N289SC

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 44,912 hrs · 27,448 cycles

DURING A MAINTENANCE LINE CHECK THE EMERGENCY LIGHT ABOVE THE L2 DOOR WAS FOUND INOPERATIVE. REMOVED AND REPLACED THE BATTERY AND CHARGER PACK, OPERATIONAL CHECKS GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 44,912 hrs · 27,448 cycles

DURING A LINE MAINTENANCE CHECK THE EMERGENCY EXIT LIGHT ABOVE THE L2 DOOR WAS FOUND TO BE INOPERATIVE. REMOVED AND REPLACED THE BATTERY PACK AND CHARGER, OPERATIONAL CHECKS GOOD.

Part: SWITCH — FAILED (NR 6 LE FLAP) · airframe 44,653 hrs · 27,321 cycles

AFTER TAKEOFF UPON FLAP RETRACTION, THE NUMBER 6 LEADING EDGE FLAP FAILED TO RETRACT WHEN GOING FROM 5 TO 2. REMOVED AND REPLACED F207 SWITCH ON NR 6 LEADING EDGE FLAP, CYCLED SEVERAL TIMES WITH GOOD INDICATION.

Part: LIGHT — INOPERATIVE (AIRSTAIR) · airframe 44,510 hrs · 27,250 cycles

DURING A MAINTENANCE LINE CHECK THE AFT AIRSTAIR EMERGENCY LIGHTS WERE FOUND TO BE WEAK. REMOVED AND REPLACED THE AIRSTAIR EMERGENCY LIGHT ASSEMBLY, OPERATIONAL CHECKS GOOD.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 44,429 hrs · 27,211 cycles

DURING HEAVY MAINTENANCE INSPECTION CORROSION WAS FOUND OUT OF LIMITS ON THE SEAT TRACK LOCATED AT FS 1030 RBL 55. REMOVED CORROSION IAW B727 SRM 511006. FABRICATED NEW SEAT TRACK PER SAMPLE FORM BAC 1520792. TREATED AND PRIMED IAW B727 SRM 511002 AND MM 512002. INSTALLED IAW B727 SRM 513002.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 44,429 hrs · 27,211 cycles

DURING HEAVY MAINTENANCE INSPECTION CORROSION WAS FOUND OUT OF LIMITS ALONG THE INNER RECESS AND TEE CAP OF THE INBOARD SEAT TRACK AT STA 340 THROUGH 415. REMOVED CORROSION IAW B727 SRM 511006. FABRICATED NEW SEAT TRACK PER SAMPLE FROM BAC 1520792. TREATED AND PRIMED IAW B727 SRM 511002 AND MM 512002. INSTALLED IAW B727 SRM 513002.

Part: SKIN — CORRODED (FUSELAGE) · airframe 44,429 hrs · 27,211 cycles

DURING C/D CHECK, CORROSION WAS FOUND OUT OF LIMITS ON THE WING CENTER SECTION LOWER SKIN, BETWEEN STATION 834 AND 843, BETWEEN RBL 17 AND RBL 35. REMOVED CORROSION PER B727 SRM 511006. FABRICATED REPAIR DOUBLER FROM 7075 T6 .063 AND TRIPLER FROM 7075 T6 .071. TREATED AND PRIMED IAW B727 SRM 511002 AND MM 513002. INSTALLED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 44,429 hrs · 27,211 cycles

DURING HEAVY MAINTENANCE INSPECTION CORROSION WAS FOUND TO BE OUT OF LIMITS ALONG THE RECESS AND TEE CAP ON THE OUTBOARD SEAT TRACK AT STA 340 THROUGH 360. REMOVED CORROSION IAW B727 SRM 511006. REMOVED SEAT TRACK IAW B727 SRM 513002. FABRICATED NEW SEAT TRACK PER SAMPLE FROM BAC1520792. TREATED AND PRIMED IAW B727 SRM 511002 AND MM 512002. INSTALLED IAW B727 SRM 513002.

Part: FRAME — CORRODED (CARGO BAY) · airframe 44,429 hrs · 27,211 cycles

DURING HEAVY MAINTENANCE INSPECTION CORROSION WAS FOUND OUT OF LIMITS IN THE AFT CARGO PIT FWD SIDE OF BS 1070 BETWEEN STR 28 AND 29R. REMOVED CORROSION IAW B727 SRM 511006. FABRICATED DOUBLER FROM 7075 T6 .080 IAW B727 SRM 514003. TREATED AND PRIMED IAW B727 SRM 511002 AND MM 512002. INSTALLED IAW B727 SRM 513002.

Part: FLOORBEAM — CORRODED (CABIN) · airframe 44,429 hrs · 27,211 cycles

DURING HEAVY MAINTENANCE CHECK, CORROSION WAS FOUND OUT OF LIMITS AT L1 DOOR ENTERANCE, FLOORBEAM, STA 340, UPPER CHORD, FROM LT INBOARD SEAT TRACK TO ENTRANCE SCUPPER PLATE. REMOVED CORROSION IAW B727 SRM 511006. FABRICATED ONE UPPER CHORD FROM BAC 1505100617, ONE ANGLE FROM BAC 14902785, ONE ANGLE FROM BAC 14902831, ONE STRAP FROM BAC 15123396 AND ONE STRAP FROM BAC 15123353 IAW B727 SRM 531008. TREATED AND PRIMED IAW B727 SRM 511002 AND MM 512002. INSTALLED IAW B727 SRM 531008 AND 513002.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 44,429 hrs · 27,211 cycles

DURING HEAVY MAINTENANCE INSPECTION CORROSION WAS FOUND OUT OF LIMITS IN THE AFT GALLEY ENTRY WAY LT SIDE FS 1020 TO 1072 FLOORBOARD SUPPORT BEAM ANGLE. REMOVED CORROSION IAW B727 SRM 511006. FABRICATED NEW ANGLE PER SAMPLE FROM BAC14902831. TREATED AND PRIMED IAW B727 SRM 511002 AND MM 512002. INSTALLED IAW B727 SRM 513002.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 44,429 hrs · 27,211 cycles

DURING HEAVY MAINTENANCE INSPECTION CORROSION WAS FOUND OUT OF LIMITS IN THE AFT CARGO COMPARTMENT CEILING AT STA 1070 FLOORBEAM LOWER SIDE FROM LBL 24 TO RBL 46. REMOVED CORROSION IAW B727 SRM 511006. REMOVED FLOORBEAM IAW B727 SRM 531008. FABRICATED FLOORBEAM FROM 7075 T6 .125, BAC 14902831 IAW B727 SRM 531008. TREATED AND PRIMED IAW B727 SRM 511002 AND MM 512002. INSTALLED IAW B727 SRM 531008.

Part: LIGHT — INOPERATIVE (OVERWING) · airframe 43,293 hrs · 26,730 cycles

DURING A MAINTENACE LINE CHECK, THE LEFT HAND AFT OVERWING EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE LEFT HAND OVERWING AFT LAMP WAS REMOVED AND REPLACED, AND OPERATIONALLY CHECKS GOOD.

Part: LIGHT — INOPERATIVE (ROW 30) · airframe 43,165 hrs · 26,681 cycles

DURING A LINE MAINTENACE CHECK, THE EMERGENCY FLOOR TRACK LIGHTING AT SEAT 30 ABC WAS FOUND INOPERATIVE. REMOVED AND REPLACED THE EMERGENCY FLOOR PATH LIGHTING STRIP AT SEATS 30 ABC, OPERATIONAL CHECK GOOD.

Part: HARNESS — INOPERATIVE (ROWS 1 - 15)

DURING A LINE MAINTENANCE CHECK, THE EMERGENCY FLOOR PATH LIGHTING FROM ROWS 1 THROUGH 15 WAS FOUND INOPERATIVE. REMOVED AND REPLACED ELECTRICAL HARNESS AT 3A. ALL EMERGENCY LIGHTS CHECK GOOD.

Part: VALVE — FAILED (CABIN PRESSURE)

APPROXIMATELY FIVE MINUTES AFTER LEVEL OFF AT 31,000 FEET, CABIN BEGAN TO DEPRESSURIZE RAPIDLY. CABIN RATE INDICATOR PEGGED AT MAXIMUM RATE OF CLIMB, SWITCHED TO MANUAL OUTFLOW VALVE INDICATOR AT FULL CLOSED POSITION RATE OF CLIMB CONTINUED AT MAXIMUM RATE OF CLIMB. PERFORMED RAPID DEPRESSURIZATION CHECKLIST AND COULD NOT STABILIZE CABIN ALTITUDE. PERFORMED RAPID DESCENT CHECKLIST AND LANDED. REMOVED AND REPLACED SAFETY OVERPRESSURE VALVE. PRESSURIZED AIRCRAFT TO 9.4 DIFFERENTIAL. OPERATIONALLY CHECKS NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING A LINE MAINTENANCE CHECK, THE L2 EMERGENCY OVERHEAD DOOR LIGHT FLASHES WHEN TESTED. REMOVED AND REPLACED THE L2 EMERGENCY DOOR LIGHT BATTERY PACK, OPERATIONALLY CHECKS NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING A LINE MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTING WAS FOUND TO BE VERY DIM. FOUND AFT TWO BATTERY PACKS NOT WIRED TO FLOOR TRACK. INSTALLED MISSING WIRE FROM PACKS AT 19ABC AND 24ABC. ALSO, REPLACED BATTERY PACK AT 24ABC. OPERATIONALLY CHECKS GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING A LINE MAINTENANCE CHECK, THE MIDDLE OVERWING EXTERIOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE ON THE LEFT SIDE OF THE AIRCRAFT. REPAIRED CHAFED WIRE TO THE LIGHT ASSEMBLY AND REPLACED THE BATTERY PACK. OPERATIONALLY CHECKS GOOD.

Part: LIGHT — INOPERATIVE (AIRSTAIR)

DURING A LINE MAINTENANCE CHECK, AN EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE IN THE AFT AIRSTAIR AREA. REMOVED AND REPLACED THE EMERGENCY LIGHT ASSEMBLY IN THE AFT AIRSTAIR AREA IAW MM 335061. OPERATIONALLY CHECKS GOOD.

Part: EXIT SIGN — INOPERATIVE (CABIN)

DURING A HEAVY MAINTENANCE CHECK, THE LEFT AFT OVERWING EXIT DOOR SELF LUMINESECNT PULL SIGN FAILS BRIGHTNESS INSPECTION. REMOVED AND REPLACED AFT OVERWING EXIT DOOR SELF LUMINESCENT PULL SIGN IAW B727 MM 335031.

Part: EXIT SIGN — INOPERATIVE (CABIN)

DURING A HEAVY MAINTENANCE CHECK THE RIGHT AFT OVERWING EXIT DOOR SELF LUMINESCENT EMERGENCY SIGN FAILS BRIGHTNESS INSPECTION. REMOVED AND REPLACED THE AFT OVERWING EXIT DOOR SELF LUMINESCENT EMERGENCY SIGN IAW B727 MM 335031.

Part: EXIT SIGN — INOPERATIVE (CABIN)

DURING A HEAVY MAINTENANCE CHECK, THE RIGHT FORWARD OVERWING EXIT DOOR SELF LUMINESCENT PULL SIGN FAILS BRIGHTNESS INSPECTION. REMOVED AND REPLACED FORWARD OVERWING EXIT DOOR SELF LUMINESCENT PULL SIGN IAW B727 MM 335031.

Part: EXIT SIGN — INOPERATIVE (CABIN)

DURING A HEAVY MAINTENANCE CHECK, THE LEFT AFT OVERWING EXIT DOOR SELF LUMINESCENT EMERGENCY SIGN FAILS BRIGHTNESS INSPECTION. REMOVED AND REPLACED THE AFT OVERWING EXIT DOOR SELF LUMINESCENT EMERGENCY SIGN IAW B727 MM 335031.

Part: EXIT SIGN — INOPERATIVE (CABIN)

DURING A HEAVY MAINTENANCE CHECK, THE LEFT FORWARD OVERWING EXIT DOOR SELF LUMINESCENT PULL SIGN FAILS BRIGHTNESS INSPECTION. REPLACED LEFT FORWARD OVERWING EXIT DOOR SELF LUMINESCENT PULL SIGN IAW B727 MM 335031.

Part: EXIT SIGN — INOPERATIVE (CABIN)

DURING A HEAVY MAINTENANCE CHECK THE RIGHT AFT OVERWING EXIT DOOR SELF LUMINESCENT PULL SIGN FAILS BRIGHTNESS INSPECTION. REPLACED THE RIGHT AFT OVERWING EXIT DOOR SELF LUMINESCENT PULL SIGN IAW B727 MM 335031.

Part: BATTERY PACK — DISCHARGED (BS 480)

DURING A HEAVY MAINTENANCE CHECK, THE EMERGENCY BATTERY PACK FOR THE EXIT LIGHT AT STA 480 WAS FOUND TO BE INOPERATIVE. REMOVED AND REPLACED THE BATTERY PACK IAW B727 MM 335071, OPERATIONALLY CHECKS GOOD IAW B727 MM 335001.

Part: FLOORBEAM — CORRODED (BS 1130)

DURING A HEAVY MAINTENANCE CHECK, CORROSION WAS FOUND AROUND THE NUT CLIP HOLE AT THE BOTTOM OF THE MAIN CABIN FLOOR T CAP AT STA 1130 BETWEEN LBL 15 AND RBL 15 IN THE AFT CARGO COMPARTMENT. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. FABRICATED REPAIR ANGLES AND FILLER FROM 7075 T6. TREATED, PRIMED AND INSTALLED PER SRM 51102 AND MM 51202.

Part: FLOORBEAM — CORRODED (BS 1166)

DURING A HEAVY MAINTENANCE CHECK, THE LEFT AFT LAVATORY AT FLOORBEAM STA 1166 HAD ELONGATED HOLE IN THE LAVATORY FLOOR STRUCTURE. REMOVED DAMAGED AREA IAW SRM 51402. FABRICATED DOUBLER IAW SRM 51402 FROM 7075 T6 .063. TREATED, PRIMED AND INSTALLED REPAIR DOUBLER IAW SRM 51102 AND MM 51202.

Part: FRAME — CORRODED (BS 1183)

DURING A HEAVY MAINTENANCE CHECK, THE AFT ENTRY DOOR LOWER RIGHT SIDE AT THE FLOOR LEVEL EXHIBITS A LARGE AREA OF CORROSION AT STA 1183. REMOVED CORROSION, REPAIRED DAMAGED FRAME AND FRAME SPLICE IAW SRM 51302.

Part: BRACKET — CORRODED (BS 1130)

DURING A HEAVY MAINTENANCE CHECK, THE RIGHT AFT LAVATORY FLOORBEAM AT STA 1130 WAS FOUND TO EXHIBIT A CORRODED BRACKET. REMOVED CORROSION IAW SRM 51106. MATERIAL CORRODED OUT OF LIMITS. FABRICATED A NEW ANGLE FROM 7075 T6. TREATED AND INSTALLED NEW BRACKET PER 51302 AND 51202.

Part: SEAT TRACK — CORRODED (BS 1064)

DURING HEAVY MAINTENANCE CHECK, CORROSION WAS FOUND OUT OF LIMITS ON SEAT TRACK AT STA 1064 RBL 44, FLANGE BROKEN. REMOVED SEAT TRACK IAW SRM 513002. FABRICATED NEW SEAT TRACK PER SAMPLE FROM BAC 1520792. TREATED AND PRIMED IAW SRM 511002, MM 512002. INSTALLED IAW SRM 513002.

Part: SEAT TRACK — CORRODED (BS 380)

DURING HEAVY MAINTENANCE CHECK, CORROSION WAS FOUND OUT OF LIMITS ON FLOORBOARD SUPPORT ANGLE BETWEEN STA 380 AND 420, RBL 26. REMOVED CORROSION IAW SRM 511006. FABRICATED NEW SEAT TRACK PER SAMPLE FROM BAC 1520792. TREATED AND PRIMED IAW SRM 511002, MM 512002. INSTALLED IAW SRM 513002.

Part: FLOORBEAM — CORRODED (BS 1110)

DURING HEAVY MAINTENANCE CHECK, CORROSION WAS FOUND OUT OF LIMITS ON BOTTOM FWD FLANGE OF MAIN FLOOR T-CAP AROUND NUT CLIP HOLES, FS 1110 BL 0. REMOVED CORROSION IAW SRM 511006. REMOVED DAMAGED AREA, FABRICATED 2 ANGLES FROM BAC 14902831, FABRICATED 1 FILLER FROM 7075 T6 .125 IAW SRM 531008. TREATED AND PRIMED IAW SRM 511002, MM 512002. INSTALLED IAW SRM 531008 AND 513002.

Part: SEAT TRACK — CORRODED (BS 1050&1070)

DURING HEAVY MAINTENANCE CHECK, CORROSION WAS FOUND OUT OF LIMITS ON SEAT TRACK ANGLE BETWEEN FS 1050 AND 1070 RBL 26. REMOVED CORROSION IAW SRM 511006. FABRICATED NEW SEAT TRACK PER SAMPLE FROM BAC 1520792. TREATED AND PRIMED IAW SRM 511002, MM 512002. INSTALLED IAW SRM 513002.

Part: ANGLE — CORRODED (BS 1050)

DURING HEAVY MAINTENANCE CHECK, CORROSION WAS FOUND OUT OF LIMITS ON LONGITUDINAL FLOORBOARD SUPPORT ANGLE, FS 1050 LBL 15. REMOVED CORROSION IAW SRM 511006. REMOVED FLOORBOARD SUPPORT IAW B727 SRM 513002. FABRICATED NEW FLOORBOARD SUPPORT FROM BAC 15064417 PER SAMPLE. TREATED IAW B727 SRM 511002. PRIMED IAW B727 MM 512002. INSTALLED IAW B727 SRM 513002.

Part: ANGLE — CORRODED (BS 1130)

DURING HEAVY MAINTENANCE CHECK, CORROSION WAS FOUND OUT OF LIMITS ON LONGITUDINAL FLOOR SUPPORT ANGLE, BETWEEN FS 1110 AND 1130 BL 0. REMOVED CORROSION IAW SRM 511006. REMOVED SUPPORT IAW SRM 513002. FABRICATED NEW FLOOR SUPPORT FROM 7075 T6 .032 PER SAMPLE. TREATED AND PRIMED IAW SRM 511002, MM 522002. INSTALLED IAW SRM 513002.

Part: SUPPORT — CORRODED (BS 385)

DURING HEAVY MAINTENANCE CHECK, CORROSION WAS FOUND OUT OF LIMITS AT INTERIOR FUSELAGE STA 385 BL 18R FLOOR SUPPORT. REMOVED CORROSION IAW B727 511006. REMOVED FLOOR SUPPORT FROM BS 385 RBL 18 PER SRM 513002. FABRICATED NEW SUPPORT FROM BAC 15064417 PER SAMPLE. TREATED PER SRM 511002. PRIMED PER MM 512002. INSTALLED PER MM 513002.

Part: FLOORBEAM — CORRODED (BS 294-344)

DURING HEAVY MAINTENANCE CHECK, CORROSION WAS FOUND OUT OF LIMITS ON FWD LAV FLOORBEAMS AT RT BS 294 TO BS 344. REMOVED CORROSION AT FS 294 TO 344 PER SRM 511006. REMOVED LAV FLOOR SUPPORT PER SRM 513002. FABRICATED NEW SUPPORT FROM BAC 1509100312 PER SAMPLE. TREATED PER SRM 511002. PRIMED PER MM 512002. INSTALLED PER SRM 513002.

Part: SUPPORT — CORRODED (BS 420)

DURING HEAVY MAINTENANCE CHECK, CORROSION WAS FOUND OUT OF LIMITS AT INTERIOR FUSELAGE STA 420 BL 36R FLOOR SUPPORT. REMOVED CORROSION IAW B727 511006. REMOVED FLOOR SUPPORT FROM BS 385 RBL 18 PER SRM 513002. FABRICATED NEW SUPPORT FROM BAC 15064417 PER SAMPLE. TREATED PER SRM 511002. PRIMED PER MM 512002. INSTALLED PER MM 513002.

Part: SUPPORT — CORRODED (BS 385)

DURING HEAVY MAINTENANCE CHECK, CORROSION WAS FOUND OUT OF LIMITS ON FLOOR SUPPORT STRUCTURE, STA 385 BL 36R. REMOVED CORROSION FROM FLOOR SUPPORT PER SRM 511006. REMOVED FLOOR SUPPORT PER SRM 513002. FABRICATED NEW SUPPORT FROM BAC 15064417 PER SAMPLE. TREATED PER SRM 511002. PRIMED PER MM 512002. INSTALLED PER SRM 513002.

Part: SEAT TRACK — CORRODED (BS 410)

DURING HEAVY MAINTENANCE CHECK, CORROSION WAS FOUND OUT OF LIMITS AT SEAT TRACK FORWARD RT CABIN, STA 410, RBL 36. REMOVED CORROSION PER SRM 511006. FABRICATED NEW SEAT TRACK PER SAMPLE FROM BAC 1520792. TREATED PER SRM 511002. PRIMED PER MM 512002. INSTALLED PER SRM 513002.

Part: BRACKET — CORRODED (BS 1183)

DURING HEAVY MAINTENANCE CHECK, CORROSION WAS FOUND OUT OF LIMITS AT STA 1183 LBL 1783 WL 208 LOWER ATTACH BRACKET FOR VERTICAL BEAM. REMOVED CORROSION IAW SRM 511006. REMOVED BRACKET IAW SRM 513002. FABRICATED NEW BRACKET PER SAMPLE FROM 7075 T6 .032. TREATED AND PRIMED IAW SRM 51006, MM 512002. INSTALLED IAW SRM 513002.

Part: SIGN — INOPERATIVE (L2 DOORWAY)

DURING A LINE MAINTENANCE CHECK, THE EMERGENCY EXIT SIGN AT THE LOWER RIGHT SIDE OF L2 DOOR WAS FOUND INOPERATIVE. REMOVED AND REPLACED THE LOWER L2 DOOR EMERGENCY EXIT SIGN, OPERATIONALLY CHECKS GOOD.

Part: CARGO NET — OUT OF POSITION (CARGO DOOR)

DURING CLIMB-OUT, UNABLE TO MAINTAIN PRESSURIZATION. TROUBLESHOT PRESSURIZATION SYSTEM AND FOUND THE AFT CARGO DOOR NET AND LATCH WEDGED BETWEEN THE CARGO DOOR AND THE DOOR FRAME. REMOVED AND RESECURED THE CARGO NET. PERFORMED AN OPERATIONAL TEST OF THE SYSTEM PER MM 21300 AND MM 213100. AIRCRAFT OK FOR SERVICE.

Part: SMOKE DETECTOR — INOPERATIVE (FWD LAVATORY)

DURING FLIGHT, THE SMOKE DETECTOR IN THE FORWARD LAV ALARMS CONTINUOUSLY AFTER TESTING. REMOVED AND REPLACED THE SMOKE DETECTOR IN THE FORWARD LAVATORY. OPS CHECKS GOOD.

Part: ACTUATOR — FAILED (NR 2 SPOILER)

DURING DESCENT, CREW OBSERVED 'A' SYSTEM HYDRAULIC FAILURE. HYDRAULIC QUANTITY AND PRESSURE READ ZERO. ALL COM PROCEDURES WERE COMPLIED WITH AND LANDING WAS UNREMARKABLE. INSPECTED AND FOUND A BLOWN O-RING ON THE NR 2 ACTUATOR FOR THE SPOILER. REMOVED AND REPLACED THE SPOILER ACTUATOR O-RING AND SYSTEM CHECKS GOOD IAW MM 276100.

Part: LIGHT — INOPERATIVE (ROW 5BAC)

DURING A LINE MAINTENANCE CHECK, THE FORWARD HALF OF THE EMERGENCY FLOOR TRACK LIGHTING WAS FOUND TO BE INOPERATIVE. REPAIRED THE CONNECTION AT SEATS 5ABC FOR FLOOR TRACK EMERGENCY LIGHTING. OPERATIONALLY CHECKS GOOD.

Part: CLAMP — LOOSE (NR 1 ENGINE)

DURING CLIMB, THE NR 1 ENGINE STRUT OVERHEAT LIGHT ILLUMINATED. LIGHT EXTINGUISHED WITH REDUCED POWER THEN ILLUMINATED AGAIN WHEN CLIMB POWER WAS SET. ALSO, LIGHT WAS ILLUMINATED WITH ASSOCIATED BLEED AND PACKS OFF. FOUND THE 13TH STAGE REGULATOR VALVE CLAMP LOOSE. TIGHTENED CLAMP AND RAN NR 1 ENGINE, OPERATIONALLY AND LEAK CHECKS GOOD.

Part: CLAMP — LOOSE (NR 1 PYLON)

DURING CLIMBOUT FROM SFO, THE ENGINE NUMBER ONE STRUT OVERHEAT LIGHT ILLUMINATED. FOUND ENGINE DUCT IN THE NUMBER ONE PYLON LEAKING JUST BEFORE THE PRECOOLER. TIGHTENED CLAMP AND RAN THE NUMBER ONE ENGINE TO LEAK CHECK. NUMBER ONE ENGINE LEAK CHECKED GOOD IAW MM CHAPTER 2100.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING A LINE MAINTENANCE CHECK, THE FORWARD SECTION OF EMERGENCY FLOOR TRACK LIGHTING WAS FOUND TO BE INOPERATIVE. REMOVED AND REPLACED FORWARD EMERGENCY FLOOR TRACK LIGHTING POWER SUPPLY. FORWARD SECTION OF FLOOR TRACK LIGHTING OPERATIONALLY CHECKS GOOD.

Part: BATTERY PACK — DISCHARGED (LT OVERWING)

DURING A LINE MAINTENANCE CHECK, THE LEFT AFT OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. REMOVED AND REPLACED THE BATTERY AND BATTERY CHARGER PACK M955. LEFT AFT EXTERIOR OVERWING EMERGENCY EXIT LIGHT OPERATIONALLY CHECKS GOOD.

Part: BATTERY PACK — DISCHARGED (E & E COMPT)

DURING A LINE MAINTENANCE CHECK, THE LEFT AFT EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. REPLACED THE EMERGENCY LIGHT BATTERY PACK AT THE E & E BAY LOCATION M955, OPERATIONALLY CHECKS GOOD.

Part: LIGHT — INOPERATIVE (CABIN)

DURING A LINE MAINTENANCE CHECK, THE L1 DOOR EMERGENCY SLIDE LIGHT WAS FOUND TO BE INOPERATIVE. CLEANED LAMP CONTACTS AND OPERATIONALLY CHECKS GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING A LINE MAINTENANCE CHECK, THE LEFT AFT OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. REMOVED AND REPLACED THE BATTERY PACK AT M955. ALL EMERGENCY LIGHTS CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN)

DURING A LINE MAINTENANCE CHECK, THE AFT AIRSTAIR OVERHEAD EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. REMOVED AND REPLACED THE ASSOCIATED LIGHT ASSEMBLY, LIGHT OPERATIONALLY CHECKS GOOD.

Part: SIGN — INOPERATIVE (L 4 DOOR)

DURING A LINE MAINTENANCE CHECK, THE LOWER EMERGENCY EXIT SIGN AT THE L4 DOOR WAS FOUND TO BE INOPERATIVE. FOUND RIBBON TO LOWER L4 DOOR EMERGENCY EXIT SIGN CUT. REPAIRED RIBBON AND OPERATIONALLY CHECKS NORMAL.

Part: WIRE — LOOSE (CABIN)

DURING A HEAVY MAINTENANCE CHECK, THE FORWARD POSTION OF THE EMERGENCY PATH LIGHTING WAS FOUND TO BE INOPERATIVE. REPAIRED WIRE IAW SWP 201013. OPERATIONALLY CHECKS GOOD IAW B727 MM 33501.

Part: SUPPORT — CORRODED (BS 320)

DURING A HEAVY MAINT CHECK, FLOORBOARD SUPPORT FRAME WAS FOUND TO HAVE CORROSION A BS STA 320. CORROSION ON FLOORBOARD SUPPORT BEAM WAS FOUND TO BE OUT OF LIMITS IAW B727 SRM 531001. REMOVED DAMAGED FLOORBEAM SUPPORT IAW B727 SRM 513002. FABRICATED NEW FLOOR BEAM SUPPORT FROM 7075 T6, EXTRUSION AND FILLER FROM 7075 T6 .063 IAW B727 SRM 531002 AND SRM 514003. TREATED AND PRIMED IAW B727 SRM 511002 AND MM 512002. INSTALLED IAW B727 SRM 513002.

Part: STRINGER — CORRODED (BS 720)

DURING A HEAVY MAINT CHECK, EXFOILIATION WAS FOUND PRESENT AT STA 720C STR 28R AT BOTTOM OF RIB UNDER LEVELING COMPOUND. REMOVED DAMAGED AREA IAW B727 SRM 513002 AND 531004 FIGURE 13. FABRICATED NEW DOUBLER OUT OF 7075 T6 .071 IAW B727 SRM 531004. TREATED AND PRIMED IAW B727 SRM 511002 AND MM 512002. INSTALLED IAW B727 SRM 513002.

Part: LIGHT — INOPERATIVE (CABIN)

DURING A LINE MAINTENANCE CHECK, THE L1 DOOR EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT. OPERATIONALLY CHECKS GOOD PER MAINTENANCE MANUAL 3350101.

Part: ACTUATOR — FAILED (NR 5 LE SLAT)

DURING CLIMB, THE NUMBER FIVE LEADING EDGE SLAT AND THE NUMBER SIX LEADING EDGE FLAP WOULD NOT RETRACT. REMOVED AND REPLACED THE NUMBER FIVE LEADING EDGE SLAT ACTUATOR PER MAINTENANCE MANUAL 278132 AND INSTALLED A NUMBER SIX LEADING EDGE FLAP INDICATION EMERGENCY HARNESS PER 2788201.

Part: POWER STOP — NOT STOWED (NR 3 ENGINE)

DURING TAKEOFF ROLL FOLLOWING A MAINTENANCE CHECK, THE AIRCRAFT WOULD NOT REACH TAKEOFF POWER ON THE NUMBER THREE ENGINE. FOUND THE PART POWER STOP IN THE PART POWER STOP POSITION. STOWED AND SAFETIED THE PART POWER STOP. ENGINE OPERATIONALLY CHECKS NORMAL.

Part: OVEN — DIRTY (GALLEY)

SMOKE WAS OBSERVED COMING OUT FROM A SPACE ABOVE THE NUMBER TWO OVEN IN THE FORWARD GALLEY. CLEANED HEATER ELEMENT AND OPERATED THE OVEN. OPERATIONALLY CHECKED GOOD.

Part: SWITCH — OUT OF ADJUST (NR 2 LE FLAP)

NUMBER 2 LT LEADING EDGE FLAP FAILED TO RETRACT ON DEPARTURE. RETURNED TO LAS. REPLACED HARDWARE ON INTRANSIT SWITCH AND READJUSTED IN ACCORDANCE WITH MM 27-80-04. FUNCTIONALLY TESTED NORMAL.

Part: BOLT — MISSING (NR 2 THROTTLE)

DURING CLIMBOUT, COULD NOT ADVANCE NUMBER 2 ENGINE THROTTLE PAST 85 PERCENT N1. AT TOP OF CLIMB, N1 WAS AT 99 PERCENT AND COULD NOT PULL BACK POWER. SHUT DOWN ENGINE FOR PRECAUTIONARY REASONS. FOUND FUEL CONTROL ROD FOR THROTTLE, FORWARD END, MISSING BOLT. INSTALLED NEW BOLT AND NUT, RAN AND RIGGED ENGINE PER B727 MM 71-00-97, OPS CHECKED GOOD.

Part: BATTERY — DISCHARGED (CABIN)

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

Part: SEAT TRACK — CORRODED (FORWARD LAV)

DURING HEAVY MAINTENANCE VISIT, FLOOR BOARD TRACK INSIDE FORWARD LAVATORY DOOR WAS FOUND CORRODED ABOVE DOGHOUSE. REMOVED TRACK, FABRICATED NEW FLOOR AND TRACK AND INSTALLED IAW SRM 51-30-2 AND 53-10-2.

Part: FLOORBEAM — CORRODED (BS 1050)

DURING HEAVY MAINTENANCE VISIT, FLOORBEAM UPPER FLANGE WAS FOUND CORRODED AT STATION 1050, RBL 42 TO 59. CUT OUT DAMAGED SECTION, FABRICATED AND INSTALLED REPAIR ANGLES PER B727 SRM 51-30-2 AND 53-10-8.

Part: SEAT TRACK — CORRODED (BS 1070-1130)

DURING HEAVY MAINTENANCE VISIT, CORROSION WAS FOUND ON SEAT TRACKS AT STATION 1110, RBL 45 AND RBL 55. REMOVED, FABRICATED AND INSTALLED BOTH SECTIONS OF SEAT TRACK FROM STATIONS 1070 TO 1130 IAW SRM 51-31-02, 51-10-6 AND 53-10-5.

Part: FITTING — CORRODED (BS 1183)

DURING HEAVY MAINTENANCE VISIT, TIE FITTING AT STATION 1183, STRINGER 25R WAS FOUND CORRODED. AFTER REMOVAL OF TIE FITTING, STRINGER 25R WAS FOUND TO HAVE EXFOLIATION CORROSION. REMOVED AND REPLACED TIE FITTING IAW B727 SRM 51-10-1 AND REMOVED AND INSTALLED NEW SECTION OF STRINGER 25R IAW 51-30-2.

Part: STRUCTURE — DAMAGED (L1 DOORWAY)

FOUND AIRCRAFT SKIN DAMAGE CAUSED BY JET WAY NEAR L-1 DOOR AT STATION 380, WL 206.1. INSTALLED NEW FRAME WEB, STRINGER REPAIRS AND FUSELAGE REPAIRS PER B727 SRM 51-40-4 AND 53-30-3.

Part: SMOKE DETECTOR — FAILED (AFT LAV)

THE AFT RIGHT LAVATORY SMOKE DETECTOR WAS FOUND TO BE INOPERATIVE. REMOVED AND REPLACED SMOKE DETECTOR, NEW DETECTOR TESTED GOOD.

Part: WIRE — BROKEN (CABIN)

THE MID CABIN FLOOR TRACK LIGHTING WAS FOUND INOPERATIVE. REPAIRED BROKEN WIRES, AND TRACK LIGHTING TESTED NORMAL.

Part: CROSS SHAFT NUT — LOOSE (NR 3 ENGINE)

DURING DESCENT HAD NO THROTTLE RESPONSE FROM THE NUMBER 3 ENGINE. FOUND UPPER THRUST CRANK ON INBOARD SIDE OF ENGINE CROSS SHAFT SECURING NUT LOOSE AND THRUST CRANK OFF THE SPRING SHAFT. REINSTALLED THRUST CRANK AND TORQUED AND SAFETIED NUT. PERFORMED ENGINE RUN CHECKED GOOD PER MM 71-00-00.

Part: WIRE — BROKEN (CABIN)

FOUND EMERGENCY FLOOR PATH LIGHTING INOP FROM ROWS 13 TO 19. FOUND AND REPAIRED BROKEN WIRE. SYSTEM FUNCTIONALLY TESTED NORMAL.

Part: EXIT SIGN — FAILED (CABIN)

EMERGENCY EXIT CIRCUIT BREAKER TRIPPED. FOUND RIGHT AFT OVERWING EXIT SIGN SHROUD SHORTING 28 VAC LINE TO GROUND. ADJUSTED SHROUD CORRECTLY AND FUNCTIONALLY TESTED NORMAL.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

RIGHT OVERWING EMERGENCY EXIT LIGHTS WERE FOUND FLICKERING. REMOVED AND REPLACED POWER SUPPLY AND OPS CHECKED GOOD IN ACCORDANCE WITH MM 33-50-22.

Part: DOOR — NOT LATCHED (E/E COMP)

DURING CLIMB, EQUIPMENT ACCESS DOOR LIGHT ILLUMINATED AND UNABLE TO PRESSURIZE CABIN. RETURNED TO MSP. INSPECTED EQUIPMENT ACCESS DOOR, SEAL AND INDICATOR SWITCH IN ACCORDANCE WITH 52-70-01, OPS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (R1 DOOR)

R1 DOOR EMERGENCY LIGHT FOUND INOP. REMOVED AND REPLACED EMERGENCY LIGHT AND BATTERIES, OPS CHECKED GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN)

OVER AISLE EMERGENCY LIGHT INOP NEAR OVERWING EXITS. REMOVED AND REPLACED BATTERY PACK AND POWER SUPPLY, OPS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN)

RIGHT OVERWING EMERGENCY EXIT LIGHT BLINK ON AND OFF. REMOVED AND REPLACED BATTERY PACK AND OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN)

PORTABLE EMERGENCY LIGHT AT L2 HAS 2 BULBS INOP. REMOVED AND REPLACED EMERGENCY LIGHT ASSEMBLY AND OPS CHECKED GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN)

FOUND OVERWING EMERGENCY AREA LIGHT DIM. REMOVED AND REPLACED BATTERY PACK AND OPS CHECKED NORMAL IN ACCORDANCE WITH MM 33-50-71.

Part: BATTERY PACK — DISCHARGED (CABIN)

RIGHT WING OVERDOOR EMERGENCY EXIT LIGHTS CAME ON FOR ONLY THREE TO FIVE SECONDS. REMOVED AND REPLACED BATTERY PACK FOR RIGHT WING OVERDOOR EMERGENCY EXIT LIGHTS IN ACCORDANCE WITH MM 33-50-0 AND OPS CHECKED NORMALLY.

Part: POWER STRIP — INOPERATIVE (CABIN)

AFT 10 FEET OF EMERGENCY FLOOR TRACK LIGHTING WAS FOUND VERY DIM. REMOVED AND REPLACED AFT POWER STRIP UNDERNEATH TRACK LIGHTS. ALSO, REPLACED ONE TRACK LIGHT STRIP JUST FORWARD OF THE L2 DOOR. SYSTEM OPS CHECKED NORMAL IN ACCORDANCE WITH MM 33-50-00.

Part: EXIT SIGN — MISSING (CABIN)

FOUND RIGHT FORWARD EMERGENCY EXIT LUMINESCENCE SIGN MISSING. REMOVED AND REPLACED RIGHT FORWARD EMERGENCY EXIT LUMINESCENT EXIT SIGN IN ACCORDANCE WITH MM 33-50-31.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

FOUND RIGHT FORWARD AND AFT OVERWING EMERGENCY EXIT SIGNS INOP. REMOVED AND REPLACED RIGHT FORWARD AND AFT OVERWING EMERGENCY EXIT POWER SUPPLY AND OPS CHECKED GOOD.

Part: WIRE — OPEN (CABIN)

FOUND AFT FLOOR TRACK LIGHTS INOP NEAR GALLEY. REPAIRED WIRING IN TRACK AND OPS CHECKED GOOD.

Part: WIRE — BROKEN (CABIN)

THE CEILING MOUNTED EMERGENCY EXIT SIGN AT THE L-2 DOOR WAS FOUND TO BE INOPERATIVE. FOUND BROKEN WIRE AT CONNECTOR TO SIGN. REPINNED CONNECTOR AND LIGHT TESTED GOOD IAW MM 33-50-91.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

FOUND RIGHT OVERWING EMERGENCY LIGHT INOP. REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY PER MM 33-50-71 AND OPS CHECKED GOOD.

Part: LAMP — FAILED (CABIN)

FOUND RIGHT HAND FORWARD EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP AND OPS CHECKED GOOD.

Part: SMOKE DETECTOR — INOPERATIVE (FWD LAV)

FORWARD LAV SMOKE DETECTOR DID NOT TEST. REMOVED AND REPLACED SMOKE DETECTOR AND OPS CHECKED NORMAL.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

FOUND R2 DOOR OVERHEAD EMERGENCY EXIT SIGN DIM. REMOVED AND REPLACED BATTERY PACK AND POWER SUPPLY IN ACCORDANCE WITH MM 33-50-91, SYSTEM OPS CHECKED GOOD.

Part: WIRE — BROKEN (CABIN)

FOUND AISLE EMERGENCY LIGHT UNSECURED AND WIRES SEVERED BETWEEN AFT SERVICE DOORS. REPAIRED EMERGENCY EXIT WIRES, RESECURED FIXTURE AND OPS CHECKED GOOD.

Part: FIRE LOOP — MALFUNCTIONED (MR 3 FIRE LOOP)

THE NUMBER 3 ENGINE FIRE WARNING LIGHT ILLUMINATED AND HORN SOUNDED. SHUT DOWN NUMBER 3 ENGINE. REMOVED AND REPLACED NUMBER 3 ENGINE FIRE LOOP, OPS CHECKED OK.

Part: RIBBON LEAD — CHAFED (CABIN)

THE EMERGENCY TRACK LIGHTING FROM SEAT 7 ABC TO 14 ABC FLICKERS ON AND OFF. FOUND CHAFED RIBBON SUPPLY LINE FROM BATTERY. REPLACED CHAFED RIBBON LEAD AND OPS CHECKED EMERGENCY LIGHTS IAW MM 33-50-00.

Part: CONNECTOR — CORRODED (CABIN)

SECOND SECTION OF EMERGENCY PATH LIGHTING FROM THE FRONT WAS FOUND TO BE INTERMITTENT. CLEANED CORROSION FROM CANNON PLUG AT THE POWER SUPPLY AND LIGHTING TESTED GOOD.

Part: BATTERY PACK — DISCHARGED (AFT CARGO DOOR)

THE EXTERIOR EMERGENCY EXIT LIGHT ON THE AFT RIGHT CARGO DOOR TESTED DIMLY. REMOVED AND REPLACED BATTERY PACK AND LIGHT TESTED GOOD.

Part: SWITCH — CORRODED (NLG)

AFTER GEAR RETRACTION NOSE GEAR INDICATION WAS RED AND GREEN AT THE SAME TIME. FOUND THE LANDING GEAR POSITION SWITCH (S93) CORRODED AND HANGING UP. REMOVED AND REPLACED SWITCH AND CANNON PLUG (D300). INDICATION CHECKED GOOD PER B727, MM 32-61-71.

Part: SWITCH — LACK OF LUBE (NLG)

AFTER GEAR RETRACTION, NOSE GEAR INDICATION WAS RED AND GREEN AT THE SAME TIME. JACKED NOSE OF THE AIRCRAFT, SWUNG GEAR, LUBED AND CLEANED THE DOWNLOCK SWITCH. INDICATION CHECKED NORMAL.

Part: SWITCH — FAILED (NLG)

AFTER GEAR RETRACTION, NOSE GEAR INDICATION WAS RED AND GREEN AT THE SAME TIME. REPLACED THE NOSE GEAR LOCK SWITCH PER MM 32-61-01 PAGE 404. PERFORMED NOSE GEAR LOCK AND POSITION SWITCH ADJUSTMENT AND TEST PER MM 32-61-71 PAGE 501.

Part: ACCESSORY UNIT — FAILED (NLG)

MCO - ON DEPARTURE AFTER GEAR RETRACTION, NOSE GEAR RED AND GREEN LIGHT REMAINED ON. RECYCLED GEAR WITH SAME RESULT. INSPECTED NOSE GEAR THROUGH VIEWER AND VISUALLY CONFIRMED NOSE GEAR UP AND DOORS CLOSED. CHECKED NOSE GEAR UPLOCK SWITCH, DOWN LOCK SWITCH AND WIRING, NO DEFECTS WERE NOTED. REMOVED AND REPLACED THE LANDING GEAR ACCESSORY UNIT PER B727 MM 32-61-01. JACKED AND SWUNG GEAR NUMEROUS TIMES AND ALL INDICATIONS WERE NORMAL.

Part: BATTERIES — DISCHARGED (L-1 DOOR)

THE OVERHEAD L-1 DOOR PORTABLE EMERGENCY EXIT LIGHT ILLUMINATES MOMENTARILY THEN GOES OUT. REMOVED AND REPLACED BATTERIES IAW MM 33-50-101, LIGHT OPS CHECKED GOOD.

Part: EEL TRACK — FAILED (CABIN)

THE EMERGENCY FLOOR TRACK LIGHTING WAS FOUND INOPERATIVE IN THE AFT CABIN. REMOVED AND REPLACED SHORTED LUMINESCENT FLOOR TRACK LIGHTING STRIP, OPS CHECKED NORMAL.

Part: EEL LAMP — FAILED (R 1 DOOR)

THE R-1 DOOR SLIDE EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. RELAMPED LIGHT AND UNIT TESTED GOOD.

Part: ACCESSORY UNIT — FAILED (LANDING GEAR)

DURING CLIMB AFTER GEAR RETRACTION, RED AND GREEN NOSE GEAR LIGHTS ILLUMINATED. ALL INDICATIONS WERE NORMAL DURING RETRACTION AND EXTENSION. REMOVED AND REPLACED LANDING GEAR ACCESSORY UNIT PER MM 32-09-12, OPS CHECKED GOOD PER MM 32-09-121.

Part: EEL SIGN — INOPERATIVE (L 1 DOOR)

THE EMERGENCY EXIT SIGN AT THE L1 DOOR WAS FOUND TO BE INOPERATIVE. REMOVED AND REPLACED EXIT SIGN AT THE L1 DOOR, LIGHT TESTED GOOD.

Part: HARNESS — CHAFED (NLG INDICATION)

NOSE GEAR INDICATION PROBLEM WAS NOTED DURING GEAR RETRACTION, AIRCRAFT RETURNED TO STATION. WHEN THE GEAR WAS LOWERED ALL INDICATIONS WERE NORMAL. DURING POST FLIGHT INSPECTION THE LOWER LINK ATTACH BOLT (NAS-104-47W), WAS FOUND CRACKED. THE BOLT WAS REPLACED. ALSO, WIRE BUNDLE 5144 WAS FOUND CHAFED AGAINST THE NUMBER 1 HIGH FREQUENCY TRANSCEIVER AND WORN THROUGH CAUSING THE NOSE GEAR INDICATION PROBLEM. REPAIRED AND REROUTED THE HARNESS, SYSTEM TESTED GOOD DURING THE NOSE GEAR SWING.

Part: BATTERY — DISCHARGED (CABIN)

THE FORWARD CEILING MOUNTED EMERGENCY AREA LIGHT WAS FOUND INOPERATIVE. REPLACED BATTERIES IAW 33-50-81 AND LIGHT TESTED GOOD.

Part: EEL ASSY — FAILED (COCKPIT)

THE COCKPIT PORTABLE EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. REMOVED AND REPLACED LIGHT ASSEMBLY AND LIGHT TESTED GOOD.

Part: EEL ASSY — INOPERATIVE (AFT ENTRY DOOR)

THE AFT ENTRY EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. REMOVED AND REPLACED AFT ENTRY EMERGENCY EXIT LIGHT ASSEMBLY PER MM 33-50-101 AND LIGHT TESTED GOOD.

Part: EEL BATTERY PACK — DISCHARGED (CABIN)

THE AFT THIRD OF EMERGENCY TRACK LIGHT WAS FOUND TO BE INOPERATIVE. REMOVED AND REPLACED THE POWER SUPPLY AND REPLACED 2 STRIPS OF FLOOR LIGHTS.

Part: EEL — FAILED (CABIN)

THE FORWARD LEFT OVERWING EXIT DOOR EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. REMOVED AND REPLACED EXIT LIGHT ASSEMBLY AND LIGHT TESTED GOOD.

Part: EEL — FAILED (CABIN)

THE AFT RIGHT OVERWING EXIT DOOR EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. RESEATED CANNON PLUG ON LIGHT ASSEMBLY AND LIGHT TESTED GOOD.

Part: EEL — FAILED (CABIN)

THE FORWARD RIGHT OVERWING EXIT DOOR EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. RESEATED CANNON PLUG ON LIGHT ASSEMBLY AND LIGHT TESTED GOOD.

Part: EEL BATTERY PACK — DISCHARGED (CABIN)

THE AFT OVERHEAD EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. REMOVED AND REPLACED BATTERY PACK AND CLEANED CORROSION ON BATTERY CONTACTS AND LIGHT TESTED GOOD.

Part: EEL BULB — FAILED (L 1 DOOR)

THE L-1 DOOR EXTERIOR EMERGENCY SLIDE LIGHT WAS FOUND TO BE INOPERATIVE. RELAMPED THE L-1 DOOR EMERGENCY SLIDE LIGHT AND LIGHT TESTED GOOD.

Part: WEB — CORRODED (BS 950)

DURING HEAVY MAINTENANCE VISIT (HMV), THE WEB AT BS 950B, LBL 10 WAS FOUND TO HAVE LEVEL 1 CORROSION. REMOVED CORROSION, FABRICATED AND INSTALLED DOUBLER AND FILLER REPAIRS IAW B727 SRM 51-40-03 AND SRM 53-10-01.

Part: BLKHD CHORD — CORRODED (BS 950)

DURING HEAVY MAINTENANCE VISIT (HMV), BS 950 BULKHEAD LOWER T-CHORD HAS LEVEL 2 INTERGRANULAR CORROSION AT STRINGER 29R. REMOVED AND REPLACED THE LOWER CHORD IAW B727 SRM 51-40-04 AND SRM 51-10-06.

Part: SUPPORT — CORRODED (BS 360-380)

DURING HEAVY MAINTENANCE VISIT (HMV), THE CABIN FLOOR SUPPORT AT BS 360-380, RBL 12 (NEAR STRINGER 17R) WAS FOUND TO HAVE LEVEL 1 CORROSION. REMOVED CORRODED FLOOR SUPPORT, FABRICATED AND INSTALLED NEW FLOOR SUPPORT IAW B727 SRM 53-10-08.

Part: SUPPORT — CORRODED (BS 380)

DURING HEAVY MAINTENANCE VISIT (HMV), LEVEL 2 CORROSION WAS FOUND ON THE CABIN FLOOR SUPPORT AT BS 380 STRINGER 17R-RBL 64. REMOVED CORRODED SECTION OF BEAM, FABRICATED, AND INSTALLED REPAIR MEMBERS IAW B727 SRM 53-10-08.

Part: SUPPORT — CRACKED (BS 284.5)

DURING HEAVY MAINTENANCE VISIT (HMV), A CRACK AND LEVEL 1 CORROSION WAS FOUND ON THE FLOOR SUPPORT AT BS 284.5, RBL 0 TO RBL 6. REMOVED CRACK AND CORROSION, FABRICATED L-ANGLE REPAIR AND FILLER AND INSTALLED IAW B727 SRM 51-40-04 AND SRM 53-10-08.

Part: SUPPORT — CORRODED (BS 380-400)

DURING HEAVY MAINTENANCE VISIT (HMV), THE FLOOR SUPPORT AT BS 380-400 RBL-WL 208 WAS FOUND TO HAVE LEVEL 1 CORROSION. REMOVED CORRODED FLOOR SUPPORT, FABRICATED AND INSTALLED NEW REPAIR MEMBERS IAW B727 SRM 53-10-08.

Part: FLOOR BEAM — CORRODED (BS 400)

DURING HEAVY MAINTENANCE VISIT (HMV), LEVEL 2 CORROSION WAS FOUND ON THE MAIN CABIN FLOOR BEAM AT BS 400 STRINGER 17-LBL 24 THRU RBL 12. REMOVED AND REPLACED THE FLOOR BEAM IAW B727 SRM 53-10-08.

Part: SEAT TRACK — CORRODED (BS 340-460)

DURING HEAVY MAINTENANCE VISIT (HMV), THE SEAT TRACK LOCATED AT BS 344-460, ON THE INBOARD SIDE OF STRINGER 17L, WAS FOUND TO HAVE LEVEL 2 CORROSION. REMOVED AND REPLACED THE SEAT TRACK IAW B727 SRM 53-10-05.

Part: DOOR JAMB — CRACKED (R1 DOOR)

DURING HEAVY MAINTENANCE VISIT (HMV), A CRACK WAS FOUND IN THE R1 DOOR JAMB LOWER FORWARD CORNER. THE DOOR JAMB WAS REMOVED, CRACK STOP DRILLED, REPAIRS FABRICATED AND INSTALLED IAW B727 SRM 51-40-03.

Part: SEAT TRACK — CORRODED (BS 360-440)

DURING HEAVY MAINTENANCE VISIT (HMV), THE OUTBOARD SEAT TRACK AT BS 360-440, NEAR STRINGER 17, WAS FOUND TO HAVE LEVEL 2 CORROSION. REMOVED AND REPLACED SEAT TRACK IAW B727 SRM 53-10-05.

Part: FLOOR BEAM — CORRODED (BS 440)

DURING HEAVY MAINTENANCE VISIT (HMV), THE CABIN FLOOR BEAM AT BS 440 RBL 4 TO RBL 12 WAS FOUND TO HAVE LEVEL 2 CORROSION. REMOVED AND REPLACED THE FLOOR BEAM IAW B727 SRM 53-10-08.

Part: SUPPORT — CORRODED (BS 344-360)

DURING HEAVY MAINTENANCE VISIT (HMV), THE CABIN FLOOR SUPPORT AT BS 344-360, RBL 12 WAS FOUND TO HAVE LEVEL 1 CORROSION. REMOVED CORRODED SECTION, FABRICATED AND INSTALLED NEW REPAIR MEMBERS IAW B727 SRM 53-10-08.

Part: FLOOR BEAM — CORRODED (BS 344)

DURING HEAVY MAINTENANCE VISIT (HMV), LEVEL 2 CORROSION WAS FOUND ON THE MAIN CABIN FLOOR BEAM UNDER TAPE AND CLIP NUTS AT BS 344, RBL 14 TO THE L-1 DOOR. REMOVED CORRODED SECTION OF BEAM, FABRICATED AND INSTALLED REPAIR MEMBERS IAW B727 SRM 53-10-08.

Part: SUPPORT — CORRODED (BS 750-740)

DURING HEAVY MAINTENANCE VISIT (HMV), LEFT LOWER SUPPORT FRAME AT BS 750E TO 740 FOR BODY FAIRINGS WAS FOUND TO HAVE LEVEL 2 CORROSION BEYOND SRM LIMITS. REMOVED AND REPLACED SUPPORT FRAME IAW B727 51-40-03.

Part: SEAT TRACK — CORRODED (BS 640)

DURING HEAVY MAINTENANCE VISIT (HMV), THE CENTER FLOOR MOUNT RAIL AFT OF BS 640, INBOARD OF STRINGER 28L, WAS FOUND TO HAVE LEVEL 2 CORROSION. REMOVED CORRODED SECTION OF SEAT TRACK, FABRICATED AND INSTALLED REPAIRS IAW B727 SRM 53-40-03.

Part: SEAT TRACK — CORRODED (BS 640)

DURING HEAVY MAINTENANCE VISIT (HMV), THE CENTER FLOOR MOUNT RAIL AFT OF BS 640, NEAR STRINGER 27R, WAS FOUND TO HAVE LEVEL 2 CORROSION. REMOVED CORRODED SECTION OF SEAT TRACK, FABRICATED AND INSTALLED REPAIRS IAW B727 51-40-03.

Part: FLOOR BEAM — CORRODED (BS 1110)

DURING HEAVY MAINTENANCE VISIT (HMV), THE FLOOR BEAM AT BS 1110 WAS FOUND TO HAVE LEVEL 2 CORROSION. REMOVED CORRODED UPPER CHORD, FABRICATED AND INSTALLED NEW UPPER CHORD, ANGLES, AND ANGLE STRAPS IAW B727 SRM 53-10-08.

Part: STRINGER — CORRODED (BS 720C-720D)

DURING HEAVY MAINTENANCE VISIT (HMV), STRINGER 27R WAS FOUND TO HAVE LEVEL 2 CORROSION BETWEEN STATION 720C THROUGH 720D. REMOVED CORRODED SECTION OF STRINGER, FABRICATED AND INSTALLED REPAIR MEMBERS IAW B727, SRM 53-10-01 AND SRM 51-40-04.

Part: EEL BATTERY PACK — DISCHARGED (CABIN)

THE FORWARD MIDDLE EMERGENCY PATH LIGHTING INOPERATIVE. REMOVED AND REPLACED THE BATTERY PACK AND LIGHTING TESTED GOOD PER MM 33-50-01.

Part: EEL — INOPERATIVE (L1 DOOR)

FOUND THE L1 DOOR EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED PORTABLE EMERGENCY SIGN OVER L1 DOOR, OPS TESTED GOOD PER B727 MM 33-50-101.

Part: EEL WIRE — DAMAGED (CABIN)

FOUND THE AFT FLOOR TRACK LIGHTS INOPERATIVE. WIRES WERE FOUND DAMAGED; REPAIRED WIRES AND FLOOR TRACK LIGHTING SYSTEM TESTED GOOD.

Part: EEL POWER SUPPLY — FAILED (R-2 DOOR)

FOUND THE EMERGENCY EXIT SIGN AT THE R2 DOOR INOPERATIVE. REMOVED AND REPLACED EMERGENCY EXIT SIGN POWER SUPPLY AND BATTERY PACK. SIGN OPS CHECKED NORMAL.

Part: EEL BATTERY PACK — DISCHARGED (CABIN)

FOUND THE R-2 DOOR EMERGENCY EXIT SIGN INOPERATIVE. REMOVED AND REPLACED BATTERY PACK, SIGN TESTED GOOD PER MM 33-50-71.

Part: OVEN — SMOKING (AFT GALLEY)

DURING CLIMB FROM LAS, AFT OVEN STARTED SMOKING. FLIGHT ATTENDANT TURNED OFF OVEN AND SMOKE STOPPED. DURING INSPECTION OF OVEN, FOUND NO EVIDENCE OF FIRE. FOUND CLEANING SOLVENT ON OUTBOARD OVEN HEATING COILS. CLEANED COILS AND TESTED OVENS PER MM 25-20-00, OVENS TESTED GOOD.

Part: EEL — FAILED (CABIN)

FOUND AFT OVERHEAD PORTABLE EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED LIGHT ASSEMBLY PER MM 33-50-101 PAGE 201. OPS CHECKED GOOD.

Part: FIRE DET BOX — FAULTY (NR 1 ENGINE)

DURING LANDING ROLL WHILE APPLYING REVERSE THRUST HAD NUMBER 1 ENGINE FIRE WARNING INDICATION. BLEW ONE FIRE BOTTLE AND SHUTDOWN ENGINE, FIRE WARNING INDICATION EXTINGUISHED. POST FLIGHT INSPECTION SHOWED NO EVIDENCE OF FIRE. REMOVED AND REPLACED FIRE DETECTION WARNING BOX, SYSTEM OPS CHECKED GOOD.

Part: DUCT — CRACKED (NR 1 ENGINE)

NR 1 ENGINE FIRE WARNING INDICATOR ILLUMINATED DURING FLIGHT. ENGINE WAS SHUTDOWN, ONE FIRE BOTTLE WAS DISCHARGED AND FIRE WARNING CEASED. TEN MINUTES LATER FIRE WARNING RE-ILLUMINATED AND SECOND BOTTLE WAS DISCHARGED, FIRE WARNING LIGHT CEASED. FIRE WARNING LIGHT ILLUMINATED AND BELL CAME ON ABOUT SIX MORE TIMES BEFORE LANDING IN ICT. A CRACK WAS FOUND IN THE 8TH STAGE DUCT WITHIN THE FIXED COWL AREA. DUCT WAS REPLACED AND LEAK CHECKED AT TAKE-OFF POWER, NO LEAKS NOTED.

Part: CONTROL CABLE — OUT OF LIMITS (RT SPOILER)

SPOILERS 10 THROUGH 14 WOULD NOT COMPLETELY STOW. PERFORMED SPOILER PANEL DEFLECTION CHECK PER B727 MM PAGES 531-532-2917. FOUND CABLES OUT OF LIMITS. REMOVED AND REPLACED RIGHT HAND SPOILER CONTROL CABLES, IPC REFERENCE 27-10-0-2 FIGURE 2 PAGE 1 ITEMS 90 AND 130. ADJUSTED RIGHT WING SPOILER CONTROL SYSTEM WING CABLES AND ACTUATORS PER BMM CHAPTER 27-61-0 PAGE 513 A. OPS CHECK NORMAL.

Part: R2 DOOR — NOT LATCHED (AFT GALLEY)

CABIN BEGAN RAPID CLIMB WITH AIRCRAFT CLIMBING THROUGH 18,OOO FEET. AN ON BOARD MECHANIC NOTED AIR LEAK AT AFT GALLEY DOOR. FOUND DOOR NOT FULLY LATCHED AT BOTTOM. DOOR WAS INSPECTED INSIDE AND OUT FOR DAMAGE AND LEAKS, NONE FOUND. OPERATIONAL CHECK AND INDICATIONS ALL NORMAL, OK FOR SERVICE.

Part: R2 DOOR — OUT OF RIG (AFT GALLEY)

AFTER DEPARTING LAS A SUBSTANTIAL AIR LEAK IN RIGHT AFT GALLEY DOOR WAS DETECTED, AND AIRCRAFT WOULD NOT PRESSURIZE PROPERLY ON CLIMB-OUT. FOUND R2 DOOR NOT CLOSED PROPERLY, FORWARD LOBE NOT IN TRACK. RECLOSED DOOR AND OPS CHECKED GOOD.

Part: APR MODULE — FAILED (AFT FUSELAGE)

CMI - FLT 687 - ON POWER UP FOR TAKEOFF, APR FAILED TO ARM. ABORTED BELOW 60 KNOTS, RESET, RETESTED SYSTEM AND OPERATIONS CHECKED NORMAL. PERFORMED GROUND CHECK PER MM 73-22-00 PG 502 SYSTEM OPERATIONS NORMAL. (W)

Part: AIR VALVE — FAULTY (RIGHT PACK)

SLC - FLT 865 - ON CLIMB-OUT, FLIGHT ENGINEER UNABLE TO CONTROL CABIN IN AUTO, STANDBY, OR MANUAL (OUTFLOW VALVE IN FULL CLOSED POSITION WITH CABIN CLIMBING). FOUND RIGHT FORWARD PACK VALVE INOPERATIVE. REPLACED RIGHT FORWARD PACK VALVE AND RAN RIGHT PACK, OPERATIONS CHECKED NORMAL. ALSO PRESSURIZED AIRCRAFT ON GROUND AND FOUND NO AIR LEAKS. AIRCRAFT PRESSURIZED NORMALLY. (X)

Part: EEL TRACK — INOPERATIVE (CABIN)

MSP - AFT ONE-THIRD OF FLOOR TRACK LIGHTING (EMERGENCY) IS INOPERATIVE. FOUND FOURTH FROM THE AFT EMERGENCY LAMP SEGMENT SHORTED. REMOVED AND REPLACED SEGMENT AND TRACK COVERING. OPS CHECK GOOD PER MM 33-50-00. (X)