# N556FE: 1972 Mcdonnell Douglas MD-10-10F, registration cancelled 2024-04-13

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: April 13, 2024
- Status when cancelled: Sale reported, canceled
- Airframe: [Mcdonnell Douglas MD-10-10F](https://openairdocs.org/model/mcdonnell-douglas-md-10-10f) (registry code 3022112)
- Engine: [GE CF6-6D](https://openairdocs.org/engine/ge-cf6-6d) (registry code 30076)
- Data sheets: [TCDS A22WE](https://openairdocs.org/tcds/A22WE), [TCDS E23EA](https://openairdocs.org/tcds/E23EA) (OpenAirDocs)
- Serial number: 46710
- Year built: 1972
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: January 11, 2006
- Last registry action: July 10, 2023
- Mode S code: A71637
- Location: [Victorville, CA](https://openairdocs.org/faa-place/CA/Victorville)
- Owner type: Individual
- Owner's area on the map: 34.5670° N, 117.3629° W: Placed by OpenAirDocs at the center of ZIP code 92394, within about 3 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N556FE
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=556FE
- Page: https://openairdocs.org/deregistered/N556FE-2024-04-13

From the FAA registry file of November 4, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe.

ADs and bulletins for the Mcdonnell Douglas MD-10-10F: https://openairdocs.org/model/mcdonnell-douglas-md-10-10f.md

## Service difficulty reports (213, newest 50)

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

- [SDR FDEA201210263757](https://openairdocs.org/sdr/FDEA201210263757), Oct 26, 2012: BATTERY. INOPERATIVE. ESCAPE SLIDE LOW PRESSURE INDICATOR PRESS TO TEST LIGHT WILL NOT TEST. R & R BATTERIES, REF AMM 25-61-01-2. OPS CHECKED GOOD.
- [SDR FDEA201210113597](https://openairdocs.org/sdr/FDEA201210113597), Oct 11, 2012: COALESCER BAG. CONTAMINATED. OIL FUMES APPEAR TO BE COMING FROM NR 3 PACK. PACK SHUTOFF, BLEED ON. OIL QUANITY STABLE IAW AMM 49-00-00-2 INSPECTED APU BLEED AIR OUTLET AND LOAD BLEED VALVE 
- [SDR FDEA201208213093](https://openairdocs.org/sdr/FDEA201208213093), Aug 21, 2012: SKIN. CRACKED. FUSELAGE SKIN CRACKED AT FWD LT SIDE OF NOSE GEAR W/W CUTOUT. COMPLIED WITH EA 8-5350-157364 & REPAIRED AREA USING SRM 53-50-00.
- [SDR FDEA201208213092](https://openairdocs.org/sdr/FDEA201208213092), Aug 21, 2012: SKIN. CRACKED. FUSELAGE SKIN CRACKED AT FWD RT SIDE OF NOSE GEAR W/W CUTOUT REPAIRED USING SRM 53-50-00 AS A REFERENCE.
- [SDR FDEA201108113201](https://openairdocs.org/sdr/FDEA201108113201), Aug 11, 2011: ENGINE. STALLED. ON CLIMBOUT, PASSING FL 290 FELT 2 FIRM JOLTS WITH YAW TO THE LT ENG INDICATIONS NORMAL IN COCKPIT. FELT LIKE COMPRESSOR STALL ON NR 1 ENG. ENG RPM'S AT THE TIM
- [SDR FDEA201105191877](https://openairdocs.org/sdr/FDEA201105191877), May 19, 2011: CONNECTOR. UNSECURE. R1 DOOR SLIDE LIGHT DOES NOT TEST. RESEATED CONNECTOR ON BACK OF PRESS TO TEST SWITCH R1 DOOR. OPS CHECKED NORMAL. OK FOR SERVICE.
- [SDR FDEA201103311265](https://openairdocs.org/sdr/FDEA201103311265), Mar 31, 2011: OIL SYSTEM. LEAKING. DURING CRUISE, NR 2 ENG OIL QTY STARTED DROPPING 1 GAL EVERY 8 MIN. WHEN QUANTITY HIT 3 AND AMBER, WE ALSO GOT AN ENG 2 OIL PRESSURE LOW ALERT AND IT STAYED ON 
- [SDR FDEA201103191081](https://openairdocs.org/sdr/FDEA201103191081), Mar 19, 2011: SHUNT. LOOSE. EMERG PWR TEST FAIL ON PREFLIGHT EPCU FAULTS "BATTERY/INTFC" REF FIM 24-30-19. TERMINAL ON SHUNT S4-1 LOOSE AND ARCING. S4-1 REPLACED SHUNT S4-1, REF WDM 24-08-
- [SDR FDEA201102040475](https://openairdocs.org/sdr/FDEA201102040475), Feb 4, 2011: FRAME. CRACKED. CAC, FWD PRESSURE BULKHEAD RT SIDE MAIN FRAME CRACKED ALLTHE WAY THROUGH AT BS 1157 BETWEEN LONGERON 27R AND 28R. REMOVED DAMAGED PARTS, FABRICATED NEW PARTS AN
- [SDR FDEA201012294761](https://openairdocs.org/sdr/FDEA201012294761), Dec 29, 2010: CONTROL UNIT. FAILED. DURING CRUISE FL360 F/O'S MCDU BLANKED OUT FOR APPROX 1 MINUTE THEN CAME BACK ON. THEN WE SMELLED ELECTRICAL FIRE/FUMES. PULLED F/O, MULTI-FUNCTION DISPLAY UNIT
- [SDR FDEA201011274501](https://openairdocs.org/sdr/FDEA201011274501), Nov 27, 2010: WIRE HARNESS. MALFUNCTIONED. EMERGENCY EXIT SIGNS INOP. RELEASED FOR SERVICE IAW MEL: 33-50-02, WHEN SHAKING HARNESS BY L1 DOOR LIGHTS COME ON, BUT UNABLE TO FIND EXACT CAUSE AT THIS TIME. 
- [SDR FDEA200812025047](https://openairdocs.org/sdr/FDEA200812025047), Dec 2, 2008: WARNING SYSTEM. ACTIVATED. LANDING MEM, 18R 3 UNSAFE (RED) GEAR LIGHTS WITH GEAR HANDLE DOWN, 3 UNSAFE ON CONFIG PAGE, QRH PROCEDURE DEPLOY ALT GEAR EXTENSION AND RECEIVED 3 GREEN SAFE (C
- [SDR 08FDEA04266](https://openairdocs.org/sdr/08FDEA04266), Oct 8, 2008: PRESSURE PANEL. CRACKED. CENTER LANDING GEAR SPACE LT WALL UPPER AFT CORNER HAS A CRACK ALONG UPPER EDGE ACROSS THREE RIVETS ENDING AT STIFFENER, FWD OF PNEUMATIC DUCT. (VERIFIED CRACK 
- [SDR 08FDEA04270](https://openairdocs.org/sdr/08FDEA04270), Oct 8, 2008: WEB. CRACKED. CENTER LANDING GEAR SPACE LT WALL UPPER AFT CORNER HAS CRACK COMING FROM HOLE FOR THERMOCOUPLE. THIS CRACK HAS BEEN STOP DRILLED TWICE AND IS CRACKED PAST SECON
- [SDR 07FDEA02558](https://openairdocs.org/sdr/07FDEA02558), Jul 20, 2007: BULKHEAD. CORRODED. CLG WHEEL WELL CAVITY, CORROSION ON BULKHEAD LOWER CIRCUMFERENCIAL ANGLE AT STA 1521 LONGERON 50R TO 49R. REMOVED CORROSION ON T-CHORD IAW MD/DC10 SRM 51-21-01 
- [SDR 07FDEA02526](https://openairdocs.org/sdr/07FDEA02526), Jul 19, 2007: SHEAR TIE. CORRODED. CLG WHEEL WELL CAVITY, CORROSION ON SHEAR TIE/LONGERON AT STA 15012 LONGERON 50L. REMOVED, FABRICATED AND INSTALLED NEW SHEAR-TIE/ FRAME IAW MD/DC10 SRM51-33-01
- [SDR 07FDEA02525](https://openairdocs.org/sdr/07FDEA02525), Jul 19, 2007: FRAME. CORRODED. CLG WHEEL WELL CAVITY CORROSION ON CIRCUMFERENTIAL ANGLE AT FWD OF STA 15121, BETWEEN LONGERON 51L AND 52. REMOVED, REPLACED AND INSTALLED 2 EACH ANGLES AT 51L 
- [SDR 07FDEA02524](https://openairdocs.org/sdr/07FDEA02524), Jul 19, 2007: FRAME. CORRODED. CLG WHEEL WELL CAVITY, CORROSION ON BULKHEAD LOWER CIRCUMFERENTIAL ANGLE AT STA 152 LONGERON 50R TO 49R. REMOVED, FABRICATED AND INSTALLED 4 EACH ANGLES 49R TO 
- [SDR 07FDEA02523](https://openairdocs.org/sdr/07FDEA02523), Jul 19, 2007: SKIN. DENTED. AFT SKIN DENTED AT APPROXIMATELY THE 5:00 POSITION ON FRAME AND IS 18 INCHES OF RVSM (CENTER PLATE). THIS SDR REPLACES (SDR#07-2123) REPAIRED SKIN IAW EA 8-5533
- [SDR 07FDEA02522](https://openairdocs.org/sdr/07FDEA02522), Jul 19, 2007: SEAT TRACK. CORRODED. CORRODED SEAT TRACK AT LBL 54 AFT BULK PIT AT STA 1801 TO1840. REMOVED, FABRICATED AND INSTALLED SEAT TRACK IAW MD/DC10 SRM 51-31-01 VOLII AND 51-21-01 VOLII AN
- [SDR 07FDEA02516](https://openairdocs.org/sdr/07FDEA02516), Jul 18, 2007: SKIN. CORRODED. CLG WHEEL WELL CAVITY, CORROSION ON SKIN INTERIOR BETWEEN LONGERON 50R AND 49R, STA 1501 TO 1520. REMOVED AND REPLACED L51R END FITTINGS IAW MD/DC10 SRM 51-35-0
- [SDR 07FDEA02514](https://openairdocs.org/sdr/07FDEA02514), Jul 18, 2007: LONGERON. CORRODED. CLG WHEEL WELL CAVITY, CORROSION ON LONGERON END FITTING AT STA 1501 TO 1521, LONGERON 51L. REMOVED, FABRICATED AND INSTALLED NEW END FITTINGS IAW MD/DC10 SRM51
- [SDR 07FDEA02494](https://openairdocs.org/sdr/07FDEA02494), Jul 16, 2007: LONGERON. CORRODED. FOUND CORROSION ON LONG END FITTINGS AT STA 1521 LONG 48L CLG WHEEL WELL. REMOVED AND REPLACED L48L END FITTINGS IAW DC/MD-10 SRM 51-33-01 VOL. II.
- [SDR 07FDEA02493](https://openairdocs.org/sdr/07FDEA02493), Jul 16, 2007: LONGERON. CORRODED. CLG WHEEL WELL CAVITY CORROSION ON LONGERON END FITTING STA 1501 TO STA 1521 LONGERON 51L TO 52L REMOVED AND REPLACED LONGERON END FITTING L52R IAW DC/MD-10 SRM
- [SDR 07FDEA02492](https://openairdocs.org/sdr/07FDEA02492), Jul 16, 2007: INTERCOSTAL. CORRODED. CLG WHEEL WELL CAVITY CORROSION ON INTERCOSTAL ABOVE LONGERON 52 R STA 1381 TO 1401. REMOVED AND REPLACED INTERCOSTAL IAW DC/MD-10 SRM 51-33-01 VOL II.
- [SDR 07FDEA02491](https://openairdocs.org/sdr/07FDEA02491), Jul 16, 2007: SKIN. CORRODED. CLG WHEEL WELL CAVITY, CORROSION ON FUSELAGE SKIN INTERIOR BETWEEN LONGERON 50R AND 49R, STA 1501 TO 1520. REMOVED AND REPLACED L51R END FITTINGS IAW DC-10/MD-1
- [SDR 07FDEA02490](https://openairdocs.org/sdr/07FDEA02490), Jul 16, 2007: LONGERON. CORRODED. CORROSION ON LONGERON END FITTING AT STA 1521, L48R CLG WHEEL/WELL. REMOVED AND REPLACED LONGERON END FITTINGS L48R IAW DC-10/MD-10 SRM 51-35-01 VOL. II.
- [SDR 07FDEA02489](https://openairdocs.org/sdr/07FDEA02489), Jul 16, 2007: SKIN. CORRODED. UPON REMOVAL OF LOWER SKIN ON LT AILERON FOUND TOP SKIN TO BE CORRODED UNDER FINGER DOUBLERS AND T/E WEDGE. REMOVED AND REPLACED SKIN IAW DC-10/MD-10 SRM 51-35-
- [SDR 07FDEA02488](https://openairdocs.org/sdr/07FDEA02488), Jul 16, 2007: SKIN. CORRODED. UPON REMOVAL OF LOWER SKIN ON LT AILERON FOUND TOP SKIN TO BE CORRODED UNDER FINGER DOUBLERS AND T/E WEDGE. REMOVED AND REPLACED SKIN IAW DC-10/MD-10 SRM 51-35-
- [SDR 07FDEA02481](https://openairdocs.org/sdr/07FDEA02481), Jul 13, 2007: LONGERON. CORRODED. LONGERON 51L IN CLG AREA BETWEEN STA 1501 AND 1521 CORRODED. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS IAW MD10-10 SRM 53-00-01 VOL 1 FIG 1A. REMOVED AND REP
- [SDR 07FDEA02484](https://openairdocs.org/sdr/07FDEA02484), Jul 13, 2007: LONGERON. CORRODED. CLG WHEEL WELL CAVITY, CORROSION ON LONGERON END FITTING AT STA 1501 TO 1521, LONGERON 49L REMOVED CORROSION ON LONGERON END FITTING AND FOUND TO BE WITHIN LIMI
- [SDR 07FDEA02483](https://openairdocs.org/sdr/07FDEA02483), Jul 13, 2007: LONGERON. CORRODED. LONGERON 51L IN CLG AREA BETWEEN STA 1501 AND 1521 CORRODED. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS IAW MD10-10 SRM 53-00-01 VOL 1 FIG 1A. REMOVED AND REP
- [SDR 07FDEA02418](https://openairdocs.org/sdr/07FDEA02418), Jul 10, 2007: SEAT TRACK. GOUGED. MAIN CABIN SEAT TRACK AT RBL - 8 AT STA 1199 IS GOUGED. BLENDED SEAT TRACK AND OUT OF LIMITS. FABRICATED SEAT TRACK AND SPLICE REPAIR IAW DC/MD 10 SRM 53- 70-00
- [SDR 07FDEA02417](https://openairdocs.org/sdr/07FDEA02417), Jul 10, 2007: SEAT TRACK. GOUGED. MAIN CABIN SEAT TRACK AT LBL - 8 BETWEEN STA 1681 AND 1701 IS GOUGED BLENDED SEAT TRACK AND OUT OF LIMITS. REMOVED AND INSTALLED NEW SEAT TRACK IAW DC/MD 10 SRM
- [SDR 07FDEA02416](https://openairdocs.org/sdr/07FDEA02416), Jul 10, 2007: SEAT TRACK. GOUGED. MAIN CABIN SEAT TRACK AT RBL-27, AT STA 1059 IS GOUGED. BLENDED SEAT TRACK AND OUT OF LIMITS. REMOVED AND INSTALLED NEW SEAT TRACK IAW DC/MD 10 SRM 53- 70-00 VO
- [SDR 07FDEA02288](https://openairdocs.org/sdr/07FDEA02288), Jun 26, 2007: SKIN. DENTED. DENT IN FUSELAGE SKIN FWD OF R-1 DOOR SILL. REMOVED DENT, FABRICATED AND INSTALLED SKIN AND FILLER IAW DC/MD10 SRM 53-20-00 VOL I FIG 6 SHT 4, 53-10-00 VOL II P
- [SDR 07FDEA02287](https://openairdocs.org/sdr/07FDEA02287), Jun 26, 2007: SKIN. CORRODED. CLG WHEEL WELL CAVITY CORROSION ON FUSELAGE CIRCUMFERENTIAL ANGLE AT STA.1521, BETWEEN LONGERON 52 AND 51R. [07-13-07] REMOVED INTERCOSTAL AT LONG 51R, FS 1501-
- [SDR 07FDEA02286](https://openairdocs.org/sdr/07FDEA02286), Jun 26, 2007: BULKHEAD. CORRODED. CLG WHEEL WELL CAVITY CORROSION ON CIRCUMFERENTIAL ANGLE AT FWD OF STA 1521, BETWEEN LONGERON 51L AND 52. [07-17-07] REMOVED,FABRICATED AND INSTALLED IAW SRM 51
- [SDR 07FDEA02285](https://openairdocs.org/sdr/07FDEA02285), Jun 26, 2007: BULKHEAD. CORRODED. CLG - WHEEL WELL CAVITY,CORROSION ON BULKHEAD LOWER CIRCUMFERENCIAL ANGLE AT STA 152, LONGERON 50R TO 49R. [07-17-07] REMOVED,FABRICATED AND INSTALLED 4 EACH EN
- [SDR 07FDEA02282](https://openairdocs.org/sdr/07FDEA02282), Jun 26, 2007: SKIN. CORRODED. CLG WHEEL WELL CAVITY, CORROSION ON LONGERON END FITTING AT STA 1501 TO 1521, LONGERON 49L. [07-13-07] REMOVED LONGERON 49L END FITTING IAW DC/MD10-10 SRM 51-33
- [SDR 07FDEA02262](https://openairdocs.org/sdr/07FDEA02262), Jun 22, 2007: SKIN. CORRODED. CLG WHEEL WELL CAVITY, CORROSION ON FUSELAGE SKIN INTERIOR SURFACE AT STA 1441, LONGERON 51R TO 51L. SKIN SECTION FROM 1401 TO 1541 IS BEING REPLACED ON N/R N00
- [SDR 07FDEA02263](https://openairdocs.org/sdr/07FDEA02263), Jun 22, 2007: SKIN. CORRODED. CLG WHEEL WELL CAVITY CORROSION ON FUSELAGE SKIN BETWEEN LONGERON 51L AND 52 STA 1350 TO 1370. CLEANED AREA IAW DC/MD10 SRM51-21-01 PARA.22 VOL. II. NO CORROSIO
- [SDR 07FDEA02250](https://openairdocs.org/sdr/07FDEA02250), Jun 21, 2007: LONGERON. CORRODED. CORROSION ON LONGERON 52 STA 1461 TO 1501,CLG WHEEL WELL CAVITY. [07-13-07] FOUND TO BE OUT OF LIMITS IAW MD10-10 SRM 51-33-01 VOL 2. FABRICATED NEW LONG SECTIO
- [SDR 07FDEA02249](https://openairdocs.org/sdr/07FDEA02249), Jun 21, 2007: LONGERON. CORRODED. CLG WHEEL WELL CAVITY, CORROSION ON LONGERON 51R STA 1441 TO 1501. [07-13-07] FOUND TO BE WITHIN LIMITS IAW MD10-10 SRM 53-00- 01 VOL 1 , ORIGINAL THICKNESS 0.1
- [SDR 07FDEA02247](https://openairdocs.org/sdr/07FDEA02247), Jun 21, 2007: ANGLE. DENTED. UPON REMOVAL OF LOWER TORQUE BOX WEB FOR SKIN REPLACEMENT ON N/R N00337, FOUND INNER CHORD ANGLE ADA0055-7 DENTED AT STA 886 JUST ABOVE L41 RIGHT. [07-17-07] RE
- [SDR 07FDEA02147](https://openairdocs.org/sdr/07FDEA02147), Jun 15, 2007: SKIN. CORRODED. CORROSION ON FUSELAGE SKIN INTERIOR AT STA 1441 TO 1481, LONGERON 50L TO 50R, CENTER LANDING GEAR WHEEL WELL CAVITY. [07-13-07] REMOVED AND REPLACED SKIN WITH N
- [SDR 07FDEA02146](https://openairdocs.org/sdr/07FDEA02146), Jun 15, 2007: SKIN. CORRODED. CENTER LANDING GEAR WHEEL WELL,CORROSION ON FUSELAGE SKIN AT STA 1501 TO 1521, LONGERON 51R TO 50R. [07-17-07] REPLACED ON N00616 WITH EA 8-5330-112939.
- [SDR 07FDEA02123](https://openairdocs.org/sdr/07FDEA02123), Jun 13, 2007: SKIN. DENTED. AFT SKIN DENTED AT APPROXIMATELY 5:00 POSITION ON FRAME AND IS WITHIN 18 INCHES OF RVSM (CENTER) PLATE. [07-17-07] REPAIRED SKIN IAW EA 8-5330-112937 MAJOR REPA
- [SDR 07FDEA02122](https://openairdocs.org/sdr/07FDEA02122), Jun 13, 2007: SKIN. CORRODED. LT O/B AILERON BULGING AT FASTENERS ON SKIN. [07-17-07] REMOVED DAMAGED SKIN AND INSTALLED NEW SKIN IAW SRM 51-35-01 VOL II . MAJOR REPAIR.
- [SDR 07FDEA02121](https://openairdocs.org/sdr/07FDEA02121), Jun 13, 2007: SEAT TRACK. CORRODED. CORRODED SEAT TRACK AT LBL 54 AFT BULK PIT AT STA 1801 TO 1840. [07-17-07] REMOVED, FABRICATED AND INSTALLED SEAT TRACK IAW SRM 51-31-01 VOL II, 51-21-01 VOL II

All 213: https://openairdocs.org/deregistered/N556FE-2024-04-13/reports.md

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