# N7739A: 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 CFM56-7B24 series](https://openairdocs.org/engine/cfm-international-cfm56-7b24-series) (registry code 13044)
- Serial number: 35110
- Year built: 2006
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: October 9, 2012
- Certificate issued: October 25, 2012
- Expires: October 31, 2028
- Mode S code: AA77C0
- 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=7739A
- Page: https://openairdocs.org/aircraft/N7739A

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 (1)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB DCA20CA050](https://openairdocs.org/ntsb/DCA20CA050), Dec 22, 2019: Boeing 737 (N7739A), Kansas City, MO, substantial damage. Probable cause: a bird strike during descent

## FAA accident and incident reports

None matched to N7739A.

## Service difficulty reports (238, 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 SWAA2026060207906](https://openairdocs.org/sdr/SWAA2026060207906), May 30, 2026: SLIDE. OUT OF POSITION. FWD PROVISIONING DOOR OPENED WITH DOOR PARTIALLY ARMED RAFT DID NOT ACTIVATE BUT FELL OUT OF DOOR PANEL. REMOVED AND REPLACED FWD SERVICE DOOR ESCAPE SLIDE IAW 
- [SDR SWAA2026033084060](https://openairdocs.org/sdr/SWAA2026033084060), Mar 27, 2026: SLIDE. UNPACKED. L1 DOOR SLIDE FELL OUT OF ITS CONTAINER WHILE OPENING THE DOOR. THE SLIDE DID NOT DEPLOY. REPACKED FWD L1 SLIDE IAW AMM 25-66-01 OPS CK GOOD.
- [SDR SWAA2026033084058](https://openairdocs.org/sdr/SWAA2026033084058), Mar 27, 2026: SLIDE. DISLODGED. L1 DOOR SLIDE FELL OUT OF ITS CONTAINER WHILE OPENING THE DOOR. C/W PER MT 725-61-06.
- [SDR SWAA2025120442494](https://openairdocs.org/sdr/SWAA2025120442494), Dec 4, 2025: MOUNT. CRACKED. FWD SERVICE DOOR AFT SLIDE MOUNT ISOLATOR CRACKED. R & R FWD SERVICE DOOR AFT SLIDE MOUNT ISOLATOR IAW SRM 51-40-02.
- [SDR SWAA2025120442489](https://openairdocs.org/sdr/SWAA2025120442489), Dec 4, 2025: MOUNT. DAMAGED. AFT ENTRY DOOR FWD SLIDE MOUNT ISOLATORS DAMAGED. R & R AFT ENTRY DOOR FWD SLIDE MOUNT ISOLATORS IAW SRM 51-40-02.
- [SDR SWAA2025120442496](https://openairdocs.org/sdr/SWAA2025120442496), Dec 4, 2025: HANDLE. LOOSE. FWD SERVICE DOOR INNER HANDLE LOOSE. SECURED FWD SERVICE DOOR INNER HANDLE IAW AMM 20-50-11.
- [SDR SWAA2025120442497](https://openairdocs.org/sdr/SWAA2025120442497), Dec 4, 2025: ACOUSTIC PANEL. DELAMINATED. NR 2 ENGINE HAS TWO AFT ACOUSTICAL PANELS THAT ARE DELAMINATED LOCATED ABOVE AND BELOW THE 3 OCLOCK STRUT. REMOVED AND REPLACED THE AFT ACOUSTICAL PANELS IAW AM
- [SDR SWAA2025082206733](https://openairdocs.org/sdr/SWAA2025082206733), Aug 21, 2025: HANDLE. LOOSE. FWD ENTRY DOOR CLOSE ASSIST HANDLE IS LOOSE<[01] SECURED FWD ENTRY DOOR CLOSE ASSIST HANDLE; REF. AMM 52-11-31.
- [SDR SWAA2025050266186](https://openairdocs.org/sdr/SWAA2025050266186), May 1, 2025: FASTENER. MISSING. FWD SVC DOOR SLIDE COVER GRIT BAR RETAINER CLIP MISSING FASTENER. REFERENCE MXI #TTG8Q00ZZBXA<[01] SECURED FWD SVC DOOR ESCAPE SLIDE GRIT BAR AFT RETAINER CLIP 
- [SDR SWAA2025042326705](https://openairdocs.org/sdr/SWAA2025042326705), Apr 21, 2025: GIRT BAR. OUT OF ADJUST. FORWARD SERVICE DOOR GRIT BAR AFT RETAINER TAB LOOSE <[01]. INSTALLED HARDWARE IN FWD SVC DOOR AFT GIRT BAR IN REF TO EA M-23-125-01839.
- [SDR SWAA2025041422822](https://openairdocs.org/sdr/SWAA2025041422822), Apr 9, 2025: LIGHT. OUT OF ADJUST. PASSENGER CABIN SEAT ROW 24 ABC PHOTOLUMINESCENT STRIPS HAS LARGE GAP<[01] REPLACED STRIP PER AMM 33-51-15;[02] INSPECTION C/W REPLACED STRIP PER AMM 33-51-15
- [SDR SWAA2025041422831](https://openairdocs.org/sdr/SWAA2025041422831), Apr 9, 2025: SEAL. CRACKED. LEFT HAND HORIZONTAL STAB UPPER SLIDER SEAL CRACKED.<[01] REMOVED AND REPLACED SEAL PER AMM 53-31-31.;[02] C/W INSP. REMOVED AND REPLACED SEAL PER AMM 53-31-31.
- [SDR SWAA2025020392096](https://openairdocs.org/sdr/SWAA2025020392096), Feb 1, 2025: GIRT BAR. LOOSE. FORWARD GALLEY DOOR GIRT BAR RETAINING BRACKET LOOSE<[01] RE-SECURE FWD GALLEY DOOR GIRT BAR BRACKET PER AMM 25-66-01.
- [SDR SWAA2024083027420](https://openairdocs.org/sdr/SWAA2024083027420), Aug 18, 2024: GROUND STUD. CORRODED. L1187 EMERGENCY EXIT INDICATOR LIGHT BS 304 WL229 LBL 67 INOP<[01] PERFORMED TROUBLESHOOTING PER WDM 33-51-21 FOUND WIRE W4142-0152-20 PULL FROM GROUND BLOCK GD
- [SDR SWAA2024090326870](https://openairdocs.org/sdr/SWAA2024090326870), Aug 16, 2024: SLIDE. NOT SEATED. FED DOOR ESCAPE SLIDE SHROUD NOT FULLY SEATED (LOWER PIN NOT ENGAGED)<[01] REMOVED AND INSTALLED PER AMM 25-66-01-400-803-NG ESCAPE SLIDE PACK AND COVER INSTALL
- [SDR SWAA2024090319382](https://openairdocs.org/sdr/SWAA2024090319382), Jul 28, 2024: SUPPORT. CRACKED. BREAKER PANEL AT BS 540 LBL 0 - LBL 25 CRACKED<[01] REMOVED AND REPLACED BREAKER PANEL ASSY AT BS 540 LBL 0-25 WL 208 IAW SRM 51-40-02-0G-0 AND DWG 143A5240;[02
- [SDR SWAA2024090315583](https://openairdocs.org/sdr/SWAA2024090315583), Jul 23, 2024: SUPPORT ANGLE. BROKEN. SUPPORT ANGLE ON FORWARD SIDE OF BS 663 VAPOR BARRIER IS BROKEN RBL 27 WL 150<[01] LOCATED AND DRILLED 1 EA ANGLE P/N 149A7218Y8 PO# 986123 AND 1 EA CLIP P/N 14
- [SDR SWAA2024090315334](https://openairdocs.org/sdr/SWAA2024090315334), Jul 22, 2024: FLOOR SUPPORT. CORRODED. FWD PASSENGER COMPARTMENT WET AREA; CORROSION ON INTERCOSTAL WL 208 BS 294.5 TO 312 LBL 12.<[01] VERIFIED SRM 53-10-51-1A-1 IS APPLICABLE. MATERIAL LOSS EXCEED 
- [SDR SWAA2024090315308](https://openairdocs.org/sdr/SWAA2024090315308), Jul 22, 2024: FLOOR SUPPORT. CORRODED. FWD PASSENGER COMPARTMENT WET AREA; CORROSION ON INTERCOSTAL WL 208 BS 276+14 CENTERLINE.<[01] REMOVED AND REPLACED INTERCOSTAL AT STA 277-294; WL 208; BL-0 PER
- [SDR SWAA2024090315312](https://openairdocs.org/sdr/SWAA2024090315312), Jul 22, 2024: FLOORBEAM. CRACKED. FWD PASSENGER COMPARTMENT WET AREA; CRACK ON FLOOR BEAM WL 208 BS 295.5 RBL 52.<[01] REMOVED DAMAGED AREA OF FLOOR BEAM AND REPAIRED AT BS 295.5 RBL 26 TO RBL 6
- [SDR SWAA2024090315316](https://openairdocs.org/sdr/SWAA2024090315316), Jul 22, 2024: FLOOR SUPPORT. CRACKED. FWD PASSENGER COMPARTMENT WET AREA; CRACK ON INTERCOSTAL WL 208 BS 344+6 RBL 31.<[01] REMOVED AND INSTALLED REPLACEMENT INTERCOSTAL WL 208; BS 344 TO 360; RBL 3
- [SDR SWAA2024090315320](https://openairdocs.org/sdr/SWAA2024090315320), Jul 22, 2024: FLOOR SUPPORT. CRACKED. FWD PASSENGER COMPARTMENT WET AREA; CRACK ON INTERCOSTAL WL 208 BS 344+5 CENTERLINE.<[01] DAMAGE EXCEEDS LIMITATIONS PER SRM 53-10-51-1A-1. REMOVED AND REPLACED
- [SDR SWAA2024082915396](https://openairdocs.org/sdr/SWAA2024082915396), Jul 22, 2024: FLOOR PANEL. DELAMINATED. PASSENGER CABIN FLOOR PANEL 241AF HAS DELAMINATION<[01] PASSENGER CABIN FLOOR PANEL 241AF WITH DELAMINATION WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL PER
- [SDR SWAA2024090314887](https://openairdocs.org/sdr/SWAA2024090314887), Jul 21, 2024: BONDING JUMPER. CORRODED. LH WING TE; LOWER O/B FIXED TE ACCESS PANEL; AILERON TRANSMITTER BONDING JUMPER SCREW HAS CORROSION.<[01] REMOVED AND INSTALLED LH WING AILERON POSITION TRANSMI
- [SDR SWAA2024090315156](https://openairdocs.org/sdr/SWAA2024090315156), Jul 21, 2024: JUMPER. CORRODED. CORROSION ON LOWER BONDING JUMPER TO AFT BOOST PUMP TANK #1.<[01] REMOVED AND REPLACED LOWER BONDING JUMPER TO AFT BOOST PUMP TANK #1 IAW AMM 28-22-41-400-801. 
- [SDR SWAA2024090314891](https://openairdocs.org/sdr/SWAA2024090314891), Jul 21, 2024: BALANCE WEIGHT. CORRODED. LH WING TE; LOWER O/B FIXED TE ACCESS PANEL; I/B AILERON BALANCE WEIGHT ORSS 514+14 HAS CORROSION.<[01] REMOVED AND REPLACED AILERON BALANCE WEIGHT IAW CMM 57-5
- [SDR SWAA2024090314873](https://openairdocs.org/sdr/SWAA2024090314873), Jul 20, 2024: STUB FRAME. CRACKED. FWD SERVICE DOOR CUTOUT SURROUND STRUCTURE; AFT FACE TO THE DOOR FRAME WL 208 RBL 55 BS 291.5+4 HAS CRACK.<[01] TRIMED OUT DAMAGE PART OF THE STUB FRAME AND FAB
- [SDR SWAA2024090314875](https://openairdocs.org/sdr/SWAA2024090314875), Jul 20, 2024: INTERCOSTAL. CRACKED. FWD ENTRY DOOR CUTOUT SURROUND STRUCTURE; INTERCOSTAL BS 303.9+8 S-6L HAS CRACK.<[01] HFEC INSPECTED FRAME AT BS 303.9+8' STR 6L PER 737NDT PART 6 51-00-00 PROC
- [SDR SWAA2024083014849](https://openairdocs.org/sdr/SWAA2024083014849), Jul 20, 2024: FLOORBEAM. CORRODED. AFT PASSENGER COMPARTMENT WET AREA; CORROSION ON FLOOR BEAM BS 986.5 LBL 35 TO 45.<[01] REMOVED AND REPAIRED BS986 L/H FLOOR BEAM UPPER CHORD RBL 36 TO RBL 48 I
- [SDR SWAA2024083014871](https://openairdocs.org/sdr/SWAA2024083014871), Jul 20, 2024: STRAP. CORRODED. AFT PASSENGER COMPARTMENT WET AREA; CORROSION ON TENSION STRAP WL 208; LBL 5; BS 1016+14.<[01] REMOVED AND REPLACED NEW TENSION STRAP LBL5 BS1006-BS1030 WL208 I
- [SDR SWAA2024090314391](https://openairdocs.org/sdr/SWAA2024090314391), Jul 19, 2024: FITTING. CORRODED. AFT PASSENGER COMPARTMENT; VERTICAL FIN FRONT SPAR FITTING; BS 1016 CENTERLINE WL 283 CORROSION ON BOTH ATTACH POINTS GALLEY.<[01] REPLACED BOTH BUSHINGS AND CL
- [SDR SWAA2024090314421](https://openairdocs.org/sdr/SWAA2024090314421), Jul 19, 2024: SHEAR WEB. CORRODED. AFT PASSENGER COMPARTMENT WET AREA; CORROSION ON SHEAR WEB SEVERAL AREAS LBL 5; BS 1016+2; 1016+16.<[01] REMOVE AND REPLACE ACCOMPLISHED ON CCN TTG8Q00UQ37R;[02
- [SDR SWAA2024090314409](https://openairdocs.org/sdr/SWAA2024090314409), Jul 19, 2024: SHEAR WEB. CORRODED. AFT PASSENGER COMPARTMENT WET AREA; CORROSION ON SHEAR WEB SEVERAL AREAS LBL 7 TO 13; BS 1016+10; 1016+16; AND LBL 17; BS 1016+5.<[01] REMOVE AND INSTALL L/H BS
- [SDR SWAA2024090314373](https://openairdocs.org/sdr/SWAA2024090314373), Jul 19, 2024: FORMER. CRACKED. R/H FAIRING FORMER BS 500D BETWEEN STRINGER 18 R/H AND 19 R/H IS CRACKED<[01] REMOVED AND REPLACED FAIRING FORMER AT BS 500D BETWEEN STR 18R TO STR 19R; WL 188 
- [SDR SWAA2024090314385](https://openairdocs.org/sdr/SWAA2024090314385), Jul 19, 2024: ATTACH ANGLE. CRACKED. R/H UPPER ATTACH ANGLE BS 663 RBL 6 WL 165 CRACKED (MARKED) B.S. 663 R/H LOWER COMPOSITE BULKHEAD UPPER ATTACH ANGLE IS CRACKED AT RBL 6 W.L. 165.<[01] REMOVED 
- [SDR SWAA2024083014405](https://openairdocs.org/sdr/SWAA2024083014405), Jul 19, 2024: FLOORBEAM. CORRODED. AFT PASSENGER COMPARTMENT WET AREA; CORROSION ON CROSSBEAM SEVERAL AREAS WL 208;BS 986.6; RBL 27 TO RBL 48.<[01] REMOVED AND REPAIRED BS986 R/H FLOOR BEAM UPPER
- [SDR SWAA2024083014415](https://openairdocs.org/sdr/SWAA2024083014415), Jul 19, 2024: STRAP. CORRODED. AFT PASSENGER COMPARTMENT WET AREA; CORROSION ON TENSION STRAP WL 208; RBL 5; BS 1006+2; 1016; 1016+10 TO 1016+14.<[01] TENSION STRAP TO BE REMOVED AND REPLACED
- [SDR SWAA2024083014425](https://openairdocs.org/sdr/SWAA2024083014425), Jul 19, 2024: STRAP. CORRODED. AFT PASSENGER COMPARTMENT WET AREA; CORROSION ON TENSION STRAP LBL 28; BS 1016+1; 1016+14; 1016+8.<[01] REMOVED AND INSTALLED NEW TENSION STRAP BS1006-BS1024 LB
- [SDR SWAA2024083014411](https://openairdocs.org/sdr/SWAA2024083014411), Jul 19, 2024: STRAP. CORRODED. AFT PASSENGER COMPARTMENT WET AREA; CORROSION ON TENSION STRAP LBL 18; BS 1016+9 TO 1016+14.<[01] REMOVED AND INSTALLED NEW TENSION STRAP BS 1006-1028 LBL 18 WL
- [SDR SWAA2024083014417](https://openairdocs.org/sdr/SWAA2024083014417), Jul 19, 2024: STRAP. CORRODED. AFT PASSENGER COMPARTMENT WET AREA; CORROSION ON TENSION STRAP WL 208; RBL 18; BS 1016+12.<[01] REMOVED AND REPLACED TENSION STRAP BS 1006-1028 RBL 18 WL 208 IA
- [SDR SWAA2024090314355](https://openairdocs.org/sdr/SWAA2024090314355), Jul 18, 2024: FLOOR PANEL. CORRODED. MAIN CABIN FLOORBOARD AREA AT RBL 6; WL 208 & STA 1008 APPROX; FOUND 1EA MISDRILLED HOLE AT PLATE MARKED<[01] TENSION STRAP TO BE REMOVED AND REPLACED ON CCN TT
- [SDR SWAA2024090313840](https://openairdocs.org/sdr/SWAA2024090313840), Jul 18, 2024: ATTACH ANGLE. CORRODED. CORROSION AFT CARGO BAY ATTACH ANGLE UNDER SHIELD HAS MULTIPLE AREAS UNDER NUT PLATES BS767 TO BS787 RBL21 WL156<[01] REMOVED AND REPLACED ANGLE UNDER SHIELD AT
- [SDR SWAA2024083014357](https://openairdocs.org/sdr/SWAA2024083014357), Jul 18, 2024: STRAP. CORRODED. MAIN CABIN FLOORBOARD AREA AT RBL 6; WL 208 & STA 1028 APPROX; FOUND CORROSION AT PLATE MARKED<[01] REMOVED AND INSTALLED NEW TENSION STRAP RBL6 BS1006-BS1028 W
- [SDR SWAA2024083013842](https://openairdocs.org/sdr/SWAA2024083013842), Jul 18, 2024: SHIELD. CORRODED. CORROSION AFT CARGO BAY SHIELD FWD OF CARGO DOOR AROUND MULTIPLE NUT PLATE HOLES BS767+3 TO BS794 RBL22 WL156<[01] REMOVED AND REPLACED SHIELD AT ACB BETWEEN BS
- [SDR SWAA2024083013844](https://openairdocs.org/sdr/SWAA2024083013844), Jul 18, 2024: STRAP. CORRODED. CORROSION AFT CARGO BAY FLOOR SPLICE STRAP AROUND NUT PLATE HOLE BS767+6 RBL11.5 WL156<[01] EVALUATED CORROSION ON STRAP BS 767+6 RBL 11.5 WL 156; FOUND TO BE O
- [SDR SWAA2024083013846](https://openairdocs.org/sdr/SWAA2024083013846), Jul 18, 2024: SUPPORT PLATE. CORRODED. CORROSION AFT CARGO BAY L/H FLOOR TO SIDEWALL SUPPORT PLATE MULTIPLE AREAS AROUND NUT PLATE HOLES BS727B TO BS767 LBL22 WL156<[01] REMOVED AND REPLACED SIDEWALL
- [SDR SWAA2024083013848](https://openairdocs.org/sdr/SWAA2024083013848), Jul 18, 2024: SUPPORT PLATE. CORRODED. CORROSION AFT CARGO BAY R/H FLOOR TO SIDEWALL SUPPORT PLATE HAS MULTIPLE AREAS AROUND NUT PLATE HOLES BS727B TO BS767 RBL22 WL156<[01] REMOVE AND REPLACE SIDEWA
- [SDR SWAA2024083013382](https://openairdocs.org/sdr/SWAA2024083013382), Jul 17, 2024: FLOOR PANEL. PULLED. FWD FLOOR PANEL 221BF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DUE TO EXTENT OF DAMAGE; FLOOR PANEL 221BF WAS REPLACED IAW SRM 51-10-02-0G-0 PAR 9.A (1).;[0
- [SDR SWAA2024083013392](https://openairdocs.org/sdr/SWAA2024083013392), Jul 17, 2024: FLOOR PANEL. PULLED. FWD FLOOR PANEL 222CF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FWD FLOOR PANEL 222CF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE
- [SDR SWAA2024083013400](https://openairdocs.org/sdr/SWAA2024083013400), Jul 17, 2024: FLOOR PANEL. PULLED. FWD FLOOR PANEL 232BF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FORWARD FLOOR PANEL 232BF UPPER SKIN; WITH AREAS OF PULLED STRANDS; WAS REPAIRED IAW SRM 53-0

All 238: https://openairdocs.org/aircraft/N7739A/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

## Earlier aircraft with N7739A

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N7739A before.

- [Cancelled 1960-05-06](https://openairdocs.org/deregistered/N7739A-1960-05-06): Cessna 180, S/N 32636. Exported to Australia. Owner: [J I Kislak Mortgage Corp Of Florida](https://openairdocs.org/faa-owner/J%20I%20KISLAK%20MORTGAGE%20CORP%20OF%20FLORIDA), [Miami, FL](https://openairdocs.org/faa-place/FL/Miami)

## 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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