# N7879A: 2005 Boeing 737-7K9

- Status: Valid registration
- Airframe: [Boeing 737-7K9](https://openairdocs.org/model/boeing-737-7k9) (registry code 138447E, 149 seats)
- Engine: [CFM International CFM56-7B24 series](https://openairdocs.org/engine/cfm-international-cfm56-7b24-series) (registry code 13044)
- Serial number: 34321
- Year built: 2005
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: November 2, 2016
- Certificate issued: December 6, 2019
- Expires: December 31, 2029
- Mode S code: AAAE1B
- 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=7879A
- Page: https://openairdocs.org/aircraft/N7879A

From the FAA registry file of October 27, 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 737-7K9)

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 N7879A.

## FAA accident and incident reports

None matched to N7879A.

## Service difficulty reports (167, 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 SWAA2026092102356](https://openairdocs.org/sdr/SWAA2026092102356), Sep 17, 2026: BRACKET. DETACHED. LOWER FUSELAGE PANEL 192E TWO FWD MOUNT BRACKETS DETACHED. R & R THE TWO BRACKETS IAW SRM 51-40-02-0G-0-A00729.
- [SDR SWAA2026092128718](https://openairdocs.org/sdr/SWAA2026092128718), Sep 17, 2026: BATTERY PACK. NO TEST. AFT RIGHT EMERGENCY LIGHT SYS BATTERY PACK FAILED A CAPACITY CHECK. REMOVED AND REPLACED THE BATTERY PACK IAW MM 33-51-06.
- [SDR SWAA2026090104673](https://openairdocs.org/sdr/SWAA2026090104673), Aug 27, 2026: BATTERY PACK. INOPERATIVE. EMERGENCY LIGHT BATTERY PACK M1675 INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK M1675 IAW B737 AMM 33-51-06. OPS CHECK GOOD.
- [SDR SWAA2026090257626](https://openairdocs.org/sdr/SWAA2026090257626), Aug 8, 2026: SCUFF PLATE. CRACKED. FWD CARGO, FWD CORNER SCUFF PLATE CRACKED. REMOVED AND REINSTALL THE SCUFF PLATE IAW AMM 53-11-02-401.
- [SDR SWAA2026090184679](https://openairdocs.org/sdr/SWAA2026090184679), Aug 8, 2026: PANEL. DAMAGED. MULTIPLE ELONGATED HOLES ON RH WING PANEL 651GB (MARKED) REPAIRED MULTIPLE ELONGATED HOLES ON RH WING PANEL 651GB IAW B737 SRM 51-70-04-2R-9 VERIFIED REPAIRED M
- [SDR SWAA2026090232651](https://openairdocs.org/sdr/SWAA2026090232651), Aug 7, 2026: COWLING. DAMAGED. ELONGATED FASTENER HOLES ON NR 2 ENGINE INLET COWL LOWER ANTI-ICE OVERBOARD EXHAUST PANEL REF 26-171-01809-TLD [TTG8Q01D1YSU]. LOCATED AND DRILLED NEW PANEL ENG
- [SDR SWAA2026082141542](https://openairdocs.org/sdr/SWAA2026082141542), Jul 24, 2026: CONTROL MODULE. FAULTED. NR 2 ENGINE OVERHEAT LIGHT ILLUMINATED AFTER START. PERFOMED BITE TEST OF ENGINE FIRE DETECTION CONTROL MODULE REF FIM 26-10 TASK 801. NO FAULTS PRESENT. PER FI
- [SDR SWAA2026051196925](https://openairdocs.org/sdr/SWAA2026051196925), May 9, 2026: SCUFF PLATE. CRACKED. FWD SERVICE DOOR SCUFF PLATE AFT CORNER HAS A 2.5 CRACK. FWD SERVICE DOOR SCUFF PLATE AFT CORNER HAS A 2.5 CRACK. R&R SCUFF PLATE IAW AMM 53-11-01.;[02] R&R SCU
- [SDR SWAA2026042993910](https://openairdocs.org/sdr/SWAA2026042993910), Apr 28, 2026: SLIDE. OUT OF POSITION. AFT L2 DOOR SLIDE GIRT BAR CURTAIN IS HANGING TO LOW. R & R SLIDE IAW MT 725-61_06.
- [SDR SWAA2026012262812](https://openairdocs.org/sdr/SWAA2026012262812), Jan 19, 2026: LUBRICATION UNIT. FAULTED. NR 1 IDG ON MEL. APU AUTO SHUTDOWN IN FLIGHT. REMOVED AND REPLACED LUBE MODULE IAW AMM 49-91-11.
- [SDR SWAA2025122253583](https://openairdocs.org/sdr/SWAA2025122253583), Dec 18, 2025: BRACKET. CRACKED. RIGHT ENGINES O/B AFT STRUT FIRE SEAL BRACKET IS CRACKED. PICTURE ADDED.<[01] 01 - REMOVED AND REPLACED PER [SRM 51-40-02-0G-0-A00729 (GENERAL - FASTENER INSTAL
- [SDR SWAA2025051268362](https://openairdocs.org/sdr/SWAA2025051268362), May 7, 2025: LIGHT. BURNED. SPARKS; ARCHING AND BURNING SMELL EMITED /OBSERVED AT CAPTAINS GRIMES LIGHT; PULLED P6-3-9 C/B TO ISOLATE POWER COMPLIED WITH CONDITIONAL INSPECTION PER AMM 05-
- [SDR SWAA2025010884146](https://openairdocs.org/sdr/SWAA2025010884146), Jan 8, 2025: MEGAPHONE. INOPERATIVE. FDW MEGAPHONE INOP<[01] R&R FWD MEGAPHONE PER AMM 25-64-01
- [SDR SWAA2024110555406](https://openairdocs.org/sdr/SWAA2024110555406), Oct 31, 2024: TAPE. MISSING. FWD CARGO COMPARTMENT AFT BULKHEAD UPPER CHORD WITH MISSING CARGO TAPE. 2024-597257<[01] INSTALLED ON FWD CARGO COMPARTMENT AFT BULKHEAD UPPER CHORD IAW AMM 25-
- [SDR SWAA2024103147341](https://openairdocs.org/sdr/SWAA2024103147341), Oct 11, 2024: WEB. CRACKED. REJECT: CRACKED NEW WEB AND ELONGATED HOLES ON BRACKETS; BILGE AREA BTW BS500 TO BS500A AT LEVEL STR 26L FWD CARGO COMPARTMENT. 2024 - 597224 REJECT: CRACKED NE
- [SDR SWAA2024110543315](https://openairdocs.org/sdr/SWAA2024110543315), Sep 28, 2024: TIE CLIP. CRACKED. CRACK TIE CLIP LOCATED 277 AND S-10R AT PASSENGER CABIN 2024-597164<[01] REPLACED TIE CLIP LOCATED 277 AND S-10R AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 AN
- [SDR SWAA2024110543030](https://openairdocs.org/sdr/SWAA2024110543030), Sep 28, 2024: ANGLE. CRACKED. CRACK ANGLE TRAILING EDGE LOCATED ORSS 271 LT WING 2024-597163<[01] REPLACED ANGLE ON TRAILING EDGE LOCATED ORSS 271 LT WING IAW B737-700 SRM 51-40-02-0G-0 AND 
- [SDR SWAA2024110542674](https://openairdocs.org/sdr/SWAA2024110542674), Sep 26, 2024: ANGLE. CRACKED. CRACK ANGLE LOCATED BS 867 BETWEEN S-2R TO S-3R AT PASSENGER CABIN 2024-597135<[01] REPLACED ANGLE LOCATED BS 867 BETWEEN S-2R TO S-3R AT PASSENGER CABIN IAW B7
- [SDR SWAA2024110541817](https://openairdocs.org/sdr/SWAA2024110541817), Sep 25, 2024: SUPPORT ANGLE. CRACKED. CRACK ANGLE - SUPPORT LOCATED BS 867 AND S-26L AFT CARGO COMPARTMENT 2024-597107<[01] MEASURE OF CRACK: 1.080 INCHES TOOL USED DIGITAL CALIPER P/N:500-197-30 S/
- [SDR SWAA2024110541820](https://openairdocs.org/sdr/SWAA2024110541820), Sep 25, 2024: SUPPORT ANGLE. CRACKED. CRACK ANGLE - SUPPORT LOCATED BS947.5 AND S-26L AFT CARGO COMPARTMENT 2024-597108<[01] REPLACED ANGLE SUPPORT LOCATED ON BS947.5 AND S-26L AFT CARGO COMPARTMENT
- [SDR SWAA2024103141625](https://openairdocs.org/sdr/SWAA2024103141625), Sep 24, 2024: HOOK. CORRODED. CORROSION EMERGENCY DOOR 833 HOOK ASSEMBLY LIFE LINE AT PASSENGER CABIN 2024-597100<[01] REPLACED EMERGENCY DOOR 833 HOOK ASSEMBLY LIFE LINE AT PASSENGER CABIN 
- [SDR SWAA2024103141626](https://openairdocs.org/sdr/SWAA2024103141626), Sep 24, 2024: WEB. CRACKED. CRACK BILGE AREA WEB BTW BS 500 TO BS 500A AT LEVEL STR 26L AT FWD CARGO COMPARTMENT 2024-597103<[01] REPLACED WEB LOC. ON BILGE AREA BTW BS 500 TO BS 500A AT L
- [SDR SWAA2024110541094](https://openairdocs.org/sdr/SWAA2024110541094), Sep 23, 2024: SCUFF PLATE. CRACKED. CRACK AFT CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT 2024-596989<[01] TOOL USED DIGITAL CALIPER P/N:500-196-30; S/N:A23046084; DUE DATE 23-MAY-25.;[02] TOOL US
- [SDR SWAA2024110541096](https://openairdocs.org/sdr/SWAA2024110541096), Sep 23, 2024: FRAME. CRACKED. CRACK FRAME WEB LOCATED BS259.5 AND BTW STR8R TO STR9R AT PASSENGER CABIN 2024-597028<[01] EQUIPMENT P/N PHASEC 3D; S/N 587435/07; DUE DATE 20-MAR-25 WAS USED O
- [SDR SWAA2024110540776](https://openairdocs.org/sdr/SWAA2024110540776), Sep 23, 2024: STIFFENER. CRACKED. CRACK STIFFENER FLOOR STRUCTURE LOCATED BS540 BETWEEN BL0 TO RBL 24.75 CENTER SECTION 2024-596932<[01] REPLACED STIFFENER LOC. ON FLOOR STRUCTURE BS540 BETWEEN 
- [SDR SWAA2024110540775](https://openairdocs.org/sdr/SWAA2024110540775), Sep 23, 2024: STIFFENER. CRACKED. CRACK STIFFENER FLOOR STRUCTURE LOCATED BS 540 BETWEEN BL 0 TO LBL 24.75 CENTER SECTION 2024-596933<[01] REPLACED STIFFENER LOC. ON FLOOR STRUCTURE BS 540 BETWE
- [SDR SWAA2024110540412](https://openairdocs.org/sdr/SWAA2024110540412), Sep 22, 2024: INTERCOSTAL. DAMAGED. ELONGATED HOLE WEB - INTERCOSTAL LOCATED BS 500D TO BS 500C AND S-26R AT FWD CARGO COMPARTMENT 2024-596806<[01] REPLACED WEB-INTERCOSTAL LOCATED BS 500D TO BS 5
- [SDR SWAA2024110540280](https://openairdocs.org/sdr/SWAA2024110540280), Sep 22, 2024: SCUFF PLATE. CRACKED. CRACK FWD CORNER SCUFF PLATE LOCATED ON FWD CARGO COMPARTMENT CUT OUT 2024-596803<[01] TOOL USED DIGITAL CALIPER P/N:500-196-30; S/N:A23046084; DUE DATE 23-MAY-
- [SDR SWAA2024110540409](https://openairdocs.org/sdr/SWAA2024110540409), Sep 22, 2024: GUSSET. CRACKED. CRACK GUSSET LOCATED BS 500D AND S-19R FWD CARGO COMPARTMENT 2024-596804<[01] REPLACED GUSSET ANGLE LOCATED BS 500D AND S-19R FWD CARGO COMPARTMENT IAW B737-700
- [SDR SWAA2024110540411](https://openairdocs.org/sdr/SWAA2024110540411), Sep 22, 2024: GUSSET. CRACKED. CRACK GUSSET LOCATED BS500D AND S-19L FWD CARGO COMPARTMENT 2024-596805<[01] REPLACED GUSSET ANGLE LOCATED BS 500D AND S-19L FWD CARGO COMPARTMENT IAW B737-700 
- [SDR SWAA2024103139801](https://openairdocs.org/sdr/SWAA2024103139801), Sep 20, 2024: FLOOR PANEL. CRACKED. CRACK FLOOR PANEL 140CF AT AFT CARGO COMPARTMENT 2024-596735<[01] FABRICATED FLOOR PANEL 140CF LOC. AT AFT CARGO COMPARTMENT MATERIAL USED ALUMINUM SHEET P/N: 2
- [SDR SWAA2024090433269](https://openairdocs.org/sdr/SWAA2024090433269), Sep 2, 2024: SLIDE. LOOSE. AFT ENTRY DOOR EMERGENCY SLIDE LOOSE IN BUSTLE<[01] SECURED SLIDE C/W T/C 725-61-06.
- [SDR SWAA2024081425545](https://openairdocs.org/sdr/SWAA2024081425545), Aug 13, 2024: SEAT. MISCONFIGURED. EXIT ROW SEAT 11B RECLINES<[01] ADJUSTED SET 11B IAW CMM 25-21-45
- [SDR SWAA2024051484189](https://openairdocs.org/sdr/SWAA2024051484189), May 10, 2024: ISOLATOR. CRACKED. AFT ENTRY DOOR DUST SEAL BRACKET AFT ISOLATOR CRACKED<[01] R&R AFT ENTRY DOOR DUST SEAL BRACKET AFT ISOLATOR IAW SRM 51-40-02.
- [SDR SWAA2024030558909](https://openairdocs.org/sdr/SWAA2024030558909), Mar 4, 2024: MEGAPHONE. INOPERATIVE. FWD F/A MEGAPHONE INOP<[01] R AND R MEGAPHONE PER AMM 25-64-00.
- [SDR SWAA2024020246911](https://openairdocs.org/sdr/SWAA2024020246911), Jan 31, 2024: GIRT BAR. UNPACKED. L1 DOOR ESCAPE SLIDE GIRT REQUIRES REPACK.<[01] REPACKED L1 DOOR ESCAPE SLIDE GRIT PER AMM 25-66-01
- [SDR SWAA2024020246912](https://openairdocs.org/sdr/SWAA2024020246912), Jan 31, 2024: SLIDE. UNPACKED. R1 DOOR ESCAPE SLIDE GIRT REQUIRES REPACK.<[01] REPACKED R1 DOOR ESCAPE SLIDE GRIT PER AMM 25E-66-01
- [SDR SWAA2023113025250](https://openairdocs.org/sdr/SWAA2023113025250), Nov 27, 2023: ROPE. OUT OF ADJUST. CA EMERGENCY ESCAPE ROPE DOOR WILL NOT OPEN.<[01] REPOSITIONED ESCAPE ROPE AWAY FROM COMPARTMENT DOOR LATCH; OPS CK GOOD PER AMM 25-61-10.
- [SDR SWAA2023111620932](https://openairdocs.org/sdr/SWAA2023111620932), Nov 13, 2023: GIRT BAR. OUT OF ADJUST. FORWARD SERVICE GIRT BAR BRACKET BROKEN ALLOWING BRACKET TO MOVE BACK AND FORTH.<[01] REPLACED FASTENER ON FWD SERVICE DOOR SLIDE GIRT BAR BRACKET PER SRM 51-40
- [SDR SWAA2023110718561](https://openairdocs.org/sdr/SWAA2023110718561), Nov 4, 2023: BRACKET. BROKEN. FORWARD SERVICE GIRT BAR BRACKET BROKEN ALLOWING BRACKET TO MOVE BACK AND FORTH. C/W EA M-23-125-01839 REQUIRES PERM REPAIR WITHIN 10 DAYS.<[01] C?W EA M-23-125
- [SDR SWAA2023101610668](https://openairdocs.org/sdr/SWAA2023101610668), Oct 13, 2023: SIGN. BROKEN. AFT OVERHEAD 'EMERGENCY EXIT' SIGN IS BROKEN<[01] R&R AFT OVERHEAD EMERGENCY EXIT SIGN REF AMM 33-51-01 OPS CK GOOD
- [SDR SWAA2023071979328](https://openairdocs.org/sdr/SWAA2023071979328), Jul 17, 2023: LAMP. INOPERATIVE. EMERGENCY LIGHT ABOVE PAX SEATING 13 DEF INOP.<[01] RELAMPED EMERGENCY AREA LIGHT OVER PAX SEATING 13 DEF IAW AMM 33-51-03. OPS CHECK GOOD.
- [SDR SWAA2023022104377](https://openairdocs.org/sdr/SWAA2023022104377), Feb 18, 2023: LIGHT. INOPERATIVE. LH EMERGENCY EXIT SIDEWALL LIGHT IS INOP.<[01] TRANS. TO MEL 33-2-03. SP1B.;[02] RELAMPED L/H EMER EXIT SIDEWALL LT PER AMM CH.33-21-00.
- [SDR SWAA2022100450876](https://openairdocs.org/sdr/SWAA2022100450876), Oct 1, 2022: NONE. OUT OF POSITION. CUSTOMER WALK - PASSENGER SEAT ROW 11 EFD ISLE SEAT RECLINES AND SHOULD NOT. (EMERGENCY EXIT ROW) / [01] ADJUSTED RECLINE FOR SEAT ROW 11 FED AS PER CMM 25-23-4
- [SDR SWAA2022100546468](https://openairdocs.org/sdr/SWAA2022100546468), Sep 29, 2022: LAMP. INOPERATIVE. EMERGENCY LIGHT INOP; OVERHEAD BIND 11DEF EMERGENCY LIGHT INOP OVERHEAD BIND 11DEF / [01] RELAMPED EMERGENCY LIGHT AT OVERHEAD BIN 11DEF AS PER B737 AMM 33-51-0
- [SDR SWAA2022100446466](https://openairdocs.org/sdr/SWAA2022100446466), Sep 28, 2022: RETAINER. BROKEN. R-1 DOOR FWD GIRT BAR RETAINER BROKEN / [01] REMOVED AND REPLACED NEW RETAINER GIRT BAR AT # 1 R DOOR AS PER B737-700 SRM 51-40-02-0G-0;[02] VERIFIED STEP 1
- [SDR SWAA2022100516020](https://openairdocs.org/sdr/SWAA2022100516020), Sep 22, 2022: LIGHT. CRAZED. MAIN CABIN ALL T PHOTOLUMINESCENCET STRIP ARE DISCOLORED AND CRAZE. / [01] THIS N/R WILL BE ACCOMPLISHED ON TTG8Q00AVSC0;[02] [FINAL] VALIDATED STEP 1
- [SDR SWAA2022100552828](https://openairdocs.org/sdr/SWAA2022100552828), Sep 13, 2022: FLANGE. CRACKED. APU INLET DUCT WITH MULTIPLE CRACKS AT FWD FLANGE / [01] REMOVED THE DAMAGED PLIES AND PREPARED AREA TO APPLY THE FABRIC REPAIR PLIES; NO WATER NOTE; AT APU INL
- [SDR SWAA2022100549193](https://openairdocs.org/sdr/SWAA2022100549193), Sep 2, 2022: FLOOR PANEL. DELAMINATED. PAX CABIN FWD WET AREA FLOOR PANEL 221EF UPPER SURFACE FLAKING / [01] MEASUREMENTS;[02] REPAIRED TOP SURFACE DAMAGE ON FLOOR PANEL 221EF AS MARKED WITH A PERMAN
- [SDR SWAA2022100549192](https://openairdocs.org/sdr/SWAA2022100549192), Sep 2, 2022: PLATE. CORRODED. *CORROSION* AFT CARGO CUTOUT CAP CORNER PLATES AT S-25R STA. 794 AND STA 847 RBL 22 WL 156 HAVE SURFACE CORROSION AS MARKED. 124-011 / [01] REPLACED CORNERS PLA

All 167: https://openairdocs.org/aircraft/N7879A/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 737-7K9 aircraft: https://openairdocs.org/model/boeing-737-7k9/aircraft.md
- The CFM International CFM56-7B24 series engine: https://openairdocs.org/engine/cfm-international-cfm56-7b24-series.md

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