N526UA
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| UNITED AIRLINES INC | Operator | 2011-09-26 – 2011-09-26 | Operator named in NTSB report |
| UNITED AIRlNES INC | Operator | 2011-09-26 – 2011-09-26 | Operator named in NTSB report |
| UNITED AIRLINES INC | Operator | 2011-05-31 – 2011-05-31 | Operator named in NTSB report |
| UNITED AIRLINES, INC. (CALA) | Operator | 2011-05-31 – 2011-05-31 | Operator named in NTSB report |
Accident & incident history
Maintenance disclosures
CABIN ALTITUDE 10,000 FEET AT FL300, DIVERTED. FOUND SECONDARY HEAT EXCHANGER BLOWN OUT AT LOWER END. REPLACED IAW AMM 21-51-02.
BS 1420 BETWEEN STRINGER 28R & 29R SHEAR TIE HAS DAMAGED HOLE. FABRICATED & INSTALLED NEW SHEAR TIE IAW SRM 51-30-01 & 51-40-05.
AFT PIT BS 1440 FRAME INBD CHORD CRACKED AT RBL 11. REMOVED DAMAGE, FABRICATED & INSTALLED REPAIR PARTS IAW ECRA 5360-01389.
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.
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.
AFT PIT BS 1380 RBL 3 FRAME SHEAR TIE CORROSION. REMOVED DAMAGE, FABRICATED & INSTALLED NEW SHEAR TIE IAW SRM 51-40-02.
NUMBER 1 PYLON AFT FAIRING FRAME AT OTBD END, PREVIOUS REPAIR GOUGED. REMOVED DAMAGE, FABRICATED & INSTALLED REPAIR PARTS IAW SRM 51-70-11.
EXT FUSE SKIN BS 430 STRINGER 15L, DENT. FABRICATED & INSTALLED REPAIR DOUBLER & FILLER IAW SRM 53-00-01.
AFT PIT BS 1472 STRINGER 29R CORROSION. FABRICATED & INSTALLED NEW STRINGER 29R FROM BS 1460 TO 1488 IAW SRM 53-00-03.
RIGHT EMPENNAGE BS 1787 STRINGER 17R - 19R. FIXED FAIRING PANEL CRACKED. FABRICATED & INSTALLED REPAIR PARTS IAW ECRA 5387-01001.
BS 1520 FRAME SPLICE ABOVE STRINGER 23R, MULTIPLE GOUGES. FABRICATED & INSTALLED NEW SPLICE IAW DWG 146N1042 & SRM 51-30-01.
FORWARD PIT BS 660 LT, FRAME SPLICE PLATE CORROSION. REMOVED DAMAGE, FABRICATED & INSTALLED NEW SPLICE PLATE IAW SRM 51-40-05 & 51-40-02.
CABIN FLOOR STRUCTURE BS 940 - 960 STRINGER 17L LT CREASE BEAM INTERCOSTAL UPPER SURFACE CORRODED. R & R CREASE BEAM.
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.
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.
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.
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.
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.
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.
FWD CARGO DOOR HANDLE ISSUE. REPLACED FWD CARGO PIT DOOR'S EXTERNAL HANDLE FAIRING BUMPER.
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.
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.
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.
EMERGENCY LIGHTING STRIP LIFTING OFF FLOOR. SECURED LOOSE EMERGENCY LIGHTING STRIP.
ARMED LIGHT FOR DOOR 1R WILL NOT ILLUMINATE. REPLACED LAMPS ARM LIGHT ABOVE DOOR. ARMING SEQUENCE NORMAL.
APU FAULT LIGHT ON, SHUTDOWN. REPLACED BATTERY CHARGER & REPLACED BATTERY IAW MM 24-31-03.
NR 1 FAN BLADE ON RT ENGINE HAS NICK NEAR THE TIP. INSPECTED AND REPAIRED NR 1 ENG FAN BLADE IAW MM.
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.
L1 DOOR EXIT LIGHT WIRE SPLICE BROKEN. SPLICED BROKEN WIRE IAW SWP 20-30-12. OPS CHECKED GOOD IAW AMM.
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.
CABIN FLOORBEAM CORRODED BS 324, RBL 41-43 ON FWD EDGE. RII INSPECTION ACCOMPLISHED.
DURING C1 CHECK, BS 1681 CREASE BEAM AT RBL 48 WAS FOUND CRACKED THRU THE HORIZONTAL FLANGE. REPAIRED IAW EA 130519, REV IR.
DURING C1 CHECK, CHAFE DAMAGE WAS FOUND ON THE RT INBD MAIN FLAP FRONT SPAR LOWER ANGLE. REPAIRED IAW EA 130508, REV IR.
DURING C1 CHECK, BS 1681 FLOORBEAM CORRODED.
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.
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.
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.
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.
BS 1660 FLOORBEAM TEE CORRODED RBL 3 TO LBL 15. REPAIRED CABIN FLOORBEAM TEE IAW ECRA 5310-05563.
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.
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.
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.
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.
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.
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.
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
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.
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.
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.
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.
L4 DOOR ESCAPE SLIDE STATIC LINE FRAYED. ESCAPE SLIDE REPLACED.
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.
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.
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.
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
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.
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.
RIGHT EMERGENCY ESCAPE SLIDE BOTTLE TEST FAILED. . REPLACED RIGHT EMERGENCY ESCAPE SLIDE BOTTLE PER AMM, OPS CHECKED NORMAL.
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.
AFTER TAKEOFF, RECEIVED STATUS MESSAGE RT ENGINE SEC CONT. MESSAGE CLEARED WHILE ACCOMPLISHING PRE-FLIGHT, AND HAS NOT RETURNED. OK TO CONTINUE.
PIN MISSING FROM FIRE EXTINGUISHER MID CABIN. REPLACED PIN AND SEAL.
RUDDER FAILED TO TRIM IN EITHER DIRECTION. REPLACED RUDDER TRIM ACTUATOR PER MM.
BELLY HAS SMALL NICKS OVER THAT ENTIRE AREA OF SKIN. REPAIRED IAW EVA-81393.
EMERGENCY LIGHTS INOPERATIVE ROW 36 AFT. REPLACED POWER LEAD BETWEEN ROW 38&39 FROM POWER SUPPLY TO EMERGENCY LIGHT AT 38, COVER INSTALLED.
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.
STA 700 FLOORBEAM CRACKED. REPAIRED PER UA EVA 80851 ACP ON SMB W-U F5524P.
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.
CREW REPORT: EMERGENCY EXIT LIGHT COVER FELL OFF AT 17ABC. REPLACED EMERGENCY LIGHT STRIP COVER.
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.
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.
RT OVERWING EXTERIOR EVAC LT INOPERATIVE. RELAMPED. OP CKS OKAY.
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.
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
RT OVERWING SLIDE INSIDE PACK IS TORN, PACK COMING LOOSE. REPLACE SLIDE ON WU R7806N.
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.
FWD RT OVERWING EMERGENCY LIGHT IS INOP. REPLACED LAMP, OPS CHECKED GOOD.
RT FWD OVER WING SLIDE EMERGENCY EXIT LIGHT INOP. RELAMPED, OPS CK GOOD.
DOOR 1R, HAS LANYARD HANGING FROM DOOR SLIDE. RE-INSTALLED LANYARD INTO SLIDE PACK.
RIGHT HAND EXTERIOR OVERWING FWD EMERGENCY LIGHT INOP. *S/D* BULB INOP. REPLACED LIGHT BULB, CHECKED GOOD.
DOOR 1L, 2L AND 3L EXTERIOR EMERGENCY LIGHTS INOP. *S/D* BULBS INOP. REPLACED BULBS, OPERATES NORMALLY.
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.
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.
CREW REPORTS CREW O2 LOW AT 1120 PSI. SERVICE CREW O2, NO LEAKS NOTED AT TIME OF SERVICE.
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.
DOOR 2R ARMED LIGHT FAILS TO ILLUMINATE WHEN DOOR ARMED. LIGHT SOCKET HAD BECOME LOOSE. RESEATED LIGHT SOCKET AND ASSY CHECKS OK.
SLIDE BOTTLE LIGHT AT DOOR 2R WON'T ILLUMINATE. REMOVED LIGHT LENS CAP AND REINSTALLED FOUND LIGHTS OPERATING NORMALLY
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.
SEATS 9ABC THRU 21ABC EMERGENCY LIGHTS INOP. FOUND POWER SUPPLY FAULTY. REPLACED POWER SUPPLY M107, OPS CHECKED NORMALLY.
SEATS 30-34ABC EMERGENCY LIGHTS INOP. FOUND LOOSE CONNECTOR. RECONNECTED LOOSE CONNECTOR- ALL TESTS ARE NORMALLY.
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.
FUSELAGE EXT SKIN IS DENTED AT APPROX BS 271, JUST BELOW STR 20L. ACCOMPLISHED MAJOR REPAIR.
EXTERIOR EMERGENCY LIGHTS INOP AT RT AFT OVERWING AND BOTH LEFT OVERWING LIGHTS. FOUND BATTERY FAULTY. REPLACED BATTERY.
L-1 DOOR OUTER SKIN GOUGED AT LOWER END OF DOOR PAN. ACCOMPLISHED MAJOR REPAIR.
FOUND DOOR 2L EMERGENCY LIGHT JIFFY SPLICE IS BROKEN. REMOVED AND REPLACED JIFFY SPLICE, OPS CHECKED NORMALLY.
NR 2 PYLON CROSS TIE FITTING HAS A CRACK ON THE OUTBOARD ATTACH FASTENER LOCATION AT NAC STA 107.7. ACCOMPLISHED MAJOR REPAIR.
FOUND DOOR R1 UPPER GATE HAS 2 CRACKS, ONE AT EACH END. REMOVED AND REPLACED UPPER GATE.
FOUND DOOR R2 UPPER HINGE CUTOUT HAS DAMAGE. ACCOMPLISHED MAJOR REPAIR.
R-4 DOOR LOWER GATE MATING SURFACE WORN AND CORRODED IN SEVERAL AREAS ALONG EDGES. INSTALLED NEW GATE.
DOOR R1 LWR GATE CRACKED AND CORRODED. REMOVED & REPLACED GATE.
CABIN FLOORBEAM UPPER FLANGE CRACKED AT RADIUS AT BS 700 LBL 25. ACCOMPLISHED MAJOR REPAIR.
DOOR L2 UPPER HINGE CUTOUT HAS DAMAGE. ACCOMPLISHED MAJOR REPAIR.
FUSELAGE FRAME OUT OF LIMITS AT BS 740 STR 27L. ACCOMPLISHED MAJOR REPAIR AT GSO.
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.
STAB TRIM LIGHT ILLUMINATED AFTER T/O,TRIM FELT LIKE REDUCED RATE.
EMERGENCY LIGHT ON OVERHEAD AISLE DISCONNECTED AND HANGING LOOSE. SECURED LIGHT ASSEMBLY.
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,
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.
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.
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.
2R EMERGENCY ESCAPE SLIDE FAILS TEST. [SUP 05-22-07] REMOVED AND REPLACED BOTTLE ASSY. OPERATIONAL TEST OK.
EMERGENCY ESCAPE SQUIB TEST INOP, RIGHT SQUIB TEST POSN TWO. [SUP 05-22-07] CLEANED CONNECTOR. OPS CHECKED NORMAL.
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.
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.
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.
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.
COCKPIT TEMPERATURE RISING & UNCONTROLLABLE. CAUSE ATTRIBUTED TO A MIX MANIFOLD SENSOR. REPLACED SENSOR.
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.
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.
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.
T/E WEDGE DELAMINATION MAJOR REPAIR ACCOMPLISHED.REPAIRED T/E WEDGE.
LT EXTERNAL FUSELAGE SKIN HAS 4 EA DENTS AT STATION 600-620 AND BETWEEN STR 15-17. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR.
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.
AFT CABIN STATION 1681 RBL 53 CORROSION BETWEEN FLOORBEAM CAP AND PRESSURE DECK. MAJOR REPAIR ACCOMPLISHED. INSTALLED FLOORBEAM CAP SPLICE.
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.
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.
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.
AFT CABIN DECK PLATE AT STATION 1680 AND RBL 25 CORRODED. MAJOR REPAIR ACCOMPLISHED. DECK PLATE REPAIR DOUBLER INSTALLED.
CABIN CREASE BEAM INNER CHORD BODY STATION 740 TO BODY STATION 757 CORRODED. MAJOR REPAIR ACCOMPLISHED. REPLACED CREASE BEAM INNER CHORD.
AFT PIT FRAME FLANGE DENT STATION 1440 AT STRINGER 26L. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGE AND INSTALLED DOUBLER.
CABIN FLOORBEAM UPPER CAP HAS EXCESSIVE MATERIAL REMOVED AT STATION 365. MAJOR REPAIR ACCOMPLISHED. INSTALLED STRAP AND ANGLE REPAIR ON FLOORBEAM.
FORWARD CARGO COMP STATION 740 FUSE FRAME UPPER CAP GOUGED ABOVE STRINGER 28L LBL 12. MAJOR REPAIR ACCOMPLISHED. INSTALLED UPPER CAP STRAP REPAIR.
FORWARD PIT FRAME STATION 720 UPPER FLANGE UPPER SURFACE GOUGED. MAJOR REPAIR ACCOMPLISHED. INSTALLED INTERNAL STRAP.
TOP CAP OF FLOORBEAM CORRODED. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR.
AFT PIT FRAME INBOARD FLANGE DENT STATION 1420 AT STRINGER 26L. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. DAMAGE REMOVED. EXTERNAL DOUBLER INSTALLED.
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.
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.
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.
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.
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.
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.