N708SW

Part: BATTERY — DISCHARGED (CABIN) · airframe 69,187 hrs · 41,375 cycles

LT OVERWING EMERGENCY EXIT LIGHTS INOP. R&R BATTERY PER AMM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 69,187 hrs · 41,375 cycles

LT OVERWING EXTERNAL EMERGENCY EXIT LIGHTS INOP. R&R BATTERY PER AMM.

Part: COVER — MISSING (R1 DOOR) · airframe 69,122 hrs · 41,332 cycles

R1 DOOR EMERGENCY EXIT LIGHT COVER MISSING RED ARROW ON COVER. R&R COVER PER AMM.

Part: COVER — MISSING (L1 DOOR) · airframe 69,122 hrs · 41,332 cycles

L1 DOOR EMERGENCY EXIT LIGHT COVER MISSING RED ARROW ON COVER. R&R COVER PER AMM.

Part: COVER — MISSING (R2 DOOR) · airframe 69,122 hrs · 41,332 cycles

R2 CABIN DOOR EMERGENCY LIGHT EXIT LENS COVERS MISSING DIRECTION ARROWS. R&R COVER PER AMM.

Part: COVER — MISSING (L2 DOOR) · airframe 69,122 hrs · 41,332 cycles

L2 CABIN DOOR EMERGENCY LIGHT EXIT LENS COVERS MISSING DIRECTION ARROWS. R&R COVER PER AMM.

Part: BOTTLE — FAULTY (AFT CARGO) · airframe 67,909 hrs · 40,586 cycles

CARGO FIRE BOTTLE DISCHARGE LIGHT ILLUMINATED IN FLIGHT FOR 10 MINUTES THEN EXTINGUISHED. AIR TURNBACK. R & R FIRE EXTINGUISHER BOTTLE IAW MM.

Part: CONTROL PANEL — FAULTY (FIRE EXTINGUISH) · airframe 67,909 hrs · 40,586 cycles

CARGO FIRE BOTTLE DISCHARGE LIGHT ILLUMINATED IN FLIGHT FOR 10 MINUTES THEN EXTINGUISHED. AIR TURNBACK. R & R THE CARGO FIRE CONTROL PANEL IAW MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 67,365 hrs · 40,250 cycles

LEFT OVERWING EXIT EXTERNAL EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMPS IAW AMM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 67,365 hrs · 40,250 cycles

CENTER AISLE MID CABIN OVERHEAD EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED THE LAMPS IAW AMM.

Part: PUMP — LEAKING (HYDRAULIC SYS) · airframe 67,287 hrs · 40,199 cycles

DECLARED EMERGENCY, MASTER CAUTION & HYDRAULIC LIGHT ILLUMINATED, DISCOVERED A SYSTEM ELECTRIC "LOW PRESS" LIGHT ILLUMINATED AND RAPIDLY DECREASING A SYSTEM QUANTITY. AFTER LANDING, FLUID DRIPPING FROM LEFT MAIN WHEEL WELL. R&R NR 1 ENGINE DRIVEN PUMP PER AMM.

Part: PUMP — LEAKING (HYDRAULIC SYS) · airframe 67,287 hrs · 40,199 cycles

DECLARED EMERGENCY, MASTER CAUTION & HYDRAULIC LIGHT ILLUMINATED, DISCOVERED A SYSTEM ELECTRIC "LOW PRESS" LIGHT ILLUMINATED AND RAPIDLY DECREASING A SYSTEM QUANTITY. AFTER LANDING, FLUID DRIPPING FROM LEFT MAIN WHEEL WELL. R&R NR 1 ELECTRIC HYDRAULIC PUMP PER AMM.

Part: RETAINER — OUT OF ADJUST (L2 GIRT BAR) · airframe 66,620 hrs · 39,784 cycles

L2 DOOR SLIDE GIRT BAR RETAINER OUT OF ADJUST. ADJUSTED THE RETAINER IAW SIP.

Part: STRAP — BROKEN (FLASHLIGHT) · airframe 66,510 hrs · 39,717 cycles

AFT FLASHLIGHT STRAP BROKEN. R & R THE STRAP IAW AMM.

Part: FITTING — CORRODED (FUSELAGE) · airframe 66,169 hrs · 39,497 cycles

PRESSURE DOME RING Y-CHORD FITTING CORRODED AT BS 1016, STR 26L. R&R FITTING IAW SRM AND DWG.

Part: FITTING — CORRODED (FUSELAGE) · airframe 66,169 hrs · 39,497 cycles

PRESSURE DOME RING Y-CHORD FITTING CORRODED AT BS 1016, STR 20R. R&R FITTING IAW SRM AND DWG.

Part: FITTING — CORRODED (FUSELAGE) · airframe 66,169 hrs · 39,497 cycles

PRESSURE DOME RING Y-CHORD FITTING CORRODED AT BS 1016, STR 22R. R&R FITTING IAW SRM AND DWG.

Part: FITTING — CORRODED (FUSELAGE) · airframe 66,169 hrs · 39,497 cycles

PRESSURE DOME RING Y-CHORD FITTING CORRODED AT BS 1016, STR 21R. R&R FITTING IAW SRM AND DWG.

Part: FITTING — CORRODED (FUSELAGE) · airframe 66,169 hrs · 39,497 cycles

PRESSURE DOME RING Y-CHORD FITTING CORRODED AT BS 1016, STR 26R. R&R FITTING IAW SRM AND DWG.

Part: FITTING — CORRODED (FUSELAGE) · airframe 66,169 hrs · 39,497 cycles

PRESSURE DOME RING Y-CHORD FITTING CORRODED AT BS 1016, STR 23R. R&R FITTING IAW SRM AND DWG.

Part: FITTING — CORRODED (FUSELAGE) · airframe 66,169 hrs · 39,497 cycles

PRESSURE DOME RING Y-CHORD FITTING CORRODED AT BS 1016, STR 22L. R&R FITTING IAW SRM AND DWG.

Part: ATTACH FITTING — CORRODED (FUSELAGE) · airframe 66,169 hrs · 39,497 cycles

PRESSURE DOME RING Y-CHORD FORWARD SIDE ATTACH FITTING CORRODED AT BS 1016, STR 21L. R&R FITTING PER SRM & DWG.

Part: ATTACH FITTING — CORRODED (FUSELAGE) · airframe 66,169 hrs · 39,497 cycles

PRESSURE DOME RING Y-CHORD FORWARD SIDE ATTACH FITTING CORRODED AT BS 1016, STR 27L. R&R FITTING PER SRM & DWG.

Part: FITTING — CORRODED (FUSELAGE) · airframe 66,169 hrs · 39,497 cycles

PRESSURE DOME RING Y-CHORD FITTING CORRODED AT BS 1016, STR 25R. R&R FITTING IAW SRM AND DWG.

Part: FITTING — CORRODED (FUSELAGE) · airframe 66,169 hrs · 39,497 cycles

PRESSURE DOME RING Y-CHORD FITTING CORRODED AT BS 1016, STR 24R. R&R FITTING IAW SRM AND DWG.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 66,169 hrs · 39,497 cycles

RT HORIZONTAL STABILIZER IN SPAR RIB CRACKED AT 92.70, LOWER FLANGE JUST AFT OF THE FIRST VERTICAL STIFFENER. REPAIRED RIB IAW EA.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 66,169 hrs · 39,497 cycles

LEFT HORIZONTAL STABILIZER REMOVABLE LEADING EDGE 4TH RIB FROM INBOARD CRACKED ON THE LOWER CORNER. R & R RIB IAW SRM & DWG.

Part: SKIN — CORRODED (FUSELAGE) · airframe 66,169 hrs · 39,497 cycles

FUSELAGE LOWER SKIN CORRODED AT BS 953, LBL 8.5. REPAIRED SKIN IAW ER AND EA.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 66,169 hrs · 39,497 cycles

RIGHT HORIZONTAL STABILIZER RIB CRACKED AT HSS 92.7, FIRST AND SECOND STIFFENER FROM FRONT SPAR, ONE INCH ABOVE LOWER SKIN. REPAIRED THE RIB IAW SRM.

Part: SKIN — CRACKED (RT WING) · airframe 66,169 hrs · 39,497 cycles

RT WING INBOARD FIXED LEADING EDGE BULLNOSE SKIN CRACKED RIVETS, ALONG AFT EDGE, INBOARD OF PYLON. REPAIRED SKIN IAW ER AND EA.

Part: CONNECTOR — BROKEN (CABIN) · airframe 66,169 hrs · 39,497 cycles

EMERGENCY EXIT AISLE LIGHT CONNECTOR ARE BROKEN AT BS 460, STR 4L. R&R CONNECTOR PER WDM & AMM.

Part: CONNECTOR — BROKEN (CABIN) · airframe 66,169 hrs · 39,497 cycles

EMERGENCY EXIT AISLE LIGHT CONNECTOR BROKEN AT BS 727B, STR 4R. R&R CONNECTOR PER WDM AND AMM.

Part: CONNECTOR — BROKEN (CABIN) · airframe 66,169 hrs · 39,497 cycles

EMERGENCY EXIT AISLE LIGHT CONNECTOR ARE BROKEN AT BS 706, STR 4L. R&R CONNECTOR PER WDM & AMM.

Part: CONNECTOR — BROKEN (CABIN) · airframe 66,169 hrs · 39,497 cycles

EMERGENCY EXIT AISLE LIGHT CONNECTOR BROKEN AT BS 867, STR 4R. R&R CONNECTOR PER WDM AND AMM.

Part: CONNECTOR — BROKEN (CABIN) · airframe 66,169 hrs · 39,497 cycles

EMERGENCY EXIT AISLE LIGHT CONNECTOR ARE BROKEN AT BS 380, STR 4L. R&R CONNECTOR PER WDM & AMM.

Part: CONNECTOR — BROKEN (CABIN) · airframe 66,169 hrs · 39,497 cycles

EMERGENCY EXIT AISLE LIGHT CONNECTOR ARE BROKEN AT BS 500B, STR 4L. R&R CONNECTOR PER WDM & AMM.

Part: INTERCOSTAL — CRACKED (BS 303) · airframe 66,169 hrs · 39,497 cycles

INTERCOSTAL CRACKED AT BS 303, STRINGER 4L. R & R THE INTERCOSTAL IAW SRM AND DWG.

Part: CONNECTOR — BROKEN (CABIN) · airframe 66,169 hrs · 39,497 cycles

EMERGENCY EXIT AISLE LIGHT CONNECTOR BROKEN AT BS 500B, STR 4R. R&R CONNECTOR PER WDM AND AMM.

Part: CONNECTOR — BROKEN (CABIN) · airframe 66,169 hrs · 39,497 cycles

EMERGENCY EXIT AISLE LIGHT CONNECTOR ARE BROKEN AT BS 559, STR 4L. R&R CONNECTOR PER WDM & AMM.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 66,169 hrs · 39,497 cycles

RIGHT HORIZONTAL STABILIZER IN SPAR RIB CRACKED AT HSS 120.30, AT THE LOWER END OF THE THIRD VERTICAL STIFFENER FROM FRONT. REPAIRED THE RIB IAW SRM.

Part: CONTROLLER — FAULTY (CABIN PRESSURE) · airframe 64,763 hrs · 38,642 cycles

DIVERSION, AT FL380, CABIN PRESSURIZATION RATE CYCLED FROM +2500 FPM TO -2000 FPM. DESCENT TO FL360, RATE CYCLED FROM +1800 TO -1000. DESCENT TO FL340. CABIN PRESSURIZATION RATE STABILIZED. R&R NR 2 CABIN PRESSURE CONTROLLER PER AMM.

Part: CONTROLLER — FAULTY (CABIN PRESSURE) · airframe 64,763 hrs · 38,642 cycles

DIVERSION, AT FL380, CABIN PRESSURIZATION RATE CYCLED FROM +2500 FPM TO -2000 FPM. DESCENT TO FL360, RATE CYCLED FROM +1800 TO -1000. DESCENT TO FL340. CABIN PRESSURIZATION RATE STABILIZED. R&R NR 1 CABIN PRESSURE CONTROLLER PER AMM.

Part: LENS — BROKEN (CABIN) · airframe 63,764 hrs · 38,073 cycles

RT EMERGENCY EXIT LIGHT LENS CAP BROKEN. R&R LIGHT PER MM.

Part: BATTERY — FAILED (CABIN) · airframe 62,238 hrs · 37,178 cycles

AIRCRAFT EMERGENCY BATTERY FAILED CAPACITY CHECK AT LOCATIONS M01672. R & R BATTERY IAW AMM.

Part: BATTERY — FAILED (CABIN) · airframe 62,238 hrs · 37,178 cycles

ACFT EMERGENCY BATTERY FAILED CAPACITY CHECK AT LOCATIONS M01675. R & R BATTERY IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 62,238 hrs · 37,178 cycles

RIGHT EMERGENCY EXIT CEILING LIGHT INOPERATIVE BETWEEN ROW 22 TO ROW 23. R & R LIGHT ASSEMBLY IAW MM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 60,966 hrs · 36,436 cycles

AFT CARGO FLOOR SUPPORT STRUCTURE CRACKED AT BS 767, RBL 13.8. R & R SUPPORT IAW SRM & DWG.

Part: SUPPORT — CRACKED (RT WING) · airframe 60,966 hrs · 36,436 cycles

RIGHT WING REAR SPAR AREA HAS BULB SEAL BRACKET SUPPORT CRACKED, BELOW SPOILER 7 - 8. R & R SUPPORT IAW SRM.

Part: SUPPORT BRACKET — CRACKED (LT WING) · airframe 60,966 hrs · 36,436 cycles

LEFT WING INBD SIDE OF NR 5 SPOILER, SUPPORT BRACKET CRACKED. R & R BRACKET IAW SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 60,966 hrs · 36,436 cycles

R1 CHORD CUT OUT NUTPLATE Z ANGLE CORRODED. R & R CHORD ASSEMBLY IAW SRM & DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 60,966 hrs · 36,436 cycles

AFT WET AREA, FLOORBEAM CAP CORRODED AT BS 986, RBL 45.5. R & R FLOORBEAM CAP IAW SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 60,966 hrs · 36,436 cycles

R2 DOOR WEB CORRODED AT BS 1006, RBL 30. R & R WEB IAW DWG & SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 60,966 hrs · 36,436 cycles

INTERCOSTAL CRACKED BETWEEN BS 277 - 294.5, BL 0. R & R INTERCOSTAL IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 60,966 hrs · 36,436 cycles

INTERCOSTAL CRACKED BETWEEN BS 312 - 328, LBL 45. R & R INTERCOSTAL IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 60,966 hrs · 36,436 cycles

INTERCOSTAL CRACKED, BETWEEN BS 312 - 328, RBL 31. R & R INTERCOSTAL IAW SRM & DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 60,966 hrs · 36,436 cycles

FLOORBEAM T CAP CORRODED AT BS 328, RBL 45. R & R T CAP IAW SRM.

Part: PAN — CORRODED (FUSELAGE) · airframe 60,966 hrs · 36,436 cycles

AFT WET AREA, AT L2 DOOR LOWER PAN, CORRODED FROM SPLICE TO SPLICE CHORD. R & R PAN IAW DWG & SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 60,966 hrs · 36,436 cycles

AFT CARGO BILGE SKIN, CORRODED AT BS 727E, BL 0. REPAIRED SKIN IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 60,966 hrs · 36,436 cycles

FLOORBEAM CAP CORRODED AT BS 986, LBL 45.5. REPAIRED CAP IAW SRM.

Part: PAN — CORRODED (FUSELAGE) · airframe 60,966 hrs · 36,436 cycles

AFT WET AREA, LOWER PAN AT R2 DOOR CHORD LOWER PAN CORRODED. R & R CHORD IAW SRM & DWG.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 60,966 hrs · 36,436 cycles

LEFT CHORD CORRODED, BETWEEN BS 312 - 344. R & R CHORD IAW SRM & DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 60,966 hrs · 36,436 cycles

FLOOR SUPPORT CORRODED, BETWEEN BS 328 - 344, LBL 11. R & R FLOOR SUPPORT IAW DWG.

Part: STRIP — CORRODED (FUSELAGE) · airframe 60,966 hrs · 36,436 cycles

AFT CARGO FLOOR SUPPORT NUTPLATE STRIP CORRODED AT BS 887. R & R STRIP IAW SRM & DWG.

Part: COOLING FAN — FAULTY (AC BAY) · airframe 59,927 hrs · 35,840 cycles

AIR TURN BACK, DECLARED EMER, STRANGE ODOR IN COCKPIT & CABIN. R & R EXHAUST EQUIPMENT COOLING FAN IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 59,503 hrs · 35,577 cycles

LEFT EMERGENCY BULLNOSE LIGHT INOPERATIVE AT ROW 17. RELAMPED LIGHT IAW AMM.

Part: SLIDE — UNSECURE (L1 DOOR) · airframe 58,806 hrs · 35,190 cycles

L1 DOOR EMER EVAC SLIDE INADVERTENTLY FELL OUT OF CASE, DID NOT DEPLOY, STILL OPERATIONAL. REINSTALLED SLIDE IAW MT.

Part: BATTERY PACK — FAILED (CABIN) · airframe 58,024 hrs · 34,755 cycles

EMERGENCY EXIT LIGHT BATTERY M1669 FAILED CAPACITY TEST. R & R BATTERY PACK IAW MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 58,024 hrs · 34,755 cycles

EMERGENCY EXIT LIGHT BATTERY M1674 FAILED CAPACITY TEST. R & R BATTERY PACK IAW MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 58,024 hrs · 34,755 cycles

EMERGENCY EXIT LIGHT BATTERY M1668 FAILED CAPACITY TEST. R & R BATTERY PACK IAW MM.

Part: LIGHT — INOPERATIVE (FUSELAGE) · airframe 56,435 hrs · 33,804 cycles

LEFT FUSELAGE EMER LAMP INOPERATIVE. RELAMPED LIGHT IAW AMM.

Part: SLIDE — LOOSE (L1 DOOR) · airframe 55,879 hrs · 33,494 cycles

L1 DOOR EMER EVAC SLIDE LOOSE. SECURED SLIDE IAW SIP.

Part: SLIDE — UNSECURE (R1 DOOR) · airframe 54,538 hrs · 32,718 cycles

R1 DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT OF COVER, DID NOT DEPLOY, STILL OPERATIONAL. R & R SLIDE IAW SWA MT.

Part: COVER — BROKEN (CABIN) · airframe 54,538 hrs · 32,718 cycles

FWD ENTRY DOOR EMERGENCY LIGHT COVER BROKEN. R & R LIGHT ASSEMBLY IAW AMM.

Part: COVER — BROKEN (CABIN) · airframe 54,371 hrs · 32,614 cycles

RT OVERWING EXIT LOWER EMERGENCY EXIT LIGHT COVER BROKEN. R & R COVER IAW AMM.

Part: BRACKET — CRACKED (RT WING) · airframe 54,144 hrs · 32,467 cycles

RT WING HYD LINE BRACKET CRACKED AT NR 2 PYLON AT WS 253.0. R & R BRACKET IAW SRM.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 54,144 hrs · 32,467 cycles

VERTICAL PRESSURE WEB CRACKED AT BS 663 LBL 40.5. REPAIRED WEB IAW SRM.

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 54,144 hrs · 32,467 cycles

VERTICAL PRESSURE WEB CRACKED AT BS 663 RBL 40.5. REPAIRED WEB IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,466 hrs · 32,069 cycles

STRINGER CLIP CRACKED AT STATION 500, STRINGER 19R. R & R CLIP IAW SRM.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 53,466 hrs · 32,069 cycles

LT NR 1 WINDOW FRAME ASSEMBLY CRACKED AT UPPER OTBD CORNER. R & R FRAME IAW ACO. CORRECTED ATA & PART DEFECT LOCAL.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,466 hrs · 32,069 cycles

FS FRAME CRACKED AT STATION 727A, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,466 hrs · 32,069 cycles

FS FRAME CRACKED AT STATION 500C, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,466 hrs · 32,069 cycles

SKIN CRACKED AT STATION 540, BETWEEN STRINGER 22L & STRINGER 23L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,466 hrs · 32,069 cycles

FS SKIN CRACKED AT BS 540, STRINGER 22R. REPAIRED SKIN IAW EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 52,740 hrs · 31,645 cycles

LONGITUDINAL FLOORBEAM CRACKED AT STA 727B, RBL 45.5. REPAIRED BEAM IAW SWA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 52,740 hrs · 31,645 cycles

LONGITUDINAL FLOORBEAM CRACKED AT STA 727B, LBL 45. REPAIRED BEAM IAW SWA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 52,740 hrs · 31,645 cycles

LONGITUDINAL FLOORBEAM CRACKED AT STA 727B, RBL 45. REPAIRED BEAM IAW SWA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 52,740 hrs · 31,645 cycles

LONGITUDINAL FLOORBEAM CRACKED AT STA 727B, RBL 24. REPAIRED BEAM IAW SWA.

Part: PANEL — DAMAGED (E&E BAY) · airframe 52,740 hrs · 31,645 cycles

DRIP SHIELD DIRECTLY ABOVE THE BATTERY CHARGER AND TRANSFORMER/RECTIFIER NR 1 HAS A LARGER HOLE MELTED AWAY. COMPLIED WITH INSPECTION, NO OTHER DAMAGED FOUND. R & R PANEL IAW MM.

Part: LENS — LOOSE (CABIN) · airframe 52,213 hrs · 31,321 cycles

L2 DOOR SIDE EGRESS LIGHT SIGN LENS LOOSE. REMOVED AND REPLACED LENS ASSY PER MM.

Part: SLAT — CRACKED (RT WING) · airframe 52,212 hrs · 31,321 cycles

RIGHT WING NR 7 LEADING EDGE SLAT CRACKED AT THE ACTUATOR MOUNT BRACKET. REMOVED AND REPLACED NR 7 LEADING EDGE SLAT PER MT AND M/M.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 50,010 hrs · 29,919 cycles

R2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW MM.

Part: FLAP — DELAMINATED (LT WING) · airframe 48,388 hrs · 28,965 cycles

LT WING INBOARD AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP ASSY PER AMM.

Part: SKIN — DAMAGED (LT WING TE FLAP) · airframe 48,312 hrs · 28,926 cycles

LT WING O/B AFT FLAP UPPER SKIN MATERIAL DAMAGED FROM UPPER SURFACE O/B CORNER. REMOVED AND REPLACED AFT FLAP PER MM.

Part: WIRE — BROKEN (CABIN) · airframe 48,075 hrs · 28,769 cycles

DURING SCHEDULED SPV CHECK, FOUND FWD OVERHEAD EMERGENCY EXIT SIGN LIGHT ASSY INOP. FOUND WIRE BROKEN. REMOVED AND REPLACED WIRE PER WDM.

Part: BATTERY — FAILED (CABIN) · airframe 47,846 hrs · 28,633 cycles

DURING SCHEDULED HC2 CHECK, EMERGENCY EXIT LIGHT BATTERIES FAILED CAPACITY CHECK. REMOVED AND REPLACED BATTERIES PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 47,472 hrs · 28,411 cycles

DURING SCHEDULED MV2 CHECK, FOUND L1 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT IAW MM.

Part: SLIDE — LOW PRESSURE (R2 DOOR) · airframe 45,778 hrs · 27,424 cycles

R2 DOOR EMERGENCY EVAC SLIDE PRESSURE GAUGE LOW. REMOVED AND REPLACED SLIDE PER MT.

Part: HANDLE — MISSING (EVAC SLIDE) · airframe 45,297 hrs · 27,149 cycles

L2 DOOR EMERGENCY EVAC SLIDE HANDLE MISSING. REMOVED AND REPLACED SLIDE PER MM.

Part: SLIDE — LOW PRESSURE (L1 DOOR) · airframe 43,709 hrs · 26,210 cycles

L1 DOOR EMERGENCY EVAC SLIDE PRESSURE GAUGE LOW. REMOVED AND REPLACED SLIDE PER MT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 43,474 hrs · 26,068 cycles

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

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 42,019 hrs · 25,235 cycles

DURING SCHEDULED MV2 CHECK, FOUND SHEAR TIE CRACKED AT BS 420, BETWEEN STR 17L TO STR 18L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 41,043 hrs · 24,660 cycles

DURING SCHEDULED HC1 CHECK, LT EEPLS FAILED CAPACITY CHECK AT ROW 6. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: FLAP — DELAMINATED (LT WING) · airframe 41,043 hrs · 24,660 cycles

DURING SCHEDULED HC1 CHECK, FOUND LT WING AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 41,043 hrs · 24,660 cycles

DURING SCHEDULED HC1 CHECK, LT EXTERIOR EMERGENCY EXIT LIGHTS FAILED CAPACITY CHECK AT BS 757. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 41,043 hrs · 24,660 cycles

DURING SCHEDULED 12Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 727B, RBL 45.5. REPAIRED BEAM PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 41,043 hrs · 24,660 cycles

DURING SCHEDULED 12Y CHECK, FOUND SKIN CRACKED AT BS 1081.5, BETWEEN STR 2R TO STR 3R. REPAIRED SKIN PER EA.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 41,043 hrs · 24,660 cycles

DURING SCHEDULED 12Y CHECK, FOUND SHEAR TIE CRACKED AT BS 1121, BETWEEN STR 2R TO STR 3R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,043 hrs · 24,660 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 907, STR 8R. REPAIRED FRAME PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 41,043 hrs · 24,660 cycles

DURING SCHEDULED 12Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 907, STR 8L. REMOVED AND REPLACED CLIP PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,043 hrs · 24,660 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 907, STR 8L. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,043 hrs · 24,660 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED BETWEEN BS 360 TO BS 907, BETWEEN STR 8L TO STR 8R. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,043 hrs · 24,660 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 440, STR 8R. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,043 hrs · 24,660 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 827, STR 8L. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,043 hrs · 24,660 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 380, STR 8L. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,043 hrs · 24,660 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 787, STR 8L. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (BS 747 S8L) · airframe 41,043 hrs · 24,660 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 747, STR 8L. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (BS 727D S8R) · airframe 41,043 hrs · 24,660 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 727D, STR 8R. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (BS 400 S8L) · airframe 41,043 hrs · 24,660 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 400, STR 8L. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (BS 400 S8R) · airframe 41,043 hrs · 24,660 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 400, STR 8R. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (BS 867 S8L) · airframe 41,043 hrs · 24,660 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 867, STR 8L. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (BS 440 S8L) · airframe 41,043 hrs · 24,660 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 440, STR 8L. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (BS 867 S8R) · airframe 41,043 hrs · 24,660 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 867, STR 8R. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (BS 747 S8R) · airframe 41,043 hrs · 24,660 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 747, STR 8R. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (BS 727B S8R) · airframe 41,043 hrs · 24,660 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 727B, STR 8R. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (BS 727D S8L) · airframe 41,043 hrs · 24,660 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 727D, STR 8L. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (BS 787 S8R) · airframe 41,043 hrs · 24,660 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 787, STR 8R. REPAIRED FRAME PER EA.

Part: BATTERY PACK — FAILED (CABIN) · airframe 39,147 hrs · 23,492 cycles

DURING SCHEDULED HC2 CHECK, RT EMERGENCY EXIT ROW BATTERY FAILED CAPACITY TEST. R&R BATTERY BACK PER MM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 38,050 hrs · 22,859 cycles

DURING SCHEDULED 10Y CHECK, FOUND SHEAR TIE CRACKED AT BS 540, RBL 40.72. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 38,050 hrs · 22,859 cycles

DURING SCHEDULED 10Y CHECK, FOUND SHEAR TIE CRACKED AT BS 540, LBL 54.60. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 38,050 hrs · 22,859 cycles

DURING SCHEDULED 10Y CHECK, FOUND SHEAR TIE CRACKED AT BS 540, RBL 54.60. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FLAP — CRACKED (RT WING) · airframe 38,050 hrs · 22,859 cycles

DURING SCHEDULED 10Y CHECK, FOUND RT WING O/B T/E AFT FLAP CRACKED. REMOVED AND REPLACED AFT FLAP PER MM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 38,050 hrs · 22,859 cycles

DURING SCHEDULED 10Y CHECK, FOUND SHEAR TIE CRACKED AT BS 540, LBL 6.14. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 38,050 hrs · 22,859 cycles

DURING SCHEDULED 10Y CHECK, FOUND SHEAR TIE CRACKED AT BS 540, LBL 32.40. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 38,050 hrs · 22,859 cycles

DURING SCHEDULED 10Y CHECK, FOUND SHEAR TIE CRACKED AT BS 540, RBL 15.04. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 38,050 hrs · 22,859 cycles

DURING SCHEDULED 10Y CHECK, FOUND SHEAR TIE CRACKED AT BS 540, RBL 6.14. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 38,050 hrs · 22,859 cycles

DURING SCHEDULED 10Y CHECK, FOUND SHEAR TIE CRACKED AT BS 540, LBL 15.04. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 38,050 hrs · 22,859 cycles

DURING SCHEDULED 10Y CHECK, FOUND SHEAR TIE CRACKED AT BS 540, RBL 32.40. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 38,050 hrs · 22,859 cycles

DURING SCHEDULED 10Y CHECK, FOUND SHEAR TIE CRACKED AT BS 540, LBL 40.87. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SLIDE — LOW PRESSURE (R1 DOOR) · airframe 38,072 hrs · 22,869 cycles

R1 DOOR EMERGENCY EVACUATION SLIDE PRESSURE LOW. REMOVED AND REPLACED SLIDE PER MT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 37,477 hrs · 22,496 cycles

DURING SCHEDULED MV1 CHECK, FOUND L1 DOOR EGRESS LIGHT INOP. RELAMPED LIGHT PER MM.

Part: FITTING — CORRODED (RT MLG) · airframe 34,419 hrs · 20,649 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT MLG TRUNNION FITTING LUGS CORRODED. REMOVED AND REPLACED FITTING PER SWA EA.

Part: FITTING — CORRODED (LT MLG) · airframe 34,419 hrs · 20,649 cycles

DURING SCHEDULED MV2 CHECK, FOUND LEFT MLG TRUNNION FITTING LUGS CORRODED. REMOVED AND REPLACED FITTING PER SWA EA.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 34,027 hrs · 20,418 cycles

L1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 33,997 hrs · 20,398 cycles

DURING SCHEDULED SPV CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP INBOARD LOWER CORNER DELAMINATED. REMOVED AND REPLACED FLAP PER MM.

Part: VALVE — INOPERATIVE (CABIN PRESSURE) · airframe 31,954 hrs · 19,188 cycles

AIR TURNBACK, AIRCRAFT DID NOT PRESSURIZE IN AUTO OR ALTERNATE MODE. REMOVED AND REPLACED NEGATIVE PRESSURE VALVE PER MM.

Part: SLIDE — DISLODGED (L1 DOOR) · airframe 31,260 hrs · 18,786 cycles

L1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM.

Part: FLOORBEAM — CORRODED (BS 328) · airframe 30,826 hrs · 18,553 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 328, RBL 19 TO RBL 57. REPAIRED FLOORBEAM PER SWA EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 30,659 hrs · 18,461 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 328, RBL 19 TO RBL 57. REPAIRED FLOORBEAM PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 30,659 hrs · 18,461 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 344, LBL 38 TO LBL 48. REPAIRED FLOORBEAM PER SRM.

Part: FLOORBEAM — CORRODED (BS 986) · airframe 30,659 hrs · 18,461 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986, RBL 40 TO RBL 44. REPAIRED BEAM PER SRM.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHT) · airframe 29,640 hrs · 17,862 cycles

DURING SCHEDULED HC2 CHECK, AFT CABIN EMERGENCY BATTERY PACKS FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACKS PER MM.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHT) · airframe 29,640 hrs · 17,862 cycles

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

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHT) · airframe 29,640 hrs · 17,862 cycles

DURING SCHEDULED HC2 CHECK, EMERGENCY BATTERY PACK AT ROW 16 ABC FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHT) · airframe 29,640 hrs · 17,862 cycles

DURING SCHEDULED HC2 CHECK, LT FWD CABIN EMERGENCY BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 29,618 hrs · 17,843 cycles

DURING SCHEDULED MV3 CHECK, FOUND MID CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 28,547 hrs · 17,220 cycles

DURING SCHEDULED MV2 CHECK, FOUND AFT CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACKS PER MM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 27,713 hrs · 16,774 cycles

R2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM.

Part: LIGHT — WORN (CABIN) · airframe 27,294 hrs · 16,534 cycles

DURING SCHEDULED HC1 CHECK, FOUND EEPLS STRIP WORN OUT BETWEEN ROW 14 TO ROW 16. REMOVED AND REPLACED STRIP PER MM.

Part: BLADE — TORN (NR 2 ENGINE) · airframe 24,695 hrs · 15,097 cycles

DURING SCHEDULED HC2 CHECK, C/W BOROSCOPE INSPECTION OF NR 2 ENGINE AND FOUND 1 EA NR 3 HPC BLADE OUT OF LIMITS. REMOVED AND REPLACED NR 2 ENGINE PER MM.

Part: GLOWSTRIP — LOOSE (CABIN) · airframe 22,355 hrs · 13,789 cycles

EMERGENCY PHOTOLUMINESCENT FLOOR STRIP FROM ROW 4 DEF TO ROW 7 DEF LOOSE. REMOVED AND REPLACED PHOTOLUMINESCENT STRIP PER MM.

Part: ACTUATOR — MALFUNCTIONED (RT MLG) · airframe 19,109 hrs · 11,970 cycles

IND - FLT 2770 - ON LANDING, RIGHT GEAR RED LIGHT ILLUMINATED WITH NO GREEN LIGHT AND GEAR WARNING HORN. CYCLED GEAR DID THE SAME, ON GO AROUND GEAR CAME DOWN, COMPLETED CHECKLIST AND LANDED. REMOVED AND REPLACED RIGHT GEAR ACTUATOR PER MM. (M)

Part: BATTERY — DISCHARGED (CABIN) · airframe 16,462 hrs · 10,479 cycles

DURING SCHEDULED RON, FOUND AFT CABIN OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 15,865 hrs · 10,151 cycles

SMALL SECTION OF EEPLS LOOSE IN CABIN. SECURED EEPLS PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 15,258 hrs · 9,798 cycles

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

Part: HARNESS — OVERTEMP (COCKPIT) · airframe 13,683 hrs · 8,896 cycles

DURING DESCENT HAD SPARKS SHOOT OUT OF FO'S SIDE WINDOW CANNON PLUG, SMELL OF BURNING RUBBER. REMOVED AND REPLACED NR 2 WINDOW HEAT COILED HARNESS PER MM.

Part: CONTROL PANEL — FAULTY (COCKPIT) · airframe 13,451 hrs · 8,781 cycles

DECLARED EMERGENCY, DIVERSION, F/O SPILLED WATER ON CENTER CONSOLE. FWD CARGO FIRE LIGHT ILLUMINATED SOME TIME LATER. DIVERTED TO MCI, AFTER LANDING CONFIRMED THERE WAS NO FIRE. FIRE SUPPRESSION NOT UTILIZED. NO FIRE MASTER LIGHT OR BELL AT ANY TIME. REMOVED AND REPLACED FIRE CONTROL PANEL PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 10,865 hrs · 7,322 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EEPLS INOP AT ROW 8. RELAMPED EEPLS PER MM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 10,537 hrs · 7,140 cycles

DURING SCHEDULED C2 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED EVAC SLIDE PER MM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 10,537 hrs · 7,140 cycles

DURING SCHEDULED C2 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED EVAC SLIDE PER MM.

Part: COVER — MISSING (CABIN) · airframe 10,223 hrs · 6,959 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EEPLS COVER MISSING AT ROW 8. INSTALLED EEPLS COVER PER MM.

Part: HINGE BRACKET — WORN (HORIZ STAB) · airframe 10,172 hrs · 6,927 cycles

DURING SCHEDULED SERVICE CHECK, FOUND BOTH HORIZ STAB NR 4 HINGE PLATE BEARINGS WORN. REMOVED AND REPLACED HORIZ STAB HINGE PLATES PER SWA RA.

Part: COVER — MISSING (CABIN) · airframe 10,101 hrs · 6,883 cycles

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

Part: BUSHING — WORN (ELEVATOR TAB) · airframe 9,530 hrs · 6,531 cycles

DURING SCHEDULED PM CHECK, SWA SI 11038-55, FOUND RT ELEVATOR TAB INBOARD HINGE BUSHING WORN. REMOVED AND REPLACED BUSHING PER MM.

Part: SLIDE — OUT OF ADJ (SERVICE DOOR) · airframe 8,927 hrs · 6,202 cycles

FWD SVC DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. RE-ADJUSTED EVAC SLIDE ASSY PER MM.

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 8,783 hrs · 6,108 cycles

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

Part: BUSHING — WORN (RT ELEV TAB)

DURING SCHEDULED SPECIAL CHECK, RT ELEVATOR TAB FAILED BEARING FREEPLAY CHECK. REMOVED AND REPLACED BUSHINGS PER MM.

Part: HMU — MALFUNCTIONED (NR 1 ENGINE)

TRIED TO SET CLIMB POWER, (CDU N1 LIMIT 99.5 PERCENT) NR 1 ENG GOT A STRONG AIRFRAME VIBRATION ANYTIME PWR WAS ADVANCED PAST 93 PERCENT N1, NO MOVEMENT IN EITHER VIBRATION GAUGE. INSPECTED AIRCRAFT, AND NO DEFECTS NOTED. REMOVED AND REPLACED HMU, LKS AND OPS CHECKED GOOD PER MM.