# N808MC: 1975 Boeing 747 212B, registration cancelled 2013-02-01 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: February 1, 2013 - Status when cancelled: Sale reported, canceled - Airframe: [Boeing 747 212B](https://openairdocs.org/model/boeing-747-212b) (registry code 1384823) - Engine: [GE CF6-50 series](https://openairdocs.org/engine/ge-cf6-50-series) (registry code 30018) - Data sheets: [TCDS E23EA](https://openairdocs.org/tcds/E23EA) (OpenAirDocs) - Serial number: 21048 - Year built: 1975 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, normal - Airworthiness date: June 23, 2004 - Last registry action: December 13, 2005 - Mode S code: AB00AB - Location: [Herndon, VA](https://openairdocs.org/faa-place/VA/Herndon) - Owner type: Individual - Owner's area on the map: 38.9798° N, 77.3798° W: Placed by OpenAirDocs at the center of ZIP code 20170, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N808MC - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=808MC - Page: https://openairdocs.org/deregistered/N808MC-2013-02-01 From the FAA registry file of October 29, 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 Boeing 747 212B: https://openairdocs.org/model/boeing-747-212b.md ## Service difficulty reports (43) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR UIEA200500004](https://openairdocs.org/sdr/UIEA200500004), Jan 26, 2005: SLIDE. FAILED. UPPER DECK EMERGENCY ESCAPE SLIDE DID NOT PROPERLY DEPLOY WHEN ACTIVATED. (EA15200503933) - [SDR UIEA200400179](https://openairdocs.org/sdr/UIEA200400179), Oct 1, 2004: INU. FAILED. ON CLIMB OUT, NR 1 INS WARNING LIGHT CAME ON. ON CLIMB OUT NR 1 INS WARNING LIGHT CAME ON. NR 1 ADI AND HEADING FAILED. SELECTED NR 3 ATTITUDE AND COMPASS. APPR - [SDR UIEA200400120](https://openairdocs.org/sdr/UIEA200400120), Jul 7, 2004: CONTROLLER. FAILED. GT 8237/03 RMS/DOV AUTO FAIL LIGHT CAME ON DURING FLIGHT: AUTO FAIL LIGHT CAME ON DURING CLIMB ABOUT 8000 FT A/C ALTITUDE OUTFLOW VALVES .2500 CLOSED USED MANUA - [SDR UIEA200400101](https://openairdocs.org/sdr/UIEA200400101), Jun 4, 2004: BEARING. MIGRATED. D-CHECK, DURING MAINTENANCE INSPECTION, ELONGATION DAMAGE WAS FOUND AT OB TRAILING EDGE FLAP TRACK NR 8 MOVABLE FAIRING ASSEMBLY HINGE FITTING LUGS. OVERSIZED T - [SDR UIEA200400103](https://openairdocs.org/sdr/UIEA200400103), Jun 4, 2004: BULKHEAD. CRACKED. D-CHECK, DURING MAINTENANCE INSPECTION. NR 4 PYLON LT SIDE, BULKHEAD STRAPS WERE FOUND CRACKED AT NAC STA 286.0 AND WL 146.5. THE AFT END OF THE STRAP CRACK WAS - [SDR UIEA200400102](https://openairdocs.org/sdr/UIEA200400102), Jun 4, 2004: BULKHEAD. CRACKED. D-CHECK, DURING MAINTENANCE INSPECTION. NR 1 PYLON LT SIDE, BULKHEAD STRAPS WERE FOUND CRACKED AT NAC STA 286.0 AND W.L. 146.5, ALSO THE STRUT SKIN ASSEMBLY AT - [SDR UIEA200400104](https://openairdocs.org/sdr/UIEA200400104), Jun 2, 2004: FRAME. DAMAGED. D CHECK, DURING MAINT INSP FOUND COCKPIT EMERGENCY EXIT DOOR CUTOUT FRAME AND CHORDS DAMAGED BETWEEN STA 360 AND 380 WITH MISDRILLED HOLES BETWEEN STRINGER 2L A - [SDR UIEA200400105](https://openairdocs.org/sdr/UIEA200400105), Jun 2, 2004: SKIN. CRACKED. D-CHECK, DAMAGE WAS FOUND ON RT SIDE OF NR 1 PYLON STRUCTURE ASSY. CRACK DAMAGE WAS AT PRECOOLER EXHAUST CUTOUT LOWER AFT CORNER AT NAC STA 248. INNER SKIN DOUB - [SDR UIEA200400107](https://openairdocs.org/sdr/UIEA200400107), Jun 2, 2004: SKIN. CRACKED. (D) CHECK, DURING MAINT INSP DAMAGE WAS FOUND ON RT SIDE OF NR 2 PYLON STRUCTURE ASSY. CRACK DAMAGE WAS AT PRECOOLER EXHAUST CUTOUT LOWER AFT CORNER AT NAC STA - [SDR UIEA200400109](https://openairdocs.org/sdr/UIEA200400109), Jun 2, 2004: SKIN. CRACKED. D-CHECK, DURING MAINT INSP, DAMAGE WAS FOUND ON RT SIDE OF NR 4 PYLON STRUCTURE ASSY. CRACK DAMAGE WAS AT PRECOOLER EXHAUST CUTOUT LOWER AFT CORNER AT NAC STA 2 - [SDR UIEA200400108](https://openairdocs.org/sdr/UIEA200400108), Jun 2, 2004: PRECOOLER. CRACKED. (D) CHECK, DURING MAINT INSP, DAMAGE WAS FOUND ON RT SIDE OF NR 3 PYLON STRUCTURE ASSY. CRACK DAMAGE WAS AT PRE-COOLER EXHAUST CUTOUT LOWER AFT CORNER AT NAC ST - [SDR UIEA200400097](https://openairdocs.org/sdr/UIEA200400097), May 25, 2004: SKIN. WRINKLED. D CHECK AT SIN. DURING MAINTENANCE INSPECTION, FOUND NR 2 PYLON RT SIDE SKIN WRINKLED. DAMAGE WAS FOUND IN FOUR BAYS OF THE RT SUBJECT SKIN ASSEMBLY AFT OF NAC - [SDR UIEA200400096](https://openairdocs.org/sdr/UIEA200400096), May 25, 2004: FITTING. CRACKED. D-CHECK. REWORK OF STRUT NR 1 DIAGONAL BRACE LOWER SPAR FITTING, SP 747-54A2196 REV 1. DURING ACCOMPLISHMENT OF THE TERMINATING ACTION, DAMAGE WAS FOUND AT THE - [SDR UIEA200400046](https://openairdocs.org/sdr/UIEA200400046), Apr 8, 2004: SLIDE. MALFUNCTIONED. UPPER RT EMERGENCY DOOR SLIDE PARTIAL DEPLOYMENT; DURING UPPER RT EMERGENCY DOOR SLIDE RAFT ASSEMBLY DEPLOYMENT TEST, SLIDE/RAFT FAILED TO FULLY INFLATE. SEQUEN - [SDR UIEA200300053](https://openairdocs.org/sdr/UIEA200300053), Aug 28, 2003: RELIEF VALVE. FAILED. LIM-MIA - DURING CLIMB AT FL250, NR 4 NACELLE TEMP WENT OT 8.0 WITH A FIRE BELL AND LIGHT IN NR 4 FIRE SWITCH. WHEN NR 4 THRUST LEVER WAS RETARDED TO IDLE, THE - [SDR UIEA200300045](https://openairdocs.org/sdr/UIEA200300045), Aug 19, 2003: RELIEF VALVE. DEFECTIVE. MIP/POS-AIR TURNBACK, AFTER T/O AND DURING CLIMB, NR 4 ENGINE FIRE WARNING CAME ON. WHEN NR 4 THROTTLE WAS CLOSED THE TEMP WENT BACK TO NORMAL. THROTTLE WAS ADV - [SDR UIEA200300027](https://openairdocs.org/sdr/UIEA200300027), Jun 27, 2003: WARNING LIGHT. FALSE INDICATION. TURN BACK, AFTER TAKEOFF THE LOWER CARGO FIRE PROTECTION AFT LIGHT CAME ON AND WENT OUT 2-4 SECONDS AFTER SILENCING THE BELL. ACCOMPLISHED CHECKLIST AND DUMPED - [SDR UIEA200300017](https://openairdocs.org/sdr/UIEA200300017), Apr 11, 2003: WARNING LIGHT. ILLUMINATED. INFLIGHT ENGINE SHUTDOWN, DURING CRUISE, NR 4 ENGINE SHUTDOWN IN FIGHT DUE TO 'OIL FILTER BYPASS LIGHT. OIL TEMPEARTURE AND PRESSURE NORMAL AT 49 PSI/120 DEGREE - [SDR UIEA200200059](https://openairdocs.org/sdr/UIEA200200059), Oct 25, 2002: SKIN. CORRODED. DURING CURRENT "C" CHECK, FOUND CORROSION BETWEEN OUTER SKIN, DOUBLER AND TRIPLER AT BS 1960 STR 42 RT, LOCATED AT THE AFT LOWER CORNER CUTOUT OF THE AFT LOWER - [SDR UIEA200200060](https://openairdocs.org/sdr/UIEA200200060), Oct 25, 2002: PANEL. CRACKED. DURING CURRENT C-CHECK, AT HKG FOUND REVEAL PANEL CRACKED AT NR 2 MED STATION 800 BETWEEN STRINGER 17L AND 18L. CRACK LENGTH IS APPROX .5 INCH LONG TERMINATING - [SDR 2002F00031](https://openairdocs.org/sdr/2002F00031), Dec 5, 2001: SMOKE DETECTOR. MALFUNCTIONED. DURING CLIMB-OUT FROM MIA AT APPROXIMATELY 21,000 FEET, THE CARGO LOWER AFT FIRE LIGHT ILLUMINATED. CHECKLIST SECTION III WAS COMPLETED. THE CARGO FLOOR FELT WA - [SDR UIEA01104](https://openairdocs.org/sdr/UIEA01104), Oct 30, 2001: FIRE WARNING. FALSE INDICATION. DURING TAKEOFF ROLL FROM SUU AT ABOUT 80 KTS, HAD A CARGO FIRE WARNING LIGHT. REJECTED TAKEOFF PERFORMED. PERFORMED VISUAL INSPECTION OF FORWARD AND AFT CARGO C - [SDR UIEA01099](https://openairdocs.org/sdr/UIEA01099), Sep 30, 2001: LIGHT. FAULTY. AIRCRAFT ATB DUE TO LOWER AFT CARGO AND BULK CARGO COMPARTMENT FIRE WARNING INDICATION. PERFORMED TROUBLE SHOOTING PER MM 26-16-00 AND FOUND NR 4, NR 5 AND NR 6 - [SDR UIEA00045](https://openairdocs.org/sdr/UIEA00045), Oct 6, 2000: DUCT. LEAKING. MIA/BOG -ATB - FLT GT063/06 - ENGINE A-LOOP FIRE WARNING FLUCTUATED, B-LOOP READ 4-5 STEADY. ENGINE SHUT DOWN AND FLIGHT RETURNED TO MIA. MIA MAINTENANCE FOUND - [SDR UIEA01026](https://openairdocs.org/sdr/UIEA01026), Mar 19, 2000: FLOORBEAM. DAMAGED. AFTER REMOVAL OF SEAT TRACK, FOUND FLOORBEAM 1840-1860 UPPER CHORD FASTENER HOLES AT LBL 98.5 ELONGATED. REAMED HOLES, PERFORMED E/C CHECK. NO CRACKS FOUND. FAB - [SDR UIEA01027](https://openairdocs.org/sdr/UIEA01027), Mar 19, 2000: BULKHEAD. CORRODED. DURING INSPECTION, FOUND THE LOWER END OF THE CANTED BULKHEAD PRESSURE WEB AT STATION 1241 CORRODED FROM LBL 11.33 TO 65. REMOVED CORROSION IN AREA PER SRM 51-1 - [SDR 20010423SG001](https://openairdocs.org/sdr/20010423SG001), Mar 19, 2000: FLOORBEAM. DAMAGED. AFTER REMOVAL OF SEAT TRACK, FOUND FLOORBEAM 1840-1860 UPPER CHORD FASTENER HOLES AT LBL 98.5 ELONGATED. REAMED HOLES, PERFORMED E/C CHECK. NO CRACKS FOUND. FAB - [SDR UIEA01025](https://openairdocs.org/sdr/UIEA01025), Mar 9, 2000: SKIN. CORRODED. DURING ROUTINE INSPECTION, FOUND UPPER SURFACE OF LOWER LEFT WING SKIN CORRODED AFT REAR SPAR WS 235. REMOVED FASTENERS FROM THE TRAILING EDGE ATTACH FITTING. A - [SDR UIEA01024](https://openairdocs.org/sdr/UIEA01024), Mar 9, 2000: SKIN. WORN. DURING ROUTINE INSPECTION, FOUND NR 3 PYLON SKIN WORN AT NAC STATION 290 WL 145 R/S ACCESS PANEL. TRIMMED OUT WORN AREA. FABRICATED FILLER FROM CRES STEEL 301.5 - [SDR UIEA01023](https://openairdocs.org/sdr/UIEA01023), Mar 9, 2000: FLAP TRACK. CORRODED. DURING ROUTINE INSPECTION, FOUND NR 6 INBOARD FLAP TRACK REAR SPAR FORWARD AFT ATTACH HOLES CORRODED. CORROSION REMOVED BY MILLING FLANGE THICKNESS TO .8799 AT - [SDR UIEA01022](https://openairdocs.org/sdr/UIEA01022), Mar 9, 2000: FRAME. DENTED. DURING ROUTINE INSPECTION, FOUND FRAME DENTED AT STATION 1860 STRINGER 12 AND 13R. TRIMMED AWAY DAMAGE. FABRICATED REPAIR DOUBLER, FILLERS AND SHEAR TIE. INSTAL - [SDR UIEA01021](https://openairdocs.org/sdr/UIEA01021), Mar 9, 2000: FRAME. DENTED. DURING ROUTINE INSPECTION, FOUND FRAME DENTED AT STATION 1840 STRINGER 12 AND 13R. TRIMMED AWAY DAMAGE. FABRICATED REPAIR DOUBLERS, FILLERS AND SHEAR TIE. INSTA - [SDR UIEA01020](https://openairdocs.org/sdr/UIEA01020), Mar 9, 2000: FRAME. DENTED. DURING ROUTINE INSPECTION, FOUND FRAME DENTED AT STATION 1820 STRINGER 12R. TRIMMED AWAY DAMAGE. FABRICATED REPAIR DOUBLERS, FILLERS AND SHEAR TIE. INSTALLED PE - [SDR UIEA01019](https://openairdocs.org/sdr/UIEA01019), Mar 9, 2000: FRAME. DENTED. DURING ROUTINE INSPECTION, FOUND FRAME DENTED AT STATION 1760 STRINGER 13R. TRIMMED AWAY DAMAGE. FABRICATED REPAIR DOUBLERS, FILLERS AND SHEAR TIE. INSTALLED PE - [SDR UIEA01018](https://openairdocs.org/sdr/UIEA01018), Mar 9, 2000: FRAME. DENTED. DURING ROUTINE INSPECTION, FOUND OUTER CHORD DAMAGED/DENTED AT BS 1680 STRINGER 15R. TRIMMED AWAY DAMAGE. MANUFACTURED FILLER, REPAIR DOUBLER AND STRAPS. INSTAL - [SDR UIEA01017](https://openairdocs.org/sdr/UIEA01017), Mar 9, 2000: SEAT TRACK. SCRATCHED. DURING ROUTINE INSPECTION, FOUND SEAT TRACK GOUGED/SCRATCHED AT LBL 75.92 BETWEEN STATION 1320 AND 1460. ALL AREAS BLENDED PER SRM 51-10-01. HFEC INSPECTION PER - [SDR UIEA01016](https://openairdocs.org/sdr/UIEA01016), Mar 9, 2000: SEAT TRACK. SCRATCHED. DURING ROUTINE INSPECTION, FOUND SEAT TRACK GOUGED/SCRATCHED AT LBL 98.58 BETWEEN STATION 1030 AND 1135. ALL AREAS BLENDED PER SRM 51-10-01. HFEC INSPECTION PER - [SDR UIEA01015](https://openairdocs.org/sdr/UIEA01015), Mar 9, 2000: SKIN. CORRODED. DURING ROUTINE INSPECTION, FOUND UPPER WING SKIN CORRODED AT BS 1140, FROM RBL 57 TO RBL 98. REMOVED CORROSION PER SRM 51-10-01, FOUND AREAS FROM RBL 57-87 WITH - [SDR UIEA01014](https://openairdocs.org/sdr/UIEA01014), Mar 9, 2000: FRAME. CRACKED. DURING ROUTINE INSPECTION, FOUND FRAME WEB CRACKED AT STATION 360 R/S STRINGER 23R CUT OUT. ROUTED CRACKED AREA OF WEB. MANUFACTURED REPAIR DOUBLER AND FILLERS. - [SDR UIEA01013](https://openairdocs.org/sdr/UIEA01013), Mar 9, 2000: FRAME. CRACKED. DURING ROUTINE INSPECTION, FOUND FRAME WEB CRACKED AT STATION 360 R/S STRINGER 15 AND 16R. TRIMMED DAMAGE AREA OF WEB. MANUFACTURED REPAIR ANGLES, FILLERS, STRA - [SDR UIEA01012](https://openairdocs.org/sdr/UIEA01012), Mar 9, 2000: SHEAR TIE. CRACKED. DURING ROUTINE INSPECTION, FOUN FRAME SHEAR TIE CRACKED IN RADIUS BETWEEN STATION 340-360 R/S AT MAIN DECK LEVEL (WBL200). TRIMMED DAMAGE AREA. MANUFACTURED REP - [SDR UIEA9909](https://openairdocs.org/sdr/UIEA9909), Feb 25, 1999: SKIN. DAMAGED. FLT GT065 - ATB - APPROX 3.5 HOURS INTO THE FLIGHT, AND ADDITIONAL CARGO CHECK WAS MADE AN A HOLE APPROXIMATELY 1 FT SQUARE WAS DISCOVERED AT THE BOTTOM LEFT CO - [SDR UIEA9706](https://openairdocs.org/sdr/UIEA9706), Jul 4, 1997: PDU. DEFECTIVE. ATB - FLT MIA-BOG - ON FLAP RETRACTION AFTER TAKEOFF, NR 4 LE ON LEFT DID NOT INDICATE UP. USED ALTERNATE SYSTEM, BUT STILL DID NOT INDICATE UP. SCANNED LED'S V ## NTSB investigations (1) From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [NTSB DCA05WA028](https://openairdocs.org/ntsb/DCA05WA028), Jan 24, 2005: Boeing B-747-200 (N808MC), Dusseldorf, Germany, incident, minor damage ## Other aircraft with N808MC - [Registered now](https://openairdocs.org/aircraft/N808MC): Raytheon HAWKER 800XP, S/N 258614, built 2003 --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.