# N7860A: 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: 29362 - Year built: 2005 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: October 9, 2017 - Certificate issued: December 16, 2022 - Expires: December 31, 2029 - Mode S code: AAA929 - 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=7860A - Page: https://openairdocs.org/aircraft/N7860A 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 N7860A. ## FAA accident and incident reports None matched to N7860A. ## Service difficulty reports (184, 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 SWAA2026091009541](https://openairdocs.org/sdr/SWAA2026091009541), Sep 9, 2026: TRANSMITTER. LOCKED. FLAP LOCK OUT BETWEEN UP AND 1 DEGREE REMOVED AND REPLACED RH FLAP POSITION TRANSMITTER REF AMM 27-58-01 - [SDR SWAA2026070217323](https://openairdocs.org/sdr/SWAA2026070217323), Jun 29, 2026: CHARGER. INOPERATIVE. AIRCRAFT EMERGENCY LIGHTS LEFT ON BY PREVIOUS CREW. FWD ENTRY EMERGENCY LIGHTS WILL NOT OPERATE OR CHARGE. REPLACED FWD LT AND RT EMERGENCY LIGHT CHARGERS AND B - [SDR SWAA2026070218015](https://openairdocs.org/sdr/SWAA2026070218015), Jun 29, 2026: BATTERY. INOPERATIVE. AIRCRAFT EMERGENCY LIGHTS LEFT ON BY PREVIOUS CREW. FWD ENTRY EMERGENCY LIGHTS WILL NOT OPERATE OR CHARGE. REPLACED FWD LT AND RT EMERGENCY LIGHT CHARGERS AND B - [SDR SWAA2026052605569](https://openairdocs.org/sdr/SWAA2026052605569), May 22, 2026: UNKNOWN. ODOR. CUSTOMER REPORTED SMOKE SMELL IN AFT CABIN. PERFORMED SOMOKE OR FUMES IN THE CABIN CONDITIONAL INSPECTION PER FIM 21-00 TASK 806. COULD NOT DUPLICATE. NO FURTHE - [SDR SWAA2026011360102](https://openairdocs.org/sdr/SWAA2026011360102), Jan 10, 2026: LIGHT. MALFUNCTIONED. CEILING LIGHTS INOPERATIVE FROM ROW 6 TO 10 INOPERATIVE, CAPTAIN`S SIDE. LIGHTS OPS CHECKED GOOD IAW AMM 33-22-00. - [SDR SWAA2025071189933](https://openairdocs.org/sdr/SWAA2025071189933), Jul 10, 2025: BATTERY PACK. INOPERATIVE. EMERGENCY LIGHTS AT ROW ABC NOT WORKING EMERGENCY LIGHTS AT ROW ABC NOT WORKING AT M2335. REPLACED BATTERY PACK FOR M2335 IAW AMM 33-51-06. - [SDR SWAA2025060275861](https://openairdocs.org/sdr/SWAA2025060275861), May 28, 2025: LENS. MISSING. AFT ENTRY DOOR EXIT LIGHT LENS COMMON TO LAV B WALL IS MISSING. <[01] INSTALLED AFT ENTRY DOOR EXIT LIGHT LENS COMMON TO LAV B WALL IAW AMM 33-51-01-960-801; [0 - [SDR SWAA2025060275272](https://openairdocs.org/sdr/SWAA2025060275272), May 26, 2025: LENS. DAMAGED. AFT LAV EMERGENCY EXIT LIGHT LENS DAMAGED<[01] REPLACED AFT LAV EMERGENCY EXIT LIGHT LENS IAW AMM 33-51-01-960-801;[02] EDIT: REPLACED AFT LAV EMERGENCY EXIT LI - [SDR SWAA2025060275274](https://openairdocs.org/sdr/SWAA2025060275274), May 26, 2025: BATTERY PACK. INOPERATIVE. EMERGENCY EXIT LIGHTS IN-OP AT FWD ENTRY LOWERED CEILING CLOSEOUT PANEL AND FSD HEADER PANEL<[01] UPON INVESTIGATION; IT WAS FOUND THAT THE EMERGENCY BATTERY PA - [SDR SWAA2025060274754](https://openairdocs.org/sdr/SWAA2025060274754), May 25, 2025: BATTERY PACK. INOPERATIVE. ALL ASSOCIATED LIGHTS OF EMERGENCY BATTERY PACK M1675 ARE INOP<[01] REMOVED; REPLACED AND GOOD TEST FOR EMERGENCY BATTERY PACK M1675 PER AMM 33-51-06-960-806.;[ - [SDR SWAA2025060274755](https://openairdocs.org/sdr/SWAA2025060274755), May 25, 2025: BATTERY PACK. INOPERATIVE. ALL ASSOCIATED LIGHTS FOR EMERGENCY BATTERY PACK M1673 ARE INOP<[01] REMOVED; REPLACED AND GOOD TEST PERFORMED FOR EMERGENCY BATTERY PACK M1673 PER AMM 33-51-06 - [SDR SWAA2025060274756](https://openairdocs.org/sdr/SWAA2025060274756), May 25, 2025: BATTERY PACK. INOPERATIVE. ALL ASSOCIATED LIGHTS FOR EMERGENCY BATTERY PACK M1699 ARE INOP<[01] REMOVED; REPLACED AND GOOD TEST FOR EMERGENCY BATTERY PACK M1699 PER AMM 33-51-06-960-806.; - [SDR SWAA2025060270103](https://openairdocs.org/sdr/SWAA2025060270103), May 12, 2025: STRINGER CLIP. CRACKED. CRACKED STR CLIP AT PAX CABIN BS727A S-6R. MARKED<[01] REMOVED AND REPLACED STRINGER CLIP PER SRM 51-40-02 AND DWG# 146A1101 REV: E; SHT 1.;[02] VERIFIED CORREC - [SDR SWAA2025060270104](https://openairdocs.org/sdr/SWAA2025060270104), May 12, 2025: STRINGER CLIP. CRACKED. CRACKED STR CLIP AT PAX CABIN BS727D S-4R. MARKED<[01] REMOVED AND REPLACED STRINGER CLIP PER SRM 51-40-02 AND DWG# 146A1111 REV: C SHT 1.;[02] VERIFIED CORRECT - [SDR SWAA2025060270105](https://openairdocs.org/sdr/SWAA2025060270105), May 12, 2025: STRINGER CLIP. CRACKED. CRACKED STR CLIP AT PAX CABIN BS727E S-5R. MARKED<[01] REMOVED AND REPLACED STRINGER CLIP PER SRM 51-40-02 AND DWG# 146A1112 REV: C SHT 1.;[02] VERIFIED CORRECT - [SDR SWAA2025060267940](https://openairdocs.org/sdr/SWAA2025060267940), May 6, 2025: SEAT TRACK. CORRODED. CORROSION ON TOP OF PAX CABIN SEAT TRACK FROM STA 500B TO STA 520 LBL 45 WL 208 MARKED.<[01] REMOVED DAMAGED PART OF THE SEAT TRACK SECTION AT BS500C+10-BS520 L - [SDR SWAA2025060266270](https://openairdocs.org/sdr/SWAA2025060266270), May 1, 2025: SHIELD. CORRODED. CORROSION FWD CARGO BAY AFT SHIELD BS500+1 TO BS500+19 RBL22 WL156 HAS MULTIPLE AREAS AROUND NUT PLATE HOLES<[01] REMOVED AND REPLACED FWD CARGO BAY AFT SHIELD - [SDR SWAA2025060266271](https://openairdocs.org/sdr/SWAA2025060266271), May 1, 2025: SHIELD. CORRODED. CORROSION AFT CARGO BAY SHIELD FWD OF CARGO DOOR AROUND MULTIPLE NUT PLATE HOLES BS767+3 TO BS794 RBL22 WL156<[01] REMOVED AND REPLACED AFT CARGO BAY SHIELD FWD - [SDR SWAA2025060266269](https://openairdocs.org/sdr/SWAA2025060266269), May 1, 2025: SUPPORT PLATE. CORRODED. CORROSION AFT CARGO BAY L/H FLOOR TO SIDEWALL SUPPORT PLATE MULTIPLE AREAS AROUND NUT PLATE HOLES BS727B TO BS767 LBL22 WL156<[01] REMOVED AND REPLACED L/H FLOO - [SDR SWAA2025060266272](https://openairdocs.org/sdr/SWAA2025060266272), May 1, 2025: SUPPORT PLATE. CORRODED. CORROSION AFT CARGO BAY R/H FLOOR TO SIDEWALL SUPPORT PLATE MULTIPLE AREAS AROUND NUT PLATE HOLES BS727B TO BS767 RBL22 WL156 CORRECTION FAULT DESCRIPTION SHOUL - [SDR SWAA2025060266273](https://openairdocs.org/sdr/SWAA2025060266273), May 1, 2025: STRAP. CORRODED. CORROSION AFT CARGO BAY FLOOR SPLICE STRAP AROUND NUT PLATE HOLE BS727D+6' RBL11.5 WL156<[01] RECEIVED NEW SERVICEABLE STRAP ON SWA P.O. 1018211/1; NEW STRAP WI - [SDR SWAA2025060266403](https://openairdocs.org/sdr/SWAA2025060266403), May 1, 2025: ATTACH ANGLE. CRACKED. CRACK ATTACHED ANGLE AT THE MID CABIN BS 717 RBL 3<[01] UPDATED STEP 2.;[02] REMOVED AND REPLACED WITH NEW CRACK ATTACHED ANGLE AT THE MID CABIN BS 717 RBL 3. H - [SDR SWAA2025060266404](https://openairdocs.org/sdr/SWAA2025060266404), May 1, 2025: FLOORBEAM. CRACKED. CRACK PANEL BREAK AT THE MID CABIN BS 540 LBL 1<[01] REMOVED AND REPLACED PANEL BREAK AT BS 540; BL0-LBL24 IAW SRM 51-40-02-0G-0 AND DWG 143A0060;[02] COMPLETE - [SDR SWAA2025060266007](https://openairdocs.org/sdr/SWAA2025060266007), Apr 30, 2025: PRESSURE DECK. CRACKED. CRACK FOUND ON HORIZONTAL PRESSURE DECK AT MID PASSENGER CABIN BS663+2 RBL 41 L: 0.35' MARKED<[01] REMOVED DAMAGE PART OF THE BEADED PRESSURE DECK WEB BS663.75- - [SDR SWAA2025060265671](https://openairdocs.org/sdr/SWAA2025060265671), Apr 29, 2025: FLOOR PANEL. DELAMINATED. CABIN FLOOR PANEL 241AF TOP SURFACE IS DELAMINATED.<[01] DUE TO THE EXTENT OF DAMAGE; FABRICATED NEW FLOOR PANEL 241AF IAW SRM 53-00-50-2R-0 AND BOEING DWG 144A - [SDR SWAA2025060265672](https://openairdocs.org/sdr/SWAA2025060265672), Apr 29, 2025: FLOOR PANEL. DELAMINATED. CABIN FLOOR PANEL 231XF HAS DELAMINATED TOP SURFACE.<[01] DUE TO THE EXTENT OF DAMAGE; REPLACED CABIN FLOOR PANEL 231XF IAW SRM 53-00-50-2R-0 AND BOEING DWG 144 - [SDR SWAA2025052965670](https://openairdocs.org/sdr/SWAA2025052965670), Apr 29, 2025: FLOOR PANEL. DELAMINATED. CABIN FLOOR PANEL 241DF TOP SURFACE IS DELAMINATED. CABIN FLOOR PANEL 241DF TOP SURFACE WITH DELAMINATIONS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 5 - [SDR SWAA2024030760182](https://openairdocs.org/sdr/SWAA2024030760182), Mar 7, 2024: SLIDE. UNSECURE. R2 SERVICE DOOR ESCAPE SLIDE NOT SECURED.<[01] RESECURED R2 FWD SERVICE DOOR SLIDE IAW M/M 25-66-01. - [SDR SWAA2024022655129](https://openairdocs.org/sdr/SWAA2024022655129), Feb 22, 2024: COVER. MISSING. AFT F/A EMERGENCY LIGHT SWITCH COVER MISSING<[01] OK TO CONTINUE PER MEL 25-10-01 SP-1B AUTH 181023;[02] R&R AFT ATTENDANT CONTROL PANEL IAW AMM 25-25-11. OPS C - [SDR SWAA2024020950634](https://openairdocs.org/sdr/SWAA2024020950634), Feb 9, 2024: LENS. MISSING. ROW 11ABC SIDEWALL EMERGENCY EXIT LIGHT LENSE MISSING<[01] REINSTALLED ROW 11ABC SIDEWALL EMERGENCY EXIT LIGHT PER AMM 33-51-01 - [SDR SWAA2023060957063](https://openairdocs.org/sdr/SWAA2023060957063), Jun 8, 2023: LIGHT. INOPERATIVE. R/H OVERWING EXIT SIDEWALL LIGHT INOP.<[01] RELAMPED PER AMM 33-51-01 - [SDR SWAA2023060957065](https://openairdocs.org/sdr/SWAA2023060957065), Jun 8, 2023: LIGHT. INOPERATIVE. L/H AND R/H OVERWING EXIT FWD EMERGENCY LIGHTS INOP<[01] RELAMPED PER AMM 33-51-01 - [SDR SWAA2023052642877](https://openairdocs.org/sdr/SWAA2023052642877), Apr 28, 2023: ANGLE. CRACKED. CRACK ANGLE LOCATED BS727B AT LEVEL STR18L AFT CARGO COMPARTMENT 2023-282723<[01] INSPECTION REJECT IN STEP 2
SEE TTG8Q00L0ECA;[02] TOOL USED: EDDY CURRENT E - [SDR SWAA2023052642496](https://openairdocs.org/sdr/SWAA2023052642496), Apr 28, 2023: RIB. CRACKED. CRACK ON INSPAR RIB LOCATED AT STAB STA 120.30 AND 1 INCH FROM FRONT SPAR AT UPPER CHORD FLANGE RT HORIZONTAL STABILIZER. 2023-282721<[01] TOOL USED PN:NORTEC 6 - [SDR SWAA2023053042204](https://openairdocs.org/sdr/SWAA2023053042204), Apr 27, 2023: PLATE. CRACKED. CRACK CORRUGATED PLATE TRAILING EDGE IRSS 230 RT WING 2023-282698<[01] REPLACED CORRUGATED PLATE LOC. TRAILING EDGE IRSS 230 RT WING I.A.W B737-700 SRM 51-40-02 - [SDR SWAA2023053042205](https://openairdocs.org/sdr/SWAA2023053042205), Apr 27, 2023: PLATE. CRACKED. CRACK CORRUGATED PLATE TRAILING EDGE ORSS 272 RT WING 2023-282699<[01] REPLACED CORRUGATED PLATE TRAILING EDGE ORSS 272 RT WING IAW B737-700 SRM 51-40-02 AND DW - [SDR SWAA2023053042206](https://openairdocs.org/sdr/SWAA2023053042206), Apr 27, 2023: PLATE. CRACKED. CRACK CORRUGATED PLATE TRAILING EDGE ORSS 272 LT WING 2023-282701<[01] REPLACED CORRUGATED PLATE TRAILING EDGE ORSS 272 RT WING IAW B737-700 SRM 51-40-02 AND DW - [SDR SWAA2023053042207](https://openairdocs.org/sdr/SWAA2023053042207), Apr 27, 2023: PLATE. CRACKED. CRACK CORRUGATED PLATE TRAILING EDGE IRSS 216 LT WING 2023-282700<[01] REPLACED CORRUGATED PLATE TRAILING EDGE IRSS 216 LT WING IAW B737-700 SRM 51-40-02 AND DW - [SDR SWAA2023052542201](https://openairdocs.org/sdr/SWAA2023052542201), Apr 27, 2023: ANGLE. CRACKED. CRACK ANGLE LOCATED BS291.5 TO BS294.5 AND RBL53 WL208.1 AT PASSENGER CABIN 2023-282695<[01] REPLACED ANGLE LOCATED BS291.5 TO BS294.5 AND RBL53 WL208.1 AT PASS - [SDR SWAA2023052542202](https://openairdocs.org/sdr/SWAA2023052542202), Apr 27, 2023: STRINGER. CRACKED. CRACK INNER CHORD LOCATED BS303.9 AND LBL53 WL208.1 AT FWD GALLEY AREA 2023-282697<[01] REPLACED INNER CHORD LOCATED BTW BS270 AND BS360 WL208.1 AT FWD GALLEY A - [SDR SWAA2023053041924](https://openairdocs.org/sdr/SWAA2023053041924), Apr 26, 2023: RIB. CRACKED. CRACK INSPAR RIB 5 STA129.50 LOCATED AT 2ND VERTICAL STIFFENER AT LT HORIZONTAL STABILIZER 2023-282678<[01] EDDY CURRENT EQUIPMENT USED P/N: NORTEC 600D; S/N: 2 - [SDR SWAA2023053041926](https://openairdocs.org/sdr/SWAA2023053041926), Apr 26, 2023: ANGLE. CRACKED. CRACK SUPPORT ANGLE LOCATED BS1016 AT LEVEL STR2L AT VERTICAL STABILIZER 2023-282677<[01] REPLACED SUPPORT ANGLE AND FASTENERS LOCATED BS1016 AT LEVEL STR2L AT - [SDR SWAA2023052641363](https://openairdocs.org/sdr/SWAA2023052641363), Apr 26, 2023: SCUFF PLATE. CRACKED. CRACK FWD CORNER SCUFF PLATE LOCATED AT FWD CARGO COMPARTMENT 2023- 282649<[01] TOOL USED DIGITAL CALIPER P/N:700-113-10;S/N:0013226;DUE DATE:08-JAN-24.;[02] RE - [SDR SWAA2023052641362](https://openairdocs.org/sdr/SWAA2023052641362), Apr 26, 2023: SCUFF PLATE. CRACKED. CRACK SCUFF PLATE AFT CORNER LOCATED AT AFT CARGO COMPARTMENT 2023-282650<[01] TOOL USED DIGITAL CALIPER P/N:700-113-10;S/N:0013226;DUE DATE:08-JAN-24.;[02] REP - [SDR SWAA2023052641364](https://openairdocs.org/sdr/SWAA2023052641364), Apr 26, 2023: SCUFF PLATE. CRACKED. CRACK CENTER SCUFF PLATE LOCATED AT AFT CARGO COMPARTMENT 2023-282651<[01] TOOL USED DIGITAL CALIPER P/N:700-113-10;S/N:0013226;DUE DATE:08-JAN-24.;[02] TOOL US - [SDR SWAA2023052541928](https://openairdocs.org/sdr/SWAA2023052541928), Apr 26, 2023: COVER. DETERIORATED. DETERIORATED LAVATORY A EMERGENCY EXIT COVER AT FWD GALLEY AREA 2023-282669<[01] REPLACED LAVATORY A EMERGENCY EXIT COVER AT FWD GALLEY AREA IAW B737-700 AMM 33 - [SDR SWAA2023053041356](https://openairdocs.org/sdr/SWAA2023053041356), Apr 25, 2023: BRACKET. CRACKED. CRACK REAR SPAR BRACKET LOC ORSS 273 AFT POSITION AT RT WING 2023-282640<[01] REPLACED BRACKET LOC ORSS 273 AFT POSITION AT RT WING.IAW B737-700 SRM 51-40-02 AN - [SDR SWAA2023053041358](https://openairdocs.org/sdr/SWAA2023053041358), Apr 25, 2023: BRACKET. CRACKED. CRACK REAR SPAR BRACKET LOC ORSS 273 FWD POSITION AT RT WING 2023-282643<[01] REPLACED REAR SPAR BRACKET AND FASTENER LOC ORSS 273 FWD POSITION AT RT WING IAW B - [SDR SWAA2023052641361](https://openairdocs.org/sdr/SWAA2023052641361), Apr 25, 2023: CARGO TRACK. CRACKED. CRACK ON CARGO TRACK LOCATED LBL 17.24 BS 727E AT AFT CARGO COMPARTMENT 2023-282645<[01] TOOL USED EDDY CURRENT EQUIPMENT P/N NORTEC 600D; S/N 60009161631 DUE D - [SDR SWAA2023052641359](https://openairdocs.org/sdr/SWAA2023052641359), Apr 25, 2023: CARGO TRACK. CRACKED. CRACK ON CARGO TRACK LOCATED RBL 13.84 BS 727E AT AFT CARGO COMPARTMENT 2023-282646<[01] TOOL USED EDDY CURRENT EQUIPMENT P/N NORTEC 600D; S/N 60009161631 DUE D All 184: https://openairdocs.org/aircraft/N7860A/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 N7860A The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N7860A before. - [Cancelled 1957-02-28](https://openairdocs.org/deregistered/N7860A-1957-02-28): Cessna 180A, S/N 32757. 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 --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.