# N994AJ: 1975 Boeing 727-233, registration cancelled 2018-02-13

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: February 13, 2018
- 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: 20942
- Year built: 1975
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: April 23, 1991
- Certificate issued: November 28, 2012
- Last registry action: November 28, 2012
- Mode S code: ADE188
- 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/N994AJ
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=994AJ
- Page: https://openairdocs.org/deregistered/N994AJ-2018-02-13

From the FAA registry file of November 5, 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 (54, newest 50)

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

- [SDR PCSA2010111601](https://openairdocs.org/sdr/PCSA2010111601), Nov 11, 2010: OVERHEAT SYS. FALSE ACTIVATION. NR 1 STRUT OVERHEAT. PERFORMED ABNORMAL PROCEDURE. NO FURTHER OCCURRENCE. MAINTENANCE PERFORMED TEST OF THE OVERHEAT SYSTEM PER AMM. TEST NORMAL. ACCOMPLISHED E
- [SDR PCSA2010092701](https://openairdocs.org/sdr/PCSA2010092701), Sep 24, 2010: ROD. BROKEN. NOSE LANDING GEAR DOOR DID NOT CLOSE WHEN GEAR WAS RETRACTED.
- [SDR PCSA2010051801](https://openairdocs.org/sdr/PCSA2010051801), May 14, 2010: CHECK VALVE. LEAKING. WHEN THROTTLES RETARDED FOR DESCENT A STRANGE ODOR IS DETECTED FOLLOWED BY A HAZE. THEN A SHORT BURST OF SMOKE. LEFT AND RIGHT PACK TEMPS 40 DEGREES. ADVANCED A
- [SDR PCSA2009031101](https://openairdocs.org/sdr/PCSA2009031101), Mar 10, 2009: FIRE WARNING. FALSE ACTIVATION. FIRE WARNING LOWER CARGO ACTIVATED AFTER TAKEOFF. DID AIR RETURN TO MKJP. INSPECTED LOWER CARGO COMPARTMENTS FOR EVIDENCE OF FIRE. NO EVIDENCE OF FIRE FOUND. PE
- [SDR PCSA2009030901](https://openairdocs.org/sdr/PCSA2009030901), Mar 7, 2009: ACTUATOR. BROKEN. ON GEAR RETRACTION LEFT MAIN GEAR RED GEAR LIGHT AND DOORS LIGHT REMAINED ILLUMINATED. MAINTENANCE FOUND THE LEFT MAIN GEAR LOCK ACTUATOR ROD END BROKEN. THE LO
- [SDR 9182007](https://openairdocs.org/sdr/9182007), Sep 18, 2007: HOSE. DAMAGED. NR 1 ENGINE STRUT OVERHEAT LIGHT CAME ON IN CLIMBOUT 6000 FT. LIGHT WENT OUT ON REDUCING POWER TO 1.4 EPR. THE AIRCRAFT RETURNED TO MIA. THE THRUST REVERSER FLE
- [SDR PCSA21820071](https://openairdocs.org/sdr/PCSA21820071), Feb 18, 2007: UPLOCK. CRACKED. FLIGHT 8714 WHILE ON TAXI FROM THE GATE AT SAP THE CREW REPORTED THAT THE RIGHT MAIN LANDING GEAR UNSAFE RED LIGHT ILLUMINATED AND WARNING HORN SOUNDED. THE AIR
- [SDR PCSA051106SUP](https://openairdocs.org/sdr/PCSA051106SUP), May 11, 2006: PUMP. FAILED. FLIGHT 843 DEPARTED MIA AND DURING THE CLIMB THE CREW REPORTED NR 1 ENGINE LOW OIL PRESSURE LIGHT CAME ON DURING FLIGHT FOLLOWED BY F/E'S OIL PRESSURE GAUGE DRO
- [SDR PCSA05110601](https://openairdocs.org/sdr/PCSA05110601), May 11, 2006: ENGINE. FAILED. FLIGHT 843 DEPARTED MIA AND DURING THE CLIMB THE CREW REPORTED NR 1 ENGINE LOW OIL PRESSURE LIGHT CAME ON DURING FLIGHT FOLLOWED BY F/E'S OIL PRESSURE GAUGE DRO
- [SDR PCSA1110601](https://openairdocs.org/sdr/PCSA1110601), Jan 11, 2006: LINE. LEAKING. DURING CLIMB, CREW REPORTED "A" SYSTEM HYD QTY IND DROPPED, CREW SUSPECTED AN "A" SYSTEM HYD FLUID LEAK. A/C RETURNED BACK TO MIA AND LANDED W/O ANY FURTHER INC
- [SDR PCSA12300501](https://openairdocs.org/sdr/PCSA12300501), Dec 30, 2005: CONTROL PANEL. UNSECURE. CLIMBED TO CRUISE, CREW REPORTED NR 3 GEN BREAKER LIGHT CAME ON & WOULD NOT HOLD POWER, NR 2 GEN BREAKER & FIELD LIGHTS CAME ON, NO FAULT NOTED, RESET NR 2 GEN 
- [SDR PCSA11190501](https://openairdocs.org/sdr/PCSA11190501), Nov 19, 2005: FLOW VALVE. DEFECTIVE. ON CLIMBOUT, CREW REPORTED PRESSURIZATION SYSTEM WILL NOT MAINTAIN CABIN ALTITUDE. AIRCRAFT RETURNED BACK TO DEPARTURE AND LANDED WITHOUT ANY FURTHER INCIDENT. 
- [SDR PCSA0906051](https://openairdocs.org/sdr/PCSA0906051), Sep 6, 2005: PROXIMITY SWITCH. FAULTY. FLIGHT 713 DURING TAKEOFF ROLL OUT OF MIA CREW REPORTED NUMBER (5) LEADING EDGE SLAT AMBER LIGHT ILLUMINATED ON FLIGHT ENGINEERS PANEL. THE CREW ABORTED THE TAK
- [SDR PCSA0719051](https://openairdocs.org/sdr/PCSA0719051), Jul 19, 2005: PCU. MALFUNCTIONED. ON TAXI OUT, ACFT ELEVATOR NOSE DOWN STIFF, NOSE UP NORMAL. TAXIED ACFT BACK TO RAMP. VISUAL INSP & TEST OF LT & RT ELEVATOR CABLE SYS & PERFORMED CK OF ELEVATO
- [SDR COOSDR040031](https://openairdocs.org/sdr/COOSDR040031), Aug 23, 2004: FLOORBEAM. CORRODED. MAIN CARGO CABIN, BODY STA 1110, UPPER CAP CORRODED IN SEVERAL PLACES, WL 208.1.
- [SDR COOSDR040029](https://openairdocs.org/sdr/COOSDR040029), Aug 17, 2004: FLOORBEAM. DAMAGED. MAIN CARGO CABIN, BS 1070, FLOORBEAM DAMAGED. REPAIRED.
- [SDR COOSDR040028](https://openairdocs.org/sdr/COOSDR040028), Aug 17, 2004: BEAM. DAMAGED. LT HORIZONTAL STABILIZER, T/E UPPER BEAM REPAIR.
- [SDR COOSDR040027](https://openairdocs.org/sdr/COOSDR040027), Aug 17, 2004: FLOORBEAM. CORRODED. MAIN CARGO CABIN, BS 1130 FLOORBEAM UPPER AND LOWER CHORD, CORRODED.
- [SDR COOSDR040026](https://openairdocs.org/sdr/COOSDR040026), Aug 17, 2004: SKIN. CORRODED. AFT CARGO COMPARTMENT, NR 3 CARGO DOOR CUTOUT SKIN CORRODED AT THE INTERNAL SURFACE.
- [SDR COOSDR040025](https://openairdocs.org/sdr/COOSDR040025), Aug 17, 2004: FLOORBEAM. CORRODED. MAIN CARGO CABIN, BS 950F, WL 208 FLOORBEAM UPPER CHORD CORRODED.
- [SDR COOSDR040024](https://openairdocs.org/sdr/COOSDR040024), Aug 17, 2004: FLOORBEAM. CORRODED. MAIN CARGO CABIN BS 720A FLOORBEAM UPPER CHORD CORRODED.
- [SDR COOSDR040023](https://openairdocs.org/sdr/COOSDR040023), Aug 17, 2004: SKIN. CORRODED. WING CENTER SECTION LOWER SKIN AFT SECTION BETWEEN LBL 30 AND RBL 30 SKIN OUTER FACE CORRODED.
- [SDR COOSDR040018](https://openairdocs.org/sdr/COOSDR040018), Aug 17, 2004: PLATE. CORRODED. LT WING, FRONT SPAR LOWER CHORD PLATE FROM FSS 731 TO FSS 759, WITH CORROSION.
- [SDR COOSDR040013](https://openairdocs.org/sdr/COOSDR040013), Aug 17, 2004: FLOORBEAM. CORRODED. MAIN CARGO CABIN AT B STA 480 FROM RBL 62 INCHES TO LBL 65 INCHES FLOORBEAM UPPER CHORD WITH CORROSION IN SEVERAL PLACES.
- [SDR COOSDR040012](https://openairdocs.org/sdr/COOSDR040012), Aug 17, 2004: SKIN. CORRODED. WING CENTER SECTION FROM STA 740 TO STA 745 BETWEEN LBL 67.000 INCHES AND LBL 61.000 INCHES, UPPER SKIN PANEL WITH CORROSION ON OUTER SURFACE.
- [SDR EE4Y040009](https://openairdocs.org/sdr/EE4Y040009), Aug 17, 2004: FLOORBEAM. CORRODED. MAIN CARGO CABIN, AT B STA 1050 FROM LBL 63 INCHES TO RBL 56 INCHES FLOORBEAM UPPER CHORD WITH HEAVY CORROSION IN SEVERAL PLACES.
- [SDR COOSDR040010](https://openairdocs.org/sdr/COOSDR040010), Jun 30, 2004: KEELBEAM. CORRODED. AFT CARGO COMPARTMENT, STR 29L KEELBEAM, OB FLANGE CORRODED.
- [SDR 2004F00330](https://openairdocs.org/sdr/2004F00330), Jan 12, 2004: CLAMP. LOOSE. FLT CREW REPORTED, AFTER ROTATION, RT DUCT PRESSURE EXCEEDED 100 PSI, ALSO WITH NR 3 ENG BLEED CLOSED FOR APPROX 2 MIN NR 3 ENG STRUT OHEAT LIGHT ILLUMINATED, C
- [SDR 2004F00229](https://openairdocs.org/sdr/2004F00229), Dec 31, 2003: CONNECTOR. INOPERATIVE. FLT 835 - KMIA-MTPP - CREW REPORTED, AFTER TAKEOFF ALL LEADING EDGES DEVICES REMAINED EXTENDED, FORWARD AND AFT GREEN LIGHT REMAINED ILLUMINATED. AIRCRAFT RETUR
- [SDR 2004F00291](https://openairdocs.org/sdr/2004F00291), Dec 24, 2003: CLAMP. LOOSE. FLT 829 - TTPP-SYCJ, FLIGHT CREW REPORTED, OVERHEAT ENGINE STRUT 3 ILLUMINATED AFTER TAKEOFF, JETTISONED FUEL, 9000 LBS. FLIGHT CREW DIVERTED AIRCRAFT BACK TO T
- [SDR 2004F00361](https://openairdocs.org/sdr/2004F00361), Nov 26, 2003: BLEED VALVE. INOPERATIVE. CREW REPORTED, NR 1 ENGINE BLEED AIR VALVE TRIP LIGHT ON DURING FLIGHT AND VALVE STATED CLOSED AFTER ACCOMPLISHING THE ALTERNATE PROCEDURE FROM AOM. AIRCRAFT RE
- [SDR PCS2003F00000](https://openairdocs.org/sdr/PCS2003F00000), Jun 17, 2002: LINE. LOOSE. CREW REPORTED NR 2 ENGINE PRECAUTIONARY SHUTDOWN DUE TO LOSS OF OIL QUANTITY AND OIL PRESSURE FLUCTUATING IN FLIGHT. AIRCRAFT LANDED AT THE INTENDED DESTINATION
- [SDR COOSDR020150](https://openairdocs.org/sdr/COOSDR020150), Jun 1, 2002: FLOORBEAM. CORRODED. MAIN CARGO CABIN - BS 620 FLOORBEAM UPPER CHORD, CORRODED.
- [SDR COOSDR020149](https://openairdocs.org/sdr/COOSDR020149), Jun 1, 2002: FLOORBEAM. CORRODED. MAIN CARGO CABIN - BS 1070 FLOORBEAM UPPER CHORD, CORRODED.
- [SDR COOSDR020148](https://openairdocs.org/sdr/COOSDR020148), Jun 1, 2002: FLOORBEAM. CORRODED. MAIN CARGO CABIN - BS 1090 FLOORBEAM UPPER CHORD CORRODED.
- [SDR COOSDR020147](https://openairdocs.org/sdr/COOSDR020147), Jun 1, 2002: ANGLE. CORRODED. LEFT WING REAR SPAR LOWER CHORD ANGLE, CORRODED.
- [SDR COOSDR02146](https://openairdocs.org/sdr/COOSDR02146), Jun 1, 2002: FLOORBEAM. CORRODED. MAIN CARGO CABIN BS 680 FLOOR BEAM UPPER CHORD CORRODED.
- [SDR COOSDR02110](https://openairdocs.org/sdr/COOSDR02110), Jun 1, 2002: BEAM. CORRODED. LEFT HORIZONTAL STAB TRAILING EDGE BEAM LOWER CHORD AT STAB STA 105 INCHES WITH CORROSION.
- [SDR COOSDR02109](https://openairdocs.org/sdr/COOSDR02109), Jun 1, 2002: BEAM. CORRODED. LEFT HORIZONTAL STAB, TRAILING EDGE BEAM UPPER CHORD AT STAB STA 198 INCHES WITH CORROSION.
- [SDR COOSDR02108](https://openairdocs.org/sdr/COOSDR02108), Jun 1, 2002: BEAM. CORRODED. LEFT WING, REAR TRUNNION SUPPORT BEAM - WBL 124.2, LOWER SURFACE CORRODED.
- [SDR COOSDR02106](https://openairdocs.org/sdr/COOSDR02106), Jun 1, 2002: FLOORBEAM. CORRODED. BS 950C FLOOR BEAM UPPER CHORD CORRODED FROM RBL 48 TO RBL 60 AND FROM LBL 46 TO LBL 60.
- [SDR COOSDR02105](https://openairdocs.org/sdr/COOSDR02105), Jun 1, 2002: SKIN. CORRODED. RIGHT WING, LOWER SKIN PANEL, INBOARD BOOST PUMP-CUTOUT, CORRODED.
- [SDR COOSDR02124](https://openairdocs.org/sdr/COOSDR02124), Jun 1, 2002: PANEL. DELAMINATED. LEFT WING, TRAILING EDGE LOWER PANEL WITH DELAMINATION.
- [SDR COOSDR02122](https://openairdocs.org/sdr/COOSDR02122), Jun 1, 2002: PANEL. DELAMINATED. RIGHT WING MAIN LANDING GEAR TRAILING EDGE UPPER PANEL WITH DELAMINATION.
- [SDR COOSDR02121](https://openairdocs.org/sdr/COOSDR02121), Jun 1, 2002: PANEL. DELAMINATED. LEFT WING, TRAILING EDGE UPPER PANEL WITH DELAMINATION.
- [SDR COOSDR02120](https://openairdocs.org/sdr/COOSDR02120), Jun 1, 2002: PANEL. DELAMINATED. LEFT WING, MAIN LANDING GEAR PANEL WITH DELAMINATION.
- [SDR COOSDR02119](https://openairdocs.org/sdr/COOSDR02119), Jun 1, 2002: FLAP. DELAMINATED. RIGHT WING INBOARD AFT FLAP WITH DELAMINATION.
- [SDR COOSDR02118](https://openairdocs.org/sdr/COOSDR02118), Jun 1, 2002: FLAP. DELAMINATED. RIGHT WING, INBOARD FORE FLAP WITH DELAMINATION.
- [SDR COOSDR02117](https://openairdocs.org/sdr/COOSDR02117), Jun 1, 2002: FLAP. DELAMINATED. LEFT WING, INBOARD AFT FLAP WITH DELAMINATION.
- [SDR COOSDR02116](https://openairdocs.org/sdr/COOSDR02116), Jun 1, 2002: AILERON. DELAMINATED. RIGHT WING, OUTBOARD AILERON TRAILING EDGE WITH DELAMINATION.

All 54: https://openairdocs.org/deregistered/N994AJ-2018-02-13/reports.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.