# N285WN: 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: 32536
- Year built: 2007
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: August 3, 2007
- Certificate issued: August 25, 2007
- Expires: February 29, 2028
- Mode S code: A2E28F
- 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=285WN
- Page: https://openairdocs.org/aircraft/N285WN

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 N285WN.

## FAA accident and incident reports

None matched to N285WN.

## Service difficulty reports (318, 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 SWAA2026101234484](https://openairdocs.org/sdr/SWAA2026101234484), Oct 6, 2026: LIGHT. INOPERATIVE. LEFT OVERWING EMERGENCY EXIT, EXTERNAL EMERGENCY LIGHT NOT WORKING. REPLACED THE EXTERNAL EMERGENCY LIGHT IAW AMM 33-51-04-960-801. OPS CHECKED GOOD.
- [SDR SWAA2026080572858](https://openairdocs.org/sdr/SWAA2026080572858), Aug 1, 2026: STRUT. CRACKED. RIGHT ENGINE TRF STRUT 1 WAS CRACKED AT C-1, 0.28 LONG. MERGED BOTH CRACKS TOGETHER ON ONE WRITE UP TTG8Q01DGQ1X.
- [SDR SWAA2026080594116](https://openairdocs.org/sdr/SWAA2026080594116), Aug 1, 2026: STRUT. CRACKED. RIGHT ENGINE TRF STRUT NR 1 IS CRACKED AT C-1 0.28 LONG AND C-2 0.49 LONG. COMPLIED WITH M-21-172-00810 TO TRIGGER EO-7256-I-11716-C THE REPETITIVE INSPECTION I
- [SDR SWAA2025100219639](https://openairdocs.org/sdr/SWAA2025100219639), Sep 29, 2025: LENS. MISSING. R-1 DOOR EMERGENCY EXIT SIGN MISSING. INSTALLED A NEW LENS IAW MM 33-51-01 OPS CHKD NORMAL
- [SDR SWAA2025060276329](https://openairdocs.org/sdr/SWAA2025060276329), May 30, 2025: HANDLE. LOOSE. LOOSE AFT SERVICE DOOR HANDLE. <[01] TIGHTENED LOOSE AFT SERVICE DOOR HANDLE IAW AMM 25-21-25-420-801. STEP 3.B(5); [02] CORRECTIVE ACTION ITEM 1 VERIFIED; CARD
- [SDR SWAA2025060276001](https://openairdocs.org/sdr/SWAA2025060276001), May 29, 2025: BATTERY PACK. INOPERATIVE. EMERGENCY EXIT LIGHTS ASSOCIATED WITH BATTERY PACK M1672 INOP <[01]. REMOVED; REPLACED WITH SERVICEABLE UNIT AND PERFORMED GOOD INSTALLATION TEST OF M1672 BATTE
- [SDR SWAA2025060274803](https://openairdocs.org/sdr/SWAA2025060274803), May 24, 2025: BATTERY PACK. FAILED. LIGHT ASSOCIATED WITH EMERGENCY BATTERY PACK M1670 FAIL<[01] REMOVED AND REPLACED AND PERFORMED GOOD TEST OF BATTERY PACK M1670 IAW AMM 33-51-06-960-805;[02] VE
- [SDR SWAA2025060274804](https://openairdocs.org/sdr/SWAA2025060274804), May 24, 2025: BATTERY PACK. FAILED. LIGHT ASSOCIATED WITH EMERGENCY BATTERY PACK M1675 FAIL<[01] REMOVED AND REPLACED AND PERFORMED GOOD TEST OF BATTERY PACK M1675 IAW AMM 33-51-06-960-805;[02] VE
- [SDR SWAA2025060274802](https://openairdocs.org/sdr/SWAA2025060274802), May 24, 2025: BATTERY PACK. FAILED. LIGHT ASSOCIATED WITH EMERGENCY BATTERY PACK M1669 FAIL<[01] REMOVED AND REPLACED BATTERY PACK M1669 AND PERFORMED GOOD TEST IAW AMM 33-51-06-960-805;[02] VERIF
- [SDR SWAA2025060274531](https://openairdocs.org/sdr/SWAA2025060274531), May 23, 2025: SKIN. DELAMINATED. DELAMINATED LOWER SURFACE AFT TRAILING EDGE RH MAIN INB FLAP<[01] OK TO INSTALL;[02] REMOVED AFT TRAILING EDGE RH MAIN I/B FLAP AND INSTALLED NEW AFT TRAILING E
- [SDR SWAA2025060272385](https://openairdocs.org/sdr/SWAA2025060272385), May 18, 2025: STRIP. CORRODED. ACB 140AF L/H CAPSTRIP CORRODED<[01] REMOVED AND INSTALLED NEW CAPSTRIP ITEM# 453A2611-8; S/N 7253311; PER SRM 51-40-02-0G-0; AMM 25-52-10-000-801; AMM 25-52-10
- [SDR SWAA2025060272386](https://openairdocs.org/sdr/SWAA2025060272386), May 18, 2025: STRIP. CORRODED. ACB 140CF L/H CAPSTRIP CORRODED<[01] REMOVED AND INSTALLED NEW CAPSTRIP ITEM# 453A2611-4; LOT#1510184-1 PER SRM 51-40-02-0G-0; AMM 25-52-10-000-801; AMM 25-52-1
- [SDR SWAA2025060272172](https://openairdocs.org/sdr/SWAA2025060272172), May 17, 2025: LIGHT. DAMAGED. AFT ENTRY CEILING EMERGENCY EXIT LIGHT HOUSING DAMAGED<[01] REMOVED DAMAGED AFT ENTRY CEILING EMERGENCY EXIT LIGHT HOUSING IAW AMM 33-51-01-960-802.;[02] REPLAC
- [SDR SWAA2025060270164](https://openairdocs.org/sdr/SWAA2025060270164), May 13, 2025: SUPPORT BRACKET. CRACKED. CRACK FOUND ON SUPPORT BRACKET OVER WHEEL AT BS 692.1 RBL 2 WL 208.1.<[01] REMOVED AND REPLACED SUPPORT BRACKET OVER WHEEL AT BS-692.1; RBL-2; WL-208.1 IAW SRM 
- [SDR SWAA2025060269360](https://openairdocs.org/sdr/SWAA2025060269360), May 9, 2025: SUPPORT BRACKET. CRACKED. CRACKED ON CHORD BS695; RBL2; BELOW UPPER DECK<[01] REPAIRED PER EA 25-153-01245-WIP1;[02] VERIFIED ACTION 1.<BR>JOB COMPLETE.
- [SDR SWAA2025060268958](https://openairdocs.org/sdr/SWAA2025060268958), May 9, 2025: SIGN. BROKEN. FWD LAV EMERGENCY EXIT LIGHT IS BROKEN.<[01] REMOVED AND REPLACED FWD LAV EMERGENCY EXIT SIGN IAW AMM 33-51-01-960-802. <BR>OPS TEST WILL BE ACCOMPLISHED ON TAS
- [SDR SWAA2025060268959](https://openairdocs.org/sdr/SWAA2025060268959), May 9, 2025: SIGN. BROKEN. G-1 EMERGENCY EXIT LIGHT IS BROKEN.<[01] REMOVED AND REPLACED FWD LAV EMERGENCY EXIT SIGN IAW AMM 33-51-01-960-802. <BR>OPS TEST WILL BE ACCOMPLISHED ON TASK CA
- [SDR SWAA2025060269359](https://openairdocs.org/sdr/SWAA2025060269359), May 9, 2025: ACCESS PANEL. CRACKED. CRACKED ON 831 ACCESS PANEL AT FWD ENTRY DOOR<[01] REMOVED 831DZ ACCESS PANEL IAW AMM 05-41-08-210-807;[02] OK TO CLOSE;[03] COMPLETED. INSTALLED 831DZ ACCESS P
- [SDR SWAA2025060268960](https://openairdocs.org/sdr/SWAA2025060268960), May 9, 2025: ATTACH FITTING. EXCESS PLAY. EXCESSIVE PLAY IN BOTH FWD AND AFT GIRT BAR FLOOR ATTACH FITTINGS AT ASD.<[01] REMOVED AND REPLACED FWD AND AFT GIRT BAR FLOOR ATTACH FITTINGS AT ASD IAW AMM 25
- [SDR SWAA2025060268534](https://openairdocs.org/sdr/SWAA2025060268534), May 7, 2025: STRAP. CRACKED. STABILIZER STRAP IS CRACKED AT BS312+10 BL0; WL198<[01] REMOVED AND REPLACED STABILIZER STRAP P/N 141A5410-31 BS312 - BS344 BL 0 WL198 IAW SRM 51-40-02 AND DWG 
- [SDR SWAA2025060268109](https://openairdocs.org/sdr/SWAA2025060268109), May 7, 2025: RIB. DEFORMED. L/H HORIZONTAL STABILIZER REMOVABLE LEADING EDGE 331B STIFFENER IS DEFORMED AT LE STA 114<[01] UPON FURTHER INVESTIGATION LIGHTLY DEFORMATION FOUND ON RIB STIFF
- [SDR SWAA2025060267171](https://openairdocs.org/sdr/SWAA2025060267171), May 3, 2025: THRESHOLD WEB. CORRODED. ACD; THRESHOLD HAS CORROSION BS 787+20 RBL 24 AND 787+24 RBL 29 (MARKED).<[01] REMOVED AND REPLACED ACB THRESHOLD WEB I.A.W SRM 51-40-02-0G-0 AND DWG 146A8340 I
- [SDR SWAA2025060267164](https://openairdocs.org/sdr/SWAA2025060267164), May 3, 2025: STIFFENER. CRACKED. ACB; ANGLE IS CRACK BEHIND TO WATER SERVICE PANEL BS 907+11 RBL 9 (MARKED).<[01] REMOVED AND INSATLLED NEW STIFFINER ITEM # 147A7221Y32 LOT# 1567118-1 BN 39 PER
- [SDR SWAA2025060267166](https://openairdocs.org/sdr/SWAA2025060267166), May 3, 2025: ANGLE. CORRODED. ACB; ZEE ANGLE HAS SEVERAL SPOTS WITH CORROSION AT BS 727 TO 847 LBL 23 (MARKED).<[01] REMOVED AND REPLACED ON ACB FLOOR TO SIDEWALL SUPPORT FROM BS 727 TO BS 8
- [SDR SWAA2025060267167](https://openairdocs.org/sdr/SWAA2025060267167), May 3, 2025: ANGLE. CORRODED. ACB; ZEE ANGLE HAS SEVERAL SPOTS WITH CORROSION AT BS 727 TO 767 RBL 23 (MARKED).<[01] REMOVED AND REPLACED ON ACB; NEW FLOOR TO SIDEWALL SUPPORT LOCATED BTW. S
- [SDR SWAA2025060267168](https://openairdocs.org/sdr/SWAA2025060267168), May 3, 2025: SHIELD. CORRODED. ACB; SUBTHRESHOLD HAS CORROSION AT BS 767 TO 787+7 RBL 23.<[01] VERIFIED OUT OF LIMITS;[02] REMOVED AND REPLACED FWD SHIELD AT BS 767 TO 787+7 RBL 23 IAW SRM 51
- [SDR SWAA2025060266809](https://openairdocs.org/sdr/SWAA2025060266809), May 2, 2025: SIDEWALL SUPPORT. CORRODED. FCB - CORROSION ON SIDEWALL SUPPORT BS500A+14; BS500B+6; BS500B+10; BS500B+18; 500C+2 RBL 24.5 WL 156 (MARKED)<[01] REMOVED AND REPLACED FLOOR TO SIDEWALL SUPPO
- [SDR SWAA2025060268108](https://openairdocs.org/sdr/SWAA2025060268108), May 2, 2025: SHIELD. CORRODED. FCB - CORROSION ON AFT SHIELD BS500+9.5 RBL 22 WL 156 (MARKED)<[01] REMOVED AND REPLACED AFT SHIELD AT FCB BS492 TO BS 500A RBL22 WL156 IAW SRM 51-10-02-0G-0 PA
- [SDR SWAA2025060266658](https://openairdocs.org/sdr/SWAA2025060266658), May 2, 2025: FAIRING. DELAMINATED. PANEL 643EB (#7 CANOE FAIRING CONE) IS DELAMINATED.<[01] RECEIVED NEW PANEL 643EB LOCATED AND DRILLED IAW SRM 51-40-05 AND AIPC 27-51-28-04;;[02] RECEIVED NEW P
- [SDR SWAA2025060266810](https://openairdocs.org/sdr/SWAA2025060266810), May 2, 2025: SIDEWALL SUPPORT. CORRODED. FCB - CORROSION ON SIDEWALL SUPPORT BS500A+6; BS500A+10; BS500A+14; BS500A+18 LBL 24.75 WL 156 (MARKED)<[01] REMOVED AND REPLACED FCB SIDEWALL SUPPORT FROM BS 4
- [SDR SWAA2025060266814](https://openairdocs.org/sdr/SWAA2025060266814), May 2, 2025: FLOOR SUPPORT. CORRODED. FCB - CORROSION ON FLOOR SUPPORT AFT BULKHEAD BS500C+18 RBL 12; LBL 14.5 WL 156 (MARKED)<[01] REMOVED AND REPLACED NEW FCB FLOOR SUPPORT AFT BULKHEAD BS500D RBL
- [SDR SWAA2025060266423](https://openairdocs.org/sdr/SWAA2025060266423), May 1, 2025: SUPPORT FRAME. CRACKED. WING TO BODY PANEL SUPPORT HAS CRACK AT BS 500D STR 19R<[01] REMOVE AND REPLACED WING TO BODY PANEL SUPPORT FRAME IAW SRM 51-10-02-0G-0 AND DWG# 116A3118 ID: 00
- [SDR SWAA2025060266420](https://openairdocs.org/sdr/SWAA2025060266420), May 1, 2025: FLOOR SUPPORT. CRACKED. CRACKED INTERCOSTAL AT FWD WET AREA BS321 LBL45 WL208. MARKED<[01] REMOVED AND REPLACED INTERCOSTAL AT FWD WET ARE BS 312-BS328 LBL45 I.A.W. SRM 51-40-02-0G-0 A
- [SDR SWAA2025060266419](https://openairdocs.org/sdr/SWAA2025060266419), May 1, 2025: FLOOR SUPPORT. CORRODED. CORROSION ON INTERCOSTAL AT FWD WET AREA BS291 BL0 WL208. MARKED<[01] REMOVED AND REPLACED INTERCOSTAL AT FWD WET ARE BS 277-BS294 BL0 I.A.W. SRM 51-40-02-0G-0 
- [SDR SWAA2025060266042](https://openairdocs.org/sdr/SWAA2025060266042), May 1, 2025: FLOOR PANEL. PULLED. AFT FLOOR PANEL 241XF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 241XF WITH AREAS OF PULLED UPPER STRANDS WAS REPAIRED IAW SRM 53-00-50-2R-1
- [SDR SWAA2025060266047](https://openairdocs.org/sdr/SWAA2025060266047), May 1, 2025: FLOOR PANEL. PULLED. AFT FLOOR PANEL 241AAF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 241AAF WITH AREAS OF UPPER SURFACE PULLED STRANDS WAS REPLACED BY FABRICATING A 
- [SDR SWAA2025060266051](https://openairdocs.org/sdr/SWAA2025060266051), May 1, 2025: FLOOR PANEL. CRACKED. AFT FLOOR PANEL 242XF LOWER SKIN IS CRACKED.<[01] DUE TO THE EXTENT OF DAMAGE; REPLACED AFT FLOOR PANEL 242XF IAW SRM 51-10-02-0G-0 PARA 9 AND AIPC 53-21-00-26 
- [SDR SWAA2025060266041](https://openairdocs.org/sdr/SWAA2025060266041), Apr 30, 2025: STUB FRAME. CRACKED. CRACK FOUND ON STUB FRAME BS 294.5 +8.5'; ABOVE SEAL DEPRESSOR; BETWEEN S-8R AND S-9R; LENGTH 1.6' (MARKED)<[01] REMOVED AND REPLACED STUB FRAME AT FWD SERVICE 
- [SDR SWAA2025060265864](https://openairdocs.org/sdr/SWAA2025060265864), Apr 30, 2025: PANEL. CRACKED. RT. ELEVATOR HINGE PANEL 344LB CRACKED.<[01] REPAIR OF PANEL ACCOMPLISHED ON WORK ORDER #582623 CUSTOMER PO: P006WAPC;[02] CORRECTIVE ACTION COMPLETED.
- [SDR SWAA2025060266039](https://openairdocs.org/sdr/SWAA2025060266039), Apr 30, 2025: SKIN. CRACKED. CRACK ON LH LOWER HORIZONTAL STABILIZER SKIN. AT STAB STA 193.90; 26' FROM FWD EDGE; .40' IN LENGTH (MARKED)<[01] REMOVED THE DAMAGED PART ON LH HORIZONTAL STAB
- [SDR SWAA2025060266038](https://openairdocs.org/sdr/SWAA2025060266038), Apr 30, 2025: SKIN. CRACKED. CRACK ON RH LOWER HORIZONTAL STABILIZER SKIN. AT STAB STA 193.90; 18' FROM FWD EDGE; .40' IN LENGTH (MARKED)<[01] REMOVED THE DAMAGED PART ON RH HORIZONTAL STAB
- [SDR SWAA2025060266040](https://openairdocs.org/sdr/SWAA2025060266040), Apr 30, 2025: BEAR STRAP. CRACKED. CRACK FOUND ON INNER BEAR STRAP OF FWD GALLEY DOOR(R1); BS 294.5; RBL 52; WL 265 BETWEEN S-8R AND S-9R; LENGTH 2.2' (MARKED)<[01] 'DAMAGE REPAIRED AS PER 737-70
- [SDR SWAA2025060265694](https://openairdocs.org/sdr/SWAA2025060265694), Apr 30, 2025: FLOOR PANEL. PULLED. FLOOR PANEL 242AF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 242AF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR P
- [SDR SWAA2025060265695](https://openairdocs.org/sdr/SWAA2025060265695), Apr 30, 2025: FLOOR PANEL. PULLED. FLOOR PANEL 242CF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 242CF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR P
- [SDR SWAA2025060265689](https://openairdocs.org/sdr/SWAA2025060265689), Apr 30, 2025: FLOOR PANEL. PULLED. FLOOR PANEL 231YF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 231YF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR P
- [SDR SWAA2025060265690](https://openairdocs.org/sdr/SWAA2025060265690), Apr 30, 2025: FLOOR PANEL. PULLED. FLOOR PANEL 241BF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 241BF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR P
- [SDR SWAA2025060265691](https://openairdocs.org/sdr/SWAA2025060265691), Apr 30, 2025: FLOOR PANEL. PULLED. FLOOR PANEL 232SF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DUE TO THE EXTENT OF DAMAGE; REPLACED FLOOR PANEL 232SF IAW SRM 51-10-02-0G-0 PARA 9 AND AIPC 53-
- [SDR SWAA2025060265692](https://openairdocs.org/sdr/SWAA2025060265692), Apr 30, 2025: FLOOR PANEL. PULLED. FLOOR PANEL 231XF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 231XF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR P
- [SDR SWAA2025060265693](https://openairdocs.org/sdr/SWAA2025060265693), Apr 30, 2025: FLOOR PANEL. PULLED. FLOOR PANEL 231ZF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DUE TO THE EXTENT OF DAMAGE; REPLACED FLOOR PANEL 231ZF IAW SRM 51-10-02-0G-0 PAR A9 AND AIPC 53-
- [SDR SWAA2025060265298](https://openairdocs.org/sdr/SWAA2025060265298), Apr 28, 2025: SCUFF PLATE. CRACKED. PASSENGER DOOR R1; SCUFF PLATE HAS A CRACK AT AFT UPPER EDGE AREA (MARKED).<[01] WELDED THE DAMAGED AREA ON SCUFF PLATE USING AMS4954 FILLER ROD LOT NUMBER M798

All 318: https://openairdocs.org/aircraft/N285WN/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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