N433AA

Part: LIGHT — DEFECTIVE (CABIN) · airframe 78,138 hrs · 36,112 cycles

FORWARD EMERGENCY LIGHT IS DIM. REPLACED LAMP FOR FORWARD EMERGENCY LIGHT.

Part: FRAME — CRACKED (FUSELAGE) · airframe 77,006 hrs · 35,489 cycles

FRAME 1418 CRACKED ON AFT SIDE AT LONGERON 2 RIGHT. INSTALLED DOUBLER AND FILLER REPAIR PER AARD 53-10-00-15 AND SRM 53-01-00.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 76,980 hrs · 35,474 cycles

EMERGENCY CEILING LIGHTS INOPERATIVE. RESEATED CEILING EMERGENCY LIGHTS BATTERY PACK. OPS CHECK NORMAL.

Part: LENS — MISSING (CABIN) · airframe 76,404 hrs · 35,188 cycles

EMERGENCY EXIT LIGHT AT LEFT AFT OVERWING EXIT DOOR MISSING LENS. REPLACED LENS. OPS CHECK NORMAL.

Part: PROXIMITY SENSOR — INOPERATIVE (LE SLAT) · airframe 76,228 hrs · 35,103 cycles

DFW - CREW REPORTED ON APPROACH WHEN LOWERING SLATS RECEIVED A SLAT DISAGREE WARNING INDICATION. EMERGENCY DECLARED FLIGHT LANDED DFW WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED PROXIMITY BOX. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: DISPLAY — INOPERATIVE (COCKPIT) · airframe 74,425 hrs · 34,168 cycles

DFW - INFLIGHT AUS-ORD. CREW REPORTED NAVIGATION DISPLAY INOPERATIVE. EMERGENCY DECLARED FLIGHT DIVERTED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED FIRST OFFICERS NAVIGATION DISPLAY. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: CHARGER — INOPERATIVE (MAIN BATTERY) · airframe 73,266 hrs · 33,604 cycles

DFW - CREW REPORTED BATTERY DISCHARGE LIGHT ILLUMINATED DURING FLIGHT. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED BATTERY CHARGER AND BOTH MAIN SHIP BATTERIES (MPN 023964000). SYSTEM GROUND CHECK NORMAL OPERATION.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,864 hrs · 33,405 cycles

STATION 161 LONGERONS 16 LEFT TO 22 LEFT, HIGH FREQUENCY EDDY CURRENT INSPECTION INDICATES CRACK AROUND FASTENERS IN FUSELAGE SKIN. INSTALLED DOUBLER PER EA MD80-53-013579.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 72,389 hrs · 33,190 cycles

EMERGENCY LIGHTING AT AFT SERVICE DOOR INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT AFT SERVICE DOOR.

Part: TUBE — LEAKING (RT ENGINE) · airframe 71,499 hrs · 32,769 cycles

SFO - CREW REPORTED RIGHT ENGINE OIL PRESSURE LIGHT DROPPED TO 20 PSI AND STABILIZED. RIGHT HAND THROTTLE REDUCED TO IDLE. FLIGHT RETURNED SFO LANDED WITHOUT INCIDENT. FOUND OIL LEAK AT 11 O`CLOCK POSITION. REMOVED AND REPLACED OIL TUBE AT OIL FILTER DIFFERENTIAL PRESSURE SWITCH. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 70,964 hrs · 32,540 cycles

SEAT 8D EGRESS LIGHT INOPERATIVE. RE-PINNED LIGHT ASSEMBLY FOR SEAT 8D EGRESS LIGHT.

Part: BATTERY — NOT SEATED (CABIN) · airframe 70,964 hrs · 32,540 cycles

EMERGENCY LIGHTS OVERHEAD ADJACENT TO AFT LAVATORIES INOPERATIVE. RE-SEATED AFT EMERGENCY LIGHT BATTERY. OPS CHECKED NORMAL.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 68,765 hrs · 31,579 cycles

NR 1 SEAT TRACK CORRODED OUT OF LIMITS. INSTALLED SEAT TRACK PLUG PER SRM 53-10-3.

Part: ANGLE — CORRODED (ZONE 100) · airframe 68,765 hrs · 31,579 cycles

CORROSION ON PLOW ANGLE AT STA 1338. INSTALLED NEW PLOW ANGLE DOUBLER, P/N 9915561-73, PER SRM 51-30-00.

Part: CARGO TRACK — CORRODED (ZONE 100) · airframe 68,765 hrs · 31,579 cycles

CORROSION ON LT TIE DOWN TRACK STA 1211-1287. SPLICED IN NEW SECTION OF TIE DOWN TRACK PER SRM 53-05-00.

Part: BRACKET — CORRODED (FUSELAGE) · airframe 68,765 hrs · 31,579 cycles

CORNER BRACKET CORRODED LOWER FWD CORNER OF AFT CARGO DOOR CUT-OUT. REPLACED BRACKET PER SRM 51-10-03.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 68,765 hrs · 31,579 cycles

CORROSION ON INTERCOSTAL IN AFT CARGO. REPLACED INTERCOSTAL PER SRM 51-30-05.

Part: SKIN — GOUGED (ZONE 200) · airframe 68,765 hrs · 31,579 cycles

DRILL DAMAGE TO SKIN 2 INCHES BELOW LONG 10L. REMOVED DAMAGE AND INSTALLED DOUBLER WITH FILLER PER EA 53-006187.

Part: CARGO TRACK — CORRODED (ZONE 100) · airframe 68,765 hrs · 31,579 cycles

RT TIE DOWN TRACK HAS CORROSION STA 1211-1287, AFT CARGO. REMOVED AND REPLACED RT AFT TIE DOWN TRACK PER SRM 51-30-00.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 68,765 hrs · 31,579 cycles

CORROSION ON RT TIE DOWN TRACK Z ANGLE IN MID CARGO. REPLACED Z ANGLE PER SRM 51-30-01.

Part: BEAM — CORRODED (FUSELAGE) · airframe 68,765 hrs · 31,579 cycles

CORROSION ON AFT CARGO DOOR BEAM. INSTALLED REPAIR DOUBLER PER AARD 53-10-00-3.

Part: SKIN — DAMAGED (ZONE 200) · airframe 68,765 hrs · 31,579 cycles

DRILL START IN EXTERIOR FUSE SKIN AT STA 886, 2 INCH BELOW L10L. INSTALLED FUSELAGE SKIN DOUBLER, STA 886 LT LONGERON 10, PER EA MD80-53-006187.

Part: PLATE — CORRODED (ZONE 100) · airframe 68,765 hrs · 31,579 cycles

CORROSION IN DELTA PLATE IN AFT CARGO.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 68,765 hrs · 31,579 cycles

CORROSION ON RT TIE DOWN TRACK IN MID CARGO. INSTALLED NEW TIE DOWN TRACK PER SRM 51-30-01.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · airframe 68,765 hrs · 31,579 cycles

CORROSION ON FLOORBOARD SUPPORT ANGLE INBD OF DOOR BEAM IN AFT CARGO. REPLACED FLOORBOARD SUPPORT ANGLE PER SRM 51-30-2.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 68,765 hrs · 31,579 cycles

REMOVED SMALL EDGE OF CUSP SHEET FOR CORROSION REMOVAL, STA 871. INSTALLED SMALL DOUBLER ON CUSP, .032; 7075-T6, PER AARD 53-20-00-16.

Part: STRAP — CORRODED (ZONE 100) · airframe 68,765 hrs · 31,579 cycles

STRAP ABOVE DOOR BEAM, ON WEB, HAS CORROSION, STA 1174. INSTALLED NEW STRAP, STA 1174, MADE OF 7075-T6; .063, PER SRM 51-30-02.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 68,765 hrs · 31,579 cycles

CORROSION OUT OF LIMITS ON SEAT TRACK NR 6 STA 1090. REMOVED CORROSION AND INSTALLED SEAT TRACK PLUG PER AARD 53-20-00-10 AND EA MD80-53-006/62

Part: SUPPORT — CORRODED (ZONE 200) · airframe 68,765 hrs · 31,579 cycles

CORROSION ON AFT GIRT BAR SUPPORT, STA 1166. INSTALLED NEW GIRT BAR SUPPORT PER SRM 51-30-05.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 68,765 hrs · 31,579 cycles

CORROSION ON TOP OF SUBFLOOR, BELOW FWD GIRT BAR SUPPORT. REMOVED DAMAGE AND INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: SUPPORT — CORRODED (GIRT BAR) · airframe 68,765 hrs · 31,579 cycles

CORROSION ON TOP OF SUBFLOOR BELOW AFT GIRT BAR SUPPORT STA 1166. CUT OUT DAMAGED AREA, INSTALLED DOUBLER .040 6AL-4V TITANIUM PER AARD 53-20-00-16.

Part: FITTING — CORRODED (ZONE 200) · airframe 68,765 hrs · 31,579 cycles

CORROSION ON FWD GIRT BAR SUPPORT FITTING STA1142. INSTALLED NEW GIRT BAR SUPPORT AT STA 1142 PER 51-30-05.

Part: SUPPORT — CORRODED (ZONE 200) · airframe 68,765 hrs · 31,579 cycles

CORROSION ON AFT GIRT BAR SUPPORT BS 1166. INSTALLED SERVICEABLE GIRT BAR SUPPORT BS 1166.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 68,765 hrs · 31,579 cycles

CORROSION ON TOP OF SUBFLOOR BELOW FWD GIRT BAR SUPPORT STA 1142. CUT OUT DAMAGE, INSTALLED DOUBLER, .0406AL-4V TITANIUM AND FILLER 7075-T6 .063 PER AARD 53-20-00-16.

Part: LONGERON — CORRODED (ZONE 100) · airframe 68,765 hrs · 31,579 cycles

CORROSION ON LONG 30. REMOVED DAMAGED SECTION AND REPAIRED PER SRM 53-02-00 FIG 18.

Part: SKIN — DENTED (FUSELAGE) · airframe 68,765 hrs · 31,579 cycles

DENT IN FUSELAGE RT SIDE (ENGINE COWL DRAIN MAST DAMAGE) STA 1309 BELOW LONGERON 18. INSTALLED DOUBLER PER SRM 53-04 FIG 38 AND INSTALLED SCUFF PLATE PER AARD 53-30-00-08.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 68,765 hrs · 31,579 cycles

CORROSION ON TOP OF SUBFLOOR, BELOW AFT GIRT BAR SUPPORT. INSTALLED REPAIR DOUBLER AND CUSP SUPPORT PER AARD 53-20-00-16.

Part: SUPPORT — CORRODED (GIRT BAR) · airframe 68,765 hrs · 31,579 cycles

CORROSION AT FWD GIRT BAR SUPPORT, STA 1142. INSTALLED NEW GIRT BAR SUPPORT PER SRM 51-30-05.

Part: FRAME — DENTED (FUSELAGE) · airframe 68,765 hrs · 31,579 cycles

FRAME DENTED AT RT STA 522 6 INCHES ABOVE CUSP. INSTALLED J ANGLE REPAIR PER AARD 53-10-00-17 FIG 1.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 68,765 hrs · 31,579 cycles

CORROSION ON CUSP SHEET, STA 503-598, RT SIDE. INSTALLED NEW CUSP SHEET, STA 503- 598, PER SRM 51-30-05.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 68,765 hrs · 31,579 cycles

CRACK IN LONG 4L. REMOVED AND REPLACED LONG 4L FROM STA 168-230 PER SRM 53-02-00.

Part: TRUNNION — CORRODED (ZONE 700) · airframe 68,765 hrs · 31,579 cycles

CORROSION ON FOWARD FACE OF FWD/AFT TRUNNION LUG FOR LT GEAR. REPAIRED PER AARD 32-10-00-1.

Part: CUSP WEB — CRACKED (ZONE 200) · airframe 68,765 hrs · 31,579 cycles

CRACK IN RT CUSP STA 597. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (ZONE 200) · airframe 68,765 hrs · 31,579 cycles

CORROSION ON LT CUSP. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: SKIN — DENTED (ZONE 200) · airframe 68,765 hrs · 31,579 cycles

DENT IN LT FUSELAGE SKIN AT LONGERON 18L. INSTALLED DOUBLER PER SRM 53-04 FIG 12B.

Part: SKIN — DENTED (FUSELAGE) · airframe 68,765 hrs · 31,579 cycles

DENT IN FUSELAGE SKIN AT LONG 23L-24L. INSTALLED DOUBLER PER SRM 53-04 FIG 12B.

Part: RIB — WORN (BS 1039) · airframe 68,765 hrs · 31,579 cycles

STA1039 HAS WORN RIB. REMOVED AND REPLACED KNUCKLE RIB ASSY PER AARD 27-80-00-2.

Part: RIB — CRACKED (ZONE 600) · airframe 68,765 hrs · 31,579 cycles

HFEC INDICATES CRACK RIB ON 2ND FROM OTBD RIB. REMOVED AND REPLACED RIB ASSY PER SRM 57-50-13.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 68,765 hrs · 31,579 cycles

VERTICAL FLOOR FRAME SUPPORT CRACKED ABOVE FUEL TANK. REPLACED SUPPORT PER SRM 51-01.

Part: WIRE — LOOSE (LT GENERATOR) · airframe 67,573 hrs

DFW - INFLIGHT, CREW REPORTED LEFT GENERATOR DC BUSS OFF INDICATION AND CROSS TIE LOCKOUT. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. FOUND AN OPEN WIRE AT P1 1221 AND R5 3. SECURED WIRE IN RECEPTICLE R5 3. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 65,690 hrs

SFO - SEAT MOUNTED EMERGENCY LIGHTS AT SEAT ROWS 21D TO 32D INOPERATIVE. REPLACED BATTERY PACK AT AB53 FOR SEAT MOUNTED EMERGENCY LIGHTS AT SEAT ROWS 21D TO 32D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: MODULE — INOPERATIVE (CABIN) · airframe 65,690 hrs

SFO - SEAT MOUNTED EMERGENCY LIGHTS AT SEAT ROWS 21D TO 32D INOPERATIVE. REPLACED MODULE FOR SEAT MOUNTED EMERGENCY LIGHT AT SEAT ROWS 21D TO 32D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 64,628 hrs

LGA - EMERGENCY LIGHTS AT SEAT ROWS 5 TO 20 INOPERATIVE. REPLACED LIGHT ASSEMBLY AT SEAT 19DEF FOR INOPERATIVE EMERGENCY LIGHTS AT SEAT ROWS 5 TO 20. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

SDF - AIRCRAFT BATTERIES AND EMERGENCY LIGHTS AT FORWARD CABIN INOPERATIVE. CHARGED AIRCRAFT BATTERY AND REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT FORWARD CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SLIDE — INOPERATIVE (L2 DOOR)

AUS LEFT NUMBER TWO DOOR SLIDE GIRT BAR FLAP DOES NOT HOLD. REPLACED LEFT NUMBER TWO DOOR SLIDE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LANDING GEAR — MALFUNCTIONED (NOSE)

DFW INFLIGHT T1676/28JUL - CREW REPORTED NOSE LANDING GEAR WOULD NOT EXTEND. MANUALLY EXTENDED GEAR. LANDED DFW WITHOUT INCIDENT. INSPECTED WITH NO DEFECTS NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: WIRE — BROKEN (EMERGENCY LIGHT)

SJC - EMERGENCY LIGHTS IN TAIL CONE COMPARTMENT INOPERATIVE. REPAIRED BROKEN WIRE FOR EMERGENCY LIGHTS IN TAIL CONE COMPARTMENT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: ENGINE — FAILED (LEFT)

DFW - INFLIGHT T1166/21 LEFT ENGINE FAILED WITH VERY LOUD BANG THAT WAS FELT AND HEARD IN COCKPIT. ENGINE WAS PREVIOUSLY RUNNING SMOOTHLY AT 1.34. STABILIZED ENGINE PRESSURES RATIO. ENGINE APPEARED TO BE SEIZED. PRELIMINARY INSPECTION REVEALED METAL IN TAILPIPE. REPLACED DAMAGE IN TAILPIPE AREA. REPLACED LEFT ENGINE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (SEAT 27D)

DFW - AFT SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT AT 27D INOPERATIVE. REPLACED THE AFT SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT 27D. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DFW - CABIN CEILING EMERGENCY LIGHTS AT ROWS 13 THROUGH 16 COME ON WHEN THE FLIGHT ATTENDANT SWITCH IS PLACED IN ON POSITION. REPLACED BATTERY PACK B5102 FOR CABIN CEILING EMERGENCY LIGHTS AT ROWS 13 THROUGH 16. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DEN - EMERGENCY LIGHTS AT AFT ATTENDANT CEILING AND AFT STAIR AREA INOPERATIVE. REPLACED BATTERY PACK AT AFT RIGHT HAND LAVATORY FOR EMERGENCY LIGHTS AT AFT ATTENDANT CEILING AND AFT STAIR AREA. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DEN - CEILING EMERGENCY LIGHTS FROM SEATS 18 TO 21 INOPERATIVE. REPLACED BATTERY PACK AT SEAT 20DEF FOR CEILING EMERGENCY LIGHTS FROM SEATS 18 TO 21. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: MODULE — INOPERATIVE (EMERGENCY LIGHTS)

SEA - EMERGENCY SEAT MOUNTED LIGHT FROM 20 AFT INOPERATIVE. REPLACED EMERGENCY LIGHT POWER SUPPLIES AT MID CABIN STATION 833R AND CONTROL MODULE AT 833R. REPLACED EMERGENCY LIGHT POWER SUPPLY AT AFT GALLEY DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONTROLLER — ARCED (COCKPIT WINDOW)

DFW INFLIGHT T802/25 FIRST OFFICERS WINDOW HEAT STARTED ARCHING ACROSS WINDOW AND WINDOW SHATTERED. RETURNED TO STATION. LANDED WITHOUT INCIDENT. REPLACED FIRST OFFICERS WINDOW AND CONTROLLER. SYSTEM GROUND CHECKED NORMAL OPERATION.--CLOSED--

Part: BATTERY PACK — DISCHARGED (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE OBSERVED EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE AT ROW 31. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE HARNESS — FAULTY (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, OBSERVED EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE AT SEAT 9D. REPLACED WIRING HARNESS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SKIN — CRACKED (FS 1380)

TUL - FOUND FUSELAGE SKIN CRACKED AT RIVET ABOVE RIGHT ENGINE PYLON STATION 1380. STOP DRILLED CRACK AND INSTALLED DOUBLER PER SRM 53-30-00-02 PAGE 1. (M)

Part: SEAT TRACK — CORRODED (FS 1194)

TUL - FOUND CORROSION ON NR 3 SEAT TRACK STATION 1194 AROUND SCREW HOLE SEAT TRACK FLANGE. BLENDED OUT CORROSION AND INSTALLED REPAIR STRAP PER 53-20-00-13 SRM. (M)

Part: BEAM — CORRODED (FS 1155-1211)

TUL - FOUND CORROSION ALONG LONGERON 28 LOWER DOOR CUTOUT BEAM AFT CARGO. INSTALLED REPAIR DOUBLER PER SRM 53-10-00-3 FIG 2. (M)

Part: ANGLE — CRACKED (FUSELAGE)

TUL - FOUND ANGLE CRACKED STATION 1474 LEFT OF VERTICAL STABILIZER. REMOVED DAMAGE AND INSTALLED REPAIR DOUBLER PER AARD 53-10-00-2. (M)

Part: WEB — CORRODED (FS 218)

TUL - FOUND CORROSION STATION 218 RBL 12. INSTALLED DOUBLER PER AARD 53-00-00-02. (M)

Part: STIFFENER — DENTED (FS 1287)

TUL - FOUND VERY DEEP DENTS IN FUSELAGE FRAME ON AFT SIDE STATION 1287 BELOW LONGERON 17L. REMOVED OLD STIFFENER/SHEAR TIE. INSTALLED DUPLICATED PART OF 2024-T0, HEAT TREATED TO T-3, .050 THICK DUPLICATED (DUPLICATED ON SHOP ORDER 2202530 DATED 6/21/01). INSTALLED PER SRM 51-30-05 AFTR TREAT/PRIME. (M)

Part: SKIN (FS 473-481)

TUL - FOUND LIGHTNING STRIKES IN FUSELAGE SKIN STATION 473 TO 481 LONGERON 7 LEFT. INSTALLED DOUBLER PER SRM 53-04 FIG 38 SHEET 24-36-37-38. (M)

Part: STIFFENER — CRACKED (FS 1338)

TUL - FOUND FS 1338 PRESSURE BULKHEAD FORWARD FACE UPPER 12 O'CLOCK STIFFENER IS CRACKED .75 INCH AT UPPER MOST END OF ATTACHMENT. REMOVED AND REPLACED VERTICAL STIFFENER ABOVE VAULT DOOR PER MM 51-01. (M)

Part: SKIN (FS 454)

TUL - FOUND LIGHTNING STRIKE PRODUCED ONE BURN HOLE .125 INCH IN DIAMETER AT STATION 454 LONGERON 7 LEFT. REMOVED DAMAGE AND INSTALLED DOUBLER PER SRM 53-04-00 FIG 18 SHEET 24-38. (M)

Part: SKIN — CRACKED (FS 1380)

TUL - FOUND CRACK IN FUSELAGE SKIN STATION 1380, ABOVE L14L, ABOVE LEFT ENGINE PYLON. STOP DRILLED CRACK AND INSTALLED REPAIR DOUBLER PER SRM 53-30-00-02. (M)

Part: LONGERON — CRACKED (FS 160)

TUL - FOUND LONGERON 4 LEFT CRACKED IN RADIUS AT STATION 160. CUT OFF DAMAGED LONGERON AND INSTALLED NEW SECTION PER SRM 53-02 PAG 48-53 FIG 18. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON CUSP AT 522-528 RIGHT. REMOVED CORROSION AND INSTALLED DOUBLER PER AARD 53-00-00-02 AND SRM 53-01 FIG 4. (M)

Part: DOOR FRAME — CRACKED (FUSELAGE)

TUL - FOUND WEB EAR CRACKED AFT OF FORWARD ENTRY DOOR AT STATION 208, LONGERON L15 DOOR JAMB. REPAIRED WITH REPAIR STRAP PER AARD 53-10-00-11. (REPAIR 11- PAX DOOR JAMB INNER SKIN REPAIR - MAJOR)

Part: SEAT TRACK — CORRODED (FS 1088)

TUL - FOUND CORROSION IN TRACK NR 6 AT STATION 1088. REMOVED DAMAGED AREA SEAT TRACK, TREATED AND PRIMED. INSTALLED SEAT TRACK PLUG PER SRM 53-05 FIG 4A, PRIMED AND TREATED AND PAINTED PLUG. (M)

Part: SEAT TRACK — CORRODED (FS 1300)

TUL - FOUND CORROSION ON SEAT TRACK NR 3 AT STATION 1300. CORROSION REMOVED AND SEAT TRACK PLUG INSTALLED PER SRM 53-05, FIG 4A. (M)

Part: SEAT TRACK — CORRODED (FS 232)

TUL - FOUND CORROSION ON SEAT TRACK NR 5 AT STATION 232-237. SEAT TRACK PLUG REPAIR COMPLETED AS PER SRM 53-05 FIG 4A. (M)

Part: SEAT TRACK — CORRODED (FS 1196-1300)

TUL - FOUND CORROSION ON TRACK NR 2 AT STATION 1196-1206 AND 1300. CORROSION REMOVED, SEAT TRACK PLUGS INSTALLED TWO LOCATIONS STATION 1196-1206 AND STATION 1300 PER SRM 53-05 FIG 4A. (M)

Part: TURBINE — LEAKING (ACM BAY)

ABQ - FLT 1216 - AFTER TAKEOFF CAPTAIN REPORTED SMELL OF SMOKE IN COCKPIT AND CABIN. NO ACTUAL SMOKE NOTED. DECLARED EMERGENCY RETURNED ABQ AND LANDED WITHOUT FURTHER INCIDENT. REPLACED TURBINE (AIR CIRCULATION MACHINE). LEAKING OIL. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: SWITCH — DEFECTIVE (RIGHT MLG)

SFO - FLT 1801 - AFTER TAKEOFF ORD WHEN LANDING GEAR RETRACTED, RIGHT MAIN LANDING GEAR REMAINED ILLUMINATED FOR APPROXIMATELY 2 MINUTES AFTER GEAR RETRACTED ADN THEN EXTINGUISHED. NO OTHER ABNORMAL INDICATIONS AND AIRCRAFT PROCEEDED TO SFO, LANDING WITHOUT INCIDENT. REPLACED RIGHT MAIN LANDING GEAR UPLOCK PROXIMITY SWITCH D1-25. ACCOMPLISHED LANDING GEAR RETRACTION CHECK WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: INDICATION LIGHT — MALFUNCTIONED (LANDING GEAR)

SFO - FLT 1801 - DURING APPROACH TO SFO WHEN LANDING GEAR EXTENDED, UNSAFE INDICATION ON ALL 3 LANDING GEARS. ACCOMPLISHED EMERGENCY GEAR EXTENSION CHECKLIST AND OBTAINED 3 GREEN LIGHTS FOLLOWED BY LIGHTS RETURNING TO RED WHEN EMERGENCY GEAR EXTENSION LEVER WAS STOWED. AIRCRAFT LANDED SFO WITHOUT INCIDENT WITH GEAR EXTENSION LEVER NOT STOWED. CHECKED LANDING GEAR PROXIMITY SENSORS AND BITE CHECKED PROXIMITY SWITCH CONTROL UNIT WITH NO DEFECTS FOUND. CHECKED S1-89 SWITCH AND THROTTLE SWITCHES S1-319 AND S1-320 WITH NO DEFECTS FOUND. ACCOMPLISHED LANDING GEAR RETRACTION CHECK WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED, NORMAL OPER. UNABLE TO DUPLICATE PROBLEM AND ACFT RETURNED TO SERVICE. (X)