# N195FE: 1967 Boeing 727-22, registration cancelled 2002-10-15

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: October 15, 2002
- Status when cancelled: Valid registration
- Airframe: [Boeing 727-22](https://openairdocs.org/model/boeing-727-22) (registry code 1384002)
- 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: 19144
- Year built: 1967
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-jet
- Airworthiness: Standard, transport
- Airworthiness date: August 29, 1967
- Certificate issued: April 9, 1990
- Last registry action: December 15, 1999
- Mode S code: A17B40
- Owner when cancelled: [Federal Express Corp](https://openairdocs.org/faa-owner/FEDERAL%20EXPRESS%20CORP)
- 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/N195FE
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=195FE
- Page: https://openairdocs.org/deregistered/N195FE-2002-10-15

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 727-22: https://openairdocs.org/model/boeing-727-22.md

## Service difficulty reports (49)

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

- [SDR 00FDEA00138](https://openairdocs.org/sdr/00FDEA00138), Mar 7, 2000: CLAMP. LOOSE. NR 1 ENGINE STRUT OVERHEAT LIGHT CAME ON. RETIGHTEN CLAMP IN THE PNEU DUCT PER MM 36-00-002-4 CK. LEAK CHECK GOOD, OK TO CONTINUE.
- [SDR 98FDEA00498](https://openairdocs.org/sdr/98FDEA00498), Aug 11, 1998: CLAMP. LOOSE. 98-0199 - DURING CLIMB-OUT PASSING 10K FT, ENG 3 STRUT LGT ILLUM. RT PACK WAS TURNED OFF AND ENG 3 BLEED CLOSED. WHILE REFERENCING RED TABS, LGT EXT LGT TESTED 
- [SDR 96FDEA01330](https://openairdocs.org/sdr/96FDEA01330), Aug 6, 1996: OVERHEAT LIGHT. ILLUMINATED. AFTER T/O ON CLIMBOUT, ENG NR 1 STRUT OVERHEAT LITE ON. RAN CHKLST. ENG AT IDLE FOR 3 MIN LITE REMAINED ON. SHUTDOWN ENG PER CHKLST. AFTER 5 MIN LITE STILL ON. 
- [SDR 96FDEA01309](https://openairdocs.org/sdr/96FDEA01309), Aug 2, 1996: LIGHT. INOPERATIVE. NRO774 AND 046, EMERGENCY EXIT LIGHT OVER FWD ENTRY DOOR DOES NOT ILLUMINATE WITH LOSS OF ESSENTIAL AC POWER. *S/D* REPLACED FWD ENTRY LIGHT ASSEMBLY, FUNCTIONA
- [SDR 96FDEA01304](https://openairdocs.org/sdr/96FDEA01304), Aug 1, 1996: LIGHT. INOPERATIVE. LP 558749 045C. EMERGENCY EXIT LIGHT OVER FORWARD ENTRY DOOR DOES NOT ILLUMINATE WITH LOSS OF ESSENTIAL AC POWER. REPLACED FORWARD ENTRY LIGHT ASSEMBLY. FUNCTIO
- [SDR 96FDEA01301](https://openairdocs.org/sdr/96FDEA01301), Jul 30, 1996: SKIN. CRACKED. NR0171 009. BS 520, STR 25, RBL 30, THERE IS A CRACK IN SKIN. ****S/D**** MECHANICALLY REMOVED CRACK IN SKIN LOCATED AT BS 520, STR 25R, RBL 30. REPAIRED SKIN P
- [SDR 96FDEA01300](https://openairdocs.org/sdr/96FDEA01300), Jul 30, 1996: SKIN. LIGHTNING STRIKE. NR 0100 044. BS 360 - 440, WL 160, STR 24-26R, THERE ARE SEVERAL LIGHTNING STRIKES (MARKED). ****S/D**** REPAIRED LIGHTNING STRIKES PER FEDEX SRM 53-30-3, FIG 2
- [SDR 96FDEA01293](https://openairdocs.org/sdr/96FDEA01293), Jul 29, 1996: CHORD. CORROSION. NR 0231 042. CORROSION C53-132-02(1) ON STA 870, UPPER CHORD LBL 58-60, 46, 36-38, 26-28, 17-19, RBL 55, 45, 10, 0 WL 172. REMOVED AND REPLACED 870 UPPER CHORD 
- [SDR 96FDEA01290](https://openairdocs.org/sdr/96FDEA01290), Jul 26, 1996: FRAME. CRACKED. NR 0370 039. BS 913, WL 194, STR 18A FRAME IS CRACKED IN MAIN WHEELWELL. REPAIRED CRACKED FRAME BS 13, WL 194, STR 18A IAW FEDEX EA 7-5310-29295A.
- [SDR 96FDEA01286](https://openairdocs.org/sdr/96FDEA01286), Jul 24, 1996: LONGERON. CRACKED. NR 0729 038. WHILE WORKING NR 0312, DISCOVERED CRACK IN FORWARD MOST FASTENER HOLE OF LONGERON AT BS 1110, STR 27R. ***S/D**** COMING.
- [SDR 96FDEA01294](https://openairdocs.org/sdr/96FDEA01294), Jul 22, 1996: FRAME. CRACKED. NR 0757 041. CRACK ON INBOARD FLANGE OF FRAME AT BS 480 STR 26R RBL 24. REMOVED DAMAGE IN FRAME AT BS 480, STR 26R RBL 24. FABRICATED REPAIR PART, ALODINED, PRI
- [SDR 96FDEA01276](https://openairdocs.org/sdr/96FDEA01276), Jul 21, 1996: FRAME. CRACKED. DISCREPANCY: (NR 0316)(036) CRACK IN FRAME AT BS 1070, LBL 37, WL 153 ABOVE STR 25L. CORRECTIVE ACTION: *****S/D **** COMING.
- [SDR 96FDEA01275](https://openairdocs.org/sdr/96FDEA01275), Jul 21, 1996: FRAME. CRACKED. NR 0321, 037 CORROSION (C53-113-01) AND CRACK AT PREVIOUS REPAIR FRAME AT BS 1057.5 RBL. *S/D* REMOVED AND REPLACED 1057.6 MAIN FRAME RT SIDE, PER FEDEX SRM 53-
- [SDR 96FDEA01260](https://openairdocs.org/sdr/96FDEA01260), Jul 16, 1996: FLOOR BEAM. CORROSION. DISCREPANCY: NR 0259(033) CORROSION (C53-111-01) AROUND NUTPLATES AROUND EXISTING FLOOR BEAM REPAIR STA 600 RBL 1, 5, 8, 12, 15, 19, 24, WL 198 (FWD BAY). CORRE
- [SDR 96FDEA01259](https://openairdocs.org/sdr/96FDEA01259), Jul 16, 1996: GUSSET. CRACKED. DISCREPANCY: NR 0340 (032) FRAME GUSSET IS CRACKED AT BS 825, LBL 67, WL 197. CORRECTIVE ACTION: REMOVED AND REPLACED GUSSET AT BS 25, LBL 67, WL 197.
- [SDR 96FDEA01256](https://openairdocs.org/sdr/96FDEA01256), Jul 15, 1996: SHEAR TIE. CORRODED. DISCREPANCY: NR 0225 (031) CORROSION ON SHEAR TIE STA 540 LT BETWEEN STR 24-25 LT FWD BAY. CORRECTIVE ACTION: *****S/D*****.
- [SDR 96FDEA01255](https://openairdocs.org/sdr/96FDEA01255), Jul 15, 1996: SHEAR TIE. CORRODED. DISCREPANCY: NR 0225 (030) CORROSION ON SHEAR TIE STA 540 LT BETWEEN STR 24-25, LT FORWARD BAY. CORRECTIVE ACTION: REPAIRED SHEAR TIE, STA 540 LT BETWEEN STR 24
- [SDR 96FDEA01254](https://openairdocs.org/sdr/96FDEA01254), Jul 15, 1996: FLOORBEAM. GOUGE. DISCREPANCY: NR 0245 (029) FOUND GOUGES IN FLOORBEAM, STR 680 RBL 25, LBL 25 WL 198 (FORWARD BAY). CORRECTIVE ACTION: BLENDED GOUGES, ONE WAS OUT OF LIMITS IN F
- [SDR 96FDEA01253](https://openairdocs.org/sdr/96FDEA01253), Jul 15, 1996: STRINGER. CORRODED. DISCREPANCY: NR 0222 (028) CORROSION (C53-111-01 (2) ON STR FLANGE, STR 23 RT, STA 489 RT, FORWARD BAY. CORRECTIVE ACTION: REPAIRED STR AT BS 489, STR 23R PER F
- [SDR 96FDEA01261](https://openairdocs.org/sdr/96FDEA01261), Jul 11, 1996: STRINGER. CRACKED. DISCREPANCY: NR 0725 (034) WHILE WORKING NR 0722, FOUND CRACK UNDERNEATH FASTENER AT BS 540, STRINGER 24 LT. REPAIRED CRACK UNDERNEATH FASTENER AT BS 540, STR 2
- [SDR 96FDEA01248](https://openairdocs.org/sdr/96FDEA01248), Jul 11, 1996: FRAME. CORROSION. DISCREPANCY: NR 0235 (027) CORROSION ON C-CHANNEL, STATION 532, RBL 26, WL 155. CORRECTIVE ACTION: REPAIRED DENT IN FRAME BS 540 BETWEEN STR 23 AND STR 24L, SRM
- [SDR 96FDEA01295](https://openairdocs.org/sdr/96FDEA01295), Jul 10, 1996: GATE BEAM. CRACKED. NR 0143 040. FORWARD ENTRY DOOR LOWER GATE BEAM IS CRACKED 2 EACH PLACES ADJACENT TO LOWER FORWARD STOP PIN FITTING. REMOVED AND REPLACED LOWER GATE BEAM PER FE
- [SDR 96FDEA01229](https://openairdocs.org/sdr/96FDEA01229), Jul 9, 1996: FRAME. CORRODED. DISCREPANCY: NR 0581(021) CORROSION (C53-221-01) ON FRAME BS 251.6, WL 223, LBL 48. CORRECTIVE ACTION *****S/D***** REPAIRED FRAME STA 251.6, WL 223, LBL 48 IAW
- [SDR 96FDEA01228](https://openairdocs.org/sdr/96FDEA01228), Jul 9, 1996: SKIN. OIL CANNED. NR 0177, 020, OIL CANNED SKIN AT 1243 TO 1253 STR 22 TO 23 LT. *S/D* REPAIRED PER SRM 53-30-3 FIG 1.
- [SDR 96FDEA01246](https://openairdocs.org/sdr/96FDEA01246), Jul 8, 1996: FRAME. DENTED. DISCREPANCY: NR 0235 (025) FOUND DENT IN FRAME STA 540 BETWEEN STRINGERS 23 TO 24 LT FORWARD BAY. CORRECTIVE ACTION: REPAIRED DENT IN FRAME STA 540 BETWEN STR 2
- [SDR 96FDEA01217](https://openairdocs.org/sdr/96FDEA01217), Jul 8, 1996: BONDING JUMPER. CORRODED. DISCREPANCY: NR 0551 (015) CORROSION (C57-562-01) NR 2 K-FLAP TO BULLNOSE INBOARD BONDING JUMPER UPPER ATTACH POINT. CORRECTIVE ACTION: CORRODED AREA FOUND TO B
- [SDR 96FDEA01216](https://openairdocs.org/sdr/96FDEA01216), Jul 8, 1996: FRAME. CORRODED. DISCREPANCY: NR 0579 (014) CORROSION (C53-221-01) ON FRAME BS 227.8 WL 226 AND 233 RBL 41-43 5. CORRECTIVE ACTION: **S/D** REPAIRED FRAME BS 227.8 W/L 226 AND 2
- [SDR 96FDEA01211](https://openairdocs.org/sdr/96FDEA01211), Jul 8, 1996: FRAME. CORRODED. DISCREPANCY: NR 0255 (011) CORROSION (C53-111-01) ON WEB/FRAME, BS 572, RBL 24-26 WL 157 FORWARD BAY. CORRECTIVE ACTION: REPAIRED WEB/FRAME BS 572, RBL 24-26, W
- [SDR 96FDEA01210](https://openairdocs.org/sdr/96FDEA01210), Jul 8, 1996: FLOOR BEAM. CORRODED. NR 0719, 010, CORROSION (C53-111-01) ON FLOOR BEAM STA 660 RBL 24 WL 198. *S/D* REPAIRED FLOOR BEAM PER SRM 53-10-8.
- [SDR 96FDEA01243](https://openairdocs.org/sdr/96FDEA01243), Jul 7, 1996: TRIPLER. CORRODED. NR 0717 024, BS 1110 TO 1130, STR 26R, WL 152. SKIN IS BULGED. *S/D* OPENED SKIN LAP REMOVED THE CORROSION BY BLENDING .002 FROM AN AREA OF 6 BY 12 ON THE SKIN.
- [SDR 96FDEA01242](https://openairdocs.org/sdr/96FDEA01242), Jul 7, 1996: CHORD. CORRODED. DISCREPANCY: NR 0622 023 CORROSION ON UPPER CHORD BS 344, RBL 7 TO LBL 55, WL 208. ***S/D *** REMOVED AND REPLACED UPPER CHORD OF FLOOR AT STATION 344, RBL 65 T
- [SDR 96FDEA01241](https://openairdocs.org/sdr/96FDEA01241), Jul 7, 1996: BULKHEAD WEB. CRACKED. DISCREPANCY: NR 0711. FOUND CRACK ON WHEELWELL BULKHEAD STA 870, WL 190, LBL 50 (CENTER TANK). CORRECTIVE ACTION: REPAIRED PER SRM 53-10-9, FIG 4.
- [SDR 96FDEA01226](https://openairdocs.org/sdr/96FDEA01226), Jul 7, 1996: BONDING JUMPER. CORRODED. NR 0552, 018, CORROSION (C57-562-01) NR 3 K-FLAP TO BULLNOSE O/B BONDING JUMPER, UPPER LOWER ATTACH POINTS. *S/D* REPLACED NR 3 K-FLAP BULLNOSE, REPAIRED K-FLAP
- [SDR 96FDEA01219](https://openairdocs.org/sdr/96FDEA01219), Jul 7, 1996: BONDING JUMPER. CORRODED. NR 0547, 007, CORROSION (C57-562-01) AT BOTH ATTACH POINTS ON THE O/B BONDING JUMPER ON THE NR 5 K-FLAP BULLNOSE. *S/D* REPAIRED UPPER ATTACH POINT PER FEDEX SR
- [SDR 96FDEA01273](https://openairdocs.org/sdr/96FDEA01273), Jul 6, 1996: FLOORBEAM. CORRODED. DISCREPANCY: (NR 0743 (035) WHILE WORKING 0251, FOUND CORROSION ON FLOORBEAM LOWER CHORD BS 540 LBL 14 TO RBL 23 WL 200. CORRECTIVE ACTION: REPAIRED FLOORBEAM L
- [SDR 96FDEA01227](https://openairdocs.org/sdr/96FDEA01227), Jul 4, 1996: UPPER LUG. CORRODED. NR 0549, 019, CORROSION (C57-562-01) ON THE O/B UPPER LUG O/B HINGE NR 4 K-FLAP. *S/D* REMOVED AND REPLACED K-FLAP PER MM 27-81-1.
- [SDR 96FDEA01215](https://openairdocs.org/sdr/96FDEA01215), Jul 4, 1996: STRINGER. CORRODED. DISCREPANCY: NR 00250 (013) CORROSION (C53-111-01) ON STR 27L CHANNEL STR 536-546 LT FORWARD BAY. CORRECTIVE ACTION: **S/D** REMOVED CORRODED SECTION OF STR FRO
- [SDR 96FDEA01218](https://openairdocs.org/sdr/96FDEA01218), Jul 2, 1996: TE SKIN. DISBONDED. NR 0464, 016, RIGHT WING O/B AILERON IS DELAMINATED AT O/B TRAILING EDGE. *S/D* REPAIRED O/B AILERON AT O/B TRAILING EDGE IAW FEDEX SRM 51-40-06.
- [SDR 96FDEA01204](https://openairdocs.org/sdr/96FDEA01204), Jul 2, 1996: SKIN. CORRODED. DISCREPANCY: NR 0205 (005). CORROSION (53-100-01). BS 1080 STR 26R, RBL 30 ON EXTERIOR SKIN AT LAP RBL 13, WL 208. REPAIRED DAMAGED AREA BS 1060 - 1080, STR 26R
- [SDR 96FDEA01203](https://openairdocs.org/sdr/96FDEA01203), Jul 2, 1996: INTERCOSTAL. CORRODED. NR 0572, 006, CORROSION (53-221-01) ON INTERCOSTAL BS 268 TO 277 RBL 13 WL 208. *S/D* REMOVED AND REPLACED INTERCOSTAL BS 268 TO 277 RBL 13 WL 208, DUE TO CORRO
- [SDR 96FDEA01202](https://openairdocs.org/sdr/96FDEA01202), Jul 2, 1996: SKIN PANEL. GOUGED. NR 0110, 004, BS 380 PLUS 15 WL 160, STR 23 TO 24R THERE IS A SHARP PROTRUDING DENTS IN SKIN. *S/D* REPAIRED DENT AT BS 380 PLUS 15 BETWEEN STR 23 AND 24 RIGHT 
- [SDR 96FDEA01201](https://openairdocs.org/sdr/96FDEA01201), Jul 2, 1996: CLIP. CORROSION. DISCREPANCY: NR 0274 (003) GOUGE IN STRING CLIP BS 910 STR 11 RT. ***S/D*** REMOVED STR CLIP AT BS 910, STR 11 RT, AND FOUND GOUGE TO BE OUT OF LIMITS PER SRM 5
- [SDR 96FDEA01200](https://openairdocs.org/sdr/96FDEA01200), Jul 2, 1996: FLOOR BEAM. CORRODED. DISCREPANCY: NR 0301 (002) CORROSION (53-113-01-27 ) ON LOWER FLANGE OF FLOORBEAM, BS 1110, BBL 50 TO LBL 30 AT THE NUTPLATE HOLES. ***S/D*** REMOVED CORROSION 
- [SDR 96FDEA01199](https://openairdocs.org/sdr/96FDEA01199), Jul 2, 1996: FRAME. CORRODED. NR 0256, 001, CORROSION (C53-111-01) ON FRAME STR 580 BETWEEN STR 22 TO 25 LT FWD BAY 8. *S/D* CORROSION ON FRAME BS 580, BETWEEN STR 22 TO 25 LT IS OUT OF LIMI
- [SDR 96FDEA01194](https://openairdocs.org/sdr/96FDEA01194), Jul 2, 1996: INTERCOSTAL. CORRODED. DISCREPANCY: NR 0563 (007) CORROSION (C53-221-01) ON INTERCOSTAL BS 277-295, LBL 13 WL 208 ***S/D*** REMOVED AND REPLACED UPPER CHORD OF INTERCOSTAL, FLOOR SUPP
- [SDR 96FDEA01214](https://openairdocs.org/sdr/96FDEA01214), Jul 1, 1996: WEB. CORRODED. DISCREPANCY: NR 0574 (012) CORROSION (C53-221-01) ON UNDERSIDE OF HORIZONTAL WEB AND L-ANGLES BS 224-259, LBL 42-54, WL 224-236 CORRECTIVE ACTION: REPAIRED HORI
- [SDR 96FDEA00720](https://openairdocs.org/sdr/96FDEA00720), Mar 30, 1996: HYDRAULIC MODULE. LEAKING. MAIN GEAR AND USED ALT FLAP EXT IN FLT AND BOTH A-SYS LOW PRESS LIGHT CAME ON, FOLLOWED BY OVERHEAT TO SYS. OVERHEAT LIGHT WENT OUT, BUT HAD A-SYS PRESS WITH GO
- [SDR 95FDEA01292](https://openairdocs.org/sdr/95FDEA01292), Sep 12, 1995: CHORD. CORROSION. NR 0232 043. CORROSION C53-132-2(1) ON STA 870 LOWER CHORD LBL 70, 38-41, RBL 20, WL 156. REMOVED AND REPLACED BS 870 LOWER CHORD, LBL 70, WL 156 PER FEDEX EA 7
- [SDR 95FDEA00314](https://openairdocs.org/sdr/95FDEA00314), Mar 18, 1995: SLIDING WINDOW. CAME OPEN. ON ROTATION L/H SLIDING WINDOW CAME OPEN. TESTED CAPTS L2 WINDOW (SLIDING WINDOW) PER 727 MM 56-12-11 PG 505 PARA A, NO DEFECT NOTED. INSPECTED ENGINE INLETS AN

## Other aircraft with N195FE

- [Registered now](https://openairdocs.org/aircraft/N195FE): Boeing 767-300F, S/N 63125, built 2021

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