# N79754: Boeing 727-227, registration cancelled 2007-05-16

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: May 16, 2007
- Exported to: Brazil
- Status when cancelled: Valid registration
- Airframe: [Boeing 727-227](https://openairdocs.org/model/boeing-727-227) (registry code 1384078)
- Data sheets: [TCDS A3WE](https://openairdocs.org/tcds/A3WE) (OpenAirDocs)
- Serial number: 21363
- Type of aircraft: Fixed wing multi engine
- Certificate issued: October 5, 2006
- Last registry action: October 5, 2006
- Mode S code: AAD52A
- Owner when cancelled: [Flightstar Group Inc](https://openairdocs.org/faa-owner/FLIGHTSTAR%20GROUP%20INC)
- Location: [Ft Lauderdale, FL](https://openairdocs.org/faa-place/FL/Ft%20Lauderdale)
- Owner type: Corporation
- Owner's area on the map: 26.0870° N, 80.1530° W: Placed by OpenAirDocs at the center of ZIP code 33315, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N79754
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=79754
- Page: https://openairdocs.org/deregistered/N79754-2007-05-16

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 727-227: https://openairdocs.org/model/boeing-727-227.md

## Service difficulty reports (89, newest 50)

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

- [SDR XN0A1334](https://openairdocs.org/sdr/XN0A1334), Jun 2, 2006: HYDRAULIC SYSTEM. CONTAMINATED. EXCESSIVE SIDE TO SIDE VIBRATION ON TAXI OUT. BLED -A- AND -B- SYSTEM HYDRAULICS SEVERAL TIMES IAW B727 MM CHAPTER 29-00-00. TAXIED AIRCRAFT, NO VIBRATION OR SI
- [SDR XN0A1336](https://openairdocs.org/sdr/XN0A1336), May 31, 2006: CYLINDER. LEAKING. A-SYSTEM FAILURE AFTER GEAR RETRACTION. FOUND NOSE GEAR HYDRAULIC TRANSFER CYLINDER LEAKING EXCESSIVELY. REMOVED AND REPLACED TRANSFER CYLINDER IAW B727 MM CHAP
- [SDR XN0A1303](https://openairdocs.org/sdr/XN0A1303), Feb 23, 2006: RUDDER. MALFUNCTIONED. RUDDER SYSTEM -A- LADDER LIGHT ON. NO RUDDER INDICATION. CYCLED RUDDER LOWER HYDRAULIC UNIT, PERFORMED OPS CK IAW B727 AMM 27-20-121, OPS CHECKED GOOD.
- [SDR XN0A1295](https://openairdocs.org/sdr/XN0A1295), Feb 7, 2006: TRANSCEIVER. INOPERATIVE. NR 1 VHF WOULD NOT TRANSMIT OR RECEIVE. REMOVED AND REPLACED VHF TRANSCEIVER IAW B727 M/M 23-21-31.
- [SDR XN0A1195](https://openairdocs.org/sdr/XN0A1195), Feb 7, 2006: TRANSCEIVER. FAILED. NR 1 VHF WOULD NOT TRANSMIT OR RECEIVE. REMOVED AND REPLACED VHF TRANSCEIVER IAW B727 M/M 23-21-31.
- [SDR XN0A1294](https://openairdocs.org/sdr/XN0A1294), Feb 6, 2006: FLAP SYSTEM. MALFUNCTIONED. NR 1 LED LOCKED UP & WOULD NOT EXTEND FOR 10 MINUTES ON FLAP EXTENSION. NR 4 LED INTRANSIT FOR 15 MINUTES ON FLAP EXTENSION. VERIFIED NR 1 LED IS AN INDICATION 
- [SDR XN0A1298](https://openairdocs.org/sdr/XN0A1298), Jan 30, 2006: SHEAR TIE. CORRODED. DURING REMOVAL OF STR 30, (FROM FS 1150 TO FS 1183), FOUND SHEAR TIE FITTING CORRODED (JACK FTG). REMOVED CORRODED JACK FITTING AND BULKHEAD STIFFENER AND INSTA
- [SDR XN0A1297](https://openairdocs.org/sdr/XN0A1297), Jan 30, 2006: STRINGER. CORRODED. DURING CPCP INSPECTION FOUND STR 30 CORRODED FROM FS 1150 TO FS 1183. REMOVED CORRODED SECTION OF STRINGER FROM FS 1150 TO FS 1183 AND REPAIRED SAME PER B727 SR
- [SDR XN0A1296](https://openairdocs.org/sdr/XN0A1296), Jan 30, 2006: STRINGER. CORRODED. DURING CPCP INSPECTION FOUND STR 25R CORRODED FROM FS 1150 TO FS 1183. REMOVED DAMAGED SECTION OF STRINGER, INSTALLED STR MATERIAL P/N BAC1498-145 PER B727 SRM 
- [SDR XN0A1197](https://openairdocs.org/sdr/XN0A1197), Jan 30, 2006: STRINGER. CORRODED. DURING CPCP INSPECTION FOUND STR 30 CORRODED FROM FS 1150 TO FS 1183. REMOVED CORRODED SECTION OF STRINGER FROM FS 1150 TO FS 1183 AND REPAIRED SAME PER B727 SR
- [SDR XN0A1292](https://openairdocs.org/sdr/XN0A1292), Dec 29, 2005: POSITION SWITCH. MALFUNCTIONED. NR 3 LED FLAP NOT ON WITH FLAP HANDLE AT 15 DEGREES, AMBER L/E FLAP LIGHT ON. REMOVED AND REPLACED NR 3 KRUEGER FLAP POSITION SWITCH IAW MM 27-82-1. OPS CHECK G
- [SDR XN0A1274](https://openairdocs.org/sdr/XN0A1274), Oct 28, 2005: ENGINE. FAILED. NR 1 ENGINE FAULT ON T/O ROLL AT STEWART, LOUD BAND HEARD FOLLOWED BY EPR REDUCTIVE TOWARDS 0. ALL OTHER ENGINE INDICATIONS NORMAL DURING T/O ROLL.
- [SDR XN0A1260](https://openairdocs.org/sdr/XN0A1260), Aug 25, 2005: DOOR. OUT OF ADJUST. PILOT REPORT, COULD NOT PRESSURIZE A/C. RE-ADJUSTED EE DOOR IAW MM 52-40-11.
- [SDR XN0A1245](https://openairdocs.org/sdr/XN0A1245), Jul 8, 2005: ENGINE. FAILED. ENGINE NR 2 WOULD NOT START. REMOVED AND REPLACED NR 2 ENGINE, OPS CK GOOD REF MM 74-11. (ORIG/CLOSED)
- [SDR XN0A1230](https://openairdocs.org/sdr/XN0A1230), Mar 1, 2005: WARNING SYSTEM. MALFUNCTIONED. TAKEOFF WARNING HORN STEADY INSTEAD OF INTEMITTENT. CLEANED AND RESET, CONNECTOR, WARNING BOX OPS CHECK GOOD AT THIS TIME IAW 727-3100.
- [SDR XN0A1229](https://openairdocs.org/sdr/XN0A1229), Feb 24, 2005: FIRE WARNING. MALFUNCTIONED. ON TAKEOFF ROLL MAIN CARGO FIRE WARNING AND BELL CAME ON. PERFORMED FUNCTIONAL CHECK OF MAIN DECK CARGO SYS, SDU'S SYSTEM CHECKED NORMAL IAW SECURE A PLANE. INS
- [SDR XNOA1218](https://openairdocs.org/sdr/XNOA1218), Dec 21, 2004: ENGINE. MALFUNCTIONED. NR 1 ENGINE WOULD NOT LIGHT OFF WHEN STARTING. PULLED AND RESET C/B PER M/M 74-00. OPS CHECK GOOD AT THIS TIME.
- [SDR XNO1218](https://openairdocs.org/sdr/XNO1218), Dec 21, 2004: ENGINE. MALFUNCTIONED. NR 1 ENGINE WOULD NOT LIGHT OFF WHEN STARTING. PULLED AND RESET C/B PER M/M 74-00. OPS CHECK GOOD AT THIS TIME.
- [SDR XNOA1213](https://openairdocs.org/sdr/XNOA1213), Nov 24, 2004: WARNING LIGHT. FALSE ACTIVATION. LOWER FORWARD CARGO FIRE LIGHT AND BELL ILLUMINATED IN FLIGHT DIVERTED TO BNA. PERFORMED OPS CHECK ON CDU, INDICATED FALSE ALARM S/N M13198. VISUALLY CHECKED LO
- [SDR XNOA1192](https://openairdocs.org/sdr/XNOA1192), Jul 13, 2004: BATTERY. MALFUNCTIONED. MAIN CARGO FIRE ALARM ILLUMINATED DURING DESCENT, VISUAL CHECK OKAY. LIGHT EXTINGUISHED SHORTLY AFTER. REMOVED AND REPLACED 2 EACH MAIN DECK SDU BATTERIES. SDU 
- [SDR XNOA1185](https://openairdocs.org/sdr/XNOA1185), Apr 27, 2004: HOUSING. CRACKED. ON DEPARTURE LOST SYSTEM A HYDRAULIC FLUID. FOUND RT MAIN GEAR SELECTOR VALVE HOUSING CRACKED, R & R VALVE, OPS AND LEAK CHECK GOOD DURING GEAR SWING IAW B727 M
- [SDR XNOA01139](https://openairdocs.org/sdr/XNOA01139), Jul 15, 2003: GYRO. INOPERATIVE. NR 2 COMPASS SYSTEM INOPERATIVE. COMPASS CARD STAYED FROZEN. REMOVED AND REPLACED THE NR 2 DIRECTIONAL GYRO. PERFORMED CHECK OF THE NR 2 COMPASS SYSTEM. OPS CHE
- [SDR XNOA01131](https://openairdocs.org/sdr/XNOA01131), Jun 7, 2003: WINDOW. CRACKED. R-1 WINDOW CRACKED. REMOVED AND REPLACED R-1 WINDOW AS REQ IAW 727 MM 56-11-11.
- [SDR XNOA01103](https://openairdocs.org/sdr/XNOA01103), Feb 11, 2003: WARNING LIGHT. FALSE ACTIVATION. DURING DE-ICE AFT LOWER CARGO FIRE WARNING AND BELL, DISPLAY READ AFT FIRE. VISUALLY INSPECTED AFT LOWER CARGO AREA, ALL CLEAR. NO DEFECTS. PERFORMED SYSTEMS CH
- [SDR XNOA01095](https://openairdocs.org/sdr/XNOA01095), Dec 20, 2002: WARNING LIGHT. ILLUMINATED. PRIOR TO TAKEOFF ROLL CARGO DOOR WARNING LIGHT ILLUMINATED. ADJUSTED FWD VENT DOOR SWITCH IAW STC WAI9815-6 PG 6.5. OPS CHECK GOOD.
- [SDR XNOA01094](https://openairdocs.org/sdr/XNOA01094), Dec 13, 2002: WARNING LIGHT. ILLUMINATED. LOWER AFT CARGO FIRE WARNING AFTER TAKEOFF. TRANSFERRED TO DMI 2844 IAW ENA 727 MEL 26-19 CAT-C PLACARDS INSTALLED.
- [SDR 20000329SH033](https://openairdocs.org/sdr/20000329SH033), Feb 18, 2000: FRAME. CORRODED. DURING A C-CHECK, CORROSION WAS NOTED ON LOWER FRAME STA 420, R-1 DOOR. (X)
- [SDR 20000329SH032](https://openairdocs.org/sdr/20000329SH032), Feb 18, 2000: STRINGER. CORRODED. DURING A C-CHECK, CORROSION WAS NOTED ON SEVERAL AREAS OF FRAME BS 950F - BS 1030, STR 28R, STRINGER SPLICE, AND FAIL SAFE CHORD. (X)
- [SDR 20000329SH031](https://openairdocs.org/sdr/20000329SH031), Feb 18, 2000: FLOORBEAM. CORRODED. DURING C-CHECK, CORROSION WAS NOTED ON FLOORBEAM RT STA 1090 - STA 1110. (X)
- [SDR 20000329SH030](https://openairdocs.org/sdr/20000329SH030), Feb 18, 2000: FLOORBEAM. CORRODED. DURING A C-CHECK, CORROSION WAS NOTED ON FLOORBEAM STA 1090 - STA 1110 (58 INCHES FROM RT SIDE). (X)
- [SDR 20000329SH029](https://openairdocs.org/sdr/20000329SH029), Feb 18, 2000: FLOORBEAM. CORRODED. DURING A C-CHECK, CORROSION WAS NOTED ON FLOORBEAM STA 303.9 - STA 344 (36 INCHES FROM LT SIDE). (X)
- [SDR 20000329SH028](https://openairdocs.org/sdr/20000329SH028), Feb 18, 2000: FLOORBEAM. CORRODED. DURING A C-CHECK, CORROSION WAS NOTED ON FLOORBEAM AT STA 1110 - STA 1130 RT. (X)
- [SDR 20000329SH027](https://openairdocs.org/sdr/20000329SH027), Feb 18, 2000: SHEAR TIE. CORRODED. DURING A C-CHECK, CORROSION WAS NOTED ON SHEAR TIE AT STA 990, STR 28 - STR 29R. (X)
- [SDR 20000329SH026](https://openairdocs.org/sdr/20000329SH026), Feb 18, 2000: FLOORBEAM. CORRODED. DURING A C-CHECK, CORROSION WAS NOTED ON FLOORBEAM LT STA 300 - STA 320 (19 INCHES FROM LT SIDE). (X)
- [SDR 99ZZZX4345](https://openairdocs.org/sdr/99ZZZX4345), Nov 17, 1999: FRAME. CORRODED. DURING A C-CHECK, CORROSION WAS NOTED ON LOWER FRAME STA 420 R-1 DOOR.
- [SDR 99ZZZX1796](https://openairdocs.org/sdr/99ZZZX1796), Apr 12, 1999: STRINGER. CORRODED. DURING A C-CHECK, CORROSION WAS NOTED ON STR 27R AT STA 620.
- [SDR 99ZZZX1787](https://openairdocs.org/sdr/99ZZZX1787), Apr 12, 1999: SEAT TRACK. CORRODED. DURING A C-CHECK, CORROSION WAS NOTED ON SEAT TRACK AT STA 740 - STA 760 LBL 45.5.
- [SDR 99ZZZX1786](https://openairdocs.org/sdr/99ZZZX1786), Apr 12, 1999: SEAT TRACK. CORRODED. DURING A C-CHECK, CORROSION WAS NOTED ON SEAT TRACK STA 848.95 - STA 870 LBL 24.75.
- [SDR 99ZZZX1785](https://openairdocs.org/sdr/99ZZZX1785), Apr 12, 1999: RETAINER. CORRODED. DURING A C-CHECK, CORROSION WAS NOTED ON RIGHT WING TRAILING EDGE PANEL SEAL RETAINER (APPROXIMATELY WS 220).
- [SDR 99ZZZX1784](https://openairdocs.org/sdr/99ZZZX1784), Apr 12, 1999: ANGLE. CORRODED. DURING A C-CHECK, CORROSION WAS NOTED ON SEVERAL SUPPORT ANGLE ON AFT AIRSTAIR STEPS.
- [SDR 99ZZZX1783](https://openairdocs.org/sdr/99ZZZX1783), Apr 12, 1999: ANGLE. CORRODED. DURING A C-CHECK, CORROSION WAS NOTED ON AFT INBOARD ATTACH ANGLE JUST AFT OF NR 5 SPOILER FITTING.
- [SDR 99ZZZX1782](https://openairdocs.org/sdr/99ZZZX1782), Apr 12, 1999: SEAT TRACK. CORRODED. DURING A C-CHECK, CORROSION WAS NOTED ON SEAT TRACK STA 1050 - STA 1070 BL 45.5 R.
- [SDR 99ZZZX1781](https://openairdocs.org/sdr/99ZZZX1781), Apr 12, 1999: STRINGER. CORRODED. DURING A C-CHECK, CORROSION WAS NOTED AT STA 720C, STR 28L - STR 28R.
- [SDR 99ZZZX1780](https://openairdocs.org/sdr/99ZZZX1780), Apr 12, 1999: SKIN. CORRODED. DURING A C-CHECK, CORROSION WAS NOTED ON SKIN UNDER LEVELING COMPOUND AT STA 680 STR 27L.
- [SDR 99ZZZX1779](https://openairdocs.org/sdr/99ZZZX1779), Apr 12, 1999: STRINGER. CORRODED. DURING A C-CHECK, CORROSION WAS NOTED ON STR 28R AT STA 480.
- [SDR 99ZZZX1778](https://openairdocs.org/sdr/99ZZZX1778), Apr 12, 1999: SEAT TRACK. CORRODED. DURING A C-CHECK, CORROSION WAS NOTED ON SEAT TRACK AT STA 950 - STA 990 RBL 24.75.
- [SDR 99ZZZX1777](https://openairdocs.org/sdr/99ZZZX1777), Apr 12, 1999: SEAT TRACK. CORRODED. DURING A C-CHECK, CORROSION WAS NOTED ON SEAT TRACK AT STA 950 - STA 1010 AT RBL 45.5.
- [SDR 99ZZZX1776](https://openairdocs.org/sdr/99ZZZX1776), Apr 12, 1999: SEAT TRACK. CORRODED. DURING A C-CHECK, CORROSION WAS NOTED ON SEAT TRACK AT STA 950 - STA 1010, RBL 45.5.
- [SDR 99ZZZX1775](https://openairdocs.org/sdr/99ZZZX1775), Apr 12, 1999: SEAT TRACK. CORRODED. DURING A C-CHECK, CORROSION WAS NOTED ON SEAT TRACK AT STA 1030 - STA 1090 (R-2 DOOR).
- [SDR 99ZZZX1286](https://openairdocs.org/sdr/99ZZZX1286), Feb 12, 1999: BOLT. MISDRILLED. CONE BOLT THROUGH-BOLT HOLE IS NOT CONCENTRIC AND HAS AN .010 INCH DEVIATION BETWEEN LEFT AND RIGHT SIDES, E.G., HOLE IS NOT STRAIGHT WHICH CONTRIBUTED TO THE T

All 89: https://openairdocs.org/deregistered/N79754-2007-05-16/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 FTW93FA100](https://openairdocs.org/ntsb/FTW93FA100), Mar 9, 1993: Boeing 727-200 (N79754), Houston, TX, no damage. Probable cause: THE FAILURE OF THE PILOT OF THE T-38A TO FOLLOW FLIGHT ADVISORIES. A FACTOR WHICH CONTRIBUTED TO THE ACCIDENT WAS THE DEVELOPMENT OF A LETTER OF AGREEMENT BETWEEN THE FAA AND NASA WHICH WAS NOT IN…

## 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 20060531009399I](https://openairdocs.org/incident/20060531009399I), May 31, 2006: Boeing 727227 (N79754), Kansas City, MO. (-23) On may 31, 2006 express net flt 204 a B-727-200 advised ATC of a hydraulic problem after gear retraction and declared an emergency. With emergency…
- [Incident 19940127016419I](https://openairdocs.org/incident/19940127016419I), Jan 27, 1994: Boeing 727227 (N79754), Houston, TX. Narrative: aircraft taxied to 14L for departure but due to thunderstorm at the departure end of that runway, the crew was instructed to taxi to runway 32R for…
- [Accident 19930309011629A](https://openairdocs.org/incident/19930309011629A), Mar 9, 1993: Boeing 727227 (N79754), Houston, TX. TCAS issued hard resolution alert to climb. Turned on seat belt sign. Abrupt climb. Traffic T38. Passenger injured.

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