# N136FE: 1968 Boeing 727-25C, registration cancelled 2012-08-06 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: August 6, 2012 - Status when cancelled: Registration pending, canceled - Airframe: [Boeing 727-25C](https://openairdocs.org/model/boeing-727-25c) (registry code 138400H) - Engine: [Pratt & Whitney JT8D series](https://openairdocs.org/engine/pratt-whitney-jt8d-series) (registry code 52053) - Serial number: 19855 - Year built: 1968 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Experimental, showing compliance - Airworthiness date: January 23, 1998 - Last registry action: December 20, 2007 - Mode S code: A091FD - Location: [Utica, NY](https://openairdocs.org/faa-place/NY/Utica) - Owner type: Individual - Owner's area on the map: 43.0813° N, 75.2258° W: Placed by OpenAirDocs at the center of ZIP code 13501, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N136FE - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=136FE - Page: https://openairdocs.org/deregistered/N136FE-2012-08-06 From the FAA registry file of October 27, 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 727-25C: https://openairdocs.org/model/boeing-727-25c.md ## Service difficulty reports (25) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR 05FDEA03795](https://openairdocs.org/sdr/05FDEA03795), Nov 14, 2005: LIGHT. INOPERATIVE. RTO FOR AFT AIRSTAIR LIGHT IAS 75 KTS. RELEASED FOR SERVICE PER MEL/CDL: 52-06-B CATEGORY: C EXPIRATION: 22NOV05 MEL 52-06-B: AMBER AFT AIRSTAIR DOOR WARNING LI - [SDR 05FDEA03509](https://openairdocs.org/sdr/05FDEA03509), Oct 26, 2005: DOOR. OPEN. AFTER DEPARTURE, AIRCRAFT WOULD NOT PRESSURIZE. RAN QRH AND NO SUCCESS. APPLIED SYSTEMS KNOWLEDGE AND COULD NOT SOLVE PROBLEM. RETURNED TO MEMPHIS. AFTER BLOCK- - [SDR 05FDEA02661](https://openairdocs.org/sdr/05FDEA02661), Aug 25, 2005: BRACKET. CRACKED. COVE PANEL BRACKET IS BROKEN ON LOWER WING PANEL BELOW NR 3 SPOILER. REMOVED AND REPLACED 3 EA BRACKET P/N 65-21658Y29, 65-21658-27, AND 65-21658Y30, AND 1 EA R - [SDR 03FDEA01982](https://openairdocs.org/sdr/03FDEA01982), Nov 25, 2003: BATTERY. DISCHARGED. FWD ENTRY AND COCKPIT EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERIES FOR OVERHEAD LIGHT ASSY'S PER FEDEX MM 33-50-101-2. CHECKS - [SDR 03FDEA01917](https://openairdocs.org/sdr/03FDEA01917), Nov 14, 2003: FRAME. CRACKED. FOUND CRACK ON FRAME TOOLING HOLE BS 1050 STR 27L. CUT OUT CRACKED AREA IN FRAME AT BS 1050, STR 27L AND INSTALLED REPAIR DOUBLER IAW SRM 51-40-3. - [SDR 03FDEA01916](https://openairdocs.org/sdr/03FDEA01916), Nov 14, 2003: FRAME. CRACKED. FOUND FRAME CRACKED AROUND OPEN HOLE BS 1070 STR 27L. CUT OUT CRACKED AREA IN FRAME AT BS 1070, STR 27L AND INSTALLED REPAIR DOUBLER IAW SRM 51-40-3 & FED EX EA - [SDR 03FDEA01912](https://openairdocs.org/sdr/03FDEA01912), Nov 13, 2003: WEB. CORRODED. CORROSION ON AFT RIGHT WEB AT BS 1130, RBL 61, WL 208. CORROSION ON AFT RIGHT WEB BS 1130, RBL 61, WL 208 FOUND TO BE OUT OF LIMITS IAW SRM 53-10-1. REPAIRED WE - [SDR 03FDEA01911](https://openairdocs.org/sdr/03FDEA01911), Nov 13, 2003: WEB. CORRODED. CORROSION (C53-224-04), SHEAR WEB BS 1166-1173, RBL 53-62, WL 208. - [SDR 03FDEA01907](https://openairdocs.org/sdr/03FDEA01907), Nov 12, 2003: BEAM. CORRODED. CORRODED LONGITUDINAL BEAM BS 846, LBL 44, WL 208. - [SDR 03FDEA01890](https://openairdocs.org/sdr/03FDEA01890), Nov 7, 2003: SKIN. BULGED. EXTERNAL SKIN BULGED AT BS 350 BETWEEN STR 25R AND 26R. INVESTIGATED BULGED SKIN BS 350, STR 25R & 26R. FOUND SKIN TO BE CORRODED BETWEEN SHIM AND SHEAR TIE. RE - [SDR 03FDEA01889](https://openairdocs.org/sdr/03FDEA01889), Nov 7, 2003: SKIN. DAMAGED. LWR AFT CARGO DOOR SKIN, SKIN DAMAGED ALONG FWD EDGE AT NR 2 STOP FITTING FROM TOP. *S/D* INSPECTED LWR AFT CARGO DOOR SKIN ALONG WD EDGE, DAMAGE WAS 1 X 16 X . - [SDR 03FDEA01891](https://openairdocs.org/sdr/03FDEA01891), Nov 7, 2003: FLOORBEAM. CORRODED. CORROSION ON UPPER CHORD OF FLOORBEAM BS 1130 RBL 61 WL 208. *S/D* REMOVED CORROSION FROM UPPER CHORD BS 1130 FLOORBEAM, RBL 61, WL 208 AND FOUND OUT OF LIMITS. - [SDR 03FDEA01404](https://openairdocs.org/sdr/03FDEA01404), Sep 3, 2003: PANEL. MALFUNCTIONED. ON INITIAL GEAR EXTENTION, ALL RED GEAR DOOR LIGHTS OPERATED NORMALLY BUT ONLY GREEN MAIN GEAR LIGHTS ILLUMINATED (NO GREEN NOSE GEAR LIGHT). RECYCLED GEAR UP / - [SDR 02FDEA00867](https://openairdocs.org/sdr/02FDEA00867), Nov 19, 2002: HANDLE. OUT OF POSITION. ON DEPARTURE, FWD CARGO DOOR LT ILLUM FOLLOWED RED TABS AND ELECTED TO RETURN TO PIT FOR MX ACTION. PRESSURIZATION NOT NORMAL/NOTED PRESS BUMP DURING CLIMBOUT. - [SDR 01FDEA00830](https://openairdocs.org/sdr/01FDEA00830), Sep 11, 2001: DUCT. CRACKED. PASSING 1500 FT ABOVE GROUND LEVEL NR 3 ENG FIRE LIGHT ILLUM WHEN THROTTLE RETARD. REMOVED AND REPLACED 8TH STAGE BLEED DUCT PER MM 36-00-001-2. - [SDR 00FDEA00807](https://openairdocs.org/sdr/00FDEA00807), Nov 29, 2000: CONNECTOR. FAILED. 00-331 ON DEPARTURE, NR 1 LOW OIL PRESS/FILTER BYPASS LIGHT ILLUMINATED. ** S/D ** ACCOMPLISH WIND MILL INSP DUE TO ENG SHUT DOWN PER MM 72-00-518D. R&R BYPASS - [SDR 99FDEA00007](https://openairdocs.org/sdr/99FDEA00007), Jan 9, 1999: RETRACT MECH. MALFUNCTIONED. 99-0007 - DURING FLAP RETRACT, NR 6 SLAT DID NOT FULLY RETRACT. UNABLE TO CORRECT WITH RED TAB PROC. INSPECT SLAT, NO DEFECT FOUND. RAN NR 1 ENG WITH HYD PRESS, - [SDR 98FDEA00372](https://openairdocs.org/sdr/98FDEA00372), May 29, 1998: GPWS. MALFUNCTION. 98-0141 - GPWS WARNING FOR GEAR AT 500 FT ABOVE GROUND LEVEL (FULL LANDING CONFIGURATION). DURING TROUBLE SHOOTING PROCESS, FOUND TAILSKID CANNON PLUG. INSTALLE - [SDR 96FDEA01421](https://openairdocs.org/sdr/96FDEA01421), Aug 30, 1996: STICK SHAKER. FAILED TEST. CONTINUOUS STICK SHAKER AT TAKEOFF. STANDARD POWER TAKEOFF 36C, ADVANCED THROTTLES TO MOMENTARY FIREWALL POWER. PULLED AC NR 1 STALL WARNING CIRCUIT BREAKER, SH - [SDR 96FDEA01369](https://openairdocs.org/sdr/96FDEA01369), Aug 15, 1996: RETURN HYD LINE. BROKEN. TOTAL LOSS OF A-SYS HYD AT FLT LEVEL 280. GEAR MANUALLY EXTENDED AND FLAPS WERE EXTENDED THROUGH ALTERNATE FLAP MASTER. REMOVED AND REPLACED SPOILER RETURN LINE - [SDR 96FDEA01050](https://openairdocs.org/sdr/96FDEA01050), May 28, 1996: FLOOR WEB. CORROSION. CABIN CORROSION ON FLOOR WEB STA 1178 APPROX 55 INCHES LBL UPPER SURFACE UNDER CHORD ANGLE. CUT OUT DAMAGED FLOOR WEB AREA, FABRICATED AND INSTALLED DOUBLER REP - [SDR 96FDEA01049](https://openairdocs.org/sdr/96FDEA01049), May 28, 1996: VERT ANGLE. CRACKED. VERT ANGLE CRACKED AT LIGHTENING HOLE AT BS 1183 RBL 26 TO 9 WL 253. PERFORMED 1183 VERTICAL BEAM MOD PER BOEING SERVICE BULLETIN 727-53-0182 PG 23 SRM 53-10-9. - [SDR 96FDEA01048](https://openairdocs.org/sdr/96FDEA01048), May 28, 1996: HINGE CASTING. BROKEN. LARGE HINGE ASSEMBLY FOR LEFT HAND O/B AILERON HAS BAR BROKEN OFF. REMOVED HINGE CASTING AND INSTALLED A SERVICEABLE CASTING PER DRAWING NR 65-19260 SHEET 1. - [SDR 96FDEA01047](https://openairdocs.org/sdr/96FDEA01047), Apr 30, 1996: DOOR FRAME. CRACKED. CRACK IN LWR FWD CORNER OF DOOR FRAME OF FWD LWR CARGO APPROX 1 INCH LONG. STOP DRILLED CRACK AND INSTALLED 7075-6, 0.90 DOUBLER ANGLE PER SRM 53-10-4 PG 39 TO - [SDR 95FDEA01510](https://openairdocs.org/sdr/95FDEA01510), Oct 7, 1995: HYD LINE. BROKEN. DURING CRUISE FL 290, A/C LOST SYS A-HYD, NO APPARENT REASON. FOUND NR 2 SPOILER PRESS LINE BROKE. REMOVED AND REPLACED PRESS LINE, REMOVED CASE DRAIN FILTERS A ## Other aircraft with N136FE - [Registered now](https://openairdocs.org/aircraft/N136FE): Boeing 767-300F, S/N 64058, built 2019 --- 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.