# N899AA: 1980 Boeing 727-223, registration cancelled 2013-05-01

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: May 1, 2013
- Exported to: Canada
- Status when cancelled: Valid registration
- 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: 22015
- Year built: 1980
- Type of aircraft: Fixed wing multi engine
- Airworthiness: Standard, transport
- Airworthiness date: October 1, 1980
- Certificate issued: March 23, 2011
- Last registry action: March 23, 2011
- Mode S code: AC66C4
- Owner when cancelled: [Cargo Aircraft Management Inc](https://openairdocs.org/faa-owner/CARGO%20AIRCRAFT%20MANAGEMENT%20INC)
- Location: [Orlando, FL](https://openairdocs.org/faa-place/FL/Orlando)
- Owner type: Corporation
- Owner's area on the map: 28.4899° N, 81.2902° W: Placed by OpenAirDocs at the center of ZIP code 32822, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N899AA
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=899AA
- Page: https://openairdocs.org/deregistered/N899AA-2013-05-01

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 727-223: https://openairdocs.org/model/boeing-727-223.md

## Service difficulty reports (71, newest 50)

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

- [SDR FOTR2111712809](https://openairdocs.org/sdr/FOTR2111712809), Aug 1, 2011: SKIN. DEBONDED. LT INBD FOREFLAP T/E HAS AREA OF DEBONDED JUST INBD OF PREVIOUS REPAIR WBL 135.0. REPAIRED ON FASI WO 21117, NR 12809.
- [SDR FOTR2111712633](https://openairdocs.org/sdr/FOTR2111712633), Jul 29, 2011: STRINGER. CORRODED. CORROSION ON OTBD SIDE OF STRINGER 28L AT BS 450. REPAIRED ON FASI WO 21117, NR 12633.
- [SDR FOTR2111712782](https://openairdocs.org/sdr/FOTR2111712782), Jul 27, 2011: TAB. DELAMINATED. LT ELEVATOR CONTROL TAB HAS A SMALL AREA OF DELAMINATION, REPAIRED ON FASI WO 21117, NR 12782.
- [SDR FOTR2111712656](https://openairdocs.org/sdr/FOTR2111712656), Jul 25, 2011: FRAME. DENTED. AFT CARGO COMPARTMENT HAS DENTS AT STA 1010 BETWEEN STR 25R AND 24R. REPAIRED ON FASI WO 21117, NR 12656.
- [SDR FOTR2111712657](https://openairdocs.org/sdr/FOTR2111712657), Jul 25, 2011: FRAME. DENTED. AFT CARGO COMPARTMENT- DENT ON FRAME STA 1030 BETWEEN STR 25R AND 24R. REPAIRED ON FASI WO 21117, NR 12657.
- [SDR FOTR2111712350](https://openairdocs.org/sdr/FOTR2111712350), Jul 25, 2011: MOUNT BRACKET. CRACKED. NR 6 SLAT ACTUATOR ATTACHED MOUNT BRACKET, ON SLAT INBD SIDE IS CRACKED, WS519.0. REPAIRED ON FASI WO 21117, NR 12350.
- [SDR FOTR2111712661](https://openairdocs.org/sdr/FOTR2111712661), Jul 25, 2011: FRAME. DENTED. AFT. CARGO COMPARTMENT- DENT ON FRAME AT STA 1010 AT STR 25L. REPAIRED ON FASI WO 21117, NR 12661.
- [SDR FOTR2111712345](https://openairdocs.org/sdr/FOTR2111712345), Jul 25, 2011: BRACKET. CRACKED. NR 7 SLAT ACTUATOR MOUNT INBD BRACKET ON SLAT IS CRACKED. REPAIRED ON FASI WO 21117, NR 12345.
- [SDR FOTR2111712726](https://openairdocs.org/sdr/FOTR2111712726), Jul 25, 2011: BRACKET. CRACKED. NR 7 SLAT ACTUATOR MOUNT OTBD BRACKET ON SLAT IS CRACKED, WS629.0. REPAIRED ON FASI WO 21117, NR 12726.
- [SDR FOTR2111712154](https://openairdocs.org/sdr/FOTR2111712154), Jul 25, 2011: RIB. CRACKED. NR 4 SLAT INBD ACTUATOR ROD END ATTACH RIB IS CRACKED, WS383. REPAIRED ON FASI WO 21117, NR12154.
- [SDR FOTR2111712669](https://openairdocs.org/sdr/FOTR2111712669), Jul 25, 2011: SKIN. BENT. AFT AIRSTAIRS RT EXTERIOR SKIN SURFACE, AFT CORNER IS BENT, SEPARATING, AND PULLED FASTENERS STA 1383. REPAIRED ON FASI WO 21117, NR12669.
- [SDR FOTR2111712817](https://openairdocs.org/sdr/FOTR2111712817), Jul 25, 2011: SKIN. DEBONDED. LT INBD FOREFLAP UPPER SURFACE HAS 6"DIAMETER DISBOND. REPAIRED ON FASI WO 21117, NR 12817.
- [SDR FOTR2111712507](https://openairdocs.org/sdr/FOTR2111712507), Jul 25, 2011: FRAME. DENTED. FWD CARGO COMPARTMENT- DENT AT STA 700 BETWEEN STR 23L AND 22L. REPAIRED ON FASI WO21117, NR 12507.
- [SDR FOTR2111712341](https://openairdocs.org/sdr/FOTR2111712341), Jul 25, 2011: FRAME. DENTED. FWD CARGO COMPARTMENT-DENT AT STA 520 LT, STR 23L. REPAIRED ON FASI WO 21117, NR 12341.
- [SDR FOTR2111712446](https://openairdocs.org/sdr/FOTR2111712446), Jul 13, 2011: STRUCTURE. CRACKED. VERTICAL STAB, L/E HAS CRACKED DOUBLER TOP OF FWD SPAR CHORD CENTER, JUST AFT OF ELEVATOR CONTROL CABLE QUADRANT. REPAIRED ON FASI WO 21117, NR 12446.
- [SDR C8GA201000010A](https://openairdocs.org/sdr/C8GA201000010A), Jun 2, 2010: ACTUATOR. MALFUNCTIONED. WHILE ON APPROACH WITH THE GEAR HANDLE IN THE DOWN POSITION THE NLG UNSAFE LIGHT ILLUMINATED. CREW PERFORMED APPROPRIATE CHECKLIST AND RECYCLED GEAR WITH ALL IN
- [SDR ABXR200908250021](https://openairdocs.org/sdr/ABXR200908250021), Aug 25, 2009: STOP FITTING. CRACKED. AFTER A POST C-CHECK TEST FLIGHT A CRACK WAS VISUALLY DISCOVERED ON THE L1 DOOR STOP IN UPPER AFT CORNER. THE CRACKED DOOR STOP FITTING WAS REMOVED, THE NEW STO
- [SDR ABXR200908240020](https://openairdocs.org/sdr/ABXR200908240020), Aug 21, 2009: VENT LINE. MISREPAIRED. DURING A C-CK ROUTINE VISUAL INSP, INCORRECT LT WING VENT LINE CLAMPS WERE FOUND UNDER PANELS 7216 AND 7215. THE CLAMPS WERE EVALUATED BY ENGINEERING. REMOVED O
- [SDR ABXR200908240019](https://openairdocs.org/sdr/ABXR200908240019), Aug 21, 2009: VENT LINE. CHAFED. DURING A C-CK ROUTINE VISUAL INSP, THE RT WING VENT LINE WAS FOUND CHAFED UNDER PANEL 7608. THE DAMAGE WAS CUT OUT, THE REWORKED AREA TREATED WITH ALODINE AND A
- [SDR ABXR200908240018](https://openairdocs.org/sdr/ABXR200908240018), Aug 21, 2009: SUPPORT ANGLE. CORRODED. DURING THE ROUTINE VISUAL INSP OF THE UPPER SIDE OF THE RT NLG DOGHOUSE WAS FOUND CORRODED. THE CORROSION WAS CLEANED AND FOUND OUT OF LIMITS. THE UPPER SIDE AN
- [SDR ABXR200908240017](https://openairdocs.org/sdr/ABXR200908240017), Aug 21, 2009: FITTING. DAMAGED. DURING THE REPETITIVE INSP NR 1 ENG PYLON SUPPORT FITTING IAW SB 2000-5410A0 2000-19-24, HOLES I, J, K, AND L WERE VISUALLY FOUND ELEGONGATED AND HOLES WERE FOU
- [SDR ABXR200908240016](https://openairdocs.org/sdr/ABXR200908240016), Aug 21, 2009: SKIN. DAMAGED. DURING A C-CK INSP, THE LT WING SKIN AT THE NR 1 SLAT OTBD TRACK CUT-OUT WAS HEAVYILY DAMAGED AND CRACKED DUE TO THE UPPER FWD SLAT ROLLER NOT BEING CAPTURED BY
- [SDR ABXR200908240015](https://openairdocs.org/sdr/ABXR200908240015), Aug 21, 2009: SKIN. CRACKED. DURING A C-CK REPETITIVE AD 2007-12-14 SB 727-53A0198, A CRACK WAS FOUND WITH EDDY CURRENT ON THE FWD ENTRY DOOR UPPER HINGE CUT-OUT. THE DAMAGE WAS CUTOUT TO A
- [SDR ABXR200908240014](https://openairdocs.org/sdr/ABXR200908240014), Aug 21, 2009: VENT LINE. DENTED. DURING A C-CK ROUTINE VISUAL INSP, THE RT WING VENT LINE WAS FOUND CHAFED ABOVE PANEL 7615. THE DAMAGE WAS CUT OUT, THE REWORKED AREA TREATED WITH ALODINE AND A
- [SDR ABXR200908240013](https://openairdocs.org/sdr/ABXR200908240013), Aug 21, 2009: VENT LINE. DENTED. DURING A C-CK ROUTINE VISUAL INSP, THE LT WING VENT LINE WAS FOUND CHAFED ABOVE PANEL 7612. THE DAMAGE WAS CUT OUT, THE REWORKED AREA TREATED WITH ALODINE AND A
- [SDR ABXR200908240012](https://openairdocs.org/sdr/ABXR200908240012), Aug 21, 2009: LINE. DENTED. DURING A C-CK ROUTINE VISUAL INSP, THE LT WING FUEL DUMP LINE WAS FOUND DENTED ABOVE PANEL 7215. THE DAMAGE WAS CUT OUT, THE REWORKED AREA TREATED WITH ALODINE 
- [SDR ABXR200908240011](https://openairdocs.org/sdr/ABXR200908240011), Aug 21, 2009: TRUNNION. CORRODED. DURING ROUTINE C-CK MX, THE LT TRUNNION FITTING WAS FOUND CORRODED OUTSIDE OF MM LIMITS INSIDE THE INNER BORE. THE LT AND RT TRUNNION FITTINGS WERE REMOVED AND 
- [SDR ABXR200908240010](https://openairdocs.org/sdr/ABXR200908240010), Aug 21, 2009: SUPPORT FITTING. DAMAGED. DURING THE REPETITIVE NR 3 ENG SUPPORT FITTING INSP IAW SB 2000-5410A01, AD 2005-19-24, HOLES I, J, K AND L WERE VISUALLY FOUND ELONGATED AND THE HOLES WERE FOU
- [SDR ABXR200908240009](https://openairdocs.org/sdr/ABXR200908240009), Aug 21, 2009: GUSSET. CRACKED. DURING THE ROUTINE VISUAL INSP OF A C-CK, THE MAIN CARGO DOOR JAMB LWR AFT GUSSET WAS FOUND GOUGED AND CRACKED IN SEVERAL PLACES. A REPLACEMENT GUSSET WAS FABRI
- [SDR ABXR200908240008](https://openairdocs.org/sdr/ABXR200908240008), Aug 21, 2009: STRUCTURE. CORRODED. DURING THE ROUTINE VISUAL INSP OF A C-CK, THE SUBFLOOR WAS FOUND CORRODED OUT OF LIMITS. THE AREA WAS REPAIRED WITH A DOUBLER FABRICATED FROM 0.050 INCH, 2024 T
- [SDR ABXR200908210007](https://openairdocs.org/sdr/ABXR200908210007), Aug 21, 2009: FLOORBEAM. CRACKED. DURING THE ACCOMPLISHMENT OF A ROUTINE VISUAL AND EDDY CURRENT INSP OF THE CARGO DOOR STRUCTURE, THE FLOORBEAM SPLICE PLATE WAS FOUND CRACKED. THE SPLICE PLATE 
- [SDR ABXR200908210006](https://openairdocs.org/sdr/ABXR200908210006), Aug 21, 2009: FLOORBEAM. CRACKED. DURING THE ACCOMPLISHMENT OF A ROUTINE VISUAL AND EDDY CURRENT INSP OF THE CARGO DOOR STRUCTURE, THE FLOORBEAM SPLICE PLATE WAS FOUND CRACKED. THE SPLICE PLATE 
- [SDR ABXR200908210005](https://openairdocs.org/sdr/ABXR200908210005), Aug 21, 2009: FLOORBEAM. CRACKED. DURING THE ACCOMPLISHMENT OF A ROUTINE VISUAL AND EDDY CURRENT INSP OF THE CARGO DOOR STRUCTURE, THE FLOORBEAM SPLICE PLATE WAS FOUND CRACKED. THE SPLICE PLATE 
- [SDR ABXR200908210004](https://openairdocs.org/sdr/ABXR200908210004), Aug 21, 2009: FLOORBEAM. CRACKED. DURING THE ACCOMPLISHMENT OF A ROUTINE VISUAL AND EDDY CURRENT INSP OF THE CARGO DOOR STRUCTURE, THE FLOORBEAM SPLICE PLATE WAS FOUND CRACKED. THE SPLICE PLATE 
- [SDR ABXR200908210003](https://openairdocs.org/sdr/ABXR200908210003), Aug 21, 2009: FLOORBEAM. CRACKED. DURING THE ACCOMPLISHMENT OF A ROUTINE VISUAL AND EDDY CURRENT INSP OF THE AEI CARGO DOOR STRUCTURE, THE FLOORBEAM SPLICE PLATE WAS FOUND CRACKED. THE SPLICE PL
- [SDR ABXR200908210002](https://openairdocs.org/sdr/ABXR200908210002), Aug 21, 2009: FLOORBEAM. CRACKED. DURING THE ACCOMPLISHMENT OF A ROUTINE VISUAL AND EDDY CURRENT OF THE CARGO DOOR FLOOR STRUCTURE, THE FLOORBEAM SPLICE PLATE WAS FOUND CRACKED. THE SPLICE PLATE
- [SDR ABXR200908200001](https://openairdocs.org/sdr/ABXR200908200001), Aug 20, 2009: SUPPORT. CORRODED. DURING A HEAVY MX INSP EVENT, SUPPORT CLIP AT STR 26R CORRODED AT 545. REMOVED AND CLEANED SUPPORT CLIP AND FOUND OUT OF LIMITS. FABRICATED CLIP FROM 7075 T6 0.
- [SDR C8GA20080012](https://openairdocs.org/sdr/C8GA20080012), Mar 25, 2008: HELICOIL. DAMAGED. FLT 708 FROM MCI TO PHX - DURING CRUISE OPERATION THE CAPTAIN WAS NOTIFIED THAT THE NR 1 ENGINE OIL QUANTITY WAS DECREASING. THE NR 1 ENGINE WAS SHUT DOWN AND E
- [SDR C8GA20070009](https://openairdocs.org/sdr/C8GA20070009), Sep 14, 2007: CONTROL VALVE. MALFUNCTIONED. FLT 720 FROM TOL TO ATL, DURING CRUISE OPERATION THE AIRCRAFT EXPERIENCED ICING CONDITIONS WITH BOTH ENGINE AND WING ANTI-ICE ON, THE LOWER AFT CARGO SMOKE DETE
- [SDR C8GA20050017](https://openairdocs.org/sdr/C8GA20050017), Aug 17, 2005: INDICATOR. INOPERATIVE. FLT 1828 FROM TOL TO RFD. NO #2 AIRSPEED INDICATION AT THE BEGINNING OF TAKE OFF ROLL. ABORTED TAKE OFF AND RETURNED TO GATE. REPLACED #2 AIRSPEED INDICATOR. LE
- [SDR C8GA20050018](https://openairdocs.org/sdr/C8GA20050018), Aug 15, 2005: ADC. INOPERATIVE. ON TAKEOFF ROLL, FO AIRSPEED INDICATION INOPERATIVE. FLAG CAME OUT AFTER STOP. CLEANED NR 2 ADC CONNECTOR PLUG AND RERACKED ADC. OPS CHECK GOOD. AIRCRAFT RETURN
- [SDR C8GA20050016](https://openairdocs.org/sdr/C8GA20050016), Jul 8, 2005: OIL FILTER. CONTAMINATED. IN CRUISE, NR 3 ENGINE LOW OIL PRESSURE/FILTER BYPASS LIGHT ILLUMINATED. REDUCED ENGINE POWER PER AOM PROCEDURES AND LIGHT EXTINGUISHED. LIGHT ILLUMINATED AGAIN
- [SDR C8GA20050013](https://openairdocs.org/sdr/C8GA20050013), May 12, 2005: COMPRESSOR. STALLED. FLT 711 FROM DEN TO TOL, ON CLIMB FROM DEN, NR 1 ENGINE COMPRESSOR STALLED. AIRCRAFT RETURNED TO DEN AND LANDED WITHOUT INCIDENT. AFTER RETURN TO BLOCKS, WITH E
- [SDR C8GA20050001](https://openairdocs.org/sdr/C8GA20050001), Jan 13, 2005: LINE. SPLIT. AFTER TAKE OFF FROM SAN, "A" HYDRAULIC SYSTEM LOW LEVEL LIGHT ILLUMINATED FOLLOWED BY RAPID QUANTITY DEPLETION. TURNED OFF BOTH THE NR 1 AND 2 HYDRAULIC PUMPS A
- [SDR C8GA20040009](https://openairdocs.org/sdr/C8GA20040009), Jun 22, 2004: PUMP. FAILED. UPON DESCENT INTO KTOL, THE NR 2 ENGINE HYDRAULIC PUMP LOW-PRESSURE WARNING LIGHT ILLUMINATED. ACCOMPLISHED ABNORMAL CCIA AIRCRAFT OPERATIONS MANUAL CHECKLIST A
- [SDR C8GA20040005](https://openairdocs.org/sdr/C8GA20040005), Jun 9, 2004: SENSOR. FAILED. FLT 2161 FROM KDFW TO KMCI. AFTER TAKEOFF FROM DFW, THE LOWER AFT CARGO FIRE WARNING CAME ON. ALSO, THE NR 2 ENGINE DUCT OVERHEAT LIGHT ON IN FLIGHT. FOLLOW ALL
- [SDR C8GA20040001](https://openairdocs.org/sdr/C8GA20040001), Feb 3, 2004: TENSION SPRING. WEAK. DURING CLIMBOUT, KIAS 225 A/C EXPERIENCE AIRFRAME VIB. ADVISED CCIA FLT FOLLOWING & ATC OF PROBLEM & AIR TURNBACK. NO EMERGENCY ACTION TAKEN & A/C LANDED W/O IN
- [SDR C8GA20030018](https://openairdocs.org/sdr/C8GA20030018), Jun 20, 2003: BEARING. SEIZED. FLT 231 FROM MIA TO PTY. AFTER TAKEOFF, NR 2 SLAT DID NOT RETRACT. CYCLED SYSTEM TWICE STILLS NO RETRACTION. FUEL WAS DUMPED AND THE AIRCRAFT RETURNED TO MIA WI
- [SDR C8GA20030017](https://openairdocs.org/sdr/C8GA20030017), Jun 3, 2003: TRANSMITTER. DEFECTIVE. FLT 001 FROM MIA TO PTO. ON ROTATION, STICK SHAKER ACTIVATED. UNABLE TO STOP STICK SHAKER IN FLIGHT, FUEL WAS DUMP AND THE FLIGHT RETURNED TO MIA. AIRCRAFT LAND
- [SDR C8GA2003002R](https://openairdocs.org/sdr/C8GA2003002R), Jan 16, 2003: ENGINE. BIRD INGESTION. Flight 737 from GDL to MTY. Bird strike on #2 engine after takeoff. Shutdown #2 engine and air turn back to GDL (Guadalajara, Mexico) aircraft landed without in

All 71: https://openairdocs.org/deregistered/N899AA-2013-05-01/reports.md

## 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 19871213074569I](https://openairdocs.org/incident/19871213074569I), Dec 13, 1987: Boeing 727223 (N899AA), Jackson, MS. Pilot declared a cabin pressure problem. Cabin altitude below 10000 feet. Found a pressurization leak not defined.
- [Incident 19850430034229I](https://openairdocs.org/incident/19850430034229I), Apr 30, 1985: Boeing 727200 (N899AA), Chicago, IL. Aborted takeoff due to contained failure in turbine section of nr 1 engine. Evacuation due to fire from engine.
- [Incident 19841024065109I](https://openairdocs.org/incident/19841024065109I), Oct 24, 1984: Boeing 7272A1 (N899AA), Ontario, CA, Minor damage. Bird strike just before touchdown. Dented skin on outboard leading flap.

## Other aircraft with N899AA

- [Registered now](https://openairdocs.org/aircraft/N899AA): Textron 172S, S/N 172S11767, built 2016

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