N564AA

Part: SKIN — CRACKED (FUSELAGE) · airframe 88,524 hrs · 40,216 cycles

CRACK IN FUSELAGE SKIN AT STATION 1437, LONGERON 3L. INSTALLED DOUBLER REPAIR IAW SRM 53-04-00 FIGURE 27.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 88,524 hrs · 40,216 cycles

CORROSION ON CASTING AFT SIDE OF 1155 FRAME AT INBD DOOR CUT OUT OF AFT CARGO DOOR. REMOVED CORROSION & FOUND CRACK IN ANGLE. R & R ANGLE IAW AARD 51-00-05-1, DWG EDK1851 & DWG 5936469.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 88,088 hrs · 39,949 cycles

EMERGENCY LIGHTS WILL NOT TEST AT ZONE AB5-1, AB5-3 & AB5-4. R & R BATTERY PACK AT ZONE AB5-4. SEE ALSO AALA20150803006 & AALA20150803006.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 88,088 hrs · 39,949 cycles

EMERGENCY LIGHTS WILL NOT TEST AT ZONE AB5-1, AB5-3 & AB5-4. R & R BATTERY PACK AT ZONE AB5-3. SEE ALSO AALA20150801003 & AALA20150803006.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 88,088 hrs · 39,949 cycles

EMERGENCY LIGHTS WILL NOT TEST AT ZONE AB5-1, AB5-3 & AB5-4. R & R BATTERY PACK AT ZONE AB5-1. SEE ALSO AALA20150801003 & AALA20150803007.

Part: LOCK SENSOR — FAULTY (NLG) · airframe 87,976 hrs · 39,890 cycles

AIR INTERRUPT, EMER DECLARED, LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. DURING CLIMB WITH GEAR UP, NLG SHOWED RED UNSAFE. ON GEAR EXTENSION MLG SHOWED GREEN & NLG SHOWED RED UNSAFE. R & R NOSE GEAR LOCKED SENSOR D1-32 IAW AMM 32-60-05. PERFORMED NLG SWING & PERFORMED PROXIMITY BOX TEST IAW AMM 32-60-05. SYS CHECKED NORMAL.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 84,508 hrs · 38,074 cycles

MID CARGO DOOR STOP PAD CASTING CRACKED. R & R STOP PAD CASTING IAW AARD 51-00-05-1.

Part: RIB — CRACKED (LT WING) · airframe 84,480 hrs · 38,058 cycles

LEFT HAND WING NR 4 SLAT TRACK LE INBD SUPPORT RIB CRACKED. REMOVED CRACK & INSTALLED WASHER SHIM & DOUBLER IAW EA MD80-57-034407.

Part: RIB — CRACKED (RT WING) · airframe 84,480 hrs · 38,058 cycles

RIGHT HAND WING NR 4 SLAT TRACK LE INBD SUPPORT RIB CRACKED. REMOVED CRACK & INSTALLED WASHER SHIM & DOUBLER IAW EA MD80-57-034407.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 83,446 hrs · 37,541 cycles

EMERGENCY LIGHTS AT FWD AREA NEAR CLASS DIVIDER IN CEILING ARE INOPERATIVE. REPLACED EMERGENCY LIGHT BATTERY PACK AT SEAT ROW 8. OPERATIONS CHECKED NORMAL.

Part: SELECTOR PANEL — FAULTY (CABIN PRESSURE) · airframe 83,444 hrs · 37,540 cycles

MSY LOSS OF CABIN PRESSURE. CABIN O2 MASKS WERE DEPLOYED. EMERGENCY DECLARED FLIGHT LANDED MSY WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. AIRCRAFT FERRIED TO TULE FOR FURTHER MAINTENANCE. REPLACED CABIN PRESSURE CONTROLLER SELECTOR PANEL, SYSTEM GROUND CHECKED NORMAL OPERATION CLOSED.

Part: SLIDE — DAMAGED (SERVICE DOOR) · airframe 83,053 hrs · 37,324 cycles

DURING PREFLIGHT, FOUND GIRT BAR AT SERVICE DOOR OUT & PINS EXPOSED. FOUND ALL PINS PULLED OUT OF SLIDE & GIRT BAR HANGERS BENT DOWN. REPAIRED HANGERS & REPLACED SLIDE ASSEMBLY.

Part: SKIN — CRACKED (FUSELAGE) · airframe 80,505 hrs · 35,973 cycles

FOUR CRACKS IN THE FUSELAGE SKIN AT LONGERON 22 FROM STATIONS 160 TO 200. INSTALLED DOUBLER PER EA MD80-53-009386.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 80,505 hrs · 35,973 cycles

SEVERAL CRACKS IN RIGHT CUSP SHEET BETWEEN STATIONS 1287 TO 1309. INSTALLED NEW CUSP SHEET FROM STATIONNS 1250 TO 1309 RIGHT PER AARD 51-00-05-1.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 80,505 hrs · 35,973 cycles

LEFT CUSP CORRODED AT STATION 256 OUTBOARD OF NUMBER 1 SEAT TRACK. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: SKIN — CRACKED (FUSELAGE) · airframe 80,505 hrs · 35,973 cycles

CRACK IN SKIN AT STATION 1309 ABOVE LONGERON 7 LEFT. INSTALLED DOUBLER PER SRM 53-04-03 FIGURE 9.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 80,505 hrs · 35,973 cycles

NUT PLATE HOLES CORRODED ON DOOR JAMB WEB UNDER AFT RIGHT TIE-DOWN TRACK BETWEEN STATIONS 1212 TO 1215. INSTALLED NEW WEB AS PER AARD 51-00-5-1.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 80,505 hrs · 35,973 cycles

STATION 160 LONGERON 2 LEFT IS CRACKED ON BOTH HAT SECTIONS. INSTALLED SPLICE REPAIR PER SRM 53-02-00 FIGURE 18.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 80,505 hrs · 35,973 cycles

WORN SPOTS ON ANGLE AT LOWER AFT SIDE OF RIGHT STATION 1309 BULKHEAD. INSTALLED ANGLE SPLICE REPAIR PER SRM 51-70-05 FIGURE 1.

Part: MEMBRANE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 80,505 hrs · 35,973 cycles

STATION 201 LEFT BUTTLINE 8, CORRODED ON SUBFLOOR. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: MEMBRANE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 80,505 hrs · 35,973 cycles

CORROSION ON SUBFLOOR FROM STATIONS 160 TO 200, RIGHT BUTTLINES 44 TO 57. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: TEE FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 80,505 hrs · 35,973 cycles

CORROSION ON CUSP TEE TAB AT RIGHT STATION 200, RIGHT BUTTLINE 55. INSTALLED TITANIUM DOUBLER PER AARD 53-20-00-14.

Part: MEMBRANE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 80,505 hrs · 35,973 cycles

E&E COMPARTMENT HAS CORROSION IN UPPER CEILING WEBBING AT FASTENER FORWARD OF AILERON SERVO UNIT. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 80,505 hrs · 35,973 cycles

STATION 200, LONGERON 4 LEFT IS CRACKED ON BOTH HAT SECTIONS. INSTALLED NEW SECTION OF LONGERON FROM STATIONS 168 TO 228 PER AARD 51-00-05-1.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 80,505 hrs · 35,973 cycles

STATION 201, RIGHT BUTTLINE 55 CORRODED ON SUBFLOOR. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 80,505 hrs · 35,973 cycles

RIGHT CUSP ANGLE CORRODED ON TOP SIDE FROM STATIONS 160 TO 200. INSTALLED DOUBLER PER SRM 53-05-00 FIGURE 55.

Part: FRAME — CRACKED (FUSELAGE) · airframe 80,505 hrs · 35,973 cycles

THE 1485 CANT FRAME CRACKED BELOW AIRSTAIR STAIR ACTUATOR. INSTALLED SPLICE DOUBLER ON 1485 CANT FRAME RIGHT BELOW AIRSTAIR ACTUATOR PER AARD 53-10-00-33.

Part: MEMBRANE — PUNCTURED (FUSELAGE) · airframe 80,505 hrs · 35,973 cycles

PUNCTURE IN FORWARD SUBFLOOR, STATION 198, LEFT BUTTLINE 24. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 80,505 hrs · 35,973 cycles

LEFT CUSP CORRODED AT STATIONS 240 TO 256. INSTALLED DOUBLER REPAIR PER AARD 51-00-05-1.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 80,505 hrs · 35,973 cycles

CABIN LONGERON INBOARD LEG IS CRACKED AT STATION 464, LONGERON 4 LEFT. REMOVED DAMAGE AND COMPLETED INSTALLATION OF LONGERON L-4 AND SPLICES FROM STATIONS 438 TO 477 PER SRM 53-02-00 FIGURE 18.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 80,505 hrs · 35,973 cycles

E AND E COMPARTMENT HAS CORROSION IN UPPER CEILING WEBBING AROUND G1 GALLEY FLOOR SERVICE PAN. INSTALLED DOUBLER ON SUBFLOOR UNDER G1 GALLEY DRAIN PAN PER AARD 53-20-00-16.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 80,505 hrs · 35,973 cycles

SEAT TRACK NUMBER 4 CORROSION BLENDED OUT OF LIMITS AT STATION 879. INSTALLED SEAT TRACK PLUG PER AARD 53-20-00-10.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 80,505 hrs · 35,973 cycles

RIGHT CUSP CRACKED FROM STATIONS 494 TO 496. INSTALLED REPAIR DOUBLER ON RIGHT CUSP PER AARD 53-20-00-16.

Part: CUSP WEB — PUNCTURED (FUSELAGE) · airframe 80,505 hrs · 35,973 cycles

MID CARGO LEFT CUSP HAS PUNCTURE AT STATION 623. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: SKIN — CRACKED (FUSELAGE) · airframe 80,505 hrs · 35,973 cycles

CRACK IN SKIN AT STATION 1309 ABOVE LONGERON 7 LEFT. INSTALLED DOUBLER, FILLER AND FINGERS PER SRM 53-04-03 FIGURE 9 AND SRM 51-01-00 PARAGRAPH 4.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 80,505 hrs · 35,973 cycles

CENTER DOOR STOP SUPPORT BRACKET CRACKED INSIDE LEFT SIDE OF VAULT DOOR JAMB. INSTALLED NEW DOOR STOP MOUNT PER AARD 51-00-05-1.

Part: BATTERY — NOT SEATED (CABIN) · airframe 79,856 hrs · 35,649 cycles

CEILING EMERGENCY LIGHTS FROM ROWS 28 TO 30. RESEATED EMERGENCY BATTERY AT ROW 28. OPS CHECK NORMAL.

Part: BATTERY — NOT SEATED (CABIN) · airframe 79,856 hrs · 35,649 cycles

CEILING EMERGENCY LIGHTS FROM ROWS 12 TO 16 INOPERATIVE. RESEATED EMERGENCY BATTERY AT ROW 15DEF. OPS CHECK NORMAL.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,282 hrs · 32,335 cycles

WHILE ACCOMPLISHING HIGH FREQUENCY EDDY CURRENT INSPECTION OF THE FUSELAGE SKIN BETWEEN STATION 160 AND STATION 200 AT LONGERON 22LEFT CRACKS WERE FOUND. INSTALLED INTERIM REPAIR PER BOEING REWORK DWG SR09530219 REV EO F AND EA MD80-53-009386.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 73,282 hrs · 32,335 cycles

LONGERON 2 FOUND CRACKED AFT OF STATION 1418. REPAIRED PER AARD 53-30-00-2 FIGURE 1 SHEET 1.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 73,282 hrs · 32,335 cycles

LONGERON 20 CRACKED ABOVE INBOARD FLAP ACTUATOR AT STATION 993 RIGHT SIDE. INSTALLED REPAIR ANGLE ON LONGERON 20 STATION 993 PER AARD 53-10-00-18.

Part: O-RING — LEAKING (FUEL SYSTEM) · airframe 72,804 hrs · 32,133 cycles

INFLIGHT LAX TO AUS. FUEL LEAK AT OUTER FUEL PUMP BOOST COVER ON TOP OF RIGHT WING. LANDED PHX WITHOUT INCIDENT. REPLACED UPPER RIGHT COMPENSATOR O-RING.

Part: SLIDE — LOW PRESSURE (SERVICE DOOR) · airframe 72,109 hrs · 31,830 cycles

AFT SERVICE DOOR SLIDE INDICATED ZERO PRESSURE ON THE SLIDE MOUNTED INDICATOR. REPLACED SLIDE.

Part: FUEL CONTROL — INOPERATIVE (LT ENGINE) · airframe 70,111 hrs · 30,971 cycles

ABQ - INFLIGHT DFW-SJC - LEFT ENGINE LOST THROTTLE RESPONSE. CREW SHUT DOWN ENGINE. SINGLE ENGINE TIME 30 MINUTES. EMERGENCY DECLARED LANDED ABQ WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT ENGINE FUEL CONTROL AND FUEL PUMP. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: ENGINE — LEAKING (RIGHT) · airframe 67,827 hrs

COS INFLIGHT T656/02MAY SAN TO ORD - NUMBER TWO ENGINE COMPRESSOR STALLED. HIGH ENGINE GAS TEMPERATURE NOTED. CREW SHUT NUMBER TWO ENGINE DOWN. LANDED COS WITHOUT INCIDENT. SINGLE ENGINE TIME TWENTY FIVE MINUTES. REPLACED NUMBER TWO ENGINE DUE TO OIL QUANTITY LOSS ON 04 MAY AT COS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SLIDE — PARTIAL INFLATE (R1 DOOR)

SFO - RIGHT NUMBER ONE DOOR EMERGENCY SLIDE INADVERTENTLY UNSUCCESSFULLY DEPLOYED WHEN OPEN FROM OUTSIDE BY CATERING PERSONNEL. REPLACED RIGHT NUMBER ONE DOOR EMERGENCY SLIDE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DFW - CEILING EMERGENCY LIGHTS ABOVE ROWS 12 TO 16 AND 22 TO 29 INOPERATIVE. REPLACED BATTERY PACKS FOR CEILING EMERGENCY LIGHTS ABOVE ROWS 12 TO 16 AND 22 TO 29. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CIRCUIT BREAKER — UNSECURE (FUEL BOOST)

ORD INFLIGHT T227/01 CENTER FUEL TANK UNABLE TO TRANSFER FUEL. DIVERTED TO TUL. LANDED WITHOUT INCIDENT. FOUND AFT CENTER TANK BOOST PUMP CIRCUIT BREAKER IN BUT NOT LATCHED. RESET CIRCUIT BREAKER. ACCOMPLISHED OVERWEIGHT INSPECTION. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

DEN - DURING OVERNIGHT MAINTENANCE, EMERGENCY LIGHT WAS INOPERATIVE LEFT SIDE FORWARD OF THE AFT ACCESSORY DOOR. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: OIL SYSTEM — LEAKING (NR 1 ENGINE)

DFW - FLT 528 - AFTER TAKEOFF, CABIN AND COCKPIT STARTED TO FILL WITH SMOKE. RETURNED AND LANDED DFW WITHOUT INCIDENT. REPLACED NR 1 ENGINE DUE OT OIL LEAK AT 13TH STAGE. ACCOMPLISHED LEAK CHECK. ACCOMPLISHED PACK BURN OUT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WEB — CRACKED (FUSELAGE)

TUL - FOUND CRACK FROM LIGHTENING HOLE IN CUSP STATION 228 LEFT SIDE. INSTALLED DOUBLER PER AARD 53-00-00-02 AND SRM 53-01 FIG 4. (M)

Part: SEAT TRACK — DAMAGED (CABIN)

TUL - FOUND NR 4 SEAT TRACK WORN AT STATION 498. REMOVED DAMAGED AREA AND INSTALLED PLUG IN NR 4 SEAT TRACK STATIN 498 PER SRM 53-05 PART 1 FIG 4A SHEET 1/2. (M)

Part: SEAT TRACK — CORRODED (CABIN)

TUL - FOUND CORROSION ON SEAT TRACK NR 1 AT STATION 1208. ACCOMPLISHED PLUG REPAIR ON TRACK PER SRM 53-05 FIG 4A. (M)

Part: SEAT TRACK — CORRODED (CABIN)

TUL - FOUND CORROSION ON SEAT TRACK NR 1 AT STATION 1236. ACCOMPLISHED PLUG REPAIR ON TRACK PER SRM 53-05 FIG 4A. (M)

Part: SEAT TRACK — CORRODED (CABIN)

TUL - FOUND CORROSION ON SEAT TRACK NR 2 AT STATION 1200. REPLACED SEAT TRACK NR 2 STATION 1186-1223. REPLACED PER SRM 51-10. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND CUSP BULGING CORRODED STATION 314. CUT OUT CORRODED SECTION ON LEFT CUSP STATION 14. INSTALLED DOUBLER PER SRM 53-01. (M)

Part: ANGLE — GOUGED (FUSELAGE)

TUL - FOUND TWO GOUGES IN RADIUS OF REPAIR ANGLE ON 1463 CANT FRAME JUST BELOW NR 18L LONGERON. BLENDED GOUGES, NDT CHECKED. INSTALLED DOUBLER PER 53-10-00-15 ON LONGERON 18L. (M)

Part: WIRE — BROKEN (CABIN)

ORD - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT ESCAPE PATH LIGHTS AT SEAT 5E INOPERATIVE. REPAIRED WIRE AT SEAT 5E. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: SENSOR — DEFECTIVE (RT MLG)

ORD - FLT 1063 - EN ROUTE YYZ-ORD, GEAR DOOR OPEN LIGHT ILLUMINATED DURING CLIMB AT APPROX 300 KNOTS. ABNORMAL PROCEDURE WAS FOLLOWED AND RIGHT PUMP PLACED IN HIGH POSITION, LIGHT EXTINGUISHED AND REMAINED OUT FOR REMAINDER OF FLIGHT. LANDED ORD WITHOUT INCIDENT. REPLACED GEAR DOOR SENSOR. ACCOMPLISHED GEAR SWING. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SENSOR — DEFECTIVE (LT MLG)

ORD - FLT 1063 - EN ROUTE YYZ-ORD, DURING CLIMB, THE GEAR DOOR LIGHT ILLUMINATED. FOLLOWED CHECKLIST, TURNED ON RIGHT ENGINE HYDRAULICS AND LIGHT REMAINED OFF FOR REST OF THE FLIGHT. LANDED ORD WITHOUT INCIDENT. REPLACED SENSOR ON LEFT MAIN LANDING GEAR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SENSOR — DAMAGED (RT MLG)

ORD - FLT 2268 - EN ROUTE DFW-ORD, GEAR DOOR OPEN LIGHT FLICKERED AND CAME ON INTERMITTENTLY DURING CLIMB IN LIGHT CHOP. LIGHT CAME ON STEADY AT CRUISE (33,000 FT) HYDRAULIC PUMPS WERE LOW/OFF. ABNORMAL PROCEDURE WAS FOLLOWED AND RIGHT PUMPED PLACED IN HIGH POSITION, LIGHT EXTINGUISHED AND REMAINED OUT FOR REMAINDER OF FLIGHT. LANDED ORD WITHOUT INCIDENT. REPLACED LIGHT MLG DOOR SENSOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (CABIN)

PHX - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS IN FIRST CLASS CABIN WERE INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT STRIP IN FIRST CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SENSOR — DEFECTIVE (LT MLG)

SFO - FLT 1041 - DURING APPROACH SFO, GEAR WAS EXTENDED AND THE LEFT MAIN GEAR INDICATED IT WAS NOT DOWN AND LOCKED. CREW ACCOMPLISHED ALTERNATE GEAR EXTENSION AND LANDED SFO WITHOUT FURTHER INCIDENT. AIRCRAFT GEAR WAS PINNED AND THE AIRCRAFT WAS TOWED TO THE GATE. MAINTENANCE PERFORMED A BITE CHECK OF THE PROXIMITY BOX WITH NO FAULTS NOTED. AS A PRECAUTIONARY, THE LEFT DOWN LOCK SENSOR WAS CHANGED AND THE GEAR OPERATED NORMALLY WHEN CYCLED SEVERAL TIMES. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SEAT TRACK — CORRODED (BS 207)

TUL - NR 2 SEAT TRACK CORROSION STATION 207. SEAT TRACK REPLACED IN AREA, SRM 53-05 FIG 4. (M)

Part: CUSP MEMBRANE — CORRODED (BS 1238)

TUL - LEFT CUSP MEMBRANE HAS CORROSION. INSTALLED DOUBLER ON CUSP MEMBRANE PER SRM 53-01 FIG 4. (M)

Part: CUSP MEMBRANE — CORRODED (BS 1253)

TUL - LEFT CUSP MEMBRANE HAS CORROSION. INSTALLED DOUBLER ON CUSP MEMBRANE PER SRM 53-01 FIG 4. (M)

Part: CUSP MEMBRANE — CORRODED (BS 553)

TUL - LEFT CUSP MEMBRANE HAS CORROSION. INSTALLED DOUBLER ON CUSP MEMBRANE PER SRM 53-04 FIG 4. (M)

Part: AIR DISTRIBUTION — ODOR (CABIN)

DFW - FLT 1593 - DURING DESCENT INTO DFW AT FL 140, BURNING PLASTIC ODOR NOTED IN CABIN WITH NO SMOKE EVIDENT. ODOR DISSIPATED PRIOR TO LANDING AND AIRCRAFT LANDED WITHOUT INCIDENT. PRECAUTIONARY CHECKED ALL INTERIOR LIGHT BALLASTS IN AFT CABIN AREA WITH NO DEFECTS NOTED. PRECAUTIONARY ACCOMPLISHED PACK BURNOUT PROCEDURE. SYSTEMS GROUND CHECKED NORMAL OPERATION WITH NO ODOR NOTED. UNABLE TO DUPLICATE PROBLEM AND AIRCRAFT RETURNED TO SERVICE. (M)

Part: ENGINE — LEAKING OIL (RIGHT)

MIA - FLT 1989 - AFTER T/O MIA, DURING INITIAL CLIMB-OUT, SMOKE NOTED IN COCKPIT AND CABIN. AIRCRAFT RETURNED TO MIA AND LANDED OVERWEIGHT WITHOUT INCIDENT. REPLACED RT ENGINE DUE TO OIL LEAK AT NR 3 BEARING DRAIN BREATHER. ACCOMPLISHED LEAK CHECK AND GROUND ENGINE RUN WITH NO DEFECTS FOUND. REPLACED ALL COALESCER BAGS AND ACCOMPLISHED PACK BURNOUT PROCEDURE. SYSTEM GROUND CHECKED NORMAL OPERATION. ACCOMPLISHED OVERWEIGHT LANDING INSPECTION WITH NO DEFECTS FOUND. ACCOMPLISHED FUNCTIONAL CHECK FLIGHT WITH NO SMOKE NOTED. SYSTEM OPERATIONAL CHECKED NORMAL. (M0