N67171
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
DE- DUE TO SLAT DISAGREE ON APPROACH. TROUBLESHOT, R & R L/E SLAT ROTARY ACTUATORS NR 5, 10, 20. (8433306) AIRCRAFT WAS GROUNDED.
CEILING EMERGENCY LIGHT AT SEAT ROW 30DEF INOP. REPLACED LAMP AT CEILING MOUNTED AISLE EMERGENCY LIGHT ASSEMBLY REF B757 AMM 33-51. (LP 8459099 - AIRCRAFT WAS GROUNDED)
PRIOR TO PUSH, LAST 3 ROWS LEFT SIDE & AFT LEFT LAV SIDE WALLS HOT TO THE TOUCH AND REPORTED A BURNING ELETRICAL SMELL. REMOVED AFT CARGO WALL, FOUND DUCT BYPASSING AT FWD CLAMP REPLACED SAME, LEAK CHECKS GOOD REF B747 IPC 36-11-01. (8281388) AIRCRAFT WAS GROUNDED
FUSELAGE FRAME, BS 1640, S14L CRACKED AND MISDRILLED IN THE PARTIAL FRAME SPLICE, MONITOR INSPECTION LOG. REPAIRED THE FRAME SPLICE BS 1640 BTWN S9 - 20L IAW ERA 631259-14AD. (1426571)
CRACKS FOUND AT THREE FASTENER HOLES, BS 1640 LT FUSELAGE FRAME, OUTER UPPER HOLE PRESENTS A CRACK ON THE FRAME WEB, OUTER ANGLE & HINGE FITTING AT 6 CLOCK; OUTER LOWER HOLE PRESENTS CRACKS ON THE FRAME WEB, OUTER ANGLE & HINGE FITTING AT 3 & 9 O`CLOCK, INNER LOWER HOLE PRESENTS CRACKS ON THE FRAME WEB & HINGE FITTING AT 3 & 9 O`CLOCK , IAW CARD 5311-01218-01A, JOB 108-0001, STEP 11. REPAIRED IAW PRI 631259-14, REV 0 - 4, & ERA 631259-14AD, REV ORIGINAL, SECTION I, PERMANENT REPAIR. (1427633).
DENT ON FRAME STA. 231 AND BL 0 AT FWD ACCESS COMAPARTMENT. FRAME STA. 231 AND BL 0 AT FWD ACCESS COMAPRTMENT WAS REPAIRED IAW SRM 53-00-07-2R REP. 7. (1418988)
AIRCRAFT 6717, CORROSION ON SIDE PLATE LT AND BS 620 AT FWD CARGO BAY. CORROSION LEVEL 2. CORROSION ON SIDE PLATE LT AND BS 620 AT FWD CARGO BAY WAS REPAIRED IAW SRM 53-00-53-2R, PROCEDURE 2, REPAIR 2. (LP 1417580)
R4 & R1 EMERGENCY POWER RESERVOIRS, LOW PRESSURE (LESS 2,000 PSI) AT R2 EMERGENCY POWER RESERVOIR. RESERVOIR AT 1R DOOR WAS REPLACED WITH SERVICEABLE RESERVOIR PER B757-200 AIPC 52-11-30-01. INSTALL ACOMPLISHED UNDER AMDS 5211-9001-1R STEP 20 AND RESERVOIR AT 4R DOOR WAS REPLACED WITH SERVICEABLE RESERVOIR, VERIFIED PER B757-200 AIPC 52-11-30-02. INSTALL ACOMPLISHED UNDER AMDS 5211-9001-4R STEP 20. (1407831)
IN REF TO AMDS 5211-6005-2L STEP 2 DURING PASSENGER DOOR BODY TORQUE TUBE SERVICE WAS FOUND WEAR ON UPPER LINK ASSY. UPPER LINK ASSY WAS REPAIRED PER ER/A 618704-14 REV ORIGINAL SECTION I. (1403815)
IN REF TO AMDS 5211-6005-4L STEP 2 DURING PASSENGER DOOR BODY TORQUE TUBE SERVICE WAS FOUND WEAR ON UPPER LINK ASSY. UPPER LINK ASSY WAS REPAIRED PER ER/A 618704-14 REV ORIGINAL SECTION 1. (1403152)
IN REFERENCE TO NRC 437 WIP 5, : (UT) MEASUREMENT THICKNESS WAS ACCOMPLISHED ON WEB SURFACE (DECK PLATE ) BTW STA 1681 AND LBL 52 AT W4, IT'S OUT OF LIMITS PER B757-200 SRM 53-60-51-1A PROCEDURE 2 ALLOWABLE DAMAGE 2. PAR. 2. C. TABLE 101. DETAIL III. TABLE 102. SUMMARY OF NRC 00688, CORROSION LEVEL 2: DECK PLATE BTW STA 1681 AND LBL 52 AT W4 WAS REPAIRED PER B757-200 SRM 53-60-51-2R PROCEDURE 2 REPAIR 2, ALTERNATIVE II. (1395340)
DEBOND WAS FOUND OF:1.250 IN X 1.250 IN LENGTH/ WIDTH UPPER SURFACE SLAT #7. OSS: 329 RH WING. UPPER SURFACE SLAT #7. OSS: 329 RH WING WAS REPAIRED PER B757-200 SRM 57-43-02-2R PROCEDURE 1 REPAIR 1 FIG.201 NOTE B AND B757-200 SRM 51-70-10-2R PROCEDURE REPAIR GENERAL. (1395619)
REFERENCE TO NRC 437 WIP 9, (UT) MEASUREMENT THICKNESS WAS ACCOMPLISHED ON WEB SURFACE (DECK PLATE ) BTW STA 1716 AND RBL 35 AT W4, IT'S OUT OF LIMITS PER B757-200 SRM 53-60-51-1A PROCEDURE 2 ALLOWABLE DAMAGE 2. PAR. 2. C. TABLE 101. DETAIL III . TABLE 102. SUMMARY, OF NRC 00692 CORROSION LEVEL 2: (DECK PLATE ) BTW STA 1716 AND RBL 35 AT W4 WAS REPAIRED PER B757-200 SRM 53-60-51-2R-14. (1394288)
DISBOND PREVIOUS REPAIR ON T.E OF SLAT N 9 BTW WS=690 TO WS=700 AT RH WING. T.E OF SLAT N 9 BTW WS=690 TO WS=700 AT RH WING PER B757-200 SRM 57-43-02-2R PROCEDURE 1 REPAIR 1 FIG.201 NOTE B AND B757-200 SRM 51-70-10-2R PROCEDURE REPAIR GENERAL. (1392951)
IN REFERENCE TO NRC 437 WIP 7, (UT) MEASUREMENT THICKNESS WAS ACCOMPLISHED ON WEB SURFACE (DECK PLATE) BTW STA 1681.8 AND RBL 47 AT W4, THEREFORE IT'S OUT OF LIMITS PER B757-200 SRM 53-60-51-1A PROCEDURE 2 ALLOWABLE DAMAGE 2. PAR. 2. C. TABLE 101. DETAIL III. TABLE 102. CORROSION LEVEL 2: DECK PLATE BTW STA 1681.8 AND RBL 47 AT W4 WAS REPAIRED PER B757-200 SRM 53-60-51- 2R REPAIR 2 ALTERNATIVE II. (1392384)
IN REFERENCE TO NRC 437 WIP 6, (UT) MEASUREMENT THICKNESS WAS ACCOMPLISHED ON WEB SURFACE (DECK PLATE ) BTW STA 1681.8 AND LBL 25 AT W4, WITH ORIGINAL THICKNESS IS 0.071IN AND MINIMUM REMAINING THICKNESS IS 0.030IN THEREFORE IT'S OUT OF LIMITS PER B757-200 SRM 53-60-51-1A PROCEDURE 2 ALLOWABLE DAMAGE 2. PAR. 2. C. TABLE 101. DETAIL III. TABLE 102. CORRECTIVE ACTION: SUMMARY OF NRC 00689 , CORROSION LEVEL 2 ; DECK PLATE BTW STA 1681.8 AND LBL 25 AT W4 WAS REPAIRED PER B757-200 SRM 53-60-51- 2R REPAIR 2 ALTERNATIVE II. (1387762)
CORROSION ON BOX BEAM (2EAS) ALSO COMMON ANGLE ( 2EAS) STA 1673 ON LBL 56 AND RBL 56 AT W4. BOX BEAM ALSO COMMON ANGLE (2EAS) BS 1673 ON LBL 56 AND RBL 56 AT W4. REPLACED IAW SRM 51-40-02-0G AND DWG 146N5246 REV. A. (1386998)
UT MEASUREMENT THICKNESS WAS ACCOMPLISHED ON UPPER AND LOWER FLANGE OF BEAM BS 1640 FROM LBL 33 TO LBL 56 THEREFORE IT IS OUT LIMITS. BEAM STA 1640 FROM LBL 33 TO LBL 56 WAS REPAIRED PER SRM 53-00-51-2R REPAIR 11. (1385192)
UT MEASUREMENT THICKNESS WAS ACCOMPLISHED ON PREVIOUS REPAIR UPPER AND LOWER FLANGE OF BEAM STA 1640 FROM LBL 33 TO RBL 10 AT W4 THEREFORE IT IS OUT LIMITS. BEAM STA 1640 FROM LBL 33 TO RBL 10 AT W4 WAS REPAIRED PER B757-200 SRM 53-00-51-2R PROCEDURE 10. REPAIR 10. (1385545)
SHIP 6717 SLIDE INDICATOR LIGHT INOP OR DAMAGED / LOCATIONS:603. CORRECTIVE ACTION: RELAMPED, FOUND FWD PROX SWITCH BAD (S10218) . R/R PER B757 AMM 25-66-11. OPS CKS GOOD. (1113102)
SHIP 6717 FND EMERGENCY LIGHTS INOP FROM ROW 38DEF TO 45 DEF. ALSO L3 DOOR EMER EXIT SIGN INOP AND LT AFT OVWG LIGHT ALSO INOP. CORRECTIVE ACTION: FND BATTERY BEHIND SEAT 38F BAD. R/R SAME NOW ALL LOCATIONS OPS CHK GOOD IAW B757 AMM 33-52. (7004614)
SHIP 6717 ON S/C FOUND FWD DOOR / CABIN SEVERAL EMERGENCY LIGHTS INOP. CORRECTIVE ACTION: FOUND PWR SUPPLY M731 AND ASSOCIATED BATTERY INOP. R/R BOTH - REF B757 AMM 33-51-07. OPS CK GOOD. (7127868)
SHIP 6717 ON SERVICE CK FOUND EMERG LIGHTS AT SEATS 19D-22D INOP. CORRECTIVE ACTION: T/S AND RESECURED FUSE ON BATTERY PACK SLED M733, EMERG LIGHTS CK OK, REF B757 AMM 33-51. (4019134)
SHIP 6717 4L DOOR WILL NOT ARM CORRECTLY. CORRECTIVE ACTION: ADJUSTED 4L DOOR EMERGENCY MECHANISM REF B757 AMM 52-11-20. TEST OK. (5738294)
SHIP 6717 SLIDE INDICATOR LIGHT INOP OR DAMAGED / LOCATIONS:603. CORRECTIVE ACTION: R+R 2L SLIDE GIRT BAR ENGHAGEMENT LIGHT IN REF TO B757 AMM 25-66 . OPS CHECK GOOD. A/C OK FOR SVC PLACARDS REMOVED. (0255322)
SHIP 6717 L4 DOOR WILL NOT ARM. CORRECTIVE ACTION: REMOVED DEBRI DOOR 4L. LUBED REF 757AMM 25-16. OP'S CK GOOD OK FOR SVC. (4344828)
SHIP 6717 3L DOOR WILL NOT ARM PROPERLY. CORRECTIVE ACTION: CYCLED DOOR 3L & OPERATED SLIDE ARM DISARM NORMAL. OK FOR SVC IAW AMM 25-66. (4344824)
SHIP 6717 DOOR ARMED KNUCKLE KNOCKER INOPERATIVE / LOCATIONS:601 KNUCKLE KNOCKER DOES NOT EXTEND. CORRECTIVE ACTION: REMOVED L1 SLIDE BUSTLE - SECURED MID DOOR LINER - KNUCKLE KNOCKER NOW OPERATES NORMAL - RE-INSTALLED SLIDE BUSTLE - WORKED PER B757 AMM 52-11. (0172690)
SHIP 6717 L1 DOOR SNUBBER PIN EXTENSION IS NOT CORRECT PER CUSTOMER CARD 2040-0191-L1. CORRECTIVE ACTION: REMOVED AND REPLACED L1 DOOR SNUBBER IAW B757 AMM 52-11. (0160578)
SHIP 6717 PASSENGER DOOR R-4 GIRT SLIDER SPRING DAMAGE. CORRECTIVE ACTION: REPLACED PASSENGER DOOR R-4 GIRT BAR SLIDER SPRING (BAR LOCK) IAW B757 AMM 25-66-01. (0155905)
SHIP 6717 PROTUDING DENT FOUND ON R/H SIDE OF FUSELAGE AT STA 199.09 PLUS (18IN) BETWEEN STRINGER 18R & 19R. CORRECTIVE ACTION: ACCOMPLISHED REPAIR BS 199.09+18 STR 18R-19R I.A.W DELTA ER/A # 614777-14 REV O. (0146952)
SHIP 6717 CORROSION FOUND ON STRAP BELOW FLOOR PANEL AT C2 DOOR CUTOUT THRESHOLD. STA 1380 TO STA 1440 WL 147. CORRECTIVE ACTION: REPLACED SIDE PANEL (STRAP) AND SPLICE PER B757-200 SRM. (0144097)
SHIP 6717 FUSELAGE / SKIN / FWD LOWER ATG4 ANTENNA / REMOVAL. CORRECTIVE ACTION: REF ERA 614166-14. (0098506)
SHIP 6717 DOOR ARMED KNUCKLE KNOCKER INOPERATIVE / LOCATIONS:01L / ACARS KNUCKLE KNOCKER DOESNOT EXTEND FULLY. CORRECTIVE ACTION: PERFORMED OPS TEST OF O1L DOOR ARM AND DISARMED PER B757 AMM 52- 11. OPS TESTS NORMAL. (2773877)
SHIP 6717 MID CABIN EXIT SIGN COVER DAMAGED/MISSING. CORRECTIVE ACTION: REATTACHED COVER IAW B757 AMM 33-51. (4739971)
SHIP 6717 EMERGENCY EXIT SIGNS INOPERATIVE / LOCATIONS:605 / COVER BELOW EXIT SIGN FALLING OFF. CORRECTIVE ACTION: RESECURED SIGN COVER, EMERGENCY EXIT SIGN OPERATES NORMALLY AS PER B757 AMM 33-51. (2672768)
R3 DOOR DIFFICULT TO ARM. KNUCKLE KNOCKER STICKING OR STUBBORN TO DEPLOY. CLEARED DEBRIS FROM EDGE OF KNUCKLE KNOCKER CUTOUT. OPS NORMAL. DOOR ARMS AND DISARMS NORMALLY.
EXIT SIGN PARTIALLY DETACHED IN MIDDLE OF A/C CEILING HALFWAY BACK OF A/C SIGN IN OVHD BIN. ALL SIGN CURRENTLY INSTALLED AND OPERATIONAL.
DIVERTED INTO MCO DUE TO DUAL BLEED FAILURE CAUSING THE LOSS OF BOTH PACKS, EMERGENCY DECENT EXECUTED. R & R THE RT ENG THE HPSOV REGULATOR, HPSOV VALVE, 450 TEMP SENSOR, AND 380 TEMP SENSOR. FOR THE LT ENG THE RFCC, 450 TEMP SENSOR, PRSOV CONTROLLER, AND HPSOV CONTROLLER WERE REPLACED. THE ISOLATION VALVE WAS ALSO REPLACED AS A PRECAUTION. A SENSE LINE LEAK CHECK, PNEUMATIC HEALTH CHECK, AND PNEUMATIC SYSTEM DATA RUN WAS ACCOMPLISHED ON BOTH ENGS. ALL PARAMETERS NORMAL.
DIVERSION INTO BHM DUE TO THE LOSS OF BOTH BLEED SYSTEMS EMERGENCY DECENT EXECUTED. T/S REPLACED LH ENG FAV, 380 TEMP SNSR, RT ENG PRECOOLER, RT ENG FAV AND FAN AIR VALV TEMP SENSOR. LEAK CK AND OPS CK GOOD.
SHIP 6717 FOUND ROW 33-37 SEAT MOUNTED EMERGENCY LIGHTS INOP. CORRECTIVE ACTION: R/R POWER SUPPLY IAW B757 AMM 33-51. OPS CHECK GOOD. (9035417)
SHIP 6717 OVHD EMERGENCY EXIT SIGN MID CABIN MISSING. CORRECTIVE ACTION: RE-INSTALLED SIGN. (8912296)
SHIP 6717 ATB- PERFORMED AIR TURN BACK TO ATL DUE TO LEFT ENGINE HIGH OIL TEMPERATURE IN CAUTION RANGE. CORRECTIVE ACTION: FOUND LEFT ENGINE OIL PUMP AND L IDG OIL TEMP EICAS MESSAGE. REPLACED LT ENGINE IDG AND LUBE PUMP.
SHIP 6717 WHILE WKG WORK CARD #5211-2301 PAX DOOR 3L MISSING 1EA STOP PLATE. CORRECTIVE ACTION: INSTALLED NBR 5 FWD DOOR STOP PLATE IAW B757 AMM 52-11-00. (8598490)
SHIP 6717 2L EXIT SIGN COVER LOOSE FALLS OFF. CORRECTIVE ACTION: SECURED EXIT SIGN LENS AT 2L PER B757 AMM 33-50. (2207412)
SHIP 6717 NO FLIGHT INDICATION WHEN 4R DOOR IS OPEN. CORRECTIVE ACTION: REMOVED AND REPLACED 4R DOOR PROX SENSOR . OPS CHK GOOD. (8794442)
SHIP 6717 DOOR ARMED KNUCKLE KNOCKER RETRACTED DURING T/O. DOOR SHOWING ARMED.O. DOOR ARMED AND SHOWING ARMED / INTERIOR. CORRECTIVE ACTION: PERFORMED OPS CHECK OF 3R DOOR IAW NB757 M/M 52-11-20. OPS. CHECKS NORMAL. (2174073)
SHIP 6717 EMERGENCY EXIT COVER DIFFUSER LENS DAMAGED OR MISSING / LOCATIONS: 26. CORRECTIVE ACTION: INSTALLED EMERGENCY EXIT SIGN LENS AT ROW 26 REF B757 AMM 33-51. (2152141)
SHIP 6717 LT MLG TRUNNION FIXED CTR FAIRING MISSING ON ARRIVAL. CORRECTIVE ACTION: REMOVED AFT LT MLG TRUNNION FAIRING PER B757 AMM 32-12. INSTALLED LT MAIN GEAR FIXED CENTER FAIRING AND AFT MOVEABLE FAIRING AS PER B757 AMM 57-51, ALL CHECKS NORMAL. (7323628)
SHIP 6717 FLIGHT DECK L3 WINDOW HAS HEAT/ARCING DAMAGE AT UPPER BUSS BAR. CORRECTIVE ACTION: REMOVED AND REPLACED L3 WINDOW FLIGHT DECK IAW B757 AMM 56-11. (2079468)
SHIP 6717 R/H SIDE OF FUSELAGE MID LAV SERVICE PANEL ACCESS DOOR HAS AREAS OF CORROSION ALONG BOTTOM OF DOORS. CORRECTIVE ACTION: BLENDED CORROSION ON R/H SIDE MID LAV SERVICE PANEL ACCESS DOOR, FOUND TO BE OUT OF LIMITS IAW B757 SRM, REMOVED AND INSTALLED NEW LAV PAN DOOR IAW B757 SRM. (2077266)
SHIP 6717 R/H PYLON DRAG FITTING #3,4,5,8,9 FASTNER DAMAGED AD-RELATED. CORRECTIVE ACTION: INSTALLED NEW FASTENER ON R/H PYLON DRAG FITTING #3,4,5,8 AND 9 HOLES IAW ERA 584511-14AD REV.C AND T/C 5720-01100-04B. (2075018)
SHIP 6717 RH ENGINE DRAG FITTING HOLE #7 HAS CRACK LIKE INDICATION NOTED AT APPROX. 1 OCLOCK POSITION IN THE FITTING AD-RELATED. CORRECTIVE ACTION: COMPLIED WITH ERA 584511-14AD REV.C REAMED HOLE WITH NO INDICATION OF CRACK NOTED AT R/H ENGINE DRAG FITTING HOLE #7. (2074992)
SHIP 6717 RH ENG. DRAG FITTING PYLON HOLE #15 HAS CRACK LIKE INDICATION WITH CORROSION IN THE FITTING LAYER AD-RELATED. CORRECTIVE ACTION: COMPLIED WITH ERA 584511-14AD REV.C REAMED HOLE WITH NO INDICATION OF CRACK NOTED AT R/H ENGINE DRAG FITTING HOLE #15. (2074987)
SHIP 6717 R/H PYLON DRAG FITTING #18 FASTNER DAMAGED. CORRECTIVE ACTION: INSTALLED NEW FASTENER ON R/H PYLON DRAG FITTING #18 HOLE IAW ERA 584511-14AD REV.C AND TASK CARD. (2075012)
SHIP 6717 REPAIR TO RH WING UPPER SKIN COMMON TO DRAG FITTING ATTACHMENT REQUIRES SUPPLEMENTAL INSPECTIONS PER ERA 584511-14AD REV. C. CORRECTIVE ACTION: REF ERA 584511-14 REV C. (2074055)
SHIP 6717 OVER WING CEILING EXIT SIGN LENS MISSING. CORRECTIVE ACTION: INSTALLED LENS. (8197578)
SHIP 6717 AIRCRAFT DAMAGED AT STA 365 TO STA 377 IN BETWEEN STR 19R AND 20R. CORRECTIVE ACTION: SUMMARY SEE NR FOR ADDITIONAL INFORMATION 003-0001:00-0653-8-3889/001 00001 COMPLIED WITH PRI 593704-14 REV O THRU REV 3, PRI 593704-14 REV O THRU REV 3 MATCH ER/A 593705-14 REV O. (1927442)
SHIP 6717 RIGHT AFT DOOR KNUCKLE KNOCKER DOES NOT ARM. CORRECTIVE ACTION: LUBED KNUCKLE KNOCKER HINGE POINT. OPS NORM. REF B757 AMM 52-11. (7370772)
SHIP 6717 REPAIR TO RH WING UPPER SKIN COMMON TO DRAG FITTING ATTACHMENT REQUIRES SUPPLEMENTAL INSPECTIONS PER ERA 584511-14 REV A. CORRECTIVE ACTION: REF ERA 584511-14 REV A. (1795669)
EMERGENCY LIGHTS AT L2 ARE INOPERATIVE. CORRECTIVE ACTION: REPLACED BATTERY. SYSTEM OPERATION IS NORMAL.
EMERGENCY EXIT COVER DIFFUSER LENS DAMAGED OR MISSING. LOCATIONS:604. INSTALLED LIGHT COVER.
EMERGENCY EXIT COVER DIFFUSER LENS DAMAGED OR MISSING. LOCATIONS: 604. SECURED 2R EMERGENCY EXIT COVER.
EMERGENCY EXIT SIGN COVER LOOSE AT THE R2 DOOR. SECURED EXIT SIGN COVER.
EMERGENCY EXIT COVER DIFFUSER LENS DAMAGED OR MISSING, LOCATION 29C. CORRECTIVE ACTION, RE-INSTALLED COVER AS REQ'D.
SHIP 6717 EMERGENCY EXIT SIGN COVER LOOSE / LOCATIONS:604. CORRECTIVE ACTION: REINSTALLED SIGN COVER. (1558357)
SHIP 6717 EMERGENCY EXIT COVER DIFFUSER LENS DAMAGED OR MISSING / LOCATIONS:604. CORRECTIVE ACTION: SECURED EMERG EXIT LENS COVER. (1557616)
MIGRATED SHIMS 1B AND 1D (2EA), ON OUTBOARD ENG DRAG FITTING AT RT WING. CORRECTIVE ACTION: REPAIRED PER ER/A 584511-14AD REV. ORIGINAL. SECTION I: PERMANENT REPAIR.
CORROSION: ELONGATED HOLES WAS FOUND ON OUTBOARD ENG DRAG FITTING, OUTBD HOLES TO ATTACH FITTING TO DRAG FITTING AT RT WING IN REF ETI-57-19-201 REV 4 STEP 23. CORRECTIVE ACTION: REPAIRED PER ER/A 584511-14AD REV ORIGINAL. SECTION I: PERMANENT REPAIR, AND ETI-57-19-201 REV 10.
SCRATCHES ON HOLES 1, 2, 3, 6, 7, 8, 9 LOCATED ON RT ENG DRAG FTG CLAMP-UP & DIAG BRACE. CORRECTIVE ACTION: REPAIRED PER ER/A 584511-14AD REV. ORIGINAL. SECTION I: PERMANENT REPAIR. AND ETI-57-19-201 REV. 10.
SEVERAL POINTS OF FRETTING CORROSION WERE FOUND ON FRONT SPAR SETTLEMENT AREA OF INBOARD AND OUTBOARD ENG DRAG FITTINGS AT RT WING IN REF ETI-57-19-201 REV. 4 STEP 23. CORRECTIVE ACTION: REPAIRED PER ER/A 584511-14AD REV. ORIGINAL. SECTION I: PERMANENT REPAIR AND ETI-57-19-201 REV. 10.
SEVERAL POINTS OF FRETTING CORROSION WERE FOUND ON OUTBOARD ENG DRAG FITTING AT RT WING IN REF ETI-57-19-201 REV. 4 STEP 23 (AD). CORRECTIVE ACTION: REPAIRED PER ER/A 584511-14AD REV. ORIGINAL. SECTION I: PERMANENT REPAIR. AND ETI-57-19-201 REV. 10.
SEVERAL POINTS OF FRETTING CORROSION WAS FOUND ON INBOARD ENG DRAG FITTING AT RT WING IN REF ETI-57-19-201 REV 4 STEP 23. CORRECTIVE ACTION: REPAIRED PER ER/A 584511-14AD REV ORIGINAL. SECTION I: PERMANENT REPAIR. AND ETI-57-19-201 REV. 10.
LOOSE FASTENERS NR 4, 5, AND 10, ON RT ENG DRAG FITTING (AD). CORRECTIVE ACTION: REPAIRED PER ER/A 584511-14AD REV ORIGINAL. SECTION I: PERMANENT REPAIR. AND ETI-57-19-201 REV 10.
HIDDEN CORROSION: NICKS WAS FOUND ON COUNTERSINK AREA OF FITTING, LOWER HOLES TO ATTACH FITTING TO FRONT SPAR AT RT WING. CORRECTIVE ACTION: REPAIRED PER ER/A 584511-14AD REV ORIGINAL. SECTION I: PERMANENT REPAIR AND ETI-57-19-201 REV 10.
LOOSE FASTENERS NR 15, ON RT ENG DRAG FITTING. CORRECTIVE ACTION: REPAIRED PER ER/A 584511-14AD REV. ORIGINAL. SECTION I, PERMANENT REPAIR AND ETI-57-19-201 REV 10.
(AIRCRAFT 6717, L/P 1434515) ELONGATED HOLES AND CORROSION ON SIDE PANEL RH BTW STA 1530 TO 1640 UPPER AND LOWER. CORRECTIVE ACTION: CORROSION LEVEL 2. REPLACED PER B757-200 SRM 51-40-02 PAR 4 AND 7.
(AIRCRAFT 6717, L/P 1435637) CORROSION ON PREVIOUS REPAIR STA 1470 FLOOR STRINGER RBL 16.10, 10.45, 2.90 AND LBL 2.90, 7.55, 10.45, 16.10 AT AFT CARGO COMPARTMENT FLOOR STRUCTURE. CORRECTIVE ACTION: CORROSION LEVEL 2. REPLACED FOR NEW ONES PER B757-200 SRM 51-40-02-0G.
(AIRCRAFT 6717, L/P 1434507) CORROSION ON FLOOR STRINGER STA 1510 LBL 2.90 RBL 2.90, 11.40 AT AFT CARGO COMPARTMENT FLOOR STRUCTURE. CORRECTIVE ACTION: CORROSION LEVEL 2. REPAIRED PER B 757-200 SRM 53-00-53-2R-1.
(AIRCRAFT 6717, L/P 1434049) CORROSION ON SIDE PANEL STA 1410 TO 1530LH UPPER AND LOWER SURFACE AT AFT CARGO COMPARTMENT FLOOR STRUCTURE. CORRECTIVE ACTION: CORROSION LEVEL 2. REPLACED PER B757-200 SRM 51-40-02-0G PAR 7.
(AIRCRAFT 6717, L/P 1433121) CORRROSION ON PREVIOUS REPAIR OF FLOOR STRINGER STA 1510 LBL 11.40, 7.55 AND RBL 7.55 AT AFT CARGO COMPARTMENT FLOOR STRUCTURE. CORRECTIVE ACTION: (LEVEL CORROSION 2). INSTALLED PER B757-200 SRM 51-40-02-0G PAR. 7.
(AIRCRAFT 6717, L/P 1434206) REPLACE R2 AFT AND R4 AFT LEAF SPRINGS DUE ENGAGEMENT DIMENSION IS LESS THAT 0.37 INCH. CORRECTIVE ACTION: REMOVED OLD R2 GIRT BARS PER B757-200 AMM 25-66-10-002-001. INSTALLED NEW R2 GIRT BARS PER B757-200 AMM 25-66-10-402-022. ADJUSTED R2 AND R4 GIRT BAR MECHANISM PER AMDS 2566-9001-4R AND AMDS 2040-0057-2R.
(AIRCRAFT 6717, L/P 1434085) CORROSION ON INTERCOSTAL BTW STA 1400 TO 1420 LBL 16.10 AT AFT CARGO COMPARTMENT. CORRECTIVE ACTION: CORROSION LEVEL 2: REPAIRED PER B757-200 SRM 51-70-11-0G.
(AIRCRAFT 6717, L/P 1434309) DURING REMOTION OF CORROSION ON SIDE PANEL WAS FOUND OUT OF LIMITS AREA BTW STA 1353 TO 1410, AFT CARGO COMPARTMENT. CORRECTIVE ACTION: (CORROSION LEVEL 2): REPAIRED PER B757-200 SRM 53-00-53-2R-3.
(AIRCRAFT 6717, L/P 1434094) STRINGER ON STA 1330 AND RBL 16.10 AT AFT CARGO COMPARTMENT WAS FOUND OUT OF LIMITS AFTER REMOVED CORROSION. CORRECTIVE ACTION: CORROSION LEVEL 2. REPAIRED PER B757-200 SRM 53-00-53-2R-1.
(AIRCRAFT 6717, L/P 1432903) CORROSION ON SIDE PANEL UPPER AND LWR SURFACE BTW STA 1530 TO 1640 LH AT AFT CARGO COMPARTMENT FLOOR STRUCTURE. CORRECTIVE ACTION: (LEVEL CORROSION 2): REPLACED FOR A NEW ONE PER B757-200 SRM 51-40-02-0G.
(AIRCRAFT 6717, L/P 1426120) R1 DOOR POWER RESERVOIR IS NOT VISIBLE AND CORROSION ON BOTTLE BODY WAS FOUND. CORRECTIVE ACTION: R/R'D PER B757-200 AMM 52-11-30.
(AIRCRAFT 6717, L/P 1424137) CORROSION ON SIDE PANEL BTW STA 1350 TO 1380 RH UPPER AND LOWER SURFACE AT AFT CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED SIDE PANEL PER B757-200 SRM 51-40-02-0G PAR. 4 AND 7.
SHIP 6717 DISBONDED AREA AT OSS 440.2 ON UPPER SKIN SLAT 8. CORRECTIVE ACTION: SUMMARY OF NRC 00173 UPPER SKIN SLAT 8 WAS REPAIRED PER B 757-200 SRM. ACCOMPLISHED POST REPAIR INSPECTION IAW SERVICE BULLETIN 757-57-0066 REV. 1 PAR. 1. E COMPLIANCE TABLE 1 CONDITION 3 ACTION 2. NO DEFECTS NOTED. (1424175)
CORROSION FOUND ON THE SUPPORT FOR THE BODY FAIRING BETWEEN BS 850 TO 950, WL 133. THE SUPPORT WAS REPLACED IAW SRM.
DEBONDED AREA OF 3.0" X 2.200" AT OSS 310.47 ON UPPER SKIN OF SLAT NR 4. THE UPPER SKIN OF SLAT NR 4 WAS REPAIRED IAW SRM.
(AIRCRAFT 6717, L/P 1409642) CORROSION ON FLOOR BEAM STA 1640 BTW LBL 15/RBL 5,AT AFT GALLEY FLOOR STRUCTURE. CORRECTIVE ACTION: REPAIRED PER B757-200 SRM 53-00-51-2R REPAIR 10 AND ER/A 521546-14 REV. ORG.
L1 DOOR KNUCKLE KNOCKER DOESN'T WORK WHEN DOOR IS ARMED. MUST BE JIMMIED OUT. VERIFIED KNUCKLE-KNOCKER FUNCTIONS PROPERLY SEVERAL TIMES, FULL EXTENDING & RETRACTING IAW AMM 25-66. OPS CHECKED GOOD. NO FURTHER DEFECTS AT THIS TIME.
(AIRCRAFT 6717, L/P 5719892) MULTIPLE LIGHTS INOP AT FWD OVERWING EMER EXIT IDENTIFIER. RELAMPED LIGHTS.
(AIRCRAFT 6717, L/P 1257167) EMERGENCY SEAT MOUNTED LIGHTING DAMAGED / INOP / LOCATIONS:302 / ACARS TEXT: FRC335202302 / INTERIOR. REPLACED LIGHT COVER WITH SERVICEABLE. OK FOR SERVICE.
SHIP 6717 EMERGENCY LIGHTS AT SEAT 23D AND 25D INOP. CORRECTIVE ACTION: REMOVED AND REPLACED EMERGENCY LIGHTS AT SEAT 23D AND 25D. OPS CHECK GOOD. (5248692)
DUE TO FIRE/OVERHEAT SYSTEM EICAS IN FLIGHT AND DID NOT RESET. TROUBLESHOT IAW FIM, REPLACED THE LT NACELLE LP2, DETECTOR NR 1 AND AFOLTS CARD. RAN ENGS CHECKED GOOD.
PLASTIC COVER FOR OVERHEAD (OVER WING) EMERG EXIT SIGN IS MISSING. REPLACED SIGN.
PASSENGER CABIN FWD WET AREA BS 335 - 358, RBL 65, THRESHOLD SUPPORT ANGLE HAS CORROSION ON UPPER SURFACE. REMOVED CORROSION AT THRESHOLD SUPPORT ANGLE IAW SRM 51-10-02, PARA 15 (A). FOUND TO BE OUT OF LIMITS IAW SRM 53-10-15, DETAIL IV. REMOVED & REPLACED THRESHOLD SUPPORT CHANNEL IAW SRM 51-40-02, PARA 4 & DWG 141N8422, REV. R.
R2 DOOR FORWARD FRAME CRACKED AT UPPER HINGE CUT OUT IN LOWER RADIUS. REPAIRED THE R2 DOOR FORWARD FRAME IAW SRM 52-10-02, REPAIR 1, FIG 201, PRI 564964-14 REV 0, AND ER/A 564964-14 REV. ORIGINAL.
L2 DOOR FORWARD FRAME CRACKED AT UPPER HINGE CUTOUT IN LOWER RADIUS. IAW SRM 52-10-02 FIG 101 FOR ALLOWABLE DAMAGE AND REPAIR DETAILS.
PASSENGER CABIN FLOOR PANEL, R4 DOORWAY THRESHOLD AFT DRAIN HOLE BRACKET CORRODED AT FASTENER. CORROSION ON ORIGINAL BRACKET FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED WITH NEW BRACKET I.A.W. DRAWING# 146N5246 REV D. ORIGINAL METAL THICKNESS .071 AFTER BLENDING .030 REMAINS.
R2 DOOR FORWARD FRAME CRACKED AT UPPER HINGE CUTOUT IN LOWER RADIUS IAW SRM 52-10-02 FIG 101 FOR ALLOWABLE DAMAGE AND REPAIR DETAILS. REPAIRED R-2 DOOR FORWARD FRAME IAW B757-200 SRM 52-10-02 REPAIR1 FIG 201,PRI 56964-14 REV 0 & ERA 564964-14 REV ORIGINIAL.
L2 DOOR FORWARD FRAME CRACKED AT UPPER HINGE CUTOUT IN LOWER RADIUS. IAW SRM 52-10-02 FIG 101 FOR ALLOWABLE DAMAGE AND REPAIR DETAILS. REMOVED DAMAGE AND INSTALLED DOUBLER ANGLE ON THE L2 DOOR FWD FRAME AND RESTORE FINISH IAW SRM 51-40-02, AND SRM 52-10-02, REPAIR NR 1.
LEFT WING TO BODY FAIRING ATTACH BRACKETS CORRODED. REMOVED CORROSION IAW SRM 51-10-02. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-71, DETAIL VII. REMOVED AND REPLACED THE BRACKET IAW SRM 51-40-02, AND DWG 140N7210, REV C.
RIGHT WING, NR 7 SLAT OTBD MAIN TRACK WEDGE SEAL PLATE IS CRACKED. REMOVED AND REPLACED THE PLATE IAW SRM 51-40-02, AND DWG 114N4154, REV A.
LEFT WING UPPER WING ROOT, WING TO BODY FAIRING ATTACH BRACKET CORRODED. REMOVED AND REPLACED THE ATTACH FITTING IAW SRM 51-40-02, AND DWG 149N7550, REV- .
PASSENGER CABIN LT SIDE CREASE BEAM WEB BELOW AFT OVERWING EMERGENCY EXIT, OTBD EDGE HAS CORROSION BY THE 4TH RIVET FROM THE FWD EDGE. CORROSION REMOVED AND FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED THE WEB IAW SRM 51-40-02 AND DWG 144N5140.
AFT CARGO BAY DOOR BOTTOM SURROUND, FLOOR SUPPORT EDGE CORRODED INBD OF THRESHOLD. REMOVED AND REPLACED THE FLOOR SUPPORT.
RT WING TO BODY FAIRING SUPPORT BRACKET CORRODED. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-71, DETAIL VII. FABRICATED, REMOVED AND REPLACED THE BRACKET IAW SRM 51-40-02, AND DWG 149N7210, REV C.
LEFT INBD SEAT TRACK AT BS 1160 WAS FOUND GOUGED OUT OF LIMITS. REPAIRED THE SEAT TRACK IAW SRM 53-00-52, REPAIR 1.
CEILING PANEL EMERGENCY LIGHT INOPERATIVE, LT SEAT ROW 36 ABC. TROUBLESHOT, FOUND THE LT OVERHEAD ROW 36 EMERGENCY LIGHT GROUND STUD TO BE LOOSE, SECURED AND CHECKED GOOD IAW AMM 33-51 AND 33-51.
EMERGENCY LIGHT SEAT 22D BROKEN. REPLACED THE LIGHT IAW CMM 25-21-52. OPS CHECKED GOOD.
LEFT AFT CABIN DOOR WILL NOT CLOSE. FOUND THE HANDLE OUT OF SINK. RESET THE HANDLE, OPS CHECKED GOOD.
L2 DOOR EMERGENCY EXIT SIGN WAS KNOCKED OFF. REINSTALLED THE LIGHT CHECKED GOOD.
R3 DOOR HANDLE STUCK IN MIDDLE POSITION, NOT ARMING PROPERLY. REMOVED DEBRIS FROM GIRT BAR LOCKS. DOOR ARMS NORMALLY. ACFT OK FOR SERVICE IAW AMM 52-11.
R1 DOOR INTERIOR ARMING HANDLE INOPERATIVE. DOOR ARMING HANDLE OPS CHECKS GOOD. ACFT OK FOR SERVICE.
R1 DOOR WILL NOT DISENGAGED. STAYS IN THE ARMED POSITION. FOUND BUCKLE FOR SURVIVAL KIT UNDER GIRT BAR. SECURED THE BUCKLE. OPS CHECKED OK.
FOUND EMERGENCY SEAT LIGHTS INOPERATIVE FROM SEAT 18-23. FOUND POWER SUPPLY UNIT FAILED. R & R POWER SUPPLY IAW AMM 33-51. OPS CHECKED GOOD. OK FOR SERVICE.
CABIN EMERGENCY AISLE LIGHTS INOPERATIVE ROWS 18DEF-22DEF. FOUND BATTERY PACK FUSE BAD. REPLACED FUSE. OPS CHK. GOOD. I/A/W B757 AIM 33-51.
EMERGENCY FLOOR LIGHTING DAMAGED OR INOPERATIVE. LEAKING, DRIPPING FROM OVHD INTERIOR. REPLACED MISSING EMER LENS COVERS PER AMM 33-52.
FLOOR EMERGENCY LIGHT LENS DAMAGED. REPLACED LENS IAW AMM 33-52.
EMERGENCY LIGHT HAS A DAMAGED LENS . REPLACED THE LENS IAW AMM 33-52.
BROKEN EXIT SIGN COVER AT ROW 26F. SECURED THE LENS.
R1 DOOR DISARM LEVER DOESN'T MOVE ALL THE WAY TO THE NORMAL DISARMED POSITION. FOUND SLIDE PACK LANYARD UNDER GIRT BAR. CORRECTED AND ALL OPS OK.
NR 2 ENGINE PYLON AFT METAL FIRE SEAL SUPPORT ANGLE CRACKED AT INBD SIDE. REPLACED SUPPORT ANGLE IAW DWG.
POSSIBLE LIGHTNING STRIKE. NO ELECTRICAL ANOMOLIES, ALL SYSTEMS APPEARED NORMAL. INSPECTED IAW AMM 05-51-19, ON SECTION 41, NOTED 9 CONTACT POINTS ON RT SIDE. 219568. COMPLIED WITH TEMPORARY REPAIR IAW ERA 540249-14, REV ORIG AT LOCATION ID NRS 1, 3, 4, 5, 6, & 9. DAMAGE CONFINED TO RIVET HEAD ONLY, NO CRACKS ON SKIN. ALL TEMP REPAIRS ID IAW PS 900-5-1, NR 04. OK FOR SERVICES. ALSO, REF LOG 7799703. LOG DEFERRED TO MON FOR 25 FLIGHT CYCLES FROM FLIGHT 1348 06OCT15 FOR PERMANANT REPAIR. ASSOCIATED ER/A 14-540249 ADDED FOR AC 6717 C/W ERA 540249-14, REV ORIGINAL SECTION 2 PERMANENT REPAIR.
RT WING L/E SLAT OUT OF RIG. PERFORMED SLAT RIG AMM 27-81-02. PERMANENT REPAIR SECTION 1 IAW EA 530172-14, REV O.
OVERHEAD EMERGENCY LIGHT INOPERATIVE. REPLACED LIGHT ASSY. CHECKED GOOD.
AFT CABIN, RT DECKPLATE HAS MULTIPLE AREAS OF CORROSION BS 1681-1720, BL 0-RBL 54. REPAIRED IAW ER/A 521547-14, REV ORIGINAL & SRM 53-60-51, FIG 201, REP 2.
FLOORBEAM CORRODED AT BS 1640 FROM LBL 6 TO RBL 6 ON UPPER & LOWER SURFACES. COMPLIED WITH ER/A 521546-14, REV ORIGINAL.
DURING LEFT OVERWING SLIDE PNUEMATIC DEPLOYMENT TEST, LEFT ROUND CRANK HANDLE WILL NOT STAY UP AND LOCKED IN THE UNLOCK POSITION AND CRANK ROLLER DOES TOUCH PISTON ROD. R & R LT OVERWING ESCAPE SYS CRANK HANDLE IAW AMM 25-65-12-404-028. ACCOMPLISHED OPS CHECK OF LT OVERWING ESCAPE SLIDE PNUEMATIC DEPLOYMENT IAW AMM 25-65-00-715-052 OPS CHECK GOOD.
SKIN, BS 590-660, S14-19L DENTED. SKIN REPAIRED BS 590-660 BETWEEN S14-19L IAW ER/A 521537-14AD.
AFT CARGO, FLOOR SUPPORT BS 1460-1480 HAS CORROSION ON UPPER SURFACE RBL 16.
FLOORBEAM AT BS 345 CORRODED ON UPPER SURFACE LBL 12 TO INNER SUPPORT ANGLE AT R1 DOOR SILL, WITH CORROSION EDGE DAMAGE AT RBL 7.5. REMOVED CORROSION IAW SRM 53-00-51, TWO BLENDED AREAS AT RBL 3 AND 63 FOUND TO BE WITHIN LIMITS, THREE BLENDED AREAS AT LBL 12, RBL 7.5 AND RBL 36 FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51. REPAIRED BLENDED OUT OF LIMIT AREAS IAW ER/A 481634-14MA, REV "A".
AFT CARGO DOOR, LOWER INTERCOSTAL ANGLE HAS CORROSION, SECOND FROM T/E JUST AFT OF LIGHT AFT CARGO DOOR. R & R IAW SRM 51-40-05, PAGE 3, SRM 51-40-02 PAGE 21 & PAGE 7.
AFT CARGO BILGE, FRAME CORRODED, UPPER, FWD AND AFT SURFACES, BS 1460 RBL 20-LBL 26. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-07 AD 1 PG 103, DETAIL II. REMOVED, FABRICATED & INSTALLED BILGE FRAME IAW SRM 51-40-02 P 2-3, PARA 4 & P. 6-7, PARA 7D.
FOUND AREAS OF LIGHT CORROSION AND GOUGES ON SEAT TRACK, LBL 45, BS 860 - 1200. REMOVED CORROSION AND GOUGES AND FOUND IN LIMITS IAW SRM 53-00-53, FIG 101, DETAIL 1. AT BS 870 OUT OF LIMITS IAW SRM 53-00-53, FIG 101, DETAIL 1. R & R SEAT TRACK SECTION FROM BS 780-880, IAW SRM 51-40-02.
AFT CARGO DOOR LOWER WEB HAS CORROSION. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. R & R WEB IAW SRM 52-30-02, FIG 101, DETAIL III, SRM 51-40-02.
DENT ON AFT CARGO BAY FRAME AT BS 1500, S26L, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-07, FIG 101, SHEET 1. PERFORMED PERMANENT FRAME REPAIR IAW SRM 53-00-07, REPAIR 5, FIG 201.
FOUND AREAS OF LIGHT CORROSION AND GOUGES ON SEAT TRACK, LBL 24 BS 860 - 1200. REMOVED CORROSION AND GOUGES AND FOUND IN LIMITS IAW SRM 53-00-52, FIG 101, DET 1. REPLACED SEAT TRACK IAW SRM 51-40-02, PAGE 7.
APU BAY FWD BULKHEAD GOUGED FROM RT DOOR SPRING LATCH CONTACT. FOUND TO BE OUT OF LIMITS IAW SRM 53-80-08, FIG 101, REPAIR 2. CUTOUT DAMAGE AREA IAW SRM 53-80-08, FIG 101. FABRICATED DOUBLER IAW SRM 53-80-08, FIG 101. INSTALLED REPAIR DOUBLER ON FWD APU FIREWALL WEB IAW SRM 53-80-08, FIG 101, REPAIR 2.
NR 9 SLAT T/E WEDGE UPPER SURFACE HAS SEVERAL DENTS. FOUND 1 EA DENT LOCATED OSS 681.5 APPROX TO BE OUT OF LIMITS, ALL OTHER DENTS FOUND TO BE WITHIN LIMITS IAW SRM 57-43-02 ALLOWABLE DAMAGE FOR DENT DETAIL III, FIGURE 101. REPAIRED ON NR 9 SLAT T/E WEDGE.
AFT CARGO FLOOR SUPPORT BS 1460-1480 HAS CORROSION ON UPPER SURFACE RBL 16. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW ER/A 491157-14MA, REV ORIGINAL. ACCOMPLISHED REPAIR IAW SRM 51-70-11.
AFT CARGO BAY BILGE FRAME HAS MULTIPLE DENTS BS 1420, ABOVE S26L. TRIMED OUT DAMAGE. FABRICATED REPAIR, LOCATED, DRILLED, & INSTALLED REPAIR IAW SRM 53-00-07, FIG 201, REPAIR 5.
AFT CARGO, BILGE FRAME HAS DENT STA 1440, S25-26L. REPAIRED IAW SRM 53-00-07.
AFT CARGO, FLOOR SUPPORT BS 1460-1480, LBL 16 HAS CORROSION ON UPPER/LOWER SURFACE. REMOVED CORROSION, FOUND OUT OF LIMITS IAW ER/A 491157-14MA, ACCOMPLISHED REPAIR IAW SRM 51-70-11, FIG 1.
AFT BULK CARGO FLOOR SUPPORT HAS CORROSION AT STA 1510, RBL 7 ON UPPER/LOWER AND INNER SURFACES. REMOVED CORROSION ON AFT CARGO FLOOR SUPPORT AND FOUND TO BE OUT OF LIMITS IAW ERA 491157-14MA. COMPLIED WITH ERA 332525-14MA, REV D.
AFT BULK CARGO FLOOR SUPPORT HAS CORROSION AT BS 1500 - 1520, LBL 7 ON UPPER/LOWER SURFACES. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW ERA 491157-14MA. COMPLIED WITH ERA 332525-14MA, REV B FOR PERMANENT REPAIR.
NR 10 SLAT T/E WEDGE UPPER SURFACE HAS SEVERAL DENTS. REPAIRED IAW SRM 51-70-10.
AFT BULK CARGO FLOOR SUPPORT HAS CORROSION AT BS 1510, LBL 12 ON UPPER/LOWER SURFACES AREA PREVIOUSLY BLENDED. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW ERA 491157-14MA. COMPLIED WITH ERA 332525-14MA, REV B.
CORROSION UNDER TWO NUTPLATES, BOTTOM OF FLOOR SUPPORT LBL 10.45, BS 750 IN FWD CARGO BAY. REMOVED NUTPLATES, REMOVED CORROSION IAW SRM 53-00-53. FOUND TO BE WITHIN LIMITS IAW ER/A 491157-14MA. TREATED AND PRIMED IAW SRM 51-20-01. APPLIED PRIMER IAW AND INSTALLED NUTPLATES IAW SRM.
CORROSION UNDER NUTPLATE, BOTTOM OF FLOOR SUPPORT RBL 7.55 AT BS 745 IN FWD CARGO BAY. REMOVED CORROSION IAW SRM 53-00-53. FOUND TO BE WITHIN LIMITS IAW ER/A 491157-14MA. TREATED AND PRIMED IAW SRM.
CORROSION UNDER TWO NUTPLATES BOTTOM OF FLOOR SUPPORT LBL 10.45, BS 750 IN FWD CARGO BAY. REPAIRED IAW ER/A 14-491157
CORROSION UNDER NUTPLATE BOTTOM SIDE OF FLOOR SUPPORT RBL 16.1 AT BS 745 IN D CARGO BAY. REMOVED CORROSION IAW SRM 53-00-53. FOUND TO BE WITHIN LIMITS IAW ER/A 491157-14MA TREATED AND PRIMED IAW SRM. INSTALLED NUTPLATE IAW SRM.
AFT BULK CARGO FLOOR SUPPORT HAS CORROSION AT BS 1500 - 1520, LBL 2.5 ON UPPER & LOWER SURFACES. REMOVED CORROSION, FOUND TO BE WITHIN LIMITS IAW ER/A 491157-14MA.
FLOORBEAM HAS CORROSION AT BS 1661, LBL 10. REMOVED CORROSION, FOUND OUT OF LIMITS IAW SRM 53-00-51. REPAIRED IAW SRM 53-00-51, & ER/A 481634-14MA, REV A.
AFT BULK CARGO FLOOR SUPPORT HAS CORROSION AT BS 1510, RBL 12 UPPER AND LOWER SURFACE. REMOVED CORROSION IAW SRM AND IAW ERA 491157-14MA, REV ORIGINAL.
AFT BULK CARGO FLOOR SUPPORT HAS CORROSION BS 1500 - 1520, RBL 2.5 ON UPPER & LOWER AND INNER SURFACES. REMOVED CORROSION IAW SRM AND IAW ERA 491157-14MA, REV ORIGINAL.
AFT CARGO, FLOOR SUPPORT BS 1460-1480, RBL 7 HAS CORROSION ON UPPER & LOWER SURFACES. REMOVED CORROSION AND FOUND TO BE WITHIN LIMITS. CORROSION REMOVED IAW SRM 53-00-53 COMPLIED WITH ERA 491157-14 MA, REV "O".
DENT ON FWD CARGO BAY FRAME BS 580, S24L TRIMMED OUT DENT & ACCOMPLISHED PERMANENT REPAIR IAW SRM 53-00-07, FIG 201, REPAIR 5.
EXTERIOR LOWER FUSELAGE BS 639-641, FOUND TWO DENTS BETWEEN S23-24L. DENTS FOUND OUT OF LIMITS AND REPAIRED IAW SRM 53-00-01, REPAIR 2, FIG 201.
DURING LINE CHECK MX FOUND EMERGENCY LIGHT IN SEAT 45D INOPERATIVE. MX CONNECTED LOOSE CONNECTER IN SEAT 45D. OPS CHECKED OK.
VERTICAL STAB SKIN FIXED PANEL HAS THREE LIGHTNING STRIKES AT UPPER END. VERTICAL STABILIZER FWD FIN TIP REMOVED IAW SRM 51-40-02, PG 10, PARA 9. HFEC HOLE INSPECTION IAW NDTM PT.6, 51-00-16, NO CRACKS NOTED AT OPEN HOLES. FASTENERS INSTALLED IAW SRM 51-40-02 AND DWG 172N4000. VERTICAL STABILIZER FWD FIN TIP INSTALLED IAW 51-40-01, PG 10.
ON A-CHECK EMERGENCY LIGHT FOR OVERWING EXIT IDENTIFIER MOUNTED ON CEILING PANEL STA 985 WOULD NOT TEST. FOUND BATTERY ON M11648 NOT SECURE AND UNPLUGGED. SECURED BATTERY AND TESTED. ALL LIGHTS OP NORMAL.
IFE SYS EMINATING ODOR FROM CAPT SIDE SEATS 14ABC IFE SHUTOFF AT F/A PANEL ODOR DISSIPATED. COULD NOT CONFIRM FAULT INSP ALL WIRING AND CONNECTORS AT 14 AND VSEB ALSO VIS INSP 13 AND 15 ABC TURNED SYS ON, NO ODOR DETECTED IFE OPERATED NORMAL THROUGHOUT A/C BITE AND CONFIG CK RE-ADDRESSED ADBS AND REPROCESSED CONFIG AS PRECAUTION PER M 44-27-01. MCO AND PLAC REMOVED A/P 2883529.
NR 6 TIRE SEPARATED CAUSING DAMAGE TO LEFT INBOARD T/E FLAP. TIRE REMAINED INFLATED. REPLACED WHEEL ASSY AND REPAIRED DAMAGE.
FOUND BY MTC NR 5 BRAKE DAMAGE STATOR REVOLVING WITH ROTOR AND IDICATOR PIN DAMAGED. REPLACED NR 5 BRAKE ASSY AND NR 5 MAIN WHEEL ASSY.
RED EMERGENCY LIGHT BY FRONT GALLEY ON F/O SIDE COVER DAMAGED. REPLACED SAME.
DURING L/O SERVICE FOUND FORWARD 10 MAN LIFE RAFT PARTIALLY INFLATED IN STOW POSITION REPLACED SAME.