N6714Q
Registered owner: DELTA AIR LINES INC, GA (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| DELTA AIR LINES, INC. (DALA) | Operator | 2011-06-21 – 2011-06-21 | Operator named in NTSB report |
| DELTA AIR LINES INC | Operator | 2011-06-21 – 2011-06-21 | Operator named in NTSB report |
Accident & incident history
Maintenance disclosures
WHEN WE FLIP THE EMERGENCY LIGHTS SWITCH GUARD CLOSED, IT UNARMS THE EMERGENCY LIGHTS. FOUND WIRE LOOP ON SWITCH OUT OF POSITION-REPOSITIONED WIRE LOOP OPS CK NORMAL. (8316116) AIRCRAFT WAS GROUNDED
R2L KNUCKLE BUSTER DOES NOT POP OUT WHEN DOOR IS CLOSED. FOUND PLACARD ON TOP OF KNUCKLE BUSTER PEELING UP, WHICH MADE CONTACT WITH DOOR LINING PREVENTING IT FROM EXTENDING. REPLACED PLACARD PER AMM 11-30. (8331154) AIRCRAFT WAS GROUNDED
ESCAPE SLIDE ARMED CONDITION INDICATORS. L2 KNOCKLE KNOCKER INOPERATIVE. KNUCKLE KNOCKER CAUGHT UP ON DOOR LINER. CLEANED AND ADJUSTED KNOCKER IAW AMM 52-11. KNOCKER WORKS GOOD. (1407722)
L2 DOOR HARD TO CLOSE. FOUND SERRATED PLATE FOR GUIDE ARM LOOSE AND HAD SLID FWD. ADJUSTED SERRATED PLATE AND SECURED. IAW AMM 52-11-04-402 -037. L2 DOOR OPENS AND CLOSES NORMAL. (1404973)
SHIP 6714 UPON ARRIVAL, GATE AGENT REPORTED LOUD POP OPENING L2 DOOR. NOW UNABLE TO CLOSE DOOR. CORRECTIVE ACTION: FOUND GUIDE ARM BOLTS LOOSE, RESECURED PER B757 AMM 52-11-04. FOUND CAM LATCH FITTINGS DAMAGED AND WITHIN TOLERANCES PER B757 AMM 52-11-37 AND C/W REPAIR PROCEDURE. COMPLETED HFEC PER B757 NDT 51-00-19 NO FAULTS. PERFORMED PRELOAD CHECK PER B757 AMM 52-11-04-822-056. SCUFF ON DOORFRAME DETERMINED TO BE PAINT CHIPPED, CLEANED AND INSPECTED PER B757 SRM 53-30-15. TOUCHED UP PAINT. REINSTALLED 2L DOOR LINER AFTER INSPECTION PER B757 AMM 52-11-02. PERFORMED PRESSURIZATION PER B757 AMM 51-11. (8586402)
EXIT ROW DOOR EXIT SIGN FELL OFF COMPLETELY / INTERIOR. RE-INSTALLED EXIT SIGN AT DOOR R2.
DOOR 4L ASSIST BOTTLE ZERO PRESSURE. R & R 4L DOOR ASSIST BOTTLE PER B757 AMM 52-11. LEAK CHECK GOOD.
SHIP 6714 DURING HOLE SCANS NOTED DEFECT AT STATION 1000 L/H OUTBOARD AFT HOLE UNDER STUB BEAM COMMON TO THE SKIN AND STRINGER. CORRECTIVE ACTION: REPAIRED STATION 1000 AFT HOLE PER ER/A 626574-14 PRI REV 04. (1045502)
SHIP 6714 R1 DOOR ROTARY SNUBBER INDICATOR PIN IS BELOW FLUSH AT +70 DEGREES F. CORRECTIVE ACTION: REPLACED R1 DOOR ROTARY SNUBBER IAW BDWG 141N6299 TYPE PL REV DVM SNUBBER WILL BE INSTALLED ON JOB CARD 5211-6005-IR STEP 6. (0980591)
SHIP 6714 R1 DOOR ROTARY SNUBBER INDICATOR PIN IS BELOW FLUSH AT +70 DEGREES F. CORRECTIVE ACTION: REPLACED R1 DOOR ROTARY SNUBBER IAW BDWG 141N6299 TYPE PL REV DVM SNUBBER WILL BE INSTALLED ON JOB CARD 5211-6005-IR STEP 6. JOB COMPLETE. (0980628)
SHIP 6714 R1 DOOR ROTARY SNUBBER INDICATOR PIN IS BELOW FLUSH AT +70 DEGREES F. CORRECTIVE ACTION: REPLACED R1 DOOR ROTARY SNUBBER IAW BDWG 141N6299 TYPE PL REV DVM SNUBBER WILL BE INSTALLED ON JOB CARD 5211-6005-IR STEP 6. JOB COMPLETE. (0980604)
SHIP 6714 FLOORBEAM STIFFENER STRAP AT STA. 365.25 IS CRACKED, LOCATED IN LEFT TUNNEL OF MEC. CORRECTIVE ACTION: FLOORBEAM STIFFENER STRAP AT STA 365.25 FOUND TO BE CRACKED. REPAIRED IAW B757-200 SRM 53-10-51-2R REPAIR 1. (0974445)
SHIP 6714 L4 DOOR BODY TORQUE TUBE ROTARY SNUBBER IS LEAKING. CORRECTIVE ACTION: REPLACED L4 DOOR BODY TORQUE TUBE ROTARY SNUBBER WITH A NEW SERVICEABLE SNUBBER WILL BE INSTALLED ON JC 5211-6005- 4L STEP 6. (0969941)
SHIP 6714 2L DOOR SLIDE PRESSURE LEVEL NOT WITHIN GREEN SLIDE RANGE. CORRECTIVE ACTION: R/R 2L DOOR SLIDE ASSY IAW B757 W/C 2566-9001-2L, INSPECTED INSTALLATION FOR SAFETY, SECURITY & APPROPRIATE CHKS / TEST OK RII COMPLEATED. (6455174)
SHIP 6714 FOUND R1 DOOR PARTIALLY OPEN. UNABLE TO CLOSE. T/S R1 DOOR AND FOUND INNER FRAME SEAL DISPLACED FROM RETAINER. REINSTALLED SEAL. FOUND UPPER AFT LATCH FITTING WORN ON BEARING. REMOVED AND REPLACED UPPER AFT LATCH FITTING PER B757 AMM 52-11 -37. OPS CHECK GOOD.
SHIP 6714-ATB/IFSD/DE- LEFT ENGINE IFSD DUE TO LOSS OF OIL PRESSURE AND QUANTITY. CORRECTIVE ACTION: FOUND OIL LEAK AT MAIN OIL FILTER COVER. REVIEWED FULL FLIGHT DATA, POSITIVE OIL PRESSURE WAS MAINTAINED DURING WINDMILL OPERATION. REPLACED EXTERNAL OIL PUMP PER B757AMM. NO LEAKS NOTED DURING OPERATIONAL CHECKS, COMPLIED WITH WINDMILL INSPECTION PER B757AMM, NO TROUBLE FOUND.
SHIP 6714 EMER ESCAPE PATH LTS 20D AND 34D MISSING WHITE LENSE. CORRECTIVE ACTION: R/R MISSING WHITE LENS EMERGENCY SEAT LIGHTS AT 20D & 34D. OPS OK, REF B757 AMM 33-51. (6585553)
SHIP 6714 SLIDE' LIGHT IN 3L DOOR WOULD NOT ARM. CORRECTIVE ACTION: CLEANED ANNUNCIATOR, OPS CHECK GOOD. (6624128)
DIV- TO MEM DUE TO WEATHER RADAR INOP AND WEATHER ENROUTE. REPLACED WEATHER RADAR DRIVE UNIT.
SHIP 6714 ESCAPE SLIDE ARMED CONDITION INDICATORS . 3R KNUCKLE KNOCKER INOP. CORRECTIVE ACTION: REMOVED DEBRIS FROM KNUCLE KNOCKER, CKS NML. (0545716)
SHIP 6714 L4 DOOR ASSIST BOTTLE AT 0 PSI. REMOVED AND REPLACED L4 EMERGENCY POWER RESERVOIR PER B757 AMM 52-11-30. (5671914)
SHIP 6714 CRACK FOUND ON UPPER FWD SIDE OF AILERON TRIM ACTUATOR LUG BETWEEN BARREL NUT AND BUSHING. CORRECTIVE ACTION: REMOVED AILERON TRIM ACTUATOR FROM LUG PER AMDS W/C 2711-01030- 01, HFEC INSPECTED AND VERIFIED CRACK PER B757 NDTM PART 6 CH 51-00-19. CRACK REPAIRED ON NR2, ERA 614747-14AD REV ORIG. (4341256)
SHIP 6714 AILERON TRIM ACTUATOR ATTACH BRACKET FOUND CRACKED. CORRECTIVE ACTION: SEE NR FOR ADDITIONAL INFORMATION 002-0001:0514-2001/002 00002 C/W LH AILERON TRIM ACTUATOR BEARING SUPPORT ASSY CRACKED LUG ERA 614747-14AD REV ORIG. ENSURED PRI 614747-14AD REV 0 THROUGH 2 MATCHES ERA 614747-14AD REV ORIG. (0144370)
SHIP 6714 - TIRE/DE - DUE TO NUMBER 2 MAIN TIRE FAILURE ON TAKEOFF. CORRECTIVE ACTION: REPLACED NUMBER 1&2 MAIN WHEEL ASSY. R/R NUMBER 2 BRAKE ASSY AS PRECAUTION.
SHIP 6714 EMERGENCY LIGHTS INOPERATIVE AT SEATS 23 THRU 26 BOTH LEFT WING EXIT DOORS, SEAT 26 CEILING EXIT SIGN, AND OUTSIDE OVERWING FRONT LIGHTS. CORRECTIVE ACTION: REFERENCED B757 SSM 33-51=01 AND WPM 33-51-13 CHECKED POWER SUPPLY M10567 FUSES, ALL WERE GOOD. REPLACED POWER SUPPLY BATTERY, SWAPPED POWER SUPPLY WITH KNOWN GOOD UNIT, OPS CHK OK. REPLACED BATTERY AND BATTERY CHARGER ASSY PER B757 AMM 33-51 OPS CK GOOD. (4297275)
SHIP 6714 CRACK INDICATION IN FRAME 1640 LH AT LOWER I/B HOLE AT APPROX 3 O'CLOCK POSITION. CORRECTIVE ACTION: REF ERA 610795-14. (2908246)
SHIP 6714 FUSELAGE SKIN STA 440 AND S-23RH/24RH DENTED. CORRECTIVE ACTION: REF ERA 610870-14. (2905912)
SHIP 6714 610795-14AD REV ORIGINAL / CRACK INDICATION IN FRAME WEB. CORRECTIVE ACTION: REF ERA 610795-14AD. (2906282)
SHIP 6714 AFT GALLEY FLOOR BEAM AT STA 1640 UNDER FLOOR PANEL 251QF HAS 3 FASTENER HOLES WITH BARE MEATAL AND LIGHT CORROSION. CORRECTIVE ACTION: SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0006:2500-2647/077 00340 REPAIRED FLOOR BEAM REF B757 SRM 53-00-51. (2901582)
SHIP 6714 AT PUSHBACK WHEN TRYING TO CLOSE BOARDING DOOR L2 THE AGENT NOTICED THE SEAT LEVER FOR THE EXTERIOR DOOR HANDLE DID NOT FUNCTION TO HOLD THE EXTERIOR DOOR HANDLE IN THE RETRACTED POSITION. CORRECTIVE ACITON: REPLACED BROKEN SPRING RETRACTION AT L2 DOOR IAW B757 AMM 52-11. OPS CHECK NML. (4053512)
SHIP 6714 FUSELAGE / STA 620 - 640 / LIGHTNING DAMAGE. CORRECTIVE ACTION: REF ERA 607354-14. (2697128)
SHIP 6714 LIGHTNING STRIKES BETWEEN STA 600 AND 690 AT LAP JOINT ON LEFT HAND SIDE. NR CARD 23,24,25,26,27, AND 28. CORRECTIVE ACTION: COMPLIED WITH PRI 607354-14 REV 0- REV 4 AND ERA 607354-14 REV ORIGINAL. PRI MATCHES ERA. (2697611)
SHIP 6714 2 LIGHTNING STRIKES AT FS 735 AT STR 25L. CORRECTIVE ACTION: CUT OUT DAMAGED AREA AND REMOVED FASTENERS IN REPAIR AREA REF B757 SRM. PERFORMED HFEC SURFACE INSPECTION AROUND SKIN CUTOUT AND BHEC OF ALL REMOVED FASTENERS IN THE REPAIR AREA PER B757 SRM. FABRICATE REPAIR PARTS REF B757 SRM, INSTALLED REPAIR PARTS REF B757 SRM. RESTORED FINISH REF B757 SRM. (2687702)
PROXIMITY EMERGENCY LIGHT COVER BROKEN. R & R IAW AMM 33-51- OPS CHECKED GOOD.
EMERGENCY LIGHT LENS BROKEN. NSTALLED A NEW LIGHT ASSY IAW AMM 33-51. OPS CHECKED GOOD.
SHIP 6714 L2 DOOR KNUCKLE KNOCKER STICKING, WILL NOT COME OUT. CORRECTIVE ACTION: ADJUSTED KNUCKLE KNOCKER, OPS CKS GOOD WHEN ARMING DOOR NUMEROUS TIMES. (8796035)
SHIP 6714 ESCAPE SLIDE ARMED CONDITION INDICATORS 2L INOP. CORRECTIVE ACTION: ADJUSTED DOOR PANEL PER B757 AMM 52-11, OPS CK NORMAL. (2402897)
SHIP 6714 -ATB- CREW PERFORMED AIR TURN BACK DUE TO RIGHT ENGINE COMPRESSOR STALL. CORRECTIVE ACTION: PERFORMED FIM INSPECTIONS INCLUDING INSPECTION OF 2.5 AND 14TH STAGE BLEED SYSTEM. ENGINE BORESCOPE INSPECTION COMPLIED WITH ALL NTF. ENGINE RUNS COMPLETE AND NTF.
SHIP 6714 RT AFT ENTRY DOOR EICAS MSG ILLUMINATED AT 100' AGL ON FINAL AND STAYED ON TO THE GATE. CORRECTIVE ACTION: INSP'D DOOR AND ALL STOPS/PADS DOOR OPS CHK'S NORMAL I.A.W. B757AMM 52-11 NO MSG'S ON EICAS NOTED
SHIP 6714 -DE- DUE TO FLAP ASYMMETRY MSG. CORRECTIVE ACTION: FOUND FAULT ON FSEU FOR LEFT WING FLAP POSITION TRANSMITTER. REPLACED LEFT WING POSITION TRANSMITTER. NO-GO ODI C/W.
SHIP 6714 ON S/C FOUND SEVERAL AFT EMER EXIT LIGHT INOP. CORRECTIVE ACTION: T/S PER B757 WDM 33-51. REPL BATT M736 PER 757 MM 33-51 CKS NML. (8245155)
SHIP 6714 DURING SVC CK FOUND 1R DOOR ASSIST BOTTLE AT 0 PSI. CORRECTIVE ACTION: REMOVED AND REPLACED 1R DOOR EMER PWR RESERVOIR PER B757 AMM 52-11. (7976891)
SHIP 6714 SEAT 18D SEAT MOUNTED EMERGENCY LIGHT DAMAGED. CORRECTIVE ACTION: REPLACED EMERGENCY LIGHT ASSY OPS OK PER B757 AMM 33-51. (7884025)
SHIP 6714 CRACK INDICATION NOTED IN UPPER I/B HOLE OF LH SIDE BS 1640 FRAME WEB, HINGE FITTING AND TEE CLIP AT 9 OCLOCK POSITION (I/B SIDE OF HOLE) FACING AFT. CORRECTIVE ACTION: ACCOMPLISHED FREEZE PLUG REPAIR ON UPPER I/B HOLE OF LH B.S. FRAME 1640 WEB IAW ER/A 593467-14AD REV ORIGINAL SECTION I. (1928183)
SHIP 6714 CRACK INDICATION NOTED IN RH SIDE FUSELAGE FRAME BS 16490 LOWER I/B HOLE AT 9 OCLOCK (O/B SIDE OF HOLE) POSITION OF FRAME WEB. HINGE FITTING AND TEE CLIP. CORRECTIVE ACTION: ACCOMPLISHED REPAIR ON RH FUSELAGE FRAME BS 1640 (FREEZE PLUG REPAIR) STR 14R IAW ER/A 593464-14AD REV ORIGINAL AND B757 SRM. (1925781)
SHIP 6714 R4 PASSENGER DOOR LOWER GATE MECHANISM HAS BENT LOWER ROD ASSY AT ROD END. CORRECTIVE ACTION: REMOVED AND REPLACED R-4 DOOR LOWER GATE MECHANISM GIRT BAR ROD ASSY, AND ADJUSTED IAW B-757 CMM 52-11-25, AMDS T/C. (1924632)
SHIP 6714 R-2 DOOR GIRT BAR P/N IS NOT EFFECTIVE. CORRECTIVE ACTION: REMOVED AND REPLACED R-3 DOOR EMERGENCY ESCAPE SLIDE GIRT BAR AND PERFORMED ADJUSTMENT AND TEST IAW B-757 AMDS T/C. (1924658)
SHIP 6714 DURING REMOVAL OF #1 ENG MAINTENANCE NOTICED THE TOOLING WOULD NOT SEAT PROPERLY ON THE LH PYLON FWD BLKD, THE INBD AND OTBD SKINS ON THE PYLON EXTEND TO FAR PAST THE EOP. CORRECTIVE ACTION: ACCOMPLISHED TRIM OF I/B & O/B SKINS FWD EDGE ON L/H PYLON, MAINTAINING 2D EDGE MARGIN IAW ERA 581756-14 REV. ORIG. SEC -1. (1918989)
SHIP 6714 KNUKLE KNOCKER ON 2R DOOR DID NOT PROTRUDE AFTER NORMAL ARMING. CORRECTIVE ACTION: EXERCISED ARM/DISARM AND NOTICED A SLIGHT INTERFERENCE ON TOP EDGE OF KNUCKLE KNOCKER. OPS NORMAL NOW. (7436062)
SHIP 6714: TOP FORWARD ROLLER LATCH CRANK BEARING MISSING ON R2 DOOR. CORRECTIVE ACTION: REPLACED TOP ROLLER. (LP 7436045)
SHIP 6714- MISC/DE- DUE TO FUEL CONFIG EICAS MESSAGE. INITIAL CORRECTIVE ACTION: RAN MAIN TANK PUMPS FOR 15 MINUTES WITH NO TRANSFER NOTED. TRANSFERRED FUEL FROM CENTER TO RT & LT MAIN TANKS. QUANTITY REMAINED STABLE. OK FOR SERVICE. FOLLOW UP ACTION: REPLACED RT MAIN TANK REFUEL VALVE CONTROLLER. BOND CHECK SATISFACTORY AND OPS CHECK OK.
SHIP 6714 R4 DOOR LOCK COLLAR BROKEN. CORRECTIVE ACTION: REMOVED AND REPLACED LOCK COLLAR AND CATCH PER B757 AMM 52-11. OPS CHECK GOOD. (4054986)
SHIP 6714 EMERGENCY EXIT COVER DIFFUSER LENS DAMAGED OR MISSING / LOCATIONS:652. CORRECTIVE ACTION: REMOVED AND REPLACED EXIT IDENTIFIER SIGN PER B757 AMM 33-51. OPS GOOD. (1549218)
SHIP 6714 4R DOOR WILL NOT ARM. CORRECTIVE ACTION: FND FWD SIDE OF GIRT BAR LOOSE. SECURED GIRT BAR FITTING TO GIRT BAR CKS GOOD REF B757 AMM 25-61. (6982624)
SHIP 6714 WHILE WKG JOB CARD 3351-7001 NUMEROUS EMERG INTERIOR LIGHTS IN THE AFT CABIN INOP. CORRECTIVE ACTION: SECURED BATTERY AT POWER SUPPLY RACK M737. RETEST EMERG LIGHT OPS CKS GOOD. (6488454)
(AIRCRAFT 6714, L/P 6398764) F/O FRONT WINDOW ARCHING AND DELAMINATING THEN MULTIPLE CRACKS. COMPLIUED W/ QRH. CORRECTIVE ACTION: REPLACED 1R WINDOW PER B757 AMM 56-11. ALL THREE TORQUES APPLIED TO 1R WINDOW PER B757 AMM 56-11. SPEED TAPE OVER AERO SEAL AROUND WINDOW REMOVED.
(AIRCRAFT 6714, L/P 1296282) DURING TEST OF EMERGENCY SCAPE SQUIB RH SIDE DOES NOT TURNED ON (TEST NOT PASS). SUMMARY OF NRC 0627: OFF-WING SLIDE PRESSURE BOTTLE WAS REMOVED PER B 757-200 AMM 25-65-02-004-010 AND INSTALLED SERVICEABLE OFF-WING SLIDE PRESSURE BOTTLE PER B 757-200 AMM 25-65-02-404-009 AND ELECTRICAL SYSTEM SQUIB AND PRESSURE SWITCH TEST WERE PERFORMED PER B-757-200 AMM 25-65-02-404-009 STEP G (21). TESTS OK.
CORROSION ON FASTENERS COUNTERSINK NR 1 TO 10 ON THE LT WING UPPER SKIN AND LT ENGINE DRAG FITTING. CORROSION ON FASTENERS COUNTERSINK REPAIRED IAW ETI-57-19-102 REV 15, & ER/A 581720-14AD, SECTION I, PERMANENT REPAIR, REV. ORIG.
A HOLE WAS FOUND WITH MORE THAN MAXIMUM DIAMETER ALLOWABLE, .286 OF .275, ON THE FAILSAFE AT THE AFT CARGO EQUIPMENT RACK. THE DIAMETER OF ADJACENT RIVET IS .269" WITH A SPACING OF 1 INCH REGARDING TO HOLE AFFECTED. OUT OF LIMITS, FRAME AT BS 1560 WAS REPAIRED IAW ER/A 581724-14AD, REV ORG SECTION 1. PERMANENT REPAIR, AND ETI-57-19-125 REV 1.
DURING DETAILED VISUAL INSPECTION ON REMOVED FWD INBD DRAG FITTING, PERFORMED IAW ETI-57-19-111 REV 1 STEP 5 AND DAMAGE ON THREE HOLES ADJACENT TO PREVIOUS REAMED HOLES WERE FOUND. REPAIRED IAW ER/A 581720-14AD REV ORIG SECTION 1, PERMANENT REPAIR, AND ETI-57-19-102 REV 15.
MIGRATION ON SHIM ID #1A WAS NOTED ON MEASUREMENT ID# 2A, AT INBOARD DRAG FITTING PERCARD 5720-01100-0101A, STEP 17. CORRECTIVE ACTION: MIGRATION SHIMS WERE REPAIRED PER ER/A 581720-14AD REV ORIGSECTION 1 AS PERMANENT REPAIR AND ETI-57-19-102 REV 15.
DAMAGE FOUND ON LOWER SIDE AND HOLES 7 AND 8 OF LH PYLON FWD INBD DRAG FITTING AFTER REMOVAL. REPAIRED IAW ER/A 581720-14AD REV ORIG SECTION 1 AS PERMANENT REPAIR AND ETI-57-19-102 REV 15.
CRACK ON INTERNAL DOUBLER AT LT PYLON, NAC. STA. 114.5 LT SIDE. THE DOUBLER WAS REPAIRED PER ER/A 581756-14 REV.ORG AND ETI-57-19-113REV. 6.
MIGRATION ON SKIN PANEL SHIM 1B WAS NOTED ON MEASUREMENT 2F AT OUTBOARD DRAG FITTING IAW CARD 5720-01100-0101A, STEP 18. THE SHIMS WERE REPAIRED IAW ER/A 581720-14AD REV ORIG SECTION 1, PERMANENT REPAIR AND ETI-57-19-102 REV 15.
DAMAGE FOUND ON THE WING UPPER SKIN, ADJACENT TO HOLES NR 2 AND 4 OF THE RT ENGINE DRAG FITTING. REPAIRED IAW ETI-57-19-099. REV.9 AND ER/A 581628-14AD REV.ORG.
SHIP 6714 AWR, AD, A.A.: CORROSION ON FASTENER HOLE BORE NBR 2 AT RH WING UPPER SKIN AND RH ENGINE DRAG FTG. CORRECTIVE ACTION: SUMMARY OF NR 00442 PERMANENT REPAIR WAS PERFORMED ON WING UPPER SKIN AND RH ENGINE DRAG FITTINGS PER ETI 57-19-099 REV. 9 AND ER/A 581628-14AD REV.ORG. SECTION I. (1290288)
CORROSION ON FASTENERS COUNTERSINK NBR 1 TO 10 AT RH WING UPPER SKIN AND RH ENGINE DRAG FITTING. CORRECTIVE ACTION: SUMMARY OF NR 00443 PERMANENT REPAIR WAS PERFORMED ON WING UPPER SKIN AND RH ENGINE DRAG FITTINGS PER ETI 57-19-099 REV. 9 AND ER/A 581628-14AD REV.ORG. SECTION I.
MIGRATION ON SKIN PANEL SHIM ID# 1A WAS NOTED ON MEASUREMENT ID# 2B AT INBOARD DRAG FITTING OF THE RH WING, PER CARD 5720-01100-0101B, STEP 17. (RH-MOT 2). CORRECTIVE ACTION: SUMMARY OF NRC S/N 00492, SHIMS WERE REPLACED PER ER/A 581628-14AD REV ORIG, AND ETI-57-19-099 REV 9.
MIGRATION ON SKIN PANEL SHIM ID # 1B WAS NOTED ON MEASUREMENT ID# 2D AT OUTBOARD DRAG FITTING OF THE RH WING, PER CARD. CORRECTIVE ACTION: SUMMARY OF NRC S/N 00493, SHIMS WERE REPLACED PER ER/A 581628-14AD REV ORIG, AND ETI-57-19-099 REV 9.
DAMAGE FOUND ON THE COUNTERSINK OF HOLES NUMBER 2, 4, 5 AND 7 AT UPPER SKIN RT ENG DRAG FITTING CLAMP. PERMANENT REPAIR WAS PERFORMED ON WING UPPER SKIN AND RT ENGINE DRAG FITTINGS PER ETI 57-19-099 REV. 9 AND ER/A 581628-14AD REV.ORG. SECTION I.
(AIRCRAFT 6714, L/P 1285570) 1 DISBOND WAS FOUND OF 20" X 19" ON L1 DOOR CUTOUT AT FWD UPPER CORNER IN REFERENCE WORK CARD 5331-01232-02G STEP 5.B.(2). CORRECTIVE ACTION: DISBOND AREA WAS BONDED AND REPAIR PERMANENT WAS PERFORMED PER ER/A 581555-14AD REV. ORG, ETI-57-19-097 REV. 6 AND AMDS 5331-01232-02G. TIME CONTROLLED ITEMS PERFORM HFEC, LFEC AND DVI AS DESCRIBED IN FIGURE 06 BEFORE 37,500 TOTAL FLIGHT CYCLES PER ERA 581555-14AD REV ORI SECTION II UNDER LOGPAGE #1284200.TIME CONTROLLED ITEMS- PERFORM HFEC, LFEC AND DVI AS DESCRIBED IN FIGURE 06 WITHIN EVERY 4,000 FLIGHT CYCLES. AFTER LOGPAGE 1284200, TIME CONTROLLED ITEMS- PERFORM HFEC AND LFEC AS DESCRIBED IN FIGURE 07 BEFORE 50,000 TOTAL FLIGHT CYCLES AND EVERY 12,000 FLIGHT CYCLES THEREAFTER PER ERA 581555-14AD REV ORI SECTION IV UNDER LOG PAGE # 1284208. TIME CONTROLLED ITEMS-REPAIR APPROVAL IS LIMITED TO 50,000 TOTAL FLIGHT CYCLES ONLY, ADDITIONAL ENGINEERING AUTHORIZATION (ER/A REVISION) IS REQUIRED FOR CONTINUED SERVICE BEYOND THIS LIMIT.
(AIRCRAFT 6714, L/P 1280610) FROM MON 36, LOG 2167125: TWO ADJACENT DENTS CLOSE TO MON DENT LOG # 2167125 AND .800" CLOSE TO PREVIOUS DOUBLER REPAIR STA 619 TO 626 BTW ST 16L AND ST18L. FUS. SUMMARY OF NRC S/N 00515 LT FUSELAGE SKIN FROM STA 590 TO STA 660 BTW STR 14 LT AND STR 19L WAS REPAIRED PER ER/A 581528-14 AD REV ORIG AND ETI-57-19-103 REV 3. DTE. REPAIR APPROVAL IS LIMITED TO 46,000 CYCLES ONLY. ADDITIONAL ENGINEERING AUTHORIZATION (ER/A REVISION) IS REQUIRED FOR CONTINUED SERVICE BEYOND THIS LIMIT PER ER/A 581528-14AD, REV ORIGINAL.
(AIRCRAFT 6714, L/P 1280728) DENT ON EXTERNAL FUSELAGE SKIN STA 1473 APPROX BTW S-27R (FUS). DENT ON EXTERNAL FUSELAGE SKIN STA 1473 APPROX BTW S-27R WAS REPAIRED PER ER/A 581527-14 REV ORIGINAL AND ETI-57-19-101 REV 2. MAINTENANCE REQUERIMENTS WERE VERIFIED AND THE FOLLOWING ACTIONS ARE REQUIRED DTE REPAIR APPROVAL IS LIMITED TO 73,200 TOTAL CYCLES ONLY ADDITIONAL ENGIEERING AUTHORIZATION (ER/A REVISION ) IS REQUIRED FOR CONTINUED SERVICE BEYOND THIS LIMIT PER ERA 581527-14 REV ORIGINAL. TIME OF ACCOMPLISHMENT MAINTENANCE REQUIRIMENTS UNDER LOG PAGE 1278940.
(AIRCRAFT 6714, L/P 1279282) AWR HIDDEN CORROSION: DURING REMOTION OF AFT CARGO LOWER SILL (SIDE PANEL), WAS FOUND CORROSION AT INNER CHORD (LOWER FACE) BTW STA 1380 TO 1440, IN REF TO NRC 00356. CORRECTIVE ACTION: SUMMARY OF NRC 456 INNER CHORD (LOWER FACE) BTW STA 1380 TO 1440, WAS REPLACED PER SRM 51-40-02 PAR. 4 AND 7 AND DGW 146N8522 REV E.
(AIRCRAFT 6714, L/P 1279781) CORROSION ON RT SIDE PANEL FROM STA 1440 TO 1530 AT AFT CARGO COMPARTMENT. CORRECTIVE ACTION: CORROSION LEVEL: 2 RT SIDE PANEL FROM STA 1440 TO 1530 AT AFT CARGO COMPARTMENT WAS REPLACED PER SRM 51-40-02 PAR 7.
(AIRCRAFT 6714, L/P 1279064) CORROSION OUT OF LIMIT ON FLOORBEAM STA 1640 BTW LBL 32 TO RBL 20 AT FLOOR STRUCTURE WET AREA. CORRECTIVE ACTION: CORROSION LEVEL 2. CORROSION ON FLOORBEAM STA 1640 BTW LBL 32 TO RBL 20 AT FLOOR STRUCTURE WET AREA WAS REPAIRED PER ER/A 581442-14 REV ORIG AND ETI-57-19-106 REV 4.
(AIRCRAFT 6714, L/P 1275787) REQUEST. DURING TEST EMERGENCY POWER ACTUATION CABLE, LOWER TORQUE TUBE ON 1 LH DOOR WAS FOUND 180 GRADE INVERTED IN REFERENCE AMDS 5211-3001-1L STEP 4. (PTAS). MODE SELECT LOCKOUT MECHANISM WAS ADJUSTED PER AMM 52-11-20-825-001. CHANGED SDR FROM N TO Y.
(AIRCRAFT 6714, L/P 1272819) INITIAL INSPECTION: WEAR ON PREVIOUS REPAIR TO NR1 PYLON STA 102 FAN COWL SUPPORT WEB RT SIDE. SUMMARY OF NRC 00437:PREVIOUS REPAIR ON NR 1 PYLON STA 102 WAS REPLACED PER EA: 06-462518-14 REV A.
(AIRCRAFT 6714, L/P 1269612) AFTER CORROSION REMOVAL A CRACK WAS FOUND ON RT SIDE PANEL STA 1617 AT AFT CARGO COMPARTMENT. RT SIDE PANEL STA 1617 AT AFT CARGO COMPARTMENT WAS REPAIRED PER SRM 53-00-53 REP 2.
(AIRCRAFT 6714, L/P 1267733) EXFOLIATION CORROSION ON FLOOR STRUCTURE, STA 436, LBL 67 AT PASSENGER CABIN (FWD WET AREA). SUMMARY: OF NRC. 00242 CORROSION LEVEL 2, FLOOR STRUCTURE, (CHORD) STA 436, LBL 67 AT PASSENGER CABIN WAS REPLACED PER SRM 51-40-02 PAR.
(AIRCRAFT 6714, L/P 1265419) AWR CORROSION OUT OF LIMITS ON FLOOR STRINGERS STA 1460 TO STA 1480 RBL AT AFT CARGO COMPARTMENT. CORROSION LEVEL 2. OUT OF LIMITS ON FLOOR STRINGERS STA 1460 TO STA 1480 AT AFT CARGO COMPARTMENT WERE REPAIR PER SRM 53-00-53 REP 1.
(AIRCRAFT 6714, L/P 1265179) AWR, CORROSION OUT OF LIMITS ON LT SIDE PANEL STA 1551 AT AFT CARGO COMPARTMENT (REF NRC 00351) (C2). SUMMARY: IN REFERENCE NRC 00536, CORROSION LEVEL 2: SIDE PANEL STA 1551 AT AFT CARGO COMPARTMENT WAS REPAIRED PER SRM 53-00-53 REPAIR 2.
(AIRCRAFT 6714, L/P 1265182) INITIAL INSPECTION: CORROSION ON LT SIDE PANEL FROM STA 1310 TO 1410 AT AFT CARGO COMPARTMENT.(ACP 0600-155-01Z).(C2). CORRECTIVE ACTION: CORROSION LEVEL 2, LT SIDE PANEL FROM STA 1310 TO 1410 AT AFT CARGO COMPARTMENT WAS REPLACED PER SRM 51-40-02 PAR 4 AND 7, AND DWG 146N5391 REV D.
(AIRCRAFT 6714, L/P 1265166) INITIAL INSPECTION: CORROSION ON STRINGERS (FLOOR SUPPORTS) 6EAS STA 1510 RBL/LBL AT AFT CARGO COMPARTMENT. (ACP 0600-155/156-01Z). (C2). CORRECTIVE ACTION: CORROSION ON STRINGERS (FLOOR SUPPORTS) 6EAS STA 1510 RBL/LBL AT AFT CARGO COMPARTMENT WERE REPAIRED PER SRM 53-00-53 REP 1.
(AIRCRAFT 6714, L/P 1260631) AWR HIDDEN CORROSION: DURING REMOTION OF AFT CARGO LOWER SILL (SIDE PANEL), WAS FOUND CORROSION ON SPLICE UNION STA 1380 (1 EA) STA 1440 (1 EA), IN REF TO NRC 00356. SUMMARY: IN REFERENCE NRC 00461: SPLICE (2 EA) AT STA 1380 AND AT STA 1440 WAS REPLACED PER SRM 51-40-02 PAR 4.
(AIRCRAFT 6714, L/P 1261677) INITIAL INSPECTION: CRACKED METALLIC STRAP ON MAIN DECK FLOOR STRUCTURE STA Y=1660 RBL=26 AT AFT OF AFT CARGO COMPARTMENT (CCT) (2020-2379). SUMMARY OF NRC 00381-METALLIC STRAP ON MAIN DECK FLOOR STRUCTURE STA Y=1660 RBL=26 WAS REPAIRED PER SRM 53-00-51 REP 12.
(AIRCRAFT 6714, L/P 1261563) LT SIDE PANEL OUT OF LIMITS FROM STA 605 TO STA 608 AT FWD CARGO COMPARTMEN. (C1), REASON FOR RE-WRITE, WRONG PROCESS ON WORK PERFORMED. LIMITS FROM STA 605 TO STA 608 AT FWD CARGO COMPARTMENT. (C1), REASON FOR RE-WRITE, WRONG PROCESS ON WORK PERFORMED. LT SIDE PANEL STA 605 TO STA 646 LT AT FWD CARGO COMPARTMENT WAS REPAIRED PER SRM 53-00-53 REPAIR 2.
(AIRCRAFT 6714, L/P 1260619) INITIAL INSPECTION: CORROSION ON LOWER SILL FROM STA 1380 TO 1440 AT AFT CARGO COMPARTMENT. (ACP 0600-156-01Z).(C2). SUMMARY: IN REFERENCE NRC 00356; LOWER SILL FROM STA 1380 TO 1440 WAS REPLACED PER SRM 51-40-02 PAR 4 AND 7.
(AIRCRAFT 6714, L/P 1258484) INITIAL INSPECTION: CRACK ON METALLIC STRAP AT PASSENGER CABIN FLOOR STRUCTURE, STA 372, LBL 26. (FWD WET AREA). SUMMARY: IN REFERENCE NRC 00236: CRACK ON METALLIC STRAP AT PASSENGER CABIN FLOOR STRUCTURE, STA 372, LBL 26 WAS REPAIRED PER SRM 53-00-51 REPAIR 12.
(AIRCRAFT 6714, L/P 1253425) INITIAL INSPECTION: CRACK ON METALLIC STRAP AT PASSENGER CABIN FLOOR STRUCTURE, STA 375, LBL 46. (FWD WET AREA). SUMMARY: OF NRC 00237. CRACK ON METALLIC STRAP AT PASSENGER CABIN FLOOR STRUCTURE, STA. 375, LBL 46. WAS REPAIRED PER, SRM 53-00-51 REPAIR 12.
(AIRCRAFT 6714, L/P 1254174) AWR HIDDEN DAMAGE: CORROSION OUT LIMITS ON RT FLOOR SUPPORTS BTW STA 1661-1681 AND RBL 56 AT AFT WET AREA. IN REFERENCES NRC 00465 (2020-2441). AREA IS OUT OF LIMITS PER SRM 53-60-15 ALLOWABLE DAMAGE 1 FIG. 101 NOTE B DET. VI. EQUIP PANAMETRICS 38DL PLUS S/N: 140940708, N/C 1326, EXP. DATE: 16/NOV/19, TRANSDUCER V260-SM S/N:11920097.FLOOR SUPPORT ON STA 1661-1681 WAS REPLACED PER SRM 51-40-05 AND SRM 51-40-02 PAR 7.
(AIRCRAFT 6714, L/P 1253004) INITIAL INSPECTION: CORROSION ON LT FLOOR SUPPORTS BTW 1640-1681 AND LBL 56 AT AFT WET AREA. (AMDS 2020-2441). AREA ARE OUT OF LIMITS PER SRM 53-60-15 ALLOWABLE. LT FLOOR SUPPORTS (2EA) BTW 1640-1681 AND LBL 56 WERE REPLACED PER SRM 51-40-02 PAR. 7.
SHIP 6714 INITIAL INSPECTION. CORROSION ON PREVIOUS DOUBLER REPAIR ON WEB STA 1718 RBL 3 AT PASSENGER FLOOR STRUCTURE. CORRECTIVE ACTION: SUMMARY OF NRC 00395: DOUBLER WAS REPLACED PER SRM. (1248370)
SHIP 6714 INITIAL INSPECTION. CORROSION ON PREVIOUS DOUBLER REPAIR ON WEB STA 1681 LBL 27 AT PASSENGER FLOOR STRUCTURE. CORRECTIVE ACTION: SUMMARY OF NRC 00394: DOUBLER WAS REPLACED PER SRM. (1248358)
EXIT SIGN CENTER AISLE ROW 20 DAMAGED. RESECURED EXIT SIGN AT ROW OPS CK GOOD.
SHIP 6714 R WING SLIDE WARNING LIGHT EICAS MSG ILLUMINATED ON FINAL TO RUNWAY. STAYED ON FOR 1 MINUTE THEN WENT OUT. CORRECTIVE ACTION: FOUND RIGHT OFF-WING SLIDE DOOR SENSOR (S10374) NEAR INDUCTANCE OUT-OF-LIMITS LOW (5.0 MH). ADJUSTED SENSOR TO GET 5.4 MH PER B757 AMM 52-71. REMOVED SAFETY PIN FROM SLIDE BOTTLE AND REARMED SLIDE PER B757 AMM 25-65-00/201, RII INSPECTION OF OFF WING SLIDE BOTTLE SAFETY PIN REMOVE & STOW C/W. (5828823)
EXIT SIGN LEN MISSING R2 DOOR. REPLACED LEN PER B757 AMM 33-51. OK FOR SVC . (LP# 5828808)
AFTER EXTENDING LNDG GEAR ON FINAL, GOT A "R SLIDE DOOR" EICAS MSG. IT EXTINGUISHED AS WE SELECTED LNDG FLAPS 25. INSPECTED RT OVERWING SLIDE ASSY AND DOORS. NO TROUBLE FOUND. COULD NOT GET MSG TO REAPPEAR. (5824586)
SHIP 6714 DURING GIRT BAR INSP /LUBE FOUND R4 DOOR ONE STOP FITTINGS BEARING PLATE MISSING. CORRECTIVE ACTION: INSTALLED BEARING PLATE IAW AMM 52-11. (5824508)
SHIP 6714 RIGHT WING SLIDE EICAS MSG. UPON GEAR EXTENSION FOR APPROXIMATELY:10. CORRECTIVE ACTION: NO FAULTS FOUND. VERIFIED OVER WING SLIDE SYS. (9550490)
(AIRCRAFT 6714, L/P 5006032) CENTER AISLE EXIT SIGN KNOCKED OFF NEAR ROW 27. SECURED CTR OVERHEAD EMERGENCY LIGHT LENS PER B757 AMM 33-50.
SHIP 6714 AFT RT LAV O2 MASK FELL OUT BUT OXYGEN GEN WASN'T ACTIVATED. CORRECTIVE ACTION: SECURED OXYGEN MASK IN AFT RT LAV. INSPECTED LATCHES AND OXYGEN GENERATOR FOR IRREGULARITIES. NONE FOUND AT THIS TIME. (5199918)
R3 DOOR ARMED KNUCKLE KNOCKER INDICATOR INOPERATIVE, WAS STIFF WHEN ARMING. ADJUSTED THE R3 DOOR LINER, DOOR ESCAPE SLIDE ARMED INDICATOR
FA REPORTED AN ODOR OF BURNING WIRE IN BACK OF THE ACFT ROW 40-43. QRH DONE. ACCOMPLISHED NO GO ODI PREVENTION STEPS PER ATA 2172 FIM CH. 21-00-01. NO DISCREPANCIES FOUND.
LEFT ELEVATOR DAMAGED, PERFORMED NDT INSPECTION FOR DELAMINATION AROUND DAMAGED AREA IAW SRM 51-70-17, PARA 3A (3). REMOVED THE DAMAGE AND INSTALLED A REPAIR IAW RI 567223-14.
KNUCKLE KNOCKER ON THE R3 DOOR WILL NOT EXTEND OR RETRACT. CLEANED THE KNUCKLE KNOCKER, OPS CHECKED NORMAL.
(AIRCRAFT 6714, L/P 0327553) EMERGENCY SEAT MOUNTED LIGHTING DAMAGED / INOP / LOCATIONS:03C / SEAT MOUNTED EMERGENCY LIGHTS. RESEATED LIGHT AT 3C.
(AIRCRAFT 6714, L/P 0327552) EMERGENCY SEAT MOUNTED LIGHTING DAMAGED / INOP / LOCATIONS:02C / SEAT MOUNTED EMERGENCY LIGHTS. RESEATED LIGHT AT 2C.
SHIP 6714 WHILE IN FOR WIFI MODIFICATION AT FS 620 BETWEEN STR 2R AND 3R, MTC FOUND 6 EXISTING HOLES IN THE LOCATION WHERE THE TEE CLIP IS TO BE MOUNTED TO THE FRAME. FOUR HOLES WILL BE PLUGGED AND TWO NEW HOLES WILL BE DRILLED PER DRAWING. CORRECTIVE ACTION: REF ERA 563164-14AD. REV B (0285114)
R2 DOOR SLIDE ARMED LIGHT TERMINAL BROKEN. REMOVED & REPLACED SLIDE LIGHT ASSY IAW 20-84. CHECKED GOOD.
L4 DOOR SNUBBER FAILED CHECK. REMOVED AND REPLACED THE DOOR SNUBBER IAW AMM 52-11.
UNABLE TO TURN OFF EMERGENCY LIGHTS ON PANEL SWITCH. COCKPIT SWITCH ONLY TUNERED OFF LIGHTS IN THE ARM POSITION. TROUBLESHOT IAW WDM 33-51-11, FOUND A LOOSE WIRE AT S10035. SECURED THE WIRE, LIGHT OPS NORMAL. OK FOR SERVICE.
ESCAPE SLIDE ARMED CONDITION INDICATOR ON THE R4 DOOR. KNUCKLE KNOCKER ADJUSTED MID DOOR BUSTLE PANEL AND TIGHTENED FASTENERS. VERIFIED NORMAL OPERATION.
PATHWAY LIGHT ON SEAT 30D IS BROKEN OFF MOUNTING. REATTACHED PATHWAY LIGHT TO SEAT ASSY AT 30D CKS GOOD.
EMERGENCY EXIT COVER DIFFUSER LENS DAMAGED. REINSTALLED EXIT SIGN COVER.
R3 DOOR KNUCKLE BUSTER DOES NOT COME OUT WHEN DOOR IS ARMED. CYCLED DOOR AND FOUND PLACARD ON TOP OF "KNOCKER" TO BE HANGING UP KNOCKER. ADJUSTED GAP & CK'S OK. (8887280)
DOOR KNUCKLE KNOCKER NOT POPPING OUT WITH DOOR ARMED. ADJUSTED KNUCKLE KNOCKER CKS OK.
AISLE EXIT SIGN INOPERATIVE BETWEEN L2 AND R2 DOORS. FOUND LIGHT EXIT ASSY L37 OVER R2 DOOR MISWIRED, CAUSING FUSE TO BLOW IN BATTERY PACK. WIRED L37 IAW WDM 33-51-13 AND REPLACED BATTERY PACK ASSY M732. OPS CHECKS GOOD.
DENT ON LT SIDE FUSELAGE OUTBD OF F/C EXT SERVICE PANEL. FOUND. LOCATED AT SEC 41, BS 395-418, STRINGERS S23- S24 LT SIDE. INSPECTED AND FOUND TO BE WITHIN LIMITS OF SRM 53-00-01 FIG 101. BUT A/Y RATIO WAS LES THAN 30... REQ VIS INSP EVERY300 FLT CYCLES. PERMANENT REPAIR IS MADE AT OR BEFORE NEXT C CHECK NOT TO EXCEED 24 MONTHS. OK FOR SERVICE. ADDED STATEMENT: LOGPAGE 2167253 & NRC 100-93 CREATED TO ACCOMPLISH REQUIRED REPETITIVE INSPECTIONS FOR THE INSTALLED DOUBLER. CLOSED LOG AND REMOVED MONITOR INSPECTION IAW PERM REPAIR INSTALLED AND TRACKING INSPECTION ON LP 2167253.
CORROSION ON FWD LAVATORY SERVICE ACCESS DOOR INNER SURFACE AND OUTER SURFACE AROUND LATCHES. ACCOMPLISHED PERMANENT REPAIR FOR A CORROSION ON FWD LAVATORY SERVICE ACCESS DOOR INNER IAW ER/A 539846-14, REV ORIG L=4.4, W=4.0, D=.019. INSTALLED ID TAG IAW TOPP 30-10-70 AND PS 900-5-1, N 04. ASSOCIATED ER/A 14-539846 ADDED FOR AC 6714.
LT INBD FLAP NR 4 BALLSCREW HAS PITTING AND PLATING MISSING FROM THREADS. REMOVED AND REPLACED THE NR 4 FLAP BALLSCREW IAW AMM 27-51-11-024-001. LT WING NR 4 FLAP BALL SCREW, OPS CHECK GOOD IAW AMM 27-51-11-424-020 AND AMM 27-51-11-024-001.
AFT CARGO DOOR EXTERNAL SKIN HAS 2 EA DENTS AT FWD LOWER SECTION. DENT NR 1 WITH A 0.8" DIAMETER FOUND CREASED ON AFT CARGO DOOR EXTERNAL SKIN FWD LOWER SECTION. DENT NR 2 FOUND TO BE A PREVIOUS DENT ON LOG 0987482. TRIMMED-OUT DENT 1 TO A 0.8" X 0.8" DIAMETER AND ACCOMPLISHED A PERMANENT REPAIR CATEGORY A IAW SRM 52-30-01, FIG 201, REPAIR 2. INSTALLED ID TAG IAW PS 900-5-1, NR 04.
AFT CARGO DOOR FWD FRAME HAS DENT AT FWD LOWER SECTION. REFORMED DENTED SEAL DEPRESSOR, FWD FRAME IAW BAC 5300 AND REF SRM 51-00-05, MATERIAL ORIGINAL THICKNESS .040", MATERIAL LOSS .010", FOUND OUT OF LIMITS IAW SRM 52-30-02, FIG 101; DETAIL V, CUT OUT DAMAGE IAW SRM 51-70-11, FIG 1, FORMED -3 DOUBLER AND -6 FILLER IAW SRM 51-70-11, FIG 1. TREATED & PRIMED AND INSTALLED -3 DOUBLER AND -6 FILLER AT AFT CARGO DOOR FWD FRAME "SEAL DEPRESSOR " AT FWD LOWER. SECTION IAW SRM 51-70-11, FIG 1. TRIM OUT DIMENSION 2.5" X1.0" X 0.5"R. DOUBLER DIMENSION 10" X 1.3" X 0.5"R . NOTE: TRIMOUT WAS A PREVIOUS BLEND. INSTALLED ID TAG IAW PS 900-5-1, NR 4.
RIGHT WING INBD MAIN FLAP T/E PANEL PUNCTURED ON BOTTOM 52" FROM INBD END 4" FROM FWD END. REMOVED ALL CONTAMINATION AND WATER FROM DAMAGED AREA IAW SRM 51-70-06 PARA 5.C.2. REMOVED DAMAGE WITH 2" DIAMETER AND PREPARED AREA FOR REPAIR IAW SRM 51-70-06 PARA 5.C.3. FABRICATED HONEYCOMB REPLACEMENT CORE AND INSTALLED IAW SRM 51-70-06 PARA 5.C.4. PREPARED AND APPLY REPAIR PLIES TO REPAIR AREA IAW SRM 51-70-06, PARA 5.C.6. APPLIED PRIMER AND TOPCOAT TO REPAIR AREA IAW AMM 51-21-10-377-039, PARA C.1.
DOOR WILL NOT ARM. REPOSITIONED LANYARD CLIP IN SLIDE PACK ASSY, DOOR ARM/DISARMS NORMALLY.
DIVERTED DUE TO LEFT HYD QTY AND PRESSURE AT ZERO, FOLLOWED BY RT HYD OVERHEAT MESSAGE ILLUMINATED THEN RT HYD SYSTEM PRESSURE ILLUMINTATED. FOUND BOTH LT GEAR DOWNLOCK ACTUATOR HYD LINES RUPTURED. REPLACED BOTH LINES, DOWLOCK ACTUATOR, LEFT EDP AND CASE DRAIN FILTER. JACKED ACFT SWUNG GEAR SYSTEM OP CHECKED NORMAL.
DURING OVERNIGHT CHECK, FOUND EMERGENCY ESCAPE LIGHTING INOPERATIVE ON ROWS 28-37. FOUND CONNECTOR DISCONNECTED BEHIND AIR RETURN GRILL AT 33 DEF AND CONNECTED, LIGHTS OPS CHECKED GOOD.
EMERGENCY LIGHTS INOPERATIVE AT ROW 28-37. REPLACED 5A FUSE AT BATTERY PACK CHARGER ML648 AND RELAMPED AISLE EMERGENCY LIGHTS AT ROW 28-37.
MAIN CABIN AT BS 324 , RBL 64 FLOORBEAM CORRODED. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. REMOVED SECTION OF FLOORBEAM UPPER ANGLE, FABRICATED AND INSTALLED ANGLE SECTION, SPLICE ANGLES AND STRAPS IAW SRM 53-10-08, REPAIR 1, FIG 201.
NR 2 ENGINE FIRE BOTTLE DISCHARGE LIGHT ON P-8 PANEL & NR 2 ENGINE BOTTLE MESSAGE ON EICAS DISPLAY. REMOVED ENGINE FIRE BOTTLE, INSTALLED ENGINE FIRE BOTTLE IAW AMM 26-21-01.
MAIN CABIN, BS 1681 LBL 32 DECK PLATE CORRODED. CUT OUT DAMAGE IAW SRM 53-60-51 FIG 21 REPAIR 3. FABRICATED REPAIR DOUBLERS & FILLERS IAW SRM 53-60-51 FIG 201 REPAIR 3. INSTALLED IAW SRM 51-40-02 & 53-60-51 FIG 201 REPAIR 3. MAJOR REPAIR.
MAIN CABIN FLOORBEAM BS 345. LBL 14 & BL 0 CORRODED. REMOVED CORROSION , AND FOUND OUT OF LIMITS, FABRICATED AND INSTALLED REPAIR ANGLE AND STIFFNER IAW SRM 51-10-02 PAR.15 AND 53-00-51 REPAIR 11 FIG 201.
AFT CABIN AFT DECK PLATE CORRODED BS 1681.8, LBL 29-52. CUT OUT DAMAGE IAW SRM 53-60-51 FIG 201 R2. FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW SRM 53-60-51 FIG 201 REPAIR 2 & 51-40-02. MAJOR REPAIR
CORROSION ON AFT GALLEY DECK PLATE FWD OF AFT PRESSURE BULKHEAD BS 1700, BL 0 - RBL 30. REMOVED CORROSION IAW SRM 51-10-02. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 53-60-51 FIG 201 REPAIR 2 ALTERNATIVE I. MAJOR REPAIR.
DENT ON FUSELAGE SKIN BS 620-640 STR 17-18L. CUT OUT DAMAGED AREA AND FABRICATED REPAIR DOUBLER AND INSTALLED IAW SRM 53-00-01 FIG 201 REPAIR 3, 51-40-02, 51-20-01 & 51-40-05.
AT 39FL, F/A REPORTED HOT ELECTRICAL ODOR IN THE CABIN AROUND ROWS 20-30 IAW QRH UTILITY BUSSES, LT RECIRCULATION FAN TURNED OFF. ODOR DISSIPATED WITH CONCURRENCE OF MX. PERFORMED INSPECTION OF SEBS FOR OBVIOUS SMOKE EMITTERS IN ROWS 20-40. INSPECTED SIDEWALL OVERHEAD LIGHTS, READING LIGHTS, E/E AND BOTH CARGO BINS. NO ODOR DETECTED. ELECTRICAL ODOR BURN WITH IFE ON BOTH UTILITY BUSSES DROPPED OFF. RECONNECTED AND NTF. THE LT RECIRCULATION FAN WAS REPLACED DUE TO ODOR.
ON WALK AROUND FOUND DENT UNDER DOOR 3L. REPAIRED PER ERA 502517-14 REV A.
DURING TAKEOFF AFTER GEAR RETRACTION, THE NR 1 ENGINE FIRE INDICATION ANNUNCIATED. THE FLIGHT CREW VERIFIED FLAMES COMING FROM THE ENGINE, SHUTDOWN THE NR 1 ENGINE, FIRED BOTH EXTINGUISHING BOTTLES, AND RETURNED. MAINTENANCE REPLACED THE NR 1 ENGINE AND BOTH FIRE EXTINGUISHING BOTTLES.
DURING LAYOVER CHECK, MX FOUND THE EMERGENCY EXIT LIGHT AT DOOR 1R TO BE INOPERATIVE. A BLOWN FUSE (F1 ON POWER SUPPLY M731) WAS IDENTIFIED AND THE POWER SUPPLY WAS REPLACED. AFTER REPLACEMENT OF POWER SUPPLY ENTIRE FIRST CLASS AISLE EMERGENCY LIGHTS WENT INOPERATIVE DUE TO A WIRE SHORTED AT 3CD. REPAIRED THE FAULTY WIRING IAW WDM AND LIGHTS NOW OPERATE NORMAL.
RT ENG OIL QTY0 / FLUX OIL PRESS, ON ARRIVAL FOUND NR 2 ENG MAIN OIL SCREEN O-RING CUT. REPLACED OIL SCREEN AND O-RING, RAN ENG. NO LKS NOTED, OK FOR SVC.
FOUND CORROSION IN AFT CARGO DOOR WAY FROM BS 1380 TO BS 1440 LOWER SILL ZONE 154. REPAIRED BY REMOVING AND REPLACING CHORD P/N 146N8522-64 IAW B757 SRM 51-40-02 AND DELTA SRM 51-00-00D.
FOUND CORRODED AFT CARGO THRESHOLD/FLOOR SUPPORT STRUCTURE AT DOOR STA 1375 - 1440 RBL 20. REPAIRED BY REMOVING AND REPLACING LOWER CHORD P/N 146N8522-57 IAW B757 SRM 51-40-02, 51-20-01, DELTA B757 SRM 51-00-00D.
FOUND FWD CABIN FLOORBEAM GOUGED AT BS 600 LBL 27, 44. REPAIRED BY CUTTING OUT GOUGED AREA BS 600 LBL 7 TO LBL 71. FABRICATED AND INSTALLED T CHORD REPAIR 69 BY 2-1/8 BY 0.125 FROM BAC1505-100617 AND REPAIR ANGLE 11 BY 2 BY 0.063" FROM BAC1490-2734 AND ANGLE REPAIR 7-1/2 BY 2 BY 0.063 IAW B757 SRM 53-00-51 REPAIR 3 FIG 201, 51-40-02 AND 51-20-01.
FOUND CORRODED FLOORBEAM AT BS 1640 BETWEEN LBL 24 - RBL 28 IN MAIN CABIN AFT SECTION. REPAIRED BY CUTTING OUT 18 CORRODED SECTION OF T CAP. FABRICATED DRILLED AND INSTALLED T CAP REPAIR 32-5/8 FROM BAC1505-100617, 2 SPLICES 9 BY 2 BY 1 AND 6 BY 2 BY 1 FROM 7075-T6 .071 AND 7075-T6 .063 IAW DELTA B757 SRM 53-00-51, 51-20-01 AND DELTA PS 900-2 NR 5.
T/E FLAP DISAGREE MESSAGE AND LIGHT ON APPROACH. COMPLETED NON-NORMAL CHECKLIST. FLAPS WENT TO 20 ELECTRICALLY. LIGHTS WENT OUT. T/S PER FIM. BITE CKD FSEU NR 1 FAULT MSG 305 FLAP DISAGREE. BITE CHECK OF FSEU 2 AND 3, NO FAULTS. FOUND LT INBD FLAP TRANS OVERLOAD INDIC SHOWING. RESET SAME. LUBED INBD TRANS AND CKD FLUID LEVELS. ALL CKD GOOD. RAN FLAPS SEVERAL TIMES ,NO EVIDENCE OF BINDING. NO FAULT MSGS PRESENT.
CREW REPORTS RT ENG OIL FILTER STATUS MSG APPEARED DURING FLIGHT. CREW FOLLOWED QRH PROCEDURES AND MSG DID NOT CLEAR. ENGINE SHUTDOWN PER QRH. REPLACED ENGINE.
EMERGENCY FLASHLIGHT AT THE L2 POSITION INOP. REPLACED SAME.
FLIGHT ATTENDANT REPORTS FWD OVERHEAD RAFT COMPARTMENT LATCH BROKEN. FOUND LIFE RAFT SLOWLY DEPLOYING IN ITS COMPARTMENT. REPLACED SAME. REPAIRED DOOR.
ELEC FUMES IN FLT DECK AND LEFT ENG GEN DROPPED OFF LINE. NO ASSOC STATUS MSGS. DIVERTED TO GSO. LEFT ENG GEN CONFIRMED FAILED. PLACED ON MCO PER MEL. FOUND EVIDENCE OF FUMES WHILE STANDBY POWER CHECK WAS PERFORMED. REPLACED MAIN BATTERY, CHARGER AND INVERTER AS PRECAUTIONARY. DURING CONTINUED T/S, FOUND BURNED TERMINALS ON 3L WINDOW HEAT TERMINAL. THE 3L WINDOW HEAT DEACTIVATED PER MEL. IT IS SUSPECTED THAT THE 3L WINDOW WAS SOURCE OF SMELL THE ENTIRE TIME.