N795SW

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 66,172 hrs · 38,857 cycles

EMERGENCY LIGHTS FAILED CAPACITY CHECK AT M01669. / R&R BATTERY PER MM.

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 66,172 hrs · 38,857 cycles

EMERGENCY LIGHTS FAILED CAPACITY CHECK AT M01673. / R&R BATTERY PER MM.

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 66,172 hrs · 38,857 cycles

EMERGENCY LIGHTS FAILED CAPACITY CHECK AT M01672. / R&R BATTERY PER MM.

Part: SENSOR — FAULTY (NLG) · airframe 65,988 hrs · 38,739 cycles

DECLARED EMERGENCY/AIR TURNBACK---------------------------------------------------BOTH RED AND GREEN NOSE GEAR INDICATOR LIGHTS ILLUMINATED AFTER SELECTING LANDING GEAR UP. / R&R SENSOR S845 PER AMM.

Part: SLIDE — DISLODGED (L1 DOOR) · airframe 65,885 hrs · 38,682 cycles

L1 DOOR ESCAPE SLIDE FELL OUT OF HOUSING. / REPOSITIONED SLIDE PER MT.

Part: HANDLE — STUCK (R2 DOOR) · airframe 65,303 hrs · 38,316 cycles

AFT SERVICE DOOR HANDLE STUCK IN CLOSED POSITION. AFT SERVICE LIGHT IS ON. OPS CHECK OF R2 DOOR PER AMM.

Part: LIGHT — DETACHED (OVERWING) · airframe 63,842 hrs · 37,369 cycles

CEILING OVERWING WINDOW EXIT SIGN LENS FELL OFF. / R&R LIGHT ASSEMBLY PER AMM.

Part: PTU — LEAKING (MLG WW) · airframe 63,241 hrs · 37,006 cycles

DECLARED EMERGENCY, FUMES DETECTED IN BOTH CABINS. FOUND HYD POWER TRANSFER UNIT LEAKING AT FLOW LIMITER. R&R POWER TRANSFER UNIT PER MM.

Part: LANYARD — LOOSE (L1 DOOR) · airframe 62,749 hrs · 36,701 cycles

L1 DOOR SLIDE COVER LANYARD LOOSE. SECURED LANYARD IAW MT.

Part: BAFFLE — CRACKED (FUSELAGE) · airframe 62,749 hrs · 36,701 cycles

FORWARD PIT BILGE BODY FRAME INTERCOSTAL BAFFLE UPPER FLANGE CRACKED AT BS 500B+1, RBL 25. R&R BAFFLE IAW DWG & SRM.

Part: BAFFLE — CORRODED (FUSELAGE) · airframe 62,749 hrs · 36,701 cycles

AFT PIT BILGE BODY FRAME INTERCOSTAL BAFFLE UPPER FLANGE CORRODED BETWEEN BS 747 TO BS 767, RBL 23. R&R BAFFLE IAW SRM AND DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 62,749 hrs · 36,701 cycles

FORWARD RT CREASE BEAM WEB PRESSURE DECK SHEAR TIE FASTENERS CORRODED AT BS 716. R&R ANGLE IAW DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 62,749 hrs · 36,701 cycles

RT CREASE BEAM WEB PRESSURE DECK SHEAR TIE FASTENERS CORRODED AT BS 716. R&R ANGLE IAW DWG.

Part: PLATE — CRACKED (LT WING) · airframe 62,749 hrs · 36,701 cycles

LT WING LOWER TRAILING EDGE WAFFLE PLATE CRACKED AT FASTENER HOLE. R&R WAFFLE PLATE IAW SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 62,749 hrs · 36,701 cycles

R1 DOOR CUTOUT FORWARD FRAME CRACKED AT LOWER EDGE BS 294. REPAIRED FRAME IAW SRM & DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 62,749 hrs · 36,701 cycles

CREASE BEAM WEB SHEAR TIE CORRODED AT BS 667, RBL 69. R&R SHEAR TIE IAW EA.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 62,749 hrs · 36,701 cycles

RT CREASE BEAM CORRODED BETWEEN BS 927+10 TO BS 986.5+6. R&R CREASE BEAM PER SRM AND DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 62,749 hrs · 36,701 cycles

RT CREASE BEAM WEB PRESSURE DECK SHEAR TIE FASTENERS CORRODED AT BS 706. R&R ANGLE IAW DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 62,749 hrs · 36,701 cycles

AFT CARGO COMPARTMENT FLOOR STRUCTURE LT SIDE Z-ANGLE CORRODED BETWEEN BS 727B+6 TO BS 847. R&R "Z" ANGLE IAW SRM AND DWG.

Part: BEAM — CRACKED (R1 DOOR) · airframe 62,749 hrs · 36,701 cycles

R1 DOOR INTERNAL NR 4 LOWER BEAM CRACKED IN RADIUS NEAR FORWARD-INBOARD FASTENER HOLE COMMON TO HANDLE BOX HOUSING. R&R NR 4 LOWER BEAM IAW SRM AND DWG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 62,749 hrs · 36,701 cycles

FORWARD CARGO PIT RT BAFFLE CLIP CRACKED AT BS 500B. R&R BAFFLE CLIP IAW DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 62,749 hrs · 36,701 cycles

FORWARD CARGO PIT LT Z-ANGLE CORRODED BETWEEN BS 400+10 TO BS 480+10, LBL 24. R&R "Z" ANGLE IAW SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 62,749 hrs · 36,701 cycles

FORWARD CARGO PIT LT BAFFLE CLIP CRACKED AT BS 500B. R&R CLIP IAW SRM & DWG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 62,749 hrs · 36,701 cycles

FORWARD CARGO PIT LT BAFFLE CLIP AFT SIDE OF BS 500B FRAME CRACKED. R&R CLIP IAW SRM & DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 62,749 hrs · 36,701 cycles

FORWARD CARGO PIT RT Z-ANGLE STA 500A-500D UPPER SURFACE CORRODED BETWEEN BS 500A TO BS. 500D. R&R Z ANGLE IAW DWG.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 62,749 hrs · 36,701 cycles

AFT CARGO COMPARTMENT FLOOR STRUCTURE TRACK CORRODED BETWEEN BS 787 TO BS 867, RBL 13. R&R TRACK IAW SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 62,749 hrs · 36,701 cycles

FORWARD CARGO PIT R/H BAFFLE CLIP CRACKED FORWARD SIDE OF BS 500C. R&R BAFFLE CLIP IAW SRM AND DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 62,749 hrs · 36,701 cycles

FORWARD CARGO PIT LT Z-ANGLE CORRODED BETWEEN BS 500+5 TO BS 500D UPPER SURFACE. R&R "Z" ANGLE IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 62,749 hrs · 36,701 cycles

RT CREASE BEAM CORRODED BETWEEN BS 927+10 TO BS 986.5+6. R&R CREASE BEAM PER SRM AND DWG.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 62,749 hrs · 36,701 cycles

RT THRESHOLD SUPPORT ANGLE ATTACHED TO CREASE BEAM CORRODED BETWEEN BS 294.5 TO BS 328, RBL 62. REMOVED ANGLE IAW AMM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 62,749 hrs · 36,701 cycles

L1 DOOR SLIDE ATTACH Z CORRODED AT BS 344, LBL 60. R&R ANGLE IAW SRM & DWG.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 62,749 hrs · 36,701 cycles

L1 DOOR CREASE BEAM CRACKED AT BS 294.5+8. R&R CREASE BEAM IAW DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 62,749 hrs · 36,701 cycles

RT CREASE BEAM CORRODED BETWEEN BS 294.5 TO BS 328+6, RBL 60. REPAIRED CREASE BEAM IAW SRM AND DWG.

Part: SKIN — CRACKED (LE SLAT) · airframe 62,749 hrs · 36,701 cycles

LT WING NR 3 SLAT LOWER SURFACE OF SLAT AT ACTUATOR ATTACH AREA CRACKED. R&R NR 3 SLAT IAW SRM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 62,302 hrs · 36,430 cycles

LT OVERWING EMERGENCY EXIT LIGHTING BATTERY PACK FAILED CAPACITY CHECK. R&R BATTERY PACK PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 62,302 hrs · 36,430 cycles

FORWARD LT EMERGENCY LIGHTING BATTERY PACK FAILED CAPACITY CHECK. R&R BATTERY PACK PER MM.

Part: PUMP — FAULTY (NR 2 ENGINE) · airframe 61,425 hrs · 35,844 cycles

AIR TURNBACK, NR 2 ENGINE WOULD NOT PRODUCE MORE THAN 86% N. REGARDLESS OF THRUST LEVER POSITION. R&R NR 2 ENGINE FUEL PUMP PER MT.

Part: HMU — MALFUNCTIONED (NR 2 ENGINE) · airframe 61,425 hrs · 35,844 cycles

AIR TURNBACK, NR 2 ENGINE WOULD NOT PRODUCE MORE THAN 86% N. REGARDLESS OF THRUST LEVER POSITION. R&R NR 2 HYDRO MECHANICAL UNIT PER MT.

Part: GLOWSTRIP — LOOSE (CABIN) · airframe 61,286 hrs · 35,759 cycles

RT PHOTOLUMINESCENT STRIP LOOSE AT ROW 1. SECURED STRIP PER MM.

Part: COVER — UNSECURE (EXIT SIGN) · airframe 61,201 hrs · 35,700 cycles

MID-CABIN OVERHEAD EXIT SIGN COVER FELL OFF. SECURED COVER PER SIP.

Part: COVER — UNSECURE (EXIT SIGN) · airframe 60,823 hrs · 35,451 cycles

OVERWING CEILING EMERGENCY EXIT SIGN COVER CAME OFF. SECURED COVER IAW SIP.

Part: ACTUATOR — LEAKING (NR 1 SPOILER) · airframe 60,458 hrs · 35,216 cycles

A SYSTEM ENGINE HYDRAULIC LOW PRESSURE LIGHT ILLUMINATED IN FLIGHT. DIVERTED AND DECLARED AN EMERGENCY. R & R THE NR 1 SPOILER ACTUATOR IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 58,595 hrs · 34,051 cycles

AFT SERVICE DOOR HEADER PANEL EMERGENCY EXIT LIGHT BULB INOP. R&R LIGHT PER AMM.

Part: BALLAST — FAILED (CABIN LIGHTS) · airframe 57,677 hrs · 33,526 cycles

DURING CRUISE FLIGHT AT FL380, RECEIVED AN INTERCOM CALL FROM FLIGHT ATTENDANTS ADVISING OF AN ELECTRICAL ODOR IN THE RT CABIN BETWEEN ROWS 5 & 6. EMERGENCY DECLARED AND RETURNED TO DEPARTURE. FOUND OVERHEAD CEILING LIGHT AT 2ABC INOPERATIVE, THE LIGHT BALLAST FAILED CAUSING THE SMOKE. R & R CEILING LIGHT ASSEMBLY IAW MM.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 57,385 hrs · 33,357 cycles

EMERGENCY LIGHT STRIP MISSING PROTECTIVE COVER AT 9 DEF. R & R THE EMERGENCY LIGHT STRIP IAW MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 56,752 hrs · 32,991 cycles

L1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW MT.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 56,335 hrs · 32,751 cycles

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

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 56,290 hrs · 32,725 cycles

EMERGENCY EXIT LIGHT POWER SUPPLY INOP AT LOCATION M1674. R&R BATTERY PACK PER AMM.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 56,290 hrs · 32,725 cycles

FLOOR TO SIDEWALL SUPPORT SHIELD CORRODED BETWEEN BS 767 TO BS 792, RBL 25. R&R SHIELD IAW SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 56,290 hrs · 32,725 cycles

LOWER BULKHEAD CHORD CRACKED AT BS 540, LT SIDE. REPAIRED CHORD PER EA.

Part: SKIN — CORRODED (FUSELAGE) · airframe 56,290 hrs · 32,725 cycles

FUSELAGE SKIN UNDER DORSAL FIN CORRODED. R&R SKIN PER ER & EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,290 hrs · 32,725 cycles

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

Part: WEB — CORRODED (FUSELAGE) · airframe 56,290 hrs · 32,725 cycles

RT OVERWING EMERGENCY EXIT CUTOUT LOWER SILL WEB CORRODED AT UPPER SURFACE. REPAIRED WEB PER SRM.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 56,290 hrs · 32,725 cycles

LT OVERWING EMERGENCY EXIT CUTOUT LOWER SILL WEB CORRODED AT UPPER SURFACE. REPAIRED WEB PER SRM.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 55,766 hrs · 32,396 cycles

R2 DOOR EMERGENCY EXIT SIGN COVER MISSING. INSTALLED COVER IAW AMM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 55,435 hrs · 32,200 cycles

R1 DOOR EMERGENCY EVAC SLIDE COVER OUT OF POSITION. REPOSITIONED SLIDE IAW MAINTENANCE.

Part: COVER — LOOSE (EXIT SIGN) · airframe 54,771 hrs · 31,824 cycles

RIGHT SIDE OVERWING EMER EXIT SIGN COVER LOOSE. SECURED COVER IAW EA.

Part: ACTUATOR — CRACKED (LE SLAT) · airframe 54,486 hrs · 31,650 cycles

RIGHT WING NR 6 LE SLAT ACTUATOR CRACKED. R & R ACTUATOR IAW AMM.

Part: SLIDE — LOOSE (R2 DOOR) · airframe 50,814 hrs · 29,540 cycles

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

Part: FLAP — CRACKED (RT WING) · airframe 50,567 hrs · 29,397 cycles

RIGHT WING INBD FLAP SECONDARY TORQUE TUBE AFT ATTACHMENT HOLE CRACKED. R & R FLAP IAW SRM & EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 50,394 hrs · 29,295 cycles

FLOORBEAM VERTICAL WEB AT CRACKED AT BS 727C, RBL 24.75 LOWER FASTENER HOLE. REPAIRED WEB IAW EA & SWA EA.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 50,394 hrs · 29,295 cycles

RIGHT HORIZONTAL STABILIZER RIB STATION 147.9 CRACKED FASTENER HOLE 32 INCHES FROM FWD SPAR INBD. REPAIRED RIB IAW EA.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 50,394 hrs · 29,295 cycles

RIGHT HORIZONTAL STABILIZER RIB STATION 147.9 CRACKED AT FASTENER HOLE 17.25 INCHES FROM FWD SPAR OTBD FLANGE. REPAIRED RIB IAW EA.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 50,394 hrs · 29,295 cycles

RIGHT HORIZONTAL STABILIZER STATION 92.7, RIB CRACKED IN VERTICAL STIFFENER 3RD FROM FRONT, 1 INCH UP FROM BOTTOM OF RIB. REPAIRED RIB IAW SRM.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 50,394 hrs · 29,295 cycles

RIGHT HORIZONTAL STABILIZER STATION 129.5, RIB CRACKED IN VERTICAL STIFFENER 1ST ONE FROM FRONT, 1 INCH UP FROM BOTTOM OF RIB. REPAIRED RIB IAW SRM.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 50,394 hrs · 29,295 cycles

RIGHT HORIZONTAL STABILIZER STATION 101.9, RIB CRACKED IN VERTICAL STIFFENER 1ST ONE FROM FRONT, 1 INCH UP FROM BOTTOM OF RIB. R & R RIB IAW SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 50,394 hrs · 29,295 cycles

FLOORBEAM CHORD CRACKED AT BS 727B, RBL 24.75. REPAIRED FLOORBEAM IAW EA.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 50,394 hrs · 29,295 cycles

RIGHT NR 3 WINDOW FRAME FASTENER HOLE, NR 2 FROM BOTTOM CRACKED. REPAIRED FRAME IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 50,394 hrs · 29,295 cycles

FORWARD SEAT TRACK INBD & OTBD FLANGE CRACKED AT BS 727B, LBL 24.75 FASTENER HOLES. REPAIRED FLANGE IAW EA & SWA EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 50,394 hrs · 29,295 cycles

FORWARD SEAT TRACK, INBD & OTBD FLANGE CRACKED AT BS 727B, RBL 45.5 FASTENER HOLES. REPAIRED TRACK IAW EA.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 50,394 hrs · 29,295 cycles

LEFT NR 3 WINDOW FRAME FASTENER HOLE, NR 3 FROM BOTTOM CRACKED. REPAIRED FRAME IAW ACO.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 50,394 hrs · 29,295 cycles

LEFT NR 3 WINDOW FRAME SECOND FROM BOTTOM FASTENER HOLE CRACKED. REPAIRED FRAME IAW ACO.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 50,394 hrs · 29,295 cycles

FORWARD SEAT TRACK, INBD & OTBD FLANGE CRACKED AT BS 727B, RBL 24.75 FASTENER HOLES. REPAIRED SEAT TRACK IAW EA.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 50,394 hrs · 29,295 cycles

RIGHT NR 1 WINDOW FRAME CRACKED. REPAIRED FRAME IAW ACO.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 50,394 hrs · 29,295 cycles

FORWARD SEAT TRACK, INBD & OTBD FLANGE CRACKED AT BS 727B, LBL 45.5 FASTENER HOLES. REPAIRED SEAT TRACK IAW EA.

Part: FLAP — DELAMINATED (RT WING) · airframe 50,394 hrs · 29,295 cycles

RIGHT WING OTBD AFT FLAP INBD CORNER DELAMINATED. REPAIRED AFT FLAP IAW SRM.

Part: LENS — UNSECURE (EXIT SIGN) · airframe 50,266 hrs · 29,226 cycles

OVERHEAD MID CABIN EXIT SIGN COVER FELL OFF. SECURED LENS COVER IAW MM.

Part: TIRE — FAILED (MLG) · airframe 49,484 hrs · 28,758 cycles

AIR TURN BACK DECLARED EMER TIRE FAILURE ON TAKEOFF. R & R NR 4 MAIN TIRE IAW MM.

Part: BATTERY — FAILED (CABIN) · airframe 47,943 hrs · 27,866 cycles

CEILING AFT ENTRY EMERGENCY LIGHTS BATTERIES FAILED CAPACITY TEST. R & R BATTERIES IAW TC & WDM.

Part: POST — CRACKED (FUSELAGE) · airframe 47,943 hrs · 27,866 cycles

CAPTAIN`S C & D WINDOW POST CRACKED. REPAIRED POST IAW EA.

Part: BATTERY — FAILED (CABIN) · airframe 47,943 hrs · 27,866 cycles

MID CABIN EMERGENCY LIGHT BATTERIES FAILED CAPACITY TEST. R & R BATTERIES IAW TC & WDM.

Part: COVER — BROKEN (CABIN) · airframe 47,002 hrs · 27,322 cycles

R1 DOOR EMERGENCY EXIT LIGHT COVER BROKEN. R & R LIGHT ASSEMBLY IAW SIP.

Part: BATTERY — FAILED (CABIN) · airframe 45,672 hrs · 26,506 cycles

RT EMERGENCY EXIT BATTERIES FAILED CAPACITY TEST. R&R BATTERIES IAW AMM.

Part: RETAINING CLIP — LOOSE (GIRT BAR) · airframe 45,672 hrs · 26,506 cycles

L1 DOOR EMERGENCY EVAC SLIDE COVER AFT GIRT BAR RETAINING CLIP LOOSE. SECURED CLIP IAW SRM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 45,508 hrs · 26,411 cycles

RT EMERGENCY EXIT INOPERATIVE. R&R CHARGER ASSEMBLY IAW AMM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 44,960 hrs · 26,085 cycles

R 2 DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT OF CONTAINER, DID NOT DEPLOY, STILL OPERATIONAL. REINSTALLED SLIDE IAW MT.

Part: SIGN — BROKEN (CABIN) · airframe 44,950 hrs · 26,078 cycles

R1 DOOR EMERGENCY EXIT SIGN BROKEN. R&R SIGN ASSEMBLY IAW AMM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 43,625 hrs · 25,284 cycles

FORWARD ENTRY ESCAPE SLIDE APPEARS TO BE HANGING LOWER THAN NORMAL. REMOVED SLIDE (L-1) REPOSITIONED SLIDE AND ADJUSTED GIRT LENGTHS AND REINSTALLED PER MT 725-61-06. CHECK'S OK.

Part: BATTERY PACK — FAILED (CABIN) · airframe 43,473 hrs · 25,187 cycles

FORWARD LEFT EMERGENCY EXIT LIGHT BATTERY PACK FAILED 15 MINUTES MINIMUM BLEED DOWN TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 43,473 hrs · 25,186 cycles

AFT CARGO, STA 727 RBL 6, APU "LOWER" DUCT PANEL SUPPORT HAS CRACKED CLIP. REMOVED AND REPLACED CLIP IAW SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 43,473 hrs · 25,186 cycles

AFT CARGO, STA 860 LBL 12, CLIP CRACKED BELOW THE FWD INBOARD LAV TANK COMPARTMENT POST. REMOVED AND REPLACED CLIP IAW SRM.

Part: BEAM — CRACKED (LT WING) · airframe 43,473 hrs · 25,186 cycles

LEFT WING, O/B FLAP WELL, I/B CLOSEOUT PANEL ATTACH BEAM IS CRACKED AT THE I/B SIDE. REMOVED AND REPLACED BEAM PER SRM.

Part: INTERCOSTAL — TORN (FUSELAGE) · airframe 43,473 hrs · 25,186 cycles

INTERCOSTAL BETWEEN THE NR 1 AND NR 2 SEAT TRACK UPPER WEB TORN OFF STA 500D+17. RE-INSTALLED WEB PER SRM.

Part: INTERCOSTAL — DAMAGED (FUSELAGE) · airframe 43,473 hrs · 25,186 cycles

INTERCOSTAL WEB DAMAGED STA 500D+17 BL 0 TO LBL 24. REMOVED AND REPLACED INTERCOSTAL PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,473 hrs · 25,186 cycles

FUSELAGE FRAME HAS CRACK INDICATION (HFEC) AT STA 440, STR 8R (I/B HOLE, AFT SIDE OF FRAME). REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,473 hrs · 25,186 cycles

FUSELAGE FRAME HAS CRACK INDICATION (HFEC) AT STA 480, STR 8R (I/B HOLE, AFT SIDE OF FRAME. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,473 hrs · 25,186 cycles

FUSELAGE FRAME HAS CRACK INDICATION (HFEC) AT STA 747, SR 8L (I/B HOLE, AFT SIDE OF FRAME). REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,473 hrs · 25,186 cycles

FUSELAGE FRAME HAS CRACK INDICATION (HFEC) AT STA 360, STR 8R (I/B HOLE, AFT SIDE OF FRAME). REPAIRED PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,473 hrs · 25,186 cycles

FUSELAGE FRAME HAS CRACK INDICATION (HFEC) AT STA 400, STR 8R (I/B HOLE, AFT SIDE OF FRAME. REPAIRED FRAME PER EA.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 43,473 hrs · 25,186 cycles

FWD GALLEY, LBL 46 STA 312-328 INTERCOSTAL IS CRACKED. REMOVED AND REPLACED INTERCOSTAL PER SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 43,473 hrs · 25,186 cycles

FORWARD CARGO, RIGHT TRANSITION ANGLE HAS SURFACE CORROSION FROM STA 489 TO STA 494. REMOVED AND REPLACED ANGLE IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 43,473 hrs · 25,186 cycles

FORWARD GALLEY, LBL 46 STA 328-344 INTERCOSTAL IS CRACKED. REMOVED AND REPLACED INTERCOSTAL PER SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 43,473 hrs · 25,186 cycles

FORWARD GALLEY, RBL 30" STA 312-328 INTERCOSTAL IS CRACKED. REMOVED AND REPLACED INTERCOSTAL PER SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 43,473 hrs · 25,186 cycles

AFT CARGO LEFT Z-ANGLE STA 727D-747 HAS CORROSION. INSTALLED RIGHT Z-ANGLE PER SRM.

Part: ANGLE — CRACKED (LT WING) · airframe 43,473 hrs · 25,186 cycles

LEFT WING UPPER SURFACE, ANGLE CRACKED UNDER PANEL 551AT AT THE FORWARD INBOARD CORNER. REPLACED ANGLE PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 43,473 hrs · 25,186 cycles

STA 986 LBL 43 FLOORBEAM HAS CORROSION AT FLOORBOARD HOLE. REMOVED AND REPLACED T-CAP PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 43,473 hrs · 25,186 cycles

AFT CARGO FLOORBEAM RBL 13 STA 787-792 HAS CORROSION. REMOVED AND REPLACED BEAM PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 43,473 hrs · 25,186 cycles

AFT CARGO FLOORBEAM RBL 13 STA 807-847 HAS CORROSION. REMOVED AND REPLACED BEAM PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 43,473 hrs · 25,186 cycles

AFT CARGO FLOORBEAM RBL 13.8 IS CRACKED AT STA 767. REMOVED AND REPLACED BEAM PER SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 43,473 hrs · 25,186 cycles

AFT CARGO RIGHT Z-ANGLE STA 727D-747 HAS CORROSION. INSTALLED RIGHT Z-ANGLE PER SRM.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 43,473 hrs · 25,186 cycles

HFEC INDICATES CRACKED SKIN AT STAB STA 184.70, LOWER STAB SKIN, LEFT SIDE, CRACK MEASURES .300. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 43,473 hrs · 25,186 cycles

HFEC INDICATES CRACKED SKIN AT STAB STA 101.9, LOWER STAB SKIN, RIGHT SIDE, CRACK MEASURES .800. REPAIRED SKIN PER SRM.

Part: LENS — LOOSE (CABIN) · airframe 43,110 hrs · 24,958 cycles

EMERGENCY ESCAPE PATCH LIGHT RED LENS AT OVERWING EXIT IS LOOSE. REMOVED AND REPLACED RED EMERGENCY FLOOR LIGHT LENS PER AMM.

Part: LIGHT — LOOSE (CABIN) · airframe 42,591 hrs · 24,646 cycles

LEFT EMERGENCY EXIT LIGHT LOOSE AT ROW 1. REMOVED AND REPLACED EEPLS PER MM.

Part: LENS — BROKEN (CABIN) · airframe 41,094 hrs · 23,727 cycles

FLOOR EMERGENCY LENS BROKEN AT 1 ABC. REPLACED LENS PER MM.

Part: LENS — MISSING (CABIN) · airframe 40,800 hrs · 23,568 cycles

EMERGENCY FLOOR TRACK LIGHT LENS MISSING ROW 11. REPLACED LENS PER MM.

Part: BEARING — DEFECTIVE (AILERON) · airframe 40,723 hrs · 23,526 cycles

AIR TURNBACK - SLIGHT BINDING IN ROLL AXIS OF FLIGHT CONTROLS WITH FLAP AT POSITION 1. REMOVED AND REPLACED AILERON CENTERING CAM BEARING PER AMM.

Part: LENS — MISSING (CABIN) · airframe 40,318 hrs · 23,291 cycles

EMERGENCY TRACK LIGHTING LENS MISSING AT SEAT ROW 1ABC. INSTALLED BULB PER MM.

Part: ACTUATOR — CRACKED (LT MLG) · airframe 39,225 hrs · 22,624 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT MAIN LANDING GEAR ACTUATOR CRACKED. REMOVED AND REPLACED LT MLG ACTUATOR PER MM.

Part: COVER — CRACKED (CABIN) · airframe 39,160 hrs · 22,586 cycles

DURING SCHEDULED HC1 CHECK, FOUND LT EEPLS COVER CRACKED AT ROW 7. REMOVED AND REPLACED COVER PER MM.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 43,486 hrs · 25,195 cycles

STANDBY HYD. BAY, I/B AFT WING-TO-BODY VERTICAL FAIRING SUPPORT IS CRACKED. REMOVED AND REPLACED STANDBY HYD BAY, I/B AFT WING-TO-BODY VERTICAL FAIRING SUPPORT IAW BOEING DWG 149A7502 AND BOEING DWG 149A7590.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 43,486 hrs · 25,195 cycles

STANDBY HYD BAY, I/B AFT WING-TO-BODY VERTICAL FAIRING SUPPORT IS CRACKED. REPAIRED PER EA 1-753-17131.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 38,952 hrs · 22,470 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT HORIZONTAL STABILIZER LOWER IN-SPAR SKIN CRACKED AT STA 101.9. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 38,952 hrs · 22,470 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT HORIZONTAL STABILIZER LOWER IN-SPAR SKIN CRACKED AT STA 157.10. REPAIRED SKIN PER SRM.

Part: LIGHT — BROKEN (CABIN) · airframe 38,295 hrs · 22,077 cycles

LT EEPLS BROKEN AT ROW 1. REMOVED AND REPLACED EEPLS PER MM.

Part: LENS — BROKEN (CABIN) · airframe 37,334 hrs · 21,520 cycles

LT EEPLS LENS BROKEN AT ROW 18. REPAIRED LENS PER MM.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 36,695 hrs · 21,141 cycles

DURING SCHEDULED 10Y CHECK, FOUND FLIGHT DECK FLOOR CENTER CHANNEL CORRODED BETWEEN BS 259 TO BS 270. REPAIRED CHANNEL PER SRM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 36,695 hrs · 21,141 cycles

DURING SCHEDULED 10Y CHECK, FOUND LT WING O/B AFT FLAP I/B TRAILING EDGE OUTER SKIN DELAMINATED. REPAIRED AFT FLAP PER SRM.

Part: SEAT TRACK — WORN (COCKPIT) · airframe 36,695 hrs · 21,141 cycles

DURING SCHEDULED 10Y CHECK, FOUND FLIGHT DECK RT SEAT TRACK WORN. REMOVED AND REPLACED SEAT TRACK PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 36,695 hrs · 21,141 cycles

DURING SCHEDULED 10Y CHECK, FOUND EEPLS INOP. REMOVED AND REPLACED BULBS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 36,241 hrs · 20,888 cycles

DURING SCHEDULED MV1 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.

Part: FITTING — CORRODED (RT MLG TRUNNION) · airframe 35,544 hrs · 20,458 cycles

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

Part: FITTING — CORRODED (LT MLG TRUNNION) · airframe 35,544 hrs · 20,458 cycles

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

Part: FAN — FAULTY (AC BAY) · airframe 35,434 hrs · 20,393 cycles

AT CRUISE ALT WITH RECIR FAN ON, BURNT RUBBER SMELL. RECIR FAN OFF- SMELL OFF. REMOVED AND REPLACED RECIR FAN & FILTER PER TASK.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 34,864 hrs · 20,043 cycles

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

Part: LENS — LOOSE (EXTERIOR) · airframe 34,864 hrs · 20,043 cycles

DURING SCHEDULED SPV CHECK, FOUND LT OVERWING EXTERIOR EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM.

Part: BATTERY — FAILED (CABIN) · airframe 34,587 hrs · 19,887 cycles

DURING SCHEDULED HC1 CHECK, EMERGENCY EXIT LIGHTS FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERIES PER MM.

Part: COVER — CRACKED (CABIN) · airframe 34,587 hrs · 19,887 cycles

DURING SCHEDULED HC1 CHECK, FOUND LT EEPLS COVER CRACKED BETWEEN ROW 1 TO ROW 22. REMOVED AND REPLACED COVER PER MM.

Part: LENS — MISSING (CABIN) · airframe 34,587 hrs · 19,887 cycles

DURING SCHEDULED HC1 CHECK, FOUND LT EEPLS LENS MISSING AT ROW 23. REMOVED AND REPLACED LENS PER MM.

Part: CAP — MISSING (CABIN) · airframe 32,462 hrs · 18,602 cycles

FWD EEPLS END CAP MISSING. INSTALLED END CAP PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,308 hrs · 18,501 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT AFT EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.

Part: COVER — MISSING (CABIN) · airframe 32,030 hrs · 18,328 cycles

FWD EEPLS COVER MISSING AT ROW 1. INSTALLED COVER PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,205 hrs · 17,241 cycles

DURING SCHEDULED MV2 CHECK, FOUND EEPLS LIGHT INOP BETWEEN ROW 11 TO ROW 15. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: COVER — DAMAGED (CABIN) · airframe 30,031 hrs · 17,142 cycles

DURING SCHEDULED 8Y CHECK, FOUND EEPLS TRACK COVERS DAMAGED. REMOVED AND REPLACED COVERS PER MM.

Part: TRACK — DAMAGED (CABIN) · airframe 30,031 hrs · 17,142 cycles

DURING SCHEDULED 8Y CHECK, FOUND EEPLS TRACK DAMAGED AT AFT GALLEY AREA. REMOVED AND REPLACED EEPLS PER MM.

Part: TRACK — DAMAGED (CABIN) · airframe 30,031 hrs · 17,142 cycles

DURING SCHEDULED 8Y CHECK, FOUND EEPLS TRACK DAMAGED AT FWD GALLEY AREA. REMOVED AND REPLACED EEPLS PER MM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 30,030 hrs · 17,141 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986, RBL 41. REPAIRED BEAM PER SRM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 29,116 hrs · 16,574 cycles

FOUND R2 DOOR EMERGENCY EXIT SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 29,116 hrs · 16,574 cycles

FOUND R2 DOOR EMERGENCY EXIT SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 28,354 hrs · 16,115 cycles

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

Part: SKIN — CRACKED (HORIZ STAB) · airframe 27,733 hrs · 15,729 cycles

DURING SCHEDULED HC2 CHECK, FOUND LEFT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 133. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 27,733 hrs · 15,729 cycles

DURING SCHEDULED HC2 CHECK, FOUND RIGHT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 133. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 27,733 hrs · 15,729 cycles

DURING SCHEDULED HC2 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 27,733 hrs · 15,729 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,733 hrs · 15,729 cycles

EEPLS INOP AT ROW 1 ABC. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: LENS — LOOSE (EMERGENCY LIGHTS) · airframe 27,393 hrs · 15,525 cycles

EEPLS LENS LOOSE AT ROW 1 ABC. SECURED LENS PER MM.

Part: CAP — MISSING (CABIN) · airframe 27,330 hrs · 15,483 cycles

EEPLS END CAP MISSING AT ROW 1 ABC. INSTALLED END CAP PER MM.

Part: LENS — CRACKED (CABIN) · airframe 27,197 hrs · 15,405 cycles

EEPLS LENS CRACKED AT ROW 1 ABC. REMOVED AND REPLACED LENS PER MM.

Part: LENS — CRACKED (CABIN) · airframe 26,596 hrs · 15,043 cycles

EEPLS LENS CRACKED AT ROW 1 ABC. REMOVED AND REPLACED LENS PER MM.

Part: LENS — CRACKED (FUSELAGE) · airframe 26,554 hrs · 15,017 cycles

EEPLS LENS CRACKED AT ROW 1 ABC. REMOVED AND REPLACED LENS PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 25,802 hrs · 14,564 cycles

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

Part: COVER — CRACKED (CABIN) · airframe 24,490 hrs · 13,774 cycles

EEPLS COVER CRACKED AT ROW 3 ABC. REMOVED AND REPLACED COVER PER MM.

Part: SLIDE — LOW PRESSURE (L2 DOOR) · airframe 23,897 hrs · 13,445 cycles

L2 DOOR EMERGENCY EVAC SLIDE PRESSURE GAUGE INDICATED OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 23,215 hrs · 13,036 cycles

DURING SCHEDULED MV2 CHECK, FOUND EEPLS INOP AT ROW 1 ABC. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: FRAME — CRACKED (BS 330 S6R) · airframe 22,612 hrs · 12,675 cycles

DURING SCHEDULED 6Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 330, STR 6R. REPAIRED FRAME SECTION PER SRM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 22,224 hrs · 12,466 cycles

L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: COVER — CRACKED (EMERGENCY LIGHT) · airframe 21,855 hrs · 12,259 cycles

DURING SCHEDULED MV3 CHECK, FOUND EEPLS COVER CRACKED AT ROW 12. REMOVED AND REPLACED EEPLS COVER PER MM.

Part: COVER — LOOSE (EMERGENCY LIGHT) · airframe 21,289 hrs · 11,961 cycles

EEPLS COVER LOOSE AT ROW 1 ABC. SECURED LIGHT COVER PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 20,551 hrs · 11,523 cycles

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

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 20,389 hrs · 11,443 cycles

EEPLS LIGHT COVER MISSING AT ROW 1 ABC. INSTALLED EEPLS COVER PER MM.

Part: COVER — LOOSE (EMERGENCY LIGHT) · airframe 20,336 hrs · 11,411 cycles

EEPLS LIGHT COVER LOOSE AT ROW 1 ABC. SECURED EEPLS COVER PER MM.

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS) · airframe 19,992 hrs · 11,213 cycles

FOUND MID CABIN EEPLS LIGHTS INOP. REMOVED AND REPLACED BULBS PER MM.

Part: SLIDE — OUT OF LIMITS (R2 DOOR) · airframe 19,442 hrs · 10,915 cycles

DURING SCHEDULED MV2 CHECK, R2 DOOR EMERGENCY EVAC SLIDE PRESSURE INDICATES OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM.

Part: SLIDE — LOOSE (L1 DOOR) · airframe 19,157 hrs · 10,733 cycles

L1 DOOR EVACUATION SLIDE DISLODGED FROM COVER. REINSTALLED SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 16,706 hrs · 9,380 cycles

DURING SCHEDULED MV2 CHECK, FOUND R2 DOOR EVACUATION SLIDE OUT OF ADJUST. ADJUSTED SLIDE ASSY PER MM.

Part: HOOK — LOOSE (L1 GIRT BAR) · airframe 16,224 hrs · 9,092 cycles

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

Part: HOOK — OUT OF ADJUST (R2 DOOR SLIDE) · airframe 15,963 hrs · 8,956 cycles

R2 DOOR EMERGENCY EVAC SLIDE GIRT BAR STOW HOOKS OUT OF ADJUST. ADJUSTED HOOKS PER MM.

Part: SLIDE — DISLODGED (R2 DOOR) · airframe 15,431 hrs · 8,660 cycles

R2 DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. SLIDE DID NOT DEPLOY. REINSTALLED SLIDE PER MM.

Part: COVER — LOOSE (EMERGENCY LIGHT) · airframe 14,792 hrs · 8,276 cycles

EEPLS COVER AT ROW 5 ABC, LOOSE. SECURED COVER PER MM.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 14,744 hrs · 8,254 cycles

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

Part: MODULE — FAULTY (B-HYD SYSTEM) · airframe 14,103 hrs · 7,885 cycles

AIR TURNBACK, FLAPS WOULD NOT RETRACT ABOVE POSITION 1. REMOVED AND REPLACED NR 2 HYDRAULIC B-SYSTEM MODULE PER MM. REMOVED AND REPLACED RIGHT W/W MAIN HYDRAULIC FILTER AND CASE DRAIN FILTERS PER MM.

Part: SLIDE — LOOSE (R1 DOOR) · airframe 13,017 hrs · 7,288 cycles

DURING SCHEDULED HC2 CHECK, FOUND R1 DOOR EVAC SLIDE LOOSE. SECURED R1 DOOR EVAC SLIDE PER MM.

Part: COVER — CRACKED (EMERGENCY LIGHT) · airframe 13,017 hrs · 7,288 cycles

DURING SCHEDULED HC2 CHECK, FOUND EEPLS LIGHT COVERS CRACKED THROUGHOUT CABIN. REMOVED AND REPLACED EEPLS STRIP COVERS PER MM.

Part: COVER — LOOSE (EMERGENCY LIGHT) · airframe 12,875 hrs · 7,200 cycles

FWD EEPLS COVER LOOSE, WIRE DISCONNECTED. SECURED COVER AND RECONNECTED WIRE PER MM.

Part: SLIDE — OUT OF ADJUST (CABIN SVC DOORS) · airframe 9,555 hrs · 5,351 cycles

DURING SCHEDULED C4 CHECK, FOUND BOTH RT CABIN SVC DOOR EMERGENCY EVAC SLIDES OUT OF ADJUST. ADJUSTED SLIDES PER MM.

Part: SLIDE — DEPLOYED (FWD ENTRY DOOR) · airframe 6,858 hrs · 3,862 cycles

FWD ENTRY DOOR EMERGENCY EVAC SLIDE DEPLOYED WHEN OPENING DOOR. REMOVED AND REPLACED SLIDE PER MM.

Part: SLIDE — UNSERVICEABLE (ENTRY DOOR) · airframe 5,241 hrs · 2,980 cycles

FWD ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM.

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 4,914 hrs · 2,808 cycles

FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT BAR NOT ALIGNED WITH RETAINER BRACKETS. REMOVED AND REPLACED SLIDE PER MM.

Part: SLIDE — UNSERVICEABLE (L1 DOOR) · airframe 4,814 hrs · 2,762 cycles

FWD ENTRY DOOR EVACUATION SLIDE PRESS INDICATOR OUT OF LIMITS. REMOVED AND REPLACED SLIDE ASSY PER MM.

Part: SLIDE — LOOSE (FWD ENTRY DOOR) · airframe 3,927 hrs · 2,258 cycles

FWD ENTRY DOOR EMERGENCY EVAC SLIDE LOOSE. SECURED SLIDE PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 2,427 hrs · 1,422 cycles

FOUND FWD EEPLS FLOOR TRACK LIGHTS INOP. RELAMPED PER MM.