# N211FE: 1984 Boeing 727-2S2F, registration cancelled 2014-05-12

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: May 12, 2014
- Exported to: Democratic Republic of the Congo
- Status when cancelled: Valid registration
- Airframe: [Boeing 727-2S2F](https://openairdocs.org/model/boeing-727-2s2f) (registry code 1384081)
- Engine: [Pratt & Whitney JT8D-17 series](https://openairdocs.org/engine/pratt-whitney-jt8d-17-series) (registry code 52049)
- Data sheets: [TCDS E2EA](https://openairdocs.org/tcds/E2EA) (OpenAirDocs)
- Serial number: 22933
- Year built: 1984
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-jet
- Airworthiness: Standard, transport
- Airworthiness date: November 21, 1997
- Certificate issued: November 12, 2013
- Last registry action: November 12, 2013
- Mode S code: A1BDBB
- Owner when cancelled: [Csc Aerospace Corp Trustee](https://openairdocs.org/faa-owner/CSC%20AEROSPACE%20CORP%20TRUSTEE)
- Location: [Doral, FL](https://openairdocs.org/faa-place/FL/Doral)
- Owner type: Corporation
- Owner's area on the map: 25.8361° N, 80.4200° W: Placed by OpenAirDocs at the center of ZIP code 33178, within about 4 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N211FE
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=211FE
- Page: https://openairdocs.org/deregistered/N211FE-2014-05-12

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 727-2S2F: https://openairdocs.org/model/boeing-727-2s2f.md

## Service difficulty reports (98, newest 50)

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

- [SDR FDEA201208042837](https://openairdocs.org/sdr/FDEA201208042837), Aug 4, 2012: GUIDE. OUT OF ADJUST. ON BLOCK-IN, CAPTAIN OPENED SLIDING WINDOW TO TALK TO GROUND CREW. UNABLE TO CLOSE. TROUBLESHOT DOWN TO FWD AND AFT GLIDES. ADJUSTED AND TESTED L2 CAPT'S SLIDIN
- [SDR FDEA201207282730](https://openairdocs.org/sdr/FDEA201207282730), Jul 28, 2012: PIN. OUT OF ADJUST. ON PREFLIGHT, CAPTAIN`S SLIDING WINDOW WILL NOT CLOSE. ADJUSTED GUIDE PIN IAW MM 56-12-011-5. OPS CHECKED NORMAL.
- [SDR FDEA201206142233](https://openairdocs.org/sdr/FDEA201206142233), Jun 14, 2012: ATTACH FITTING. WORN. OPEN RT ATTACH FITTING FOR L1 DOOR THAT HOLD ESCAPE SLIDE HAS ONE OF THE FITTINGS WORN. OTHER SIDE SNAPS IN WORN FITTING. HOLDS ROD IN WITH NO RESTRAINT. REMOVE
- [SDR FDEA201206142244](https://openairdocs.org/sdr/FDEA201206142244), Jun 14, 2012: POSITION SWITCH. FAILED. RETRACTING FLAPS FROM 5 TO 2 DEGREES, AMBER L/E FLAPS LIGHT STAYED ON. S/O POSITION TEST SELECTOR SHOWED NR 2 KREGER FLAP OUT. COMPLIED WITH QRH. NO HELP. RETUR
- [SDR FDEA201206012042](https://openairdocs.org/sdr/FDEA201206012042), Jun 1, 2012: SLIDE. DISLODGED. EVACUATION SLIDE FELL OUT OF ITS CONTAINER. STOWED L1 DOOR ESCAPE SLIDE IAW AMM 25-60-015-2.
- [SDR FDEA201205312036](https://openairdocs.org/sdr/FDEA201205312036), May 31, 2012: SLIDE. DISLODGED. EVACUATION SLIDE FELL OUT OF ITS CONTAINER. STOWED L1 DOOR ESCAPE SLIDE PER AMM 25-60-015-2.
- [SDR FDEA201201190264](https://openairdocs.org/sdr/FDEA201201190264), Jan 19, 2012: SLIDE. DISLODGED. SLIDE FELL OFF L1 DOOR. REINSTALLED SLIDE L-1 DOOR.
- [SDR FDEA201201170272](https://openairdocs.org/sdr/FDEA201201170272), Jan 17, 2012: SLIDE. DISLODGED. SLIDE FELL OFF L1 DOOR. REINSTALLED SLIDE L-1 DOOR REF AMM 25-60-015-2.
- [SDR FDEA201111275062](https://openairdocs.org/sdr/FDEA201111275062), Nov 27, 2011: SLIDE. UNSECURE. WHEN OPENING L1 DOOR FOR PREFLIGHT CHECK FOUND DOOR SLIDE LAYING ON FLOOR. REINSTALLED SLIDE ON L1 DOOR REF AMM 25-60-015-2. ACFT OK FOR SERVICE.
- [SDR FDEA201110284672](https://openairdocs.org/sdr/FDEA201110284672), Oct 28, 2011: SLIDE. DISLODGED. FOUND ESCAPE SLIDE OUT OF COMPARTMENT AND UNPACKED, LAYING IN COURIER COMPARTMENT. INSTALLED SERVICABLE ESCAPE SLIDE IAW MM 25-60-015-2.
- [SDR FDEA201109113826](https://openairdocs.org/sdr/FDEA201109113826), Sep 11, 2011: WEB. DAMAGED. L1 DOOR INTERIOR WEB DAMAGED, INSIDE SECOND LIGHTNING HOLE FROM BOTTOM NEAR CRNTER OF DOOR BS 328. DAMAGE OUT OF LIMITS IAW SRM 52-00-2. REMOVED WEB IAW SRM 51-
- [SDR FDEA201109103823](https://openairdocs.org/sdr/FDEA201109103823), Sep 10, 2011: SKIN. GOUGED. RT WING, NR 7 SLAT OTBD HOOK AREA HAS GOUGE ON T/E SKIN OTBD SIDE. REMOVED DAMAGED DOUBLER IAW SRM REV 103 51-30-2 FABRICATED DOUBLER AND INSTALLED IAW SRM 57-5
- [SDR FDEA201109093811](https://openairdocs.org/sdr/FDEA201109093811), Sep 9, 2011: RIB. CRACKED. LEFT WING NR 3 SLAT INBOARD ACTUATOR ATTACH RIB INSIDE SLAT IS CRACKED. REMOVED CRACKED RIB IAW SRM 51-30-2 REV 103. FABRRICATED NEW RIB IAW DRAWING 65-17294 AN
- [SDR FDEA201109083777](https://openairdocs.org/sdr/FDEA201109083777), Sep 8, 2011: RIB. CRACKED. LT WING NR 3 SLAT OTBD ACTUATOR ATTACH RIB INSIDE SLAT IS CRACKED. REMOVED RIB IAW SRM REV 103 51-30-2. FABRICATED NEW RIB IAW DWG 65-17294 AND SRM 51-20-1 FIG 
- [SDR FDEA201109083776](https://openairdocs.org/sdr/FDEA201109083776), Sep 8, 2011: SUPPORT. CORRODED. UPPER FUSELAGE INTERIOR, MAIN CARGO DOOR UPPER SILL SUPPORT LOWER SURFACE HAS LIGHT SURFACE CORROSION AT BS 661, STRINGER 2L. REMOVED DAMAGED SILL SUPPORT IAW S
- [SDR FDEA201109083772](https://openairdocs.org/sdr/FDEA201109083772), Sep 8, 2011: STRINGER. CORRODED. UPPER FUSELAGE INTERIOR, STRINGER 4L HAS CORROSION AT BS 682. REPLACED STRINGER SPLICE.
- [SDR FDEA201109083771](https://openairdocs.org/sdr/FDEA201109083771), Sep 8, 2011: STRINGER SPLICE. CORRODED. UPPER FUSELAGE INTERIOR, STRINGER 4L HAS CORROSION AT BS 678 SPLICE. REMOVED SPLICE IAW SRM 51-30-2 REV 103. FORMED NEW SPLICE IAW SRM 53-10-2. INSTALLED NEW SP
- [SDR FDEA201109083770](https://openairdocs.org/sdr/FDEA201109083770), Sep 8, 2011: SEAT TRACK. CORRODED. CORROSION ON SEAT TRACK FLANGE BS 344 LBL 25. REMOVED SEAT TRACK SECTION IAW SRM 51-30-2 REV 103. FABRICATED & INSTALLED SEAT TRACK SECTION IAW SRM 53-10-2 FIG.
- [SDR FDEA201109063726](https://openairdocs.org/sdr/FDEA201109063726), Sep 6, 2011: SKIN. CORRODED. CORROSION ON INNER SKIN AT DRAIN VALVE, FWD. PIT BS 682 - 686, RBL 3.0. CUT OUT DAMAGED AREA IAW SRM REV.103, 53-30-3 FIG 3A. FABRICATED REPAIR DOUBLER AND FILL
- [SDR FDEA201109063725](https://openairdocs.org/sdr/FDEA201109063725), Sep 6, 2011: SKIN. GOUGED. EXTERIOR SURFACE GOUGE AT BS 520 AT S27L. CUT OUT DAMAGED AREA IAW SRM 53-30-3 REV 103 FIGURE 14. FABERICATED REPAIR DOUBLER, STRUCTURAL FILLER, AND FILLER IAW 
- [SDR FDEA201109063724](https://openairdocs.org/sdr/FDEA201109063724), Sep 6, 2011: STRINGER. CORRODED. UPPER FUSELAGE INTERIOR, STRINGER 4 LT HAS CORROSION AT BS 720. CUT OUT DAMAGED AREA IAW SRM 53-10-3 REV 103 FIG 3. FABERICATED REPAIR PARTS IAW SRM 53-10-3 FIG
- [SDR FDEA201109063723](https://openairdocs.org/sdr/FDEA201109063723), Sep 6, 2011: STRINGER. CORRODED. UPPER FUSELAGE INTERIOR, STRINGER 5 LEFT HAS CORROSION AT BS 720A 3 INCHES. CUT OUT DAMAGED AREA IAW SRM REV.103 53-10-3 FIG3 FABRICATED REPAIR STARS AND FILLER
- [SDR FDEA201109043662](https://openairdocs.org/sdr/FDEA201109043662), Sep 4, 2011: STRINGER. CORRODED. UPPER FUSELAGE INTERIOR STRINGER 5 LT HAS CORROSION AT BS 702. CUT OUT DAMAGED AREA IAW SRM 53-10-3 REV 103 FIG 3. FABRICATED STRAPS AND FILLER IAW SRM 53-10-3 
- [SDR FDEA201109013603](https://openairdocs.org/sdr/FDEA201109013603), Sep 1, 2011: SKIN. GOUGED. EXTERIOR FUSELAGE, 2 LONG GOUGES UNDER L-1 DOOR. CUTOUT DAMAGE AREA IAW SRM 53-30-3 REV 103 FIG 1. FABRICATED REPAIR DOUBLER AND FILLER IAW SRM 53-30-3 FIG 1. I
- [SDR FDEA201108313717](https://openairdocs.org/sdr/FDEA201108313717), Aug 31, 2011: ATTACH ANGLE. CRACKED. RIGHT WING, NR 8 SPOILER ACTUATOR SUPPORT FITTING, HAS LOWER LT SIDE ATTACH ANGLE CRACKED AT WBL 120. REMOVED SECTION OF ATTACH ANGLE AND FABRICATED REPAIR PART
- [SDR FDEA201108313641](https://openairdocs.org/sdr/FDEA201108313641), Aug 31, 2011: STRUCTURE. CRACKED. RT WING, INBD FLAP, MID FLAP AFT CHORD IS CRACKED AT 2 EA AREAS, NEAR THE MOST INBD HINGE AND ACTUATING ROD FOR AFT FLAP. CUT OUT DAMAGED AREA IAW SRM 51-40-4 F
- [SDR FDEA201108303573](https://openairdocs.org/sdr/FDEA201108303573), Aug 30, 2011: WEB. CRACKED. CRACK IN SIDE WEB AT LIGHTING HOLE RT SIDE AFT VENTRAL STAIRS BS 1239. CUT OUT DAMAGE AREA TORQUE BOX WEB IAW SRM 51-40-2 FIG 1. FABRICATED REPAIR DOUBLER IAW S
- [SDR FDEA201108303574](https://openairdocs.org/sdr/FDEA201108303574), Aug 30, 2011: WEB. CRACKED. CRACK IN SIDE WEB AT LIGHTING HOLE LT SIDE AFT VENTRAL STAIR OPENING, BS 1303. CUTOUT DAMAGE AREA TORQUE BOX WEB IAW SRM 51-10-1, FIG 1. FABRICATED REPAIR DOUBL
- [SDR FDEA201108193383](https://openairdocs.org/sdr/FDEA201108193383), Aug 19, 2011: SLIDE. DAMAGED. FWD ENTRY DOOR ESCAPE SLIDE, PART OF THE SLIDE DROOPING OUT OF CONTAINER. TROUBLESHOOTING. REMOVED ESCAPE SLIDE FROM ENCLOSURE. SECURED LOOSE ITEMS WITH EXISTIN
- [SDR FDEA201107022556](https://openairdocs.org/sdr/FDEA201107022556), Jul 2, 2011: FITTING. INOPERATIVE. SLIDE FALLS OUT TOO EASILY. REPLACED GIRT BAR PLASTIC CLIPS.
- [SDR FDEA201005071486](https://openairdocs.org/sdr/FDEA201005071486), May 7, 2010: GEARBOX. LEAKING. DURING CRUISE NR 3 LOW OIL FILTER BYPASS LITE ILLUMINATED. OIL PRESSURE INDICATED 28PSI QTY WAS 3.5 GALLONS AND TEMP WAS 95 DEG, OPERATED 2 MIN AT IDLE SHUTDOWN
- [SDR FDEA200910153577](https://openairdocs.org/sdr/FDEA200910153577), Oct 15, 2009: SWITCH. FAILED. AILERON SYS A ANNUNCIATOR LIGHT ON F/O PANEL CAME ON 30 AFTER LEVEL OFF, NO LOSS OF A SYS A HYD FLUID. REMOVED AND REPLACED AILERON "A" SYS HYD LOW PRESSURE WAR
- [SDR FDEA200902270766](https://openairdocs.org/sdr/FDEA200902270766), Feb 27, 2009: WARNING LIGHT. FALSE ACTIVATION. TAILSKID LIGHT REMAINED ON AFTER GEAR RETRACTION. CREW REPORTED THAT AFTER CYCLING GEAR THE SYSTEM WORKED NORMALLY AND ON APPROACH, SYSTEM FUNCTIONED NORMAL. IN
- [SDR 08FDEA03520](https://openairdocs.org/sdr/08FDEA03520), Aug 20, 2008: FITTING. CORRODED. GENERATED BY EO 7-5510-7-5000, HORIZONTAL STAB RT HINGE FITTING O/B BUSHING BORE HAS CORROSION OVERSIZED LUG BORE TO 2.2244 INCH CORROSION REMOVED. HFEC INSPECT
- [SDR 08FDEA03498](https://openairdocs.org/sdr/08FDEA03498), Aug 19, 2008: SUPPORT ANGLE. CORRODED. RT WHEEL WELL, LOWER FUSELAGE FAIRING SUPPORT FRAME HAS CORROSION, RBL 21, STA 950 FABRICATED TEE ANGLE FROM RT WHEEL WELL FUSELAGE FAIRING SUPPORT STA 950 REFB
- [SDR 08FDEA03456](https://openairdocs.org/sdr/08FDEA03456), Aug 16, 2008: BRACKET. CRACKED. AIRSTAIR COMPARTMENT LT BRACKET FOR FIRE LOOP SUPPORT IS CRACKED AT BULKHEAD STA 1183 NEAR FLOOR LEVEL. REMOVED OLD BRACKET REF SRM 51-30-02 P 1-7, IDENTIFIED M
- [SDR 08FDEA03455](https://openairdocs.org/sdr/08FDEA03455), Aug 16, 2008: BEAM. CORRODED. LT MLG W/W UPPER BOX BEAM LOWER WEBS AFT OF STA 910 AND 930 HAVE CORROSION REMOVED FASTENERS FOR ACCESS. REMOVED CORROSION, ORIGINAL .080 REMAINING .070. REMOVE
- [SDR 08FDEA03451](https://openairdocs.org/sdr/08FDEA03451), Aug 16, 2008: FAIRING. CRACKED. RT WING NR 6 FLAP TRANSMISSION FAIRING IS CRACKED AT CENTER ATTACH HOLE REMOVED FAIRING REF 51-30-2, PG 1-7 STOP DRILLED CRACKS REF 727 SRM 51-10-1 PG 13. NDT V
- [SDR 08FDEA03449](https://openairdocs.org/sdr/08FDEA03449), Aug 16, 2008: FAIRING. CRACKED. NR 5 FLAP TRACK MIDDLE FAIRING, AFT SKIN BENT/CRACKED. REMOVED DAMAGED SKIN, REF 51-30-2, PG 1-7. ORIGINAL SKIN AND REPLACEMENT BOTH IDENTIFIED AS 7075-T6, .040
- [SDR 08FDEA03448](https://openairdocs.org/sdr/08FDEA03448), Aug 16, 2008: ATTACH ANGLE. CRACKED. RT WING, LOWER T/E PANEL BELOW NR 13 SPOILER ACTUATOR I/B ATTACH ANGLE CRACKED. REMOVED AND REPLACED CHANNEL REF SRM 51-30-5, SRM 51-30-2. THIS IS CLASSIFIED AS
- [SDR 08FDEA03447](https://openairdocs.org/sdr/08FDEA03447), Aug 16, 2008: ATTACH ANGLE. CRACKED. RT WING LOWER T/E PANEL BELOW NR 13 SPOILER ACTUATOR O/B ATTACH ANGLE CRACKED. REMOVED AND REPLACED CHANNEL REF SRM 51-30-5, SRM 51-30-2. THIS IS CLASSIFIED AS 
- [SDR 08FDEA03446](https://openairdocs.org/sdr/08FDEA03446), Aug 16, 2008: BRACKET. CRACKED. FWD NOSE COMPARTMENT WEATHER RADAR MOUNT BRACKET CRACKED REMOVED WEATHER RADAR R/T. REPLACED MOUNT BRACKET, INSTALLED WEATHER RADAR R/T AND PERFORMED GOOD OPS C
- [SDR 08FDEA03407](https://openairdocs.org/sdr/08FDEA03407), Aug 13, 2008: ANGLE. CRACKED. LT WING ROOT TE UPPER PNL IB OF NR 7 SPOILER HAS FRETTED/CRACKED IB SUPPORT ANGLE BS 950A, WBL 70. REPLACED SUPPORT ANGLES REF SRM 51-30-02 PG 1. THIS IS CLASSI
- [SDR 08FDEA03406](https://openairdocs.org/sdr/08FDEA03406), Aug 13, 2008: ANGLE. CRACKED. LEFT WING OB LE CAVITY, LE UPPER SKIN FORMED SUPPORT ANGLE CRACKED AT AFT END ABOVE TAI DUCT AT INBD END OF NR 4 SLAT WELL. REMOVED INTERCOSTAL AND DAMAGED SUPP
- [SDR 08FDEA03403](https://openairdocs.org/sdr/08FDEA03403), Aug 13, 2008: DUCT. CRACKED. RT EXT FUSE NR 3 ENG FAN AIR EXH PORT ASSY IS FRETTED/CRACKED. REMOVED AND REPLACED FAN AIR EXH POT ASSY REF SRM 51-30-2 PG 1-32, REF MM 51-20-151-7 PG 1-5, REF
- [SDR 08FDEA03402](https://openairdocs.org/sdr/08FDEA03402), Aug 13, 2008: FRAME. CORRODED. LWR EXT FUSE BODY FRAME LWR CHORD IS CORRODED BS 351, LBL 17, WL 148-150. REMOVED CORROSION AT LWR EXT FUSE BODY FRAME LWR CHORD STA 351 LBL 17 - RBL 17, REF SR
- [SDR 08FDEA03401](https://openairdocs.org/sdr/08FDEA03401), Aug 13, 2008: SUPPORT ANGLE. CRACKED. RIGHT WING OB LE CAVITY, LE UPPER SKIN FORMED SUPPORT ANGLE CRACKED AT AFT END ABOVE TAI DUCT AT INBD END OF NR 5 SLAT WELL. REMOVED INTERCOSTAL AND SUPPORT ANG
- [SDR 08FDEA03400](https://openairdocs.org/sdr/08FDEA03400), Aug 13, 2008: FLOORBEAM. CRACKED. MAIN DECK FLOORBEAM INTERCOSTAL MID CHORD EXISTING REPAIR DOUBLER IS CRACKED BS 302, WL 207 FABRICATED NEW REPAIR ANGLE REF SRM 51-40-3 PG 1. TREATED AND PRIMED
- [SDR 08FDEA03391](https://openairdocs.org/sdr/08FDEA03391), Aug 12, 2008: BRACKET. CORRODED. CORROSION ON RT A/C BAY FWD COMPARTMENT LIGHT LENS RETAINER AND LIGHT MOUNT BRACKET. REPLACED FWD COMPARTMENT LIGHT, LENS RETAINER AND LIGHT MOUNT BRACKET. REFE
- [SDR 08FDEA03390](https://openairdocs.org/sdr/08FDEA03390), Aug 12, 2008: DUCT. CRACKED. BLEED AIR EXH DUCT ON FUSELAGE ABOVE NR 1 ENG PYLON CRACKED AT AFT EDGE OF OPENING. REMOVED AND REPLACED BLEED AIR EXH DUCT ON FUSELAGE ABOVE NR 1 ENG PYLON. RE

All 98: https://openairdocs.org/deregistered/N211FE-2014-05-12/reports.md

## FAA accident and incident reports (1)

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 19840727038339I](https://openairdocs.org/incident/19840727038339I), Jul 27, 1984: Boeing 727200 (N211FE), Atlanta, GA, Substantial damage. During a heavy thunderstorm gusty winds blew a parked DC3 into the parked 727200. No tie down ropes on DC3.

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