# N395AJ: 1975 Boeing 727-233, registration cancelled 2019-03-09

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: March 9, 2019
- Status when cancelled: Registration expired, pending cancellation
- Airframe: [Boeing 727-233](https://openairdocs.org/model/boeing-727-233) (registry code 138408A)
- Engine: [Pratt & Whitney JT8D-15](https://openairdocs.org/engine/pratt-whitney-jt8d-15) (registry code 52051)
- Data sheets: [TCDS A3WE](https://openairdocs.org/tcds/A3WE), [TCDS E2EA](https://openairdocs.org/tcds/E2EA) (OpenAirDocs)
- Serial number: 21100
- Year built: 1975
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: December 6, 1994
- Certificate issued: November 28, 2012
- Last registry action: August 11, 2015
- Mode S code: A49565
- Owner when cancelled: [Amerijet International Inc](https://openairdocs.org/faa-owner/AMERIJET%20INTERNATIONAL%20INC)
- Location: [Fort Lauderdale, FL](https://openairdocs.org/faa-place/FL/Fort%20Lauderdale)
- Owner type: Corporation
- Owner's area on the map: 26.1015° N, 80.1209° W: Placed by OpenAirDocs at the center of ZIP code 33316, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N395AJ
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=395AJ
- Page: https://openairdocs.org/deregistered/N395AJ-2019-03-09

From the FAA registry file of November 7, 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 727-233: https://openairdocs.org/model/boeing-727-233.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 PCSA2017120801](https://openairdocs.org/sdr/PCSA2017120801), Dec 8, 2017: WARNING LIGHT. ILLUMINATED. #1 ENGINE SHUTDOWN (BY CREW)DUE TO OIL PRESSURE LIGHT ILLUMINATED.
- [SDR SPUY201605060006](https://openairdocs.org/sdr/SPUY201605060006), May 6, 2016: BEAM. CORRODED. LEFT HORIZONTAL STABILIZER T/E LOWER BEAM SHOWS CORROSION AT SEVERAL LOCATIONS.
- [SDR SPUY201605060005](https://openairdocs.org/sdr/SPUY201605060005), May 6, 2016: SPLICE. CORRODED. WING TO BODY SPLICE PLATE ATTACH, UNDER WING TO BODY WITH CORROSION BS 870, WLB 70.5 LT REF N/R 0337.
- [SDR SPUY201605060004](https://openairdocs.org/sdr/SPUY201605060004), May 6, 2016: FRAME. CORRODED. WING CENTER FRONT SPAR LOWER CHORD, CENTER WING WITH CORROSION BS 740.00 LT LBL 20,
- [SDR SPUY201605060003](https://openairdocs.org/sdr/SPUY201605060003), May 6, 2016: PLATE. CORRODED. SPLICE PLATE ATTACHMENT UNDER WING TO BODY SHOW CORROSION AT BS 870, WLB 70.5.
- [SDR PCSA2015011202](https://openairdocs.org/sdr/PCSA2015011202), Jan 8, 2015: WARNING LIGHT. ILLUMINATED. LEFT GEAR UNSAFE LIGHT.
- [SDR PCSA2015011201](https://openairdocs.org/sdr/PCSA2015011201), Jan 8, 2015: WARNING LIGHT. ILLUMINATED. LEFT MAIN GEAR UNSAFE LIGHT ILLUMINATED.
- [SDR PCSA2014060501](https://openairdocs.org/sdr/PCSA2014060501), Jun 5, 2014: COMPRESSOR. STALLED. AT 3500’ NR 3 ENG COMPRESSOR STALL. RETARDED THRUST, SLOWLY INCREASED THRUST, COMPRESSOR STALLED AGAIN. THRUST AT IDLE, RETURNED TO MIAMI.
- [SDR PCSA2014012201](https://openairdocs.org/sdr/PCSA2014012201), Jan 21, 2014: FLEX HOSE. RUPTURED. LOSS OF B SYS HYD FLUID IN FLIGHT. DECLARED EMERGENCY & RETURNED TO MIA.
- [SDR SPUY201302020026](https://openairdocs.org/sdr/SPUY201302020026), Feb 2, 2013: SPAR. CORRODED. DURING ROUTINE C-CHECK INSPECTION, LT WING FRONT SPAR LOWER CHORD SHOWS CORROSION WS 383.5.
- [SDR SPUY201302020025](https://openairdocs.org/sdr/SPUY201302020025), Feb 2, 2013: SKIN. CORRODED. DURING ROUTINE C-CHECK INSPECTION, CARGO BAY UPPER INNER SKIN SHOWS CORROSION BS 740, STRINGER 1 LT.
- [SDR SPUY201302020024](https://openairdocs.org/sdr/SPUY201302020024), Feb 2, 2013: SKIN. CORRODED. DURING ROUTINE C-CHECK INSPECTION, CARGO COMPARTMENT INNER UPPER SKIN SHOWS CORROSION BS 740, S1R.
- [SDR SPUY201302020023](https://openairdocs.org/sdr/SPUY201302020023), Feb 2, 2013: STIFFENER. CORRODED. DURING ROUTINE C-CHECK INSPECTION, LT WING FRONT SPAR STIFFENER SHOWS CORROSION, WS 224.5.
- [SDR SPUY201302020022](https://openairdocs.org/sdr/SPUY201302020022), Feb 2, 2013: STIFFENER. CORRODED. DURING ROUTINE C-CHECK INSPECTION, LT WING FRONT SPAR STIFFENER CORRODED, WS 198.
- [SDR SPUY201302020021](https://openairdocs.org/sdr/SPUY201302020021), Feb 2, 2013: STIFFENER. CORRODED. DURING ROUTINE C-CHECK INSPECTION, RT WING FRONT SPAR STIFFENER SHOWS CORROSION, WS 212.
- [SDR SPUY201302020020](https://openairdocs.org/sdr/SPUY201302020020), Feb 2, 2013: SKIN. CORRODED. DURING ROUTINE C-CHECK INSPECTION, LT WING NR 2 SLAT SKIN SHOWS CORROSION, WS 656.5, REF N/R 0440.
- [SDR SPUY201302020019](https://openairdocs.org/sdr/SPUY201302020019), Feb 2, 2013: FITTING. CORRODED. DURING ROUTINE C-CHECK INSPECTION, RT WING L/E FLAP FITTING CORRODED, WS 198.0, WS 224.5 REF N/R 0393.
- [SDR SPUY201302020018](https://openairdocs.org/sdr/SPUY201302020018), Feb 2, 2013: FITTING. CORRODED. DURING ROUTINE C-CHECK INSPECTION, RT WING L/E FLAP FITTING CORRODED WS 188.0, REF NR 0392.
- [SDR SPUY201302020017](https://openairdocs.org/sdr/SPUY201302020017), Feb 2, 2013: ANGLE. CORRODED. DURING ROUTINE C-CHECK INSPECTION, RT WING L/E FLAP HOUSING ANGLE CORRODED, WS 171.5, WS 198.0.
- [SDR SPUY201302020016](https://openairdocs.org/sdr/SPUY201302020016), Feb 2, 2013: ANGLE. CORRODED. DURING ROUTINE C-CHECK INSPECTION, RT WING FRONT SPAR ANGLE CORRODED WS 198.0, REF N/R.
- [SDR SPUY201302020015](https://openairdocs.org/sdr/SPUY201302020015), Feb 2, 2013: STIFFENER. CORRODED. DURING ROUTINE C-CHECK INSPECTION, RT WING FRONT SPAR STIFFENER SHOWS CORROSION WS 251.0.
- [SDR SPUY201302020014](https://openairdocs.org/sdr/SPUY201302020014), Feb 2, 2013: STIFFENER. CORRODED. DURING ROUTINE C-CHECK INSPECTION, RT WING FRONT SPAR STIFFENER SHOWS CORROSION WS 222.0.
- [SDR SPUY201302020013](https://openairdocs.org/sdr/SPUY201302020013), Feb 2, 2013: INTERCOSTAL. CORRODED. DURING ROUTINE C-CHECK INSPECTION, RT MLG INTERIOR UPPER PART INTERCOSTAL SHOWS CORROSION FS 920.
- [SDR SPUY201302020012](https://openairdocs.org/sdr/SPUY201302020012), Feb 2, 2013: FRAME. CORRODED. DURING ROUTINE C-CHECK INSPECTION, CARGO COMPARTMENT. FRAME SHOWS CORROSION AT STA 1168 NEAR STRINGER S16R.
- [SDR SPUY201302020011](https://openairdocs.org/sdr/SPUY201302020011), Feb 2, 2013: STRUCTURE. CRACKED. DURING ROUTINE C-CHECK INSPECTION, LT WING LOWER CHORD (NEAR MLG SUPPORT BEAM) CRACKED 4 WS 244.5, REF N/R 0305.
- [SDR SPUY201302020010](https://openairdocs.org/sdr/SPUY201302020010), Feb 2, 2013: SKIN. CORRODED. DURING ROUTINE C-CHECK INSPECTION, LOWER HALF FUSELAGE. RT UPPER AFT FUSELAGE SKIN SHOWS CORROSION FROM BS 1343 TO BS 1376.
- [SDR SPUY201302020009](https://openairdocs.org/sdr/SPUY201302020009), Feb 2, 2013: SKIN. CORRODED. DURING ROUTINE C-CHECK INSPECTION, LT WING UPPER SKIN NEAR REAR SPAR SHOWS CORROSION WS 601.5, REF NR 0258.
- [SDR SPUY201302020008](https://openairdocs.org/sdr/SPUY201302020008), Feb 2, 2013: SKIN. CORRODED. DURING ROUTINE C-CHECK INSPECTION, LT WING UPPER SKIN T/E NEAR OTBD AILERON CORRODED WBL 492.0, REF NR 0257.
- [SDR SPUY201302020007](https://openairdocs.org/sdr/SPUY201302020007), Feb 2, 2013: FLAP TRACK. CORRODED. DURING ROUTINE C-CHECK INSPECTION, LT WING LOWER SURFACE INBD FLAP TRACK COUPLING SHOWS CORROSION WS 304.0, REF N/R 0250.
- [SDR SPUY201302020006](https://openairdocs.org/sdr/SPUY201302020006), Feb 2, 2013: SKIN. CORRODED. DURING ROUTINE C-CHECK INSPECTION, LT WING LOWER SURFACE SHOWS CORROSION WS 491.5 REF NR 0249.
- [SDR SPUY201302020005](https://openairdocs.org/sdr/SPUY201302020005), Feb 2, 2013: SKIN. CORRODED. DURING ROUTINE C-CHECK INSPECTION, RT WING UPPER SKIN L/E SHOWS CORROSION L/E STA 130.7, REF NR 0183.
- [SDR PCSA2012082403](https://openairdocs.org/sdr/PCSA2012082403), Aug 12, 2012: SEAT TRACK. CORRODED. SEAT TRACK AT STA 360 TO 480 LBL 45.5 CORRODED.
- [SDR PCSA2012082402](https://openairdocs.org/sdr/PCSA2012082402), Aug 12, 2012: SEAT TRACK. CORRODED. SEAT TRACK AT STA 950 TO 950C LBL 24.7 CORRODED.
- [SDR PCSA2012082401](https://openairdocs.org/sdr/PCSA2012082401), Aug 12, 2012: SEAT TRACK. CORRODED. SEAT TRACK AT STA 689 CORRODED.
- [SDR PCSA2012050301](https://openairdocs.org/sdr/PCSA2012050301), May 2, 2012: SPLICE. CRACKED. FOUND 1.5 INCH CRACK AT STA 481 BETWEEN 13R AND 14R ON THE BUTT SPLICE.
- [SDR PCSA2011011801](https://openairdocs.org/sdr/PCSA2011011801), Jan 17, 2011: FIRE DETECTOR. UNSECURE. NR 1 STRUT OVERHEAT LIGHT ILLUMINATES WITH NR 1 ENGINE BLEED AIR VALVE CLOSED. MECH FOUND FIRE DETECTOR UNIT UN-SECURED. RE-RACKED AND SECURED FIRE DETECTOR UNI
- [SDR PCSA2010120101](https://openairdocs.org/sdr/PCSA2010120101), Dec 1, 2010: WARNING LIGHT. ILLUMINATED. NR1 STRUT OVERHEAT LIGHT ILLUMINATED AT 33,000 FT. CLOSED NR 1 POWER LEVER AND LIGHT EXTINGUISHED. MX OPENED NR 1 PYLON, PRESSURIZED PNEUMATIC SYS CHECK FOR LEA
- [SDR PCSA2010110501](https://openairdocs.org/sdr/PCSA2010110501), Nov 3, 2010: WARNING SYSTEM. ACTIVATED. NR 1 STRUT OVERHEAT LIGHT ILLUMINATED DURING CRUISE WITH ENGINE ANTI-ICE ON. WHEN THE ANTI-ICE WAS TURNED OFF THE LIGHT WENT OUT.
- [SDR PCSA201010210](https://openairdocs.org/sdr/PCSA201010210), Oct 19, 2010: WARNING LIGHT. ILLUMINATED. LOG ITEM LEFT ENGINE STRUT OVERHEAT LIGHT ILLUMINATED. REDUCED THRUST LEVER PER PROCEDURE. LIGHT EXTINGUISHED AFTER APPROX 30 SECONDS. RETURNED TO MIA. MAINTENA
- [SDR PCSA2010011301](https://openairdocs.org/sdr/PCSA2010011301), Jan 11, 2010: FIRE WARNING. MALFUNCTIONED. AFTER GEAR RETRACTION RECEIVED APU FIRE WARNING. FOLLOWED AMJ PRECEDURES. MAINTENANCE ACCOMPLISHED AN APU INSPECTION. NO SIGNS OF FIRE NOTICED. OPERATIONAL AND 
- [SDR PCSA2009051801](https://openairdocs.org/sdr/PCSA2009051801), May 9, 2009: SENSOR. OUT OF POSITION. NR1 STRUT OVERHEAT LIGHT ILLUMINATED IN FLIGHT. SHUTDOWN NR1 ENGINE AND RETURNED TO DEPARTURE. WINDMILLING 15 MINUTES, OIL PRESSURE WITHIN LIMITS. MX FOUND NR 1
- [SDR PCSA2008093001](https://openairdocs.org/sdr/PCSA2008093001), Sep 30, 2008: ACTUATOR. LEAKING. LOST A HYDR SYS AFTER FLAP RETRACTION DEPARTING. ON APPROACH TO POS NR 7 L/E SLAT FAILED TO EXTEND. LANDING GEARS WERE EXTENDED MANUALLY, THE AC LANDED SAFELY A
- [SDR PCSA818200701](https://openairdocs.org/sdr/PCSA818200701), Aug 18, 2007: ENGINE. MALFUNCTIONED. FLIGHT 861 DEPARTED SJU AND DURING THE TOP OF THE CLIMB THE CREW REPORTED THE NUMBER 1 ENGINE OIL PRESSURE DROPPED TO ZERO, THE NUMBER 1 ENGINE WAS SHUTDOWN AND
- [SDR PCSA7090601](https://openairdocs.org/sdr/PCSA7090601), Jul 9, 2006: FUEL TANK. LEAKING. DURING THE MAINTENANCE WALK AROUND INSPECTION, A FUEL LEAK WAS DISCOVERED AT THE REAR SPAR OF THE NR 2 FUEL TANK (WING BOX CENTER SECTION). FURTHER INSPECTION R
- [SDR PCSA033006](https://openairdocs.org/sdr/PCSA033006), Mar 30, 2006: ENGINE. DAMAGED. FLIGHT 848 AFTER PUSHBACK FROM PAP, THE CREW REPORTED WHEN POWER WAS ADDED THE NUMBER ONE ENGINE EXPERIENCED A VIBRATION. THE AIRCRAFT RETURNED TO THE GATE WITH
- [SDR PCSA708051](https://openairdocs.org/sdr/PCSA708051), Jul 8, 2005: MODULE. MALFUNCTIONED. ON DEPARTURE, CREW REPORTED STALL WARNING STICK SHAKER CAME ON AT ROTATION. CREW DUMPED FUEL, RETURNED AND LANDED WITHOUT ANY FURTHER INCIDENT. MAINTENANCE TROU
- [SDR PCSA6210501](https://openairdocs.org/sdr/PCSA6210501), Jun 21, 2005: OIL SYSTEM. LEAKING. DURING CRUISE NR 3 ENGINE OIL TEMP WAS BETWEEN 125 & 130 DEG FOR 15 MINUTES. PERFORMED ALT PROCEDURES, RETARDED THROTTLE, DIDN'T HELP. SHUTDOWN NR 3 ENGINE, ENG
- [SDR PCSA0518051](https://openairdocs.org/sdr/PCSA0518051), May 18, 2005: COVER. LEAKING. DURING CLIMB CREW REPORTED LOSS OF HYDRAULIC (A) SYSTEM. AIRCRAFT WAS DIVERTED AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE FOUND FEEL COMPUTER FILTER COVER
- [SDR COOSDR030158](https://openairdocs.org/sdr/COOSDR030158), Dec 1, 2003: SKIN. CORRODED. LT WING, LOWER SKIN, LOWER SURFACE, ACCESS DOOR CUTOUT CORRODED. (K)
- [SDR COOSDR030159](https://openairdocs.org/sdr/COOSDR030159), Dec 1, 2003: FRAME. CORRODED. RT MAIN GEAR WHEEL WELL, STA 950 WL 201, FORGING FRAME, HORIZONTAL FLANGE, LOWER SURFACES CORRODED.

All 70: https://openairdocs.org/deregistered/N395AJ-2019-03-09/reports.md

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