N434AA

Part: LIGHT — NO TEST (CABIN) · airframe 88,618 hrs · 42,010 cycles

PORTABLE EMERGENCY LIGHT FAILED TEST. REMOVED AND REPLACED LIGHT ASSEMBLY IAW AMM 33-53-00.

Part: WINDOW — OBSTRUCTED (COCKPIT) · airframe 884,973 hrs · 41,920 cycles

CAPTAIN`S SLIDING WINDOW WILL NOT OPEN OR SLIDE BACK. FOUND INSIDE WINDOW TRIM BLOCKING OPENING OF WINDOW. WINDOW OPERATES NORMALLY WITH TRIM REMOVED. INSTALLED WINDOW TRIM IAW AMM 25-11-00. OPS CHECKED GOOD.

Part: CSD — FAULTY (LT ENGINE)

AIRCRAFT WAS GROUNDED. DURING CRUISE THE LEFT GENERATOR OFF AND LEFT CSD PRESSURE LOW LIGHT ILLUMINATED ACCOMPANIED BY THE ATTENDANTS REPORTING A FAINT BURNING ELECTRICAL SMELL. FOUND LEFT CSD OIL QUANTITY OVER FULL WITH METAL CONTAMINATION AND THE SCAVENGE FILTER DIFFERENTIAL PRESSURE INDICATOR POPPED. 06/14/16 - REMOVED AND REPLACED LEFT ENGINE GENERATOR (AALA20160610004) AND CONSTANT SPEED DRIVE IAW AMM 24-10-01. LEAK AND OPERATIONAL CHECK GOOD.

Part: CSD — CONTAMINATED (ZONE 100) · airframe 87,449 hrs · 41,287 cycles

DURING CRUISE, THE LT GENERATOR OFF & LT CSD PRESSURE LOW LIGHT ILLUMINATED, ACCOMPANIED BY THE F/A REPORTING A FAINT BURNING ELECTRICAL ODOR BY THE AFT F/A JUMPSEAT, WHICH DISSIPATED AFTER APPROXIMATELY 5 TO 10 MINUTES. FOUND LT CSD OIL QUANTITY OVER FULL WITH METAL CONTAMINATION AND THE SCAVENGE FILTER DIFFERENTIAL PRESSURE INDICATOR POPPED. REMOVED AND REPLACED LEFT ENGINE GENERATOR AND CONSTANT SPEED DRIVE IAW AMM 24-10-01. LEAK AND OPS CHECKED GOOD. AIRCRAFT WAS GROUNDED.

Part: SKIN — CRACKED (FUSELAGE) · airframe 86,903 hrs · 40,987 cycles

AIRCRAFT WAS IN BASE MX. FUSELAGE SKIN CRACKED AT STATION 1474 & LONGERON 24R. REPAIRED SKIN IAW SRM 53-01-00-001.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 86,850 hrs · 40,954 cycles

CEILING EPL LIGHTS INOPERATIVE. REPLACED EMER LIGHT BATTERY PACKS IAW AMM 33-53-00. OPERATIONS CHECKED GOOD. ACFT IN BASE MX.

Part: A/C PACK — DIRTY (ZONE 100) · airframe 84,541 hrs · 39,592 cycles

DURING CLIMB A STRONG ACRID ODOR WAS DETECTED WHICH INCREASED IN STRENGTH & SPREAD TO THE CABIN. SOME EYE IRRITATION NOTICED. ODOR BEGAN TO DISSIPATE AFTER LANDING. EMERGENCY DECLARED & LANDING UNEVENTFUL. LANDING UNEVENTFUL. TROUBLE SHOT IAW 21-20-00 & DETERMINED POLLEN TO BE ODOR SOURCE. ACCOMPLISHED PACK BURN OUT IAW CARD 21-92-12. SYS CHECKED NORMAL.

Part: SLIDE — UNSERVICEABLE (R1 DOOR) · airframe 83,909 hrs · 39,262 cycles

R1 DOOR SLIDE BOTTLE PRESS OUT OF GREEN. R & R R1 DOOR SLIDE IAW AMM 25-62-00.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 83,309 hrs · 38,953 cycles

FORWARD CARGO DOOR STOP CRACKED. R & R DOOR STOP.

Part: FORMER — CRACKED (LE SLAT) · airframe 83,179 hrs · 38,886 cycles

LEFT WING LE NR 4 SLAT TRACK INBD FORMER IS CRACKED. INSTALLED LT WING NR 4 SLAT INBD FORMER DOUBLER & HAT BUSHING IAW WORK CARD 57-98-05.

Part: FORMER — CRACKED (LE SLAT) · airframe 83,179 hrs · 38,886 cycles

RIGHT WING LE NR 4 SLAT TRACK INBD FORMER IS CRACKED. INSTALLED RT WING NR 4 INBD FORMER DOUBLER & HAT BUSHING IAW WORK CARD 57-98-06.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 82,907 hrs · 38,736 cycles

AB5-2 POSITION BATTERY PACK DISCHARGED. REPLACED BATTERY PACK AT AB5-2. OPERATIONS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 82,907 hrs · 38,736 cycles

BATTERY PACK FOR CABIN EMER LIGHTS NOT FUNCTIONING. CHANGED BATTERY PACK. OPERATIONS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (TAILCONE) · airframe 82,907 hrs · 38,736 cycles

TAIL CONE SLIDE LIGHT INOPERATIVE. REPLACED BATTERY PACK FOR TAIL CONE SLIDE LIGHT. OPERATIONS CHECKED NORMAL.

Part: GENERATOR — FAILED (LT ENGINE) · airframe 80,877 hrs · 37,712 cycles

ORD LT GEN LIGHT & LT BUSS LIGHTS ILLUMINATED. EMERGENCY DECLARED FLIGHT LANDED ORD WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LT HAND GEN. SYSTEM GROUND CHECKED NORMAL OPERATION CLOSED.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 80,560 hrs · 37,516 cycles

EMERGENCY LIGHTS IN COCKPIT INOPERATIVE. REPLACED COCKPIT EMERGENCY LIGHTS BATTERY PACK. OPERATIONS CHECKED NORMAL.

Part: CLAMP — DISCONNECTED (ZONE 500) · airframe 80,244 hrs · 37,336 cycles

BNA INFLIGHT DFW-PHL CREW REPORTED WING FUEL IMBALANCE. EMERGENCY DECLARED FLIGHT DIVERTED BNA LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND A DISCONNECTED FUEL LINE CLAMP IN THE CENTER TANK. RECONNECTED CLAMP. SYSTEM GROUND CHECKED NORMAL. OPERATION (CLOSED)

Part: CADC — MALFUNCTIONED (NR 1) · airframe 79,872 hrs · 37,135 cycles

MX CREW REPORTED MULTIPLE FLIGHT CONTROL FUNCTION MALFUNCTION INDICATIONS. EMERGENCY DECLARED FLIGHT RETURNED TO DEPARTURE, LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. REPLACED NR 1 CENTRAL AIR DATA COMPUTER. SYS GROUND CHECK NORMAL OPERATION.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 79,265 hrs · 36,799 cycles

FUSELAGE SKIN IS BULGED BETWEEN STATIONS 650 AND 655 AT LONGERON 30. ACCOMPLISHED REPAIR PER SRM 53-04-03 AND EA.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 79,265 hrs · 36,799 cycles

CORROSION IN DOUBLER AT AFT INBOARD G2 GALLEY MOUNT. INSTALLED REPAIR DOUBLER PER AARD 53-20-00-16.

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 79,265 hrs · 36,799 cycles

CORROSION ON SUBFLOOR AT STATION 205. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 79,265 hrs · 36,799 cycles

FUSELAGE SKIN IS BULGED BETWEEN STATIONS 725 TO 731 AND LONGERON 29 RIGHT. INSTALLED DOUBLER PER SRM 53-04-03.

Part: LONGERON — CORRODED (FUSELAGE) · corrosion level 2 · airframe 79,265 hrs · 36,799 cycles

LONGERON 26 LEFT HAS CORROSION AT STATION 1287+2. INSTALLED FINGER DOUBLER, LONGERON AND SPLICES PER SRM 53-02 AND AARD 53-00-00-05.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 79,265 hrs · 36,799 cycles

SHEAR TIE HAS CORROSION AT STATION 1287 AND LONGERON 30. REMOVED AND REPLACED SHEAR TIE PER AARD 51-00-05.

Part: CASTING — CRACKED (SPOILER) · airframe 79,265 hrs · 36,799 cycles

RIGHT WING TRAILING EDGE: GROUND SPOILER FITTING "ON WING" IS CRACKED ON FORWARD INBOARD AND OUTBOARD ENDS. INSTALLED NEW RIGHT SPOILER CASTING PER SRM 51-30-01 AND SRM 51-30-02.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 79,265 hrs · 36,799 cycles

AFT CABIN: CORROSION ON SEAT TRACK NUMBER 3 AROUND OUTBOARD FASTENER HOLES BETWEEN STATIONS 1174 TO 1231, UNDER NUT CLIPS. INSTALLED NEW SECTION OF SEAT TRACK FROM STATIONS 1165 TO 1309 PER AARD 51-00-05-1.

Part: DIAPHRAGM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 79,265 hrs · 36,799 cycles

CORROSION UNDER G-1 GALLEY DRAIN PAN. INSTALLED DOUBLER ON SUBFLOOR UNDER G-1 GALLEY DRAIN PAN PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 79,265 hrs · 36,799 cycles

CORROSION ON SUBFLOOR AT STATION 205, FORWARD OF SEAT TRACK NUMBER 6. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 79,265 hrs · 36,799 cycles

CORROSION ON SEAT TRACK NUMBER 6 AT STATION 677. INSTALLED SEAT TRACK REPAIR PLUG PER SRM 53-05-00 FIGURE 4A AND AARD 53-20-00-10.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 79,265 hrs · 36,799 cycles

CORROSION ON SEAT TRACK NUMBER 6 FROM STATIONS 1149 TO 1151. INSTALLED SEAT TRACK REPAIR PLUG PER SRM 53-05-00 FIGURE 4A AND AARD 53-20-00-10.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 79,265 hrs · 36,799 cycles

CORROSION ON SEAT TRACK NUMBER 6 AT STATION 285. INSTALLED SEAT TRACK REPAIR PLUG PER SRM 53-05-00 FIGURE 4A AND AARD 53-20-00-10.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 79,265 hrs · 36,799 cycles

CORROSION ON SEAT TRACK NUMBER 6 AT STATION 325. INSTALLED SEAT TRACK REPAIR PLUG PER SRM 53-05-00 FIGURE 4A AND AARD 53-20-00-10.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 79,265 hrs · 36,799 cycles

CRACK ON SEAT TRACK SUPPORT VERTICAL FITTING BELOW NUMBER 2 SEAT TRACK AT STATION 927. REPLACED VERTICAL SUPPORT PER AARD 51-00-05-1.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 79,265 hrs · 36,799 cycles

CRACK ON SEAT TRACK SUPPORT VERTICAL FITTING BELOW NUMBER 4 SEAT TRACK AT STATION 886. REPLACED SUPPORT PER AARD 51-00-05-1.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 79,265 hrs · 36,799 cycles

UPPER AFT CORNER WINDOW FRAME CRACKED FORWARD SIDE OF STATION 1193 RIGHT SIDE. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: PAN — CRACKED (FUSELAGE) · airframe 79,265 hrs · 36,799 cycles

UPPER AFT CORNER OF WINDOW PAN CRACKED AT STATION 1041 LEFT SIDE. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 79,031 hrs · 36,677 cycles

RIGHT CEILING EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR RIGHT CEILING EMERGENCY LIGHT. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 79,031 hrs · 36,677 cycles

CENTER CEILING EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR CENTER CEILING EMERGENCY LIGHT. OPS CHECK NORMAL.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 79,000 hrs · 36,666 cycles

FORWARD ENTRY LOWER EMERGENCY FLASHLIGHT BATTERY HAS NO CHARGE. REPLACED EMERGENCY FLASHLIGHT BATTERY. OPS CHECK NORMAL.

Part: CONNECTOR — NOT SEATED (AC BAY) · airframe 78,413 hrs · 36,369 cycles

TAIL COMPARTMENT EMERGENCY LIGHTS ABOVE CATWALK INOPERATIVE. RESEATED EMERGENCY LIGHT CONNECTOR. OPS CHECK NORMAL.

Part: BATTERY PACK — NOT SEATED (CABIN) · airframe 75,720 hrs · 35,014 cycles

FORWARD CABIN AND FLIGHT DECK EMERGENCY LIGHTS INOPERATIVE. RESEATED FORWARD DROP CEILING BATTERY PACK. OPS CHECK NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 75,720 hrs · 35,014 cycles

CEILING EMERGENCY LIGHTS FROM ROW 13 TO ROW 16 INOPERATIVE. REPLACED BATTERY PACK AT OVERHEAD RIGHT AFT LAVATORY FOR CEILING EMERGENCY LIGHTS FROM ROWS 13 TO 16. OPS CHECK NORMAL.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 75,568 hrs · 34,934 cycles

DAMAGE ON LEFT SIDE OF FUSELAGE STATION 275 BETWEEN LONGERONS 23 AND 24 LEFT. ACCOMPLISHED DOUBLER REPAIR PER SRM 53-04-03.

Part: BATTERY PACK — DIRTY (CABIN) · airframe 74,929 hrs · 34,579 cycles

ROW 23 TO 27 OVERHEAD EMERGENCY LIGHT INOPERATIVE. REMOVED DEBRIS AND RESEATED EMERGENCY BATTERY PACK AT ROW 23. OPS CHECK NORMAL.

Part: ENGINE — DAMAGED (LEFT) · airframe 74,604 hrs · 34,400 cycles

STL - CREW REPORTED HIGH LEFT ENGINE EXHAUST GAS TEMPERATURE. EMERGENCY DECLARED FLIGHT RETURNED STL LANDED WITHOUT INCIDENT. UPON LANDING RECEIVED NUMBER ONE ENGINE FIRE WARNING AND BOTH FIRE BOTTLES WERE DISCHARGED. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT ENGINE ON 06/05/2011 AT STL. REPLACED BOTH FIRE BOTTLES. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 74,572 hrs · 34,384 cycles

TAIL CONE CEILING EGRESS LIGHTS INOPERATIVE. REPLACED EMERGENCY BATTERY PACK AFT RIGHT LAVATORY CEILING. OPS CHECK NORMAL.

Part: PAN — CRACKED (WINDOW) · airframe 74,008 hrs · 34,084 cycles

RIGHT WINDOW PAN CRACKED, UPPER AFT SIDE AT STATION 1060. INSTALLED DOUBLER PER AARD53-10-00-25.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 72,603 hrs · 33,444 cycles

LEFT FORWARD ENTRY PORTABLE EMERGENCY LIGHT IS VERY DIM. REPLACED THE LEFT FORWARD ENTRY PORTABLE EMERGENCY LIGHT. OPS CHECKED NORMAL.

Part: LENS — DAMAGED (CABIN) · airframe 72,603 hrs · 33,444 cycles

EMERGENCY FLOOR PATH LIGHT LENS AT SEAT 14 SMASHED. REPLACED LENS FOR EMERGENCY FLOOR PATH LIGHT AT SEAT 14. OPS CHECKED NORMAL.

Part: GUARD — DAMAGED (CABIN) · airframe 72,603 hrs · 33,444 cycles

EMERGENCY FLOOR PATH LIGHT GUARD AT SEAT 14 SMASHED. REPLACED GUARD FOR EMERGENCY FLOOR PATH LIGHT AT SEAT 14. OPS CHECKED NORMAL.

Part: GUARD — DAMAGED (EMERGENCY LIGHT) · airframe 72,603 hrs · 33,444 cycles

EMERGENCY FLOOR PATH LIGHT LENS GUARD IS SMASHED AT SEAT 8. REPLACED GUARD. OPS CHECKED NORMAL.

Part: LAMP — DAMAGED (CABIN) · airframe 72,603 hrs · 33,444 cycles

EMERGENCY FLOOR PATH LIGHT LAMP SMASHED AT SEAT 14. REPLACED LAMP FOR EMERGENCY FLOOR PATH LIGHT AT SEAT 14. OPS CHECKED NORMAL.

Part: GUARD — DAMAGED (CABIN) · airframe 72,603 hrs · 33,444 cycles

EMERGENCY FLOOR PATH LIGHT LENS GUARD IS SMASHED AT SEAT 11. REPLACED GUARD, OPS CHECKED NORMAL.

Part: SKIN — DENTED (ZONE 200) · airframe 67,764 hrs · 31,266 cycles

DENT IN FUSELAGE SKIN AT STATION 236 BETWEEN LONGERON 17L AND 18L. INSTALLED REPAIR PER SRM 53-04 FIGURE 38 SHEET 22 VIEW G.

Part: SEAT TRACK — CORRODED (ZONE 100) · airframe 67,764 hrs · 31,266 cycles

NUMBER 6 SEAT TRACK STATION 216 TO 217, CORRODED. REPAIRED PER SRM 53-05-00 FIGURE 4F SHEET 5.

Part: LUG — CORRODED (ZONE 300) · airframe 67,764 hrs · 31,266 cycles

TAIL, NUMBER 1 LUG PLATE HAS CORROSION. INSTALLED A SERVICEABLE NUMBER 1 LUG.

Part: BEAM — CORRODED (ZONE 100) · airframe 40,668 hrs · 3,127 cycles

BEAM CORRODED, LOWER DOORWAY, STATION 1155 TO 1193. REMOVED CORROSION AND REPAIRED PER AARD 53-10-00-3.

Part: LUG — CORRODED (ZONE 300) · airframe 40,670 hrs · 3,127 cycles

NUMBER 5 VERTICAL STABILIZER PIVOT LUG HAS CORROSION. INSTALLED A SERVICEABLE NUMBER 5 LUG.

Part: LUG — CORRODED (ZONE 300) · airframe 67,764 hrs · 31,266 cycles

TAIL, NUMBER 4 LUG PLATE HAS CORROSION. INSTALLED A SERVICEABLE NUMBER 4 LUG.

Part: ANGLE — CORRODED (ZONE 800) · airframe 67,764 hrs · 31,266 cycles

AFT CARGO DOOR LOWER AFT CORNER OF DOORWAY, LOWER ANGLE CORRODED. INSTALLED SERVICEABLE ANGLE PER SRM 51-10-01.

Part: CARGO TRACK — CORRODED (ZONE 100) · airframe 40,670 hrs · 3,127 cycles

LEFT TIE DOWN TRACK SPLICE CORRODED, STATION 1212 - 1224, TOP AND BOTTOM. REPLACED SPLICE PER SRM 51-20-00.

Part: LUG — CORRODED (VERTICAL STAB) · airframe 67,764 hrs · 31,266 cycles

TAIL, NUMBER 8 VERTICAL STABILIZER PIVOT LUG HAS CORROSION. INSTALLED A SERVICABLE NUMBER 8 LUG.

Part: LUG — CORRODED (ZONE 300) · airframe 40,670 hrs · 3,127 cycles

NUMBER 7 VERTICAL STABILIZER PIVOT LUG HAS PITTING ON FACE. INSTALLED A SERVICEABLE NUMBER 7 LUG.

Part: LUG — CORRODED (ZONE 300) · airframe 67,764 hrs · 31,266 cycles

TAIL, NUMBER 2 LUG PLATE HAS CORROSION. INSTALLED A SERVICABLE NUMBER 2 LUG.

Part: LUG — CORRODED (ZONE 300) · airframe 40,670 hrs · 3,127 cycles

NUMBER 6 VERTICAL STABILIZER PIVOT LUG HAS CORROSION. INSTALLED A SERVICEABLE NUMBER 6 LUG.

Part: FITTING — CORRODED (ZONE 300) · airframe 67,764 hrs · 31,266 cycles

TAIL, NUMBER 3 LUG PLATE HAS CORROSION. INSTALLED A SERVICEABLE NUMBER 3 LUG.

Part: CUSP WEB — CORRODED (ZONE 100) · airframe 40,670 hrs · 3,127 cycles

CORROSION ON UNDERSIDE OF CUSP STATION 522 TO 541. REMOVED CORROSION AND INSTALLED DOUBLER, FROM STATION 518 TO 549 PER SRM 53-20-00-16.

Part: LONGERON — CRACKED (ZONE 100) · airframe 40,670 hrs · 3,127 cycles

LONGERON 2L CRACKED AT STATION 160. SPLICED IN NEW SECTION LONGERON FROM STATION 148 TO 170.

Part: FRAME — CORRODED (ZONE 100) · airframe 40,670 hrs · 3,127 cycles

CORROSION ON STATION 1322 FRAME FORWARD AND TOPSIDE L30 - L28L.

Part: LONGERON — CRACKED (ZONE 200) · airframe 67,764 hrs · 31,266 cycles

LONGERON 4L CRACKED AT STATION 200. REPLACED LONGERON 4L FROM 148 TO 224.

Part: BEAM — CORRODED (ZONE 100) · airframe 40,670 hrs · 3,127 cycles

MID CARGO DOOR BEAM (LOWER) HAS CORROSION ON HORIZONTAL LEG STATION 650 TO 692. REMOVED CORROSION AND INSTALLED DOOR BEAM DOUBLER PER AARD 53-10-00-3.

Part: HINGE — WORN (ZONE 700) · airframe 40,670 hrs · 3,127 cycles

MAIN LANDING GEAR DOOR STRUT HINGE WORN. REPLACED HINGE ON MAIN LANDING GEAR DOOR STRUT PER ESO 80029.

Part: SKIN — CORRODED (ZONE 100) · airframe 67,764 hrs · 31,266 cycles

SKIN BULGE AT STATION 750 BETWEEN LONGERONS 29L AND 29R. REPAIRED PER SRM 53-04 FIGURE 12B SHEET 31.

Part: SEAT TRACK — CORRODED (ZONE 100) · airframe 40,670 hrs · 3,127 cycles

FORWARD END OF NUMBER 6 SEAT TRACK STATION 213 TO 215 SUPPORT ANGLE CORRODED (G-2 MOUNT). INSTALLED A SERVICEABLE G-2 MOUNT AT FORWARD END OF NUMBER 6 SEAT TRACK PER SRM 51-30-00.

Part: CUSP WEB — CORRODED (ZONE 100) · airframe 40,670 hrs · 3,127 cycles

RIGHT CUSP CORRODED FROM STATION 503 TO 589. REPLACED CUSP SHEET FROM STATION 503 TO 589.

Part: WEDGE — CRACKED (RT WING TE FLAP) · airframe 67,764 hrs · 31,266 cycles

RIGHT WING INBOARD END OF FIBERGLASS TRAILING EDGE WEDGE CRACKED AND SPLIT RIGHT WING INBOARD FLAP. REPAIRED AREA PER SRM 57-03-00 FIGURE 10 SHEET 1.

Part: ANGLE — CORRODED (ZONE 100) · airframe 40,670 hrs · 3,127 cycles

AFT CARGO LOWER FORWARD CORNER DOORWAY ANGLE CORRODED. INSTALLED A SERVICEABLE DOOR WAY ANGLE.

Part: SKIN — CRACKED (RT WING TE FLAP) · airframe 67,764 hrs · 31,266 cycles

RIGHT WING, INBOARD FLAP OUTBOARD END OF FIBERGLASS TRAILING EDGE DAMAGED. REPAIRED DAMAGE PER SRM 57-03-00 SHEET 1 FIGURE 10.

Part: SKIN — DENTED (RT WING TE FLAP) · airframe 67,764 hrs · 31,266 cycles

RIGHT WING, SMALL DING IN TRAILING EDGE FLAP AFT OF NR 4 MAIN GEAR. INSTALLED FLUSH REPAIR PER SRM 57-01-00, FIGURE 5 SHEET 2.

Part: CUSP WEB — CORRODED (ZONE 100) · airframe 40,668 hrs · 3,127 cycles

CORROSION ON RIGHT HAND CUSP. INSTALLED REPAIR PER AARD 53-20-00-16.

Part: CUSP WEB — CRACKED (ZONE 100) · airframe 40,670 hrs · 3,127 cycles

LEFT SIDE, CUSP CRACKED AT STATION 218 THRU ALIGNMENT HOLE. REPLACED CUSP SHEET FROM STATION 218 TO 237.

Part: ANGLE — CRACKED (ZONE 200) · airframe 67,764 hrs · 31,266 cycles

FORWARD SIDE OF STATION 1338 BULKHEAD VERTICAL ANGLE BETWEEN AIR CONDITIONING DUCTS CRACKED AT TOP FASTENERS. INSTALLED REPAIR PER AARD 53-10-00-15.

Part: FITTING — CRACKED (CARGO DOOR) · airframe 67,764 hrs · 31,266 cycles

CARGO DOOR FORWARD BOTTOM STOP PAD FITTING CRACKED. REMOVED AND REPLACED FITTING.

Part: FITTING — CRACKED (CARGO DOOR) · airframe 67,764 hrs · 31,266 cycles

CARGO DOOR STOP FITTING ON FORWARD SIDE CRACKED. REPLACED FITTING PER ESO 80174.

Part: FITTING — WRONG PART (UNKNOWN) · airframe 67,764 hrs · 31,266 cycles

FITTING WRONG TYPE. REMOVED AND REPLACED FITTING PER S/B DC9-52-189.

Part: FITTING — WRONG PART (UNKNOWN) · airframe 67,764 hrs · 31,266 cycles

FITTING WRONG TYPE. REMOVED AND REPLACED UPPER FORWARD FITTING PER S/B DC9-52-189.

Part: FITTING — WRONG PART · airframe 67,764 hrs · 31,266 cycles

FITTING WRONG TYPE. REMOVED AND REPLACED UPPER AFT FITTING PER S/B DC9-52-189.

Part: FITTING — WRONG PART (UNKNOWN) · airframe 67,764 hrs · 31,266 cycles

FITTING WRONG TYPE. REMOVED AND REPLACED FITTING, PER S/B DC9-52-189.

Part: FITTING — WRONG PART (CARGO DOOR) · airframe 67,764 hrs · 31,266 cycles

LOWER FORWARD CLIP WRONG TYPE ON CARGO DOOR. REMOVED AND REPLACED FITTING (CLIP) PER S/B DC 9 - 52- 189.

Part: FITTING — WRONG PART (CARGO DOOR) · airframe 67,764 hrs · 31,266 cycles

CARGO DOOR LOWER AFT CLIP WRONG TYPE. REMOVED AND REPLACED FITTING (CLIP) PER S/B DC-9-52-189.

Part: FITTING — WRONG PART (UNKNOWN) · airframe 67,764 hrs · 31,266 cycles

UPPER FORWARD CLIP (FITTING) WRONG TYPE. REMOVED AND REPLACED FITTING PER S/B DC9-52-189.

Part: FITTING — WRONG PART (CARGO DOOR) · airframe 67,764 hrs · 31,266 cycles

CARGO DOOR UPPER AFT FITTING WRONG TYPE. REMOVED AND REPLACED FITTING PER S/B DC9-52-189.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 67,570 hrs

EXTERNAL EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK FOR EXTERNAL EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED)

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 67,570 hrs

EMERGENCY LIGHTS AT MID CABIN INOPERATIVE. REPLACED BATTERY PACK AT SEAT ROW 20 FOR EMERGENCY LIGHTS AT MID CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED)

Part: ACTUATOR — INOPERATIVE (NLG)

NOSE GEAR FAILED TO EXTEND NORMALLY. RECYCLED THREE TIMES WITH NO HELP. MANUALLY EXTENDED GEAR. LANDED ORD WITHOUT INCIDENT. REPLACED NOSE LANDING GEAR BUNGEE ACTUATOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SENSOR — INOPERATIVE (NLG)

LAX INFLIGHT T452/20FEB - RED NOSE GEAR LIGHT ILLUMINATED AFTER TAKEOFF. RETURNED TO LAX AND LANDED WITHOUT INCIDENT. SERVICE NOSE STRUT, REPLACED SHRADER VALVE, AND REPLACED D1 NOSE GEAR PISTON SENSOR AND REPACKED LOWER PISTON. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

SFO - OVERHEAD EMERGENCY LIGHTS FROM ROWS 23 TO 27 INOPERATIVE. REPLACED BATTERY PACK FOR OVERHEAD EMERGENCY LIGHTS AT ROWS 23 TO 27. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

SFO - EMERGENCY EXIT SIGNS AT BOTH LEFT AND RIGHT HAND INOPERATIVE. REPLACED BATTERY PACK AT B549 FOR EMERGENCY EXIT SIGNS AT BOTH LEFT AND RIGHT HAND. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — INOPERATIVE (CABIN)

SFO - EMERGENCY LIGHTS IN FIRST CLASS INOPERATIVE. REPLACED CONNECTOR UNDER SEAT 3F FOR EMERGENCY LIGHTS IN FIRST CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

LGA - SEAT MOUNTED ESCAPE PATH EMERGENCY LIGHTS AT ROWS 20 TO 32 INOPERATIVE. REPLACED BATTERY PACK IN AFT POSITION AT ROW 20 FOR SEAT MOUNTED ESCAPE PATH EMERGENCY LIGHTS AT ROWS 20 TO 32. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY EXIT)

ORD - EMERGENCY LIGHTS ABOVE LEFT AND RIGHT AFT OVERWING EXIT DOORS INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS ABOVE LEFT AND RIGHT AFT OVERWING EXIT DOORS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: O-RING — LEAKING (APU OIL SYS)

EWR INFLIGHT T1877/09, SMOKE IN CABIN AFTER TAKEOFF. SLIGHT ODOR IN COCKPIT. FLIGHT ATTENDANT REPORTED SMOKE WAS NOT GOING AWAY. RAN CABIN FIRE SMOKE PROCEDURE AND DEPRESSURIZED CABIN TO REMOVE SMOKE. RETURNED TO EWR AND LANDED WITHOUT INCIDENT. FOUND APU OIL LEAK INTO AIR INLET. REPLACED APU CHIP DETECTOR O-RING AND ACCOMPLISHED PACK BURN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

RDU EMERGENCY PATH LIGHT AT ROW 15D INOPERATIVE. REPLACED EMERGENCY PATH LIGHT ASSEMBLY FOR ROW 15D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY LIGHTS FROM ROWS 27-31 INOPERATIVE. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (CABIN)

RDU - DURING OVERNIGHT MAINTENANCE, STAIRWAY MOUNTED EMERGENCY EXIT PATH LIGHT INOPERATIVE. CLEANED CONTACTS ON LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: HANDLE — CORRODED (SERVICE DOOR)

TUL - FOUND DOOR HANDLE MECH, FORWARD GALLEY SERVICE DOOR, SLEEVES HAS CORROSION BETWEEN SLEEVES. REMOVED AND REPLACED DOOR HANDLE MECHANISM WITH SERVICEABLE PER ESO 80177. (M)

Part: WEB — GOUGED (FUSELAGE)

TUL - FOUND SMALL GOUGE IN MEMBRANE STATION 198 RBL 16. ACCOMPLISHED DOUBLER REPAIR 7075 T-6.026 AFTER DAMAGED AREA CUTOUT AS PER AARD 53-00-00-02. (M)

Part: DOOR FRAME — CRACKED (FUSELAGE)

TUL - FOUND DOOR JAMB WEB CRACKED STATION 208 LONGERON 15L. INSTALLED DOUBLER PER AARD 53-10-00-11. (M)

Part: SKIN — CRACKED (FS 1380)

TUL - FOUND CRACK IN FUSELAGE SKIN AT FASTENERS HOLE STATION 1380 LEFT SIDE APPROX 12 INCHES ABOVE PYLON. INSTALLED DOUBLER OVER CRACK IAW SRM 53-01 FIG 2. (M)

Part: DOOR FRAME — GOUGED (FUSELAGE)

TUL - FOUND FORWARD SERVICE DOOR JAMB FRAME GOUGED LOWER AFT CORNER. REMOVED AND REPLACED FORWARD SERVICE DOOR JAMB ASSEMBLY 4002982 PER SRM 51-01. (M)

Part: BRACKET — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON DOOR CUTOUT LOWER ATTACH CORNER CURVED BRACKET. INSTALLED SERVICEABLE BRACKET SRM 51-01. (M)

Part: FITTING — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON DOOR CUTOUT LOWER AFT CORNER FITTING. INSTALLED NEW CORNER FITTING SRM 51-01. (M)

Part: BRACKET — CORRODED (FS 1155)

TUL - FOUND CORROSION ON DOOR CUTOUT FORWARD LOWER CORNER CURVED BRACKET. INSTALLED NEW BRACKET SRM 51-01. (M)

Part: SKIN (FS 933)

TUL - FOUND DEEP BLENDOUT IN SKIN STATION 933 LONGERON 10R. INSTALLED INTERNAL DOUBLER PER SRM 53-04 FIG 38 AND ESO 80559 DATED 5-8-2001. (M)

Part: CARGO TRACK — CORRODED (FUSELAGE)

TUL - FOUND LEFT TIE DOWN TRACK CORRODED FS 1117, 1174-1206. REMOVED AND REPLACED SECTION OF LEFT TIE DOWN TRACK FROM STATION 1007-1221. (M)

Part: FITTING — CORRODED (FS 1155)

TUL - FOUND CORROSION ON DOOR CUTOUT FORWARD LOWER CORNER FITTING. INSTALLED NEW CORNER FITTING SRM 51-01. (M)

Part: TRACK — CORRODED (FUSELAGE)

TUL - FOUND LAV TIE DOWN AT STATION 255 LBL 32 CORRODED. REMOVED AND REPLACED TIE DOWN TRACK WITH NEW SRM 51-01. (M)

Part: TRACK — CORRODED (FUSELAGE)

TUL - FOUND LAVATORY TIE DOWN AT STATION 253 LBL 19 CORRODED. REMOVED AND REPLACED TIE DOWN SECTION WITH NEW SRM 51-01. (M)

Part: WEB — GOUGED (FUSELAGE)

TUL - FOUND DEEP GOUGE IN RIGHT CUSP WEB APPROX STATION 313. CUT OUT DAMAGE, DRILLED DOUBLER, .032, 7025T6, INSTALLED FASTENERS, PER SRM 53-01. (M)

Part: SKIN — DAMAGED (FUSELAGE)

TUL - FOUND DEEP BLENDOUT AREA OF FUSELAGE SKIN AT LONGERON 22R APPROX STATION 304. INSTALLED DOUBLER. REMOVED REPAIR FORWARD OF DAMAGE AND INCORPORATED INTO NEW REPAIR PER 53-04 FIG 38. (M)

Part: WEB — GOUGED (FUSELAGE)

TUL - FOUND GOUGE IN SUBFLOOR STATION 200 RBL 21. REMOVED DAMAGE, INSTALLED DOUBLER PER AARD 53-00-00-00-02 PAGE 1. (M)

Part: SKIN (FS 644-648)

TUL - FOUND TWO DEEP BLENDOUT ON FUSELAGE SKIN. INSTALLED INTERNAL DOUBLER SRM 53-05 FIG 38 PAGE 218. (M)

Part: SKIN (FS 615)

TUL - FOUND THREE DEEP BLEND OUTS ON FUSELAGE SKIN STATION 610 TO STATION 619 BELOW LONGERON 26 LEFT. BLENDOUTS OUT OF LIMIT, INSTALLED INTERNAL DOUBLER PER SRM 53-04 FIG 38. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND AREA OF CORROSION AT GALLEY TIE DOWN AND FLOOR DIAPHRAGM. REMOVED SECTION OF CORRODED DIAPHRAGM AND INSTALLED DOUBLER PER AARD 53-00-00-2. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL - FOUND PITTING CORROSION, NR 6 SEAT TRACK, STATION 392. ACCOMPLISHED SEAT TRACK PLUG REPAIR PER SRM 53-05 PART NR 1, FIG 4. TREATED AND PRIMED PER SRM 53-10-3. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND UPPER SURFACE OF CUSP CORROSION RIGHT STATION 500. REPAIR DOUBLER INSTALLED AS PER SRM 53-01 FIG 4 SH 3. (M)

Part: APU — LEAKING (TAIL)

DFW - FLT 1837 - ON CLIMB-OUT FROM DFW, THE CABIN FILLED WITH WHITE SMOKE AND AN ACRID SMELL. AIR INTERRUPTED AND RETURNED TO DFW. ON DESCENT, THE SMOKE CLEARED AND THE SMELL DECREASED. LANDED DFW WITHOUT INCIDENT. REPLACED AUXILLARY POWER UNIT. REPLACED COALESCER BAGS AND ACOMPLISHED PACK BURNOUT. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: FUSELAGE — DENTED (RT LOWER FWD)

TUL - DENT IN FUSELAGE, FS 570 - FS 589 ABOVE L21R. REPAIRED IAW SRM 53-04 FIG 12B SHT 5. TST: 33,764 HOURS. CYCLES: 17,035. (X)

Part: CUSP WEB — CORRODED (INBD OF AFT SVS)

TUL - CORROSION ON CUSP WEB UNDER SEAT TRACK NR 1 AT STA 1174. INSTALLED DOUBLER 4 INCHES BY 5 INCHES AFTER CUT-OUT OF DAMAGE PER SRM 53-01. (X)

Part: LIGHT — INOPERATIVE (CABIN)

ORD - DURING OVERNIGHT CHECK, LEFT HAND OVERHEAD EMERGENCY LIGHTS AT ROW 3 WERE FOUND INOPERATIVE. SYSTEM CHECKED AND UNABLE TO DUPLICATE. SYSTEM GROUND CHECKED NORMAL OPERATION. (X)

Part: COALESCER — DIRTY (ACM BAY)

DFW - FLT T0429 - EN ROUTE MEM/DFW, SLIGHT BURNING ODOR NOTED DURING ALL PHASES OF FLIGHT WITH NO OTHER ABNORMAL INDICATIONS. AIRCRAFT LANDED DFW WITHOUT INCIDENT. REPLACED ALL COALESCER BAGS AND ACCOMPLISHED GROUND ENGINE RUN WITH NO DEFECTS FOUND. ACCOMPLISHED FUNCTIONAL CHECK FLIGHT WITH NO ODOR OR OTHER DEFECTS FOUND. SYSTEM OPERATIONAL CHECKED NORMAL. (X)

Part: CONNECTOR — LOOSE (CABIN)

DFW - DURING OVERNIGHT CHECK, DISCOVERED EMERGENCY FLOOR LIGHTS BY FORWARD GALLEY INOPERATIVE. RESECURED LOOSE EMERGENCY FLOOR LIGHT CONNECTOR AT FORWARD END OF FIRST CLASS CABIN. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)