# N809MC: 1974 Boeing 747-228F, registration cancelled 2010-11-08 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: November 8, 2010 - Status when cancelled: Triennial form not returned - Airframe: [Boeing 747-228F](https://openairdocs.org/model/boeing-747-228f) (registry code 1384895) - Engine: [GE CF6-50 series](https://openairdocs.org/engine/ge-cf6-50-series) (registry code 30018) - Data sheets: [TCDS A20WE](https://openairdocs.org/tcds/A20WE), [TCDS E23EA](https://openairdocs.org/tcds/E23EA) (OpenAirDocs) - Serial number: 20887 - Year built: 1974 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, normal - Airworthiness date: June 23, 2004 - Certificate issued: October 31, 2006 - Last registry action: November 17, 2009 - Mode S code: AB0462 - Owner when cancelled: [Atlas Air Inc](https://openairdocs.org/faa-owner/ATLAS%20AIR%20INC) - Location: [Purchase, NY](https://openairdocs.org/faa-place/NY/Purchase) - Owner type: Corporation - Owner's area on the map: 41.0382° N, 73.7107° W: Placed by OpenAirDocs at the center of ZIP code 10577, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N809MC - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=809MC - Page: https://openairdocs.org/deregistered/N809MC-2010-11-08 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 747-228F: https://openairdocs.org/model/boeing-747-228f.md ## Service difficulty reports (70, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR UIEA200900002](https://openairdocs.org/sdr/UIEA200900002), Dec 30, 2008: BLADES. MISSING. DURING DESCENT CREW REPORTED SIGNIFICANT VIBRATION FROM NR 1 ENGINE. INSPECTION FOUND MISSING BLADES IN THE LPT AREA. ENGINE CHANGE IS IN PROGRESS. - [SDR UIEA200900003](https://openairdocs.org/sdr/UIEA200900003), Dec 24, 2008: INU. FAILED. AIR TURN BACK DUE TO NR 1 INS RED WARNING LIGHT ON WITH HDG AND FLIGHT DIRECTOR FLAGS IN VIEW. FOUND NR 1 INU FAILED. REPLACED INU, OPS CHECKED OK. - [SDR UIEA200800328](https://openairdocs.org/sdr/UIEA200800328), Oct 12, 2008: PANEL. CRACKED. NOSE WHEEL WELL LT SIDE AT STA 273.0, WATER LINE 160 HAS A 0.250 INCH CRACK DETECTED WITH HFEC INSPECTION. INTERM REPAIR WAS ACCOMPLISHED IAW SRM 53-10-04, FIG - [SDR UIEA200800329](https://openairdocs.org/sdr/UIEA200800329), Oct 12, 2008: SKIN PANEL. DEBONDED. RT WING UPPER SURFACE L/E PANEL AT ILES 328.5 HAS A PREVIOUS REPAIR AREA 7.0 BY 6.0 INCHES DISBONDING AND CRACKING. PERMANENT REPAIR ACCOMPLISHED IAW SRM 51-40- - [SDR UIEA200800295](https://openairdocs.org/sdr/UIEA200800295), Aug 18, 2008: INU. FAILED. NR 1 INS DIFFERS FROM NR 2 INS BY 35 NM OR 50 KTS. FAILED ACCURACY TEST. DUMPED FUEL AND DIVERTED TO JFK. REPLACED NR 1 INU AND ALIGNED OPS CHECKED OK PER 34-41 - [SDR UIEA200800192](https://openairdocs.org/sdr/UIEA200800192), May 14, 2008: DOOR. DAMAGED. WHILE TROUBLESHOOTING INBOUND LOG ITEM FOR NR 1 HYD SYSTEM OVERHEAT BODY GEAR DOORS BOTH SIDES CAME IN CONTACT WITH THE TIRES WHEN HYD POWER WAS APPLIED. CAUSIN - [SDR UIEA200800185](https://openairdocs.org/sdr/UIEA200800185), May 11, 2008: PUMP. FAILED. CREW REPORTED HYD SYSTEM NR 1 OVERHEAT. ADP AND EDP TURNED OFF. ALL PUMPS ON NR 1 OFF OCCASIONAL OVERHEAT INDICATION CONTINUED. AFTER 1 HOUR NO OVERHEAT INDICAT - [SDR UIEA200800181](https://openairdocs.org/sdr/UIEA200800181), May 9, 2008: SKIN PANEL. DELAMINATED. RT WING UPPER FIXED T/E PANEL HAS LOOSE AND WORKING FASTENERS, PANEL IS DELAMINATED. PANEL LOCATED INBOARD OF INBOARD AILERON, AT WBL STA 445.0, DELAMINATION AF - [SDR UIEA200800180](https://openairdocs.org/sdr/UIEA200800180), May 9, 2008: SKIN PANEL. DELAMINATED. RT WING UPPER FIXED L/E PANEL DELAMINATED, 6.0 FEET OUTBOARD OF NR 3 ENGINE, 12 INCHES FROM AFT EDGE OF PANEL AT ILES STA 772.5. AREA OF DELAMINATION IS 14.0 IN - [SDR UIEA200800179](https://openairdocs.org/sdr/UIEA200800179), May 9, 2008: SKIN PANEL. CRACKED. RT WING UPPER FIXED TRAILING EDGE PANEL HAS COMPOSITE CRACK, 3.5 INCHES FROM FORWARD EDGE OF PANEL AT WBL STA 515. PERMANENT REPAIR ACCOMPLISHED AS PER B747-200 - [SDR UIEA200800178](https://openairdocs.org/sdr/UIEA200800178), May 9, 2008: SKIN PANEL. DELAMINATED. LT WING UPPER FIXED L/E PANEL DELAMINATED, INBOARD OF NR 2 ENGINE, 8.0 INCHES FROM AFT EDGE OF PANEL AT ILES STA 545.56. AREA OF DELAMINATION IS 2.0 BY 2.0 INCH - [SDR UIEA200800177](https://openairdocs.org/sdr/UIEA200800177), May 9, 2008: SKIN PANEL. CRACKED. LT WING UPPER FIXED LEADING EDGE PANEL CRACKED AND DELAMINATED, ILES 833.00, 20 INCHES FROM AFT EDGE OF PANEL. PERMANENT REPAIR ACCOMPLISHED AS PER B747-200 SRM - [SDR UIEA200800006](https://openairdocs.org/sdr/UIEA200800006), Jan 6, 2008: O-RING. LEAKING. APPROX 1 HOUR 15 MIN AFTER T/O NR 1 ENGINE OIL QTY IND ZERO, TEMP AND PRESS NORMAL ABOUT 2 HOURS 30 MIN AFTER T/O PRESSURE BEGAN VERY SLOW DROP WITH SLOW FLUX 5 - [SDR UIEA200700481](https://openairdocs.org/sdr/UIEA200700481), Nov 30, 2007: SKIN. DELAMINATED. RIGHT WING SPOILER NR 7 HAS DELAMINATION. DISBONDED UPPER AND LOWER SURFACE 35" BY 25". REMOVED AND REPLACED THE NR 7 SPOILER IAW AMM 27-62-01 OPS CHECKED TRANS - [SDR UIEA200700451](https://openairdocs.org/sdr/UIEA200700451), Oct 3, 2007: ACCESS PANEL. DELAMINATED. AIR CONDITION ACCESS PANEL 192ER EXTERNAL SURFACE IS DELAMINATED. REPAIRED AS PER SRM 51-40-17 AND BOEING MESSAGE 1-638498164-2. - [SDR UIEA200700446](https://openairdocs.org/sdr/UIEA200700446), Oct 1, 2007: FITTING. CORRODED. BS 230 RBL 1 BILGE AREA BEAM WEB SUPPORT FITTING CORRODED. REPLACED FITTING AS PER SRM 51-10-01 AND BOEING MESSAGE 1-637033946-3. - [SDR UIEA200700444](https://openairdocs.org/sdr/UIEA200700444), Oct 1, 2007: BULKHEAD. CRACKED. RIGHT SIDE NOSE WHEEL WELL BULKHEAD WEB CRACKED AT STATION 260, WL 182 RBL 38. WEB REPAIRED AS PER BOEING MESSAGE 1-636527780-4. - [SDR UIEA200700447](https://openairdocs.org/sdr/UIEA200700447), Sep 30, 2007: SKIN. CORRODED. NR 8 SPOILER AREA OF UPPER SKIN AND REAR SPAR HAS AREA OF CORROSION. REPAIRED AS PER BOEING MESSAGE 1--638467931-2. - [SDR UIEA200700450](https://openairdocs.org/sdr/UIEA200700450), Sep 29, 2007: BRACE. LOOSE. NR 1 PYLON DIAGONAL BRACE UNDERWING FITTING TENSION FASTENER HEAD SHEARED. REMOVED AND INSTALLED FASTENER AS PER 51-30-02. - [SDR UIEA200700449](https://openairdocs.org/sdr/UIEA200700449), Sep 29, 2007: SPAR CAP. CORRODED. RIGHT WING FRONT SPAR LOWER CHORD AREA BETWEEN FSSO 1322 AND 1340 CORRODED. CORROSION REMOVED AS PER SRM 51-10-01 AND BOEING MESSAGE 1-638497220-2. - [SDR UIEA200700448](https://openairdocs.org/sdr/UIEA200700448), Sep 29, 2007: SPAR CAP. CORRODED. RIGHT WING FRONT SPAR LOWER CHORD AREA FSSO 1356 CORRODED. CORROSION REMOVED AS PER SRM 51-10-01 AND BOEING MESSAGE 1-638497220-2. - [SDR UIEA200700443](https://openairdocs.org/sdr/UIEA200700443), Sep 29, 2007: BRACE. CHAFED. NR 4 STRUT DIAGONAL BRACE FORWARD END CHAFED. CHAFING AREA DAMAGE BLENDED AS PER BOEING MESSAGE 1-636565614-4. - [SDR UIEA200700445](https://openairdocs.org/sdr/UIEA200700445), Sep 26, 2007: FAIRING. DELAMINATED. FUSELAGE FAIRING 193C AREA OF DELAMINATION. DELAMINATED AREA REPAIRED AS PER SRM 51-40-12 - [SDR UIEA200700324](https://openairdocs.org/sdr/UIEA200700324), Aug 24, 2007: SKIN. DELAMINATED. LT WING UPPER SURFACE TRAILING EDGE FIXED PANEL AT STATION 1224 HAS AN AREA OF 2.0 INCH LONG BY 15.0 INCH WIDE AREA OF DELAMINATION. PERMANENT REPAIR OF AREA WA - [SDR UIEA200700248](https://openairdocs.org/sdr/UIEA200700248), Jun 16, 2007: SKIN. DENTED. LOWER FUSELAGE, RT SIDE AT STA 660 HAS A DENT BETWEEN S43 AND S44 RT CAUSED BY ACCIDENT DURING STORM. ACCOMPLISHED PERMANENT REPAIR OF EXTERIOR SKIN AS PER 747- - [SDR UIEA200700247](https://openairdocs.org/sdr/UIEA200700247), Jun 16, 2007: SKIN. UNKNOWN. RADOME SKIN HAS A 2.0 INCH BY 4.0 INCH PREVIOUS REPAIR FILLER ERODED AT 11 O'CLOCK POSITION. ACCOMPLISHED PERMANENT REPAIR AS PER 747-200 SRM 53-50-03 PAGE 23, - [SDR UIEA200700144](https://openairdocs.org/sdr/UIEA200700144), Mar 24, 2007: SKIN. CRACKED. FUSELAGE SKIN HAS A CRACK APPROX 400", AT BS 789 S46R AND RIVET PULLING THROUGH. REPAIRED ACCOMPLISHED AS PER XEO NR 53-032207. - [SDR UIEA200700132](https://openairdocs.org/sdr/UIEA200700132), Mar 2, 2007: OIL FILTER. UNSERVICEABLE. NR 2 OIL FILTER BY PASS LIGHT ILLUMINATED DURING DESCENT, LIGHT REMAINED AT IDLE THRUST, SHUT DOWN NR 2 ENGINE. REMOVED AND REPLACED NR 2 ENGINE OIL FILTER AS P - [SDR UIEA200700002](https://openairdocs.org/sdr/UIEA200700002), Jan 8, 2007: SEAT TRACK. BROKEN. MAIN CARGO COMPARTMENT SEAT TRACK AT STATION 1960 RT, RBL 11 HAS 1 EACH BROKEN CROWN LUG. REMOVED AND REPLACED SECTION OF SEAT TRACK FROM STATION 1946 TO 1969 R - [SDR UIEA200600291](https://openairdocs.org/sdr/UIEA200600291), Nov 12, 2006: CIRCUIT CARD. FAILED. RED GEAR LIGHT CAME ON AFTER RETRACTION WITH AURAL WARNING ON IN UP POSITION, GEAR UNSAFE CHECK ACCOMPLISHED PER FHB PROCEDURES AND RETURNED FOR LANDING. T/S FO - [SDR UIEA200600282](https://openairdocs.org/sdr/UIEA200600282), Nov 1, 2006: SKIN. CRACKED. MAIN ENTRY DOOR L-1, LOWER, FORWARD HINGE CUT-OUT HAS A CRACK AT PREVIOUS REPAIR DOUBLER. PERMANENT EXTERNAL DOUBLER REPAIR WAS ACCOMPLISHED IAW SB 747-52-2144 - [SDR UIEA200600197](https://openairdocs.org/sdr/UIEA200600197), Aug 4, 2006: SKIN. DELAMINATED. RT AFT IB FLAP UPPER AND LOWER SIDES OF SKIN HAVE AN AREA OF DELAMINATION. UPPER SIDE IS AT WBL 278.750 AND DAMAGE AREA IS 1.5 INCHES. LOWER SIDE IS AT WBL 272. - [SDR UIEA200600156](https://openairdocs.org/sdr/UIEA200600156), Jul 2, 2006: FLAP. ACTIVATED. AFTER CLIMB-OUT AND FLAP RETRACTION FROM 5*-1*, FLAPS STAYED IN FLAPS 5* POSITION, ACCOMPLISHED ALT FLAP OPERATION SECT III FLAPS MOVED TO APPROX 3*, THEN STOPP - [SDR UIEA200600142](https://openairdocs.org/sdr/UIEA200600142), Jun 22, 2006: STEERING SYS. MALFUNCTIONED. RTO AT 30 KTS AIRCRAFT DRIFTED LEFT WITH NO EFFECTIVE CONTROL, W/NOSE WHEEL STEERING. NOSE WHEEL STEERING APPEARS TO BE INOP. TRANSF TO DMI M06-076 PER MEL 32-1 - [SDR UIEA200700249](https://openairdocs.org/sdr/UIEA200700249), Jun 16, 2006: PANEL. CRACKED. LT HORIZONTAL STABILIZER, LOWER T/E ACCESS PANEL 334 GBL HAS 2 EACH CRACKS ON INBOARD SIDE OF PANEL. CRACKS ARE 2.0 INCH IN LENGTH. ACCOMPLISHED PERMANENT REPAI - [SDR UIEA200600122](https://openairdocs.org/sdr/UIEA200600122), Jun 1, 2006: APU. MALFUNCTIONED. APU FIRE BOTTLE WAS DISCHARGED DUE TO HEAVY BLACK SMOKE COMING FROM INLET, TAILPIPE, AND COWLING OF APU. APU INOP DUE TO FIRE BOTTLE PREVIOUSLY DISCHARGED. FIRE - [SDR UIEA200600115](https://openairdocs.org/sdr/UIEA200600115), May 8, 2006: SKIN. DENTED. FOUND DENTS AT BS 660 BETWEEN S-46L AND S-45R. REPAIR ACCOMPLISHED AS PER BOEING MESSAGE 1-17408378 AND FAA FORM 8100-9. - [SDR UIEA200600114](https://openairdocs.org/sdr/UIEA200600114), May 8, 2006: SKIN. CRACKED. NR 1 PYLON RIGHT SIDE SKIN ASSEMBLY WAS FOUND CRACKED IN THE AREA COVERED BY TITANIUM DOUBLERS. INTERIM REPAIR FOR THE NR 1 PYLON 65B94100 SKIN ASSEMBLY, WAS AC - [SDR UIEA200600113](https://openairdocs.org/sdr/UIEA200600113), May 8, 2006: SKIN. CRACKED. DURING A C-CHECK, CRACK DAMAGE WAS FOUND IN THE 65B94052 SKIN ASSEMBLY NR 3 STIFFENER AND PRE-COOLER EXHAUST CUT OUT EDGE ADJACENT TO N.S. 248 NR 2 PYLON. INTER - [SDR UIEA200600111](https://openairdocs.org/sdr/UIEA200600111), May 8, 2006: SKIN. CRACKED. THE CRACKS WERE FOUND IN THE SUBJECT STRUT CAP SKIN ASSEMBLY AND ADJACENT BULKHEAD STRAP AT STA-286 BULKHEAD INSTALLATION CROWN AREA AT B-L. 0-0. THE AFT EDGE O - [SDR UIEA200600110](https://openairdocs.org/sdr/UIEA200600110), May 8, 2006: SKIN. CRACKED. CRACK DAMAGE WAS FOUND IN THE 65B94052 SKIN ASSEMBLY NR 3 STIFFENER, AND PRE-COOLER EXHAUST CUT OUT ADJACENT TO THE AFT CORNER AT N.S.248, ON THE RIGHT SIDE OF - [SDR UIEA200600106](https://openairdocs.org/sdr/UIEA200600106), May 8, 2006: BULKHEAD. CRACKED. BS 2598 BULKHEAD AFT OUTER CHORD ATTACH FASTENER CRACKS AT STR 12L,LBL 50-55, WL 310-315. REPAIR ACCOMPLISHED AS PER BOEING MESSAGE 1-17563784 AND FAA FORM 8100 - [SDR UIEA200600105](https://openairdocs.org/sdr/UIEA200600105), May 8, 2006: SKIN. CORRODED. CORROSION IN THE INTERNAL BEAR STRAP AT THE RT AFT CORNER OF THE FORWARD LAVATORY SERVICE DOOR CUT-OUT, BS 560, STR 46R. REPAIR ACCOMPLISHED AS PER BOEING MESSA - [SDR UIEA200600108](https://openairdocs.org/sdr/UIEA200600108), May 4, 2006: FLOORBEAM. CORRODED. REPORTED CORROSION ADJACENT TO AN EXISTING REPAIR ANGLE AT THE MAIN DECK FLOORBEAM UPPER T-CHORD HORIZONTAL FLANGE AT STA 620. REPAIR ACCOMPLISHED AS PER BOEING - [SDR UIEA200600103](https://openairdocs.org/sdr/UIEA200600103), May 4, 2006: FLOORBEAM. CORRODED. REPORTED CORROSION ON THE MAIN DECK FLOORBEAM UPPER T-CHORD HORIZONTAL FLANGE AT STA 500 BETWEEN APPROXIMATELY LBL 50.0 AND LBL 60.0. THE UPPER CHORD WAS REPLAC - [SDR UIEA200600112](https://openairdocs.org/sdr/UIEA200600112), May 3, 2006: SPAR. CORRODED. CORROSION DAMAGE FOUND IN SUBJECT SPAR AFT FLANGE AT WBL 770. INTERIM REPAIR TO OUTBOARD TRAILING EDGE MIDFLAP, NR 3 SPAR LOWER CHORD ACCOMPLISHED AS PER BOEING - [SDR UIEA200600109](https://openairdocs.org/sdr/UIEA200600109), May 3, 2006: SKIN. CRACKED. CRACKED RT OUTBOARD ELEVATOR PANEL AT ELEV STA 244 AND 306, P/N 65B05730-2. REPAIR ACCOMPLISHED AS PER BOEING MESSAGE 1-174409992 AND FAA FORM 8100-9. - [SDR UIEA200600107](https://openairdocs.org/sdr/UIEA200600107), Apr 25, 2006: WEB. CRACKED. CRACKED WEB AND LOWER CHORD AT THE RT HORIZONTAL STABILIZER STA BL 421.50. WEB AND LOWER CHORD REPAIR CARRIED OUT AS PER BOEING MESSAGE 1-17410726 AND FAA FORM - [SDR UIEA200600104](https://openairdocs.org/sdr/UIEA200600104), Apr 25, 2006: WEB. CRACKED. LT HORIZONTAL STAB, UPPER CHORD AT STAB BL 421.5 FOUND 1/2" CRACK AT AFT END. CHORD REPAIR CARRIED OUT AS PER BOEING MESSAGE 1-176012397 AND FAA FORM 8100-9. - [SDR UIEA200600085](https://openairdocs.org/sdr/UIEA200600085), Apr 25, 2006: FRAME. CRACKED. RT STA 360 FRAME WEB AT STR 14E CUT OUT FOUND CRACKED 7.5". CRACKS WERE FOUND ON FRAME WEB. REPAIR DOUBLERS WERE INSTALLED IAW BOEING MESSAGE NR 1-175762603, AN All 70: https://openairdocs.org/deregistered/N809MC-2010-11-08/reports.md ## Other aircraft with N809MC - [Registered now](https://openairdocs.org/aircraft/N809MC): Socata TBM 700, S/N 651, built 2013 --- 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.