N713SY

Part: FAIRING — DAMAGED (NR 1 FLAP TRACK) · airframe 59,988 hrs · 39,561 cycles

NR 1 FLAP AFT FAIRING HAS DAMAGE ON INNER SKIN. REPAIRED NR 1 FLAP AFT FAIRING INNER SKIN, IAW ER 20-03509 REV IR AND SC EA 57-0055.

Part: SKIN — DAMAGED (LT WING FLAP LE) · airframe 59,988 hrs · 39,561 cycles

LT OUTBOARD FLAP LEADING EDGE PANEL 567AT DAMAGED. LT OUTBOARD FLAP LEADING EDGE PANEL 567AT FOUND TO BE OUT OF LIMITS, IAW SRM 57-53-01-1A-3 RECEIVED NEW FLAP LEAD EDGE. LOCATED, DRILLED, TOP COATED IAW SRM 51-40-05-0G-0 AMM 51-21-99-300-801.

Part: FAIRING — DAMAGED (LT WING TE FLAP) · airframe 59,988 hrs · 39,561 cycles

LT WING NR 3 FLAP AFT FAIRING HAS DAMAGE ON INNER SKIN. REPAIRED LT WING NR 3 FLAP AFT FAIRING INNER SKIN, IAW ER 20-0352 REV IR AND SC EA 57-0054.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 59,988 hrs · 39,561 cycles

FRAME HOLE AT BS 951.07 LBL 55 WL 208 IS OUT OF ROUND. REPAIRED FRAME HOLE AT STA 951.07, LBL 55, WL 208, IAW ATS ER 20-03506 REV IR DATED 06-NOV-2020 AND SCA EA 53-0062.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 59,988 hrs · 39,561 cycles

FRAME HOLE AT BS 992.8 LBL 55 WL 208 IS OUT OF ROUND. REPAIRED FRAME HOLE AT STA 992.8, LBL 55, WL 208, IAW ATS ER 20-03503 REV IR DATED 06-NOV-2020 AND SCA EA 53-0061.

Part: PANEL — DAMAGED (RT WING TE FLAP) · airframe 59,988 hrs · 39,561 cycles

RT WING INBOARD FLAP PANEL 653ET HAS DAMAGED HONEYCOMB ON LOWER SURFACE. REPAIRED DAMAGE TO HONEYCOMB ON LOWER (INNER) SURFACE OF RT WING INBOARD FLAP PANEL 653ET, PER SRM 51-70-10-2R-4.

Part: PANEL — BURNED (NACELLE) · airframe 59,988 hrs · 39,561 cycles

PYLON PANEL 441 ER IS BURNT INTO THE COMPOSITE MATERIAL. REPAIRED BURNT INTO THE COMPOSITE MATERIAL ON PYLON PANEL 441ER, IAW 737 SRM 54-50-70-2R-2 AND SRM 51-70-05 REPAIR 6.

Part: PANEL — DAMAGED (FUSELAGE) · airframe 59,988 hrs · 39,561 cycles

PANEL 191FL HAS DAMAGED SCREW HOLES. REPAIRED DAMAGED SCREW HOLES ON PANEL 191FL, IAW 737 SRM 53-30-70-2R-1 AND SRM 51-70-05 REPAIR 8.

Part: FLOORBEAM — CORRODED (CABIN) · airframe 59,988 hrs · 39,561 cycles

CORROSION AROUND FASTENER HOLE ON FLOOR BEAM AT BODY STATION 986.5 LBL 43 TO RBL 50 WL 208. REMOVED AND REPLACED FS 986.5 FLOOR BEAM "T" CAP (PREVIOUS REPAIR) RBL 55-LBL 55 WL 208, IAW SRM 51-40-02-0G-0, SRM 53-70-51-2R-4 AND SCA EC/TC ENG-53SCA-09268.

Part: PANEL — DAMAGED (FUSELAGE) · airframe 59,988 hrs · 39,561 cycles

PANEL 192F AFT INSIDE EDGE OF PANEL HEAVILY WORN. REPAIRED DAMAGE TO AFT INSIDE EDGE OF PANEL 192F IAW SRM 51-70-05-2R-6 PER SRM 53-40-70-2R-1 PARA 4D(1) TABLE 202.

Part: FLOORBEAM — CORRODED (CABIN) · airframe 59,988 hrs · 39,561 cycles

CORROSION AROUND FASTENER HOLE ON FLOOR SUPPORT BEAM AT BS 950 LBL 48 WL 208. REMOVED FLOOR SUPPORT BEAM AT BS 950 LBL 48 WL 208 DUE TO DAMAGE FOUND OUT OF LIMITS, PER SRM 53-70-51-1A-1. INSTALLED NEW FLOOR SUPPORT BEAM, PER SRM 51-40-02-0G-0 AND DWG 147A5650.

Part: PANEL — DAMAGED (FUSELAGE) · airframe 59,988 hrs · 39,561 cycles

PANEL 192HR HAS DAMAGED SCREW HOLES. REPAIRED DAMAGED SCREW HOLES ON PANEL 192HR, IAW SRM 51-70-05-2R-8 PER SRM 53-40-70-2R-1 PARA 4D(1) TABLE 202.

Part: FLOORBEAM — CORRODED (CABIN) · airframe 59,988 hrs · 39,561 cycles

CORROSION AROUND FASTENER ON FLOOR SUPPORT BEAM AT BS 950 LBL 50 WL 208. REMOVED DAMAGED FLOOR SUPPORT BEAM AT BS 950 LBL 50 WL 208 AND INSTALLED NEW FLOOR SUPPORT BEAM, PER SRM 51-40-02-0G-0 AND 2 EA CLIPS PER SRM 51-40-02-0G-0 AND DWG 147A5650 REV-C.

Part: PANEL — DAMAGED (FUSELAGE) · airframe 59,988 hrs · 39,561 cycles

PANEL 192HL HAS DAMAGED SCREW HOLES. REPAIRED DAMAGED SCREW HOLES ON PANEL 192HL, IAW SRM 51-70-05-2R-8.

Part: PANEL — DAMAGED (FUSELAGE) · airframe 59,988 hrs · 39,561 cycles

PANEL 192AR HAS DAMAGED SCREW HOLES. REPAIRED DAMAGED SCREW HOLES, IAW SRM 53-40-70-2R-1, 51-70-05-2R-8.

Part: PANEL — DAMAGED (FUSELAGE) · airframe 59,988 hrs · 39,561 cycles

PANEL 191FR HAS DAMAGED SCREW HOLES. REPAIRED DAMAGED SCREW HOLES ON PANEL 191FR, IAW 737 SRM 53-30-70-2R-1 AND SRM 51-70-04 REPAIR 9 AND 10.

Part: PANEL — DAMAGED (FUSELAGE) · airframe 59,988 hrs · 39,561 cycles

PANEL 192AL HAS DAMAGED SCREW HOLES. REPAIRED DAMAGED SCREW HOLES, IAW SRM 53-40-70-2R-1, 51-70-05-2R-8.

Part: PANEL — DAMAGED (WING) · airframe 59,988 hrs · 39,561 cycles

PANEL 671BB HAS MULTIPLE SCREW HOLES CRACKED/DAMAGED. REPAIRED DAMAGED SCREW HOLES ON PANEL 671BB, IAW SRM 51-70-04-2R-9 PER SRM 57-51-01-2R-1 PARA 4D TABLE 202.

Part: TORQUE TUBE — CHAFED (RT WING TE FLAPS) · airframe 59,988 hrs · 39,561 cycles

RT INBOARD MAIN FLAP HAS MINOR WEAR ON TORQUE TUBE AT INBOARD SIDE WITH MISSING CIC AND PRIMER. REWORK/REPAIR ACCOMPLISHED FOR TORQUE TUBE, IAW ENGINEERING TASK CARD 737-53-1264-01-GROUP 2.

Part: FAIRING — DAMAGED (NR 1 FLAP TRACK) · airframe 59,988 hrs · 39,561 cycles

NR 1 FLAP AFT FAIRING HAS DAMAGE AT LEADING EDGE. REPAIRED DAMAGE AT LEADING EDGE OF NR 1 AFT FLAP TRACK FAIRING, PER SRM 57-53-70-2R-5.

Part: PANEL — DAMAGED (HORIZONTAL STAB) · airframe 59,988 hrs · 39,561 cycles

PANEL 333EB SCREW HOLE DAMAGED. PANEL 333EB DAMAGED SCREW HOLE REPAIRED, IAW B737 SRM 55-10-01-2R-9 TABLE 203 AND IAW B737 SRM 51-70-05-2R-8.

Part: PANEL — DAMAGED (HORIZONTAL STAB) · airframe 59,988 hrs · 39,561 cycles

PANEL 343CB HAS MULTIPLE DAMAGED SCREW HOLES. PANEL 343CB MULTIPLE DAMAGED SCREW HOLES REPAIRED, IAW B737 SRM 55-10-01-2R-9 TABLE 203 AND IAW B737 SRM 51-70-04-2R-9.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 59,988 hrs · 39,561 cycles

LT WING OUTBOARD AFT FLAP INBOARD LOWER CORNER IS DELAMINATED. REPAIRED DELAMINATION INBOARD LOWER CORNER ON LT WING OUTBOARD AFT FLAP, IAW SRM 51-70-10-2R-4 57-53-01-2R-14.

Part: SKIN — WORN (LT WING TE FLAP) · airframe 59,988 hrs · 39,561 cycles

LT OUTBOARD AFT FLAP INBOARD EDGE HAS WEAR MARK 9 INCHES UP FROM TRAILING EDGE. REPAIRED WORN AREA 9 INCHES UP FROM TRAILING EDGE ON LT OUTBOARD AFT FLAP INBOARD EDGE, IAW SRM 57-53-01-2R-14 + SRM 51-70-10-2R-4.

Part: RETAINER — CORRODED (HORIZONTAL STAB) · airframe 59,988 hrs · 39,561 cycles

PANEL 333AB FIXED RUB STRIP CLAMP CORRODED IN MULTIPLE SPOTS. ORDERED AND RECEIVED NEW 186A3002-29 RETAINER AND 186A3004-3, -4 SEAL ASSEMBLYS FOR PANEL 333AB. TRANSFERED ORIGINAL HOLE PATTERN TO NEW RETAINER (RUB STRIP CLAMP), PER SRM 51-40-05 AND 51-40-08. INSTALLATION OF PANEL TO BE ACCOMPLISHED ON CARD ZONE 330-CLOSE.

Part: PANEL — DAMAGED (LT NACELLE) · airframe 59,988 hrs · 39,561 cycles

LEFT PYLON PANEL 431ER COMPOSITE DAMAGED ALONG EDGE. LEFT PYLON PANEL 431ER COMPOSITE DAMAGE ALONG EDGE REPAIRED, IAW B737 SRM 54-50-70-2R-2 TABLE 202 AND IAW B737 SRM 51-70-05-2R-6.

Part: RETAINER — CORRODED (HORIZONTAL STAB) · airframe 59,988 hrs · 39,561 cycles

PANEL 343AB FIXED RUB STRIP CLAMP CORRODED IN MULTIPLE SPOTS. ORDERED AND RECEIVED NEW 186A3002-30 RETAINER AND 186A3004-4 SEAL ASSEMBLY FOR PANEL 343AB. TRANSFERRED ORIGINAL HOLE PATTERN TO NEW RETAINER (RUB STRIP CLAMP) PER SRM 51-40-05 AND 51-40-08. INSTALLATION TO BE ACCOMPLISHED ON CARD ZONE 340-CLOSE.

Part: SKIN — DAMAGED (LT WING TE FLAP) · airframe 59,988 hrs · 39,561 cycles

ACCOMPLISH PERMANENT REPAIR OF LT INBOARD FLAP OUTBOARD FAIRING CENTER SEAL FASTENER HOLES. ACCOMPLISHED PERMANENT REPAIR OF LT INBOARD FLAP TRACK FAIRING OUTBOARD CENTER BULB SEAL FASTENER HOLES, PER SRM 57-53-70-2R-2 PARA 5.

Part: PANEL — DAMAGED (FUSELAGE) · airframe 59,988 hrs · 39,561 cycles

PANEL 192E HAS DAMAGED SCREW HOLES. REPAIRED DAMAGED SCREW HOLES, IAW SRM 51-70-04-2R-9 ON PANEL 192F.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 59,988 hrs · 39,561 cycles

PANEL 194CL HAS DAMAGED SCREW HOLE. REPAIRED DAMAGED SCREW HOLE ON PANEL 194CL, IAW SRM 51-70-04-2R-9.

Part: PANEL — DAMAGED (WING) · airframe 59,988 hrs · 39,561 cycles

PANEL 671DB HAS MULTIPLE SCREW HOLES DAMAGED. REPAIRED MULTIPLE SCREW HOLES ON PANEL 671DB, PER SRM 51-70-05-2R-8.

Part: PANEL — DAMAGED (TE FLAP) · airframe 59,988 hrs · 39,561 cycles

PANEL 571BB HAS DAMAGED SCREW HOLES. REPAIRED DAMAGED SCREW HOLES, IAW SRM 57-51-01-2R-1, 51-70-05-2R-8.

Part: PANEL — DAMAGED (FLAP) · airframe 59,988 hrs · 39,561 cycles

PANEL 571AB HAS DAMAGED SCREW HOLE. REPAIRED DAMAGED SCREW HOLE ON PANEL 571AB, IAW 737 SRM 57-51-01-2R-1 AND SRM 51-70-05 REPAIR 8.

Part: FLOOR PANEL — PUNCTURED (CABIN) · airframe 59,988 hrs · 39,561 cycles

FLOOR PANEL 241YF HAS A PUNCTURE ON UPPER SURFACE. REPAIRED PUNCTURE ON UPPER SURFACE ON FLOOR PANEL 241YF, IAW SRM 53-00-50-2R-1.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · airframe 58,973 hrs · 39,159 cycles

RI MAIN CABIN DOOR MOP SILL ATTACH ANGLE HAS CORROSION. REMOVED AND REPLACED ANGLE AT R1 MAIN CABIN DOOR-MOP SILL.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 58,973 hrs · 39,159 cycles

L1 MAIN CABIN DOOR MOP SILL HAS CORROSION. REMOVED AND REPLACED L1 MAIN CABIN CARGO DOOR MOP SILL.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 58,973 hrs · 39,159 cycles

L-2 DOOR INNER CHORD DOOR SILL HAS CORROSION. REMOVED AND REPLACED L-2 INNER CHORD DOOR SILL.

Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 58,973 hrs · 39,159 cycles

DAMAGED FLOOR PANEL 231CF AT CORNER. REPAIRED DAMAGED FLOOR PANEL 231CF AT CORNER.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 58,973 hrs · 39,159 cycles

MAIN CABIN FWD WET AREA STA 328 RBL24 FLOORBEAM UPPER FLANGE CORRODED. REMOVED AND REPLACED FLOORBEAM UPPER FLANGE ONBS 328 RBL0 TO .63.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 58,973 hrs · 39,159 cycles

MAIN CABIN FWD WET AREA STA 312 TO 328 RBL 33 INTERCOSTAL IS CRACKED. REMOVED AND INSTALLED NEW WER IN MAIN CABIN FWD AREA STA 312-320 RBL 33.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 58,973 hrs · 39,159 cycles

MAIN CABIN FWD WET AREA STA 277 TO 294.5 BL0 INTERCOSTAL CRACKED. REMOVED AND INSTALLED NEW WET AND MAIN CABIN FWD AREA STA 277 TO 294.5 BLO.

Part: STRAP — CORRODED (FUSELAGE) · airframe 58,973 hrs · 39,159 cycles

AT STATION 1016 SHEAR WEB STRAP AT RBL 25 HAS CORROSION. REMOVE + REPLACED STRAP @ STP 1016 RBL 25.

Part: SUPPORT FITTING — CORRODED (FUSELAGE) · airframe 58,973 hrs · 39,159 cycles

MAIN CABIN FWD WET AREA STA 344 LBL64 SUPPORT FITTING CORRODED. REMOVED CORRODED MOUNT AND INSTALLED NEW MOUNT.

Part: MOUNT — CORRODED (FUSELAGE) · airframe 58,973 hrs · 39,159 cycles

MAIN CABIN FWD WET AREA STA 312 LBL 64 SUPPORT MOUNT IS CORRODED. REMOVED CORRODED MOUNT AND INSTALLED NEW MOUNT.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 58,973 hrs · 39,159 cycles

FLOORBEAM AT STATION 947.5 LT SIDE HAS CORROSION. CORROSION ALSO IS RUNNING UNDER L-2 DOOR INNER CHORD. REPAIRED FLOORBEAM UPPER T-CAP @ STA 947.5 THE ENTIRE CAP.

Part: SEAL — BROKEN (PANEL) · airframe 58,973 hrs · 39,159 cycles

PANEL 671CB HAS ATTACHING PANEL WITH SEAL THAT IS BROKEN. REPAIRED PANEL 671CB. RESTORED FINISH.

Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 58,973 hrs · 39,159 cycles

DAMAGED FLOOR PANEL 231BF AT CORNER. REPAIRED DAMAGED FLOOR PANEL 231 BF AT CORNER.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 58,973 hrs · 39,159 cycles

R1 CABIN DOOR MOP SILL HAS CORROSION. REMOVED AND REPLACED R1 CABIN DOOR MOP SILL.

Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 58,973 hrs · 39,159 cycles

FLOOR PANEL 232AF 4 CORNERS DAMAGED. REPAIRED DAMAGED FLOOR PANEL 232AF (4 CORNERS).

Part: STRAP — CORRODED (FUSELAGE) · airframe 58,973 hrs · 39,159 cycles

AT STATION 1016 SHEAR WEB STRAP ON RT SIDE HAS CORROSION. REMOVED + REPLACED SHEAR WEB STRAP @ STA 1016 RT O/B.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 58,973 hrs · 39,159 cycles

MAIN CABINFWD WET AREA STA 328 RBL 47 FLOORBEAM UPPER FLANGE SHOWS CORROSION. REMOVED AND REPLACED FLOORBEAM UPPER FLANGE AT STA 328 RBL 47.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 58,973 hrs · 39,159 cycles

AFT FLOORBEAM, BS 986.5 RBL 0 TO RBL 13 HAS CORROSION. ALL WORK ACCOMPLISHED.

Part: STRAP — CORRODED (FUSELAGE) · airframe 58,973 hrs · 39,159 cycles

AT STATION 1016 SHEAR WEB STRAP AT RBL 0 HAS CORROSION. REMOVED + REPLACED SHEAR WEB STRAP @ STA 1016 RB10.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 58,973 hrs · 39,159 cycles

AFT FLOORBEAM BS 986.5, LBL 0, TO LBL 13. HAS CORROSION. ALL WORK ACCOMPLISHED.

Part: SHEAR WEB — CORRODED (FUSELAGE) · airframe 58,973 hrs · 39,159 cycles

STATION 986.5 RT SIDE CLOSE OUT WEB HAS CORROSION ON TOP AND BOTTOM SIDE. REMOVED + REPLACED LT + RT SHEAR WEB FROM STATION 986-1016.

Part: STRAP — CORRODED (FUSELAGE) · airframe 58,973 hrs · 39,159 cycles

AT STATION 1016 SHEAR WEB STRAP HAS CORROSION AT LBL 0. REMOVED + REPLACED STRAP @ STATION 1016 SHEAR WEB @ LBL 0.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · airframe 58,973 hrs · 39,159 cycles

L1 MAIN CABIN DOOR MOP SILL ATTACH ANGLE HAS CORROSION. REMOVED AND REPLACED ANGLE AT L1 MAIN CABIN DOOR MOP SILL.

Part: PANEL — DAMAGED (WING) · airframe 58,973 hrs · 39,159 cycles

DAMAGED FASTENER HOLES IN PANEL 521JB (2 EACH). REPAIRED DAMAGED FASTENER HOLES ON PANEL 521JB (2 EACH) AND PRIMED PANEL 521JB AND PAINTED PANEL 521JB.

Part: SUPPORT ROD — WORN (RT WING) · airframe 58,973 hrs · 39,159 cycles

RT LOWER TRAILING EDGE PNL SUPPORT ROD ATTACH POINTS WORN, ROD IS LOOSE. (AT WS 317, MARKED WITH STREAMER). REMOVED RT TE PNL SUPPORT ROD. REPLACED BUSHINGS AND INSTALLED ROD.

Part: PANEL — DAMAGED (WING) · airframe 58,973 hrs · 39,159 cycles

PANEL 621LB ENLARGED HOLE. REPAIRED PNL 621LB.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 58,973 hrs · 39,159 cycles

AFT FLOORBEAM, BS 986.5 RBL 13 TO DOOR SILL HAS CORROSION. REPLACED UPPER T-CAP @ STP 986.5.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 58,973 hrs · 39,159 cycles

AFT FLOORBEAM, BS 986.5, LBL13N TO DOOR SILL HAS CORROSION. ALL WORK ACCOMPLISHED.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 58,973 hrs · 39,159 cycles

MAIN CABIN FWD WET AREA STA 312 TO 328 LT INTERCOSTAL CRACKED. REMOVED AND REPLACED ON MAIN CABIN FWD WET AREA STA 312 TO 328 LT INTERCOSTAL.

Part: CLOSEOUT PANEL — CRACKED (LT MLG WW) · airframe 58,973 hrs · 39,159 cycles

CLOSE OUT PNL ON AFT SIDE OF LT WHEEL WELL CRACKED. REPAIRED CLOSE OUT PNL ON AFT SIDE OF LT WHEEL WELL.

Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 58,973 hrs · 39,159 cycles

FLOOR PANEL 222DF HAS 2 CORNERS DAMAGED. REPAIRED DAMAGED FLOOR PANEL 222DF (2 CORNERS).

Part: BRACKET — CORRODED (FUSELAGE) · airframe 58,973 hrs · 39,159 cycles

AFT FLOORBEAM, BS 992.8 LBL24 GALLEY MOUNT HAS CORROSION. FABRICATED NEW BRACKET AFT FLOORBEAM BS 992.8 LBL 24.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 58,973 hrs · 39,159 cycles

MAIN CABIN FWD WET AREA STA 270 TO 277 BL0 INTERCOSTAL CRACKED. REMOVED AND INSTALLED NEW WET AND MAIN CABIN FWD AREA STA 270 TO STA 277 BLO.

Part: SCUFF PLATE — CRACKED (FUSELAGE) · airframe 58,973 hrs · 39,159 cycles

AFT DOOR CARGO DOOR SCUFF-PLATE CRACKED. LOCATED AND DRILLED AFT DOOR CARGO DOOR SCUFF PLATE. INSTALLED NEW SCUFF PLATE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 57,823 hrs · 38,488 cycles

21ABC EMERGENCY LIGHT INOP. R&R LAMP 21ABC EMERGENCY LIGHT. OPS CHECK OK.

Part: BATTERY PACK — FAILED (CABIN) · airframe 56,690 hrs · 37,845 cycles

EMERGENCY BATTERY PACK CAPACITY FUNCTIONAL CHECK. SEAT 13 AND 9 CBA EMERGENCY LIGHTS FAILED AT 10 MINUTES INTO TEST. REMOVED AND REPLACED POWER SUPPLY M1670 AT STA 727C +13 AND INSTALLED NEW BATTERY PACK. BATTERY NEEDS CHARGE AND CAPACITY CHECK. AIRGRILL REMOVED, NEEDS INSTALL. PERFORMED CAPACITY CHECK. NO DEFECTS NOTED. OK FOR SERVICE.

Part: POWER SUPPLY — FAILED (CABIN) · airframe 56,690 hrs · 37,845 cycles

EMERGENCY BATTERY PACK CAPACITY FUNCTIONAL CHECK. AFT CARGO EMERGENCY LIGHT FAILED TEST AT 10 MINUTES INTO TEST. REMOVED AND REPLACED POWER SUPPLY M1670 AT STA 727C+13 AND INSTALLED NEW BATTERY PACK. BATTERY NEED CHARGE AND CAPACITY CHECK. PERFORMED CAPACITY CHECK. NO DEFECTS NOTED. OK FOR SERVICE.

Part: SKIN — CRACKED (NR 8 SLAT) · airframe 56,031 hrs · 37,486 cycles

DURING A WALK AROUND, FOUND A CRACK IN THE NR 8 SLAT CENTER LINE 3/8 INCH ON ONE SIDE AND 1/8 INCH ON THE OTHER OF RIVET HOLE AT SLAT ACTUATOR MOUNT AREA. REMOVED AND REPLACED THE NR 8 LEADING EDGE SLAT.

Part: SKIN — CRACKED (L1 DOOR) · airframe 55,813 hrs · 37,396 cycles

L1 DOOR APPEARS TO HAVE ABOUT A 3" CRACK ON THE EXTERIOR SKIN LOCATED AT THE LOWER FORWARD CORNER ABOVE THE GATE. REMOVED DOOR SLIDE AND LINER FOR ACCESS AND REMOVED FASTENERS AS REQUIRED. CUT OUT CRACKED SKIN. REQUIRES HFEC INSPECTION TO ENSURE DAMAGE REMOVED. HFEC TO ENSURE DAMAGE IS REMOVE WAS ACCOMPLISHED. NO CRACKS NOTED. ORIGINAL SKIN MAX THICKNESS IN CUTOUT AREA IS .063". FABRICATED .063" FILLER FROM 2024-T3 AND .071" 2024-T3 DOUBLER. READY TO INSTALL. LEVELING COMPOUND NEEDS TO BE CLEANED FROM INNER LOWER CORNER. INSTALLED DOUBLER. NEEDS LINER AND SLIDE REINSTALLED. OK TO INSTALL REPAIR WAS GIVEN BEFORE REPAIR WAS INSTALLED. RII ACCOMPLISHED ON REPAIR. OK TO INSTALL DOOR LINER. INSTALLED LINER. OK TO INSTALL DOOR SLIDE. INSTALLED SLIDE. RII ACCOMPLISHED ON DOOR SLIDE INSTALLATION.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 54,073 hrs · 36,736 cycles

FWD PIT CARGO THRESHOLD WEB HAS MULTIPLE SPOTS OF CORROSION. REMOVED "OUT OF LIMITS" FWD PIT CARGO THRESHOLD WEB.(100% LOSS). INSTALLED NEW-58 WEB AS REQ'D.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 54,073 hrs · 36,736 cycles

AFT CARGO COMPARTMENT THRESHOLD WEB CORRODED FROM STA 790-807. BLENDED CORROSION ON AFT CARGO THRESHOLD WEB, FOUND ORIG. 100% MATERIAL LOSS TO BE "OUT OF LIMITS". REMOVED & REPLACED THRESHOLD WEB.

Part: SUPPORT — WORN (FUSELAGE) · airframe 54,073 hrs · 36,736 cycles

SUPPORT STRUCTURE FOR RT WTB PANEL (193AR) IS WORN IN SEVERAL SPOTS. BLENDED WEAR SPOTS ON RT PANEL 193AR SUPPORT STRUCTURE. FOUND TO BE 100% AND LOSS. REMOVED AND REPLACED FRAME PART NUMBER 149A7214-20.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 54,073 hrs · 36,736 cycles

AFT CARGO COMPARTMENT STA 727D+12-767 RT Z ANGLE HEAVILY CORRODED AROUND FASTENER HOLES. REMOVED CORROSION RT Z ANGLE STA 727D+12" - 767, ORIG T .045" WITH .013" REMAINING .032", OUT OF LIMITS. REMOVED & REPAIRED Z ANGLE STA 727D+12 - 767.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 54,073 hrs · 36,736 cycles

FWD CARGO COMPARTMENT AFT BULKHEAD LOWER CENTER SUPPORT HAS CORROSION. REMOVED DAMAGED FWD CARGO COMPARTMENT AFT BULKHEAD LOWER CENTER SUPPORT AND REPLACED IT.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 54,073 hrs · 36,736 cycles

FWD CARGO Z SHIELD AFT OF CARGO DOOR OPENING STA 490-500A. RT SIDE MULTIPLE SPOTS OF HEAVY CORROSION. BLENDED CORROSION ON FWD CARGO Z SHIELD AND FOUND TO BE 100% MATERIAL LOSS. FABRICATED AND INSTALLED NEW Z SHIELD.

Part: SUPPORT — CRACKED (RT WING) · airframe 54,073 hrs · 36,736 cycles

RT I/B WING JUST FWD OF RT MLG WHEEL WELL, PANEL SUPPORT ROD ABOVE 651BB HAS 1.5" CRACK. REPLACED SUPPORT ROD ON RT I/B WING FORWARD OF RT MLG WHEEL WELL ABOVE PANEL 651 BB.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 54,073 hrs · 36,736 cycles

AFT CARGO COMPARTMENT STA 807-827 RT Z SHIELD CORRODED AROUND FASTENER HOLES. REMOVED CORROSION ON 2 CHANNEL 100% LOSS OF MATERIAL, FOUND OUT OF LIMITS. REMOVED RECEIVED, VERIFIED NEW PART AS 146A8127Y5. INSTALLED.

Part: PANEL — DEBONDED (LE SLAT) · airframe 54,073 hrs · 36,736 cycles

RIGHT WING, SLAT PANEL 621JB HAS A DISBONDED CORNER. REPAIRED DAMAGE TO RIGHT WING, SLAT PANEL 621 JB.

Part: THRESHOLD — CRACKED (FUSELAGE) · airframe 54,073 hrs · 36,736 cycles

WHILE REMOVING AFT CARGO AFT THRESHOLD CORNER TO ACCESS THE CORROSION ON WEB FOUND LARGE CRACK IN THRESHOLD RADIUS. LOCATED & DRILLED NEW AFT CARGO AFT THRESHOLD CORNER P/N 654A0004-169.

Part: RUB STRIP — DAMAGED (TE FLAP) · airframe 54,073 hrs · 36,736 cycles

LT WING, OUTBOARD FLAP, INBD TRAILING EDGE RUB STRIP DAMAGED. REPLACED DAMAGE PORTION OF RUB STRIP ON LT WING OUTBOARD FLAP.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 54,073 hrs · 36,736 cycles

FWD CARGO LT Z ANGLE STA 380-500D MULTIPLE SPOTS OF HEAVY CORROSION AT FASTENER HOLES. BLENDED CORROSION ON Z ANGLE. ORIGINAL "T" .050" REMAINING .040" LOSS OF .010" FOUND TO BE OUT OF LIMITS. REMOVED, FABRICATED, & INSTALLED NEW Z ANGLE.

Part: PANEL — DEBONDED (LT WING) · airframe 54,073 hrs · 36,736 cycles

LT WING PANEL 521JB METAL EDGE TRIM DISBONDED. REPAIRED LT WING PANEL 521JB METAL EDGE TRIM DISBOND.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 54,073 hrs · 36,736 cycles

FWD CARGO PIT RT Z ANGLE FROM STA 500-500D MULTIPLE SPOTS OF HEAVY CORROSION AT FASTENER HOLES. BLENDED CORROSION ON Z ANGLE & FOUND TO BE 100% MATERIAL LOSS. REMOVED, FABRICATED, & INSTALLED NEW Z ANGLE.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 54,073 hrs · 36,736 cycles

FWD RT EMERGENCY LIGHT BATTERY PACK DEAD. REMOVED & RESTORED RT FWD EMERGENCY LIGHT POWER SUPPLY AND BATTERY PACK. OPS CHECK GOOD.

Part: SUPPORT ANGLE — DAMAGED (FUSELAGE) · airframe 54,073 hrs · 36,736 cycles

AFT CARGO COMPARTMENT AT FORWARD BULKHEAD, STA 731 LBL21. LEFT SIDE SUPPORT ANGLE HAS ENLARGED FASTENER HOLE AT LOWER END. REMOVED & REPLACED AFT CARGO FWD BULKHEAD STA 731 LBL21 SUPPORT.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 54,073 hrs · 36,736 cycles

AFT CARGO COMPARTMENT FLOOR SUPPORTS STA 727D+6" CORRODED FROM LBL12-RBL12. REMOVED CORROSION ON AFT CARGO FLOOR SUPPORTS STA 727D+12 LBL12 - RBL 12 AND REPAIRED.

Part: THRESHOLD — CRACKED (FUSELAGE) · airframe 54,073 hrs · 36,736 cycles

WHILE REMOVING AFT CARGO FWD THRESHOLD CORNER FOUND LARGE CRACK IN RADIUS. LOCATED & DRILLED NEW AFT CARGO FWD THRESHOLD CORNER P/N 654A0004-97.

Part: PANEL — DEBONDED (RT WING) · airframe 54,073 hrs · 36,736 cycles

RT WING L/E PANEL 621HB HAS DISBONDING AT EDGE AND SEVERAL FASTENER HOLES DAMAGED. REPAIRED RT WING L/E PANEL 621 HB.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 54,073 hrs · 36,736 cycles

AFT CARGO COMPARTMENT STA 767-787 RT Z SHIELD CORRODED AROUND FASTENER HOLES. REMOVED CORROSION FROM STA 767-787, RT SIDE, Z-SHIELD. ORIG MATERIAL THICKNESS IS .050" WITH A LOSS OF .020". REMAINING MATERIAL 'T' OF .030" IS OUT OF LIMITS. REMOVED AND REPLACED WITH NEW 2-SHIELD 146A8127-1 AT STA 767-787 RT SIDE.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 54,073 hrs · 36,736 cycles

AFT CARGO COMPARTMENT LT "Z" ANGLE STA 727D+10"-847 CORRODED AROUND FASTENER HOLES. REMOVED CORROSION ON Z-ANGLE. FOUND TO BE 100% MATERIAL LOSS AND OUT OF LIMITS. REMOVED AND REPLACED LT Z-ANGLE FROM STA 727-847.

Part: PANEL — DEBONDED (LT WING) · airframe 54,073 hrs · 36,736 cycles

LT WING PANEL 521WB METAL EDGE TRIM DISBONDED. REPAIRED LT WING PANEL 521WB METAL EDGE TRIM DISBOND.

Part: RUB STRIP — DAMAGED (LT SPOILER) · airframe 54,073 hrs · 36,736 cycles

LT WING, INBD GROUND SPOILER, TRAILING EDGE RUB STRIP DAMAGED. REPLACED LT WING, INBD GROUND SPOILER, TRAILING EDGE RUB STRIP.

Part: PANEL — DEBONDED (LT WING) · airframe 54,073 hrs · 36,736 cycles

LT WING PANELS 521CB METAL EDGE TRIM DISBONDED. REPAIRED DAMAGE TO LT WING PANEL 521CB.

Part: MOUNT — WORN (FLAP FAIRING) · airframe 54,073 hrs · 36,736 cycles

NR 6 FWD FLAP TRACK FAIRING FWD MOUNT IS WORN. REMOVED & REPLACED NR 6 FWD FLAP TRACK FWD FAIRING MOUNT.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 54,073 hrs · 36,736 cycles

FORWARD CARGO COMPARTMENT AFT BULKHEAD RT SUPPORT ANGLE IS CORRODED AT FLOOR LEVEL, RBL23 TO RBL26. BLENDED CORROSION ON FWD CARGO COMP AFT BULKHEAD RT SUPPORT ANGLE & FOUND ORIGINAL "T" .071" REMAINING .052" LO0SS OF .019". FOUND TO BE OUT OF LIMITS. LOCATED, DRILLED, & INSTALLED NEW SUPPORT ANGLE.

Part: PANEL — DEBONDED (LT WING) · airframe 54,073 hrs · 36,736 cycles

LT WING PANEL 521ZB METAL EDGE TRIM DISBONDED. REPAIRED LT WING PANEL 5212B METAL EDGE.

Part: RUB STRIP — DAMAGED (RT SPOILER) · airframe 54,073 hrs · 36,736 cycles

RT WING, INBD GROUND SPOILER, TRAILING EDGE RUB STRIP DAMAGED. REPLACED RT WING, INBD GROUND SPOILER, TRAILING EDGE RUB STRIP.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 54,073 hrs · 36,736 cycles

AFT CARGO COMPARTMENT LT Z-ANGLE AT STA 727E+9 TO 777 HAS MULTIPLE CORRODED FASTENER HOLES ON UPPER AND LOWER SURFACE AREAS. REMOVED CORROSION ON Z-ANGLE. FOUND TO BE 100% MATERIAL LOSS AND OUT OF LIMITS. Z-ANGLE REPLACED.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 54,073 hrs · 36,736 cycles

AFT CARGO COMPARTMENT FLOOR SUPPORT STA 787+10" RBL 17 IS CORRODED AROUND FASTENER HOLES. REMOVED CORRODED OUT OF LIMITS FLR SUPPORT RBL 13.64 STA 757-867 AND INSTALLED NEW FLOOR SUPPORT AS REQ'D.

Part: IRU — MALFUNCTIONED (COCKPIT) · airframe 51,881 hrs · 35,862 cycles

IRS FAULT DURING APPROACH PHASE OF FLIGHT, BELOW 19,000 FT. R&R LEFT IRU. OPS CHECK NORMAL - NO FAULTS SHOWING.

Part: FRAME — CRACKED (BS 500A) · airframe 51,472 hrs · 35,668 cycles

BS 500A FRAME CRACKED AT THE BRACKET ATTACHMENT INBD FASTENER BETWEEN STRINGERS 8 AND 9R. VERIFIED WITH HFEC AND MFEC. REPAIRED THE FRAME.

Part: FUSE — BURNED OUT (EMERGENCY LIGHTS) · airframe 51,472 hrs · 35,668 cycles

RIGHT OVERWING EXIT, FWD LOWER BATTERY POWER SUPPLY FOUND TO BE MISSING OUTPUT. REPLACED BURNED FUSES ON THE POWER SUPPLY. TEST PASSED.

Part: FRAME — CRACKED (BS 747) · airframe 51,472 hrs · 35,668 cycles

BS 747 FRAME CRACKED AT THE BRACKET ATTACHMENT INBD FASTENER BETWEEN STRINGERS 8 AND 9R. VERIFIED WITH HFEC AND MFEC. REPAIRED THE FRAME.

Part: FRAME — CRACKED (BS 827) · airframe 51,472 hrs · 35,668 cycles

BS 827 FRAME CRACKED AT BRACKET ATTACHMENT INBD FASTENER BETWEEN STRINGER 8 AND 9L. VERIFIED WITH HFEC AND MFEC. REPAIRED THE FRAME.

Part: FRAME — CRACKED (BS 867) · airframe 51,472 hrs · 35,668 cycles

BS 867 FRAME CRACKED AT BRACKET ATTACHMENT INBD FASTENER BETWEEN STRINGER 8 AND 9L. VERIFIED WITH HFEC AND MFEC. REPAIRED THE FRAME.

Part: FRAME — CRACKED (BS 787) · airframe 51,472 hrs · 35,668 cycles

BS 787 FRAME CRACKED AT THE BRACKET ATTACHMENT INBD FASTENER BETWEEN STRINGER 8 AND 9R. VERIFIED WITH HFEC AND MFEC. REPAIRED THE FRAME.

Part: FRAME — CRACKED (FUSELAGE) · airframe 51,472 hrs · 35,668 cycles

AD DRIVEN. STA 360 LT FRAME CRACKED AT AC BRACKET ATTACHMENT IB FASTENER BETWEEN S-8 AND S-9. VERIFIED WITH HFEC AND MFEC. REPAIRED STA 360 LT FRAME BETWEEN S-8 & S-9.

Part: FRAME — CRACKED (BS 500A) · airframe 51,472 hrs · 35,668 cycles

BS 500A FRAME CRACKED BETWEEN STRINGERS 8 AND 9L. VERIFIED WITH HFEC AND MFEC. REPAIRED THE FRAME.

Part: FRAME — CRACKED (BS 827) · airframe 51,472 hrs · 35,668 cycles

BS 827 FRAME CRACKED AT THE BRACKET ATTACHMENT INBD FASTENER BETWEEN STRINGER 8 AND 9R. VERIFIED WITH HFEC AND MFEC. REPAIRED THE FRAME.

Part: FRAME — CRACKED (BS 440) · airframe 51,472 hrs · 35,668 cycles

BS 440 FRAME CRACKED AT THE BRACKET ATTACHMENT INBD FASTENER BETWEEN STRINGER 8 AND 9R. VERIFIED WITH HFEC AND MFEC. REPAIRED THE FRAME.

Part: DIFFUSER — CRACKED (BS 727D-727E) · airframe 51,472 hrs · 35,668 cycles

PSU RAIL DIFFUSER ASSY CRACKED BS 727D-727E. REMOVED AND INSTALLED A NEW PSU RAIL DIFFUSER ASSY.

Part: FRAME — CRACKED (FUSELAGE) · airframe 51,472 hrs · 35,668 cycles

AD DRIVEN. STA 400 LT FRAME CRACKED AT AC BRACKET ATTACHMENT IB FASTENER BETWEEN S-8 AND S-9. VERIFIED WITH HFEC AND MFEC. REPAIRED STA 400 LT FRAME BETWEEN S-8 & S-9.

Part: SKIN — PUNCTURED (FUSELAGE) · airframe 51,472 hrs · 35,668 cycles

WING TO BODY PANEL 193AR HAS THREE PUNCTURES TO EXTERIOR SKIN. REPAIRED THE PUNCTURES TO EXTERIOR SKIN ON PANEL 193AR.

Part: SUPPORT BRACKET — CRACKED (BS 360) · airframe 51,472 hrs · 35,668 cycles

BS 360 FRAME SUPPORT BRACKET CRACKED BETWEEN STRINGERS 8 AND 9R. REMOVED AND REPLACED SUPPORT BRACKET.

Part: FRAME — CRACKED (BS 480) · airframe 51,472 hrs · 35,668 cycles

BS 480 FRAME CRACKED AT THE BRACKET ATTACHMENT INBD FASTENER BETWEEN STRINGER 8 AND 9R. VERIFIED WITH HFEC AND MFEC. REPAIRED THE FRAME.

Part: BRACKET — CRACKED (L1 DOOR) · airframe 51,472 hrs · 35,668 cycles

L1 DOOR UPPER SUPPORT BRACKET ASSY HAS A CRACK. DRILLED & TRIMMED NEW BRACKET. PRIMED, PAINTED, AND INSTALLED NEW BRACKET.

Part: FRAME — CRACKED (BS 727D) · airframe 51,472 hrs · 35,668 cycles

BS 727D FRAME CRACKED BETWEEN STRINGER 8 AND 9L. VERIFIED WITH HFEC AND MFEC. REPAIRED THE FRAME.

Part: SEAL — WORN (HORIZONTAL STAB) · airframe 51,472 hrs · 35,668 cycles

RIGHT HORIZONTAL STABILIZER, GAP COVER PANEL, 343AB, AFT METAL SLIDING SEAL WORN THROUGH. REMOVED AND REPLACED METAL SLIDER SEAL ON PANEL 343AB.

Part: FRAME — CRACKED (BS 907) · airframe 51,472 hrs · 35,668 cycles

BS 907 FRAME CRACKED AT THE BRACKET ATTACHMENT INBD FASTENER BETWEEN STRINGERS 8 AND 9R. VERIFIED WITH HFEC AND MFEC. REPAIR THE FRAME.

Part: HANDLE — MALFUNCTIONED (AFT CARGO DOOR) · airframe 51,472 hrs · 35,668 cycles

AFT CARGO DOOR HANDLE HARD TO PULL OUT AND PAN IS GOUGED. REMOVED AND REPLACED AFT CARGO DOOR HANDLE ASSY.

Part: FRAME — CRACKED (FUSELAGE) · airframe 51,472 hrs · 35,668 cycles

AD DRIVEN. STA 480 LT FRAME CRACKED AT AC BRACKET ATTACHMENT IB FASTENER BETWEEN S-8 AND S-9. VERIFIED WITH HFEC AND MFEC. REPAIRED STA 480 LT FRAME BETWEEN S-8 & S-9.

Part: BALANCE WEIGHT — ERODED (RUDDER) · airframe 51,472 hrs · 35,668 cycles

RUDDER BALANCE ARM WEIGHT ON LEADING EDGE ERODED. REMOVED AND REPLACED RUDDER BALANCE ARM WEIGHT.

Part: FAIRING — PUNCTURED (RT WNG-BODY) · airframe 51,472 hrs · 35,668 cycles

RIGHT MAIN WHEEL WELL WING TO BODY PANEL 193AR HAS COMPOSITE DAMAGE IN INTERIOR SIDE. REPAIRED THE PUNCTURES TO INTERIOR SIDE OF PANEL 193AR.

Part: INSERT — DAMAGED (FLOORBOARD) · airframe 51,472 hrs · 35,668 cycles

FLOORBOARD 242AF HAS A DAMAGED INSERT. REPLACED THE FLOORBOARD INSERTS.

Part: DEFLECTOR — DAMAGED (LT WING) · airframe 51,472 hrs · 35,668 cycles

LEFT WING TE DEFLECTOR PANEL IS LOOSE AT SERRATED PLATES. REPAIRED THE DEFLECTOR PANEL.

Part: RIVET — SHEARED (RT WING LE) · airframe 51,472 hrs · 35,668 cycles

RIGHT WING UPPER SURFACE FIXED LEADING EDGE JUST INBD OF PYLON HAS SEVERAL RIVETS WITH SHEARED HEADS. REPLACED THE FASTENERS.

Part: DIFFUSER — CRACKED (BS 727-727A) · airframe 51,472 hrs · 35,668 cycles

PSU RAIL DIFFUSER ASSY. CRACKED BS 727-727A. REMOVED AND INSTALLED A NEW PSU RAIL DIFFUSER ASSY.

Part: FRAME — CRACKED (BS 727B) · airframe 51,472 hrs · 35,668 cycles

BS 727B FRAME CRACKED BETWEEN STRINGERS 8 AND 9L. VERIFIED WITH HFEC AND MFEC. REPAIRED THE FRAME.

Part: BALANCE ARM — CORRODED (VERTICAL STAB) · airframe 51,472 hrs · 35,668 cycles

VERTICAL STABILIZER, RUDDER BALANCE WEIGHT ARM, LT AND RT LOWER AFT BLADE SEALS CORRODED. REPLACED THE LT & RT VERTICAL STABILIZER RUDDER BALANCE WEIGHT ARM LOWER AFT SEAL.

Part: ATTACH ANGLE — CORRODED (VERTICAL STAB) · airframe 51,472 hrs · 35,668 cycles

VERTICAL STABLIZER FIN T/E, RIB ATTACH ANGLE RT SIDE CORRODED WL 147.09. REPAIRED THE VERITICAL STABLIZER FIN TE RIB ATTACH ANGLE.

Part: DIFFUSER — CRACKED (BS 787-807) · airframe 51,472 hrs · 35,668 cycles

PSU RAIL DIFFUSER ASSY CRACKED BS 787-807. REMOVED AND INSTALLED PSU RAIL DIFFUSER ASSY.

Part: FRAME — CRACKED (BS 500C) · airframe 51,472 hrs · 35,668 cycles

BS 500C FRAME CRACKED BETWEEN STRINGERS 8 AND 9L. VERIFIED WITH HFEC AND MFEC. INSTALLED REPAIR ANGLES.

Part: SEAL — WORN (HORIZONTAL STAB) · airframe 51,472 hrs · 35,668 cycles

LEFT HORIZONTAL STABILIZER, GAP COVER PANEL, 333AB, AFT METAL SLIDING SEAL WORN THROUGH. REMOVED AND REPLACED METAL SLIDER SEAL ON PANEL 333AB.

Part: FRAME — CRACKED (BS 400) · airframe 51,472 hrs · 35,668 cycles

BS 400 FRAME CRACKED AT THE BRACKET ATTACHMENT INBD FASTENER BETWEEN STRINGER 8 AND 9R. VERIFIED WITH HFEC AND MFEC. REPAIRED THE FRAME.

Part: FRAME — CRACKED (BS 360) · airframe 51,472 hrs · 35,668 cycles

BS 360 FRAME CRACKED AT THE BRACKET ATTACHMENT INBD FASTENER BETWEEN STRINGER 8 AND 9R. VERIFIED WITH HFEC AND MFEC. REPAIRED THE FRAME.

Part: FRAME — CRACKED (BS 907) · airframe 51,472 hrs · 35,668 cycles

BS 907 FRAME CRACKED AT BRACKET ATTACHMENT INBD FASTENER BETWEEN STRINGER 8 AND 9L. VERIFIED WITH HFEC AND MFEC. REPAIRED THE FRAME.

Part: FRAME — CRACKED (BS 747) · airframe 51,472 hrs · 35,668 cycles

BS 747 FRAME CRACKED BETWEEN STRINGER 8 AND 9L. VERIFIED WITH HFEC AND MFEC. REPAIRED THE FRAME.

Part: FRAME — CRACKED (BS 520) · airframe 51,472 hrs · 35,668 cycles

BS 520 FRAME CRACKED AT THE BRACKET ATTACHMENT INBD FASTENER BETWEEN STRINGERS 8 AND 9R. VERIFIED WITH HFEC AND MFEC. REMOVED THE DAMAGE AND FABRICATED AND INSTALLED REPAIR.

Part: FRAME — CRACKED (BS 727D) · airframe 51,472 hrs · 35,668 cycles

BS 727D FRAME CRACKED AT THE BRACKET ATTACHMENT INBD FASTENER BETWEEN STRINGERS 8 AND 9R. VERIFIED WITH HFEC AND MFEC. REPAIRED THE FRAME.

Part: FRAME — CRACKED (BS 787) · airframe 51,472 hrs · 35,668 cycles

BS 787 FRAME CRACKED AT BRACKET ATTACHMENT INBD FASTENER BETWEEN STRINGERS 8 AND 9L. VERIFIED WITH HFEC AND MFEC. REPAIRED THE FRAME.

Part: FRAME — CRACKED (BS 867) · airframe 51,472 hrs · 35,668 cycles

BS 867 FRAME CRACKED AT THE BRACKET ATTACHMENT INBD FASTENER BETWEEN STRINGERS 8 AND 9R. VERIFIED WITH HFEC AND MFEC. REPAIRED THE FRAME.

Part: BOLT — LOOSE (RT WING) · airframe 51,472 hrs · 35,668 cycles

RIGHT WING OTBD FLAP INBD FIXED T/E SUPPORT RIB ATTACH BOLTS LOOSE AT SERRATED PLATES. REPAIRED THE WING OB FLAP IB FIXED T/E DEFLECTION CONTROL RIB.

Part: DIFFUSER — CRACKED (BS 727B-727C) · airframe 51,472 hrs · 35,668 cycles

PSU RAIL DIFFUSER ASSY CRACKED BS 727B-727C. REMOVED AND INSTALLED A NEW PSU RAIL DIFFUSER ASSY.

Part: FRAME — CRACKED (BS 500C) · airframe 51,472 hrs · 35,668 cycles

BS 500C FRAME CRACKED AT THE BRACKET ATTACHMENT INBD FASTENER BETWEEN STRINGERS 8 AND 9R. VERIFIED WITH HFEC AND MFEC. REPAIRED THE FRAME.

Part: FAIRING — CHAFED (WING TO BODY) · airframe 51,472 hrs · 35,668 cycles

WING TO BODY PANEL 193AR I/B EDGE BAND IS CHAFED AND GOUGED. REPAIRED PANEL 193AR I/B EDGEBAND.

Part: CHARGER — NO TEST (EMERGENCY LIGHTS) · airframe 51,030 hrs · 35,505 cycles

LEFT EMERGENCY LIGHT BATTERY PACK FAILED CAPACITY CHECK. REMOVED AND REPLACED THE BATTERY PACK AND CHARGER. FUNCTIONAL CHECK GOOD.

Part: CHARGER — NO TEST (EMERGENCY LIGHTS) · airframe 51,030 hrs · 35,505 cycles

LEFT FWD EMERGENCY BATTERY PACK FAILED CAPACITY CHECK. REMOVED AND REPLACED THE BATTERY PACK AND CHARGER. FUNCTIONAL CHECKED GOOD.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 51,030 hrs · 35,505 cycles

RIGHT AFT EMERGENCY LIGHT BATTERY PACK FAILED CAPACITIANCE CHECK. R & R THE BATTERY PACK. OPS TESTED GOOD.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 51,030 hrs · 35,505 cycles

RIGHT OVERWING WINDOW EMERGENCY LIGHT BATTERY PACK FAILED CAPACITIANCE CHECK. R & R BATTERY PACK. OPS CHECKED GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 51,030 hrs · 35,505 cycles

ROW 22DEF EMERENCY LIGHT INOPERATIVE. REPLACED THE LAMP.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 51,030 hrs · 35,505 cycles

LEFT AFT EMERGENCY LIGHT BATTERY PACK NOT CHARGING. R & R THE BATTERY PACK AND CHARGER. FUNCTION CHECKED GOOD.

Part: WINDOW FRAME — CRACKED (R1) · airframe 50,700 hrs · 35,382 cycles

WHILE INSPECTING R1 WINDOW FRAME, FOUND THE UPPER OUTBOARD FRAME CRACKED. ACCOMPLISHED REPAIR.

Part: WINDOW FRAME — CRACKED (R1) · airframe 50,700 hrs · 35,382 cycles

R1 UPPER OUTBOARD WINDOW FRAME IS CRACKED. ACCOMPLISHED REPAIR.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 45,028 hrs · 33,064 cycles

R2 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE, REPLACED THE LAMP.

Part: DOOR SILL — CORRODED (CARGO DOORWAY) · airframe 43,717 hrs · 32,580 cycles

AFT CARGO DOOR SURROUND LOWER SILL PLATE CORRODED ON UPPER AND LOWER SURFACE. AFT CARGO DOOR SURROUND LOWER SILL PLATE FOUND TO BE OUT OF LIMITS. FABRICATED WEB AND INTALLED.

Part: CARGO TRACK — CORRODED (BS 943) · airframe 43,717 hrs · 32,580 cycles

AFT CARGO BAY TIE DOWN TRACK AT LBL 3.0, CORRODED AROUND NUTPLATES AT THE AFT TIE-DOWN JUST FWD OF BS 943. BLENDED CORROSION ON TIE DOWN TRACK AND FOUND TO BE OUT OF LIMITS. R & R TRACK ASSY.

Part: FLOOR SUPPORT — CORRODED (CARGO BAY) · airframe 43,717 hrs · 32,580 cycles

FWD CARGO DOOR SURROUND AFT BOTTOM TRANSITION STRIP FLOOR SUPPORT CORRODED. INSTALLED NEW FWD CARGO DOOR SURROUND AFT BOTTOM TRANSITION STRIP FLOOR SUPPORT.

Part: INTERCOSTAL — CRACKED (BS 344) · airframe 43,717 hrs · 32,580 cycles

BS 344, BL 0 FOUND INTERCOSTAL CRACKED. LOCATED, DRILLED AND REPLACED THE INTERCOSTAL.

Part: INTERCOSTAL — CRACKED (BS 328-344) · airframe 43,717 hrs · 32,580 cycles

FOUND CRACKED INTERCOSTAL BETWEEN BS 328-344 INSIDE L1 DOOR. REMOVED DAMAGE. FABRICATED, LOCATE, DRILLED AND INSTALLED REPAIR.

Part: BEAM — CORRODED (BS 951-967) · airframe 43,717 hrs · 32,580 cycles

BEAM JUST INBD OF R2 MOP SEAL HAS CORROSION BETWEEN BS 951-967. BLENDED CORROSION, FOUND TO BE OUT OF LIMITS. R & R BEAM.

Part: WEB — CORRODED (BS 787-795) · airframe 43,717 hrs · 32,580 cycles

WEB ASSY BS 787-795 RBL 18 CORRODED ON UPPER SURFACE. REMOVED CORROSION FOUND TO BE OUT OF LIMITS. REMOVED, FABRICATED NEW AND INSTALLED WEB ASSY.

Part: CARGO TRACK — CRACKED (BS 794) · airframe 43,717 hrs · 32,580 cycles

AFT CARGO BAY RT BS 794, RBL 13.84 TIE DOWN TRACK HAS A CRACK ON LOWER WEB. CARGO TRACK REPLACED FROM BS 727-887.

Part: WEB — CORRODED (BS 767-787) · airframe 43,717 hrs · 32,580 cycles

AFT CARGO WEB ASSY BS 767-787 RBL 18 UPPER SURFACE CORRODED. BLENDED CORROSION FOUND TO BE OUT OF LIMITS. REMOVED, FABRICATED NEW AND INSTALLED WEB ASSY.

Part: WEB — CORRODED (BS 767-787) · airframe 43,717 hrs · 32,580 cycles

AFT CARGO WEB ASSY BS 767-787 RBL 18 UPPER SURFACE CORRODED JUST FWD OF DOOR OPENING. BLENDED CORROSION FOUND TO BE OUT OF LIMITS. R & R WEB.

Part: FLOOR SUPPORT — CORRODED · airframe 43,717 hrs · 32,580 cycles

FWD CARGO DOOR SURROUND FWD BOTTOM TRANSITION STRIP FLOOR SUPPORT NUT PLATE HOLES CORRODED. R & R FWD CARGO DOOR SURROUND FWD BOTTOM TRANSITION STRIP FLOOR SUPPORT.

Part: FLOOR SUPPORT — CORRODED (BS 986-1016) · airframe 43,717 hrs · 32,580 cycles

FLOOR SUPPORT AT ABOUT RBL 32 HAS CORROSION BETWEEN BS 986.5 - 1016. R & R FLOOR SUPPORT.

Part: CHANNEL — CORRODED (MOP SILL) · airframe 43,717 hrs · 32,580 cycles

FOUND MOP SILL CORRODED AT L2 DOOR OPENING. FOUND OUT OF LIMITS. REMOVED AND INSTALLED SERVICEABLE L2 MOP SILL.

Part: WINDOW — CRACKED (COCKPIT) · airframe 43,717 hrs · 32,580 cycles

RT FLIGHT COMPARTMENT WINDOW NR 3, FOUND TWO CRACKS. REPAIRED CRACKS.

Part: FLOORBEAM — CORRODED (BS 947) · airframe 43,717 hrs · 32,580 cycles

AFT CARGO BAY FLOORBEAM ANGLE AT BS 947.5 CORRODED ON UPPER AND LOWER SURFACE FROM RBL 3 - LBL 8.1. REMOVED ANGLE AND INSTALLED NEW.

Part: FLOOR SUPPORT — CORRODED (BS 967-986) · airframe 43,717 hrs · 32,580 cycles

FLOOR SUPPORT CAP AT LBL 16 HAS CORROSION ON THE TOP AND BOTTOM SIDE BETWEEN BS 967 - 986.5. BLENDED CORROSION FOUND TO BE OUT OF LIMITS. R & R THE FLOOR SUPPORT.

Part: FLOORBEAM — CORRODED (BS 947) · airframe 43,717 hrs · 32,580 cycles

FLOORBEAM HAS CORROSION ON THE TOP AND BOTTOM SIDE AT BS 947.5 BETWEEN LBL 16 AND RBL 16. REPAIRED FLOORBEAM.

Part: FLOOR SUPPORT — CORRODED (BS 986-1016) · airframe 43,717 hrs · 32,580 cycles

FLOOR SUPPORT AT ABOUT LBL 32 HAS CORROSION ON THE TOP AND BOTTOM SIDE BETWEEN BS 986.5 - 1016. BLENDED CORROSION FOUND TO BE OUT OF LIMITS. R & R FLOOR SUPPORT.

Part: FLOORBEAM — CORRODED (BS 992) · airframe 43,717 hrs · 32,580 cycles

RT FLOORBEAM ANGLE AT BS 992.8 HAS CORROSION. R & R RT FLOORBEAM ANGLE AT BS 992.8.

Part: FLOOR SUPPORT — CORRODED (BS 951-967) · airframe 43,717 hrs · 32,580 cycles

FLOOR SUPPORT AT LBL 16 HAS CORROSION ON THE TOP AND BOTTOM SIDE BETWEEN BS 951 - 967. BLENDED CORROSION FOUND TO BE OUT OF LIMITS. R & R FLOOR SUPPORT.

Part: FLOOR SUPPORT — CORRODED (BS 1006-1016) · airframe 43,717 hrs · 32,580 cycles

FLOOR SUPPORT AT BL 0 HAS CORROSION BETWEEN FS 1006 AND FS 1016. REMOVED CORROSION FOUND TO BE OUT OF LIMITS. FABRICATED NEW FLOOR SUPPORT.

Part: BEAM — CORRODED (BS 967-985) · airframe 43,717 hrs · 32,580 cycles

BEAM CAP AT RBL 16 HAS CORROSION ON THE TOP AND BOTTOM SIDE BETWEEN BS 967 AND 985.5. REMOVED BEAM CAP AT RBL 16 BETWEEN FS 967-985.5 CORRODED BEYOND LIMITS. REPLACED.

Part: FLOOR SUPPORT — CORRODED (BS 344) · airframe 43,717 hrs · 32,580 cycles

CABIN FLOOR SUPPORT CORRODED ABOUT BS 344. REPAIRED FLOOR SUPPORT.

Part: FLOORBEAM — CORRODED (BS 951) · airframe 43,717 hrs · 32,580 cycles

FLOORBEAM CAP AT BS 951 HAS CORROSION BETWEEN LBL 24 AND LT L2 DOOR MOP SEAL. R & R FLOORBEAM CAP.

Part: DOOR SILL — CORRODED (CARGO DOORWAY) · airframe 43,717 hrs · 32,580 cycles

AFT CARGO DOOR SURROUND LOWER SILL UPPER STRAP CORRODED. REMOVED CORROSION FOUND TO BE OUT OF LIMITS. INSTALLED NEW.

Part: CARGO TRACK — UNKNOWN (CARGO BAY) · airframe 43,717 hrs · 32,580 cycles

AFT CARGO TIE DOWN TRACK FROM BS 727-BS 887, RBL 13.8.

Part: FLOORBEAM — CORRODED (BS 986) · airframe 43,717 hrs · 32,580 cycles

FLOORBEAM HAS CORROSION ON THE TOP AND BOTTOM SIDE END TO END AT BS 986.5. REMOVED CORROSION FOUND TO BE OUT OF LIMITS. REPAIRED FLOORBEAM.

Part: FLOORBEAM — CORRODED (BS 967) · airframe 43,717 hrs · 32,580 cycles

FLOORBEAM AT BS 967 HAS CORROSION JUST INBD OF L2 DOOR MOP SEAL. REPAIRED FLOORBEAM.

Part: FLOORBEAM — CORRODED (BS 967) · airframe 43,717 hrs · 32,580 cycles

FLOORBEAM HAS CORROSION AT FS 967 BETWEEN RBL 16 AND RBL 24.

Part: CHANNEL — CORRODED (R2 DOOR MOPSILL) · airframe 43,717 hrs · 32,580 cycles

R2 DOOR MOP SILL HAS CORROSION AT SEVERAL SPOTS ON THE TOP AND BOTTOM SIDE, BETWEEN BS 951-992.8. R & R MOP SILL.

Part: FLOORBEAM — CORRODED (BS 992) · airframe 43,717 hrs · 32,580 cycles

LEFT FLOORBEAM ANGLE AT BS 992.8, HAS CORROSION. BLENDED CORROSION ON ANGLE MATERIAL LOSS OUT OF LIMITS. R & R NEW FLOORBEAM ANGLE.

Part: CIRCUIT BREAKER — TRIPPED (EMERGENCY LIGHTS) · airframe 42,695 hrs · 32,203 cycles

DURING CLIMBOUT, BOTH LT AND RT OVERWING LIGHTS ILLUMINATED. FOUND OVERWING FLIGHT LOCK RT & LT CIRCUIT BREAKERS OPEN. RESET BREAKERS AND TESTED EMERGENCY EXIT DOOR SYSTEM AND TESTS OK.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 41,612 hrs · 31,773 cycles

AFT LT OVERHEAD BIN EMERGENCY LIGHTS GO OUT IN 10 MINUTES. REPLACED POWER SUPPLY AND BATTERY PACK ABOVE AFT LEFT JUMP SEAT IN CEILING.

Part: SIGN — DETACHED (EMERGENCY LIGHTS) · airframe 41,259 hrs · 31,634 cycles

AFT GALLEY EXIT SIGN ON CEILING CAME LOOSE DURING TAKEOFF. REPLACED LIGHT ASSY.

Part: LENS — DISLODGED (EMERGENCY LIGHT) · airframe 40,974 hrs · 31,540 cycles

AFT EXIT SIGN LENS COVER FELL OFF. INSTALLED AFT OVERHEAD EXIT COVER.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 35,288 hrs · 29,594 cycles

HIGH PITCH, LOW VOLUME SQUEAL NEAR L2 WINDOW WITH DIFFERENTIAL PRESSURE ABOVE 3.0. FOUND L3 WINDOW LEAKING AT UPPER FWD CORNER. FOUND WINDOW SEAL DETERIORATED. FOUND CRACK AT SECOND HOLE ON FWD WINDOW FRAME. CRACK RUNS THROUGH FASTENER HOLE & THROUGH RADIUS ON INBOARD FWD SIDE, AND FASTENER HOLE AROUND AFT EDGE OF FRAME. REMOVED WINDOW FRAME. INSTALLED NEW WINDOW FRAME.

Part: MODULE — FAULTY (CABIN) · airframe 35,047 hrs · 29,500 cycles

EMERGENCY EXIT LIGHTS ILLUMINATED AFTER TAKEOFF WITH LIGHT SWITCH IN THE ARMED POSITION. MX REMOVED & REPLACED AFT F/A STATION CONTROL PANEL SWITCH MODULE. OPS CHECKS NORMAL.