# N7746C: 2007 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: 33934
- Year built: 2007
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: June 14, 2007
- Certificate issued: July 2, 2013
- Expires: July 31, 2029
- Mode S code: AA7B10
- 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=7746C
- Page: https://openairdocs.org/aircraft/N7746C

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

None matched to N7746C.

## FAA accident and incident reports

None matched to N7746C.

## Service difficulty reports (233, 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 SWAA2026090445301](https://openairdocs.org/sdr/SWAA2026090445301), Aug 31, 2026: ELEC CONNECTOR. LOOSE. NR 1 FIRE HANDLE WILL NOT ILLUMINATE DURING FIRE TEST IN NORMAL NR 1 FIRE HANDLEWILL NOT ILLUMINATE DURING FIRE TEST IN NORMAL OK TO CONTINUE PER MEL. 26-2-01 (
- [SDR SWAA2026061712171](https://openairdocs.org/sdr/SWAA2026061712171), Jun 13, 2026: HANDLE. DETACHED. FWD ENTRY DOOR ASSIST-TO-OPEN HANDLE (GRIP) DETACHED. SECURED FWD ENTRY DOOR ASSIST HANDLE PER AMM 52-11-31.
- [SDR SWAA2026061010872](https://openairdocs.org/sdr/SWAA2026061010872), Jun 10, 2026: HOSE. DAMAGED. AFTER LANDING NR 1 ENGINE A HYDRAULIC SYSTEM LOW PRESSURE LIGHT CAME ON. NOTICED BOTH QTY & PRESSURE FOR A SYSTEM HYDRAULICS GOING TO ZERO. BOTH NR 1 ENG AND EL
- [SDR SWAA2026061010951](https://openairdocs.org/sdr/SWAA2026061010951), Jun 10, 2026: PUMP. LEAKING. AFTER LANDING NR 1 ENGINE A HYDRAULIC SYSTEM LOW PRESSURE LIGHT CAME ON. NOTICED BOTH QTY & PRESSURE FOR A SYSTEM HYDRAULICS GOING TO ZERO. BOTH NR 1 ENG AND EL
- [SDR SWAA2026051897669](https://openairdocs.org/sdr/SWAA2026051897669), May 12, 2026: SLIDE. TORN. FORWARD SERVICE DOOR EMERGENCY ESCAPE SLIDE SKIRT WHERE GIRT BAR ATTACHES IS TORN. R&R FORWARD SERVICE DOOR EMERGENCY ESCAPE SLIDE IAW AMM 25-66-01. REF. TTG8Q0
- [SDR SWAA2026040786131](https://openairdocs.org/sdr/SWAA2026040786131), Apr 3, 2026: ENGINE. FAILED. DURING TAKE OFF NR 1 ENGINE FAILED. RTO APPROX 133 KTS. NO ABNORMAL SMELLS IN THE COCKPIT OR CABIN. NO FIRE INDICATIONS IN COCKPIT. CFR ADVISED SMOKE COMING FRO
- [SDR SWAA2026012664484](https://openairdocs.org/sdr/SWAA2026012664484), Jan 25, 2026: UNKNOWN. SMOKE. SMOKE IN THE FLIGHT WHEN LT PACK TURNED ON. C/W SMOKE OR FUMES IN CABIN CONDITIONAL INSPECTION IAW AMM 05-51-56, NO DEFECTS NOTED. RAN LT & RT PACKS USING APU A
- [SDR SWAA2025121852529](https://openairdocs.org/sdr/SWAA2025121852529), Dec 15, 2025: FASTENER. MISSING. L1 DOOR EMERGENCY ESCAPE SLIDE COMPTARTMENT AFT GIRT BAR RETAINER MISSING ONE FASTENER. REPLACED THE MISSING FASTENER ON THE AFT GIRT BAR RETAINER IAW SRM 51-40
- [SDR SWAA2025120842731](https://openairdocs.org/sdr/SWAA2025120842731), Dec 4, 2025: SLIDE. MISSING. FWD. ENTRY ESCAPE SLIDE IS NOT INSTALLED. R & R FWD ENTRY DOOR ESCAPE SLIDE PER MT 725-61-06-FE, OK FOR SERVICE.
- [SDR SWAA2025120442732](https://openairdocs.org/sdr/SWAA2025120442732), Dec 4, 2025: GIRT BAR. BROKEN. FWD ENTRY DOOR SLIDE GIRT BAR HOOK ON COVER HAS BROKEN FASTENER. ACCOMPLISHED EA M-23-125-01839 WITH SAFETY WIRE.
- [SDR SWAA2025110732299](https://openairdocs.org/sdr/SWAA2025110732299), Nov 6, 2025: BATTERY PACK. NO TEST. FWD SERVICE DOOR OVERHEAD EMERGENCY LIGHT WILL NOT TEST. R & R BATTERY PACK IAW MM 33-51-06.
- [SDR SWAA2025081403575](https://openairdocs.org/sdr/SWAA2025081403575), Aug 13, 2025: DOOR. CRACKED. LEFT WING MLG MIDDLE DOOR CRACKED.<[01] REMOVED INNER AND CENTER GEAR DOORS REF 32-13-11 AND OK TO CONT REF AUTH# 273828
- [SDR SWAA2025022590630](https://openairdocs.org/sdr/SWAA2025022590630), Jan 28, 2025: SKIN. CRACKED. CRACK FOUND ON LH HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STATION 193.90 RIB; 17.5 INCHES FROM FRONT SPAR; INB SIDE OF RIB LENGTH APPROX= 0.875 INCHES. 2025
- [SDR SWAA2025022589281](https://openairdocs.org/sdr/SWAA2025022589281), Jan 24, 2025: TIE CLIP. CRACKED. CRACK TIE CLIP LOCATED BS277 AND S-10R PASSENGER CABIN 2025-80691<[01]. REPLACED TIE CLIP LOCATED BS277 AND S-10R PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND 
- [SDR SWAA2025022589378](https://openairdocs.org/sdr/SWAA2025022589378), Jan 24, 2025: RIB. CRACKED. CRACK RIB LOCATED LE STA 105.26 AT LT HORIZONTAL STABILIZER 2025-80697 <[01]. REPLACED RIB LOCATED LE STA 105.26 AT LT HORIZONTAL STABILIZER IAW B737-700 SRM 51
- [SDR SWAA2025022589377](https://openairdocs.org/sdr/SWAA2025022589377), Jan 24, 2025: RIB. CRACKED. CRACK LEADING EDGE RIB ACCESS PANEL 341B LOCATED LE STA 105.26 AT RT HORIZONTAL STABILIZER 2025-80698 <[01]. REPLACED RIB LOCATED ACCESS PANEL 341B LOCATED LE S
- [SDR SWAA2025022489278](https://openairdocs.org/sdr/SWAA2025022489278), Jan 24, 2025: WEB. CRACKED. CRACK WEB LOCATED BS 294.5 TO BS 303.9 AND S-16L AT PASSENGER CABIN 2025-80693<[01] REPLACED WEB LOCATED BS 294.5 TO BS 303.9 AND S-16L AT PASSENGER CABIN IAW B
- [SDR SWAA2025022489015](https://openairdocs.org/sdr/SWAA2025022489015), Jan 24, 2025: STRIP. DETERIORATED. DETERIORATE PHOTOLUMINESCENT STRIP AT PASSENGER CABIN (8EA) 2025-80680 <[01]. REPLACED PHOTOLUMINESCENT STRIP AT PASSENGER CABIN (8EA) IAW DWG:33500007; REV:2; 
- [SDR SWAA2025022489279](https://openairdocs.org/sdr/SWAA2025022489279), Jan 24, 2025: BATTERY PACK. INOPERATIVE. INOP BATTERY PACK EMERGENCY EXIT LIGHT STA 727D LT SIDE AT PASSENGER CABIN (1EA) 2025-80690<[01]. REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERY PACK STA 727D LT
- [SDR SWAA2025022489282](https://openairdocs.org/sdr/SWAA2025022489282), Jan 24, 2025: BATTERY PACK. INOPERATIVE. INOP BATTERY PACK EMERGENCY EXIT LIGHT STA 500C LT SIDE AT PASSENGER CABIN (1EA) 2025-80692 <[01]. REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERY PACK STA 500C L
- [SDR SWAA2025022489280](https://openairdocs.org/sdr/SWAA2025022489280), Jan 24, 2025: BATTERY PACK. INOPERATIVE. INOP BATTERY PACK EMERGENCY EXIT LIGHT AFT LOWERED CEILING RT SIDE AT AFT GALLEY AREA (1EA) 2025-80694 <[01]. NON MAINTENANCE ACTION REQUIRED FOR REPLACED BATER
- [SDR SWAA2025022589008](https://openairdocs.org/sdr/SWAA2025022589008), Jan 23, 2025: ANGLE. CRACKED. CRACK BLADE ANGLE ACCESS PANEL 333AT AT LT HORIZONTAL STABILIZER 2025-80645 <[01]. REPLACED BLADE ANGLE ACCESS PANEL 333AT AT LT HORIZONTAL STABILIZER IAW B737-
- [SDR SWAA2025022589011](https://openairdocs.org/sdr/SWAA2025022589011), Jan 23, 2025: PANEL. CRACKED. CRACK BLADE ANGLE ACCESS PANEL 343AT AT RT HORIZONTAL STABILIZER 2025-80651<[01]. REPLACED BLADE ANGLE LOCATED ON ACCESS PANEL 343AT AT RT HORIZONTAL STABILIZER
- [SDR SWAA2025022489004](https://openairdocs.org/sdr/SWAA2025022489004), Jan 23, 2025: FLOOR SUPPORT. CRACKED. CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BS 312 TO BS 328 AND LBL 46 FWD GALLEY AND LAV 2025-80640<[01] REPLACED WEB-INTERCOSTAL FLOOR STRUCTURE LOCATED 
- [SDR SWAA2025022489005](https://openairdocs.org/sdr/SWAA2025022489005), Jan 23, 2025: FLOOR SUPPORT. CRACKED. CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BS 344 TO BS 360 AND BL 0 FWD GALLEY AND LAV 2025-80642<[01] REPLACED WEB - INTERCOSTAL FLOOR STRUCTURE LOC. ON 
- [SDR SWAA2025022488559](https://openairdocs.org/sdr/SWAA2025022488559), Jan 22, 2025: STUB FRAME. CRACKED. CRACK INDICATION ON STUB FRAME LOCATED BETWEEN BS 294.5 TO BS 296 AND BTW S-8R TO S-9R AT FWD GALLEY DOOR AREA CRACK LENGTH 0.687 IN. APPROX. AT PASSENGER CABIN
- [SDR SWAA2025022487810](https://openairdocs.org/sdr/SWAA2025022487810), Jan 20, 2025: SCUFF PLATE. CRACKED. CRACK AFT CORNER SCUFF PLATE LOC AT AFT CARGO COMPARTMENT 2025-80506<[01] TOOL USED: RADIOMETER KIT; P/N: XRP-3000; S/N: 1859843; DUE DATE: 10-MAR-25.;[02] REPA
- [SDR SWAA2025022487436](https://openairdocs.org/sdr/SWAA2025022487436), Jan 19, 2025: BATTERY PACK. INOPERATIVE. INOP BATTERY PACK AT AFT CEILING PANEL (2EA) 2025-80443 <[01]. REPLACED BATTERY PACK AT AFT CEILING PANEL (2EA) IAW B737-700 AMM 33-51-06-960-805 INSTALLATION T
- [SDR SWAA2025022587255](https://openairdocs.org/sdr/SWAA2025022587255), Jan 18, 2025: VAPOR BARRIER. CRACKED. CRACK BODY STATION 663.75 VAPOR BARRIER LBL 45 AT MAIN WHEEL WELL COMPARTMENT 2025-80432 <[01]. TOOL USED P/N: EPOCH 600; S/N: 120357005; CAL DUE: 10-JUN-25.;[0
- [SDR SWAA2025022587256](https://openairdocs.org/sdr/SWAA2025022587256), Jan 18, 2025: VAPOR BARRIER. CRACKED. CRACK BODY STATION 663.75 VAPOR BARRIER RBL 38 AT MAIN WHEEL WELL COMPARTMENT 2025-80433<[01]. TOOL USED: CALIPER PN: 500-196-30; SN: B24006487; DUE DATE: 11-SE
- [SDR SWAA2024122379758](https://openairdocs.org/sdr/SWAA2024122379758), Dec 20, 2024: SLIDE. LOOSE. FWD SERVICE DOOR SLIDE HAS ZIP TIE EXTRUDING OUT OF FWD SLIDE<[01] RESECURED ZIP TIE AS REQUIRED PER SIP
- [SDR SWAA2024112670594](https://openairdocs.org/sdr/SWAA2024112670594), Nov 22, 2024: SLIDE. OUT OF ADJUST. WHEN FWD SVC DOOR WAS OPENED EMERGENCY SLIDE FELL OUT ONTO PROVO TRUCK GIRT BAR WAS ENGAGED<[01] ADJUSTED FWD DOOR SERVICE SIDE IN REFERENCE TO AMM 25-66-00
- [SDR SWAA2024102953132](https://openairdocs.org/sdr/SWAA2024102953132), Oct 25, 2024: SEAL. CRACKED. RIGHT STABILIZER-TO-BODY UPPER FRONT SPAR SLIDING SEAL CRACKED.<[01] 01 - REMOVED AND REPLACED PER [AMM 53-31-31-401 CONFIG 2-NG (STABILIZER TO BODY FRONT SPAR 
- [SDR SWAA2024102953134](https://openairdocs.org/sdr/SWAA2024102953134), Oct 25, 2024: SEAL. CRACKED. LEFT STABILIZER-TO-BODY UPPER FRONT SPAR SLIDING SEAL CRACKED.<[01] REMOVED AND REPLACED LEFT HORIZONTAL STABILIZER UPPER FWD SLIDING SEAL PER AMM 53-31-31
- [SDR SWAA2024102952894](https://openairdocs.org/sdr/SWAA2024102952894), Oct 25, 2024: SEAL. CRACKED. RIGHT STABILIZER-TO-BODY UPPER FRONT SPAR SLIDING SEAL CRACKED.<[01] 01 - REMOVED AND REPLACED PER [AMM 53-31-31-401 CONFIG 2-NG (STABILIZER TO BODY FRONT SPAR 
- [SDR SWAA2024102952895](https://openairdocs.org/sdr/SWAA2024102952895), Oct 25, 2024: SEAL. CRACKED. LEFT STABILIZER-TO-BODY UPPER FRONT SPAR SLIDING SEAL CRACKED.<[01] REMOVED AND REPLACED LEFT HORIZONTAL STABILIZER UPPER FWD SLIDING SEAL PER AMM 53-31-31
- [SDR SWAA2024012544544](https://openairdocs.org/sdr/SWAA2024012544544), Jan 25, 2024: BATTERY PACK. NO TEST. R/H AFT EMERGENCY LIGHTING BATTERY PACK FAILED CAPACITY CHECK.<[01] REMOVED AND REPLACED BATTERY PACK PER M/M 33-51-06
- [SDR SWAA2023122133723](https://openairdocs.org/sdr/SWAA2023122133723), Dec 19, 2023: LENS. MISSING. ROW 20 BULLNOSE EMERGENCY EXIT LIGHT LENS MISSING<[01] INSTALLED LENS REF AMM 33-51-03
- [SDR SWAA2023030812423](https://openairdocs.org/sdr/SWAA2023030812423), Mar 4, 2023: BATTERY. INOPERATIVE. FWD UPPER EMERGENCY FLASHLIGHT INOP.<[01] R & R?D BATTERY REF. M/M 25-64-00
- [SDR SWAA2023030211286](https://openairdocs.org/sdr/SWAA2023030211286), Mar 1, 2023: LIGHT. BURNED OUT. R2 DOOR EMERGENCY EXIT LIGHT WITH 1EA PEANUT BURN. 2023-99422<[01] REPLACED R2 DOOR EMERGENCY EXIT LIGHT WITH 1EA PEANUT AIW B737-700 AMM 33-51-01-960-802;[02] 
- [SDR SWAA2023030605216](https://openairdocs.org/sdr/SWAA2023030605216), Feb 20, 2023: SKIN. ELONGATED. REJECT ELONGATED HOLE EXTERNAL SKIN SEVERAL POSITION LOWER AREA STAB STA 120.30 LEVEL AT RT HORIZONTAL STABILIZER 2023-99403<[01] ET TOOL USED: PN: MIZ-21C ; SN
- [SDR SWAA2023030601299](https://openairdocs.org/sdr/SWAA2023030601299), Feb 9, 2023: FASTENER. CORRODED. CORROSION BILGE AREA FASTENER SHOP HEADS REPAIR AREA LOCATED BTW BS500A TO BS500B AND BTW STR28R TO STR28L AT FWD CARGO COMPARTMENT 2023-99371<[01] AFFECTED FAS
- [SDR SWAA2023030699725](https://openairdocs.org/sdr/SWAA2023030699725), Feb 7, 2023: BRACKET. CRACKED. CRACK SUPPORT BRACKET BODY STATION 663.75 AND BTW LBL 45.64 TO LBL 54.21 AND WL 160 AT MAIN WHEEL WELL COMPARTMENT 2023-99340<[01] REPLACED SUPPORT BRACKET AND 
- [SDR SWAA2023030600238](https://openairdocs.org/sdr/SWAA2023030600238), Feb 7, 2023: WEB. ELONGATED. (CUSTOMER REQUEST) ELONGATED HOLES (8 EA) ON WEB LOCATED ON BS663 AND BETWEEN LBL6.13 AND LBL31 AT MAIN WHEEL WELL COMPARTMENT 2023-99353<[01] REPLACED WEB LOCA
- [SDR SWAA2023030600237](https://openairdocs.org/sdr/SWAA2023030600237), Feb 7, 2023: RIB. CRACKED. CRACK LEADING EDGE RIB IN LE STA 95.96 AT RT HORIZONTAL STABILIZER 2023-99350<[01] REPLACED LEADING EDGE RIB IN LE STA 95.96 AT RT HORIZONTAL STABILIZER IAW B73
- [SDR SWAA2023030299730](https://openairdocs.org/sdr/SWAA2023030299730), Feb 7, 2023: LIGHT. INOPERATIVE. INOP GALLEY 4 EMERGENCY EXIT ASSY LIGHT AT AFT GALLEY AREA 2023-99308<[01] REPLACED GALLEY 4 EMERGENCY EXIT ASSY LIGHT AT AFT GALLEY ARE IAW B737-700 AMM 33-51-
- [SDR SWAA2023030699717](https://openairdocs.org/sdr/SWAA2023030699717), Feb 6, 2023: ANGLE. CRACKED. CRACK ANGLE LOCATED BETWEEN BS 867 AND STR26L TO STR27L AFT CARGO COMPARTMENT 2023-99292<[01] REPLACED ANGLE LOCATED BETWEEN BS 867 AND STR26L TO STR27L AFT CAR
- [SDR SWAA2023030699720](https://openairdocs.org/sdr/SWAA2023030699720), Feb 6, 2023: SUPPORT. CORRODED. CORROSION SUPPORT ZEE LOCATED BETWEEN BS727 TO BS767 RBL21 WL155 AFT CARGO COMPARTMENT 2023-99295<[01] REPLACED SUPPORT ZEE LOCATED BETWEEN BS727 TO BS767 RBL21
- [SDR SWAA2023030399718](https://openairdocs.org/sdr/SWAA2023030399718), Feb 6, 2023: ANGLE. CRACKED. CRACK ANGLE LOCATED BETWEEN BS 827 AND STR25R TO STR26R AFT CARGO COMPARTMENT 2023-99291<[01] REPLACED NEW ANGLE LOCATED BETWEEN BS 827 AND STR25R TO STR26R AFT
- [SDR SWAA2023030399719](https://openairdocs.org/sdr/SWAA2023030399719), Feb 6, 2023: ANGLE. CRACKED. CRACK ANGLE LOCATED BETWEEN BS 907 TO BS 927 AND STR25R TO STR27R AFT CARGO COMPARTMENT 2023-99293<[01] REPLACED ANGLE LOCATED BETWEEN BS 907 TO BS 927 AND STR2

All 233: https://openairdocs.org/aircraft/N7746C/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

## 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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