# N7732A: 2006 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 CFM56-7B22 series](https://openairdocs.org/engine/cfm-international-cfm56-7b22-series) (registry code 13043)
- Serial number: 34861
- Year built: 2006
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: July 16, 2012
- Certificate issued: July 23, 2012
- Expires: July 31, 2028
- Mode S code: AA76CB
- 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=7732A
- Page: https://openairdocs.org/aircraft/N7732A

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 CFM56-7B22 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 CFM56-7B22 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

None matched to N7732A.

## FAA accident and incident reports

None matched to N7732A.

## Service difficulty reports (264, 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 SWAA2026100529585](https://openairdocs.org/sdr/SWAA2026100529585), Sep 29, 2026: SKIN. DAMAGED. BIRD STRIKE, NR 2 ENGINE INLET, CLEANED AND PERFORMED A CONDITIONAL INSPECTION IAW AMM 05-51-18.
- [SDR SWAA2026091661201](https://openairdocs.org/sdr/SWAA2026091661201), Sep 12, 2026: FIRE WARNING. NO TEST. DURING FIRE WARNING TEST, NO FIRE BELL SOUNDED AND MAIN FIRE WARNING CUTOUT LIGHTS ON CAPT AND FO SIDE FAILED TO ILLUMINATE. DURING FIRE WARNING TEST NO FIRE BE
- [SDR SWAA2026081764202](https://openairdocs.org/sdr/SWAA2026081764202), Aug 10, 2026: SIGN. LOOSE. CABIN CENTER EXIT SIGN LOOSE. INSTALLED SECURED EXIT SIGN CENTER CABIN IAW SOPM 20-50-01, REV 40.
- [SDR SWAA2026081478820](https://openairdocs.org/sdr/SWAA2026081478820), Aug 7, 2026: SEAL. DETERIORATED. DETERIORATED SEAL ON ACCESS PANEL 324ADR AT VERTICAL STABILIZER. REPLACED SEAL PANEL 324ADR AT VERTICAL STABILIZER IAW SRM 51-10-02, ITEM 9, & AMM 55-05-02-211-
- [SDR SWAA2026081204933](https://openairdocs.org/sdr/SWAA2026081204933), Jul 17, 2026: TIE CLIP. CRACKED. CRACKED TIE CLIP, BS 360, STR 8R IN THE PAX CABIN. REPLACED THE TIE CLIP AND FASTENERS IAW SRM 51-10-02, ITEM 9, SRM 51-40-02 AND DWG 140A9111, SHT 69, REV C.
- [SDR SWAA2026081212781](https://openairdocs.org/sdr/SWAA2026081212781), Jul 16, 2026: ACCESS PANEL. CRACKED. CRACKED ACCESS PANEL 542CR, LT WING. REPLACED AND INSTALLED THE ACCESS PANEL 542CR, DOCUMENT ON TTG8Q01CPSAM.
- [SDR SWAA2026081292571](https://openairdocs.org/sdr/SWAA2026081292571), Jul 16, 2026: ACCESS PANEL. CRACKED. CRACK ON ACCESS PANEL 542CL LT WING. REPLACED AND INSTALLED ACCESS PANEL 542CL LT WING IS DOCUMENT ON TTG8Q01CPSAM.
- [SDR SWAA2026081294700](https://openairdocs.org/sdr/SWAA2026081294700), Jul 13, 2026: SUPPORT ANGLE. CRACKED. CRACK SUPPORT ANGLE LOCATED BETWEEN BS 344 - 360, RBL 5 EQUIPMENT/ELECTRONIC COMPARTMENT. REPLACED THE SUPPORT ANGLE IAW SRM 51-40-02 & SRM 51-10-02, ITEM 9.
- [SDR SWAA2026081224942](https://openairdocs.org/sdr/SWAA2026081224942), Jul 12, 2026: THRUST REVERSER. DELAMINATED. DELAMINATED OTBD THRUST REVERSER, AFT LOWER AREA, NR 1 ENGINE. REPAIRED THE OTBD THRUST REVERSER IAW SRM 51-70-05-2R-1, REPAIR 1.
- [SDR SWAA2026081253425](https://openairdocs.org/sdr/SWAA2026081253425), Jul 12, 2026: ANGLE. CRACKED. CRACKED SEAL PLATE, ACCESS PANEL 333AT ANGLE, LT HORIZONTAL STAB. REPLACED THE SEAL PLATE ANGLE IAW SRM 51-10-02, ITEM 9, & SRM 51-40-02.
- [SDR SWAA2026081297463](https://openairdocs.org/sdr/SWAA2026081297463), Jul 11, 2026: CHANNEL. CORRODED. CORRODED ZEE CHANEL SIDEPLATE, BS 767 - 794.3, S25R IN THE AFT CARGO BAY. REPLACED THE ZEE CHANEL SIDEPLATE AND FASTENERS IAW SRM 51-40-02, SRM 51-10-02, ITEM 9
- [SDR SWAA2026081220315](https://openairdocs.org/sdr/SWAA2026081220315), Jul 11, 2026: SUPPORT. CORRODED. CORRODED SUPPORT ZEE, BS 727B - 807, STRINGER 25L IN THE AFT CARGO BAY. REPLACED THE SUPPORT ZEE & FASTENERS LOCATED BTWN BS 727 - 847, S25L IAW SRM 51-10-02, I
- [SDR SWAA2026081277334](https://openairdocs.org/sdr/SWAA2026081277334), Jul 11, 2026: SUPPORT ANGLE. CORRODED. CORRODED SUPPORT ZEE, AFT CARGO BAY BTWN BS 727B - 767, STR 25R BILGE AREA. REPLACED SUPPORT ZEE BTWN BS 727 - 767, RBL 21, WL 156 IAW SRM 51-40-02, SRM 51-10-0
- [SDR SWAA2026081265493](https://openairdocs.org/sdr/SWAA2026081265493), Jul 10, 2026: CROSSBEAM. CRACKED. CRACKED BRAKE PANEL BS 540 BTW BL 0 TO LBL 24.75. REPLACED THE BRAKE PANEL IAW SRM 51-40-02, AND DWG 143A5240, SHEET 14, REV-.
- [SDR SWAA2026081286183](https://openairdocs.org/sdr/SWAA2026081286183), Jul 10, 2026: SUPPORT ANGLE. CRACKED. CRACKED SUPPORT ANGLE, BS 500D, STR 28R IN THE FWD CARGO BAY. REPLACED THE SUPPORT ANGLE IAW SRM 51-10-02, ITEM 9, AND DWG 143A7902, SHT 126, REV A.
- [SDR SWAA2026081201198](https://openairdocs.org/sdr/SWAA2026081201198), Jul 10, 2026: STRUCTURE. CRACKED. CRACK ON THE LT WING ACCESS PANEL 542BB INTERNAL CAVITY. REPAIRED THE ACCESS PANEL INTERNAL CAVITY ON THE LT WING IAW M-21-157-01063.
- [SDR SWAA2026081266013](https://openairdocs.org/sdr/SWAA2026081266013), Jul 9, 2026: ACCESS PANEL. DELAMINATED. DELAMINATED ACCESS PANEL 194FL, LOWER BELLY FAIRING. REPAIRED THE ACCESS PANEL IAW SRM 51-70-05-2R-2, REPAIR 2.
- [SDR SWAA2026081272883](https://openairdocs.org/sdr/SWAA2026081272883), Jul 9, 2026: RING. CORRODED. CORROSION ON RING, FUEL TANK ACCESS PANEL 632HB, RT WING. REPLACED THE RING ON THE FUEL TANK ACCESS PANEL IAW SRM 51-10-02, ITEM 9.
- [SDR SWAA2026081282730](https://openairdocs.org/sdr/SWAA2026081282730), Jul 9, 2026: SUPPORT ANGLE. CRACKED. CRACKED SUPPORT ANGLE, BS 500D, STR 28L IN THE FWD CARGO BAY. REPLACED THE SUPPORT ANGLE IAW SRM 51-10-02, ITEM 9, & DWG 143A7902, SHT 126, REV A.
- [SDR SWAA2026081243890](https://openairdocs.org/sdr/SWAA2026081243890), Jul 8, 2026: ACCESS PANEL. DAMAGED. ELONGATED HOLE ACCESS PANEL 561BB AT LT WING. REPAIRED THE ACCESS PANEL IAW SRM 51-70-04-2R-10, REPAIR 10.
- [SDR SWAA2026081230020](https://openairdocs.org/sdr/SWAA2026081230020), Jul 8, 2026: ACCESS PANEL. ELONGATED. ELONGATED HOLE ACCESS PANEL 661BB AT RT WING 2026-411954 STEP 11. REPAIRED ACCESS PANEL 661BB AT RT WING IAW SRM 51-70-04-2R-10 REPAIR 10.
- [SDR SWAA2026081247759](https://openairdocs.org/sdr/SWAA2026081247759), Jul 7, 2026: STRAP. CRACKED. CRACK INDICATION FOUND AROUND OPEN FASTENER HOLE, AFT POSITION AT STUB BEAM STRAPS, BS 639, RBL 45.57. CRACK DIRECTION 3 O`CLOCK LOOKING FWD FROM INBD FACE. REP
- [SDR SWAA2026081273592](https://openairdocs.org/sdr/SWAA2026081273592), Jul 7, 2026: FRAME. CRACKED. CRACKED FRAME, BS 440, STR 8L - 9L. REPAIRED THE FRAME IAW EA 26-153-01892-WIP1, EA 26-153-01892-WIP2, & EA 26-153-01892.
- [SDR SWAA2026081282516](https://openairdocs.org/sdr/SWAA2026081282516), Jul 7, 2026: FRAME. CRACKED. CRACKED FRAME, BS 360, STR 8R - 9R. REPAIRED THE FRAME IAW EA 26-153-01890-WIP1, EA 26-153-01890-WIP2, AND EA 26-153-01890.
- [SDR SWAA2026081281556](https://openairdocs.org/sdr/SWAA2026081281556), Jul 7, 2026: FRAME. CRACKED. CRACKED FRAME, BS 400, STR 8R - 9R. REPAIRED THE FRAME IAW EA 26-153-01891-WIP1, EA 26-153-01891-WIP2, EA 26-153-01891-WIP3, AND EA 26-153-01891.
- [SDR SWAA2026081285510](https://openairdocs.org/sdr/SWAA2026081285510), Jul 6, 2026: ANGLE. CRACKED. CRACKED ANGLE FLOOR STRUCTURE BS 695 & BL 0 IN THE PAX CABIN. REPLACED ANGLE FLOOR STRUCTURE BS 695, BL 0 IAW SRM 51-40-02, SRM 51-10-02, ITEM 9,& DWG 273A9110,
- [SDR SWAA2026081202758](https://openairdocs.org/sdr/SWAA2026081202758), Jul 6, 2026: SCUFF PLATE. CRACKED. CRACK ON CENTER SCUFF PLATE OF FWD SERVICE DOOR AT FWD AREA GALLEY. REPAIRED THE CENTER SCUFF PLATE OF FWD SERVICE DOOR AT FWD AREA GALLEY IAW SRM 53-10-15-2R-2
- [SDR SWAA2026081204757](https://openairdocs.org/sdr/SWAA2026081204757), Jul 5, 2026: ANGLE. CRACKED. CRACKED ANGLE, BS 400, STR 26L IN THE FWD CARGO BAY. REPLACED THE ANGLE IAW SRM 51-40-02, AND DWG 143A7505, SHEET 81, REV-.
- [SDR SWAA2026081285768](https://openairdocs.org/sdr/SWAA2026081285768), Jul 5, 2026: STIFFENER. CRACKED. CRACKED STIFFENER ON FWD SIDE OF THE BULKHEAD BS 540, LBL 25 IN THE FWD CARGO BAY. REPLACED THE STIFFENER AND FASTENERS IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, 
- [SDR SWAA2026081293681](https://openairdocs.org/sdr/SWAA2026081293681), Jul 5, 2026: GUSSET. CRACKED. CRACKED GUSSET ANGLE, BS 500D, STR 19R IN THE FWD CARGO BAY. REPLACED THE GUSSET AND FASTENERS IAW SRM 51-40-02, 51-10-02, ITEM 9, & DWG 143A7902, SHT 174, REV-
- [SDR SWAA2026081210055](https://openairdocs.org/sdr/SWAA2026081210055), Jul 5, 2026: GUSSET. CRACKED. CRACK GUSSET ANGLE LOCATED BS 500D AT LEVEL STR 19L AT FWD CARGO BAY. REPLACED THE GUSSET AND FASTENERS IAW SRM 51-40-02, 51-10-02, ITEM 9, AND DWG 143A7902, SH
- [SDR SWAA2026081239428](https://openairdocs.org/sdr/SWAA2026081239428), Jul 4, 2026: PRESSURE DECK. CRACKED. CRACK INDICATION ON HORIZONTAL PRESSURE DECK WEB, RBL 42, BS 663 - 675 IN MAIN WHEEL WELL. REPAIRED THE PRESSURE DECK WEB IAW SRM 53-40-51-2R-2 REPAIR 2.
- [SDR SWAA2026081262575](https://openairdocs.org/sdr/SWAA2026081262575), Jul 3, 2026: SCUFF PLATE. CRACKED. CRACKED FWD CORNER SCUFF PLATE, AFT CARGO BAY. REPAIRED THE FWD CORNER SCUFF PLATE IAW SRM 53-60-15-2R-1, REPAIR 1, & BAC 5975.
- [SDR SWAA2026052605816](https://openairdocs.org/sdr/SWAA2026052605816), May 23, 2026: OIL SYSTEM. LEAKING. OIL QTY LO ON THE #2 ENGINE CAME ON AT FL360. OIL QUANTITY ON THE NR 2 ENGINE DECREASED TO ZERO DURING OUR DECENT INTO KRIC. OIL TEMP REMAINED BETWEEN 115 DEGRE
- [SDR SWAA2026022071817](https://openairdocs.org/sdr/SWAA2026022071817), Feb 18, 2026: SEAT BACK. OUT OF ADJUST. EMERGENCY EXIT ROW SEAT RECLINE NOT LOCKED OUT AT SEAT 14F. REPAIRED IAW AMM 25-22-00-710-803-NG.
- [SDR SWAA2025060276065](https://openairdocs.org/sdr/SWAA2025060276065), May 29, 2025: HANDLE. LOOSE. FWD ENTRY DOOR UPPER ASSIST HANDLE LOOSE. <[01] RE SECURED FWD ENTRY DOOR UPPER ASSIST HANDLE REF AMM 20-50-11.
- [SDR SWAA2024102351835](https://openairdocs.org/sdr/SWAA2024102351835), Oct 23, 2024: MEGAPHONE. INOPERATIVE. AFT CABIN MEGAPHONE INOP<[01] REPLACED MEGAPHONE IAW AMM 25-64-00
- [SDR SWAA2024082324161](https://openairdocs.org/sdr/SWAA2024082324161), Aug 9, 2024: ACCESS PANEL. DEFORMED. DEFORMATION ACCESS PANEL 551AB LINK AT LT WING 2024-501578.<[01] REPLACED ACCESS PANEL 551AB LINK AT LT WIN IAW B737-700 SRM 51-10-02 STEP 9 AND SRM 51-40-02-0G
- [SDR SWAA2024082315300](https://openairdocs.org/sdr/SWAA2024082315300), Jul 22, 2024: BRACKET. CRACKED. CRACK ON SUPPORT BRACKET ACCESS PANEL 651FB TRAILING EDGE AT RT WING 2024-443808<[01] REPLACED SUPPORT BRACKET AND FASTENERS ON ACCESS PANEL 651FB TRAILING EDGE
- [SDR SWAA2024082315142](https://openairdocs.org/sdr/SWAA2024082315142), Jul 21, 2024: ACCESS PANEL. CRACKED. CRACK ON ACCESS PANEL 334GB ELEVATOR LT HORIZONTAL STABILIZER 2024-443804<[01] TOOL USED; CALIPER PN: 500-197-30; SN: A18229508; DUE DATE: 14/JAN/25.;[02] TOOL 
- [SDR SWAA2024082314333](https://openairdocs.org/sdr/SWAA2024082314333), Jul 18, 2024: FLOOR SUPPORT. CRACKED. AAI REPORT: PASSENGER CABIN FLOOR STRUCTURE SUPPORT HAS CRACK AT STA 540 BL O TO RBL 24.75 2024-443778<[01] REPLACED CABIN FLOOR STRUCTURE SUPPORT LOC. STA 540 
- [SDR SWAA2024082314334](https://openairdocs.org/sdr/SWAA2024082314334), Jul 18, 2024: FLOOR SUPPORT. CRACKED. AAI REPORT: PASSENGER CABIN FLOOR STRUCTURE SUPPORT HAS CRACK AT STA 540 BL 0 TO LBL 24.75. 2024-443779<[01] REPLACED CABIN FLOOR STRUCTURE SUPPORT LOC. STA 540
- [SDR SWAA2024082313794](https://openairdocs.org/sdr/SWAA2024082313794), Jul 17, 2024: BRACKET. ELONGATED. ELONGATED HOLE BRACKET ANGLE LOCATED OUTBOARD THRUST REVERSER AFT UPPER EDGE ON ENGINE 2 2024-443746<[01] REPLACED BRACKET ANGLE LOCATED OUTBOARD THRUST REVERSE
- [SDR SWAA2024082213342](https://openairdocs.org/sdr/SWAA2024082213342), Jul 16, 2024: HOUSING. BROKEN. BROKEN EXIT SIGN HOUSING ASSY ON AFT LOWERED CEILING AT AFT GALLEY AREA 2024-443723<[01] REPLACED EXIT SIGN HOUSING ASSY ON AFT LOWERED CEILING AT AFT GALLEY AR
- [SDR SWAA2024082213344](https://openairdocs.org/sdr/SWAA2024082213344), Jul 16, 2024: LENS. DAMAGED. DAMAGE PLATE NEAR EMERGENCY LIGHT LENS ON LAVATORY A AT FWD GALLEY AREA 2024-443731<[01] REPLACED PLATE NEAR EMERGENCY LIGHT LENS ON LAVATORY A AT FWD GALLEY AR
- [SDR SWAA2024082213105](https://openairdocs.org/sdr/SWAA2024082213105), Jul 16, 2024: ANGLE. CRACKED. CRACK ON ANGLE LOCATED STA663.75 AND RBL7 AT CENTER WING BOX 2024-443718<[01] TOOL USED: TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 112031023 DUE DATE 22 JAN
- [SDR SWAA2024082312925](https://openairdocs.org/sdr/SWAA2024082312925), Jul 15, 2024: SKIN. CRACKED. CRACK INDICATION FOUND ON RT HORIZONTAL STABILIZER LOWER SKIN PANEL. LOCATED AT STAB STA 193.9 RIB AND 16 INCH. FROM FRONT SPAR. INBOARD SIDE OF RIB. CRACK LENG
- [SDR SWAA2024082312186](https://openairdocs.org/sdr/SWAA2024082312186), Jul 14, 2024: PLATE. CRACKED. CRACK CORRUGATED PLATE TRAILING EDGE LOCATED AT LEVEL IRSS 214 AT RT WING 2024-443662<[01] EVALUATED CORRUGATED PLATE TRAILING EDGE LOCATED AT LEVEL IRSS 214 AT
- [SDR SWAA2024082212187](https://openairdocs.org/sdr/SWAA2024082212187), Jul 14, 2024: FRAME. CORRODED. CORROSION FRAME ON BS 303.9 LEVEL STRINGER 17L AND WL 208.1 FWD GALLEY AND LAV. REPAIRED FRAME ON BS 303.9 LEVEL STRINGER 17L AND WL 208.1 FWD GALLEY AND LAV IA
- [SDR SWAA2024082212591](https://openairdocs.org/sdr/SWAA2024082212591), Jul 14, 2024: PLATE. CRACKED. CRACK CORRUGATED PLATE TRAILING EDGE AT LEVEL IRSS 214 AT LT WING 2024-443668<[01] REPLACED CORRUGATED PLATE TRAILING EDGE AT LEVEL IRSS 214 AT LT WING IAW B737

All 264: https://openairdocs.org/aircraft/N7732A/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 CFM56-7B22 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 N7732A

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N7732A before.

- [Cancelled 1957-01-17](https://openairdocs.org/deregistered/N7732A-1957-01-17): Cessna 180, S/N 32629. Owner: [Cessna Aircraft Co](https://openairdocs.org/faa-owner/CESSNA%20AIRCRAFT%20CO), [Wichita, KS](https://openairdocs.org/faa-place/KS/Wichita)

## Related

- Other Boeing 737-7BD aircraft: https://openairdocs.org/model/boeing-737-7bd/aircraft.md
- The CFM International CFM56-7B22 series engine: https://openairdocs.org/engine/cfm-international-cfm56-7b22-series.md

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