N702ML

Part: LIGHT — INOPERATIVE (CABIN) · airframe 74,938 hrs · 60,509 cycles

ONE EA EEPLS INOP AT ROW 12. RELAMPED EEPLS PER MM.

Part: ACTUATOR — WORN (NLG STEERING) · airframe 74,905 hrs · 60,464 cycles

NOSE STEERING SYS INOP. C/W FOURTH LIFE PER MT, REMOVED AND REPLACED UPPER AND LOWER STEERING PLATES AND ACTUATOR ASSY PER MM.

Part: BEARING — WORN (NR 2 THROTTLE) · airframe 74,003 hrs · 60,077 cycles

NR 2 ENGINE THROTTLE STIFF AND WILL NOT STAY AT IDLE. REMOVED AND REPLACED NR 2 ENGINE THROTTLE CONTROL CROSS SHAFT BEARING PER MM.

Part: SLIDE — DISLODGED (AFT SVC DOOR) · airframe 74,644 hrs · 60,130 cycles

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

Part: INDICATOR — OUT OF POSITION (ESCAPE SLIDE) · airframe 74,446 hrs · 59,871 cycles

DURING SCHEDULED SERVICE CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM.

Part: INDICATOR — OUT OF POSITION (ESCAPE SLIDE) · airframe 74,446 hrs · 59,871 cycles

DURING SCHEDULED SERVICE CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM.

Part: ENGINE — LEAKING (NR 2) · airframe 74,427 hrs · 59,848 cycles

NR 2 ENGINE FUEL LEAKING FROM ENGINE CASE DIRECTLY UNDER P/D VALVE. REMOVED AND REPLACED NR 2 ENGINE PER MM.

Part: LENS — MISSING (EEPLS) · airframe 74,406 hrs · 59,819 cycles

EEPLS LIGHT AND LENS MISSING AT ROW NR 8. INSTALLED EEPLS LIGHT AND LENS ASSY PER MM.

Part: LIGHT — MISSING (CABIN) · airframe 74,337 hrs · 59,771 cycles

EEPLS RED LIGHTS MISSING AT OVERWING EXITS. INSTALLED EEPLS LIGHT BULB AND LENSES PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 74,323 hrs · 59,713 cycles

EEPLS INOP AT OVERWING EMERGENCY EXIT. REPAIRED EEPLS PER MM.

Part: SKIN — CRACKED (NR 3 L/E SLAT) · airframe 74,051 hrs · 59,368 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND NR 3 L/E SLAT SKIN CRACKED AT L/E, OUTBD OF ACTUATOR. REPAIRED NR 3 L/E SLAT PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 74,051 hrs · 59,368 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FLOORBEAM CORRODED AT BS 344, BL 0. REPAIRED FLOORBEAM PER SRM.

Part: WINDOW — CRACKED (COCKPIT) · airframe 18,566 hrs · 11,558 cycles

CAPT'S NR 1 WINDOW ARCING AND CRACKED. REMOVED AND REPLACED NR 1 WINDOW PER MM.

Part: COVER — CRACKED (CABIN) · airframe 73,890 hrs · 58,178 cycles

DURING SCHEDULED A1 CHECK, FOUND EEPLS COVER STRIP CRACKED AT MOST FWD 24. REMOVED AND REPLACED EEPLS STRIP PER MM.

Part: SWITCH — FAULTY (COCKPIT) · airframe 73,559 hrs · 59,131 cycles

ABORTED TAKEOFF, TAKEOFF WARNING HORN ACTIVATED. REMOVED AND REPLACED SPEED BRAKE TAKEOFF WARNING SWITCH PER MM.

Part: BATTERY — DISCHARGED (CARGO BAY) · airframe 73,831 hrs · 59,092 cycles

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

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 73,693 hrs · 58,917 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FWD SERVICE DOOR FRAME CRACKED AT BS 332.1, STR 8R. REPAIRED DOOR FRAME PER SWA EA.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 73,625 hrs · 58,831 cycles

DURING SCHEDULED C3 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: INDICATOR — OUT OF POSITION (ESCAPE SLIDE) · airframe 73,625 hrs · 58,831 cycles

DURING SCHEDULED C3 CHECK, FOUND AFT ENTRY DOOR EVACUATION SLIDE PRESSURE INDICATOR OUT OF VIEW. REPOSITIONED SLIDE ASSY PER MM.

Part: LIGHT — INOPERATIVE (MID CABIN) · airframe 73,611 hrs · 58,812 cycles

DURING SCHEDULED PM CHECK, FOUND OVERHEAD EMERGENCY EXIT LIGHT INOP AT MID CABIN. REMOVED AND REPLACED OVERHEAD EMERGENCY EXIT LIGHT ASSY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,279 hrs · 58,401 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 530, ABOVE STR 15L. REPAIRED SKIN PER SWA EA.

Part: CONTROL PANEL — MALFUNCTIONED (COCKPIT) · airframe 72,774 hrs · 57,772 cycles

BOTH FLIGHT DIRECTORS WENT TO GA MODE AND ARCED SMELL IN COCKPIT. REMOVED AND REPLACED SELECTOR FLIGHT DIRECTOR MODE CONTROL PANEL PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 72,767 hrs · 57,761 cycles

DURING SCHEDULED A1 CHECK, FOUND THE OVERWING EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED THE OVERWING EMERGENCY EXIT LIGHT BATTERY PACK PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 72,656 hrs · 57,617 cycles

DURING SCHEDULED PM CHECK, FOUND OVERHEAD EMERGENCY EXIT LIGHT LOOSE AT MID CABIN. SECURED EXIT LIGHT PER MM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 72,270 hrs · 57,144 cycles

EMERGENCY FLASHLIGHT INOP AT FWD CABIN INBD. REMOVED AND REPLACED BATTERY PER MM.

Part: PCU — LEAKING (ELEVATOR) · airframe 71,725 hrs · 56,459 cycles

AIR TURNBACK, AFTER TAKEOFF LOST 'B' HYDRAULIC SYSTEM QUANTITY. FOUND 'B' SYSTEM ELEVATOR PCU LEAKING. REMOVED AND REPLACED 'B' SYSTEM ELEVATOR PCU PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 71,653 hrs · 56,370 cycles

DURING SCHEDULED A2 CHECK, FOUND EMERGENCY EXIT LIGHT AT MID CABIN OVERHEAD INOP AND LENS BROKEN. REMOVED AND REPLACED BATTERY AND LENS PER MM.

Part: BRACKET — LOOSE (AFT SVC DOOR.) · airframe 71,476 hrs · 56,144 cycles

DURING SCHEDULED CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR BRACKET LOOSE. REMOVED AND REPLACED FWD GIRT BAR BRACKET FASTENERS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 71,336 hrs · 55,970 cycles

DURING SCHEDULED PM CHECK, FOUND AFT SVC DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED EXIT LIGHT ASSY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,310 hrs · 55,941 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT FWD RADIO ALTIMETER ANTENNA CUT OUT, BS 370 AND WL 148. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 70,820 hrs · 55,328 cycles

DURING SCHEDULED C3 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 70,797 hrs · 55,298 cycles

DURING SCHEDULED A1 CHECK, FOUND OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 70,780 hrs · 55,276 cycles

DURING SCHEDULED RON, FOUND BOTH AFT CABIN DOOR EMERGENCY EVAC SLIDE LIGHTS INOP. REMOVED AND REPLACED SLIDE LIGHT BATTERY PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 70,466 hrs · 54,884 cycles

EEPLS INOP AT ROW NR 3. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: WEB — CRACKED (FUSELAGE) · airframe 70,119 hrs · 54,466 cycles

DURING SCHEDULED 1/4D CHECK, FOUND VERTICAL BEAM WEB CRACKED .75 INCH LONG AT BS 180,WL 177 AND LBL 5.7. REPAIRED WEB PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,119 hrs · 54,466 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FWD ENTRY DOOR LOWER HINGE CUTOUT CRACKED. REPAIRED SKIN PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 70,119 hrs · 54,466 cycles

DURING SCHEDULED 1/4D CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 182, WL 185 & RBL 5.7. REPAIRED WEB PER SWA RA.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 70,119 hrs · 54,466 cycles

DURING SCHEDULED 1/4D CHECK, FOUND VERTICAL CHORD CRACKED 1.0 INCH LONG AT BS 178, WL 183 AND RBL 5.7. REMOVED AND REPLACED CHORD PER SRM.

Part: STIFFENER — CRACKED (LT MLG W/W) · airframe 70,119 hrs · 54,466 cycles

DURING SCHEDULED 1/4D CHECK, FOUND VERTICAL STIFFENER CRACKED AT BS 663, LBL 57. REMOVED AND REPLACED STIFFENER PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 70,119 hrs · 54,466 cycles

DURING SCHEDULED 1/4D CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 180, WL 184 AND RBL 5.7. REPAIRED WEB PER SWA RA.

Part: SHEAR TIE — CORRODED (FWD CARGO) · airframe 70,119 hrs · 54,466 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BELTFRAME SHEAR TIE CORRODED AT BS 500, RBL 10.5. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (E/E COMP) · airframe 70,119 hrs · 54,466 cycles

DURING SCHEDULED 1/4D CHECK, FOUND SHEAR TIE CORRODED AT BS 360, RBL 10. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 70,119 hrs · 54,466 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 500, STR 27R. REPAIRED SKIN PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 70,119 hrs · 54,466 cycles

DURING SCHEDULED 1/4D CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 180, WL 183.5 AND RBL 17.1. REPAIRED WEB PER SRM.

Part: BRACKET — CORRODED (CABIN FLOOR) · airframe 70,119 hrs · 54,466 cycles

DURING SCHEDULED 1/4D CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE GIRT BAR AFT FLOOR BRACKET CORRODED. REMOVED AND REPLACED GIRT BAR BRACKET PER MM.

Part: SOCKET — DEFECTIVE (CABIN) · airframe 69,977 hrs · 54,317 cycles

EEPLS INOP AT OVERWING EMERGENCY EXIT. REMOVED AND REPLACED LIGHT SOCKET PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 69,932 hrs · 54,265 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FWD LT EXTERIOR EMERGENCY LIGHT INOP. RELAMPED LIGHT PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 69,782 hrs · 54,098 cycles

EEPLS LOOSE AT ROW 2. SECURED EEPLS PER MM.

Part: SLIDE — UNSERVICEABLE (R1 DOOR) · airframe 69,608 hrs · 53,894 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FWD SERVICE DOOR EVACUATION SLIDE PRESS IND LOW. REMOVED AND REPLACED SLIDE ASSY PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 69,334 hrs · 53,551 cycles

DURING SCHEDULED A2 CHECK, FOUND EEPLS INOP AT ROW 18. RELAMPED EEPLS PER MM.

Part: LENS — MISSING (CABIN) · airframe 69,164 hrs · 53,349 cycles

EEPLS MISSING LENS AT ROWS 4 & 6. INSTALLED LENSES PER MM..

Part: LENS — MISSING (CABIN) · airframe 69,164 hrs · 53,349 cycles

EEPLS MISSING LENS AT ROW 18. INSTALLED LENS PER MM.

Part: LIGHT — INOPERATIVE (AFT ENTRY DOOR) · airframe 69,126 hrs · 53,299 cycles

DURING SCHEDULED SERVICE CHECK, FOUND AFT ENTRY DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: LENS — LOOSE (CABIN) · airframe 68,752 hrs · 52,849 cycles

DURING SCHEDULED A2 CHECK, FOUND OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. SECURED EXIT LIGHT LENS PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 68,752 hrs · 52,849 cycles

DURING SCHEDULED A2 CHECK, FOUND 3 EMERGENCY EXIT CEILING LIGHTS INOP. REMOVED AND REPLACED EXIT LIGHT BATTERY PACKS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 68,642 hrs · 52,721 cycles

DURING SCHEDULED C4 CHECK, FOUND EEPLS LOOSE, MISSING LENS AND INOP AT ROW 18. REMOVED AND REPLACED EEPLS ASSY PER MM.

Part: LIGHT — DAMAGED (CABIN) · airframe 68,634 hrs · 52,711 cycles

EEPLS DAMAGED AT ROW 1. REPAIRED EEPLS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 68,486 hrs · 52,535 cycles

DURING SCHEDULED RON CHECK, FOUND SEVERAL EEPLS INOP AND LOOSE. REPAIRED AND SECURED EEPLS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 68,297 hrs · 52,324 cycles

EEPLS INOP AT ROW 3. RELAMPED EEPLS PER MM.

Part: LENS — MISSING (CABIN) · airframe 68,060 hrs · 52,054 cycles

EEPLS LENSES MISSING AT ROW 18 AND ROW 20. REPLACED EEPLS LENSES PER MM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 67,953 hrs · 51,936 cycles

AFT ENTRY DOOR AND AFT SVC DOOR EMERGENCY EVAC SLIDES PRES IND OUT OF VIEW. REPOSITIONED EMERGENCY EVAC SLIDES PER MM.

Part: BATTERY PACK — LOOSE (CABIN) · airframe 67,866 hrs · 51,840 cycles

DURING SCHEDULED C3 CHECK, FOUND EMERGENCY EXIT LIGHT BATTERY PACK LOOSE AT AFT CABIN. SECURED BATTERY PACK PER MM.

Part: LENS — MISSING (CABIN) · airframe 67,866 hrs · 51,840 cycles

DURING SCHEDULED C3 CHECK, FOUND EEPLS FLOOR TRACK BROKEN AT ROW 15, LENS MISSING AT ROW 20 & END CAP MISSING AT AFT SECTION. REPLACED TRACK COVER, LENS & END CAP PER MM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 67,771 hrs · 51,734 cycles

AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED EVAC SLIDE ASSY PER MM.

Part: LENS — MISSING (CABIN) · airframe 67,520 hrs · 51,426 cycles

EEPLS LENS COVER MISSING AT ROW 18. INSTALLED LENS PER MM.

Part: SKIN — DELAMINATED (T/E FLAP) · airframe 67,363 hrs · 51,259 cycles

DURING SCHEDULED SERVICE CHECK, FOUND LT INBD T/E AFT FLAP OTBD EDGE DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.

Part: SLIDE — OUT OF POSITION (SEVICE DOOR) · airframe 67,187 hrs · 51,064 cycles

AFT ENTRY AND SVC DOOR EMERGENCY EVAC SLIDE PRESS INDICATORS OUT OF VIEW. RE-ADJUSTED EVAC SLIDE ASSY PER MM.

Part: INDICATOR — OUT OF POSITION (SLIDE) · airframe 67,089 hrs · 50,949 cycles

DURING SCHEDULED C2 CHECK, FOUND AFT SVC AND ENTRY DOOR EMERGENCY EVAC SLIDE PRESS INDICATORS OUT OF VIEW. REPOSITIONED EVAC SLIDE ASSY''S PER MM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 66,871 hrs · 50,716 cycles

R2 DOOR EVAC SLIDE PRESS INDICATOR OUT OF VIEW. REPOSITIONED SLIDE ASSY PER MM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 66,814 hrs · 50,653 cycles

AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED EVAC SLIDE ASSY PER MM.

Part: INDICATOR — OUT OF POSITION (ESCAPE SLIDE) · airframe 66,546 hrs · 50,360 cycles

BOTH EMEGRENCY EVAC SLIDE PRESS INDS OUT OF VIEW. REPOSITIONED BOTH SLIDE ASSY''S PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 66,278 hrs · 50,060 cycles

DURING SCHEDULED C1 CHECK, FOUND OVERHEAD EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY CHARGER BASE PER MM.

Part: INDICATOR — OUT OF POSITION (SLIDE) · airframe 66,278 hrs · 50,060 cycles

DURING SCHEDULED C1 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. RE-ADJUSTED SLIDE ASSY PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 65,968 hrs · 49,712 cycles

EMERGENCY EXIT LIGHT COVER LOOSE AT MID CABIN. SECURED COVER PER MM.

Part: BATTERY — INOPERATIVE (CABIN) · airframe 65,968 hrs · 49,712 cycles

DURING SCHEDULED SERVICE CHECK, FOUND AFT GALLEY AISLE EMERGENCY LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: COVER — LOOSE (CABIN) · airframe 65,968 hrs · 49,712 cycles

DURING SCHEDULED SERVICE CHECK, FOUND MID CABIN EMERGENCY EXIT LIGTH COVER LOOSE. SECURED COVER PER MM.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 65,958 hrs · 49,698 cycles

DURING SCHEDULED A2 CHECK, FOUND LT WING O/B TRAILING EDGE FLAP O/B UPPER SKIN DELAMINATED. REMOVED AND REPLACED FLAP ASSY PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,728 hrs · 49,452 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BS 178 BULKHEAD LT SIDE CHORD CRACKED, LBL 28. REPAIRED CHORD SECTION PER ACO.

Part: MODULE — MALFUNCTIONED (FLAP/SLAT) · airframe 65,728 hrs · 49,452 cycles

ABORTED TAKEOFF, NR 1 KRUEGER FLAP TRANSIT LIGHT ILLUMINATED. REMOVED AND REPLACED FLAP/SLAT POS MODULE PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 65,385 hrs · 49,058 cycles

DURING SCHEDULED A2 CHECK, FOUND EEPLS INOPERATIVE AT ROWS 7 AND 19. R & R LIGHT ASSY''S PER MM.

Part: COVER — MISSING (CABIN) · airframe 64,971 hrs · 48,622 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EEPLS TRACK COVER MISSING AT ROW 7. REPLACED TRACK COVER PER MM.

Part: COVER — MISSING (ROW 14) · airframe 64,952 hrs · 48,600 cycles

EEPLS TRACK COVER MISSING AT ROW 14. INSTALLED TRACK COVER PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 64,763 hrs · 48,406 cycles

SEVERAL EEL ARE LOOSE. SECURED AND REPAIRED LIGHT ASSY PER MM.

Part: INDICATOR — OUT OF POSITION (ESCAPE SLIDE) · airframe 64,655 hrs · 48,281 cycles

DURING SCHEDULED C3 CHECK, FOUND AFT SERVICE DOOR EVACUATION SLIDE PRESSURE INDICATOR OUT OF VIEW. REPOSITIONED SLIDE ASSY PER MM.

Part: INDICATOR — DISLODGED (ESCAPE SLIDE)

AFT SERVICE DOOR EVACUATION SLIDE PRESS INDICATOR OUT OF VIEW. REPOSITIONED SLIDE ASSY PER MM.

Part: LIGHT — INOPERATIVE (CABIN)

EEPLS LIGHT AFT END INOP. RELAMPED LIGHT ASSY PER MM.

Part: SKIN — CRACKED (BS 520)

DURING SCHEDULED RON, FOUND FUSELAGE EXTERNAL SKIN CRACKED, BS 520, STRINGER 16R. REPAIRED SKIN PER SRM.

Part: WIRE — FAILED (COMMUNICATIONS)

AIR TURNBACK, BOTH COMMUNICATION RADIOS INOP AFTER TAKEOFF. REPAIRED SHORT WIRE IN CAPT'S SIDEWALL PANEL, AND REMOVED AND REPLACED CAPT'S HAND MIC JACK.

Part: LIGHT — INOP (CABIN)

DURING SCHEDULED D CHECK, FOUND AFT LT AND RT EMERGENCY EVACUATION SLIDE EXIT LIGHTS INOP. REMOVED AND REPLACED LIGHT ASSY'S PER MM.

Part: STIFFNER — CORRODED (BS 235)

DURING SCHEDULED D CHECK, FOUND CORRODED STIFFENER CHORD, BS 235, RBL 9, WL 182. REMOVED AND REPLACED CHORD SECTION PER SRM.

Part: FLOORBEAM — CRACKED (BS 520)

DURING SCHEDULED D CHECK, FOUND BS 520 FLOORBEAM CRACKED AT 2 EACH PLACES, LBL 45 AND RBL 45. REPAIRED FLOORBEAM PER SRM.

Part: BULKHEAD WEB — CRACKED (BS 663)

DURING SCHEDULED D CHECK, FOUND BS 663 PRESSURE WEB CRACKED, RBL 39, WL 203. REPAIRED WEB PER ER NR 99-5890.

Part: BEAM — CORROSION (LH MLG)

DURING SCHEDULED D CHECK, FOUND CORROSION ON LT MAIN LANDING GEAR BEAM ATTACH FITTING, FWD OUTBOARD HOLE. REPAIRED BEAM PER ER NR 99-5782.

Part: BULKHEAD — CORRODED (BS 1016)

DURING SCHEDULED D CHECK, FOUND BS 1016 PRESSURE BULKHEAD CORRODED, LBL 7, WL 192. REPAIRED BULKHEAD PER BS 737-53A1075 AND DRAWING 65C28106.

Part: FITTING — CORRODED (LT MLG)

DURING SCHEDULED D CHECK, FOUND CRACKED RT MAIN LANDING GEAR BEAM ATTACH FITTING AT SECOND INBOARD HOLE. REPAIRED BEAM ASSY PER ER 99-5833.

Part: TRACK — CORRODED (LT TE FLAP)

DURING SCHEDULED D CHECK, FOUND NR 2 FLAP TRACK HAS PITTING CORROSION ON AFT MOUNTING SURFACE. REMOVED AND REPLACED NR 2 FLAP TRACK ASSY PER MM.

Part: STRINGER — CORROSION (AFT FUSELAGE)

DURING SCHEDULED D CHECK, FOUND STRINGER 24R CORRODED, BS 986-1016. REMOVED AND REPLACED STRINGER SECTION PER SRM.

Part: BEAM — CRACKED (BS 727)

DURING SCHEDULED D CHECK, FOUND CREASE BEAM INBOARD CHORD CRACKED, BS 727, RBL 63. REMOVED AND REPLACED CREASE BEAM INBOARD SECTION, BS 672-727+6 PER SRM.

Part: KEEL BEAM — CORRODED (BS 727-817)

DURING SCHEDULED D CHECK, FOUND CORRODED KEEL BEAM, BS 727 TO BS 817 RT SIDE. REMOVED AND REPLACED KEEL BEAM SECTION PER SRM.

Part: STRINGER — CRACKED (BS 908)

DURING SCHEDULED D CHECK, FOUND STRINGER SPLICE CRACKED BS 908, STR 4L. REMOVED AND REPLACED STRINGER SPLICE SECTION PER ER NR 99-5927.

Part: FLOORBEAM — CORRODED (BS 1016)

DURING SCHEDULED D CHECK, FOUND BS 1016 FLOORBEAM CORRODED, LBL 28.5-33.5. REPAIRED BEAM PER ER NR 99-5770.

Part: SHEAR TIE — CORRODED (BS 1040)

DURING SCHEDULED D CHECK, FOUND BS 1040 SHEAR TIE CRACKED AT STRINGER 13R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (BS 520)

DURING SCHEDULED D CHECK, FOUND BS 520 SHEAR TIE CORRODED AT STRINGER 27L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CRACKED (BS 360)

DURING SCHEDULED D CHECK, FOUND FUSELAGE SHEAR TIE CRACKED, BS 360, BELOW STRINGER 14R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (BS 767)

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED, BS 767, LBL 69, WL 236. REPAIRED FRAME PER MM.

Part: SKIN — CRACKED (VERT STAB)

DURING SCHEDULED D CHECK, FOUND LT SIDE OF VERTICAL STAB SKIN CRACKED, STA 91, JUST AFT OF FRONT SPAR. REPAIRED SKIN PER SRM.

Part: CREASE BEAM — CORROSION (BS 812)

DURING SCHEDULED D CHECK, FOUND CORRODED CREASE BEAM, BS 812, RBL 64. REPAIRED CREASE BEAM PER SRM.

Part: FLOORBEAM — CORRODED (BS 794)

DURING SCHEDULED D CHECK, FOUND CORRODED FLOORBEAM LOWER SURFACE, BS 794, RBL 64. REPAIRED BEAM PER SRM.

Part: FRAME — CORRODED (CARGO DOOR)

DURING SCHEDULED D CHECK, FOUND CORROSION ON FWD CARGO DOOR FRAME, BS 492. REPAIRED FRAME PER SRM.

Part: PLATE — CORRODED (PAX DOORWAY)

DURING SCHEDULED D CHECK, FOUND FWD ENTRY DOOR, FWD GIRT BAR ATTACH BRACKET MOUNT PLATE CORRODED. REMOVED AND REPLACED MOUNT PLATE PER MM.

Part: STRINGER — CRACKED (BS 375)

DURING SCHEDULED D CHECK, FOUND STRINGER 5L LOWER FLANGE CRACKED AT BS 375. REPAIRED STRINGER PER SRM.

Part: STRINGER — CRACKED (BS 1010)

DURING SCHEDULED D CHECK, FOUND STRINGER 7L CRACKED, BS 1010. REPAIRED STRINGER PER SRM.

Part: RIB — CRACKED (LT HORIZ STAB)

DURING SCHEDULED D CHECK, FOUND LT HORIZONTAL STAB L/E RIB CRACKED, STA 123.85. REPAIRED RIB PER SRM.

Part: CHORD — CORRODED (BS 270)

DURING SCHEDULED D CHECK, FOUND CORROSION ON Z-CHORD, BS 270, LBL 6.5-RBL 3. REMOVED AND REPLACED CHORD PER SRM.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED D CHECK, FOUND 3 EACH CRACKS AT BS 178 BULKHEAD, BETWEEN LBL 5- LBL 12. REPAIRED BULKHEAD PER SRM.

Part: CLIP — CRACKED (BS 520)

DURING SCHEDULED D-CHECK, FOUND 2 STRINGER CLIPS CRACKED, BS 520, STRINGERS 19L AND 19R. REMOVED AND REPLACED STRINGER CLIPS PER SRM.

Part: BULKHEAD — CRACKED (BS 178.)

DURING SCHEDULED D-CHECK, FOUND BS 178 BULKHEAD CRACKED, RBL 10, WL 234. REPAIRED BULKHEAD PER SRM.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY ESCAPE FLOOR TRACK LIGHT INOP AT FWD END. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING SCHEDULED RON CHECK, FOUND FWD OVERHEAD EMERGENCY EXIT SIGN INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SKIN — CRACKED (BS 727)

DURING SCHEDULED C4 CHECK, FOUND ONE 2.5 INCH CRACK, ONE 2 INCH CRACK AT FUSELAGE SKIN BS 727B, WL 200. ALSO, FOUND A 4.5 INCH CRACK AT BS 727A, WL 200. REPAIRED SKIN CRACKS PER SRM.

Part: LIGHT — INOPERATIVE (ROW 15 & 17)

EMERGENCY LIGHTING TRACK CAME LOOSE AT ROW 17 AND INOPERATIVE AT ROW 15. SECURED LIGHT AT ROW 17 AND REPLACED TRACK SECTION AT ROW 15 PER MM.

Part: SKIN — CRACKED (BS 732)

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 732, S23R. REPAIRED PER BOEING SRM.

Part: SLIDE — LOW PRESS (CABIN)

DURING SC, FOUND FWD SERVICE DOOR ESCAPE SLIDE PRESS LOW. REPLACED PER BOEING M/M.

Part: SKIN — CRACKED (BS 944)

DURING SCHEDULED C3, FOUND FUSE SKIN CRACKED AT BS 944, AT S24L. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (BS 760/727)

DURING SCHEDULED T/C CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 760 AT S17L, 3 AFT OF EXISTING DOUBLER AND AT BS 727C, AT S16R BETWEEN EXISTING DOUBLER. REPAIRED BOTH PER BOEING SRM.

Part: SLIDE — HIGH PRESS (SERVICE DOOR)

DURING WALKAROUND CHECK, FOUND AFT SERVICE DOOR SLIDE PRESSURE EXCESSIVE. REPLACED SLIDE PER BOEING M/M.

Part: BATTERY — UNSECURED (CABIN)

DURING 1/4 D-CHECK, FOUND EMERGENCY ESCAPE LIGHTING BATTERY PACK NOT SECURED. PROPERLY SECURED BATTERY PACK PER BOEING M/M.

Part: WIRE — BROKEN (CABIN)

DURING SCHEDULED RON CHECK, FOUND MID CABIN EMERGENCY EXIT LIGHT INOP. REPAIRED A BROKEN WIRE AT NR 1 PIN PER BOEING M/M.

Part: SKIN — CRACKED (FUSELAGE)

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED, AT FWD END BY EXTERNAL AIR ACCESS PANEL. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (BS 727)

DURING SCHEDULED A1 CHECK, FOUND A 2 FUSELAGE SKIN CRACK AT BS 727B-C, AT S17L. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (BS 727)

DURING SCHEDULED A1 CHECK, FOUND A 2 FUSELAGE SKIN CRACK AT BS 727A, AT S16L. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (SERVICE DOORWAY)

DURING SCHEDULED B-CHECK, FOUND FWD SERVICE AND AFT SERVICE DOORS LOWER HINGE CUTOUTS CRACKED. REPAIRED PER BOEING SRM.

Part: LIGHT — INOPERATIVE (CABIN)

DURING SCHEDULED B-CHECK, FOUND FWD SERVICE OVERHEAD EMERGENCY EXIT LIGHT INOP. RELAMPED AND OP CHECKED PER BOEING M/M.

Part: SKIN — CRACKED (BS 767)

DURING SCHEDULED SPECIAL VISIT CHECK, FOUND FUSELAGE SKIN DENTED AT BS 767, S18L. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (BS 727)

DURING SCHEDULED SPECIAL VISIT CHECK, FOUND SKIN CRACKED AT BS 727 PLUS 2, S17L. REPAIRED PER BOEING SRM.

Part: SLIDE — LOW PRESS (PAX DOOR)

DURING SCHEDULED TERMINAL CHECK, FOUND FWD ENTRY DOOR SLIDE PRESSURE LOW. REPLACED SLIDE PER BOEING M/M.

Part: SKIN — CRACKED (BS 807)

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 807, STRINGER 18L. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (BS 750)

DURING SCHEDULED TERMINAL CHECK, FOUND FUSELAGE SKIN CRACK ON RT SIDE ABOVE WING FAIRING AT BS 750. REPAIRED PER BOEING SRM.

Part: BATTERY — DISCHARGED (CABIN)

DURING SCHEDULED A2 CHECK, FOUND EMERGENCY BATTERY PACKS FOR OVERWING LIGHTS WILL NOT HOLD CHARGE. REPLACED BATTERY PACKS PER BOEING M/M.

Part: SKIN — CRACKED (PAX DOOR CUTOUT)

DURING SCHEDULED SV CHECK, FOUND FUSELAGE SKIN CRACKED .5 INCH ON LOWER AFT ENTRY DOOR CUTOUT. REPAIRED PER BOEING SRM AND S/B 737-53-1074.

Part: BATTERY — DISCHARGED (CABIN)

DURING SCHEDULED SV CHECK, FOUND LEFT OVERWING EXTERNAL EMERGENCY EXIT LIGHT INOP. REPLACED BATTERY PACK PER BOEING M/M.

Part: SKIN — CRACKED (SERV DR CUTOUT)

DURING SCHEDULED SV CHECK, FOUND FUSELAGE SKIN CRACKED .25 INCH ON UPPER HINGE CUTOUT AT AFT SERVICE DOOR. REPAIRED PER BOEING SRM.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING SCHEDULED A2 CHECK, FOUND EMERGENCY EXIT LIGHTS AT OVERWING EXIT INOP. REPLACED BATTERY PACK PER BOEING M/M.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING SCHEDULED A1 CHECK, FOUND MID CABIN CEILING LIGHTS INOP. REPLACED BATTERY PACK PER BOEING M/M.

Part: EEL — INOP (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND ALL EMERGENCY EXIT LIGHTS INOP. REPLACED FWD FLOOR TRACK BATTERY HOUSING, AFT FLOOR TRACK BATTERY PACK, AFT SERVICE DOOR PORTABLE LIGHT ASSEMBLY, RELAMPED FLOOR TRACK LIGHTS AND EXIT SIGNS PER BOEING M/M.

Part: SKIN — CRACKED (BS 530/534)

DURING SCHEDULED 1/2 D-CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 534 AND 530, AT S14L. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: BELTFRAME — CRACKED (RT AC BAY)

DURING SCHEDULED 1/2 D-CHECK, FOUND FAIRING SUPPORT BELT FRAME CRACKED 2 INCHES BELOW AIR DUCT. REPAIRED PER SWA ACO 518-53.

Part: CHORD — CRACKED (BS 663.75)

DURING SCHEDULED 1/2 D-CHECK, FOUND COMPRESSION CHORDS CRACKED AT BS 663.75, LBL 24.75 AND AT RBL 24.75. REPAIRED PER BOEING DRAWING 691A0032 AND BOEING STRUCTURAL REPAIR MANUAL.

Part: FRAME — CRACKED (BS 727)

DURING SCHEDULED 1/2 D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727B BETWEEN S4 AND 5L. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: BLKHD CHORD — CRACKED (BS 1156)

DURING SCHEDULED 1/2 D-CHECK, FOUND BS 1156 BULKHEAD LEFT CHORD CRACKED 1.5 INCHES IN LENGTH AND RUNNING VERTICALLY. REPAIRED PER SWA ACO 473-53 AND BOEING STRUCTURAL REPAIR MANUAL.

Part: WEB — CRACKED (APU INLET)

DURING SCHEDULED 1/2 D-CHECK, FOUND APU AIR INLET O/B WEB CRACKED 1 INCH LONG WITH A HOLE .25 INCH WIDE. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: WEB — CRACKED (SERVICE DOORWAY)

DURING SCHEDULED 1/2 D-CHECK, FOUND AFT SERVICE DOORWAY WEB BELOW ASSIST HANDLE CRACKED AT UPPER END. REPAIRED PER SWA ACO 471-53.

Part: ANGLE — CRACKED (BS 540)

DURING SCHEDULED 1/2 D-CHECK, FOUND ANGLE CRACKED AT BS 540 AT TOP FAIRING SUPPORT FRAME. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: CHORD — CRACKED (WBL 135.5)

DURING SCHEDULED 1/2 D-CHECK, FOUND RIGHT WING RIB LOWER CHORD CRACKED AT WBL 135.5, FWD OF S2 AT RADIUS. REPAIRED PER SWA ACO 587-57.

Part: HYD LINE — RUPTURED (AILERON PCU)

ON APPROACH, CREW EXPERIENCED A-SYSTEM PRESSURE LOSS. AIRCRAFT LANDED WITHOUT INCIDENT. INSPECTED AND FOUND AN AILERON PCU LINE RUPTURED. REPLACED LINE, FLUSHED SYSTEM, AND INSPECTED FILTERS PER BOEING M/M.

Part: WEB — CRACKED (BS 639)

DURING SCHEDULED C3 CHECK, FOUND WEB CRACKED AT FLOOR LEVEL FWD OF BELT FRAME AT BS 639. REPAIRED PER BOEING SRM.