N439AA

Part: CSD — FAULTY (LT ENGINE) · airframe 89,089 hrs · 42,726 cycles

AIRCRAFT WAS GROUNDED. ON TAKEOFF, LOUD NOISE DETECTED ON THE LEFT SIDE OF AIRPLANE, AFT OF THE COCKPIT. REMOVED AND REPLACED LEFT ENGINE CONSTANT SPEED DRIVE TRANSMISSION ASSEMBLY IAW AMM 24-10-01 AND THE AC GENERATOR IAW AMM 24-20-01 (AALA20170103018). OPERATIONAL CHECK GOOD.

Part: GENERATOR — FAULTY (LT ENGINE) · airframe 89,089 hrs · 42,726 cycles

AIRCRAFT WAS GROUNDED. ON TAKEOFF, LOUD NOISE DETECTED ON THE LEFT SIDE OF AIRPLANE, AFT OF THE COCKPIT. REMOVED AND REPLACED LEFT ENGINE CONSTANT SPEED DRIVE TRANSMISSION ASSEMBLY IAW AMM 24-10-01 (AALA20170103017) AND THE AC GENERATOR IAW AMM 24-20-01. OPERATIONAL CHECK GOOD.

Part: FLASHLIGHT — INOPERATIVE (FWD CABIN) · airframe 88,967 hrs · 42,643 cycles

FLIGHT ATTENDANT EMERGENCY FLASHLIGHT AT L2 DOOR IS NOT FLASHING. REMOVED AND REPLACED FLASHLIGHT ASSEMBLY IAW AMM 25-60-00. OPERATIONAL CHECKED GOOD.

Part: SKIN — CRACKED (BS 168-172) · airframe 88,233 hrs · 42,178 cycles

CRACK ON INSIDE OF FORWARD PASSENGER DOOR ON WEB FORWARD UPPER CORNER. INSTALLED DOUBLER IAW EA 262994 AND SRM 52-01-00-001 FIG 2 SHEET 3.

Part: FRAME — WORN (BS 1510) · airframe 88,233 hrs · 42,178 cycles

FRAME AT BS 1510 IS WORN ON LOWER LEFT SIDE BETWEEN L20 - 27L. REPAIRED THE FRAME IAW SRM 53-01-00-001 FIGURE 2 AND EA 262881.

Part: STOP FITTING — CRACKED (FWD CARGO DOOR) · airframe 88,233 hrs · 42,178 cycles

FORWARD CARGO DOOR LOWER FORWARD STOP FITTING IS CRACKED. REMOVED AND REPLACED THE STOP FITTING IAW AARD 51-00-05-1 AND DRAWING 5910141.

Part: PRESSURE SWITCH — LEAKING (APU) · airframe 874,375 hrs · 417,678 cycles

AIRCRAFT WAS GNDED. DURING BOARDING THE CABIN BEGAN TO FILL WITH SMOKE. APU AIR WAS TURNED OFF. FOUND THE APU LOW OIL PRESS SWITCH LEAKING. R & R SWITCH & ACCOMPLISHED LEAK CHECK IAW AMM 49-90-03. SYS CHECKED NORMAL.

Part: BATTERY — DISCHARGED (CABIN) · airframe 86,749 hrs · 41,293 cycles

AFT EPM LIGHTS DIM WHEN TESTING DUAL FEED CHECK WITH AB5-2 & AB5-3 BATTERY PACKS. REPLACED BATTERY AT AB5-3 IAW AMM 33-60-98, OPERATIONALLY CHECKED NORMAL. THE ACFT WAS NOT GNDED.

Part: VERTICAL GYRO — FAULTY (ZONE 100) · airframe 86,606 hrs · 41,215 cycles

AIRCRAFT WAS GNDED. AIR INTERRUPT, EMER DECLARED, LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. DURING CRUISE ALTERNATE HORIZON LIGHT ILLUMINATED IN BOTH FMAS & THE FIRST OFFICER`S DIRECTIONAL GYRO BECAME INOPERATIVE. R & R NR 2 VERTICAL GYRO IAW AMM 34-23-01 & NR 2 DIGITAL FLIGHT GUIDANCE COMPUTER IAW AMM 22-01-01. PERFORMED RTS IAW AMM 22-01-05. OK FOR SERVICE. SEE ALSO AALA20160111002.

Part: COMPUTER — FAULTY (FLIGHT GUIDANCE) · airframe 86,606 hrs · 41,215 cycles

AIRCRAFT WAS GNDED. AIR INTERRUPT, EMER DECLARED, LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. DURING CRUISE ALTERNATE HORIZON LIGHT ILLUMINATED IN BOTH FMAS & THE FIRST OFFICER`S DIRECTIONAL GYRO BECAME INOPERATIVE. R & R NR 2 VERTICAL GYRO IAW AMM 34-23-01 & NR 2 DIGITAL FLIGHT GUIDANCE COMPUTER IAW AMM 22-01-01. PERFORMED RTS IAW AMM 22-01-05. OK FOR SERVICE. SEE ALSO AALA20160109008.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 85,559 hrs · 40,574 cycles

EXTERIOR OVERWING EMER LIGHTS INOPERATIVE. R & R BATTERY PACK B5-49 FOR OVERWING EMER LIGHTS IAW AMM 33-53-00. SYSTEM CHECKED NORMAL.

Part: SEALANT — FAILED (WINDOW) · airframe 85,057 hrs · 40,279 cycles

AIR INTERRUPT, EMER DECLARED, LANDING UNEVENTFUL & ACFT OVERWEIGHT. DURING CLIMB R1 WINDOW SEALANT FAILED AT LOWER RT SIDE OF WINDOW SMEARING ACROSS CORNER OF WINDOW. RESEALED WINDOW.

Part: RIB — CRACKED (LT WING) · airframe 80,716 hrs · 38,012 cycles

LT WING AT NR 4 SLAT TRACK INBD SUPPORT RIB CRACKED. INSTALLED NEW SERVICEABLE RIB SUPPORT.

Part: SUPPORT — CRACKED (RT WING) · airframe 80,716 hrs · 38,012 cycles

RT WING LE SUPPORT FORMER CRACKED AT NR 4 SLAT TRACK. INSTALLED NEW SERVICEABLE RT LE SUPPORT FORMER.

Part: BRACKET — CRACKED (EMERGENCY EXIT) · airframe 80,716 hrs · 38,012 cycles

RT AFT OVERWING EXIT DOOR CRACKED AT UPPER FORWARD CORNER AT UPPER BRACKET. INSTALLED DOUBLER IAW SRM 52-05-00.

Part: ANGLE — CRACKED (RT WING) · airframe 80,716 hrs · 38,012 cycles

RT WING UPPER ANGLE CRACKED INSIDE TANK PLATE 1440C. REPLACED ANGLE PN IAW AARD 51-00-05-1 & DRAWING 3951378.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 80,716 hrs · 38,012 cycles

LT CUSP CORRODED ON UPPER SURFACE AT STATION 1285 BETWEEN NRS 1 & 2 SEAT TRACKS. INSTALLED NEW CUSP SHEET FROM STATIONS 1250 TO 1309 IAW AARD 51-00-05-1.

Part: FITTING — CRACKED (FUSELAGE) · airframe 80,716 hrs · 38,012 cycles

FITTING JUST FWD OF CANT FRAME 1463, LT SIDE IS CRACKED. REPLACED FITTING IAW AARD 51-00-05-1.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 80,716 hrs · 38,012 cycles

INTERGRANULAR CORROSION FROM STATIONS 1062 TO 1063, RT CUSP. REPLACED CUSP SHEET IAW SRM53-05-00 FIGURE 131A-23.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 80,716 hrs · 38,012 cycles

CORROSION AT FRAME STATION 1155 & LONGERON 26R. INSTALLED DOUBLER IAW EA MD80-53-031966.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 80,716 hrs · 38,012 cycles

CORROSION AT STATION 1155 T-CLIP AT DOOR BEAM. REPLACED T-CLIP IAW AARD 51-00-05-1.

Part: TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 80,716 hrs · 38,012 cycles

CORROSION ON TIE DOWN TRACK FROM STATIONS 1117 TO 1212. SPLICE REPAIRED IAW SRM 53-05-00 FIGURE 4G.

Part: SUPPORT — CRACKED (CARGO BAY) · airframe 80,716 hrs · 38,012 cycles

TIE DOWN TRACK SUPPORT AT STATION 1151 BETWEEN LONGERONS 30 & 29 RT CRACKED. REPLACED SUPPORT IAW AARD 51-00-05-1.

Part: DOME NUT — STRIPPED (FUSELAGE) · airframe 80,716 hrs · 38,012 cycles

LT NACELLE LIGHT HAS A BAD DOMENUT AT ABOUT 7 O"CLOCK POSITION & STATION 1186 ABOVE LONGERON 17 LT. REPLACED DOMENUTS & INSTALLED ON FABRICATED STRAP IAW SRM 53-05-00 FIG 124 & AARD 51-00-00-07.

Part: SPLICE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 80,716 hrs · 38,012 cycles

TIE DOWN TRACK "SPLICE" CORRODED FROM STATIONS 1212 TO 1220. REPLACED TRACK IAW AARD 51-00-05-1.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 80,716 hrs · 38,012 cycles

CORROSION ON UPPER OTBD FLANGE OF NR 1 SEAT TRACK AT STATION 1250. INSTALLED NR 1 SEAT TRACK FLANGE STRAP AT OTBD STATION 1250 IAW AARD 53-20-00-13.

Part: FITTING — CRACKED (LT WING) · airframe 80,716 hrs · 38,012 cycles

LT WING HAS A CRACK IN OTBD RADIUS ON FWD SPAR PULLEY FITTING INBD OF NR 8 SLAT TRACK. INSTALLED NEW FWD SPAR PULLEY FITTING IAW SRM 51-30-05, SRM 51-60-00 & SRM 51-10-04.

Part: FITTING — CRACKED (FUSELAGE) · airframe 80,716 hrs · 38,012 cycles

LT LAVATORY, STATION 1338 & LONGERON 14 LT, LONGERON END FITTING CRACKED. INSTALLED NEW STRINGER END CAP FITTING AT STATION 1338 & LONGERON 14 LT IAW AARD 51-00-05-1.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 80,716 hrs · 38,012 cycles

CORROSION ON CUSP ANGLE FROM STATIONS 830-840. INSTALLED CUSP ANGLE FILLER & DOUBLER IAW AARD 53-20-00-16.

Part: SKIN — DAMAGED (RUDDER) · airframe 80,716 hrs · 38,012 cycles

SMALL PUNCTURE ON UPPER RT LE SIDE OF RUDDER. ACCOMPLISHED REPAIR IAW SRM 51-70-01A, WET LAYUP.

Part: MEMBRANE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 80,716 hrs · 38,012 cycles

CORROSION ON SUBFLOOR DOUBLER FROM STATIONS 200 TO 204 RT. INSTALLED SUBFLOOR DOUBLER FROM STATIONS 200 TO 207 RT.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 80,716 hrs · 38,012 cycles

INTERGRANULAR CORROSION FROM STATIONS 1165 TO 1166 ON RT CUSP. INSTALLED CUSP DOUBLER IAW AARD 53-20-00-16 & SRM 51-30-05.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 80,716 hrs · 38,012 cycles

INTERGRANULAR CORROSION FROM STATIONS 1185 TO 1186 ON RT CUSP. INSTALLED REPAIR DOUBLER IAW AARD 53-20-00-16.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 80,716 hrs · 38,012 cycles

SEVERAL AREAS OF CORROSION ON SEAT TRACK 6 FROM STATIONS 200 TO 385. REPLACED NR 6 SEAT TRACK FROM STATIONS 200 TO 455 IAW SRM 53-05-00 FIGURE 4.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 80,716 hrs · 38,012 cycles

RT CUSP CORRODED FROM STATIONS 503 TO 598. REPLACED RT CUSP SHEET IAW AARD 51-00-05-1.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 80,716 hrs · 38,012 cycles

CRACK IN RT CUSP AT STATION 259 UNDER NR 6 SEAT TRACK. INSTALLED DOUBLER IAW AARD 53-20-00-16.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 80,716 hrs · 38,012 cycles

LONGERON 4L CRACKED AT STATION 207. INSTALLED LONGERON SPLICE REPAIR FROM STATION 168LH TO STATION 228LH

Part: PAN — CRACKED (FUSELAGE) · airframe 80,716 hrs · 38,012 cycles

LT WINDOW PAN CRACKED AT TOP AFT CORNER BS 1079. INSTALLED DOUBLER IAW AARD 53-10-00-25.

Part: PAN — CRACKED (FUSELAGE) · airframe 80,716 hrs · 38,012 cycles

LT WINDOW PAN CRACKED AT TOP AFT CORNER BS 1060. INSTALLED DOUBLER IAW AARD 53-10-00-25.

Part: PAN — CRACKED (FUSELAGE) · airframe 80,716 hrs · 38,012 cycles

LT WINDOW PAN CRACKED AT TOP FWD CORNER, BS 1022. INSTALLED DOUBLER IAW AARD 51-10-00-25.

Part: PAN — CRACKED (FUSELAGE) · airframe 80,716 hrs · 38,012 cycles

RT WINDOW PAN CRACKED TOP AFT CORNER AT BS 1117. INSTALLED REPAIR DOUBLER IAW AARD 53-10-00-25.

Part: PAN — CRACKED (FUSELAGE) · airframe 80,716 hrs · 38,012 cycles

WINDOW PAN IS CRACKED TOP AFT CORNER AT BS 1193. INSTALLED REPAIR DOUBLER IAW AARD 53-10-00-25.

Part: STOP FITTING — CRACKED (FUSELAGE) · airframe 80,716 hrs · 38,012 cycles

FOUND CRACKED DOOR STOP FITTING ON RT SIDE, WL+36 OF VAULT DOOR JAMB. REPLACED DOOR STOP FITTING.

Part: PAN — CRACKED (FUSELAGE) · airframe 80,716 hrs · 38,012 cycles

LT WINDOW PAN CRACKED TOP FORWARD AT BS 846. ACCOMPLISHED REPAIR IAW AARD 53-10-00-25.

Part: PAN — CRACKED (FUSELAGE) · airframe 80,716 hrs · 38,012 cycles

RT WINDOW PAN IS CRACKED AT TOP AFT AT BS 1079. INSTALLED REPAIR DOUBLER.

Part: PAN — CRACKED (FUSELAGE) · airframe 80,716 hrs · 38,012 cycles

LT WINDOW PAN IS CRACKED AT TOP FWD AT BS 846. INSTALLED REPAIR ANGLE IAW AARD 53-10-00-25.

Part: PAN — CRACKED (FUSELAGE) · airframe 80,716 hrs · 38,012 cycles

RT WINDOW PAN IS CRACKED AT TOP AFT CORNER AT BS 1098. INSTALLED REPAIR ANGLE DOUBLER IAW AARD 53-10-00-25.

Part: PAN — CRACKED (FUSELAGE) · airframe 80,716 hrs · 38,012 cycles

RT WINDOW PAN IS CRACKED AT LOWER FWD CORNER AT BS 1155. INSTALLED DOUBLER IAW AARD 53-10-00-25.

Part: RIB — CRACKED (LE SLAT) · airframe 80,716 hrs · 38,012 cycles

NR 5 SLAT, LT RIB NR 15 SHOWS CRACK INDICATION. INSTALLED NEW ATTACH FITTING IAW AARD 51-00-05.

Part: RIB — CRACKED (LE SLAT) · airframe 80,716 hrs · 38,012 cycles

LT NR 14 SLAT RIB SHOWS A CRACK INDICATION. INSTALLED NEW ATTACH FITTING IAW AARD 51-00-05-1 REPAIR 1.

Part: PAN — CRACKED (FUSELAGE) · airframe 80,716 hrs · 38,012 cycles

RT WINDOW PAN IS CRACKED AT LOWER FWD CORNER AT BS 1136. ACCOMPLISHED REPAIR IAW AARD 53-10-00-25.

Part: SMOKE DETECTOR — FAULTY (CARGO BAY) · airframe 78,582 hrs · 36,859 cycles

BNA INFLIGHT PIT-DFW CREW REPORTED FORWARD CARGO FIRE DETECTION WARNING INDICATION. DISCHARGED EXTINGUISHERS PER QRH PROCEDURES. EMERGENCY DECLARED FLIGHT DIVERTED BNA LANDED WITHOUT INCIDENT. CFR INVESTIGATION UPON LANDING HAD NO EVIDENCE OF FIRE. AIRCRAFT REMOVED FROM SERVICE. REPLACED FAULTY B1 AND B2 SMOKE DETECTORS AND NUMBERS 1 AND 2 CARGO FIRE BOTTLES. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,023 hrs · 36,073 cycles

FUSELAGE SKIN CRACKED AT CANT FRAME 1474, RIGHT SIDE, AFT OF ELEVATOR ACCESS DOOR. STOP DRILLED CRACK AND INSTALLED DOUBLER PER SRM 53-01-00.

Part: VALVE — INOPERATIVE (AC BAY) · airframe 75,391 hrs · 35,283 cycles

LAS - INFLIGHT RNO-DFW. CREW REPORTED LEFT AND RIGHT PACKS FAILED INFLIGHT. AT APPROXIMATELY 15000 FEET ALTITUDE, RIGHT PACK RESTORED NORMAL PRESSURIZATION TO LANDING. EMERGENCY DECLARED FLIGHT DIVERTED LAS LANDED WITHOUT INCIDENT. REPLACED LEFT AND RIGHT PRESSURE REGULATING VALVES AND FLOW CONTROL VALVES. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: STIFFENER — OUT OF POSITION (COCKPIT) · airframe 71,112 hrs · 33,163 cycles

DFW - ON APPROACH GEAR HANDLE STUCK IN *UP* POSITION. HANDLE WOULD NOT *PULL OUT* NO HANDLE MOVEMENT AT ALL AVAILABLE. WENT AROUND. STARTED CHECKLIST AFTER STABLE AT 4000 FEET AND CHECKED HANDLE ONE MORE TIME AND GEAR HANDLE AND EXTENSION WERE NORMAL. NO FAULTS NOTED. EMERGENCY DECLARED LANDED DFW WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND GEAR LINKAGE BEHIND CENTER DASH RUBBING ON STIFFENER. REPOSITIONED STIFFENER. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: BATTERY PACK — NOT SEATED (CABIN) · airframe 69,598 hrs · 32,467 cycles

FOUND TAIL CONE EMERGENCY LIGHTS OUT. RESEATED BATTERY PACK AT LEFT AFT LAVATORY.

Part: LIGHT — WRONG PART (CABIN) · airframe 69,598 hrs · 32,467 cycles

EMERGENCY LIGHTS ABOVE LEFT NUMBER ONE DOOR AND GALLEY CEILING INOPERATIVE. FOUND WRONG BULBS INSTALLED. REMOVED BULBS AND INSTALLED CORRECT BULBS, OPS CHECK.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 69,278 hrs · 32,325 cycles

BATTERY PACK FAILED OPERATIONAL CHECK. REPLACED BATTERY PACK.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 69,000 hrs · 32,198 cycles

CORROSION ON LEFT TIE DOWN TRACK, AFT CARGO STATION 1231-1322. REPLACED TIE DOWN TRACK UNDER SRM 51-30-01.

Part: LONGERON — CORRODED (FUSELAGE) · corrosion level 2 · airframe 69,000 hrs · 32,198 cycles

LONGERON 29R HAS CORROSION OUTBOARD SIDE OF AFT END STATION 1334. REMOVED CORRODED SECTION AND INSTALLED LONGERON SPLICE UNDER SRM 53-02.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 69,000 hrs · 32,198 cycles

CORROSION ON UPPER AND LOWER SIDE OF AFT LOWER FLANGE AT FRAME 1309. CUT OUT CORRODED FRAME SECTION STATION 1309 L26L-L26R AND INSTALLED FRAME SPLICE UNDER SRM 53-03-00 FIGURE 2A.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 69,000 hrs · 32,198 cycles

CORROSION ON RIGHT TIE DOWN TRACK, AFT CARGO STATION 1212-1309. REPLACED TIE DOWN TRACK STATION 1212-1309 UNDER SRM 53-05-00.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,992 hrs · 32,192 cycles

LEFT INTERCOSTAL UNDER LEFT TIE DOWN TRACK CORRODED STATION 1309 - 1322 L28L-L27L. REPLACED INTERCOSTAL UNDER SRM 51-30-5 AND 51-30-2.

Part: SHEAR TIE — DAMAGED (FUSELAGE) · airframe 68,992 hrs · 32,194 cycles

SUPPORT ANGLE AND SHEAR TIE DRILLED INCORRECTLY AT STATION 1250 LONGERON 28R. REPAIRED FRAME UNDER SRM 53-03 FIGURE 5. REPAIRED SHEAR TIE UNDER EA MD80-53-006927. REPLACED SUPPORT ANGLE UNDER SRM 51-30-5.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,992 hrs · 32,192 cycles

CORROSION ON DOOR CUTOUT BEAM WEB STATION 1206-1212. REPLACED WEB PER BOEING DRAWING 5936442 AND SRM 51-60-00.

Part: STRAP — CORRODED (CARGO BAY) · corrosion level 2 · airframe 68,992 hrs · 32,192 cycles

STRAP CORRODED IN AFT CARGO AT L28R STATION 1212. REMOVED CORROSION AND INSTALLED DOUBLER PER EA MD 80-53-006855.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 68,992 hrs · 32,192 cycles

HOLE DRILLED THROUGH FUSELAGE SKIN ABOVE LEFT PYLON ON STUB WING ABOVE UPPER ATTACH ANGLE STATION 1464. INSTALLED REPAIR DOUBLER PER AARD 53-30-00-02.

Part: CASTING — CRACKED (SPOILER) · airframe 68,992 hrs · 32,192 cycles

TUL - RIGHT OUTBOARD FLIGHT SPOILER PANEL CENTER HINGE CASTING IS CRACKED AT INBOARD RADIUS. REPLACED FLIGHT SPOILER.

Part: SKIN — DENTED (FUSELAGE) · airframe 68,992 hrs · 32,192 cycles

DENT IN FUSELAGE AT STATION 218 AND JUST ABOVE LONGERON 19L. DENT COLD WORKED AND DYE CHECKED. INSTALLED DOUBLER PER AARD 53-30-00-9.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 68,992 hrs · 32,192 cycles

LEFT STUB WING TO FUSE TOP ANGLE AFT END CRACKED STATION 1446. STOP DRILLED CRACKS AND INSTALLED DOUBLER PER AARD 54-20-00-1.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,992 hrs · 32,192 cycles

TUL - CORROSION ON INTERCOSTAL LOWER ATTACH ANGLE STATION 1212-1220 BETWEEN L30 AND L29R. REPLACED LOWER ATTACH ANGLE UNDER SRM 51-00-00-12.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,992 hrs · 32,192 cycles

TUL - CORROSION UPPER AND LOWER SIDE OF AFT LOWER FLANGE AT FRAME 1309, LONG 27L-27R. REMOVED CORRODED SECTION OF FRAME AND INSTALLED FRAME SPLICE REPAIR PER SRM 53-03-00 FIGURE A SHEET 1.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 68,992 hrs · 32,192 cycles

DAMAGE TO FUSELAGE SKIN RIGHT SIDE BETWEEN L22R AND L23R STATION 218. INSTALLED DOUBLER PER AARD 53-30-00-9.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,992 hrs · 32,192 cycles

CORROSION FOUND UNDER MID CARGO DRAIN AT STATION 655 BETWEEN L29R-L30. CUT OUT BLENDED AREA AND DYE CHECKED, NO CRACKS FOUND. INSTALLED DOUBLER, FILLER, AND NEW DRAIN COVER UNDER SRM 53-04 FIGURE 38 SHEET 23 VIEW H.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,992 hrs · 32,192 cycles

HEAVY CARGO/AFT CORROSION ON DOOR CUTOUT BEAM HORIZONTAL LEG OUTBOARD EDGE STATION 1155 TO STATION 1212. INSTALLED DOOR BEAM DOUBLER PER AARD 53-10-00-3.

Part: LONGERON — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,992 hrs · 32,192 cycles

LONGERON 29 CORRODED BETWEEN STATION 1285-1288. CUT OUT CORRODED SECTION OF L29 BETWEEN STATION 1277-1295 AND INSTALLED NEW LONGERON EXTRUSION AND REPAIR SPLICE PER SRM 53-02-00 FIG 18 AND AARD 53-00-00-5.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,992 hrs · 32,192 cycles

CORROSION ON AFT SIDE OF DOUBLER / STIFFENER (PLOW ANGLE) AT STATION 1338 L29R. REPLACED PLOW ANGLE PER SRM 51-30-05.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 68,992 hrs · 32,192 cycles

INTERCOSTAL CRACKED AT AFT END BELOW CABIN FLOOR AT CENTERLINE STATION 1309. REPLACED INTERCOSTAL PER SRM 51-30-5.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,992 hrs · 32,192 cycles

CORROSION UNDER PLASTIC DRAIN COVER ON FUSELAGE SKIN STATION 731 BETWEEN L29R AND L30. REMOVED CORROSION PER SRM 51-10-03 AND REPAIRED PER AARD 53-30-00-9.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,992 hrs · 32,192 cycles

CORROSION ON AFT SIDE OF FRAME 1250 L27L-L28R. REMOVED CORROSION AND INSTALLED J-ANGLE. REPAIRED UNDER AARD 53-10-00-14.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,992 hrs · 32,192 cycles

CORROSION AFT SIDE OF FRAME LONGERON 28L-27R STATION 1271. INSTALLED REPAIR DOUBLER PER AARD 53-10-00-14.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,992 hrs · 32,192 cycles

CORROSION ON CUSP BELOW FORWARD GIRT BAR FITTING AT AFT SERVICE DOOR. INSTALLED REPAIR DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,992 hrs · 32,192 cycles

CORROSION UNDER AFT GIRT BAR FITTING AT AFT SERVICE DOOR. INSTALLED REPAIR DOUBLER PER AARD 53-20-00-16.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 68,992 hrs · 32,192 cycles

CRACK IN LONGERON 3L AT STATION 160. INSTALLED SPLICE REPAIR AT L3 STATION 167 AND NEW SECTION OF LONGERON FROM STATION 150-167 PER SRM 53-20-00.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 68,992 hrs · 32,192 cycles

AFT ACCESSORY SHEAR TIE CRACKED AFT SIDE OF 1451 AFT OF LONGERON 2L. REMOVED AND REPLACED SHEAR TIE PER SRP 51-30.

Part: MOUNT — CORRODED (GALLEY) · corrosion level 2 · airframe 68,992 hrs · 32,192 cycles

CORROSION ON GALLEY TIE DOWN FITTING INBOARD OF NUMBER FOUR SEAT TRACK. INSTALLED NEW GALLEY MOUNT PER SRM 51-30.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,992 hrs · 32,192 cycles

RIGHT CUSP HAS CORROSION AT STATION 237. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — DAMAGED (FUSELAGE) · airframe 68,992 hrs · 32,192 cycles

TOOLING DAMAGE IN CUSP BELOW NUMBER ONE SEAT TRACK. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,992 hrs · 32,192 cycles

CORROSION ON LOWER AFT FLANGE OF FRAME 1231 28L-27R. REPAIRED IN ACCORDANCE WITH AARD 53-10-00-14 FIG 1.

Part: WEB — CRACKED (FUSELAGE) · airframe 68,992 hrs · 32,192 cycles

SUBFLOOR AT STATION 214 CRACKED AROUND FASTENER FOR NUMBER SIX SEAT TRACK AT GALLEY TIE DOWN STATION 214. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 68,992 hrs · 32,192 cycles

LEFT CUSP SHEET CRACKED BETWEEN STATION 218-237. REPAIRED UNDER AARD 53-20-00-16.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 68,992 hrs · 32,192 cycles

HORSE COLLAR HAS ELONGATED FASTENER HOLE. REPLACED HORSE COLLAR AT STATION 845 LEFT HAND PER SRM 51-30-35.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 68,992 hrs · 32,192 cycles

CRACKED DOOR JAMB WEBBING AFT TAB. INSTALLED DOUBLER ON DOOR JAMB WEBBING PER AARD 53-10-00-11.

Part: WEB — GOUGED (FUSELAGE) · airframe 68,992 hrs · 32,192 cycles

GOUGE IN SUB FLOOR AT STATION 165 TWELVE INCHES LEFT OF CENTER. CUT OUT DAMAGED AREA AND INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 68,992 hrs · 32,192 cycles

CABIN FORWARD ENTRY JAMB CRACKED TAB ON DOOR JAMB WEB STATION 208 AT LONGERON 15L. INSTALLED DOUBLER PER AARD 53-10-00-11.

Part: WEB — GOUGED (FUSELAGE) · airframe 68,992 hrs · 32,192 cycles

GOUGES IN SUB FLOOR BETWEEN 5 AND 6 SEAT TRACK. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: DOUBLER — DAMAGED (FUSELAGE) · airframe 68,992 hrs · 32,192 cycles

LEFT HAND PRIMARY STATIC PORT INTERNAL DOUBLER DAMAGED AT HOLE FOR PRIMARY STATIC PORT PLATE. FABRICATED AND REPLACED DOUBLER PER SRM 51-01 AND 51-30.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 68,476 hrs

LGA - CEILING EMERGENCY LIGHTS FROM ROWS 22 TO 26 INOPERATIVE. REPLACED BATTERY PACK AT B5-104.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT) · airframe 66,889 hrs

SFO - EMERGENCY LIGHT AT SEAT 18D INOPERATIVE. REPINNED CONNECTOR AT SEAT 18D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 66,818 hrs

LGA - EMERGENCY LIGHT OVER RIGHT AFT EMERGENCY EXIT INOPERATIVE. REPLACED BATTERY PACK AT B5105. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BULB — BROKEN (EMERGENCY LIGHTS)

BOS - EMERGENCY LIGHT LAMP AT ROW 12AB SIDEWALL BROKEN BY PASSENGER. RELAMPED EMERGENCY LIGHT AT ROW 12AB SIDEWALL. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: APU — INOPERATIVE (APU BAY)

TPA - SMOKE AND ODOR IN CABIN. RETURNED TPA AND LANDED WITHOUT INCIDENT. PERFORMED SPECIAL ITEMS CARD 21 92 12 PACK BURN OUT AND OVERWEIGHT LANDING. REPLACED SEPARATOR BAG AND ACCOMPLISHED FUNCTIONAL CHECK FLIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

DFW FORWARD GALLEY OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR FORWARD GALLEY OVERHEAD EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

DFW - FORWARD GALLEY CEILING EMERGENCY LIGHT DIM. REMOVED AND REPLACED BATTERY PACK R5-23 IN FORWARD DROP DOWN CEILING PANEL. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SKIN — CRACKED (FUSELAGE)

TUL - FOUND CRACK ON SKIN STATION 1380 L14R. STOP DRILL, CRACK AND INSTALLED DOUBLER PER SRM 53-01 FIG 2 SHEET 3. (M)

Part: SKIN — CRACKED (FUSELAGE)

TUL - FOUND CRACK ON SKIN STATION 1380 L14L. STOP DRILLED CRACK TO APPLIED DOUBLER TO AREA SPECIFIED PER SRM 53-01 FIG 2. (M)

Part: BOLT — LOOSE (APU)

BOS - FLT 509 - EN ROUTE BOS-ORD, AFTER TAKEOFF THERE WAS SMOKE IN THE CABIN, THEN IN COCKPIT. DECLARED EMERGENCY. SMOKE STAYED. RETURNED BOS AND LANDED WITHOUT INCIDENT. TIGHTENED BOLT ON APU MASTER CHIP DETECTOR. PERFORMED COMPLETE PACK BURN. REPLACED COALESCER BAGS AND ACCOMPLISHED PACK BURN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BELTFRAME — DENTED (FUSELAGE)

TUL - FOUND BELTFRAME DENTED BETWEEN L26L AND L27L STATION 1250. INSTALLED DOUBLER PER AARD 53-10-00-17. (M)

Part: CARGO TRACK — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON TIE DOWN TRACK. REPLACED TIE DOWN TRACK W/NEW TRACK PER SRM 53-01. (M)

Part: BEAM — CORRODED (CARGO DOOR)

TUL - FOUND CORROSION ON VERTICAL AND HORIZONTAL LEGS OF DOOR BEAM FROM STATION 1155-1212, SEVERAL AREAS. INSTALLED DOUBLER AND FASTENERS, TREATED AND PRIMED AREAS PER ESO 80559 DATED 9/28/01. (M)

Part: CARGO TRACK — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON RIGHT TIE DOWN TRACK AT 1136 AND 1142. REMOVED OLD TRACK AND INSTALLED NEW TIE DOWN TRACK SRM 51-01. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND STATION 218 RBL 58 CORRODED ON CUSP MEMBRANE AND STATION 230 RBL 58 CORROSION ON CUSP MEMBRANE. REMOVED AND REPLACED CUSP STATION 218 TO 237 PER SRM 51-01. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON SEAT TRACK FROM BS 234 TO BS 237. INSTALLED TRACK SPLICE ON NR 5 SEAT TRACK STATION 200 THROUGH 265 PER SRM 53-05-00. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL - FOUND SEAT TRACK NR 5 CORRODED STATION 200. INSTALLED TRACK SPLICE ON NR 5 SEAT TRACK STATION 200-265 PER SRM 53-05-00. (M)

Part: FRAME — WORN (FUSELAGE)

TUL - WORN AREA ON FRAME STATION 1418, LONGERON 7L TO 8L. INSTALLED DOUBLER PER AARD 53-10-00-14. (M)

Part: STOP FITTING — CRACKED (FUSELAGE)

TUL - FOUND LEFT CENTER VAULT DOOR CUTOUT STOP SUPPORT CASTING HAS VISUAL INDICATION OF CRACK OF BOTTOM OF PAD BOLT. INSTALLED SERVICEABLE CASTING SRM 51-01. (M)

Part: LONGERON — CRACKED (FUSELAGE)

TUL - FOUND CRACK IN LONGERON L4 AT STATION 160. REMOVED DAMAGED SECTION OF LONGERON AND REPAIRED PER SRM 53-02 PAGE 48. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND LEFT CUSP CORROSION AT STATION 708. CUT OUT CORRODED AREA PER SRM 51-10-3. INSTALLED DOUBLER REPAIR PER SRM 53-01 FIG 4 SH 3. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND LEFT CUSP CORROSION AT STATION 725. REMOVED CORROSION BY DRILLING .25 INCH HOLE, PLUGGED HOLE WITH FASTENER PER SRM 53-01 FIG 1, SH 2. (M)

Part: SKIN — DENTED (FUSELAGE)

TUL - FOUND DENT ON FUSELAGE UNDER RIGHT STATION 1305 BETWEEN LONGERON 18R AND 19R ADL NR 4390015. INSTALLED DOUBLER PER SRM 53-04 FIG 38. (M)

Part: SEAT TRACK — WORN (FUSELAGE)

TUL - FOUND WORN AREA ON NR 6 SEAT TRACK FROM BS 702-705. INSTALLED SEAT TRACK PLUG PER SRM 53-20-00-10. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND DIAPHRAGM WEB BELOW G2 TIE DOWN CORRODED STATION 218 RBL 13 INCHES. CUT OUT CORRODED AREA AND INSTALLED DOUBLER REPAIR PER AARD 53-00-00-02. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON NR 6 SEAT TRACK FROM STATION 826 TO 830. REMOVED DAMAGED AREA AND INSTALLED PLUG PER AARD 53-20-00-10. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON NR 6 SEAT TRACK. INSTALLED SEAT TRACK PLUG, SRM 53-03 FIG 41. (M)

Part: FITTING — CORRODED (FUSELAGE)

TUL - - FOUND STATION 215 G2 FORWARD TIE DOWN CORRODED. REPLACED CORRODED TIE DOWN BRACKET WITH NEW BRACKET AND HARDWARE SRM 51-01. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON UPPER SURFACE OF NR 3 SEAT TRACK FROM STATION 1301 TO 1305 AT AFT GALLEY MOUNT. REMOVED CORROSION AND INSTALLED PLUG REPAIR IN TRACK PER SRM 53-05 FIG 4. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT IN AFT CABIN AND STAIRWELL AREA INOPERATIVE. REPLACED EMERGENCY EXIT BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: APU — LEAKING (APU BAY)

ORD - FLT 1229 - AFTER TAKEOFF ORD, FLIGHT ATTENDANTS REPORTED SMOKE IN THE CABIN. RETURNED TO ORD AND LANDED OVERWEIGHT WITHOUT INCIDENT. FOUND APU LEAKING OIL FROM THE MASTER CHIP DETECTOR REPLACED APU ASSEMBLY AND LEAKED CHECKED GOOD. ACCOMPLISHED PACK BURN, NO SMELL NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: ENGINE — FAILED (RIGHT)

PDX - FLT 1812 - ON TAKEOFF, EXPERIENCED COMPRESSOR STALL ON RIGHT ENGINE JUST AT ROTATION. ENGINE WAS SURGING AND VIBRATING. TOWER AND CABIN REPORTED FLAME OT OF ENGINE. STABILIZED WHEN THROTTLE WAS RETARDED. RETURNED AND LANDED PDX WITHOUT INCIDENT. REPLACED RIGHT ENGINE. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: CABLE — LOOSE (TAIL CONE)

ORD - FLT 1427 - TAIL CONE LIGHT ILLUMINATED AFTER LANDING ORD. RESECURED LOCKING CABLE AND INSPECTED INTEGRITY OF ENTIRE TAIL CONE RELEASE SYSTEM. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: APU — BYPASSING OIL (APU BAY)

ORD - FLT 390 - AFTER TAKEOFF ORD DURING CLIMB-OUT, SMOKE NOTED IN CABIN AND COCKPIT. ACCOMPLISHED ABNORMAL PROCEDURES AND AIRCRAFT RETURNED TO ORD, LANDING WITHOUT INCIDENT. REPLACED APU DUE TO APU BYPASSING OIL. SUBSEQUENTLY, AIRCRAFT DEPARTED ORD AND PROBLEM REPEATED. ACCOMPLISHED ABNORMAL PROCEDURES AND AIRCRAFT RETURNED TO ORD. REPLACED LEFT AND RIGHT COALESCER BAGS AND ACCOMPLISHED PACK BURNOUT PROCEDURE. SYSTEM GROUND CHECKED NORMAL OPERATION. ACCOMPLISHED FUNCTIONAL CHECK FLIGHT WITH NO SMOKE NOTED. SYSTEM OPERATIONAL CHECKED NORMAL. (M)

Part: TEMP SENSOR — DEFECTIVE (TAIL COMPT)

DFW - FLT 2016 - ON ROTATION OUT OF DFW, THE TAIL COMPARTMENT HIGH TEMPERATURE LIGHT ILLUMINATED. RETURNED TO LAND DFW AND LIGHT EXTINGUISHED WITH POWER REDUCTION. LIGHT ILLUMINATED AGAIN WITH POWER INCREASE. LANDED DFW WITHOUT INCIDENT AND NORMAL WEIGHT. REPLACED BOTH TAIL COMPARTMENT HIGH TEMPERATURE SENSOR AND ACCOMPLISHED DUCT LEAK CHECK DURING ENGINE RUN UP AT HIGH POWER. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)