# N7868K: 2001 Boeing 737-79P

- Status: Valid registration
- Airframe: [Boeing 737-79P](https://openairdocs.org/model/boeing-737-79p) (registry code 13844JA, 149 seats)
- Engine: [CFM International CFM56-7B24 series](https://openairdocs.org/engine/cfm-international-cfm56-7b24-series) (registry code 13044)
- Serial number: 29364
- Year built: 2001
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: June 4, 2018
- Certificate issued: December 16, 2022
- Expires: December 31, 2029
- Mode S code: AAAA4A
- 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=7868K
- Page: https://openairdocs.org/aircraft/N7868K

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 737-79P)

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 N7868K.

## FAA accident and incident reports

None matched to N7868K.

## Service difficulty reports (231, 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 SWAA2026100762237](https://openairdocs.org/sdr/SWAA2026100762237), Oct 1, 2026: BATTERY PACK. INOPERATIVE. SEVERAL EMERGENCY LIGHTS INOPERATIVE. REMOVED, REPLACED, AND PERFORMED SATISFACTORY OPS CHECK OF EMERGENCY LIGHT BATTERIES LOCATION M1675, M01669, M01672, AND M
- [SDR SWAA2026100714266](https://openairdocs.org/sdr/SWAA2026100714266), Oct 1, 2026: BATTERY PACK. INOPERATIVE. SEVERAL EMERGENCY LIGHTS INOPERATIVE. REMOVED, REPLACED, & PERFORMED A SATISFACTORY OPS CHECK OF THE BATTERIES, M1675, M01669, M01672, & M01673 IAW IAW AMM 33-5
- [SDR SWAA2026100791478](https://openairdocs.org/sdr/SWAA2026100791478), Oct 1, 2026: BATTERY PACK. INOPERATIVE. SEVERAL EMERGENCY LIGHTS INOPERATIVE. REMOVED, REPLACED, & PERFORMED SATISFACTORY OPS CHECK OF EMERGENCY LIGHT BATTERIES, M1675, M01669, M01672, & M01673 IAW AM
- [SDR SWAA2026100774168](https://openairdocs.org/sdr/SWAA2026100774168), Oct 1, 2026: BATTERY PACK. INOPERATIVE. SEVERAL EMERGENCY LIGHTS WERE INOPERATIVE. REMOVED, REPLACED, & PERFORMED A SATISFACTORY OPS CHECK OF THE EMERGENCY LIGHT BATTERIES, M1675, M01669, M01672, & M0
- [SDR SWAA2026100754271](https://openairdocs.org/sdr/SWAA2026100754271), Oct 1, 2026: BATTERY PACK. INOPERATIVE. SEVERAL EMERGENCY LIGHTS INOPERATIVE. REMOVED, REPLACED AND PERFORMED SATISFACTORY OPS CHECK OF EMERGENCY LIGHT BATTERIES M1675, M01669, M01672, & M01673 IAW AM
- [SDR SWAA2026080320505](https://openairdocs.org/sdr/SWAA2026080320505), Jul 30, 2026: LAMP. INOPERATIVE. LEFT OVERWING EXIT WINDOW LIGHT INOPERATIVE. RELAMPED IAW 33-51-01.
- [SDR SWAA2026070618272](https://openairdocs.org/sdr/SWAA2026070618272), Jul 3, 2026: GIRT BAR. OUT OF ADJUST. L1 DOOR LT GIRT BAR CLIP LOST TENSION AND GIRT BAR SLIPS OUT. ADJUSTED GIRT BAR CLIPS ON L1 DOOR IAW SIP. OPS CHECKED GOOD.
- [SDR SWAA2026070618013](https://openairdocs.org/sdr/SWAA2026070618013), Jul 2, 2026: SLIDE. OUT OF POSITION. L1 DOOR EMERGENCY ESCAPE SLIDE NOT IN STOWED POSITION. SECURED FWD ENTRY DOOR SLIDE PER MT 725-61-06.
- [SDR SWAA2026062415020](https://openairdocs.org/sdr/SWAA2026062415020), Jun 22, 2026: HOOK. LOOSE. GIRT BAR STOWAGE HOOKS AT FWD SERVICE DOOR LOOSE. ADJUSTED THE HOOKS IAW MM SIP.
- [SDR SWAA2026060808621](https://openairdocs.org/sdr/SWAA2026060808621), Jun 2, 2026: SENSOR. OUT OF RANGE. MAX T/O THRUST MTJ 97.1 N1 ON CLIMB NR 2 EGT INDICATED 966. REDUCED NR 2 THRUST BELOW REDLINE. INDICATIONS NORMAL AFTER - NO MASTER CAUTION LIGHTS. CW FIM 77-21
- [SDR SWAA2025120339727](https://openairdocs.org/sdr/SWAA2025120339727), Nov 26, 2025: FUSE. BLOWN. MULTIPLE EMERGENCY LIGHTS SURROUNDING RT OVERWING EXIT INOPERATIVE. REPLACED THE FUSE AND PERFORMED A GOOD OPS TEST OF EMERGENCY LIGHTS SURROUNDING RT OVERWING 
- [SDR SWAA2025120338522](https://openairdocs.org/sdr/SWAA2025120338522), Nov 21, 2025: LIGHT. DAMAGED. FWD OF RT OVERWING EXIT DOOR EXIT LIGHT DAMAGED. INSTALLED NEW RT OVERWING EXIT DOOR LIGHT ASSY IAW AMM 33-51-01-960-802, STEPS 3, (C).(9).(10). PERFORMED SUCCE
- [SDR SWAA2025120336818](https://openairdocs.org/sdr/SWAA2025120336818), Nov 19, 2025: GLOWSTRIP. DAMAGED. CABIN PHOTOLUM, SHIP SET FOUND DAMAGED REQUIRE REPLACEMENT. INSTALLED PHOTOLUMINESCENT STRIPS EXCEPT SEGMENTS AP AND AN PER SWA DWG 33500007 REV 2, AND AMM 33-5
- [SDR SWAA2025121534525](https://openairdocs.org/sdr/SWAA2025121534525), Nov 13, 2025: RIB. CRACKED. FOUND ONE CRACK RADIATING FROM FASTENER HOLE AT LT HORIZONTAL STAB RIB 5, HSS 129.50, LOWER FLANGE ADJACENT TO THE NR 1 VERTICAL STIFFENER.
- [SDR SWAA2025120334898](https://openairdocs.org/sdr/SWAA2025120334898), Nov 13, 2025: STIFFENER. CRACKED. FOUND CRACK RADIATING FROM ONE FASTENER HOLE, LT HORIZONTAL STAB RIB 5 HSS 129.50 LOWER FLANGE ADJACENT TO NR 4 VERTICAL STIFFENER. REPAIRED LWR FLANGE NR.4 STI
- [SDR SWAA2025120334113](https://openairdocs.org/sdr/SWAA2025120334113), Nov 12, 2025: ATTACH ANGLE. CRACKED. CRACKED ATTACH ANGLE AT FCB BS 500B AFT SIDE, RBL 25, WL 154. REMOVED AND REPLACED THE ATTACH ANGLE IAW SRM 51-40-05, & DWG 143A7505 REV A.
- [SDR SWAA2025120334515](https://openairdocs.org/sdr/SWAA2025120334515), Nov 12, 2025: SEAL. CRACKED. RIGHT HORIZONTAL STAB FWD UPPER SLIDE SEAL CRACKED. REMOVED AND REPLACED THE HORIZONTAL STAB FWD UPPER SLIDE SEAL IAW AMM 53-31-31-000-802, & AMM 53-31-31-400-8
- [SDR SWAA2025120334112](https://openairdocs.org/sdr/SWAA2025120334112), Nov 12, 2025: STIFFENER. CRACKED. NUMBER 2 VERTICAL STIFFENER AT LT HORIZONTAL STAB, RIB 5, HSS 129.50 IS CRACKED. REPAIRED THE STIFFENER; IAW SRM 55-10-09-2R-4.
- [SDR SWAA2025120333713](https://openairdocs.org/sdr/SWAA2025120333713), Nov 11, 2025: WEB. CHAFED. E/E BAY DOOR SURROUND STRUCTURE LONGITUDINAL CLOSE-OUT WEB HAS CHAFING DAMAGE ON THE TOP EDGE, BS 337.5, RBL 11.5. REMOVED, FABRICATED, & REPLACED THE CLOSE-OUT
- [SDR SWAA2025120334103](https://openairdocs.org/sdr/SWAA2025120334103), Nov 11, 2025: GUSSET. CRACKED. FWD CARGO BAY AFT BULKHEAD SUPPORT GUSSET IS CRACKED, BS 500D, S19R, WL 193. REMOVED & REPLACED THE SUPPORT GUSSET IAW SRM 51-40-02, & DWG 143A79020259, REV -.
- [SDR SWAA2025120334102](https://openairdocs.org/sdr/SWAA2025120334102), Nov 11, 2025: GUSSET. CRACKED. FWD CARGO BAY AFT BULKHEAD SUPPORT GUSSET IS CRACKED, BS 500D, S19L, WL 193. REMOVED & REPLACEDTHE SUPPORT GUSSET IAW SRM 51-40-02, & DWG 143A79020259, REV -.
- [SDR SWAA2025120334105](https://openairdocs.org/sdr/SWAA2025120334105), Nov 11, 2025: ATTACH ANGLE. CRACKED. CRACKED ATTACH ANGLE AT FCB BS 500C, FWD SIDE, LBL 25, WL 154. REMOVED AND REPLACED ATTACH ANGLE IAW SRM 51-40-02, & DWG 143A75050005, REV -.
- [SDR SWAA2025120334108](https://openairdocs.org/sdr/SWAA2025120334108), Nov 11, 2025: ATTACH ANGLE. CRACKED. CRACKED ATTACH ANGLE AT FCB BS 500C, AFT SIDE, LBL 25, WL 154. REMOVED AND REPLACED THE ATTACH ANGLE IAW SRM 51-40-02, & DWG 143A75050005, REV-.
- [SDR SWAA2025120334106](https://openairdocs.org/sdr/SWAA2025120334106), Nov 11, 2025: ATTACH ANGLE. CRACKED. CRACKED ATTACH ANGLE AT FCB BS 500C, FWD SIDE, RBL 25, WL 154. REMOVED AND REPLACED THE ATTACH ANGLE IAW SRM 51-40-02, AND DWG 143A7505, REV D.
- [SDR SWAA2025120334109](https://openairdocs.org/sdr/SWAA2025120334109), Nov 11, 2025: ATTACH ANGLE. CRACKED. CRACKED ATTACH ANGLE AT FCB BS 500B, FWD SIDE, RBL 25, WL 154. REMOVED AND REPLACED THE ATTACH ANGLE IAW SRM 51-40-05, AND DWG 143A7505, REV B.
- [SDR SWAA2025120334110](https://openairdocs.org/sdr/SWAA2025120334110), Nov 11, 2025: ATTACH ANGLE. CRACKED. CRACKED ATTACH ANGLE AT FCB BS 400, LBL 25, WL 154. REMOVED AND REPLACED THE ATTACH ANGLE IAW SRM 51-40-02, & DWG 143A75050012 REV -.
- [SDR SWAA2025120335209](https://openairdocs.org/sdr/SWAA2025120335209), Nov 11, 2025: WIRE. PULLED. FOUND WIRES W3142-476-20 AND W3142-474-20 PULLED FROM GROUND BLOCK BS 986 LT. TERMINATED WIRES W3142-476-20 AND W3142-474-20 & INSTALLED ON GB3814 IAW SWPM 20-9
- [SDR SWAA2025120334104](https://openairdocs.org/sdr/SWAA2025120334104), Nov 11, 2025: SUPPORT. CRACKED. RIGHT WING TO BODY FORMER SUPPORT CRACKED JUST INBD OF FIXED L/E BS 500D, S19R, ACCESS PANEL 191FR. REMOVED AND REPLACED THE WING TO BODY FORMER SUPPORT IAW SRM
- [SDR SWAA2025120333709](https://openairdocs.org/sdr/SWAA2025120333709), Nov 10, 2025: STRINGER CLIP. CRACKED. ATTACH ANGLE BS 259.5 S8L CRACKED. REMOVED AND REPLACED STRINGER CLIP BS 259.5 S8L HEAT TREATED TO T6 CONDITION ON CARD RO 1065210-SWA IAW SRM 51-40-02-0G-0 AND
- [SDR SWAA2025120333182](https://openairdocs.org/sdr/SWAA2025120333182), Nov 9, 2025: ATTACH ANGLE. CORRODED. AFT CARGO BAY FRAME TO SIDEWALL SUPPORT ATTACH ANGLE HAS CORROSION ON UPPER FLANGE AT FASTENER HOLES, BS 727D, S19L - S25L. REMOVED AND REPLACED AFT CARGO BAY F
- [SDR SWAA2025120333187](https://openairdocs.org/sdr/SWAA2025120333187), Nov 9, 2025: SIDEWALL SUPPORT. CORRODED. FORWARD CARGO BAY DOOR SURROUND STRUCTURE HAS CORROSION ON AFT FLOOR TO SIDEWALL SUPPORT AROUND FASTENER HOLES, BS 492 - 500A, RBL 24. REMOVED & REPLACED SIDWAL
- [SDR SWAA2025120333188](https://openairdocs.org/sdr/SWAA2025120333188), Nov 9, 2025: SIDEWALL SUPPORT. CORRODED. FORWARD CARGO BAY DOOR SURROUND STRUCTURE FORWARD FLOOR TO SIDEWALL SUPPORT HAS CORROSION AROUND FASTENER HOLES; BS 420 - 440, RBL 24. REMOVED & REPLACED THE SI
- [SDR SWAA2025120333428](https://openairdocs.org/sdr/SWAA2025120333428), Nov 9, 2025: PANEL. DELAMINATED. PANEL 194CR HAS DELAMINAION ON OUTER SURFACE. PANEL 194CR WITH DELAMINATION ON OUTER SURFACE WAS REPAIRED IAW SRM 51-70-05-2R-2, & SRM 53-60-70-2R-1.
- [SDR SWAA2025120333427](https://openairdocs.org/sdr/SWAA2025120333427), Nov 9, 2025: PANEL. DELAMINATED. PANEL 194CL HAS DELAMINAION ON OUTER SURFACE. REPAIRED IAW AMM 51-21-99-300-802.
- [SDR SWAA2025120332952](https://openairdocs.org/sdr/SWAA2025120332952), Nov 8, 2025: SIDEWALL SUPPORT. CORRODED. AFT CARGO BAY CORROSION ON LT FLOOR TO SIDEWALL SUPPORT AT FASTENER HOLES; BS 727 - 847. REMOVED AND REPLACED SIDEWALL SUPPORT IAW SRM 51-40-02-0G-0 AND DWG 146
- [SDR SWAA2025120332951](https://openairdocs.org/sdr/SWAA2025120332951), Nov 8, 2025: SIDEWALL SUPPORT. CORRODED. AFT CARGO BAY CORROSION ON RT FLOOR TO SIDEWALL SUPPORT AT FASTENER HOLES, BS 767 - 787. REMOVED AND REPLACED AFT CARGO BAY RT FLOOR TO SIDEWALL IAW SRM 51-40-0
- [SDR SWAA2025120332954](https://openairdocs.org/sdr/SWAA2025120332954), Nov 8, 2025: SIDEWALL SUPPORT. CORRODED. AFT CARGO BAY CORROSION AT FASTENER HOLES ON R/H FLOOR TO SIDEWALL SUPPORT BS 727-767. REMOVED AND REPLACED THE SIDEWALL SUPPORT IAW SRM 51-40-02-0G-0 AND DWG 1
- [SDR SWAA2025120332586](https://openairdocs.org/sdr/SWAA2025120332586), Nov 7, 2025: SCUFF PLATE. CRACKED. FCB FWD CORNER SCUFF PLATE IS CRACKED. RECEIVED NEW FCB FWD CORNER SCUFF PLATE AND WILL BE INSTALLED ON TC TTG8Q00A5WT6.
- [SDR SWAA2025120332947](https://openairdocs.org/sdr/SWAA2025120332947), Nov 7, 2025: SCUFF PLATE. CRACKED. ACD FWD CORNER SCUFF PLATE IS CRACKED. REPAIRED ACB FWD CORNER SCUFF PLATE PER SRM 53-60-15-2R-1. TASK CARD COMPLETED.
- [SDR SWAA2025120332826](https://openairdocs.org/sdr/SWAA2025120332826), Nov 7, 2025: INTERCOSTAL. CRACKED. FED INTERCOSTAL FROM BS 294.5 - 303.9, S16L, WL 216 CRACKED. REMOVED AND REPLACED FED INTERCOSTAL IAW SRM 51-40-02 AND DWG 141A8180 REV: C.
- [SDR SWAA2025120332827](https://openairdocs.org/sdr/SWAA2025120332827), Nov 7, 2025: RIB. CRACKED. STIFFENER NR 3 AT LT HORIZONTAL STAB (RIB 5) HSS 129.50 CRACKED. REPAIRED THE STIFFENER; IAW SRM 55-10-09-2R-4, HSS 129.5.
- [SDR SWAA2025121532380](https://openairdocs.org/sdr/SWAA2025121532380), Nov 6, 2025: DRIP TRAY. CRACKED. AFT RT DRIP SHIELD IS CRACKED.
- [SDR SWAA2025120332382](https://openairdocs.org/sdr/SWAA2025120332382), Nov 6, 2025: BATTERY PACK. NO TEST. BATTERY PACK M1670 FAILED TEST. R & R BATTERY PACK M1670 IAW AMM 33-51-06-960-805 & PERFORMED GOOD OPS CHECK.
- [SDR SWAA2025120232381](https://openairdocs.org/sdr/SWAA2025120232381), Nov 6, 2025: BATTERY PACK. NO TEST. BATTERY PACK M1668 FAILED TEST. R & R BATTERY PACK M1668 AND PERFORMED GOOD OPS CHECK IAW AMM 33-51-06-960-805.
- [SDR SWAA2025120332129](https://openairdocs.org/sdr/SWAA2025120332129), Nov 5, 2025: SCUFF PLATE. CRACKED. FORWARD SERVICE DOOR AFT LOWER CORNER; SCUFF PLATE HAS A CRACK. WELDED CRACKED / DAMAGED AREA OF SCUFF PLATE IAW SRM 53-10-15-2R-2, STEP 4.B.(4). APPLIED TWO CO
- [SDR SWAA2025071791330](https://openairdocs.org/sdr/SWAA2025071791330), Jul 15, 2025: SCUFF PLATE. CRACKED. AFT CARGO DOOR CENTER SCUFF PLATE HAS A LARGE CENTER DENT AND CRACK ON ITS RADIUS. REMOVED AND REPLACED PER AMM 53-11-02-401-NG (CARGO DOOR SCUFF PLATE - REMOVA
- [SDR SWAA2025030601928](https://openairdocs.org/sdr/SWAA2025030601928), Mar 4, 2025: BATTERY PACK. INOPERATIVE. EMERGENCY LIGHTS ABOVE L1 DOOR AND OUTSIDE THE R1 DOOR ARE INOP.<[01] 01 - REMOVED AND REPLACED M1674 BATTERY PACK PER [AMM 33-51-06-960-805-NG (POWER SUPPLY - 
- [SDR SWAA2024101446131](https://openairdocs.org/sdr/SWAA2024101446131), Oct 8, 2024: BATTERY PACK. NO TEST. AFT R/H EMERGENCY LIGHTING BATTERY PACK FAILED CAPACITY CHECK.<[01] REMOVED AND REPLACED BATTERY PACK PER M/M 33-51-06
- [SDR SWAA2024080221385](https://openairdocs.org/sdr/SWAA2024080221385), Aug 1, 2024: SEAT BACK. OUT OF ADJUST. SEAT 11D IN FRONT OF EXIT ROW RECLINES<[01] INSTALLED RECLINE LOCKS IAW AMM 25-22-00
- [SDR SWAA2024051585436](https://openairdocs.org/sdr/SWAA2024051585436), May 14, 2024: SEAT TRACK. CRACKED. CAPTS I/B FWD SEAT TRACK IS CRACKED<[01] R/R?D CAPTS I/B FWD SEAT TRACK IAW MM 25-11-11

All 231: https://openairdocs.org/aircraft/N7868K/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 737-79P aircraft: https://openairdocs.org/model/boeing-737-79p/aircraft.md
- The CFM International CFM56-7B24 series engine: https://openairdocs.org/engine/cfm-international-cfm56-7b24-series.md

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