# N7825A: 2003 Boeing 737-7CT - Status: Valid registration - Airframe: [Boeing 737-7CT](https://openairdocs.org/model/boeing-737-7ct) (registry code 13844NE, 149 seats) - Engine: [CFM International CFM56-7B24 series](https://openairdocs.org/engine/cfm-international-cfm56-7b24-series) (registry code 13044) - Serial number: 32750 - Year built: 2003 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: August 6, 2015 - Certificate issued: February 27, 2015 - Expires: February 29, 2028 - Mode S code: AA9AFC - 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=7825A - Page: https://openairdocs.org/aircraft/N7825A From the FAA registry file of October 28, 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. ## NTSB investigations None matched to N7825A. ## FAA accident and incident reports (1) From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [Incident 20170612006899I](https://openairdocs.org/incident/20170612006899I), Jun 12, 2017: Boeing 737-7CT (N7825A), Chicago, IL, Minor damage. On Monday, June 12, 2017 approximately 1411 CST, southwest airlines co. (swaa) flight SWA1914 with service from Chicago midway airport (mdw) to windsor locks… ## ADs that may apply (OpenAirDocs): 19 in force ### Matched by airframe (Boeing 737-7CT) 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 ## Service difficulty reports (196, 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 SWAA2026101272071](https://openairdocs.org/sdr/SWAA2026101272071), Oct 7, 2026: TRAY TABLE. BROKEN. PASSENGER SEAT TRAY TABLE DAMAGED. REPLACED MISSING SCREW IAW AMM 25-22-00. - [SDR SWAA2026090803429](https://openairdocs.org/sdr/SWAA2026090803429), Sep 3, 2026: ENGINE. SHUTDOWN. NR 2 ENGINE SHUTDOWN ON TAXI OUT, RESTARTED WITH NO FURTHER INCIDENT. CHECKED IDG OIL LEVEL, CHECKED GOOD. CHECKED NR 2 SPAR VALVE OPERATION, CHECKED GOOD IAW M - [SDR SWAA2026043093048](https://openairdocs.org/sdr/SWAA2026043093048), Apr 26, 2026: METERING VALVE. FAILED. LINED UP AIRCRAFT ON 27R, ENGINES STABILIZED AT 40% N1, RELEASE BRAKES AND ACFT IMMEDIATELY PULLS HARD RIGHT 30-35. ABORTED TAKE OFF AND TAXIED BACK TO GATE. GR - [SDR SWAA2025122253871](https://openairdocs.org/sdr/SWAA2025122253871), Dec 19, 2025: CLAMP. OUT OF ADJUST. FWD SERVICE DOOR HAS A LOOSE RETENTION GIRT BAR CLAMP. ADJUSTED FWD SERVICE DOOR GIRT BAR CLAMPS PER SIP. - [SDR SWAA2025121752557](https://openairdocs.org/sdr/SWAA2025121752557), Dec 14, 2025: SCREW. MISSING. RIGHT FORWARD SERVICE DOOR EMERGENCY EVAC SLIDE COVER LEFT SIDE SCREW IS MISSING. INSTALLED NEW FASTENER @FWD SERVICE DOOR SLIDE CONTAINER IAW AMM 20-50-11. - [SDR SWAA2025100319191](https://openairdocs.org/sdr/SWAA2025100319191), Sep 29, 2025: FUEL SYS. LEAKING. SUSPECTED FUEL LEAK FROM NO.1 ENGINE SIDE. NEEDED TO CROSSFEED TWICE DUE TO 400 LB. IMBALANCE. NOTED FUEL FLOW NR 1 SIDE HIGHER THAN NR 2 SIDE BY AS MUCH AS 200 - [SDR SWAA2025040720989](https://openairdocs.org/sdr/SWAA2025040720989), Apr 2, 2025: AIR DATA MODULE. FAILED. IAS DISAGREE ON BOTH PFDS - CAPT SIDE UNRELIABLE. LOST AIRSPEED / ALTITUDE / EECS ON ALTN / SPEED TRIM FAIL.<[01] R&R FO?S AIR DATA MODULE IAW AMM 34-21-04;[02] - [SDR SWAA2025022498763](https://openairdocs.org/sdr/SWAA2025022498763), Feb 20, 2025: O-RING. LEAKING. SUSPECTED HYDRAULIC LEAK IN MAIN WHEEL WELL. REMOVED AND REPLACED O-RING AT BOTTOM OF ALT. BRAKE SELECTOR VALVE REF AMM 32-41-93 - [SDR SWAA2025021294982](https://openairdocs.org/sdr/SWAA2025021294982), Feb 11, 2025: BATTERY PACK. INOPERATIVE. ALL EMERGENCY LIGHTS RELATED TO BATTERY PACK M2335 INOP<[01] REMOVED; REPLACED WITH SERVICEABLE UNIT; AND PERFORMED GOOD INSTALLATION TEST OF M2335 BATTERY PACK - [SDR SWAA2025021389623](https://openairdocs.org/sdr/SWAA2025021389623), Jan 25, 2025: THRESHOLD WEB. CORRODED. .MULTIPLE SPOT WITH CORROSION ON FCB DOOR CUTOUT SURROUND THRESHOLD BS440+6 TO BS460+13 RBL30;WL156<[01] FCB DOOR CUTOUT SURROUND THRESHOLD REPAIR BY REPLACEMEN - [SDR SWAA2025021389624](https://openairdocs.org/sdr/SWAA2025021389624), Jan 25, 2025: THRESHOLD. CORRODED. MULTIPLE SPOT WITH CORROSION ON ACB DOOR CUTOUT SURROUND THRESHOLD BS794.3 TO BS827+3 RBL30 WL156.<[01] UPDATED STEP 3;[02] 01 - REMOVED AND REPLACED PER [SRM 5 - [SDR SWAA2025021388732](https://openairdocs.org/sdr/SWAA2025021388732), Jan 23, 2025: SEAT TRACK. CORRODED. CORROSION ON SEAT TRACK RBL 45.5 BS616+10; BS616+13; BS616+14; BS639+15; BS663+15; BS663+18; WL 208 (MARKED)<[01] CERTIFY ACTION #2;[02] UPDATED MEASUREMENT TAB - [SDR SWAA2025021388731](https://openairdocs.org/sdr/SWAA2025021388731), Jan 23, 2025: SEAT TRACK. CORRODED. CORROSION ON SEAT TRACK RBL 45.5 BS540+1.5; BS540+8; BS540+11.5; BS540+19; BS559+7; BS559+15; BS578+13; BS597+4; BS597+8.5; BS597+12; BS597+13 (MARKED)<[01] SEA - [SDR SWAA2025021388733](https://openairdocs.org/sdr/SWAA2025021388733), Jan 23, 2025: SEAT TRACK. CORRODED. CORROSION ON SEAT TRACK RBL 45.5 BS706+4; BS706+5.5; BS706+7; BS706+17.5; BS727+13; BS727+17.5; BS727A+6.5; BS727A+8.5 WL 208 (MARKED<[01] SEAT TRACK AT BS 540- - [SDR SWAA2025021288726](https://openairdocs.org/sdr/SWAA2025021288726), Jan 23, 2025: FLOOR PANEL. PULLED. FLOOR PANEL 241AF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FABRICATED NEW FLOOR PANEL 241AF IAW SRM 53-00-50-2R-0 AND BOEING DWG 144A5810 ID: 0127.;[02] VER - [SDR SWAA2025021088724](https://openairdocs.org/sdr/SWAA2025021088724), Jan 23, 2025: FLOOR PANEL. PULLED. FLOOR PANEL 231XF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 231XF HAS BEEN REPLACED IAW SRM 53-00-50-2R-0 PARA 1. A. NOTE:;[02] VERIFIED CORRECTI - [SDR SWAA2025021088727](https://openairdocs.org/sdr/SWAA2025021088727), Jan 23, 2025: FLOOR PANEL. PULLED. FLOOR PANEL 241DF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] 04 - REPAIRED PULLED STRANDS ON UPPER SURFACE PER [SRM 53-00-50-2R-0-A00938 (REPAIR GENERAL - COM - [SDR SWAA2025021388720](https://openairdocs.org/sdr/SWAA2025021388720), Jan 22, 2025: SCUFF PLATE. CRACKED. AFT CARGO COMPARTMENT FWD CORNER SCUFFPLATE IS CRACKED.<[01] VERIFIED APPLICABILITY OF SRM 53-60-15-2R-1;[02] REPAIRED AFT CARGO COMPARTMENT FWD CORNER SCUFFPLA - [SDR SWAA2025021387665](https://openairdocs.org/sdr/SWAA2025021387665), Jan 19, 2025: PANEL. DEBONDED. RIGHT WING L/E PANEL 621DB HAS DISBONDS AT I/B FWD CORNER AND FWD PANEL CUTOUT CORNERS<[01] RIGHT WING L/E PANEL 621DB WAS REPAIRED IAW SRM 51-70-05-2R-6;[02] J - [SDR SWAA2024102852089](https://openairdocs.org/sdr/SWAA2024102852089), Oct 23, 2024: BATTERY PACK. FAILED. L/H FWD EMERGENCY LIGHTING BATTERY PACK FAILED THE CAPACITY CHECK.<[01] REMOVED AND REPLACED BATTERY PACK PER M/M 33-51-06. - [SDR SWAA2024102852088](https://openairdocs.org/sdr/SWAA2024102852088), Oct 23, 2024: BATTERY PACK. FAILED. R/H FWD EMERGENCY LIGHTING BATTERY PACK FAILED THE CAPACITY CHECK.<[01] REMOVED AND REPLACED BATTERY PACK PER M/M 33-51-06. - [SDR SWAA2024070308105](https://openairdocs.org/sdr/SWAA2024070308105), Jul 2, 2024: DOUBLER. CRACKED. EXTERNAL POWER DOOR DOUBLER CUTOUT CRACKED<[01] REPAIRED DAMAGED PER SRM 53-10-15-2R-4;[02] VERIFIED REPAIRED DAMAGED PER SRM 53-10-15-2R-4 - [SDR SWAA2024070106886](https://openairdocs.org/sdr/SWAA2024070106886), Jun 27, 2024: DOUBLER. CRACKED. EXTERNAL POWER DOOR DOUBLER CUTOUT CRACKED<[01] COMPLIED WITH EA 24-153-01763 - [SDR SWAA2024062103450](https://openairdocs.org/sdr/SWAA2024062103450), Jun 20, 2024: HANDLE. LOOSE. LEFT EMERGENCY HATCH ASSIST HANDLE SURROUND NOT SECURE<[01] 01 - RESECURED LEFT EMERGENCY HATCH ASSIST HANDLE SURROUND PER [AMM 52-22-51-400-801-NG (EMERGENCY E - [SDR SWAA2023112724727](https://openairdocs.org/sdr/SWAA2023112724727), Nov 25, 2023: SLIDE. OUT OF LIMITS. AFT LEFT EMERGENCY ESCAPE SLIDE PRESSURE GAUGE BELOW LIMITS.<[01] REMOVED AND REPLACED AFT ENTRY DOOR ESCAPE SLIDE REF MM 25-66-01. - [SDR SWAA2023101309589](https://openairdocs.org/sdr/SWAA2023101309589), Oct 11, 2023: PANEL. DELAMINATED. #2 ENGINE; AFT ACOUSTICAL PANEL ABOVE THE 3 OCLOCK STRUT HAS DELAMINATED SKIN WITH EXPOSED CORE<[01] R&R?D #2 ENG; AFT ACOUSTICAL PANEL LOCATED ABOVE 3 O?CLOCK - [SDR SWAA2023021494067](https://openairdocs.org/sdr/SWAA2023021494067), Jan 22, 2023: SUPPORT ANGLE. CRACKED. CRACK ON SUPPORT ANGLE LOCATED FRONT SPAR WEB BOOST PUMP IFSS 120 AT LT WING 2023-38078<[01] TOOL USED DIGITAL CALIPER P/N: 500-193-30 S/N: 0000293 DUE DATE: 12 - [SDR SWAA2023021491846](https://openairdocs.org/sdr/SWAA2023021491846), Jan 15, 2023: PANEL. ELONGATED. ELONGATED HOLE LOC. BTW STAB STA133.15 TO STA 151.15 AT L/H HORIZONTAL STABILIZER LEADING EDGE PANEL 2023-38061<[01] EDDY CURRENT EQUIPMENT P/N: NORTEC500D; S/N - [SDR SWAA2023021491842](https://openairdocs.org/sdr/SWAA2023021491842), Jan 15, 2023: BRACKET. CRACKED. CRACK BODY STATION 540 LBL 19 BRACKET AT AIR CONDITIONING BAY 2023-38044<[01] REPLACED BRACKET LOCATED AT BODY STATION 540 LBL 19 AIR CONDITIONING BAY IAW B737- - [SDR SWAA2023021491843](https://openairdocs.org/sdr/SWAA2023021491843), Jan 15, 2023: ANGLE. CRACKED. CRACK BODY STA 663.75 ANGLE RBL 19 AT AIR CONDITIONING BAY 2023-38046<[01] TOOL USED: TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 112031023 DUE DATE: 01-FEB-2 - [SDR SWAA2023021491844](https://openairdocs.org/sdr/SWAA2023021491844), Jan 15, 2023: ANGLE. CRACKED. CRACK BODY STA 663.75 ANGLE LBL 20 AT AIR CONDITIONING BAY 2023-38045<[01] TOOL USED: ET EQUIPMENT P/N: NORTEC 500D; S/N: N500X12101V022233; DUE DATE: 30-AUG-23 - [SDR SWAA2023021391845](https://openairdocs.org/sdr/SWAA2023021391845), Jan 15, 2023: ANGLE. CRACKED. CRACK BODY STA 663.75 ANGLE RBL 43 AT AIR CONDITIONING BAY 2023-38047<[01] FAULT RESOLVED IN OTHER FAULT SEE TTG8Q00H93R9;[02] FAULT RESOLVED IN OTHER FAULT SEE - [SDR SWAA2023021491563](https://openairdocs.org/sdr/SWAA2023021491563), Jan 13, 2023: WEB. CORRODED. CORROSION FRONT SPAR ON INDICATOR FUEL TANK WEB AT RT WING 2023-38015<[01] REPLACED REFUEL PANEL P15 IAW B737-700 AMM 28-21-00-000-801; AMM 28-41-61-000-801; AM - [SDR SWAA2023021391366](https://openairdocs.org/sdr/SWAA2023021391366), Jan 13, 2023: STRIP. BROKEN. BROKEN CARPET PHOTOLUMINESCENTS STRIPS (10EA) AT PASSENGER CABIN (10 EA) 2023-38003<[01] REPLACED CARPET PHOTOLUMINESCENTS STRIPS (10EA) AT PASSENGER CABIN (10 - [SDR SWAA2023021491241](https://openairdocs.org/sdr/SWAA2023021491241), Jan 12, 2023: TRACK. CRACKED. CRACK TRACK RBBL 13.80 LOCATED BS 727E AFT CARGO COMPARTMENT 2023-37981<[01] EDDY CURRENT EQUIPMENT USED P/N: NORTEC 600D; S/N: 210138203; DUE DATE: 11-APR-23;[ - [SDR SWAA2023021491003](https://openairdocs.org/sdr/SWAA2023021491003), Jan 12, 2023: SUPPORT ANGLE. CRACKED. CRACK ON SUPPORT ANGLE LOCATED BTW BS 907 TO BS 927 AFT POSITION RBL 4 AT AFT CARGO COMPARTMENT 2023-37978<[01] REPLACED SUPPORT ANGLE LOCATED BTW BS 907 TO BS - [SDR SWAA2023021491001](https://openairdocs.org/sdr/SWAA2023021491001), Jan 12, 2023: SUPPORT. CORRODED. CORROSION SUPPORT ZEE LOCATED BTW BS 787 TO BS 727B LBL 21 WL 156 AFT CARGO COMPARTMENT 2023-37979<[01] TOOL USED: ULTRASONIC THICKNESS GAGE; P/N: 45MG; S/N: 22 - [SDR SWAA2023021490852](https://openairdocs.org/sdr/SWAA2023021490852), Jan 11, 2023: SUPPORT ANGLE. CRACKED. CRACK ANGLE - SUPPORT LOCATED BS 807 RBL 21 AT LEVEL FLOOR STRUCTURE AFT CARGO COMPARTMENT 2023-37954<[01] REPLACED ANGLE - SUPPORT LOCATED BS 807 RBL 21 AT LEV - [SDR SWAA2023021490854](https://openairdocs.org/sdr/SWAA2023021490854), Jan 11, 2023: STRINGER. CRACKED. CRACK STRINGER 27R BS 540 FWD CARGO COMPARTMENT 2023-37966<[01] TOOL USED: ULTRASONIC THICKNESS GAGE P/N: 45MG; S/N: 130066401; DUE DATE: 21-SEP-23;[02] TOOLS U - [SDR SWAA2023021490851](https://openairdocs.org/sdr/SWAA2023021490851), Jan 11, 2023: RIB. CRACKED. CRACK LEADING EDGE RIB LOCATED L/E STA. 78.29 AT LT HORIZONTAL STABILIZER 2023-37953<[01] REPLACED RIB LOCATED L/E STA. 78.29 AT LT HORIZONTAL STABILIZER IAW SR - [SDR SWAA2023021490075](https://openairdocs.org/sdr/SWAA2023021490075), Jan 10, 2023: RIB. CRACKED. CRACK ON UPPER CHORD OF INSPAR RIB 120.30 FRONT SPAR AT RT HORIZONTAL STABILIZER 2023-37915<[01] TOOLS USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 1 - [SDR SWAA2023021490076](https://openairdocs.org/sdr/SWAA2023021490076), Jan 10, 2023: RIB. CRACKED. CRACK LOWER CHORD OF INSPAR RIB STAB STA 120.30 FRONT SPAR AT RT HORIZONTAL STABILIZER 2023-37916<[01] 'REFERT TO FAULT TTG8Q00H5JYF WHERE EA 23-155-00202 WAS A - [SDR SWAA2023021490470](https://openairdocs.org/sdr/SWAA2023021490470), Jan 10, 2023: RIB. CRACKED. CRACK LEADING EDGE RIB LOCATED LE STA 151.75 RT HORIZONTAL STAB 2023-37939<[01] REPLACED LEADING EDGE RIB LOCATED LE STA 151.75 RT HORIZONTAL STAB IAW SRM B737- - [SDR SWAA2023021490468](https://openairdocs.org/sdr/SWAA2023021490468), Jan 10, 2023: ACTUATOR. CRACKED. CRACK FUEL FLOAT ACTUATOR ON VALVE ACTUATOR VENT BTW RIB 21 AND RIB 22 AT RT WING 2023-37926<[01] REPLACED FLOAT ACTUATOR ON VALVE ACTUATOR VENT BTW RIB 21 AND - [SDR SWAA2023021490069](https://openairdocs.org/sdr/SWAA2023021490069), Jan 9, 2023: BRACKET. CRACKED. CRACK BILGE AREA BRACKET LOC BS 400 AND LBL 21.80 AT FWD CARGO COMPARTMENT 2023-37860<[01] REPLACED BRACKET AND FASTENERS LOC BS 400 AND LBL 21.80 AT FWD CARGO - [SDR SWAA2023021490067](https://openairdocs.org/sdr/SWAA2023021490067), Jan 9, 2023: STRINGER. CRACKED. CRACK STRINGER 23R BS 540 FWD CARGO COMPARTMENT 2023-37865<[01] EQUIPMENT P/N 45MG; S/N 130066701; DUE DATE 08-APR-23 WAS USED.;[02] TOOLS USED: TEMPERATURE CON - [SDR SWAA2023021490068](https://openairdocs.org/sdr/SWAA2023021490068), Jan 9, 2023: GUSSET. CRACKED. CRACK GUSSET LOC BS 500D AND STR 19L FWD CARGO COMPARTMENT 2023-37861<[01] REPLACED GUSSET LOC BS 500D AND STR 19L FWD CARGO COMPARTMENT IAW SRM B737-700 51-10- - [SDR SWAA2023021489755](https://openairdocs.org/sdr/SWAA2023021489755), Jan 9, 2023: SUPPORT ANGLE. CRACKED. CRACK ON SUPPORT ANGLE LOCATED FRONT SPAR WEB BOOST PUMP IFSS 120 AT LT WING 2023-37834<[01] FAULT RESOLVED IN OTHER FAULT SEE TTG8Q00HDJ3H;[02] FAULT RESOLVED - [SDR SWAA2023021489745](https://openairdocs.org/sdr/SWAA2023021489745), Jan 8, 2023: TIE CLIP. CRACKED. CRACK TIE CLIP BS 277 AT STR 10R AT PASSENGER CABIN 2023-37813<[01] REPLACED TIE CLIP BS 277 AT STR 10R AT PASSENGER CABIN IAW B737-700 SRM 51-40-02; SRM 51-10- - [SDR SWAA2023021489744](https://openairdocs.org/sdr/SWAA2023021489744), Jan 8, 2023: STUB FRAME. CRACKED. CRACK FRAME STUB ON BS 294.5 AT LEVEL STR 17R AT PASSENGER CABIN 2023-37814<[01] EDDY CURRENT EQUIPMENT P/N: NORTEC500D; S/N: N500X12101V022235; DUE DATE: 03-AU All 196: https://openairdocs.org/aircraft/N7825A/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 N7825A The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N7825A before. - [Cancelled 1957-01-08](https://openairdocs.org/deregistered/N7825A-1957-01-08): Cessna 180A, S/N 32722. Owner: [Cessna Aircraft Co](https://openairdocs.org/faa-owner/CESSNA%20AIRCRAFT%20CO), [Wichita, KS](https://openairdocs.org/faa-place/KS/Wichita) ## Related - Other Boeing 737-7CT aircraft: https://openairdocs.org/model/boeing-737-7ct/aircraft.md - The CFM International CFM56-7B24 series engine: https://openairdocs.org/engine/cfm-international-cfm56-7b24-series.md --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.