N281SC

Part: CHARGER — INOPERATIVE (CABIN) · airframe 49,372 hrs · 28,698 cycles

DURING HEAVY MAINTENANCE INSPECTION THE FORWARD OVERHEAD EMERGENCY EXIT LIGHT WAS FOUND INOP. REPLACED CHARGER IAW B727 MM 335081. OPS CHECK NORMAL IAW B727 MM 335001.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 49,372 hrs · 28,698 cycles

DURING HEAVY MAINTENANCE INSPECTION CORROSION WAS FOUND OUT OF LIMITS ON SEAT TRACK AT BS 344 TO 460 RBL 24. REMOVED CORROSION IAW B727 SRM 511006. REMOVED SEAT TRACK IAW B727 SRM 513002. FABRICATED NEW SEAT TRACK PER SAMPLE AND INSTALLED IAW B727 SRM 513002.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 49,372 hrs · 28,698 cycles

DURING HEAVY MAINTENANCE INSPECTION CORROSION WAS FOUND OUT OF LIMITS ON SEAT TRACK AT BS 344 TO 420 RBL 44. REMOVED CORROSION IAW B727 SRM 511006. REMOVED DAMAGED SECTION IAW B727 SRM 513002. FABRICATED NEW SEAT TRACK PER SAMPLE INSTALLED IAW B727 SRM 513002.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 49,372 hrs · 28,698 cycles

DURING HEAVY MAINTENANCE INSPECTION CORROSION WAS FOUND OUT OF LIMITS AT BS 420 0 BL FLOORBEAM TEE CAP. REMOVED CORROSION IAW B277 SRM 511006. CUT OUT DAMAGED SECTION IAW B727 SRM 531008. FABRICATED REPAIRS IAW B727 SRM 531008. INSTALLED IAW B727 SRM 513002.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 49,372 hrs · 28,698 cycles

DURING HEAVY MAINTENANCE INSPECTION CORROSION WAS FOUND OUT OF LIMITS ON FLOORBEAM TEE CAP AT BS 380 LBL 20 TO RBL 64. REMOVED CORROSION IAW B727 SRM 511006. REMOVED DAMAGED SECTION IAW B727 SRM 513002. FABRICATED REPAIRS AND INSTALLED IAW B727 SRM 513002.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 49,372 hrs · 28,698 cycles

DURING HEAVY MAINTENANCE INSPECTION CORROSION WAS FOUND OUT OF LIMITS BS 400 LBL 20 TO RBL 44 FLOORBEAM TEE CAP. REMOVED CORROSION IAW B727 SRM 511006. REMOVED DAMAGED AREA IAW B727 SRM 531008. REMOVED FLOOR SUPPORT AND INTERCOSTAL IAW B727 SRM 513002. FABRICATED FLOORBEAM REPAIRS IAW B727 SRM 531008. INSTALLED IAW B727 SRM 513002 AND 531008.

Part: OVERHEAT LOOP — DEFECTIVE (OVERHEAT DETECT) · airframe 49,256 hrs · 28,640 cycles

LOWER AFT BODY OVERHEAT LIGHT WILL NOT ILLUMINATE WHEN TEST BUTTON IS PUSHED, WILL ILLUMINATE IF LIGHT IS PUSHED DIRECTLY. CORRECTED BY REMOVING AND REPLACING OVERHEAT DETECTOR.

Part: WARNING SYSTEM — FAILED (COCKPIT) · airframe 48,859 hrs · 28,455 cycles

APU FIRE BELL DID NOT SOUND DURING TEST. REMOVED AND REPLACED WARNING BOX, OPS GOOD.

Part: SWITCH — FAULTY (T/O WARNING SYS) · airframe 48,467 hrs · 28,290 cycles

DURING TAKEOFF ROLL, WHEN THE POWER WAS ADVANCED THE TAKEOFF WARNING HORN SOUNDED. ABORTED TAKEOFF, VERIFIED SPEED BRAKES STOWED, FLAPS 15 DEGREES, TRIM 6.7 AUTOPACK NORMAL. REMOVED AND REPLACED UPPER TAKEOFF WARNING SWITCH (STABILIZERS).

Part: LIGHT — INOPERATIVE (CABIN) · airframe 48,299 hrs · 28,225 cycles

DURING A MAINTENANCE LINE INSPECTION THE EMERGENCY EXIT LIGHT ABOVE 1L WAS FOUND INOPERATIVE. REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT ASSEMBLY AT 1L.

Part: CONTROL UNIT — FAILED (AILERON) · airframe 48,030 hrs · 28,110 cycles

DURING CLIMBOUT FROM LAS THE A-SYSTEM HYDRAULICS FAILED. REMOVED AND REPLACED THE AILERON HYDRAULIC SYSTEM MODULAR UNIT.

Part: COMPRESSOR — STALLED (NR 3 ENGINE) · airframe 27,852 hrs · 47,474 cycles

DURING LANDING ROLL AT MSP SOFT COMPRESSOR STALL ON ENGINE NUMBER THREE. INSPECTED INLETS AND EXAUST ON NUMBER THREE ENGINE. NO DEFECTS NOTED.

Part: BRAKE ASSY — FAILED (MLG) · airframe 47,161 hrs · 27,696 cycles

DURING LANDING THE NUMBER ONE MAIN TIRE FAILED. THE NUMBER ONE BRAKE WAS FOUND LOCKED UP AND DAMAGED THE NUMBER ONE TIRE. REMOVED AND REPLACED THE NUMBER ONE BRAKE AND THE NUMBER ONE AND TWO TIRES. OPERATIONAL CHECKS GOOD.

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 45,601 hrs · 26,984 cycles

DURING A MAINTENANCE LINE CHECK, THE R2 DOOR EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. REMOVED AND REPLACED R2 DOOR EMERGENCY EXIT LIGHT BATTERY PACK. OPERATIONALLY CHECKS GOOD.

Part: LIGHT — INOPERATIVE (AIRSTAIR) · airframe 44,804 hrs · 26,637 cycles

DURING A ROUTINE MAINTENANCE CHECK, THE AFT AIRSTAIR ENTRY DOOR EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. THE AFT ENTRY STAIR DOOR EMERGENCY EXIT LIGHT ASSEMBLY WAS REMOVED AND REPLACED. OPERATIONAL CHECK WAS FOUND GOOD IAW 335000.

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 44,804 hrs · 26,637 cycles

DURING A ROUTINE MAINTENANCE CHECK, THE FOWARD AISLE EMERGENCY EXIT SIGN WAS FOUND AS INOPERATIVE. THE FORWARD AISLE EMERGENCY EXIT SIGN BATTERY PACK (CHARGER) WAS REMOVED AND REPLACED. THE EMERGENCY EXIT SIGN WAS FOUND TO OPERATIONALLY CHECK GOOD IAW 335001.

Part: LIGHT — MISSING (CABIN)

DURING LINE MAINTENANCE CHECK, THE AFT ENTRY OVERHEAD PORTABLE EMERGENCY EXIT LIGHT WAS FOUND MISSING. INSTALLED PORTABLE LIGHT ASSEMBLY IAW MM 3350101. OPERATIONAL CHECKS GOOD.

Part: BATTERY PACK — INOPERATIVE (CABIN)

DURING A HEAVY MAINTENANCE CHECK THE L2 AND R2 DOOR SLIDE LIGHTS WERE FOUND INOPERATIVE. REPLACED BATTERY PACK IAW B727 MM 335051. OPERATIONALLY CHECKS GOOD IAW B727 MM 335001.

Part: LIGHT — INOPERATIVE (CABIN)

DURING A HEAVY MAINTENANCE CHECK, THE R1 DOOR EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. REPLACED R1 DOOR EMERGENCY EXIT LIGHT WITH NEW ONE IAW B727 MM 335001.

Part: WIRE — FAILED (CABIN)

DURING A LINE MAINTENANCE CHECK, THE EMERGENCY EXIT LIGHTING DIM CIRCUIT BREAKER POPPED. RESET AND CIRCUIT BREAKER POPPED AGAIN. REPAIRED SHORT IN LEFT FORWARD OVERWING EXIT LIGHTING. OPERATIONALLY CHECKS GOOD PER IAW MM 332511.

Part: BATTERY PACK — DISCHARGED (R2 DOOR)

DURING A LINE MAINTENANCE CHECK, THE EMERGENCY LIGHTS ABOVE THE R2 DOOR WERE FOUND TO BE INOPERATIVE. REMOVED AND REPLACED THE BATTERY PACK AND POWER SUPPLY AT M1093. ALL EMERGENCY LIGHTING OPERATIONALLY CHECKS GOOD.

Part: BATTERIES — DISCHARGED (AFT AIRSTAIRS)

DURING A LINE MAINTENANCE CHECK, THE AFT AIRSTAIR EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. REMOVED AND REPLACED THE AFT AIRSTAIR EMERGENCY EXIT LIGHT BATTERIES. OPERATIONALLY CHECKS GOOD IAW MM 335071.

Part: BATTERY PACK — DISCHARGED (LT EMER EXIT)

DURING A LINE MAINTENANCE CHECK, THE LEFT MIDDLE OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. REMOVED AND REPLACED BOTH THE BATTERY PACK AND POWER SUPPLY, OPERATIONALLY CHECKS GOOD IAW MM 335100.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING A LINE MAINTENANCE CHECK, THE FORWARD CABIN OVER AISLE EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. REMOVED AND REPLACED THE BATTERY PACK, OPERATIONALLY CHECKS GOOD IAW MM 335100.

Part: SIGN — INOPERATIVE (R1 DOOR)

DURING A LINE MAINTENANCE CHECK, THE R1 DOOR EMERGENCY EXIT SIGN WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPAIRED WIRING AT THE R1 DOOR EXIT SIGN, FUNCTIONALLY CHECKS GOOD.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

DURING A LINE MAINTENANCE CHECK, THE CENTER CABIN OVER AISLE EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. REMOVED AND REPLACED THE EMERGENCY LIGHT POWER SUPPLY, OPERATIONALLY CHECKS GOOD IAW MM 335100.

Part: SEAT TRACK — CORRODED (BS 1090-1130)

DURING A HEAVY LINE MAINTENANCE CHECK, THE SEAT TRACK AT STA 1090 TO 1130 WAS CORRODED OUT OF LIMITS IN VARIOUS PLACES. REMOVED CORROSION FROM SEAT TRACK IAW B727 SRM 531001. FABRICATED NEW SEAT TRACK FROM BAC1520792. TREATED AND PRIMED IAW B727 SRM 511002 AND MM 512002. INSTALLED PER SRM 531005.

Part: BEAM — CORRODED (NLG ACTUATOR)

DURING A HEAVY MAINTENANCE CHECK, FOUND NOSE LANDING GEAR ACTUATOR SUPPORT BEAM LEFT HAND FORWARD MOUNT WITH DEEP PITTED CORROSION. REMOVED SUPPORT IAW B727 SRM 513002. CORROSION WAS FOUND OUT OF LIMITS IAW 727 SRM 531001. FOUND MATERIAL TO BE 7075 T6 IAW WITH CONDUCTIVITY TEST B727 SRM 511003. FABRICATED NEW PART IAW B727 SRM 511003. INSTALLED IAW B727 SRM 513002.

Part: SEAT TRACK — CORRODED (BS 400)

DURING A HEAVY LINE MAINTENANCE CHECK, THE RIGHT HAND OUTBOARD SEAT TRACK AT STA 400 RBL 44 WAS CORRODED OUT OF LIMITS. REMOVED CORROSION FROM SEAT TRACK IAW B727 SRM 531001. FABRICATED NEW SEAT TRACK FROM BAC1520792. TREATED AND PRIMED IAW B727 SRM 511002 AND MM 512002. INSTALLED PER SRM 531005.

Part: FLOORBEAM — CORRODED (BS 380)

DURING A HEAVY LINE MAINTENANCE CHECK, THE FLOORBEAM AT STA 380 RBL 24 THROUGH 30 WAS FOUND CORRODED OUT OF LIMITS. REMOVED CORROSION ON FLOORBEAM IAW B727 SRM 531001. CUT DAMAGED AREA OUT, FABRICATED REPAIR PARTS FROM 7075 T6 BAC 14902831, 14902785, 150051001617, 15123353, 15123396 IAW B727 SRM 531008. TREATED AND PRIMED IAW B727 SRM 511002 AND MM 512002. INSTALLED IAW SRM B727 531008 AND 513002.

Part: SEAT TRACK — CORRODED (BS 1130)

DURING A HEAVY MAINTENANCE CHECK, THE SEAT TRACK AT STA 1130 WAS FOUND CORRODED OUT OF LIMITS AT THE ATTACH POINT TO THE FLOORBEAM. REMOVED CORROSION IAW B727 SRM 531001. FABRICATED NEW SEAT TRACK FOM BAC 1520792 IAW B727 SRM 511001. TREATED AND PRIMED IAW B727 SRM 511002 AND MM 512002. INSTALLED NEW SEAT TRACK IAW B727 SRM 513002.

Part: FLOORBEAM — CORRODED (BS 1110)

DURING A HEAVY MAINTENANCE CHECK, THE FLOORBEAM AT STA 1110 HAS CORRISION OUT OF LIMITS ON THE TOP OF THE FLOORBEAM BETWEEN LT BUTTLINE 24 AND RT BUTTLINE 24. REMOVED CORROSION IAW B727 SRM 531001. FABRICATED NEW FLOORBEAM SUPPORT IAW B727 SRM 531008. TREATED AND PRIMED IAW B727 SRM 511002 AND MM 512002. INSTALLED IAW B727 SRM 513002.

Part: SKIN — CORRODED (EMER EXIT DRWAY)

DURING A HEAVY MAINTENANCE CHECK, FOUND CORROSION IN THE MAIN CABIN LEFT HAND AFT EMERGENCY EXIT HATCH AT THE LOWER FORWARD CORNER OF CUTOUT. REMOVED CORROSION IAW SRM B727 511006. CORROSION WAS FOUND OUT OF LIMITS PER SRM B727 531001. FABRICATED DOUBLER FROM 301 1/2 HARD STEEL .125 IAW SRM 533003. ALODINED AND PRIMED IAW B727 SRM 511002 AND MM 512002. INSTALLED IAW B727 SRM 533003.

Part: LIGHT — INOP (R1 DOOR)

DURING A LINE MAINTENANCE CHECK, THE R1 DOOR EXTERIOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. RELAMPED THE R1 DOOR EXTERIOR EMERGENCY LIGHT. LIGHT OPERATIONALLY CHECKS GOOD.

Part: WIRE — FAILED (CABIN)

DURING A LINE MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTING WAS FOUND TO BE INOPERATIVE IN THE AFT SECTION OF THE CABIN. REMOVED AND REPLACED SUPPLY WIRES UNDER CARPET TO SIDEWALL. OPERATIONALLY CHECKS GOOD.

Part: LIGHT — INOP (L1 DOOR)

DURING A LINE MAINTENANCE CHECK, THE L1 EMERGENCY SLIDE LIGHT WAS FOUND TO BE INOPERATIVE. REMOVED AND REPLACED THE BULB, OPERATIONALLY CHECKS GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING A LINE MAINTENANCE CHECK, THE LEFT NR 2 LEFT OVERWING EXTERIOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. REMOVED AND REPLACED THE NR 2 LEFT OVERWING EXTERIOR EMERGENCY LIGHT BATTERY PACK. OPERATIONALLY CHECKS NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING A LINE MAINTENANCE CHECK, THE EMERGENCY LIGHTS OVER BOTH RIGHT OVERWING EXITS WERE FOUND TO FLASH ON AND OFF. REMOVED AND REPLACED THE BATTERY PACK AND OPERATIONALLY CHECKS GOOD.

Part: ACTUATOR — FAILED (NR 8 LE FLAP)

ON CLIMB, THE NUMBER EIGHT LEADING EDGE SLAT WOULD NOT RETRACT ON SCHEDULE. TWO ATTEMPTS WERE MADE TO RECYCLE FLAPS AS PER COM PROCEDURE BUT THE NUMBER EIGHT SLAT REMAINED FULLY EXTENDED AS CONFIRMED BY VISUAL INSPECTION. FOUND THE LEADING EDGE NUMBER EIGHT SLAT ACTUATOR STICKING. REMOVED AND REPLACED THE ACTUATOR IN ACCORDANCE WITH MAINTENANCE MANUAL CHAPTER 278132. OPERATIONAL AND LEAK CHECK GOOD.

Part: BULB — FAILED (CABIN)

DURING A MAINTENANCE CHECK, ONE BULB FOR THE EMERGENCY LIGHT IN THE AFT CARGO DOOR WAS FOUND TO BE INOPERATIVE. RELAMPED LIGHT BULB AND OPERATIONALLY CHECKS GOOD.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

DURING A MAINTENANCE CHECK, THE R1 AND R2 DOOR SLIDE EMERGENCY EXIT LIGHTS WERE FOUND TO BE INOPERATIVE. REMOVED AND REPLACED THE BATTERY AND POWER SUPPLY ASSEMBLY AT M982. ALL EMERGENCY LIGHTS OPERATIONALLY CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING A MAINTENANCE CHECK, THE LEFT AFT OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. REMOVED AND REPLACED BATTERY PACK AND OPERATIONALLY CHECKS GOOD.

Part: BATTERIES — DISCHARGED (CABIN)

DURING A MAINTENANCE CHECK, THE LEFT FUSELAGE EMERGENCY LIGHT FOR THE OVERWING EXIT WOULD NOT TEST. PLACED THE COCKPIT EMERGENCY EXIT LIGHT SWITCH IN THE ARM POSITION FOR SEVERAL MINUTES TO ALLOW AIRCRAFT TO CHARGE BATTERIES. TEST CHECKED GOOD FOLLOWING CHARGE CYCLE.

Part: BLADE — DAMAGED (NR 2 ENGINE)

THE NUMBER 2 ENGINE WAS SHUTDOWN DUE TO ENGINE VIBRATION AND LOSS OF N1 INDICATION. BORESCOPE INSPECTION OF THE NUMBER 2 ENGINE REVEALED A DAMAGED LPT BLADE. REMOVED AND REPLACED ENGINE PER B727 MM 71-00.

Part: INTERCOSTAL — CORRODED (BS 344)

DURING HEAVY MAINTENANCE VISIT, FOUND FLOOR BOARD SUPPORT INTERCOSTAL CORRODED BEYOND LIMTS AT FS 344, LBL 30. REMOVED DAMAGED SUPPORT, FABRICATED AND INSTALLED A NEW SUPPORT IN ACCORDANCE WITH SRM 53-10-2, 51-20-1, 51-10-2 AND 51-30-2.

Part: SUPPORT — CORRODED (BS 1130-1140)

DURING HEAVY MAINTENANCE VISIT, FOUND A FLOOR SUPPORT AT FS 1130 TO 1148, LBL 10, CORRODED BEYOND LIMITS. REMOVED DAMAGED PARTS, FABRICATED AND INSTALLED REPAIR PARTS IN ACCORDANCE WITH SRM 53-10-2, 51-10-2, AND 51-40-5.

Part: ANGLE — CORRODED (DOOR SILL)

DURING HEAVY MAINTENANCE VISIT, FOUND CORROSION ON ATTACHMENT HOLES FOR THE LEFT AFT GALLEY SERVICE DOOR LOWER SILL. REMOVED DOOR SILL ANGLE, FABRICATED AND INSTALLED REPLACEMENT PART IAW SRM 51-40-3.

Part: SUPPORT — CORRODED (BS 400)

DURING HEAVY MAINTENANCE VISIT, A FLOORBEAM SUPPORT AT FS 400, RBL 10 WAS FOUND CORRODED BEYOND LIMITS. FABRICATED AND INSTALLED A REPAIR IN ACCORDANCE WITH SRM 53-10-8, FIGURE 3.

Part: SEAT TRACK — CORRODED (BS 1020)

DURING HEAVY MAINTENANCE VISIT, THE NUMBER 2 SEAT TRACK AT FS 1010 TO 1030, LBL 24 WAS FOUND CORRODED BEYOND LIMITS. REMOVED CORRODED SECTION OF TRACK, SPLICED IN NEW SECTION OF TRACK IN ACCORDANCE WITH SRM 53-10-5.

Part: SEAT TRACK — CORRODED (BS 1010-1030)

DURING HEAVY MAINTENANCE VISIT, THE NUMBER 1 SEAT TRACK AT FS 1010 TO 1030, LBL 48, WAS FOUND CORRODED BEYOND LIMITS. REMOVED CORRODED SECTION OF TRACK, SPLICED IN NEW SECTION OF TRACK IN ACCORDANCE WITH SRM 53-10-5.

Part: SEAT TRACK — CORRODED (BS 400-420)

DURING HEAVY MAINTENANCE VISIT, THE NUMBER 5 SEAT TRACK AT FS 400 TO 420, RBL 48 WAS FOUND CORRODED BEYOND LIMITS. REMOVED CORRODED SECTION OF TRACK, SPLICED IN NEW SECTION OF TRACK IN ACCORDANCE WITH SRM 53-10-5.

Part: STIFFENER — CORRODED (CABIN)

DURING HEAVY MAINTENANCE VISIT, FOUND A STIFFENER JUST AFT OF THE LEFT LAV FLOOR PAN WITH CORROSION BEYOND LIMITS. REMOVED CORRODED SECTION, FABRICATED AND INSTALLED A REPAIR IN ACCORDANCE WITH SRM 51-40-2.

Part: FLAP — CORRODED (NR 4 LE SLAT)

DURING HEAVY MAINTENANCE VISIT, FOUND CORROSION BEYOND LIMITS ON NUMBER 4 KRUEGER FLAP OUTBOARD RIB. REMOVED AND REPLACED NUMBER 4 KRUEGER FLAP PER MM 27-81-1.

Part: SILL — CORRODED (L2 DOOR)

DURING HEAVY MAINTENANCE VISIT, DISCOVERD EXTENSIVE CORROSION AT THE L2 SERVICE DOOR AREA. CORROSION WAS COMMON TO DOOR SILL AND FLOOR STRUCTURE. CLEANED UP CORROSION, REMOVED AND REPLACED COMPONENTS AS NECESSARY.

Part: LAV PAN — CORRODED (BS 303)

DURING HEAVY MAINTENANCE VISIT, FOUND CORROSION BEYOND LIMITS ON FORWARD LAV PAN, FS 303, RBL 20. REMOVED PAN, FABRICATED AND INSTALLED NEW PAN IN ACCORDANCE WITH SRM 51-30-2, 52-20-1 AND 51-30-2.

Part: WEB — CRACKED (CABIN)

DURING HEAVY MAINTENANCE VISIT, A WEB WAS FOUND CRACKED JUST FWD OF THE AFT PRESSURE BULKHEAD, AND JUST AFT OF THE AFT LEFT LAV FLOOR PAN. FABRICATED AND INSTALLED REPAIR ANGLES IN ACCORDANCE WITH SRM 51-40-2.

Part: SIGN — BROKEN (CABIN)

THE L1 DOOR EMERGENCY EXIT SIGNS WERE FOUND BROKEN. INSTALLED 2 NEW EMERGENCY EXIT SIGN, OPS CHECKED NORMAL.

Part: COMPRESSOR — FAILED (NR 2 ENGINE)

THE NUMBER 2 ENGINE COMPRESSOR STALLED AT FL 350. STALLS CONTINUED DURING DESCENT THEREFORE ENGINE WAS SHUTDOWN. REMOVED AND REPLACED NUMBER 2 ENGINE DUE TO STAGE 6 COMPRESSOR BLADE LIBERATION.

Part: MOUNT — LOOSE FASTENER (1/3 ENGINES)

THE NUMBER 1 AND 3 ENGINE FORWARD MOUNT UPPER FLANGES WERE FOUND TO HAVE 1 LOOSE HI-LOK FASTENER EACH AT ENGINE STATION 146. REMOVED FASTENERS AND REAMED HOLES PER SUN COUNTRY ENGINEERING ORDER, PERFORMED HFEC ON OPEN HOLES, NO CRACKS NOTED. INSTALLED REPLACEMENT FASTENERS.

Part: BATTERY PACK — DISCHARGED (CABIN)

EMERGENCY LIGHT PORTION OF DUAL LIGHTED EXIT SIGN, ON CEILING BETWEEN OVERWING EXITS, WAS FOUND INOPERATIVE. REPLACED BATTERY PACK, EXIT SIGN TESTED GOOD PER B727 MM 33-50-71.

Part: LIGHT — DAMAGED (CABIN)

THE FORWARD CABIN FLOOR TRACK LIGHTING WAS FOUND INOPERATIVE. REPLACED EMERGENCY LIGHT SEGMENT AT ROW 4, LIGHT CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN)

EMERGENCY FLOOR TRACK LIGHTING IS INOP FROM SEAT ROW 23 TO ROW 29. REMOVED AND REPLACED FEEDER STRIP FROM WALL, OPS CHECKED GOOD IN ACCORDANCE WITH 30-50-00.

Part: BATTERY PACK — DISCHARGED (CABIN)

FOUND AFT AIRSTAIR EMERGENCY LIGHT INOP. REPLACED AFT AIRSTAIR EMERGENCY LIGHT BATTERIES AND OPS CHECKED GOOD IN ACCORDANCE WITH MM 33-50-01.

Part: LIGHT — INOPERATIVE (CABIN)

FOUND AFT SELF CONTAINED EMERGENCY LIGHT BATTERIES DISCHARGED AND LIGHT INOP. REMOVED AND REPLACED EMERGENCY LIGHT.

Part: STRINGER — CORRODED (BS 950)

DURING HEAVY MAINTENANCE VISIT, CORROSION WAS FOUND ON STRINGER 29R BETWEEN STATION 950A AND STATION 950C. REPAIR WAS ACCOMPLISHED PER ENGINEERING AUTHORIZATION INSTRUCTIONS.

Part: CONNECTOR — DIRTY (TE FLAPS)

SPLIT FLAP INDICATION, INBOARD FLAP INDICATED 3 DEGREES. AIRCRAFT DIVERTED TO TULSA FOR MAINTENANCE. OPERATED BYPASS ACTUATOR DRIVE TO FULL UP, CLEANED AND RECONNECTED BYPASS CANNON PLUG, OPERATED SYSTEM IN BOTH NORMAL AND ALTERNATE THREE TIMES EACH. NO BINDING, ASSYMETRY, OR SPLIT NOTICED AND ALL HARDWARE INTACT. OPERATES NORMAL PER MM 27-51-0.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

EMERGENCY FLOOR TRACK LIGHTING WAS FOUND INOP AT ROWS 9 THROUGH 16. REMOVED AND REPLACED BATTERY (P/N 5776-1) AND POWER SUPPLY (P/N 5822-14) AND REPLACED EMERGENCY LIGHT TRACK LEAD ASSEMBLY, OPS CHECKED NORMAL.

Part: BULB — FAILED (CABIN)

LEFT FORWARD OVERWING EXIT SIGN HAS BULBS BURNT OUT. RELAMPED SIGN AND OPS CHECKED NORMAL.

Part: BULB — FAILED (CABIN)

EXIT SIGN OVER AFT LEFT ENTRY DOOR WAS FOUND WITH TWO BULBS INOP. RELAMPED SIGN AND OPS CHECKED GOOD.

Part: BULB — FAILED (CABIN)

CENTER AISLE OVERHEAD EXIT SIGN HAS TWO BULBS INOP. RELAMPED AND OPS CHECKED GOOD.

Part: EMERGENCY LIGHT — INOPERATIVE (CABIN)

RIGHT FORWARD OVERWING, FORWARD LOWER EMERGENCY LIGHT FOUND INOPERATIVE. REMOVED AND REPLACED BROKEN TERMINAL, OPS CHECKED GOOD.

Part: BULB — FAILED (CABIN)

CENTER AISLE EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. REMOVED AND REPLACED BULBS, OPS CHECK OK.

Part: BATTERY PACK — DISCHARGED (CABIN)

AFT FLOOR TRACK EMERGENCY LIGHTS ARE VERY DIM. REMOVED AND REPLACED BATTERY PACK. SYSTEM OPS CHECKED NORMAL IAW 33-50-01.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING LINE CHECK, THE EMERGENCY EXIT LIGHT AT THE LOWER AFT AIRSTAIR DOOR, L-2 LOWER EXIT LIGHT AND FLOOR TRACK LIGHTING FROM SEAT 30 TO 34 CAME ON MOMENTARILY AND THEN WENT OUT. REMOVED AND REPLACED BATTERY PACK IAW MM 33-50-01 AND EMERGENCY LIGHTS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN)

THE CENTER SECTION OF EMERGENCY TRACK LIGHTING WAS FOUND TO BE INOPERATIVE. REMOVED AND REPLACED BATTERY PACK, LIGHTING TESTED GOOD IAW MM 33-50-00.

Part: BATTERY PACK — DISCHARGED (CABIN)

THE MID-CABIN FLOOR TRACK LIGHTING WAS FOUND TO BE INOPERATIVE. REMOVED AND REPLACED MID-CABIN FLOOR TRACK LIGHTING BATTERY PACK AND SYSTEM CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN)

THE R-2 DOOR EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. REMOVED AND REPLACED BATTERY PACK AT THE TOP OF THE R-2 DOOR AND LIGHT TESTED GOOD IAW MM 33-50-01.

Part: EEL — INOPERATIVE (CABIN)

THE EMERGENCY FLOOR TRACK LIGHTING WAS FOUND TO BE INOPERATIVE BETWEEN ROW 16 TO ROW 19. ALL CONNECTIONS WERE CHECKED, REMOVED DEBRIS AND WIPED UP MOISTURE FROM EMERGENCY FLOOR TRACK AND LIGHTS TESTED NORMAL.

Part: EEL WIRING — DAMAGED (CABIN)

EMERGENCY PATH LIGHTING WAS FOUND INOPERATIVE IN THE FORWARD SECTION OF THE CABIN. A BROKEN FEEDER WIRE WAS FOUND DAMAGED. REPAIRED WIRE AND THE EMERGENCY PATH LIGHTING TESTED GOOD.

Part: DOUBLER — CRACKED (RT ELEVATOR)

DURING C-CHECK, A CRACKED DOUBLER WAS FOUND ON THE RIGHT ELEVATOR REAR SPAR JUST ABOVE THE CONTROL ROD. REMOVED CRACKED DOUBLER, FABRICATED AND INSTALLED NEW DOUBLER IAW B727 SRM 55-26-01.

Part: EEL POWER SUPPLY — MALFUNCTIONED (CABIN)

THE LEFT AFT TRACK LIGHTING WAS FOUND TO BE DIM WHEN CHECKED. REMOVED AND REPLACED POWER SUPPLY M9204 AND PERFORMED OPERATIONAL TEST IAW MM 33-50-01 PAGE 501, LIGHTS CHECKED GOOD.

Part: EEL POWER PACK — FAILED (CABIN)

THE FORWARD CABIN CEILING MOUNTED EMERGENCY AREA LIGHT WAS FOUND TO BE INOPERATIVE. REMOVED AND REPLACED THE OVERHEAD EMERGENCY AREA LIGHT POWER PACK IAW MM 33-50-81 AND THE LIGHT TESTED GOOD.

Part: EEL BATTERY PACK — DISCHARGED (CABIN)

THE AFT SECTION OF EMERGENCY FLOOR TRACK LIGHTING WAS FOUND TO BE INOPERATIVE. REMOVED AND REPLACED THE AFT BATTERY PACK AND LIGHTS, OPS CHECKED NORMAL.

Part: LOCK ACTUATOR — BROKEN (NOSE GEAR)

NOSE GEAR DID NOT EXTEND DURING GEAR EXTENSION, A-SYSTEM HYDRAULIC INDICATIONS WERE NORMAL. NOSE GEAR WAS EXTENDED MANUALLY. NOSE GEAR LOCK ACTUATOR WAS FOUND BROKEN. REMOVED AND REPLACED NOSE GEAR LOCK ACTUATOR AND PERFORMED EMERGENCY EXTENSION CHECK AND RESET MANUAL EXTENSION SYSTEM PER MM 32-33-11.

Part: EEL BATTERY — DISCHARGED (CABIN)

FOUND THE ZONE 5 EMERGENCY FLOOR TRACK LIGHTING INOPERATIVE. REMOVED AND REPLACED EMERGENCY BATTERY AT ZONE 5 AND FLOOR TRACK LIGHTING TESTED GOOD PER MM 33-50-01.

Part: OVEN — FAULTY (AFT GALLEY)

AFT OVEN SWITCHED OFF WHILE COOKING MEALS, AFTER REMOVING MEALS, OVEN BEGAN TO SMOKE AND SMELL BURNED. REMOVED AND REPLACED OVEN AND UNIT CHECKED GOOD.

Part: EEL BATTERY — DISCHARGED (CABIN)

EMERGENCY EXIT SIGN ABOVE R-2 DOOR FOUND TO BE INOPERATIVE. REPLACED BATTERY PACK AND LIGHT OPS CHECKED GOOD.

Part: EEL POWER SUPPLY — FAILED (CABIN)

MSP - THE L1 AND R1 EMERGENCY ESCAPE SLIDE LIGTHS INOPERATIVE. REMOVED AND REPLACED ESCAPE SLIDE LIGHT POWER SUPPLY M982. (W)

Part: EEL ASSY — FAILED (COCKPIT)

MSP - EMERGENCY LIGHT OVER COCKPIT DOOR IS INOPERATIVE. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSEMBLY OVER COCKPIT DOOR. OPERATIONAL CHECK GOOD PER 33-50-00. (W)