N474UP

Part: FLOORBEAM — CORRODED (ZONE 100) · airframe 23,216 hrs · 15,710 cycles

DURING OK TO INSTALL PANELS ON AFT CARGO BULKHEAD FOUND CORROSION LOCATED ON FLOOR BEAM, UPPER FLANGE LOWER FACE AT STA 1681.8, BETWEEN RBL12 AND RBL62. (015-14) ATA53. ACCOMPLISHED THE CATEGORY A REPAIR PER VT-SAA EA 757-5310-01-B0306 IR AND EO-92081-REQ1. R

Part: ENGINE — FLAMED OUT (RIGHT) · airframe 22,701 hrs · 15,413 cycles

DURING DESCENT INTO TPA, OUT OF FL200,RIGHT ENGINE FLAMED OUT. ACCOMPLISHED QRH & LANDED, "R ENG LP PUMP" STATUS MSG DISPLAYED. DID NOT ATTEMPT RELIGHT. OPEN

Part: GOVERNOR — UNSERVICEABLE (FUEL FLOW) · airframe 22,701 hrs · 15,413 cycles

*SUPPLEMENTAL SDR* *IFSD* DURING DESCENT INTO TPA, OUT OF FL200,RIGHT ENGINE FLAMED OUT. ACCOMPLISHED QRH & LANDED, "R ENG LP PUMP" STATUS MSG DISPLAYED. DID NOT ATTEMPT RELIGHT. C/W RII 2. CESAR MENDIETA (TECHNICIAN), 28-FEB-2024 23:47 UTC INSTALLED RT ENG LP FUEL PUMP PER AMM 73-11-01 UP TO STEP 3. I. LOW PRESSURE PUMP TEST, REQUIRES PP TESTS 1,2. INSTALLED RT ENG HP FUEL PUMP PER 73-11-03 UP TO STEP 3. I. HIGH PRESSURE PUMP TEST, REQUIRES PP TESTS 1,2. INSTALLED RT ENG FFG PER AMM 73-21-01 UP TO STEP 1 J. FFG INSTALLATION TEST. REQUIRES PP TESTS 1,2,9,,10,11 C/W PP TESTS 1,2,9,10,11, AND 13 IAW MM 71-00-00. OPS AND LK CKS GOOD.

Part: SENSOR — FAULTED (RT TAT) · airframe 21,908 hrs · 14,852 cycles

ATB, EMERGENCY DECLARED, TAT PROB EICAS AT 400 FT AGL. REMOVED AND REPLACED TAT PROBE, OPS CHECK GOOD IAW AMM 34-12-02.

Part: FRAME — NONE (BS 1560) · airframe 21,908 hrs · 14,852 cycles

INSPECTION TYPE:SEG4*MAJOR REPAIR* UPON COMPLETION OF EO B757-5310-73926-A FOUND AN EXISTING FRAME REPAIR AT R/H STA 1560 BETWEEN S-23R AND S-27R. ALTERNATE INSPECTION REQUIRED.ACCOMPLISHED REPAIR PER EO B757-5310-27080-C, UPS RCD 264242 AND VT MAE 757-5360-27-A3105 REV. UPS EO NO: B757-5310-83888-A

Part: FRAME — NOT REPORTED (BS 1320 S25-28R) · airframe 21,908 hrs · 14,852 cycles

INSPECTION TYPE: SEG4, UPON COMPLETION OF EO B757-5310-3926-A FOUND AN EXISTING FRAME REPAIR AT R/H STA 1320 BETWEEN S-25R AND S-28R. ALTERNATE INSPECTION REQUIRED. ACCOMPLISHED REPAIR PER EO B757-5310-27069-C, RCD 264241 AND 5360-27-A3106 REV.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 20,354 hrs · 13,852 cycles

INSPECTION TYPE:N/AEMERGENCY LTS FAILED TESTR/R'D EMERGENCY LT BATT PACK IAW AMM 33-51-07-902-001 . TEST NORMAL

Part: ANNUNCIATOR — FAULTED (TAT PROBE) · airframe 19,960 hrs · 13,628 cycles

INSPECTION TYPE:N/A** ATB ** NO EMERGENCY DECLARED ** LANDED UNEVENTFULLY ** SHORTLY AFTER TAKEOFF TAT PROB ANNUNCIATOR EICAS MESSAGE ILLUMINATED 15 TO 20 SECONDS LATER L EEC & R EEC EICAS MESSAGE RECEIVED.R&R CURRENT SENSING RELAY K410 FOR T/S IAW 757 SWPM 20 81 22 TAT HEAT SYSTEM PASS IAW 757 AMM 30 33 00 JK 1060117 4/28/21 / R&R TAT PROBE OPS CK PASS IAW 757 AMM 34 12 02 EFF SOURCE REF 757 IPC 34 12 02 05 005J

Part: SKIN — DELAMINATED (TE FLAP) · airframe 19,793 hrs · 13,526 cycles

INSPECTION TYPE: DEG 4 DELAMINATION AT APPROXIMATELY STA 42,5 MARKED IN RED DOT 8-002 ON UPPER SURFACE PANEL 113N3600. REPAIRED AREA OF DELAMINATION, IAW B757 SRM 51-70-07-OG, PER SRM 57-53-01-2R-1.

Part: FLOOR PANEL — DAMAGED (MCD) · airframe 19,793 hrs · 13,526 cycles

INSPECTION TYPE: SEG FLOOR PANEL 211XAF DAMAGED. FABBED PANEL 211XAF FROM 5024N400001SS-G, BATCH 3546253, PER SREO B757-5320-9692-K.

Part: FLOOR PANEL — DAMAGED (MCD) · airframe 19,793 hrs · 13,526 cycles

INSPECTION TYPE: SEG FLOOR PANEL 212XAF DAMAGED. FABBED PANEL 212XAF FROM 5024N400001SS-G, BATCH 3546253, PER SREO B757-5320-9692-K.

Part: TRANSCEIVER — MALFUNCTIONED (WEATHER RADAR) · airframe 18,949 hrs · 13,003 cycles

INSPECTION TYPE:N/ADURING DEPARTURE APX3000FT CREW DETECTED STRONG ELECTRICAL AKRID SMELL BOTH RADAR SWITCHES OFF SMELL COMPLETELY GONE LESS THAN 1 MINUTE. ABOVE 10000 FT EACH RADAR SWITCH TURNED ON THEN OFF NO SMELL CAPTS RADAR OPS NORMAL DURING FLT F/O OFFOPERATED LH &RH A/C PACKS INDIVIDUALLY NO UNUSUAL SCENTS/SMELLS NOTICED ACCOMPLISHED OPS TST OF AIR RECIRC SYST PER MM 21-25-00-50 REF FIM 21-00-01-301 NO FAULTS C/W WEATHER RADAR TEST PER MM 34-43-00-501 REMOVED AND REPLACED WEATHER RADAR RCVR/TCVR PER MM 34-43-01-401 & 34-43-01-404 ADJ TEST 34-43-

Part: SENSE LINE — LOOSE (LT ENGINE) · airframe 17,933 hrs · 12,420 cycles

INSPECTION TYPE:N/A DIVERSION - DURING CRUISE FLIGHT @ FL 390, M.79, OAT -51C) ENGINE INDICATIONS BECAME ABNORMAL FOR PHASE OF FLIGHT THE FOLLOWING INDICATION WERE OBSERVED: LEFT EPR 1.65, N1 91.0, EGT 626, N2 85, FF 4.4. RIGHT EPR 1.80, N1 74.2, EGT 523, N2 75, FF 2.5..(SEE HARD COPY FOR EXTENDED WRITE UP) BITE CHECK ON EEC SHOWED FAULT CODE 47 (P1 SIGNAL FROM EPR EXMITER) CHECK SECURITY OF P1 LINE & FOUND LINE LOOSE AT THE P1 PROBE TIGHTENED LINE PER MM 20-00 PREFORMED ENG RUN PER 71-00-00-715-223-R03 TO 1.60 EPR THROTTLE ALLINEMENT & ENG INDICATIONS NORMAL

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 17,892 hrs · 12,399 cycles

EMERGENCY LIGHT HAS FOUR INOP BULBS.RELAMPED FOUR BULBS IN EMERGENCY LIGHT PER AMM 33-51-01-2.

Part: FLOOR PANEL — DAMAGED (MAIN CARGO BAY) · airframe 17,530 hrs · 12,184 cycles

INSPECTION TYPE:SEG2, FLOOR PANEL 241XCF HAS A BROKEN CORNER. FABBED PANEL 241XCF FROM 5024N400001SS-G BATCH 3350636 PER SREO B757-5320-9692-K.

Part: FLOOR PANEL — DAMAGED (MAIN CARGO) · airframe 17,530 hrs · 12,184 cycles

INSPECTION TYPE:SEG2 MAIN CARGO FLOOR PANEL 241XFF NEEDS COMPOSITE REPAIR ON CENTER FASTENER. DOT# 6707-2FABBED PANEL 241XFF FROM 5024N400001SS-G BATCH# 3350658 PER B757-5320-9692-K.

Part: FLOOR PANEL — DAMAGED (MAIN CARGO) · airframe 17,530 hrs · 12,184 cycles

INSPECTION TYPE:SEG2 MAIN CARGO FLOOR PANEL 242XJF NEEDS COMPOSITE REPAIR ON CENTER FASTENER. DOT#6707-1FABBED PANEL242XJF FROM 5024N400001SS-G BATCH# 3350658 PER B757-5320-9692-K.

Part: RELAY — MALFUNCTIONED (ENGINE PROBE) · airframe 17,114 hrs · 11,957 cycles

RIGHT ENGINE PROBE HEAT STATUS MESSAGE DISPLAYED DURING CLIMB THROUGH AN ALTITUDE OF 8000 FEET. ALL OTHER ENGINE INDICATIONS NORMAL. DIVERTED. REPLACED THE RELAYS K10479, K213, K10341, AND K178 IAW FIM 30-34-00-815-802, AND WDM 30-24-22. TESTED SATISFACTORY.

Part: OIL SYSTEM — OVERSERVICED (RT ENGINE) · airframe 17,048 hrs · 11,902 cycles

CREW DELARED EMERGENCY LANDING DUE TO FUMES IN THE COKPIT, EXITED A/C THROUGH WINDOW BY MEANS OF ESCAPE ROPES. COMPLIED WITH AMM 05-51-56-202-001, AND FIM 21-00-01-301 REF 1. FOUND THE RIGHT ENGINE OIL OVERSERVICED. DRAINED, AND SERVICED THE ENGINE IAW AMM 12-13-01-0301. OPERATED BOTH ENGINES TO MAX TAKE-OFF POWER IAW AMM 71-00-00-715-223-R03, TEST 13. CONFIRMED NO FUMES OR SMOKE IAW AMM 21-00-01-0301

Part: STRAP — DAMAGED (SMOKE GOGGLES) · airframe 15,562 hrs · 10,954 cycles

SMOKE GOGGLES STRAP IN THE SUPERNUMERARY SEAT IS DAMAGED. REMOVED & REPLACED SMOKE GOGGLES STRAP @ SUPERNUMERARY SEAT AS PER STANDARDED PRACTICES OKAY FOR SVS

Part: LIGHT — UNKNOWN (COCKPIT) · airframe 14,944 hrs · 10,466 cycles

EMERGENCY LIGHTS UNARMED INDICATION, LIGHT, ILLUMINATED IN FLIGHT WITH SWITCH IN ARMED POSITION. POSSIBLE SPRING TENSION PROBLEM. EMERGENCY LIGHTS FUNCTIONS NORMALLY. CHECKED EMERGENCY LIGHTS IAW 33-54-00. WORKS NORMAL COULD NOT DUPLICATE. OK TO CONTINUE SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 14,787 hrs · 10,325 cycles

EMERGENCY LIGHTS FOUND TO BE INOPERATIVE. R & R THE EMERGENCY BATTERY PACK IAW MM 33-51-07-902-001 PN, PN/OFF 2013-1A, SN ON 36483, SN OFF 35465. SYSTEM OPS CHECKED NORMAL, OK FOR SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 14,431 hrs · 10,060 cycles

INSPECTION TYPE:IN, EMERGENCY LIGHTS WILL NOT STAY ON IN THE ON POSITION. CHANGED BATTERY PACK IAW MM 33-51-07. OPS CK GOOD.

Part: SKIN — DENTED (BS 263-280) · airframe 14,211 hrs · 9,900 cycles

INSPECTION TYPE:C, FUSELAGE SKIN DENTED BETWEEN FS 263 AND FS 280 BELOW S-20L, LT SIDE FWD OF CREW DOOR, D536379, TRANSFERER FROM LOGPAGE 441143, ITEM 3 REPAIRED IAW REO G18801, REV C AND EO B757-5330-57152-A.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 14,211 hrs · 9,900 cycles

INSPECTION TYPE:C-8, MAIN CABIN FLOOR PANEL 241XGF HAS DAMAGE TO CORE. RECREATED FROM 2015040687754, FABRICATED NEW FLOOR PANEL IAW SREO B757-5320-9692-H.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 14,211 hrs · 9,900 cycles

INSPECTION TYPE:C-8, MAIN CABIN FLOR PANEL 241XEF HAS DAMAGE TO CORE. FABRICATED NEW FLOOR PANEL IAW SREO B757-9692-H.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 14,211 hrs · 9,900 cycles

INSPECTION TYPE:C8 MAIN CABIN FLOOR PANEL 222XCF IS DELAMINATED ON THE TOP OF THE PANEL. FABRICATED NEW FLOOR PANEL IAW SREO B757-5320-9692-H.

Part: FRAME — DENTED (BS 1280) · airframe 14,211 hrs · 9,900 cycles

INSPECTION TYPE: C8, AFT PIT LT SIDE FRAME AT STA 1280, STR 25L DENTED. REPAIRED IAW SRM 53-00-07-2R PROCEDURE 6, REPAIR 6, DETAIL 1.

Part: FRAME — DENTED (BS 1500) · airframe 14,211 hrs · 9,900 cycles

INSPECTION TYPE:C8, AFT PIT RT SIDE FRAM AT STA 1500, STR 26R DENTED. REPAIRED IAW SRM 53-00-07-2R, PROCEUDRES, REPAIR 5, DETAIL I.

Part: FRAME — DENTED (BS 1260) · airframe 14,211 hrs · 9,900 cycles

INSPECTION TYPE:C8, AFT PIT LT SIDE HAS SIDE DENT IN FRAM STA 1260, STR 26L, REPAIRED IAW SRM 53-00-07-2R PROCEDURE 6, DETAIL VI.

Part: FRAME — DENTED (BS 1340) · airframe 14,211 hrs · 9,900 cycles

INSPECTION TYPE:C8, AFT PIT LT SIDE FRAME AT STA 1340, ATR 25L HAS DENT. REPAIRED IAW SRM 53-00-07-2R PROCEDURE 5, REPAIR 5, DETAIL III.

Part: FLOOR PANEL — CRACKED (CABIN) · airframe 14,211 hrs · 9,900 cycles

INSPECTION TYPE:C-8, MAIN FLOOR PANEL 241XFF IS CRACKED. FABRICATED MAIN CABIN FLOOR PANEL 241XFF IAW SREO B757-5320-96-92-H.

Part: FLOOR PANEL — CRACKED (CABIN) · airframe 14,211 hrs · 9,900 cycles

INSPECTION TYPE:C-8, MAIN CABIN FLOOR PANEL 231XGF IS CRACKED. FABRICATED FLOOR PANEL IAW SREO B757-5320-96-92-H.

Part: FLOOR PANEL — CRACKED (CABIN) · airframe 14,211 hrs · 9,900 cycles

INSPECTION TYPE:C-8, MAIN CABIN FLOOR PANEL 241XHF IS CRACKED. FABRICATED MAIN CABIN FLOOR PANEL IAW SREO B757-5320-9692-H.

Part: STRUCTURE — DAMAGED (BS 480) · airframe 14,211 hrs · 9,900 cycles

MAIN CABIN INNER CHORD BS 480-BS 487 HAS 4 EA DAMAGED HOLES. REPAIRED HOLES IAW REO G18847 AND UPS EO B757-5340-57167-A.

Part: FLOOR PANEL — CRACKED (BS 110) · airframe 14,211 hrs · 9,900 cycles

INSPECTION TYPE:C8, MAIN CABIN FLOOR PANEL 241XJF IS CRACKED. FABRICATED NEW FLOOR PANEL IAW SREO B757-5320-9692-H.

Part: FLOOR PANEL — DELAMINATED (BS 560) · airframe 14,211 hrs · 9,900 cycles

INSPECTION TYPE:C8, MAIN CABIN FLOOR PANEL 231 XJF IS DELAMINATED. FABRICATED NEW FLOOR PANEL IAW SREO B757-5320-9692-H.

Part: FLOORBOARD — DAMAGED (CABIN) · airframe 14,211 hrs · 9,900 cycles

INSPECTION TYPE:C-8, MAIN CABIN FLOORBOARD 221XLF IS DENTED AND CRUSHED. FABRICATED FLOORBOARD IAW IAW SREO.

Part: FLOOR PANEL — DAMAGED (BS 620) · airframe 14,211 hrs · 9,900 cycles

INSPECTION TYPE:C8, MAIN CABIN FLOOR PANEL 231XHF IS CRACKED. FABRICATED NEW FLOOR PANEL 231XHF IAW SREO B757-5320-9692-H.

Part: FLOOR PANEL — DELAMINATED (BS 480) · airframe 14,211 hrs · 9,900 cycles

INSPECTION TYPE:C8, MAIN CABIN FLOOR PANEL 231XFF IS DELAMINATED. FABRICATED NEW FLOOR PANEL IAW SREO B757-5320-9692-H.

Part: FLOOR PANEL — CRACKED (BS 1420) · airframe 14,211 hrs · 9,900 cycles

INSPECTION TYPE:C8, MAIN CABIN FLOOR PANEL 252XLF IS CRACKED AND BROKEN. FABRICATED NEW FLOOR PANEL IAW SREO B757-5320-9692-H.

Part: FLOOR PANEL — DAMAGED (BS 879) · airframe 14,211 hrs · 9,900 cycles

INSPECTION TYPE:C8, MAIN CABIN FLOOR PANEL 231XTF DAMAGED AT CORNER. CORE FABRICATED FLOOR PANEL 231XTF IAW UPS SREO B757-5320-9692-H.

Part: SEAT TRACK — CORRODED (BS 1543) · airframe 14,211 hrs · 9,900 cycles

INSPECTION TYPE:C-8, MAIN DECK INTERNAL, SEAT TRACK FLANGE CORROSION. REPLACED SEAT TRACK IAW DWG 146N5540.

Part: DOOR SILL — DENTED (CARGO BAY) · airframe 14,211 hrs · 9,900 cycles

INSPECTION TYPE:C-8, MAIN CARGO DOOR SILL AT NR 2 RECESS CUP AREA SILL IS DENTED. REPAIRED ARE IAW REO G188821, REV A AND EO B757-5310-57165-A.

Part: SKIN — DENTED (HORIZONTAL STAB) · airframe 14,211 hrs · 9,900 cycles

INSPECTION TYPE: C-8, LT HORIZONTAL STABILIZER UPPER SURFACE DENT AT 16" FROM STAB ROOT & 16" FROM STABILIZER FRONT SPAR AS MARKED REPAIRED STAB PANEL WITH METAL HOT BOND DOUBLER IAW SRM 51-70-10, REPAIR 2 & REPAIR 2R GENERAL 755-10-01.

Part: SKIN — DENTED (HORIZONTAL STAB) · airframe 14,211 hrs · 9,900 cycles

INSPECTION TYPE:C-8, RT HORIZONTAL STABILIZER UPPER SURFACE DENT AT 152" FROM STABILIZER ROOT AND 9" FROM STABILIZER FRONT SPAR AS MARKED. REPAIRED STAB. PANEL WITH METAL HOTBOND REPAIR IAW SRM 51-70-10, REPAIR 4 & 51-70-10-2R GENERAL.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

EMERGENCY LIGHTS INOPERTIVE. R & R BATTERY PACK. OPS CHECKED GOOD. ALL WORK DONE IAW AMM 33-51-07.

Part: ADF — INOPERATIVE (LEFT)

LEFT ADF POINTER DOES NOT POINT PROPERLY ON BOTH RDMI'S. AUDIO IS NORMAL. WINDS WERE OUT OF LIMITS FOR ANY OTHER RUNWAY. HIT BINGO FUEL RETURNED BACK TO DEPARTURE. REPLACED LEFT ADF RECEIVER IAW MM 34-57-01.

Part: SKIN — DENTED (BS 263-280)

SKIN DENTED BETWEEN BS 263 - 280 BELOW S20L. REPAIRED IAW EO B757-5330-55316-B.

Part: LIFE VEST — TORN

RIGHT SUPER NUMERARY LIFE VEST OUTER JACKET IS TORN. R & R LIFE VEST IAW MM 25-64-00-201.

Part: LIFE VEST — TORN

LEFT SUPER NUMERARY LIFE VEST OUTER JACKET IS TORN. R & R LIFE VEST IAW MM 25-64-00-201.

Part: WARNING MESSAGE — FALSE INDICATION (ELEVATORS)

ELEVATOR ASYM STATUS MESSAGE. FOUND NO ELEVATOR ASYM STATUS OR MX MESSAGES. OPS CHECKED ELEVATOR POSITION SYS IAW AMM 27-38-00-715-002. NO FAULTS FOUND.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHT)

EXTERIOR EMERGENCY LIGHT IS INOPERATIVE. REPLACED EMERGENCY BATTERY CHARGER IAW AMM 33-51-11-01, ITEM 21.

Part: RECEPTACLE — DIRTY (EMERGENCY LIGHT)

EXTERIOR EMERGENCY LIGHT INOPERATIVE. CLEANED LIGHT ASSY RECEPTACLE, INSTALLED BULB. OPS CHECKED GOOD IAW MM 33-50-00.

Part: SKIN — DENTED (LT WING TE FLAP)

LT WING OTBD T/E AFT FLAP DENTED. REPAIRED IAW EO B757-5750-49452-A.

Part: SKIN — DENTED (LT WING TE FLAP)

LEFT WING OTBD T/E AFT FLAP DENTED. REPAIRED IAW EO B757-5750-49452-A.

Part: WEDGE — DAMAGED (LT WING TE FLAP)

LT WING OTBD FLAP T/E WEDGE DAMAGED. REPAIR IAW EO B757-5750-48837-A.

Part: WEDGE — DAMAGED (LT WING SLAT)

LT WING NR 5 SLAT T/E WEDGE DAMAGED. REPAIRED IAW EO B757-5750-47957-B.

Part: SKIN — DENTED (LT ELEVATOR)

LT ELEV UPPER SKIN DENTED/PUNCTURED IN 2 PLACES. REPAIRED IAW EO B757-5520-48836-A, REF NR 509278 AND 509279.

Part: SKIN — GOUGED (CARGO DOOR)

MAIN CARGO DOOR SKIN GOUGED AND DENTED. REPAIRED IAW EO B757-5230-48631-A.

Part: SKIN — DAMAGED (RT ELEVATOR)

RT ELEVATOR HAS 3 HAIL DAMAGE HOLES IN UPPER SKIN. 1 IS WITHIN THE CRITICAL AREA. HOLE IS 67.000 FROM INBD EDGE AND 29.500 FROM T/E. REPAIRED IAW SRM 55-20-01-1A, FIG 101.

Part: SKIN — DENTED (RT ELEVATOR)

RT ELEVATOR HAS 1 DENT THAT IS WITHIN THE CRITICAL AREA. DENT IS 110.000 FROM INBD EDGE AND 19.250 FROM THE T/E. CLASSIFIED AS MAJOR REPAIR. REPAIRED IAW EO B757-5520-47896A. THIS CLEARS D478494.

Part: SKIN — DENTED (LT WING TE FLAP)

LARGE DENT FOUND ON PANEL ON INBD FLAP UPPER SURFACE, SURFACE ABOVE INBD CANOE. REMOVED DAMAGED AND REPAIRED IAW EO B757-5750-47546-B.

Part: JAM-NUT — LOOSE (SLIDING WINDOW)

CAPT SLIDING WINDOW LOCK BINDING AFTER PRESSURIZED FLIGHT. FOUND LINK ARM JAM NUT LOOSE. CHECKED LINK ARM DIMENSIONS IAW AMM 56-11-02-5. WINDOW OPS CK NORMAL.

Part: SLIDING WINDOW — BINDING (COCKPIT)

CAPTS SLIDING WINDOW LOCK BINDING, FORCING LOCK TO OPEN AND SLIDING WINDOW OPEN, CAUSES TO LOCK TEMPORARILY. AFTER FLIGHT AND PRESSURIZING THE ACFT WINDOW LOCK IS BINDING AGAIN. CLEANED AND LUBED CAPTS WINDOW SLIDE TRACK. OPS CHECKS OK IAW AMM 56-11-00.

Part: FLOOR SUPPORT — CORRODED (BS 1020 BL0) · airframe 11,791 hrs · 8,187 cycles

INSPECTION TYPE:C1, FLOOR SUPPORT CORRODED STA 1020, BL 0. REPLACED FLOOR SUPPORT IAW SRM 51-40-02, REO-G13756 IR, AND EO B757-5310-43101-A.

Part: SKIN — PUNCTURED (RT WING TE FLAP) · airframe 11,791 hrs · 8,187 cycles

INSPECTION TYPE:C1, RT WING INBD FLAP OTBD LOWER SURFACE PUNCTURED AND HAS AREA OF BARE METAL. REPAIRED IAW SRM 51-70-10, FIG 203, REPAIR 2. CLASSIFIED AS A MAJOR REPAIR.

Part: FIRE WARNING — FALSE ACTIVATION (RT NACELLE)

EICAS STATUS MSG: R ENG FIRE LP 1 DISPLAYED. ACCOMPLISHED VISUAL INSP OF FIRE DETECTION LOOPS. NO DEFECTS NOTED. ACCOMPLISHED FIM 26-11-00, FIG 103, SYS BITE CHECKS NORMAL. RESEATED & CLEANED AFLOTS CARD NR 2 IAW AMM 26-10-01-4. OPS CHECKS GOOD IAW BITE TEST FIM 26-11-00, FIG 103.

Part: WINDOW — OUT OF ADJUST (L2 WINDOW)

INSPECTION TYPE:N/A UNABLE TO OPEN CAPTAIN'S EMERGENCY ESCAPE WINDOW. D418898. C/W ADJUSTMENT TEST IAW MM 56-11-02-5. W/E PRY TEST & DETERMINED WINDOW NEEDED ADJUSTMENT FWD IAW PARA F STEP NR 2. HANDLE NOW TAKES 1 LB PRESS TO MOVE. OPS CHECK GOOD. THIS CLEARS D418898. STICKER REMOVED.

Part: WINDOW — STUCK (COCKPIT)

CAPT SLIDING WINDOW DIFFICULT TO OPEN AND CLOSE. FOUND CAPT NR 2 WINDOW OUT OF RIG. REMOVED TRIM PANELS TO ACCESS MECHANISM FOR ADJUSTMENT PER MM 56-11-04-1. ADJUSTED PER MM 56-11-02-5.

Part: ATTACH BRACKET — CRACKED (CARGO BAY) · airframe 10,097 hrs · 7,018 cycles

INSPECTION TYPE:C1 FWD CARGO BAY E5 PANEL DOOR LWR DOOR SUPPORT UPPER ATTACH BRACKET IS CRACKED. REMOVED, FABRICATED AND INSTALLED REPLACEMENT BRACKET PER SRM 51-40-02.

Part: CHANNEL — CRACKED (ZONE 200) · airframe 10,097 hrs · 7,018 cycles

INSPECTION TYPE:C1 WHILE WORKING CUSTOMER CARD ID NR 804162, FOUND RT MLG WHEEL WELL FWD SEAL RETAINER CHANNEL CRACKED AT OTBD LEG. REMOVED CRACKED CHANNEL, BACKDRILLED HOLES, COUNTERSUNK INSTALLED CHANNEL PER SRM 51-40-02-0G.

Part: ANGLE — CHAFED (ZONE 400) · airframe 10,097 hrs · 7,018 cycles

INSPECTION TYPE:C1 CHAFED AREA OF ATTACH ANGLE FOR NR 2 PYLON ACCESS PANEL NR 442AL LT SIDE 44.5 INCHES AFT OF FWD END. REPAIRED PER SRM 51-70-11-0G.

Part: SKIN — DENTED (NR 5 SLAT) · airframe 10,097 hrs · 7,018 cycles

INSPECTION TYPE:C1 NR 5 SLAT HAS A DISBONDED DENT ON THE T/E WEDGE UPPER SURFACE 57 INCH INBD OF OTBD END. REPAIRED DENT/DISBOND IAW SRM 51-70-10-2R3.

Part: BRACKET — CRACKED (ZONE 100) · airframe 10,097 hrs · 7,018 cycles

INSPECTION TYPE:C1 RT MLG W/W SEAL RETAINER ATTACH ANGLE CRACKED ADJACENT TO MLG BODY DOOR UPSWITCH STA 1065 RBL59 WL133. REMOVED AND REPLACED BRACKET IAW SRM 51-40-02-0G.

Part: WINDOW — OUT OF ADJUST (COCKPIT)

INSPECTION TYPE:N/A CAPTAIN'S SIDE WINDOW HARD TO OPEN. ADJUSTED L2 WINDOW W/REF TO AMM 56-11-02-5. WINDOW HANDLE OPERATES NORMALLY.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT)

INSPECTION TYPE:N/A EMERGENCY EGRESS LIGHT ON FUSELAGE INOP. RELAMPED EMERGENCY EGRESS LIGHT, OPS CHECKED GOOD.

Part: BRACKET — DAMAGED (R2 WINDOW)

INSPECTION TYPE:N/A F/O R2 WINDOW DIFFICULT TO UNLATCH, HAD TO DEPRESS BUTTON TO UNLATCH. REWORKED THE FORWARD LATCH STRIKER BRACKET IAW EO B757-5610-5738 PAR 2, OPS CHECK GOOD.

Part: MODULE — FAULTY (RT MLG WARNING)

INSPECTION TYPE:N/A ATB - RIGHT MLG INDICATING DOWN AND LOCKED WITH GEAR HANDLE IN NEUTRAL POSITION. *SUPPLEMENTAL SDR* T/S PER FIM 32-61-00 FIG 103. ALSO HAD MX MSG RT GEAR DOWN, T/S TO BLOCK 21. REMOVED AND REPLACED PSEU IAW MM 32-09-04-4. TESTS GOOD IAW SAME MM. REMOVED RT GEAR LIGHT MODULE PER MM 33-16-02-2 AFTER RE-TERMINATING PINS 2 & 3. CHECKED GOOD ON GEAR SWINGS. REMOVED AND REPLACED RELAY K10370 PER WDM 32-61-00-5. PERFORMED GEAR SWING/ALT EXT IAW MM 32-35-00-5. ALL CHECK GOOD.

Part: SKIN — DAMAGED (BS 440-660) · airframe 7,167 hrs · 5,088 cycles

INSPECTION TYPE:DROP REMOVE DAMAGED SKIN AND INSTALL NEW SKIN STA 440- STA 660 26R - 26L. REMOVED DAMAGED SKIN FROM STA 440 - 660 26R- 26L. LOCATED AND DRILLED NEW SKIN. INSTALLED NEW SKIN PER SRM 51-40-02 AND DWG 143N3400.

Part: STRINGER — DENTED (BS 540) · airframe 7,167 hrs · 5,088 cycles

INSPECTION TYPE:DROP FUSELAGE STRINGER 27R AT STA 540 IS DENTED. REMOVED DAMAGED STRINGER SECTION. INSTALLED NEW STRINGER SECTION PER SRM 51-40-02 AND SRM 53-00-03-2R.

Part: SKIN — DAMAGED (BS 460-470)

INSPECTION TYPE: N/A SKIN DAMAGE UNDER FUSELAGE, ANTENNA DAMAGE, POSSIBLE STRINGER (FRAME) DAMAGE. RS NR06-0523. DAMAGE AT BS 460-470 S26R TO CENTER OF FUSELAGE. REMOVED DAMAGED SKIN FROM STA 440-660 26R-26L. LOCATED AND DRILLED NEW SKIN, INSTALLED NEW SKIN IAW SRM 51-40-02 AND DWG 143N3400. D329362 CLOSED.

Part: SMOKE DETECTOR — CONTAMINATED (CARGO BAY)

FWD CARGO BAY SMOKE DETECTOR 10459 FAILED (TC 26-016-05). REMOVED COVER ON SMOKE DETECTOR. FOUND LARGE CONCENTRATION OF BUGS INSIDE SMOKE DETECTOR. CLEANED SENSE TUBES IN FWD PIT AND INSTALLED NEW SMOKE DETECTOR. OPS CHECK GOOD. ALL WORK IAW MM 26-16-01-2.

Part: FIRE LOOP — INOPERATIVE (NR 1 ENGINE)

INSPECTION TYPE:N/A R/H ENGINE #1 F/LOOP NO TEST. #2 ON DEFERRAL ***SUPPLEMENTAL MRR*** REMOVED AND REPLACED #1 FIRE LOOP PER MM 26-11-00