N565AA

Part: SUMP — CONTAMINATED (ZONE 300) · airframe 88,655 hrs · 40,572 cycles

EMERGENCY DECLARED, LANDING UNEVENTFUL, ACFT NOT OVERWEIGHT, ACFT WAS GNDED. DURING APPROACH THE RUDDER TRAVEL UNRESTRICTED LIGHT DID NOT ILLUMINATE & RUDDER FELT STIFF. APPROACH ABORTED. DURING SECOND APPROACH THE LIGHT ILLUMINATED. THAWED ACFT IN HANGAR & DRAINED MOISTURE FROM RUDDER PITOT TUBE SUMP DRAIN IAW AMM 27-20-00. RUDDER SYS OPERATES FREELY WITH NO FURTHER DEFECTS NOTED AT THIS TIME.

Part: SKIN — CRACKED (FUSELAGE) · airframe 88,084 hrs · 40,226 cycles

CRACK IN FUSELAGE SKIN AT STATION 1437 BETWEEN L3L & L4L. ACCOMPLISHED DOUBLER REPAIR IAW SRM 53-04-00-001.

Part: SWITCH — INOPERATIVE (CABIN PRESSURE) · airframe 85,949 hrs · 39,092 cycles

AIRCRAFT FAILED TO PRESSURIZE ON CLIMB OUT. EMER DECLARED FLIGHT RETURNED & LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. REPLACED BOTH SECOND SEGMENT CLIMB SWITCHES. SYS GND CHECKED NORMAL, OPERATION CLOSED.

Part: OVERHEAT SENSOR — SHORTED (AC BAY) · airframe 84,503 hrs · 38,333 cycles

DFW CREW REPORTED TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. REPLACED RT OVERHEAT TEMPERATURE SENSOR THAT HAD SHORTED. SYS GND CHECKED NORMAL, OPERATION CLOSED.

Part: SKIN — CRACKED (FUSELAGE) · airframe 84,202 hrs · 38,180 cycles

RT HAND FUSELAGE, RT HAND STRUT DOOR, AFT HINGE ATTACH POINT SKIN CRACKED. INSTALLED DOUBLER IAW SRM 53-05-00-001.

Part: RIB — CRACKED (LT WING) · airframe 84,202 hrs · 38,180 cycles

LT HAND WING NR 4 SLAT TRACK INBD RIB CRACKED. INSTALLED DOUBLER IAW EA MD80-57-033447.

Part: SPAR — CRACKED (RT WING) · airframe 84,202 hrs · 38,180 cycles

RT WING REAR SPAR CRACKED AT OTBD FLAP INBD HINGE LOWER INBD ATTACH STUD HOLD. INSTALLED AFT WING SPAR WEB SPLICE AT STATION XRS 95.5 THRU XRS 111 IAW BOEING DRAWING J060165.

Part: GYRO — FAILED (ZONE 100) · airframe 83,779 hrs · 37,953 cycles

BWI CREW REPORTED FIRST OFFICERS DIRECTIONAL GYRO FAILED. EMERGENCY DECLARED FLIGHT RETURNED BWI LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED NR 1 DIRECTIONAL GYRO. SYSTEM GROUND CHECKED NORMAL OPERATION CLOSED.

Part: LENS — MISSING (CABIN) · airframe 83,241 hrs · 37,643 cycles

EMERGENCY LIGHT AT SEAT 14DEF MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 14DEF. OPERATIONS CHECKED NORMAL.

Part: BATTERY — DISCHARGED (CABIN) · airframe 81,474 hrs · 36,727 cycles

CEILING EMERGENCY LIGHTS AT ROWS 6, 7 AND 8 INOPERATIVE. REPLACED BATTERY AND CHARGER AT SEAT 8DEF. OPS CHECK NORMAL.

Part: DUCT — DISCONNECTED (AC BAY) · airframe 81,286 hrs · 36,629 cycles

ORF - CREW REPORTED TAIL COMPARMENT TEMPERATURE HIGH LIGHT ILLUMINATED DURING CLIMBOUT. EMERGENCY DECLARED FLIGHT RETURNED ORF LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. RESECURED LEFT PACK DISCHARGED DUCT THAT WAS DISCONNECTED. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 80,992 hrs · 36,488 cycles

CEILING EMERGENCY LIGHTS FROM ROWS 7 TO 11 INOPERATIVE. RECHARGED BATTERY PACK. OPS CHECK NORMAL.

Part: TERMINAL — LOOSE (BATTERY PACK) · airframe 80,992 hrs · 36,488 cycles

CEILING EMERGENCY LIGHTS FROM ROWS 28 TO ROW 30 INOPERATIVE. SECURED BATTERY PACK TERMINALS. OPS CHECK NORMAL.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 79,825 hrs · 35,935 cycles

CORROSION ON FRAME AT STATION 1309. ACCOMPLISHED FRAME SPLICE DOUBLER REPAIR PER SRM 53-03-00 FIGURE 2A.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 79,825 hrs · 35,935 cycles

CORROSION ON LONGERON 28 RIGHT STATION 1287. INSTALLED NEW LONGERON SECTION/SPLICE REPAIR ON LONGERON 28 RIGHT AT STATION 1287 PER SRM 53-02-00 AND SRM 51-30-05.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 79,825 hrs · 35,935 cycles

RIGHT CUSP SHEET AT STATION 840 CORRODED. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 79,825 hrs · 35,935 cycles

CORROSION UNDER G1 DRAIN PAN. INSTALLED DOUBLER PER AARD53-20-00-16.

Part: PAN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 79,825 hrs · 35,935 cycles

AFT LAVATORY SERVICE PAN CORRODED. REPLACED AFT LAVATORY SERVICE PAN.

Part: SKIN — DENTED (FUSELAGE) · airframe 79,825 hrs · 35,935 cycles

DENT IN FUSELAGE AT STATIONS 370 TO 389, LONGERONS 23 TO 24 LEFT. INSTALLED DOUBLER PER SRM 53-04-02.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 79,825 hrs · 35,935 cycles

SEAT TRACK NUMBER 5 SUPPORT CRACKED AT STATION 927. REPLACED SEAT TRACK SUPPORT PER AARD 51-00-05-1.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 79,825 hrs · 35,935 cycles

CORROSION ON CUSP WEB, RIGHT SIDE OF STATION 180. CUT OUT CORRODED AREA AND SPLICED IN NEW SECTION OF WEB PER AARD 53-20-00-16.

Part: FRAME — CRACKED (FUSELAGE) · airframe 79,825 hrs · 35,935 cycles

STATION 1418 FRAME CRACKED IN RADIUS, AFT SIDE AT LONGERON 2 LEFT. INSTALLED FRAME DOUBLER REPAIR PER SRM 53-01-00 AND AARD 53-10-00-15.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 79,825 hrs · 35,935 cycles

FLOOR SUPPORT AT STATION 927 LEFT BUTTLINE 44 CRACKED. REPLACED ANGLE PER AARD 51-00-05-1.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 79,825 hrs · 35,935 cycles

LONGERON 2 LEFT CRACKED AT STATION 1418. SPLICED IN NEW SECTION OF LONGERON PER SRM 53-02-00 FIGURE 18.

Part: BEAM — CORRODED (FUSELAGE) · airframe 79,825 hrs · 35,935 cycles

CORROSION ON LOWER DOOR BEAM FLANGE AT AFT CARGO DOOR OUT OF LIMITS. INSTALLED DOOR BEAM DOUBLER AS PER AARD 53-10-00-3 FIGURE 3 SHEET 1.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 79,825 hrs · 35,935 cycles

LONGERON 14 LEFT CRACKED AT STATION 160. REMOVED OLD LONGERON AND INSTALLED NEW LONGERON 4 FROM STATIONS 148 TO 229 PER SRM 53-14-01.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 79,825 hrs · 35,935 cycles

LEFT CUSP AT STATION 565 FORWARD OF T-ANGLE CORRODED. INSTALLED DOUBLER AT LEFT CUSP SHEET AT STATION 598 PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 79,825 hrs · 35,935 cycles

LEFT CUSP FROM STATIONS 511 TO 515 CORRODED. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 79,825 hrs · 35,935 cycles

APPROXIMATELY 2 INCH CRACK IN RIGHT CUSP STATION. REPLACED CUSP SHEET FROM STATIONS 1266 TO 1309 PER AARD 51-00-05-1.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 79,825 hrs · 35,935 cycles

LEFT CUSP STATION 598 FORWARD OF T-ANGLE CORRODED. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 79,825 hrs · 35,935 cycles

CUSP CRACKED AT FORWARD LAVATORY TOILET BALL VALVE. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: MOUNT — CORRODED (FUSELAGE) · airframe 79,825 hrs · 35,935 cycles

G-1 GALLEY MOST INBOARD FLOOR MOUNT CORRODED. REPLACED G-1 GALLEY MOUNT PER AARD 51-00-05-1.

Part: SKIN — DENTED (FUSELAGE) · airframe 79,825 hrs · 35,935 cycles

A 1 INCH DENT WITH HIGH METAL, 3 FEET AFT OF OVER PRESSURIZATION VALVES 3 FEET BELOW FLOOR LINE LEFT SIDE OF FUSELAGE. INSTALLED INTERNAL REPAIR DOUBLER, SHIMS AND FILLER PLUG PER SRM 53-04-02 FIGURE 2.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 79,825 hrs · 35,935 cycles

VERTICAL ANGLE CRACKED AT STATION 927, BELOW SEAT TRACK NUMBER 2. REMOVED AND REPLACED VERTICAL ANGLE PER AARD 51-00-05-1.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 79,825 hrs · 35,935 cycles

CENTER VERTICAL STIFFENER ABOVE VAULT DOOR CRACKED AT TOP END. REPLACED STIFFENER PER AARD 51-00-05-1.

Part: SKIN — DAMAGED (RT ELEVATOR) · airframe 79,825 hrs · 35,935 cycles

MULTIPLE HAIL DENTS ON THE RIGHT ELEVATOR. INSTALLED DOUBLER REPAIR AT 102 INCHES FROM I/B EDGE PER SRM 55-03-00 FIG 13A. MRT# 037758.

Part: PUMP — INOPERATIVE (HYDRAULIC SYS) · airframe 79,602 hrs · 35,809 cycles

YYC - CREW REPORTED LOSS OF LEFT HYDRAULIC SYSTEM QUANTITY WITH NO PRESSURE. EMERGENCY DECLARED FLIGHT LANDED YYC WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT ENGINE DRIVEN HYDRAULIC PUMP. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: TRANSMITTER — INOPERATIVE (HYDRAULIC SYS) · airframe 79,542 hrs · 35,786 cycles

ORD - CREW REPORTED HYDRAULIC PRESSURE LOW AND HYDRAULIC QUANTITY ABNORMALLY HIGH ON LEFT SYSTEM. ACCOMPLISHED QRH PROCEDURE. EMERGENCY DECLARED FLIGHT LANDED ORD WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT HYDRAULIC QUANTITY TRANSMITTER. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: TUBE — BROKEN (AC BAY) · airframe 79,513 hrs · 35,770 cycles

PHX - CREW REPORTED DURING CLIMBOUT TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED. EMERGENCY DECLARED FLIGHT RETURNED PHX LANDED WITHOUT INCIDENT. REPLACED TUBE ASSEMBLY-TURBINE NOZZLE TO EJECTOR VALVE LINE. REPLACED PERISEALS AT COUPLING FORWARD OF HEAT EXCHANGER. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: ENGINE — FAILED (LEFT) · airframe 79,508 hrs · 35,767 cycles

RDU - CREW REPORTED DURING CLIMBOUT LEFT ENGINE OIL PRESSURE INDICATION WENT TO ZERO. PERFORMED IN-FLIGHT SHUTDOWN OF LEFT ENGINE (SINGLE ENGINE TIME 24 MINS). EMERGENCY DECLARED FLIGHT RETURNED RDU LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT ENGINE AT RDU ON 05/20/2012. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: SPAR CAP — DAMAGED (VERTICAL STAB) · airframe 79,371 hrs · 35,692 cycles

UNABLE TO PERFORM HFEC ROTARY HOLE PROBE INSPECTION TO AREA 12.5" BELOW LEFT SIDE OF VERTICAL STABILIZER FRONT SPAR CAP AT STATION ZFS=52.267, BECAUSE THE FASTENER HOLES IN THE SPAR CAP FORWARD FLANGE (12EACH) ARE OUT OF ALIGNMENT WITH REFERENCE TO HOLES IN THE DORSAL FIN LOWER ASSEMBLY. INSTALLED DOUBLER PER SRM 55-03-00 FIGURE 31.

Part: COMPUTER — FAILED (COCKPIT) · airframe 79,327 hrs · 35,664 cycles

DFW - CREW REPORTED COMPUTER FAILURE CAUSING AURAL WARNING ON CLIMBOUT. FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED CENTRAL AURAL WARNING COMPUTER. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 77,869 hrs · 34,946 cycles

FORWARD CABIN AND FLIGHT DECK EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK AT FORWARD LAVATORY DROP CEILING. OPS CHECK NORMAL.

Part: BATTERY — NOT SEATED (CABIN) · airframe 77,326 hrs · 34,661 cycles

EMERGENCY LIGHTS IN TAIL COMPARTMENT INOPERATIVE. RESEATED BATTERIES FOR TAIL COMPARTMENT EMERGENCY LIGHTS. OPS CHECK NORMAL.

Part: BATTERY — NOT SEATED (CABIN) · airframe 77,326 hrs · 34,661 cycles

EMERGENCY LIGHTS AT ROWS 3 TO 6, 28-30, AND IN TAIL COMPARTMENT. RESEATED BATTERIES FOR ROWS 3-6, 28-30, AND TAIL COMPARTMENT, ALL CHECKS NORMAL.

Part: BATTERY — NOT SEATED (CABIN) · airframe 77,326 hrs · 34,661 cycles

EMERGENCY LIGHTS AT ROWS 28 TO 30 INOPERATIVE. RESEATED BATTERIES FOR ROWS 28 TO 30 EMERGENCY LIGHTS. OPS CHECK NORMAL.

Part: SMOKE DETECTOR — INOPERATIVE (LAVATORY) · airframe 76,567 hrs · 34,266 cycles

DFW - FLIGHT ATTENDANT REPORTED SMOKE FROM RIGHT AFT LAVATORY TRASH CONTAINER DUE TO CIGARETTE. SMOKE DETECTOR DID NOT GO OFF. EXTINGUISHED WITH HAND HELD FIRE EXTINGUISHERS. FLIGHT LANDED DFW WITHOUT ICIDENT. REPLACED BOTH FIRE EXTINGUISHERS AND SMOKE DETECTOR. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: SKIN — CRACKED (FUSELAGE) · airframe 76,103 hrs · 34,035 cycles

CRACK IN SKIN STATION 1429 ABOVE LONGERON 4 RIGHT 1.25 INCHES LONG. INSTALLED DOUBLER PER SRM 53-01-00.

Part: BATTERY PACK — NOT SEATED (CABIN) · airframe 73,599 hrs · 32,825 cycles

DURING TEST OF EMERGENCY LIGHT SYSTEM FOUND AFT CABIN OVERHEAD AND AFT ACCESSORY COMPARTMENT (CATWALK AND INTERIOR TAIL CONE AREA) OVERHEAD EMERGENCY LIGHTS INOPERATIVE. RESEATED AND SECURED BATTERY PACKS IN AFT RIGHT LAVATORY OVERHEAD PANEL. ALL EMERGENCY LIGHTS CHECK NORMALLY DURING TEST.

Part: CONTROL VALVE — INOPERATIVE (RIGHT) · airframe 73,057 hrs · 32,592 cycles

ORD - ON DEPARTURE AIRCRAFT FAILED TO PRESSURIZE. RETURNED ORD WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND RIGHT FLOW CONTROL VALVE STICKING IN CLOSED POSITION. REPLACED RIGHT CONTROL VALVE. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 71,986 hrs · 32,120 cycles

EMERGENCY LIGHT BATTERY PACK IS WEAK. REPLACED BATTERY PACK FOR EMERGENCY LIGHT UNDER AMM 33-60-98-4.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 71,986 hrs · 32,120 cycles

EMERGENCY LIGHT BATTERY PACK IS WEAK. REPLACED BATTERY PACK FOR EMERGENCY LIGHT UNDER AMM 33-60-98-4.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 71,986 hrs · 32,120 cycles

EMERGENCY LIGHT BATTERY PACK IS WEAK. REPLACED BATTERY PACK FOR EMERGENCY LIGHT UNDER AMM 33-60-98-4.

Part: BATTERY PACK — DISCONNECTED (EMERGENCY LIGHTS) · airframe 70,202 hrs

LGA - EMERGENCY LIGHTS AT AFT GALLEY INOPERATIVE. RECONNECTED BATTERY PACK AT AFT GALLEY.

Part: CAM — WORN (TAILCONE) · airframe 68,045 hrs · 30,369 cycles

TUL - TAILCONE RELEASE MECHANISM CAM IS WORN. REPLACED TAILCONE MECHANISM CAM ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: STRUT — INOPERATIVE (NOSE GEAR)

YYC INFLIGHT T1166/03DEC - NOSE GEAR WOULD NOT RETRACT AFTER TAKEOFF. RETURNED TO YYC AND LANDED WITHOUT INCIDENT. ACCOMPLISHED NOSE STRUT REPAIR AND GEAR SWING. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

LGA - BOTH FORWARD EMERGENCY OVERWING EXIT LIGHTS INOPERATIVE. RESET BATTERY IN EMERGENCY LIGHT BATTERY PACK FOR BOTH FORWARD EMERGENCY OVERWING EXIT LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

OVERHEAD LT AND RT OVERWING EMERGENCY EXIT SIGNS INOPERATIVE. REPLACED BATTERY PACK FOR OVERHEAD LEFT AND RIGHT HAND OVERWING EMERGENCY EXIT SIGNS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

SEA - AFT ENTRY OVERHEAD EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED BATTERY PACK AT B527 FOR AFT ENTRY OVERHEAD EMERGENCY EXIT LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DEN - EMERGENCY LIGHTS AT B5-27 INOPERATIVE. REPLACED BATTERY PACK AT B5-27 FOR EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: WIRE — OVERHEATED

WIRE RING TERMINALS AT RESISTOR R4-9 SHOWS SIGNS OF OVERHEATING. REPLACED WIRE RING TERMINALS AT R4-9 RESISTOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: WIRE — OVERHEATED (COCKPIT)

TUL POWER CABLE TERMINAL ENDS ON WIRES 3X1C2A, 3X2C2B, AND 3X3C2C AT LEFT AUXILLARY POWER RELAY T1, T2, AND T3, AND AT S3-23, 1, 2, 3 POSTS AND WIRE RING TERMINALS OF WIRES 3X2T20B AND 3X3T20C AT S3-23 POSTS 2 AND 3 SHOWS SIGNS OF OVERHEATING. REPLACED POWER CABLES 3X1C2A, 3X3C2C, AND 3X3C2C AND REPLACED RING TERMINALS ON WIRES 3X2T20B AND 3X3T20C AT S3-23. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: WIRE — DAMAGED (CABIN)

DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SIDEWALL LIGHTS INOPERATIVE. REPAIRED WIRE ON EMERGENCY EXIT SIDEWALL LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, ENTRY CEILING EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SKIN — DENTED (FUSELAGE)

TUL - FOUND DENT IN FUSELAGE STATION 1309 LONGERON 18R, ADL NR 5650034. INSTALLED DOUBLER PER SRM 53-04 FIG 38 SHEET 23 AND INSTALLED SCUFF PLATE PER AARD 53-30-00-8 PAGE 1/2. (M)

Part: SKIN — GOUGED (NR 2 SLAT)

TUL - FOUND TWO DEEP GOUGES IN FIXED L/E AFT OF NR 2 SLAT INBOARD OF NR 7 SLAT TRACK. REPAIRED FORWARD DAMAGED AREA PER SRM 57-06B. (M)

Part: SKIN — CORRODED (FUSELAGE)

TUL - FOUND DOOR CUTOUT (AFT CARGO) CHORD ANGLE BOTTOM OF DOOR CUTOUT CORRODED NUMEROUS AREAS STATION 1155-1211. REMOVED CORROSION. INSTALLED DOUBLER REPAIR PER ESO 80559 DATED 08-09-2000. (M)

Part: FRAME — CRACKED (FUSELAGE)

TUL - FOUND STATION 630 FRAME WEB CRACKED AT LOWER FORWARD WEB CUT OUT. REMOVED WEB SECTION WITH CRACK. INSTALLED NEW SECTION PER AARD 53-10-00-2-1 PAGE 1. (M)

Part: SKIN — DENTED (FUSELAGE)

TUL - FOUND BELLY SKIN DENTED STATION 389, LONGERON 29R TO LONGERON 29L. INSTALLED DOUBLER AND FILLER PER SRM 53-04 PAGE 33-39. (M)

Part: SKIN — DAMAGED (FUSELAGE)

TUL - FOUND LARGE SCRAPE ALONG FUSELAGE SKIN STATION 294-370. CUT OUT THE OUT OF LIMITS AREA AND INSTALLED DOUBLER PER SRM 53-04 PAGE 33. (M)

Part: SKIN — DENTED (CARGO DOOR)

TUL - FOUND DENT FOUND OF FORWARD CARGO DOOR. CUT OUT DAMAGED AREA AND INSTALLED DOUBLER PER SRM 53-04 PAGE 33. (M)

Part: LONGERON — DAMAGED (FUSELAGE)

TUL - FOUND LONGERON 20R DAMAGED STATION 332. CUT OUT DAMAGE AND INSTALLED SPLICE PER SRM SRM 53-02 PAGE 48 FIG 18. (M)

Part: PANEL — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON RIGHT CUSP PANEL, STATION 1210-1227, RIGHT CUSP, CORROSION RUNS UNDER SEAT TRACK THIS AREA. CUT OUT CORRODED AREA AND APPLIED DOUBLER PER AARD 53-00-00-02. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON SEAT TRACK NR 1 STATION 796. REMOVED DAMAGED SECTION, SPLICED IN NEW SECTION PER SRM 53-05 PART 1. (M)

Part: LONGERON — CRACKED (FUSELAGE)

TUL - FOUND LONGERON NR 3 LEFT CRACKED AT FRAME NR 160 LEFT AT HUCK FASTENER IN LONGERON. INSTALLED LONGERON REPAIR, AS PER SRM 53-02. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON CUSP MEMBRANE STATION 1307 LEFT BETWEEN NR 1 AND NR 2 SEAT TRACKS. CUT OUT CORROSION 1 INCH BY 1.5 INCHES AND INSTALLED REPAIR DOBLER PER AARD 53-00-00-2. (M)

Part: SKIN — GOUGED (NR 2 SLAT)

TUL - FOUND 2 DEEP GOUGES IN FIXED L/E AFT OF NR 2 SLAT INBOARD OF NR 7 SLAT TRACK. REPAIRED AFT DAMAGED AREA PER AARD 57-30-00-8. (M)

Part: LONGERON — CRACKED (FUSELAGE)

TUL - FOUND NR 4 LONGERON CRACKED AT ATTACH POINT AT FRAME NR 160 LEFT SIDE. REMOVED AND REPLACED LONGERON NR 4 AND SPLICED PER SRM 53-02. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON CUSP MEMBRANE STATION 801 RIGHT. TRIMMED OUT CORROSION AND INSTALLED REPAIR DOUBLER PER AARD 53-00-00-2 SRM 53-01 FIG 4. (M)

Part: CARGO TRACK — CORRODED (FUSELAGE)

TUL - FOUND RIGHT CARGO TIE DOWN TRACK CORRODED IN CENTER OF TRACK STATION 1079 TO STATION 1155, ALSO CORRODED ON OUTBOARD FLANGE STATION 1155. REMOVED TIE DOWN TRACK AND INSTALLED NEW TRACK SRM 51-01. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL - FOUND SEAT TRACK NR 2 HAS CORROSION AT STATION 1202. ACCOMPLISHED SEAT TRACK PLUG REPAIR PER AARD 53-20-00-10. (M)

Part: SWITCH — BROKEN (CONTROL COLUMN)

AIRCRAFT DEPARTED PHOENIX SKY HARBOR INT'L AIRPORT AND RETURNED WHEN CREW ENCOUNTERED A STABILIZER TRIM MALFUNCTION. THE FLIGHT CREW REPORTED INTERMITTENT OPERATION AND THEN A LOSS OF BOTH THE PRIMARY AND ALTERNATE SYSTEMS. TROUBLESHOOTING DETERMINED THE TRIM SWITCH IN THE FIRST OFFICER'S CONTROL COLUMN FOR THE TRIM MOTOR SIDE HAD FAILED INTERNALLY CAUSING UNCOMMANDED INTERMITTENT OPERATION OF THE PRIMARY TRIM MOTOR CAUSING IT TO OVERHEAT AND TRIP THROUGH THE INTERNAL THERMAL PROTECTIVE DEVICE. THE SWITCH WAS REPLACED AND THE TRIM SYSTEM FUNCTIONED NORMALLY. (X)

Part: SWITCH — DEFECTIVE (COCKPIT)

PHX - FLT 1538 - DURING FLIGHT AT 13,000 FEET STABILIZER TRIM JAMMED. OPERATION INTERMITTENT THEN BOTH SYSTEMS INOPERATIVE. DIVERTED AND LANDED PHX WITHOUT INCIDENT. USED EXTRA BACK PRESSURE TO MAINTAIN FLIGHT. REPLACED HORIZONTAL STABILIZER TRIM CONTROL. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: SWITCH — FAILED (COCKPIT)

ORD - FLT 1224 - EN ROUTE SAN-ORD - ON APPROACH SLAT DISAGREE LIGHT ILLUMINATED WHEN FLAPS EXTENDED TO 15 DEGREES. CREW DECLARED AN EMERGENCY. LIGHT EXTINGUISHED AFTER APPROX 30 MINUTES. LANDED ORD WITHOUT INCIDENT. REPLACED FLAPS/SLAT HANDLE SWITCH. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SUPPORT — CORRODED (BS 256)

TUL - CORROSION ON LAVATORY SUPPORT STRUCTURE AFT END BETWEEN SEAT TRACKS NR 2 AND NR 3 AT STA 256. INSTALLED MANUFACTURED SUPPORT. (X)

Part: SEAT TRACK — CORRODED (BS 1309)

TUL - CORROSION IN NR 2 SEAT TRACK AT STA 1309. REMOVED SEAT TRACK SECTION FROM STA 1262 TO STA 1309. SPLICED IN NEW SECTION PER SRM 53-05. TST: 33,318.18 HOURS. CYCLES: 15,937. (X)

Part: CUSP — CORRODED (BS 190)

TUL - CORROSION ON CUSP. CUT OUT CORRODED SECTION AND INSTALLED DOUBLER PER SRM 53-01. (X)