# N7729A: 2006 Boeing 737-76N

- Status: Valid registration
- Airframe: [Boeing 737-76N](https://openairdocs.org/model/boeing-737-76n) (registry code 13844CH, 149 seats)
- Engine: [CFM International CFM56-7B22 series](https://openairdocs.org/engine/cfm-international-cfm56-7b22-series) (registry code 13043)
- Serial number: 32675
- Year built: 2006
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: June 13, 2006
- Certificate issued: January 8, 2022
- Expires: January 31, 2029
- Mode S code: AA7409
- 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: Individual
- 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=7729A
- Page: https://openairdocs.org/aircraft/N7729A

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 737-76N)

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 N7729A.

## FAA accident and incident reports

None matched to N7729A.

## Service difficulty reports (249, 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 SWAA2026101473546](https://openairdocs.org/sdr/SWAA2026101473546), Oct 10, 2026: GIRT BAR. OUT OF POSITION. AFT ENTRY DOOR GIRT FLAP OBSTRUCTION DOOR CLOSURE. ADJUSTED AFT ENTRY DOOR GIRT Z-FOLD TO LIFT GIRT ABOVE DOOR FRAME AND PREVENT INTERFERENCE IAW AMM 25-66-01.
- [SDR SWAA2026052705761](https://openairdocs.org/sdr/SWAA2026052705761), May 23, 2026: RIB. CRACKED. RT WING OUTBOARD AFT FLAP HAS A CRACK INDICATION ON THE INBOARD CLOSURE RIB. TOP OF. CLOSURE RIB BOTTOM PORTION. HFEC VERIFIED. REMOVED AND INSTALLED OUTBOARD T
- [SDR SWAA2026050494648](https://openairdocs.org/sdr/SWAA2026050494648), May 1, 2026: FAN. ODOR. ELECTRICAL ODOR IN FLIGHT DECK ONLY WITH ENGINES RUNNING AND APU ON. SMELL DISSIPATED AFTER SWAPPING TO EXTERNAL POWER. CABIN UTILITIES SWITCH OFF. T/S ELECTRIC
- [SDR SWAA2026042491684](https://openairdocs.org/sdr/SWAA2026042491684), Apr 22, 2026: HANDLE. LOOSE. R1 SERVICE DOOR LINER DOOR ASSIST HANDLE LOOSE. REMOVED AND REPLACED R1 DOOR LINER ASSIST HANDLE NUTS REF. AMM 52-41-31
- [SDR SWAA2026041688589](https://openairdocs.org/sdr/SWAA2026041688589), Apr 12, 2026: BULB. BURNED OUT. EMERGENCY EXIT LIGHT ABOVE AFT SERVICE DOOR HAS 1 EA BURN OUT PEANUT BULB. REPLACED BULB (1EA) ON EMERGENCY EXIT LIGHT ABOVE AFT SERVICE DOOR IAW AMM 33-51-01-9
- [SDR SWAA2026041688586](https://openairdocs.org/sdr/SWAA2026041688586), Apr 12, 2026: HANDLE. LOOSE. PAX CABIN AFT ENTRY DOOR ASSISTANT HANDLE LOOSE. INSTALLED CORRECTLY PAX CABIN AFT ENTRY DOOR ASSISTANT HANDLE IAW AMM 52-13-31-400-802 STEP 3.G.(2).
- [SDR SWAA2026041688588](https://openairdocs.org/sdr/SWAA2026041688588), Apr 12, 2026: HANDLE. LOOSE. PAX CABIN AFT RIGHT SERVICE DOOR ASSISTANT HANDLE LOOSE. INSTALLED CORRECTLY PAX CABIN AFT RIGHT SERVICE DOOR ASSISTANT HANDLE IAW AMM 52-41-31-400-802, STEP 3.
- [SDR SWAA2026041687875](https://openairdocs.org/sdr/SWAA2026041687875), Apr 9, 2026: HANDLE. MISSING. MISSING ENTRY DOORWAY LINNING LOWER HANDLE ASSY AT FWD GALLEY AREA. INSTALLED ENTRY DOORWAY LINNING LOWER HANDLE ASSY AT FWD GALLEY AREA IAW B737-700 AMM 52-11-
- [SDR SWAA2026041683113](https://openairdocs.org/sdr/SWAA2026041683113), Mar 25, 2026: LINK. CRACKED. CRACKED AFT SUPPORT LINK ON STABILIZER FWD CONTROL MECHANISM AT FWD NOSE BAY. REPLACED AFT SUPPORT LINK ON STABILIZER FWD CONTROL MECHANISM AT FWD NOSE COMPARTM
- [SDR SWAA2026041680108](https://openairdocs.org/sdr/SWAA2026041680108), Mar 15, 2026: SHEAR TIE. CORRODED. CORRODED SUPPORT ANGLE, BS 520, STR 28L - 28R IN THE FWD CARGO BAY. REPLACED THE SHEAR TIE AND FASTENERS IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, DWG 143A3230, S
- [SDR SWAA2026041680111](https://openairdocs.org/sdr/SWAA2026041680111), Mar 15, 2026: ANGLE. CORRODED. CORRODED ANGLE, BS 767 - 787, RBL 21, WL 156 IN THE AFT CARGO BAY. REPLACED ANGLE IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, & DWG 146A8123, SHEET 16, REV-.
- [SDR SWAA2026041680018](https://openairdocs.org/sdr/SWAA2026041680018), Mar 15, 2026: ANGLE. CRACKED. CRACKED ANGLE LOCATED BS500D, STR 28R FWD CARGO BAY. REPLACED THE ANGLE AND FASTENERS IAW SRM 51-10-02-0G-0 ITEM 9; SRM 51-40-02-0G-0 AND DWG 143A7902 SHEET: 12
- [SDR SWAA2026041580017](https://openairdocs.org/sdr/SWAA2026041580017), Mar 15, 2026: STRINGER. CORRODED. CORRODED STRINGER 23R LOCATED BS540 WL165 AT FWD CARGO COMPARTMENT. REPAIRED STRINGER 23R LOCATED LOCATED BETWEEN BS 500D TO BS 540 WL165 AT FWD CARGO COMPARTME
- [SDR SWAA2026041580019](https://openairdocs.org/sdr/SWAA2026041580019), Mar 15, 2026: STRINGER. CRACKED. CRACKED STRINGER 26L LOCATED BS540 FWD CARGO COMPARTMENT. PERFORMED PERMANENT REPAIR ON STRINGER SECTION 26L LOCATED BETWEEN BS 500D MORE 10 INCHES TO BS 540 AT
- [SDR SWAA2026041480109](https://openairdocs.org/sdr/SWAA2026041480109), Mar 15, 2026: SHIELD. CORRODED. CORROSION SHIELD WEB LOCATED BS767 TO BS794 RBL21 AND WL156 AT AFT CARGO COMPARTMENT. REPLACED SHIELD WEB LOCATED BS767 TO BS794 RBL21 AND WL156 AT AFT CARGO CO
- [SDR SWAA2026041579824](https://openairdocs.org/sdr/SWAA2026041579824), Mar 14, 2026: FRAME. CRACKED. CRACK FRAME ON BS 440 BTW STR 8R TO STR 9R AT PASSENGER CABIN. REPAIRED FRAME UPPER FUSELAGE AIR CONDITIONING BRACKETS AREA AT BSTA 440 AND BETWEEN S-8R AND S-9
- [SDR SWAA2026041579825](https://openairdocs.org/sdr/SWAA2026041579825), Mar 14, 2026: FRAME. CRACKED. CRACKED FRAME ON BS 440 BTW STR 8L TO STR 9L AT PASSENGER CABIN. REPAIRED FRAME UPPER FUSELAGE AIR CONDITIONING BRACKETS AREA AT BSTA 440 AND BETWEEN S-8L AND S
- [SDR SWAA2026041679621](https://openairdocs.org/sdr/SWAA2026041679621), Mar 13, 2026: ANGLE. CRACKED. CRACKED ANGLE, BS 440, STR 26L IN THE FWD CARGO BAY. REPLACED ANGLE-CLIP AND FASTENERS IAW SRM 51-10-02 ITEM 9, SRM 51-40-02, AND DWG 143A7505, SHEET 82, REV - 
- [SDR SWAA2026041679501](https://openairdocs.org/sdr/SWAA2026041679501), Mar 13, 2026: NUT PLATE. CRACKED. CRACK INTERNAL CAVITY RAIL NUT PLATE LEADING EDGE OFSS 491 AT RT WING. REPLACED THE RAIL NUT PLATE IAW SRM 51-10-02, ITEM 9, AND DWG 112A4402, REV -.
- [SDR SWAA2026041679504](https://openairdocs.org/sdr/SWAA2026041679504), Mar 13, 2026: NUT PLATE. CRACKED. CRACK INTERNAL CAVITY RAIL NUT PLATE LEADING EDGE OFSS 634 AT RT WING. REPLACED THE RAIL NUT PLATE IAW SRM 51-10-02-0G-0 ITEM 9, SRM 51-40-02, & DWG 112A4402, S
- [SDR SWAA2026041679502](https://openairdocs.org/sdr/SWAA2026041679502), Mar 13, 2026: NUT PLATE. CRACKED. CRACK INTERNAL CAVITY RAIL NUT PLATE, OFSS 286, RT WING L/E. REPLACED THE NUT PLATE IAW SRM 51-10-02, ITEM 9, AND DWG 112A4402, REV -.
- [SDR SWAA2026041679620](https://openairdocs.org/sdr/SWAA2026041679620), Mar 13, 2026: ANGLE. CRACKED. CRACKED ANGLE BS 400 AND STR 26L FWD CARGO COMPARTMENT. FAULT RESOLVED ON TTG8Q01AUG1J;[03] FAUL RESOLVED ON TTG8Q01AUG1J
- [SDR SWAA2026041579623](https://openairdocs.org/sdr/SWAA2026041579623), Mar 13, 2026: FITTING. WORN. WEAR GIRT BAR FITTING ON SERVICE DOOR AT AFT GALLEY AREA. REPLACED GIRT BAR FITTING ON SERVICE DOOR AT AFT GALLEY AREA IAW AMM 25-66-02-400-801. FOR THE INSTALL
- [SDR SWAA2026041679069](https://openairdocs.org/sdr/SWAA2026041679069), Mar 12, 2026: NUT PLATE. CRACKED. CRACK RAIL NUT PLATES INTERNAL CAVITY LEADING EDGE OFSS 332 LT WING. REPLACED THE RAIL NUT PLATES AND FASTENERS IAW SRM 51-40-02-0G-0.
- [SDR SWAA2026041679067](https://openairdocs.org/sdr/SWAA2026041679067), Mar 12, 2026: NUT PLATE. CRACKED. CRACKED RAIL NUT PLATES INTERNAL CAVITY LEADING EDGE OFSS 572 LT WING. REPLACED THE RAIL NUT PLATES IAW SRM 51-10-02 ITEM 9 AND DWG 112A4402; SHEET 13; REV -.
- [SDR SWAA2026041679064](https://openairdocs.org/sdr/SWAA2026041679064), Mar 12, 2026: NUT PLATE. CRACKED. CRACKED RAIL NUT PLATES INTERNAL CAVITY LEADING EDGE OFSS 503 LT WING. REPLACED THE RAIL NUT PLATES AND FASTENERS IAW SRM 51-10-02 ITEM 9, SRM 51-40-02, AND DWG
- [SDR SWAA2026041679065](https://openairdocs.org/sdr/SWAA2026041679065), Mar 12, 2026: NUT PLATE. CRACKED. CRACK RAIL NUT PLATES INTERNAL CAVITY LEADING EDGE OFSS 449 LT WING. REPLACED THE RAIL NUT PLATES AND FASTENERS IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 
- [SDR SWAA2026041678879](https://openairdocs.org/sdr/SWAA2026041678879), Mar 11, 2026: LIGHT. INOPERATIVE. INOP EMERGENCY LIGHT ASSY ON STOWAGE BIN 7 LH AT PASSENGER CABIN. REPLACED EMERGENCY LIGHT ASSY ON STOWAGE BIN 7 LH AT PASSENGER CABI IAW B737-700 AMM:33-51-03-
- [SDR SWAA2026041678878](https://openairdocs.org/sdr/SWAA2026041678878), Mar 11, 2026: BATTERY PACK. INOPERATIVE. INOPERATIVE BATTERY PACK BTW BS 597 TO 616 LT & RT SIDES. REPLACED EMERGENCY LIGHT POWER SUPPLY-BATTERY PACK (M1668) BTW STA 597 TO STA 616 LH SIDE AND REPLACED
- [SDR SWAA2026041678727](https://openairdocs.org/sdr/SWAA2026041678727), Mar 11, 2026: FLOORBEAM. CRACKED. CRACKED FLOORBEAM, BS 540 AND RBL 1. REPLACED FLOORBEAM IAW SRM 51-10-02-0G-0, ITEM 9, SRM 51-40-02-0G-0, DWG 143A5240, SHEET 14, REV-, AND DWG 143A0060, SHEET 
- [SDR SWAA2026041578877](https://openairdocs.org/sdr/SWAA2026041578877), Mar 11, 2026: PLATE. CORRODED. SEVERAL CORROSION ON PLATE LOCATED ON FLOOR AREA AT BS 787 AFT CARGO COMPARTMENT. REPLACED PLATE LOCATED ON FLOOR AREA AT BS 787 AFT CARGO COMPARTMENT IAW SRM 5
- [SDR SWAA2026041578880](https://openairdocs.org/sdr/SWAA2026041578880), Mar 11, 2026: BATTERY PACK. INOPERATIVE. INOPERATIVE BATTERY PACK BTW BS 727C - 727D LT SIDE. REPLACED THE BATTERY PACK (M1670) IAW AMM 33-51-06-960-805.
- [SDR SWAA2026041578541](https://openairdocs.org/sdr/SWAA2026041578541), Mar 10, 2026: RIB. CRACKED. CRACK INSPAR RIB 120.30 AT 27 INCHES FROM FRONT SPAR AT LT HORIZONTAL STABILIZER. PERFORMED PERMANENT REPAIR LOCATED ON INSPAR RIB 120.30 AT 27 INCHES FROM FRON
- [SDR SWAA2026041578540](https://openairdocs.org/sdr/SWAA2026041578540), Mar 10, 2026: RIB. CRACKED. CRACK INSPAR RIB 120.30 AT 19 INCHES FROM FRONT SPAR AT LT HORIZONTAL STABILIZER. PERFORMED PERMANENT REPAIR LOCATED INSPAR RIB 120.30 AT 19 INCHES FROM FRONT S
- [SDR SWAA2026041578535](https://openairdocs.org/sdr/SWAA2026041578535), Mar 10, 2026: WINDOW FRAME. CRACKED. CRACK INDICATION ON WINDOW FRAME RT SIDE . CRACK LENGTH= 0.115 INCH APPROX. 2026-186433 .<[01] ON STEP 5. REPAIRED THE RT WINDOW FRAME C-D POST IAW EA 26-153-00
- [SDR SWAA2026041677951](https://openairdocs.org/sdr/SWAA2026041677951), Mar 9, 2026: TAIL CONE. DEBONDED. FUSELAGE SECTION 48 DISBONDING COMMON TO TAIL CONE LOWER AREA LOC. AT 5.5IN FROM FWD EDGE. REPAIRED TAIL CONE LOWER AREA IAW SRM 51-70-04-2R-2, REPAIR 2.
- [SDR SWAA2026041677950](https://openairdocs.org/sdr/SWAA2026041677950), Mar 9, 2026: TAIL CONE. DEBONDED. FUSELAGE SECTION 48 DISBONDING COMMON TO TAIL CONE RT SIDE. DAMAGE 1 LOC. AT 7.5IN FROM FWD EDGE AND DAMAGE 2 LOC. AT 11.5IN FROM FWD EDGE. REPAIRED TAIL CONE R
- [SDR SWAA2026041677808](https://openairdocs.org/sdr/SWAA2026041677808), Mar 8, 2026: ACCESS PANEL. DAMAGED. ELONGATED HOLES ON ACCESS PANEL 561BB AT LT WING. REPAIRED ACCESS PANEL 561BB AT LT WING IAW B737-700 SRM 51-70-04-2R-10 REPAIR 10.
- [SDR SWAA2026041677529](https://openairdocs.org/sdr/SWAA2026041677529), Mar 7, 2026: ACCESS PANEL. CRACKED. CRACK ON INTERNAL SKIN OF ACCESS PANEL 544BB, LT WING. REPAIRED THE ACCESS PANEL 544BB IAW EA 26-157-00726-WIP1.
- [SDR SWAA2026041677379](https://openairdocs.org/sdr/SWAA2026041677379), Mar 7, 2026: GUSSET. CRACKED. CRACKED GUSSET, BS 500D, STR 19L IN THE FWD CARGO BAY. REPLACED THE GUSSET IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 143A7902, SHEET 174, REV -.
- [SDR SWAA2026041677380](https://openairdocs.org/sdr/SWAA2026041677380), Mar 7, 2026: GUSSET. CRACKED. CRACKED GUSSET, BS 500D, STR 19R IN THE FWD CARGO BAY. REPLACED THE GUSSET AND FASTENERS IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, AND DWG 143A7902, SHEET 174, RE
- [SDR SWAA2026041677381](https://openairdocs.org/sdr/SWAA2026041677381), Mar 7, 2026: ANGLE. CRACKED. CRACKED ANGLE, BS 400, LBL 21 IN THE FWD CARGO BAY. REPLACED THE ANGLE AND FASTENERS IAW SRM 51-40-02, ITEM 9, SRM 51-40-02, AND DWG 143A7505, SHEET 82, REV - .
- [SDR SWAA2025120441567](https://openairdocs.org/sdr/SWAA2025120441567), Dec 2, 2025: BATTERY PACK. NO TEST. BATTERY AT SEAT 17ABC NOT LASTING 15 MINUTES. R & R CABIN CABIN EMERGENCY BATTERY PACK M1670 AT SEAT 17ABC IAW AMM 33-51-06.
- [SDR SWAA2025120441560](https://openairdocs.org/sdr/SWAA2025120441560), Dec 2, 2025: TAIL CONE. DELAMINATED. TAIL CONE RT SIDE HAS SKIN DELAMINATION JUST FORWARD AND BELOW THE TAIL CONE ACCESS DOOR NEAR BS 1190. COMPLIED WITH 25-153-03292 (COMPONENT - REPAIR - FUSELAGE
- [SDR SWAA2025103129768](https://openairdocs.org/sdr/SWAA2025103129768), Oct 29, 2025: FUSE. INOPERATIVE. RIGHT SIDE EMERGENCY EXIT INSTRUCTIONS LIGHT INOPERATIVE. LAMP REPLACED NO HELP REF AMM 33-22-00. OK TO CONTINUE MEL 33-2-03 SP1B. REMOVED AND REPLACED RT EMERG
- [SDR SWAA2025062083718](https://openairdocs.org/sdr/SWAA2025062083718), Jun 19, 2025: LENS. DETACHED. CEILING EMERGENCY EXIT COVER FELL OFF.<[01] SECURED LENS PER S.I.P.
- [SDR SWAA2025040119708](https://openairdocs.org/sdr/SWAA2025040119708), Mar 30, 2025: LAMP. INOPERATIVE. AFT R/H EMERGENCY GROUND ILLUMINATION LIGHT INOP.<[01] REMOVED AND REPLACED AFT R/H EMERGENCY EXIT GROUND ILLUMINATION LIGHT LAMP PER AMM 33-51-04. OPS TEST GOO
- [SDR SWAA2024100444699](https://openairdocs.org/sdr/SWAA2024100444699), Oct 3, 2024: GIRT BAR. LOOSE. R2 DOOR SLIDE GIRT NEEDS TO BE RESECURED<[01] RESECURED R2 DOOR SLIDE GIRT WITH VELCRO PER AMM 25-66-01.
- [SDR SWAA2024100444693](https://openairdocs.org/sdr/SWAA2024100444693), Oct 3, 2024: GIRT BAR. LOOSE. L2 DOOR SLIDE GIRT NEEDS TO BE RESECURED<[01] RESECURED L2 DOOR SLIDE GIRT WITH VELCRO PER AMM 25-66-01.
- [SDR SWAA2024051476286](https://openairdocs.org/sdr/SWAA2024051476286), Apr 18, 2024: BATTERY PACK. INOPERATIVE. INOP BATTERY PACK ON EMERGENCY EXIT HATCH DOOR LT AND RT SIDE PAX CABIN 2024-253432<[01] REPLACED BATTERY PACK ON EMERGENCY EXIT HATCH DOOR LT AND RT SIDE PAX C

All 249: https://openairdocs.org/aircraft/N7729A/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 N7729A

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N7729A before.

- [Cancelled 1956-11-02](https://openairdocs.org/deregistered/N7729A-1956-11-02): Cessna 180, S/N 32626. Owner: [Cessna Aircraft Co](https://openairdocs.org/faa-owner/CESSNA%20AIRCRAFT%20CO), [Wichita, KS](https://openairdocs.org/faa-place/KS/Wichita)

## Related

- Other Boeing 737-76N aircraft: https://openairdocs.org/model/boeing-737-76n/aircraft.md
- The CFM International CFM56-7B22 series engine: https://openairdocs.org/engine/cfm-international-cfm56-7b22-series.md

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