# N7828A: 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: 33697
- Year built: 2003
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: August 20, 2015
- Certificate issued: March 24, 2015
- Expires: March 31, 2028
- Mode S code: AA9B65
- 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=7828A
- Page: https://openairdocs.org/aircraft/N7828A

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 737-7CT)

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 N7828A.

## FAA accident and incident reports

None matched to N7828A.

## Service difficulty reports (208, 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 SWAA2026083132559](https://openairdocs.org/sdr/SWAA2026083132559), Aug 27, 2026: SLIDE. OUT OF POSITION. CABIN - AFT GALLEY SERVICE DOOR R2 SLIDE GIRT HANGS LOW. REPACKED CABIN AFT GALLEY SERVICE DOOR R2 SLIDE GIRT REF AMM 25-66-01.
- [SDR SWAA2026083122879](https://openairdocs.org/sdr/SWAA2026083122879), Aug 27, 2026: PANEL. CRACKED. CABIN - AFT GALLEY SERVICE DOOR R2 LOWER PANEL 844DZ AFT MOUNTING BRACKET CRACKED. R/R AFT GALLEY SERVICE DOOR R2 LOWER PAN ASSY REF AMM 52-41-31.
- [SDR SWAA2026081050870](https://openairdocs.org/sdr/SWAA2026081050870), Aug 6, 2026: LIGHT. DETACHED. RT OVERWING AND FWD SERVICE DOOR INDICATOR LIGHTS FELL FROM OVERHEAD PANEL ON TAKEOFF RESECURED RT OVERWING AND FWD SERVICE INDICATOR LIGHTS IAW SIP. OPS CHECK 
- [SDR SWAA2026070617710](https://openairdocs.org/sdr/SWAA2026070617710), Jul 1, 2026: LIGHT. BROKEN. OVERWING EXIT KORRY LIGHT BROKEN. REINSTALLED IAW SIP.
- [SDR SWAA2025062383727](https://openairdocs.org/sdr/SWAA2025062383727), Jun 19, 2025: CABIN AIR SYS. ODOR. FORWARD FLIGHT ATTENDANTS REPORTED A EXHAUST SMELL ON A CLIMBOUT. NO ABNORMAL SMELLS OR INDICATION ON THE COCKPIT OR AFT SECTION OF THE AIRPLANE <[01]. C/W COND
- [SDR SWAA2025043021762](https://openairdocs.org/sdr/SWAA2025043021762), Apr 4, 2025: STRINGER SPLICE. CORRODED. CORROSION STRINGER SPLICE 28L STA360 AT EQUIPMENT ELECTRONIC COMP 2025-238305<[01] TOOLS USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 142811020; DUE 
- [SDR SWAA2025043021682](https://openairdocs.org/sdr/SWAA2025043021682), Apr 4, 2025: PLATE. CRACKED. CRACK CORRUGATED PLATE TRAILING EDGE LOCATED AT LEVEL IRSS 215 AT LT WING 2025-238300<[01] REPLACED NEW CORRUGATED PLATE TRAILING EDGE LOCATED AT LEVEL IRSS 215
- [SDR SWAA2025043021684](https://openairdocs.org/sdr/SWAA2025043021684), Apr 4, 2025: PLATE. CRACKED. CRACK CORRUGATED PLATE TRAILING EDGE LOCATED AT LEVEL ORSS 261 AT RT WING 2025-238301<[01] REPLACED NEW CORRUGATED PLATE TRAILING EDGE LOCATED AT LEVEL ORSS 261
- [SDR SWAA2025043021685](https://openairdocs.org/sdr/SWAA2025043021685), Apr 4, 2025: ANGLE. CRACKED. CRACK ANGLE TRAILING EDGE LOCATED ORSS 272 DEFLECTION CONTROL RIB AREA AT RT WING 2025-238302<[01] REPLACED ANGLE TRAILING EDGE LOCATED ORSS 272 DEFLECTION CONT
- [SDR SWAA2025043055843](https://openairdocs.org/sdr/SWAA2025043055843), Apr 4, 2025: PLATE. CRACKED. CRACK CORRUGATED PLATE TRAILING EDGE LOCATED AT LEVEL IRSS 215 AT LT WING 2025-238300<[01] REPLACED NEW CORRUGATED PLATE TRAILING EDGE LOCATED AT LEVEL IRSS 215
- [SDR SWAA2025043055845](https://openairdocs.org/sdr/SWAA2025043055845), Apr 4, 2025: PLATE. CRACKED. CRACK CORRUGATED PLATE TRAILING EDGE LOCATED AT LEVEL ORSS 261 AT RT WING 2025-238301<[01] REPLACED NEW CORRUGATED PLATE TRAILING EDGE LOCATED AT LEVEL ORSS 261
- [SDR SWAA2025043055846](https://openairdocs.org/sdr/SWAA2025043055846), Apr 4, 2025: ANGLE. CRACKED. CRACK ANGLE TRAILING EDGE LOCATED ORSS 272 DEFLECTION CONTROL RIB AREA AT RT WING 2025-238302<[01] REPLACED ANGLE TRAILING EDGE LOCATED ORSS 272 DEFLECTION CONT
- [SDR SWAA2025042955847](https://openairdocs.org/sdr/SWAA2025042955847), Apr 4, 2025: STRINGER SPLICE. CORRODED. CORROSION STRINGER SPLICE 28L STA360 AT EQUIPMENT ELECTRONIC COMP 2025-238305<[01] TOOLS USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 142811020; DUE 
- [SDR SWAA2025043055842](https://openairdocs.org/sdr/SWAA2025043055842), Apr 3, 2025: PLATE. CRACKED. CRACK CORRUGATED PLATE TRAILING EDGE LOCATED AT LEVEL ORSS261 AT LT WING 2025-238292<[01] REPLACED NEW CORRUGATED PLATE TRAILING EDGE LOCATED AT LEVEL ORSS261 A
- [SDR SWAA2025042955841](https://openairdocs.org/sdr/SWAA2025042955841), Apr 3, 2025: FRAME. CRACKED. CRACK ON FRAME LOCATED BS 727D BTW STR 8R TO STR 9R AT PASSENGER CABIN 2025-238282<[01] PERFORMED REPAIR ON FRAME LOCATED BS 727D BTW STR 8R TO STR 9R AT PASSEN
- [SDR SWAA2025043020500](https://openairdocs.org/sdr/SWAA2025043020500), Apr 1, 2025: PRESSURE WEB. CRACKED. CRACK INDICATION FOUND ON HORIZONTAL PRESSURE DECK WEB AT RBL 41 BETWEEN STA 663 TO BS 675 AT MAIN WHEEL WELL COMPARTMENT. CRACK LENGTH: 0.375 IN. APPROX 2025-2
- [SDR SWAA2025043020347](https://openairdocs.org/sdr/SWAA2025043020347), Apr 1, 2025: THRESHOLD. CRACKED. CRACK ON THRESHOLD SHEET AFT CARGO COMPARTMENT 2025-238163<[01] REPLACED THRESHOLD SHEET AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 146A8340
- [SDR SWAA2025043020771](https://openairdocs.org/sdr/SWAA2025043020771), Apr 1, 2025: FLOORBEAM. CRACKED. CRACK ON BRAKE PANEL FLOOR STRUCTURE LOCATED STA540 AND LBL 1 AT PASSENGER CABIN 2025-238184<[01] REPLACED BRAKE PANEL FLOOR STRUCTURE LOCATED STA540 AND BETWEE
- [SDR SWAA2025043020501](https://openairdocs.org/sdr/SWAA2025043020501), Apr 1, 2025: ACCESS PANEL. DELAMINATED. DELAMINATED ACCESS PANEL 193B BODY FAIRING AT LOWER FUSELAGE 2025-238170<[01] TOOL USED CALIPER PN: 500-197-30; SN: B20189334; DUE DATE: 26/JAN/26.;[02] TOOL US
- [SDR SWAA2025043020348](https://openairdocs.org/sdr/SWAA2025043020348), Apr 1, 2025: SCUFF PLATE. CRACKED. CRACK FWD CORNER SCUFF PLATE AFT CARGO COMPARTMENT 2025-238162<[01] TOOL USED DIGITAL CALIPER P/N: 500-193-30; S/N: 0000291; DUE DATE: 01-NOV-25.;[02] TOOL USED
- [SDR SWAA2025043055801](https://openairdocs.org/sdr/SWAA2025043055801), Apr 1, 2025: THRESHOLD. CRACKED. CRACK ON THRESHOLD SHEET AFT CARGO COMPARTMENT 2025-238163<[01] REPLACED THRESHOLD SHEET AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 146A8340
- [SDR SWAA2025043055802](https://openairdocs.org/sdr/SWAA2025043055802), Apr 1, 2025: SCUFF PLATE. CRACKED. CRACK FWD CORNER SCUFF PLATE AFT CARGO COMPARTMENT 2025-238162<[01] TOOL USED DIGITAL CALIPER P/N: 500-193-30; S/N: 0000291; DUE DATE: 01-NOV-25.;[02] TOOL USED
- [SDR SWAA2025043055807](https://openairdocs.org/sdr/SWAA2025043055807), Apr 1, 2025: FLOORBEAM. CRACKED. CRACK ON BRAKE PANEL FLOOR STRUCTURE LOCATED STA540 AND LBL 1 AT PASSENGER CABIN 2025-238184<[01] REPLACED BRAKE PANEL FLOOR STRUCTURE LOCATED STA540 AND BETWEE
- [SDR SWAA2025043055804](https://openairdocs.org/sdr/SWAA2025043055804), Apr 1, 2025: ACCESS PANEL. DELAMINATED. DELAMINATED ACCESS PANEL 193B BODY FAIRING AT LOWER FUSELAGE 2025-238170<[01] TOOL USED CALIPER PN: 500-197-30; SN: B20189334; DUE DATE: 26/JAN/26.;[02] TOOL US
- [SDR SWAA2025042955803](https://openairdocs.org/sdr/SWAA2025042955803), Apr 1, 2025: PRESSURE WEB. CRACKED. CRACK INDICATION FOUND ON HORIZONTAL PRESSURE DECK WEB AT RBL 41 BETWEEN STA 663 TO BS 675 AT MAIN WHEEL WELL COMPARTMENT. CRACK LENGTH: 0.375 IN. APPROX 2025-2
- [SDR SWAA2025043020344](https://openairdocs.org/sdr/SWAA2025043020344), Mar 31, 2025: ACCESS PANEL. CRACKED. CRACK AROUND HOLES ACCESS PANEL 561CB TRAILING EDGE AT LT WING 2025-238153<[01] TOOL USED ON STEP 12:ULTRASONIC EQUIPMENT P/N:EPOCH 650; S/N:190984811; DUE DATE
- [SDR SWAA2025043055798](https://openairdocs.org/sdr/SWAA2025043055798), Mar 31, 2025: ACCESS PANEL. CRACKED. CRACK AROUND HOLES ACCESS PANEL 561CB TRAILING EDGE AT LT WING 2025-238153<[01] TOOL USED ON STEP 12:ULTRASONIC EQUIPMENT P/N:EPOCH 650; S/N:190984811; DUE DATE
- [SDR SWAA2025043055740](https://openairdocs.org/sdr/SWAA2025043055740), Mar 29, 2025: NUT. DETERIORATED. DETERIORATED ENTRY DOOR ASSIST HANDLE NUT FWD AND LOWER POSITION AT FWD GALLEY AREA (4 EA) 2025-237983<[01] REPLACED ENTRY DOOR ASSIST HANDLE NUT FWD AND LOWER 
- [SDR SWAA2025043055745](https://openairdocs.org/sdr/SWAA2025043055745), Mar 29, 2025: DOUBLER. CORRODED. DOUBLER BTW BS 400 TO BS 420 BETWEEN S-1 AND S-2L REQUIRES REMOVAL AND REPAIR. 2025-237993<[01] TOOL USED ON STEP 3: EDDY CURRENT EQUIPMENT P/N: NORTEC 600D; S/
- [SDR SWAA2025031704784](https://openairdocs.org/sdr/SWAA2025031704784), Mar 13, 2025: BATTERY PACK. FAILED. R/H AFT EMERGENCY LIGHTING BATTERY PACK FAILED THE CAPACITY CHECK. <[01] REMOVED AND REPLACED BATTERY PACK PER M/M 33-51-06.
- [SDR SWAA2025031704783](https://openairdocs.org/sdr/SWAA2025031704783), Mar 13, 2025: 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 SWAA2025020693656](https://openairdocs.org/sdr/SWAA2025020693656), Feb 6, 2025: LIGHT. INOPERATIVE. R1 DOOR OUTER EMERGENCY LIGHT INOP<[01] REPLACED R1 DOOR EMERGENCY EXIT LIGHT IAW AMM 33-51-04.
- [SDR SWAA2024110857259](https://openairdocs.org/sdr/SWAA2024110857259), Nov 6, 2024: PUMP. LEAKING. HYD SYS B QTY WENT TO 0; FOLLOWED BY ENG HYD LOW PRESS LIGHT.<[01] FOUND B ENGINE DRIVEN HYDRAULIC PUMP LEAKING AT PRESSURE FITTING. DUE TO POSSIBILITY DAMAGE F
- [SDR SWAA2024100744537](https://openairdocs.org/sdr/SWAA2024100744537), Oct 2, 2024: LIGHT. MISSING. EMERGENCY EXIT OVERHEAD LIGHT MISSING<[01] RELAMPED PER [AMM 33-18-00-960-801-NG (INDICATOR LIGHT - LAMP REPLACEMENT - PERMANENT)]
- [SDR SWAA2024061300962](https://openairdocs.org/sdr/SWAA2024061300962), Jun 13, 2024: BATTERY PACK. NO TEST. EMX BATTERY PACK M01668 FAILS CAPACITANCE CHECK<[01] 01 - REMOVED AND REPLACED EMX BATTERY PACK M01668 PER [AMM 33-51-06-960-805-NG (POWER SUPPLY - BATTERY PACK
- [SDR SWAA2024061300960](https://openairdocs.org/sdr/SWAA2024061300960), Jun 13, 2024: BATTERY PACK. NO TEST. EMX BATTERY PACK M01669 FAILS CAPACITANCE CHECK<[01] 01 - REMOVED AND REPLACED EMX BATTERY PACK M01669 PER [AMM 33-51-06-960-805-NG (POWER SUPPLY - BATTERY PACK
- [SDR SWAA2024061300966](https://openairdocs.org/sdr/SWAA2024061300966), Jun 13, 2024: SKIN. CRACKED. LEFT WING #2 SLAT LOWER SKIN HAS A CRACK APPROXIMATELY .3 LONG EXTENDING FROM A FASTENER BELOW ACTUATOR ATTACH POINT. REMOVED AND REPLACED #2 SLAT IAW AMM OPS C
- [SDR SWAA2023080786040](https://openairdocs.org/sdr/SWAA2023080786040), Aug 5, 2023: LENS. OBSTRUCTED. R WING ESCAPE LOWER EMER LIGHT LENS PAINTED OVER<[01] REMOVED PAINT FROM LENS PER SIP
- [SDR SWAA2023062167907](https://openairdocs.org/sdr/SWAA2023062167907), Jun 21, 2023: BATTERY PACK. INOPERATIVE. L/H FWD EMERGENCY LIGHTING BATTERY PACK ONLY LAST 45 SECONDS BEFORE LIGHTS GO OUT.<[01] REMOVED AND REPLACED BATTERY PER M/M 33-51-06.
- [SDR SWAA2023050527306](https://openairdocs.org/sdr/SWAA2023050527306), Apr 13, 2023: RIB. CRACKED. CRACK ACCESS PANEL 341B RIB LE STA 105.26 AT RH HORIZONTAL STABILIZER 2023-212862<[01] REPLACED RIB LOCATED STA 105.26 AT RH HORIZONTAL STABILIZER IAW B737-700 
- [SDR SWAA2023050524476](https://openairdocs.org/sdr/SWAA2023050524476), Apr 6, 2023: SUPPORT. CRACKED. CRACK ANGLE - SUPPORT LOCATED BTW BS 727E PLUS 12INCH TO BS 847 LBL 52 AT AFT CARGO COMPARTMENT 2023-212858<[01] REPLACED ANGLE - SUPPORT AND FASTENERS LOCATED 
- [SDR SWAA2023050523372](https://openairdocs.org/sdr/SWAA2023050523372), Apr 3, 2023: ANGLE. CRACKED. CRACK FRONT SPAR ANGLE LOCATED FUEL BOOST PUMP IFSS 120 AT RT WING 2023-212848<[01] REPLACED FRONT SPAR ANGLE LOCATED FUEL BOOST PUMP IFSS 120 AT RT WING IAW B7
- [SDR SWAA2023050522952](https://openairdocs.org/sdr/SWAA2023050522952), Apr 2, 2023: BATTERY PACK. FAULTY. DOES NOT PASS THE OPERATIONAL TEST ON BATTERY PACK LH SIDE LOCATED ON LOWERED CEILING PANEL AFT GALLEY AREA 2023-212845<[01] REPLACED BATTERY PACK LH SIDE LOCAT
- [SDR SWAA2023050522482](https://openairdocs.org/sdr/SWAA2023050522482), Mar 30, 2023: BRACKET. CRACKED. CRACK SUPPORT BRACKET LOCATED BS947.5 AT LEVEL STR26L AT AFT CARGO COMPARTMENT 2023-212795<[01] REPLACED SUPPORT BRACKET LOCATED BS947.5 AT LEVEL STR26L AT AFT 
- [SDR SWAA2023050522488](https://openairdocs.org/sdr/SWAA2023050522488), Mar 30, 2023: FRAME. CRACKED. CRACK FRAME ON BS 907 AND BETWEEN STR25R TO STR26R AFT CARGO COMPARTMENT 2023-212796<[01] REPLACED FRAME ON BS 907 AND BETWEEN STR24R TO STR24L AFT CARGO COMPAR
- [SDR SWAA2023050522481](https://openairdocs.org/sdr/SWAA2023050522481), Mar 30, 2023: SUPPORT. CRACKED. CRACK ANGLE - SUPPORT LOCATED BS907 TO BS927 AND BETWEEN STR25R TO STR27R AFT CARGO COMPARTMENT (2 EA) 2023-212794<[01] REPLACED ANGLE - SUPPORT AND FASTENERS L
- [SDR SWAA2023050522479](https://openairdocs.org/sdr/SWAA2023050522479), Mar 30, 2023: TIE. CRACKED. CRACK TIE CLIP BS 277 STR 10R AT PASSENGER CABIN 2023-212776<[01] REPLACED TIE CLIP BS 277 STR 10R AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-4
- [SDR SWAA2023050522253](https://openairdocs.org/sdr/SWAA2023050522253), Mar 30, 2023: KEELBEAM. BROKEN. BROKEN HANDLE CENTRE TANK SUMP DRAIN (KEEL BEAM) AT LOWER FUSELAGE 2023-212770<[01] REPLACED SUMP DRAIN VALVE(KEEL BEAM) AT LOWER FUSELAGE IAW B737-700 AMM 28-1
- [SDR SWAA2023050522487](https://openairdocs.org/sdr/SWAA2023050522487), Mar 30, 2023: SUPPORT. CORRODED. CORROSION SUPPORT TEE LOCATED BS794 BETWEEN STR25R TO STR26R AND WL157 AT AFT CARGO COMPARTMENT 2023-212787<[01] REPLACED SUPPORT TEE LOCATED BS794 BETWEEN STR2
- [SDR SWAA2023050521717](https://openairdocs.org/sdr/SWAA2023050521717), Mar 28, 2023: STRINGER. CRACKED. CRACK STRINGER 23R AT BS540 FWD CARGO COMPARTMENT 2023-212749<[01] UT EQUIPMENT P/N: 45MG; S/N: 221859911; DUE DATE: 07-NOV-23;[02] TOOLS USED: TEMPERATURE CONT

All 208: https://openairdocs.org/aircraft/N7828A/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 N7828A

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N7828A before.

- [Cancelled 1957-01-08](https://openairdocs.org/deregistered/N7828A-1957-01-08): Cessna 180A, S/N 32725. 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

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