# N7875A: 2004 Boeing 737-7Q8

- Status: Valid registration
- Airframe: [Boeing 737-7Q8](https://openairdocs.org/model/boeing-737-7q8) (registry code 1384418, 149 seats)
- Engine: [CFM International CFM56-7B24 series](https://openairdocs.org/engine/cfm-international-cfm56-7b24-series) (registry code 13044)
- Serial number: 29354
- Year built: 2004
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: June 23, 2016
- Certificate issued: December 22, 2022
- Expires: December 31, 2029
- Mode S code: AAAD8F
- 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=7875A
- Page: https://openairdocs.org/aircraft/N7875A

From the FAA registry file of October 29, 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 737-7Q8)

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 N7875A.

## FAA accident and incident reports

None matched to N7875A.

## Service difficulty reports (245, 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 SWAA2026072131862](https://openairdocs.org/sdr/SWAA2026072131862), Jul 17, 2026: COVER. DAMAGED. ILLUMINATED LOWER EXIT SIGN AT R/H OVERWING EXIT HAS DAMAGED VERBIAGE. REPLACED LOWER EXIT SIGN COVER AT R/H OVERWING EXIT REF. AMM 33-51-01.
- [SDR SWAA2026060107574](https://openairdocs.org/sdr/SWAA2026060107574), May 29, 2026: SENSOR. FAULTY. TAKE OFF CONFIG WARNING ON TAKE OFF. FLAPS INDICATION SPLIT RIGHT 1/2 DEGREE HIGHER THEN LEFT. FOUND FC 27-53255 FLAP 6 SKEW. REPLACED 6 FLAP SKEW SENSOR IAW AM
- [SDR SWAA2026060196871](https://openairdocs.org/sdr/SWAA2026060196871), May 8, 2026: ANGLE. CRACKED. CRACK ANGLE LOCATED IRSS 139 TRAILING EDGE AT RT WING. REPLACED ANGLE LOCATED IRSS 139 TRAILING EDGE AT RT WING IAW SRM 51-10-02-0G-0 PARAGRAPH 9; SRM 51-40-02-
- [SDR SWAA2026060196874](https://openairdocs.org/sdr/SWAA2026060196874), May 8, 2026: SUPPORT BEAM. CRACKED. CRACKED SUPPORT BEAM ORSS 297 TRAILING EDGE AT LT WING. REPLACED SUPPORT BEAM LOCATED BTW ORSS 277 TO ORRS 328 APROX. TRAILING EDGE AT LT WING IAW SRM 51-10-02;
- [SDR SWAA2026060196872](https://openairdocs.org/sdr/SWAA2026060196872), May 8, 2026: PLATE. DAMAGED. ELONGATED HOLE ON CORRUGATED PLATE LOCATED ORSS 261 TRAILING EDGE AT RT WING. REPLACED CORRUGATED PLATE AND FASTENERS LOCATED ORSS 261 TRAILING EDGE AT RT WING 
- [SDR SWAA2026060196873](https://openairdocs.org/sdr/SWAA2026060196873), May 8, 2026: PLATE. DAMAGED. ELONGATED HOLE ON CORRUGATED PLATE LOCATED ORSS 261 TRAILING EDGE AT LT WING. REPLACED CORRUGATED PLATE LOCATED ORSS 261 TRAILING EDGE AT LT WING IAW SRM 51-10-
- [SDR SWAA2026060196179](https://openairdocs.org/sdr/SWAA2026060196179), May 6, 2026: STRAP. CORRODED. CORROSION ON STRAP LOCATED BETWEEN STA794.3 TO STA807 AND RBL18 WL156 AT AFT CARGO COMPARTMENT. REPLACED STRAP LOCATED BETWEEN STA794.3 TO STA807 AND RBL18 WL15
- [SDR SWAA2026060196180](https://openairdocs.org/sdr/SWAA2026060196180), May 6, 2026: SUPPORT BRACKET. CRACKED. CRACKED SUPPORT BRACKET BS 867, S3R. REPLACED BRACKET SUPPORT LOCATED BS867 AT LEVEL STR 3R AT PASSENGER CABIN IAW SRM 51-10-02-0G-0 PARAGRAPH 9; SRM 51-40-02-0
- [SDR SWAA2026060195684](https://openairdocs.org/sdr/SWAA2026060195684), May 5, 2026: FLOOR PANEL. DELAMINATED. DELAMINATED FLOOR PANEL 242AF AT PASSENGER CABIN. REPAIRED FLOOR PANEL 242AF AT PASSENGER CABIN IAW SRM 53-00-50-2R-7 REPAIR 7 AND SRM 53-00-50-2R-0 REPAIR GENE
- [SDR SWAA2026060195686](https://openairdocs.org/sdr/SWAA2026060195686), May 5, 2026: FLOOR PANEL. DELAMINATED. DELAMINATED FLOOR PANEL 231XF AT PASSENGER CABIN. REPAIRED FLOOR PANEL 231XF AT PASSENGER CABIN IAW SRM 53-00-50-2R-7 REPAIR 7 AND SRM 53-00-50-2R-0 REPAIR GENE
- [SDR SWAA2026060195805](https://openairdocs.org/sdr/SWAA2026060195805), May 5, 2026: WINDOW POST. CRACKED. CRACK WINDOW 1 POST INTERNAL AREA AFT UPPER CORNER POSITION RH SIDE. PERFORMED REPAIR ON UPPER CORNER WINDOW R1 AT COCKPIT AREA IAW EA 26-153-01227 THRU WIP1 TO
- [SDR SWAA2026060195177](https://openairdocs.org/sdr/SWAA2026060195177), May 4, 2026: PRESSURE BLKHD. CRACKED. CRACK INDICATION ON HORIZONTAL PRESSURE DECK WEB RBL 40 STA 663 AT PASSENGER CABIN. PERFORMED REPAIR ON HORIZONTAL PRESSURE DECK WEB LOCATED BTW RBL 30 TO RBL 6
- [SDR SWAA2026060195306](https://openairdocs.org/sdr/SWAA2026060195306), May 4, 2026: SEAT TRACK. CORRODED. CORROSION ON SEAT TRACK LOCATED BTW BS 500B BS500C WL208 AND LBL 45.50 AT PASSENGER CABIN. REWORKED AND EVALUATED AREA ON SEAT TRACK LOCATED BTW BS 500B TO BS 5
- [SDR SWAA2025100822131](https://openairdocs.org/sdr/SWAA2025100822131), Oct 7, 2025: LIGHT. INOPERATIVE. MULTIPLE EMERGENCY LIGHTS INOP THROUGHOUT THE CABIN. REMOVED AND REPLACED IAW AMM 33-51-03-960-801.
- [SDR SWAA2025060577660](https://openairdocs.org/sdr/SWAA2025060577660), Jun 2, 2025: GIRT BAR. OUT OF ADJUST. RH FWD SERVICE DOOR AFT GIRT BAR HOOK IS LOOSE RH FWD SVC DOOR <[01]. C/W EA M-23-125-01839 TEMP REPAIR.
- [SDR SWAA2025012890255](https://openairdocs.org/sdr/SWAA2025012890255), Jan 28, 2025: LENS. WRONG PART. R1 DOOR LOWER EXIT SIGN MISSING DIRECTIONAL ARROW.<[01] 01 - REMOVED AND REPLACED PER [AMM 33-51-01-201-NG (EXIT SIGNS - MAINTENANCE PRACTICES - PERMANENT)]
- [SDR SWAA2024082128481](https://openairdocs.org/sdr/SWAA2024082128481), Aug 21, 2024: SIGN. INOPERATIVE. AFT GALLEY EMER EXIT SIGN W0152 INOP<[01] FOUND ONLY EXIT SIGN W0152 TO BE INOP. REMOVED AND REPLACED AFT GALLEY EXIT SIGHT PER AMM 33-51-01. DID NOT FIX. REMOV
- [SDR SWAA2024082128709](https://openairdocs.org/sdr/SWAA2024082128709), Aug 21, 2024: BATTERY PACK. INOPERATIVE. AFT GALLEY EMER EXIT SIGN W0152 INOP<[01] FOUND ONLY EXIT SIGN W0152 TO BE INOP. REMOVED AND REPLACED AFT GALLEY EXIT SIGHT PER AMM 33-51-01. DID NOT FIX. REMOV
- [SDR SWAA2024082128711](https://openairdocs.org/sdr/SWAA2024082128711), Aug 21, 2024: CHARGER. INOPERATIVE. AFT GALLEY EMER EXIT SIGN W0152 INOP<[01] FOUND ONLY EXIT SIGN W0152 TO BE INOP. REMOVED AND REPLACED AFT GALLEY EXIT SIGHT PER AMM 33-51-01. DID NOT FIX. REMOV
- [SDR SWAA2024070906947](https://openairdocs.org/sdr/SWAA2024070906947), Jun 29, 2024: LIGHT. INOPERATIVE. R2 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE.<[01] RELAMPED R2 DOOR EXTERIOR EMERGENCY LIGHT AS PER REF AMM 33-51-04-960-801. OPERATIONAL TEST PASSED;[02] VERIF
- [SDR SWAA2024070906946](https://openairdocs.org/sdr/SWAA2024070906946), Jun 29, 2024: LIGHT. INOPERATIVE. EMERGENCY OVERHEAD BIN LIGHT AT SEAT ROW 6L/H INOPERATIVE.<[01] RELAMPED EMERGENCY OVERHEAD BIN LIGHT AT SEAT ROW 6L/H AS PER REF AMM 33-51-03-960-801. OPERATIO
- [SDR SWAA2024070906467](https://openairdocs.org/sdr/SWAA2024070906467), Jun 27, 2024: BATTERY PACK. INOPERATIVE. MULTIPLE PAX EMERGENCY LIGHTS INOP<[01] REMOVED AND REPLACED EMERGENCY BATTERY PACKS AT POSITIONS M1672 AND M1674 AS PER REF B737 AMM 33-51-06-960-805. OPERATIO
- [SDR SWAA2024070902654](https://openairdocs.org/sdr/SWAA2024070902654), Jun 17, 2024: FLOOR PANEL. DETERIORATED. FOUND PANEL 231UF DETERIORATED. FOUND MAIN CABIN FLOOR PANEL 231UF DETERIORATED.<[01] REPLACED MAIN CABIN FLOOR PANEL 231UF REF. B737-700 AMM 53-21-00-400-801. 
- [SDR SWAA2024070903520](https://openairdocs.org/sdr/SWAA2024070903520), Jun 14, 2024: CONNECTOR. DEFECTIVE. AFT CARGO CONNECTOR D11082 M/W L00547 FOUND DEFECTIVE AT STA 747<[01] REMOVED AND REPLACED AFT CARGO CONNECTOR D11082 M/W L00547 AS PER REF B737 SWPM 20-61-28 A
- [SDR SWAA2024070901753](https://openairdocs.org/sdr/SWAA2024070901753), Jun 14, 2024: FLOORBEAM. CRACKED. MAIN CABIN FLOOR STRUCTURE PANEL BREAK ASSY STA 540 BL 0 TO LBL 25 FOUND CRACKED<[01] REMOVED AND REPLACED MAIN CABIN FLOOR SUPPORT BREAK PANEL ASSY. AT STA 540
- [SDR SWAA2024070997589](https://openairdocs.org/sdr/SWAA2024070997589), Jun 2, 2024: SUPPORT FITTING. DAMAGED. L/W REAR SPAR FIXED T/E LOWER PANEL 551GB I/B AFT SUPPORT ROD UPPER SUPPORT FITTING HAS ELONGATED HOLE MKD DOT<[01] REMOVED AND REPLACED L/W REAR SPAR FIXED T/E
- [SDR SWAA2024070997588](https://openairdocs.org/sdr/SWAA2024070997588), Jun 2, 2024: FITTING. CRACKED. L/W REARE SPAR FIXED T/E DEFLECTION CONTROL RIB PANEL LOWER VERTICAL BULB SEAL FITTING CRACKED MKD DOT<[01] REMOVED AND REPLACED BULB SEAL FITTING AT L/W REAR S
- [SDR SWAA2024070991681](https://openairdocs.org/sdr/SWAA2024070991681), May 30, 2024: ATTACH FITTING. CORRODED. FLIGHT COMPARTMENT LH ESCAPE ROPE WORN SPOTS AND ATTACH FITTING WITH CORROSION.<[01] REMOVED AND REPLACED LH ESCAPE ROPE AS REF. B737-700 AMM 25-61-10-000-801 A
- [SDR SWAA2024070991682](https://openairdocs.org/sdr/SWAA2024070991682), May 30, 2024: ESCAPE ROPE. WORN. FLIGHT COMPARTMENT RH ESCAPE ROPE WORN SPOTS AND ATTACH FITTING WITH CORROSION.<[01] REMOVED AND REPLACED RH ESCAPE ROPE AS REF. B737-700 AMM 25-61-10-000-801 A
- [SDR SWAA2024070991297](https://openairdocs.org/sdr/SWAA2024070991297), May 29, 2024: FLOOR PANEL. CORRODED. AFT CARGO COMPARTMENT;CAP STRIP FLOOR PANEL 140DF HAS CORROSION.<[01] RECIEVED NEW AFT CARGO COMP CAP STRIP FLOOR PANEL 140DF P/N 453A2611-5 INSTALLATION WILL B
- [SDR SWAA2024070990626](https://openairdocs.org/sdr/SWAA2024070990626), May 28, 2024: FLOOR PANEL. DELAMINATED. MAIN CABIN FLOOR PANEL # 232SF COMPOSITE MATERIAL DELAMINATION AT AFT INB CORNER.<[01] REPAIRED DAMAGE AREA AS MARKED ON MAIN CABIN FLOOR PANEL #232SF AS PER B7
- [SDR SWAA2024070990625](https://openairdocs.org/sdr/SWAA2024070990625), May 28, 2024: FLOOR PANEL. PEELING. MAIN CABIN FLOOR PANEL # 231XF COMPOSITE MATERIAL PEELING OFF.<[01] RECEIVED NEW CABIN FLOOR PANEL #231XF P/N 144A5810-126; REFERENCE AAR TAG # PD232; PO# 20597
- [SDR SWAA2024070990624](https://openairdocs.org/sdr/SWAA2024070990624), May 28, 2024: FLOOR PANEL. DELAMINATED. MAIN CABIN FLOOR PANEL # 241BF COMPOSITE MATERIAL DELAMINATION AT FWD INB CORNER.<[01] RECEIVED NEW CABIN FLOOR PANEL #241BF P/N 144A5810-189; REFERENCE AAR TAG
- [SDR SWAA2024070990617](https://openairdocs.org/sdr/SWAA2024070990617), May 28, 2024: FLOOR PANEL. PEELING. MAIN CABIN FLOOR PANEL # 241FF COMPOSITE MATERIAL PEELING OFF.<[01] RECEIVED NEW CABIN FLOOR PANEL #241FF P/N 144A5810-131; REFERENCE AAR TAG # HA1091; PO# 2059
- [SDR SWAA2024070989994](https://openairdocs.org/sdr/SWAA2024070989994), May 25, 2024: PANEL. CRACKED. AFT ENTRY DOOR (L-2) PANEL 834DZ IS CRACKED AND BENT ALL AROUND. (DOT #28-1)<[01] REPLACED AFT ENTRY DOOR (L-2) PANEL 834DZ PER SRM 51-40-02-0G-0;[02] CORRECTIO
- [SDR SWAA2024070989655](https://openairdocs.org/sdr/SWAA2024070989655), May 24, 2024: SEAT TRACK. CORRODED. CABIN SEAT TRACK CROWN BOTTOM AREA HAS CORROSION SPOTS BETWEEN STA 360+11' TO 380 LBL 45.50 MKD (107-023)<[01] REMOVED AND REPLACED CABIN SEAT TRACK FROM STA 36
- [SDR SWAA2024070989645](https://openairdocs.org/sdr/SWAA2024070989645), May 24, 2024: SEAT TRACK. CHAFED. MAIN CABIN SEAT TRACK CROWN UPPER AREA HAS A CHAFE MARK AT STA 520 LBL 24.75 MKD (107-016) MAIN CABIN SEAT TRACK CROWN UPPER AREA HAS A CHAFE MARKS AND GOUGE AT
- [SDR SWAA2024070989648](https://openairdocs.org/sdr/SWAA2024070989648), May 24, 2024: SEAT TRACK. CHAFED. MAIN CABIN SEAT TRACK CROWN UPPER AREA HAS A CHAFE MARK AT STA 520 LBL 45.50 MKD (107-017)<[01] EVALUATED DAMAGE REMOVAL AT SEAT TRACK CROWN UPPER SURFACE; MATE
- [SDR SWAA2024070989552](https://openairdocs.org/sdr/SWAA2024070989552), May 24, 2024: DOUBLER. CRACKED. EXTERNAL POWER RECEPTACLE ACCESS DOOR CUTOUT SKIN DOUBLER HAS A CRACK AT LOWER SIDE (AT FASTENER)<[01] REMOVED AND DISCARDED DAMAGED EGPR DOUBLER; LOCATED; DRIL
- [SDR SWAA2024070989649](https://openairdocs.org/sdr/SWAA2024070989649), May 24, 2024: SEAT TRACK. CORRODED. CABIN SEAT TRACK CROWN BOTTOM AREA HAS CORROSION SPOTS BETWEEN STA 360+11' TO 380 LBL 24.75 MKD (107-024)<[01] REMOVED AND REPLACED SEAT TRACK FROM STA 360+ 10 
- [SDR SWAA2024070989135](https://openairdocs.org/sdr/SWAA2024070989135), May 23, 2024: SCUFF PLATE. DETERIORATED. ANTI-SKID TAPE AT MAIN ENTRY AND SERVICE DOORS L-1; L-2; R-1 AND R-2 SCUFF PLATES DETERIORATED<[01] INSTALLED ANTI-SKID TAPE AT MAIN ENTRY AND SERVICE DOORS L-1
- [SDR SWAA2023090697211](https://openairdocs.org/sdr/SWAA2023090697211), Sep 6, 2023: LIGHT. OUT OF ADJUST. ROW 1DEF CENTER ISLE PHOTOLUMINESCENT STRIP HAS MOISTURE IN IT AND LOOSE.<[01] REMOVED AND REPLACED 1DEF PHOTOLUMINESCENT STRIIP IAW AMM 33-51-15.
- [SDR SWAA2023042630505](https://openairdocs.org/sdr/SWAA2023042630505), Apr 23, 2023: LIGHT. INOPERATIVE. EMERGENCY EXIT LIGHT ON RIGHT HAND OVERWING EXIT INOP<[01] RE-LAMPED EMERGENCY EXIT INFORMATION LIGHT ON RIGHT HAND OVERWING EXIT IN REF TO AMM 33-25-00. OPS TE
- [SDR SWAA2022091952989](https://openairdocs.org/sdr/SWAA2022091952989), Sep 14, 2022: NONE. FAULTY. ON APPROACH FLAP HANDLE PLACED TO 1. LEFT TRAILING EDGE FLAP INDICATOR SHOWED LESS THAN 1. RT TRAILING EDGE FLAP INDICATOR SHOWED 0. NO LEADING EDGE FLAP MOVEME
- [SDR SWAA2022081040438](https://openairdocs.org/sdr/SWAA2022081040438), Aug 10, 2022: HOOK. BROKEN. AFT ENTRY DOOR GIRT BAR PLASTIC CLIP BROKEN / [01] REMOVED AND REPLACED GIRT BAR STOP RING PER AMM 25-66-01.
- [SDR SWAA2022060814418](https://openairdocs.org/sdr/SWAA2022060814418), Jun 2, 2022: BATTERY PACK. INOPERATIVE. EMERGENCY LIGHTS COMMON TO BATTERY PACK M1668 ARE INOP. / [01] REPLACED; AND PERFORMED GOOD TEST OF BATTERY PACK M1668 PER AMM 33-51-06-960-805.;[02] VERIFIED A
- [SDR SWAA2022060814417](https://openairdocs.org/sdr/SWAA2022060814417), Jun 2, 2022: LIGHT. INOPERATIVE. AFT ENTRY DOOR SLIDE LIGHT INOP. / [01] REPLACED LAMP AND PERFORMED GOOD TEST OF AFT ENTRY DOOR SLIDE LIGHT PER AMM 33-51-04-960-801.;[02] VERIFIED CORRECTIVE A
- [SDR SWAA2022060813419](https://openairdocs.org/sdr/SWAA2022060813419), May 30, 2022: LIGHT. INOPERATIVE. EMERGENCY EXIT LIGHTS COME ON WHEN POWER IS OFF AND SWITCH IS ALSO OFF / [01] WHILE TROUBLESHOOTING DISCOVERED W4142-0032-22 WAS BROKEN CAUSING THE EMERG. EXIT 
- [SDR SWAA2022060808279](https://openairdocs.org/sdr/SWAA2022060808279), May 17, 2022: INTERCOSTAL. CRACKED. CRACK ON INTERCOSTAL AT AFT CARGO BAY BS 927-BS 947 RBL 21 / [01] DAMAGE FOUND ON AFT CARGO BAY INTERCOSTAL BS 927- BS947 RBL 21 FOUND TO BE OUT OF LIMIT PART W
- [SDR SWAA2022060807253](https://openairdocs.org/sdr/SWAA2022060807253), May 12, 2022: ANGLE. CRACKED. CRACK IN VERTICAL L ANGLE BS 692 RBL 0.5 WL 206.5. VERIFIED THE APPLICABILITY OF SRM 51-10-02-0G-0; REMOVED THE CRACKED VERTICAL L ANGLE BS 692 RBL 0.5 WL 206.5

All 245: https://openairdocs.org/aircraft/N7875A/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

## Related

- Other Boeing 737-7Q8 aircraft: https://openairdocs.org/model/boeing-737-7q8/aircraft.md
- The CFM International CFM56-7B24 series engine: https://openairdocs.org/engine/cfm-international-cfm56-7b24-series.md

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