N153SY

Part: UNKNOWN — CORRODED (UNKNOWN) · airframe 19,946 hrs · 11,712 cycles

AFT WET AREA L/H FLOOR BEAM CORRODED APPROX. 2.5 INCHES OF FRAME 84 AT SEAT TRACK AND OUTBOARD FLANGE (C-CHECK RO 1/7/2024) PERFORMED PERMANENT DOUBLER REPAIR ON LH INBD FLOOR BEAM SEAT TRACK AT FR 84-85. REF. ETD2023-170-032099. SEE CONTINUE CARD FOR FURTHER WORK PERFORNED. WEIGHED REPAIR PARTS FOR LH INBD FLOOR BEAM SEAT TRACK FR 84-85 PERMANENT REPAIR. MEASURED 156.1 GRAMS. REF. GMM CH. 3 SEC. 12, 1.1.3. THIS REPAIR DOES NOT AFFECT WEIGHT AND BALANCE OF ACFT.

Part: UNKNOWN — GOUGED (UNKNOWN) · airframe 19,946 hrs · 11,712 cycles

LH I/B FLOOR SEAT TRACK GOUGED JUST AFT OF FR19 (C-CHECK RO 1/7/2024) PERFORMED PERMANENT DOUBLER REPAIR ON LH INBD FLOOR BEAM SEAT TRACK FR 19-20 REF. ETD2023-170-032122. SEE CONTINUATION CARD FOR FURTHER WORK PERFORMED. THIS REPAIR DOES NOT EFFECT WEIGHT AND BALANCE TO AIRCRAFT.

Part: NONE — DENTED · airframe 16,047 hrs · 9,075 cycles

TRANSFER FROM EAML 898285 : REF EAML 898120: FOUND DENT MEASURING 6.5" LONG X 3 3/8' WIDE AT ITS WIDEST POINT AND 5/16" DEEP AT FRAMES 16 AND 17 AND STRINGER 17R JUST FORWARD OF THE FWD CARGO DOOR (FLIGHT 4727 - FILED CLOSED) REPAIRED DENT IN FUSELAGE SKIN AT FRAMES 16 AND 17 AND STRINGER 17R JUST FORWARD OF THE FWD CARGO DOOR IN REF TO ETD2022-170-016275, REV B, DATED 05/05/2022. COMPLETED TASK CARD M-337 AND 51-00-00-002-SKY-U FOR MAJOR STRUCTURAL REPAIR.

Part: ISOLATOR — BROKEN (FWD SERVICE DOOR) · airframe 13,173 hrs · 7,399 cycles

FWD SERVICE DOOR INNER CUTOUT HAS 2EA BROKEN ISOLATERS ON UPPER SIDE AS MARKED. (C-CHECK) RO 2/1/2021 REMOVED AND REPLACED 2EA FWD SERVICE DOOR INNER CUTOUT ISOLATERS ON UPPER SIDE REF. SRM 51-40-08.

Part: FRAME ANGLE — DAMAGED · airframe 13,173 hrs · 7,399 cycles

3 EACH FASTENER HOLES ELONGATED DURING STUCK FASTENER REMOVAL ON FRAME 52 ANGLE. / ENLARGED 2 FASTENER HOLES FOR OVERSIZED FASTENERS AND REPAIRED 1 HOLE WITH FABRICATED BUSHINGS PER ETD2021-170-002242. REPAIR IS TEMPORARY FOR 12 MONTHS AS OF JANUARY 25, 2021. BUSHINGS ARE NEGLABLE WEIGHT AND HAVE NO EFECT ON ACFT WEIGHT.

Part: SEAL DEPRESSOR — CORRODED (FWD CARGO DOOR) · airframe 13,173 hrs · 7,399 cycles

FORWARD CARGO DOOR CUTOUT, LOWER FORWARD CORNER SEAL DEPRESSOR HAS 1 EACH NUT PLATE WITH CORRODED RIVETS. (C-CHECK) RO 2/1/2021 REMOVED AND REPLACED 1 EA NUTPLATE ON FORWARD CARGO DOOR CUTOUT LOWER FORWARD CORNER SEAL DEPRESSOR REF EMB SRM 51-45-00.

Part: BRACKET — CORRODED (AFT FAIRING) · airframe 13,173 hrs · 7,399 cycles

AFT FUSELAGE FAIRING 195NL NUTPLATE BRACKET THAT CONNECTS TO MID FUSELAGE FAIRING 192DL CORRODED. (C-CHECK) RO 2/1/2021 REMOVED AND REPLACED AFT FUSELAGE FAIRING 195NL NUTPLATE BRACKET THAT CONNECTS TO MID FUSELAGE FAIRING 192DL PER AMM 20-10-07-910-801-A

Part: FRAME ANGLE — CRACKED · airframe 13,173 hrs · 7,399 cycles

L/H FRAME 52 ANGLE BRACKET CRACKED. (C-CHECK) RO 2/1/2021 REMOVED AND REPLACED LH FR52 ANGLE SUPPORT BRACKET, REF. SRM 51-40-08.

Part: SEAL DEPRESSOR — CORRODED (FWD CARGO DOOR) · airframe 13,173 hrs · 7,399 cycles

FORWARD CARGO DOOR CUTOUT, LOWER CENTER SEAL DEPRESSOR HAS 4 EACH NUT PLATES WITH CORRODED RIVETS. (C-CHECK) RO 2/1/2021 REMOVED AND REPLACED 4 EA NUTPLATES ON FORWARD CARGO DOOR CUTOUT LOWER CENTER SEAL DEPRESSOR REF EMB SRM 51-45-00.

Part: SEAL DEPRESSOR — CORRODED (FWD CARGO DOOR) · airframe 13,173 hrs · 7,399 cycles

FORWARD CARGO DOOR CUTOUT, LOWER AFT CORNER SEAL DEPRESSOR HAS 1 EACH NUT PLATE WITH CORRODED RIVETS. (C-CHECK) RO 2/1/2021 REMOVED AND REPLACED 1 EA NUTPLATE ON FORWARD CARGO DOOR CUTOUT LOWER AFT CORNER SEAL DEPRESSOR REF EMB SRM 51-45-00.

Part: CLOSEOUT PANEL — CORRODED (FWD CARGO DOOR) · airframe 13,173 hrs · 7,399 cycles

FORWARD CARGO DOOR CLOSEOUT PANEL HAS CORROSION IN THE CHAFED AREA WHERE THE FLOOR PANEL RESTS. (C-CHECK) RO 2/1/2021 REMOVED AND REPLACED FWD CARGO THRESHOLD CLOSEOUT PLATE. REF. EMB 175 AMM 20-10-01. SEE CONTINUATION CARD FOR WORK PERFORMED.

Part: WASHER — CORRODED (LT FLAP TRACK) · airframe 13,173 hrs · 7,399 cycles

L/H WING #2, #3, AND #4 FLAP TRACK SUPPORT FWD MOUNT BOLT SPRING WASHER CORRODED (C-CHECK) RO 2/1/2021 REPLACED L/H WING #2, #3, AND #4 FLAP TRACK SUPPORT FWD MOUNT BOLT SPRING WASHER CORRODED, REF E175 AMM 57-57-31

Part: GUSSET — CORRODED (FRAME 90) · airframe 13,173 hrs · 7,399 cycles

CORROSION ON AFT WET AREA GUSSET AT FR90 RBL 11" (C-CHECK) RO 2/1/2021 REMOVED AND REPLACED AFT WET AREA GUSSET AT FR90 RBL 11" REF EMB SRM 51-40-08

Part: GUSSET — CORRODED (FRAME 90) · airframe 13,173 hrs · 7,399 cycles

CORROSION ON AFT WET AREA GUSSET AT FR90 LBL 11" (C-CHECK) RO 2/1/2021 REMOVED AND REPLACED NEW GUSSET AT FR90 LBL 11" , REF. SRM: 51-40-08

Part: SPLICE — CORRODED (FRAME 90) · airframe 13,173 hrs · 7,399 cycles

CORROSION ON AFT WET AREA SPLICE AT FR90 BL 0. (C-CHECK) RO 2/1/2021 REMOVED AND REPLACED NEW SPLICE AT FR90 BL 0 , REF. SRM: 51-40-08

Part: WASHER — CORRODED (RT FLAP TRACK) · airframe 13,173 hrs · 7,399 cycles

R/H WING #2, #3, AND #4 FLAP TRACK SUPPORT FWD MOUNT BOLT SPRING WASHERS CORRODED (C-CHECK) RO 2/1/2021 REMOVED AND REPLACED R/H WING #2, #3, AND #4 FLAP TRACK SUPPORT FWD MOUNT BOLT SPRING WASHERS REF EMB 175 AMM 57-54-21, 57-57-31.

Part: SPLICE — CORRODED (FRAME 89) · airframe 13,173 hrs · 7,399 cycles

CORROSION ON AFT WET AREA SPLICE AT FR89 RBL 11" (C-CHECK) RO 2/1/2021 REMOVED AND REPLACED NEW SPLICE AT FR89 RBL 11" , REF. SRM: 51-40-08

Part: FASTENER — SHEARED (FRM 57 BULKHEAD) · airframe 13,173 hrs · 7,399 cycles

R/H WHEEL WELL FRAME 57 PRESSURIZED BULKHEAD HAS A SHEARED FASTENER. (C-CHECK) RO 2/1/2021 REMOVED AND REPLACED FASTENER ON R/H WHEEL WELL FR 57 PRESSURIZED BULKHEAD. REF EMB SRM 51-40-08. SEE CONTINUATION FOR WORK PERFORMED.

Part: SUPPORT — CORRODED (WET AREA) · airframe 13,173 hrs · 7,399 cycles

CORROSION ON FWD WET AREA AFT R/H SILL BETWEEN FR17-19 IN 3 LOCATIONS. (C-CHECK) RO 2/1/2021 REMOVED AND REPLACED RH FLOOR SILL BETWEEN FRAMES 17-19. / REF SRM 51-40-08

Part: FLOOR SUPPORT — CORRODED (FRAME 15) · airframe 13,173 hrs · 7,399 cycles

CORROSION ON FWD WET AREA FLOOR SUPPORT AT FR15 RBL 30". (C-CHECK) RO 2/1/2021 REMOVED CORROSION ON FWD WET AREA FLOOR SUPPORT AT FR15 RBL 30" REF EMB SRM 51-10-03. MAT'L IS .080", AFTER BLENDOUT .073". MAT'L LOSS OF .007" IS OUT OF LIMITS REF EMB SRM 51-75-76. TOOL ASSET #TC2-50431 CAL DUE 11/12/21. REMOVED FWD WET AREA FLOOR SUPPORT AT FR15 RBL 30" REF. SRM 51-40-08. INSTALLED NEW PART STOCK FLOORBOARD SUPPORT AT FR15 RBL 30". LINED THE NEW HOLE FOR THE NUT SPRING WITH THE FLOORBOARD AND RESTORED PROTECTIVE COATING REF. SRM 51-40-08, SRM 51-23-05, AND SRM 51-23-06.

Part: AXLE — DAMAGED (MLG) · airframe 45,160 hrs · 16,997 cycles

ON ARRIVAL TO THE GATE THE NUMBER EIGHT WHEEL AND BRAKE WERE FOUND TO BE SMOKING. THE WHEEL IS ALSO NOT SITTING ON THE AXLE STRAIGHT. REMOVED AND REPLACED AXLE, SLEEVE AND NUT, AS WELL AS THE ASSOCIATED WHEEL AND BRAKE.

Part: DUCT — LEAKING (A/C BAY) · airframe 45,160 hrs · 16,997 cycles

DURING CLIMBOUT FROM MSP THE NUMBER THREE PNEUMATIC FAIL LIGHT ILLUMINATED. FOUND DUCT AAM7235-501 LEAKING AFT OF AFT WALL NUMBER THREE PACK BAY. PERFORMED REPAIR OF CHAFED DUCT, REPOSITIONED AND LEAK CHECKED.

Part: BRAKE — FIRE (MLG) · airframe 44,944 hrs · 16,923 cycles

AFTER LANDING AT MCO THE CREW WAS NOTIFIED THAT THE NUMBER EIGHT BRAKE WAS ON FIRE. REMOVED AND REPLACED NUMBER EIGHT BRAKE, TIRE, AND BRAKE SLEEVE. OPERATIONAL CHECKS GOOD.

Part: DOOR FRAME — GOUGED (CARGO DOOR) · airframe 43,751 hrs · 16,520 cycles

DURING A MAINTENANCE HEAVY CHECK, TWO DEEP GOUGES WERE FOUND OUT OF LIMITS IN THE AFT CARGO DOOR JAMB. CUT OUT DAMAGED AREA AND INSTALLED FILLER.

Part: STABILIZER — CRACKED (HORIZONTAL STAB) · airframe 43,751 hrs · 16,520 cycles

DURING A HEAVY MAINTENANCE CHECK, A HFEC INSPECTION OF THE RIGHT HORIZONTAL STABILIZER UPPER OUTER SECTION OF THE REAR SPAR CAP BETWEEN THE FORWARD AND AFT BARREL NUT HOLES REVEALED AN OUT OF LIMITS CRACK. REMOVED AND REPLACED THE RIGHT HORIZONTAL STABILIZER PER MM 551003.

Part: STRUT — LEAKING (LT MLG) · airframe 42,970 hrs · 16,190 cycles

AFTER TAKEOFF UPON SELECTING GEAR UP, THE LEFT MAIN GEAR UNSAFE LIGHTS ON BOTH CONSOLES ILLUMINATED. THE FLIGHT CREW PERFORMED COM PROCEDURES AND VISUALLY COMPARED BOTH MAIN GEAR / DOOR MECHANICAL POSITION INDICATORS, AND FOUND THE LEFT GEAR AND GEAR DOOR NOT FULLY UP AND LOCKED. RETURNED TO POINT OF ORIGIN (MSP). THE MAIN STRUT WAS FOUND NOT TO BE FULLY EXTENDED WITH WEIGHT OFF THE WHEELS. REMOVED AND RESEALED THE SHOCK STRUT AND UPPER CHAMBER WITH NEW PACKINGS, AND PERFORMED A GEAR SWING. GEAR SWING OPERATIONALLY CHECKS GOOD.

Part: WIRE — INOPERATIVE (CABIN)

DURING A LINE MAINTENANCE CHECK, THE AFT EMERGENCY FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE IN THE FIRST HALF OF THE AFT CABIN. FOUND SHORTED WIRE ON THE RIGHT SIDE OF THE AIRCRAFT. REPLACED THE WIRE WITH A NEW WIRE. EMERGENCY LIGHTS OPERATIONALLY CHECK GOOD.

Part: SMOKE DETECTOR — INOP (CARGO COMPT)

DURING FLIGHT, THE AFT CARGO FIRE INDICATION AND NR 2 AFT SMOKE DETECTOR WAS ON INTERMITTENTLY. FIRED NR 1 AND NR 2 BOTTLES AND COMPLIED WITH THE COM. REMOVED AND REPLACED THE NR 2 AFT CARGO SMOKE DETECTOR AND BOTH FIRE BOTTLES. OPERATIONAL TEST WAS NORMAL.

Part: TIRE — FAILED (MLG)

DURING LANDING ROLL, THE NR 8 MAIN LANDING GEAR TIRE BLEW. ROLL OUT WAS UNEVENTFUL. REMOVED AND REPLACED THE NR 8 MAIN LANDING GEAR TIRE ASSEMBLY.

Part: TIRE — FAILED (MLG)

DURING LANDING, THE NR 8 MAIN TIRE BLEW OUT. REMOVED AND REPLACED THE NR 8 AND NR 7 TIRE PER MM 324101.

Part: OVEN — FAILED (GALLEY)

THE AFT OVEN, 2ND ONE FROM THE AFT, FAN SMOKES WHEN TURNED ON. REMOVED AND REPLACED THE OVEN, OPERATIONALLY CHECKS GOOD.

Part: BATTERIES — DISCHARGED (L2 DOOR SLIDE)

DURING A LINE MAINTENANCE CHECK, THE L2 EMERGENCY SLIDE LIGHT WAS FOUND TO BE INTERMITTENT AND THE SLIDE LIGHT BATTERY CONTACTS WERE FOUND BROKEN. SECURED THE SLIDE LIGHT BATTERIES IN THE HOLDER.

Part: CONTROL CABLE — OUT OF ADJ (RT MLG WW)

DURING APPROACH, GEAR WOULD NOT EXTEND NORMALLY, GEAR HANDLE WOULD NOT MOVE FURTHER THAN HALF TRAVEL. LANDING GEAR EXTENDED USING ALTERNATE SYSTEM. LANDED AIRCRAFT UNEVENTFULLY. FOUND EXTEND CABLE ABOVE RIGHT WHEEL WELL CEILING BULKHEAD OFF OF PULLEY. REINSTALLED CABLE AND PERFORMED TENSION CHECK PER MM 323101. ALSO, REPLACED TURNBUCKLE W AND TENSIONED CABLE 109. PERFORMED GEAR RETRACT/EXTEND TEST PER MM 323000 WITH NO TROUBLE FOUND.

Part: SUPPORT — CORRODED (BS 2007)

DURING A HEAVY MAINTENANCE CHECK, OUT OF LIMITS CORROSION ON THE BULKHEAD FLOOR SUPPORT WAS NOTED AT FS 2007 AT THE AFT BULKHEAD RBL 60 AND LBL 23 AT CABIN FLOOR LEVEL. REMOVED AND REPLACED TEE FLOOR SUPPORT PER SRM 510000 VOLUME II (C) AND SRM 512101 VOLUME II PAGES 1, 2, 21, 24 AND 25 AND SRM 534000 VOLUME I.

Part: FRAME — CORRODED (CARGO DOORWAY)

DURING A HEAVY MAINTENANCE CHECK, THE AFT CARGO DOOR, AFT FRAME WAS FOUND TO BE CORRODED OUT OF LIMITS. INSTALLED A NEW FRAME, ANGLE AND DOOR SEAL RETAINER PER SRM 513501 AND 513301 VOLUME II.

Part: PIN — DAMAGED (C1 DOOR)

DURING A HEAVY MAINTENANCE CHECK, THE FORWARD CARGO DOOR HINGE PIN WAS FOUND TO EXHIBIT CORROSION AND DAMAGED THREADS. REPLACED HINGE PIN PER MM 523104.

Part: SUPPORT — CORRODED (BS 1841-2007)

DURING A HEAVY MAINTENANCE CHECK, A GALLEY FLOOR SUPPORT WAS FOUND CORRODED OUT OF LIMITS AT FS 1841 TO 2007 IN THE AFT LEFT OUTBOARD GALLEY FLOOR. REMOVED AND REPLACED THE GALLEY FLOOR SUPPORT AT FS 1841 TO 2007 PER SRM 510000 VOLUME II (C) AND SRM 512101 VOLUME II PAGE 1, 2, 21, 24 AND 25.

Part: SUPPORT — CORRODED (BS 1841-2007)

DURING A HEAVY MAINTENANCE CHECK, A GALLEY FLOOR SUPPORT WAS FOUND CORRODED OUT OF LIMITS AT FS 1841 TO 2007 IN THE AFT RIGHT OUTBOARD GALLEY FLOOR. REMOVED AND REPLACED THE GALLEY FLOOR SUPPORT AT FS 1841 TO 2007 PER SRM 510000 VOLUME II (C) AND SRM 512101 VOLUME II PAGE 1, 2, 21, 24 AND 25.

Part: SUPPORT — CORRODED (BS 1837-2007)

DURING A HEAVY MAINTENANCE CHECK, A GALLEY FLOOR SUPPORT WAS FOUND CORRODED OUT OF LIMITS AT FS 1837 TO 2007 IN THE AFT LEFT INBOARD GALLEY FLOOR. REMOVED AND REPLACED THE GALLEY FLOOR SUPPORT AT FS 1837 TO 2007 PER SRM 512000 VOLUME II (C) AND SRM 512101 VOLUME II PAGE 1, 2, 21, 24 AND 25.

Part: SUPPORT — CORRODED (BS 1841-2007)

DURING A HEAVY MAINTENANCE CHECK, A GALLEY FLOOR SUPPORT WAS FOUND CORRODED OUT OF LIMITS AT FS 1841 TO 2007 IN THE AFT RIGHT INBOARD GALLEY FLOOR. REMOVED AND REPLACED THE GALLEY FLOOR SUPPORT AT FS 1841 TO 2007 PER SRM 512000 VOLUME II (C) AND SRM 512101 VOLUME II PAGE 1, 2, 21, 24 AND 25.

Part: SUPPORT — CORRODED (BS 1841-2007)

DURING A HEAVY MAINTENANCE CHECK, A GALLEY FLOOR SUPPORT WAS FOUND CORRODED OUT OF LIMITS AT FS 1841 TO 2007 IN THE AFT LEFT INBOARD GALLEY FLOOR. REMOVED AND REPLACED THE GALLEY FLOOR SUPPORT AT FS 1841 TO 2007 PER SRM 512000 VOLUME II (C) AND SRM 512101 VOLUME II PAGE 1, 2, 21, 24 AND 25.

Part: SUPPORT — CORRODED (BS 1841-2007)

DURING A HEAVY MAINTENANCE CHECK, A GALLEY FLOOR SUPPORT WAS FOUND CORRODED OUT OF LIMITS AT FS 1841 TO 2007 IN THE AFT RIGHT INBOARD GALLEY FLOOR. REMOVED AND REPLACED THE GALLEY FLOOR SUPPORT AT FS 1841 TO 2007 PER SRM 512000 VOLUME II (C) AND SRM 512101 VOLUME II PAGE 1, 2, 21, 24 AND 25.

Part: ENGINE — FAILED (NR 3)

DURING THE TAKEOFF ROLL, A LOUD BANG WAS HEARD ACCOMPANIED BY HEAVY VIBRATION OF UNKNOWN ORIGIN. TAKEOFF WAS ABORTED AT 125 KNOTS. DURING A BORESCOPE INSPECTION OF THE NUMBER THREE ENGINE METAL WAS FOUND IN THE TAILPIPE.

Part: SPAR CAP — CRACKED (WS 415)

DURING A HEAVY MAINTENANCE CHECK, THE LEFT WING REAR SPAR CAP SPLICE WAS FOUND TO EXHIBIT A 2 INCH CRACK AT STA XORS 415.00. REMOVED AND REPLACED THE SPAR TANG AFT AT STA XORS 415.00 AT THE LEFT REAR SPAR PER SRM 513301.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING EMERGENCY LIGHT SELF TEST IN THE COCKPIT THE AFT EMERGENCY LIGHTS POWER SUPPLY FAILS. REMOVED AND REPLACED THE AFT CABIN EMERGENCY LIGHTS POWER SUPPLY AND BATTERY PACK PER MAINTENANCE MANUAL 332301, OPERATIONALLY CHECKS GOOD.

Part: PROXIMITY SENSOR — INOPERATIVE (NLG)

DURING CLIMB, THE RED NOSE GEAR LIGHT CAME ON. PERFORMED COM CHECKLIST WITH ALL GEAR DOWN INDICATIONS NORMAL. DIVERTED TO MIA. FOUND TARGET ON DOWNLOCK PROXIMITY SENSOR OUT OF ADJUSTMENT. ADJUSTED DOWN LOCK SENSORS IN ACCORDANCE WITH MAINTENANCE MANUAL 326103, FUNCTIONALLY CHECKS GOOD.

Part: N1 INDICATOR — INOPERATIVE (NR 3 ENGINE)

NR 3 ENGINE N1 INDICATOR STUCK AT 78 PERCENT WITH TAKEOFF POWER. ENGINE FAIL LIGHT ILLUMINATED AND TAKEOFF ABORTED. REMOVED AND REPLACED NR 3 N1 INDICATOR, FUNCTIONALLY CHECK GOOD.

Part: ENCODER — FAILED (CABIN)

DURING OXYGEN DROP FOR A SEAT REMOVAL, OXYGEN PANEL AT 8D DID NOT DEPLOY. REMOVED AND REPLACED UNDERSEAT ENCODER AT SEAT 8D PERFORMED OXYGEN DROP AGAIN, OPS CHECKED GOOD.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

THE MID CABIN LEFT FORWARD EMERGENCY LIGHTS WERE FOUND INOPERATIVE. REMOVED AND REPLACED POWER SUPPLY AND BATTERY PACK, LIGHTS TESTED GOOD IAW DC-10 MM 33-51-01.

Part: SMOKE DETECTOR — FAILED (LAVATORY)

THE SMOKE DETECTOR IN THE LAVATORY NEAR THE R-2 DOOR WAS FOUND TO BE INOPERATIVE. REMOVED AND REPLACED SMOKE DETECTOR, OPS CHECKED GOOD.

Part: SMOKE DETECTOR — FAILED (CARGO COMPT)

THE NUMBER 4 SMOKE DETECTOR IN THE AFT CARGO COMPARTMENT WOULD NOT TEST. REMOVED AND REPLACED NUMBER 4 SMOKE DETECTOR, NEW DETECTOR TESTED GOOD PER DC-10 MAINTENANCE MANUAL 26-10-00.

Part: BATTERIES — DISCHARGED (CABIN)

THE R-3 EMERGENCY SLIDE WOULD NOT TEST. REMOVED AND REPLACED TEST BATTERIES, SLIDE TESTED GOOD.

Part: SMOKE DETECTOR — FAILED (CARGO COMPT)

THE NUMBER 3 AFT CARGO SMOKE DETECTOR WOULD NOT TEST IN FLIGHT. RELAMPED NUMBER 3 AFT CARGO SMOKE DETECTOR, DETECTOR TESTED GOOD.

Part: SMOKE DETECTOR — FAILED (CARGO COMPT)

THE FORWARD CARGO PIT NUMBER 2 SMOKE DETECTOR DOES NOT TEST. REMOVED AND REPLACED SMOKE DETECTOR, SYSTEM TESTED GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN)

THE EMERGENCY PATH LIGHTING IN THE FORWARD CABIN WAS FOUND TO BE INOPERATIVE. REMOVED AND REPLACED THE FORWARD CABIN BATTERY PACK, PATH LIGHTING TESTED GOOD.