N411DA

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING L/O CHECK, FOUND SVL EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTS AND PACKS, ALL CHECK OK.

Part: WIRE — BROKEN (CABIN)

CEILING EMERGENCY EXIT LIGHT NEAR OVERWING EXIT IS INOP. REPAIRED A BROKEN WIRE AT THE LIGHT ASSY CONNECTOR.

Part: SKIN — CRACKED (BS 360-480)

DURING LFEC INSPECTION PER SI 4-74176-12AD, NUMEROUS CRACK INDICATIONS WERE FOUND IN THE VARIOUS FRAME BAYS EXTENDING FROM BS 360-480 ALONG S4R. THERE WAS A PREVIOUS REPAIR PER ERA 332834-14AD, REV B WHICH WILL BE REMOVED AND INCORPORATED INTO THIS REPAIR. REPAIRED PER ERA 367552-14AD, REV A.

Part: SKIN — CRACKED (BS 360-480)

INTERNAL HFEC INSPECTION OF THE LOWER FASTENER ROW OF THE STRINGER 4L SKIN LAP SPLICE BETWEEN FS 360 AND 480 INDICATED 14 CRACKS ALONG THE PANEL LENGTH. THE SKIN LAP FOR THE PANEL WAS CUTOUT AND REPAIRED WITH AND EXTERNAL ALUMINUM DOUBLER PER ER/A 367553-14AD.

Part: FLAP TRACK — CORRODED (RT TE FLAP)

DURING OUTSIDE REPAIR OF COMPONENT AND OVERHAUL PER CMM AND MOD PER SB 727-57-0178, TYPICAL CORROSION WAS FOUND ON THE MLG BEAM AND SPOILER BEAM ATTACH PAD AND HOLES. AUTHORIZED OVERSIZED FASTENERS, BUSHING REPAIR AND LEAVING THE OVERSIZED MLG BEAM ATTACH HOLES AS-IS.

Part: FLAP TRACK — CORRODED (LT TE FLAP)

DURING OUTSIDE REPAIR, OVERHAUL PER CMM AND MOD PER SB 727-57-0178, TYPICAL CORROSION WAS FOUND TO THE FWD ATTACH LUGS AND THE MLG BEAM AND SPOILER BEAM ATTACH PADS AND HOLES. AUTHORIZED BUSHING REPAIR FOR FWD ATTACH LUG AND OVERSIZED SPOILER BEAM ATTACH HOLES. AUTHORIZED LEAVING OVERSIZED MLG BEAM ATTACH HOLE AS-IS. INSTALLED SPLICE PLATE REPAIR PER SB.

Part: SKIN — MISDRILLED (BS 1233)

FUSELAGE SKIN WAS MISDRILLED AT S11R AT BS 1233. REPAIRED PER ERA 332842-14, REV A.

Part: FITTING — CORRODED (RT MLG)

CORROSION FOUND IN THE RT MLG SUPPORT BEAM O/B BORE AND IN THE FWD AND AFT FITTINGS. REWORKED PER ERA 332851-14.

Part: FRAME — CORRODED (BS 600)

BS 600 FRAME BELOW THE CARGO FLOOR AT STR 28R WAS FOUND CORRODED. THE UPPER FRAME OF THE LOWER LOBE CTR FRAME SECTION AND SOME EXISTING REPAIRS WERE ALSO FOUND CORRODED. REPAIRED PER ERA 332893-14, REV A.

Part: SKIN — CRACKED (BS 481-680)

WHILE ACCOMPLISHING LFEC INSP PER SI 4-74176-12, ON THE S4R LAP JOINT CRACK INDICATIONS WERE FOUND BETWEEN BS 481 AND 680. HFEC CONFIRMED 15 CRACK INDICATIONS IN THE LWR FASTENER ROW OF THE LAP JOINT IN THE LWR SKIN. REPAIRED PER ERA 332838-14AD, REV A.

Part: SKIN — CRACKED (BS 430)

WHILE ACCOMPLISHING LFEC INSPECTIONS PER SI 4-74176-12AD ON S4R LAP JOINT, 2 CRACK INDICATIONS WERE FOUND BETWEEN BS 360 AND 481. HFEC INSP VERIFIED CRACK INDICATIONS. REPAIRED PER ERA 332834-14AD, REV A.

Part: SKIN — CRACKED (BS 681-740)

WHILE ACCOMPLISHING LFEC INSPECTIONS PER SI 4-74176-12 ON THE S4R LAP JOINT CRACK INDICATIONS WERE FOUND BETWEEN BS 681 AND BS 740. HFEC INSPECTION CONFIRMED 8 CRACK INDICAITONS IN THE LOWER FASTENER ROW OF THE LAP JOINT, IN THE LWR SKIN. REPAIRED PER ERA 332843-14AD, REV A.

Part: FRAME — DENTED (BS 950)

TWO DENTED AREAS WERE FOUND ON THE I/B CHORD OF THE BS 950C FRAME BETWEEN S24L AND 27L. REPAIRED PER ERA 332897-14, REV A.

Part: FITTING — CORRODED (BS 870)

CORROSION WAS FOUND IN THE BORE OF THE RT WING AFT TERMINAL FITTING. REPAIRED PER ERA 366788-14, REV A.

Part: FITTING — WORN (VERT STAB)

WEAR WAS FOUND ON BOTH ATTACH LUGS FOR THE HORIZ STAB JACK SCREW MECHANISM. WEAR WAS ON BOTH I/B AND O/B FACES OF EACH LUG. REWORKED PER ERA 332860-14, REV A.

Part: FRAME — DENTED (BS 950)

FRAME DENTED AFT CARGO COMPT LT FRAME DENTED AT STA 950B ABOVE STR 26L. REMOVED DAMAGED PER SRM 53-10-4 FIG 27. DYE PENETRANT CHECKED PER PS 900-6-3, NO CRACKS NOTED. DRILLED NEW DUCT PER SRM 53-10-4 FIG 27. REMOVED WEB FROM STA 950A TO 950B AT STR 25L. INSTALLED PER SRM 53-10-4 FIG 27.

Part: FRAME — DENTED (BS 1070)

FRAME DENTED LT FS 1070, STR 26L. REMOVED DAMAGED AREA, DYE CHECKED PER PS 900-6-3 NR 1. NO FURTHER DAMAGE FOUND. FABRICATED DOUBLER, INSTALLED DOUBLER PER SRM 53-10-4 FIG 27.

Part: SKIN — TORN (BS 990)

GOUGE IN SKIN AT THE AFT EDGE OF THE C-2 DOOR CUTOUT AT FS 990. DAMAGED AREA LOCATED AT 2-24R. SKIN, DOUBLER, TRIPLER AND BEAR STRAP ARE ALL DAMAGED. ACTION TAKEN, ERA 332858-14.

Part: FITTING — CORRODED (RT WING)

AT HMV2, FOUND CORROSION IN BORES AND MATING SEAM OF AFT RT WING AND FUS REMINAL FITTINGS. BLENDED CORROSION, CHECKED, REWORKED PER ERA 366788-14, INSTALLED BUSHNG.

Part: FRAME — CRACKED (EMER EXIT DRWAY)

OVERWING EXIT FRAME STA 761 RT, 784 LT AND 784 RT FOUND CRACKED IN I/B FLANGE. ACTION TAKEN, ERA 361976-14AD.

Part: SKIN — DAMAGED (BS 277)

LIGHTNING STRIKE DAMAGE AT AN EXISTING FASTENER IN THE SKIN BETWEEN S-7R AND S-8R AT STA 277. ACTION TAKEN, ERA 255827-14.

Part: SKIN — WORN (LT TE FLAP)

LOWER L/E SKIN WORN O/B END OF FLAP APPROX 6 INCHES LONG. REPAIRED PER MM 57-52-0 FIG 803.

Part: SPAR — DAMAGED (LT TE FLAP)

AFT SPAR RAIL DAMAGED AT 2ND FROM I/B AFT FLAP TRACK CUT OUT. REPAIRED PER M/M 57-52-0 FIG 802.

Part: SKIN — CRACKED (AIRSTAIR DOORWAY)

AT HMV2, FOUND SKIN CRACKED - EMPENNAGE EXIT, LOC AT FWD RT CORNER OF AFT AIRSTAIRS CUTOUT. FABRICATED DOUBLER PER MM 53-30-00 PG 803. STOP DRILLED CRACK, INSTALLED DOUBLER.

Part: FRAME — DENTED (BS 950)

FRAME DENTED AFT CARGO COMPT RT FRAME DENTED AT STA 950C SEVERAL PLACES FROM STR 25R TO STR 26R. CUT OUT DAMAGE PER SRM 53-10-4 FIG 27. DYE PENETRANT INSPECTED CUTOUT PER PS 900-6-3 NO 1 AND FOUND OK. DRILLED DOUBLER AND FILLER PER SRM 53-10-4 FIG 27 AND TREATED PER PS 900-2-4-1, NR 2. PAINTED PER PS 900-3-6. INSTALLED REPAIR PARTS PER SRM 53-10-4 FIG 27.

Part: FRAME — DENTED (BS 950)

FRAME DENTED AFT CARGO COMPT LT FRAME DENTED AT STA 950C SEVERAL PLACES FROM STR 27L TO 25L. REMOVED DAMAGE PER SRM 53-10-4 FIG 27, FABRICATED DOUBLER PER SRM 53-10-4 FIG 27. REMOVED FACTORY SPLICE. INSTALLED REPAIR PER SRM 53-10-4 FIG 27 REV NR 1170.

Part: SKIN — CRACKED (FUSELAGE)

SKIN CRACKED EMPENNAGE EXT LOC AT AFT I/B CORNER OF ACCESS PNL 3903 CUTOUT. FABRICATED DOUBLER PER M/M 53-30-0 PG 803. STOP DRILLED CRACK, INSTALLED DOUBLER PER MM 53-30-0 PG 803, IDENTIFIED PER PS 900-5-1 NR 4.

Part: SKIN — CRACKED (LT TE MIDFLAP)

DURING SHOP INSPECTION, THE COVE SKIN WAS FOUND CRACKED IN TWO PLACES AT THE I/B AFT FLAP DRIVE ROD CUTOUT. THE CRACK WAS REMOVED AND A DOUBLER INSTALLED PER 727 MM 57-52-0 FIG 809.

Part: RETRACT MECH — LACK OF LUBE (TE FLAPS)

OUTBOARD FLAPS WOULD NOT EXTEND PAST 15 TO 20 DEGS. DIVERTED TO JFK. PERFORMED OPS CHECK, COULD NOT DUPLICATE. DUE PREVIOUS ITEMS, SERVICED TRANS AND JACKSCREW GEARBOXES LUBED TRACKS AND JACKSCREW BALLNUTS ON OUTBOARD FLAPS.

Part: WIRE — SHORTED (ROW 12)

FOUND ON MAINT PREFLIGHT ROWS 12-19 EMERGENCY TRACK LIGHTINGINOP REPLACED BLOWN FUSE ON FWD POWER SUPPLY AFTER REPAIRINGBARE WIRES UNDER SEAT ROW 12 DEF LIGHT OPN NORMAL REPLACED FWD BATTERY PRECAUTIONARY.

Part: BATTERY — DISCHARGED (SEAT ROW 25)

SEAT ROW 25 OVERHEAD EMERGENCY LIGHT INOP. REPLACED BATTERY, OPS NOW OK.

Part: ANGLE — CRACKED (RT TE MIDFLAP)

DURING SHOP INSPECTION, THE AFT LOWER CLOSEOUT ANGLE WAS FOUND CRACKED 35 INCHES FROM THE I/B END. THE ANGLE WAS REPAIRED BY INSTALLING A DOUBLER PER 727 MM 57-52-0, FIG 802.

Part: ANGLE — CRACKED (TR TE MIDFLAP)

DURING SHOP INSPECTION, THE AFT LOWER CLOSEOUT ANGLE WAS FOUND CRACKED 19 AND 23 INCHES FROM I/B END. THE ANGLE WAS REPAIRED PER 727 MM 57-52-0, FIG 802 BY INSTALLING A DOUBLER.

Part: ANGLE — CRACKED (RT TE MIDFLAP)

DURING SHOP INSPECTION, THE AFT LOWER CLOSEOUT ANGLE WAS FOUND CRACKED 37 INCHES FROM I/B END. THE ANGLE WAS REPAIRED PER 727 MM 57-52-0, FIG 802 BY INSTALLING A DOUBLER.

Part: ANGLE — CRACKED (RT TE MIDFLAP)

DURING SHOP INSPECTION, THE AFT LOWER CLOSEOUT ANGLE WAS FOUND CRACKED 44 INCHES FROM O/B END. THE ANGLE WAS REPAIRED PER 727 MM 57-52-0, FIG 802 BY INSTALLING A DOUBLER.

Part: STIFFENER — CRACKED (NR 3 LE SLAT)

NR 3 SLAT O/B TRACK I/B SPAR STIFFENER CRACKED. REPAIRED PER MM 57-20-21 P 813.

Part: SKIN — CRCAKED (L-1 DOORWAY)

FOUND AT A-1 LETTER CHECK, 1.125 INCH CRACK AT FUSELAGE SKIN AT MAIN ENTRY DOOR UPPER HINGE CUTOUT. REPAIRED PER 53-30-3.

Part: RIB — CRACKED (NR 6 LE SLAT)

FOUND ON A-1 LETTER CHECK, NR 6 SLAT NOSE RIB CRACKED I/B SIDE OF ACTUATOR .75 INCH. REPAIRED PER M/M 57-54-0.

Part: FITTING — CRACKED (FUSELAGE)

TAIL SECTION TIE BOLT FITTING CRACKED LT I/B FITTING, CRACKED JUST O/B OF BOLT HEAD. REPLACED FITTING PER BOEING DWG 65-17509 REV M.

Part: BRACKET — CRACKED (NR 1 LE SLAT)

NR 1 SLAT ACT O/B ATTACH BRACKET CRACKED AT I/B WEB. REPAIRED PER MM 57-20-21 P 812.

Part: BATTERY — DISCHARGED (COCKPIT)

ON PREFLIGHT, COCKPIT EMERGRNCY LIGHT DID NOT ILLUM IN STBY PWR. REPLACED BATTS, OPS NOW OK.

Part: SKIN — CRACKED (LT ELEVATOR)

.5 INCH CRACK IN LOWER SKIN OF LT ELEVATOR 5 INCHES FROM I/B EDGE. REPAIRED PER SRM 55-20-3.

Part: WEB — CRACKED (BS 1223)

.0625 INCH CRACK AT RT VERT TORQUE BOX WEB LWR LIGHTING HOLE AT STA 1223 RT. REPAIR PER MM 53-11-0.

Part: SKIN — CRACKED (LT ELEVATOR)

.5 INCH CRACK IN LOWER SKIN OF LEFT ELEVATOR 5 IN FROM I/B EDGE. REPAIR PER SRM 55-20-3.

Part: STRINGER — CRACKED (VERTICAL FIN)

VERT FIN STR 9L IS CRACKED AT FIN STA 133.800. REPAIR PER MM 55-30-0.

Part: STRINGER — CRACKED (VERTICAL FIN)

VERT FIN STR 9L CRACKED AT FIN STA 157.200. REPAIR PER MM 55-30-0.

Part: LIGHT — INOPERATIVE (CABIN)

LEFT FORWARD DOOR EXIT IDENITIFIER LIGHT INOP. REPLACED POWER SUPPLY (M9026), CKS OK.

Part: SUPPORT — CRACKED (NR 7 LE SLAT ACT)

THE NR 7 SLAT ACTUATOR OUTBOARD SUPPORT BRACKET DOUBLER (P/N 66-19114-2) AT SLAT STA 288.60 IS CRACKED. THIS AREA WILL BE REPAIRED PER S/B 727-57-0130, REV 2.

Part: BULB — FAILED (CABIN)

EMERGENCY PATH LIGHT INOP AT ROW 12. REPLACED BULB AND LENS AT ROW 12.

Part: STIFFENER — CRACKED (LT WING)

FOUND ON F-1 LETTER CK, 2 SPAR STIFFENERS CRACKED 1.5. LOCATED ON INBD SIDES OF NR 2 AND NR 3 SLATS INBD SIDE OF INBD TRACK. REPAIRED PER MM 57-20-21.

Part: LIGHT — MISSING (CABIN)

35D RED TRACK LIGHT OUT. REPLACED PIGTAIL AND LENS, CHKS OK.

Part: ACTUATOR — FAILED (NR 2 LE SLAT)

HYD SYS 'A' LOSS, CLIMBING THROUGH 8000 FT. OVERWEIGHT LANDING AT SEA 159,000 LBS, SMOOTH LANDING. FOUND NR 2 SLAT ACTUATOR END CAP BLEW OFF CAUSING LOSS OF 'A' SYS HYD FLUID. REPLACED SLAT ACTUATOR. PERFORMED OVERWEIGHT LANDING INSP PER M/M. REPLACED CASE DRAIN FILTERS FOR HYD PUMPS 'A' SYS.

Part: BULB — INOPERATIVE (CABIN)

EMERGENCY TRACK LIGHTING HAD ONE BULB INOP BETWEEN ROWS 32-35. REPLACED BULB. CKS OK.

Part: SKIN — CRACKED (PAX DOOR)

A .375 INCH CRACK MAIN CABIN DOOR OUTER SKIN AT UPPER AFT CORNER BELOW GATE HINGE. INSTALLED DOUBLER PER M/M 52-11-01 FIG 804.

Part: BULB — FAILED (CABIN)

OVERWING EMERGENCY DOOR EXIT SIGNS DIM. REPLACED BULB.

Part: BULB — FAILED (CABIN)

AFT RT SERVICE DOOR EXIT SIGN DIM. RELAMPED.

Part: BATTERY PACK — DISCHARGED (CABIN)

OVERHEAD EXIT SIGN AT SEAT ROW 21 INOP. REPLACED BATT PACK M1086.

Part: BULB — FAILED (CABIN)

EXIT LIGHT AT R1 DOOR DIM. RELAMPED.

Part: BULB — FAILED (CABIN)

EXIT SIGN AT L1 DOOR DIM. RELAMPED.

Part: BULB — FAILED (CABIN)

EXIT SIGN AT OVERHEAD 1ST CLASS DIM. RELAMPED.

Part: BULB — FAILED (CABIN)

AFT AIRSTAIR EXIT SIGN DIM. RELAMPED.

Part: BULB — FAILED (CABIN)

OVERHEAD EXIT SIGN AT SEAT ROW 32 DIM. RELAMPED.

Part: BATTERY PACK — DISCHARGED (CABIN)

ON LAYOVER, FOUND RT OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED BATTERY PACK.

Part: TE WEDGE — DENTED (NR 5 LE SLAT)

NR 5 L/E SLAT T/E WEDGE UPPER SURFACE DENTED. REPLACED WEDGE PER SRM 57-43-02.

Part: WEB — CRACK (BS 1243)

FOUND DURING E-1 LETTER CHECK, .25 INCH CRACK LWR TORQUE BOX VERTICAL WEB LIGHTENING HOLE FWD OF BS 1243 LEFT SIDE. REPAIRED PER M/M 53-11-0 PAR 15.

Part: SKIN — TORN (RT ELEV)

FOUND DURING E-1 LETTER CHECK, .75 INCH TEAR RIGHT ELEVATOR LWR SKIN 15 INCHES AFT OF HINGE CENTERLINE AND 6 FEET O/B OF I/B END. REPAIRED PER SRM 55-20-3 FIG 4.

Part: EEL BATTERY PACK — DISCHARGED (CABIN)

DURING INSPECTION, RT AFT SERVICE DOOR EMERGENCY LIGHT INOP. REPLACED BATTERY PACK OPERATION NORMAL.

Part: RIB — CRACKED (NR 4 LE FLAP)

DURING SHOP INSPECTION, NR 4 L/E SLAT WAS FOUND WITH NR 6 L/E SUPPORT RIB CRACKED. REPAIRED PER MM 57-54-0 FIG 814.

Part: LE RIB — CRACKED (NR 4 LE SLAT)

DURING SHOP INSPECTION, NR 4 L/E SLAT WAS FOUND WITH CRACKED L/E RIB AT THE ACTUATOR ATTACH FITTING. REPAIRED PER MM 57-54-0 FIG 804.

Part: EEL BATTERY PACK — DISCHARGED (CABIN)

AFT LEFT AND RIGHT SERVICE DOOR EMERGENCY SLIDE LIGHT INOP. SECURED BATTERY PACK AT M983 POWER SUPPLY.

Part: ANGLE — CRACKED (NR 7 SLAT)

A .5 AND .25 CRACK ON NR 7 SLAT SUPPORT ANGLE BELOW TAI DUCT. FOUND DURING D-2 LTR CK TPAMM. REPAIRED PER MM 57-54-0.

Part: ANGLE — CRACKED (NR 3 LE SLAT)

NR 3 SLAT COVE SKIN ANGLE CRACKED UNDER TAI DUCT. FOUND DURING D-2 LTR CK TPAMM. REPAIRED PER MM 57-54-0.

Part: FUEL PUMP — SHEARED SHAFT (NR 1 ENGINE)

AFTER TAKEOFF, AT 500 FEET NR 1 ENGINE FLAMED-OUT. RETURNED BDL. TROUBLESHOOTING FOUND NO FUEL FLOW TO ENGINE. REPLACED ENGINE DRIVEN PUMP AND FUEL CONTROL, OPERATION NORMAL.

Part: DOOR FRAME — CRACKED (SERVICE DOOR)

FOUND ON CV2 CHECK, .5 INCH CRACK EXTENDING FROM LOWER AFT STOP CASTING IN FWD SVC DOOR FRAME REPAIRED PER M/M 52-12-0.

Part: ANGLE — CRACKED (NR 6 SLAT)

DURING CORROSION ISNPECTION, FOUND NR 6 SLAT WITH A .5 INCH CRACK IN ATTACH ANGLE BELOW ANTI-ICE DUCT TEE. REPAIRED PER MM 57-54-0 PG 807A.

Part: SKIN — CRACKED (NR 6 SLAT)

DURING CORROSION INSPECTION, RT WING NR 6 SLAT WAS FOUND WITH A 2.25 INCH CRACK IN LOWER AFT SKIN. REPAIRED PER MM 57-54-0 PG 801.

Part: RIB — CRACKED (NR 6 SLAT)

DURING CORROSION INSPECTION, RIGHT WING NR 6 SLAT WAS FOUND WITH A 1 INCH CRACK IN L/E RIB, JUST OUTBOARD OF INBOARD SLAT TRACK. REPAIRED PER MM 57-54-0 PG 815-815A.

Part: ANGLE — CRACKED (NR 6 SLAT)

DURING CORROSION INSPECTION, RIGHT WING NR 6 SLAT WAS FOUND WITH A .5 INCH CRACK IN O/B ATTACH ANGLE, JUST I/B OF O/B STOP. REPAIRED PER MM 57-54-0 PG 816.

Part: HORIZ WALKWAY — CORRODED (FS 303.9)

FOUND ON CV2 CHECK TPAMM, OUTBOARD LEG OF LEFT NLG HORIZONTAL WALKWAY CORRODED STA 303.9. REPAIRED PER SRM 53-10-4 AND ERA 303065-14.

Part: FLOOR BEAM — CORRODED (FS 1030)

FOUND ON CV2 CHECK TPAMM, CORROSION ON FLOOR BEAM STA 1030. REPAIRED PER SRM 53-10-8 FIG 3.

Part: SEAT TRACK — CRACKED (FS 1033)

FOUND ON CV2 CHECK TPAMM, LEFT INBD SEAT TRACK CRACKED STA 1033. REPAIRED PER SRM 53-10-5 FIG 7.

Part: SEAT TRACK — CORRODED (BS 380)

FOUND ON CV2 CHECK TPAMM, CORROSION ON SEATTRACK BS 380 RBL48. REPAIRED PER SRM 53-10-5 FIG 7.

Part: FORMER — CRACKED (FS 600)

FOUND ON CV2 CHECK TPAMM, 1 INCH CRACK FORMER UP RADIUS STA 600, REPAIRED PER SRM 53-10-4 FIG 21.

Part: SEAT TRACK — CORRODED (FS 1030-1050)

FOUND ON CV2 CHECK, CORROSION ON LEFT O/B SEAT TRACK BETWEEN STA 1030 AND 1050 BOTH SIDES OF TRACK, REPAIR. REPLACED SEAT TRACK SECTION PER CVSRM 53-10-5.

Part: SEAT TRACK — CORRODED (FS 1110-1130)

FOUND ON CV2 CHECK, CORROSION FOUND SEAT TRACK LOCATED AT LBL 25 BETWEEN 1130 AND 1110, REPAIR. REPLACED SEAT TRACK SECTION PER SRM 53-10-5 FIG 3.

Part: FLOOR BEAM — CORROSION (FS 1050)

FOUND ON CV2 CHECK, CORROSION ON BEAM TOP/BOTTOM AT STA 1050 BETWEEN LEFT INBOARD AND LEFT O/B SEAT TRACK REPAIRED PER M/M 53-20-11 PG 802.

Part: FLOOR BEAM — CORRODED (FS 1030)

FOUND ON CV2 CHECK, CORROSION TOP OF FLOOR BEAM STA 1030 AT CENTER LINE, REPAIR. FABRICATED AND INSTALLED SEC OF T CAP PER SRM 53-10-8 FIG 3.

Part: SEAT TRACK — CORRODED (FS 420)

FOUND ON CV2 CHECK, CORROSION ON SEAT TRACK O/B RT STA 420-445, REPAIRED PER SRM 53-10-5 FIG 7.

Part: SEAT TRACK — CORRODED (FS 344)

FOUND ON CV2 CHECK, CORROSION ON SEAT TRACK STA 344. REPAIRED PER SRM 53-10-5 FIG 7.

Part: SEAT TRACK — CORRODED (FS 1090-1036)

FOUND ON CV2 CHECK, CORRROSION FOUND SEAT TRACK RBL 45 BETWEEN 1090 AND 1136 TOP AND BOTTOM SIDES, REPAIR. REPLACED SEAT TRACK FROM 1110 TO 1136 PER SRM 53-10-3 FIG 7.

Part: SEAT TRACK — CORRODED (FS 380-480)

FOUND ON CV2 CHECK, CORROSION SEVERAL PLACES ON RT I/B SEAT TRACK RBL 23 FROM STA 380 - 480, REPAIR. REPLACED SEAT TRACK SECTION FROM STA 380 TO 440 PER SRM 53-10-5 FIG 7.