# N765AT: 1983 Boeing 727-264, registration cancelled 2010-08-06

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: August 6, 2010
- Exported to: Brazil
- Status when cancelled: Valid registration
- Airframe: [Boeing 727-264](https://openairdocs.org/model/boeing-727-264) (registry code 138408M)
- Engine: [Pratt & Whitney JT8D-17 series](https://openairdocs.org/engine/pratt-whitney-jt8d-17-series) (registry code 52049)
- Data sheets: [TCDS A3WE](https://openairdocs.org/tcds/A3WE), [TCDS E2EA](https://openairdocs.org/tcds/E2EA) (OpenAirDocs)
- Serial number: 23014
- Year built: 1983
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-jet
- Airworthiness: Standard, transport
- Airworthiness date: February 15, 1983
- Certificate issued: June 23, 2010
- Last registry action: June 23, 2010
- Mode S code: AA542D
- Owner when cancelled: [Rio Airlines USA Inc](https://openairdocs.org/faa-owner/RIO%20AIRLINES%20USA%20INC)
- Location: [Miami, FL](https://openairdocs.org/faa-place/FL/Miami)
- Owner type: Corporation
- Owner's area on the map: 25.7549° N, 80.1985° W: Placed by OpenAirDocs at the center of ZIP code 33129, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N765AT
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=765AT
- Page: https://openairdocs.org/deregistered/N765AT-2010-08-06

From the FAA registry file of October 28, 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 727-264: https://openairdocs.org/model/boeing-727-264.md

## Service difficulty reports (93, newest 50)

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

- [SDR DHLA200900034](https://openairdocs.org/sdr/DHLA200900034), Jun 7, 2009: BATTERY PACK. MALFUNCTIONED. DEFECT DESCRIPTION; ENTRY WAY EMERGENCY EXIT LIGHT FLICKERS AND IS DIM WHEN STDY BATTERY CHECK IS DONE. REMOVED AND REPLACED ENTRY EMERGENCY EXIT LIGHT BATTERIE
- [SDR DHLA20087651016](https://openairdocs.org/sdr/DHLA20087651016), Oct 16, 2008: CASTING. CRACKED. UPON VISUAL INSPECTION FOUND THE NR 6 K-FLAP CENTER HINGE CASTING OUTBOARD SIDE AT THE ATTACH POINT FOR THE ACTUATOR ROD END CRACKED APPROX 2 INCHES IN LENGTH. 
- [SDR DHL2008F00000](https://openairdocs.org/sdr/DHL2008F00000), Jul 2, 2008: PIN. DAMAGED. SMALL DAMAGE ON NR (6) L/E SLAT AT IB GUIDE PIN EXISTING DOUBLER. DAMAGE WAS BLENDED SMOOTH LESS THAN 1 INCH X .100 MATERIAL LOSS, WORK ACCOMPLISHED IAW SRM 57-
- [SDR DHLA200800041](https://openairdocs.org/sdr/DHLA200800041), Apr 22, 2008: FIRE WARNING. MALFUNCTIONED. FLT NR 1489 FIRE WARNING BELL ONLY AT CRUISE FL 330 COMPLETED ABNORMAL PROCEDURES ALL SYSTEMS TESTED NORMAL. PERFORMED SYSTEM CK OF FIRE DETECTION SYSTEM OPS NO
- [SDR DHLA200800039](https://openairdocs.org/sdr/DHLA200800039), Apr 9, 2008: TRIM SWITCH. BROKEN. FLT 589, WHEN THRUST LEVERS ADVANCED FOR TAKEOFF, TAKEOFF WARNING HORN ACTIVATED. FLAPS 15 SPEED BRAKES STOWED TRIM SET AT 6.6. FOUND UPPER STAB. TRIM SWITCH (S
- [SDR DHL2008765033](https://openairdocs.org/sdr/DHL2008765033), Feb 1, 2008: RIB. CRACKED. DURING C CHECK, NR 2 SLAT INBOARD ACTUATOR SUPPORT RIB CRACKED. REMOVED INNER SKIN PANEL FOR ACCESS IAW SRM 51-30-2. REMOVED DAMAGE INBOARD RIB IAW SRM 51-30-2.
- [SDR DHL2008765020](https://openairdocs.org/sdr/DHL2008765020), Feb 1, 2008: SKIN. DENTED. DURING C CHECK, 2 EACH PROTRUDING DENTS ON RIGHT HORIZONTAL STABILIZER UPPER SURFACE 3" INBOARD OF PCU PANEL. REWORKED TO ORIGINAL CONTOUR IAW SRM 51-40-1, 2 EA
- [SDR DHL2008765015](https://openairdocs.org/sdr/DHL2008765015), Feb 1, 2008: STRUCTURE. CRACKED. DURING C CHECK, LEFT INBOARD MID FLAP LOWER TRAILING EDGE WBL 102 AT PUSH-ROD IS CRACKED, INBOARD. REMOVED INBOARD MID FLAP LOWER SKIN AND NR 3 TEAR DROP FOR AC
- [SDR DHL2008765010](https://openairdocs.org/sdr/DHL2008765010), Jan 29, 2008: FRAME. GOUGED. DURING C CHECK, FUSELAGE FRAME GOUGED AT BS 480 BELOW STRINGER 17L. BLENDED AREA AT BS 480 BELOW STRINGER 17L, ORIGINAL MATERIAL 0.150", MATERIAL REMAINING WAS 
- [SDR DHL2008765009](https://openairdocs.org/sdr/DHL2008765009), Jan 29, 2008: FRAME. DAMAGED. DURING C CHECK, 2 MISDRILLED HOLES IN FUSELAGE FRAME STRINGER 18L BS 480. REMOVED AND REINSTALLED HINGE ASSEMBLY AT FRAME, STRINGER 18 BS 480 IAW STC DRAWING 72
- [SDR DHL2008765001](https://openairdocs.org/sdr/DHL2008765001), Jan 29, 2008: SKIN. MISREPAIRED. DURING C CHECK, EXISTING REPAIR HAS BLIND RIVETS INSTALLED IN DOUBLER SHOULD BE SOLID FASTENERS PER SRM AT BS 1185 STRINGER 17L. REMOVED EXISTING REPAIR IAW SRM
- [SDR DHL2008765024](https://openairdocs.org/sdr/DHL2008765024), Jan 27, 2008: SKIN. CRACKED. DURING C CHECK, NR 4 SLAT UPPER SKIN CRACKED AT INBOARD HOOK MOUNT SCREW WS 390. STRIPPED AREA IAW B727 MM 51-20-1, C/S HFEC IAW B727 NDTM PT6 51-00-00 FIG 23. 
- [SDR DHL2008765022](https://openairdocs.org/sdr/DHL2008765022), Jan 27, 2008: BEAM. DAMAGED. DURING C CHECK, REJECTED NR 105146 BECAUSE ORIGINAL FABRICATED 'J' BEAM WAS DAMAGED UPON INSTALLATION. RT WING TRAILING EDGE UPPER 'J' BEAM IS CRACKED AT WBL 11
- [SDR DHL2008765016](https://openairdocs.org/sdr/DHL2008765016), Jan 25, 2008: BEAM. CRACKED. DURING C CHECK, LT WING UPPER TRAILING EDGE PANEL SUPPORT 'J' BEAM WBL 124 IS CRACKED IN CUT OUT FORWARD OF NR 7 SPOILER ACTUATOR. REMOVED TRAILING EDGE UPPER P
- [SDR DHL2008765034](https://openairdocs.org/sdr/DHL2008765034), Jan 23, 2008: BULKHEAD. CORRODED. DURING C CHECK, BS 227.8 BULKHEAD FORWARD LOWER WEB AND STIFFENER IS CORRODED. REMOVED STIFFENERS AND ATTACHED PARTS IN AREA FOR ACCESS IAW SRM 51-30-2. CUT OUT
- [SDR DHL2008765014](https://openairdocs.org/sdr/DHL2008765014), Jan 21, 2008: STRUCTURE. CRACKED. DURING C CHECK: DISCREPANCY - RIGHT WING INBOARD FLAP, MID FLAP AFT IS CRACKED ON BOTH INBOARD AND OUTBOARD SIDE WBL 90.69 AND WBL 104.0. REMOVED NR 5 AND 6 TEA
- [SDR DHL2008765012](https://openairdocs.org/sdr/DHL2008765012), Jan 21, 2008: STRINGER. CORRODED. DURING C CHECK: DISCREPANCY - RT WHEEL WELL STRINGER 18A IS CORRODED AT WBL 70 ON FORWARD SIDE OF BS 880. REMOVED STRINGER 18A IAW SRM 51-30-2. FABRICATED STRIN
- [SDR DHL2008765011](https://openairdocs.org/sdr/DHL2008765011), Jan 21, 2008: SUPPORT. CRACKED. DURING C CHECK, RIGHT WHEEL WELL SUPPORT STRUCTURE HAS CRACK AT BS 880 RBL 26. REMOVED SUPPORT STRUCTURE AT RIGHT WHEEL WELL BS 880 RBL 26 IAW SRM 51-30-2. FABR
- [SDR DHL2008765003](https://openairdocs.org/sdr/DHL2008765003), Jan 21, 2008: TORQUE BOX. CRACKED. DURING C CHECK, AFT STAIRWELL LIGHTENING HOLE CRACKED 5 O'CLOCK POSITION RIGHT SIDE BS 1265 (TORQUE BOX). CUT OUT DAMAGED AREA AT AFT STAIRWELL LIGHTENING HOLE 
- [SDR DHL2008765021](https://openairdocs.org/sdr/DHL2008765021), Jan 20, 2008: HINGE. CRACKED. DURING C CHECK, MCD AFT HINGE SECTION IS CRACKED AT BS 612 STRINGER 4L. REMOVED AFT HINGE SECTION AT MAIN CARGO DOOR BS 612 STRINGER 4L IAW MM FIG 5201B REV E. 
- [SDR DHL2008765032](https://openairdocs.org/sdr/DHL2008765032), Jan 19, 2008: RIB. CRACKED. DURING C CHECK, NR 2 SLAT OUTBOARD ACTUATOR SUPPORT RIB CRACKED. REMOVED ACCESS PANEL AT NR 2 SLAT IAW SRM 51-30-2. LOCATED AND DRILLED HOLES ON NEW RIB IAW SRM
- [SDR DHL2008765030](https://openairdocs.org/sdr/DHL2008765030), Jan 19, 2008: RIB. CRACKED. DURING C CHECK, CRACK INDICATION ON NR 4 SLAT OUTBOARD ACTUATOR SUPPORT RIB. REMOVED ACCESS PANEL AT NR 4 SLAT IAW SRM 51-30-2. LOCATED AND DRILLED HOLES ON NEW
- [SDR DHL2008765025](https://openairdocs.org/sdr/DHL2008765025), Jan 19, 2008: SKIN. CRACKED. DURING C CHECK, CRACKED ON NR 3 SLAT UPPER SURFACE AT INBOARD SLAT HOOK MOUNT SCREW WS 520. REMOVED HOOK FROM AREA IAW SRM 51-30-2. FABRICATED REPAIR DOUBLER IA
- [SDR DHL2008765005](https://openairdocs.org/sdr/DHL2008765005), Jan 19, 2008: TORQUE BOX. CRACKED. DURING C CHECK, AFT STAIRWELL LIGHTENING HOLE CRACKED 6 O'CLOCK POSITION RIGHT SIDE BS 1240 (TORQUE BOX). CUT OUT DAMAGED AREA AT AFT STAIRWELL LIGHTENING HOLES
- [SDR DHL2008765004](https://openairdocs.org/sdr/DHL2008765004), Jan 19, 2008: TORQUE BOX. CRACKED. DURING C CHECK, AFT STAIRWELL LIGHTENING HOLE CRACKED 12 O'CLOCK POSITION RIGHT SIDE OF STAIRWELL BS 1243 (TORQUE BOX). CUT OUT DAMAGED AREA AT AFT STAIRWELL LI
- [SDR DHL2008765002](https://openairdocs.org/sdr/DHL2008765002), Jan 19, 2008: WEB. CRACKED. DURING C CHECK, CUT OUT DAMAGED AREA AFT STAIRWELL LIGHTENING HOLE 10 O'CLOCK POSITION DIMENSION CUT OUT 1.5" BY .75" IAW SRM 51-40-2 FIG 1. FABRICATED DOUBLER 
- [SDR DHL2008765006](https://openairdocs.org/sdr/DHL2008765006), Jan 18, 2008: COVER. GOUGED. DURING C CHECK, RT INBOARD AILERON UPPER INBOARD HINGE COVER HAS DEEP GOUGE. REMOVED COVER IAW SRM 51-30-2. FABRICATED NEW COVER IAW SRM 57-50-2 FIGURE 7 AND 51
- [SDR DHL2008765031](https://openairdocs.org/sdr/DHL2008765031), Jan 17, 2008: RIB. CRACKED. DURING C CHECK, CRACK INDICATION ON PREVIOUS REPAIR OF NR 3 SLAT OUTBOARD ACTUATOR SUPPORT RIB. REMOVED NR 3 SLAT ACCESS PANEL IAW SRM 51-30-2. REMOVED CRACKED 
- [SDR DHL2008765018](https://openairdocs.org/sdr/DHL2008765018), Jan 16, 2008: STRUCTURE. GOUGED. DURING C CHECK, RIGHT WING NR 6 SLAT TRAILING EDGE GOUGED AT HOOK FITTINGS WS 150 APPROXIMATE. REMOVED HOOK FITTING FROM ACCESS IAW SRM 51-30-2. FABRICATED REPA
- [SDR DHL2008765017](https://openairdocs.org/sdr/DHL2008765017), Jan 16, 2008: SKIN. CRACKED. DURING C CHECK, RT WING NR 4 LEADING EDGE FLAP INNER SKIN CRACKED 3 PLACES AROUND RIVETS AT INBOARD IND WS 150. STOP DRILLED 3 EACH CRACKED PLACES AROUND RIVETS
- [SDR DHL2008765026](https://openairdocs.org/sdr/DHL2008765026), Jan 15, 2008: SKIN. CRACKED. DURING C CHECK, NR 2 SPOILER NR 2 HINGE CUT OUT ON LT WING TRAILING EDGE CRACKED. REMOVED ON LT WING TRAILING EDGE SKIN SECTION AT NR 2 SPOILER DIMENSION 36" BY
- [SDR DHL2008765013](https://openairdocs.org/sdr/DHL2008765013), Jan 15, 2008: SKIN. GOUGED. DURING C CHECK, LT OUTBOARD FORE FLAP OUTBOARD LEADING EDGE REPAIR IS GOUGED 2 PLACES. REMOVED OLD DOUBLER REPAIR IAW SRM 51-30-2. FABRICATED NEW DOUBLER REPAIR
- [SDR DHL2008765007](https://openairdocs.org/sdr/DHL2008765007), Jan 15, 2008: SKIN. DENTED. DURING C CHECK, RT WING WS 760 NR 8 SLAT UPPER SURFACE HAS A DENT AROUND FASTENER. EVALUATED AND FOUND DENT OUT OF LIMITS IAW SRM 57-50-1 FIG 2 DUE TO DENT BEIN
- [SDR DHL2008765008](https://openairdocs.org/sdr/DHL2008765008), Jan 12, 2008: INTERCOSTAL. CRACKED. DURING C CHECK, AFT CARGO COMPARTMENT BS 950A + 19" INTERCOSTAL LBL 5" HAS FASTENERS POPPED AND METAL CRACKED. REMOVED INTERCOSTAL AT AFT CARGO PIT IAW SRM 51-3
- [SDR DHL2008765027](https://openairdocs.org/sdr/DHL2008765027), Jan 11, 2008: SKIN. CRACKED. DURING C CHECK, NR 3 SPOILER NR 3 HINGE CUT OUT ON LT WING TRAILING EDGE IS CRACKED. STOP DRILLED CRACK 0.250 IAW SRM 51-10-1. FABRICATED DOUBLER REPAIR IAW SRM
- [SDR DHL2008765029](https://openairdocs.org/sdr/DHL2008765029), Jan 9, 2008: SKIN. CRACKED. DURING C CHECK, NR 4 SPOILER NR 2 HINGE CUT OUT ON LT WING TRAILING EDGE CRACKED. STOP DRILLED CRACK DIAMETER 0.250 INCH AND FABRICATED REPAIR DOUBLER IAW SRM 5
- [SDR DHL2008765028](https://openairdocs.org/sdr/DHL2008765028), Jan 9, 2008: SKIN. CRACKED. DURING C CHECK, NR 4 SPOILER NR 3 HINGE CUT OUT ON LEFT WING TRAILING EDGE CRACKED. STOP DRILLED CRACK DIAMETER 0.250" IAW SRM 51-10-1 AND 57-30-4 FIG 10, NDT S
- [SDR DHL2008765019](https://openairdocs.org/sdr/DHL2008765019), Jan 9, 2008: STRINGER. CRACKED. DURING C CHECK, VERTICAL STABILIZER NR 8 STRINGER CRACKED FIN STATION 133. REMOVED PREVIOUS REPAIR FROM AREA IAW SRM 51-30-2. FABRICATED 2 EACH REPAIR ANGLES IA
- [SDR DHL2007765001](https://openairdocs.org/sdr/DHL2007765001), Nov 24, 2007: WEB. CRACKED. A-8 CHECK REF N/R 054239 AFT AIRSTAIR AREA LT TORQUE BOX AT STA 1263 LWR LIGHTING HOLE SKIN HAS 1 INCH CRACK AT 11:00 POSITION. CUT OUT DAMAGED AREA AT AFT AIRS
- [SDR DHLA200700046](https://openairdocs.org/sdr/DHLA200700046), Sep 26, 2007: LIGHT. DISLODGED. FOUND UPPER EMERG EXIT LIGHT DISLODGED. RE INSTALLED UPPER EMERGENCY EXIT LIGHT PER MM 33-50-00.
- [SDR DHLA200700041](https://openairdocs.org/sdr/DHLA200700041), Aug 31, 2007: LIGHT. LOOSE. EMERGENCY LIGHT ILLUMINATED ON TAKEOFF. FOUND COCKPIT EMERGENCY LIGHT ASSY LOOSE. RESECURED IN PLACE PERFORMED GROUND TEST IAW M/M33-50-01,TEST OK
- [SDR DHL2006765004](https://openairdocs.org/sdr/DHL2006765004), Nov 1, 2006: BRAKE ASSY. NOISY. LEFT BRAKE MAKES NOISE WHEN DEPRESSED AND AIRCRAFT SHAKES. BLED LEFT MLG BRAKES PER B727 MM CH 32-41-00. OPS AND LEAK CHECK GOOD.
- [SDR DHL2006765003](https://openairdocs.org/sdr/DHL2006765003), Sep 22, 2006: INDICATOR. FAILED. NR 3 OIL PRESSURE WENT TO 100 PSI ON T/O ROLL. ABORTED T/O AT 10 KTS. REMOVED AND REPLACED NR 3 OIL PRESSURE IND IAW MM 79-32-00. OPS CHECK GOOD IAW JRH 5.2.
- [SDR DHL2006765002](https://openairdocs.org/sdr/DHL2006765002), Jun 27, 2006: ENGINE. MALFUNCTIONED. ON ENG START - START WAS NORMAL. ENG ACCELERATED TO 30 PERCENT N1, 520 EGT 52 PERCENT N2. GRD PERSONNEL REPORTED ENG SMOKING & ENG FLAMED-OUT. ENG FAILURE CHECK
- [SDR DHL2006765001](https://openairdocs.org/sdr/DHL2006765001), Apr 12, 2006: ACCESSORY UNIT. WARNING LIGHT. RT MAIN (RED) GEAR LIGHT ILLUMINATED IN FLIGHT. EXTINGUISHED AFTER GEAR EXTENSION. COULD NOT DUPLICATE. REPLACED RT GEAR RED KORRY LIGHT ASSY. REPLACED LANDING 
- [SDR DHL2005765511](https://openairdocs.org/sdr/DHL2005765511), Dec 15, 2005: STRINGER. CRACKED. FOUND FWD PIT STRINGER CRACKED STA 675 S-29L. CUT OUT CRACKED SECTION OF STRINGER AT STA 675 STR 29L. FABRICATED AND INSTALLED REPAIR STRINGER SECTION 20-5/8" F
- [SDR DHL2005765502](https://openairdocs.org/sdr/DHL2005765502), Dec 15, 2005: CHANNEL. CORRODED. AFT CARGO PIT FLOOR SUPPORT CHANNEL IS CRACKED BEYOND STOP DRILL HOLES (6" FWD OF STA 950F, RBL 4). REMOVED FLOOR SUPPORT IAW B727 SRM 51-30-2. FABRICATED AND I
- [SDR DHL2005765507](https://openairdocs.org/sdr/DHL2005765507), Dec 12, 2005: HINGE FITTING. CORRODED. FOUND LEFT HORIZ STAB T/E NR 1 ELEVATOR ATTACH HINGE LUGS INNER FACES HAS PITTING CORROSION. BLENDED CORROSION ON LUGS IAW TIMCO REO-983 REV IR DATED 12/01/05. 
- [SDR DHL2005765506](https://openairdocs.org/sdr/DHL2005765506), Dec 12, 2005: FLOOR SUPPORT. CORRODED. AFT BAGGAGE PIT CORROSION ON FLOOR SUPPORT CHANNEL, LWR SIDE, BETWEEN STA 1030 AND 1050 RBL 12. REMOVED SECTION OF FLOOR SUPPORT STA 1030 - 1082. FABRICATED AND
- [SDR DHL2005765508](https://openairdocs.org/sdr/DHL2005765508), Dec 12, 2005: HINGE FITTING. CORRODED. RT HORIZ STAB T/E NR 1 ELEVATOR ATTACH HINGE LUGS INNER FACES HAS PITTING CORROSION. BLENDED CORROSION ON LUGS IAW TIMCO REO-983 REV IR DATED 12/01/05. FOUND LU

All 93: https://openairdocs.org/deregistered/N765AT-2010-08-06/reports.md

## 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 19951105045609I](https://openairdocs.org/incident/19951105045609I), Nov 5, 1995: Boeing 727264 (N765AT), Indianapolis, IN. Narrative: on November 5, 1995, at 1127 EDT, a Boeing 727, N765AT registered to first security bank Utah and operated by American trans air (amta), under FAR…

## Other aircraft with N765AT

- [Registered now](https://openairdocs.org/aircraft/N765AT): Gulfstream Aerospace GV-SP (G550), S/N 5063, built 2004

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