N426AA

Part: CABLE — UNSECURE (L2 DOOR SLIDE) · airframe 85,004 hrs · 46,030 cycles

L2 DOOR SLIDE HAS A CABLE PROTRUDING FROM PACK. REMOVED AND REPLACED SLIDE IAW AMM 25-62-00. OPS CHECKED GOOD. AIRCRAFT WAS GROUNDED.

Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY) · airframe 84,982 hrs · 46,016 cycles

AIRCRAFT WAS NOT GROUNDED. SMOKE DETECTOR AFT LEFT LAVATORY WARNING INDICATION AND CHIME INTERMITTENTLY DURING FLIGHT. REMOVED AND REPLACED SMOKE DETECTOR IAW AMM 26-11-00. OPERATIONAL CHECK GOOD.

Part: PIN — BACKED OUT (ZONE 700) · airframe 84,784 hrs · 45,879 cycles

AIRCRAFT WAS NOT GROUNDED. DURING TAKEOFF, THE WHEEL NOT ROLLING LIGHT ILLUMINATED. REJECTED TAKEOFF AT 70 KNOTS. INSPECTED ALL WHEEL SPEED TRANSDUCERS AND FOUND TRANSDUCER NR 2 PINS BACKED OUT. REINSTALLED PINS IAW AMM 32-43-02. OPERATIONAL CHECK GOOD.

Part: SLIDE — UNSECURE (R1 DOOR) · airframe 84,716 hrs · 45,833 cycles

AIRCRAFT WAS NOT GROUNDED. R1 DOOR EMERGENCY EVACUATION SLIDE IS UNPACKED UNDER THE COVER. REMOVED AND REPLACED SLIDE IAW AMM 25-62-00. OPERATIONAL CHECK GOOD.

Part: PORTABLE LIGHT — DIM (CABIN) · airframe 84,336 hrs · 45,590 cycles

AIRCRAFT WAS NOT GROUNDED. INTERIOR PORTABLE EMERGENCY LIGHT BY FORWARD ENTRY DOOR TESTED DIM. REMOVED AND REPLACED PORTABLE LIGHT ASSEMBLY IAW 33-53-00.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 82,036 hrs · 44,177 cycles

AIRCRAFT WAS IN BASE MX. LEFT CUSP IS CRACKED AT FS 224. ACCOMPLISHED DOUBLER REPAIR IAW AARD 53-20-00-16.

Part: SKIN — CRACKED (FUSELAGE) · airframe 82,036 hrs · 44,177 cycles

AIRCRAFT WAS IN BASE MX. FUSELAGE SKIN IS CRACKED, STATION 1309, BETWEEN L6L & L7L. ACCOMPLISHED TEMPORARY EXTERNAL DOUBLER REPAIR IAW SRM 53-04-02 FIG.2 SHEET 29 WITH BLIND FASTENERS IAW SRM 53-04-02 PARAGRAPH 3 C C 1.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 82,036 hrs · 44,177 cycles

AIRCRAFT WAS IN BASE MX. AFT CARGO DOOR, SECOND FROM BOTTOM STOP IS CRACKED. R & R FITTING IAW AARD 51-00-05-1.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 82,036 hrs · 44,177 cycles

AIRCRAFT WAS IN BASE MX. FWD CARGO DOOR AFT CTR STOP FITTING IS CRACKED. R & R FITTING IAW SRM 51-30-05.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 82,036 hrs · 44,177 cycles

AIRCRAFT WAS IN BASE MX. MID CARGO DOOR FWD CTR STOP FITTING IS CRACKED. R & R FITTING IAW AARD 51-00-05-1.

Part: PISTON — DEFLATED (NLG) · airframe 81,590 hrs · 43,895 cycles

DURING CLIMB, THE UNSAFE GEAR LIGHT ILLUMINATED. THE CREW LOWERED THE GEAR & THE LIGHT EXTINGUISHED. AN EMER WAS DECLARED & THE FLIGHT RETURNED TO FIELD. FLIGHT LANDED WITHOUT FURTHER INCIDENT. THE ACFT WAS REMOVED FROM SERVICE. FOUND THE LOWER PISTON NOT EXTENDING FULLY. R & R LOWER PISTON IAW MCM 32-92-12. OPERATIONALLY & LEAK CHECKED GOOD. NOSE GEAR RETRACTS NORMAL, NO FAULTS NOTED.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 81,197 hrs · 43,656 cycles

EMERGENCY LIGHT SYS TEST FAILED AT B5-104 & B5-105. R & R BATTERY PACK BS-105. SYS CHECKED NORMAL. SEE ALSO AALA20150724006.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 81,197 hrs · 43,656 cycles

EMERGENCY LIGHT SYS TEST FAILED AT B5-104 & B5-105. R & R BATTERY PACK BS-104. SYS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 80,929 hrs · 43,501 cycles

EMERGENCY EVACUATION LIGHT BATTERY PACK B5-27 IS INOPERATIVE. R & R BATTERY PACK B5-27 IAW AMM 33-53-00. PERFORMED OPERATIONAL CHECK. SYS CHECKED NORMAL.

Part: ACCUMULATOR — UNDERSERVICED (RUDDER) · airframe 80,889 hrs · 43,475 cycles

EMERGENCY DECLARED, LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. EXPERIENCING UNCOMMANDED RUDDER INPUTS DURING CLIMB. FOUND RUDDER ACCUMULATOR AT ZERO. SERVICED ACCUMULATOR IAW AMM 27-20-15. PERFORMED RUDDER THRU LIMITER SENSOR CHECK IAW AMM 27-20-06, YAW DAMPER ACTUATOR NULL POSITION IAW AMM 22-13-01. SYSTEM CHECKED NORMAL.

Part: GASKET — LEAKING (AC CHECK VALVE) · airframe 79,095 hrs · 42,406 cycles

TAIL COMPARTMENT HIGH TEMP INDICATION DURING CLIMB OUT. EMER DECLARED FLIGHT RETURNED & LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. REPLACED RT GND AIR CONDITIONING CHECK VLV GASKET THAT WAS LEAKING. SYS GND CHECKED NORMAL OPERATION CLOSED.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 78,873 hrs · 42,247 cycles

STRINGER 17 CRACKED ACROSS TOP DOWN TO FASTENER HOLE. REPLACED CRACKED SECTION OF STRINGER 17 IAW EA 53-036197.

Part: SKIN — CRACKED (FUSELAGE) · airframe 78,873 hrs · 42,247 cycles

LOW FREQUENCY EDDY CURRENT INDICATED SUBSURFACE CRACK AT RIVET AT UPPER FWD CORNER OF SERVICE DOOR JAMB. FABRICATED & INSTALLED TRIPLER IAW DWG SR09530172 & EA MD80-53-036082.

Part: SUPPORT RIB — CRACKED (RT WING) · airframe 78,873 hrs · 42,247 cycles

RIGHT WING NR 4 SLAT INBD SUPPORT RIB CRACKED. ACCOMPLISHED REPAIR IAW EA MD80-57-036083.

Part: RIB — CRACKED (LT WING) · airframe 78,873 hrs · 42,247 cycles

LEFT WING NR 4 SLAT TRACK INBD SUPPORT RIB CRACKED. ACCOMPLISHED REPAIR IAW EA MD 8057-036083.

Part: CUSP WEB — DAMAGED (FUSELAGE) · airframe 78,873 hrs · 42,247 cycles

TWO HOLES OFF LINE AT LT CUSP FROM STATIONS 339 TO 340. INSTALLED DOUBLER IAW AARD 53-20-00-16.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 78,873 hrs · 42,247 cycles

SHEAR TIE AT STATION 1287 BETWEEN LONGERONS 26 TO 20 LT CORRODED. INSTALLED NEW PART IAW SRM 51-30-02.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 78,873 hrs · 42,247 cycles

FLOORBEAM INTERCOSTAL BETWEEN STATIONS 1287 TO 1309 AT CENTERLINE CRACKED. REPLACED INTERCOSTAL IAW SRM 51-30-05.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 78,873 hrs · 42,247 cycles

CRACK IN UPPER END OF STIFFENER ON FWD SIDE OF STATION 1338 BULKHEAD AFT OF LONGERON 1. INSTALLED STIFFENER IAW AARD 51-00-05-1 & 9915562 FINAL ASSEMBLY DWG.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 78,873 hrs · 42,247 cycles

LEFT CUSP CORRODED FROM STATIONS 1054 TO 1060. INSTALLED NEW CUSP SHEET IAW AARD 53-20-00.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 78,873 hrs · 42,247 cycles

OUTBOARD END OF SHEAR TIE CRACKED AT STATION 1429 & LONGERON 2 LT. REPLACED CLIP IAW AARD 51-00-05-1.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 78,873 hrs · 42,247 cycles

LEFT CUSP CORRODED FROM STATIONS 310 TO 313. INSTALLED DOUBLER IAW AARD 53-20-00-16.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 78,873 hrs · 42,247 cycles

RIGHT CUSP CRACKED AT STATION 1155. INSTALLED CUSP DOUBLER AT STATION 1155 IAW AARD 53-20-00-16.

Part: CUSP WEB — DAMAGED (FUSELAGE) · airframe 78,873 hrs · 42,247 cycles

TWO RIVET HOLES IN CUSP UNDER NR 1 SEAT TRACK DAMAGED AT STATION 1022. INSTALLED NEW CUSP SHEET IAW AARD 53-20-00-16 & 51-00-01-5.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 78,873 hrs · 42,247 cycles

SEAT TRACK NR 6 FROM STATIONS 1227 TO 1228 CORRODED. INSTALLED REPAIR PLUG IAW AARD 53-20-00-10.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 78,873 hrs · 42,247 cycles

CORROSION ON WEB AT FRAME STATION 1155 & LONGERON 28 RT. ACCOMPLISHED NESTED ANGLE REPAIR IAW EA MD80 -53-036034.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 78,873 hrs · 42,247 cycles

SEAT TRACK NR 4 FROM STATIONS 1227 TO 1228 CORRODED. INSTALLED REPAIR PLUG IAW AARD 53-20-00-10.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 78,873 hrs · 42,247 cycles

AFT CARGO FWD LT TIE DOWN TRACK FROM STATIONS 1003 TO 1155 CORRODED. REPLACED TRACK IAW AARD 51-00-05-01.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 78,873 hrs · 42,247 cycles

LEFT CUSP CORRODED FROM STATIONS 247 TO 248. INSTALLED DOUBLER IAW AARD 53-20-00-16.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 78,873 hrs · 42,247 cycles

ELONGATED HOLE AT STATION 780 LT SIDE FILLET ATTACH. INSTALLED REPAIR DOUBLER IAW SRM 53-04-00-57C.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 78,873 hrs · 42,247 cycles

SEAT TRACK NR 6 FROM STATIONS 209 TO 237 CORRODED. SPLICED IN NEW SECTION OF SEAT TRACK FROM STATIONS 209 TO 348 IAW SRM 53-05-00-001 FIGURE 4F.

Part: STRUCTURE — CRACKED (MLG DOOR) · airframe 78,873 hrs · 42,247 cycles

CRACK AT OTBD CHANNEL FWD CORNER AT UPLOCK. INSTALLED DOUBLER IAW SRM 52-05-00-001 FIGURE 59.

Part: FRAME — CRACKED (FUSELAGE) · airframe 78,873 hrs · 42,247 cycles

CRACK IN FRAME 1322 RT SIDE AT LONGERON 17 RT. INSTALLED FRAME REPAIR ANGLE IAW EA MD80-53-036016.

Part: FRAME — CRACKED (FUSELAGE) · airframe 78,873 hrs · 42,247 cycles

CRACK IN FRAME AT STATION 1322 & LONGERON 17 LT. ACCOMPLISHED NESTED ANGLE REPAIR IAW SRM 53-03-00-001 PARAGRAPH 45 FIGURE 51 & EA MD80-53-036016.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 78,873 hrs · 42,247 cycles

SUBFLOOR CUSP AT STATION 177 AT RBL 54 HAD CRACKS AROUND FASTENER HOLE. REMOVED DAMAGED SECTION OF SUBFLOOR CUSP FORM STATIONS 160 TO 200 & RBL 42 TO 58 & INSTALLED DOUBLER IAW AARD 53-20-00-16.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 78,121 hrs · 41,808 cycles

OVERHEAD EMERGENCY LIGHTS FROM ROWS 12 TO 16. REPLACED BATTERY PACK FOR OVERHEAD EMERGENCY LIGHTS FROM ROWS 12 TO 16, OPERATIONS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (AC BAY) · airframe 78,121 hrs · 41,808 cycles

BOTTOM TAIL CONE EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK B5-28, OPERATIONS CHECKED NORMAL.

Part: COVER — MISSING (BATTERY PACK) · airframe 78,121 hrs · 41,808 cycles

FORWARD OVERWING EMERGENCY LIGHT BATTERY PACK MISSING TOP COVER. REPLACED FWD OVERWING EMERGENCY LIGHT BATTERY PACK, OPERATIONS CHECKED NORMAL.

Part: BATTERY — DISCHARGED (CABIN) · airframe 78,121 hrs · 41,808 cycles

EMERGENCY LIGHTS FROM ROWS 20 TO 32 INOPERATIVE. REPLACED BATTERY IN MODULE AB5-3, OPERATIONS CHECKED NORMAL.

Part: CONTROL MODULE — INOPERATIVE (CABIN) · airframe 77,744 hrs · 41,587 cycles

AFT ZONE EMERGENCY SEAT PATH LIGHTING WILL NOT TEST. REPLACED AFT ZONE ESCAPE PATH LIGHTING CONTROL MODULE. OPERATIONS CHECKED NORMAL.

Part: SLIDE — LOW PRESSURE (L1 DOOR) · airframe 76,415 hrs · 40,812 cycles

LT NR 1 DOOR SLIDE PRESSURE BELOW GREEN. REPLACED LT NR 1 DOOR SLIDE. OPERATIONS CHECKED NORMAL.

Part: SPAR CAP — CRACKED (LT WING) · airframe 75,229 hrs · 40,143 cycles

CRACK ON THE AFT SIDE OF THE LEFT WING REAR SPAR LOWER CAP AT STATION XRS 164 LEFT. WING LOWER SPAR SPLICE REPAIR COMPLETED PER BOEING DRAWING J060165 AND EA MD80-57-028642.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 75,052 hrs · 40,045 cycles

RIGHT CENTER EMERGENCY LIGHTS BETWEEN AFT LAVATORIES INOPERATIVE. REPLACED BATTERY PACK FOR RIGHT CENTER EMERGENCY LIGHTS BETWEEN AFT LAVATORIES. OPS CHECK NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 75,052 hrs · 40,045 cycles

TAIL COMPARTMENT EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR TAIL COMPARTMENT EMERGENCY LIGHTS. OPS CHECK NORMAL.

Part: BATTERY PACK — NOT SEATED (CABIN) · airframe 75,052 hrs · 40,045 cycles

CEILING EMERGENCY LIGHTS FROM ROWS 3 TO 6 INOPERATIVE. RESEATED BATTERY PACK FOR CEILING EMERGENCY LIGHTS FROM ROWS 3 TO 6. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABNI) · airframe 73,898 hrs · 39,393 cycles

LEFT NUMBER 1 DOOR PORTABLE EMERGENCY LIGHT INOPERATIVE. REPLACED LEFT NUMBER 1 DOOR PORTABLE EMERGENCY LIGHT. OPS CHECK NORMAL.

Part: FAN — MALFUNCTIONED (CABIN) · airframe 72,986 hrs · 38,882 cycles

DFW - CREW REPORTED AFTER TAKEOFF, AFT CABIN FILLED WITH SMOKE AND OILY FUMES. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED RECIRCULATION FAN. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: APU — LEAKING (APU BAY) · airframe 72,986 hrs · 38,881 cycles

DFW - CREW REPORTED DARK SMOKE IN AFT OF CABIN. FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND AUXILIARY POWER UNIT LEAKING OIL. REPLACED APU. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: LIGHT — LOW (CABIN) · airframe 70,758 hrs · 37,618 cycles

FORWARD LEFT NUMBER 1 DOOR EMERGENCY LIGHT ASEMBLY DIM. REPLACED FORWARD EMERGENCY LIGHT ASSEMBLY. OPS CHECK NORMAL.

Part: BATTERY PACK — DISCHARGED (AC BAY) · airframe 70,758 hrs · 37,618 cycles

TAIL COMPARTMENT EMERGENCY LIGHTS ABOVE CATWALK INOPERATIVE. REPLACED BATTERY PACK. OPS CHECK NORMAL.

Part: MODULE — INOPERATIVE (FUEL QUANTITY) · airframe 68,461 hrs · 36,301 cycles

IND - CREW REPORTED ALL FUEL QUANTITY INDICATIONS WENT BLANK. EMERGENCY DECLARED FLIGHT RETURNED IND LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED STANDARD ELECTRIC MODULE IN FUEL QUANTITY INDICATOR. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 67,756 hrs · 35,923 cycles

CABIN FORWARD ENTRY STRINGER 4 LEFT CRACKED AT STATION 200 AT LOWER FASTENER. INSTALLED LONGERON 4 LEFT FROM STATION 165 LEFT TO STATION 226 LEFT PER SRM 53-02-00 FIG 18 AND AARD 51-60-00-01.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,756 hrs · 35,923 cycles

AFT CARGO HAS CORROSION IN SHEAR TIE AT STATION 1287 BETWEEN LONGERON 26 LEFT TO LONGERON 28 LEFT. INSTALLED REPAIR SECTION OF SHEAR TIE AT STATION 1287 BETWEEN LONGERON 26 LEFT TO LONGERON 28 LEFT PER BOEING DRAWING NUMBER 9957739 AND SRM 53-03-00.

Part: FLAP — GOUGED (RT WING) · airframe 67,756 hrs · 35,923 cycles

RIGHT WING, OUTBOARD MID FLAP, MOST INBOARD BULL-NOSE IS GOUGED AT HINGE FAIRING AREA. BLENDED GOUGED AREA AND DYE CHECKED, NO CRACKS FOUND, PER ESO 80559. ALODINED BLENDED AREA, FLUSH FILLED, PRIMED, FABRICATED AND INSTALLED REPAIR DOUBLER, PER EA MD80-57-009671.

Part: WEB — DAMAGED (CARGO DOOR) · airframe 67,756 hrs · 35,923 cycles

STATIONS 1215 TO 1219 CARGO DOOR WEB CORRODED. ACCOMPLISHED SPLICE REPAIR PER AARD 53-10-00-24.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 67,756 hrs · 35,923 cycles

RIGHT J-BEAM DOUBLER IS CRACKED AT THE AFT SIDE UPPER FASTENER (MARKED) STATION 47 LONGERON 27 RIGHT. INSTALLED REPAIR PER AARD 53-10-00-4.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 67,756 hrs · 35,923 cycles

CRACK IN LONGERON 5 RIGHT STATIONS 1298 TO 1338. REPLACED DAMAGED LONGERON PER SRM 53-02-00 FIGURE 18.

Part: SKIN — CANNING (ENTRY DOOR) · airframe 67,756 hrs · 35,923 cycles

FORWARD ENTRY DOOR OIL CANNING AND DAMAGED AT BOTTOM OF DOOR. CUT OUT DAMAGED BOTTOM SECTION AND INSTALLED DOUBLER REPAIR AS PER SRM 52-05 00 FIGURE 37 PAGE 210.

Part: SKIN — DAMAGED (ENTRY DOOR) · airframe 67,756 hrs · 35,923 cycles

FORWARD ENTRY DOOR HOLD OPEN HOOK EXTERIOR SKIN DAMAGE. INSTALLED DOUBLER REPAIR AS PER SRM 52-05-00 FIGURE 20 PAGE 1.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,756 hrs · 35,923 cycles

SEAT TRACK NUMBER 4 LUG IS OUT OF LIMITS AT STATION 710. INSTALLED SEAT TRACK PLUG ON SEAT TRACK NUMBER 4 AT STATION 710 AS PER SRM 53-05 FIGURE 4A. TREATED AND PRIMED AREA AS PER SRM 51-10-3.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,756 hrs · 35,923 cycles

RIGHT CUSP CORRODED FROM STATION 1250 TO 1309. DAMAGED CUSP REMOVED AND NEW CUSP SHEET INSTALLED PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,756 hrs · 35,923 cycles

CORROSION ON LEFT CUSP STATION 1250 TO 1309. REMOVED CORRODED CUSP SHEET AND INSTALLED NEW SHEET PER AARD 53-20-00-16.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,756 hrs · 35,923 cycles

SEAT TRACK 1 CORRODED STATION 1280 TO 1284. REMOVED CORROSION AND REPAIRED PER AARD 53-20-00-10.

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 67,756 hrs · 35,923 cycles

CRACK IN RIGHT WHEEL WELL PRESSURE DECK STATION 1003 OUTBOARD SIDE. CRACK STOP DRILLED AND DOUBLER INSTALLED PER AARD53-30-00-13 AND SRM 53-01-00.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,756 hrs · 35,923 cycles

CORROSION ON THE LEFT CUSP UNDER THE AFT SERVICE DOOR AFT GIRT FITTING SUPPORT BRACKET AT THE FASTENER HOLES STATION 1168. COMPLETED CUSP REPAIR PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,756 hrs · 35,923 cycles

STATION 522 RIGHT CUSP CORROSION ON BOTTOM SIDE NEAR FRAME FOOT. COMPLETED REPAIR INSTALLATION PER AARD 53-20-00-16.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 67,756 hrs · 35,923 cycles

FUSELAGE CRACKED AT CANT LEFT 1474. INSTALLED DOUBLER PER SRM 53-01-00 FIGURE 2 SHEET 3.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,756 hrs · 35,923 cycles

CORROSION ON LEFT CUSP STATION 896. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — WORN (FUSELAGE) · airframe 67,756 hrs · 35,923 cycles

WORN SPOT TOP OF CUSP STATION 1250 BETWEEN NUMBER 1 AND NUMBER 2 SEAT TRACKS. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: SKIN — DAMAGED (LT WING) · airframe 67,756 hrs · 35,923 cycles

TOP CENTER OUTER SKIN HAS LARGE CREASE IN TRAILING EDGE. FABRICATED AND INSTALLED DOUBLER PER ESO80174, PAGE 6(B)MRT025229.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 67,756 hrs · 35,923 cycles

STATION 218 RIGHT CUSP SHEET IS CRACKED AND CORRODED AT AFT OUTBOARD CORNER AREA AT NUMBER 6 SEAT TRACK AREA. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: PAN — CRACKED (WINDOW) · airframe 67,756 hrs · 35,923 cycles

AT STATION 1060 LEFT FOUND THE LOWER FORWARD EAR OF THE WINDOW PAN CRACKED. CUT OUT CRACKED AREA OF RING PAN AND INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 67,756 hrs · 35,923 cycles

AT STATION 1098 LEFT FOUND THE UPPER AFT EAR OF THE WINDOW PAN CRACKED. CUT OUT CRACKED AREA OF RING PAN AND INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: RIB — CRACKED (LE SLAT) · airframe 67,756 hrs · 35,923 cycles

RIGHT NUMBER 5 SLAT, NUMBER 14 SLAT TRACK RIB CRACKED AT OUTBOARD SIDE. REPLACED DAMAGED NUMBER 14 RIB ON NUMBER 5 SLAT UNDER ESO 80117.

Part: RIB — CRACKED (LE SLAT) · airframe 67,756 hrs · 35,923 cycles

RIGHT NUMBER 5 SLAT, NUMBER 15 SLAT TRACK RIB CRACKED ON OUTBOARD SIDE. REPLACED NUMBER 15 RIB ON NUMBER 5 SLAT UNDER ESO 80117.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 66,970 hrs · 35,488 cycles

EMERGENCY EXIT LIGHT FLOOR LEVEL BY FORWARD LAVATORY INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT FORWARD GALLEY EXTERIOR OPPOSITE LAVATORY. OPS CHECK GOOD.

Part: BATTERY — NOT SEATED (CABIN) · airframe 66,970 hrs · 35,488 cycles

EMERGENCY LIGHT IN TAIL COMPARTMENT INOPERATIVE. RESEATED BATTERIES IN AFT LAVATORY. OPS CHECK GOOD PER MM.

Part: BATTERY PACK — NOT SEATED (CABIN) · airframe 66,383 hrs

LGA - TAIL COMPARTMENT EMERGENCY LIGHTS INOPERATIVE. RESEATED BATTERY PACK FOR TAIL COMPARTMENT EMERGENCY LIGHTS.

Part: GUARD — DAMAGED (CABIN)

DFW - EMERGENCY LIGHT GUARD AT SEAT 9D DAMAGED. REPLACED GUARD FOR EMERGENCY LIGHT AT SEAT 9D.

Part: CONNECTOR — LOOSE (NR 2 START VALVE) · airframe 64,928 hrs

INFLIGHT, RIGHT ENGINE START VALVE INDICATION. RETURNED TO TUL AND LANDED WITHOUT INCIDENT. RESEATED VALVE CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: STRAP — MISSING (FLASHLIGHT) · airframe 64,602 hrs

LGA - EMERGENCY FLASHLIGHT AT AFT JUMPSEAT HAS MISSING STRAP. REPLACED STRAP FOR EMERGENCY FLASHLIGHT AT AFT JUMPSEAT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: PUMP — FAILED (FUEL SYSTEM) · 64,147 cycles

ABQ INFLIGHT T1968/14AUG SLC TO DFW. CREW REPORTED CENTER TANK FUEL UNUSABLE. LANDED ABQ WITHOUT INCIDENT. REPLACED BOTH CENTER TANK FUEL PUMPS. SYSTEM GROUND CHECKED NORMAL OPS.

Part: SENSOR — INOPERATIVE (RT ENGINE)

STL INFLIGHT T755/20SEP ORD TO SAT - RIGHT ENGINE OIL TEMPERATURE FLUCTUATED DURING CLIMB FROM 110 DEGREES TO 130 DEGREES. AT CRUISE THE TEMPERATURE ROSE TO ABOVE 140 DEGREES. DIVERTED TO STL AND LANDED WITHOUT INCIDENT. REPLACED RIGHT ENGINE OIL TEMPERATURE SENSOR AND RIGHT ENGINE OIL FILTER. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LENS — BROKEN (EMERGENCY LIGHT)

MSP - EMERGENCY LIGHTS AT SEAT 19D HAS BOTH LENS AND HOUSINGS BROKEN. REPLACED BOTH LENS AND HOUSINGS FOR EMERGENCY LIGHTS AT SEAT 19D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SHROUD — BROKEN (EMERGENCY LIGHTS)

DFW - EMERGENCY LIGHTS AT SEATS 9D AND 12D HAVE BROKEN SHROUDS. REPLACED SHROUDS FOR EMERGENCY LIGHTS AT SEATS 9D AND 12D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — LOOSE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS IN OVERHEAD BETWEEN AFT LAVATORIES INOPERATIVE. TIGHTENED EMERGENCY EXIT LIGHTS BATTERY IN PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: PACKING — LEAKING (APU)

MEX - FLT 1156 - EN ROUTE MEX-DFW, NOTICED HEAVY SMOKE IN CABIN RIGHT AFTER TAKEOFF AT MEX. RAN CABIN FIRE AND SMOKE CHECKLIST, SMOKE DISSIPATED WHEN PACKS AND RECIRCULATION FAN TURNED OFF. RETURNED AND LANDED MEX WITHOUT INCIDENT. REPLACED PACKING AT APU MASTER CHIP DETECTOR. RAN APU, NO OIL LEAKS NOTED. PERFORMED AIRCRAFT PACKS AND HIGH PRESSURE PNEUMATIC DUCTING BURN OUT. REPLACED BOTH PACKS COALESCERS BAGS. RAN UP AIRCRAFT PACKS, NO SMOKE OR ODOR NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: DOOR FRAME — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON SEVERAL AREAS OF AFT CARGO DOOR BEAM. REMOVED AND REPLACED AFT CARGO DOOR BEAM PER SRM 51-01. (M)

Part: SEAT TRACK — DAMAGED (FUSELAGE)

TUL - FOUND NUT PLATE MISSING FOR GALLEY TIE DOWN. CUT OUT AREA AND INSTALLED SEAT TRACK PLUG PER 53-05. (M)

Part: SHEAR TIE — CRACKED (FUSELAGE)

TUL - FOUND SHEAR TIE CRACKED IN AFT ACCESSORY STATION 1437 INBOARD OF LONGERON 3R AFT FACE OF FRAME. REMOVED AND REPLACED SHEAR TIE PER SRM 51-01. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON TOP AND BOTTOM OF LEFT CUSP AROUND LIGHTNING 2 HOLES. REMOVED CORROSION AND INSTALLED DOUBLER PER AARD 53-00-00-02 AND SRM 53-01 FIG 4. (M)

Part: INTERCOSTAL — CRACKED (FUSELAGE)

TUL - FOUND INTERCOSTAL CRACKED IN AFT CARGO BLO STATION 1287-1309 BETWEEN FLOORBEAMS. REMOVED AND REPLACED INTERCOSTAL PER SRM 51-01. (M)

Part: LONGERON — CRACKED (FUSELAGE)

TUL - FOUND LONGERON 3L CRACKED IN RADIUS INBOARD OF OUTBOARD FASTENER STATION 160. SPLICED NEW LONGERON FROM STATION 170 FORWARD IAW SRM 53-02 FIG 18 SHEETS 1-4-5-6. (M)

Part: SKIN — GOUGED (FUSELAGE)

TUL - FOUND .25 INCH BY .25 INCH GOUGE AND DENT ON LEFT FUSELAGE APPROXIMATELY 10 INCHES BELOW FORWARD STATIC PORT. REMOVED DAMAGE AND INSTALLED A DOUBLER PER SRM 53-04 FIG 38 SHEET 23. (M)

Part: LONGERON — CRACKED (FUSELAGE)

TUL - FOUND LONGERON 4L CRACKED AT FRAME STATION 160. CUT OUT DAMAGED AREA AND INSTALLED SPLICE PER SRM 53-02 FIG 18. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL - FOUND NR 3 SEAT TRACK CORRODED STATION 1231-1233. INSTALLED SEAT TRACK PLUG REPAIR PER AARD 53-20-00-10, PAGE 2 FIG 1. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON RIGHT CUSP STATION 731. REMOVED CORROSION AND INSTALLED DOUBLER PER AARD 53-00-00-02. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL - NR 5 SEAT TRACK CORRODED STATION 233. INSTALLED SEAT TRACK PLUG PLUG PER SRM 53-05 FIG 4A. RESTORED PROTECTIVE FINISH. (M)

Part: SKIN — CRACKED (FUSELAGE)

TUL - FOUND FUSELAGE SKIN CRACKED ABOVE NR 2 ENGINE PYLON STATION 1380 LONGERON 13R. STOP DRILLED CRACK AND INSTALLED DOUBLER PER SRM 53-01 FIG 2 SHEET 3. (M)

Part: SKIN — CRACKED (FUSELAGE)

TUL - FOUND STATION 1380 ABOVE NR 1 ENGINE PYLON ABOVE LONGERON 13L OUTER SKIN CRACKED 2 PLACES AT SHEAR TIE LOWER RIVET. STOP DRILLED CRACK OK. INSTALLED DOUBLER PER SRM 53-01-00 FIG 2 SHEET 3. (M)

Part: COALESCER BAG — CONTAMINATED (A/C BAY)

SJC - FLT 1549 - SJC-SAN, AIR INTERRUPTED DUE TO SMOKE IN CABIN. AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED CONICAL CONDENSER, CLEAN DUCTS, AND ACCOMPLISHED PACK BURN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

ORD - DURING OVERNIGHT MAINTENANCE, RIGHT FORWARD OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED BATTERY PACK RIGHT FORWARD OVERWING EMERGENCY EXIT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LONGERON — CRACKED (FUSELAGE)

TUL - FOUND LONGERON 4L CRACKED AT STATION 160. REPAIRED PER SRM 53-02, FIG 18. (M)

Part: SOCKET — DEFECTIVE (CABIN)

ORD - FLT 2244 - EN ROUTE DFW-ORD, DURING LANDING ELECTRICAL BURNING SMELL AROUND AISLE 25 AFTER LANDING GEAR FULLY EXTENDED REPORTED BY FLIGHT ATTENDANT. LANDED ORD WITHOUT INCIDENT. REPLACED RIGHT OVERHEAD FLUORESCENT LAMP HOLDER AT ROW 19. NO OTHER DEFECTS NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — BROKEN (TAILCONE)

DFW - DURING OVERNIGHT MAINTENANCE, TAILCONE EMERGENCY EXIT LIGHT INOPERATIVE. REPAIRED WIRE TO TAILCONE EMEREGNCY EXIT LIGHT. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: WIRE — BROKEN (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT IN CEILING JUST FORWARD OF AFT STAIR DOOR INOPERATIVE. REPAIRED WIRING FOR EMERGENCY EXIT LIGHT IN CEILING JUST FORWARD OF AFT STAIR DOOR. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: COALESCER — DIRTY (A/C BAY)

ORD - FLT 366 - DURING CLIMB-OUT, FLIGHT ATTENDANT REPORTED A STRONG HOT BURNING METAL SMELL IN AFT COACH CABIN. FLIGHT AIR INTERRUPTED AND RETURNED ORD WITHOUT FURTHER INCIDENT. BURNIG SMELL DISSIPATED WHEN AIRCRAFT LANDED. MAINTENANCE TROUBLE SHOT SYSTEM UNABLE TO DUPLICATE SMELL. AS A PRECAUTIONARY, MAINTENANCE REMOVED AND REPLCED COALESCER BAGS AND PERFORMED PACK BURN OUT PER THE MM. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — FAILED (CABIN)

DFW - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR PATH LIGHTING INOPERATIVE. REPAIRED EMERGENCY EXIT FLOOR PATH CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: FLOWMETER — FAILED (NR 2 ENGINE)

BOS - FLT 2221 - DURING CLIMB-OUT PVD, RIGHT FUEL FLOW INDICATOR BEGAN OPERATING ERRATICALLY WITH CLIMB POWER. FLIGHT AIR INTERRUPTED AND LANDED BOS WITHOUT INCIDENT. MAINTENANCE REPLACED RIGHT FUEL FLOW TRANSMITTER. RIGHT ENGINE WAS GROUND RUN AT POWER WITH NO IRREGULARITIES OR LEAKS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (COCKPIT)

DFW - DURING OVERNIGHT CHECK, EMERGENCY LIGHT IN COCKPIT INOPERATIVE. SECURED GROUND ON EMERGENCY LIGHT IN COCKPIT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: ANGLE — CORRODED (BS 617-619)

TUL - FOUND CORROSION ON BOTTOM OF CUSP MEMBRANE STATION 617 TO STATION 619, LONGERON 18L. REMOVED OLD CUSP. MANUFACTURED AND INSTALLED DOUBLER PER SRM 53-01 FIG 4-3. (M)

Part: UPLOCK SENSOR — DEFECTIVE (NLG)

DFW - FLT 1351 - AFTER TAKEOFF IAD AND LANDING GEAR RETRACTED, RED NLG LIGHT ILLUMINATED FOR APPROXIMATELY 1 MINUTE AND THEN EXTINGUISHED WITH NO OTHER ABNORMAL INDICATIONS. AIRCRAFT PROCEEDED TO DFW AND LANDED WITHOUT INCIDENT. REPLACED NLG UPLOCK SENSOR. SYSTEM GROUND CHECKED, NORMAL OPERATION.

Part: PRESSURIZATION — MALFUNCTIONED (CABIN)

DCA - FLT 1416 - EN ROUTE DFW-BDL, DURING CRUISE AT FL 370, CABIN BEGAN A 100 FPM CLIMB AND FLOW LIGHT ILLUMINATED FOLLOWED BY AN INCREASE IN CABIN CLIMB RATE. INITIATED EMERGENCY DESCENT. ALL PAX OXYGEN MASKS DEPLOYED SUCCESSFULLY. AIRCRAFT DIVERTED TO DCA AND LANDED WITHOUT INCIDENT. CHECKED AIR CYCLE MACHINE DUCTING FOR LEAKS WITH NO DEFECTS FOUND. ACCOMPLISHED GROUND ENGINE RUN AND PRESSURIZATION SYSTEM CHECKED NORMAL IN AUTO AND MANUAL MODES. RESTOWED ALL PASSENGER OXYGEN MASKS. ACCOMPLISHED FUNCTIONAL CHECK FLIGHT WITH NO DEFECTS FOUND. SYSTEM OPERATIONAL CHECKED NORMAL. UNABLE TO DUPLICATE PROBLEM AND AIRCRAFT RETURNED TO SERVICE. (M)