# N7736A: 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: 35109
- Year built: 2006
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: June 19, 2014
- Certificate issued: July 8, 2014
- Expires: July 31, 2027
- Mode S code: AA7757
- 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=7736A
- Page: https://openairdocs.org/aircraft/N7736A

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 N7736A.

## FAA accident and incident reports

None matched to N7736A.

## Service difficulty reports (258, 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 SWAA2026101999022](https://openairdocs.org/sdr/SWAA2026101999022), Oct 15, 2026: SEAT. OUT OF ADJUST. SEAT 15D WILL NOT STAY UPRIGHT, OKAY TO CONTINUE IAW MEL 25-6-02 SP 1B. SEAT LOCKED UPRIGHT AND IS USABLE REF. LP 3439875
- [SDR SWAA2026101967765](https://openairdocs.org/sdr/SWAA2026101967765), Oct 15, 2026: HYDROLOCK. OUT OF ADJUST. 15D SEATBACK WILL NOT STAY IN UPRIGHT IF OCCUPIED. OK TO CONTINUE PER MEL 25-6-01 SP1B. ADJUSTED LOCKING NUTS RECLINE HYDROLOCK TO LOCK SEAT IN UPRIGHT POSITION
- [SDR SWAA2026101999040](https://openairdocs.org/sdr/SWAA2026101999040), Oct 13, 2026: GIRT BAR. OUT OF ADJUST. R1 DOOR GIRT BAR LOOSE. ADJUSTED GIRT BAR IAW AMM 25-66-01
- [SDR SWAA2026101269883](https://openairdocs.org/sdr/SWAA2026101269883), Oct 6, 2026: LIGHT. INOPERATIVE. SEVERAL EMERGENCY LIGHTS INOPERATIVE. REMOVED, REPLACED, AND PERFORMED SATISFACTORY OPS CHECK IAW AMM 33-51-06-960-805.
- [SDR SWAA2026101209695](https://openairdocs.org/sdr/SWAA2026101209695), Sep 26, 2026: LAMP. INOPERATIVE. L2 DOOR EXTERIOR EMERGENCY LIGHT INOP. REPLACED THE LAMPS FOR EMERGENCY LIGHT AND PERFORMED SATISFACTORY OPS CHECK IAW AMM 33-51-04-960-801.
- [SDR SWAA2026100953693](https://openairdocs.org/sdr/SWAA2026100953693), Sep 26, 2026: LAMP. INOPERATIVE. MULTIPLE MAIN CABIN EMERGENCY LIGHTS INOPERATIVE. RELAMPED MULTIPLE MAIN CABIN LIGHTS AND PERFROMED SUCCESSFUL OPS CHECK IAW AMM 33-51-00 AND AMM 33-51-03.
- [SDR SWAA2026072091488](https://openairdocs.org/sdr/SWAA2026072091488), Jul 15, 2026: BATTERY PACK. FAILED. FWD LEFT ENTRY EMERGENCY BATTERY PACK AT M1675 FAILED CAPACITY CHECK. R & R CABIN EMERGENCY BATTERY PACK IAW AMM 33-51-06.
- [SDR SWAA2026072052339](https://openairdocs.org/sdr/SWAA2026072052339), Jul 15, 2026: BATTERY PACK. FAILED. FWD RT SERVICE EMERGENCY BATTERY PACK AT M1674 FAILED CAPACITY CHECK. R & R CABIN EMERGENCY BATTERY PACK IAW AMM 33-51-06.
- [SDR SWAA2026072077792](https://openairdocs.org/sdr/SWAA2026072077792), Jul 15, 2026: LIGHT. INOPERATIVE. LEFT OVERWING EXIT LIGHT INOPERATIVE. R & R CABIN OVERWING EXIT LIGHT ASSY IAW AMM 33-21-00.
- [SDR SWAA2026050695904](https://openairdocs.org/sdr/SWAA2026050695904), May 6, 2026: ENGINE. FIRE. ON TAKEOFF ROLL AIRCRAFT BEHIND REPORTED FLAMES FROM NR 2 ENGINE. NO ABNORMAL INDICATIONS ON THE FLIGHT DECK.. INSPECTED NR 2 ENGINE FOR LEAKS WITH OIL PUDDLING
- [SDR SWAA2026042787198](https://openairdocs.org/sdr/SWAA2026042787198), Apr 7, 2026: CREASE BEAM. CORRODED. CORRODED RT CREASE BEAM WEB, BS 827, RBL 67, WL 208. REMOVED & REPLACED THE CREASE BEAM WEB IAW SRM 51-40-02-0G-0, DWG 146A5900, SHEET 71, REV B. AND DWG 146A59
- [SDR SWAA2026042785989](https://openairdocs.org/sdr/SWAA2026042785989), Apr 2, 2026: WINDOW FRAME. CRACKED. F/O NR 1 WINDOW FRAME OTBD UPPER CORNER CRACKED ACCOMPLISHED REPAIR NR 1 WINDOW OTBD POST IAW EA 26-153-00937 WIP1 AND WIP2.
- [SDR SWAA2026042785642](https://openairdocs.org/sdr/SWAA2026042785642), Apr 1, 2026: CREASE BEAM. CORRODED. PASSENGER CABIN, RT CREASE BEAM INNER CHORD, BS 631 - 642, RBL 65, WL 208 CORRODED. REMOVED AND REPLACED THE CREASE BEAM IAW SRM 51-40-02-0G-0, AND DWG 144A5901
- [SDR SWAA2026042785638](https://openairdocs.org/sdr/SWAA2026042785638), Apr 1, 2026: ATTACH ANGLE. CRACKED. RIGHT BS 663 UPPER ATTACH ANGLE CRACKED ON VAPOR BARRIER, RBL 8, WL 167.68. CRACK WAS FOUND TO BE OUT OF LIMITS AND ATTACH ANGLE WAS REPAIRED IAW SRM 57-10-10-2
- [SDR SWAA2026042785639](https://openairdocs.org/sdr/SWAA2026042785639), Apr 1, 2026: FLOOR SUPPORT. CRACKED. FLOOR SUPPORT CRACKED AT BS 540, RBL 1, WL 208. REMOVED & REPLACED THE FLOOR SUPPORT. LOCATED & DRILLED THE FLOORBOARD HOLES IAW SRM 51-40-02, SRM 51-40-05, & D
- [SDR SWAA2026042785640](https://openairdocs.org/sdr/SWAA2026042785640), Apr 1, 2026: FLOOR SUPPORT. CRACKED. FLOOR SUPPORT CRACKED AT BS 540 LBL 1 WL 208. REMOVED & REPLACED THE FLOOR SUPPORT. LOCATED AND DRILLED FLOOR BOARD PANEL HOLES IAW SRM 51-40-02, SRM 51-40-05, 
- [SDR SWAA2026042785645](https://openairdocs.org/sdr/SWAA2026042785645), Apr 1, 2026: STRINGER CLIP. CRACKED. CRACKED STRINGER CLIP AT BS 257 COMMON TO STR 10L. REMOVED AND REPLACED STRINGER CLIP AT BS 257 COMMON TO STR 10L IAW SRM 51-40-02-0G-0 AND DWG 141A0720; REV:A.
- [SDR SWAA2026042785643](https://openairdocs.org/sdr/SWAA2026042785643), Apr 1, 2026: STRAP. CORRODED. PASSENGER CABIN STRAP ON TOP OF WHEEL WELL BS 686; RBL 71; WL 202.5 WAS CORRODED. REFER TO FAULT TTG8Q01BF4AP WHERE EA 26-153-00948 WAS ADDED AS A SUBTASK REMOV
- [SDR SWAA2026042785644](https://openairdocs.org/sdr/SWAA2026042785644), Apr 1, 2026: STRAP. CORRODED. PASSENGER CABIN STRAP ON TOP OF WHEEL WELL BS 693; RBL 69-71; WL 202.5 WAS CORRODED. REFER TO FAULT TTG8Q01BF4AP WHERE EA 26-153-00948 WAS ADDED AS A SUBTASK.
- [SDR SWAA2026042785647](https://openairdocs.org/sdr/SWAA2026042785647), Apr 1, 2026: STRAP. CORRODED. PASSENGER CABIN STRAP ON TOP OF WHEEL WELL BS 713, RBL 71, WL 202.5 WAS CORRODED. REFER TO FAULT TTG8Q01BF4AP WHERE EA 26-153-00948 WAS ADDED AS A SUBTASK.ACTIO
- [SDR SWAA2026042785417](https://openairdocs.org/sdr/SWAA2026042785417), Apr 1, 2026: PIN. CORRODED. RT HORIZONTAL STAB REAR SPAR MIDDLE FAILSAFE ATTACH PIN WAS PITTED. FAILSAFE ATTACH PIN WILL BE INSTALLED ON TASK CARD TTG8Q002MTQZ STEP 15.
- [SDR SWAA2026042485641](https://openairdocs.org/sdr/SWAA2026042485641), Apr 1, 2026: CROSSBEAM. CRACKED. PASSENGER CABIN PANEL BREAK AT BS 540, RBL 45 - RBL 65, WL 208, TOP PLATE IS CRACKED. COMPLETED STEP 2 AND UPDATED STEP 1. REMOVED AND REPLACED PASSENGER CABIN 
- [SDR SWAA2026042784852](https://openairdocs.org/sdr/SWAA2026042784852), Mar 31, 2026: RIB. CRACKED. RIGHT HORIZONTAL STAB RIB NR 5 THIRD FROM FWD STIFFENER, CRACKED AT LOWER END. REMOVED, REPAIRED, AND REINSTALLED THE NR 5 RIB IAW SRM 55-10-09-2R-5, SRM 51-40-
- [SDR SWAA2026042784840](https://openairdocs.org/sdr/SWAA2026042784840), Mar 30, 2026: SCUFF PLATE. CRACKED. FORWARD SERVICE DOOR SCUFF PLATE CRACKED. REMOVED ALL THE COATINGS AND UNWANTED MATERIALS FROM THE SCUFF PLATE BEFORE WELDING IAW SRM 53-10-15-2R-2 STEP 4.B.(3)
- [SDR SWAA2026042484847](https://openairdocs.org/sdr/SWAA2026042484847), Mar 30, 2026: STRAP. CORRODED. CORROSION AFT CARGO BAY FLOOR SPLICE STRAP AROUND NUT PLATE HOLE BS 767+6, RBL 11.5, WL 156. CORROSION ON STRAP WAS FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS A
- [SDR SWAA2026042484841](https://openairdocs.org/sdr/SWAA2026042484841), Mar 30, 2026: SUPPORT. CORRODED. CORROSION AFT CARGO BAY L/H FLOOR TO SIDEWALL SUPPORT PLATE MULTIPLE AREAS AROUND NUT PLATE HOLES BS727B TO BS767 LBL22 WL156. REMOVED AND REPLACED FLOOR TO SID
- [SDR SWAA2026042484839](https://openairdocs.org/sdr/SWAA2026042484839), Mar 30, 2026: SCUFF PLATE. CRACKED. FORWARD CARGO BAY FWD CORNER SCUFF PLATE IS CRACKED. REPAIRED FORWARD CARGO BAY FORWARD CORNER SCUFF PLATE PER AMM 53-30-15-2R-1.
- [SDR SWAA2026042484835](https://openairdocs.org/sdr/SWAA2026042484835), Mar 30, 2026: SCUFF PLATE. CRACKED. AFT CARGO BAY AFT CORNER SCUFF PLATE IS CRACKED. REPAIRED AFT CARGO BAY AFT CORNER SCUFF PLATE PER AMM 53-60-15-2R-1.
- [SDR SWAA2026042484838](https://openairdocs.org/sdr/SWAA2026042484838), Mar 30, 2026: STUB FRAME. CRACKED. CRACK FOUND R1 DOOR STUB FRAME .7' ABOVE SEAL DEPRESSOR BS 291.5 +9 L: .4'. REMOVED DAMAGE FSD STUB FRAME BS 291.5 + 9; LOCATED; DRILLED AND INSTALLED NEW FSD S
- [SDR SWAA2026042784398](https://openairdocs.org/sdr/SWAA2026042784398), Mar 29, 2026: PANEL. DEBONDED. PANEL 194CR HAS DISBONDS ON OUTER SURFACE. PANEL 194CR WAS REPAIRED IAW SRM 51-70-05-2R-2.
- [SDR SWAA2026032382414](https://openairdocs.org/sdr/SWAA2026032382414), Mar 22, 2026: COVER. MISSING. LOWER OVERWING EXIT SIGN F/O SIDE MISSING. INSTALLED LIGHT COVER IAW AMM 33-51-04.
- [SDR SWAA2025122654858](https://openairdocs.org/sdr/SWAA2025122654858), Dec 22, 2025: LENS. MISSING. CREW REPORTS EMERGENCY EXIT LENS MISSING ON OVERWING EXIT FO SIDE. INSTALLED EMERGENCY EXIT LENS COVER IAW AMM 33-51-01.
- [SDR SWAA2025102024970](https://openairdocs.org/sdr/SWAA2025102024970), Oct 16, 2025: FUSE. BLOWN. EMERGENCY LIGHT BEHIND L2 INOPERATIVE. R & R THE FUSE FROM BATTERY POWER SUPPLY M1673 IAW AMM 33-51-06-960-804. TEST PASSED.
- [SDR SWAA2025100620766](https://openairdocs.org/sdr/SWAA2025100620766), Oct 3, 2025: SKIRT. OUT OF LIMITS. PASSENGER CABIN AFT SERVICE DOOR ESCAPE SLIDE GIRT SKIRT IN POOR CONDITION. REMOVED AND REPLACED AFT SERVICE DOOR ESCAPE SLIDE PER MT 756-61-06
- [SDR SWAA2025092918567](https://openairdocs.org/sdr/SWAA2025092918567), Sep 26, 2025: COVER. UNSECURE. ROW 12F EMERGENCY EXIT LIGHT COVER WILL NOT STAY ATTACHED TO LIGHT. INSTALLED NEW LIGHT COVER PER AMM 33-51-01.
- [SDR SWAA2025051369467](https://openairdocs.org/sdr/SWAA2025051369467), May 10, 2025: GIRT BAR. OUT OF ADJUST. R1 DOOR GIRT BAR RETAINER CLIPS LOOSE; GIT BAR COMING OUT WHEN DOOR OPENED<[01] TIGHTENED RETAINER CLIPS FOR THE GIRT BAR IN REFERENCE TO SIP
- [SDR SWAA2024120673607](https://openairdocs.org/sdr/SWAA2024120673607), Dec 2, 2024: DOOR. CRACKED. CRACK IN FWD SERVICE DOOR (R1) FWD SIDE WHERE SEAL MATES. JUST BEHIND UPPER HINGE. CRACK MEASURES .250. REMOVED AND REPLACED 141A8358Y6 (BOX; R1 DOOR UPPER HING
- [SDR SWAA2024120673609](https://openairdocs.org/sdr/SWAA2024120673609), Dec 2, 2024: HINGE BOX. CRACKED. CRACK EXTENDS BEYOND BLENDED AREA WHILE PERFORMING NDT PER EA 24-153-03356 WIP1 FOUND CRACK TO EXTEND APROX. .125' BEYOND BLENDED AREA.<[01] REMOVED AND REPLACE
- [SDR SWAA2024111860983](https://openairdocs.org/sdr/SWAA2024111860983), Nov 17, 2024: SLIDE. OUT OF POSITION. FWD ENTRY DOOR ESCAPE SLIDE FELL OUT OF CONTAINER BUT DID NOT DEPLOY<[01] REMOVE AND REPLACE FORWARD ENTRY DOOR SLIDE I.A.W. 25-66-01 OK FOR SERVICE
- [SDR SWAA2024081425799](https://openairdocs.org/sdr/SWAA2024081425799), Aug 14, 2024: SEAT. MISCONFIGURED. SEAT 11B & 11C RECLINING INTO OVERWING EXIT ROW<[01] LOCKED OUT SEATS 11B AND 11C PER AMM 25-22-00.
- [SDR SWAA2024052287850](https://openairdocs.org/sdr/SWAA2024052287850), May 19, 2024: SLIDE. DISLODGED. FORWARD SERVICE DOOR EMERGENCY ESCAPE SLIDE DISLODGED WHEN DOOR OPENED. GIRT BAR WAS NOT ENGAGED; SLIDE WAS NOT ACTIVATED.<[01] RE INSTALLED FWD SERVICE DOOR ES
- [SDR SWAA2024052086045](https://openairdocs.org/sdr/SWAA2024052086045), May 15, 2024: LAMP. INOPERATIVE. INOP LAVATORY A EMERGENCY LIGHT AT FWD GALLEY AREA 2024-259404<[01] REPLACED LAMPS IN LAVATORY A EMERGENCY LIGHT AT FWD GALLEY AREA IAW B737-700 AMM 33-51-01-96
- [SDR SWAA2024051578352](https://openairdocs.org/sdr/SWAA2024051578352), Apr 23, 2024: STUB FRAME. CRACKED. CRACK INDICATION IN HOLE FROM STUB FRAME LOCATED BS 294.5 AT LEVEL STR 17R AT FWD GALLEY AREA. LOOKING FWD CRACK DIRECTION IS: 7 O CLOCK. 2024-259366 CRACK ON W
- [SDR SWAA2024052084498](https://openairdocs.org/sdr/SWAA2024052084498), Apr 17, 2024: ANGLE. PERFORATED. PERFORATION ON ANGLE LOCATED BS540 PLUS 8INCH AND RBL41 AT AIR CONDITIONING BAY 2024-259288<[01] TOOL USED P/N: NORTEC 500D; S/N: 500X1693P030457; CAL DUE: 15-O
- [SDR SWAA2024052076303](https://openairdocs.org/sdr/SWAA2024052076303), Apr 17, 2024: BRACKET. CRACKED. CRACK BRACKET LOCATED BS540 AND RBL7 AT AIR CONDITIONING BAY 2024-259286<[01] REPLACED BRACKET LOCATED BS540 AND RBL7 AT AIR CONDITIONING BAY IAW B737-700 SRM 5
- [SDR SWAA2024052076304](https://openairdocs.org/sdr/SWAA2024052076304), Apr 17, 2024: BRACKET. CRACKED. CRACK BRACKET LOCATED BS540 AND LBL7 AT AIR CONDITIONING BAY 2024-259287<[01] REPLACED BRACKET LOCATED BS540 AND LBL7 AT AIR CONDITIONING BAY IAW B737-700 SRM 5
- [SDR SWAA2024051676300](https://openairdocs.org/sdr/SWAA2024051676300), Apr 17, 2024: ANGLE. CRACKED. CRACK ANGLE TRAILING EDGE LOCATED ORSS273 ON DEFLECTION CONTROL RIB AREA LT WING 2024-259282<[01] REPLACED ANGLE TRAILING EDGE LOCATED ORSS273 ON DEFLECTION CON
- [SDR SWAA2024051676302](https://openairdocs.org/sdr/SWAA2024051676302), Apr 17, 2024: PLATE. CRACKED. CRACK CORRUGATED PLATE TRAILING EDGE LOCATED IRSS217 AT LT WING 2024-259283<[01] REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED IRSS217 AT LT WING IAW B737-700
- [SDR SWAA2024051576306](https://openairdocs.org/sdr/SWAA2024051576306), Apr 17, 2024: LIGHT. BROKEN. BROKEN EMERGENCY EXIT LIGHT ASSY ON BIN 6 LH SIDE 2024-259291<[01] REPLACED EMERGENCY EXIT LIGHT ASSY ON BIN 6 LH SIDE IAW B737-700 AMM 33-51-03-960-802; STEP 3
- [SDR SWAA2024052075514](https://openairdocs.org/sdr/SWAA2024052075514), Apr 16, 2024: ANGLE. CRACKED. CRACK ON ANGLE LOCATED BS 947.5 AT LEVEL STR 25L AT AFT CARGO COMPARTMENT 2024-259235<[01] REPLACED ANGLE AND FASTENERS LOCATED BS 947.5 AT LEVEL STR 25L AT AFT

All 258: https://openairdocs.org/aircraft/N7736A/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 N7736A

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N7736A before.

- [Cancelled 1956-11-02](https://openairdocs.org/deregistered/N7736A-1956-11-02): Cessna 180, S/N 32633. 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 CFM56-7B24 series engine: https://openairdocs.org/engine/cfm-international-cfm56-7b24-series.md

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