# N750US: 1978 Boeing 727-214, registration cancelled 2010-02-03

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: February 3, 2010
- Exported to: Brazil
- Status when cancelled: Valid registration
- Airframe: [Boeing 727-214](https://openairdocs.org/model/boeing-727-214) (registry code 138407R)
- Engine: [Pratt & Whitney JT8D-9 series](https://openairdocs.org/engine/pratt-whitney-jt8d-9-series) (registry code 52048)
- Data sheets: [TCDS A3WE](https://openairdocs.org/tcds/A3WE), [TCDS E2EA](https://openairdocs.org/tcds/E2EA) (OpenAirDocs)
- Serial number: 21512
- Year built: 1978
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-jet
- Airworthiness: Standard, transport
- Airworthiness date: May 16, 1978
- Certificate issued: August 8, 2007
- Last registry action: August 8, 2007
- Mode S code: AA1BDC
- Owner when cancelled: [Airlease International Inc](https://openairdocs.org/faa-owner/AIRLEASE%20INTERNATIONAL%20INC)
- Location: [Hot Springs, AR](https://openairdocs.org/faa-place/AR/Hot%20Springs)
- Owner type: Corporation
- Owner's area on the map: 34.5267° N, 92.9735° W: Placed by OpenAirDocs at the center of ZIP code 71901, within about 6 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N750US
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=750US
- Page: https://openairdocs.org/deregistered/N750US-2010-02-03

From the FAA registry file of October 31, 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 727-214: https://openairdocs.org/model/boeing-727-214.md

## Service difficulty reports (72, newest 50)

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

- [SDR GAIA0711OP](https://openairdocs.org/sdr/GAIA0711OP), Aug 2, 2007: FIRE DETECTOR. FALSE INDICATION. FLT 706 - DFW-IAH - DURING CLIMB, THE FLIGHT CREW HAD AN INDICATION OF AN APU FIRE. THE APU FIRE HANDLE WAS PULLED AND THE FIRE BOTTLE WAS DISCHARGED. THE AIRCR
- [SDR GAI2007F00001](https://openairdocs.org/sdr/GAI2007F00001), May 4, 2007: CONNECTOR. DIRTY. (REF NR: GAIA 07-05 OP) DURING CLIMB THE FLIGHT CREW RETRACTED THE FLAPS NORMALLY HOWEVER, AT ZERO DEGREES FLAPS THE AMBER LIGHT REMAINED ILLUMINATED ON THE FRO
- [SDR GAI2007F00000](https://openairdocs.org/sdr/GAI2007F00000), Apr 27, 2007: TORQUE BOX. CRACKED. DURING INSPECTION IT WAS DISCOVERED THAT THE AFT AIRSTAIRS WOULD NOT TRAVEL TO THE FULLY CLOSED POSITION. FURTHER INSPECTION FOUND A CRACK IN SECTION 48 LOWER A
- [SDR GAIA0703OP](https://openairdocs.org/sdr/GAIA0703OP), Feb 22, 2007: RECEIVER. SHORTED. DURING APPROACH TO LANDING, THE FLIGHT CREW REPORTED SMOKE IN THE COCKPIT. AN EMERGENCY WAS DECLARED AND AN UNEVENTFUL LANDING WAS MAD. INSPECTION REVEALED THAT
- [SDR GAIA0701OP](https://openairdocs.org/sdr/GAIA0701OP), Jan 17, 2007: STRUT. BROKEN. FLIGHT 360 - MCO-ATL - DURING TAXI TO PARKING IN ATL THE RIGHT MAIN LANDING GEAR WARNING LIGHT ILLUMINATED WITH SUBSEQUENT DOOR WARNING LIGHT ON GEAR ANNUNCIATO
- [SDR GAIA06010](https://openairdocs.org/sdr/GAIA06010), Jan 15, 2006: ACTUATOR. LEAKING. DURING DESCENT/APPROACH, LOSS OF (A) SYSTEM HYDRAULIC FLUID. LANDING WAS MADE WITHOUT INCIDENT. REMOVED AND REPLACED NR 4 KRUEGER FLAP ACTUATING CYLINDER IAW MM
- [SDR GAIA05013OP](https://openairdocs.org/sdr/GAIA05013OP), Mar 3, 2005: AIR CLEANER. CRACKED. DURING CLIMBOUT THE LOWER AFT BODY OVERHEAT LIGHT CAME ON. THE AC RETURNED TO AIRPORT AND AN UNEVENTFUL LANDING WAS MADE. REMOVED AND REPLACED THE NR 1 ENGINE A
- [SDR GAIA05013AOP](https://openairdocs.org/sdr/GAIA05013AOP), Mar 3, 2005: WARNING LIGHT. ILLUMINATED. FLT 750 - MIA - DURING CLIMB-OUT, THE LOWER AFT BODY OVERHEAT LIGHT CAME ON. THE AIRCRAFT RETURNED TO MIA AND AN UNEVENTFUL LANDING WAS MADE. (M)
- [SDR GAIA05011ST](https://openairdocs.org/sdr/GAIA05011ST), Mar 1, 2005: RIB. CRACKED. DURING C-CHECK, A 1 INCH CRACK WAS FOUND ON THE C3 CARGO DOOR OUTER CHORD BY THE LOWER STOP FITTING. REMOVED AND REPLACED THE CRACKED FORWARD CLOSURE RIB ON THE
- [SDR GAIA05010ST](https://openairdocs.org/sdr/GAIA05010ST), Mar 1, 2005: SKIN. CRACKED. DURING C-CHECK, A SMALL CRACK WAS FOUND ON THE FUSELAGE SKIN BY THE UPPER FORWARD CORNER OF THE R1 DOOR CUTOUT. CUTOUT CRACKED AREA AND INSTALLED REPAIR IAW BOE
- [SDR GAIA05009ST](https://openairdocs.org/sdr/GAIA05009ST), Mar 1, 2005: SKIN. DENTED. DURING C-CHECK, A DENT AND GOUGE WAS FOUND AT FS 630 ON THE MAIN CARGO DOOR DOUBLER. INSTALLED 8 INCH BY 10 INCH DOUBLER REPAIR IAW KITTY HAWK EA B7-53-123. AIR
- [SDR GAIA05008ST](https://openairdocs.org/sdr/GAIA05008ST), Mar 1, 2005: SKIN. CRACKED. DURING C-CHECK, A SMALL CRACK WAS FOUND AT THE SKIN LAP AT FS 588 STRINGER 4R. CUT OUT CRACKED AREA AND INSTALLED REPAIR IAW BOEING 727 SRM CHAPTER 53-30-3 FIG 
- [SDR GAIA04170OP](https://openairdocs.org/sdr/GAIA04170OP), Oct 12, 2004: BRAKE ASSY. DRAGGING. DURING LANDING, FLIGHT 750 IAG-MSP: VIBRATION IN LANDING GEAR DURING LANDING AND TAXI. LANDING WAS MADE WITHOUT INCIDENT. FOUND NR 1 MLG BRAKE DRAGGING. REMOVED
- [SDR GAIA04073OP](https://openairdocs.org/sdr/GAIA04073OP), May 15, 2004: LIGHT. INOPERATIVE. FOUND EMERGENCY EXIT LIGHT OVER COCKPIT DOOR, BATTERY LOW. REMOVED COCKPIT EMERGENCY LIGHT FOR RECHARGING. INSTALLED NEW EMERGENCY EXIT LIGHT. OPS CHECK GOOD. A
- [SDR GAIA04020OP](https://openairdocs.org/sdr/GAIA04020OP), Jan 29, 2004: COMPUTER. MALFUNCTIONED. DURING CRUISE, THE AIRCRAFT PITCHES UP AND DOWN WITH THE AUTOPILOT IN B-MODE. REMOVED AND REPLACED THE PITCH CHANNEL COMPUTER. OPS CHECK GOOD. AIRCRAFT WAR RELE
- [SDR GAIA03161A](https://openairdocs.org/sdr/GAIA03161A), Nov 6, 2003: PLENUM. CONTAMINATED. FERRY FLIGHT NR 750 - MZJ-JAX - DURING CRUISE, THE CREW NOTICED AN OIL ODOR IN THE COCKPIT FROM THE AIRCONDITIONING. AN UNEVENTFUL LANDING WAS MADE. CLEANED THE
- [SDR GAIA03161OP](https://openairdocs.org/sdr/GAIA03161OP), Nov 6, 2003: ODOR. DETECTED. FERRY FLIGHT NR 750 MCJ TO JAX: DURING CRUISE THE CREW NOTICED AN OIL SMELL IN THE COCKPIT FROM THE AIR CONDITIONING. AN UNEVENTFUL LANDING WAS MADE.
- [SDR GAIA01258OP](https://openairdocs.org/sdr/GAIA01258OP), Jul 9, 2001: LIGHT. INOPERATIVE. DURING ROUTINE MAINTENANCE AT PHX, IT WAS DISCOVERED THAT THE L1 DOOR POSITION EMERGENCY EXIT LIGHT WAS INOPERATIVE. REMOVED AND REPLACED THE L1 DOOR POSITION E
- [SDR GAIA01242OP](https://openairdocs.org/sdr/GAIA01242OP), Jun 15, 2001: CLAMP. LOOSE. FLT 707 - PHX-OKC - LOWER AFT BODY HEAT LIGHT ILLUMINATED IN FLIGHT. FOLLOWED PROCEDURE. AIRCRAFT MADE AN UNEVENTFUL RETURN TO PHX. INSPECTED LEFT AND RIGHT PAC
- [SDR GAIA01155OP](https://openairdocs.org/sdr/GAIA01155OP), Apr 24, 2001: ACCESSORY UNIT. FAILED. FLT 710 - TOL-MKE - AFTER TAKEOFF FROM TOL, THE FLIGHT CREW FOUND THAT THE LANDING GEAR HANDLE WUOLD NOT MOVE PASSED THE OFF POSITION TO THE UP POSITION WITHOUT
- [SDR GAIA00799](https://openairdocs.org/sdr/GAIA00799), Dec 30, 2000: VALVE. LEAKING. FLT 2723 - BOS-TOL - UPON GEAR RETRACTION, NOSE GEAR DOOR LIGHTS ON FORWARD AND FE PANEL ILLUMINATED. THE LIGHTS EXTINGUISHED AFTER RECYCLING LANDING GEAR ON TH
- [SDR GAIA00625](https://openairdocs.org/sdr/GAIA00625), Sep 27, 2000: LOOP. OUT OF POSITION. DISCREPANCY: DURING CRUISE, THE #3 ENGINE STRUT OVERHEAD LIGHT ILLUMINATED. EXECUTED PROCEDURES IAW KHA AOM VOLUME 1. THE AIRCRAFT CONTINUED TO TOL AND MADE AN 
- [SDR GAIA00508](https://openairdocs.org/sdr/GAIA00508), Aug 29, 2000: CONTROL CABLE. BROKEN. FLT 504 - TOL-DAL - DURING TAKEOFF, THE CREW EXPERIENCED ASYMMETRICAL FLAP SPLIT ON THE OUTBOARD FLAPS, RT AT 5 DEGREES, LEFT AT FLAPS 15 DEGREES. TEH CREW DECL
- [SDR GAIA00441](https://openairdocs.org/sdr/GAIA00441), Jul 24, 2000: DETECTOR. OUT OF POSITION. FLT 2731 - LRD-BRO - LOWER AFT BODY OVERHEAT LIGHT ILLUMINATED ON DESCENT INTO BRO. FOLLOWED AOM LOER AFT BODY OVERHEAT PROCEDURES. THE AIRCRAFT MADE AN UNEVENT
- [SDR GAIA00437](https://openairdocs.org/sdr/GAIA00437), Jul 20, 2000: MODULE. MALFUNCTIONED. FLT 2708 - MEM-SLC - DURING CLIMB-OUT, THE LOWER BODY AFT OVER HEAT LIGHT WAS ILLUMINATED. THE AIRCRAFT CONTINUED TO SLC AND MADE A NORMAL ROUTINE LANDING. MAIN
- [SDR GAIA00279](https://openairdocs.org/sdr/GAIA00279), May 16, 2000: BOOT. TORN. LRD/BRO - FLT 2731 - DURING CRUISE, LOWER AFT BODY OVERHEAT LIGHT ILLUMINATED. FOUND SEVERAL LOOSE CLAMPS, ALSO TORN BOOT ON LEFT INLET DUCT. REMOVED AND REPLAC
- [SDR GAIA00259](https://openairdocs.org/sdr/GAIA00259), Apr 27, 2000: WARNING LIGHT. ILLUMINATED. DURING FLT 731, LRD-IAH - RED LEFT GEAR WARNING LIGHT ILLUMINATED. RECYCLED, LIGHT REMAINED ILLUMINATED. TEN MINUTES LATER LIGHT EXTINGUISHED. INSPECTED PROX SW
- [SDR GAIA00181](https://openairdocs.org/sdr/GAIA00181), Apr 10, 2000: STRINGER. CRACKED. DURING LIGHT C-CHECK AT TIMCO/OSC, FOUND STRINGER CRACKED 4 INCHES AFT OF BS 720B.L REPAIRED AIW SRM 53-10-3. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)
- [SDR GAIA00182](https://openairdocs.org/sdr/GAIA00182), Apr 10, 2000: FRAME. DAMAGED. DURING LIGHT C-CHECK AT TIMCO/OSC, FOUND BS 540 FUSELAGE FRAME DAMAGED AT AND BELOW STRINGER 16R. REPAIRED IAW SRM 51-40-3. THE AIRCRAFT WAS RETURNED TO SERVICE
- [SDR GAIA00183](https://openairdocs.org/sdr/GAIA00183), Apr 10, 2000: SEAT TRACK. CORRODED. DURING LIGHT C-CHECK AT TIMCO/OSC, FOUND CORROSION ON SEAT TRACK END AT RBL 24, FS 480. REPAIRED IAW SRM 53-10-5. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)
- [SDR GAIA00184](https://openairdocs.org/sdr/GAIA00184), Apr 10, 2000: SEAT TRACK. CORRODED. DURING LIGHT C-CHECK AT TIMCO/OSC, FOUND CORROSION ON SEAT TRACK STATION 345, RBL 25. REPAIRED IAW SRM 53-10-5. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)
- [SDR GAIA00185](https://openairdocs.org/sdr/GAIA00185), Apr 10, 2000: FRAME. DAMAGED. DURING LIGHT C-CHECK AT TIMCO/OSC, FOUND BS 520 FUSELAGE FRAME INBOARD FLANGE DAMAGED AT AND BELOW STRINGER 16R. REPAIRED IAW SRM 51-40-3. THE AIRCRAFT WAS RETU
- [SDR GAIA00186](https://openairdocs.org/sdr/GAIA00186), Apr 10, 2000: SHEAR TIE. CORRODED. DURING LIGHT C-CHECK AT TIMCO/OSC, FOUND SHEAR TIE CORRODED AT BS 640, RBL 13. REPAIRED IAW SRM 51-20-1. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)
- [SDR GAIA00187](https://openairdocs.org/sdr/GAIA00187), Apr 10, 2000: STRINGER CLIP. CORRODED. DURING LIGHT C-CHECK AT TIMCO/OSC, FOUND CORROSION ON STRINGER SPLICE ON STRINGER 28R, BS 680. REPAIRED IAW SRM 53-10-2. THE AIRCRAFT WAS RETURNED TO SERVICE. (
- [SDR GAIA00188](https://openairdocs.org/sdr/GAIA00188), Apr 10, 2000: STRINGER CLIP. CORRODED. DURING LIGHT C-CHECK AT TIMCO/OSC, FOUND CORROSION ON STRINGER SPLICE ON STRINGER 28L, BS 680. REPAIRED IAW SRM 53-10-2. THE AIRCRAFT WAS RETURNED TO SERVICE. (
- [SDR GAIA00189](https://openairdocs.org/sdr/GAIA00189), Apr 10, 2000: STRINGER CLIP. CORRODED. DURING LIGHT C-CHECK AT TIMCO/OSC, FOUND CORROSION ON STRINGER SPLICE ON STRINGER 27L, BS 680. REPAIRED IAW SRM 53-10-2. THE AIRCRAFT WAS RETURNED TO SERVICE. (
- [SDR GAIA00190](https://openairdocs.org/sdr/GAIA00190), Apr 10, 2000: DOOR FRAME. CRACKED. DURING LIGHT C-CHECK AT TIMCO/OSC, FOUND EXIT DOOR FRAME CRACKED AFT OF LATCH FITTING ON AIRCRAFT STATION 440R. REPAIRED IAW SRM 51-40-2. THE AIRCRAFT WAS RETUR
- [SDR GAIA00191](https://openairdocs.org/sdr/GAIA00191), Apr 10, 2000: FRAME. DENTED. DURING LIGHT C-CHECK AT TIMCO/OSC, FOUND BS 440 FUSELAGE FRAME INBOARD FLANGE DENTED AT STRINGER 16R. REPAIRED IAW SRM 51-40-3. THE AIRCRAFT WAS RETURNED TO SER
- [SDR GAIA00192](https://openairdocs.org/sdr/GAIA00192), Apr 10, 2000: FRAME. DENTED. DURING LIGHT C-CHECK AT TIMCO/OSC, FOUND BS 660 FUSELAGE FRAME INBOARD FLANGE DENTED BELOW STRINGER 16R. REPAIRED IAW SRM 51-40-3. THE AIRCRAFT WAS RETURNED TO 
- [SDR GAIA00193](https://openairdocs.org/sdr/GAIA00193), Apr 10, 2000: FRAME. MISDRILLED. DURING LIGHT C-CHECK AT TIMCO/OSC, FOUND BS 950C FUSELAGE FRAME INBOARD FLANGE HAS DOUBLE DRILLED HOLE BELOW STRINGER 16L. REPAIRED IAW SRM 51-40-3. THE AIRCRAF
- [SDR GAIA00194](https://openairdocs.org/sdr/GAIA00194), Apr 10, 2000: FRAME. CRACKED. DURING LIGHT C-CHECK AT TIMCO/OSC, FOUND BS 540 RBL 60, WL 212 INNER FRAME DOUBLER CRACKED. REPAIRED IAW SRM 51-40-3. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)
- [SDR GAIA00195](https://openairdocs.org/sdr/GAIA00195), Apr 10, 2000: KEELBEAM. CRACKED. DURING LIGHT C-CHECK AT TIMCO/OSC, FOUND CRACK IN KEEL BEAM LEFT LOWER CHORD. VERTICAL FLANGE FROM STATION 870 TO FIRST HI-LOCK HOLE. REPAIRED IAW SB 727-53-020
- [SDR GAIA00196](https://openairdocs.org/sdr/GAIA00196), Apr 10, 2000: FLOORBEAM. MISDRILLED. DURING LIGHT C-CHECK AT TIMCO/OSC, FOUND FLOORBEAM UPPER CHORD HAS NUMEROUS HOLES DRILLED AT BS 460, LBL 45. REPAIRED IAW SRM 53-10-8. THE AIRCRAFT WAS RETURNED
- [SDR GAIA00197](https://openairdocs.org/sdr/GAIA00197), Apr 10, 2000: FRAME. DENTED. DURING LIGHT C-CHECK AT TIMCO/OSC, FOUND CIRCUMFERENTIAL FRAME DENTED BS 1166, LBL 63, WL 212. REPAIRED IAW SRM 51-40-3. THE AIRCRAFT WAS RETURNED TO SERVICE. (
- [SDR GAIA00198](https://openairdocs.org/sdr/GAIA00198), Apr 10, 2000: ANGLE. CORRODED. DURING LIGHT C-CHECK AT TIMCO/OSC, FOUND CORROSION ON LOWER L-ANGLE HORIZONTAL FLANGE AT STATION 880 WHEEL WELL WEB RBL 69, WL 189. REPAIRED IAW SRM 51-20-01. T
- [SDR GAIA00199](https://openairdocs.org/sdr/GAIA00199), Apr 10, 2000: ANGLE. CORRODED. DURING LIGHT C-CHECK AT TIMCO/OSC, FOUND J-ANGLE CORRODED BS 1090 INBOARD SIDE AT STRINGER 29R. REPAIRED IAW SRM 51-20-01. THE AIRCRAFT WAS RETURNED TO SERVICE.
- [SDR GAIA00200](https://openairdocs.org/sdr/GAIA00200), Apr 10, 2000: ANGLE. CORRODED. DURING LIGHT C-CHECK AT TIMCO/OSC, FOUND J-ANGLE CORRODED BS 1090 TO 1100 OUTBOARD SIDE STRINGER 29R. REPAIRED IAW SRM 51-20-01. THE AIRCRAFT WAS RETURNED TO SE
- [SDR GAIA00201](https://openairdocs.org/sdr/GAIA00201), Apr 10, 2000: STRINGER. CORRODED. DURING LIGHT CHECK AT TIMCO/OSC, FOUND CORROSION ON STRINGER 29R BS 1090. REPAIRED IAW SRM 53-10-3. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)
- [SDR GAIA00202](https://openairdocs.org/sdr/GAIA00202), Apr 10, 2000: STRINGER. CORRODED. DURING LIGHT C-CHECK AT TIMC/OSC, FOUND STRINGER 30 HAS CORROSION JUST FORWARD OF FRAME 1166 IN BELLY OF AFT CARGO COMPARTMENT. REPAIRED IAW SRM 53-10-3. THE AI
- [SDR GAIA00203](https://openairdocs.org/sdr/GAIA00203), Apr 10, 2000: SKIN. CORRODED. DURING LIGHT C-CHECK AT TIMCO/OSC, FOUND SKIN PILLOWED BELOW AFT WASTE SERVICE PANEL. REPAIRED IAW SRM 51-20-1 AND TIMCO REO S00124. THE AIRCRAFT WAS RETURNED T

All 72: https://openairdocs.org/deregistered/N750US-2010-02-03/reports.md

## 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 19910606020319I](https://openairdocs.org/incident/19910606020319I), Jun 6, 1991: Boeing 727214 (N750US), Boston, MA, Minor damage. NR2 engine failed after departure returned. Third and fourth stage turbine blades exited from tail pipe.

## Other aircraft with N750US

- [Registered now](https://openairdocs.org/aircraft/N750US): Croke Jonathon P CH 750 CRUZER, S/N 75-10048, built 2015

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