# N7832A: 2003 Boeing 737-79P

- Status: Valid registration
- Airframe: [Boeing 737-79P](https://openairdocs.org/model/boeing-737-79p) (registry code 13844JA, 149 seats)
- Engine: [CFM International CFM56-7B24 series](https://openairdocs.org/engine/cfm-international-cfm56-7b24-series) (registry code 13044)
- Serial number: 30657
- Year built: 2003
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: October 29, 2015
- Certificate issued: December 21, 2022
- Expires: December 31, 2029
- Mode S code: AA9E4A
- 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=7832A
- Page: https://openairdocs.org/aircraft/N7832A

From the FAA registry file of October 27, 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 737-79P)

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

None matched to N7832A.

## FAA accident and incident reports

None matched to N7832A.

## Service difficulty reports (221, 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 SWAA2026081348791](https://openairdocs.org/sdr/SWAA2026081348791), Aug 12, 2026: UNKNOWN. ODOR. BURNING RUBBER ODOR IN FWD CABIN WITH GROUND AIR AND PACKS ON. ACCOMPLISHED FIM TASK 21-00 TASK 806 FOR FUMES AND ODOR IN THE CABIN. NO DEFECTS NOTED ACFT OK FO
- [SDR SWAA2026061009657](https://openairdocs.org/sdr/SWAA2026061009657), Jun 6, 2026: LAMP. INOPERATIVE. L2 SLIDE EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMPS IAW AMM 33-51-04.
- [SDR SWAA2026040886775](https://openairdocs.org/sdr/SWAA2026040886775), Apr 6, 2026: GIRT BAR. OUT OF ADJUST. FWD GALLEY GRIT BAR NOT SEATING PROPERLY IN DOOR HOLDER. REPOSITIONED GRIT IN LOWER FLAP REF AMM 25-66-01. GRIT BAR STOWS AND ARMS PROPERLY IN FLOOR MOUNTS WITH
- [SDR SWAA2026021670089](https://openairdocs.org/sdr/SWAA2026021670089), Feb 11, 2026: ENGINE. NO DISCREPANCY. 20 KNOT RTO DUE TO NR 2 ENGINE SLOW TO SPOOL. PERFORMED ACCELERATION TEST ON NR 2 ENGINE. FOUND ENGINE TO BE WITHIN LIMITS, WORK DONE IAW 71-00-00 OF THE AMM.
- [SDR SWAA2025081293720](https://openairdocs.org/sdr/SWAA2025081293720), Jul 21, 2025: FITTING. CRACKED. CRACK SERVICE DOOR FITTING LOC LOWER AFT CORNER AT FWD GALLEY AREA. REPLACED FITTING 1(E/A) AND FASTENERS LOCATED ON SERVICE DOOR LOWER AFT CORNER AT FWD GALLEY
- [SDR SWAA2025081293401](https://openairdocs.org/sdr/SWAA2025081293401), Jul 20, 2025: ANGLE. CORRODED. CORROSION ON ANGLE LOCATED BS 794.3 BETWEEN STR 22R AND STR 23R AT AFT CARGO COMPARTMENT. REPLACED ANGLE LOCATED BS 794.3 BETWEEN STR 22R AND STR 23R AT AFT CAR
- [SDR SWAA2025081292843](https://openairdocs.org/sdr/SWAA2025081292843), Jul 18, 2025: PLATE. CRACKED. CRACK ON CORRUGATED PLATE TRAILING EDGE LOCATED ORSS 241 AT LT WING. REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED ORSS 241 AT LT WING IAW SRM 51-40-02 AND DR
- [SDR SWAA2025081292846](https://openairdocs.org/sdr/SWAA2025081292846), Jul 18, 2025: PLATE. CRACKED. CRACK ON CORRUGATED PLATE TRAILING EDGE LOCATED IRSS 217 AT LT WING. REPLACED CORRUGATED PLATE LOCATED ON TRAILING EDGE IRSS 217 AT LH WING IAW SRM 51-40-02 AND
- [SDR SWAA2025081292845](https://openairdocs.org/sdr/SWAA2025081292845), Jul 18, 2025: ANGLE. CRACKED. CRACK ON ANGLE LOCATED ORSS 271 TRAILING EDGE AT LT WING. REPLACED ANGLE LOCATED ORSS 271 TRAILING EDGE AT LT WING IAW SRM 51-40-02, SRM SRM 51-10-02, ITEM 9, A
- [SDR SWAA2025081292841](https://openairdocs.org/sdr/SWAA2025081292841), Jul 18, 2025: PLATE. CRACKED. CRACK ON CORRUGATED PLATE TRAILING EDGE LOCATED ORSS 241 AT RT WING 2025-452361<[01] REPLACED CORRUGATED PLATE AND FASTENERS TRAILING EDGE LOCATED ORSS 241 AT R
- [SDR SWAA2025081292842](https://openairdocs.org/sdr/SWAA2025081292842), Jul 18, 2025: PLATE. CRACKED. CRACK ON CORRUGATED PLATE TRAILING EDGE LOCATED IRSS 217 AT RT WING. REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED IRSS 217 AT RT WING IAW SRM 51-40-02 AND DW
- [SDR SWAA2025081292837](https://openairdocs.org/sdr/SWAA2025081292837), Jul 18, 2025: SUPPORT ANGLE. BROKEN. BROKEN SUPPORT ANGLE LOCATED IRSS 212 TRAILING EDGE AT RT WING, REPLACED SUPPORT ANGLE LOCATED IRSS 212 TRAILING EDGE AT RT WING IAW SRM 51-10-02; SRM 51-40-02 
- [SDR SWAA2025081292838](https://openairdocs.org/sdr/SWAA2025081292838), Jul 18, 2025: PLATE. CORRODED. CORROSION SUPPORT PLATE LOCATED ORSS 376 INTERNAL CAVITY UPPER AREA TRAILING EDGE AT RT WING. REPLACED SUPPORT PLATE LOCATED ORSS 376 INTERNAL CAVITY UPPER AREA
- [SDR SWAA2025081292839](https://openairdocs.org/sdr/SWAA2025081292839), Jul 18, 2025: WEB. CRACKED. CRACK ON WEB TRAILING EDGE LOCATED ORSS 276 AT RT WING. REPLACED WEB TRAILING EDGE LOCATED ORSS 276 AT RT WING IAW SRM 51-40-02 AND DWG 115A2512 SHEET 5 REV. B 
- [SDR SWAA2025081292840](https://openairdocs.org/sdr/SWAA2025081292840), Jul 18, 2025: SUPPORT ANGLE. CRACKED. CRACK ON SUPPORT ANGLE INTERNAL CAVITY LOCATED ORSS 271 TRAILING EDGE AT RT WING. REPLACED SUPPORT ANGLE INTERNAL CAVITY LOCATED ORSS 271 TRAILING EDGE AT RT WI
- [SDR SWAA2025081292298](https://openairdocs.org/sdr/SWAA2025081292298), Jul 17, 2025: ACCESS PANEL. ELONGATED. ELONGATED HOLE ACCESS PANEL 561AB TRAILING EDGE AT LT WING. REPAIRED THE ACCESS PANEL 561AB TRAILING EDGE AT LT WING IAW SRM 51-70-04-2R-10, REPAIR 10.
- [SDR SWAA2025081292291](https://openairdocs.org/sdr/SWAA2025081292291), Jul 17, 2025: ANGLE. CRACKED. CRACK ANGLE ON SLAT 6 INBOARD AUXILIARY AT RT WING (1 E/A), REPLACED ANGLE LOCATED ON SLAT 6 INBOARD AUXILIARY AT RT WING IAW SRM 51-40-02 AND DWG 114A5030, SHE
- [SDR SWAA2025081292545](https://openairdocs.org/sdr/SWAA2025081292545), Jul 17, 2025: LIGHT. BROKEN. BROKEN PHOTOLUMINESCENT STRIP LH (5EA) AT PASSENGER CABIN. THE REPLACEMENT PHOTOLUMINESCENT STRIP LH (5EA) SEE TTG8Q003KHW1.
- [SDR SWAA2025081292546](https://openairdocs.org/sdr/SWAA2025081292546), Jul 17, 2025: LIGHT. BROKEN. BROKEN PHOTOLUMINESCENT STRIP RH (5EA) AT PASSENGER CABIN. THE REPLACEMENT PHOTOLUMINESCENT STRIP RH (5EA) SEE TTG8Q003KHW1.
- [SDR SWAA2025081291740](https://openairdocs.org/sdr/SWAA2025081291740), Jul 15, 2025: PRESSURE DECK. CRACKED. CRACK INDICATION ON THE HORIZONTAL PRESSURE DECK LOCATED AT BS 663 PLUS 1 INCH AND LBL 31 AT MAIN WHEEL WELL COMPARTMENT. PERFORMED PERMANENT REPAIR ON HORIZONT
- [SDR SWAA2025081291749](https://openairdocs.org/sdr/SWAA2025081291749), Jul 15, 2025: SKIN PANEL. CRACKED. CRACK INDICATION FOUND ON RT HORIZONTAL STAB LOWER SKIN PANEL. LOCATED AT STAB STA 193.9 RIB AND 7.5 INCH. FROM FRONT SPAR. INBOARD SIDE OF RIB. CRACK LENGTH = 
- [SDR SWAA2025081291747](https://openairdocs.org/sdr/SWAA2025081291747), Jul 15, 2025: SCUFF PLATE. CRACKED. CRACK ON CENTER SCUFF PLATE AT FWD CARGO COMPARTMENT. REPAIRED CENTER SCUFF PLATE AT FWD CARGO COMPARTMENT IAW SRM 53-30-15-2R-1 REPAIR 1.
- [SDR SWAA2025081291739](https://openairdocs.org/sdr/SWAA2025081291739), Jul 15, 2025: INTERCOSTAL. CRACKED. CRACKED INTERCOSTAL - WEB FLOOR STRUCTURE LOCATED BS540 AT LEVEL BL0 TO RBL24 PASSENGER CABIN. REPLACED BREAK PANEL FLOOR STRUCTURE LOCATED BS540 AT LEVEL BL0 T
- [SDR SWAA2025060276006](https://openairdocs.org/sdr/SWAA2025060276006), May 29, 2025: SEAL. CRACKED. R/H HORIZONTAL STABILIZER FWD LWR SLIDING SEAL BENT WITH HORIZONTAL CRACK EXTENDING FROM THE EDGE ALONG THE BEND AND HAS A VERTICAL CRACK APPROX. 1 INCH ALONG F
- [SDR SWAA2025051469903](https://openairdocs.org/sdr/SWAA2025051469903), May 11, 2025: PANEL. LOOSE. CAPTAIN SIDE LOWER PANEL EXIT ROW PANEL LOOSE<[01] RE-SECURED EMERGENCY EXIT DOOR STRAP PANEL PER AMM 52-22-51
- [SDR SWAA2025040922076](https://openairdocs.org/sdr/SWAA2025040922076), Apr 6, 2025: GIRT BAR. DAMAGED. PLASTIC COVER ON RIGHT FORWARD ENTRY DOOR (R1) GIRT BAR PARTIALLY BROKEN <[01]. REPLACED EVAC RELEASE STOP ON R1 GIRT BAR IN REFERENCE TO AMM 25-66-00.
- [SDR SWAA2025031104125](https://openairdocs.org/sdr/SWAA2025031104125), Mar 10, 2025: COVER. DETACHED. F/O SIDE EMERGENCY EXIT COVER FELL OFF TSR 2025001786<[01] C/W EA 25-152-00618
- [SDR SWAA2024112161264](https://openairdocs.org/sdr/SWAA2024112161264), Nov 18, 2024: SIGN. LOOSE. LENS COVER BELOW EXIT SIGN FWD GALLEY LOOSE. LIGHT INDICATE NORMALLY.<[01] SECURED LENS. OK TO CONTINUE PER MEL 25-10-01 SP1B AUTH # 223999;[02] REMOVED & REPLA
- [SDR SWAA2024101748359](https://openairdocs.org/sdr/SWAA2024101748359), Oct 14, 2024: SLIDE. DISLODGED. AFT SERVICE DOOR ESCAPE SLIDE FELL OUT OF HOUSING<[01] C/W MT 725-61-06 OF AFT SERVICE DOOR SLIDE.
- [SDR SWAA2024082628817](https://openairdocs.org/sdr/SWAA2024082628817), Aug 22, 2024: ISOLATION MOUNT. BROKEN. AFT PASSENGER DOOR FWD UPPER AND LOWER SLIDE MOUNT ISOLATORS BROKEN.<[01] R&R AFT PASSENGER DOOR FWD UPPER AND LOWER SLIDE MOUNT ISOLATORS IAW SRM 51-40-02.;[02
- [SDR SWAA2024060799020](https://openairdocs.org/sdr/SWAA2024060799020), Jun 7, 2024: LIGHT. INOPERATIVE. R1 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. R&R R1 DOOR SLIDE/OVERWING LAMP IAW AMM 33-51-04 OPS CHECK GOOD.
- [SDR SWAA2024030458537](https://openairdocs.org/sdr/SWAA2024030458537), Mar 2, 2024: SLIDE. DISLODGED. FWD ENTRY DOOR ESCAPE DOOR ESCAPE CAME OUT OF THE HOUSING<[01] COMPLIED WITH MT 725-61-06 REM/INST; A/C OK FOR SVC
- [SDR SWAA2023090595915](https://openairdocs.org/sdr/SWAA2023090595915), Sep 1, 2023: NUT. DETERIORATED. DETERIORATED SERVICE DOORWAY ASSIST HANDLE NUT AT AFT GALLEY AREA (2 EA) 2023-469812<[01] REPLACED SERVICE DOORWAY ASSIST HANDLE NUT AT AFT GALLEY AREA (2 EA) I
- [SDR SWAA2023090190358](https://openairdocs.org/sdr/SWAA2023090190358), Aug 17, 2023: STIFFENER. CRACKED. CRACK ON STIFFENER LOC. INSPAR RIB 120.30 AT 19 INCH FRONT SPAR AT RH HORIZONTAL STABILIZER 2023-470223 CORRECT FAULT DESCRIPTION: CRACK ON STIFFENER LOC. INSPA
- [SDR SWAA2023090186254](https://openairdocs.org/sdr/SWAA2023090186254), Aug 5, 2023: STRAP. CORRODED. CORROSION ON STRAP LOCATED BS 360 BTW STR 26R TO STR 27R RBL 5 WL 152 AT ELECTRONIC COMPARTMENT 2023-470200 CORRECTED LOCATION CORROSION ON STRAP LOCATED BS 360
- [SDR SWAA2023090585379](https://openairdocs.org/sdr/SWAA2023090585379), Aug 3, 2023: SUPPORT ANGLE. CRACKED. CRACK ON SUPPORT ANGLE LOCATED BS 1016 BTW STR 4L TO STR 4R INTERNAL AREA OF VERTICAL STABILIZER 2023-470167<[01] REPLACED SUPPORT ANGLE LOCATED BS 1016 BTW STR
- [SDR SWAA2023090185537](https://openairdocs.org/sdr/SWAA2023090185537), Aug 3, 2023: RIB. CRACKED. CRACK INSPAR RIB 120.30 AT 28 INCHES OF FRONT SPAR LT HORIZONTAL STAB 2023-470175<[01] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600 D; S/N: 6000916163
- [SDR SWAA2023090185536](https://openairdocs.org/sdr/SWAA2023090185536), Aug 3, 2023: RIB. CRACKED. CRACK INSPAR RIB 120.30 AT 19 INCHES OF FRONT SPAR AT RT HORIZONTAL STABILIZER 2023-470169<[01] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600 D; S/N: 6
- [SDR SWAA2023090185169](https://openairdocs.org/sdr/SWAA2023090185169), Aug 2, 2023: FRAME. CRACKED. CRACK ON FRAME LOCATED BS 727D BTW STR 8L TO STR 9L AT PASSENGER CABIN 2023-470152<[01] TOOL USED: ET EQUIPMENT; P/N: NORTEC 600D; S/N: 210138103; DUE DATE: 02-
- [SDR SWAA2023090184937](https://openairdocs.org/sdr/SWAA2023090184937), Aug 2, 2023: BRACKET. CRACKED. CRACK ON SUPPORT BRACKET LOCATED BS 867 BTW STR 2R TO STR 3R CEILING AREA AT PASSENGER CABIN 2023-470150<[01] REPLACED SUPPORT BRACKET LOCATED BS 867 BTW STR 2R
- [SDR SWAA2023090584765](https://openairdocs.org/sdr/SWAA2023090584765), Aug 1, 2023: PLATE. CORRODED. CORROSION RAIL NUT PLATE O/B FIXED LEADING EDGE OFSS 449 AT LT WING 2023-470129<[01] REPLACED RAIL NUT PLATE O/B FIXED LEADING EDGE OFSS 449 AT LT WING IAW B737
- [SDR SWAA2023090584764](https://openairdocs.org/sdr/SWAA2023090584764), Aug 1, 2023: STRINGER. CRACKED. CRACK FUEL TANK LOC. BTW RIB 21 AND RIB 22 STRINGER 9 INTERNAL AREA UPPER AFT POSITION AT RT WING 2023-470128<[01] REPAIRED STRINGER 9 INTERNAL AREA UPPER AFT P
- [SDR SWAA2023090184763](https://openairdocs.org/sdr/SWAA2023090184763), Aug 1, 2023: CARGO TRACK. CRACKED. CRACK TRACK ON BS 460 AT RBL 14 AT FWD CARGO COMPARTMENT 2023-470102<[01] TOOL USED: EDDY CURRENT EQUIPMENT; P/N: NORTEC 500D; S/N: N500X11290U021704; DUE DATE:
- [SDR SWAA2023090184594](https://openairdocs.org/sdr/SWAA2023090184594), Aug 1, 2023: STRINGER. CRACKED. CRACK STRINGER 26L LOCATED STA 540 FWD CARGO COMPARTMENT 2023-470108<[01] TOOL USED: ULTRASONIC THICKNESS GAGE. P/N: 35DL. S/N: 091419910. DUE DATE: 13-MAR-24.;
- [SDR SWAA2023090184593](https://openairdocs.org/sdr/SWAA2023090184593), Aug 1, 2023: STRINGER. CRACKED. CRACK STRINGER 25L LOCATED STA 540 FWD CARGO COMPARTMENT 2023-470107<[01] TOOL USED: ULTRASONIC THICKNESS GAGE. P/N: 35DL. S/N: 091419910. DUE DATE: 13-MAR-24.;
- [SDR SWAA2023090184592](https://openairdocs.org/sdr/SWAA2023090184592), Aug 1, 2023: STRINGER. CRACKED. CRACK STRINGER 23L LOCATED STA 540 FWD CARGO COMPARTMENT 2023-470106<[01] TOOL USED USED EDDY CURRENT FLAW DETECTOR PN: NORTEC 600D; SN: 60009161631 CAL DUE DAT
- [SDR SWAA2023090184591](https://openairdocs.org/sdr/SWAA2023090184591), Aug 1, 2023: STRINGER. CRACKED. CRACK STRINGER 26R LOCATED STA 540 FWD CARGO COMPARTMENT 2023-470105<[01] TOOL USED USED EDDY CURRENT FLAW DETECTOR PN: NORTEC 600D; SN: 60009161631 CAL DUE DAT
- [SDR SWAA2023090184590](https://openairdocs.org/sdr/SWAA2023090184590), Aug 1, 2023: STRINGER. CRACKED. CRACK STRINGER 25R LOCATED STA 540 FWD CARGO COMPARTMENT 2023-470104<[01] TOOL USED: ULTRASONIC THICKNESS GAGE. P/N: 35DL. S/N: 091419910. DUE DATE: 13-MAR-24.;
- [SDR SWAA2023090184589](https://openairdocs.org/sdr/SWAA2023090184589), Aug 1, 2023: STRINGER. CRACKED. CRACK STRINGER 23R LOCATED STA 540 FWD CARGO COMPARTMENT 2023-470103<[01] TOOL USED: ULTRASONIC THICKNESS GAGE. P/N: 35DL. S/N: 091419910. DUE DATE: 13-MAR-24.;
- [SDR SWAA2023090184586](https://openairdocs.org/sdr/SWAA2023090184586), Aug 1, 2023: STRINGER. CRACKED. CRACK ON STRINGER 7L LOCATED BTW BS 294.5 TO BS 303.9 AT FWD GALLEY AREA 2023-470098<[01] ULTRASONIC EQUIPMENT USED P/N: 38DLPLUS; S/N:120398603 AND DUE DATE: 0

All 221: https://openairdocs.org/aircraft/N7832A/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 N7832A

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N7832A before.

- [Cancelled 1957-01-08](https://openairdocs.org/deregistered/N7832A-1957-01-08): Cessna 180A, S/N 32729. Owner: [Cessna Aircraft Co](https://openairdocs.org/faa-owner/CESSNA%20AIRCRAFT%20CO), [Wichita, KS](https://openairdocs.org/faa-place/KS/Wichita)

## Related

- Other Boeing 737-79P aircraft: https://openairdocs.org/model/boeing-737-79p/aircraft.md
- The CFM International CFM56-7B24 series engine: https://openairdocs.org/engine/cfm-international-cfm56-7b24-series.md

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