# N598AJ: 1979 Boeing 727-212, registration cancelled 2019-02-01

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: February 1, 2019
- Status when cancelled: Registration expired, pending cancellation
- Airframe: [Boeing 727-212](https://openairdocs.org/model/boeing-727-212) (registry code 138407G)
- Data sheets: [TCDS A3WE](https://openairdocs.org/tcds/A3WE) (OpenAirDocs)
- Serial number: 21947
- Year built: 1979
- Type of aircraft: Fixed wing multi engine
- Certificate issued: September 10, 2004
- Last registry action: April 16, 2015
- Mode S code: A7BB28
- 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/N598AJ
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=598AJ
- Page: https://openairdocs.org/deregistered/N598AJ-2019-02-01

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 727-212: https://openairdocs.org/model/boeing-727-212.md

## Service difficulty reports (64, newest 50)

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

- [SDR PCSA2014122201](https://openairdocs.org/sdr/PCSA2014122201), Dec 20, 2014: ENGINE. MAKING METAL. ENGINE NR 3 HAD A COMPRESSOR STALL & A FLAMEOUT AT FL320. METAL FOUND IN TAIL PIPE.
- [SDR 3FMR20140903001](https://openairdocs.org/sdr/3FMR20140903001), Sep 3, 2014: SKIN. CORRODED. DURING ACCOMPLISHMENT OF AD 85-24-02, CORROSION WAS FOUND IN LOWER SKIN BS 870, RBL 3 - 8, WATERLINE 160.8.
- [SDR 3FMR20140903006](https://openairdocs.org/sdr/3FMR20140903006), Sep 3, 2014: SKIN. CORRODED. DURING ACCOMPLISHMENT OF AD 82-24-02, CORROSION WAS FOUND IN THE LT AIR CONDITIONING PLENUM AREA ON THE LOWER SURFACE SKIN AT BS 826 - 848 AT LBL 32, W/L 160.8.
- [SDR 3FMR20140903004](https://openairdocs.org/sdr/3FMR20140903004), Sep 3, 2014: STRUCTURE. CORRODED. DURING ACCOMPLISHMENT OF AD 2005-05-19, CORROSION WAS FOUND ON THE LT FRONT SPAR LOWER ANGLE AT WS 383 - 465. FOUND TO BE OUT OF SRM LIMITS. REPAIRED.
- [SDR 3FMR20140903005](https://openairdocs.org/sdr/3FMR20140903005), Sep 3, 2014: SPAR CAP. CORRODED. CORROSION WAS FOUND ON THE RT HORIZONTAL STABILIZER. CORROSION IS LOCATED AT HORIZONTAL STAB STATION 78.13. FOUND TO BE OUT OF MFG SRM LIMITS. REPAIRED IAW DWG 
- [SDR 3FMR20140903003](https://openairdocs.org/sdr/3FMR20140903003), Sep 3, 2014: SKIN. CORRODED. RIGHT WING LOWER SKIN WAS FOUND CORRODED AROUND FRONT SPAR ATTACH FASTENERS LOCATED AT WING STA 509 - 519. CORROSION WAS FOUND TO BE OUT OF SRM LIMITS. REPAIRED
- [SDR 3FMR20140903002](https://openairdocs.org/sdr/3FMR20140903002), Sep 3, 2014: SPAR. CORRODED. DURING ACCOMPLISHMENT OF AD 2005-05-19, CORROSION WAS FOUND ON THE RIGHT HAND WING, FRONT SPAR, LOWER CHORD AT WING STATION 509 TO 519. CORROSION WAS FOUND OUTS
- [SDR PCSA2013092501](https://openairdocs.org/sdr/PCSA2013092501), Sep 23, 2013: DUCT. RUPTURED. LOWER AFT BODY OVERHEAT LIGHT ILLUMINATED. FOUND DUCT RUPTURED
- [SDR PCSA2013051001](https://openairdocs.org/sdr/PCSA2013051001), May 6, 2013: FUEL CONTROL. FAULTY. ENGINER 2 FLAMEOUT AT CRUISE. ALL PARAMETERS NORMAL. ENG WINDMILL FOR ABOUT 15 MIN. 20 PSI OIL PRESS. THE NR 2 ENGINE OIL FILTER WAS CHECKED, FOUND NORMAL, THE 
- [SDR PCSA2012072101](https://openairdocs.org/sdr/PCSA2012072101), Jul 19, 2012: CONNECTOR. DAMAGED. ENGINE NR 2 FIRE WARNING BELL AND LIGHT ACTUATED IN FLIGHT.
- [SDR PCSA2012072001](https://openairdocs.org/sdr/PCSA2012072001), Jul 19, 2012: CONNECTOR. DEFECTIVE. NR 2 ENGINE FIRE WARNING SOUNDED INTERMITTENTLY IN FLIGHT.
- [SDR SPUY20120628024](https://openairdocs.org/sdr/SPUY20120628024), Jun 28, 2012: SUPPORT. CORRODED. AFTER REMOVAL OF LT MLG FWG TRUNNION SUPPORT FITTING FOUND INBD SUPPORT ASSY RUSTED.
- [SDR SPUY20120628023](https://openairdocs.org/sdr/SPUY20120628023), Jun 28, 2012: SUPPORT. CORRODED. AFTER REMOVAL OF RT MLG FWD TRUNNION SUPPORT FITTING FOUND INBD SUPPORT ASSY RUSTED.
- [SDR SPUY20120627022](https://openairdocs.org/sdr/SPUY20120627022), Jun 27, 2012: SUPPORT. CORRODED. RT WING REAR SPAR AREA. REAR SUPPORT TO FLAP TRACK NR 5 SHOWS CORROSION AT WS 224.50 (FWD PART).
- [SDR SPUY20120627021](https://openairdocs.org/sdr/SPUY20120627021), Jun 27, 2012: SUPPORT. CORRODED. LEFT WING REAR SPAR AREA. REAR SPAR SUPPORT TO FLAP TRACK NR 4 SHOWS CORROSION AT WS 224.50. (FWD PART)
- [SDR SPUY20120620020](https://openairdocs.org/sdr/SPUY20120620020), Jun 20, 2012: TRUNNION. CORRODED. RT WING MLG FORWARD TRUNNION ATTCH FITTING INBD FLANGE SHOWS CORROSION.
- [SDR SPUY20120620019](https://openairdocs.org/sdr/SPUY20120620019), Jun 20, 2012: TRUNNION. CORRODED. LEFT WING MLG FOWARD TRUNNION ATTACH FITTING INBD FLANGE SHOWS CORROSION.
- [SDR SPUY20120620018](https://openairdocs.org/sdr/SPUY20120620018), Jun 20, 2012: FRAME. DEFORMED. MAIN CARGO BAY FRAME DEFORMED, BS 380.
- [SDR SPUY20120620017](https://openairdocs.org/sdr/SPUY20120620017), Jun 20, 2012: FLOORBEAM. CORRODED. MAIN CARGO BAY AFT UPPER FLANGE OF FLOORBEAM SHOWS CORROSION RBL 10 BS 950.
- [SDR SPUY20120620016](https://openairdocs.org/sdr/SPUY20120620016), Jun 20, 2012: FLOORBEAM. CORRODED. MAIN CARGO BAY FLOORBEAM UPPER FLANGE SHOWS CORROSION BS 1070 BETWEEN LBL 45" AND LBL 62.5.
- [SDR SPUY20120620015](https://openairdocs.org/sdr/SPUY20120620015), Jun 20, 2012: CARGO TRACK. CORRODED. CARGO TRACK SHOWS CORROSION BS 1010, LBL 62.5.
- [SDR SPUY20120620014](https://openairdocs.org/sdr/SPUY20120620014), Jun 20, 2012: CARGO TRACK. CORRODED. CARGO TRACK SHOWS CORROSION BS 950 LBL 24.5.
- [SDR SPUY20120620013](https://openairdocs.org/sdr/SPUY20120620013), Jun 20, 2012: CARGO TRACK. CORRODED. CARGO TRACK UPPER AND LOWER LT FLANGE SHOWS CORROSION BETWEEN BS 950C AND BS 950D, RBL 24.5.
- [SDR SPUY20120620012](https://openairdocs.org/sdr/SPUY20120620012), Jun 20, 2012: CARGO TRACK. CORRODED. CARGO TRACK LOWER PART BOTH FLANGES SHOW CORROSION BS 1130, RBL 24.5.
- [SDR SPUY20120620011](https://openairdocs.org/sdr/SPUY20120620011), Jun 20, 2012: CARGO TRACK. CORRODED. CARGO TRACK RT FLANGE SHOWS CORROSION BETWEEN BS 950C AND BS 950F LBL 24.5.
- [SDR SPUY20120620010](https://openairdocs.org/sdr/SPUY20120620010), Jun 20, 2012: CARGO TRACK. CORRODED. CARGO TRACK SHOWS CORROSION UPPER LBL 62.5 BS 445.000, BS 485.000 AND BS 502.00.
- [SDR SPUY20120620009](https://openairdocs.org/sdr/SPUY20120620009), Jun 20, 2012: BEAM. CORRODED. MAIN CARGO BAY BEAM FWD LOWER FLANGE SHOWS POINTS OF CORROSION AT STA 890, RBL 35".
- [SDR SPUY20120620008](https://openairdocs.org/sdr/SPUY20120620008), Jun 20, 2012: BEAM. CORRODED. MAIN CARGO BAY BEAM FWD LOWER FLANGE SHOWS CORROSION AT STA 900 RBL 45"
- [SDR SPUY20120620007](https://openairdocs.org/sdr/SPUY20120620007), Jun 20, 2012: FLOORBEAM. CORRODED. MAIN CARGO BAY FLOORBEAM LOWER FLANGE SHOWS CORROSION STA 890, LBL 30".
- [SDR SPUY20120620006](https://openairdocs.org/sdr/SPUY20120620006), Jun 20, 2012: CARGO TRACK. CORRODED. NR 1 CARGO TRACK LOWER PART CORRODED AT BS 950, LBL 62.5.
- [SDR SPUY20120620005](https://openairdocs.org/sdr/SPUY20120620005), Jun 20, 2012: SKIN. CORRODED. CENTER SECTION LOWER SKIN SHOWS CORROSION STA 804-5 - STA 825.95, LBL25.
- [SDR SPUY20120620004](https://openairdocs.org/sdr/SPUY20120620004), Jun 20, 2012: SPAR. CORRODED. LT WING FRONT SPAR LOWER CHORD SHOWS CORROSION BETWEEN WS 304.0 AND WS 320.5
- [SDR SPUY20120620003](https://openairdocs.org/sdr/SPUY20120620003), Jun 20, 2012: FRAME. DEFORMED. FWD CARGO BAY FRAME DEFORMED BS 560, STRINGER 24L TO 25L.
- [SDR SPUY20120620001](https://openairdocs.org/sdr/SPUY20120620001), Jun 20, 2012: FRAME. CRACKED. FWD CARGO BAY FRAME CRACKED .5" BS 580, STRINGER 23L TO 25L.
- [SDR SPUY20120620002](https://openairdocs.org/sdr/SPUY20120620002), Jun 20, 2012: FRAME. DEFORMED. FWD CARGO BAY FRAME DEFORMED BS 520, S22-26L.
- [SDR PCSA2011012201](https://openairdocs.org/sdr/PCSA2011012201), Jan 22, 2011: ACTUATOR. LEAKING. DURING CLIMBOUT, LOST HYDRAULIC SYSTEM "A" QUANTITY AND PRESSURE. T/S FOUND LEAKING NR 5 KRUEGER FLAP ACTUATOR. REMOVED AND REPLACED ACTUATOR AND OPS AND LEAK C
- [SDR PCSA10420071](https://openairdocs.org/sdr/PCSA10420071), Jan 4, 2007: COMPRESSOR. DAMAGED. FLIGHT 743 DURING THE TAKEOFF ROLL FROM MIA THE CREW EXPERIENCED A VIBRATION ON THE NUMBER 3 ENGINE, THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED BACK TO T
- [SDR PCSA111706SUP](https://openairdocs.org/sdr/PCSA111706SUP), Nov 17, 2006: OIL FILTER. BYPASSING. FLIGHT 858 DEPARTED MAR AND DURING THE CLIMB THE CREW REPORTED THE NR 1 ENGINE LOW OIL FILTER BYPASS LIGHT ILLUMINATED, THE CREW ACCOMPLISHED COMPANY ALTERNATE 
- [SDR PCSA7140601](https://openairdocs.org/sdr/PCSA7140601), Jul 14, 2006: ACTUATOR. CORRODED. THE NOSE LANDING GEAR MANUAL EXTENSION INBOARD & OUTBOARD SHAFT SEGMENTS WERE FOUND TO HAVE CORROSION, THE DRAG BRACE PIN & FITTING & THE TRANSFER CYLINDER WERE
- [SDR PCSA6130601](https://openairdocs.org/sdr/PCSA6130601), Jun 13, 2006: COMPRESSOR. STALLED. FLIGHT 721 PREPARED TO TAKEOFF FROM MIA; THE CREW REPORTED NR 2 ENGINE COMPRESSOR STALLING AS POWER WAS APPLIED. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURN
- [SDR PCSA05190601](https://openairdocs.org/sdr/PCSA05190601), May 19, 2006: HANDLE. DAMAGED. FLIGHT 741 DEPARTED MIA THE CREW REPORTED DURING CLIMB ON GEAR RETRACTION THE LEFT GEAR DOOR AMBER LIGHT CAME ON, AMERIJET PROCEDURES WERE FOLLOWED AND THE AIRC
- [SDR PCSA03030601](https://openairdocs.org/sdr/PCSA03030601), Mar 3, 2006: SWITCH. FALSE INDICATION. FLIGHT 859 DEPARTED MIA THE CREW REPORTED DURING CLIMB THE NUMBER 3 LEADING EDGE FLAP IN TRANSIT LIGHT STAYED ON AFTER THE FLAPS WERE RETRACTED ON THE FLIGHT EN
- [SDR PCSA01310601](https://openairdocs.org/sdr/PCSA01310601), Jan 29, 2006: NUT. LOOSE. KMIA-MDSD FLIGHT 871 - CREW REPORTED APPROXIMATELY 20 MINUTES INTO CRUISE, NR 1 ENGINE EGT, N1 AND N2 RAPIDLY APPROACHED THEIR LIMITS. ENGINE NR 1 WAS SHUTDOWN 
- [SDR PCSA12070502](https://openairdocs.org/sdr/PCSA12070502), Dec 7, 2005: ADC. FAILED. FLIGHT 8216 DURING TAKEOFF FROM CUR CREW REPORTED CAPTAIN'S AIRSPEED INDICATION SHOWED NO AIRSPEED INDICATION, THE F/O'S AIRSPEED INDICATOR WAS SHOWING 80 KNOTS
- [SDR PCSA11250501](https://openairdocs.org/sdr/PCSA11250501), Nov 25, 2005: FUEL HEATER. FAILED. AT TOP OF DESCENT NR 2 ENGINE OIL TEMP BEGAN TO RISE, NR 2 FUEL HEAT VALVE WAS STUCK OPEN. NR 2 ENGINE FUEL HEAT VALVE WAS CYCLED, BUT WOULD NOT CLOSE, OIL TEMP
- [SDR PCSA11030501](https://openairdocs.org/sdr/PCSA11030501), Nov 3, 2005: ENGINE. VIBRATION. WHILE IN CRUISE, CREW REPORTED VIBRATION ON THE CENTER CONSOLE, WHEN NR 1 ENGINE THROTTLE WAS PULLED BACK VIBRATION SEEMS TO DIMINISH. AIRCRAFT RETURNED AND LAN
- [SDR PCSA7060501](https://openairdocs.org/sdr/PCSA7060501), Jul 4, 2005: ADC. FALSE INDICATION. ON TAKEOFF ROLL, CAPT AIRSPEED INDICATOR WENT TO 300 KNOTS AT AROUND 60 KNOTS INDICATED. CREW ABORTED TAKEOFF AND RETURNED TO BLOCKS. NO FURTHER INCIDENT REPORT
- [SDR PCSA04270501](https://openairdocs.org/sdr/PCSA04270501), Apr 27, 2005: PROXIMITY SWITCH. OUT OF ADJUST. FLIGHT 881 DEPARTED MIA DURING CLIMBOUT CREW REPORTED AMBER LEADING EDGE FLAP INTRANSIT LIGHT REMAINED ILLUMINATED ON CAPTAINS FWD PANEL, CREW VERIFIED INDICATI
- [SDR PCSA04260501](https://openairdocs.org/sdr/PCSA04260501), Apr 26, 2005: OUTFLOW VALVE. INTERMITTENT. FLIGHT 710 MID-MIA, DURING CLIMBOUT CREW REPORTED PRESSURIZATION OUTFLOW VALVE WOULD NOT CLOSE IN ANY MODE IN FLIGHT ON DEPARTURE FROM MID. AIRCRAFT RETURNED BA
- [SDR PCSA05041401](https://openairdocs.org/sdr/PCSA05041401), Apr 14, 2005: HOUSING. STRIPPED. FLT 8414 ON APPROACH TO MIA CREW REPORTED NR 1 ENGINE LOST OIL, ENG. NR 1 WAS SHUTDOWN AS A PRECAUTION. A/C LANDED AT INTENDED DESTINATION WITHOUT FURTHER INCID

All 64: https://openairdocs.org/deregistered/N598AJ-2019-02-01/reports.md

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