# N289CT: 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: 36633
- Year built: 2007
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: August 14, 2007
- Certificate issued: September 6, 2007
- Expires: May 31, 2028
- Mode S code: A2EFAE
- 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=289CT
- Page: https://openairdocs.org/aircraft/N289CT

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 (1)

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

- [NTSB DCA21LA133](https://openairdocs.org/ntsb/DCA21LA133), May 21, 2021: Boeing 737-7H4 (N289CT), Chicago, IL, substantial damage. Probable cause: the failure of the flight crew of N8686A to provide sufficient clearance while taxiing past N289CT, which was stopped.

## FAA accident and incident reports (2)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Accident 20210521004232A](https://openairdocs.org/incident/20210521004232A), May 21, 2021: Boeing 737-7H4 (N289CT), Chicago, IL, Substantial damage. On may 21, 2021 at Midway International Airport, Chicago, IL, [privacy data omitted], was proceding on their ATC clearance to taxi to runway 22L, from gate…
- [Accident 20150706015989A](https://openairdocs.org/incident/20150706015989A), Jul 6, 2015: Boeing 737-7H4 (N289CT), Phoenix, AZ, Substantial damage. On July 6, 2015 at approximately 2215 (local time), southwest airlines aircraft N289CT, operating as flight 211 departed sky Harbor international airport,…

## Service difficulty reports (260, 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 SWAA2025101323850](https://openairdocs.org/sdr/SWAA2025101323850), Oct 11, 2025: SLIDE. DETACHED. FORWARD ENTRY SLIDE HARD TO ARM AND PART OF SLIDE FELL OUT. RE-ATTACHED VELCRO AT BOTTOM OF FWD ENTRY DOOR SLIDE IAW AMM 25-66-01
- [SDR SWAA2025032002743](https://openairdocs.org/sdr/SWAA2025032002743), Mar 7, 2025: PANEL. CRACKED. PANEL 621PB CRACKED AT FWD I/B END. <[01] CRACK AT FWD I/B END OF PANEL 621PB WAS REPAIRED IAW SRM 51-70-05-2R-6.; [02] VERIFIED CORRECTIVE ACTION #1.
- [SDR SWAA2025032498497](https://openairdocs.org/sdr/SWAA2025032498497), Feb 21, 2025: ATTACH ANGLE. CRACKED. VERTICAL FIN FRONT SPAR; FWD SPRING ANGLE (176A3101-26) CRACKED AT LT ATTACH POINT<[01] REMOVED AND REPLACED VERTICAL FIN FRONT SPAR FWD SPRING ANGLE IAW SRM 51
- [SDR SWAA2025032498188](https://openairdocs.org/sdr/SWAA2025032498188), Feb 20, 2025: SKIN. CRACKED. CRACK ON RH LOWER HORIZONTAL STABILIZER SKIN. AT STAB STA 193.90; 25' FROM FWD EDGE; 0.6' IN LENGTH (MARKED)<[01] REPAIRED RH LOWER HORIZONTAL STABILIZER SKIN A
- [SDR SWAA2025032497561](https://openairdocs.org/sdr/SWAA2025032497561), Feb 18, 2025: STUB FRAME. CRACKED. CRACK FOUND ON R1 DOOR STUB FRAME 0.7' ABOVE SEAL DEPRESSOR; 0.6' FWD FROM DOOR CUT OUT. L: 0.5' MARKED. <[01] REMOVED CRACKED R1 DOOR STUB FRAME AND REPLACED A
- [SDR SWAA2025032497558](https://openairdocs.org/sdr/SWAA2025032497558), Feb 18, 2025: FRAME. CORRODED. CORROSION ON BS 303 FRAME LBL 56 WL 208. <[01] REPAIRED CORROSION ON BS 303 FRAME LBL 56 WL 208 PER EA 25-153-00457-WIP1; [02] VERIFIED ITEM 1.
- [SDR SWAA2025032497560](https://openairdocs.org/sdr/SWAA2025032497560), Feb 18, 2025: SUPPORT ANGLE. CORRODED. CORROSION ON FWD ENTRY DOOR THRESHOLD SUPPORT ANGLE BS 320 AND 338 LBL 56 WL 208. <[01] REMOVED AND REPLACED FWD ENTRY DOOR THRESHOLD SUPPORT ANGLE I.A.W SRM 51
- [SDR SWAA2025032497565](https://openairdocs.org/sdr/SWAA2025032497565), Feb 18, 2025: INTERCOSTAL. CRACKED. CRACKED INTERCOSTAL BS 380-400 RBL 40 WL 208. <[01] REMOVED AND REPLACED CRACKED INTERCOSTAL WITH NEW AT BS 380-400 RBL 40 WL 208. VERIFIED SRM 53-00-04-1A-1 IS
- [SDR SWAA2025032497573](https://openairdocs.org/sdr/SWAA2025032497573), Feb 18, 2025: STRAP. CORRODED. CORROSION ON STRAP BS 1028 RBL 18 WL 208. <[01] REMOVED AND REPLACED NEW STRAP BS 1016-1026 RBL 18 WL 208 I.A.W SRM 51-40-02-0G-0 AND BOEING DWG 147A5730 REV:C;
- [SDR SWAA2025032497569](https://openairdocs.org/sdr/SWAA2025032497569), Feb 18, 2025: STRAP. CORRODED. CORROSION ON STRAP BS 1016-1026 RBL 3 WL 208. <[01] REMOVED AND REPLACED NEW STRAP BS 1016-1026 RBL 3 WL 208 I.A.W SRM 51-40-02-0G-0 AND BOEING DWG 147A5730 REV
- [SDR SWAA2025032497570](https://openairdocs.org/sdr/SWAA2025032497570), Feb 18, 2025: STRAP. CORRODED. CORROSION ON STRAP BS 1017 LBL 3 WL 208. <[01] REMOVED AND REPLACED STRAP BS1017 LBL3 WL208 I.A.W SRM 51-40-02-0G-0 AND BOEING DWG 147A5600 REV:B; [02] VERIFIED
- [SDR SWAA2025032497559](https://openairdocs.org/sdr/SWAA2025032497559), Feb 18, 2025: SILL DRAIN. CORRODED. CORROSION ON FWD ENTRY DOOR MOP SILL BS 303 LBL 56 WL 208.<[01] REMOVED AND REPLACED FED MOPSILL I.A.W SRM 51-40-02-0G-0 AND BOEING DWG 141A8110 REV A;[02] VERI
- [SDR SWAA2025032497098](https://openairdocs.org/sdr/SWAA2025032497098), Feb 18, 2025: STUB FRAME. CRACKED. FOLDING AND PEELING OFF INTERNAL FUSELAGE SKIN ON UPPER-FWD COUNTER FRAME OF R1 DOOR; DIMENSIONS OF 3' LONG; 1' DEEP; AND 3/32' PEELING OFF.<[01] DURING INSPECT
- [SDR SWAA2025032497564](https://openairdocs.org/sdr/SWAA2025032497564), Feb 18, 2025: FLOOR SUPPORT. CRACKED. CRACKED INTERCOSTAL BS 312-328 LBL45 WL 208.<[01] REMOVED CRACKED INTERCOSTAL AND REPLACED WITH NEW INTERCOSTAL BS 312-328 LBL45 WL 208.;[02] ALL TASK STEPS COM
- [SDR SWAA2025032497562](https://openairdocs.org/sdr/SWAA2025032497562), Feb 18, 2025: FLOOR SUPPORT. CRACKED. CRACKED INTERCOSTAL BS 312-328 RBL 30 WL 208.<[01] REMOVED CRACKED INTERCOSTAL AND REPLACED WITH NEW INTERCOSTAL BS 312-328 RBL 30 WL 208.;[02] ALL TASKS STEPS 
- [SDR SWAA2025032497082](https://openairdocs.org/sdr/SWAA2025032497082), Feb 17, 2025: 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 <[01]. CORROSION ON AFT CARGO 
- [SDR SWAA2025032497079](https://openairdocs.org/sdr/SWAA2025032497079), Feb 17, 2025: SCUFF PLATE. CRACKED. AFT CARGO BAY AFT CORNER SCUFF PLATE IS CRACKED <[01]. AFT CARGO BAY AFT CORNER SCUFF PLATE REPAIRED PER SRM 53-60-15-2R-1.
- [SDR SWAA2025032097081](https://openairdocs.org/sdr/SWAA2025032097081), Feb 17, 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]. CORROSION ON AFT CARGO BAY 
- [SDR SWAA2025031997078](https://openairdocs.org/sdr/SWAA2025031997078), Feb 17, 2025: SCUFF PLATE. CRACKED. FWD CARGO BAY FWD CORNER SCUFF PLATE IS CRACKED <[01]. FWD CARGO BAY FWD CORNER SCUFF PLATE WAS REPAIRED PER SRM 53-30-15-2R-1.
- [SDR SWAA2025031997085](https://openairdocs.org/sdr/SWAA2025031997085), Feb 17, 2025: FLOOR PANEL. DELAMINATED. CABIN FLOOR PANEL 232AF TOP SURFACE IS DELAMINATED. <[01] CABIN FLOOR PANEL 232AF WITH TOP SURFACE DELAMINATION WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER 
- [SDR SWAA2025031997096](https://openairdocs.org/sdr/SWAA2025031997096), Feb 17, 2025: FLOOR PANEL. DELAMINATED. CABIN FLOOR PANEL 221FF TOP SURFACE IS DELAMINATED. <[01] CABIN FLOOR PANEL 221FF TOP SURFACE WITH DELAMINATION WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER 
- [SDR SWAA2025031997090](https://openairdocs.org/sdr/SWAA2025031997090), Feb 17, 2025: FLOOR PANEL. DELAMINATED. CABIN FLOOR PANEL 241ACF HAS TOP SURFACE DELAMINATION. <[01] CABIN FLOOR PANEL 241ACF WITH TOP SURFACE DELAMINATION WAS REPAIRED IAW SRM 53-00-50-2R-1.
- [SDR SWAA2025031997092](https://openairdocs.org/sdr/SWAA2025031997092), Feb 17, 2025: FLOOR PANEL. DELAMINATED. CABIN FLOOR PANEL 241UF HAS TOP SURFACE DELAMINATION. <[01] CABIN FLOOR PANEL 241UF; WITH TOP SURFACE DELAMINATION; WAS REPAIRED IAW SRM 53-00-50-2R-0.; [02] IT
- [SDR SWAA2025031997080](https://openairdocs.org/sdr/SWAA2025031997080), Feb 17, 2025: SHIELD. CORRODED. CORROSION AFT CARGO BAY SHIELD FWD OF CARGO DOOR AROUND MULTIPLE NUT PLATE HOLES BS767+3 TO BS794 RBL22 WL156<[01] CORROSION ON AFT CARGO BAY R/H SHIELD; FOUND 
- [SDR SWAA2025031997087](https://openairdocs.org/sdr/SWAA2025031997087), Feb 17, 2025: CARGO TRACK. CRACKED. AFT CARGO BAY CARGO TRACK IS CRACKED BS747 AND BS727E RBL13 WL156<[01] REMOVED AND REPLACED AFT CARGO BAY CARGO TRACK BS727+4 - BS887 RBL13 WL156 IAW SRM 51-40-
- [SDR SWAA2025032496721](https://openairdocs.org/sdr/SWAA2025032496721), Feb 16, 2025: STRUCTURE. CORRODED. CORROSION ON INNER CHORD AT BS 698 RBL 63 WL 208. (MARKED) <[01] REFER TO FAULT TTG8Q00YQ2WS WHERE EA 25-153-00417 WAS ADDED AS A SUBTASK; [02] VERIFIED CORRECT
- [SDR SWAA2025032095952](https://openairdocs.org/sdr/SWAA2025032095952), Feb 14, 2025: PANEL. CRACKED. PANEL 621YB CRACKED ON O/B FWD. END <[01] PANEL 621YB WITH CRACK ON O/B FWD END WAS REPAIRED PER SRM 51-70-05-2R-6.
- [SDR SWAA2025031995954](https://openairdocs.org/sdr/SWAA2025031995954), Feb 14, 2025: FLOOR PANEL. DEBONDED. CABIN FLOOR PANEL 231JF HAS DISBONDED TOP SURFACE. <[01] CABIN FLOOR PANEL 231JF DISBONDED TOP SURFACE REPAIRED IAW SRM 53-00-50-2R-0; [02] CORRECTION TO ITEM 1
- [SDR SWAA2025031995955](https://openairdocs.org/sdr/SWAA2025031995955), Feb 14, 2025: FLOOR PANEL. DELAMINATED. CABIN FLOOR PANEL 242DF HAS DELAMINATED TOP SURFACE. <[01] REPLACED DAMAGED 242DF FLOOR PANEL WITH SERVICEABLE PANEL P/N:144A5810-150 IAW SRM 51-10-02-0G-0 PARA
- [SDR SWAA2025031995959](https://openairdocs.org/sdr/SWAA2025031995959), Feb 14, 2025: FLOOR PANEL. DEBONDED. CABIN FLOOR PANEL 241EF HAS DISBONDED TOP SURFACE. <[01] CABIN FLOOR PANEL 241EF WITH DISBONDED TOP SURFACE WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 
- [SDR SWAA2025031995961](https://openairdocs.org/sdr/SWAA2025031995961), Feb 14, 2025: FLOOR PANEL. DEBONDED. CABIN FLOOR PANEL 232FF HAS DISBONDED TOP SURFACE. <[01] CABIN FLOOR PANEL 232FF DISBONDED TOP SURFACE REPAIRED IAW SRM 53-00-50-2R-0.; [02] CORRECTION TO ITEM 
- [SDR SWAA2025031995963](https://openairdocs.org/sdr/SWAA2025031995963), Feb 14, 2025: FLOOR PANEL. DELAMINATED. CABIN FLOOR PANEL 242BF HAS DELAMINATED TOP SURFACE. <[01] REPLACED DAMAGED 242BF FLOOR PANEL WITH SERVICEABLE PANEL P/N:144A5810-149 IAW SRM 51-10-02-0G-0 PARA
- [SDR SWAA2025031995967](https://openairdocs.org/sdr/SWAA2025031995967), Feb 14, 2025: FLOOR PANEL. DEBONDED. CABIN FLOOR PANEL 231ZF HAS DISBONDED TOP SURFACE. <[01] CABIN FLOOR PANEL 231ZF; WITH DISBONDED TOP SURFACE; WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL I
- [SDR SWAA2025031995962](https://openairdocs.org/sdr/SWAA2025031995962), Feb 14, 2025: FLOOR PANEL. DEBONDED. CABIN FLOOR PANEL 231MF HAS DISBONDED TOP SURFACE. <[01] 231MF FLOOR PANEL DISBOND DAMAGE ON UPPER AND LOWER SURFACE HAS BEEN REPAIRED PER [SRM 53-00-50-2R-1-A0
- [SDR SWAA2025031995957](https://openairdocs.org/sdr/SWAA2025031995957), Feb 14, 2025: FLOOR PANEL. DELAMINATED. CABIN FLOOR PANEL 242AF HAS DELAMINATED TOP SURFACE. <[01] CABIN FLOOR PANEL 242AF WITH DELAMINATED TOP SURFACE WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL
- [SDR SWAA2025031995964](https://openairdocs.org/sdr/SWAA2025031995964), Feb 14, 2025: FLOOR PANEL. DELAMINATED. CABIN FLOOR PANEL 231XF HAS DELAMINATED TOP SURFACE. <[01] CABIN FLOOR PANEL 231XF; WITH TOP SURFACE DELAMINATION; WAS REPLACED WITH A NEWLY FABRICATED FLOOR PA
- [SDR SWAA2025031995958](https://openairdocs.org/sdr/SWAA2025031995958), Feb 14, 2025: FLOOR PANEL. DELAMINATED. CABIN FLOOR PANEL 241AF HAS DELAMINATED TOP SURFACE. <[01] CABIN FLOOR PANEL 241AF WITH DELAMINATED TOP SURFACE WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL
- [SDR SWAA2025031995965](https://openairdocs.org/sdr/SWAA2025031995965), Feb 14, 2025: FLOOR PANEL. DELAMINATED. CABIN FLOOR PANEL 231YF HAS DELAMINATED TOP SURFACE. <[01] CABIN FLOOR PANEL 231YF WITH DELAMINATED TOP SURFACE WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL
- [SDR SWAA2025031995966](https://openairdocs.org/sdr/SWAA2025031995966), Feb 14, 2025: FLOOR PANEL. DELAMINATED. CABIN FLOOR PANEL 241BF HAS DELAMINATED TOP SURFACE. <[01] CABIN FLOOR PANEL 241BF WITH DELAMINATED TOP SURFACE WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL
- [SDR SWAA2025031995956](https://openairdocs.org/sdr/SWAA2025031995956), Feb 14, 2025: FLOOR PANEL. DELAMINATED. CABIN FLOOR PANEL 232RF HAS DELAMINATED TOP SURFACE. <[01] DAMAGE TO CABIN FLOOR PANEL 232RF WAS BEYOND ECONOMICAL REPAIR; FABRICATED NEW PANEL IAW SRM 53-00-50
- [SDR SWAA2025032495947](https://openairdocs.org/sdr/SWAA2025032495947), Feb 13, 2025: STRAP. CORRODED. CORROSION ON STRAP AT MID CABIN BS696 RBL67 WL203. MARKED <[01] REJECTED; AMT REQUEST FOR NDI TO VERIFY REMAINING THICKNESS OF PART. AMT DID PROVIDE STRUCTURE I
- [SDR SWAA2025032495948](https://openairdocs.org/sdr/SWAA2025032495948), Feb 13, 2025: STRAP. CORRODED. CORROSION ON STRAP AT MID CABIN BS703 RBL64 WL203. MARKED <[01] REJECTED; AMT REQUEST FOR NDI TO VERIFY REMAINING THICKNESS OF PART. AMT DID PROVIDE STRUCTURE I
- [SDR SWAA2025032495942](https://openairdocs.org/sdr/SWAA2025032495942), Feb 13, 2025: STRAP. CORRODED. CORROSION ON STRAP AT MID CABIN BS707 RBL63 WL203. MARKED <[01] REJECTED; AMT REQUEST FOR NDI TO VERIFY REMAINING THICKNESS OF PART. AMT DID NOT PROVIDE STRUCTU
- [SDR SWAA2025032495945](https://openairdocs.org/sdr/SWAA2025032495945), Feb 13, 2025: STRUCTURE. CORRODED. CORROSION ON INNER CHORD AT MID CABIN BS696; BS704 RBL63 WL208. MARKED <[01] REMOVED CORROSION IN MULTIPLE AREAS AREAS BS695 RBL63 WL 208 BLEND WAS .080'X.070'X
- [SDR SWAA2025032495946](https://openairdocs.org/sdr/SWAA2025032495946), Feb 13, 2025: STRAP. CORRODED. CORROSION ON STRAP AT MID CABIN BS692 RBL62 WL203. MARKED <[01] REJECTED; AMT REQUEST FOR NDI TO VERIFY REMAINING THICKNESS OF PART. AMT DID PROVIDE STRUCTURE I
- [SDR SWAA2025012086531](https://openairdocs.org/sdr/SWAA2025012086531), Jan 16, 2025: MOUNT BRACKET. CRACKED. R/H A/C BAY FWD PNEUMATIC APU BLEED AIR TO PACK VALVE DUCT MOUNT BRACKET CRACKED JUST OTBD OF KEEL BEAM BOX STRUCTURE. (SEE PIC)<[01] REMOVED AND REPLACED PER A
- [SDR SWAA2025012086512](https://openairdocs.org/sdr/SWAA2025012086512), Jan 16, 2025: BRACKET. CRACKED. RIGHT MLG WHEEL WELL; FWD. BULKHEAD; ABOVE BOOST PUMP; BRACKET CRACKED<[01] REMOVED AND REPLACED RIGHT MLG WHEEL WELL FWD BULKHEAD; ABOVE BOOST PUMP BRACKET IN 
- [SDR SWAA2025011686522](https://openairdocs.org/sdr/SWAA2025011686522), Jan 16, 2025: HANDLE. LOOSE. R1 DOOR INTERIOR HANDLE LOOSE<[01] TIGHTENED R1 DOOR INTERIOR HANDLE PER AMM 52-41-11.
- [SDR SWAA2025011686524](https://openairdocs.org/sdr/SWAA2025011686524), Jan 16, 2025: HANDLE. LOOSE. R1 DOOR ASSIST HANDLE LOOSE<[01] TIGHTENED R1 DOOR ASSIST HANDLE PER AMM 52-41-31.
- [SDR SWAA2025011686508](https://openairdocs.org/sdr/SWAA2025011686508), Jan 16, 2025: DOOR. CRACKED. LEFT MLG CENTER GEAR DOOR CRACKED AT FORWARD ATTACH POINT<[01] REMOVED LEFT MLG CENTER AND LOWER/INNER DOOR ASSEMBLY IN REF AMM 32-13-11.

All 260: https://openairdocs.org/aircraft/N289CT/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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