N7525A

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,160 hrs · 33,171 cycles

CRACK IN SKIN AT STATION 1437 BELOW LONGERON 3 RIGHT. STOP DRILLED CRACK AND INSTALLED DOUBLER PER AARD 53-30-00-02.

Part: BATTERY — NOT SEATED (CABIN) · airframe 60,808 hrs · 31,302 cycles

INTERIOR EMERGENCY LIGHTS IN MID AND CENTER CABIN NOT WORKING. RESEATED EMERGENCY LIGHT BATTERIES IN MID AND AFT CABIN. OPS CHECK NORMAL.

Part: CYLINDER — INOPERATIVE (LT MLG) · airframe 56,957 hrs · 29,159 cycles

STL - LEFT MAIN LANDING GEAR WOULD NOT RETRACT ON TAKEOFF. EMERGENCY DECLARED, RETURNED STL WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT MAIN GEAR RETRACT SUPPORT FITTING AND LEFT MAIN GEAR RETRACT CYLINDER AND CYLINDER LINKAGES. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: DRAIN PAN — CRACKED (GALLEY) · corrosion level 2 · airframe 56,525 hrs · 28,915 cycles

GALLEY 1 DRAIN PAN FOUND CRACKED. SUPPORT DOUBLER FOUND CORRODED OUT OF LIMITS. REMOVED CORROSION AND INSTALLED DOUBLER PER AARD 53-20-00-16 AND REPLACED G1 GALLEY DRAIN PAN PER SRM 51-30.

Part: ATTACH ANGLE — BROKEN · airframe 56,525 hrs · 28,915 cycles

LEFT ANTI FLOAT GEAR TAB CONTROL ROD FAIRING UPPER ATTACH ANGLE BROKEN. INSTALLED DOUBLER PER ENGINEERING AUTHORIZATION MD80-55-007984.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 56,525 hrs · 28,915 cycles

CRACK IN CUSP MEMBRANE AT STATION 1176 LEFT AND SIDE. INSTALLED NEW CUSP SHEET AT LEFT STATION 1174 TO 1250 PER AARD 53-20-00-16.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 56,525 hrs · 28,915 cycles

INTERCOSTAL CRACKED BETWEEN FLOORBEAMS AT STATION 1289 TO1309. INSTALLED NEW INTERCOSTAL PER SRM 53-01.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 56,525 hrs · 28,915 cycles

FLOORBOARD SUPPORT CRACKED AT STATION 180 LEFT BUTTLINE 15 TO LEFT BUTTLINE 35. INSTALLED NEW SUPPORT PER SRM 51-30-01.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 56,525 hrs · 28,915 cycles

STATION 1380 FRAME SHEAR-TIE CRACKED BETWEEN LONGERON 13 RT AND LONGERON 14 RT. INSTALLED SHEAR-TIE DOUBLER PER ENGINEERING AUTHORIZATION MD80-53-007956.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 56,525 hrs · 28,915 cycles

CENTER ANGLE ABOVE VAULT DOOR IS CRACKED AT UPPER FASTENER. COMPLETED STIFFENER INSTALLATION PER SRM CH 51-01-00.

Part: CUSP WEB — DAMAGED (FUSELAGE) · airframe 56,525 hrs · 28,915 cycles

DAMAGE TO LEFT CUSP AT STATION 1250 TO 1309. INSTALLED NEW CUSP PER AARD 53-20-00-16.

Part: PAN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,525 hrs · 28,915 cycles

FORWARD GALLEY FLOOR PAN CORRODED AT STATION 170-200 UNDER PHENOLIC H-CHANNEL AT FORWARD SERVICE DOOR. REMOVED CORROSION AND INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 56,525 hrs · 28,915 cycles

CRACK IN CUSP AT STATION 1189 LEFT SIDE. REMOVED CRACK AND INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 56,525 hrs · 28,915 cycles

FUSELAGE HAS A GOUGE ON LEFT SIDE APPROXIMATELY 8 INCHES FORWARD OF PRODUCTION SPLICE STATION 221 JUST BELOW NUMBER 4 LONGERON. INSTALLED DOUBLER AT STATION 216 TO 226 BETWEEN LONGERON 4 AND 6 LEFT SIDE OF AIRCRAFT PER SRM 53-04-00 FIG 12B.

Part: FITTING — CRACKED (PAX DOOR) · airframe 56,525 hrs · 28,915 cycles

VAULT DOOR HAS A CRACKED ANGLE JUST BELOW THE LOWER LATCH PIN LINK. REMOVED CRACKED FITTING AND INSTALLED NEW PER ESO 80186.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,525 hrs · 28,915 cycles

CORROSION ON UNDERSIDE OF CUSP SHEET OUTBOARD HOLES FORWARD OF STATION 541, LEFT HAND SIDE OF CABIN. INSTALLED DOUBLER AS PER AARD 53-20-00-16.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 56,525 hrs · 28,915 cycles

FLOOR PAN CRACKED IN RADIUS STATION 219 OUTBOARD SIDE OF SEAT TRACK 2. INSTALLED NEW CUSP SHEET LEFT STATION 218 TO 237 AND INSTALLED DOUBLER STATION 223 FOR WIRE BUNDLE ACCESS PER AARD 53-20-00-16.

Part: PAN — CRACKED (ENTRY DOOR) · airframe 56,525 hrs · 28,915 cycles

HANDLE PAN ON FORWARD ENTRY DOOR CRACKED. INSTALLED NEW HANDLE PAN PER ESO 80172.

Part: CUSP WEB — DAMAGED (FUSELAGE) · airframe 56,525 hrs · 28,915 cycles

FOUND AT .375 INCH HOLE IN CUSP AT RIGHT STATION 334. INSTALLED DOUBLER.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 56,525 hrs · 28,915 cycles

VERTICAL STIFFENER CRACKED AT TOP FASTENER HOLE ABOVE VAULT DOOR. REMOVED AND INSTALLED NEW STIFFENER.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,525 hrs · 28,915 cycles

LEFT HAND CUSP HAS CORROSION AT STATION 1250 TO 1309. CUSP SHEET REMOVED AND NEW SHEET INSTALLED.

Part: SKATE ANGLE — CRACKED (FUSELAGE) · airframe 56,525 hrs · 28,915 cycles

FUSELAGE TO VERTICAL STABILIZER LEFT SKATE ANGLE IS CRACKED BETWEEN FASTENER HOLES. INSTALLED DOUBLER.

Part: SLAT — DAMAGED (RT WING) · airframe 56,525 hrs · 28,915 cycles

RIGHT WING NUMBER 2 SLAT RUBSTRIP LOOSE ON DE-ICE TUBE ACCESS. BLENDED SMOOTH WORN AREA, ALODINED AREA AND FILLED AREAS WITH DEVCON F. RE-ATTACHED RUB STRIP PER ESO 80559 DATED 10/28/09.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 56,525 hrs · 28,915 cycles

AFT CARGO DOOR STOP PAD FITTING AT FORWARD END AT NUMBER 1 BEAM CRACKED. REPLACED STOP PAD FITTING PER ESO 80172.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 56,525 hrs · 28,915 cycles

FORWARD CARGO DOOR CRACKED AT STOP PAD FITTING AT AFT NUMBER TWO BEAM. REPLACED STOP PAD FITTING PER SEO 80174.

Part: TAB — CRACKED (WINDOW PAN) · airframe 56,525 hrs · 28,915 cycles

FOUND CRACK AT LEFT UPPER AFT WINDOW PAN TAB AT STATION 1060. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 56,525 hrs · 28,915 cycles

FORWARD CARGO DOOR CRACKED AT STOP PAD FITTING AT AFT NUMBER 5 BEAM. REPLACED STOP PAD FITTING PER ESO 80174.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 56,525 hrs · 28,915 cycles

MID CARGO DOOR LOWER STOP FITTING IS CRACKED. REPLACED WITH NEW STOP FITTING PER ESO 80174.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 56,525 hrs · 28,915 cycles

FORWARD CARGO DOOR STOP PAD FITTING AT AFT NUMBER 4 BEAM CRACKED. REPLACED STOP PAD FITTING PER ESO 80174.

Part: TAB — CRACKED (WINDOW PAN) · airframe 56,525 hrs · 28,915 cycles

FOUND CRACK AT LEFT UPPER AFT WINDOW PAN TAB AT STATION 1041. INSTALLED DOUBLER ANGLE PER AARD 53-10-00-25.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 56,525 hrs · 28,915 cycles

MID CARGO DOOR UPPER STOP FITTING IS CRACKED. REPLACED STOP FITTING PER ESO 80174.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 56,525 hrs · 28,915 cycles

FORWARD CARGO DOOR CRACKED AT STOP PAD FITTING AT AFT NUMBER ONE BEAM. REPLACED STOP PAD FITTING PER ESO 80174.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 56,525 hrs · 28,915 cycles

CRACKED DOOR STOP FITTING AT NUMBER 2 BEAM FORWARD OF CARGO DOOR. INSTALLED NEW FITTING PER ESO 80174.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 56,525 hrs · 28,915 cycles

CRACKED DOOR STOP FITTING NUMBER 3 BEAM FORWARD CARGO DOOR. INSTALLED NEW FITTING PER ESO 80174.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 56,525 hrs · 28,915 cycles

AFT CARGO DOOR STOP PAD CRACKED ON AFT EDGE OF CARGO DOOR. REPLACED DOOR STOP PAD PER ESO 80174.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 56,525 hrs · 28,915 cycles

AFT CARGO DOOR STOP PAD CRACKED ON AFT EDGE OF CARGO DOOR. REPLACED DOOR STOP PAD PER ESO 80174.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 56,352 hrs · 28,823 cycles

PULLEY SUPPORT BRACKET IS CRACKED. REPAIRED PER AARD 53-10-00-15.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 56,033 hrs · 28,653 cycles

AFT EMERGENCY LIGHTS WEAK. INSTALLED SERVICEABLE BATTERY PACK FOR AFT EMERGENCY LIGHTS.

Part: LENS — WRONG PART (EMERGENCY LIGHTS) · airframe 54,984 hrs

LGA - WRONG EMERGENCY LIGHT LENS INSTALLED AT ROW 28 FORWARD. REPLACED LENS AT ROW 28 FORWARD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 54,984 hrs

LGA FIRST CLASS EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR FIRST CLASS EMERGENCY LIGHTS.

Part: PAN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,525 hrs · 28,915 cycles

FLOOR PAN CORRODED STA 207-210 FORWARD OF NUMBER 6 SEAT TRACK. INSTALLED REPAIR PER AARD 53-20-00-16.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 53,791 hrs

LGA - EXTERIOR EMERGENCY LIGHTS AT AFT CARGO COMPARTMENT INOPERATIVE. REPLACED BATTERY PACK FOR EXTERIOR EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONTROLLER — INOPERATIVE (L/E SLAT)

PHX INFLIGHT T1023/05JUN AUS TO SJC. DURING SLAT RETRACTION SLAT DISAGREE LIGHT ILLUMINATED. LANDED PHX WITHOUT INCIDENT. REPLACED PROXIMITY SWITCH CONTROL. SYSTEM GROUND CHECKED NORMAL OPERATION. (A)

Part: FLASHLIGHT — CRACKED (CABIN)

LGA - EMERGENCY FLASHLIGHT AT LEFT EMERGENCY DOOR HAS CRACKED CASE. REPLACED EMERGENCY FLASHLIGHT AT LEFT EMERGENCY DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

SFO RT EMERGENCY LIGHTS ABOVE OVERWING DOOR AT ROW 21D INOPERATIVE. REPLACED BATTERY PACK AND RELAMPED RT EMERGENCY LIGHTS ABOVE OVERWING DOOR AT ROW 21D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS)

DTW - EMERGENCY OVERHEAD LIGHTS IN TWO AREAS OF CABIN INOPERATIVE. REPLACED CHARGER ASSEMBLIES FOR EMERGENCY OVERHEAD IGHTS IN TWO AREAS OF CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DFW - CEILING EMERGENCY LIGHTS AT ROW 14D INOPERATIVE. REPLACED BATTERY PACK AND CHARGER ASSEMBLY FOR CEILING EMERGENCY LIGHTS AT ROW 14D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: MODULE — INOPERATIVE (EMERGENCY LIGHT)

ATL - FORWARD SECTION EMERGENCY PATH LIGHTING WILL NOT TEST. REPLACED BATTERY AND MODULE FOR FORWARD SECTION EMERGENCY PATH LIGHTING. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: WIRE — BROKEN (EMERGENCY LIGHT)

DTW - LOWER EMERGENCY EXIT LIGHT MARKER BETWEEN FIRST CLASS GALLEY AND FIRST CLASS SEATS INOPERATIVE. FOUND BROKEN WIRE IN FLOOR NEAR LIGHT. SPLICED NEW WIRE FOR LOWER EMERGENCY EXIT LIGHT MARKER BETWEEN FIRST CLASS GALLEY AND FIRST CLASS SEATS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT)

DURING OVERNIGHT MAINTENANCE, CEILING EMERGENCY EXIT LIGHT AT ROWS 18-26 INOPERATIVE. SECURED EMERGENCY EXIT LIGHT BATTEYR FOR ROW 18-26. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON SUB FLOOR STATION 188 TO STATION 200 AT THE FORWARD SERVICE DOOR. CUT OUT DAMAGED AREA AND INSTALLED REPAIR PER SRM 53-01-00 FIG 4 SHT 3. (M)

Part: SKIN — CRACKED (FUSELAGE)

TUL - FOUND THREE CRACKS EXTENDING FROM TWO RIVET HOLES STATION 1380 10 INCHES ABOVE RIGHT ENGINE PYLON. REPAIRED CRACKS BY INSTALLING DOUBLER IAW SRM 53-04 FIG 18. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

TUL - FOUND FORWARD SIDE OF FLOORBEAM WEB CORRODED STATION 200 RIGHT SIDE AT BELTFRAME ATTACH. CUT OUT CORRODED SECTION AND INSTALLED DOUBLER PER SRM 51-70-4 PAGE 5 FIG 2. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND RIGHT CUSP CORRODED STATION 636-655. INSTALLED DOUBLER AT STATION 636-655 AS PER SRM 51-01. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL - FOUND NR 1 SEAT TRACK CORRODED STATION 1281, 1218, 1176, 1188. REPLACED NR 1 SEAT TRACK BETWEEN STATION 1174 AND 1307 PER SRM 53-05. (M)

Part: PAN — CRACKED (FUSELAGE)

TUL - FOUND WINDOW RING PAN CRACK AT UPPER RIGHT CORNER AT STATION 947 LEFT. INSTALLED DOUBLER AT STATION 947 UPPER RIGHT CORNER LEFT SIDE PER AARD 53-10-00-25. (M)

Part: THRESHOLD — CORRODED (FUSELAGE)

TUL - FOUND AFT CARGO DOOR OPENING LOWER THRESHOLD IS CORRODED STATION 1155 TO 1211. REPAIRED PER AARD 53-10-00-16, AARD 53-10-00-3. (M)

Part: WEB — CRACKED (FUSELAGE)

TUL - FOUND RIGHT CUSP CRACKED AT LIGHTNING HOLE STATION 780. REMOVED CRACK AND INSTALLED DOUBLER PER SRM 53-01 PAGE 18. (M)

Part: WINDOW — CRACKED (CABIN)

BNA - FLT 1379 - EN ROUTE PIT-DFW, AIR INTERRUPTED TO BNA DUE TO CRACKED WINDOW AT 14A. LANDED BNA WITHOUT INCIDENT. REPLACED CRACKED WINDOW AT 14A. PRESSURIZATION AND LEAK CHECK OK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: DETECTOR — FAILED (NR 2 ENGINE)

DFW - FLT T1056 - DURING CRUISE, NR 2 ENGINE FIRE WARNING LIGHT ILLUMINATED. CREW ACCOMPLISHED THE FIRE DETECTOR LOOP LIGHT WITHOUT FIRE WARNING CHECK LIST. SECURED NR 2 ENGINE AND DISCHARGED FIRE BOTTLE. ENGINE SHUTDOWN WAS NORMAL, AND FIRE WARNING LIGHT EXTINGUISHED AFTER 2 MINUTES. AIRCRAFT LANDED DFW WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND NR 2 ENGINE A/B FIRE LOOP WOULD NOT TEST. REPLACED NR 2 A/B FIRE LOOP, FIRE BOTTLE EXTINGUISHER, AND ENGINE OIL FILTERS. RAN NR 2 ENGINE AT POWER WITH NO LEAKS. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)