# N264LV: 2007 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: 32521 - Year built: 2007 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: January 23, 2007 - Certificate issued: February 28, 2007 - Expires: September 30, 2029 - Mode S code: A28EE7 - 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=264LV - Page: https://openairdocs.org/aircraft/N264LV 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 N264LV. ## FAA accident and incident reports None matched to N264LV. ## Service difficulty reports (274, 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 SWAA2026081146248](https://openairdocs.org/sdr/SWAA2026081146248), Aug 7, 2026: LENS. LOOSE. EMERGENCY LIGHT LENS AT COCKPIT LOOSE. R & R FWD CENTERLINE EMERGENCY EXIT SIGN HOUSING IAW MM 33-51-01 - [SDR SWAA2026071696568](https://openairdocs.org/sdr/SWAA2026071696568), Jul 14, 2026: FLOOR PANEL. CRACKED. CRACKED FLOOR OF AFT CARGO BAY FLOOR PANEL.. REMOVED AFT CARGO PANEL 140 BF INSTALLED AFT CARGO FLOOR PANEL 140BF IAW AMM 25-52-10. - [SDR SWAA2026051296699](https://openairdocs.org/sdr/SWAA2026051296699), May 8, 2026: COVER. DETACHED. CABIN EMERGENCY LIGHT COVER FELL OFF UNDER 1ABC OVHD BIN. OK TO CONTINUE PER MEL 25-10-01 SP# 1B; AUTH # 318563. INSTALLED NEW EMERGENCY LIGHT COVER PER SIP. - [SDR SWAA2025110630515](https://openairdocs.org/sdr/SWAA2025110630515), Oct 31, 2025: DOUBLER. CORRODED. FOUND CORROSION ON BS 887 BUTT SPLICE INTERNAL STRAP DOUBLER UNDER FUSELAGE SKIN AFTER ACCOMPLISHING EA 25-153-02998. CORROSION MEASURES 2.50 BY 1.0 . REPAIRED - [SDR SWAA2025110630856](https://openairdocs.org/sdr/SWAA2025110630856), Oct 30, 2025: STRINGER. CORRODED. PAINT BUBBLING ON FUSELAGE AT BS 887, STRINGER L25 +3'. REPAIRED PER EA 25-153-02998. - [SDR SWAA2025110329964](https://openairdocs.org/sdr/SWAA2025110329964), Oct 30, 2025: PAN. BUCKLED. FUSELAGE TOILET SERVICE DOOR PAN, AFT LOWER CORNER IS BUCKLED. REMOVED FUSELAGE TOILET SERVICE DOOR PAN IAW SRM 51-40-02. AFTER REMOVAL OF FUSELAGE TOILET SERVI - [SDR SWAA2025090309800](https://openairdocs.org/sdr/SWAA2025090309800), Aug 30, 2025: BULB. INOPERATIVE. RH OVER WING EMERGENCY LIGHT OUT. REPLACED BULB PER AMM 33-51-04. - [SDR SWAA2025070186835](https://openairdocs.org/sdr/SWAA2025070186835), Jun 30, 2025: TAILPIPE. FIRE. #2 ENGINE TAILPIPE FIRE REPORTED. EXTINGUISHED AFTER SHUTDOWN. NO ABNORMAL ENGINE INDICATIONS<[01] INSPECTED #2 ENGINE IN REF TO AMM 71-00-00-800-803-F00. NO OI - [SDR SWAA2025062383013](https://openairdocs.org/sdr/SWAA2025062383013), Jun 19, 2025: DOOR. CRACKED. R/H MLG CTR DOOR HAS CRACK AT LWR FWD CUTOUT AT MOUNT ATTACH POINT. <[01] REMOVED R/H CTR & INNER MLG DOOR ASSEMBLY I.A.W AMM 32-13-11 OK TO CONTINUE SERVICE PE - [SDR SWAA2025041422673](https://openairdocs.org/sdr/SWAA2025041422673), Apr 8, 2025: PUMP. FAILED. #1 ENG. STUCK ON 86.0 ON CLIMB OUT AND WOULD NOT ADVANCE WITH MANUAL ADVANCE OF THRUST LEVER; POWER SETTINGS WORKED NORMAL ON RETURN TO FIELD <[01]. REPLACED #1 - [SDR SWAA2024120573909](https://openairdocs.org/sdr/SWAA2024120573909), Dec 4, 2024: LIGHT. INOPERATIVE. R1 DOOR EXTERIOR EMERGENCY LIGHT INOP<[01] RELAMPED R1 DOOR EXTERIOR EMERGENCY EXIT LIGHT PER AMM 33-51-04 - [SDR SWAA2024090532667](https://openairdocs.org/sdr/SWAA2024090532667), Sep 1, 2024: LIGHT. INOPERATIVE. AED EXTERIOR EMERGENCY EXIT LIGHT IS INOPERABLE AED EXTERIOR EMERGENCY EXIT LIGHT IS INOPERABLE<[01] RELAMPED EXTERIOR EMERGENCY EXIT LIGHT AND PERFORMED A GOOD - [SDR SWAA2024090532661](https://openairdocs.org/sdr/SWAA2024090532661), Aug 31, 2024: BATTERY PACK. INOPERATIVE. EMERGENCY LIGHTS ASSOCIATED WITH BATTERY PACK M1673 ARE INOP<[01] REMOVED; REPLACED; AND PERFORMED GOOD TEST OF M1673 PER AMM33-51-06-960-805 - [SDR SWAA2024090528299](https://openairdocs.org/sdr/SWAA2024090528299), Aug 20, 2024: FLOORBEAM. CRACKED. REJECT - FLOOR BEAM REPAIR STRAP HAS 1EA OPEN COUNTERSUNK FASTENER HOLE @ BS294; RBL-37;WL-208. REPAIR ANGLE HAS 1EA HILOK W/O COLLAR; 1EA UNDERSIZED HILOK @ BS - [SDR SWAA2024090526529](https://openairdocs.org/sdr/SWAA2024090526529), Aug 16, 2024: SUPPORT. ELONGATED. FWD CARGO BAY AFT CENTER BULKHEAD RH SUPPORT HAS 2EA ELONGATED FASTENER HOLES AT BS 500D; RBL 25; WL 157<[01] REMOVED AND REPLACED FWD CARGO BAY AFT CENTER BULK - [SDR SWAA2024090625975](https://openairdocs.org/sdr/SWAA2024090625975), Aug 14, 2024: SCUFF PLATE. CRACKED. FCB FWD CORNER SCUFF CRACKED<[01] REPAIRED THE CORNER SCUFF PLATE WITH ACCOMPLISHED STEPS 1 - 6 IAW SRM 53-30-15-2R-1. REPAIR 1.;[02] VERIFIED COMPLETION CORREC - [SDR SWAA2024090625576](https://openairdocs.org/sdr/SWAA2024090625576), Aug 13, 2024: INTERCOSTAL. CRACKED. INTERCOSTAL HAS CRACK BTW STA 294.5 & 303.9; STR 16L.<[01] REMOVED AND INSTALLED NEW INTERCOSTAL STA 294.5 & 303.9; STR 16L.IAW SRM 51-40-02 AND DWG 141A8180 RE - [SDR SWAA2024090624707](https://openairdocs.org/sdr/SWAA2024090624707), Aug 10, 2024: ANGLE. CORRODED. CORROSION ON THRESHOLD ATTATCHMENT ANGLE ATTACHED TO THE R1 DOOR MOPSILL FROM BS 294 - 328 RBL 57 WL208<[01] REMOVED AND REPLACED THRESHOLD ATTACH ANGLE; ANGLE - [SDR SWAA2024090523306](https://openairdocs.org/sdr/SWAA2024090523306), Aug 6, 2024: BEAR STRAP. CRACKED. CRACKED BEAR STRAP AT R1 DOOR JUST ABOVE SEAL DEPRESSOR; 3' BELOW FWD UPPER STOP FITTING. MARKED CORRECTION: CRACK FOUND ON FSD STUB FRAME.<[01] REMOVED AND REP - [SDR SWAA2024090523304](https://openairdocs.org/sdr/SWAA2024090523304), Aug 6, 2024: SLIDE. MISINSTALLED. AFT ENTRY DOOR SLIDE PACK NOT INSTALLED CORRECTLY.<[01] INSTALLED CORRECTLY AFT ENTRY DOOR SLIDE PACK IAW AMM 25-66-01-400-801 AND MT 725-61-06 AE ON FAULT TTG8 - [SDR SWAA2024090622032](https://openairdocs.org/sdr/SWAA2024090622032), Aug 2, 2024: SEAT TRACK. DAMAGED. MAIN CABIN SEAT TRACK MISSING A PIECE OF THE CROWN AT WL208 RBL45 BS500+7. MARKED<[01] REMOVED AND REPLACED NEW ON MAIN CABIN OF SEAT TRACK BS 480 TO BS520 RBL - [SDR SWAA2024090622033](https://openairdocs.org/sdr/SWAA2024090622033), Aug 2, 2024: SEAT TRACK. CORRODED. MAIN CABIN SEAT TRACK HAS CORROSION AT WL208 RBL45 BS500C+8<[01] THIS FAULT WILL BE ACCOMPLISHED ON CARD TTG8Q00UZBY9 (REPLACEMENT OF PART);[02] VERIFIED CORREC - [SDR SWAA2024090621613](https://openairdocs.org/sdr/SWAA2024090621613), Aug 2, 2024: PANEL. DEBONDED. PANEL 195BR OUTER SKIN IS DISBONDED NEAR AFT END. (MARKED)<[01] 195BR OUTER SKIN DISBOND DAMAGE HAS BEEN REPAIRED IAW SRM 51-70-05-2R-2.

ATTACHED CURE SH - [SDR SWAA2024090621009](https://openairdocs.org/sdr/SWAA2024090621009), Aug 1, 2024: SUPPORT BRACKET. CRACKED. WATER SERVICE PAN SUPPORT AFT BRACKET CRACKED AT BS BETWEEN 907-927 (MARKED) BRACKET IS INSIDE AFT CARGO BAY<[01] REMOVED AND REPLACED WATER SERVICE PAN SUPPORT - [SDR SWAA2024090621039](https://openairdocs.org/sdr/SWAA2024090621039), Aug 1, 2024: SHEAR WEB. CORRODED. CORROSION ON SHEAR WEB AT STA 1003+4 LBL 38; WL 208.2<[01] REFER TO FAULT TTG8Q00UYAWJ FOR REPAIR RESOLUTION;[02] REFER TO FAULT TTG8Q00UYAWJ FOR REPAIR RESOLUT - [SDR SWAA2024090621593](https://openairdocs.org/sdr/SWAA2024090621593), Aug 1, 2024: ANGLE. CRACKED. CRACKED INTERCOSTAL AT FWD WET AREA BS387 LBL13 WL208.<[01] REMOVED AND REPLACED INTERCOSTAL (ANGLE) BETWEEN BS.380 - BS400 LBL.13 WL.208.IAW B-737-700 SRM 51-4 - [SDR SWAA2024090621604](https://openairdocs.org/sdr/SWAA2024090621604), Aug 1, 2024: SHIELD. CORRODED. CORROSION ON AFT SHIELD AT FCB BS500 - BS500A RBL24 WL156. MARKED<[01] REMOVED AND REINSTALLED SHIELD IAW SRM 51-40-02
AND DWG# 143A8126 REV:-
CARD COMPLE - [SDR SWAA2024090621606](https://openairdocs.org/sdr/SWAA2024090621606), Aug 1, 2024: SUPPORT ANGLE. CORRODED. CORROSION ON AFT BULKHEAD TO SIDEWALL SUPPORT ANGLE AT FCB BS500D RBL25 WL157. MARKED<[01] VERIFIED STEP 3 IN PARTIAL.;[02] REMOVED AND REPLACED SIDEWALL SUPPOR - [SDR SWAA2024090621340](https://openairdocs.org/sdr/SWAA2024090621340), Aug 1, 2024: FLOOR SUPPORT. CORRODED. CORROSION ON FLOOR SUPPORT AT FWD WET AREA BS297; BS302 LBL11 WL208.<[01] REMOVED AND REPLACED INTERCOSTAL AT BS294.5-BS312 LBL11 IAW SRM 51-40-02 AND DWG 141A5 - [SDR SWAA2024090621041](https://openairdocs.org/sdr/SWAA2024090621041), Aug 1, 2024: STRAP. CORRODED. CORROSION ON TENESION STRAP AT STA 1016 RBL 3 AND STA 1016+6 TO 1016+14 RBL 3.<[01] REMOVE AND REPLACED AFT WET AREA TENSION STRAP P/N 147A5744-1 AT BS 1006 TO - [SDR SWAA2024090621342](https://openairdocs.org/sdr/SWAA2024090621342), Aug 1, 2024: FLOOR SUPPORT. CRACKED. CRACKED INTERCOSTAL AT FWD WET AREA BS321 LBL45 WL208.<[01] 01 - REMOVED AND REPLACED INTERCOSTAL AT FWD WET AREA BS321 LBL45 WL208 PER SRM 51-40-02.;[02] 01 - - [SDR SWAA2024090621040](https://openairdocs.org/sdr/SWAA2024090621040), Aug 1, 2024: STRAP. CORRODED. CORROSION ON TENSION STRAP AT STA 1006+1 LBL 7.7; 1006+7 LNL 4.5 STA 1016+7 LBL 2.5.<[01] REMOVED AND INSTALLED TENSION STRAP BS 1006 TO BS 1026 LBL3 IAW SRM 51 - [SDR SWAA2024090520991](https://openairdocs.org/sdr/SWAA2024090520991), Aug 1, 2024: FLOOR PANEL. PULLED. FLOOR PANEL 231FF HAS MULTIPLE AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 231FF UPPER SKIN WITH MULTIPLE AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE - [SDR SWAA2024090520993](https://openairdocs.org/sdr/SWAA2024090520993), Aug 1, 2024: FLOOR PANEL. PULLED. FLOOR PANEL 231JF HAS MULTIPLE AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 231JF WAS REPLACED BY FABRICATING A NEW PANEL IAW SRM 53-00-50-2R-0; AND BOEING DWG 143 - [SDR SWAA2024090520996](https://openairdocs.org/sdr/SWAA2024090520996), Aug 1, 2024: FLOOR PANEL. PULLED. FLOOR PANEL 231WF HAS MULTIPLE AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 231WF WAS REPLACED BY FABRICATING A NEW PANEL IAW SRM 53-00-50-2R-0; AND BAC DWG 143A58 - [SDR SWAA2024090520995](https://openairdocs.org/sdr/SWAA2024090520995), Aug 1, 2024: FLOOR PANEL. PULLED. FWD FLOOR PANEL 221EF UPPER SKIN HAS MULTIPLE AREAS OF PULLED STRANDS.<[01] DUE TO EXTENT OF DAMAGE; FLOOR PANEL WAS REPLACED IAW SRM 51-10-02-0G-0 PAR 9.A (1). - [SDR SWAA2024090520985](https://openairdocs.org/sdr/SWAA2024090520985), Aug 1, 2024: FLOOR PANEL. PULLED. FWD FLOOR PANEL 221FF UPPER SKIN HAS MULTIPLE AREAS OF PULLED STRANDS.<[01] FWD FLOOR PANEL 221FF UPPER SKIN WITH MULTIPLE AREAS OF PULLED STRANDS WAS REPLACED - [SDR SWAA2024090520999](https://openairdocs.org/sdr/SWAA2024090520999), Aug 1, 2024: FLOOR PANEL. PULLED. FLOOR PANEL 232DF HAS MULTIPLE AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 232DF UPPER SKIN WITH MULTIPLE AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE - [SDR SWAA2024090520998](https://openairdocs.org/sdr/SWAA2024090520998), Aug 1, 2024: FLOOR PANEL. PULLED. FWD FLOOR PANEL 231CF UPPER SKIN HAS MULTIPLE AREAS OF PULLED STRANDS.<[01] FWD FLOOR PANEL 231CF UPPER SKIN WITH MULTIPLE AREAS OF PULLED STRANDS WAS REPLACED - [SDR SWAA2024090520987](https://openairdocs.org/sdr/SWAA2024090520987), Aug 1, 2024: FLOOR PANEL. PULLED. FWD FLOOR PANEL 222CF UPPER SKIN HAS AN AREA OF PULLED STRANDS. (MARKED)<[01] AREAS OF PULLED STRANDS ON UPPER SKIN OF FWD FLOOR PANEL 222CF WERE REPAIRED IAW S - [SDR SWAA2024090521002](https://openairdocs.org/sdr/SWAA2024090521002), Aug 1, 2024: FLOOR PANEL. PULLED. FWD FLOOR PANEL 222DF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] AREAS OF PULLED STRANDS ON UPPER SKIN OF FWD FLOOR PANEL 222DF WERE REPAIRED IAW SRM 53-00-50 - [SDR SWAA2024090521010](https://openairdocs.org/sdr/SWAA2024090521010), Aug 1, 2024: FLOOR PANEL. PULLED. AFT FLOOR PANEL 241UF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] 241UF FLOOR PANEL FABRICATION HAS BEEN ACCOMPLISHED IAW SRM 53-00-50-2R-0 AND BOEING DWG: 146 - [SDR SWAA2024090521016](https://openairdocs.org/sdr/SWAA2024090521016), Aug 1, 2024: FLOOR PANEL. PULLED. AFT FLOOR PANEL 241VF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DUE TO EXTENT OF DAMAGE; FLOOR PANEL 241VF WAS REPLACED IAW SRM 51-10-02-0G-0 PAR 9.A (1).;[0 - [SDR SWAA2024090521017](https://openairdocs.org/sdr/SWAA2024090521017), Aug 1, 2024: FLOOR PANEL. PULLED. AFT FLOOR PANEL 241WF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DUE TO EXTENT OF DAMAGE; FLOOR PANEL 41WF WAS REPLACED IAW SRM 51-10-02-0G-0 PAR 9.A (1).;[02 - [SDR SWAA2024090521018](https://openairdocs.org/sdr/SWAA2024090521018), Aug 1, 2024: FLOOR PANEL. PULLED. AFT FLOOR PANEL 242QF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DUE TO EXTENT OF DAMAGE; FLOOR PANEL 242QF WAS REPLACED IAW SRM 51-10-02-0G-0 PAR 9.A (1).;[0 - [SDR SWAA2024090521019](https://openairdocs.org/sdr/SWAA2024090521019), Aug 1, 2024: FLOOR PANEL. PULLED. AFT FLOOR PANEL 241XF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] AFT FLOOR PANEL 241XF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPAIRED PER SRM 53-00-50-2 - [SDR SWAA2024090521014](https://openairdocs.org/sdr/SWAA2024090521014), Aug 1, 2024: FLOOR PANEL. PULLED. AFT FLOOR PANEL 241ZF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] AFT FLOOR PANEL 241ZF AREAS OF PULLED STRANDS ON UPPER SKIN WERE REPAIRED IAW SRM 53-00-50-2R - [SDR SWAA2024090521023](https://openairdocs.org/sdr/SWAA2024090521023), Aug 1, 2024: FLOOR PANEL. PULLED. AFT FLOOR PANEL 241ABF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] AREAS OF PULLED STRANDS ON UPPER SKIN OF AFT FLOOR PANEL 241ABF WERE REPAIRED IAW SRM 53-00- - [SDR SWAA2024090521028](https://openairdocs.org/sdr/SWAA2024090521028), Aug 1, 2024: FLOOR PANEL. PULLED. AFT FLOOR PANEL 241ADF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 241ADF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE F - [SDR SWAA2024090521025](https://openairdocs.org/sdr/SWAA2024090521025), Aug 1, 2024: FLOOR PANEL. PULLED. AFT FLOOR PANEL 242TF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] AFT FLOOR PANEL 242TF UPPER SKIN; WITH AREAS OF PULLED STRANDS; WAS REPAIRED IAW SRM 53-00-50 All 274: https://openairdocs.org/aircraft/N264LV/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 --- 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.