N604UA
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| UNITED AIRLINES, INC. (CALA) | Operator | on 1992-05-13 | Operator named in NTSB report |
Accident & incident history
Operated by UNITED AIRLINES (per NTSB report)
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
134 reports on file, 1995-09-18 – 2004-08-07.
Part: COMPRESSOR — STALLED (RT ENGINE) · airframe 75,873 hrs · 19,416 cycles
RT ENG COMPRESSOR EXPERIENCED A COMPRESSOR STALL. STALL STOPPED WHEN RT THROTTLE RETARDED. RESET BLEED ALL INDICATIONS NORMAL. ALL POST-COMPRESSOR STALL TROUBLESHOOTING ACCOMPLISHED IMMEDIATELY AFTER EVENT, NO DEFECTS FOUND. DECIDED TO WATCH ENG FOR ANY REPEAT STALLING, NO FURTHER ANOMALIES NOTED. ENGINE REMOVED AND INSTALLED ON ANOTHER AIRCRAFT FOR ENG REPOSITIONING PURPOSES ONLY WITH NO FURTHER STALLING EVENTS. THE AIRCRAFT AND ENGINE WAS RETIRED. CAUSE OF INITIAL EVENT WILL REMAIN 'UNKNOWN'. NO FURTHER ACTIONS REQUIRED.
Part: WARNING LIGHT — ILLUMINATED (TE FLAPS) · airframe 75,146 hrs · 19,270 cycles
LANDED LAX UNDER AMBER ALERT DUE TO FLAP DISAGREE INDICATION. ACCOMPLISHED FLAP POSITION TRANSMITTER SYNCHRONIZATION CHECK ON 3, 4, AND 5 FLAP POSITION TRANSMITTERS. FOUND NR 4 OUT OF LIMITS. ADJUSTED TRANSMITTER.
Earlier reports · 1995–2003 · 132 reports
2003
Part: SKIN — PUNCTURED (TAIL CONE) · airframe 71,732 hrs · 18,596 cycles
FUSELAGE TAILCONE SKIN AT STA 1848, LBL 24 PUNCTURED. MAJOR REPAIR ACCOMPLISHED. FABRICATED & INSTALLED REPAIR DOUBLER.
Part: WEB — CORRODED (DOOR SILL) · airframe 71,732 hrs · 18,596 cycles
AFT CARGO PIT AT BS 1329-1351, LOWER DOOR SILL LOWER WEB IS CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED & INSTALLED REPAIR DOUBLER. INSTALLED WEB AND SPLICE REPAIR.
Part: STRINGER — CORRODED (FUSELAGE) · airframe 71,732 hrs · 18,596 cycles
AFT CARGO STRINGER 34R AT STA 1337 HAS HEAVY CORROSION ON SIDE. MAJOR REPAIRED ACCOMPLISHED. INSTALLED SPLICE REPAIR.
Part: STRINGER — DAMAGED (FUSELAGE) · airframe 71,732 hrs · 18,596 cycles
BS 1361-1379 STRINGER SECTION REQUIRES REPLACEMENT IN ORDER TO MAINTAIN 20 INCH MINIMUM SPACING BETWEEN STRINGER SPLICE AT STATION 1337, STRINGER 34R. MAJOR REPAIR ACCOMPLISHED. REPLACED STRINGER SECTION AND SPLICE.
Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 71,732 hrs · 18,596 cycles
BS 1335, BETWEEN STRINGERS 33R AND 34R, SHEAR TIE CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED SHEAR TIE.
Part: STRINGER — CORRODED (FUSELAGE) · airframe 71,732 hrs · 18,596 cycles
AFT CARGO STRINGER 34R AT STATION 1337 HAS HEAVY CORROSION ON SIDE. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW SECTION AND DOUBLER REPAIR.
Part: STRINGER — MISREPAIRED (FUSELAGE) · airframe 71,732 hrs · 18,596 cycles
STATION 1361 TO 1379, STRINGER 34R, STRINGER SECTION AND SPLICE DO NOT HAVE REQUIRED EDGE DISTANCE BETWEEN REPAIR SPLICES. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED STRINGER & SPLICE REPAIRS.
Part: CLIP — DAMAGED (FUSELAGE) · airframe 71,732 hrs · 18,596 cycles
BS 1346, STR 34R, FRAME ATTACH CLIP REQUIRES REPLACEMENT FOR STRINGER REPAIR. MAJOR REPAIR ACCOMPLISHED. REPLACED CLIP.
Part: STRINGER — CORRODED (FUSELAGE) · airframe 71,732 hrs · 18,596 cycles
AFT CARGO PIT AT BS 1081-1087, STRINGER 37L IS CORRODED AT END FITTING. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED STRINGER SECTION AND SPLICE.
2002
Part: SKIN — CORRODED (FUSELAGE) · airframe 68,692 hrs · 17,973 cycles
AFT EXTERNAL FUSELAGE, AFT WATER DRAIN MAST, CORROSION AROUND BASE, BODY STATION 1417, STRINGER 35R. MAJOR REPAIR ACCOMPLISHED. REPAIRED SKIN WITH EXTERNAL DOUBLER.
Part: FITTING — CRACKED (RT WING) · airframe 68,692 hrs · 17,973 cycles
RIGHT HAND WING FRONT SPAR OUTBOARD PITCHLOAD FITTING CRACKED AT THE FORWARD UPPER RADIUS ABOVE FITTING LUG, CRACK FOUND AND CONFIRMED. MAJOR REPAIR ACCOMPLISHED. REPLACED OUTBOARD PITCHLOAD FITTING.
2001
Part: CHARGER — DEFECTIVE (CABIN) · airframe 65,466 hrs · 17,313 cycles
EMERGENCY LIGHTS ILLUMINATED ON LEFT SIDE FROM DOOR 1 LEFT TO OVERWING EXIT BOTH UPPER LIGHTING AND EEL. *S/D* REPLACED BATTERY CHARGER AND BATTERY M735 AND EEL POWER SUPPLY. TEST OK.
Part: POWER SUPPLY — MALFUNCTIONED (CABIN) · airframe 65,461 hrs · 17,311 cycles
EMERGENCY PATH LIGHTING SECTION LEFT FWD OF COACH SECTION INTERMITTENTLY ON-OFF THROUGHOUT FLIGHT. ALSO BUSINESS CLASS SECTION. *S/D* POWER SUPPLY AT STATION 425 LT. ALL LIGHTS OPS NORMAL.
Part: CLIP — MISALIGNED (FUSELAGE) · airframe 65,446 hrs · 17,305 cycles
STRINGER 39L FORWARD END CLIP DOES NOT ALIGN WITH PREDRILLED STRINGER STATION 325. MAJOR REPAIR ACCOMPLISHED. REPLACED CLIP PER BAC DRAWING 141T3001 AND T-ANGLE PER BAC DRAWING 141T1220 AND SRM 51-40-02.
Part: CLIP — CRACKED (FUSELAGE) · airframe 65,446 hrs · 17,305 cycles
FORWARD PIT STATION 370 FRAME CLIP CRACKED BETWEEN STRINGERS 39R AND 39L. *S/D* MAJOR REPAIR ACCOMPLISHED. REPLACED FRAME CLIP PER SRM 51-40-2 AND BAC DRAWING 141T3220.
Part: CLIP — CRACKED (FUSELAGE) · airframe 65,446 hrs · 17,305 cycles
AFT PIT STATION 1351, STRINGER 34L, STRINGER CLIP IS CRACKED. *S/D* MAJOR REPAIR ACCOMPLISHED. REPLACED CLIP PER BAC DRAWING 140T2101 AND SRM 51-30-2.
Part: ATTACH ANGLE — CORRODED (FUSELAGE) · airframe 65,446 hrs · 17,305 cycles
AFT CARGO PIT BS 1087 AT STR 39L, STRINGER TO FRAME ATTACH ANGLE CORRODED.
Part: SPLICE — CRACKED (FUSELAGE) · airframe 65,446 hrs · 17,305 cycles
FORWARD PIT STRINGER 34R BS 434 HAS A CRACK. *S/D* MAJOR REPAIR ACCOMPLISHED. REPLACED SPLICE PER SRM 53-00-03 AND BAC DRAWING 140T0115-4.
Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 65,446 hrs · 17,305 cycles
AFT PIT APPROX BS 1279 SHEAR TIE BETWEEN 33R AND 34R CORRODED. *S/D* MAJOR REPAIR ACCOMPLISHED. REPLACED SHEAR TIE PER BAC DRAWING 146T8561 AND SRM 51-40-2.
Part: STRINGER — CORRODED (FUSELAGE) · airframe 65,446 hrs · 17,305 cycles
AFT PIT STRINGER 34L BS 1329 - 1362 CORRODED.SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. REPAIRED STRINGER PER SRM 53-00-03 AND 51-20-2.
Part: SKIN — CRACKED (NR 1 PYLON) · airframe 65,446 hrs · 17,305 cycles
NR 1 ENG PYLON LT OUTBOARD SIDE, PANEL 436BL CUTOUT IS CRACKED AT FWD UPPER FASTENER HOLE. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. REPAIRED SKIN PER SRM 54-53-97.
Part: SPLICE — DAMAGED (FUSELAGE) · airframe 65,446 hrs · 17,305 cycles
STRINGER 38R SPLICE AT STATION 434 HAS AN ELONGATED HOLE FOR STRINGER CLIP. *S/D* MAJOR REPAIR ACCOMPLISHED. REPLACED SPLICE PER SRM 53-30-03 AND 51-40-2.
Part: SPLICE — CORRODED (FUSELAGE) · airframe 65,446 hrs · 17,305 cycles
SPLICE 146T1033-60 CORRODED BEYOND LIMITS STATION 1439, BETWEEN STRINGERS 25R AND 26R. *S/D* MAJOR REPAIR ACCOMPLISHED. REPLACED SPLICE PER BAC DRAWING 146T1033 AND SRM 51-40-2.
Part: CLIP — MISALIGNED (FUSELAGE) · airframe 65,446 hrs · 17,305 cycles
STRINGER 39R FORWARD END CLIP DOES NOT ALIGN WITH PRE-DRILLED STRINGER STATION 325. *S/D* MAJOR REPAIR ACCOMPLISHED. REPLACED CLIP PER BAC DRAWING 141T1220-45 AND SRM 51-40-2.
Part: CLIP — CRACKED (FUSELAGE) · airframe 65,446 hrs · 17,305 cycles
STRINGER CLIP CRACKED AT STATION 434, STRINGER 38L. *S/D* MAJOR REPAIR ACCOMPLISHED. REPLACED CLIP AS PER BAC DRAWING 141T1225 AND SRM 51-40-2.
Part: CLIP — CRACKED (FUSELAGE) · airframe 65,446 hrs · 17,305 cycles
FORWARD PIT, STRINGER CLIP CRACKED STATION 434 STRINGER 39L. *S/D* MAJOR REPAIR ACCOMPLISHED. REPLACED CLIP PER BAC DRAWING 141T1225 AND SRM 51-40-2.
Part: STRINGER — CRACKED (FUSELAGE) · airframe 65,446 hrs · 17,305 cycles
STRINGER 38R CRACKED AT THE END UNDER FRAME STA 456 RT. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. REPAIRED STRINGER PER SRM 53-00-03 AND 51-40-2.
Part: WEB — CORRODED (FUSELAGE) · airframe 65,446 hrs · 17,305 cycles
AFT CARGO PIT BS 1329-1351, LBL 26 TO BL 0, SHEAR PANEL CORRODED ON UPPER SURFACE OF PANEL.UPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED.REPLACED WEB PER 146T5000-3 AND SRM 51-40-2.
Part: STRINGER CLIP — BROKEN (FUSELAGE) · airframe 65,446 hrs · 17,305 cycles
FORWARD PIT, STRINGER CLIP AT STATION 434 STRINGER 38R BROKEN. *S/D* MAJOR REPAIR IS ACCOMPLISHED. REPLACED CLIP PER BAC DRAWING 140T2101-573 AND SRM 51-40-2.
Part: STRINGER — CORRODED (FUSELAGE) · airframe 65,446 hrs · 17,305 cycles
CORROSION INSIDE STRINGER 33R BETWEEN FRAME STA 478-500 RT. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED.REPAIRED STRINGER AS PER SRM 53-00-03 AND 51-40-2.
Part: ANGLE — CORRODED (FUSELAGE) · airframe 65,446 hrs · 17,305 cycles
AFT CARGO PIT BS 1087 AT STR 36R FRAME TO STRINGER ATTACH ANGLE CORRODED. *S/D* MAJOR REPAIR ACCOMPLISHED. REPLACED FRAME ATTACH ANGLE PER BAC DRAWING 146T1070-5 AND SRM 51-40-2.
Part: SKIN — GROOVED (FUSELAGE) · airframe 65,446 hrs · 17,305 cycles
LEFT SIDE OF EMPENNAGE SKIN HAS LONG WEAR GROOVE FS 1809, WL 226.10. *S/D* MAJOR REPAIR ACCOMPLISHED. REPAIRED SKIN AS PER SRM 53-80-01.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 65,446 hrs · 17,305 cycles
MAIN CABIN UNDER FLOOR T-CAP CORRODED BS 873, RBL 12. *S/D* MAJOR REPAIR ACCOMPLISHED. REPAIRED T-CAP PER SRM 53-00-51.
Part: SKIN — DAMAGED (FUSELAGE) · airframe 65,446 hrs · 17,305 cycles
LOWER FUSELAGE SKIN HAS HOLE AT STA 380, BL 0. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. INSTALLED SKIN REPAIR PER SRM 53-00-01, FIG 214, AND SRM 51-40-2.
Part: STRINGER — CORRODED (FUSELAGE) · airframe 65,446 hrs · 17,305 cycles
CORROSION ON STRINGER 34R FROM STATION 412 - 434, FORWARD PIT. *S/D* MAJOR REPAIR ACCOMPLISHED. REPAIRED STRINGER AS PER SRM 53-00-03 AND 51-40-2.
Part: STRINGER CLIP — BROKEN (FUSELAGE) · airframe 65,446 hrs · 17,305 cycles
FORWARD PIT, STRINGER CLIP AT STATION 434, STRINGER 37L BROKEN. *S/D* MAJOR REPAIR IS ACCOMPLISHED. REPLACED CLIP PER BAC DRAWING 140T2101-573 AND SRM 51-40-2.
Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 65,446 hrs · 17,305 cycles
FORWARD PIT STATION 412 AND STRINGER 37L, CLIP IS CORRODED. *S/D* MAJOR REPAIR IS ACCOMPLISHED. REPLACED STRINGER CLIP PER SRM 51-40-2 AND BAC DRAWING 141T1225.
Part: STRINGER — CRACKED (FUSELAGE) · airframe 65,446 hrs · 17,305 cycles
STRINGER 38R CRACKED AT THE END UNDER FRAME STATION 456 RT. MAJOR REPAIR ACCOMPLISHED. REPAIRED STRINGER PER SRM 53-00-03 AND 51-40-02.
Part: STRINGER — CORRODED (FUSELAGE) · airframe 65,446 hrs · 17,305 cycles
CORROSION ON STRINGER 34R FROM STATION 412-434 FORWARD PIT. *S/D* MAJOR REPAIR ACCOMPLISHED. REPAIRED STRINGER PER SRM 53-00-03 AND 51-40-2.
Part: ATTACH ANGLE — CRACKED (E/E BAY DOOR) · airframe 65,446 hrs · 17,305 cycles
FORWARD EQUIPMENT BAY DOOR HAS A CRACK ON ATTACH ANGLE IN HANDLE BAY, CENTER OF DOOR.SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED REMOVED INNER DOOR SKIN, FABRICATED NEW ATTACH ANGLE PER BAC DRAWING 141T6422 AND INSTALLED PER SRM 51-40-02, REINSTALLED SKIN DOOR PER SRM 51-40-02.
Part: STRINGER — DAMAGED (FUSELAGE) · airframe 65,446 hrs · 17,305 cycles
BS 434 STRINGER 38R DAMAGED. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW STRINGER IN ACCORDANCE WITH SRM 51-40-02.
Part: SPLICE — CRACKED (FUSELAGE) · airframe 65,446 hrs · 17,305 cycles
BS 434 - 456 STRINGER 38R - 37 STRINGER SPLICE CRACKED AND CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED REPAIR IN ACCORDANCE WITH BAC DRAWING 140T0115 AND SRM 53-00-03 FIGURE 202.
Part: STRINGER — CRACKED (FUSELAGE) · airframe 65,446 hrs · 17,305 cycles
BS 434 STRINGER 35R CRACKED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED REPAIR IN ACCORDANCE WITH BAC DRAWING 140T1228 AND SRM 51-40-02.
Part: STRINGER — DAMAGED (FUSELAGE) · airframe 65,446 hrs · 17,305 cycles
BS 434 - 325 STRINGER 39R REQUIRES REPLACEMENT WITH BELLY SKIN. *S/D* MAJOR REPAIR ACCOMPLISHED. INSTALLED STRINGER 39R IN ACCORDANCE WITH SRM 51-40-02.
Part: SKIN — CORRODED (FUSELAGE) · airframe 65,446 hrs · 17,305 cycles
BELLY SKIN BS 287 - 434 STRINGER 37L TO 37R HAS HEAVY CORROSION. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW IN ACCORDANCE WITH SRM 51-40-02.
Part: STRINGER CLIP — BROKEN (FUSELAGE) · airframe 65,446 hrs · 17,305 cycles
BS 434 STRINGER 34R CLIP BROKEN. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED REPAIR IN ACCORDANCE WITH BAC DRAWING 143T1225 AND SRM 51-40-02.
Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 65,446 hrs · 17,305 cycles
BS 610 STR 39L-39R SHEAR TIE CORRODED.SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED REPAIR IN ACCORDANCE WITH BAC DRAWING 140T2102 AND SRM 51-40-02
Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 65,446 hrs · 17,305 cycles
BS 368 STR 38R TO 37R SHEAR TIE CORRODED.
Part: STRINGER — CRACKED (FUSELAGE) · airframe 65,446 hrs · 17,305 cycles
BS 438 STRINGER 35R CRACKED. *S/D* MAJOR REPAIR ACCOMPLISHED. FABRICATED AND REPAIRED IN ACCORDANCE WITH SRM 53-30-03, FIG 202.
Part: STRINGER — CORRODED (FUSELAGE) · airframe 65,446 hrs · 17,305 cycles
BS 610-620 STRINGER 37R INTERCOSTAL CORRODED. *S/D* MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED REPAIR IN ACCORDANCE WITH BAC DRAWING 143T5000 AND SRM 51-40-02.
Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 65,446 hrs · 17,305 cycles
BS 456 STR 39L-38L SHEAR TIE CORRODED.SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED REPAIR IN ACCORDANCE WITH BAC DRAWING 140T2102-307.
Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 65,446 hrs · 17,305 cycles
BS 1153 STR 37R-38R SHEAR TIE CORRODED.SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED REPAIR IN ACCORDANCE WITH BAC DRAWING 140T2103-446 AND SRM51-40-02.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 65,446 hrs · 17,305 cycles
BS 347 LBL 5 STR CLIP CRACKED.SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED CLIP IN ACCORDANCE WITH BAC DRAWING 141T1221 AND SRM 51-40-02.
Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 65,446 hrs · 17,305 cycles
BS 434 STR 35R-34R SHEAR TIE CORRODED.SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED REPAIR IN ACCORDANCE WITH BAC DWG 140T2102 AND SRM 51-40-02.
Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 65,446 hrs · 17,305 cycles
BS 325 RBL 4 SHEAR TIE CORRODED.SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. REPLACED SHEARTIE IN ACCORDANCE WITH SRM 51-40-02.
Part: SPLICE — CORRODED (FUSELAGE) · airframe 65,446 hrs · 17,305 cycles
BS 434 STRINGER SPLICE 39R CORRODED. *S/D* MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED REPAIR IN ACCORDANCE WITH BAC DRAWING 140T0115 AND SRM 51-40-02.
Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 65,446 hrs · 17,305 cycles
BS 347 STR 38R-39R SHEAR TIE CORRODED.SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED REPAIR IN ACCORDANCE WITH BAC DRAWING 141T1221 AND SRM 51-40-02.
Part: STRINGER — CORRODED (FUSELAGE) · airframe 65,446 hrs · 17,305 cycles
BS 434-456 STRINGER 37R STRINGER CORRODED. *S/D* MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED REPAIR IN ACCORDANCE WITH SRM 53-30-03 AND 51-40-02.
Part: SPLICE — CORRODED (FUSELAGE) · airframe 65,446 hrs · 17,305 cycles
BS 434 STRINGER 39L SPLICE CORRODED. *S/D* MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED REPAIR IN ACCORDANCE WITH BAC DRAWING 140T01115 AND SRM 51-40-02.
Part: SPLICE — DAMAGED (FUSELAGE) · airframe 65,446 hrs · 17,305 cycles
BS 434 STRINGER 36R TO 36L BUTT SPLICE DAMAGED. *S/D* MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED BUTT SPLICE IN ACCORDANCE WITH BAC DRAWING 140T0111 AND SRM 51-40-02.
Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 65,446 hrs · 17,305 cycles
HOLES KNIFE EDGED AT BS 1350-1370 STR 34L.
Part: STRINGER CLIP — BROKEN (FUSELAGE) · airframe 65,446 hrs · 17,305 cycles
BS 434 STR 35R CLIP BROKEN.
Part: CLIP — CORRODED (FUSLEAGE) · airframe 65,446 hrs · 17,305 cycles
BS 370 STR 39L FRAMER ATTCH CLIP CORRODED.
Part: SPLICE — CORRODED (FUSELAGE) · airframe 65,446 hrs · 17,305 cycles
BS 434 STR 36R STRINGER SPLICE CORRODED.
Part: STRINGER — CRACKED (FUSELAGE) · airframe 65,446 hrs · 17,305 cycles
BS 456 STR 39R CRACKED.
Part: SPLICE — CORRODED (FUSELAGE) · airframe 65,446 hrs · 17,305 cycles
BS 434 STR 38R SPLICE CORRODED.
Part: STRINGER — CRACKED (FUSLEAGE) · airframe 65,446 hrs · 17,305 cycles
BS 434 STR 37L CRACKED AT SPLICE.
Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 65,446 hrs · 17,305 cycles
BS 1131 STR 39L-39R SHEARTIE CORRODED.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 65,446 hrs · 17,305 cycles
BS 412 STR 39R STRINGER CLIP CRACKED.
Part: STRINGER CLIP — BROKEN (FUSELAGE) · airframe 65,446 hrs · 17,305 cycles
BS 500 STR 39R CLIP BROKEN.
Part: SPLICE — CORRODED (FUSELAGE) · airframe 65,446 hrs · 17,305 cycles
BS 347 RBL5 STRINGER CLIP CORRODED.
Part: WEB — CORRODED (FUSELAGE) · airframe 65,446 hrs · 17,305 cycles
BS 1329-1351 RB17 TO LBL6 SHEARWEB CORRODED.
Part: CLIP — CORRODED (FUSELAGE) · airframe 65,446 hrs · 17,305 cycles
BS 370 FRAME ATTCH. CLIP STR 39R CORRODED.
Part: FRAME — CORRODED (FUSELAGE) · airframe 65,446 hrs · 17,305 cycles
BS 1395 FRAME T-CAP CORRODED AT RBL 44. MAJOR REPAIR ACCOMPLISHED FABRICATED AND INSTALLED REPAIR.
Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 65,446 hrs · 17,305 cycles
BS 347 STRINGER 39L-STRINGER 39R SHEARTIE CORRODED. MAJOR REPAIR ACCOMPLISHED FABRICATED AND INSTALLED REPAIR IN ACCORDANCE WITH BAC DRAWING140T2102 AND SRM 51-40-02.
Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 65,446 hrs · 17,305 cycles
BS 390 STRINGER 38R-39R SHEARTIE CORRODED. FABRICATED AND INSTALLED REPAIR IN ACCORDANCE WITH BAC DRAWING 140T1223 AND SRM 51-40-02.
Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 65,446 hrs · 17,305 cycles
BS 566 STRINGER 39L-39R SHEARTIE CORRODED. FABRICATED AND INSTALLED REPAIR IN ACCORDANCE WITH BAC DRAWING 140T2102 AND SRM 51-40-02.
Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 65,446 hrs · 17,305 cycles
BS 390 STRINGER 39L TO 39R SHEAR TIE CORRODED. FABRICATED AND INSTALLED REPAIR IN ACCORDANCE WITH BAC DRAWING 141T1223.
Part: STRINGER — CORRODED (FUSELAGE) · airframe 65,446 hrs · 17,305 cycles
BS 1241-1263 STRINGER 39L CORRODED. FABRICATED AND INSTALLED REPAIR IN ACCORDANCE WITH SRM 53-00-03 FIGURE 202.
Part: STRINGER — DAMAGED (FUSELAGE) · airframe 65,446 hrs · 17,305 cycles
BS 434 TO 325 STRINGER 39L TO BE REPLACED WITH BELLY SKIN. *S/D* MAJOR REPAIR ACCOMPLISHED. INSTALLED STRINGER 39L PER SRM 51-40-02.
Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 65,446 hrs · 17,305 cycles
BS 588 STRINGER 39L-39R SHEARTIE CORRODED. MAJOR REPAIR ACCOMPLISHEDFABRICATED AND INSTALLED REPAIR IN ACCORDANCE WITH BAC DRAWING 140T2102 AND SRM 51-40-02.
Part: STRINGER — CORRODED (FUSELAGE) · airframe 65,446 hrs · 17,305 cycles
BS1210-1252 STRINGER 39L CORRODED. FABRICATED AND INSTALLED REPAIR IN ACCORDANCE WITH SRM 53-00-03 AND 51-40-02.
Part: STRINGER — CORRODED (FUSELAGE) · airframe 65,446 hrs · 17,305 cycles
BS 1404-1439 STRINGER 34R CORRODED. FABRICATED AND INSTALLED REPAIR IN ACCORDANCE WITH SRM 53-00-03 AND 51-40-02.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 65,446 hrs · 17,305 cycles
BS 1153 BL-0 TO RBL 46 T-CAP CORRODED. FABRICATED AND INSTALLED REPAIR IN ACCORDANCE WITH BAC DRAWING 146T1060-2 AND SRM 51-40-02.
Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 65,446 hrs · 17,305 cycles
BS 412 STRINGER 38L-39L SHEAR TIE CORRODED. FABRICATED AND INSTALLED REPAIR IN ACCORDANCE WITH BAC DRAWING 141T1224.
Part: SPLICE — CORRODED (FUSELAGE) · airframe 65,446 hrs · 17,305 cycles
STATION 1439 FRAME SPLICE CORRODED AT STRINGERS 25R TO 26R. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW FRAME SPLICE IN ACCORDANCE WITH SRM 51-40-02.
Part: FRAME — CORRODED (FUSELAGE) · airframe 65,446 hrs · 17,305 cycles
BS 1131 LBL 40-45 FRAME T-CAP IS CORRODED. MAJOR REPAIR ACCOMPLISHEDFABRICATED AND INSTALLED REPAIR IN ACCORDANCE WITH BAC DRAWING 146T203-5 ANDSRM 51-40-02.
Part: FITTING — CORRODED (FUSELAGE) · airframe 65,446 hrs · 17,305 cycles
BS 1373 STRINGER 39L END FITTING IS CORRODED. MAJOR REPAIR ACCOMPLISHEDFABRICATED AND INSTALLED REPAIR IN ACCORDANCE WITH BAC DRAWING 146T3240 AND BAC DRAWING 146T3006.
Part: FAILSAFE — DAMAGED (FUSELAGE) · airframe 65,446 hrs · 17,305 cycles
REMOVED FAILSAFE STRAP TO FACILITATE STRINGER REPAIR STATION 368 STRINGERS 37R TO 39R. MAJOR REPAIR ACCOMPLISHEDCUT OUT REQUIRED SECTION, FABRICATED AND INSTALLED REPAIR IN ACCORDANCE WITH SRM 51-70-12.
Part: FRAME — DAMAGED (FUSELAGE) · airframe 65,446 hrs · 17,305 cycles
BS 1307 LBL 16.5 T-CAP HAS HOLE DRILLED IN RADIUS. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED REPAIR IN ACCORDANCE WITH BAC DRAWING 146T1211 AND SRM 51-40-02.
Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 65,446 hrs · 17,305 cycles
BS 1461 STRINGERS 39L TO 39R SHEAR TIE CORRODED. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHEDFABRICATED AND INSTALLED REPAIR IN ACCORDANCE WITH BAC DRAWING 140T2102.
Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 65,446 hrs · 17,305 cycles
BS 1175 STRINGERS 39R TO 39L SHEAR TIE CORRODED. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED.FABRICATED AND INSTALLED REPAIR IN ACCORDANCE WITH BAC DRAWING 140T2102 AND SRM 51-40-02.
Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 65,446 hrs · 17,305 cycles
BETWEEN STRINGERS 38R - 39R SHEAR TIE CORRODED. MAJOR REPAIR ACCOMPLISHEDFABRICATED AND INSTALLED REPAIR IN ACCORDANCE WITH SRM 51-40-02 AND BAC DRAWING 140T2102.
Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 65,446 hrs · 17,305 cycles
AFT CARGO PIT AT BS 1241 BETWEEN STRINGERS 36L AND 37L, SHEAR TIE IS CORRODED. MAJOR REPAIR ACCOMPLISHED REPLACED SHEAR TIE PER BAC DRAWING 140T21023 AND INSTALLED PER SRM 51-40-02.
Part: STRINGER — CORRODED (FUSELAGE) · airframe 65,446 hrs · 17,305 cycles
BS 1540 TO 1562 STRINGER 28R CORRODED. MAJOR REPAIR ACCOMPLISHED.FABRICATED AND INSTALLED REPAIR IN ACCORDANCE WITH SRM 53-00-03 FIGURE 202 AND SRM 51-40-02.
Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 65,446 hrs · 17,305 cycles
BS 1395 STRINGERS 36L TO 37L SHEAR TIE CORRODED. MAJOR REPAIR ACCOMPLISHED FABRICATED AND INSTALLED REPAIR IN ACCORDANCE WITH BAC DRAWING 140T2102 AND SRM 51-40-02.
Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 65,446 hrs · 17,305 cycles
STATION 1241 STRINGER 39L TO 39R SHEAR TIE CORRODED. MAJOR REPAIR ACCOMPLISHED FABRACATED AND INSTALLED REPAIR IN ACCORDANCE WITH BAC DRAWING 140T2102 ANDSRM 51-40-02.
Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 65,446 hrs · 17,305 cycles
AFT PIT BS 1395 STRINGERS 38L TO 39L SHEAR TIE CORRODED. MAJOR REPAIR ACCOMPLISHED FABRICATED AND INSTALLED REPAIR IN ACCORDANCE WITH BAC DRAWING 140T2102 AND SRM 51-40-02.
Part: FLOORBEAM — DAMAGED (FUSELAGE) · airframe 65,446 hrs · 17,305 cycles
MAIN CABIN FLOORBEAM T-CAP HAS DOUBLE DRILLED HOLES BS 790 TO 880 LBL 33. MAJOR REPAIR ACCOMPLISHEDFABRICATED AND INSTALLED REPAIR IN ACCORDANCE WITH SRM 53-00-51 AND 51-40-02.
Part: STRINGER — CORRODED (FUSELAGE) · airframe 65,446 hrs · 17,305 cycles
BS 1540 TO 1562 STRINGER 32R CORRODED. MAJOR REPAIR ACCOMPLISHED.FABRICATED AND INSTALLED NEW REPAIR IN ACCORDANCE WITH SRM 53-00-03 FIGURE 202 AND SRM 51-40-02.
Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 65,446 hrs · 17,305 cycles
BS 1439 STRINGERS 39L TO 39R SHEAR TIE CORRODED. MAJOR REPAIR ACCOMPLISHED FABRACATED AND INSTALLED REPAIR IN ACCORDANCE WITH BAC DRAWING 140T2102 AND SRM 51-40-02.
Part: FRAME — CORRODED (FUSELAGE) · airframe 65,446 hrs · 17,305 cycles
STATION 560 STRINGER 38L FRAME LOWER FLANGE CORRODED. MAJOR REPAIR ACCOMPLISHED FABRACATED AND INSTALLED REPAIR IN ACCORDANCE WITH SRM 53-00-07 AND51-40-02.
Part: FRAME — CORRODED (FUSELAGE) · airframe 65,446 hrs · 17,305 cycles
BS 764 FRAME CORRODED BETWEEN STRINGS 39R TO 35R. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED REPAIR IN ACCORDANCE WITH SRM 53-00-07 FIGURE 202.
Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 65,446 hrs · 17,305 cycles
AFT PIT BS 1153 BETWEEN STRINGERS 39L AND 39R SHEAR TIE CORRODED. MAJOR REPAIR ACCOMPLISHEDFABRICATED AND INSTALLED REPAIR IN ACCORDANCE WITH BAC DRAWING 140T2102 AND SRM 51-40-02.
Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 65,446 hrs · 17,305 cycles
BS 742 STRINGER 39L TO 39R SHEAR TIE CORRODED. MAJOR REPAIR ACCOMPLISHED FABRACATED AND INSTALLED REPAIR IN ACCORDANCE WITH BAC DRAWING 140T2102 ANDSRM 51-40-02.
Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 65,446 hrs · 17,305 cycles
BS 1373 STRINGERS 36L TO 37L SHEAR TIE CORRODED. MAJOR REPAIR ACCOMPLISHED FABRACATED AND INSTALLED REPAIR IN ACCORDANCE WITH BAC DRAWING 140T2102 ANDSRM 51-40-02.
Part: STRINGER — CORRODED (FUSELAGE) · airframe 65,446 hrs · 17,305 cycles
BS 1285 TO 1307 STRINGER 34R CORRODED. MAJOR REPAIR ACCOMPLISHEDFABRICATED AND INSTALLED REPAIR IN ACCORDANCE WITH SRM 53-00-03 FIGURE 204.
Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 65,446 hrs · 17,305 cycles
BS 1417 STRINGERS 38R TO 39R SHEAR TIE CIRRIDED. MAJOR REPAIR ACCOMPLISHEDFABRACATED AND INSTALLED REPAIR IN ACCORDANCE WITH BAC DRAWING 140T2102 ANDSRM 51-40-02.
Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 65,446 hrs · 17,305 cycles
BS 1131 STRINGERS 34R TO 35R SHEAR TIE CORRODED. MAJOR REPAIR ACCOMPLISHED FABRACATED AND INSTALLED REPAIR IN ACCORDANCE WITH BAC DRAWING 140T2102 ANDSRM 51-40-02.
Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 65,446 hrs · 17,305 cycles
AFT BS 1395 STRINGERS 39L TO 39R SHEAR TIE CORRODED. MAJOR REPAIR ACCOMPLISHED FABRICATED AND INSTALLED REPAIR IN ACCORDANCE WITH BAC DRAWING 140T2102 AND SRM 51-40-02.
Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 65,446 hrs · 17,305 cycles
AFT CARGO PIT AT BS 1241 BETWEEN STRINGERS 37L TP 39L, SHEAR TIE CORRODED. MAJOR REPAIR ACCOMPLISHED REPLACED SHEAR TIE PER BAC DRAWING 140T2102 AND INSTALLED PER SRM 51-40-02.
Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 65,446 hrs · 17,305 cycles
AFT PIT STATION 1241 STRINGERS 35R TO 36R SHEAR TIE CORRODED. MAJOR REPAIR ACCOMPLISHED FABRICATED AND INSTALLED REPAIR IN ACCORDANCE WITH BAC DRAWING 140T2102 AND SRM 51-40-02.
Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 65,446 hrs · 17,305 cycles
FORWARD PIT BS 522 STRINGERS 33L TO 34L SHEAR TIE CORRODED. MAJOR REPAIR ACCOMPLISHED INSTALLED NEW SHEAR TIE IN ACCORDANCE WITH SRM 51-40-02.
Part: STRINGER — CORRODED (FUSELAGE) · airframe 65,446 hrs · 17,305 cycles
CORROSION IN STRINGER S35R BETWEEN FRAMES STATION 610 TO 632. MAJOR REPAIR ACCOMPLISHED INSTALLED REPAIR PER SRM 53-00-03, FIGURE 204.
Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 65,446 hrs · 17,305 cycles
FORWARD PIT BS 742 STRINGERS 38R TO 39R SHEAR TIE CORRODED. MAJOR REPAIR ACCOMPLISHED INSTALLED NEW SHEAR TIE IN ACCORDANCE WITH SRM 51-40-02.
Part: STRINGER — DENTED (FUSELAGE) · airframe 65,446 hrs · 17,305 cycles
BS 390 TO 412 STRINGERS 27L TO 28L DENT WITH CREASE IN AIRCRAFT SKIN. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED REPAIR IN ACCORDANCE WITH SRM 53-00-01 FIGURE 206.
Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 65,446 hrs · 17,305 cycles
AFT PIT BS 1395 STRINGERS 37R TO 38R SHEAR TIE CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED REPAIR IN ACCORDANCE WITH BAC DRAWING 140T2102 AND SRM 51-40-02.
Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 65,446 hrs · 17,305 cycles
BS 1439 STRINGER 38R TO 39R SHEAR TIE CORRODED. MAJOR REPAIR ACCOMPLISHED FABRICATED AND INSTALLED REPAIR IN ACCORDANCE WITH BAC DRAWING 140T2102 AND SRM 51-40-02.
Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 65,446 hrs · 17,305 cycles
FORWARD PIT BS 742 STRINGERS 38R TO 39R SHEAR TIE CORRODED. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED FABRICATED AND INSTALLED NEW SHEAR TIE IN ACCORDANCE WITH BAC DRAWING 140T2102 AND SRM 51-40-02.
Part: FRAME — CORRODED (FUSELAGE) · airframe 65,446 hrs · 17,305 cycles
BS 1263 BL0-LBL 30 FRAME T-CAP CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED REPAIR IN ACCORDANCE WITH BAC DRAWING 146T1209-5 AND SRM 51-40-02.
Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 65,446 hrs · 17,305 cycles
BS 1417 STRINGERS 39L TO 39R SHEAR TIE CORRODED. MAJOR REPAIR ACCOMPLISHED FABRACATED AND INSTALLED SHEAR TIE IN ACCORDANCE WITH BAC DRAWING 140T2102 ANDSRM 51-40-02.
Part: STRINGER — CORRODED (FUSLEAGE) · airframe 65,446 hrs · 17,305 cycles
BS 1241 TO 1263 STRINGER 39R CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED REPAIR IN ACCORDANCE WITH SRM 53-00-03 FIGURE 202 AND SRM 51-40-02.
Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 17,305 hrs
CORROSION IN SHEAR TIE UNDER FRAME STA. 654 BETWEEN STRINGERS 39L AND 37R. MAJOR REPAIR ACCOMPLISHEDFABRICATED AND INSTALLED SHEAR TIE IN ACCORDANCE WITH B767 DRAWING 140T2103 AND SRM 51-40-02.
Part: STRINGER — CORRODED (FUSELAGE) · airframe 65,446 hrs · 17,305 cycles
AFT CARGO PIT AT STA 1219 - 1241, STRINGER 34R IS CORRODED. MAJOR REPAIR ACCOMPLISHED REPAIRED STRINGER PER SRM 53-00-03, FIGURE 204.
2000
Part: HARNESS — BURNED (GALLEY) · airframe 64,346 hrs · 17,091 cycles
SMOKE IN MID CABIN REPORTED BY FLIGHT ATTENDANT. DISCONNECTED PIG TAIL AND ISOLATED. SMOKE AND ORDER DISSIPATED. SUPPLEMENTAL DATA UPDATE CART HEATER PIG TAIL OVERHEATED WITH EVIDENCE OF BLACK CHARRING. CART HEATER PIG TAIL WAS REPLACED, CART HEATER OPERATIONALLY CHECKED GOOD. NO FURTHER INCIDENCES.
1998
Part: FAN — FAILED (LT AC SYST)
CREW ADVISED SMELLING SMOKE ODOR IN CABIN. DIVERTED TO DEN. *S/D* LEFT AIR CONDITIONING RECIRCULATION FAN WAS REPLACED DUE TO SMELL LIKE SMOKE. SHOP FINDINGS CONFIRMED ROUGH AND DRY BEARINGS, BUT NO OTHER INTERNAL HEAT DAMAGE. PROBABLE CAUSE OF SMOKE ODOR IS BEARING OVERHEAT RESULTING IN SMOKING GREASE.
1997
Part: BEARING — FAILED (RT ENGINE)
RIGHT ENGINE FUEL CUTOFF VALVE SHUT DOWN INDICATION WITH RIGHT ENGINE SHUTDOWN EICAS AND SPEEDS DISPLAYED. ENGINE CONTINUED TO RUN. SUPPLEMENTAL DATA UPDATE FAILED BEARING INSIDE CONDITION MOTOR ACTUATOR .
1996
Part: EEC — FAILED (RT ENGINE)
ABORTED TAKEOFF AT 80 KNOTS DUE TO RIGHT ENGINE OVER TEMP CONDITION. *S/D* A FAULTY ELECTRONIC ENGINE CONTROL UNIT HAD JUST BEEN INSTALLED ON THE RIGHT ENGINE BEFORE THE OVER TEMP DISCREPANCY OCCURRED. THE EEC WAS REPLACED, OPERATIONS CHECK NORMAL.
Part: HYD VALVE — LEAKING (FLAP/SLAT SYST)
LANDED UNDER AMBER ALERT DUE TO ZERO QUANTITY INDICATION FOR CENTER HYDRAULIC SYSTEM FLUID. FLUID LOST DUE TO LEAK IN SOLENOID ON FLAP/SLAT HYD SHUTOFF VALVE. REPLACED BOTH SOLENOIDS AND GASKET PLATES ON FLAP/SLAT HYD VALVE. SERVICED CENTER SYSTEM. OPERATION CHECKS NORMAL.
1995
Part: EEL LAMP — INOP (CABIN)
EMERGENCY EXIT LIGHT INOP ROW 32. REPLACED LAMP, CHECKS OK.
Part: EEC — MALFUNCTIONED (NR 1 ENGINE)
ABORTED TAKEOFF DUE TO NR 1 ENGINE EEC LIGHT. ELECTRONIC ENGINE CONTROL WAS REPLACED PER FAULT ISOLATION MANUAL, SYSTEM CHECKED O.K. CONTROL WAS BENCH CHECKED IN THE SHOP WITH NO FAULTS FOUND. SUSPECT LOOSE CONNECTION WHEN INSTALLED.
Part: BLADES — DAMAGED (NR 2 ENGINE)
NR TWO ENGINE EXPERIENCED COMPRESSOR STALL IN STEADY STATE CLIMB. RETARDED THROTTLE TO IDLE AND USED POWER ON LANDING. ENGINE WAS BORESCOPED AND LOW PRESSURE COMPRESSOR BLADES WERE FOUND DAMAGED. ENGINE WAS REMOVED AND ROUTED TO THE SHOP.