N278NV

ATA 3350

Part: EPSU — NO TEST (ZONE 200) · airframe 49,212 hrs · 21,174 cycles

(AIRCRAFT NOT GROUNDED) DURING EPSU SYSTEM TEST BAT/EPSU(10WL) FWD L FAULT. / FOLLOWING TSM 33-51-00-810-829-A, REMOVED AND REPLACED 10WL EPSU BATTERY IAW AMM 33-51-38-000-002-A AND AMM 33-51-38-400-002-A. OPS CHECK SATISFACTORY."

ATA 2560

Part: BATTERY — INOPERATIVE (ZONE 200) · airframe 49,120 hrs · 21,127 cycles

(AIRCRAFT NOT GROUNDED) FLASHLIGHT BATTERY IN AFT JUMPSEAT INOP OR NOT CHARGING. REPLACED BATTERY IN AFT JUMPSEAT PER AMM 25-60-02"

ATA 2560

Part: HORN — FALSE ACTIVATION (ZONE 200) · airframe 48,112 hrs · 20,629 cycles

(AIRCRAFT NOT GROUNDED) UNCOMMMANDED EVACUATION HORN ACTIVATION, RESET PER QRH, RESET SUCCESSFUL.. UNCOMMMANDED EVACUATION HORN ACTIVATION / RESET PER QRH/ RESET SUCCESSFUL. NOTED BY MOC."

ATA 2120

Part: UNKNOWN — ODOR (CABIN) · airframe 47,993 hrs · 20,585 cycles

(AIRCRAFT NOT GROUNDED) FROM APPROX 15000 FT TO 1000 FT DIRTY SOCK SMELL IN CABIN ON DESCENT. FLIGHT DECK FO NOTICED SMELL 4,000 TO 1,000 FT. COMPLIED WITH TC A32X-21-000-200. COMPLY WITH TASK CARD 21-000-003 WITHIN 10 CALENDAR DAYS. CW LVL 3 REF TC.

ATA 2560

Part: GIRT BAR — OUT OF ADJUST (ZONE 800) · airframe 47,163 hrs · 20,206 cycles

(AIRCRAFT NOT GROUNDED) L1 DOOR SLIDE ARMING LEVER DOES NOT STAY FULLY IN ARMED POSITION / REF LP 2075758 FOR SLIDE REPLACMENT, LEVER WAS STILL NOT STAYING IN FULL ARM POSITION. REMVOED SLIDE, ADJUSTED GIRT BAR , AND INSTALLED SLIDE. L1 DOOR SLIDE LEVER STAYS IN ARM POSTION. REF AMM 25-62-44-000-012-A AND 25-62-44-400-007-A. OP'S CHECK GOOD."

ATA 5730

Part: SKIN — CRACKED (LT WING LE) · airframe 44,177 hrs · 18,591 cycles

(MAJOR REPAIR - DISCREPANCY NOTED DURING HEAVY) LH WING LEADING EDGE , CRACK FOUND ON UP STOP #3 / L/H WING LEADING EDGE SKIN AT UP STOP #3 PERMANENTLY REPAIRED AS PER SRM 57-41-11-300-006 REV.148. REPAIR CATEGORY A. NO FURTHER ACTION REQUIRE. P/N: 2024T3 .063 P/O: 1701026."

ATA 2750

Part: APPU — FAULTED (TE FLAP SYS) · airframe 44,087 hrs · 18,547 cycles

(EMERGENCY DECLARED) F/CTL FLAPS LOCKED WING TIP BRK ON GOING FROM FLAPS 1 TO 2 ON APPROACH / WHILE ACCMP TSM 27-51-00-810-819-A ON PAGE 2 STEP #4 SUBSTEP 4 PARA A, VISUALLY EXAMINED THE APPU (30VU) FOR SIGNS OF WATER THROUGH THE SIGHT GLASS, FOUND WATER DAMAGE INSIDE THE APPU (RIGHT WING FIN 30VU). REMOVED AND REPLACED 30CV APPU IAW AMM 27-51-18-000-001-A AND 27-51-18-400-001-A. OPS CHECK GOOD.

ATA 2750

Part: FLAP SYSTEM — FAULTED · airframe 44,087 hrs · 18,547 cycles

(EMERGENCY DECLARED) F/CTL FLAPS LOCKED WING TIP BRK ON GOING FROM FLAPS 1 TO 2 ON APPROACH / WHILE ACCMP TSM 27-51-00-810-819-A ON PAGE 2 STEP #4 SUBSTEP 4 PARA A, VISUALLY EXAMINED THE APPU (30VU) FOR SIGNS OF WATER THROUGH THE SIGHT GLASS, FOUND WATER DAMAGE INSIDE THE APPU (RIGHT WING FIN 30VU). REMOVED AND REPLACED 30CV APPU IAW AMM 27-51-18-000-001-A AND 27-51-18-400-001-A. OPS CHECK GOOD."

ATA 2560

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 43,067 hrs · 18,053 cycles

FOUND AFT MEGAPHONE TO BE EXPIRED / REMOVED AND REPLACED AFT MEGAPHONE REF LOPA. OPS CHECK GOOD."

ATA 3350

Part: EPSU — UNKNOWN (UNKNOWN) · airframe 43,050 hrs · 18,046 cycles

BAT/EPSU FAULT WHILE PERFORMING EPSU TEST (10WL & 13WL) / REMOVED AND REPLACED EPSU BATTERY (10WL & 13WL) IAW AMM 33-51-38-000-002-A & 33-51-38-400-002-A."

ATA 3350

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 41,542 hrs · 17,303 cycles

RIGHT OVERWING EMEGENCY EXIT LIGHTS AND SIGN INOP / REMOVED AND REPLACED EMERGENCY BATTERY REF TSM 33-51-00-810-812-A OPS CHECK GOOD"

ATA 2720

Part: HINGE ARM — CRACKED (VERTICAL STAB) · airframe 41,229 hrs · 17,133 cycles

THE HINGE ARM BR1 AND ATTACH FORK FITTING OF THE VERTICAL STABILIZER WAS FOUND WITH A CRACK AT HOLES #5 AND #7 DURING INSPECTIONS. MAINTENANCE ATTEMPTED TO REMOVE THE CRACK DAMAGE BY OVERSIZING. THE CRACK STILL REMAINS AT EACH HOLE WITH A DIAMETER OF 0.279".