# N528MC: 1984 Boeing 747-2D7B, registration cancelled 2013-04-30

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: April 30, 2013
- Status when cancelled: Registration expired, pending cancellation
- Airframe: [Boeing 747-2D7B](https://openairdocs.org/model/boeing-747-2d7b) (registry code 1384803)
- 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: 22472
- Year built: 1984
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, normal
- Airworthiness date: June 23, 2004
- Certificate issued: September 5, 2006
- Last registry action: September 15, 2009
- Mode S code: A6A7BC
- 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/N528MC
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=528MC
- Page: https://openairdocs.org/deregistered/N528MC-2013-04-30

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 747-2D7B: https://openairdocs.org/model/boeing-747-2d7b.md

## Service difficulty reports (63, newest 50)

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

- [SDR UIEA200800281](https://openairdocs.org/sdr/UIEA200800281), Aug 3, 2008: RELIEF VALVE. LEAKING. AT CRUISE NR 4 ENG HAD MULTPLE FIRE WARNINGS ON BOTH A&B. PERFORMED IN FLIGHT SHUT DOWN AND AIR TURNBACK. MAINTENANCE FOUND LEAKING PRESSURE RELIEF VALVE, WHICH
- [SDR UIEA200800169](https://openairdocs.org/sdr/UIEA200800169), May 5, 2008: SHEAR PIN. BROKEN. AIR TURN BACK, SIDE CARGO DOOR LIGHT ILLUMINATED DURING TAKEOFF ROLL. RETURNED TO BLOCKS PER FHB. FOUND OUTSIDE MASTER LATCH LOCK HANDLE SHEAR PIN BROKEN. REMOV
- [SDR UIEA200800163](https://openairdocs.org/sdr/UIEA200800163), May 1, 2008: REGULATOR VALVE. LEAKING. NR 1 ENGINE FULL POWER TAKEOFF ON CLIMB-OUT BOTH A/B LOOPS REACHED 3.0. AFTER POWER REDUCTION BOTH LOOPS CAME BACK DOWN TO 2.0. REST OF FLIGHT WAS OK. OPENED CO
- [SDR UIEA200800114](https://openairdocs.org/sdr/UIEA200800114), Apr 7, 2008: SKIN PANEL. CORRODED. EVIDENCE OF CORROSION UNDER LAP JOINT STRINGER 46 RIGHT, BETWEEN STA 1737-1745. INTERIM REPAIR ACCOMPLISHED IAW SRM 53-30-03 FIG 17 TABLE LLL WITH INITIAL INSPE
- [SDR UIEA200800113](https://openairdocs.org/sdr/UIEA200800113), Apr 7, 2008: SKIN. DELAMINATED. RIGHT WING INBOARD SPOILER UPPER SURFACE HAS DELAMINATION WBL 235.150. REMOVED NR 7 GROUND SPOILER IAW MM 27-62-01. REPAIRED DELAMINATION IAW SRM 51-40-20. INST
- [SDR UIEA200800042](https://openairdocs.org/sdr/UIEA200800042), Feb 13, 2008: RADOME. DAMAGED. AIRCRAFT WAS HIT BY LIGHTNING STRIKE. ENTRANCE AT THE RADOME. NO COMMUNICATIONS OR NAV FAILURES REPORTED BY CREW. FOUND RADOME DAMAGED BY LIGHTNING STRIKE. FOUN
- [SDR UIEA200700352](https://openairdocs.org/sdr/UIEA200700352), Sep 5, 2007: WEB. CRACKED. OLEO 1450 FWD CRACKED JUST FWD OF NR 25 V/C FLAP UPPER FITTING. CARRY OUT REPAIR AS PER SRM 51-40-03.
- [SDR UIEA200700349](https://openairdocs.org/sdr/UIEA200700349), Sep 5, 2007: NOZZLE. DENTED. NR 1 ENGINE EXHAUST NOZZLE DENTED AT 0300. NDT CHECKED NIL CRACK DENT AREA WITHIN LIMITS AMM 78-11-01 PAGE 601.
- [SDR UIEA200700347](https://openairdocs.org/sdr/UIEA200700347), Sep 5, 2007: WEB. CRACKED. UPON L/E CAP REMOVAL OLES 1522, NR 26VC FLAP UPPER STOP FTG FWD WEB DOUBLER FOUND CRACKED. DOUBLER REPLACED IAW SRM 51-10-01.
- [SDR UIEA200700346](https://openairdocs.org/sdr/UIEA200700346), Sep 5, 2007: FRAME. CRACKED. R1 MED LOWER AFT CORNER FRAME CRACKED AT STA 490 RT S-25R TO S-26R AREA. C/OUT AS PER SRM 52-10-02 FIG 10.
- [SDR UIEA200700345](https://openairdocs.org/sdr/UIEA200700345), Sep 5, 2007: DOOR FRAME. CRACKED. M/D R4 MED FWD UPPER CORNER FRAME CRACKED AT STA 1670 S-16R TO S-17R AREA. CARRY OUT REPAIR AS PER SRM 52-10-02, FIG 10.
- [SDR UIEA200700344](https://openairdocs.org/sdr/UIEA200700344), Sep 5, 2007: DOOR FRAME. CRACKED. R3 DOOR FWD UPPER CORNER FRAME FOUND CRACKED. C/OUT AS PER SRM 52-10-02, FIG 10.
- [SDR UIEA200700343](https://openairdocs.org/sdr/UIEA200700343), Sep 5, 2007: WEB. CORRODED. BULK CARGO BS 1980-2030 DOOR LOWER SILL FLOOR WEB, CORRODED. CORROSION REMOVED AND REPROTECTED AS PER SRM 51-10-01 AND SRM 51-10-02 WITHIN ALLOWABLE LIMIT AS PE
- [SDR UIEA200700342](https://openairdocs.org/sdr/UIEA200700342), Sep 5, 2007: PANEL. CONTAMINATED. RT WING I/B T/E PANEL FOUND WATER. REPLACE RHW I/B T/E PANEL AS PER SRM 51-10-01 AND SRM 51-30-02.
- [SDR UIEA200700348](https://openairdocs.org/sdr/UIEA200700348), Sep 5, 2007: FRAME. CRACKED. AFT REMOVAL OF L/E NOSE CAP FOUND THAT "D" SECTION CRACKED. CARRY OUT REPAIR AS PER SRM 57-20-03.
- [SDR UIEA200700350](https://openairdocs.org/sdr/UIEA200700350), Sep 5, 2007: NOZZLE. DENTED. NR 3 ENGINE EXHAUST NOZZLE EXTERIOR SKIN DENTED AT 0900. NDT CHECKED NIL CRACK DENT AREA WITHIN LIMIT AMM 78-11-01 PAGE 601.
- [SDR UIEA200700351](https://openairdocs.org/sdr/UIEA200700351), Sep 5, 2007: NOZZLE. DENTED. NR 4 ENGINE EXHAUST NOZZLE EXTERIOR SKIN DENTED AT 0700 TO 0900. NDT CHECKED NIL CRACK DENT AREA WITHIN LIMIT AMM 78-11-01 PAGE 601.
- [SDR UIEA200700336](https://openairdocs.org/sdr/UIEA200700336), Aug 31, 2007: ACCESS PANEL. ELONGATED. AIR COND, BAY ACCESS PANEL 192ER EXT SURFACE FOUND SKIN ELONGATION. AIR COND BAY ACCESS PANEL 192ER REPAIRED WITH PRE-PRED FABRIC AS PER MESSAGE NR 1-497468248-
- [SDR UIEA200700329](https://openairdocs.org/sdr/UIEA200700329), Aug 31, 2007: FRAME. CRACKED. BS 800 S17 LT ONE FASTENER HOLE FOUND CRACK ON FWD INNER CHORD ANGLE. REPLACEMENT PER BOEING CONTROL NO PO24708.
- [SDR UIEA200700337](https://openairdocs.org/sdr/UIEA200700337), Aug 31, 2007: ACCESS PANEL. DELAMINATED. AIR COND, BAY ACCESS PANEL 192HR EXT SURFACE FOUND SKIN DELAMINATION. AIR COND BAY ACCESS PANEL 192HR REPAIRED WITH PRE-PRED FABRIC AS PER MESSAGE NR 1-49746824
- [SDR UIEA200700335](https://openairdocs.org/sdr/UIEA200700335), Aug 31, 2007: ACCESS PANEL. ERODED. AIR COND, BAY ACCESS PANEL 191HL EXT SURFACE FOUND ERODED. AIR COND BAY ACCESS PANEL 191HL REPAIRED WITH PRE-PRED FABRIC AS PER MESSAGE NR 1-497468248-2.
- [SDR UIEA200700332](https://openairdocs.org/sdr/UIEA200700332), Aug 31, 2007: FLOORBEAM. CRACKED. FLOOR STRUCTURE BEAM WEB CRACKED. C/OUT AS PER BOEING MESSAGE NR 1-497681686-1.
- [SDR UIEA200700338](https://openairdocs.org/sdr/UIEA200700338), Aug 31, 2007: TORQUE LINK. CHAFED. NLG LOWER TORSION LINK FOUND CHAFING. BLEND OUT THE CHAFING AREA WITH MIN 20-1 BLEND-RATIO.
- [SDR UIEA200700331](https://openairdocs.org/sdr/UIEA200700331), Aug 31, 2007: SKIN. DENTED. HORIZONTAL STAB RT I/B ELEVATOR L/E UPPER SKIN DENTED. REPAIRED IAW BOEING MESSAGE SR 1-514407012.
- [SDR UIEA200700333](https://openairdocs.org/sdr/UIEA200700333), Aug 31, 2007: FLOORBEAM. CRACKED. FLOOR STRUCTURE BEAM WEB CRACKED. REPAIRED IAW BOEING MESSAGE NR 1-497681686-1.
- [SDR UIEA200700339](https://openairdocs.org/sdr/UIEA200700339), Aug 31, 2007: SKIN. DENTED. FX EXTERIOR SKIN DENT AS MARKED APPR, 1" SQ IN AT BS 780 S47-R. REINSTALLED A REPAIRED DOUBLER AS PER SRM 53-30-03 DETAILS AS PER SWS SHOWN.
- [SDR UIEA200700334](https://openairdocs.org/sdr/UIEA200700334), Aug 31, 2007: PAN. CRACKED. COCKPIT 2ND OBSERVER SEAT PAN CRACKED. REPAIRED IAW BOEING MESSAGE NR 1-497681686-1.
- [SDR UIEA200700340](https://openairdocs.org/sdr/UIEA200700340), Aug 31, 2007: HINGE FITTING. CRACKED. BS 2598 H/S RT RBL 40" REAR SPAR UPPER I/B OF HINGE FITTING OPEN HOLE. OVERSIZE TO 0.403", USED BACB30 US6K21Y BOLT. CARRIED OUT NDT TEST OF THE OPEN OVERSIZE H
- [SDR UIEA200700330](https://openairdocs.org/sdr/UIEA200700330), Aug 31, 2007: PANEL. CONTAMINATED. LT WING T/E I/B PANEL FOUND WATER. REPLACE LHW T/E I/B FIXED PAL AS PER SRM 51-10-01 AND SRM 51-30-02, AND PANEL REPAIR IAW BOEING MESSAGE 31-516595696-1 TO 1-5
- [SDR UIEA200700260](https://openairdocs.org/sdr/UIEA200700260), Jul 8, 2007: UNKNOWN. ODOR. AT DEPARTURE SMOKE AND BURNING ODOR IN COCKPIT, ELECTRICAL ODOR. PULLED C/BS FOR T/R UNITS, SMOKE AND ODOR STOPPED. WIRE BUNDLES AND AREA BELOW F/E PANEL (4) IN
- [SDR UIEA200700259](https://openairdocs.org/sdr/UIEA200700259), Jul 3, 2007: SEAL. LOOSE. L-3 WINDOW SEAL LIFTING IN THE WIND WITH EXCESSIVE COCKPIT NOISE. ALSO, DURING LEVEL FLIGHT APPROX TIME 1335Z FL 31.0 TEMP -09 TAT HEARD BANG AIRCRAFT SHOOK, PO
- [SDR UIEA200700255](https://openairdocs.org/sdr/UIEA200700255), Jun 21, 2007: PANEL. CORRODED. LOWER FUSELAGE CENTER PANELS 191HH AND 191JJ BETWEEN NR 1 AND NR 3 ACM'S HAVE AREA OF CORROSION. PERMANENT REPAIR WAS ACCOMPLISHED AS PER 747-200 SRM 51-40-02 F
- [SDR UIEA200700252](https://openairdocs.org/sdr/UIEA200700252), Jun 21, 2007: FAIRING. DAMAGED. RT WING, NR 8 FLAPTRACK FORWARD FIXED FAIRING HAS SEVERAL SMALL HOLES AT LEADING EDGE AREA. ACCOMPLISHED PERMANENT REPAIR AS PER 747-200 SRM 51-40-09, FIG 6, TA
- [SDR UIEA200700254](https://openairdocs.org/sdr/UIEA200700254), Jun 21, 2007: SUPPORT. CORRODED. LOWER FUSELAGE AIR CONDITIONING ACCESS DOOR AREA, BELOW KEEL BEAM BOX, EXTERIOR CENTER PANEL SUPPORT EXTRUSION HAS CORROSION. PERMANENT REPAIR WAS ACCOMPLISHED 
- [SDR UIEA200700251](https://openairdocs.org/sdr/UIEA200700251), Jun 21, 2007: FAIRING. CRACKED. RT WING NR 7 FLAP TRACK CANOE FAIRING DAMAGED AT LOWER SIDE, AFT OF ACCESS PANEL 667CB. ACCOMPLISHED PERMANENT REPAIR AS PER 747-200 SRM 51-40-09, FIG 6 TABLE I
- [SDR UIEA200700253](https://openairdocs.org/sdr/UIEA200700253), Jun 21, 2007: SKIN. DELAMINATED. NR 4 ENGINE RT REVERSER AT NAC STATION 206.10 UPPER SIDEWALL SKIN DELAMINATED. PERMANENT REPAIR WAS ACCOMPLISHED AS PER CF6-50 ENGINE MANUAL 78-32-03, REPAIR NR
- [SDR UIEA200700148](https://openairdocs.org/sdr/UIEA200700148), Apr 8, 2007: SKIN. CRACKED. FUSELAGE SKIN HAS 12" CRACK FROM STA 2650 TO 2658 ON RIGHT SIDE OF AIRCRAFT BETWEEN STRINGERS 11R AND 13R. FOUND CRACKED IN A SEMI-CIRCULAR SHAPE. REPAIRED PER 
- [SDR UIEA200700068](https://openairdocs.org/sdr/UIEA200700068), Feb 5, 2007: ALTIMETER. FAULTY. CAPT ALT UNRESPONSIVE TO ALL CHANGE BOTH CADC/STBY MODES, PERFORMED CHECK DIFFERENCE BETWEEN ALT INDICATORS (3,34,7), CHANGE ALT LAGS IN DESCENT BY OVER 300' AN
- [SDR UIEA200700066](https://openairdocs.org/sdr/UIEA200700066), Feb 4, 2007: CADC. STICKING. DURING CLIMB CAPT ALTIMETER NEEDLE WOULD STICK IN POSITION CAUSING PULL-UP TERRAIN WARNINGS, DON’T SINK WARNING AUDIBLES, ALTIMETER READ 37.0, ATC 36.8. PERFORM
- [SDR UIEA200700065](https://openairdocs.org/sdr/UIEA200700065), Feb 3, 2007: ALTIMETER. STICKING. DURING CLIMB CAPT'S ALTIMETER NEEDLE WOULD STICK IN POSITION CAUSING PULL-UP TERRAIN WARNING, DON'T SINK WARNING AUDIBLES. CAPT'S ALTIMETER REMOVED AND REPLACED
- [SDR UIEA200700026](https://openairdocs.org/sdr/UIEA200700026), Jan 27, 2007: PANEL. CRACKED. LT WING PYLON GAP PANEL AT ILES 640.47 HAS A 3.0 INCH CRACK. ACCOMPLISHED PERMANENT REPAIR AS PER 747 SRM 51-40-09 FIG 18 SHEET 5 AND SRM 51-40-12, ALSO REFEREN
- [SDR UIEA200700027](https://openairdocs.org/sdr/UIEA200700027), Jan 27, 2007: PANEL. CRACKED. LT WING UPPER FIXED PANEL, 12 INCHES FROM FORWARD EDGE OF NR 5 SPOILER, WBL 421.00 HAS A 6.0 INCH CRACK. ACCOMPLISHED PERMANENT REPAIR AS PER 747 SRM 51-40-09 F
- [SDR UIEA200600290](https://openairdocs.org/sdr/UIEA200600290), Nov 15, 2006: SKIN. PUNCTURED. NR 21 LEADING EDGE DEVICE FOLDING NOSE FOUND DAMAGED ON ARRIVAL. NOSE HINGE ARM FOUND BROKEN AND SKIN PUNCTURED. UNABLE TO CONCLUSIVELY DETERMINE THE REASON FOR
- [SDR UIEA200600158](https://openairdocs.org/sdr/UIEA200600158), Jul 2, 2006: DUCT. RUPTURED. FOLLOWING TAKEOFF NR 4 ENG FIRE INDICATIONS NACELLE TEMPS A/B HIGH, THEN TO FIRE "F" AND FULL WARNING ENG NR 4 SHUTDOWN AS PER CHECKLIST. NR 4 ENG FIRE BOTTLE "
- [SDR UIEA200700256](https://openairdocs.org/sdr/UIEA200700256), Jun 21, 2006: SKIN. DENTED. NR 4 ENGINE LT REVERSER HAS DENT ON UPPER SIDE OF TRANSLATING COWL AT NAC STATION 224.6. PERMANENT REPAIR WAS ACCOMPLISHED AS PER CF6-50 ENGINE MANUAL 78-32-01,
- [SDR UIEA200600131](https://openairdocs.org/sdr/UIEA200600131), Jun 13, 2006: HYDRAULIC LINE. CRACKED. DURING CLIMB NR 4 HYD SYSTEM STARTED DECREASING AND LOW QUANTITY LIGHT CAME ON. FHB PROCEDURES C/W AND QUANTITY WAS STILL DECREASING. ENG PUMP SWITCH WAS POSITI
- [SDR UIEA200600136](https://openairdocs.org/sdr/UIEA200600136), Jun 11, 2006: START VALVE. DAMAGED. NR4 ENGINE SHUT DOWN AT 1945Z DUE TO NR 4 START VALVE ENGINE LIGHT FLICKERING AND THEN COMING ON. REMOVED AND REPLACED NR 4 START VALVE AS PER AMM 80-11-04. PER
- [SDR UIEA200600121](https://openairdocs.org/sdr/UIEA200600121), May 26, 2006: SEAL. DAMAGED. ACCOMPLISHED AIR TURNBACK DUE TO LOSS OF ALL OIL IN ENGINE NR 1, DURING CLIMBOUT. FOLLOWED SHORTLY BY A DROP IN OIL PRESSURE INTO THE MID TO LOWER AMBER BAND. F
- [SDR UIEA200600127](https://openairdocs.org/sdr/UIEA200600127), May 24, 2006: RELIEF VALVE. LEAKING. AT 3000 FT DURING CLIMBOUT FIRE DETECTION LIGHT ON PILOT'S CENTER ANNUNCIATOR PANEL ILLUMINATED, FOLLOWED SHORTLY BY A FIRE INDICATION ON NR 1 ENGINE. FIRE CAUS
- [SDR UIEA200600006](https://openairdocs.org/sdr/UIEA200600006), Feb 14, 2006: PANEL. MISSING. ON WALKAROUND FOUND NR 1 ENGINE LOWER ACCESS PANEL MISSING.

All 63: https://openairdocs.org/deregistered/N528MC-2013-04-30/reports.md

## Other aircraft with N528MC

- [Registered now](https://openairdocs.org/aircraft/N528MC): Canadair CL-600-2B16, S/N 5328, built 1996

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