N916WN

Part: TRUNNION — CORRODED (RT MLG) · airframe 42,672 hrs · 25,625 cycles

R/H MLG FWD TRUNNION SUPPORT FITTING UPPER I/B LUG BORE HAS EVIDENCE OF CORROSION. / REMOVED CORROSION PER EA 1-A57-3246 REV 11 STEP 8.

Part: TRUNNION — CORRODED (RT MLG) · airframe 42,672 hrs · 25,625 cycles

R/H MLG FWD TRUNNION SUPPORT FITTING UPPER O/B LUG BORE HAS EVIDENCE OF CORROSION. / REMOVED CORROSION PER EA 1-A57-3246 REV 11 STEP 8.

Part: BALLAST — INOPERATIVE (EMERGENCY LIGHT) · airframe 42,503 hrs · 25,536 cycles

SIDE WALL LIGHT, LEFT SIDE OVER-WING EXIT INOPERATIVE. DMA 0425300. R & R EMERGENCY LIGHT BALLAST, PER AMM 33-21-00 C NR 58667.

Part: FLASHLIGHT — MISSING (CABIN) · airframe 40,535 hrs · 24,290 cycles

AFT GALLEY EMERGENCY FLASHLIGHT ASSEMBLIES MISSING. / INSTALLED NEW EMERGENCY FLASHLIGHT ASSEMBLIES IN THE AFT GALLEY I.A.W CMM 25-60-02.

Part: FLASHLIGHT — MISSING (CABIN) · airframe 40,534 hrs · 24,290 cycles

AFT GALLEY EMERGENCY FLASHLIGHT ASSEMBLIES MISSING. / INSTALLED FLASHLIGHT ASSEMBLIES IAW CMM.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 40,535 hrs · 24,290 cycles

FWD ENTRY DOOR EMERGENCY LIGHT IS INOP. / REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY PER AMM 33-51-06

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 40,534 hrs · 24,290 cycles

FORWARD ENTRY DOOR EMERGENCY LIGHT INOP. / R&R POWER SUPPLY PER AMM.

Part: FLOORBEAM — DAMAGED (BS 540) · airframe 40,534 hrs · 24,290 cycles

CABIN FLOOR STRUCTURE BREAKAWAY INTERCOSTAL BROKEN AT BS. 540, BETWEEN RBL 24 TO RBL 45. / R&R INTERCOSTAL PER SRM.

Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 40,534 hrs · 24,290 cycles

L/H HORIZONTAL STABILIZER RIB #5 STA. 129.5 CRACKED ON VERTICAL STIFFENER FIRST HOLE PAST #2 STIFFENER LOWER SIDE. / REPAIRED STIFFENER PER SRM.

Part: FLOOR SUPPORT — CRACKED (BS 500D-520) · airframe 40,534 hrs · 24,290 cycles

PASSENGER CABIN FLOOR STRUCTURE INTERCOSTAL CRACKED AT UPPER SURFACE BETWEEN BS. 500D TO BS. 520, BL 0. / R&R INTERCOSTAL PER SRM.

Part: FLOOR SUPPORT — CRACKED (BS 380-400) · airframe 40,534 hrs · 24,290 cycles

INTERCOSTAL CRACKED AT UPPER SURFACE BETWEEN BS. 380 TO BS. 400, BL 0. / R&R INTERCOSTAL ANGLE PER SRM.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 40,534 hrs · 24,290 cycles

L/H HORIZONTAL STABILIZER #5 RIB STAB. STA. 129.5 CRACKED ON VERTICAL STIFFENER #4 FROM FORWARD END. / R&R RIB PER SRM.

Part: FITTING — CRACKED (BS 947) · airframe 40,534 hrs · 24,290 cycles

AFT CARGO AFT BULKHEAD LOWER FITTING CRACKED AT BS. 947, LBL 10. / R&R FITTING PER SRM.

Part: FLOOR SUPPORT — CRACKED (BS 540) · airframe 40,534 hrs · 24,290 cycles

PASSENGER CABIN FLOOR STRUCTURE INTERCOSTAL CRACKED AT BS. 540, RBL 1. / R&R INTERCOSTAL PER SRM.

Part: HANDLE — LOOSE (L1 DOOR) · airframe 40,534 hrs · 24,290 cycles

FORWARD ENTRY DOOR BOTH DOOR CLOSING ASSIST HANDLES LOOSE. / SECURED HANDLES PER AMM.

Part: INTERCOSTAL — CRACKED (BS 847-867) · airframe 40,534 hrs · 24,290 cycles

AFT CARGO CEILING INTERCOSTAL CRACKED BETWEEN CABIN FLOOR BEAMS BETWEEN BS. 847 TO BS. 867, LBL 20. / R&R INTERCOSTAL PER SRM.

Part: BEAM — CRACKED (R1 DOOR) · airframe 40,534 hrs · 24,290 cycles

R1 DOOR #4 UPPER BEAM OUTBOARD AFT HOLE CRACKED. / R&R R1 DOOR PER AMM.

Part: WEB — CORRODED (CARGO BAY) · airframe 40,534 hrs · 24,290 cycles

AFT CARGO WEB INBOARD OF CARGO DOOR BELOW SCUFF PLATE CORRODED MULTIPLE LOCATIONS. / R&R WEB PER SRM.

Part: FLOORBEAM — CORRODED (BS 987) · airframe 40,534 hrs · 24,290 cycles

FLOOR BEAM IN AND AROUND FASTENER HOLE CORRODED AT BS. 987, RBL 43. / REPAIRED FLOOR BEAM PER EA.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 40,534 hrs · 24,290 cycles

L/H HORIZONTAL STABILIZER #5 RIB STAB. STA. 129.5 CRACKED ON VERTICAL STIFFENER #3 FROM FORWARD END. / R&R RIB PER SRM.

Part: ANGLE — CORRODED (BS 927-990) · airframe 40,534 hrs · 24,290 cycles

R/H Z ANGLE CORRODED ON SURFACE BETWEEN BS. 927 TO BS. 990. / REPAIRED Z ANGLE PER SRM.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 40,534 hrs · 24,290 cycles

R/H HORIZONTAL STABILIZER #4 INSPAR RIB CRACKED 1 EACH AT STIFFENERS 2, 3, AND 4. / R&R #4 INSPAR RIB PER SRM.

Part: ANGLE — CORRODED (THRESHOLD) · airframe 40,534 hrs · 24,290 cycles

AFT GALLEY DOOR THRESHOLD Z ANGLE CORRODED. / R&R Z ANGLE PER SRM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 40,534 hrs · 24,290 cycles

L/H OVER WING DOOR LOWER EMERGENCY EXIT SIGN NEEDED RE-LAMPING. / RELAMPED SIGN PER AMM.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 40,534 hrs · 24,290 cycles

EMERGENCY LIGHT PACK M1675 WOULD NOT HOLD CHARGE FOR FIFTEEN MINUTES. / R&R LIGHT PACK PER AMM.

Part: FITTING — UNSECURE (ELEVATOR) · airframe 39,661 hrs · 23,689 cycles

FLIGHT ATTENDANTS REPORTED SMOKE SMELL IN MIDDLE PART OF CABIN. DID NOT SEE VISIBLE SIGNS OF SMOKE OR FIRE. DIVERTED OUT OF ABUNDANCE OF CAUTION. FOUND HEAVY HYDRAULIC LEAK & FOGGING AT ELEVATOR FEEL COMPUTER B PRESSURE LINE. SECURED FITTING PER AMM.

Part: BRACKET — TIGHT (L1 DOOR) · airframe 38,774 hrs · 23,093 cycles

L1 DOOR GIRT BAR HOLDER WAS TOO TIGHT. LOOSENED GIRT BRACKET PER SIP.

Part: WIRE HARNESS — FAULTY (NR 2 ENGINE) · airframe 36,561 hrs · 21,687 cycles

DIVERSION, RT ENGINE OVERHEAT PASSING FL 280. RED BOX AND INDICATOR SHOWED (+70) LEVELED OFF AT FL290. R&R NR 2 ENGINE EGT J10 HARNESS PER AMM.

Part: STRAP — MISSING (R2 DOOR) · airframe 36,221 hrs · 21,463 cycles

R2 DOOR SAFETY STRAP MISSING SNAP. R&R STRAP PER AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 35,108 hrs · 20,768 cycles

RT OVERWING EMERGENCY EXIT LIGHT INOP. R&R BATTERY PACK ASSEMBLY PER AMM.

Part: FITTING — CORRODED (LT MLG) · airframe 34,672 hrs · 20,499 cycles

LEFT MAIN LANDING GEAR FORWARD TRUNNION SUPPORT LUG FACE FITTING CORRODED. REPAIRED TH EFITTING IAW EA.

Part: FITTING — CORRODED (RT MLG) · airframe 34,672 hrs · 20,499 cycles

RIGHT MAIN LANDING GEAR FORWARD TRUNNION SUPPORT LUG FACE FITTING CORRODED. REPAIRED THE FITTING IAW EA.

Part: BATTERY PACK — FAILED (CABIN) · airframe 34,209 hrs · 20,215 cycles

EMERGENCY LIGHT BATTERY PACK FAILED CAPACITY CHECK AT POSITION M01673. R&R BATTERY PACK PER AMM AND DWG.

Part: BATTERY PACK — FAILED (CABIN) · airframe 34,209 hrs · 20,215 cycles

EMERGENCY LIGHT BATTERY PACK FAILED CAPACITY CHECK AT POSITION M01670. R&R BATTERY PACK PER AMM AND DWG.

Part: BATTERY PACK — FAILED (CABIN) · airframe 34,209 hrs · 20,215 cycles

EMERGENCY LIGHT BATTERY PACK FAILED CAPACITY CHECK AT POSITION M01672. R&R BATTERY PACK PER AMM AND DWG.

Part: LIGHT — LOOSE (CABIN) · airframe 34,209 hrs · 20,215 cycles

CENTER AISLE OVERHEAD EMERGENCY EXIT LIGHT ASSEMBLY LOOSE. SECURED LIGHT ASSEMBLY PER MM.

Part: SIGN — LOOSE (CABIN) · airframe 34,204 hrs · 20,211 cycles

OVERHEAD EMERGENCY EXIT SIGN LIGHT LOOSE IN MIDDLE OF CABIN. SECURED LIGHT PER AMM.

Part: ANGLE — CORRODED (BS 727D-787) · airframe 34,170 hrs · 20,190 cycles

AFT CARGO LEFT ZEE ANGLE CORRODED BETWEEN BS 727D TO 787. REPAIRED THE ANGLE SECTION IAW SRM.

Part: ANGLE — CORRODED (BS 727D-767) · airframe 34,170 hrs · 20,190 cycles

AFT CARGO RIGHT ZEE ANGLE CORRODED BETWEEN BS 727D TO 767. REPAIRED THE ANGLE IAW SRM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 34,170 hrs · 20,190 cycles

L1 DOOR SLIDE OUT OF POSITION. REPOSITIONED THE SLIDE IAW MT.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 34,170 hrs · 20,190 cycles

LT OVERWING EXIT SIGN SIDEWALL LIGHT INOP. R&R LIGHT IAW AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 33,390 hrs · 19,708 cycles

R1 DOOR EMERGENCY LIGHT INOP BETWEEN ROW 3 TO ROW 6. R&R BATTERY PACK IAW MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 33,390 hrs · 19,708 cycles

RT EMERGENCY LIGHT INOP BETWEEN ROW 3 TO ROW 6. R&R BATTERY PACK IAW MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 33,026 hrs · 19,475 cycles

LEFT EMERGENCY EXIT SIDEWALL LIGHT INOPERATIVE. REPLACED THE LAMPS IAW MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 33,026 hrs · 19,475 cycles

RIGHT EMERGENCY EXIT SIDEWALL LIGHT INOPERATIVE. REPLACED THE LAMPS IAW MM.

Part: COVER — BROKEN (EXTERIOR LIGHT) · airframe 32,473 hrs · 19,141 cycles

R1 DOOR EXTERIOR EMERGENCY LIGHT LENS COVER BROKEN. R&R COVER PER AMM.

Part: SIGN — BROKEN (CABIN) · airframe 32,205 hrs · 18,993 cycles

R2 DOOR EXIT SIGN BROKEN. R&R SIGN PER MM.

Part: COVER — MISSING (RT OVERWING DOOR) · airframe 31,894 hrs · 18,812 cycles

RIGHT OVERWING EMERGENCY DOOR STRAP COVER MISSING. REPLACED THE COVER IAW SIP.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 31,339 hrs · 18,495 cycles

R1 DOOR SLIDE OUT OF ADJUST. ADJUSTED THE SLIDE IAW AMM.

Part: SIGN — LOOSE (CABIN) · airframe 30,304 hrs · 17,880 cycles

OVERWING OVERHEAD EXIT SIGN LOOSE. R&R LIGHT ASSEMBLY PER SIP.

Part: GLOWSTRIP — DAMAGED (ROW 24) · airframe 29,796 hrs · 17,587 cycles

LEFT GLOWSTRIP DAMAGED AT ROW 24. R & R THE GLOWSTRIP IAW AMM.

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 29,796 hrs · 17,587 cycles

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

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 29,796 hrs · 17,587 cycles

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

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 29,796 hrs · 17,587 cycles

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

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 29,796 hrs · 17,587 cycles

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

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 29,796 hrs · 17,587 cycles

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

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 29,796 hrs · 17,587 cycles

EMERGENCY LIGHT BATTERY FAILED THE CAPACITY TEST8. R & R THE BATTERY IAW AMM.

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 29,796 hrs · 17,587 cycles

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

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 28,041 hrs · 16,577 cycles

AFT CARGO SUPPORT ANGLE CRACKED, AT BS 867, LBL 10. R & R ANGLE IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 28,041 hrs · 16,577 cycles

FLOORBEAM CORRODED AT BS 986.5, LBL 43. REPAIRED BEAM IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 28,041 hrs · 16,577 cycles

INTERCOSTAL CRACKED AT BS 317, RBL 31. R & R INTERCOSTAL IAW SRM.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · airframe 28,041 hrs · 16,577 cycles

FORWARD GALLEY DOOR LOWER SILL THRESHOLD ATTACH ANGLE CORRODED, BETWEEN BS 300 - 320. R & R ANGLE IAW SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 28,041 hrs · 16,577 cycles

FORWARD GALLEY ENTRY DOOR Z ANGLE CORRODED. REPAIRED Z ANGLE IAW EA.

Part: SKIN — CHAFED (FUSELAGE) · airframe 28,041 hrs · 16,577 cycles

FUSELAGE SKIN CHAFED, BETWEEN BS 850 - 856, BETWEEN RBL 2 TO LBL 2. REPAIRED SKIN IAW EA.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 28,041 hrs · 16,577 cycles

FORWARD CARGO THRESHOLD WEB SURFACE CORRODED, BETWEEN BS 440 - 485. REPAIRED WEB IAW SRM.

Part: PRESSURE DECK — CRACKED (RT MLG WW) · airframe 27,660 hrs · 16,352 cycles

VERTICAL PRESS DECK WEB CRACKED AT BS 663, RBL 45.0. REPAIRED WEB IAW EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,288 hrs · 16,130 cycles

LEFT AFT EMER SLIDE LIGHT INOPERATIVE. RELAMPED LIGHT IAW AMM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 27,288 hrs · 16,130 cycles

RIGHT AFT EMER SLIDE LIGHT INOPERATIVE. RELAMPED LIGHT IAW AMM.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 27,288 hrs · 16,130 cycles

SKIN DOUBLER CRACKED AT THE AFT SIDE OF THE EXTERNAL POWER DOOR NR 114R CUT OUT. REPAIRED SKIN IAW SRM.

Part: COVER — BROKEN (EXIT SIGN) · airframe 25,972 hrs · 15,383 cycles

RIGHT LOWER FWD OVERWING EMER EXIT SIGN COVER BROKEN. R & R SIGN ASSEMBLY IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,453 hrs · 15,101 cycles

RIGHT EMER EXIT SIDEWALL LIGHT INOPERATIVE. R & R LIGHT ASSEMBLY IAW MM.

Part: RETAINING CLIP — LOOSE (R1 DOOR) · airframe 25,413 hrs · 15,080 cycles

R1 DOOR EMER EVAC SLIDE GIRT BAR RETAINING CLIP LOOSE. SECURED CLIP IAW SIP.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 25,182 hrs · 14,952 cycles

R1 DOOR EXTERIOR EMER LIGHT INOPERATIVE. RELAMPED LIGHT IAW AMM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 25,182 hrs · 14,952 cycles

R2 DOOR EXTERIOR EMER LIGHT INOPERATIVE. RELAMPED LIGHT IAW AMM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 25,182 hrs · 14,952 cycles

L2 DOOR EXTERIOR EMER LIGHT INOPERATIVE. RELAMPED LIGHT IAW AMM.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 24,574 hrs · 14,605 cycles

FORWARD OTBD HOLE SEAT TRACK CRACKED AT BS 727B, LBL 24.5. REPAIRED SEAT TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 24,574 hrs · 14,605 cycles

AFT INBD & FWD OTBD HOLE SEAT TRACK CRACKED AT BS 727B, RBL 45.5. REPAIRED SEAT TRACK IAW EA & ACO.

Part: COVER — MISSING (CABIN) · airframe 22,456 hrs · 13,378 cycles

LEFT OVERWING EMER EXIT LIGHT COVER MISSING. INSTALLED COVER IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,661 hrs · 12,932 cycles

R1 DOOR EMERGENCY EXIT LIGHT INOPERATIVE. R & R BULB IAW AMM.

Part: FAIRING — CRACKED (TE FLAP) · airframe 21,446 hrs · 12,807 cycles

LEFT WING TE FLAP NR 3 AFT FAIRING FWD OTBD CORNER CRACKED AT EDGE. REPAIRED FAIRING IAW EA.

Part: STIFFENER — CRACKED (RT HORIZ STAB) · airframe 21,446 hrs · 12,807 cycles

RIGHT HORIZONTAL STABILIZER STATION 129.5 RIB VERTICAL STIFFENER CRACKED AT AFT OF FRONT SPAR. REPAIRED STIFFENER IAW SRM.

Part: ANGLE — CORRODED (BS 747-787) · airframe 21,446 hrs · 12,807 cycles

LEFT ZEE ANGLE CORRODED BETWEEN BS 747 TO 787, LBL 22. R & R ZEE ANGLE IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 21,446 hrs · 12,807 cycles

AFT CARGO COMPARTMENT LT Z ANGLE CORRODED BETWEEN BS 787 TO BS 827, LBL 22. REPAIRED Z ANGLE IAW SRM.

Part: ANGLE — CORRODED (BS 727C-727D) · airframe 21,446 hrs · 12,807 cycles

LEFT ZEE ANGLE CORRODED BETWEEN BS 727C TO 727D, LBL 22. R & R ZEE ANGLE IAW SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 21,446 hrs · 12,807 cycles

Z ANGLE CORRODED BETWEEN BS 747 TO BS 767, RBL 22. R & R Z ANGLE IAW SRM.

Part: ANGLE — CORRODED (BS 727D-747) · airframe 21,446 hrs · 12,807 cycles

LEFT ZEE ANGLE CORRODED BETWEEN BS 727D TO 747, LBL 22. R & R ZEE ANGLE IAW SRM.

Part: WINDOW FRAME — CRACKED (COCKPIT) · airframe 21,446 hrs · 12,807 cycles

LEFT NR 1 FLIGHT DECK WINDOW FRAME CUT OUT CRACKED. REPAIRED FRAME IAW EA.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 21,446 hrs · 12,807 cycles

RIGHT HORIZONTAL STABILIZER STATION 120.30 RIB LOWER SURFACE OTBD FASTENER HOLE CRACKED 7 INCHES AFT OF FRONT SPAR. REPAIRED RIB IAW EA.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 21,446 hrs · 12,807 cycles

FLOOR SUPPORT RAIL CORRODED AT BS 747, RBL 13. R & R SUPPORT IAW SRM.

Part: PANEL — CRACKED (FUSELAGE) · airframe 21,446 hrs · 12,807 cycles

FLOOR SUPPORT PANEL CRACKED AT BS 540, RBL 1. R & R PANEL IAW SRM & DWG.

Part: BULKHEAD — CRACKED (BS 663) · airframe 21,446 hrs · 12,807 cycles

MLG WW SPAR VERTICAL PRESSURE WEB CRACKED AT BS 663, LBL 42. REPAIRED WEB IAW SRM.

Part: WINDOW FRAME — CRACKED (NR 1 WINDOW) · airframe 21,446 hrs · 12,807 cycles

LEFT NR 1 WINDOW FRAME OTBD UPPER CORNER CRACKED. REPAIRED WINDOW FRAME IAW ACO.

Part: BATTERY PACK — FAILED (CABIN) · airframe 21,109 hrs · 12,589 cycles

FWD EMERGENCY EXIT LIGHT BATTERY PACK FAILED CAPACITY TEST. R & R BATTERY PACK IAW MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 21,109 hrs · 12,589 cycles

AFT EMERGENCY EXIT LIGHT BATTERY PACK FAILED CAPACITY TEST. R & R BATTERY PACK IAW MM.

Part: SKIN — CRACKED (TAILCONE) · airframe 18,998 hrs · 11,387 cycles

APU TAIL CONE SKIN CRACKED ON UPPER LT SIDE. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 18,909 hrs · 11,331 cycles

RT HORIZONTAL LOWER SKIN CRACKED AT STAB BS 138.70, 9" FWD OF AFT SPAR 7TH RIB O/B FROM FUSELAGE. REPAIRED SKIN IAW SRM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 18,850 hrs · 11,296 cycles

L1 DOOR EMERGENCY EVAC SLIDE PACK FELL OUT OF COMPARTMENT, DID NOT DEPLOY, STILL OPERATIONAL. REINSTALLED SLIDE IAW MT.

Part: LIGHT — DAMAGED (CABIN) · airframe 18,850 hrs · 11,296 cycles

EMERGENCY EXIT LIGHT ASSEMBLY AT OVERWING CEILING AISLE DAMAGED. R&R LIGHT ASSEMBLY IAW AMM.

Part: SIGN — UNSECURE (CABIN) · airframe 18,051 hrs · 10,825 cycles

OVERWING EMERGENCY EXIT SIGN FELL OFF. REMOVED AND REPLACED SIGN PER MM.

Part: COFFEEMAKER — MALFUNCTIONED (GALLEY) · airframe 17,892 hrs · 10,727 cycles

DIVERSION -- LOUD BANG IN AF GALLEY WITH WHITE SMOKE. REMOVED AND REPLACED COFFEEMAKERS PER MM.

Part: SIGN — BROKEN (CABIN) · airframe 16,356 hrs · 9,830 cycles

OVERHEAD EMERGENCY EXIT ROW SIGN BROKEN. REMOVED AND REPLACED SIGN PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,004 hrs · 9,601 cycles

MAIN CABIN FWD FLOOR EMERGENCY LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: LENS — MISSING (CABIN) · airframe 16,004 hrs · 9,601 cycles

MAIN CABIN FWD FLOOR EMERGENCY LENS MISSING. INSTALLED LENS PER MM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 15,369 hrs · 9,215 cycles

L2 DOOR SLIDE HANGING LOW. ADJUSTED SLIDE IAW MM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 15,307 hrs · 9,175 cycles

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

Part: COVER — MISSING (CABIN) · airframe 14,924 hrs · 8,951 cycles

EEPLS COVER MISSING AT ROW 11. INSTALLED COVER PER MM.

Part: LENS — BROKEN (CABIN) · airframe 14,345 hrs · 8,617 cycles

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

Part: LENS — CRACKED (CABIN) · airframe 14,064 hrs · 8,465 cycles

EMERGENCY FLOOR LIGHTING LENS CRACKED AT ROW 6. REMOVED AND REPLACED LENS PER AMM.

Part: LENS — MISSING (CABIN) · airframe 13,453 hrs · 8,100 cycles

DURING SCHEDULED MV2 CHECK, FOUND FLOOR PROXIMITY LIGHT LENS COVER MISSING. INSTALLED NEW LENS COVER PER MM.

Part: FITTING — LOOSE (GIRT BAR) · airframe 12,965 hrs · 7,799 cycles

DURING SCHEDULED CV CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE GIRT BAR FITTINGS LOOSE. SECURED FITTINGS PER MM.

Part: CAP — MISSING (CABIN) · airframe 12,965 hrs · 7,799 cycles

DURING SCHEDULED CV CHECK, FOUND FWD EEPLS END CAP MISSING. INSTALLED END CAP PER MM.

Part: COVER — CRACKED (CABIN) · airframe 12,965 hrs · 7,799 cycles

DURING SCHEDULED CV CHECK, FOUND LT EEPLS COVER CRACKED BETWEEN ROW 1 TO ROW 10. REMOVED AND REPLACED COVER PER MM.

Part: COVER — CRACKED (CABIN) · airframe 12,965 hrs · 7,799 cycles

DURING SCHEDULED CV CHECK, FOUND LT EEPLS COVER CRACKED AT ROW 11. REMOVED AND REPLACED COVER PER MM.

Part: LIGHT — MISSING (CABIN) · airframe 11,267 hrs · 6,805 cycles

DURING SCHEDULED MV1 CHECK FOUND, OVERWING EMERGENCY EXIT LIGHT COVER MISSING. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 11,186 hrs · 6,754 cycles

R2 DOOR EMERGENCY EXIT LIGHT LOOSE. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: COVER — BROKEN (CABIN) · airframe 11,186 hrs · 6,754 cycles

LT EEPLS COVER BROKEN. REMOVED AND REPLACED EEPLS PER MM.

Part: CONNECTOR — DAMAGED (CABIN) · airframe 10,524 hrs · 6,382 cycles

FWD EEPLS INOP. FOUND WIRE BROKEN. REPAIRED CONNECTOR PER MM.

Part: LENS — MISSING (CABIN) · airframe 9,829 hrs · 5,964 cycles

EEPLS LENS MISSING AT ROW 9. INSTALLED LENS PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 9,829 hrs · 5,964 cycles

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

Part: COVER — MISSING (CABIN) · airframe 9,441 hrs · 5,748 cycles

LT OVERWING EEPLS COVER MISSING. INSTALLED COVER PER MM.

Part: LENS — MISSING (CABIN) · airframe 9,381 hrs · 5,707 cycles

OVERWING EEPLS LENS MISSING. INSTALLED LENS PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 9,312 hrs · 5,665 cycles

DURING SCHEDULED HC2 CHECK, RT EMERGENCY EXIT LIGHTS FAILED TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 9,312 hrs · 5,665 cycles

DURING SCHEDULED HC2 CHECK, LT EMERGENCY EXIT LIGHTS FAILED TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: COVER — MISSING (CABIN) · airframe 8,803 hrs · 5,360 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT EEPLS COVER MISSING AT ROW 11. REMOVED AND REPLACED COVER PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 7,830 hrs · 4,780 cycles

DURING SCHEDULED MV2 CHECK, FOUND L2 DOOR EMERGENCY ESCAPE SLIDE LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: COVER — CRACKED (CABIN) · airframe 6,164 hrs · 3,779 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT EEPLS COVER CRACKED AT ROW 8. REMOVED AND REPLACED COVER PER MM.

Part: LENS — MISSING (CABIN) · airframe 4,339 hrs · 2,630 cycles

DURING SCHEDULED MV2 CHECK, FOUND EEPLS LENS MISSING AT ROW 4. INSTALLED LENS PER MM

Part: LENS — LOOSE (CABIN) · airframe 4,015 hrs · 2,434 cycles

EEPLS LENS LOOSE AT FWD END. REMOVED AND REPLACED EEPLS LENS PER MM.

Part: LENS — MISSING (CABIN) · airframe 3,942 hrs · 2,390 cycles

EGRESS LIGHT LENS MISSING AT ROW 1. INSTALLED LENS PER MM.

Part: LENS — MISSING (CABIN) · airframe 3,828 hrs · 2,322 cycles

FWD EEPLS LIGHT LENS MISSING. INSTALLED LENS PER MM.

Part: COVER — MISSING (CABIN) · airframe 3,727 hrs · 2,261 cycles

EEPLS LIGHT COVER MISSING. INSTALLED COVER PER MM.

Part: LENS — DAMAGED (CABIN) · airframe 3,032 hrs · 1,836 cycles

L1 DOOR EEPLS LENS DAMAGED. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 1,132 hrs · 677 cycles

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

Part: WIRE — LOOSE (CABIN) · airframe 423 hrs · 276 cycles

DURING SCHEDULED MV2 CHECK, FOUND EEPLS INOP AT 5 ABC TO ROW 10 ABC. FOUND LOOSE WIRE AT LIGHT ASSY. SECURED LOOSE WIRE PER MM.