# N7823A: 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: 32749 - Year built: 2003 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: June 29, 2015 - Certificate issued: February 13, 2015 - Expires: February 29, 2028 - Mode S code: AA9AB6 - 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=7823A - Page: https://openairdocs.org/aircraft/N7823A 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. ## 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 ## NTSB investigations None matched to N7823A. ## FAA accident and incident reports None matched to N7823A. ## Service difficulty reports (227, 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 SWAA2026081758366](https://openairdocs.org/sdr/SWAA2026081758366), Aug 11, 2026: SEAL. CRACKED. LEFT HORIZONTAL STAB FWD UPPER SLIDING SEAL WAS CRACKED ALONG FORWARD TRACK EDGE. R & R LT HORIZONTAL STAB SLIDING SEAL IAW AMM 53-31-31. - [SDR SWAA2025112036937](https://openairdocs.org/sdr/SWAA2025112036937), Nov 20, 2025: ISOLATOR MOUNT. CRACKED. PASSENGER CABIN ESCAPE SLIDE FWD UPPER ISOLATOR CRACKED. R & R PASSENGER CABIN ESCAPE SLIDE FWD UPPER ISOLATOR IAW SRM 51-40-02. INSPECTION C/W R&R PASSENGER CA - [SDR SWAA2025061077148](https://openairdocs.org/sdr/SWAA2025061077148), Jun 2, 2025: BULB. INOPERATIVE. DURING EMERGENCY LIGHT OPERATIONAL TEST. FOUND AFT EMERGENCY LIGHT BULB IN R/H OVERWING EXIT WINDOW LIGHT ASSEMBLY INOP DURING EMERGENCY LIGHT OPERATIONAL TEST - [SDR SWAA2025061076837](https://openairdocs.org/sdr/SWAA2025061076837), May 31, 2025: BATTERY PACK. INOPERATIVE. EMERGENCY EXIT LIGHTS ASSOCIATED WITH BATTERY PACK (M1672) DO NOT ILLUMINATE. REMOVED AND REPLACED BATTERY PACK M1672 IAW AMM 33-51-06-960-805 AND PERFORMED GOO - [SDR SWAA2025061076627](https://openairdocs.org/sdr/SWAA2025061076627), May 30, 2025: BATTERY PACK. INOPERATIVE. EMERGENCY EXIT LIGHTS ASSOCIATED WITH BATTERY PACK (M1670) DO NOT ILLUMINATE. REPLACED EMERGENCY BATTERY PACK (M1670); PERFORMED GOOD TEST PER AMM 33-51-06-960- - [SDR SWAA2025061073449](https://openairdocs.org/sdr/SWAA2025061073449), May 21, 2025: FLOORBEAM. CRACKED. CRACKED PANEL BREAK AT MID CABIN BS540 RBL1 WL208. MARKED<[01] REMOVED AND REPLACED PANEL BREAK AT MID CABIN BS540 RBL1 WL208 IAW SRM 51-40-02 AND DWG# 143A5240 - [SDR SWAA2025061073451](https://openairdocs.org/sdr/SWAA2025061073451), May 21, 2025: FLOORBEAM. CRACKED. CRACKED PANEL BREAK AT MID CABIN BS540 RBL1 WL208<[01] THIS IS DUPLICATED CARD... REMOVED AND REPLACED ON FAULT# TTG8Q010QNP2;[02] CORRECTIVE ACTION ITEM 1 VERI - [SDR SWAA2025061073450](https://openairdocs.org/sdr/SWAA2025061073450), May 21, 2025: PANEL. CRACKED. VERTICAL STAB PANEL 323AL LOWER CLIP CRACKED.<[01] RECEIVED SERVICEABLE PANEL 323AL P/N:654A0004-711; BN 396992. PANEL WILL BE INSTALLED ON TASK CARD TTG8Q00Z3W - [SDR SWAA2025061073097](https://openairdocs.org/sdr/SWAA2025061073097), May 20, 2025: FLOORBEAM. CRACKED. CRACKED PANEL BREAK AT MID CABIN BS540 LBL1 WL208. MARKED<[01] REMOVED AND REPLACED BS540 LBL1 PANEL BREAK P/N#143A5240-63 IAW SRM 51-40-02 AND PER AIPC# 53-31- - [SDR SWAA2025061072596](https://openairdocs.org/sdr/SWAA2025061072596), May 19, 2025: ATTACH ANGLE. CRACKED. LT WING DEFLECTION CONTROL RIB UPPER PANEL ATTACHMENT CRACKED.<[01] REPAIRED LT WING DEFLECTION CONTROL RIB UPPER PANEL ATTACHMENT IAW SRM 57-51-02-2R-3.;[02] C - [SDR SWAA2025060972772](https://openairdocs.org/sdr/SWAA2025060972772), May 19, 2025: SKIN. CRACKED. CRACK ON LH LOWER HORIZONTAL STABILIZER SKIN. AT STAB STA 193.90; 23. 5' FROM FWD EDGE; .3' IN LENGTH (MARKED)<[01] REMOVED THE DAMAGED PART ON LH HORIZONTAL ST - [SDR SWAA2025061072458](https://openairdocs.org/sdr/SWAA2025061072458), May 18, 2025: SEAL. MISSING. R/H LOWER FWD SLIDE SEAL AND HARDWARE MISSING<[01] REPLACED R/H LOWER FWD SLIDE SEAL AND HARDWARE IAW AMM 53-31-31-400-803.;[02] CORRECTIVE ACTION COMPLETED. - [SDR SWAA2025042226090](https://openairdocs.org/sdr/SWAA2025042226090), Apr 18, 2025: LAMP. INOPERATIVE. EMERGENCY AREA LIGHTS AT SEAT ROW 12 LH & 13 RH INOP<[01] RELAMPED EMERGENCY AREA LIGHTS AT SEAT ROW 12 LH & 13 RH IAW AMM 33-51-03 OPS CHECK OK - [SDR SWAA2024102350782](https://openairdocs.org/sdr/SWAA2024102350782), Oct 19, 2024: LIGHT. INOPERATIVE. EMERGENCY LIGHT INOP AT SEAT ROW 4 LH<[01] RELAMPED EMERGENCY LIGHT AT SEAT ROW 4 LH IAW AMM 33-51-03 OPS CHECK OK - [SDR SWAA2024072617637](https://openairdocs.org/sdr/SWAA2024072617637), Jul 25, 2024: SENSOR. FAULTY. PER MOC/AHM DATA FLAP SENSOR LOCK OUT PENDING. PER QRH PERFORMED ZERO FLAPS LANDING WITH L/E ALT FLAP EXTENDED. NO ROLL OR ABNORMAL FLIGHT CHARACTERISTIC.<[01] - [SDR SWAA2024070808686](https://openairdocs.org/sdr/SWAA2024070808686), Jul 3, 2024: BALLAST. ODOR. DURING CLIMBOUT AT APPROXIMATLY 6000' WE ENCOUNTERED A STRONG ELECTRICAL BURNING SMELLTHAT DID NOT DISAPATEUNTILL AFTER LANDING<[01] PERFORMED SMOKE OR FUMES CO - [SDR SWAA2024070808807](https://openairdocs.org/sdr/SWAA2024070808807), Jul 3, 2024: BALLAST. OVERHEATED. DURING CLIMBOUT AT APPROXIMATLY 6000' WE ENCOUNTERED A STRONG ELECTRICAL BURNING SMELLTHAT DID NOT DISAPATEUNTILL AFTER LANDING<[01] PERFORMED SMOKE OR FUMES CO - [SDR SWAA2024050983471](https://openairdocs.org/sdr/SWAA2024050983471), May 8, 2024: BATTERY PACK. FAILED. BATTERY PACK M1674 FAILED CAPACITY CHECK. BATTERY PACKS M1674 AND M1675 FAILED CAPACITY CHECK.<[01] R&R BATTERY PACKS M1674 AND M1675 IAW AMM 33-51-06. - [SDR SWAA2024050984027](https://openairdocs.org/sdr/SWAA2024050984027), May 8, 2024: BATTERY PACK. FAILED. BATTERY PACK M1674 FAILED CAPACITY CHECK. BATTERY PACKS M1674 AND M1675 FAILED CAPACITY CHECK.<[01] R&R BATTERY PACKS M1674 AND M1675 IAW AMM 33-51-06. - [SDR SWAA2024031563927](https://openairdocs.org/sdr/SWAA2024031563927), Mar 15, 2024: BATTERY PACK. INOPERATIVE. EMERGENCY LIGHTS INOP IN AFT GALLEY.<[01] R/R BATTERY PACK M1673 PER AMM 33-51-06. - [SDR SWAA2023112825056](https://openairdocs.org/sdr/SWAA2023112825056), Nov 26, 2023: HANDLE. LOOSE. FWD ENTRY DOOR INTERIOR HANDLE LOOSE. MOVES UP APPROX 1 DURING FLIGHT<[01] C/W GUIDE ARM ADJUSTMENT ON FWD ENTRY DOOR PER MT 752-11-01 - [SDR SWAA2023112824735](https://openairdocs.org/sdr/SWAA2023112824735), Nov 25, 2023: GIRT BAR. OUT OF ADJUST. FWD ENTRY DOOR (L1) GIRT BAR WILL NOT SEAT<[01] REPACKED L1 SLIDE PER MT725-61-06. GIRT BAR STOWS PROPERLY - [SDR SWAA2023092905208](https://openairdocs.org/sdr/SWAA2023092905208), Sep 28, 2023: MEGAPHONE. INOPERATIVE. FWD L/H BULKHEAD MEGA PHONE INOP<[01] R/R FWD L/H BULKHEAD MEGA PHONE AMM 25-64-00 - [SDR SWAA2023061548548](https://openairdocs.org/sdr/SWAA2023061548548), May 13, 2023: ANGLE. CRACKED. CRACK ANGLE LOCATED ON FRONT SPAR WEB FUEL BOOST PUMP UPPER SURFACE BTW IFSS110 TO IFSS120 AT RT WING 2023-310574<[01] REPLACED ANGLE LOCATED ON FRONT SPAR WEB - [SDR SWAA2023061448066](https://openairdocs.org/sdr/SWAA2023061448066), May 12, 2023: ANGLE. CRACKED. CRACK ANGLE LOCATED UPPER SIDE BS663 RBL42 AND WL168 AT AIR CONDITIONING BAY 2023-310571<[01] TOOL USED: TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 142811020 - [SDR SWAA2023061547678](https://openairdocs.org/sdr/SWAA2023061547678), May 11, 2023: BALANCE WEIGHT. CORRODED. CORROSION AILERON BALANCE ADJUNTO WEINGHT LOC BALANCE BAY NO 5 UPPER AND LOWER AT RT WING (2 EA) 2023-310531<[01] REPLACED AILERON BALANCE WEIGHT LOC. BALANCE B - [SDR SWAA2023061547823](https://openairdocs.org/sdr/SWAA2023061547823), May 11, 2023: BALANCE WEIGHT. CORRODED. CORROSION AILERON BALANCE ADJUNTO WEINGHT LOC BALANCE BAY NO5 UPPER AND LOWER AT LT WING (6 EA) 2023-310556<[01] REPLACED AILERON BALANCE WEIGHT LOC. BALANCE BA - [SDR SWAA2023061447482](https://openairdocs.org/sdr/SWAA2023061447482), May 11, 2023: ROPE. MISSING. MISSING COMPARTMENT DOOR ESCAPE ROPE STRAP LT SIDE AT COCKPIT (1 EA) 2023-310520<[01] INSTALLED COMPARTMENT DOOR ESCAPE ROPE STRAP LT SIDE AT COCKPIT (1 EA) IAW - [SDR SWAA2023061447681](https://openairdocs.org/sdr/SWAA2023061447681), May 11, 2023: TIE CLIP. CRACKED. CRACK BILGE AREA TIE CLIP BS 500D LEVEL STRINGER 26L AT FWD CARGO COMPARTMENT 2023-310551<[01] REPLACED TIE CLIP LOC BILGE AREA BS 500D LEVEL STRINGER 26L AT FW - [SDR SWAA2023061447680](https://openairdocs.org/sdr/SWAA2023061447680), May 11, 2023: WEB. CRACKED. CRACK WEB INTERNAL STRUCTURE INBOARD FAN COWL ON ENGINE 1 2023-310525<[01] REPLACED WEB INTERNAL STRUCTURE INBOARD FAN COWL ON ENGINE 1 IAW GOODRICH AEROSTRUCTU - [SDR SWAA2023061447827](https://openairdocs.org/sdr/SWAA2023061447827), May 11, 2023: BRACKET. ELONGATED. ELONGATED HOLE INTERNAL CAVITY SUPPORT BRACKET INBOARD LEADING EDGE AT RT WING 2023-310566<[01] REPLACED BRACKET INBOARD LEADING-EDGE AT RT WING I.A.W. B737-700 - [SDR SWAA2023061547148](https://openairdocs.org/sdr/SWAA2023061547148), May 10, 2023: ANGLE. CRACKED. CRACK ANGLE LOCATE ON FRONT SPAR WEB FUEL BOOST PUMP UPPER SURFACE BTW IFSS110 TO IFSS120 AT LT WING 2023-310499<[01] REPLACED ANGLE LOCATE ON FRONT SPAR WEB FU - [SDR SWAA2023061447359](https://openairdocs.org/sdr/SWAA2023061447359), May 10, 2023: ANGLE. CRACKED. CRACK FLOOR STRUCTURE ANGLE ASSY LOCATED BS540 AND RBL1 WL208.1 AT PASSENGER CABIN 2023-310502<[01] REPLACED FLOOR STRUCTURE ANGLE ASSY LOCATED BS540 AND RBL1 W - [SDR SWAA2023061447360](https://openairdocs.org/sdr/SWAA2023061447360), May 10, 2023: ANGLE. CRACKED. CRACK FLOOR STRUCTURE ANGLE ASSY LOCATED BS540 AND LBL1 WL208.1 AT PASSENGER CABIN 2023-310503<[01] REPLACED ANGLE ASSY AND FASTENERS LOCATED FLOOR STRUCTURE BS - [SDR SWAA2023061447361](https://openairdocs.org/sdr/SWAA2023061447361), May 10, 2023: ANGLE. CRACKED. CRACK ANGLE LOCATED BS695 AND RBL24.75 WL203 AT PASSENGER CABIN 2023-310504<[01] TOOL USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811019; DUE DATE - [SDR SWAA2023061446840](https://openairdocs.org/sdr/SWAA2023061446840), May 9, 2023: LIGHT. DETERIORATED. DETERIORATED STRIP PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING AT PASSENGER CABIN (6 EA) 2023-310454<[01] REPLACED STRIP PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING - [SDR SWAA2023061447138](https://openairdocs.org/sdr/SWAA2023061447138), May 9, 2023: SUPPORT. CORRODED. CORROSION SUPPORT ZEE BTW STA 727 TO STA 767 RBL 21 AFT CARGO COMPARTMENT 2023-310488<[01] TOOL USED: ULTRASONIC THICKNESS GAGE. P/N: 45MG. S/N: 130064101. DUE - [SDR SWAA2023061447011](https://openairdocs.org/sdr/SWAA2023061447011), May 9, 2023: PLATE. CORRODED. CORROSION BILGE AREA PLATE BTW BS 767 TO BS 787 RBL 21 AT AFT CARGO COMPARTMENT 2023-310476<[01] TOOL USED: ULTRASONIC EQUIPMENT P/N: 45 MG; S/N: 130060401; DUE - [SDR SWAA2023061447006](https://openairdocs.org/sdr/SWAA2023061447006), May 9, 2023: FRAME. CRACKED. CRACK FRAME BS480 AND BETWEEN STR8R TO STR9R AT PASSENGER CABIN 2023-310471<[01] TOOL USED: EDDY CURRENT EQUIPMENT PN: NORTEC 600D; SN: 220272712; DUE DATE: 17- - [SDR SWAA2023061446832](https://openairdocs.org/sdr/SWAA2023061446832), May 9, 2023: GRIP. BROKEN. BROKEN EMERGENCY DOOR GRIP ASSY LT SIDE AT PASSENGER CABIN (1 EA) 2023-310447<[01] REPLACED EMERGENCY DOOR GRIP ASSY LT SIDE AT PASSENGER CABIN (1 EA) IAW B737- - [SDR SWAA2023061446833](https://openairdocs.org/sdr/SWAA2023061446833), May 9, 2023: GRIP. BROKEN. BROKEN EMERGENCY DOOR GRIP ASSY RT SIDE AT PASSENGER CABIN (1 EA) 2023-310448<[01] REPLACED EMERGENCY DOOR GRIP ASSY RT SIDE AT PASSENGER CABIN (1 EA) IAW B737- - [SDR SWAA2023061447008](https://openairdocs.org/sdr/SWAA2023061447008), May 9, 2023: SUPPORT ANGLE. CRACKED. CRACK ANGLE - SUPPORT BS 727B TO BS 827 AT LEVEL STR18L AND WL202 AT AFT CARGO COMPARTMENT 2023-310473<[01] REPLACED ANGLE - SUPPORT BS 727B TO BS 827 AT LEVEL - [SDR SWAA2023061446831](https://openairdocs.org/sdr/SWAA2023061446831), May 8, 2023: FRAME. CRACKED. CRACK FRAME LOCATED BS312 AND BETWEEN STR5L TO STR6L AT PASSENGER CABIN 2023-310438<[01] REPAIRED FRAME LOCATED BS312 AND BETWEEN STR5L TO STR6L AT PASSENGER CA - [SDR SWAA2023061446830](https://openairdocs.org/sdr/SWAA2023061446830), May 8, 2023: TIE CLIP. CRACKED. CRACK TIE CLIP LOCATED BS277 AND STR10R AT PASSENGER CABIN 2023-310435<[01] REPLACED TIE CLIP LOCATED BS277 AND STR10R AT PASSENGER CABIN IAW B737-700 SRM 51-10 - [SDR SWAA2023061446744](https://openairdocs.org/sdr/SWAA2023061446744), May 8, 2023: STRINGER. CRACKED. CRACK STRINGER 26L BS 540 FWD CARGO COMPARTMENT 2023-310422<[01] TOOL USED P/N: 35DL; S/N: 091419910; CAL DUE: 13-MAR-24.;[02] TOOL USED: ET EQUIPMENT P/N: NORT - [SDR SWAA2023061446745](https://openairdocs.org/sdr/SWAA2023061446745), May 8, 2023: STRINGER. CRACKED. CRACK STRINGER 23L BS 540 FWD CARGO COMPARTMENT 2023-310421<[01] TOOL USED P/N: 35DL; S/N: 091419910; CAL DUE: 13-MAR-24.;[02] TOOL USED: ET EQUIPMENT P/N: NORT - [SDR SWAA2023061446747](https://openairdocs.org/sdr/SWAA2023061446747), May 8, 2023: PANEL. CRACKED. CRACK SEAL PLATE ACCESS PANEL 343AB AT RT HORIZONTAL STAB 2023-310433<[01] REPLACED SEAL PLATE ACCESS PANEL 343AB AT RT HORIZONTAL STA I.A.W B737-700 SRM 51-10- - [SDR SWAA2023061446297](https://openairdocs.org/sdr/SWAA2023061446297), May 7, 2023: SCUFF PLATE. CRACKED. CRACK FWD CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT 2023-310372<[01] TOOL USED DIGITAL CALIPER P/N:54-100-000-2;S/N:AE-32464;DUE DATE:04-MAR-24.;[02] TOOL USE - [SDR SWAA2023061446296](https://openairdocs.org/sdr/SWAA2023061446296), May 7, 2023: SCUFF PLATE. CRACKED. CRACK SCUFF PLATE AFT CORNER AT AFT CARGO COMPARTMENT 2023-310371<[01] TOOL USED DIGITAL CALIPER P/N:54-100-000-2;S/N:AE-32464;DUE DATE:04-MAR-24.;[02] TOOL USE - [SDR SWAA2023061446303](https://openairdocs.org/sdr/SWAA2023061446303), May 7, 2023: LENS. BROKEN. BROKEN EMERGENCY EXIT LENS GALLEY 4 AT AFT GALLEY AREA (1 EA) 2023-310382<[01] REPLACED EMERGENCY EXIT LENS GALLEY 4 AT AFT GALLEY AREA (1 EA) IAW B737-700 AMM- All 227: https://openairdocs.org/aircraft/N7823A/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 N7823A The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N7823A before. - [Cancelled 1956-12-18](https://openairdocs.org/deregistered/N7823A-1956-12-18): Cessna 180A, S/N 32720. 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.