N2807W

Part: ANGLE — CORRODED (FUSELAGE)

CORROSION ON SECONDARY HEAT EXCHANGER CLOSE OUT PANEL ATTACH ANGLE LT SIDE I/B ANGLE. INSTALLED REPAIR PER MM 53-30-1.

Part: RIB — CRACKED (NR 2 LE SLAT)

FOUND DURING MV2/F-1 LETTER CHECK, .75 INCH CRACK AT NR 2 SLAT NOSE RIB O/B SIDE OF ACTUATOR AT AFT LWR CORNER. REPAIRED PER M/M 57-54-0.

Part: ANGLE — CRACKED (AFT AIRSTAIR)

A 2 INCH VISIBLE CRACK RT LOWER TORQUE BOX SUPPORT ANGLE BELOW AIRSTAIR ACTUATOR ATTACH FITTING STA 1263 RT (MARKED). REPLACED PART PER SRM 53-10-10.

Part: RIB — CRACKED (LT WING)

FOUND DURING MV2/F 1 LETTER CHECK, .75 INCH CRACK AT NR 3 SLAT NOSE RIB O/B SIDE OF ACTUATOR AFT LWR CORNER. REPAIRED PER M/M 57-54-0.

Part: BULKHEAD ANGLE — CRACKED (BS 178)

REF NR 214, 215, 216, 217, 218 AND 219 REPAIRED STA 178 BLKHD AND REPLACED UPPER AND LWR ANGLES PER SRM 53-10-9 FIG 14. COMPLETED AND FORWARDED DATA RETRIEVAL.

Part: BATTERY PACK — DISCHARGED (L1 EXIT)

EMERG EXIT LIGHT ABOVE L1 DOOR WEAK DURING TEST. REPLACED BATTERY PACK.

Part: SKIN — DELAMINATED (LT/RT ELEVATOR)

T/E OF LT AND RT ELEV DELAMINATED FROM I/B EDGE TO 15 INCHES O/B OF ELEV TAB. REPAIRED PER MM 55-20-0 P 801.

Part: SKIN — CRACKED (FUSELAGE)

A .5 INCH CRACK ON A/C SKIN FROM RT SIDE OF AIRSTAIR CUTOUT FWD SIDE. REPAIRED PER MM 53-30-0 P 803.

Part: WEB — CRACKED (BS 1228)

A .5 INCH CRACK LIGHTENING HOLE STA 1248 ON AIRSTAIR CUTOUT VERTICAL WEB LT SIDE. A .25 INCH CRACK LIGHTENING HOLE STA 1228 ON AIRSTAIR CUTOUT VERTICAL WEB RT SIDE. REPAIRED PER MM 53-11-0 P 828.

Part: BEAR STRAP — CORRODED (BS 1070)

THE R2 DOOR SURROUND BEAR STRAP WAS FOUND CORRODED APPROX 5 ABOVE THE SKIN LAP SPLICE. THE CORROSION WAS REMOVED WITH A 2.25 X 2.25 CUTOUT IN THE BEARSTRAP. THE DAMAGE WAS REPAIRED WITH AN EXTERNAL DOUBLER AND TRIPLER PER ER/A 363324-14, REV A.

Part: PUMP — LEAKING (B-HYD SYST)

ON CLIMBOUT WITH B-SYS PUMP NR 2 B PRESSURE STARTED TO DROP TOWARD ZERO. SWAPPED B-PUMPS THEM B-SYS HYD QTY DROPPED TO ZERO. REPLACED HYD PUMP.

Part: WIRE — CROSSED (CABIN)

RT AFT EXTERIOR EMERGENCY LIGHT INOP. FOUND WIRES SWAPPED AT PLUG D5024. REPAIRED SAME AND REPLACED M957 FOR FUSES BLOWN, SYS CHKS GOOD.

Part: BRACKET — CRACKED (NR 1 SLAT ACT)

1.5 INCH VISIBLE CRACK IN NR 1 SLAT ACTUATOR ATTACH BRACKET I/B SIDE, FOUND AT E1 LTR CK. REPAIR PER M/M 57-20-21.

Part: CLAMP — FAILED (NR 1 ENGINE)

ON CLIMBOUT, GOT NUMBER 1 ENGINE FIRE WARNING, BOTH LOOPS AND BELL. RETARDED THE THROTTLE AND FIRE WARNING LIGHTS AND BELL WENT OUT. DID NOT SHUT DOWN ENGINE, DID NOT FIRE BOTTLE. RETURNED TO ATLANTA. FOUND CLAMP HAD FAILED ON THIRTEENTH STAGE DUCT IN PYLON. REPLACED CLAMP.

Part: ACTUATOR — DESTROYED (NR 4 LE SLAT)

ON CLIMBOUT THROUGH 7,000 FEET, THE A-SYSTEM HYDRAULIC QUANTITY WENT TO ZERO AND THE PRESSURE WENT TO ZERO, FOLLOWED POM. FOUND THE NR 4 SLAT ACTUATOR CASTING END BLOWN OUT. REPLACED ACTUATOR.

Part: BULKHEAD WEB — CRACKED (BS 1183)

BS 1183 BULKHEAD FOUND CRACKED IN THE WEB. STOPPED DRILLED AND REPAIRED TO SRM 53-10-9, FIG. 4.

Part: HYD MODULE — CRACKED (A HYD SYST)

SYS-A HYD QTY LEAKED BELOW 2.5 GALS COMPLETED POM PROCEDURES LEAK STOPPED WITH PRESSURE OFF. FOUND A-SYS MODULE LEAKING. BORROWED PART FROM FEDX (S/N 260SA), INSTALLED. PERFORMED OPERATIONAL CK OUT, ALL NML NO LEAKS.

Part: SKIN — CRACKED (NR 6 LE SLAT)

INNER SKIN CRACKED BETWEEN RIBS 10/11. REPAIRED PER M/M 57-54-0.

Part: DOOR — CRACKED (R1)

THE R-1 DOOR WAS FOUND CRACKED AT THE UPPER FWD CORNER. REPAIRED PER 52-12-0, FIG 805.

Part: LIGHT — INOPERATIVE (CABIN)

R2 ABOVE DOOR EXIT EMERGENCY LIGHT INOP. REPLACED EXIT LIGHT AND BATTERIES, CKS NORMAL.

Part: SKIN — FATIGUE (L1 DOOR CUTOUT)

THE FUSELAGE SKIN AND UNDERLYING DOUBLER WAS FOUND TO HAVE A ONE INCH CRACK IN THE UPPER FWD CORNER OF THE L-1 DOOR CUTOUT. REPAIRED PER DAL ER/A 303614-14AD.

Part: SKIN — CRACKED (L-1 DOOR CUTOUT)

DURING INSPECTION, FOUND 1 INCH CRACK IN THE UPPER FWD CORNER OF THE L-1 DOOR CUTOUT. REPAIRED PER ER/A 303614-14AD.

Part: WEB — CRACKED (BS 285.5-294.5)

DURING INSPECTION, THE LT SIDEWALL WEB OF THE NOSE WHEEL WELL HAS A 1.25 INCH CRACK BETWEEN STA 294.5 AND 285.5, APPROXIMATELY AT WL 170. THE REPAIR IS ACCOMPLISHED IN ACCORDANCE WITH S/B 727-53-145.

Part: ANGLE — CRACKED (NR 7 SLAT)

FOUND ON C-2 LETTER CHECK, COVE SKIN SUPPORT ANGLE CRACKED .0625 INCH BELOW NR 7 SLAT ANTI-ICE DUCT. REPAIRED PER MM 57-54-0.

Part: BUSHING — WORN (NLG DOOR)

ON CLIMBOUT FROM RIC AT 360 KTS, THE NOSE WHEEL DOORS WERE SLAMMING OPEN AND SHUT REPEATEDLY. FOUND NLG DOOR OUT OF RIG AND BUSHINGS WORN IN ROD ON FWD QUAD. REPLACED ROD AND RIGGED NLG DOORS.

Part: SKIN — CRACKED (NR 6 LE SLAT)

AFT LOWER SKIN CRACKED I/B END. REPAIRED PER M/M 57-54-0.

Part: BATTERY — DISCHARGED (CABIN)

DURING LAYOVER, MTC FOUND EMERGENCY LIGHT ABOVE AFT RIGHT SERVICE DOOR WOULD NOT TEST. REPLACED BATTERIES, NOW OPERATION IS NORMAL.

Part: SKIN — CORROSION (BS 1010-1030)

AT CV2 IN TPA, CORROSION WAS DISCOVERED ON THE FUSELAGE SKIN BETWEEN STA 1010 AND 1030 STR 23R AND 24R. A SECTION OF THE BONDED DOUBLER AT STR 24R AND TWO AREAS OF THE FUSELAGE SKIN, 4 INCH BY 1.25 INCH AND 2.75 INCH BY 2.5 INCH WERE CUT OUT TO REMOVE CORROSION. ALSO, STR 23R WAS CUT AT APPROX STA 1040 AND REMOVED UP TO STA 1010. A FILLER AND DOUBLER WAS INSTALLED, ACCOMPLISHED REPAIRS PER DL ERA 302689-14.

Part: SKIN — CORROSION (FS 720)

ADDITIONAL CORROSION WAS CUT OUT JUST AFT OF FS 720A. THE NEW CUT OUT AND THE PREVIOUS CUT OUT ARE SEPARATED BY APPROXIMATELY 5.5 INCHES. THE ORIGINAL DOUBLER WAS REMOVED AND A NEW DOUBLER FOR BOTH CUT OUTS WAS INSTALLED. THE DOUBLER DOES AND WILL CONTINUE TO BUTT UP AGAINST THE SPLICE DOUBLER INSTALLED AT FS 720 PER ER/A 210265-14.

Part: BATTERY — DISCHARGED (CABIN)

AFT RIGHT SERVICE DOOR OVERHEAD EMERGENCY LIGHT INOP. REPLACED BATTERIES, CHECKS NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN)

FWD RT SERVICE DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. REPLACED RACK AND BATTERIES, OPERATION NORMAL.

Part: ANGLE — CRACKED (FS 1263)

CRACK IN THE ANGLE OF THE FWD TRANSVERSE BEAM OF THE RT TORQUE BOX AT STA 1263. REPAIRED PER DL ERA 302068-14AD.

Part: SKIN — CRACKED (RT ELEV)

RT ELEVATOR LWR SKIN CRACKED 1 INCH AT L/E AFT OF NR 4 BALANCE BOARD. FOUND AT C-1 LTR CK. REPAIRED PER SRM 55-20-3 FIG 4.

Part: SKIN — CORRODED (FUSELAGE)

FOUND A LINE OF SMALL NICKS 6 INCHES LONG COMING DOWN FROM AFT LAV SERVICE PAN ON THE FUSELAGE SKIN WITH CORROSION. FOUND DURING C-1 LTR CK TPAMM. REPAIRED PER SRM 53-30-1, FOUND IN ALLOWABLE LIMITS.

Part: SKIN — CORRODED (FS 720)

SKIN CORRODED AT STA 720C STR 10 RT. FOUND DURING C-1 LTR CK TPAMM. REPAIRED PER SRM 53-30-3 FIG 5, TIME LIMITED DOUBLER.

Part: SKIN — CRACKED (RT ELEV)

A .5 INCH CRACK RT ELEVATOR LWR SKIN AFT OF NR 4 BALANCE BOARD. FOUND DURING C-1 LTR CK TPAMM. REPAIRED PER SRM 55-20-3 FIG 4.

Part: BULKHEAD — DAMAGED (FS 178)

PERFORM BODY STA 178 BULKHEAD ACCESS HOLE INSTALLATION PER SRM 53-10-9 PG 8 TO FOM. INSTALLED REPAIR PER SRM 53-10-9 PG 8 AND 9.

Part: RIB — CRACKED (NR 3 SLAT)

DURING SHOP INSPECTION, FOUND NR 6 RIB FOR NR 3 SLAT CRACKED. REPAIRED PER SRM 57-54-0.

Part: BALLAST — SHORTED (CABIN)

DURING CRUISE, CABIN CEILING LIGHTS CIRCUIT BRAKER TRIPPED. HAD BURNING ODOR AT SEAT ROW 13. FOUND BALLAST FOR CEILING LIGHTS SHORTED. REPLACED BALLAST OPERATION NORMAL.