# N7640U: 1969 Boeing 727-222, registration cancelled 2007-03-14

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: March 14, 2007
- Exported to: Mexico
- Status when cancelled: Valid registration
- Airframe: [Boeing 727-222](https://openairdocs.org/model/boeing-727-222) (registry code 1384073)
- Engine: [Pratt & Whitney JT9D series](https://openairdocs.org/engine/pratt-whitney-jt9d-series) (registry code 52054)
- Data sheets: [TCDS A3WE](https://openairdocs.org/tcds/A3WE) (OpenAirDocs)
- Serial number: 19913
- Year built: 1969
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: February 10, 1969
- Certificate issued: March 6, 2007
- Last registry action: March 6, 2007
- Mode S code: AA52CF
- Owners when cancelled: [Fhe Inc DBA](https://openairdocs.org/faa-owner/FHE%20INC%20DBA), [International Aviation Support](https://openairdocs.org/faa-owner/INTERNATIONAL%20AVIATION%20SUPPORT)
- Location: [Carrollton, TX](https://openairdocs.org/faa-place/TX/Carrollton)
- Owner type: Corporation
- Owner's area on the map: 32.9619° N, 96.8993° W: Placed by OpenAirDocs at the center of ZIP code 75006, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N7640U
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=7640U
- Page: https://openairdocs.org/deregistered/N7640U-2007-03-14

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 727-222: https://openairdocs.org/model/boeing-727-222.md

## Service difficulty reports (65, newest 50)

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

- [SDR C7WA200600007](https://openairdocs.org/sdr/C7WA200600007), Mar 22, 2006: CONTROL BOX. FALSE INDICATION. NR 1 ENGINE FIRE WARNING LIGHT ILLUMINATED SHUTDOWN ENGINE AND RETURNED TO DEPARTURE. REMOVED AND REPLACED NR 1 ENGINE FIRE DETECTION CONTROL BOX OPS CHECK GOOD
- [SDR C7WA200600008](https://openairdocs.org/sdr/C7WA200600008), Mar 22, 2006: CLAMP. LOOSE. NR 1 ENGINE FIRE WARNING LIGHT AND BELL ILLUMINATED IN FLIGHT. PERFORMED ENGINE SHUTDOWN AND RETURNED TO DEPARTURE. INSPECTED ENGINE FOR LEAKS AND DAMAGE. TIGHT
- [SDR C7WA200600003](https://openairdocs.org/sdr/C7WA200600003), Feb 22, 2006: ENGINE. FOD. IN FLIGHT, AT FL 28.0, NR 2 ENGINE COMPRESSOR STALLED. ENGINE WAS IN STABLE OPERATION, NO BLEED AT 1.80 EPR. EPR DROPPED TO 1.4 EGT RUNS 80 TO 100 HOTTER THAN E
- [SDR C7WA200500110](https://openairdocs.org/sdr/C7WA200500110), Jul 23, 2005: OVERHEAT LOOP. GROUNDED. LOWER AFT BODY OVERHEAT LIGHT ON. COMPLETED EMERGENCY PROCEDURE, FOUND IT TO BE NR 2 ENGINE. INSPECTED NUMBER 2 ENGINE FOUND LOOP TOUCHING BLEED AIR DUCT. REPOS
- [SDR C7WA200300077](https://openairdocs.org/sdr/C7WA200300077), Jan 15, 2005: CONNECTOR. DIRTY. AIR RETURN, UPON FLAP RETRACTION ON CLIMB-OUT, NR 1 SLAT FAILED TO RETRACT. CLEANED CONNECTOR IAW 20-80-01, OPS CHECKED FLAPS AND SLATS PER MM 27-80-0. ALL INDI
- [SDR C7WA200400041](https://openairdocs.org/sdr/C7WA200400041), Sep 7, 2004: TRANSMITTER. FROZEN. EXPERIENCED FLAP PROBLEM ON EXTENSION, PERFORMED CHECK LIST. LANDED WITHOUT INCIDENT. FOUND LT IB FLAP POSITION TRANSMITTER FROZEN. REMOVED AND REPLACED TRANSMI
- [SDR C7WA2004000AA](https://openairdocs.org/sdr/C7WA2004000AA), Aug 25, 2004: SWITCH. INOPERATIVE. ENGINE SHUTDOWN: IN CRUISE NR 3 ENGINE START VALVE OPEN LIGHT ILLUMINATED AT THE SAME TIME THE RT DUCT OVERHEAT LIGHT CAME ON. ACCOMPLISHED ASSOCIATED EMERGENCY
- [SDR 2004F00172](https://openairdocs.org/sdr/2004F00172), Feb 4, 2004: ACCESSORY UNIT. FAULTY. ON APPROACH INTO DAY, UNSAFE RIGHT MAIN LANDING GEAR INDICATION. RED LIGHT WAS ILLUMINATED. GEAR WS VISUALLY VERIFIED DOWN BY THE TOWER. ACCOMPLISHED APPROPRIAT
- [SDR 2004F00167](https://openairdocs.org/sdr/2004F00167), Feb 2, 2004: DUCT. CRACKED. ON TAKEOFF ROLL OUT OF ICT, NR 3 ENGINE FIRE WARNING CAME ON. SHUTDOWN NR 3 ENGINE IAW RYAN PROCEDURES AND RETURNED ICT. AIRCRAFT LANDED ICT WITHOUT INCIDENT. R
- [SDR 2004F00110](https://openairdocs.org/sdr/2004F00110), Dec 11, 2003: GENERATOR. FAILED. DURING TAKEOFF FROM BNA, AIRCRAFT LOST NR 3 GENERATOR, EPR WENT TO 1.6 AND OIL PRESSURE FELL TO REDLINE. PERFORMED ENGINE SHUTDOWN PROCEDURES AND DECLARED EMERG
- [SDR 2004F00072](https://openairdocs.org/sdr/2004F00072), Sep 30, 2003: HINGE. CRACKED. AT B-CHECK, FOUND AFT SECTION OF MAIN CARGO DOOR HINGE CRACKED AT AFT END AIRFRAME SIDE. REMOVED CRACKED SECTION OF MAIN CARGO DOOR HINGE. FABRICATE, TREAT, PRI
- [SDR 2004F00057](https://openairdocs.org/sdr/2004F00057), Sep 30, 2003: ANGLE. CRACKED. AT B-CHECK, FOUND NR 2 SPOILER ACTUATOR IB MOUNT BRACKET CRACKED. REMOVED AND REPLACED NR 2 SPOILER ACTUATOR IB MOUNT BRACKET. RIGG AND LEAK CHECKED NORMAL. (M)
- [SDR RYN2004F00027](https://openairdocs.org/sdr/RYN2004F00027), Sep 16, 2003: MODULE. FAILED. AFTER TAKEOFF, RETRACTED FLAPS AND RECEIVED AN A-HYDRAULIC LOW PRESSURE INDICATION AT FLIGHT ENGINEER PANEL AND PILOTS FWD PANEL. FOLLOWED HYDRAULIC LOSS PROCED
- [SDR 2003F00420](https://openairdocs.org/sdr/2003F00420), Mar 14, 2003: FLOOR SUPPORT. DENTED. AT C-CHECK, FOUND DENT ON AFT CARGO FLOOR SUPPORT, STATION 950F, RBL 17. FABRICATE REPAIR DOUBLER AND FILLER. TREATED AND PRIMED PARTS AND AREA. INSTALLED DOUBL
- [SDR 2003F00419](https://openairdocs.org/sdr/2003F00419), Mar 14, 2003: FRAME. CRACKED. AT C-CHECK, FOUND CRACK ON FORWARD CARGO FRAME AT BS 660, STRINGER 23R/24R. FABRICATE REPAIR ANGLE. TREATED, PRIMED AND INSTALLED REPAIR ANGLE ON FORWARD CARGO 
- [SDR 2003F00417](https://openairdocs.org/sdr/2003F00417), Mar 14, 2003: FRAME. CRACKED. AT C-CHECK, FOUND CRACK ON FORWARD CARGO FRAME AT BS 680, STRINGER 23R/24R. FABRICATED REPAIR. TREATED, PRIMED AND INSTALLED REPAIR ON FORWARD CARGO FRAME STATI
- [SDR 2003F00413](https://openairdocs.org/sdr/2003F00413), Mar 14, 2003: FLOOR SUPPORT. DENTED. AT C-CHECK, FOUND DENT ON AFT CARGO FLOOR SUPPORT, STATION 950F, RBL 13. FABRICATED REPAIR DOUBLER AND FILLER. TREATED AND PRIMED PARTS AND AREA. INSTALLED REPA
- [SDR 2003F00412](https://openairdocs.org/sdr/2003F00412), Mar 14, 2003: FLOOR SUPPORT. DENTED. AT C-CHECK, FOUND DENT ON AFT CARGO FLOOR SUPPORT, STATION 950F, RBL 9. FABRICATE REPAIR DOUBLER AND FILLER. TREATED AND PRIMED PARTS AND AREA. INSTALLED DOUBLE
- [SDR 2003F00410](https://openairdocs.org/sdr/2003F00410), Mar 14, 2003: ACCESS PANEL. CRACKED. AT C-CHECK, FOUND CRACK ON RIGHT WING, NR 6 SLAT LOWER ACCESS PANEL NR 6589. FABRICATED NEW PANEL. ALODINED, PRIMED AND INSTALLED NEW ACCESS PANEL AT RIGHT LOWE
- [SDR 2003F00409](https://openairdocs.org/sdr/2003F00409), Mar 14, 2003: BRACKET. BROKEN. AT C-CHECK, FOUND NR 6 SLAT INBOARD FIXED LEADING EDGE CAVITY STOP BRACKET BROKEN. REPLACD NR 6 SLAT INBOARD FIXED LEADING EDGE CAVITY STOP BOLT BRACKET. (M)
- [SDR 2003F00405](https://openairdocs.org/sdr/2003F00405), Mar 14, 2003: FRAME. CRACKED. AT C-CHECK, FOUND DENT ON FORWARD CARGO FRAME AT BS 720A, STRINGER 24L. FABRICATED REPAIR ANGLE. TREATED, PRIMED AND INSTALLED REPAIR ANGLE ON FORWARD CARGO FRA
- [SDR 2003F00404](https://openairdocs.org/sdr/2003F00404), Mar 14, 2003: FRAME. CRACKED. AT C-CHECK, FOUND DENTS ON FORWARD CARGO FRAME AT BS 700, STRINGER 24L/25L. FABRICATED REPAIR. TREATED, PRIMED AND INSTALLED REPAIR ON FORWARD CARGO FRAME STATI
- [SDR 2003F00403](https://openairdocs.org/sdr/2003F00403), Mar 14, 2003: FLOOR SUPPORT. DENTED. AT C-CHECK, FOUND DENT ON AFT CARGO COMPARTMENT FLOOR SUPPORT, STATION 950E, LBL 10. FABRICATED REPAIR DOUBLER AND FILLER. TREATED AND PRIMED PARTS AND AREA. IN
- [SDR 2003F00401](https://openairdocs.org/sdr/2003F00401), Mar 14, 2003: PANEL. CRACKED. AT C-CHECK, FOUND CRACK ON RIGHT WING, OUTBOARD TRAILING EDGE WING FIXED PANEL INBOARD ATTACH BRACKET. FABRICATED BRACKET. TREATED, PRIMED AND INSTALLED BRACKET
- [SDR 2003F00397](https://openairdocs.org/sdr/2003F00397), Mar 14, 2003: FLOORBEAM. CRACKED. AT C-CHECK, FOUND CRACK ON AFT CARGO FLOORBEAM AT STATION 950B, BL 0. FABRICATE NEW ANGLE. TREATED, PRIMED AND INSTALLED NEW ANGLE AT STATION 950B BL 0. (M)
- [SDR 2003F00418](https://openairdocs.org/sdr/2003F00418), Mar 13, 2003: STRINGER CLIP. CRACKED. AT C-CHECK, FOUND CRACKED STRINGER CLIP AT STAITON 540, STRINGER 5R. FABRICATE NEW ATTACH CLIP. TREATED, PRIMED AND INSTALLED NEW STRINGER TO FRAME ATTACH CLIP 
- [SDR 2003F00416](https://openairdocs.org/sdr/2003F00416), Mar 13, 2003: FRAME. CRACKED. AT C-CHECK, OFUND CRACK ON LOWER LEFT PANEL MOUNT FRAME AT LOWER END, BS 720. FABRICATE REPAIR ANGLE. ALODINED, PRIMED AND INSTALLED NEW ANGLE AT LOWER LEFT PAN
- [SDR 2003F00415](https://openairdocs.org/sdr/2003F00415), Mar 13, 2003: SKIN. CRACKED. AT C-CHECK, FOUND CRACK ON OUTER SKIN OF CO-PILOT WINDOW POST AT BS 203. FABRICATE DOUBLER REPAIR. ALODINED, PRIMED AND INSTALLED REPAIR DOUBLER ON OUTER SKIN O
- [SDR 2003F00414](https://openairdocs.org/sdr/2003F00414), Mar 13, 2003: FAIRING. CRACKED. AT C-CHECK, FOUND CRACK ON LEFT AIR CONDITIONING BAY FAIRING BELOW TAXI LIGHT. CUT OUT CRACKED SECTION AND INSTALLED DOUBLER AT LEFT AIR CONDITIONING BAY FAIRIN
- [SDR 2003F00402](https://openairdocs.org/sdr/2003F00402), Mar 13, 2003: CLIP. CRACKED. AT C-CHECK, FOUND CRACKED STRINGER FRAME ATTACH CLIP AT STATION 570, STRINGER 5R. FABRICATE NEW ATTACH CLIP. TREATED, PRIMED AND INSTALLED NEW ATTACH CLIP AT ST
- [SDR 2003F00400](https://openairdocs.org/sdr/2003F00400), Mar 13, 2003: CLIP. CRACKED. AT C-CHECK, FOUND CRACKED STRINGER CLIP AT STATION 720, STRINGER 3L. FABRICATE NEW ATTACH CLIP. TREATED, PRIMED AND INSTALLED NEW STRINGER TO FRAME ATTACH CLIP 
- [SDR 2003F00399](https://openairdocs.org/sdr/2003F00399), Mar 13, 2003: CLIP. CRACKED. AT C-CHECK, FOUND CRACKED STRINGER CLIP AT STATION 720C, STRINGER 5R. FABRICATE NEW ATTACH CLIP. TREATED, PRIMED AND INSTALLED NEW STRINGER TO FRAME ATTACH CLIP
- [SDR 2003F00398](https://openairdocs.org/sdr/2003F00398), Mar 13, 2003: CLIP. CRACKED. AT C-CHECK, FOUND CRACKED STRINGER CLIP AT STATION 720A, STRINGER 5L. FABRICATE NEW ATTACH CLIP. TREATED, PRIMED AND INSTALLED NEW ATTACH CLIP AT STATION 720A S
- [SDR 2003F00422](https://openairdocs.org/sdr/2003F00422), Mar 13, 2003: STRINGER CLIP. CRACKED. AT C-CHECK, FOUND CRACKED STRINGER CLIP AT STATION 720E, STRINGER 5L. FABRICATE NEW ATTACH CLIP. TREATED, PRIMED AND INSTALLED NEW STRINGER TO FRAME ATTACH CLIP
- [SDR 2003F00421](https://openairdocs.org/sdr/2003F00421), Mar 13, 2003: DUCT. CRACKED. AT C-CHECK, FOUND CRACK ON HEATING AND AIR CONDITIONING DUCT AT BS 720E/D, STRINGER 12/13. STOP DRILLED CRACKS. FABRICATED DOUBLER. ALODINED, PRIMED AND INSTALL
- [SDR 2003F00441](https://openairdocs.org/sdr/2003F00441), Mar 12, 2003: FRAME. CRACKED. AT C-CHECK, FOUND INDICATION OF CRACK AT TERMINAL HOLE FITTING, BS 870. STOP DRILLED CRACK AT SECOND FASTENER ROW, SECOND FASTENER DOWN FROM STRINGER 9R ON BS 8
- [SDR 2003F00440](https://openairdocs.org/sdr/2003F00440), Mar 12, 2003: SKIN. CRACKED. AT C-CHECK, FOUND FORWARD GALLEY DOOR CUTOUT, LOWER AFT CORNER SKIN CRACKED. STOPPED DRILLED CRACKS ON RIGHT FORWARD GALLEY DOOR CUTOUT, LOWER AFT CORNER SKIN. 
- [SDR 2003F00439](https://openairdocs.org/sdr/2003F00439), Mar 12, 2003: FRAME. CRACKED. AT C-CHECK, FOUND TIE FRAME TO FUSELAGE CRACKED AT STATION 680, STRINGER 17L. FABRICATED ANGLE REPAIR. ALODINED, PRIMED AND INSTALLED ANGEL REPAIR ON BS 680, ST
- [SDR 2003F00429](https://openairdocs.org/sdr/2003F00429), Mar 12, 2003: SKIN. CRACKED. AT C-CHECK, FOUND FORWARD GALLEY DOOR CUTOUT LOWER FORWARD CORNER SKIN CRACKED. STOP DRILLED CRACK ON RIGHT FORWARD GALLEY DOOR CUTOUT, FORWARD, LOWER CORNER SK
- [SDR 2003F00493](https://openairdocs.org/sdr/2003F00493), Mar 10, 2003: SKIN. CRACKED. AT C-CHECK, FOUND CRACK ON LEADING EDGE WING SKIN AT NR 5 OUTBOARD SLAT TRACK. STOP DRILLED CRACK. FABRICATED DOUBLER. ALODINED AND PRIMED AREA REPAIR DOUBLER. 
- [SDR 2003F00458](https://openairdocs.org/sdr/2003F00458), Mar 10, 2003: SKIN. CRACKED. AT C-CHECK, FOUND CRACK AT RT WING LEADING EDGE ABOVE NR 5 INBOARD SLAT TRACK LEADING EDGE CUTOUT UPPER RADIUS. STOP DRILLED CRACK AT RIGHT WING LEADING EDGE NR
- [SDR 2003F00457](https://openairdocs.org/sdr/2003F00457), Mar 10, 2003: PANEL. CRACKED. AT C-CHECK, FOUND CRACK AT LEFT ELEVATOR BALANCE BAY PANEL 9720. ROUTED CRACKED AREA ON LT ELEVATOR BALANCE PANEL NR 9720. TREATED, PRIMED AND INSTALLED REPAIR 
- [SDR 2003F00449](https://openairdocs.org/sdr/2003F00449), Mar 10, 2003: RETAINER. CRACKED. AT C-CHECK, FOUND CRACK AT RIGHT WING NR 5 SLAT OUTBOARD SEAL RETAINER. REMOVED AND REPLACED RIGHT WING NR 5 SLAT, OUTBOARD HOOK SEAL, UPPER LEADING EDGE WING, 
- [SDR 2003F00448](https://openairdocs.org/sdr/2003F00448), Mar 10, 2003: PLATE. CRACKED. AT C-CHECK, FOUND CRACK AT NR 6 SLAT LOWER BACKSIDE ACTUATOR ROD END ACCESS CUTOUT SUPPORT PLATE. REMOVED DAMAGED PLATE FROM RIGHT WING NR 6 SLATE LOWER BACKSID
- [SDR 2003F00436](https://openairdocs.org/sdr/2003F00436), Mar 10, 2003: RETAINER. CRACKED. AT C-CHECK, FOUND CRACK AT NR 5 SLAT, INBOARD HOOK SEAL CUTOUT, OUTBOARD SEAL RETAINER. REMOVED AND REPLACED NR 5 SLAT INBOARD HOOK SEAL, UPPER LEADING EDGE, OU
- [SDR 2003F00435](https://openairdocs.org/sdr/2003F00435), Mar 10, 2003: BRACKET. CRACKED. AT C-CHECK, FOUND CRACK AT NR 6 SLATE ACTUATOR SUPPORT BRACKET. ACCOMPLISHED AN HFEC INSPECTION ON RIGHT WING NR 6 SLAT ACTUATOR OUTBOARD MOUNT BRACKET. NO CRAC
- [SDR 2003F00430](https://openairdocs.org/sdr/2003F00430), Mar 10, 2003: ANGLE. CRACKED. AT C-CHECK, FOUND STRUCTURE CRACKED, NOSE WHEEL WELL AT BS 294.5, LBL 12 RT, WL 177. STOP DRILLED CRACKS. FABRICATED FORMED ANGLE REPAIRS AND STRAPS. TREATED, P
- [SDR 2003F00433](https://openairdocs.org/sdr/2003F00433), Mar 9, 2003: SKIN. BURNED. AT C-CHECK, FOUND STATIC DISCHARGE BURN, RIGHT ELEVATOR OUTBOARD TRAILING EDGE CORNER. CUT OUT DAMAGED AREA ON RIGHT ELEVATOR OUTBOARD TRAILING EDGE CORNER. FAB
- [SDR 2003F00427](https://openairdocs.org/sdr/2003F00427), Mar 9, 2003: FRAME. CRACKED. AT C-CHECK, FOUND TIE FRAME CRACKED AT BS 480, STRINGER 17L. FABRICATED REPAIR ANGLES. TREATED AND PRIMED FABRICATED REPAIR ANGLES. INSTALLED AT STATION 480, ST
- [SDR 2003F00446](https://openairdocs.org/sdr/2003F00446), Mar 8, 2003: BRACKET. CRACKED. AT C-CHECK, FOUND CRACK AT LT WING LOWER TRAILING EDGE PANEL SUPPORT BRACKET, OUTBOARD OF NR 2 SPOILER ACTUATOR. REMOVED AND REPLACED BRACKET ON LEFT WING LOWER

All 65: https://openairdocs.org/deregistered/N7640U-2007-03-14/reports.md

## 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 DCA84AA025](https://openairdocs.org/ntsb/DCA84AA025), May 31, 1984: Boeing 727-222 (N7640U), Denver, CO, substantial damage

## FAA accident and incident reports (3)

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 19920414018129I](https://openairdocs.org/incident/19920414018129I), Apr 14, 1992: Boeing 727222 (N7640U), Allentown, PA, Minor damage. Aircraft hit jetway on departure from gate. Marshaller and wing walker tried to signal pilot.
- [Incident 19870102013249I](https://openairdocs.org/incident/19870102013249I), Jan 2, 1987: Boeing 727222 (N7640U), Akron, OH. During taxi the left main departed pavement and the aircraft became stuck in the mud.
- [Incident 19790318008769I](https://openairdocs.org/incident/19790318008769I), Mar 18, 1979: Boeing 727222 (N7640U), Seattle, WA. Pressurization surged in flight. Replaced emergency relief valves.

## Other aircraft with N7640U

- [Registered now](https://openairdocs.org/aircraft/N7640U): Cirrus Design SR20, S/N 10561, built 2025

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