# N7745A: 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 CFM56-7B22 series](https://openairdocs.org/engine/cfm-international-cfm56-7b22-series) (registry code 13043)
- Serial number: 33933
- Year built: 2007
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: May 24, 2007
- Certificate issued: August 28, 2014
- Expires: August 31, 2027
- Mode S code: AA7AEB
- 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=7745A
- Page: https://openairdocs.org/aircraft/N7745A

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 N7745A.

## FAA accident and incident reports

None matched to N7745A.

## Service difficulty reports (205, 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 SWAA2025121249009](https://openairdocs.org/sdr/SWAA2025121249009), Dec 9, 2025: SEAT BACK. OUT OF ADJUST. SEAT BACK 11D RECLINES INTO EMERGENCY EXIT ROW. SECURED THE RECLINE LOCK AT SEAT BACK 11D IAW CMM 25-43-67.
- [SDR SWAA2025121244184](https://openairdocs.org/sdr/SWAA2025121244184), Dec 9, 2025: SEAT BACK. OUT OF ADJUST. SEAT BACK 11D RECLINES INTO EMERGENCY EXIT ROW. SECURED THE RECLINE LOCK ON SEAT BACK 11D IAW CMM 25-43-67.
- [SDR SWAA2025100320268](https://openairdocs.org/sdr/SWAA2025100320268), Oct 1, 2025: BATTERY PACK. INOPERATIVE. OVH EXIT SIGN INOPERATIVE. REPLACED BATTERY PACK REF 33-51-06 AMM . OPS CK GOOD
- [SDR SWAA2025031095656](https://openairdocs.org/sdr/SWAA2025031095656), Feb 13, 2025: BRACKET. CRACKED. CRACK BRACKET LOCATED BS540 AND RBL7 AT CENTER WING BOX 2025-110686 CRACK BRACKET LOCATED BS540 AND LBL7 AT CENTER WING BOX<[01] REPLACED BRACKET LOCATED BS540 
- [SDR SWAA2025031095427](https://openairdocs.org/sdr/SWAA2025031095427), Feb 12, 2025: INTERCOSTAL. CRACKED. CUSTOMER REQUEST AAI INSPECTION: MAIN CABIN; FLOOR STRUCTURE HAS CRACK AT STA 540 BL0 TO LBL 24.75 2025-110798 <[01]. REPLACED INTERCOSTAL WEB AND FASTENERS LOC
- [SDR SWAA2025031094214](https://openairdocs.org/sdr/SWAA2025031094214), Feb 8, 2025: ACCESS PANEL. CRACKED. CRACK SEAL - PLATE ACCESS PANEL 343AB AT RT HORIZONTAL STAB 2025-110734<[01] REPLACED SEAL - PLATE ACCESS PANEL 343AB AT RT HORIZONTAL STAB IAW B737-700 SRM 51-
- [SDR SWAA2025031093915](https://openairdocs.org/sdr/SWAA2025031093915), Feb 6, 2025: SKIN PANEL. CRACKED. CRACK INDICATION FOUND ON RT HORIZONTAL STABILIZER LOWER SKIN PANEL. LOCATED AT STAB STA 193.9 RIB AND 8.0 INCH. FROM FRONT SPAR. INBOARD SIDE OF RIB. CRACK LEN
- [SDR SWAA2025031093738](https://openairdocs.org/sdr/SWAA2025031093738), Feb 6, 2025: PLATE. CRACKED. CRACK CORRUGATED PLATE TRAILING EDGE LOCATED ORSS 422 AT LT WING 2025-110659<[01] REPLACED CORRUGATED PLATE LOCATED ORSS 422 AT LT WING IAW B737-700 SRM 51-10-0
- [SDR SWAA2025031093556](https://openairdocs.org/sdr/SWAA2025031093556), Feb 5, 2025: WEB. CRACKED. CRACK ON WEB FWD GALLEY AREA AT LEVEL STR 17R BS 294.5 2025-110634<[01] REPLACED WEB LOC. BTW 291.5 TO BS 332.2 AT LEVEL STR 17R FWD GALLEY AREA IAW B737-700 SR
- [SDR SWAA2025031093375](https://openairdocs.org/sdr/SWAA2025031093375), Feb 5, 2025: NUT PLATE. CORRODED. CORROSION LEADING EDGE RAIL NUTPLATE LOCATED OFSS449 AT RT WING 2025-110631<[01] REPLACED RAIL NUTPLATE LOCATED OFSS449 AT RT WING ON LEADING EDGE IAW B737-700 
- [SDR SWAA2025031093374](https://openairdocs.org/sdr/SWAA2025031093374), Feb 5, 2025: RIB. CRACKED. CRACK ACCESS PANEL 331B LEADING EDGE RIB LOCATED LE STA 95.96 AT LT HORIZONTAL STABILIZER 2025-110625<[01] REPLACED RIB LOCATED ACCESS PANEL 331B LEADING EDGE L
- [SDR SWAA2025031093555](https://openairdocs.org/sdr/SWAA2025031093555), Feb 5, 2025: PLATE. CRACKED. CRACK CORRUGATED PLATE TRAILING EDGE LOCATED ORSS451 AT RT WING 2025-110633<[01] REPLACED CORRUGATED PLATE AND FASTENERS TRAILING EDGE LOCATED ORSS451 AT RT WIN
- [SDR SWAA2025031092940](https://openairdocs.org/sdr/SWAA2025031092940), Feb 4, 2025: SUPPORT. CORRODED. CORROSION SUPPORT ZEE LOCATED BETWEEN BS727 TO BS847 LBL21 AND WL156 AFT CARGO COMPARTMENT 2025-110533 <[01]. REPLACED SUPPORT ZEE LOCATED BETWEEN BS727 TO BS84
- [SDR SWAA2025031092941](https://openairdocs.org/sdr/SWAA2025031092941), Feb 4, 2025: SUPPORT. CORRODED. CORROSION SUPPORT ZEE LOCATED BETWEEN BS727D TO BS787 RBL21 AND WL156 AFT CARGO COMPARTMENT 2025-110534 CORROSION SUPPORT ZEE LOCATED BETWEEN BS727D TO BS767 RB
- [SDR SWAA2025031093189](https://openairdocs.org/sdr/SWAA2025031093189), Feb 4, 2025: BRACKET. DETERIORATED. DETERIORATED HARDWARE GIRT BAR FLOOR BRACKETS SIDE ENTRY AND SERVICE AT FWD GALLEY AREA 2025-110611<[01]. REPLACED HARDWARE GIRT BAR FLOOR BRACKETS SIDE ENTRY A
- [SDR SWAA2025031093190](https://openairdocs.org/sdr/SWAA2025031093190), Feb 4, 2025: BRACKET. DETERIORATED. DETERIORATED HARDWARE GIRT BAR FLOOR BRACKETS SIDE ENTRY AND GALLEY AT AFT GALLEY AREA 2025-110612 <[01]. REPLACED HARDWARE GIRT BAR FLOOR BRACKETS SIDE ENTRY A
- [SDR SWAA2025031092767](https://openairdocs.org/sdr/SWAA2025031092767), Feb 3, 2025: WEB. CRACKED. CRACK INDICATION ON HORIZONTAL PRESSURE DECK BETWEEN STA. 663 TO STA. 675 LBL 30. CRACK LENGTH 0.875 IN. PASSENGER CABIN 2025-110513 <[01]. TOOL USED ON STEP 5;
- [SDR SWAA2025031092764](https://openairdocs.org/sdr/SWAA2025031092764), Feb 3, 2025: DOOR FRAME. CRACKED. CRACK INDICATION ON STUB FRAME LOCATED ON BS 296.5 BTW S-8R TO S-9R AT FWD GALLEY DOOR AREA CRACK LENGTH 0.312 IN. APROX.AT PASSENGER CABIN 2025-110503<[01] REP
- [SDR SWAA2025031092771](https://openairdocs.org/sdr/SWAA2025031092771), Feb 3, 2025: STUB FRAME. CRACKED. CRACK FRAME STUB LOCATED ON BS 294.5 AT LEVEL STR 17R AT PASSENGER CABIN 2025-110507<[01] EQUIPMENT P/N PHASEC 3D; S/N 800YBRK; DUE DATE 16-JUL-25 WAS USED ON S
- [SDR SWAA2025031092765](https://openairdocs.org/sdr/SWAA2025031092765), Feb 3, 2025: WEB. CRACKED. CRACK WEB BTW BS 294.5 TO BS 303.9 AT LEVEL STR 16L AT PASSENGER CABIN 2025-110509<[01] REPLACED INTERCOSTAL WEB LOCATED BTW BS 294.5 TO BS 303.9 AT LEVEL STR 1
- [SDR SWAA2025031092772](https://openairdocs.org/sdr/SWAA2025031092772), Feb 3, 2025: SUPPORT ANGLE. CRACKED. CRACK SUPPORT ANGLE ON BS 685 PLUS 6 INCHES ON BL 0 AT PASSENGER CABIN 2025-110515<[01] TOOLS USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811020; 
- [SDR SWAA2025031092766](https://openairdocs.org/sdr/SWAA2025031092766), Feb 3, 2025: STRINGER CLIP. CRACKED. CRACK TIE CLIP ON BS 277 AT STR 10R AT PASSENGER CABIN 2025-110510<[01] REPLACED TIE CLIP LOC.ON BS 277 AT STR 10R AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 
- [SDR SWAA2025031092350](https://openairdocs.org/sdr/SWAA2025031092350), Feb 2, 2025: FLOOR PANEL. CRACKED. CRACK FLOOR PANEL 140BF AT AFT CARGO COMPARTMENT 2025-110408 <[01]. REPLACED FLOOR PANEL 140BF AT AFT CARGO COMPARTMENT IAW B737-700 AMM 25-52-01-201-801; B737-
- [SDR SWAA2025031091983](https://openairdocs.org/sdr/SWAA2025031091983), Feb 1, 2025: SCUFF PLATE. CRACKED. CRACK AFT CORNER SCUFF PLATE AT FWD CARGO COMPARTMENT 2025-110375<[01] TOOL USED DIGITAL CALIPER P/N: 500-196-30 S/N: B23399190; DUE DATE: 04-MAR-25.;[02] TOOL 
- [SDR SWAA2025031091880](https://openairdocs.org/sdr/SWAA2025031091880), Jan 31, 2025: FLOOR PANEL. CRACKED. CRACK FLOOR PANEL 140CF AT AFT CARGO COMPARTMENT 2025-110336 <[01]. REPLACED FLOOR PANEL 140CF LOCATED AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 SRM 51
- [SDR SWAA2024091636197](https://openairdocs.org/sdr/SWAA2024091636197), Sep 10, 2024: BRACKET. SEPARATED. L/H ENGINE LOW PRESSURE TURBINE CASE COOLING TUBE SUPPORT ANGLE BRACKET; AT 4 OCLOCK POSITION; FORWARD FLANGE IS SEPARATED (SHEARED) FROM BRACKET. REMOVED AND R
- [SDR SWAA2024091235883](https://openairdocs.org/sdr/SWAA2024091235883), Sep 10, 2024: FLOOR SUPPORT. CRACKED. FORWARD CARGO A/C DISTRIBUTION BAY; FLOOR INTERCOSTAL CRACKED AT STATION 540 JUST RIGHT OF PASSENGER CABIN FLOOR CENTERLINE. (SEE PICTURES)<[01] REMOVED RH INTE
- [SDR SWAA2024061299737](https://openairdocs.org/sdr/SWAA2024061299737), Jun 8, 2024: LIGHT. MALFUNCTIONED. F/AS ADVISED OVERHEAD EXIT SIGN IN OVERWING EMERGENCY EXIT ROW IS FLICKERING<[01] PERFORMED EMERGENCY EXIT LIGHT OPERATION TEST PER AMM33-51-00. NO DEFECT NOTED
- [SDR SWAA2023121431606](https://openairdocs.org/sdr/SWAA2023121431606), Dec 14, 2023: BATTERY PACK. NO TEST. M1669 FAILED CAPACITY CHECK<[01] R/R M1669 BATTERY PACK PER AMM 33-51-06
- [SDR SWAA2023031414508](https://openairdocs.org/sdr/SWAA2023031414508), Mar 9, 2023: ANGLE. CRACKED. CRACK ANGLE TRAILING EDGE LOCATED AT FIXED ACCESS PANEL LOWER AREA AT LT WING 2023-119652<[01] TOOL USED CALIPER P/N: 500-196-30:; S/N: A21126170; DUE DATE: 09-
- [SDR SWAA2023031504389](https://openairdocs.org/sdr/SWAA2023031504389), Feb 17, 2023: INTERCOSTAL. CRACKED. CRACK WEB - INTERCOSTAL LOCATED ON FLOOR STRUCTURE BTW BS277 AND BS294.5 ON BL0 AT FWD GALLEY AREA 2023-119601<[01] REPLACED WEB AND FASTENERS LOCATED ON FLOOR 
- [SDR SWAA2023031503874](https://openairdocs.org/sdr/SWAA2023031503874), Feb 16, 2023: INTERCOSTAL. CRACKED. CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BTW BS 280 TO BS 294.T RBL 5 FWD GALLEY AND LAV 2023-119580<[01] OPEN FAULT HAS AN ERROR AND IS BEING CORRECTED 
- [SDR SWAA2023031503875](https://openairdocs.org/sdr/SWAA2023031503875), Feb 16, 2023: INTERCOSTAL. CRACKED. CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BTW BS 344 TO BS 360 RBL 4 FWD GALLEY AND LAV 2023-119582FLOOR STRUCTURE EXACTLY LOCATION BTW BS 344 TO BS 360 B
- [SDR SWAA2023031503892](https://openairdocs.org/sdr/SWAA2023031503892), Feb 16, 2023: ANGLE. CRACKED. CRACK ANGLE LOCATED BS947.5 AND S-26L AFT CARGO COMPARTMENT 2023-119581<[01] REPLACED ANGLE AND FASTENERS LOCATED BS947.5 AND S-26L AT AFT CARGO COMPARTMENT IAW
- [SDR SWAA2023031503893](https://openairdocs.org/sdr/SWAA2023031503893), Feb 16, 2023: ANGLE. CRACKED. CRACK ANGLE LOCATED BS 907 TO BS 927 BETWEEN S27R TO S-25R AFT POSITION AFT CARGO COMPARTMENT 2023-119581<[01] REPLACED ANGLE LOCATED BETWEEN BS907 TO BS927 AND
- [SDR SWAA2023031503891](https://openairdocs.org/sdr/SWAA2023031503891), Feb 16, 2023: SUPPORT. CRACKED. CRACK ANGLE - SUPPORT LOCATED BS 727 BETWEEN S-27LTO S-27R AFT CARGO COMPARTMENT 2023-119578<[01] REPLACED ANGLE SUPPORT LOCATED BS 727 BETWEEN S-27LTO S-27R AF
- [SDR SWAA2023031503883](https://openairdocs.org/sdr/SWAA2023031503883), Feb 16, 2023: WEB. ELONGATED. ELONGATED HOLE WEB LOCATED BTW BS 1006 TO BS 1016 AT AFT GALLEY AREA 2023-119598<[01] REPLACED WEB AND FASTENERS LOCATED BTW BS 986.5 TO BS 1016 AT AFT GALLEY A
- [SDR SWAA2023031503887](https://openairdocs.org/sdr/SWAA2023031503887), Feb 16, 2023: INTERCOSTAL. CORRODED. CORROSION WEB - INTERCOSTAL LOCATED BS847 TO BS 867 AND S-25R WL 156 AT AFT CARGO COMPARTMENT 2023-119595 CORROSION WEB - INTERCOSTAL LOCATED BS847 TO BS 867 AN
- [SDR SWAA2023031503884](https://openairdocs.org/sdr/SWAA2023031503884), Feb 16, 2023: STRAP. CORRODED. CORROSION STRAP LOCATED BS 787 TO BS 794.5 AND S-25R WL 156 AT AFT CARGO COMPARTMENT 2023-119591<[01] REPLACED STRAP LOCATED BS 787 TO BS 794.5 AND S-25R WL 156
- [SDR SWAA2023031503878](https://openairdocs.org/sdr/SWAA2023031503878), Feb 16, 2023: STRAP. CORRODED. CORROSION STRAP LOCATED BS 847 TO BS 857 AND S-25R WL 156 AT AFT CARGO COMPARTMENT 2023-119594<[01] REPLACED STRAP LOCATED BS 847 TO BS 857 AND S-25R WL 156 AT 
- [SDR SWAA2023031503879](https://openairdocs.org/sdr/SWAA2023031503879), Feb 16, 2023: ANGLE. CORRODED. CORROSION ANGLE LOCATED BS 767 TO BS 787 AND S-25R WL 156 AT AFT CARGO COMPARTMENT 2023_119593<[01] REPLACED ANGLE LOCATED BS 767 TO BS 787 AND S-25R WL 156 AT 
- [SDR SWAA2023031503880](https://openairdocs.org/sdr/SWAA2023031503880), Feb 16, 2023: INTERCOSTAL. CORRODED. CORROSION WEB - INTERCOSTAL LOCATED BS767 TO BS 787 AND S-25R WL 156 AT AFT CARGO COMPARTMENT 2023_119592<[01] REPLACED WEB-INTERCOSTAL (SHIELD) LOCATED ON BS 7
- [SDR SWAA2023031503886](https://openairdocs.org/sdr/SWAA2023031503886), Feb 16, 2023: STRAP. CORRODED. CORROSION STRAP LOCATED BS 807 AND S-25R WL 156 AT AFT CARGO COMPARTMENT 2023-119585<[01] REPLACED STRAP LOCATED BS 767 TO 867 AND S-25R WL 156 AT AFT CARGO COM
- [SDR SWAA2023031503889](https://openairdocs.org/sdr/SWAA2023031503889), Feb 16, 2023: SUPPORT. CORRODED. CORROSION SUPPORT ZEE LOCATED BS 727 TO BS 767 AND S-25R WL 156 AT AFT CARGO COMPARTMENT 2023-119584<[01] REPLACED SUPPORT ZEE AND FASTENERS LOCATED BS 727 TO B
- [SDR SWAA2023031503890](https://openairdocs.org/sdr/SWAA2023031503890), Feb 16, 2023: SUPPORT. CORRODED. CORROSION SUPPORT ZEE LOCATED BS 727 TO B 847 AND S-25L WL 156 AT AFT CARGO COMPARTMENT 2023-119583<[01] REPLACED SUPPORT ZEE LOCATED BS 727 TO B 847 AND S-25L 
- [SDR SWAA2023031503885](https://openairdocs.org/sdr/SWAA2023031503885), Feb 16, 2023: INTERCOSTAL. CORRODED. CORROSION WEB - INTERCOSTAL LOCATED BS 794.5 TO BS 807 AND S-25R WL 156 AT AFT CARGO COMPARTMENT 2023-119590<[01] TOOL USED: ULTRASONIC THICKNESS GAUGE; PN: 45M
- [SDR SWAA2023031503516](https://openairdocs.org/sdr/SWAA2023031503516), Feb 16, 2023: STRAP. CORRODED. CORROSION STRAP LOCATED AT BS 767 PLUS 5 INCHES BETWEEN S-25R AND S-25L WL 156 AT AFT CARGO COMPARTMENT 2023-119577<[01] REPLACED STRAP LOCATED AT BS 767 PLUS 5
- [SDR SWAA2023031502971](https://openairdocs.org/sdr/SWAA2023031502971), Feb 14, 2023: FLOOR PANEL. BROKEN. BROKEN FLOOR PANEL 222AF AT PASSENGER CABIN 2023-119541<[01] TOOL USED CALIPER P/N: 500-197-30; S/N:B20189526; DUE DATE:20-DEC-23.;[02] TOOL USED: HOT BONDER P/
- [SDR SWAA2023031502973](https://openairdocs.org/sdr/SWAA2023031502973), Feb 14, 2023: ANGLE. CRACKED. CRACK ON SUPPORT ANGLE LOCATED BS 847 BTW STR 2R TO STR 3R AT PASSENGER CABIN 2023-119544<[01] REPLACED SUPPORT ANGLE AND FASTENERS LOCATED BS 847 BTW STR 2R TO
- [SDR SWAA2023031502974](https://openairdocs.org/sdr/SWAA2023031502974), Feb 14, 2023: ANGLE. CRACKED. CRACK ON SUPPORT ANGLE LOCATED BS 867 BTW STR 2R TO STR 3R AT PASSENGER CABIN 2023-119545<[01] REPLACED SUPPORT ANGLE LOCATED BS 867 BTW STR 2R TO STR 3R AT PAS

All 205: https://openairdocs.org/aircraft/N7745A/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 N7745A

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N7745A before.

- [Cancelled 1956-12-18](https://openairdocs.org/deregistered/N7745A-1956-12-18): Cessna 180, S/N 32642. 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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