# N561WN: 2003 Boeing 737-73V

- Status: Valid registration
- Airframe: [Boeing 737-73V](https://openairdocs.org/model/boeing-737-73v) (registry code 1384540, 149 seats)
- Engine: [CFM International CFM56-7B24 series](https://openairdocs.org/engine/cfm-international-cfm56-7b24-series) (registry code 13044)
- Serial number: 32417
- Year built: 2003
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: July 30, 2015
- Certificate issued: April 1, 2025
- Expires: April 30, 2032
- Mode S code: A72CA2
- Registered owner: [Wilmington Trust Co Trustee](https://openairdocs.org/faa-owner/WILMINGTON%20TRUST%20CO%20TRUSTEE)
- Location: [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington)
- Owner type: Corporation
- Owner's area on the map: 39.7236° N, 75.5412° W: Placed by OpenAirDocs at the center of ZIP code 19801, 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=561WN
- Page: https://openairdocs.org/aircraft/N561WN

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 737-73V)

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 N561WN.

## FAA accident and incident reports

None matched to N561WN.

## Service difficulty reports (200, 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 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 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 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 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 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
- [SDR SWAA2024091838104](https://openairdocs.org/sdr/SWAA2024091838104), Sep 16, 2024: LAMP. INOPERATIVE. ROW 11DEF BULLNOSE EMERGENCY LIGHT INOP<[01] RELAMPED ROW 11DEF BULLNOSE EMERGENCY LIGHT (AREA LIGHT) REF AMM 33-51-03. OPS CHECKS GOOD AT THIS TIME.
- [SDR SWAA2024030559234](https://openairdocs.org/sdr/SWAA2024030559234), Mar 4, 2024: SLIDE. LOOSE. L1 ESCAPE SLIDE HAS TOO MUCH SLACK HANGING OUT<[01] RE-POSITION FWD ENTRY SLIDE REF TASK CARD 725-61-06
- [SDR SWAA2023072580815](https://openairdocs.org/sdr/SWAA2023072580815), Jul 21, 2023: CONNECTOR. DIRTY. P-18 PANEL PASSENGER CABIN EMERGENCY CHARGER LT AFT TRIPS AND WILL NOT RESET 2023-394884<[01] INSTALLED CORRECTLY AND CLEANED CONNECTOR D10712 ON BATTERY POWER 
- [SDR SWAA2023072578150](https://openairdocs.org/sdr/SWAA2023072578150), Jul 13, 2023: SUPPORT ANGLE. DAMAGED. ELONGATED HOLE ANGLE - SUPPORT ON COCKPIT DOOR LOC STA 259 AT FWD GALLEY AREA 2023-394849<[01] REPLACED ANGLE - SUPPORT ON COCKPIT DOOR LOC STA 259 AT FWD GALLE
- [SDR SWAA2023072773275](https://openairdocs.org/sdr/SWAA2023072773275), Jun 22, 2023: PANEL. CRACKED. CRACK ACCESS PANEL 632NB FUEL TANK ON FUEL PUMP FLOAT AT RT WING 2023-394805<[01] REPLACED ACCESS PANEL 632NB FUEL TANK ON FUEL PUMP FLOAT AT RT WING IAW B737-7
- [SDR SWAA2023071970791](https://openairdocs.org/sdr/SWAA2023071970791), Jun 22, 2023: FITTING. WORN. WORN ADAPTER PLATE AND SHIM GIRT BAR FITTING SERVICE DOOR AT AFT GALLEY AREA 2023-394801<[01] REPLACED ADAPTER PLATE AND SHIM GIRT BAR FITTING SERVICE DOOR AT A
- [SDR SWAA2023071970797](https://openairdocs.org/sdr/SWAA2023071970797), Jun 22, 2023: PLATE. WORN. WORN ADAPTER PLATE AND SHIM OF GIRT BAR FITTING ENTRY DOOR AT AFT GALLEY AREA 2023-394800<[01] REPLACED ADAPTER PLATE AND SHIM OF GIRT BAR FITTING ENTRY DOOR AT
- [SDR SWAA2023072670423](https://openairdocs.org/sdr/SWAA2023072670423), Jun 21, 2023: DEPRESSOR. CRACKED. CRACK FWD SERVICE DOOR CUTOUT REVEAL LOCATED BS 294.5 BTW STR 8R TO STR 10R AT PASSENGER CABIN 2023-394780<[01] REPLACED DEPRESSOR (REVEAL) AND FASTENERS LOC. F
- [SDR SWAA2023072570170](https://openairdocs.org/sdr/SWAA2023072570170), Jun 21, 2023: ANGLE. CRACKED. CRACK ANGLE BTW BS 907 TO BS 927 AND BTW S 25R TO S 26R AT AFT CARGO COMPARTMENT 2023-394775<[01] TOOL USED DIGITAL CALIPER P/N: 500-196-30 S/N: A20227391 DUE D
- [SDR SWAA2023072570424](https://openairdocs.org/sdr/SWAA2023072570424), Jun 21, 2023: NUT PLATE. CRACKED. CRACK INTERNAL CAVITY LEADING EDGE NUTPLATE RAIL AT LEVEL OFSS 308 AT LT WING 2023-394781<[01] REPLACED NUTPLATE RAIL AT LEVEL OFSS 308 AT LEADING EDGE LT WING 
- [SDR SWAA2023072566734](https://openairdocs.org/sdr/SWAA2023072566734), Jun 20, 2023: FRAME. CRACKED. CRACK FRAME ON BS 907 BTW STR 25R TO STR 26R AT AFT CARGO COMPARTMENT 2023-394761<[01] REPLACED FRAME ON BS 907 BTW STR 25R TO STR 26R AT AFT CARGO COMPARTMENTI
- [SDR SWAA2023072561131](https://openairdocs.org/sdr/SWAA2023072561131), Jun 20, 2023: STRINGER. CRACKED. CRACK STRINGER 27L LOCATED BS 540 FWD CARGO COMPARTMENT 2023-394759<[01] ULTRASONIC EQUIPMENT USED P/N: 45MG ; S/N: 221861811 AND DUE DATE: 08-NOV-23.;[02] TOOL
- [SDR SWAA2023072561132](https://openairdocs.org/sdr/SWAA2023072561132), Jun 20, 2023: STRINGER. CRACKED. CRACK STRINGER 26L LOCATED BS 540 FWD CARGO COMPARTMENT 2023-394758<[01] ULTRASONIC EQUIPMENT USED P/N: 45MG ; S/N: 221861811 AND DUE DATE: 08-NOV-23.;[02] TOOL
- [SDR SWAA2023072561133](https://openairdocs.org/sdr/SWAA2023072561133), Jun 20, 2023: STRINGER. CRACKED. CRACK STRINGER 23L LOCATED BS 540 FWD CARGO COMPARTMENT 2023-394757<[01] TOOL USED: EDDY CURRENT EQUIPMENT; PN: NORTEC 600D; SN:220273012; DUE DATE:17-DEC-23;[0
- [SDR SWAA2023072561134](https://openairdocs.org/sdr/SWAA2023072561134), Jun 20, 2023: STRINGER. CRACKED. CRACK STRINGER 25R LOCATED BS 540 FWD CARGO COMPARTMENT 2023-394756<[01] EQUIPMENT P/N 45MG; S/N 221859911; DUE DATE 07-NOV-23 WAS USED;[02] TOOL USED: EDDY CUR
- [SDR SWAA2023072561135](https://openairdocs.org/sdr/SWAA2023072561135), Jun 20, 2023: STRINGER. CRACKED. CRACK STRINGER 23R LOCATED BS 540 FWD CARGO COMPARTMENT 2023-394755<[01] ULTRASONIC EQUIPMENT USED P/N: 45MG ; S/N: 221861811 AND DUE DATE: 08-NOV-23.;[02] TOOL
- [SDR SWAA2023072560919](https://openairdocs.org/sdr/SWAA2023072560919), Jun 19, 2023: FRAME. CRACKED. CRACK FRAME ON BS 312 AT LEVEL STR 5L AT FWD GALLEY AREA 2023-394709<[01] REPAIRED FRAME ON BS 312 AT LEVEL STR 5L AT FWD GALLEY AREA IAW B737-700 EA NÏ¿½ M-22-
- [SDR SWAA2023072560708](https://openairdocs.org/sdr/SWAA2023072560708), Jun 19, 2023: LIGHT. BROKEN. BROKEN STRIP PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING AT PASSENGER CABIN (6 EA) 2023-394697<[01] INSTALLED STRIP PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING AT P
- [SDR SWAA2023072560921](https://openairdocs.org/sdr/SWAA2023072560921), Jun 19, 2023: TIE CLIP. CRACKED. CRACK ON TIE CLIP LOCATED BS 277 AT LEVEL STR 10R AT FWD AT FWD GALLEY AREA 2023-394712<[01] REPLACED TIE CLIP LOCATED BS 277 AT LEVEL STR 10R AT FWD GALLEY ARE
- [SDR SWAA2023072560922](https://openairdocs.org/sdr/SWAA2023072560922), Jun 19, 2023: SUPPORT ANGLE. CRACKED. CRACK ON SUPPORT ANGLE FLOOR STRUCTURE LOCATED BTW BS 291.5 TO BS 294.5 AT LEVEL STR 17R AT FWD GALLEY AREA 2023-394717<[01] REPLACED SUPPORT ANGLE (CLIP) FLOOR
- [SDR SWAA2023072560195](https://openairdocs.org/sdr/SWAA2023072560195), Jun 18, 2023: SUPPORT ANGLE. CRACKED. CRACK ANGLE - SUPPORT ON ACCESS PANEL 844DZ AT AFT GALLEY AREA 2023-394666<[01] REPLACED ANGLE-SUPPORT ON ACCESS PANEL 844DZ AT AFT GALLEY AREA I.A.W. B737-700 
- [SDR SWAA2023072560185](https://openairdocs.org/sdr/SWAA2023072560185), Jun 18, 2023: SUPPORT ANGLE. CRACKED. CRACK ON SUPPORT ANGLE LOCATED AUXILIARY TRACK OF SLAT 8 LEADING EDGE AT RT WING 2023-394663<[01] REPLACED SUPPORT ANGLE LOCATED AUXILIARY TRACK OF SLAT 8 LEADI
- [SDR SWAA2023072560193](https://openairdocs.org/sdr/SWAA2023072560193), Jun 18, 2023: COUNTERWEIGHT. CORRODED. CORROSION AILERON BALANCE ADJUSTMENT WEIGHT LOCATED BALANCE BAY #5 UPPER AND LOWER AT LT WING 2023-394673<[01] REPLACED AILERON BALANCE WEIGHT LOC. BALANCE BAY 
- [SDR SWAA2023072560194](https://openairdocs.org/sdr/SWAA2023072560194), Jun 18, 2023: COUNTERWEIGHT. CORRODED. CORROSION AILERON BALANCE ADJUSTMENT WEIGHT LOCATED BALANCE BAY #5 UPPER AND LOWER AT RT WING 2023-394674<[01] REPLACED AILERON BALANCE WEIGHT LOC. BALANCE BAY 
- [SDR SWAA2023072559814](https://openairdocs.org/sdr/SWAA2023072559814), Jun 16, 2023: BATTERY PACK. INOPERATIVE. INOP EMERGENCY DOOR BATERY PACK RT SIDE AT PASSENGER CABIN (1 EA) 2023-394576<[01] REPLACED EMERGENCY DOOR BATERY PACK RT SIDE AT PASSENGER CABIN (1 EA) I.A.W B
- [SDR SWAA2023072559815](https://openairdocs.org/sdr/SWAA2023072559815), Jun 16, 2023: BATTERY PACK. INOPERATIVE. INOP EMERGENCY DOOR BATERY PACK LT SIDE AT PASSENGER CABIN (1 EA) 2023-394575<[01] REPLACED EMERGENCY DOOR BATERY PACK LT SIDE AT PASSENGER CABIN (1 EA) I.A.W B
- [SDR SWAA2023072560181](https://openairdocs.org/sdr/SWAA2023072560181), Jun 16, 2023: GUSSET. CRACKED. CRACK GUSSET LOCATED BS500D AND STR19L FWD CARGO COMPARTMENT 2023-394588<[01] REPLACED GUSSET LOCATED BS500D AND STR19L FWD CARGO COMPARTMENT IAW B737-700 SRM 5
- [SDR SWAA2023072559811](https://openairdocs.org/sdr/SWAA2023072559811), Jun 15, 2023: SCUFF PLATE. CRACKED. CRACK FWD CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT 2023 394560<[01] TOOL USED DIGITAL CALIPER P/N:500-197-30;S/N:B20189515;DUE DATE:19-DEC-23.;[02] TOOL USED

All 200: https://openairdocs.org/aircraft/N561WN/reports.md

## STCs that may be installed (OpenAirDocs) (2)

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 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 737-73V aircraft: https://openairdocs.org/model/boeing-737-73v/aircraft.md
- The CFM International CFM56-7B24 series engine: https://openairdocs.org/engine/cfm-international-cfm56-7b24-series.md

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