# N296WN: 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: 36613
- Year built: 2007
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: October 22, 2007
- Certificate issued: November 14, 2007
- Expires: November 30, 2028
- Mode S code: A30DC5
- 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=296WN
- Page: https://openairdocs.org/aircraft/N296WN

From the FAA registry file of October 22, 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 N296WN.

## FAA accident and incident reports

None matched to N296WN.

## Service difficulty reports (272, 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 SWAA2026092187992](https://openairdocs.org/sdr/SWAA2026092187992), Sep 15, 2026: LIGHT. INOPERATIVE. EMERGENCY LIGHT AT SEAT 16FED IS INOPERATIVE. REMOVED AND REPLACED THE EMERGENCY LIGHT IAW AMM 33-51-03-960-801. OP CHKD GOOD.
- [SDR SWAA2026060810077](https://openairdocs.org/sdr/SWAA2026060810077), Jun 7, 2026: ENGINE. FAILED. NR 2 ENGINE FAILURE ON TAKE OFF ROLL AT APPROX 40 KTS; N1 & N2 BOTH INDICATED ZERO. AS SOON AS TOGA WAS SELECTED, THERE WAS A LOUD BANG FOLLOWED BY AN AGGRESSIV
- [SDR SWAA2026031177605](https://openairdocs.org/sdr/SWAA2026031177605), Mar 8, 2026: LAMP. INOPERATIVE. L2 EXTERIOR EMERGENCY EXIT LIGHT INOPERATIVE. R & R THE L2 EXTERIOR EMERGENCY EXIT LAMP IAW AMM 33-51-04. R & R THE BATTERY PACK & CHARGER ASSY IAW AMM 33-51-06
- [SDR SWAA2026021670373](https://openairdocs.org/sdr/SWAA2026021670373), Feb 13, 2026: BARREL NUT. BROKEN. FWD ENTRY DOOR SLIDE BARREL NUT AND RETAINER BROKEN. REPLACED FWD ENTRY DOOR SLIDE BARREL NUT AND RETAINER. IAW AMM 52-11-31.
- [SDR SWAA2026021671268](https://openairdocs.org/sdr/SWAA2026021671268), Feb 13, 2026: RETAINER. BROKEN. FWD ENTRY DOOR SLIDE BARREL NUT AND RETAINER BROKEN. REPLACED FWD ENTRY DOOR SLIDE BARREL NUT AND RETAINER IAW AMM 52-11-31.
- [SDR SWAA2025073091271](https://openairdocs.org/sdr/SWAA2025073091271), Jul 15, 2025: PLATE. CRACKED. CRACKS ON PLATE ASSY- AT IRSS 199+17; FOR ATTACHMENT OF ACCESS PANEL 651EB INBOARD SIDE. REMOVED AND REPLACED THE RT WING I/B SIDE WIGGLE PLATE AT IRSS 199+17 F
- [SDR SWAA2025072990095](https://openairdocs.org/sdr/SWAA2025072990095), Jul 11, 2025: FAIRING. CRACKED. NUMBER 1 ENG STRUT AFT FAIRING TRAILING EDGE IS CRACKED. R & R NR 1 ENG STRUT AFT FAIRING TRAILING EDGE IAW SRM 51-40-02-0G-0, & DWG 313A2400 REV A. ALL STEPS C
- [SDR SWAA2025072989360](https://openairdocs.org/sdr/SWAA2025072989360), Jul 9, 2025: INSERT. DAMAGED. PANEL 241ABF AFT GIRT FITTING, AFT FASTENER HOLE 2-PIECE INSERT IS DAMAGED. REMOVED AND REPLACED DAMAGED INSERT FOR AFT GIRT FITTING ON PANEL 241ABF IAW SRM 53-
- [SDR SWAA2025072988395](https://openairdocs.org/sdr/SWAA2025072988395), Jul 4, 2025: SEAT TRACK. CORRODED. CORROSION FOUND ON PASSENGER SEAT TRACK AT LBL 45, WL 208, BS 360+9 ON WELL, BS 360+14 ON CROWN BS 360+16 ON WELL, BS 380 ON CROWN & WELL, BS 400+1 ON CROWN & W
- [SDR SWAA2025072988004](https://openairdocs.org/sdr/SWAA2025072988004), Jul 3, 2025: DOUBLER. CORRODED. WIFI ANTENNA AREA; EXTERIOR FUSELAGE CROWN SKIN DOUBLER FOUND CORROSION AT STA 727C BTWN STGR 1 AND 2 RH AT SEVERAL FASTENERS. RESOLVE FAULT ON TTG8Q013J793 WHE
- [SDR SWAA2025073187674](https://openairdocs.org/sdr/SWAA2025073187674), Jul 2, 2025: SEAT TRACK. CORRODED. CORROSION FOUND ON PASSENGER SEAT TRACK AT LBL 45 BS 360+9, 360+14, 360+16, 380 , 400+1, 420+11, & 500A+4. WL 208. TASK TO BE ACCOMPLISHED ON CUSTOMER CARDS TTG
- [SDR SWAA2025072987675](https://openairdocs.org/sdr/SWAA2025072987675), Jul 2, 2025: DOUBLER. CRACKED. DURING OK TO INSTALL RT BS 663 RBL 6-32 LWR DOUBLER; FOUND DOUBLER CRACKED AT THE CORNER. REMOVED AND REPLACED ON FAULT TTG8Q013CQB6.
- [SDR SWAA2025072987671](https://openairdocs.org/sdr/SWAA2025072987671), Jul 2, 2025: SEAT TRACK. CORRODED. CORROSION FOUND ON PASSENGER SEAT TRACK AT RBL45 BS380+13 ON CROWN, BS400+10 ON CROWN, BS480+6 ON CROWN, BS500A+14 ON CROWN, BS520 ON WELL WL208. ACCOMPLISHED O
- [SDR SWAA2025072987350](https://openairdocs.org/sdr/SWAA2025072987350), Jul 1, 2025: SEAT TRACK. CORRODED. CORROSION FOUND ON PASSENGER SEAT TRACK AT LBL 25 BS 360+10 ON CROWN AND WELL, BS 400 ON CROWN, BS 480+13 ON CROWN AND WELL, BS 500A+6 ON WELL; BS 500B+11 ON CR
- [SDR SWAA2025072986999](https://openairdocs.org/sdr/SWAA2025072986999), Jun 30, 2025: STRINGER CLIP. CRACKED. CRACKED STRINGER CLIP AT PAX CABIN, BS 767, S6L. REMOVED AND REPLACED THE STRINGER CLIP IAW SRM 51-40-02 AND DWG 146A1132 REV -.
- [SDR SWAA2025072987000](https://openairdocs.org/sdr/SWAA2025072987000), Jun 30, 2025: STRINGER CLIP. CRACKED. CRACKED STRINGER CLIP AT PAX CABIN, BS 727E, S5R. REMOVED AND REPLACED THE STRINGER CLIP IAW SRM 51-40-02 AND DWG 146A1112 REV-.
- [SDR SWAA2025072987001](https://openairdocs.org/sdr/SWAA2025072987001), Jun 30, 2025: STRINGER CLIP. CRACKED. CRACKED STRINGER CLIP AT PAX CABIN, BS 727C, S6L. REMOVED AND REPLACED THE STRINGER CLIP IAW SRM 51-40-02 AND DWG 146A1103 REV. -
- [SDR SWAA2025072987002](https://openairdocs.org/sdr/SWAA2025072987002), Jun 30, 2025: STRINGER CLIP. CRACKED. CRACKED STRINGER CLIP AT PAX CABIN, BS 727B, S7L. REMOVED AND REPLACED THE STRINGER CLIP IAW SRM 51-40-02 AND DWG 146A1102 REV.-.
- [SDR SWAA2025072987003](https://openairdocs.org/sdr/SWAA2025072987003), Jun 30, 2025: STRINGER CLIP. CRACKED. CRACKED STRINGER CLIP AT PAX CABIN BS727E S-6L. REMOVED AND REPLACED STRINGER CLIP IAW SRM 51-40-02 AND DWG NBR 146A1112 REV .-.
- [SDR SWAA2025072987004](https://openairdocs.org/sdr/SWAA2025072987004), Jun 30, 2025: STRINGER CLIP. CRACKED. CRACKED STRINGER CLIP AT PAX CABIN, BS 727E, S-5L. REMOVED AND REPLACED STRINGER CLIP IAW SRM 51-40-02 AND DWG NBR 146A1112 REV.-.
- [SDR SWAA2025072987005](https://openairdocs.org/sdr/SWAA2025072987005), Jun 30, 2025: STRINGER CLIP. CRACKED. CRACKED STRINGER CLIP AT PAX CABIN BS727D S-7L. REMOVED AND REPLACED STRINGER CLIP IAW SRM 51-40-02 AND DWG NBR 146A1111 REV.-.
- [SDR SWAA2025072987006](https://openairdocs.org/sdr/SWAA2025072987006), Jun 30, 2025: STRINGER CLIP. CRACKED. CRACKED STRINGER CLIP AT PAX CABIN, BS 727B, S-6L. REMOVED AND REPLACED STRINGER CLIP IAW SRM 51-40-02 AND DWG NBR 146A1102 REV.-.
- [SDR SWAA2025072987007](https://openairdocs.org/sdr/SWAA2025072987007), Jun 30, 2025: STRINGER CLIP. CRACKED. CRACKED STRINGER CLIP AT PAX CABIN, BS 727A S-7L. REMOVED AND REPLACED STR CLIP AT PAX CABIN BS 727A S-7L PER REF SRM 51-40-02 AND DWG NBR 146A1101 REV. -.
- [SDR SWAA2025072986189](https://openairdocs.org/sdr/SWAA2025072986189), Jun 27, 2025: STIFFENER. CRACKED. CRACKED LOWER SIDE STIFFENER 3 AT INSPAR RIB 3 (STAB STA 111.10) - L/H HORIZONTAL STABILIZER. REPAIRED LOWER SIDE OF STIFFENER #3 AT INSPAR RIB #3(STAB STA 111.
- [SDR SWAA2025072993051](https://openairdocs.org/sdr/SWAA2025072993051), Jun 27, 2025: FLAP TRACK. WORN. RIGHT WING I/B AFT FLAP O/B TRACK WORN ON LOWER FLANGE. REMOVED AND RE-INSTALLED RIGHT WING I/B AFT FLAP TO REPLACE WORN O/B TRACK IAW AMM 27-51-12-000-801; AMM
- [SDR SWAA2025072986191](https://openairdocs.org/sdr/SWAA2025072986191), Jun 27, 2025: FLOOR PANEL. DELAMINATED. PASSENGER CABIN FLOOR PANEL 241VF UPPER SKIN HAS AREAS OF DELAMINATION. REPLACED DAMAGED 241VF FLOOR PANEL WITH A NEW FLOOR PANEL IAW SRM 51-40-02-0G-0 PARA 9 A
- [SDR SWAA2025073085564](https://openairdocs.org/sdr/SWAA2025073085564), Jun 26, 2025: PANEL. DELAMINATED. PANEL 521CB FWD I/B CORNER DELAMINATED. REPAIRED PER [SRM 51-70-05-2R-6-A00737 (REPAIR 6 - REPAIR OF DAMAGE TO THE EDGEBAND OF A HONEYCOMB PANEL - AIRFRAME - PE
- [SDR SWAA2025073085852](https://openairdocs.org/sdr/SWAA2025073085852), Jun 26, 2025: WEB. CRACKED. LEFT WING TRAIING EDGE TRANSVERSE WEB OTBD ATTACH ANGLE CRACKED. REMOVED & REPLACED A NEW ATTACH ANGLE AT LT WING T/E TRANSVERSE WEB OTBD SIDE IAW SRM 51-40-02 
- [SDR SWAA2025072985848](https://openairdocs.org/sdr/SWAA2025072985848), Jun 26, 2025: FLOORBEAM. CRACKED. CRACKED ON FLOORBEAM AT BS 328; RBL 18.5; WL208. REMOVED AND REPAIRED DAMAGE PART OF THE UPPER FLANGES FLOOR BEAM BS328 FROM RBL1-RBL60 WL208 I.A.W SRM 53-10-51
- [SDR SWAA2025072985850](https://openairdocs.org/sdr/SWAA2025072985850), Jun 26, 2025: INTERCOSTAL. CRACKED. CRACKED ON INTERCOSTAL AT BS 393; RBL 10; WL 208. REMOVED AND REPLACED INTERCOSTAL BS380-BS400 RBL8.2 WL208 I.A.W SRM 51-10-02-0G-0 PAR 9.C; SRM 51-40-02-0G-0 A
- [SDR SWAA2025072985837](https://openairdocs.org/sdr/SWAA2025072985837), Jun 26, 2025: SCUFF PLATE. CRACKED. FWD ENTRY DOOR FWD LOWER SCUFF PLATE IS CRACKED ON AFT EDGE. REPAIRED CRACKED FED FWD SCUFF PLATE PER EA 25-153-01771-WIP1; ACCOMPLISHED ON TASK ID TTG8Q013H6V.
- [SDR SWAA2025072985841](https://openairdocs.org/sdr/SWAA2025072985841), Jun 26, 2025: BULKHEAD WEB. CORRODED. 1016 BULKHEAD WEB HAS CORROSION BS 1020; LBL 9; WL 208. REMOVED DAMAGE ON BULKHEAD WEB BS 1029 LBL 9+ WL 208 2.0'X1.0'WITH .003' MATERIAL REMOVED. ORIGINAL MATE
- [SDR SWAA2025072985563](https://openairdocs.org/sdr/SWAA2025072985563), Jun 26, 2025: BEAM. CORRODED. BS 986 BEAM PREVIOUS REPAIR IS CORRODED ON UPPER SURFACE AND BETWEEN REPAIR PARTS FROM RBL 42 TO RBL 45, WL 207.9 TO WL 208.1. DISCREPANCY AREA TO BE REMOVE AND
- [SDR SWAA2025072985834](https://openairdocs.org/sdr/SWAA2025072985834), Jun 26, 2025: SCUFF PLATE. CRACKED. AFT CARGO BAY AFT CORNER SCUFF PLATE IS CRACKED. REPAIRED IAW SRM 53-60-15-2R-1. SCUFF PLATE WILL BE INSTALLED ON CUSTOMER CARD TTG8Q013BV69.
- [SDR SWAA2025072985845](https://openairdocs.org/sdr/SWAA2025072985845), Jun 26, 2025: TAIL CONE. CRACKED. PERFROM PERMENANT REPAIR TO 1 INCH CRACK ON TOP LEFT SIDE OF TAILCONE. ACCOMPLISHED PERMANENT REPAIR TO 1 INCH CRACK ON TOP LEFT SIDE OF TAILCONE IAW SRM 51-70-
- [SDR SWAA2025073185555](https://openairdocs.org/sdr/SWAA2025073185555), Jun 25, 2025: ATTACH ANGLE. CORRODED. CORROSION AFT CARGO BAY ATTACH ANGLE UNDER SHIELD, HAS MULTIPLE AREAS UNDER NUT PLATES BS 767 TO BS 787, RBL21, WL156. CORROSION ON AFT CARGO BAY ATTACH ANGLE U
- [SDR SWAA2025072985369](https://openairdocs.org/sdr/SWAA2025072985369), Jun 25, 2025: FLOOR PANEL. DELAMINATED. PASSENGER CABIN FLOOR PANEL 241TF HAS DELAMINATION. REMOVED CABIN FLOOR PANEL 241TF IAW AMM 53-21-00-000-801. REPAIRED AND REINSTALLED FLOOR PANEL 241TF PER AMM
- [SDR SWAA2025072985368](https://openairdocs.org/sdr/SWAA2025072985368), Jun 25, 2025: FLOOR PANEL. DELAMINATED. PASSENGER CABIN FLOOR PANEL 241SF HAS DELAMINATION . REMOVED CABIN FLOOR PANEL 241SF IAW AMM 53-21-00-000-801. DUE TO THE EXTENT OF DAMAGE; REPLACED PASSENGER C
- [SDR SWAA2025072985365](https://openairdocs.org/sdr/SWAA2025072985365), Jun 25, 2025: FLOOR PANEL. DELAMINATED. PASSENGER CABIN FLOOR PANEL 242AF HAS DELAMINATION. REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.
- [SDR SWAA2025072985366](https://openairdocs.org/sdr/SWAA2025072985366), Jun 25, 2025: FLOOR PANEL. DELAMINATED. PASSENGER CABIN FLOOR PANEL 241BF HAS DELAMINATION. DUE TO THE EXTENT OF DAMAGE, REPLACED THE FLOOR PANEL 241BF IAW SRM 51-10-02-0G-0 PARA 9 AND AIPC 53-21-00-4
- [SDR SWAA2025072985556](https://openairdocs.org/sdr/SWAA2025072985556), Jun 25, 2025: SUPPORT PLATE. CORRODED. CORROSION FWD CARGO BAY LT FLOOR TO SIDEWALL SUPPORT PLATE MULTIPLE AREAS AROUND NUT PLATE HOLES BS 400 TO BS 500D LBL22 WL156, FOUND TO BE OUT OF LIMITS. REMOV
- [SDR SWAA2025072985553](https://openairdocs.org/sdr/SWAA2025072985553), Jun 25, 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. EVALUATED; LOCATED; DRILLED; REMO
- [SDR SWAA2025072985554](https://openairdocs.org/sdr/SWAA2025072985554), Jun 25, 2025: SUPPORT PLATE. CORRODED. CORROSION AFT CARGO BAY R/H FLOOR TO SIDEWALL SUPPORT PLATE HAS MULTIPLE AREAS AROUND NUT PLATE HOLES BS727B TO BS767 RBL22 WL156, FOUND TO BE OUT OF LIMITS. RE
- [SDR SWAA2025072985557](https://openairdocs.org/sdr/SWAA2025072985557), Jun 25, 2025: SHIELD. CORRODED. CORROSION AFT CARGO BAY SHIELD FWD OF CARGO DOOR AROUND MULTIPLE NUT PLATE HOLES BS767+3 TO BS794 RBL22 WL156, FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GI
- [SDR SWAA2025072985558](https://openairdocs.org/sdr/SWAA2025072985558), Jun 25, 2025: STRAP. CORRODED. CORROSION AFT CARGO BAY ON TIE STRAP BS 787+16, RBL 20, WL 156, FOUND TO BE OUT OF LIMITS. REMOVED; REPLACED AND INSTALLED NEW TIE STRAP IAW SRM 51-40-02-0G-0; 
- [SDR SWAA2025072985356](https://openairdocs.org/sdr/SWAA2025072985356), Jun 25, 2025: ATTACH ANGLE. CRACKED. LANDING GEAR MANUAL EXTENSION CONTROL DRUM BOX ATTACH ANGLE CRACKED AT BS 253, RBL 7, WL 207. REMOVED AND REPLACED LANDING GEAR MANUAL EXTENSION CONTROL DRUM AT
- [SDR SWAA2025072985560](https://openairdocs.org/sdr/SWAA2025072985560), Jun 25, 2025: STRAP. CORRODED. CORROSION ON STRAP AT BS719; RBL66; WL203. REMOVED AND TREATED PER EA 25-153-01775-WIP1; TASK ID TTG8Q013HMEX; AND WIP2; TASK ID TTG8Q013QUEY.
- [SDR SWAA2025072985561](https://openairdocs.org/sdr/SWAA2025072985561), Jun 25, 2025: STRAP. CORRODED. CORROSION ON STRAP AT MID CABIN BS696 LBL66 WL203. IAW EA 25-153-01786; THE REWORK IS ACCEPTABLE AS A CONTINUE-IN-SERVICE CONDITION WITHOUT REPETITIVE INSPECTIO
- [SDR SWAA2025072985562](https://openairdocs.org/sdr/SWAA2025072985562), Jun 25, 2025: ATTACH ANGLE. CRACKED. CRACKED ATTACH ANGLE AT MID CABIN BS 691, RBL1, WL206. REMOVED, FABRICATED, AND REPLACED ATTACH ANGLE IAW SRM 51-10-02-0G-0, SRM 51-40-02-0G-0, BOEING 111A6000 
- [SDR SWAA2025072985125](https://openairdocs.org/sdr/SWAA2025072985125), Jun 25, 2025: PANEL. DEBONDED. PANEL 193AR OUTER SKIN IS DISBONDED. REPAIRED IAW SRM 51-70-05-2R-4.

All 272: https://openairdocs.org/aircraft/N296WN/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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