# N7702A: 2004 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: 33917
- Year built: 2004
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: April 25, 2012
- Certificate issued: May 14, 2012
- Expires: May 31, 2028
- Mode S code: AA6BA6
- 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=7702A
- Page: https://openairdocs.org/aircraft/N7702A

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 N7702A.

## FAA accident and incident reports

None matched to N7702A.

## Service difficulty reports (275, 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 SWAA2026101271646](https://openairdocs.org/sdr/SWAA2026101271646), Oct 7, 2026: BATTERY PACK. NO TEST. FWD LEFT EMERGENCY BATTERY PACK M1675 FAILED CAPACITY CHECK. R & R CABIN EMERGENCY BATTERY PACK IAW AMM 33-51-06.
- [SDR SWAA2026101210513](https://openairdocs.org/sdr/SWAA2026101210513), Oct 7, 2026: BATTERY PACK. NO TEST. FWD RT BATTERY PACK M1674 FAILED CAPACITY CHECK. R & R BATTERY PACK PER AMM 33-51-06 C/W INSPECTION
- [SDR SWAA2026091560171](https://openairdocs.org/sdr/SWAA2026091560171), Sep 14, 2026: INDICATOR. MALFUNCTIONED. AIRSPEED DISAGREE DISPLAYED. PERFORMED AIRSPEED DISAGREE FAULT ISOLATION IAW FIM 31-62 TASK 876. NO FAULTS FOUND ON ADIRS BITE TEST IAW B737 FIM 34-21 TASK 801.
- [SDR SWAA2026083181234](https://openairdocs.org/sdr/SWAA2026083181234), Aug 28, 2026: BATTERY PACK. INOPERATIVE. RIGHT AFT EMERGENCY LIGHT CHARGER CIRCUIT BREAKER TRIPPED. REPLACED THE RT EMERGENCY EXIT BATTERY PACK & CHARGER IAW AMM 33-51-06. OPS CHECKED GOOD.
- [SDR SWAA2026083199923](https://openairdocs.org/sdr/SWAA2026083199923), Aug 28, 2026: CHARGER. INOPERATIVE. R AFT EMERG CHGR LIGHTING CIRCUIT BREAKER POPPED_ REPLACED RH EMERGENCY EXIT BATTERY PACK AND CHARGER IAW AMM 33-51-06. OPS CHECKS GOOD.
- [SDR SWAA2026040786142](https://openairdocs.org/sdr/SWAA2026040786142), Apr 3, 2026: CAP. LOOSE. FLIGHT ATTENDANT REPORTS A PLASTIC WHITE CAP CAME LOOSE FROM THE FORWARD ENTRY DOOR GIRT BAR.<[01] REPLACED STOP RELEASE ON FRW ENTRY DOOR REF AMM 25-66-00
- [SDR SWAA2026021268527](https://openairdocs.org/sdr/SWAA2026021268527), Feb 6, 2026: BATTERY PACK. INOPERATIVE. EMERGENCY EXIT LIGHTS ASSOCIATED WITH BATTERY PACK M1670, DO NOT ILLUMINATE. REPLACED & PERFORMED A GOOD OPS CHECK IAW 33-51-06-960-805.
- [SDR SWAA2026021265852](https://openairdocs.org/sdr/SWAA2026021265852), Jan 30, 2026: STIFFENER. CORRODED. CORROSION ON PRESSURE DECK WEB STIFFENER ANGLE, BS 695+7.5, RBL 62 - 68, WL 200. REMOVED AND REPLACED THE STIFFENER ANGLE IAW AMM SRM 51-40-02-0G-0.
- [SDR SWAA2026021265853](https://openairdocs.org/sdr/SWAA2026021265853), Jan 30, 2026: STIFFENER. CORRODED. CORROSION ON PRESSURE DECK WEB STIFFENER ANGLE, BS 706+2, RBL 60-65, WL 200. REMOVED AND REPLACED THE PRESSURE DECK WEB STIFFENER ANGLE IAW SRM 51-40-02-0G-0.
- [SDR SWAA2026021265496](https://openairdocs.org/sdr/SWAA2026021265496), Jan 29, 2026: FLOOR PANEL. PULLED. FLOOR PANEL 231XF UPPER SKIN HAD AREAS OF PULLED STRANDS. FABRICATION OF A NEW FLOOR PANEL REPLACEMENT ACCOMPLISHED IAW SRM 53-00-50-2R-0.
- [SDR SWAA2026021265498](https://openairdocs.org/sdr/SWAA2026021265498), Jan 29, 2026: FLOOR PANEL. PULLED. FLOOR PANEL 241AF UPPER SKIN HAD AREAS OF PULLED STRANDS. THE FLOOR PANEL WAS FOUND TO BE OUT OF ALLOWABLE LIMITS IAW SRM 53-00-50-1A-1, PARA 4.F, & FABRICATED 
- [SDR SWAA2026021265497](https://openairdocs.org/sdr/SWAA2026021265497), Jan 29, 2026: FLOOR PANEL. PULLED. FLOOR PANEL 232SF UPPER SKIN HAS AREAS OF PULLED STRANDS. FLOOR PANEL FABRICATION COMPLETE. THE FLOOR PANEL WAS REPLACED WITH THE NEWLY FABRICATED FLOOR PANEL I
- [SDR SWAA2026012663627](https://openairdocs.org/sdr/SWAA2026012663627), Jan 22, 2026: GIRT BAR. OUT OF ADJUST. AFT GALLEY SERVICE DOOR R2 ESCAPE SLIDE GIRT BAY HANGS TOO LOW. REPACKED AFT GALLEY SERVICE DOOR R2 ESCAPE SLIDE GIRT BAR IAW AMM 25-66-01.
- [SDR SWAA2026011259840](https://openairdocs.org/sdr/SWAA2026011259840), Jan 9, 2026: CHARGER. FAILED. AFT FA HEARD A LOUD NOISE POP IN THE AFT GALLEY AND AFTERWARDS ELECTRICAL SMELL COMING FROM AFT CONDITIONAL 05-51-56. PERFORMED CONDITIONAL INSPECTION SMOKE/FUM
- [SDR SWAA2026011260616](https://openairdocs.org/sdr/SWAA2026011260616), Jan 9, 2026: BATTERY PACK. FAILED. AFT FA HEARD A LOUD NOISE POP IN THE AFT GALLEY AND AFTERWARDS ELECTRICAL SMELL COMING FROM AFT CONDITIONAL 05-51-56. PERFORMED CONDITIONAL INSPECTION SMOKE/FUM
- [SDR SWAA2026011259229](https://openairdocs.org/sdr/SWAA2026011259229), Jan 7, 2026: SCUFF PLATE. CRACKED. R1 DOOR THRESHOLD SCUFF PLATE CRACKED ON FWD AND AFT SIDES. REMOVED AND REPLACED THE R1 DOOR SCUFF PLATE IAW AMM 53-11-01.
- [SDR SWAA2025101323381](https://openairdocs.org/sdr/SWAA2025101323381), Oct 9, 2025: UNKNOWN. ODOR. IN DESCENT SUBTLE BURNING SMELL LIKE SULFUR & ACETONE. CW CONDITIONAL SMOKE OR FUMES IN CABIN INSPEXTION PER AMM 05-51-56 & FIM 21-00 TASK 806. NO SMELLS OR FUM
- [SDR SWAA2025100620941](https://openairdocs.org/sdr/SWAA2025100620941), Oct 2, 2025: ACM. FAILED. ON TAXI OUT GOT A STRONG BURNING SMELL, FOLLOWED BY A LEFT PACK TRIP-OFF. TRIP-OFF WOULD NOT RESET. FOUND LT ACM NOT SPINNING. REMOVED AND REPLACED LT ACM IN RE
- [SDR SWAA2025093018890](https://openairdocs.org/sdr/SWAA2025093018890), Sep 28, 2025: MEGAPHONE. DAMAGED. AFT GALLEY MEGAPHONE HOUSING SCREW SPINNING.<[01] R/R AFT GALLEY MEGAPHONE IAW AMM 25-64-00. OPS CHECK GOOD.
- [SDR SWAA2025060377259](https://openairdocs.org/sdr/SWAA2025060377259), Jun 1, 2025: MEGAPHONE. INOPERATIVE. AFT MEGAPHONE INOP <[01]. REMOVED AND REPLACED AFT MEGAPHONE PER AMM25-64-00.
- [SDR SWAA2025052975195](https://openairdocs.org/sdr/SWAA2025052975195), May 26, 2025: BATTERY PACK. INOPERATIVE. AFT RH CABIN EMERGENCY LIGHTS INOP <[01]. REPLAED M1672 POWER SUPPLY AND BATTERY PACK IAW MM 33-51-06.
- [SDR SWAA2025042326810](https://openairdocs.org/sdr/SWAA2025042326810), Apr 21, 2025: SLIDE. LOOSE. FWD ENTRY DOOR SLIDE FELL OUT FROM CONTAINER. <[01] REMOVED SLIDE ASSY FROM CONTAINER AND FOUND SLIDE LATCHING MECHANISM TO THE CONTAINER DAMAGED (FELL A PART) 
- [SDR SWAA2025042326537](https://openairdocs.org/sdr/SWAA2025042326537), Apr 20, 2025: SEAT. OUT OF POSITION. SEATS ROW 12ABC NOT SEATED PROPERLY. <[01] R & R PASSENGER SEAT ROW 12ABC ASSEMBLY PER AMM 25-22-00; OPS CHECK GOOD.
- [SDR SWAA2025021896864](https://openairdocs.org/sdr/SWAA2025021896864), Feb 16, 2025: HOOK. OUT OF ADJUST. GIRTBAR R1 DOOR HOOK NOT RIGHT<[01] ADJUSTED GIRT BAR STOWAGE HOOK PER SIP FA CONFIRMED GOOD
- [SDR SWAA2024112671887](https://openairdocs.org/sdr/SWAA2024112671887), Nov 25, 2024: COUNTER. SMOKE. SMOKE COMING FROM FO TRIP COUNTER ON YOKE<[01] C/W SMOKE IN CABIN INSP 05-51-56 AMM ONLY FOUND KNOWN CAUSE F/O YOKE CONTROL WHEEL COUNTER PREVIOUSLY INSTALLED R
- [SDR SWAA2024110858019](https://openairdocs.org/sdr/SWAA2024110858019), Nov 8, 2024: TAILPIPE. FIRE. DURING TAXI #1 HAD A POSSIBLE TAIL PIPE FIRE AFTER F/AS AND PAX HEARD A POPPING NOISE; NO FIRE INDICATIONS IN FLIGHT DECK AND NO OTHER ABNORMAL INDICATIONS<[01]
- [SDR SWAA2024090433309](https://openairdocs.org/sdr/SWAA2024090433309), Sep 2, 2024: BATTERY. INOPERATIVE. RED BULLHORN FOR FLIGHT ATTENDANTS TO ADDRESS PAX IN REAR INOP<[01] REMOVED AND REPLACED MEGAPHONE BATTERIES PER AMM 25-64-00. OPS CHECK NORMAL.
- [SDR SWAA2024071211585](https://openairdocs.org/sdr/SWAA2024071211585), Jul 12, 2024: BOLT. INCORRECT. ON REMOVALOF THE FWD SER DR SLIDE CONAINER INCORRECT HARDWARE WAS FOUND<[01] REMOVED INCORRECT FWD SERVICE DOOR SLIDE CONTAINER BOLT AND REPLACED WITH CORRECT S
- [SDR SWAA2024070910036](https://openairdocs.org/sdr/SWAA2024070910036), Jul 6, 2024: BATTERY. INTERMITTENT. AFT MEGAPHONE INTERMITTENT<[01] REMOVED AND REPLACED BATTERIES IN AFT MEGAPHONE REF. AMM 25-64-00 OPS CHECK GOOD
- [SDR SWAA2024041874346](https://openairdocs.org/sdr/SWAA2024041874346), Apr 13, 2024: SUPPORT BRACKET. CRACKED. RIGHT ENGINE STARTER VALVE DUCT SUPPORT BRACKET IS CRACKED AT 9 O'CLOCK POSITION.<[01] REMOVED AND REPLACED STARTER DUCT SUPPORT BRACKET AT #2 ENGINE 9 O'CLOCK 
- [SDR SWAA2024041874175](https://openairdocs.org/sdr/SWAA2024041874175), Apr 12, 2024: SUPPORT. CORRODED. CORROSION. R/H SUPPORT ASSY-WHL WELL RING SEAL RETAINER AFT SECTION 4EA<[01] DEEP CORROSION AND EXFOLIATION AT SEALS RETAINER 4EA. FOUND OUT OF LIMITS. WILL BE 
- [SDR SWAA2024041874174](https://openairdocs.org/sdr/SWAA2024041874174), Apr 12, 2024: SUPPORT. CORRODED. CORROSION. L/H SUPPORT ASSY-WHL WELL RING SEAL RETAINER AFT SECTION 4EA<[01] REMOVED AND REPLACED L/H SUPPORT ASSY-WHL WELL RING SEAL RETAINERS AFT SECTION (4EA
- [SDR SWAA2024041772644](https://openairdocs.org/sdr/SWAA2024041772644), Apr 10, 2024: FUSE. DEFECTIVE. AFT LOWER CEILING PANEL CENTER EMERGENCY EXIT SING INOP<[01] PERFORMED TROUBLESHOOTING CENTER EMERGENCY EXIT SING AS PER B737 WDM 33-51-14. FOUND FUSE DEFECTIVE
- [SDR SWAA2024041870614](https://openairdocs.org/sdr/SWAA2024041870614), Apr 4, 2024: TRACK. BROKEN. LH HORIZ STAB FWD LOWER SLIDING SEAL TRACK AFT BROKEN.<[01] REMOVED AND REPLACED LEFT HORIZONTAL STAB FWD LOWER SLIDING SEAL AFT TRACK STRIP; REF AMM 53-31-31-4
- [SDR SWAA2024041867266](https://openairdocs.org/sdr/SWAA2024041867266), Mar 24, 2024: SEAT TRACK. CORRODED. F/O FWD INBOARD AND OUTBOARD SEAT TRACKS WITH CORROSION AT LOWER SURFACE<[01] REMOVED AND REPLACED F/O FWD INBOARD AND OUTBOARD SEAT TRACKS IN REFERENCE SOPM 20
- [SDR SWAA2024041866328](https://openairdocs.org/sdr/SWAA2024041866328), Mar 21, 2024: HINGE FITTING. CORRODED. FWD ENTRY DOOR CUTOUT LOWER HINGE SUPPORT FITTING HAS CORROSION AROUND BOLT HOLE.<[01] REMOVED AND REPLACED FWD ENTRY LOWER HINGE BOX FITTINGS AS PER B737-700 S
- [SDR SWAA2024041866027](https://openairdocs.org/sdr/SWAA2024041866027), Mar 21, 2024: SUPPORT. CORRODED. CORROSION FOUND ON L/W T/E PANEL 561BB SUPPORT STRUCTURE AROUND FASTENER HOLES.<[01] REMOVED AND REPLACED ATTACHMENT SUPPORT STRUCTURE BEAM L/W FOR PANEL 561BB;
- [SDR SWAA2024041865125](https://openairdocs.org/sdr/SWAA2024041865125), Mar 18, 2024: SEAL. CRACKED. LEFT HORIZONTAL STABILIZER TO FUSELAGE UPPER FWD SLIDING METAL SEAL IS CRACKED.<[01] REMOVED AND REPLACED LEFT HORIZONTAL STABILIZER TO FUSELAGE UPPER FWD SLIDI
- [SDR SWAA2024041865017](https://openairdocs.org/sdr/SWAA2024041865017), Mar 18, 2024: FLOOR PANEL. DEFORMED. FLIGHT DECK FLOOR PANEL#211AF IS DEFORMED.<[01] REPLACED FLIGHT DECK FLOOR PANEL #211AF AS PER REF 51-40-02-0G-0. INSTALLATION TO BE ACCOMPLISHED ON FAULT TTG8Q
- [SDR SWAA2024041974173](https://openairdocs.org/sdr/SWAA2024041974173), Mar 17, 2024: PLATE. DAMAGED. AFTER INSPECTED L/H WING DEFLECTION RIB FOUND SERRATED PLATE WITH ELONGATED HOLE AND HARDWARE WORN (PREVIOUS REPAIR)<[01] REMOVED AND REPLACED LEFT WING DEFLECT
- [SDR SWAA2024041964818](https://openairdocs.org/sdr/SWAA2024041964818), Mar 17, 2024: FITTING. CRACKED. RIGHT WING REAR SPAR DEFLECTOR CONTROL RIB FIXED PANEL VERTICAL SEAL FITTING CRACKED MKD DOT<[01] REMOVED AND REPLACED SEAL FITTING AND SEAL AT RT WING REAR SPA
- [SDR SWAA2024041964703](https://openairdocs.org/sdr/SWAA2024041964703), Mar 17, 2024: SEAT TRACK. CORRODED. CORROSION *** MAIN CABIN CENTER SECTION FLOOR R/H O/B SEAT TRACK I/B FLANGE RBL 45 STA 639+20' MKD DOT<[01] ACCOMPLISHED EA 24-153-00729. REF TASK CARDS TTG8Q00
- [SDR SWAA2024041864696](https://openairdocs.org/sdr/SWAA2024041864696), Mar 17, 2024: FITTING. CORRODED. CORROSION ** FWD CABIN FWD ENTRY L-1 DOOR CUTOUT AFT SAFETY STRAP FITTING CORR. MKD DOT<[01] REMOVED AND REPLACED L-1 DOOR CUTOUT AFT SAFETY STRAP FITTING IAW B
- [SDR SWAA2024041864700](https://openairdocs.org/sdr/SWAA2024041864700), Mar 17, 2024: FLOORBEAM. CRACKED. MAIN CABIN CENTER SECTION FLOOR SUPPORT BREAK CRACKED @ RBL 1 STA 540 MKD DOT<[01] REMOVED AND REPLACED BREAK PANEL ASSY AT MAIN CABIN CENTER SECTION; RBL 1 STA
- [SDR SWAA2024041864698](https://openairdocs.org/sdr/SWAA2024041864698), Mar 17, 2024: FLOORBEAM. DELAMINATED. MAIN CABIN CENTER SECTION FLOOR SUPPORT BREAK TOP LAYER DELAMINATED BETWEEN RBL 45.5 AND RBL 64 STA 540 MKD DOT<[01] REMOVED AND REPLACED FLOOR SUPPORT BREAK ;T
- [SDR SWAA2024041864821](https://openairdocs.org/sdr/SWAA2024041864821), Mar 17, 2024: ATTACH BRACKET. CRACKED. LEFT WING REAR SPAR DEFLECTOR CONTROL RIB HORIZONTAL BULB RETAINER O/B ATTACHED BRACKET CRACKED MKD DOT<[01] REMOVED AND REPLACED HORIZONTAL RETAINER TO DEFLECT
- [SDR SWAA2024041863556](https://openairdocs.org/sdr/SWAA2024041863556), Mar 15, 2024: CHANNEL. CORRODED. CORROSION FOUND AFT CARGO RH 'Z' CHANNEL FROM STA 727B TO STA 727C RBL 21 WL 155.5 HAS SPOT OF CORROSION.<[01] REMOVED AND REPLACED R/H Z-CHANNEL AT AFT CARGO C
- [SDR SWAA2024041863550](https://openairdocs.org/sdr/SWAA2024041863550), Mar 15, 2024: CHANNEL. CORRODED. CORROSION FOUND AFT CARGO RH 'Z' CHANNEL FROM STA 727D TO STA 727E RBL 21 WL 155.5 HAS SPOTS OF CORROSION.<[01] R/H Z-CHANNEL WAS REMOVED AND REPLACED ON TASK C
- [SDR SWAA2024041863557](https://openairdocs.org/sdr/SWAA2024041863557), Mar 15, 2024: CHANNEL. CORRODED. CORROSION FOUND AFT CARGO RH 'Z' CHANNEL FROM STA 727E TO STA 747 RBL 21 WL 155.5 HAS SPOTS OF CORROSION.<[01] R/H Z-CHANNEL WAS REMOVED AND REPLACED ON TASK CA
- [SDR SWAA2024041863558](https://openairdocs.org/sdr/SWAA2024041863558), Mar 15, 2024: CHANNEL. CORRODED. CORROSION FOUND AFT CARGO RH 'Z' CHANNEL FROM STA 747 TO STA 767 RBL 21 WL 155.5 HAS SPOTS OF CORROSION.<[01] R/H Z-CHANNEL WAS REMOVED AND REPLACED ON TASK CAR

All 275: https://openairdocs.org/aircraft/N7702A/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 N7702A

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N7702A before.

- [Cancelled 1956-10-17](https://openairdocs.org/deregistered/N7702A-1956-10-17): Cessna 180, S/N 32599. 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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