N8520Q

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 29,313 hrs · 14,692 cycles

EMERGENCY EXIT LIGHT BATTERY PACK M1695 WILL NOT HOLD CHARGE. REMOVED & REPLACED THE BATTERY IAW AMM 33-51-06-960-805. OPS CHECK GOOD.

Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 29,313 hrs · 14,692 cycles

PASSENGER CABIN FLOOR PANEL 231UF HAS FIBERS MISSING AND PULLING LOOSE IN MULTIPLE AREAS ON UPPER SURFACE. REPAIRED PASSENGER CABIN FLOOR PANEL 231 UF UPPER SURFACE IAW SRM 53-00-50-2R-1 AND SRM 53-00-50-2R-0 REPAIR GENERAL.

Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 29,313 hrs · 14,692 cycles

MID CABIN FLOOR EXPANSION JOINT AT BS 540 CRACKED AT FASTENER LOCATION NEAR LBL 1. REMOVED AND REPLACED FLOORBEAM IAW SRM 51-40-02-0G-0, 51-40-05-0G-0, AND DWG 143A0060, SHEET 64, REV -. APPLIED CIC IAW AMM 51-21-91-620-802.

Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 29,313 hrs · 14,692 cycles

MID CABIN FLOOR EXPANSION JOINT AT BS 540 CRACKED AT FASTENER LOCATION NEAR RBL 1. REMOVED AND REPLACED THE FLOORBEAM ASSY IAW SRM 51-40-02-0G-0, 51-40-05-0G-0, AND DWG 143A0060, SHEET 64, REV- APPLIED CIC IAW AMM 51-21-91-620-802.

Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 29,313 hrs · 14,692 cycles

PASSENGER CABIN FLOOR PANEL 241AF HAS PULLED FIBERS ON TOP SIDE. FLOOR PANEL 241AF REPAIRED IAW SRM 53-00-50-2R-1, AND EA M-25-153-02385.

Part: FLOOR PANEL — PULLED (ZN 200 FUS TOP) · airframe 29,313 hrs · 14,692 cycles

PASSENGER CABIN FLOOR PANEL 242BF HAS PULLED FIBERS ON TOP SIDE. REPAIRED PASSENGER CABIN FLOOR PANEL 242BF ON UPPER SURFACE IAW SRM 53-00-50-2R-1 AND SRM 53-00-50-2R-0 REPAIR GENERAL.

Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 29,313 hrs · 14,692 cycles

PASSENGER CABIN FLOOR PANEL 231ZF HAS PULLED FIBERS ON TOP SIDE. FLOOR PANEL 231ZF REPAIRED IAW SRM 53-00-50-2R-1 AND EA M-25-153-02385.

Part: FLOOR PANEL — PULLED (ZN 200 FUS TOP) · airframe 29,313 hrs · 14,692 cycles

PASSENGER CABIN FLOOR PANEL 231YF HAS PULLED FIBERS ON TOP SIDE. FLOOR PANEL 231YF REPAIRED IAW SRM 53-00-50-2R-1 AND EA M-25-153-02385.

Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 29,313 hrs · 14,692 cycles

PASSENGER CABIN FLOOR PANEL 241DF HAS PULLED FIBERS ON TOP SIDE. FLOOR PANEL 241DF REPAIRED IAW SRM 53-00-50-2R-1 AND EA M-25-153-02385.

Part: FLASHLIGHT — INOPERATIVE (ZONE 200) · airframe 28,551 hrs · 14,283 cycles

AFTER GALLEY FLIASHLIGHT ON FOS SIDE INOPERATIVE. REMOVED AND REPLACED BATTERY PER AMM 25-64-00.

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 28,035 hrs · 14,021 cycles

FWD FA FLASHLIGHT IS INOP FWD FLIGHT ATTENDANT FLASH LIGHT IS INOP<[01] REMOVED AND REPLACED BATTERY PER AMM 25-64-00.

Part: LIGHT — INOPERATIVE (ZONE 800) · airframe 27,785 hrs · 13,893 cycles

L2 DOOR EXTERIOR EMER LIGHT INOP <[01]. 01 - REMOVED AND REPLACED PER [AMM 33-51-04-960-801- NG (SLIDE/OVERWING LIGHT - LAMP REPLACEMENT - PERMANENT)].

Part: FLAP SYSTEM — LOCKED (ZONE 500) · airframe 27,403 hrs · 13,688 cycles

ON APPROACH; FLAP HANDLE WAS AT 15; FLAP TRAILING EDGE INDICATED LEFT 10; RIGHT TRAILING EDGE INDICATED 5. ON GO AROUND; BOTH TRAILING EDGE FLAPS INDICATED 10. QRH DIRECTED ALTERNATE FLAP (CONTINUED) USAGE TO FLAPS 15. NORMAL BRAKING USED. AUTO BRAKE 3. NORMAL PARK AT GATE RECEIVED FAULT CODES FLIGHT LEG 0: TE FLAP SNSR R 27-52260 L28VDC EXC INV 27-53279 E 28VAC EXC INV 27-53280 ASYM ENABLED 27-81283 FLIGHT LEG -75 FAULT CODES : ASYM ENABLED 27-81283 FLIGHT LEGN-110 FAULT CODES: ASYM ENABLED 27-81283<[01] AHM SHOWS RT FLAP POSITION TRANSMITTER FAILED. R & R RT FLAP POSITION TRANSMITTER REF AMM 27-58-01; R & R FLAP POSITION INDICATOR FOR COMPANY CONVENIENCE REF AMM 27-58-02; R & R FSEU FOR COMPANY CONVENIENCE REF AMM 27-51-01

Part: SIGN — OUT OF ADJUST (ZONE 200) · airframe 27,049 hrs · 13,502 cycles

R/H OVERWING EMER EXIT LIGHT/SIGN FELL OFF <[01]. INSTALLED NEW EMER EXIT LIGHT/SIGN AMM 33-51-01.

Part: ENGINE — LEAKING (ZONE 400) · airframe 26,871 hrs · 13,416 cycles

BEGAN WITH 87% OIL QUANTITY ON ENGINE #2. AFTER TAKEOFF IT WENT TO 1% WITH WHITE BOX. AFTER REDUCING THRUST OIL QUANTITY INCREASED TO 15% TO 30%. WHEN ON GROUND WHEN INCREASING THRUST OIL QUANTITY DROPS SIGNIFICANTLY. PERFORMED #2 ENGINE EXTERNAL OIL SYSTEM INSPECTION PER AMM 79-00-00; FOUND EVIDENCE OF OIL LEAK INSIDE OF PRIMARY EXHAUST NOZZLE. PERFORMED #2 ENGINE EXTERNAL OIL SYSTEM INSPECTION PER AMM 79-00-00; FOUND EVIDENCE OF OIL LEAK INSIDE OF PRIMARY EXHAUST NOZZLE AND STAGE 4 LPT BLADE/ TURBINE FRAME STRUT AT 6 O'CLOCK POSITION. R & R #2 ENG IAW MT 771-00-01. INSPECTED PER AMM 79-00-00-200-802-F00-NG (EXTERNAL OIL SYSTEM INSPECTION - PERMANENT)

Part: ANGLE — CRACKED (ZN 100 FUS LOWER) · airframe 26,025 hrs · 12,954 cycles

LEFT AIR CONDITIONING COMPARTMENT UPPER INBD L ANGLE AT STA 663 POSSIBLE CRACK PHOTO ATTACHED<[01] ACCOMPLISHED HFEC SURFACE INSPECTION PER NDT PART 6 51-00-00 PROC. 23 OF SUSPECT AREA VERIFIED ANGLE IS CRACKED.;[02] CRACK LENGTH IS .200';[03] CRACK LOCATED IN ANGLE AT STA. 663; LBL 9; EMITTING FROM FASTENER HOLE IN VERTICAL LEG. CRACK LENGTH .200'. CRACK VERIFIED BY NDT IN CORRECTIVE ACTION #1.[09] FABRICATED REPAIR ANGLE AND SPLICE PARTS AND LOCATED HOLES COMMON TO REPAIR ANGLE PER SRM 57-10-10-2R-5.<BR>ALODINE AND PRIME REPAIR PARTS PER SRM 51-20-01; SOPM 20-41-02;[10] REPAIR PARTS FABRICATED FROM .071 2024 T3.;[11] 9;10 INSPECTED WORK ABOVE OK TO INSTALL;[12] INSTALLED FASTENERS COMMON TO FUEL TANK PER SRM 57-10-10-2R-5.;[18] REPAIRED PER SRM 57-10-10-2R-5.;[19] RII INSPECTION PORTION COMPLIED WITH. SEE C/A?S AND STEPS FOR ALL WORK PERFORMED. REPAIRED PER SRM 57-10-10-2R-5.

Part: ANGLE — CRACKED (ZN 100 FUS LOWER) · airframe 26,025 hrs · 12,954 cycles

RIGHT AIR CONDITIONING COMPARTMENT UPPER INBD L ANGLE AT STA 663 POSSIBLE CRACK PHOTO ATTACHED<[01] ACCOMPLISHED HFEC SURFACE INSPECTION PER NDT PART 6 51-00-00 PROC. 23 OF SUSPECT AREA VERIFIED ANGLE IS CRACKED.;[02] CRACK LENGTH IS .700';[09] FABRICATED REPAIR ANGLE AND SPLICE PARTS AND LOCATED HOLES COMMON TO REPAIR ANGLE PER SRM 57-10-10-2R-5[18] ACCOMPLISHED REMAINING INSTALLED OF REPAIR OUTSIDE OF FUEL TANK PER SRM.57-10-10-2R-5;[19] ADD PARTS;[20] INSPECTED WORK OUTSIDE OF FUEL TANK. COMPLETE.<BR>02 - INSPECTED PER [SRM 57-10-10-2R-5-B01456 (REPAIR 5 - WING CENTER SECTION REAR SPAR VAPOR BARRIER ATTACH ANGLE REPAIR - PERMANENT)];[21] REPAIRED PER SRM 57-10-10-2R-5.;[22] RII INSPECTION PORTION COMPLIED WITH. SEE C/A?S AND STEPS FOR ALL WORK PERFORMED. REPAIRED PER SRM 57-10-10-2R-5.

Part: BATTERY PACK — INOPERATIVE (ZN 200 FUS TOP) · airframe 26,025 hrs · 12,954 cycles

EMERGENCY LIGHT BATTERY PACK AT STA 727C L/H IS INOP<[01] REMOVED AND REPLACED BATTERY PACK PER MM 33-51-06.EMERGENCY LIGHTS OPS CHECKED GOOD PER MM 33-51-06;[02] C/W INSPECTION.

Part: BATTERY PACK — INOPERATIVE (ZN 200 FUS TOP) · airframe 26,025 hrs · 12,954 cycles

EMERGENCY LIGHT BATTERY PACK AT STA 527C R/H IS INOP<[01] REMOVED AND REPLACED BATTERY PACK PER MM 33-51-06.EMERGENCY LIGHTS OPS CHECKED GOOD PER MM 33-51-06;[02] C/W INSPECTION.

Part: BATTERY PACK — INOPERATIVE (ZN 200 FUS TOP) · airframe 26,025 hrs · 12,954 cycles

EMERGENCY LIGHT BATTERY PACK AT STA 565 LEFT OVERWING IS INOP<[01] REMOVED AND REPLACED BATTERY PACK PER MM 33-51-06.EMERGENCY LIGHTS OPS CHECKED GOOD PER MM 33-51-06;[02] C/W INSPECTION.

Part: FLOOR PANEL — DEBONDED (ZN 200 FUS TOP) · airframe 26,025 hrs · 12,954 cycles

PNL 231XF HAS DISBONDED AND EXPOSED FIBERS<[01] R+R'D FLOOR PANEL 231XF. REF AMM 53-21-00;[02] GRANTED : OK TO INSTALLED;[03] VERIFIED C/A # 1 : YOSVANYS LEMAS SANTO (TECHNICIAN); 29-OCT-2024 23:20 UTC<BR>R+R'D FLOOR PANEL 231XF. REF AMM 53-21-00

Part: FLOOR PANEL — DEBONDED (ZN 200 FUS TOP) · airframe 26,025 hrs · 12,954 cycles

PNL 241AF HAS DISBONDED AND EXPOSED FIBERS<[01] R+R'D FLOOR PANEL 241AF. REF AMM 53-21-00;[02] GRANTED : OK TO INSTALLED;[03] VERIFIED C/A # 1 : YOSVANYS LEMAS SANTO (TECHNICIAN); 29-OCT-2024 23:18 UTC<BR>R+R'D FLOOR PANEL 241AF. REF AMM 53-21-00

Part: FLOOR PANEL — CORRODED (ZN 100 FUS LOWER) · airframe 26,025 hrs · 12,954 cycles

FWD CARGO FLOOR PANEL HAS CORROSION ALONG AFT EDGE; 120DF.<[01] R/R FWD CARGO FLOOR PANEL 120DF REF. AMM 25-52-10.;[02] INSPECTED WORK PERFORMED. R/R FWD CARGO FLOOR PANEL 120DF REF. AMM 25-52-10.

Part: SCUFF PLATE — CRACKED (ZONE 100) · airframe 26,025 hrs · 12,954 cycles

FORWARD CARGO FORWARD CORNER SCUFF PLATE IS CRACKED.<[01] OK TO INSTALL;[02] REPLACED FORWARD CARGO FORWARD CORNER SCUFF PLATE PER AMM 53-11-02-420-801

Part: PLATE — CORRODED (ZN 100 FUS LOWER) · airframe 26,025 hrs · 12,954 cycles

AFT CARGO COMPARTMENT FLOOR STRUCTURE; LEFT SIDE PLATE HAS SURFACE CORROSION FROM STA 727H-727I AROUND FASTENER HOLES.<[01] MEASURED CORROSION DAMAGE AT AFT CARGO LEFT SIDE SUPPORT ZEE STATION 727H TO 727I; ORIGINAL THICKNESS IS .040?; DAMAGE DEPTH IS .006? AT DEEPEST LOCATION; REMAINING THICKNESS IS .034? AND IS OUT OF LIMITS I/A/W SRM 53-00-53-1A-2.;[02] REMOVED DAMAGE PER SRM 53-00-53-1A-2. AFTER DAMAGE REMOVAL; FOUND DAMAGE REMOVAL WITHIN LIMITS PER SRM 53-00-53-1A-2. MIN REMAINING THICKNESS 0.036?.;[03] VERIFIED. REMOVED DAMAGE PER SRM 53-00-53-1A-2. AFTER DAMAGE REMOVAL; FOUND DAMAGE REMOVAL WITHIN LIMITS PER SRM 53-00-53-1A-2. MIN REMAINING THICKNESS 0.036. SIGN OFF FOR CORRECTIVE ACTION #2.;[04] OK TO ALODINE AND PRIME.;[05] TREATED AND PRIMED DAMAGED AREA PER SRM 53-00-53-1A-2.;[06] VERIFIED. REMOVED DAMAGE PER SRM 53-00-53-1A-2. AFTER DAMAGE REMOVAL; FOUND DAMAGE REMOVAL WITHIN LIMITS PER SRM 53-00-53-1A-2. MIN REMAINING THICKNESS 0.036. SIGN OFF FOR CORRECTIVE ACTION #2.VERIFIED.TREATED AND PRIMED DAMAGED AREA PER SRM 53-00-53-1A-2.

Part: SCUFF PLATE — CRACKED (ZONE 100) · airframe 26,025 hrs · 12,954 cycles

FORWARD CARGO AFT CORNER SCUFF PLATE IS CRACKED<[01] OK TO INSTALL;[02] REPLACED FORWARD CARGO AFT CORNER SCUFF PLATE PER AMM 53-11-02-420-801

Part: BRACKET — CRACKED (ZONE 100) · airframe 26,025 hrs · 12,954 cycles

APU FEEDER CABLE SUPPORT BRACKET CRACKED STA 867 RBL 18 WL300<[01] FABRICATED FEEDER CABLE SUPPORT BRACKET; P/N 287A4015-9; PER BOEING DRAWING #287A4015 AND SMAL - BOEING CONTROL NUMBER 0271023258.;[02] VERIFIED. FABRICATED FEEDER CABLE SUPPORT BRACKET; P/N 287A4015-9; PER BOEING DRAWING #287A4015 AND SMAL - BOEING CONTROL NUMBER 0271023258.;[03] REMOVED AND INSTALLED NEW APU FEEDER CABLE SUPPORT BRACKET AT STA 867 RBL 18 WL300 IAW SRM 51-40-02. SEE CORRECTIVE ACTIONS; STEPS AND SA-M 1057 PARTS PROCESS TRAVELER P/O # P005BA6L FOR ALL WORK PREFORMED.;[04] VERIFIED WORK.....REMOVED AND INSTALLED NEW APU FEEDER CABLE SUPPORT BRACKET AT STA 867 RBL 18 WL300 IAW SRM 51-40-02 ALL STEPS COMPLETE

Part: ANGLE — CRACKED (ZN 200 FUS TOP) · airframe 26,025 hrs · 12,954 cycles

CRACK IN FLOOR BEAM WEB ANGLE BETWEEN STA. 380-400 RBL 10<[01] REMOVED CRACK FLOOR BEAM WEB ANGLE BETWEEN STA. 380-400 RBL 10.<BR>LOCATED; DRILLED AND INSTALLED NEW FLOOR BEAM WEB ALL WORK REFERENCE 51-40-02;[02] INSPECTED WORK ABOVE

Part: ANGLE — CRACKED (ZN 200 FUS TOP) · airframe 26,025 hrs · 12,954 cycles

CRACK IN FLOOR BEAM WEB ANGLE BETWEEN STA. 380-400 LBL 13<[01] REMOVED CRACK FLOOR BEAM WEB ANGLE BETWEEN STA. 380-400 LBL 13.<BR>LOCATED; DRILLED AND INSTALLED NEW FLOOR BEAM WEB ALL WORK REFERENCE 51-40-02;[02] INSPECTED WORK ABOVE

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 24,575 hrs · 12,166 cycles

SEVERAL EMERGENCY LIGHTS WILL NOT ILLUMINATE THROUGHOUT THE AIRCRAFT<[01] REMOVED AND REPLACED BATTERY PACKS AT THE FOLLOWING POSITIONS; M1671;M1672;M1675 AND M2335 PER AMM 33-51-06

Part: MEGAPHONE — INTERMITTENT (ZN 200 FUS TOP) · airframe 23,854 hrs · 11,769 cycles

FWD MEGAPHONE INTERMITTENT<[01] R AND R FWD MEGAPHONE AND OPS CK OK. REF AMM 25-64-00. BATTERY EXP JUN 2025

Part: SIGN — INOPERATIVE (ZN 200 FUS TOP) · airframe 23,396 hrs · 11,506 cycles

FWD RH EXTERIOR EMERGENCY LIGHT AND FWD OVER DOOR EXIT SIGN LIGHT INOP<[01] REMOVED AND REPLACED APPLICABLE EMERGENCY LIGHT BATTERY PACK IAW AMM 33-51-06. OPS CHECK GOOD

Part: FLASHLIGHT — INOPERATIVE (ZN 200 FUS TOP) · airframe 23,283 hrs · 11,431 cycles

AFT LEFT FLASHLIGHT INOP<[01] R/R AFT LEFT FLASHLIGHT BATTERY PER AMM 25-64-00

Part: WEB — CRACKED (RT WING) · airframe 19,499 hrs · 9,300 cycles

RH WING PNL SUPPORT WEB CRACKED. RH WING PNL SUPPORT WEB CRACKED JUST INBD OF DEFLECTION CONTROL RIB. REMOVED AND REPLACED DAMAGED SUPPORT WEB PER SRM 51-40-02.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 19,499 hrs · 9,300 cycles

CABIN FLOOR PANEL 231XF HAS MULTIPLE FIBERS EXPOSED. / [01] REMOVE AND REPLACED FLOOR BOARD PER AMM 53-21-00.;[02] REMOVE AND REPLACED FLOOR BOARD PER AMM 53-21-00.<BR>PART INFORMATION NEEDED.

Part: ANGLE — DAMAGED (BS 500B-500G) · airframe 19,499 hrs · 9,300 cycles

FWD CARGO, LT TRANSITIONAL ANGLE AT BS 500B+8 THRU 500G+10, WAS FOUND TO BE OUT OF LIMITS. REMOVED DAMAGE SECTION IAW SRM 51-40-02. LOCATED AND DRILLED FWD SPICE AT BS 500B +9 IAW SRM 53-00-53-2R-5. REPAIRED IAW SRM 53-00-53-2R-5, REPAIR 5, AND EA M-22-153-01550.

Part: FLOOR SUPPORT — CORRODED (BS 747-767 RBL21) · airframe 19,499 hrs · 9,300 cycles

FLOOR SUPPORT BETWEEN STA 747 AND 767 RBL 21 HAS CORROSION AROUND NUTPLATE HOLES. LOCATED, DRILLED, AND INSTALLED A NEW FLOOR SUPPORT IAW SRM 51-40-02.

Part: ANGLE — CORRODED (BS 770-774) · airframe 19,499 hrs · 9,300 cycles

THE AFT CARGO R/H TRANSITION ANGLE HAS CORROSION FROM STA 770 TO 774 / [01] FOUND CORROSION ON R/H SIDE PLATE FROM STA 767-792 TO BE OUT OF ALLOWABLE LIMITS PER SRM 53-00-53-1A-2.;[02] REMOVED SHIELD; MATCH DRILLED NEW SHIELD PER SRM 51-40-05;[03] INSP DRILLING OF NEW SHIELD;[04] REMOVED AND REPLACED SHIELD PER SRM 51-10-02

Part: ANGLE — CORRODED (BS 500A-500I) · airframe 19,499 hrs · 9,300 cycles

RIGHT TRANSITION ANGLE; STA. 500A THRU 500I CORRODED, FOUND OUT OF LIMITS. LOCATED AND DRILLED NEW IAW SRM 51-40-02. REPLACED THE RH SIDE TRANSITION ANGLE IAW SRM 51-40-02.

Part: SHIELD — CORRODED (BS 492-500A) · airframe 19,499 hrs · 9,300 cycles

RIGHT SHIELD, RBL 21 BS 492-500A HAS CORROSION. SHIELD REMOVED AND REPLACED WITH NEW IAW SRM 51-40-02.

Part: ANGLE — CORRODED (BS 727H-767) · airframe 19,499 hrs · 9,300 cycles

THE AFT CARGO R/H TRANSITION ANGLE HAS CORROSION FROM STA 727H +8 TO 767, FOUND TO BE OUT OF LIMITS IAW SRM 53-0053-1A-2. REMOVED DAMAGED SECTION OF RT TRANSITION ANGLE IAW SRM 53-00-53-2R-5. LOCATED, DRILLED, TREATED AND PRIMED. IAW SRM 53-00-53-2R-5. INSTALLED THE NEW TRANSITION ANGLE IAW SRM 53-00-53-2R-5.

Part: ANGLE — CORRODED (BS 727F-807) · airframe 19,499 hrs · 9,300 cycles

THE AFT CARGO L/H TRANSITION ANGLE HAS CORROSION FROM STA 727F+10 TO 807 / LT TRANSITION ANGLE UPPER SURFACE FORM STA 727I TO STA 807; LBL 21; WAS FOUND TO BE OUT OF ALLOWABLE LIMITS IAW SRM 53-00-53-1A-2. REMOVED DAMAGED SECTION OF LT SIDEPLATE CHANNEL ASSEMBLY FORM STA 727H+11 TO STA 807+10; LBL 21; IAW SRM 53-00-53-2R-5.;[06] LOCATED ;DRILLED ;TREATED AND PRIME LT TRANSITION ANGLE AND REPAIR SPLICE PER SRM 53-00-53-2R-5.;[07] INSPECTED LOCATING ; DRILLING ;TREATING AND PRIMING OF L/H TRANSITION ANGLE AND REPAIR SPLICE PER SRM 53-00-53-2R-5] REMOVED; LOCATED ; DRILLED TREAT AND PRIME L/H TRANSITION ANGLE & REPAIR SPLICE PER SRM 53-00-53-2R -5;[11] REVERSION STEP 10 REMOVED; LOCATED ; DRILLED TREAT AND PRIME L/H TRANSITION ANGLE & REPAIR SPLICE AT BS 817-847 PER SRM 53-00-53-2R -5;[12] C/W INSP STEP #10 AND #11.;[13] INSTALLED RIVETS ON L/H TRANSITION ANGLE SPLICE BETWEEN STA 807 AND STA 827 PER SRM 53-00-53-2R-5. C/W INSPECTION OF L/H TRANSITION ANGLE SPLICE BETWEEN BETWEEN STA 807 AND STA 827 PER SRM 53-00-53-2R-5. INSTALLED AFT CARGO LT SIDEPLATE CHANNEL REPAIR PARTS FORM STA 727H+11 TO STA 847; LBL 21; IAW SRM 53-00-53-2R-5

Part: SUPPORT CHANNEL — CORRODED (BS 500B-500D) · airframe 19,499 hrs · 9,300 cycles

FWD CARGO STA. 500B-500D CORROSION AROUND NUT-PLATE HOLES ON LEFT SUPPORT CHANNEL/TRANSITION ANGLE. / [01] WORK TO BE PERFORMED ON NR TTG8Q00FS334

Part: SUPPORT CHANNEL — CORRODED (BS 500D-500F) · airframe 19,499 hrs · 9,300 cycles

FWD CARGO STA. 500D-500F CORROSION AROUND NUT-PLATE HOLES ON LEFT SUPPORT CHANNEL/TRANSITION ANGLE. / [01] WORK TO BE PERFORMED ON NR TTG8Q00FS334

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 19,499 hrs · 9,300 cycles

CABIN FLOOR PANEL 241DF HAS MULTIPLE FIBERS EXPOSED. / [01] REMOVE AND REPLACED FLOOR BOARD PER AMM 53-21-00.;[02] PARTS ONLY;[03] REMOVE AND REPLACED FLOOR BOARD PER AMM 53-21-00.<BR>PART INFORMATION.

Part: SUPPORT CHANNEL — CORRODED (BS 500B-500D) · airframe 19,499 hrs · 9,300 cycles

FWD CARGO STA. 500B-500D CORROSION AROUND NUT-PLATE HOLES ON RIGHT SUPPORT CHANNEL/TRANSITION ANGLE. / [01] ALL WORK TO BE PERFORMED ON NR TTG8Q00FRQC8 #1660;[02] C/W INSPECTION.

Part: CHANNEL — CORRODED (BS 500I) · airframe 19,499 hrs · 9,300 cycles

FWD CARGO STA. 500I; AFT BULKHEAD NUT-PLATE CHANNEL LBL 23 TO RBL 23 HAS CORROSION AROUND NUT-PLATE HOLES. REMOVED AND REPLACED WITH ASSEMBLY PER SRM 51-40-02;[02] C/W INSPECTION.

Part: ANGLE — CORRODED (BS 500-500B) · airframe 19,499 hrs · 9,300 cycles

FWD CARGO STA. 500-500B CORROSION AROUND NUT-PLATE HOLES ON LEFT SUPPORT CHANNEL/TRANSITION ANGLE. / [01] REMOVED LIGHT SURFACE CORROSION; FOUND WITH IN LIMITS TREATED AND PRIMED PER SRM 53-00-53-1A-2

Part: SUPPORT CHANNEL — CORRODED (BS 500G-500I) · airframe 19,499 hrs · 9,300 cycles

FWD CARGO STA. 500G-500I CORROSION AROUND NUT-PLATE HOLES ON RIGHT SUPPORT CHANNEL/TRANSITION ANGLE. / [01] ALL WORK TO BE PERFORMED ON NR TTG8Q00FRQC8 #1660;[02] C/W INSPECTION.

Part: CHANNEL — CORRODED (BS 396) · airframe 19,499 hrs · 9,300 cycles

FWD CARGO STA. 396 CORROSION AROUND NUT-PLATE HOLES ON RIGHT SUPPORT CHANNEL/TRANSITION ANGLE. REMOVED LIGHT SURFACE CORROSION; FOUND WITH IN LIMITS TREATED AND PRIMED PER SRM 53-00-53-1A-2.

Part: ANGLE — CORRODED (BS 500-500B) · airframe 19,499 hrs · 9,300 cycles

FWD CARGO STA. 500-500B CORROSION AROUND NUT-PLATE HOLES ON RIGHT SUPPORT CHANNEL/TRANSITION ANGLE. / [01] ALL WORK TO BE PERFORMED ON NR TTG8Q00FRQC8 #1660;[02] C/W INSPECTION.

Part: CHANNEL — CORRODED (BS 420-440) · airframe 19,499 hrs · 9,300 cycles

FWD CARGO STA. 420-440 CORROSION AROUND NUT-PLATE HOLES ON RIGHT SUPPORT CHANNEL/TRANSITION ANGLE. REMOVED AND REPLACED WITH NEW PART PER SRM 51-40-02

Part: ANGLE — CORRODED (BS 500G-500I) · airframe 19,499 hrs · 9,300 cycles

FWD CARGO STA. 500G-500I CORROSION AROUND NUT-PLATE HOLES ON LEFT SUPPORT CHANNEL/TRANSITION ANGLE. REMOVED LIGHT SURFACE CORROSION; FOUND WITH IN LIMITS; TREATED AND PRIMED PER SRM 53-00-53-1A-2.

Part: ANGLE — CORRODED (BS 500D-500F) · airframe 19,499 hrs · 9,300 cycles

FWD CARGO STA. 500D-500F CORROSION AROUND NUT-PLATE HOLES ON RIGHT SUPPORT CHANNEL/TRANSITION ANGLE. ALL WORK TO BE PERFORMED ON NR TTG8Q00FRQC8 #1660.

Part: FLOOR SUPPORT — CRACKED (BS 540 LBL 3) · airframe 19,499 hrs · 9,300 cycles

FLOORBOARD SUPPORT ANGLE CRACKED AT BS540 LBL3 / [01] REMOVED AND REPLACED FLOORBOARD SUPPORT ANGLE AT BS540 LBL3 IAW SRM 51-40-02

Part: FLOOR SUPPORT — CRACKED (BS 540) · airframe 19,499 hrs · 9,300 cycles

FLOORBOARD SUPPORT ANGLE CRACKED AT BS540 RBL3 / [01] REMOVED AND REPLACED FLOORBOARD SUPPORT ANGLE AT BS540 RBL3 IAW SRM 51-40-02

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 19,447 hrs · 9,269 cycles

L1 DOOR EMERGENCY SLIDE OUT OF CONTAINMENTER / [01] REINSTALLED L1 DOOR SLIDE IAW AMM 25-66-01. NO FURTHER DEFECTS NOTED. AC OK FOR SERVICE

Part: SIGN — LOOSE (OVERHEAD CABIN) · airframe 18,382 hrs · 8,671 cycles

OVERHEAD CEILING EXIT SIGN MID CABIN IS HANGING LOOSE / [01] REINSTALLED EXIT SIGN PER S.I.P.

Part: DOOR ACTUATOR — OUT OF POSITION · airframe 17,476 hrs · 8,173 cycles

AFT ENTRY DOOR WILL NOT OPEN. / [01] PER FIM 52-10-00. FOUND DOOR SNUBBER LEAKING AND SNUBBER BUMPER MISSING. REMOVED AND REPLACED DOOR SNUBBER AND INSTALLED NEW SNUBBER BUMPER PER AMM %2-13-51. DOOR OPERATION NORMAL; NO DEFECTS NOTED AT THIS TIME.

Part: FLASHLIGHT — INOPERATIVE (AFT CABIN) · airframe 16,817 hrs · 7,803 cycles

FLASHLIGHT AFT CABIN WILL NOT TEST ; / [01] OK TO CONTINUE PER MEL 25-12-01 SP1B AUTH43958; [02] RESEATED AND RESEALEDFLASH LIGHT AT AFT CABINO/B IAW AMM 25-64-00 OPS CK GOOD.

Part: LIGHT — INOPERATIVE · airframe 7,338 hrs · 15,935 cycles

RIGHT FOWARD OVERWING EMERGENCY EXIT DOOR LIGHT INOP (SIDEWALL LIGHT) ( CABIN INTERIOR ILLUM BOEING SKY INTERIOR PHOTOLUMINESCENT ) / R&R FWD OVERWING EMERGENCY EXIT LIGHT PER AMM 33-21-00. OPS CHECK GOOD. P/N OFF/ON 9701-14-001 S/N OFF 3729 S/N ON BN 142521CL# 95417

Part: MEGAPHONE — MISSING (CABIN) · airframe 6,908 hrs · 15,131 cycles

CREW REPORTS MEGAPHONE IS MISSING FROM FWD GALLEY / INSTALLED NEW MEGAPHONE IAW AMM 25-64-04

Part: FLASHLIGHT — INOPERATIVE (AFT CABIN) · airframe 13,584 hrs · 6,103 cycles

AFT NR 3 EMERGENCY FLASHLIGHT INOPERABLE. REPLACED AFT NR 3 EMERGENCY FLASHLIGHT, PER AMM 25-64-00.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 13,086 hrs · 5,849 cycles

L1 SLIDE FELL OUT OF SLIDE PACK. RE-PACKED L1 DOOR SLIDE PACK, IAW MT 725-61-06 (ASSISTED BY 87336).

Part: SLIDER — CRACKED (HORIZONTAL STAB) · airframe 13,010 hrs · 5,811 cycles

L/H HORIZONTAL UPPER FWD SLIDER IS CRACKED / REMOVED AND REPLACED PER M/M 53-31-31INSPECTOR: E50309

Part: SLIDER — CRACKED (HORIZONTAL STAB) · airframe 13,010 hrs · 5,811 cycles

R/H HORIZONTAL UPPER FWD SLIDER IS CRACKED / REMOVED AND REPLACED PER M/M 53-31-31.INSPECTOR: E50309

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 9,262 hrs · 3,988 cycles

CABIN CREW REPORTS R2 DOOR SLIDE DATE ILLEGIBLE. REPOSITIONED SLIDE ASSEMBLY PER MT.

Part: LIGHT — LOOSE (CABIN) · airframe 2,329 hrs · 980 cycles

LT AFT LAV REAR EMERGENCY EXIT LIGHT LOOSE. SECURED LIGHT PER AMM.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 984 hrs · 410 cycles

AFT GALLEY RIGHT SIDE EMERGENCY FLASHLIGHT INOP. REPAIRED FLASHLIGHT PER MM.