# N854AA: 1976 Boeing 727-223, registration cancelled 2018-02-21 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: February 21, 2018 - Status when cancelled: Registration expired, pending cancellation - Airframe: [Boeing 727-223](https://openairdocs.org/model/boeing-727-223) (registry code 1384074) - Data sheets: [TCDS A3WE](https://openairdocs.org/tcds/A3WE) (OpenAirDocs) - Serial number: 20995 - Year built: 1976 - Type of aircraft: Fixed wing multi engine - Airworthiness: Standard, transport - Airworthiness date: June 17, 1976 - Certificate issued: September 5, 2008 - Last registry action: October 11, 2012 - Mode S code: ABB635 - Owner when cancelled: [Exim America Corp](https://openairdocs.org/faa-owner/EXIM%20AMERICA%20CORP) - Location: [Doral, FL](https://openairdocs.org/faa-place/FL/Doral) - Owner type: Corporation - Owner's area on the map: 25.7867° N, 80.3649° W: Placed by OpenAirDocs at the center of ZIP code 33172, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N854AA - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=854AA - Page: https://openairdocs.org/deregistered/N854AA-2018-02-21 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 727-223: https://openairdocs.org/model/boeing-727-223.md ## Service difficulty reports (79, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR GAIA06002](https://openairdocs.org/sdr/GAIA06002), Feb 15, 2006: FRAME. CRACKED. DURING INSPECTION A FRAME WAS FOUND BENT AND CRACKED AT WSTA 560 BY STR 9R. ACCOMPLISHED FUSELAGE FRAME REPAIR TO STA 560, STR 9R IAW SRM. AIRCRAFT RETURNED TO - [SDR GAIA06003](https://openairdocs.org/sdr/GAIA06003), Feb 15, 2006: FRAME. CRACKED. DURING INSPECTION A FRAME WAS FOUND BENT AND CRACKED AT STA 380 BETWEEN STR6,STR7L. ACCOMPLISHED FUSELAGE FRAME REPAIR TO STA 380 BY STR 7L IAW SRM. AIRCRAFT RE - [SDR GAIA06004](https://openairdocs.org/sdr/GAIA06004), Feb 15, 2006: FRAME. CRACKED. DURING INSPECTION A FRAME WAS FOUND BENT AND CRACKED AT STA 360 BETWEEN STR 7 AND 8L. ACCOMPLISHED FUSELAGE FRAME REPAIR TO STA 360 IAW SRM. AIRCRAFT RETURNED T - [SDR GAIA05028ST](https://openairdocs.org/sdr/GAIA05028ST), Oct 27, 2005: SPAR. CRACKED. DURING B-CHECK A FUEL LEAK WAS FOUND ON THE FUSELAGE AT STA 740. INSPECTION REVEALED A CRACK ON THE WING CENTER SECTION SPAR WEB. THE WING SPAR WEB WAS REPAIRED - [SDR GAIA05027ST](https://openairdocs.org/sdr/GAIA05027ST), Oct 27, 2005: SKIN. CRACKED. DURING B-CHECK A 1 INCH CRACK WAS FOUND ON THE FUSELAGE SKIN AT STA 530 STRINGER 26R ON THE LAP SEAM BELOW THE C-1 CARGO DOOR. THE SKIN WAS REPAIRED IAW SRM. AI - [SDR GAIA05020OP](https://openairdocs.org/sdr/GAIA05020OP), Apr 23, 2005: LIGHT. INOPERATIVE. DURING PREFLIGHT, EMERGENCY EXIT LIGHTS INOPERATIVE. REMOVED AND REPLACED EMERGENCY EXIT LIGHTS. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (K) - [SDR GAIA04051OP](https://openairdocs.org/sdr/GAIA04051OP), Mar 18, 2004: SMOKE DETECTOR. INOPERATIVE. DURING CRUISE, THE UPPER DECK CARGO SMOKE WARNING LIGHT CAME ON. NO SMOKE OBSERVED ON WALK THROUGH. CREW CONTINUED NORMAL OPERATIONS. REMOVED AND REPLACED CONTR - [SDR GAIA04041OP](https://openairdocs.org/sdr/GAIA04041OP), Feb 27, 2004: SMOKE DETECTOR. INOPERATIVE. FLT 734 - FWA-DFW - DURING CRUISE, THE UPPER DECK CARGO SMOKE WARNING LIGHT CAME ON. NO SMOKE OBSERVED ON WALK THROUGH. CREW CONTINUED NORMAL OPERATIONS. REMOVE - [SDR GAIA04032OP](https://openairdocs.org/sdr/GAIA04032OP), Feb 21, 2004: ACTUATOR. OUT OF ADJUST. AIRCRAFT ROLLS TO THE LEFT WHEN THE SPEED BRAKES ARE EXTENDED. ADJUSTED THE NR 3 SPOILER ACTUATOR IAW THE BOEING MM. GROUND OPS CHECK OK. THE AIRCRAFT WAS RETUR - [SDR GAIA04031OP](https://openairdocs.org/sdr/GAIA04031OP), Feb 20, 2004: ACTUATOR. MALFUNCTIONED. AIRCRAFT ROLLS TO THE LEFT WHEN THE SPEED BRAKES ARE EXTENDED. FOUND NR 3 SPOILER ACTUATOR BYPASSING. REMOVED AND REPLACED THE NR 3 SPOILER ACTUATOR IAW THE BOE - [SDR GAIA03109OP](https://openairdocs.org/sdr/GAIA03109OP), Sep 24, 2003: BOLT. SHEARED. FLT 714 - FWA-MCO - DURING GEAR EXTENSION ON APPROACH TO MCO THE LEFT MAIN GEAR DID NOT EXTEND. THE CREW PERFORMED THE ABNORMAL CHECKLIST AND MANUALLY LOWERED T - [SDR GAIA02165OP](https://openairdocs.org/sdr/GAIA02165OP), Dec 16, 2002: LIGHT. INOPERATIVE. DURING ROUTINE MAINTENANCE AT FWA, IT WAS DISCOVERED THAT THE L1 FORWARD ENTRY EMERGENCY EXIT LIGHT WAS INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT ASSEMB - [SDR GAIA02048OP](https://openairdocs.org/sdr/GAIA02048OP), Apr 30, 2002: LIGHT. INOPERATIVE. DURING PERIODIC SERVICE CHECK MAINTENANCE FOUND THE EMERGENCY EXIT LIGHTING OVER THE LEFT NUMBER 1 DOOR INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE UNSERV - [SDR GAIA02026OP](https://openairdocs.org/sdr/GAIA02026OP), Mar 13, 2002: LIGHT. INOPERATIVE. DURING ROUTINE MAINTENANCE AT DFW, IT WAS DISCOVERED THAT THE FORWARD ENTRY DOOR EMERGENCY EXIT LIGHT WAS INOPERATIVE. REMOVED AND REPLACED THE FORWARD ENTRY EM - [SDR GAIA01244BOP](https://openairdocs.org/sdr/GAIA01244BOP), Jun 26, 2001: BATTERY. DISCHARGED. FLT 1800 - MCO-CLT - AT 75K, GOT AFT LOWER FIRE WARNING INDICATION. CREW DECLARED AN EMERGENCY. AIRCRAFT MADE AN UNEVENTFUL REJECTED TAKEOFF (75K) IN MCO. REMOV - [SDR GAIA01244AOP](https://openairdocs.org/sdr/GAIA01244AOP), Jun 1, 2001: FIRE WARNING. MALFUNCTIONED. FLT 1800 - MCO-CLT - AT 75K, GOT AFT LOWER FIRE WARNING INDICATION. CREW DECLARED AN EMERGENCY. AIRCRAFT MADE AN UNEVENTFUL REJECTED TAKEOFF (75K) IN MCO. DEFER - [SDR GAIA01040](https://openairdocs.org/sdr/GAIA01040), Jan 30, 2001: WIRE. BROKEN. FLT 1807 - DEN-PHX - RED NOSE GEAR LIGHT ILLUMINATED, GREEN NOSE GEAR LIGHT NOT ILLUMINATED ON PRIOR TO LANDING. AIRCRAFT MADE AN UNEVENTFUL LANDING IN PHX. FOU - [SDR GAIA00291](https://openairdocs.org/sdr/GAIA00291), May 24, 2000: BEAM. CORRODED. DURING LIGHT C-CHECK AT TIMCO/OSC THE FOLLOWING DISCREPANCY WAS FOUND, FASTENER HOLES FOR RIGHT WALKING BEAM PANEL HAS CORROSION ON LANDING GEAR BEAM. REPAIRED - [SDR GAIA00292](https://openairdocs.org/sdr/GAIA00292), May 24, 2000: ANGLE. CORRODED. DURING LIGHT C-CHECK AT TIMCO/OSC THE FOLLOWING DISCREPANCY WAS FOUND, STA 294 TO STA 303, RBL 17 INSIDE TORQUE BOX HAS CORROSION ON TOP ANGLE. REPAIRED ANGLE I - [SDR GAIA00293](https://openairdocs.org/sdr/GAIA00293), May 24, 2000: ANGLE. CORRODED. DURING LIGHT C-CHECK AT TIMCO/OSC, THE FOLLOWING DISCREPANCY WAS FOUND, BODY STATION 294.5 TO BS 351.2 RIGHT WALKWAY SUPPORT ANGLE HAS CORROSION. REPAIRED ANGLE - [SDR GAIA00294](https://openairdocs.org/sdr/GAIA00294), May 24, 2000: BEAM. CORRODED. DURING LIGHT C-CHECK AT TIMCO/OSC, THE FOLLOWING DISCREPANCY WAS FOUND, LEFT WALKING BEAM PANEL ATTACH HOLES ON BEAM HAS CORROSION. REPAIRED BEAM IAW TIMCO REO - [SDR GAIA00284](https://openairdocs.org/sdr/GAIA00284), May 24, 2000: LIGHT. INOPERATIVE. FLT 1807 - CLT-MIA - COCKPIT EMERGENCY EXIT LIGHT DOES NOT ILLUMINATE. REMOVED AND REPLACED COCKPIT EMERGENCY EXIT LIGHT. OPS CHECK GOOD IAW B727 MM. AIRCRAFT R - [SDR GAIA00285](https://openairdocs.org/sdr/GAIA00285), May 24, 2000: ANGLE. CRACKED. DURING LIGHT C-CHECK AT TIMCO/OSC, THE FOLLOWING DISCREPANCY WAS FOUND, TOP CAP ANGLE FORWARD SPAR RUDDER STATION 254 CAP ANGLE CRACKED. REPAIRED ANGLE IAW TIMC - [SDR GAIA00286](https://openairdocs.org/sdr/GAIA00286), May 24, 2000: SKIN. CORRODED. DURING LIGHT C-CHECK AT TIMCO/OSC THE FOLLOWING DISCREPANCY WAS FOUND, CORROSION ON FUSELAGE SKIN AT BS 440 CIRCUMFERENTIAL JOINT BETWEEN STRINGER 24L TO STRING - [SDR GAIA00287](https://openairdocs.org/sdr/GAIA00287), May 24, 2000: SKIN. PUNCTURED. DURING LIGHT C-CHECK AT TIMCO/OSC THE FOLLOWING DISCREPANCY WAS FOUND, FUSELAGE STATION 550 9 INCHES ABOVE STATIC PORT RIGHT SIDE HAS PUNCTURE. REPAIRED STATIC - [SDR GAIA00288](https://openairdocs.org/sdr/GAIA00288), May 24, 2000: STIFFENER. CRACKED. DURING LIGHT C-CHECK AT TIMCO/OSC, THE FOLLOWING DISCREPANCY WAS FOUND, RIGHT NLG TRUNNION SUPPORT VERTICAL STIFFENER CRACKED. REPAIRED TRUNNION SUPPORT STIFFEN - [SDR GAIA00289](https://openairdocs.org/sdr/GAIA00289), May 24, 2000: FITTING. CORRODED. DURING LIGHT C-CHECK AT TIMCO/OSC, THE FOLLOWING DISCREPANCY WAS FOUND, NLG RIGHT TRUNNION SUPPORT FITTING HAS PITTING CORROSION ON FLANGE. REPAIRED SUPPORT FIT - [SDR GAIA00290](https://openairdocs.org/sdr/GAIA00290), May 24, 2000: FRAME. CORRODED. DURING LIGHT C-CHECK AT TIMCO/OSC, THE FOLLOWING DISCREPANCY WAS FOUND. CORROSION ON LOWER FLANGE OF FRAME AT STA 950C STRINGER 29L. REPAIRED FRAME IAW SRM 53-1 - [SDR GAIA00273](https://openairdocs.org/sdr/GAIA00273), Apr 28, 2000: FLOORBEAM. DAMAGED. DURING LIGHT C-CHECK AT TIMCO/OSC, THE FOLLOWING DISCREPANCY WAS FOUND, ELONGATED HOLE IN FLOORBEAM AT STATION 360 LBL 45. REPAIRED FLOORBEAM PER IAW SRM 53-10- - [SDR GAIA00261](https://openairdocs.org/sdr/GAIA00261), Apr 28, 2000: FRAME. DENTED. DURING LIGHT C-CHECK AT TIMCO/OSC THE FOLLOWING DISCREPANCY WAS FOUND, DENT IN BELT FRAME STATION 1090 BETWEEN STRINGER 26 AND 27R. REPAIRED FRAME PER IAW SRM 5 - [SDR GAIA00262](https://openairdocs.org/sdr/GAIA00262), Apr 28, 2000: FRAME. DENTED. DURING LIGHT C-CHECK AT TIMCO/OSC THE FOLLOWING DISCREPANCY WAS FOUND, BS 520 FRAME DENTED JUST BELOW STRINGER 16R. REPAIRED FRAME PER IAW SRM 51-40-3. THIS AIR - [SDR GAIA00263](https://openairdocs.org/sdr/GAIA00263), Apr 28, 2000: FLAP TRACK. CORRODED. DURING LIGHT C-CHECK AT TIMCO/OSC, THE FOLLOWING DISCREPANCY WAS FOUND, NR 4 FLAP TRACK FORWARD MOUNT BOLT HOLES HAS CORROSION. REPAIRED FLAP TRACK PER IAW S/B - [SDR GAIA00264](https://openairdocs.org/sdr/GAIA00264), Apr 28, 2000: FRAME. MISDRILLED. DURING LIGHT C-CHECK AT TIMCO/OSC THE FOLLOWING DISCREPANCY WAS FOUND, BS 600 FRAME HAS BEEN DRILLED INTO NEAR STRINGER 16R. REPAIRED FRAME PER IAW SRM 51-20-1 - [SDR GAIA00265](https://openairdocs.org/sdr/GAIA00265), Apr 28, 2000: FRAME. MISDRILLED. DURING LIGHT C-CHECK AT TIMCO/OSC, THE FOLLOWING DISCREPANCY WAS FOUND AT STATION 700 STRINGER 16L FRAME HAS HOLES ON INBOARD CHORD. REPAIRED FRAME PER IAW SRM - [SDR GAIA00266](https://openairdocs.org/sdr/GAIA00266), Apr 28, 2000: FRAME. MISDRILLED. DURING LIGHT C-CHECK AT TIMCO/OSC THE FOLLOWING DISCREPANCY WAS FOUND, STATION 720E STRINGER 16L FRAME HAS HOLES ON INBOARD CHORD. REPAIRED FRAME PER IAW SRM 51 - [SDR GAIA00267](https://openairdocs.org/sdr/GAIA00267), Apr 28, 2000: FRAME. CRACKED. DURING LIGHT C-CHECK AT TIMCO/OSC THE FOLLOWING DISCREPANCY WAS FOUND, STATION 1166 STRINGER 16L FRAME CRACKED. REPAIRED FRAME PER IAW 51-40-3. THIS AIRCRAFT WA - [SDR GAIA00268](https://openairdocs.org/sdr/GAIA00268), Apr 28, 2000: FRAME. MISDRILLED. DURING LIGHT C-CHECK AT TIMCO/OSC THE FOLLOWING DISCREPANCY WAS FOUND, STATION 1030 STRINGER 16L FRAME HAS FIGURE EIGHT HOLE. REPAIRED FRAME PER IAW TIMCO REO S - [SDR GAIA00269](https://openairdocs.org/sdr/GAIA00269), Apr 28, 2000: FRAME. DENTED. DURING LIGHT C-CHECK AT TIMCO/OSC, THE FOLLOWING DISCREPANCY WAS FOUND, STATION 580 BETWEEN STRINGER 9R AND STRINGER 10R CIRCUMFERENTIAL DENTED. REPAIRED FRAME - [SDR GAIA00270](https://openairdocs.org/sdr/GAIA00270), Apr 28, 2000: FRAME. DAMAGED. DURING LIGHT C-CHECK AT TIMCO/OSC, THE FOLLOWING DISCREPANCY WAS FOUND, STATION 1148 STRINGER 16L FRAME HAS HOLES ON INBOARD CHORD. REPAIRED FRAME PER IAW SRM 5 - [SDR GAIA00271](https://openairdocs.org/sdr/GAIA00271), Apr 28, 2000: WEB. CRACKED. DURING LIGHT C-CHECK AT TIMCO/OSC, THE FOLLOWING DISCREPANCY WAS FOUND, WEB CRACKED BS 580 TO BS 600 STRINGER 29L. REPAIRED WEB PER IAW SRM 51-30-2. THIS AIRCRA - [SDR GAIA00272](https://openairdocs.org/sdr/GAIA00272), Apr 28, 2000: FRAME. MISDRILLED. DURING LIGHT C-CHECK AT TIMCO/OSC, THE FOLLOWING DISCREPANCY WAS FOUND, TWO FIGURE EIGHT HOLES IN FRAME BS 560, STRINGER 26R. REPAIRED FRAME PER IAW TIMCO REO S - [SDR GAIA00274](https://openairdocs.org/sdr/GAIA00274), Apr 28, 2000: ANGLE. CORRODED. DURING LIGHT C-CHECK AT TIMCO/OSC, THE FOLLOWING DISCREPANCY WAS FOUND, CORROSION ON ANGLE UNDER RIGHT SIDE SUPPORT ABOVE STRINGER 26R AT BS 735. REPAIRED ANGLE - [SDR GAIA00242](https://openairdocs.org/sdr/GAIA00242), Apr 27, 2000: FRAME. DENTED. DURING LIGHT C-CHECK TIMCO/OSC THE FOLLOWING DISCREPANCY WAS FOUND, FUSELAGE FRAME AT BS 360 IS DENTED JUST ABOVE FLOOR LEVEL LEFT SIDE. REPAIRED FRAME PER IAW - [SDR GAIA00221](https://openairdocs.org/sdr/GAIA00221), Apr 25, 2000: STRINGER. PUNCTURED. DURING LIGHT C-CHECK AT TIMCO/OSC, THE FOLLOWING DISCREPANCY WAS FOUND, SPLICE ON STRINGER 28R HAS PUNCTURE ON INBOARD UPPER RADIUS AFT OF BS 480 FORWARD PIT. R - [SDR GAIA00222](https://openairdocs.org/sdr/GAIA00222), Apr 25, 2000: FRAME. CRACKED. DURING LIGHT C-CHECK AT TIMCO/OSC, THE FOLLOWING DISCREPANCY WAS FOUND, FUSELAGE FRAME AT BS 380 BETWEEN STRINGER 5 AND STRINGER 6 IS DENTED AND CRACKED. REPAIR - [SDR GAIA00223](https://openairdocs.org/sdr/GAIA00223), Apr 25, 2000: FRAME. CRACKED. DURING LIGHT C-CHECK AT TIMCO/OSC THE FOLLOWING DISCREPANCY WAS FOUND, FUSELAGE FRAME AT BS 400 BETWEEN STRINGER 5 AND STRINGER 6 DENTED AND CRACKED. REPAIRED F - [SDR GAIA00224](https://openairdocs.org/sdr/GAIA00224), Apr 25, 2000: SHEAR TIE. CRACKED. DURING LIGHT C-CHECK AT TIMCO/OSC, THE FOLLOWING DISCREPANCY WAS FOUND, CRACKED SHEAR TIE ON FORWARD SIDE OF BELLY FRAME AT BS 1030, LBL 6. REPAIRED SHEAR TIE I - [SDR GAIA00225](https://openairdocs.org/sdr/GAIA00225), Apr 25, 2000: HINGE FITTING. DAMAGED. DURING LIGHT C-CHECK AT TIMCO/OSC THE FOLLOWING DISCREPANCY WAS FOUND LEFT MLG WING DOOR FORWARD HINGE FITTING ATTACH HOLES ELONGATED ON FLAP TRACK. REPAIRED HI - [SDR GAIA00226](https://openairdocs.org/sdr/GAIA00226), Apr 25, 2000: SEAT TRACK. GOUGED. DURING LIGHT C-CHECK AT TIMCO/OSC THE FOLLOWING DISCREPANCY WAS FOUND, SEAT TRACK GOUGED AT BS 763, LBL 24. REPAIRED SEAT TRACK IAW SRM 53-10-5. THE AIRCAFT WAS - [SDR GAIA00227](https://openairdocs.org/sdr/GAIA00227), Apr 25, 2000: ATTACH FITTING. DAMAGED. DURING LIGHT C-CHECK AT TIMCO/OSC, THE FOLLOWING DISCREPANCY WAS FOUND, RIGHT ELEVATOR NR 1 ATTACH FITTING ON HORIZONTAL HAS INBOARD HOLE ELONGATED. OUTBOARD HO All 79: https://openairdocs.org/deregistered/N854AA-2018-02-21/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 IAD76AI091](https://openairdocs.org/ntsb/IAD76AI091), Aug 8, 1976: Boeing 727 (N854AA), Bethlehem, PA, no damage ## FAA accident and incident reports (4) 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 19920918050149I](https://openairdocs.org/incident/19920918050149I), Sep 18, 1992: Boeing 727223 (N854AA), Nashville, TN. Pilot found NR3 wheeltire assembly missing on gate arrival. Assembly found on runway. Safety bolt still attached. - [Incident 19850607027769I](https://openairdocs.org/incident/19850607027769I), Jun 7, 1985: Boeing 727223 (N854AA), Las Vegas, NV. Engine strut overheat light came on. Found 13 stage bleed air valve sense line broken with hot air going to loop. - [Incident 19820830046299I](https://openairdocs.org/incident/19820830046299I), Aug 30, 1982: Boeing 727223 (N854AA), Dallas, TX, Minor damage. Pilot shut down engine due to loss of oil pressure and high EGT. Pneumatic duct failed and cut engine oil line. - [Incident 19800924070789I](https://openairdocs.org/incident/19800924070789I), Sep 24, 1980: Boeing 727223 (N854AA), Chicago, IL. Engine shutdown after compressor stall in climb. Overweight landing made, replaced burner pressure fitting. ## Other aircraft with N854AA - [Registered now](https://openairdocs.org/aircraft/N854AA): Anduril Industries ROADRUNNER, S/N 4007 --- 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.