N7526A

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,013 hrs · 33,699 cycles

1474 CANT FRAME CRACKED AFT OF LONGERON 18 LEFT. INSTALLED DOUBLER PER AARD 53-10-00-15.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 65,013 hrs · 33,699 cycles

SHEAR TIE CRACKED AFT SIDE OF STATION 1451 AFT OF LONGERON 2 RIGHT. INSTALLED REPLACEMENT SHEAR TIE PER AARD 51-00-05-1.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 61,241 hrs · 31,520 cycles

SHEAR TIE CRACKED AFT SIDE OF 1451 FRAME AFT OF LONGERON 2 RIGHT. REPLACED SHEAR TIE PER SRM 51-10-00-5.

Part: COUPLING — LEAKING (AC BAY) · airframe 60,333 hrs · 31,025 cycles

DFW - CREW REPORTED ON CLIMBOUT TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED. QRH PROCEDURE ACCOMPLISHED AND LIGHT WENT OUT. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND DUCT COUPLINGS LEAKING BETWEEN FLOW CONTROL VALVE AND PRIMARY HEAT EXCHANGER ON BOTH PACKS. REPLACED SEALS IN BOTH COUPLINGS. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: SHIM — CRACKED (ACM) · airframe 60,117 hrs · 30,920 cycles

DFW - CREW REPORTED TAIL COMPARTMENT TEMP HIGH LIGHT ILLUMINATED DURING CLIMBOUT. FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT SIDE AIR CYCLE MACHINE SHIM THAT WAS CRACKED. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: STRUT — FLAT (NLG) · airframe 58,784 hrs · 30,171 cycles

DFW - CAPTAIN RECEIVED UNSAFE NOSE GEAR INDICATION AND NOSE LANDING GEAR WOULD NOT RETRACT. FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. THE NOSE GEAR WAS FLAT ON ARRIVAL. AIRCRAFT REMOVED FROM SERVICE. REPACKED NOSE STRUT ASSEMBLY. LEAK CHECK AND GEAR SWING CHECK OK. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: SPLICE PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,214 hrs · 29,295 cycles

AFT- CORROSION ON LEFT TIE-DOWN TRACK SLICE PLATES STATION 1220. (MKD) INSTALLED NEW SPLICE PARTS PER SRM 51-30-05.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 57,214 hrs · 29,295 cycles

AFT CARGO BEAM AREA STATION 1165 TO 1200 SKIN UNDER BEAM HAS TOOLING MARKS FROM CLEAN-UP OF BEAM HORIZONTAL FLANGE. REMOVED DAMAGE AND INSTALLED DOUBLER REPAIR PER SRM 53-04 FIGURE 38 (SHEET 21) AND EA MD80-53-009976.

Part: BEAM — CORRODED (FUSELAGE) · airframe 57,214 hrs · 29,295 cycles

CORROSION ON LOWER DOOR BEAM AT AFT CARGO DOOR OPENING. REMOVED CORROSION AND INSTALLED DOUBLER REPAIR PER AARD 53-10-00-3.

Part: MEMBRANE — PUNCTURED (FUSELAGE) · airframe 57,214 hrs · 29,295 cycles

PUNCTURE IN MEMBRANE AT STATION 176 APPROXMATELY 20 INCHES INBOARD OF FOWARD ENTRY DOOR. REPAIR DOUBLER INSTALLED PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 57,214 hrs · 29,295 cycles

RIGHTHAND CUSP CORRODED AT STATION 656. REMOVED CORROSION AND INSTALLED DOUBLER REPAIR PER AARD 53-20-00-16.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 57,214 hrs · 29,295 cycles

INTERCOSTAL AT STATION 176 JUST INBOARD OF FORWARD ENTRY DOOR UNDER MEMBRANE IS CRACKED. NEW INTERCOSTAL INSTALLED PER SRM 51-30-05.

Part: SKIN — DENTED (FUSELAGE) · airframe 57,214 hrs · 29,295 cycles

FUSELAGE SKIN DENT AT STATION 1305 BELOW LONGERON 18 RIGHT. INSTALLED INTERNAL DOUBLER PER SRM 53-04-00. INSTALLED SCUFF PLATE PER AARD 53-30-00-8.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 57,214 hrs · 29,295 cycles

SEAT TRACK 6 CORROSION BLEND BEYOND LIMITS STATION 563. REMOVED DAMAGE INSTALLED SEAT TRACK PLUG REPAIR PER AARD 53-20-00-10.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 57,214 hrs · 29,295 cycles

LONGERON 29 LEFT END CAP IS CRACKED AT STATION 1338. INSTALLED NEW END CAP PER SRM 51-30-05.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 57,214 hrs · 29,295 cycles

STATION 927 BELOW SEAT TRACK NUMBER 3 VERTICAL SUPPORT CRACKED AT BOTTOM AFT FASTENER. NEW BRACKET INSTALLED PER SRM 51-30-05 AND 51-30-01.

Part: MOUNT — DAMAGED (GALLEY) · airframe 57,214 hrs · 29,295 cycles

CABIN GALLEY TIEDOWN CORRODED STATION 210 RIGHT BUTTLINE 11. REPLACED GALLEY MOUNT STATION 210 RIGHT BUTTLINE 11 PER SRM 51-10.

Part: FLOOR SUPPORT — DAMAGED (FUSELAGE) · airframe 57,214 hrs · 29,295 cycles

CABIN FLOORBOARD SUPPORT CORRODED STATION 201 RIGHT BUTTLINE 50 TO 56. REPLACED FLOORBOARD SUPPORT AT STATION 201 RIGHT BUTTLINE 50 TO 56 PER SRM 51-01.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,214 hrs · 29,295 cycles

LEFT HAND CUSP STATION 1174 CORROSION BEYOND LIMITS. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: DOUBLER — DAMAGED (FUSELAGE) · airframe 57,214 hrs · 29,295 cycles

TEMPORARY REPAIR DOUBLER ON FUSELAGE SKIN AT STATION 237 LEFT SIDE APPROXIMATELY 4 INCHES BY 5 INCHES BELOW LONGERON 17 LEFT. INSTALLED DOUBLER AND STRAP PER SRM 53-04 FIGURE 12B.

Part: TAB — CRACKED (FUSELAGE) · airframe 57,214 hrs · 29,295 cycles

PASSENGER DOOR L15L HAS CRACKED TAB AT STATION 208. INSTALLED DOUBLER AND SHIM PER AARD 53-10-00-11.

Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 57,214 hrs · 29,295 cycles

VERTICAL SUPPORT CRACKED. INSTALLED NEW SUPPORT BELOW NUMBER 3 SEAT TRACK PER SRM 51-30-05.

Part: MEMBRANE — PUNCTURED (FUSELAGE) · airframe 57,214 hrs · 29,295 cycles

SUBFLOOR PUNCTURED AT STATION 163 LEFT BUTTLINE 3. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,214 hrs · 29,295 cycles

CORROSION BLEND OUT BEYOND LIMITS ON SEAT TRACK 6 STATIONS 216 TO 218. INSTALLED PLUG PER SRM 53-05-00 AND AARD 53-20-00-10.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,214 hrs · 29,295 cycles

CORROSION BEYOND LIMITS ON NUMBER 1 SEAT TRACK STATION 1210. CUT OUT CORRODED AREA AND INSTALLED SEAT TRACK PLUG PER SRM 53-05-00.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 57,214 hrs · 29,295 cycles

CORROSION OUT OF LIMITS SEAT TRACK NUMBER 3 AT STATIONS 541 TO 547. REMOVED CORROSION AND INSTALLED SEAT TRACK REPAIR PLUG PER AARD 53-20-0-10.

Part: TAB — DAMAGED (ELEVATOR) · airframe 57,214 hrs · 29,295 cycles

LEFT ELEVATOR CONTROL TAB HAS STATIC DISCHARGE BURN ON TRAILING EDGE. HOT BONDED METAL DOUBLER TO BURN AREA PER SRM 51-70-02.

Part: PAN — CRACKED (WINDOW) · airframe 57,214 hrs · 29,295 cycles

RIGHT WINDOW PAN CRACKED AT LOWER FORWARD FASTENER AT STATION 1041 ABOVE STRINGER 15 RIGHT. REPAIRED PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 57,214 hrs · 29,295 cycles

WINDOW RING PAN CRACKED AT LOWER FORWARD FASTENER AT STATION 1155 ABOVE LONGERON 15 RIGHT. CUT OUT DAMAGE AND INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: FITTING — CRACKED (CARGO DOOR) · airframe 57,214 hrs · 29,295 cycles

LOWER AFT T-CLIP IS CRACKED. REMOVED AND REPLACED LOWER AFT T-CLIP ON FORWARD CARGO DOOR PER ESO 80174.

Part: RIB — CRACKED (LE SLAT) · airframe 57,214 hrs · 29,295 cycles

NUMBER 15 WING LEADING EDGE SLAT RIB IS CRACKED. REMOVED 2ND FROM OUTBOARD ATTACH FITTING (NUMBER 15). LOCATED, DRILLED, AND INSTALLED NEW ATTACH FITTING PER ESO 80117.

Part: PAN — CRACKED (WINDOW) · airframe 57,214 hrs · 29,295 cycles

CRACK AT LEFT WINDOW PAN UPPER FORWARD TANG STATION 946 AFT SIDE. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 57,214 hrs · 29,295 cycles

CRACK IN LEFT WINDOW PAN UPPER FORWARD TANG STATION 788 AFT SIDE. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: FITTING — WORN (LE SLAT) · airframe 57,214 hrs · 29,295 cycles

RIGHT WING SLAT NUMBER 4 KNUCKLE FITTING WORN AT OUTBOARD END. REMOVED WORN ATTACH FITTING. LOCATED, DRILLED, AND INSTALLED NEW ATTACH FITTING PER ESO 80117.

Part: PAN — CRACKED (WINDOW) · airframe 57,214 hrs · 29,295 cycles

CRACK AT LEFT WINDOW UPPER FORWARD TANG STATION 845 AFT SIDE. INSTALLED DOUBLER AARD 53-10-00-25.

Part: RIB — CRACKED (LE SLAT) · airframe 57,214 hrs · 29,295 cycles

NUMBER 14 WING LEADING EDGE SLAT RIB IS CRACKED. REMOVED 2ND FROM OUTBOARD ATTACH FITTING (NUMBER 14). LOCATED, DRILLED, AND INSTALLED NEW ATTACH FITTING PER ESO 80117.

Part: PAN — CRACKED (WINDOW) · airframe 57,214 hrs · 29,295 cycles

WINDOW RING PAN CRACKED AT TOP AFT FASTENER AT STATION 1193 BELOW LONGERON 11 RIGHT. CUT OUT DAMAGE AND INSTALLED REPAIR DOUBLER PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 57,214 hrs · 29,295 cycles

CRACK AT RIGHT WINDOW PAN UPPER FORWARD CORNER AFT OF STATION 807. CUT OUT CRACK AND INSTALLED NEW REPAIR ANGLE PER AARD 53-10-00-25 AT STATION 807 WINDOW PAN UPPER FORWARD CORNER.

Part: PAN — CRACKED (WINDOW) · airframe 57,214 hrs · 29,295 cycles

LEFT WINDOW RING PAN LOWER FORWARD CLIP CRACKED AT STATION 1022. REPAIRED PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 57,214 hrs · 29,295 cycles

CRACK AT LEFT WINDOW PAN UPPER AFT TANG STATION 1022 FORWARD SIDE. TRIMMED OUT CRACK AND INSTALLED REPAIR ANGLE PER AARD 53-10-00-25.

Part: FITTING — CRACKED (WINDOW PAN) · airframe 57,214 hrs · 29,295 cycles

CRACK AT LEFT WINDOW PAN LOWER FORWARD CLIP STATION 1022 AFT SIDE. TRIMMED OUT CRACK AND INSTALLED REPAIR ANGLE PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 57,214 hrs · 29,295 cycles

RIGHT WINDOW RING PAN CRACKED AT STATION 1059 BELOW STRINGER 11 RIGHT. REPAIRED PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 57,214 hrs · 29,295 cycles

LEFT WINDOW PAN UPPER AFT CLIP CRACKED AT STATION 1022. REPAIRED PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 57,214 hrs · 29,295 cycles

RIGHT WINDOW RING PAN CRACKED AT STATION 1061 ABOVE STRINGER 15 RIGHT. REPAIRED PER AARD 53-10-00-25.

Part: CONTACT — DIRTY (BATTERY PACK) · airframe 56,034 hrs · 28,675 cycles

EMERGENCY LIGHT BATTERY PACK B5-28 INOPERATIVE. CLEANED BATTERY PACK CONTACTS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — DAMAGED (CABIN) · airframe 56,034 hrs · 28,675 cycles

EMERGENCY LIGHT AT SEAT 13D DAMAGED. SHROUD AND LENS BROKEN OFF. REPLACED SHROUD AND LENS AT SEAT 13D.

Part: CONNECTOR — LOOSE (CABIN) · airframe 56,034 hrs · 28,675 cycles

EMERGENCY LIGHT AT SEAT 25D INOPERATIVE. SECURED WIRE HARNESS OUTBOARD CONNECTOR AT SEAT 25D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: PLACARD — DAMAGED (ZONE 200) · airframe 55,873 hrs · 28,580 cycles

RIGHT FORWARD OVERWING EMERGENCY EXIT DECALS UNREADABLE. REPLACED FORWARD OVERWING EMERGENCY DOOR DECAL.

Part: PLACARD — DAMAGED (CABIN) · airframe 55,873 hrs · 28,580 cycles

LEFT FORWARD OVERWING EMERGENCY EXIT DECALS UNREADABLE. REPLACED LEFT OVERWING EXIT PLACARD.

Part: PLACARD — DAMAGED (ZONE 200) · airframe 55,873 hrs · 28,580 cycles

UPPER DECAL ON RIGHT FORWARD OVERWING EXIT UNREADABLE. REPLACED UPPER DECAL RIGHT FORWARD OVERWING EXIT.

Part: PLACARD — DAMAGED (CABIN) · airframe 55,873 hrs · 28,580 cycles

LEFT FORWARD OVERWING EMERGENCY EXIT DECALS UNREADABLE. REPLACED LEFT OVERWING EXIT PLACARD.

Part: PLACARD — DAMAGED (ZONE 200) · airframe 55,873 hrs · 28,580 cycles

RIGHT AFT EXTERIOR OVERWING EMERGENCY EXIT DECALS UNREADABLE. REPLACED AFT EXTERIOR OVERWING EMERGENCY DOOR DECAL.

Part: PLACARD — DAMAGED (OVERWING EXIT) · airframe 55,873 hrs · 28,580 cycles

UPPER DECAL ON RIGHT AFT OVERWING EXIT UNREADABLE. REPLACED UPPER DECAL RIGHT AFT OVERWING EXIT.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 55,589 hrs · 28,413 cycles

CEILING EGRESS LIGHTS ROW 7-16 INOPERATIVE. REPLACED BATTERY PACK FOR CEILING EGRESS LIGHTS FROM ROWS 7-16. OPS CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 55,589 hrs · 28,413 cycles

CEILING EGRESS LIGHTS INOPERATIVE ON ROW 7-14. REPLACED BATTERY PACK FOR CEILING EGRESS LIGHTS FROM ROWS 7-14. OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (AC BAY) · airframe 54,417 hrs

LGA AFT CATWALK EMERGENCY LIGHT ABOVE TAILCONE SLIDE INOPERATIVE. REPLACED LAMP AT AFT CATWALK EMERGENCY LIGHT ABOVE TAILCONE SLIDE.

Part: CONTROL BOX — FAULTED (ANTI SKID SYSTEM) · airframe 53,719 hrs

DFW INFLIGHT - CREW REPORTED ATT FOUR ANTISKID WARNING LIGHTS ILLUMINATED WHEN GEAR LOWERED. LANDED DFW WITHOUT INCIDENT. REPLACED ANTI SKID CONTROL BOX. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,254 hrs · 27,154 cycles

SMALL CRACK ON CANT FRAME 1510. REPAIR ACCOMPLISHED WITH A 3 INCH BY 9 INCH DOUBLER IAW ESO 80559 DATED 10/6/08.

Part: SCREW — BROKEN (GIRT BAR)

LT NR (1) SLIDE GIRT BAR FWD RETAINER CLIP BROKEN. REPLACED ATTACH SCREW IN FWD SLIDE GIRT BAR SUPPORT BRACKET. SYSTEM GROUND CHECKED NORMAL OPERATION. (K)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 51,868 hrs

LGA - EMERGENCY LIGHTS AT OVERHEAD AFT GALLEY INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT OVERHEAD AFT GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 51,868 hrs

LGA - EMERGENCY LIGHT AT FORWARD ENTRY INOPERATIVE. REPLACED LAMPS FOR EMERGENCY LIGHTS AT FORWARD ENTRY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 51,868 hrs

LGA - EMERGENCY LIGHT AT OVERHEAD AFT GALLEY INOPERATIVE. REPLACED BATTERY PACK B5107 FOR EMERGENCY LIGHT AT OVERHEAD AFT GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY — LOOSE (EMERGENCY LIGHTS) · airframe 51,265 hrs

LGA - EMERGENCY LIGHTS AT OVERHEAD FIRST CLASS CABIN INOPERATIVE. SECURED BATTERIES FOR EMERGENCY LIGHTS AT OVERHEAD FIRST CLASS CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY — DISCHARGED (CABIN)

DEN - EMERGENCY LIGHT AT ROW 4 TO ROW 7 CEILING INOPERATIVE. REPLACED BATTERY AT OVERHEAD BIN ROW 6EF FOR ROWS 4 THROUGH 7 CEILING EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

SAN CEILING EMERGENCY LIGHTS AT ROWS 4 AND 7 INOPERATIVE. REPLACED BATTERY PACKS FOR CEILING EMERGENCY LIGHTS AT ROWS 4 AND 7. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: PBE — INOPERATIVE (CABIN)

RDU - DURING OVERNIGHT MAINTENANCE, FOUND FLIGHT ATTENDANT PROTECTIVE BREATHING EQUIPMENT INOPERATIVE. REPLACED PROTECTIVE BREATHING EQUIPMENT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT)

ORD - EMERGENCY EXIT LIGHT AT FORWARD ENTRY, FORWARD GALLEY, AND OVER LEFT SEATS 26-29 DIM. CLEANED EMERGENCY EXIT LIGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — LOOSE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY CEILING EXIT LIGHTS AT ROW 27-31 INOPERATIVE. RESEATED EMERGENCY EXIT LIGHT BATTERY CONNECTION. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND CUSP LINE WEB CORRODED 20 INCHES INBOARD OF SERVICE DOOR JAMB AT STATION 200 AND FORWARD ALONG JAMB TO STATION 180. INSTALLED NEW SECTION OF CUSP BETWEEN STATION 160 TO STATION 200 PE SRM 53-15. (M)

Part: DOOR FRAME — DENTED (FUSELAGE)

TUL - FOUND DENT AT FORWARD UPPER SIDE OF MID CARGO DOOR FRAME. PERFORMED REPAIR PER ESO 80559 2/21/02. (M)

Part: FRAME — WORN (FUSELAGE)

TUL - FOUND STATION 1401 TWO HAVE WEAR MARKS ON TOP OF BELL FRAME. INSTALLED DOUBLER PER AARD 53-10-00-14. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND CUSP LINE WEB CORRODED UNDER AND OUTBOARD OF NR 5 SEAT TRACK. INSTALLED NEW SECTION OF CUSP UNDER SEAT TRACK NR 5 FROM STATION 200 TO 218 PER SRM 53-05. (M)

Part: SKIN — DAMAGED (FUSELAGE)

TUL - FOUND DAMAGE TO OUTER SKIN AT HOLD OPEN HOOK. INSTALLED DOUBLER TO DAMAGED AREA PER SRM 52-05-00. (M)

Part: FRAME — WORN (FUSELAGE)

STA 1418 WEAR MARK FROM STANDOFF CLAMP RIGHT LOWER SIDE ON TOP OF BELL FRAME. INSTALLED DOUBLER IAW AARD.

Part: SKIN — CANNING (PAX DOOR)

TUL - FOUND OUTER SKIN OIL CANNING AT BOTTOM OF DOOR. CUT OUT DAMAGED AREA AND INSTALLED DOUBLER PER ESO 80172. (M)

Part: SKIN — DENTED (AIRSTAIR)

TUL - FOUND LARGE DENT IN LOWER RT AFT SIDE OF AFT AIRSTAIR SKIN. INSTALLED DOUBLER PER SRM 52-01 FIG 2 SHEET 3. (M)

Part: SKIN — DAMAGED (FUSLEAGE)

TUL - FOUND APPROX STATION 47 ABOVE FORWARD NLG DOOR LEFT SIDE FUSELAGE SKIN IS CREASED JUST FORWARD OF FRAME. INSTALLED DOUBLER PER AARD 53-30-00-02 AND SRM 53-01 FIG 2 SHEET 3. (M)

Part: PANEL — CORRODED (FUSELAGE)

TUL - FOUND FORWARD CARGO AREA LOWER PANEL HAS CORROSION UNDER LOWER FLANGE, ON DOOR BEAM. INSTALLED NEW LOWER PAND AND SPLICES AT LOWER FORWARD CARGO DOOR CUTOUT PER SRM 53-05, FIG 44. REPLACED FORWARD CARGO DOOR LOWER BEAM PER SRM 51-01 PAGE 1 STATION 370-426. (M)

Part: FRAME — CRACKED (FUSELAGE)

TUL - FOUND RIGHT SIDE BELT FRAME IS CRACKED JUST BELOW AIRSTAIR ACT AT MOUNT BRACKET. REPAIRED PER AARD 53-10-00-33 PAGE 1, 2, 3. (M)

Part: WEB — CRACKED (FUSELAGE)

TUL - FOUND LEFT CUSP CRACKED IN TWO PLACES BETWEEN STATION 218-237 (E58 NR 4173738). INSTALLED NEW SECTION OF CUSP LEFT SIDE BETWEEN STATION 218-237 PER SRM 53-01. (M)

Part: WINDOW — CRACKED (CABIN)

TUL - FOUND UPPER RIGHT CORNER OF WINDOW PANEL CRACKED AT STATION 1021, RIGHT SIDE. INSTALLED DOUBLER PER AARD 53-10-00-25. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON NR 1 SEAT TRACK BETWEEN STATION 1174 AND STATION 1309. INSTALLED NEW NR 1 SEAT TRACK BETWEEN STATION 1174 TO STATION 1309. (M)

Part: WINDOW — CRACKED (CABIN)

TUL - FOUND LOWER FORWARD CORNER OF WINDOW PANEL CRACKED AT STATION 1175, RIGHT SIDE. DOUBLER INSTALLED PER 53-10-00-25. (M)

Part: SENSOR — DEFECTIVE (NR 1 BRAKE)

SFO - FLT 1782 - EN ROUTE DFW-SFO - DURING FINAL DESCENT, DECLARED EMERGENCY LANDING DUE TO NR 1 BRAKE EXCESSIVE HIGH TEMPERATURE. LANDED SFO WITHOUT INCIDENT. REPLACED NR 1 BRAKE TEMP SENSOR. PERFORMED OPS CHECK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BATTERY — DISCHARGED (CABIN)

DFW - FOUND DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT AFT CABIN DIM. REPLACED EMERGENCY EXIT LIGHT BATTERY AT AFT CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: VALVE — DEFECTIVE (FUSELAGE)

SJC - FLT 2769 - SHORTLY AFTER TAKEOFF, ENTIRE CABIN FILLED WITH SMOKE AND HAZE. DETECTED A STRONG BURNING SMELL. AIR INTERRUPTED AND LANDED SJC WITHOUT INCIDENT. REPLACED LEFT PACK. REPLACED LEFT SIDE AUGMENTATION VALVE. REPLACED LEFT AND RIGHT SIDE COALESCER SOCKS. PERFORMED PACK BURNOUT CHECKS PER MM. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT CHECK, FORWARD ENTRY DOOR PORTABLE EMERGENCY LIGHT WAS INOPERATIVE. REPLACED PORTABLE LIGHT AT FORWARD ENTRY DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: VALVE — DEFECTIVE (NLG STRUT)

TUL - FLT 1031 - AFTER TAKEOFF AT TUL, NOSE GEAR WOULD NOT RETRACT. HYDRAULIC PRESSURE WAS NORMAL. RETURNED AND LANDED TUL WITHOUT FURTHER INCIDENT. REPLACED SCHRADER VALVE. SERVICED STRUT AND PERFORMED LEAK CHECK. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)