# N7862A: 2005 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: 33009
- Year built: 2005
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: November 21, 2017
- Certificate issued: December 19, 2022
- Expires: December 31, 2029
- Mode S code: AAA96F
- 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=7862A
- Page: https://openairdocs.org/aircraft/N7862A

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 737-79P)

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 N7862A.

## FAA accident and incident reports

None matched to N7862A.

## Service difficulty reports (236, 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 SWAA2025110531910](https://openairdocs.org/sdr/SWAA2025110531910), Nov 4, 2025: COALESCER BAG. ODOR. ON TAXI IN, STARTED APU, TURNED ON APU AIR. SMELLED SMOKE, TURNED OFF APU AIR AND APU. TURNED OFF RECIRCULATION FAN ODOR CLEARED. SMOKE ODOR IN ENTIRE CABIN, FW
- [SDR SWAA2025110327051](https://openairdocs.org/sdr/SWAA2025110327051), Oct 22, 2025: LAMP. NOT SEATED. LEFT EMERGENCY EXIT HATCH OVERHEAD LIGHT INOPERATIVE. ON INVESTIGATION FOUND LT EMERGENCY EXIT HATCH OVERHEAD LAMP INCORRECTLY SEATED, SEATED CORRECTLY AND PERF
- [SDR SWAA2025110327053](https://openairdocs.org/sdr/SWAA2025110327053), Oct 22, 2025: CONNECTOR. DISCONNECTED. SEVERAL RT & LT OVERHEAD STOWAGE BULLNOSE EMERGENCY EXIT LIGHTS INOPERATIVE. RECONNECTED CONNECTOR D13018 TO EMERGENCY LIGHT POWER SUPPLY M2335 IAW AMM 33-51-06
- [SDR SWAA2025110323750](https://openairdocs.org/sdr/SWAA2025110323750), Oct 12, 2025: GLOWSTRIP. DAMAGED. MULTIPLE PHOTOLUMINESCENT STRIPS FOUND DAMAGED. REPLACED AND INSTALLED NEW PHOTOLUMINESCENTS STRIPS KIT IAW DWG 33500007, REV 2.
- [SDR SWAA2025103022363](https://openairdocs.org/sdr/SWAA2025103022363), Oct 8, 2025: RIB. CRACKED. FOUND CRACK LOCATED AT RT HORIZONTAL STAB NR 4 RIB STAB STA 120.30 NR 1 VERTICAL STIFFENER. REPAIRED IAW SRM 55-10-09-2R-4.
- [SDR SWAA2025103022364](https://openairdocs.org/sdr/SWAA2025103022364), Oct 8, 2025: RIB. CRACKED. FOUND CRACK LOCATED AT RT HORIZONTAL STAB NR 4 RIB STAB STA 120.30 NR 4 VERTICAL STIFFENER. REPAIRED IAW SRM 55-10-09-2R-5.
- [SDR SWAA2025103022362](https://openairdocs.org/sdr/SWAA2025103022362), Oct 8, 2025: RIB. CRACKED. FOUND CRACKS LOCATED AT RT HORIZONTAL STAB NR 4 RIB HSS 120.30, FRONT SPAR ATTACH STIFFENER. REMOVED AND REPLACED RT HORIZONTAL STAB RIB FRONT STIFFENER IAW SRM
- [SDR SWAA2025110421441](https://openairdocs.org/sdr/SWAA2025110421441), Oct 4, 2025: ANGLE. DEFORMED. DEFORMED ANGLE RBL20.6 STA1096 WL 249.61 HORIZONTAL BEAM LOWER. RII ITEMS COMPLIED WITH ON 25-153-02689-WIP1-WIP4. NO RII REQUIREMENTS ON 25-153-01768-WIP1. REM
- [SDR SWAA2025110421439](https://openairdocs.org/sdr/SWAA2025110421439), Oct 4, 2025: STIFFENER. DEFORMED. DEFORMED STIFFENER BS 1096, RBL 10 - 30.6, WL 249.61 HORIZONTAL BEAM LOWER. REMOVED AND REPLACED THE STIFFENER IAW SRM 51-40-02-0G-0 AND EA 25-153-02689, FIGURE
- [SDR SWAA2025110321440](https://openairdocs.org/sdr/SWAA2025110321440), Oct 4, 2025: STIFFENER. DEFORMED. DEFORMED STIFFENER BS 1088, RBL 15 TO RBL 29, WL 249.61. HORIZONTAL BEAM LOWER. REFER TO FAULT TTG8Q015D0QP WHERE EA 25-153-02689 WAS ADDED AS A SUBTASK..
- [SDR SWAA2025110321438](https://openairdocs.org/sdr/SWAA2025110321438), Oct 4, 2025: ANGLE. DEFORMED. DEFORMED ANGLE, RBL 20.6, BS 1088 - 1096, WL 249.61, HORIZONTAL BEAM LOWER. REMOVED AND REPLACED THE ANGLE IAW SRM 51-40-02-0G-0, AND EA 25-153-02689, FIGURE 3,
- [SDR SWAA2025103018362](https://openairdocs.org/sdr/SWAA2025103018362), Sep 26, 2025: INTERCOSTAL. CORRODED. CORROSION ON AFT CARGO BAY INTERCOSTAL AT BS 767 TO 787 RBL 6 WL 150. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 51-40-02-0G, AND DWG 146A8130, REV B.
- [SDR SWAA2025103018363](https://openairdocs.org/sdr/SWAA2025103018363), Sep 26, 2025: INTERCOSTAL. CORRODED. CORROSION ON AFT CARGO BAY INTERCOSTAL AT BS 787 TO 807 RBL 6 WL 150. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 51-40-02-0G AND DWG 146A8130, REV B.
- [SDR SWAA2025110318359](https://openairdocs.org/sdr/SWAA2025110318359), Sep 25, 2025: WEB. CORRODED. CORROSION ON AFT CARGO BAY SUB WEB THRESHOLD AT BS 794 - 847, RBL 25, WL 155. REMOVED AND REPLACED ACB SUB THRESOLD WEB IAW SRM 51-40-02 AND DWG 146A8120 REV: E
- [SDR SWAA2025103018360](https://openairdocs.org/sdr/SWAA2025103018360), Sep 25, 2025: INTERCOSTAL. CORRODED. CORROSION ON AFT CARGO BAY INTERCOSTAL AT BS 767 - 807, RBL 6, WL 150. OPEN
- [SDR SWAA2025103018356](https://openairdocs.org/sdr/SWAA2025103018356), Sep 25, 2025: SIDEWALL SUPPORT. CORRODED. CORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT BS 727C - 787, LBL 21, WL 155. REMOVED & REPLACED THE FLOOR TO SIDEWALL SUPPORT IAW SRM 51-40-02-0G-0 & 
- [SDR SWAA2025103018361](https://openairdocs.org/sdr/SWAA2025103018361), Sep 25, 2025: SIDEWALL SUPPORT. CORRODED. CORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT BS 727C - 787, RBL 21, WL155. REMOVED & REPLACED FLOOR TO SIDEWALL SUPPORT IAW SRM 51-40-02, & DWG 146A7
- [SDR SWAA2025110417169](https://openairdocs.org/sdr/SWAA2025110417169), Sep 22, 2025: SEAT TRACK. CORRODED. CORROSION ON SEAT TRACK, LBL 45, BS 480+18, 500A+9, 500D+10. THIS FAULT WILL BE RESOLVED IN FAULT TTG8Q015AMZ5; DUE REPLACEMENT OF SEAT TRACK.
- [SDR SWAA2025110317055](https://openairdocs.org/sdr/SWAA2025110317055), Sep 22, 2025: SHIELD. CORRODED. CORROSION ON AFT SHIELD BS 500-500A, S27R WL 156. REMOVED AND REPLACED FCB AFT SHIELD IAW SRM 51-40-02-0G-0 AND DWG 143A0080 REV -.
- [SDR SWAA2025110317053](https://openairdocs.org/sdr/SWAA2025110317053), Sep 22, 2025: DOOR FRAME. CRACKED. PASSENGER CABIN FWD ENTRY DOOR STOP FITTING WEB CRACKED BS295 S-16L. REMOVED AND REPLACED PASSENGER CABIN FWD ENTRY DOOR STOP FITTING INTERCOSTAL S16L IAW SRM 5
- [SDR SWAA2025103017185](https://openairdocs.org/sdr/SWAA2025103017185), Sep 22, 2025: STRINGER CLIP. CRACKED. CRACKED STRINGER CLIP, BS 727A, S7R. REMOVED AND REPLACED THE STRINGER CLIP IAW SRM 51-40-02-0G-0, AND DWG 146A1102, REV E.
- [SDR SWAA2025103017186](https://openairdocs.org/sdr/SWAA2025103017186), Sep 22, 2025: STRINGER CLIP. CRACKED. CRACKED STRINGER CLIP AT BS 727B, S7R. REMOVED AND REPLACED THE STRINGER CLIP IAW SRM 51-40-02-0G-0, AND DWG 146A1102 REV D.
- [SDR SWAA2025103016913](https://openairdocs.org/sdr/SWAA2025103016913), Sep 21, 2025: RIB. CRACKED. DURING INSPECTION FOUND CRACK AT NR 4 RIB STA 120.30 STIFFENER NR 2. REPAIRED IAW SRM 55-10-09-2R-5.
- [SDR SWAA2025110316500](https://openairdocs.org/sdr/SWAA2025110316500), Sep 20, 2025: SCUFF PLATE. CRACKED. AFT CARGO DOOR FWD CORNER SCUFF PLATE IS CRACKED. RECEIVED NEW AFT CARGO DOOR FWD CORNER SCUFF PLATE ITEM 146A8341-07. IT WILL BE INSTALL ON TASK CARD TTG8Q0157
- [SDR SWAA2025110316512](https://openairdocs.org/sdr/SWAA2025110316512), Sep 20, 2025: FITTING. CRACKED. CRACKED FITTING, BS 559+8, LBL 6, WL 148.5. RECEIVED NEW FITTING. REMOVED AND REPLACED THE FITTING IAW SRM 51-40-02-0G-0, AND AIPC 53-12-11-25 FIG 2.
- [SDR SWAA2025110316718](https://openairdocs.org/sdr/SWAA2025110316718), Sep 20, 2025: FLOORBEAM. CRACKED. CRACKED FLOORBEAM, BS 540, LBL 2, WL 208. REMOVED AND INSTALLED A NEW FLOORBEAM IAW SRM 51-40-02 AND DWG 143A0060.
- [SDR SWAA2025110316719](https://openairdocs.org/sdr/SWAA2025110316719), Sep 20, 2025: FLOORBEAM. CRACKED. CRACKED FLOORBEAM BS 540, RBL 2, WL 208. REMOVED AND REINSTALLED THE FLOORBEAM IAW SRM 51-40-02 AND DWG 143A0060.
- [SDR SWAA2025103016496](https://openairdocs.org/sdr/SWAA2025103016496), Sep 19, 2025: STRINGER CLIP. NO DISCREPANCY. FUSELAGE STRINGER CLIP BS 706, S10L CRACKED. HFEC INSPECTED AREA IAW NDTM PART 6, 51-00-00, PROCEDURE 23. NO CRACKS NOTED.
- [SDR SWAA2025103016497](https://openairdocs.org/sdr/SWAA2025103016497), Sep 19, 2025: STRINGER CLIP. NO DISCREPANCY. FUSELAGE STRINGER CLIP BS 727A S15L CRACKED. HFEC INSPECTED AREA IAW NDTM PART 6; 51-00-00, PROCEDURE 23. NO CRACKS NOTED.
- [SDR SWAA2025110316163](https://openairdocs.org/sdr/SWAA2025110316163), Sep 18, 2025: PRESSURE DECK. CRACKED. CRACK NOTED ON LEFT HORIZONTAL PRESSURE DECK WEB BS 673, LBL 32, WL 202.5. L: 0.4. REPAIRED THE PRESSURE DECK AND REMOVED & REPLACED ALL SHORT AND HIGH FASTENER
- [SDR SWAA2025103015048](https://openairdocs.org/sdr/SWAA2025103015048), Sep 16, 2025: FLOOR PANEL. PULLED. FLOOR PANEL 232SF UPPER SKIN HAS AREAS OF PULLED STRANDS. REPAIRED THE FLOOR PANEL IAW SRM 53-00-50-2R-0-A00938.
- [SDR SWAA2025103015049](https://openairdocs.org/sdr/SWAA2025103015049), Sep 16, 2025: FLOOR PANEL. PULLED. FLOOR PANEL 231XF UPPER SKIN HAS AREAS OF PULLED STRANDS. REPAIRED THE FLOOR PANEL IAW SRM 53-00-50-2R-0-A00938.
- [SDR SWAA2025103015050](https://openairdocs.org/sdr/SWAA2025103015050), Sep 16, 2025: FLOOR PANEL. PULLED. FLOOR PANEL 231ZF UPPER SKIN HAS AREAS OF PULLED STRANDS. REPAIRED THE FLOOR PANEL IAW SRM 53-00-50-2R-0-A00938.
- [SDR SWAA2025103015052](https://openairdocs.org/sdr/SWAA2025103015052), Sep 16, 2025: FLOOR PANEL. PULLED. FLOOR PANEL 241BF UPPER SKIN HAS AREAS OF PULLED STRANDS. FLOOR PANEL 241BF REPLACED WITH A NEW FABRICATED FLOOR PANEL IAW SRM 53-00-50-2R-0.
- [SDR SWAA2025103015054](https://openairdocs.org/sdr/SWAA2025103015054), Sep 16, 2025: FLOOR PANEL. PULLED. FLOOR PANEL 242AF UPPER SKIN HAS AREAS OF PULLED STRANDS. REPAIRED THE FLOOR PANEL IAW SRM 53-00-50-2R-0-A00938.
- [SDR SWAA2025103015057](https://openairdocs.org/sdr/SWAA2025103015057), Sep 16, 2025: FLOOR PANEL. PULLED. FLOOR PANEL 241DF UPPER SKIN HAS AREAS OF PULLED STRANDS. REPAIRED THE FLOOR PANEL IAW SRM 53-00-50-2R-0-A00938.
- [SDR SWAA2025103015056](https://openairdocs.org/sdr/SWAA2025103015056), Sep 16, 2025: FLOOR PANEL. PULLED. FLOOR PANEL 242CF UPPER SKIN HAS AREAS OF PULLED STRANDS. REPAIRED FLOOR PANEL IAW SRM 53-00-50-2R-0-A00938.
- [SDR SWAA2025103015058](https://openairdocs.org/sdr/SWAA2025103015058), Sep 16, 2025: FLOOR PANEL. PULLED. FLOOR PANEL 242DF UPPER SKIN HAS AREAS OF PULLED STRANDS. FABRICATED A NEW FLOOR PANEL IAW DWG 144A5810 0123.
- [SDR SWAA2025103015051](https://openairdocs.org/sdr/SWAA2025103015051), Sep 16, 2025: FLOOR PANEL. PULLED. FLOOR PANEL 241AF UPPER SKIN HAS AREAS OF PULLED STRANDS. FABRICATION OF NEW 241AF FLOOR PANEL REPLACEMENT HAS BEEN ACCOMPLISHED IAW SRM 53-00-50-2R-0-A00938.
- [SDR SWAA2025103015047](https://openairdocs.org/sdr/SWAA2025103015047), Sep 16, 2025: FLOOR PANEL. PULLED. FLOOR PANEL 232RF UPPER SKIN HAS AREAS OF PULLED STRANDS FABRICATION OF NEW FLOOR PANEL REPLACEMENT HAS BEEN ACCOMPLISHED IAW SRM 53-00-50-2R-0-A00938.
- [SDR SWAA2025110415045](https://openairdocs.org/sdr/SWAA2025110415045), Sep 15, 2025: SKIN. NO DISCREPANCY. SUSPECT CRACK RT WING NR 5 SLAT LEADING EDGE AT ACTUATOR ATTACH FITTING, SLAT STATION 85.19. HFEC INSPECTED RT WING #5 SLAT LEADING EDGE AT ACTUATOR ATTACH FITT
- [SDR SWAA2025110415026](https://openairdocs.org/sdr/SWAA2025110415026), Sep 15, 2025: INLET. PULLED. PULLED THROUGH FASTENERS 2 O' CLOCK POSITION ON RIGHT INLET COWL OUTER LIP SKIN. REMOVED AND REPLACED RT INLET COWL OUTER LIP SKIN IAW SRM 54-10-01-1A-2 AND SRM
- [SDR SWAA2025040720513](https://openairdocs.org/sdr/SWAA2025040720513), Apr 1, 2025: DOOR. WARNING LIGHT. CLIMBING OUT GOT AFT ENTRY DOOR LT; RAN QRH HANDLE HAD MOVED; LT WENT OUT; DOOR LT CAME BACK ON A 2ND TIME ON FINAL; AT DIVERT CITY OF KLIT.<[01] REMOVED DEBRIS
- [SDR SWAA2025010783480](https://openairdocs.org/sdr/SWAA2025010783480), Jan 6, 2025: BATTERY PACK. NO TEST. ALL LIGHT RELATED TO BATTERY PACK M2335 FAIL TEST. REPLACED EMERGENCY BATTERY PACK. PERFORMED GOOD TEST PER AMM 33-51-06-960-805.
- [SDR SWAA2025010783482](https://openairdocs.org/sdr/SWAA2025010783482), Jan 6, 2025: LAMP. FAILED. LEFT AND RIGHT OVERWING ESCAPE GROUND ILLUMINATION FAIL EMERGENCY LIGHT TEST (L548) (L547)<[01] REPLACED LAMP TO LEFT AND RIGHT OVERWING ESCAPE (L548) AND (L547
- [SDR SWAA2025010783481](https://openairdocs.org/sdr/SWAA2025010783481), Jan 6, 2025: LAMP. INOPERATIVE. EMERGENCY LIGHT AFT ESCAPE SLIDE LIGHT (L732) OUTSIDE SERVICE DOOR LH SIDE INOP<[01] REPLACED LAMP TO EMERGENCY LIGHT AFT ESCAPE SLIDE LIGHT (L732) OUTSIDE SERV
- [SDR SWAA2025010681802](https://openairdocs.org/sdr/SWAA2025010681802), Dec 30, 2024: INTERCOSTAL. CRACKED. INTERNAL DAMAGE BETWEEN STA 927 AND 947 STR 21 L/H INTERCOSTAL CRACKED.<[01] PART TO BE REPAIRED BY REPLACEMENT PER SRM 51-10-02-0G-0 PARAGRAPH 9.<BR><BR>REMOVE
- [SDR SWAA2024123080862](https://openairdocs.org/sdr/SWAA2024123080862), Dec 26, 2024: INTERCOSTAL. CRACKED. INTERNAL DAMAGE BETWEEN STA 927 AND 947 STR 21 LH INTERCOSTAL IS CRACK.<[01] PREFORMED SURFACE CRACK NDT PER PART 6 51-00-00 PRO 23;[02] PERFORMED EA 24-153-035
- [SDR SWAA2024123080858](https://openairdocs.org/sdr/SWAA2024123080858), Dec 26, 2024: SKIN. CRACKED. INTERNAL DAMAGE AT STA 927 STR 21 LH CRACK. PREFORMED SURFACE CRACK NDT PER PART 6 51-00-00 PRO 23. PERFORMED EA 24-153-03554'. ADD A REFERENCE TO THE FAULT TTG
- [SDR SWAA2024102852533](https://openairdocs.org/sdr/SWAA2024102852533), Oct 24, 2024: SEAL. CRACKED. LEFT HORIZONTAL STABILIZER UPPER STAB TO BODY SLIDING SEAL IS CRACKED.<[01] 01 - REMOVED AND REPLACED PER [AMM 53-31-31-401 CONFIG 1-NG (STABILIZER TO BODY FRON

All 236: https://openairdocs.org/aircraft/N7862A/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 N7862A

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N7862A before.

- [Cancelled 1957-02-28](https://openairdocs.org/deregistered/N7862A-1957-02-28): Cessna 180A, S/N 32759. Owner: [Cessna Aircraft Co](https://openairdocs.org/faa-owner/CESSNA%20AIRCRAFT%20CO), [Wichita, KS](https://openairdocs.org/faa-place/KS/Wichita)

## Related

- Other Boeing 737-79P 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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