# N288WN: 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: 36611
- Year built: 2007
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: August 15, 2007
- Certificate issued: September 5, 2007
- Expires: May 31, 2028
- Mode S code: A2EDB4
- 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=288WN
- Page: https://openairdocs.org/aircraft/N288WN

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 N288WN.

## FAA accident and incident reports

None matched to N288WN.

## 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 SWAA2026031879789](https://openairdocs.org/sdr/SWAA2026031879789), Mar 15, 2026: LIGHT. INOPERATIVE. EXTERIOR EMERGENCY LIGHT ON L1 DOOR INOPERATIVE. R&R THE LIGHT ASSEMBLY IAW AMM 33-51-04. OPS CHECKED GOOD.
- [SDR SWAA2026021068112](https://openairdocs.org/sdr/SWAA2026021068112), Feb 6, 2026: ISOLATION MOUNT. CRACKED. AFT ENTRY DOOR FWD SLIDE MOUNT ISOLATOR CRACKED. R & R AFT ENTRY DOOR FWD SLIDE MOUNT ISOLATORS IAW SRM 51-40-02.
- [SDR SWAA2026012965618](https://openairdocs.org/sdr/SWAA2026012965618), Jan 29, 2026: BATTERY. INOPERATIVE. FWD AND AFT GALLEYS EMERGENCY FLASHLIGHTS REQUIRES REPLACEMENT. REPLACED FWD AND AFT GALLEY EMERGENCY FLASHLIGHT BATTERIES AND PLACARDS IAW AMM 25-64-00.
- [SDR SWAA2025112438033](https://openairdocs.org/sdr/SWAA2025112438033), Nov 20, 2025: LENS. BROKEN. EMERGENCY LIGHT LENS BROKEN AT ROW 1C (BULLNOSE). INSTALLED MISSING LENS ON EMERGENCY LIGHT AT 1C PER AMM 33-51-03.
- [SDR SWAA2025060373647](https://openairdocs.org/sdr/SWAA2025060373647), May 21, 2025: LIGHT. BROKEN. AFT ENTRY LOWERED CEILING PANEL EXIT LIGHT HOUSING IS BROKEN.<[01] REMOVED AND REPLACED AND PERFORMED OPS CHECK GOOD ON AFT ENTRY LOWERED CEILING PANEL EXIT LIG
- [SDR SWAA2025060268965](https://openairdocs.org/sdr/SWAA2025060268965), May 8, 2025: FLOOR PANEL. DEFORMED. FLOOR PANEL 221EF HAS SOFT EDGE AT L/H AFT CORNER.<[01] FLOOR PANEL 221EF WITH SOFT EDGE AT L/H AFT CORNER WAS REPAIRED PER SRM 53-00-50-2R-10.;[02] VERIFIED CO
- [SDR SWAA2025060368418](https://openairdocs.org/sdr/SWAA2025060368418), May 7, 2025: STIFFENER. ELONGATED. STIFFENER AT BS663 LBL40 WL160 HAS ELONGATED FASTENER HOLE<[01] REMOVED AND REPLACED STIFFENER AT BS663 LBL40 WL160 IAW SRM 51-40-02-0G-0 AND DWG 111A7000 REV:-
- [SDR SWAA2025060366068](https://openairdocs.org/sdr/SWAA2025060366068), Apr 30, 2025: FRAME. CRACKED. CRACK ON BS 312 FRAME COMMON TO STR 5L ABOVE FWD ENTRY DOOR UPPER SILL WEB.<[01] REPAIRED BS 312 FRAME COMMON TO STR 5L ABOVE FWD ENTRY DOOR UPPER SILL WEB IAW 
- [SDR SWAA2025060365870](https://openairdocs.org/sdr/SWAA2025060365870), Apr 30, 2025: SEAT TRACK. CORRODED. CORROSION ON PAX CABIN SEAT TRACK LBL 45 WL 208 FROM BS 495 TO BS 520 ON TOP MARKED<[01] REMOVED AND REPLACED SEAT TRACK AT LBL 45 WL 208 FROM BS 480-520 IAW SR
- [SDR SWAA2025060365868](https://openairdocs.org/sdr/SWAA2025060365868), Apr 30, 2025: SEAT TRACK. CORRODED. CORROSION ON PAX CABIN SEAT TRACK LBL 25 WL 208 FROM BS 495 TO BS 520 ON TOP MARKED.<[01] REMOVED CORROSION ON CROWN AT BS 519. BLEND WAS .9'X.4'X.028' FOUND TO
- [SDR SWAA2025060366062](https://openairdocs.org/sdr/SWAA2025060366062), Apr 30, 2025: SKIN. CRACKED. CRACK ON LH LOWER HORIZONTAL STABILIZER SKIN. AT STAB STA 193.90; 18' FROM FWD EDGE; .3' IN LENGTH (MARKED)<[01] REPAIRED LH LOWER HORIZONTAL STABILIZER SKIN. A
- [SDR SWAA2025060366066](https://openairdocs.org/sdr/SWAA2025060366066), Apr 30, 2025: SKIN. CRACKED. CRACK ON RH LOWER HORIZONTAL STABILIZER SKIN. AT STAB STA 193.90; 17.5' FROM FWD EDGE; .55' IN LENGTH (MARKED)<[01] REPAIRED RH LOWER HORIZONTAL STABILIZER SKIN
- [SDR SWAA2025060266067](https://openairdocs.org/sdr/SWAA2025060266067), Apr 30, 2025: FRAME. CRACKED. CRACKED FRAME BS 259.5 AT CUTOUT RBL 40 WL 260.<[01] THE DAMAGE WAS REPAIRED WITH A WEB SEGMENT SPLICE PER EA 25-153-01133. AN INSPECTION THRESHOLD IS DEFINED I
- [SDR SWAA2025060266057](https://openairdocs.org/sdr/SWAA2025060266057), Apr 30, 2025: VAPOR BARRIER. CRACKED. BS 663 VAPOR BARRIER CRACKED BEHIND HYDRAULIC SYSTEM B GROUND SERVICE DISCONNECT MODULE - RBL 52; WL 184.<[01] BS 663 VAPOR BARRIER CRACK AT RBL 52 WL 184 WAS R
- [SDR SWAA2025060365706](https://openairdocs.org/sdr/SWAA2025060365706), Apr 29, 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<[01] CORROSION ON AFT CARGO BA
- [SDR SWAA2025060365705](https://openairdocs.org/sdr/SWAA2025060365705), Apr 29, 2025: SIDEWALL SUPPORT. 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 L/
- [SDR SWAA2025060365704](https://openairdocs.org/sdr/SWAA2025060365704), Apr 29, 2025: SCUFF PLATE. CRACKED. AFT CARGO BAY AFT CORNER SCUFF PLATE IS CRACKED<[01] REPAIRED AFT CARGO BAY AFT CORNER SCUFF PLATE PER SRM 53-60-15-2R-1;[02] VERIFIED CORRECTIVE ACTION
- [SDR SWAA2025060365366](https://openairdocs.org/sdr/SWAA2025060365366), Apr 29, 2025: SKIN. DEBONDED. PANEL 194E OUTER SKIN HAS 2 DISBONDS. (MARKED)<[01] PANEL 194E OUTER SKIN WITH 2 DISBONDS AS MARKED PLUS ONE ADDITIONAL UNMARKED UPPER SKIN DISBOND WERE ALL REP
- [SDR SWAA2025060265707](https://openairdocs.org/sdr/SWAA2025060265707), Apr 29, 2025: CARGO TRACK. CRACKED. AFT CARGO BAY CARGO TRACK IS CRACKED BS767 RBL13 WL156<[01] REMOVED AND REPLACED AFT CARGO BAY CARGO TRACK BS 727+4 - BS 887 RBL 13 WL 156 IAW SRM 51-40-02-0G-0
- [SDR SWAA2025060365360](https://openairdocs.org/sdr/SWAA2025060365360), Apr 28, 2025: FLOOR PANEL. DELAMINATED. FLOOR PANEL 221AF IS DELAMINATED<[01] FLOOR PANEL 221AF WITH UPPER SKIN DELAMINATIONS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A
- [SDR SWAA2025060365347](https://openairdocs.org/sdr/SWAA2025060365347), Apr 28, 2025: FLOOR PANEL. DELAMINATED. FLOOR PANEL 221FF IS DELAMINATED<[01] FLOOR PANEL 221FF UPPER SKIN WITH DELAMINATIONS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A
- [SDR SWAA2025060365352](https://openairdocs.org/sdr/SWAA2025060365352), Apr 28, 2025: FLOOR PANEL. DELAMINATED. FLOOR PANEL 221GF IS DELAMINATED; CORNER CRACKS AND 1 BAD INSERT<[01] FLOOR PANEL 221GF WITH UPPER SKIN DELAMINATIONS; CORNER CRACKS AND 1 BAD INSERT WAS REPLAC
- [SDR SWAA2025060365346](https://openairdocs.org/sdr/SWAA2025060365346), Apr 28, 2025: FLOOR PANEL. DELAMINATED. FLOOR PANEL 231AF IS DELAMINATED<[01] FLOOR PANEL 231AF WITH UPPER SKIN DELAMINATIONS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A
- [SDR SWAA2025060365345](https://openairdocs.org/sdr/SWAA2025060365345), Apr 28, 2025: FLOOR PANEL. DELAMINATED. FLOOR PANEL 232FF IS DELAMINATED. DUE TO EXTENT OF THE DAMAGE FABRICATED NEW 232FF FLOOR PANEL IAW SRM 53-00-50-2R-0.;[02] VERIFIED CORRECTIVE ACTION ITEM 1.
- [SDR SWAA2025060365344](https://openairdocs.org/sdr/SWAA2025060365344), Apr 28, 2025: FLOOR PANEL. DELAMINATED. FLOOR PANEL 231JF IS DELAMINATED<[01] DUE TO EXTENT OF THE DAMAGE FABRICATED NEW 231JF FLOOR PANEL IAW SRM 53-00-50-2R-0.;[02] VERIFIED CORRECTIVE ACTION ITEM 1
- [SDR SWAA2025060365060](https://openairdocs.org/sdr/SWAA2025060365060), Apr 28, 2025: FLOOR PANEL. DELAMINATED. FLOOR PANEL 241VF DELAMINATED<[01] FLOOR PANEL 241VF WITH UPPER SKIN AREAS OF DELAMINATION WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PAR
- [SDR SWAA2025060365057](https://openairdocs.org/sdr/SWAA2025060365057), Apr 28, 2025: WEB. CORRODED. CORROSION ON L/H SHEAR WEB AT BS 1026 LBL 7 AND LBL 13 WL 208<[01] REMOVED AND REPLACED L/H SHEAR WEB BS1006-1029 BL0-LBL33 WL 208 IAW SRM 51-40-02-0G-0 AND BOE
- [SDR SWAA2025060365340](https://openairdocs.org/sdr/SWAA2025060365340), Apr 28, 2025: ANGLE. CRACKED. CRACKED ANGLE ON INTERCOSTAL AT BS 380-400 RBL 40 WL 208<[01] REPLACED A NEW ANGLE ON INTERCOSTAL AT BS 380-400; RBL40; WL208 IAW SRM 51-40-02 AND BOEING DWG 14
- [SDR SWAA2025060365339](https://openairdocs.org/sdr/SWAA2025060365339), Apr 28, 2025: FLOORBEAM. CORRODED. CORROSION ON FILLER OF FLOOR BEAM AT BS 986 RBL 45 WL 208 MARKED<[01] REMOVED; FABRICATED AND REPLACED FILLER AS SHOWN PREVIOUS REPAIR RECORD ON CCN TTG8Q00L09B
- [SDR SWAA2025060265061](https://openairdocs.org/sdr/SWAA2025060265061), Apr 28, 2025: FLOOR PANEL. DELAMINATED. FLOOR PANEL 241XF DELAMINATED<[01] FLOOR PANEL 241XF DELAMINATION WAS REPAIRED IAW SRM 53-00-50-2R-1.
- [SDR SWAA2025060265063](https://openairdocs.org/sdr/SWAA2025060265063), Apr 28, 2025: FLOOR PANEL. DELAMINATED. FLOOR PANEL 241YF DELAMINATED<[01] 241YF FLOOR PANEL DELAMINATION DAMAGE HAS BEEN REPAIRED PER [SRM 53-00-50-2R-1-A00939 (REPAIR 1 - REPAIR OF DAMAGE TO ONE FAC
- [SDR SWAA2025060265062](https://openairdocs.org/sdr/SWAA2025060265062), Apr 28, 2025: FLOOR PANEL. DELAMINATED. FLOOR PANEL 241ABF DELAMINATED<[01] FLOOR PANEL 241ABF WITH DELAMINATION WAS REPAIRED IAW SRM 53-00-50-2R-1.
- [SDR SWAA2025060265064](https://openairdocs.org/sdr/SWAA2025060265064), Apr 28, 2025: FLOOR PANEL. DELAMINATED. FLOOR PANEL 242UF DELAMINATED AND 5EA BAD INSERTS<[01] FLOOR PANEL 242UF WITH DELAMINATION WAS REPAIRED AND REPLACE DAMAGED INSERTS IAW SRM 53-00-50-2R-1.
- [SDR SWAA2025060265358](https://openairdocs.org/sdr/SWAA2025060265358), Apr 28, 2025: FLOOR PANEL. DELAMINATED. FLOOR PANEL 221EF IS DELAMINATED<[01] FLOOR PANEL 221EF UPPER SKIN WITH DELAMINATIONS AS MARKED WAS REPAIRED PER SRM 53-00-50-2R-1.;[02] VERIFIED CORRECTIVE ACT
- [SDR SWAA2025060265359](https://openairdocs.org/sdr/SWAA2025060265359), Apr 28, 2025: FLOOR PANEL. DELAMINATED. FLOOR PANEL 221CF IS DELAMINATED<[01] FLOOR PANEL 221CF WITH DELAMINATION WAS REPAIRED IAW SRM 53-00-50-2R-1.
- [SDR SWAA2025060364397](https://openairdocs.org/sdr/SWAA2025060364397), Apr 26, 2025: FLOOR PANEL. PULLED. FLOOR PANEL 241DF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DUE TO EXTENT OF THE DAMAGE FABRICATED NEW 241DF FLOOR PANEL IAW SRM 53-00-50-2R-0.;[02] VERIFIED
- [SDR SWAA2025060364396](https://openairdocs.org/sdr/SWAA2025060364396), Apr 26, 2025: FLOOR PANEL. PULLED. FLOR PANEL 241BF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DUE TO EXTENT OF THE DAMAGE FABRICATED NEW 241BF FLOOR PANEL IAW SRM 53-00-50-2R-0.;[02] VERIFIED 
- [SDR SWAA2025060364392](https://openairdocs.org/sdr/SWAA2025060364392), Apr 26, 2025: FLOOR PANEL. PULLED. FLOOR PANEL 231XF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DUE TO EXTENT OF THE DAMAGE FABRICATED NEW 231XF FLOOR PANEL IAW SRM 53-00-50-2R-0.;[02] VERIFIED
- [SDR SWAA2025060264393](https://openairdocs.org/sdr/SWAA2025060264393), Apr 26, 2025: FLOOR PANEL. PULLED. FLOOR PANEL 231ZF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DUE TO EXTENT OF THE DAMAGE FABRICATED NEW 241ZF FLOOR PANEL IAW SRM 53-00-50-2R-0.;[02] CORRECTI
- [SDR SWAA2025060264394](https://openairdocs.org/sdr/SWAA2025060264394), Apr 26, 2025: FLOOR PANEL. PULLED. FLOOR PANEL 232SF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 232SF WAS REPLACED IAW SRM 53-00-50-2R-0;[02] FLOOR PANEL 232SF WAS REPLACED IAW SRM 
- [SDR SWAA2025060264395](https://openairdocs.org/sdr/SWAA2025060264395), Apr 26, 2025: FLOOR PANEL. PULLED. FLOOR PANEL 241FF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 241FF WAS REPLACED IAW SRM 53-00-50-2R-0 PARA 1.A. NOTE:;[02] VERIFIED CORRECTIVE ACT
- [SDR SWAA2025060264398](https://openairdocs.org/sdr/SWAA2025060264398), Apr 26, 2025: FLOOR PANEL. PULLED. FLOOR PANEL 242CF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 242CF WAS REPLACED IAW SRM 53-00-50-2R-0 PARA 1. A. NOTE:;[02] VERIFIED CORRECTIVE AC
- [SDR SWAA2025060358379](https://openairdocs.org/sdr/SWAA2025060358379), Apr 25, 2025: LAMP. BURNED. LH #1 BIN EMERGENCY LIGHT IS BURNED OUT<[01] REPLACED LH#1 BIN EMERGENCY LIGHT AND PERFORMED GOOD FUNCTIONAL TEST IAW AMM 33-51-03-960-801.-;[02] VERIFIED
- [SDR SWAA2025060264390](https://openairdocs.org/sdr/SWAA2025060264390), Apr 25, 2025: VAPOR BARRIER. CRACKED. L/H BS663 VAPOR BARRIER IS CRACKED AT LBL30 WL140<[01] L/H BS663 VAPOR BARRIER; CRACK AT LBL30 WL140; WAS REPAIRED IAW SRM 51-70-04-2R-10.
- [SDR SWAA2025021996875](https://openairdocs.org/sdr/SWAA2025021996875), Feb 17, 2025: LIGHT. INOPERATIVE. R1 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP<[01] R/R THE CHARGER ASSY. FOR M1674; THE R1 EMERGENCY SLIDE LIGHT OP?S CHECKS IAW AMM 33-51-06.
- [SDR SWAA2025031094471](https://openairdocs.org/sdr/SWAA2025031094471), Feb 8, 2025: COMPRESSOR. STALLED. #1 ENG COMPRESSOR STALL ON TAKEOFF ROLL; PAX REPORT FLAMES OUT OF BACK OF ENGINE SMELL NOTED IN CABIN UNEVENTFUL LANDING (SMOOTH ROLLOUT) <[01]. PERFORMED COMPR
- [SDR SWAA2025011384163](https://openairdocs.org/sdr/SWAA2025011384163), Jan 8, 2025: FAIRING. CRACKED. LOWER BODY FAIRING 193D HAS DAMAGE. REMOVED PANEL 193D IAW AMM 53-51-21. INSTALLED PANEL 193D REF AMM 53-51-21.
- [SDR SWAA2025010884161](https://openairdocs.org/sdr/SWAA2025010884161), Jan 8, 2025: FAIRING. DELAMINATED. 194GL HAS TWO AREAS OF DELAMINATION ON PANEL. REF TTG8Q00Y1F7A AND TTG8Q00Y1HPD FOR REPLACEMENT OF PANEL 194GL
- [SDR SWAA2025010884158](https://openairdocs.org/sdr/SWAA2025010884158), Jan 8, 2025: FAIRING. DELAMINATED. WING TO BODY FAIRING 194CL 3EA AREAS OF DELAMINATION. R&R WING TO BODY FAIRING PER AMM 53-51-21
- [SDR SWAA2025010681968](https://openairdocs.org/sdr/SWAA2025010681968), Dec 31, 2024: BATTERY PACK. INOPERATIVE. EXTERIOR EMERGENCY LIGHT NEAR FWD SERVICE DOOR INOP.<[01] REMOVED AND REPLACED M1674 EMERGENCY LIGHT POWER SUPPLY PER AMM 33-51-06. OPS CHECK GOOD.

All 272: https://openairdocs.org/aircraft/N288WN/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.