N522AX

MCDONNELL-DOUGLAS DC-10-30 · 1988 · Fixed-wing multi-engine · 3 engines · 345 seats · Valid Registration

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.

25 reports on file, 2009-03-04 – 2020-07-03.

FALSE WARNING · 2020-07-03 Unresolved
ATA 3610

Part: BOLT — MISSING (BLEED AIR SYS) · airframe 58,826 hrs · 17,421 cycles

"AT ROTATE SPEED NR 2 ENG INDICATED FIRE. ALL ENG INDICATORS DISPLAYED NORMAL PARAMETERS FOR CONDITIONS. PERFORMED ENG SHUTDOWN IAW QRH. UPON PLACING FUEL LEVER TO OFF, FIRE INDICATION EXTINGUISHED. SHORTLY THEREAFTER NR 2 ENG REV PSI LIGHT BEGAN TO FLICKER UNTIL DOWNWIND WHEN LIGHT REMAINED ON STEADY FOR REMAINDER OF FLIGHT. UPON INVESTIGATION FOUND HIGH PRESSURE VALVE CLAMP SEPARATED AND PRESSURE REDUCING VALVE SHROUD DAMAGED AND SEVERAL WIRES DAMAGED. REMOVED AND REPLACED HIGH PRESSURE VALVE IAW AMM 36-11-02. REMOVED AND REPLACED PRESSURE REDUCING VALVE IAW AMM 36-12-01 AND REPAIRED DAMAGED WIRES IAW SWPM 20-10-03. ALL OPS CHECKS GOOD. REFERENCE LOG PAGE 53114 ITEM 2 FOR NR 2 ENGINE REV PSI LIGHT ON. MALFUNCTION WAS CAUSED BY MISSING HARDWARE (PIECES NOT RECOVERED) ON CDP DUCT TO HIGH PRESSURE BLEED VALVE CLAMP ALLOWING CDP BLEED AIR INTO THE SURROUNDING ENGINE COWL. NEW HARDWARE WAS INSTALLED IN CLAMP AT THE CDP TUBE TO CUSTOMER HIGH PRESSURE BLEED VALVE AS IDENTIFIED IN GE SERVICE BULLETIN 75-0078 REV 4, FIGURE 3, SHT 2, A. CLAMP HARDWARE TIME IS UNKNOWN IN THE OPERATING FLEET, MISSING HARDWARE/RUN DOWN TORQUE IS UNKNOWN. REPLACE OPERATING FLEET CLAMP HARDWARE WITH NEW AT EARLIEST CONVENIENCE, 2 EACH BOLT P/N BOLT J816P026A, 2 EACH NUT MS210436 PER ENGINE/PER AIRCRAFT.

Source: SDR ZTRR20200708001
Earlier reports · 2009–2011 · 24 reports

2011

NO TEST · 2011-05-02 Matched by certificate designator
ATA 2565

Part: LIGHT — NO TEST (L1 DOOR SLIDE) · airframe 57,077 hrs · 15,685 cycles

L1 DOOR SLIDE EMERGENCY LIGHTS FAILED TO ILLUMINATE DURING OPS TEST. SLIDE DEPLOYED NORMALLY. REPLACED SLIDE ASSY.

Source: SDR CNMA20110024

2010

FLUID LOSS; WARNING INDICATION · 2010-12-29 Matched by certificate designator
ATA 7261

Part: SCAVENGE PUMP — LEAKING (NR 3 ENGINE) · airframe 56,436 hrs · 15,558 cycles

NR 3 ENG OIL QTY WENT TO ZERO IN FLIGHT, VERIFIED BY LOSS OF OIL PRESS & LOW OIL PRESS LIGHT. TROUBLESHOT DOWN TO NR 3 ENGINE OIL LUBE AND SCAVENGE PUMP ASSY. R & R PUMP ASSY IAW MM 79-20-04, SERVICED 25 QTS OF OIL IN ENGINE LEAK CKS AND OPS CKS GOOD.

Source: SDR CNMA20100036
OTHER · 2010-07-24 Matched by certificate designator
ATA 5730

Part: PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 55,686 hrs · 15,397 cycles

EXFOLIATED CORROSION ON RT WING LOWER PLATE BELOW ACCESS PANEL 616BB AT XQRS 346. REMOVED DAMAGED SECTION OF LOWER WING SKIN, ACCOMPLISHED SURFACE SCAN AND OPEN HOLE HFEC INSP, ROTO PEENED AFFECTED AREA. FABRICATED ALL REPAIR PARTS. INSTALLED ALL REPAIR PARTS IAW ASI DWG. NR 5750930-1 & EO D57-13.

Source: SDR CNMA20100028

2009

OTHER · 2009-03-13 Matched by certificate designator
ATA 5320

Part: SUPPORT FITTING — DAMAGED (BS 1997-2007) · airframe 51,917 hrs · 14,634 cycles

BS 1997-2007, LBL 60 CORROSION ON SUPPORT FITTING. DAMAGED AREA REMOVED. REINFORCED AREA WITH REPAIR DOUBLER (PN 5340599-1-3) IAW SWG NO 5340599-1 USING FASTENERS IAW SRM VOL 2 51-31-01, HL 18PB-6-4, BN 583113-01, HL70-G, BN 53406-01. (ACCOMPLISHED WORK IAW EO D53-15 AND ASI DWG 5340599-1 ).

Source: SDR CNMA20090007
OTHER · 2009-03-04 Matched by certificate designator
ATA 5315

Part: FLOORBEAM — CRACKED (BS 1900) · airframe 51,911 hrs · 14,633 cycles

FOUND CRACK ON FLOOR PANEL SUPPORT AT STD 1900 LBL - 5. DAMAGED SUPPORT REMOVED NEW FABRICATED PN OAI-53-0011 IAW SRM VOL 3 53-16-01 AND GMM 4.45 USING FASTENERS IAW SRM VOL 2 51-31-01, HL18PB6-4, B/N 89623-01, HL70-6 B/N 53306.

Source: SDR CNMA2009A0140
OTHER · 2009-03-04 Matched by certificate designator
ATA 5210

Part: WEB — CRACKED (PAX DOOR) · airframe 51,911 hrs · 14,633 cycles

CRACK ON WEB OF PASS DOOR 3R LWR FWD CORNER B/T STA 1256-1273 STR 27R. CRACKED AREA TRIMMED OUT. REINFORCED AREA WITH DOUBLER AND FILLER PN N522AX-NRC495-2/2 IAW SRM VOL 1, 53-00-001 FIG 4 USING FASTENERS IAW SRM VOL 2 51-31-01, HL 18PBG-G, PN 89623-01, HLF0-6, B/N 53406-01.

Source: SDR CNMA20090129
OTHER · 2009-03-04 Matched by certificate designator
ATA 5320

Part: BRACKET — BROKEN (BS 1099) · airframe 51,911 hrs · 14,633 cycles

BRACKETS ARE BROKEN C/TO FRAME OF FAIRING STA 1099, STR 30L AND STR 30R. 2 BRACKETS REMOVED NEW FABRICATED PN: OAI-53-0009/-0010 IAW SRM VOL 3 53-53-01 FIG. 3A AND GMM 4.45 USING FASTERERS IAW SRM 51-31-01, MS7-885/G-4-08.

Source: SDR CNMA20090127
OTHER · 2009-03-04 Matched by certificate designator
ATA 5230

Part: WEB — CRACKED (BS 1741-1721) · airframe 51,911 hrs · 14,633 cycles

BS 1741-1721, S-31R APPROX, DURING CTR CARGO DOOR REPAIR WAS FOUND CRACK ON THE INNER WEB. CRACK WAS TRIMMED OUT. AREA WAS REINFORED WITH A DOUBLER PN N522AX-NRC57-1 IAW SRM VOL 1-52-00-01, FIGURE 9 AND INSTALLED USING FASTENERS MS20470D-6-5 B/N 63540-02 IAW SRM 51-35-01 VOL 2.

Source: SDR AAAAACNMA20090144
OTHER · 2009-03-04 Matched by certificate designator
ATA 5320

Part: SUPPORT — CORRODED (BS 457-495) · airframe 51,911 hrs · 14,633 cycles

BS 457-495, RBL 53 CORROSION ON LAVATORY SUPPORT AT 2 EA PLCS. CORRRODED SUPPORT REMOVED. NEW FABRICATED PN OAI-53-001 IAW SRM VOL 3 53-11-01, FIG 1 AND GMM 4.45 USING FASTENERS IAW SRM VOL 2 31-31-01.

Source: SDR CNMA20090132
OTHER · 2009-03-04 Matched by certificate designator
ATA 5347

Part: CARGO TRACK — CORRODED (BS 457-475) · airframe 51,911 hrs · 14,633 cycles

B5 457-475, RBL 56 CORROSION ON TIE DOWN TRACK. DAMAGED AREA TRIMMED OUT. REINFORCED AREA WITH 2 PLATES AND FILLER PN N522AX -NRC595-1/2/3 IAW SRM VOL 1 53-00-01, FIG 7 USING FASTENERS IAW SRM VOL 2 51-31-01.

Source: SDR CNMA20090131
OTHER · 2009-03-04 Matched by certificate designator
ATA 5347

Part: SEAT TRACK — CORRODED (BS 2007) · airframe 51,911 hrs · 14,633 cycles

CORROSION ON LWR SIDE OF RAIL TRACK NEAR STA 2007. DAMAGED AREA TRIMMED OUT REINFORCED AREA WITH DOUBLER AND FILLER PN N522AX, NRC717-1/2 IAW SRM VOL 1, 53-00-01, FIG 2 USING FASTENERS IAW SRM VOL 2 51-31-01, HL19PR6-7, BN 75176-001.

Source: SDR CNMA20090136
OTHER · 2009-03-04 Matched by certificate designator
ATA 5340

Part: FITTING — CRACKED (BS 1257) · airframe 51,911 hrs · 14,633 cycles

LWR AUX FUEL TANK FITTING AT STA 1257, LBL 11, IS CRACKED. CRACKED ANGLE REMOVED NEW ANGLE PN OAI - 53-0005 INSTALLED USING HL18P138-6 HI LOWA B/N 6010-01 WITH HL70-8 COLCARS B/N 53U06-01 FASTENERS INSTALLED IAW SRM VOL II 51-31-01.

Source: SDR CNMA20090138
OTHER · 2009-03-04 Matched by certificate designator
ATA 5315

Part: FLOORBEAM — CRACKED (BS 1980) · airframe 51,911 hrs · 14,633 cycles

FOUND CRACKS ON FLOOR PANEL SUPPORTS AT STD 1980 RBL- 2 AND LBL- 5. DAMAGED FLOORBEAM PARTS REMOVED. NEW FABRICATED SEGMENT PN OAI-53-00121-0013 IAW SRM VOL 3 53-16-01 AND GMM 4.43 USING FASTENERS IAW SRM VOL 2 51-31-01, HL18PB6-4, B/N 69623-01, HL70-6, B/N 53406-01.

Source: SDR CNMA20090141
OTHER · 2009-03-04 Matched by certificate designator
ATA 5312

Part: BULKHEAD — DENTED (MLG WW) · airframe 51,911 hrs · 14,633 cycles

AFT OF CTR LANDING GEAR THERE IS A DENT AT LONGERON 52 APPROX BS 1545. DENTED SKIN LOCALLY TRIMMED, AT DENT PERIPHERY. AREA REINFORCED WITH REPAIR DOUBLERS AND FINGER DOUBLER PN'S N522AX-NRC989-1 THRU - 4 IAW SRM VOL I 53-20-00, FIG 6 (CLASS I REPAIR).

Source: SDR CNMA20090145
OTHER · 2009-03-04 Matched by certificate designator
ATA 5315

Part: FLOORBEAM — CORRODED (BS 2007) · airframe 51,911 hrs · 14,633 cycles

CORROSION ON CHANNEL STA 2007, RBL 53. DAMAGED FLOOR SUPPORT REMOVED. NEW FABRICATED PN OAI 53-0003 IAW SRM VOL 3 53-16-01 AND OMNI 4.45 USING FASTENERS IAW SRM VOL 2, 51-31-01, HL18PB5-4, BN 58313-01, HL70-5, BN 39320-03.

Source: SDR CNMA20090135
OTHER · 2009-03-04 Matched by certificate designator
ATA 5340

Part: FITTING — CRACKED (FUEL TANK) · airframe 51,911 hrs · 14,633 cycles

LWR AUX FUEL TANK FITTING AT STA 1278 RBL 11 IS CRACKED. CRACKED ANGLE REMOVED. NEW ANGLE PN OAI 53-0004 INSTALLED USING HL18PB8-6 HI LOWS (BN 6010U-01) WITH HL70-8 COLLARS BN 53406-01 FASTENERS INSTALLED IAW SRM VOL II 51-31-01.

Source: SDR CNMA20090137
OTHER · 2009-03-04 Matched by certificate designator
ATA 5320

Part: ANGLE — BROKEN (BS 1239-1256) · airframe 51,911 hrs · 14,633 cycles

ANGLE IS BROKEN C/TO EXTERNAL FUSELAGE SKIN B/T STA 1239 AND STA 1256 STR 27L AND STR 28L. BROKEN ANGLE WAS REMOVED AND REPLACED WITH NEW PN OAI 53-0007 FABRICATED AND INSTALLED IAW SRM VOL 3, 53-53-01 FIG 3A AND CMM 4-45 USING FASTENERS PN HL18PBS-4 BN 58513-01 IAW SRM VOL 2 51-33-01.

Source: SDR CNMA20090128
OTHER · 2009-03-04 Matched by certificate designator
ATA 5313

Part: LONGERON — CRACKED (BS 119) · airframe 51,911 hrs · 14,633 cycles

FOUND CRACK ON U CHANNEL BETWEEN STA 1119-1139 STA 51 AREA . DAMAGED CHANNEL REMOVED. NEW FABRICATED PN OAI-53-0008 IAW SRM VOL 3 53-13-01 FIG 11A AND GMM 4.45 USING FASTENERS IAW SRM VOL 2 51-31-01 HL20PB-6-4 B/N 64202-21.

Source: SDR CNMA20090139
OTHER · 2009-03-04 Matched by certificate designator
ATA 5320

Part: SUPPORT — CORRODED (BS 427) · airframe 51,911 hrs · 14,633 cycles

BS 427, RBL 30 CORROSION ON GALLEY SUPPORT. DAMAGED FLOOR SUPPORT REMOVED. NEW FABRICATED PN OAI 53-0002 IAW SRM VOL 3 53-11-01, FIG 1 AND GMM 4.45 USING FASTERERS IAW SRM 51-31-01, VOL 2, HL18PBG-3, BN 63402-01.

Source: SDR CNMA20090133
OTHER · 2009-03-04 Matched by certificate designator
ATA 5340

Part: TEE FITTING — DAMAGED (BS 2007) · airframe 51,911 hrs · 14,633 cycles

BS 2007, RBL 53, DURING TEE FITTING REPAIR WAS FOUND FITTING WITH 5 EA DAMAGED HOLES. DAMAGED FITTING REMOVED. NEW INSTALLED PN: AJC7634-2 IAW SRM VOL 2 51-31-01, HL18PB-6-6, B/N 68329-01, HL70-6, B/N 53406-01.

Source: SDR CNMA20090143
OTHER · 2009-03-04 Matched by certificate designator
ATA 5340

Part: TEE FITTING — CORRODED (BS 2007) · airframe 51,911 hrs · 14,633 cycles

BS 2007, RBL 53 DURING CHANNEL REMOVING IAW NRC 715 WAS FOUND CORROSION ON TEE CHORD UNDERNEATH MENTIONED CHANNEL. DAMAGED PARTS REMOVED. REINFORCED AREA WITH NEW PARTS PN 5320-598-ERA-11 STRAP/ -9 ANGLE/ -5 ANGEL -3 ANGEL/ -7 FILLER IAW SRM VOL 1 53-40-00 FIG 18 USING FASTENERS IAW SROM VOL 2 51-31-01, HL18PB6-6, BN 26206, HL70-6 B/N 53406-01.

Source: SDR CNMA20090142
OTHER · 2009-03-04 Matched by certificate designator
ATA 5320

Part: SUPPORT CHANNEL — TORN (BS 1739) · airframe 51,911 hrs · 14,633 cycles

TEAR ON SUPPORT CHANNEL, STA 1739 ABOVE STR 52. DAMAGED (TEAR) AREA TRIMMED OUT. REINFORCED AREA WITH ANGLE REPAIR PN N522AX NRC301-1 IAW SRM VOL 1 DC 10 53-00-01 FIG 8 USING FASTENERS IAW SRM VOL 2 DC 10- 51-31-01.

Source: SDR CNMA20090126
OTHER · 2009-03-04 Matched by certificate designator
ATA 5320

Part: SUPPORT FITTING — CORRODED (BS 1997-2007) · airframe 51,911 hrs · 14,633 cycles

BS 1997-2007, LBL 60, CORROSION ON SUPPORT FITTING. DAMAGED AREA REMOVED. REINFORCED AREA WITH REPAIR DOUBLER PN 5340599-1-3 IAW SWG NR 5340599-1 USING FASTENERS IAW SRM VOL 2, 51-31-01, HL 18PB-6-4, BN 583113-01, HL70-G, BN 53406-01.

Source: SDR CNMA20090134
OTHER · 2009-03-04 Matched by certificate designator
ATA 5210

Part: WEB — CRACKED (PAX DOOR) · airframe 51,911 hrs · 14,633 cycles

CRACK ON WEB OF PASS DOOR 3L LWR FWD CORNER B/T STA 1256, STA 1273, STR 27L. DAMAGED AREA TRIMMED OUT REINFORCED AREA WITH PN N522AX-NRC301-1 IAW SRM VOL 1 53-00-01 FIG 4 USING FASTENERS IAW SRM VOL 2 31-31-01, FIG 1.

Source: SDR CNMA20090130