N830SY

Part: LAMP — INOPERATIVE (ZONE 200) · airframe 69,747 hrs · 31,929 cycles

EMERGENCY EXIT LOWER SIGN AT L1 DOOR IS INOPERATIVE. REPLACED L1 LOWER EXIT SIGN LIGHT LAMPS IAW AMM 33-51-01. OPS CHECK GOOD.

Part: LAMP — INOPERATIVE (ZONE 200) · airframe 69,747 hrs · 31,929 cycles

EMERGENCY LIGHT AT 17DEF IS INOPERATIVE. REPLACED EMERGENCY AREA LIGHT LAMP AT ROW 17DEF IAW AMM 33-51-03. OPS CHECK GOOD.

Part: NUT PLATE — MISSING (ZONE 200) · airframe 69,313 hrs · 31,697 cycles

REMOVED ESCAPE SLIDE GIRT BAR BRACKETS FOM, AFT ADAPTER PLATE AFT SCREW NUTPLATE FOUND TO BE MISSING, RTV HELD SCREW IN PLACE. REMOVE ESCAPE SLIDE GIRT BAR BRACKETS FOM, REF AMM 25-66-02. INSTALLED NUT PLATE AMM20-20 INSTALLED L1 DOOR ESCAPE SLIDE GIRT BAR FLOOR BRACKETS IAW AMM 25-66-02.

Part: INSERT — LOOSE (ZONE 200) · airframe 69,313 hrs · 31,697 cycles

L1 DOOR ENTRY GALLEY MAT THRESHOLD PLATE HAS LOOSE INSERTS IN FLOORBOARD BETWEEN GIRT BAR FLOOR MOUNTS. INSTALLED NEW INSERTS AND SECURED THRESHOLD PLATE.

Part: BATTERY PACK — NO TEST (ZONE 200) · airframe 69,262 hrs · 31,677 cycles

EMERGENCY LIGHT BATTERY PACK AT POSITION M1675 FAILED CAPACITY CHECK. REMOVED AND REPLACED EMERGENCY LIGHTING BATTERY PACK AT POSITION M1675 REF. AMM 33-51-06, OPS CHECK GOOD.

Part: BATTERY PACK — NO TEST (ZONE 200) · airframe 69,262 hrs · 31,677 cycles

EMERGENCY LIGHTING BATTERY PACK AT POSITION M1670 FAILED CAPACITY CHECK. REMOVED AND REPLACED EMERGENCY LIGHTING BATTERY PACK AT POSITION M1670 REF. AMM 33-51-06, OPS CHECK GOOD.

Part: ENGINE — FAILED (NR 2) · airframe 69,182 hrs · 31,648 cycles

SEVERE ENGINE DAMAGE #2 CLIMBING OUT OF 14,000 FT REDLINE EGT NO ROTATION N2 N1 14% FA'S REPORTED ALOT OF SPARKS MODERATE VIBRATION. REMOVED AND REPLACED #2 ENGINE REF TASK CARD # 710000000 ACCOMPLISHED ENGINE RUN TEST 9 AND TEST 5 REF AMM 71-00-00 ALL SYSTEMS CHECK NORMAL.

Part: SENSOR — FAULTED (FLAP SYS) · airframe 69,163 hrs · 31,639 cycles

DEFECT 801870: TRAILING EDGE FLAP ASYMMETRY RT FLAP INDICATOR SHOWS UP, LEFT FLAP INDICATOR SHOWS LESS THAN UP. - (EMERGENCY DECLARED) - RESOLUTION: FSEU BITE PROCEDURE INDICATED FLAP SKEW FAULT 27-53409. NO 28VAC WAS PRESENT AT PIN 2 OF #4 SKEW SENSOR . FOUND PIN 1&2 WIRES BROKEN . REMOVED AND REPLACED #4 SENSOR CONNECTOR . ALL CHECKS GOOD . REF FIM 27-51 TASK 810

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 69,163 hrs · 31,639 cycles

ROW 15-22 EMERGANCY LIGHTS OUT.R & R EMERGANCY LIGHT BATTERY PACK IAW AMM 33-51-06. OPS CHECKS GOOD.

Part: VENT — CORRODED (ZONE 100) · airframe 67,290 hrs · 30,781 cycles

CORROSION FOUND AT LH AFT FUSELAGE UNDER AFT LAV VENT AT LAP SEAM NEAR FRAME STA 916 STRINGER 22. - - RESOLUTION: ACCOMPLISHED REPAIR AT EXTERNAL FUSELAGE SKIN BETWEEN BSTA 907 AT LAP SPLICE S-23L IAW FAS EA 24008 REV IR.

Part: BATTERY PACK — NO TEST (ZONE 200) · airframe 67,287 hrs · 30,780 cycles

AFT L/H EMERGENCY BATTERY PACK FAILED TEST. REMOVED AND REPLACED AFT L/H EMERGENCY BATTERY PACK REF AMM 33-51-00

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 67,287 hrs · 30,780 cycles

WORK ORDER 89036, NR00009: AFT R/H EMERGENCY BATTERY PACK FAIL TEST. - -RESOLUTION: REMOVED AND REPLACED AFT R/H EMERGENCY BATTERY PACK REF AMM 33-51-00

Part: GIRT BAR — OUT OF ADJUST (L2 DOOR) · airframe 66,389 hrs · 30,391 cycles

DEFECT 731966 ITEM 2 : L2 DOOR GIRT BAR HARD TO GET INTO PLACE. ADJUSTED GIRT BAR CLIP TENSION. REF AMM 26-60-00

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 65,156 hrs · 29,801 cycles

DEFECT 705338: DURING CRUISE L1 WINDOW STARTED ARCING AND CAUSED SEVERE DAMAGE TO OUTER PANE.- - - RESOLUTION: (IN PROGRESS)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 65,139 hrs · 29,793 cycles

DEFECT W/O 81151 NRC00002: #3 BRAKE WAS WRITTEN UP BY FLIGHT CREW AS READING 8.6 INSPECTION OF BRAKE FOUND IT GLOWING RED AND STARTED ON FIRE. - - - RESOLUTION: (IN PROGRESS)

Part: ANGLE — CRACKED (BS 1016 S2L-R) · airframe 64,741 hrs · 29,265 cycles

DEFECT WO 74296 NR00083: CRACK ANGLE LOCATED BETWEEN BS1016 AND STR2L TO STR2R AT VERTICAL STAB ILIZER - - REPLACED ANGLE LOCATED BETWEEN BS1016 AND STR2L TO STR2R AT VERTICAL STABILIZER A.I.W. B737-800 SRM 51-40-02-0G-0 AND DWG 176A3101 SHEET 4 REVDONERESOLUTION:

Part: STRINGER — CRACKED (BS 727 S27L) · corrosion level 2 · airframe 64,741 hrs · 29,625 cycles

DEFECT WO 74296 NR00096: CRACK STRINGER 27L LOCATED KEEL BEAM ON BS727 AT AFT CARGO COMPARTMENT - - RESOLUTION: PERFORMED PERMANENT REPAIR LOCATED KEEL BEAM ON BS 727 PLUS 13.5 IN AT AFT CARGO COMPARTMENT IAW B737-800 SRM 53-60-12-2R - 1 REPAIR 1 THIS REPAIR IS A CATEGORY A. NO FURTHER ACTION REQUIRED

Part: SUPPORT ANGLE — CRACKED (LT WING) · airframe 64,741 hrs · 29,625 cycles

DEFECT WO 74296 NR00098: CRACK ON SUPPORT ANGLE LOCATED AT LEVEL ORSS 277 TRAILING EDGE AT LT W ING - - RESOLUTION: REPLACED ANGLE LOCATED AT LEVEL ORSS 277 TRAILING EGGE AT LT WING B737-800 SRM 51-40-02 AND DWG 115A6200 SHEET 9 REV: A

Part: FLOORBEAM — CRACKED (BS 540 BL0-LBL25) · airframe 64,741 hrs · 29,625 cycles

DEFECT WO 74296 NR00075: CRACK ON INTERCOSTAL LOCATED FLOOR STRUCTURE BS 540 BTW BL 0 TO LBL 2 4.75 AT PASSENGER CABIN - - RESOLUTION: REPLACED PLATE ON INTERCOSTAL LOCATED ON FLOOR STRUCTURE BS 540 BTW BL 0 TO LBL 24.75 AT PASSENGER CABIN IAW B737-800 SRM 51-40-02-0G-0 AND DWG 143A5240

Part: FRAME — CRACKED (BS 400 S8-9L) · airframe 64,741 hrs · 29,625 cycles

DEFECT WO 74296 NR00026: CRACK FRAME LOCATED BS 400, BETWEEN STRINGER 8L AND STRINGER 9L AT PASSE NGER CABIN. - - RESOLUTION: PERFORMED PERMANENT REPAIR ON FRAME LOCATED BS 400, BTW STRG 8L AND STRG 9L AT PASSENGER CABIN IAW EA #53-0192-23 REV 0. THIS REPAIR IS CATEGORY B INSPECTION THRESHOLD AT 50,000 FC

Part: SUPPORT ANGLE — CRACKED (LT WING) · airframe 64,741 hrs · 29,625 cycles

DEFECT WO 74296 NR00097: CRACK ON SUPPORT ANGLE LOCATED AT LEVEL ORSS 268 TRAILING EDGE AT LT WING. - - RESOLUTION: REPLACED SUPPORT ANGLE LOCATED AT LEVEL ORSS 268 TRAILING EDGE AT LT WING IAW B737-800 SRM51-40-02 DWG 115A2930 SHEET 7 REV

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 64,741 hrs · 29,625 cycles

DEFECT 724361: R1 AND R2 EMERGENCY LIGHT BATTERIES ARE BAD. - - - RESOLUTION: (IN PROGRESS)

Part: CARGO TRACK — CRACKED (BS 727E-727I) · corrosion level 2 · airframe 64,741 hrs · 29,625 cycles

DEFECT WO 74296 NR00087: CRACK FLOOR STRUCTURE CARGO TRACK LBL 17.24, AT LEVEL BS 727E, 727I A T AFT CARGO COMPARTMENT - - RESOLUTION: PERFORMED PERMANENT REPAIR LOC LBL 17.24 BTW BS727D TO BS727F AND LBL 17.24 BTW BS727D TO BS727H TO BS727J ON AFT CARGO COMPARTMENT IAW B737-800 SRM, 53-00-53-2R-3 REPAIR 3 THIS REPAIR IS A PERMANENT , NO FURTHER ACTION REQUIRED

Part: FLOOR SUPPORT — CORRODED (BS 947-967) · corrosion level 2 · airframe 64,741 hrs · 29,625 cycles

DEFECT WO 74296 NR00049: CORROSION ON FLOOR STRUCTURE INNER CHORD LOCATED BTW BS 947.5 TO BS 96 7 AT LEVEL STR 17L AFT GALLEY AREA - - RESOLUTION: REPLACED INNER CHORD BS 887 TO BS 1016 AT LEVEL STR 17L IAW B737-800 SRM 51-10-02 STEP 9 AND DRAWING 147A8501 SHEET 78 REV. B

Part: CARGO TRACK — CRACKED (BS 727E-727I) · corrosion level 2 · airframe 64,741 hrs · 29,625 cycles

DEFECT WO 74296 NR00084 CRACK FLOOR STRUCTURE CARGO TRACK LOCATED STA 727E AND RBL 13.84, STA 727G AND RBL 13.84, STA 727H AND RBL 13.84, STA 727I AND RBL 13.84,STA 727J AND RBL 13.84,STA 747 AND RBL 13.84 AT AFT CARGO COMPARTMENT:- - RESOLUTION:PERFORMED PERMANENT REPAIR LOC RBL 13.84 AND BTW BS727D PLUS 13.5INCH TO BS 727FPLUS 11INCH AND BTW BS 727F PLUS 11INCH TO BS767 PLUS 11INCH AFT, CARGO COMPARTMENT IAW B737-800 SRM 53-00-53-2R-3 REPAIR 3 THIS REPAIR IS A PERMANENT , NO FURTHER ACTION REQUIRED

Part: INTERCOSTAL — CRACKED (BS 927-947) · corrosion level 2 · airframe 64,741 hrs · 29,625 cycles

DEFECT WO74296 NR00095: CRACK WEB - INTERCOSTAL LOCATED BETWEEN BS927 TO BS947 AND RBL21 AFT C ARGO COMPARTMENT- - RESOLUTION: REPLACED INTERCOSTAL AND FASTENERS BTW BS 927 TO BS 947 AND RBL 21 AFT CARGO COMPARTMENT IAW B737-800 SRM 51-40-02 , SRM 51-10-02 ITEM 9 AND, DWG:147A7500 SHEET 11 REV

Part: FRAME — CRACKED (BS 400 S8-9R) · airframe 64,741 hrs · 29,625 cycles

DEFECT 74296 NR00025: CRACK FRAME LOCATED BS 400, BETWEEN STRINGER 8R AND STRINGER 9R AT PASSE NGER CABIN - - RESOLUTION: PERFORMED PERMANENT REPAIR ON FRAME LOCATED BS 400, BTW STRG 8R AND STRG 9R AT PASSENGER CABIN IAW EA #53-0198-23 REV 0. THIS REPAIR IS CATEGORY B INSPECTION THRESHOLD AT 50,000 FC

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 64,741 hrs · 29,625 cycles

DEFECT W/O 74298 NR00029: DETERIORATED EMERGENCY LIGHT ON LH EMERGMENCY EXIT FWD. - - - RESOLUTION (IN PROGRESS)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 64,554 hrs · 29,533 cycles

DEFECT 729450: FLAP ASSYMETRY - APPROACH PHASE OF FLIGHT - FLAPS 1 - R UP - L HALFWAY TO ONE - YAW DAMPER KICKED OFF - RAN QRH 9346, 9.32. EMERGENCY DECLARED, LANDED SAFELY. OPEN

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 64,554 hrs · 29,533 cycles

DEFECT 729450: FLAP ASSYMETRY - APPROACH PHASE OF FLIGHT - FLAPS 1 - R UP - L HALFWAY TO ONE - YAW DAMPER KICKED OFF - RAN QRH 9.46, 9.32 (EMERGENCY DECLARED, LANDED SAFELY) - - -RESOLUTION: REMOVED BOTH ENDS OF DAMAGED TORQUE TUBE ASSY REF 27-51-00. REMOVED TORQUE TUBE FROM TORQUE TUBE FITTING ASSY AND ORDERED NEW TORQUE TUBE, SHEAR BOLT, AND COLLAR. REMOVED #8 OB SUPPORT AFT FAIRING TO FACILITATE ACCESS TO FLAP TRANSMISSION FOR SERVICING REF AMM 27-51-28 DRAINED AND SERVICED #8, #7, #6, & #5 FLAP TRANSMISSION IAW AMM 12-22-51 VISUALLY INSPECTED ALL SAMPLES FOR WATER - NO WATER WATER NOTED INSTALLED NEW FLAP TORQUE TUBE IN R/H WHEEL WELL IAW AMM 27-51-58, INSTALLED # 8 CANOE FAIRING REF AMM 27-51-28 AND INSTALLED NEW R/H TORQUE TUBE ASSY AND COUPLING SEALS BETWEEN FLAP DRIVE AND #5 GEAR BOX. REF AMM 27-51-58 FLAP SYSTEM OPS CHECK TO BE PERFORMED ON N/R 0006

Part: FLAP SYSTEM — WARNING LIGHT · airframe 63,474 hrs · 29,124 cycles

DEFECT 724694: AFTER FLAPS WERE SET T 5 WITH A LE FLAPS EXT GREEN LIGHT LE FLAPS INTRANSIT AMBER LIGHT COMES ON WITH #2 AMBER LIGHT OVERHEAD PANEL THEN EXTINGISHED FLAPS WERE RAISED TO UP AND INTRANSIT AND #2 COMES ON AGAIN. RESOLUTION: PERFORMED FIM TASK 27-88 TASK 820 LEADING EDGE TRANSMITT LIGHT ILLUMINATED PREOBLEM, NO DEFECTS NOTED. PERFORMED FIM TASK 27-51 TASK 801 FSEU BITE PROCEDURE, NO DEFECT NOTED. THIS CLEARS MEL 27-4-7 MDDR# 114340.

Part: GIRT BAR — STIFF · airframe 63,082 hrs · 28,945 cycles

DEFECT: 2L GIRT BAR DIFFCULT TO REMOVE FROM CLIPS WHEN ARMING. RESOLUTION: GIRT BAR WITHIN LIMITS. REF AMM 25-66-01

Part: GIRT BAR — LOOSE · airframe 63,061 hrs · 28,937 cycles

DEFECT: 2L GIRT BAR DOOR BRACKET DOESNT HOLD GIRT BAR SECURELY. RESOLUTION: INSPECTED L2 DOOR GIRT BAR BRACKET. NO DEFECTS NOTED. GIRT BAR IS HELD SECURELY IN BRACKET. WORK PERFORMED IAW AMM 25-66-00

Part: BRAKE — DAMAGED (NR 2) · airframe 61,759 hrs · 28,425 cycles

AT GATE, NUMBER TWO TIRE BRAKE OVERHEAT. RIGHT BRAKE 5.0 AT GATE, RAMP PERSON CAME TO FLIGHT DECK AND REPORTED SMALL FIRE AND FLAMES BUT WENT OUT QUICKLY. PERFORMED FIM 32-46 TASK 808 FOR BRAKE TEMP LIGHT. FOUND LOWER BRAKE PISTION DAMAGED. PERFORMED HEAT DAMAGE INSPECTION OF AXLE REF. AMM 05-51-17 NO DAMAGE FOUND. R/R #2 BRAKE ASSY. REF AMM 32-41-41. ACFT OK FOR SERVICE.