N399DA

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 73,326 hrs · 34,082 cycles

EMERGENCY LIGHTS ROW 11-15 NOT ILLUMINATING. R & R BATTERY PACK (M1676) REF B737 AMM 33-51. OPS CHK GOOD.

Part: SHUTOFF VALVE — BYPASSING (ZONE 100) · airframe 73,299 hrs · 34,064 cycles

DECLARED EMERGENCY AND DIVERTED TO ONT DUE TO FLT CONTROL 'B' LOW PRESSURE LIGHT ILLUMINATED. FOUND SYSTEM 'B' FLIGHT CONTROL SHUTOFF VALVE BYPASSING. REPLACED SAME. OPS CHECK GOOD.

Part: CASE — BIRD INGESTION (ENGINE FAN) · airframe 72,976 hrs · 33,885 cycles

RETURNED TO MIA DUE TO RIGHT ENGINE BIRD STRIKE AFTER TAKEOFF. MAINTENANCE FOUND MULTIPLE FAN BLADES AND FAN CASE DAMAGED. FAN CASE DAMAGE EXCEEDS B737AMM LIMIT. ENGINE CHANGE ON LOG PAGE 1199194.

Part: SEAT — LOOSE (ZONE 200) · airframe 71,154 hrs · 33,064 cycles

(LOG 6912038) DURING CHECK, FOUND SEAT 15DEF ROW SEAT ASSY LOOSE FROM TRACK. TIGHTENED LOOSE SEAT ASSY HARDWARE PER B737 AMM 25-22. OK FOR SVC.

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 70,061 hrs · 32,605 cycles

(LOG 6101623) LT AFT VERTICAL EMERGENCY EXIT DOOR SIGN LIGHT INOP. INSTALLED AFT LEFT EXITS DOOR LIGHT ASSY PER B737 AMM 33-51.OPS CHK GOOD.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 69,442 hrs · 32,354 cycles

(LOG 0438541) CORROSION OUT OF LIMITS ON FLOOR SUPPORTS BTW STA 727A LBL 13.84 AND RBL 12.5 AND STA 727I RBL 8.1 AND 3.0. FLOOR SUPPORT STA 727A LBL 13.84 AND RBL 12.5 WERE REPAIRED PER B737-800 SRM 53-00-53-2R PROCEDURE 3 REPAIR 3 AND FLOOR SUPPORT ON STA. 727I RBL 3 AND RBL 8.1 WERE REPAIRED PER B737-800 SRM 53-00-53-2R.

Part: TRIM PANEL — CORRODED (GALLEY ACCESS) · corrosion level 2 · airframe 69,442 hrs · 32,354 cycles

(LOG 0438104) CORROSION ON TRIM UNDER OF THE DOOR ACCESS A423 AT GALLEY 4. TRIM UNDER OF THE DOOR ACCESS A423 AND A417 AT GALLEY 4 WERE FABRICATED AND INSTALLED PER ER/A NO. 619100-14.

Part: SKIN — GOUGED (ZONE 200) · airframe 69,442 hrs · 32,354 cycles

(LOG 0437697) GOUGE SKIN FROM STA. 727D TO 727E AND BTW S-1L TO S-2L AT INTERNAL FUSELAGE SKIN.FUSELAGE SKIN FROM STA. 727D TO 727E AND BTW S-1L TO S-2L WAS REPAIRED PER ER/A 619002-14AD REV. A SECTION I PERMANENT REPAIR AND FASTENER ON UPPER SKIN FROM STA. 727C TO 727D WERE REPLACED PER B737-800 SRM 51-40-02-0G.

Part: SKIN — GOUGED (ZONE 200) · airframe 69,442 hrs · 32,354 cycles

(LOG 0436172) WHILE ACCOMPLISHING INSPECTION WORK CARD 2330-2048 FOR THE AREA COMMON TO THE DOUBLERS INSTALLED BY THE VIASAT IFE/C RADOME, THE SKIN WAS FOUND GOUGED AT THE FWD TWO ROWS OF THE DOUBLER INSTALLED BETWEEN FS727D AND FS727E AND STRINGERS S-1 AND S-2L. REPAIRED DAMAGE PER ERA 619002-14.

Part: PLATE — CORRODED (AFT CARGO) · corrosion level 2 · airframe 69,442 hrs · 32,354 cycles

(LOG 0432574) CORROSION ON SIDE PLATE LH/RH SIDE STA 727 TO 887 AT AFT CARGO COMPARTMENT. SIDE PLATE LH AND RH SIDE BTW STA 727 TO 887 AT AFT CARGO COMPARTMENT WERE REPLACED PER B737-800 SRM 51-40-02-0G.

Part: WEB — CORRODED (AFT CARGO) · corrosion level 2 · airframe 69,442 hrs · 32,354 cycles

(LOG 0429660) CORROSION ON WEB AT AREA TO INSTALL SCUFF PLATE OF AFT CARGO COMPARTMENT. SCUFF PLATE OF AFT CARGO COMPARTMENT WAS REPLACED PER B737-800 SRM 51-40-02-0G.

Part: FLOORBEAM — CORRODED (BS 986 R-LBL45) · corrosion level 2 · airframe 69,442 hrs · 32,354 cycles

(LOG 0427216) CORROSION ON FLOOR BEAM UPPER SURFACE AND FASTENERS HOLES STA 985.5 AND LBL.45 TO RBL.45 AT PASSENGER CABIN FLOOR STRUCTURE. FLOOR BEAM STA.986.5 WAS REPAIRED PER B737-800 SRM 53-70-51-2R REPAIR 4.

Part: FLOOR SUPPORT — CORRODED (BS 948-995) · corrosion level 2 · airframe 69,442 hrs · 32,354 cycles

(LOG 0427486) CORROSION ON FLOOR ANGLE SILL BTW. STA 947.5 TO 995 AND LBL.51 ALSO CORROSION ON FLOOR ANGLE SILL BTW. STA 967 TO 986.5 AND RBL.51 AT PASSENGER CABIN FLOOR STRUCTURE. FLOOR ANGLE SILL BTW. STA 947.5 TO 995 AND LBL.51, AND FLOOR ANGLE SILL BTW. STA 967 TO 986.5 AND RBL.51 AT PASSENGER CABIN FLOOR STRUCTURE WERE REPLACED PER B737-800 SRM 5140-02-0G.

Part: FLOORBEAM — CORRODED (BS 991 RBL34-45) · corrosion level 2 · airframe 69,442 hrs · 32,354 cycles

FLOOR ANGLE: 1EA ( STA. 991 AND RBL.34 TO RBL.45) ( OUT OF LIMITS ) AT PASSENGER CABIN. FLOOR ANGLE STA. 991 AND RBL.34 TO RBL.45 AT PASSENGER CABIN WAS REPLACED PER DWG 147A5700 REV.C AND B737-800 SRM 51-40-02-0G.

Part: FLOORBEAM — CORRODED (BS 948) · corrosion level 2 · airframe 69,442 hrs · 32,354 cycles

(LOG 0427149) CORROSION ON FLOOR BEAM BELOW LAVATORY ATTACH FITTING BTW STA. 947.5 AND RBL.51 AT PASSENGER CABIN FLOOR STRUCTURE. FLOOR BEAM BELOW LAVATORY ATTACH FITTING BTW STA. 947.5 AND RBL.51 AT PASSENGER CABIN FLOOR STRUCTURE WAS REPAIRED PER B737-800 SRM 53-70-51-2R PROCEDURE 5. REPAIR 5.

Part: FRAME — CRACKED (BS 907 S8-9L) · airframe 69,442 hrs · 32,354 cycles

CRACK (0.100IN LENGTH) ON FUSELAGE FRAME AT INBOARD FASTENER HOLE STA 907 BTW S-8L & S-9L. FUSELAGE FRAME STA 907 BTW S-8L & S-9L WAS REPAIRED UNDER AMDS 2526-01236-03A.

Part: SUPPORT — CORRODED (FWD CARGO) · corrosion level 2 · airframe 69,442 hrs · 32,354 cycles

CORROSION ON LOWER SILL AT FWD CARGO COMPARTMENT. LOWER SILL AT FWD CARGO COMPARTMENT WAS REPLACED PER B737-800 SRM 51-40-02-0G.

Part: FLOORBEAM — CORRODED (BS 948 RBL27-49) · corrosion level 2 · airframe 69,442 hrs · 32,354 cycles

(LOG 0423548) CORROSION OUT LIMITS ON FLOOR " T" SUPPORT 1EA (BTW. STA.947.5 AND RBL.26.5 TO RBL.49) AT PASSENGER CABIN FLOOR STRUCTURE. PASSENGER CABIN FLOOR STRUCTURE WAS REPLACED PER B737-800 SRM 51-40-02-0G.

Part: STRAP — CORRODED (BS 312-344 LBL12) · corrosion level 2 · airframe 69,442 hrs · 32,354 cycles

(LOG 0423713) CORROSION ON STABILIZER STRAP (2 EAS) BTW STA 312 AND 344 LBL 12 AT W1. STABILIZER STRAP (2 EAS) BTW STA 312 AND 344 LBL 12 WERE REPLACED PER B737-800 SRM 51-40-02-0G.

Part: FLOOR SUPPORT — CORRODED (BS 948-967) · corrosion level 2 · airframe 69,442 hrs · 32,354 cycles

(LOG 0422146) CORROSION ON FLOOR SUPPORT BTW. STA.947.5 TO 967 AND RBL.51 AT PASSENGER CABIN FLOOR STRUCTURE. REPAIR FLOOR SUPPORT BTW. STA 947.5 TO 967 AND RBL.51 AT PASSENGER CABIN FLOOR STRUCTURE PER B737-800 SRM 51-40-02-0G.

Part: FRAME — CRACKED (BS 727B S8-9R) · airframe 69,442 hrs · 32,354 cycles

(LOG 0416124) CRACK (0.380IN LENGTH) ON FUSELAGE FRAME AT INBOARD FASTENER HOLE STA 727B BTW S-8R & S-9R. FUSELAGE FRAME STA 727B BTW S-8R & S-9R WAS REPAIRED UNDER AMDS 2526-01236-02B.

Part: FRAME — CRACKED (BS 727B S8-9L) · airframe 69,442 hrs · 32,354 cycles

(LOG 0415526) CRACK (0.480IN LENGTH) ON FUSELAGE FRAME AT INBOARD FASTENER HOLE STA 727B BTW S-8L & S-9L. FUSELAGE FRAME STA 727B BTW S-8L & S-9L WAS REPAIRED UNDER AMDS 2526-01236-02A.

Part: FRAME — CRACKED (BS 500C S8-9L) · airframe 69,442 hrs · 32,354 cycles

CRACK (0.400IN LENGTH) ON FUSELAGE FRAME AT INBOARD FASTENER HOLE STA 500C BTW S-8L & S-9L. FUSELAGE FRAME STA 500C BTW S-8L & S-9L WAS REPAIRED UNDER AMDS 2526-01236-02A.

Part: FRAME — CRACKED (BS 500C S8-9R) · airframe 69,442 hrs · 32,354 cycles

(LOG 0416116) CRACK (0.400IN LENGTH) ON FUSELAGE FRAME AT INBOARD FASTENER HOLE STA 500C BTW S-8R & S-9R. FUSELAGE FRAME STA 500C BTW S-8R & S-9R WAS REPAIRED UNDER AMDS 2526-01236-02B.

Part: PLATE — CORRODED (BS 500E-500I) · corrosion level 2 · airframe 69,442 hrs · 32,354 cycles

CORROSION OUT LIMITS ON LH SIDEPLATE FROM STA 500E TO STA 500I AT FWD CARGO COMPARTMENT. SIDE PLATE FROM STA BETWEEN 500 D AND 500 E TO STA 500 I AT FWD CARGO COMPARTMENT WAS REPLACED PER B737-800 SRM 53-00-53-2R.

Part: FRAME — CRACKED (BS 827 S8-9R) · airframe 69,442 hrs · 32,354 cycles

(LOG 0416127) CRACK (0.200IN LENGTH) ON FUSELAGE FRAME AT INBOARD FASTENER HOLE STA 827 BTW S-8R & S-9R. FUSELAGE FRAME STA 827 BTW S-8R & S-9R WAS REPAIRED UNDER AMDS 2526-01236-02B.

Part: FRAME — CRACKED (BS 440 S8-9L) · airframe 69,442 hrs · 32,354 cycles

CRACK (1.000IN LENGTH) ON FUSELAGE FRAME AT INBOARD FASTENER HOLE STA 440 BTW S-8L & S-9L. FUSELAGE FRAME STA 440 BTW S-8L & S-9L WAS REPAIRED UNDER CARD(AMDS) 2526-01236-02A.

Part: FRAME — CRACKED (BS 27D S8-9L) · airframe 69,442 hrs · 32,354 cycles

(LOG 0415377) CRACK (0.280IN LENGTH) ON FUSELAGE FRAME AT INBOARD FASTENER HOLE STA 727D BTW S-8L & S-9L. FUSELAGE FRAME STA 727D BTW S-8L & S-9L WAS REPAIRED UNDER AMDS 2526-01236-02A.

Part: FRAME — CRACKED (BS 380 S8-9L) · airframe 69,442 hrs · 32,354 cycles

(LOG 0415333) CRACK (0.520IN LENGTH) ON FUSELAGE FRAME AT INBOARD FASTENER HOLE STA 380 BTW S-8L & S-9L AND CRACK (0.200IN LENGTH) ON FUSELAGE FRAME AT OUTBOARD FASTENER HOLE STA 380 BTW S-8L & S-9L.

Part: FRAME — CRACKED (BS 500A S8-9L) · airframe 69,442 hrs · 32,354 cycles

(LOG 0415367) CRACK (0.120 IN LENGTH) ON FUSELAGE FRAME AT INBOARD FASTENER HOLE STA 500A BTW S-8L & S-9L. FUSELAGE FRAME STA 500A BTW S-8L & S-9L WAS REPAIRED UNDER AMDS 2526-01236-02A.

Part: FRAME — CRACKED (BS 380 S8-9R) · airframe 69,442 hrs · 32,354 cycles

CRACK (0.680IN LENGTH) ON FUSELAGE FRAME AT INBOARD FASTENER HOLE STA 380 BTW S-8R & S-9R. FUSELAGE FRAME STA 380 BTW S-8R & S-9R WAS REPAIRED UNDER AMDS 2526-01236-02B.

Part: SEAT TRACK — CORRODED (BS 520 RBL25) · corrosion level 2 · airframe 69,442 hrs · 32,354 cycles

CORROSION OUT LIMITS ON SEAT TRACK STA 520 RBL 25 AT FLOOR STRUCTURE. SEAT TRACK STA 520 RBL 25 AT FLOOR STRUCTURE WAS REPLACED PER B737-800 SRM 51-40-02-0G.

Part: BEAM — CORRODED (BS 294) · corrosion level 2 · airframe 69,442 hrs · 32,354 cycles

(LOG 0404892) CORROSION ON BEAM STA 294 RBL 10 AT W1. BEAM STA 294 RBL 10 AT W1 WAS REPAIRED PER B737-800 SRM 53-10-51-2R.

Part: STRAP — CORRODED (BS 312-328) · corrosion level 2 · airframe 69,442 hrs · 32,354 cycles

(LOG 0404888) CORROSION ON STABILIZER STRAP BTW STA 312 AND 328 RBL 10 AT W1. STABILIZER STRAP BTW STA 312 AND 328 RBL 10 AT W1 WAS REPLACED PER B737-800 SRM 51-40-02-0G.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 68,503 hrs · 31,909 cycles

(LOG 5081756) FOUND UPPER AND LOWER EXIT LIGHTS AT AFT LEFT DOOR INOP. REMOVED AND REPLACED BATTERY PACK M1673 IAW B737 AMM 33-51.

Part: BATTERY PACK — INOPERATIVE · airframe 66,449 hrs · 30,944 cycles

(LOG 5519314) DURING INSPECTION FOUND SEVERAL AFT CABIN SEAT ROWS EMERGENCY AISLE LIGHTS INOP. R/R BATTERY PACK M1672 REF B737 AMM 33-51. OPS OK.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 66,250 hrs · 30,845 cycles

(LOG 4030192) DURING INSPECTION FOUND ROW 16 SEATS FED ISLE ILLUMINATION EMERGENCY LIGHT INOP. FOUND CONNECTOR UNDER SEAT DISCONNECTED . RECONNECTED AND PERFORMED OPERATIONAL TEST PER B737 AMM 33-51. CHECKS SATISFACTORY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 64,925 hrs · 30,251 cycles

(LOG 9443576) DURING INSPECTION FOUND 17F VERTICLE EXIT LIGHT INOP. REPLACED LIGHT ASSY PN BR9476-G-145-01 REF B737 IPC 33-51-01-06C ITEM 545, REF B737 AMM 33-51-01-201.

Part: NONE — NONE · airframe 64,637 hrs · 30,105 cycles

(LOG 2406863) DURING INSPECTION FOUND EMERGENCY SEAT MOUNTED LIGHTING DAMAGED / INOP / LOCATIONS:33D. RESECURED EMERGENCY SEAT MOUNTED LIGHTING AT LOCATION 33D PER B737 AMM 33-14. CHKS OK.

Part: TRANSMITTER — INOPERATIVE (TE FLAPS) · airframe 62,160 hrs · 28,955 cycles

SHIP 3729 -DE- DUE TO FLAPS WOULD NOT EXTEND ON APPROACH. PERFORMED FSEU BITE CHECK FAULT 27-53256 (FLAP 7 SKEW) REPORTED. REPLACED #7 FLAP SKEW SENSOR. REPLACED RIGHT FLAP POSITION TRANSMITTER PRECAUTIONARY DUE TO AHM REPORT. OPS CHECKS GOOD.

Part: WIRE — DAMAGED (EMERGENCY LIGHTS) · airframe 61,463 hrs · 28,675 cycles

(LOG 1877385) DURING INSPECTION FOUND EMERGENCY SEAT PATH LIGHTING INOP RH SIDE BETWEEN STA 663 TO STATION 927. REPAIRED EEPL WIRING AT SEAT 28FED AND 33FED, REPLACED FUSES AT POWER SUPPLY M1671, AND PERFORMED OPS CHECK OF THE EEPLS PER B737 AMM 33-51-06, B737 SWPM 20-30-12, B737 SWPM 20-42-01, B737.

Part: LIGHT — INOPERATIVE (SEAT ROW 28FED) · airframe 61,463 hrs · 28,675 cycles

(LOG 1877386) DURING INSPECTION FOUND EMERGENCY AREA LIGHT (OVERHEAD BIN) AT SEAT ROW 28FED INOP. REMOVED AND REPLACED EMERGENCY AREA LIGHT (OVERHEAD BIN) AT SEAT ROW 28FED IAW B737 AMM 33-51-03-960-802 OPS CHECK GOOD.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHTS) · airframe 54,511 hrs · 25,698 cycles

(LOG 4855139) EMERGENCY CEILING AREA LIGHTS AT 1AB AND 10ABC INOP DURING WORKCARD 3350-7390 EMERGENCY LIGHT CHECK. TROUBLESHOT SYSTEM FOUND CANNON PLUG D11088 AND D11344 CAP AND STOWED. RECONNECTED PLUGS OPS CHECK GOOD PER WORKCARD 3350-7390.

Part: STRUCTURE — DAMAGED · airframe 53,944 hrs · 25,451 cycles

DURING INSPECTION FOUND ELONGATED HOLES ON J22 JUNCTION BOX ASSEMBLY. ELONGATED HOLES ON J22 JUNCTION BOX ASSEMBLY WAS REPAIR PER ETI-37-18-497, REV ORIG AND ERA 571331-14AD REV ORIG.

Part: FRAME — DENTED (FUSELAGE) · airframe 53,944 hrs · 25,451 cycles

DURING INSPECTION FOUND AFT CARGO COMPARTMENT STA 727J FUSELAGE FRAME FREE FLANGE IS DENTED, STR 25R. FRAME STR 23-24RH WAS ACCOMPLISHED SECTION I AS PERMANENT REPAIR PER ETI-37-18-496 REV 1 AND ER/A 571308-14 REV ORIG.

Part: FRAME — DENTED (FUSELAGE) · airframe 53,944 hrs · 25,451 cycles

DURING INSPECTION FOUND AFT CARGO COMPARTMENT STA 727G FUSELAGE FRAME FREE FLANGE IS DENTED BTW STR 25L. FRAME STR 25L WAS ACCOMPLISHED SECTION I AS PERMANENT REPAIR PER ETI-37-18-491 REV 2 AND ER/A 571309-14 REV ORIG.

Part: FRAME — DENTED (FUSELAGE) · airframe 53,944 hrs · 25,451 cycles

DURING INSPECTION FOUND AFT CARGO COMPARTMENT STA 727G FUSELAGE FRAME FREE FLANGE IS DENTED BTW STR 24L. FRAME STR 24L WAS ACCOMPLISHED SECTION I AS PERMANENT REPAIR PER ETI-37-18-491 REV 2 AND ER/A 571309-14 REV ORIG.

Part: FRAME — DENTED (FUSELAGE) · airframe 53,944 hrs · 25,451 cycles

DURING INSPECTION FOUND FWD CARGO COMPARTMENT STATION 500B FUSELAGE FRAME FREE FLANGE IS DENTED STR 25L. FWD CARGO COMPARTMENT STA 500B, STR 25L WAS ACCOMPLISHED SECTION I AS PERMANENT REPAIR PER ETI-37-18-502 REV 1 AND ER/A 571312-14 REV ORIG.

Part: FRAME — DENTED (FUSELAGE) · airframe 53,944 hrs · 25,451 cycles

DURING INSPECTION FOUND FWD CARGO COMPARTMENT STA 500A FUSELAGE FRAME FREE FLANGE IS DENTED BTW STR 25L - 26L. FRAME BTW STR 25L - 26L WAS ACCOMPLISHED SECTION I AS PERMANENT REPAIR PER ETI-37-18-501 REV 1 AND ER/A 571311-14 REV ORIG.

Part: FRAME — DENTED (FUSELAGE) · airframe 53,944 hrs · 25,451 cycles

DURING INSPECTION FOUND AFT CARGO COMPARTMENT STA 727H FUSELAGE FRAME FREE FLANGE IS DENTED, STR 25R. FRAME AT STR 25R WAS ACCOMPLISHED SECTION II AS PERMANENT REPAIR PER ETI-37-18-500 REV 1 AND ER/A 504542-14 REV B.

Part: FRAME — DENTED (FUSELAGE) · airframe 53,944 hrs · 25,451 cycles

DURING INSPECTION FOUND FWD CARGO COMPARTMENT STA 500C FUSELAGE FRAME FREE FLANGE IS DENTED BTW STR 25L. FRAME AT STR 25L WAS ACCOMPLISHED SECTION I AS PERMANENT REPAIR PER ETI-37-18-503 REV 1 AND ER/A 571313-14 REV ORIG.

Part: FRAME — DENTED (FUSELAGE) · airframe 53,944 hrs · 25,451 cycles

DURING INSPECTION FOUND AFT CARGO COMPARTMENT STA 727G FUSELAGE FRAME FREE FLANGE IS DENTED, STR 25R. FRAME AT STR 25R WAS ACCOMPLISHED SECTION I AS PERMANENT REPAIR PER ETI-37-18-499 REV 1 AND ER/A 571310-14 REV ORIG.

Part: PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,944 hrs · 25,451 cycles

DURING INSPECTION FOUND CORROSION OUT LIMIT ON LT ZEE SIDE PLATE AT FWD CARGO COMPARTMENT STA 360 TO 500D S26L. CORROSION LEVEL 2. LT ZEE SIDE PLATE AT FWD CARGO COMPARTMENT STA 360 TO 500D S26L WAS REPAIRED PER SRM 53-00-53 REP 6.

Part: PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,944 hrs · 25,451 cycles

DURING INSPECTION FOUND CORROSION ON LT SIDE PLATE FROM STA 727 TO 847, IN AFT CARGO COMPARTMENT. LEVEL CORROSION 2; SIDE PLATE WAS REPLACED PER SRM 53-00-53 REP 5.

Part: SEAT TRACK — WORN (FUSELAGE) · airframe 53,944 hrs · 25,451 cycles

DURING INSPECTION FOUND CABIN SEAT TRACK IS WORN ON THE CROWN, STA 520 RBL 24. CABIN SEAT TRACK WAS REPAIRED PER SRM 53-00-52 REP 4.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,944 hrs · 25,451 cycles

DURING INSPECTION FOUND INITIAL INSPECTION: CORROSION ON FLOORBEAM STA Y=312 LBL 11 AT PAX CABIN ( W1 ). CORROSION LEVEL 2. FLOORBEAM STA Y=312 LBL 11 WAS ACCOMPLISHED SECTION I AS PERMANENT REPAIR PER ETI-37-18 -486 REV 1 AND ER/A 571228-14 REV ORIG.

Part: FLOORBEAM — CORRODED (BS 887) · corrosion level 2 · airframe 53,944 hrs · 25,451 cycles

DURING INSPECTION FOUND CORROSION ON FLOORBEAM, BS 887, BETWEEN STRINGERS 25L & 26R , IN THE AFT CARGO BAY. THE FLOORBEAM WAS REPLACED IAW SRM 51-40-02, AND DWG 146A9401, REV C.

Part: NOT REPORTED — DAMAGED (BS 360-500I) · airframe 53,944 hrs · 25,451 cycles

DURING INSPECTION FOUND OUT OF LIMITS DURING REWORK ON CORRODED AEAS FROM NRC 00523. STA 360 TO 500I CRACK WAS FOUND IN STATION 500A +5. OUT OF LIMIT AREAS ON STA 360 TO 500I AND CRACK IN STA 500 A+5 WERE REPLACED. PER B737-800 SRM 53-00-53 REPAIR 6.

Part: DOOR FRAME — CORRODED (BS 294.5) · corrosion level 2 · airframe 53,944 hrs · 25,451 cycles

DURING INSPECTION, FOUND CORROSION ON THE R1 DOOR FRAME, BS 294.5, RBL 55. DAMAGE AREA WAS REPAIRED IAW ETI 37-18-485, REV 1, AND ERA 571022-14, REV ORIG.

Part: SKIN — WORN (BS 224-235) · airframe 53,944 hrs · 25,451 cycles

DURING INSPECTION, FOUND WARE ON A PREVIOUS REPAIR AROUND EXTERNAL POWER RECEPTACLE CUT OUT AREA BETWEEN BS 224 - 235, STRINGERS 21R - 23R. THE POWER RECEPTACLE CUT OUT AREA WAS REPAIRED IAW ER/A 453862-14.

Part: SKIN — CRACKED (LT WING TE FLAP) · airframe 53,944 hrs · 25,451 cycles

DURING INSPECTION, FOUND A CRACK ON THE INBD FLAP LOWER SURFACE ON THE LT WING. REPAIRED IAW SRM 57-53-01, REPAIR 4, AND SRM 51-70-10, REPAIR GENERAL.

Part: FRAME — CRACKED (BS 500A) · airframe 53,944 hrs · 25,451 cycles

DURING INSPECTION, FOUND A CRACK ON THE FRAME AT BS 500A, BETWEEN STRINGERS 8R & 9R. FRAME WAS REPAIRED ER/A 570792-14AD, REV ORIG.

Part: FLOOR SUPPORT — CRACKED (BS 344-360) · airframe 53,944 hrs · 25,451 cycles

DURING INSPECTION, FOUND A CRACK ON THE INTERCOSTAL BETWEEN BS 360 AND 344, LBL 1. THE INTERCOSTAL WAS REPLACED IAW SRM 51-40-02.

Part: FRAME — CRACKED (BS 400) · airframe 53,944 hrs · 25,451 cycles

DURING INSPECTION, FOUND A CRACK ON THE FRAME, BS 400, BETWEEN STRINGERS 8R & 9R. THE FRAME WAS REPAIRED IAW ERA 570792-14AD, REV ORIG.

Part: FRAME — CRACKED (BS 480) · airframe 53,944 hrs · 25,451 cycles

DURING INSPECTION, FOUND A CRACK ON THE FRAME AT BS 480, BETWEEN STRINGERS 8R & 9R. THE FRAME WAS REPAIRED IAW ER/A 570792-14AD, REV ORIG.

Part: FRAME — CRACKED (BS 480) · airframe 53,944 hrs · 25,451 cycles

DURING INSPECTION, FOUND A CRACK ON THE FRAME AT BS 480 BETWEEN STRINGERS 8L TO 9L. MAINTENANCE REPAIRED THE FRAME IAW ERA 570792-14.

Part: FRAME — CRACKED (BS 400) · airframe 53,944 hrs · 25,451 cycles

DURING INSPECTION, FOUND A CRACK ON THE FRAME AT BS 400, BTW STRINGERS 8L & 9L. THE FRAME WAS REPAIRED IAW ER/A 570792-14AD, REV ORIG.

Part: FRAME — CRACKED (BS 867) · airframe 53,944 hrs · 25,451 cycles

DURING INSPECTIONM FOUND CRACK ON THE FRAME AT BS 867, BETWEEN STRINGERS 8R & 9R. THE FRAME WAS REPAIRED IAW ER/A 570792-14AD, REV ORIG.

Part: FRAME — CRACKED (BS 440) · airframe 53,944 hrs · 25,451 cycles

DURING INSPECTION, FOUND A CRACK ON THE FRAME AT BS 440, BETWEEN STRINGERS 8R & 9R. THE FRAME WAS REPAIRED IAW ER/A 570792-14AD, REV ORIGINAL.

Part: ANGLE — CRACKED (BS 927-947) · airframe 53,944 hrs · 25,451 cycles

DURING INSPECTION, FOUND A CRACK ON THE ANGLE BETWEEN BS 927 AND 947.5, LBL 1. THE ANGLE WAS REPLACED IAW SRM 51-40-02, PAR 4, AND DWG 147A5430, REV.A.

Part: FLOORBEAM — CORRODED (BS 947.5) · corrosion level 2 · airframe 53,944 hrs · 25,451 cycles

DURING INSPECTION, FOUND CORROSION ON THE FLOORBEAM BS 947.5, BETWEEN LBL 40 - 52. THE FLOORBEAM WAS REPAIRED IAW SRM 53-70-51, REP 5.

Part: FLOOR SUPPORT — CRACKED (BS 344-360) · airframe 53,944 hrs · 25,451 cycles

DURING INSPECTION, FOUND A CRACK ON THE FLOOR SUPPORT BETWEEN BS 360 AND 344, LBL 12. REPAIRED IAW SRM 51-40-02, PAR 7, SRM 53-10-51, REPAIR 6, SRM 51-30-01, AND AMM 51-01-72-370-804.

Part: FLOOR SUPPORT — CRACKED (BS 277-294) · airframe 53,944 hrs · 25,451 cycles

DURING AN INSPECTION, FOUND A CRACK ON THE FLOOR SUPPORT BETWEEN BS 277 AND 294, RBL 1. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-40-02.

Part: SKIN — CRACKED (BS 224-235) · airframe 53,944 hrs · 25,451 cycles

DURING INSPECTION, FOUND A CRACK ON THE EXTERNAL POWER RECEPTACLE CUT OUT AREA, BS 224 - 235, AND STRINGERS 22R - 23R ON THE LOWER FUSELAGE. THE DAMAGED AREA WAS REPAIRED IAW SRM 53-10-15, REP 4.

Part: FLOOR SUPPORT — CRACKED (BS 312-328) · airframe 53,944 hrs · 25,451 cycles

DURING INSPECTION, FOUND A CRACK ON THE FLOOR SUPPORT BETWEEN BS 312 AND 328, LBL 44. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CRACKED (BS 312-328) · airframe 53,944 hrs · 25,451 cycles

DURING INSPECTION, FOUND A CRACK ON THE FLOOR SUPPORT BETWEEN BS 312 AND 328, RBL 31. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-40-02.

Part: ENGINE — MAKING METAL (NR 1) · airframe 53,645 hrs · 25,351 cycles

ATO - DURING TAKEOFF AS TO/GA WAS SELECTED AND THE THROTTLES STARTED TOWARD TAKEOFF SETTING A LARGE VIBRATION WAS FELT AND ENGINE FAIL MESSAGE ILLUMINATED. CREW ABORTED TAKEOFF. MAINTENANCE FOUND METAL FRAGMENTS IN TAIL PIPE OF NUMBER 1 ENGINE. REMOVED AND REPLACED NUMBER ONE ENGINE. AIRCRAFT RETURNED TO SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 50,694 hrs · 24,312 cycles

DURING INSPECTION, FOUND THE EMERGENCY LIGHTS INOPERATIVE FROM THE R1 DOOR TO SEAT 10D. MAINTENANCE REMOVED AND REPLACED BATTERY IAW AMM 33-51. OPS CHECKED OK.

Part: SEAT TRACK — DAMAGED (BS 727H) · airframe 45,784 hrs · 22,626 cycles

DURING INSPECTION FOUND SEAT TRACK DAMAGED AT APPROXIMATELY BS 727H AND RBL 24.75. MAINTENANCE REPAIRED SEAT TRACK IAW SRM 53-00-52, REPAIR 5 AND ERA 545846-14, REV ORIGINAL REF NRC 067.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 43,420 hrs · 21,789 cycles

DURING TESTING, FOUND EMERGENCY LIGHT BATTERY PACK M1671 FAILED THE CAPACITY CHECK. MAINTENANCE R & R THE BATTERY PACK IAW MM 33-51-06. OPS CHECKED GOOD.

Part: LIGHT — DAMAGED (SEAT 11D) · airframe 41,889 hrs · 21,255 cycles

DURING INSPECTION, FOUND EMERGENCY SEAT MOUNTED LIGHTING DAMAGED INOPERATIVE AT LOCATIONS 11D. REPLACED ENTIRE LIGHT MOUNT ASSEMBLY.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 40,724 hrs · 20,852 cycles

DURING INSPECTION FOUND SCRAPE ON FUSELAGE 18 INCHES AFT OF L2 DOOR AT VIEWING PORT HEIGHT. MAINTENANCE REPAIRED IAW SRM 53-00-01. CLEANED AND BURNISHED DAMAGED AREA. HFEC INSPECTED IAW NDT PART 6, 51-00-00, NO CRACKING FOUND. OK TO PAINT, PAINTED DAMAGED AREA.

Part: FRAME — DENTED (BS 727H) · airframe 40,059 hrs · 20,626 cycles

DURING INSPECTION, A DENT WAS FOUND ON THE INNER FLANGE OF THE A FRAME AT BS 727H BETWEEN S-23-24R. MAINTENANCE REPAIRED IAW ERA 504542-14.

Part: FLOORBEAM — CRACKED (BS 727B) · airframe 39,848 hrs · 20,560 cycles

DURING INSPECTION FOUND FLOORBEAM BS 727B SPLICE STRAP RBL 24.75, LBL 45.50, AND RBL 45.50 HAS CRACK DAMAGE. MAINTENANCE REPAIRED ON NON-ROUTINES 157, 158, 159 IAW ERA 527462-14AD, REV ORIG.

Part: LIGHT — DAMAGED (CABIN) · airframe 38,513 hrs · 20,082 cycles

DURING INSPECTION, FOUND EMERGENCY FLOOR LIGHTING DAMAGED OR INOPERATIVE AT LOCATIONS 130. MAINTENANCE REPAIRED FLOOR LIGHTING DAMAGE, REF AMM 33-51. OPS TEST OK.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 36,747 hrs · 19,409 cycles

DURING TEST FOUND FOUR EMERGENCY LIGHT BATTERY PACKS FAILED CAPACITY TEST. MX R & R BATTERY PACKS M1672, M1674, M1675, M1695. TESTED OK IAW AMM 33-51-06/201.

Part: SKIN — CORRODED (FUSELAGE) · airframe 36,431 hrs · 19,281 cycles

FUSELAGE SKIN FS 510 BETWEEN STR 28R - 28L CORROSION. REPAIRED AIW ERA 499799-14 LOG 0880419.

Part: STRINGER — DENTED (FUSELAGE) · airframe 33,265 hrs · 18,107 cycles

AFT CARGO COMPARTMENT STRINGER DENTED AT STA 727, 23R AND 24R. REPAIRED IAW ERA 504542-14 REV ORIG.

Part: SEAT TRACK — WORN (FUSELAGE) · airframe 33,265 hrs · 18,107 cycles

SEAT TRACK AT STA 521.5 LBL 45 FOUND TO BE WORN. REPAIRED IAW B737-800 SRM 53-00-52 REPAIR 4.

Part: SEAT TRACK — WORN (FUSELAGE) · airframe 33,265 hrs · 18,107 cycles

CABIN SEAT TRACK AT STA 521.5 RBL 24 WORN. REPAIRED IAW B737-800 SRM 53-00-52.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 33,265 hrs · 18,107 cycles

LEFT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 120.30. REPAIRED IAW B737-800 SRM 55-10-01 REPAIR 11.

Part: FSEU — FAILED (E/E BAY) · airframe 6,789 hrs · 7,028 cycles

RETURN TO ATL, WITH LEADING EGDE SLAT NR 1 AND LEADING EDGE FLAPS NR 1 AND NR 4, REMAINING ILLUMINATED AMBER ON AFT OVERHEAD ANNUNCIATOR, LE FLAP TRANSIT REMAINED ILLUMINATED CREATING LE LOCKOUT NO ADVERSE ROLL. REPLACED FSEU FOR FAULT CODE 27-51105.

Part: UNKNOWN — ODOR (CABIN) · airframe 927 hrs · 1,173 cycles

DURING T/O, AS PWR WAS ADVANCED-A VERY STRONG ODOR LIKE PLASTIC WITH NO SMOKE. ODOR SLOWLY DISSAPATED DURING FLT. AND THEN RETURNED DURING DESCENT BUT NOT AS STRONG AS T/O. C/A OPERATED BOTH AC PACKS PER AMM21-00-01-2. PLASTIC ODOR DISSAPATED AFTER SEVERAL MINUTES. NO ODOR REMAINED.

Part: ENGINE — FAILED (NR 2) · airframe 926 hrs · 1,172 cycles

SPOOLING UP NR 2 ENG , AT 40 PERCENT FOR TAKE OFF, AIRCRAFT SHUDDERED. ENGINE SHUT DOWN ON ITS OWN AND ENGINE FAIL LIGHT ILLUMINATED. ENGINE OVERTEMPED. ENGINE CHANGED.