# N7738A: 2006 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: 33930
- Year built: 2006
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: September 12, 2012
- Certificate issued: October 3, 2012
- Expires: October 31, 2028
- Mode S code: AA779D
- 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=7738A
- Page: https://openairdocs.org/aircraft/N7738A

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 N7738A.

## FAA accident and incident reports

None matched to N7738A.

## Service difficulty reports (255, 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 SWAA2026060809478](https://openairdocs.org/sdr/SWAA2026060809478), Jun 4, 2026: FLAP SYSTEM. FAULTED. ON APPROACH TO PVR HAD T/E FLAP DISAGREEMENT WHEN FLAP LEVER WAS SET TO POSITION 5. RAN QRH CHECKLIST. CW FSEU BITE WITH NO CURRENT OR EXISTING FAULTS PER FIM 2
- [SDR SWAA2026052204558](https://openairdocs.org/sdr/SWAA2026052204558), May 19, 2026: COVER. MISSING. EMERGENCY EXIT LIGHT COVER LOWER LEFT SIDE MISSING. INSTALLED EMERGENCY EXIT LIGHT COVER ON LOWER LEFT SIDE OF RH EMERGENCY EXIT DOOR PER AMM 33-51-01.
- [SDR SWAA2026051898217](https://openairdocs.org/sdr/SWAA2026051898217), May 13, 2026: BATTERY. CORRODED. FWD MEGA PHONE BATTERIES ARE CORRODED.<[01] REPLACED FWD MEGA PHONE BATTERIES I.A.W AMM 25-64-00. OPS CHECKS GOOD.
- [SDR SWAA2026050493463](https://openairdocs.org/sdr/SWAA2026050493463), Apr 28, 2026: SLIDE. OUT OF ADJUST. R 1 DOOR SLIDE Z FOLD FOR COVER IS INCORRECT NEEDS ADJUSTMENT. VERIFIED ADJUSTMENT OF Z FOLD IN TO R1 CORRECT POSITION IAW AMM 25-66-00;[02] ADJUSTED R1 DOOR SL
- [SDR SWAA2026040786286](https://openairdocs.org/sdr/SWAA2026040786286), Apr 4, 2026: LAMP. INOPERATIVE. EMERGENCY EXIT LIGHT AT ROW 15 FED INOPERATIVE. REPLACED THE LAMP AT THE OVERWING EXIT LIGHT ROW 15DEF IAW AMM 33-21-00, OPS CHECKED GOOD.
- [SDR SWAA2026040786285](https://openairdocs.org/sdr/SWAA2026040786285), Apr 4, 2026: LAMP. INOPERATIVE. EMERGENCY EXIT LIGHT AT ROW 14 CB INOPERATIVE. REPLACED THE LAMP AT THE OVERWING EXIT LIGHT ROW 14ABC IAW AMM 33-21-00. OPS CHECKED GOOD.
- [SDR SWAA2026040285015](https://openairdocs.org/sdr/SWAA2026040285015), Mar 30, 2026: SLIDE. LOW PRESSURE. FWD SERVICE ESCAPE SLIDE PRESSURE IN RED. REPLACED FWD SERVICE DOOR EMERGENCY SLIDE ASSEMBLY WITH A SERVICEABLE UNIT IAW AMM 25-66-01 AND MT 725-61-06 AS REQUIR
- [SDR SWAA2026032380289](https://openairdocs.org/sdr/SWAA2026032380289), Mar 17, 2026: LENS. DETACHED. EMERGENCY EXIT LIGHTING LENS COVER AT ROW 23ABC CAME OFF. OK TO CONTINUE PER MEL 25-10-01. LIGHT STILL FULLY FUNCTIONAL. INSTALLED ROW 23ABC EMERGENCY AREA LIGH
- [SDR SWAA2026030275216](https://openairdocs.org/sdr/SWAA2026030275216), Feb 27, 2026: LENS. MISSING. 23 ABC EMERGENCY LIGHT COVER MISSING. EMERG LIGHT LENS AT 22ABC - 23ABC IS ON MEL.
- [SDR SWAA2026022674338](https://openairdocs.org/sdr/SWAA2026022674338), Feb 25, 2026: LENS. MISSING. EMERGENCY LIGHT LENS ON OVERHEAD BIN BETWEEN 22ABC & 23ABC MISSING. OK TO CONT PER MEL 25-10-01 SP1B. REPLACED LENS IAW AMM 33-51-03. OP CHECK GOOD. THIS CLEARS
- [SDR SWAA2025121246012](https://openairdocs.org/sdr/SWAA2025121246012), Dec 9, 2025: LIGHT. LOOSE. PASSENGER CABIN SEAT ROW 1 DEF PHOTOILLUM STRIP LOOSE AT RT FWD WINDSCREEN. SECURED THE STRIP IAW AMM 33-51-03.
- [SDR SWAA2025121243990](https://openairdocs.org/sdr/SWAA2025121243990), Dec 9, 2025: LIGHT. LOOSE. PASSENGER CABIN SEAT ROW 1 DEF PHOTOILLUM STRIP LOOSE AT RIGHT FWD WIND SCREEN. SECURED LOOSE CABIN PHOTOILLUM STRIP IAW AMM 33-51-03.
- [SDR SWAA2025092416768](https://openairdocs.org/sdr/SWAA2025092416768), Sep 21, 2025: LIGHT. INOPERATIVE. ROW 1DEF PHOTOLUMINESCENT STRIP INOPERATIVE. REMOVED AND REPLACED IAW AMM 33-51-15-201-NG.
- [SDR SWAA2025030400451](https://openairdocs.org/sdr/SWAA2025030400451), Feb 28, 2025: FITTING. CRACKED. LEFT CENTER GEAR DOOR CRACKED AT FWD FITTING <[01]. REMOVED L/H CTR/INNER GEAR DOOR ASSY. I.A.W. AMM 32-13-11 OK TO CONTINUE SERVICE PER CDL 32-10-3 XC.
- [SDR SWAA2024102953903](https://openairdocs.org/sdr/SWAA2024102953903), Oct 26, 2024: COVER. LOOSE. EMERGENCY EXIT LIGHT COVER LEFT SIDE OFF<[01] RESECURED CAPT SIDE EMER EXIT LIGHT COVER PER SIP.
- [SDR SWAA2024101647568](https://openairdocs.org/sdr/SWAA2024101647568), Oct 12, 2024: COVER. OUT OF ADJUST. PAX CABIN LEFT AFT SERVICE DOOR SLIDE COVER RUBBING AGAINST TO DOOR SCUFF PLATE TO CLOSE POSITION. 2024-565673<[01] INSTALLED CORRECTLY DOOR SLIDE COVER GIRT I.
- [SDR SWAA2024101647567](https://openairdocs.org/sdr/SWAA2024101647567), Oct 12, 2024: HANDLE. LOOSE. PAX CABIN AFT RIGHT SERVICE DOOR LINING ;ASSISTANT HANDLE LOOSE. 2024-565671<[01] INSTALLED CORRECTLY ASSISTANT HANDLE PAX CABIN AFT RIGHT SERVICE DOOR LINING I
- [SDR SWAA2024101647581](https://openairdocs.org/sdr/SWAA2024101647581), Oct 12, 2024: LIGHT. INOPERATIVE. EXTERIOR FUSELAGE FWD AREA RIGHT EMERGENCY LIGHT INOP 2024-565696<[01] REPLACED EXTERIOR FUSELAGE FWD AREA RIGHT EMERGENCY LIGHT IAW B737-700 AMM 33-51-04-960-8
- [SDR SWAA2024101647570](https://openairdocs.org/sdr/SWAA2024101647570), Oct 12, 2024: HANDLE. LOOSE. PAX CABIN AFT ENTRY AREA AFT LEFT BULKHEAD O/B SIDE OF FA SEAT ;ASSISTANT HANDLE LOOSE 2024-565682<[01] INSTALLED CORRECTLY ASSIT HANDLE ON PAX CABIN AFT ENTRY 
- [SDR SWAA2024101644930](https://openairdocs.org/sdr/SWAA2024101644930), Oct 4, 2024: SEAT. OUT OF ADJUST. RECLINE SEAT 11C EMERGENCY EXIT PASSENGER SEAT 2024-565614<[01] PERFORMED ADJUSTMENT ON PASSENGER SEAT 11C EMERGENCY EXIT PASSENGER SEAT IAW CMM 25-21-45 B/E AE
- [SDR SWAA2024101644929](https://openairdocs.org/sdr/SWAA2024101644929), Oct 3, 2024: RIB. CRACKED. CRACK ON INSPAR RIB 129.50 MORE 34 INCH FROM TO FRONT SPAR RT HORIZONTAL STABILIZER 2024-565613<[01] TOOL USED ON STEP 3 AND 4:EDDY CURRENT FLAW DETECTOR P/N:NO
- [SDR SWAA2024101642350](https://openairdocs.org/sdr/SWAA2024101642350), Sep 27, 2024: FLOOR SUPPORT. CRACKED. CRACK ON HOLE OF INTERCOSTAL LOCATED BS 251.6 AND LBL 16 FLIGHT DECK FLOOR 2023-565606<[01] REPLACED INTERCOSTAL LOCATED BTW BS 251.6 AND LBL 15.3 AT LBL 24.7 F
- [SDR SWAA2024101641390](https://openairdocs.org/sdr/SWAA2024101641390), Sep 24, 2024: WEB. CRACKED. CRACK FLOOR STRUCTURE WEB STA 291.5 TO STA 332.10 AT LEVEL OF STR17R AT FWD GALLEY AREA 2024-565603<[01] REPLACED WEB STA 291.5 TO STA 332.10 AT LEVEL OF STR17R
- [SDR SWAA2024101639384](https://openairdocs.org/sdr/SWAA2024101639384), Sep 20, 2024: VAPOR BARRIER. CRACKED. CRACK INDICATION FOUND ON VAPOR BARRIER LOWER WEB AT BS 663 AND LBL 50 CRACK LENGTH IS 5 INCH 2024-565593<[01] TOOL USED: CALIPER P/N: 500-197-30; S/N: A2402853
- [SDR SWAA2024101637137](https://openairdocs.org/sdr/SWAA2024101637137), Sep 12, 2024: FLOOR SUPPORT. CORRODED. AAI-INSPECTION AFT CARGO COMPARTMENT; FLOOR SUPPORT BRACKET HAS CORROSION BWT STA 847 & STA 867; STR 25R 2024-565563<[01] REPLACED SUPPORT BRACKET AND FASTENER 
- [SDR SWAA2024101637138](https://openairdocs.org/sdr/SWAA2024101637138), Sep 12, 2024: FLOORBEAM. CRACKED. AAI-INSPECTION PASSENGER CABIN; FLOOR STRUCTURE SUPPORT HAS CRACK AT STA 540; BL 0 TO RBL 24.75 2024-565565<[01] REPLACED BRAKE CHANNEL LOCATED ON BS 540; BL 0 
- [SDR SWAA2024101637139](https://openairdocs.org/sdr/SWAA2024101637139), Sep 12, 2024: FLOOR SUPPORT. CRACKED. AAI-INSPECTION PASSENGER CABIN; FLOOR STRUCTURE SUPPORT HAS CRACK AT STA 540; BL 0 TO LBL 24.75 2024-565566<[01] REPLACED BRAKE CHANNEL LOCATED ON BS 540; BL 0 
- [SDR SWAA2024101637131](https://openairdocs.org/sdr/SWAA2024101637131), Sep 12, 2024: ACCESS PANEL. CRACKED. CRACK BLADE ACCESS PANEL 343AT AT RT HORIZONTAL STAB 2024-565546<[01] REPLACED BLADE ACCESS PANEL 343AT AT RT HORIZONTAL STAB IAW B737-700 SRM 51-40-02;[02] TAS
- [SDR SWAA2024101636640](https://openairdocs.org/sdr/SWAA2024101636640), Sep 11, 2024: ACCESS PANEL. CRACKED. CRACK ANGLE TRAILING EDGE ACCESS PANEL 651GB RT WING 2024-565519<[01] REPLACED ANGLE TRAILING EDGE ACCESS PANEL 651GB ON RT WING I.A.W B737-700 SRM 51-40-02 AND
- [SDR SWAA2024101636053](https://openairdocs.org/sdr/SWAA2024101636053), Sep 10, 2024: ANGLE. CRACKED. CRACK ANGLE TRAILING EDGE LOCATED ORSS 273 LT WING 2024-565491<[01] REPLACED ANGLE TRAILING EDGE LOCATED ORSS 273 LT WING IAW B737-700 SRM 51-40-02 AND B737-700
- [SDR SWAA2024101035684](https://openairdocs.org/sdr/SWAA2024101035684), Sep 9, 2024: PLACARD. DETERIORATED. DETERIORATED PLACARD CAUTION ESCAPE SLIDE ON SLIDE COVER FWD ENTRY DOOR (1EA) 2024-565485<
- [SDR SWAA2024101635238](https://openairdocs.org/sdr/SWAA2024101635238), Sep 7, 2024: BRACKET. CRACKED. CRACK SLAT 2 O/B AUXILIARY TRACK I/B SUPPORT ANGLE AT LT WING 2024-565422<[01] REPLACED BRACKET LOC. SLAT 2 O/B AUXILIARY TRACK I/B SUPPORT ANGLE AT LT WING I.A
- [SDR SWAA2024101634950](https://openairdocs.org/sdr/SWAA2024101634950), Sep 6, 2024: SUPPORT ANGLE. CRACKED. CRACK ANGLE - SUPPORT BS 727B AND LBL 52 CEILING AREA AFT CARGO COMPARTMENT 2024-565342<[01] STEP 6 TOOL USED EDDY CURRENT EQUIPMENT P/N: NORTEC 600D; S/N: 2101
- [SDR SWAA2024101634955](https://openairdocs.org/sdr/SWAA2024101634955), Sep 6, 2024: CARGO TRACK. CRACKED. CRACK TRACK RBBL 13.84 AND BS 747 AFT CARGO COMPARTMENT 2024-565348<[01] FAULT RESOLVED IN OTHER FAULT SEE TTG8Q00VPXBM;[02] CORRECTED ITEM 1: FAULT RESOLVED IN
- [SDR SWAA2024101634948](https://openairdocs.org/sdr/SWAA2024101634948), Sep 6, 2024: HANDLE. BROKEN. BROKEN DOOR LINING HANDLE AFT SERVICE DOOR AT AFT GALLEY AREA (1 EA) 2024-565228<[01] REPLACED DOOR LINING HANDLE AFT SERVICE DOOR AT AFT GALLEY AREA (1 EA) I.A
- [SDR SWAA2024101634954](https://openairdocs.org/sdr/SWAA2024101634954), Sep 6, 2024: CARGO TRACK. CRACKED. CRACK TRACK RBBL 13.84 AND BS 727E AFT CARGO COMPARTMENT 2024-565347<[01] TOOL USED ON STEP 4: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600D; S/N: 60009161631; D
- [SDR SWAA2024101634951](https://openairdocs.org/sdr/SWAA2024101634951), Sep 6, 2024: FLOORBEAM. CORRODED. CORROSION FLOOR BEAM LOCATED STA986.5 AND LBL43 WL208.1 AT AFT GALLEY AREA 2024-565332<[01] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600 D; S/N: 20004
- [SDR SWAA2024101634952](https://openairdocs.org/sdr/SWAA2024101634952), Sep 6, 2024: FLOORBEAM. CORRODED. CORROSION FLOOR BEAM LOCATED STA986.5 AND RBL33 TO RBL43 WL208.1 AT AFT GALLEY AREA 2024-565333<[01] TOOL USED IN STEP 5; TOOL USED: ULTRASONIC THICKNESS GAGES;
- [SDR SWAA2024101634956](https://openairdocs.org/sdr/SWAA2024101634956), Sep 6, 2024: CARGO TRACK. CRACKED. CRACK TRACK RBBL 13.84 AND BS 767 AFT CARGO COMPARTMENT 2024-565349<[01] FAULT RESOLVED IN OTHER FAULT SEE TTG8Q00VPXBM;[02] CORRECTED ITEM 1: FAULT RESOLVED IN
- [SDR SWAA2024101634958](https://openairdocs.org/sdr/SWAA2024101634958), Sep 6, 2024: BRACKET. CRACKED. CRACK FLOOR STRUCTURE BRACKET BS 947.5 AND STRINGER 25L AT AFT CARGO COMPARTMENT 2024-565352<[01] REPLACED FLOOR STRUCTURE BRACKET AND FASTENERS LOCATED BTW BS 
- [SDR SWAA2024101634957](https://openairdocs.org/sdr/SWAA2024101634957), Sep 6, 2024: SUPPORT ANGLE. CRACKED. CRACK ANGLE - SUPPORT BETWEEN BS 907 TO BS 927 STRINGER 25R AND STRINGER 27R AFT CARGO COMPARTMENT 2024-565351<[01] REPLACED ANGLE-SUPPORT (STIFFENER) AND FASTE
- [SDR SWAA2024101634869](https://openairdocs.org/sdr/SWAA2024101634869), Sep 6, 2024: ANGLE. CRACKED. CRACK SUPPORT STRUCTURE WING TO BODY FAIRING ANGLE BS 500D AT LEVEL STRINGER 19R AT LOWER FUSELAGE 2024-565327<[01] REPLACED SUPPORT STRUCTURE WING TO BODY FAIR
- [SDR SWAA2024101634870](https://openairdocs.org/sdr/SWAA2024101634870), Sep 6, 2024: ANGLE. CRACKED. CRACK SUPPORT STRUCTURE WING TO BODY FAIRING ANGLE BS 500D AT LEVEL STRINGER 19L AT LOWER FUSELAGE 2024-565328<[01] REPLACED SUPPORT STRUCTURE WING TO BODY FAIR
- [SDR SWAA2024101634640](https://openairdocs.org/sdr/SWAA2024101634640), Sep 5, 2024: STUB FRAME. CRACKED. CRACK STUB FRAME LOCATED STA294.5 AND STR17R AT PASSENGER CABIN 2024-565307<[01] EQUIPMENT P/N PHASEC 3D; S/N 587435/07; DUE DATE 20-MAR-25 WAS USED ON STEP 7;[
- [SDR SWAA2024101634644](https://openairdocs.org/sdr/SWAA2024101634644), Sep 5, 2024: STUB FRAME. CRACKED. CRACK INDICATIONS ON STUB FRAME LOCATED ON BS 294.5 BTW S-8R T O S-9R (2 EA) AT FWD GALLEY DOOR AREA CRACKS LENGTH 0.312 IN.AT PASSENGER CABIN 2024-565314<[01] 
- [SDR SWAA2024101634457](https://openairdocs.org/sdr/SWAA2024101634457), Sep 5, 2024: SUPPORT ANGLE. CRACKED. CRACK SUPPORT ANGLE LOCATED STA695 AND LBL24.75 CENTER SECTION 2024-565246<[01] TOOL USED: TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 14282005 DUE DATE 22 JA
- [SDR SWAA2024101634637](https://openairdocs.org/sdr/SWAA2024101634637), Sep 5, 2024: INTERCOSTAL. CRACKED. CRACK WEB INTERCOSTAL LOCATED BETWEEN STA294.5 TO STA303.9 AND STR16L AT PASSENGER CABIN 2024-565293<[01] TOOLS USED: TEMPERATURE CONTROLLER P/N P3015GOES00000 
- [SDR SWAA2024101634455](https://openairdocs.org/sdr/SWAA2024101634455), Sep 5, 2024: FLOOR SUPPORT. CRACKED. CRACK ANGLE FLOOR STRUCTURE LOCATED STA695 AND BL0 WL208.1 CENTER SECTION 2024-565243<[01] TOOL USED: TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 14282005 DUE
- [SDR SWAA2024101634645](https://openairdocs.org/sdr/SWAA2024101634645), Sep 5, 2024: BEAR STRAP. CRACKED. CRACK INDICATION ON BEAR STRAP FORWARD GALLEY DOOR AREA BS 290-296 BETWEEN S-8R AND S-9R AT PASSENGER CABIN.CRACK LENGTH 0.375 IN.(1EA) 2024-565315<[01] STEP 5 
- [SDR SWAA2024101634454](https://openairdocs.org/sdr/SWAA2024101634454), Sep 5, 2024: RIB. CRACKED. CRACK INSPAR RIB 111.10 LOCATED AT 28 INCHES OF FRONT SPAR AT RT HORIZONTAL STABILIZER 2024-565244<[01] TOOL USED ON STEP 3 AND 4 ET EQUIPMENT: P/N: NORTEC 600D

All 255: https://openairdocs.org/aircraft/N7738A/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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