N233TM

Part: STRINGER — CORRODED (FUSELAGE)

DURING A SCHEDULED C-CHECK INSPECTION, LEVEL TWO CORROSION WAS DISCOVERED ON STRINGER 26L STATION 950 BL 10L. REMOVED AND REPLACED THE CORRODED SECTION OF STRINGER 26L AT STATION 950 BL 10L IAW BOEING SRM 53-10-3. (M)

Part: STRINGER CLIP — CORRODED (FUSELAGE)

DURING A SCHEDULED C-CHECK INSPECTION, LEVEL TWO CORROSION WAS DISCOVERED ON STRINGER TIES AT STATION 967 STRINGER 26L AND STRINGER 27L. REMOVED AND REPLACED CORRODED STRINGER TIES OF STRINGER 26L AND STRINGER 27L AT STATION 967. STRINGER TIES WERE FABRICATED FROM 7075-T6 .063. WORK DONE IAW BOEING SRM CHAPTER 51-30-2. (M)

Part: STRINGER — CORRODED (FUSELAGE)

DURING A SCHEDULED C-CHECK INSPECTION, LEVEL TWO CORROSION WAS DISCOVERED ON STRINGER 27L AT STATION 950 LBL 5. REMOVED AND REPLACED CORRODED SECTION OF STRINGER 27L AT STATION 950 LBL 5 IAW BOEING SRM CHAPTER 53-10-3. (M)

Part: FRAME — CORRODED (FUSELAGE)

DURING A SCHEDULED C CHECK INSPECTION, LEVEL TWO CORROSION WAS DISCOVERED ON A FRAME RIB AT STATION 285 FROM STRINGER 24L TO STRINGER 28L. CUTOUT CORRODED AREA OF FRAME AT STATION 285 FROM STRINGER 24L TO STRINGER 28L. FABRICATED FILLER AND DOUBLER USING 7075-T6 .040. INSTALLED FASTENERS AND REPAIR PARTS IAW BOEING SRM CHAPTER 51-40-2. TREATED AND PRIMED FABRICATED PARTS AND SURROUNDING STRUCTURE IAW BOEING SRM CHAPTER 51-30-2. (M)

Part: SUPPORT BRACKET — CORRODED (SLAT ACTUATOR)

DURING A SCHEDULED C-CHECK INSPECTION, LEVEL TWO CORROSION WAS DISCOVERED ON A LEADING EDGE SLAT ACTUATOR SUPPORT BRACKET ON THE LEFT WING SPAR AT WING STATION 421. REMOVED AND REPLACED THE SUPPORT BRACKET AT THE CENTER OF THE NUMBER TWO LEADING EDGE SLAT ACTUATOR ATTACHMENT LOCATED ON THE LEFT HAND WING SPAR AT STATION 421 IAW BOEING SRM CHAPTER 51-30-2. (M)

Part: STRINGER CLIP — CORRODED (FUSELAGE)

DURING A SCHEDULED C-CHECK INSPECTION, LEVEL TWO CORROSION WAS DISCOVERED ON TWO STRINGER TIE OF STRINGER 26L LOCATED AT STATION 947. REMOVED AND REPLACED CORRODED STRINGER TIE OF STRINGERS 26L AT STATION 947. STRINGER TIES WERE FABRICATED FROM 7075-T6 .063. WORK DONE IAW BOEING SRM 51-30-2. (M)

Part: BRACKET — CORRODED (FUSELAGE)

DURING A SCHEDULED C-CHECK INSPECTION, LEVEL TWO CORROSION WAS DISCOVERED ON A BRACKET LOCATED AT STATION 950 LBL 15. REMOVED AND REPLACED CORRODED BRACKET LOCATED AT STATION 950 LBL 15. BRACKET WAS FABRICATED FROM 7075-T6 .050. WORK DONE IAW BOEING SRM 51-30-2. (M)

Part: LIGHT — INOPERATIVE (CABIN)

AFT EMERGENCY TRACK LIGHT AND BOTTOM AFT EXIT LIGHTS INOPERATIVE. REMOVED AND REPLACED LIGHT STRIP IAW CMM 33-50-01. OPERATIONAL CHECK OK.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT)

LT SIDE EMERGENCY OVER-WING LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY BATTERY PACK, OPERATIONAL CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT)

RT SIDE EMERGENCY OVER-WING LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY BATTERY PACK, OPERATIONAL CHECK GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

FOUND LEFT EXTERIOR EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED THE BATTERY PACK IAW AMM 33-51-31. (M)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

FOUND RIGHT EXTERIOR EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED THE BATTERY PACK IAW AMM 33-51-31. (M)

Part: BATTERY — INOPERATIVE (LT OVERWING)

DURNG A MAINTENANCE WALK AROUND CHECK, THE LEFT OVERWING EMERGENCY EXIT LIGHT WOULD NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE BATTERY AND BATTERY CHARGER ASSEMBLY P/N 6104789 FOR THE LEFT OVERWING EMERGENCY EXIT LIGHT IAW BOEING MM 33-51-81. THE LEFT OVERWING EMERGENCY EXIT LIGHT NOW OPERATES NORMALLY. (M)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DURING A MAINTENANCE WALK AROUND CHECK, THE FORWARD CABIN DOOR R1 EMERGENCY EXIT LIGHT WOULD NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK FOR THE FWD R1 CABIN DOOR IAW BOEING MM 33-51-81. THE FWD R1 CABIN DOOR EMERGENCY EXIT LIGHT NOW OPERATES NORMALLY. (M)

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT)

DURING A MAINTENANCE WALK AROUND CHECK, THE MID CABIN OVERHEAD EMERGENCY EXIT LIGHT WOULD NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE BATTERY CARTRIDGE IAW BOEING MM 33-51-31. THE MID CABIN OVERHEAD EMERGENCY EXIT LIGHT NOW OPERATED NORMALLY. (M)

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT)

DURING A MAINTENANCE WALK AROUND CHECK, THE AFT CABIN OVERHEAD EMERGENCY EXIT LIGHT WOULD NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE BATTERY CARTRIDGE FOR THE AFT CABIN OVERHEAD EMERGENCY EXIT LIGHT IAW BOEING MM 33-51-81. THE AFT CABIN OVERHEAD EMERGENCY EXIT LIGHT NOW OPERATES NORMALLY. (M)

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT)

DURING A MAINTENANCE WALK AROUND CHECK, AN AISLE EMERGENCY EXIT SIGN WOULD NOT TEST. MAINTENANCE REMOVED AND REPLACED THE BATTERY CARTRIDGE PER BOEING MM 33-51-81, SYSTEM NOW CHECKS NORMAL. (M)

Part: ENGINE — FAILED (NR 1)

ON TAKEOFF AT 80 KNOTS, NR 1 ENGINE FAILED. THE TOWER REPORTED THE ENGINE WAS ON FIRE, NO FIRE WARNING INDICATION. DISCHARGED THE FIRE BOTTLE. INSPECTION REVEALED EXTENSIVE DAMAGE TO THE T-1 THROUGH T-4 TURBINE BLADES, TURBINE FAILURE WAS CONTAINED. FAILURE CAUSE NOT DETERMINED, ENGINE PARTED OUT AND SOLD.

Part: TIRE — SEPARATED (NLG)

ON TAKEOFF ROLL HEARD LOUD BANG JUST BEFORE ROTATION. INSPECTION FOUND NR 2 NOSE TIRE HAD THROWN TREAD. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DURING A MAINTENANCE PREFLIGHT INSPECTION, THE EMERGENCY EXIT LIGHT OVER THE R-2 DOOR WOULD NOT ILLUMINATE WITH THE SWITCH IN THE ON POSITON. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT ASSEMBLY, SYSTEM CHECKS NORMALLY. (M)

Part: LIGHT — DISCONNECTED (CABIN)

EMERGENCY FLOOR PROXIMITY LIGHTING (FROM PASSENGER ROWS 14 THROUGH 17) NOT LIGHTING DURING OPERATIONAL CHECK. MAINTENANCE DISCOVERED THAT THE LIGHTING STRIP FOR THIS SECTION HAD BECOME DISCONNECTED FROM ITS POWER SOCKET. LIGHT STRIP WAS REATTACHED AND OPERATIONALLY TESTED NORMAL PER LUMINESCENT COMPONENT MM 33-51-01. (M)

Part: LIGHT — BROKEN (PAX CABIN)

EMERGENCY FLOOR LIGHTING STRIP BROKEN AT SEAT 15D. INSTALLED LIGHT STRIP AS REQUIRED, OPS CHECK GOOD, IAW AMM 33-51-07. (M)

Part: BATTERY PACK — DISCHARGED (FLASHLIGHT)

AFT EMERGENCY FLASH LIGHT BATTERY CONDITION INDICATOR NOT BLINKING. REPLACED BATTERY PACK, NORMAL MAINTENANCE. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

CORROSION ADJACENT TO WATER DRAIN LINE FORWARD UNDER SIDE OF R2 DOOR SCUFF PLATE AREA BS 958 RBL 53. REMOVED CORROSION FROM LOWER OUTBOARD FLOORBEAM SUPPORT, CORROSION WENT OUT OF LIMITS. FABRICATED REPAIR DOUBLER AND INSTALLED IAW B737 SRM 51-40-3, 51-10-2, 51-20-1 AND 51-30-2. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

DURING A SCHEDULED C-CHECK INSPECTION DISCOVERED LEVEL 2 CORROSION ADJACENT TO WATER DRAIN LINE FORWARD UNDER SIDE OF R2 DOOR SCUFF PLATE AREA BS 958 RBL 53. REMOVED CORROSION FROM LOWER OUTBOARD FLOORBEAM SUPPORT, CORROSION WENT OUT OF LIMITS. FABRICATED REPAIR DOUBLER AND INSTALLED IAW B737 SRM 51-40-3, 51-10-2, 51-20-1 AND 51-30-2. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

DURING SCHEDULED C-CHECK INSPECTION DISCOVERED, L1 DOOR AFT GIRTH BAR ATTACH FITTING AND OUTBOARD FLOORBOARD SUPPORT AT BS 346 LBL 60 CORRODED. FOUND GIRTH BAR FITTING AND FLOORBOARD SUPPORT CORRODED OUT OF LIMITS FORMED REPAIR FLOORBOARD SUPPORT AND GIRTH BAR FITTING. INSTALLED IAW B737 SRM 51-40-3, FIG 1, 51-30-2, 51-10-2, 51-10-7, 51-30-8 AND 51-10-1. (M)

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2

DURING A SCHEDULED C-CHECK INSPECTION OF THE AFT CARGO COMPARTMENT BILGE AREA, DISCOVERED LEVEL 2 CORROSION. ON THE FORWARD END OF STRINGERS 25L AT STATION 967. CUT OUT DAMAGED SECTION, IAW BOEING SRM 53-10-3 FIGURE 1. FABRICATED AND INSTALLED STRINGER REPAIR IAW BOEING SRM 53-10-3. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2

DURING A SCHEDULED C-CHECK INSPECTION, DISCOVERED AFT FUSELAGE FLOOR SUPPORT FRAME AT STATION 951 FROM LBL 20 TO LBL 36 HAS LEVEL 2 CORROSION. REMOVED FLOOR SUPPORT FRAME, FABRICATED AND INSTALLED FRAME REPAIR IAW BOEING SRM 53-10-2 AND 51-30-2. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

DURING SCHEDULED C-CHECK INSPECTION DISCOVERED FLOOR SUPPORT BETWEEN FRAME 947-967 RIGHT APPROX BL40R HAS FLAKING CORROSION. FLOOR SUPPORT CORRODED OUT OF LIMITS. FABRICATED REPLACEMENT SUPPORT AND INSTALLED IAW B737 SRM 53-10-1, 51-10-2 AND 51-30-2. (M)

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2

DURING A SCHEDULED C-CHECK INSPECTION OF THE FORWARD CARGO COMPARTMENT, DISCOVERED A TWO INCH SPOT OF LEVEL 2 CORROSION ON STRINGER 27L AT STATION 389. FABRICATED AND INSTALLED STRINGER REPAIR IAW BOEING 737 SRM 51-10-2, 51-10-6, 51-30-2, 53-10-01 FIGURE 1 AND 53-10-3 FIGURE 1. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

DURING SCHEDULED C-CHECK INSPECTION DISCOVERED FORWARD LAVATORY FLOOR STATION 294.5 WL 208 LBL 12 FLOORBEAM HAS 12 INCHES OF CORROSION. FLOORBEAM CORRODED MORE THAN 50 PERCENT, OUT OF LIMITS. REMOVED CORRODED FLOORBEAM UPPER T-CAP AND SPLICE. FABRICATED REPAIR T-CAP AND SPLICE. INSTALLED IAW B737 53-10-9 AND 51-30-2 FIG 5. (M)

Part: ANGLE — CRACKED (HORIZ STAB)

LEFT CENTER HORIZONTAL STABILIZER REAR STABILIZER FITTING HAS CRACKED ANGLE STATION 1170, BELOW LEFT HORIZONTAL STABILIZER PIN/AFT. REMOVED CRACKED ANGLE IAW B737 SRM 51-30-2. TRIMMED TO FIT NEW SUPPORT ANGLE IAW B737 SRM 51-30-5, 51-10-1, 51-20-1 FIG 1/2. INSTALLED IAW B737 SRM 51-30-2. (M)

Part: SKIN — GOUGED (T/E FLAP)

RIGHT WING OUTBOARD FLAP, LOWER FORE FLAP LEADING EDGE SKIN GOUGED, FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED REPAIR DOUBLER IAW B737 SRM 57-50-4 FIG 2, 51-10-2 AND 51-30-8. (M)

Part: SKIN — DELAMINATED (T/E FLAP)

DURING SCHEDULED C-CHECK INSPECTION DISCOVERED RIGHT WING INBOARD AFT FLAP LOWER SKIN DELAMINATED AT T/E SECTION. CUT OUT DELAMINATED AREA .5 INCH BY 1 INCH. FABRICATED AND INSTALLED SKIN SECTION AND DOUBLER. BONDED AND APPLIED FIBERGLASS REPAIR IAW B737 SRM 51-40-2 AND TIMCO REO-L00602 REV A. (M)

Part: STRINGER CLIP — CORRODED (FUSELAGE)

AFT FUSELAGE FLOORBEAM STATION 967 LEFT SIDE WHERE MEETS CIRCUMFERENTIAL FRAME HAS CORRODED STRINGER TIE. REMOVED STRINGER TIE CLIP, FABRICATED AND INSTALLED REPAIR CLIP IAW B737 SRM 51-10-2, 51-30-2 AND 51-20-1. (M)

Part: INTERCOSTAL — CORRODED (FUSELAGE)

NOSE WHEEL WELL LEFT SIDE AT AFT ACCESS PANEL SUPPORT BEAMS, THREE EACH HAS EXFOLIATED CORROSION FS 280. REMOVED AND REPLACED TWO EXFOLIATED INTERCOSTALS IAW B737 SRM 51-30-2, 51-20-1, B737 MM 51-21-0. REMOVED CORROSION FROM THIRD VERICAL BEAM FOUND TO BE WITHIN LIMITS. (M)

Part: STRINGER — CORRODED (FUSELAGE)

DURING SCHEDULED C-CHECK INSPECTION DISCOVERED AFT LOWER BILGE STATION 1006, STRINGER 23L, CLIP CORRODED. REMOVED CLIP AND S23L IN THE AFT LOWER BILGE BS 1006. FORMED REPAIR STRINGER AND CLIP AND INSTALLED IAW B737 SRM 53-10-3 AND 51-10-2. (M)

Part: SKIN — CRACKED (L/E SLAT)

LEFT WING NR 2 SLAT TRAILING EDGE CHAFED AND CRACKED AT OUTBOARD AUX SLAT TRACK. REPAIRED CRACKED AND CHAFED LEFT WING NR 2 SLAT TRAILING EDGE AT OUTBOARD AUX SLAT TRACK BY CUTTING OUT DAMAGED SECTION, FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW B737 SRM 51-30-2 AND 51-40-2. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

FLOORBEAM BS 976, LBL 53 HAS EXFOLIATED CORROSION. REMOVED FLOORBEAM, FABRICATED AND INSTALLED FLOORBEAM REPAIR 55 INCHES BY 1.5 INCHES BAC1505-100617, IAW TIMCO REO-L00597 REV A. (M)

Part: LIGHT — INOPERATIVE (CABIN)

FLOOR EMERGENCY LIGHTS MID-SECTION INOPERATIVE. RECONNECTED LAMP TESTED.

Part: BATTERY — INOPERATIVE (CABIN)

COCKPIT EMERGENCY LIGHT INOPERATIVE. REMOVE AND REPLACE BATTERIES ON BATTERY PACK PER MM. OPS TEST NORMAL.

Part: POWER SUPPLY — DISCHARGED (CABIN)

FOUND LEFT EXTERIOR OVERWING EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY POWER SUPPLY IAW BMM 33-51-31, CHECKS NORMAL. (M)

Part: LIGHT — INOPERATIVE (L2 DOOR)

L2 DOOR EMERGENCY EXIT PORTABLE LIGHT INOPERATIVE. REMOVED AND REPLACED PORTABLE EMERGENCY EXIT LIGHT ON L2 DOOR, OPS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN)

LEFT EXTERIOR OVER WING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY POWER SUPPLY BATTERY PACK ASSEMBLY. OPS CHECK OK

Part: CONTROLLER — MALFUNCTIONED (CABIN PRESSURE)

CABIN RATE OF CLIMB/DESCENT TEMPORARILY INTERMITTENT OPERATION DURING CLIMB IN BOTH 'STANDBY' AND 'MANUAL' MODE. OUTFLOW VALVE WOULD NOT MOVE IN 'MANUAL' MODE. REPLACED OUTFLOW VALVE P/N 763810-2 AND CABIN PRESSURIZATION CONTROLLER P/N 7110033 AS REQUIRED BY MM 21-31. GROUND OPERATIONAL CHECKS AS PER BMM 21-31-0 NORMAL. (M)

Part: LIGHT — INOPERATIVE (CABIN)

ON WALK AROUND, DISCOVERED LUMINESCENT STRIP ON EMERGENCY TRACK LIGHTING INOPERATIVE. REMOVED AND REPLACED LUMINESCENT STRIP IAW LOETITE LUMINESCENT SYSTEMS, BMM 33-51-01, OPS CHECK GOOD. (M)

Part: LIGHT — LOOSE (CABIN)

L3 DOOR EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND RESEATED L3 DOOR LIGHT ASSEMBLY IAW 33-51-01, OPS CHECK GOOD. (M)

Part: LIGHT — DAMAGED (CABIN)

AFT CABIN EMERGENCY EXIT TRACK LIGHT DAMAGED BEYOND REPAIR. REMOVED AND REPLACED AFT CABIN EMERGENCY EXIT TRACK LIGHTING, OPS CHECK GOOD IAW 33-51-01. (M)

Part: LIGHT — DISCONNECTED (CABIN)

FOUND FORWARD FLOOR MOUNTED EMERGENCY EXIT LIGHTS INOPERATIVE. SWAPPED BATTERY PACK WITH CENTER TRACK LIGHTING BATTERY FOUND SERVICEABLE, BUT TRACK NR 1 SECTION FOUND UNHOOKED FROM CIRCUIT. RECONNECTED LIGHTS, OPS CHECK GOOD IAW BMM 33-52-11. (M)

Part: BATTERY — DISCHARGED (CABIN)

ON WALK AROUND, FOUND OVERWING EXIT EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY CARTRIDGE AND POWER UNIT IAW 33-53-00. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

CENTER CABIN EMERGENCY EXIT SIGN LIGHTS INOPERATIVE. REMOVED AND REPLACED LIGHTS BATTERY PACKS 2. OPS CHECK OF EMERGENCY EXIT LIGHTS GOOD IAW BMM 33-51-51. (M)

Part: GUARD — BROKEN (LIGHT SWITCH)

FOUND EMERGENCY LIGHT SWITCH GUARD SPRING BROKEN. REMOVED AND REPLACED GUARD ON EMERGENCY LIGHT SWITCH P5 PANEL 33-5-01, OPS CHECK NORMAL. (M)

Part: LIGHT — INOPERATIVE (CABIN)

EMERGENCY FLOOR TRACK FORWARD SECTION INOPERATIVE. CLEANED CONNECTOR ON POWER SUPPLY, OPS TESTED PER LOCTITE LUMINESCENT SYSTEM COMPONENT MANUAL 33-50-01. (M)

Part: BATTERY — DISCHARGED (SMOKE DETECTOR)

OVERHEAD MAINTENANCE LIGHT ILLUMINATED FOR LOWER CARGO COMPARTMENT FIRE DETECTION AND SUPPRESSION SYSTEM. AIRCRAFT RELEASED PER MEL 26-19-5-6, ITEM TRANSFERRED TO DMI LOG DMI NR 207, ITEM PLACARDED. REF MEL 26-19-56, DMI 0207, REMOVED AND REPLACED BATTERIES ON FORWARD SMOKE DETECTOR, S/N F12671. OPS CHECKS PER STC 3000 COMPONENT INSTALLATIONS MANUAL. (M)

Part: SMOKE DETECTOR — MALFUNCTIONED (CARGO BAY)

CARGO COMPARTMENT FIRE DETECTION AND SUPPRESSION SYSTEM MESSAFE 1 F12671 ON OVERHEAD CONTROL DISPLAY UNIT. REMOVED AND REPLACED FORWARD SMOKE DETECTOR PER ST 3000 COMPONENT INSTALLATION MANUAL, OPS TESTED SYSTEM NORMAL. (M)

Part: LIGHT — INOPERATIVE (CABIN)

FLOOR EMERGENCY LIGHT LAMP INOPERATIVE AT ROW 4 D/E/F. AIRCRAFT RELEASED PER MEL 33-19, ITEM TRANSFERRED TO DMI LOG NR 0127, ITEM PLACARDED. REF MEL 33-19, DMI 0127, REMOVED AND REPLACED LAMP ON FLOOR TRACK PER LUMINESCENT CCM2-5-1. (M)

Part: LIGHT — INOPERATIVE (CABIN)

AFT OVERHEAD EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED LIGHT ASSEMBLY PER 33-51-91. OPS CHECK NORMAL. (M)

Part: BATTERY PACK — INOPERATIVE (CABIN)

EMERGENCY EXIT LIGHT INTERIOR OVERWING EXIT HATCH INOPERATIVE, LEFT AND RIGHT. REPLACED EMERGENCY LIGHT BATTERY PACK POWER SUPPLY, OPS CHECK NORMAL IAW BMM 33-51-31. (M)

Part: BATTERY PACK — INOPERATIVE (CABIN)

AFT EMERGENCY TRACK LIGHTS AND REAR DOORS INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK. OPS CHECK GOOD IAW BMM 33-51-51. (M)

Part: BLEED VALVE — CONTAMINATED (APU)

SMOKE IN CABIN, ALARM SOUNDED. INVESTIGATION DETERMINED LUBE FROM PREVIOUS BLEED VALVE LUBRICATION, TO BE CAUSE OF SMOKE. SEPARATED RT AND LT PACKS WITH BOTH APU BLEED AND ENGINE BLEED SUFFICIENTLY TO CLEAR SYSTEM OF ANY AND ALL RESIDUE. AIR CONDITIONING SYSTEM, OPS CHECK SATISFACTORY AT THIS TIME PER BMM 21-51-0. (M)

Part: BATTERY PACK — INOPERATIVE (CABIN)

FORWARD EMERGENCY EXIT DOOR LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY PACK, OPS CHECK NORMAL IAW 33-51-1. (M)

Part: BATTERY PACK — INOPERATIVE (CABIN)

LEFT SIDE OVERWING EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED OVERWING EMERGENCY LIGHT BATTERY PACK, OPS CHECK NORMAL IAW BMM 33-51-31. (M)

Part: LIGHT — INOPERATIVE (CABIN)

FLOOR EMERGENCY LIGHTS MID SECTION INOPERATIVE. CLEANED CONNECTOR BEHIND SIDEWALL PANEL, OPS TESTED PER LUMINESCENT SYSTEM 33-50-01, PAGE 503, TEST OK. (M)

Part: GENERATOR — FAILED (NR 1)

LOST BATTERY CHARGER, NR 1 TANK FUEL BOOST PUMPS BOTH FORWARD AND AFT, LOST NR 1 B-HYD PUMP SYSTEM NR 1 ENGINE THRUST REVERSER CIRCUIT BREAKERS UNABLE TO RESET. RESET CIRCUIT BREAKERS RAN ENGINE, DETERMINED PROBLEM TO BE NR 1 GENERATOR. A/C RELEASED PER MEL 24-1, DMI 0215, ITEM PLACARD AND TRANSFERRED TO DMI LOG. TIGHTENED AND REPAIRED GROUND WIRES AS REQUIRED IAW 20-20-00, STD WIRING PRACTICES, REMOVED AND REPLACED NR 1 GENERATOR PER BMM 24-21-11, OPS CHECK OK. (M)

Part: LINE — CHAFED (HYD SYSTEM)

AFTER DEPARTING IND, PILOT NOTICED LOW 'A' SYSTEM HYDRAULIC QTY. SOON AFTER LOW PRESSURE OF NR 1 HYD PUMP 'A' SYSTEM MASTER CAUTION WARNING FOLLOWED BY NR 2 HYD PUMP 'A' SYSTEM MASTER CAUTION WARNING.. CREW IMPLEMENTED QHR PROCEDURE AND LANDED AT STL. UPON INSPECTION ON GROUND, NR 1 ENGINE 'A' PUMP PRESSURE LINE WAS EXCESSIVELY CHAFED. NR 1 ENGINE 'A' PUMP PRESSURE LINE WAS REPLACED. AIRCRAFT WAS REPOSITIONED TO EKO WITHOUT FURTHER PROBLEMS. (M)

Part: CONNECTOR — CONTAMINATED (CABIN)

CENTER SECTION OF EMERGENCY LIGHT WON'T COME ON WITH MASTER SWITCH. CLEANED CONNECTOR MATING ON EL LAMP, TESTED EMERGENCY LIGHT SYSTEM, PER LOCTITE MAINTENANCE MANUAL. OPS TEST OK. (M)

Part: TURBINE SECTION — FAILED (ENGINE)

FLT 233, A REPOSITION FLIGHT, FROM KTVL TO KSFO, STARTUP, TAXI WERE ACCOMP W/O INCIDENT. AFTER BEING CLEARED FOR T/O, POWER WAS ADVANCED TO T/O EPR OF 2.18. APPROX 2 TO 5 SECONDS AFTER BRAKE RELEASE THE CREW OBSERVED A LOUD BANG COMING FROM THE REAR OF THE A/C. THE CREW FIRST THOUGHT IT WAS A MAIN TIRE BLOWOUT. THE CREW IMMEDIATELY RETRACED THE ENGINES TO IDLE. THE A/C WAS ONLY MOVING ABOUT 5 MPH. THE CREW OBSERVED EGT AT APPROX 650 DEGREES CENTAGRADE. ENGINE SHUT DOWN WAS ACCOMP AS PER THE 'ENGINE FIRE AND SEVERE DAMAGE OR SEPARATION' CHECKLIST. AFTER COMPLETION OF CHECKLIST THE CREW TAXIED TO THE HARDSTAND WITH EQUIP STANDING BY. NO FURTHER PROBLEMS. EXAMINATION OF ENGINE REVEILED A CONTAINED TURBIN

Part: LIGHT — INOPERABLE (CABIN)

CENTER SECTION OF EMERGENCY FLOOR TRACK LIGHTING INOPERABLE. REMOVED AND REPLACED CENTER SECTION FLOOR TRACK LIGHTING PER LUMINESCENT SYSTEM MANUAL 33-50-01 PAGE 106. (X)

Part: LIGHT — INOPERABLE (L1 DOOR)

L2 DOOR EMERGENCY LIGHT INOPERABLE (EXTERIOR). CLEANED LIGHT SOCKET. LIGHT NOW WORKS IAW 33-51-61. (X)

Part: CONNECTOR — DIRTY (CABIN)

WITH FLOOR TRACK LIGHTING ON, STANDING AT MID-CABIN, LIGHTS FLICKER. CLEANED AND SECURED CONNECTIONS. OPS CHECK GOOD. (X)

Part: BATTERY PACK — DISCHARGED (CARGO COMPT)

LEFT OVERWING EMERGENCY EXIT LIGHT INOPERABLE. REMOVED AND RPELACED AFT PIT EMERGENCY BATTEYR PACK PER BMM 33-51-31. OPS CHECK GOOD. (X)

Part: COLUMN — CRACKED (LT CONTROL)

CRACKED ON FRONTSIDE ABOUT 1 INCH LONG. CRACKS CAUSED BY HIGH TT AND TWISTING LOAD.