N387DA

Part: SKIN — DAMAGED (ZONE 100) · airframe 77,496 hrs · 31,332 cycles

FUSELAGE SKIN DAMAGE FS 887 BTWN S-26L AND S-27L. C/W ERA 628536-14 REV ORIG FUSELAGE SKIN DAMAGE FS 887 BTWN S-26L AND S-27L. ENSURED PRI 628536-14 REV 0,1,2,3 MATCHES ERA 628536-14 REV ORIG.

Part: SKIN — DENTED (ZONE 100) · airframe 77,496 hrs · 31,332 cycles

DENT DAMAGE TO THE FUSELAGE SKIN SUSTAINED IN BOS. THE DENTED AREA EXISTS BETWEEN STA 891-902 AND BETWEEN STRINGERS 26L TO 27L. MAINTENANCE REPAIRED DAMAGE PER ERA 628536-14.

Part: RADOME — DAMAGED (ZONE 100) · airframe 76,119 hrs · 30,705 cycles

(LOG 6892042) DAMAGE ON FRONT LEFT OF AIRPLANE NOSE. REPAIRED DAMAGED AREA IAW ERA 624396-14 REV O. VERIFIED ER/A AND PRI REVS 1-5 MATCH.

Part: SKIN — GROUND DAMAGE (ZONE 100) · airframe 76,084 hrs · 30,686 cycles

AIRCRAFT 3717, WHILE OVERNIGHT IN ATL, A WEATHER EVENT WITH HIGH WIND PUSHED A SET OF GROUND STAIRS INTO THE LEFT SIDE OF THE FUSELAGE BETWEEN STA 177-188. CORRECTIVE ACTION: PERFORMED HFEC INSPECTION, REMOVED DAMAGED AREA AND INSTALLED REPAIR DOUBLERS AND RE-INFORCEMENT REPAIRS PER ER/A 624396-14. (LP 0834921)

Part: SKIN — DAMAGED (ZONE 100) · airframe 76,084 hrs · 30,686 cycles

AIRCRAFT 3717, IN COURSE OF ACCOMPLISHMENT OF A FUSELAGE SKIN REPAIR TO THE NOSE SKIN NEAR THE LH AOA VANE PER ER/A 624396-14, ADDITIONAL INTERNAL ACCESS IS NEEDED TO INSTALL PERMANENT FASTENERS DUE TO STRUCTURE BLOCKING THE REPAIR AREA. THE COCKPITFLOOR SUPPORT BEAM (141A5180-1 INSTL) AT LBL 24.97 NEEDS TO BE CUT AS SHOWN IN FIGURE 1. THIS ER/A PROVIDES DISPOSITIONTO CUT OUT THE FWD. TWO LIGHTENING HOLES FROM THE BEAM WEB (141A5180-15) AND THE NECESSARY RESTORATION OF THE WEB AFTERCOMPLETION OF ALL REPAIRS. THE SUBJECT BEAM WEB IS MADE FROM 0.050" THICK 7075-T6 AL BARE SHEET. CORRECTIVE ACTION: COMPLIED WITH E/RA 624671-14 REV. ORIG. PRI REV. "0","1", "2" REPAIR INSTRUCTIONAL STEPS. ENSURED ALL E/RA 624671-14 REV. ORIG. PRI REV. "0","1","2" REPAIR INSTRUCTIONAL STEPS ARE COMPLETED AND MATCH FINAL - FUSELAGE / COCKPIT FLOOR SUPPORT STRUCTURE / 24.97 SUPPORT BEAM WEB / ACCESS CUTOUT / REPAIR - ER/A 624671-14 REV. ORIG. SECTION I PERMANENT REPAIR INSTRUCTIONAL STEPS. (LP 0836186)

Part: ELEC CONNECTOR — LOOSE (ZONE 200) · airframe 75,775 hrs · 30,548 cycles

(LOG 6042606) ON S/C FOUND EMER LT. INOP AT G2 GALLEY (RED). FOUND CONNECTOR ABOVE G-2 GALLEY LOOSE. SECURED SAME. CK'S GOOD. REF B737 AMM 33-51.

Part: SEAT — LOOSE (ZONE 200) · airframe 74,905 hrs · 30,175 cycles

(LOG 5618654) DURING SEAT CK. FOUND SEATS 2AB + 4AC LOOSE IN SEAT TRACK. SECURED PER B737 AMM 25-22. CKS GOOD.

Part: WINDOW FRAME — CRACKED (L3 WINDOW) · airframe 73,466 hrs · 29,506 cycles

(LOG 0260024) LH #3 WINDOW FRAME CRACKED2ND FASTENER FROM BOTTOM. REPAIRED #3 LH WINDOW FRAME IAW DELTA ER/A 616263-14.

Part: WINDOW FRAME — CRACKED (COCKPIT WINDOW) · airframe 73,462 hrs · 29,504 cycles

(LOG 0252173) LH #3 FLIGHT COMPARTMENT WINDOW FRAME LOWER FWD CORNER CRACKED. REPAIRED PER ERA ER/A 616263-14.

Part: FLOORBEAM — CORRODED (BS 328 RBL 51) · corrosion level 2 · airframe 73,462 hrs · 29,504 cycles

(LOG 0235443) FLOOR BEAM STA 328 TOP CORROSION AROUND FASTENER RBL 51. REPAIRED FLOOR BEAM STA 328 IAW DELTA ER/A 615971-14.

Part: LUG — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 73,462 hrs · 29,504 cycles

(LOG 0233989) RH STAB AFT LOWER LUG POSSIBLE SIGNS OF PITTING CORROSION AT FWD SIDE. REPAIRED RH HORIZONTAL STAB REAR LOWER LUG & BUSHING IAW DELTA ERA 615761-14 REV ORIG.

Part: FLOORBEAM — CORRODED (BS 312) · corrosion level 2 · airframe 73,462 hrs · 29,504 cycles

(LOG 0230972) FWD FLOOR BEAM STA 312 TOP CORRODED IN SPOTS BETWEEN LBL11-46. REPAIRED FLOOR BEAM STA 312 BETWEEN LBL11-46 IAW DELTA ER/A 615636-14 REV ORIG.

Part: NOT REPORTED — DAMAGED (NOT REPORTED) · airframe 73,462 hrs · 29,504 cycles

(LOG 0231604) WHILE WORKING NON ROUTINE TO CHANGE NUTPLATES FOUND DAMAGED FASTENER HOLE. REPAIRED FASTENER HOLE IAW ER/A 615972-14 REV ORIG.

Part: CARGO TRACK — CRACKED (BS 793-847) · corrosion level 2 · airframe 73,462 hrs · 29,504 cycles

(LOG 0230130) AFT CARGO FS 793-847 RBL14 CARGO TRACK UPPER SURFACE CORRODED. AFT CARGO FS 793-847 RBL14 CARGO TRACK UPPER SURFACE CORRODED.

Part: CARGO TRACK — CRACKED (BS 727J RBL 14) · airframe 73,462 hrs · 29,504 cycles

(LOG 0230115) AFT CARGO FS 727J RBL14 CARGO TRACK CRACKED WHERE MOUNTS TO FRAME. FABRICATED & REPLACED CARGO TRACK AND SPLICE IN AFT CARGO FS 727J RBL14 IAW BOEING 737-800 SRM 53-00-53-2R.

Part: SKIN — DAMAGED (BS 500G S19-20R) · airframe 73,462 hrs · 29,504 cycles

(LOG 0225930) FUSELAGE SKIN / STA 500G / STR 19R - STR 20R FASTENER HOLE DAMAGE. REPAIRED PER ERA 615972-14.

Part: TRANSITION PANEL — DAMAGED (BS 727B-727C) · airframe 73,462 hrs · 29,504 cycles

(LOG 0223823) AFT PIT LH TRANSITION PANEL HAS ELONGED HOLE BETWEEN STA 727B-727C. REPAIRED AFT PIT LH TRANSITION PANEL BETWEEN STA 727B-727C IAW BOEING 737-800 SRM 53-00-53-2R-5.

Part: BUSHING — GOUGED (HORIZONTAL STAB) · corrosion level 2 · airframe 73,462 hrs · 29,504 cycles

(LOG 0222399) RH STAB FWD UPPER LUG BUSHING GOUGED AT FWD SIDE. REPAIRED RH STAB FWD UPPER LUG & REMOVED, REPLACED BUSHING IAW DELTA ER/A 615564-14 REV ORIG.

Part: CHANNEL — CORRODED (RT DOOR WAY) · corrosion level 2 · airframe 73,462 hrs · 29,504 cycles

(LOG 0220609) RH MOP SILL CHORD TOP CORRODED. REMOVED AND REPLACED RH MOP SILL CHORD IAW BOEING 737-800 SRM 51-40-02.

Part: FLOORBEAM — CORRODED (BS 344 LBL 8) · corrosion level 2 · airframe 73,462 hrs · 29,504 cycles

(LOG 0220618) FLOOR BEAM STA 344 LBL8 TOP CORRODED. REPAIRED FLOOR BEAM STA 344 LBL 8 IAW BOEING 737-800 SRM 53-10-51-2R-9.

Part: CHANNEL — CORRODED (L1 DOOR) · corrosion level 2 · airframe 73,462 hrs · 29,504 cycles

(LOG 0219355) LH MOP SILL CHORD TOP CORRODED L1. REMOVED AND REPLACED L1 MOP SILL CHORD IAW BOEING 737-800 SRM 51-40-02.

Part: SCUFF PLATE — CORRODED (RT SERV DOOR) · corrosion level 2 · airframe 73,462 hrs · 29,504 cycles

(LOG 0219335) RH SERVICE DOOR SCUFF PLATE SUPPORT CORRODED. REMOVED AND REPLACED SUPPORT IAW BOEING 737-800 SRM 51-40-02.

Part: INTERCOSTAL — DAMAGED (BS 986-1006) · airframe 73,462 hrs · 29,504 cycles

(LOG 0218231) INTERCOSTAL & ATTACHING CLIP STA 986-1006 HAVE ELONGATED FASTENER HOLES AT STA 986. REMOVED AND REPLACED INTERCOSTAL AND ATTACHING CLIP IAW BOEING 737-800 SRM 51-40-02.

Part: FLOORBEAM — CORRODED (BS 986) · corrosion level 2 · airframe 73,462 hrs · 29,504 cycles

(LOG 0217669) AFT FLOOR BEAM STA 986 TOP IS CORRODED BOTH RH & LH OUTBOARD ENDS. REMOVED AND REPLACED FLOOR BEAM UPPER T-CHORD STA 986 IAW BOEING 737-800 SRM 53-70-51-2R-4.

Part: MOUNT — CORRODED (LAVATORY) · corrosion level 2 · airframe 73,462 hrs · 29,504 cycles

(LOG 0216334) FWD FLOOR LAV MOUNT INTERCOSTAL LBL11.5 STA 294-312 TOP CORRODED. LOCATED & DRILLED NEW INTERCOSTAL IAW BOEING 737-800 SRM 51-40-05. INSTALL ACCOMPLISHMENT IS ON DELTA NON ROUTINE 9087851.

Part: CARGO TRACK — DAMAGED (BS 787 LBL 17) · airframe 73,462 hrs · 29,504 cycles

(LOG 0216392) AFT CARGO FS 787 LBL17 CARGO TRACK TIE DOWN DAMAGED. REMOVED AND INSTALLED NEW CARGO TRACK IAW BOEING 737-800 SRM 53-00-53-2R-3.

Part: CARGO TRACK — CORRODED (BS 727D LBL 17) · corrosion level 2 · airframe 73,462 hrs · 29,504 cycles

(LOG 0216365) AFT CARGO FS 727D+6 LBL17 CARGO TRACK CORRODED. REMOVED AND INSTALLED NEW CARGO TRACK IAW BOEING 737-800 SRM 53-00-53-2R-3.

Part: STOP FITTING — GOUGED (FWD PAX DOOR) · airframe 73,462 hrs · 29,504 cycles

(LOG 0214805) FWD ENTRY DOOR FUSELAGE FRAME UPPER AFT DOOR STOP GOUGED. REMOVED FWD ENTRY L1 DOOR STOP AND REPLACED WITH NEW IAW BOEING 737-800 SRM 51-40-02.

Part: INTERCOSTAL — DAMAGED (BS 500I-520) · airframe 73,462 hrs · 29,504 cycles

(LOG 0214832) FWD CARGO FS 500I-520 INTERCOSTAL DAMAGED. REMOVED AND REPLACED INTERCOSTAL FS 500I-520 IAW BOEING 737-800 SRM 51-40-02.

Part: STRINGER — CORRODED (BS 500C-500G) · corrosion level 2 · airframe 73,462 hrs · 29,504 cycles

(LOG 0213623) FWD CARGO FS 500C-500G+10 STR 28L CORROSION AROUND FASTENERS. REPAIRED STR 28L FWD CARGO FS 500C-500G+10 IAW BOEING 737-800 SRM 53-00-03-2R REPAIR 1.

Part: FLOORBEAM — CORRODED (BS 727I) · corrosion level 2 · airframe 73,462 hrs · 29,504 cycles

(LOG 0211976) AFT CARGO FS 727I+6 RBL8 FLOOR BEAM CORRODED. REPAIRED FLOOR BEAM FS 727I+6 RBL8 IAW BOEING 737-800 SRM 53-00-53-2R-2.

Part: FLOORBEAM — CORRODED (BS 727D) · corrosion level 2 · airframe 73,462 hrs · 29,504 cycles

(LOG 0211991) AFT CARGO FS 727D+6 RBL8 FLOOR BEAM CORRODED. REPAIRED FLOOR BEAM FS 727D+6 RBL8 IAW BOEING 737-800 SRM 53-00-53-2R-2.

Part: FLOORBEAM — CORRODED (BS 727I) · corrosion level 2 · airframe 73,462 hrs · 29,504 cycles

(LOG 0211955) AFT CARGO FS 727I+6 LBL3 FLOOR BEAM CORRODED. REPAIRED FLOOR BEAM FS 727I+6 LBL3 IAW BOEING 737-800 SRM 53-00-53-2R-2.

Part: FLOORBEAM — CORRODED (BS 722) · corrosion level 2 · airframe 73,462 hrs · 29,504 cycles

(LOG 0210310) AFT CARGO FS 722 LBL8 FLOOR BEAM CORRODED. REPAIRED AFT CARGO FS 772 LBL8 FLOOR BEAM IAW BOEING 737-800 SRM 53-00-53-2R-2.

Part: FLOORBEAM — CORRODED (BS 727D) · corrosion level 2 · airframe 73,462 hrs · 29,504 cycles

(LOG 0210625) AFT CARGO FS 727D+6 LBL8 FLOOR BEAM CORRODED. REPAIRED FLOOR BEAM FS 727D+6 LBL8 IAW BOEING 737-800 SRM 53-00-53-2R-2.

Part: FLOORBEAM — CORRODED (BS 727D) · corrosion level 2 · airframe 73,462 hrs · 29,504 cycles

(LOG 0210637) AFT CARGO FS 727D+6 LBL3 FLOOR BEAM CORRODED. REPAIRED FLOOR BEAM FS 727D+6 LBL3 IAW BOEING 737-800 SRM 53-00-53-2R-2.

Part: SHEAR WEB — CRACKED (BS 986) · airframe 73,462 hrs · 29,504 cycles

(LOG 0210610) LH AFT SHEAR WEB STA 986 TO APB CRACKED. LOCATED AND DRILLED NEW LH AFT SHEAR WEB STA 986 IAW BOEING 737-800 SRM 51-40-05.

Part: FLOORBEAM — CORRODED (BS 772) · corrosion level 2 · airframe 73,462 hrs · 29,504 cycles

(LOG 0210299) AFT CARGO FS 772 LBL 3 FLOOR BEAM CORRODED. REPAIRED AFT CARGO FS 772 LBL3 FLOOR BEAM IAW BOEING 737-800 SRM 53-00-53-2R-2.

Part: SUPPORT — UNKNOWN (BS 294-312) · corrosion level 2 · airframe 73,462 hrs · 29,504 cycles

(LOG 0210256) FWD FLOOR PANEL BREAKER STA 294-312 RBL 11.5. REMOVED AND REPLACED PANEL BREAKER AT STA 294-312 RBL11.5 IAW BOEING 737-800 SRM 51-40-02.

Part: FLOORBEAM — CORRODED (BS 727D) · corrosion level 2 · airframe 73,462 hrs · 29,504 cycles

(LOG 0210627) AFT CARGO FS 727D+6 RBL3 FLOOR BEAM CORRODED. REPAIRED FLOOR BEAM FS 727D+6 RBL3 IAW BOEING 737-800 SRM 53-00-53-2R-2.

Part: FLOORBEAM — CORRODED (BS 772) · corrosion level 2 · airframe 73,462 hrs · 29,504 cycles

(LOG 0210316) AFT CARGO FS 772 RBL8 FLOOR BEAM CORRODED ON UPPER AND LOWER SURFACE. REPAIRED AFT CARGO FS 772 RBL8 FLOOR BEAM IAW BOEING 737-800 SRM 53-00-53-2R-2.

Part: FLOORBEAM — CORRODED (BS 772) · corrosion level 2 · airframe 73,462 hrs · 29,504 cycles

(LOG 0210279) AFT CARGO STA 772 RBL3 FLOOR BEAM CORRODED. REPAIRED AFT CARGO FS 772 RBL3 FLOOR BEAM IAW BOEING 737-800 SRM 53-00-53-2R-2.

Part: FLOORBEAM — CORRODED (BS 947) · corrosion level 2 · airframe 73,462 hrs · 29,504 cycles

(LOG 0209210) AFT FLOOR BEAM STA 947 LBL 48 TOP CORRODED. REMOVED AND REPLACED T-CHORD STA 947 LBL 48 IAW 53-70-51-2R-5.

Part: SUPPORT — CORRODED (BS 992) · corrosion level 2 · airframe 73,462 hrs · 29,504 cycles

(LOG 0209103) WALL SUPPORT LBL 36-42 STA 992 LOWER FLANGE CORRODED. FABRICATED AND INSTALLED NEW WALL SUPPORT AT STA 992 LBL 36-42 IAW BOEING 737-800 SRM 51-40-05, 51-40-02.

Part: FRAME — CRACKED (BS 480) · airframe 73,462 hrs · 29,504 cycles

(LOG 0207386) RIGHT FUSELAGE FRAME STA 480 IS CRACKED AT I/B & O/B FASTENERS OF THE AC RAIL ATTACH BRACKET AT STR 8. REPAIRED RH FUSELAGE FRAME STA 480 AT AC BIN RAIL BRACKET IAW DELTA TASK CARD 2526-01236-02B.

Part: FRAME — CRACKED (BS 440) · airframe 73,462 hrs · 29,504 cycles

(LOG 0207369) FUSELAGE FRAME STA 440 IS CRACKED AT I/B HOLE FOR BIN ATTACH BRACKET BETWEEN STR 8L & 9L. REPAIRED LH FUSELAGE FRAME STA 440 AT AC BIN RAIL ATTACH BRACKET IAW DELTA TASK CARD 2526-01236-02A.

Part: FRAME — CRACKED (BS 440) · airframe 73,462 hrs · 29,504 cycles

(LOG 0207403) RIGHT FUSELAGE FRAME STA 440 IS CRACKED AT THE I/B, O/B FASTENER AND IN THE RADIUS AT THE AC RAIL ATTACH BRACKET AT STR 8. REPAIRED FUSELAGE FRAME STA 440 AT THE AC RAIL ATTACH BRACKET IAW DELTA TASK CARD 2526-01236-04B.

Part: FRAME — CRACKED (BS 500C) · airframe 73,462 hrs · 29,504 cycles

(LOG 0207478) RIGHT FUSELAGE FRAME STA 500C IS CRACKED AT THE I/B FASTENER OF THE AC RAIL ATTACH BRACKET AT STR 8. REPAIRED FUSELAGE FRAME STA 500C AT AC BIN RAIL ATTACH BRACKET IAW DELTA TASK CARD 2526-01236-04B.

Part: FRAME — CRACKED (BS 907) · airframe 73,462 hrs · 29,504 cycles

(LOG 0207510) LH FUSELAGE FRAME STA 907 IS CRACKED AT I/B HOLE FOR BIN ATTACH BRACKET BETWEEN STR 8L - 9L. REPAIRED LH FUSELAGE FRAME STA 907 AT AC BIN RAIL ATTACH BRACKET IAW DELTA TASK CARD 2526-01236-03A.

Part: FRAME — CRACKED (BS 380) · airframe 73,462 hrs · 29,504 cycles

(LOG 0207293) RIGHT FUSELAGE FRAME STA 380 IS CRACKED AT THE I/B FASTENER OF THE AC RAIL ATTACH BRACKET AT STR 8. REPAIRED RH FUSELAGE FRAME STA 380 AT AC RAIL BRACKET IAW DELTA TASK CARD 2526-01236-02B.

Part: FRAME — CRACKED (BS 400) · airframe 73,462 hrs · 29,504 cycles

(LOG 0207337) RH FUSELAGE FRAME STA 400 IS CRACKED AT THE I/B FASTENER OF THE AC BIN RAIL BRACKET AT STR 8R. REPAIRED RH FUSELAGE FRAME STA 400 AT BIN RAIL ATTACH BRACKET IAW DELTA TASK CARD 2526-01236-02B.

Part: FRAME — CRACKED (BS 380) · airframe 73,462 hrs · 29,504 cycles

(LOG 0207323) FUSELAGE FRAME AT STA 380 IS CRACKED AT I/B AND O/B HOLES FOR BIN RAIL ATTACH BRACKET BETWEEN STA 8L & 9L. REPAIRED LH FUSELAGE FRAME STA 380 AT BIN RAIL BRACKET IAW DELTA TASK CARD 2526-01236-04A.

Part: FRAME — CRACKED (BS 727D) · airframe 73,462 hrs · 29,504 cycles

(LOG 0207506) RIGHT FUSELAGE FRAME STA 727D IS CRACKED AT THE I/B FASTENER OF THE AC RAIL ATTACH BRACKET AT STR 8. REPAIRED RH FUSELAGE FRAME STA 727D AT AC BIN RAIL ATTACH BRACKET IAW DELTA TASK CARD 2526-01236-04B.

Part: FRAME — CRACKED (BS 867) · airframe 73,462 hrs · 29,504 cycles

(LOG 0207502) RIGHT FUSELAGE FRAME STA 867 IS CRACKED AT THE I/B FASTENER OF THE AC RAIL ATTACH BRACKET AT STR 8. REPAIRED RH FUSELAGE FRAME STA 867 AT AC BIN RAIL ATTACH BRACKET IAW DELTA TASK CARD 2526-01236-02B.

Part: FRAME — CRACKED (BS 400) · airframe 73,462 hrs · 29,504 cycles

(LOG 0207353) FUSELAGE FRAME STA 400 IS CRACKED AT I/B HOLE FOR BIN ATTACH BRACKET BETWEEN STA 8L & 9L. REPAIRED LH FUSELAGE FRAME STA 400 AT AC BIN RAIL BRACKET IAW DELTA TASK CARD 2526-01236-02A.

Part: FRAME — CRACKED (BS 727B) · airframe 73,462 hrs · 29,504 cycles

(LOG 0207496) LH FUSELAGE FRAME STA 727B IS CRACKED AT I/B HOLE FOR BIN ATTACH BRACKET BETWEEN STR 8L - 9L. REPAIRED LH FUSELAGE FRAME STA 727B AT AC BIN RAIL ATTACH BRACKET IAW DELTA TASK CARD 2526-01236-02A.

Part: FRAME — CRACKED (BS 500A) · airframe 73,462 hrs · 29,504 cycles

(LOG 0207465) RIGHT FUSELAGE FRAME STA 500A IS CRACKED AT THE I/B FASTENER OF THE AC RAIL ATTACH BRACKET AT STR 8. REPAIRED RH FUSELAGE FRAME STA 500A AT AC BIN RAIL ATTACH BRACKET IAW DELTA TASK CARD 2526-01236-02B.

Part: TRANSITION PANEL — CORRODED (BS 727-727F) · corrosion level 2 · airframe 73,462 hrs · 29,504 cycles

(LOG (0207260) AFT CARGO RH TRANSITION PANEL STA 727+4 - 727F+10 CORRODED. REMOVED AND REPLACED AFT CARGO RH TRANSITION PANEL STA 727+4 -727F+10 IAW BOEING 737-800 SRM 51-40-02.

Part: FRAME — CRACKED (BS 500C) · airframe 73,462 hrs · 29,504 cycles

(LOG 0207454) FUSELAGE FRAME STA 500C IS CRACKED AT I/B HOLE FOR BIN ATTACH BRACKET BETWEEN STR 8L - 9L. REPAIRED LH FUSELAGE FRAME STA 500C AT AC BIN RAIL ATTACH BRACKET IAW DELTA TASK CARD 2526-01236-02A.

Part: FRAME — CRACKED (BS 907) · airframe 73,462 hrs · 29,504 cycles

(LOG 0207515) RIGHT FUSELAGE FRAME STA 907 IS CRACKED AT THE I/B FASTENER OF THE AC RAIL ATTACH BRACKET AT STR 8. REPAIRED RH FUSELAGE FRAME STA 907 AT AC BIN RAIL ATTACH BRACKET IAW DELTA TASK CARD 2526-01236-03B.

Part: FRAME — CRACKED (BS 500A) · airframe 73,462 hrs · 29,504 cycles

(LOG 0207421) LH FUSELAGE FRAME STA 500A IS CRACKED AT I/B HOLE FOR BIN ATTACH BRACKET BETWEEN STR 8L & 9L. REPAIRED LH FUSELAGE FRAME STA 500A AT AC BIN RAIL ATTACH BRACKET IAW DELTA TASK CARD 2526-1236-04A.

Part: FRAME — CRACKED (BS 727B) · airframe 73,462 hrs · 29,504 cycles

(LOG 0207499) RIGHT FUSELAGE FRAME STA 727B IS CRACKED AT THE I/B FASTENER OF AC RAIL ATTACH BRACKET STR 8. REPAIRED RH FUSELAGE FRAME STA 727B AT AC BIN RAIL ATTACH BRACKET IAW DELTA TASK CARD 2526-01236-02B.

Part: TRANSITION PANEL — CORRODED (BS 727F) · corrosion level 2 · airframe 73,462 hrs · 29,504 cycles

(LOG 0207253) AFT CARGO RH TRANSITION FS 727F+10 - 767 CORRODED AND PUNCTURED AT FA 727H. REMOVED AND REPLACED AFT CARGO TRANSITION PANEL STA 727F+10 -767 IAW BOEING 737-800 SRM 51-40-02.

Part: FRAME — CRACKED (BS 500D) · airframe 73,462 hrs · 29,504 cycles

(LOG 0207488) LH FUSELAGE FRAME STA 500D IS CRACKED AT I/B HOLE FOR BIN ATTACH BRACKET BETWEEN STR 8L - 9L. REPAIRED LH FUSELAGE FRAME STA 500D AT AC BIN RAIL ATTACH BRACKET IAW DELTA TASK CARD 2526-01236-02A.

Part: FLOORBEAM — CORRODED (BS 772) · corrosion level 2 · airframe 73,462 hrs · 29,504 cycles

(LOG 0202813) AFT CARGO FS 772 LBL12 FLOOR BEAM CORRODED. REPAIRED AFT CARGO FS 772 LBL12 FLOORBEAM IAW BOEING 737-800 SRM 53-00-53-2R-2.

Part: CHANNEL — CORRODED (R2 DOOR MOP SILL) · corrosion level 2 · airframe 73,462 hrs · 29,504 cycles

(LOG 0197046) RH R2 MOP SILL CHORD TOP IS CORRODED. LOCATED & DRILLED NEW R2 MOP SILL CHORD IAW BOEING 737-800 SRM 51-40-05. INSTALL ACCOMPLISHED ON DELTA NON ROUTINE 9087841 W/O 1021997 2000-0026.

Part: CHANNEL — CORRODED (L2 DOOR MOP SILL) · corrosion level 2 · airframe 73,462 hrs · 29,504 cycles

(LOG 0197040) LH L2 MOP SILL CHORD TOP IS CORRODED. LOCATED & DRILLED NEW L2 MOP SILL CHORD IAW BOEING 737-800 SRM 51-40-05. INSTALL ACCOMPLISHMENT IS ON DELTA NON ROUTINE 9087841 W/O 1021997 2000-0026.

Part: STRAP — CORRODED (BS 1016) · corrosion level 2 · airframe 73,462 hrs · 29,504 cycles

(LOG 0194023) AFT FLOOR WEB STRAP LBL 17.5 BETWEEN 1016 & APB TOP IS CORRODED. REMOVED, FABRICATED NEW STRAP & INSTALLED IAW BOEING 737800 SRM 51-40-05, 51-40-02.

Part: FLOOR SUPPORT — INOPERATIVE (BS 947-967 LBL51) · corrosion level 2 · airframe 73,462 hrs · 29,504 cycles

(LOG 0192658) LH LAV MOUNT FLOOR SUPPORT STA 947-967 LBL 51 TOP CORRODED. LOCATED & DRILLED NEW LH LAV MOUNT FLOOR SUPPORT STA 947-967 LBL 51 IAW BOEING 737-800 SRM 51-40-05.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 72,029 hrs · 28,844 cycles

(LOG 4909470) 4 EMERGENCY EXIT DOOR HANDLE EMERGENCY LIGHTS INOPERATIVE. RELAMPED ALL OVERWING EXIT DOOR HANDLE EMERGENCY LIGHTS AS REQUIRED PER B737 AMM 33-51. OPERATIONAL CHECK NORMAL.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 71,109 hrs · 28,415 cycles

(LOG 2684241) DURING INSPECTION FOUND DURING CRV FOUND FLOOR EMERGENCY ESCAPE PATH LIGHT WITH BROKEN HOLDER. DEF FOR PARTS REQUIREMENTS.

Part: SKIN — DAMAGED (BS 727A-727B) · corrosion level 2 · airframe 70,487 hrs · 28,180 cycles

WHILE PERFORMING A SCRIBE LINE INSPECTION PER A.A. WORK CARD 5330-01197-18 IN ATL, MTC DISCOVERED THREE (3) SCRIBE LINES ON THE FUSELAGE CROWN SKIN BETWEEN BS 727A  727B AND S-1  S-2R. THESE ARE COMMON TO WHERE THE ADF ANTENNA WAS MOUNTED. ADDITIONALLY, SEVEN (7) HOLE LOCATIONS WERE FOUND TO HAVE CORROSION WITHIN THE SAME AREA. MAINTENANCE REPAIRED DAMAGE PER ERA 604661-14AD.

Part: SKIN — DAMAGED (BS 727G-727H) · airframe 70,487 hrs · 28,180 cycles

WHILE IN ATL FOR THE VIASAT INSTALLATION (WC 2330-01337-42), MTC FOUND EXISTING DOUBLERS THAT DIFFER FROM THE EXPECTED SIZE. THE 2 OUTBOARD DOUBLERS ON THE IDTV INSTALL EXTEND 2 ROWS AND 2 COLUMNS PAST THE TYPICAL INSTALLATION. THEY ARE LOCATED AT BS 727G TO 727H AND JUST INBOARD OF S-3R AND S-3L. MAINTENANCE REPAIRED DAMAGE PER ERA 604700-14AD.

Part: DOUBLER — ABNORMAL · airframe 70,539 hrs · 28,223 cycles

(LOG 2568726) DURING VIASAT WIFI INSTALL, ATYPICAL DOUBLERS FOUND PAST DWG LIMITS. DEMOD DOUBLER MODIFIED TO BE WIDER. ASSOCIATED ER/A 00-604661 ADDED FOR AC 3717.

Part: SUPPORT — CORRODED (ACCESS PANEL) · airframe 66,921 hrs · 26,520 cycles

(LOG 1889292) DURING INSPECTION FOUND FRITTING CORROSION AND ELONGATED HOLES ON AFT PANEL SUPPORT STRUCTURE OF ACCESS PANEL 193D. PANEL SUPPORT STRUCTURE OF ACCESS PANEL 93D WAS REPAIRED PER ETI-37-21-439 REVISION 2 AND ER/A 592996-14.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 66,921 hrs · 26,520 cycles

(LOG 1882530) DURING C-CHECK INSPECTIONS THREE ELONGATED HOLES WERE FOUND BEYOND THE ALLOWABLE LIMITS COMMON TO FUSELAGE SKIN, STRINGER 2-2L AND STRINGER S-2R. MAINTENANCE REPAIRED DAMAGE PER ERA 592935-14.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 65,502 hrs · 25,806 cycles

DURING INSPECTION FOUND EMERGENCY LIGHTS INOPERATIVE IN ZONES M1675, M1676, M1670, M1671, M1672. R/R BATTERY PACKS FOR ZONES M1675, M1676 PER B737 AMM 33-51. OPS CHK NORMAL.

Part: SIGN — MISSING (CABIN) · airframe 64,135 hrs · 25,246 cycles

(LOG 5980263) DURING INSPECTION FOUND EMERGENCY EXIT SIGN ABOVE DOOR 1R MISSING. REPLACED LENS PER B737 AMM 33-51.

Part: FRAME — DENTED (BS 727C) · airframe 63,417 hrs · 24,920 cycles

DURING HCK AT QRO, A DENT WAS FOUND ON FRAME ASSY P/N 146A1202-4 UPPER CHORD (M/F 0.050 INCH THICK, 2024-T3) AT BS 727C BETWEEN STRINGERS 23L-24L. MAINTENANCE REPAIRED DAMAGE PER ERA 565335-14.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 61,958 hrs · 24,315 cycles

DURING INSPECTION FOUND 1L F/A EMERGENCY FLASHLIGHT NOT FLASHING. REPLACED FLASHLIGHT AND BATTERY PER B737 AMM 25-64.

Part: UNKNOWN — HANDLER ERROR (UNKNOWN) · airframe 72,918 hrs · 29,249 cycles

(LOG 0399444) FUSELAGE SKIN DAMAGED BY GROUND EQUIPMENT BETWEEN STATION 360 AND 380 ABOVE STRINGER 18L. DAMAGE REPAIRED PER ERA 385262-14.

Part: SIGN — BROKEN (CABIN) · airframe 61,779 hrs · 24,246 cycles

DURING INSPECTION FOUND L1 DOOR EMER EXIT SIGN BROKEN. MAINTENANCE REPLACED EMER EXIT SIGN AND BASE.

Part: SKIN — DENTED (FUSELAGE) · airframe 61,612 hrs · 24,171 cycles

(LOG 0890513) WHILE IN QRO FOR A HEAVY MAINTENANCE VISIT, AND DURING THE 2KU WIFI MODIFICATION, THE FWD ATG4 ANTENNA WAS BEING REMOVED MTC REPORTED THE CLOSE PROXIMITY OF AN EXISTING REPAIR DOUBLER/TRIPLER. UPON FURTHER EVALUATION OF THE AREA MTC REPORTED A DENT MEASURING 6.50 BY 3.50 WITH A MAXIMUM DEPTH OF 0.060, A GOUGE THAT WAS BLENDED MEASURING 4.375 BY 0.750 WITH A MAXIMUM BLEND DEPTH OF 0.003 AND SEVEN (QTY: 7) OVERSIZED HOLES. MAINTENANCE REPAIRED THE DAMAGE PER ERA 564877-14.

Part: WIRE — SHORTED (L1 WINDOW) · airframe 61,311 hrs · 24,079 cycles

(LOG 4865885) SHIP 3717 - SMOKE AFTER LANDING, THE CAPTAIN NOTICED A SMALL SPARK AND LITTLE SMOKE NEAR L1 WINDOW. CLEARED VERY RAPIDLY. CORRECTIVE ACTION: MAINTENANCE FOUND WIRE TO L1 WINDOW SHORTED TO GLARE SHIELD SUPPORT BRACKET. REPAIRED WIRE PER B737 SSM AND SWPM AND REPLACED GLARE SHIELD SUPPORT BRACKET PER B737 AMM. REPLACED WHCU PRECAUTIONARY. OPS CHECK GOOD, AIRCRAFT RETURNED TO SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 61,211 hrs · 24,039 cycles

DURING TESTING FOUND ROWS 1 TO 40 EMERGENCY ESCAPE SEAT PATH LIGHTING NOT WORKING. R&R FWD POWER SUPPLY BATTERY PACK PER AMM 33-51. CABIN SEAT 1 - 4 ESCAPE PATH LIGHTS CK GOOD.

Part: LENS — UNSECURE (CABIN) · airframe 60,736 hrs · 23,817 cycles

EMERGENCY EXIT COVER DIFFUSER LENS DAMAGED OR MISSING. SECURED COVER. OK FOR SERVICE.

Part: SKIN — DAMAGED (BS 500B-500C) · airframe 58,480 hrs · 22,995 cycles

PROTUBERANCE ON FUSELAGE SKIN BETWEEN BS 500B AND 500C, BTW STRINGERS 21 - 22R. THE SKIN WAS REPAIRED IAW ETI-37-18-360, REV 4, AND ER/A 564756-14AD, REV ORG.

Part: SKIN — DAMAGED (BS 500E) · airframe 58,480 hrs · 22,995 cycles

PROTUBERANCE ON EXTERNAL FUSELAGE SKIN AT BS 500E+7, BETWEEN STRINGER 27L AND 27R. THE SKIN WAS REPAIRED IAW PRI 564877-14, REV 5, AND ER/A 564877, REV ORIG.

Part: FRAME — DENTED (BS 500C) · airframe 58,480 hrs · 22,995 cycles

DENTED FRAME BS 500C, BETWEEN STRINGERS 23 & 24L IN THE FWD CARGO BAY. THE FRAME WAS REPAIRED IAW ETI-37-18-316, REV ORG, AND ER/A 565336-14, REV ORG.

Part: FRAME — DENTED (BS 727I) · airframe 58,480 hrs · 22,995 cycles

DENTED FRAME BS 727I, STRINGER 24L IN THE AFT CARGO BAY. THE FRAME WAS REPAIRED IAW ETI-37-18-324, REV 2, AND ER/A 565388-14, REV ORIG.

Part: FRAME — DENTED (BS 727H) · airframe 58,480 hrs · 22,995 cycles

DENTED FRAME BS 727H, STRINGER 23R IN THE AFT CARGO BAY. THE FRAME WAS REPAIRED IAW ETI-37-18-323, REV 2, AND ER/A 565392-14, REV ORIG.

Part: FRAME — DENTED (BS 727H) · airframe 58,480 hrs · 22,995 cycles

DENTED FRAME BS 727H BETWEEN STRINGERS 24 & 25L IN THE AFT CARGO BAY. THE FRAME WAS REPAIRED IAW ETI 37-18-323, REV 2, AND ER/A 565392-14, REV ORIG.

Part: FRAME — DENTED (BS 727J) · airframe 58,479 hrs · 22,994 cycles

DENTED FRAME, BS 727J, STRINGER 24L. THE FRAME WAS REAIRED IAW ETI-37-18-325, REV 2, AND ER/A 565380-14, REV ORG.

Part: FRAME — DENTED (BS 827) · airframe 58,480 hrs · 22,995 cycles

DENTED FRAME BS 827, BETWEEN STRINGERS 22 - 23L IN THE AFT CARGO BAY. THE FRAME WAS REPAIRED IAW ETI-37-18-327, REV 3, AND ER/A 565386-14, REV ORG.

Part: FRAME — DENTED (BS 500E) · airframe 58,479 hrs · 22,994 cycles

DENTED FRAME, BS 500E, STRINGER 24L. THE FRAME WAS REPAIRED IAW ETI-37-18-317, REV 4, AND ER/A 565387-14, REV ORG.

Part: FRAME — DENTED (BS 727J) · airframe 58,480 hrs · 22,995 cycles

DENTED FRAME BS 727J, STRINGER 25R IN THE AFT CARGO BAY. THE FRAME WAS REPAIRED IAW ETI-37-18-325, REV 2, AND ER/A 565380-14, REV ORG.

Part: FRAME — DENTED (BS 727F) · airframe 58,480 hrs · 22,995 cycles

DENT FOUND ON THE FRAME BS 727F, STRINGER 25L IN THE AFT CARGO BAY. THE FRAME WAS REPAIRED IAW ETI-37-18-321, REV 1, AND ER/A 565341-14, REV ORG.

Part: FRAME — DENTED (BS 500F) · airframe 58,479 hrs · 22,994 cycles

DENTED FRAME, BS 500F, STRINGER 24L. THE FRAME WAS REPAIRED IAW ETI 37-18-318, REV 4, AND ER/A 565382-14, REV ORG.

Part: FRAME — DENTED (BS 727F) · airframe 58,480 hrs · 22,995 cycles

DENTED FRAME BS 727F, STRINGER 23R IN THE AFT CARGO BAY. THE FRAME WAS REPAIRED IAW ETI-37-18-321, REV 1, AND ER/A 565341-14, REV ORG.

Part: FRAME — DENTED (BS 500) · airframe 58,589 hrs · 23,031 cycles

DURING AN H CHECK, A DENT WAS FOUND ON THE FRAME AT BS 500 BETWEEN STRINGERS 25 - 26L. REPAIRED THE FRAME IAW ERA 565385-14.

Part: FRAME — DENTED (BS 727G) · airframe 58,479 hrs · 22,994 cycles

DENTED FRAME, BS 727G, STRINGER 24L. THE FRAME WAS REPAIRED IAW ETI-37-18-322, REV 2, AND ER/A 565383-14, REV O.

Part: FRAME — DENTED (BS 500) · airframe 58,480 hrs · 22,995 cycles

DENTED FRAME BS 500, BETWEEN STRINGERS 24 - 25L IN THE FWD CARGO BAY. THE FRAME WAS REPAIRED IAW ETI-37-18-311, REV 3, AND ER/A 565385-14, REV ORG.

Part: FRAME — DENTED (FUSELAGE) · airframe 58,580 hrs · 23,027 cycles

DURING HCK AT QRO, TWO DENTS WERE FOUND ON FRAME ASSY P/N 146A1244-2 UPPER CHORD AT BS 727J, ONE OVER STRINGER 24L, AND THE OTHER ONE BETWEEN STRINGER 25R & 26R. MAINTENANCE REPAIRED PER 565380-14.

Part: FRAME — DENTED (FUSELAGE) · airframe 58,580 hrs · 23,027 cycles

DURING HCK AT QRO, A DENT WAS FOUND ON FRAME ASSY P/N 143A1231-2 UPPER CHORD AT STA 500F ON STRINGER 25L. MAINTENANCE REPAIRED PER ERA 565382-14.

Part: PLATE — CORRODED (BS 500-500B) · corrosion level 2 · airframe 58,479 hrs · 22,994 cycles

CORRODED ZEE SIDE PLATE, BS 500-500A AND 500A-500B. REPLACED IAW SRM 53-00-53, REPAIR 6. SRM 51-40-05, AND SRM 51-40-08.

Part: FRAME — DENTED (BS 500B) · airframe 58,479 hrs · 22,994 cycles

DENTED FRAME BS 500B, STRINGER 24L. REPAIRED IAW ER/A 565364-14, REV ORIGINAL, AND ETI 37-18-315, REV 1.

Part: FRAME — DENTED (BS 727B) · airframe 58,479 hrs · 22,994 cycles

DENTED FRAME BS 727B, STRINGER 23L IN THE AFT CARGO BAY. THE FRAME WAS REPAIRED IAW ETI-37-18-319 REV 1, AND ER/A 565372-14, REV ORIG.

Part: INLET — CRACKED (RT ENGINE) · airframe 58,479 hrs · 22,994 cycles

CRACK ON NOSE COWL INLET LIP, UPPER AREA, INNER SURFACE, BETWEEN 11 AND 12 HRS ON THE RT ENGINE. REPAIRED IAW SRM 54-10-02, REPAIR 15.

Part: FRAME — DENTED (BS 727C) · airframe 58,479 hrs · 22,994 cycles

DENTED FRAME BS 727C, STRINGER 23L IN THE AFT CARGO BAY. THE FRAME WAS REPAIRED IAW ETI-37-18-320, REV 1, AND ER/A 565335-14, REV ORIG.

Part: FRAME — DENTED (BS 500A) · airframe 58,479 hrs · 22,994 cycles

DENTED FRAME BS 500A, STRINGER 24L. THE FRAME WAS REPAIRED IAW ER/A 565339-14, REV ORIG, AND ETI-37-18-314, REV 2.

Part: FRAME — CRACKED (BS 727B) · airframe 63,417 hrs · 24,920 cycles

DURING HCK AT QRO, A DENT WAS FOUND ON FRAME ASSY P/N 146A1201-4 UPPER CHORD (M/F 0.056 INCH THICK, 2024-T3) AT STA 727B BETWEEN STRINGERS 22LH AND 23LH. MAINTENANCE REPAIRED DAMAGE PER ERA 565372-14.

Part: FRAME — DENTED (BS 500C) · airframe 63,417 hrs · 24,920 cycles

DURING HCK AT QRO, A DENT WAS FOUND ON FRAME ASSY P/N 143A1224-21 UPPER CHORD AT STA 500C BETWEEN STRINGERS 24LH AND 25LH. MAINTENANCE REPAIRED DAMAGE PER ERA 565336-14.

Part: FLOORBEAM — CORRODED (BS 986) · corrosion level 2 · airframe 58,479 hrs · 22,994 cycles

CORROSION ON THE FLOORBEAM BS 986, LBL 43. THE FLOORBEAM WAS REPAIRED IAW ETI 37-18-303, REV 3, AND ER/A 565237-14, REV ORIG.

Part: FLOORBEAM — CORRODED (BS 986) · corrosion level 2 · airframe 58,479 hrs · 22,994 cycles

CORROSION ON PREVIOUS REPAIR ON THE FLOORBEAM BS 986, RBL 43. THE FLOORBEAM WAS REPAIRED IAW ETI-37-18-303, REV 3, AND ER/A 565237-14, REV ORIG.

Part: SKIN PANEL — DENTED (FUSELAGE) · airframe 58,479 hrs · 22,994 cycles

DENT DAMAGE REMOVED AND FWD ATG4 DE-MOD DOUBLER COMBINED WITH A REPAIR IN PROXIMITY.

Part: PLATE — CORRODED (BS 727-907) · corrosion level 2 · airframe 58,479 hrs · 22,994 cycles

CORROSION FOUND ON THE LT SIDEPLATE FROM BS 727 TO 907 IN THE AFT CARGO BAY. THE SIDEPLATE WAS REPLACED IAW SRM 53-00-53, AND SRM 51-10-02.

Part: PLATE — CORRODED (BS 727-947) · corrosion level 2 · airframe 58,479 hrs · 22,994 cycles

CORROSION ON THE RT SIDEPLATE FROM BS 727 TO 947 IN THE AFT CARGO COMPARTMENT. THE PLATE WAS REPLACED IAW SRM 51-10-02, AND SRM 53-00-53.

Part: FRAME — CORRODED (BS 663.75) · corrosion level 2 · airframe 58,479 hrs · 22,994 cycles

EXFOLIATION FOUND ON FRAME BS 663.75, STRINGERS 4L & 5L. REPAIRED THE FRAME IAW ETI-37-18-300, REV 1, AND ERA 565128-14, REV ORIGINAL.

Part: DOUBLER — CRACKED (SKIN) · airframe 58,479 hrs · 22,994 cycles

DURING INSPECTION, FOUND CRACKED DOUBLER CUTOUT OF EXTERNAL POWER RECEPTABLE FWD EDGE. MAINTENANCE REPAIRED IAW SRM. 53-10-15 FIG.202 REPAIR 5 AND 51-40-02.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,479 hrs · 22,994 cycles

DURING INSPECTION FOUND CORROSION ON FLOORBEAM STATION Y= 947 LBL 53 AND BTW RBL 50 TO 53 AT CABIN PAX. MAINTENANCE REPAIRED PER SRM 53-70-51 REPAIR 5, ALTERNATIVE 2.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,479 hrs · 22,994 cycles

DURING INSPECTION FOUND CORROSION ON INTERCOSTAL BTW STATION Y=947 AND Y= 967 LBL 53 AT CABIN PAX. MAINTENANCE INTERCOSTAL WAS REPLACED PER SRM 51-40-02.

Part: WEB — CRACKED (LT WING) · airframe 58,479 hrs · 22,994 cycles

DURING INSPECTION, FOUND ONE CRACK ON WEB AT REAR SPAR UPPER SECTION LBL 45. TWO CRACKS ON WEB RBL 37. MAINTENANCE REPAIRED THE WEB IAW SRM 57-10-10 REP.3

Part: SKIN — DENTED (NR 8 SPOILER) · airframe 58,479 hrs · 22,994 cycles

DURING INSPECTION, FOUND SEVERAL DENTS ON THE RT WING SPOILERS NR 8 UPPER SURFACE. MAINTENANCE REPAIRED THE SPOILER IAW SRM 57-70-01, REP 1, SRM 51-70-10, REP 4, AND SRM 51-70-10 REPAIR GENERAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 53,450 hrs · 21,234 cycles

DURING INSPECTION FOUND OVERHEAD AISLE EMERGENCY LIGHT AT 10DEF INOPERATIVE. MAINTENANCE DISCONNECTED D12060 FOUND LOOSE. RECONNECTED, LIGHT WORKING GOOD. OK FOR SERVICE.

Part: BAFFLE — CORRODED (FUSELAGE) · airframe 54,327 hrs · 21,549 cycles

DURING INSPECTION FOUND FORWARD PIT RIGHT SIDE BAFFLE CORRODED BETWEEN STATION 500F TO 500G. MAINTENANCE REMOVED AND REPLACED WITH NEW BAFFLE IAW DRAWING 143A7505 REV B, AND SRM 51-40-02.

Part: BAFFLE — CORRODED (FUSELAGE) · airframe 54,327 hrs · 21,549 cycles

DURING INSPECTION FOUND FORWARD PIT RIGHT SIDE BAFFLE CORRODED BETWEEN STATION 500G TO 500H. MAINTENANCE REMOVED AND REPLACED WITH NEW BAFFLE IAW DRAWING 143A7505 REV B, AND SRM 51-40-02.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 54,327 hrs · 21,549 cycles

DURING INSPECTION FOUND FORWARD CARGO RIGHT HAND TRANSITION ANGLE HAS CORROSION ON UPPER SURFACE FROM STAT 500B-520. MAINTENANCE REMOVED AND REPLACED IAW SRM 53-00-53, DWG 143A7500, AND AMM 51-21-91.

Part: BAFFLE — CORRODED (FUSELAGE) · airframe 54,327 hrs · 21,549 cycles

DURING INSPECTION FOUND FORWARD PIT RIGHT SIDE BAFFLE CORRODED BETWEEN STATION 500H TO 500I. MAINTENANCE REMOVED AND REPLACED WITH NEW BAFFLE IAW DRAWING 143A7505 REV B, AND SRM 51-40-02.

Part: BAFFLE — CORRODED (FUSELAGE) · airframe 54,327 hrs · 21,549 cycles

DURING INSPECTION FOUND FORWARD PIT RIGHT SIDE BAFFLE CORRODED BETWEEN STATION 500E TO 500F. MAINTENANCE REMOVED AND REPLACED WITH NEW BAFFLE IAW DRAWING 143A7505 REV B, AND SRM 51-40-02.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 54,327 hrs · 21,549 cycles

DURING INSPECTION FOUND FORWARD PIT SIDE PLATE Z ANGLE CORRODED FROM STATION 500F TO 500I. MAINTENANCE REMOVED AND REPLACED IAW SRM 53-00-53 REPAIR 6 AND DWG 143A7500.

Part: BAFFLE — CORRODED (FUSELAGE) · airframe 54,327 hrs · 21,549 cycles

DURING INSPECTION FOUND FORWARD PIT RIGHT SIDE BAFFLE CORRODED BETWEEN STATION 500D TO 500E. MAINTENANCE REMOVED AND REPLACED WITH NEW BAFFLE IAW DRAWING 143A7505 REV B, AND SRM 51-40-02.

Part: ANGLE — CORRODED (BS 767) · airframe 50,601 hrs · 20,314 cycles

DURING INSPECTION, FOUND AFT CARGO TRANSITION ANGLE HAS CORROSION ON UPPER SURFACE AT BS 767 LT SIDE. MAINTENANCE R & R DAMAGED SECTION ON LT SIDE BS 727F TO BS 777 IAW SRM 53-00-53, REPAIR 5.

Part: THRESHOLD — CORRODED (CARGO BAY) · airframe 50,601 hrs · 20,314 cycles

DURING INSPECTION AFT CARGO DOOR THRESHOLD HAS CORROSION ON WEB UNDER CENTER SCUFF PLATE. MAINTENANCE REMOVED AND INSTALLED NEW WEB IAW DWG 146A8340, REV A.

Part: DOOR FRAME — DAMAGED (SERVICE DOOR) · airframe 50,601 hrs · 20,314 cycles

DURING INSPECTION CORROSION WAS FOUND ON THE UPPER SURFACE OF THE R2 DOORWAY, LOWER MAIN SILL INNNER CHORD AT RBL 47 BETWEEN BS 967 AND 987. MAINTENANCE REPAIRED CORRISION IAW ERA 537923-14.

Part: CARGO TRACK — CORRODED (BS 787-827) · airframe 50,601 hrs · 20,314 cycles

DURING INSPECTION FOUND AFT CARGO FLOOR SUPPORT TIE DOWN TRACK CORRODED AT BS 787-827, RBL 13.8. MAINTENANCE R & R TRACK IAW SRM 53-00-53, SRM 53-40-02, DWG 146A7500.

Part: FLOOR SUPPORT — CORRODED (BS 967-687) · airframe 50,602 hrs · 20,315 cycles

DURING INSPECTION, FOUND AFT CARGO EQUIPMENT BAY, BS 967 TO BS 987, RBL 47", CABIN FLOOR STRUCTURE HAS CORROSION, AS SEEN FROM BELOW THRU OUTFLOW VALVE OPENING. MAINTENANCE REPAIRED IAW ERA 537923-14.

Part: FLOORBEAM — CORRODED (BS 987) · airframe 50,601 hrs · 20,314 cycles

DURING INSPECTION FOUND AFT CARGO EQUIPMENT BAY, BS 987, RBL 40" CABIN FLOORBEAM HAS CORROSION. MAINTENANCE REPAIRED IAW ERA 464736.

Part: SEAT TRACK — GOUGED (BS 520) · airframe 50,601 hrs · 20,314 cycles

DURING INSPECTION FOUND SEAT TRACK GOUGED AT BS 520, RBL 45. MAINTENANCE FABRICATED AND INSTALLED REPAIR SEAT TRACK PARTS IAW SRM 53-00-52, REPAIR 4.

Part: SEAT TRACK — GOUGED (BS 520) · airframe 50,601 hrs · 20,314 cycles

DURING INSPECTION FOUND SEAT TRACK GOUGED AT BS 520, RBL 24. MAINTENANCE FABRICATED AND INSTALLED REPAIR SEAT TRACK PARTS IAW SRM 53-00-52, REPAIR 4.

Part: SEAT TRACK — GOUGED (BS 520) · airframe 50,601 hrs · 20,314 cycles

DURING INSPECTION, FOUND SEAT TRACK GOUGED AT BS 520, LBL 24. MAINTENANCE FABRICATED AND INSTALLED REPAIR SEAT TRACK PARTS IAW SRM 53-00-52, REPAIR 4.

Part: SEAT TRACK — GOUGED (BS 520) · airframe 50,601 hrs · 20,314 cycles

DURING INSPECTION, FOUND SEAT TRACK GOUGED AT BS 520, LBL 45. MAINTENANCE FABRICATED AND INSTALLED REPAIR SEAT TRACK PARTS IAW SRM 53-00-52, REPAIR 4.

Part: FIRE WARNING — ACTIVATED (CARGO BAY) · airframe 50,601 hrs · 20,314 cycles

DURING TAXI, WHILE CROSSING THE HOLD SHORT FOR TAKEOFF, THE FORWARD CARGO FIRE LIGHT ILLUMINATED. CREW PERFORMED QRH CARGO FIRE PROCEDURES DISCHARGING CARGO FIRE BOTTLES WITH INDICATION REMAINING. CREW PERFORMED QRH EVACUATION OF ACFT. ALL SLIDES DEPLOYED, ACFT WAS CLEARED. MAINTENANCE LATER CHANGED FIRE BOTTLES AND SLIDES AND INSPECTED ACFT.

Part: POWER SUPPLY — INOPERATIVE · airframe 48,342 hrs · 19,516 cycles

DURING INSPECTION FOUND EMERGENCY LIGHT AT LT WING DOOR INOPERATIVE. MAINTENANCE REPLACED POWER SUPPLY M1670 IAW AMM 737 33-51-06. OPS CHECK OK.

Part: ANGLE — CRACKED (BS 500C & 500F) · airframe 47,163 hrs · 19,127 cycles

DURING INSPECTION FOUND FOUND TWO ANGLES CRACKED, ONE AT WEB ABOVE STRINGER 26R BS 500C. AND THE OTHER AT WEB ABOVE STRINGER 26R BS 500F. MAINTENANCE REPAIRD IAW SRM 51-70.

Part: WEB — DAMAGED (BS 500C-500D) · airframe 47,163 hrs · 19,127 cycles

WEB ABOVE STRINGER 26R BS 500C - 500D DAMAGED. MAINTENANCE REMOVED DAMAGE AND INSTALLED DOUBLER IAW SRM 51-70-11.

Part: STRINGER — DAMAGED (BS 500C-500D) · airframe 47,163 hrs · 19,127 cycles

FOUND DAMAGE AT STRINGER 26R BETWEEN BS 500C - 500D. MAINTENANCE FABRICATED DOUBLER IAW SRM 53-00-03, REPAIR 1. INSTALLED THE DOUBLER IAW SRM 53-00-03, REPAIR 1.

Part: STRINGER — DENTED (BS 500B-500C) · airframe 47,163 hrs · 19,127 cycles

FOUND STRINGER S25R DENTED BETWEEN BS 500B - 500C. MAINTENANCE REMOVED DAMAGE, AND PERFORMED HFEC INSPECTION IAW NDT MANUAL 51-00-00, FIG 23. NO DEFECTS NOTED. FABRICATED DOUBLER IAW SRM 53-00-03 REPAIR 1. INSTALLED DOUBLERS.

Part: SKIN — DAMAGED (BS 917) · airframe 46,478 hrs · 18,885 cycles

DURING INSPECTION, FOUND CORROSION AND TWO CRACKS ON THE FUSELAGE SKIN AT THE LOWER EDGE OF THE AFT LAV VENT. THE VENT IS LOCATED NEAR BS 917 BETWEEN STRINGERS S-21L AND S-22L. MAINTENANCE REPAIRED IAW ERA 528276-14.

Part: FLOOR SUPPORT — CRACKED (BS 727B) · airframe 43,681 hrs · 17,912 cycles

DURING INSPECTION, FOUND CRACK INDICATIONS IN NINE OF THE SIXTEEN FASTENER HOLES COMMON TO THE LONGITUDINAL FLOOR SUPPORT SPLICE STRAP AT BS 727B. REPAIRED IAW ERA 520074-14 REV ORIGINAL.

Part: WIRE — PULLED (EMERGENCY LIGHT) · airframe 43,617 hrs · 17,883 cycles

DURING INSPECTION, FOUND EMERGENCY LIGHT 24DEF INOPERATIVE. MAINTENANCE FOUND WIRE PULLED FROM CONNECTOR AT SIDEWALL RETERMINATED. OPS CHECK OK.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHT) · airframe 40,835 hrs · 16,830 cycles

DURING TESTING, THE EMERGENCY LIGHT BATTERY PACKS FAILED CAPACITY TEST. MX R & R BATTERY PACKS M1670, M1671, M1694, M1695. OPS TEST OK IAW AMM 33-51-06/201.

Part: VALVE — OUT OF TOLERANCE (LEFT) · airframe 27,253 hrs · 11,548 cycles

LEFT OUTBD TIRE BURST AFTER LANDING. TROUBLESHOOT ANTI-SKID SYSTEM FOUND LEFT OUTBD ANTI-SKID NORMAL VALVE RESISTANCE OUT OF RANGE PER FIM 32-42-00-810-804. BITE A/S BOX FOUND VLV1 WITH SP-CO-VI. T/S PER FIM 32-42-00-810-804 FOUND NR 1 NORMAL A/S VALVE RESIS OUT OF RANGE. REPLACED NR 1 NORMAL A/S VALVE PER AMM. CKS GOOD LEAK CHECK GOOD

Part: BULKHEAD — GOUGED (BS 1016 LBL 20) · airframe 22,531 hrs · 9,806 cycles

THE AFT PRESSURE BULKHEAD WEB SUSTAINED TOOLING DAMAGE. THE DAMAGED SECTION OF WEB WAS CUT OUT AND A DOUBLER WAS INSTALLED.

Part: ROD — BROKEN (LT NLG DOOR) · airframe 16,998 hrs · 7,642 cycles

DURING ROTATION LOUD POP NEAR COCKPIT. GEAR CAME UP NORMALLY WITH LIGHTS OUT. GEAR LOWERED, GEAR NORMALLY ALL GREEN. RETURNED TO TPA. MTC FOUND L NLG DOOR PUSH ROD BROKEN. REPLACED SAME PER MM.

Part: SENSOR — FAILED (RIGHT GEAR WELL) · airframe 6,254 hrs · 2,942 cycles

AIR RETURN TO SLC. AFTER LIFTOFF GOT PSEU LIGHT, AUTO THROTTLES DISENGAGED, TCAS INOP, FEEL DIFF PRESSURE, AND TAKEOFF WARNING HORN WHEN THROTTLES ADVANCED. REPEAT WRITE-UP OF PREVIOUS DAYS AIR RETURN. PSEU HAS A HARD FAULT OF THE SPOILERS GROUND INTERLOCK SENSOR S1050. FAULT CODE 31-51001 GSBV CL FAULT. SUSPECT PROX SENSOR S1050. CA RPLD SENSOR, OP CKS NML