N789TM

Part: SKIN — DAMAGED (TE FLAP)

FOUND THE LEFT INBOARD FORE FLAP TRAILING EDGE DAMAGED FROM POSSIBLE FOD. REMOVED AND REPLACED THE LEFT INBOARD FORE FLAP IAW THE AMM 27-51-41. (M)

Part: BATTERY PACK — INGESTED (FLASHLIGHT)

FORWARD FLIGHT ATTENDANT UPPER EMERGENCY FLASHLIGHT CHARGE INDICATOR DOES NOT BLINK. REMOVED AND REPLACED THE FLASHLIGHT BATTERY PACK IAW AMM 25-69-00. (M)

Part: POWER SUPPLY — INOPERATIVE (ESCAPE SLIDE)

AFT EMERGENCY ESCAPE SLIDE LIGHTS INOPERATIVE. REMOVED AND REPLACD THE AFT EMERGENCY LIGHT BATTERIES IAW AMM 31-51-71. (M)

Part: BATTERY — DISCHARGED (EMERGENCY LIGHT)

DURING A MAINTENANCE WALK AROUND CHECK, THE RT SIDE OVER-WING EMERGENCY EXIT LIGHT WOULD NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE POWER SUPPLY AND BATTERY PACK FOR THE RT HAND OVER-WING EMERGENCY EXIT LIGHT IAW MFG MM. EMERGENCY EXIT LIGHTS NOW OPERATE NORMALLY.

Part: POWER SUPPLY — DISCHARGED (EMERGENCY LIGHT)

MAINTENANCE REMOVED AND REPLACED THE POWER SUPPLY AND BATTERY PACK FOR THE RT OVER-WING EMERGENCY EXIT LIGHT IAW MFG MM. EMERGENCY EXIT LIGHTS NOW OPERATE NORMALLY.

Part: BATTERY PACK — WILL NOT TEST (RT OVERWING)

RIGHT OVERWING EXTERNAL EMERGENCY EXIT LIGHTS WILL NOT TEST. REPLACED BATTERY PACK PER AMM 33-51-31. (M)

Part: SWITCH — INOPERATIVE (EMERGENCY LIGHT)

DURING A PREFLIGHT CHECK, EXTERIOR EMERGENCY EXIT LIGHTS DID NTO ILLUMINATE. MAINTENANCE DISCOVERED THE EMERGENCY EXIT LIGHT SWITCH WAS NOT WORKING. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT SWITCH IAW BOEING MM 33-51-01. EXTERIOR EMERGENCY LIGHTS NOW ILLUMINATE. (M)

Part: WEB — CORRODED (FUSELAGE)

DURING A SCHEDULED MAINTENANCE VISIT, LEVEL 2 CORROSION WAS DISCOVERED ON AN AFT OVERHEAD WEB LOCATED AT FS 994 LBL 50. REMOVED THE L2 DOOR THRESHOLD DRAIN PAN FOR ACCESS TO CORRODED SECTION OF WEB, CORROSION ALSO EXTENDED TO THE INBOARD CHORD. REMOVED THE CORRODED SECTION OF WEB AND CHORD. FABRICATED AND INSTALLED REPAIR PARTS IAW BOEING 737 SRM 51-10-1 PAGE 8, 51-21-1 FIGURES 3 AND 7, 51-10-2, AND 51-30-2. (M)

Part: SKIN — CORRODED (LT WING)

DURING A SCHEDULED MAINTENANCE VISIT, LEVEL 2 CORROSION WAS DISCOVERED ON THE LT WING OUTBOARD BOOST PUMP CUTOUT AREA. BLENDED OUT THE CORROSION, HOWEVER THE REMAINING MATERIAL THICKNESS WAS BELOW MINIMUM REQUIRED, AND THE CUT OUT OF MATERIAL WAS BEYOND SRM LIMITS. FABRICATED AND INSTALLED REPAIR FILLERS IAW SRM.

Part: FRAME — CORRODED (FUSELAGE)

DURING A SCHEDULED MAINTENANCE, LEVEL 2 CORROSION WAS DISCOVERED IN THE AFT CARGO PIT ON A FRAME MEMBER LOCATED AT BS787 BETWEEN STRINGERS 22 AND 24 LEFT.

Part: SKIN — CORRODED (NR 2 ENG NACELLE)

DURING A SCHEDULED MAINTENANCE, LEVEL 2 CORROSION WAS DISCOVERED ON NR 2 ENGINE INBOARD COWLING. CORROSION WAS LOCATED UNDERNEATH THE FIRE SEAL AREA THROUGHOUT THE FORWARD AND AFT SECTION. REMOVED FIRE SEAL FOR ACCESS TO THE CORRODED SECTION OF SKIN. REMOVED THE CORRODED SECTION OF SKIN, FABRICATED AND INSTALLED NEW SECTION OF SKIN IAW SRM. FIRE SEAL WAS THEN REATTACHED TO ENGINE COWLING.

Part: STRINGER — CORRODED (FUSELAGE)

DURING A SCHEDULED MAINTENANCE, LEVEL 2 CORROSION WAS DISCOVERED IN THE AFT CARGO PIT ON STRINGER 26 RIGHT, LOCATED AT BS 980. REMOVED THE CORRODED SECTION OF STRINGER, FABRICATED AND INSTALLED REPAIR SECTION AND STRINGER SPLICE IAW WITH SRM.

Part: FITTING — CORRODED (HORIZONTAL STAB)

DURING SCHEDULED MAINTENANCE, CORROSION WAS FOUND IN THE BORES OF THE HORIZONTAL STABILIZER CENTER SECTION FORWARD TERMINAL FITTINGS UPPER AND LOWER AFT LUGS. THE BORES WERE REAMED TO THE MAXIMUM DIAMETER (1.125 INCH) SHOWN IAW SB. AFTER REAMING INSPECTION SHOWED THAT CORROSION WAS STILL PRESENT. REO-L00628 PROVIDED FOR ADDITIONAL REAMING OF THE SUBJECT BORES TO REMOVE THE CORROSION, AND FOR THE FABRICATING AND INSTALLATION OF OVERSIZED BUSHINGS. REPAIR APPROVED, AND 8110-3 ISSUED BY DER RICHARD C SALTIVAN.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

DURING A SCHEDULED MAINTENANCE VISIT, LEVEL 2 CORROSION WAS DISCOVERED ON A FLOOR SUPPORT LOCATED IN THE AFT CARGO BAY AT FS 772 LBL 5. REMOVED THE CORRODED SECTION OF FLOOR SUPPORT, FABRICATED AND INSTALLED NEW REPAIR SECTION IAW BOEING 737 SRM 53-10-5 FIGURE 6. (M)

Part: SPLICE — CORRODED (FUSELAGE)

DURING A SCHEDULED MAINTENANCE VISIT, LEVEL 2 CORROSION WAS DISCOVERED ON A STRINGER SPLICE LOCATED ON STRINGER 22 LEFT AT STATION 727-727A. REMOVED THE CORRODED STRINGER SPLICE, FABRICATE AND INSTALLED REPLACEMENT PARTS IAW BOEING SRM 51-20-1 FIGURE 7, PATE 18 AND 51-30-2 FIGURE 11, PAGE 39. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

DURING A SCHEDULED MAINTENANCE VISIT, LEVEL 2 CORROSION WAS DISCOVERED ON A CABIN FLOOR SUPPORT ANGLE LOCATED AT BS 277 BL 10L WL 208.1. REMOVED THE CORRODED SECTION OF FLOOR SUPPORT, FABRICATED AND INSTALLED REPLACEMENT PARTS IAW BOEING 737 SRM 53-10-9 FIGURE 1, 53-10-1 FIGURE 1, AND 51-40-4. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

DURING A SCHEDULED MAINTENANCE VISIT, LEVEL 2 CORROSION WAS DISCOVERED ON A PASSENGER CABIN SEAT TRACK LOCATED AT BS 360 LEFT OUTBOARD SIDE. REMOVED THE CORRODED SECTION OF SEAT TRACK AND REPLACED WITH A NEW SECTION MADE OUT OF BOEING EXTRUSION P/N BAC 1520-792. WORK DONE IAW BOEING 737 SRM 53-10-5 FIGURE 2, 53-10-01 PAGE 18, AND 51-10-2. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

DURING A SCHEDULED MAINTENANCE VISIT, LEVEL 2 CORROSION WAS DISCOVERED ON THE SCALLOPS AND WELLS OF A PASSENGER CABIN SEAT TRACK LOCATED AT BS 344-360 LEFT INBOARD SIDE. REMOVED THE CORRODED SECTION OF SEAT TRACK AND REPLACED WITH A NEW SECTION MADE OUT OF BOEING EXTRUSION P/N BAC1520-792. WORK DONE IAW BOEING 737 SRM 53-10-5 FIGURE 2. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

DURING A SCHDULED MAINTENANCE VISIT, LEVEL 2 CORROSION WAS DISCOVERED ON AN AFT RIGHT CABIN FLOOR SUPPORT LOCATED AT FS 957. TIMCO REMOVED THE CORRODED SECTION OF FLOOR SUPPORT, FABRICATED AND INSTALLED REPLACEMENT FLOOR SUPPORT AND FILLER MADE FROM 7075-T6 .100 MATERIAL. WORK DONE IAW BOEING 737 SRM 51-30-2, AND 51-10-2. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

DURING A SCHEDULED MAINTENANCE VISIT, LEVEL 2 CORROSION WAS DISCOVERED ON A FLOORBEAM LOCATED IN THE FORWARD CARGO COMPARTMENT AT FS 500 PLUS 40 INCH BL 12R, AREA OF CORROSION IS APPROXIMATELY 3 INCHES BY 1 INCH ON THE FRAME LOWER FORWARD FLANGE. REMOVED THE CORRODED SECTION AND FABRICATED AND INSTALLED A REPAIR ANGLE IAW BOEING 737 SRM 53-10-4 FIGURE 7, 6, 8, AND 9. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

DURING A SCHEDULED MAINTENANCE VISIT, LEVEL 2 CORROSION WAS DISCOVERED ON A FLOOR SUPPORT LOCATED IN THE AFT PIT AT FS 1000 LBL 17. REMOVED THE SUPPORT FITTING, FABRICATED AND INSTALLED NEW REPAIR PART IAW BOEING 737-200 SRM 51-10-2, AND 51-30-2. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

DURING A SCHEDULED MAINTENANCE VISIT, LEVEL 2 CORROSION WAS DISCOVERED ON A FLOOR SUPPORT ANGLE LOCATED AT BS 285, BL 12L, WL 208.1. REMOVED CORRODED SECTION, FABRICATED AND INSTALLED A REPLACEMENT FLOOR SUPPORT ANGLE FROM BAC 1510-335 EXTRUSION. DIMENSION OF REPAIR IS APPROXIMATELY 3.3750 INCHES X 30.5000 INCHES. WORK WAS DONE IAW SRM.

Part: SUPPORT BRACKET — CORRODED (FUSELAGE)

DURING A SCHEDULED MAINTENANCE VISIT, LEVEL 2 CORROSION WAS DISCOVERED ON AN APU BLEED AIR SUPPORT BRACKET LOCATED IN THE AFT PIT ACCESSORY COMPARTMENT AT STA 1016. REMOVED AND REPLACED THE CORRODED SUPPORT BRACKET IAW SRM.

Part: SKIN — CRACKED (FUSELAGE)

DURING A SCHEDULED MAINTENANCE VISIT, A CRACK WAS DISCOVERED IN FUSELAGE SKIN OF THE FORWRAD ENTRY DOOR LOWER HINGE CUTOUT. CRACK EXTENDS FROM THE RADIUS OF THE HINGE CUTOUT FORWARD 1.9 INCHES, TERMINATING AT A FASTENER HOLE. CRACK IS SIMILAR TO THOSE SHOWN IN 737 SRM 53-30-3 FIGURE 31, HOWEVER THE CRACK EXTENDS PAST THE MAXIMUM 1.7 INCH CUTOUT SHOWN IN THE SRM REPAIR. ENGINEERING DESIGNED AND OBTAINED APPROVAL FOR PERMANENT REPAIR. CRACKED SKIN WAS REMOVED, FABRICATED REPAIR DOUBLER AND FILLER PER REPAIR ENGINEERING ORDER REQ-L00625 REVISION A, DATED 01/28/2003. AS REQUIRED BY FINAL REPAIR ENGINEERING ORDER, REPAIR IS TO BE REINSPECTED AT 60,000 CYCLES, AND THEN REPEATED AT 4,000 CYCLE INTERVALS. (M)

Part: PANEL — CORRODED (FUSELAGE)

DURING A SCHEDULED MAINTENANCE VISIT, LEVEL 2 CORROSION, AND BROKEN RIVETS WERE DISCOVERED AROUND AIR CONDITIONING GROUND SERVICE PANEL AT FS 520 STRINGER 29L-28R. TIMCO REMOVED CORRODED SKIN SECTION, FABRICATED AND INSTALLED FILLER AND REPAIR DOUBELR OUT OF 2024 T3. 071 MATERIAL. REPAIR DIMENSIONS APPROXIMATELY 19 INCHES BY 20 INCHES. WORK DONE IAW BOEING 737-200 SRM 53-30-3, FIGURE 28. (M)

Part: PANEL — CORRODED (FUSELAGE)

DURING A SCHEDULED MAINTENANCE VISIT, LEVEL 2 CORROSION WAS DISCOVERED ON THE FORWARD RIGHT SIDE OF THE FUSELAGE TO WING FILLET PANEL NR 3479R, AFT SUPPORT. REMOVED AND REPLACED THE CORRODED TAPERED SHIMS IAW BOEING 737-200 SRM 51-10-1 PAGE 8. (M)

Part: POWER SUPPLY — DISCHARGED (CARGO BAY)

RIGHT OVER WING EXTERIOR EMERGENCY EXIT LIGHTS INOPERATIVE ON TEST. REPLACED POWER SUPPLY PER BMM 33-51-31. (M)

Part: ACTUATOR — FAILED (LT MLG)

LEFT MAIN LANDING GEAR RED LIGHT REMAINS ON AFTER GEAR IS RAISED AND WHEN GEAR HANDLE IS IN OFF POSITION, LEFT MAIN GEAR FALLS TO THE DOWN POSITION. REMOVED AND REPLACED LEFT MAIN LANDING GEAR UPLOCK ACTUATOR, PER BMM 32-32-41. PERFORMED MAIN LANDING GEAR EXTENSION AND RETRACTION TEST PER BMM 32-32-0. PERFORMED MANUAL EXTENSION TEST PER BMM 32-34-0. (M)

Part: POWER SUPPLY — DISCHARGED (CABIN)

L1 AND R1 EXTERIOR EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY POWER SUPPLY FORWARD CARGO COMPARTMENT PER BMM 33-51-71, CHECKS NORMAL. (M)

Part: LIGHT — INOPERATIVE (COCKPIT)

FOUND COCKPIT EMERGENCY LIGHT INOPERATIVE. REPLACED EMERGENCY LIGHT ASSEMBLY PER BMM 33-51-101, GROUND CHECKS NORMAL. (M)

Part: LANDING GEAR — MALFUNCTIONED (MLG)

WHEN LANDING GEAR HANDLE IS RAISED IN FLIGHT, RED LEFT GEAR LIGHT REMAINS ILLUMINATED. WHEN GEAR HANDLE IS POSITIONED TO OFF GREEN LEFT GEAR LIGHT ILLUMINATES AND LEFT MAIN EXTENDS. WHEN HANDLE IS PLACED IN DOWN POSITION ALL GREEN GEAR LIGHTS ILLUMINATE AND ALL GEAR ARE DOWN AND LOCKED. ACCOMPLISHED LUBE OF ALL LANDING GEAR AND ASSOCIATED LINKAGES PER MM 12-21. ACCOMPLISHED SEVERAL GEAR RETRACTIONS AND FREE-FALL OPERATIONS OPS CHECK OK, AIRCRAFT RELEASED FOR SERVICE. (M)

Part: ENGINE — STALLED (NR 2)

ENGINE NR 2, COMPRESSOR STALL ABOVE IDLE. (M)

Part: ENGINE — FAILED (NR 2)

SHUT DOWN NR 2 ENGINE DUE TO LOW OIL QUANTITY AND HIGH OIL TEMP. FOUND OIL EXITING THROUGH TAIL PIPE. (M)

Part: POWER SUPPLY — DISCHARGED (CABIN)

RIGHT AND LEFT EMERGENCY EXIT INTERIOR OVERWING LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY PACK AND BATTERY POWER SUPPLY UNIT, OPS NORMAL IAW 33-51-41, AND 33-51-31. (M)

Part: CONNECTOR — LOOSE (CABIN)

FLOOR EMERGENCY LIGHTS FORWARD INOPERATIVE. INSPECTED FOUND LOOSE CONNECTION, REINSTALLED AND CLEANED OPS CHECK NORMAL. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

MID CABIN EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED BATTERY PACK, OPS CHECK NORMAL IAW 33-51-11. (M)

Part: LAMP — INOPERATIVE (DOOR EMER EXT LT)

LT 1 DOOR EMERGENCY EXTERIOR LIGHT INOPERATIVE. REMOVED AND REPLACED LAMP, OPS CHECK NORMAL.

Part: LATCH — UNLATCHED (NACELLE)

DURING FLIGHT, THE SR FLIGHT ATTENDANT NOTIFIED THE CAPTAIN THAT A PIECE OF COWLING WAS LOOSE. THE CAPT CONFIRMED THAT THE NACELLE FAIRING THAT LIES BETWEEN THE WING AND THE ENGINE COWLING WAS LOOSE, THE COWLING LATCH HAD COME UNDONE AND THE FAIRING WAS AJAR AND RAISED FROM THE NORMAL POSITION. THE CAPTAIN MADE THE DECISION TO LAND AND HAVE THE FAIRING SECURED. MAINTENANCE INSPECTED AREA, SECURED THE LOOSE LATCH, OPS CHECK GOOD.

Part: CONNECTOR — DISCONNECTED (CABIN)

EMERGENCY ESCAPE PATH MARKING SYSTEM INOPERATIVE FROM ROW 1 TO ROW 15. FOUND FLOOR CONNECTOR UNPLUGGED, RECONNECTED, OPS CHECK GOOD, OK FOR SERVICE.

Part: THRUST REVERSER — DAMAGED (NR 2 ENGINE)

ON WALK AROUND, DISCOVERED 2 INCH BY 1 INCH HOLE IN SUPPRESSION MATERIAL OF ENGINE NR 2 THRUST REVERSER. PERFORMED FERRY FLIGHT INSPECTION IAW WITH CASINO EXPRESS MPP CHAPTER 8-1, FOUND A/C OK FOR FERRY FLIGHT FROM CLT TO GSO. REMOVED AND REPLACED THRUST REVERSER. REMOVED NR 2 ENGINE AND INSTALLED ENGINE. (M)

Part: LIGHT — INOPERATIVE (EXTERIOR)

L1 DOOR EMERGENCY EXTERIOR LIGHT INOPERATIVE. RELAMPED LIGHT, OPS CHECK NORMAL IAW 33-51-61. (M)

Part: TURBINE — FAILED (NR 2 ENGINE)

ON TAKEOFF, HEARD LOUD BOOM FROM NR 2 ENGINE. ABORTED TAKEOFF. FOUND NR 2 ENGINE HAD SUSTAINED A CONTAINED TURBINE FAILURE. REMOVED AND ENGINE S/N 709439, AND SENT TO SHOP FOR EVALUATION. (M)

Part: SEAL — LEAKING (ACCESS PANEL)

FUEL LEAKING FROM RIGHT WING IN FLIGHT, ALSO ON GROUND FROM OUTSIDE INSPECTION PANEL. REMOVED ACCESS PANEL AT SURGE TANK FOUND SEAL COMING LOOSE, CLEANED PANEL RESEALED AND CURED SEALANT FOR 4 HOURS. REINSTALLED ACCESS PANEL PER MM 28-11-011-4, LEAK CHECKED GOOD. (M)

Part: LIGHT — INOPERATIVE (EXTERIOR)

FOUND EXTERIOR EMERGENCY LIGHT AT L1 DOOR INOPERATIVE. RELAMPED, OPS CHECK NORMAL, IAW BMM 33-51-61. (M)

Part: TIRE — DEFORMED (NLG)

WHEN GEAR IS RETRACTED MUCH VIBRATION, ALSO VIBRATION WHEN HIGH SPEED BEFORE ROTATION. INSPECTED NOSE TIRES AND FOUND THEM GROSSLY OUT OF ROUND. REMOVED AND REPLACED NOSE TIRES PER BMM 32-45-21. (M)

Part: MODULE — NOT SEATED (EE BAY)

WHEEL WELL FIRE WARNING WON''T TEST. AIRCRAFT RELEASED PER MEL 26-4, DMI0214. REF MEL 26-4, DMI 0214, RESEATED OVERHEAT MODULE M237 IN ELECTRONIC COMP. OPS CHECK NORMAL. PLACARD REMOVED. (M)

Part: LIGHT — INOPERATIVE (EXTERIOR)

LEFT HAND EXTERIOR EMERGENCY LIGHT, INOPERATIVE. RELAMPED. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN)

AFT EXTERIOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED RIGHT AFT EXTERIOR EMERGENCY LIGHT REFLECTOR PER BMM 33-51-41. OPS CHECKED SATISFACTORY AT THIS TIME. (X)

Part: POWER SUPPLY — INOPERATIVE (CABIN)

AFT PASSENGER CABIN EMERGENCY CEILING LIGHT INOPERATIVE. REMOVED AND REPLACED POWER SUPPLY PER LUMINESCENT SYSTEM MAINTENANCE AND INSTALLATION MANUAL 33-50-01 PAGE 703 TEST, OK. (M)

Part: BATTERY PACK — INOPERATIVE (CABIN)

AFT EMERGENCY TRACK LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK, IAW CMM 33-50-01. (M)

Part: POWER SUPPLY — INOPERATIVE (CABIN)

AFT EMERGENCY LIGHTS FLOOR AND DOOR INOPERATIVE. REMOVED AND REPLACED AFT EMERGENCY LIGHT POWER SUPPLY, OPS CHECK GOOD, 33-51-81. (X)

Part: ENGINE — MALFUNCTIONED (NR 1)

IN FLIGHT SHUTDOWN NR 1 ENGINE, RAPID DROP OF OIL PRESSURE. ENGINE WINDMILL TIME APPROX 12 MINUTES. TROUBLESHOT IAW 79-32-0, OIL PRESSURE, FOUND TO BE OK, NORMAL. NO OTHER PROBLEMS AT THIS STATION. WINDMILL TIME 12 MINUTES, NO ACTION REQUIRED. OK FOR RETURN TO SERVICE. (M)

Part: LIGHT — INOPERATIVE (CABIN)

RIGHT EMERGENCY EXIT MARKER LIGHT INOPERATIVE. REMOVED AND REPLACED RIGHT EMERGENCY EXIT MARKER LIGHT IAW LOCTITE LUMINESCENT SYSTEMS MANUAL 33-50-01. (M)

Part: POWER SUPPLY — INOPERATIVE (CABIN)

LEFT EMERGENCY EXIT MARKER LIGHT INOPERATIVE. REMOVED AND REPLACED BATTERY POWER SUPPLY FOR LEFT EMERGENCY EXIT MARKER LIGHTS IAW LOCTITE LUMINESCENT SYSTEM MANUAL 33-50-01. (M)

Part: LIGHT — INOPERATIVE (CABIN)

EXTERIOR EMERGENCY LIGHT AFT OF R1 DOOR INOPERATIVE. REMOVED AND REPLACED THE REFLECTOR ASSY PER BMM 33-51-01, OPS CHECK GOOD AT THIS TIME. (M)

Part: LIGHT — INOPERATIVE (CABIN)

EXTERIOR EMERGENCY LIGHT AFT OF L2 DOOR INOPERATIVE. REMOVED AND REPLACED THE REFLECTOR ASSY PER BMM 33-51-01, OPS CHECK GOOD AT THIS TIME. (M)

Part: SHEAR TIE — CORRODED (FUSELAGE)

AFTER REMOVING THE LOWER SKIN PANEL, STATION 727 TO 907, THE 65-46551-16 FRAME SHEAR TIE BETWEEN STRINGER 27 AND 26 LEFT WAS FOUND TO HAVE CORROSION BEYOND LIMITS. THE -16 FRAME ASSEMBLY IS NOT AVAILABLE IN PRODUCTION AND THE 65-46551-38 IS USED IN THIS LOCATION. REPAIRED IAW BOEING SUPPLIED ENGINEERING. (M)

Part: LIGHT — INOPERATIVE (EXTERIOR)

AFT L2 OUTSIDE EMERGENCY EXIT LIGHT INOPERATIVE. CLEANED CORROSION FROM LIGHT SOCKET IAW BMM 20-40-12, OPS CHECK GOOD. (M)

Part: LIGHT — INOPERATIVE (OVERWING)

LEFT OVERWING LOWER EMERGENCY EXIT LIGHTS ARE INOPERATIVE. DISCOVERED THE CONNECTOR TO THE POWER SUPPLY NOT SEATED AND LOCKED IN POSITION, CORRECTLY MATED CONNECTOR AND OPS CHECKED SYSTEM NORMAL IAW LLS MM 33-50-01 PAGE 104. (M)

Part: ADC — MALFUNCTIONED (COCKPIT)

DURING CRUISE, SEVERAL ABNORMAL INDICATIONS OCCURRED, AS FOLLOWS, NR 1 ALTIMETER WITH OFF FLAGS AND SPINNING, MACH TRIM FAIL LIGHT, NR 1 AIRSPEED WITH FLAGS WITH BARBER POLE REDUCED TO 260 KNOTS, GROUND PROX INOPERATIVE, EPR INOPERATIVE, AND PDC WENT INTO TEST MODE. RE-RACKED AIR DATA COMPUTER PER 34-12-0. OPERATION OF EFFECTED SYSTEM CHECK OK. (M)

Part: ACCESSORY UNIT — MALFUNCTIONED (LANDING GEAR)

ABNORMAL GEAR RETRACTION. VISUALLY CHECKED ALL LANDING GEAR, UPLOCK AND DOWNLOCK SENSORS AND WIRING. REPLACED LANDING GEAR ACCESSORY UNIT AND TESTED IAW BMM 32-09-100. ALL TESTS WERE NORMAL JACKED AIRCRAFT AND PERFORMED EXT/RET TEST IAW BMM 7-11-11. ALL TESTS NORMAL. AIRCRAFT CHECK FLIGHT COMPLETED. NO DISCREPANCIES NOTED. (M)

Part: BATTERY PACK — DISCHARGED (LT EMER EXIT)

LEFT EMERGENCY OVERWING EXIT LIGHTS INOPERATIVE, INTERIOR. REMOVED AND REPLACED LEFT EMERGENCY OVERWING INTERIOR BATTERY PACK, IAW BMM 33-51-01, OPS CHECK NORMAL. (M)

Part: LIGHT — INOPERATIVE (L2 DOOR)

EMERGENCY EXIT LIGHT ON L-2 DOOR INOPERATIVE. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ON L-2 DOOR PER 33-51-101. (X)