# N763AT: 1982 Boeing 727-264, registration cancelled 2010-07-09

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: July 9, 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: 22983
- Year built: 1982
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-jet
- Airworthiness: Standard, transport
- Airworthiness date: December 3, 1982
- Certificate issued: July 1, 2010
- Last registry action: July 1, 2010
- Mode S code: AA4CBF
- 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/N763AT
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=763AT
- Page: https://openairdocs.org/deregistered/N763AT-2010-07-09

From the FAA registry file of November 7, 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 (77, newest 50)

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

- [SDR DHLA200800118](https://openairdocs.org/sdr/DHLA200800118), Oct 29, 2008: CIRCUIT BREAKER. TRIPPED. DURING THE CLIMB-OUT OF KILN, EMERGENCY EXIT CONTROL RT C/B POPPED. COCKPIT EMERGENCY EXIT LIGHTS OPERATE NORMAL.
- [SDR DHL2008763530](https://openairdocs.org/sdr/DHL2008763530), Mar 24, 2008: FLOORBEAM. CORRODED. EXFOLIATION FOUND ON FLT DECK FLOORBEAM UPPER CAP AT BS 266, BL 0. REMOVED AND REPLACED UPPER CHORD SECTION WITH P/N 65-17588-2, PO NR 8109233, PER B727 SRM 51-
- [SDR DHL2008763529](https://openairdocs.org/sdr/DHL2008763529), Mar 19, 2008: RIB. CRACKED. NR 5 L/E SLAT INB TRACK INTERIOR, O/B RIB IS CRACKED. REMOVED AND REPLACED RIB ASSY (I/B AND O/B) WITH P/N 65-17281-13, PO3 8109195, PER B727 SRM 51-30-2.
- [SDR DHL2008763523](https://openairdocs.org/sdr/DHL2008763523), Mar 16, 2008: FRAME. DENTED. FRAME DAMAGED IN CARGO COMPT AT BS 347, ALONG STR 4L. CUT OUT DAMAGE, INSTALLED FRAME REPAIR PARTS, P/N AE727-2-360-11 AND AE727-2-360-12, PO NR 810972, PER B72
- [SDR DHL2008763511](https://openairdocs.org/sdr/DHL2008763511), Mar 16, 2008: HINGE. CRACKED. MCD AFT HINGE SEGMENT AFT LOBE CRACKED. REMOVED AND REPLACED HINGE SEGMENT WITH MS 20001-16-7200 MATERIAL PO NR 9002527 PER AEI B727-200 FREIGHTER MM CH 52 FIG 
- [SDR DHL2008763509](https://openairdocs.org/sdr/DHL2008763509), Mar 16, 2008: SKIN. CHAFED. RT I/B FORE FLAP I/B L/E CHAFED AT RWBL 73. DAMAGE BEYOND SERVICE LIMITS. REMOVED, FABRICATED, AND INSTALLED SKIN PANEL, 2024-T3 .050 INCH BY 14 INCH BY 14.5 IN
- [SDR DHL2008763528](https://openairdocs.org/sdr/DHL2008763528), Mar 14, 2008: SUPPORT FITTING. CRACKED. NR 6 K-FLAP ACTUATOR MOUNT SPT FITTING CRACKED AT WS 307.5. REMOVED ACTUATOR SUPPORT MOUNT ASSY. FABRICATED SUPPORT WEBS FROM 2024-T3, .063" BY 8" BY 3.5" (2 EA
- [SDR DHL2008763527](https://openairdocs.org/sdr/DHL2008763527), Mar 14, 2008: SUPPORT FITTING. CRACKED. NR 1 K-FLAP ACTUATOR MOUNT SPT FITTING CRACKED AT WS 307.5 AND 315.3. REMOVED ACTUATOR SUPPORT MOUNT ASSY, FABRICATED SUPPORT WEBS FROM 2024-T3, .063" BY 8" BY 
- [SDR DHL2008763518](https://openairdocs.org/sdr/DHL2008763518), Mar 14, 2008: SEAT TRACK. CORRODED. FOUND SEAT TRACK CORRODED AT BS 480-600, RBL 24. REMOVED, FABRICATED FROM BAC 1520-792, PO NR 9006020, 209" LONG, AND INSTALLED PER B727 SRM 53-10-2 FIG 7 AND 5
- [SDR DHL2008763515](https://openairdocs.org/sdr/DHL2008763515), Mar 14, 2008: SEAT TRACK. CORRODED. SEAT TRACK DAMAGED BS 520 TO 540, LBL 45. REMOVED AND REPLACED SEAT TRACK SECTION WITH P/N 65-23637-53, PO NR 658565, 220 INCH LONG, PER B727 SRM 53-10-2 FIG 7 
- [SDR DHL2008763526](https://openairdocs.org/sdr/DHL2008763526), Mar 13, 2008: SEAT TRACK. CORRODED. CABIN SEAT TRACK CORRODED AT BS 990 TO 1130, LBL 45.75. REMOVED, FABRICATED SEAT TRACK SECTION FROM BAC1520-792, 297.875" LONG, PO NR 9006020, AND INSTALLED PER
- [SDR DHL2008763508](https://openairdocs.org/sdr/DHL2008763508), Mar 13, 2008: RIB. CRACKED. PREVIOUS REPAIR ON L/WING O/B FORE FLAP UPPER SURFACE CHAFED, LWBL 400. REMOVED EXISTING REPAIR AND ASSOCIATED INTERNAL RIB. FABRICATED AND INSTALLED NEW REPAIR
- [SDR DHL2008763517](https://openairdocs.org/sdr/DHL2008763517), Mar 12, 2008: SEAT TRACK. CORRODED. SEAT TRACK CORRODED AT BS 1110-1130, LBL 24. REMOVED, FABRICATED FROM BAC 1520-792, PO NR 9006020, 297" LONG, AND INSTALLED PER B727 SRM 53-10-2 FIG 7 AND 53-10
- [SDR DHL2008763510](https://openairdocs.org/sdr/DHL2008763510), Mar 12, 2008: ATTACH ANGLE. CRACKED. R/WING L/E INTERIOR, CRACKED RIB ATTACH ANGLE AT RWS 125 (FRONT SPAR). FABRICATED AND INSTALLED REPAIR DOUBLER, 7075-T6 .050 INCH BY 10.5 INCH BY 2.5 INCH, PO N
- [SDR DHL2008763512](https://openairdocs.org/sdr/DHL2008763512), Mar 9, 2008: SUPPORT ANGLE. CRACKED. RMLG BODY DOOR ACTUATOR HANGER SUPPORT ANGLE CRACKED AT BS 870. REMOVED, FABRICATED, AND INSTALLED SUPPORT ANGLE, 7075-T6 .100 INCH BY 3.75 INCH BY 3.375 INCH, 
- [SDR DHL2008763516](https://openairdocs.org/sdr/DHL2008763516), Mar 8, 2008: SEAT TRACK. CORRODED. SEAT TRACK CORRODED AT BS 560-600, LBL 25. REMOVED, FABRICATED FROM BAC1520-792, PO NR 9006020, 209" LONG, AND REPLACED SEAT TRACK SECTION PER B727 SRM 53-10-1 
- [SDR DHL2008763514](https://openairdocs.org/sdr/DHL2008763514), Mar 8, 2008: SEAT TRACK. CORRODED. SEAT TRACK CORRODED BS 760 TO 850, RBL 25. REMOVED AND REPLACED SEAT TRACK SECTION WITH BAC1520-841 EXTRUSION, PO NR 810987, 95 INCH LONG, PER B727 SRM 53-10-2 
- [SDR DHL2008763513](https://openairdocs.org/sdr/DHL2008763513), Mar 7, 2008: SEAT TRACK. CORRODED. SEAT TRACK CORRODED BS 760 TO 850, RBL 45. REMOVED AND REPLACED SEAT TRACK SECTION WITH BAC1520-841 EXTRUSION, PO NR 810987, 95 INCHES LONG, PER B727 SRM 53-10-
- [SDR DHL2008763525](https://openairdocs.org/sdr/DHL2008763525), Mar 4, 2008: STRINGER SPLICE. CORRODED. AFT CARGO COMP AT BS 1010, STR 29R SPLICE CORRODED O/B SIDE. REMOVED, FABRICATED NEW SPLICE FROM BAC1498-131, 15" LONG, PO NR 9005686, AND INSTALLED PER B727 SR
- [SDR DHL2008763522](https://openairdocs.org/sdr/DHL2008763522), Mar 2, 2008: FRAME. DENTED. FRAME DENTED AND GOUGED IN CARGO COMPT AT BS 660, ABOVE STR 17R. CUT OUT DAMAGE, FABRICATED FRAME REPAIR, AND INSTALLED PER B727 SRM 51-40-3 FIG 1, 53-10-2 FIG 
- [SDR DHL2008763521](https://openairdocs.org/sdr/DHL2008763521), Mar 2, 2008: FRAME. DENTED. FRAME DENTED AND GOUGED IN CARGO COMPT AT BS 640, ABOVE STR 17R. CUT OUT DAMAGE, FABRICATED FRAME REPAIR, AND INSTALLED PER B727 SRM 51-40-3 FIG 1, 53-10-2 FIG 
- [SDR DHL2008763520](https://openairdocs.org/sdr/DHL2008763520), Mar 2, 2008: FRAME. GOUGED. FRAME GOUGED IN CARGO COMPT AT BS 600, ABOVE STR 17R. CUT OUT DAMAGE, FABRICATED FRAME REPAIR, AND INSTALLED PER B727 SRM 51-40-3 FIG 1, 53-10-2 FIG 3, AND 51-3
- [SDR DHL2008763502](https://openairdocs.org/sdr/DHL2008763502), Mar 2, 2008: SEAT TRACK. CORRODED. SEAT TRACK CORRODED AT FLANGE, BS 850-870, LBL 45. REMOVED TRACK SECTION, FABRICATED SECTION FROM BAC 1520-1466, PO NR 730788, 15.75 INCHES LONG, AND INSTALLED 
- [SDR DHL2008763501](https://openairdocs.org/sdr/DHL2008763501), Mar 2, 2008: SEAT TRACK. CORRODED. SEAT TRACK CORRODED AT FLANGE, BS 850-870, LBL 24. REMOVED TRACK SECTION, FABRICATED SECTION FROM BAC1520-1466, PO NR 730788, 15.75 INCHES LONG, AND INSTALLED P
- [SDR DHL2008763500](https://openairdocs.org/sdr/DHL2008763500), Mar 2, 2008: SEAT TRACK. CORRODED. SEAT TRACK CORRODED AT BS 850-870, RBL 45. REMOVED TRACK SECTION, FABRICATED SECTION FROM BAC1520-1466, PO NR 730788, 15.75" LONG, AND INSTALLED PER B727 SRM 53
- [SDR DHL2008763524](https://openairdocs.org/sdr/DHL2008763524), Mar 1, 2008: SHEAR TIE. CORRODED. FRAME SHEAR TIE CORRODED AT BS 1130, BETWEEN STR 28R AND 29R, AFT SIDE. REMOVED, FABRICATED SHEAR TIE FROM 7075-T6, .050" BY 6" BY 2.5", PO NR 9006153, AND INST
- [SDR DHL2008763519](https://openairdocs.org/sdr/DHL2008763519), Mar 1, 2008: FRAME. DENTED. FRAME DENTED IN CARGO COMPT AT BS 580, ABOVE STR 17R. CUT OUT DAMAGE, FABRICATED FRAME REPAIR, AND INSTALLED PER B727 SRM 51-40-3 FIG 1, 53-10-2 FIG 3, AND 51-3
- [SDR DHL2008763507](https://openairdocs.org/sdr/DHL2008763507), Mar 1, 2008: FRAME. DENTED. FRAME GOUGED AND DENTED AT BS 560, ABOVE STR 17R. CUT OUT DAMAGED AREA. FABRICATED AND INSTALLED FRAME REPAIR FROM 7075T6, .063 INCHES BY 7.25 INCHES BY 3.25 IN
- [SDR DHL2008763506](https://openairdocs.org/sdr/DHL2008763506), Mar 1, 2008: FRAME. DENTED. FRAME GOUGED AND DENTED AT BS 540, ABOVE STR 17R. CUT OUT DAMAGED AREA. FABRICATED AND INSTALLED FRAME REPAIR FROM 7075T6, .063 INCH BY 7.25 INCH BY 3.25 INCH, 
- [SDR DHL2008763505](https://openairdocs.org/sdr/DHL2008763505), Mar 1, 2008: FRAME. DENTED. FRAME GOUGED AND DENTED AT BS 520, ABOVE STR 17R. CUT OUT DAMAGED AREA. FABRICATED AND INSTALLED FRAME REPAIR FROM 7075T6, .063 INCH BY 7.25 INCH BY 3.25 INCH, 
- [SDR DHL2008763504](https://openairdocs.org/sdr/DHL2008763504), Mar 1, 2008: FRAME. DENTED. FRAME GOUGED AND DENTED AT BS 500 ABOVE STR 17R. CUT OUT DAMAGED AREA. FABRICATED AND INSTALLED FRAME REPAIR FROM 7075T6, .063 INCH BY 7.25 INCH BY 3.25 INCH, P
- [SDR DHL2008763503](https://openairdocs.org/sdr/DHL2008763503), Mar 1, 2008: FRAME. DENTED. FRAME GOUGED AND DENTED AT BS 480, ABOVE STR 17R. CUT OUT DAMAGED AREA. FABRICATED AND INSTALLED FRAME REPAIR FROM 7075T6, .063 INCHES BY 7.25 INCHES BY 3.25 IN
- [SDR DHL2007763002](https://openairdocs.org/sdr/DHL2007763002), Dec 18, 2007: PANEL. DELAMINATED. 7 BY 5 INCH AREA OF DELAMINATION ON PANEL JUST O/B OF NR 1 SPOILER. DELAMINATION LOCATED JUST ABOVE JACKSCREW GEAR BOX, PANEL NR 8155.
- [SDR DHL2007763001](https://openairdocs.org/sdr/DHL2007763001), Nov 10, 2007: WEB. CRACKED. A-6 CHECK, DISCREPANCY: AFT AIR STAIRS RT FWD LWR LIGHTING HOLE TORQUE BOX SKIN AREA IS CRACKED. ROUTED OUT CRACK IAW SRM 51-10-1 FABRICATED REPAIR DOUBLER FROM
- [SDR DHL2006763006](https://openairdocs.org/sdr/DHL2006763006), Nov 26, 2006: RELAY. FAILED. EMERG LTS COME ON IN ARMED POS. REPLACED R-70 RELAY AND CHECK SERV PER B-727 M/M 33-50-101 P/N 9524-6508.
- [SDR DHL2006763005](https://openairdocs.org/sdr/DHL2006763005), Nov 26, 2006: BATTERY. DISCHARGED. FWD ENTRY DOOR EMERGENCY LIGHTS INOP. REPLACED BATTERIES P/N 37067-001 2 EA IAW B727 M/M 33-50-101. OPS CHECK SERVICEABLE.
- [SDR DHL2006763004](https://openairdocs.org/sdr/DHL2006763004), Oct 31, 2006: COALESCER BAG. DIRTY. VERY STRONG ODOR, LIKE BURNING OIL COMING FROM PACKS DURING T/O AND CLIMB, GOES AWAY AFTER APPROX 20 MIN. REMOVED AND CLEANED BOTH WATER SEPARATOR COALESCER SOC
- [SDR DHL2006763003](https://openairdocs.org/sdr/DHL2006763003), Sep 7, 2006: CONNECTOR. DAMAGED. ON DEPARTURE LANDING GEAR WOULD NOT GO PAST OFF ABNORMAL PROCEDURES WAS PERFORMED HORN SOUNDED AT FLAPS 2 FLAPS WERE SELECTED BACK TO 5 AND GEAR HANDLE SELECTED
- [SDR DHL2006763002](https://openairdocs.org/sdr/DHL2006763002), Sep 7, 2006: ACCESSORY UNIT. FAILED. ON DEP F/O WENT TO RAISE GEAR, GEAR HANDLE WOULD NOT GO PAST OFF. F/O PULLED LEVER LATCH TO RAISE GEAR. ON FLAP RETRACTION WARNING HORN SOUNDED ON FLAPS UP, COM
- [SDR DHL2006763001](https://openairdocs.org/sdr/DHL2006763001), Jun 6, 2006: ACCESSORY UNIT. MALFUNCTIONED. RAISED GEAR, L GEAR UNSAFE LIGHT ILLUMINATED. PERFORMED AB PROC, L & R GEAR UNSAFE LIGHT & DOOR LIGHT ILLUMINATED. RII REQUIRED. REPLACED LANDING GEAR ACCESSORY
- [SDR DHL2006763505](https://openairdocs.org/sdr/DHL2006763505), Jan 25, 2006: ANGLE. GOUGED. FWD CARGO S-27R AT BS 560 HAS EXFOLIATION CORROSION. CUT OUT CORRODED SECTION BS 568 - 547.2 S-27R. FABRICATED AND INSTALLED REPAIRS 3.150" X .090" X .800" FROM
- [SDR DHL2006763503](https://openairdocs.org/sdr/DHL2006763503), Jan 25, 2006: CAP. CORRODED. S/O 284007 N/R 031817 - FWD CARGO AFT DOOR OPENING FRAME CAP BS 620 S-26R HAS EXFOLIATION CORROSION. CUT OUT CORRODED SECTION OF FRAME CAP. FABRICATED AND INSTL
- [SDR DHL2006763517](https://openairdocs.org/sdr/DHL2006763517), Jan 23, 2006: SKIN. PUNCTURED. S/O 284007 N/R 032223 - RT INBD FORE FLAP PUNCTURED APPROX 4 FEET FROM INBD END. CUT OUT PUNCTURED AREA 1" X 3". FABRICATED AND INSTALLED REPAIR DOUBLER 3 X 6" 
- [SDR DHL2006763510](https://openairdocs.org/sdr/DHL2006763510), Jan 22, 2006: INTERCOSTAL. CORRODED. S/O 284007 N/R 032047 - CORRODED SHEAR CLIP INTERCOSTAL, 6 INCHES FWD OF BS 990 OUTBD OF S-28R (BS 984). CUT OUT CORRODED SECTION. FABRICATED AND INSTALLED INTE
- [SDR DHL2006763515](https://openairdocs.org/sdr/DHL2006763515), Jan 21, 2006: SKIN. CHAFED. S/O 284007 N/R 032201 - RT INBD T/E FORE FLAP L/E SKIN CHAFED BEYOND LIMITS AT WBL 72 AND 166, 1.5" AND 96" INBD END. REMOVED 2 EA L/E PANELS THAT WERE OUT OF L
- [SDR DHL2006763516](https://openairdocs.org/sdr/DHL2006763516), Jan 21, 2006: SKIN. CRACKED. S/O 284007 N/R 032203 - RT INBD T/E FORE FLAP L/E SKIN CRACKED ON LOWER SURFACE 53.5" FROM INBD END WBL 124. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR
- [SDR DHL2006763501](https://openairdocs.org/sdr/DHL2006763501), Jan 21, 2006: FITTING. BROKEN. S/O 284007 N/R 031639 - LT OUTBD AILERON TAB HAS EXCESSIVE PLAY. OPEN LT OUTBD AILERON SKIN, FOUND INTERNAL TAB MOUNT FITTING BROKEN. REMOVED AND REPLACED FITTI
- [SDR DHL2006763514](https://openairdocs.org/sdr/DHL2006763514), Jan 20, 2006: SKIN. CHAFED. S/O 284007 N/R 032199 - LTOUTBD T/E FORE FLAP L/E SURFACE CHAFED BETWEEN IND AND CENTER HINGES WBL 367. TRIMMED OUT CHAFED AREA. FABRICATED AND INSTALLED REPAIR
- [SDR DHL2006763518](https://openairdocs.org/sdr/DHL2006763518), Jan 19, 2006: FRAME. CRACKED. S/O 284007 N/R 032154 - CRACK ABOUT 10 INCHES LONG ON FRAME WEB AT BS 1352 RT LOWER SIDE FROM 4 O'CLOCK POSITION TO 5 O'CLOCK AFT SIDE OF WEB. CUT OUT CRACKED A
- [SDR DHL2006763513](https://openairdocs.org/sdr/DHL2006763513), Jan 19, 2006: NUT PLATE. MISSING. S/O 284007 N/R 032195 - LT OUTBD FLAP OUTBD ATTACH FITTING ATTACH POINT HAS MISSING NUTPLATE. REMOVED EXISTING REPAIR DOUBLER, CUT OUT SKIN FOR ACCESS, REMOVED 

All 77: https://openairdocs.org/deregistered/N763AT-2010-07-09/reports.md

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