N76753

Part: WARNING LIGHT — ILLUMINATED (CSD TEMP) · airframe 56,797 hrs · 36,534 cycles

NR 3 CSD OIL TEMP GANGE INDICATE 160 DEGREE FOR CSD "IN" INDICATION. TRANFERRED TO DMI 4874 IAW MEL 24-3 (STATUS:ORIG/OPEN).

Part: SWITCH — DAMAGED (LE FLAPS)

NR 6 LED FAILED TO RETRACT AFTER T/O. FOUND PUSHED PIN AT NR 6 LED FLAP POS SWITCH. RESEATED PIN IAW MM CH. 20-11-07. OPS CHECKS GOOD IAW MM CH. 27-82-11.

Part: POSITION SWITCH — OUT OF ADJUST (TE FLAPS)

NR 6 LED FAILED TO RETRACT. ADJUSTED NR 6 LEADING EDGE FLAP POS SWITCH IAW MM CH. 27-82-11.

Part: WARNING LIGHT — FALSE INDICATION (NLG) · airframe 56,452 hrs · 36,200 cycles

NOSE LANDING GEAR WARNING LIGHT REMAINS ILLUMINATED WITH NO GEAR EXTENSION, DURING GEAR EXTENSION. ACCOMPLISHED ABNORMAL PROCEDURES CHECKLIST. LUBED NOSE LANDING GEAR PER B727 M/M CHAPTER 12-12-11. PERFORMED L/G CONTROL SYSTEM ADJUSTMENT AND TEST PER B727 M/M CHAPTER 32-31-0. NO DEFECTS NOTED. EXERCISED NOSE GEAR LOCK SWITCH. OPS CK NORMAL. INSPECTED CABLES AND GEAR SELECTOR VALVE. NO DEFECTS NOTED.

Part: LANDING GEAR — MALFUNCTIONED (NOSE) · airframe 56,402 hrs · 36,156 cycles

ON FINAL, NOSE GEAR WOULD NOT EXTEND, RECYCLED PER CHECKLIST AND LANDED. PERFORMED NORMAL LANDING GEAR CONTROL SYSTEM TEST IAW B727MM 32-31-0. TEST GOOD.

Part: PROXIMITY SWITCH — MALFUNCTIONED (MLG)

RIGHT GEAR LIGHT REMAINS ON AFTER GEAR-UP, FOLLOW AS PER FOM. REMOVED AND REPLACED RT MLG PROX SWITCH IAW B727 MM 32-61-21, NO HELP. REMOVED AND REPLACED LANDING GEAR ACCESSORY UNIT IAW B727 MM 32-09-111. PERFORMED OPERATIONAL GEAR SWING IAW B727 MM 7-11-0 & 32-31-1, NO DEFECTS NOTED AT THIS TIME.

Part: CONNECTOR — LOOSE (MLG)

AFTER GEAR RETRACTION, RED RIGHT GEAR DOOR LIGHT ON AFTER GEAR HANDLE IN OFF POSITION. AND R GEAR DOOR LT. ON ENGINEER'S PANEL ON. PERFORMED CHECKLIST. LIGHT WENT OUT. CLEANED AND RESEATED CONNECTOR ON RIGHT GEAR DOOR UPLOCK SWITCH IAW B727 MM 32-62-11. GEAR DOORS OPS CHECKS GOOD.

Part: CONNECTOR — DIRTY (RT MLG DOOR)

ON DEPART FROM BOS RT MAIN GEAR DOOR LIGHT. RECYCLE GEAR. DOOR LIGHT OUT. ACTION TAKEN: CLEANED AND RESEATED RT MAIN GEAR DOOR SWITCH CONNECTOR PLUG. CYCLED THROUGH SEVERAL TIMES. OPS CHECK NORMAL IAW ENA MM 32-12-1.

Part: BRAKE ASSY — UNKNOWN (MLG) · airframe 55,892 hrs · 35,712 cycles

AFTER RELEASING BRAKES; ON POWER OUT OF MCO HEARD LOUD POP AND WHEN APPLYING PRESSURE TO BRAKES FELT VIBRATION COMING FROM MLG AREA. JACKED EACH MLG, INSPECTED EACH BRAKE & CYCLED NUMEROUS TIMES. NO DEFECTS NOTED. SERVICED ALL BRAKE LOCKOUTS. BRAKES CHECKED GOOD AS PER B727 MM 32-40-0.

Part: WARNING LIGHT — ILLUMINATED (MLG)

AFTER GEAR RETRACTION ALL 3 RED GEAR UNSAFE LIGHTS ILLUMINATED WITH GEAR LEVER IN GEAR UP POSITION. ALSO TAIL SKID LIGHT REMAINED ILLUMINATED. PERFORMED ABNORMAL CHECKLIST. ALL LIGHT EXTINGUISHED. CONTINUED TO KRDU.

Part: THROTTLE — OUT OF ADJUST (NR 1 ENGINE)

ON TAKEOFF ENG NR 2 & 3 NORMAL. ENG NR 1 THROTTLE 4 KNOBS MORE OUT OF ALIGN WITH 2.2 EPR AND 88 PERCENT N1. TAKEOFF REJECTED. FOUND NR 1 EPR INACCURATE. TRANSFERRED TO DMI 3383 IN ACCORDANCE WITH MEL 77-1-2. PLACARDS INSTALLED.

Part: ACCESSORY UNIT — MALFUNCTIONED (MLG)

AFTER GEAR RETRACTION ALL 3 RED GEAR UNSAFE LIGHTS REMAIN ILLUMINATED. GEAR POSITION INDICATOR INDICATED GEAR UP. ON GEAR RETRACTION TAIL SKID LIGHT REMAIN ILLUMINATED. FOM PROCEDURE INDICATED INSUFFICIANT FUEL FOR TRIP WITH TAIL SKID EXTENDED. RETURN TO FLL. REMOVED AND REPLACED LANDING GEAR ACCESSORY UNIT IAW B727 MM 32-09-121. PERFORMED GEAR SWING IAW B727 32-30-1. OPS CHECK NORMAL.

Part: MECHANISM — STUCK (DOOR RELEASE)

AFTER GEAR ROTATION MDT-WITH GEAR HANDLE PLACED TO OFF, RED DOOR LIGHT ILLUMINATED WITH AMBER. R-GEAR DOOR LIGHT ON FE'S PANEL. CYCLED GEAR PER ENA ABNORMAL CHECKLIST. BOTH LIGHTS EXTINGUISHED. FOUND MANUAL DOOR RELEASE QUADRANT & DOOR LOCK RELEASE STICKING TO OPEN POSITION WHEN GROUND RELEASE HANDLE STOWED. LUBE QUADRANTS & LOCK RELEASE. OPS CHECK GOOD. REF MM CH 32-12.

Part: SWITCH — DIRTY (MLG DOOR)

ON DEPARTURE FROM BWI RT MAIN GEAR DOOR WARNING LIGHT ILLUMINATED. RECYCLED PER CHECK LIST. DOOR LIGHT OUT. CLEANED & INSPECTED RT MAIN GEAR DOOR SWITCH. DOOR OPS CHECK GOOD IAW B727 MM 52-81-0.

Part: WARNING LIGHT — ILLUMINATED (MLG DOOR)

ON DEPARTURE FROM ICT RT MAIN GEAR DOOR WARNING LIGHT ILLUMINATED. RECYCLE PER CHECK LIST. DOOR LIGHT OUT.

Part: CONNECTOR — MALFUNCTIONED (MLG DOOR)

ON DEPARTURE FROM ICT RT MAIN GEAR DOOR WARNING LIGHT ILLUMINATED. RECYCLE LANDING GEAR PER CHECK LIST. DOOR LIGHT OUT. CLEANED AND RECONNECTED CONNECTOR ON RT DOOR SWITCH. OPS CHECK GOOD IAW 727 MM 32-10-00.

Part: WARNING LIGHT — ILLUMINATED (RUDDER LOAD)

AFTER PUSHBACK, ENGINES STARTED. FOUND LOWER RUDDER LOAD LIMITED LIGHT ON. TRANSFERRED TO DMI 3159 PER ENA MEL 27-22. CAT C PLACARDS INSTALLED. SP 27-22 APPLY.

Part: WINDOW — CRACKED (COCKPIT)

AFTER T/O R-1 WINDOW PANE CRACKED. REMOVED & REPLACED R-1 WINDSHIELD AS REQ IAW B727 ENA MM REF 56-11-11. NO OTHER DEFECTS NOTED AT THIS TIME.

Part: FLOORBEAM — CORRODED (FUSELAGE)

DURING A C-CHECK, CORROSION WAS NOTED ON FLOORBEAM AT BS 1030 ON UPPER FLANGES AT RBL 30 AND RBL 55. (X)

Part: FLOORBEAM — CORRODED (FUSELAGE)

DURING A C-CHECK, CORROSION WAS NOTED ON FLOORBEAM AT STA 1090 RBL 18 ON UPPER FLANGE. (X)

Part: FRAME — CORRODED (BS 1163)

DURING A C-CHECK, CORROSION WAS NOTED ON FRAME AT STA 1163 STR 13 AND STR 14L.

Part: INTERCOSTAL — CRACKED (BS 360)

DURING CONFORMITY INSPECTION, AN INTERCOSTAL WAS FOUND CRACKED AT STA 360, S16L.

Part: SUPPORT — CORRODED (BS 950)

DURING A C-CHECK, CORROSION WAS NOTED AT FS 950A-950E, LBL 4, 6, 12, AND 16 ON FLOOR SUPPORTS.

Part: FITTING — CORRODED (CARGO DOOR)

DURING A C-CHECK, CORROSION WAS NOTED ON THE C-1 DOOR SUPPORT STRUT FITTING.

Part: SKIN — CORRODED (BS 950)

DURING A C-CHECK, CORROSION WAS NOTED ON BELLY SKIN STR 28R TO STA 950F.

Part: STRINGER — CORRODED (BS 1166-1183)

DURING A C-CHECK, CORROSION WAS NOTED ON STR 29L BETWEEN STA 1166 - STA 1183.

Part: ANGLE — CORRODED (BS 259)

DURING A C-CHECK, CORROSION WAS NOTED IN COCKPIT ON FLOORBEAM ATTACH ANGLE STA 259.5.

Part: STRINGER — CORRODED (BS 1060)

DURING A C-CHECK, CORROSION WAS NOTED ON STR 28R AT STA 1060.

Part: STRINGER — CORRODED (BS 1130-1150)

DURING A C-CHECK, CORROSION WAS NOTED ON STR 28L BETWEEN STA 1130 - STA 1150.

Part: SHEAR TIE — CORRODED (BS 1166)

DURING A C-CHECK, CORROSION WAS NOTED ON SHEAR TIE AT STA 1166 BETWEEN STR 27 - STR 29R.

Part: FRAME — CORRODED (BS 1148)

DURING A C-CHECK, CORROSION WAS NOTED ON FRAME AT STA 1148 BETWEEN BILGE AND STR 29R.

Part: SUPPORT — CORRODED (BS 540)

DURING A C-CHECK, CORROSION WAS NOTED ON FLOOR SUPPORT STA 540 ABOVE STR 27R.

Part: SUPPORT — CORRODED (BS 620-720D)

DURING A C-CHECK, CORROSION WAS NOTED ON SEVERAL FLOOR SUPPORTS STA 620 - STA 720D, STR 27L - STR 27R.

Part: SPLICE — CORRODED (BS 1010)

DURING A C-CHECK, CORROSION WAS NOTED AT STR SPLICE 29L, STA 1010.

Part: ANGLE — CORRODED (BS 360-380)

DURING A C-CHECK, CORROSION WAS NOTED ON ANGLE BETWEEN STA 360 - STA 380, STR 28L - STR 28R.

Part: SHEAR TIE — CORRODED (BS 1010)

DURING A C-CHECK, CORROSION WAS NOTED ON SHEAR TIE STA 1010 - STR 28R.

Part: SKIN — CORRODED (BS 1050-1070)

DURING A C-CHECK, CORROSION WAS NOTED ON EXTERIOR SKIN STA 1050 - STA 1070, STR 29R.

Part: SUPPORT — CORRODED (BS 1130-1148)

DURING A C-CHECK, CORROSION NOTED ON FLOOR SUPPORT RIGHT BETWEEN STA 1130 AND STA 1148.

Part: SEAT TRACK — CORRODED (BS 848)

DURING A C-CHECK, CORROSION NOTED ON STA 848 - STA 740, LBL 45.5.

Part: SHEAR TIE — CORRODED (BS 540)

DURING A C-CHECK, CORROSION NOTED AT STA 540 BETWEEN STA 28L AND STA 28R.

Part: SEAT TRACK — CORRODED (BS 950)

DURING A C-CHECK, CORROSION WAS NOTED ON SEAT TRACK STA 950A - STA 950B, LBL 45.5.

Part: WEB — CORRODED (BS 1166)

DURING A C-CHECK, CORROSION WAS NOTED ON CENTER OF FLOOR WEB STA 1166, BL ZERO.

Part: FLOORBEAM — CORRODED (E/E BAY)

DURING A C-CHECK, CORROSION WAS NOTED ON FLOOR BEAM STA 380, E/E BAY.

Part: SKIN — CORRODED (BS 277)

DURING A C-CHECK, CORROSION NOTED ON SKIN FS 277 AT STR 18R.

Part: BULKHEAD — CORRODED (BS 304)

DURING A C-CHECK, CORROSION WAS NOTED ON THE BULKHEAD AT STA 304. (ONE AT FLOOR LEVEL - OTHER NEAR CENTER.)

Part: SEQUENCE VLV — LEAKING (LT MLG)

THE A SYSTEM HYDRAULIC FLUID WAS LOST WHEN LANDING GEAR WAS RETRACTED AFTER TAKEOFF FROM CRP. THE FLIGHT WAS CONTINUED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE LT MLG LOCK SEQUENCE VALVE LEAKING. THE SEQUENCE VALVE WAS REMOVED AND REPLACED IAW MM 32-32-31. THE HYDRAULIC SYSTEM WAS SERVICED. A GEAR RETRACTION WAS PERFORMED AND OPERATIONAL CHECKS WERE GOOD.

Part: GUIDE VANE — CRACKED (NR 2 ENGINE)

THE NR 2 ENGINE EXPERIENCED POWER REDUCTION DURING CLIMBOUT. THE CREW ADVANCED THE THROTTLE TO MAINTAIN CLIMB POWER, RESULTING IN THE NR 2 THROTTLE BEING THREE KNOBS AHEAD OF NR 1 AND NR 3, WITH SLIGHTLY HIGHER EGT. THE AIRCRAFT WAS RETURNED TO EWR. THE NR 2 ENGINE WAS REMOVED AND REPLACED. *S/D* SHOP FINDINGS REVEALED CRACKED AND BOWED NOZZLE GUIDE VANES.

Part: CHORD — CRACKED (NR 2 LE SLAT)

INSPECTION FOUND A 3 INCH CRACK ON LOWER LEADING EDGE CHORD JUST OUTBOARD OF OUTBOARD TRACK FOR NR 2 LEADING EDGE SLAT. THE CRACK WAS STOP DRILLED, AN ANGLE REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-4.

Part: CHORD — CRACKED (NR 2 LE SLAT)

INSPECTION FOUND A 3.5 INCH CRACK ON LOWER LEADING EDGE CHORD JUST INBOARD OF INBOARD TRACK FOR NR 2 LEADING EDGE SLAT. THE CRACK WAS STOP DRILLED, AN ANGLE REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-4.

Part: FLOORBEAM — CORRODED (BS 1158)

INSPECTION FOUND FLOORBEAM CORRODED AT STA 1158, LBL 49. THE CORRODED AREA WAS CUT OUT, FILLER AND STRAP WERE FABRICATED AND INSTALLED IAW ECRA 5310-03355.

Part: PULLEY — BEARING FAILED (RT INB AIL)

DURING MID-D CHECK INSPECTION, RT INBD AILERON TAB CONTROL CABLE TURNAROUND PULLEY WAS FOUND TO HAVE A RUSTED AND FROZEN BEARING. SUSPECT CAUSES ARE WATER INTRUSION OR INSUFFICIENT LUBRICATION DURING MANUFACTURE. SUBMITTER STATED SPECIAL ATTENTION SHOULD BE GIVEN TO THIS PULLEY BEARING DURING INSPECTION TO DETECT EARLY SIGNS OF RUSTING OR WEAR. REF IPC 27-10-0-24. AC TT 50080. AC CYC 32554.

Part: PULLEY — BEARING FAILED (LT INBD AIL)

DURING MID-D CHECK INSPECTION, LT INBD AIL TAB CONTROL CABLE TURNAROUND PULLEY WAS FOUND TO HAVE A RUSTED AND FAILED BEARING. SUSPECT CAUSES ARE WATER INTRUSTION OR INSUFFICIENT LUBRICATION DURING BEARING MANUFACTURE. SUBMITTER STATED SPECIAL ATTENTION SHOULD BE GIVEN TO THIS PULLEY BEARING DURING INSPECTION TO DETECT EARLY SIGNS OF RUSTING OR WEAR. REF IPC 27-10-0-24.

Part: BRACKET ASSY — WORN BOLT HOLE (RT INBD AIL)

DURING MID-D CHECK INSPECTION, RT INBD AILERON TAB CONTROL CABLE TURNAROUND PULLEY MOUNTING BRACKET WAS FOUND WITH ELONGATED PULLEY MOUNT BOLT HOLES. CAUSE WAS A RUSTED AND FROZEN BEARING IN P/N 65-25546-7 PULLEY. SPECIAL ATTENTION SHOULD BE GIVEN TO THE PULLEY TO DETECT EARLY SIGNS OF RUST AND FAILURE OF THE BEARING. REF IPC 27-10-0-24. AC TT 50080. AC CYC 32554.

Part: STRINGER — CORRODED (BS 1166)

INSPECTION FOUND STRINGER 24R CORRODED IN AFT CARGO COMPARTMENT AT STA 1166 UNDER CIRCUMFERENTIAL. THE CORRODED SECTION OF STRINGER WAS REMOVED AND A REPLACEMENT WAS FABRICATED AND INSTALLED IAW SRM 53-10-3.

Part: STRINGER — CORRODED (BS 1050-1070)

INSPECTION FOUND STRINGER 27L CORRODED FROM STA 1050-1070. THE CORRODED SECTION OF STRINGER WAS CUT OUT. A REPLACEMENT WAS FABRICATED AND INSTALLED IAW SRM 53-10-3.

Part: SKIN — CORRODED (BS 1010-1030)

INSPECTION FOUND SKIN AND STRINGERS IN AFT CARGO COMPARTMENT CORRODED BETWEEN STA 1010 AND 1030, STRINGERS 30R - 29R. THE CORRODED AREAS WERE REMOVED. A REPLACEMENT CHANNEL WAS FABRICATED AND INSTALLED IAW SRM 51-10-1 AND 51-30-2.

Part: INTERCOSTAL — CRACKED (BS 990-1010)

INSPECTION FOUND A 2 INCH CRACK AT SCREW HOLE IN FLOOR SUPPORT INTERCOSTAL BETWEEN FLOORBEAMS AT STA 990-1010, BL ZERO.

Part: STRINGER — CORRODED (BS 1148-1166)

INSPECTION FOUND STRINGER 30 AND SKIN CORRODED BETWEEN STA 1148 TO 1166. THE CORRODED AREA WAS CUT OUT, A STRINGER AND TWO SPLICES WERE FABRICATED AND INSTALLED IAW SRM 53-10-3.

Part: HINGE HOUSING — CRACKED (L2 DOOR)

INSPECTION FOUND A .50 INCH CRACK IN L-2 DOOR UPPER HINGE HOUSING. THE HINGE HOUSING WAS REMOVED AND REPLACED IAW SRM 51-10-2.

Part: ANGLE — CORRODED (BS 1140)

INSPECTION FOUND THE RIGHT AFT LAV FLOOR SUPPORT, JUST AFT OF FORWARD WALL U-CHANNEL CORRODED AT BS 1140. THE SUPPORT ANGLE WAS REMOVED AND A REPLACEMENT WAS FABRICATED AND INSTALLED IAW SRM 51-40-4.

Part: SKIN — CORRODED (BS 720)

INSPECTION FOUND FUSELAGE SKIN PANEL BULGED JUST AFT OF RT RAM AIR DOOR ACTUATOR STA 720, STRINGER 28R. THE CORROSION WAS REMOVED, A FILLER AND DOUBLER WAS FABRICATED AND INSTALLED IAW ECRA 5330-02459.

Part: FLOORBEAM — CORRODED (BS 380)

INSPECTION FOUND CORROSION ON TOP OF FLOORBEAM AT BS 380, RBL 48 TO RBL 67. THE CORRODED AREA WAS CUT OUT, A REPAIR WAS INSTALLED IAW SRM 53-10-8, FIGURE 1.

Part: ANGLE — CORRODED (BS 392)

INSPECTION FOUND FORWARD LAV FLOOR ANGLE CORRODED AT B.S. 392. THE FLOOR ANGLE WAS REMOVED AND A REPLACEMENT ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-10-1.

Part: SKIN — DENTED (BS 416)

INSPECTION FOUND THE RT FUSELAGE SKIN DENTED AT STA 416 JUST BELOW AND AFT OF OXYGEN SERVICE DOOR. THE DENTED AREA WAS CUT OUT. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-30-3, FIGURE 1.

Part: SKIN — GOUGED (RT ELEVATOR)

INSPECTION FOUND THE RT ELEVATOR LOWER SKIN GOUGED JUST AFT OF NR 2 HINGE. THE GOUGED AREA WAS CUT AWAY. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 55-30-3.

Part: SKIN — CRACKED (NR 4 LE FLAP)

INSPECTION FOUND A 1 INCH CRACK IN LOWER OUTBOARD AREA OF RT NR 4 LEADING EDGE FLAP AFT SURFACE. THE CRACK WAS STOP DRILLED. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-10-1, 51-10-2, AND ECRA 5720-01064.

Part: SKIN — CRACKED (BS 1050)

INSPECTION FOUND A 3 INCH CRACK IN LOWER FUSELAGE SKIN AT STA 1050, STRINGER 27L. THE CRACKED AREA WAS CUT OUT. A FILLER AND DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-30-3 AND 51-40-5.

Part: ANGLE — CORRODED (LOWER FUSELAGE)

INSPECTION FOUND LOWER BEACON LIGHT PANEL BULGED AT RT EDGE. CORRODED ANGLES WERE REMOVED AND REPLACEMENT ANGLES WERE FABRICATED AND INSTALLED IAW SRM 51-40-4.

Part: INTERCOSTAL — BROKEN (BS 720)

INSPECTION FOUND INTERCOSTAL BROKEN OUT ALONG TOP AT SCREW HOLES (BELOW FLOOR PANEL NR 49) AT BL ZERO BETWEEN FLOORBEAMS, B.S. 720-720A. THE INTERCOSTAL ANGLE WAS REMOVED AND A REPLACEMENT ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-10-1.

Part: SKIN — CRACKED (RT WING LE)

INSPECTION FOUND THE RT WING LEADING EDGE SKIN DENTED WITH A .25 INCH CRACK JUST OUTBOARD OF NR 5 SLAT INBOARD TRACK. THE CRACK WAS STOP DRILLED AND A DOUBLER WAS INSTALLED IAW SRM 57-30-4, FIGURE 1.

Part: SKIN — CRACKED (NR 4 LE FLAP)

INSPECTION FOUND THREE 1 INCH CRACKS IN RT NR 4 LEADING EDGE FLAP AFT SURFACE. THE CRACKS WERE STOP DRILLED. DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 51-10-1, 51-10-2, AND ECRA 5720-01064.

Part: EEL SOCKET — SHORTED (CABIN)

FLT NR 0623 - EWR - LAST EIGHT ROWS, L2, R2 AND AFT AIRSTAIR EMERGENCY LIGHTS INOPERATIVE. TROUBLE SHOT TO AFT LEFT EXIT SIGN, REMOVED AND REPLACED SHORTED SOCKET ASSY. OPERATION OF THE EMERGENCY LIGHTING WAS RESTORED. (M)

Part: EEL BATTERY PACK — DISCHARGED (CABIN)

EWR - FLT 0623 - INSPECTION FOUND EMERGENCY EXIT LIGHT AT LEFT AFT SERVICE DOOR INOPERATIVE. THE BATTERY PACK WAS REMOVED AND REPLACED AND OPERATION OF THE EMERGENCY EXIT LIGHT WAS RESTORED. (X)