# N472MC: 1992 Boeing 747-45E - Status: Valid registration - Airframe: [Boeing 747-45E](https://openairdocs.org/model/boeing-747-45e) (registry code 1384947, 495 seats) - Engine: [GE CF6-80C2B1F](https://openairdocs.org/engine/ge-cf6-80c2b1f) (registry code 30106) - Data sheets: [TCDS E13NE](https://openairdocs.org/tcds/E13NE) (General Electric Company GE Aerospace) (OpenAirDocs) - Serial number: 27062 - Year built: 1992 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: January 16, 2018 - Certificate issued: September 18, 2017 - Expires: September 30, 2027 - Mode S code: A5C99E - Registered owner: [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 is based - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=472MC - Page: https://openairdocs.org/aircraft/N472MC 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): 33 in force ### Matched by airframe (Boeing 747-45E) None in force. ### Matched by engine (GE CF6-80C2B1F) - [AD 2023-20-08](https://openairdocs.org/ad/2023-20-08): Engine (Turbine/Turboprop) · General Electric CF6-80C2B1F, CF6-80C2B2F, CF6-80C2B4F and 4 more. Effective Oct 19, 2023 - [AD 2021-26-22](https://openairdocs.org/ad/2021-26-22): Turbine Section · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 21 more. Effective Mar 14, 2022 - [AD 2021-14-11](https://openairdocs.org/ad/2021-14-11): Turbine Section · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 25 more. Effective Aug 27, 2021 - [AD 2021-03-02](https://openairdocs.org/ad/2021-03-02): Fuel Control/Turbine Engines · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 16 more. Effective Mar 31, 2021 - [AD 2020-22-02](https://openairdocs.org/ad/2020-22-02): Engine Fuel and Control · General Electric CF6-80C2A5F, CF6-80C2B1F, CF6-80C2B2F and 13 more. Effective Dec 3, 2020 - [AD 2016-08-10](https://openairdocs.org/ad/2016-08-10): Accessory heat shield · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 26 more. Effective Jun 1, 2016 - [AD 2014-21-01](https://openairdocs.org/ad/2014-21-01): Fuel manifold · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 26 more. Effective Nov 28, 2014 - [AD 2013-08-20](https://openairdocs.org/ad/2013-08-20): Fuel tube · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 14 more. Effective May 31, 2013 - [AD 2012-03-12](https://openairdocs.org/ad/2012-03-12): No. 3 bearing packing · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 21 more. Effective Apr 5, 2012 - [AD 2012-04-05](https://openairdocs.org/ad/2012-04-05): Electronic control unit (ECU) · General Electric CF6-80C2B1F, CF6-80C2B1F1, CF6-80C2B1F2 and 8 more. Effective Mar 30, 2012 - [AD 2009-21-07](https://openairdocs.org/ad/2009-21-07): Thrust and thrust control · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 21 more. Effective Dec 1, 2009 - [AD 2009-07-03](https://openairdocs.org/ad/2009-07-03): Eddy current inspection (ECI) · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 26 more. Effective Apr 30, 2009 - [AD 2009-04-10](https://openairdocs.org/ad/2009-04-10): Critical life-limited parts · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 30 more. Effective Mar 30, 2009 - [AD 2008-21-11](https://openairdocs.org/ad/2008-21-11): Low-pressure turbine (LPT) cases · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 25 more. Effective Nov 28, 2008 - [AD 2007-11-20](https://openairdocs.org/ad/2007-11-20): Fuel shroud retaining rings · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 22 more. Effective Jul 10, 2007 - [AD 2007-05-14](https://openairdocs.org/ad/2007-05-14): Cast titanium weld- repaired forward engine mount platforms · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 16 more. Effective Apr 9, 2007 - [AD 2006-16-06](https://openairdocs.org/ad/2006-16-06): Certain stage 1 high- pressure turbine (HPT) rotor disks · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 21 more. Effective Sep 5, 2006 - [AD 2005-17-05](https://openairdocs.org/ad/2005-17-05): High pressure compressor rotor (HPCR) · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 25 more. Effective Sep 27, 2005 - [AD 2004-22-07](https://openairdocs.org/ad/2004-22-07): Stage 2 nozzle guide vanes (HPT S2 NGVs) · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 16 more. Effective Dec 1, 2004 - [AD 2003-02-07](https://openairdocs.org/ad/2003-02-07): Low pressure turbine (LPT) shrouds · General Electric CF6-50A, CF6-50C, CF6-50C1 and 30 more. Effective Mar 3, 2003 - [AD 2002-25-08](https://openairdocs.org/ad/2002-25-08): High pressure compressor rotor · General Electric CF6-45A, CF6-45A2, CF6-50A and 40 more. Effective Jan 23, 2003 - [AD 2002-22-12](https://openairdocs.org/ad/2002-22-12): Titeflex hoses · BAE Systems ATP, Avro 146-RJ100A, Avro 146-RJ70A and 122 more. Effective Dec 13, 2002 - [AD 2000-03-04](https://openairdocs.org/ad/2000-03-04): General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 19 more. Effective Apr 10, 2000 - [AD 99-01-01](https://openairdocs.org/ad/99-01-01): Accessory Gearbox (AGB) idler adapters · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 19 more. Effective Jan 21, 1999 - [AD 98-22-06](https://openairdocs.org/ad/98-22-06): Fan Disks · General Electric CF6-45A, CF6-45A2, CF6-50A and 41 more. Effective Nov 23, 1998 - [AD 97-22-14](https://openairdocs.org/ad/97-22-14): (HPCR) 3-9 Spool · General Electric CF6-50A, CF6-50C, CF6-50C1 and 29 more. Effective Nov 17, 1997 - [AD 96-16-07](https://openairdocs.org/ad/96-16-07): Rear Right Hand Mount Link · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 17 more. Effective Aug 28, 1996 - [AD 95-10-11](https://openairdocs.org/ad/95-10-11): Fan Reversers · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 17 more. Effective May 31, 1995 - [AD 94-20-06](https://openairdocs.org/ad/94-20-06): Oil System · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 16 more. Effective Dec 27, 1994 - [AD 94-06-03](https://openairdocs.org/ad/94-06-03): High Pressure Turbine Disk · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 16 more. Effective Apr 29, 1994 - [AD 93-14-18](https://openairdocs.org/ad/93-14-18): High pressure turbine (HPT) thermal shields · General Electric CF6-45A, CF6-45A2, CF6-50A and 40 more. Effective Oct 4, 1993 - [AD 91-15-25](https://openairdocs.org/ad/91-15-25): High Pressure Compressor Rotor · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 16 more. Effective Sep 6, 1991 - [AD 91-11-05](https://openairdocs.org/ad/91-11-05): High Pressure Compressor Rotor · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 16 more. Effective Jul 5, 1991 ### Historical (superseded or no longer in force) - [AD 2020-20-13](https://openairdocs.org/ad/2020-20-13) (historical): Turbine Section · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 21 more. Effective Nov 12, 2020 - [AD 2018-15-04](https://openairdocs.org/ad/2018-15-04) (historical): Turbine/Turboprop Engine--Turbine Section · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 21 more. Effective Oct 2, 2018 - [AD 2009-05-02](https://openairdocs.org/ad/2009-05-02) (historical): Drainless fuel manifold assemblies · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 26 more. Effective Mar 31, 2009 - [AD 2007-12-07](https://openairdocs.org/ad/2007-12-07) (historical): Electronic control units (ECUs) · General Electric CF6-80C2B1F, CF6-80C2B2F, CF6-80C2B4F and 5 more. Effective Jul 11, 2007 - [AD 2004-04-07](https://openairdocs.org/ad/2004-04-07) (historical): Stage 1 HPT rotor disks · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 21 more. Effective Mar 12, 2004 - [AD 2002-07-12](https://openairdocs.org/ad/2002-07-12) (historical): Life Limits Section of Continued Airworthiness (ICA) - Selected Critical Life-limited Parts · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 27 more. Effective May 15, 2002 - [AD 2001-10-07](https://openairdocs.org/ad/2001-10-07) (historical): High Pressure Turbine Rotor Disks · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 19 more. Effective Jun 18, 2001 - [AD 2000-16-12](https://openairdocs.org/ad/2000-16-12) (historical): High Pressure Compressor Rotor Stage 3-9 Spools · General Electric CF6-45A, CF6-45A2, CF6-50A and 39 more. Effective Sep 5, 2000 - [AD 2000-04-14](https://openairdocs.org/ad/2000-04-14) (historical): Fuel tube flange seating · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 12 more. Effective May 1, 2000 - [AD 99-24-15](https://openairdocs.org/ad/99-24-15) (historical): High Pressure Compressor Rotor (HPCR) Stage 3-9 Spools · General Electric CF6-45A, CF6-45A2, CF6-50A and 39 more. Effective Jan 28, 2000 - [AD 99-08-13](https://openairdocs.org/ad/99-08-13) (historical): General Electric CF6-80A, CF6-80A1, CF6-80A2 and 26 more. Effective May 13, 1999 - [AD 91-20-02](https://openairdocs.org/ad/91-20-02) (historical): Fuel Manifolds · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 12 more. Effective Nov 25, 1991 - [AD 90-26-01](https://openairdocs.org/ad/90-26-01) (historical): Fuel Manifold Systems · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 11 more. Effective Dec 20, 1990 ## Information bulletins (advisory) (5 in force) - [SAIB 2023-15](https://openairdocs.org/saib/2023-15): Falsified Forms from AOG Technics. Issued Dec 19, 2023 - [SAIB NE-11-27](https://openairdocs.org/saib/NE-11-27): Fuel Injector Nozzle - CF6-80 Improperly Welded Fuel Nozzles. Issued Apr 5, 2011 - [SAIB NE-10-37](https://openairdocs.org/saib/NE-10-37): Engine Fuel and Control: FADEC Fuel Metering Valve Resolver Feedback Faults. Issued Jul 12, 2010 - [SAIB NE-08-44](https://openairdocs.org/saib/NE-08-44): Engine Thrust Reverser Transcowl Clevis Pin. Issued Sep 3, 2008 - [SAIB NE-07-01](https://openairdocs.org/saib/NE-07-01): Dual engine flameouts on twin engine airplanes. Issued Oct 12, 2006 ## NTSB investigations None matched to N472MC. ## FAA accident and incident reports (1) From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [Incident 20180619008259I](https://openairdocs.org/incident/20180619008259I), Jun 19, 2018: Boeing 747-45E (N472MC), Chicago, IL, No damage. On June 19, 2018 N472MC a B747-400 bedeck special freighter (bdsf) operated as gti 2134 from anchorage, Alaska (anc) to Chicago, Illinois (ord). While on… ## Service difficulty reports (171, newest 50) 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 UIEA2026102200992](https://openairdocs.org/sdr/UIEA2026102200992), Oct 22, 2026: ADC. FAULTED. RTO DUE TO MASTER CAUTION ASSOCIATED WITH AN APPERENT ADC-L FAILURE. CAPT PFD LOST AIRSPEED, ALTITUDE + V/S INDICATIONS(

R/R LEFT ADC REF AIPC 34-12-01-61 &AM - [SDR UIEA2026102300993](https://openairdocs.org/sdr/UIEA2026102300993), Oct 12, 2026: FIRE WARNING. FALSE ACTIVATION. CARGO FIRE AFT MASTER WARNING AFTER LANDING. PERFORMED LWR CARGO SMOKE DETECTION OPS TEST, TEST PASSED IAW AMM 26-16-00. - [SDR UIEA2026052900368](https://openairdocs.org/sdr/UIEA2026052900368), May 29, 2026: PSEU. FAULTED. GEAR DOOR ADVISORY MSG AFTER TAKE OFF. GEAR DOOR & GEAR MONITOR STATUS MESSAGES. FOUND FAULTS J6 32795, 32717, 326675 & 32677. T/S PERFORMED PER FIM 32-61 TASK - [SDR UIEA2025111901313](https://openairdocs.org/sdr/UIEA2025111901313), Nov 19, 2025: DUCT. DAMAGED. BLEED 2 DUCT LEAK RH STATUS MSG. R & R R4 PDU PNEUMATIC DUCT IAW AMM 27-81-03-002-001. OPS & LEAK CHECKED OK. - [SDR UIEA2025090401155](https://openairdocs.org/sdr/UIEA2025090401155), Sep 6, 2025: RIVET. DAMAGED. STA 200 STR 31AL L/H 1 EA RIVET FOUND LIGHTNING STRIKE. STA 200 STR 31AL L/H 1EA RIVET HEAD LIGHTNING STRIKE REPAIRED IAW SRM 53-00-01-2R-9 REPAIR 9 SECTION II - [SDR UIEA2025090401156](https://openairdocs.org/sdr/UIEA2025090401156), Sep 6, 2025: RIVET. DAMAGED. FX - STA 200 STR 23-24A R/H 1EA RIVET FOUND LIGHTNING STRIKE. STA 200 STR 23-24A R/H 1EA RIVET HEAD LIGHTNING STRIKE REPAIRED IAW SRM 53-00-01-2R-9 REPAIR 9 SEC - [SDR UIEA2025090401157](https://openairdocs.org/sdr/UIEA2025090401157), Sep 6, 2025: RIVET. DAMAGED. FX - STA 215 STR 31AL L/H 1EA RIVET FOUND LIGHTNING STRIKE STA 21 STR 31AL L/H 1EA RIVET HEAD LIGHTNING STRIKE REPAIRED IAW SRM 53-00-01-2R-9 REPAIR 9 SECTION I - [SDR UIEA2025090401158](https://openairdocs.org/sdr/UIEA2025090401158), Sep 6, 2025: RIVET. DAMAGED. FX - STA 140-160 STR 24A R/H 1EA RIVET FOUND LIGHTNING STRIKE. FX - STA 140-160 STR 24A RT 1EA RIVET HEAD LIGHTNING STRIKE REPAIRED IAW SRM 53-00-01-2R-9 REPAIR - [SDR UIEA2025090401159](https://openairdocs.org/sdr/UIEA2025090401159), Sep 6, 2025: RIVET. DAMAGED. FX - STA 160 STR 24A-26 R/H 1EA RIVET FOUND LIGHTNING STRIKE(

FX - STA 160 STR 24A-26 R/H 1EA RIVET HEAD LIGHTNING STRIKE REPAIRED IAW SRM 53-00-01-2R-9 REPAI - [SDR UIEA2025090501162](https://openairdocs.org/sdr/UIEA2025090501162), Sep 6, 2025: PANEL. TORN. LEFT WING INBD L/E UPPER (ILES550-ILES630) PANEL FOUND TORN. PERFORMED TIME LIMITED COMPOSITE REPAIR IAW EA-4457A244, PART 1, REV 0. NO FURTHER DEFECTS NOTED. - [SDR UIEA2025040700445](https://openairdocs.org/sdr/UIEA2025040700445), Apr 8, 2025: RIB. CRACKED. EMP - RH HORI STAB TIP CLOSURE RIB LOWER CHORD CRACK.(

LOWER CHORD REPLACED AS PER SRM 51-10-02 & NEW LOWER CHORD HOLES TRANSFERRED AS PER SRM 51-40-05 AN - [SDR UIEA2025040700446](https://openairdocs.org/sdr/UIEA2025040700446), Apr 8, 2025: NUT PLATE. CRACKED. EMP RH HORI STAB TIP CLOSURE RIB LOWER CHORD ATT NUT PLATE STRAP CRACK.(

CRACK NUTPLATE STRAP FABRICATED & INSTALLED AS PER RI-55-10-17555 REV.A. NO FURTH - [SDR UIEA2024080100765](https://openairdocs.org/sdr/UIEA2024080100765), Jul 28, 2024: CIRCUIT CARD. FAULTED. AFT CGO FIRE WARNING ON SHORT FINAL. R & R AFOLTS AFT CGO CIRCUIT CARD YLPA032 IAW AMM 26-10-01 & IPC 26-14-02-01. OPS CHECK / GND TEST PASS. NO DEFECTS NOTED. - [SDR UIEA2024061300518](https://openairdocs.org/sdr/UIEA2024061300518), Jun 13, 2024: FILTER. FAILED. DURING ENROUTE CLIMB FROM FL 300 TO FL 400, EICAS ENG 1 AND 4 FUEL FILTER MSG DISPLAYED.(

REF FIM 73-00 RPLD 1 AND 4 FUEL FILTERS PER AMM 73-11-02 AND SUMP DR - [SDR UIEA2024040500265](https://openairdocs.org/sdr/UIEA2024040500265), Apr 3, 2024: SKIN. CORRODED. CORROSION - SKIN LEFT UNDERWING REAR SPAR OVERRIDE JETTISON PUMP AREA.(

1. BLENDED OUT THE DAMAGE AREA IAW SRM 51-10-02-0G-0 REV 119 2. ACCOMPLISHED EI T2024A - [SDR UIEA2024040500264](https://openairdocs.org/sdr/UIEA2024040500264), Apr 3, 2024: SKIN. CORRODED. CORROSION - SKIN, LH WING INSPAR UPR SURFACE T/E AREA WS 469.82 ~ WS 478.80 REAR SPAR AREA(

1. REMOVED THE AFFECTED FASTENERS IAW SRM 51-40-02-0G-0 REV 120 2. - [SDR UIEA2024040500263](https://openairdocs.org/sdr/UIEA2024040500263), Apr 3, 2024: BEAM. CORRODED. CORROSION - FOUND L/H H.S.T T/E BEAM ELEV STA 257 LOWER CHORD CORROSION(

1. ACCOMPLISH EI T2024A55M-509 REV 0 2. ACCOMPLISHED EI T2024A55M-509 REV 1 3. JOB CO - [SDR UIEA2024040500262](https://openairdocs.org/sdr/UIEA2024040500262), Apr 3, 2024: FAIRING. CORRODED. CORROSION ON AFT WTB FAIRING LWR CHORD AT STA 1480. LBL 16 ~ RBL 16(

1. REMOVE DAMAGE PART IAW SRM 51-40-02-OG-0 REV 120 2. FABRICATED PART IAW WORKSHEET 4023 - [SDR UIEA2024040500261](https://openairdocs.org/sdr/UIEA2024040500261), Apr 3, 2024: BRACKET. CORRODED. CORROSION-BRACKET, LH WING T/E CAVITY HYD TUBE BLOCK - CLAMP WBL 178(

1. REMOVE DAMAGE PART IAW SRM 51-40-02-OG-0 REV 120 2. INSTALL NEW PART IAW SRM 51-40-02 - [SDR UIEA2024040500260](https://openairdocs.org/sdr/UIEA2024040500260), Apr 3, 2024: FLOORBEAM. NONE. PERFORM EO A453B457 SEC 42 UPPER DECK FLOOR BEAM REPEAT INSP FOUND FILLED DEVIATION AT STA 660 RBL 13(

1. REMOVED DAMAGED PART IAW SRM 51-40-02-0G-01 REV 120 - [SDR UIEA2024040500259](https://openairdocs.org/sdr/UIEA2024040500259), Apr 3, 2024: SPAR. CRACKED. FOUND LH WING FRONT SPAR WEB CRACK NEAR FSSI 656(

1. REPAIR DAMAGED AREA IAW EI T2024A57M-424 REV 4 2. ACCOMPLISHED EI T2024A57M-424 REV 5 3. JOB COMPLETED AN - [SDR UIEA2024040500258](https://openairdocs.org/sdr/UIEA2024040500258), Apr 3, 2024: SKIN. CORRODED. FOUND LH WING LOWER SKIN HAVE CORROSION AT FSSI 628 ~ FSSI 660(

1. REPAIR DAMAGED AREA IAW EI T2024A57M-480 REV 6 2. JOB COMPLETED AND CONDITION CHECK NORMAL< - [SDR UIEA2024040500257](https://openairdocs.org/sdr/UIEA2024040500257), Apr 3, 2024: SKIN. CORRODED. CORROSION DAMAGES ON THE LH WING UPPER SKIN (P/N= 112U3102-3) UPPER SURFACE NEAR WS 323.82 (WBL 150.00) , S-16 ~ S-17(

1. REMOVED THE AFFECTED FASTENERS IAW S - [SDR UIEA2024040500256](https://openairdocs.org/sdr/UIEA2024040500256), Apr 3, 2024: SKIN. CORRODED. CORROSION DAMAGES ON THE LH WING UPPER SKIN (P/N= 112U3101-3) UPPER SURFACE NEAR WS 469.82, S-3 ~ S-4(

1. REMOVED THE AFFECTED FASTENERS IAW SRM 51-40-02-0G-0 - [SDR UIEA2024040500255](https://openairdocs.org/sdr/UIEA2024040500255), Apr 3, 2024: SKIN. CORRODED. CORROSION DAMAGES ON THE LH WING UPPER SKIN (P/N= 112U3101-3) UPPER SURFACE NEAR WBL 150.00, MID SPAR(

1. REMOVED THE AFFECTED FASTENERS IAW SRM 51-40-02-0G-0 - [SDR UIEA2024040500254](https://openairdocs.org/sdr/UIEA2024040500254), Apr 3, 2024: CHANNEL. CRACKED. CRACK-CHANNEL, SEC 42 UPPER DECK TENSION TIE FOWARD CHANNEL AT STA 960LH(

1. ACCOMPLISHED TENSION TIE REPAIR AT LH STA 960 BETWEEN STR 10R AND 10L IAW EI T202 - [SDR UIEA2024040500253](https://openairdocs.org/sdr/UIEA2024040500253), Apr 3, 2024: FRAME. CRACKED. CRACK-FRAME, SEC 42 UPPER DECK TENSION TIE AT THE AREA OF ATTACHMENT TO FRAME 1 EA HOLE, AT STA 960 RH(

1. ACCOMPLISHED FRAME WEB REPAIR AT RH STA 960 BETWEEN - [SDR UIEA2024040500252](https://openairdocs.org/sdr/UIEA2024040500252), Apr 3, 2024: CHANNEL. CRACKED. CRACK-CHANNEL, SEC 42 UPPER DECK TENSION TIE - FOWARD CHANNEL AT STA 900 LH(

1. ACCOMPLISHED TENSION TIE REPAIR AT LH, STA 900 BETWEEN STR 9L AND 10L IAW EI&N - [SDR UIEA2024040500251](https://openairdocs.org/sdr/UIEA2024040500251), Apr 3, 2024: CHANNEL. CRACKED. CRACK-CHANNEL, SEC 42 UPPER DECK TENSION TIE - FOWARD CHANNEL AT STA 940 RH(

1. ACCOMPLISHED TENSION TIE REPAIR AT RH STA 940 BETWEEN STR 10R AND STR 10AR IAW - [SDR UIEA2024040500250](https://openairdocs.org/sdr/UIEA2024040500250), Apr 3, 2024: DOOR FRAME. CORRODED. CRACK-VERTICAL FRAME, L2 MAIN ENTRY DOOR FWD UPPER SIDE.(

1. PERFORM EI T2024A52M-488, SEQUENCE A REV=0 2. ACCOMPLISHED EI T2024A52M-488 REV=1 3. JOB COMPLETE - [SDR UIEA2024040500249](https://openairdocs.org/sdr/UIEA2024040500249), Apr 3, 2024: DOOR FRAME. CORRODED. FIND DOOR R1 AFT LOWER SIDE FRAME WEB CORROSION(

1. PERFORM EI T2024A52M-491, SEQUENCE A. REV=0 2. ACCOMPLISHED EI T2024A52M-491. REV=1 3. JOB COMPLETED AND C - [SDR UIEA2024040500248](https://openairdocs.org/sdr/UIEA2024040500248), Apr 3, 2024: FRAME. CRACKED. CRACK-FRAME, LH INTERNAL FUSELAGE FRAME WEB AT STA 1060, WL 329(

1. ACCOMPLISH EI T2024A53M-432 REV:1, SEQUENCE A PART 1: FRAME WEB SHEAR TIE REPAIR AT STA 10 - [SDR UIEA2024040500247](https://openairdocs.org/sdr/UIEA2024040500247), Apr 3, 2024: FRAME. CRACKED. CRACK-FRAME, LH INTERNAL FUSELAGE FRAME WEB AT STA 1100, WL 329(

1. ACCOMPLISH EI T2024A53M-432 REV:1, SEQUENCE A PART 5: FRAME WEB SHEAR TIE REPAIR AT STA 11 - [SDR UIEA2024040500246](https://openairdocs.org/sdr/UIEA2024040500246), Apr 3, 2024: FRAME. CRACKED. CRACK-FRAME, RH INTERNAL FUSELAGE FRAME WEB AT STA 1080, WL 329(

1. FRAME WEB SHEAR TIE REPAIR AT STA 1080 RH IAW EI T2024A53M-432, SEQUENCE A PART 4 REV=01 2 - [SDR UIEA2024040500245](https://openairdocs.org/sdr/UIEA2024040500245), Apr 3, 2024: FRAME. CRACKED. CRACK-FRAME, RH INTERNAL FUSELAGE FRAME WEB AT STA 1060, WL 329(

1. FRAME WEB SHEAR TIE REPAIR AT STA 1060 RH IAW EI T2024A53M-432, SEQUENCE A PART 2 REV=01. - [SDR UIEA2024040500244](https://openairdocs.org/sdr/UIEA2024040500244), Apr 3, 2024: FRAME. CRACKED. CRACK-FRAME, LH INTERNAL FUSELAGE FRAME WEB AT STA 1080, WL 329(

1. ACCOMPLISH EI T2024A53M-432, REV=1, SEQUENCE A PART 3, FRAME WEB SHEAR TIE REPAIR AT STA 1 - [SDR UIEA2024040500243](https://openairdocs.org/sdr/UIEA2024040500243), Apr 3, 2024: FRAME. CRACKED. CRACK- FRAME - RH INTERNAL FUSELAGE FRAME WEB AT STA 1100, WL 329(

1. FRAME WEB SHEAR TIE REPAIR AT STA 1100 RH IAW EI T2024A53M-432, SEQUENCE A. REV=1 PART 6 - [SDR UIEA2024040500242](https://openairdocs.org/sdr/UIEA2024040500242), Apr 3, 2024: FRAME. CRACKED. FND BULK CGO BILGE FRAME CRACK AT STA 2260 RBL 53(

1. REPAIRED CRACK AREA IAW EI T2024A53M-518 REV-1, SEQUENCE B. 2. ACCOMPLISHED EI T2024A53M-518, REV=2 3. J - [SDR UIEA2024040500241](https://openairdocs.org/sdr/UIEA2024040500241), Apr 3, 2024: SKIN. DENTED. DENT- PANEL 587LT EXTERNAL, LH OUTBD MID FLAP WBL 582(

1. PERFORM REPAIR OF DENT SKIN DAMAGE AT L/H WING OUTBD MID FLAP TOP PANEL 587LT EXTERNAL SURFACE. PLEA - [SDR UIEA2024040500240](https://openairdocs.org/sdr/UIEA2024040500240), Apr 3, 2024: SKIN. DENTED. DENT- LH OUTBD FORE FLAP OUTBD TOP PNL EXTERNAL WBL 655(

1. PERFORM REPAIR OF DENT SKIN DAMAGE AT L/H WING OUTBD FORE FLAP TOP PANEL EXTERNAL SURFACE. PLEASE - [SDR UIEA2024040500239](https://openairdocs.org/sdr/UIEA2024040500239), Apr 3, 2024: SKIN. DENTED. DENT PANEL 677IT EXTERNAL SURFACE, RH INBD MID FLAP WBL 373.33(

1. PERFORM REPAIR OF DENT SKIN DAMAGE AT R/H WING INBD MID FLAP PANEL 677IT EXTERNAL SURFACE. - [SDR UIEA2024040500238](https://openairdocs.org/sdr/UIEA2024040500238), Apr 3, 2024: SKIN. DENTED. DENT- SKIN, R/H WING INBD MID FLAP PANEL 677IT EXTERNAL SURFACEWBL 374.83(

1. PERFORM REPAIR OF CHAFING SKIN DAMAGE AT R/H WING INBD MID FLAP PANEL 677IT EXTE - [SDR UIEA2024040500237](https://openairdocs.org/sdr/UIEA2024040500237), Apr 3, 2024: SKIN. CHAFED. CHAFING - SKIN PNL, RH WING INBD AILERON OUTBD TE UPPER SKIN WBL 515(

1. PERFORM REPAIR OF CHAFING SKIN DAMAGE AT R/H WING INBD AILERON T/E OUTBD SIDE. PLEASE - [SDR UIEA2023091500833](https://openairdocs.org/sdr/UIEA2023091500833), Sep 14, 2023: TIRE. UNKNOWN. MLG TIRE #6 BLOWOUT DURING LANDING/TOUCHDOWN(

R/R MLG TIRE #6 & #5. ACCOMPLISHED A TIRE TREAD LOSS CONDITIONAL INSPECTION AS PER B747 AMM 05-51-34-201. AP - [SDR UIEA2022102401172](https://openairdocs.org/sdr/UIEA2022102401172), Oct 23, 2022: FAIRING. INFLT SEPARATION. #3 FLAP MOVABLE FAIRING DEPARTED AIRCRAFT ON LANDING RFD(

REMOVED ENTIRE FAIRING. PERFORMED CHAPTER 5 CONDITIONAL INSPECTION 1 AREA OF DAMAGE REPAIRED PER SRM - [SDR UIEA2022100601094](https://openairdocs.org/sdr/UIEA2022100601094), Oct 6, 2022: NONE. NONE. SLOW SPEED REJECTED TAKE OFF DUE TO SINGLE SOURCE CAUTION AURAL WARNING(

REMOVED AND REPLACED LH AND RH AURAL WARNING CARD (PRINTED CIRCUT ASSY - SYNTHESIZER) - [SDR UIEA2022083000927](https://openairdocs.org/sdr/UIEA2022083000927), Sep 29, 2022: NONE. NONE. UPPER DECK EMER LT EXIT SIGN M4717 AT STA 690 L/H EXIT DOOR INOP.(

EMER LT PWR PACK ASSY M5057 REPLACED AND INSTALLATION TEST NORMAL IAW AMM 33-51-00, 33-51-0 - [SDR UIEA2022091200954](https://openairdocs.org/sdr/UIEA2022091200954), Sep 29, 2022: NONE. NONE. LHW I/B FORE FLAP L/E FAIRING FOUND DELAMINATION (3 LOCATION) AT CTR POSITION(

PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM51-70-07 PAR.5A&NBSP;

) - [SDR UIEA2022091200955](https://openairdocs.org/sdr/UIEA2022091200955), Sep 29, 2022: NONE. NONE. LHW-L/H O/B MID FLAP L/E FOUND DELAMINATION (56" APPROX TO EDGE)(

PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM51-70-07 PAR.5A&NBSP;

) - [SDR UIEA2022091200956](https://openairdocs.org/sdr/UIEA2022091200956), Sep 29, 2022: NONE. NONE. LHW-L/H O/B MID FLAP L/E FOUND DELAMINATION (96" APPROX TO EDGE)(

PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM51-70-07 PAR.5A&NBSP;

) All 171: https://openairdocs.org/aircraft/N472MC/reports.md ## STCs that may be installed (OpenAirDocs) (5) 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 engine (GE CF6-80C2B1F) - [STC SE01543CH](https://openairdocs.org/stc/SE01543CH): Replace Hamilton Sundstrand P/N 778839-13, 778839-14, 778839-19, 778839-20, 778839-37, 778839-38, 816682-1, 840618-2, 880724 carbon bushings with Cook Airtomic P/N AIR22947 Slotted Entry Busing in the High Pressure Shutoff Valve. Cook Airtomic - [STC SE01478CH](https://openairdocs.org/stc/SE01478CH): Installation of Cook Airtomic alignment joint p/n AIR 22912. Cook Airtomic - [STC SE01471AT](https://openairdocs.org/stc/SE01471AT): Replace right and left side Rohr, Inc. fire detection harness on GE CF6-80C2 engine. Unison Industries. Lists CF6-80C2 Series - [STC SE00463LA](https://openairdocs.org/stc/SE00463LA): Install fireproof blankets on the engine fan reverser intermediate fireseal, in lieu of fireproof intumescent coating. This STC is jointly by owned by Hi Temp Insulation and MRA Systems acting through Middle River Aircraft Systems, 103 Chesapeake Park Plaza, Baltimore, MD 21220. Hi Temp Insulation Inc - [STC SA2227SO](https://openairdocs.org/stc/SA2227SO): Installation of wiring and associated components for utilization of the Rolls Royce, Inc., ARINC, interface/readers UT1317 or UT1317/1, for the purpose of acquisition, recording, and analysis in real time of engine/aircraft/ systems. (767 SERIES POWERED BY RR RB-11-524 SERIES. Rolls Royce, Inc. Lists CF6-80 Series ## Earlier aircraft with N472MC The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N472MC before. - [Cancelled 2015-08-26](https://openairdocs.org/deregistered/N472MC-2015-08-26): Boeing 747-430, S/N 24288. Owner: [Atlas Air Inc](https://openairdocs.org/faa-owner/ATLAS%20AIR%20INC), [Purchase, NY](https://openairdocs.org/faa-place/NY/Purchase) ## Related - Other Boeing 747-45E aircraft: https://openairdocs.org/model/boeing-747-45e/aircraft.md - The GE CF6-80C2B1F engine: https://openairdocs.org/engine/ge-cf6-80c2b1f.md --- 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.