N283AU

Part: SKIN — CRACKED (FUSELAGE)

CLT - FOUND .25 INCH CRACK, FUSELAGE SKIN UPPER CORNER L1 WINDOW. INSTALLED DOUBLER PER 53-30-3. (M)

Part: STRINGER — CRACKED (FUSELAGE)

CLT - FOUND STRINGER CRACKED .125 INCH, STRINGER 15R BETWEEN STATION 520 AND 540. REMOVED AND INSTALLED NEW STRINGER SECTION PER SRM 53-10-03. (M)

Part: FRAME — CORRODED (FUSELAGE)

CLT - FOUND FRAME CORRODED 1 INCH BY 3 INCHES, BS 767 BETWEEN STRINGER 26R AND 26L, LBL 0. INSTALLED REPAIR DOUBLER PER SRM 53-10-04, FIG 11. CORROSION LEVEL 1. (M)

Part: SKIN — CORRODED (FUSELAGE)

CLT - FOUND SKIN CORRODED 4 INCHES, STATION 947.5 FUSELAGE DRAIN BETWEEN STRINGER 27L AND 27R. INSTALLED DOUBLER AND FILLER PER SRM 53-30-3. CORROSION LEVEL 1. (M)

Part: SKIN — CORRODED (FUSELAGE)

CLT - FOUND SKIN CORRODED 3 INCHES BY 6 INCHES, BETWEEN BS 767 AND 787, BL 0 VHF ANTENNA NR 3. INSTALLED DOUBLER PER SRM 53-30-3, FIG 6. (M)

Part: FLOORBEAM — CRACKED (CABIN)

CLT - FOUND T-CAP AND WEB CRACKED 5 INCHES, UPPER T-CAP AND CHORD BS 663, BL 0. REPAIRED T-CAP AND CHORD PER EA 67418 AND TR 57-10-04. (M)

Part: STRINGER — CORRODED (FUSELAGE)

CLT - FOUND STRINGER CORRODED 7 INCHES BY 7 INCHES, STATION 922-929 UNDER STRINGER 27R. INSTALLED REPAIR DOUBLER PER SRM 53-30-3. CORROSION LEVEL 1, C53-208-01. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

CLT - FOUND FLOORBEAM CORRODED 3 INCHES, STATION 1006 STRINGER 20L. SPLICE AND INSTALLED DOUBLERS PER SRM 53-10-4, 51-30-1 AND 04. CORROSION LEVEL 1, C53-202-01. (M)

Part: PRESSURE PANEL — CRACKED (FUSELAGE)

CLT - FOUND SKIN CRACKED .5 INCH, W/W STATION 664, LBL 31 PRESSURE DECK SKIN. REPAIRED PER TR 53-60-04 FIG 1. (M)

Part: ANGLE — CORRODED (FUSELAGE)

CLT - FOUND Z-ANGLE CORRODED .250 INCH BY .250 INCH, BS 270, BL 0. REPLACED Z-ANGLE PER TR 53-20-04. (M)

Part: TIE CLIP — CRACKED (FUSELAGE)

CLT - FOUND TIE CLIP CRACKED .25 INCH, BS 360, STRINGER 4R TIE CLIP. REPAIRED PER SRM 51-10-01. (M)

Part: FLOORBEAM — CRACKED (FUSELAGE)

CLT - FOUND T-CAP CRACKED 1 INCH, STATION 520 FLOORBEAM T-CAP UPPER RADIUS, LBL 24.5. REPAIRED PER EA 67383. (M)

Part: WEB — CRACKED (FUSELAGE)

CLT - FOUND 3 CRACKS .250 INCH, WEB UNDER SCUFF PLATE FROM STATION 807 TO 839, BL 18R. REPLACED WEB PER 51-10-1. (M)

Part: STRINGER — CRACKED (FUSELAGE)

CLT - FOUND STRINGER CRACKED .250 INCH, BS 344-360, STRINGER 15R. INSTALLED NEW STRINGER PER SRM 51-10-1, SRM 51-10-2. (M)

Part: FLOORBEAM — CRACKED (FUSELAGE)

CLT - FOUND T-CAP FLOORBEAM CRACKED .5 INCH, AFT SIDE STATION 520 UPPER RADIUS LBL 45.5. INSTALLED FILLERS, CHANNELS, WEB ANGLE PER EA67383. (M)

Part: WEB — CRACKED (FUSELAGE)

CLT - FOUND WEB CRACKED 1 INCH, STATION 948, BELOW STRINGER 11L. INSTALLED REINFORCING STRAP PER TR 53-30-07A. (M)

Part: SKIN — CRACKED (FUSELAGE)

CLT - FOUND SKIN CRACKED 2.25 INCH, AFT LOWER CORNER FORWARD SERVICE DOOR CUTOUT. REPAIRED WITH DOUBLER AND FILLER PER SRM 53-30-3 AND 53-30-10. (M)

Part: TIE CLIP — CRACKED (FUSELAGE)

CLT - FOUND TIE CLIP CRACKED .25 INCH, BS 360, STRINGER 4R. FABRICATED TIE CLIP PER SRM 51-10-01. (M)

Part: TIE CLIP — CRACKED (FUSELAGE)

CLT - FOUND TIE CLIP CRACKED .025 INCH, STRINGER 10R AT BS 747. REPLACED TIE CLIP PER EO 393G227. (M)

Part: TIE CLIP — CRACKED (FUSELAGE)

CLT - FOUND TIE CLIP CRACKED .250 INCH, BS 597 STRINGER 9L. REMOVED AND REPLACED WITH NEW CLIP PER SRM 51-10-1. (M)

Part: TIE CLIP — CRACKED (FUSELAGE)

CLT - FOUND TIE CLIP .025 INCH CRACK, STRINGER 5L AT BS 685. REPLACED TIE CLIP PER SRM 51-10-1. (M)

Part: TIE CLIP — CRACKED (FUSELAGE)

CLT - FOUND TIE CLIP CRACKED .5 INCH, STATION 597 RT STRINGER 9R. REMOVED AND REPLACED NEW CLIP PER SRM 51-10-01. (M)

Part: TIE CLIP — CRACKED (FUSELAGE)

CLT - FOUND TIE CLIP CRACKED .5 INCH, STATION 616 RT, STRINGER 3R. REMOVED AND REPLACED WITH NWE CLIP PER SRM 51-10-01. (M)

Part: ANGLE — CRACKED (FUSELAGE)

CLT - FOUND SUPPORT ANGLE CRACKED, BS 291.5, BETWEEN STRINGER 11 AND 12R. REPAIRED PER SRM 51-10-1. (M)

Part: TIE CLIP — CRACKED (FUSELAGE)

CLT - FOUND STRINGER TIE CLIP CRACKED .5 INCH IN 2 PLACES, STATION 380, LBL 22, LWR FRAME. REPLACED TIE CLIP PER SRM 51-10-1. (M)

Part: TIE CLIP — CRACKED (FUSELAGE)

CLT - FOUND TIE CLIP CRACKED .025 INCH, STRINGER 11L AT BS 663. REPLACED CLIP PER SRM 51-10-1. (M)

Part: SKIN — CRACKED (FUSELAGE)

CLT - FOUND SKIN CRACKED .125 INCH, STATION 380 EQUIP COOLING DUCT. INSTALLED DOUBLER PER TR 53-30-04 DWG NR 65C33930. (M)

Part: TIE CLIP — CRACKED (FUSELAGE)

CLT - FOUND TIE CLIP CRACKED .025 INCH, STRINGER 6R AT BS 747. RE-INSTALLED TIE CLIP PER EO 393G227. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

CLT - FOUND FLOORBEAM T-CAP CORRODED 1 INCH IN 6 AREAS, BS 344 LBL 49, BL 0 FASTENER HOLES. INSTALLED NEW T-CAP PER TR 53-10-13. (M)

Part: TIE CLIP — CRACKED (FUSELAGE)

CLT - FOUND TIE CLIP CRACKED .025 INCH, BS 663, STRINGER 10R. INSTALLED TIE CLIP PER EO 5393G227. (M)

Part: TIE CLIP — CRACKED (FUSELAGE)

CLT - FOUND TIE CLIP CRACKED .5 INCHES, BS 344, STRINGER 2R. INSTALLED TIE CLIP PER EO 393G227. (M)

Part: TIE CLIP — CRACKED (FUSELAGE)

CLT - FOUND TIE CLIP CRACKED .5 INCH, BS 344, STRINGER 1. INSTALLED TIE CLIP PER EO 5393G227. (M)

Part: TIE CLIP — CRACKED (FUSELAGE)

CLT - FOUND STRINGER TIE CLIP CRACKED .5 INCH, STATION 597 LT, STRINGER 9L. INSTALLED TIE CLIP PER SRM 51-10-1. (M)

Part: TIE CLIP — CRACKED (FUSELAGE)

CLT - FOUND STRINGER TIE CLIP CRACKED .5 INCHES, STATION 639 LT, STRINGER 4L. REPLACED CLIP PER SRM 51-10-1. (M)

Part: TIE CLIP — CRACKED (FUSELAGE)

CLT - FOUND STRINGER TIE CLIP CRACKED .5 INCH, STATION 616 LT, STRINGER 2L. INSTALLED TIE CLIP PER EO 5393G227. (M)

Part: TIE CLIP — CRACKED (FUSELAGE)

CLT - FOUND TIE CLIP CRACKED .25 INCH, STATION 616 RT, STRINGER 2R. REPLACED TIE CLIP PER SRM 51-10-1. (M)

Part: TIE CLIP — CRACKED (FUSELAGE)

CLT - FOUND TIE CLIP CRACKED .025 INCH, BS 727B, STRINGER 8R. INSTALLED TIE CLIP PER EO 393G227. (M)

Part: TIE CLIP — CRACKED (FUSELAGE)

CLT - FOUND TIE CLIP CRACKED .025 INCH, BS 706, STRINGER 3L. REPLACED TIE CLIP PER SRM 51-30-02. (M)

Part: TIE CLIP — CRACKED (FUSELAGE)

CLT - FOUND TIE CLIP CRACKED .025 INCH, BS 706, STRINGER 11L. INSTALLED TIE CLIP EO 5393G227. (M)

Part: TIE CLIP — CRACKED (FUSELAGE)

CLT - FOUND TIE CLIP CRACKED .025 INCH, BS 706, STRINGER 13R. REINSTALLED TIE CLIP PER SRM 51-30-02. (M)

Part: TIE CLIP — CRACKED (FUSELAGE)

CLT - FOUND TIE CLIP CRACKED .025 INCH, BS 727B, STRINGER 5R. INSTALLED TIE CLIP PER EO 393G337. (M)

Part: TIE CLIP — CRACKED (FUSELAGE)

CLT - FOUND TIE CLIP CRACKED .25 INCH, BS 787 STRINGER 10R. INSTALLED NEW TIE CLIP PER EO 5393G227. (M)

Part: PCU — FAILED (RUDDER)

MCO - FLT 2611 - CAPTAIN REPORTED THAT 40 MILES NORTH OF MCO, AT FL120, THEY EXPERIENCED A POSSIBLE LEFT UNCOMMANDED RUDDER MOVEMENT. ROLL DISCONTINUED WHEN AUTOPILOT WAS DISENGATED. THE FIRST OFFICER OBSERVED THE AIRCRAFT ROLLED 25 DEGREES. FLIGHT CONTINUED AND LANDED AT MCO WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE RUDDERPOWER CONTROL UNIT PER MM 27-21-9. RIGGING AND OPERATIONAL CHECK GOOD. COMPLIED WITH WORK CARD J227-21-00. (M)

Part: CONNECTOR — DIRTY (RT WING)

TPA - FLT 2642 - DURING CLIMB-OUT FROM TPA, THE NR 2 ENGINE FUEL SHUTOFF VLV CLOSED LIGHT BEGAN FLICKERING ON AND OFF THEN ILLUMINATED STEADY. ENGINE INDICATIONS WERE NORMAL. FLIGHT RETURNED TO FIELD AT TPA AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE CLEANED THE NR 2 ENGINE FUEL SHUTOFF VALVE CANNON PLUG. OPERATED VALVE NUMEROUS TIMES. OPERATIONAL CHECK GOOD. (M)

Part: ENGINE — FAILED (RIGHT)

RDU - FLT 2695 - APPROXIMATELY 60 MILES SOUTH OF ORF AT FL 350, THE NR 2 ENGINE EXPERIENCED A COMPRESSOR STALL AND STARTED TO LOSE POWER. AIRFRAME VIBRATION WAS ALSO NOTED. CREW BROUGHT THROTTLE BACK AND RESTORED PARTIAL ENGINE POWER. FLIGHT DIVERTED TO RDU AND LANDED WITHOUT FURTHER INCIDENT. NO ENGINE SHUT DOWN OCCURRED, BUT AN EMERGENCY WAS DECLARED. MAINTENANCE INSPECTED THE NR 2 ENGINE INTAKE AND EXHAUST. RAN ENGINE TO TAKEOFF POWER. COULD NOT DUPLICATE ON GROUND RUN. AIRCRAFT WAS MAINTENANCE FERRIED TO CLT WHERE THE NR 2 ENGINE ASSY WAS REMOVED AND REPLACED PER JOB CARD. OPERATIONAL CHECK AND LEAK CHECK GOOD. (X)

Part: O-RING — DAMAGED (MLG WW)

PBI-BWI - FLT 2615, DURING CRUISE, THE SYSTEM 'B' HYDRAULIC QUANTITY LIGHT ILLUMINATED FOLLOWED BY LOSS OF PRESSURE ON HYDRAULIC GAUGE. SHORTLY AFTER, THE LOW PRESSURE LIGHTS ON THE 'B' PUMPS ILLUMINATED. CREW SHUT OFF THE 'B' PUMPS AND DECLARED AN EMERGENCY. FLIGHT LANDED WITHOUT FURTHER INCIDENT AT BWI. SYSTEM 'A' HYDRAULIC SYSTEM READ ONE GALLON UPON LANDING. MAINTENANCE FOUND AN O-RING DAMAGED AT THE NR 2 'B' PUMP PRESSURE LINE FITTING. REPLACED O-RING AND SERVICED SYSTEM. LEAK CHECK GOOD. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

ALB - MAINTENANCE FOUND FOUR ROWS OF LOW LEVEL LIGHTING, AFT OF THE OVERWING EXIT IN THE MID CABIN, INOP. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. (M)

Part: SWITCH — DEFECTIVE (CABIN)

BWI - EMERGENCY LIGHTS FAIL TO EXTINGUISH. FOUND SWITCHES (S-538) AT AFT FLIGHT ATTENDANTS STATION DEFECTIVE. REMOVED AND REPLACED SWITCH (S-538). SYSTEM OPERATIONALLY CHECKED, OK. (M)

Part: BLEED VALVE — FAILED (NR 2 ENGINE)

MCI - FL 2160 - ON T/O ROLL, THE NR 2 ENG HAD ABNORMAL LOW EPR AND N1 READINGS AND VERY HIGH EGT. FUEL FLOW AND N2 WERE NORMAL. EXCEEDING 100 KNOTS, CAPT ELECTED TO CONTINUE TAKEOFF. DURING CLIMB-OUT, CREW PULLED BACK ON POWER AND READINGS CONTINUED. CAPT ELECTED TO RETURN TO MCI AND LANDED W/O INCIDENT. NO EMERG DECLARED. MX INSPECTED NR 2 ENG PS-3 FILTER AND PT2 AND PT7 LINES. CHECKED GOOD. PERFORMED LUBRICATION FOR BLEED VALVES PER MM 75-31-0, PAGE 601. RAN ENG PER MM 71-09-256 AND 72-05-03A, MAX EGT TEST. OP CHECKED GOOD. SUBSEQUENTLY, THE NEXT DAY THE NR 2 ENG WOULD NOT MAKE T/O POWER. MX REMOVED AND REPLACED THE NR 2 ENG RATION BLEED CONTROL VLV PER MM 75-31-11. RAN ENG AT T/P POWER. OPS CHE

Part: BATTERY PACK — FAILED (CABIN)

PHL - MAINTENANCE FOUND A ROW OF EMERGENCY LIGHTS AT THE OVERWING EXITS INOP AND AT THE AFT GALLEY DOOR INOP. MAINTENANCE REMOVED AND REPLACED THE BATTERY CHARGER AND BATTERY PACK AT THE CABIN AFT RIGHT POSITION. OPERATIONAL CHECK GOOD. REFERENCE USAASB97134

Part: BATTERY CHARGER — FAILED (CABIN)

PHL - MAINTENANCE FOUND A ROW OF EMERGENCY LIGHTS AT THE OVERWING EXITS INOP AND AT THE AFT GALLEY DOOR INOP. MAINTENANCE REMOVED AND REPLACED THE BATTERY CHARGER AND BATTERY PACK AT THE CABIN AFT RIGHT POSITION. OPERATIONAL CHECK GOOD. (M)

Part: CIRCUIT BREAKER — TRIPPED (LANDING GEAR)

PHL - FL 1723 - GEAR WOULD NOT RETRACT AFTER TAKEOFF FROM PHL. CREW WENT THROUGH CHECKLIST/RECYCLED GEAR. FLIGHT RETURNED TO FIELD TO PHL. NO EMERGENCY WAS DECLARED AND THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE LANDING GEAR LIGHTS CIRCUIT BREAKER POPPED. RESET BREAKER. SYSTEM CHECKS GOOD. ALL INDICATIONS CHECK NORMAL. (M)

Part: FLOOR BEAM — CHAFFING (BS720)

INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 10 INCHESCHAFFING STATION 720 RHS KEEL BEAM LOWER CORD OUTBOARD FLANGE. INSTALLEDREPAIR STRAP, REPAIRED PER EA 41322. (M)

Part: BULKHEAD SKIN — SCRATCH (AFT PRESSBLKHD)

INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND .75 INCH SCRATCHAFT PRESSURE BULKHEAD SKIN 5 O'CLOCK POSITION. INSTALLED DOUBLER, REPAIREDPER SRM 53-10-4 FIG 3. (M)

Part: FLOOR BEAM — CORROSION (BS 360)

INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 2 INCHCORRODED AREA FLOOR BEAM BS 360 RBL 54. INSTALLED REPAIR ANGLE, REPAIREDPER TR 53-10-05 C. CORROSION TASK NR C53-107-02, CORROSION LEVEL 1.(M)

Part: STRINGER — CORROSION (BS947-995)

INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND SPOTS OFCORROSION ALONG SIDES OF STRINGER BS 947-995 S-27L. REMOVED STRINGERSECTION, FABRICATED NEW SECTION AND INSTALLED, REPAIRED PER SRM 53-10-3.CORROSION TASK NR C53-202-01 CORROSION LEVEL 1. (M)

Part: FLOOR BEAM — CORROSION (BS 947.5)

INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND .33 INCH CORRODEDAREA FLOOR BEAM BS 947.5 RBL 10 TO LBL 36. INSTALLED REPLACEMENT T-CAP,REPAIRED PER TR 53-10-05C. CORROSION TASK NR C53-107-02, CORROSION LEVEL 1. (M)

Part: FLOOR BEAM — CORROSION (BS312)

INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND TWO 1 INCH BY 3INCH CORRODED AREAS AT NUT PLATE HOLES T-CAP, BS 312 FLOOR BEAM BBL 0, RBL8. INSTALLED T-CAP REPAIR AND REPAIRED PER SRM 53-10-9. CORROSION TASK NRC53-107-02, CORROSION LEVEL 1. (M)

Part: FLOOR BEAM — CORROSION (BS1016)

INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 4 INCHCORRODED AREA ON TOP OF FLOOR BEAM BS 1016 LBL 16 LBL 5. INSTALLED FLOORBEAM REPAIR, REPAIRED PER SRM 53-10-9. CORROSION TASK NR C53-017-02,CORROSION LEVEL 1. (M)

Part: STRINGER — CORROSION (BS960-967)

INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 7 INCHCORRODED AREA AT INBOARD SIDE STRINGER BS 960-967 STRINGER 26R. INSTALLEDSTRINGER SPLICE/REPAIR. REPAIRED PER SRM 53-10-3 PAGE 10 FIG 1. CORROSIONTASK NR C53-202-01, CORROSION LEVEL 1. (M)

Part: SKIN — GOUGES (HORIZ STAB)

INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND TWO GOUGES 1 INCHAND .625 INCH SKIN STABILIZER STATION 226 15 INCHES AND 20 INCHES AFT OFFRONT SPAR. INSTALLED DOUBLER, REPAIRED PER SRM 55-10-3.(M)

Part: SKIN — CRACKED (BS 917)

INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND CRACK .375 INCHSTATION 917 BETWEEN STRINGERS 21L AND 22L SKIN. INSTALLED DOUBLER, REPAIREDPER SRM 53-30-3. (M)

Part: SKIN — GOUGED (HORIZ STAB)

INT - DURING Q-6 CHECK VISUAL INSPECTION FOUND TWO GOUGES .75INCH AND .625 INCH SKIN STABILIZER STATION 92.7 APPROXIMATELY 17 INCHES FROMAFT SPAR. INSTALLED DOUBLER, REPAIRED PER SRM 55-10-3.(M)

Part: SKIN — DENTED (HORIZSTAB)

INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 1 INCH INDENTEDAREA STABILIZER SKIN STATION 111.1 APPROX 12 INCHES FORWARD OF AFT SPAR.INSTALLED DOUBLER, REPAIRED PER SRM 55-10-3. (M)

Part: FLOORBEAM — CORROSION (BS 1006)

INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND CORROSION 3INCHES AT FLOOR BEAM STATION 1006 LBL 8. CUT OFF T-CAP THAT WAS OUT OFLIMITS, FABRICATED REPLACEMENT AND INSTALLED PER SRM 53-10-9 FIG 2.CORROSION TASK NR C53-107-02, CORROSION LEVEL 1. (M)

Part: FLOORBEAM — CORROSION (BS 967)

INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 1 INCH CORRODEDAREAS FLOOR BEAM BS 967. INSTALLED DOUBLER REPAIRED PER SRM 53-10-9.CORROSION TASK NR C53-107-02, CORROSION LEVEL 1 (M)

Part: FLOOR BEAM — CORROSION (BS328)

INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND SEVERAL 1 INCH BY1 INCH CORRODED AREAS ON FLOOR BEAM BS 328 RBL 12 INCH TO RBL 45 INCH.INSTALLED NEW T-CAP WITH REPAIR ANGLES, REPAIRED PER TR 53-10-13. CORROSIONTASK NR C53-107-02, CORROSION LEVEL 1. (M)

Part: FRAME — CORROSION (BS 990)

INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCHBY 1 INCH FRAME STATION 990 WL 208. INSTALLED FRAME REPAIR AND REPLACED 'Z'ANGLE, REPAIRED PER SRM 51-40-03, 51-10-2. CORROSION TASK NR 53-107-02,CORROSION LEVEL 1. (M)

Part: FLOOR BEAM — CORROSION (BS986)

INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND CORROSION 90INCHES AT STATION 986 FLOOR BEAM UPPER CHORD. INSTALLED NEW SECTION WITHREPAIR ANGLES AND STRAPS, REPAIRED EA 41317. CORROSION TASK NR C53-107-02,CORROSION LEVEL 1. (M)

Part: T3 BLADE — FAILED (NR 1 ENGINE)

FLT 1930 - PHL - NR 1 ENG COMPRESSOR STALLED, WOULD NOT SPOOL UP AFTER. DURING TAXI BACK IDLE EGT KEPT CREEPING UP, SHUT IT DOWN A T530. AT GATE GROUND PERSONNEL REPORTED TAIL PIPE FIRE. FIRED BOTH BOTTLES AND EVACUATED AIRCRAFT. NO FIRE WARNING, FIRE WARNING WAS CHECKED ON SHUTDOWN OK, TURBINE FAILURE CAUSED DAMAGE TO LEFT HORIZONTAL STABILIZER. MAINTENANCE REPLACED NR 1 ENGINE AND LEFT LEADING EDGE OF HORIZONTAL STABILIZER. ENGINEERING ANALYSIS FOUND THAT A T3 BLADE FAILED POSSIBLY FROM EXCESSIVE SHROUD WEAR. (M)

Part: STRINGER — CORRODED (BS 986-1016)

ROA - DURING CX-4 CHECK VISUAL INSPECTION, FOUND 3 INCH BY 1 INCH CORRODED AREA STRINGER 27L BETWEEN STATION 986-1016. SPLICED NEW STRINGER, REPAIRED PER SRM 53-10-3. (M)

Part: SKIN — CORRODED (BS 747)

ROA - DURING CX-4 CHECK VISUAL INSPECTION, FOUND 6.5 INCH BY 8 INCH CORRODED SKIN, BS 747 S-27R. REMOVED CORROSION AND INSTALLED DOUBLER, REPAIRED PER SRM 53-10-4. (M)

Part: FLOOR LIGHTS — MALFUNCTION (CABIN EEL)

PHL - EMERGENCY EXIT LIGHTS ILLUMINATE ABOUT EVERY 45 MINUTES, THEN SLOWLY FADE BACK TO OFF. MAINTENANCE FOUND FLOOR LIGHTS ON CONSTANTLY IN ARM. DISCONNECTED PLUG D4049F TO CHECK POWER. POWER CHECKED GOOD. WHEN RECONNECTED, PROBLEM DID NOT OCCUR. OPS CHECK NORMAL. (X)