N456TM

Part: LIGHT — INOPERATIVE (CABIN)

EMERGENCY EXIT LIGHT OVER L2 DOOR INOPERATIVE. REMOVED AND REPLACED LIGHT ASSY, OPS CHECKS NORMAL. (M)

Part: FILTER — CONTAMINATED (OIL SYSTEM)

NR 1 POSITIONOIL FILTER BYPASS LIGHT ILLUMINATED IN FLIGHT, PULLED BACK POWER TO IDLE TO CHECK IF LIGHT WOULD GO OFF, IT STAYED ON. SHUT DOWN NR 1 ENGINE PER CHECKLIST, LANDED IN LEX WITHOUT FURTHER INCIDENT. REMOVED MAIN OIL FILTER AND CHECKED FOR CONTAMINATION, NO CONTAMINATION FOUND. DETERMIED BYPASS SWITCH TO BE FAULTY. AIRCRAFT RELEASED PER DMI NR 054 MEL 79-2 ENTERED IN DMI LOG AND PLACARDED. (M)

Part: SKIN — CRACKED (FUSELAGE)

DURING CPCP INSPECTION, FOUND CRACKS ABOVE FORWARD WING TO BODY FAIRING AFT OF WING ILLUMINATION LIGHT OF LEFT WING IN FUSELAGE. REPAIRED IAW BOEING SUPPLIED ENGINEERING. (M)

Part: LIGHT — INOPERATIVE (EXTERIOR)

R1 EXTERIOR EMERGENCY LIGHT INOPERATIVE. RELAMPED IAW BOEING MM 33-51-21, OPS CHECK OK AT THIS TIME. (M)

Part: LIGHT — INOPERATIVE (CABIN)

FORWARD AISLE EMERGENCY EXIT LIGHT SYSTEM INOPERATIVE. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSY IAW BOEING MM 33-11-0, OPS CHECK OK. (M)

Part: BATTERY — INOPERATIVE (CABIN)

AFT AISLE OVERHEAD EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK, IAW BOEING MM 33-51-81, AND RELAMPED IAW BOEING MM 33-51-92, OPS CHECK NORMAL AT THIS TIME. (M)

Part: WINDSHIELD — FAILED (COCKPIT)

SHATTERED OUTER PANE ON NR 2 CAPTAIN'S WINDOWS. QRH PROCEDURES FOLLOWED. REMOVED AND REPLACED LEFT SLIDING NR 2 WINDOW IAW BMM 56-12-11. (X)

Part: HOSE — DAMAGED ('A' HYD SYSTEM)

LOSS OF SYSTEM 'A' HYDRAULIC SYSTEM IN FINAL APPROACH. REMOVE AND REPLACE BRAKE FLEX LINE IAW MM 20-10-52. INSPECTED CASE DRAIN FILTER MAGNETIC PLUGS IAW MM 29-11-41, SERVICED HYDRAULIC SYSTEM IAW 12-12-0. RAN ENGINES, OPS AND LEAK CHECKED OK. (M)

Part: LIGHT — FAILED (CABIN)

FOUND FORWARD BULLNOSE EMERGENCY LIGHT OUT. REMOVED AND REPLACED LIGHT ASSY IAW 33-51-11, OPS CHECKS OK. (M)

Part: LIGHT — FAILED (RT EMER EXIT)

RIGHT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE ON TEST. REPLACED EMERGENCY EXIT LIGHT ASSY, IAW BMM 33-51-31, GROUND CHECKS NORMAL IAW BMM 33-51-21. (M)

Part: LIGHT — LOOSE (CABIN)

EMERGENCY EXIT TRACK LIGHTING STRIP IS LOOSE. RESET FLOOR TRACK AS NECESSARY, OK FOR SERVICE. (M)

Part: ACTUATOR — FAILED (NLG)

NOSE GEAR WOULD NOT RETRACT. REMOVE AND REPLACED NOSE GEAR LOCK ACTUATOR PER BMM 32-33-21. (M)

Part: COVER — BROKEN (CABIN)

WIRES EXPOSED, AFT PLASTIC PROTECTIVE COVER BROKEN ON EMERGENCY TRACK LIGHTING SYSTEM. PROTECTED EXPOSED WIRING IAW BMM 20-10-14, EMERGENCY LIGHTING OPERATES NORMALLY. PENDING INSTALLATION OF PLASTIC PROTECTIVE COVER. (X)

Part: SPLICE — BAD (CABIN)

CABIN EMERGENCY EXIT LIGHTS INTERMITTENT. FOUND BAD WIRE SPLICE AT CABIN, REPAIRED IAW BMM 33-51-0. OPS CHECKS GOOD. (X)

Part: PUMP — FAILED ('A' HYD SYSTEM)

NR 1 'A' SYSTEM ENGINE HYDRAULICS INOPERATIVE. REMOVED AND REPLACED NR 1 'A' SYSTEM ENGINE HYDRAULIC DRIVE PUMP IAW BMM 29011-31, OPS CHECKS GOOD AT THIS STATION. REPAIRED BROKEN WIRE IN LEFT GEAR WELL FOR LEFT ENGINE HYDRAULIC S/O VALVE, IAW BMM 20-10-13. GROUND CHECKS NORMAL. (M)

Part: HUB — DAMAGED (LT ENGINE)

HIT DEER ON LEFT ENGINE NACELLE DURING TAKEOFF ROLL (AT V1). REMOVED AND REPLACED NOSE COWL ASSY, NOSE BULLET ASSY PER PWMM 72-000-23. REMOVED AND REPLACED C1 FAN ASSY PER PWMM 72-30-0, PEFORMED TEST I AND G. REFERENCE GE ON WING SUPPORT SERVICE WORK ORDER UH0486, ALL SYSTEMS CHECK NORMAL. (X)

Part: LIGHT — INOPERATIVE (CABIN)

R-2 EMERGENCY EXIT INTERIOR LIGHT INOP. REMOVED AND REPLACED BATTERY HOLDER ON LIGHT UNIT PER BMM 33-51-01. (M)

Part: LIGHT — INOPERATIVE (CABIN)

PASSENGER CABIN R1 DOOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY EXIT LIGHT AT R1 DOOR PER BMM 33-51-101, PAGE 201 THROUGH 203. (X)

Part: SLIDE — FELL OFF (R1 DOOR)

R-I EMERGENCY ESCAPE SLIDE FELL OFF DOOR. MECHANIC REATTACHED TO DOOR, REINSPECTED SLIDE PACK ASSY PER BMM 25-61-311. (M)

Part: CONNECTOR — CONTAMINATED (APU)

BEFORE DEPARTURE APU FIRE DETECTION SYSTEM ACTIVATED. REFER TO DMI 1103, MEL 26-8-1, CLEANED MOISTURE FROM CONNECTOR. OPS CHECK OK IAW BMM 26-11-0. (M)

Part: LIGHT — INOPERATIVE (CABIN)

L2 INTERIOR EMERGENCY LIGHT DIM. REPLACED EMERGENCY LIGHT ASSY PER BMM 33-51-101, GROUND CHECKS NORMAL. (M)

Part: LIGHTS — INOPERATIVE (CABIN)

COCKPIT EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED COCKPIT EMERGENCY EXIT LIGHT PER 33-51-101. (M)

Part: BATTERY — DISCHARGED (CABIN)

R1 AND L1 EXTERIOR EMERGENCY LIGHTS INOPERABLE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK FOR R1 AND L1 DOORS PER BMM 33-51-71. OPERATES NORMALLY PER BMM 33-51-0. (X)

Part: LIGHT — INOPERATIVE (CABIN)

R2 EMERGENCY EXIT DOOR LIGHT INOPERATIVE. REMOVED AD REPLACED EXIT DOOR LIGHT ASSY PER BMM 33-51-01. (X)

Part: LIGHT — INOPERATIVE (CABIN)

R2 EMERGENCY EXIT DOOR LIGHT INOP. REMOVED AND REPLACED R2 EMERGENCY EXIT DOOR LIGHT ASSY PER BMM 33-51-01. (M)

Part: LIGHT — INOPERATIVE (CABIN)

LEFT DOOR EMERGENCY LIGHTS DO NOT WORK. REMOVED AND REPLACED EMERGENCY LIGHT PER BMM 33-51-51. (X)

Part: SQUIB — FAILED (APU FIRE BOTT)

SQUIB FAILED TO FIRE APU BOTTLE. REMOVED AND REPLACED APU FIRE BOTTLE SQUIB PER BMM 26-22-21. (M)

Part: LIGHT — INOPERATIVE (CABIN)

L1 DOOR EMERGENCY LIGHT DOES NOT WORK. REMOVED AND REPLACED EMERGENCY LIGHT PER BMM 33-51-51. (M)

Part: FIRE LOOP — FAILED (APU)

APU FIRE DETECT INOP. AIRCRAFT RELEASED PER MEL 26-8 DMI NR 908 ITEM PLACARDED AND TRANSFERED TO DMI. (M)

Part: CONNECTOR — FAILED (APU)

APU FIRE DETECTION LIGHT CAME ON, DIVERTED TO AMA. REMOVED AND REPLACED CONNECTOR ON FIRE LOOP THAT WAS SHORTING TO GROUND PER BSWPM 20-62-16. OPS CHECK GOOD PER BMM 26-15-0. (M)

Part: CONNECTOR — FAILED (APU)

APU FIRE EXTINGUISHER SYSTEM INOP. REMOVED AND REPLACED CONNECTOR ON FIRE LOOP THAT WAS SHORTING TO GROUND. OPS CHECK GOOD PER BMM 26-15-0. (M)

Part: ADC CONNECTOR — BENT (E/E COMPT)

AT ALTITUDE, LOST MODE C, MACH TRIM GPWS, AND AUTOPILOT DISENGAGED. FOUND PIN 16 ON ADC BENT. CHECKED ARCING CONNECTOR AT ADC. RE-INSTALLED ADC ACCOMPLISHED SYSTEM TEST PER MM 34-12-11 AND FAR 43, APPENDIX F. (X)

Part: SWITCH — OUT OF ADJUST (GROUND SENSING)

TRANSPONDER 1 AND 2 MODE C INOPERABLE. CABIN WOULD NOT PRESSURIZE. REPOSITIONED GROUND SENSING SWITCH TARGET. (X)

Part: BATTERY PACK — DISCHARGED (CABIN)

FORWARD ENTRY DOOR EMERGENCY EXIT SIGN INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATERY PACK PER BMM 33-51-01. OPS CHECK GOOD THIS STATION. (M)

Part: LIGHT — INOPERATIVE (REAR PIT)

RIGHT EMERGENCY LIGHTING INOP (NEAR REAR PIT) EXTERIOR. REMOVED AND REPLACED EXTERIOR EMERGENCY LIGHT SOCKET (REFLECTION ASSY) PER BMM 33-51-01. OPS CHECK GOOD AT THIS TIME. (M)

Part: BATTERY — DISCHARGED (CABIN)

AFT BULL NOSE EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERYS IAW BMM 33-51-01. OPS CHECK OK. (M)

Part: BATTERY — DISCHARGED (CABIN)

L1 PORTABLE EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERYS IAW BMM 33-51-101. OPS CHECK OK. (M)

Part: WIRE — BROKEN (CABIN)

AFT RIGHT DOOR LOWER EMERGENCY EXIT LIGHT INOP. SPLICED BROKEN WIRE TO LIGHT PER STANDARD PRACTICE MANUAL 20-30-22. (M)

Part: EVAC SLIDE — BOTTLE LEAKING (R-2 DOOR)

R-2 SLIDE LEAKING PRESSURE FROM BOTTLE. REMOVED AND REPLACED THE R-2 SLIDE PER BMM 25-61-311. (M)

Part: BULB — FAILED (CABIN)

EMERGENCY EXIT TRACK HAS LIGHT OUT AT ROW 6. REMOVED AND REPLACED PIT TAIL AS REQUIRED, OPS GOOD AT THIS TIME. (M)

Part: BLKHD WEB — CRACKED (BS 294.5)

REPAIRED FUSELAGE BULKHEAD WAS DUE TO CRACKS AT BS 294.5 LBL 3.5 TO LBL 9.5 AND RBL 5 TO RBL 11 BETWEEN WL 172.5 TO WL 150.5 IAW FAX BOEING M-7272-953780 DATED JULY 21, 1995 AND SKETCH CIN FAAX952195 1/1, DOCUMENTED ON FAA FORM 8110-3. (M)

Part: BLKHD WEB — DENTED (BS 1016)

REPAIRED FUSELAGE AFT BULKHEAD WEB DUE TO DENT AT BS 1016 BETWEEN STIFFENERS NR 6 LEFT AND NR 7 LEFT IAW SRM 53-10-4, FIG 12. (M)

Part: SKIN — CRACKED (BS 727)

REPAIRED FUSELAGE SKIN DUE TO CRACK AT BS 727 BETWEEN STRINGER NR 20 AND STRINGER NR 19 RIGHT IAW DRAWING NR CEX3-53-1 DATED JULY 15, 1995, DOCUMENTED ON FAA FORM 8110-3. (M)

Part: STRINGER — CRACKED (LT WING)

REPAIRED LEFT WING DUE TO CRACK AT WBL 227 UPPER STRINGER NR 11 AND STRINGER NR 12 ON THE RIB ATTACHMENT FLANGE IAW CASINO DWG NR CEX3-57-4, DATED JULY 20, 1995, DOCUMENTED ON FAA FORM 8110-3.

Part: FLOOR BEAM — CORRODED (BS 312)

REPAIRED FLOOR BEAM UPPER CHORD DUE TO CORROSION AT BS 312 WL 208.1 BETWEEN LBL 18 TO RBL 5 IAW SRM 53-10-9, FIG 5. (M)

Part: STRINGER — CRACKED (LT WING)

REPAIRED LEFT WING DUE TO CRACK AT WBL 279.5 UPPER STRINGER NR 9 ON THE RIB ATTACHMENT FLANGE IAW CASINO DRAWING NR CEX3-57-3 DATED JULY 20, 1995, DOCUMENTED ON FAA FORM 8110-3. (M)

Part: STRINGER — CRACKED (BS 1035-1045)

REPAIRED STRINGER NR 9 LEFT DUE TO CRACK BETWEEN BS 1035 TO BS 1045 IAW SRM 53-10-3, FIG2. (M)

Part: STRINGER — CRACKED (BS 903-913)

REPLACED SPLICE IN RIGHT STRINGER NR 4 DUE TO CRACK BETWEEN BS 903 TO BS 913 IAW SRM 51-10-1, 51-30-2 AND 51-20-1. (M)

Part: CHORD — CORRODED (BS 267)

REPLACED CHORD SECTION DUE TO CORROSION ON NOSE GEAR TORQUE BOX AT BS 267 WL 144 BETWEEN LBL 20 TO RBL 20 IAW SRM 51-10-1 AND 51-30-2. (M)

Part: FLOOR BEAM — CORRODED (BS 1006)

REPAIRED FLOOR BEAM UPPER CHORD DUE TO CORROSION AT BS 1006 WL 208.1 BETWEEN BL 0 TO LBL 23 IAW SRM 53-10-9, FIG 7. (M)

Part: FLOOR BEAM — CORRODED (BS 947.5)

REPAIRED FLOOR BEAM UPPER CHORD DUE TO CORROSION AT BS 947.5 WL 208.1 RBL 7 TO RBL 54 IAW SRM 53-10-9, FIG 2. (M)

Part: FLOOR BEAM — CORRODED (BS 328)

REPAIRED FLOOR BEAM WEB DUE TO CORROSION AT BS 328 WL 200 BETWEEN LBL 52 TO LBL 64 IAW SRM 51-40-2, FIG 1. (M)

Part: FLOOR BEAM — CORRODED (BS 344)

REPAIRED FLOOR BEAM UPPER CHORD DUE TO CORROSION AT BS 344 WL 208.1 BETWEEN LBL 12 TO LBL 58 IAW SRM 53-10-9, FIG 5. (M)

Part: FLOOR BEAM — CORRODED (BS 967)

REPAIRED FLOOR BEAM UPPER CHORD DUE TO CORROSION AT BS 967 WL 208.1 BETWEEN LBL 1 TO LBL 16 IAW SRM 53-10-9, FIG 7. (M)

Part: FLOOR BEAM — CORRODED (BS 277)

REPAIRED FLOOR BEAM WWEB DUE TO CORROSINO AT BS 277 WL 194 BETWEEN LBL 9.50 TO LBL 12.50 IAW SRM 51-40-2, FIG 1. (M0

Part: EEL — BROKEN (CABIN)

ROW 7 EMERGENCY EXIT LIGHT INOPERATIVE. REPAIRED SPLICE ON ROW 7 EMERGENCY EXIT LIGHT. SYSTEM OPS CHECKED GOOD PER BMM 33-51-11.

Part: WIRE — BROKEN (CABIN EEL)

EMERGENCY LIGHTING INOP, ROWS 1-6. REPAIRED BROKEN WIRE WITH BUTT SPLICE PER BSWP 20-30-22. SYSTEM OP CHECKED GOOD PER BMM 33-51-0. (X)

Part: EEL — LOOSE (L1 DOOR)

FORWARD EXTERIOR EMERGENCY EXIT LIGHTS INOP. ACFT RELEASED PER MEL 33-14 DMI NR 024, ITEM TRANSFERRED TO CEX FORM 4001 AND PLACARDED, DAY OPERATIONS ONLY. REFER TO MEL 33-14 DMI NR 024 EXTERIOR EMERGENCY LIGHT SYSTEMS INOP. FOUND L1 DOOR RETRACTABLE EXIT LIGHT DISLODGED, RESECURED. OPS CHECKS GOOD AT THIS TIME IAW 33-51-0. (X)

Part: EEL REFLECTOR — CORRODED (CABIN)

THE RT FWD EXTERIOR EMERGENCY LIGHT INOP. REMOVED AND REPLACED FWD EXTERIOR EMERGENCY LIGHT REFLECTOR ASSY AND LAMP. OPS CHECKS NORMAL. (W)

Part: EEL REFLECTOR — CORRODED (CABIN)

THE LT FWD EXTERIOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED FWD EXTERIOR EMERGENCY EXIT LIGHT REFLECTOR ASSY AND LAMP. OPS CHECKS NORMAL. (W)

Part: EEL BULB — FAILED (CABIN)

THE FWD EXTERIOR EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED LIGHT BULBS L1, R1 DOOR LIGHTS EXTERIOR IAW 33-51-21. (W)