N556NW
Registered owner: DELTA AIR LINES INC, GA (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
3L DOOR NOT ARMING PROPERLY. ADJUSTED KNUCKLE KNOCKER ON L3 DOOR. DOOR ARMS NORMAL. (880476) AIRCRAFT WAS GROUNDED.
DURING FCF "L WING SLIDE" ON EICAS AND "EMER DOOR" ON ANNUNCIATOR PANEL. FOUND L OVEWRWING SLIDE DOOR OPEN UPON ARRIVAL AND SLIDE DOOR WAS CLOSED CORRECTLY PER B-757-200 AMM 25-65-00. (8560620)
CORROSION ON INTERNAL DOUBLER OF TRAY SERVICE WASTE BTW STA 418 TO STA 440 AND STGR 29L TO STGR 29R AT E/E COMPARMENT. CORROSION LEVEL 2. INTERNAL DOUBLER OF TRAY SERVICE WASTE BTW STA 418 TO STA 440 AND STGR 29L TO STGR 29R AT E/E COMPARTMENT WAS REPLACED PER B757-200 SRM 51-40-02-0G PAR. 4 AND 7. (1504672)
AFTER AFT WASTE PANEL REMOVAL, CORROSION ON FUSELAGE SKIN OF SETTLEMENT AREA OF AFT WASTE PANEL WAS FOUND. CORROSION LEVEL 2 ON FUSELAGE SKIN OF SETTLEMENT AREA OF AFT WASTE PANEL WAS REPAIRED PER ER/A-632886- 14AD REV. ORIGINAL. (1505433)
FUSELAGE SKIN, AFT LAV SERVICE PANEL CUTOUT, BS 1676 - 1705, S26R TO S29R, CORROSION. MONITOR INSPECTION LOG REPAIR TO FUSELAGE SKIN BETWEEN STA 1681-1701 & S26-29R. REF ERA 632886-14AD.
AFTER AFT WASTE PANEL REMOVAL, CRACKS ( 2EAS) ON REINFORCED DOUBLER AT REAR SIDE WASTE PANEL OF AFT WASTE PANEL WERE FOUND ALSO CRACKS (2EAS) ON EXTERIOR SIDE OF WASTE PANEL OF AFT WASTE PANEL WERE FOUND. AFT LAVATORY SERVICE PAN WAS REPAIRED PER PRI 632865-14 REV. 0 TO REV 2. AND ERA 632865-14 REV. ORIGINAL SECTION I: TIME LIMITED REPAIR. (1502401)
REPAIR TO FUSELAGE AFT LAVATORY SERVICE PAN AT STA 1681-1701 AND S27R - 29R CRACKED. REQUIRES ACTIONS PER ERA 632865-14 REV ORIG. REF ERA 632865-14. (1502037)
AFT LEAF SPRING DOES NOT RETAIN THE SLIDER AND SLIDER RIDES OVER THE SPRING AT GIRT BART R1 DOOR IN REF AMDS 2561- 01257-01B. GIRT BART R1 DOOR WAS REPLACED AND VERIFIED PER B757-200 AIPC 25-66-05-05 ITEM 112W WHIT NEW GIRT BAR AND GIRT BAR TEST WAS PERFORMED UNDER AMDS 2561-01257-01B FROM STEP 10. TO STEP 14. TEST OK. (1493250) (AIRCRAFT GROUNDED)
CRACK WAS FOUND OF 0.203IN LENGTH APPROX ON THE STA 1640 FUSELAGE FRAME INNER-CHORD FWD RETURN FLANGE RADIUS, LOCATED 0.500IN BELOW THE FASTENER HOLE AT S-14L, IN REF CARD 5311-01218-01A JOB # 106-0001, STEP 7. FRAME ON STA 1640 BETWEEN STRG 9LH AND STRG 20LH WAS REPAIRED PER PRI 632412-14 REV. 0 TO 2 AND ER/A- 632412-14AD REV. ORIGINAL SECTION I : PERMANENT REPAIR. (1493045) (AIRCRAFT GROUNDED)
DTA MONITOR INSPECTION LOG REF ERA 632412-14, FUSELAGE FRAME, LT BS 1640 INNER CHORD AT S-14L CRACK. REF ERA 632412-14AD. (1491247)
SHIP 5656 CORROSION ON SEAT TRACKS IN RBL= 25, RBL= 45 AND BTW STA 364 TO STA 377 AT FWD GALLEY AREA (W1). CORRECTIVE ACTION: SUMMARY OF NRC 00368, CORROSION LEVEL 2: SEAT TRACKS IN RBL= 25, RBL= 45 AND BTW STA 364 TO STA 377 AT FWD GALLEY AREA WAS REPLACED PER B757-200 SRM 51-40-02-0G. (1482751)
SHIP 5656 BROKEN STABILIZER STRAP ON STA 377.7 TO LBL 45.5 AT E&E BAY. CORRECTIVE ACTION: SUMMARY OF NRC 00190: STABILIZER STRAP ON STA 377.7 TO LBL 45.5 AT E&E BAY WAS REPAIRED PER B757-200 SRM 53-00-51-2R PROCEDURE 12 REPAIR 12. (1481171)
SHIP 5656 CORROSION ON PLATE AT STA 685, RBL 50 AT PAX CABIN ( IT IS OUT OF LIMITS). CORRECTIVE ACTION: SUMMARY OF NRC 00547, CORROSION LEVEL 2, PLATE AT STA 685, RBL 50 AT PAX CABIN, WAS REPLACED PER B757-200 SRM 51-40-02-0G PAR. 7.D. (1481101)
CORROSION ON FLOOR ANGLE AT STA 758, LBL 62 AT PAX CABIN ( IT IS OUT OF LIMITS ). CORROSION LEVEL 2, FLOOR ANGLE AT STA 758, LBL 62 AT PAX CABIN AT PAX CABIN WAS REPAIRED PER B757-200 SRM 53-00-13-2R-2 REPAIR 2. (1478009)
SHIP 5656 ROTATORY SNUBBER OUT LIMITS ON TORQUE TUBE OF PASSENGER DOOR L2. CORRECTIVE ACTION: SUMMARY OF NRC 00063: ROTATORY SNUBBER ON TORQUE TUBE OF PASSENGER DOOR L2 WAS REPLACED PER B757-200 AMM 52-11-10. (1478891)
OUT OF LIMITS PIN EXTENSION ON ROTARY SNUBBER AT 4 RH DOOR. THE ROTARY SNUBBER WAS REMOVED PER AMM 52-11-10 AND INSTALL SERVICEABLE ROTARY SNUBBER UNDER AMDS 5211-6005-4R. (1477637)
CORROSION ON BEAM STA 1640 AND BTW LBL=58 TO RBL=24 AT AFT GALLEY AREA (W4) THEREFORE IT' IS OUT OF LIMITS. (1471342)
SHIP 5656 A.A. - A.D. DISBOND (1.0IN X 1.0IN) AT OSS 486.1 AT UPPER SURFACE, LE SLAT #8 TRAILING EDGE WEDGE, RH WING. CORRECTIVE ACTION: SUMMARY OF NRC 00023: OSS 486.1 AT UPPER SURFACE, LE SLAT #8 TRAILING EDGE WEDGE, RH WING WAS REPAIRED PER B757-200 SRM 51-70 -10-2R PROCEDURE REPAIR GENERAL IN REFERENCE TO B757-200 SRM 57- 43-02-2R PROCEDURE 1 REPAIR 1. (1467861)
FOUND ENTRANCE DOOR EXIT SIGN LIGHT INOP. REPLACED BATTERY PACK REF. B757 AMM 33-51. (LP 7275678)
DOOR 1L SLIDE RESERVOIR PRESSURE LOW. REPLACED 1L DOOR SLIDE PER W/C 2566-9001-1L.
SHIP 5656 -DIV/DE- TO ATL DUE TO TAT PROBE MESSAGE. CORRECTIVE ACTION: REPLACED TAT PROBE CURRENT SENSE RELAY K410.
SHIP 5656 -MISC/DE- LOSS OF LEFT HYDRAULIC QUANTITY AND PRESSURE AFTER GEAR EXTENSION. CORRECTIVE ACTION: REPLACED LEFT GEAR DOWNLOCK ACTUATOR RETURN LINE.
SHIP 5656 SEAT 1 FWD EEPLS INOP. CORRECTIVE ACTION: FOUND DAMAGED WIRE BENEATH SEAT 1C. REPAIRED WIRE IAW B757 SWPM 20-10. OPS CK GOOD. (6464750)
SHIP 5656 DAMAGE AT L2 DOOR (FUSELAGE STA. 640 / STR. 18L TO 20L / DENT & GOUGE. CORRECTIVE ACTION: REF NR 001 ON WP # 706300 20AUG24. CW ERA 619917-14AD. (0487582)
SHIP 5656 **DTE REQUIRED**, ERA 619917-14, STA 640 / STR18L & STR 20L / DENT AND GOUGES MONITOR INSPECTION LOG REPAIR TO FUSELAGE FRAME AT STA 640 BETWEEN S-18L & S-20L. CORRECTIVE ACTION: REF ERA 619917-14. (0486260)
OUT OF LIMIT SNUBBER PIN LENGHT AT 1R PASSENGER DOOR. SUMMARY OF NRC 00103: DAMAGED ROTARY SNUBBER AT 1R PASSENGER DOOR WAS REPLACED FOR A SERVICEABLE ROTARY SNUBBER PER B757-200 AMM 52- 11-10. (0269986)
SHIP 5656 CORROSION ON INTERNAL SKIN STA 1790 BTW STRINGER 3R/S4R AT AFT ACCESORY COMPARTMENT. CORRECTIVE ACTION: SUMMARY OF NRC 00118: STRAP ON INTERNAL SKIN STA 1790 BTW STRINGER 3R/S4R AT AFT ACCESSORY COMPARTMENT WAS REPLACED PER B757-200 SRM. (0267884)
SHIP 5656 CRACKED STABILIZATION STRAP AT BTW STA 350, 370 AND 400 LBL 25 AT E/E COMPARTMENT. CORRECTIVE ACTION: SUMMARY OF NRC 00084: STABILIZATION STRAP AT BTW STA 350, 370 AND 400 LBL 25 AT E/E COMPARTMENT. (E/E) WAS REPAIRED PER B757- 200 SRM. (0265780)
SHIP 5656 OUT OF LIMIT SNUBBER PIN LENGHT AT 1L PASSENGER DOOR. CORRECTIVE ACTION: SUMMARY OF NRC 00102: ROTARY SNUBBER AT 1L PASSENGER DOOR WAS REMOVED AND REPAIRED ROTARY SNUBBER AT L1 PASSENGER DOOR WAS INSTALLED PER B757-200 AMM 52-11-10. (0265003)
SHIP 5656 F/O FWD WINDSHIELD APPEARS O BE DEFORMED. BURNT ON MAJORITY OF LOWER SECTION. CORRECTIVE ACTION: RMVD & REPL NO. 1 RT WINDSHIELD REF B757 AMM 56- 11. REMOVED & REPL. RT SIDE WINDOW HEAT CONT. REF B757 AMM 30-41. (5755800)
SHIP 5656 -MISC/DE- DUE TO LT HYD QTY DECREASE DURING FLIGHT. C/W QRH AND LANDED AND TAXIED IN NORMALLY. CORRECTIVE ACTION: LOCATED LEAK IN LT PYLON. REPLACED PACKINGS AT DPI OF THE LT EDP FILTER MODULE AND SERVICED HYD SYS.
SHIP 5656 -ATB/PRES- DUE TO CABIN ALTITUDE WARNING WITH HIGH CABIN ALTITUDE. CORRECTIVE ACTION: REPLACED CABIN PRESSURE CONTROLLER, CONTROL PANEL AND OUTFLOW VALVE.
SHIP 5656 EXIT SIGN IN CIELING ABOVE EMERGENCY EXIT 10W KNOCKED DOWN BY PASSENGER. CORRECTIVE ACTION: REINSTALLED & OPS CHECK GOOD. (4639206)
SHIP 5656 ISLE OVERHEAD EXIT COVER FELL OFF. ROW 26. CORRECTIVE ACTION: RESECURED EXIT SIGN COVER. OPS CHECKS NO FURTHER DAMAGE NOTED. (9372354)
SHIP 5656 PLASTIC "EXIT" SIGN DETACHED FROM EXIT ROW. CORRECTIVE ACTION: SECURED "EXIT" SIGN COVER. (8655680)
SHIP 5656 4RR DOOR ASSIST BOTTLE LOW PRESSURE. CORRECTIVE ACTION: REPLACED 4R DOOR ASSIST BOTTLE PER B757 AMM 52-11. OPS CHECK GOOD.
SHIP 5656 - MISC/DE - ON APPROACH DUE TO T/E FLAP DISAGREE MSG WHEN GOING FROM 20 TO 2. CORRECTIVE ACTION: BITE ALL FSEUS. FOUND FAULT ON FSEU 1. T/S PER ASSOCIATED FIM AND NTF. C/W NO GO PROCEDURES.
SHIP 5656 DOOR ARMED KNUCKLE KNOCKER INOPERATIVE / LOCATIONS: 1R. CORRECTIVE ACTION: RESEALED 1R DOOR ARMED KNUCKLE KNOCKER PLACARD.OPS CHECK NORMAL. (2208826)
SHIP 5656 "WING SLIDE" APPEARED IMMEDIATELY AFTER TAKEOFF. VISUALLY CONFIRMED NO SLIDE DEPLOYMENT. CORRECTIVE ACTION: FOUND LEFT WING SLIDE COMPARTMENT DOOR UNLATCHED; CLOSED AND LATCHED DOOR PER B757 AMM 25-65-09. (8250538)
SHIP 5656 L4 DOOR SNUBBER REQUIRES SERVICING. CORRECTIVE ACTION: REMOVED AND REPLACED L4 DOOR SNUBBER IAW B-757 AMM 52-11-10. (2196117)
SHIP 5656 EMERGENCY EXIT SIGN 2R DOOR FELL OFF. CORRECTIVE ACTION: REINSTALLED R2 DOOR EXIT SIGN COVER PER B757 AMM 33-51. (8602854)
SHIP 5656 EXIT SIGN LOOSE AT R2 DOOR. CORRECTIVE ACTION: SECURED EXIT SIGN. (8602856)
SHIP 5656 2R DOOR EMERGENCY EXIT SIGN FELL OFF ON LANDING. CORRECTIVE ACTION: REMOVED AND REPLACED EMERGENCY EXIT LENS PER B757 AMM 33-51. (8602844)
SHIP 5656 AFT LH DOOR EXTERIOR HANDLE RELEASE BUTTON IS BROKEN (BUTTERFLY HANDLE). CORRECTIVE ACTION: REPLACED BROKEN SPRING ON AFT LH DOOR BUTTERFLY HANDLE. OPS CK GOOD. (8602823)
SHIP 5656 CEILING LIGHT COVER FELL OFF MID CABIN. CORRECTIVE ACTION: LIGHT COVER CAME FROM OVERHEAD AISLE EMERGENCY LIGHT LOCATED JUST AFT OF MID LAV. RESECURED LIGHT COVER AND LIGHT ASSY. (7529918)
SHIP 5656 LT WING SLIDE EICAS MESSAGE AND EMER DOOR LIGHT. CORRECTIVE ACTION: FOUND SLIDE COMPARTMENT DOOR NOT PROPERLY SECURED.RE-SECURED DOOR AND VERIFIED THAT ROUND CRANK HANDLE IS IN THE LOCKED POSITION. REF WORK -CARD. (7942132)
SHIP 5656 4R GIRTBAR FWD LEAF SPRING FAILED. CORRECTIVE ACTION: SUMMARY SEE NR FOR ADDITIONAL INFORMATION 021-0001:2561-01257-01F/001 00004 REPLACED GIRT BAR ASSY REF B757AMM 25-66. (1847102)
SHIP 5656 REPAIR TO RH WING UPPER SKIN COMMON TO DRAG FITTING ATTACHMENT REQUIRES SUPPLEMENTAL INSPECTIONS PER ERA 585711-14 REV A. CORRECTIVE ACTION: REF ERA 585711-14 UPDATED TO REV. B. (1799137)
SHIP 5656 ON S/C FOUND EMER LIGHTS INOP SEAT ROWS 27-32DEF. CORRECTIVE ACTION: REMOVED & REPLACED BATTERY PACK & CHARGER ASSY REF B757 AMM 33-51 CKS GOOD. (4268888)
SHIP 5656 FOUND SEATS 23-26 EMERGENCY LIGHTS INOP. CORRECTIVE ACTION: ISOLATE TO M10567.R/R BATTERYPACK REF 757 AMM 33-51. (4268880)
SHIP 5656 ON T.O ROLL 100 KTS "L WING SLIDE" CAUTION MSG. UPON POST FLT INSPECTION LEFT OVER WING , SLIDE DOOR OPEN WITH SLIDE INSIDE. CORRECTIVE ACTION: LH FWD LATCH FITTING STUD ON SLIDE COMPARTMENT DOOR WAS ADJUSTED AND DOOR WAS CLOSED PER B757-200 AMM 25-65. (6895952)
SHIP 5656 INITIAL INSPECTION : DISBONDING ON INNER SKIN OF LE PANEL HOR. STAB. RH, SEGMENT # 342BR. CORRECTIVE ACTION: SUMMARY OF NRC S/N 00101: DAMAGE AREA WAS REPAIRED PER ER/A 585689-14 REV. ORIGINAL SECTION I. (1520263)
(AIRCRAFT 5656, L/P 1516402) DENTS ON UPPER SURFACE AT O/B MAIN FLAP APPROX FROM WS 476/488 AT LH WING. CORRECTIVE ACTION: REPAIRED PER B-757-200 S.R.M. 51-70-07-0G PAR.5.A. ON REFERENCE OF B-757-200 S.R.M. 57-53-01-2R-1 DETAIL III TABLE III. AND PERFORM DECAL CONDITION EVERY "L" CHECK SERVICE PER TOPP 30-10-70 PAGE14. PAR. I.
(AIRCRAFT 5656, L/P 1516474) LOOSE FASTENER NBR 1, 2, 3, 6, 7, 8, 9 AND 10 BY CRACKED PAINT ALL THE WAY AROUND THE FASTENER HEAD AT RH WING UPPER SKIN DRAG FITTING. CORRECTIVE ACTION: RH WING UPPER SKIN DRAG WERE REPLACED PER AMDS 5720-01100-0101B AND FASTENER NBR 4,6,10 WERE REPLACED PER ETI-57-20-041 REV. 3. ERA 585711-14AD REV.ORIGINAL AND PERFORM DAMAGE TOLERANCE EVALUATION.
(AIRCRAFT 5656, L/P 1515122) OUT OF LIMITS DENTS 12, 16 , 24, 25 AND 31 ON SLAT #6. CORRECTIVE ACTION: REPAIRED PER B-757-200 SRM 51-70-01-2R-1 ON REFERENCE OF B-757-200 S.R.M. 57-43-02-1A-1 NOTE J. AND PERFORM DECAL CONDITION INSPECTION EVERY L CHECK PER TOPP MANUAL 30-10-70 PAR. I PAGE. 14.
(AIRCRAFT 5656, L/P 1515039) DENTS OUT OF LIMITS (08 EA) ON UPPER SURFACE WEDGE AREA AT SLAT # 10. RH WING. CORRECTIVE ACTION: REPAIRED PER B-757-200 S.R.M. 51-70-01-2R-1 ON REFERENCE OF B-757-200 S.R.M. 57-43-02-1A-1 FIGURE 101 NOTE J.PERFORM DECAL CONDITION EVERY CHECK "L" SERVICE PER TOPP 30-10-70 PAGE 14,PAR. I.
(AIRCRAFT 5656, L/P 1513389) CORROSION ON SIDE PANEL BTW STA Y=1480-1640 LH AND STA Y=1480-1590 RH OF FLOOR STRUCTURE. AT AFT CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED PER B757-200 SRM 51-40-02-0G PAR 4 AND 7.
(AIRCRAFT 5656, L/P 1513890) LOOSE FASTENER NBR 13, 14, 15, AND 18 BY CRACKED PAINT ALL THE WAY AROUND THE FASTENER HEAD AT RH WING UPPER SKIN DRAG FITTING (IN REF AMDS 5720-01100-0101B STEP 13). CORRECTIVE ACTION: REPLACED PER ETI-57-20-041 REV. 3 AND ER/A: 585711-14AD REV . ORIGINAL SECTION I PERMANENT REPAIR. IN ACCORDANCE TO TIME OF ACCOMPLISHMENT: REPAIR APPROVAL IS LIMITED TO 24 MONTHS SERVICE ONLY TO FEB.26, OR 23,823 TOTAL AIRFRAME FLIGHT CYCLES, WHICHEVER OCCURS FIRST.
(AIRCRAFT 5656, L/P 1510844) DENTS OUT OF LIMITS (07 EA) ON UPPER SURFACE WEDGE AREA AT SLAT #2. LH WING (AI). CORRECTIVE ACTION: REPAIRED PER B-757-200 S.R.M. 51-70-01-2R-1 PAR. 4. B. AND PAR. 4. D.N ON REFERENCE OF B-757-200 S.R.M. 57-43-02-1A-1 FIGURE 101. AND PERFORM DECAL CONDITION INSPECTION EVERY L CHECK PER TOPP MANUAL 30-10-70. I PAGE 14.
(AIRCRAFT 5656, L/P 1510702) IN REFERENCE NRC # 0116, DENTS OUT OF LIMITS (06 EA) ON UPPER SURFACE WEDGE AREA AT SLAT # 4. LH WING (AI). CORRECTIVE ACTION: REPAIRED PER B-757-200 S.R.M. 51-70-01-2R-1 PAR. 4. B. AND PAR. 4. D.N ON REFERENCE OF B-757-200 S.R.M. 57-43-02-1A-1 FIGURE 101.
(AIRCRAFT 5656, L/P 1509688) SEVERAL DENTS AND DELAMINATION ON FLOOR PANEL NBR 250-26; 250-28; 250-30 AND 250-31 AT PAX CABIN. CORRECTIVE ACTION: FLOOR PANELS REPLACED AND IDENTIFIED PER B757-200 AMM 53-01-01-201.
(AIRCRAFT 5656, L/P 1510875) IN REFERENCE NRC # 0181 ,DENT OUT OF LIMITS (01 EA) ON UPPER SURFACE WEDGE AREA AT SLAT #8. RH WING. CORRECTIVE ACTION: REPAIRED PER B757-200 S.R.M. 51-70-01-2R-1 PAR. 4. B. AND PAR. 4. D.N ON REFERENCE OF B-757-200 S.R.M. 57-43-02-1A-1 FIGURE 101. PERFORM DECAL CONDITION INSPECTION EVERY L CHECK PER TOPP MANUAL 30-10-70. I PAGE 14.
(AIRCRAFT 5656, L/P 1510921) IN REFERENCE NRC # 0182, DENTS OUT OF LIMITS (06 EA) ON UPPER SURFACE WEDGE AREA AT SLAT # 9. RH WING (AD). CORRECTIVE ACTION: REPAIRED PER B-757-200 S.R.M. 51-70-01-2R-1 PAR. 4. . B. AND PAR. 4. D.N ON REFERENCE OF B-757-200 S.R.M. 57-43-02-1A-1 FIGURE 101. AND PERFORM DECAL CONDITION INSPECTION EVERY L CHECK PER TOPP MANUAL 30-10-70. I PAGE 14.
(AIRCRAFT 5656, L/P 1510696) DENTS OUT OF LIMITS (07 EA) ON UPPER SURFACE WEDGE AREA AT SLAT # 1. LH WING (AI). CORRECTIVE ACTION: REPAIRED PER B-757-200 S.R.M. 51-70-01-2R-1 PAR. 4. B. AND PAR. 4. D.N ON REFERENCE OF B-757-200 S.R.M. 57-43-02-1A-1 FIGURE 101.
(AIRCRAFT 5656, L/P 1510856) DENTS OUT OF LIMITS (05 EA) ON UPPER SURFACE WEDGE AREA AT SLAT # 7.RH WING. CORRECTIVE ACTION: REPAIRED PER B-757-200 S.R.M. 51-70-01-2R-1 PAR. 4. B. AND PAR. 4. D.N ON REFERENCE OF B-757-200 S.R.M. 57-43-02-1A-1 FIGURE 101. AND PERFORM DECAL CONDITION INSPECTION EVERY L CHECK PER TOPP MANUAL 30-10-70. I PAGE 14.
(AIRCRAFT 5656, L/P 1505438) CORROSION ON SPLICE REPAIR OF STRINGER RH, STA Y=1469 AT FLOOR STRUCTURE. AFT CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED PER B757-200 SRM 53-00-53-2R-1 REPAIR 1.
(AIRCRAFT 5656, L/P 1505466) STRINGER OF FLOOR SUPPORT (LBL 2.90) AT STA 1510 OUT OF LIMITS BY CORROSION. AFT COMP. CARGO. CORRECTIVE ACTION: REPAIRED PER B757-200 SRM 53-00-53-2R-1 REPAIR 1.
(AIRCRAFT 5656, L/P 1505253) CORROSION ON SPLICE REPAIR OF STRINGER RH ON STA Y=1510. AT AFT CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED PER B757-200 SRM 53-00-53-2R-1 REPAIR 1.
(AIRCRAFT 5656, L/P 1505271) CRACKED ANGLE SUPPORT ON STA 1300 BTW STR 26LH AND 25LH AT WING TO BODY FUSELAGE AREA. CORRETIVE ACTION: REPAIRED PER B757-200 SRM 53-60-71-2R-1.
(AIRCRAFT 5656, L/P 1506066) CRACK ON INTERCOSTAL BTW STA 660 AND 680, S-12R AT PAX CABIN. CORRECTIVE ACTION: REPLACED PER B757-200 SRM 51-40-02-0G PAR 4 AND PAR. 7.
(AIRCRAFT 5656, L/P 1505439) CORROSION ON STRINGERS LH AND RH ,STA Y=1329.5 AND STA Y=1469 LH, AT FLOOR STRUCTURE. AFT CARGO COMPARTMENT. CORRECTIVE ACTION: REPAIRED PER B757-200 SRM 53-00-53-2R-1 REPAIR 1.
(AIRCRAFT 5656, L/P 1505007) CORROSION ON FLOOR ANGLE FROM STA 1010 TO 1040 RBL 64 AT WING BOX. AMDS 2020-2396. CORRECTIVE ACTION: REPLACED PER B757-200 SRM 51-40-02-0G PAR 4 AND 7.
(AIRCRAFT 5656, L/P 1504651) CORROSION SETTLEMENT AREAS ON FLOOR ANGLE FROM STA 984 TO 1040 LBL 64 AT WING BOX. CORRECTIVE ACTION: REPLACED PER B757-200 SRM 51-40-02-0G PAR.4 AND 7.
(AIRCRAFT 5656, L/P 1501229) CRACK ON CEILING SUPPORT STA 1661, 26 RBL AT AFT CARGO COMPARTMENT CEILING STRUCTURE. CORRECTIVE ACTION: REPAIRED PER ER/A 384483-14 MA REV D AND B757-200 SRM 51-40-02-0G PAR. 4B.
(AIRCRAFT 5656, L/P 1500677) CORROSION LEVEL 2 ON FLOOR SUPPORT BTW STA 1670 TO 1681 RBL 55 AND LBL 55 AT PAX CABIN FLOOR STRUCTURE. CORRECTIVE ACTION: REPLACED PER B757-200 SRM 51-40-02 PAR 7.
SHIP 5656 CORROSION ON L2 LOWER SILL INTERCOSTAL BTW STA 720/740 AND 63 LBL PASSENGER CABIN (W2) LOG-PAGE UPDATED SUMMARY OF NRC 00359 CORROSION LEVEL 2 LOWER SILL BTW STA 720/ 740, 63 LBL WAS REPLACED PER B757-200 SRM 51-40-02-0G PAR 4 AND 7 (1499637)
(AIRCRAFT 5656, L/P 1497222) THICKNNESS DECK PLATE FROM STA 1681 TO 1720 IS .071" AND REMAINING THICKNESS ON STA 1681 LBL 27 TO LBL 1 IS .056" THEREFORE THIS AREAS ARE OUT OF LIMITS PER B-757-200 SRM 53-60-51-2R-2 FIG. 201 STEP 5.A. CORRECTIVE ACTION: REPAIRED PER B757-200 SRM 53-60-51-2R-2 ALTERNATIVE I.
(AIRCRAFT 5656, L/P 1495720) CRACK ON STRINGER LH,STA Y=1398 AT FLOOR STRUCTURE. AFT CARGO COMPARTMENT. CORRECTIVE ACTION: REPAIRED PER B757-200 SRM 53-00-53-2R-1.
(AIRCRAFT 5656, L/P 1495181) CRACK ON FLOOR SUPPORT BTW STA 345/365 AND 25 RBL FLOOR STRUCTURE. CORRECTIVE ACTION: REPLACED PER B757-200 SRM 51-40-02-0G PAR. 4 AND PAR. 7.
DOOR ARMED KNUCKLE KNOCKER INOPERATIVE. LUBED ARMING LEVER HINGED COVER.
(AIRCRAFT 5656, L/P 6293921) 1R DOOR KNUCKLE KNOCKER NOT FULLY EXTENDED WITH DOOR ARMED. FOUND KNUCKLE BUSTER BOX ASSY OUT OF ADJUSTMENT WITH DECORATIVE TRIM. ADJUSTED BOX ASSY PER AMM 52-11-20.
SHIP 5656 REPAIR AFT CARGO RT SIDEWALK STA 1350 -1470 REF SRM. CORRECTIVE ACTION: REPAIRED AFT CARGO RT SIDEWALK STA 1350 -1470 REF SRM. (1248441)
SHIP 5656 R1 DOOR GIRT BAR, FAILED ENGAGMENT CHECK AT FORWARD FLOOR FITTING. CORRECTIVE ACTION: SUMMARY SEE NR FOR ADDITIONAL INFORMATION 014-0001:2561-01257-01B/002 00275 REMOVED AND REPLACED GIRT BAR REF AMM 25-66. (1248816)
SHIP 5656 MULTIPLE AREAS OF CORROSION STA 1435-1450 AFT CARGO LT SIDEWALK. CORRECTIVE ACTION: SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0262:2020-2366-AF/009 00263 REWORKED AREA PER ERA 580907-14 REV. ORIGINAL. (1246853)
SHIP 5656 MULTIPLE AREAS OF CORROSION STA 1360-1380 AFT CARGO LT SIDEWALK. CORRECTIVE ACTION: C/W ERA 580907-14 REV ORIG. (1246842)
R4 DOOR LOWER GUIDE ARM ROD END AT DOOR WORN "M". CHECK LIMITS AND REPLACED GUIDE ARM ROD END IAW AMM 52-11-04, AND AMDS 2040-0191-4R. DID AN OPS CKECK AND IT CHECKED OK.
4L DOOR SLIDE, UPPER FWD PARACHUTE PIN LACING CORD BROKEN. REMOVED AND REPLACED LACING PER ZODIAC AEROSPACE EVACUATION SYSTEMS CMM 25-61-28 FIGURE 717.
AILERON TRIM ACTUATOR BEARING FAILS ROTATION CHECK. REMOVED AND REPLACED AILERON TRIM ACTUATOR REF B757 AMM 27-11-14. OPS CHECK OK.
SHIP 5656- ATB - DUE TO UNRELIABLE AIRSPEED AFTER T/O CAPT./STBY/FO (AIRSPEED). INVESTIGATION REVEALS WASP/BEE LODGED IN BOTH CAPT. AND FO PITOT PROBES. R/R CAPT. AND FO PITOT PROBES. PURGED AUX 1, FO AND CAPT. PITOT LINES. PERFORMED AOA SENSOR TEST, ALL READINGS GOOD AND SMOOTH DURING MOVEMENT. REPLACED RT ADC AND PERFORMED TEST 30 PITOT STATIC LEAK AND OPS TEST. ALL INDICATIONS NORMAL.
DIVERTED DUE TO UNRELIABLE CAPTAIN, F/O & STBY AIRSPEED. PERFORMED PITOT SYSTEM TEST. REPLACED LT ADC & CAPTAIN'S ASI. OK FOR SERVICE.
R2 EXIT SIGN FELL OFF. SECURED, NOW OK FOR SVC.
EMERGENCY LIGHT CAME OFF OF SEAT 18D. REPLACED THE LIGHT ASSY AT 18D IAW AMM 33-51.
SHIP 5656 LT FWD AND AFT OVERWING EMERGENCY EXIT LIGHTS INOP. CORRECTIVE ACTION: REPLACED FUSE ON EMERGENCY LIGHT POWER SUPPLY. (6015067)
NR 1 ENGINE PYLON LOWER SKATE ANGLE SUPPORT CRACKED. REMOVED DAMAGED ANGLE ANDINSTALLED NEW ANGLE. REF: B757 SRM 54-51-02.
SHIP 5656 DOOR ARMED KNUCKLE KNOCKER INOPERATIVE / LOCATIONS: 1R / SLIDE LIGHT IS OFF WDOOR ARMED 1R. CORRECTIVE ACTION: OPS CHECKS NML REF AMM 25-61. (0958031)
SHIP 5656 ON TKOFF GOT "EMERG DOORS" DISCRETE LT@:LT WING SLIDE" EICAS LTS ILLUMINATED ENTIRE FLIGHT. PRESSURIZATION NORMAL ENTIRE FLT. FLT ATTENDANT VISUALLY SCAN FROM CABIN .NO INDICATION DOOR OPEN/SLIDE DEPLOYED LIKE PREVIOUS FLT LT ILLUMINATING - 100 KN GNTK. CORRECTIVE ACTION: OPENED AFT BB FWD BULKHEAD PANEL. PINNED AND CAPPED LT OVERWING SLIDE BOTTLE. R/R LT DOOR LATCH TUBE AND AFT DOOR LATCH FITTING PER AMM 25-65. REACTIVATED LT DOOR SLIDE PER AMM 25-65. RII INSPECTION COMPLIED WITH- VERIFY SLIDE BOTTLE PIN REMOVED QC CLOSED B/B PNL. LT WING ESCAPE SLIDE DOOR CKS GOOD. (5233456)
SHIP 5656 ON TAEKOFF ROLL GOT "EMERG DOORS" DISCRETE LIGHT OVHD PANEL AND "LT WING SLIDE " EICAS. LTS STAYED ILLUMINATED FOR REMAINDER OF FLIGHT, PRESSURIZATION NORMAL ENTIRE FLIGHT, FLT ATTENDANT VISUALLY SCAN FROM CABIN, NO INDICATION DOOR OPEN / SLIDE DEPLOYED. CORRECTIVE ACTION: VERIFIED SECURITY OF SLIDE PACK, VERIFIED SLIDE BOTTLE PRESSURE AND SQUIB CHECK. CLOSED SLIDE PACK DOOR AND VERIFIED DOOR LATCH TUBE POSITION INSIDE SLIDE COMPARTMENT DOOR LATCHES ONCE CLOSED. DISARM AND RE-ARM SLIDE BOTTLE AFTER MTC. PER AMM 25-65. REQUIRED INSPECTION C/W.
R1 RIGHT FWD ENTRY DOOR KNUCKLE KNOCKER STICKS IN WHEN ARMING THE DOOR. R1 DOOR KNUCKLE KNOCKER CLEANED/ADJUSTED FOR SMOOTHER MOVEMENT.
RIGHT ENG REPORT OF FLAME AND SMOKE ON SHUTDOWN. R&R FUEL CTL MM 73-21 NEED LEAK/HIGH PWR RUN. FOUND NO OTHER EVIDENCE OF LEAKAGE.
THE EMERGENCY EXIT SIGN, FWD CENTER GALLEY WAS INOPERATIVE. FOUND THE FUSE BLOWN ON THE BATTERY CHARGER M730. R & R IAW AMM 33-51.
1R SLIDE LIGHT NOT COMING ON. REMOVED AND REPLACED THE SLIDE LIGHT ASSEMBLY IAW AMM 33-51.
L1 DOOR EXIT SIGN DETACHED. ATTACHED THE SIGN.
COCKPIT VOICE RECORDER MICROPHONE STARTED TO MELT IN THE COCKPIT. REMOVED AND REPLACED VOICE RECORDER. OPS TESTED NORMAL.
RUST EMANATING FROM THE NR 4 FLAP JACKSCREW UPPER BALLNUT GIMBAL. REPLACEED THE JACK SCREW IAW AMM 27-51-11.
NLG: RUST EMANATING FROM RIGHT TRUNNION PIN. REMOVED AND REPLACED THE NOSE LANDING GEAR RIGHT PIVOT PIN IAW AMM 32-21-01.
WHEN FLAPS SELECTED TO ONE, FLAPS FROZE HALFWAY TO ONE. TE FLAP ASYMETRY AND TRAILING EDGE LIGHT & MESSAGE. COMPLIED WITH QRH, LANDED NO FLAPS. FSEU NR 1 MESSAGE RT FLAP TRANSMITTER WIRE MESSAGE 313. FSEU NR 2, NO FAULTS. IAW FIM 27-51-00-815-805. FOUND THE CONNECTOR ON FLAP POSITION TRANSMITTER NOT CONNECTED. INSTALLED THE CONNECTOR, CHECKED WIRING FROM FSEU 1 TO RT FLAP POSITION TRANSMITTER IAW 27-51-41 AND FSEU 2 TO RT FLAP POSITION TRANSMITTER IAW 27-51-61. ALL GOOD AND NO SHORTS TO GROUND. PERFORMED FLAP LUBE IAW AMM 12-21-09. VERIFIED TRANSMISSION OIL SERVICE IAW AMM 12-13-06M REMOVED NR 06 CANOE. REMOVED AND REPLACED NR 06 RT FLAP TRANSMISSION IAW AMM 27-51. RIG AND OPS CHECKED OK IAW AMM 27-59.
DURING APPROACH, WHEN EXTENDING FLAPS TO 1, RECEIVED A TE FLAP ASSYM MESSAGE. PERFORMED QRH PROCEDURE, LANDED SLATS ONLY. REMOVED AND REPLACED THE NR 1 & 2 FSEU IAW AMM 27-51. OPS CHECKED GOOD.
DURING PRE-FLIGHT, FOUND THE LT EMERGENCY ESCAPE SQUIB LIGHT ILLUMINATED ON AUX MAINTENANCE PANEL. REMOVED CONNECTOR OFF THE PRESSURE SWITCH. LIGHT WENT OUT. REINSTALLED THE CONNECTOR. LIGHT WAS WORKING NORMAL. DURING FURTHER INSPECTION FOUND CONNECTOR RECEPTACLE ON BOTTLE PIN MISALIGNED. CORRECTED THE PIN AND CLEANED THE CONNECTOR. OPS CHECKED GOOD IAW AMM 25-65.
NR 1 ENGINE PYLON SKATE ANGLE CRACKED. N: REMOVED AND REPLACED THE SKATE ANGLE.
RIGHT AILERON HAS LIGHTNING STRIKE DAMAGE APPROXIMATELY 36INCHES FROM THE OUTBD. END. REMOVED RT AILERON FOR SHOP REPAIR. REMOVED DAMAGE UPPER AND LOWER T/E SKIN, PREP'D SAME FOR LAYUP OF REPAIR PLIESPER N757 SRM 57-60-01(425439). OK TO LAY UP REPAIR(QC1807). LAID UP, BAGGED AND CURED REPAIR PLIES PER B757 SRM 57-60-01. PERFORMED POST REPAIR NDT INSPECTION, NO ITEMS. REPAIRS COMPLETED PER B757 SRM 57-60-01(425439). PERFORMED WET BALANCE PER B757 SRM 51-60-01, WITHIN THE LIMIT -16.38 TR.LBS. REINSTALLED RT AIL ON AMDS WORKCARD 2700-4133-02.
LIGHTNING STRIKE AT STA 732 STRINGER 26 (SKIN DAMAGE AWAY FROM A FASTNER. CORRECTIVE ACTION:LIGHTNING STRIKE WAS AWAY FROM A FASTNER LOCATION. REPAIRED DAMAGE PER SRM. (2701338)
LIGHTING STRIKE AT STA 1387 STRINGER 25L. LIGHTING STRIKE WAS AWAY FROM A FASTENER. REPAIRED DAMAGE PER SRM. (2701342)
LIGHTNING STRIKE AT BS 751 STRINGER 26L ( SKIN DAMAGE AWAY FROM A FASTNER). LIGHTING STRIKE WAS AWAY FROM A FASTNER. REPAIRED DAMAGE PER SRM.
LIGHTING STRIKE AT BS 1430 STRINGER 25L (SKIN DAMAGE AWAY FROM A FASTNER). CORRECTIVE ACTION: LIGHTING STRIKE WAS AWAY FROM A FASTNER. REPAIRED DAMAGE PER SRM.
OVERHEAD MID CABIN EXIT SIGN DETACHED. SECURED THE SIGN IAW AMM 33-22.
COMPLY WITH ERA 545575-14-BS 655 S21R/S22R DRAIN FITTING HOLE IN FUSELAGE SKIN REPAIR. COMPLY WITH ERA 545575-14 -STA 655 S21R/S22R DRAIN FITTING HOLE IN FUSELAGE SKIN REPAIR.
EMERGENCY LIGHT INOPERATIVE AT 25C AND 29C CEILING LIGHT. REPLACED BATTERY PACK AT POWER SUPPLY M10954, ROW 29F FLOOR IAW AMM 33-51, OPS CK GOOD.
LT EXTERNAL FUSELAGE, DENT ON SKIN AT BS 620, 4 INCHES ABOVE STR 17L.
LT EXTERNAL FUSELAGE, DENT ON SKIN AT BS 620, 4 INCHES ABOVE STRINGER 17LT.
AFT CARGO DOOR EXTERIOR SKIN UPPER EDGE AT AFT CORNER HAS PREVIOUS EDGE DAMAGE WITH NO REPAIR DECAL. REPAIRED DAMAGE AT AFT CARGO DOOR EXTERIOR SKIN UPPER AFT EDGE IAW SRM 52-30-01, REPAIR 4. CATEGORY B REPAIR, ADDITIONAL INSPECTION REQUIRED. INSPECTION THRESHOLD 37,500, TOTAL FLIGHT CYCLES, REPEAT INSPECTION ALTERNATIVE II REQUIRED AT 6000 TOTAL DOOR FLIGHT CYCLES IAW SRM 52-30-01
LT STABILIZER UPPER SURFACE, 19" FROM L/E & 64" OTBD OFF USELAGE, APPROXIMATELY 1.5" DENT AT MINOR AXIS. EVALUATED & REPAIRED DENT ON LT HORIZONTAL STABILIZER. UPPER SURFACE 19" FROM L/E AND 64" OTBD OF FUSELAGE IAW SRM 55-10-01 AND SRM 51-70 -10 OF SRM.
AFT CARGO DOOR EXTERIOR SKIN UPPER EDGE AT AFT CORNER HAS PREVIOUS EDGE DAMAGE WITH NO REPAIR DECAL. DAMAGE TO DOOR FOUND TO BE OUT OF LIMITS, REF: SRM 52- 30-01 ALLOW. DAMAGE 1, FIG 101, SHT 4, DETAIL V. REPAIRED DAMAGE DOOR, EXTERIOR AT AFT CORNER UPPER EDGE AS REQUIRED, IAW SRM 52-30-01, REP 4, DAMAGE DEPTH OF .200" EXCEEDS MAX ALLOWABLE DEPTH OF .100". REPAIR IS CONSIDERED TO BE A CATEGORY B REPAIR.
NR 1 PYLON INBD SIDE CENTER PANEL SUPPORT LOWER ATTACH ANGLE CRACKED. RECEIVED NEW LOWER ATTACH ANGLE ON NR 1 PYLON INBD SIDE OF CENTER PANEL 313N3033-13, NEW ATAG A87264, LOCATED AND DRILLED NEW ANGLE BRACKET, IAW SRM 51-40-05, INSTALLED NEW ANGLE BRACKET IAW SRM 51-40-02.
AFT CARGO COMPARTMENT DOOR OPENING LOWER THRESHOLD PLATE CRACKED AND DAMAGED AT MULTIPLE LOCATIONS. WELD REPAIR ACCOMPLISHED.
FOUND DAMAGE TO LINER AFT OF FAN 7 O'CLOCK POSITION ON NR 1 ENGINE INSTALLED, PERMANENT REPAIR IAW MM 72-33-03-348-010.
L4 PASSENGER DOOR EXT EMERGENCY LIGHT INOPERATIVE. FOUND BATTERY PACK CONNECTOR LOOSE. RESECURED CONNECTOR.
IN SEAT EMERGENCY LIGHTS OUT BETWEEN ROWS 24-28. R & R EMERGENCY BATTERY PACK IAW MM 33-51. OPS NORMAL.
RIGHT AILERON UPPER SURFACE 20 INCHES FROM INBD END FOUND AREA DENTED AND DELAMINATED. REPAIRED IAW SRM 51-70-17.
RAM AIR ACTUATOR ACCESS PANEL 193BL HAS EROSION DAMAGE ON L/E. ACCOMPLISHED REPAIR OF THE DISCREPANT AREA ON RAM ACTUATOR ACCESS PANEL 193BL IAW SRM 51-70-05 AND ER/A 522503-14.
FUSELAGE SKIN, BS 600-660, S14-19L DENTED. NEW SKIN SECTION WAS SPLICED IN FROM BS 590-660 IAW ER/A 522499-14AD.
LEFT WING , NR 2 SLAT COVE SKIN CRACKED. REPAIRED IAW ER/A 366767-14MA, REV B.
NR 3 SLAT T/E WEDGE LOWER SKIN WORN. REPAIRED IAW SRM 51-70-10, PARA 6, 7, 8, 14, 15, 20 & 22, & SRM 57-43-02, FIG 201.
NR 1 SLAT COVE SKIN CRACKED AT OTBD MAIN TRACK ATTACH FITTING. R & R COVE SKIN AT NR 1 SLAT OTBD MAIN TRACK IAW SRM 51-40-05, PG 1-10, SRM 57-43-01 & DWG 114N4075.
NR 9 SLAT L/E, INBD END HAS A DENT, FOUND OUT OF LIMITS, CUTOUT DAMAGE IAW SRM 57-43-01. REPAIRED IAW SRM 57-43-01. REPAIR 1 AT NR 9 SLAT L/E, INBD.
NR 2 SLAT T/E WEDGE LOWER SKIN WORN. REPAIRED IAW SRM 51-70 -10 PARA 6, 7, 8, 9, 14, 15, 18, 20, 21C & 22.
FUSELAGE FRAME IN FWD CARGO BAY ABOVE S24L BS 620 DAMAGED. REPAIRED FRAME IAW REF SRM 53-00-07, REP 5, FIG 201.
AFT CARGO FLOORBOARD PUNCTURED. FABRICATED REPLACEMENT FLOORBOARD IAW SRM 51-40-05 AND 51-40-08.
DENT ON FUSELAGE FRAME IN FWD CARGO BETWEEN S23-24L, BS 580. FRAME REPAIRED IAW SRM 53-00-07.
RIGHT INNER CREASEBEAM ANGLE CORRODED AT BS 758. REMOVED CORROSION IAW SRM 53-30-13. R & R CREASE BEAM ANGLE BS 758 - 900 IAW SRM 51-40-02 & SRM 53-30-13.
FLOORBEAM STABILIZER STRAP CRACKED AT BS 367, LBL 25. STRAP REPAIRED IAW ER/A384483-14MA, REV D.
AFT DECK PLATE IN MAIN CABIN HAS CORROSION IN NUMEROUS AREAS FROM BS 1681-1720, BL-0 TO RBL 53. REMOVED CORROSION ON AFT DECK PLATE BS 1621-1720, BL 0 - RBL 53. BLEND OUT AT BS 1709 RBL 2 FOUND OUT OF LIMITS, ALL OTHER BLEND OUTS ARE WITHIN LIMITS IAW SRM 53-60-51, REPAIR 2, PG 201, FIG 201. ACCOMPLISHED DOUBLER REPAIR IAW SRM 53-60-51, REPAIR 2, PG 201, FIG 201 ALTERNATIVE 1.
LEFT WINGLET INBD SURFACE OF VERTICAL SECTION HAS THREE CRACKED SPOTS IN SKIN. REPAIRED IAW SRM 51-70-17.
AFT LEFT LAVATORY EMERGENCY LIGHT MODULE INOPERATIVE. RELAMPED ALL LIGHTS IN MODULE NO HELP. FURTHER TROUBLESHOOTING NEEDED. OUT OF TIME. FWD AND PLACARD IAW MEL 33-51-03. TROUBLESHOT SYS AND FOUND WIRES BROKEN TO LIGHT REPAIR WIRES OPS CHECKED NORMAL.
NR 7 SLAT SUSTAINED HAIL DAMAGE ON THE TRAILING EDGE WEDGE. WEDGE WAS REPAIRED IAW ERA 486708-14MA.
REF NR133, FUSELAGE SKIN (RT) - DENTED APPROX STA. 450 - BETWEEN STRS 24R AND 25R (CORRECTION) REPAIRED DAMAGE PER B757 SRM 53-00-01 REPAIR NR 2 FIG 201. REFERENCE NR 133.
EMERGENCY LIGHTS WILL NOT TURN OFF WITH SWITCH. MAINTENANCE REPLACED THE OVERHEAD EMERGENCY LIGHT PANEL AND SYSTEM NOW TESTS NORMAL.
NR 9 SLAT T/E WEDGE HAS MULTIPLE HAIL STRIKES. REMOVED NR 9 SLAT INSTALLED SLAT PER B757 AMM 27-81-02 NEEDS RIG CHECK 467881. RIGGED AND SAFETIED NR 9 SLAT PER AMM 27-81-02. REMOVED NR 9 SLAT 467881. INSTALLED SLAT PER B757 AMM 27-81-02.
NR 10 SLAT T/E WEDGE HAS MULTIPLE HAIL STRIKES. REMOVED AND REPLACED NR 10 SLAT PER B757 AMM 27-81-02.
NR 5 SLAT T/E WEDGE HAS MULTIPLE HAIL STRIKES. REMOVED AND REPLACED NR 5 SLAT PER B757 AMM 27-81-01.
NR 8 SLAT T/E WEDGE HAS MULTIPLE HAIL STRIKES. REMOVED AND REPLACED NR 8 SLAT PER B757 AMM 27-81-02.
NR 4 SLAT HAS MULTIPLE HAIL STRIKES ON T/E WEDGE. REMOVED AND REPLACED NR 4 SLAT PER B757 AMM 27-81-02.
HAIL DAMAGE TO LEFT WING AILERON UPPER SURFACE 4 PUNCTURES LOCATED 12 IN. IN FROM O/B EDGE IN APPROX CENTER AND 12 INCHES IN FROM I/B EDGE. REMOVED LT AILERON PER B757 AMM 27-11-21 467881. OK TO INSTALL QC3703. INSTALLED AILERON PER B757 AMM 27-11-21 NEEDS RIG CHECK 467881. COMPLIED WITH RIG CHECK PER B757 AMM 27-11-21256054. CLOSED WING PANELS. AILERON, LEFT, OFF 55-5751-9-0001 28469 ON 55-5751-9-0001 98403.
NR 3 SLAT T/E WEDGE HAS MULTIPLE HAIL STRIKES. REMOVED NR 3 SLAT. INSTALLED SLAT PER B757 AMM 27-81-02 NEEDS RIG CHECK 467881. RIGGED AND SAFTIED NR 3 SLAT PER B757 AMM 27-81-02.256054.
NR 2 SLAT T/E WEDGE HAS MULTIPLE HAIL STRIKES. REMOVED AND REP NR 2 SLAT PER B757 AMM 27-81-02 SLAT, NR 2 L/E; OFF 56-5754-9-0002 90039 ON 56-5754-9-0002 10748.
DURING OVERNIGHT LINE CHECK FOUND EXTERIOR EMERGENCY LIGHT INOP AT DOOR 4L. REPLACED LIGHT ASSEMBLY.
EXTERIOR SLIDE LIGHTS AFT OF DOORS 2R AND 4L INOPERATIVE. RELAMPED BOTH LIGHTS. LOG PAGE 7065081 FOR DOOR 4L.
THE FUEL SUPPLY TUBE IN THE RIGHT PYLON WAS FOUND TO BE CHAFING AGAINST THE PYLON SUPPORT STRUCTURE (P/N 112N4115-6). THE DAMAGE TO THE FUEL TUBE EXCEEDED THE ALLOWABLE 0.004 INCH OF DAMAGE. REPLACED THE FUEL LINE. REPAIRED PER EA 56-197969. OPERATIONAL CHECK GOOD.