# N7727A: 2006 Boeing 737-76N, registration cancelled 2026-06-05

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: June 5, 2026
- Status when cancelled: Valid registration
- Airframe: [Boeing 737-76N](https://openairdocs.org/model/boeing-737-76n) (registry code 13844CH)
- Engine: [CFM International CFM56-7B22 series](https://openairdocs.org/engine/cfm-international-cfm56-7b22-series) (registry code 13043)
- Serial number: 32673
- Year built: 2006
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: May 11, 2006
- Certificate issued: November 1, 2021
- Last registry action: June 23, 2023
- Mode S code: AA73C3
- Owner when cancelled: [Southwest Airlines Co](https://openairdocs.org/faa-owner/SOUTHWEST%20AIRLINES%20CO)
- Location: [Dallas, TX](https://openairdocs.org/faa-place/TX/Dallas)
- Owner type: Corporation
- Owner's area on the map: 32.8326° N, 96.8491° W: Placed by OpenAirDocs at the center of ZIP code 75235, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N7727A
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=7727A
- Page: https://openairdocs.org/deregistered/N7727A-2026-06-05

From the FAA registry file of November 5, 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 737-76N: https://openairdocs.org/model/boeing-737-76n.md

## Service difficulty reports (188, newest 50)

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

- [SDR SWAA2025101423610](https://openairdocs.org/sdr/SWAA2025101423610), Oct 11, 2025: LIGHT. INOPERATIVE. L2 DOOR EXTERIOR EMERGENCY LIGHT INOPERTIVE. REMOVED AND REPLACED L2 SLIDE EMERGENCY LIGHT IAW AMM 33-51-04. OPS CHECK GOOD.
- [SDR SWAA2025092215809](https://openairdocs.org/sdr/SWAA2025092215809), Sep 18, 2025: BRACKET. CRACKED. L/H WING UPPER TRAILING EDGE SHELF PANEL BETWEEN #5 &#6 SPOILER LOWER CENTER SUPPORT BRACKET CRACKED<[01] REMOVED AND REPLACED L/H WING TRAILING EDGE SUPPORT WE
- [SDR SWAA2025090210162](https://openairdocs.org/sdr/SWAA2025090210162), Aug 31, 2025: EEC. FAULTED. LEFT ENGINE UNRESPONSIVE AT ALTITUDE. PERFORMED BITE CHECK OF#1 EEC AND NO FAULTS CURRENT OR IN HISTORY NOTED BUT NO CHANNEL B ON GROUND TEST. REMOVED AND REPLA
- [SDR SWAA2025030400729](https://openairdocs.org/sdr/SWAA2025030400729), Feb 28, 2025: APU. SMOKE. AFTER APU SHUTDOWN; SMOKE OBSERVED COMING OUT APU AHM HAS SHOWN 'LOW OIL QTY.' SINCE THERE WAS SMOKE FROM THE TAIL PIPE AND THE LOW OIL QTY SUGGEST LOOKING DOWN
- [SDR SWAA2024121675484](https://openairdocs.org/sdr/SWAA2024121675484), Dec 10, 2024: BATTERY PACK. FAILED. M1675 FAILED CAPACITY CHECK<[01] R/R M1675 EMERGENCY LIGHT BATTERY PACK PER AMM 33-51-06
- [SDR SWAA2024121675485](https://openairdocs.org/sdr/SWAA2024121675485), Dec 10, 2024: BATTERY PACK. FAILED. M1674 FAILED CAPACITY CHECK<[01] R/R M1674 BATTERY PACK PER AMM 33-51-06
- [SDR SWAA2024110856318](https://openairdocs.org/sdr/SWAA2024110856318), Nov 4, 2024: GIRT BAR. MISINSTALLED. FORWARD ENTRY DOOR EMERGENCY SLIDE GIRT INCORRECTLY VELCROED TO BACKING PAN SHELF<[01] REMOVED FWD ENTRY DOOR SLIDE AND ADJUSTED SLIDE GIRT VELCRO AND REINSTALL
- [SDR SWAA2024050281670](https://openairdocs.org/sdr/SWAA2024050281670), May 2, 2024: SLIDE. DISLODGED. FORWARD ENTRY DOOR EMERGENCY EXIT SLIDE CAME OUT OF CONTAINER<[01] R & R FWD ENTRY SLIDE REF AMM 25-66-01
- [SDR SWAA2024031563584](https://openairdocs.org/sdr/SWAA2024031563584), Mar 15, 2024: PANEL. CRACKED. LH PANEL 194BL CRACKED. R & R LH PANEL 194BL PER AMM 53-51-21.
- [SDR SWAA2024020547052](https://openairdocs.org/sdr/SWAA2024020547052), Jan 31, 2024: GIRT BAR. CHAFED. AFT ENTRY DOOR (L-2) GIRT BAR SKIRT RUBBING AGAINST THRESHOLD WHEN OPENING AND CLOSING DOOR.<[01] JOB ACCOMPLISHED ON TTG8Q00R9LS3;[02] VERIFIED CORRECTIVE ACTI
- [SDR SWAA2024020547053](https://openairdocs.org/sdr/SWAA2024020547053), Jan 31, 2024: GIRT BAR. CHAFED. AFT SERVICE DOOR (R-2) GIRT BAR SKIRT RUBBING AGAINST THRESHOLD WHEN OPENING AND CLOSING DOOR.<[01] JOB ACCOMPLISHED ON TTG8Q00R9LWJ.;[02] VERIFIED CORRECTIVE A
- [SDR SWAA2024020246219](https://openairdocs.org/sdr/SWAA2024020246219), Jan 30, 2024: CONNECTOR. DISCONNECTED. L2 EXTERIOR EMERGENCY LIGHT INOP<[01] PERFORMED TROUBLESHOOTING AS PER B737 WDM 33-51-14. FOUND CONNECTOR D11086 DISCONNECTED. CONNECTOR D11086 WAS CONNECTED PR
- [SDR SWAA2024020545213](https://openairdocs.org/sdr/SWAA2024020545213), Jan 27, 2024: TEE ANGLE. CRACKED. LT W/W APPROX. STA 727 LBL 20 W/W STRUCTURE LOWER T CLIP IS CRACKED AT LOWER END.<[01] REMOVED AND REPLACED LOWER T CLIP AT LT W/W APPROX. STA 727 LBL 20 SRM 51
- [SDR SWAA2024020545212](https://openairdocs.org/sdr/SWAA2024020545212), Jan 26, 2024: SUPPORT ANGLE. CRACKED. LT W/W APPROX. STA 727 LBL 20 W/W STRUCTURE SUPPORT VERTICAL ANGLE IS CRACKED AT LOWER END. 124-010<[01] REMOVED CRACK ANGLE AT L/H W/W APPROX. STA. 727 AND LBL
- [SDR SWAA2024020244789](https://openairdocs.org/sdr/SWAA2024020244789), Jan 26, 2024: BATTERY PACK. INOPERATIVE. SEVERAL EMERGENCIES LIGHT INOP AT MAIN CABIN. SEVERAL EMERGENCY LIGHTS INOP AT MAIN CABIN.<[01] PERFORMED T/S OF THE EMERGENCY LIGHTS; FOUND M1672 AND M1673 DEF
- [SDR SWAA2024020244046](https://openairdocs.org/sdr/SWAA2024020244046), Jan 24, 2024: PIN. OUT OF POSITION. G1 GALLEY EMERGENCY EXIT LIGHT WIRE BROKEN AT CONNECTOR G1 GALLEY LOWER EMERGENCY EXIT SIGN INOP<[01] REMOVED AND REINSTALLED G1 GALLEY EMERGENCY EXIT LIGHT L11
- [SDR SWAA2024020543680](https://openairdocs.org/sdr/SWAA2024020543680), Jan 22, 2024: PANEL. CRACKED. CRACK - AT UPPER AFT CORNER (PANEL 192BR FAIRING- UNDERWING RIGHT FAIRING ABOVE A/C DOOR)<[01] REPAIRED PANEL #192BR AT DAMAGD AREA PER B737 SRM 51-70-04-2R-2; 
- [SDR SWAA2024020542629](https://openairdocs.org/sdr/SWAA2024020542629), Jan 19, 2024: ACCESS PANEL. CRACKED. L/H WING UPPER I/B ACCESS PANEL 551 DT CRACK AT T/E<[01] APPLIED REPAIR AT PANEL#551DT PER B737 SRM 51-70-04-2R-0 PARAGRAPH 4.N MATERIAL USED RESIN EY 3804 PO#2
- [SDR SWAA2024020241577](https://openairdocs.org/sdr/SWAA2024020241577), Jan 16, 2024: STRAP. CORRODED. *CORROSION* AFT CARGO FLOOR SUPPORT STRAP AT STA 767 BETWEEN LBL 21 AND RBL 21 WL 156.3<[01] FOUND EXFOLIATED CORROSION OUT OF LIMITS AT AFT CARGO FLOOR SUPPORT
- [SDR SWAA2024020241576](https://openairdocs.org/sdr/SWAA2024020241576), Jan 16, 2024: STRAP. CORRODED. *CORROSION* AFT CARGO FLOOR SUPPORT STRAP AT STA 727D BETWEEN LBL 21 AND RBL 21 WL 156.3<[01] FOUND EXFOLIATED OUT OF LIMITS CORROSION AT AFT CARGO FLOOR SUPP S
- [SDR SWAA2024020540175](https://openairdocs.org/sdr/SWAA2024020540175), Jan 11, 2024: STRINGER. DEBONDED. AFT CABIN CEILING AT STA 787 STR16L STRINGER COVERS DISBONDED. AFT CABIN L/H SIDE AT STA 787 STR16L STRINGER COVERS DISBOMDED<[01] REBONDED STRINGER COVERS AT A
- [SDR SWAA2024020539669](https://openairdocs.org/sdr/SWAA2024020539669), Jan 10, 2024: SUPPORT ANGLE. CRACKED. FWD CABIN FLOOR STRUCTURE BETWEEN STA 380 AND 400 LBL 13 WL 208.1 INTERCOSTAL UPPER FLOOR SUPPORT ANGLE IS CRACKED. 124-053<[01] REMOVED AND INSTALLED NEW ANGLE
- [SDR SWAA2024020539812](https://openairdocs.org/sdr/SWAA2024020539812), Jan 10, 2024: SUPPORT ANGLE. CRACKED. FWD CABIN FLOOR STRUCTURE BETWEEN STA 380 AND 400 RBL 8.5 WL 208.1 INTERCOSTAL UPPER FLOOR SUPPORT ANGLE IS CRACKED. 124-054<[01] REMOVED AND REPLACED NEW INTER
- [SDR SWAA2024020538521](https://openairdocs.org/sdr/SWAA2024020538521), Jan 7, 2024: FLOOR PANEL. PEELING. MAIN CABIN AFT WET AREA FLOOR PNL 241ABF UPPER SURFACE DELAMINATED<[01] RECEIVED NEW AFT WET AREA FLOOR PANEL 241ABF; PANEL WILL BE INSTALLED ON TTG8Q00PGLTN.;[
- [SDR SWAA2024020537081](https://openairdocs.org/sdr/SWAA2024020537081), Jan 2, 2024: DOOR SILL. CRACKED. FOUND CRACK AT LH INNER CHORD L-1 DOOR SILL AREA STA 303.9<[01] REMOVED AND REPLACED INNER CHORD AT L1 DOOR BETWEEN STA 277 TO 360 SRM 51-40-02-0G-0 AND DWG 141
- [SDR SWAA2024013136056](https://openairdocs.org/sdr/SWAA2024013136056), Dec 28, 2023: FLOOR PANEL. DELAMINATED. CABIN FLOOR PANEL 232QF UPPER SKIN AFT EDGE DENTED/DELAMINATED 1' SQUARE APPROX.<[01] INSTALLED FLOOR PANEL 232QF AS PER B737 AMM 53-21-00-400-801.;[02] CORRECT
- [SDR SWAA2024020535400](https://openairdocs.org/sdr/SWAA2024020535400), Dec 26, 2023: SEAL. DAMAGED. R/H HORIZONTAL STAB. UPPER ACCESS PANEL # 343AT HAS 2 EA RUBBER SEAL WITH ELONGATED HOLES<[01] REMOVED AND REPLACED R/H HORIZONTAL STAB. UPPER ACCESS PANEL # 34
- [SDR SWAA2024020535396](https://openairdocs.org/sdr/SWAA2024020535396), Dec 26, 2023: FLOOR SUPPORT. CORRODED. AFT CARGO FLOOR SUPPORT AT B/S 887 22' RIGHT TO 8' LEFT IS CORRODED.<[01] REMOVED AND REPLACED TEE ASSY (PN: 146A9401U39 PO: 1728471) AT AFT CARGO COMPT STA 887
- [SDR SWAA2024020535398](https://openairdocs.org/sdr/SWAA2024020535398), Dec 26, 2023: WEB. CORRODED. AFT CARGO THRESHOLD WEB HAS LIGHT CORROSION<[01] REMOVED CORROSION AT AFT CARGO COMPT THRESHOLD WEB FROM STA 794.37 TO STA 847; RBL 23 TO RBL 28; PER REF SRM 51
- [SDR SWAA2024020535466](https://openairdocs.org/sdr/SWAA2024020535466), Dec 26, 2023: DOOR. CORRODED. ***CORROSION*** AT LH INNER CORE FROM STA 312 TO 344; SEVERAL SPOTS OF CORROSION. DOT 82-010.<[01] THE DISCREPANCY WAS COMPLETED IN THE [TTG8Q00QNCTV] SRM 51-40
- [SDR SWAA2024020535110](https://openairdocs.org/sdr/SWAA2024020535110), Dec 24, 2023: FRAME. CORRODED. CORROSION....R/H CABIN FLOOR FRAME @ STA 1016 RBL 34 WL 208.1 FASTENER HOLE HAS CORROSION. (18-021)<[01] ACCOMPLISHED REPAIR AT RT. CABIN FLOOR FRAME STA 1016 R
- [SDR SWAA2024020535104](https://openairdocs.org/sdr/SWAA2024020535104), Dec 23, 2023: SKIN. CRACKED. CRACK FOUND AT LT HORIZONTAL STABILIZER LOWER SKIN STAB STA 193.90; CRACK LENGTH 0.750'; I/B OF I/B FASTENER ROW; 16.5' FROM L/E. CRACK FOUND AT LT HORIZONTAL S
- [SDR SWAA2024020239482](https://openairdocs.org/sdr/SWAA2024020239482), Dec 23, 2023: SUPPORT BRACKET. CRACKED. PNEUMATIC CROSSOVER DUCT R/H SUPPORT BRACKET CRACKED<[01] REMOVED AND REPLACED PNEUMATIC CROSSOVER DUCT R/H SUPPORT BRACKET IN REF TO B737 SRM 51-40-02-0G-0.;[0
- [SDR SWAA2024013135042](https://openairdocs.org/sdr/SWAA2024013135042), Dec 23, 2023: SUPPORT BRACKET. CRACKED. PNEUMATIC CROSSOVER DUCT L/H SUPPORT BRACKET CRACKED<[01] REMOVED AND REPLACED PNEUMATIC CROSSOVER DUCT L/H SUPPORT BRACKET IN REF TO B737 SRM 51-40-02-0G-0.;[0
- [SDR SWAA2024020534834](https://openairdocs.org/sdr/SWAA2024020534834), Dec 22, 2023: FLOOR PANEL. PEELING. MAIN CABIN FLOOR PANEL 241UF UPPER SURFACE HAS PEELED FIBERS (017)<[01] FLOOR PANEL 241UF WILL BE ACCOMPLISHED ON TTG8Q00QKN94.;[02] STEP 1: ENTER IN ERROR.<BR>
- [SDR SWAA2024020534825](https://openairdocs.org/sdr/SWAA2024020534825), Dec 22, 2023: FLOOR PANEL. PEELING. MAIN CABIN FLOOR PANEL 241ACF UPPER SURFACE HAS PEELED FIBERS (014)<[01] RECEIVED NEW FLOOR PANEL 241ACF; P/N D104MM0003-311.<BR>PO# 2052116.<BR>PANEL 241ACF WI
- [SDR SWAA2024020534838](https://openairdocs.org/sdr/SWAA2024020534838), Dec 22, 2023: FLOOR PANEL. PEELING. MAIN CABIN FLOOR PANEL 242UF UPPER SURFACE HAS PEELED FIBERS (015)<[01] RECEIVED AFT WET AREA FLOOR PANEL 242UF; PANEL WILL BE INSTALLED ON TTG8Q00PGM33.;[02] V
- [SDR SWAA2024020534832](https://openairdocs.org/sdr/SWAA2024020534832), Dec 22, 2023: FLOOR PANEL. PEELING. MAIN CABIN FLOOR PANEL 241AAF UPPER SURFACE HAS PEELED FIBERS (016)<[01] RECEIVED AFT WET AREA FLOOR PANEL 241AAF; PANEL WILL BE INSTALLED ON TTG8Q00PGLTQ.;[02]
- [SDR SWAA2024020534835](https://openairdocs.org/sdr/SWAA2024020534835), Dec 22, 2023: FLOOR PANEL. CORRODED. MAIN CABIN FLOOR PANEL 241C HAS CORRODED INSERTS (011)<[01] REMOVED AND REPLACED BROKEN INSERTS AT MAIN CABIN FLOOR PANEL 241C REF. SRM. 53-00-50-2R-0;[02] VERI
- [SDR SWAA2024020534823](https://openairdocs.org/sdr/SWAA2024020534823), Dec 22, 2023: FLOOR PANEL. CORRODED. MAIN CABIN FLOOR PANEL 242VF HAS CORRODED INSERTS (004)<[01] REMOVED AND REPLACED. INSERTS BROKEN AT MAIN CABIN FLOOR PANEL 242VF. REF. SRM. 53-00-50-2R-0;[02] 
- [SDR SWAA2024020534824](https://openairdocs.org/sdr/SWAA2024020534824), Dec 22, 2023: FLOOR PANEL. CORRODED. MAIN CABIN FLOOR PANEL 241ACF HAS CORRODED INSERTS (005)<[01] THIS ITEM WILL BE ACCOMPLISHED ON TTG8Q00QGLT3; RECEIVED NEW FLOOR PANEL 241ACF.;[02] VERIFIED STE
- [SDR SWAA2024020534837](https://openairdocs.org/sdr/SWAA2024020534837), Dec 22, 2023: FLOOR PANEL. CORRODED. MAIN CABIN FLOOR PANEL 241ADF HAS CORRODED INSERTS (006)<[01] REMOVED AND REPLACED BROKEN INSERTS AT MAIN CABIN FLOOR PANEL 241ADF REF.SRM. 53-00-50-2R-0;[02] V
- [SDR SWAA2024020534827](https://openairdocs.org/sdr/SWAA2024020534827), Dec 22, 2023: FLOOR PANEL. CORRODED. MAIN CABIN FLOOR PANEL 242UF HAS CORRODED INSERTS (003)<[01] PANEL 242UF WILL BE REPLACED ON TTG8Q00QGN40;[02] VERIFIED STEP 1
- [SDR SWAA2024020534829](https://openairdocs.org/sdr/SWAA2024020534829), Dec 22, 2023: FLOOR PANEL. CORRODED. MAIN CABIN FLOOR PANEL 242B HAS CORRODED INSERTS (001)<[01] REMOVED AND REPLACED INSERTS BROKEN AT MAIN CABIN FLOOR PANEL 242B. REF. SRM. 53-00-50-2R-0;[02] VER
- [SDR SWAA2024020534830](https://openairdocs.org/sdr/SWAA2024020534830), Dec 22, 2023: FLOOR PANEL. CORRODED. MAIN CABIN FLOOR PANEL 241ABF HAS CORRODED INSERTS (009)<[01] PANNEL ASSY 241ABF WILL BE RE PLACED ON ITEM TTG8Q00QSA0K;[02] VERIFIED STEP 1
- [SDR SWAA2024020534839](https://openairdocs.org/sdr/SWAA2024020534839), Dec 22, 2023: FLOOR PANEL. CORRODED. MAIN CABIN FLOOR PANEL 241AAF HAS CORRODED INSERTS (008)<[01] THIS ITEM WILL BE ACCOMPLISHED ON TTG8Q00QGLV0.;[02] VERIFIED STEP 1
- [SDR SWAA2024020534392](https://openairdocs.org/sdr/SWAA2024020534392), Dec 21, 2023: SUPPORT FRAME. CRACKED. FWD CABIN WET AREA FUSELAGE SUPPORT FRAME CRACKED @ CUTOUT ABOVE L-1 DOOR FWD STA 312 MKD DOT<[01] ACCOMPLISHED REPAIR FOR EA NO:M-22-153-01244;[02] VERIFIED RE
- [SDR SWAA2024020534397](https://openairdocs.org/sdr/SWAA2024020534397), Dec 21, 2023: FLOOR PANEL. PEELING. CABIN FLOOR PANEL 231BF HAS PEELED UPPER SURFACE FIBERS. 124-028<[01] RECEIVED FLOOR PANEL #231BF WITH P/N: 141A5810-168. INSTALLATION WILL BE ACCOMPLISHED ON T
- [SDR SWAA2024020534626](https://openairdocs.org/sdr/SWAA2024020534626), Dec 21, 2023: FLOOR PANEL. PEELING. CABIN FLOOR PANEL 231AF HAS PEELED UPPER SURFACE FIBERS. 124-030<[01] RECEIVED CABIN FLOOR PANEL 231AF WILL BE INSTALLATION WILL BE ACCOMPLISHED ON TTG8Q00PGM3R
- [SDR SWAA2024020534627](https://openairdocs.org/sdr/SWAA2024020534627), Dec 21, 2023: FLOOR PANEL. PEELING. CABIN FLOOR PANEL 222BF HAS PEELED UPPER SURFACE FIBERS. 124-024<[01] RECEIVED FLOOR PANEL #222BF; WITH P/N:141A5810-507. INSTALLATION WILL BE ACCOMPLISHED ON T

All 188: https://openairdocs.org/deregistered/N7727A-2026-06-05/reports.md

## Other aircraft with N7727A

- [Cancelled 1956-11-02](https://openairdocs.org/deregistered/N7727A-1956-11-02): Cessna 180, S/N 32624. Owner: [Cessna Aircraft Co](https://openairdocs.org/faa-owner/CESSNA%20AIRCRAFT%20CO), [Wichita, KS](https://openairdocs.org/faa-place/KS/Wichita)

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