# N300NE: Boeing 727-25, registration cancelled 2017-06-07 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: June 7, 2017 - Status when cancelled: Registration expired, pending cancellation - Airframe: [Boeing 727-25](https://openairdocs.org/model/boeing-727-25) (registry code 1384006) - Serial number: 18974 - Type of aircraft: Fixed wing multi engine - Certificate issued: July 20, 2002 - Last registry action: July 15, 2008 - Mode S code: A32083 - Owner when cancelled: [Dodson International Parts Inc](https://openairdocs.org/faa-owner/DODSON%20INTERNATIONAL%20PARTS%20INC) - Location: [Rantoul, KS](https://openairdocs.org/faa-place/KS/Rantoul) - Owner type: Corporation - Owner's area on the map: 38.5420° N, 95.1245° W: Placed by OpenAirDocs at the center of ZIP code 66079, within about 3 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N300NE - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=300NE - Page: https://openairdocs.org/deregistered/N300NE-2017-06-07 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 727-25: https://openairdocs.org/model/boeing-727-25.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 EISA99147](https://openairdocs.org/sdr/EISA99147), Jul 28, 1999: MECHANISM. NOT LATCHED. FORWARD ENTRY DOOR NOT CLOSED PROPERLY, COULD NOT PRESSURIZE AIRCRAFT. OPENED DOOR AND CLOSED PROPERLY. (M) - [SDR EISA99142](https://openairdocs.org/sdr/EISA99142), Jul 13, 1999: ANTENNA. OUT OF ADJUST. RADARS SPOKING AND WOULD NOT PAINT TARGETS. REPLACED CONTROL PANEL, REPLACED RADOME INSTALLED WAVE GUIDE WINDOW. CHECKED AND ADJUSTED ANTENNA PITCH. CLEANED RAD - [SDR EISA99023](https://openairdocs.org/sdr/EISA99023), Feb 12, 1999: SMOKE DETECTOR. MALFUNCTIONED. CARGO SMOKE LIGHT ILLUMINATED IN FLIGHT NO OTHER INDICATIONS OF SMOKE, LIGHT WENT OUT AFTER 10 MINUTES. PERFORMED FUNCTIONAL CHECK OF CARGO SMOKE DETECTOR. (M) - [SDR EISA98214](https://openairdocs.org/sdr/EISA98214), Sep 9, 1998: SMOKE DETECTOR. MALFUNCTIONED. NR 4 SMOKE DETECTOR WILL NOT TEST, ON PREFLIGHT, GENERATED BY PILOT REPORT. REMOVED AND REPLACED NR 4 SMOKE DETECTOR POWER SUPPLY. OPS CHECK NORMAL PER MM CHAPT - [SDR EISA98205](https://openairdocs.org/sdr/EISA98205), Aug 13, 1998: SENSOR. FAILED. LOWER RUDDER IND FULL LEFT DEFLECTION ALL TIME, ON GROUND. REMOVED AND REPLACED LOWER RUDDER POSITION SENSOR PER 22-11-51. OPS CHECK NORMAL. (M) - [SDR EISA98199](https://openairdocs.org/sdr/EISA98199), Jul 30, 1998: SHUTOFF VALVE. FAILED. AFTER TAKEOFF FROM BDL, AIRCRAFT WOULD NOT PRESSURIZE, RETURNED TO BDL GENERATED FROM PILOT REPORT. REMOVED AND REPLACED LEFT PACK VALVE. REMOVED AND REPLACED O - [SDR EISA98198](https://openairdocs.org/sdr/EISA98198), Jul 30, 1998: RT PACK. MALFUNCTIONED. AFTER TAKEOFF AIRCRAFT WOULD NOT PRESSURIZE, RETURNED TO BDL. GENERATED FROM PILOT REPORT. RESET RIGHT PACK. (M) - [SDR 98ZZZM625](https://openairdocs.org/sdr/98ZZZM625), Jul 30, 1998: CONTROL VALVE. FAILED. AFTER TAKEOFF FROM BDL, AIRCRAFT WOULD NOT PRESSURIZE, RETURNED TO BDL GENERATED FROM PILOT REPORT. REMOVED AND REPLACED LEFT PACK VALVE. REMOVED AND REPLACED O - [SDR 98ZZZM624](https://openairdocs.org/sdr/98ZZZM624), Jul 30, 1998: OUTFLOW VALVE. FAILED. AFTER TAKEOFF FROM BDL, AIRCRAFT WOULD NOT PRESSURIZE, RETURNED TO BDL GENERATED FROM PILOT REPORT. REMOVED AND REPLACED LEFT PACK VALVE. REMOVED AND REPLACED O - [SDR EISA98180](https://openairdocs.org/sdr/EISA98180), Jul 22, 1998: CONNECTOR. CONTAMINATED. DURING PRE-FLIGHT, THE SECOND FROM THE LEFT BUTTON, MAIN CARGO SMOKE DETECTOR SYSTEM WOULD NOT TEST. GENERATED FROM PILOT REPORT. CLEANED CANNON PLUG PER MM CHA - [SDR EISA98175](https://openairdocs.org/sdr/EISA98175), Jul 11, 1998: VALVE. FAILED. CLIMBING THROUGH 17,000 FEET, LOSS OF ALL PRESSURIZATION, CABIN CLIMBED TO 14,000 FEET. NO CONTROL IN ANY MODE. INITIATED DESCENT TO 9,000 FEET. CABIN ALTITUDE - [SDR EISA98143](https://openairdocs.org/sdr/EISA98143), Jun 20, 1998: SMOKE DETECTOR. MALFUNCTIONED. MAIN CARGO SMOKE DETECTOR INDICATOR 'CARGO SMOKE' ILLUMINATED WILL NOT EXTINGUISH. WILL NOT TEST. REPLACED NR 3 SMOKE DETECTOR, SYSTEM CHECKED NORMAL PER MM 26- - [SDR EISA97173](https://openairdocs.org/sdr/EISA97173), Aug 6, 1997: WEB. CRACKED. DURING B-SERVICE AND THE ACCOMPLISHMENT OF CPCP CARD NR C53-224-01, FOUND CRACK AT FLOOR WEB, FS 1050 - FS 1070. TT: 73,279:23 HOURS. TC: 55,830. (X) - [SDR EISA97172](https://openairdocs.org/sdr/EISA97172), Aug 6, 1997: CROSS RIB. CRACKED. DURING B-SERVICE AND THE ACCOMPLISHMENT OF CPCP CARD NR C53-224-01, FOUND CROSS-RIB CRACKED AT FS 1110 BETWEEN SEAT TRACKS. FABRICATED AND INSTALLED REPAIR SRM - [SDR EISA97171](https://openairdocs.org/sdr/EISA97171), Aug 6, 1997: ANGLE. CORRODED. DURING B-SERVICE AND THE ACCOMPLISHMENT OF CPCP CARD NR C53-111-01, FOUND CORROSION ON ANGLE IN LOWER LOBE, FS 196.5. REMOVED ANGLE, FABRICATED AND INSTALLED NE - [SDR EISA97170](https://openairdocs.org/sdr/EISA97170), Aug 6, 1997: SUPPORT. CRACKED. DURING B-SERVICE AND THE ACCOMPLISHMENT OF CPCP CARD NR C53-113-01, FOUND FLOOR SUPPORT CRACK AT FS 540, STR 27. FABRICATED AND INSTALLED REPAIR DOUBLER PER SRM - [SDR EISA97169](https://openairdocs.org/sdr/EISA97169), Aug 6, 1997: FLOOR BEAM. CRACKED. DURING B-SERVICE AND THE ACCOMPLISHMENT OF CPCP CARD NR 53-113-01, FOUND CRACK IN FLOOR SUPPORT AT FS 600 - FS 620, STR 27R, FORWARD CARGO PIT AREA. FABRICATED - [SDR EISA97168](https://openairdocs.org/sdr/EISA97168), Aug 6, 1997: FLOOR BEAM. CORRODED. DURING B-SERVICE AND THE ACCOMPLISHMENT OF CPCP CARD C53-111-01 PJ2 FOUND FORWARD CARGO BIN FLOOR STRUCTURE EXFOLIATED AT FS 680, STR 26L. REMOVED DAMAGED MATER - [SDR EISA97118](https://openairdocs.org/sdr/EISA97118), Jun 3, 1997: LIGHT. INOPERATIVE. EMERGENCY EXIT LIGHTS ARE DISCHARGED. REPLACED LIGHT ASSEMBLY AT COCKPIT DOOR OPS CHECK GOOD. (M) - [SDR EISA97081](https://openairdocs.org/sdr/EISA97081), Apr 23, 1997: FIRE WARNING. ILLUMINATED. WHEEL WELL FIRE LIGHT CAME ON WHILE RETURNING TO DAL, PERFORMED EMERGENCY ITEMS, LIGHT WENT OUT. PERFORMED INSPECTION OF WHEEL WELL AND FIRE DETECTOR LOOPS. FOU - [SDR EISA96263](https://openairdocs.org/sdr/EISA96263), Sep 15, 1996: RIB. CRACKED. FOUND RIB CRACKED AT FORWARD SIDE OF UPPER VENT BOX AT WING STATION 686.5. INSTALLED REPAIR PER SRM 57-10-05. (M) - [SDR EISA96262](https://openairdocs.org/sdr/EISA96262), Sep 15, 1996: RIB. CRACKED. FOUND 2 CRACKS FROM FASTENER HOLES IN RIGHT WING RIB CHORD UPPER VERTICAL FLANGE WS 70.5 RT SIDE. INSTALLED REPAIR PER SB 727-57-0112. (M) - [SDR EISA96261](https://openairdocs.org/sdr/EISA96261), Sep 15, 1996: CHORD. CRACKED. RIGHT PLUS CHORD CRACKED AT FS 760.95 RBL 70.5. STOP DRILLED CRACK AND INSTALLED REPAIR PER SB 727-57-0112. (M) - [SDR EISA96260](https://openairdocs.org/sdr/EISA96260), Sep 15, 1996: SKIN. CORROSION. FUSELAGE SKIN CORROSION AT FS 303 LEFT SIDE, JUST BELOW FORWARD AIRSTAIR DOOR. REMOVED AND REPLACED DAMAGED SKIN PER SRM 51-10-06 FROM STATION 259 TO 360. (M) - [SDR EISA96259](https://openairdocs.org/sdr/EISA96259), Sep 15, 1996: WIRE. MISINSTALLED. DURING INSTALLATION OF SERVICE BULLETIN NR 727-2-008 ON MAIN CARGO DOOR FOUND WIRING TO NOT BE IN CONFORMITY WITH WIRING PRINT NR AE727-2-008. REWIRED MCD PER A - [SDR EISA96258](https://openairdocs.org/sdr/EISA96258), Sep 15, 1996: RIB. CRACKED. FOUND WING RIB CRACKED IN TWO PLACES AT RIGHT WS 629.5. INSTALLED REPAIR PER SRM 57-10-05. (M) - [SDR EISA96257](https://openairdocs.org/sdr/EISA96257), Sep 15, 1996: RIB. CRACKED. FOUND RIB CRACKED IN THREE PLACES AT LT WS 629.5. INSTALLED NEW RIB PER SB 57-017. (M) - [SDR EISA96256](https://openairdocs.org/sdr/EISA96256), Sep 15, 1996: RIB. CRACKED. FOUND WING RIB CRACKED AT RT WS 601.5. REMOVED AND REPLACED DAMAGED RIB PER SB 727-57A-159. (M) - [SDR EISA96255](https://openairdocs.org/sdr/EISA96255), Sep 15, 1996: RIB. CRACKED. FOUND WING RIB CRACKED AT RT WS 546.5. FABRICATED AND INSTALLED REPAIR CHANNEL PER 57-10-05. (M) - [SDR EISA96254](https://openairdocs.org/sdr/EISA96254), Sep 15, 1996: STRINGER. CRACKED. FOUND STRINGER CRACKED, 3RD UPPER, FORWARD OF REAR SPAR LEFT WS 546.5. STOP DRILLED CRACK AND INSTALLED REPAIR PER SB 727-57-129. (M) - [SDR EISA96253](https://openairdocs.org/sdr/EISA96253), Sep 15, 1996: RIB. CRACKED. FOUND THREE CRACKS IN WING RIB AT LEFT WS 601.5. FABRICATED AND INSTALLED REPAIR PER SRM 57-10-00. (M) - [SDR EISA96252](https://openairdocs.org/sdr/EISA96252), Sep 15, 1996: FRAME. MISDRILLED. FOUND FUSELAGE FRAME MISDRILLED AT BS 783.95, LEFT, 4TH FASTENER HOLE UP FROM CABIN FLOOR. INSTALLED REPAIR KIT PER SB 727-53-0197. (M) - [SDR EISA96251](https://openairdocs.org/sdr/EISA96251), Sep 15, 1996: FRAME. MISDRILLED. FOUND FUSELAGE FRAME MISDRILLED AT BS 825.95, LEFT, 4TH FASTENER HOLE UP FROM CABIN FLOOR. HOLE TO FIRST OVERSIZE AND INSTALLED REPAIR STRAP PER SB 727-53-0197. - [SDR EISA96250](https://openairdocs.org/sdr/EISA96250), Sep 15, 1996: FRAME. CRACKED. FOUND FUSELAGE FRAME CRACKED AT BS 760.95 RIGHT, 4TH FASTENER HOLE UP FROM CABIN FLOOR. INSTALLED REPAIR KIT PER SB 53-0197. (M) - [SDR EISA96249](https://openairdocs.org/sdr/EISA96249), Sep 15, 1996: ANGLE. CRACKED. NR 2 LE FLAP ACTUATOR MOUNT, INBOARD UPPER ANGLE CRACKED. FABRICATED AND INSTALLED NEW ANGLE PER SRM 51-10-0 AND 51-12-1. (M) - [SDR EISA96248](https://openairdocs.org/sdr/EISA96248), Sep 15, 1996: RIB. CRACKED. FOUND RIGHT WING LEADING EDGE RIB CRACKED AT WS 330. FABRICATED AND INSTALLED DOUBLER PER SRM 51-30-02. (M) - [SDR EISA96247](https://openairdocs.org/sdr/EISA96247), Sep 15, 1996: ANGLE. CRACKED. FOUND GALLEY SERVICE DOOR ANGLE CRACKED AT BOTTOM LOWER FRAME AT FORWARD END. REPLACED ANGLE PER SRM 51-30-02. (M) - [SDR EISA96246](https://openairdocs.org/sdr/EISA96246), Sep 15, 1996: ANGLE. CORRODED. FOUND FORWARD ENTRY DOOR LOWER FRAME CORNER AFT ANGLE HAS EXFOLIATING CORROSION. REMOVED AND REPLACED ANGLE PER SRM 51-10-01. (M) - [SDR EISA96245](https://openairdocs.org/sdr/EISA96245), Sep 15, 1996: FRAME. CRACKED. FOUND 3.25 INCH CRACK IN FRAME OF FORWARD ENTRY DOOR AS SEEN FROM 2ND LIGHTENING HOLE FROM AFT, 6, UP FROM LOWER FRAME. FABRICATED AND INSTALLED REPAIR PER SRM - [SDR EISA96244](https://openairdocs.org/sdr/EISA96244), Sep 15, 1996: RIB. CRACKED. FOUND LEFT WING RIB CRACKED AT WS 656.5, 2ND LOWER STRINGER FROM REAR SPAR. INSTALLED RIB REPAIR PER SRM 57-10-05. (M) - [SDR EISA96243](https://openairdocs.org/sdr/EISA96243), Sep 15, 1996: WINDOW POST. CRACKED. FOUND CAPTAINS E-F WINDOW POST CRACKED. INSTALLED DOUBLER PER SB 53-0086. (M) - [SDR EISA96242](https://openairdocs.org/sdr/EISA96242), Sep 15, 1996: INTERCOSTAL. CRACKED. FOUND CABIN LEFT FS 804, STRINGER 17 INTERCOSTAL WEB CRACKED. FABRICATED AND INSTALLED DOUBLER PER SRM 51-30-02. (M) - [SDR EISA96241](https://openairdocs.org/sdr/EISA96241), Sep 14, 1996: FLOOR BEAM. CRACKED. FOUND CABIN FLOOR BEAM CRACKED FROM FASTENER HOLE TO AFT END FS 940 RBL 58. INSTALLED FLOOR BEAM REPAIR PER SB 727-53. (M) - [SDR EISA96240](https://openairdocs.org/sdr/EISA96240), Sep 14, 1996: RIB. CRACKED. FOUND NR 3 ENGINE PYLON RIB CRACKED, ACCESS THROUGH PANEL 5510. BLENDED DAMAGED AREA, FABRICATED AND INSTALLED PER SRM 54-20-03. (M) - [SDR EISA96239](https://openairdocs.org/sdr/EISA96239), Sep 14, 1996: PYLON. CRACKED. FOUND NR 1 ENGINE PYLON TRAILING EDGE CRACKED JUST AFT OF BULB SEAL. FABRICATED NEW TRAILING EDGE ANGLES AND INSTALLED PER SRM 53-20-02. (M) - [SDR EISA96238](https://openairdocs.org/sdr/EISA96238), Sep 14, 1996: RIB. BULGED. FOUND NR 5 SLAT, OUTBOARD TRACK FITTING, INBOARD RIB WEB BULGING. INSTALLED NEW FITTING PER SRM 51-10-1. (M) - [SDR EISA96237](https://openairdocs.org/sdr/EISA96237), Sep 14, 1996: RIB. CRACKED. NR 5 SLAT, INTERNAL OUTBOARD NOSE RIB CRACKED. REMOVED AND REPLACED RIB PER SRM 51-10-06. (M) - [SDR EISA96236](https://openairdocs.org/sdr/EISA96236), Sep 14, 1996: SKIN. CRACKED. FOUND BONDED BEAD'S IN ELEVATOR SKIN, INTERNAL SURFACE ARE CRACKED IN THREE PLACES, INBOARD, END. STOP DRILLED CRACKS, FABRICATED AND INSTALLED DOUBLERS PER SRM - [SDR EISA96235](https://openairdocs.org/sdr/EISA96235), Sep 14, 1996: DOOR. CRACKED. FOUND GALLEY DOOR UPPER GATE DOOR IS CRACKED. REPLACED DOOR WITH SERVICEABLE UNIT. (M) - [SDR EISA96234](https://openairdocs.org/sdr/EISA96234), Sep 14, 1996: RIB. CRACKED. FOUND RIGHT WING RIB CRACKED AT 3RD LOWER STRINGER FROM AFT SPAR, WS 546.5. FABRICATED AND INSTALLED REPAIR CHANNEL PER SRM 57-10-05. (M) All 70: https://openairdocs.org/deregistered/N300NE-2017-06-07/reports.md ## Other aircraft with N300NE - [Registered now](https://openairdocs.org/aircraft/N300NE): Beech 95-B55 (T42A), S/N TC-1172, built 1968 --- 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.