N526UA

Part: SHEAR TIE — DAMAGED (FUSELAGE) · airframe 76,735 hrs · 27,931 cycles

BS 1420 BETWEEN STRINGER 28R & 29R SHEAR TIE HAS DAMAGED HOLE. FABRICATED & INSTALLED NEW SHEAR TIE IAW SRM 51-30-01 & 51-40-05.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 76,735 hrs · 27,931 cycles

AFT PIT BS 1406 STRINGER 29R IS CORRODED. R & R STRINGER 29R FROM BS 1406 TO 1452 IAW SRM 51-40-02 & SRM 51-40-05.

Part: FRAME — CRACKED (FUSELAGE) · airframe 76,735 hrs · 27,931 cycles

AFT PIT BS 1440 FRAME INBD CHORD CRACKED AT RBL 11. REMOVED DAMAGE, FABRICATED & INSTALLED REPAIR PARTS IAW ECRA 5360-01389.

Part: FRAME — DENTED (FUSELAGE) · airframe 76,735 hrs · 27,931 cycles

AFT PIT BS 1600 STRINGER 26L DENT ON UPPER SURFACE OF FRAME. REMOVED DAMAGE, FABRICATED & INSTALLED REPAIR PARTS IAW SRM 53-00-07 REPAIR 5.

Part: REPAIR — GOUGED (NR 1 PYLON) · airframe 76,735 hrs · 27,931 cycles

NUMBER 1 PYLON AFT FAIRING FRAME AT OTBD END, PREVIOUS REPAIR GOUGED. REMOVED DAMAGE, FABRICATED & INSTALLED REPAIR PARTS IAW SRM 51-70-11.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 76,735 hrs · 27,931 cycles

AFT PIT BS 1380 RBL 3 FRAME SHEAR TIE CORROSION. REMOVED DAMAGE, FABRICATED & INSTALLED NEW SHEAR TIE IAW SRM 51-40-02.

Part: SKIN — DENTED (FUSELAGE) · airframe 76,735 hrs · 27,931 cycles

EXT FUSE SKIN BS 430 STRINGER 15L, DENT. FABRICATED & INSTALLED REPAIR DOUBLER & FILLER IAW SRM 53-00-01.

Part: FAIRING — CRACKED (FUSELAGE) · airframe 76,735 hrs · 27,931 cycles

RIGHT EMPENNAGE BS 1787 STRINGER 17R - 19R. FIXED FAIRING PANEL CRACKED. FABRICATED & INSTALLED REPAIR PARTS IAW ECRA 5387-01001.

Part: FRAME SPLICE — GOUGED (FUSELAGE) · airframe 76,735 hrs · 27,931 cycles

BS 1520 FRAME SPLICE ABOVE STRINGER 23R, MULTIPLE GOUGES. FABRICATED & INSTALLED NEW SPLICE IAW DWG 146N1042 & SRM 51-30-01.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 76,735 hrs · 27,931 cycles

AFT PIT BS 1472 STRINGER 29R CORROSION. FABRICATED & INSTALLED NEW STRINGER 29R FROM BS 1460 TO 1488 IAW SRM 53-00-03.

Part: FRAME SPLICE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 76,735 hrs · 27,931 cycles

FORWARD PIT BS 660 LT, FRAME SPLICE PLATE CORROSION. REMOVED DAMAGE, FABRICATED & INSTALLED NEW SPLICE PLATE IAW SRM 51-40-05 & 51-40-02.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 76,735 hrs · 27,931 cycles

CABIN FLOOR STRUCTURE BS 940 - 960 STRINGER 17L LT CREASE BEAM INTERCOSTAL UPPER SURFACE CORRODED. R & R CREASE BEAM.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 72,917 hrs · 26,758 cycles

AFTER STATION 1681 FRAME SECTION REMOVAL FOUND OTBD CHORD BETWEEN STRINGS 17R & 18R TO HAVE THREE EACH HOLES WITH PREVIOUS COUNTER BORES. REMOVED DAMAGED SECTION OF THE OTBD CHORD, FABRICATED REPLACEMENT CHORD & SPLICE ANGLE. INSTALLED REPLACEMENT CHORD IAW EA 130464IR & ECRA 5360-01303 AT BS 1681 BETWEEN STRINGERS 14R & 20R. MUST BE INSPECTION EVERY 24 MONTHS OR 3000 FLT CYCLES WHICHEVER COMES FIRST. ACCOMPLISHED INSPECTION IAW PART 2 OF ECRA 5360-01303. INSPECTED & COMPLIED WITH METER IAW PART 2 OF ECRA 5360-01303. NO RECORDABLE DISCREPANCIES NOTED.

Part: RUDDER — DAMAGED (TAIL) · airframe 76,735 hrs · 27,931 cycles

LIGHTNING STRIKE INSPECTION FOUND RUDDER DAMAGE ON TE. TE DAMAGE 20 INCHES FROM TOP WITH 1 INCH BY .5 INCH DAMAGE REPAIRED. REINSTALLED STATIC WICK.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 76,735 hrs · 27,931 cycles

CABIN STATION 1680 LBL 50 FWD SIDE OF T CAP UPPER & LOWER SURFACE IS CORRODED. REPLACED CABIN FLOORBEAM STATION 1680 LBL 60 TO RBL 60 IAW SRM 51-40-02, DWG 146N5091, EA 130412IR & ECRA 5360-01298.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 76,735 hrs · 27,931 cycles

FORWARD PAX AREA BS 377.7 RBL 54 TO 56 FLOORBEAM HAS UPPER SURFACE CORROSION. REPAIRED FWD PAX COMP BS 377.7 RBL 54 TO 56 BY INSTALLATION OF REPAIR STRAP & TAPERED FILLERS. THIS IS A CAT A REPAIR.

Part: IDG — MALFUNCTIONED (NR 2 ENGINE) · airframe 76,406 hrs · 27,838 cycles

RIGHT GEN OFF LIGHT ON VERY START OF TAKEOFF ROLL. BPCU BITE SHOWED IDG PMG WIRING & OVER FREQ TRIP ON SAME CHANNEL. R & R NR2 ENG IDG IAW AMM 24-11-01.

Part: APU — FLAMED OUT (APU BAY) · airframe 74,854 hrs · 27,381 cycles

EVIDENCE OF FLAME & SMOKE COMING FROM APU TAILPIPE. SUSPECT APU TURBINE SEALS BLOWN & WILL REQUIRE APU REPLACEMENT. IAW DF151, APU FIRE SYS DEACTIVATED. DO NOT OPERATE APU UNTIL FIRE SYS RESTORED. APU SMOKE, FLT CREW ELECTED TO DISCHARGE APU FIRE BOTTLE PRECAUTIONARY. NO EVIDENCE OF DAMAGE TO APU COMPARTMENT NOTED. CHECKED APU EXHAUST AREA & APU COMPARTMENT, NO DEFECTS & OR HEAT DAMAGE NOTED. APU NOT TO BE OPERATED UNTIL FIRE EXTINGUISHING SYS IS REPAIRED & MADE SERVICEABLE. REPLACED APU FIRE BOTTLE & DISCHARGE IAW MM.

Part: BUMPER — DEFECTIVE (CARGO DOOR) · airframe 74,725 hrs · 27,339 cycles

FWD CARGO DOOR HANDLE ISSUE. REPLACED FWD CARGO PIT DOOR'S EXTERNAL HANDLE FAIRING BUMPER.

Part: SLIDE — DEPLOYED (R4 DOOR) · airframe 74,577 hrs · 27,283 cycles

GATE GOURMET INFORMED THAT DOOR 4R WOULD NOT CLOSE. R & R DOOR SLIDE AT DOOR 4R WITH SLIDE ROBBED FROM AIRCRAFT 5428 DOOR 4R IAW MM. DOOR OPERATIONS CHECKED OKAY. OK FOR SERVICE.

Part: WINDSHIELD WIPER — DEFECTIVE (COCKPIT) · airframe 74,559 hrs · 27,277 cycles

WINDSHIELD WIPERS WILL NOT WIPE CLEAN. CAPTAIN`S WIPER DOES NOT CLEAR WINDSHIELD, OBSCURED VISIBILITY. REPLACED CAPTAIN`S WIPER & ADJUSTED IAW MM, OPERATIONS CHECKED GOOD.

Part: EEC — FAULTY (RT ENGINE) · airframe 73,983 hrs · 27,090 cycles

RT ENG WILL NOT REDUCE TO LOW POWER. CREW INFO: N1 #134.6 #2 55.5 EGT #1 312 #2 358 N2 #1 77 #2 82 FF #1 .07 #2 2.3. REPLACED NR 2 ENGINE EEC IAW MM-73-21-04. NO FAULTS. SEE SEQ #9832003.

Part: LIGHT — UNSECURE (CABIN) · airframe 73,807 hrs · 27,025 cycles

EMERGENCY LIGHTING STRIP LIFTING OFF FLOOR. SECURED LOOSE EMERGENCY LIGHTING STRIP.

Part: LAMP — FAULTY (DOOR ARM) · airframe 73,571 hrs · 26,953 cycles

ARMED LIGHT FOR DOOR 1R WILL NOT ILLUMINATE. REPLACED LAMPS ARM LIGHT ABOVE DOOR. ARMING SEQUENCE NORMAL.

Part: CHARGER — FAULTY (APU) · airframe 73,336 hrs · 26,881 cycles

APU FAULT LIGHT ON, SHUTDOWN. REPLACED BATTERY CHARGER & REPLACED BATTERY IAW MM 24-31-03.

Part: BLADE — DAMAGED (NR 1 ENG FAN) · airframe 73,217 hrs · 26,845 cycles

NR 1 FAN BLADE ON RT ENGINE HAS NICK NEAR THE TIP. INSPECTED AND REPAIRED NR 1 ENG FAN BLADE IAW MM.

Part: WIRE — BROKEN (MLG DOOR SWITCH) · airframe 72,922 hrs · 26,760 cycles

LANDING GEAR ALTERNATE EXTENSION CONTROLLER CIRCUIT BREAKER TRIPPED. CIRCUIT BREAKER TRIPS WITH GEAR DOOR UP. IT TRIPS SLOWLY, TAKES A MINUTE OR LESS. FOUND SHORTED WIRE W2426-1026-18 FOR LT MAIN GEAR DOOR CLOSED SWITCH S10037. REPLACED IAW SSM 32-12-12. OPS CHECKED GOOD.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 75,917 hrs · 26,758 cycles

L1 DOOR EXIT LIGHT WIRE SPLICE BROKEN. SPLICED BROKEN WIRE IAW SWP 20-30-12. OPS CHECKED GOOD IAW AMM.

Part: SPAR — DAMAGED (RT WING TE FLAP) · airframe 72,917 hrs · 26,758 cycles

DURING C1 CHECK, CHAFE DAMAGE WAS FOUND ON THE RT INBD MAIN FLAP FRONT SPAR LOWER ANGLE. REPAIRED IAW EA 130508, REV IR.

Part: FRAME — DAMAGED (BS 1681 S17-18R) · airframe 72,917 hrs · 26,758 cycles

BS 1681, FRAME SECTION REMOVED AND FOUND OTBD ANGLE BETWEEN STRINGS 17 AND 18R TO HAVE THREE HOLES WITH PREVIOUS COUNTER BORES. REMOVED DAMAGED SECTION OF THE OTBD ANGLE, FABRICATED REPLACEMENT AND SPLICE ANGLE. INSTALLED REPLACEMENT ANGLE IAW EA 130464IR & ECRA 5360-01303. MAJOR REPAIR.

Part: FLOORBEAM — CORRODED (BS 1681) · corrosion level 2 · airframe 72,917 hrs · 26,758 cycles

DURING C1 CHECK, BS 1681 FLOORBEAM CORRODED.

Part: SKIN — DAMAGED (BS 740-860) · airframe 72,917 hrs · 26,758 cycles

DURING C1 CHECK, MULTIPLE DAMAGE NOTED ON FUSELAGE SKIN FROM BS 740-860 BETWEEN S26L-16R. REMOVED DAMAGE & REPAIRED SKIN REF EA130454 & ECRA 5330-04598.

Part: CREASE BEAM — CRACKED (BS 1681) · airframe 72,917 hrs · 26,758 cycles

DURING C1 CHECK, BS 1681 CREASE BEAM AT RBL 48 WAS FOUND CRACKED THRU THE HORIZONTAL FLANGE. REPAIRED IAW EA 130519, REV IR.

Part: FLOORBEAM — CORRODED (BS 324) · corrosion level 2 · airframe 72,917 hrs · 26,758 cycles

CABIN FLOORBEAM CORRODED BS 324, RBL 41-43 ON FWD EDGE. RII INSPECTION ACCOMPLISHED.

Part: FLOORBEAM — CORRODED (BS 377.7) · corrosion level 2 · airframe 72,917 hrs · 26,758 cycles

FWD PAX AREA BS 377.7, RBL 54 TO 56 FLOORBEAM HAS UPPER TEE CORRODED. REPAIRED IAW EA130361IR AND ECRA 5310-05748 THIS IS A CAT "A" REPAIR.

Part: FLOORBEAM — CORRODED (BS 1680) · corrosion level 2 · airframe 72,917 hrs · 26,758 cycles

FLOORBEAM BS 1680, LBL 50 FWD SIDE OF TEE UPPER AND LOWER SURFACE IS CORRODED. REPLACED FLOORBEAM BS 1680 LBL 60 TO RBL 60 IAW SRM 51-40-02 DWG 146N509, 1 EA 130412IR AND ECRA 5360-01298. MAJOR REPAIR.

Part: FLOORBEAM — CORRODED (BS 1660) · corrosion level 2 · airframe 72,917 hrs · 26,758 cycles

BS 1660 FLOORBEAM TEE CORRODED RBL 3 TO LBL 15. REPAIRED CABIN FLOORBEAM TEE IAW ECRA 5310-05563.

Part: SKIN — PUNCTURED (BS 1675) · airframe 72,917 hrs · 26,758 cycles

FUSELAGE SKIN HAS A PUNCTURE AT BS 1675, S22 & 23R. FABRICATED DOUBLER IAW SRM 53-00-01, INSURANCE CUT IAW SRM 53-00-01, REPAIR S, STEP 4. TREATED AND PRIMED IAW SRM 51-20-01. INSTALLED REPAIR IAW 53-00-01 AND 51-40-02, REPAIR 3. MAJOR REPAIR.

Part: STRINGER — DAMAGED (BS 1681 S19R) · airframe 72,917 hrs · 26,758 cycles

DURING REMOVAL OF STRINGER SPLICE ON S19R TO REPAIR FRAME AT BS 1681, FOUND AFT HOLES ELONGATED ON STRINGER. R & R STRINGER SECTION FROM BS 1681-1720, S19R.

Part: CREASE BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 72,917 hrs · 26,758 cycles

CREASE BEAM WEB AT R4 DOOR HAS CORROSION ON TOP SURFACE. REMOVED CORROSION DAMAGE IS 100 PERCENT OF THICKNESS OUT OF LIMITS IAW SRM 53-60-15. R & R BEAM IAW SRM 51-40-02 AND DWG 146N8122. MAJOR REPAIR.

Part: SKIN — DAMAGED (RUDDER) · airframe 72,917 hrs · 26,758 cycles

FROM LIGHTNING STRIKE INSPECTION, FOUND RUDDER DAMAGE ON T/E. T/E DAMAGE 20 INCHES FROM TOP WITH 1 X .5 INCHES DAMAGE REPAIRED IAW EA130389 REINSTALLED STATIC WICK IAW AMM 23-61-01 AND ECRA 5540-01344.

Part: RADOME — DAMAGED (FUSELAGE) · airframe 72,917 hrs · 26,758 cycles

EXTERNAL SURFACE NOSE RADOME, SEGMENTED LIGHTNING DIVERTER STRIP AT 2 O"CLOCK, MISSING TOO MANY SEQUENTIAL METALLIC BUTTONS. R & R RADOME. ADJUSTED RADOME & BONDING CHECK GOOD AMM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 72,917 hrs · 26,758 cycles

FLOORBEAM UPPER TEE FROM LBL 3 TO RBL 60 CORRODED. REMOVED DAMAGE TEE AND RESTORED IAW ECRA 5310-05536 REPAIR 3. FABRICATED AND INSTALLED REPAIR PARTS AND COMPLETED ALL WORK IAW ECRA 5310-05536. MAJOR REPAIR.

Part: FLOOR SUPPORT — CORRODED (BS 324-345) · corrosion level 2 · airframe 72,917 hrs · 26,758 cycles

BS 324 TO BS 345, RBL 56.5 FLOOR SUPPORT HAS SURFACE CORROSION. REMOVED FLOOR SUPPORT. INSTALLED NEW FLOOR SUPPORT IAW DWG 141N5160, SRM 53-00-04 AND AMM 20-11-00 AND AMM 51-31-01. MAJOR REPAIR.

Part: FLOORBEAM — CORRODED (BS 324 RBL 41-43) · corrosion level 2 · airframe 72,917 hrs · 26,758 cycles

FWD PAX COMPARTMENT, BS 324, RBL 41 TO 43, FLOORBEAM HAS CORROSION ON FWD EDGE. REMOVED CORROSION AND LOSS OF .030 IS OOL CUT AND REPAIRED DMG SECTION IAW SRM 53-10-08, REPAIR 1. FABRICATED PTS IAW SRM 53-10-08. INSTALLED REPAIR PARTS IAW 53-10-08 AND GNMM 5-0-6-007. MAJOR REPAIR

Part: SKIN — DENTED (BS 1598, S19R) · airframe 72,917 hrs · 26,758 cycles

SKIN DENTED BS 1598, S19R. CUT OUT DAMAGE AND INSTALLED DOUBLER REPAIR PER SRM 53-00-01 REPAIR 3. HFEC VERIFIED DAMAGE REMOVED REF NDT PT 6, 51-00-19. MAJOR REPAIR.

Part: SHEAR TIE — MISLOCATED (BS 1420) · airframe 72,917 hrs · 26,758 cycles

SKIN BUCKLED BS 1420, ABOVE S14R. REMOVED TWO MISLOCATED SHEAR TIES. NO SKIN BUCKLING NOTED. HFEC INSPECTED AREA HOLES AND SKIN, IAW NDT PT 6, 51-00-19, NO DEFECTS NOTED. INSTALLED SHEAR TIES IAW SRM 51-40-02 AND MM 25-21-05. MAJOR REPAIR.

Part: WEB — DAMAGED (BS 324) · airframe 72,917 hrs · 26,758 cycles

FOUND A .407 DIAMETER HOLE AT APPROX RBL 60 WEB. REMOVED AND REPLACED BS 324 WEB FROM RBL 31 TO RBL 69 IAW DWG 141N2930 AND SRM 51-40-02.

Part: FLOORBEAM — DAMAGED (BS 324) · corrosion level 2 · airframe 72,917 hrs · 26,758 cycles

BS 324 FLOORBEAM, RBL 56, WL 200, ATTACH FASTENER HOLE FOR ANGLE TO WEB OUT-OF-ROUND IN ANGLE. REPAIRED IAW EA 1304 11, REV IR, AND ECRA 5310-05724. MAJOR REPAIR.

Part: FLOORBEAM — CORRODED (BS 345) · corrosion level 2 · airframe 72,917 hrs · 26,758 cycles

BS 345 FLOORBEAM BL 52 TO 60 HAS CORROSION AROUND FASTENER HOLES. CUT OUT DAMAGE AND SLICED IN CORD REPAIR PER ECRA 5310-05536, REPAIR 3, TABLE IV, STEP 3. MAJOR REPAIR.

Part: STATIC LINE — FRAYED (L4 DOOR SLIDE) · airframe 72,917 hrs · 26,758 cycles

L4 DOOR ESCAPE SLIDE STATIC LINE FRAYED. ESCAPE SLIDE REPLACED.

Part: STIFFENER — DENTED (FWD CARGO DOOR) · airframe 72,917 hrs · 26,758 cycles

FORWARD CARGO DOOR, INTERIOR SIDE, LOWER EDGE, SECOND FROM AFT STIFFENER IS DENTED ON FLANGE. EVALUATED DENT AND FOUND TO BE OUT OF LIMITS IAW SRM 52-30-02. REMOVED AND REPLACED STIFFENER ANGLE IAW SRM 51-40-02 AND 51-40-05. MAJOR REPAIR.

Part: FLOOR SUPPORT — CORRODED (BS 316) · corrosion level 2 · airframe 72,917 hrs · 26,758 cycles

FWD PASSENGER COMPARTMENT BS 316 RBL 9 FLOOR SUPPORT HAS UPPER SURFACE CORRODED AROUND FASTENER HOLES. REMOVED AND REPLACED FLOOR SUPPORT BS 316 RBL 9 IAW SRM 51-10-02 AND DWG 141N5160 REV A.

Part: CHANNEL — CORRODED (BS 310.5-332.5) · corrosion level 2 · airframe 72,917 hrs · 26,758 cycles

FWD PASSENGER COMPARTMENT BS 310.5 TO 332.5 RBL 32 HAS UPPER CHANNEL SURFACE CORRODED. CORROSION MATERIAL LOSS WAS 100%. REMOVED AND REPLACED UPPER CHANNEL IAW SRM 51-40-02, SRM 53-00-04 AND DWG141N5160. MAJOR REPAIR

Part: SKIN — DENTED (BS 620) · airframe 72,917 hrs · 26,758 cycles

SKIN DENT BS 620, BELOW S18L. CUT OUT DAMAGED SKIN, FABRICATED REPAIR DOUBLER AND INSTALLED PER SRM 53-30-0 1, REPAIR 2, AND SRM 51-40-05. MAJOR REPAIR.

Part: SKIN — DENTED (BS 340 S18L) · airframe 72,911 hrs · 26,754 cycles

DENT BELOW L1 DOOR APPROXIMATELY BS 340 S18 AT SKIN LAP 8.5L BY 7.5W BY .150 DEEP. REMOVED SHEAR TIE. COMPLIED WITH REPAIR PER ECRA 5330 04470 AND AVO ESC 130317-5426-1A, 130317-5426-1, 130316-5426-1.

Part: BOTTLE — NO TEST (RT OVRWING SLIDE) · airframe 72,603 hrs · 26,655 cycles

RIGHT EMERGENCY ESCAPE SLIDE BOTTLE TEST FAILED. . REPLACED RIGHT EMERGENCY ESCAPE SLIDE BOTTLE PER AMM, OPS CHECKED NORMAL.

Part: SHOULDER BELT — FRAYED (COCKPIT) · airframe 72,281 hrs · 26,548 cycles

F/O'S LEFT SHOULDER HARNESS EDGE IS FRAYED AND WORN ON EDGE. REMOVED AND REPLACED F/O'S SHOULDER HARNESS ASSY, OPS CHECKS GOOD.

Part: WARNING LIGHT — FALSE ACTIVATION (RT ENGINE) · airframe 70,784 hrs · 26,030 cycles

AFTER TAKEOFF, RECEIVED STATUS MESSAGE RT ENGINE SEC CONT. MESSAGE CLEARED WHILE ACCOMPLISHING PRE-FLIGHT, AND HAS NOT RETURNED. OK TO CONTINUE.

Part: PIN — MISSING (FIRE BOTTLE) · airframe 69,186 hrs · 25,477 cycles

PIN MISSING FROM FIRE EXTINGUISHER MID CABIN. REPLACED PIN AND SEAL.

Part: ACTUATOR — FAULTY (RUDDER TRIM) · airframe 68,325 hrs · 25,155 cycles

RUDDER FAILED TO TRIM IN EITHER DIRECTION. REPLACED RUDDER TRIM ACTUATOR PER MM.

Part: SKIN — NICKED (FUSELAGE) · airframe 68,323 hrs · 25,154 cycles

BELLY HAS SMALL NICKS OVER THAT ENTIRE AREA OF SKIN. REPAIRED IAW EVA-81393.

Part: FEEDER CABLE — DAMAGED (EMERGENCY LIGHT) · airframe 68,323 hrs · 25,154 cycles

EMERGENCY LIGHTS INOPERATIVE ROW 36 AFT. REPLACED POWER LEAD BETWEEN ROW 38&39 FROM POWER SUPPLY TO EMERGENCY LIGHT AT 38, COVER INSTALLED.

Part: BLADE — DAMAGED (NR 1 ENGINE) · airframe 68,319 hrs · 25,152 cycles

DURING LANDING, NR 1 ENGINE INGESTED WHAT APPEARS TO BE FLOCK OF BIRDS. HIT TWO HAWKS ON RUNWAY JUST WHEN APPLYING REVERSE. FELT THUMPS THEN NOTICED LEFT ENGINE HAD DIED. ALL BLADES & INLET DAMAGE. NR 2 ENGINE HAS MULTIPLE BLADE DAMAGE.

Part: FLOORBEAM — CRACKED (BS 700) · airframe 67,148 hrs · 24,718 cycles

STA 700 FLOORBEAM CRACKED. REPAIRED PER UA EVA 80851 ACP ON SMB W-U F5524P.

Part: COVER — DAMAGED (CABIN) · airframe 66,977 hrs · 24,655 cycles

FOUND EEL TRACK COVER BROKEN LAST 4-5 ROW SEATING. ACP INTERIM REPAIR WITH TAPE 912-0889 TO SECURE EEL TRACK. EEL LIGHT OPERATION IS NOT OBSTRUCTED. WILL NEED 1EA 560-0801 EEL TRACK (ISSUE AS 24FT) REPLACED AT NEXT MAINT OPPORTUNITIY. WILL NEED 560-0801 EEL TRACK COVER & 560-0802 TRACK BASE REPLACED. COVERS REPLACED BY THE CABIN CREW. OK FOR SVC. CLEARED DEFERRAL.

Part: COVER — UNSECURE (CABIN) · airframe 66,804 hrs · 24,592 cycles

CREW REPORT: EMERGENCY EXIT LIGHT COVER FELL OFF AT 17ABC. REPLACED EMERGENCY LIGHT STRIP COVER.

Part: DOOR — DAMAGED (RT MLG) · airframe 66,526 hrs · 24,482 cycles

FOUND RT MAIN GEAR DOOR MISSING ALL DOUBLER REPAIR PLIES-GRAPHITE-AT LOCATION 50 INCH AFT OF LEADING EDGE AND 12 INCH DOWN FROM HINGE LINE LOCATION IS OUTER SKIN AT RETRACT ACTUATOR ATTACH BRACKET FWD FASTENERS AREA. DAMAGE IS IN CRITICAL AREA. REMOVED DOOR AND SENT TO SHOP. DOOR WAS REMOVED AND ROUTED TO SHOP AND REINSTALLED PER MM.

Part: RADOME — DAMAGED (NOSE) · airframe 63,763 hrs · 23,431 cycles

BIRD STRIKE ON RADOME. COMPLETED BIRD STRIKE INSP 05-51-18-201 AND CLEANED RADOME REF 12-25-00. FOUND SEGMENTED L IGHTING DIVERTER STRIP DISBONDED AT STA 166 0N UPPER RT OF RADOME MISSING PAINT ABOUT 1. NO OTHER DAMAGE FOUND REF MM 53-12 -03 P 201 PAR 2(A). DIVERTER STRIP TAPED WITH NON METALIZED TAPE 853. REPAIR DIVERTER STRIP REF MM 53-12-03 OR REPLACE RADOME WITHIN 300 FT HR, INP EVERY 50 FT HR TIL REPAIR. SECURED AREA OF METALLIC BUTTONS. PRIMED AND PAINTED AREA.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 62,381 hrs · 22,911 cycles

RT OVERWING EXTERIOR EVAC LT INOPERATIVE. RELAMPED. OP CKS OKAY.

Part: SKIN — DELAMINATED (THRUST REVERSER) · airframe 62,011 hrs · 22,763 cycles

NR 2 ENGINE OUTER REVERSER, RT UPPER BIFURCATION PANEL INNER SKIN DELAMINATED 36 BY 7 INCH APPROX 257 INCH. ACCOMPLISHED BIFURCATION REPAIR. REMOVED, RE-INSTALLED AND OP CHECKED REVERSER.

Part: ENGINE — BIRD INGESTION (NR 2) · airframe 61,401 hrs · 22,533 cycles

BURNING ODOR IN CABIN ON FINAL. FOUND BIRD DEBRIS IN THE NR 2 ENGINE INLET. ACCOMPLISHED BORESCOPE INSPECTION, CLEANED ENGINE. INSPECTED AIRCRAFT FOR FURTHER DAMAGE AND ACCOMPLISHED PACK BURNOUT. THE OIL CONSUMPTION HISTORY OF BOTH ENGINES AND THE APU ARE NORMAL. A STRONG ODOR ON TAKE-OFF WAS REPORTED ON THE NEXT FLIGHT BUT DISSIPATED DURING FLIGHT. SUSPECTED FROM BIRD STRIKE ON PREVIOUS FLIGHT. PERFORMED PACK BURNOUT FOR 10 MINUTES ON HIGH, NO ODOR DETECTED

Part: SLIDE — TORN (OVERWING EXIT) · airframe 61,229 hrs · 22,465 cycles

RT OVERWING SLIDE INSIDE PACK IS TORN, PACK COMING LOOSE. REPLACE SLIDE ON WU R7806N.

Part: CABLE — FAULTY (CABIN) · airframe 60,381 hrs · 22,125 cycles

EMERGENCY FLOOR LIGHT COVER CAME OFF AT ROW 18. REPLACED POWER CABLE FROM WALL TO FLOOR LIGHTING STRIP AND REPLACED COVER OVER FLOOR LIGHTS IN ROW 18 AREA. CHECK OK.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 60,179 hrs · 22,040 cycles

FWD RT OVERWING EMERGENCY LIGHT IS INOP. REPLACED LAMP, OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 59,696 hrs · 21,842 cycles

RT FWD OVER WING SLIDE EMERGENCY EXIT LIGHT INOP. RELAMPED, OPS CK GOOD.

Part: LANYARD — OUT OF POSITION (EVAC SLIDE) · airframe 59,460 hrs · 21,754 cycles

DOOR 1R, HAS LANYARD HANGING FROM DOOR SLIDE. RE-INSTALLED LANYARD INTO SLIDE PACK.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 58,267 hrs · 21,302 cycles

RIGHT HAND EXTERIOR OVERWING FWD EMERGENCY LIGHT INOP. *S/D* BULB INOP. REPLACED LIGHT BULB, CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 52,959 hrs · 19,503 cycles

DOOR 1L, 2L AND 3L EXTERIOR EMERGENCY LIGHTS INOP. *S/D* BULBS INOP. REPLACED BULBS, OPERATES NORMALLY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 57,695 hrs · 21,096 cycles

CREW REPORT, MULTIPLE SECTIONS EMERGENCY LIGHTS INOP IN COACH. EMERGENCY LIGHT SYS IS STILL INOP AT DOOR 4L. TEST SW10295 IS INOP. WHILE AC IS ONLY BEING SUPPLIED BY GROUND SERVICE BUSS AFTER A TIME DELAY OF ABOUT 20 MINUTES THE GROUP OF EMERGENCY LIGHT PWR SUPPLYS THAT ARE IN SERIES WITH DOOR 4L TEST SW TURN ON AND DRAIN BATTERY PACKS. ALL OK WHEN ON SHIPS PWR. FOUND CONTACT FROZEN. REPLACED S10295 AT DOOR 4L BECAUSE CONTACTS C (COMMON) AND NO (NORM OPEN) STUCK CLOSED CAUSING LIGHTS TO COME ON WITH AIRCRAFT POWER ON AND OFF SEQUENCE AND GND PWR SEQUENCE, EMERG LGHTS OP CK OK.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 57,695 hrs · 21,096 cycles

FOUND EEL FLOOR LIGHTS INOP AT AFT LAV, ROWS 34 THRU 30, ROWS 22 THRU 16 AND EMERGENCY AISLE LIGHTS INOP AT ROWS 34 THRU 26 BOTH SIDES AND ROWS 18 THRU 14 LT SIDE. FOUND INVERTER FAILED. REPLACED INVERTER AT ROW 17ABC LT BATTERY PACK REPLACED AT M10818 AND FUSES CHKD ON PWR SUPPLY AT M735.ORANGE EGRESS EEL LIGHT STRIP AND FC EEL LIGHT STRIP REPLACED.

Part: OXYGEN SYSTEM — READS LOW (CREW) · airframe 57,679 hrs · 21,089 cycles

CREW REPORTS CREW O2 LOW AT 1120 PSI. SERVICE CREW O2, NO LEAKS NOTED AT TIME OF SERVICE.

Part: GIRT BAR — OBSTRUCTED (DOOR 2L) · airframe 56,704 hrs · 20,738 cycles

SLIDE LT DOOR 2R INOPERATIVE. *S/D* GIRT BAR NOT ENGAGING FULLY DUE TO DEBRIS. CLEANED GIRT BAR FITTINGS AND DOOR ARMING SYSTEM OPERATES NORMALLY.

Part: SLIDE — INOPERATIVE (L2 DOOR) · airframe 56,704 hrs · 20,738 cycles

SLIDE LEFT DOOR 2R INOPERATIVE.

Part: SOCKET — FAILED (DOOR LIGHT) · airframe 56,666 hrs · 20,727 cycles

DOOR 2R ARMED LIGHT FAILS TO ILLUMINATE WHEN DOOR ARMED. LIGHT SOCKET HAD BECOME LOOSE. RESEATED LIGHT SOCKET AND ASSY CHECKS OK.

Part: LIGHT — INOPERATIVE (EVAC SLIDE) · airframe 56,646 hrs · 20,721 cycles

SLIDE BOTTLE LIGHT AT DOOR 2R WON'T ILLUMINATE. REMOVED LIGHT LENS CAP AND REINSTALLED FOUND LIGHTS OPERATING NORMALLY

Part: BATTERY PACK — FAULTY (EMERGENCY LIGHTS) · airframe 56,613 hrs · 20,705 cycles

EMERGENCY LIGHT SIGN AT DOOR 3R IS ILLUMINATED AS WELL AS SEVERAL FLOOR PATH LIGHTS IN SEVERAL AREAS WITH EMERGENCY LIGHTS IN OFF AS WELL AS ARMED. BATTERY PACK FAILURE. REPLACED BATTERY PACKS M10817 AND M10818. EMER LIGHTS OPERATE NORMALLY.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 56,549 hrs · 20,683 cycles

EXTERIOR EMERGENCY LIGHTS INOP AT RT AFT OVERWING AND BOTH LEFT OVERWING LIGHTS. FOUND BATTERY FAULTY. REPLACED BATTERY.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 56,549 hrs · 20,683 cycles

SEATS 9ABC THRU 21ABC EMERGENCY LIGHTS INOP. FOUND POWER SUPPLY FAULTY. REPLACED POWER SUPPLY M107, OPS CHECKED NORMALLY.

Part: SIGN — SHORTED (LT OVERWING) · airframe 56,549 hrs · 20,683 cycles

L4 LEFT OVERWING AND R4 EXTERNAL EMERGENCY LIGHTS INOP. FOUND SIGN AT L4 LEFT O/W DOOR SHORTED INTERNALLY. REPLACED SIGN AT LEFT O/W DOOR, OPS TESTED NORMAL.

Part: SKIN — DENTED (BS 271 S20L) · airframe 56,549 hrs · 20,683 cycles

FUSELAGE EXT SKIN IS DENTED AT APPROX BS 271, JUST BELOW STR 20L. ACCOMPLISHED MAJOR REPAIR.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHTS) · airframe 56,549 hrs · 20,683 cycles

SEATS 30-34ABC EMERGENCY LIGHTS INOP. FOUND LOOSE CONNECTOR. RECONNECTED LOOSE CONNECTOR- ALL TESTS ARE NORMALLY.

Part: SKIN — GOUGED (L1 DOOR) · airframe 56,549 hrs · 20,683 cycles

L-1 DOOR OUTER SKIN GOUGED AT LOWER END OF DOOR PAN. ACCOMPLISHED MAJOR REPAIR.

Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 56,549 hrs · 20,683 cycles

FOUND DOOR 2L EMERGENCY LIGHT JIFFY SPLICE IS BROKEN. REMOVED AND REPLACED JIFFY SPLICE, OPS CHECKED NORMALLY.

Part: FITTING — CRACKED (NR 2 PYLON) · airframe 56,549 hrs · 20,683 cycles

NR 2 PYLON CROSS TIE FITTING HAS A CRACK ON THE OUTBOARD ATTACH FASTENER LOCATION AT NAC STA 107.7. ACCOMPLISHED MAJOR REPAIR.

Part: SKIN — DAMAGED (R2 DOOR CUTOUT) · airframe 56,549 hrs · 20,683 cycles

FOUND DOOR R2 UPPER HINGE CUTOUT HAS DAMAGE. ACCOMPLISHED MAJOR REPAIR.

Part: GATE — CRACKED (R1 DOOR) · airframe 56,549 hrs · 20,683 cycles

FOUND DOOR R1 UPPER GATE HAS 2 CRACKS, ONE AT EACH END. REMOVED AND REPLACED UPPER GATE.

Part: GATE — DAMAGED (R4 DOOR) · airframe 56,549 hrs · 20,683 cycles

R-4 DOOR LOWER GATE MATING SURFACE WORN AND CORRODED IN SEVERAL AREAS ALONG EDGES. INSTALLED NEW GATE.

Part: GATE — CRACKED (R1 DOOR) · airframe 56,549 hrs · 20,683 cycles

DOOR R1 LWR GATE CRACKED AND CORRODED. REMOVED & REPLACED GATE.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 56,549 hrs · 20,683 cycles

CABIN FLOORBEAM UPPER FLANGE CRACKED AT RADIUS AT BS 700 LBL 25. ACCOMPLISHED MAJOR REPAIR.

Part: STRUCTURE — DAMAGED (L2 DOOR) · airframe 56,549 hrs · 20,683 cycles

DOOR L2 UPPER HINGE CUTOUT HAS DAMAGE. ACCOMPLISHED MAJOR REPAIR.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 56,549 hrs · 20,683 cycles

FUSELAGE FRAME OUT OF LIMITS AT BS 740 STR 27L. ACCOMPLISHED MAJOR REPAIR AT GSO.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 56,549 hrs · 20,683 cycles

MAIN CABIN FLOORBEAM UPPER CHORD CORRODED BS 324 RBL 50 TO 62 WL 207. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGED T-CHORD. FABRICATED & INSTALLED NEW T-CHORD.

Part: WARNING LIGHT — ILLUMINATED (STAB TRIM) · airframe 56,519 hrs · 20,674 cycles

STAB TRIM LIGHT ILLUMINATED AFTER T/O,TRIM FELT LIKE REDUCED RATE.

Part: LIGHT — DISCONNECTED (CABIN) · airframe 56,298 hrs · 20,602 cycles

EMERGENCY LIGHT ON OVERHEAD AISLE DISCONNECTED AND HANGING LOOSE. SECURED LIGHT ASSEMBLY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 55,858 hrs · 20,428 cycles

ONE SEGMENT OF EEL LAMP AT ROW 3 IS CUT OFF. ALSO THE LAST SEGMENT OF EEL LAMP AT ROW 32 IS INOP. REPLACED WITH LAMP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 55,858 hrs · 20,428 cycles

EEL LAMP IN FRONT OF MID LAV IS COVERED BY CARPETING AND INOP. 10-11-07 REMOVED CARPET FROM OVER LIGHT ASSEMBLY. MADE PERMANENT REPAIR TO LIGHT ASSEMBLY POWER LEAD,

Part: POWER CABLE — OUT OF POSITION (CABIN) · airframe 55,858 hrs · 20,428 cycles

EEL LAMP AT ROW 31 IS PARTIALLY COVERED BY POWER CABLE. 10-11-07 INSTALLED LAMP OVER POWER CABLE. LAMP NOW FULLY VISIBLE. NO NEED FOR ANY REPLACEMENT OF COMPONENTS.

Part: COFFEEMAKER — SMOKE (GALLEY) · airframe 55,539 hrs · 20,300 cycles

FOUND SMOKE IN CABIN. SMOKE IN CABIN CAUSED BY A BURNED COFFEE PACK. COFFEE PACKET WAS ON THE DUAL COFFEE WARMER IN FLIGHT AND WAS SMOLDERING. CLEANED AREA AND OPERATED WARMING PLATES FOR 30 MINUTES. EVERYTHING CHECKED NORMAL AND BACK PLATE WAS COOL.

Part: BOTTLE — NO TEST (R2 DOOR SLIDE) · airframe 54,099 hrs · 19,782 cycles

2R EMERGENCY ESCAPE SLIDE FAILS TEST. [SUP 05-22-07] REMOVED AND REPLACED BOTTLE ASSY. OPERATIONAL TEST OK.

Part: CONNECTOR — DIRTY (ESCAPE SLIDE) · airframe 54,079 hrs · 19,776 cycles

EMERGENCY ESCAPE SQUIB TEST INOP, RIGHT SQUIB TEST POSN TWO. [SUP 05-22-07] CLEANED CONNECTOR. OPS CHECKED NORMAL.

Part: WARNING MESSAGE — ILLUMINATED (RT ENGINE) · airframe 53,210 hrs · 19,456 cycles

RT ENGINE HIGH STAGE LIGHT ILLUMINATED AND RT ENGINE HIGH STAGE EICAS MSG IN CLIMB. REPLACED HIGH STAGE PILOT VALVE AND 14TH STAGE PILOT CONTROLLER.

Part: SHEAR TIE — DENTED (FUSELAGE) · airframe 52,948 hrs · 19,373 cycles

DENT FOUND IN LEFT SIDE OF FUSELAGE 30 INCHES DOWN FROM DOOR 1 LEFT, DENT IS IN LAP JOINT AROUND 0.125 DEEP, 6 INCHES LONG AND 3 TO 4 INCHES WIDE. DENT AT STRINGER STA 345. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGED SHEAR TIE. FABRICATED AND INSTALLED NEW SHEAR TIE.

Part: BOTTLE — LOW (ESCAPE SLIDE) · airframe 52,320 hrs · 19,165 cycles

LOW BOTTLE PRESSURE REMOVED VALVE FOR OVERHAUL, REPLACED WITH OVERHAULED VALVE. SUSPECT VALVE DID NOT SHOW ANY LEAKAGE AFTER 2 HOUR LEAK TEST. REPLACED WITH ANOTHER BOTTLE AND A VALVE. RESULTS INCONCLUSIVE.

Part: SMOKE — DETECTED (COCKPIT) · airframe 48,485 hrs · 17,798 cycles

STRONG SMOKE ODOR IN FLIGHT DECK AND SMOKE ODOR AT ROW 16. THE SMELL IN THE CABIN WAS CORRECTED BY SEVERAL RELATED ACTIONS DURING THE TROUBLESHOOTING OF THE AIRCONDITIONING SYSTEM. THE PACKS WERE RECYCLED AND SEVERAL FILTERS WERE REPLACED. NOTE: OVEN WAS REMOVED AND SENT TO HOMESHOP FOR INSPECTION AND SERVICE. NO FINDINGS REPORTED TO INDICATE MALFUNCTION WITH AN OVEN.

Part: SENSOR — FAILED (MIX MANIFOLD) · airframe 47,414 hrs · 17,405 cycles

COCKPIT TEMPERATURE RISING & UNCONTROLLABLE. CAUSE ATTRIBUTED TO A MIX MANIFOLD SENSOR. REPLACED SENSOR.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 46,778 hrs · 17,152 cycles

FUSELAGE SKIN AT STA 1600 STR 14R IS DAMAGED. SUPPLEMENTAL DATA UPDATE DENT DAMAGE CAUSED BY IMPACT WITH FUSELAGE SKIN. MAJOR REPAIR ACCOMPLISHED. SKIN DAMAGE WAS CUTOUT AND REPAIR DOUBLER AND STRUCTURAL FILLER INSTALLED.

Part: PROXIMITY SENSOR — INOPERATIVE (L2 DOOR) · airframe 46,151 hrs · 16,905 cycles

DOORS 2L AND 2R ARMED LTS DO NOT COME ON WITH DOORS ARMED. GIRT BAR ANN LIGHT L406 FOR DOOR 2R FOUND SHORTED - REPLACED LIGHT. 2R FORWARD AND REAR PROXIMITY SENSORS FOUND BAD - BOTH SENSORS REPLACED.

Part: SKIN — DEBONDED (NR 6 SLAT) · airframe 45,603 hrs · 16,694 cycles

RIGHT INBOARD LEADING EDGE WEDGE DISBONDED FROM SLAT. *S/D* A SECTION OF THE NR 6 SLAT TRAILING EDGE WEDGE SEPARATED FROM THE SLAT ASSEMBLY. DURING DISASSEMBLE OF THE SLAT WEDGE FOR REPAIR, COMPONENT SHOP FOUND EVIDENCE OF CORROSION ON THE ALUMINUM HONEYCOMB CORE AND SKIN WHICH ALSO MIGHT BE THE CAUSE OF THE DISBOND OF THE SLAT WEDGE. REPLACED TRAILING EDGE WEDGE.

Part: WEDGE — DELAMINATED (NR 6 SLAT)

T/E WEDGE DELAMINATION MAJOR REPAIR ACCOMPLISHED.REPAIRED T/E WEDGE.

Part: SKIN — DENTED (FUSELAGE) · airframe 42,120 hrs · 15,469 cycles

LT EXTERNAL FUSELAGE SKIN HAS 4 EA DENTS AT STATION 600-620 AND BETWEEN STR 15-17. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 38,534 hrs · 14,144 cycles

HOLE IN FUSELAGE FWD OF MID LAV SERVICE PANEL. HOLE IS LOCATED 2 INCHES ABOVE STRINGER 226 AT APPROX STA 691. HOLE MEASURES .75 INCH IN DIAMETER. MAJOR REPAIR ACCOMPLISHED. INSTALLED REPAIR DOUBLER.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 37,781 hrs · 13,857 cycles

AFT CABIN STATION 1681 RBL 53 CORROSION BETWEEN FLOORBEAM CAP AND PRESSURE DECK. MAJOR REPAIR ACCOMPLISHED. INSTALLED FLOORBEAM CAP SPLICE.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 37,781 hrs · 13,857 cycles

CABIN AFT SHEAR DECK UPPER SURFACE CORROSION WITH EXCESSIVE MATERIAL LOSS STATION 1680 TO 1682 LBL 10 TO LBL 41. MAJOR REPAIR ACCOMPLISHED. DOUBLER AND TWO ANGLES INSTALLED.

Part: INTERCOSTAL · airframe 37,781 hrs · 13,851 cycles

AFT CABIN BETWEEN STATION 1640 TO STA 1660, BL0, INTERCOSTAL NEEDS REMOVAL FOR ACCESS. MAJOR REPAIR ACCOMPLISHED. INTERCOSTAL REMOVED AND REINSTALLED WITH NEW ANGLES AND SPACERS.

Part: SKIN — DENTED (FUSELAGE) · airframe 37,781 hrs · 13,857 cycles

LEFT HAND EXTERNAL FUSELAGE HAS A 6 INCH VERTICAL DENT AT BODY STATION 760 BETWEEN STRINGER 15L TO 16L. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR.

Part: FRAME — DENTED · airframe 37,781 hrs · 13,857 cycles

AFT PIT FRAME FLANGE DENT STATION 1440 AT STRINGER 26L. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGE AND INSTALLED DOUBLER.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 37,781 hrs · 13,857 cycles

CABIN CREASE BEAM INNER CHORD BODY STATION 740 TO BODY STATION 757 CORRODED. MAJOR REPAIR ACCOMPLISHED. REPLACED CREASE BEAM INNER CHORD.

Part: PLATE — CORRODED (FUSELAGE) · airframe 37,781 hrs · 13,857 cycles

AFT CABIN DECK PLATE AT STATION 1680 AND RBL 25 CORRODED. MAJOR REPAIR ACCOMPLISHED. DECK PLATE REPAIR DOUBLER INSTALLED.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 37,781 hrs · 13,857 cycles

CABIN FLOORBEAM UPPER CAP HAS EXCESSIVE MATERIAL REMOVED AT STATION 365. MAJOR REPAIR ACCOMPLISHED. INSTALLED STRAP AND ANGLE REPAIR ON FLOORBEAM.

Part: FRAME — GOUGED (FUSELAGE) · airframe 37,781 hrs · 13,857 cycles

FORWARD CARGO COMP STATION 740 FUSE FRAME UPPER CAP GOUGED ABOVE STRINGER 28L LBL 12. MAJOR REPAIR ACCOMPLISHED. INSTALLED UPPER CAP STRAP REPAIR.

Part: FRAME — GOUGED · airframe 37,781 hrs · 13,857 cycles

FORWARD PIT FRAME STATION 720 UPPER FLANGE UPPER SURFACE GOUGED. MAJOR REPAIR ACCOMPLISHED. INSTALLED INTERNAL STRAP.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 37,781 hrs · 13,857 cycles

TOP CAP OF FLOORBEAM CORRODED. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR.

Part: FLANGE — DENTED · airframe 37,781 hrs · 13,857 cycles

AFT PIT FRAME INBOARD FLANGE DENT STATION 1420 AT STRINGER 26L. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. DAMAGE REMOVED. EXTERNAL DOUBLER INSTALLED.

Part: FLANGE — DENTED · airframe 37,781 hrs · 13,857 cycles

AFT PIT FRAME INBOARD FLANGE TWO DENTS AT STATION 1400 AT STRINGER 25L AND 26L. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. DAMAGE REMOVED. EXTERNAL DOUBLER INSTALLED.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 37,781 hrs · 13,857 cycles

CABIN FLOORBEAM CORRODED AFT UPPER FLANGE UPPER AND LOWER SURFACES STATION 377 LBL 58. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGE AND INSTALLED DOUBLER AND TRIPLER.

Part: HYDRAULIC LINE — FAILED (HYDRAULIC SYS) · airframe 37,729 hrs · 13,837 cycles

LEFT MAIN GEAR DOWNLOCK ACTUATOR LINE RUPTURED. LOSS OF LEFT HYDRAULIC SYSTEM. FATIGUE FAILURE OF HOSE IN BRAIDS AT SWAGGED B-NUT END. REPLACED HOSE.

Part: STATOR — FAILED (LT ENGINE)

PASSING FL280 LEFT ENGINE INSTRUMENTS RAPIDLY ROLLED BACK. FLIGHT ATTENDANT REPORTED LEFT ENGINE ON FIRE. LEFT ENGINE WAS SHUTDOWN. AIRCRAFT RETURNED TO LAX. *S/D* UPON ARRIVAL AT LAX FOUND METAL IN THE TAILPIPE DUE TO AN HPC FAILURE, THE FIRE WAS INTERNAL DUE TO THE FAILURE. THE ENGINE WAS REPLACED. SHOP FINDINGS WERE THAT A 10TH STAGE HPC STATOR HAD FAILED. THIS FAILURE IS A KNOWN MODE AND THIS EVENT IS STILL UNDER INVESTIGATION BY UA AND PWA.

Part: REGULATOR — FAILED (EXCAPE SLIDE)

SLIDE REMOVED FOR TIME CONTROLLED OVERHAUL. DURING FLAT FIRE, BOTTLE VALVE FAILED TO FULLY OPEN DUE TO DAMAGED ROTATION SHAFT AND PIN. OVERHAULED VALVE, REPLACED SHAFT AND CONTACTED MANUFACTURER.

Part: BULB — FAILED (RT MLG)

RIGHT LANDING GEAR HAD NO INDICATION WITH GEAR DOWN AND FLAPS AT 30 DEGREES. WITH GEAR DOWN AND THROTTLES AT IDLE NO HORN. COMPLETED TOWER FLYBY FOR GEAR DOWN VERIFICATION. LANDED UNDER AMBER ALERT. SUPPLEMENTAL DATA UPDATE: RIGHT MAIN LANDING GEAR INDICATOR LIGHT HAD A BURNED OUT BULB. RELAMPED OPERATION CHECKS NORMAL.