N805EA

Part: ANGLE — CRACKED (NO.12 SPOILER) · airframe 51,400 hrs · 31,947 cycles

NO. 12 SPOILER ACTUATOR ATTACH BRACKET CRACKED OUT BOARD ENDREPLACED ATTACH ANGLE

Part: BATTERY — DISCHARGED (CABIN) · airframe 50,992 hrs · 31,639 cycles

FWD GALLEY DOOR EMERGENCY EXIT LIGHT INOP. WILL NOT TEST, REPLACED BATTERIES AND BULBS OPERATIONAL CHECKS NORMAL.

Part: FUEL CONTROL — MALFUNCTIONED (NR 3 ENGINE) · airframe 50,700 hrs · 31,440 cycles

ON CLIMBOUT AUS NUMBER 3 ENGINE SLOWLY ROLLED BACK TO IDLE. ENGINE SHUTDOWN ON FINAL DFW. REPLACED FUEL PUMP AND FUEL CONTROL RIGGED AND TRIMMED ENGINE, ALL OPS CHECK NORMAL.

Part: RIB — CRACKED (L/E SLAT) · airframe 50,015 hrs · 30,953 cycles

L/E NOSE RIB ON NR 5 SLAT I/B SIDE OF ACTUATOR ROD END IS CRACKED. REPAIRED PER M/M 57-54-000-8 AND ERA 382989-14.

Part: SWITCH — CONTAMINATED (NOSE) · airframe 48,581 hrs · 30,040 cycles

NOSE GEAR RED UNSAFE LIGHT ILLUM IN FLT ON GEAR EXTENSION RED AND GREEN NOSE GEAR IND LIGHT ILLUM. MTC FOUND THE NOSE GEAR RED LIGHT ILLUM AT THE GATE CLEANED THE CANNON PLUG FOR THE NOSE GEAR LOCK SWITCH AND OPS CHECK NORMAL PER THE MTC MANUAL.

Part: STRINGER — CRACKED (VERT STAB) · airframe 48,577 hrs · 30,037 cycles

VERT STAB STRINGER 6R CRACKED AT STA 6.372 REPAIRED PER MM 55-30-000-8 FIG 803

Part: STRINGER — CRACKED (STR 6R STA 6.372) · airframe 48,577 hrs · 30,037 cycles

VERT STAB STR 6R CRACKED @ STA 6.372 REPAIRED PER M/M 55-30-000-8 FIG 803

Part: LIGHT — INOPERATIVE (CABIN) · airframe 48,514 hrs · 29,991 cycles

PAX SEAT 15 & 29 EMERGENCY LIGHTS INOP. RE-ATTACHED CONNECTOR AT SEAT ROW 15 AND RELAMPED SEAT ROW 29.

Part: ACTUATOR — BYPASSING (NLG) · airframe 47,982 hrs · 29,639 cycles

ON GEAR EXTENSION MAIN GEAR EXTENDED NORMALLY NOSE GEAR DID NOT. FOUND LOCK ACTUATOR BYPASSING INTERNALLY. REPLACED SAME.

Part: ACTUATOR — LEAKING (RT MLG DOOR) · airframe 47,895 hrs · 29,583 cycles

COMPLETE LOSS OF A SYSTEM HYD UPON GEAR RETRACTION. FOUND RT GEAR DOOR ACTUATOR LEAKING. REPLACED SAME PER M/M.

Part: CONNECTOR — INOPERATIVE (CABIN) · airframe 47,518 hrs · 29,327 cycles

RED EMERGENCY LIGHT INOPERATIVE INBD SIDE OF FWD COAT CLOSET. FOUND WIRE PULLED FRM CONNECTOR. REPAIRED CONNECTOR

Part: ANGLE — CRACKED (NR 6 SLAT) · airframe 46,927 hrs · 28,930 cycles

FOUND ON C1 LETTER CK, TWO .25 INCH CRACKS IN THE NUMBER 6 SLAT LOWER COVE SKIN ATTACH ANGLE. REPAIRED PER MM 57-54-000-8.

Part: FUEL HEATER — FAILED (NR 1 ENGINE) · airframe 45,287 hrs · 27,815 cycles

NEAR TOP OF CLIMB FL330 NR 1 OIL TEMP WAS 140 DEG CELSIUS. REMAINED IN YELLOW FOR 15 MIN. PERFORMED POM. REPLACED NR 1 FUEL HEAT VALVE, CKS GOOD.

Part: ACTUATOR — FAILED (RT MLG DOOR) · airframe 45,268 hrs · 27,803 cycles

THE RIGHT MAIN LANDING GEAR WOULD NOT EXTEND NORMALLY. CHECKLIST PROCEDURES FOLLOWED, GEAR WAS MANUALLY EXTENDED (IE CRANKED DOWN). NORMAL INDICATIONS APPEARED AFTER MANUAL EXTENSION. LANDING UNEVENTFUL. INSTALLED 3000 PSI GAUGE TO UPLINE OF GEAR ACTUATOR AND FOUND ZERO PRESSURE. REPLACED DOOR SEQUENCE VALVE, NO HELP. REPLACED RT GEAR DOOR ACTUATOR PER M/M. GEAR RETRACTS AND EXTENDS NORMALLY. ALL INDICATIONS GOOD.

Part: FRAME — CORRODED (FUSELAGE) · airframe 44,954 hrs · 27,590 cycles

THE VERTICAL LEG OF THE LOWER CHORD OF THE FRONT SPAR ON THE LT WING WAS FOUND CORRODED AT FSS 402. THE CHORD PLATE WAS ALSO FOUND WITH CORROSION DAMAGE ON ITS LOWER SURFACE IN THE SAME AREA. DAMAGE WILL BE REPAIRED BY NESTED ANGLES AND A STRAP. ER/A 334398-14.

Part: SEQUENCE VALVE — CHAFED (RT MLG WW) · airframe 44,822 hrs · 27,505 cycles

AFTER T/O LOST A SYS HYD FLUID. AIR TURNBACK TO ABQ. FOUND LINE IN RT MAIN GEAR FROM SEQUENCE VALVE CHAFED THROUGH. MTC REPLACING SAME.

Part: SEAL — LEAKING (PAX DOOR)

AIRCRAFT WOULD NOT HOLD SCHEDULED CABIN PRESSURE WITH SINGLE PACK OPS AT FL 210. CABIN WAS 8000 FT, CLIMBING 500-700 FEET PER MIN. DESCENDED TO 15,000 TO HOLD LEVEL AT 8000 FEET CABIN PRESSURE. PRESSURIZED ACFT. FOUND AIR LEAKS AT L-1 AND R-1 DOOR SCUFF PLATES. REPAIRED PLATES AND SEALS ON BOTH DOORS. REPLACED RIGHT PNEUMATIC HIGH PRESSURE REGULATOR AS PRECAUTION.

Part: ANGLE — CRACKED (NR 4 SLAT)

COVE SKIN ANGLE CRACKED 2 PLACES NR 4 SLAT O/B OF ACTUATOR ROD END. REPAIRED PER MM 57-54-0.

Part: ANGLE — CRACKED (NR 3 SLAT)

COVE SKIN ANGLE CRACKED NR 3 SLAT I/B OF ACTUATOR ROD END REPAIR PER MM 57-54-0.

Part: ANGLE — CRACKED (NR 6 SLAT)

LOWER COVE SKIN ATTACH ANGLE CRACKED AT NR 6 SLAT I/B STOP PAD. REPAIRED PER M/M 57-54-0 FIG 812 & ERA 368813-14.

Part: CONNECTOR — LOOSE (ROW 4AB)

FIRST CLASS CABIN EMERGENCY LIGHTS WON'T TEST. RESEATED PIN AT QUICK DISCONNECT AT SEAT 4AB. SYSTEM CHECKS NORMAL.

Part: SKIN — DAMAGED (CARGO DOOR)

ON SHOP VISIT, DAMAGE WAS FOUND TO THE TOP HALF OF THE C1 DOOR, OUTER SKIN. THE SKIN WAS TRIMMED BETWEEN THE NR 3 AND NR 4 STOP BEAMS AND REMOVED TO THE UPPER EDGE. A NEW SECTION WAS FABRICATED AND SPLICE INSTALLED. THE SPLICE CONSISTED OF AN EXTERNAL DOUBLER AND TRIPLER.

Part: WIRE — BROKEN (ROW 26D)

EMERGENCY LIGHT AT SEAT 26D INOP. FOUND BROKEN WIRE AT CONNECTOR. SPLICED WIRE, OPS CHECK GOOD.

Part: VALVE — INOPERATIVE (RT WING)

WHILE DEPARTING ATL, CENTER FUEL GAUAGE WAS READING 2500 LBS LOWER, WHILE RT WING GAUGE WAS READING HIGHER BY THE SAME. TWO UNITS TRIM REQUIRED FOR LEVEL FLT. AFTER RETURNING TO GATE, FOUND NR 3 TANK VALVE SWITCH IN THEOPEN POSITION DUE TO A BROKEN GUARD COVER ON THE WING REFUELING STATION. ALSO FOUND THE DEFUEL VALVE DEFECTIVE. TRANSFERRED FUEL ON THE GROUND WITH THE DEFUEL VALVE IN THE CLOSED POSTION. REPLACED DEFUEL VALVE.

Part: BALLAST — FAILED (CABIN)

AFT CABIN AISLE FLUORESCENT LIGHTING (OVERHEAD) WAS SMOKING AND HAD ELECTRICAL SMELL WITH SPARKING. UPON INSPECTION CEILING RAFTER C/B WAS POPPED. REPLACED LIGHT BALLAST.

Part: BATTERY PACK — DISCHARGED (CABIN)

FWD F/C EMER EXIT LIGHT STROBES INOP DURING TEST. REPLACED BATTERY PACK.

Part: WEB — CRACKED (BS 1223-1233)

FOUND ON A1 LETTER CK, RT VERTICAL WEB IN LOWER TORQUE BOX AREA CRACKED STA 1223 AND 1233 AT LIGHTENING HOLES. REPAIRED PER MM 53-11-0.

Part: ANGLE — CRACKED (NR 3 LE SLAT ACT)

FOUND ON A1 LETTER CK, NR 3 SLAT I/B ACTUATOR ATTACH ANGLE CRACKED. REPAIRED PER MM 57-54-0.

Part: LIGHT — INOPERATIVE (CABIN)

AFT AIRSTAIR EMERG LIGHT INOP. REPLACED LIGHT ASSY AND BATTERY PACK.

Part: STRINGER — CORRODED (BS 950)

FUSELAGE/STRINGER 29R/FS 950D PLUS 10, FS 1007. SPLICE REPAIR A SECTION OF STRINGER 29R NEAR FS 950D PLUS 10 WAS FOUND BADLY CORRODED. THE STRINGER WAS CUT AT STATION 950D PLUS 10 AND THE AFT END REMOVED. A NEW SECTION WAS SPLICED IN PER ER/A 363641-14, REV C.

Part: SKIN — TORN (BS 1160)

WHILE ACCOMPLISHING MODIFICATIONS AROUND THE AFT LAV SERVICE PANEL CUTOUT IN THE SKIN, THE BONDED INTERNAL DOUBLER WAS TORN IN SEVERAL LOCATIONS. THE SKIN AND BONDED DOUBLER WERE CUTOUT AND REMOVED BETWEEN FS 1158 AND 1183 AND BETWEEN STR 20L AND 23L. A NEW SECTION OF SKIN WAS SPLICED IN PER ER/A 363813-14, REV B.

Part: SKIN — CORRODED (BS 490)

FUSELAGE SKIN WAS FOUND CORRODED BETWEEN STA 480 AND 500 AND BETWEEN S28L AND BL 0. THE CORROSION WAS TRIMMED AWAY WITH A 9 BY 20 CUTOUT. REPAIRED PER ERA 363693-14.

Part: SKIN — CORRODED (BS 500)

THE FUSELAGE SKIN BETWEEN STA 490 TO 520 WAS FOUND CORRODED AT STRINGER 27R. THE DAMAGED SKIN WAS CUTOUT AND A DOUBLER AND STRUCTURAL FILLER WERE INSTALLED. THE REPAIR WAS ACCOMPLISHED PER ER/A 363702-14, REV B.

Part: BEAM — CORRODED (MLG)

TYPICAL CORROSION WAS FOUND IN MANY OF THE HOLE BORES OF THE LT AND RT MAIN LANDING GEAR SUPPORT BEAMS AT THE SKIN PANEL ATTACH LOCATIONS. SURFACE CORROSION WAS ALSO FOUND ON THE BEAMS. THE SURFACE WAS MACHINED TO REMOVE CORROSION AND THE HOLE BORES WERE OVERSIZED. BUSHINGS AND OVERSIZE FASTENERS WERE INSTALLED PER ER/A 363569-14.

Part: SKIN — CORRODED (CENTER WING)

CORROSION WAS FOUND DURING 4-37113-3 IN THE CENTER WING LWR SKIN. DAMAGE LOCATED BETWEEN S3C AND S7C FROM RBL 15 TO RBL 32 ON THE LWR SURFACE. REPAIRED PER ERA 331186-14AD.

Part: ANGLE — CRACKED (NR 3 TE MIDFLAP)

NR 3 MIDFLAP WAS FOUND WITH A CRACKED LOWER AFT SPAR ANGLE DURING SHOP INSPECTION. THE ANGLE WAS REPAIRED BY INSTALLING A DOUBLER PER 727 MM 57-52-0.

Part: ANGLE — CRACKED (NR 3 TE MIDFLAP)

NR 3 MIDFLAP WAS FOUND WITH A CRACKED LOWER AFT SPAR RAIL. DURING SHOP INSPECTION, THE ANGLE WAS REPAIRED BY INSTALLING A DOUBLER PER 727 MM 57-52-0.

Part: ANGLE — CRACKED (NR 3 TE MIDFLAP)

NR 3 MIDFLAP WAS FOUND WITH A CRACK IN THE AFT LOWER SPAR ANGLE DURING SHOP INSPECTION. THE ANGLE WAS REPAIRED BY INSTALLING A DOUBLER PER 727 MM 57-52-0.

Part: SKIN — TORN (LT TE MID FLAP)

.625 INCH LONG CRACK, CONE SKIN 31 FROM I/B END OF FLAP, ALSO COVE SKIN TORN 32 FROM O/B END OF FLAP. BOTH AREAS REPAIRED PER MM 57-52-FIG 809.

Part: BEARING — FAILURE (NR 1 ENGINE)

ON TAKEOFF, NR 1 ENGINE OIL BYPASS LIGHT CAME ON. BROUGHT THROTTLE BACK TO IDLE, ALL INDICATIONS NORMAL. AFTER CRUISE THROTTLE WAS MOVED FROM IDLE AND OIL TEMP CLIMBED WITH THROTTLE MOVEMENT. THROTTLE RETARDED AND PILOT MENTIONED HE SHUT ENGINE DOWN FOR PRECAUTION. WHEN AIRCRAFT ARRIVED, PULLED ENGINE OIL FILTERS. FOUND EXCESSIVE METAL IN SCREEN, SENT OIL OUT FOR ANALYSIS. RESULTS INDICATE BEARING FAILURE. REMOVED AND REPLACED NR 1 ENGINE. (M)

Part: ENGINE — FAILED (NR 1)

ON TAKEOFF NR 1 ENGINE OIL BYPASS LIGHT CAME ON. BROUGHT THROTTLE BACK TO IDLE, ALL INDICATIONS NORMAL. AFTER CRUISE THROTTLE WAS MOVED FROM IDLE AND OIL TEMP CLIMBED WITH THROTTLE MOVEMENT. THROTTLE RETARDED AND SHUT ENGINE DOWN FOR PRECAUTION. WHEN AIRCRAFT ARRIVED, PULLED ENGINE OIL FILTERS. FOUND EXCESSIVE METAL IN SCREEN, SENT OIL OUT FOR ANALYSIS. RESULTS INDICATE BEARING FAILURE. REMOVED AND REPLACED NR 1 ENGINE.

Part: SQUAT SWITCH — MALFUNCTIONED (NLG)

FLT KIC019 - AKL-SYD - ON LANDING, BOTH RIGHT MAIN TIRES BLEW CAUSING GEAR DOOR AND FLAP TRACK DAMAGE. FOUND NOSE GEAR SQUAT SWITCH (S480) OUT OF RIG. RIGGED SWITCH PER MM 32. REPLACED NR 4 BRAKE ANTI-SKID VALVE (LOOSE SOLENOID). REPLACED RIGHT BRAKE CONTROL VALVE AS A PRECAUTIONARY MEASURE. BRAKE CONTROL AND ANTI-SKID SYSTEMS TESTED OK PER MM 32. REPLACED DAMAGED DOOR AND FAIRINGS. ACCOMPLISHED B-CHECK AND RETURNED AIRCRAFT BACK TO SERVICE.