# N417WN: 2001 Boeing 737-7H4, registration cancelled 2025-09-29

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: September 29, 2025
- Status when cancelled: Valid registration
- Airframe: [Boeing 737-7H4](https://openairdocs.org/model/boeing-737-7h4) (registry code 1384404)
- Engine: [CFM International CFM56 series](https://openairdocs.org/engine/cfm-international-cfm56-series) (registry code 13802)
- Data sheets: [TCDS A16WE](https://openairdocs.org/tcds/A16WE) (OpenAirDocs)
- Serial number: 29822
- Year built: 2001
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: November 8, 2001
- Certificate issued: April 26, 2002
- Last registry action: October 13, 2023
- Mode S code: A4F022
- Owner when cancelled: [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 was based
- The mark today: https://openairdocs.org/aircraft/N417WN
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=417WN
- Page: https://openairdocs.org/deregistered/N417WN-2025-09-29

From the FAA registry file of October 29, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe.

ADs and bulletins for the Boeing 737-7H4: https://openairdocs.org/model/boeing-737-7h4.md

## Service difficulty reports (318, newest 50)

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR SWAA2025050566699](https://openairdocs.org/sdr/SWAA2025050566699), May 2, 2025: INLET. PULLED. #2 ENGINE INLET HAS 17 FASTENERS PULLED THRU ON OUTBOARD SIDE 3OCLOCK POSITION.<[01] REMOVED #2 ENGINE INLET REF AMM 71-11-01;[02] 01 - REMOVED AND REPLACED PER
- [SDR SWAA2025041524243](https://openairdocs.org/sdr/SWAA2025041524243), Apr 13, 2025: SKIN. DEBONDED. LEFT OUTBOARD TRAILING EDGE FLAP UPPER SKIN HAS MISSING AND DISBONDED/DEFORMED MATERIAL ON THE INBD EDGE AND 10IN FROM THE TRAILING EDGE<[01] REMOVED LH OTBD TR
- [SDR SWAA2025041424037](https://openairdocs.org/sdr/SWAA2025041424037), Apr 12, 2025: SLIDE. LOOSE. FWD SERVICE DOOR SLIDE LOOSE<[01] FOUND GIRT ASSY UNFOLDED. C/W ESCAPE SLIDE PACK CHECK AND FOLDED GIRT ASSY IAW AMM 25-66-01
- [SDR SWAA2025041423226](https://openairdocs.org/sdr/SWAA2025041423226), Apr 10, 2025: SKIN. DEBONDED. LEFT OUTBOARD TRAILING EDGE FLAP UPPER SKIN HAS MISSING AND DISBONDED/DEFORMED MATERIAL ON THE INBD EDGE AND 10IN FROM THE TRAILING EDGE.<[01] PERFORMED EA- 25-
- [SDR SWAA2024112060963](https://openairdocs.org/sdr/SWAA2024112060963), Nov 17, 2024: LENS. OUT OF ADJUST. FWD ENTRY EMERY LIGHT LENS<[01] REINSTALLED FWD ENTRY EMERG LIGHT LENS PER AMM 33-51-00
- [SDR SWAA2024111358293](https://openairdocs.org/sdr/SWAA2024111358293), Nov 10, 2024: BATTERY PACK. INOPERATIVE. FWD GALLEY EMERGENCY EXIT SIGNS LIGHTS INOP.<[01] REMOVED AND REPLACED FWD GALLEY EMERGENCY EXIT LIGHTS BATTERY PACKS PER AMM 33-51-06.
- [SDR SWAA2024091236152](https://openairdocs.org/sdr/SWAA2024091236152), Sep 11, 2024: SLIDE. BULGED. FWD ENTRY DOOR SLIDE BULGING OUT ON AFT LOWER SIDE<[01] REMOVED AND REPLACED FWD ENTRY DOOR SLIDE REF AMM 25-66-01 AND TASK CARD 25-66-01. REFERENCE TTG8Q00VSP6
- [SDR SWAA2024083032419](https://openairdocs.org/sdr/SWAA2024083032419), Aug 29, 2024: SLIDE. OUT OF ADJUST. F/A REPORTS RT FORWARD SERVICE DOOR SLIDE EXTENDS FROM BOTTOM FURTHER THEN NORMAL<[01] RESCURED SLIDE PER AMM 25-66-00
- [SDR SWAA2024061400443](https://openairdocs.org/sdr/SWAA2024061400443), Jun 11, 2024: SKIN. PULLED. #2 ENGINE INLET COWL HAS MULTIPLE RIVETS PULLED THROUGH INLET SKIN. FWD AND AFT EDGES<[01] REMOVED AND REPLACED #2 ENGINE INLET COWL IAW AMM 71-11-01. OPS CHECK
- [SDR SWAA2024052288194](https://openairdocs.org/sdr/SWAA2024052288194), May 20, 2024: SLIDE. DISLODGED. R1 DOOR SLIDE PARTIALLY DISLODGED<[01] SECURED SLIDE PER MT 725-61-06
- [SDR SWAA2024031462578](https://openairdocs.org/sdr/SWAA2024031462578), Mar 13, 2024: SEAL. CRACKED. LH HORIZONTAL STABILIZER FWD LOWER SLIDING SEAL CRACKED.<[01] 01 - REMOVED AND REPLACED PER [AMM 53-31-31-000-803-NG (STABILIZER-TO-BODY LOWER FRONT SPAR SLIDIN
- [SDR SWAA2024031362566](https://openairdocs.org/sdr/SWAA2024031362566), Mar 13, 2024: BATTERY PACK. NO TEST. EMX LIGHT BATT PACK M01674 FAILS CAPACITANCE CHECK<[01] 01 - REMOVED AND REPLACED EMX BATTERY PACK M01674 PER [AMM 33-51-06-960-805-NG (POWER SUPPLY - BATTERY P
- [SDR SWAA2024031362565](https://openairdocs.org/sdr/SWAA2024031362565), Mar 13, 2024: BATTERY PACK. NO TEST. EMX LIGHT BATT PACK M01668 FAILS CAPACITANCE CHECK<[01] 01 - REMOVED AND REPLACED EMX BATTERY PACK M01668 PER [AMM 33-51-06-960-805-NG (POWER SUPPLY - BATTERY P
- [SDR SWAA2024022053492](https://openairdocs.org/sdr/SWAA2024022053492), Feb 17, 2024: SLIDE. LOW PRESSURE. FWD SERVICE DOOR SLIDE PRESSURE OUT OF RANGE<[01] R/R FWD SERVICE DOOR SLIDE PER MT 725-61-06FS
- [SDR SWAA2023112223910](https://openairdocs.org/sdr/SWAA2023112223910), Nov 22, 2023: LIGHT. DAMAGED. ROW 1ABC PHOTOLUMINESENT STRIP HAS MOISTURE IN IT.<[01] R/R ROW 1ABC PHOTOLUMINESCENT STRIP IAW AMM 33-51-15
- [SDR SWAA2023103015501](https://openairdocs.org/sdr/SWAA2023103015501), Oct 28, 2023: LAMP. INOPERATIVE. RIGHT OVERWING EXIT WINDOW LIGHT INOP. RELAMPED IAW AMM 33-51-01. OPS CHECK GOOD.
- [SDR SWAA2023082391898](https://openairdocs.org/sdr/SWAA2023082391898), Aug 20, 2023: LENS. BROKEN. CREW REPORTS; L1 DOOR ON FWD LAV AFT WALL EMERGENCY EXIT SIGN LENS FELL OFF / BROKEN<[01] R&R?D L1 DOOR ON FWD LAV AFT WALL EMERGENCY EXIT SIGN LENS IN REF. TO 
- [SDR SWAA2023072080367](https://openairdocs.org/sdr/SWAA2023072080367), Jul 19, 2023: SLIDE. OUT OF POSITION. AFT SERVICE DOOR SLIDE INSPECTION STICKER BLOCKS NEEDLE HARD TO READ<[01] FOUND AFT ENTRY DOOR SLIDE INSPECTION DECAL MISPOSITIONED ; REPLACED DOOR SLIDE DECAL 
- [SDR SWAA2023071174613](https://openairdocs.org/sdr/SWAA2023071174613), Jul 4, 2023: BATTERY PACK. INOPERATIVE. EMERGENCY LIGHTS ASSOCIATED WITH BATTERY PACK M1670 ARE INOP<[01] COMPLETED STEP 1.;[02] REPLACED M1670 EMERGENCY LIGHTS BATTERY AND TESTED PER AMM 33-51-06-960
- [SDR SWAA2023071761688](https://openairdocs.org/sdr/SWAA2023071761688), Jun 20, 2023: STIFFENER. CRACKED. LEFT HORIZONTAL STABILIZER RIB 2ND STIFFENER IS CRACKED AT STAB STA 129.50<[01] REMOVED THE DAMAGED PART AT LH HORIZONTAL STABILIZER STA 129.50 RIB 2ND VERTICAL
- [SDR SWAA2023071761681](https://openairdocs.org/sdr/SWAA2023071761681), Jun 20, 2023: STRINGER. CRACKED. CRACKED STRINGER END AT AREA AFT OF FWD CARGO BAY BS540 STR 23R<[01] REMOVED EXISTING REPAIR AT FCB STA-500D TO STA-540 STR-23R IAW SRM 51-40-02-0G-0;[02] UPDAT
- [SDR SWAA2023071761683](https://openairdocs.org/sdr/SWAA2023071761683), Jun 20, 2023: STRINGER. CRACKED. CRACKED STRINGER END AT AREA AFT OF FWD CARGO BAY BS540 STR 26R<[01] CUT AND REMOVED DAMAGED STRINGER FCB STR-26R STA-500D+10'' IAW SRM 51-10-02-0G-0;[02] PARTI
- [SDR SWAA2023071761684](https://openairdocs.org/sdr/SWAA2023071761684), Jun 20, 2023: STRINGER. CRACKED. CRACKED STRINGER END AT AREA AFT OF FWD CARGO BAY BS540 STR 23L<[01] PARTIALLY COMPLETED STEPS 1-2;[02] REMOVED DAMAGED STRINGER SECTION FROM BS 500D+7 TO BS 53
- [SDR SWAA2023071761685](https://openairdocs.org/sdr/SWAA2023071761685), Jun 20, 2023: STRINGER. CRACKED. CRACKED STRINGER END AT AREA AFT OF FWD CARGO BAY BS540 STR 26R BS 540 STR 26L<[01] PARTIALLY COMPLETED STEPS 1-2;[02] REMOVED DAMAGED STRINGER SECTION FROM BS 
- [SDR SWAA2023071261682](https://openairdocs.org/sdr/SWAA2023071261682), Jun 20, 2023: STRINGER. CRACKED. CRACKED STRINGER END AT AREA AFT OF FWD CARGO BAY BS540 STR 25R<[01] CUT AND REMOVED DAMAGED STRINGER FCB STR-25R STA-500D+10'' IAW SRM 51-10-02-0G-0;[02] UPDAT
- [SDR SWAA2023071161686](https://openairdocs.org/sdr/SWAA2023071161686), Jun 20, 2023: THRESHOLD. CORRODED. AFT CARGO BAY SUBTHRESHOLD IS CORRODED. CORROSION IS MEASURED FROM FWD EDGE OF PART AND IS MARKED ACCORDINGLY. (+8 TO+14); (+14 TO +16); (+17 TO+19); (+23 TO +2
- [SDR SWAA2023071161703](https://openairdocs.org/sdr/SWAA2023071161703), Jun 20, 2023: THRESHOLD. CORRODED. AFT CARGO BAY SUB THRESHOLD CORRODED. CORROSION MEASURED FROMFWD EDGE AND IS MARKED ACCORDINGLY. (+36 TO +37); (+39); (+41 TO +42); (+44)<[01] REMOVED CORROSION
- [SDR SWAA2023071760761](https://openairdocs.org/sdr/SWAA2023071760761), Jun 19, 2023: PANEL. CRACKED. VERTICAL FIN PANEL 324AL LOWER CLIP IS CRACKED<[01] CRACKED ON VERTICAL FIN PANEL 324AL LOWER CLIP WITH NEXT DIMENSION L=3.220 TOOL USED CALIPER 2738; DUE:04/20
- [SDR SWAA2023071760757](https://openairdocs.org/sdr/SWAA2023071760757), Jun 19, 2023: SKIN. CORRODED. SPOTTY SKIN CORROSION; BS1050 -1088; BETWEEN SKATE ANGLE AND AFT LEFT VERTICAL FIN FWD SUPPORT ANGLE<[01] SEVERAL AREAS OF CORROSION ON THE ANGLE AT BS 1036 FRO
- [SDR SWAA2023071760668](https://openairdocs.org/sdr/SWAA2023071760668), Jun 19, 2023: PLATE. CRACKED. LEFT WING LOWER T/E WIGGLE PLATE IS CRACKED AND LOOSE JUST I/B OF #1 PYLON<[01] REMOVED AND REPLACED LEFT WING LOWER T/E WIGGLE PLATE I/B OF #1 PYLON<BR>IAW SRM
- [SDR SWAA2023071260663](https://openairdocs.org/sdr/SWAA2023071260663), Jun 19, 2023: FLOOR PANEL. PULLED. CENTER CABIN FLOOR PANEL 242CF HAS A PULLED THROUGH INSERT<[01] IDENTIFIED FLOOR PANEL 242CF MATERIAL IAW SRM 53-00-50-0I-1 FIGURE 4 TABLE 4 AND BWG DWG 144A581
- [SDR SWAA2023071159999](https://openairdocs.org/sdr/SWAA2023071159999), Jun 18, 2023: SCUFF PLATE. CRACKED. AFT CARGO BAY FWD CORNER SCUFF PLATE IS CRACKED; INCLUDNG ACROSS PREVIOUS WELD REPAIR<[01] VERIFIED APPLICABILITY PER SRM NOT ALLOWABLE DAMAGE PARTS DO NOT HAVE
- [SDR SWAA2023071759983](https://openairdocs.org/sdr/SWAA2023071759983), Jun 17, 2023: STIFFENER. CRACKED. LEFT HORIZONTAL STABILIZER RIB 3RD STIFFENER IS CRACKED AT STAB STA 129.50<[01] REMOVED THE DAMAGED PART AT LH HORIZONTAL STABILIZER STA 129.50 RIB 3RD VERTICAL
- [SDR SWAA2023071759980](https://openairdocs.org/sdr/SWAA2023071759980), Jun 16, 2023: WEB. CRACKED. BS 663 LH SIDE VAPOR BARRIER WEB HAS CRACKS AND A TEMPORARY REPAIR; LBL 6 TO LBL 15.<[01] IDENTIFIED IAW SRM 57-10-10-0I-2 FIGURE 2 TABLE 2 ITEM 4<BR><BR>DAMAGE
- [SDR SWAA2023071759572](https://openairdocs.org/sdr/SWAA2023071759572), Jun 16, 2023: PANEL. PULLED. R/W L/E PANEL 621PB HAS PULLED FASTENER HOLE (MARKED)<[01] IDENTIFIED PART AND MATERIAL IAW SRM 57-41-01-0I-4 FIGURES 1+3; TABLE 3; ITEM [1].<BR>FOUND DAMAGE TO
- [SDR SWAA2023071759574](https://openairdocs.org/sdr/SWAA2023071759574), Jun 16, 2023: PANEL. PULLED. L/W L/E PANEL 621HB HAS PULLED FASTENER HOLES (MARKED)<[01] IDENTIFIED PANEL 621HB MATERIAL IAW SRM 57-41-01-0I-4; FIGURE 4; SHEET1; TABLE 4; ITEM [1]. <BR><BR>
- [SDR SWAA2023071759577](https://openairdocs.org/sdr/SWAA2023071759577), Jun 16, 2023: PANEL. PULLED. R/W L/E PANEL 621SB HAS PULLED FASTENER HOLES (MARKED)<[01] IDENTIFIED PANEL 621SB MATERIAL IAW SRM 57-41-01-0I-4 TABLE 3 FIGURE 3 ITEM 1. DAMAGE AT DISCREPANT 
- [SDR SWAA2023071759970](https://openairdocs.org/sdr/SWAA2023071759970), Jun 16, 2023: PANEL. PULLED. L/W L/E PANEL 521TB HAS PULLED FASTENER HOLES (MARKED)<[01] IDENTIFIED 521TB PANEL IAW SRM 57-41-01-0I-4 FIGURE 3; ITEM 1; TABLE 3<BR>FOUND DAMAGE TO BE OUT OF 
- [SDR SWAA2023071759974](https://openairdocs.org/sdr/SWAA2023071759974), Jun 16, 2023: PANEL. PULLED. L/W L/E PANEL 521JB HAS PULLED FASTENER HOLES (MARKED)<[01] IDENTIFIED PANEL MATERIAL IAW SRM 57-41-01-0I-4 FIG 4 TABLE 4 ITEM 1.<BR>FOUND DAMAGE TO 3EA FASTENE
- [SDR SWAA2023071759973](https://openairdocs.org/sdr/SWAA2023071759973), Jun 16, 2023: PANEL. PULLED. L/W L/E PANEL 521MB HAS PULLED FASTENER HOLES (MARKED)<[01] IDENTIFIED PANEL 521MB IAW SRM 57-41-01-0I-4 FIGURE 4 ITEM [1]; DAMAGE TO THE PANEL IS BEYOND THE AL
- [SDR SWAA2023071759972](https://openairdocs.org/sdr/SWAA2023071759972), Jun 16, 2023: PANEL. PULLED. L/W L/E PANEL 521QB HAS PULLED FASTENER HOLES (MARKED)<[01] IDENTIFIED 521QB PANEL IAW SRM 57-41-01-0I-4 FIGURE 3; ITEM 1; TABLE 3<BR>FOUND DAMAGE TO BE OUT OF 
- [SDR SWAA2023071759971](https://openairdocs.org/sdr/SWAA2023071759971), Jun 16, 2023: PANEL. PULLED. L/W L/E PANEL 521WB HAS PULLED FASTENER HOLES (MARKED)<[01] IDENTIFIED 521WB PANEL IAW SRM 57-41-01-0I-4 FIGURE 2; ITEM 1; TABLE 2<BR>FOUND DAMAGE TO BE OUT OF 
- [SDR SWAA2023071759976](https://openairdocs.org/sdr/SWAA2023071759976), Jun 16, 2023: PANEL. PULLED. L/W L/E PANEL 521CB HAS PULLED FASTENER HOLES (MARKED)<[01] IDENTIFIED PANEL MATERIAL IAW SRM 57-41-01-0I-4 FIG 5 TABLE 5 ITEM 3.<BR>FOUND DAMAGE TO 3EA FASTENE
- [SDR SWAA2023061659140](https://openairdocs.org/sdr/SWAA2023061659140), Jun 14, 2023: SPAR CAP. CORRODED. RT WING LOWER FWD SPAR CAP SHOWS EVIDENCE OF CORROSION UNDER PANEL 621DB APPROX WS 293.0. EVALUATED EXFOLIATION CORROSION ON LOWER CHORD RT WING LOWER FWD SPAR 
- [SDR SWAA2023030611235](https://openairdocs.org/sdr/SWAA2023030611235), Feb 28, 2023: HANDLE. LOOSE. FLIGHT ATTENDANT REPORTS AFT ENTRY DOOR HANDLE IS LOOSE<[01] SECURED AFT ENTRY DOOR HANDLE IAW M/M 52-13-31
- [SDR SWAA2023030110978](https://openairdocs.org/sdr/SWAA2023030110978), Feb 28, 2023: SLIDE. MISSING. FORWARD SERVICE DOOR SLIDE IS MISSING VELCRO MANUAL HANDLE COVER<[01] REMOVED AND REPLACED FWD SERVICE DOOR SLIDE PER MT 725-61-06
- [SDR SWAA2023020800065](https://openairdocs.org/sdr/SWAA2023020800065), Feb 6, 2023: SLIDE. OUT OF POSITION. L2 SLIDE APPEARS DISLODGED<[01] REPOSITIONED L2 SLIDE IN CASE IAW AMM 25-66-01 OK FOR SERVICE
- [SDR SWAA2023011791756](https://openairdocs.org/sdr/SWAA2023011791756), Jan 15, 2023: LAMP. INOPERATIVE. LEFT AFT EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMPS IAW AMM 33-51-04.
- [SDR SWAA2022113076657](https://openairdocs.org/sdr/SWAA2022113076657), Nov 30, 2022: BATTERY PACK. NO TEST. FORWARD RT EMERGENCY LIGHT BATTERY PACK FAILED A CAPACITY TEST. REMOVED AND REPLACED THE BATTERY PACK IAW MM 33-51-06.
- [SDR SWAA2022111170118](https://openairdocs.org/sdr/SWAA2022111170118), Nov 10, 2022: GAUGE. OBSTRUCTED. AFT ENTRY DOOR SLIDE PRESSURE GAUGE NEEDLE COVERED BY INSPECTION STICKER. REMOVED SLIDE AND UNCOVERED NEEDLE AND REINSTALLED SLIDE PER MT 725-61-06.

All 318: https://openairdocs.org/deregistered/N417WN-2025-09-29/reports.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.