# Boeing 737-73V

- Type: Aircraft model (FAA registry)
- Registry code: 1384540
- Manufacturer (registry): BOEING
- Model: 737-73V
- Aircraft type: Fixed wing multi engine
- Category: Airplane
- Engines: 2 · Turbo-fan
- Seats: 149
- Weight class: 20,000 lb and over
- Certification: Type certificated
- Registered aircraft: 2
- Page: https://openairdocs.org/model/boeing-737-73v

Model codes come from the FAA registry's reference file. ADs are matched to them by model name and maker.

## ADs that may apply (OpenAirDocs)

Matched to this model by model name and maker. Each AD's applicability may narrow it by serial number, part number or equipment.

None matched.

## Registered aircraft (2)

- [N558WN](https://openairdocs.org/aircraft/N558WN): [Southwest Airlines Co](https://openairdocs.org/faa-owner/SOUTHWEST%20AIRLINES%20CO), [Dallas, TX](https://openairdocs.org/faa-place/TX/Dallas), built 2002, S/N 30248
- [N561WN](https://openairdocs.org/aircraft/N561WN): [Wilmington Trust Co Trustee](https://openairdocs.org/faa-owner/WILMINGTON%20TRUST%20CO%20TRUSTEE), [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington), built 2003, S/N 32417

## NTSB investigations

None matched to aircraft with this model.

## 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.

- [Incident 20130418006529I](https://openairdocs.org/incident/20130418006529I), Apr 18, 2013: Boeing 737-73V (N710SY), Lansing, MI, Minor damage. On April 18, 2013 scna flight 266 enroute from dca to lan encountered moderate continuous turbulence while on approach to rwy 28L. Winds were reported by the…
- [Incident 20120328029199I](https://openairdocs.org/incident/20120328029199I), Mar 28, 2012: Boeing 737-73V (N711SY), Arlington, VA, Minor damage. On March 28, 2012, at 1011 EDT, sun country airlines flight scx 265, a Boeing 737-700 N711SY, was involved in an incident at ronald reagan Washington national…

## Service difficulty reports (1,826, newest 50)

As reported by operators and repair stations, by the model named in the report.

- [SDR SWAA2026062213876](https://openairdocs.org/sdr/SWAA2026062213876), Jun 18, 2026: SIGN. DETACHED. FORWARD ENTRY DOOR EXIT SIGN DETACHED. REATTACHED EXIT SIGN IAW AMM 33-51-01.
- [SDR SWAA2026060808664](https://openairdocs.org/sdr/SWAA2026060808664), Jun 3, 2026: LIGHT. INOPERATIVE. CENTER AISLE AT SEAT 26ABC CEILING MOUNTED EMERGENCY LIGHT INOPERATIVE. R & R EMERGENCY LIGHT IAW AMM 33-51-03.
- [SDR SWAA2026060808676](https://openairdocs.org/sdr/SWAA2026060808676), Jun 3, 2026: ISOLATION MOUNT. CRACKED. FWD SERVICE DOOR AFT ISOLATOR CRACKED. R & R FWD SERVICE DOOR AFT ISOLATOR IAW SRM 51-40-02. INSPECTION C/W R&R FWD SERVICE DOOR AFT ISOLATOR IAW SRM 51-40-02.
- [SDR SWAA2026020566836](https://openairdocs.org/sdr/SWAA2026020566836), Feb 2, 2026: DOUBLER. CRACKED. EXTERNAL GROUND POWER RECEPTACLE DOUBLER DAMAGED. REMOVED DAMAGED SECTION OF DOOR SURROUND DOUBLER IAW SRM 53-10-15-2R-4, ZONE 2 ALTERNATIVE 2, PERFORMED HFEC S
- [SDR SWAA2026020567948](https://openairdocs.org/sdr/SWAA2026020567948), Jan 29, 2026: WEEP HOLE. BLOCKED. NR 1 ENGINE WOULD NOT SPOOL UP FOR TAKEOFF . N1 WOULD NOT SPOOL UP, N2 WOULD. FOUND NR 1 ENGINE PS3 SENSE LINE WEEP HOLE BLOCKED. CLEANED IAW AMM 72-00-00. ENGI
- [SDR SWAA2026011961618](https://openairdocs.org/sdr/SWAA2026011961618), Jan 15, 2026: LIGHT. INOPERATIVE. RIGHT OVERWING EMERGENCY LIGHT INOPERATIVE. R & R RT OVERWING LIGHT IAW AMM 33-51-04.
- [SDR SWAA2025082608019](https://openairdocs.org/sdr/SWAA2025082608019), Aug 24, 2025: SLIDE. UNPACKED. AFT RIGHT EGRESS SLIDE NEED TO BE REPACKED. REPOSITIONED SLIDE IN CONTAINER PER MT 725-61-06.
- [SDR SWAA2025073195500](https://openairdocs.org/sdr/SWAA2025073195500), Jul 25, 2025: ANTI-SKID VALVE. OUT OF LIMITS. ANTI-SKID INOP ILLUM ON APPROACH<[01] PERFORMED ALT ANTI-SKID VALVE T/S REF FIM 32-42 TASK 805. FOUND R/H ALT ANTI-SKID VALCE OUT OF RESISTANCE. REMOVED AND REP
- [SDR SWAA2025070882301](https://openairdocs.org/sdr/SWAA2025070882301), Jun 16, 2025: ATTACH ANGLE. CRACKED. B.S. 663 LOWER COMPOSITE BULKHEAD UPPER ATTACH ANGLE IS CRACKED AT R.B.L. 10; W.L. 167.<[01] REPAIRED VAPOR BARRIER UPPER ATTACH ANGLE AT BS 663 BETWEEN RBL 5 T
- [SDR SWAA2025070882393](https://openairdocs.org/sdr/SWAA2025070882393), Jun 16, 2025: FLOORBEAM. CRACKED. CRACKED ANGLE ON FLOOR SUPPORT WING CENTER SECTION STA 685+7 LBL 23 WL 203 (MARKED)<[01] REMOVED AND REPLACED ANGLE ON FLOOR SUPPORT WING CENTER SECTION STA 685
- [SDR SWAA2025070882120](https://openairdocs.org/sdr/SWAA2025070882120), Jun 15, 2025: SCUFF PLATE. CRACKED. AFT CARGO BAY FWD CORNER SCUFF PLATE CRACKED<[01] REPAIRED AFT CARGO BAY FWD CORNER SCUFF PLATE PER SRM 53-60-15-2R-1. RESTORED FINISHES ON INNER SURFACE PER AM
- [SDR SWAA2025070782119](https://openairdocs.org/sdr/SWAA2025070782119), Jun 15, 2025: SCUFF PLATE. CRACKED. FWD CARGO BAY AFT CORNER SCUFF PLATE CRACKED<[01] LOCATED AND DRILLED NEW FCB AFT CORNER SCUFF PLATE IAW SRM 51-40-05 AND DWG143A8331;[02] LOCATED AND DRILLED N
- [SDR SWAA2025070781514](https://openairdocs.org/sdr/SWAA2025070781514), Jun 14, 2025: THRESHOLD WEB. CORRODED. CORROSION ON FCB DOOR CUTOUT SURROUND SUB-THRESHOLD BS460+5, RBL29, WL156. REMOVED AND REPLACED ON FCB DOOR CUTOUT SURROUND SUB-THRESHOLD WEB IAW SRM 51-40-02-0
- [SDR SWAA2025070880894](https://openairdocs.org/sdr/SWAA2025070880894), Jun 12, 2025: DOOR. CRACKED. L/H MLG STRUT DOOR IS CRACKED<[01] L/H MAIN LANDING GEAR STRUT DOOR REPAIRED ON WORK ORDER P007K2E9-1 JOB #583943.<BR>REMOVED AND REINSTALLED L/H MLG STRUT 'CEN
- [SDR SWAA2025061180307](https://openairdocs.org/sdr/SWAA2025061180307), Jun 11, 2025: BATTERY PACK. FAILED. R/H FWD. EMERGENCY LIGHTING BATTERY PACK FAILED THE CAPACITY CHECK. REMOVED & REPLACED R/H FWD EMERGENCY LIGHTING BATTERY PACK PER AMM 33-51-06.
- [SDR SWAA2025060376794](https://openairdocs.org/sdr/SWAA2025060376794), Jun 1, 2025: COVER. MISSING. 9C EMER LIGHT LENS COVER MISSING <[01]. OK TO CONTINUE PER MEL 33-15-02 SP1 SECURED WITH TAPE; [02] INSTALLED EMERGENCY LIGHT COVER AT SEAT 9C PER SIP.
- [SDR SWAA2025060275376](https://openairdocs.org/sdr/SWAA2025060275376), May 27, 2025: LAMP. INOPERATIVE. L/H EMERGENCY EXIT LIGHT INOP<[01] RELAMPED EMERGENCY EXIT LIGHT IAW AMM 33-51-01. OPS CKD GOOD.
- [SDR SWAA2025051971617](https://openairdocs.org/sdr/SWAA2025051971617), May 15, 2025: FLOOR PANEL. CRACKED. RAMP REPORTED AFT CARGO FLOOR PANEL CRACK<[01] OK TO CONTINUE PER MEL 25-16-01; SP#1B. AUTH#252257;[02] 01 - REMOVED AND REPLACED PER [AMM 25-52-10-401-NG (CARG
- [SDR SWAA2025050164931](https://openairdocs.org/sdr/SWAA2025050164931), Apr 28, 2025: DOUBLER. CRACKED. TRANSFERRING WORK FROM FAULT TTG8Q01034TE: EXTERNAL POWER CUTOUT CRACK FOUND ON AFT SECTION OF CUTOUT.<[01] REMOVED -1 DOUBLER AND -2 FILLER FROM PREVIOUSLY ACC
- [SDR SWAA2025050164932](https://openairdocs.org/sdr/SWAA2025050164932), Apr 28, 2025: DOUBLER. CRACKED. EXTERNAL POWER CUTOUT CRACK FOUND ON LOWER SECTION OF CUTOUT.<[01] RR?D REPAIR DOUBLER PER SRM 53-10-15-2R-4
- [SDR SWAA2025043064609](https://openairdocs.org/sdr/SWAA2025043064609), Apr 27, 2025: DOUBLER. DAMAGED. EXTERNAL POWER CUTOUT LOWER AND AFT SECTION HAS SHARP EDGES<[01] REMOVED -1 DOUBLER AND -2 FILLER FROM PREVIOUSLY ACCOMPLISHED SRM 53-10-15-2R-4 REPAIR PER SRM 
- [SDR SWAA2025043064610](https://openairdocs.org/sdr/SWAA2025043064610), Apr 27, 2025: DOUBLER. CRACKED. FOUND CRACK ON EGPR SURROUND DOUBLER FWD SIDE UNDER LOWER HINGE<[01] REPAIRED PER EA 25-153-01072; REF TTG8Q0103QYZ AND TTG8Q01048AL FOR WORK ACCOMPLISHED;[02] 
- [SDR SWAA2025013091376](https://openairdocs.org/sdr/SWAA2025013091376), Jan 29, 2025: GIRT BAR. LOOSE. FLIGHT ATTENDANT REPORTS THAT THE AFT ENTRY DOOR GIRT BAR IS LOOSE<[01] SECURED AFT ENTRY DOOR GIRT BAR PER S.I.P.
- [SDR SWAA2025011685446](https://openairdocs.org/sdr/SWAA2025011685446), Jan 13, 2025: LIGHT. INOPERATIVE. EMERGENCY LIGHT ON THE AFT RECESSED PANEL IS INOP<[01] RELAMPED EMERGENCY LIGHT ON THE AFT RECESSED PANEL; PERFORMED GOOD TEST PER AMM 33-51-03-960-801.<BR>TASK
- [SDR SWAA2025011685544](https://openairdocs.org/sdr/SWAA2025011685544), Jan 13, 2025: BULB. INOPERATIVE. PASSENGER CABIN RH OVERWING EMERGENCY EXIT LIGHT INOP.<[01] RELAMPED INOP BULBS IN R/H OWE OVERHEAD SIGN AND PERFORMED GOOD INSTALLATION TEST IAW AMM 33-51-01-9
- [SDR SWAA2025011679949](https://openairdocs.org/sdr/SWAA2025011679949), Dec 20, 2024: ANGLE. CRACKED. L-CLIP CRACKED ON FWD EDGE OF PANEL 651FB CRACKED; 29' FROM O/B EDGE OF PANEL<[01] REMOVED AND REPLACED L-CLIP ON FWD EDGE OF PANEL 651FB; 29' FROM O/B EDGE IAW
- [SDR SWAA2025011579953](https://openairdocs.org/sdr/SWAA2025011579953), Dec 20, 2024: FLOOR PANEL. DELAMINATED. PASSENGER CABIN FLOOR PANEL 241AF TOP SURFACE DELAMINATED<[01] FLOOR PANEL 241AF WITH TOP SURFACE DELAMINATION WAS REPLACED BY FABRICATING A NEW PANEL IAW SRM 5
- [SDR SWAA2025011579951](https://openairdocs.org/sdr/SWAA2025011579951), Dec 20, 2024: FLOOR PANEL. DELAMINATED. PASSENGER CABIN FLOOR PANEL 231XF TOP SURFACE DELAMINATED<[01] FABRICATION OF NEW 231XF FLOOR PANEL REPLACEMENT HAS BEEN ACCOMPLISHED PER [SRM 53-00-50-2R-0-A00
- [SDR SWAA2025011579952](https://openairdocs.org/sdr/SWAA2025011579952), Dec 20, 2024: FLOOR PANEL. DELAMINATED. PASSENGER CABIN FLOOR PANEL 241DF TOP SURFACE DELAMINATED<[01] FLOOR PANEL 241DF WITH TOP SURFACE DELAMINATION WAS REPLACED BY FABRICATING A NEW PANEL IAW SRM 5
- [SDR SWAA2025011579958](https://openairdocs.org/sdr/SWAA2025011579958), Dec 20, 2024: FLOOR PANEL. DELAMINATED. PANEL 241EF HAS DELAMINATION ON FRONT EDGE AND OUTBOARD AFT EDGE CORNER TOP PLY FIBERGLASS (MARKED)<[01] PANEL 241EF HAD DELAMINATION ON FRONT EDGE AND OUTBOARD
- [SDR SWAA2025011582995](https://openairdocs.org/sdr/SWAA2025011582995), Dec 20, 2024: FLOOR PANEL. DAMAGED. PANEL 242AF HAS FRAYED TOP PLY FIBERGLASS (MARKED)<[01] ATTACHED PLACARDS TO FWD AND AFT UPPER SURFACE AREAS USING BAC27DCA854 LOT # 1589317-1 IAW BOEING DWG: 1
- [SDR SWAA2025011582996](https://openairdocs.org/sdr/SWAA2025011582996), Dec 20, 2024: FLOOR PANEL. DAMAGED. PANEL 241BF HAS FRAYED TOP PLY FIBERGLASS (MARKED)<[01] ATTACHED PLACARDS TO FWD AND AFT UPPER SURFACE AREAS USING BAC27DCA854 LOT # 1589317-1 IAW BOEING DWG: 1
- [SDR SWAA2025011579957](https://openairdocs.org/sdr/SWAA2025011579957), Dec 20, 2024: FLOOR PANEL. DELAMINATED. PANEL 242AF HAS DELAMINATION ON FRONT EDGE AND OUTBOARD FWD EDGE CORNER TOP PLY FIBERGLASS (MARKED)<[01] FLOOR PANEL 242AF NEW PANEL FABRICATION ACCOMPLISHED ON
- [SDR SWAA2025011579959](https://openairdocs.org/sdr/SWAA2025011579959), Dec 20, 2024: FLOOR PANEL. DELAMINATED. PANEL 241FF HAS DELAMINATION ON FWD INBOARD EDGE CORNER TOP PLY FIBERGLASS (MARKED)<[01] DAMAGE TO PANEL 241FF WAS FOUND TO BE OUT OF ECONOMICAL REPAIR; NEW FLO
- [SDR SWAA2025011679649](https://openairdocs.org/sdr/SWAA2025011679649), Dec 19, 2024: SCUFF PLATE. CRACKED. ACB CRACKED AFT CORNER SCUFF PLATE<[01] REPAIRED ACB AFT CORNER SCUFF PLATE PER SRM 53-60-15-2R-1. REFERRED TO BAC5975. EQUIPMENT USED: WELDING MACHINE ID# 1058
- [SDR SWAA2025011679650](https://openairdocs.org/sdr/SWAA2025011679650), Dec 19, 2024: DOOR. CRACKED. LEFT HAND MAIN LANDING GEAR CENTER DOOR IS CRACKED (MARKED)<[01] REMOVED LEFT HAND MAIN LANDING GEAR CENTER DOOR IAW AMM 32-13-11-000-804;[02] UPDATED STEP 1;[0
- [SDR SWAA2025011679645](https://openairdocs.org/sdr/SWAA2025011679645), Dec 19, 2024: SCUFF PLATE. CRACKED. FCB FWD SCUFF PLATE CRACKED<[01] REMOVED ALL THE COATINGS FROM THE CORNER SCUFF PLATE APPROXIMATELY 1 INCH AWAY FROM THE WELD AREA PER SRM 53-30-15-2R-1 PARA 4.
- [SDR SWAA2025011679646](https://openairdocs.org/sdr/SWAA2025011679646), Dec 19, 2024: WEB. CORRODED. FWD CARGO DOOR CUTOUT SURROUND; CORROSION ON TRESHOLD WEB (AS MARKED)<[01] REMOVED AND REPLACED FCB SUB-THRESHOLD WEB IAW SRM 51-40-02 AND DWG 143A8330 REV:A;[0
- [SDR SWAA2025011679648](https://openairdocs.org/sdr/SWAA2025011679648), Dec 19, 2024: SCUFF PLATE. CRACKED. ACB CRACKED FWD CORNER SCUFF PLATE<[01] REPAIRED ACB CRACKED FWD CORNER SCUFF PLATE PER SRM WELDED THE ACB; FWD CORNER SCUFF PLATE USING ER4043 FILLER ROD LOT N
- [SDR SWAA2025012079276](https://openairdocs.org/sdr/SWAA2025012079276), Dec 18, 2024: PANEL. CRACKED. CRACKED AFT DOOR SURROUND PANEL FSD (MARKED)<[01] REPAIRED AFT DOOR SURROUND PANEL FSD IAW CMM 25-00-66 PG. 601-602 REPAIR 1-2 SECT. 2.;[02] VERIFIED CORRECTIVE
- [SDR SWAA2024120968444](https://openairdocs.org/sdr/SWAA2024120968444), Dec 5, 2024: TANK UNIT. OUT OF LIMITS. MID FLIGHT NOTICED ABNORMAL FUEL DECREASING. NOTICED UP TO 700 LBS FUEL IMBALANCE. NO TRANSFER OF FUEL FROM TANK TO TANK. NO 1 TANK LOW. PHX PERFORMED COMPARISO
- [SDR SWAA2024120968445](https://openairdocs.org/sdr/SWAA2024120968445), Dec 5, 2024: TANK UNIT. OUT OF LIMITS. MID FLIGHT NOTICED ABNORMAL FUEL DECREASING. NOTICED UP TO 700 LBS FUEL IMBALANCE. NO TRANSFER OF FUEL FROM TANK TO TANK. NO 1 TANK LOW. PHX PERFORMED COMPARISO
- [SDR SWAA2024120968446](https://openairdocs.org/sdr/SWAA2024120968446), Dec 5, 2024: TANK UNIT. OUT OF LIMITS. SUPPLEMENTAL INFORMATION: MID FLIGHT NOTICED ABNORMAL FUEL DECREASING. NOTICED UP TO 700 LBS FUEL IMBALANCE. NO TRANSFER OF FUEL FROM TANK TO TANK. NO 1 TANK LO
- [SDR SWAA2024120968447](https://openairdocs.org/sdr/SWAA2024120968447), Dec 5, 2024: TANK UNIT. OUT OF LIMITS. MID FLIGHT NOTICED ABNORMAL FUEL DECREASING. NOTICED UP TO 700 LBS FUEL IMBALANCE. NO TRANSFER OF FUEL FROM TANK TO TANK. NO 1 TANK LOW. PHX PERFORMED COMPARISO
- [SDR SWAA2024120968448](https://openairdocs.org/sdr/SWAA2024120968448), Dec 5, 2024: TANK UNIT. OUT OF LIMITS. MID FLIGHT NOTICED ABNORMAL FUEL DECREASING. NOTICED UP TO 700 LBS FUEL IMBALANCE. NO TRANSFER OF FUEL FROM TANK TO TANK. NO 1 TANK LOW. PHX PERFORMED COMPARISO
- [SDR SWAA2024120968449](https://openairdocs.org/sdr/SWAA2024120968449), Dec 5, 2024: TANK UNIT. OUT OF LIMITS. MID FLIGHT NOTICED ABNORMAL FUEL DECREASING. NOTICED UP TO 700 LBS FUEL IMBALANCE. NO TRANSFER OF FUEL FROM TANK TO TANK. NO 1 TANK LOW. PHX PERFORMED COMPARISO
- [SDR SWAA2024120968450](https://openairdocs.org/sdr/SWAA2024120968450), Dec 5, 2024: TANK UNIT. OUT OF LIMITS. MID FLIGHT NOTICED ABNORMAL FUEL DECREASING. NOTICED UP TO 700 LBS FUEL IMBALANCE. NO TRANSFER OF FUEL FROM TANK TO TANK. NO 1 TANK LOW. PHX PERFORMED COMPARISO
- [SDR SWAA2024120968451](https://openairdocs.org/sdr/SWAA2024120968451), Dec 5, 2024: TANK UNIT. OUT OF LIMITS. SUPPLEMENTAL INFORMATION: MID FLIGHT NOTICED ABNORMAL FUEL DECREASING. NOTICED UP TO 700 LBS FUEL IMBALANCE. NO TRANSFER OF FUEL FROM TANK TO TANK. NO 1 TANK LO
- [SDR SWAA2024120968452](https://openairdocs.org/sdr/SWAA2024120968452), Dec 5, 2024: TANK UNIT. OUT OF LIMITS. SUPPLEMENTAL INFORMATION: MID FLIGHT NOTICED ABNORMAL FUEL DECREASING. NOTICED UP TO 700 LBS FUEL IMBALANCE. NO TRANSFER OF FUEL FROM TANK TO TANK. NO 1 TANK LO
- [SDR SWAA2024120974349](https://openairdocs.org/sdr/SWAA2024120974349), Dec 5, 2024: FUEL TANK. ABNORMAL. MID FLIGHT NOTICED ABNORMAL FUEL DECREASING. NOTICED UP TO 700 LBS FUEL IMBALANCE. NO TRANSFER OF FUEL FROM TANK TO TANK. NO 1 TANK LOW. PHX PERFORMED COMPARISO

All 1,826: https://openairdocs.org/model/boeing-737-73v/reports.md

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