N211UP

Part: SMOKE DETECTOR — INOPERATIVE (CARGO BAY)

INSPECTION TYPE:N/A, MCD SMOKE DETECTOR NO TEST. RELAMPED SMOKE DETECTOR.

Part: REGULATOR — INOPERATIVE (COCKPIT O2 MASK)

INSPECTION TYPE:N/A, CAPTS O2 REG INOP. *S/D* REMOVED AND REPLACED 02 REG.

Part: FIRE LIGHT — MALFUNCTIONED (APU)

INSPECTION TYPE-N/A, BLOCK TURN BACK DUE TO APU FIRE LIGHT ON INDICATION. PULLED THE SWITCH AND PRESS THE DISCHARGE BUTTON. DEFERRED APU PER MEL 49-1 AND DEFERRED FIRE WARNING SYSTEM PER MEL 26-11-0-2.

Part: COALESCER BAG — DIRTY (CABIN)

CREW REPORTED STRONG FUMES IN COCKPIT SHUT DOWN PAX INFLIGHT, PREVIOUS WRITE-UP SDF, MX DEFERED APU M 152622. SUBMITTER STATES, SUSPECT FUEL FUMES, VAPORS IN COALESTER BAGS AOG NEW BAGS AND O-RINGS FOR T-FITTING FOR SOLENOID VALVE. REPLACED BAGS AND O-RINGS TO FUEL SOLENOID VALVE RAN ENGINE FOR SEVERAL HRS NO VAPORS NOTED.

Part: SKIN — CRACKED (NR 2 LE FLAP)

INSPECTION TYPE-SI, NR 2 SLAT LOWER SKIN FASTENERS SHEARED AND CRACK EMITTING FROM FASTENER HOLE JUST BELOW UPSTOP (I/B). REMOVED AND REPLACED NR 2 SLAT IAW MM 27-81-11.

Part: FITTING — CORROSION (TE FLAP)

INSPECTION TYPE:SI CORROSION (C57-581-06.00-03) NR 1 FORWARD TRACK FITTING ON ONE LUG FACE AND THE LARGE FASTENER ATTACH HOLES. REMOVED FITTING, REWORKED PER ER NR98-2405, REINSTALLED SERVICABLE FITTING.

Part: SKIN — CORROSION (BS 823)

INSPECTION TYPE:SI CORROSION (C53-224-05.00-01) ON UPPER SKIN OF FUEL CELL BS 823 LBL 34 WL 196. REMOVED CORROSION BLENDED AND REFINISHED PER ER NR 98-2375.

Part: SHEAR TIE — CORROSION (BS 660)

INSPECTION TYPE-SI, CORROSION (C53-111-01.00-02) FWD CARGO BAY SHEAR TIE AT BS 660 AT STR 26 RT ON FWD FACE. CORROSION OUT OF LIMITS. REMOVED SHEAR TIE AND INSTALLED NEW SHEAR TIE IAW SRM 51-30-2.

Part: TRACK — CORROSION (NR 1 TE FLAP)

INSPECTION TYPE-SI, CORROSION (C57-581-06.00-03) NR 1 FLAP TRACK FWD LUG INTERFACE. FLAP TRACK REMOVED, REPAIRED AND RETURNED TO SERVICEABLE CONDITION AT MACHINE SHOP TO BE INSTALLED ON TC NR C57-581-04-3D.

Part: TRACK — CORROSION (NR 2 TE FLAP)

INSPECTION TYPE-SI, CORROSION (C57-581-06.00-03) IN NR 2 FLAP TRACK CENTER MOUNT HOLE. FLAP TRACK REMOVED, REPAIRED AND RETURNED TO SERVICEABLE CONDITION BY NEWELL CORP JOB NR 11804 TRACK TO BE INSTALLED ON TC NR C57-581-04-3D.

Part: SKIN — CORROSION (BS 470)

INSPECTION TYPE-SI, CORROSION (6-53-20) AT ANTENNA CUT OUT BOTTOM OF FUSELAGE 20 AFT OF E-BAY DOOR, BS 470 WL 138.5 BL 0. REMOVED CORROSION, FABRICATED DOUBLER AND INSTALLED IAW SRM 53-30-1, 51-10-6, 53-30-3, 51-30-5.

Part: CLIP — CORRODED (BS 720)

INSPECTION TYPE:SI CORROSION (C53-224-01.00-01) ON FRAME AND STRINGER CLIPS AT STA 720B STR CLIPS 5-8 RT FRAME AT STR 2-10 RT STR CLIPS 4-9 LT CORROSION ON STRINGER CLIPS AT BS 720B STR 5 AND 6 RIGHT, 9 RIGHT AND STR 5 AND 6 LEFT WERE FOUND OUT OF LIMITS PER SRM 51-10-6. NEW CLIPS WERE INSTALLED PER SRM 53-30-2 AND MM 51-20-21.

Part: FLOORBEAM — CORRODED (BS 720)

INSPECTION TYPE:SI CORROSION (C53-111-01.00-02)FWD CARGO BAY BS 720 LOWER FLANGE OF FLOORBEAM IN AND AROUND NUT PLATE HOLES LBL 45 TO RBL 25 WL 200, A 2.2 BY .9 BY .125 AREA OF THE LOWER FLANGE AT LBL 16 WAS FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. A STANDARD FLOORBEAM L ANGLE EXTRUSION REPAIR WAS INSTALLED PER SRM 53-10-8, MM 51-20-151 AND MM 51-20-31.

Part: SEAT TRACK — CORRODED (BS 520-683)

INSPECTION TYPE:SI MAIN DECK SEAT TRACK BS 520-683 RBL 45 WL 208 HAS CORROSION ON FLANGE AND IN WELL AREA, AS MARKED. CORROSION FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. NEW SEAT TRACK FABRICATED PER SRM 53-10-5 AND INSTALLED PER SRM 51-10-2.

Part: E1 RACK — WATER CONTAM (E/E COMPT)

ON FINAL APPROACH, FLAPS WERE SELECTED TO 2 DEGREES. ALL POWER TO AIRCRAFT WAS LOST EXCEPT CAPTAIN'S INSTRUMENTS. ALL LIGHTS DIMMED AND NO INDICATION ON ENGINEER'S PANEL (PANEL WAS DARK) AFTER A PACK WAS DOWNLOADED. POWER CAME BACK ON. NR 1 AND NR 2 BUS. FOUND WATER INTRUSION IN FWD PORTION OF E/E. REMOVED WATER AND CLEANED ALL UNITS ON E1 RACK. PERFORMED ENG RUN ON ALL 3 ENGS. W/LOAD. NO DEFECTS NOTED. OPS CHK OK.

Part: SKIN — DELAMINATION (RT TE FORE FLAP)

INSPECTION TYPE: C. RIGHT WING INBOARD FOREFLAP HAS AREA OF DELAMINATION ON LOWER SURFACE INBOARD TRAILING EDGE. REPAIRED PER SRM 51-40-06.

Part: RIB — CRACKED (RT TE FORE FLAP)

INSPECTION TYPE: C. RIGHT WING INBOARD MIDFLAP HAS CRACKED RIB AT CENTER FOREFLAP TRACK OUTBOARD RIB. REMOVED AND REPLACED CRACKED RIB IAW SRM 51-30-2, OHM 57-52-01 MM 27-51-00.

Part: SHEAR TIE — CORRODED (BS 1130)

INSPECTION TYPE: C. CORROSION ON SHEAR TIE AT BS 1130 RBL 10 WL 149. REMOVED CORROSION FROM SHEAR TIE AT STA 1130 RBL 10 WL 149. REWORK DEEMED OUT OF LIMITS IAW 53-10-1. REPAIRED SHEAR TIE IAW SRM 53-10-4.

Part: SKIN — DISBOND (RT TE FOREFLAP)

INSPECTION TYPE-C, RIGHT WING I/B FOREFLAP 10 INCHES FROM I/B END UPPER SURFACE HAS AREA OF DISBOND. REPAIRED DISBONDS, 10 INCHES FROM I/B END AND AT 39 INCHES FROM I/B END IAW SRM 51-40-6.

Part: SKIN — DISBOND (RT TE FOREFLAP)

INSPECTION TYPE: C. RIGHT WING INBOARD FOREFLAP 65 FROM INBOARD END UPPER SURFACE HAS SMALL DISBOND. REPAIRED DISBOND ON RT WING INBOARD FOREFLAP IAW SRM 51-40-6.

Part: HAT SECTION — CORRODED (BS 304)

INSPECTION TYPE: C. CORROSION AT BS 304 RBL 12 WL 207.5 AT HAT SECTION. REMOVED, FABRICATED FROM EXTRUSION STOCK, AND REPLACED FLOOR STRUCTURE HAT SECTION IAW SRM'S 51-30-2, 51-20-4, 51-10-6, 51-10-2.

Part: WEB — CORRODED (BS 575-580)

INSPECTION TYPE: C. CORROSION ON WEB STA 575-580 RBL 22 WL 152. MECH REMOVED CORROSION, REWORK DEEMED OUT OF LIMITS IAW SRM'S 53-20-1 51-30-2, 51-10-2 AND MM 51-20-151.

Part: CHANNEL — CORRODED (BS 302)

INSPECTION TYPE: C. CORROSION AT BS 302 LBL 12-RBL 12 WL 207.5 AT NUTPLATES IN U-CHANNEL. REMOVED, FABRICATED, AND REPLACED FLOOR STRUCTURE U-CHANNEL IAW SRM'S 51030-3, 51-30-8, 51-20-4, AND 51-10-6, 51-10-2.

Part: FRAME — CORRODED (BS 720)

INSPECTION TYPE: C. CORROSION ON LOWER FLANGE OF FRAME STA 720A WL 149 RBL 7-10. CUT OUT DAMAGED SECTION AND ACCOMPLISHED REPAIR IAW SRM 53-10-4.

Part: SPLICE — CORRODED (BS 675-685)

INSPECTION TYPE: C. CORROSION ON STR 28R SPLICE STA 675-685 WL 149. REMOVED, FABRICATED FROM STOCK, AND REPLACED STRINGER SPLICE IAW SRM'S 51-10-6, 51-10-1, 51-30-2, AND 51-10-5.

Part: SHEAR TIE — CORRODED (BS 950)

INSPECTION TYPE: C. CORROSION ON FRAME AROUND FASTENERS AT BS 950F RBL 3 WL 151. REMOVED CORROSION FROM FRAME AT STA 950F RBL 3 WL 151. REWORKED FRAME FOUND TO BE WITHIN LIMITS IAW SRM 53-10-1, HOWEVER, CORROSION WAS FOUND ON SHEAR TIE OUT OF LIMITS IAW SRM 53-10-1. REPAIRED SHEAR TIE IAW SRM 53-10-4.

Part: SHEAR TIE — CORRODED (BS 500)

INSPECTION TYPE: C. CORROSION ON SHEAR TIE STA 500 RBL 17-22 WL 150. MECH REMOVED CORROSION FROM SHEAR TIE AT STA 500 RBL 17-22 WL 150. REWORKED DEEMED OUT OF LIMITS IAW SRM 53-10-1. REPAIRED SHEAR TIE IAW SRM 53-10-4.

Part: SPLICE — CORRODED (BS 675-685)

INSPECTION TYPE: C. CORROSION ON STR 27R SPLICE STA 675-685 AREA MARKED. REMOVED, FABRICATED FROM STOCK, AND REPLACED STRINGER SPLICE IAW SRM'S 51-10-1, 51-10-6, AND 51-10-5 AND 51-30-2.

Part: ANGLE — CORRODED (BS 610-613)

INSPECTION TYPE: C. CORROSION ON SUPPORT ANGLE STA 610-613 RBL 13 WL 158. REMOVED, FABRICATED AND REPLACED ANGLE IAW SRM'S 51-30-2, 53-10-2 AND MM 57-20-31.

Part: RIB — CRACKED (RT TE FOREFLAP)

INSPECTION TYPE: C. RT WING INBOARD MIDFLAP HAS CRACKED NOSE RIB IN L/E AT CENTER FOREFLAP TRACK INBOARD OF TRACK. REMOVED DAMAGED RIB, INSTALLED NEW RIB, ALL WORK DONE PER SRM'S 51-30-2 AND 51-30-5.

Part: BATTERY — DISCHARGED (CABIN)

MAINTENANCE FOUND CREW FWD ENTRY DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERIES. OPS CHECK GOOD.

Part: EEL BATTERY — DISCHARGED (FLIGHT DECK)

MAINTENANCE REPORTED EMERGENCY EXIT LIGHT ON OVERHEAD ON ENTRY DOOR INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERIES. PERFORMED OPS CHECK. OP CHK GOOD ON GROUND.