N213UP

Part: MECHANISM — OUT OF RIG (MANUAL EXTEND)

ON DEPARTUE FROM LAN AT GEAR RETRACT (GEAR HANDLE UP) RED DOOR LIGHT (FRONT) AND " LEFT GEAR DOOR" ILLUMINATED, PER CHECKLIST RECYCLED O F GEAR (BACK DOWN) RED "LT GEAR AND RT GEAR" AND "LT GEAR DOOR AND R T GEAR DOOR ILLUMINATED. PER CHECKLIST LEFT GEAR HANDLE DOWN REMAIND ER OF FLIGHT. FOUND LT MLG MANUAL EXTEND MECHAINISM IN THE GEAR EXTEND POSITION. R ESET AND PERFORMED GEAR SWING.

Part: LIGHT — MALFUNCTIONED (CREW DOOR)

INSPECTION TYPE:N/A EMERGENCY EXIT LIGHT OVER CREW ENTRY DOOR ILLUM IN FLIGHT. *S/D* REMOVED AND REPLACED ENTRY DOOR EMERGENCY EXIT LIGHT GROUND OPS NORMAL.

Part: WIRE — BROKEN (STALL WARNING) · airframe 28,500 hrs · 22,105 cycles

INSPECTION TYPE:C, AT ROTATION STICK SHAKER BEGAN AND CONTINUED UNTIL AIRCRAFT LANDED AND NOSE WHEEL TOUCHED DOWN. REPAIRED BROKEN WIRE W1129-301-22R AT STA 560 PER WDM 20-30-12 OP CHECKED STALL WARNING SYSTEM PER MM 34-18-00, OPS CHECKED GOOD.

Part: WIRE — BROKEN (STALL WARNING)

INSPECTION TYPE:N/A AT ROTATION STICK SHAKER BEGAN AND CONTINUED UNTIL AIRCRAFT LANDED AND NOSE WHEEL TOUCHED DOWN. REPAIRED BROKEN WIRE W1129-301-22R AT STA-560 PER WDM-20-30-12. OP CHECKED STALL WARNING SYSTEM PER MM 34-18-00. OPS CHECKS GOOD.

Part: WEB — CRACKED (FUSELAGE) · airframe 29,061 hrs · 27,906 cycles

INSPECTION TYPE: C, TWO CRACKS AND ONE MISSING FASTENER ON UPPER FLANGE OF WEB BETWEEN BS 400 AND BS 420, WL 206, BL 0. REMOVED WEB AND L ANGLE FABRICATED NEW WEB AND L ANGLE AND INSTALLED IAW SRM 51-10-3, 51-20-1, 51-20-2 AND 51-20-15

Part: STIFFENER — CORRODED (FUSELAGE) · airframe 29,061 hrs · 27,906 cycles

INSPECTION TYPE:C CORROSION IN RT MLG WW ON STIFFENER AND LOWER CHANNEL AT BS 919, WL 188, RBL 65 REMOVED CORRODED STIFFENER, FABRICATED AND INSTALLED PER SRM 51-10-6, 51-30-2, 51-10-1 AND BOEING DRAWING 65-16335 PL AND SHT 2 AT BS 919, WL 188, RBL 65

Part: LINE — LEAKING (O2 SYSTEM)

INSPECTION TYPE:PFLT 1ST OBS 02 PRESS LINE LEAKING. *S/D* REMOVED CAP AND INSTALLED NEW O2 FLEX LINE (P/N 10-60174-36) (SP0707172) PER M/M 35-00-00/201-204. INSTALLED DEMAND DILUTER REGULATOR AND TESTED PER M/M 35-11-31, LEAKED CK''ED BOTH LINE AND REGULATOR, CK''S OK.

Part: STRUCTURE — CRACKED (FUSELAGE)

INSPECTION TYPE:IN, CRACK FOUND IN LIGHTENING HOLE, AFT AIRSTAIRS AREA AT APPROX STATION 1283 AT WL 175, LT SIDE. STOPPED DRILLED CRACK PER SRM 51-10-1/11, ITEM 9A.

Part: LIGHT — INOP (COCKPIT)

COCKPIT EMERGENCY LIGHT INOP. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AND TESTED PER MM 33-50-101. OPS CHECK GOOD.

Part: BEAM — CORRODED (LT MLG)

INSPECTION TYPE:SI, LT MLG BEAM IS CORRODED AT NR 4 FLAP TRACK MOUNT BOLT HOLES. REMOVED CORROSION AND REPAIRED LG BEAM PER ER NR 99-6038.

Part: CHORD — CORRODED (BS 345-350)

INSPECTION TYPE:SI WHILE WORKING CARD NR919297 DISCOVERED GOUGES AND CORROSION ON BS 345-350 RBL 20 WL 148 (DAMAGED RT NOSE GEAR DRAG BRACE SIDE CHORD). REMOVED AND REPLACED PER SRM 51-30-2.

Part: FLAP TRACK — CORRODED (TE FLAPS)

INSPECTION TYPE:SI, NR 5 FLAP TRACK IS CORRODED AT FWD ATTACH LUG AND AT SPOILER BEAM ATTACH POINT. REPLACED NR 5 FLAP TRACK. REMOVAL AND INSTALLATION ACCOMPLISHED ON TC NR C57-581-04-4A.

Part: WING — CORRODED (84-5)

INSPECTION TYPE:SI NR 4 FLAP TRACK CORRODED AT SPOILER BEAM MOUNT BOLT HOLES AREA AND FWD FITTING MOUNT BOLT HOLE. REPLACED NR 4 FLAP TRACK. INSTALLATION OF NEW NR 4 TRACK WILL ACCOMPLISHED ON TC NR C57-581-04-3D.

Part: FLAP TRACK — CORRODED (NR 6)

INSPECTION TYPE:SI NR 6 FLAP TRACK IS CORRODED AT FWD ATTACH LUG AND AT SPOILER BEAM ATTACH POINT. REPLACED NR 6 FLAP TRACK. INSTALLATION OF NEW NR 6 FLAP TRACK WILL BE ACCOMPLISHED ON TC NR C57-581-04-4D.

Part: FRAME — CRACKED (BS 360)

INSPECTION TYPE:SI, FRAME IS CRACKED AROUND FASTENER HOLE AT BS 360 LBL 68, WL 303 JUST ABOVE STR 8. DAMAGE WAS OUT OF LIMITS. CUT OUT DAMAGE AREA 2.0' X 2.4 X .050, FABRICATED REPAIR DOUBLER OUT OF 7075.0. 50. SENT TO HEAT TREAT TO-T6 CONDITION AND INSTALLED REPAIR IAW SRM 51-40-3, SRM 51-30-2.

Part: SEAT TRACK — CORRODED (BS 700)

INSPECTION TYPE:SI, SEAT TRACK CORRODED AT BS 700 LBL 25 WL 208. REPLACED SEAT TRACK EXTRUSION FROM BS 690 TO BS 720D+10 PER 727 SRM 53-10-5.

Part: FRAME — CORRODED (BS 720)

INSPECTION TYPE:SI, CORROSION ON FRAME HAT SECTION AT BS 720E FRAME ABOVE STR 5R TO STR 15R. CORROSION OUT OF LIMITS, FABRICATED NEW FRAME, REPLACEMENT PER SRM 53-10-4.

Part: SEAT TRACK — CORRODED (BS 372-377)

INSPECTION TYPE:SI, CORROSION ON SEAT TRACK B STA 372 TO 377, LBL 45, WL 208. CORROSION CLEAN-UP BEYOND ACCEPTABLE LIMITS. FABRICATED AND INSTALLED REPLACEMENT SEAT TRACK PER SRM 51-30-5 AND 51-30-8.

Part: FRAME — CRACKED (BS 360)

INSPECTION TYPE:SI, BS 360 FRAME IS CRACKED AT NUT PLATE HOLE, BS 360 WL 218, LBL 68. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR PARTS PER SRM 51-40-3 PG 1-6.

Part: SEAT TRACK — CORRODED (BS 580-600)

INSPECTION TYPE:SI, SEAT TRACK CORRODED BETWEEN 580 - 600 RBL 45 WL 208. REPLACED SEAT TRACK RBL 45 BS 540 TO 610 PER SRM 53-10-5.

Part: SEAT TRACK — CORRDED (BS 950-1010)

INSPECTION TYPE:SI, SEAT TRACK CORRODED AT BS 950F - 1010 LBL 45 AT NUT PLATE HOLES. CORROSION FOUND TO BE OUT OF LIMITS PER SRM 53-10-1 FIG 3. REMOVED AND REPLACED SEAT TRACK FROM BS 950E BS 1020 LBL 45 PER 53-10-5.

Part: SEAT TRACK — CORRODED (FUSELAGE)

INSPECTION TYPE:SI, SEAT TRACK CORRODED AT BS 950B-950C LBL 25 WL 208. CORROSION FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. REMOVED AND REPLACED SEAT TACK FROM BS 950+10 TO BS 950F+10 LBL 25 PER SRM 53-10-5.

Part: SEAT TRACK — CORRODED (BS 480-520)

INSPECTION TYPE:SI, SEAT TRACK CORRODED BETWEEN BS 480 - 520 BL 0, WL 208. CORROSION CLEAN-UP BEYOND ACCEPTABLE LIMITS. FABRICATED AND INSTALLED REPLACEMENT TRACK PER SRM 51-10-8 AND 53-10-5.

Part: STRINGER — CORRODED (WS 224.5-251)

INSPECTION TYPE:SI, CORROSION (C57-571-01.02-02) RW FUEL CELL INTERIOR AROUND FASTENERS ON STR 4 BETWEEN WS 224.5 AND WS 251.0. REPAIRED PER ER 99-6010 FILE NR 727-57-2110.

Part: STRINGER — CORRODED (WS 251-277.5)

INSPECTION TYPE:SI, CORROSION (C57-571-01.02-02) RW FUEL CELL INTERIOR ON STR 4 AROUND SEVERAL FASTENERS BETWEEN WS 251.0 AND WS 277.5. REPAIR WORK DONE PER ER 99-6010 FILE NR 727-57-2110.

Part: STRINGER — CORRODED (WS 277.5-304)

INSPECTION TYPE:SI, CORROSION IN 3 AREAS R/W FUEL CELL INTERIOR, UPPER SURFACE OF LOWER SKIN BETWEEN WS 304 AND WS 277.5 STR 10-11. REMOVED CORROSION PER SRM 51-10-6, REPAIRED STRINGER 10 PER SRM 57-10-4 AND ER 99-6058.

Part: FLOORBEAM — CORRODED (FUSELAGE)

INSPECTION TYPE: SI, CORROSION ON FLOORBEAM UPPER TEE BS 620 RBL 26 TO 43. CORROSION FOUND TO BE OUT OF LIMITS ON CHORD AT RBL 31-36.5. PERFORMED FLOORBEAM REPAIR PER SRM 53-10-8.

Part: SEAT TRACK — CORRODED (BS 680-740)

INSPECTION TYPE:SI SEAT TRACK CORRODED AT BS 680-740 LBL 45 WL 208. REMOVED AND REPLACED SEAT TRACK FROM BS 660-740 PER SRM 51-30-2 AND 53-10-5 FIG 1.

Part: BEAM — CORRODED (WING)

INSPECTION TYPE:SI, SPOILER BEAM MOUNT PAD FOR NR 6 FLAP TRACK IS CORRODED (ON WING SIDE). REMOVED AND REPLACED SPOILER BEAM MOUNT PAD PER SRM 51-20-151, 51-30-2.

Part: BATTERIES — DISCHARGED (EMER EXIT)

INSPECTION TYPE:N/A, EMERGENCY EXIT LIGHT OVER MAIN FWD ENTRY DOOR INOP. CHANGED BATTERIES IN BATTERY PACK, OPS CKS GOOD.

Part: BATTERY PACK — DISCHARGED (COCKPIT)

INSPECTION TYPE-N/A, EMERGENCY LIGHTS INOP IN COCKPIT AND ENTRY DOOR. REPLACED EMERGENCY BATTERY PACK ASSY'S.

Part: FIRE LIGHT — ILLUMINATED (COCKPIT)

INSPECTION TYPE N/A, RED FIRE WARNING LIGHT ON MASTER GLARESHIELD ILLUMINATED ON CLIMBOUT. NO OTHER FIRE LIGHTS ASSOCIATED WITH IT. SILENCED BELL AND LIGHT WENT OUT. ALL FIRE LIGHTS TESTED. PERFOMRED TEST ON FIRE WARNING A & B, CHECKED FIRE LOOPS A & B, FOUND NO DISCREPANCIES

Part: SKIN — CRACKED (RT ELEVATOR)

INSPECTION TYPE-C, X-RAY INSP EXHIBITS LINEAR INDICATIONS IN RT VIEW NR 30 AND REQUIRES INVESTIGATION. REPAIRED RT ELEVATOR IAW SRM 55-20-3.

Part: SKIN — CRACKED (RT ELEVATOR)

INSPECTION TYPE-C, X-RAY INSP EXHIBITS LINEAR INDICATIONS IN RT VIEW NR 18 AND REQUIRES INVESTIGATION. REPAIRED RT ELEVATOR IAW SRM 55-20-3.

Part: FLAP — DELAMINATED (RT TE AFT FLAP)

INSPECTION TYPE-C, RIGHT WING INBOARD AFT FLAP IS DELAMINATED 74.5 INCHES INBOARD FROM THE OUTBOARD END AT THE TRAILING EDGE. REPAIRED AREA IAW SRM 51-40-6.

Part: LIGHT — INOPERATIVE (CABIN)

INSPECTION TYPE-N/A, WITH EMERGENCY LIGHT SWITCH IN OFF POSITION, SHUTTING OFF A/C POWER, THIS UNIT COMES ON AND MUST BE RESET MANUALLY. REMOVED AND REPLACED UNIT, OPS CK NORMAL.

Part: CLOCK — BAD GROUND (COCKPIT F/E)

DURING TAKEOFF AND FLIGHT, WHEN F/O O2 MASK METAL COMES IN CONTACT WITH F/E CLOCK ON F/E'S PNL, SPARKS FLY OFF OF MASK AND CLOCK. FOUND BAD GROUND. WIRE RETERMINATED, NEW GROUND LUG AND OP'S CHECK OK.

Part: LIGHT — INOPERATIVE (COCKPIT)

MAINTENANCE REPORTED, COCKPIT EMERGENCY EXIT LIGHT LOOSE. COCKPIT EMERGENCY EXIT LIGHT SECURING CLAMPS ADJUSTED ASSY RESECURED AND TESTED SERVICEABLE AS PER MM 33-50-01.

Part: STRUT — FLAT (NLG)

CREW REPORTED, AFTER TAKEOFF NOSE GEAR INDICATED OPEN. ON RECYCLE ALL DOORS WERE OPEN WHEN HANDLE PLACED OFF, MAIN INDICATED DOWN. ALL 3 OPEN WHEN HANDLE PLACED DOWN, ALL INDICATIONS NORMAL. REPLACED NLS SHOCK STRUT SEALS IAW 12-15-24 AND OPS CHECKED GOOD.

Part: RIBS — CORRODED (RT AILERON)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND 2ND, 4TH, 5TH AND 6TH RIBS FROM I/B END CORRODED ON RT I/B AILERON. REMOVED CORRODED RIBS AND INSTALLED NEW RIBS PER SRM 51-00, 51-30-2, 51-10-1.

Part: BULLNOSE — CRACKED (NR 4)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND NR 4 BULLNOSE F/B ATTACH POINT IS CRACKED AT BOTH I/B ATTACH POINTS. REMOVED CRACKED BULLNOSE, INSTALLED SERVICEABLE BULLNOSE IAW SRM 51-30-2 MM 27-81-01.

Part: AIR INTAKE — CORRODED (BS 1200)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND PULLED FASTENER IN NR 2 ENG DUCT, BL O APPROX BS 1200. FOUND CORROSION IN THE LOCATION OF PULLED FASTENER. REMOVED DAMAGED SECTION AND REPAIRED 1AW 727 SRM 54-10-3.

Part: HINGE TAB — CORRODED (RT AILERON)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND R/W I/B AILERON TAB FITTINGS ARE CORRODED. REMOVED CORRODED TAB FITTINGS, INSTALLED NEW TAB FITTINGS IAW SRM 51-30-2 MM 27-10-11.

Part: HINGE TAB — CORRODED (LT AILERON)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND LEFT WING I/B AILERON FWD, LOWER BALANCE PANEL HINGE PIN IS CORRODED. REMOVED CORRODED HINGE PIN, INSTALLED NEW HINGE PIN IAW 27-10-21.

Part: SKIN — DISBONDED (LT TE FOREFLAP)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND LT WING I/B FOREFLAP HAS LARGE DISBONDS IN CENTER OF FLAP ON THE UPPER SURFACE. REPAIRED PER SRM 51-40-6 AND MM 51-20-02.

Part: HINGE PIN — CORRODED (LT AILERON)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND LEFT WING I/B AILERON FWD, LOWER BALANCE PANEL HINGE PIN IS CORRODED. REMOVED CORRODED HINGE PIN, INSTALLED NEW HINGE PIN IAW 27-10-21.

Part: HINGE TAB — CORRODED (LT AILERON)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND L/W I/B AILERON TAB FITTINGS ARE CORRODED. REMOVED CORRODED FITTINGS, REPLACED WITH NEW FITTINGS IAW SRM 51-30-2 MM 27-10-11.

Part: SKIN — DISBONDED (LT TE FOREFLAP)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND LT WING I/B FOREFLAP HAS DISBOND 12 INCHES FROM I/B END UPPER SURFACE. REPAIRED PER SRM 51-40-6 AND MM 51-20-02.

Part: EEL BATTERY — DISCHARGED (CABIN)

WHILE ON GROUND, MAINTENANCE FOUND BOTH EMERGENCY EXIT LIGHTS INOP. REPLACED BATTERIES IN COCKPIT, LT ASSY, AND REPLACED FORWARD ENTRY LIGHT ASSY. OPS CKS OK. S/N OFF 72254. S/N ON 4663.