# N762AT: 1981 Boeing 727-2B7, registration cancelled 2010-11-30

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: November 30, 2010
- Exported to: Nigeria
- Status when cancelled: Valid registration
- Airframe: [Boeing 727-2B7](https://openairdocs.org/model/boeing-727-2b7) (registry code 138407L)
- 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: 22162
- Year built: 1981
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-jet
- Airworthiness: Standard, transport
- Airworthiness date: February 20, 1981
- Certificate issued: July 22, 2010
- Last registry action: July 22, 2010
- Mode S code: AA4908
- Owner when cancelled: [Bank Of Utah Trustee](https://openairdocs.org/faa-owner/BANK%20OF%20UTAH%20TRUSTEE)
- Location: [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City)
- Owner type: Corporation
- Owner's area on the map: 40.7558° N, 111.8843° W: Placed by OpenAirDocs at the center of ZIP code 84111, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N762AT
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=762AT
- Page: https://openairdocs.org/deregistered/N762AT-2010-11-30

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 727-2B7: https://openairdocs.org/model/boeing-727-2b7.md

## Service difficulty reports (65, newest 50)

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

- [SDR EE4Y10351](https://openairdocs.org/sdr/EE4Y10351), Aug 18, 2010: FLOORBEAM. CORRODED. DURING INSP, LOWER FUSELAGE AFT CARGO COMPARTMENT STA 1130 FLOORBEAM UPPER CHORD CORRODED.
- [SDR EE4Y1010347](https://openairdocs.org/sdr/EE4Y1010347), Aug 17, 2010: SKIN. DENTED. RIGHT WING OTBD AILERON, LOWER SURFACE WITH DENT AND BULGED SKIN.
- [SDR EE4Y1010346](https://openairdocs.org/sdr/EE4Y1010346), Aug 17, 2010: STRINGER. CRACKED. (EE4Y) EMPENAGE VERTICAL STABILIZER INTERNAL CAVITY, ST STA 157 STR 7L CRACKED.
- [SDR EE4Y1010345](https://openairdocs.org/sdr/EE4Y1010345), Aug 17, 2010: STRINGER. CRACKED. EMPENNAGE VERTICAL STABILIZER INTERNAL CAVITY, STR 8R AT STA 180 CRACKED.
- [SDR EE4Y1010344](https://openairdocs.org/sdr/EE4Y1010344), Aug 17, 2010: STRINGER. CRACKED. EMPENAGE VERTICAL STABILIZER INTERNAL CAVITY, STR 6L CRACKED AT STA 180.
- [SDR EE4Y1010343](https://openairdocs.org/sdr/EE4Y1010343), Aug 17, 2010: STRINGER. CRACKED. EMPENAGE VERTICAL STABILIZER INTERNAL CAVITY,STR 5L AT STA 22.5 AND STA 157 WITH CRACK.
- [SDR EE4Y1010342](https://openairdocs.org/sdr/EE4Y1010342), Aug 17, 2010: STRINGER. CRACKED. EMPENAGE VERTICAL STABILIZER CAVITY,STR 9L CRACKED AT STA 110.
- [SDR EE4Y1010341](https://openairdocs.org/sdr/EE4Y1010341), Aug 17, 2010: STRINGER. CRACKED. EMPENAGE VERTICAL STABILIZER INTERNAL CAVITY, STR 8L CRACKED AT STA 157, STA 133 AND STA 22.5.
- [SDR EE4Y1010329](https://openairdocs.org/sdr/EE4Y1010329), Aug 10, 2010: KEELBEAM. CORRODED. LOWER FUSELAGE AFT CARGO COMPARTMENT FROM 950D TO STA 1000, KEEL BEAM LT CORRODED.
- [SDR EE4Y1010328](https://openairdocs.org/sdr/EE4Y1010328), Aug 10, 2010: COVER. CORRODED. LOWER FUSELAGE, RAM AIR DOOR INLET AREA, VERTICAL FIXED COVER WITH CORROSION.
- [SDR EE4Y1010327](https://openairdocs.org/sdr/EE4Y1010327), Aug 10, 2010: FLOOR SUPPORT. CORRODED. MAIN CARGO CABIN FLOOR SUPPORT CHANNEL CORRODED AT BS 1145, LBL 12.
- [SDR EE4Y1010326](https://openairdocs.org/sdr/EE4Y1010326), Aug 10, 2010: KEELBEAM. CORRODED. LOWER FUSELAGE AFT CARGO COMPARTMENT FROM BS 950A TO BS 989, KEEL BEAM RT WITH CORROSION.
- [SDR EE4Y1010325](https://openairdocs.org/sdr/EE4Y1010325), Aug 10, 2010: SKIN PANEL. CRACKED. LOWER FUSELAGE SKIN WITH CRACK AT BS 243, WL 178, LT SIDE.
- [SDR DHLA200800132](https://openairdocs.org/sdr/DHLA200800132), Nov 19, 2008: OIL FILTER. BYPASSING. NR 3 OIL FILTER BYPASS LIGHT ILLUMINATED IN FLIGHT PRESS TO TEST CAUSED LIGHT TO BE BRIGHTER SHUT DOWN ENGINE IN ACCORDANCE WITH ABNORMAL PROCEDURES RESOLUTION:
- [SDR DHL2008F00001](https://openairdocs.org/sdr/DHL2008F00001), Jun 27, 2008: TAB. DELAMINATED. A 3 X 1 INCH DELAMINATION ON RT WING O/B AILERON BALANCE TAB AT TRAILING EDGE. AILERON BALANCE TAB WAS REMOVED AND REPLACED IAW BOEING 727 MAINTENANCE MANUAL 27
- [SDR DHLA200800007](https://openairdocs.org/sdr/DHLA200800007), Jan 19, 2008: BATTERY. INOPERATIVE. FLT 152, EMERGENCY EXIT LIGHTS DON'T WORK. REMOVED AND REPLACED BATTERIES IN FWD AND AFT EMERGENCY EXIT LIGHTS, OPS CHECK GOOD IAW B727 MM 33-50-71, P/N 37067-0
- [SDR DHLA200800005](https://openairdocs.org/sdr/DHLA200800005), Jan 18, 2008: LIGHT. DISLODGED. FLT 577, EMERGENCY EXIT LIGHT OVER MAIN ENTRY DOOR FELL OFF DURING TAKEOFF ROLL. REINSTALLED EMERGENCY EXIT LIGHT OVER MAIN ENTRY DOOR. OPS CK. GOOD PER MM 33-5
- [SDR DHLA200700080](https://openairdocs.org/sdr/DHLA200700080), Dec 8, 2007: SWITCH. MALFUNCTIONED. APPROXIMATLY 35 MIN, AFTER TAKEOFF NR 3 ENG OIL PRESSURE/BYPASS LIGHT ILLUMINATED. ABNORMAL PROCEDURE ACCOMPLISHED, DETERMINED THAT BYPASS MODE WAS RESPONSIBLE 
- [SDR DHLA200700050](https://openairdocs.org/sdr/DHLA200700050), Oct 3, 2007: FITTING. FAILED. UPON FLAP RETRACTION FROM FLAPS 2 TO 0, SYSTEM A HYD QTY WENT TO 0. FOUND FITTING BLOWN OUT ON NR 7 SLAT SHUTTLE VALVE. REPLACED NR 7 SLAT ACTUATOR SHUTTLE VALV
- [SDR DHL2007762502](https://openairdocs.org/sdr/DHL2007762502), Mar 23, 2007: SUPPORT ANGLE. CRACKED. FOUND CRACK IN LT AFT AIR STAIRS TORQUE BOX ON UPPER WEB SUPPORT ANGLE, APPROX BS 1253. MADE TWO EACH CUT OUTS FOR ACCESS, 4 BY 4 AT UPPER WEB IAW B727 SRM 51-1
- [SDR DHL2007762501](https://openairdocs.org/sdr/DHL2007762501), Mar 23, 2007: TORQUE BOX. GOUGED. LEFT AFT AIR STAIRS TORQUE BOX LIGHTING HOLE GOUGED BS 1320. ROUTED OUT GOUGED AREA, MATERIAL LOSS .008 IAW B727 SRM 53-30-1 FIG 1. FAB REPAIR DOUBLER 4" BY 2.5
- [SDR DHL2006762511](https://openairdocs.org/sdr/DHL2006762511), Jul 12, 2006: SEAT TRACK. CORRODED. FOUND CABIN SEAT TRACK HAS CORROSION AT BS 650 LBL 45. REMOVED CORROSION AT MAIN CABIN SEAT TRACK BS 650 LBL 45, CORROSION IS OUT OF LIMITS IAW B727 SRM 51-10-1
- [SDR DHL2006762512](https://openairdocs.org/sdr/DHL2006762512), Jul 8, 2006: SEAT TRACK. CORRODED. FOUND CABIN SEAT TRACK RBL 24 HAS CORROSION AT BS 480-620. REMOVED FLOORBOARDS FROM BL 0 - RBL 24 STA 480-690 IAW B727 SRM 51-30-2. REMOVED SEAT TRACK AT RBL 24
- [SDR DHL2006762510](https://openairdocs.org/sdr/DHL2006762510), Jul 8, 2006: SEAT TRACK. CORRODED. CABIN SEAT TRACK LBL 24 HAS CORROSION AT BS 480-620. REMOVED FLOORBOARDS FROM BL 0 TO LBL 45 FOR ACCESS IAW SRM 51-30-2, BS 480-690 SEAT TRACK CORROSION FOUND O
- [SDR DHL2006762508](https://openairdocs.org/sdr/DHL2006762508), Jul 6, 2006: MOUNT. CRACKED. NR 5 LE FLAP INBD ACTUATOR MOUNT BRACKET IS CRACKED BY THE LWR CORNER. REMOVED NR 5 LE FLAP ACTUATOR MOUNT WEB IAW B727 SRM 51-30-2. FAB NEW I/B MOUNT WEB IAW D
- [SDR DHL2006762515](https://openairdocs.org/sdr/DHL2006762515), Jun 30, 2006: SEAT TRACK. CORRODED. CABIN SEAT TRACK HAS CORROSION AT BS 480-620 RBL 45" BALL MAT AREA. REMOVED CABIN FLOORBOARDS RBL 24-RBL 65 FOR ACCESS IAW B727 SRM 51-30-2. REMOVED SEAT TRACK 
- [SDR DHL2006762501](https://openairdocs.org/sdr/DHL2006762501), Jun 30, 2006: FRAME. CRACKED. NR 6 SLAT AT ACT ROD END ATTACHMENT WS 515 HAS BOTH I/B & O/B FRAMES CRACKED FWD. REMOVED I/B & O/B NR 6 SLAT FRAMES AT WS 515 IAW B727 SRM 51-30-2, FAB NEW I/B
- [SDR DHL2006762514](https://openairdocs.org/sdr/DHL2006762514), Jun 29, 2006: WEDGE. DENTED. RT O/B AILERON WEDGE UPPER SURFACE IS DENTED 2 PLACES. REMOVED RT O/B AILERON WEDGE AS PER B727 SRM 51-30-2. INSTALLED REPAIRED WEDGE VENDOR ORDER NR 500080771 
- [SDR DHL2006762513](https://openairdocs.org/sdr/DHL2006762513), Jun 29, 2006: FIREWALL. DAMAGED. NR 2 VERT FIREWALL HAS HOLE WORN THROUGH DOUBLER 6:30 POSITION AT T/E STA 1352. REMOVED EXISTING REPAIR AT NR 2 VERT FIREWALL 6:30 POSITION IAW B727 SRM 51-30-2
- [SDR DHL2006762509](https://openairdocs.org/sdr/DHL2006762509), Jun 29, 2006: SKIN. DELAMINATED. LT WING, INBD FLAP TE IS DELAMINATED ON OUTBD TE WBL 243. REMOVED PREVIOUS REPAIR AND VACUUM BAGGED FOR MOISTURE REMOVAL. FABRICATED REPAIR SKIN APPROX 6 1/2" B
- [SDR DHL2006762506](https://openairdocs.org/sdr/DHL2006762506), Jun 29, 2006: SKIN. WORN. LT WING INBD FLAP, FORE FLAP L/E HAS WEAR SPOT ON SKIN WBL 114. REMOVED DAMAGED DOUBLER L/WING I/B FORE FLAP L/E WBL 114 AS PER B727 SRM 51-30-2. FABRICATED NEW
- [SDR DHL2006762507](https://openairdocs.org/sdr/DHL2006762507), Jun 29, 2006: SKIN. CRACKED. REF NR 072657 DISCREPANCY, RT WING T/E UPPER SURFACE AT NR 13 SPOILER CTR HINGE HAS SKIN CRACKED. REMOVED FASTENERS ON RT T/E UPPER NR 13 SPOILER IAW SRM 51-30-
- [SDR DHL2006762504](https://openairdocs.org/sdr/DHL2006762504), Jun 29, 2006: SKIN. DELAMINATED. RIGHT O/B MID FLAP WBL 348-358 HAS UPPER T/E DELAMINATED. CUT OUT DELAMINATED AREA R/W O/B MID FLAP UPPER SKIN APPROX 3.25 X 22 INCHES IAW SRM 51-40-20 PARA 6 &
- [SDR DHL2006762525](https://openairdocs.org/sdr/DHL2006762525), Jun 28, 2006: WEB. CRACKED. AT RT SIDE OF AFT AIRSTAIR WELL CRACK EMANATING FROM LOWER LIGHTENING HOLE ON TORQUE BOX AT BS 1237. CUT OUT DAMAGED SECTION 11/8X1 AT RT SIDE OF AFT AIRSTAIR W
- [SDR DHL2006762522](https://openairdocs.org/sdr/DHL2006762522), Jun 28, 2006: TORQUE BOX. CRACKED. AT LT SIDE OF AFTSTAIR WELL, CRACK EMANATING FROM UPPER LIGHTENING HOLE IN TORQUE BOX AT BS 1263. REMOVED EXISTING DOUBLER AT LT SIDEWALL AFT AIRSTAIR WEB BS 12
- [SDR DHL2006762521](https://openairdocs.org/sdr/DHL2006762521), Jun 28, 2006: STRUCTURE. CRACKED. AT LT SIDE OF AFT AIRSTAIR WELL 2 CRACKS EMANATING FROM LOWER LIGHTENING HOLE ON TORQUE BOX AT BS 1237. REMOVED EXISTING DOUBLER AT LT SIDE AFT AIRSTAR WEB BS 1
- [SDR DHL2006762517](https://openairdocs.org/sdr/DHL2006762517), Jun 28, 2006: WEB. CRACKED. AFT AIRSTAIR DOOR SIDEWALL CRACKED AT LT ROLLER ON LOWER END OF STAIRS. REMOVED EXISTING REPAIR DOUBLER AT AFT AIRSTAIR SIDEWALL WEB LT ROLLER IAW B727 SRM 51-3
- [SDR DHL2006762516](https://openairdocs.org/sdr/DHL2006762516), Jun 28, 2006: TORQUE BOX. CRACKED. AT LT SIDE OF AIRSTAIR WELL CRACK EMANATING FROM UPPER LIGHTENING HOLE TORQUE BOX AT BS 1303. REMOVED PREVIOUS REPAIR DOUBLER AT LT SIDE AFT AIRSTAIR SIDEWALL W
- [SDR DHL2006762500](https://openairdocs.org/sdr/DHL2006762500), Jun 28, 2006: WEB. CRACKED. AT RIGHT SIDE OF AFT AIRSTAIR WELL, CRACK EMANATING FROM LOWER LIGHTENING HOLE ON TORQUE BOX AT BS 1225. REMOVED INTERIOR ACCESS PANEL AT RT SIDE OF AFT AIRSTAI
- [SDR DHL2006762520](https://openairdocs.org/sdr/DHL2006762520), Jun 27, 2006: ANGLE. CRACKED. RIGHT INBD MID FLAP REAR LWR CHORD ANGLE CRACKED WBL 105. REMOVED SEAL RETAINER AND LWR CHORD ANGLE SECTION AND LOWER SKIN IAW B727 SRM 51-30-2. FAB NEW LOWER C
- [SDR DHL2006762518](https://openairdocs.org/sdr/DHL2006762518), Jun 27, 2006: ANGLE. CRACKED. LEFT INBD MID FLAP REAR LWR CHORD ANGLE SHOW CRACKS 2 WBL 105. REMOVED MID FLAP LOWER SKIN FOR ACCESS IAW B727 SRM 51-30-2. REMOVED LEFT INBD MID FLAP LWR CHORD
- [SDR DHL2006762503](https://openairdocs.org/sdr/DHL2006762503), Jun 27, 2006: HINGE. CRACKED. L1 DOOR CUTOUT, UPPER HINGE HAS EVIDENCE CRACK. NDT CONFIRMED CRACK IS ABOUT 1 INCH LONG, MARKED END OF CRACK 727 NDT PART 6, 51-00-00 FIG 23. OPENED AREA INTER
- [SDR DHL2006762502](https://openairdocs.org/sdr/DHL2006762502), Jun 26, 2006: SKIN. DENTED. EXT FUS BS 1055 BELOW STR 20R HAS DENT. DENT AT BS 1055 BELOW STR 20R IS OUT OF LIMITS IAW B727 SRM 53-30-1 FIG 1. CUTOUT DAMAGE AREA DIM 2" BY 2 3/4" AND 2" BY
- [SDR DHL2006762523](https://openairdocs.org/sdr/DHL2006762523), Jun 26, 2006: SKIN PANEL. DELAMINATED. L/WING TE UPPER PANEL DELAMINATED AT LWBL 88 BS 889 IN/SQ WITH NO CRACKS EVIDENT IN OUTER SKIN. CUT OUT DELAMINATED AREA ON UPPER SKIN OF L/WING TE PANEL APPROX
- [SDR DHL2006762505](https://openairdocs.org/sdr/DHL2006762505), Jun 26, 2006: MOUNT. CRACKED. NR 5 KRUGER FLAP ACTUATOR MOUNT W.S. 230 OB LOWER CORNER IS CRACKED. REMOVED NR 5 LE FLAP ACTUATOR MOUNT WEB IAW SRM 51-30-2 . FAB NEW OB ACTUATOR MOUNT WEB IAW
- [SDR DHL2006762001](https://openairdocs.org/sdr/DHL2006762001), Jan 26, 2006: BRAKE. MALFUNCTIONED. LEFT BRAKE IS SOFT AND REQUIRES TWICE AS MUCH PRESSURE TO STOP AIRCRAFT AS RIGHT BRAKE. INSPECTED ALL BRAKES , NO DEFECTS NOTED. TAXIED AIRCRAFT, TESTED BRAKES,
- [SDR DHL2005762004](https://openairdocs.org/sdr/DHL2005762004), Oct 28, 2005: BATTERY. INOPERATIVE. EMERGENCY EXIT LIGHT IN GALLEY WON`T TEST. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERIES IAW M/M 33-50-101, OPS CK NORMAL P/N MISC062.
- [SDR DHL2005762003](https://openairdocs.org/sdr/DHL2005762003), May 3, 2005: OIL COOLER. LEAKING. AT 10,000FT, THE CREW OBSERVED THE NR 3 ENGINE PARAMETERS FLUCTUATING,FOLLOWED SPECIAL PROCEDURES SHUT DOWN THE ENGINE,DECLARED AN EMERGENCY AND DIVERTED BACK T
- [SDR DHL2005762002](https://openairdocs.org/sdr/DHL2005762002), Apr 23, 2005: LIGHT. LOOSE. EMERGENCY EXIT LIGHTS AT FRONT ENTRY DOOR NEEDS TO BE REMOUNTED. INSTALLED EMERGENCY LIGHT AT FWD ENTRY DOOR AND OPS CHECKS SERVICEABLE IAW MM 33-50-01.
- [SDR DHL2005762001](https://openairdocs.org/sdr/DHL2005762001), Jan 20, 2005: BRAKE ASSY. MALFUNCTIONED. LEFT BRAKE STICKS AND CHATTERS WHEN TAXIING. BLEED NR 2 BRAKE IAW MM 32-41-00. TAXIED A/C, OPS CKS GOOD. OK TO CONTINUE.

All 65: https://openairdocs.org/deregistered/N762AT-2010-11-30/reports.md

## Other aircraft with N762AT

- [Registered now](https://openairdocs.org/aircraft/N762AT): Steven P Short KITFOX SUPER SPORT 7, S/N KA19350434, built 2026

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