N666DN

Part: SENSOR — OUT OF ADJUST (ZONE 800) · airframe 87,412 hrs · 40,821 cycles

LEFT CENTER ENTRY DOOR EICAS MSG UPON LANDING. FOUND THE SENSOR OF THE L2 (CTR) ENTRY DOOR OPERATIVE, WOULD EXTINGUISH LIGHT & MSG WHEN OPERATED MANUALLY. SENSOR MECHANISM FOR L2 FOUND TO BE OUT OF ADJUSTMENT. ADJUSTED SENSOR S10095 IAW AMM 52-71-00-501, LIGHT & MESSAGE RELIABLY EXTINGUISH. (8108934)

Part: DOOR — FOD (ZONE 800) · airframe 87,330 hrs · 40,767 cycles

DOOR 1R WILL NOT ARM. REMOVED DEBRIS AND ARMED DOOR, OPS CHECKS NORMAL. (7624942)

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 87,188 hrs · 40,676 cycles

EMERGENCY LIGHTS AT L1 AND R1 INOP. REMOVED AND REPLACED BATTERY PACK FOR L1 AND R1 DOORS IAW B757 AMM 33-51. (7132824)

Part: OIL SYSTEM — LOST (NR 2 ENGINE) · airframe 87,135 hrs · 40,652 cycles

SHIP 666 -ATB/DE- AIR TURN BACK DUE TO #2 ENGINE LOSS OF OIL QUANTITY AND PRESSURE AROUND 10,000 FEET. ENGINE PULLED BACK TO IDLE BUT NOT SHUT DOWN UNTIL AFTER LANDING. CORRECTIVE ACTION: ENGINE REPLACED DUE TO OPERATED AT 0.0 PSI FOR APPROXIMATELY 1 MIN.

Part: POWER SUPPLY — INOPERATIVE (ZONE 200) · airframe 86,979 hrs · 40,568 cycles

SHIP 666 2L DOOR INTERIOR EMERGENCY LIGHTS INOP. CORRECTIVE ACTION: REPLACED PWR SUPPLY FUSES AND BATT PACK PER B757 AMM 33-51.(M733). EMER LIGHTS CK GOOD. (6577993)

Part: SIGN — MISSING (ZONE 200) · airframe 86,888 hrs · 40,521 cycles

SHIP 666 DOOR 2L EXIT SIGN MISSING. CORRECTIVE ACTION: PER ERA 625553-14. COMPLIED WITH SECTION I: TIME LIMITED REPAIR. R/R 2L EXIT SIGN AS PER B757 AMM 52-11; ER/ A 625553-14 REV 1R SECTION 3 PERMANENT REPAIR C/W. (7102092)

Part: GIRT BAR — OUT OF POSITION (ZONE 800) · airframe 86,698 hrs · 40,403 cycles

SHIP 666 R1 GIRT BAR FOUND OUT OF POSISTION - GIRT BAR WILL NOT ENGAGE. CORRECTIVE ACTION: REPOSITIONED GIRT BAR. ARMED/DISARMED DOOR, GIRT BAR ENGAGES/ DISENGAGES. DOOR CHECKS GOOD REF B757 AMM 52-11. (6579678)

Part: COVER — LOOSE (ZONE 200) · airframe 86,653 hrs · 40,379 cycles

SHIP 666 EMERGENCY EXIT SIGN COVER LOOSE / LOCATIONS:603 / KEEPS FALLING OFF, ONE SIDE OF PLASTIC WINDOW MISSING / INTERIOR. CORRECTIVE ACTION: RESCURED LOOSE HARDWARE. 90784601)

Part: SWITCH — DIRTY (DOOR SLIDE) · airframe 86,330 hrs · 40,164 cycles

SHIP 666 CREW ACARS REPORTED R1 DOOR WOULD NOT ARM. CORRECTIVE ACTION: CLEANED DOOR SLIDE DOOR SWITCH. OPS CHECK GOOD. REF B-757 AMM 52-71. (5383541)

Part: WARNING MESSAGE — ILLUMINATED (ZONE 800) · airframe 86,245 hrs · 40,110 cycles

SHIP 666 L2 ENTRY DOOR ANNUNCIATES ON THE EICAS DURING TAXI. CORRECTIVE ACTION: T/S PER B757 FIM 52-71 TASK 802. NO DEFECTS NOTED. CYCLED DOOR SEVERAL TIMES. INDICATIONS NORMAL. MEL/PLACARDS. (5533154)

Part: GIRT BAR — UNSECURE (L2 DOOR) · airframe 86,160 hrs · 40,062 cycles

SHIP 666 2L SLIDE GIRT BAR FELL OUT OF HOLDER. CORRECTIVE ACTION: REINSTALLED GIRT BAR IAW B757 AMM 52-11. OPN CKS OK. (9583562)

Part: COVER — LOOSE (L2 DOOR SLIDE) · airframe 86,160 hrs · 40,062 cycles

SHIP 666 L2 DOOR DOESNT SEAT PROPERLY WHEN CLOSING. L2 DOOR SLIDE COVER FOUND LOOSE AND CATCHING ON LOWER LINING NEAR GIRT BAR ATTACHMENTS, RESEATED DOOR LINING AND TIGHTENED STRAP ON L2 DOOR SLIDE COVER PER B757 AMM 52-11, DOOR OPENS/ CLOSES NML AND NO LONGER CATCHING. (9583564)

Part: GIRT BAR — OUT OF TOLERANCE (L2 DOOR) · airframe 86,153 hrs · 40,059 cycles

SHIP 666 2L GIRT BAR FAILED MINIMUM ENGAGEMENT ON FORWARD FITTING. CORRECTIVE ACTION: SUMMARY SEE NR FOR ADDITIONAL INFORMATION 080-0001:2560-01492- 0101/001 00480 REPLACED GIRT BAR REF B757 AMM 25-66. COMPLIED WITH ADJUSTMENT ON AMDS 2566-9001-2L AND AMDS2040-0191-2L, BOTH REF B757 AMM 52-11. ALSO COMPLIED WITH INSPECTIONS ON AMDS. (0367039)

Part: SNUBBER — OUT OF TOLERANCE (L2 DOOR) · airframe 86,153 hrs · 40,059 cycles

SHIP 666 DOOR 2L ROTARY SNUBBER DIMENSION INCORRECT. CORRECTIVE ACTION: SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0160:2040-0191-2L/ 001 00455 REMOVED AND REPLACED SNUBBER IAW B757 AMM 52-11-10. OPS CHECK GOOD. FULL RIG ON AMDS. (0365245)

Part: LANYARD — UNSECURE (R2 DOOR) · airframe 86,153 hrs · 40,059 cycles

SHIP 666 DOOR 2R, GREEN SLIDE LANYARD HANGING BELOW DOOR LEVEL AT GIRT BAR. CORRECTIVE ACTION: SUMMARY SEE NR FOR ADDITIONAL INFORMATION 117-0007:0591-0201/008 00424 SECURED LANYARD AS PER B757 AMM 25-66-01. (0365075)

Part: WEDGE — DAMAGED (SLAT) · airframe 86,114 hrs · 40,037 cycles

SHIP 666 AD2017-22-12WORK CRD 5740-01145-05E DURING SLAT WEDGE INSP. FOUND NBR 5 SLAT TOP OUTBOARD CORNER FAILED TAP TEST. CORRECTIVE ACTION: -APPLIED SPEED TAPE PER B757 SRM 57-43-02-1A-1 FIGURE 101 PG3 BLOCK G. CAT D TOPP 40-60-05 SECONDARY STRUCTURE WITHIN 4 INCHES . REMOVED TAPE, PAINT AND DAMAGED POTTING COMPOUND. TAP TEST GOOD. RE-POTTED SLAT #5 WEDGE DENT PER B757-200 SRM 57-43-02-1A PROCEDURE 1 ALLOWABLE DAMAGE 1. RESTORED FINISH PER B757-200 AMM 25-51-10. (9583514)

Part: LIGHT — DAMAGED (CABIN) · airframe 86,114 hrs · 40,037 cycles

AIRCRAFT 0666, OVERHEAD WARING LIGHT PANEL "EMER DOOR" LT ASSY DAMAGED. CORRECTIVE ACTION: REPLACED P5 OVERHEAD WARNING LIGHT MODULE. (LP 9583516)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 85,804 hrs · 39,856 cycles

SHIP 0666 DOOR 2L WILL NOT ARM. CORRECTIVE ACTION: PERMOED OPS CHECK ON DOOR ARMED/DISARMED 2L DOOR MULTIPLE TIMES NO FAULTS FOUND AT THIS TIME A/C OK FOR SERVICE IAW B757 AMM 52-12. (5002873)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 85,756 hrs · 39,832 cycles

2L DOOR SLIDE LIGHT INOPERATIVE. CORRECTIVE ACTION: R&R L2 DOOR LIGHT CAP PER B757 IPC 33-51-53-01. OPS CHK GOOD.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 85,765 hrs · 39,837 cycles

SHIP 666 DOOR L2 SLIDE LIGHT ALWAYS ON. CORRECTIVE ACTION: T/S L2 DOOR LIGHT AT LEFT SENSOR LOCATION, FOUND FAULTY. REMOVED AND REPLACED LT GIRT BAR PROXIMITY SENSOR PER B757 AWDM 25-66- 11. OPS CK OK. (5002837)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 85,734 hrs · 39,821 cycles

DR 2R "SLIDE" LIGHT INOPERATIVE. T/S R/R DOOR R2 SLIDE ARMED LIGHT SOCKET AND LAMP. R/R SENSOR PER B757 AMM 25-66. OPS CK GOOD.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 85,599 hrs · 39,735 cycles

SHIP 666 EMERGENCY LIGHTS INOP AT RH OVERWING EXIT AND ROWS 9, 10 & 11. CORRECTIVE ACTION: EPLACED BATTERY PACK PER B757 AMM 33-51. OPS OK. (4840061)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 85,565 hrs · 39,717 cycles

SHIP 0666 SLIDE INDICATOR LIGHT INOPERATIVE OR DAMAGED / LOCATIONS: 2R. CORRECTIVE ACTION: ARMED + DISRMED DOOR SEVERAL TIMES. 2 R DOOR SLIDE LIGHT OPERATES AS DESIGNED PER B757 52-20 AMM. (2951916)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 85,635 hrs · 39,759 cycles

SHIP 666 DURING CMV VISIT EMERGENCY PROXIMITY LIGHT FOUND DAMAGED. CORRECTIVE ACTION: REPLACED DAMAGE EMERGENCY LIGHT COVER ABOVE DOOR 2R PER B757 AMM 33-51. OPS CHK GOOD. (2931991)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 85,513 hrs · 39,686 cycles

SHIP 666 2R DOOR WILL NOT ARM COMPLETELY. SLIDE LIGHT WILL NOT TURN ON, KNUCKLE KNOCKER ONLY GOES HALF WAY ACROSS. CORRECTIVE ACTION: VERIFIED DOOR ARMING NORMAL WITH VISUAL GIRT INSPECTION. KNUCKLE KNOCKER CHECKS OK . FOUND 2R ESCAPE SLIDE ARMED LIGHT NOT FULLY SEATED. RESECURED LIGHT AND OPS CHECK GOOD. (9723966)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 85,440 hrs · 39,652 cycles

SHIP 666 EMERGENCY EXIT SIGNS INOPERATIVE / LOCATIONS: 2R. CORRECTIVE ACTION: CANNOT DUPLICATE FAULT OPS CHK NML PER B757 AMM 35-51. (2761429)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 85,421 hrs · 39,644 cycles

SHIP 666 SLIDE HARNESS DOES NOT HAVE CORRECT CHAIN CONFIG. CORRECTIVE ACTION: SLIDE OFF AND ON AND DOOR ASSIT ARE PINNED. ALL H/W ATTACHED TO NEW SLIDE OR DOOR. INSTALLED CORRECT LATCH (CHAIN) ASSY IN REF WITH AIPC 25-66-01-10 #034, ACCOMPLISHED. STEP 7 OF W/C 2566-9001-1R. C/W STEP 8-14 OF W/C 2566-9001-1R. (4119349)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 85,391 hrs · 39,628 cycles

SHIP 666 LT OVER WING EXIT LIGHTS INOP. CORRECTIVE ACTION: REMOVED AND REPLACED LT OVERWING EXIT EMERGENCY BATTERY PACK PER B757 AMM 33-51. (4119324)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 85,304 hrs · 39,580 cycles

SHIP 666 DURING SERVICE CHECK FOUND EMER. LIGHT R2 CLOSET EXIT SIGN INOP. CORRECTIVE ACTION: REMOVED & REPLACED BATTERY PACK M9325 IAW B575 WDM 33-51. OPS CHECK GOOD. (4112858)

Part: NONE — NONE · airframe 85,227 hrs · 39,528 cycles

SHIP 666 1R DOOR SLIDE PACK STRAP DETACHED. CORRECTIVE ACTION: REPLACED VELCRO AND REATTACHED SLIDE STRAP. (9901242)

Part: BOTTLE — LOW PRESSURE (R4 DOOR SLIDE) · airframe 85,163 hrs · 39,479 cycles

R4 SLIDE LOW PSI. REMOVED AND REPLACED 4R DOOR SLIDE IAW B757 TASK CARD. (9848264)

Part: DRAG FITTING — CORRODED · corrosion level 2 · airframe 84,722 hrs · 39,202 cycles

SHIP 666 A.D.//A.A. DAMAGES WERE FOUND ON OPEN HOLES AT RH ENG DRAG FTG CLAMP-UP & DIAG BRACE AS FOLLOW; HOLE #2 CORROSION ON SKIN AND FITTING BTW 2 TO 3 AND 9 TO 11 OCLOCK POSITION; HOLE #3 CRACK ON FITTING BTW 9 OCLOCK POSITION, CORROSION ON SKIN AND FITTING BTW 1 TO 4 AND 8 TO 11 OCLOCK POSITION; HOLE #4 CORROSION ON SKIN AND FITTING BTW 8 TO 10 OCLOCK POSITION; HOLE #8 CORROSION ON SKIN AND FITTING BTW 1 TO 3 AND 8 TO 9 OCLOCK POSITION, SCRATCHES ON FITTING BTW 12 OCLOCK POSITION; HOLE #9 CORROSION ON SKIN AND FITTING BTW 8 TO 11 OCLOCK POSITION, IN REF. CARD 5720-01100-04B. CORRECTIVE ACTION: SUMMARY OF NRC 00257 CORROSION LEVEL 2 HOLES AT RH ENG DRAG FITTING CLAMP-UP WERE REPAIRED PER. ER/A 599250-14AD REV. ORIGINAL SECTION I PERMANENT REPAIR AND PRI 599250-14 REV. 3. (2267325)

Part: DOOR SILL — CORRODED · airframe 84,722 hrs · 39,202 cycles

SHIP 666 DTE, ER/A 598751-14; FUSELAGE / LH NO. 2 PASSENGER DOORWAY LOWER SILL / STA. 730 -745, / CORROSION. CORRECTIVE ACTION: REF ERA 598751-14. (2267884)

Part: FLOOR SUPPORT — CORRODED · corrosion level 2 · airframe 84,722 hrs · 39,202 cycles

SHIP 666 CORROSION ON FLOOR SUPPORT ANGLE AT LBL 58. W2 BTW STA 730 AND 760 ON PAX CABIN. CORRECTIVE ACTION: SUMMARY OF NRC 00517 FLOOR SUPPORT ANGLE AT LBL 58.W2 BTW STA 730 AND 760 ON PAX CABIN WAS REPAIRED PER PRI 598751-14 REV 1. AND ERA 598751-14 REV ORIG. (2268132)

Part: SKIN — NONE · airframe 84,722 hrs · 39,202 cycles

SHIP 666 REPAIR TO RH WING UPPER SKIN COMMON TO DRAG FITTING ATTACHMENT REQUIRES SUPPLEMENTAL INSPECTIONS PER ERA 599250-14. CORRECTIVE ACTION: REF ERA 599250-14. (2266999)

Part: FRAME — DENTED · airframe 84,721 hrs · 39,201 cycles

SHIP 666 DENT ON FRAME (UPPER SIDE) AT AFT CARGO COMPARTMENT, STA. 1540, LBL 25. CORRECTIVE ACTION: SUMMARY OF NRC 00246- FRAME (UPPER SIDE) AT AFT CARGO COMPARTMENT, STA. 1540, LBL 25 WAS REPAIRED PER. B757-200 SRM. (2264702)

Part: DRAG FITTING — CORRODED · corrosion level 2 · airframe 84,721 hrs · 39,201 cycles

SHIP 666 [AD/ AA] LH ENG DRAG FITTING HOLES 11 TO 18 WERE INSPECTED AND FOLLOWING DAMAGES WERE FOUND: HOLE #13 CORROSION BTW SKIN AND FITTING BTW 2 - 4 CLOCK POS ; HOLE #17 CORROSION BTW SKIN AND FITTING AT 5 CLOCK POS. IN REF TASK CARD. CORRECTIVE ACTION: SUMMARY OF NRC 00266: HOLES #13 & #17 WERE REPAIRED PER ER/A 599264-14 PRI REV 2 & ER/A 599264-14AD REV. ORIG. (2264035)

Part: SKIN — DENTED · airframe 84,721 hrs · 39,201 cycles

SHIP 666 (AWR)DURING HFEC INSPECTION ON FUS SKIN DENT AT FUS STA 710 BTW S26R - S27R 1EA SEVERAL CRACKS WERE FOUND ON A 0.250IN DIAMETER AREA. IN REF MON/0666/2492880 JOB#152. CORRECTIVE ACTION: SUMMARY OF NRC 00620:DENT AT FUS STA 710 BTW S26R - S27R WAS REPAIRED (PERMANENT REPAIR) PER B757-200 SRM. (2264240)

Part: SKIN — DENTED · airframe 84,721 hrs · 39,201 cycles

SHIP 666 (AWR)DURING HFEC INSPECTION ON FUS SKIN DENT AT FUS STA 710 BTW S26R - S27R 1EA SEVERAL CRACKS WERE FOUND ON A 0.250IN DIAMETER AREA. IN REF MON/0666/2492880 JOB#152. CORRECTIVE ACTION: SUMMARY OF NRC 00620:DENT AT FUS STA 710 BTW S26R - S27R WAS REPAIRED (PERMANENT REPAIR) PER B757-200 SRM. (2264243)

Part: DRAG FITTING — CORRODED · corrosion level 2 · airframe 84,721 hrs · 39,201 cycles

SHIP 666 [AD / AA] LH ENG DRAG FITTING HOLES NBR 1 TO 10 WERE INSPECTED AND FOLLOWING DAMAGES WERE FOUND: HOLE #2 CORROSION ON SKIN AND FITTING BTW 2-4 CLOCK POS ; HOLE #3 CORROSION ON SKIN AND FITTING AT 10 CLOCK POS AND BTW 3 - 5 CLOCK POS ; HOLE #4 CORROSION ON SKIN AND FTG BTW 2 - 4 CLOCK POS ; HOLE #5 CORROSION BTW HOLE AND FITTING BTW 5 TO 7 CLOCK POS ; HOLE #8 CORROSION ON SKIN AND FITTING BTW 2 - 4 CLOCK POS ; HOLE #9 CORROSION BTW SKIN AND ITTING BTW 3 - 4 CLOCK POS. IN REF TASK CARD 5720-01100-04A JOB#171-0001 STEP 14B. CORRECTIVE ACTION: SUMMARY OF NRC 00265: HOLES #2 #3 #4 #5 #8 & #9 WERE REPAIRED PER ER/A 599264-14 PRI REV 2 & ER/A 599264- 14AD REV. ORIG. (2264046)

Part: FLOOR PANEL — CORRODED · corrosion level 2 · airframe 84,721 hrs · 39,201 cycles

SHIP 666 CORROSION OUT LIMITS ON SIDE PLATE FLOOR PANEL BTW STA 660 TO 700 IN REF. TO NRC 00208. CORRECTIVE ACTION: SUMMARY OF NRC 00636-CORROSION LEVEL 2- SIDE PLATE RH FLOOR PANEL BTW STA 660 TO 700 WAS REPAIRED PER B757-200 SRM. (2261863)

Part: SKIN — NONE · airframe 84,721 hrs · 39,201 cycles

SHIP 666 REPAIR TO LH WING UPPER SKIN COMMON TO DRAG FITTING ATTACHMENT REQUIRES SUPPLEMENTAL INSPECTIONS PER ERA 599264-14. CORRECTIVE ACTION: REF ERA 599264-14. (2261617)

Part: SKIN — CRACKED · airframe 84,721 hrs · 39,201 cycles

SHIP 666 CRACK ON COVE SKIN OF THE SLAT #1, OSS 810, ( ADJACENT TO OUTBD MAIN TRACK) AT LH WING. CORRECTIVE ACTION: SUMMARY OF NRC 00109: SLAT COVE SKIN WAS REPAIRED PER B757-200 SRM. (2259760)

Part: SKIN — CRACKED · airframe 84,721 hrs · 39,201 cycles

SHIP 666 CRACK ON COVE SKIN OF THE SLAT #1, OSS 810, ( ADJACENT TO OUTBD MAIN TRACK) AT LH WING. CORRECTIVE ACTION: SUMMARY OF NRC 00109: SLAT COVE SKIN WAS REPAIRED PER B757-200 SRM. (2259937)

Part: SKIN — CORRODED · corrosion level 2 · airframe 84,721 hrs · 39,201 cycles

SHIP 666 CORROSION ON INTERNAL SKIN BTW STA 560/580 AND S28L/ S28R AT FWD CARGO COMPARTMENT STRUCTURE. CORRECTIVE ACTION: SUMMARY OF NRC 00188 SKIN BTW STA 560/580 AND S28L/ S28R AT FWD CARGO COMPARTMENT STRUCTURE WAS REPAIRED PER PRI 599409-14 REV. 1 AND ER/A 599409-14 REV. ORIGINAL. (2259095)

Part: BUSHING — CORRODED · airframe 84,721 hrs · 39,201 cycles

SHIP 666 CORRISION ON INB. BUSHING AT FWD UPPER LINK ATTACH FITTING (RH PYLON). CORRECTIVE ACTION: SUMMARY OF NRC 00404. INB. BUSHING AT FWD UPPER LINK ATTACH FITTING (RH PYLON) WAS REPLACED BY A NEW BUSHING PER B757-200 SRM. (2259747)

Part: BUSHING — MIGRATED · airframe 84,721 hrs · 39,201 cycles

SHIP 666 MIGRATED OUTB. BUSHING ON FWD UPPER LINK ATTACH FITTING AT RH PYLON. CORRECTIVE ACTION: SUMMARY OF NRC 00403: UPPER LINK ATTACH FITTING AT RH PYLON WAS REPAIRED PER B757-200 SRM (2258946)

Part: SKIN — DENTED · airframe 84,721 hrs · 39,201 cycles

SHIP 666 DURING HFEC INSPECTION ON FUS SKIN DENT AT FUS STA 710 BTW S26R - S27R 1EA SEVERAL CRACKS WERE FOUND ON A 0.250IN DIAMETER AREA. CORRECTIVE ACTION: SUMMARY OF NRC 00620: SEVERAL CRACKS ON DENT AT FUS STA 710 BTW S26R - S27R WERE FOUND ON A 0.250IN DIAMETER AREA. IN REF MON/ 0666/2492880 JOB#152 WAS REPAIRED PER B757-200 SRM. (2257545)

Part: SKIN — CORRODED · corrosion level 2 · airframe 84,721 hrs · 39,201 cycles

SHIP 666 REFERENCE ER/A 599409-14 FWD CARGO COMPARTMENT / LOWER SKIN / BTW STA 560 & STA 580 AND BTW S-28R & S-28L / CORROSION. CORRECTIVE ACTION: REF ERA 599409-14. (2258649)

Part: FLOOR SUPPORT — CORRODED · corrosion level 2 · airframe 84,721 hrs · 39,201 cycles

SHIP 666 CORROSION ON FLOOR SUPPORT STRINGER (RBL 7.55) AT AFT CARGO COMPARTMENT, BTW STA. 1510, AND 1530. CORRECTIVE ACTION: SUMMARY OF NRC 00241: SUPPORT STRINGER (RBL 7.55) AT AFT CARGO COMPARTMENT, BTW STA 500 TO STA 550 WAS REPLACED PER. B757-200 SRM. (2258464)

Part: BEAM — CORRODED · corrosion level 2 · airframe 84,721 hrs · 39,201 cycles

SHIP 666 CORROSION ON BEAM UPPER CHORD AT STA 760 BTW RBL 2 TO RBL 10 ( CPAX)(W2) IN REF NRC 00525. CORRECTIVE ACTION: SUMMARY OF NRC 00660 BEAM UPPER CHORD AT STA 760 BTW RBL 2 TO RBL 10 WAS REPAIRED PER B757-200 SRM. (2253469)

Part: SNUBBER — OUT OF LIMITS · airframe 84,721 hrs · 39,201 cycles

SHIP 666 LENGTH OUT OF LIMITS (PIN EXTENSION) OF ROTARY SNUBBER AT 1L DOOR. (IN REF AMDS). CORRECTIVE ACTION: SUMMARY OF NRC 00092: OUT OF LIMITS ROTARY SNUBBER WAS REPLACED FOR A SERVICEABLE ROTATORY SNUBBER PER B757-200 AMM 52-11-10. (2254127)

Part: STRINGER — CORRODED · corrosion level 2 · airframe 84,721 hrs · 39,201 cycles

SHIP 666 EXCESSIVE CORROSION ON FLOOR SUPPORT STRINGER ( LBL 7.55) AT AFT CARGO COMPARTMENT, STA 1510, IN REFERENCE TO NRC 244. CORRECTIVE ACTION: SUMMARY OF NRC 00639, FLOOR SUPPORT STRINGER (LBL 7.55) AT AFT CARGO COMPARTMENT, STA 1510 WAS REPAIRED PER B757-200 SRM. (2251353)

Part: CHANNEL — CORRODED · corrosion level 2 · airframe 84,721 hrs · 39,201 cycles

SHIP 666 CORROSION ON CHANNEL STA 740 BTW S-28R-S-27R AT FWD CARGO COMPARTMENT. SUMMARY OF NRC 00205 CHANNEL STA 740 BTW S- 28R-S-27R AT FWD CARGO COMPARTMENT WAS REPLACED PER B757-200 SRM. (2251691)

Part: SIDEWALL PANEL — CORRODED · corrosion level 2 · airframe 84,721 hrs · 39,201 cycles

SHIP 666 CORROSION ON RH SIDE PANEL BTW STA 560/645 AT FWD CARGO COMPARTMENT STRUCTURE. CORRECTIVE ACTION: SUMMARY OF NRC 00261-RH SIDE PANEL BTW STA 560 TO 645 AT FWD CARGO COMPARTMENT STRUCTURE WAS REPLACED PER B757-200 SRM. (2251708)

Part: STRAP — MISREPAIRED · airframe 84,721 hrs · 39,201 cycles

SHIP 666 HOLE INCORRECTLY DRILLED (DISTANCE WITH ADJACENT RIVET) ON STABILIZATION STRAP AT PASSENGER FLOOR STRUCTURE (LOOKING UP FROM AFT CARGO), STA. 1520, RBL 24. CORRECTIVE ACTION: SUMMARY OF NRC 00248: STABILIZATION STRAP AT PASSENGER FLOOR STRUCTURE WAS REPAIRED PER B757-200 SRM. (2250183)

Part: ANGLE — CORRODED · corrosion level 2 · airframe 84,721 hrs · 39,201 cycles

SHIP 666 CORROSION ON ANGLE STA 786 BTW S-28L-S-28R AT FWD CARGO COMPARTMENT. CORRECTIVE ACTION: SUMMARY OF NRC 00180- ANGLE STA 786 BTW S-28L-S -28R AT FWD CARGO COMPARTMENT WAS REPLACED PER B757-200 SRM. (2249379)

Part: SEAT TRACK — CORRODED · corrosion level 2 · airframe 84,721 hrs · 39,201 cycles

SHIP 666 CORROSION ALONG LH OUTBD SEAT TRACK AT THE FOLLOW STAS: 680-700, 715 AT FLOOR STRUCTURE PASSENGER CABIN. ( IN REFERENCE NRC 00080). CORRECTIVE ACTION: SUMMARY OF NRC 00617, LH OUTBD SEAT TRACK BTW STA 660 TO STA 790 WAS REPLACED PER B757-200 SRM. (2250335)

Part: NONE — NONE · airframe 84,721 hrs · 39,201 cycles

SHIP 666 AFTER FASTENERS REMOVAL, CRACK WAS FOUND ON ANGLE BTW STA 1640 AND S-14R. CORRECTIVE ACTION: SUMMARY OF NRC 00184: CRACK ANGLE WAS REPLACED PER B757-200 SRM. (2248930)

Part: NONE — NONE · corrosion level 2 · airframe 84,721 hrs · 39,201 cycles

SHIP 666 CORROSION ON FLOOR SUPPORT STRINGER (RBL 2.90) AT AFT CARGO COMPARTMENT, STA?S 1493 AND STA . 1510. CORRECTIVE ACTION: SUMMARY OF NRC 00242: FLOOR STRINGER RBL 2.90 BTW STA 1493 WAS REPLACED PER B757-200 SRM AND CORROSION OUT OF LIMIT ON RBL 2.90 STA. 1510 WAS ATTENDET WITH NRC #00616 WITH LOG PAGE # 2246545. (2247506)

Part: NONE — NONE · corrosion level 2 · airframe 84,721 hrs · 39,201 cycles

SHIP 666 IN REF. NRC #00541: CORROSION ON FLOOR SUPPORT BTW STA 1660 TO STA 1680 AT L4 DOOR LOWER SILL. CORRECTIVE ACTION: SUMMARY OF NRC 00653: FLOOR SUPPORT BTW STA 1660 TO STA 1680 AT L4 DOOR LOWER SILL WAS REPLACED PER B757-200 SRM. (2246598)

Part: NONE — NONE · corrosion level 2 · airframe 84,721 hrs · 39,201 cycles

SHIP 666 NITIAL INSPECTION. CORROSION ON FLOOR SUPPORT STRINGER ( RBL 2.90) AT AFT CARGO COMPARTMENT STA. 1510. (IN REFERENCE NRC 00242). CORRECTIVE ACTION: SUMMARY OF NRC 00616 : FLOOR SUPPORT STRINGER (RBL 2.90) AT AFT CARGO COMPARTMENT STA. 1510 WAS REPAIRED PER B757-200 SRM. (2246592)

Part: NONE — NONE · corrosion level 2 · airframe 84,721 hrs · 39,201 cycles

SHIP 666 CORROSION ON FLOOR SUPPORT STRINGER ( RBL 2.90) AT AFT CARGO COMPARTMENT STA. 1510. (IN REFERENCE NRC 00242). CORRECTIVE ACTION: SUMMARY OF NRC 00616: FLOOR SUPPORT STRINGER (RBL 2.90) AT AFT CARGO COMPARTMENT STA. 1510 WAS REPAIRED PER B757-200 SRM 53-00-53. PERFORM A DECAL CONDITION INSPECTION EVERY. C. CHECK PER TOPP 30 -10-70. (2246545)

Part: STRINGER — CORRODED · corrosion level 2 · airframe 84,721 hrs · 39,201 cycles

SHIP 666 EXCESSIVE CORROSION ON FLOOR SUPPORT STRINGER ( LBL 7.55) AT AFT CARGO COMPARTMENT, STA 1510, IN REFERENCE TO NRC 24. CORRECTIVE ACTION: SUMMARY OF NRC 00639, FLOOR SUPPORT STRINGER (LBL 7.55) AT AFT CARGO COMPARTMENT, STA 1510 WAS REPAIRED PER B757-200 SRM 53-00-53-2R-1. (2246473)

Part: NONE — NONE · airframe 84,721 hrs · 39,201 cycles

SHIP 666 CRACK ON STABILIZATION STRAP AT PASSENGER FLOOR STRUCTURE (LOOKING UP FROM AFT CARGO), STA. 1520, RBL 45. CORRECTIVE ACTION: SUMMARY OF NRC 00247: STABILIZATION STRAP AT PASSENGER FLOOR STRUCTURE (LOOKING UP FROM AFT CARGO), STA 1520, RBL 45. WAS REPAIRED PER B757-200 SRM. (2246364)

Part: NONE — NONE · airframe 84,721 hrs · 39,201 cycles

SHIP 666 AWR. OUT OF TOLERANCE DIAMETER ON HOLE # 1, 6, 7, 10, 11, 12, 14 , 15, 16 AND 18 (0.5640") AT LH ENG DRAG FITTING. (IN REF PRI 599264-14 REV 1 FIG 1 TABLE 1 AND 2). CORRECTIVE ACTION: SUMMARY OF NRC 00644: HOLE # 1, 6, 7, 10, 11, 12, 14, 15, 16 AND 18 WERE REAMED UP TO FIRST OVERSIZE PER CARD. (2243523)

Part: NONE — NONE · airframe 84,721 hrs · 39,201 cycles

SHIP 666 WEAR ON WEB AT NAC STA 102 INB. SIDE AT RH PYLON. CORRECTIVE ACTION: SUMMARY OF NRC 00398-PREVIUS REPAIR DOUBLER ON WEB AT NAC STA 102 INB. SIDE AT RH PYLON WAS REPLACED PER B757-200 SRM. (2242910)

Part: NONE — NONE · corrosion level 2 · airframe 84,721 hrs · 39,201 cycles

SHIP 666 CORROSION ON FLOOR PANELS (121DF) OF THE FWD CARGO COMPARTMENT. CORRECTIVE ACTION: SUMMARY OF NRC 00082-CORROSION LEVEL 2-FLOOR PANEL 121DF WAS REPLACED PER B757-200 SRM. (2242642)

Part: NONE — NONE · corrosion level 2 · airframe 84,721 hrs · 39,201 cycles

SHIP 666 CORROSION ON RH FLOOR PANEL NBR 121BF AT FWD CARGO COMPARTMENT. CORRECTIVE ACTON: SUMMARY OF NRC 00085- RH FLOOR PANEL NBR 121BF AT FWD CARGO COMPARTMENT WAS REPLACED PER B757-200 SRM 53-30-53. (2242598)

Part: FITTING — CORRODED · airframe 84,721 hrs · 39,201 cycles

SHIP 666 CORROSION ON GIRT BAR FITTING OF THE R1 SLIDE DOOR. CORRECTIVE ACTION: SUMMARY OF NRC 00077: PLATE CENTER GIRT BAR AT ESCAPE SLIDE R1 DOOR WAS REPLACED PER B757-200 AMM 25-66-10. (2239600)

Part: FITTING — CORRODED · airframe 84,721 hrs · 39,201 cycles

SHIP 666 CORROSION ON GIRT BAR FITTING OF THE L4 SLIDE DOOR. CORRECTIVE ACTION: SUMMARY OF NRC 00076: PLATE CENTER GIRT BAR AT ESCAPE SLIDE L4 DOOR WAS REPLACED PER B757-200 AMM 25-66-10. (2239595)

Part: FITTING — CORRODED · airframe 84,721 hrs · 39,201 cycles

SHIP 666 CORROSION ON GIRT BAR FITTING OF THE L2 SLIDE DOOR. CORRECTIVE ACTION: SUMMARY OF NRC 00078: PLATE CENTER GIRT BAR AT ESCAPE SLIDE L2 DOOR WAS REPLACED PER B757-200 AMM 25-66-10. (2239642)

Part: NONE — NONE · corrosion level 2 · airframe 84,721 hrs · 39,201 cycles

SHIP 666 CORROSION ON ANTENNA PLATE AT AFT CARGO COMPARTMENT, STA. 1510, BTW S-28R AND S-29R. CORRECTIVE ACTION: SUMMARY OF NRC 00224, ANTENNA PLATE AT AFT CARGO COMPARTMENT, STA. 1510, BTW S-28R AND S-29R. WAS REPLACED PER ERA NO. 480021-14 REV.A. (2238159)

Part: STRINGER — CORRODED · corrosion level 2 · airframe 84,721 hrs · 39,201 cycles

SHIP 666 CORROSION ON FLOOR STRINGER 7.55 RBL BTW STA 1480 TO 1460 AFTER CARGO COMPARTMENT. CORRECTIVE ACTION: SUMMARY OF NRC 00292. REPLACED PER B757-200 SRM. (2231892)

Part: STRINGER — CORRODED · corrosion level 2 · airframe 84,721 hrs · 39,201 cycles

SHIP 666 CORROSION ON FLOOR STRINGER 7.55 RBL BTW STA 1480 TO 1460 AFTER CARGO COMPARTMENT. CORRECTIVE ACTION: SUMMARY OF NRC 00292. FLOOR STRINGER WAS REPLACED PER B757-200 SRM. (2230745)

Part: LENS — DAMAGED · airframe 84,721 hrs · 39,201 cycles

SHIP 666 EMERGENCY EXIT COVER DIFFUSER LENS DAMAGED OR MISSING / LOCATIONS:02L. CORRECTIVE ACTION: ATTACHED LENS. (2211519)

Part: NONE — NONE · airframe 84,270 hrs · 38,932 cycles

SHIP 666 FOUND EMERGENCY EXIT SIGN ABOVE R1 DOOR INOP. CORRECTIVE ACTION: FOUND GND 498 TO CONNECTOR D04530 LOOSE. SECURED CKS GOOD. (7990982)

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 84,103 hrs · 38,815 cycles

SHIP 666 EMERGENCY LIGHT EXIT ID LENS BROKEN AT DOOR 2L. CORRECTIVE ACTION: REPLACED LENS AS REQUIRED. (7382319)

Part: SENSOR — OUT OF ADJUST (L1 DOOR) · airframe 84,051 hrs · 38,790 cycles

SHIP 666 WITH L1 ENTRY DOOR OPEN, ENTRY DOORS LIGHT REMAIN EXTINGUISHED, NO ENTRY DOOR EICAS MESSAGE DISPLAYED. CORRECTIVE ACTION: ADJUSTED SENSOR PER B757 AMM 52-71-00-825-001. OPS CHK GOOD. (7773764)

Part: SINK — LEAKING (LAVATORY) · airframe 84,027 hrs · 38,779 cycles

SHIP 666 3R LAV SINK HAS LEAK. A CHARTER PAX WAS STANDING IN THE WATER HE TOUCHED THE MIRROR TO THE RIGHT OF THE LARGE MIRROR AND GOT ELECTRICALLY SHOCKED. CORRECTIVE ACTION: NO SIGN OF LEAK WATER OR ELECTRICALLY SHOCKED. OK FOR SERVICE. (7773731)

Part: SPRING — BROKEN (SWITCH COVER) · airframe 83,598 hrs · 38,503 cycles

L2 DOOR EMERGENCY LIGHT TEST SWITCH COVER SPRING BROKEN AND COVER INSTALLED UPSIDE DOWN. MAINTENANCE REPLACED GUARD SPRING AND REATTACHED COVER. SYSTEM OPERATION NORMAL.

Part: FITTING — OUT OF ADJUST (CABIN) · airframe 83,598 hrs · 38,503 cycles

DOOR 2L, GIRT BAR, AFT SLIDER FAILED ENGAGEMENT CHECK. FOUND FLOOR FITTINGS NOT PERPENDICULAR WITH GIRT BAR. ADJUSTED FLOOR FITTINGS AND GIRT BAR PER AMM 52-11-25. GIRT BAR LEAF SPRING TEST PASSED ON AMDS 2560-01492-0101.

Part: GIRT BAR — DEFECTIVE (R1 DOOR) · airframe 83,598 hrs · 38,503 cycles

1R DOOR GIRT BAR, AFT SLIDER FAILED ENGAGEMENT CHECK. REMOVED AND REPLACED DOOR1 RT GIRT BAR REF 25-66.

Part: RETAINER — DAMAGED (R2 DOOR STOP PIN) · airframe 83,598 hrs · 38,503 cycles

R2 DOOR AFT SIDE STOP PAD PIN SAFETY NOT INSTALLED CORRECTLY. REINSTALLED A NEW SPRING RETAINER AND CHECKED STOP CLEARANCE AMM 52-11.

Part: BATTERY — DISCHARGED (CABIN) · airframe 83,598 hrs · 38,503 cycles

SHIP 666 EXIT SIGN BEHIND ROW 8R W/N ILLUMINATE. CORRECTIVE ACTION: INSTALLED SERVICEABLE BATTERY ASSY IN BATTERY PACK M10568 PER B757 AMM 33-51. (6990927)

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 83,481 hrs · 38,426 cycles

CEILING EMERGENCY LIGHT AT ROW 8.5 INOPERATIVE. FOUND A BROKEN WIRE ON LIGHT ASSY. REPAIRED THE WIRE IAW WDM 33-51. OPS CHECKED GOOD.

Part: WIRE — BROKEN (SEAT 11B) · airframe 83,249 hrs · 38,282 cycles

(AIRCRAFT 666, L/P 5448655) SEAT 11B HAS BROKEN WIRE UNDER SEAT. CORRECTIVE ACTION: RECONNECTED WIRE AT SEAT 11B PER B757 SWPM 20-30-12.

Part: PUSHROD — OUT OF ADJUST (L4 GIRT BAR) · airframe 83,214 hrs · 38,260 cycles

SHIP 666 DOOR 4L HAS ISSUES OF HARD TO ARM/DISARM. CORRECTIVE ACTION: FOUND GIRT BAR PUSHROD FWD SIDE OUT OF ADJUSTMENT/ ADJUSTED PUSHROD REF. B757 AMM 52-11-25-825-001. OPS CHECKS GOOD. (1306357)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 83,190 hrs · 38,244 cycles

(AIRCRAFT 666, L/P 4996880) DURING SVC FOUND EEPL LIGHTS INOP AT EXT L1, L2, R2, R4 INTERIOR R2 SIGNS L2 SIGNS SEATS 6, 7, 8 BIG LAV AND R2 CLOSET. R/R BULBS AT LT OVERWING AND DOOR 3RT OPS CKS GOOD. R/R BOTH FWD CHARGER AND BATTERY PACKS IN OVER HEAD AT FWD GALLEY AREA REF MM 33-51. ALL LIGHTS OPS CKED GOOD. AND R/R BATTERY PACKS AT DOOR 2RT AND 2 LT. FOUND PIN PULLED R/R AFT TWO BATTERYS IN AFT GALLEY. SYSTEM OPS CKS GOOD. REF MM33-51OUT AT PLUG AT 2RT SEAT. REPINNED REF SWP CHAP 20CKS OK.

Part: SWITCH — OBSTRUCTED (L1 DOOR) · airframe 83,186 hrs · 38,243 cycles

(AIRCRAFT 0666, L/P 4996878) DOOR L1 SW WILL NOT ACTIVATE OVHD ANNUNCIATOR LIGHT. REMOVED UNWANTED MATERIAL FROM L1 DOOR LATCH PINS AND LATCH FITTINGS REF FIM FAULT CODE 52900144. OVHD ANNUNCIATOR LIGHT ILLUMINATES & EXTINGUISHES WHEN DOOR IS OPENED AND CLOSED.

Part: OVEN — MALFUNCTIONED (GALLEY) · airframe 83,126 hrs · 38,214 cycles

(AIRCRAFT 666, L/P 4996822) OVEN F103 LOUD FAN NOISE WHEN TURNED ON SOME SMOKE FROM OVEN. REMOVED AND REPLACED F103 OVEN PER AMM 25-31.

Part: UNKNOWN — UNKNOWN (L3 DOOR ARMING) · airframe 83,004 hrs · 38,144 cycles

SHIP 666 3L DOOR WILL CLOSE BUT WILL NOT ARM AT PUSH BACK. CORRECTIVE ACTION: ACTUATED ARM/DISARM LEVER. DOOR NOW ARMS NORMALLY. (4746298)

Part: WINDOW — ARCED (COCKPIT) · airframe 82,995 hrs · 38,137 cycles

SHIP 666 CA SIDE L-FWD WINDOW ARCING WITH WINDOW HEAT SWITCH ON. CORRECTIVE ACTION: SWAPPED WINDOW TEMP CONTROL SENSOR AND SPARE SENSOR. DID BIT/VERIFIY TEST ON WINDOW HEAT CONTROL UNIT ARCED IN UPPER LEFT CORNER OF L1 WINDOW. REMOVED & REPLACED L1 WINDOW IAW MM 56-11-01 401. (4746290)

Part: BATTERY — DISCHARGED (CABIN) · airframe 82,963 hrs · 38,119 cycles

SHIP 666 ON S/C FOUND EMERGENCY LIGHTS INOP AT 9,10,11. CORRECTIVE ACTION: REPLACED BATTERY AND CHARGER M10568 PER MM REF 33-51. (4746266)

Part: MECHANISM — OBSTRUCTED (GIRT BAR) · airframe 82,957 hrs · 38,114 cycles

SHIP 666 DOOR L3 WILL NOT ARM. COULD NOT MOVE ARMING LEVER TO ARMED POSITION. CORRECTIVE ACTION: CLEARED DEBRIS AND WATER FROM L3 DOOR GIRT BAR MECHANISM, WORKING ACTION NOW NORMAL. (4746260)

Part: BAR — OUT OF ADJUST (CONTACT) · airframe 82,926 hrs · 38,092 cycles

SHIP 666 RIGHT OVERWING EXIT ARMING LEVER COVER DOES NOT CLOSE. CORRECTIVE ACITON: ADJUSTED LOWER CONTACT BAR. (4746213)

Part: GIRT BAR — LACK OF LUBE (L2 DOOR SLIDE) · airframe 82,908 hrs · 38,080 cycles

SHIP 666 2L DOOR WILL NOT DISARM. LUBRICATED 2L SLIDE GIRT BAR PER B757 AMM 12-21 OPER CHECK OKAY. (5086893)

Part: TRIGGER — MALFUNCTIONED (L3 DOOR) · airframe 82,902 hrs · 38,077 cycles

L3 DOOR WILL NOT ARM. RESET L3 DOOR SLIDE TRIGGER MECHANISM IAW B757 AMM 52-11.(5086884)

Part: SLIDE — INOPERATIVE (L1 DOOR) · airframe 82,903 hrs · 38,079 cycles

L1 DOOR SLIDE INOP. REMOVED & REINSTALLED L1 DOOR SLIDE PER W/C.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 82,718 hrs · 37,960 cycles

SHIP 666 EXIT LITE ASSY ABOVE R2 DOOR MISSING CLEAR PLASTIC LENS. CORRECTIVE ACTION: REPLACED LENS ASSY OPS NRML PER B757 AMM 33-51. (5117210)

Part: LINKAGE — OUT OF ADJUST (PROX SWITCH) · airframe 82,657 hrs · 37,916 cycles

SHIP 666 1L DOOR DID NOT SHOW OPEN ON INDICATOR LIGHT ON EICAS WILL NOT TRIGGER ACARS IN TIME 2L DOOR DOSE WORK. CORRECTIVE ACTION: ADJUSTED LINKAGE ON DOOR PROX SWITCH PER AMM 52-70. (4276462)

Part: LIGHT — INTERMITTENT (CABIN) · airframe 82,610 hrs · 37,892 cycles

EMERGENCY CABIN LIGHTS COME ON ZONE 10 AFT & CABIN FLOOR OVERHEAD AND GALLEY WHEN LANDING/DECENT INTERMITTENT ON & OFF. OPS CK EMERGENCY LIGHTS PER AMM 33-51. NO TROUBLE FOUND. A/C OK FOR SVC.

Part: SPRING — BROKEN (SWITCH GUARD) · airframe 82,542 hrs · 37,848 cycles

EMERGENCY LIGHT SWITCH GUARD WAS BROKEN. FOUND THE SPRING BROKEN ON THE SWITCH GUARD. REPLACED THE GUARD.

Part: SWITCH — DEFECTIVE (L1 DOOR) · airframe 82,534 hrs · 37,840 cycles

WITH DOOR 1L OPEN ENTRY DOORS LIGHT ON PILOTS OVERHEAD NOT ILLUMINATED & NO ECAS MESSAGE. FOUND L1 DOOR SWITCH PLUNGER STUCK DOWN. FREED AND LUBRICATE, L1 DOOR ENTRY LIGHT AND EICAS INDICATIONS NOW NORMAL.

Part: LENS — BROKEN (EXIT SIGN) · airframe 82,529 hrs · 37,837 cycles

ON LANDING EXIT SIGN LENS COVER OVER DOOR 2R FELL & BROKE. REPLACED LENS PER AMM 33-51. LIGHT OPS OK.

Part: LOCKWASHER — BROKEN (GIRT BAR) · airframe 82,512 hrs · 37,829 cycles

R1 DOOR SLIDE ARM LIGHT DIDN'T ALWAYS LIGHT UP. GIRT BAR SLIDERS NOT ALWAYS TRAVELING FAR ENOUGH FOR PROPER ENGAGEMENT FROM DISARM. SLIDE REMOVED IAW TASK 2566-900HR, FOUND THE ROD END LOCK WASHER BROKEN FOR AFT GIRT BAR ARM. REPLACED THE LOCK WASHER CLAMP BUSHING. ADJUSTED THE GIRT BAR MECHANISM IAW AMM 52-11-25-825-001. OK FOR SERVICE.

Part: PIN — BROKEN (R4 DOOR SLIDE) · airframe 82,512 hrs · 37,829 cycles

R4 DOOR SLIDE, AFT UPPER PIN THREAD WAS BROKEN. REPLACED THE SLIDE IAW AMDS CARD 2566-9001-4R.

Part: PIN — DISLODGED (RT OVRWG SLIDE) · airframe 82,512 hrs · 37,829 cycles

DURING A RIGHT OVERWING SLIDE ACCESS AND MAINTENANCE CHECK, THE SLIDE RETAINER PIN AND RETENTION CORDS WERE DISLODGED. REMOVED AND REPLACED THE SLIDE IAW AMM 25-65-01.

Part: SPRING — WORN (GIRT BAR) · airframe 82,512 hrs · 37,829 cycles

1L DOOR SLIDE GIRT BAR FORWARD AND AFT SLIDER ENGAGEMENT DIMENSION IS LESS THAN .370". LEAF SPRINGS REQUIRE REPLACEMENT. REPLACED GIRT BAR REF AMM 25-66-10. GIRT BAR ADJUSTMENT TO BE ACCOMPLISHED WITH 2040-0191-1L.

Part: SPRING — WORN (GIRT BAR) · airframe 82,512 hrs · 37,829 cycles

2L DOOR SLIDE GIRT BAR FORWARD AND AFT SLIDER ENGAGEMENT DIMENSION IS LESS THAN .370". LEAF SPRINGS REQUIRE REPLACEMENT. REPLACED GIRT BAR REF AMM 25-66-10. GIRT BAR ADJUSTMENT TO BE ACCOMPLISHED WITH 2040-0191-2L.

Part: FUSE — FAILED (EMERGENCY LIGHTS) · airframe 82,475 hrs · 37,801 cycles

FOUND THE RT SIDE EMERGENCY LIGHT AFT OVERWING AND EMERGENCY AISLE LIGHT AT BS 1595 INOPERATIVE. R & R THE POWER SUPPLY M738 FUSE IAW AMM 33-51-07-962.

Part: SWITCH — STUCK (L1 DOOR) · airframe 82,301 hrs · 37,683 cycles

NO ENTRY DOORS ANNUNCIATOR, NO FWD ENTRY DOOR EICAS MESSAGE, AND NO ACARS IN TIME. FOUND THE L1 DOOR SWITCH STUCK CLOSE, CLEANED THE SWITCH IAW AMM 52-71.

Part: LENS — DAMAGED (EMERGENCY LIGHT) · airframe 81,945 hrs · 37,468 cycles

SEAT 19C EMERGENCY LIGHT WHITE LENS DAMAGED. INSTALLED A SERVICEABLE WHITE LENS IAW AMM 33-51.

Part: LENS — DAMAGED (EMERGENCY LIGHT) · airframe 81,945 hrs · 37,468 cycles

R2 DOOR EMERGENCY EXIT SIGN ABOVE DOOR DAMAGED. INSTALLED A NEW EXIT SIGN LENS IAW AMM 33-51.

Part: VANE — BROKEN (AOA) · airframe 81,403 hrs · 37,148 cycles

ON APPROACH INTO KTPK AT ABOUT 1200' MULTIPLE BIRDS HIT LEFT FWD FUSELAGE. LEFT AIRSPEED WENT TO ZERO, AOA INOP. QRH COMPLETED AND DIVERTED. INSP AIRCRAFT AND FOUND NO EVIDENCE OF A BIRD STRIKE. FOUND LT AOA VANE BROKEN OFF. REMOVED AND REPLACED LEFT AOA VANE IAW AMM 34-12. OPS CHECK GOOD. PERFORMED LOW LEVEL PITOT CHECK TO CAPTAINS SYSTEM AND AIRSPEED CHECKS GOOD.

Part: WIRE — BROKEN · airframe 81,202 hrs · 37,035 cycles

LIGHT FOR THE RT EMERGENCY ESCAPE BOTTLE PRESSURE IS INOPERATIVE. OVER WING SLIDE. REPLACED BROKEN WIRE IAW SWPM 20-30-12 ON WIRE. PERFORMED SATISFACTORY ELECTRICAL SYS PRESSURE TEST IAW AMM 25-65. REMOVED AND REINSTALLED VIP CEILING PANEL IAW AMM-25-50.

Part: SKIN — DENTED (FUSELAGE) · airframe 81,202 hrs · 37,035 cycles

DENT LOCATED AT EXTERNAL FUSELAGE 750, BETWEEN L26R & L27R. FOUND DENT TO BE OUT OF LIMITS. CUT OUT DAMAGE, FABRICATED REPAIR AND INSTALLED REF ERA 546689-14, REV O.

Part: ACTUATOR — CORRODED (L1 DOOR) · corrosion level 2 · airframe 81,201 hrs · 37,034 cycles

L-1 DOOR PNEUMATIC ACTUATOR IS CORRODED. R & R L1 DOOR PNEUMATIC ACTUATOR IAW AMM 52-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 81,201 hrs · 37,034 cycles

AFT CARGO COMPARTMENT BS 1510 FLOOR SUPPORTS LBL20-RBL 20 LOWER SURFACES AT N/P'S HAVE EXFOLIATED CORROSION AT N/P'S. REMOVED DAMAGE, FABRICATED REPAIR, AND INSTALLED IAW ERA 332525-14MA, REV E AND IAW SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 81,201 hrs · 37,034 cycles

AFT CARGO COMP BS1510, BL 0, FLOOR SUPPORT LOWER SURFACE IS EXFOLIATED CORROSION AT N/P'S. REMOVED DAMAGE AREA, FABRICATED REPAIR AND INSTALLED IAW ERA 332525-14MA.

Part: FRAME — CORRODED (BS 1480) · corrosion level 2 · airframe 81,201 hrs · 37,034 cycles

AFT CARGO COMP FRAME BS 1480 BETWEEN STR 26-27 RT IS CORRODED. AREA OUT OF LIMITS, CUT OUT DAMAGE IAW SRM. FABRICATED REPAIR AND INSTALLED IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 81,201 hrs · 37,034 cycles

AFT CARGO COMP FRAME BS 1681.8 WEB IS CORRODED BETWEEN STR 28RT-29RT. ACCOMPLISHED CORROSION REMOVAL FROM FRAME WEB BS 1681.8, STR 28RT-29RT IAW ERA 546693-14, REV O.

Part: SKIN — CORRODED (BS 1720-1787) · corrosion level 2 · airframe 81,201 hrs · 37,034 cycles

EXTERIOR SKIN BETWEEN BS 1720-1787.45 STR 25RT & 25LT HAS PITTING CORROSION. R & R EXTERIOR SKIN FROM BS 1720-BS 1787.45, STR IAW SRM & DWG.

Part: STRINGER — CORRODED (BS 1390-1410) · corrosion level 2 · airframe 81,201 hrs · 37,034 cycles

AFT CARGO COMPARTMENT STR 29RT BETWEEN BS 1390-1410 PREVIOUS REPAIR SECTION CORRODED. REMOVED CORROSION FROM STR 29R PREVIOUS REPAIR IAW SRM AREA FOUND TO BE OUT OF LIMITS IAW SRM 53-00-03. REMOVED STRINGER REPAIR SECTION, FABRICATED NEW STR SECTION, LOCATED AND DRILLED NEW STR REPAIR SECTION AND INSTALLED NEW STR REPAIR SECTION ALL IAW SRM, DWG, REV A AND ERA 479759-14, REV O.

Part: FRAME — DENTED (BS 1400) · airframe 81,201 hrs · 37,034 cycles

AFT CARGO COMP BS 1400, ABOVE STR 25 LT FRAME HAS SHARP DENT WITH UP FLANGE BENT. CUT OUT DAMAGE, FABRICATED REPAIR AND INSTALLED IAW SRM.

Part: STRINGER SPLICE — CORRODED (BS 1620) · corrosion level 2 · airframe 81,201 hrs · 37,034 cycles

AFT CARGO COMPARTMENT BS 1620, STR 30 END SPLICE IS CORRODED. REMOVED SPLICE FROM AFT CARGO COMP BS 1620, STR 30 IAW SRM, FABRICATED AND INSTALLED NEW SPLICE AT BS 1620, STR 30 IAW DWG REV C & SRM.

Part: STRINGER — CORRODED (BS 1400-1420) · corrosion level 2 · airframe 81,201 hrs · 37,034 cycles

AFT CARGO COMPARTMENT BS 1400-1420, STR 29LT LEVELING COMPOUND IN STR CHANNEL IS BLOWN-UP 2PL WITH CORROSION. FOUND MATERIAL LOSS OUT OF LIMITS REF SRM. R & R AFT CARGO COMPARTMENT STR 29 LT FROM BS1400 TO BS 1460 IAW SRM AND DWG.

Part: STRINGER — CORRODED (BS 1400-1420) · airframe 81,201 hrs · 37,034 cycles

AFT CARGO COMPARTMENT BS 1400-1420 STR 29 RT HAS CORROSION AT SPLITAND BOTH LEGS EXTENDING BACK. REMOVED CORROSION ON AFT CARGO BS 1400-1420 STRINGER 29RT IAW SRM 51-10-2 DIM 2" X 1" AREA WITH ORIGINAL THICKNESS, .140 MATERIAL LOSS, .070 MATERIAL REMAINING .070. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53. R & R STR SECTION FROM 1390 TO 1460, PN 146N3110-183, PO 666DN-00325 IAW SRM 51-40-02 & DWG 146N3305, REV A INSTALLED STR 29R IAW DWG 146N3305, REV A.

Part: STRINGER CLIP — CRACKED (BS 1440) · airframe 81,201 hrs · 37,034 cycles

BS 1440 STRINGER CLIP IS CRACKED, STR 29L. REMOVED 1440 STR CLIP, STR 29L IAW SRM 51-40-02. LOCATED AND DRILLED NEW CLIP PN 140N2001U56 PO 666DN-00347 IAW SRM 51-40-05 INSTALLED CLIP IAW DWG 146N1012, REV C.

Part: SUPPORT ANGLE — CORRODED (BS 879) · airframe 81,201 hrs · 37,034 cycles

CORRODED FRAME SUPPORT ANGLE BL0 AFT SIDE OF BS879 FRAME IN AFT SECTION OF FWD CARGO. REMOVED FRAME SUPPORT ANGLE FROM BS 879 BL 0, FABRICATED NEW FRAME SUPPORT ANGLE AND INSTALLED AT BS879 BL 0 IAW DWG 143N1023, REV B, 140N2002 REV EU AND SRM 51-40-02, SRM 51-40-05. NO FURTHER INSPECTION REQUIRED, PLEASE CLOSE LOG.

Part: SKIN — CORRODED (BS 1487) · airframe 81,201 hrs · 37,034 cycles

EXTERIOR SKIN BETWEEN BS 1787.45-BS 1862.70 STR 25RT-25L THE PITTING CORROSION. FOUND PITTING CORROSION ON ALL EXTERIOR SKIN BETWEEN BS 1783.45 TO BS 1862.70, STR 25RT TO 25LT OUT OF LIMITS IAW SRM 51-10-02, SRM 53-00-01. REMOVED FUSELAGE SKIN IAW SRM 51-40-02. LOCATED AND DRILLED NEW SKIN PN 148N3216Y1, PO 666DN-00322 IAW SRM 51-40-05 AND DWG 148N3206, REV B. INSTALLED NEW SKIN IAW DWG 148N3206, REV B AND SRM 51-40-02.

Part: STRINGER CLIP — CRACKED (BS 1420) · airframe 81,201 hrs · 37,034 cycles

BS 1420, STRINGER CLIP IS CRACKED, STR 29L. REMOVED STRINGER CLIP IAW SRM, FABRICATED REPAIR AND INSTALLED IAW SRM AND DWG.

Part: TRANSITION PANEL — CORRODED (BS 1410-1530) · airframe 81,201 hrs · 37,034 cycles

AFT CARGO COMPARTMENT BS 1410-1530 LT. TRANSITION PANEL UPPER SURFACE. REMOVED CORROSION AND FOUND TO BE WITH IN LIMITS REF SRM AND ERA 491157-14MA, REV A. PRIMED AND TOP COATED AREA IAW SRM AND AMM.

Part: SHEAR TIE — CRACKED (BS 640) · airframe 81,201 hrs · 37,034 cycles

MAIN CABIN FRAME SHEAR TIE BS 640 LT BETWEEN STR 16L TO 17L IS CRACK. R & R MAIN CABIN FRAME SHEAR TIE BS 640, LT BETWEEN STR 16L TO 17L IAW DWG, REV J, HEAT TREAT IAW FORM REV O, INSTALLED SHEAR TIE IAW DWG, REV J.

Part: FLOORBEAM — CRACKED (BS 377) · airframe 81,201 hrs · 37,034 cycles

MAIN CABIN BS 377, LBL 25 FLOORBEAM STABILIZER STRAP IS CRACK. REMOVED FASTENERS & DAMAGED SECTION OF STRAP BETWEEN BS 365-377, LBL 25 IAW SRM 53-00-51, REPAIR 12. HFEC INSP OF HOLES AND TRIM OUT IAW NDTM PT6 51-00-19 & 51-00-16 ASSET 15270, NO DEFECTS NOTED. PERFORMED DVI AT BS 365-377 LBL IAW SRM 53-00-51, REPAIR 12, STEP 4G, NO DEFECTS NOTED. FABRICATED, LOCATED, DRILLED & DEBURRED -1 STRAP 7075T6 .040 PO ST-00005636 & -2 FILLER 7075T56 .032 PO ST00006304 IAW SRM 53-00-51, REPAIR 12. ALODINED & PRIMED IAW SRM 51-20-01. INSTALLED -1 STRAP & -2 FILLER AT BS 365-377, LBL 25 IAW SRM 53-00-51, REPAIR 12. NO FURTHER INSPECTION REQUIRED.

Part: FLOORBEAM — CRACKED (BS 345) · airframe 81,201 hrs · 37,034 cycles

BS 345, BL 0, FLOORBEAM LOWER STABILIZATION STRAP IS CRACK. CP53-221-071. REMOVED FASTENERS & DAMAGED SECTION OF STRAP BS 345-324, BL0 IAW SRM 53-00-51, REPAIR 13. HFEC INSP OF HOLES & TRIM OUT IAW NDTM PT 6 51-00-19 & 51-00-16 ASSET 15270, NO DEFECTS NOTED. PERFORMED DVI AT BS 345, BL 0 FLOORBEEAM IAW SRM 53-00-51. REPAIR 13, STEP 4G NO DEFECTS NOTED. FABRICATED, LOCATED, DRILLED AND DEBURRED -1 STRAP 7075T6 .040 PO ST-00005363 & -2 FILLER 7075T6 .032 PO ST-00007152 IAW SRM 53-00-51, REPAIR 13, ALODINED & PRIMED IAW SRM 51-20-01. INSTALLED -1 STRAP & -2 FILLER AT BS 324-345, BL0 IAW SRM 53-00-51, REPAIR 13. NO FURTHER INSPECTION REQUIRED

Part: SHEAR TIE — CRACKED (BS 580) · airframe 81,201 hrs · 37,034 cycles

MAIN CABIN FRAME SHEAR TIE BS 580 LT BETWEEN STR 14L TO 15L IS CRACK. REMOVED DAMAGED SHEAR TIE FROM BS 580 STR 14-15 LT, FABRICATED NEW SHEAR TIE & INSTALLED SHEAR TIE IAW SRM AND DWG, REV C & EV.

Part: SHEAR TIE — CRACKED (BS 600) · airframe 81,201 hrs · 37,034 cycles

MAIN CABIN FRAME, BS 600 LT BETWEEN STR 14L TO 15L SHEAR TIE CRACKED. REMOVED DAMAGE AND FABRICATED REPAIR AND INSTALLED IAW SRM AND DWG REV D AND REV EV.

Part: FLOOR SUPPORT — CORRODED (BS 324-350) · corrosion level 2 · airframe 81,201 hrs · 37,034 cycles

FLOOR SUPPORT IN MAIN CABIN CORRODED BS 324-350, BL 0. FOUND CORROSION TO BE OUT OF LIMITS IAW SRM. R & R FLOOR SUPPORT IAW DWG REV B AND REV CD.

Part: FLOOR SUPPORT — CORRODED (BS 324-350) · corrosion level 2 · airframe 81,201 hrs · 37,034 cycles

MAIN CABIN FLOOR SUPPORT CORRODED BETWEEN BS 324 - 350. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM. R & R FLOOR SUPPORT IAW DWG, REV B AND CD.

Part: ROD END — CORRODED (LT ELEVATOR) · airframe 81,201 hrs · 37,034 cycles

LT ELEVATOR OTBD. PCA PGO ROD END CORRODED. R & R LT ELEVATOR OTBD PCA POGO ROD IAW AMM 27-31-06, FUNCTIONALLY CHECK/ADJUSTMENT WILL BE ACCOMPLISHED ON N/R

Part: FLOOR SUPPORT — CORRODED (BS 375) · corrosion level 2 · airframe 81,201 hrs · 37,034 cycles

FLOOR SUPPORT CORRODED AT BS 375, LBL 61. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM. FABRICATED REPAIR AND INSTALLED IAW SRM AND DWG, REV C.

Part: FLOOR SUPPORT — CORRODED (BS 324-350) · corrosion level 2 · airframe 81,201 hrs · 37,034 cycles

MAIN CABIN FLOOR SUPPORT CORRODED BETWEEN BS 324 & 350, LBL 30. R & R THE FLOOR SUPPORT IAW DWG, REV C.

Part: FLOORBEAM — CORRODED (BS 333) · airframe 81,201 hrs · 37,034 cycles

MAIN CABIN BS 333, FLOORBEAM ANGLE CORRODED. R & R THE FLOORBEAM ANGLE IAW DWG, REV C.

Part: FLOOR SUPPORT — CORRODED (BS 324-345) · corrosion level 2 · airframe 81,201 hrs · 37,034 cycles

BS 324-345, LBL 24 FLOOR SUPPORT CORRODED. R & R THE FLOOR SUPPORT IAW DWG AND SRM.

Part: FLOOR SUPPORT — CORRODED (BS 680-700) · corrosion level 2 · airframe 81,201 hrs · 37,034 cycles

MAIN CABIN FLOOR SUPPORT CORRODED BETWEEN BS 680-700, LBL 60. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. REMOVED FLOOR SUPPORT IAW SRM 51-40-02. FABRICATED NEW GUTTER SUPPORT IAW DWG. LOCATED & DRILLED NEW GUTTER SUPPORT & DETAIL IAW SRM. TREATED, PRIMED & TOPCOATED SUPPORT & DETAIL IAW SRM AND AMM 51-21. INSTALLED NEW GUTTER SUPPORT & DETAIL AT BS 680-BS 700, LBL 60 IAW SRM.

Part: FLOORBEAM — CORRODED (BS 345) · corrosion level 2 · airframe 81,201 hrs · 37,034 cycles

BS 345 FLOORBEAM IS CORRODED AT LBL 20. FOUND TO BE OUT OF LIMITS. CUT OUT DAMAGE, FABRICATED REPAIR AND INSTALLED REF SRM.

Part: FLOOR SUPPORT — CORRODED (BS 345-365) · airframe 81,201 hrs · 37,034 cycles

BL 0 FLOOR SUPPORT IS CORRODED BS 345-365. FOUND TO BE OUT OF LIMITS IAW SRM. R & R FLOOR SUPPORT IAW SRM AND DWG.

Part: FLOOR SUPPORT — CRACKED (BS 345-365) · corrosion level 2 · airframe 81,201 hrs · 37,034 cycles

MAIN CABIN FLOOR SUPPORT CRACKED BETWEEN BS 345-365, RBL 24. R & R MAIN CABIN FLOOR SUPPORT BETWEEN BS 345-365, RBL 24 IAW SRM AND DRW, FOUND CRACKED AND CORRODED.

Part: SEAT TRACK — CORRODED (BS 476-478) · airframe 81,201 hrs · 37,034 cycles

MAIN CABIN SEAT TRACK BS476-BS478 LBL45, FOUND OUT OF LIMITS PER DELTA J/C. CORRECTIVE ACTION: CUT OUT APR DIM 50", FABRICATED REPAIR PARTS & INSTALLED NEW SEAT TRACK SECTION & SPLICE BETWEEN BS 440 TO 490 LBL 45 IAW SRM.

Part: FLOOR SUPPORT — CORRODED (BS 1660-1681) · airframe 81,201 hrs · 37,034 cycles

MAIN CABIN FLOOR SUPPORT CORRODED BETWEEN BS 1660-1681 LBL 52CP53-251-01I. REMOVED CORROSION ON MAIN CABIN FLOOR SUPPORT BETWEEN BS 1660-1681, LBL 52 IAW SRM 51-10-02 AREA WITH MATERIAL LOSS 100 PERCENT. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51. R & R FLOOR SUPPORT, PN 146N5246U5, PO 666DN00161 IAW SRM 51-40-02 AND DWG 146N5230, REV.

Part: FLOORBEAM — CORRODED (BS 377) · airframe 81,201 hrs · 37,034 cycles

MAIN CABIN T CAP ON FLOORBEAM CORRODED BS 377.7, BL0-LBL5. REMOVED CORROSION AT EXISTING REPAIR FOUND TO BE 100 PERCENT OUT OF LIMITS IAW SRM 53-00-51, REMOVED EXISTING REPAIR AT MAIN CABIN FLOORBEAM T CAP BS 377.7 IAW SRM 53-00-51. REPAIR 3, INSTALLED REPAIR PARTS MAIN CABIN T-CAP ON FLOORBEAM AT BS 377.7, BL 0-LBL 5 IAW SRM 53-00-51, REPAIR 3, THIS IS A CATEGORY A REPAIR, NO FURTHER INSPECTION REQUIRED, PLEASE CLOSE.

Part: FLOOR SUPPORT — CORRODED (BS 1660-1681) · corrosion level 2 · airframe 81,201 hrs · 37,034 cycles

MAIN CABIN FLOOR SUPPORT CORRODED BETWEEN BS 1660-1681, RBL 52. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. REPLACED FLOOR SUPPORT PN 146N5246U6, PO 666DN-00161 IAW SRM AND DWG, REV D.

Part: SEAT TRACK — CORRODED (BS 377) · corrosion level 2 · airframe 81,201 hrs · 37,034 cycles

MAIN CABIN SEAT TRACK, BS 377, RBL 22, HAS CORROSION. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. REMOVED SEATTRACK IAW SRM LOCATED & DRILLED NEW SEATTRACK IAW SRM. INSTALLED NEW SEATTRACK IAW SRM AND DWG REV A.

Part: SKIN — DENTED (FUSELAGE) · airframe 81,654 hrs · 37,304 cycles

DENT FOUND ON FUSELAGE NEAR 2L DOOR JUST BELOW WING ILLUMINATION LIGHT. CUT OUT DAMAGED SKIN SECTION FROM BS570 TO BS660 BETWEEN STR 14-19LT, FABRICATED NEW SKIN SECTION, SPLICES & DOUBLER, INSTALLED REPAIR PARTS IAW SRM 53-30-01 REPAIR 2, SRM 51-20-01, SRM 51-40-08, SRM 51-40-05 & ERA 546672-14AD REV O.

Part: FLAP TRACK — CORRODED (NR 2 FLAP) · airframe 79,989 hrs · 36,533 cycles

NR 2 FLAP TRACK RUSTED AT AFT ATTACH POINT AT WING TO TRACK INTERFACE. SUMMARY NR FOR ADDITIONAL INFORMATION 001-0264:2020-2718/024 -00106 COMPLETED INSTALLATION/OP'S OF NR 2 FLAP TRACK REF AMM 27-51-15 AND COMPLETED INSTALLATION/OP'S OF NR 2 FLAP TRANSMISSION REF AMM 27-51-17.

Part: TUBE — CORRODED (LT MLG WW) · airframe 79,989 hrs · 36,533 cycles

LT WHEEL WELL INBD FLAP. TUBE THAT CONNECTS THE CARRIAGE TO THE FLAP HAS RUST ON THE FLAP SIDE. REPLACED OUTER TORQUE TUBE, FAIL SAFE TORQUE TUBE AND SUPPORT FITTINGS, REF EA 06-097981-14, REV A.

Part: ATTACH ANGLE — CORRODED (HORIZONTAL STAB) · airframe 79,989 hrs · 36,533 cycles

LEFT HORIZONTAL STABILIZER OTBD PCA POGO AFT ATTACH POINT RUSTED. REPLACED 1 BOLT, WASHER AND NUT LOCATED ON THE LT HORIZONTAL STAB OTBD POGO AFT ATTACH POINT REF. AMM 27-31-05.

Part: INTERCOSTAL — CORRODED (BS 1360-1380) · airframe 79,989 hrs · 36,533 cycles

INTERCOSTAL CORRODED BETWEEN BS 1360 AND 1380 AND BETWEEN STR 26 AND STR 27. REPLACED INTERCOSTAL REF B757, SRM 51-10-02.

Part: SKIN — DAMAGED (BS 500-508) · airframe 76,846 hrs · 35,129 cycles

FUSELAGE SKIN AT S-27L, BS 500-508 DAMAGED. REPAIRED IAW ERA 514752-14, REV A

Part: SKIN — DAMAGED (BS 660) · airframe 75,752 hrs · 34,731 cycles

FUSELAGE SKIN & BUTT SPLICE STRAP, BS 660 & S-28R, SHEARED FASTENER HEAD & CORROSION. REF ERA ER/A 516096-14, REV A.

Part: PUMP — FAILED (FUEL CELL) · airframe 75,572 hrs · 34,661 cycles

DIVERTED DUE TO CENTER TANK FUEL PUMPS. REPLACED LEFT PUMP AND REPAIRED RIGHT PUMP SHIELD GROUND, BOTH OPS NORMAL.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 75,346 hrs · 34,549 cycles

EMERGENCY EXIT COVER DIFFUSER LENS DAMAGED, WIRES HANGING OUT. FOUND OVERWING EXIT COVER MISSING. COVER REPLACED. OK FOR SERVICE IAW AMM 33-51.

Part: CONTROLLER — FAULTED (CABIN PRESSURE) · airframe 74,976 hrs · 34,375 cycles

DUE TO CABIN ALTITUDE, AUTO 1 AND CABIN ALTITUDE AUTO 2 EICAS MESSAGES WITH NO CONTROL OF CABIN PRESSURE IN EITHER MODE. BITE CHECK OF CONTROLLERS FOUND CONTROLLER FAULT ON EACH ONE. REPLACED BOTH CABIN PRESSURE AUTO CONTROLLERS IAW AMM 21-31 AND CHECKED OK.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 74,892 hrs · 34,346 cycles

LOWER CARGO BAY FLOOR PANELS DAMAGED. R & R IAW DWG 45N1805-157, FAB.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 74,479 hrs · 34,160 cycles

RED AND WHITE SEAT MOUNTED EMERGENCY LIGHT INOPERATIVE. INSTALLED NEW SPLICE IAW AMM 20-36, OPS CK GOOD OF BOTH LIGHTS.

Part: BALL SCREW — CORRODED (RT TE FLAP) · corrosion level 2 · airframe 73,683 hrs · 33,852 cycles

RT INBD FLAP BALL SCREW CORRODED. R & R FLAP BALL SCREW, AMM 27-51.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 73,588 hrs · 33,812 cycles

EMERGENCY LIGHT INOPERATIVE AT 4CD. REPLACED LIGHT ASSY. OPS CHECKED GOOD.

Part: SENSOR — OUT OF ADJUST (FWD LT DOOR) · airframe 73,331 hrs · 33,721 cycles

ON TAXI AN EMERGENCY DOOR LIGHT ILLUMINATED. AMM TASK 52-71 FOUND FWD LT EMERGENCY EXIT HATCH SENSOR OUT OF ADJUSTMENT. ADJUSTED IAW AMM TASK 52-71. NO CURRENT FAULTS.

Part: WARNING LIGHT — FALSE ACTIVATION (EMERGENCY EXIT) · airframe 73,324 hrs · 33,719 cycles

EMERGENCY DOOR LIGHT ILLUMINATED INTERMITTENTLY. CHECKED SECURITY OF DOORS, NO PROBLEM FOUND, COULD NOT DUPLICATE PROBLEM.

Part: SKIN — DAMAGED (BS 1600) · airframe 73,709 hrs · 33,862 cycles

FUSELAGE SKIN, BS 1600 / BETWEEN S27-28L GOUGED AND DENTED. REPAIRED IAW ERA 516903-14. TRIMMED DAMAGED AREA OF SKIN IAW SRM 53-00-01. MADE INSURANCE CUT AND FABRICATED REPAIR. TREATED AND PAINTED REPAIR IAW SRM 53-00-01.

Part: LIGHT — INOPERATIVE (26D SEAT) · airframe 72,838 hrs · 33,543 cycles

PASSENGER SEAT 26D, EMERGENCY SEAT MOUNTED, LIGHTING DAMAGED. EMER LIGHT DANGLING FROM SEAT, BROKEN. REPLACED BULBS AND LENS. RESTOWED LOOSE WIRING, OPS CHECKED GOOD.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 71,907 hrs · 33,161 cycles

FOUND SEAT ROW 22DEF AND 25DEF EMERGENCY LIGHTS INOPERATIVE. FOUND BROKEN WIRES AT HARNESS TO LIGHT ASSY AT BOTH SEAT LOCATIONS. REPLACED HARNESSES AND TESTED EMERGENCY LIGHTS. ALL LIGHTS OPS OK.

Part: RIVET — MISSING (LT EXHAUST DUCT) · airframe 71,360 hrs · 32,927 cycles

RIVET AFT FAIRING EXHAUST OF LT ENGINE MISSING. REPLACED MISSING RIVET IAW SRM 54-51.

Part: WIRE — CUT (CABIN) · airframe 68,059 hrs · 31,482 cycles

LINE MAINTENANCE FOUND EMERGENCY PATH LIGHTS AT FORWARD GALLEY INOPERATIVE BECAUSE WIRES HAD BEEN ACCIDENTLY SEVERED. WIRES SPLICED AND EMERGENCY PATH LIGHTS OPERATION NORMAL.

Part: LIGHT — BROKEN (CABIN) · airframe 67,622 hrs · 31,268 cycles

SDR - EMERGENCY LIGHT ASSY AT SEAT 42 DEF BROKEN. REMOVED AND REPLACED EMERGENCY LIGHT ASSY SHROUD AT SEAT 42 DEF IAW B757-SRM 51-40-02PG 1 AT SAA/SAT DURING PSV18 ON N/R 190236 W/O 88954530001.

Part: DOUBLER — DENTED (FUSELAGE) · airframe 67,622 hrs · 31,268 cycles

DENT ON REPAIR DOUBLER FUSELAGE STA 616 TO 630 S15-17L. ACCOMPLISHED ERA 496632-14 REV A.

Part: WIRE — DAMAGED (CABIN) · airframe 65,735 hrs · 30,497 cycles

DURING A LAYOVER CHECK, MAINTENANCE FOUND THE EMERGENCY PATH LIGHTS FROM ROWS 28 TO 37 INOPERATIVE. MAINTENANCE REPAIRED THE WIRING NEAR SEAT 27F. OPERATIONAL CHECK WAS GOOD.

Part: WIRE — BROKEN (CABIN) · airframe 65,482 hrs · 30,397 cycles

DURING A LAYOVER CHECK, MAINTENANCE FOUND THE EMERGENCY PATHLIGHTS AT 21D INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE. OPERATIONAL CHECK WAS GOOD. (2011-D0209)

Part: LIGHT — INOPERATIVE (SEAT 26D) · airframe 65,470 hrs · 30,394 cycles

DURING A LAYOVER CHECK, MX FOUND THE EMERGENCY PATHLIGHT AT SEAT 26D INOPERATIVE. MX REPLACED THE LIGHT ASSY. OPS CHECK WAS GOOD.

Part: ATTACH FITTING — DAMAGED (NR 2 PYLON) · airframe 62,849 hrs · 29,193 cycles

NR 2 PYLON NEW SIDE LINK ATTACH FITTING P.N. 012N88887-10 HOLE NR 3 ANGLE MEASURE 94.4 DEGREE PER STEP 16 CONTACT ENGINEERING FOR INSTRUCTIONS / ACCOMPLISHED ERA 479772-14AD REV ORG AT SAA SAT REF NON ROUTINE 148876.

Part: SKIN — DAMAGED (NR 2 PYLON) · airframe 62,849 hrs · 29,193 cycles

AFTER REMOVAL OF LT SKIN ON NR 2 PYLON FOUND 1 EA OVERSIZE HOLE AT STA 107 / ACCOMPLISHED ERA 479549-14 REV ORIGINAL AT SAT SAA REF NON ROUTINE CARD 157703.

Part: TRIPLER — CORRODED (BS 1460-1480) · airframe 62,849 hrs · 29,193 cycles

AFTER REMOVAL OF ANTENNA AT 1460-1480 & 30 AND 29R FOUND CORROSION ON EXTERNAL TRIPLER / REPLACED TRIPLER AT SAT SAA REF NON ROUTINE CARD 157572

Part: GATE — CORRODED (L-1 DOOR) · airframe 62,849 hrs · 29,193 cycles

L-1 DOOR UPPER GATE, INSIDE POCKET HAS CORROSION / REPLACED L-1 DOOR UPPER GATE AT SAT SAA REF NON ROUTINE 148850.

Part: FLOORBEAM — CORRODED (BS 758) · airframe 62,849 hrs · 29,193 cycles

CORROSION ON MAIN CABIN FLOOR STRUCTURE BOX BEAM BETWEEN STA 758, LBL 18 AND LBL 40 / REPLACED FLOOR STRUCTURE BOX BEAM AT SAT SAA REF NON ROUTINE CARD 151033

Part: CUSP WEB — CORRODED (BS 940 LBL 68) · airframe 62,849 hrs · 29,193 cycles

CUSP WEB CORRODED AT STA 940 LBL 68 AND WL 208 / REPLACED CUSP WEB AT SAT SAA REFERENCE NON ROUTINE CARD 147822

Part: BULKHEAD — DAMAGED (NR 1 NACELLE) · airframe 62,849 hrs · 29,193 cycles

CHAFING MARK ON #1 PYLON AFT BULKHEAD, NAC STA 201.02 L/H LOWER CORNER / ACCOMPLISHED ERA 479553-14AD REB B AT SAT SAA REF NON ROUTINE 151013

Part: BULKHEAD — CHAFED (NR 2 NACELLE) · airframe 62,849 hrs · 29,193 cycles

CHAFING MARD ON NR 2 STRUT AFT BULKHEAD, NAC STA 201.02, LT LOWER CORNER / ACCOMPLISHED ERA 479555-14AD REB B AT SAA SAT REF NON ROUTINE CARD 151012.

Part: BULKHEAD — DAMAGED (NR 2 NACELLE) · airframe 62,849 hrs · 29,193 cycles

CHAFING MARK ON NR 2 STRUT AFT BULKHEAD NAC STA 201 RT LOWER CORNER / ACCOMPLISHED ER/A 479554-14AD REV B AT SAT SAA REF NON ROUTINE 145882.

Part: WEB — CORRODED (BS 1675-1720) · airframe 62,849 hrs · 29,193 cycles

AFT GALLEY AREA SUB FLOOR SKIN WEBB HAS AREAS OF CORROSION FROM STA 1675 TO 1720 BETWEEN BL 0 AND RBL 60 / REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR DOUBLERS AT SAT SAA REF NON ROUTINE CARD 151147.

Part: WEB — CORRODED (BS 1675-1720) · airframe 62,849 hrs · 29,193 cycles

AFT GALLEY AREA SUB FLOOR SKIN WEB HAS AREAS OF CORROSION FROM STA 1675 TO 1720 BETWEEN BL 0 AND LBL 60 / REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR DOUBLERS AT SAA SAT REF NON ROUTINE CARD 151146

Part: FLOORBEAM — CORRODED (BS 345) · airframe 62,849 hrs · 29,193 cycles

BS 345 FLOORBEAM UPPER CAP HAS CORROSION BETWEEN LBL 20 TO RBL65 / REMOVED DAMAGED FLOORBEAM UPPER CAP AND REPAIRED AT SAT SAA REF NON ROUTINE 148194.

Part: FLOORBEAM — CORRODED (BS 377 BL 0) · airframe 62,849 hrs · 29,193 cycles

STA 377 FLOORBEAM HAS CORROSION FROM BL-0 TO LBL 65 / REPAIRED FLOORBEAM AT SAT SAA REF NON ROUTINE 148821

Part: FLOOR SUPPORT — CORRODED (BS 340-365) · airframe 62,849 hrs · 29,193 cycles

FLOOR SUPPORT ANGLE BETWEEN STA 340 AND 365 BL-0 HAS CORROSION UPPER TO LWR SIDES / REPLACED FLOOR SUPPORT ANGLE AT SAT SAA REF NON ROUTINE CARD 148195

Part: INTERCOSTAL — CORRODED (BS 1500-1520) · airframe 62,849 hrs · 29,193 cycles

AFT CARGO INTERCOSTAL CORRODED ENTIRE LENGTH OF LOWER LEG BETWEEN STA 1500 & 1520 BETWEEN STR 30 & 29 LT / REPLACED INTERCOSTAL AT SAT SAA REF NON ROUTINE 147963

Part: INTERCOSTAL — CORRODED (BS 1430-1440) · airframe 62,849 hrs · 29,193 cycles

AFT CARGO INTERCOSTAL BETWEEN STA 1430 & 1440 CORRODED ON ENTIRE SURFACE BETWEEN STR 28L & 29L / REMOVED AND REPLACED INTERCOSTAL AT SAT SAA REF NON ROUTINE CARD 150386

Part: SEAT TRACK — CRACKED (BS 1320 LBL 45) · airframe 62,849 hrs · 29,193 cycles

MAIN CABIN SEAT TRACK CRACKED IN UPPER FWD RADIUS OF LOWER T-CHORD SECTION AFT SIDE OF STA 1320 FLOORBEAM LBL 45 / REMOVED DAMAGE, FABRICATED AND INSTALLED SEAT TRACK SEGMENT AND SPLICE AT SAA SAT REF NON ROUTINE CARD 147886

Part: SKIN — DAMAGED (BS 345-350) · airframe 62,849 hrs · 29,193 cycles

3 EA LIGHTNING STRIKES, 2 EA ON FUSELAGE SKIN NEXT TO PREVIOUS LIGHTNING STRIKE REPAIR RIVETS AND 1 EA ON EXISTING FASTERNER AT STA 345, 349 & 350 BETWEEN STR 23L & 24L / REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR DOUBLERS AT SAA SAT REF NON ROUTINE CARD 148780

Part: STRUCTURE — DAMAGED (BS 620 S16L) · airframe 62,849 hrs · 29,193 cycles

STA 620 AT STR 16L CREASE AT SHEAR TIE AND DENT AT STRINGER 6" AFT / REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR AT SAA SAT REF NON ROUTINE 150382

Part: DUCT — OBSTRUCTED (INSTRUMENT PANEL) · airframe 58,137 hrs · 26,866 cycles

ON TAXI OUT HAD ELECTRICAL SMELL IN COCKPIT. FOUND BLOCKAGE IN COOLING TUBE TO CAPT'S VOR/DME CONTROL PANEL. CLEARED BLOCKAGE. ALSO, REPLACED CAPT'S VOR/DME CONTROL PANEL WHICH WAS CAUSE OF SMOKE FROM OVERHEAT. PANEL REPLACED WAS MFG NR 285T0554-5, S/N DO3712.

Part: FAN — SMOKE (CABIN) · airframe 56,442 hrs · 26,067 cycles

LT RECIRC FAN INOP. LT RECIRC FAN NOISY CAUSING SMOKE IN CABIN. NEED DL P/N 216001033 FWD TO MCO/PLAC PER MEL 21-25-01B. REMOVED LT FAN 964727. INSTALLED LT RECIRC FAN, OPS NML MCO A PLAC REMOVED.

Part: TIRE — SEPARATED (NR 2 MLG WHEEL) · airframe 46,272 hrs · 22,069 cycles

SUSPECT TIRE FAILURE ON T/O. REPLACED NR 2 MAIN WHEEL ASSY PER M/M TIRE CAP FAILURE. TIRE PRESS OK ON ARRIVAL.

Part: RECEIVER — OVERHEATED (E/E BAY) · airframe 45,324 hrs · 21,662 cycles

CREW REPORTED FUMES IN CABIN AND FLIGHT DECK DURING CRUISE. TURNING OFF UTILITY BUSSES ALLOWED ODOR TO DISSIPATE. CREW ELECTED TO DIVERT INTO IAD (ATL-PVD FLIGHT). DL MTC AND FLT CREW REPORTED FINDING LT ILS RECEIVER CIRCUIT BREAKER TRIPPED. FURTHER MTC INSPECTION OF ILS RECEIVER SHOWED UNIT TO HAVE FAILED/SMOKED AND EMINATING STRONG ODOR. REPLACED TRANSCEIVER.

Part: SKIN — DENTED (FUSELAGE) · airframe 41,180 hrs · 19,963 cycles

THE FUSELAGE SKIN WAS FOUND WITH SEVERAL DENTS BETWEEN FS 620 & 640 AND BETWEEN STRINGERS 15L & 17L. THE CREASE BEAM AT STRINGER 16L WAS DENTED. THE SKIN DENTS WERE REMOVED WITH CUTOUTS AND A SECTION OF THE CREASE BEAM WAS CUTOUT TO REMOVE DAMAGE. THE BEAM WAS REPAIRED, REPAIR ANGLES AND THE SKIN WITH A SINGLE ALUMINUM REPAIR DOUBLER PER ER/A 384312-14, REV C.

Part: WIRE — BROKEN (CABIN) · airframe 39,258 hrs · 19,060 cycles

EMERGENCY LIGHTS INOP AT R4 AND L4 EXTERIOR EGRESS, 45DEF OVERHEAD AND BOTH AFT RIGHT LAV MODULE. FOUND BROKEN WIRE BETWEEN SEAT ROWS 44 AND 45DEF. REPAIRED WIRE, ALL EMERGENCY LIGHTS NOW CHECK NORMAL.

Part: WIRE — BROKEN (CABIN) · airframe 38,825 hrs · 18,838 cycles

EMERGENCY EVACUATION LIGHTING. SEAT 3C, LIGHT INOPERATIVE. C/A FOUND WIRE BROKEN. REPAIRED SAME.

Part: BULB — BURNED OUT (EXTERIOR) · airframe 38,751 hrs · 18,799 cycles

4L AND 4R DOOR EXTERIOR EMERG LITES OUT C/A RELAMPED

Part: SKIN — TORN (BS 520-540)

THE FUSELAGE SKIN WAS TORN AND GOUGED AT STRINGER 16L BETWEEN FS 520 TO 540 DUE TO CONTACT WITH A JETWAY. THE DAMAGED SKIN WAS CUTOUT OVER A 24 INCH LONG AREA. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER INSTALLED PER ER/A 366403-14.

Part: SKIN — DENTED (BS 625)

THE FUSELAGE SKIN AT FS 625 WAS FOUND WITH AN OIL CANNED DENT BETWEEN STRINGERS 16L AND 17L. THE DAMAGED AREA OF SKIN WAS CUTOUT AND AN EXTERNAL ALUMINUM REPAIR DOUBLER WAS INSTALLED. THE REPAIR WAS ACCOMPLISHED PER ER/A 365010-14.

Part: PUMP — FAILED (HYD SYSTEM)

PRIOR TO TAKEOFF, ELECTRICAL PUMP OVERHEAT LIGHT ILLUMINATED, FOLLOWED BY A LOSS OF ALL LEFT HYD QUANTITY. MAINTENANCE INSPECTION FOUND FLUID LEAKING OUT OF PUMP SPLINE DRAIN. THE FLUID LEAKED INTO ELECTRICAL PORTION OF PUMP AND NOTICED ARCING AND A BURNING SMELL. PUMP WAS REPLACED, OPERATION NORMAL.

Part: RADOME — DELAMINATED (NOSE)

RECEIVED RADOME IN SHOP FOR DELAMINATION. INSPECTED RADOME AND FOUND EXCESSIVE MOISTURE. REMOVED INSIDE SKIN TO DRY MOISTURE. REPLACED DAMAGE CORE, REPLACED INSIDE SKIN AS PER SRM 53-10-72 ERROSION PROTECTION AND PAINT APPLIED AS PER PS 900-9-1-11, NR 05. TRANSMISSIVITY TESTED AND PASSED TEST. RADOME SENT TO STOCK.

Part: SKIN — LIGHTING STRIKE (UPPER FUSELAGE)

FOUND DURING LETTER CHECK, SEVERAL LIGHTNING STRIKES UPPER FUSELAGE BELOW SKY RADIO ANTENNA AND ALONG STRINGER 3L. REPAIRED PER SRM 53-00-01 FIG 207.

Part: SKIN — LIGHTING STRIKES (UPPER FUSELAGE)

FOUND DURING LETTER CHECK INSPECTION SEVERAL LIGHTNING STRIKES UPPER FUSELAGE IN AREA OF UPPER ANTI-COLLISON LIGHT FS 420 FS 580 FS 620 FS 690 REPAIRED FS 580 620 690 PER SRM 53-00-01 PERMANENT REPAIR FS 420 HAS TEMP REPAIR OF BLIND FASTENER PER SRM 53-00-01.