N456UP
Registered owner: UNITED PARCEL SERVICE CO, KY (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
AIR TURN BACK, GEAR DISAGREE EICAS MSG AND GEAR LIGHT PRESENT AFTER T/O. ATB AS DIRECTED BY FLIGHT CONTROL. GEAR OPERATED NORMALLY DURING EXTENSION. FOUND FAULT S10065 AND S10078 ON PSEU. C/W OPS OF PSEU IAW AMM 32-61-03. OPS CHECK GOOD. LUBRICATED NLG LOCK ACTUATOR AND LOCK MECHANISM IAW AMM 12-21-12. RETRACTED AND EXTEND NLG IAW 32-34-00. NO FAULTS NOTED AT THIS TIME.
WORKING FAULT T3F18E007KJYV LINE 920 STA 879 FLOOR BEAM FOUND CORROSION ON LWR. FWD STRAP ATA-53-05 INSP VERIFIED STEP 16 OUT OF SEQUENCE INSTALLED REPLACEMENT RADIUS FILLER P/N 143N5553-1 PER BOEING DWG. 143N5255 REQUIREMENT AND B757-200PF SRM 51-40-02-0G -0.
WORKING FAULT T3F18E007KJYV LINE 920 STA 879 FLOOR BEAM FOUND CORROSION ON LWR. FWD STRAP ATA-53-05.FABRICATED STRAP P/N 143N5553-1SAAU FOR LWR FWD FLOOR BEAM, IAW DWG 143N5553. WORK ACCOMPLISHED ON TRAVELER #7003269899
FOUND DURING DVI NR 1 PYLON OTBD SIDE HAS A CRACKED PANEL LANDING UNDER PANEL P/N 311N5049-139. INSTALL REPAIR DOUBLER, FILLERS 2 EACH /ALL REPAIR PARTS AT # 1 PYLON O/B SIDE IAW EA # 757-5450-01-B0589 STEP 17. ACCOMPLISH REPAIR PER VT-SAA EA 757-5450-01-B0589 REV. I/R., PRIOR TO FURTHER FLIGHT.
MAIN DECK CARGO COMPARTMENT BELOW ACCESS PANNEL FLOOR 231XSF HAS CORROSION. ACCOMPLISHED REPAIR PER EO-95804-REQ1 AND VT-SAA EA 757-5310-01-B0586, REV. IR, PRIOR TO FURTHER FLIGHT.
MAIN DECK CABIN FLOORBEAM LOWER CHORD HAS CORROSION ONTO SEVERAL AREAS AT APPROX BS 1360, BL 0 THRU LBL 45.50, ACCOMPLISH REPAIR PER EO-95790-REQ1 AND VT-SAA EA 757-5310-01-B0588, REV. IR, PRIOR TO FURTHER FLIGHT.
MAIN DECK CABIN FLOOR SEAT TRACK HAS 2 EA AREAS WITH CORROSION AT APPROX FROM BS 1660 TO BS 1681, RBL 45.50, ACCOMPLISH REPAIR IN ACCORDANCE WITH EO-95706-REQ1 AND VT-SAA EA 757-5300-01-B0624 REV IR PRIOR TO FURTHER FLIGHT.
MAIN DECK CABIN FLOORBEAM UPPER CHORD HAS CORROSION AT APPROX BS 1600, LBL 45.50 THRU LBL 62.22, ACCOMPLISHED REPAIR PER VT-SAA EA 757-5300-01-B0603, REV IR.
MAIN DECK CABIN FLOOR SEAT TRACK HAS 2 EA AREAS WITH CORROSION AT APPROX FROM BS 1660 TO BS 1681, RBL 45.50.
STR, MAIN DECK CABIN FLOOR STRUCTURE STRAP HAS CORROSION AT APPROX FROM BS 1660 TO BS 1681, RBL 61, ID STICKER NUM. (061-002). ATA 53-05. INSTALLED NEW RETAINER P/N 146N5064-2SAAU AND NEW FILLER ON MAIN DECK CABIN FLOOR AT APPROX FROM BS 1660 TO BS 1681, RBL 61 IAW B757-200PF SRM 51-40-02-0G-0. REVIEWED
MAIN DECK CARGO COMPARTMENT STA 620 RBL-45.5 TO RBL-54.9 BELOW ACCESS PANNEL FLOOR 232XPF HAS CORROSION ON FLOORBEAM LOWER AREA, INSTALLED REPAIR PARTS AND TWO ANGLES ON FLOORBEAM UPPER CHORD APPROX. STA 620 BETWEEN RBL 45.5 AND RBL 62 IAW SRM 53-00-51-2R-6 REPAIR 6. REPAIR PER BOEING SRM 53-00-51-2R-6 REPAIR 6 FIGURE 201 REV 121.
MAIN DECK CARGO COMPARTMENT BELOW FLOOR ACCESS PANEL 222XAF HAS CORROSION. REMOVED AND REPLACED FITTING P/N 141N5131-35 PER BOEING DRAWINGS 141N5131 AND 141N5250 AND B757-200PF SRM B757-200PF-SRM-51-40-02-0G-0.
RT ELEV TIP HAS CORROSION ON UPPER AND LOWER STRAPS, FLL-003, INSTALL CONDUCTIVE FRAME AT R/H ELEVATOR TIP UPPER SURFACE REF. B-757-200 SRM 51-40-02-OG-0. INSTALLED CONDUCTIVE FRAME, 2EA. STRAPS 1EA. SHIMS, 1EA. FITTING, AT R/H ELEVATOR TIP UPPER SURFACE REF. B-757-200 SRM 51-40-02-OG-0, DWG 183N2007, TOP COATED AREA IAW 757 SRM 51-20-01-OG-0.
RT APU DOOR SUPPORT LONGERON HAS MULTIPLE AREAS OF CORROSION. ACCOMPLISHED REPAIR PER EA 757-5330-01-B0582, REV IR.
SECTION 48 CORRODED FUSELAGE SKIN BET. STA.1885.20 TO 1918.90 LH SIDE JUST ABOVE THE APU LH DOOR FWD HINGE AS MARKED (059-07). ACCOMPLISHED REPAIR IN ACCORDANCE WITH EO-95725-REQ1 AND VT-SAA EA 757-5330-01-B0581 REV IR. REVIEWED
ATB GEAR DOORS EICAS MESSAGE. CYCLED FROM OFF TO UP PER QRH.MESSAGE CLEARED. UPON TROUBLESHOOTING FOUND LFT MAIN GEAR DOOR PROXIMITY SWITCH S10242 DAMAGED. R & RÃâ¬â¢D S10242 IAW MM 32-61-02-201, SYS OPS CKÃâ¬â¢S NORMAL.
*** SDR FILED OPEN *** R WINDOW HEAT EICAS MSG. NO HEAT ON #3 RT SIDE WINDOW DEFERRED RT #3 SIDE WINDOW HEAT IAW MEL 30-41-1-3. C/W DMP.
R WINDOW HEAT EICAS MSG. NO HEAT ON #3 RT SIDE WINDOW R/R #3 RT SIDE WINDOW IAW AMM 56-11-10-424-015. WINDOW HEAT OPS CHECK AND LEAK CHECK CW. NO FAULTS NOTED. THIS CLEARS THIS DEFERRAL. DMP REVERSED, PLAC REMOVED.
FAULT: R/H WTB T-CHORDS STA 1240 FOUND EXFOLIATED CORROSION, BETWEEN RBL 57.50 TO RBL 63. INSTALLED NEW T-CHORD AND 4 E/A PLATES I.A.W SRM 51-40-02-0G.- REVIEWED
FAULT: R/H WTB T-CHORD STA 1220, FOUND EXFOLIATED CORROSION. INSTALLED NEW PART P/N UP536071D1-1 IAW B757 SRM 51-40-02-0G. REVIEWED
FAULT: R/H WTB T-CHORD, RBL 63, FOUND EXFOLIATED CORROSION. INSTALLED T-CHORD AT RBL 63 BETWEEN FS 1180 TO FS 1240 IAW SRM 51-40-02-0G. REF, STEP 14 WORK VERIFIED. INSTALLED T-CHORD AT RBL 63 BETWEEN FS 1180 TO FS 1240 .INSPECTED.
*MAJOR REPAIR* FAULT: #1 ENGINE PYLON O/B AFT. SKIN HAS CORROSION AT INNER SKIN APP. STA 154. NO DOT. VERIFIED COMPLIED WITH FINAL EA 757-5450-27-A3447 REV -. AND UPS EO 88763-REQ1
FAULT: WTB STRUCTURE - FRAME WTB STRUCTURE STA. 1240 BETWEEN RBL 57 AND RBL 63 IS EXFOLIATED. INSTALLED CHANNEL STA.1240 RBL 63 I.A.W. SRM 51-40-02-0G STEP. 4,7,8 AND SRM 51-70-11-0G-0. REVIEWED
FAULT: WTB STRUCTURE - FRAME WTB STRUCTURE BETWEEN STA. 1180 AND 1240. RBL 63 IS EXFOLIATED. INSTALLED WEB STA.1180 TO 1240 RH, 6 EA STIFFENERS BETWEEN STA.1187 TO 1235, ANGLES 1180 RBL 63 AND STA 1200 RBL 63 AND FRAME STA 1220 RBL 63 I.A.W SRM 51-40-02-0G.- VERIFIED WEB STA.1180 TO 1240 RH, 6 EA STIFFENERS BETWEEN STA.1187 TO 1235, ANGLES 1180 RBL 63 AND STA 1200 RBL 63 AND FRAME STA 1220 RBL 63 I.A.W SRM 51-40-02-0G.-INSTALLED. REVIEWED
*SUPPLEMENTAL SDR* FAULT: R/H WTB T-CHORD, RBL 67, FOUND EXFOLIATED CORROSION, BET STA 1037 TO 1060. INSTALLED T- CHORD RBL 67 STA 1037 TO 1060 IAW SRM 51-40-02-OG. REVIEWED
FAULT-FUS BELLY FAIRING AFT W/W CUTOUT SUPPORT FITTING WITH CORROSION SEVERAL PLACES. INSTALLED T-CHORD AT LBL 5750 BETWEEN STA 1180 TO 1240 IAW SRM 51-40-02-0G. WORK VERIFIED, NUTPLATES INSTALLED NUTPLATES P/N; BACN11P3A5C, BATCH #0004204060. RIVETS P/N: MS20426AD3-9, BATCH #0004191556. JOB COMPLETED.-
FAULT: WTB STRUCTURE - T-CHORD STA 1060 IS CORRODED BETWEEN LBL 20 TO LBL 30. INSTALLED T-CHORD SECTION I.A.W. B757-200 S.R.M. 51-40-02-OG. REVIEWED
*** SUPPLEMENTAL SDR *** FAULT: WTB STRUCTURE - T-CHORD STA 1037.67 IS CORRODED BETWEEN LBL 20 TO LBL 65 REVIEWED
*** SUPPLEMENTAL SDR *** FAULT: MAIN CARGO DECK - FLOOR BEAM STA 1057 BL 0 TO RBL 24.75 WITH CORROSION (UNDER FLOOR PANEL 242XGF) . DOT 07608-026 INSTALLED SUPPORT BEAM IAW SRM 51-40-02-0G. REVIEWED
WTB STRUCTURE - T-CHORD STA 1037.67 IS CORRODED BETWEEN LBL 20 TO LBL 65 REF. STEP 3 , WORK VERIFIED. REMOVED T-CHORD STA 1037.67 BETWEEN LBL 20 TO LBL 65 INSPECTED.
*** SDR FILED OPEN *** FAULT: WTB STRUCTURE - T-CHORD STA 1060 IS CORRODED BETWEEN LBL 50 TO LBL 65 EVALUATED T-CHORD AT STA 1060 BETWEEN LBL 50 TO LBL 65, EXFOLIATED CORROSION NOTED, AFTER FUTHER INVESTIGATION FOUND TO BE OUT LIMITS I.A.W SRM 53-00-71-1A-1 FIG 101 SHEET 6 NOTED D, DETAIL VII. REMOVED T-CHORD AT STA 1060 LH I.A.W SRM 51-40-02. VERIFIED REMOVAL
WTB STRUCTURE - T-CHORD STA 1060 IS CORRODED BETWEEN LBL 50 TO LBL 65. INSTALLED NEW T-CHORD STA 1060 IAW SRM 51-40-02, STEP 4. REVIEWED
MAIN CARGO DECK - FLOOR BEAM STA 1057 BL 0 TO RBL 24.75 WITH CORROSION (UNDER FLOOR PANEL 242XGF) .
*** SUPPLEMENTAL SDR *** FAULT RT WING TO BODY AREA ABOVE RAT DOOR INTERIOR AREA SHOWS EVIDENCE OF CORROSION DOT 47-09 INSTALLED T-CHORD I.A.W SRM 51-40-02-0G INSTALLED HINGE ASSY (4EA) AND GAUSSET ASSY 5(EA) I.A.W SRM 51-40-02-0G. REVIEWED
*** SUPPLEMENTAL SDR *** FAULT LEFT WING TO BODY SUPPORT AREA FWD OF W/W SHOWS EVIDENCE OF CORROSION DOT 47-05 INSTALLED T-CHORD STA 1037,67 TO 1060 LH SIDE IAW SRM 51-40-02, STEP 4. REVIEWED
*MAJOR REPAIR* FAULT: #1 ENGINE PYLON I/B AFT. SKIN HAS CORROSION AT INNER SKIN APP. STA 154 . DOT 07308-005 (PLACED AT EXTERNAL SKIN) VERIFIED COMPLIED WITH EO 88741-REQ1 AND EA 757-5450-27-A3437 REV. -. JOB COMPLETE
LEFT WING TO BODY SUPPORT AREA FWD OF W/W SHOWS EVIDENCE OF CORROSION DOT 47-05 REMOVED T-CHORD FROM STA 1037.67 TO 1060 LH SIDE LBL 67 IAW SRM 51-40-02-0G. VERIFIED T-CHORD AT STA 1037.67 TO 1060 LH SIDE REMOVED.
*** SDR FILED OPEN *** FAULT RT WING TO BODY AREA ABOVE RAT DOOR INTERIOR AREA SHOWS EVIDENCE OF CORROSION DOT 47-09 REMOVED T-CHORD AT AREA INTERIOR DOOR RAT I.A.W SRM 51-40-02-0G.- VERIFIED REMOVAL OF T-CHORD INTERIOR RAT DOOR AREA.
*** SDR FILED OPEN *** FAULT: RH RAM AIR INLET STRUCTURE AT APROX STA 880 HAS 2 ANGLES WITH CORROSION. DOT 07608-006 REMOVED RAM AIR INLET ASSY P/N: 149N7160-31 IAW AMM 21-53-01-004-001 AND LIP P/N: 149N7160-24 AND 2 CHANNELS WITH CORROSION P/N: 149N7160-8 & 149N7160-7 IAW SRM 51-40-02-0G-0. VERIFIED REMOVAL OF 1EA LIP AND 2 CHANNELS.
*** SUPPLEMENTAL SDR *** FAULT: WTB STRUCTURE - WEB FOR T-CHORD STA 900 HAS CORROSION AT APROX LBL 10 - DOT 07608-002 INSTALLED WEB AT STA 900 I.A.W. SRM 51-40-02-0G. INSTALLED SECTION T-CHORD I.A.W. SRM 51-40-02-0G. INSTALLED INTERCOSTAL AT STA 900 I.A.W. SRM 51-40-02-0G.
WTB STRUCTURE - T-CHORD STA 900 HAS CORROSION AT APROX LBL 16 - DOT 07608-005 PERFORMED CUT OUT DAMGED T-CHORD L= 75.5" STA 900 IAW SRM 51-10-02.
WTB STRUCTURE - WEB FOR T-CHORD STA 900 HAS CORROSION AT APROX LBL 10 - DOT 07608-002 REMOVED WEB ON FRAME STA 900 L/H IAW B757 SRM 51-40-02. VERIFIED WEB ON FRAME STA. 900 LH REMOVED.
FAULT: AFT CARGO PIT - FRAME STA. 1460 RH SIDE BETWEEM STR. 25R AND 26R HAS A DENT AT UPPER FLANGE. DOT 07308-001. INSTALLED NEW CLIP I.A.W SRM 51-40-02-0G.- SUPPLEMENTAL INSPECTIONS DEFERRED IAW B757-200PF REV 118.00 SRM CHAPTER 53-00-07-2R-5, TABLE #3, FOR ZONE #1.C/W SREO 84585 REQ001
ATB, ON CLIMB OUT RT ENGINE HAD SOME SURGING WITH HIGHER GET THAN LEFT ENGINE. IN CRUISE, SETTLED DOWN NORMAL. DISPATCH INSTRUCTED US TO PERFORM AN AIR TURN BACK. (OR FLUCTUATIONS). OPEN
ATB ON CLIMB OUT RT ENGINE HAD SOME SURGING WITH HIGHER GET THAN LEFT ENGINE. IN CRUISE, SETTLED DOWN NORMAL. DISPATCH INSTRUCTED US TO PERFORM AN AIR TURN BACK. (OR FLUCTUATIONS) REF.LINE ITEMS 9 AND 13. TECH RECOMMENDS R&R OF RT ENG BLEED VALVES AND SOLENOIDS. R&R COMPLETE AND OPS/LEAK CHECK OK PER AMM 71-00-00. POWER PLANT TEST #3. A/C OK FOR CONT. SERVICE
**ATB**RIGHT ENG EGT REMOVED AND REPLACED RT BVCU PER AMM 75-32-01-404-023 OPS CHK OK
INSPECTION TYPE:N/AREF D779518 FUSELAGE TAILCONE UPPER SURFACE DENTREPAIRED PER EO B757-5330-83549-C
INSPECTION TYPE:SEGAFT CARGO COMPARTMENT ON RH SIDE STA 1200-1380 TRANSITION PANEL HAVE 2 FITTINGS CORROTED..REMOVED AND REPLACED 2 EA FITTINGS IAW B-757 SRM 51-40-02-0G
INSPECTION TYPE:757LEFT ELEVATEOR UPPER SKIN SURFACE PUNCTURE,DAMAGED 9.5" FROM STAB EDGE AND 42.75" FROM FUSELAGEREPAIRED IAW SRM 55-20-01 AND SRM 51-70-17
INSPECTION TYPE:N/A**ATB - NO EMERG DECL'D - NO EMERG EQUIP USED** ON TAKEOFF ROLL NOTICED A THUMP NOISE. RETRACTED GEAR & RCVD A GEAR DISAGREE EICAS, WITH VIBRATION. COMPLETED QRH GEAR EXTENDED WITH ALT GEAR EXTENSION.R/R NLG RETRACT ACTUATOR IAW MM 32-34-01. COMPLETED AMM 32-34-01-404-008 STEP F6 - STEMP F14 USING AIRPLANE NO ON JACK METHOD. STEPS G1 & G2 COMPLETED. COMPLETED AMM 32-34-03-004-037 STEP 7C - STEP 24. RMVD DOOR LOCKS &CLOSED DOORS IAW MM 32-34-01-404-008 ST G3. M746439 CLOSED. DMP REV. IPC 32-34-01-02-500L
INSPECTION TYPE:ASEEMERGENCY EXIT LIGHTS INOPREPLACED EXIT LIGHT BATTERY. OPS CK GOOD PER AMM 33-51-07-902-001 EFF SOURCE IPC 33-51-11-01 IT 045S
INSPECTION TYPE:NAEMERGENCY UNARMED LT INOP.REMOVED AND REPLACED EMERGENCY UNARMED LT PER AMM 33-13-00. OPS CHECKED OK
INSPECTION TYPE: SEG4, DELMINATED DENT ON THE NR 2 SLAT T E WEDGE UPPER SURFACE. REPAIRED THE NR 2 TE SLAT WEDGE IAW SRM 57-43-02-2R-1, AND SRM 51-70-10-2R-4.
INSPECTION TYPE:N/AREJECTED TAKEOFF APROX 110KTS (PLUS/MINUS) DUE TO SMOKE IN COCKPIT. THICK BLOCK SMOKE CAME FROM FO SIDE OF COCKPIT FIRST THEN FROM CAPT. SIDE. THEN SMOKE CAME FROM BELOW INSTRUMENT PANEL/FOOT WELL AREAS ON BOTH SIDES. AFTER CLEARING RUNNWAY.REMOVED AND REPLACED HYD RSVR PRESS MODULE AND C HYD RSVR DEPRESSURIZATION VLV AMM 29-11-16, 29-11-25. RAN ENGS AT HIGH POWER SETTINGS FOR A LONG PERIOD OF TIME APU AND BOTH PACKS. NO SMOKE IN COCKPIT GENERAL VISUAL WHEELS AND BRAKES OK, OK FOR SERVICE. ESR: 29-11-16-05-100, 29-11-30-01-001
INSPECTION TYPE:N/AEMERGENCY LIGHTS INOPR&R EMERGENCY LIGHTS BATTERY PACK IAW AMM 33-51-07. OP/C GOOD.
INSPECTION TYPE:SDR JUMPSEAT SMOKE GOGGLES CRACKED. REPAIRED IN REF TO AMM 25-64-00.
EMERGENCY LIGHT HAS THREE BULBS INOPERATIVE. REPLACED THE BULBS IAW AMM 33-51-01-2.
INSPECTION TYPE: SEG3, APU INLET DOOR AFT MIDDLE STRAP, BS 1825 IS CORRODED. REPAIRED THE STRAP ON THE APU INLET DOOR IAW SRM 53-80-15-2R-1.
INSPECTION TYPE: SEG 3, MAIN DECK CARGO FLOOR PANEL 231XAF IS DELAMINATED. FABRICATED A NEW FLOOR PANEL IAW SREO B757-5320-9692-K.
INSPECTION TYPE: SEG 3, MAIN CARGO FLOOR PANEL 232XCF IS DELAMINATED. FABRICATED A NEW FLOOR PANEL IAW SREO B757-5320-9692-K.
INSPECTION TYPE: SEG 3, MAIN DECK CARGO FLOOR PANEL 232XHF WAS DELAMINATED. FABRICATED A NEW FLOOR PANEL IAW SREO B757-5320-9692-K.
INSPECTION TYPE: SEG 3, MAIN DECK CARGO FLOOR PANEL 231XGF WAS DELAMINATED. FABRICATED A NEW FLOOR PANEL IAW SREOB757-5320-9692-K.
INSPECTION TYPE: SEG 3, MAIN DECK CARGO FLOOR PANEL 231XHF WAS DELAMINATED. FABRICATED A NEW FLOOR PANEL IAW SREO B757-5320-9692-K.
INSPECTION TYPE: SEG 3, MAIN DECK CARGO FLOOR PANEL 242XMF WAS BROKEN. FABRICATED A NEW FLOOR PANEL IAW SREO B757-5320-9692-K.
INSPECTION TYPE: SEG 3, MAIN DECK CARGO FLOOR PANEL 232XFF WAS DELAMINATED. FABRICATED A NEW FLOOR PANEL IAW SREO B757-5320-9692-K.
INSPECTION TYPE: SEG 3, MAIN DECK CARGO FLOOR PANEL 232XGF WAS DELAMINATED. FABRICATED A NEW FLOOR PANEL IAW SREA B7575320-9692-K.
INSPECTION TYPE: SEG 3, MAIN DECK CARGO FLOOR PANEL 232XAF WAS DELAMINATED. FABRICATED A NEW FLOOR PANEL IAW SREO B757-5320-9692-K.
INSPECTION TYPE: SEG3, MAIN CARGO FLOOR PANEL 231XCF IS DELAMINATED. FABRICATED A NEW FLOOR PANEL IAW SREO B757-5320-9692-K.
INSPECTION TYPE: SEG3, MAIN CABIN FLOOR PANEL 232XJF IS DELAMINATED. FABRICATED A NEW FLOOR PANEL IAW SREO B757-5320-9692-K.
INSPECTION TYPE: SEG3, MAIN CARGO FLOOR PANEL 231XFF IS DELAMINATED. FABRICATED A NEW FLOOR PANEL IAW SREO B757-5320-9692-K.
INSPECTION TYPE: SEG3, MAIN CARGO FLOOR PANEL 231XMF IS DELAMINATED. FABRICATED A NEW FLOOR PANEL IAW SREO B757-5320-9692-K.
INSPECTION TYPE: SEG3, MAIN CARGO FLOOR PANEL 231XJF IS DELAMINATED. FABRICATED A NEW FLOOR PANEL IAW SREO B757-5320-9692-K
INSPECTION TYPE: SEG 3, MAIN DECK CARGO FLOOR PANEL 231XEF WAS DELAMINATED. FABRICATED A NEW FLOOR PANEL IAW SREO B757-5320-9692-K.
INSPECTION TYPE: SEG 3, MAIN DECK,CARGO FLOOR PANEL 232XDF IS DELAMINATED. FABRICATED A NEW FLOOR PANEL IAW SREO B757-5320-9692-K.
INSPECTION TYPE: SEG 3, MAIN DECK CARGO FLOOR PANEL 231XDF IS DELAMINATED. FABRICATED A NEW FLOOR PANEL IAW SREO B757-5320-9692-K.
INSPECTION TYPE: SEG 3, MAIN DECK CARGO FLOOR PANEL 231XBF WAS DELAMINATED. FABRICATED A NEW FLOOR PANEL IAW SREO B757-5320-9692-K.
INSPECTION TYPE: SEG 3, MAIN DECK CARGO FLOOR PANEL 232XBF WAS DELAMINATED. FABRICATED A NEW FLOOR PANEL IAW SREO B757-5320-9692-K.
INSPECTION TYPE: SEG 3, MAIN DECK CARGO FLOOR PANEL 232XEF IS DELAMINATED. FABRICATED A NEW FLOOR PANEL IAW SREO B757-5320-9692-K.
INSPECTION TYPE: SEG 3, MAIN DECK CARGO FLOOR PANEL 222XAF IS DELAMINATED. FABRICATED A NEW FLOOR PANEL IAW SREO B757-5320-9692-K.
INSPECTION TYPE: SEG 3, MAIN DECK CARGO FLOOR PANEL 221XAF IS DELAMINATED. FABRICATED A NEW FLOOR PANEL IAW SREO B757-5320-9692-K.
INSPECTION TYPE: SEG 3, MAIN DECK FLOOR PANEL 221XBF FOUND DELAMINATED. FABRICATED A NEW FLOOR PANEL IAW SREO B757-5320-9692-K.
INSPECTION TYPE: SEG 3, MAIN DECK CARGO FLOOR PANEL 222XCF FOUND DELAMINATED. FABRICATED A NEW FLOOR PANEL IAW SREO B757-5320-9692-K.
INSPECTION TYPE: SEG 3, MAIN DECK FLOOR PANEL 221XCF IS DELAMINATED. FABRICATED A NEW FLOOR PANEL IAW SREO B757-5320-9692-K.
INSPECTION TYPE: SEG 3, MAIN DECK FLOOR PANEL 222XBF IS DELAMINATED. FABRICATED A NEW FLOOR PANEL IAW SREO B757-5320-9692-K.
TAT PROBE EICAS CAUTION MESSAGE SHORTLY AFTER ROTATION RESULTED IN ATB DUE TO ICING CONDITIONS AT DESTINATION. REPLACED RELAY K140 AND REPLACED TAT SENSOR IAW AMM 34-12-02. OPS CK GOOD. IPC REF 34-12-02-5.
L FWD ENTRY DOOR EICAS ON TAKEOFF ROLL REJECTED AT 105 KTS BTB. C/W 52-12-00 PB 501 CREW ENTRY ADJ TEST AND AMM 52-12-00-705-001 TEST LATCH SYSTEM ( FISH SCALE 22LBS AND 1 LB) WITHIN LIMITS AND VERIFIED AMM 52-71-00-825-223 DOOR SENSOR CREW ENTRY DOOR ALL INDICATIONS NORMAL AC OK TO CONTINUE.
DURING FLIGHT, THE L1 DOOR EICAS & LIGHT ILLUMINATED. ACCOMPLISHED A SENSOR ADJUSTMENT IAW AMM 52-71-00-825-223. INDICATION WORKING OK
PASSING 10,000 FT, FOUL ODOR SEEMED TO GET STRONGER. REMAINED AT THE STRONG LEVEL FOR REMAINDER OF FLIGHT. DURING INITIAL INVESTIGATION OF ODOR, RAN ENGINES THEN APU, SOURCE ODOR ATTRIBUTED TO BUG ACCUMULATION AT APU INLET SCREEN. REMOVED BUGS FROM APU SCREEN. ACCOMPLISHED TASK 21-00-01-002-001 TO REMOVE ODOR FROM DUCTING.
FWD CARGO LOWER DOOR SILL FITTING CORRODED AT BS 610. R & R THE FITTING IAW SRM 51-40-02.
INSPECTION TYPE: C10, VERTICAL STABILIZER RT LOWER FWD PANEL HAS 2 DENTS STREAMER ATTACHED, DENTS FOUND TO BE DISBOND. R & R PANEL IAW DWG 175N2001.
INSPECTION TYPE: C10, FWD CARGO LOWER DOOR SILL ANGLE IS CORRODED AT BS 580. R & R THE DOOR SILL ANGLE IAW SRM 51-40-02.
INSPECTION TYPE:C10, LT WING NR 3 SLAT LOWER T/E SKIN CHAFED AS MARKED REPAIRED, CHAFED AREA NR 3 SLAT LOWER SURFACE IAW SRM 57-43-02, 51-70-10 AND EO B757-5750-59872-A.
CAPTAIN`S AND F/O`S WINDOWS OPERATE NORMALLY. LEVER REQUIRES MORE FORCE THAN USUAL., LATCH HANDLE TO BE 10 LBS. TRANSFERRED TO DMI 542707 IAW MM 56-11-02-715-20. ADJUSTED LOWER CLEVIS AND UPPER COUTERING ROLLER BRACLET ACHEIVED 6 LBS OF PULL LATCH BREAKOUT BUT STILL SEEMS STIFF WHEN GOING TO UNLATCH POSITION WC 1400508 MADE ABOVE ADJUSTMENT IAW AMM 56-11-02-829-001, PARA 2.
COCKPIT EMERGENCY LIGHT INOPERATIVE. R & R THE POWER SUPPLY IAW AMM 33-51-07-902, OPS CHECKED GOOD.
T/E FLAP DISAGREE, FLAPS STUCK AT 20 ON EXTENTION. WHEN MOVING FLAP HANDLE FROM 20-25 AT 170KTS, MESSAGE AT TRANSIENT, LOAD RELEIF EICAS MESSAGE. EMERGENCY DECLARED. PERFORMED FSEU BITE IAW FIM 27-51-00-815-805-104, NO FAULTS NOTED. T/E FLAP LOAD RELIEF SYS TEST OK IAW AMM 27-51-00-735-16 1. FLAP HYD TEST OK IAW AMM 27-51-00-715-001, PAR H. NO MSG ON ARRIVAL OR DURING OPS CHECK.
EICAS MESSAGE LT ENGINE HYD PUMP STATUS MESSAGE POWER TRANSFER UNIT. REPLACED NR 1 EDP IAW MM 29-11-05-404.
T/E FLAP ASYMMETRY ISSUE DURING APPROACH, DECLARED EMERGENCY, NO T/E LOCK OUT FOUND, FLAPS MOVE NORMALLY. CONFIRMED WITH TECH, NO FLAP ASSYMETRY LOGGED EVENTS OCCURRED THROUGH FLIGHT DATA RECORDER DOWNLOAD. R & R FLAP POSITION INDICATOR IAW AMM 27-58-02. EFF SOURCE, REF IPC 27-58-00-01-005.
DURING APPROACH, AFTER SELECTING FLAP LEVER TO 5. FLAP INDICATOR INDICATED LT FLAP 5 RT FLAP 1, EMERGENCY DECLARED. TROUBLESHOOT SYSTEM IAW FIM 27-51-00-815-812. R & R RT FLAP POSITION TRANSMITTER IAW MM 27-58-03-401.
INSPECTION TYPE: C, EVIDENCE OF CORROSION ON VERTICAL STAB T/E BEAM RUDDER STA 131 TO RUDDER STA 206. BLENDED AREA AND REPAIRED IAW EA 120227.
INSPECTION TYPE: C, LEFT MLG WHEEL WELL FRAME AT INBD FLAP TRANSMISSION, CHAFING WITH WING UPPER T/E Z-ANGLE. REMOVED DAMAGED AREA, FABRICATED REPAIR ANGLES, AND RE-INSTALLED.
INSPECTION TYPE: C, MAIN CARGO BAY, BS 1720, FLOOR DRAIN PAN FASTENER HOLES HAVE CORROSION. REMOVED CORROSION, ALODINED, PRIMED AND CIC'D AREA.
INSPECTION TYPE: C, MAIN CARGO COMPARTMENT FLOOR TRACK STA 1080 TO 1180, RBL 45 CORRODED ON UPPER SURFACE AT NUTPLATE HOLES. FABRICATED NEW SEAT TRACK FROM PRODUCTION SPLICES 1080 TO 1180, RBL 45 IAW DWG 144N5024.
INSPECTION TYPE:C-CK, FOUND DAMAGE TO TOP SIDE OF FLOORBOARD 231XLF. FABRICATED NEW FLOORBOARD IAW EO B757-5320-9692-H.
INSPECTION TYPE:C-CK, MAIN CARGO COMPARTMENT FLOOR PANEL 232XGF IS CRACKED THROUGH COMPOSITE AND HAS PUNCTURES. FABRICATED NEW FLOOR PANEL IAW EO B757-5320-9692-H.
INSPECTION TYPE:C-CK, MAIN CARGO COMPARTMENT FLOOR PANEL 231XNF HAS HOLE FABRICATED NEW FLOOR PANEL IAW EO B757-5320-9692-H.
INSPECTION TYPE:C-CK, MAIN CARGO CLOOR PANEL 221XCF IS BROKEN IN HALF. FABRICATED MAIN CARGO FLOOR PANEL 221XCF IAW EO B757-5320-9692-H.
INSPECTION TYPE:C, MAIN CARGO COMPARTMENT BS 520, S17R DENTED. REPAIRED DENT IAW EA 120232, IR STEP A 1-23, AND EO B757-5310-4 6258-A.
INSPECTION TYPE:C CK, MAIN CARGO COMPARTMENT SEAT TRACK FROM STA 1660 TO 1680, LBL 45, FLOOR PANEL HOLES HAVE CORROSION. REPLACED SEAT TRACK FROM STA 1540 TO 1681, LBL 45 IAW SRM.
INSPECTION TYPE: C, MAIN CARGO COMPARTMENT FLOOR PANEL 242XDF IS DAMAGED. FABRICATED NEW FLOOR PANEL 242XDF IAW EO B757-5320-9692-H.
INSPECTION TYPE:C, FLOORBOARD 222XCF HAS BROKEN AND CORRODED INSERTS. FABRICATED FLOORBOARD 222XCF IAW EO B757-5320-9692-H.
INSPECTION TYPE:C-CK FLOORBOARD 232XAF HAS DAMAGE. FABRICATED NEW FLOORBOARD IAW EO B757-5320-9692-H.
INSPECTION TYPE:C-CK FLOORBOARD 232XUF HAS DAMAGE. FABRICATED NEW FLOORBOARD IAW EO B757-5320-9692-H.
INSPECTION TYPE:C, MAIN CARGO COMPARTMENT FLOOR PANEL 232XFF HAS EDGE DAMAGE. FABRICATED NEW FLOOR PANEL 232XFF IAW EO B757-5320-9692-H.
INSPECTION TYPE:C, FLOORBOARD 242XFF HAS EDGE DAMAGE. FABRICATED NEW FLOOR PANEL 242XFF IAW EO B757-5320-9692-H.
INSPECTION TYPE:C, FLOORBOARD 242XAF HAS CORNER AND EDGE DAMAGE. FABRICATED NEW FLOORBOARD IAW EO B757-5320-9692-H.
INSPECTION TYPE: C, MAIN CARGO COMPARTMENT FLOOR PANEL 241XDF IS DAMAGED. FABRICATED NEW FLOOR PANEL 241XDF IAW EO B757-5320-9692-H.
INSPECTION TYPE:C-CK MAIN CARGO FLOOR PANEL 231XMF IS DELAMINATED. FABRICATED MAIN CARGO FLOOR PANEL 231XMF IAW EO B757-5320-9692-H.
INSPECTION TYPE:C-CK, MAIN CARGO FLOOR PANEL 231XHF HAS EDGE DAMAGE. FABRICATED MAIN CARGO FLOOR PANEL 231XHF IAW EO B757-5320-9692-H.
INSPECTION TYPE:C-CK, MAIN CARGO FLOOR PANEL 231XJF HAS INSERT DAMAGE AND DELAMINATED. FABRICATED MAIN CARGO FLOOR PANEL 231XJF IAW EO B757-5320-9692-H.
INSPECTION TYPE:C-CK MAIN CARGO FLOOR PANEL 231XWF HAS DENTS. FABRICATED MAIN CARGO FLOOR PANEL 231XWF IAW EO B757-5320-9692-H.
INSPECTION TYPE:C-CK, MAIN CARGO FLOOR PANEL 231XEF IS CRACKED AND DELAMINATED. FABRICATED MAIN CARGO FLOOR PANEL 231XEF IAW EO B757-5320-9692-H.
INSPECTION TYPE:C-CK, MAIN CARGO FLOOR PANEL 231 XFF IS CRACKED AND DELAMINATED. FABRICATED MAIN CARGO FLOOR PANEL 231XFF IAW EO B757-5320-9692-H.
INSPECTION TYPE:C-CK, MAIN CARGO FLOOR PANEL 231XDF IS DELAMINATED. FABRICATED MAIN CARGO FLOOR PANEL 231XDF IAW EO B757-5320-9692-H.
INSPECTION TYPE:C-CK, FLOOR PANEL 211XAF MISSING INSERTS. FABRICATED NEW FLOOR PANEL 211XAF IAW EO B757-5320-9692-H.
INSPECTION TYPE:C-CK MAIN CARGO FLOOR PANEL 231XCF IS CRACKED AND DELAMINATED. FABRICATED MAIN CARGO FLOOR PANEL 231XCF IAW EO B757-5320-9692-H.
INSPECTION TYPE:C-CK, MAIN CARGO FLOOR PANEL 231XRF HAS DENTS. FABRICATED MAIN CARGO FLOOR PANEL 231XRF IAW B757-5320-9692-H.
INSPECTION TYPE:C-CK MAIN CARGO FLOOR PANEL 231XGF HAS INSERT DAMAGE. FABRICATED MAIN CARGO FLOOR PANEL 231XGF IAW EO B757-5320-9692-H
INSPECTION TYPE:C-CK MAIN CARGO FLOOR PANEL 231XKF HAS EDGE DAMAGED AND DELAMINATED. FABRICATED MAIN CARGO FLOOR PANEL 231XKF IAW EO B757-5320-9692-H.
INSPECTION TYPE:C-CK, MAIN CARGO FLOOR PANEL 231XQF HAS INSERT DAMAGED AND BROKEN IN HALF. FABRICATED MAIN CARGO FLOOR PANEL 231XQF IAW EO B757-5320-9692-H.
INSPECTION TYPE:C-CK, MAIN CARGO FLOOR PANEL 231XTF HAS INSERT DAMAGED. FABRICATED MAIN CARGO FLOOR PANEL 231XTF IAW EO B757-5320-9692-H.
INSPECTION TYPE:C-CK, MAIN CARGO FLOOR PANEL 231XPF HAS DENTS AND EDGE DAMAGE. FABRICATED MAIN CARGO FLOOR PANEL 231XPF IAW EO B757-5320-9692-H.
INSPECTION TYPE:C-CK, MAIN CARGO FLOOR PANEL 241XGF HAS EDGE DAMAGE. FABRICATED MAIN CARGO FLOOR PANEL 241XGF IAW EO B757-5320-9692-H.
INSPECTION TYPE:C-CK, MAIN CARGO FLOOR PANEL 232XCF IS DELAMINATED. FABRICATED MAIN CARGO FLOOR PANEL 232XCF IAW EO B757-5320-9692-H.
INSPECTION TYPE:C-CK, MAIN CARGO FLOOR PANEL 232XDF HAS EDGE DAMAGE. FABRICATED MAIN CARGO FLOOR PANEL 232XDF IAW EO B757-5320-9692-H.
INSPECTION TYPE:C-CK, MAIN CARGO FLOOR PANEL 232XPF HAS EDGE DAMAGE. FABRICATED MAIN CARGO FLOOR PANEL 232XPF IAW EO B757-5320-9692-H.
INSPECTION TYPE:C-CK, MAIN CARGO FLOOR PANEL 232XWF HAS EDGE DAMAGE. FABRICATED MAIN CARGO FLOOR PANEL 232XWF IAW EO B757-5320-9692-H.
INSPECTION TYPE:C-CK, MAIN CARGO FLOOR PANEL 251XJF IS DENTED AND MISSING INSERTS. FABRICATED MAIN CARGO FLOOR PANEL 251XJF IAW EO B757-5320-9692-H.
INSPECTION TYPE:C-CK, MAIN CARGO FLOOR PANEL 251XHF IS DENTED AND EDGE DAMAGED. FABRICATED MAIN CARGO FLOOR PANEL 251XHF IAW EO B757-5320-9692-H.
INSPECTION TYPE:C-CK, MAIN CARGO FLOOR PANEL 251XMF IS CRACKED. FABRICATED MAIN CARGO FLOOR PANEL XMF IAW EO B757-5320-9692-H.
INSPECTION TYPE:C-CK, MAIN CARGO FLOOR PANEL 251XKF HAS DENT. FABRICATED MAIN CARGO FLOOR PANEL 251XKF IAW EO B757-5320-9692-H.
INSPECTION TYPE:C-CK, MAIN CARGO FLOOR PANEL 251XLF HAS DENTED AND EDGE DAMAGE. FABRICATED MAIN CARGO FLOOR PANEL 251XLF IAW EO B757-5320-9692-H.
INSPECTION TYPE:C-CK, MAIN CARGO FLOOR PANEL 251XGF IS DENTED. FABRICATED MAIN CARGO FLOOR PANEL 251XGF IAW EO B757-5320-9692-H.
INSPECTION TYPE:C-CK, MAIN CARGO FLOOR PANEL 252XCF HAS DENTED AND MISSING INSERTS. FABRICATED MAIN CARGO FLOOR PANEL 252XCF IAW EO B757-5320-9692-H.
INSPECTION TYPE:C-CK MAIN CARGO FLOOR PANEL 252XAF HAS DENT. FABRICATED MAIN CARGO FLOOR PANEL 252XAF IAW EO B757-5320-9692-H.
INSPECTION TYPE:C-CK, MAIN CARGO FLOOR PANEL 252XFF IS BROKEN. FABRICATED MAIN CARGO FLOOR PANEL 252XFF IAW EO B757-5320-9692-H.
INSPECTION TYPE:C-CK, MAIN CARGO FLOOR PANEL 252XEF IS BROKEN. FABRICATED MAIN CARGO FLOOR PANEL 252XEF IAW EO B757-5320-9692-H.
INSPECTION TYPE:C-CK, MAIN CARGO FLOOR PANEL 252XDF HAS DENT DAMAGE. FABRICATED MAIN CARGO FLOOR PANEL 252XDF IAW EO B757-5320-9692-H.
INSPECTION TYPE:C-CK, MAIN CARGO FLOOR PANEL 252XJF HAS DENT DAMAGE, DELAMINATED. FABRICATED MAIN CARGO FLOOR PANEL 252XJF IAW EO B757-5320-9692-H.
INSPECTION TYPE:C-CK, MAIN CARGO FLOOR PANEL 252XQF HAS DENT DAMAGE, DELAMINATED. FABRICATED MAIN CARGO FLOOR PANEL 252XQF IAW EO B757-5320-9692-H.
INSPECTION TYPE:C-CK, MAIN CARGO FLOOR PANEL 252XNF HAS DENT DAMAGE. FABRICATED MAIN CARGO FLOOR PANEL 252XNF IAW EO B757-5320-9692-H.
INSPECTION TYPE:C-CK, MAIN CARGO FLOOR PANEL 252 XPF HAS DENT DAMAGE, DELAMINATED. FABRICATED MAIN CARGO FLOOR PANEL 252XPF IAW EO B757-5320-9692-H.
INSPECTION TYPE:C-CK, MAIN CARGO FLOOR PANEL 241XJF HAS DENT DAMAGE AND MISSING INSERTS. FABRICATED MAIN CARGO FLOOR PANEL 241XJF IAW EO B757-5320-9692-H.
INSPECTION TYPE:C-CK, MAIN CARGO FLOOR PANEL 251XDF IS DENTED. FABRICATED MAIN CARGO FLOOR PANEL 251XDF IAW EO B757-5320-9692-H.
INSPECTION TYPE:C-CK MAIN CARGO FLOOR PANEL 251XEF IS DENTED HOLES. FABRICATED MAIN CARGO FLOOR PANEL 251XEF IAW EO B757-5320-9692-H.
INSPECTION TYPE:C-CK, MAIN CARGO FLOOR PANEL 251XBF IS DENTED, DELAMINATED. FABRICATED MAIN CARGO FLOOR PANEL 251XBF IAW EO B757-5320-9692-H.
INSPECTION TYPE:C-CK, MAIN CARGO FLOOR PANEL 251XCF IS DENTED MISSING INSERTS. FABRICATED MAIN CARGO FLOOR PANEL 251XCF IAW EO B757-5320-9692-H.
INSPECTION TYPE:C-CK MAIN CARGO FLOOR PANEL 242XLF IS DENTED AND MISSING INSERTS. FABRICATED MAIN CARGO FLOOR PANEL 242XLF IAW EO B757-5320-9692-H
INSPECTION TYPE:C-CK, MAIN CARGO FLOOR PANEL 242XKF IS DELAMINATED AND MISSING INSERTS. FABRICATED MAIN CARGO FLOOR PANEL 242XKF IAW EO B757-5320-9692-H.
INSPECTION TYPE:C-CK MAIN CARGO FLOOR PANEL 241XHF IS DELAMINATED AND DAMAGED. FABRICATED MAIN CARGO FLOOR PANEL 241XHF IAW EO B757-5320-9692-H.
INSPECTION TYPE:C-CK, MAIN CARGO FLOOR PANEL 241XLF HAS EDGE DAMAGE. FABRICATED MAIN CARGO FLOOR PANEL 241XLF IAW EO B757-5320-9692-H.
INSPECTION TYPE:C-CK, MAIN CARGO FLOOR PANEL 232XSF HAS EDGE DAMAGE. FABRICATED MAIN CARGO FLOOR PANEL 232XSF IAW EO B757-5320-9692-H.
INSPECTION TYPE:C-CK, MAIN CARGO FLOOR PANEL 232XTF HAS EDGE DAMAGE. FABRICATED MAIN CARGO FLOOR PANEL 232XTF IAW EO B757-5320-9692-H.
INSPECTION TYPE:C-CK, MAIN CARGO FLOOR PANEL 232XYF HAS EDGE DAMAGE. FABRICATED MAIN CARGO FLOOR PANEL 232XYF IAW EO B757-5320-9692-H.
INSPECTION TYPE: C, MAIN CARGO COMPARTMENT FLOOR PANEL 241XMF MISSING INSERTS. REPAIRED IAW EO B757-5320-9692-H.
INSPECTION TYPE:C-CK, MAIN CARGO COMPARTMENT FLOOR PANEL 222XAF HAS EDGE DAMAGE. FABRICATED NEW FLOOR PANEL 222XAF IAW EO B757-5320-9692-H.
INSPECTION TYPE:C, MAIN CARGO COMPARTMENT FLOOR PANEL 242XHF NUMEROUS MISSING INSERTS. FABRICATED NEW FLOOR PANEL IAW EO B757-5320-9692-H.
INSPECTION TYPE:C, MAIN CARGO COMPARTMENT FLOOR PANEL 241XEF HAS MISSING INSERTS. FABRICATED NEW FLOOR PANEL 241XEF IAW EO B757-5320-9692-H.
INSPECTION TYPE:C-CK, MAIN CARGO COMPARTMENT FLOOR PANEL 231XAF HAS EDGE DAMAGE. FABRICATED NEW FLOOR PANEL 231XAF IAW EO B757-5320-9692-H.
INSPECTION TYPE:C, MAIN CARGO COMPARTMENT FLOOR PANEL 221XAF HAS EDGE DAMAGE. FABRICATED NEW FLOOR PANEL 221XAF IAW EO B757-5320-9692-H.
INSPECTION TYPE:C, MAIN CARGO COMPARTMENT FLOOR PANEL 251XFF HAS INSERTS MISSING. FABRICATED NEW FLOOR PANEL 251XFF IAW EO B757-5320-9692-H.
INSPECTION TYPE:C, MAIN CARGO COMPARTMENT FLOOR PANEL 252XLF HAS MISSING INSERTS. FABRICATED NEW FLOOR PANEL 252XLF IAW EO B757-5320-9692-H.
INSPECTION TYPE:C, MAIN CARGO COMPARTMENT FLOOR PANEL 221XBF HAS HOLE PUNCTURES. FABRICATED NEW FLOOR PANEL 221XBF IAW EO B757-5320-9692-H.
INSPECTION TYPE: C, VERTICAL STAB PANEL, 322DL, HAS HOLES WITH EXPOSED COMPOSITE. REPAIRED PANEL 322DL IAW SRM 51-70-17-0G.
INSPECTION TYPE: C, MAIN CARGO BAY BS 1577 RT CREASE BEAM CORRODED. REPAIRED CREASE BEAM IAW EA 120255 IR, AND EO.
INSPECTION TYPE:C, MAIN CARGO COMPARTMENT RT SIDE BS 1055, RBL 41 AT FLOOR SUPPORT HAS (2) AREAS OF CORROSION AT SCREW HOLES. REMOVED CORROSION, ORIGINAL MATERIAL THICKNESS .050 100 PERCENT MATERIAL LOSS AT FASTENER HOLE FABRICATED AND REPLACED FLOOR SUPPORT IAW DWG 144N5005 AND CMM 9-10 INSTALLED NEW SUPPORT IAW SRM 51-40-02.
INSPECTION TYPE: C, MAIN CARGO FLOORBEAM STA 1200, LBL 45 TO RBL 55 FLOORBEAM CORRODED ON UPPER FLANGE AT NUTPLATE HOLES. REMOVED CORROSION. ORIGINAL THICKNESS .270, MATERIAL REMOVED IS .025-.05, REMAINING THICKNESS .180-.205, OUT OF LIMITS IAW SRM 53- 00-51-1A1. REPAIRED DAMAGED AREA IAW EA 120257 EO B757-5310-4624 2-A.
INSPECTION TYPE: C, MAIN CARGO COMPARTMENT STA 1680, RBL 3 TO RBL 23, FLOOR DECKING HAS CORROSION. REMOVED CORROSION AT STA 1680, RBL 3 TO RBL 23, ORIGINAL THICKNESS IS .075, LOSS OF .003- .017 WITH .072- .058 REMAINING IS OUT OF LIMITS. REMOVED DAMAGE AND REPAIRED IAW EA 128249 IR/EO B757-5310-46277-A.
INSPECTION TYPE: C, MAIN CARGO TRACK STA 1060 TO 1100, LBL 60, 3 EA NUTPLATES CORRODED. REMOVED CORROSION. ORIGINAL MATERIAL THICKNESS .075 MAX LOSS OF .020 WITH .055 REMAINING IS OUT OF LIMITS IAW 53-00-52-1A1. ACCOMPLISHED STEPS OF EA 120230 IR EO B757-5310-46193-A.
INSPECTION TYPE: C, MAIN CARGO BAY BS 1680, LBL 3 TO LBL 14, FLOORBEAM HAS CORROSION. REMOVED CORROSION, ORIGINAL THICKNESS IS .075 LOSS OF .005-.025 WITH .070- .050 REMAINING IS OUT OF LIMITS. REMOVED DAMAGE AND REPAIRED IAW EA 128249 EO B757-5310-46277-A.
INSPECTION TYPE: C, MAIN CARGO TRACK BS 1080 TO 1200, RBL 45, CARGO TRACK CORRODED ON UPPER SURFACE AT NUTPLATE HOLES. REMOVED CORROSION ORIGINAL THICKNESS .080 LOSS OF .032 WITH .047 IS OUT OF LIMITS. R & R CARGO TRACK IAW SRM 51-40-02 AND DWGS 146N5218 AND 146N5217.
INSPECTION TYPE: C, MAIN CARGO FLOORBEAM, BS 1100, BL 0 TO RBL 45, CORRODED ON UPPER SURFACE AT NUTPLATE HOLES. REMOVED CORROSION ON FLOORBEAM, ORIGINAL MATERIAL .0196 LOSS OF .101 WITH .095. FOUND OUT OF LIMITS IAW SRM 53-00-51-1A1. REMOVED DAMAGE AND REPAIRED FLOORBEAM IAW EA 120225 IR B757-5310-46239-A.
INSPECTION TYPE: C, MAIN CARGO COMPARTMENT STA 1660 TO 1680, LBL 26, 7EA FLOOR PANEL FASTENER HOLES HAVE CORROSION. REMOVED CORROSION ORIGINAL THICKNESS .080 LOSS OF .036 WITH .044 IS OUT OF LIMITS. R & R SEAT TRACK IAW SRM 51-40-02 AND DWGS 146N5220 AND 146N5217, FROM STA 1540-1681.
INSPECTION TYPE:C-CK, MAIN CARGO FLOOR PANEL 251XNF IS DELAMINATED. FABRICATED MAIN CARGO FLOOR PANEL 251XNF IAW EO B757-5320-9692-H.
INSPECTION TYPE:C-CK, MAIN CARGO FLOOR PANEL 251XQF HAS COMPOSITE DAMAGE. FABRICATED MAIN CARGO FLOOR PANEL 251XQF IAW EO B757-5320-9692-H.
INSPECTION TYPE:C-CK, MAIN CARGO FLOOR PANEL 251XPF HAS COMPOSITE DAMAGE. FABRICATED MAIN CARGO FLOOR PANEL 251XPF IAW EO B757-5320-9692-H.
INSPECTION TYPE:C-CK, MAIN CARGO FLOOR PANEL 252XTF HAS EDGE DAMAGE. FABRICATED MAIN CARGO FLOOR PANEL 252XTF IAW EO B757-5320-9692-H.
INSPECTION TYPE:C-CK, MAIN CARGO FLOOR PANEL 252XSF HAS EDGE DAMAGE. FABRICATED MAIN CARGO FLOOR PANEL 252XSF IAW EO B757-5320-9692-H.
INSPECTION TYPE:C-CK MAIN CARGO FLOOR PANEL 252XRF HAS EDGE DAMAGE FABRICATED MAIN CARGO FLOOR PANEL 252XRF IAW EO B757-5320-9692-H
INSPECTION TYPE: C, MAIN CARGO BAY BS 1680, RBL 27 TO RBL 41, FLOORBEAM HAS CORROSION. REMOVED CORROSION ORIGINAL THICKNESS IS .075, LOSS OF .003- .030 WITH .072- .045. REMAINING IS OUT OF LIMITS, REMOVED DAMAGE AND REPAIRED IAW EA 128249. EO B757-5310-46277-A.
INSPECTION TYPE:C, MAIN CARGO BS 640R FRAME FLANGE HAS WEAR AREA 14" ABOVE FLOOR. BLENDED WEAR AREA AT BS 640R FRAME FLANGE 14" ABOVE FLOOR, ORIGINAL MATERIAL THICKNESS .056 WITH A LOSS OF .007 AND .049 REMAINING IS OUT OF LIMITS IAW SRM 53-00-07-1A1. ACCOMPLISHED STEP A OF EA FOR EXTENDED LIMITS AIW EA 120243 EO B757-5310-46173-A.
INSPECTION TYPE: C, FWD CARGO BAY BS 760 STR 23L VERTICAL FRAME IS DENTED. REMOVED DAMAGE FROM FRAME. FABRICATED AND INSTALLED FRAME REPAIR IAW SRM 53-00-07-2R5, DETAIL 2.
INSPECTION TYPE: C, FWD CARGO BAY BS 780 VERTICAL FRAME IS DENTED BETWEEN STR 23L AND 24L. REMOVED DAMAGE AT FWD CARGO PIT STA 780, VERTICAL FRAME BETWEEN STR 23L AND 24L. FABRICATED AND INSTALLED FRAME REPAIR MADE FROM 7075.0 .063 AND HEAT TREATED TO T6 CONDITION IAW SRM 53-00-07-2R5, DETAIL 2.
INSPECTION TYPE: C, AFT CARGO FRAME DENTED AT BS 1320, S26L. REPAIRED FRAME IAW SRM 53-00-07-2R 5, DETAIL REV 82.
INSPECTION TYPE: C, AFT CARGO BS 1580 FRAME DENTED BETWEEN S25L AND S26L REPAIRED FRAME IAW SRM 53-0 0-07-2R REPAIR 5, DETAIL 3, REV 82.
INSPECTION TYPE: C, AFT CARGO STA 1520 FRAME DENTED JUST INBD OF S25L. REPAIRED FRAME IAW SRM 53-00-07-2R, REPAIR 5, DETAIL 3, REV 82.
INSPECTION TYPE: C, FWD CARGO BAY BS 760 VERTICAL FRAME IS DENTED BETWEEN S-23R AND S-24R. REPAIRED FRAME IAW SRM 53-00 -07-2R REPAIR 5, DETAIL 1, REV 82.
INSPECTION TYPE: C, AFT CARGO BS 1540 FRAME DENTED AT S26R, REPAIRED FRAME IAW SRM 53-00-07-2R, REPAIR 5, DETAIL 1, REV 82.
INSPECTION TYPE: C, AFT CARGO BS 1500 FRAME DENTED AT S 26L. REPAIRED FRAME IAW SRM 53-00-07 2R, REPAIR 5, DETAIL 1.
INSPECTION TYPE: C, FWD CARGO BAY BS 700, S24R VERTICAL FRAME IS DENTED CUTOUT DAMAGE AND REPAIRED FRAME AT STA 700, STR 24R BY INSTALLING REP AIR DOUBLER FABRICATED FROM 7075-T6- .071 IAW SRM 53-00-07-2R5, DETAIL 3.
INSPECTION TYPE:C-CK, FWD CARGO PIT STA 820 VERTICAL FRAME IS DENTED BETWEEN STR 23L AND 24L. CUT OUT DAMAGE AND REPAIRED FRAME AT STA 820 BETWEEN STR 23L AND 24L BY INSTALLING REPAIR DOUBLER FABRICATED FROM 7075-T6-.063 IAW SRM 53-00 -07-2R5 DETAIL 2.
INSPECTION TYPE:C-CK, FWD CARGO PIT STA 800, STR 24L VERTICAL FRAME IS DENTED. CUT OUT DAMAGE AND REPAIRED FRAME AT STA 800, STR 24L BY INSTALLING REPAIR DOUBLER FABRICATED FROM 7075-T6-.080 IAW SRM 53-00-07-2R5 DETAIL 3.
INSPECTION TYPE: C, BS 1480 FRAME DENTED AT S26L. REPAIRED FRAME IAW SRM 53-00-07 2R REPAIR 5, DETAIL 1.
INSPECTION TYPE: C, MAIN CARGO BS 1055, BL 0 TO RBL 25 FLOOR SUPPORT INTERCOSTAL HAS CORROSION AROUND 4 EA NUT PLATE HOLES. REMOVED CORROSION, ORIGINAL MATERIAL THICKNESS .050 MATERIAL LOSS OF .013 WITH .037 REMAINING IS OUT OF LIMITS IAW SRM 53-00-51-1A1. FABRICATED AND REPLACE FLOOR SUPPORT INTERCOSTAL IAW DWG 144N5005 AND CMM 9-10 ISTSTALLED NEW SUPPORT IAW SRM 51-40-02.
INSPECTION TYPE: C, MAIN CARGO BAY BS 345 S16R INBD SURFACE OF FRAME CHAFED FROM SIDEWALL FASTENER. REMOVED DAMAGE, ORIGINAL MATERIAL THICKNESS .050 LOSS OF .020 REMAINING .030 IS OUT OF LIMITS IAW SRM 53-00-07-1A1.
INSPECTION TYPE:C, MAIN CARGO BAY BS 1100, LBL 25 TO LBL 45 FLOORBEAM TEE CAP HAS CORROSION AROUND EVERY NUT PLATE HOLES. REMOVED CORROSION, ORIGINAL MATERIAL THICKNESS .196 LOSS OF .056 WITH .140. REMAINING IS OUT OF SRM LIMITS REPAIRS IAW EA 120254 EO B757-5310-46223-A.
INSPECTION TYPE:C-CK, AFT CARGO BS 1500 FRAME DENTED AT STR 23R. CUT OUT DAMAGE AT FRAME STA 1500, STR 23R. FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 53-00-07-2R5.
INSPECTION TYPE: C, LEFT WING INBD MAIN FLAP, OTBD LOWER SURFACE DENTED, 38" FORWARD OF T/E AND 36" FROM OTBD EDGE. REPAIRED AREA IAW SRM 51-70-10-2R2.
INSPECTION TYPE: C, AFT CARGO BAY, FRAME BS 1220 ABOVE S26R DENTED. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER & FILLER IAW EA 120180 IR/ EO B757-5310-46276-A.
INSPECTION TYPE: C, MAIN FUSELAGE FRAME BS 720, S15L DAMAGED. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER IAW EA EO B757-5310-46272-A.
INSPECTION TYPE: C, AFT CARGO BAY, FRAME BS 1300 ABOVE S26R DENTED. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR PARTS IAW EA 120181, EO B757-5310-46279-A.
INSPECTION TYPE: C, MAIN CARGO BAY, BS 1180 BETWEEN STRINGER 15L AND 16L, FRAME FREE FLANGE IS GOUGED. REMOVED DAMAGE, ORIGINAL THICKNESS .375 WITH A LOSS OF .045 AND .330. OUT OF LIMITS IAW SRM 53-40-08-1A3. ACCOMPLISHED EA 120250, EO B757-5310-46174-A.
INSPECTION TYPE: C, FWD CARGO BAY, BS 780, S24R VERTICAL FRAME DENTED. REMOVED DAMAGE AT FRAME, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 53-00-07-2R5, DETAIL 3.
INSPECTION TYPE: C, MAIN CARGO BS 680R, FRAME FLANGE WEAR AREA 14" ABOVE FLOOR. BLENDED DAMAGE AREA AT BS 680R FRAME FLANGE 14" ABOVE FLOOR ORIGINAL MATERIAL .056" WITH A LOSS OF .007" AND .049" REMAINING IS OUT OF LIMITS IAW SRM 53-00-07-1A-1 ACCOMPLISHED EA INSTRUCTIONS FOR EXTENDED LIMITS IAW EA 120242 EO B757-5310-46167-A.
INSPECTION TYPE: C, MAIN CARGO BAY BS 1063-1080, LBL 25 OTBD SEAT TRACK FLANGE HAS CORROSION AROUND 4EA NUT PLATE HOLES. BLENDED CORROSION ORIGINAL MATERIAL THICKNESS .090 WITH A LOSS OF .033 AND .057 REMAINING IS OUT OF LIMITS IAW SRM 53-00-51-1A1. REMOVED, FABRICATED, AND INSTALLED UPPER CHORD IAW SRM 51-40-02, AND DWG 144N8017.
INSPECTION TYPE: C, AFT CARGO, BS 1480 RT SIDEWALL ATTACH ANGLE CORRODED JUST BELOW S26R. REMOVED SIDEWALL ATTACH ANGLE AND REPLACED WITH NEW ANGLE IAW SRM 51-40-02 AND GMM 9-10-01-4.
INSPECTION TYPE:C-CK, AFT CARGO STA 1560 FRAME DENTED AT STR 26L. REMOVED DAMAGE AT STA 1560 FRAME, STR 26L FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 53-00-07-2R5, DETAIL 2.
INSPECTION TYPE:C, MAIN CARGO PIT STA 940, BETWEEN STRINGER 15R AND 16R, FRAME FREE FLANGE IS GOUGED IN 1 EA AREAS. BLENDED GOUGE AT STA 940. BETWEEN STR 15R AND 16R, ORIGINAL THICKNESS .163 WITH A LOSS OF .021 WTIH .142 REMAINING IS OUT OF LIMITS IAW SRM 53-00-07-1A1. ACCOMPLISHED STEP OF EA FOR EXTENDED LIMITS AIW EA 120236 EO B757-5310-46167-A.
INSPECTION TYPE:C, MAIN CARGO UPSTAIRS FRAME 740 STR 15L DAMAGED. BLENDED DAMAGE AT FRAME STA 740, STR 15L, ORIGINAL THICKNESS .063 WITH A LOSS OF .011 ANS .052 REMAINING IS OUT OF LIMITS IAW SRM 53-00-07-1A1 ACCOMPLISHED STEPS OF EA FOR EXTENDED LIMITS IAW EA 120241, EO B757-5310-46177-A.
INSPECTION TYPE: C, MAIN CARGO COMPARTMENT STA 600R STR 17 DENTED. REPAIRED DENT IAW EA 120240IR, AND EO B757-5310-46219-A.
INSPECTION TYPE: C, AFT CARGO BS 1540, FRAME DENTED AT S22R. REPAIRED FRAME IAW SRM 53-00-07 2R REPAIR 5, TABLE 2.
INSPECTION TYPE:C, FLOOR PANEL 212XAF HAS EDGE DAMGE AND SEVERAL PUNCTURES. FABRICATED NEW FLOOR PANEL 212XAF IAW EO B757-5320-9692-H.
INSPECTION TYPE:C-CK, MAIN CARGO COMPARTMENT FLOOR PANEL 251XJF DAMAGED. REPLACE FLOOR PANEL 251XJF IAW B757-5320-9692-H.
MAIN CARGO DOOR SKIN DAMAGED. REPAIRED IAW EO B757-5230-44889A.
MAIN CARGO DOOR OUTER SKIN DENTED. REPAIRED FWD DENT ON MCD STA 520 IAW EO B757-5230-44346-A AND SRM 52-30-01-2R, REPAIR 4.
EMERGENCY EXIT LIGHTS GO OFF AFTER 5 SEC. R & R BATTERY PACK IAW AMM 33-51-07-2. OPS CK NORMAL.
SHORTLY AFTER TAKEOFF CREW NOTICED LT SYS HYD QTY MSG. DID ATB ACFT LANDED WITH .08 REMAINING QTY. MAINT FOUND LT ENG DRIVEN HYD PRESSURE AND CASE DRAIN MODULE LEAKING. REPLACED FILTER MODULE ASSY, IAW MM 29-11-17-4. CHECKED GOOD.
INSPECTION TYPE:C3 UPON REMOVAL OF FLOOR PANEL FROM BS 1100-1200, FOUND SEAT TRACK TO HAVE CORROSION AROUND NUT PLATE HOLES BS 1160-1187, RBL 65, WL 208. REMOVED AND REPLACE SEAT TRACK B/S 1060-1180, RBL 65, WL 208 IAW SRM 51-40-05, 51-40-08-0G, 51-40-02-0G, AND ER NR 10-1692.
INSPECTION TYPE:MOD RIGHT PYLON LEFT UNDERWING FAIRING SUPPORT STRUCTURE BULLNOSE ATTACH BRACKET HAS ELONGATED FASTENER HOLES AT PPS 170. REPLACED CHANNEL IAW SRM 51-40-02-0G, SRM 51-40-05, DWG313N5004 AMM 51-21-10.
INSPECTION TYPE:MOD NR 2 PYLON AFT FAIRING STRUCTURE RT FWD VERTICAL ANGLE IS CHAFED ON THE OUTER RADIUS. PPS 208.47 P/N 313N5033-100. REPLACED ANGLE IAW SRM 51-40-02-0G, SRM 51-40-05-0G, BOEING DWG 313N5033, SRM 51-40-08-0G, AMM 51-21-04-07, AMM 51-21-10-7.
INSPECTION TYPE:MOD RT PYLON RT UNDER WING FAIRING SUPPORT STRUCTURE AFT BRACE HAS A CRACK IN THE UPPER RADIUS AT PPS 185.35. REPLACED RT PYLON RT UNDERWING FAIRING SUPPORT STRUCTURE AFT BRACE PER SRM 51-40-05-0G, SRM 51-40-08-0G, SRM 51-40-02, SRM 54-50-71-1A 1.
INSPECTION TYPE:MOD RIGHT PYLON RT UNDERWING FAIRING SUPPORT STRUCTURE FWD BRACE HAS UPPER TAB BROKEN OFF AT PPS 185.35. REPLACED BRACE IAW SRM 51-40-02, SRM 51-40-05, SRM 54-50-71-1A 1.
INSPECTION TYPE:C3 REPAIR VALIDATION REQUIRED FOR EFN 4562008 1013, MAIN DECK FLOOR PANEL AT BS 1100-1200, LBL 45-65. FLOOR PANEL WAS REPLACED PER EO B757-5320-9692-G.
INSPECTION TYPE:C3, AFT CARGO BAY FLOOR PANEL NR4 IS CORRODED ON UPPER SURFACE. R & R AFT CARGO FLOOR PNL IAW SRM 51-40-02; SRM 51-40-08; SRM 51-20-01; SRM 53-60-53-0I-1.
INSP TYPE:C3, AFT CARGO BAY FLOOR PANEL NR 3 IS CORRODED ON UPPER SURFACE. REPLACED FLOOR PANEL IAW SRM 53-60-53-0I1, SRM 51-40-05, SRM 51-40-08, AND SRM 51-20-01-0G.
INSP TYPE:C3, FWD CARGO BAY FLOOR PANEL NR 3 IS CORRODED. FABRICATED FLOOR PANEL IAW SRM 51-40-08-0G, SRM 53-30-53-01-1 AND DWG 435N1170.
INSP TYPE:C3, AFT CARGO BAY FLOOR PANEL NR 2 IS PUNCTURED. REPLACED IAW SRM 53-60-53-0I1, SRM 51-40-05, SRM 51-40-08, SRM 51-20-01-0G.
INSP TYPE:C3 FWD CARGO BAY FLOOR PANEL NR 4 IS CORRODED. FABRICATED FLOOR PANEL IAW SRM 53-60-53-01-1, SRM 51-40-05 AND SRM 51-40-08.
INSPECTION TYPE:C3 AFT CARGO BAY FLOOR PANEL NR 4 IS CORRODED ON UPR SURFACE. R & R FLOOR PANEL IAW SRM 51-40-02; SRM 51-40-08; SRM 53-00-53-1A1; 53-60-53-01-1.
INSPECTION TYPE:C3, RT WING FUELING PANEL 621GB IS CORRODED UNDER THE GAUGES. FUELING PANEL WAS REPLACED IAW MM 28-21-08-4.
INSPECTION TYPE:C3, WHILE PERFORMING THE REPAIR ASSESSMENT FOUND THE NR7 SLAT T/E WEDGE TO HAVE A DELAM AT THE PREVIOUS REPAIR AT OSS 377.45-383.15 AND 4.5" FWD OF THE T/E EDGE (456-W4-03). NR 7 SLAT T/E WEDGE UPPER SURFACE WAS REPAIRED IAW SRM 51-70-10-2R.
INSPECTION TYPE:C3 RT HORIZONTAL STAB LOWER SURFACE HAS "OUT OF LIMITS" GOUGE APPROXIMATELY 8 FT FROM OTBD END, 14 INCHES AFT OF L/. BLENDED AREA, ACCOMPLISHED REMAINING MATERIAL THICKNESS CHECK ACCOMPLISHED NDI TO VERIFY NO CRACK OR DELAMINATION PRESENT, FILLED GOUGE, SANDED AND REFINISHED AREA IAW ATS ER 10-1575 SRM 51-70-01 UPS EO B757-5510-36880-A.
INSP TYPE:C3, MCB FLOOR PANEL, LBL 25-45, BS 900-1020 INBD CORNER IS BROKEN PANEL WAS REPLACED IAW EO NR B757-5320-9692-G.
INSP TYPE:C3, MCB FLOOR PANEL, RBL 25-45, BS 1020-1060 IS DAMAGED AT FASTENER HOLES. PANEL WAS REPLACED IAW EO NR B757-5320-9692-G.
INSPECTION TYPE:C3, MCB FLOOR PANEL RT 1680-1720 IS PUNCTURED IN SEVERAL AREAS. PANEL WAS REPLACED IAW EO NR B757-5320-9692G.
INSP TYPE:C3, MCB FLOOR PANEL, RBL 25-45, BS 900-1020 IS DAMAGED. PANEL WAS REPLACED IAW EO NR B757-5320-9692-G.
INSPECTION TYPE:C3, MCB FLOOR PANEL, LBL 45-65, BS 900-1020 IS DAMAGED AT FASTENER HOLE. PANEL WAS REPLACED IAW EO NR B757-5320-9692-G.
INSP TYPE:C3, MAIN CABIN INTERIOR, SECT 44, RBL 45-65, BS 900-BS 1000, FLOOR PANEL OTBD AFT CORNER IS BROKEN. PANEL WAS REPLACED IAW EO B757-5320-9692-G.
INSP TYPE:C3, MCB FLOOR PANEL LT 1680-1720 IS DELAMINATED. PANEL WAS REPLACED IAW EO B757-5320-9692-G.
FUSELAGE SKIN DAMAGE AFT OF CREW ENTRY DOOR 34 INCHES. INSTALLED REPAIR IAW EO B757-5330-36563-A.
INSPECTION TYPE:N/A MCD FLOOR PANEL POS 15R DAMAGED. REPAIRED PER EO B757-5320-34136-A.
DIVERSION - BOTH CONTROL WHEEL'S STAB TRIM SWITCHES INOP IN FLT. NO FAULTS BALL ON SMMS PRESENT CONTINUED T/S STAB TRIM MSG APPEARS WHEN GOING TO A/P NOSEDOWN DIRECTION & AT HALF SPEED. STOPPED T/S AT START 3 BLOCK 26 D. R&R'D BRAKE PRESS SWITCH PER FM - NO HELP. R&R'D STAB TRIM LIMIT SWITCH & POSITION PER MM 27-48-01-4. REQ ADJ TEST. ALL CHECKS NORMAL PER MM 27-48-00-5.
INSPECTION TYPE:C-2 CORROSION ON SEAT TRACK AT NUTPLATE BS 1075, RBL 24, WL 208. REPAIRED SEAT TRACK IAW ATS EO NR 08-1354 AND UPS EO NR B757-5310-28743-A.
INSPECTION TYPE:C-2 LW LWR SKIN T/E CHAFED IB AND OB OF NR 1 FLAP TRACK. REPAIRED LT WING LWR SKIN IAW ATS ER 08-1340.
INSPECTION TYPE:C-2 MAIN DECK FLOORBEAM UPPER CHORD FWD FLANGE, NUT PLATE HOLES HAS CORROSION, BS 1200, LBL 55-RBL 55. REPAIRED FLOORBEAM UPPER CHORD FWD FLANGE IAW ATS ER NR 08-1351 AND UPS EO B757-5310-28698-A.
INSPECTION TYPE:C2 MAIN CARGO COMPARTMENT FLOOR PANEL DENTED BS 1488 RBL 55 WL 208. REMOVED DAMAGED FLOOR PANEL, FABRICATED REPLACEMENT PANEL. INSTALLED REPLACEMENT PANEL PER B757-5320-9692-F M/M 25-55-04-4.
INSPECTION TYPE:C2 MAIN CARGO COMPARTMENT FLOOR PANEL DENTED AT BS 1488 RBL 42 WL 208. REMOVED DAMAGED FLOOR PANEL, FABRICATED REPLACEMENT PANEL. INSTALLED REPLACEMENT PANEL PER B757-5320-9692F M/M 25-55-04-4.
INSPECTION TYPE:C2 CORROSION ON SEAT TRACK UPPER SURFACE BS 1181-1175 LBL 60 WL 208. CORROSION OUT OF LIMITS PER SRM 53-00-52-1A; REMOVED AND REPLACED TRACK.
CAPT SIDE EMERGENCY ESCAPE ROPE ACCESS DOOR WILL NOT STAY IN PLACE. REPLACED BROKEN LATCH ON UPPER LT SIDE PANEL. CAPT'S EMERGENCY ESCAPE ROPE ACCESS DOOR NOW SECURED.
INSPECTION TYPE:N/A R-3 WINDOW CRACKED & ARCING. REMOVED AND REPLACED RIGHT WINDOW NR 3 PER MM 56-11-10-4. FIRST TORQUE AND SEALANT APPLIED.
ON SHORT FINAL, RT WINDSHIELD WIPER FROZE 30 SECS AFTER SMELLED ELECTRICAL SMOKE. TURNED OFF WIPERS ODOR DISSIPATED. ALSO WHILE ON GND LT PACK WAS MAKING A LOUD NOISE. OPERATED THE WINDSHIELD WIPER SYSTEM ON THE GND. SYS CKD NORMAL. LT PACK CONTROLLER BITE DID NOT PASS. LT PACK INOP LIGHT ON OVHD PANEL ILLUMINATED. DEFERRED LT PACK INOP PER MEL 21-51-1 CTRL NR M324970. REMOVED AND REPLACED LT ACM PER MM 21-51-03-4. THIS CLEARS DEFERRAL 324970.
COMPARTMENT TEMPS 99/85/85 AND ARE UNCONTROLLABLE IN AUTO OR MANUAL MODES. REMOVED AND REPLACED TRIM AIR PRESSURE REGULATING VALVE PER MM 21-61-06-4 AND REMOVED AND REPLACED ZONE TEMP CONTROLLER PER MM 21-61-03-4. OPS CK'D 45 MINS, OPS NORMAL.
NR 2 APPROXIMATELY 20 MINUTES AFTER DEPARTURE, CREW REPORTED UNABLE TO CONTROL THE CABIN OR CARGO TEMP. INDICATED C/P TEMP WAS ABOVE 90 DEGREES. LT PACK INOP. DEFERRED M324970. C/W LT PACK TEMP CONTROL BITE, REMOVED AND REPLACED MIX MANIFOLD SENSOR, NO HELP. FOUND AIR CYCLE MACHINE CEASED. REMOVED AND REPLACED LT ACM ON LP #394627.
SMOKE GOGGLES ON CAPT'S SIDE ARE DEFECTIVE. REPLACED DAMAGED SMOKE GOGGLES W/ NEW IN REF TO MM CH 25-00.
DEMO LIFE VEST CONTAMINATED WITH LAV WATER. REMOVED AND REPLACED DEMO LIFE VEST.
EMERGENCY EXIT UNARMED LIGHT INOP. RELAMPED, OPS NORMAL.
INSPECTION TYPE-N/A, LEFT GEN FAILED. EICAS MSG L GEN DRIVE DISPLAYED. GEN DRIVE LIGHT ILLUM. GEN DRIVE DISCONECTED, RIGHT GEN WAS DEFERRED. FOUND FILTER BYPASS POPPED AND METAL CHIPS IN FILTER. REPLACED LT IDG (P/N 727792K), (S/N A1120) OFF, (S/N A1004) ON. SEE ITEM 3 FOR POSSIBLE OIL COOLER CONTAMINATION. WORK PER MM 24-11-01, OPS CHECKS GOOD PER MM 24-11-00.