N779SW

Part: LIGHT — INOPERATIVE (CABIN) · airframe 67,129 hrs · 39,569 cycles

L/H AFT GALLEY FLOOR TRACK PHOTO LUMINESCENT LIGHTS INOP LAST FOOT. / R&R PHOTO LUMINESCENT LIGHT AMM.

Part: PLATE — CRACKED (RT WING) · airframe 65,150 hrs · 38,294 cycles

RT WING WIGGLE PLATE AFT OF ENGINE PYLON CRACKED. R&R WIGGLE PLATE PEER SRM.

Part: FLAP — DELAMINATED (LT WING) · airframe 64,961 hrs · 38,163 cycles

LT OUTBOARD TRAILING EDGE AFT FLAP DELAMINATED ON LOWER INBOARD CORNER. REPAIRED AFT FLAP PER AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,518 hrs · 37,875 cycles

FUSELAGE SKIN CRACKED AT STA 106, STR 23L. REPAIRED SKIN PER SWA EA.

Part: FITTING — CRACKED (R1 DOOR) · airframe 63,414 hrs · 37,141 cycles

R1 DOOR FORWARD GIRT BAR STOWAGE CLIP ATTACHMENT CRACKED. REPAIRED CLIP PER EA.

Part: FUSE — INOPERATIVE (CABIN) · airframe 63,405 hrs · 37,134 cycles

L1 DOOR EMERGENCY EXIT LIGHT ON LOWER AFT LAV WALL INOP. R&R POWER SUPPLY FUSE PER AMM.

Part: FUSE — INOPERATIVE (CABIN) · airframe 63,405 hrs · 37,134 cycles

R1 DOOR HEADER PANEL EXIT LIGHT INOP. R&R POWER SUPPLY FUSE PER AMM.

Part: LENS — MISSING (CABIN) · airframe 63,405 hrs · 37,134 cycles

LT EMERGENCY LIGHT LENS MISSING ON OVERHEAD BIN AT ROW 9. INSTALLED LENS IAW MM.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 63,405 hrs · 37,134 cycles

GUSSET CRACKED AT BS 500D, STR 19R. R&R GUSSET IAW SRM AND DWG.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 63,405 hrs · 37,134 cycles

AFT CARGO FLOOR INTERCOSTAL CORRODED BETWEEN BS 847 TO BS 856, RBL 24. R&R INTERCOSTAL PER SRM AND DWG.

Part: SUPPORT FRAME — CHAFED (FAIRING) · airframe 63,405 hrs · 37,134 cycles

L1 DOOR FAIRING FORMER FRAME CHAFED BETWEEN BS 653 TO BS 674, LBL 27. R&R FRAME IAW SRM & DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 63,405 hrs · 37,134 cycles

FORWARD CARGO BAY ON FLOOR TO SIDEWALL SUPPORT CORRODED AT BS 416, RBL 24. R&R SUPPORT PER SRM AND DWG.

Part: ATTACH ANGLE — CRACKED (RT MLG WW) · airframe 63,405 hrs · 37,134 cycles

REAR SPAR VAPOR BARRIER ATTACH ANGLE CRACKED AT BS 663, RBL 8. REPAIRED ANGLE PER EA.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 63,405 hrs · 37,134 cycles

FORWARD CARGO BAY ON FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 400 TO BS 500D, LBL 24. R&R SUPPORT IAW SRM AMM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 63,405 hrs · 37,134 cycles

FORWARD CARGO BAY ON AFT BULKHEAD CENTER PANEL LOWER SUPPORT CORRODED AT BS 500D, BETWEEN LBL 24 TO RBL 24. R&R SUPPORT IAW SRM AND DWG.

Part: BEAM — CRACKED (R1 DOOR) · airframe 63,405 hrs · 37,134 cycles

R1 DOOR NR 4 BEAM CRACKED. R&R R1 DOOR IAW AMM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 63,405 hrs · 37,134 cycles

L1 DOOR MOPSILL ATTACHED ANGLE CORRODED BETWEEN BS 303 TO BS 348, LBL 61. R&R ANGLE IAW SRM AND DWG.

Part: STIFFENER — CRACKED (RT MLG WW) · airframe 63,405 hrs · 37,134 cycles

VAPOR BARRIER STIFFENER CRACKED AT BS 663, BETWEEN RBL 6 TO RBL 31. R&R STIFFENER IAW DWG AND SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 63,405 hrs · 37,134 cycles

FORWARD CABIN FLOORBEAM CORRODED AT BS 328, BETWEEN RBL 20 TO RBL 56. R&R TEE CAP PER SRM & EA.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 63,405 hrs · 37,134 cycles

FORWARD CARGO BAY SIDEWALL SUPPORT SHIELD CORRODED BETWEEN BS 500 TO BS 500A, RBL 21. R&R SHIELD PER SRM AND DWG.

Part: STRAP — CORRODED (FUSELAGE) · airframe 63,405 hrs · 37,134 cycles

AFT CARGO BAY CUTOUT SURROUND STRUCTURE STRAP CORRODED AT BS 789+14, RBL 21. R&R STRAP IAW SRM AND DWG.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 63,405 hrs · 37,134 cycles

AFT CARGO BAY CUTOUT SURROUND STRUCTURE SUB WEB THRESHOLD. R&R WEB PER SRM AND DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,405 hrs · 37,134 cycles

INTERCOSTAL CRACKED BETWEEN BS 312 TO BS 328, LBL 46. R&R INTERCOSTAL IAW SRM AND DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 63,405 hrs · 37,134 cycles

AFT CARGO BAY FLOORBEAM CORRODED AT BS 727D+5, RBL 7.5. REPAIRED FLOORBEAM IAW EA.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,405 hrs · 37,134 cycles

INTERCOSTAL CRACKED BETWEEN BS 277 TO BS 294, RBL 2. R&R INTERCOSTAL IAW SRM AND DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 63,405 hrs · 37,134 cycles

BULKHEAD ANGLE ASSEMBLY CORRODED AT BS 947.5, BETWEEN LBL 9 TO RBL 21. R&R ANGLE IAW SRM AND DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 63,405 hrs · 37,134 cycles

AFT CARGO BAY FLOORBEAM CORRODED AT BS 772, LBL 2.5. REPAIRED FLOORBEAM IAW EA.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,405 hrs · 37,134 cycles

INTERCOSTAL CRACKED BETWEEN BS 328 TO BS 344, LBL 46. R&R INTERCOSTAL IAW SRM AND DWG.

Part: WEB — CORRODED (FUSELAGE) · airframe 63,405 hrs · 37,134 cycles

AFT CARGO BAY DOOR CUTOUT LOWER SILL VERTICAL WEB CORRODED BETWEEN BS 795 TO BS 846, RBL 19.5. R&R WEB PER SRM & DWG.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 63,405 hrs · 37,134 cycles

AFT CARGO BAY FLOOR TRACK ASSEMBLY CORRODED BETWEEN BS 727 TO BS 867, LBL 17. R&R TRACK ASSEMBLY IAW SRM AND DWG.

Part: PLATE — CORRODED (FUSELAGE) · airframe 63,405 hrs · 37,134 cycles

AFT CARGO BAY SIDE PLATE ASSEMBLY CORRODED BETWEEN BS 727 TO BS 847, LBL 22. R&R SIDE PLATE ASSEMBLY IAW SRM AND DWG.

Part: PLATE — CORRODED (FUSELAGE) · airframe 63,405 hrs · 37,134 cycles

AFT CARGO BAY SIDE PLATE ASSEMBLY CORRODED BETWEEN BS 867 TO BS 947, RBL 20. R&R SIDE PLATE ASSEMBLY IAW SRM AND DWG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 63,405 hrs · 37,134 cycles

AFT CARGO BAY FLOOR TRACK ASSEMBLY CORRODED BETWEEN BS 925 TO BS 935, LBL 2.5. R&R FLOOR TRACK ASSEMBLY IAW DWG & SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 63,405 hrs · 37,134 cycles

AFT CARGO BAY FLOORBEAM ASSEMBLY CORRODED AT BS 927, RBL 7.5. R&R FLOORBEAM ASSEMBLY IAW DWG & SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 63,405 hrs · 37,134 cycles

AFT CARGO BAY WASTE COMP SURROUND STRUCTURE CLIP CRACKED AT BS 865, LBL 10. R&R CLIP IAW SRM AND DWG.

Part: STRAP — CORRODED (FUSELAGE) · airframe 63,405 hrs · 37,134 cycles

AFT CARGO BAY STRAP ASSEMBLY CORRODED BETWEEN BS 794.5 TO BS 800, RBL 19.5. R&R STRAP IAW SRM AND DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 63,405 hrs · 37,134 cycles

BULKHEAD ANGLE ASSEMBLY CORRODED AT BS 947.5, BETWEEN STR 21R TO STR 25R. R&R SUPPORT IAW SRM AND DWG.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 63,405 hrs · 37,134 cycles

AFT CARGO BAY SIDEWALL SUPPORT SHIELD CORRODED AT BS 847+10, RBL 21. R&R SHIELD IAW SRM AND DWG.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 63,405 hrs · 37,134 cycles

L2 DOOR MOPSILL CORRODED BETWEEN BS 941.5 TO BS 986.5. R&R MOPSILL IAW SRM AND DWG.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 63,405 hrs · 37,134 cycles

FORWARD CARGO BAY DOOR CUTOUT SURROUND STRUCTURE SUB WEB THRESHOLD CORRODED. R&R WEB IAW SRM AND DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 63,405 hrs · 37,134 cycles

AFT CARGO BAY FLOORBEAM CORRODED AT BS 772, LBL 7.5. REPAIRED FLOORBEAM IAW EA.

Part: PLATE — CORRODED (FUSELAGE) · airframe 63,405 hrs · 37,134 cycles

AFT CARGO BAY SIDE PLATE ASSEMBLY CORRODED BETWEEN BS 727 TO BS 767, RBL 22. R&R SIDE PLATE ASSEMBLY IAW SRM AND DWG.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 63,405 hrs · 37,134 cycles

FORWARD CARGO BAY SIDEWALL SUPPORT SHIELD CORRODED BETWEEN BS 420 TO BS 440, RBL 21. R&R SHIELD PER SRM AND DWG.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 63,405 hrs · 37,134 cycles

AFT CARGO BAY SIDEWALL SHIELD CORRODED AT BS 787, RBL 21. R&R SHIELD IAW DWG & SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 63,405 hrs · 37,134 cycles

AFT CARGO BAY SURROUND STRUCTURE WEB CORRODED AT BS 787+3, RBL 21. R&R WEB IAW SRM & DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 63,405 hrs · 37,134 cycles

FORWARD CABIN FLOOR SUPPORT CORRODED AT BS 326 -2, RBL 10. R&R SUPPORT PER SRM AND DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 63,405 hrs · 37,134 cycles

AFT CARGO BAY FLOORBEAM CORRODED AT BS 772, RBL 2.5. REPAIRED FLOORBEAM IAW EA.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 63,405 hrs · 37,134 cycles

AFT CARGO BAY INTERCOSTAL CORRODED BETWEEN BS 767 TO BS 787, RBL 6. R&R INTERCOSTAL PER SRM & DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 63,405 hrs · 37,134 cycles

AFT WET AREA FLOOR BEAM UPPER T-CHORD CORRODED AT BS 986.5, BETWEEN LBL 6 TO RBL 52. R&R TEE CAP PER SRM AND EA.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 63,405 hrs · 37,134 cycles

R1 DOOR MOPSILL CORRODED BETWEEN BS 291 TO BS 332, RBL 60. R&R MOPSILL IAW SRM AND DWG.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 63,405 hrs · 37,134 cycles

R2 DOOR MOPSILL CORRODED BETWEEN BS 927 TO BS 986+9, WL 208. R&R MOPSILL IAW SRM AND DWG.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 63,405 hrs · 37,134 cycles

L1 DOOR MOPSILL CORRODED BETWEEN BS 303 TO BS 348, LBL 60. R&R MOPSILL IAW SRM AND DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 63,405 hrs · 37,134 cycles

R2 DOOR MOPSILL SPLICE ANGLE CORRODED BETWEEN BS 1006 TO BS 1008, RBL 41. R&R ANGLE IAW SRM AND DWG.

Part: STIFFENER — CRACKED (LT MLG WW) · airframe 63,405 hrs · 37,134 cycles

FORWARD SIDE OF BULKHEAD VAPOR BARRIER WEB STIFFENER CRACKED AT BS 663, BETWEEN LBL 6 TO LBL 31. R&R STIFFENER IAW SRM AND DWG.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 63,405 hrs · 37,134 cycles

R1 DOOR CHORD ATTACH TO MOPSILL CORRODED BETWEEN BS 300 TO BS 320, RBL 60. R&R CHORD IAW SRM AND DWG.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 63,405 hrs · 37,134 cycles

L1 DOOR ZEE CHORD CORRODED BETWEEN BS 315 TO BS 340, LBL 63. R&R ZEE CHORD IAW SRM & DWG.

Part: BULKHEAD — CRACKED (LT MLG WW) · airframe 63,405 hrs · 37,134 cycles

LT WHEEL WELL VAPOR BARRIER LOWER WEB CRACKED FROM LOWER EDGE AT BS 663, LBL 12. REPAIRED WEB IAW SRM.

Part: PRESSURE DECK — CRACKED (FUSELAGE) · airframe 63,405 hrs · 37,134 cycles

HORIZONTAL PRESSURE DECK CRACKED BETWEEN BS 673 TO BS 664, BETWEEN RBL 40 TO RBL 41. REPAIRED WEB IAW EA.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 63,064 hrs · 36,914 cycles

R1 DOOR EMERGENCY LIGHTS INOP. R&R BATTERY PACK ASSEMBLY IAW MM.

Part: KEELBEAM — CRACKED (R/H WHEEL WELL) · airframe 62,363 hrs · 36,474 cycles

RIGHT WHEEL WELL KEEL BEAM CRACKED FORWARD LOWER WALL. REPAIRED THE KEEL BEAM PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 61,958 hrs · 36,215 cycles

RT OFF-WING HATCH EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER AMM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 61,896 hrs · 36,173 cycles

R1 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMPS IAW MM.

Part: SLIDE — BROKEN (R2 DOOR) · airframe 61,767 hrs · 36,087 cycles

R2 DOOR EMERGENCY EVAC SLIDE LATCH BROKEN. R&R SLIDE PER MT.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 61,767 hrs · 36,087 cycles

L2 DOOR SLIDE OUT OF POSITION. REPOSITIONED THE SLIDE IAW MT.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 61,581 hrs · 35,970 cycles

RIGHT WING OUTBOARD AFT FLAP DELAMINATED ON THE INBOARD LOWER SURFACE. R & R THE AFT FLAP IAW MM.

Part: SLIDING WINDOW — ARCED (L2) · airframe 61,542 hrs · 35,947 cycles

CAPTAIN'S SLIDING WINDOW ARCED INFLIGHT. R & R THE L2 WINDOW ASSEMBLY IAW MT.

Part: SKIN — CRACKED (LE SLAT) · airframe 61,233 hrs · 35,731 cycles

RT WING NR 6 SLAT LOWER SKIN CRACKED. REPAIRED SKIN IAW EA.

Part: LENS — LOOSE (EXIT SIGN) · airframe 60,494 hrs · 35,249 cycles

OVERWING CENTER AISLE AFT EXIT SIGN LENS LOOSE. SECURED SIGN IAW AMM.

Part: FLAP — DELAMINATED (TE FLAP) · airframe 59,810 hrs · 34,848 cycles

LT WING INBOARD MID-FLAP DELAMINATED ON OUTBOARD TRAILING EDGE. R&R MID FLAP IAW AMM.

Part: SIGN — BROKEN (CABIN) · airframe 58,066 hrs · 33,807 cycles

RT OVERWING EMERGENCY EXIT SIGN BROKEN. R&R SIGN PER MM.

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 57,626 hrs · 33,528 cycles

FORWARD RIGHT BATTERY FAILED TIME TEST. R & R THE BATTERY IAW AMM.

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 57,626 hrs · 33,528 cycles

AFT RIGHT BATTERY FAILED TIME TEST. R & R BATTERY IAW AMM.

Part: LAMP — UNSECURE (EMERGENCY LIGHT) · airframe 57,082 hrs · 33,207 cycles

LEFT OVERHEAD BIN EMERGENCY LIGHT INOPERATIVE BETWEEN ROWS 23 TO 24. RESEATED THE LAMP IAW AMM.

Part: BULKHEAD — CRACKED (RT MLG WW) · airframe 57,082 hrs · 33,207 cycles

RIGHT MAIN WHEEL WELL REAR SPAR VAPOR BARRIER, FIBERGLASS BULKHEAD CRACKED. REPAIRED BULKHEAD PER EA.

Part: STRINGER CLIP — CRACKED (BS 360) · airframe 57,082 hrs · 33,207 cycles

STRINGER CLIP CRACKED AT BS 360, STRINGER 8R. R & R THE STRINGER CLIP IAW SRM.

Part: FRAME — CRACKED (BS 440) · airframe 57,082 hrs · 33,207 cycles

FRAME CRACKED AT BS 440, STRINGER 8R. REPAIRED THE FRAME IAW EA.

Part: FRAME — CRACKED (BS 500C) · airframe 57,082 hrs · 33,207 cycles

FRAME CRACKED AT BS 500C, STRINGER 8R. REPAIRED THE FRAME IAW EA.

Part: FRAME — CRACKED (BS 727B) · airframe 57,082 hrs · 33,207 cycles

FRAME CRACKED AT BS 727B, STRINGER 8R. REPAIRED THE FRAME IAW EA.

Part: FRAME — CRACKED (BS 787) · airframe 57,082 hrs · 33,207 cycles

FRAME CRACKED AT BS 787, STRINGER 8L. REPAIRED THE FRAME IAW EA.

Part: FRAME — CRACKED (BS 480) · airframe 57,082 hrs · 33,207 cycles

FRAME CRACKED AT BS 480, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (BS 500C) · airframe 57,082 hrs · 33,207 cycles

FRAME CRACKED AT BS 500C, STRINGER 8L. REPAIRED THE FRAME IAW EA.

Part: FRAME — CRACKED (BS 480) · airframe 57,082 hrs · 33,207 cycles

FRAME CRACKED AT BS 480, STRINGER 8R. REPAIRED THE FRAME IAW EA.

Part: FRAME — CRACKED (BS 867) · airframe 57,082 hrs · 33,207 cycles

FRAME CRACKED AT BS 867, STRINGER 8L. REPAIRED THE FRAME IAW EA.

Part: FRAME — CRACKED (BS 380) · airframe 57,082 hrs · 33,207 cycles

FRAME CRACKED AT BS 380, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (BS 500A) · airframe 57,082 hrs · 33,207 cycles

FRAME CRACKED AT BS 500A, STRINGER 8R. REPAIRED THE FRAME IAW EA.

Part: FRAME — CRACKED (BS 787) · airframe 57,082 hrs · 33,207 cycles

FRAME CRACKED AT BS 787, STRINGER 8R. REPAIRED THE FRAME IAW EA.

Part: FRAME — CRACKED (BS 907) · airframe 57,082 hrs · 33,207 cycles

FRAME CRACKED AT BS 907, STRINGER 8R. REPAIRED THE FRAME IAW EA.

Part: FRAME — CRACKED (BS 747) · airframe 57,082 hrs · 33,207 cycles

FRAME CRACKED AT BS 747, STRINGER 8L. REPAIRED THE FRAME IAW EA.

Part: FRAME — CRACKED (BS 727D) · airframe 57,082 hrs · 33,207 cycles

FRAME CRACKED AT BS 727D, STRINGER 8L. REPAIRED THE FRAME IAW EA.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 55,700 hrs · 32,438 cycles

LEFT & RIGHT AC BAY KEEL BEAM DUCT BRACKETS CRACKED. R & R BRACKET IAW SIP.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 54,614 hrs · 31,797 cycles

LEFT HORIZONTAL STABILIZER LOWER IN-SPAR SKIN, CRACKED IN SKIN ON INBD SIDE OF STAB STATION 184.70, RIB, 10.0" FROM AFT EDGE OF SKIN PANEL. REPAIRED SKIN IAW SRM.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 54,614 hrs · 31,797 cycles

RIGHT NR 3 WINDOW FRAME, NR 4 HOLE UP FROM BOTTOM CRACKED. REPAIRED WINDOW IAW ACO.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 54,614 hrs · 31,797 cycles

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

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 54,614 hrs · 31,797 cycles

RIGHT NR 3 WINDOW FRAME, SECOND HOLE UP FROM BOTTOM CRACKED. REPAIRED FRAME IAW ACO.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 54,614 hrs · 31,797 cycles

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

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 54,614 hrs · 31,797 cycles

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

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 54,614 hrs · 31,797 cycles

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

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 54,614 hrs · 31,797 cycles

LEFT NR 3 WINDOW FRAME, NR 3 HOLE UP FROM BOTTOM CRACKED. R & R FRAME IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 54,614 hrs · 31,797 cycles

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

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 54,614 hrs · 31,797 cycles

AFT SEAT TRACK INBD FLANGE CRACKED AT BS 727B, RBL 24.75. REPAIRED SEAT TRACK IAW EA.

Part: SKIN — CRACKED (LT WING) · airframe 54,167 hrs · 31,516 cycles

LEFT WING LOWER SKIN AT WING STATION 671.5, AFT OF AFT SPAR CRACKED. REPAIRED SKIN IAW EA.

Part: SLIDE — DAMAGED (R1 DOOR) · airframe 53,870 hrs · 31,353 cycles

R1 DOOR AFT SLIDE MOUNT PAD CRACKED. R & R SLIDE IAW SRM.

Part: PLATE — CRACKED (LT WING) · airframe 53,870 hrs · 31,353 cycles

LEFT WING PANEL 551GB WIGGLE PLATE CRACKED. R & R WIGGLE PLATE IAW SRM.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 52,847 hrs · 30,786 cycles

AFT GALLEY EXIT SIGN LIGHT BULB INOPERATIVE. RELAMPED BULB IAW MM.

Part: ACTUATOR — MALFUNCTIONED (FUEL SYSTEM) · airframe 51,578 hrs · 30,060 cycles

NUMBER 1 FUEL IMBALANCE AT 1 HR 40 MIN INTO FLIGHT. CORRECTED VIA FUEL BALANCE PROCEDURES. UPON RESETTING CROSS FEED VLV TO CLOSED POSITION HAD NO LIGHT INDICATING POSITION OF VLV. CB CROSS FEED VLV POPPED DID NOT RESET. R & R CROSS FEED ACTIVATOR IAW MM.

Part: FLAP — DELAMINATED (LT WING) · airframe 50,618 hrs · 29,514 cycles

LEFT WING OTBD AFT FLAP INBD EDGE DELAMINATED. REPAIRED AFT FLAP IAW SRM.

Part: ATTACH ANGLE — CRACKED (LT WING) · airframe 49,267 hrs · 28,768 cycles

LEFT WING UPPER TE PANEL TO ROLLER CASTING WEB ATTACH ANGLE CRACKED. R & R ANGLE IAW SRM.

Part: ACTUATOR — LEAKING (RT MLG) · airframe 46,945 hrs · 27,331 cycles

RT MAIN GEAR RETRACT ACTUATOR LEAKED. R&R RT MLG RETRACT ACTUATOR IAW MM.

Part: SIGN — DETACHED (CABIN) · airframe 45,985 hrs · 26,775 cycles

AFT ENTRY EXIT SIGN FELL OFF. REMOVED AND REPLACED SIGN PER MM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 45,880 hrs · 26,722 cycles

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

Part: HOOK — LOOSE (R1 DOOR) · airframe 45,880 hrs · 26,722 cycles

R1 DOOR EMERGENCY EVAC SLIDE COVER FWD GIRT BAR HOOK LOOSE. SECURED HOOK PER SRM & MT.

Part: WINDOW POST — CRACKED (R1) · airframe 43,647 hrs · 25,330 cycles

R1 WINDOW POST CRACKED AT UPPER AFT CORNER. REMOVED AND REPLACED POST PER SRM AND DWG.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 43,647 hrs · 25,330 cycles

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

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 43,647 hrs · 25,330 cycles

RIGHT HORIZONTAL STABILIZER RIB CRACKED AT STA 92.70. REPAIRED RIB PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,647 hrs · 25,330 cycles

FRAME CRACKED AT BS 827, STR 8R. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,647 hrs · 25,330 cycles

FRAME CRACKED AT BS 867, STR 8R. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,647 hrs · 25,330 cycles

FRAME CRACKED AT BS 827, STR 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,647 hrs · 25,330 cycles

FRAME CRACKED AT BS 727D, STR 8R. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,647 hrs · 25,330 cycles

FRAME CRACKED AT BS 907, STR 8L. REPAIRED FRAME PER ER AND EA.

Part: STRAP — CORRODED (FUSELAGE) · airframe 43,647 hrs · 25,330 cycles

LEFT OVERWING EXIT CUTOUT LOWER SILL I/B FWD HORIZONTAL STRAP CORRODED AT BS 620. REPAIRED STRAP IAW SRM.

Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 43,647 hrs · 25,330 cycles

FLOORBEAM UPPER CHORD SUPPORT CLIP CRACKED AT BS 727B, RBL 45. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,647 hrs · 25,330 cycles

FRAME CRACKED AT BS 400, STR 8R. REPAIRED FRAME IAW EA.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 43,647 hrs · 25,330 cycles

RIGHT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 101.90. REPAIRED SKIN IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 43,647 hrs · 25,330 cycles

STRINGER CLIP CRACKED AT BS 856, STR 25R. REMOVED AND REPLACED CLIP PER SRM AND DWG.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 43,647 hrs · 25,330 cycles

BULKHEAD CRACKED AT BS 663, LBL 34. REPAIRED BULKHEAD PER ER & EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,647 hrs · 25,330 cycles

FRAME CRACKED AT BS 360, STR 8R. REPAIRED FRAME PER ER AND EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,647 hrs · 25,330 cycles

FRAME CRACKED AT BS 400, STR 8L. REPAIRED FRAME IAW EA.

Part: WEB — CORRODED (FUSELAGE) · airframe 43,647 hrs · 25,330 cycles

SUB THRESHOLD WEB CORRODED BETWEEN BS 795 TO BS 847, RBL 26. REMOVED AND REPLACED WEB ASSY IAW SRM & DWG.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 42,953 hrs · 24,937 cycles

LEFT HORIZONTAL STAB LOWER SKIN CRACKED AT STA 147.90. REPAIRED SKIN PER SRM.

Part: LENS — BROKEN (CABIN) · airframe 41,615 hrs · 24,145 cycles

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

Part: SKIN — PUNCTURED (LT WING) · airframe 40,630 hrs · 23,601 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT WING L/E SKIN PUNCTURED AT WS 432. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 40,630 hrs · 23,601 cycles

DURING SCHEDULED HC2 CHECK, FOUND RT WING NR 7 SLAT LOWER SKIN L/E CRACKED. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (LE SLAT) · airframe 40,630 hrs · 23,601 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT WING NR 2 SLAT LOWER SKIN L/E CRACKED. REMOVED AND REPLACED SLAT PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 40,630 hrs · 23,601 cycles

DURING SCHEDULED HC2 CHECK, FOUND RT DOOR EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 40,483 hrs · 23,508 cycles

L2 DOOR EMERGENCY EXIT SIGN LIGHT INOP. REMOVED AND REPLACED LIGHT PER MM.

Part: SIGN — LOOSE (CABIN) · airframe 40,332 hrs · 23,425 cycles

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

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 40,038 hrs · 23,264 cycles

DURING SCHEDULED MV1 CHECK, FOUND LT HORIZ STAB INSPAR SKIN CRACKED AT STA 129.50, FORWARD F/O REAR SPAR LOWER SURFACE. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 40,038 hrs · 23,264 cycles

DURING SCHEDULED MV1 CHECK, FOUND LT HORIZ STAB INSPAR SKIN CRACKED AT STA 92.70, FORWARD F/O REAR SPAR LOWER SURFACE. REPAIRED SKIN PER SRM.

Part: ACTUATOR — FAULTY (FUEL SYSTEM) · airframe 37,980 hrs · 22,047 cycles

DIVERSION - CROSSFEED VALVE CIRCUIT BREAKER TRIPPED INFLIGHT. REMOVED AND REPLACED CROSSFEED VALVE ACTUATOR PER MM.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 36,893 hrs · 21,436 cycles

DURING SCHEDULED 10Y CHECK, FOUND INTERCOSTAL CORRODED AT BS 270, BL 0. REPAIRED INTERCOSTAL PER EA.

Part: FITTING — CRACKED (CENTER WING BOX) · airframe 36,893 hrs · 21,436 cycles

DURING SCHEDULED 10Y CHECK, FOUND CENTER WING BOX SHEAR FITTING CRACKED AT BS 540, RBL 15. REMOVED AND REPLACED FITTING PER SRM.

Part: FITTING — CRACKED (CENTER WING BOX) · airframe 36,893 hrs · 21,436 cycles

DURING SCHEDULED 10Y CHECK, FOUND CENTER WING BOX SHEAR FITTING CRACKED AT BS 540, LBL 7. REMOVED AND REPLACED FITTING PER SRM.

Part: FITTING — CRACKED (CENTER WING BOX) · airframe 36,893 hrs · 21,436 cycles

DURING SCHEDULED 10Y CHECK, FOUND CENTER WING BOX SHEAR FITTING CRACKED AT BS 540, LBL 15. REMOVED AND REPLACED FITTING PER SRM.

Part: FITTING — CRACKED (CENTER WING BOX) · airframe 36,893 hrs · 21,436 cycles

DURING SCHEDULED 10Y CHECK, FOUND CENTER WING BOX SHEAR FITTING CRACKED AT BS 540, RBL 7. REMOVED AND REPLACED FITTING PER SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 36,116 hrs · 20,975 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT WING NR 1 SLAT CRACKED AT LOWER SKIN. R&R NR 1 SLAT PER MM.

Part: HOLDER — LOOSE (GIRT BAR) · airframe 36,116 hrs · 20,975 cycles

DURING SCHEDULED HC2 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE GIRT BAR HOLDER LOOSE. SECURED HOLDER PER MM.

Part: COVER — MISSING (CABIN) · airframe 35,663 hrs · 20,714 cycles

OVERWING EMERGENCY EXIT SIGN COVER MISSING. REMOVED AND REPLACED COVER PER MM.

Part: FITTING — CORRODED (RT MLG TRUNNION) · airframe 35,216 hrs · 20,438 cycles

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

Part: FITTING — CORRODED (LT MLG TRUNNION) · airframe 35,216 hrs · 20,438 cycles

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

Part: LIGHT — LOOSE (CABIN) · airframe 34,778 hrs · 20,175 cycles

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

Part: BALLAST — FAULTY (CABIN) · airframe 33,922 hrs · 19,653 cycles

AIR TURNBACK / DECLARED EMERGENCY. FLIGHT ATTENDANT REPORTED ELECTRICAL SMELL FROM AFT ENTRY LIGHT IN AFT GALLEY. ALL A/C SYSTEMS OPERATED NORMALLY DURING FLIGHT. INSPECTED AFT GALLEY AREA AND AFT ENTRY LIGHT, NO DEFECTS NOTED. SUSPECT AFT ENTRY LIGHT BALLAST. REMOVED AND REPLACED BALLAST PER MM.

Part: HOOK — LOOSE (GIRT BAR) · airframe 33,922 hrs · 19,653 cycles

DURING SCHEDULED HC1 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR HOOK LOOSE. SECURED HOOK PER MM.

Part: HOOK — LOOSE (GIRT BAR) · airframe 33,922 hrs · 19,653 cycles

DURING SCHEDULED HC1 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR HOOK LOOSE. SECURED HOOK PER MM.

Part: LENS — LOOSE (CABIN) · airframe 32,677 hrs · 18,869 cycles

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

Part: LENS — LOOSE (CABIN) · airframe 32,677 hrs · 18,869 cycles

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

Part: LENS — LOOSE (CABIN) · airframe 32,581 hrs · 18,818 cycles

FWD ENTRY EMERGENCY EXIT LIGHT LENS LOOSE. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: FLAP — DELAMINATED (LT WING) · airframe 31,640 hrs · 18,280 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT WING O/B AFT FLAP I/B END DELAMINATED. REMOVED AND REPLACED FLAP PER MM.

Part: BLADES — DAMAGED (NR 1 ENGINE) · airframe 31,669 hrs · 18,292 cycles

DURING SCHEDULED HC2 CHECK, FOUND NR 1 ENGINE HPC BLADES DAMAGED. REMOVED AND REPLACED NR 1 ENGINE PER MT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,253 hrs · 18,062 cycles

DURING SCHEDULED MV3 CHECK, FOUND OVERHEAD BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 16. RELAMPED LIGHT PER MM.

Part: GLOWSTRIP — WORN (CABIN) · airframe 30,309 hrs · 17,488 cycles

DURING SCHEDULED 8Y CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIPS WORN IN LT MID CABIN. REMOVED AND REPLACED STRIPS PER MM.

Part: GLOWSTRIP — WORN (CABIN) · airframe 30,309 hrs · 17,488 cycles

DURING SCHEDULED 8Y CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIPS WORN IN RT AFT CABIN. REMOVED AND REPLACED STRIPS PER MM.

Part: FRAME — CRACKED (BS 295) · airframe 30,309 hrs · 17,488 cycles

DURING SCHEDULED 8Y CHECK, FOUND FUSELAGE STUB FRAME CRACKED AT BS 295, RBL 54. REPAIRED FRAME PER SRM.

Part: FLOORBEAM — CORRODED (BS 328) · airframe 30,309 hrs · 17,488 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 328, RBL 32.5 TO RBL 11. REPAIRED BEAM PER SWA EA.

Part: FLOORBEAM — CORRODED (BS 328) · airframe 30,309 hrs · 17,488 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 328, RBL 11 TO RBL 36.5. REPAIRED FLOORBEAM PER SWA EA.

Part: FLOORBEAM — CORRODED (BS 986) · airframe 30,309 hrs · 17,488 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986.5, RBL 5 TO RBL 43. REPAIRED FLOORBEAM PER SWA EA.

Part: CONNECTOR — CRACKED (EMERGENCY LIGHT) · airframe 30,309 hrs · 17,488 cycles

DURING SCHEDULED 8Y CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT CONNECTOR CRACKED. REPAIRED CONNECTOR PER WDM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 28,804 hrs · 16,546 cycles

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

Part: LIGHT — LOOSE (CABIN) · airframe 24,934 hrs · 14,233 cycles

DURING SCHEDULED MV1 CHECK, FOUND EEPLS LOOSE BETWEEN ROW 8 ABC & 10 ABC. SECURED EEPLS PER MM.

Part: COVER — LOOSE (CABIN) · airframe 24,868 hrs · 14,197 cycles

EEPLS COVER LOOSE AT ROW 6 ABC. SECURED COVER PER MM.

Part: STRIP — WORN (CABIN) · airframe 24,600 hrs · 14,054 cycles

DURING SCHEDULED HC1 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP WORN AT ROW 8 ABC TO ROW 11 ABC. REMOVED AND REPLACED STRIP PER MM.

Part: LENS — BROKEN (CABIN) · airframe 24,448 hrs · 13,960 cycles

EMERGENCY EXIT LOWER LIGHT LENS AT L2 DOOR BROKEN. REMOVED AND REPLACED LIGHT LENS PER MM.

Part: FAN — ODOR (GASPER) · airframe 24,344 hrs · 13,899 cycles

WITH GASPER FAN OPERATING, SMELL/ODOR IN CABIN. REMOVED AND REPLACED GASPER FAN PER MM.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 22,308 hrs · 12,749 cycles

RIGHT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LIGHT LENS PER MM.

Part: BATTERY — FAILED (CABIN) · airframe 22,117 hrs · 12,649 cycles

DURING SCHEDULED HC2 CHECK, ALL EMERGENCY EXIT LIGHT BATTERY PACKS FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACKS PER MM.

Part: SIGN — BROKEN (L1 DOOR) · airframe 19,816 hrs · 11,364 cycles

DURING SCHEDULED RON CHECK, FOUND L1 DOOR EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED SIGN PER MM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 18,598 hrs · 10,640 cycles

DURING SCHEDULED 5Y CHECK, FOUND FUSELAGE FLOORBEAM CORRODED AT BS 767, BETWEEN LBL 12.0 TO RBL 7.5. REPAIRED FLOORBEAM PER SWA EA.

Part: SLIDE — DEPLOYED (R2 DOOR) · airframe 14,592 hrs · 8,329 cycles

DURING SCHEDULED MV1 CHECK, FOUND R2 DOOR EVAC SLIDE DEPLOYED. REMOVED AND REPLACED R2 DOOR EVAC SLIDE PER MM.

Part: BUSHING — WORN (RT ELEVATOR) · airframe 10,097 hrs · 5,849 cycles

DURING SCHEDULED SERVICE CHECK, SWA SI 11038-55, FOUND RT ELEVATOR TAB NR 4 HINGE WORN. REMOVED AND REPLACED HARDWARE AND BUSHING ON NR 4 HINGE PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 8,623 hrs · 4,997 cycles

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

Part: BUSHING — WORN (LEFT ELEVATOR) · airframe 8,351 hrs · 4,838 cycles

DURING SCHEDULED A1 CHECK, FOUND LT ELEVATOR TAB HINGE NR 2, NR 3 AND NR 4 BUSHINGS WORN. REMOVED AND REPLACED TAB HINGE BUSHINGS PER MM.

Part: BUSHING — WORN (RT ELEVATOR) · airframe 8,351 hrs · 4,838 cycles

DURING SCHEDULED A1 CHECK, FOUND RT ELEVATOR TAB HINGE NR 2, NR 3 AND NR 4 BUSHINGS WORN. REMOVED AND REPLACED TAB HINGE BUSHINGS AND HARDWARE PER MM.

Part: COVER — CRACKED (CABIN) · airframe 7,908 hrs · 4,573 cycles

DURING SCHEDULED C3 CHECK, FOUND EEPLS COVERS CRACKED AT ROW NR 3, 4, 5, 11 AND 23. REMOVED AND REPLACED EEPLS COVERS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 7,782 hrs · 4,494 cycles

DURING SCHEDULED A2 CHECK, FOUND EEPLS INOP AT FWD CABIN. RELAMPED EEPLS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 7,247 hrs · 4,184 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EEPLS INOP AND LENS MISSING AT ROW NR 1. RELAMPED LIGHT AND INSTALLED LENS PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 7,247 hrs · 4,184 cycles

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

Part: COVER — CRACKED (CABIN) · airframe 6,753 hrs · 3,891 cycles

DURING SCHEDULED C2 CHECK, FOUND EEPLS COVERS MISSING AT ROW 13 AND CRACKED AT FWD END. REMOVED AND REPLACED COVERS PER MM.

Part: SLIDE — OUT OF POSITION (AFT ENTRY DOOR) · airframe 4,510 hrs · 2,628 cycles

AFT ENTRY DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REMOVED AND REPLACED SLIDE PER MM.

Part: BOTTLE — DISCHARGED (PAX DOOR SLIDE) · airframe 761 hrs · 427 cycles

FWD ENTRY EMERGENCY EVAC SLIDE PRESS IND LOW. REMOVED AND REPLACED SLIDE ASSY PER MM.