N385DN

Part: NONE — NONE (NONE) · airframe 75,260 hrs · 30,293 cycles

(LOG 0393704) ACCOMPLISH VA 100468MA REV H IN CONJUNCTION WITH AA 2540-01414.

Part: INDICATOR — INOPERATIVE (TE FLAPS) · airframe 74,950 hrs · 30,169 cycles

SHIP 3715 -UFC- DECLARED EMERGENCY AND PERFORMED GO AROUND DUE TO TRAILING EDGE FLAP LOCKOUT ON APPROACH SLC. CORRECTIVE ACTION: MAINTENANCE REPLACED FLAP POSITION INDICATOR PER B737 AMM 27-58.

Part: WIRE — SHORTED (ANTI-SKID VALVE) · airframe 74,321 hrs · 29,884 cycles

SHIP 3715 -MISC/DE- DECLARED EMERGENCY DUE TO ANTISKID LIGHT ILLUMINATED. CORRECTIVE ACTION: FOUND SHORTED WIRING AT RIGHT INBOARD ANTISKID VALVE PLUG D930. REPLACED CONNECTOR. OPS CHECKS GOOD.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 74,172 hrs · 29,823 cycles

(LOG 0148660) LH SHEAR WEB STA 990 IS CORRODED. REPAIRED LH SHEAR WEB IAW DELTA ER/A 614469-14.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 74,172 hrs · 29,823 cycles

(LOG 0146981) AFT WET AREA FLOOR BEAM STA 967 RBL5, 18, 30 CORROSION AROUND SCREW HOLES. REPAIRED FLOOR BEAM STA 967 IAW DELTA ER/A 614359-14 REV ORIG.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 74,172 hrs · 29,823 cycles

(LOG 0134213) AFT CARGO TRACK RBL 14 STA 727G TO 727J CRACKED WHERE MOUNTS TO FRAME. REMOVED AND REPLACED CARGO TRACK FROM STA 727F TO 787 RBL 14 IAW BOEING 737-800 SRM 53-00-53-2R.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 74,172 hrs · 29,823 cycles

(LOG 0134055) PERFORM LH #1 FLIGHT DECK WINDOW FRAME PERMANENT REPAIR. REPAIRED LH #1 FLIGHT DECK WINDOW FRAME IAW DELTA ERA 611573-14 REV ORIG.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 74,172 hrs · 29,823 cycles

(LOG 0134220) AFT CARGO TRACK RBL 14 STA 767-827 CORRODED. REMOVED AND REPLACED CARGO TRACK FROM STA 767 TO 827 RBL 14 IAW BOEING 737-800 SRM 53-00-53-2R.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 74,172 hrs · 29,823 cycles

(LOG 01323864) PANEL BREAK AT STA 540 CABIN FLOOR IS CRACKED BETWEEN BL 0 -LBL 22. REMOVED AND REPLACED PANEL BREAK AT STA 540 CABIN FLOOR IAW BOEING 737-800 SRM 51-40-02.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 74,172 hrs · 29,823 cycles

(LOG 0132685) AFT CARGO STA 727D STR 26L-26R LOWER FRAME CHORD EXFOLIATED. REPAIRED AFT CARGO STA 727D STR 26L-26R LOWER FRAME CHORD IAW DELTA ERA 614277-14 REV ORIG.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 74,172 hrs · 29,823 cycles

(LOG 0132675) LH WING RIB 18 UPPER SKIN SHEAR TIE CUT BETWEEN STR 8 & STR 9 WHEN SHOULD HAVE BEEN CUT BETWEEN STR 9 & STR 10. REPAIRED RIB 18 BETWEEN STR 8 & STR 9 IAW DELTA ERA 614253-14 REV ORIG.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 74,172 hrs · 29,823 cycles

(LOG 0129550) FWD CARGO STA 500G LBL 24 WEB ANGLE CRACKED. REMOVED AND REPLACED DAMAGED WEB IAW BOEING 737-800 SRM 51-40-02.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 74,172 hrs · 29,823 cycles

(LOG 0129558) FWD CARGO STA 500H LBL24 WEB ANGLE CRACKED. REMOVED AND REPLACED DAMAGED WEB IAW BOEING 737-800 SRM 51-40-02.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 74,172 hrs · 29,823 cycles

(LOG 0129526) FWD WET AREA FLOOR BEAM STA 328 LBL23 - RBL30 HAS AREAS OF CORROSION ON UPPER SURFACE. REPAIRED FLOOR BEAM STA 328 IAW BOEING 737-800 SRM 53-10-51-2R REPAIR 12.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 74,172 hrs · 29,823 cycles

(LOG 0123141) AFT CARGO TRACK LBL14 STA 767 CRACKED WHERE MOUNTS TO FRAME. REPAIRED AFT CARGO TRACK AT LBL14 STA 767 IAW BEOING 737-800 SRM 53-00-53-2R REPAIR 3.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 74,172 hrs · 29,823 cycles

(LOG 0121710) AFT WET AREA L/H MOP SILL CORRODED. REMOVED AND REPLACED AFT LH MOP SILL IAW BOEING 737-800 SRM 51-40-02.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 74,172 hrs · 29,823 cycles

(LOG 0121641) AFT WET AREA R/H MOP SILL CORRODED. REMOVED AND REPLACED RH AFT MOP SILL IAW BOEING 737-800 SRM 51-40-02.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 74,172 hrs · 29,823 cycles

(LOG 0121664) AFT WET AREA STA 987 RBL44 WEB CORRODED. REMOVED AND REPLACED AFT RH SHEAR WEB IAW BOEING 737-800 SRM 51-40-02.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 74,172 hrs · 29,823 cycles

(LOG 0121746) FWD CARGO STA 500H LOWER FRAME INNER CHORD AT LBL28 IS DENTED. REPAIRED FWD CARGO FRAME STA 500H LBL 28 IAW BOEING 737-800 SRM 53-30-07-2R.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 74,172 hrs · 29,823 cycles

(LOG 0117372) SEAT TRACK DAMAGED STA 727 RBL 45.5. REPAIRED SEAT TRACK STA 727 RBL 45.5 IAW BOEING 737-800 SRM 53-00-52-2R REPAIR 3.

Part: FLOORBEAM — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 74,172 hrs · 29,823 cycles

(LOG 0117481) AFT WET AREA FLOOR BEAM STA 986.5 LBL51-RBL51 CORRODED ON UPPER SURFACE. REMOVED , FABRICATED & INSTALLED NEW TOP CAP FOR EXISTING BEAM REPAIR AT STA 986 IAW BOEING 737-800 SRM 53-70-51-2R-4.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 74,172 hrs · 29,823 cycles

(LOG 0117402) FWD CARGO FRAME STA 500C LBL29 HAS DENT IN RADIUS OF FRAME. REPAIRED FWD CARGO FRAME STA 500C IAW BOEING 737-800 SRM 53-30-07-2R PROCEDURE 1 REPEAT INSPECTION IS REQUIRED IAW BOEING 737-800 SRM 53-30-07-2R.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 74,172 hrs · 29,823 cycles

(LOG 0117377) PANEL BREAK AT STA 540 CABIN FLOOR AREA IS CRACKED BETWEEN BL0-RBL22. REMOVED AND REPLACED PANEL BREAK AT STA 540 BL0-RBL22 IAW BOEING 737-800 SRM 51-40-02.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 74,172 hrs · 29,823 cycles

(LOG 0115827) AFT WET AREA FLOOR SUPPORT STA 967-986.5 RBL 16 CORRODED ON UPPER SURFACE. REMOVED SUPPORT AND LOCATED AND DRILLED NEW SUPPORT FOR STA 967-986.5 RBL AND INSTALLED IAW BOEING 737-800 SRM 51-40-02.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 74,172 hrs · 29,823 cycles

(LOG 0115875) FWD CARGO FRAME STA 500C LBL 29 HAS A DENT IN RADIUS OF FRAME. REPAIRED FWD CARGO FRAME STA 500C LBL29 IAW BOEING 737-800 SRM 53-30-07-2R PROCEDURE 1.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 74,172 hrs · 29,823 cycles

(LOG 0115818) AFT WET AREA FLOOR SUPPORT FS 967-986.5 LBL 16 CORRODED ON UPPER SURFACE. REMOVED FLOOR SUPPORT & LOCATED AND DRILLED NEW SUPPORT FOR STA 967-986.5 LBL 16 AND INSTALLED IAW BOEING 737-800 SRM 51-40-02.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 74,172 hrs · 29,823 cycles

(LOG 0115871) FWD CARGO STA 500H LOWER FRAME INNER CHORD AT LBL28 IS DENTED. REPAIRED FWD CARGO FRAME STA 500H LBL28 IAW BOEING 737-800 SRM 53-30-07-2R PROCEDURE 1.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 74,172 hrs · 29,823 cycles

(LOG 0112867) LH SIDE OF VERTICAL FIN FWD SKATE ANGLE DAMAGED. REMOVED AND REPLACED LH FWD SKATE ANGLE IAW BOEING 737-800 SRM 51-40-02.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 74,172 hrs · 29,823 cycles

(LOG 0111440) AFT WET AREA FLOOR BEAM STA 947 LBL6 -RBL54 CORRODED ON TOP SURFACE. REPAIRED FLOOR BEAM STA 947 LBL6-RBL54 IAW BOEING 737-800 SRM 53-70-51-2R-5.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 74,172 hrs · 29,823 cycles

(LOG 0111412) AFT WET AREA FLOOR SUPPORTS STA 947-967 RBL 50 CORROSION AROUND SCREW HOLE. REMOVED AND REPLACED FLOOR SUPPORT STA 947-967 IAW BOEING 737-800 SRM 51-40-02.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 74,172 hrs · 29,823 cycles

(LOG 0111389) FWD WET AREA R/H MOP SILL CORRODED. REMOVED & REPLACED FWD R/H MOP SILL IAW BOEING 737-800 SRM 51-40-02.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 74,172 hrs · 29,823 cycles

(LOG 0111396) FWD WET AREA R/H MOP SILL CORRODED. REMOVED & REPLACED FWD R/H MOP SILL IAW BOEING 737-800 SRM 51-40-02.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 74,172 hrs · 29,823 cycles

(LOG 0111436) AFT WET AREA FLOOR SUPPORT STA 950 RBL 45 CORROSION AROUND SCREW HOLE. REMOVED AND REPLACED FLOOR SUPPORT STA 950 RBL 45 IAW BOEING 737-800 SRM 51-40-02.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 74,172 hrs · 29,823 cycles

(LOG 0108345) LH FUSELAGE FRAME STA 907 IS CRACKED BETWEEN STR 8 & 9 AT I/B HOLE FOR AC RAIL BIN SUPPORT BRACKET. REPAIRED LH FRAME STA 907 BETWEEN STR 8 & 9 IAW DELTA TASK CARD 2526-01236-03A

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 74,172 hrs · 29,823 cycles

(LOG 0107148) RH FUSELAGE FRAME AT STA 500C IS CRACKED BETWEEN STR 8 AND 9 AT I/B HOLE FOR AC BIN RAIL SUPPORT BRACKET. REPAIRED RH FUSELAGE FRAME STA 500C BETWEEN STR 8 & 9 IAW DELTA TASK CARD 2526-01236-02B.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 74,172 hrs · 29,823 cycles

(LOG 0107242) RH FUSELAGE FRAME AT STA 907 IS CRACKED BETWEEN STA 8 & 9 AT I/B HOLE FOR AC RAIL BIN SUPPORT. REPAIRED RH FRAME STA 907 BETWEEN STR 8 & 9 IAW DELTA TASK CARD 2526-01236-03B

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 74,172 hrs · 29,823 cycles

(LOG 0107061) LH FUSELAGE FRAME STA 500D IS CRACKED AT THE I/B FASTENER HOLE FOR AC RAIL BRACKET BETWEEN STR 8 & 9. REPAIRED LH FUSELAGE FRAME STA 500D BETWEEN STR 8 & 9 IAW DELTA TASK CARD 2523-01236-02A.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 74,172 hrs · 29,823 cycles

(LOG 0107088) RH FUSELAGE FRAME STA 480 IS CRACKED AT THE I/B FASTENER HOLE FOR AC RAIL BRACKET BETWEEN STR 8 & 9. REPAIRED RH FUSELAGE FRAME STA 480 BETWEEN STR 8 & 9 IAW DELTA TASK CARD 2526-01236-02B.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 74,172 hrs · 29,823 cycles

(LOG 0107020) LH FUSELAGE FRAME STA 827 IS CRACKED AT THE I/B FASTENER HOLE FOR AC RAIL BRACKET BETWEEN STR 8 & 9. REPAIRED LH FUSELAGE FRAME STA 827 BETWEEN STR 8 & 9 IAW DELTA TASK CARD 2526-01236-02A.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 74,172 hrs · 29,823 cycles

(LOG 0107225) FWD WET AREA LH MOP SILL CORRODED. REMOVED & REPLACED L1 MOP SILL CHORD IAW BOEING 737-800 SRM 51-40-02.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 74,172 hrs · 29,823 cycles

(LOG 0107028) LH FUSELAGE FRAME STA 500A IS CRACKED AT THE I/B FASTENER HOLE FOR AC RAIL BRACKET BETWEEN STR 8 & 9. REPAIRED LH FUSELAGE FRAME STA 500A BETWEEN STR 8 & 9 IAW DELTA TASK CARD 2526-01236-02A.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 74,172 hrs · 29,823 cycles

(LOG 0107054) LH FUSELAGE FRAME STA 500C IS CRACKED AT THE I/B FASTENER HOLE FOR AC RAIL BRACKET BETWEEN STR 8 & 9. REPAIRED LH FUSELAGE FRAME STA 500C BETWEEN STR 8 & 9 IAW DELTA TASK CARD 2526-01236-02A.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 74,172 hrs · 29,823 cycles

(LOG 0107157) RH FUSELAGE FRAME AT STA 500D IS CRACKED BETWEEN STR 8 AND 9 AT I/B HOLE FOR AC BIN RAIL SUPPORT BRACKET. REPAIRED RH FUSELAGE FRAME STA 500D BETWEEN STR 8 & 9 IAW DELTA TASK CARD 2526-01236-02B.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 74,172 hrs · 29,823 cycles

(LOG 0107165) RH FUSELAGE FRAME CRACKED AT 727B BETWEEN STR 8 & 9 AT I/B HOLE FOR AC RAIL BIN SUPPORT. REPAIRED RH FUSELAGE FRAME STA 727B BETWEEN STR 8 & 9 IAW DELTA TASK CARD 2526-01236-02B.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 74,172 hrs · 29,823 cycles

(LOG 0107014) LH FUSELAGE FRAME STA 727B IS CRACKED AT THE I/B FASTENER HOLE FOR AC RAIL BRACKET BETWEEN STR 8 & 9. REPAIRED LH FUSELAGE FRAME STA 727B BETWEEN STR 8 & 9 IAW DELTA TASK CARD 2526-01236-02A.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 74,172 hrs · 29,823 cycles

(LOG 0107069) RH FUSELAGE FRAME STA 440 IS CRACKED AT THE I/B FASTENER HOLE FOR AC RAIL BRACKET BETWEEN STR 8 & 9. REPAIRED RH FUSELAGE FRAME STA 440 BETWEEN STR 8 & 9 IAW DELTA TASK CARD 2526-01236-02A.

Part: WEB — CORRODED (UNKNOWN) · corrosion level 2 · airframe 74,172 hrs · 29,823 cycles

(LOG 0104333) FWD CARGO DOOR CUTOUT THRESHOLD WEB IS CORRODED. REMOVED AND REPLACED WEB IAW BOEING 737-800 SRM 51-40-02.

Part: INTERCOSTAL — CRACKED (UNKNOWN) · airframe 74,172 hrs · 29,823 cycles

(LOG 0100882) FWD WET AREA INTERCOSTAL FS 312-328 LBL-45 CRACKED. REPLACED INTERCOSTAL AT FWD WET AREA FS 312-328 LBL 45 IAW B737-800 SRM 51-40-02-0G.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 74,172 hrs · 29,823 cycles

(LOG 0100878) FWD WET AREA FLOOR SUPPORT FS 312-328 LBL12 CORRODED. REPLACED DAMAGED INTERCOSTAL AT FWD WET AREA FS 312 TO 328 LBL 12 IAW B737-800 SRM 51-40-02-0G.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 74,172 hrs · 29,823 cycles

(LOG 0098150) FWD WET AREA FLOOR SUPPORT STA 294.5-312 RBL10 CORROSION ON UPPER SURFACE. REMOVED AND REPLACED DAMAGED INTERCOSTAL FLOOR SUPPORT STA 294.5-312 RBL10 IAW BOEING 737-800 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (UNKNOWN) · corrosion level 2 · airframe 74,172 hrs · 29,823 cycles

(LOG 0098134) FWD WET AREA FLOOR SUPPORT FS 328-344 LBL 10 CORRODED ON SURFACE. REMOVED & REPLACED DAMAGED INTERCOSTAL FLOOR SUPPORT STA 328-344 LBL 10 IAW BOEING 737-800 SRM 51-40-02.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 74,172 hrs · 29,823 cycles

(LOG 0097052) FWD WET AREA STA 277-294.5 BL0 INTERCOSTAL CRACKED. REMOVED AND REPLACED DAMAGED INTERCOSTAL STA 277-294.5 BL0 IAW BOEING 737-800 SRM 51-40-02.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 74,172 hrs · 29,823 cycles

(LOG 0095497) AFT CARGO AFT SHIELD CRACKED. REMOVED & REPLACED AFT CARGO AFT SHIELD IAW BOEING 737-800 SRM 51-40-02

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 74,172 hrs · 29,823 cycles

(LOG 0095450) FWD WET AREA INTERCOSTAL FS 277-294.5 RBL 43 CORROSION ON UPPER SURFACE NEXT TO GALLEY MOUNT. REMOVED AND REPLACED INTERCOSTAL FWD AREA FS 277-294.5 RBL 43 IAW BOEING 737-800 SRM 51-40-02.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 74,172 hrs · 29,823 cycles

(LOG 0093857) AFT CARGO FWD SHIELD PUNCTURED. REMOVED & REPLACED FWD SHIELD AFT PIT IAW BOEING 737-800 SRM 51-40-02-0G.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 74,172 hrs · 29,823 cycles

(LOG 0086315) AFT CARGO LH TRANSITION PLATE IS PUNCTURED BETWEEN STA 727G-727H. REPAIRED LH TRANSITION PLATE IAW BOEING 737-800 SRM 53-00-53-2R-5.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 74,123 hrs · 29,796 cycles

SHIP 3715 -MISC/DE- DUE TO LEFT ADIRU FAILURE AND LOSS OF CAPTAIN'S FLIGHT DATA. CORRECTIVE ACTION: REPLACED LEFT ADIRU. OPS CHECKS GOOD. (LP 9136494)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 73,731 hrs · 29,614 cycles

(LOG 2954285) CAPTAINS UPPER O/B CORNER OF WINDOW FRAME IS CRACKED. REPAIRED PER PRI 611573-14 REV 1 AND ER/A 611573-14 REV ORIGINAL.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 73,731 hrs · 29,614 cycles

(LOG 2941297) CRACK FOUND IN THE LH #1 WINDOW FRAME IN FLIGHT COMPARTMENT. MAINTENANCE REPAIRED PER ERA 611573-14.

Part: BATTERY PACK — INOPERATIVE (UNKNOWN) · airframe 73,728 hrs · 29,610 cycles

(LOG 4624613) EMERGENCY EXIT SIGNS AT 1L DOOR INOP. REMOVED AND REPLACED POWER SUPPLY AND BATTERY PER B737 AMM 33-51-06. TESTS GOOD OK FOR SVC.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 73,146 hrs · 29,352 cycles

SHIP 3715 -DIV/PRESS- DIVERTED TO AUS DUE TO CABIN ALTITUDE CLIMBING TO 10,000FT. CREW DONNED O2 MASKS, DECLARED EMERGENCY AND DESCENDED TO FL100. UNABLE TO MAKE ATL WITH FUEL ON BOARD. CORRECTIVE ACTION: PERFORMED CPC 1-2 BITE TEST IAW B737 AMM. PERFORMED CABIN ZONE TEMP CONTROLLER BITE. NO TROUBLE FOUND. OPS CHECKS GOOD.

Part: BATTERY PACK — INOPERATIVE · airframe 73,062 hrs · 29,304 cycles

(LOG 4110264) DURING INSPECTION FOUND EMERGENCY AISLE LIGHTS FOR FIRST CLASS SEATS AND EMERGENCY LIGHT FOR R1 DOOR INOP. REMOVED AND REPLACED FWD R/H EMERGENCY BATTERY PACK REF. B737 AMM 33-51. OPS CHECK GOOD.

Part: BATTERY PACK — INOPERATIVE · airframe 72,881 hrs · 29,210 cycles

(LOG 9499574) DURING INSPECTION FOUND ALL COMFORT PLUS SEAT EMERGENCY LIGHTS INOP (ESCAPE PATH LIGHTING). REMOVED AND REPLACED COMFORT PLUS SEAT EMERGENCY ESCAPE PATH LIGHTING BATTERY PACK PER B737 AMM 33-51. ALL CHECKS GOOD.

Part: BATTERY PACK — INOPERATIVE · airframe 72,830 hrs · 29,176 cycles

(LOG 9499514) DURING INSPECTION FOUND RT HAND ROWS 23-33 & R2 DOOR EMERGENCY LIGHTS INOP. R/R AFT GALLEY BATTERY PACK (M1672) IAW B737 AMM 33-51. ALL EMERGENCY LIGHTS OPERATE NMLY. A/C OK FOR SVC.

Part: CHARGER — INOPERATIVE · airframe 71,749 hrs · 28,725 cycles

(LOG 9576220) DURING INSPECTION FOUND 4R LIGHTED EXIT SIGN INOP. R/R AFT RT CHARGER ASSY (M1672) IAW B737 AMM 33-51.

Part: LIGHT — BROKEN · airframe 70,251 hrs · 28,049 cycles

(LOG 8738990) DURING INSPECTION FOUND MID CABIN EMERGENCY EXIT LIGHT ON CEILING BROKEN. SECURED SIGN MOUNT REINSTALLED AFT EXIT LENS OK FOR CONT SVC.

Part: HOUSING — DAMAGED · airframe 70,251 hrs · 28,049 cycles

(LOG 2206238) INSPECTED MID CABIN EMERGENCY EXIT LIGHT PER B737 AMM 33-51. EXIT LIGHT HOUSING ASSY NEEDS REPLACED. FOUND DAMAGE ON EMERGENCY EXIT SIGN. R/R EMERGENCY SIGN PER B737 AMM 33-15. OK FOR SVC.

Part: BATTERY PACK — INOPERATIVE · airframe 68,714 hrs · 27,342 cycles

(LOG 8063809) DURING INSPECTION FOUND LEFT AFT EXTERNAL EMER LIGHT INOP. REPLACED BATTERY PACK FOR LEFT AFT EXTERNAL EMER LIGHT PER B737 AMM 33-51. OPS CK OK.

Part: SIGN — DETACHED (EMERGENCY LIGHTS) · airframe 68,472 hrs · 27,231 cycles

(LOG 1916518) DURING INSPECTION FOUND EMERGENCY EXIT SIGNS INOPERATIVE. REATTACHED SIGN.

Part: GROUND WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 68,348 hrs · 27,175 cycles

DURING INSPECTION FOUND SEAT 11D EMERGENCY LIGHT OUT. FOUND GROUND WIRE BROKEN UNDER SEAT 11E. SPLICED GROUND WIRE. REFERENCE B737 SWPM 20-30-00. OPS CHECK OK.

Part: GUST LOCK — MALFUNCTIONED (PAX DOOR) · airframe 67,882 hrs · 26,971 cycles

(LOG 7823822) FA REPORTS DOOR DIFFICULT TO OPEN AFTER LANDING. TOOK SEVERAL ATTEMPTS TO OPEN. REPLACED ASSOCIATED L1 DOOR GUST LOCK HARD WARE. PER B737 AMM 52-11. DOOR OPERATES SMOOTHLY. OK FOR SVC.

Part: OIL COOLER — LEAKING (APU) · airframe 67,331 hrs · 26,768 cycles

(LOG 4823792) STRONG ODER OF WET SOCK AFTER LANDING WHICH PERSISTED FOR SEVERAL MINUTES. FOUND APU OIL COOLER LEAKING. REM/RPLCD SAME AND CLEANED PLENUM PER 737 MM 49-91.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 67,282 hrs · 26,749 cycles

(LOG 4823769) DURING TESTING FOUND EMERGENCY EXIT SIGN ABOVE LEFT OVERWING EXIT DOORS DO NOT ILLUMINATE. REPLACED BATTERY PACK M01694 PER B737 AMM 33-51 , OPS CKS GOOD.

Part: ACCESS DOOR — CRACKED (GROUND POWER) · airframe 66,340 hrs · 26,329 cycles

DURING INSPECTION FOUND CRACK ON FWD FUSELAGE CUTOUT OF EXTERNAL POWER RECEPTACLE ACCESS DOOR NBR 114AR. POWER RECEPTACLE WAS REPAIRED, PER ETI-37-20-342 REV 3 AND ERA 094569-14.

Part: SUPPORT — DAMAGED (BS 727) · airframe 66,340 hrs · 26,329 cycles

DURING INSPECTION FOUND ELONGATED HOLES ON FAIRING SUPPORT STRUCTURE STA BS 727+2.7 BL 0 TO LBL 15 AT BODY FAIRING. ELONGATED HOLES ON FAIRING SUPPORT STRUCTURE STA BS 727+2.7 LBL 0 TO LBL 15 AT BODY FAIRING WAS REPAIRED, PER ETI-37-20-347 REV ORIGINAL AND ERA 588405-14AD REV ORIGINAL.

Part: SUPPORT — DAMAGED (BS 727C) · corrosion level 2 · airframe 66,340 hrs · 26,329 cycles

DURING INSPECTION FOUND CORROSION ON FAIRINGS SUPPORTS STRUCTURE STATION BS 727C BETWEEN LBL 0 TO LBL 10 ALSO RBL 0 TO RBL 10 AT BODY FAIRING. BODY FAIRING WERE REPAIRED, PER ETI-37-20-347 REV ORIGINAL AND ERA 588405-14AD REV ORIGINAL.

Part: SUPPORT — DAMAGED (BS 727) · airframe 66,340 hrs · 26,329 cycles

DURING INSPECTION FOUND ELONGATED HOLES ON FAIRING SUPPORT STRUCTURE STA BS 727+2.7 BL 0 TO RBL 15 AT BODY FAIRING. ELONGATED HOLES ON FAIRING SUPPORT STRUCTURE STA BS 727+2.7 RBL 0 TO RBL 15 AT BODY FAIRING WERE REPAIRED, PER ETI-37-20-347 REV ORIGINAL AND ERA 588405-14AD.

Part: ACCESS DOOR — DAMAGED (GROUND POWER) · airframe 66,340 hrs · 26,329 cycles

THE AFT EDGE OF THE GROUND POWER ACCESS DOOR CUTOUT SURROUND DOUBLER IS DAMAGED AT THE AFT, CENTER LATCH LAND SURFACE. THE EDGE IS MISSING A PIECE APPROXIMATELY 1.0 LONG THROUGH THE LOWER ATTACH FASTENER FOR THE LAND SURFACE WEAR PLATE. MAINTENANCE REPAIRED DAMAGE, PER ERA 094569-14.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 66,000 hrs · 26,164 cycles

DURING INSPECTION FOUND AFT LT SECTION OF EMERGENCY LIGHTS AROUND L2 DOOR AND ABOVE AFT LEFT SEATS IS INOPERATIVE. REMOVED AND REPLACED BATTERY PACK IN AFT CEILING LT SIDE. OPS CHECK GOOD PER B737.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 65,916 hrs · 26,111 cycles

DURING INSPECTION, FOUND EMERGENCY LIGHTS INOPERATIVE AT DELTA COMFORT SECTION. REPLACED BATTERY PACK AT SEAT ROW 11DEF PER AMM 33-51-06. OPS CKS GOOD.

Part: LIGHT — INOPERATIVE (EMERGENCY EXIT) · airframe 61,786 hrs · 24,357 cycles

(LOG 0840142) DURING INSPECTION FOUND EMERGENCY EXIT SIGNS INOPERATIVE. IN STALLED ROBBED LIGHT ASSY FROM A/C 3742 PER B737 AMM 33-51. OPS CHECK GOOD.

Part: LIGHT — ODOR (CABIN) · airframe 61,646 hrs · 24,290 cycles

AT CRUISE AND AFTER GOING THROUGH BRIEF LIGHT AND MODERATE CHOP, THE F/A'S NOTICED AN ACRID ELECTRICAL SMELL NEAR SEATS 16 DEF. AFTER THEY TURNED OFF THE CEILING LIGHT NIGHT MODE THE SMELL WENT AWAY NO SMOKE WAS EVER SEEN. MAINTENANCE REPLACED LIGHT ASSY AT SEAT 16 DEF CEILING LIGHT PER MM 33-22.

Part: PUMP — SPLIT (HYD SYSTEM) · airframe 60,296 hrs · 23,772 cycles

DURING FLIGHT, THE AIRCRAFT EXPERIENCED AN -A- HYDRAULIC SYSTEM LOSS OF QUANTITY. CREW PERFORMED QRH, DECLARED EMERGENCY AND UTILIZED THE ALTERNATE GEAR EXTENSION. MAINTENANCE FOUND THE ACMP CASE SPLIT IN THE LEFT WHEEL WELL. REPLACED HYDRAULIC PUMP, ENGINE DEMAND PUMP AND CASE DRAIN FILTERS. OPS CHECKED NORMAL, NO LEAKS NOTED, AIRCRAFT RETURNED TO SERVICE.

Part: SLAT SYSTEM — MALFUNCTIONED · airframe 59,021 hrs · 23,285 cycles

LE FLAPS TRANST LIGHT ILLUMINATED WITH FLAPS AT 2 AND 5, LIGHT EXTINGUISHES ONCE FLAPS SET TO 10. HYDRAULIC SYSTEM B REQUIRES RF. SERVICED HYD IAW AMM 12-12 PSU TESTED OK WITH NO FAULTS IAW AMM 32-09. FSEU BITE CHECKED. NO FAULTS IAW AMM 27-51. INSPECTED LE SLAT AND FLAPS, ALL OK. CYCLED NUMEROUS TIMES,ALL OK. REMOVED NR 8 SLAT ACTUATOR IAW AMM 27-81. INSTALLED THE L/E SLAT ACTUATOR IAW AMM 27-81-41 910423. COMPLIED WITH WIRING CHECKS IAW WDM 27-81-22. NO TROUBLE FOUND. NO FAULTS ON FSEU IAW IAW FIM 27-51.

Part: FRAME — DENTED (BS 727F) · airframe 58,975 hrs · 23,267 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: BULKHEAD WEB — CRACKED (BS 663) · airframe 58,659 hrs · 23,140 cycles

DURING INSPECTION, FOUND A CRACKED UPPER WEB ON THE BS 663 BULKHEAD, RBL 35. MAINTENANCE REPAIRED THE BULKHEAD WEB IAW SRM 57-10-10, FIGURE 203, REPAIR 3.

Part: BULKHEAD WEB — CRACKED (BS 663) · airframe 58,659 hrs · 23,140 cycles

DURING INSPECTION, FOUND A CRACKED UPPER WEB ON THE BS 663 BULKHEAD WEB, RBL 35. MAINTENANCE REPAIRED THE BULKHEAD WEB IAW SRM 57-10-10, FIGURE 203, REPAIR 3.

Part: BULKHEAD WEB — CRACKED (BS 663) · airframe 58,659 hrs · 23,140 cycles

DURING INSPECTION, FOUND A CRACKED UPPER WEB ON THE BS 663 BULKHEAD WEB, RBL 35. MAINTENANCE REPAIRED THE BULKHEAD WEB IAW SRM 57-10-10, FIGURE 203, REPAIR 3.

Part: BULKHEAD WEB — CRACKED (BS 663) · airframe 58,659 hrs · 23,140 cycles

DURING INSPECTION, FOUND A CRACKED UPPER WEB ON THE BS 663 BULKHEAD, RBL 35. MAINTENANCE REPAIRED THE BULKHEAD IAW SRM 57-10-10, FIGURE 203, REPAIR 3.

Part: BRACKET — CORRODED · airframe 58,438 hrs · 23,072 cycles

(LOG 0319114) DURING INSPECTION FOUND CORROSION ON BRACKETS MIDDLE SECTION OF GALLEY 2. MAINTENANCE FABRICATEDGALLEY 2 BRACKETS PER ERA 562384-14 REV. ORIGINAL AND ETI-37-17-337 REV ORIGINAL.

Part: BRACKET — CORRODED · airframe 58,438 hrs · 23,072 cycles

(LOG 0319091) DURING INSPECTION FOUND CORROSION ON BRACKETS AT MID SECTION OF GALLEY 4. MAINTENANCE REPLACED BRACKETS PER ERA 562390-14 REV. ORIGINAL AND ETI-37-17-338 REV. ORIGINAL.

Part: FLOOR SUPPORT — CORRODED (BS 927-992.8) · airframe 58,436 hrs · 23,071 cycles

DURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT BETWEEN BS 927 TO 992.8. MAINTENANCE REPAIRED THE FLOOR SUPPORT IAW ERA 562411-14, REV ORIG. AND ETI-37-17-344, REV 4.

Part: FLOOR SUPPORT — CORRODED (BS 927-992.8) · airframe 58,436 hrs · 23,071 cycles

DURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT BETWEEN BS 927 TO 992.8. REPAIRED IAW ERA 562413-14, REV ORIG. AND ETI-37-17-346, REV 2.

Part: FLOOR SUPPORT — CORRODED (AFT CARGO) · airframe 58,436 hrs · 23,071 cycles

DURING INSPECTION, FOUND CORROSION ON THE FLOOR SUPPORT FROM BS 727 TO 947 IN THE AFT CARGO BAY. REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (BS 951-992) · airframe 58,436 hrs · 23,071 cycles

DURING AN H CHECK, CORROSION WAS FOUND ON THE LOWER FLOOR SUPPORT, AT RBL 48 AND BS 951 -992.8. REPAIRED IAW ERA 562413-14.

Part: FLOORBEAM — CORRODED (BS 986.5) · airframe 58,436 hrs · 23,071 cycles

DURING INSPECTION FOUND CORROSION ON THE FLOORBEAM PREVIOUS REPAIR, BS 986.5 BETWEEN RBL18 TO RBL45 AND LBL 31 TO LBL 45. MAINTENANCE REPAIRED THE FLOORBEAM IAW ER/A 562381-14, REV ORIG, AND ETI-37-17-335, REV 3.

Part: FLOOR SUPPORT — CRACKED (BS 922-967) · airframe 58,436 hrs · 23,071 cycles

DURING AN H CHECK, CORROSION AND A CRACK WERE FOUND ON THE LOWER MAIN FLOOR SUPPORT AT LBL 48, BETWEEN BS 922 - 967. REPAIRED IAW ERA 562.

Part: PLATE — CORRODED (BS 727-947) · airframe 58,436 hrs · 23,071 cycles

DURING INSPECTION, FOUND CORROSION ON THE LT SIDEPLATE BETWEEN BS 727 & 947, LBL 20 IN THE AFT CARGO BAY. MAINTENANCE REPLACED THE SIDE PLATE IAW SRM 51-40-02.

Part: WEB — CORRODED (LT NACELLE) · airframe 58,436 hrs · 23,071 cycles

DURING INSPECTION, FOUND CORROSION ON THE LOWER WEB AT THE LT ENGINE STRUT AFT FAIRING STRUCTURE. MAINTENANCE REPLACED WEB IAW SRM 51-40-02, PAR 7.

Part: BULKHEAD — CANNING (FUSELAGE) · airframe 58,436 hrs · 23,071 cycles

DURING INSPECTION FOUND OIL-CAN CONDITION ON AFT PRESSURE BULKHEAD, BTW 9 TO 10 O'CLOCK POSITION. (S-10L TO S-12L). MAINTENANCE REPAIRED PER ETI-37-17-340 REV 2 AND ER/A 562402-14AD.

Part: VAPOR BARRIER — CRACKED (RT MLG WW) · airframe 58,436 hrs · 23,071 cycles

DURING INSPECTION FOUND CRACKED RT VAPOR BARRIER BAY NR 2 AND NR 8 AT RT MLG WHEEL WELL. MAINTENANCE REPAIRED PER SRM 57-10-10 REPAIR 2.

Part: BULKHEAD — CANNING (FUSELAGE) · airframe 58,436 hrs · 23,071 cycles

DURING INSPECTION FOUND FUSELAGE MAIN FRAME BULKHEAD AT AFT BULKHEAD WEB, STATION 1016 OIL CANING. MAINTENANCE REPAIRED PER ERA 562402-14.

Part: PLATE — CORRODED (FUSELAGE) · airframe 58,436 hrs · 23,071 cycles

DURING INSPECTION FOUND CORROSION ON RT SIDEPLATE BTW STATION 727 AND 767 RBL 20 AT AFT CARGO COMP. MAINTENANCE REPLACED RT SIDEPLATE BTW STATION 727 AND 767 RBL 20 WAS REPLACED PER SRM 53-00-53 FIG 202 AND SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 58,436 hrs · 23,071 cycles

DURING INSPECTION FOUND CORROSION ON LT/RT "Z" FLOOR SUPPORTS AT FWD CARGO COMPARTMENT. MAINTENANCE REPLACED FLOOR SUPPORTS SIDE PLATE LT AND RT PER SRM 53-00-53.

Part: LATCH — CORRODED (LAV SERVICE PNL) · airframe 58,436 hrs · 23,071 cycles

DURING INSPECTION FOUND CORROSION ON DOOR LATCH OF LAVATORY SERVICE PANEL. MAINTENANCE REPLACED LATCH PER SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 58,436 hrs · 23,071 cycles

DURING INSPECTION FOUND CORROSION ON LT/RT "Z" FLOOR SUPPORTS AT FWD CARGO COMPARTMENT. MAINTENANCE REPLACED FLOOR SUPPORTS SIDE PLATE PER 51-40-02.

Part: WEB — CORRODED (FUSELAGE) · airframe 58,436 hrs · 23,071 cycles

DURING INSPECTION FOUND CORROSION ON WEB FLOOR BTW STATION 217 TO 219 AND LBL 11 AND LBL 14 AT COCKPIT. MAINTENANCE REPAIRED PER SRM 53-10-51.

Part: FLOORBEAM — CORRODED (BS 947.5) · airframe 58,436 hrs · 23,071 cycles

DURING INSPECTION, FOUND CORROSION ON THE FLOORBEAM BS 947.5 BETWEEN RBL 44 & 48. MAINTENANCE REPAIRED THE FLOORBEAM IAW SRM 53-70-51, FIG 206, REPAIR 5.

Part: FLOOR SUPPORT — CRACKED (BS 277-294) · airframe 58,436 hrs · 23,071 cycles

DURING INSPECTION, FOUND A CRACKED FLOOR SUPPORT BETWEEN BS 277 TO 294, BL 0. MAINTENANCE REPLACED THE FLOOR SUPPORT IAW SRM 53-10-51.

Part: DOOR FRAME — CRACKED (SERVICE DOOR) · airframe 58,436 hrs · 23,071 cycles

DURING INSPECTION, FOUND A CRACK ON THE FWD DOOR FRAME BS 294.5, RBL 55. MAINTENANCE REPAIRED THE DOOR FRAME IAW ER/A 562377-14, REV ORIGINAL, AND ETI -37-17-334, REV 1.

Part: WEB — CORRODED (BS 986-992) · airframe 58,436 hrs · 23,071 cycles

DURING INSPECTION, FOUND CORROSION ON THE FLOOR WEB BETWEEN BS 986.5 & 992.8, LBL45 TO LBL 46. MAINTENANCE REPLACED THE WEB IAW SRM 51-40-02, PAR 4, 7, AND DWG 147A5712, REV F.

Part: FLOOR SUPPORT — CORRODED (BS 947-967) · airframe 58,436 hrs · 23,071 cycles

DURING INSPECTION FOUND CORROSION ON FLOOR SUPPORT BETWEEN BS 947.5 - 967, RBL 46. REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02, PAR 4, AND 7.

Part: BULKHEAD — CRACKED (LT MLG WW) · airframe 58,436 hrs · 23,071 cycles

DURING INSPECTION FOUND CRACKED UPPER WEB (1 EA) ON WING CENTER SECTION (BULKHEAD) STATION 663 LBL 35 Z -6 AT LT MLG WHEEL WELL. MAINTENANCE REPAIRED PER SRM 57-10-10 FIGURE 203 REPAIR 3.

Part: BULKHEAD — CRACKED (RT MLG WW) · airframe 58,436 hrs · 23,071 cycles

DURING INSPECTION FOUND CRACKED UPPER WEB (1 EA) ON WING CENTER SECTION (BULKHEAD) STATION 663 RBL 35 Z -6 AT RT MLG WHEEL WELL. MAINTENANCE REPAIRED PER SRM 57-10-10 FIGURE 203 REPAIR 3.

Part: FITTING — CORRODED (FUSELAGE) · airframe 58,436 hrs · 23,071 cycles

DURING INSPECTION FOUND CORROSION ON FLOOR FITTING, AT STA 344 LBL-60. MAINTENANCE REPLACED FITTING PER SRM 51-40-02.

Part: BULKHEAD WEB — CRACKED (BS 663) · airframe 58,436 hrs · 23,071 cycles

CRACKED UPPER BULKHEAD WEB BS 663, LBL 35. THE AREA WAS REPAIRED IAW SRM 57-10-10, FIGURE 203, REPAIR 3, ALTERNATIVE 1.

Part: BULKHEAD WEB — CRACKED (BS 663) · airframe 58,436 hrs · 23,071 cycles

CRACKED UPPER BULKHEAD WEB BS 663, RBL 35. THE BULKHEAD WEB WAS REPAIRED IAW SRM 57-10-10, FIGURE 203, REPAIR 3, ALTERNATIVE 1.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 58,436 hrs · 23,071 cycles

DURING INSPECTION, FOUND A CRACK ON A PRODUCTION DOUBLER CUTOUT OF EXTERNAL POWER RECEPTABLE. REPAIRED IAW SRM 53-10-15 REP.4

Part: FLOOR SUPPORT — CRACKED (BS 312-328) · airframe 58,436 hrs · 23,071 cycles

DURING INSPECTION, FOUND A CRACKED FLOOR SUPPORT BS 312 - 328, LBL 46. MAINTENANCE REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 56,944 hrs · 22,545 cycles

DURING INSPECTION FOUND R1 AND L1 EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED L1 EMERGENCY POWER SUPPLY AND BATTERY PACK AND REPLACED, REMOVED R1 BATTERY PACK AND REPLACED IAW AMM 33-51-06. OPS CHECK OK.

Part: SEAT TRACK — CORRODED (BS 709) · airframe 51,059 hrs · 20,582 cycles

DURING INSPECTION FOUND PASSENGER CABIN FLOOR STRUCTURE, LT SIDE OTBD SEAT TRACK HAS CORROSION ON TOP OF CROWN AND IN BOTTOM OF CROWN CHANNEL, BS 709+9". MAINTENANCE REPAIRED PASSENGER CABIN FLOOR STRUCTURE LT SIDE OTBD SEAT TRACK ON TOP OF CROWN AND IN BOTTOM OF CROWN CHANNEL BS 706+9" IAW SRM 53-00-52, REPAIR 3.

Part: SEAT TRACK — WORN · airframe 51,059 hrs · 20,582 cycles

DURING INSPECTION FOUND PASSENGER CABIN SEAT TRACK AT LBL 24 HAS WEAR ON CROWN. MAINTENANCE FABRICATED AND INSTALLED NEW -1 REPAIR SEAT TRACK IAW SRM 53-00-52, REPAIR 4.

Part: SEAT TRACK — WORN · airframe 51,059 hrs · 20,582 cycles

DURING INSPECTION FOUND PASSENGER CABIN SEAT TRACK AT RBL 45 HAS WEAR ON CROWN. MAINTENANCE FABRICATED & INSTALLED -1, REPAIR SEAT AND -2 REPAIR CHANNEL IAW SRM 53-00-52, REPAIR 4.

Part: BOOT — UNSECURE (APU BLEED DUCT) · airframe 50,279 hrs · 20,327 cycles

ON LANDING DESCENT AT 37K, AS THROTTLES WENT TO IDLE, THE CABIN ALTITUDE HORN SOUNDED AT 10,000 FEET. CREW DECLARED AN EMERGENCY, DESCENDED RAPIDLY AND CABIN STAYED AT 10,000 FEET TILL LEVEL. MAINTENANCE FOUND APU BLEED DUCT RUBBER BOOT LOOSE. SECURED AND TESTED IAW AMM 05-51-91-790-801. PRESSURIZATION SATISFACTORY, ACFT RETURNED TO SERVICE.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 47,510 hrs · 19,362 cycles

DURING TESTING, FOUND BATTERY PACK M1672 FAILED EMERGENCY LIGHTS CAPACITY TEST. MAINTENANCE REPLACED BATTERY PACK IAW AMM 33-51-06. OPS CHECKED OK.

Part: CLAMP — UNSECURE (FLEX DUCT) · airframe 46,836 hrs · 19,148 cycles

DURING FLIGHT AT FL 370, CREW WAS UNABLE TO MAINTAIN CABIN PRESSURE IN AUTO/MANUAL. DECLARED AN EMERGENCY, DESCENDED TO 10,000 FT FROM FL370 AND DIVERTED. MAINTENANCE PERFORMED PRESSURIZATION LEAK CHECK. BOTH CONTROLLERS LISTED "LO INFL/HI LEAK RATE CODES. FOUND AFT P-DOME FLEX DUCT CLAMP NOT SECURED. REPLACED CLAMP. PERFORMED CABIN PRESSURE LEAK TEST IAW AMM. CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: FASTENER — NOT REPORTED (SEAT TRACK) · airframe 44,102 hrs · 18,169 cycles

FUSELAGE SEAT TRACKS FASTENERS, REPAIRED IAW 5321-01065.

Part: UNKNOWN — CRACKED · airframe 44,102 hrs · 18,169 cycles

DURING INSPECTION, FOUND FWD INBD HOLE HAS CRACK INDICATION, RBL 45.5. MX REPAIRED IAW ERA 519357-14, REV O.

Part: UNKNOWN — CRACKED · airframe 44,102 hrs · 18,169 cycles

DURING INSPECTION, FOUND INBD FWD BOLT HOLE AND BOTH OTBD BOLT HOLES SHOW CRACK INDICATION AT LBL 24.75. MX REPAIRED IAW ERA 519357-14, REV O.

Part: UNKNOWN — CRACKED · airframe 44,102 hrs · 18,169 cycles

DURING INSPECTION, FOUND OTBD AFT BOLT HOLE SHOWS CRACK INDICATION AT LBL 45.5. MX REPAIRED IAW ERA 519357-14, REV O.

Part: LIGHT — INOPERATIVE (R1 DOOR) · airframe 41,633 hrs · 17,264 cycles

DURING INSPECTION, FOUND DOOR 1R EMERGENCY LIGHT INOPERATIVE. MX REPLACED DOOR 1R EMERGENCY LIGHT IAW AMM 33-51. OPS CHECK OK.

Part: WIRE HARNESS — DAMAGED (EMERGENCY LIGHT) · airframe 41,597 hrs · 17,252 cycles

EMERGENCY LIGHTS TEST, FOUND SEATS 11 AND 28 LIGHTS INOPERATIVE. MX REPLACED HARNESSES. OPS CHECKED NORMAL.

Part: LANYARD — DETACHED (R1 DOOR SLIDE) · airframe 41,258 hrs · 17,133 cycles

DURING PUSHBACK FOUND RT FORWARD DOOR SLIDE PACK LANYARD NOT ATTACHED. MX RESECURED DOOR 1R SLIDE ROLL PIN IN DOOR SLIDE. ACFT RETURNED TO SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 40,996 hrs · 17,050 cycles

DURING TESTING FOUND EMERGENCY LIGHT BATTERY PACKS M1673, M1674 AND M1695 FAILED. MX REPLACED M1673, M1674, M1695 BATTERY PACKS. OPS CHECKED OK.

Part: STRINGER — DAMAGED (BS 1040 S25L) · airframe 40,926 hrs · 17,015 cycles

DURING INSPECTION, FOUND STRINGER 25L AT BS 1040 AND BRACKET FOR APU BLEED AIR DUCT DAMAGED. MX R & R DAMAGED SECTION OF STRINGER IAW ERA 508442-14.

Part: VALVE — OUT OF LIMITS (BLEED SYS) · airframe 40,924 hrs · 17,014 cycles

DURING FLIGHT AT 36,000 FT, ACFT EXPERIENCED CABIN HORN LEFT BLEED TRIP OFF LIGHT. CREW PERFORMED QRH PROD RUN, TRIP RESET DID NOT CLEAR PROBLEM. PERFORMED EMERGENCY DECENT AND DIVERTED. MX PERFORMED PNEUMATIC HEALTH CHECK ON LT ENGINE. FOUND PRECOOLER VALVE OUT OF SPEC AND HIGH STAGE BLEED HOSE LEAKING. REPLACED PRECOOLER VALVE AND HIGH STAGE HOSE. LEAK CHECK OK, AIRCRAFT RETURNED TO SERVICE.

Part: WIRE HARNESS — DISCONNECTED (EMERGENCY LIGHT) · airframe 39,306 hrs · 16,439 cycles

DURING EMERGENCY LIGHT TEST FOUND SEAT 24 DEF PATH LIGHT INOPERATIVE. RECONNECTED WIRE HARNESS AND TESTED GOOD.

Part: FRAME — CRACKED (FUSELAGE) · airframe 37,491 hrs · 15,790 cycles

STA 380 RT FRAME CRACKED AT INBD STRINGER 8. REPAIRED PER ERA 494564-14.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 37,491 hrs · 15,790 cycles

STA 400 STRINGER 8 RT CRACKED. REPAIRED PER ERA 494564-14.

Part: FRAME — CRACKED (FUSELAGE) · airframe 37,491 hrs · 15,790 cycles

STA 480 FRAME CRACKED AT STRINGER 8 LT. REPAIRED PER ERA 494564-14.

Part: FRAME — CRACKED (FUSELAGE) · airframe 37,491 hrs · 15,790 cycles

PASSENGER CABIN FUSELAGE FRAME AT STA 440 LT HAS CRACK AT INBD RIVET HOLE AT AT PSU ATTACH CLIP STRINGER. REPAIRED PER ERA 494564-14.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 37,491 hrs · 15,790 cycles

STA 380 STRINGER 8 LT CRACKED. REPAIRED PER ERA 494564-14.

Part: FRAME — CRACKED (FUSELAGE) · airframe 37,491 hrs · 15,790 cycles

STA 400 LT FRAME CRACKED AT STRINGER 8. REPAIRED PER ERA 494564-14.

Part: UNKNOWN — ODOR (LAVATORY) · airframe 36,665 hrs · 15,460 cycles

A/C 3715 FLT 1002 SLC-JFK: AFT RIGHT LAVATORY SMOKE DETECTOR WENT OFF AND FLIGHT ATTENDANT REPORTED HOT METAL/BURNING ODOR. FUME DISSIPATED AND REOCCURRED MULTIPLE TIMES. PASSENGER IN LAVATORY AT INITIAL DETECTOR SOUNDING. FLIGHT DIVERTED INTO OMA, LANDING UNEVENTFULLY. TROUBLESHOT PER FIM, UNABLE TO DUPLICATE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 35,208 hrs · 14,891 cycles

DURING MX CHECK OF EMERGENCY EGRESS LIGHTING, FOUND RT WING EXTERIOR SLIDE LIGHTS AND AISLE ROW 24DEF, INOPERATIVE. RE-LAMPED RT WING EXTERIOR EGRESS LIGHTS (LOG 760524004), AND REPLACED SEAT HARNESS AT ROW 24.

Part: SHUTOFF VALVE — MALFUNCTIONED (NR 2 BLEED) · airframe 34,359 hrs · 14,566 cycles

THE NR 2 ENGINE BLEED TRIPPED AT 39,000 FT. THE CABIN CLIMBED TO ABOVE 10,000 FT WITH AN INTERMITTENT CABIN ALTITUDE WARNING HORN SOUNDING. CREW EXECUTED AN EMERGENCY DESCENT, COMPLIED WITH QRH PROCEDURES, AND CONTINUED TO DESTINATION. MX REPLACED THE NR2 ENGINE PRSOV AND FUNCTIONALLY CHECKED THE SYS.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 34,277 hrs · 14,531 cycles

A/C CONTACTED THE JET TUG DURING PUSHBACK IN SEA. NEAR FS 190 JUST FWD OF THE FWD E/E DOOR. C/W PERM REPAIR PER ERA 486916-1A REV A. (DL738102997)

Part: SKIN — DAMAGED (FUSELAGE) · airframe 34,248 hrs · 14,522 cycles

DURING OPS IN SEA THE A/C IMPACTED A PUSHBACK TUG NEAR STA 190 AND BL 0. THE CONTACT RESULTED IN THREE DAMAGE LOCATIONS ON THE SKIN. REPAIRED PER ERA 486916-14. (DL738102995)

Part: BULKHEAD — CRACKED (LT MLG WW) · airframe 33,585 hrs · 14,246 cycles

AT PSV FOUND LEFT WHEEL WELL BULKHEAD CRACKED AT PACK EXHAUST DUCT. REPAIRED AS SPECIFIED IN APB SRM 57-10-10 REPAIR 2 (DL738102022).

Part: FCU — MALFUNCTIONED (TE FLAPS) · airframe 14,033 hrs · 6,731 cycles

LE FLAP TRANSIT LIGHT AMBERON FLAP RETRACT DURING TAKEOFF/ DEPARTURE. LE SLATS 2, 3 AMBER ILLUMINATED. AFTER CYCLING FLAPS TO 1 AND BACK TO UP IAW CHK LIST, LE SLATS 2,3 6 AND 7 TURNED AMBER. RETURNED FLAPS 15 FOR LANDING. 225 KNOTS MAX AIRSPEED DURING FLIGHT. FSEU FAULTED MULTIPLE PROX (MSG 27-81224). RAN ALT FLAPS/ SLATS TO EVEN SLATS. CLEARED FSEU. RAN FLAPS SLATS MULTIPLE TIMES WITH ALL INDICATIONS AND MOVEMENTS NORMAL. INTERMITTENT FAULT IAW M/M.