N306SW

Part: LOCKING CAM — LACK OF LUBE (GIRT BAR) · airframe 12,306 hrs · 4,571 cycles

AIRCRAFT WAS GROUNDED: FLIGHT ATTENDANT REPORTS FRONT RIGHT GIRT BAR WAS HARD TO REMOVE WHILE DISARMING. LUBED GIRT BAR ARMING CLIPS. OPERATIONAL CHECK GOOD. PER AMM25-66-01.

Part: SLIDE — DAMAGED (ZONE 800) · airframe 12,306 hrs · 4,571 cycles

AIRCRAFT WAS GROUNDED: AFTER INSPECTION OF R1 DOOR SLIDE FOUND SLIDE WILL NEED TO BE REPLACED BEFORE FURTHER FLIGHT. REMOVED AND REPLACED R1 DOOR ESCAPE SLIDE. PER JOB CARD NUMBER 09L20025004.

Part: LOCKING CAM — LACK OF LUBE (GIRT BAR) · airframe 12,228 hrs · 4,540 cycles

AIRCRAFT WAS NOT GROUNDED: GIRT BAR FORWARD SERVICE DOOR VERY DIFFICULT TO LOCK AND UNLOCK. LUBED AND ACCOMPLISHED MULTIPLE ARMING AND DISARMING, FORWARD R1 DOOR SLIDE OPERATIONAL CHECK GOOD. PER AMM 25-66-00.

Part: MECHANISM — LACK OF LUBE (GIRT BAR) · airframe 11,922 hrs · 4,431 cycles

AIRCRAFT WAS NOT GROUNDED: L1 GIRT BAR DIFFICULT TO ARM AND DISARM. CLEANED AND LUBED L1 DOOR GIRT BAR, OPERATIONAL CHECK GOOD. PER AMM 52-20-01.

Part: GIRT BAR — DIRTY (ZONE 800) · airframe 11,828 hrs · 4,394 cycles

AIRCRAFT WAS NOT GROUNDED: FLIGHT ATTENDANT REPORT L1 GIRT BAR IS DIFFICULT TO INSTALL AND REMOVE WHEN ARMING AND DISARMING THE L1 DOOR. REMOVED DIRT CLEAN AND LUBRICATED GIRT BAR, OPERATIONAL CHECK GOOD. PER AMM 25-66-01.

Part: SKIN — DAMAGED (ZONE 500) · airframe 11,816 hrs · 4,388 cycles

AIRCRAFT IN BASE MAINTENANCE: LEFT WING LOWER SKIN DAMAGED DUE TO TIRE BUST ON TAKEOFF. (SEE AALA202508280585), LOCATED AT WS 156. REPLACED SKIN PER 367894 AND BOEING WORK ORDER AAL-RE-25000250.

Part: FLASHLIGHT — MISSING (ZONE 200) · airframe 11,817 hrs · 4,388 cycles

AIRCRAFT IN BASE MAINTENANCE: FLASHLIGHT MISSING IN FORWARD FLIGHT ATTENDANT SEAT AT LEFT HAND SIDE. REPLACED MISSING FLASHLIGHT. PER AMM 25-64-00.

Part: TUBE — MISSING (GIRT BAR) · airframe 11,817 hrs · 4,388 cycles

AIRCRAFT IN BASE MAINTENANCE: L2 DOOR SLIDE CASE GIRT BAR RED SHRINK TUBE NEED REPLACED AT AFT. REPLACED HEAT SHRINK TUBING. PER 737MAX AARD 25-66-00.

Part: TUBE — DEGRADED (ZONE 800) · airframe 11,817 hrs · 4,388 cycles

AIRCRAFT IN BASE MAINTENANCE: R1 DOOR RED HEAT SHRINK TUBING DEGRADED ON BOTH ENDS OF GIRT BAR. REMOVED AND REPLACED R1 DOOR SLIDE CASE GIRT BAR RED SHRINK TUBE. PER AARD 25-66-00.

Part: LIFE VEST — OPEN (ZONE 200) · airframe 11,817 hrs · 4,388 cycles

AIRCRAFT IN BASE MAINTENANCE, SEAT 4B PASSENGER LIFE VEST PLASTIC BAG OPENED. REMOVED AND REPLACED PASSENGER LIFE VEST AT SEAT 4B. PER AMM 25-22-00.

Part: TUBE — CRACKED (ZONE 800) · airframe 11,817 hrs · 4,388 cycles

AIRCRAFT IN BASE MAINTENANCE: L1 DOOR RED HEAT SHRINK TUBING CRACKED AND TORN ON BOTH ENDS OF GIRT BAR. REMOVED AND REPLACED L1 DOOR SLIDE CASE GIRT BAR RED SHRINK TUBE. PER AARD 25-66-00.

Part: TUBE — TORN (ZONE 800) · airframe 11,817 hrs · 4,388 cycles

AIRCRAFT IN BASE MAINTENANCE: L1 DOOR SLIDE CASE GIRT BAR RED SHRINK TUBE NEED REPLACED BOTH FORWARD AND AFT. REMOVED AND REPLACED L1 DOOR SLIDE CASE GIRT BAR RED SHRINK TUBE. PER AARD 25-66-00.

Part: TUBE — MISSING (ZONE 800) · airframe 11,817 hrs · 4,388 cycles

AIRCRAFT IN BASE MAINTENANCE: R1 DOOR SLIDE CASE GIRT BAR RED SHRINK TUBE NEED REPLACED AT AFT. REMOVED AND REPLACED R1 DOOR SLIDE CASE GIRT BAR RED SHRINK TUBE. PER AARD 25-66-00.

Part: TIRE — EXPLODED (LANDING GEAR) · airframe 11,816 hrs · 4,387 cycles

AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED DUE TO: DURING TAKEOFF ROLL LEFT MAIN TIRES EXPLODED. AIRCRAFT REJECTED TAKEOFF AND STOP ON THE RUNWAY. **SUPPLEMENTAL REPORT WILL BE SUBMITTED**(OPEN).

Part: TIRE — FAILED (ZONE 700) · airframe 11,816 hrs · 4,387 cycles

AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED DUE TO: DURING TAKEOFF ROLL LEFT MAIN TIRES EXPLODED. AIRCRAFT REJECTED TAKEOFF AND STOP ON THE RUNWAY. DUE TO TIRE BLOWN ON TAKE OFF, LEFT HAND MLG REQUIRES REPLACEMENT. REPLACED MLG ASSEMBLY. PER W/C 09L30032001.

Part: PRESSURE SWITCH — FAILED (SPOILER SYSTEM) · airframe 9,483 hrs · 3,514 cycles

AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED DUE TO: AT TOP OF CLIMB SPOILER LIGHT ILLUMINATED. AFTER LANDING MASTER CAUTION AND MAINTENANCE LIGHT ILLUMINATED; AIRCRAFT LANDED SAFELY AT MIA. REPLACED ARM SOLENOID PRESSURE SWITCH. ACCOMPLISHED ALL TEST REQUIRED AND LEAKS CHECK GOOD. PER CMM 27-60-01.

Part: UNKNOWN — ODOR (ZONE 200) · airframe 8,457 hrs · 3,131 cycles

AIRCRAFT WAS NOT GROUNDED: MULTIPLE WRITE-UP OF FOUL ODOR COMING FROM DOOR ENTRY AREA'S.**SUPPLEMENTAL REPORT FOR (AALA202407168897): SANITIZED GALLEYS AND LAVATORIES. PER AMM 25-00-00 AND W/C 09C10038005, NO FAULT FOUND**(CLOSED).

Part: UNKNOWN — ODOR (CABIN) · airframe 8,457 hrs · 3,131 cycles

AIRCRAFT WAS NOT GROUNDED: MULTIPLE WRITE-UP OF FOUL ODOR COMING FROM DOOR ENTRY AREA'S. (OPEN).

Part: UNKNOWN — ODOR (LAVATORY) · airframe 6,775 hrs · 2,494 cycles

AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED DUE TO: FLIGHT ATTENDANT NOTIFIED FLIGHT DECK OF A FAINT ELECTRICAL BURNING SMELL COMING FROM LAVATORY D. AIRCRAFT LANDED SAFELY AT MIA WITHOUT FURTHER INCIDENT. ACCOMPLISHED WORK CARD 09L00021001. NO ODOR NOTED.

Part: DOOR LATCH — LOOSE (ZONE 800 - DOORS) · airframe 3,623 hrs · 1,302 cycles

AIRCRAFT IN BASE MAINTENANCE: AFT RIGHT LAVATORY DOOR LATCH TOO TIGHT. PASSENGER LOCKING THEMSELVES IN THE LAVATORY. TROUBLESHOOT THE AFT RIGHT LAV E, LOCKING MECHANISM AND FOUND LOOSE. ADJUSTED THE LATCH MECHANISM

Part: RELAY — FAULTY (STAB TRIM) · airframe 3,532 hrs · 1,266 cycles

AIRCRAFT WAS GROUNDED: MAIN ELECTRIC TRIM FAILED AT 5000 FEET. EMERGENCY DECLARED; FLIGHT RETURNED TO MIA LANDING SAFELY. REMOVED AND REPLACED MAIN TRIM ARM RELAY R1193 (AALA202301232322) AND STAB TRIM CONTROL RELAY R64 (AALA202301231567) PER WDM 27-41-12. REPLACED STAB TRIM MOTOR M1659 PER AMM 27-41-71 (AALA202301235481). ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK. ACCOMPLISHED SATISFACTORY FUNCTIONAL CHECK FLIGHT.

Part: RELAY — FAULTED (STAB TRIM) · airframe 3,532 hrs · 1,266 cycles

AIRCRAFT WAS GROUNDED: MAIN ELECTRIC TRIM FAILED AT 5000 FEET. EMERGENCY DECLARED; FLIGHT RETURNED TO MIA LANDING SAFELY. REMOVED AND REPLACED MAIN TRIM ARM RELAY R1193 (AALA202301232322) AND STAB TRIM CONTROL RELAY R64 (AALA202301231567) PER WDM 27-41-12. REPLACED STAB TRIM MOTOR M1659 PER AMM 27-41-71 (AALA202301235481). ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK. ACCOMPLISHED SATISFACTORY FUNCTIONAL CHECK FLIGHT.

Part: MOTOR — FAULTED (STAB TRIM) · airframe 3,532 hrs · 1,266 cycles

AIRCRAFT WAS GROUNDED: MAIN ELECTRIC TRIM FAILED AT 5000 FEET. EMERGENCY DECLARED; FLIGHT RETURNED TO MIA LANDING SAFELY. REMOVED AND REPLACED MAIN TRIM ARM RELAY R1193 (AALA202301232322) AND STAB TRIM CONTROL RELAY R64 (AALA202301231567) PER WDM 27-41-12. REPLACED STAB TRIM MOTOR M1659 PER AMM 27-41-71 (AALA202301235481). ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK. ACCOMPLISHED SATISFACTORY FUNCTIONAL CHECK FLIGHT.

Part: RELAY — FAULTED (STAB TRIM) · airframe 3,531 hrs · 1,265 cycles

AIRCRAFT WAS GROUNDED: DURING CLIMB OUT MACH ELECTRIC STAB TRIM FAILED. AUTOPILOT TRIM OK. EMERGENCY DECLARED; FLIGHT RETURNED TO MIA LANDING SAFELY. REMOVED AND REPLACED MAIN TRIM FLAPS RELAY R1192 PER SWPM 20-81-16. ACCOMPLISHED SATISFACTORY STABILIZER TRIM MOTOR TEST AT FLAP UNITS 1 AND 5 PER AMM 27-41-71-700-801.

Part: GIRT BAR — OUT OF POSITION (ZONE 800 - DOORS) · airframe 1,725 hrs · 646 cycles

AIRCRAFT WAS NOT GROUNDED: 1R DOOR GIRT BAR JAMMED. CHECKED AND RE-POSITION IR DOOR GIRT BAR PER AMM 25-66-01.

Part: SHROUD — OUT OF POSITION (ZONE 800 - DOORS) · airframe 1,725 hrs · 646 cycles

AIRCRAFT WAS NOT GROUNDED: GIRT BAR SHROUD NEAR RIGHT END/CLIP NEED ADJUSTED CENTERED SO AS NOT TO CLIP OR CATCH ANT CLIPS. LUBRICATED AND RE-POSITION GIRT BAR SHROUD PER AMM 25-66-01.

Part: BATTERY — FAULTY (ZONE 200 - FUSE) · airframe 1,125 hrs · 443 cycles

AIRCRAFT WAS NOT GROUNDED: FORWARD RIGHT FLIGHT ATTENDANT EMERGENCY FLASHLIGHT TEST LED LIGHT ILLUMINATES RED. REPLACED BATTERY AND TESTED PER AMM 25-64-00.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 77,080 hrs · 71,678 cycles

DURING SCHEDULED CV CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 77,080 hrs · 71,678 cycles

DURING SCHEDULED CV CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 77,080 hrs · 71,678 cycles

DURING SCHEDULED CV CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 75,051 hrs · 70,307 cycles

DURING SCHEDULED 24Y CHECK, FOUND RT WING NR 6 SLAT I/B UPPER T/E WEDGE DELAMINATED. REPAIRED WEDGE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,051 hrs · 70,307 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STR 20R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,051 hrs · 70,307 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 18L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,051 hrs · 70,307 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 24R. REMOVED AND REPLACED CLIP PER SRM.

Part: SLAT — DELAMINATED (LT WING) · airframe 76,212 hrs · 71,087 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT WING NR 2 SLAT DELAMINATED AT O/B END. REMOVED AND REPLACED SLAT PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 76,212 hrs · 71,087 cycles

DURING SCHEDULED HC2 CHECK, FOUND SKIN CRACKED AT BS 270, STR 9L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (R1 DOOR) · airframe 76,212 hrs · 71,087 cycles

DURING SCHEDULED HC2 CHECK, FOUND R1 DOOR SKIN CRACKED AT LOWER AFT CORNER OR DOOR HINGE CUTOUT. REMOVED AND REPLACED DOOR PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 76,212 hrs · 71,087 cycles

DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR ABOVE LOWER GATE. REPAIRED SKIN PER MM.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 76,001 hrs · 70,928 cycles

DURING SCHEDULED MV1 CHECK, FOUND FWD FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 75,898 hrs · 70,861 cycles

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

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 75,452 hrs · 70,565 cycles

L1 DOOR EMERGENCY EXIT SLIDE FELL OUT, DID NOT DEPLOY. REMOVED AND REPLACED SLIDE PER MM.

Part: GASPER FAN — FAULTY (CABIN) · airframe 75,465 hrs · 70,573 cycles

DECLARED EMERGENCY, SMOKE IN CABIN - ACRID SMELL NEAR AFT GALLEY CONCENTRATED IN REAR WITH SOME VISIBLE SMOKE. F/O TURNED DOWN RT PACK AFTER CALL - IT HELPED. REMOVED AND REPLACED GASPER FAN PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 75,418 hrs · 70,539 cycles

DURING SCHEDULED 24Y CHECK, FOUND EMERGENCY EXIT LIGHT INOP AT ROW 23. REMOVED AND REPLACED LAMP PER MM.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 75,418 hrs · 70,539 cycles

DURING SCHEDULED 24Y CHECK, FOUND LT KEEL BEAM CORRODED AT BS 500C + 12, STR 27R. REPAIRED BEAM PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 75,418 hrs · 70,539 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 727C BETWEEN STR 26L TO STR 27L. REPAIRED SHEAR TIE PER SRM.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 75,418 hrs · 70,539 cycles

DURING SCHEDULED 24Y CHECK, FOUND LT KEEL BEAM CORRODED AT BETWEEN BS 700 TO BS 714, RBL 24. REPAIRED BEAM PER SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 75,418 hrs · 70,539 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE SKIN CORRODED AT BETWEEN BS 506D TO 512D, STR 28L. REPAIRED SKIN PER ER.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 75,418 hrs · 70,539 cycles

DURING SCHEDULED 24Y CHECK, FOUND LT KEEL BEAM CORRODED AT BETWEEN BS 500C + 14 TO BS 500C + 17. REPAIRED BEAM PER SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 75,418 hrs · 70,539 cycles

DURING SCHEDULED 24Y CHECK, FOUND AFT CARGO BAY FLOORBEAM SUPPORT CORRODED AT BS 727D + 6, LBL 8. REPAIRED BEAM PER SWA EA.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 75,418 hrs · 70,539 cycles

DURING SCHEDULED 24Y CHECK, FOUND AFT CARGO BAY FLOORBEAM SUPPORT CORRODED AT BS 727D + 6, LBL 3. REPAIRED BEAM PER SWA EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 75,418 hrs · 70,539 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 727E, BETWEEN STR 26L TO STR 27L. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 75,418 hrs · 70,539 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 727D, BETWEEN STR 26L TO 27L. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 75,418 hrs · 70,539 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 540, STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 75,418 hrs · 70,539 cycles

DURING SCHEDULED 24Y CHECK, FOUND FLOORBEAM WEB CRACKED AT BETWEEN BS 707 TO BS 714, BL 0. REPAIRED WEB PER PAE ER.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 75,418 hrs · 70,539 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 520, O/B OF LT KEEL BEAM. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 75,418 hrs · 70,539 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CORRODED AT BETWEEN BS 785 TO BS 823, STR 26L. REMOVED AND REPLACED STRINGER PER SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 75,418 hrs · 70,539 cycles

DURING SCHEDULED 24Y CHECK, FOUND AFT CARGO FLOOR SUPPORT CORRODED BETWEEN BS 772 TO BS 774, RBL 3. REPAIRED FLOOR SUPPORT PER EA.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 75,418 hrs · 70,539 cycles

DURING SCHEDULED 24Y CHECK, FOUND AFT CARGO FLOOR SUPPORT CORRODED BS 727D + 6. REPAIRED FLOOR SUPPORT PER EA.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 75,418 hrs · 70,539 cycles

DURING SCHEDULED 24Y CHECK, FOUND CARGO BAY FLOOR SUPPORT BEAM CORRODED AT BETWEEN BS 772 TO BS 774, RBL 8. REPAIRED BEAM PER SWA EA.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 75,418 hrs · 70,539 cycles

DURING SCHEDULED 24Y CHECK, FOUND CARGO BAY FLOOR SUPPORT BEAM CORRODED AT BETWEEN BS 772 TO BS 774, LBL 8. REPAIRED BEAM PER SWA EA.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 75,418 hrs · 70,539 cycles

DURING SCHEDULED 24Y CHECK, FOUND AFT CARGO FLOOR SUPPORT CORRODED AT BETWEEN BS 772 TO BS 774, LBL 13. REPAIRED FLOOR SUPPORT PER SWA EA.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 75,418 hrs · 70,539 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 747, STR 26L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 75,418 hrs · 70,539 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 787, STR 25L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 75,418 hrs · 70,539 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CORRODED AT BS. 827, STR 26L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 75,418 hrs · 70,539 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER SPLICE CORRODED AT BS 908, STR 27L. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 75,418 hrs · 70,539 cycles

DURING SCHEDULED 24Y CHECK, FOUND CARGO BAY FLOOR SUPPORT BEAM COORDED AT BS 729E, LBL 3. REPAIRED BEAM PER SWA EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 74,764 hrs · 70,082 cycles

DURING SCHEDULED HC1 CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 74,764 hrs · 70,082 cycles

DURING SCHEDULED HC1 CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: SIGN — LOOSE (CABIN) · airframe 74,030 hrs · 69,531 cycles

LEFT OVERWING EMERGENCY EXIT LIGHT SIGN LOOSE. SECURED SIGN PER MM.

Part: STIFFENER — CRACKED (LT MLG WW) · airframe 73,968 hrs · 69,483 cycles

DURING SCHEDULED SPV CHECK, FOUND LEFT MLG W/W FWD BULKHEAD STIFFENER CRACKED AT BS 663.75, LBL 6.15. REPAIRED STIFFENER PER SWA EA.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 73,818 hrs · 69,373 cycles

DURING SCHEDULED MV1 CHECK, FOUND FWD CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,171 hrs · 68,899 cycles

DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 960, STR 5R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,171 hrs · 68,899 cycles

DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 338 AND BS 350, STR 1. REPAIRED SKIN PER SRM.

Part: LENS — LOOSE (EXTERIOR) · airframe 73,171 hrs · 68,899 cycles

DURING SCHEDULED HC2 CHECK, FOUND R1 DOOR EMERGENCY EXIT EXTERIOR LIGHT LENS LOOSE. SECURED LENS PER MM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 73,171 hrs · 68,899 cycles

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

Part: SKIN — DELAMINATED (T/E FLAP) · airframe 73,171 hrs · 68,899 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT WING INBOARD FOREFLAP UPPER SURFACE DELAMINATED. REMOVED AND REPLACED FLAP PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 73,163 hrs · 68,895 cycles

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

Part: FRAME — CRACKED (BS 727 S14R) · airframe 70,953 hrs · 67,164 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727, STR 14R. REPAIRED FRAME PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,953 hrs · 67,164 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT FWD SERVICE DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER ER.

Part: FRAME — CRACKED (BS 500C S20R) · airframe 70,953 hrs · 67,164 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 20R. REPAIRED FRAME PER SRM.

Part: SHEAR TIE — CORRODED (BS 787 S28R) · airframe 70,953 hrs · 67,164 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 787, STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (BS 727 S21R) · airframe 70,953 hrs · 67,164 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727, STR 21R. REPAIRED FRAME PER ER.

Part: FRAME — CRACKED (BS 500B S20R) · airframe 70,953 hrs · 67,164 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500B, STR 20R. REPAIRED FRAME PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,953 hrs · 67,164 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR LOWER HINGE CUTOUT FWD UPPER CORNER. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,953 hrs · 67,164 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR LOWER HINGE CUTOUT AFT UPPER CORNER. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,953 hrs · 67,164 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D, STR 20R. REPAIRED SKIN PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,953 hrs · 67,164 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 19R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 70,953 hrs · 67,164 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 767, STR 27L AND STR 27R. REPAIRED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (BS 727B S13L) · airframe 70,953 hrs · 67,164 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727B, STR 13L. REPAIRED FRAME PER ER.

Part: SHEAR TIE — CRACKED (BS 500B S13L) · airframe 70,953 hrs · 67,164 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 500B, STR 13L. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER SPLICE — CORRODED (BS 908 S24L) · airframe 70,953 hrs · 67,164 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CORRODED AT BS 908, STR 24L. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: SHEAR TIE — CRACKED (BS 767 S27L) · airframe 70,953 hrs · 67,164 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 767, STR 27L. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,953 hrs · 67,164 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,953 hrs · 67,164 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 294, STR 11L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 70,953 hrs · 67,164 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 908, STR 24L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,953 hrs · 67,164 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 294, STR 12L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,953 hrs · 67,164 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME WEB CRACKED AT BS 277, BL 0, WL 182.1. REPAIRED WEB PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,953 hrs · 67,164 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 70,953 hrs · 67,164 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 787, STR 27R. REPAIRED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,953 hrs · 67,164 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 13R. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,953 hrs · 67,164 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 70,953 hrs · 67,164 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 14L. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,953 hrs · 67,164 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 7L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,953 hrs · 67,164 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 13L. REPAIRED FRAME PER SWA EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 70,953 hrs · 67,164 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 787, STR 27L. REPAIRED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,953 hrs · 67,164 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500D, STR 14R. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,953 hrs · 67,164 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,953 hrs · 67,164 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,953 hrs · 67,164 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 887, STR 14L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,953 hrs · 67,164 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 767, STR 14R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,953 hrs · 67,164 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 807, STR 8L. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,953 hrs · 67,164 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,953 hrs · 67,164 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,953 hrs · 67,164 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 3R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,953 hrs · 67,164 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,953 hrs · 67,164 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 907, STR 2R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,953 hrs · 67,164 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 9R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,953 hrs · 67,164 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,953 hrs · 67,164 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,953 hrs · 67,164 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,953 hrs · 67,164 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,953 hrs · 67,164 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,953 hrs · 67,164 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 10L. R&R STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,953 hrs · 67,164 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 7L. R&R STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,953 hrs · 67,164 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 9L. R&R STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,953 hrs · 67,164 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 16L. R&R STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,953 hrs · 67,164 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,953 hrs · 67,164 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,953 hrs · 67,164 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727C, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,953 hrs · 67,164 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500D, STR 13L. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,953 hrs · 67,164 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 8L. R&R STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,953 hrs · 67,164 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 16L. R&R STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,953 hrs · 67,164 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,953 hrs · 67,164 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 7R. R&R STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,953 hrs · 67,164 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 2R. R&R STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,953 hrs · 67,164 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727B, STR 8R. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,953 hrs · 67,164 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 10R. R&R STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,953 hrs · 67,164 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 8R. R&R STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,953 hrs · 67,164 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 8L. R&R STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,953 hrs · 67,164 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 2L. R&R STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,953 hrs · 67,164 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 5L. R&R STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,953 hrs · 67,164 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 4L. R&R STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,953 hrs · 67,164 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727E, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,953 hrs · 67,164 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 8L. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,953 hrs · 67,164 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 8L. R&R STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,953 hrs · 67,164 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500B, STR 3L. R&R STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,953 hrs · 67,164 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 8R. R&R STRINGER CLIP PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 70,953 hrs · 67,164 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 500D, STR 15L. R&R SHEAR TIE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,953 hrs · 67,164 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 520, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 400 S8R) · airframe 70,953 hrs · 67,164 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8R. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (BS 767 S10R) · airframe 70,953 hrs · 67,164 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 727D S6L) · airframe 70,953 hrs · 67,164 cycles

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

Part: STRINGER CLIP — CRACKED (BS 727D S5L) · airframe 70,953 hrs · 67,164 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 5L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 727D S6R) · airframe 70,953 hrs · 67,164 cycles

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

Part: STRINGER CLIP — CRACKED (BS 747 S5L) · airframe 70,953 hrs · 67,164 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 5L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 727C S6L) · airframe 70,953 hrs · 67,164 cycles

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

Part: STRINGER CLIP — CRACKED (BS 727A S2L) · airframe 70,953 hrs · 67,164 cycles

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

Part: FRAME — CRACKED (BS 295 S11L) · airframe 70,953 hrs · 67,164 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME WEB CRACKED AT BS 295, STR 11L. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (BS 767 S9L) · airframe 70,953 hrs · 67,164 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 9L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 887 S6L) · airframe 70,953 hrs · 67,164 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 887, STR 6L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 727D S8L) · airframe 70,953 hrs · 67,164 cycles

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

Part: STRINGER CLIP — CRACKED (BS 727A S3L) · airframe 70,953 hrs · 67,164 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 3L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 787 S10R) · airframe 70,953 hrs · 67,164 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (BS 295 S12L) · airframe 70,953 hrs · 67,164 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME WEB CRACKED AT BS 295, STR 12L. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (BS 847 S10R) · airframe 70,953 hrs · 67,164 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 847, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 907 S2R) · airframe 70,953 hrs · 67,164 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 907, STR 2R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,953 hrs · 67,164 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME WEB CRACKED AT BS 277, STR 16L. REPAIRED WEB PER SRM.

Part: SKIN — CRACKED (BS 460 S16R) · airframe 70,758 hrs · 67,027 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 460, STR 16R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 450 S16R) · airframe 70,758 hrs · 67,027 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 450, STR 16R. REPAIRED SKIN PER SWA EA.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 70,217 hrs · 66,627 cycles

R2 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM.

Part: LAMP — LOOSE (EMERGENCY LIGHT) · airframe 70,146 hrs · 66,566 cycles

EMERGENCY EXIT LIGHT INOP AT ROW 10 ABC. FOUND LOOSE LIGHT BULB, SECURED BULB PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,906 hrs · 66,380 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 934, STR 23R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,906 hrs · 66,380 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 782, STR 18L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 944) · airframe 69,906 hrs · 66,380 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 944, STR 24R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,906 hrs · 66,380 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 516D, STR 7R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,906 hrs · 66,380 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 375.5, STR 15R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,906 hrs · 66,380 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 494, STR 17L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,906 hrs · 66,380 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 497 TO BS 500A, STR 16L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 515D S9R) · airframe 69,554 hrs · 66,129 cycles

FUSELAGE SKIN CRACKED AT BS 515D, STR 9R. REPAIRED SKIN PER SWA EA.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 69,450 hrs · 66,046 cycles

DURING SCHEDULED 22Y CHECK, FOUND R1 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: BATTERY — FAULTY (EMERGENCY LIGHT) · airframe 69,450 hrs · 66,046 cycles

DURING SCHEDULED 22Y CHECK, FOUND FWD CABIN EMERGENCY EXIT LIGHTS INTERMITTENT. REMOVED AND REPLACED EMERGENCY BATTERY PACK PER MM.

Part: FITTING — CORRODED (R2 DOOR GIRT BAR) · airframe 69,450 hrs · 66,046 cycles

DURING SCHEDULED 22Y CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING CORRODED. REMOVED AND REPLACED GIRT BAR FITTING PER MM.

Part: SKIN — CUT (LT WING SPOILER) · airframe 69,450 hrs · 66,046 cycles

DURING SCHEDULED 22Y CHECK, FOUND CUT DAMAGE ON LT WING SPOILER AT OUTBOARD T/E. REPAIRED SPOILER PER SRM.

Part: STRINGER — CRACKED (BS 1006 S8L) · airframe 69,450 hrs · 66,046 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER 8L CRACKED AT BS 1006. REMOVED AND REPLACED STRINGER SECTION PER SRM.

Part: STRINGER — CRACKED (BS 420 S17R) · airframe 69,450 hrs · 66,046 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER 17R WEB CRACKED AT BS 420, RBL 44. REPAIRED STRINGER SECTION PER SRM.

Part: DOOR FRAME — CRACKED (CARGO DOORWAY) · airframe 69,450 hrs · 66,046 cycles

DURING SCHEDULED 22Y CHECK, FOUND FWD CARGO DOOR CUTOUT FWD FRAME CRACKED AT NR 5 DOOR STOP. REMOVED AND REPLACED FRAME SECTION PER ACO.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 69,450 hrs · 66,046 cycles

DURING SCHEDULED 22Y CHECK, FOUND FLOORBEAM CORRODED AT BS 328, RBL 0 TO RBL 10. REPAIRED FLOORBEAM PER SRM.

Part: SKIN — CRACKED (BS 504 S16R) · airframe 69,331 hrs · 65,957 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 504, STR 16R. REPAIRED SKIN PER SWA EA.

Part: BOLT — WORN (ELEVATOR TAB) · airframe 69,331 hrs · 65,957 cycles

DURING SCHEDULED C2 CHECK, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED NR 1 TAB HINGE BOLT PER MM.

Part: BOLT — WORN (ELEVATOR TAB) · airframe 69,331 hrs · 65,957 cycles

DURING SCHEDULED C2 CHECK, LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED NR 1 TAB HINGE BOLT PER MM.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHTS) · airframe 68,244 hrs · 65,075 cycles

DURING SCHEDULED SPV CHECK, FOUND FWD CABIN EMERGENCY EXIT LIGHTS INOP. RESECURED CONNECTOR ON FWD EMERGENCY EXIT LIGHT BATTERY PER MM.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHTS) · airframe 68,244 hrs · 65,075 cycles

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

Part: WINDOW — ARCED (COCKPIT) · airframe 68,133 hrs · 64,981 cycles

COCKPIT R1 WINDOW ARCING AT UPPER SIDE. REMOVED AND REPLACED R1 WINDOW PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,728 hrs · 64,628 cycles

DURING WALKAROUND INSP, FOUND FUSELAGE SKIN CRACKED AT BS 405, BETWEEN STR 15L TO STR 16L. REPAIRED SKIN PER SWA EA.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 67,533 hrs · 64,469 cycles

DURING SCHEDULED C4 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: SKIN — CRACKED (BS 578) · airframe 67,533 hrs · 64,469 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 578, STR 10R. REPAIRED SKIN PER SWA EA.

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS) · airframe 67,533 hrs · 64,469 cycles

DURING SCHEDULED C4 CHECK, FOUND LT AFT EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 67,093 hrs · 64,138 cycles

AFT GALLEY OVERHEAD EMERGENCY EXIT SIGN LENS BROKEN. REMOVED AND REPLACED LENS PER MM.

Part: SKIN — CRACKED (BS 751) · airframe 67,018 hrs · 64,080 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 751, STR 18L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 394) · airframe 67,018 hrs · 64,080 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 394, STR 17R. REPAIRED SKIN PER SWA EA & SRM.

Part: SKIN — CRACKED (BS 376) · airframe 67,018 hrs · 64,080 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 376, STR 17R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 504A) · airframe 67,018 hrs · 64,080 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 504A, STR 17R. REPAIRED SKIN PER SWA EA & SRM.

Part: SKIN — CRACKED (BS 440) · airframe 66,526 hrs · 63,717 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 440, STR 26L. REPAIRED SKIN PER SWA EA & SRM.

Part: SKIN — CRACKED (BS 500D) · airframe 66,526 hrs · 63,717 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D, STR 12R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 578) · airframe 66,526 hrs · 63,717 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 578, STR 10L. REPAIRED SKIN PER SWA EA.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 66,526 hrs · 63,717 cycles

DURING SCHEDULED C3 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 66,526 hrs · 63,717 cycles

DURING SCHEDULED C3 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,506 hrs · 62,948 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SWA EA & SRM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 65,506 hrs · 62,948 cycles

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

Part: SLIDE — DISLODGED (L1 DOOR) · airframe 65,398 hrs · 62,873 cycles

L1 DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. SLIDE DID NOT DEPLOY. REINSTALLED SLIDE PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 64,588 hrs · 62,207 cycles

DURING SCHEDULED SERVICE CHECK, FOUND LT AFT CABIN EMERGENCY LIGHTS INOP AT BS 753. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,588 hrs · 62,207 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 727E + 15, STR 19R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,588 hrs · 62,207 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 500C + 17, STR 15R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,588 hrs · 62,207 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 500C + 5, STR 15L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,588 hrs · 62,207 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 395, STR 16L. MX FERRY TO DALLAS. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,588 hrs · 62,207 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D, STR 16L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,588 hrs · 62,207 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 416, STR 26L. MX FERRY TO DALLAS. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,588 hrs · 62,207 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 460, STR 17R TO STR 18R. MX FERRY TO DALLAS. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,588 hrs · 62,207 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 944, STR 24L. MX FERRY TO DALLAS. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,588 hrs · 62,207 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 443, STR 26L. MX FERRY TO DALLAS. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,588 hrs · 62,207 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 480, STR 16R. REPAIRED SKIN PER SRM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 64,524 hrs · 62,166 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY AISLE LIGHTS INOP AT BS 720 & BS 850. REMOVED AND REPLACED BATTERY AND CHARGER ASSY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,727 hrs · 61,533 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN AT BS 390, STRINGER 15R, CRACKED. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,727 hrs · 61,533 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN AT BS 370, STRINGER 26L, CRACKED. REPAIRED SKIN PER EA.

Part: SKIN — DELAMINATED (LT WING FLAP) · airframe 63,727 hrs · 61,533 cycles

DURING SCHEDULED C4 CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED T/E AFT FLAP PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,350 hrs · 61,250 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 947.5, STRINGER 21L, CRACKED. REPAIRED SKIN SECTION PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,183 hrs · 61,123 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 426, STRINGER 16R, CRACKED. REPAIRED SKIN SECTION PER EA.

Part: CABLE — MISROUTED (L2 DOOR SLIDE) · airframe 62,712 hrs · 60,758 cycles

DURING SCHEDULED C3 CHECK, FOUND L2 DOOR EVAC SLIDE CABLE MISROUTED. REROUTED L2 DOOR EVAC SLIDE CABLE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,172 hrs · 60,758 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN AT BS 813, STRINGER 19L, CRACKED. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,712 hrs · 60,758 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN AT BS 486, STRINGER 17L, CRACKED. REPAIRED SKIN PER SRM.

Part: SKIN — DELAMINATED (RT WING FLAP) · airframe 61,769 hrs · 59,989 cycles

DURING SCHEDULED C2 CHECK, FOUND RT WING OUTBOARD AFT T/E FLAP DELAMINATED. REMOVED AND REPLACED RT WING OUTBOARD AFT T/E FLAP PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,769 hrs · 59,989 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT BS 500B + 4, STRINGER 16R, BS 500B + 14, STRINGER 16R, BS 500B + 10, STRINGER 6R, BS 500D + 6, STRINGER 15R, CRACKED. REPAIRED FUSELAGE SKIN PER EA AND SRM.

Part: WEB — CRACKED (NLG SUPPORT) · airframe 61,769 hrs · 59,989 cycles

DURING SCHEDULED C2 CHECK, FOUND FWD NLG SUPPORT WEB, CRACKED. REMOVED AND REPLACED NLG FWD SUPPORT WEB PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,514 hrs · 59,784 cycles

DURING SCHEDULED SERVICE CHECK, FOUND 2 EACH FUSELAGE SKIN CRACKS AT RT BS 400, WL 208. REPAIRED SKIN CRACKS PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,514 hrs · 59,784 cycles

DURING SCHEDULED SERVICE CHECK, FOUND 2 EACH FUSELAGE SKIN CRACKS AT BS 787, STRINGER 18L. REPAIRED SKIN PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 61,246 hrs · 59,579 cycles

DURING SCHEDULED D CHECK, FOUND CREASE BEAM AT BS 380, RBL 56, CORRODED. REMOVED AND REPLACED CREASE BEAM SECTION PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 61,246 hrs · 59,579 cycles

DURING SCHEDULED D CHECK, FOUND FRAME AT BS 198, STRINGER 17R, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,246 hrs · 59,579 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN AT BS 311, BETWEEN STRINGER 19R AND STRINGER 20R, CRACKED. REPAIRED SKIN PER ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 61,246 hrs · 59,579 cycles

DURING SCHEDULED D CHECK, FOUND FRAME AT BS 328, BETWEEN STRINGER 20R AND STRINGER 21R, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 61,246 hrs · 59,579 cycles

DURING SCHEDULED D CHECK, FOUND STRINGER 26R, BETWEEN BS 814 AND BS 821, CORRODED. REPAIRED STRINGER PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 61,246 hrs · 59,579 cycles

DURING SCHEDULED D CHECK, FOUND STRINGER CLIP AT BS 827, LBL 8, WL 149, CRACKED. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FITTING — CRACKED (KEELBEAM) · airframe 61,246 hrs · 59,579 cycles

DURING SCHEDULED D CHECK, FOUND BULKHEAD TEE FITTING AT BS 727, LBL 6, CRACKED. REMOVED AND REPLACED T-FITTING PER SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 61,426 hrs · 59,579 cycles

DURING SCHEDULED D CHECK, FOUND STRINGER CLIP AT BS 787, STRINGER 26R, CORRODED. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 61,246 hrs · 59,579 cycles

DURING SCHEDULED D CHECK, FOUND KEELBEAM AT RT BS 500C + 18, AND LT BS 500C + 18, INBOARD FLANGE, CORRODED. REPAIRED KEEL BEAM LT AND RT CHORD PER MM.

Part: WEB — CRACKED (FUSELAGE) · airframe 61,246 hrs · 59,579 cycles

DURING SCHEDULED D CHECK, FOUND FLOOR WEB AT BS 188 TO BS 198, STRINGER 17R, AND BS 188 TO BS 196, STRINGER 17L, CRACKED. REMOVED AND REPLACED FLOOR WEB SECTION PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 61,246 hrs · 59,579 cycles

DURING SCHEDULED D CHECK, FOUND BULKHEAD WEB AT BS 1016, STRINGER 6R, CRACKED. REPAIRED BULKHEAD PER ER.

Part: FITTING — CORRODED (HORIZONTAL STAB) · airframe 61,246 hrs · 59,579 cycles

DURING SCHEDULED D CHECK, FOUND LT AND RT, FWD AND REAR SPAR, HORIZONTAL STAB CENTER SECTION LUG FACES CORRODED. REPAIRED STAB PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 61,246 hrs · 59,579 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMES AT BS 188, STRINGER 17R AND STRINGER 17L, CRACKED. REMOVED AND REPLACED FRAME SECTIONS PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 61,246 hrs · 59,579 cycles

DURING SCHEDULED D CHECK, FOUND BULKHEAD CHORD AT BS 727 BBL 0, CORRODED. REMOVED AND REPLACED BULKHEAD CHORD PER SRM AND BAC DRAWING.

Part: CLIP — CRACKED (FUSELAGE) · airframe 61,246 hrs · 59,579 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS AT BS 360, STRINGER 8R, BS 420, STRINGER 3L, BS 420, STRINGER 9R, BS 420, STRINGER 1R, CRACKED. REMOVED AND REPLACED STRINGER CLIPS PER SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 61,246 hrs · 59,579 cycles

DURING SCHEDULED D CHECK, FOUND L2 DOOR FRAME LOWER HINGE CUTOUT CRACKED. REPAIRED L2 DOOR CUTOUT PER ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 61,246 hrs · 59,579 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FRAME AT BS 297, STRINGER 17R, CRACKED. REPAIRED FRAME SECTION PER ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 61,246 hrs · 59,579 cycles

DURING SCHEDULED D CHECK, FOUND FRAME WEB AT BS 303.9, STRINGER 16L, CRACKED. REMOVED AND REPLACED FRAME WEB SECTION PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 61,246 hrs · 59,579 cycles

DURING SCHEDULED D CHECK, FOUND FLOORBEAM AT BS 219, LBL 16, CORRODED. REPAIRED FLOORBEAM PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 61,246 hrs · 59,579 cycles

DURING SCHEDULED D CHECK, FOUND FRAME AT BS 360, BETWEEN STRINGER 8L, AND STRINGER 9L, CRACKED. REPAIRED FRAME SECTION PER SRM.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 61,246 hrs · 59,579 cycles

DURING SCHEDULED D CHECK, FOUND CREASE BEAM AT BS 520, LBL 64, CRACKED. REMOVED AND REPLACED CREASE BEAM SECTION PER SRM.

Part: SPLICE — CORRODED (FUSELAGE) · airframe 61,246 hrs · 59,579 cycles

DURING SCHEDULED D CHECK, FOUND STRINGER SPLICE AT BS 907, STR 21L, CORRODED. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 61,246 hrs · 59,579 cycles

DURING SCHEDULED D CHECK, FOUND FWD CARGO COMPARTMENT AT BS 500 B + 16, TO 430, STRINGER 27 L, CORRODED. REPAIRED STRINGER PER SRM.

Part: FITTING — CORRODED (CABIN) · airframe 61,246 hrs · 59,579 cycles

DURING SCHEDULED D CHECK, FOUND L1 DOOR EVAC SLIDE GIRT BAR FITTINGS CORRODED. REPAIRED GIRT BAR FITTINGS PER SRM.

Part: TIE — CORRODED (FUSELAGE) · airframe 61,246 hrs · 59,579 cycles

DURING SCHEDULED D-CHECK, FOUND SHEAR TIES AT BS 747, STR 27R, BS 867, BL 0, BS 807, LBL 18 AND LBL 9, CORRODED. REPAIRED SHEAR TIES PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 61,246 hrs · 59,579 cycles

DURING SCHEDULED D-CHECK, FOUND FLOORBEAMS AT BS 328, RBL 42, BS 344, LBL 50 TO RBL 0, CORRODED. REPAIRED FLOORBEAMS PER SRM.

Part: TIE — CORRODED (FUSELAGE) · airframe 61,246 hrs · 59,579 cycles

DURING SCHEDULED D-CHECK, FOUND SHEAR TIES AT BS 440, BETWEEN STR 26L AND STR 27L, BS 500A, BETWEEN STR 28L AND STR 28R, CORRODED. REPAIRED SHEAR TIES PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 61,246 hrs · 59,579 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAMES AT BS 747, STR 9L, BS 767 STR 9R AND 9L, BS 807, STR 9R, BS 827, STR 9L AND 9R, BS 887, STR 9R AND 8L, CRACKED. REPAIRED FRAMES PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 61,246 hrs · 59,579 cycles

DURING SCHEDULED D CHECK, FOUND FLOORBEAM AT BS 294.5, RBL 39, CORRODED. REPAIRED FLOORBEAM PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 61,246 hrs · 59,579 cycles

DURING SCHEDULED D CHECK, FOUND SHEAR TIE AT BS 1006, LBL 6, CORRODED. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 61,246 hrs · 59,579 cycles

DURING SCHEDULED D CHECK, FOUND STRINGER CLIP AT BS 500 D, STR 8 R, CRACKED. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,246 hrs · 59,579 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN AT BS 375, STRINGER 19R, CRACKED. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,246 hrs · 59,579 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN AT BS 944, STRINGER 25R, CRACKED. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,246 hrs · 59,579 cycles

DURING SCHEDULED D CHECK, FOUND R2 DOOR UPPER HINGE CUTOUT REPAIR DOUBLER CRACKED. REMOVED AND REPLACED DOUBLER PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,900 hrs · 59,301 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500B, STRINGER 19R. REPAIRED SKIN PER SRM.

Part: FLAP — DELAMINATED (LT WING) · airframe 60,900 hrs · 59,301 cycles

DURING SCHEDULED C1 CHECK, FOUND LT WING INBOARD AFT FLAP DELAMINATED ON T/E. REMOVED AND REPLACED LT WING INBOARD FLAP PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,900 hrs · 59,301 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 277 + 11.5, STRINGER 16L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,486 hrs · 58,969 cycles

DURING SCHEDULED A1 CHECK, FOUND SKIN CRACK AT BS 790, STRINGER 18R. REPAIRED SKIN PER SRM.

Part: SKIN — DELAMINATED (RT WING SLAT) · airframe 59,988 hrs · 58,548 cycles

DURING SCHEDULED C4 CHECK, FOUND #6 L/E SLAT DELAMINATED AT MID SPAN AREA. REMOVED AND REPLACED SLAT ASSY PER MM.

Part: BLADE — DAMAGED (NR 2 ENGINE) · airframe 59,988 hrs · 58,548 cycles

DURING SCHEDULED C4 CHECK, NR 1 ENG FAILED BORESCOPE INSPECTION DUE MISSING MATERIAL AT 1 EA HPT BLADE T/E. REMOVED AND REPLACED NR 2 ENG PER MM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 59,121 hrs · 57,863 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 520, STR 28L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,121 hrs · 57,863 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED (2 EA) ABOVE STR 16L, BS 277 AND BS 520. REPAIRED SKIN PER SRM.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 59,121 hrs · 57,863 cycles

DURING SCHEDULED C3 CHECK, FOUND OVERHEAD CEILING EMERGENCY EXIT LIGHT LENS MISSING AT ROW NR 2. INSTALLED EMERGENCY EXIT LIGHT LENS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,215 hrs · 57,147 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 430, FWD END OF NR 2 RADIO ALTIMETER ANTENNA CUTOUT. REPAIRED SKIN PER SWA EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 58,215 hrs · 57,147 cycles

DURING SCHEDULED C2 CHECK, FOUND BOTH AFT SVC & AFT ENTRY OVERHEAD EMERGENCY EXIT LIGHTS INOP. RELAMPED BOTH AFT SVC & AFT ENTRY EMERGENCY EXIT LIGHTS PER MM.

Part: SKIN — CRACKED (FUSELAGE.) · airframe 57,207 hrs · 56,343 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED 1.5 LONG, BS 500D, STRINGER 7R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,207 hrs · 56,343 cycles

DURING SCHEDULED C1 CHECK, FOUND 2 EA FUSELAGE SKIN CRACKS, BS 520, STRINGER 12R AND BS 515, STRINGER 16R. REPAIRED SKIN PER SRM.

Part: CABLE — FRAYED (AFT ENTRY DOOR) · airframe 54,524 hrs · 54,209 cycles

DURING SCHEDULED C2 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE GIRT BAR CABLE FRAYED. REMOVED AND REPLACED CABLE PER MM.

Part: SLIDE — OUT OF ADJUST (FWD ENTRY DOOR) · airframe 54,524 hrs · 54,209 cycles

DURING SCHEDULED C2 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: BEAM — CRACKED (CENTER WING BOX) · airframe 53,531 hrs · 53,399 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BS 663 FLOORBEAM CRACKED, BBL 0. REPAIRED BEAM PER BOEING SB 737-57-1210

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,512 hrs · 53,382 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, ABOVE STR 14L. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,512 hrs · 53,382 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 540, STR 10R. REPAIRED FRAME PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 53,512 hrs · 53,382 cycles

DURING SCHEDULED 1/4D CHECK, FOUND STRINGER CRACKED AT BS 500C, STR 15R. REPAIRED STR PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,512 hrs · 53,382 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE FRAME CRACKED (3 EA) AT BS 663.5, STRS 2L, 3L AND 2R. REPAIRED FRAME PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,512 hrs · 53,382 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKINCRACKED AT FWD ENTRY DOOR LOWER HINGE CUT OUT. REPAIRED SKIN PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,512 hrs · 53,382 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 15L. REPAIRED FRAME PER SRM.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 53,512 hrs · 53,382 cycles

DURING SCHEDULED 1/4D CHECK, FOUND STRINGER SPLICE CRACKED AT BS 908, STR 10R. REMOVED AND REPLACED STR SPLICE PER SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 53,512 hrs · 53,382 cycles

DURING SCHEDULED 1/4D CHECK, FOUND STRINGER TIE CLIP CRACKED AT BS 663.5, STR 4R. REMOVED AND REPLACED STR TIE CLIP PER SRM.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 53,512 hrs · 53,382 cycles

DURING SCHEDULED 1/4D CHECK, FOUND STRINGER SPLICES CRACKED (2 EA) AT STR 4L, BS 360 AND BS 908. REMOVED AND REPLACED STR SPLICES PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 53,512 hrs · 53,382 cycles

DURING SCHEDULED 1/4D CHECK, FOUND WEB CRACKED AT BS 178, LBL 17.1 AND WL 183. REPAIRED WEB PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,512 hrs · 53,382 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 14R. REPAIRED FRAME PER SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 53,512 hrs · 53,382 cycles

DURING SCHEDULED 1/4D CHECK, FOUND STRINGER TIE CLIPS CRACKED (2 EA) AT BS 616, STRS 5L AND 5R. REMOVED AND REPLACED TIE CLIPS PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 53,512 hrs · 53,382 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FRAME SHEAR TIES CRACKED (2 EA) AT BS 360 BETWEEN STRS 13L AND 15L. REPAIRED SHEAR TIES PER SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 53,512 hrs · 53,382 cycles

DURING SCHEDULED 1/4D CHECK, FOUND STRINGER TIE CLIP CRACKED AT BS 767, STR 11R. REMOVED AND REPLACED TIE CLIP PER SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 53,512 hrs · 53,382 cycles

DURING SCHEDULED 1/4D CHECK, FOUND STRINGER TIE CLIP CRACKED AT BS 685, STR 4R. REMOVED AND REPLACED TIE CLIP PER SRM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 53,496 hrs · 53,365 cycles

DURING SCHEDULED RON, FOUND FWD SVC DOOR EXTERIOR EMERGENCY LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 53,191 hrs · 53,109 cycles

DURING SCHEDULED PM CHECK, FOUND FWD ENTRY DOOR OVERHEAD AND SEVERAL BULLNOSE EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: TARGET — OUT OF ADJ (NLG) · airframe 53,104 hrs · 53,034 cycles

WHEN GEAR LOWERED FOR LANDING, GREEN LIGHT FOR NOSE GEAR DID NOT ILLUMINATE. AFTER MANUAL EXTENSION ALL INDICATIONS OK. FOUND NOSE GEAR POSITION SENSOR TARGET GAP OUT OF TOLERANCE. ADJUSTED TARGET AND CLEANED SENSOR PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,973 hrs · 52,913 cycles

DURING WALK AROUND INSPECTION FOUND FUSELAGE SKIN CRACKED 4 INCHES LONG BETWEEN BS 500A & BS 500C, STR 14R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,780 hrs · 52,758 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500C, STR 10L. REPAIRED SKIN PER SRM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 51,832 hrs · 51,945 cycles

DURING SCHEDULED C3 CHECK, FOUND EEPLS INOP. REMOVED AND REPLACED FWD AND AFT EEPLS BATTERY PACKS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,832 hrs · 51,945 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 767, STR 19L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,832 hrs · 51,945 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 380, STR 15L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,832 hrs · 51,945 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 480 & BS 500A, STR 10L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,832 hrs · 51,945 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT ENTRY DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF ADJ (ENTRY DOOR) · airframe 51,832 hrs · 51,945 cycles

DURING SCHEDULED C3 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUSTMENT. ADJUSTED EMERGENCY EVAC SLIDE GIRT ASSY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,832 hrs · 51,945 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D, JUST ABOVE STR 12L. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 51,698 hrs · 51,827 cycles

AFT SVC DOOR EMERGENCY EVAC SLIDE FELL OUT OF THE CASE. REINSTALLED SLIDE PER MM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 51,676 hrs · 51,809 cycles

AFT SVC DOOR EMERGENCY EVAC SLIDE FELL OUT OF THE CASE. REINSTALLED SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,187 hrs · 51,402 cycles

DURING WALK AROUND INSPECTION, FOUND 4 EXTERNAL FUSELAGE SKIN CRACK AT BS 747, BELOW STR 18R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,986 hrs · 51,228 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EXTERNAL FUSELAGE SKIN CRACKED AT AFT SVC DOOR LOWER FWD CUTOUT. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF ADJ (SERVICE DOOR) · airframe 50,916 hrs · 51,164 cycles

DURING SCHEDULED C2 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. RE-ADJUSTED EVAC SLIDE ASSY PER MM.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 49,953 hrs · 50,387 cycles

DURING SCHEDULED C1 CHECK, FOUND 1.25 INCH CRACK AT LT HORIZ STAB LWR SKIN, AFT SPAR, APPROX STA 157. REPAIRED SKIN PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,251 hrs · 49,814 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BS 178 BULKHEAD RT SIDE CHORD CRACKED, WL 207. REPAIRED CHORD PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 49,176 hrs · 49,745 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BS 178 BULKHEAD CRACKED, RBL 11.5 AND LBL 2.5. REPAIRED BULKHEAD PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 49,139 hrs · 49,711 cycles

DURING SCHEDULED C4 CHECK, FOUND STRINGER 10L CRACKED, BS 490. REPAIRED STRINGER PER SRM.

Part: WIRE — BROKEN (LH WING SLAT) · airframe 48,588 hrs · 49,234 cycles

AIR TURNBACK, NR 1 L/E SLAT TRANSIT LIGHT ILLUMINATED WITH FLAPS RETRACTED. VERIFIED FLAP/SLAT POSITION AND DEFERRED PER MEL. LATER AT DAL DURING RON REPAIRED BROKEN WIRE SPLICE AT NR 1 L/E SLAT ROD END.

Part: BATTERY — INOPERATIVE (CABIN) · airframe 48,349 hrs · 49,024 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EEPLS INOP FROM ROW 18 TO AFT END. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: PANEL — LOOSE (COCKPIT DOOR) · airframe 47,926 hrs · 48,670 cycles

COCKPIT DOOR EMERGENCY EXIT PANELS LOOSE. R&R COCKPIT DOOR PANELS BRAKE AWAY PIN PER MM.

Part: SKIN — CRACKED (BS 751)

DURING WALKAROUND INSPECTION, FOUND FUSELAGE SKIN CRACKED, BS 751, STRINGER 18R. REPAIRED PER SRM.

Part: SEAL — FAILED (NR 1 ENGINE)

AIR TURNBACK, IN FLIGHT SHUTDOWN. NR 1 ENG OIL QTY DECREASED TO LESS THAN .5 GAL, LOW OIL PRESS LIGHT ILLUMINATED. REMOVED AND REPLACED NR 1 ENG STARTER GEAR PAD SEAL PER MM.

Part: BRACKET — MISALIGNED (PAX DOORWAY)

LEFT AFT ENTRY DOOR LATCH WILL NOT ENGAGE GIRT BAR. REPOSITIONED AFT GIRT BAR BRACKET PER MM.

Part: FLOORBEAM — CORRODED (BS 294)

DURING SCHEDULED 1/2D CHECK, FOUND CORROSION AT FLOORBEAM, BS 294, LBL 7-11. REPAIRED BEAM PER SRM.

Part: FLOORBEAM — CORRODED (BS 312)

DURING SCHEDULED 1/2D CHECK, FOUND CORROSION ON FLOORBEAMS, BS 312, LBL 6-RBL 8, BS 294, LBL 21-RBL 24, AND BS 328 RBL 14. REPAIRED BEAM PER SRM.

Part: FLOORBEAM — CRACKED (BS 500)

DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CRACKED AT BS 500, RBL 14. REPAIRED BEAM PER SRM.

Part: BRACKET — CORRODED (PASSENGER DOOR)

DURING SCHEDULED 1/2D CHECK, FOUND CORROSION ON FWD AND AFT GIRT BAR ATTACH BRACKETS AT FWD ENTRY DOOR FLOOR. REMOVED AND REPLACED BRACKET ASSYS PER MM.

Part: BULB — FAILED (COCKPIT)

DURING SCHEDULED CHECK, FOUND EMERGENCY LIGHT INOP BEHIND CAPT SEAT. RELAMPED AND OPS GOOD PER M/M.

Part: SKIN — CRACKED (BS 178)

DURING SCHEDULED SC CHECK, FOUND SEVERAL FUSELAGE SKIN CRACK INDICATIONS AT BS 178. REPAIRED PER BOEING SRM.

Part: WEB — CRACKED (BS 663)

DURING SCHEDULED SC CHECK, FOUND 2 BEADED PRESSURE WEB CRACKS AT BS 663. REPAIRED PER SWA RA 1-353-1956.

Part: CHORD — CRACKED (BS 178)

DURING SCHEDULED SC CHECK, FOUND BS 178 T-CHORD CRACKED. REPAIRED PER SWA RA 1-353-1959.

Part: STRAP — SEVERED (BS 178)

DURING SCHEDULED SC CHECK, FOUND SUPPORT STRAP SEVERED AT BS 178. REPAIRED PER BOEING SRM.

Part: ANGLE — BROKEN (CARGO DOORWAY)

DURING SCHEDULED SERVICE CHECK, FOUND FWD B/B DOOR UP LATCH SUPPORT ANGLE BROKEN. REMOVED AND REPLACED SUPPORT ANGLE PER BOEING SRM.

Part: SKIN — CRACKED (PAX DOORWAY)

DURING SCHEDULED C2 CHECK, FOUND AFT ENTRY DOOR UPPER HINGE CUTOUT CRACKED .350. REPAIRED PER BOEING SRM.

Part: ENGINE — FAILED TEST (NR 1)

DURING SCHEDULED B/C CHECK, NR 1 ENGINE FAILED BORESCOPE INSPECTION, HPT BLADES OUT OF LIMITS. REPLACED ENGINE, THRUST LINK ASSEMBLY AND PRE-COOLER PER BOEING M/M.

Part: BATTERY — DISCHARGED (CABIN)

DURING SCHEDULED TERMINAL CHECK, FOUND FWD CABIN EMERGENCY TRACK LIGHTS INOP. REPLACED BATTERY PACK PER BOEING M/M.