N490DA

Part: BATTERY PACK — DISCHARGED (AFT CABIN) · airframe 75,260 hrs · 59,056 cycles

AFT CABIN O/H EMERGENCY LIGHT BETWEEN LAVS INOP. REPLACED BATTERY PACK.

Part: ACTUATOR — LEAKING (NR 1 SPOILER) · airframe 73,648 hrs · 57,961 cycles

LOSS OF SYSTEM A HYDRAULIC IN FLIGHT. INITIAL 0 QTY INDICATION WITH NO OTHER ABNORMALS. THEN SYS A ENG 1 AND 2 PUMPS FLICKERED AND RECOVERED SEVERAL TIMES. POM PROCEDURES FOR LOSS OF SYS A COMPLIED WITH. LANDED JFKL AND TOWED TO GATE. ZERO QTY INDICATION SHOWED 0.6 GALLONS (3 QTS) AFTER STOPPING ON RUNWAY. FOUND NR 1 SPOILER ACTUATOR LEAKING. REPLACED SAME.

Part: RIB — CRACKED (SLAT) · airframe 73,576 hrs · 57,914 cycles

RIB NUMBER 7 CRACKED MANUFACTURED DOUBLER. INSTALLED DOUBLER PER 57-54-0 FIG 814 MM.

Part: SHEAR CLIP — CRACKED (BS 1263)

THE SHEAR CLIP FOR THE FS 1263 FRAME BETWEEN STRINGERS 13L AND 14L WAS FOUND WITH A 1 INCH CRACK IN THE SKIN FLANGE RADIUS. THE SKIN FLANGE WAS TRIMMED OFF TO REMOVE THE CRACK. THE SHEAR CLIP WAS RESTORED BY INSTALLING AN ALUMINUM REPAIR ANGLE PER ER/A 368904-14, REV A.

Part: BRACKET — CRACKED (LE FLAP ACTUATOR)

NR 1 LEADING EDGE SLAT I/B AND O/B ACTUATOR MOUNT BRACKETS CRACKED. REPAIRED PER MM 57-20-21.

Part: STIFFENER — CRACKED (LE FLAP)

VERTICAL SPAR STIFFENER CRACKED NR 7 SLAT O/B SIDE OF I/B TRACK. REPLACED SPAR STIFFENER PER MM 57-20-21.

Part: SKIN — CRACKED (LE FLAP)

A .5 INCH CRACK AT FWD LWR SIDE OF NR 2 MIDFLAP AT I/B AFT FLAP ACTUATING ROD CUTOUT. REPAIRED PER MM 57-52-0 AND ERA 368899-14.

Part: ANGLE — CRACKED (LE FLAP)

COVE SKIN ANGLE CRACKED 15 INCHES O/B OF NR 7 SLAT ACTUATOR ROD. REPAIRED PER MM 57-54-0.

Part: BEAM — CRACKED (CARGO DOOR)

C-2 DOOR HORIZONTAL BEAM WEB DAMAGED AT LIGHTNING HOLE AT DOOR HANDLE SNUBBER SRM 52-30-2D FIG 802D.

Part: POWER SUPPLY — FAILED (BS 800)

RT FWD EMERG EXIT HATCH EMERGENCY LT INOP. FOUND FUSE BROKEN OFF IN SOCKET OF PWR SUPPLY. REPLACED SAME.

Part: BATTERY PACK — DISCHARGED (LT EMER EXIT)

ON L/O, FOUND LT OVERWING EMER EXIT LIGHT INOP. REPLACED BATTERY PACK, CHECKS GOOD.

Part: BATTERY PACK — DISCHARGED (L1 DOORWAY)

ON L/O, FOUND L1 EMER EXIT LIGHT INOP. REPLACED BATTERY PACK, RACK AND REFLECTOR.

Part: MOUNT — CORRODED (NR 2 ENGINE)

ON HUSHKIT MOD, FOUND NR 2 AFT ENG MOUNT CORRODED. REPLACED MOUNT.

Part: ANGLE — CORRODED (NR 2 ENG MOUNT)

ON HUSHKIT MODIFICATION, NR 2 ENG AFT MOUNT CHORD ANGLE CORRODED. REPLACED ANGLE WITH NEW MANUFACTURED PART LEFT SIDE.

Part: RIB — CRACKED (HORZ STAB)

LT ELEV HINGE SUPPORT RIB CRACKED BETWEEN NR 3 AND 4 BAL BOARDS AT LOWER END. REPAIRED PER MM 55-10-31.

Part: SKIN — CRACKED (BS 480-680)

LFEC INSPECTION OF THE STRINGER 26L SKIN LAP SPLICE BETWEEN FS 480 AND 680 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED A FEW CRACKS IN CONSECUTIVE SKIN FRAME BAYS. THE ENTIRE SKIN LAP SPLICE WAS CUTOUT AND REPAIRED WITH AN EXTERNAL REPAIR. THE SKIN FROM FS 480 TO 520 WAS REPLACED WITH A NEW PIECE TO ELIMINATE EXISTING CORROSION REPAIRS.

Part: SKIN — CRACKED (BS 680-740)

LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 680 AND 740 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED 43 TOTAL CRACKS ALONG THE PANEL. THE SKIN LAP SPLICE WAS CUT OUT ALONG THE ENTIRE PANEL LENGTH AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 367029-14AD, REV A.

Part: SKIN — CRACKED (BS 360-481)

LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 360 AND 481 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED 8 CRACKS IN THREE FRAME BAYS. THE SKIN LAP SPLICE WAS CUT OUT ALONG THE PANEL LENGTH AND REPAIRED WITH AND EXTERNAL ALUMINUM DOUBLER PER ER/A 367026-14AD, REV A.

Part: SKIN — CRACKED (BS 480-680)

LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 480 AND 680 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED 71 TOTAL CRACKS. THE SKIN LAP SPLICE WAS CUT OUT ALONG THE PANEL LENGTH AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 367028-14AD, REV A.

Part: SKIN — CORRODED (BS 480-500)

THE FUSELAGE SKIN WAS FOUND WITH AN AREA OF CORROSION AT FS 485 AND STRINGER 28R. THE CORROSION WAS REMOVED WITH A 7 X 3.5 CUTOUT. THERE WERE THREE OTHER REPAIR DOUBLERS NEAR THIS AREA FOR REPAIRS OF SIMILAR CUTOUTS. THE REPAIRS WERE REMOVED RESULTING IN 4 SKIN CUTOUTS BETWEEN FS 480 AND 500 AND BETWEEN S-27R AND 27L. THE CUTOUTS WERE REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER AND TRIPLER PER ER/A 366528-14.

Part: ANGLE — CORRODED (BS 740)

FOUND DURING MV-1 CHECK, CORROSION ON SUPPORT ANGLE AT STA 740 STR 27 RT. REPLACED ANGLE PER M/M 53-11-0 FIG 826.

Part: FLOORBEAM — CORRODED (BS 344)

FOUND DURING MV-1 CORROSION VISIT NRC 46, CORROSION AT FLOORBEAM STA 344 RBL 5 TO LBL 60 UPPER AND LOWER SIDES. REPAIRED PER SRM 53-10-8 FIG 11.

Part: FRAME — CRACKED (PAX DOORWAY)

FOUND DURING MV-1 CORROSION VISIT NRC 16, .25 INCH CRACK VISIBLE AT AFT ENTRY DOOR FRAME UPPER LT LOCATION. REPAIRED PER SRM 53-10-9 FIG 11.

Part: BATTERY PACK — DISCHARGED (CABIN)

LT MID WING SLIDE EMERGENCY LIGHT INOP. REPLACED BATTERY RACK M954, OPS CHKS GOOD.

Part: BATTERY — DISCHARGED (CABIN)

BOTH FWD EXIT SLIDE EMERGENCY LIGHTS INOP. REPLACED BATTERY ON RACK M982, OPS CHKS GOOD.

Part: BATTERY — DISCHARGED (CABIN)

FLASHLIGHT NOT BLINKING. REPLACED FLASHLIGHT BATTERY, BULB, AND PLAC. OPS CKS GOOD.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

FOUND EMERGENCY LIGHT SECTION IN CABIN INOP. REPLACED PWR SUPPLY, SYSTEM CHECKS NORMAL.

Part: SPAR — CRACKED (LT ELEVATOR)

THE LT ELEVATOR REAR SPAR WAS FOUND WITH A TYPICAL CRACK AT THE SECOND FROM THE OUTBD END HINGE. THE CRACK WAS STOP DRILLED PER THE REQUIREMENTS OF BOEING S/B 727-55-0089 AND IS BEING TRACKED PER ER/A 364195-14AD. THE PERMANENT REPAIR WILL MODIFY THE SPAR PER S/B 727-55-0089.

Part: CHANNEL — CRACKED (BS 1263)

THE FS 1263 UPPER CHANNEL ON THE LT AFT VENTRAL STAIRWELL TORQUE BOX WAS FOUND WITH A 1.5 INCH CRACK IN THE TYPICAL LOCATION PER S/B 727-53-0129. THE DAMAGED CHANNEL WAS REPLACED PER THE S/B AND DOCUMENTED PER ER/A 364193-14AD.

Part: BATTERY — DISCHARGED (CABIN)

ON PREFLIGHT, FWD EMERGENCY FLASHLIGHT WOULD NOT TEST. REPLACED BATT.

Part: BALLAST — FAILED (CABIN)

SMOKE IN AFT 48 SECTION. REPLACED AFT LAV LIGHT BALLAST M276.

Part: ANGLE — CRACKED (BS 870)

FOUND ON B1 LETTER CK, .5 INCH CRACK FWD LOWER RT INBD VERTICAL KEEL BEAM ANGLE AT STA 870. REPAIRED PER SRM 53-10-9.

Part: STIFFENER — CRACKED (L/E SPAR)

WING L/E SPAR STIFFENER CRACKED NR 4 SLAT INBD TRACK INBD SIDE. REPLACED ANGLE PER M/M 57-20-21.

Part: WATER HEATER — OVERHEATED (AFT LAVATORY)

SMOKE REPORTED IN AFT CABIN BY F/A, CONFIRMED BY SECOND OFFICER. BOTH AFT LAV SMOKE DETECTORS ALARMED, DID SMOKE CLEARANCE CHECKLIST. REPLACED AFT LAV WATER HEATER, CHECKS NORMAL.

Part: POWER CONTL UNIT — LEAKING (LT ELEVATOR)

ATB - DUE TO HYDRAULIC FLUID LOSS FROM THE LEFT ELEVATOR, POWER CONTROL UNIT LEAKS.

Part: LIGHT — INOPERATIVE (CABIN)

EMERGENCY EXIT LIGHT ABOVE L-2 DOOR DID NOT COME ON DURING TEST. REPLACED LIGHT ASSY, OPS NORMAL.

Part: BATTERIES — DISCHARGED (CABIN)

CENTER AISLE EMERGENCY EXIT LIGHT BETWEEN AFT LAVS DID NOT COME ON DURING TEST. REPLACED BATTERIES AND BULBS OPS NORMAL.

Part: ANGLE — CRACKED (NR 2 LE SLAT)

COVE SKIN ATTACH ANGLE CRACKED 1 INCH AT ANTI-ICE TUBE CUTOUT, NR 2 SLAT. REPAIRED PER M/M 57-54-0.

Part: SKIN — DAMAGED (BS 1080)

AIRCRAFT STRUCK BY A GROUND SERVICE TRUCK, DAMAGE CONSISTED OF A DENTED SKIN, A BROKEN STRINGER AND A CRACKED SHEAR CLIP. THE DENT WAS REMOVED WITH A CUTOUT AT STA 1080, THE STRINGER HAS BEEN CUT AND WILL BE SPLICED IN THE BAYS FWD AND AFT OF THE DAMAGE. ALSO, THE CLIP ABOVE STR-22L HAS BEEN TRIMMED OFF. ALL DAMAGE WILL BE REPAIRED PER THE SRM.

Part: SKIN — DENTED (BS 1080-1100)

FROM AC LOG 759101001, FUSELAGE SKIN DENTED FS 1080 THROUGH 1100 STR 23L. STR 23L AND SKIN REPAIRED PER ERA 303624-14.

Part: DOUBLER — CRACKED (NR 4 TE MIDFLAP)

DURING SHOP INSPECTION, NR 4 MIDFLAP WAS FOUND WITH CRACKED DOUBLER AT AFT CLOSE OUT RIB LOWER AFT CORNER. REPAIRED PER MM 57-52-0.

Part: LE SKIN — WORN (LT TE MID FLAP)

L/E EDGE SKIN WORN AT I/B END OF NR 1 MIDFLAP. REPAIRED PER MM 57-53-00.

Part: RIB — CRACKED (BS 760)

DURING ACCOMPLISHMENT OF EO 4-58560-3AD, A CRACK WAS DISCOVERED IN THE VERTICAL FLANGE OF THE LBL 70.5 WING RIB CHORD. THE CRACK RAN FROM ONE OF THE UPPER FASTENERS IN THE VERTICAL FLANGE AT STA 760.95 DOWN TO THE HORIZONTAL FLANGE. THIS CRACK REQUIRES AN ALTERNATE METHOD OF REMOVAL TO THE ONE IN THE REFERENCED EO. THE RIB CHORD IS MANUFACTURED FROM 7075-T6 EXTRUSION. REPAIRED PER DL ERA 302686-14AD.

Part: FRAME — CRACKED (LT SERVICE DOOR)

DURING INSPECTION, A 2 INCH CRACK WAS FOUND EMANATING FROM THE CORNER OF THE UPPER HINGE CUTOUT ON THE FWD FRAME OF THE LT AFT SERVICE DOOR. IN ACCORDANCE WITH B727 SRM 52-40-2 FIG 4, A DOUBLER WAS INSTALLED AROUND THE DAMAGE.

Part: DOUBLER — CRACKED (NR 2 TE MIDFLAP)

NR 2 MIDFLAP WAS FOUND TO HAVE CRACKED DOUBLER AT AFT LOWER SPAR ANGLE REPAIR AT I/B QUADRANT CUTOUT. REPAIR WAS PERFORMED PER M/M 57-52-0 FIG 802. FOUND DURING SHOP MTC VISIT.

Part: RIB — CRACKED (RT WS 629)

FOUND ON HMV, RIGHT WING STRINGER TO RIB FASTENER HOLE HAS CRACK INDICATION AT STA. 629, 3RD STRINGER FWD FROM AFT SPAR. STOP DRILLED CRACK PER M/M 57-13-0.

Part: SKIN — PUNCTURED (CARGO DOOR)

DURING INSPECTION, C-3 CARGO DOOR WAS FOUND WITH INNER SKIN PUNCTURED, REPAIRED PER SRM 52-00-3.

Part: STRINGER — CRACKED (WS 656.5)

FOUND DURING HMV, RT OUTER WING UPPER STRINGER TO RIB SHOWS CRACK INDICATION ON FASTENER HOLE AT W.S. 656.5, STRINGER 10. MANUFACTURED REPAIR DOUBLER PER M/M 57-13-0 AND INSTALLED DOUBLER PER M/M 57-13-0, PG. 801.

Part: SKIN — DENTED (LT AILERON)

DURING INSPECTION, FOUND LEFT OUTBOARD AILERON WITH DENTS IN UPPER SKIN. ACCOMPLISHED REPAIRS PER SRM 57-50 -5.

Part: DOUBLER — DISBONDED (FS 1158-1183)

FUSELAGE SKIN REPAIR AT AFT LAVATORY SERVICE PANEL CUTOUT, FS 1158 TO FS 1183, BETWEEN S-20L AND S-24L. DURING ACCOMPLISHMENT OF EO 4-69078-3AD, THE INTERNAL BONDED DOUBLER WAS FOUND DISBONDED IN SEVERAL LOCATIONS AROUND THE AFT LAVATORY SERVICE PANEL. AFFECTED UNITS S-14L AND S-20L SKIN ASSY: 65-54583-156, S-20L/S-26L SKIN ASSY: 65-54583-142; -125 SKIN; -126 DOUBLER; 65-25607-2 TRIPLER. FAA/DER APPROVAL FORM 8110-3, DTD 11-16-95.

Part: RIB — CRACKED (NR 5 SLAT)

DURING HMV, FOUND NR 5 SLAT, NR 1 RIB WAS CRACKED. REPAIRED CRACKED RIB PER M/M 57-54-0.

Part: RIB — CRACKED (NR 3 SLAT)

DURING HMV, FOUND NR 3 SLAT, NR 12 RIB WAS CRACKED. FABRICATED REPAIR DOUBLER AND INSTALLED PER 57-54-0.

Part: RIB — CRACKED (NR 2 SLAT)

DURING HMV, FOUND NR 2 SLAT, RIB NR 7 WAS CRACKED. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR DOUBLER PER M/M 57-54-0 PG 818.

Part: FRAME — CRACKED (BS 930)

DURING HMV, FOUND STATION 930 FRAME ABOVE PREVIOUS REPAIR CRACKED BETWEEN BOTTOM OF WINDOW AND STRINGER 14L. REPAIR DOUBLER WAS MADE AND INSTALLED PER M/M 53-10-4 FIG 25.

Part: RIB — CRACKED (NR 2 SLAT)

DURING HMV, FOUND NR 2 SLAT, RIB NR 6 WAS CRACKED. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR DOUBLER PER M/M 57-54-1 PG 818.

Part: RIB — CRACKED (NR 6 SLAT)

DURING HMV, FOUND NR 6 SLAT, NR 12 RIB WAS CRACKED. STOP DRILLED NR 12 RIB AND REPAIRED CRACK PER M/M 57-54-0 FIG 814.

Part: RIB — CRACKED (NR 6 SLAT)

DURING HMV, FOUND NR 6 SLAT, NR 7 RIB WAS CRACKED. STOP DRILLED CRACK AND REPAIRED RIB PER M/M 57-54-0 FIG 814.

Part: RIB — CRACKED (NR 4 SLAT)

DURING HMV, FOUND NR 4 SLAT, NR 2 RIB WAS CRACKED. FABRICATED REPAIR AND INSTALLED PER M/M 57-54-0 PG 818.

Part: RIB — CRACKED (NR 7 SLAT)

DURING HMV, FOUND NR 7 SLAT, NR 8 RIB CRACKED AND NR 10 RIB MISSING FASTENER AND ONE IS LOOSE. REPAIRED NR 8 PER M/M 57-54-0 PGS 818 AND 819. REPLACED LOOSE AND MISSING FASTENER ON NR 10 RIB.

Part: RIB — CRACKED (NR 4 SLAT)

DURING HMV, FOUND NR 4 SLAT, NR 3 RIB WAS CRACKED. MANUFACTURED AND INSTALLED REPAIR PER M/M 57-54-0 PG 818.

Part: RIB — CRACKED (NR 2 SLAT)

DURING HMV, FOUND NR 2 SLAT, RIB NR 8 IS CRACKED. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR DOUBLER PER M/M 57-54-0 PG 819.

Part: BUSHING — MISSING (STRUT DOOR)

FOUND DURING HMV, NR 5 FLAP TRACK FWD STRUT DOOR HINGE BUSHING MISSING. REMOVED FWD FITTING AND MACHINE BORED PER M/M 57-43-0 AND INSTALLED BUSHING PER M/M 57-43-0.

Part: BULKHEAD — CRACKED (FS 870)

FOUND AT HMV, FS 870 BULKHEAD CRACKED AT APU BLEED AIR DUCT CUTOUT AT LWR O/B CORNER. REPAIRED PER SRM 53-10-9.

Part: BLKHD SUPPORTS — WORN (BS 720)

FOUND AT HMV, RT VERTICAL BULKHEAD SUPPORTS WORN AT FLOATING MOUNT BOLTS TO CABIN FLOORBEAM STRINGER 26R AND 22R, C-1 BIN FS 720D. REPAIRED PER SRM 53-10-9 FIG 9.

Part: BLKHD SUPPORTS — WORN (BS 720)

FOUND AT HMV, LT VERTICAL BULKHEAD SUPPORTS WORN AT FLOATING MOUNT BOLTS TO CABIN FLOORBEAMS ABOVE STRINGER 26L AND 22L, FS 720D C1 BAG BIN. REPAIRED PER SRM 53-10-9 FIG 9.

Part: RIB — CRACKED (NR 2 SLAT)

DURING HMV, FOUND NR 2 FLAT, RIB NR 18 CRACKED AT UPPER SKIN AREA. STOP DRILLED CRACK AND FABRICATED REPAIR DOUBLER PER M/M 57-54-00 FIG 809. INSTALLED DOUBLER.

Part: WEB — DAMAGED (VENTRAL STAIRS)

DURING HMV, FOUND STATION 1240 RIGHT SIDE LOWER WEB IN VENTRAL STAIRS HAS TEMPORARY REPAIRS. REMOVED REPAIR AND INSTALLED PERMANENT REPAIR PER M/M 53-11-0 PG 832 AND ID TAGGED PER PS 900-5-1.

Part: WEB — DAMAGED (VENTRAL STAIRS)

DURING HMV, FOUND STATION 1240, LEFT SIDE LOWER WEB IN VENTRAL STAIRS HAS TEMPORARY REPAIRS. REMOVED REPAIR AND INSTALLED PERMANENT REPAIR PER M/M 53-11-0 PG 832 AND ID TAGGED PER PS 900-5-1.

Part: BRACKET — CRACKED (NR 2 FLAP ACT)

DURING HMV, FOUND NR 2 FLAP ACTUATOR SUPPORT BRACKET CRACKED AT UPPER O/B CORNER. REMOVED SUPPORT BRACKET AND INSTALLED DOUBLER PER M/M 57-20-1. REINSTALLED SUPPORT BRACKET.

Part: BRACKET — CRACKED (NR 2 FLAP ACT)

DURING HMV, FOUND NR 2 FLAP ACTUATOR SUPPORT BRACKET CRACKED AT UPPER AND LOWER CORNERS OF I/B SIDE. REMOVED FLAP ACTUATOR, REMOVED SUPPORT BRACKET AND INSTALLED DOUBLER PER M/M 57-20-1 PG 811. REINSTALLED ACTUATOR.

Part: STRINGER — CRACKED (VERT STAB)

FOUND AT HMV, STRINGER 11L CRACKED AT STA 1342 INSIDE VERT STAB. REPAIRED PER MM 53-30-0 PG 803.

Part: STRINGER — CRACKED (VERT STAB)

FOUND AT HMV, STRINGER 8R CRACKED IN VERTICAL STAB INTERIOR IN 2ND BAY DOWN. REPAIRED PER MM 55-30-0 PG 803.

Part: EEL — INOPERATIVE (CARGO DOOR)

EXTERIOR EMERGENCY LIGHT ON AFT CARGO DOOR INOP. NEEDS RACK M957 FWD TO MCO AND PLAC. REPLACED RACK, OPERATION NORMAL.

Part: EEL — INOPERATIVE (COCKPIT)

COCKPIT EMERGENCY LIGHT INOP. REPLACED RACK, OPS NORMAL.

Part: VALVE — FAILED (NR 2 ENGINE)

ON CLIMBOUT, HAD NR 2 ENGINE START VALVE LIGHT ILLUMINATE. PER CHECKLIST, ENGINE WAS SHUTDOWN. FOUND NR 2 ENGINE START VALVE WITH SOLENOID SEPARATED FROM HOUSING. REPLACED VALVE, OPERATION NORMAL.

Part: WEB — CRACKED (NR 6 SLAT)

FOUND ON F1 LTR CK, NR 6 SLAT OTBD ACT ROD END WEB CRACKED AFT SIDE. REPAIRED PER M/M 57-54-0 PAR 3.

Part: BULLNOSE — CRACKED (NR 4 LE FLAP)

CRACK AT I/B BULLNOSE HINGE ATTACH POINT, NR 4 KRUGER FLAP. REPAIRED PER SRM 57-50-3 PG 32.

Part: ANTI-ICE DUCT — CRACKED (NR 4 LE FLAP)

WHILE IN SHOP 380, THE NR 4 KRUEGER FLAP ANTI-ICE DUCT TORQUE TUBE WAS FOUND WITH TWO CRACKS EXTENDING FROM AN EXISTING CUT OUT LOCATED 22.5 INCH FROM THE I/B EDGE OF THE FLAP. REPAIRED PER DL ERA 270445-14.

Part: DUCT — BROKEN (AC COMPARTMENT)

DURING CLIMB-OUT, AIRCRAFT WOULD NOT HOLD PRESSURE, SELECTED ALTERNATE BLEED WITH NO HELP. DIVERTED TO MCO. FOUND LEFT PACK WATER SEPARATOR ASSEMBLY LEAKING AIR. ALSO, FOUND DUCT FROM MIX VALVE TO SEPARATOR ASSEMBLY BROKEN IN SEVERAL PLACES. REPLACED DUCT OPERATION NORMAL.