N384DA

Part: FLAP SYSTEM — FALSE INDICATION · airframe 78,675 hrs · 31,681 cycles

SHIP 3714 FCNT/DE DECLARED EMERGENCY DUE TO FLAP LOCKOUT ON APPROACH MEX. PERFORMED FSEU BITE CHECK. NO FAULTS. OPERATED FLAPS SEVERAL CYCLES. OPS CHECK GOOD.

Part: BATTERY PACK — NO TEST (ZONE 200) · airframe 78,258 hrs · 31,479 cycles

(LOG 7385044) DURING SERVICE CHECK FOUND CABIN EMERGENCY LIGHTS ON R1 DOOR AND RIGHT SIDE 1-4 ROWS INOP. R/R BATTERY PACK PER B737 AMM 33-51. EMERGENCY LIGHTS OPS CHECK GOOD.

Part: FLAP SYSTEM — LOCKED · airframe 78,193 hrs · 31,437 cycles

SHIP 3714 -UFC/DE- DECLARED EMERGENCY DUE TO FLAP LOCKOUT ON APPROACH TO LAND. CORRECTIVE ACTION: REPLACED FSEU. LUBRICATED #1 FLAP ROLLER. AHM REPORT SHOWS #4 SKEW SENSOR INVALID. REPLACED #4 AND #7 SKEW SENSORS. OPS CHECK GOOD.

Part: RECEIVER — OUT OF ADJUST (ZONE 800) · airframe 77,890 hrs · 31,303 cycles

(LOG 6402398) L1 DOOR WILL NOT CLOSE / LATCH. ADJUSTED UPPER 2 RECEIVER'S 2 TEETH AND LOWER 2 RECEIVER'S 1 TOOTH, IN AN ALL 4. DOOR OP CK'S GOOD. ALL PER B737 AMM 52-11-00-820-801.

Part: ELEC CONNECTOR — DISCONNECTED (ZONE 200) · airframe 76,528 hrs · 30,686 cycles

(LOG 5699717) EXTERIOR EMERGENCY LIGHTING SYSTEM INOP. FOUND CONNECTOR UNPLUGGED FROM MAIN WIRING HARNESS. RESECURED CONNECTOR REF B737 AMM 33-51, VERIFIED LIGHT OPERATES NORMALLY.

Part: BOLT — MISSING (ZONE 800) · airframe 76,069 hrs · 30,494 cycles

(LOG 6733784) DURING WAKE- UP CHECK AFT LEFT ENTRY DOOR WILL NOT OPEN. FOUND LOWER PUSH ROD BOLT MISSING. REINSTALLED BOLT AND OPS CK GOOD REF B737 AMM 52-41.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 73,331 hrs · 29,316 cycles

(LOG 0110413) AFT PRESSURE BULKHEAD UPPER AREA STA 1060 STRGR S-4L ATTACH FITTING WITH CRACKS AROUND FASTENERS. PRESSURE BULKHEAD UPPER AREA STA 1016 STGR S-4L ATTACH FITTING WAS REPLACED I.A.W P.R.I. 614042-14 REV 0 AND ER/A 614042-14.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 73,331 hrs · 29,316 cycles

(LOG 0111797) A/C RAIL BRACKETS STA 400LH CRACK DETECTED IN FRAME AT FASTENER HOLE. A/C RAIL BRACKETS STA 400LH, FRAME WAS REPAIRED I.A.W. B737-800 WORK CARD 2526-01236-04A FULL REPAIR, RII SECTION 04.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 73,331 hrs · 29,316 cycles

(LOG 0110489) AFT ENTRY DOOR CUTOUT INT STRUCTURE BS 992.8 AND S-15L ANGLE CORROSION. AFT ENTRY DOOR CUTOUT INT STRUCTURE BS 992.8 AND S-15L ANGLE WAS REPLACED I.A.W. ER/A 614271-14 REV ORIGINAL.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 73,331 hrs · 29,316 cycles

(LOG 0108988) ZONE 240- PASSENGER COMPARTMENT, AFT GALLEY, AFTER THE REMOVAL OF THE STABILIZER CORROSION WAS FOUND ON GALLEY FLOOR STRUCTURE. PASSENGER COMPARTMENT, AFT GALLEY FLOOR STRUCTURE STABILIZER WAS REPLACED I.A.W. B737-800 SRM 51-40-02-0G.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 73,331 hrs · 29,316 cycles

(LOG 0109013) ZONE 240- PASSENGER COMPARTMENT, AFT GALLEY, CORROSION WAS FOUND ON STABILIZER. PASSENGER COMPARTMENT, AFT GALLEY, STABILIZER WAS REPLACED I.A.W. SRM 51-40-02-0G.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 73,331 hrs · 29,316 cycles

(LOG 0107499) PASSENGER COMPARTMENT, AFT WET AREA, CORROSION ON STA 947.5 AND LBL 55.5. PASSENGER COMPARTMENT AFT WET AREA ON STA 947.5 AND LBL 55.5 FLOOR CUT PLATE WAS REPLACED PER B737-800 SRM 51-40-02-0G.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 73,331 hrs · 29,316 cycles

(LOG 0107361) PASSENGER COMPARTMENT, FWD WET AREA 1, CORROSION ON STA 328 ON RBL 50.5. PASSENGER COMPARTMENT, WET AREA 1 ON CUT PLATE BTW STA 244.5 AND STA 328 ON RBL 50.5 SILL BEAM WAS REPLACED I.A.W. B737-800 SRM 51-10-02-0G.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 73,331 hrs · 29,316 cycles

(LOG 0107496) PASSENGER COMPARTMENT, AFT WET AREA, CORROSION ON FLOOR CUT PLATE BETWEEN STA 947.5 AND STA 993, ON LBL 55. PASSENGER COMPARTMENT, AFT WET AREA, FLOOR CUT PLATE BETWEEN STA 947.5 AND STA 993, ON LBL 55, WEB WAS REPLACED PER B737-800 SRM 51-40-02-0G.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 73,331 hrs · 29,316 cycles

(LOG 0102789) A/C RAIL BRACKETS STA 380LH CRACK DETECTED IN FRAME AT FASTENER HOLE. A/C RAIL BRACKETS STA 380LH, FRAME WAS REPAIRED I.A.W. B737-800 WORKCARD 2526-01236-02A.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 73,331 hrs · 29,316 cycles

(LOG 0102782) A/C RAIL BRACKETS STA 440LH CRACK DETECTED IN FRAME AT FASTENER HOLE. A/C RAIL BRACKETS STA 440LH, FRAME WAS REPAIRED I.A.W. B737-800 WORDCARD 2526-01236-02A.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 73,331 hrs · 29,316 cycles

(LOG 0101421) LEFT SIDE VERTICAL PRESSURE DECK WEB, BETWEEN LBL25 AND LBL45 CRACKED. LEFT SIDE VERTICAL PRESSURE DECK WEB BETWEEN LBL 45 LBL 25 WAS REPAIRED IAW B737-800 SRM 57-10-10 REPAIR 3.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 73,331 hrs · 29,316 cycles

(LOG 0101473) DURING MAJOR MAINTENANCE SERVICE ON MXA MRO AT MEX, WHILE PERFORMING DELTA TASK NO. 2020-9002 "CHECK - AIRCRAFT EXTERNAL DAMAGE IDENTIFICATION (ADF FILE) AND DENT RE-EVALUATION", A DENT WITH CREASE (LOG 0253353) WAS RE-EVALUATED ON RH FUSELAGE SKIN BETWEEN STA 847 AND STA 855, AND BETWEEN STRINGER 21 AND STRINGER 22. DAMAGE REPAIRED PER ERA 613760-14.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 73,331 hrs · 29,316 cycles

(LOG 0100334) A/C RAIL BRACKETS STA 500A RH CRACK DETECTED IN FRAME AT FASTENER HOLE. A/C RAIL BRACKETS STA 500A RH, FRAME WAS REPAIRED I.A.W. B737-800 WORKCARD 2526-01236-02B.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 73,331 hrs · 29,316 cycles

(LOG 0100018) RH HORIZONTAL STABILIZER, SEVERAL CRACKS ON LOWER SKIN BTW STAB STA-101.90 / STAB STA-166.30 AND FRONT SPAR / REAR SPAR. RH HORIZONTAL STABILIZER ON LOWER SKIN BTW STAB STA 101.90 / STA 166.30 AND FRONT SPAR/REAR SPAR WERE REPAIR PER B737-800 SRM 55-10-01-2R-11.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 73,331 hrs · 29,316 cycles

(LOG 0099981) A/C RAIL BRACKETS STA 400RH CRACK DETECTED IN FRAME AT FASTENER HOLE. A/C RAIL BRACKETS STA 400RH, FRAME WAS REPAIRED I.A.W. B737-800 WORKCARD 2526-01236-02B.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 73,331 hrs · 29,316 cycles

(LOG 0098870) PASSENGER COMPARTMENT, BROKEN SEAT TRACK BETWEEN STA 727 H AND STA STA 727 I ON LBL 45.5. PASSENGER COMPARTMENT SEAT TRACK BETWEEN STA 727H AND 727I ON LBL 45.5 WAS REPAIRED I.A.W. B737-800 SRM 53-00-52-2R REPAIR 5.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 73,331 hrs · 29,316 cycles

(LOG 0097438) A/C RAIL BRACKETS STA 907RH CRACK DETECTED IN FRAME AT FASTENER HOLE. A/C RAIL BRACKETS STA 907RH, FRAME WAS REPAIRED I.A.W. B737-800 WORKCARD

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 73,331 hrs · 29,316 cycles

(LOG 0098766) PASSENGER COMPARTMENT, BROKEN SEAT TRACK ON RBL 46.5 AND BETWEEN STA 787 AND STA 807. PASSENGER COMPARTMENT SEAT TRACK ON RBL 46.5 AND BETWEEN STA 787 AND STA 807 WAS REPAIRED I.A.W. B737-800 SRM 53-00-52-2R REPAIR 5.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 73,331 hrs · 29,316 cycles

(LOG 0111878) PASSENGER COMPARTMENT, AFT WET AREA, CORROSION ON STA 986.5 AND LBL 47. PASSENGER COMPARTMENT, AFT WET AREA, T-CHORD ON STA 986.5 AND LBL 47 WAS REPLACED PER B737-800 SRM 51-40-02-0G.

Part: FLOORBEAM — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 73,331 hrs · 29,316 cycles

(LOG 0111883) PASSENGER COMPARTMENT, AFT WET AREA, CORROSION ON STA 986.5, FROM LBL 47 TO RBL 47. PASSEGER COMPARTMENT, AFT WET AREA ON STA 986.5 FROM LBL 47 TO RBL 47, T-CHORD WAS REPLACED PER B737-800 SRM 51-40-02-0G.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 73,331 hrs · 29,316 cycles

(LOG 0097411) PASSENGER COMPARTMENT, WET AREA 1, CORROSION ON STA 328 AND LBL 58.5. PASSENGER COMPARTMENT, WET AREA 1, ON STA 328 AND LBL 58.5 CHORD BEAM WAS REPAIRED I.A.W B737-800 SRM 53-10-51-2R

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 73,331 hrs · 29,316 cycles

(LOG 0098777) LEFT SIDE VERTICAL PRESSURE DECK WEB, BETWEEN LBL25 AND LBL45, WITH A CRACK. LEFT SIDE VERTICAL PRESSURE DECK WEB BETWEEN LBL 45 LBL 25 WAS REPAIRED I.A.W B737-800 SRM 57-10-10 REPAIR 3.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 73,331 hrs · 29,316 cycles

(LOG 0097423) A/C RAIL BRACKETS STA 907LH CRACK DETECTED IN FRAME AT FASTENER HOLE. A/C RAIL BRACKETS STA 907LH, FRAME WAS REPAIRED I.A.W. B737-800 WORKCARD 2526-01236-03A.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 73,331 hrs · 29,316 cycles

(LOG 0100111) A/C RAIL BRACKETS STA 480RH CRACK DETECTED IN FRAME AT FASTENER HOLE. A/C RAIL BRACKETS STA 480RH, FRAME WAS REPAIRED I.A.W. B737-800 WORKCARD 2526-01236-02B

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 73,331 hrs · 29,316 cycles

(LOG 0100086) A/C RAIL BRACKETS STA 727B RH CRACK DETECTED IN FRAME AT FASTENER HOLE. A/C RAIL BRACKETS STA 727B RH, FRAME WAS REPAIRED I.A.W. B737-800 WORKCARD 2526-01236-02B.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 73,331 hrs · 29,316 cycles

(LOG 0099843) A/C RAIL BRACKETS STA 827 RH CRACK DETECTED IN FRAME AT FASTENER HOLE. A/C RAIL BRACKETS STA 827 RH, FRAME WAS REPAIRED I.A.W. B737-800 WORKCARD 2526-01236-02B.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 73,331 hrs · 29,316 cycles

(LOG 0097114) A/C RAIL BRACKETS STA 480LH CRACK DETECTED IN FRAME AT FASTENER HOLE. A/C RAIL BRACKETS STA 480 LH, FRAME WAS REPAIRED I.A.W. B737-800 WORKCARD 2526-01236-02A.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 73,331 hrs · 29,316 cycles

(LOG 0100104) A/C RAIL BRACKETS STA 500C RH CRACK DETECTED IN FRAME AT FASTENER HOLE. A/C RAIL BRACKETS STA 500C RH, FRAME WAS REPAIRED I.A.W. B737-800 WORKCARD 2526-01236-02B.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 73,331 hrs · 29,316 cycles

(LOG 00891088) PASSENGER COMPARTMENT, WET AREA 1, CORROSION BETWEEN STA 294.5 AND STA 344 ON LBL 12, INTERCOSTALS. WET AREA 1 BTW STA 294.5 AND STA 344 ON LBL 12 INTERCOSTAL WAS REPLACED AND INSTALLED. I.A.W B737-800 SRM 51-10-02-0G.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 73,331 hrs · 29,316 cycles

(LOG 0091136) PASSENGER COMPARTMENT, WET AREA 1, CORROSION ON CUT PLATE BETWEEN STA 244.5 AND STA 328, ON RBL 50.5. CUT PLATE BTW STA 244.5 AND STA 328 ON RBL 50.5 SILL BEAM WAS REPLACED I.A.W B737-800 SRM:51-10-02-0G.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 73,331 hrs · 29,316 cycles

(LOG 0108716) PASSENGER COMPARTMENT, WET AREA 1, CORROSION BETWEEN STA 328 AND STA 344, ON RBL 58.5. PASENGER COMPARTMENT, WET AREA 1 ON CUT PLATE BTW STA 244.5 AND STA 328 ON RBL 50.5 SILL BEAM WAS REPLACED I.A.W.B737-800 SRM 51-10-02-0G.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 73,331 hrs · 29,316 cycles

AIRCRAFT 3714, DURING HCK AT QRO, A CRACK WAS FOUND EMANATING FROM A FASTENER HOLE OF LH WING SURFACE, STA 558, S-5L. AFFECTED ELEMENTS ARE SKIN 112A4102-207 (M/F 2324-T39 MACHINED PLATE PER BMS 7.254) & STRINGER 112A4205-207 (M/F 2224-T3511 EXTRUSION PER BMS 7-255). CORRECTIVE ACTION: OVERSIZED THE HOLE UNTIL THE CRACK IS REMOVED WITH INCREMENTS OF 0.016 /0.035, DO NOT EXCEED 0.340 / 0.342 HOLE DIAMETER. PERFORMED A 0.047" INSURANCE CUT AFTER HFEC INSPECTING THE OVERSIZED FASTENER HOLE IN BOTH THE SKIN AND THE STRINGER TO ENSURE NO FURTHER CRACKING DAMAGE EXISTS. COUNTERSINK THE OVERSIZED HOLE ON SKIN WITH 100-DEGREE COUNTERSINK, ENSURE THE COUNTERSINK DEPTH IS BETWEEN 0.070 AND 0.072. 6. FABRICATED ONE STRAIGHT REPAIR BUSHING FOR THE STRINGER FROM 7075-T6 AL-BAR, SAME THICKNESS AS REQUIRED TO MATCH THE THICKNESS OF THE PART PER B737-800 SRM 51-20-10. (LP 0045278)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 72,895 hrs · 29,106 cycles

(LOG 2944766) WHILE OVERNIGHT IN MIA, THE AIRCRAFT EXPERIENCED GROUND DAMAGE RESULTING IN A DENT AND GOUGE DAMAGE COMMON TO THE FWD CARGO DOOR SURROUND SKIN, (P/N: 143A3232-7), BEARSTRAP (143A3254-2), EXISTING REPAIR, AND BULLNOSE CHORD. MAINTENANCE REPAIRED DAMAGE PER ERA 611132-14.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 72,893 hrs · 29,104 cycles

(LOG 2913432) WHILE OVERNIGHT IN MIA, THE AIRCRAFT ENCOUNTERED GROUND DAMAGE RESULTING IN A DENT AND GOUGE DAMAGE COMMON TO THE FWD CARGO DOOR SURROUND SKIN.MAINTENANCE REPAIRED DAMAGE PER ERA 611132-14.

Part: BATTERY PACK — INOPERATIVE (UNKNOWN) · airframe 72,630 hrs · 28,991 cycles

(LOG 4834714) LT OVERWING EXIT SIGNS INOP DURING EMERGENCY LIGHT TEST. REPLACED BATTERY PACK M1668 IAW B737 AMM 33-51.

Part: LIGHT — INOPERATIVE · airframe 71,780 hrs · 28,585 cycles

(LOG 9518196) DURING INSPECTION FOUND EXIT SIGNAL MISSING AFT GALLEY. REPLACED AFT GALLEY EMERGENCY EXIT SIGN PER B737 AMM 33-00. OK FOR SVC.

Part: SKIN — DAMAGED (NOT REPORTED) · airframe 71,252 hrs · 28,330 cycles

(LOG 2566948) DURING CCK IN QRO, WHILE PERFORMING STEP 17 OF WORK CARD 2330-01337-1001, ELONGATED HOLES WERE FOUND BEYOND THE ALLOWABLE LIMITS (0.200/0.203) COMMON TO SKIN P/N 146A3101-14 & BONDED DOUBLER P/N 146A3101-15. MAINTENANCE REPAIRED DAMAGE PER ERA 590048-14AD.

Part: LIGHT — DETACHED (CABIN) · airframe 71,073 hrs · 28,243 cycles

DURING INSPECTION FOUND AISLE EXIT LIGHT NEAR OVERWING EXITS IS BROKEN. RE-ATTACHED AISLE EMER. EXIT LIGHT.

Part: CHARGER — INOPERATIVE · airframe 70,881 hrs · 28,146 cycles

(LOG 9434358) DURING INSPECTION FOUND EMERG LIGHTS OUT FROM SEATS 23DEF TO AFT RT SVC DOOR. REPLACED BATTERY PACK AND CHARGER PER B737 AMM 33-51. OPS OK.

Part: NONE — NONE · airframe 70,692 hrs · 28,063 cycles

(LOG 2434795) DURING INSPECTION FOUND RIGHT SIDE FUSELAGE STA 440 AND STR 24R / FWD CARGO DOOR SURROUND / IMPACT DAMAGE. REPAIRED PER PRI 602546-14.

Part: NONE — NONE · airframe 70,692 hrs · 28,063 cycles

(LOG 2434794) DURING INSPECTION FOUND FASTENER HOLE ENLARGED TO.233 DIAMETER AT STATION 400 STR 22R. INSTALLED REPAIR FASTENER PER ERA 602546-14 REV ORIG.

Part: NONE — NONE · airframe 70,685 hrs · 28,059 cycles

(LOG 9141644) DURING INSPECTION FOUND FWD CARGO DOOR OPENING DAMAGE ON FWD SIDE. COMPLIED WITH ERA 602435-14 REV. A SECTION II PERMANENT REPAIR INSTRUCTIONS. INSTALLED REPAIR DOUBLERS PER ERA 602546-14 REV. ORIG. SECTION I PERMANENT REPAIR INSTRUCTIONS.

Part: BATTERY PACK — INOPERATIVE · airframe 70,563 hrs · 28,001 cycles

(LOG 9050276) DURING INSPECTION FOUND AFT LT DOOR EMERGENCY LIGHT SIGNS INOP. R/R LT DOOR EMERGENCY BATT PACK ASSY IAW B737 AMM 33-51.

Part: BATTERY PACK — INOPERATIVE · airframe 69,076 hrs · 27,286 cycles

(LOG 8515175) DURING INSPECTION FOUND RT OVER WING EMER BATTERY PACK WILL NOT HOLD ITS CHARGE. REMOVED AND REPLACED RIGHT OVER WING BATTERY PACK. OPS CK GOOD IAW B737 AMM 33-51-06.

Part: NONE — NONE · airframe 69,042 hrs · 27,266 cycles

SHIP 3714 -ATB/GEAR- LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. CORRECTIVE ACTION: FOUND GEAR PINS INSTALLED. REMOVED GEAR PINS. AIRCRAFT RETURNED TO SERVICE.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 73,331 hrs · 29,316 cycles

AIRCRAFT 3714, DURING HCK AT QRO, A CRACK WAS FOUND EMANATING FROM A FASTENER HOLE OF RH WING SURFACE, STA 553, S-9R. AFFECTED ELEMENTS ARE SKIN 112A4102-208 (M/F 2324-T39 MACHINED PLATE PER BMS 7-254) & STRINGER 112A4205-208 (M/F 2224-T3511 EXTRUSION PER BMS 7255). CORRECTIVE ACTION: REMOVED EXISTING PRODUCTION FASTENER OF 0.246 HOLE DIAMETER. OVERSIZED THE HOLE IN SKIN AND STRINGER UNTIL THE CRACK IS REMOVED WITH INCREMENTS OF 0.016 /0.035, DO NOT EXCEED 0.311 / 0.313 HOLE DIAMETER. FABRICATED ONE STRAIGHT REPAIR BUSHING FOR THE STRINGER FROM 7075-T6 AL-BAR, SAME THICKNESS AS REQUIRED TO MATCH THE THICKNESS OF THE PART PER B737-800 SRM 51-20-10. FABRICATED ONE COUNTERSINK REPAIR BUSHING FOR THE SKIN FROM 7075-T6 AL-BAR, SAME THICKNESS AS REQUIRED TO MATCH THE THICKNESS OF THE PART PER B737-800 SRM 51-20-10. (LP 1984281)

Part: NONE — NONE · airframe 68,270 hrs · 26,917 cycles

(LOG 1982194) DURING INSPECTION FOUND B737-800 / WINGS / OUTER WING / LWR SKIN, LHS / STGR 5, STA 558 CRACK REPAIR. REPAIRED CRACK DAMAGE PER ERA 562339-14.

Part: SUPPORT — CORRODED (WNG-BDY FAIRING) · corrosion level 2 · airframe 66,231 hrs · 26,193 cycles

(LOG 1732334) DURING INSPECTION FOUND CORROSION AND ELONGATED FASTENER HOLES (2 EA) AT SUPPORT STRUCTURE ATTACHMENT OF WING-TO-BODY FAIRING PANEL 193D BS 727+2.7. SUPPORT STRUCTURE ATTACHMENT OF WING-TO-BODY FAIRING PANEL 193D BS 727+2.7 WAS REPAIRED PER ERA 590110-14AD REV. ORIGINAL AND ETI-37-21-314 REV. 1.

Part: NONE — NONE · airframe 69,164 hrs · 27,326 cycles

(LOG 1731222) ELONGATED HOLES FOUND DURING IDTV REMOVAL. DAMAGE REPAIRED PER ERA 590048-14.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 66,231 hrs · 26,193 cycles

(LOG 1731225) DURING INSPECTION FOUND BROKEN CUTOUT OF EXTERNAL POWER RECEPTACLE ACCESS DOOR NR 144AR. ACCESS DOOR WAS REPAIRED PER ETI-57-21-312 REV. 2 AND ERA 590089-14 REV. ORIGINAL.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 66,231 hrs · 26,193 cycles

(LOG 1729707) DURING INSPECTION FOUND CORROSION ON FUSELAGE SKIN AROUND OF WASTE TANK VENT PORT BTW STA 905 AND STA 927 AND BTW S20L. FUSELAGE SKIN AROUND OF WASTE TANK VENT PORT BTW STA 905 AND STA 927 AND BTW S20L WAS REPAIRED PER B737-800 SRM 53-70-01-2R REPAIR 3.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 65,972 hrs · 26,080 cycles

(LOG 6860718) DURING INSPECTION FOUND EMERGENCY LIGHT BATTERY PACK M1671 AT SIDE WALL ROW 23D FAILED OPERATIONAL CHECK. R/R EMERGENCY LIGHT BATTERY PACK M1671 PER B737 AMM 33-51. OPS CHECK NORMAL.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 64,509 hrs · 25,426 cycles

DURING INSPECTION FOUND EMERGENCY LIGHT IN-OP ATL1 DOOR EXTERIOR AND EXIT SIGN. REPLACED BATTERY PACK D10750 PER AMM 33-51. OPS CKS GOOD.

Part: LENS — DAMAGED (EMERGENCY LIGHT) · airframe 64,509 hrs · 25,426 cycles

DURING INSPECTION FOUND EMERGENCY EXIT COVER DIFFUSER LENS DAMAGED OR MISSING. INSTALLED AFT EMERGENCY EXIT OVERHEAD SIGN LENS PER AMM 33-50. OPS CK GOOD.

Part: CONNECTOR — SHORTED (HYD PUMP) · airframe 63,828 hrs · 25,124 cycles

DURING SECOND PUSHBACK WHEN THE ELEC HYD PUMP WAS TURNED ON. THE OVERHEAT LIGHT CAME ON IMMEDIATELY AND NOTICED AN ELECTRICAL SMELL. THE LIGHT BURNED OUT AFTER ABOUT 30 SECONDS. THE SWITCH WAS TURNED OFF AND THE SMELL WENT AWAY. T/S PER B737 WDM 29-34-11 FOUND PIN 7 OF "B" ELEC 1 HYD PUMP CONNECTOR SHORTED INTERNALLY TO OTHER PINS IN PUMP. REPLACED SYS "B" ELEC 1 HYD. PUMP PER B737 AMM 29-11 OPS CK NML. REPLACED HYD OVERHEAD PANEL P5-8 PER B737 AMM 29-11 OPS CK NML. PUMP LK AND OPS CK GOOD.

Part: FUSE — FAILED (EMERGENCY LIGHTS) · airframe 63,804 hrs · 25,115 cycles

DURING INSPECTION FOUND RT AFT OVER WING EXIT EXTERIOR EXIT LIGHT INOPERATIVE. GAINED ACCESS TO BATTERY PACK AND REPLACED FUSE PER B737 AMM 33-51. LIGHT CHECKS GOOD

Part: FASTENER — LOOSE · airframe 63,548 hrs · 25,009 cycles

(LOG 3795282) PREVIOUS CREW REPORTED ELECTRICAL SMELL POST LANDING, AFTER DOOR CLOSURE AT PUSH STRONG ELECTRICAL SMELL IN COCKPIT. FOUND TB5060E BURNT AT PIN 7 DUE TO LOOSE HARDWARE. RPLCD THE TERMINAL STRIP AND WIRE LUG GOING TO PIN 7 PER WDM 24-51. OPS CHECK OK.

Part: BOLT — LOOSE (GROUND START) · airframe 62,938 hrs · 24,767 cycles

SHIP 3714 - DIV/PRES - DURING FLIGHT AT FL 340 CABIN ALTITUDE LIGHT ILLUMINATED AND WARNING HORN CAME ON. AIRCRAFT DESCENDED AND PASSENGER MASKS DEPLOYED. AIRCRAFT DIVERTED TO MEM. CORRECTIVE ACTION: MAINTENANCE RETOURQUED LOOSE GROUND START CONNECTION BOLTS AND FOUND SEVERAL BELLY DRAIN VALVES STUCK OPEN. CLEANED ALL VALVES. OPS CHECK GOOD AND PRESSURIZATION LEAK CHECK OK. AIRCRAFT RETURNED TO SERVICE.

Part: SKIN — DENTED (FUSELAGE) · airframe 62,743 hrs · 24,684 cycles

DURING INSPECTION FOUND LARGE DENT MEASURING 13.5" BY 11" BY A DEPTH OF 0.375 WITH A 0.75" LONG MINOR GOUGE AS SEEN IN FIGURE 12. THE SUBJECT DENT IS LOCATED BETWEEN STA 492-500B AND STR 21R-23R. UNDERLYING STR 22R IS BENT. REPAIRED PER PRI 575226-14 REV 4. RECEIVED FINAL ERA 575226-14 REV 0.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT) · airframe 62,394 hrs · 24,550 cycles

(LOG 5199407) DURING INSPECTION FOUND R/H BULLNOSE EMERG LIGHT INOPERATIVE AT ROWS 15/16. FOUND LOOSE CONNECTOR - SECURED CONNECTOR - OPS NORMALLY.

Part: SOCKET — DAMAGED (CABIN) · airframe 62,163 hrs · 24,453 cycles

DURING INSPECTION FOUND EMERGENCY LIGHT AT BIN 15 D, E, F INOPERATIVE. MAINTENANCE FOUND LIGHT SOCKET DAMAGED. R&R SOCKET PER AMM 33-51. OPS CHECKS GOOD.

Part: BRACKET — CORRODED (GALLEY) · airframe 58,657 hrs · 23,097 cycles

DURING INSPECTION FOUND CORROSION ON BRACKETS (2EAS) OF GALLEY NR 2. MAINTENANCE REPLACED BRACKETS (2EAS) OF GALLEY NR 2 PER ER/A 560952-14 REV ORIG AND ETI-37-17-316 REV 2.

Part: TIE DOWN — CORRODED (GALLEY) · airframe 58,657 hrs · 23,097 cycles

DURING INSPECTION FOUND CORROSION ON FREEZER TIEDOWN BLOCK OF AFT RT GALLEY NR 2. MAINTENANCE REPLACED FREEZER TIEDOWN BLOCK OF AFTER RT GALLEY NR 2 PER ER/A 560958-14 REV ORIGINAL AND ETI-37-17-320 REV 1.

Part: FITTING — CORRODED (GALLEY) · airframe 58,657 hrs · 23,097 cycles

DURING INSPECTION FOUND CORROSION ON FITTING OF AFT RT GALLEY NR 2. MAINTENANCE REPLACED FITTING OF AFT RT GALLEY NR 2 PER ER/A 560953-14 REV ORIG AND ETI-37-17-317 REV 1.

Part: BRACKET — CORRODED (GALLEY) · airframe 58,657 hrs · 23,097 cycles

DURING INSPECTION FOUND CORROSION ON BRACKETS (17 EAS) OF GALLEY NR 4. MAINTENANCE REPLACED 2 BRACKETS (17EA) OF GALLEY NR 4 WERE REPLACED PER ERA 560951-14 REV ORIG AND ETI-37-17-315 REV 1.

Part: FLOORBEAM — CORRODED (BS 986.5) · airframe 58,657 hrs · 23,097 cycles

DURING INSPECTION, FOUND CORROSION ON PREVIOUS REPAIR AT CABIN FLOORBEAM BS 986.5, RBL 43 AND LBL 43. MAINTENANCE REPAIRED THE FLOORBEAM IAW ERA 560955-14, REV ORIGINAL, AND ETI-37-17-319, REV.

Part: BRACKET — CORRODED (LAVATORY MODULE) · airframe 58,657 hrs · 23,097 cycles

DURING INSPECTION, FOUND CORROSION ON BRACKET OF THE LT AFT LAVATORY MODULE. MAINTENANCE REPLACED THE BRACKET IAW ETI-37-17-322, REV ORIGINAL, AND ER/A 562338-14, REV ORIGINAL.

Part: CARGO TRACK — CRACKED (BS 727I) · airframe 58,657 hrs · 23,097 cycles

DURING INSPECTION, FOUND A CRACKED CARGO TRACK, BS 727I, STRINGER 27R. REPAIRED IAW ETI-37-17-332, REV 1, ERA 562360-14, REV ORIGINAL.

Part: SKIN — DAMAGED (BS 490-500) · airframe 58,657 hrs · 23,097 cycles

DURING AN H CHECK, NICKS WERE FOUND ON FUSELAGE SKINS AT BS 490 AND 500, BETWEEN STRINGERS 23R AND 25R. REPAIRED IAW ERA 562355-14.

Part: FLOORBEAM — CORRODED (BS 947.5) · airframe 58,657 hrs · 23,097 cycles

DURING INSPECTION, FOUND CORROSION ON THE CABIN FLOORBEAM BS 947.5, BETWEEN RBL 47 TO RBL 53. REPAIRED IAW ERA 560954-14, REV ORIG, AND ETI -37-17-318, REV 4.

Part: FRAME — CRACKED (BS 294) · airframe 58,657 hrs · 23,097 cycles

DURING INSPECTION, FOUND A CRACK ON THE FRAME BS 294, RBL 54. REPAIRED IAW ERA 562337-14, REV ORIG, AND ETI 37-17-321, REV 4.

Part: SEAT TRACK — CRACKED (BS 727-855) · airframe 58,657 hrs · 23,097 cycles

DURING INSPECTION, FOUND A CRACKED SEAT TRACK CROWN, LBL 45, BS 727C AND 855 IN THE PAX CABIN. MAINTENANCE REPAIRED THE SEAT TRACK IAW SRM 53-00-52, FIGURE 202, SHEET 1 -5, REPAIR 5.

Part: STRUCTURE — CRACKED (LT WING) · airframe 58,657 hrs · 23,097 cycles

DURING INSPECTION, FOUND A CRACK AT HOLE, STRINGER 5L. LWS 558, BETWEEN RIBS 18 - 19. REPAIRED IAW ERA 562339-14, REV ORIG, AND ETI-37-17-323, REV 5..)

Part: SKIN — CRACKED (RT WING) · airframe 58,657 hrs · 23,097 cycles

DURING AN H CHECK, A CRACK WAS FOUND EMANATING FROM A FASTENER HOLE OF THE RT WING SKIN, LWS 553, STRINGER 9R. MAINTENANCE REPAIRED THE SKIN IAW ERA 562340-14.

Part: SKIN — CRACKED (LT WING) · airframe 58,657 hrs · 23,097 cycles

DURING H CHECK, A CRACK WAS FOUND EMANATING FROM A FASTENER HOLE OF THE LT WING SURFACE, LWS 558, STRINGER 5L. REPAIRED IAW ERA 562339-14.

Part: WEB — CORRODED (RT NACELLE) · airframe 58,657 hrs · 23,097 cycles

DURING INSPECTION, FOUND CORROSION ON LOWER WEB UNDER THE HEAT SHIELD FAIRINGS, AT THE RT ENGINE STRUT AFT FAIRING STRUCTURE. MAINTENANCE REPLACED THE WEB IAW SRM 51-40-02, PAR.7, 51-20-01, PAR 5, AND AMM 51-21-72.

Part: WEB — CORRODED (LT NACELLE) · airframe 58,657 hrs · 23,097 cycles

DURING INSPECTION, FOUND CORROSION ON THE LOWER WEB, UNDER THE HEAT SHIELD FAIRINGS, AT THE LT ENGINE STRUT AFT FAIRING STRUCTURE. MAINTENANCE REPLACED THE WEB IAW SRM 51-40-02, PAR 7, 51-20-01, PAR.5, AND AMM 51-21-72.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 58,657 hrs · 23,097 cycles

DURING INSPECTION, FOUND CORROSION ON THE FLOOR SUPPORT BS 967, RBL 47 IN THE PAX CABIN. MAINTENANCE REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02 PAR. 7C.

Part: FLOORBEAM — CORRODED (BS 772) · airframe 58,657 hrs · 23,097 cycles

DURING INSPECTION, FOUND CORROSION ON THE FLOORBEAM AT BS 772 BETWEEN STRINGERS 26R TO 26L IN THE AFT CARGO BAY. MAINTENANCE REPLACED AND FABRICATED NEW FLOORBEAM ANGLE IAW SRM 53-60-51, FIG 103, PAR A, AND DWG 146A9401, REV C.

Part: PLATE — CORRODED (BS 727-727H) · airframe 58,657 hrs · 23,097 cycles

DURING INSPECTION, FOUND CORROSION ON THE RT PLATE CHANNEL FROM BS 727 TO 727H, STRINGERS 26R TO 27R IN THE AFT CARGO BAY. MAINTENANCE REPLACED THE PLATE IAW SRM 51-40-02.

Part: SKIN — DENTED (LT WING SPOILER) · airframe 66,231 hrs · 26,193 cycles

(LOG 0255040) DURING INSPECTION FOUND DENT (UPPER SKIN ZONE 1) ON SPOILER PANEL NO. 1 AT LH WING. SPOILER PANEL NO. 1 WAS REPAIRED PER B737-800 SRM 51-- 70-10 REPAIR GENERAL.

Part: SKIN — DENTED (SPOILER) · airframe 58,657 hrs · 23,097 cycles

DURING INSPECTION, FOUND A DENT IN THE SKIN OF THE SPOILER PANEL NR 1 ON THE LT WING. MAINTENANCE REPAIRED IAW SRM 51-70-10, REPAIR GENERAL.

Part: INTERCOSTAL — CORRODED (BULKHEAD) · airframe 58,657 hrs · 23,097 cycles

DURING INSPECTION, FOUND CORROSION ON THE INTERCOSTAL ON AFT PRESSURE DOME LOWER AREA BETWEEN LBL 41 TO RBL 41. MAINTENANCE REPLACED THE INTERCOSTAL IAW SRM 53-80-08.

Part: SHIELD — CORRODED (BS 767-787) · airframe 58,657 hrs · 23,097 cycles

DURING INSPECTION, FOUND CORROSION ON THE RT FWD SHIELD FROM BS 767 TO 787, ABOVE STRINGER 26R IN THE AFT CARGO BAY. MAINTENANCE INSTALLED A NEW SHIELD IAW SRM 51-40-02, SRM 51-20-07, SRM 51-20-01, AND AMM 51-21.

Part: FLOOR SUPPORT — CORRODED (BS 344) · airframe 58,657 hrs · 23,097 cycles

DURING INSPECTION, FOUND CORROSION ON THE FLOOR SUPPORT BS 344, LBL 59. MAINTENANCE REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02, PAR 9.

Part: INTERCOSTAL — CORRODED (BS 767-777) · airframe 58,657 hrs · 23,097 cycles

DURING INSPECTION, FOUND CORROSION ON WEB INTERCOSTAL FROM BS 767 TO 777, BETWEEN STRINGERS 26 & 27R IN THE AFT CARGO BAY. MAINTENANCE REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 51-40-02, FABRICATED IAW SRM 53-60-15.

Part: BULKHEAD WEB — CRACKED (BS 663) · airframe 58,657 hrs · 23,097 cycles

DURING INSPECTION, FOUND A CRACKED UPPER BULKHEAD WEB BS 663, RBL 40. MAINTENANCE REPAIRED THE BULKHEAD WEB IAW SRM 57-10-10 REPAIR 3.

Part: FLOOR SKIN — CORRODED (BS 223-226) · airframe 58,657 hrs · 23,097 cycles

DURING INSPECTION, FOUND CORROSION ON COCKPIT FLOOR WEB, BS 223 - 226, LBL 7 - 9. MAINTENANCE REPAIRED THE FLOOR WEB IAW SRM 53-10-51, REPAIR 2.

Part: MOTOR — FAILED (STAB TRIM) · airframe 57,986 hrs · 22,855 cycles

DURING DEPARTURE, LOST ELECTRIC STAB TRIM ON DEPARTURE. FOLLOWED QRH AND DID A FLAP 15 LANDING. MAINTENANCE REMOVED AND REPLACED THE STABILIZER TRIM MOTOR IAW AMM 27-41 AND COMPLIED WITH A TEST IAW AMM 27-41. CHECKED GOOD.

Part: SKIN — CRACKED (BS 540) · airframe 51,432 hrs · 20,677 cycles

BS 540 SKIN CRACKED, REPAIRED IAW AA 5331-01257

Part: SEAT TRACK — WORN (BS 540) · airframe 51,432 hrs · 20,677 cycles

DURING INSPECTION FOUND PASSENGER CABIN SEAT TRACK AT BS 540, RBL 24 WORN ON THE CROWN. MAINTENANCE R & R THE SEAT TRACK IAW SRM 53-00-52, REPAIR 3.

Part: SKIN — CORRODED (BS 1016) · airframe 51,432 hrs · 20,677 cycles

DURING INSPECTION, FOUND LOWER EXTERNAL FUSELAGE SKIN LT SIDE BS 1016, STRINGERS 20 - 27L SKIN CORRODED AT BUTT JOINT. MAINTENANCE REPAIRED THE SKIN IAW PRI 537900-14, REV 0 AND ER/A 537900-14, REV ORIGINAL.

Part: SEAT TRACK — WORN (BS 540) · airframe 51,432 hrs · 20,677 cycles

DURING INSPECTION, FOUND PASSENGER SEAT TRACK AT BS 540, LBL 45 WORN ON THE CROWN. MAINTENANCE INSTALLED SEAT TRACK REPAIR IAW SRM 53-00-52, REPAIR 3.

Part: SEAT TRACK — WORN (BS 540) · airframe 51,432 hrs · 20,677 cycles

DURING INSPECTION, FOUND PASSENGER SEAT TRACK, BS 540, RBL 45 WORN ON THE CROWN. MAINTENANCE INSTALLED SEAT TRACK REPAIR IAW SRM 53-00-52, REPAIR 3.

Part: SEAT TRACK — WORN (BS 520) · airframe 51,432 hrs · 20,677 cycles

DURING INSPECTION, FOUND PASSENGER SEAT TRACK BS 520, RBL 45 HAS WEAR ON THE CROWN. MAINTENANCE R & R SEAT TRACK IAW SRM 53-00-52, REPAIR 4.

Part: SEAT TRACK — WORN (BS 520) · airframe 51,432 hrs · 20,677 cycles

DURING INSPECTION, FOUND PASSENGER SEAT TRACK BS 520, LBL 24 WORN ON THE CROWN. MAINTENANCE R & R SEAT TRACK IAW SRM 53-00-52, REPAIR 4.

Part: SEAT TRACK — WORN (BS 520) · airframe 51,432 hrs · 20,677 cycles

DURING INSPECTION, FOUND PASSENGER SEAT TRACK BS 520, RBL 24 HAS WEAR ON THE CROWN. MAINTENANCE R & R SEAT TRACK IAW SRM 53-00-52, REPAIR 4.

Part: SEAT TRACK — WORN (BS 520) · airframe 51,432 hrs · 20,677 cycles

DURING INSPECTION, FOUND PASSENGER SEAT TRACK BS 520, RBL 45 WORN ON THE CROWN. MAINTENANCE R & R SEAT TRACK IAW SRM 53-00-52, REPAIR 4.

Part: ATTACH ANGLE — CORRODED (BS 864) · airframe 51,432 hrs · 20,677 cycles

DURING INSPECTION FOUND AFT CARGO BAY LT SIDE BS 864 VACUUM WASTE COMPARTMENT LOWER PANEL ATTACH ANGLE HAS CORROSION. MAINTENANCE RECIEVED NEW ANGLE FROM STORES, PN 149A8109U125. LOCATED, DRILLED, AND INSTALLED NEW ANGLE IAW SRM 51-30-01, PG 1, 51-40-08, PG1, 51-20-05, PG 201, 51-40-05, PG 1-7, 51-40-02, PG 1-5.

Part: ATTACH ANGLE — CRACKED (BS 864) · airframe 51,432 hrs · 20,677 cycles

DURING INSPECTION FOUND AFT CARGO BAY LT SIDE BS 864 VACUUM WASTE COMPARTMENT SUPPORT STANCHION LOWER ATTACH ANGLE CRACKED. MAINTENANCE REMOVED CRACKED ATTACH ANGLE IN AFT CARGO PIT LT SIDE BS 864. RECEIVED NEW ANGLE, PN 149A8109U114 FROM STORES, LOCATED, DRILLED AND INSTALLED NEW ANGLE IAW SRM 51-40-05.

Part: SKIN — DAMAGED (BS 500E-500F) · airframe 47,941 hrs · 19,507 cycles

DURING INSPECTION FOUND DAMAGE TO THE FUSELAGE SKIN AND UNDERLYING STRUCTURE BETWEEN BS 500E - 500F S26-28R. REPAIRED IAW ERA 525412.

Part: STRINGER — DAMAGED (BS 500E-500F) · airframe 46,735 hrs · 19,074 cycles

DURING INSPECTION FOUND STRINGER DAMAGE STRINGER 28R IS DAMAGED, TWISTED, BETWEEN BS 500E - 500F. MAINTENANCE FABRICATED REPAIR PARTS IAW SRM 53-00-03, REPAIR 1. CHEM TREATED IAW SRM 53-00-03, REPAIR 1. PAINTED IAW SRM 53-00-03, REPAIR 1. INSTALLED STRINGER 28R IAW PRI 525412-14, REV 4. C/W PERMANENT REPAIR IAW ERA 525412-14, REV ORIG AND SRM 53-00-03, REPAIR 1.

Part: SKIN — DAMAGED (BS 500E-500F) · airframe 46,701 hrs · 19,063 cycles

DAMAGE WAS FOUND TO FUSELAGE SKIN BETWEEN BS 500E - 500F AND STRINGERS 26 AND 28R. MAINTENANCE REPAIRED IAW ERA 525412.

Part: SKIN — DAMAGED (BS 500E-500F) · airframe 46,735 hrs · 19,074 cycles

DURING INSPECTION FOUND LOWER FUSELAGE SKIN DAMAGE BS 500E-500F BETWEEN S26-28R. MAINTENANCE REPAIRED IAW ERA 525412-14.

Part: SKIN — DAMAGED (BS 196.5) · airframe 44,941 hrs · 18,436 cycles

DURING INSPECTION FOUND LIGHTNING DAMAGE TO FASTENER HOLE ON SKIN BS 196.5, BL 0. MX REPAIRED IAW ERA 508731-14, REV A.

Part: SEAT TRACK — WORN (BS 727B) · airframe 44,620 hrs · 18,304 cycles

DURING INSPECTION, FOUND SPLICE STRAP HOLES WORN ON SEAT TRACK AT BS 727B, LBL 24.75. MX REPAIRED IAW ERA 518961-14, REV ORIG.

Part: SEAT TRACK — WORN (BS 727B) · airframe 44,620 hrs · 18,304 cycles

DURING INSPECTION, FOUND SPLICE STRAP HOLES WORN ON SEAT TRACK AT BS 727B, LBL 45.50. MX REPAIRED IAW ERA 518961-14, REV ORIG.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 42,772 hrs · 17,600 cycles

DURING INSPECTION, FOUND EMERGENCY LIGHT OVER ROW 17A-F INOPERATIVE. MX REPLACED BATTERY CHARGER IAW AMM 33-50. OPS CHECKED OK.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHT) · airframe 41,351 hrs · 17,053 cycles

EMERGENCY LIGHT BATTERY PACK FAILED TEST. MX REPLACED BATTERY PACKS. OPS CHECKED OK.

Part: CAP — CORRODED (FUSELAGE) · airframe 37,936 hrs · 15,766 cycles

STA 312 LBL 12 CORRODED. REPAIRED PER ERA 494561-14.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 34,051 hrs · 14,236 cycles

DURING OPS CHECK OF EMERGENCY LIGHTS, FOUND SEAT MOUNTED LIGHTS INOPERATIVE FROM ROW 23 UP TO RT GALLEY AREA. REPLACED THE BATTERY PACK.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 34,051 hrs · 14,236 cycles

DURING OPS CHECK OF EMERGENCY LIGHTS, FOUND RT AFT EMERGENCY OVERWING EXIT DOOR LIGHT INOPERATIVE. REPLACED BOTH CHARGER BATTERY PACKS FOR EQUIPMENT M1671.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 33,942 hrs · 14,192 cycles

EMERGENCY EGRESS AISLE LIGHTS INOPERATIVE, ROWS 23 THROUGH 33. REPLACED BATTERY PACK M10672, CHECKS GOOD (2010-D0901) (DL738101965).

Part: LIGHT — INOPERATIVE (CABIN) · airframe 33,829 hrs · 14,150 cycles

THE EMERGENCY EGRESS LIGHTING INOPERATIVE AT INTERIOR RIGHT AFT OVERWING EXIT AND EXTERIOR DOOR 2R. MAINTENANCE RE-LAMPED BOTH AND SYSTEM NOW CHECKS GOOD (2010-D0833) (DL738101837).

Part: WIRE — DAMAGED (EMERGENCY LIGHTS) · airframe 33,618 hrs · 14,064 cycles

DURING LAYOVER CHECK, MX FOUND SEAT 20D EMERGENCY PATH LIGHT INOPERATIVE. MX REPAIRED THE WIRE CONNECTION. OPS CHECK WAS GOOD. (DL738101612)

Part: WIRE — DAMAGED (CABIN) · airframe 33,187 hrs · 13,879 cycles

EMERGENCY EGRESS AISLE LIGHTS INOP AT ROW 11R. REPLACED WIRE TO LIGHT, OPS CHECK GOOD.

Part: UNKNOWN — ODOR (CABIN) · airframe 31,554 hrs · 13,212 cycles

NO SMOKE JUST FUMES FIRST TIME SMELLED LIKE STYROFOAM MID CABIN TURNED GALLEY POWER OFF / FUMES GONE QUICKLY / 60 MIN LATER MORE ELECTRICAL SMELL RETURNED. RAN SMOKE / FUMES CHECKLIST ODOR WENT AWAY SEATS 18-23 STRONGEST. OPERATED ALL OVENS AND COFFEEMAKERS FWD AND AFT GALLEY / NO SMELL NOTED. OPERATED ENTERTAINMENT SYS AND ALL LIGHTING FOR POSSIBLE BALLAST PROBLEMS, NONE FOUND, NO ODOR/ FUMES NOTED.

Part: ACTUATOR — BYPASSING (NR 1) · airframe 14,482 hrs · 6,691 cycles

AFTER TAKEOFF UPON FLAP/SLAT RETRACTION THE LEADING EDGE SLATS LOCKED OUT. TROUBLESHOOTING PER MAINTENANCE MANUAL AND BOEING SERVICE BULLETIN, FOUND NUMBER 1 AND NUMBER 8 LEADING EDGE SLAT ACTUATORS BYPASSING. REPLACED BOTH ACTUATORS PER M/M, OPERATIONAL CHECKS OK.

Part: ACTUATOR — FAILED (NR 5 SLAT) · airframe 13,626 hrs · 6,364 cycles

AFTER TAKEOFF UPON FLAP RETRACTION FROM FLAPS 1 TO UP L/E FLAPS TRANSIT LIGHT REMAINED ILLUMINATED WITH T/E FLAPS RETRACTED. PERFORMED LEADING EDGE FLAP TRANSIT CHECKLIST BUT NO CHANGE OCCURRED. T/E FLAPS OPERATED NORMALLY L/E DEVICES LOCKED OUT. REPLACED NR 5 SLAT ACTUATOR.