# N204FE: 1983 Boeing 727-2S2F, registration cancelled 2015-10-01

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: October 1, 2015
- 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: 22926
- Year built: 1983
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-jet
- Airworthiness: Standard, transport
- Airworthiness date: August 1, 1983
- Certificate issued: February 3, 2014
- Last registry action: February 3, 2014
- Mode S code: A1A161
- 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/N204FE
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=204FE
- Page: https://openairdocs.org/deregistered/N204FE-2015-10-01

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

## Service difficulty reports (70, newest 50)

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

- [SDR FDEA201307051482](https://openairdocs.org/sdr/FDEA201307051482), Jul 5, 2013: LIGHT. INOPERATIVE. ON SERVICE CHECK, FOUND L1 DOOR EXIT LIGHT INOPERATIVE. R & R L1 DOOR EMERGENCY LIGHT, REF AMM 33-50-101-2. OPS CHECKED GOOD. ACFT OK TO CONTINUE.
- [SDR FDEA201305060923](https://openairdocs.org/sdr/FDEA201305060923), May 6, 2013: BATTERY PACK. INOPERATIVE. FOUND EMERGENCY LIGHT ABOVE MAIN ENTRY DOOR INOPERATIVE. REPLACED EMERGENCY LIGHT BATTERIES IAW MM 33-50-101-2. OPS CHECKED NORMAL. OK FOR SERVICE.
- [SDR FDEA201303010488](https://openairdocs.org/sdr/FDEA201303010488), Mar 1, 2013: TRANSMITTER. MALFUNCTIONED. DURING FLAP RETRACTION, SYS A PRESSURE DECREASED TO APROX 1000 PSI FROM FLAPS 5 -2 PRESSURE DECREASED. ENG 1 A PUMP LIGHT ILLUMINATED INT AND WITH FLAP RETRACTI
- [SDR FDEA201211073901](https://openairdocs.org/sdr/FDEA201211073901), Nov 7, 2012: BATTERY PACK. INOPERATIVE. EMERGENCY EXIT LIGHT ABOVE COCKPIT DOOR DOES NOT ILLUMINATE DURING BATTERY AND STANDBY POWER CHECK. R & R BATTERIES IN EMERGENCY EXIT LIGHT ABOVE COCKPIT DOOR I
- [SDR FDEA201209293512](https://openairdocs.org/sdr/FDEA201209293512), Sep 29, 2012: HINGE. DAMAGED. LOUD SQUEL COMING FROM AREA UPPER FRONT SIDE OF COCKPIT NEXT TO S/O PANEL. CLOSING CARGO OUTFLOW VALVE HAS NO EFFECT. STARTED DURING CLIMB AROUND 250. WENT AWAY
- [SDR FDEA201208183072](https://openairdocs.org/sdr/FDEA201208183072), Aug 18, 2012: BATTERY PACK. FAILED. L1 DOOR EMERGENCY EXIT LIGHTS LT SIDE, LIGHT INOPERATIVE. BATTERY PACK ONLY READS 1.3VDC, REMOVED AND REPLACED EMERGENCY EXIT LIGHT POWER SUPPLY LIGHTS. OPS CHE
- [SDR FDEA201207282729](https://openairdocs.org/sdr/FDEA201207282729), Jul 28, 2012: BOTTLE. DISCHARGED. LEFT "BOTTLE DISCHARGED" LIGHT ILLUMINATED ON OVERHEAD PANEL. R & R LT ENGINE FIRE EXTINGUISHER BOTTLE IAW MM 26-21-001-4 AND PERFORMED INSPECTION CHECK IAW MM2
- [SDR FDEA201206062104](https://openairdocs.org/sdr/FDEA201206062104), Jun 6, 2012: DOOR. OUT OF ADJUST. ON LANDING, FWD ENTRY DOOR LIGHT ILLUMINATED ON S/O PANEL VISUAL INSPECTION, DURING SHUTDOWN VERIFIED FWD ENTRY DOOR WAS SLIGHTLY AJAR. ADJUSTED UPPER LINK ARM 
- [SDR FDEA201206022057](https://openairdocs.org/sdr/FDEA201206022057), Jun 2, 2012: WARNING LIGHT. FALSE ACTIVATION. ON LANDING, FWD ENTRY DOOR LIGHT ON S/O PANEL ILLUMINATED. VISUAL INSPECTION DURING SHUTDOWN, CHECKLIST VERIFIED FWD ENTRY DOOR WAS SLIGHTLY AJAR. OPS CHECK OF 
- [SDR FDEA201205302014](https://openairdocs.org/sdr/FDEA201205302014), May 30, 2012: DOOR. OUT OF ADJUST. DURING CLIMB, PASSING 2000 AGL. FWD ENTRY ANNUNCIATOR LIGHT ON, SO PANEL ANNUNCIATED. RAN QRH. INSPECTED DOOR HANDLE AND LIGHT EXTINGUISHED. PRESSURIZATION OK T
- [SDR FDEA201205231937](https://openairdocs.org/sdr/FDEA201205231937), May 23, 2012: DOOR. OUT OF ADJUST. FWD ENTRY DOOR HANDLE MOVED SLIGHTLY TOWARD OPEN DURING LANDING AND FWD ENTRY DOOR LIGHT ILLUMINATED. ADJUSTED FWD ENTRY DOOR FOR SOFT UNLATCHING AND OPS CHECKE
- [SDR FDEA201204171447](https://openairdocs.org/sdr/FDEA201204171447), Apr 17, 2012: LIGHT. LOOSE. EMERGENCY EXIT LIGHT CAME LOOSE ON LANDING. RE-INSTALLED LIGHT IAW AMM 33-50-001-2-0. OPS NORMAL.
- [SDR FDEA201112285452](https://openairdocs.org/sdr/FDEA201112285452), Dec 28, 2011: WIRE. DAMAGED. UPON INTIAL FLAP RETRACTION FROM 5 DEG TO 2 DEG, NR6 L/E FLAP DID NOT RETRACT, QRH PROCEDURE RAN WITH NO SUCCESSFUL RETRACTION. ON TAXI-IN, FLAP HANDLE BROUGHT 
- [SDR FDEA201110124477](https://openairdocs.org/sdr/FDEA201110124477), Oct 12, 2011: BATTERY PACK. INOPERATIVE. EMERGENCY EXIT LIGHT INOPERATIVE DURING STBY POWER TEST OVER COCKPIT DOOR & OVER MAIN ENTRANCE DOOR. REPLACED EMERGENCY EXIT LIGHTS BATTERY IAW SMP. OPS CHECKED
- [SDR FDEA201109224037](https://openairdocs.org/sdr/FDEA201109224037), Sep 22, 2011: DOOR. OUT OF ADJUST. UPON LANDING THE FWD ENTRY LIGHT ON THE SO DOOR WARNING PANEL ILLUMINATED. ON INSPECTION, CREW FOUND CREW ENTRY DOOR TO BE OPEN AND UNSECURED. PERFORMED ADJUSTM
- [SDR FDEA201109113992](https://openairdocs.org/sdr/FDEA201109113992), Sep 11, 2011: DOOR. UNSECURE. UPON LANDING THE FWD ENTRY LIGHT ON THE SO DOOR WARNING PANEL ILLUMINATED. UPON INSP, CREW FOUND CREW ENTRY DOOR TO BE OPEN AND UNSECURED. PERFORMED ADJUSTMNET 
- [SDR FDEA201105111800](https://openairdocs.org/sdr/FDEA201105111800), May 11, 2011: ENGINE. OVERHEATED. NR 2 ENG FIRE LIGHT AT 340, BOTH BOTTLES FIRED AFTER FOLLOWING QRH. FIRE DEPT INDICATED NR 2 ENG HAD SIGNIFICANT HEAT SIGNATURE. R & R NR 2 ENG FIRE SENSING ELE
- [SDR FDEA201012214734](https://openairdocs.org/sdr/FDEA201012214734), Dec 21, 2010: FIRE LOOP. DIRTY. RECEIVED NR 1 ENGINE FIRE INDICATION ON FINAL APPROACH WITH POWER AT IDLE. SYS TESTED OK & ENGINE WAS SHUTDOWN AND BOTTLE DISCHARGED IAW CHECKLIST. FIRE WARNING
- [SDR FDEA201010033888](https://openairdocs.org/sdr/FDEA201010033888), Oct 3, 2010: SMOKE WARNING. FALSE ACTIVATION. DURING FLIGHT, LOWER AFT CARGO SMOKE AND ARMED LIGHT ILLUMINATE WITH ASSOCIATED BELL. THIS OCCURED 10 SECONDS AFTER WING ANTI-ICE SELECTED OPEN. LIGHT WENT OUT 
- [SDR FDEA201009263714](https://openairdocs.org/sdr/FDEA201009263714), Sep 26, 2010: SEAT TRACK. CORRODED. MAIN CABIN SEAT TRACK AT BS 495 LBL 45 INBD FLANGE LOWER SURFACE IS CORRODED.
- [SDR FDEA201009253710](https://openairdocs.org/sdr/FDEA201009253710), Sep 25, 2010: SEAT TRACK. GOUGED. AFT CABIN STA 1150-1160 BL0 AFT SEAT TRACK SECTION HAS GOUGES AND DAMAGE AROUND SEVERAL SCALLOPS.
- [SDR FDEA201009243705](https://openairdocs.org/sdr/FDEA201009243705), Sep 24, 2010: STIFFENER. CRACKED. NR 1 ENGINE NOSE COWL EXTERIOR AFT BACKSIDE BULKHEAD I/B AT 5 O'CLOCK POSITION VERTICAL ANGLE STIFFENER SUPPORT IS CRACKED AT TOP END REMOVED VERTICAL STIFFENER
- [SDR FDEA201009233660](https://openairdocs.org/sdr/FDEA201009233660), Sep 23, 2010: NOSE COWL. DAMAGED. DAMAGE BOTTOM NR 3 NOSE COWL. REMOVED AND REPLACED NR 3 ENGINE NOSE COWL IAW MM 71-10-021-4. REFERENCE NON-ROUTINE N00917 WORK ORDER 00049152.
- [SDR FDEA201009223663](https://openairdocs.org/sdr/FDEA201009223663), Sep 22, 2010: SEAT TRACK. DAMAGED. MAIN CABIN SEAT TRACK AT BS 500-510 BL 0 HAS BROKEN SCALLOPS. REMOVED SEAT TRACK SECTION AT STA 360 TO 550 BL0, FABRICATED SEAT TRACK FROM BAC 1520-1331 7178-T6
- [SDR FDEA201009223666](https://openairdocs.org/sdr/FDEA201009223666), Sep 22, 2010: SEAT TRACK. DAMAGED. MAIN CABIN SEAT TRACK SEAT TRACK BS 835 LBL 45 HAS BROKEN SCALLOP. REMOVED AND REPLACE SEAT TRACK SECTION FROM BAC 1520-1331 7178-T6511 DIM 95 1/8" IAW SRM 51-3
- [SDR FDEA201009223653](https://openairdocs.org/sdr/FDEA201009223653), Sep 22, 2010: SKIN. GOUGED. NR 2 SLAT LOWER T/E SKIN GOUGED AT O/B SLAT HOOK AREA TRIMMED OUT DAMAGED AREA DIM: 1/2" X 1/2" IAW SRM 51-10-1. FABRICATED REPAIR PLATE FROM 2024 T-3 .125" DIM
- [SDR FDEA201009203664](https://openairdocs.org/sdr/FDEA201009203664), Sep 20, 2010: SEAT TRACK. DAMAGED. MAIN CABIN SEAT TRACK AT BS 680-700, LBL 62.5 HAS DAMAGED SCALLOPS. CUT OUT DAMAGED AREA BS 656 TO 728 LBL 62.5, FABRICATED NEW SECTION, SPLICE REPAIR, ANGLES, 
- [SDR FDEA201009173521](https://openairdocs.org/sdr/FDEA201009173521), Sep 17, 2010: WEB. CRACKED. AFT AIRSTAIRS LT LOWER TORQUE BOX INBD WEB HAS CRACK AT LIGHTING HOLE BS 1220. TRIMMED OUT DAMAGED AREA DIM. 3/4" X 3/8" IAW SRM 51-10-1. FABRICATED REPAIR DOUB
- [SDR FDEA201009163511](https://openairdocs.org/sdr/FDEA201009163511), Sep 16, 2010: SHEAR TIE. CORRODED. CORROSION ON SHEAR TIE AT BS 950E BETWEEN STRINGERS 29R AND 28R. FABRICATED NEW STUB FRAME FROM 7075 0 .040" DIM 22" X 5" IAW SRM 51-10-3 AND 51-20-1 FIG 7 REV 
- [SDR FDEA201009153526](https://openairdocs.org/sdr/FDEA201009153526), Sep 15, 2010: FLOORBEAM. CORRODED. MAIN CABIN FLOORBEAM AT BS 400 BETWEEN LBL 45 AND 25 UPPER I BEAM TOP AND BOTTOM SURFACE IS CORRODED. CUT OUT DAMAGED AREA IAW SRM 53-10-8 FIG 3. FABRICATED REP
- [SDR FDEA201009143414](https://openairdocs.org/sdr/FDEA201009143414), Sep 14, 2010: FRAME SPLICE. DAMAGED. UPON FRAME REMOVAL, FOUND DOUBLE DRILLED HOLES IN FRAME SPLICE, STA 950B, STR 24L. REMOVED PRODUCTION SPLICE/DOUBLER IAW SRM 51-30-2 FORMED NEW DOUBLER IAW SRM 
- [SDR FDEA201009133422](https://openairdocs.org/sdr/FDEA201009133422), Sep 13, 2010: FLOORBEAM. CORRODED. CORROSION ON UPPER FLANGE OF FLOORBEAM AT BS 344 FROM LBL 10 TO RBL 10. REMOVED DAMAGED AREA 8' SECTION IAW SRM 53-10-8 AND 51-30-2. FABRICATED REPAIR TEE SECTI
- [SDR FDEA201009103343](https://openairdocs.org/sdr/FDEA201009103343), Sep 10, 2010: ATTACH ANGLE. CRACKED. LT WING FALSE SPAR ATTACH ANGLE IS CRACKED WBL 118. REMOVED DOUBLER AND CUT OUT LOWER CHORD IAW DRAWING SR27-57-038 REV C. FABRICATED REPAIR ANGLES, NEW WEB, NE
- [SDR FDEA201009093329](https://openairdocs.org/sdr/FDEA201009093329), Sep 9, 2010: KEELBEAM. CRACKED. RT WW, RT KEEL BEAM IS CRACKED AT BS 875 RBL10 TRIMMED OUT DAMAGED AREA AT LOWER CHORD OF KEEL BEAM STA 875 RBL 6 IAW SRM 51-10-1. FABRICATED DOUBLER FROM PN 15
- [SDR FDEA201009083316](https://openairdocs.org/sdr/FDEA201009083316), Sep 8, 2010: STRINGER. CORRODED. CORROSION ON STRINGER 29L BETWEEN BS 950D AND 950E. REMOVED AND REPLACED STRINGER 29L FROM BS 950 - 1010 IAW B727 SRM 53-10-2 FIG 9, 51-30-5 AND 51-30-2 REV 103
- [SDR FDEA201009043277](https://openairdocs.org/sdr/FDEA201009043277), Sep 4, 2010: SKIN. CORRODED. UPON REMOVAL OF STRINGER SECTION, FOUND SKIN CORRODED, BS 1030 AFT OF FRAME AT STRINGER 26R. CUT OUT DAMAGED AREA AT BS 1045 DIM 9" X 3" IAW B727 SRM 53-30-3 FI
- [SDR FDEA201009033341](https://openairdocs.org/sdr/FDEA201009033341), Sep 3, 2010: SKIN. CORRODED. SKIN BULGE STA 1173 AT LAP SEAM STR 20R. COMPLIED WITH EA 7-5330-135593.
- [SDR FDEA201009033269](https://openairdocs.org/sdr/FDEA201009033269), Sep 3, 2010: STRINGER. CORRODED. STRINGER 26L AT BS 1040-1055 IS CORRODED AT LOWER SURFACED. CUT OUT DAMAGED STRINGER FROM STA 1040 TO 1055 IAW SRM 53-10-1 FIG 1. FABRICATED STRINGER FROM BAC14
- [SDR FDEA201009033266](https://openairdocs.org/sdr/FDEA201009033266), Sep 3, 2010: WEB. CRACKED. AFT AIRSTAIRS RT LOWER TORQUE BOX INBD WEB HAS CRACK AT LIGHTING HOLE BS 1303. TRIMMED OUT DAMAGED AREA DIM. 1" X 1/2" IAW SRM 51-10-1. FABRICATED REPAIR DOUBLE
- [SDR FDEA201009033265](https://openairdocs.org/sdr/FDEA201009033265), Sep 3, 2010: WEB. CRACKED. AFT STAIRWELL LT LOWER TORQUE BOX INBD WEB IS CRACKED AT LIGHTING HOLE BS 1223. TRIMMED OUT DAMAGED AREA DIM. 1/2" X 1/4" AND 1/2" X 1/8" IAW SRM 51-10-1. FABRI
- [SDR FDEA201009033268](https://openairdocs.org/sdr/FDEA201009033268), Sep 3, 2010: SKIN. BULGED. SKIN BULGE STA 1052, STR 26L, LAP SEAM. CUT OUT LOWER SKIN DIM. 2" X 2" AT STA 1052 STR 26L LAP SEAM. FABRICATED REPAIR FROM 2024T3 0.071" DIM. 9.750" X 9", DOU
- [SDR FDEA201009023342](https://openairdocs.org/sdr/FDEA201009023342), Sep 2, 2010: SKIN. CRACKED. RT LOWER AFT FUSELAGE AT BS 1010 STR 28R EXTERIOR SKIN IS CRACKED AND BULGING. CUT OUT DAMAGED AREA IAW SRM 53-30-3 FIG 3A REV 103. FABRICATED REPAIR DOUBLER AN
- [SDR FDEA201009023272](https://openairdocs.org/sdr/FDEA201009023272), Sep 2, 2010: SKIN. BULGED. SKIN BULGE STA 1045 STR 26R LAP SEAM. REMOVED CORRODED STRINGER SECTION FROM BS 1026 TO 1070, STR 26R IAW SRM 51-30-2. FABRICATED 3 (EA) STRINGER SECTIONS FROM 
- [SDR FDEA200902070480](https://openairdocs.org/sdr/FDEA200902070480), Feb 7, 2009: INDICATOR. BURNED. AT FLIGHT LEVEL 390 SMELLED FUMES IN COCKPIT. DECLARED AN EMERGENCY AND LANDED AT DEN AIRPORT. MED BRAKE WAS USED AND EMERGENCY EGRESS CONDUCTED. FSFO CHECKLIST
- [SDR FDEA200901200268](https://openairdocs.org/sdr/FDEA200901200268), Jan 20, 2009: INDICATOR. FAILED. F/O AIRSPEED INDICATOR FAILED: NEEDLE STOPPED AT 200 KTS AND OFF FLAG, RESTORED THEN SECOND FAILURE AT 250 KTS AND OFF FLAG. REMOVED AND REPLACED NR 2 AIRSPEED 
- [SDR FDEA200812025037](https://openairdocs.org/sdr/FDEA200812025037), Dec 2, 2008: ACTUATOR. BROKEN. AFT AIRSTAIR LIGHT ILLUMINATED IN-FLIGHT CLIMBING THROUGH 4,500 FEET. ACN RELEASED FOR SERVICE PER MEL/CDL: 52-06-B. AMBER AFT AIRSTAIR DOOR WARNING LIGHT INOP.
- [SDR 07FDEA04548](https://openairdocs.org/sdr/07FDEA04548), Oct 10, 2007: TRANSMITTER. LOOSE. NR 2 LOW OIL PRESSURE FILTER BYPASS LIGHT ILLUMINATED IN DESCENT FOLLOWED BY OIL PRESSURE DROP TO ZERO. QRH PERFORMED, ENGINE SHUT DOWN WITH OIL PRESSURE AT 5 T
- [SDR 05FDEA02424](https://openairdocs.org/sdr/05FDEA02424), Aug 11, 2005: WINDOW. DELAMINATED. UPPER PORTION OF WINDOW R1 IS DELAMINATING, AND A BUBBLING FLUID IS PRESENT INSIDE THE DELAM, R1 OUTER PANE CRACKED. REMOVED AND REPLACED RT NR 1 WINDSHIELD PER
- [SDR 05FDEA02124](https://openairdocs.org/sdr/05FDEA02124), Jul 28, 2005: PUMP. FAILED. HYD SYS B OVERHEAT LIGHT IN FLT TURNED ELEC PUMP NR 1 OFF AND LIGHT WENT OUT. REMOVED AND REPLACED NR 1 B PUMP PER MM-29-12-011-2. OPS CKS AND LEAK CKS GOOD. CY
- [SDR 05FDEA01866](https://openairdocs.org/sdr/05FDEA01866), Jul 8, 2005: FLAP. JAMMED. ASYMETRICAL INBOARD TRAILING EDGE FLAPS AT 2 DEGREES UPON FLAP RETRACTION. RAN APPROPRIATE QRH PROCEDURES, FOUND LT INBD FLAP COCKED AND JAMMED INTO INBD AILERO

All 70: https://openairdocs.org/deregistered/N204FE-2015-10-01/reports.md

## 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 20071009832349I](https://openairdocs.org/incident/20071009832349I), Oct 9, 2007: Boeing 7272S2F (N204FE), Indianapolis, IN, No damage. (-23) According to pilot descrepancy in aircraft logbook, upon descent into ind from mke #2 low oil pressure filter bypass light illuminated followed by oil…
- [Incident 19960912033309I](https://openairdocs.org/incident/19960912033309I), Sep 12, 1996: Boeing 7272S2F (N204FE), Great Falls, MT. Narrative: on 9/12/96 federal express flight #1531 (B727, N204FE) from memphis reported a fire warning light on the #1 engine while the aircraft was 2 miles…

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