N603AX
Registered owner: BC AIRCRAFT LEASING LLC, NM (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
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.
29 reports on file, 2008-12-15 – 2011-08-08.
Part: ENGINE — FAILED (NR 1) · airframe 74,938 hrs · 12,496 cycles
2000 FT FROM LEVEL OFF NR1 ENGINE SHUTDOWN, EGT RED FLAG WITH NO N1 OR N2. PREFORMED QRH PROCEEDURE. METAL IN TAILPIPE & EXCESSIVE DAMAGE TO LPT. R & R NR1 ENG IAW WC 10UN-101. ACHIEVED ENG PARAMETERS IAW MM 71-00.
Earlier reports · 2008–2010 · 28 reports
2010
Part: DUCT — BLOWN (NR 1 ENGINE) · airframe 72,182 hrs · 11,927 cycles
NR 1 ENGINE FIRE WARNING DURING CLIMB OUT AT 13000 FT. N1'S 103.5. FIRE WARNING EXTINGUISHED WHEN THROTTLE WAS RETARDED. COMPLIED WITH QRH 4-1-1-1. INSP NR 1 ENG FOUND BLOWN DUCT FOR HP RECOUP AIR ASSY. REPLACED NR 1 ENG HP RECOUP AIR ASSY DUCT WITH SERVICABLE DUCT ASSY PN 9054M52G01 REF MM 75-15, LEAK CHECKED OK WITH HIGH POWER RUNS REF JRH.
2009
Part: SCAVENGE PUMP — LEAKING (NR 1 ENGINE) · airframe 70,005 hrs · 11,483 cycles
40 MINUTES INTO FLIGHT, NR 1 ENG OIL QTY WAS OBSERVED TO BE AT 4 QTS AND STEADILY DECREASING TO 0. OIL TEMP WAS AT 155 AND INCREASED TO 165. OIL PRESS WAS AT 45 AND DECREASED TO 30 PRIOR TO ENG SHUTDOWN. ENG COOLED FOR 3.5 - 4 MINUTES PRIOR TO SHUTDOWN. REMOVED AND REPLACED LUBE AND SCAVAGE PUMP ON NR 1 ENG IAW MM 79-20. OPS AND LEAK CHECK IAW OPS AND LEAK CHECK GOOD.
Part: OIL SYSTEM — MALFUNCTIONED (ENGINE) · airframe 69,676 hrs · 11,419 cycles
UPON DECENT PRESS DROPPED BELOW 10PSI AND ENGINE LOW OIL PRESSURE LIGHT ILLUMINATED PERFORMED INFLIGHT ENGINE SHUTDOWN IAW QRH 20 MIN PRIOR TO LANDING.
2008
Part: SUPPORT — BROKEN (BS 1781) · airframe 68,786 hrs · 11,241 cycles
BS 1781, RBL 60 ANGLE SUPPORT IS BROKEN AT CRT CARGO DOOR CUT OUT (AUS TANK AREA). BROKEN ANGLE REMOVED. NEW ANGLE INSTALLED (PN OAI-53-0007) USING MS7885/6-4-08 (B/N 40970-04). FASTENERS INSTALLED IAW SRM VOL II 51-31-01 FIG 2.
Part: STRUCTURE — DAMAGED (BS 1741) · airframe 68,786 hrs · 11,241 cycles
FOUND TURN ANGLE WITH TEMPORARY REPAIR ON CTR CARGO DOOR ABOVE ACTUATOR ARMING AT STA 1741. TEMP REPAIR REMOVED. NEW INTERCOSTAL INSTALLED AND REPAIR PARTS INSTALLED IAW SRM VOL I 52-00-01, FIG 9.
Part: SUPPORT — CORRODED (BS 1581 S41-42L) · airframe 68,786 hrs · 11,241 cycles
BS 1581 STR 41L-42L CORROSION ON AFT LT FAIRING SUPPORT. CLEAN UP CORROSION AT NOTED AREA IAW SRM 51-21-01 AND AREA REINFORCED IAW SRM VOL I 53-00-01, FIG 7, IAW SRM 51-31-01.
Part: FLOORBEAM — CORRODED (BS 1781) · airframe 68,786 hrs · 11,241 cycles
BS 1781, LBL 0-LBL 20, CORROSION ON CARGO FLOORBEAM. CORRODED FLOORBEAM REMOVED. NEW FLOORBEAM INSTALLED IAW SRM VOL II 51-31-01 FIG 2.
Part: SUPPORT — BROKEN (BS 939 S47L) · airframe 68,786 hrs · 11,241 cycles
BS 939, STR 47L BROKEN SUPPORT. TRIMMED FLANGE AT DAMAGE AREA. A REINFORCEMENT ANGLE, INSTALLED IAW SRM 53-00-01, FIG 8 (VOL I) INSTALLED FASTENERS IAW 51-31-01 VOL II.
Part: STRUCTURE — CRACKED (DOOR FRAME) · airframe 68,786 hrs · 11,241 cycles
CTR CARGO COMP BS 1721 - 1741 LT CHAIN HAT IS CRACKED. CTR CARGO COMP STA 1721 TO 1741 APPROX IN DOORWAY DAMAGED CHAIN HAT REPLACED IAW MM 25-57-00.
Part: BRACKET — CRACKED (BS 1341) · airframe 68,786 hrs · 11,241 cycles
BS 1341, LBL N60 CTR WING LWR BARREL STRUCTURE CRACKED BRACKET. DAMAGED BRACKET REMOVED. NEW BRACKET INSTALLED IAW SRM 51-31-01 ( VOL II).
Part: SUPPORT — CRACKED (BS 1781) · airframe 68,786 hrs · 11,241 cycles
BS 1781, LBL 64, THERE IS A CRACK ON AFT WALL SUPPORT. CRACKED PART REMOVED AND NEW PART OAI-53-0005 INSTALLED WITH FASTENERS IAW SRM VOL 2 51-31-01, BACR15CE5D-5 B/N 3847703.
Part: FRAME — DAMAGED (BS 1039) · airframe 68,786 hrs · 11,241 cycles
BS 1039, LBL 49 DOUBLE HOLES ON FRAME. FLANGE WITH DOUBLE HOLES TRIMMED. REINFORCEMENT PART INSTALLED AS RQUIRED IAW SRM VOL I, 53-00-01, FIG 7.
Part: STRUCTURE — CRACKED (DOOR FRAME) · airframe 68,786 hrs · 11,241 cycles
CTR CARGO COMP BS 1681-1701 LT CHAIN HAT IS CRACKED. REPLACED BY NEW HAT MM 25-52-08.
Part: FLOOR SUPPORT — BROKEN (BS 840) · airframe 68,786 hrs · 11,241 cycles
BS 840 RBL 60 ON FLOOR SUPPORT BROKEN. DAMAGED FLOOR SUPPORT REMOVED. NEW FABRICATED PN OAI-53-0003 IAW SAMPLE AND IAW SRM VOL 3 53-13-01 FIG 8. USING WITH FASTENERS IAW SRM VOL 2 51-31-01 PN HL8PB6-4 B/N 89623-01.
Part: FLOORBEAM — CRACKED (BS 1521) · airframe 68,786 hrs · 11,241 cycles
CRACK AND TORN ANGLE FLOORBEAM ON FWD FRAME STA 1521, RBL 15. REMOVED DAMAGED PART AND NEW PART OAI 53-0003 INSTALLED DUE TO FABRICATION PART IAW SRM 53-11-01, FIG 9, OMNI GMM 4.45, USING FASTENERS HL19PB6-4, B/N 56100-01, HL70-6 B/N 534106-01 AND BACR15CE6D-5 B/N 82298-01 IAW SRM 51-31-01.
Part: STRUCTURE — CRACKED (BS 1721-1741) · airframe 68,786 hrs · 11,241 cycles
CRACK FOUND STA 1721 ON LWR CHORD B/T STA 1721-1741 RBL - 0 B/T STR 51 TO 52 RT. TRIM OUT CRACK AND AREA REINFORCEMENT IAW SRM VOL 2 51-31-01.
Part: FLOORBEAM — CRACKED (BS 1781) · airframe 68,786 hrs · 11,241 cycles
STA 1781 LBL-8 LT UPPER FLOORBEAM TEE-CRACK ON FLOORBEAM AT UPPER TEE. REMOVED NEW SUPPORT INSTALLED IAW SRM VOL II 51-31-01.
Part: ANGLE — CRACKED (BS 1902) · airframe 68,786 hrs · 11,241 cycles
BS 1902 RBL 10 AND LBL 44 CRACK ON ANGLES. DAMAGED ANGLE REMOVED. NEW FABRICATED PN OAI-53-0004 IAW SAMPLE AND IAW SRM VOL 3 53-13-01 FIG 8 USING WITH FASTENERS IAW SRM VOL 2 51-31-01. PN HL18PB6-4 B/N 89623-01.
Part: FLOORBEAM — CORRODED (BS 1039) · airframe 68,786 hrs · 11,241 cycles
BS 1039, RBL 45 CORROSION ON FLOORBEAM. CORRODED FLOORBEAM REMOVED. NEW FLOORBEAM INSTALLED IAW SRM VOL II 51-31-01.
Part: FLOORBEAM — DAMAGED (BS 1741) · airframe 68,786 hrs · 11,241 cycles
STA 1741 LBL 50 DOUBLE HOLES ON FLOORBEAM. DAMAGED SUPPORT REMOVED NEW FLOORBEAM INSTALLED IAW SRM VOL II 51-31-01 IG 2.
Part: ANGLE — BROKEN (BS 1781) · airframe 68,786 hrs · 11,241 cycles
BS 1781 LBL 60 ANGLE IS BROKEN C/TO AFT WALL SUPPORTS. BROKEN ANGLE REMOVED. NEW ANGLE INSTALLED IAW SRM VOL II 51-31-01 FIG 2.
Part: POST — BENT (BS 1921) · airframe 68,786 hrs · 11,241 cycles
BS 1921, LBL 12 AND LBL 28 POSTS OF AFT WALL ARE BENT. DAMAGED POSTS REMOVED. NEW POSTS PN OAI-53-0010 AND OAI-53-0009 INSTALLED USING MS20470D6-5 RIVETS (B/N 311872-02) HL18PB6-5 (B/N 26206-04) AND HL70-6 COLLARS (B/N 53406-01) IAW SRM 51-31-01 (VOL II).
Part: INTERCOSTAL — BROKEN (BS 1783) · airframe 68,786 hrs · 11,241 cycles
BS 1783 BROKEN INTERCOSTALS. BROKEN PARTS REMOVED. NEW INTERCOSTALS AND ANGLE, & STRAP INSTALLED WITH FASTENERS IAW SRM VOL II FIG 2 51-3101.
Part: STUD — DAMAGED (BS 939) · airframe 68,786 hrs · 11,241 cycles
BS 939, LBL 15 BROKEN ELEC SUPPORT STUD. DAMAGED AREA TRIMMED A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-00-01, FIG 8.
Part: FLOORBEAM — CORRODED (BS 1341) · airframe 68,786 hrs · 11,241 cycles
AT STA 1701, LBL 10 CORROSION ON FLOORBEAM. CORRODED FLOORBEAM REMOVED NEW FLOORBEAM INSTALLED IAW SRM VOL II 51-31-01.
Part: FLOOR SUPPORT — BROKEN (BS 879) · airframe 68,786 hrs · 11,241 cycles
BS 879, RBL 60 ON FLOOR SUPPORT BROKEN. DAMAGED FLOOR SUPPORT REMOVED. NEW FABRICATED PN OAI-53-0004 IAW SAMPLE AN IAW SRM VOL 3 53-11-01, FIG 8 USING FASTENERS IAW SRM VOL 2 51-31-01 PN HL18PB-6-4 B/N 89623-01.879
Part: POST — BENT (BS 1921) · airframe 68,786 hrs · 11,241 cycles
BS 1921, RBL 12-28 POSTS OF AFT WALL ARE BENT. ONE POST WAS STRAIGHTENED AND FOUND FREE OF CRACKS AS STATED ON THE BACK OF THIS CARD. SECOND DAMAGED POST REMOVED NEW POST P/N OAI-53-0014 INSTALLED USING MS20470D6-5 (B/N 26206-04), HL18PB6-5 (B/N 31172-02) IAW SRM VOL II 51-31-01.
Part: BRACKET — CRACKED (BS 1341) · airframe 68,786 hrs · 11,241 cycles
BS 1341, RBL N60 CTR WING LWR BARREL STRUCTURE CRACKED BRACKET. CRACKED ANGLE REMOVED, NEW ANGLE INSTALLED IAW SRM VOL II 51-31-01.