# N76752: Boeing 727-227, registration cancelled 2006-09-25 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: September 25, 2006 - 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: 21248 - Type of aircraft: Fixed wing multi engine - Certificate issued: September 5, 2006 - Last registry action: September 5, 2006 - Mode S code: AA5EAB - 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/N76752 - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=76752 - Page: https://openairdocs.org/deregistered/N76752-2006-09-25 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 (97, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR XN0A1329](https://openairdocs.org/sdr/XN0A1329), May 12, 2006: START VALVE. MALFUNCTIONED. ON PUSHBACK AT PHL COULD NOT GET NR 1 START VALVE TO OPEN ELECTRICALLY. COULD NOT DUPLICATE, OPERATED NR 1 START VALVE NUMEROUS TIMES, SYSTEM OPS CHECK GOOD IAW - [SDR XN0A1320](https://openairdocs.org/sdr/XN0A1320), Apr 20, 2006: BRAKE ASSY. DRAGGING. ON TAXI OUT AIRCRAFT BRAKES SEEMED TO DRAG, AIRCRAFT CAME TO A STOP. REMOVED AND REPLACED NR 1 BRAKE ASSY IAW B727 MM CHAPTER 32-41-32. REMOVED AND REPLACED NR - [SDR XN0A1920](https://openairdocs.org/sdr/XN0A1920), Apr 20, 2006: BRAKE ASSY. DRAGGING. ON TAXI OUT AIRCRAFT BRAKES SEEMED TO DRAG, AIRCRAFT CAME TO A STOP. REMOVED AND REPLACED NR 1 BRAKE ASSY IAW B727 MM CHAPTER 32-41-32. REMOVED AND REPLACED NR - [SDR XN0A1284](https://openairdocs.org/sdr/XN0A1284), Dec 14, 2005: SWITCH. INOPERATIVE. AMBER LE LIGHT ON WITH FLAPS SET TO 15 DEGREES. NR 6 LE SLAT DOES NOT INDICATE EXTEND. REPLACED NR 6 SLAT POSITION INDICATING SWITCH. OPS CHECKS GOOD IAW MM CHA - [SDR XN0A1263](https://openairdocs.org/sdr/XN0A1263), Sep 13, 2005: CABIN PRESSURE. MALFUNCTIONED. AIRCRAFT WOULD NOT PRESSURIZE IN ANY MODE - AUTO, STANDBY OR MANUAL AC OR DC. TRANSFERRED TO MEL 5718 IAW MEL 21-16-2D. PLACARDS INSTALLED CAT-C. - [SDR XN0A1254](https://openairdocs.org/sdr/XN0A1254), Aug 10, 2005: BRAKE ASSY. VIBRATES. ON TAXIOUT, BRAKES VIBRATE WHEN APPLIED. BLED BRAKES AS REQ'D IAW B727 MM REF 32-41-0, SYSTEM OPS CHECKS GOOD. - [SDR XN0A1253](https://openairdocs.org/sdr/XN0A1253), Aug 9, 2005: EXCITER. FAILED. ON ENGINE START NR 2 ENGINE WOULD NOT START, START VALVE OPENS PRESSURE DROP NO EGT. REMOVED AND REPLACED NR 2 ENG EXCITER BOX IAW MM 74-11-1, OPS GOOD. - [SDR XN0A1236](https://openairdocs.org/sdr/XN0A1236), May 13, 2005: WARNING LIGHT. ILLUMINATED. DURING EMERGENCY DESCENT, LT DUCT OVERHEAT LIGHT TRIP, PERFORMED ALL CHECKLIST. - [SDR XN0A1235](https://openairdocs.org/sdr/XN0A1235), May 11, 2005: IGNITION UNIT. MALFUNCTIONED. NR 2 ENGINE WILL NOT START, NO IGNITION. NR 2 ENGINE IGNITION CB'S RESET, OP'S CHECK GOOD. - [SDR XNOA1225](https://openairdocs.org/sdr/XNOA1225), May 11, 2005: ENGINE. INOPERATIVE. NR 2 ENGINE WILL NOT START, NO IGNITION. NR 2 ENGINE IGNITION CB'S RESET, OP'S CHECK GOOD. - [SDR XNOA1231](https://openairdocs.org/sdr/XNOA1231), Apr 14, 2005: SELECTOR SWITCH. BURNED OUT. AFTER STARTING NR 3 ENGINE, AC FREQUENCY METER PEGGED OUT AND SMOKE POURED OUT OF FREQ (AC) SELECTOR SWITCH. REMOVED AND REPLACED AC FREQ METER SELECTOR SWITCH - [SDR XN0A1227](https://openairdocs.org/sdr/XN0A1227), Dec 24, 2004: WARNING LIGHT. ILLUMINATED. NR 3 ENGINE CSD LOW PRESSURE WARNING LIGHT ON WITH NO FREG. DISCONNECTED NR 3 CSD DEFERRED NR 3 GENERATOR INOP IAW ENA B727 MEL 24-1 PROCEDURES DMI 4858 CAT-B I - [SDR XNOA1183](https://openairdocs.org/sdr/XNOA1183), Apr 13, 2004: SWITCH. OUT OF ADJUST. DURING CLIMB, MAIN CARGO DOOR LIGHT ILLUMINATED. ADJUSTED DOOR CLOSED SWITCH IAW HAMILTON-TIMCO SUPPLEMENTAL MM 7-11-1. OPS CHECKS GOOD IAW HAMILTON TIMCO-SUPPL - [SDR XNOA1179](https://openairdocs.org/sdr/XNOA1179), Mar 5, 2004: ENGINE. MALFUNCTIONED. NR 2 ENGINE WILL NOT ACHIEVE TAKE-OFF POWER. PERFORMED NR 2 ENGINE RUN. NR 2 ENGINE MAKES ITS TARGET POWER IAW P&W JT8D MM 72-00-00. NO DEFECTS NOTED. (STATUS: - [SDR CALA9801670](https://openairdocs.org/sdr/CALA9801670), Sep 9, 1998: HYD LINE. LEAKING. THE A HYDRAULIC SYSTEM WAS LOST ON FINAL APPROACH TO EWR. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 2 ENGINE A SYSTEM HYDRAULIC PRESSURE LI - [SDR CALA9800736](https://openairdocs.org/sdr/CALA9800736), May 3, 1998: HYD LINE. LEAKING. LOSS OF A-SYSTEM HYDRAULIC FLUID UPON RETRACTING THE LANDING GEAR. REMOVED AND REPLACED TAIL SKID RIGHT HYDRAULIC LINE PER MM 32-71-12. - [SDR CALA9800138](https://openairdocs.org/sdr/CALA9800138), Jan 29, 1998: BULKHEAD. CRACKED. INSPECTION FOUND, A 1 CRACK IN FORWARD FACE OF STA 1183 BULKHEAD ON RT SIDE ABOVE OUTFLOW VALVE. A WEB REPAIR WAS INSTALLED IAW BOEING DRAWING NR 65C31446, SRM - [SDR CALA9800129](https://openairdocs.org/sdr/CALA9800129), Jan 27, 1998: BATTERY PACK. DISCHARGED. INSPECTION FOUND, THE AFT ENTRY EMERGENCY EXIT LIGHT BATTERY PACK INOPERATIVE. THE BATTERY PACK WAS REMOVED AND REPLACED. - [SDR CALA9800128](https://openairdocs.org/sdr/CALA9800128), Jan 27, 1998: RIB. CRACKED. INSPECTION FOUND A 2 INCH CRACK AT FASTENER OF RT WING LEADING EDGE RIB, INBOARD OF NR 4 LEADING EDGE FLAP, AT L/E STA 130. THE CRACKED AREA WAS REMOVED. A REPA - [SDR CALA9800127](https://openairdocs.org/sdr/CALA9800127), Jan 27, 1998: SKIN. CRACKED. INSPECTION FOUND A .5, 1, AND 2 CRACK IN RT SIDE OF VERTICAL STABILIZER SKIN LOWER SECTION AT STA 1343. THE AREA WAS REPAIRED IAW ECRA 5530-01190. - [SDR CALA9800126](https://openairdocs.org/sdr/CALA9800126), Jan 27, 1998: STOP. CRACKED. INSPECTION FOUND A 1 CRACK IN L-1 AFT UPPER DOOR STOP AT FITTING. THE L-1 AFT UPPER DOOR STOP WAS REMOVED AND REPLACED IAW SRM 52-40-1. - [SDR CALA9800105](https://openairdocs.org/sdr/CALA9800105), Jan 24, 1998: RIB. CRACKED. INSPECTION FOUND A 2 INCH CRACK AT FASTENER IN RT WING RIB INBOARD OF NR 4 LEADING EDGE FLAP AT L/E STA 130. THE CRACKED AREA WAS REMOVED, A REPAIR WAS FABRICAT - [SDR CALA9800078](https://openairdocs.org/sdr/CALA9800078), Jan 16, 1998: BRACKET. CRACKED. INSPECTION FOUND A .2812 INCH CRACK OUTBOARD OF NR 8 SPOILER ACTUATOR IN RT WING INBOARD TRAILING EDGE PANEL SUPPORT BRACKET AT WS 232. THE CRACK WAS STOP DRILL - [SDR CALA9800077](https://openairdocs.org/sdr/CALA9800077), Jan 16, 1998: SKIN. CRACKED. INSPECTION FOUND A 2 INCH CRACK IN RT WING LEADING EDGE LOWER SKIN ABOVE NR 5 LEADING EDGE FLAP ACTUATOR, WS 224. THE CRACKED AREA WAS REMOVED AND A DOUBLER WAS - [SDR CALA9800076](https://openairdocs.org/sdr/CALA9800076), Jan 16, 1998: ANGLE. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN FRAME TO FUSELAGE ATTACH ANGLE IN AFT STAIR COMPARTMENT, RT SIDE, STA 1283. THE ANGLE WAS REMOVED, AN ANGLE REPAIR WAS FABRIC - [SDR CALA9800075](https://openairdocs.org/sdr/CALA9800075), Jan 15, 1998: LIGHT. INOPERATIVE. INSPECTION FOUND EMERGENCY FLOOD LIGHT AT LEFT SIDE OVER AFT AIRSTAIRS INOPERATIVE. THE LIGHT ASSEMBLY WAS REMOVED AND REPLACED. - [SDR CALA9800073](https://openairdocs.org/sdr/CALA9800073), Jan 15, 1998: RIB. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN RT WING LEADING EDGE RIB OUTBOARD OF NR 6 LEADING EDGE SLAT STA 234. AN ANGLE DOUBLER WAS INSTALLED IAW SRM 51-40-3. - [SDR CALA9800072](https://openairdocs.org/sdr/CALA9800072), Jan 15, 1998: RIB. CRACKED. INSPECTION FOUND A .75 INCH CRACK IN RT WING LEADING EDGE RIB OUTBOARD OF BOTTLE PIN ABOVE PNEUMATIC DUCT FORWARD SUPPORT BRACKET AT FSS 106.8. A REPAIR WAS INS - [SDR CALA9800071](https://openairdocs.org/sdr/CALA9800071), Jan 15, 1998: SKIN. CRACKED. INSPECTION FOUND A .25 INCH CRACK IN RT WING LEADING EDGE SKIN AT NR 6 SLAT OUTBOARD HOOK. THE CRACK WAS STOP DRILLED PER SRM 51-10-1, A DOUBLER REPAIR WAS FABR - [SDR CALA9800070](https://openairdocs.org/sdr/CALA9800070), Jan 15, 1998: SKIN. BENT. INSPECTION FOUND LT WING OUTBOARD AILERON TAB LOWER LEADING EDGE SKIN BENT AND DEBONDED. THE AILERON TAB WAS REMOVED AND REPLACED IAW MM 27-10-41. - [SDR CALA9800067](https://openairdocs.org/sdr/CALA9800067), Jan 15, 1998: STRINGER. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN RT SIDE OF VERTICAL STABILIZER STRINGER NR 9 BETWEEN RIB NR 7 AND NR 8. THE CRACK WAS LOCATED AT ATTACH BOLT. THE FASTENERS W - [SDR CALA9800066](https://openairdocs.org/sdr/CALA9800066), Jan 15, 1998: STRINGER. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN LT SIDE OF VERTICAL STABILIZER STRINGER NR 8 BETWEEN RIB NR 8 AND NR 9. THE FASTENERS WERE REMOVED AND A REPAIR WAS FABRICATE - [SDR CALA9800064](https://openairdocs.org/sdr/CALA9800064), Jan 14, 1998: STRINGER. CRACKED. INSPECTION FOUND A .5 INCH CRACK AT FASTENER HOLE IN LT WING SECOND UPPER STRINGER FROM REAR SPAR ABOVE RIB AT WS 629. THE FASTENERS AND CLAMPS WERE REMOVED IAW - [SDR CALA9800063](https://openairdocs.org/sdr/CALA9800063), Jan 14, 1998: STRINGER. CRACKED. INSPECTION FOUND A .75 INCH CRACK IN RT WING STRINGER AT WS 656.5, TOP OF RIB ATTACH POINT ACCESS THROUGH PANEL 7617. THE CRACK WAS STOP DRILLED AND THE AREA WA - [SDR CALA9800062](https://openairdocs.org/sdr/CALA9800062), Jan 14, 1998: RIB. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN RT WING LEADING EDGE RIB OUTBOARD OF BOTTLE PIN LOWER EDGE AT FSS 106.8. AN ANGLE REPAIR WAS INSTALLED IAW SRM 51-40-3. - [SDR CALA9800061](https://openairdocs.org/sdr/CALA9800061), Jan 14, 1998: RIB. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN WING LEADING EDGE RIB INBOARD OF NR 4 LEADING EDGE FLAP AT LEADING EGDE STA 130. THE CRACK WAS STOP DRILLED AND AN ANGLE WAS - [SDR CALA9800060](https://openairdocs.org/sdr/CALA9800060), Jan 14, 1998: SKIN. CRACKED. INSPECTION FOUND FOUR .5 INCH CRACKS AROUND FASTENERS OUTBOARD OF LAMP LIGHT IN WING LEADING EDGE INTERNAL SKIN AT FSS 106. THE CRACKED AREAS WERE CUT OUT. REPA - [SDR CALA9800059](https://openairdocs.org/sdr/CALA9800059), Jan 14, 1998: RIB. CRACKED. INSPECTION FOUND A .5 INCH CRACK INSIDE LT WING LEADING EDGE AT RIB LEADING EDGE STA 130 ABOVE HOT AIR DUCT PLENUM. ALSO, A .5 INCH CRACK WAS FOUND INSIDE LT WI - [SDR CALA9800058](https://openairdocs.org/sdr/CALA9800058), Jan 14, 1998: SKIN. CRACKED. INSPECTION FOUND A 2 INCH CRACK IN LEADING EDGE SKIN AT DOUBLER STRAP INSIDE LT WING DIRECTLY ABOVE NR 2 LEADING EDGE FLAP ACTUATOR AT WS 224. THE CRACKED DOUBL - [SDR CALA9800057](https://openairdocs.org/sdr/CALA9800057), Jan 14, 1998: STRINGER. CRACKED. INSPECTION FOUND A .5 INCH CRACK AT FASTENER HOLE IN LT WING FIRST UPPER STRINGER FROM REAR SPAR, ABOVE RIB AT WS 656.50. THE FASTENERS AND CLAMPS WERE REMOVED. - [SDR CALA9800056](https://openairdocs.org/sdr/CALA9800056), Jan 14, 1998: SKIN. CRACKED. INSPECTION FOUND A .25 INCH CRACK AT LT WING FIXED UPPER LEADING EDGE SKIN AT AFT END OF CUTOUT WHERE NR 4 SLAT OUTBOARD HOOK ATTACHES. A DOUBLER WAS INSTALLED - [SDR CALA9800055](https://openairdocs.org/sdr/CALA9800055), Jan 14, 1998: SKIN. CRACKED. INSPECTION FOUND A .25 INCH CRACK AT LT WING FIXED UPPER LEADING EDGE SKIN AT AFT END OF CUTOUT WHERE NR 3 SLAT INBOARD HOOK ATTACHES. A REPAIR WAS FABRICATED A - [SDR CALA9800054](https://openairdocs.org/sdr/CALA9800054), Jan 14, 1998: SKIN. CORRODED. INSPECTION FOUND LT WING INBOARD MIDFLAP SKIN CORRODED OUTBOARD OF INBOARD CARRIAGE MOUNT AREA. A SKIN REPAIR WAS INSTALLED IAW SRM 57-50-4. - [SDR CALA9800053](https://openairdocs.org/sdr/CALA9800053), Jan 14, 1998: BRACKETS. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN INBOARD AND OUTBOARD BRACKETS WHERE LT WING NR 2 LEADING EDGE FLAP ACTUATOR MOUNTS. NEW BRACKETS WERE FABRICATED AND INSTALL - [SDR CALA9800052](https://openairdocs.org/sdr/CALA9800052), Jan 14, 1998: BRACKETS. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN INBOARD AND OUTBOARD BRACKETS WHERE LT WING NR 1 LEADING EDGE FLAP ACTUATOR MOUNTS. THE BRACKETS WERE REMOVED AND REPLACED I - [SDR CALA9800051](https://openairdocs.org/sdr/CALA9800051), Jan 14, 1998: GUSSET. CRACKED. INSPECTION FOUND A .5 INCH CRACK AT TOP CORNER AND A .5 INCH CRACK AT LOWER CORNER OF GUSSET ON RT SIDE OF VERTICAL STABILIZER AT STRINGER 9 BETWEEN RIB NR 6 AN - [SDR CALA9800050](https://openairdocs.org/sdr/CALA9800050), Jan 14, 1998: SUPPORT. CORRODED. INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 996, RBL 36. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 51-10-1 A - [SDR CALA9800049](https://openairdocs.org/sdr/CALA9800049), Jan 14, 1998: STRINGER. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN STRINGER 15L AND 15R AT STA 720B. THE CRACKED AREAS WERE CUT OUT, REPAIR PARTS WERE FABRICATED AND INSTALLED IAW SRM 51-10-2 - [SDR CALA9800048](https://openairdocs.org/sdr/CALA9800048), Jan 14, 1998: STRINGER. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN END OF STRINGER 15L AT STA 720C. THE CRACKED AREA WAS CUT OUT, A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-10-2 AND 53- - [SDR CALA9800047](https://openairdocs.org/sdr/CALA9800047), Jan 14, 1998: DOUBLER. CRACKED. INSPECTION FOUND THREE CRACKS AT HI-LOKS ON DOUBLER UPPER SIDE OF CARGO DOOR FRAME CUTOUT BETWEEN FS 604 TO 608, STRINGER 10R. THE CRACKS WERE .25 TO 1 INCH LON All 97: https://openairdocs.org/deregistered/N76752-2006-09-25/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 MIA95IA134](https://openairdocs.org/ntsb/MIA95IA134), May 19, 1995: Boeing 727-227 (N76752), Brooksville, FL, incident, no damage. Probable cause: AN ELDERLY PASSENGER LOSING HIS BALANCE AS THE AIRCRAFT OPERATED IN SMOOTH AIR. ## FAA accident and incident reports (2) 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 19950519013729I](https://openairdocs.org/incident/19950519013729I), May 19, 1995: Boeing 727227 (N76752), Brooksville, FL. (.4) While the flight was cruising in smooth air, an elderly passenger fell as he exited the lavatory. It was later determined that he experience a broken hip. - [Incident 19911121057879I](https://openairdocs.org/incident/19911121057879I), Nov 21, 1991: Boeing 727222 (N76752), Kansas City, MO. High voltage in ac generating system,returned. NR1 generator placarded inoperative. ## Other aircraft with N76752 - [Cancelled 1985-05-22](https://openairdocs.org/deregistered/N76752-1985-05-22): Cessna 140, S/N 11184. Owner: [Francis Gerald C](https://openairdocs.org/faa-owner/FRANCIS%20GERALD%20C), [Lansing, MI](https://openairdocs.org/faa-place/MI/Lansing) --- 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.