# N565WN: 2002 Boeing 737-76Q, registration cancelled 2026-04-22

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: April 22, 2026
- Status when cancelled: Valid registration
- Airframe: [Boeing 737-76Q](https://openairdocs.org/model/boeing-737-76q) (registry code 13845AA)
- Engine: [CFM International CFM56-7B22 series](https://openairdocs.org/engine/cfm-international-cfm56-7b22-series) (registry code 13043)
- Serial number: 30282
- Year built: 2002
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: June 17, 2014
- Certificate issued: March 23, 2022
- Last registry action: November 6, 2023
- Mode S code: A73B7E
- 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/N565WN
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=565WN
- Page: https://openairdocs.org/deregistered/N565WN-2026-04-22

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 737-76Q: https://openairdocs.org/model/boeing-737-76q.md

## Service difficulty reports (264, newest 50)

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

- [SDR SWAA2025122955746](https://openairdocs.org/sdr/SWAA2025122955746), Dec 26, 2025: REGULATOR. LOW PRESSURE. AT FL250 CABIN PRESSURE DROPPED TO -4000 PSI; ALT HORN SOUNDED. RAN QRH PRESSURE WAS CONTROLLED IN MANUAL. INSPECTED BOTH CARGO DOOR PRESSURE SEALS IAW MM 52-09
- [SDR SWAA2025122956227](https://openairdocs.org/sdr/SWAA2025122956227), Dec 26, 2025: REGULATOR. LOW PRESSURE. AT FL250 CABIN PRESSURE DROPPED TO -4000 PSI; ALT HORN SOUNDED. RAN QRH PRESSURE WAS CONTROLLED IN MANUAL. INSPECTED BOTH CARGO DOOR PRESSURE SEALS IAW MM 52-09
- [SDR SWAA2025122956228](https://openairdocs.org/sdr/SWAA2025122956228), Dec 26, 2025: VALVE. LOW PRESSURE. AT FL250 CABIN PRESSURE DROPPED TO -4000 PSI, ALT HORN SOUNDED. RAN QRH PRESSURE WAS CONTROLLED IN MANUAL. INSPECTED BOTH CARGO DOOR PRESSURE SEALS IAW MM 52-09
- [SDR SWAA2025122956229](https://openairdocs.org/sdr/SWAA2025122956229), Dec 26, 2025: VALVE. LOW PRESSURE. AT FL250 CABIN PRESSURE DROPPED TO -4000 PSI; ALT HORN SOUNDED. RAN QRH PRESSURE WAS CONTROLLED IN MANUAL. INSPECTED BOTH CARGO DOOR PRESSURE SEALS IAW MM 52-09
- [SDR SWAA2025121651775](https://openairdocs.org/sdr/SWAA2025121651775), Dec 12, 2025: SCREW. MISSING. LEFT OVERWING EMERGENCY EXIT DOOR HANDLE HOUSING MISSING SCREW LEFT OVERWING EMERGENCY EXIT DOOR HANDLE HOUSING MISSING SCREW. REPLACED LT OVERWING EMERGENCY EX
- [SDR SWAA2025090912957](https://openairdocs.org/sdr/SWAA2025090912957), Sep 8, 2025: FSEU. FAULTED. TRAILING EDGE FLAPS INOPERATIVE. FIM 27-59 TASK 808 CARRIED OUT. OHMED FOR CONTINUITY, SHORTS, INSULATION RESISTANCE & DAR TEST IAW WDM 27-53-21. NO FINDINGS. R
- [SDR SWAA2025090210292](https://openairdocs.org/sdr/SWAA2025090210292), Sep 1, 2025: SENSOR. FAULTED. AFTER PUTTING FLAP LEVER TO 5 THE FLAPS DID NOT EXTEND. WE NOTICED A VERY SMALL SPLIT IN THE TRAILING EDGE FLAPS. LE DEVICES WERE EXTENDED WITH THE ALTERNATE FL
- [SDR SWAA2025081804438](https://openairdocs.org/sdr/SWAA2025081804438), Aug 14, 2025: FLAP SYSTEM. FAULTED. AS WE WERE ABOUT TO SELECT FLAPS 1 (210KTS) WE NOTICED THE FLAP GAUGE INDICATING ZERO - ONE ON RT SIDE. WHEN WE SELECTED F1 THE FLAPS/SLATS DID NOT EXTEND. SELE
- [SDR SWAA2025062785458](https://openairdocs.org/sdr/SWAA2025062785458), Jun 25, 2025: SKIRT. OUT OF POSITION. AFT ENTRY DOOR SLIDE EXCESSIVE FABRIC<[01] REPOSITIONED AFT ENTRY SKIRT SLIDE PER AMM 25-66-01 AND TASK MT 725-61-06.
- [SDR SWAA2025050667536](https://openairdocs.org/sdr/SWAA2025050667536), May 4, 2025: SIGN. INOPERATIVE. CREW REPORTS OVER WING EMERGENCY EXIT INDICATOR LIGHT INOP. REMOVED AND REPLACED EXIT INDICATOR SIGN PER AMM 33-51-01.
- [SDR SWAA2025022699482](https://openairdocs.org/sdr/SWAA2025022699482), Feb 24, 2025: LENS. MISSING. L/H OVER WING EMERGENCY EXIT LIGHT LENS COVER MISSING<[01] INSTALLED L/H OVER WING EMERGENCY EXIT LUGHT LENS COVER PER SIP
- [SDR SWAA2025012789283](https://openairdocs.org/sdr/SWAA2025012789283), Jan 24, 2025: SHROUD. MISINSTALLED. FWD ENTRY DOOR SLIDE SHROUD NOT INSTALLED PROPERLY AT BOTTOM CENTER OF SHROUD<[01] INSTALLED CORRECTLY FWD ENTRY DOOR-SLIDE IAW AMM 25-66-01-400-801.;[02] INSTA
- [SDR SWAA2025012788590](https://openairdocs.org/sdr/SWAA2025012788590), Jan 22, 2025: LIGHT. INOPERATIVE. EMERGENCY LIGHT L1065 INOP APROX STA 480 LEFT<[01] RELAMPED EMERGENCY LIGHT L1065 APROX STA 480 LEFT; PERFORMED GOOD TEST PER AMM 33-51-03-960-801;[02] VERIFIED
- [SDR SWAA2025012388436](https://openairdocs.org/sdr/SWAA2025012388436), Jan 22, 2025: ELEC CONNECTOR. DISCONNECTED. EMERGENCY EXIT CEILING LIGHT L1419 INOP.<[01] PERFORMED TROUBLESHOOTING FOUND CONNECTOR D40038J DISCONNECT. RECONNECTED CONNECTOR D40038P FOR THE EMERGENCY LIGH
- [SDR SWAA2025012385910](https://openairdocs.org/sdr/SWAA2025012385910), Jan 14, 2025: SEAT TRACK. CRACKED. PASSENGER CABIN SEAT TRACK AFT FASTENER HEAD HAS A CRACK AT BS 727B; RBL 24.75. (MARKED)<[01] FINISHED PER EA-25-153-00101;[02] VERIFIED CORRECTIVE ACTION COMPL
- [SDR SWAA2025012884184](https://openairdocs.org/sdr/SWAA2025012884184), Jan 8, 2025: TRACK. CRACKED. RT HAND FWD UPPER TRACK ASSY FOR PANEL 343AT CRACKED.<[01] REMOVED AND REPLACED RT HAND FWD UPPER TRACK ASSY FOR PANEL 343AT IAW AMM 27-41-31-400-802.; [02] VER
- [SDR SWAA2025012283949](https://openairdocs.org/sdr/SWAA2025012283949), Jan 7, 2025: SCUFF PLATE. CRACKED. FCB FWD CORNER SCUFF PLATE CRACKED<[01] REPAIRED IAW SRM 53-30-15-2R-1; NDI CRACK FREE; FCB FWD CORNER SCUFF PLATE;[02] VERIFIED ALL STEPS; CORRECTION ACTION IT
- [SDR SWAA2025012283947](https://openairdocs.org/sdr/SWAA2025012283947), Jan 7, 2025: SCUFF PLATE. CRACKED. ACB AFT CORNER SCUFF PLATE CRACKED<[01] VERIFIED
- [SDR SWAA2025012283948](https://openairdocs.org/sdr/SWAA2025012283948), Jan 7, 2025: SCUFF PLATE. CRACKED. ACB FWD CORNER SCUFF PLATE CRACKED<[01] VERIFIED
- [SDR SWAA2025012283447](https://openairdocs.org/sdr/SWAA2025012283447), Jan 6, 2025: FLOORBEAM. CRACKED. BS540 FLOOR SUPPORT (PANEL BREAK) IS CRACKED RBL1; WL208<[01] REOMOVED AND REPLACED NEW FLOOR SUPPORT (PANEL BREAK) BS540 RBL1 TO RBL24 IAW SRM 51-40-02 AND DWG
- [SDR SWAA2025012283452](https://openairdocs.org/sdr/SWAA2025012283452), Jan 6, 2025: FLOORBEAM. CRACKED. BS540 FLOOR SUPPORT (PANEL BREAK) IS CRACKED LBL1; WL208<[01] REMOVED AND REPLACED FLOOR SUPPORT (PANEL BREAK) BS540 LBL1 TO LBL24 IAW SRM 51-40-02 AND DWG 143A
- [SDR SWAA2025012083130](https://openairdocs.org/sdr/SWAA2025012083130), Jan 5, 2025: FLOOR PANEL. PULLED. PASSENGER CABIN FLOOR PANEL 231XF HAS AREAS OF PULLED STRANDS<[01] PASSENGER CABIN FLOOR PANEL 231XF WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A NEWLY FABR
- [SDR SWAA2025012083131](https://openairdocs.org/sdr/SWAA2025012083131), Jan 5, 2025: FLOOR PANEL. PULLED. PASSENGER CABIN FLOOR PANEL 231YF HAS AREAS OF PULLED STRANDS<[01] PASSENGER CABIN FLOOR PANEL 231YF WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A NEWLY FABR
- [SDR SWAA2025012083128](https://openairdocs.org/sdr/SWAA2025012083128), Jan 5, 2025: FLOOR PANEL. PULLED. PASSENGER CABIN FLOOR PANEL 231ZF HAS AREAS OF PULLED STRANDS<[01] PASSENGER CABIN FLOOR PANEL 231ZF WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A NEWLY FABR
- [SDR SWAA2025012083132](https://openairdocs.org/sdr/SWAA2025012083132), Jan 5, 2025: FLOOR PANEL. PULLED. PASSENGER CABIN FLOOR PANEL 241BF HAS AREAS OF PULLED STRANDS<[01] PASSENGER CABIN FLOOR PANEL 241BF WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A NEWLY FABR
- [SDR SWAA2025012083133](https://openairdocs.org/sdr/SWAA2025012083133), Jan 5, 2025: FLOOR PANEL. PULLED. PASSENGER CABIN FLOOR PANEL 241DF HAS AREAS OF PULLED STRANDS<[01] PASSENGER CABIN FLOOR PANEL 241DF; WITH AREAS OF PULLED STRANDS; WAS REPLACED WITH A NEWLY FA
- [SDR SWAA2025012083129](https://openairdocs.org/sdr/SWAA2025012083129), Jan 5, 2025: FLOOR PANEL. PULLED. PASSENGER CABIN FLOOR PANEL 241EF HAS AREAS OF PULLED STRANDS<[01] FOUND DAMAGE TO PANEL 241EF BE BEYOND ECONOMICAL REPAIR; FABRICATED NEW FLOOR PANEL FROM BMS 
- [SDR SWAA2025012083134](https://openairdocs.org/sdr/SWAA2025012083134), Jan 5, 2025: FLOOR PANEL. PULLED. PASSENGER CABIN FLOOR PANEL 241FF HAS AREAS OF PULLED STRANDS<[01] FOUND DAMAGE TO PANEL 241FF BE BEYOND ECONOMICAL REPAIR; FABRICATED NEW FLOOR PANEL FROM BMS 
- [SDR SWAA2024111960573](https://openairdocs.org/sdr/SWAA2024111960573), Nov 16, 2024: HANDLE. BROKEN. GRAB ASSIST HANDLE BROKEN FWD ENTRY DOOR<[01] RE SECURED PER SIP NO DEFECTS NOTED.
- [SDR SWAA2024093041679](https://openairdocs.org/sdr/SWAA2024093041679), Sep 24, 2024: SIGN. DETACHED. F/O SIDE EXIT SIGN AT FOOT LEVEL FELL OFF AND COULDNT BE REATTACHED<[01] RE-ATTACHED LIGHT LENS PER AMM 33-51-01
- [SDR SWAA2024071612661](https://openairdocs.org/sdr/SWAA2024071612661), Jul 15, 2024: LIGHT. MISSING. EMERGENCY EXIT LIGHT COVER MISSING F/O SIDE OVERWING EXIT LOWER LENS<[01] INSTALLED LIGHT COVER F/O SIDE EMERGENCY EXIT LIGHT PER AMM 33-51-04
- [SDR SWAA2024042578757](https://openairdocs.org/sdr/SWAA2024042578757), Apr 24, 2024: COVER. MISSING. ROW 12DEF EMERGENCY EXIT FWD LIGHT ASSY COVER IS MISSING<[01] INSTALLED EMERGENCY LIGHT LENS COVER AT ROW 12 DEF FWD LIGHT ASSY IAW AMM 33-51-01.
- [SDR SWAA2023080284905](https://openairdocs.org/sdr/SWAA2023080284905), Aug 1, 2023: CONNECTOR. FAULTY. FLAP ASYMMETRY DISCOVERED DURING CRUISE BY SPLIT NEEDLES ON FLAP GAUGE. RT FLAP SHOWED FULL UP; LT FLAP WAS BETWEEN UP AND 1. VERIFIED ASYMMETRY BY CONFIGURING 
- [SDR SWAA2023080284536](https://openairdocs.org/sdr/SWAA2023080284536), Aug 1, 2023: SENSOR. FAULTY. FLAP ASYMMETRY DISCOVERED DURING CRUISE BY SPLIT NEEDLES ON FLAP GAUGE. RT FLAP SHOWED FULL UP; LT FLAP WAS BETWEEN UP AND 1. VERIFIED ASYMMETRY BY CONFIGURING 
- [SDR SWAA2023073183616](https://openairdocs.org/sdr/SWAA2023073183616), Jul 29, 2023: SENSOR. DIRTY. AT CRUISE NOTICED A SMALL SPLIT ON THE FLAP GAUGE. RIGHT FLAP AT 0 LEFT FLAP AT .2. ON CONFIGURATION FOR LANDING FLAPS 1 SELECTED WITH NO MOVEMENT OF THE FLAPS.
- [SDR SWAA2023072481696](https://openairdocs.org/sdr/SWAA2023072481696), Jul 24, 2023: STARTER. LEAKING. ON DECENT #2 ENGINE OIL QTY DROPPED TO 21% ON DECENT #2 ENGINE OIL QTY DROPPED TO 21%.WHEN THRUST LEVER WAS MOVED FORWARD THE QTY DROPPED TO 19% WE KEPT THE #2 
- [SDR SWAA2023071478500](https://openairdocs.org/sdr/SWAA2023071478500), Jul 14, 2023: SENSOR. FAULT MESSAGE. SELECTED FLAPS 5; ONE FLAP STAYED AT ZERO; OTHER FLAP STOPPED AT LESS THEN 1.<[01] UPDATING PARTS TRANSACTION;[02] PERFORMED PARTS TRANSACTION ONLY;[03] FSEU FA
- [SDR SWAA2023060556070](https://openairdocs.org/sdr/SWAA2023060556070), Jun 3, 2023: TRANSMITTER. FAULTY. ON APPROACH WITH FLAPS 5 SELECTED FLAPS LOCKED OUT BETWEEN 1 AND UP. SMOOTH NORMAL LANDING.<[01] R&R RH FLAP POSITION TRANSMITTER IAW AMM 27-58-01. OPS CHECK GO
- [SDR SWAA2023051949416](https://openairdocs.org/sdr/SWAA2023051949416), May 17, 2023: STRIP. PEELING. RUDDER CONDUCTIVE FRAME PREVIOUS REPAIR SPLICE STRIP PEELED BACK; LH SIDE AT TE.<[01] INSTALLED NEW SPLICE STRIP AND VERIFIED CONDUCTIVITY LESS THAN 0.01 OHM IA
- [SDR SWAA2023050131165](https://openairdocs.org/sdr/SWAA2023050131165), Apr 25, 2023: WIRE. OPEN. MULTIPLE CABIN EMERGENCY LIGHT INOP<[01] FOUND CABIN EMERGENCY LIGHTS INOP AT 6C 8D 9C 12C 13D 18D. R/R POWER SUPPLY AND BATTERY PACK AT 7A ALONG THE SIDEWALL N
- [SDR SWAA2023021598916](https://openairdocs.org/sdr/SWAA2023021598916), Feb 5, 2023: CONNECTOR. DISCONNECTED. AISLE LIGHT AT STA727E+13 RBL29 AND AFT SERVICE DOOR SLIDE LIGHT DO NOT ILLUMINATE DURING INSTALLATION TEST OF M1672 BATTERY<[01] **FOUND CONNECTOR D11336 DISCO
- [SDR SWAA2023021697987](https://openairdocs.org/sdr/SWAA2023021697987), Feb 2, 2023: FLOOR PANEL. DAMAGED. NEED TO RELOCATE FLOOR PANEL #241FF INSERT (1 EACH) DUE TO REPAIRED INSTALLED ON THE FLOORBEAM AT BS727+6 LBL 45.57.<[01] FABRICATED NEW FLOOR PANEL 241FF USING
- [SDR SWAA2023021598915](https://openairdocs.org/sdr/SWAA2023021598915), Jan 28, 2023: WIRE. PULLED. 1 EACH WIRE IS PULLED OUT OF GROUND BLOCK BEHIND AFT LAV; JUST FWD OF BS 1006 ON L/H SIDEWALL<[01] RETERMINATED WIRE W3142-0451-18 TO GD3778 PER WDM 33-51-14.;[
- [SDR SWAA2023021694367](https://openairdocs.org/sdr/SWAA2023021694367), Jan 23, 2023: BAFFLE. CRACKED. BAFFLE UNDER L/H FLOOR TO SIDEWALL SUPPORT BS 400-420 LBL 25 IS CRACKED<[01] REMOVED BAFFLE UNDER FLOOR TO SIDEWALL SUPPORT BS 400-420 LBL 25 PER SRM 51-40-02-0
- [SDR SWAA2023021693554](https://openairdocs.org/sdr/SWAA2023021693554), Jan 21, 2023: FLOOR PANEL. PULLED. FLOOR PANEL 242DF UPPER SKIN HAS MULTIPLE AREAS OF PULLED STRANDS.<[01] IDENTIFIED PANEL 242DF MATERIAL IAW SRM 53-00-50-0I-1 FIGURE 4; TABLE 4; AND DWG DOC: 14
- [SDR SWAA2023021693555](https://openairdocs.org/sdr/SWAA2023021693555), Jan 21, 2023: FLOOR PANEL. PULLED. FLOOR PANEL 242CF UPPER SKIN HAS MULTIPLE AREAS OF PULLED STRANDS.<[01] IDENTIFIED PANEL 241CF MATERIAL IAW SRM 53-00-50-0I-1 FIG 4 TABLE 4 AND DWG: 144A5810 ID
- [SDR SWAA2023021693552](https://openairdocs.org/sdr/SWAA2023021693552), Jan 21, 2023: FLOOR PANEL. PULLED. FLOOR PANEL 241FF UPPER SKIN HAS MULTIPLE AREAS OF PULLED STRANDS.<[01] PART/MATERIAL IDENTIFIED PER SRM 53-00-50-0I-1 FIG 4 TABLE 4 LOW TRAFFIC<BR>NUMEROUS PUL
- [SDR SWAA2023021693547](https://openairdocs.org/sdr/SWAA2023021693547), Jan 21, 2023: FLOOR PANEL. DEBONDED. FLOOR PANEL 232RF UPPER SKIN PREVIOUS REPAIR IS DISBONDED. (MARKED)<[01] IDENTIFIED FLOOR PANEL 232RF MATERIAL IAW SRM 53-00-50-0I-1 FIG 4 TABLE 4<BR><BR>FOUND 
- [SDR SWAA2023021693546](https://openairdocs.org/sdr/SWAA2023021693546), Jan 21, 2023: FLOOR PANEL. PULLED. FLOOR PANEL 231XF UPPER SURFACE HAS MULTIPLE AREAS OF PULLED STRANDS.<[01] IDENTIFIED PANEL 231XF MATERIAL IAW SRM 53-00-50-0I-1 FIG 4 TABLE 4 AND DWG: 144A5810
- [SDR SWAA2023021691551](https://openairdocs.org/sdr/SWAA2023021691551), Jan 13, 2023: GUSSET. CRACKED. CRACK ON FWD CARGO BAY GUSSET AT BS 500D STRINGER 19R.<[01] DAMAGE FOUND AT FWD CARGO BAY GUSSET BS 500D STR-19R FOUND TO BE OUT OF LIMIT DUE TO NO LIMTE ON SRM

All 264: https://openairdocs.org/deregistered/N565WN-2026-04-22/reports.md

## NTSB investigations (1)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB DCA16CA133](https://openairdocs.org/ntsb/DCA16CA133), Apr 14, 2016: Boeing 737 76Q (N565WN), San Diego, CA, no damage. Probable cause: the ramp agents failure to keep his right hand at a safe distance from the underside of the moving belt.

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