# N612AX: Mcdonnell-Douglas DC-10-30

- Status: Valid registration
- Airframe: [Mcdonnell-Douglas DC-10-30](https://openairdocs.org/model/mcdonnell-douglas-dc-10-30) (registry code 3023501, 345 seats)
- Data sheets: [TCDS A22WE](https://openairdocs.org/tcds/A22WE) (The Boeing Company) (OpenAirDocs)
- Serial number: 48290
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Certificate issued: November 21, 2013
- Expires: November 30, 2029
- Mode S code: A7F642
- Registered owner: [Bc Aircraft Leasing LLC](https://openairdocs.org/faa-owner/BC%20AIRCRAFT%20LEASING%20LLC)
- Location: [Albuquerque, NM](https://openairdocs.org/faa-place/NM/Albuquerque)
- Owner type: LLC
- Owner's area on the map: 35.0071° N, 106.6098° W: Placed by OpenAirDocs at the center of ZIP code 87106, within about 3 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=612AX
- Page: https://openairdocs.org/aircraft/N612AX

From the FAA registry file of October 24, 2026. ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination.

## ADs that may apply (OpenAirDocs): 240 in force

### Matched by airframe (Mcdonnell-Douglas DC-10-30)

- [AD 2026-13-15](https://openairdocs.org/ad/2026-13-15): Navigation · Boeing 707-100 Long Body, 707-200, 707-100B Long Body and 74 more. Effective Jul 1, 2026
- [AD 2026-13-02](https://openairdocs.org/ad/2026-13-02): Navigation · Airbus Canada Limited Partnership 18, 49-46, 80-A and 555 more. Effective Jul 1, 2026
- [AD 2025-23-53](https://openairdocs.org/ad/2025-23-53): Nacelles/pylons · Boeing MD-11, MD-11F, MD-10-10F and 8 more. Effective Dec 1, 2025
- [AD 2023-12-15](https://openairdocs.org/ad/2023-12-15): Navigation · Boeing 707-100 Long Body, 707-200, 707-100B Long Body and 74 more. Effective Jun 21, 2023
- [AD 2023-10-02](https://openairdocs.org/ad/2023-10-02): Indicating/Recording System, Navigation · Boeing 18, 23, 35 and 1,060 more. Effective May 26, 2023
- [AD 2021-08-10](https://openairdocs.org/ad/2021-08-10): Nacelles/pylons · Boeing DC-10-10, DC-10-10F, DC-10-15 and 6 more. Effective May 25, 2021
- [AD 2020-22-15](https://openairdocs.org/ad/2020-22-15): Fuselage · Boeing DC-10-10, DC-10-10F, DC-10-15 and 8 more. Effective Dec 18, 2020
- [AD 2018-22-10](https://openairdocs.org/ad/2018-22-10): Fuel · Boeing DC-10-10, DC-10-10F, DC-10-15 and 8 more. Effective Dec 12, 2018
- [AD 2015-02-05](https://openairdocs.org/ad/2015-02-05): Navigation · Boeing 717-200, DC-10-10, DC-10-10F and 13 more. Effective Mar 5, 2015
- [AD 2014-21-05](https://openairdocs.org/ad/2014-21-05): Fuselage · Boeing DC-10-10, DC-10-10F, DC-10-30 and 4 more. Effective Dec 2, 2014
- [AD 2012-19-03](https://openairdocs.org/ad/2012-19-03): Fuselage · Boeing DC-10-10, DC-10-10F, DC-10-15 and 6 more. Effective Nov 5, 2012
- [AD 2011-21-08](https://openairdocs.org/ad/2011-21-08): Equipment/Furnishings · ATR - GIE Avions de Transport Régional ATR42-200, ATR42-300, ATR42-320 and 202 more. Effective Nov 23, 2011
- [AD 2011-12-01](https://openairdocs.org/ad/2011-12-01): Equipment/Furnishings · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 268 more. Effective Aug 1, 2011
- [AD 2011-11-05](https://openairdocs.org/ad/2011-11-05): Fuel · Boeing DC-10-10, DC-10-10F, DC-10-15 and 10 more. Effective Jul 6, 2011
- [AD 2010-21-13](https://openairdocs.org/ad/2010-21-13): Fuel · Boeing DC-10-10, DC-10-10F, DC-10-30 and 3 more. Effective Nov 18, 2010
- [AD 2010-20-13](https://openairdocs.org/ad/2010-20-13): Fuel · Boeing DC-10-30, DC-10-30F (KC-10A, KDC-10), DC-10-40 and 2 more. Effective Nov 9, 2010
- [AD 2010-20-14](https://openairdocs.org/ad/2010-20-14): Fuel · Boeing DC-10-10, DC-10-10F, DC-10-15 and 8 more. Effective Nov 5, 2010
- [AD 2010-09-12](https://openairdocs.org/ad/2010-09-12): Fuel · Boeing DC-10-10, DC-10-10F, DC-10-15 and 8 more. Effective Jun 8, 2010
- [AD 2009-21-10 R1](https://openairdocs.org/ad/2009-21-10-R1): Oxygen · Airbus A300 B4-605R, A300 B4-620, A300 B4-622 and 138 more. Effective Feb 4, 2010
- [AD 2008-06-21 R1](https://openairdocs.org/ad/2008-06-21-R1): Fuel tank systems · Boeing DC-10-10, DC-10-10F, DC-10-15 and 8 more. Effective Dec 10, 2009
- [AD 2009-03-02](https://openairdocs.org/ad/2009-03-02): Auxiliary hydraulic pumps · Boeing DC-10-10, DC-10-10F, DC-10-15 and 8 more. Effective Mar 31, 2009
- [AD 2008-17-16](https://openairdocs.org/ad/2008-17-16): Fuel boost pump · Boeing DC-10-10, DC-10-10F, DC-10-15 and 8 more. Effective Oct 2, 2008
- [AD 2006-16-18 R1](https://openairdocs.org/ad/2006-16-18-R1): Installing a warning placard on the TAWS/RMI · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 100 more. Effective Jul 18, 2008
- [AD 2007-25-20](https://openairdocs.org/ad/2007-25-20): Thrust reverser command wiring · Boeing DC-10-10, DC-10-10F, DC-10-15 and 6 more. Effective Jan 22, 2008
- [AD 2007-19-17](https://openairdocs.org/ad/2007-19-17): System 3 hydraulic piping · Boeing DC-10-10, DC-10-10F, DC-10-15 and 8 more. Effective Oct 26, 2007
- [AD 2007-19-02](https://openairdocs.org/ad/2007-19-02): Fuel tank and the fuel transfer pump housing flange · Boeing DC-10-30, DC-10-30F (KC-10A, KDC-10), DC-10-40 and 4 more. Effective Oct 17, 2007
- [AD 2007-13-10](https://openairdocs.org/ad/2007-13-10): Fuel pump wire harness · Boeing DC-10-30 and DC-10-30F (KC-10A, KDC-10). Effective Aug 3, 2007
- [AD 2007-11-15](https://openairdocs.org/ad/2007-11-15): Center main wheel well · Boeing DC-10-30, DC-10-30F (KC-10A, KDC-10), DC-10-40 and 2 more. Effective Jul 5, 2007
- [AD 2007-10-12](https://openairdocs.org/ad/2007-10-12): Reinforced flight deck door · Reinforced cockpit door (Safran Cabin STC ST01335LA or 2 others). Effective Jun 27, 2007
- [AD 2007-04-17](https://openairdocs.org/ad/2007-04-17): Control modules of the fire detection systems · Boeing DC-10-10, DC-10-10F, DC-10-15 and 6 more. Effective Mar 23, 2007
- [AD 2006-19-03](https://openairdocs.org/ad/2006-19-03): Fabrication and installation of a wire harness guard in the right wheel well of the main  
 landing gear (MLG) · Boeing DC-10-10, DC-10-10F, DC-10-15 and 8 more. Effective Oct 17, 2006
- [AD 2006-16-12](https://openairdocs.org/ad/2006-16-12): Fuel tanks 1, 2, and 3 · Boeing DC-10-10, DC-10-10F, DC-10-30 and 3 more. Effective Sep 13, 2006
- [AD 2006-04-04](https://openairdocs.org/ad/2006-04-04): Smoke detectors · ATR - GIE Avions de Transport Régional ATR42-200, ATR42-300, ATR42-320 and 37 more. Effective Mar 24, 2006
- [AD 2006-03-13](https://openairdocs.org/ad/2006-03-13): Inboard and outboard hinge fittings · Boeing DC-10-10, DC-10-10F, DC-10-15 and 8 more. Effective Mar 16, 2006
- [AD 2006-02-11](https://openairdocs.org/ad/2006-02-11): Drain holes of the pitot tubes · Boeing DC-10-10, DC-10-10F, DC-10-15 and 8 more. Effective Mar 3, 2006
- [AD 2005-20-15](https://openairdocs.org/ad/2005-20-15): Rudder pedal torque tube assembly · Boeing DC-10-10, DC-10-10F, DC-10-15 and 8 more. Effective Nov 10, 2005
- [AD 2005-17-04](https://openairdocs.org/ad/2005-17-04): Fire extinguishing system · Boeing DC-10-10, DC-10-10F, DC-10-15 and 8 more. Effective Sep 26, 2005
- [AD 2005-15-12](https://openairdocs.org/ad/2005-15-12): Exterior emergency control handle assemblies of the forward passenger doors · Boeing DC-10-10, DC-10-10F, DC-10-15 and 8 more. Effective Aug 30, 2005
- [AD 2005-15-03](https://openairdocs.org/ad/2005-15-03): Exterior emergency control handle assemblies · Boeing DC-10-10, DC-10-10F, DC-10-15 and 8 more. Effective Aug 25, 2005
- [AD 2005-14-10](https://openairdocs.org/ad/2005-14-10): Structural inspections · Boeing DC-10-10, DC-10-10F, DC-10-15 and 4 more. Effective Aug 18, 2005
- [AD 2004-22-01](https://openairdocs.org/ad/2004-22-01): Cargo restraint strap assemblies · Cargo restraint straps (Airline Container Manufacturing STC ST01004NY). Effective Dec 1, 2004
- [AD 2004-18-15](https://openairdocs.org/ad/2004-18-15): Flight engineer's station · Boeing DC-10-10, DC-10-10F, DC-10-15 and 6 more. Effective Oct 19, 2004
- [AD 2004-10-12](https://openairdocs.org/ad/2004-10-12): Power Feeder Cable Assembly of the Auxiliary Power Unit (APU) · Boeing DC-10-30. Effective Jun 25, 2004
- [AD 2004-05-06](https://openairdocs.org/ad/2004-05-06): Number one passenger door slide · Boeing DC-10-10, DC-10-10F, DC-10-15 and 8 more. Effective Apr 7, 2004
- [AD 2004-02-06](https://openairdocs.org/ad/2004-02-06): Forward aft bracket · Boeing DC-10-10, DC-10-10F, DC-10-15 and 8 more. Effective Mar 5, 2004
- [AD 2003-25-13](https://openairdocs.org/ad/2003-25-13): Power feeder cables · Boeing DC-10-10, DC-10-10F, DC-10-15 and 4 more. Effective Jan 27, 2004
- [AD 2003-24-10](https://openairdocs.org/ad/2003-24-10): Rudder pedal arm assembly · Boeing DC-10-10, DC-10-10F, DC-10-15 and 8 more. Effective Jan 8, 2004
- [AD 2003-03-15 R1](https://openairdocs.org/ad/2003-03-15-R1): Airplane Flight Manual (AFM) - oxygen masks · Boeing 707-100 Long Body, 707-100B Long Body, 707-100B Short Body and 90 more. Effective Dec 22, 2003
- [AD 2003-19-05](https://openairdocs.org/ad/2003-19-05): Inboard and outboard flaps · Boeing DC-10-10, DC-10-10F, DC-10-15 and 6 more. Effective Oct 27, 2003
- [AD 2003-17-07 R1](https://openairdocs.org/ad/2003-17-07-R1): Auxiliary power unit (APU) · Boeing DC-10-10, DC-10-10F, DC-10-15 and 57 more. Effective Sep 24, 2003

### Historical (superseded or no longer in force)

- [AD 2022-09-18](https://openairdocs.org/ad/2022-09-18) (historical): Navigation · Boeing 707-100 Long Body, 707-100B Long Body, 707-100B Short Body and 72 more. Effective May 23, 2022
- [AD 2016-04-16](https://openairdocs.org/ad/2016-04-16) (historical): Fuel · Boeing DC-10-10, DC-10-10F, DC-10-15 and 8 more. Effective Apr 15, 2016
- [AD 2013-08-23](https://openairdocs.org/ad/2013-08-23) (historical): Fuel · Boeing DC-10-10, DC-10-10F, DC-10-15 and 8 more. Effective May 29, 2013
- [AD 2009-26-17](https://openairdocs.org/ad/2009-26-17) (historical): Fuselage · Boeing DC-10-10, DC-10-10F, DC-10-15 and 6 more. Effective Feb 4, 2010
- [AD 2009-21-10](https://openairdocs.org/ad/2009-21-10) (historical): Oxygen · Airbus A300, Model B4-605R, A300, Model B4-620, A300, Model B4-622 and 138 more. Effective Dec 17, 2009
- [AD 2008-06-21](https://openairdocs.org/ad/2008-06-21) (historical): Fuel tank systems · McDonnell Douglas DC-10-10, DC-10-10F, DC-10-15 and 8 more. Effective Apr 23, 2008
- [AD 2007-15-05](https://openairdocs.org/ad/2007-15-05) (historical): Fuel pump housing electrical connector · Boeing DC-10-10, DC-10-10F, DC-10-15 and 9 more. Effective Aug 8, 2007
- [AD 2006-16-03](https://openairdocs.org/ad/2006-16-03) (historical): Bonding straps · McDonnell Douglas DC-10-10, DC-10-10F, DC-10-15 and 5 more. Effective Sep 7, 2006
- [AD 2005-12-05](https://openairdocs.org/ad/2005-12-05) (historical): Flight deck door · Reinforced cockpit door (Safran Cabin STC ST01335LA or 2 others). Effective Jul 19, 2005
- [AD 2004-05-20](https://openairdocs.org/ad/2004-05-20) (historical): Electric motor operated auxiliary hydraulic pumps · McDonnell Douglas DC-10-10, DC-10-10F, DC-10-15 and 9 more. Effective Apr 15, 2004
- [AD 2003-17-07](https://openairdocs.org/ad/2003-17-07) (historical): Fire Extinguishers for the Engine and Auxiliary Power Unit (APU) · McDonnell Douglas DC-10-10, DC-10-10F, DC-10-15 and 60 more. Effective Sep 24, 2003
- [AD 2003-14-04](https://openairdocs.org/ad/2003-14-04) (historical): Flight Deck Door Pressure Relief Latch Assemblies · Boeing 737-200 Series, 737-300 Series, 737-400 Series and 14 more. Effective Jul 25, 2003
- [AD 2003-03-15](https://openairdocs.org/ad/2003-03-15) (historical): Airplane Flight Manual (AFM) - Oxygen Masks · Boeing 707 Series (all), 720 Series (all), 727 Series (all) and 75 more. Effective Mar 7, 2003
- [AD 2000-16-10](https://openairdocs.org/ad/2000-16-10) (historical): Inboard and Outboard Flap Assembly · McDonnell Douglas DC-10-10, DC-10-10F, DC-10-15 and 3 more. Effective Sep 25, 2000
- [AD 95-04-07 R2](https://openairdocs.org/ad/95-04-07-R2) (historical): Engine Mount Bolts · McDonnell Douglas DC-10-10, DC-10-10F, DC-10-15 and 2 more. Effective Nov 10, 1999
- [AD 74-08-09 R2](https://openairdocs.org/ad/74-08-09-R2) (historical): Waste Receptacles · Aero Spacelines 377, 377MG, 377SGT and 268 more. Effective Jul 29, 1996
- [AD 96-07-01](https://openairdocs.org/ad/96-07-01) (historical): Vertical Stabilizer Attachments · McDonnell Douglas DC-10-10, DC-10-10F, DC-10-15 and 4 more. Effective Apr 24, 1996
- [AD 95-04-07 R1](https://openairdocs.org/ad/95-04-07-R1) (historical): Lockwires On Forward Engine Mount Bolts · McDonnell Douglas DC-10-10, DC-10-15, DC-10-30 and 1 more. Effective Mar 17, 1995
- [AD 95-04-07](https://openairdocs.org/ad/95-04-07) (historical): Lockwires on Engine Mount Bolts · McDonnell Douglas DC-10-10, DC-10-15, DC-10-30 and 1 more. Effective Mar 17, 1995
- [AD 91-21-05](https://openairdocs.org/ad/91-21-05) (historical): Wing Rear Spar · McDonnell Douglas DC-10-10, DC-10-10F, DC-10-15 and 4 more. Effective Oct 23, 1991
- [AD 88-16-02 R1](https://openairdocs.org/ad/88-16-02-R1) (historical): Landing gear brakes · McDonnell Douglas DC-10-30, DC-10-30F (KC-10A, KDC-10) and DC-10-40. Effective Oct 14, 1988
- [AD 75-04-11](https://openairdocs.org/ad/75-04-11) (historical): Ingestion of Ice and Snow · McDonnell Douglas DC-10-10, DC-10-10F, DC-10-30 and 1 more. Effective Feb 21, 1975

All 262: https://openairdocs.org/aircraft/N612AX/ads.md

## Information bulletins (advisory) (3 in force)

- [SAIB NE-19-03](https://openairdocs.org/saib/NE-19-03): Escape Slide Maintenance Tasks and Intervals - JASC 2565. Issued Feb 19, 2019
- [SAIB NM-15-03](https://openairdocs.org/saib/NM-15-03): Flight Controls. Issued Nov 24, 2014
- [SAIB NM-09-03](https://openairdocs.org/saib/NM-09-03): Engine Fuel and Control - Implementing Fuel Tank System Airworthiness Limitations. Issued Dec 11, 2008

## NTSB investigations

None matched to N612AX.

## FAA accident and incident reports

None matched to N612AX.

## Service difficulty reports (31)

As reported by operators and repair stations. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR ZTRR20200910002](https://openairdocs.org/sdr/ZTRR20200910002), Aug 30, 2020: HINGE. DEPARTED. 2020-08-30 UPON LANDING DURING MX WALK-AROUND NR 2 ENGINE RIGHT CORE COWL WAS NOTICED TO HAVE FAILED DURING FLIGHT, PI-REP ENG 2 CORE COWL DAMAGED AND PIECES MI
- [SDR CNMA20110007](https://openairdocs.org/sdr/CNMA20110007), Mar 24, 2011: PAN. CORRODED. FWD P17, STA 870, LWR BILGE LAV DUMP PAN HAS SEVERAL AREAS OF CORROSION ON TOP AND RT SIDE OF PAN. REMOVED CORROSION FROM RT SIDE OF PAN FOUND TO BE WITHIN LIMI
- [SDR CNMA20110011](https://openairdocs.org/sdr/CNMA20110011), Mar 19, 2011: INTERCOSTAL. CORRODED. SUPPORT ANGLE AND INTERCOSTAL AT APPROX LONGERON 44L HAS AREAS OF CORROSION AND FASTENER HEADS POPPED FROM STA 535 TO 595. REPAIRED INTERCOSTAL IAW SRM VOL I 53
- [SDR CNMA20110006](https://openairdocs.org/sdr/CNMA20110006), Mar 19, 2011: ATTACH ANGLE. CORRODED. CORROSSION ON FUSELAGE FRAME ATTACH ANGLE AT LONGERON 51L STA. 1119. REMOVED CORROSSION FOUND OUT OF LIMITS FABRICATED REPAIR DOUBLER FROM .080 7075-0 HEAT TREA
- [SDR CNMA20110005](https://openairdocs.org/sdr/CNMA20110005), Mar 19, 2011: DOOR FRAME. CORRODED. SURFACE CORROSSION ON AFT PIT DOOR FWD SIDE OF FRAME ON LOWER AFT SIDE AT LONGERON 42L TO 46L AT STA 1957. R & R FRAME AT STA 1957 IAW SRM VOL II 51-35-01, PG 1
- [SDR CNMA20110004](https://openairdocs.org/sdr/CNMA20110004), Mar 19, 2011: BULKHEAD. CRACKED. NR 3 PYLON HAS CRACK ON AFT BULKHEAD UPPER INBD FLANGE COMING OUT OF RADIUS AT PYLON STA 418. REMOVED NR 3 PYLON REPLACED AFT PYLON BULKHEAD IAW DWG NR AWB70125
- [SDR CNMA20100035](https://openairdocs.org/sdr/CNMA20100035), Dec 29, 2010: STRAINER. CLOGGED. ENG 3 OIL STRAINER CLOG LIGHT ILLUMINATED STEADY IN FLIGHT, ACCOMPLISHED QRH PROCEDURE NR3 ENGINE SHUTDOWN. C/A: REPLACED ENGINE.
- [SDR CNMA20100019](https://openairdocs.org/sdr/CNMA20100019), May 8, 2010: DECODER. FAILED. F/A'S BROUGHT TO ATTENTION OF COCKPIT THAT IF READING LIGHTS, CALL LIGHTS AND AUDIO INOP IN B ZONE MAY EFFECT O2 GENERATORS, MAINT CONTROL CONFIRMED RETURNED TO
- [SDR CNMA20100004](https://openairdocs.org/sdr/CNMA20100004), Feb 9, 2010: INDICATOR. DEFECTIVE. FL300 PRESSURE DIFF INDICATING 4 PSID, ALT INDICATED 3500' DECREASED CABIN TO 1800' PRESS RELIEF LIGHT ON, NEITHER DIFF INDICATION OR ALT WERE GIVING CORRECT IN
- [SDR CNMA20100001](https://openairdocs.org/sdr/CNMA20100001), Jan 7, 2010: RETRACT CYLINDER. DEFECTIVE. UPON GEAR RETRACTION, LT MLG RED LIGHT ON LOOKED THRU VIEWER, SAW GROUND LIGHTS, FELT VIBRATION. REMOVED AND REPLACED LT MLG RETRACT ACTUATOR. OPS CHECKS GOOD I
- [SDR CNMA20090001](https://openairdocs.org/sdr/CNMA20090001), Mar 28, 2009: ENGINE. POWER LOSS. NR 2 ENGINE COMPRESSOR STALL CLIMBING THRU 320 NO THROTTLE MOVEMENT SMOOTH WEATHER. N1 DROPPED TO 90%, EGT 850 WITH VIBRATION. CORRECTIVE ACTION REPLACED ENGINE
- [SDR CNMA20090102](https://openairdocs.org/sdr/CNMA20090102), Jan 22, 2009: PANEL. CRACKED. NR1 PYLON PRE-COOLER EXHAUST GRILL PANEL HAS 4 INCH CRACK AT 3RD INBD SCREW HOLE. PERFROMED A REPAIR IAW SRM VOL 1, 54-00-01, FIG 2B. INSTALLED FASTENERS IAW SR
- [SDR CNMA20090101](https://openairdocs.org/sdr/CNMA20090101), Jan 22, 2009: CHANNEL. DAMAGED. RT WING L/E LWR PANEL XORS 917 -949 DEEP ABRASION ON INNER CHANNEL C/TO PANEL. DAMAGED CHANNEL WAS REMOVED NEW CABLE GUARD WAS FABRICATED AND INSTALLED IAW DWG 
- [SDR CNMA20090100](https://openairdocs.org/sdr/CNMA20090100), Jan 22, 2009: SKIN. CRACKED. BS 515-535, STR 32L, THERE IS A CRACK ON AIR CON BAY DOOR SKIN UPPER EDGE. DAMAGED AREA WAS TRIMMED OUT. DOOR WAS REINFORCED WITH 2 DOUBLERS AND 1 FILLER PN N61
- [SDR CNMA20090099](https://openairdocs.org/sdr/CNMA20090099), Jan 22, 2009: FLOOR SUPPORT. CORRODED. B/T STA 824 AND STA 859, LBL 38 CORROSION ON FLOOR SUPPORT. CORROSION WAS BLENDED OUT IAW SRM VOL 2, 51-21-01 AREA WAS REINFORCED WITH A STRAP IAW SRM VOL 1, 53
- [SDR CNMA20090098](https://openairdocs.org/sdr/CNMA20090098), Jan 22, 2009: FLOOR SUPPORT. CORRODED. STA 889, LBL 38, CORROSION ON FLOOR SUPPORT. CORROSION WAS BLENDED OUT IAW SRM VOL 2, 51-21-01 AREA WAS REINFORCED WITH A STRAP IAW SRM VOL 1, 53-00-01, FIG 7. 
- [SDR CNMA20090097](https://openairdocs.org/sdr/CNMA20090097), Jan 22, 2009: FLOOR SUPPORT. DAMAGED. DOUBLE HOLE ON FLOOR SUPPORT STA 1884, LBL 4. DAMAGED FLOOR SUPPORT WAS REMOVED. NEW FLOOR SUPPORT FABRICATED AND INSTALLED IAW SRM VOL 3, 53-16-01 AND GMM 4.45
- [SDR CNMA20090095](https://openairdocs.org/sdr/CNMA20090095), Jan 22, 2009: CHANNEL. DAMAGED. LT WING L/E LWR 4TH PANEL FROM TIP INNER CHANNEL TORN. DAMAGED CHANNEL REMOVED. FABRICATED NEW CHANNEL IAW DWG ARB2946-24 AND GMM 4.45. INSTALLED FASTENERS IAW 
- [SDR CNMA20090094](https://openairdocs.org/sdr/CNMA20090094), Jan 22, 2009: FITTING. DAMAGED. CTR CARGO COMP AFT WALL IN FRONT OF AFT FUEL TANK ON EACH BREAKER (NOT SURE CAN'T READ WORD?) FOUND CRACKED. DAMAGED FITTING WAS REMOVED. A NEW FITTING WAS FABR
- [SDR CNMA20090093](https://openairdocs.org/sdr/CNMA20090093), Jan 22, 2009: SKIN. DAMAGED. LT OTBD FLAP VANE HAS A SMALL HOLE AT UPPER SKIN ABOVE FLAP OTBD FAIRING. HOLE ON OTBD FLAP VANE REPAIRED WITH EXTERNAL DOUBLER IAW SRM 51-71-00, PAR 16B.
- [SDR CNMA20090092](https://openairdocs.org/sdr/CNMA20090092), Jan 22, 2009: STRAP. DAMAGED. BS 1931, LBL 27, DOUBLE HOLE ON STRAP WITH NUT PLATES. DAMAGED AREA TRIMMED OUT. REINFORCED AREA WITH ANGLE IAW SRM VOL 1, 53-00-01, FIG 8 INSTALLED FASTENERS I
- [SDR CNMA20090091](https://openairdocs.org/sdr/CNMA20090091), Jan 22, 2009: FRAME. CORRODED. BS 1902, FROM BL 0.0 TO LBL15, CORROSION ON FRAME LWR CHORD. CORRODED SECTION OF CHORD WAS TRIMMED OUT. CHORD WAS REINFORCED WITH A REPAIR ANGLE, STRAP AND FILL
- [SDR CNMA20090090](https://openairdocs.org/sdr/CNMA20090090), Jan 22, 2009: INTERCOSTAL. CRACKED. BS 1701-1721, STR 38L-39L, THERE IS A CRACK ON THE INTERCOSTAL. CRACK WAS DRILLED OUT, INTERCOSTAL WAS REINFORCED WITH AN ANGLE AND INSTALLED IAW SRM VOL 1, 53-
- [SDR CNMA20090089](https://openairdocs.org/sdr/CNMA20090089), Jan 22, 2009: INTERCOSTAL. BROKEN. BS 1741-1761, STR 38L-39L, INTERCOSTAL IS BROKEN. BROKEN EDGE WAS TRIMMED OUT, INTERCOSTAL WAS REINFORCED WITH AN ANGLE. FABRICATED AND INSTALLED IAW SRM VOL 1 
- [SDR CNMA20090088](https://openairdocs.org/sdr/CNMA20090088), Jan 22, 2009: SUPPORT. BROKEN. BS 999, LBL 13, CABLE ANGLE SUPPORT IS BROKEN. DAMAGED SUPPORT REMOVED AND NEW FABRICATED IAW DWG AAP8000-1077, GMM 4.45 INSTALLED FASTENERS IAW SRM VOL 2, 51-3
- [SDR CNMA20090087](https://openairdocs.org/sdr/CNMA20090087), Jan 22, 2009: SUPPORT. BROKEN. BS979, LBL13, CABLE ANGLE SUPPORT IS BROKEN. DAMAGED SUPPORT REMOVED AND INSTALLED IAW DWG AAP8000-1077, GMM 4.45. INSTALLED FASTENERS IAW SRM VOL 2, 51-31-01.
- [SDR CNMA20090086](https://openairdocs.org/sdr/CNMA20090086), Jan 22, 2009: BRACKET. BROKEN. BS 959, LBL 13, CABLE ANGLE SUPPORT IS BROKEN C/T INTERCOSTAL. DAMAGED BRACKET REMOVED AND NEW PN OAI-53-0001 IAW DWG AAP 8000 -1077, GMM 4.45 USING FASTENERS I
- [SDR CNMA20090085](https://openairdocs.org/sdr/CNMA20090085), Jan 22, 2009: CHANNEL. CRACKED. BS 879, RBL 16, THERE IS A CRACK ON U-CHANNEL. DAMAGED CHANNEL WAS REMOVED. A NEW FLOOR SUPPORT WAS FABRICATED IAW SRM VOL 3, 53-13-01, FIG 12 AND GMM 4.45 AND 
- [SDR CNMA20090084](https://openairdocs.org/sdr/CNMA20090084), Jan 22, 2009: SUPPORT. CRACKED. BS 1341, STR 31L, THERE IS A CRACK ON OVERWING FAIRING SUPPORT. CRACKED AREA TRIMMED OUT. REINFORCED AREA WITH DOUBLER PN NG12AX-NRC454-1 IAW SRM VOL 1, 53-00-0
- [SDR CNMA20090083](https://openairdocs.org/sdr/CNMA20090083), Jan 22, 2009: FLOOR SUPPORT. DAMAGED. BS 1741, LBL 40 DOUBLE-MOLE ON CARGO FLOOR SUPPORT. REMOVED DAMAGED FLOOR SUPPORT AND NEW FLOOR SUPPORT PN AOI-53-0015 ARE INSTALLED IAW SRM VOL III 53-15-01 AN
- [SDR CNMA20090082](https://openairdocs.org/sdr/CNMA20090082), Jan 22, 2009: FLOOR SUPPORT. DAMAGED. BS1741, RBL 40 DOUBLE HOLE ON FLOOR SUPPORT. REMOVED DAMAGED FLOOR SUPPORT AND NEW FLOOR SUPPORT PN OAI - 53-0014 IAW SRM VOL III 53-15-01 AND GMM 4.45.

## STCs that may be installed (OpenAirDocs) (382, first 50)

Approved for this aircraft's airframe or engine model, in force first, then newest. The registry doesn't record which STCs an aircraft has; its records do.

### Approved for the airframe (Mcdonnell-Douglas DC-10-30)

- [STC ST00272AT](https://openairdocs.org/stc/ST00272AT): Installation of an Airshow 210 enter- tainment system. AIRCRAFT RECONFIG TECHNOLOGIES, LLC. Lists DC-10 Series
- [STC ST00952LA](https://openairdocs.org/stc/ST00952LA): Installation of Mass Systems fire extinguisher cartridges as replacements for Kidde fire extinguisher cartridges in fire extinguisher bottles. AMETEK AMERON LLC d/b/a MASS Systems
- [STC SA2622NM](https://openairdocs.org/stc/SA2622NM): Installation of Precise Flight Pulselite Control Unit in landing/taxi system. (767-200 B17) (DHC-8 101). Precise Flight Inc
- [STC SA5040NM](https://openairdocs.org/stc/SA5040NM): Installation of cargo pallet and net. Satco Inc
- [STC ST00030IB](https://openairdocs.org/stc/ST00030IB): Installation of Test Tech ELT. APTOZ EHF
- [STC ST03885AT](https://openairdocs.org/stc/ST03885AT): Installation of an Avionica, Inc. avCM Cellular Module. Aircraft Systems and Manufacturing Inc
- [STC SA1368NM](https://openairdocs.org/stc/SA1368NM): Installation of C&D Interiors P/N 1441002. Safran Cabin Inc
- [STC SA1369NM](https://openairdocs.org/stc/SA1369NM): Installation of closets. Safran Cabin Inc
- [STC SA2049NM](https://openairdocs.org/stc/SA2049NM): Installation of C&D Interiors P/N 1751001-101, -102. Safran Cabin Inc
- [STC SA2175NM](https://openairdocs.org/stc/SA2175NM): Installation of the Centerline Overhead Stowage Retrofit Kit. Safran Cabin Inc
- [STC SA2471NM](https://openairdocs.org/stc/SA2471NM): Installation of centerline bin, overhead side bin. Safran Cabin Inc
- [STC SA2499NM](https://openairdocs.org/stc/SA2499NM): Installation of closet/windscreen. Safran Cabin Inc
- [STC SA3127NM](https://openairdocs.org/stc/SA3127NM): Installation of Closet. Safran Cabin Inc
- [STC SA3422NM](https://openairdocs.org/stc/SA3422NM): Installation of a galley. Safran Cabin Inc
- [STC SA3460NM](https://openairdocs.org/stc/SA3460NM): Installation of centerline stowage bins. Safran Cabin Inc. Lists DC-10 Series
- [STC SA3804NM](https://openairdocs.org/stc/SA3804NM): Installation of the Centerline SkyBin Stowage Interior kit. Safran Cabin Inc
- [STC SA3967NM](https://openairdocs.org/stc/SA3967NM): Installation of bi-fold lavatory door. Safran Cabin Inc
- [STC SA4832NM](https://openairdocs.org/stc/SA4832NM): Installation of C&D Interiors Part Numbers 3001001-105 Credenza, 4761001-101 C/L Closet, and 4771001-101 and -102 L.H. and R.H. Closet. Safran Cabin Inc
- [STC SA5492NM](https://openairdocs.org/stc/SA5492NM): Installation of galleys, dividers, closet, and fold-down table. Safran Cabin Inc
- [STC SA8001NM](https://openairdocs.org/stc/SA8001NM): Installation of C&D Interiors class divider and ceiling panel. Safran Cabin Inc
- [STC ST00495LA](https://openairdocs.org/stc/ST00495LA): Installation of lavatories. Safran Cabin Inc
- [STC ST00584LA](https://openairdocs.org/stc/ST00584LA): Installation of centerline bin kits. Safran Cabin Inc
- [STC ST00650LA](https://openairdocs.org/stc/ST00650LA): Installation of lavatories. Safran Cabin Inc
- [STC ST01077LA](https://openairdocs.org/stc/ST01077LA): Installation of passenger service unit (PSU). Safran Cabin Inc
- [STC ST01391LA](https://openairdocs.org/stc/ST01391LA): Installation of a reinforced cockpit door. Safran Cabin Inc
- [STC SA3411NM](https://openairdocs.org/stc/SA3411NM): Installation of floor proximity emergency escape path marking system. Bruce Aerospace Inc
- [STC ST01694AT](https://openairdocs.org/stc/ST01694AT): Installation of additional sensors for recording additional parameters on Digital Flight Data Recorder (DFDR). Acron Aviation Inc
- [STC ST02472AT](https://openairdocs.org/stc/ST02472AT): Installation of a mini Quick Access Recorder (QAR) model MKI, MKII, or MKIII. Aircraft Systems and Manufacturing Inc
- [STC ST02117CH](https://openairdocs.org/stc/ST02117CH): Installation of Honeywell Enhanced Ground Proximity Warning System and GPS antenna. Amphenol Cable and Interconnect Technologies Inc
- [STC ST02184CH](https://openairdocs.org/stc/ST02184CH): Installation of elementary or enhanced surveillance Mode S transponders. Amphenol Cable and Interconnect Technologies Inc
- [STC ST00079IB](https://openairdocs.org/stc/ST00079IB): Integration of Halon-free Portable Fire Extinguisher HAFEX. UMLAUT ENGINEERING GMBH
- [STC ST02131AT](https://openairdocs.org/stc/ST02131AT): Installation of SAF-T-GLO photoluminescent floor proximity emergency escape with marking system (FPEEPMS). STG Aerospace Inc
- [STC SA3474NM](https://openairdocs.org/stc/SA3474NM): Installation of Galley 1, Galley 2, Galley 1A, Coartoom and Lavatories. Safran Cabin Inc
- [STC ST01986CH](https://openairdocs.org/stc/ST01986CH): Installation of a Honeywell RESCU 406AF Emergency Locator Transmitter (ELT) system. Honeywell International Inc
- [STC ST02929AT](https://openairdocs.org/stc/ST02929AT): Installation of an Artex Model C406-1 Emergency Locator Transmitter (ELT). Woven Electronics LLC
- [STC SA1220NW](https://openairdocs.org/stc/SA1220NW): Installation of Universal flight data recorder. Honeywell International Inc
- [STC SA3046SO](https://openairdocs.org/stc/SA3046SO): Installation of a single/dual TRA-67 Mode S ATC transponder system. Honeywell International Inc
- [STC SA3061SO](https://openairdocs.org/stc/SA3061SO): Installation of a CAS-81 TCAS II system. Honeywell International Inc
- [STC SA5794NM](https://openairdocs.org/stc/SA5794NM): Installation of Mark VII ground proximity and windshear warning system. Honeywell International Inc
- [STC ST00536SE](https://openairdocs.org/stc/ST00536SE): Installation of the Honeywell MK VII Enhanced Ground Proximity Warning System (EGPWS). Honeywell International Inc
- [STC SA5672SW-D](https://openairdocs.org/stc/SA5672SW-D): Modification of air to air heat exchanger (P/N 187900-9). Honeywell International Inc
- [STC SA8928SW](https://openairdocs.org/stc/SA8928SW): Replace core assembly of AiResearch Bleed Air Precooler, part numbers 187890-3 and 189740-3. Honeywell International Inc
- [STC SA8757SW](https://openairdocs.org/stc/SA8757SW): Replace core assembly of Janitrol Constant Speed Drive (CSD) Oil Cooler, part number B63D89. Honeywell International Inc
- [STC SA7419SW](https://openairdocs.org/stc/SA7419SW): Rebuild DC-10 Auxiliary Power Unit Oil Cooler Assembly by manufacturing a new core assembly. Honeywell International Inc. Lists DC-10 Series
- [STC SA4010WE](https://openairdocs.org/stc/SA4010WE): Installation of video projection system. Burrana Inc
- [STC SA4070WE](https://openairdocs.org/stc/SA4070WE): A video projection system is installed. Burrana Inc
- [STC SA451NE](https://openairdocs.org/stc/SA451NE): Installation of Inflight Services video projection system DC-10 Bangladesh P/N 105-D-1228. Burrana Inc
- [STC SA930EA](https://openairdocs.org/stc/SA930EA): Installation of Inflight Motion Pictures, Inc., Projection Unit Assembly DC-10 16mm Tri-Jet System, P/N 10300 or Light Weight Tri-Jet Projection System, DC-10, P/N 10307. Burrana Inc
- [STC SA947EA](https://openairdocs.org/stc/SA947EA): Installation of Inflight Motion Pictures, Inc. screen assemblies. Burrana Inc
- [STC SA990EA](https://openairdocs.org/stc/SA990EA): Installation of Inflight Motion Pictures 16mm projection unit assembly and center stowage bins, P/N 10310 and/or P/N 10311. Burrana Inc

All 382: https://openairdocs.org/aircraft/N612AX/stcs.md

## Related

- Other Mcdonnell-Douglas DC-10-30 aircraft: https://openairdocs.org/model/mcdonnell-douglas-dc-10-30/aircraft.md

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