# N7724A: 2009 Boeing 737-7BD

- Status: Valid registration
- Airframe: [Boeing 737-7BD](https://openairdocs.org/model/boeing-737-7bd) (registry code 1384511, 149 seats)
- Engine: [CFM International CFM56-7B24 series](https://openairdocs.org/engine/cfm-international-cfm56-7b24-series) (registry code 13044)
- Serial number: 36725
- Year built: 2009
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: September 23, 2013
- Certificate issued: November 6, 2013
- Expires: November 30, 2029
- Mode S code: AA735A
- Registered owner: [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 is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=7724A
- Page: https://openairdocs.org/aircraft/N7724A

From the FAA registry file of October 24, 2026. ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination. The registry lists only the engine series, so ADs for every CFM International CFM56-7B24 model are included.

## ADs that may apply (OpenAirDocs): 19 in force

### Matched by airframe (Boeing 737-7BD)

None in force.

### Matched by engine (CFM International CFM56-7B24 series)

- [AD 2023-05-05](https://openairdocs.org/ad/2023-05-05): Turbine Engine Compressor Section · CFM International CFM56-5B1, CFM56-5B1/2P, CFM56-5B1/3 and 98 more. Effective May 10, 2023
- [AD 2022-02-03](https://openairdocs.org/ad/2022-02-03): Turbine Engine Accessory Drive · CFM International CFM56-3, CFM56-3B, CFM56-3C and 34 more. Effective Mar 22, 2022
- [AD 2021-16-08](https://openairdocs.org/ad/2021-16-08): Turbine Section · CFM International CFM56-5B1, CFM56-5B1/2P, CFM56-5B1/P and 55 more. Effective Sep 28, 2021
- [AD 2018-26-01](https://openairdocs.org/ad/2018-26-01): Turbine Engine Compressor Section · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B20/3 and 46 more. Effective Jan 10, 2019
- [AD 2018-09-51](https://openairdocs.org/ad/2018-09-51): Engine · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B20/3 and 46 more. Effective Jun 7, 2018
- [AD 2015-18-04](https://openairdocs.org/ad/2015-18-04): 73-tooth gearshaft located in the engine accessory gearbox (AGB) · CFM International CFM56-3, CFM56-7B20, CFM56-7B20/2 and 47 more. Effective Oct 20, 2015
- [AD 2015-04-02](https://openairdocs.org/ad/2015-04-02): Dual engine thrust instability event · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B20/3 and 46 more. Effective Mar 31, 2015
- [AD 2010-13-09](https://openairdocs.org/ad/2010-13-09): Stage 3 low-pressure turbine (LPT) · CFM International CFM56-5, CFM56-5-A1/F, CFM56-5A4 and 88 more. Effective Jul 26, 2010
- [AD 2010-01-05](https://openairdocs.org/ad/2010-01-05): LP turbine rear frames · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B20/3 and 25 more. Effective Feb 18, 2010
- [AD 2009-11-02](https://openairdocs.org/ad/2009-11-02): HPC 4-9 spools · CFM International CFM56-2, CFM56-2A, CFM56-2B and 109 more. Effective Jun 23, 2009
- [AD 2008-03-09](https://openairdocs.org/ad/2008-03-09): Low pressure turbine rear frames (TRFs) · CFM International CFM56-7B18, CFM56-7B20, CFM56-7B22 and 10 more. Effective Mar 10, 2008
- [AD 2006-26-01](https://openairdocs.org/ad/2006-26-01): Fuel filters · CFM International CFM56-2, CFM56-2A, CFM56-2B and 93 more. Effective Jan 3, 2007
- [AD 2002-16-18](https://openairdocs.org/ad/2002-16-18): Low pressure turbine (LPT) nozzle segments · CFM International CFM56-5B1, CFM56-5B1/2P, CFM56-5B1/P and 33 more. Effective Sep 18, 2002
- [AD 2002-13-03](https://openairdocs.org/ad/2002-13-03): Turbofan Engines · CFM International CFM56-2, CFM56-2A, CFM56-2B and 55 more. Effective Aug 1, 2002
- [AD 2001-11-05](https://openairdocs.org/ad/2001-11-05): No. 4 Bearings · CFM International CFM56-2, CFM56-2B, CFM56-3 and 45 more. Effective Jun 11, 2001
- [AD 2001-02-12](https://openairdocs.org/ad/2001-02-12): On-Wing Torque Inspection · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B22 and 11 more. Effective Feb 14, 2001
- [AD 98-21-23](https://openairdocs.org/ad/98-21-23): Electronic Engine Control · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B22 and 10 more. Effective Nov 2, 1998
- [AD 98-19-20](https://openairdocs.org/ad/98-19-20): Hydromechanical Unit · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B22 and 7 more. Effective Oct 7, 1998
- [AD 98-14-51](https://openairdocs.org/ad/98-14-51): Accessory Gearbox · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B22 and 10 more. Effective Oct 1, 1998

### Historical (superseded or no longer in force)

- [AD 2021-10-09](https://openairdocs.org/ad/2021-10-09) (historical): Turbine Engine Compressor Section · CFM International CFM56-5B1, CFM56-5B1/2P, CFM56-5B1/3 and 82 more. Effective Jun 24, 2021
- [AD 2019-12-05](https://openairdocs.org/ad/2019-12-05) (historical): Turbine Section · CFM International CFM56-5B1, CFM56-5B1/2P, CFM56-5B1/P and 39 more. Effective Jul 5, 2019
- [AD 2018-18-01](https://openairdocs.org/ad/2018-18-01) (historical): Turbine Engine Compressor Section · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B20/3 and 46 more. Effective Oct 16, 2018
- [AD 2018-10-11](https://openairdocs.org/ad/2018-10-11) (historical): Turbine Engine Compressor Section · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B20/3 and 46 more. Effective Jun 1, 2018
- [AD 2018-09-10](https://openairdocs.org/ad/2018-09-10) (historical): Turbine Engine Compressor Section · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B20/3 and 46 more. Effective May 14, 2018
- [AD 2013-26-01](https://openairdocs.org/ad/2013-26-01) (historical): Oil dynamic seal assembly · CFM International CFM56-3, CFM56-3B, CFM56-3C and 52 more. Effective Feb 3, 2014
- [AD 2000-12-01](https://openairdocs.org/ad/2000-12-01) (historical): Critical Life-Limited Parts · CFM International CFM56-2, CFM56-2A, CFM56-2B and 54 more. Effective Dec 11, 2000

## Information bulletins (advisory) (1 in force)

- [SAIB NE-08-17R3](https://openairdocs.org/saib/NE-08-17R3): Turbine Section - Propulsion Technology LLC Unapproved Repair. Issued May 28, 2014
- [SAIB NE-08-17R2](https://openairdocs.org/saib/NE-08-17R2) (historical): Turbine Section - Propulsion Technology LLC Unapproved Repair. Issued Mar 7, 2011
- [SAIB NE-08-17R1](https://openairdocs.org/saib/NE-08-17R1) (historical): Propulsion Technology LLC Unapproved Repair. Issued May 22, 2008
- [SAIB NE-08-17](https://openairdocs.org/saib/NE-08-17) (historical): Propulsion Technologies International Unapproved Repair. Issued May 14, 2008

## 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 DCA25LA185](https://openairdocs.org/ntsb/DCA25LA185), Apr 17, 2025: Boeing 737 (N7724A), Houston, TX, no damage. Probable cause: Serious Injury to a flight attendant sustained during an evacuation.

## FAA accident and incident reports

None matched to N7724A.

## Service difficulty reports (183, newest 50)

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

- [SDR SWAA2026090956952](https://openairdocs.org/sdr/SWAA2026090956952), Sep 5, 2026: BULB. INOPERATIVE. CEILING LIGHTS OUT ABOVE ROWS 2 3 4 5 D SIDE. 2 BULBS BURNED OUT.
- [SDR SWAA2026082431110](https://openairdocs.org/sdr/SWAA2026082431110), Aug 18, 2026: SEAT TRACK. WORN. CAPT'S INBD AFT SEAT TRACK WORN BEYOND LIMITS. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 25-11-11-400-801.
- [SDR SWAA2026082414256](https://openairdocs.org/sdr/SWAA2026082414256), Aug 18, 2026: BATTERY PACK. NO TEST. FWD LT EMERGENCY BATTERY PACK M1675 FAILED CAPACITY CHECK. R & R CABIN EMERGENCY BATTERY PACK IAW AMM 56-51-06.
- [SDR SWAA2026082425311](https://openairdocs.org/sdr/SWAA2026082425311), Aug 18, 2026: BATTERY PACK. NO TEST. AFT RT EMERGENCY BATTERY PACK M1672 FAILED CAPACITY CHECK. R & R CABIN EMERGENCY BATTERY PACK PER AMM 56-51-06 C/W INSPECTION
- [SDR SWAA2026082473215](https://openairdocs.org/sdr/SWAA2026082473215), Aug 18, 2026: SEAT TRACK. WORN. F/O'S IB AFT SEAT TRACK WORN BEYOND LIMITS. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 25-11-11-400-801.
- [SDR SWAA2026082439972](https://openairdocs.org/sdr/SWAA2026082439972), Aug 18, 2026: BATTERY PACK. NO TEST. 20 ABC EMERGENCY BATTERY PACK M1670 FAILED CAPACITY CHECK. R & R CABIN EMERGENCY BATTERY PACK IAW AMM 56-51-06.
- [SDR SWAA2026050494197](https://openairdocs.org/sdr/SWAA2026050494197), Apr 30, 2026: BULB. INOPERATIVE. EMERGENCY LIGHTS ABOVE ROW 5DEF AND 20ABC INOP. REMOVED AND REPLACED EMERGENCY AREA LIGHT BULB ABOVE ROW 5DEF AND 20ABC REF 737 AMM 33-51-03 OPS CHECK GOOD
- [SDR SWAA2025122955937](https://openairdocs.org/sdr/SWAA2025122955937), Dec 27, 2025: SLIDE. LOOSE. L1 SLIDE UNSECURED FROM DOOR/HOUSING. RESECURED L1 SLIDE ASY IAW AMM 25-66-01. OK TO CONTINUE SERVICE.
- [SDR SWAA2025052875048](https://openairdocs.org/sdr/SWAA2025052875048), May 25, 2025: LIGHT. INOPERATIVE. EXIT SIGN ON DOOR R1 WILL NOT STAY ATTACHED<[01] REMOVED AND REPLACED EMERGENCY LIGHT HOUSING ASSY REF AMM 33-51-01
- [SDR SWAA2025042326624](https://openairdocs.org/sdr/SWAA2025042326624), Apr 21, 2025: LIGHT. INOPERATIVE. R2 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. <[01] RELAMPED R2 DOOR EXTERIOR EMERGENCY LIGHT IAW AMM 33-51-04.
- [SDR SWAA2025042126118](https://openairdocs.org/sdr/SWAA2025042126118), Apr 17, 2025: ENGINE. SMOKE. #2 ENG OVERTEMP AT APPPROX 700FT. HEARD POPPING SOUND. RAN QRC/QRH ENGINE SEIZURE DUNE TO HIGH VIBRATION. LANDED AIRCRAFT. F/AS REPORTED BURNT SMELL IN CABIN. E
- [SDR SWAA2025021394775](https://openairdocs.org/sdr/SWAA2025021394775), Feb 11, 2025: SEAL. CRACKED. TAIL LH HORIZONTAL STABILIZER UPPER FRONT SPAR SLIDING SEAL IS CRACKED.<[01] 01 - REMOVED AND REPLACED PER [AMM 53-31-31-400-802-NG (STABILIZER-TO-BODY UPPER FR
- [SDR SWAA2025021194926](https://openairdocs.org/sdr/SWAA2025021194926), Feb 10, 2025: STRAP. DETACHED. CREW REPORTS AFT FLASHLIGHT STRAP NOT ATTACHED CORRECTLY<[01] INSTALLED SCREW FOR FLASHLIGHT STRAP PER SIP
- [SDR SWAA2025010783530](https://openairdocs.org/sdr/SWAA2025010783530), Jan 7, 2025: LIGHT. MISSING. PAX CABIN FWD SERVICE DOOR AREA ;EXIT LIGHT LENS WITH MISSING ARROW. 2024-763844<[01] REPLACED EXIT LIGHT ASSY FWD SERVICE DOOR I.A.W B737-700 AMM 33-51-01-960-
- [SDR SWAA2025010878802](https://openairdocs.org/sdr/SWAA2025010878802), Dec 18, 2024: WEB. CRACKED. CRACK WEB LOCATED BTW LBL6.13 TO LBL31.83 AT BS663 ON VAPOR BARRIER LT SIDE MAIN WHEEL WELL 2024-763790<[01] REPLACED WEB LOCATED BTW LBL6.13 TO LBL31.83 AT BS6
- [SDR SWAA2025010877818](https://openairdocs.org/sdr/SWAA2025010877818), Dec 15, 2024: SUPPORT. CORRODED. CORROSION SUPPORT ZEE LBL21 BETWEEN BS 727D TO BS 727E AT AFT CARGO COMPARTMENT 2024-763757<[01] TOOL USED ON STEP 3 UT EQUIPMENT. P/N: 45MG; S/N: 232017609; CA
- [SDR SWAA2025010877819](https://openairdocs.org/sdr/SWAA2025010877819), Dec 15, 2024: SUPPORT. CORRODED. CORROSION SUPPORT ZEE LBL 21 BETWEEN BS 747 TO BS 767 AT AFT CARGO COMPARTMENT 2024-763758<[01] TOOL USED ON STEP 3 UT EQUIPMENT. P/N: 45MG; S/N: 232017609; CAL
- [SDR SWAA2025010777820](https://openairdocs.org/sdr/SWAA2025010777820), Dec 15, 2024: SUPPORT. CORRODED. CORROSION SUPPORT ZEE RBL 21 BETWEEN BS 727C TO BS 727D AT AFT CARGO COMPARTMENT. FAULT RESOLVED ON OTHER FAULT.
- [SDR SWAA2025010777821](https://openairdocs.org/sdr/SWAA2025010777821), Dec 15, 2024: SUPPORT. CORRODED. CORROSION SUPPORT ZEE RBL 21 BETWEEN BS 727D TO BS727E AT AFT CARGO COMPARTMENT 2024- 763760<[01] ON STEP 3: FAULT RESOLVED ON OTHER FAULT.
- [SDR SWAA2025010777816](https://openairdocs.org/sdr/SWAA2025010777816), Dec 15, 2024: ACCESS DOOR. DAMAGED. ELONGATED HOLES ON GROUND SERVICE ACCESS DOOR 114AR LOWER FUSELAGE 2024-763752<[01] REPLACED GROUND SERVICE ACCESS DOOR 114AR LOWER FUSELAGE IAW B737-700 AMM 52
- [SDR SWAA2025010877420](https://openairdocs.org/sdr/SWAA2025010877420), Dec 14, 2024: GUSSET. CRACKED. CRACK GUSSET BS 500D AND STRINGER 19R AT FWD CARGO COMPARTMENT 2024-763726<[01] REPLACED GUSSET LOCATED BS 500D AND STRINGER 19R AT FWD CARGO COMPARTMENT IAW B7
- [SDR SWAA2025010877422](https://openairdocs.org/sdr/SWAA2025010877422), Dec 14, 2024: GUSSET. CRACKED. CRACK GUSSET BS 500D AND STRINGER 19L AT FWD CARGO COMPARTMENT 2024-763729<[01] REPLACED GUSSET LOC. BS 500D AND STRINGER 19L AT FWD CARGO COMPARTMENT IAW B737-
- [SDR SWAA2025010877602](https://openairdocs.org/sdr/SWAA2025010877602), Dec 14, 2024: SUPPORT ANGLE. CRACKED. CRACK SUPPORT ANGLE BS 867 AND STRINGER 26L AT AFT CARGO COMPARTMENT 2024-763734<[01] REPLACED SUPPORT ANGLE BS 867 AND STRINGER 26L AT AFT CARGO COMPARTMENT IA
- [SDR SWAA2025010877419](https://openairdocs.org/sdr/SWAA2025010877419), Dec 14, 2024: SUPPORT ANGLE. CRACKED. CRACK SUPPORT ANGLE BS 867 BETWEEN STRINGER 2R TO STRINGER 3R AT PASSENGER CABIN 2024-763721<[01] REPLACED ANGLE AND FASTENERS LOCATED BS 867 BETWEEN STRINGER 2
- [SDR SWAA2025010877421](https://openairdocs.org/sdr/SWAA2025010877421), Dec 14, 2024: ANGLE. CRACKED. CRACK ANGLE - CLIP BS 400 AND STRINGER 26L FWD CARGO COMPARTMENT 2024-763727<[01] REPLACED ANGLE - CLIP BS 400 AND STRINGER 26L FWD CARGO COMPARTMENT IAW B737-7
- [SDR SWAA2025010877600](https://openairdocs.org/sdr/SWAA2025010877600), Dec 14, 2024: SUPPORT BRACKET. CRACKED. CRACK SUPPORT BRACKET BS 947.5 AND STRINGER 26L AT AFT CARGO COMPARTMENT 2024-763732<[01] REPLACED SUPPORT BRACKET BS 947.5 AND STRINGER 26L AT AFT CARGO COMPAR
- [SDR SWAA2025010877601](https://openairdocs.org/sdr/SWAA2025010877601), Dec 14, 2024: SUPPORT BRACKET. CRACKED. CRACK SUPPORT ANGLE BETWEEN BS 907 TO BS 927 STRINGER 25R AND STRINGER 27R AT AFT CARGO COMPARTMENT 2024-763733<[01] TOOL USED DIGITAL CALIPER P/N:500-196-30; S
- [SDR SWAA2025010777604](https://openairdocs.org/sdr/SWAA2025010777604), Dec 14, 2024: SUPPORT. CORRODED. CORROSION SUPPORT ZEE LBL 21 BETWEEN BS 727B TO BS 807 AT AFT CARGO COMPARTMENT. REPLACED SUPPORT ZEE LBL 21 BETWEEN BS 727 TO BS 847 AT AFT CARGO COMPARTMENT I
- [SDR SWAA2025010777599](https://openairdocs.org/sdr/SWAA2025010777599), Dec 14, 2024: SUPPORT. CORRODED. CORROSION SUPPORT ZEE RBL 21 BETWEEN BS 727C TO BS 767 AT AFT CARGO COMPARTMENT. REPLACED SUPPORT ZEE RBL 21 BETWEEN BS 727 TO BS 767 AT AFT CARGO COMPARTMENT I
- [SDR SWAA2025010777603](https://openairdocs.org/sdr/SWAA2025010777603), Dec 14, 2024: SUPPORT BRACKET. CRACKED. CRACK SUPPORT BRACKET AFT FACE BULKHEAD BS 727 LEVEL STRINGER 27R AT AFT CARGO COMPARTMENT 2024-763735<[01] REPLACED SUPPORT BRACKET LOC. AFT FACE BULKHEAD BS 7
- [SDR SWAA2025010876593](https://openairdocs.org/sdr/SWAA2025010876593), Dec 12, 2024: FLOORBEAM. CRACKED. CRACK BRAKE PANEL FLOOR STRUCTURE BS 540 BETWEEN BL 0 TO RBL 24.75 AT PASSENGER CABIN 2024-763639<[01] REPLACED BRAKE PANEL LOCATED FLOOR STRUCTURE BS 540 BETWE
- [SDR SWAA2025010876594](https://openairdocs.org/sdr/SWAA2025010876594), Dec 12, 2024: FLOORBEAM. CRACKED. CRACK BRAKE PANEL FLOOR STRUCTURE BS 540 BETWEEN BL 0 TO LBL 24.75 AT PASSENGER CABIN 2024-763640<[01] REPLACED BRAKE PANEL FLOOR STRUCTURE BS 540 BETWEEN BL 0 
- [SDR SWAA2025010876595](https://openairdocs.org/sdr/SWAA2025010876595), Dec 12, 2024: FLOOR SUPPORT. CRACKED. CRACK LOWER SUPPORT ANGLE FLOOR STRUCTURE BS 695 AND RBL 24.75 AT CENTER SECTION 2024-763641<[01] TOOL USED: TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 14281
- [SDR SWAA2025010776856](https://openairdocs.org/sdr/SWAA2025010776856), Dec 12, 2024: SEAL. CRACKED. CRACK SEAL - PLATE ACCESS PANEL 333AB AT LT HORIZONTAL STAB 2024-763646<[01] REPLACED SEAL - PLATE LOC. ACCESS PANEL 333AB AT LT HORIZONTAL STAB IAW B737-700 SR
- [SDR SWAA2025010876407](https://openairdocs.org/sdr/SWAA2025010876407), Dec 11, 2024: SCUFF PLATE. CRACKED. CRACK FWD CORNER SCUFF PLATE AT FWD CARGO COMPARTMENT 2024-763622<[01] TOOL USED DIGITAL CALIPER P/N: 500-196-30 S/N: B23399190; DUE DATE: 04-MAR-25.;[02] EQUIP
- [SDR SWAA2025010775977](https://openairdocs.org/sdr/SWAA2025010775977), Dec 11, 2024: DOUBLER. CRACKED. CRACK LOCATED ON EGPR SURROUND DOUBLER 2024-763604<[01] STEP 6. EDDY CURRENT EQUIPMENT USED P/N: NORTEC 600D; S/N: 210138103 AND DUE DATE: 10-JUN-25;[02] PERFOR
- [SDR SWAA2025010875958](https://openairdocs.org/sdr/SWAA2025010875958), Dec 10, 2024: SCUFF PLATE. CRACKED. CRACK FWD CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT 2024-763537<[01] TOOL USED DIGITAL CALIPER P/N: 500-196-30 S/N: B23399190; DUE DATE: 04-MAR-25.;[02] EQUIP
- [SDR SWAA2025010875959](https://openairdocs.org/sdr/SWAA2025010875959), Dec 10, 2024: SCUFF PLATE. CRACKED. CRACK AFT CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT 2024-763540<[01] TOOL USED DIGITAL CALIPER P/N: 500-196-30 S/N: B23399190; DUE DATE: 04-MAR-25.;[02] TOOL 
- [SDR SWAA2025010775957](https://openairdocs.org/sdr/SWAA2025010775957), Dec 10, 2024: SCUFF PLATE. CRACKED. CRACK CENTER SCUFF PLATE AT AFT CARGO COMPARTMENT 2024-763535<[01] EQUIPMENT P/N XRP-3000; S/N 1998072; DUE DATE 23-JAN-25 WAS USED ON STEP 4;[02] REPAIRED CENT
- [SDR SWAA2025010775324](https://openairdocs.org/sdr/SWAA2025010775324), Dec 9, 2024: FLOOR PANEL. CRACKED. CRACK FLOOR PANEL 120BF AT FWD CARGO COMPARTMENT. FABRICATED FLOOR PANEL 120BF AT FWD CARGO COMPARTMENT. I.A.W. B737-700 AMM 25-52-01-201-801. STEP 1.F. AND DRA
- [SDR SWAA2025010775321](https://openairdocs.org/sdr/SWAA2025010775321), Dec 9, 2024: VAPOR BARRIER. CRACKED. CRACK ON VAPOR BARRIER LOCATED BS663.75 LBL 34 APROX. MAIN WHEEL WELL 2024-763426<[01] REPLACED VAPOR BARRIER LOC. BS 663 BTW LBL5 TO LBL75 MAIN WHEEL WELL IAW 
- [SDR SWAA2025010775325](https://openairdocs.org/sdr/SWAA2025010775325), Dec 9, 2024: VAPOR BARRIER. CRACKED. CRACK ON VAPOR BARRIER LOCATED BS663.75 RBL 34 APROX. MAIN WHEEL WELL 2024-763446<[01] TOOL USED ON STEP 11. ULTRASONIC FLAW DETECTOR P/N: EPOCH 650; S/N: 19098
- [SDR SWAA2025010775413](https://openairdocs.org/sdr/SWAA2025010775413), Dec 9, 2024: LIGHT. DETERIORATED. DETERIORATED PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING LT SIDE AT PASSENGER CABIN (10 EA) 2024-763449<[01] REPLACED PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING LT
- [SDR SWAA2025010775412](https://openairdocs.org/sdr/SWAA2025010775412), Dec 9, 2024: LIGHT. DETERIORATED. DETERIORATED PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING RT SIDE AT PASSENGER CABIN (10 EA) 2024-763453<[01] REPLACED PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING RT
- [SDR SWAA2024090633518](https://openairdocs.org/sdr/SWAA2024090633518), Sep 3, 2024: BATTERY PACK. INOPERATIVE. EMERGENCY LIGHTS AT RT EMERGENCY DOOR EXIT INOP<[01] R/R BATTERY PACK M1669 IAW AMM 33-51-06.
- [SDR SWAA2024032868486](https://openairdocs.org/sdr/SWAA2024032868486), Mar 28, 2024: LIGHT. INOPERATIVE. EXTERIOR EMERGENCY LIGHT BESIDE AFT SVC DOOR WILL NOT ILLUMINATE.<[01] RELAMPED PER AMM 33-51-00.
- [SDR SWAA2024020950613](https://openairdocs.org/sdr/SWAA2024020950613), Feb 9, 2024: GIRT BAR. LOOSE. FWD GALLEY DOORGIRT BAR LOOSE.EASILY FALLS OFFDOOR WHEN STOWED IN BRACKETS ON GROUND<[01] ADJUSTED GIRT BAR RETAINER CLEAT PER AMM 25-66-01 AND SIP
- [SDR SWAA2024012343279](https://openairdocs.org/sdr/SWAA2024012343279), Jan 21, 2024: BATTERY PACK. INOPERATIVE. FORWARD ENTRY AND GALLEY EMERGENCY LIGHTS INOP.<[01] R/R CHARGER ASSEMBLY AND BATTERY PACK PER AMM 33-51-06.;[02] LOCATION M1674.
- [SDR SWAA2023091400346](https://openairdocs.org/sdr/SWAA2023091400346), Sep 14, 2023: SEAL. CRACKED. R/H HORIZONTAL STABILIZER FWD UPPER SLIDING SEAL CRACKED<[01] R&R R/H HORIZONTAL STABILIZER FWD UPPER SLIDING SEAL. IAW AMM 53-31-31
- [SDR SWAA2023091400347](https://openairdocs.org/sdr/SWAA2023091400347), Sep 14, 2023: SEAL. CRACKED. L/H HORIZONTAL STABILIZER FWD UPPER SLIDING SEAL CRACKED<[01] R&R L/H HORIZONTAL STABILIZER FWD UPPER SLIDING SEAL IAW AMM 53-31-31.

All 183: https://openairdocs.org/aircraft/N7724A/reports.md

## STCs that may be installed (OpenAirDocs) (2)

Approved for this aircraft's airframe or engine model, in force first, then newest. The registry doesn't record which STCs an aircraft has; its records do.

### Approved for the engine (CFM International CFM56-7B24 series)

- [STC SE04840NY](https://openairdocs.org/stc/SE04840NY): Installation of HarcoSemco Exhaust Gas Temperature (EGT) Electrical Harnesses in CFM56-7 engine. Kilroy Aviation LLC
- [STC SE03036CH](https://openairdocs.org/stc/SE03036CH): Application of a deep compressive stress layer using a Low Plasticity Burnishing (LPB) process on CFM56-7 Series Engines Stage 1 High Pressure Compressor (HPC) Blade Dovetails in accordance with Delta Air Lines Inc. Drawing No. 72-0396, Revision B, dated November 3, 2011, or later FAA Approved revision. Delta Air Lines Inc

## Earlier aircraft with N7724A

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N7724A before.

- [Cancelled 1970-05-11](https://openairdocs.org/deregistered/N7724A-1970-05-11): Cessna 180, S/N 32621. Exported to Canada. Owner: [Northern Light Gospel Missions](https://openairdocs.org/faa-owner/NORTHERN%20LIGHT%20GOSPEL%20MISSIONS), [Loman, MN](https://openairdocs.org/faa-place/MN/Loman)

## Related

- Other Boeing 737-7BD aircraft: https://openairdocs.org/model/boeing-737-7bd/aircraft.md
- The CFM International CFM56-7B24 series engine: https://openairdocs.org/engine/cfm-international-cfm56-7b24-series.md

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