# N7751A: 2008 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: 36717
- Year built: 2008
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: May 27, 2014
- Certificate issued: June 19, 2014
- Expires: June 30, 2027
- Mode S code: AA7E16
- 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=7751A
- Page: https://openairdocs.org/aircraft/N7751A

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 N7751A.

## FAA accident and incident reports (1)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 20170227007319I](https://openairdocs.org/incident/20170227007319I), Feb 27, 2017: Boeing 737-7BD (N7751A), Omaha, NE, Minor damage. On February 27, 2017 at approximately 2150 CST, N7751A, a Boeing 737-7BD, flight 1426 operated by southwest airlines, struck a flock of snow geese while on…

## Service difficulty reports (202, 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 SWAA2026060808789](https://openairdocs.org/sdr/SWAA2026060808789), Jun 3, 2026: HANDLE. OUT OF ADJUST. AFT GALLEY SERVICE DOOR INSIDE OPEN DOOR HANDLE HAS PLAY. AFT GALLEY SERVICE DOOR HANDLE ADJUSTED IAW AMM 52-41-00.
- [SDR SWAA2026060808784](https://openairdocs.org/sdr/SWAA2026060808784), Jun 3, 2026: SLIDER. CRACKED. RIGHT HORIZONTAL UPPER FWD SLIDER CRACKED. REMOVED AND REPLACED RT HORIZONTAL STAB UPPER FWD SLIDER IAW AMM 53-31-31.
- [SDR SWAA2026060808772](https://openairdocs.org/sdr/SWAA2026060808772), Jun 3, 2026: SKIN. DEBONDED. LEFT WING OTBD TE FLAP HAS DISBONDED SKIN ON THE INBD UPPER SURFACE. REMOVED LT OTBD AFT FLAP IAW AMM 27-51-22. REMOVED AND REPLACED IAW AMM 27-51-22-401.
- [SDR SWAA2026060308795](https://openairdocs.org/sdr/SWAA2026060308795), Jun 3, 2026: BATTERY PACK. NO TEST. AFT LT EMERGENCY LIGHTING BATTERY PACK FAILED THE CAPACITY CHECK. REMOVED AND REPLACED EMERGENCY LIGHTING BATTERY PACK IAW MM 33-51-06.
- [SDR SWAA2026021068698](https://openairdocs.org/sdr/SWAA2026021068698), Feb 7, 2026: SKIN. DEBONDED. ON WALK AROUND FOUND R/H OUTBOARD AFT FLAP UPPER SURFACE DISBONDED/MISSING WITH COMB EXPOSED. REMOVED AND REPLACED RH OTBD AFT FLAP IAW AMM 27-51-22.
- [SDR SWAA2025092307645](https://openairdocs.org/sdr/SWAA2025092307645), Aug 23, 2025: PLATE. CRACKED. CRACK CORRUGATED PLATE TRAILING EDGE, IRSS 181, RT WING. REPLACED THE CORRUGATED PLATE AND FASTENERS IAW SRM 51-10-02 ITEM 9, AND SRM 51-40-02.
- [SDR SWAA2025092307065](https://openairdocs.org/sdr/SWAA2025092307065), Aug 21, 2025: SEAT TRACK. CORRODED. MAIN CABIN SEAT TRACK BS 727B; REPAIR HAS TWO FASTENERS LOOSE AND EVIDENCE OF CORROSION AT RBL 45.50, INBD SIDE. REPLACED FASTENERS ON THE SEAT TRACK STA 727B; 
- [SDR SWAA2025092307062](https://openairdocs.org/sdr/SWAA2025092307062), Aug 21, 2025: ACCESS PANEL. CRACKED. CRACK ON ANGLE ACCESS PANEL 834DZ ENTRY DOOR. REPLACED THE ANGLE ACCESS PANEL 834DZ IAW SRM 51-10-02, SRM 51-40-02, AND DWG 411A2119, SHEET 72, REV -. .
- [SDR SWAA2025092307064](https://openairdocs.org/sdr/SWAA2025092307064), Aug 21, 2025: FLOORBEAM. CRACKED. AAI: MAIN CABIN - FLOORBEAM HAS CRACK AT STA 540; BL 0 TO RBL 24.75. REPLACED FLOORBEAM IAW SRM 51-40-02, AND SRM 51-10-02-0G-0, PARAGRAPH 9.
- [SDR SWAA2025092206640](https://openairdocs.org/sdr/SWAA2025092206640), Aug 20, 2025: FRAME. CRACKED. DURING INSPECTION JOB CARD 753-350-00-00, FOUND A CRACK ON FRAME WEB, BS 259.5, BTW STRINGERS 8R & 9R. PERFORMED A PERMANENT FRAME REPAIR IAW EA 25-153-02325.
- [SDR SWAA2025092305982](https://openairdocs.org/sdr/SWAA2025092305982), Aug 19, 2025: ACCESS PANEL. ELONGATED. ELONGATED HOLES ON ACCESS PANEL 561CB AT LT WING. REPAIRED ACCESS PANEL 561CB AT LT WING IAW B737-700 SRM 51-70-04-2R-10 REPAIR 10.
- [SDR SWAA2025092305983](https://openairdocs.org/sdr/SWAA2025092305983), Aug 19, 2025: ACCESS PANEL. ELONGATED. ELONGATED HOLES ON ACCESS PANEL 561AB AT LT WING. REPAIRED ACCESS PANEL 561AB AT LT WING IAW B737-700 SRM 51-70-04-2R-10 REPAIR 10.
- [SDR SWAA2025092305468](https://openairdocs.org/sdr/SWAA2025092305468), Aug 17, 2025: RIB. CRACKED. CRACKED ACCESS PANEL 331B LEADING EDGE ON RIB, LE STA 95.96 AT LT HORIZONTAL STABILIZER. REPLACED RIB LOCATED ON ACCESS PANEL 331B LEADING EDGE ON STA95.96 AT L
- [SDR SWAA2025092305370](https://openairdocs.org/sdr/SWAA2025092305370), Aug 17, 2025: INTERCOSTAL. CRACKED. CRACKED WEB BTW BS 294.5 & 303.9, STR 16L, FWD GALLEY AREA. REPLACED WEB-INTERCOSTAL IAW SRM 51-40-02-0G-0, DWG 141A8180, SHEET 27, REV C, DWG 141A8180, SHEET 2
- [SDR SWAA2025092305369](https://openairdocs.org/sdr/SWAA2025092305369), Aug 17, 2025: TIE CLIP. CRACKED. CRACK TIE CLIP BS 277, STR 10R, PAX CABIN. REPLACED THE TIE CLIP IAW SRM-51-40-02, DWG 141A1110, SHEET 18, REV-, AND DWG 141A8380, SHEET 21, REV-.
- [SDR SWAA2025092305371](https://openairdocs.org/sdr/SWAA2025092305371), Aug 17, 2025: FRAME. CRACKED. CRACK FRAME ON BS 312 BTW STRINGERS 4L - 5L IN FWD GALLEY AREA. PERFORMED FRAME REPAIR IAW M-22-153-01244.
- [SDR SWAA2025092205466](https://openairdocs.org/sdr/SWAA2025092205466), Aug 17, 2025: FRAME. CRACKED. CRACKED FRAME ON BS 907 BTW STRINGERS 8R & 9R IN PAX CABIN. PERFORMED A PERMANENT FRAME REPAIR IAW EA 25-153-02348, REV A.
- [SDR SWAA2025092305210](https://openairdocs.org/sdr/SWAA2025092305210), Aug 16, 2025: WEB. CORRODED. CORROSION DOOR CUTOUT WEB UPPER POSITION LOCATED BETWEEN BS 794 AND BS 847 AFT CARGO COMPARTMENT. REPLACED WEB LOCATED ON DOOR CUT OUT UPPER POSITION BETWEEN BS
- [SDR SWAA2025092205127](https://openairdocs.org/sdr/SWAA2025092205127), Aug 16, 2025: WEB. CORRODED. CORROSION FLOOR STRUCTURE LOCATED BS1016 TO BS1016 PLUS 14 INCH BETWEEN BL0 TO LBL14 AT AFT GALLEY AREA. REPLACED WEB AND FASTENERS FLOOR LOCATED BS1016 TO BS10
- [SDR SWAA2025092205131](https://openairdocs.org/sdr/SWAA2025092205131), Aug 16, 2025: FLOORBEAM. CORRODED. CORROSION ON EXISTING REPAIR FLOORBEAM LOCATE BS986.5, LBL 44, WL 208 IN AFT GALLEY AREA. REPLACED FILLER ON EXISTING FLOORBEAM REPAIR IAW SRM 53-70-51-2R-6, RE
- [SDR SWAA2025092205126](https://openairdocs.org/sdr/SWAA2025092205126), Aug 16, 2025: FLOORBEAM. CORRODED. CORROSION EXISTING REPAIR FLOORBEAM LOCATED BS 986.5, RBL 44, WL 208 IN AFT GALLEY AREA. REPLACED THE FILLER ON EXISTING FLOORBEAM REPAIR IAW SRM 53-70-51-2R-6,
- [SDR SWAA2025092205128](https://openairdocs.org/sdr/SWAA2025092205128), Aug 16, 2025: INTERCOSTAL. CRACKED. CRACK WEB - INTERCOSTAL CEILING AREA LOCATED BS847 TO BS867 AT LEVEL LBL30 AT AFT CARGO COMPARTMENT 2025-499739<[01] REPLACED WEB - INTERCOSTAL CEILING AREA LOC
- [SDR SWAA2025092304900](https://openairdocs.org/sdr/SWAA2025092304900), Aug 15, 2025: TEE ANGLE. CORRODED. CORROSION ON FLOOR STRUCTURE TEE ANGLE BETWEEN BS 270 TO BS 277 AND LBL 10 WL 208. REPLACED TEE ANGLE BS 270 TO BS 277, LBL 10, WL 208 IAW SRM 51-40-02 AND DWG 
- [SDR SWAA2025092304700](https://openairdocs.org/sdr/SWAA2025092304700), Aug 15, 2025: BATTERY PACK. INOPERATIVE. BATTERY PACK INOPERATIVE FOR EMERGENCY LIGHT BTW BS 597 - 616 RT PASSENGER CABIN. REPLACED POWER SUPPLY BATTERY PACK EMERGENCY LIGHT BTW STA 597 TO STA 616 RH S
- [SDR SWAA2025092304699](https://openairdocs.org/sdr/SWAA2025092304699), Aug 15, 2025: BATTERY PACK. INOPERATIVE. BATTERY PACK INOPERATIVE FOR EMERGENCY LIGHT BTW BS 597 - 616, LT PASSENGER CABIN. REPLACED POWER SUPPLY BATTERY PACK IAW AMM 33-51-06-960-805 AND OPS TESTED OK
- [SDR SWAA2025092304898](https://openairdocs.org/sdr/SWAA2025092304898), Aug 15, 2025: FLOOR SUPPORT. CRACKED. CRACKED FLOOR SUPPORT BETWEEN BS 277 TO BS 294.5, BL 0 IN THE FWD GALLEY. REPLACED FLOOR SUPPORT IAW SRM 51-40-02-0G-0 AND DWG 141A5400, SHEET 39, REV -.
- [SDR SWAA2025092304904](https://openairdocs.org/sdr/SWAA2025092304904), Aug 15, 2025: INTERCOSTAL. CRACKED. CRACKED FLOOR SUPPORT BETWEEN BS 312 - 328, LBL 46 IN THE FWD GALLEY AND LAV. REPLACED FLOOR SUPPORT IAW SRM 51-10-02-0G-0, SRM 51-40-02-0G-0, AND DWG 141A5400,
- [SDR SWAA2025092204901](https://openairdocs.org/sdr/SWAA2025092204901), Aug 15, 2025: FLOOR PANEL. BROKEN. BROKEN FLOOR PANEL 241AEF AT AFT GALLEY AREA. REPAIRED FLOOR PANEL 241AEF AT AFT GALLEY AREA IAW SRM 53-00-50-2R-1 REPAIR 1 .
- [SDR SWAA2025092204905](https://openairdocs.org/sdr/SWAA2025092204905), Aug 15, 2025: FLOOR SUPPORT. CRACKED. CRACK WEB - INTERCOSTAL FLOOR STRUCTURE BETWEEN BS 312 TO BS 328 AND RBL 31 FWD GALLEY AND LAV. REPLACED WEB-INTERCOSTAL FLOOR STRUCTURE LOCATED BTW BS 312 TO B
- [SDR SWAA2025092304685](https://openairdocs.org/sdr/SWAA2025092304685), Aug 14, 2025: SUPPORT ANGLE. CORRODED. CORROSION SUPPORT ANGLE BS 500D BETWEEN STRINGERS 26L TO 26R, IN FWD CARGO BAY. REPLACED THE SUPPORT ANGLE IAW SRM 52-40-02, SRM 51-10-02, STEP 9, AND DWG 143A9
- [SDR SWAA2025092304683](https://openairdocs.org/sdr/SWAA2025092304683), Aug 14, 2025: ANGLE. CRACKED. CRACK ANGLE LOCATED BS 827 AT LEVEL STR 25R AFT CARGO BAY. REPLACED THE ANGLE IAW SRM 51-10-02, ITEM 9, AND DWG 146A8120, SHEET 37, REV -; DWG 146A0081, SHEET 3
- [SDR SWAA2025092304688](https://openairdocs.org/sdr/SWAA2025092304688), Aug 14, 2025: ANGLE. CRACKED. CRACK ANGLE LOCATED BS 807, S25R IN AFT CARGO BAY. REPLACED THE ANGLE IAW SRM 51-10-02, ITEM 9, AND DWG 146A8120, SHEET 37, REV -, AND DWG 146A0081, SHEET 38, R
- [SDR SWAA2025092304681](https://openairdocs.org/sdr/SWAA2025092304681), Aug 14, 2025: SUPPORT ANGLE. CORRODED. CORROED SUPPORT ANGLE, BS 767 - 787, S25R IN CARGO BAY. REPLACED THE SUPPORT ANGLE IAW SRM 51-40-02-0G-0, SRM 51-10-02-0G-0, ITEM 9, DWG 146A0081, SHEET 37, REV
- [SDR SWAA2025092304689](https://openairdocs.org/sdr/SWAA2025092304689), Aug 14, 2025: SUPPORT BRACKET. CRACKED. CRACK SUPPORT BRACKET. BS 947.5, STRINGER 26L IN AFT CARGO BAY. EVALUATED DAMAGE AND NOT FOUND ALLOWABLE DAMAGE FOR CRACK. MEASUREMENT: L= 2.350, IAW SRM . REPL
- [SDR SWAA2025092204680](https://openairdocs.org/sdr/SWAA2025092204680), Aug 14, 2025: INTERCOSTAL. CORRODED. CORROSION WEB - INTERCOSTAL LOCATED BS767 TO BS787 AT LEVEL STR25R AFT CARGO COMPARTMENT. REPLACED WEB - INTERCOSTAL AND FASTENERS LOCATED BS767 TO BS787 AT LEV
- [SDR SWAA2025092204253](https://openairdocs.org/sdr/SWAA2025092204253), Aug 13, 2025: STIFFENER. CRACKED. FWD CARGO COMPARTMENT 540 BULKHEAD VERTICAL STRUCTURE STIFFENER HAS CRACK STA 540 LBL 24.97. REPLACED BULKHEAD VERTICAL STIFFENER STA 540 LBL 24.97 ON FWD CARGO
- [SDR SWAA2025092203990](https://openairdocs.org/sdr/SWAA2025092203990), Aug 13, 2025: RIB. CRACKED. CRACKED HORIZONTAL STAB INSPAR RIB HSS 129.50, 26 INCHS OF THE FRONT SPAR. PERFORMED PERMANENT RIB REPAIR IAW SRM 55-10-09-2R-5, REPAIR 5.
- [SDR SWAA2025092204239](https://openairdocs.org/sdr/SWAA2025092204239), Aug 13, 2025: FLOOR PANEL. DELAMINATED. DELAMINATED FLOOR PANEL 221DF AT PASSENGER CABIN. REPLACED THE FLOOR PANEL 221DF IAW AMM-53-21-00-401.
- [SDR SWAA2025092204240](https://openairdocs.org/sdr/SWAA2025092204240), Aug 13, 2025: FLOOR PANEL. DELAMINATED. DELAMINATED FLOOR PANEL 221CF AT PASSENGER CABIN. REPLACED FLOOR PANEL 221CF AT PASSENGER CABIN IAW B737-700 AMM-53-21-00-401 FOR INSTALLATION SEE TTG8Q0147YH1.
- [SDR SWAA2025092303342](https://openairdocs.org/sdr/SWAA2025092303342), Aug 12, 2025: STUB FRAME. CRACKED. CRACK INDICATION FOUND ON STUB FRAME LOCATED ON BS 296.5 BTW S8R - 9R AT FWD GALLEY DOOR AREA. REPLACED STUB FRAME IAW SRM 51-40-02-0G-0, AND DWG 141A8370, SHEE
- [SDR SWAA2025092203341](https://openairdocs.org/sdr/SWAA2025092203341), Aug 12, 2025: BEAR STRAP. CRACKED. CRACK INDICATION FOUND ON BEAR STRAP LOCATED BS 294.5 BETWEEN S-8R TO S-9R AT FWD GALLEY DOOR AREA. REPAIRED IAW SRM 53-10-01-2R-6 AND EA M-25-153-01539.
- [SDR SWAA2025092203678](https://openairdocs.org/sdr/SWAA2025092203678), Aug 12, 2025: FLOOR PANEL. PEELING. PEELED SURFACE ON FLOOR PANEL 120BF INCLUDING FLOOR PANEL 120CF FWD CARGO COMPARTMENT. APPLIED PROTECTIVE TREATMENT ON FLOOR PANEL 120BF AND 120CF IAW SRM 51-20
- [SDR SWAA2025092303058](https://openairdocs.org/sdr/SWAA2025092303058), Aug 11, 2025: WEB. CORRODED. CORROSION WEB INDICATORS FUEL LOCATED INTERNAL CAVITY LEADING EDGE AT RT WING. PERFORMED PERMANENT REPAIR ON WEB INDICATION OF FUEL SYSTEM PANEL IAW EA 25-157-0
- [SDR SWAA2025092303340](https://openairdocs.org/sdr/SWAA2025092303340), Aug 11, 2025: SCUFF PLATE. CRACKED. CRACK AFT CORNER SCUFF PLATE IN AFT CARGO BAY. REPAIRED AFT CORNER SCUFF PLATE IAW SRM 53-60-15-2R-1, REPAIR 1, PARAGRAPH 4. B, STEPS 2 AND 4 - 7.
- [SDR SWAA2025092300276](https://openairdocs.org/sdr/SWAA2025092300276), Aug 10, 2025: GLOWSTRIP. CRACKED. CRACK ON PHOTOLUMINESCENT STRIP, RT PASSENGER CABIN. REPLACED THE PHOTOLUMINESCENT STRIP IAW AMM-33-51-15-400-802.
- [SDR SWAA2025092300275](https://openairdocs.org/sdr/SWAA2025092300275), Aug 10, 2025: GLOWSTRIP. CRACKED. CRACKS ON PHOTOLUMINESCENT STRIP, LT PASSENGER CABIN. REPLACED PHOTOLUMINESCENT STRIP IAW AMM-33-51-15-400-802.
- [SDR SWAA2025092300043](https://openairdocs.org/sdr/SWAA2025092300043), Aug 10, 2025: LENS. BROKEN. BROKEN BASE OF EXIT LIGHT. REPLACED EXIT LIGHT ASSY LENS IAW AMM-33-51-01-960-802, STEP 3 C.
- [SDR SWAA2025092300049](https://openairdocs.org/sdr/SWAA2025092300049), Aug 10, 2025: LENS. BROKEN. BROKEN BASE EXIT LIGHT ASSY. AFT GALLEY AREA. REPLACED EXIT LIGHT ASSY LENS IAW AMM-33-51-01-960-802 STEP 3.C.
- [SDR SWAA2025092300048](https://openairdocs.org/sdr/SWAA2025092300048), Aug 10, 2025: LENS. BROKEN. BROKEN BASE EXIT LIGHT ASSY AT LAVATORY A. REPLACED EXIT LIGHT ASSY LENS IAW AMM-33-51-01-960-802 STEP 3.C.
- [SDR SWAA2025092300047](https://openairdocs.org/sdr/SWAA2025092300047), Aug 10, 2025: LENS. BROKEN. BROKEN BASE EXIT LIGHT ASSY AT GALLEY 1. REPLACED EXIT LIGHT ASSY LENS IAW AMM-33-51-01-960-802 STEP 3.C. (

All 202: https://openairdocs.org/aircraft/N7751A/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

## 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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