# N246LV: 2006 Boeing 737-7H4

- Status: Valid registration
- Airframe: [Boeing 737-7H4](https://openairdocs.org/model/boeing-737-7h4) (registry code 1384404, 143 seats)
- Engine: [CFM International CFM56-7B24 series](https://openairdocs.org/engine/cfm-international-cfm56-7b24-series) (registry code 13044)
- Data sheets: [TCDS A16WE](https://openairdocs.org/tcds/A16WE) (The Boeing Company) (OpenAirDocs)
- Serial number: 32507
- Year built: 2006
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: June 30, 2006
- Certificate issued: August 17, 2006
- Expires: February 29, 2028
- Mode S code: A24757
- 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=246LV
- Page: https://openairdocs.org/aircraft/N246LV

From the FAA registry file of October 24, 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 737-7H4)

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 N246LV.

## FAA accident and incident reports

None matched to N246LV.

## Service difficulty reports (322, 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 SWAA2026081857572](https://openairdocs.org/sdr/SWAA2026081857572), Aug 7, 2026: VAPOR BARRIER. CRACKED. CRACK FOUND IN BS 639 L/H STUB BEAM STRAPS AFT FASTENER HOLE DURING NDI INSPECTION, ENGINEERING REQUIRED CRACK FOUND IN BS 639 L/H STUB BEAM STRAPS AFT FASTENER
- [SDR SWAA2026070216974](https://openairdocs.org/sdr/SWAA2026070216974), Jun 28, 2026: CABLE. DISCONNECTED. SEAT 15C, EMERGENCY EXIT ROW WILL NOT STAY UPRIGHT. SEAT SECURED UPRIGHT POSITION OK TO CONTINUE PER MEL 25-6-01 SP1B AUTH 326674. RECONNECTED RECLINE CABLE FOR
- [SDR SWAA2026030973597](https://openairdocs.org/sdr/SWAA2026030973597), Feb 24, 2026: STIFFENER. CRACKED. LEFT HORIZONTAL STAB RIB NR 4, HSS 120, STIFFENER NR 4 LOWER RADIUS CRACKED. REPAIRED IAW SRM 55-10-09-2R-4, REPAIR 4 ON THE LT HORIZONTAL STAB RIB NR 4, STIFFE
- [SDR SWAA2026031172744](https://openairdocs.org/sdr/SWAA2026031172744), Feb 20, 2026: FLOOR PANEL. PULLED. FLOOR PANEL 231XF UPPER SKIN HAS MULTIPLE AREAS OF PULLED STRANDS. FABRICATION OF NEW 231XF FLOOR PANEL REPLACEMENT HAS BEEN ACCOMPLISHED IAW SRM 53-00-50-2R-0.
- [SDR SWAA2026031072038](https://openairdocs.org/sdr/SWAA2026031072038), Feb 19, 2026: MEGAPHONE. DAMAGED. AFT MEGAPHONE HANDLE FASTENER STRIPPED. TASK CARD COMPLETED, REPLACED AFT MEGAPHONE IAW AMM USE OF STANDARD INDUSTRY PRACTICES OPS CHECK GOOD.
- [SDR SWAA2026031072301](https://openairdocs.org/sdr/SWAA2026031072301), Feb 19, 2026: LIGHT. DAMAGED. G1 EMERGENCY EXIT LIGHT DAMAGED. REMOVED AND REPLACED G1 EMERGENCY EXIT LIGHT IAW AMM 33-51-01-960-802..
- [SDR SWAA2026031072039](https://openairdocs.org/sdr/SWAA2026031072039), Feb 19, 2026: BRACKET. CRACKED. PANEL 551GB INBD BRACKET CRACKED. THE BRACKET WAS REMOVED FROM PANEL 551GB IAW SRM 51-40-02-0G-0. INSTALLED A NEW BRACKET IAW SRM 51-40-02-0G-0.
- [SDR SWAA2026030972037](https://openairdocs.org/sdr/SWAA2026030972037), Feb 18, 2026: DIFFUSER. MISSING. CEILING PANEL EXIT LIGHT ASSY FOR OVERWING EXITS IS MISSING DIFFUSER ATTACH CLIP. REMOVED AND REPLACED CEILING PANEL EXIT LIGHT ASSY FOR OVERWING EXITS IAW AMM 
- [SDR SWAA2026031171727](https://openairdocs.org/sdr/SWAA2026031171727), Feb 17, 2026: LIGHT. BROKEN. LAVATORY A, CENTER FWD LOWER CEILING EXIT LIGHT ASSY HAS BROKEN TABS. REMOVED AND REPLACED THE LIGHT ASSY IAW AMM 33-51-01-960-802 STEP 3. C. (6).
- [SDR SWAA2026031069610](https://openairdocs.org/sdr/SWAA2026031069610), Feb 11, 2026: STRINGER CLIP. CRACKED. CRACKED STRINGER CLIP 2L AT BS 686. FABRICATED AND INSTALLED A NEW STRINGER CLIP IAW SRM 51-40-02-0G-0, & DWG 144A1106, REV A.
- [SDR SWAA2026031069611](https://openairdocs.org/sdr/SWAA2026031069611), Feb 11, 2026: STRINGER CLIP. CRACKED. CRACKED STRINGER CLIP, BS 706, S6L.. FABRICATED AND INSTALLED A NEW STRINGER CLIP IAW SRM 51-40-02-0G-0, & DWG 144A1107, REV A.
- [SDR SWAA2026030969606](https://openairdocs.org/sdr/SWAA2026030969606), Feb 11, 2026: STIFFENER. CRACKED. LEFT HORIZONTAL STAB RIB #4 (STAB STA 120) STIFFENER #2 LOWER RADIUS IS CRACKED.<[01] REPAIRED IAW SRM 55-10-09-2R-5 REPAIR 5<BR>L/H H. STAB RIB #4 STIFFENER #2
- [SDR SWAA2026031068185](https://openairdocs.org/sdr/SWAA2026031068185), Feb 6, 2026: COVER. CRACKED. RIGHT ELEVATOR LOWER INBD HINGE COVER PANEL 344GB CRACKED. NEW PANEL 344GB WILL BE IMSTALLED ON TTG8Q01A3LE5 IAW AMM 20-50-11-910-801.
- [SDR SWAA2026031168018](https://openairdocs.org/sdr/SWAA2026031168018), Feb 5, 2026: SHIELD. CORRODED. CORRODED FWD CARGO FWD SHIELD, BS 420+1 - 420+19, RBL 22, WL 156 HAD MULTIPLE AREAS AROUND NUT PLATE HOLES. REMOVED AND REPLACED THE SHIELD IAW SRM 51-40-02, & 
- [SDR SWAA2026031068180](https://openairdocs.org/sdr/SWAA2026031068180), Feb 5, 2026: SCUFF PLATE. CRACKED. FWD SERVICE DOOR SCUFF PLATE CRACKED ON THE AFT EDGE. REMOVED THE COATINGS AND UNWANTED MATERIALS FROM THE SCUFF PLATE BEFORE WELDING IAW SRM 53-10-15-2R-2, STE
- [SDR SWAA2026030968179](https://openairdocs.org/sdr/SWAA2026030968179), Feb 5, 2026: STRINGER. CORRODED. CORROSION ON STRINGER AT AREA AFT OF FWD CARGO BAY BS535 S-25R WL153 APROX. REPAIRED PER EA 26-153-00361. THIS IS A CATEGORY A REPAIR AS DEFINED IN 737-700 SRM 
- [SDR SWAA2026030968017](https://openairdocs.org/sdr/SWAA2026030968017), Feb 5, 2026: SHIELD. CORRODED. CORROSION AFT CARGO BAY SHIELD FWD OF CARGO DOOR AROUND MULTIPLE NUT PLATE HOLES BS 767+3 TO BS 794, RBL 22, WL 156. REMOVED AND REPLACED THE SHIELD IAW SRM 51-
- [SDR SWAA2026031067601](https://openairdocs.org/sdr/SWAA2026031067601), Feb 4, 2026: SEAT TRACK. CORRODED. CORROSION ON SEAT TRACK, LBL 45, BS 480+11 TOP, BS 500+6 TOP, BS 500B WELL, 500D+15 TOP, & 500D+15 WELL, WL 208. THE SEAT TRACK WILL BE REPLACED ON TASK CARD TT
- [SDR SWAA2026031067602](https://openairdocs.org/sdr/SWAA2026031067602), Feb 4, 2026: SEAT TRACK. CORRODED. CORROSION ON SEAT TRACK LBL 25, BS 500+7 TOP, BS 500B+2 TOP, BS 500A+18 TOP, BS 500C+11 TOP, BS 500D+15, WELL, WL 208. THE SEAT TRACK TO BE REPLACED ON CCN TTG8
- [SDR SWAA2026031067808](https://openairdocs.org/sdr/SWAA2026031067808), Feb 4, 2026: SEAT TRACK. CORRODED. CORROSION ON PAX CABIN SEAT TRACK, RBL 25, BS 578+16 TOP, BS 663+18 WELL, BS 683+3 TOP, BS 708+8 WELL, BS 727A+8 TOP, WL 208. REMOVED CORROSION ON SEAT TRACK IA
- [SDR SWAA2026031167430](https://openairdocs.org/sdr/SWAA2026031167430), Feb 3, 2026: SCUFF PLATE. CRACKED. AFT CARGO BAY FWD CORNER SCUFF PLATE IS CRACKED. AFT CARGO BAY FWD CORNER SCUFF PLATE REPAIRED IAW SRM 53-60-15-2R-1.
- [SDR SWAA2026031067085](https://openairdocs.org/sdr/SWAA2026031067085), Feb 3, 2026: DOUBLER. CORRODED. LAV SERVICE DOOR HAS CORROSION ON EXTERIOR SURFACE ON PREVIOUS REPAIR DOUBLER. REMOVED AND REPLACED LAV SERVICE DOOR IAW AMM 52-49-07-000-801; AMM 52-49-07-400-
- [SDR SWAA2026031067429](https://openairdocs.org/sdr/SWAA2026031067429), Feb 3, 2026: SCUFF PLATE. CRACKED. AFT CARGO BAY AFT CORNER SCUFF PLATE IS CRACKED. AFT CARGO BAY AFT CORNER SCUFF PLATE REPAIRED IAW SRM 53-60-15-2R-1.
- [SDR SWAA2026031067437](https://openairdocs.org/sdr/SWAA2026031067437), Feb 3, 2026: BEAR STRAP. CRACKED. CRACK NOTED ON R1 DOOR BEAR STRAP AROUND FASTENER, L: 0.3, BS 291.5+4, BETWEEN S8R - 9R, WL 265. REPAIRED IAW SRM 53-10-01-2R-6, AND EA M-25-153-01539.
- [SDR SWAA2026031067041](https://openairdocs.org/sdr/SWAA2026031067041), Feb 2, 2026: DOUBLER. CRACKED. EGPR SURROUND DOUBLER IS CRACKED BS 233, WL 175, 8 INCHES ABOVE S24R. CRACK WAS FOUND TO BE OUT OF LIMITS IAW SRM 53-10-15-1A-5. TRIMMED OUT THE DAMAGED AREA OF
- [SDR SWAA2026030967042](https://openairdocs.org/sdr/SWAA2026030967042), Feb 2, 2026: BATTERY PACK. NO TEST. EMERGENCY BATTERY PACK M1670 FAILS CAPACITANCE TEST. REMOVED, REPLACED, AND PERFORMED GOOD TEST OF EMERGENCY BATTERY PACK M1670 IAW AMM 33-51-06-960-805.
- [SDR SWAA2026030967046](https://openairdocs.org/sdr/SWAA2026030967046), Feb 2, 2026: BATTERY PACK. FAILED. EMERGENCY BATTERY PACK M1669 FAILS CAPACITANCE TEST. REMOVED AND REPLACED EMERGENCY BATTERY PACK M1669, OPS CHECK PERFORMED, GOOD FOR SERVICE IAW AMM 33-51-06-9
- [SDR SWAA2026010859138](https://openairdocs.org/sdr/SWAA2026010859138), Jan 6, 2026: ENGINE. DAMAGED. AFTER TAKE OFF AT ABOUT 800 FEET BIRD STRIKE NR 1 ENGINE SMELLED IN THE CABIN / FLIGHT DECK. NR 1 ENGINE 100 DEGREES HOTTER, REF LOG PAGE 2953324 FOR ACCOMPLISH
- [SDR SWAA2026010557431](https://openairdocs.org/sdr/SWAA2026010557431), Jan 1, 2026: SLIDE. DISLODGED. R2 DOOR SLIDE FELL OUT OF BOX. REPACKED AFT SERVICE DOOR SLIDE IAW MT 725-61-06. AC OK FOR SERVICE
- [SDR SWAA2025120442190](https://openairdocs.org/sdr/SWAA2025120442190), Dec 3, 2025: FASTENER. MISSING. FWD SERVICE DOOR SLIDE COMPARTMENT GIRT BAR RETAINER MISSING FASTNER. INSTALLED THE FASTENER IAW SRM 51-40-02
- [SDR SWAA2025112639309](https://openairdocs.org/sdr/SWAA2025112639309), Nov 23, 2025: GIRT BAR. DETACHED. BRACKET FOR GIRT BAR DETACHED FROM EMERGENCY SLIDE COVER. PERFORMED MX TASK 725-61-06 REM/INST AND PERFORMED EA M-23-125-01839 AND INSTALLED THREADED FASTNER/NU
- [SDR SWAA2025092216225](https://openairdocs.org/sdr/SWAA2025092216225), Sep 19, 2025: SPRING. UNSECURE. AFT F/A EMERGENCY EXIT LIGHT SWITCH COVER SPRING INOPERATIVE. SECURED AFT F/A EMERGENCY EXIT LIGHT SWITCH COVER SPRING IAW AMM SIP.
- [SDR SWAA2025070788513](https://openairdocs.org/sdr/SWAA2025070788513), Jul 5, 2025: CIRCUIT BREAKER. TRIPPED. CIRCUIT BREAKER P18-3 B10 FOUND POPPED ON PREFLIGHT LIGHTING EMERGENCY CHGR<[01] PERFORMED FILM 33-50 TASK 801 RESET C/B & EMERGENCY LIGHTS OPS CHECK OK @ THIS 
- [SDR SWAA2025060678633](https://openairdocs.org/sdr/SWAA2025060678633), Jun 5, 2025: APU. FAILED. DRIVE #2 LIGHT CAME ON DURING LANDING MX VERIFIED APU OIL QTY IS FULL 22-APR-2025 14:21 UTC FAULT: FLIGHT CREW REPORTS #2 ENG DRIVE LIGHT TEMPORARILY ILLUMINATE
- [SDR SWAA2025052273416](https://openairdocs.org/sdr/SWAA2025052273416), May 20, 2025: BRACKET. BENT. AFT ENTRY DOOR GIRT BAR BRACKET (ON DOOR) BENT <[01]. ADJUSTED GIRT BAR HOLD BRACKET PER S.I.P.
- [SDR SWAA2024072515996](https://openairdocs.org/sdr/SWAA2024072515996), Jul 24, 2024: ISOLATOR. BROKEN. FWD SERVICE DOOR SLIDE AFT TOP ISOLATOR BRACKET IS BROKEN.<[01] R&R FWD SERVICE DOOR SLIDE AFT TOP ISOLATOR IAW SRM 51-40-02;
- [SDR SWAA2024062104244](https://openairdocs.org/sdr/SWAA2024062104244), Jun 20, 2024: LAMP. BURNED OUT. FWD GALLEY CEILING LIGHT BURNED OUT<[01] RELAMPED FWD GALLEY CEILING LT (SERV. DOOR SIDE) PER AMM 33-26-02.
- [SDR SWAA2024041875954](https://openairdocs.org/sdr/SWAA2024041875954), Apr 17, 2024: GIRT BAR. LOOSE. FWD SERVICE DOOR GIRT BAR IS LOOSE IN ITS HOLDER<[01] 04 - REPAIRED PER [AMM 25-66-00-201-NG (DOOR-MOUNTED ESCAPE SYSTEM - MAINTENANCE PRACTICES - PERMANENT)] T
- [SDR SWAA2024041875908](https://openairdocs.org/sdr/SWAA2024041875908), Apr 17, 2024: LAMP. INOPERATIVE. EXTERIOR EMERGENCY DOOR LIGHT BY THE L2 DOOR IS INOP. RELAMPED EXTERIOR EMERGENCY DOOR LIGHT BY THE L2 DOOR. OPS CHECK IS GOOD. REF. AMM 33-51-03
- [SDR SWAA2024031354985](https://openairdocs.org/sdr/SWAA2024031354985), Feb 23, 2024: PANEL. CRACKED. CRACK ENTRY DOOR SUPPORT ANGLE PANEL AT AFT GALLEY AREA (1 EA) 2024 123501<[01] REPLACED DOOR SUPPORT ANGLE PANEL AT AFT GALLEY AREA (1 EA) I.A.W B737-700 SRM 5
- [SDR SWAA2024031255489](https://openairdocs.org/sdr/SWAA2024031255489), Feb 23, 2024: LIGHT. DETERIORATED. DETERIORATED PHOTOLUMINESCENT STRIP AT PASSENGER CABIN (10EA) 2024-123518<[01] REPLACED PHOTOLUMINESCENT STRIP AT PASSENGER CABIN I.A.W B737-700 AMM 33-51-15-40
- [SDR SWAA2024031454029](https://openairdocs.org/sdr/SWAA2024031454029), Feb 20, 2024: ANGLE. CRACKED. CRACK ANGLE LOCATED BS867 AND STR26L AFT CARGO COMPARTMENT 2024-123445<[01] REPLACED ANGLE AND FASTENERS LOCATED BS867 AND STR26L AFT CARGO COMPARTMENT IAW B737
- [SDR SWAA2024031454031](https://openairdocs.org/sdr/SWAA2024031454031), Feb 20, 2024: INTERCOSTAL. CORRODED. CORROSION WEB - INTERCOSTAL LOCATED BTW BS767 TO BS794.3 WL156 AND RBL 21.83 AFT CARGO COMPARTMENT 2024-123447<[01] REPLACED WEB - INTERCOSTAL LOCATED BTW BS 76
- [SDR SWAA2024031454032](https://openairdocs.org/sdr/SWAA2024031454032), Feb 20, 2024: ANGLE. CORRODED. CORROSION ANGLE LOCATED BTW BS767 TO BS794.3 WL156 AND RBL21.83 AFT CARGO COMPARTMENT 2024-123448<[01] REPLACED ANGLE LOCATED BTW BS767 TO BS794.3 WL156 AND RBL
- [SDR SWAA2024031254028](https://openairdocs.org/sdr/SWAA2024031254028), Feb 20, 2024: SUPPORT. CORRODED. CORROSION SUPPORT ZEE LOCATED BTW BS727B TO BS787 LBL 21.83 WL 156.5 AFT CARGO COMPARTMENT 2024-123450<[01] TOOL USED: ULTRASONIC THICKNESS GAUGE; PN: 45MG; SN:
- [SDR SWAA2024031453829](https://openairdocs.org/sdr/SWAA2024031453829), Feb 19, 2024: ANGLE. CRACKED. CRACK ANGLE LOCATED BTW BS 907 TO BS 927 AND BTW STR25R TO STR27R AFT POSITIO AT AFT CARGO COMPARTMENT 2024-123422<[01] REPLACED ANGLE LOCATED BTW BS 907 TO BS 
- [SDR SWAA2024031453828](https://openairdocs.org/sdr/SWAA2024031453828), Feb 19, 2024: ANGLE. CRACKED. CRACK ANGLE LOCATED BTW BS907 TO BS 927 AND BTW STR25R TO STR 27R FWD POSITION AT AFT CARGO COMPARTMENT 2024-123420<[01] REPLACED ANGLE LOCATED BTW BS907 TO BS 
- [SDR SWAA2024031453831](https://openairdocs.org/sdr/SWAA2024031453831), Feb 19, 2024: SUPPORT. CRACKED. CRACK ANGLE - SUPPORT LOCATED BS 947.5 AT LEVEL STR 26L AT AFT CARGO COMPARTMENT 2024-123424<[01] REPLACED ANGLE - SUPPORT LOCATED BS 947.5 AT LEVEL STR 26L AT 
- [SDR SWAA2024031453729](https://openairdocs.org/sdr/SWAA2024031453729), Feb 19, 2024: ANGLE. CRACKED. CRACK ANGLE BS 663.75 AND RBL 9 WL 173.5 AT CENTER WING BOX 2024-123402<[01] TOOL USED: TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 142811020 DUE DATE: 23-JAN
- [SDR SWAA2024031453733](https://openairdocs.org/sdr/SWAA2024031453733), Feb 19, 2024: BRACKET. CRACKED. CRACK SUPPORT BRACKET LOCATED BS 540 AND LBL 6 AT LT AIR CONDITIONING BAY 2024-123405<[01] REPLACED SUPPORT BRACKET LOCATED BS 540 AND LBL 6 AT LT AIR CONDITION

All 322: https://openairdocs.org/aircraft/N246LV/reports.md

## STCs that may be installed (OpenAirDocs) (32)

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 airframe (Boeing 737-7H4)

- [STC ST00555AT](https://openairdocs.org/stc/ST00555AT): Installation of Airshow 210 system. AIRCRAFT RECONFIG TECHNOLOGIES, LLC. Lists 737 Series
- [STC SA4842SW](https://openairdocs.org/stc/SA4842SW): Modification of air to air heat exchanger (P/N 182820-2 Series 2). Honeywell International Inc. Lists 737 Series
- [STC SA270NW](https://openairdocs.org/stc/SA270NW): Installation of modified seat. Aviation Technical Services. Lists 737 Series
- [STC ST01162NY](https://openairdocs.org/stc/ST01162NY): Installation of Literature Pockets. Magee Plastics Company. Lists 737 Series
- [STC SA2607SO](https://openairdocs.org/stc/SA2607SO): Installation of coffee maker P/N 416-1001-29. B/E Aerospace Inc. Lists 737 Series
- [STC SA2608SO](https://openairdocs.org/stc/SA2608SO): Installation of rail assembly, P/N 416-0201-15. B/E Aerospace Inc. Lists 737 Series
- [STC SA3058SO](https://openairdocs.org/stc/SA3058SO): Installation of coffee maker 416-0001-23 and rail assembly 416-0201-5. B/E Aerospace Inc. Lists 737 Series
- [STC ST01476AT](https://openairdocs.org/stc/ST01476AT): Installation of coffee maker. B/E Aerospace Inc. Lists 737 Series
- [STC ST01778AT](https://openairdocs.org/stc/ST01778AT): Installation of espresso maker p/n 3510-0066-01. B/E Aerospace Inc. Lists 737 Series
- [STC SA629GL](https://openairdocs.org/stc/SA629GL): Installation of Grimes galley, Model 1545LW unit 2 and unit 4. B/E Aerospace. Lists 737 Series
- [STC ST01332AT](https://openairdocs.org/stc/ST01332AT): Installation of Galley Service Carts. Champ International, Inc. Lists 737 Series
- [STC ST09870SC](https://openairdocs.org/stc/ST09870SC): Installation of Mechanical Window Shades. Lou Martin & Associates. Lists 737 Series
- [STC ST00033AT](https://openairdocs.org/stc/ST00033AT): Installation of a single Mode S system and provisions for a TCAS II system. General Aerospace, Inc. Lists 737 Series
- [STC SA4532NM](https://openairdocs.org/stc/SA4532NM): Installation of Coltech, CTD-80 ATSCALL, enabling company calling of selected aircraft via company selected radio. Avtech Corporation. Lists 737 Series
- [STC ST4532NM](https://openairdocs.org/stc/ST4532NM): Installation of Coltech CTD-80 ATSCALL, enabling company calling of selected aircraft via company selected radio. Avtech Corporation. Lists 737 Series
- [STC ST00774NY](https://openairdocs.org/stc/ST00774NY): Installation of a passenger cabin Liquor/beverage service cart P/N E500170. (757-222) (767-222) (727-222) (737 SERIES 222, 291, 322, 522) (747-100 SERIES 238B). Driessen Aircraft Interior Systems USA, Inc. Lists 737 Series
- [STC ST02052AT](https://openairdocs.org/stc/ST02052AT): Installation of a single Collins GNLU910A flight management system, along with global navigation satellite system sensor. General Aerospace, Inc. Lists 737 Series
- [STC SA02034AT](https://openairdocs.org/stc/SA02034AT): Manufacture of tray carrier, P/N 2282-506. BFE Services. Lists 737 Series
- [STC ST01968AT](https://openairdocs.org/stc/ST01968AT): Manufacture of inserts for galley stowage. JK Aerospace, Inc. Lists 737 Series
- [STC SA01916AT](https://openairdocs.org/stc/SA01916AT): Manufacture of Tray Carrier P/N 1839-501. BFE Services. Lists 737 Series
- [STC SA2534SO](https://openairdocs.org/stc/SA2534SO): Installation of window shades, acoustic panes and reveals. Magee Plastics Company. Lists 737 Series
- [STC ST179CH](https://openairdocs.org/stc/ST179CH): Installation of cargo container curtain. Plastic Composites Corp. Lists 737 Series
- [STC SA00056LA](https://openairdocs.org/stc/SA00056LA): Installation of Weber Coffeemaker, P/N 870130-415. Monogram Systems. Lists 737 Series
- [STC SA6090NM](https://openairdocs.org/stc/SA6090NM): Installation of emergency vision assurance system (EVAS). VisionSafe Corporation. Lists 737 Series
- [STC SA370NW](https://openairdocs.org/stc/SA370NW): Removal of passenger interior, installation of cargo compartment liners and cargo tie down equipment. Western Metal Products. Lists 737 Series
- [STC SA2589CE](https://openairdocs.org/stc/SA2589CE): Install Bennetts Seat Converter Stowage Compartment on passenger seat(s). John's Aircraft and Upholstery. Lists 737 Series
- [STC SA1029NW](https://openairdocs.org/stc/SA1029NW): Installation of a cargo system. Western Metal Products. Lists 737 Series
- [STC SA1258EA](https://openairdocs.org/stc/SA1258EA): Installation of Cosco model78-( ) child restraint system. (172M S/N 17263459 - 17267584). Miller Stuart R. Lists 737 Series
- [STC SA1052SO](https://openairdocs.org/stc/SA1052SO): Installation of GE battery P/N43B022RB36 in place of Marathon P/N CA-727-7, CA-727-20, or CA-27-20 batteries or SAFT P/N23180 batteries; or installation of GE battery P/N 43B020RB10 replacing Marathon P/N CA-727-7, CA-727-20 or CA-27-20 or SAFT P/N 23186 or 23180 batteries. General Electric Company. Lists 737 Series
- [STC SA1082NW](https://openairdocs.org/stc/SA1082NW) (historical): Installation of auxiliary fuel tanks in the aft cargo compartment. (737 series -2K9A). Rogerson ATS. Lists 737 Series

### 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 737-7H4 aircraft: https://openairdocs.org/model/boeing-737-7h4/aircraft.md
- The CFM International CFM56-7B24 series engine: https://openairdocs.org/engine/cfm-international-cfm56-7b24-series.md

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