N761RR

Part: LIGHT — INOPERATIVE (CABIN) · airframe 66,500 hrs · 38,893 cycles

L2 DOOR EMERGENCY LIGHT INOP. RELAMPED LIGHT PER AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 63,378 hrs · 36,899 cycles

AFT RT EMERGENCY LIGHT INOP. R&R BATTERY PACK PER MM.

Part: WIRE — BROKEN (CABIN) · airframe 63,250 hrs · 36,819 cycles

LT OVERWING EMERGENCY ESCAPE HATCH LIGHT INOP. FOUND BROKEN WIRE FROM TERMINAL ON CONNECTOR. R&R TERMINAL IAW SWPM.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHTS) · airframe 62,680 hrs · 36,460 cycles

L2 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. CONNECTED THE CONNECTOR IAW AMM.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 62,680 hrs · 36,460 cycles

RIGHT OVERWING EXIT FORWARD LOWER EMERGENCY EXIT SIGN LENS MISSING. INSTALLED LENS IAW AMM.

Part: BATTERY — FAILED (EMERGENCY LIGHTS) · airframe 62,680 hrs · 36,460 cycles

FORWARD ENTRY EMERGENCY LIGHT FAILED. R & R BATTERY IAW AMM.

Part: CRADLE — CRACKED (FLASHLIGHT) · airframe 62,680 hrs · 36,460 cycles

FORWARD LEFT EMERGENCY FLASHLIGHT BASE CRACKED. R & R THE FLASHLIGHT BASE IAW AMM.

Part: HOUSING — DAMAGED (EMERGENCY SIGN) · airframe 62,680 hrs · 36,460 cycles

FORWARD LAVATORY AFT WALL LOWER EMERGENCY EXIT SIGN HOUSING DAMAGED. R & R THE SIGN IAW AMM.

Part: FLOOR SUPPORT — CORRODED (BS 986-1006) · airframe 62,680 hrs · 36,460 cycles

CABIN FLOOR SUPPORT CORRODED BETWEEN BS 986 TO 1006, RBL 38. R & R THE FLOOR SUPPORT IAW DWG.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 62,680 hrs · 36,460 cycles

R1 DOOR FORWARD LOWER STUB FRAME ATTACH ANGLE CRACKED. R&R STUB FRAME IAW SRM AND DWG.

Part: WEB — CORRODED (FUSELAGE) · airframe 62,680 hrs · 36,460 cycles

R2 DOOR CREASE BEAM WEB CORRODED. R & R THE WEB IAW EA, SRM, AND DWG.

Part: SKIN — CORRODED (BS 420) · airframe 62,680 hrs · 36,460 cycles

EXTERIOR FUSELAGE SKIN CORRODED AT BS 420+10, BETWEEN STRINGERS 28L TO 28R. REPAIRED THE SKIN IAW SRM IAW EA.

Part: FLOORBEAM — CORRODED (BS 986) · airframe 62,680 hrs · 36,460 cycles

FLOORBEAM TEE CORRODED AT BS 986, BETWEEN RBL 20 TO RBL 48. REPAIRED THE FLOORBEAM TEE IAW EA, SRM, & DWG.

Part: BEAM — CORRODED (BS 303-350) · airframe 62,680 hrs · 36,460 cycles

L1 DOOR SURROUND BEAM CORRODED BETWEEN BS 303 TO 350. R & R IAW SRM AND DWG.

Part: CREASE BEAM — CORRODED (BS 947-992) · airframe 62,680 hrs · 36,460 cycles

CREASE BEAM CORRODED BETWEEN BS 947 - 992. R & R THE CREASE BEAM IAW SRM AND DWG.

Part: PRESSURE DECK — CRACKED (FUSELAGE) · airframe 62,680 hrs · 36,460 cycles

HORIZONTAL PRESSURE DECK WEB CRACKED AT BS 664, LBL 32. REPAIRED WEB IAW EA.

Part: WEB — CRACKED (BS 665) · airframe 62,680 hrs · 36,460 cycles

HORIZONTAL PRESSURE DECK WEB CRACKED AT BS. 665, RBL 42. / REPAIRED WEB IAW EA.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 62,680 hrs · 36,460 cycles

INTERCOSTAL CRACKED BETWEEN BS 344 TO BS 328, LBL 47. REPAIRED INTERCOSTAL IAW SRM & DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 62,680 hrs · 36,460 cycles

INTERCOSTAL CRACKED BETWEEN BS 312 TO BS 328, RBL 33. R&R INTERCOSTAL IAW SRM & DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 62,680 hrs · 36,460 cycles

INTERCOSTAL CRACKED BETWEEN BS 294.5 TO BS 276.5, RBL 1. R&R INTERCOSTAL DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 62,680 hrs · 36,460 cycles

INTERCOSTAL CRACKED BETWEEN BS 294 TO BS 312, RBL 16. R&R INTERCOSTAL IAW SRM AND DWG.

Part: STRAP — CORRODED (FUSELAGE) · airframe 62,680 hrs · 36,460 cycles

R1 DOOR CREASE BEAM INNER CHORD VERTICAL FLANGE STRAP CORRODED BETWEEN BS 291 TO BS 301. R&R STRAP IAW DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 62,680 hrs · 36,460 cycles

R1 DOOR CREASE BEAM INNER CHORD CORRODED BETWEEN BS 291 TO BS 332. R&R CREASE BEAM IAW DWG & AMM.

Part: STUB FRAME — CRACKED (BS 294) · airframe 62,680 hrs · 36,460 cycles

R1 DOOR SURROUND LOWER STUB FRAME CRACKED AT BS 294. R & R THE STUB FRAME IAW SRM AND DWG.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 62,680 hrs · 36,460 cycles

FORWARD CARGO PIT AFT BULKHEAD STRUCTURE GUSSET CRACKED AT BS 500D, STR 19L. R&R GUSSET IAW DWG & AMM.

Part: TEE FITTING — CORRODED (FUSELAGE) · airframe 62,680 hrs · 36,460 cycles

T CLIP CORRODED AT BS 794, RBL 18. R&R "T" CLIP IAW EA.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · airframe 62,680 hrs · 36,460 cycles

L1 DOOR SURROUND CREASE BEAM INNER CHORD ATTACH ANGLE CORRODED BETWEEN BS 313 TO BS 342. R&R ANGLE IAW SRM AND DWG.

Part: PLATE — CRACKED (RT WING) · airframe 62,680 hrs · 36,460 cycles

RT WING AFT TRAILING EDGE CAVITY RSS 261 LOCATION WAFFLE PLATE CRACKED. R&R WAFFLE PLATE IAW DWG & SRM.

Part: BAFFLE — CRACKED (BS 500A) · airframe 62,680 hrs · 36,460 cycles

FORWARD CARGO BAY, LT BAFFLE CLIP FORWARD CRACKED AT BS 500A. R & R THE BAFFLE CLIP IAW SRM AND DWG.

Part: ANGLE — CORRODED (BS 500A-500D) · airframe 62,680 hrs · 36,460 cycles

FORWARD CARGO BAY, RT ZEE ANGLE CORRODED BETWEEN BS 500A & 500D, RBL 24. REPAIRED THE ANGLE IAW SRM.

Part: MOUNT FITTING — CORRODED (CABIN) · airframe 62,680 hrs · 36,460 cycles

L1 DOOR SURROUND AFT GIRT BAR MOUNT FITTING CORRODED AT BS 344. R&R MOUNT IAW SOPM.

Part: FLOOR SUPPORT — CORRODED (BS 767-807) · airframe 62,680 hrs · 36,460 cycles

AFT CARGO BAY LT SIDE FLOOR SUPPORT CORRODED BETWEEN BS 767 TO 807. R & R THE FLOOR SUPPORT IAW AMM AND SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 62,680 hrs · 36,460 cycles

L1 DOOR SURROUND CREASE BEAM SILL WEB MIDDLE SUPPORT Z CORRODED BETWEEN BS 315 TO BS 339. R&R CHORD PER SRM & DWG.

Part: BAFFLE — CRACKED (BS 500B) · airframe 62,680 hrs · 36,460 cycles

FORWARD CARGO BAY, LT BAFFLE CRACKED AT BS 500B, LBL 24. R & R THE BAFFLEP IAW SRM & DWG.

Part: WEB — CRACKED (RT WING) · airframe 62,680 hrs · 36,460 cycles

RIGHT WING UPPER SURFACE TRAILING EDGE FIXED PANEL BETWEEN NR 7 & 8 SPOILER MIDDLE SUPPORT BRACKETS CRACKED. R & R THE WEB ASSEMBLY IAW SRM.

Part: BULKHEAD — CRACKED (BS 663) · airframe 62,680 hrs · 36,460 cycles

BULKHEAD WEB CRACKED AT BS 663. REPAIRED THE BULKHEAD IAW EA.

Part: BAFFLE — CRACKED (BS 500-500A) · airframe 62,618 hrs · 36,419 cycles

FORWARD CARGO BAY, LT BAFFLE CRACKED BETWEEN BS 500 & 500A. R & R THE BAFFLE IAW SRM & DWG.

Part: LENS — MISSING (EXIT SIGN) · airframe 61,754 hrs · 35,861 cycles

R1 DOOR EXIT SIGN LENS MISSING. INSTALLED LENS PER SIP.

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 60,930 hrs · 35,387 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1670. R & R THE BATTERY IAW AMM.

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 60,930 hrs · 35,387 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1675. R & R THE BATTERY IAW AMM.

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 60,930 hrs · 35,387 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1672. R & R THE BATTERY IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 60,726 hrs · 35,266 cycles

LT EMERGENCY EXIT LIGHT INOP AT ROW 11 ABC. RELAMPED PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 59,684 hrs · 34,660 cycles

RT OVERHEAD BULLNOSE BIN EMERGENCY LIGHT INOP AT ROW 22. RELAMPED LIGHT PER AMM.

Part: SCUFF PLATE — CRACKED (FUSELAGE) · airframe 58,986 hrs · 34,262 cycles

AFT CARGO DOOR CUTOUT AFT CORNER SCUFF PLATE CRACKED. R & R SCUFF PLATE IAW AMM.

Part: SLIDE — UNSECURE (L1 DOOR) · airframe 58,599 hrs · 34,036 cycles

L1 DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT, DID NOT DEPLOY, STILL OPERATIONAL. REINSTALLED SLIDE IAW MAINTENANCE.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,421 hrs · 33,387 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,421 hrs · 33,387 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,421 hrs · 33,387 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,421 hrs · 33,387 cycles

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

Part: SKIN — CRACKED (LE SLAT) · airframe 57,421 hrs · 33,387 cycles

RIGHT WING NR 7 SLAT LE CRACKED, AT LOWER SKIN ACTUATOR AREA. REPAIRED NR 7 SLAT IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,421 hrs · 33,387 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,421 hrs · 33,387 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,421 hrs · 33,387 cycles

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

Part: FITTING — CRACKED (FUSELAGE) · airframe 57,421 hrs · 33,387 cycles

CLIP CRACKED AT BS 380, STRINGER 8L. R & R CLIP IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,421 hrs · 33,387 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,421 hrs · 33,387 cycles

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

Part: SKIN — CRACKED (LE SLAT) · airframe 57,421 hrs · 33,387 cycles

RIGHT WING NR 8 SLAT LE CRACKED, AT LOWER ACTUATOR SKIN AREA. REPAIRED SLAT IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,421 hrs · 33,387 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,421 hrs · 33,387 cycles

EXTERNAL POWER DOOR CUT OUT CRACKED. REPAIRED CUT OUT IAW EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 55,826 hrs · 32,443 cycles

BULLNOSE EMER LIGHT INOPERATIVE AT 11 DEF. RELAMPED IAW MM.

Part: COVER — UNSECURE (EXIT SIGN) · airframe 55,699 hrs · 32,357 cycles

R2 DOOR EXIT SIGN COVER FELL OFF. R & R SIGN ASSEMBLY IAW MM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 55,608 hrs · 32,298 cycles

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

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 55,608 hrs · 32,298 cycles

L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUSTMENT. R & R SLIDE IAW MT.

Part: GIRT BAR — LOOSE (R1 DOOR) · airframe 55,522 hrs · 32,252 cycles

R1 DOOR EVAC SLIDE GIRT BAR LOOSE. SECURED & ADJUSTED GIRT BAR HOOKS IAW MM.

Part: LENS — BROKEN (CABIN) · airframe 55,350 hrs · 32,164 cycles

R1 DOOR EXIT LOWER LIGHT LENS BROKEN. R & R LIGHT ASSEMBLY IAW AMM.

Part: GLOWSTRIP — DAMAGED (CABIN) · airframe 54,763 hrs · 31,849 cycles

FORWARD CABIN EMER PHOTO LUMINESCENT FLOOR STRIPS DAMAGED. R & R STRIP IAW AMM.

Part: THRESHOLD — CRACKED (FUSELAGE) · airframe 54,763 hrs · 31,849 cycles

FUSELAGE AFT CARGO DOOR CUT OUT LOWER CTR THRESHOLD CRACKED. R & R THRESHOLD IAW SRM.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 54,753 hrs · 31,841 cycles

FORWARD SEAT TRACK CRACKED AT BS 727B, RBL 24.7. REPAIRED SEAT TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 54,753 hrs · 31,841 cycles

FORWARD SEAT TRACK CRACKED AT BS 727B, RBL 45.5. REPAIRED SEAT TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 54,753 hrs · 31,841 cycles

FORWARD SEAT TRACK CRACKED AT BS 727B, LBL 24.7. REPAIRED SEAT TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 54,753 hrs · 31,841 cycles

FORWARD SEAT TRACK CRACKED AT BS 727B, LBL 45.5. REPAIRED SEAT TRACK IAW EA.

Part: GLOWSTRIP — CRACKED (CABIN) · airframe 54,753 hrs · 31,841 cycles

RIGHT PHOTO LUMINESCENT STRIP CRACKED AT BS 685. R & R STRIP IAW AMM.

Part: HYDRAULIC LINE — LOOSE (LT MLG WW) · airframe 54,209 hrs · 31,538 cycles

DIVERSION, ENG DRIVEN A PUMP LIGHT ILLUMINATED AT FL410. QTY % READ 21%. SHUTDOWN THE PUMP. PRESS READ 3040 WITHOUT FLUCTUATION. ELEC NR 1 PUMP LOW PRESS LIGHT DID NOT ILLUMINATE. FOUND LOOSE HYD LINE AT HYD GND SPOILER CONTROL VLV. SECURED HYD LINE IAW AMM 27-62-41.

Part: LENS — LOOSE (CABIN) · airframe 53,676 hrs · 31,221 cycles

ENTRY DOOR LOWER EMER EXIT LIGHT LENS LOOSE. R & R LIGHT ASSEMBLY IAW MM.

Part: MOUNT — DAMAGED (R1 DOOR) · airframe 52,571 hrs · 30,603 cycles

R1 DOOR EMER EVAC SLIDE UPPER AFT ATTACH POINT UPPER SHOCK MOUNT DAMAGED. R & R MOUNT IAW SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 52,571 hrs · 30,603 cycles

LEFT WING NR 2 SLAT LE SKIN CRACKED AT TWO FASTENERS AT THE ACTUATOR ATTACH BRACKET. R & R NR 2 SLAT IAW MM.

Part: ATTACH FITTING — LOOSE (TE FLAP TRACK) · airframe 52,571 hrs · 30,603 cycles

LEFT WING OTBD AFT FLAP TRACK OTBD ATTACHMENT LOOSE. R & R AFT FLAP TRACK IAW MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 52,571 hrs · 30,603 cycles

LEFT MID CABIN EMER LIGHTING BATTERY PACK FAILED CAPACITY TEST. R & R BATTERY PACK IAW AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 52,571 hrs · 30,603 cycles

RIGHT MID CABIN EMER LIGHTING BATTERY PACK FAILED CAPACITY TEST. R & R BATTERY PACK IAW AMM.

Part: DOOR — CRACKED (LT MLG) · airframe 52,194 hrs · 30,375 cycles

LEFT MLG INNER DOOR CRACKED. R & R DOOR ASSEMBLY IAW MM.

Part: LIGHT — MISSING (CABIN) · airframe 50,872 hrs · 29,596 cycles

FORWARD GALLEY DOOR LOWER SIDEWALL EGRESS LIGHT MISSING. INSTALLED LIGHT IAW AMM.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 50,872 hrs · 29,596 cycles

LEFT NR 1 WINDOW FRAME UPPER AFT CORNER CRACKED. R & R FRAME IAW ACO.

Part: STIFFENER — CRACKED (RT HORIZ STAB) · airframe 50,872 hrs · 29,596 cycles

RT HORIZONTAL STABILIZER STAB STATION 92.7 LOWER RIB THIRD STIFFENER CRACKED. REPAIRED STIFFENER IAW SRM.

Part: CAP — CRACKED (RT HORIZ STAB) · airframe 50,872 hrs · 29,596 cycles

RIGHT HORIZONTAL STABILIZER STAB STATION 129.50 RIB LOWER T CAP 10 INCHES AFT OF SPAR CRACKED. R & R T CAP IAW EA.

Part: STIFFENER — CRACKED (RT HORIZ STAB) · airframe 50,872 hrs · 29,596 cycles

RT HORIZONTAL STABILIZER STAB STATION 92.7, LOWER RIB FOURTH STIFFENER CRACKED. REPAIRED STIFFENER IAW SRM.

Part: STIFFENER — CRACKED (RT HORIZ STAB) · airframe 50,872 hrs · 29,596 cycles

RT HORIZONTAL STABILIZER STAB STATION 92.7, LOWER RIB SECOND STIFFENER CRACKED. REPAIRED STIFFENER IAW SRM.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 50,872 hrs · 29,596 cycles

LEFT HORIZONTAL STAB RIB CRACKED AT STATION 92.70. REPAIRED RIB IAW SRM.

Part: STIFFENER — CRACKED (LT HORIZ STAB) · airframe 50,872 hrs · 29,596 cycles

LT HORIZONTAL STABILIZER RIB 92.70, 29 INCHES AFT OF FWD SPAR, RIB VERTICAL STIFFENER CRACKED. REPAIRED STIFFENER IAW SRM.

Part: STIFFENER — CRACKED (RT HORIZ STAB) · airframe 50,872 hrs · 29,596 cycles

RT HORIZONTAL STABILIZER STAB STATION 92.7, LOWER RIB FIRST STIFFENER CRACKED. REPAIRED STIFFENER IAW SRM.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 50,872 hrs · 29,596 cycles

FLIGHT DECK LT NR 1 WINDOW FRAME CRACKED IN UPPER AFT CORNER. R & R FRAME IAW ACO.

Part: POST — CRACKED (FUSELAGE) · airframe 50,872 hrs · 29,596 cycles

COCKPIT RT NR 3 WINDOW FRAME E - F POST CRACKED. REPAIRED POST IAW ACO & EA.

Part: WINDOW FRAME — CRACKED (NR 3 WINDOW) · airframe 50,872 hrs · 29,596 cycles

COCKPIT LT NR 3 WINDOW FRAME E F POST CRACKED AT SECOND HOLE FROM BOTTOM. REPAIRED FRAME IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,872 hrs · 29,596 cycles

LOWER FUSELAGE SKIN CRACKED AT BS 540, STRINGER 22L. REPAIRED SKIN IAW EA.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 50,872 hrs · 29,596 cycles

MAIN WW SPAR VERTICAL PRESS WEB CRACKED AT BS 663, BETWEEN LBL 25 TO LBL 45. REPAIRED WEB IAW EA.

Part: SUPPORT BRACKET — CRACKED (RT WING) · airframe 50,872 hrs · 29,596 cycles

RT WING UPPER TE PANEL L SUPPORT BRACKET CRACKED BETWEEN NR 7 & NR 8 SPOILER. R & R L BRACKET IAW SRM & DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 50,872 hrs · 29,596 cycles

INTERCOSTAL CRACKED AT BS 540, STRINGER 22L. R & R INTERCOSTAL IAW SRM & DWG.

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 50,872 hrs · 29,596 cycles

MAIN WW VERTICAL PRESS WEB CRACKED AT BS 663, RBL 41. R &R WEB IAW SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 50,872 hrs · 29,596 cycles

RIGHT OVERWING EMERGENCY EXIT AFT LIGHT INOPERATIVE. RELAMPED LIGHT IAW AMM.

Part: BATTERY — FAILED (CABIN) · airframe 50,495 hrs · 29,380 cycles

RT EMERGENCY LIGHT BATTERIES FAILED CAPACITY TEST. R & R BATTERY IAW MM.

Part: BATTERY — FAILED (CABIN) · airframe 50,495 hrs · 29,380 cycles

LT EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST. R & R BATTERY IAW AMM.

Part: ATTACH BRACKET — CRACKED (FUSELAGE) · airframe 50,495 hrs · 29,380 cycles

KEEL BEAM PANEL 192E FWD LT ATTACH BRACKET CRACKED. R & R BRACKET IAW SRM.

Part: LENS — MISSING (CABIN) · airframe 49,552 hrs · 28,806 cycles

LT OVERWING EMERGENCY EXIT COVER MISSING AT ROW 11. INSTALLED LENS IAW MM.

Part: CHANNEL — BROKEN (RT WING) · airframe 48,316 hrs · 28,081 cycles

RT WING AT PYLON FIXED UPPER T/E PANEL SUPPORT CHANNEL BROKEN. R & R SUPPORT CHANNEL IAW SRM.

Part: SUPPORT ANGLE — CRACKED (RT MLG WW) · airframe 48,316 hrs · 28,081 cycles

RIGHT MLG WHEEL WELL VAPOR BARRIER UPPER SUPPORT ANGLE CRACKED AT FASTENER HOLE. REPAIRED ANGLE IAW EA.

Part: LENS — BROKEN (CABIN) · airframe 46,745 hrs · 27,143 cycles

EMERGENCY EXIT LIGHT LENS BROKEN AT L-1 DOOR. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSY AT FWD ENTRY DOOR NEAR GALLEY FLOOR, NEXT TO F/A SEAT PER AMM.

Part: GCU — FAULTY (NR 2 ENGINE) · airframe 46,633 hrs · 27,073 cycles

2 ENGINE GENERATOR DRIVE LIGHT ILLUMINATED, ACRID SMELL PRESENT IN CABIN AND COCKPIT. REPLACED UNIT PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 45,939 hrs · 26,652 cycles

R2 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT IAW M/M.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 45,290 hrs · 26,223 cycles

RIGHT OVERWING EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER M/M.

Part: FASTENER — LOOSE (L1 DOOR) · airframe 44,981 hrs · 26,040 cycles

L1 DOOR EMERGENCY EVAC SLIDE CONTAINER GIRT BAR HOOK RIGHT LOOSE. SECURED FASTENERS ASSY PER SRM.

Part: FASTENER — LOOSE (L1 DOOR) · airframe 44,981 hrs · 26,040 cycles

L1 DOOR EMERGENCY EVAC SLIDE CONTAINER GIRT BAR HOOK LOOSE. REMOVED AND REPLACED FASTENER ASSY PER SRM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 44,674 hrs · 25,869 cycles

LEFT EEPLS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SIGN — DAMAGED (CABIN) · airframe 44,148 hrs · 25,560 cycles

EMERGENCY EXIT SIGN ASSEMBLY ON AFT LAV DAMAGED. REMOVED AND REPLACED SIGN IAW AMM.

Part: CONNECTOR — UNSECURE (CABIN) · airframe 44,148 hrs · 25,560 cycles

LEFT OVERWING EMERGENCY EXIT SIGN INOP. SECURED CONNECTOR IAW AMM & WDM.

Part: LIGHT — DAMAGED (CABIN) · airframe 44,148 hrs · 25,560 cycles

EMERGENCY EXIT LIGHT ASSEMBLY DAMAGED ON FORWARD LAVATORY. REMOVED AND REPLACED LIGHT ASSY IAW AMM.

Part: LIGHT — DAMAGED (CABIN) · airframe 44,148 hrs · 25,560 cycles

EMERGENCY EXIT LIGHT ASSEMBLY DAMAGED. REMOVED AND REPLACED LIGHT ASSY IAW AMM.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 44,148 hrs · 25,560 cycles

RT MAIN LANDING GEAR BULKHEAD SUPPORT BRACKET CRACKED AT BS 663, RBL 14. REMOVED AND REPLACED BRACKET IAW SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 44,148 hrs · 25,560 cycles

PASSENGER CABIN FLOOR WEB CRACKED AT BS 1015, LBL 39. REPAIRED WEB IAW SRM AMM.

Part: SUPPORT BRACKET — CRACKED (LT MLG WW) · airframe 44,148 hrs · 25,560 cycles

LEFT WHEEL WELL BULKHEAD SUPPORT BRACKET IS CRACKED AT BS 663, LBL 26. REMOVED AND REPLACED BRACKET IAW SRM & MM.

Part: SEAT TRACK — WORN (FUSELAGE) · airframe 44,148 hrs · 25,560 cycles

SEAT TRACK WORN AT BS 500D + 10, RBL 24. REPAIRED TRACK PER EA.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 44,148 hrs · 25,560 cycles

BULKHEAD ANGLE CRACKED AT BS 663, RBL 8. REPAIRED ANGLE IAW SRM AND BOEING DWG.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 44,148 hrs · 25,560 cycles

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

Part: BATTERY — FAILED (CABIN) · airframe 44,073 hrs · 25,521 cycles

LT EMERGENCY BATTERY PACKS FAILED CAPACITY CHECK. REMOVED AND REPLACED BATTERIES PER MM.

Part: BATTERY — FAILED (CABIN) · airframe 44,073 hrs · 25,521 cycles

RT EMERGENCY BATTERY PACKS FAILED CAPACITY CHECK. REMOVED AND REPLACED BATTERIES PER MM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 44,073 hrs · 25,521 cycles

LEFT FWD EMERGENCY LIGHT BATTERY CHARGER INOP. REMOVED AND REPLACED CHARGER PER MM

Part: BATTERY PACK — FAILED (CABIN) · airframe 41,803 hrs · 24,221 cycles

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

Part: BATTERY PACK — FAILED (CABIN) · airframe 41,803 hrs · 24,221 cycles

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

Part: BATTERY PACK — FAILED (CABIN) · airframe 41,803 hrs · 24,221 cycles

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

Part: SLIDE — LOOSE (R2 DOOR) · airframe 39,214 hrs · 22,773 cycles

R2 DOOR EMERGENCY EVAC SLIDE LOOSE. SECURED SLIDE PER MT.

Part: RIVET — BROKEN (GIRT BAR HOOK) · airframe 37,058 hrs · 21,508 cycles

DURING SCHEDULED HC1 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR HOOK RIVET BROKEN. REMOVED AND REPLACED HOOK ASSY PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 37,033 hrs · 21,487 cycles

DURING SCHEDULED 10Y CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT PER MM.

Part: SLIDE — LOW PRESSURE (R2 DOOR) · airframe 36,004 hrs · 20,852 cycles

DURING SCHEDULED MV3 CHECK, FOUND R2 DOOR EVAC SLIDE PRESSURE IND OUT OF LIMITS. REMOVED AND REPLACED SLIDE ASSY PER MT.

Part: SUPPORT FITTING — CORRODED (LT MLG TRUNNION) · airframe 35,095 hrs · 20,249 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT MLG FWD TRUNNION SUPPORT FITTING, LUG FACES CORRODED. REMOVED AND REPLACED FITTING PER SWA EA.

Part: SUPPORT FITTING — CORRODED (RT MLG TRUNNION) · airframe 35,095 hrs · 20,249 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT MLG FWD TRUNNION SUPPORT FITTING, LUG FACES CORRODED. REMOVED AND REPLACED FITTING PER SWA EA.

Part: BATTERY PACK — FAILED (CABIN) · airframe 32,659 hrs · 18,776 cycles

DURING SCHEDULED HC1 CHECK, AFT RT EMERGENCY EXIT LIGHT BATTERY PACK FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 32,659 hrs · 18,776 cycles

DURING SCHEDULED HC1 CHECK, FOUND R1 DOOR SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MT.

Part: BATTERY PACK — FAILED (CABIN) · airframe 32,659 hrs · 18,776 cycles

DURING SCHEDULED HC1 CHECK, FWD LT EMERGENCY EXIT LIGHT BATTERY PACK FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 30,240 hrs · 17,339 cycles

DURING SCHEDULED 8Y CHECK, FOUND AFT PRESSURE BULKHEAD WEB CORRODED AT BS 1016, RBL 4 TO RBL 13. REPAIRED WEB PER ER.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 30,227 hrs · 17,333 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM UPPER CHORD CORRODED AT BS 986, LBL 5 TO RBL 40. REPAIRED CHORD PER SWA EA.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 30,227 hrs · 17,333 cycles

DURING SCHEDULED 8Y CHECK, FOUND LT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 128. REPAIRED SKIN PER SRM.

Part: SLIDE — UNSERVICEABLE (L2 DOOR) · airframe 29,691 hrs · 17,004 cycles

DURING SCHEDULED MV1 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE PRESSURE GAUGE INDICATED OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE PER MM.

Part: LENS — MISSING (CABIN) · airframe 26,749 hrs · 15,210 cycles

DURING SCHEDULED CV CHECK, FOUND FWD CABIN EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM.

Part: BLADE — DAMAGED (NR 2 ENGINE) · airframe 25,635 hrs · 14,390 cycles

INFLIGHT SHUT DOWN / DECLARED EMERGENCY / DIVERSION. DURING CLIMB NR 2 COMPRESSOR STALLED, SHUT DOWN NR 2 ENGINE PER QRH. FOUND DAMAGED COMPRESSOR BLADES. REMOVED AND REPLACED NR 2 ENGINE PER MM AND MT.

Part: BATTERY — FAILED (EMERGENCY LIGHT) · airframe 23,009 hrs · 13,065 cycles

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

Part: GLOWSTRIP — CRACKED (ROW 15-17 DEF) · airframe 20,640 hrs · 11,714 cycles

DURING SCHEDULED MV2 CHECK, FOUND PHOTOLUMINESCENT STRIP CRACKED BETWEEN ROW 15 DEF TO ROW 17 DEF. REMOVED AND REPLACED PHOTOLUMINESCENT STRIP PER MM.

Part: BULKHEAD — ACTIVATED (FUSELAGE) · airframe 13,374 hrs · 7,625 cycles

DURING SCHEDULED C4 CHECK, FOUND AFT PRESS BULKHEAD BS 1016 OIL CANNED AT STR 16. REPAIRED BULKHEAD PER SWA EA.

Part: SLIDE — OUT OF ADJUST (AFT ENTRY DOOR) · airframe 11,004 hrs · 6,318 cycles

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

Part: BUSHING — WORN (ELEVATOR TAB) · airframe 9,648 hrs · 5,556 cycles

DURING SCHEDULED PM CHECK, SWA SI 11038-55, FOUND LT ELEVATOR TAB BUSHINGS WORN AT HINGE ATTACH POINTS NR 2, NR 3 AND NR 4. REMOVED AND REPLACED LT ELEVATOR TAB PER MM.

Part: BUSHING — WORN (ELEVATOR TAB) · airframe 9,648 hrs · 5,556 cycles

DURING SCHEDULED PM CHECK, SWA SI 11038-55, FOUND RT ELEVATOR TAB BUSHINGS WORN AT HINGE ATTACH POINTS NR 2, NR 3 AND NR 4. REMOVED AND REPLACED RT ELEVATOR TAB PER MM.

Part: BUSHING — WORN (LT ELEVATOR) · airframe 8,822 hrs · 5,107 cycles

DURING SCHEDULED C4 CHECK, SWA SI 11038-55, FOUND LT ELEVATOR TAB HINGE ATTACH POINTS NR 2, NR 3 AND NR 4 WORN. REMOVED AND REPLACED HARDWARE AND BUSHINGS PER MM.

Part: BUSHING — WORN (RT ELEVATOR) · airframe 8,822 hrs · 5,107 cycles

DURING SCHEDULED C4 CHECK, SWA SI 11038-55, FOUND RT ELEVATOR TAB HINGE POINT NR 2 WORN. REMOVED AND REPLACED HARDWARE AND BUSHING PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 8,493 hrs · 4,878 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EEPLS FWD END CAP BROKEN AND LIGHT INOP. REMOVED AND REPLACED END CAP AND RELAMPED LIGHT PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 5,652 hrs · 3,251 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FWD ENTRY DOOR LOWER EXTERIOR EMERGENCY LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: LENS — CRACKED (CABIN) · airframe 338 hrs · 197 cycles

DURING SCHEDULED SERVICE CHECK, FOUND RT OVERWING EXTERNAL EMERGENCY EXIT LIGHT LENS CRACKED. REMOVED AND REPLACED LENS PER MM.