N122AA

Part: GCU — MALFUNCTIONED (NR 2)

NR 2 AC BUS TIE ISOL LIGHT CAME ON IN FLIGHT PERFORMED PROCEDURES IN FCOM, LIGHT REMAINED ON. REMOVED AND REPLACED NR 2 GCU AND BCU. GROUND RUN CHECK OK. (M)

Part: BOLT — BROKEN (NR 1 PYLON)

TUL - FLT 4101 - FUEL LEAK LEFT WING NR 1 ENGINE PYLON AREA. FOUND NR 1 PYLON FOOTSTOOL LOWER INBOARD, OUTBOARD BOLT BROKEN, NR 4. REPLACED BOLT PER AD96-06-08 WITH (H11 TYPE) INCONEL PER AD. (M)

Part: FRAME — CORRODED (BS 410)

TUL - DURING CHECK FOUND FUSELAGE FRAME CORRODED AT THE FORWARD LAVATORY SERVICE PANEL 9 INCHES BY 2 INCHES AT FORWARD E/E STATION 410. DEPTH IS .063. FRAME SPLICED WITH FILLER PLATE INSTALLED PER ESO 7349, DATED 3/12/99. (M)

Part: PANEL — CORRODED (WS 399)

DURING C-21 CHECK, FOUND AREA OF CORROSION ON OUTER WING PANEL .5 INCH BY .5 INCH WITH DEPTH OF .070 AT STATION XORS 399. FOUND BY VISUAL INSPECTION. INSPECTION WAS INTERNAL. BLENDED CORROSION AND REWORKED AREA IAW E50 7349, DATED 03/09/99. (M)

Part: STRUCTURE — CORRODED (BS 561-565)

TUL - FOUND CORROSION ON FRAME STATION 564 IN TWO PLACES FORWARD OF AC EXHAUST DUCT. CORROSION ON 1/B TEE OF CHORD STATION 561 TO 565. SKIN CORROSION STATION 575 AT EXHAUST DUCT (AC BAY) CORROSION ON FITTING INBOARD OF EXHAUST DUCT. INSTALLED REPAIR PER ESO 7349, DATED 3/3/99. (M)

Part: STRINGER — CORRODED (BS 1821)

TUL - DURING C-1 CHECK, FOUND CORROSION ON STRINGER NEAR FORWARD FITTINGS. INSTALLED REPAIR DOUBLER PER 53-40-00 FIGURE 20 AND ESC 7349, DATED 3/17/99. (M)

Part: SPLICE — CRACKED (WS 372)

TUL - FOUND LEFT LONGERON 16 TO 22 SPLICE CRACKED INSIDE NR 1 FUEL TANK WING STATION XORS 372. INSTALLED AND SECURED SERVICEABLE LONG 16 TO 22 IAW AARD 51-01-00-05. (M)

Part: SUPPORT — CORRODED (BS 2007)

TUL - FOUND CORROSION AT LAV SUPPORT TO BULKHEAD TEE AFT OF SEAT TRACK NR 1. REPLACED LAV SUPPORT PER AARD 51-10-00-10. (M)

Part: STRINGER — CORRODED (BS 1124)

TUL - FOUND CORROSION ON STRINGER 48 LEFT. REPLACED STRINGER SECTION FROM STATION 1099 TO 1139 PER 51-01-00-05 CARD. (M)

Part: SPRING — FAILED (GEAR HANDLE)

SEA - FLT 11 - ON TAKEOFF ROLL LANDING GEAR UNSAFE LIGHT CAME ON. ABORTED TAKEOFF. REPLACED LANDING GEAR HANDLE LOCK LEVER SPRING. (X)

Part: BULB — FAILED (COCKPIT)

FLT 1 - HNL - LEFT GEAR GREEN LIGHT DOES NOT ILLUMINATE WITH GEAR HANDLE DOWN. A/C DID A FLYBY, BY THE TOWER TO CONFIRM THAT THE LANDING GEAR WAS DOWN. A/C DID A FLYBY, BY THE TOWER TO CONFIRM THAT THE LANDING GEAR WAS DOWN. A/C MADE AN UNEVENTFUL LANDING AT HNL. FOUND LEFT MAIN LANDING GEAR DOWN LIGHT BULBS BURNED. REPLACED BULBS, OPS CHECK OK. PERFORMED BITE OF PROX BOX OK. CHECKED CONDITION AND SECURITY OF LEFT MLG SWITCHES, OK. (M)

Part: CONTROLLER — MALFUNCTIONED (E/E BAY)

FLT 2 - HNL - ON PREFLIGHT, FOUND 'B' LOOP LIGHT ILLUMINATED FOR NR 1 FIRE DETECTION SYSTEM. REMOVED AND REPLACED CONTROLLER, SYSTEM OP CHECKS NORMAL. (M)

Part: INDICATOR — FAILED (COCKPIT)

FLT 9 - HNL - TCAS INOP IN FLIGHT AT THE SAME TIME GPWS CMPT FAIL AND WINDSHEAR INOP LIGHTS ILLUMINATED. BOTH RADAR SCREENS WENT BLANK WITH THESE WORDS APPEARING, RADIO ALT NR 1 AND NR 2 ON DESCENT WHEN NR 1 RADIO ALT WAS TURNED ON AND TESTED TCAS APPEARED TO WORK NORMALLY. REPLACED NR 2 RADIO ALTIMETER T/R. RERACKED NR 1 RADIO ALTIMETER T/R. GROUND CHECK NORMAL. (M)

Part: ACM — FAILED (AC SYSTEM)

FLT 14 - ON TAXI ADVISED BY CABIN CREW OF SMOKE IN THE CABIN AREA ROWS 23 TO 35. FLT ENGINEER WENT BACK, DESCRIBED FOGGY OR HAZY. SOME FLT ATTENDANTS DESCRIBED SMELL OF ELECTRICAL, OTHERS AS LIKE A BURNED MATCH SMELL. RETURNED TO GATE. TURBINE INLET TEMP OBSERVED AS 235 DEG F COMPLETED AIR CONDITIONING SMOKE CHECKLIST AND INITIALLY FIRST PART OF ELECTRICAL FIRE OR SMOKE OF UNKNOWN ORIGIN CHECKLIST SINCE WE COULD NOT INITIALLY RULE OUT AN ELECTRICAL COMPONENT AS THE SOURCE OF THE SMOKE. (M)

Part: BRACKET — FAILED (NLG WW)

LAX - FLT 9 - RIGHT NOSE GEAR DOOR DID NOT RETRACT. REMOVED AND REPLACED FORWARD RIGHT DRIVE LINK ASSY. (M)

Part: SHEAR TIE — CORRODED (BS 1206)

DURING C-CHECK, FOUND CORROSION ON THE FORWARD SIDE OF THE SHEAR TIE AT STATION 1207, STRINGER 51 AND 52L. REPAIRED SHEAR TIE PER SRM 53-30-00. TREATED AND PRIMED AREA PER SRM 51-21-01. (M)

Part: SKIN — CORRODED (BS 862/864)

DURING C-CHECK, FOUND FUSELAGE SKIN BULGED AND FASTENERS PULLED THROUGH SHOWING CORROSION UNDER SKIN AT LONGERON 43R AT FORWARD END OF FORWARD CARGO DOOR STATION 462 TO 474. REMOVED CORROSION AND INSTALLED CLASS 1 DOUBLER PER ESO 7349, DATED 12/5/96. (M)

Part: SPAR — CORROSION (WS 376)

DURING C-CHECK, FOUND CORROSION AROUND HI LOCK FASTENERS AT FRONT SPAR LOCATION LOWER SKIN AT RIGHT WING AT STATION XORS 376. REMOVED CORROSION AND INSTALLED DOUBLER REPAIR PER ESO 7349, DATED 12/5/96. (M)

Part: LONGERON — CORRODED (BS 1330-1340)

DURING C-CHECK, FOUND CORROSION ON THE LONGERON OUTBOARD OF THE LOWER LEG OF 51L AT STATION 1330 TO 1340. REPAIRED LONGERON PER SRM 53-10-00. TREATED AND PRIMED PER SRM 51-21-01. (M)

Part: CHANNEL — CORRODED (BS 879)

DURING C-CHECK, FOUND CORROSION ON SUPPORT CHANNEL UNDERNEATH NR 2 ROLLER TRAY AFT END IN THE LOWER GALLEY. INSTALLED NEW SUPPORT CHANNEL UNDER NR 2 ROLLER TRAY PER SRM 51-20-00. (M)

Part: ANGLE — CORRODED (WS 164/171)

DURING C-CHECK, FOUND CORROSION ON THE FORWARD INBOARD SIDE OF THE FALSE SPAR ON THE LEFT WING AT STATION XORS 164 TO 171. INSTALL NEW REPAIR ANGLE WET, ALODINED AND PRIMED PARTS AND INSTALLED HI LOCKS PER ESO 7349, DATED 12/5/96. (M)

Part: STRINGER — CORRODED (BS 814-820)

DURING C-CHECK, FOUND CORROSIONI ON STRINGER 52 FROM STATION 814 TO 820 IN THE FORWARD CARGO COMPARTMENT. REMOVED CORRODED STRINGER AND REPLACED WITH ATTACHED SPLICES PER AARD 51-01-00. (M)

Part: SPLICE — CORRODED (WS 264)

SPLICE PLATE HAS CORROSION DAMAGE ON THE FALSE SPAR FORWARD SIDE JUST OUTBOARD OF NR 1 SPOILER ACTUATOR ON THE RIGHT WING TE AT STATION XORS 264. REPAIRED CORROSION DAMAGE RED SRM VOL 1, CHAPTER 51 STR GENERAL AND ESO 7349, REF DATED 12/3/96. (M)

Part: PANEL — CORROSION (BS 1370)

DURING C-CHECK, FOUND HEAVY INTERGRANNULAR CORROSION ON THE LOWER OUTBOARD CORNER OF THE LEFT MAIN GEAR WHEEL WELL SLANT PANEL. REPAIRED PER ENGINEERING INSTRUCTIONS ON ESO 7349, DATED 12/4/96. (M)

Part: CLIP — CORRODED (WS 356)

DURING C-CHECK, FOUND THE PICK UP CLIP AT THE FALSE SPAR FORWARD OF THE INBOARD EDGE OF THE AILERON CLIP ON THE FORWARD SIDE OF THE FALSE SPAR ON TEH RIGHT WING TRAILING EDGE HAS CORROSION DAMAGE. REPAIRED THE CORRODED AREA PER SRM VOL 1, CHAPTER 57-00-01, FIG 3 SHEET 2 AND ESO 7349 REF DATED 12/3/96. (M)

Part: BELTFRAME — CORRODED (BS 939)

DURING C-CHECK, FOUND CORROSION UNDER A PREVIOUSLY INSTALLED DOUBLER AT FORWARD CARGO COMPARTMENT FUSE STATION 939, STRINGER 51 LEFT AND RIGHT. REMOVED DAMAGED SECTION OF BELT FRAME AND SPLICED IN NEW SECTION PER SRM 53-30-00, PAGE 15. (M)

Part: ANGLE — CORRODED (BS 1968-1970)

DURING C-CHECK, FOUND THE AFT CARGO WALL AND CEILING SUPPORT ANGLE HAS CORROSION AROUND SCREW HOLES. INSTALLED NEW ANGLE PER ESO 7349 AND AARD 53-01-00-05. (M)

Part: CHAIN DRV TRACK — CORRODED (BS 879)

DURING C-CHECK, FOUND THE INBOARD CHAIN DRIVE TRACK TRAY IN THE FORWARD CARGO COMPARTMENT CORRODED AT THE FORWARD END ON THE UNDERSIDE. REPLACED THE CHAIN DRIVE TRACK PER AARD 53-10-00-1. (M)

Part: LONGERON — CORRODED (BS 1964/1965)

DURNG C-CHECK, FOUND CORROSION ON LONGERON 51R BETWEEN STATION 1964 AND STATION 1975. INSTALLED LONGERON SPLICE REF SRM 53-10-00. ALL PARTS ALODINED, PRIMED AND SEALED PER SRM 51-21-01. (M)

Part: ANGLE — CORRODED (BS 1701)

DURING C-CHECK, FOUND THE CENTER CARGO FLOORBOARD SUPPORT WITH DEEP CORROSION ON THE AFT SIDE BETWEEN THE RIGHT TRAY AND THE RT FORWARD DRIVE CHAIN CHANNEL. INSTALLED NEW FLOORBOARD SUPPORT ANGLE PER AARD 51-01-00-05. ALODINED AND PRIMED PER SRM 51-21-00-VOL 1 STATION 1701. (M)

Part: LONGERON — CORROSION (BS 937/959)

DURING C-CHECK, FOUND CORROSION INSIDE AND ON TOP OF LONGERON 52 AND ON SPLICE PLATES AT FUSE STATION 937 AND 959. REMOVED DAMAGED LONGERON. SPLICE NEW SECTION IN PER MM REF SRM 53-10-00. (M)

Part: ROLLER TRAY — CORRODED (BS 1701/1781)

DURING C-CHECK, FOUND THE LEFT TRAY IN THE CENTER CARGO FLOOR HAS CORROSION INSIDE AT SEVERAL AREAS. REMOVED DAMAGED TRAY AND INSTALLED NEW LEFT TRAY PER AARD 51-01-00-05. (M)

Part: ANGLE — CORROSION (WS 336)

DURING C-CHECK, FOUND THE PICK UP ANGLE ON THE FORWARD SIDE OF THE FALSE SPAR AT THE OUTSIDE OF NR 1 SPOILER HINGE HAS A BRACKET WITH CORROSION DAMAGE, RT WING. INSTALLED NEW PICK UP ANGLE PER SRM 51-10-00-01. (M)

Part: FLOOR BEAM — CORRODED ANGLE (BS 1841)

DURING C-CHECK, FOUND CORROSION ON FLOOR BEAM ANGLE TOP FLANGE AT FUSE STATION 1841 BETWEEN LONGERON 46R AND LONGERON 45R. REPAIRED FRAME CAP ANGLE AT STATION 1841 BETWEEN LONGERON 46R AND 45R REF SRM 53-30-00 FIG 8. ALODINED AND PRIMED RED SRM 51-21-01. (M)

Part: DOUBLER — CORRODED (BS 1851.85/1868)

DURING C-CHECK, FOUND CORROSION ON SKIN DOUBLER BETWEEN FUSELAGE STATION 1851.85 AND 1868 AT LONGERON 52 LEFT. REMOVED CORRODED DOUBLER, FABRICATED AND INSTALLED NEW DOUBLER PER SRM 51-10-00-01. (M)

Part: BALLAST — OVERHEATED (CABIN)

FLT NR 22 - SEA - FLUORESCENT LIGHT BALLAST FIRE AT SEAT 2A BEGAN TO SMOKE HEAVILY AT CRUISE. POWER REMOVED AND ASSOCIATED CIRCUIT BREAKERS PULLED, SMOKE DISSIPATED. REPLACED BOTH BALLAST ABOVE 2A. OPS CHECKED NORMAL. NO INDICATION OF FIRE. (M)

Part: FUSE HOLDER — ARCING (LAV 1B)

FLT NR 22 - SEA - NR 5 LAVATORY LIGHT FUSE ARCING IN FUSE HOLDER. POOR SOLDER CONNECTION. INSULATING TAPE FOUND SMOLDERING. FUSE REMOVED AND LAVATORY SECURED. RESOLDERED NR 5 LAV 1B LIGHT FUSE HOLDER. OPS CHECKED NORMAL. (M)