# N133FE: 1967 Boeing 727-25C, registration cancelled 2004-08-26 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: August 26, 2004 - Status when cancelled: Triennial form not returned - Airframe: [Boeing 727-25C](https://openairdocs.org/model/boeing-727-25c) (registry code 138400H) - Engine: [Pratt & Whitney JT8D-1](https://openairdocs.org/engine/pratt-whitney-jt8d-1) (registry code 52044) - Data sheets: [TCDS E2EA](https://openairdocs.org/tcds/E2EA) (OpenAirDocs) - Serial number: 19851 - Year built: 1967 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: January 2, 1968 - Certificate issued: May 8, 1980 - Last registry action: September 16, 2003 - Mode S code: A086D8 - Owner when cancelled: [Federal Express Corporation](https://openairdocs.org/faa-owner/FEDERAL%20EXPRESS%20CORPORATION) - Location: [Memphis, TN](https://openairdocs.org/faa-place/TN/Memphis) - Owner type: Corporation - Owner's area on the map: 35.0351° N, 89.9272° W: Placed by OpenAirDocs at the center of ZIP code 38118, within about 3 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N133FE - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=133FE - Page: https://openairdocs.org/deregistered/N133FE-2004-08-26 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 727-25C: https://openairdocs.org/model/boeing-727-25c.md ## Service difficulty reports (38) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR 99FDEA00104](https://openairdocs.org/sdr/99FDEA00104), Mar 16, 1999: WINDOW. CRACKED. PILOTS WINDOW CRACKED IN FLIGHT. INSTALL SERVICEABLE L-1 WINDOW, REFERENCE B727-100 MM 56-11-011-4. - [SDR 99FDEA00026](https://openairdocs.org/sdr/99FDEA00026), Jan 23, 1999: COMPUTER. MALFUNCTIONED. 99-002O - ELEVATOR HAS 5 TO 6 INCH OF FREEPLAY IN THE YOKE (I.E.) MOVING THE YOKE AND NO RESPONSE FROM THE ELEVATOR. REMOVED AND REPLACED ELEV FEEL COMPUTER, AD - [SDR 98FDEA00742](https://openairdocs.org/sdr/98FDEA00742), Dec 11, 1998: FEEL UNIT. INOP. AFTER DEPARTURE AT 2000 TO 3000 FT MSL, 200 PLUS KNOTS, ELEVATOR FEEL WENT LIMP FOR 3 TO 5 SEC. THEN WITHOUT WARNING FEEL RETURN. *S/D* REMOVED AND REPLACED PNL - [SDR 98FDEA00499](https://openairdocs.org/sdr/98FDEA00499), Aug 11, 1998: SOCKET. MALFUNCTIONED. 98-200 - ON SHORT FINAL, NOSE GEAR MAIN GREEN LIGHTS BOTH WENT OUT. AFTER GO AROUND RECYCLED GEAR AND BOTH LIGHTS KEPT FLICKERING. BULBS TESTED GOOD. INSPECTED - [SDR 98FDEA00405](https://openairdocs.org/sdr/98FDEA00405), Jun 17, 1998: WINDSHIELD. CRACKED. 98-0155 - STA-IAD - SAW FLAME AND ARCING ON COPILOTS FROM WIND SCREEN RIGHT NR 1 FROM WINDOW HEAT. WINDOW HEAT WAS SECURED ON RIGHT SIDE, MINUTES LATER WIND SCR - [SDR 98FDEA00115](https://openairdocs.org/sdr/98FDEA00115), Feb 18, 1998: DOOR. BLOWN OFF. AIRCRAFT HYDRAULIC SERVICE ACCESS DOOR BLOWN OFF IN FLIGHT. CANNIBALIZED DOOR FROM AIRCRAFT 146 AND INSTALLED ON AIRCRAFT 133, OPS CHECK GOOD. - [SDR 97FDEA00298](https://openairdocs.org/sdr/97FDEA00298), May 21, 1997: POSITION SWITCH. MALFUNCTION. WHEN GEAR PLACED DOWN, NOSE WHEEL GREEN LIGHT WOULD NOT ILLUMINATE. PRESS TO TEST GOOD. CYCLED GEAR AND GOT A GREEN DOWN AND LOCKED LIGHT. AFTER TROUBLESHOOTING - [SDR 95FDEA01753](https://openairdocs.org/sdr/95FDEA01753), Nov 14, 1995: FITTING. CORRODED. LT STA 740 WING TERMINAL FITTING ON FUSELAGE, BORE IS CORRODED. REMOVED CORROSION BY BORING HOLE TO 3500 PER SRM 57-10-7 PAGE 3, MADE SLEEVE PER SRM 57-10-7 PAR - [SDR 95FDEA01722](https://openairdocs.org/sdr/95FDEA01722), Nov 13, 1995: FLOORBEAM. CORRODED. STA 380 FLOORBEAM FOUND TO BE TOO THIN AFTER CORROSION REWORK AT APPROX LBL 54 UPPER AFT FLANGE. REPAIRED FLOORBEAM PER EA 7-5310-25983 DATED 10-26-95. - [SDR 95FDEA01723](https://openairdocs.org/sdr/95FDEA01723), Nov 9, 1995: TRUNNION. CRACKED. L/W FRONT SPAR BOTTLE BOLT TRUNNION FS 740 CRACKED INSIDE PIN HOLE, 3 PLACES. REMOVED AND REPLACED TRUNNION IAW BOEING DRAWING NR 65C29064. - [SDR 95FDEA01637](https://openairdocs.org/sdr/95FDEA01637), Oct 30, 1995: FLOOR BEAM. CORRODED. MAIN CARGO - CORROSION ON BOTTOM OF UPPER FLANGE OF FLOOR BEAM AT STA 640 BETWEEN NR 5 AND NR 6 SEAT TRACK. REMOVED CORROSION PER SRM 51-10-06. REPAIRED FLOOR B - [SDR 95FDEA01636](https://openairdocs.org/sdr/95FDEA01636), Oct 30, 1995: DOOR FRAME. CRACKED. FORWARD CARGO AFT CARGO DOOR FRAME STA 572 CRACKED FROM AROUND RIVET ON FRAME AFT DOOR STOP AREA. REMOVED RIVET AND STOP DRILLED. INSTALLED DOUBLER PER 51-10-4, - [SDR 95FDEA01638](https://openairdocs.org/sdr/95FDEA01638), Oct 29, 1995: SPAR CHORD. CORRODED. BS 740, LBL 40 - 46: WING CENTER SECTION FRONT SPAR LOWER CHORD TO LOWER TANK SKIN HAS HEAVY CORROSION. RIVET HEADS SHEARED AND SKIN BULGING. REPAIR PER EA NR 7 - [SDR 95FDEA01597](https://openairdocs.org/sdr/95FDEA01597), Oct 24, 1995: INTERCOSTAL. CRACKED. AFT CARGO CEILING CORROSION AROUND NUTPLATES STA 1110 AT BL 0. REMOVED CORROSION AND REPAIRED BOTTOM CAP OF BL 0 INTERCOSTAL STA 1110 PER ESO 11782 WITH FEDEX E - [SDR 95FDEA01634](https://openairdocs.org/sdr/95FDEA01634), Oct 23, 1995: SPAR WEB. CORRODED. WING CENTER SECTION, RT SPAR LOWER PORTION OF WEB, SHOWS EVIDENCE OF BULGING AND CORROSION AT LBL 20, BS 870, WEB AND LOWER SPAR CHORD. REMOVED CORROSION AND IN - [SDR 95FDEA01631](https://openairdocs.org/sdr/95FDEA01631), Oct 23, 1995: SKIN. CORRODED. LFEC INSPECTION INDICATES CORROSION EXCEEDING 10 PERCENT AT BS 441 BETWEEN STR 23-24R FWD LAP. REMOVED CORROSION AND INSTALLED 6.50 INCH BY 14 INCH DOUBLER PER - [SDR 95FDEA01582](https://openairdocs.org/sdr/95FDEA01582), Oct 23, 1995: SKIN. CORRODED. LFEC INSP INDICATES CORROSION EXCEEDING 10 PERCENT AT BS 441 BETWEEN STR 23 TO 24 RT FWD LAP. REMOVED CORROSION AND INSTALLED 6.5 INCH BY 14 INCH DOUBLER PER SR - [SDR 95FDEA01640](https://openairdocs.org/sdr/95FDEA01640), Oct 20, 1995: STRINGER. CRACKED. STR 8L IS CRACKED AT LOWER FLANGE ATTACH POINT TO FRAME AT STA 460 IN UPPER LOBE. REMOVED DAMAGED SECTION OF STR 8L STR 460 IN UPPER LOBE. REPAIRED PER SRM 53-1 - [SDR 95FDEA01635](https://openairdocs.org/sdr/95FDEA01635), Oct 20, 1995: SKIN. CRACKED. SKIN CRACKED JUST BELOW STR 6 AT FWD ENTRY CUT-OUT (MARKED). INSTALLED FWD ENTRY DOUBLER PER SB 727-53-18621 AND AGING AIRCRAFT AD 94-05-04. - [SDR 95FDEA01633](https://openairdocs.org/sdr/95FDEA01633), Oct 20, 1995: STRINGER. CRACKED. MAIN CARGO STR 16R CRACK AT FRAME STA 500. REMOVED INTERCOSTAL, CUT OUT DAMAGED SECTION OF STRINGER AND INSTALLED REPAIR PER SRM 53-10-3. - [SDR 95FDEA1570](https://openairdocs.org/sdr/95FDEA1570), Oct 19, 1995: FLOORBEAM. CHIPPED. STA 920 FLOORBEAM IN UPPER LOBE, LOWER FLANGE CHIPPED OUT AT FASTENER HOLE RBL 28 (NR 0753). REMOVED DAMAGED PORTION OF FLOORBEAM AND REPAIRED PER ESO 11782 DAT - [SDR 95FDEA1569](https://openairdocs.org/sdr/95FDEA1569), Oct 19, 1995: STRINGER. CRACKED. MAIN CARGO UPPER LOBE, STR 16R CRACKED AT STA 380 ATTACHMENT TO FRAME (NR 1020). CUT OUT DAMAGED AREA, REPAIRED PER SRM 53-10-3 PG 3. - [SDR 95FDEA01721](https://openairdocs.org/sdr/95FDEA01721), Oct 19, 1995: FLOORBEAM. DAMAGED. STA 920 FLOORBEAM IN UPPER LOBE, LOWER FLANGE CHIPPED OUT AT FASTENER HOLE RBL 28. REMOVED DAMAGED PORTION OF FLOORBEAM AND REPAIRED PER ESO 11782 DATED 10-13-9 - [SDR 95FDEA1568](https://openairdocs.org/sdr/95FDEA1568), Oct 18, 1995: CARGO FLOOR. CRACKED. AFT CARGO FLOOR CRACK IN FRAME AROUND TOOLING HOLE STA 1090, JUST ABOUT STR 27 LT (NR 1020). FABRICATED FRAME REPAIR PER SRM 51-40-3, DOUBLER INSTALLED. - [SDR 95FDEA1567](https://openairdocs.org/sdr/95FDEA1567), Oct 18, 1995: DOUBLER. CRACKED. TOP FUSELAGE SKIN AT RADOME BULKHEAD STATION 178 CENTER, DOUBLER TOP OF SKIN IS CUT HAS SEVERAL CRACKS AT EDGE (NR 0704). REMOVED OLD DOUBLER, FABRICATED AND IN - [SDR 95FDEA1566](https://openairdocs.org/sdr/95FDEA1566), Oct 18, 1995: CLIP. GOUGED. STR 4L GOUGED UNDER STR CLIP STATION 970, (NR 0707). INSTALLED STR SPLICE AND FILLER PER SRM 53-10-3 FIG 3 PG 5 TO 8. - [SDR 95FDEA1565](https://openairdocs.org/sdr/95FDEA1565), Oct 18, 1995: PRESS DECK. CORRODED. HEAVY CORROSION IN RT WHEEL WELL PRESSURE DECK LOCATED JUST O/B AND AFT OF VIEW WINDOW (NR 1036). FILE OPEN - [SDR 95FDEA1564](https://openairdocs.org/sdr/95FDEA1564), Oct 18, 1995: FLOORBEAM. CORRODED. CORROSION ON BOTTOM AND TOP OF UPPER FLANGE OF FLOORBEAM STA 480 LBL 24 RBL 24 IN UPPER LOBE (NR 0757). FILE OPEN - [SDR 95FDEA01719](https://openairdocs.org/sdr/95FDEA01719), Oct 18, 1995: TANK. CORRODED. CTR FUEL TANK NR 3 BAY RIVET HEAD POPPED AND WEB BULGING AT STA 870, APPROX RBL 12 AT UPPER REAR CHORD ANGLE. INSTALLED REPAIR PER ESO 11782 DATED 10-12-95 AND - [SDR 95FDEA01718](https://openairdocs.org/sdr/95FDEA01718), Oct 18, 1995: PIN. CORRODED. LT REAR SPAR TO BODY TERMINAL PIN IS CORRODED. REPLACED CORRODED PIN WITH NEW PIN. - [SDR 95FDEA01717](https://openairdocs.org/sdr/95FDEA01717), Oct 18, 1995: PIN. CORRODED. LT REAR SPAR TO BODY TERMINAL PIN IS CORRODED. REPLACED CORRODED PIN WITH NEW PIN. - [SDR 95FDEA01632](https://openairdocs.org/sdr/95FDEA01632), Oct 18, 1995: STRINGER. DAMAGED. STR 41 GOUGED UNDER STR CLIP STA 970. INSTALLED STR SPLICE AND FILLER PER SRM 53-10-3, FIG 3, PG 5-8. - [SDR 95FDEA01600](https://openairdocs.org/sdr/95FDEA01600), Oct 18, 1995: FLOORBEAM. CORRODED. CORROSION ON TOP AND BOTTOM OF UPPER FLANGE OF FLOORBEAM STA 480 LBL 24 RBL 24 IN UPPER LOBE. REMOVED CORROSION AND INSTALLED REPAIR IAW 53-10-8 AND EA 7-5310-2 - [SDR 95FDEA01720](https://openairdocs.org/sdr/95FDEA01720), Oct 17, 1995: PIN. CORRODED. R/W REAR SPAR TO BODY FITTING PIN CORRODED. REMOVED RUSTED CORRODED BODY FITTING PIN. INSTALLED NEW R/W REAR TO BODY FITTING PIN MM 57-41-1. - [SDR 95FDEA01560](https://openairdocs.org/sdr/95FDEA01560), Oct 17, 1995: FLOORBEAM. CORRODED. CORROSION ON LWR SIDE OF UPPER LOBE FLOORBEAM STA 480 LBL 24 TO 44. INSTALLED REPAIR IAW 53-10-8 FIG 5 OF SRM AND IAW ATTACHED JOB PROGRESS FORM. - [SDR 95FDEA01559](https://openairdocs.org/sdr/95FDEA01559), Oct 17, 1995: FLOOR WEB. CORRODED. UPPER LOBE FLOOR WEB CORRODED AT STA 540 LBL 44 TO 65. REMOVED CORROSION PER SRM 51-10-6 PG 4 AND INSTALLED DOUBLER PER SRM CHAPTER 53-10-9. - [SDR 95FDEA01547](https://openairdocs.org/sdr/95FDEA01547), Oct 16, 1995: SILL. CORRODED. MCD THRESHOLE SILL PLATE CORRODED AT STA 560. REMOVED CORROSION PER 51-10-6 PG 4 TO 5, INSTALLED DOUBLER AT STA 560 PER SRM 53-10-9 PG 11, REF NR 0098. - [SDR 95FDEA01531](https://openairdocs.org/sdr/95FDEA01531), Oct 10, 1995: FRAME. CORRODED. THE AREA ABOVE CARGO DOOR, CORROSION ON FRAME BETWEEN STA 1070 TO 1090 RT BELOW STR 18R. ## 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 19870624046669I](https://openairdocs.org/incident/19870624046669I), Jun 24, 1987: Boeing 72725C (N133FE), Memphis, TN, Minor damage. Returned with fire warning light on. Found hole in starter duct elbow. ## Other aircraft with N133FE - [Registered now](https://openairdocs.org/aircraft/N133FE): Boeing 767-3S2F, S/N 43549, built 2016 --- 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.