# N7861J: 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: 33008
- Year built: 2005
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: October 17, 2017
- Certificate issued: December 19, 2022
- Expires: December 31, 2029
- Mode S code: AAA954
- 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=7861J
- Page: https://openairdocs.org/aircraft/N7861J

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.

## NTSB investigations (1)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB DCA24LA219](https://openairdocs.org/ntsb/DCA24LA219), Jun 25, 2024: Boeing 737-79P (N7861J), Portland, ME, incident, no damage. Probable cause: The flight crew’s inadequate review of preflight information and the flight dispatcher’s noncompliance with company guidance requiring the placement of a flight lock, which resulted in the flight’s…

## FAA accident and incident reports

None matched to N7861J.

## 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

## Service difficulty reports (195, 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 SWAA2026081923403](https://openairdocs.org/sdr/SWAA2026081923403), Aug 15, 2026: WIRE HARNESS. BROKEN. NR 2 ENGINE -A- FIRE DETECTION LOOP INOP T/S PER FIM 26-10 TASK 801. FOUND ENGINE #2 LOOP A CORE LEFT HARNESS BROKEN AT LOOP ELEMENT. REMAINING HARNESS TOO SHOR
- [SDR SWAA2026051297922](https://openairdocs.org/sdr/SWAA2026051297922), May 11, 2026: LIMITER. FAILED. LOSS OF SYS B HYD PRESSURE AND FLUID. FOUND O-RING ON TRAILING EDGE FLAP FLOW LIMITER TORN. O-RINGS REPLACED & REPLACED TRAILING EDGE FLAP FLOW LIMITER REF AMM 
- [SDR SWAA2026051297935](https://openairdocs.org/sdr/SWAA2026051297935), May 11, 2026: O-RING. TORN. LOSS OF SYS B HYD PRESSURE AND FLUID. FOUND O-RING ON TRAILING EDGE FLAP FLOW LIMITER TORN. O-RINGS REPLACED & REPLACED TRAILING EDGE FLAP FLOW LIMITER REF AMM 
- [SDR SWAA2026031178260](https://openairdocs.org/sdr/SWAA2026031178260), Mar 10, 2026: PUMP. INOPERATIVE. LOSS OF HYDRAULIC B SYSTEM, NO OVERWEIGHT LANDING. REMOVED AND INSTALLED DUE TO HYDRAULIC LOSS, B ELECTRIC PUMP, B SYSTEM HYD FILTER, & TRAILING EDGE FLAP FLOW 
- [SDR SWAA2026031178667](https://openairdocs.org/sdr/SWAA2026031178667), Mar 10, 2026: FILTER. INOPERATIVE. LOSS OF HYDRAULIC B SYSTEM, NO OVERWEIGHT LANDING. REMOVED AND INSTALLED DUE TO HYDRAULIC LOSS, B ELECTRIC PUMP, B SYSTEM HYD FILTER, & TRAILING EDGE FLAP FLOW 
- [SDR SWAA2026031178668](https://openairdocs.org/sdr/SWAA2026031178668), Mar 10, 2026: LIMITER. LEAKING. LOSS OF HYDRAULIC B SYSTEM, NO OVERWEIGHT LANDING. REMOVED AND INSTALLED DUE TO HYDRAULIC LOSS, B ELECTRIC PUMP, B SYS HYDLAULIC FILTER, & TRAILING EDGE FLAP FL
- [SDR SWAA2025102217859](https://openairdocs.org/sdr/SWAA2025102217859), Sep 24, 2025: RIB. CRACKED. CRACK ON FRONT SPAR UPPER FLANGE INSPAR RIB 120.30 LT HORIZONTAL STAB. PERFORMED PERMANENT REPAIR ON RIB IAW EA 25-155-02690-WIP1 REV A, EA 25-155-02690, AND SR
- [SDR SWAA2025102217089](https://openairdocs.org/sdr/SWAA2025102217089), Sep 22, 2025: VAPOR BARRIER. CRACKED. TWO CRACKS ON VAPOR BARRIER BS 663.75 LH SIDE MAIN WHEEL WELL COMPARTMENT. THIS FAULT IS RESOLVED ON FAULT TTG8Q01564Z0.
- [SDR SWAA2025102315280](https://openairdocs.org/sdr/SWAA2025102315280), Sep 16, 2025: SILL DRAIN. CORRODED. CORROSION LOWER SILL LOCATED BETWEEN STA794.3 TO STA847 AND RBL24 WL156 AT AFT CARGO COMPARTMENT. REPLACED LOWER SILL LOCATED BETWEEN STA794.3 TO STA847 AND RBL
- [SDR SWAA2025102314819](https://openairdocs.org/sdr/SWAA2025102314819), Sep 15, 2025: SUPPORT BRACKET. CRACKED. CRACK SUPPORT BRACKET LOCATED BS540 AT LEVEL LBL 6 AT AIR CONDITIONING BAY. REPLACED SUPPORT BRACKET LOCATED BS540 AT LEVEL LBL 6 AT AIR CONDITIONING BAY IAW B7
- [SDR SWAA2025102314816](https://openairdocs.org/sdr/SWAA2025102314816), Sep 15, 2025: TIE CLIP. CRACKED. CRACK TIE CLIP BS 277 AND STRINGER 10R PASSENGER CABIN. REPLACED TIE CLIP AND FASTENERS LOC.BS 277 AND STRINGER 10R PASSENGER CABIN IAW SRM 51-40-02; SRM B737-7
- [SDR SWAA2025102314813](https://openairdocs.org/sdr/SWAA2025102314813), Sep 15, 2025: SUPPORT ANGLE. CRACKED. CRACK SUPPORT ANGLE BETWEEN BS 291.5 TO BS 294.5 AT LEVEL STRINGER 17R PASSENGER CABIN. REPLACED SUPPORT ANGLE LOC. BETWEEN BS 291.5 TO BS 294.5 AT LEVEL STRING
- [SDR SWAA2025102314821](https://openairdocs.org/sdr/SWAA2025102314821), Sep 15, 2025: SUPPORT BRACKET. CRACKED. CRACK SUPPORT BRACKET LOCATED BS540 AT LEVEL RBL 6 AT AIR CONDITIONING BAY . REPLACED SUPPORT BRACKET LOCATED BS540 AT LEVEL RBL 6 AT AIR CONDITIONING BAY IAW S
- [SDR SWAA2025102214625](https://openairdocs.org/sdr/SWAA2025102214625), Sep 15, 2025: VAPOR BARRIER. CRACKED. CRACK ON VAPOR BARRIER BS 663.75 LH SIDE MAIN WHEEL WELL COMPARTMENT. REPAIRED VAPOR BARRIER BS 663.75 LH SIDE MAIN WHEEL WELL COMPARTMENT IAW SRM 51-70-04-2R-1
- [SDR SWAA2025102214626](https://openairdocs.org/sdr/SWAA2025102214626), Sep 15, 2025: LIGHT. DETERIORATED. DETERIORATED PHOTOLUMINESCENT FLOOR PROXIMITY LIGHT LT SIDE 7 EA AND RT SIDE 7 EA. REPLACED PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING IAW AMM 33-51-15-400-802.
- [SDR SWAA2025102314618](https://openairdocs.org/sdr/SWAA2025102314618), Sep 14, 2025: STRAP. CORRODED. CORROSION STRAP LOCATED BETWEEN BS787 TO BS794 AND WL154 FROM STR25R TO STR26R AFT CARGO COMPARTMENT. REPLACED STRAP LOCATED BETWEEN BS787 TO BS794 AND WL154 FR
- [SDR SWAA2025102314619](https://openairdocs.org/sdr/SWAA2025102314619), Sep 14, 2025: STRAP. CORRODED. CORROSION STRAP LOCATED BETWEEN BS794 TO BS807 AND WL154 FROM STR25R TO STR26R AFT CARGO COMPARTMENT. REPLACED STRAP LOCATED BETWEEN BS794 TO BS807 AND WL154 FR
- [SDR SWAA2025102314554](https://openairdocs.org/sdr/SWAA2025102314554), Sep 14, 2025: ACCESS PANEL. CRACKED. CRACK ANGLE ACCESS PANEL 844DZ AT AFT GALLEY DOOR. REPLACED ANGLE ACCESS PANEL 844DZ AT AFT GALLEY DOOR DUE TO ALLOWABLE DAMAGE NOT FOUND IN SRM 52-10-02-1A-4; 
- [SDR SWAA2025102214613](https://openairdocs.org/sdr/SWAA2025102214613), Sep 14, 2025: CARGO TRACK. CRACKED. CRACK TRACK LBBL 17.24 LOCATED BS767 AFT CARGO COMPARTMENT. REPAIRED CARGO TRACK LOC LBL17.24 BTW BS 747 TO BS 787 IAW B737-700 SRM 53-00-53-2R-3 REPAIR 3.
- [SDR SWAA2025102314161](https://openairdocs.org/sdr/SWAA2025102314161), Sep 13, 2025: SUPPORT. CRACKED. CRACK CHANNEL SUPPORT LOCATED STA727 AND RBL 3 AT AFT CARGO COMPARTMENT. REPLACED CHANNEL SUPPORT LOCATED STA727 AND RBL 3 AT AFT CARGO COMPARTMENT IAW B737 700
- [SDR SWAA2025102314157](https://openairdocs.org/sdr/SWAA2025102314157), Sep 13, 2025: GUSSET. DAMAGED. ELONGATED HOLE GUSSET LOCATED BS500D AND STR19R FWD CARGO COMPARTMENT. REPLACED GUSSET LOCATED BS500D AND STR19R FWD CARGO COMPARTMENT IAW SRM 51-10-02 PARAGRAP
- [SDR SWAA2025102314160](https://openairdocs.org/sdr/SWAA2025102314160), Sep 13, 2025: WEB. CORRODED. CORROSION SHIELD WEB FLOOR STRUCTURE LOCATED BETWEEN STA767 TO STA794.3 AND RBL21 WL156 AT AFT CARGO COMPARTMENT. REPLACED SHIELD WEB AND FASTENERS LOC. ON FLOO
- [SDR SWAA2025102214154](https://openairdocs.org/sdr/SWAA2025102214154), Sep 13, 2025: RIB. CRACKED. CRACKED INSPAR RIB LOCATED STAB STA 120.30 AND 34 INCHES FROM FRONT EDGE LT HORIZONTAL STAB. PERFORMED PERMANENT REPAIR ON INSPAR RIB IAW SRM 51-40-02, AND SRM 
- [SDR SWAA2025102214155](https://openairdocs.org/sdr/SWAA2025102214155), Sep 13, 2025: RIB. CRACKED. CRACKED INSPAR RIB LOCATED STAB STA 120.30 AND 27 INCHES FROM FRONT EDGE LT HORIZONTAL STAB. PERFORMED PERMANENT REPAIR ON INSPAR RIB IAW SRM 51-40-02, AND SRM 
- [SDR SWAA2025102214156](https://openairdocs.org/sdr/SWAA2025102214156), Sep 13, 2025: RIB. CRACKED. CRACK INSPAR RIB LOCATED STAB STA 120.30 AND 19 INCHES FROM FRONT EDGE LT HORIZONTAL STAB. PERFORMED PERMANENT REPAIR ON INSPAR RIB IAW SRM 51-40-02, AND SRM 55
- [SDR SWAA2025102314094](https://openairdocs.org/sdr/SWAA2025102314094), Sep 12, 2025: RIB. CRACKED. CRACK INSPAR RIB LOCATED STAB STA 120.30 AND 27 INCHES FROM FRONT EDGE LT HORIZONTAL STAB.
- [SDR SWAA2025102314093](https://openairdocs.org/sdr/SWAA2025102314093), Sep 12, 2025: RIB. CRACKED. CRACK INSPAR RIB LOCATED STAB STA120.30 AND 19 INCHES FROM FRONT EDGE LT HORIZONTAL STAB.
- [SDR SWAA2025102214153](https://openairdocs.org/sdr/SWAA2025102214153), Sep 12, 2025: RIB. CRACKED. CRACK INSPAR RIB LOCATED STAB STA 129.50 AND 34 INCH FROM FRONT EDGE AT RT HORIZONTAL STAB. PERFORMED PERMANENT REPAIR ON INSPAR RIB IAW SRM 55-10-09-2R-5, REPA
- [SDR SWAA2025102313442](https://openairdocs.org/sdr/SWAA2025102313442), Sep 11, 2025: ANGLE. CRACKED. CRACK ANGLE FLOOR STRUCTURE LOCATED BS 695 AND RBL 24.75 AT PASSENGER CABIN. REPLACED ANGLE ON FLOOR STRUCTURE LOCATED BS 695 AND RBL 24.75 AT PASSENGER CABIN I
- [SDR SWAA2025102313443](https://openairdocs.org/sdr/SWAA2025102313443), Sep 11, 2025: STIFFENER. CRACKED. CRACK STIFFENER ASSY FLOOR STRUCTURE LOCATED BS 540 BETWEEN BL 0 AND RBL 24.75 PASSENGER CABIN. REPLACED STIFFENER ASSY FLOOR STRUCTURE AND FASTENERS LOCATED BS
- [SDR SWAA2025102313453](https://openairdocs.org/sdr/SWAA2025102313453), Sep 11, 2025: BEAM. CRACKED. CRACK INDICATION ON RADIUS OF FORWARD SERVICE DOOR 141A6536-14 BEAM #4.LENGTH OF CRACK: 0.625 IN. EO 5241-C-14093 OR 5241-C-14344 WILL BE ADDED TO REPAIR ORDER 
- [SDR SWAA2025102213441](https://openairdocs.org/sdr/SWAA2025102213441), Sep 11, 2025: ANGLE. CRACKED. CRACKED ANGLE LOCATED BS 695 BL0 AFT SIDE. REPLACED ANGLE IAW SRM 51-10-02, PARAGRAPH 9, SRM 51-40-02, AND DWG 273A9110, SHEET 6, REV A.
- [SDR SWAA2025102213444](https://openairdocs.org/sdr/SWAA2025102213444), Sep 11, 2025: ANGLE. CRACKED. CRACKED ANGLE LOCATED BS 695 AND BL0 FWD SIDE. REPLACED ANGLE IAW SRM 51-10-02, PARAGRAPH 9, SRM 51-40-02, AND DWG 273A9110, SHEET 6, REV A.
- [SDR SWAA2025071691040](https://openairdocs.org/sdr/SWAA2025071691040), Jul 14, 2025: LIGHT. INOPERATIVE. SEAT ROW 6ABC EMERGENCY LIGHT OUT. RELAMPED SEAT ROW 6ABC EMERGENCY AREA LIGHT. OPS CHECK GOOD PER AMM 33-51-03.
- [SDR SWAA2025052775456](https://openairdocs.org/sdr/SWAA2025052775456), May 26, 2025: UNKNOWN. ODOR. F/A REPORTS SMELL OF SMOKE IN THE AFT CABIN<[01] C/W SMOKE OR FUMES IN CABIN CONDITIONAL INSPECTION IAW AMM 05-51-56 AND FIM 21-00 TASK 806. NO DEFECTS NOTED AT
- [SDR SWAA2025052071311](https://openairdocs.org/sdr/SWAA2025052071311), May 15, 2025: LOCK. OUT OF ADJUST. PASSENGER CABIN SEAT EXIT ROW 11C IS RECLINING.<[01] ADJUSTED HYDRO-LOCK PER AMM 25-22-00;[02] INSPECTED C/A 1. ROBERT FRENZEL (TECHNICIAN); ADJUSTED HYDRO-LOCK
- [SDR SWAA2025012489208](https://openairdocs.org/sdr/SWAA2025012489208), Jan 23, 2025: COMPRESSOR. STALLED. ON CLIMB OUT THROUGH 9000 FEET; AIRCRAFT SHUDDERED AND ENGINE #1 N1 BEGAN CYCLING THROUGH 80% AND 90% N1. ENGINE REDUCED TO 50% N1 AND ENGINE INDICATIONS WERE N
- [SDR SWAA2024111157548](https://openairdocs.org/sdr/SWAA2024111157548), Nov 7, 2024: COVER. MISINSTALLED. AFT SERVICE DOOR HAS THE INCORRECT DIRECTION EMERGENCY LENS COVER.<[01] 01 - REMOVED AND REPLACED PER [AMM 33-51-01-960-802-NG (EXIT SIGN - LIGHT ASSEMBLY REPLA
- [SDR SWAA2024081526100](https://openairdocs.org/sdr/SWAA2024081526100), Aug 15, 2024: BALANCE WEIGHT. CORRODED. RUDDER BALANCE WEIGHT HAS EVIDENCE OF CORROSION<[01] R AND R RUDDER BALANCE WEIGHT PER EA 24-155-02244
- [SDR SWAA2024032667236](https://openairdocs.org/sdr/SWAA2024032667236), Mar 24, 2024: DOUBLER. CRACKED. GROUND POWER DOOR CUTOUT DOUBLER AFT EDGE FOUND CRACK<[01] PERFORMED HFEC OF THE CUTOUT REF 737 NDT MANUAL PART 6 51-00-00 PROCEDURE 23. NO DEFECTS NOTED AT THI
- [SDR SWAA2024031964420](https://openairdocs.org/sdr/SWAA2024031964420), Mar 16, 2024: EXTINGUISHER. LEAKING. COCKPIT FIRE EXTINGUISHER HAS A SLOW LEAK.<[01] REPLACED COCKPIT FIRE EXTINGUISHER PER AMM 26-26-01.
- [SDR SWAA2024011540601](https://openairdocs.org/sdr/SWAA2024011540601), Jan 13, 2024: TRANSMITTER. FAULTY. ON FINAL AFTER SELECTING FLAPS 10 FROM FLAPS 5 FLAPS SPLIT-LEFT INDICATED 6 RIGHT =8 LANDED FLAPS 5 POSITION-AFTER LANDING FLAPS INDICATED 5;PSEU LIGHT AFTER LA
- [SDR SWAA2023092603524](https://openairdocs.org/sdr/SWAA2023092603524), Sep 25, 2023: LIGHT. INOPERATIVE. EMERGENCY EXIT LIGHT ON L/H OWE FWD OF WINDOW LIGHT INOP<[01] RELAMPED AND PERFORMED GOOD INSTALLATION TEST OF EMERGENCY EXIT LIGHT ON FWD SIDE OF L/H OWE WINDO
- [SDR SWAA2023092603526](https://openairdocs.org/sdr/SWAA2023092603526), Sep 25, 2023: LIGHT. INOPERATIVE. BULLNOSE EMERGENCY EXIT LIGHT INOP AT SEAT ROW 4ABC<[01] RELAMPED AND PERFORMED GOOD INSTALLATION TEST OF BULLNOSE EMERGENCY EXIT LIGHT AT SEAT ROW 4ABC IAW AMM
- [SDR SWAA2023092603525](https://openairdocs.org/sdr/SWAA2023092603525), Sep 25, 2023: LIGHT. INOPERATIVE. EMERGENCY EXIT LIGHT IN BETWEEN FWD RECESSED CEILING LIGHTS INOP<[01] RELAMPED AND PERFORMED GOOD INSTALLATION TEST OF FWD RECESSED CEILING EMERGENCY EXIT LIGHT
- [SDR SWAA2023092603523](https://openairdocs.org/sdr/SWAA2023092603523), Sep 24, 2023: LIGHT. INOPERATIVE. EMERGENCY EXIT AREA LIGHT AT SEAT ROW 16FED IS INOP<[01] REMOVED AND REPLACED AREA LIGHT LAMP AT SEAT ROW 16FED OPS CHECK GOOD IAW AMM 33-51-03-960-801.;[02] VE
- [SDR SWAA2023092603382](https://openairdocs.org/sdr/SWAA2023092603382), Sep 22, 2023: LIGHT. BROKEN. LWH OVERWING EXIT LIGHT FWD OF DOOR CUTOUT IS BROKEN.<[01] REPLACED LWH OVERWING EXIT LIGHT FWD OF DOOR AND GOOD OPERATIONAL TEST PER AMM 33-51-01-960-802.;[02]
- [SDR SWAA2023092699962](https://openairdocs.org/sdr/SWAA2023092699962), Sep 13, 2023: PANEL. CRACKED. CRACKED BREAK PANEL STA 540; RBL 1; WL 208.<[01] UPDATED TABLE;[02] COMPLETED STEPS 1-2; OK TO INSTALL STEP 3.;[03] REMOVED & INSTALLED NEW BREAK PANEL AT BS 54
- [SDR SWAA2023092699961](https://openairdocs.org/sdr/SWAA2023092699961), Sep 13, 2023: PANEL. CRACKED. CRACKED BREAK PANEL STA 540; LBL 1; WL 208.<[01] COMPLETED STEPS 1-2; OK TO INSTALL STEP 3.;[02] REMOVED AND REPLACED BREAK PANEL AT BS 540 LBL 1 WL 208 PER SRM
- [SDR SWAA2023092899197](https://openairdocs.org/sdr/SWAA2023092899197), Sep 11, 2023: SCUFF PLATE. CRACKED. AFT CARGO BAY FWD CORNER SCUFF PLATE IS CRACKED<[01] REPAIRED THE CORNER SCUFF PLATE PER SRM 53-60-15-2R-1 PARAGRAPH 4.B.(4) AND BAC 5975 &NBSP;&NBSP;&NBSP;&NBS

All 195: https://openairdocs.org/aircraft/N7861J/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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