING SCHEDULED 18Y CHECK, FOUND SKIN CRACKED AT BS 526, STR 4L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,084 hrs · 48,981 cycles

DURING SCHEDULED 18Y CHECK, FOUND SKIN CRACKED AT BS 798, STR 7R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,084 hrs · 48,981 cycles

DURING SCHEDULED 18Y CHECK, FOUND SKIN CRACKED AT BS 436, STR 4L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,084 hrs · 48,981 cycles

DURING SCHEDULED 18Y CHECK, FOUND SKIN CRACKED BETWEEN BS 416 TO BS 417.5, STR 15R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,084 hrs · 48,981 cycles

DURING SCHEDULED 18Y CHECK, FOUND SKIN CRACKED BETWEEN BS 500D+3.5 TO +7, STR 4R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,084 hrs · 48,981 cycles

DURING SCHEDULED 18Y CHECK, FOUND SKIN CRACKED AT BS 892, STR 4R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,084 hrs · 48,981 cycles

DURING SCHEDULED 18Y CHECK, FOUND SKIN CRACKED AT BS 500B+15, STR 4R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,084 hrs · 48,981 cycles

DURING SCHEDULED 18Y CHECK, FOUND SKIN CRACKED BETWEEN BS 761.5 TO BS 762.5, STR 10R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,084 hrs · 48,981 cycles

DURING SCHEDULED 18Y CHECK, FOUND SKIN CRACKED AT BS 500C+5, STR 4L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,084 hrs · 48,981 cycles

DURING SCHEDULED 18Y CHECK, FOUND SKIN CRACKED AT BS 500B+3, STR 4R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,084 hrs · 48,981 cycles

DURING SCHEDULED 18Y CHECK, FOUND SKIN CRACKED AT BS 495, STR 4R. REPAIRED SKIN PER SRM.

Part: LUG — BROKEN (SPOILER) · airframe 57,832 hrs · 48,801 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT WING NR 4 GROUND SPOILER O/B ACTUATOR ATTACH FITTING LUG BROKEN. REMOVED AND REPLACED SPOILER PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 57,689 hrs · 48,686 cycles

DURING SCHEDULED MV3 CHECK, FOUND FLIGHT DECK EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,511 hrs · 47,789 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 501C, STR 15R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,511 hrs · 47,789 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 977.5, STR 21L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,511 hrs · 47,789 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 511D, STR 16L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,511 hrs · 47,789 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 934, STR 24L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,511 hrs · 47,789 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 977.5, STR 21L. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,660 hrs · 47,146 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 444.5, STR 10L. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,660 hrs · 47,146 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 790, STR 4L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,660 hrs · 47,146 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 504B, STR 4L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,660 hrs · 47,146 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 483.5, STR 4L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,660 hrs · 47,146 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 513.3B, STR 10L. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,660 hrs · 47,146 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 780, STR 4L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,660 hrs · 47,146 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 513.5B, STR 10L. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,664 hrs · 47,147 cycles

DURING SCHEDULED OTS, FOUND FUSELAGE SKIN CRACKED AT BS 504B, STR 4L. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 54,951 hrs · 46,622 cycles

L1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,825 hrs · 46,528 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND SKIN CRACKED AT BS 476, STR 10L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,825 hrs · 46,528 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND SKIN CRACKED AT BS 503D, STR 10R. REPAIRED SKIN PER SRM.

Part: COVER — CRACKED (R1 DOOR) · airframe 54,825 hrs · 46,528 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE COVER CRACKED. REPAIRED SLIDE COVER PER EA.

Part: COVER — LOOSE (CABIN) · airframe 54,825 hrs · 46,528 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND L1 DOOR LOWER EMERGENCY EXIT LIGHT COVER LOOSE. SECURED COVER PER MM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 54,135 hrs · 46,032 cycles

AFT GALLEY EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: LIGHT — BROKEN (CABIN) · airframe 53,925 hrs · 45,871 cycles

RIGHT EEPLS BROKEN AT ROW 8. REMOVED AND REPLACED EEPLS PER MM.

Part: GASPER FAN — FAULTY (COCKPIT) · airframe 53,130 hrs · 45,275 cycles

SMELLED SLIGHT ELECTRICAL ODOR IN COCKPIT. REMOVED AND REPLACED GASPER FAN PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,901 hrs · 45,112 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 515D, STR 16R. REPAIRED SKIN PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 52,538 hrs · 44,838 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 794, BETWEEN STR 25R TO STR 26R. REPAIRED FRAME PER ACO.

Part: SKIN — DELAMINATED (RT WING) · airframe 52,538 hrs · 44,838 cycles

DURING SCHEDULED 16Y CHECK, FOUND RT WING O/B AFT FLAP LOWER SURFACE DELAMINATED. REPAIRED AFT FLAP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,538 hrs · 44,838 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME WEB CRACKED AT BS 303, STR 16L. REPAIRED FRAME PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,538 hrs · 44,838 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 360, STR 11L. REPAIRED SKIN PER AAR EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,538 hrs · 44,838 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 303.9, STR 16L. REPAIRED FRAME PER ACO.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 52,538 hrs · 44,838 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO FLOORBEAM CORRODED AT BS 772, LBL 3. REPAIRED BEAM PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,538 hrs · 44,838 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED BS 663, STR 10R. REMOVED AND REPLACED CLIP PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 52,538 hrs · 44,838 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM CORRODED AT BS 987, LBL 48. REPAIRED BEAM PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 52,538 hrs · 44,838 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 747, BETWEEN STR 26R TO STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,538 hrs · 44,838 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 11R. REMOVED AND REPLACED CLIP PER SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 52,538 hrs · 44,838 cycles

DURING SCHEDULED 16Y CHECK, FOUND DOOR ANGLE CRACKED AT BS 291.5, BETWEEN STR 11R TO STR 12R. REPAIRED ANGLE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,538 hrs · 44,838 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 20R. REMOVED AND REPLACED CLIP PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 52,538 hrs · 44,838 cycles

DURING SCHEDULED 16Y CHECK, FOUND LT FLOORBEAM UPPER CAP CRACKED AT BS 328, LBL 28. REPAIRED BEAM PER SRM.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 52,538 hrs · 44,838 cycles

DURING SCHEDULED 16Y CHECK, FOUND LT WING NR 1 SLAT UPPER SURFACE O/B END DELAMINATED. REPAIRED SLAT PER SRM.

Part: FLAP — DELAMINATED (LT WING) · airframe 52,538 hrs · 44,838 cycles

DURING SCHEDULED 16Y CHECK, FOUND LT WING O/B AFT FLAP O/B UPPER END DELAMINATED. REPAIRED AFT FLAP PER SRM.

Part: ATTACH FITTING — CORRODED (GIRT BAR) · airframe 52,538 hrs · 44,838 cycles

DURING SCHEDULED 16Y CHECK, FOUND L1 DOOR LOWER AFT GIRT BAR ATTACH MOUNT FITTING CORRODED AT BS 344. REMOVED AND REPLACED FITTING PER SRM.

Part: ATTACH FITTING — CORRODED (GIRT BAR) · airframe 52,538 hrs · 44,838 cycles

DURING SCHEDULED 16Y CHECK, FOUND L1 DOOR LOWER FWD GIRT BAR ATTACH MOUNT FITTING CORRODED AT BS 312. REMOVED AND REPLACED FITTING PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,538 hrs · 44,838 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 25R. REMOVED AND REPLACED CLIP PER SRM.

Part: LENS — LOOSE (CABIN) · airframe 52,538 hrs · 44,838 cycles

DURING SCHEDULED 16Y CHECK, FOUND RT SIDEWALL EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 52,538 hrs · 44,838 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO PIT SKIN CUTOUT CORRODED AT BS 727D +11, BETWEEN STR 27L TO STR 27R. REPAIRED SKIN PER BOEING DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,538 hrs · 44,838 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 25R. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,537 hrs · 44,838 cycles

DURING SCHEDULED MV2 CHECK, FOUND RADIO ALTIMETER CUTOUT FUSELAGE BELLY SKIN CRACKED AT BS 410. REPAIRED SKIN PER SWA EA.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 52,049 hrs · 44,512 cycles

DURING SCHEDULED MV2 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT COVER MISSING AT ROW 8. INSTALLED COVER PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,879 hrs · 44,389 cycles

DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SWA EA.

Part: SPOILER — DELAMINATED (RT WING) · airframe 51,879 hrs · 44,389 cycles

DURING SCHEDULED HC2 CHECK, FOUND RT WING NR 7 SPOILER DELAMINATED. REMOVED AND REPLACED SPOILER PER MM.

Part: COVER — MISSING (CABIN) · airframe 51,683 hrs · 44,250 cycles

DURING SCHEDULED MV2 CHECK, FOUND BULLNOSE LIGHT LENS COVER MISSING AT ROW 8. INSTALLED COVER PER MM.

Part: COVER — MISSING (CABIN) · airframe 51,683 hrs · 44,250 cycles

DURING SCHEDULED MV2 CHECK, FOUND BULL NOSE LIGHT COVER MISSING AT ROW 8. INSTALLED COVER PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,423 hrs · 44,060 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 420, STR 2R. REPAIRED SKIN PER SWA EA.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 51,173 hrs · 43,877 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CRACKED AT BS 492, STR 16R. REPAIRED STRINGER PER SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 51,173 hrs · 43,877 cycles

DURING SCHEDULED SPV CHECK, FOUND FWD CARGO DOOR CUTOUT AFT FRAME CRACKED AT LOWER STOP FITTING. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,173 hrs · 43,877 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BETWEEN BS 500D + 1 TO 500D + 3, STR 12R. REPAIRED SKIN PER SWA EA.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 51,173 hrs · 43,877 cycles

DURING SCHEDULED SPV CHECK, FOUND FWD CARGO DOOR CUTOUT FWD FRAME CRACKED AT LOWER STOP FITTING. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: SIGN — BROKEN (CABIN) · airframe 51,008 hrs · 43,755 cycles

FOUND FWD OVERHEAD EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED LENS ASSY PER MM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 50,861 hrs · 43,639 cycles

DURING SCHEDULED MV2 CHECK, FOUND STRINGER CRACKED AT BS 500B + 2.4, STR 10R. REPAIRED STRINGER PER SRM.

Part: FLOOR SUPPORT — CRACKED (BS 706-708) · airframe 50,261 hrs · 43,205 cycles

DURING SCHEDULED HC1 CHECK, FOUND LONGITUDINAL FLOOR SUPPORT WEB CRACKED AT BS 706 AND BS 708, LBL 25. REPAIRED FLOOR SUPPORT PER ER.

Part: KEELBEAM — CORRODED (BS 504D) · airframe 50,261 hrs · 43,205 cycles

DURING SCHEDULED HC1 CHECK, FOUND KEELBEAM CORRODED AT BS 504D, STR 28L, WL 148. REPAIRED KEELBEAM PER SRM.

Part: SKIN — CRACKED (BS 503C S15L) · airframe 50,261 hrs · 43,205 cycles

DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 503C, STR 15L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,893 hrs · 42,951 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT ENTRY DOOR LOWER FWD CORNER. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,336 hrs · 42,554 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 430, RBL 4. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,336 hrs · 42,554 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 410, RBL 2. REPAIRED SKIN PER SWA EA.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 49,336 hrs · 42,554 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,336 hrs · 42,554 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 450, LBL 4. REPAIRED SKIN PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,634 hrs · 42,038 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727D, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,634 hrs · 42,038 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8L. REPAIRED FRAME PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,634 hrs · 42,038 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 415 TO BS 429, STR 1. REPAIRED SKIN PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,634 hrs · 42,038 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8R. REPAIRED FRAME PER SWA EA.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 48,634 hrs · 42,038 cycles

DURING SCHEDULED 14Y CHECK, FOUND LT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 152. REPAIRED SKIN PER BOEING SB.

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,634 hrs · 42,038 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727D, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,634 hrs · 42,038 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8R AND STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,634 hrs · 42,038 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,634 hrs · 42,038 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,634 hrs · 42,038 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,634 hrs · 42,038 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,634 hrs · 42,038 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,634 hrs · 42,038 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,634 hrs · 42,038 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8L. REPAIRED FRAME PER SWA EA.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 48,634 hrs · 42,038 cycles

DURING SCHEDULED 14Y CHECK, FOUND L2 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED BATTERY CHARGER PER MM.

Part: SKIN — CRACKED (BS 450) · airframe 48,634 hrs · 42,038 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 450, RBL 1.5. REPAIRED SKIN PER ACO.

Part: SKIN — CRACKED (BS 430) · airframe 48,634 hrs · 42,038 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 430, RBL 3. REPAIRED SKIN PER ACO.

Part: SKIN — CRACKED (BS 410) · airframe 48,634 hrs · 42,038 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 410, RBL 2. REPAIRED SKIN PER ACO.

Part: SKIN — CRACKED (BS 486 S10R) · airframe 48,368 hrs · 41,843 cycles

DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 486, STR 10R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,875 hrs · 41,469 cycles

DURING SCHEDULED C2 CHECK, FOUND R1 DOOR FUSELAGE SKIN CRACKED AT LOWER HINGE CUTOUT. REPAIRED SKIN PER SWA EA.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 47,521 hrs · 41,176 cycles

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

Part: FIRE WARNING — MALFUNCTIONED (COCKPIT) · airframe 47,201 hrs · 40,927 cycles

DECLARED EMERGENCY. DESCENDING INTO SEA FWD CARGO FIRE LIGHT ILLUMINATED, DISCHARGED FIRE BOTTLES. NO EVIDENCE OF FIRE. REMOVED AND REPLACED FIRE BOTTLES AND SQUIBS PER MM.

Part: SKIN — CRACKED (R1 DOOR) · airframe 46,979 hrs · 40,746 cycles

DURING SCHEDULED C1 CHECK, FOUND R1 DOOR SKIN CRACKED AT LOWER AFT CORNER. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (R1 DOOR) · airframe 46,979 hrs · 40,746 cycles

DURING SCHEDULED C1 CHECK, FOUND R1 DOOR SKIN CRACKED AT UPPER FWD CORNER. REPAIRED SKIN PER SRM.

Part: COFFEEMAKER — FAULTY (GALLEY) · airframe 46,278 hrs · 40,219 cycles

F/A REPORTED ELECTRICAL ODOR COMING FROM AFT GALLEY COFFEEMAKER, F/A PULLED C/B AS PRECAUTIONARY MEASURE. INSPECTED AFT GALLEY AREA ISOLATED FAULT TO NR 1 COFFEEMAKER. REMOVED AND REPLACED NR 1 COFFEEMAKER PER MM.

Part: GENERATOR — FAULTED (NR 1) · airframe 46,249 hrs · 40,197 cycles

DIVERSION, EQUIPMENT COOLING OFF LIGHT ILLUMINATED AT FL 350, SWITCHED TO ALTERNATE PER QRH. F/A REPORTED HOT ELECTRICAL ODOR, NO SMOKE IN CABIN. NR 1 GEN SHOWING LOW VOLTS AND FREQS, PUT APU ON BUSS NR 1 SIDE. REMOVED AND REPLACED NR 1 GEN AND EQUIPMENT COOLING FAN PER MM.

Part: SKIN — CRACKED (R1 DOOR) · airframe 45,954 hrs · 39,962 cycles

DURING SCHEDULED SPV CHECK, FOUND R1 DOOR SKIN CRACKED AT BS 304, STR 15R. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (R1 DOOR) · airframe 45,943 hrs · 39,954 cycles

DURING SCHEDULED SPV CHECK, FOUND R1 DOOR SKIN CRACKED AT BS 316, STR 10R. REPAIRED SKIN PER SRM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 45,729 hrs · 39,790 cycles

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

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 44,139 hrs · 38,550 cycles

DURING SCHEDULED C2 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 44,139 hrs · 38,550 cycles

DURING SCHEDULED C2 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: SIGN — BROKEN (CABIN) · airframe 43,991 hrs · 38,434 cycles

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

Part: SIGN — BROKEN (EMERGENCY EXIT) · airframe 43,953 hrs · 38,405 cycles

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

Part: HINGE — WORN (LT ELEVATOR TAB) · airframe 43,338 hrs · 37,929 cycles

DURING SCHEDULED C1 CHECK, LT ELEVATOR NR 1 TAB HINGE, FAILED FREE PLAY CHECK. REMOVED AND REPLACED NR 1 TAB HINGE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 43,338 hrs · 37,929 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 943.5, STR 25R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 43,338 hrs · 37,929 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT EQUIPMENT COOLING EXHAUST CUTOUT, BS 378.3, LBL 2.8. REPAIRED SKIN PER SWA EA.

Part: SIGN — BROKEN (CABIN) · airframe 43,338 hrs · 37,929 cycles

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

Part: SIGN — BROKEN (CABIN) · airframe 43,334 hrs · 37,925 cycles

L2 DOOR EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED EMERGENCY EXIT SIGN PER MM.

Part: LENS — LOOSE (CABIN) · airframe 42,925 hrs · 37,601 cycles

DURING SCHEDULED SERVICE CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 42,415 hrs · 37,233 cycles

DURING SCHEDULED C4 CHECK, FOUND FWD CABIN EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM.

Part: SLIDE — LOOSE (R2 DOOR) · airframe 42,415 hrs · 37,233 cycles

DURING SCHEDULED C4 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE LOOSE. SECURED SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 42,415 hrs · 37,233 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR UPPER HINGE CUTOUT BEAR STRAP, BS 303.90, WL 259.88. REPAIRED SKIN PER SRM.

Part: HINGE FITTING — CRACKED (L1 DOOR) · airframe 42,415 hrs · 37,233 cycles

DURING SCHEDULED C4 CHECK, FOUND L1 DOOR UPPER HINGE BOX FITTING CRACKED. MX FERRY TO DHN FOR REPAIRS. REPAIRED HINGE BOX PER SWA EA.

Part: FLOORBEAM — CRACKED (BS 668) · airframe 41,050 hrs · 36,152 cycles

DURING SCHEDULED 1/4D CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 668, RBL 24.75. REPAIRED FLOORBEAM PER SWA EA.

Part: FLOORBEAM — CRACKED (BS 668) · airframe 41,050 hrs · 36,152 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM CRACKED AT BS 668, LBL 24.75. REPAIRED FLOORBEAM PER SWA EA.

Part: SKIN — CRACKED (BS 500D + 18) · airframe 41,050 hrs · 36,152 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D + 18, STR 12L. REPAIRED SKIN PER SWA EA.

Part: FLOORBEAM — CORRODED (BS 845) · airframe 41,050 hrs · 36,152 cycles

DURING SCHEDULED 1/4D CHECK, FOUND LONGITUDINAL FLOORBEAM CORRODED AT BS 845, LBL 8. REPAIRED FLOORBEAM PER SWA EA.

Part: STIFFENER — CORRODED (BS 1016) · airframe 41,050 hrs · 36,152 cycles

DURING SCHEDULED 1/4D CHECK, FOUND LT CHANNEL STIFFENER CORRODED AT BS 1016 BULKHEAD, BL 0. REPAIRED STIFFENER PER BOEING DRAWING.

Part: TERMINAL — FAULTY (TE FLAPS) · airframe 40,406 hrs · 35,608 cycles

AIR TURNBACK, AFTER DEPARTURE, L/E FLAPS TRANSIT LIGHT AND NR 1 FLAP OVERHEAD LIGHT STAYED ILLUMINATED. RECYCLED FLAPS, NO CHANGE. REMOVED AND REPLACED NR 1 FLAP GROUND TERMINAL PER MM.

Part: FAN — FAULTY (E&E BAY) · airframe 38,667 hrs · 34,201 cycles

DECLARED EMERGENCY, 25 MINUTES OUT OF AUS, F/A'S NOTICED AND SMELLED SMOKE IN CABIN. COULD NOT DETERMINE IF SMOKE WAS ELECTRICAL OR FROM PACKS. REMOVED AND REPLACED GASPER FAN PER MM.

Part: SKIN — DELAMINATED (LT WING FLAP) · airframe 38,475 hrs · 34,041 cycles

DURING SCHEDULED A1 CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP DELAMINATED. REPAIRED LT T/E AFT FLAP PER SRM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 37,821 hrs · 33,531 cycles

DURING SCHEDULED SERVICE CHECK, FOUND BULL NOSE EMERGENCY EXIT LIGHT AT ROW 2 ABC, INOP. RELAMPED LIGHT PER MM.

Part: COVER — LOOSE (EMERGENCY LIGHT) · airframe 36,061 hrs · 32,082 cycles

DURING SCHEDULED SERVICE CHECK, FOUND RT EMERGENCY EXIT DOOR EXIT LIGHT COVER LOOSE. SECURED EMERGENCY EXIT LIGHT COVER PER MM.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 33,188 hrs · 29,758 cycles

DURING SCHEDULED D CHECK, FOUND EEPLS INOP ( 5 EA ) IN AFT CABIN. R&R POWER SUPPLY PER MM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 33,188 hrs · 29,758 cycles

DURING SCHEDULED D-CHECK, FOUND CREASE BEAM WEB CORRODED BETWEEN BS 887 AND BS 907, RT SIDE. REPAIRED CREASE BEAM WEB PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 33,188 hrs · 29,758 cycles

DURING SCHEDULED D-CHECK, FOUND CREASE BEAM WEB CORRODED BETWEEN BS 727D AND BS 727C, LT SIDE. REPAIRED CREASE BEAM WEB PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 33,188 hrs · 29,758 cycles

DURING SCHEDULED D-CHECK, FOUND CREASE BEAM WEB CORRODED BETWEEN BS 360 AND BS 380, BS 460 AND BS 488 AND BETWEEN BS 727D AND BS 727E, RT SIDE. REPAIRED CREASE BEAM WEB PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 33,188 hrs · 29,758 cycles

DURING SCHEDULED D-CHECK, FOUND SHEAR TIE CRACKED AT BS 360, STR 13L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SKIN — DELAMINATED (LT & RT SLATS) · airframe 33,188 hrs · 29,758 cycles

DURING SCHEDULED D-CHECK, FOUND NR 2 AND NR 5 L/E SLATS DELAMINATED. REPAIRED NR 2 AND NR 5 L/E SLAT PER SRM.

Part: BEAM — CORRODED (FUSELAGE) · airframe 33,188 hrs · 29,758 cycles

DURING SCHEDULED D-CHECK, FOUND LT CREASE BEAM WEB CORRODED FROM BS 747 TO BS 889. REPAIRED CREASE BEAM WEB PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 33,188 hrs · 29,758 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT SERVICE DOOR CUTOUT, FWD LOWER CORNER. REPAIRED SKIN PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,188 hrs · 29,758 cycles

DURING SCHEDULED D-CHECK, FOUND BOTH LT/RT FUSELAGE FRAMES CRACKED AT BS 188, STR 17L AND 17R. REMOVED AND REPLACED FRAMES PER SRM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 32,786 hrs · 29,435 cycles

DURING SCHEDULED SERVICE CHECK, FOUND BOTH AFT CABIN DOOR OVERHEAD EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY CHARGER AND CHARGED BATTERY PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 31,366 hrs · 28,312 cycles

DURING SCHEDULED C4 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: OUTFLOW VALVE — FAILED (CABIN PRESSURE) · airframe 31,025 hrs · 28,018 cycles

DECLARED EMERGENCY, DIVERSION, AT FL310, ALTITUDE WARNING HORN CAME ON. CABIN ALT AT 10,000 FEET CLIMBING. REMOVED AND REPLACED FWD AND AFT OUT FLOW VALVES, DELTA P MODULE, OVERHEAD MODULE, A/C ACCESSORY UNIT, CABIN PRESS CONTROLLER AND LOWER SAFETY RELIEF VALVE PER MM.

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 30,237 hrs · 27,372 cycles

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

Part: MEC — FAULTY (NR 2 ENGINE) · airframe 28,808 hrs · 26,191 cycles

AIR TURNBACK, DECLARED EMERGENCY, NR 2 ENGINE UNWOUND FROM TAKEOFF THRUST TO IDLE RPM WITH NO THRUST LEVER MOVEMENT. REMOVED AND REPLACED MEC AND FUEL PUMP PER MM.

Part: CLIP — LOOSE (L1/R1 DOORS) · airframe 28,644 hrs · 26,054 cycles

DURING SCHEDULED C1 CHECK, FOUND BOTH FWD DOOR EVACUATION SLIDE GIRT BARS CLIP HOOKS LOOSE. SECURED BOTH CLIP HOOKS PER MM.

Part: SLIDE — OUT OF ADJ (R2 DOOR) · airframe 27,801 hrs · 25,363 cycles

DURING SCHEDULED C4 CHECK, FOUND FWD SERVICE DOOR EVACUATION SLIDE OUT OF ADJUST. REPOSITIONED SLIDE ASSY PER MM.

Part: TAB — DELAMINATED (LH ELEVATOR) · airframe 27,734 hrs · 25,301 cycles

DURING SCHEDULED SERVICE CHECK, FOUND LH ELEVATOR TAB DELAMINATED AT T/E. R&R ELEVATOR TAB PER MM.

Part: FLAP — DELAMINATED (RT WING) · airframe 25,561 hrs · 23,446 cycles

DURING SCHEDULED RON CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP DELAMINATED. REPAIRED FLAP PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,480 hrs · 23,379 cycles

DURING SCHEDULED RON CHECK, FOUND BULLNOSE EGRESS LIGHT INOP AT FWD CABIN, RT SIDE. R&R LIGHT HOUSING PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 25,337 hrs · 23,270 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BS 178 BULKHEAD RT SIDE CHORD CRACKED. R&R SIDE CHORD PER PER ACO 7342-53.

Part: FRAME — CRACKED (FUSELAGE) · airframe 25,337 hrs · 23,270 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BS 178 BULKHEAD LT SIDE CHORD CRACKED. R&R SIDE CHORD PER ACO 7338-53.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 25,337 hrs · 23,270 cycles

DURING SCHEDULED 1/4D CHECK, FOUND STR CLIP CRACKED AT BS 867, STR 27L. R&R STR CLIP PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 25,337 hrs · 23,270 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BS 178 BULKHEAD WEBS CRACKED AT WL 199 RBL 5, WL 199 LBL 5 & WL 202 RBL 5. REPAIRED BULKHEAD WEBS PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,048 hrs · 23,017 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EEPLS INOP AT ROWS 18, 19 AND 24. RE-LAMPED AND RE-CONNECTED EEPLS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,964 hrs · 22,944 cycles

DURING SCHEDULED RON, FOUND EEPLS INOP AT ROW 21 - 22. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 24,964 hrs · 22,944 cycles

DURING SCHEDULED RON, FOUND EEPLS INOP AT ROWS 21, 22 AND AFT ENTRY DOOR. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: PANEL — INOPERATIVE (COCKPIT) · airframe 24,540 hrs · 22,590 cycles

DIVERSION, MCP INOP, DIVERTED TO CLE DUE TO WEATHER. C/W BITE CHECK AND REMOVED AND REPLACED MCP PANEL PER MM.

Part: SLIDE — DISLODGED (PAX DOOR) · airframe 24,404 hrs · 22,483 cycles

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

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 24,027 hrs · 22,147 cycles

DURING SCHEDULED C4 CHECK, FOUND RT HORIZONTAL STAB LOWER SKIN HAS A 2 INCH LONG CRACK NEAR FRONT SPAR, I/B BALANCE PANEL. REPAIRED SKIN PER SRM.

Part: SLIDE — DISLODGED (PAX DOOR) · airframe 23,371 hrs · 21,585 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,326 hrs · 21,546 cycles

DURING SCHEDULED A1 CHECK, FOUND AFT SECTION OF EEPLS INOP. REMOVED AND REPLACED LIGHT SOCKET PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,142 hrs · 21,392 cycles

EEPLS INOP AND LOOSE AT OVERWING EXIT. RESECURED LIGHT ASSY PER MM.

Part: COVER — MISSING (CABIN) · airframe 23,061 hrs · 21,324 cycles

EEPLS TRACK COVER MISSING AT OVERWING EXIT. INSTALLED TRACK COVER SECTION PER MM.

Part: COVER — MISSING (CABIN)

EEPLS LIGHT COVER MISSING AT OVERWING EXIT. INSTALLED TRACK COVER PER MM.

Part: LIGHT — LOOSE (ROW 15)

EEPLS LOOSE AT ROW 15. RESECURED TRACK LIGHTS PER MM.

Part: LIGHT — INOPERATIVE (ROW 15 - 17)

EEPLS INOP AT ROWS 15-17. REPAIRED LIGHTS PER MM.

Part: SLIDES — SAGGING (DOORS)

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

Part: TO WARNING — SOUNDED (COCKPIT)

ABORTED TAKEOFF, UPON ADVANCING THROTTLES FOR TAKEOFF WARNING HORN SOUNDED. (FLAPS AND SPEEDBRAKED CORRECTLY SET). INSPECTED AND OPERATED TAKEOFF WARNING SYSTEM. NO DEFECTS NOTED LATER ON PERFORMED TAKEOFF WARNING TEST PER MM. NO DEFECTS NOTED.

Part: SLIDE — LOW PRESS (SERVICE DOOR)

DURING SCHEDULED SERVICE CHECK, FOUND AFT SERVICE DOOR EVACUATION SLIDE PRESSURE BELOW LIMITS. REMOVED AND REPLACED SLIDE ASSY PER MM.

Part: GIRT BAR — NOT LATCHED (PASSENGER DOOR)

DURING SCHEDULED C3 CHECK, FOUND L1 DOOR EVACUATION SLIDE GIRT BAR HOOK NOT LATCHING. REMOVED AND REPLACED BAR HOOK PER MM.

Part: LIGHT — MISSING (RT EMER EXIT)

COVER MISSING FROM RT EMERGENCY EXIT MARKER LIGHT. REPLACED LIGHT ASSY PER MM.

Part: SLIDE — DETACHED (SERVICE DOOR)

FWD SERVICE DOOR SLIDE FELL OUT. SECURED BACK SLIDE ASSY ON TO DOOR PER MM.

Part: TERMINAL — LOOSE (NR 1 LE FLAP)

MDW-STL DURING TAXI OUT WHILE EXTENDING FLAPS TO POSITIONS, NR 1 L/E FLAP WENT TO AMBER ON EXT AND WOULD NOT ILLUMINATE GREEN, FLAPS POSITIONED UP AND DOWN WITH NO HELP. MAINT ADVISED FLAPS APPEARED TO BE IN NORMAL POSITION. RETURNED TO GATE. REPLACED TERMINAL END TO NR 1 KRUEGER FLAP GROUND STUD PER M/M, ALL CKS NORMAL.

Part: SIGN — DETACHED (EMER EXIT DOOR)

DURING SCHEDULED BC2 CHECK, FOUND EMERGENCY EXIT SIGN ABOVE RT EMERGENCY EXIT DOOR PULLED OUT. RESECURED SIGN LIGHT LENS PER BOEING MM.

Part: LIGHT — INOP (ROW 12-18)

DURING SCHEDULED BC2 CHECK, FOUND EMERGENCY EXIT LIGHTING INOP FROM ROWS 12 TO 18. REPOSITIONED LIGHTS.

Part: SIGN — LOOSE (EMER EXIT DOOR)

DURING SCHEDULED BC2 CHECK, FOUND CABIN EMERGENCY EXIT SIGN ABOVE RT EMERGENCY EXIT DOOR PULLED OUT. RESECURED PER BOEING M/M.

Part: LIGHT — INOP (ROW 12-18)

DURING SCHEDULED BC2 CHECK, FOUND CABIN EMERGENCY TRACK LIGHTING INOP FROM SEAT ROWS 12 TO 18. REPAIRED LIGHTING PER BOEING M/M.

Part: BULB — FAILED (CABIN)

DURING WALKAROUND CHECK, FOUND EMERGENCY EGRESS PATH LIGHTS (RED) OUT AT MIDDLE CABIN AT EMERGENCY EXIT ROW. REPLACED LIGHT BULBS AND REINSTALLED LIGHT ASSY OPS, CKD OK PER BOEING MM.

Part: WEB — CRACKED (BS 291.5)

DURING SCHEDULED 1/2 D-CHECK, FOUND CRACKED WEB ATTACH ANGLE JUST FWD OF GALLEY DOOR CUTOUT AT BS 291.5 ABOVE STR 9R. REPAIRED PER BOEING SRM.

Part: WEB — CORRODED (BS 847-867)

DURING SCHEDULED 1/2 D-CHECK, FOUND CORRODED SUPPORT WEB AT BS 847 TO 867, JUST AFT OF DOOR CUTOUT. REMOVED AND REPLACED PER BOEING SRM.

Part: WEB — CORRODED (BS 767-797)

DURING SCHEDULED 1/2 D-CHECK, FOUND CRACKED AND CORRODED SIDEWALL SUPPORT WEB FWD OF DOOR CUTOUT AT BS 767 TO 797. REMOVED AND REPLACED PER BOEING SRM.

Part: ANGLE — CORRODED (GALLEY DOORWAY)

DURING SCHEDULED 1/2 D-CHECK, FOUND CORRODED Z-ANGLE I/B OF FWD GALLEY DOOR THRESHOLD AROUND SCREW HOLES. REMOVED AND REPLACED PER BOEING SRM.

Part: ANGLE — CORRODED (GALLEY DOORWAY)

DURING SCHEDULED 1/2 D-CHECK, FOUND CORRODED FLOOR SUPPORT ANGLE. REMOVED AND REPLACED PER BOEING SRM.

Part: INTERCOSTAL — CRACKED (BS 540)

DURING SCHEDULED 1/2 D-CHECK, FOUND BROKEN INTERCOSTAL AT BS 540, LBL 3. REMOVED AND REPLACED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 344)

DURING SCHEDULED 1/2 D-CHECK, FOUND CORRODED FLOORBEAM HOLE AT BS 344, LBL 9 AND BS 344, RBL 1. REMOVED AND REPLACED PER BOEING SRM.

Part: FRAME — CRACKED (GALLEY DOORWAY)

DURING SCHEDULED 1/2 D-CHECK, FOUND CRACKED FRAME AT FWD LOWER CORNER OF FWD GALLEY DOOR CUTOUT. REPAIRED PER BOEING SRM.

Part: SKIN — GOUGED (SERVICE DOORWAY)

DURING SCHEDULED 1/2 D-CHECK, FOUND FUSELAGE SKIN 6.5 AFT OF FWD SERVICE DOOR GOUGED BELOW STR 8R. REPAIRED PER BOEING SRM.

Part: ANGLE — CRACKED (PAX DOOR)

DURING SCHEDULED 1/2 D-CHECK, FOUND CRACKED DOOR LINER RETAINER SUPPORT ANGLE, LOWER AFT CORNER. REMOVED AND REPLACED PER BOEING SRM.

Part: WIRE — DISCONNECTED (CABIN)

DURING SCHEDULED C2 CHECK, FOUND EMERGENCY TRACK LIGHTING INOPERATIVE AT ROWS 11 AND 13. REPAIRED WIRING PER BOEING M/M.

Part: WIRE — BROKEN (NR 1 TE FLAP)

AFTER TAKEOFF, NR 1 T/E FLAP TRANSIT LIGHTS (FWD AND OVERHEAD) REMAINED ILLUMINATED. AIRCRAFT RETURNED TO PHX AND MADE AN UNEVENTFUL LANDING. INSPECTED AND REPAIRED BROKEN GROUND LUG WIRE PER BOEING M/M.

Part: SKIN — DENTED (FWD FUSELAGE)

DURING SCHEDULED TERM CHECK, FOUND FUSELAGE SKIN DENTED 30 BELOW CAPT WINDOW. REPAIRED PER BOEING SRM.

Part: SKIN — GOUGED (FUSELAGE)

DURING SCHEDULED C2/C4 CHECK, FOUND GOUGE UNDER FWD ENTRY DOOR AT AFT CORNER MEASURING 5 INCH BY .250 INCH BY .018 INCH DEEP. REPAIRED PER SWA RA 1-353-1370.