N590AA

Part: CONTROL BOX — FAULTY (ZONE 700) · airframe 80,066 hrs · 36,279 cycles

AIRCRAFT WAS GROUNDED. IN CRUISE FLT AT 310, WE RECEIVED AUDIBLE SLAT OVERSPEED SLAT DISAGREE LIGHT AND RIGHT GEAR UNSAFE RED LIGHT, ALL 3 LASTED 1 MINUTE AND WENT BACK TO NORMAL. MAINTENANCE REPLACED PROXIMITY (CONTROL) BOX PER MM 32-60-04 AND ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.

Part: BATTERY PACK — NO TEST (FLASHLIGHT) · airframe 79,651 hrs · 36,017 cycles

FLIGHT ATTENDANT EMERGENCY LED FLASHLIGHT AT THE AFT JUMPSEAT DOES NOT FLASH. REMOVED AND REPLACED FLASHLIGHT BATTERY PACK IAW AMM 33-00-00. OPS CHECKED GOOD.

Part: AUTOBRAKE SYS — MALFUNCTIONED · airframe 79,392 hrs · 35,852 cycles

AFTER TOUCHDOWN, WITH AUTO BRAKE SELECTED AND ARMED, THERE WAS A SHARP JOLT AND THE AUTO BRAKES DISENGAGED. AUTO BRAKE FAIL LIGHT ILLUMINATED. TROUBLESHOT AUTOMATIC BRAKE SYSTEM IAW AMM 32-44-00-101 WITH NO FAULTS FOUND. OPERATIONAL CHECKED GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 78,597 hrs · 35,351 cycles

EMERGENCY CEILING LIGHTS INOP FROM ROW 13 TO 16. REMOVED & REPLACED BATT PACK. EMERGENCY LIGHTS OP CHK OK. THE AIRCRAFT WAS NOT GROUNDED.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 78,158 hrs · 35,079 cycles

TWO FORWARD OVERWING EMERGENCY EXIT LIGHTS ARE INOPERATIVE. REMOVED AND REPLACED THE BATTERY PACK IAW AMM 33-53-00. OPS CHECKED GOOD.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 77,987 hrs · 34,972 cycles

FORWARD CARGO DOOR FORWARD 4TH FROM BOTTOM STOP FITTING IS CRACKED. REMOVED AND REPLACED THE STOP FITTING IAW 51-00-05-1 AND DRAWING 3187063.

Part: FITTING — CRACKED (CARGO DOOR) · airframe 77,987 hrs · 34,972 cycles

FORWARD CARGO DOOR FORWARD BOTTOM STOP FITTING IS CRACKED. REMOVED AND REPLACED THE STOP FITTING IAW 51-00-05-1 AND DRAWING. 3187062.

Part: SKIN — CRACKED (BS 1309) · airframe 77,987 hrs · 34,972 cycles

FUSELAGE SKIN IS CRACKED FROM FASTENER HOLE AT BS 1309 JUST ABOVE LONGERON 7L. REPAIRED SKIN IAW SRM 53-04-00 FIGURE 32 AND EA 266587.

Part: RETAINING CLIP — DIRTY (ZONE 800) · airframe 77,920 hrs · 34,926 cycles

AIRCRAFT NOT GROUNDED. AFT GALLEY DOOR GIRT BAR RETAINER CLIPS NEED CLEANING. CLEANED CLIPS IAW AMM 25-62-00. OPERATIONAL CHECK GOOD.

Part: LIGHT — FAULTY (CABIN) · airframe 76,642 hrs · 34,136 cycles

L1 PORTABLE EMERGENCY LIGHT IS INOPERATIVE. REMOVED AND REPLACED LIGHT ASSEMBLY IAW AMM 33-53-00. OPERATIONAL CHECK NORMAL.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 76,642 hrs · 34,136 cycles

OVERHEAD EMERGENCY LIGHTS BY AFT CBIN DOOR WILL NOT TEST. REMOVED AND REPLACED AFT CABIN EMERGENCY BATTERY ASSEMBLY IAW AMM 33-53-00. OPERATIONAL CHECK NORMAL.

Part: SENSOR — OUT OF ADJUST (LE SLAT) · airframe 76,274 hrs · 33,914 cycles

AIRCRAFT WAS NOT GNDED. DURING APPROACH RECEIVED A SLATS DISAGREE INDICATION & AUTO THROTTLES DISENGAGED. FOUND MID SLAT POSITION SENSOR OUT OF ADJUSTMENT. ADJUSTED IAW AMM 27-80-00. SYS CHECKED NORMAL.

Part: SMOKE DETECTOR — INOPERATIVE (LAVATORY) · airframe 75,502 hrs · 33,470 cycles

EMERGENCY LANDING DECLARED. ACCOUNT RT AFT LAVATORY PAPER TOWEL DISPENSER WAS ON FIRE. FLIGHT ATTENDANT PUT OUT FIRE WITH HALON BOTTLE. THE SMOKE DETECTOR DID NOT OPERATE. ACFT LANDED SAFELY. REMOVED RT LAVATORY PAPER TOWEL DISPENSER DOOR & INSPECTED PAPER TOWEL COMPARTMENT FOR DAMAGE, NO DEFECTS NOTED. REPLACED DISPENSER DOOR, AFT LT CABIN HALON PORTABLE FIRE EXTINGUISHER BOTTLE & RT LAVATORY SMOKE DETECTOR. THE ACFT WAS GNDED.

Part: CONTROLLER — MALFUNCTIONED (CABIN PRESSURE) · airframe 72,985 hrs · 32,024 cycles

EMERGENCY DECLARED, LANDING UNEVENTFUL & ACFT WAS NOT OVERWEIGHT. LOSS OF CABIN AUTO PRESSURIZATION CONTROL INBD. CREW SWITCHED TO MANUAL CONTROL & LANDED WITHOUT INCIDENT. REPLACED COCKPIT PRESSURE CONTROLLER IAW 21-32-00.

Part: FITTING — LEAKING (LT ENGINE) · airframe 72,843 hrs · 31,946 cycles

AIR INTERRUPT, DIVERTED & EMER DECLARED. LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. DURING CRUISE, CREW REPORTED LOSS OF LT ENG OIL QTY. ENGINE SHUTDOWN IN FLIGHT. FOUND A LEAK AT THE LP 6 GEAR BOX BANJO FITTING. REPAIRED IAW TI 217 322R7 & 72-61-01. PERFORMED ENG RUN & LEAK CHECK IAW CARD 7907.

Part: CASTING — CRACKED (RT SPOILER) · airframe 70,421 hrs · 30,674 cycles

RIGHT WING GND SPOILER ACTUATOR CASTING IS CRACKED ABOVE THE OTBD END OF THE ACTUATOR FWD MOUNT. REPLACED GND SPOILER ACTUATOR CASTING.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 70,421 hrs · 30,674 cycles

CORROSION ON SEAT TRACK NR 5 FROM STATIONS 200 TO 243 CORRODED. SPLICED SEAT TRACK NR 5 FROM STATIONS 200 TO 243 IAW SRM 53-05-00 FIGURE 4F.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 70,421 hrs · 30,674 cycles

CORROSION ON NR 6 SEAT TRACK FROM STATIONS 218 TO 323 CORRODED. R & R SEAT TRACK IAW SRMS 53-40-01-2, SRM 53-05-00 FIGURE 4 & AARD 53-00-00-08.

Part: DIAPHRAGM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 70,421 hrs · 30,674 cycles

STATIONS 160 TO 200 & RBL 42 TO 57 SUBFLOOR CORRODED. INSTALLED DOUBLER IAW AARD 53-20-00-16.

Part: MOUNT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 70,421 hrs · 30,674 cycles

GALLEY MOUNT AT STATION 218 & RBL 11 CORRODED. REPLACED MOUNT IAW AARD 51-00-05-1.

Part: SPLICE — CORRODED (FUSELAGE) · airframe 70,421 hrs · 30,674 cycles

FORWARD CARGO SEAL DEPRESSOR SPLICES FWD & AFT OF LOWER DOOR ARE CORRODED. INSTALLED NEW SEAL DEPRESSOR SPLICE IAW AARD 51-00-05-1.

Part: MOUNT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 70,421 hrs · 30,674 cycles

GALLEY MOUNT AT END OF NR 6 SEAT TRACK & STATION 216 CORRODED. REMOVED & INSTALLED NEW MOUNT IAW AARD 53-00-05.

Part: MOUNT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 70,421 hrs · 30,674 cycles

CORROSION ON GALLEY SUPPORT, 11 INCHES RT FROM CTR AT STATION 168. INSTALLED NEW GALLEY MOUNT IAW AARD 51-00-05-1.

Part: DIAPHRAGM — DAMAGED (FUSELAGE) · airframe 70,421 hrs · 30,674 cycles

FOUND HOLES IN SUBFLOOR AT RBL 6 & STATION 147. CUT OUT DAMAGE & INSTALLED DOUBLER IAW AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 70,421 hrs · 30,674 cycles

CORROSION ON CUSP FROM STATIONS 200 TO 218. INSTALLED DOUBLER IAW AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 70,421 hrs · 30,674 cycles

CORROSION ON CUSP SHEET FROM STATIONS 218 TO 235. REPLACED CUSP SHEET IAW AARD 51-00-05-1.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 70,421 hrs · 30,674 cycles

CORROSION ON CUSP TEE ANGLE FROM STATIONS 200 TO 207. INSTALLED DOUBLER IAW AARD 53-20-00-14.

Part: PIN — CRACKED (RADOME) · airframe 70,421 hrs · 30,674 cycles

CRACK AT RADOME GUIDE PIN AT STATION 37, 6 O`CLOCK POSITION. STOP DRILLED CRACK & INSTALLED DOUBLER IAW SRM 53-01-00 FIGURE 2 SHEET 3.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 70,421 hrs · 30,674 cycles

CORROSION ON GALLEY SUPPORT 11 INCHES FROM RT FROM CTR AT STATION 148. REPLACED SUPPORT IAW AARD 51-00-05-1.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 70,421 hrs · 30,674 cycles

CRACK FOUND AT STATION 37, 4 O`CLOCK POSITION LT SIDE. CUT OUT CRACK, INSTALLED DOUBLER & FILLER IAW AARD 53-10-00-19.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 70,421 hrs · 30,674 cycles

CRACKED INTERCOSTAL AT STATION 1041 & BL 0. REMOVED & INSTALLED NEW INTERCOSTAL.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 3 · airframe 70,421 hrs · 30,674 cycles

CORROSION ON CUSP AT STATION 575. REMOVED DAMAGED SECTION & INSTALLED DOUBLER IAW AARD 53-20-00-16.

Part: FRAME — GOUGED (FUSELAGE) · airframe 70,421 hrs · 30,674 cycles

DAMAGE TO FRAME STATION 1231, LT HAND BETWEEN LONGERONS 7 & 8. ACCOMPLISHED REINFORCING REPAIR DOUBLER IAW SRM 51-70-05 & EA MD80-53-034063.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 3 · airframe 70,421 hrs · 30,674 cycles

CORROSION ON RT HAND CUSP FROM STATIONS 510 TO 522 OTBD OF NR 6 SEAT TRACK. REMOVED DAMAGED SECTION & INSTALLED REPAIR DOUBLER IAW AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 70,421 hrs · 30,674 cycles

CARGO AFT CARGO CORROSION ON BOTTOM OF LT HAND CUSP SIDE FROM STATIONS 1174 TO 1176. INSTALLED DOUBLER IAW AARD 53-20-00-16.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 70,421 hrs · 30,674 cycles

CORROSION ON FWD DOOR BEAM SUPPORT AT STATION 1155 AFT CARGO. INSTALLED NEW CORNER FITTING IAW SRM 51-30-05.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 70,421 hrs · 30,674 cycles

LEFT HAND AFT CARGO TIE DOWN TRACK FROM STATIONS 1210 TO 1268 CORRODED. REPLACED TRACK IAW SRM 53-01-00.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 70,421 hrs · 30,674 cycles

AFT CARGO CORROSION ON DOOR BEAM STATIONS 1155 TO 1212. INSTALLED DOUBLER IAW SRM 53-01-00.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 70,421 hrs · 30,674 cycles

CORROSION ON NR 1 SEAT TRACK ATTACH ANGLE, AFT SIDE OF FLOOR BEAM, STATION 1174, AROUND SEAT TRACK BOLT HOLES. REMOVED & INSTALLED NEW SERVICEABLE FLOOR BEAM END FITTING IAW AARD 51-00-05-1.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 70,421 hrs · 30,674 cycles

FORWARD UPPER WINDOW FRAME CRACKED THRU FASTENER HOLE FROM STATIONS 946 TO 965 RT HAND. INSTALLED DOUBLER IAW AARD 53-10-025.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 70,421 hrs · 30,674 cycles

CRACKED GUSSET AT STATION 210. FABRICATED & INSTALLED NEW GUSSET IAW AARD 53-10-00-11.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 70,421 hrs · 30,674 cycles

RIGHT HAND FWD LOWER WINDOW FRAME CRACKED AT STATION 1136. INSTALLED DOUBLER IAW AARD 53-10-00-25.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 70,421 hrs · 30,674 cycles

WINDOW FRAME CRACKED AT STATION 1097 & STRINGER 14 LT. INSTALLED DOUBLER ANGLE IAW AARD 53-10-00.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 70,421 hrs · 30,674 cycles

CRACK IN UPPER FWD CORNER OF WINDOW FRAME AT STATION 888 LT HAND. INSTALLED DOUBLER IAW AARD 53-10-00-25.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 70,421 hrs · 30,674 cycles

WINDOW FRAME AT STATION 1061 & STRINGER 14 LT CRACKED, INSTALLED DOUBLER IAW AARD 53-10-00-25.

Part: DIAPHRAGM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 70,421 hrs · 30,674 cycles

CORROSION ON BOTTOM OF SUBFLOOR STATION 160 JUST INBD OF FWD SERVICE DOOR JAMB. CUT OUT CORRODED AREA OF SUBFLOOR & INSTALLED DOUBLER IAW AARD 53-20-00-16.

Part: STRUT — LOW (NLG) · airframe 70,220 hrs · 30,574 cycles

ATL CREW REPORTED ON LG RETRACTION THE NOSE GEAR DOOR DID NOT CLOSE & RED NOSE GEAR DOOR LIGHT REMAINED ON. EMERGENCY DECLARED FLIGHT RETURNED ATL LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. SERVICED NLG STRUT. SYS GND CHECKED NORMAL OPERATION CLOSED.

Part: PORTABLE LIGHT — INOPERATIVE (CABIN) · airframe 70,012 hrs · 30,466 cycles

LT NR 1 DOOR PORTABLE EMERGENCY LIGHT INOPERATIVE. REPLACED LT NR 1 DOOR PORTABLE EMERGENCY LIGHT. OPERATIONS CHECKED NORMAL.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 66,747 hrs · 28,764 cycles

AFT CARGO INNER SKIN DOUBLER HAS CORROSION FROM STATIONS 1155 TO 1212. INSTALLED DOUBLER ON INNER SKIN DOUBLER PER EA MD80-53-027062.

Part: BUNGEE CYLINDER — BROKEN (RT MLG) · airframe 66,411 hrs · 28,597 cycles

DFW - CREW REPORTED DURING GEAR RETRACTION RIGHT GEAR UNSAFE INDICATION. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND RIGHT MAIN LANDING GEAR BUNGEE CYLINDER FRACTURED AT UPPER ATTACH POINT. REMOVED AND REPLACED BUNGEE CYLINDER. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: MOUNT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 66,056 hrs · 28,425 cycles

CENTER G-1 GALLEY MOUNT AT STATION 160 CORRODED. INSTALLED NEW G1 GALLEY MOUNT PER AARD 51-10-00-5.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 66,056 hrs · 28,425 cycles

LOWER CUSP UNDER G-1 GALLEY HAS CORROSION AT DRAIN. INSTALLED REPAIR DOUBLER FROM RIGHT BUTTLINES 39.5 TO 52 AND STATIONS 149 TO 160 PER AARD 53-20-00-16.

Part: WARNING SYSTEM — ACTIVATED (AC BAY) · airframe 63,268 hrs · 27,012 cycles

DFW - CREW REPORTED TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED AFTER TAKEOFF. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. CURRENTLY UNDERGOING MAINTENANCE FOR MULTIPLE LEAKS. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: SWITCH — DEFECTIVE (AC BAY) · airframe 61,262 hrs · 26,061 cycles

DFW - CREW REPORTED DURING CLIMB TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED. POWER WAS REDUCED AND LIGHT WENT OUT BUT WHEN POWER WAS APPLIED TO ENGINES LIGHT CAME BACK ON. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED RIGHT AND LEFT OVER TEMP SWITCHES AND SENSORS. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 60,304 hrs · 25,605 cycles

SEAT MOUNT ESCAPE LIGHTS INOPERATIVE. REPLACED BATTERY PACK.

Part: FRAME — CRACKED (FUSELAGE) · airframe 58,526 hrs · 24,772 cycles

FRAME AND STIFFENER CRACK AT LONGERON 2 RIGHT AT STATION 1418. INSTALLED REPAIR DOUBLERS PER ENGINEERING AUTHORIZATION MD80-53-0082 60.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,526 hrs · 24,772 cycles

CORROSION ON SKIN AT MID CARGO STATION 726 TO 731, LONGERON 29 RIGHT TO 30 RIGHT. REMOVED CORROSION AND REPAIRED WITH EXTERNAL DOUBLER IAW SRM 53-04-00 FIG 12B, SHT 6.

Part: BEAM — CORRODED (CARGO BAY) · corrosion level 2 · airframe 58,526 hrs · 24,772 cycles

CORROSION AT MID CARGO ALONG LOWER DOOR CUTOUT BEAM AT STATION 636 TO 655. INSTALLED REPAIR DOUBLER PER AARD 53-10-00-03.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 58,526 hrs · 24,772 cycles

CUSP CRACKED AT LIGHTENING AT STATION 220, RIGHT SIDE. REMOVED AND REPLACED CUSP PER AARD 53-20-00-16.

Part: WEB — CORRODED (FUSELAGE) · airframe 58,526 hrs · 24,772 cycles

WEB MEMBRANE CUT AT INBOARD OF NUMBER 4 SEAT TRACK AT STATION 218. REPAIRED WEB MEMBRANE PER SRM 53-14-01 AND AARD 53-20-00-16.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 58,526 hrs · 24,772 cycles

FUSELAGE TO VERTICAL STABILIZER ATTACH ANGLE CRACKED. REMOVED DAMAGE AND INSTALLED REPAIR ANGLE PER AARD 53-10-00-2.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 58,526 hrs · 24,772 cycles

CRACK IN LEFT CUSP AT STATION 215. INSTALLED NEW CUSP SHEET.

Part: STOP FITTING — CRACKED (FUSELAGE) · airframe 58,526 hrs · 24,772 cycles

AFT PRESSURE BULKHEAD JAMB HAS CRACKED STOP. INSTALLED NEW STOP.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,526 hrs · 24,772 cycles

RIGHT CUSP AT STATION 732 TO 738 CORROSION OUT OF LIMITS. INSTALLED DOUBLER AT STATION 732 TO 738 PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,526 hrs · 24,772 cycles

CORROSION ON CUSP OUT OF LIMITS STATION 160. INSTALLED DOUBLERS PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,526 hrs · 24,772 cycles

CUSP CORROSION OUT OF LIMITS. INSTALLED CUSP REPAIR PER AARD 51-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,526 hrs · 24,772 cycles

CORROSION OUT OF LIMITS ON CUSP AT STATION 418 LEFT SIDE. REMOVED CORROSION AND INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: SKIN — SCRATCHED (FUSELAGE) · airframe 58,526 hrs · 24,772 cycles

DEEP SCRATCH IN FUSELAGE AT APPROXIMATELY STATION 245 ABOVE LONGERON 18 LEFT. INSTALLED DOUBLER PER SRM 53-04-02.

Part: RIB — CRACKED (LE SLAT) · airframe 58,526 hrs · 24,772 cycles

NUMBER 5 LEFT SLAT AT NUMBER 15 OUTBOARD RIB CRACK INDICATION. REMOVED AND REPLACED OUTBOARD ATTACH RIB PER ESO81117.

Part: RIB — CRACKED (NR 5 SLAT) · airframe 58,526 hrs · 24,772 cycles

NUMBER 5 RIGHT SLAT AT NUMBER 15 OUTBOARD RIB CRACKED. REPLACED CRACKED NUMBER 15 RIB AT NUMBER 5 RIGHT SLAT.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 58,526 hrs · 24,772 cycles

SUPPORT CASTING CRACKED BELOW NUMBER 5 SEAT TRACK AT RIGHT STATION 927. REMOVED AND INSTALLED NEW SEAT TRACK SUPPORT PER SRM 51-01.

Part: PAN — CRACKED (BS 1117) · airframe 58,526 hrs · 24,772 cycles

RIGHT UPPER AFT TAB CRACKED ON WINDOW PAN, STATION 1117. REMOVED DAMAGED SECTION AND INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: INTERCOSTAL — CRACKED (NR 5 SLAT TRACK) · airframe 58,526 hrs · 24,772 cycles

INTERCOSTAL ATTACH ANGLE CRACKED BELOW NUMBER 5 SLAT TRACK. REPAIRED PER ENGINEERING AUTHORIZATION MD80-008221 DATED 11/24/09.

Part: PAN — CRACKED (BS 1155) · airframe 58,526 hrs · 24,772 cycles

RIGHT WINDOW PAN IS CRACKED AT THE RIGHT FORWARD LOWER CORNER. REMOVED DAMAGE AND INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 58,526 hrs · 24,772 cycles

AFT CARGO DOOR NR 1 STOP FITTING CRACKED ON AFT SIDE OF DOOR. REMOVED AND REPLACED STOP FITTING PER ESO 80174.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 661,364 hrs

LGA - SEAT EXIT LIGHTS FOR ROW 3 TO ROW 20 INOPERATIVE. REPLACED BATTERY PACK FOR SEAT EXIT LIGHTS FOR ROW 3 TO 20.

Part: RELAY — INOPERATIVE (WARNING SYSTEM) · airframe 56,194 hrs · 23,733 cycles

DFW - CAPTAIN ADVISED DISPATCH THAT AT 500FT AGL THE LANDING GEAR WAS IN QUESTION. FLIGHT ABORTED APPROACH. THE CREW DECLARED AN EMERGENCY DID FLY BY OF THE TOWER AND WAS ADVISED THAT THE GEAR LOOKED OK. FLIGHT LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED R2-1 RELAY FOR GROUND POSITION WARNING SYSTEM. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 56,332 hrs

LGA - EMERGENCY EXIT SIGN LIGHT AT AFT CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY EXIT SIGN LIGHT AT AFT CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: ACCUMULATOR — LEAKING (THRUST REVERSER)

DFW INFLIGHT - DURING CLIMB CREW COULD SMELL ODOR IN COCKPIT. FLIGHT ATTENDANT REPORTED SMELL AND SMOKE IN CABIN. TURNED PACKS TO COLD AND RETURNED TO DFW AND LANDED WITHOUT INCIDENT. SMOKE CLEARED PRIOR TO LANDING. FOUND LEFT THRUST REVERSER ACCUMULATOR LEAKING. REPLACED LEFT THRUST REVERSER ACCUMULATOR. PERFORMED BURN OUT OF HIGH PRESSURE PNEUMATIC DUCTING. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LINE — LEAKING (APU)

TPA - INFLIGHT AFTER TAKEOFF SMOKE APPEARED IN COCKPIT AND CABIN. RETURNED TO TPA AND LANDED WITHOUT INCIDENT. FOUND OIL LINE LEAKING FROM APU. REPAIRED LINE AND REPLACED BOTH PACKS SOCKS. ACCOMPLISHED PACK BURN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: ACTUATOR — INOPERATIVE (MLG)

JFK - FLIGHT DIVERTED TO JFK DUE TO THREE RED GEAR WARNING LIGHTS WHEN LANDING GEAR WAS LOWERED. AIRCRAFT LANDED WITHOUT INCIDENT. FOUND LANDING GEAR HANDLE MECHANICALLY BINDING. FREED UP SLIDING ACTION OF HANDLE AND THREE RED LIGHTS EXTINGUISHED. AIRCRAFT FERRIED GEAR DOWN TO LGA FOR FOLLOW UP. REPLACED ROLLER ACTUATOR FOR 5189 SWITCH AT LANDING GEAR HANDLE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DFW - OVERHEAD EMERGENCY LIGHTS AT ROWS 23 THROUGH 26 INOPERATIVE. REPLACED BATTERY PACK FOR OVERHEAD EMERGENCY LIGHTS AT ROWS 23 THROUGH 26. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY — INOPERATIVE (CABIN)

DURING OVERNIGHT MAINTENANCE, FIRST CLASS OVERHEAD EMERGENCY EXIT LIGHTS INOPERATIVE. RESEATED EMERGENCY EXIT LIGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BEAM — CORRODED (CARGO DOOR)

TUL - FOUND CORROSION ON AFT CARGO DOOR BEAM STATION 1155-1212. REMOVED AND REPLACED AFT CARGO DOOR BEAM FROM STATION 1117 TO 1250 PER AARD 53-10-00-3. (M)

Part: FRAME — CRACKED (FUSELAGE)

TUL - FOUND CANT FRAME AT STATION 1485 HAS CRACKS UNDER AFT STAIR ACTUATOR CASTING ATTACH POINT. CUT OFF DAMAGED SECTION OF FRAME AND INSTALLED DOUBLER REPAIR PER AARD 53-10-00-33 (CANT FRAME REPAIR). (M)

Part: SUPPORT — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON F/B SUPPORT STATION 1212 L29R-L30. INSTALLED NEW FLOOR SUPPORT AT STATION 1212 L29R TO L30 SRM 51-01. (M)

Part: FRAME — GOUGED (FUSELAGE)

TUL - FOUND FRAME AT STATION 1401 HAS DEEP GOUGE AT INSTRUMENT AIRLINE ATTACH POINT AT LONGERON 21 RT. INSTALLED REPAIR DOUBLER AT STATION 1401 PER SRM 53-03 PAGE 5. (M)

Part: FRAME — CRACKED (FUSELAGE)

TUL - FOUND FRAME 1416 CRACKED FROM UNDER FILLER BLOCKS LONGERON 2R AND LONGERON 2L. REMOVED AND REPLACED CRACKED ANGLE FRAME 1416 L5L TO L5R. (M)

Part: SHEAR TIE — CRACKED (FUSELAGE)

TUL - FUOND TWO SHEAR TIES CRACKED ON AFT SIDE OF FRAME 1433 JUST INBOARD OF STRINGER 3R AND STRINGER 3L. REMOVED AND REPLACED WITH NEW SHEAR TIE PER SRM 53-01. (M)

Part: WEB — DAMAGED (FUSELAGE)

TUL - FOUND HOLE IN CUSP UNDER NR 6 SEAT TRACK. CUT OUT AND INSTALLED DOUBLER .025 7075 T6 PER AARD 53-00-00-02. (M)

Part: STIFFENER — CRACKED (FUSELAGE)

TUL - FOUND THE VERTICAL STIFFENER ON THE FORWARD SIDE OF AFT PRESS BULKHEAD ABOVE VAULT DOOR IS CRACKED. REMOVED CRACKED STIFFENER AND INSTALLED NEW STIFFENER PER SRM 51-01-00. (M)

Part: RIB — TORN (HORIZONTAL STAB)

TUL - FOUND OUTBOARD LEADING EDGE RIB TORN AT AFT UPPER CORNER ON LEFT HORIZONTAL STABILIZER. INSTALLED NEW LEADING EDGE RIB ON LEFT HORIZONTAL STABILIZER OUTBOARD END PER SRM 55-01. (M)

Part: SHEAR TIE — CRACKED (FUSELAGE)

TUL - FUOND FRAME 1429 SHEAR TIE CRACKED LEFT AFT SIDE JUST OUTBOARD OF TAIL TIE FITTING. INSTALLED NEW SHEAR TIE PER SRM 53-01. (M)

Part: FRAME — CRACKED (FUSELAGE)

TUL - FOUND FRAME 1429 SHEAR TIE CRACKED 2 PLACES RIGHT AFT SIDE LONGERON 2 RT. INSTALLED NEW SHEAR TIE SRM 51-01. (M)

Part: SKIN — DAMAGED (FUSELAGE)

TUL - FOUND CREASE IN FUSE SKIN STATION 278 AT LONGERON 26 LT. CUT OUT DAMAGED AREA AND INSTALLED DOUBLER PER SRM 53-04 FIG 12B SHEETS 7-22 AND 35. (M)

Part: FLOORBEAM — DAMAGED (FUSELAGE)

TUL - FOUND FLOORBEAM LOWER FLANGE AT 389 RBL 15 DAMAGED FROM CARGO DOOR. CUT OUT DAMAGE AND INSTALLED L-ANGLE DOUBLER PER AARD 53-20-00-21. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON LEFT CUSP AT STATION 1155. CUT OUT CORROSION AND INSTALLED DOUBLER PER SRM 53-01 PAGE 18. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL - FOUND CORROSION SEAT TRACK NR 1 FS 1208-1209. CUT OUT DAMAGED AREA AND INSTALLED PLUG PER AARD-53-70-00-10. (M)

Part: CONNECTOR — DISCONNECTED (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 7D INOPERATIVE. RE-CONNECTED EMERGENCY EXIT LIGHT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — DISCONNECTED (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 7D INOPERATIVE. RE-CONNECTED EMERGENCY EXIT LIGHT CONNECTOR AT SEAT 7D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (TAIL)

DFW - DURING OVERNIGHT MAINTENANCE, TAIL COMPARTMENT EMERGENCY ESCAPE LIGHT INOPERATIVE. REPAIRED OPEN CONTACT ON LIGHT ASSEMBLY. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: ENGINE — DEFECTIVE (NR 1)

SJC - FLT 0740 - ON TAKEOFF SJC/DFW, BOTH LEFT AND RIGHT AIR CONDITIONING SUPPLY HIGH TEMPERATURE LIGHTS ILLUMINATED. HIGH PRESSURE BLEED AIR SUPPLY WAS SHUT OFF AND LIGHTS EXTINGUISHED. STRONG FUEL ODOR DETECTED IN CABIN. AIRCRAFT RETURNED TO SJC AND LANDED WITHOUT INCIDENT. REPLACED NR 1 ENGINE. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: WEB — CORRODED (BS 598-712)

TUL - FOUND CUSP SECTION FROM RT STATION 598 TO STATION 712 RT, REQUIRES REPLACEMENT DUE TO SEVERAL AREAS OF CORROSION THAT WENT BEYOND LIMITS. REPLACED CUSP SECTION FROM STATION 598 TO STATION 712 PER AARD 53-20-00-16. (M)

Part: TRACK — CORRODED (BS 1212-1322)

TUL - FOUND CORROSION IN RT TIE DOWN TRACK AT FASTENERS THAT ATTACH TRACK TO FRAMES. REPLACED TIE DOWN TRACK. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT CHECK, DISCOVERED FIRST CLASS EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED LIGHT STRIP AT FIRST CLASS EMERGENCY EXIT. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: CONNECTOR — MISINSTALLED (CABIN)

SFO - DURING OVERNIGHT MAINTENANCE, FOUND THE EMERGENCY EXIT FLOOR PATH LIGHTS AT SEAT 22F, LOWER, AND AFT SERVICE DOOR INOPERATIVE. REVERSED POLARITY ON CONNECTOR AT ROW 21. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)