# N7880D: 2007 Boeing 737-7K5

- Status: Valid registration
- Airframe: [Boeing 737-7K5](https://openairdocs.org/model/boeing-737-7k5) (registry code 1384518, 151 seats)
- Engine: [CFM International CFM56-7B24 series](https://openairdocs.org/engine/cfm-international-cfm56-7b24-series) (registry code 13044)
- Serial number: 34693
- Year built: 2007
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: November 10, 2016
- Certificate issued: April 7, 2016
- Expires: April 30, 2029
- Mode S code: AAB09A
- Registered owner: [Wells Fargo Trust Co Na Trustee](https://openairdocs.org/faa-owner/WELLS%20FARGO%20TRUST%20CO%20NA%20TRUSTEE)
- Location: [Columbia, MD](https://openairdocs.org/faa-place/MD/Columbia)
- Owner type: Corporation
- Owner's area on the map: 39.2060° N, 76.8282° W: Placed by OpenAirDocs at the center of ZIP code 21045, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=7880D
- Page: https://openairdocs.org/aircraft/N7880D

From the FAA registry file of October 27, 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 737-7K5)

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 N7880D.

## FAA accident and incident reports

None matched to N7880D.

## Service difficulty reports (235, 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 SWAA2026102668005](https://openairdocs.org/sdr/SWAA2026102668005), Oct 25, 2026: SIGN. DETACHED. AFT CABIN OVERHEAD EMERGENCY EXIT LIGHT DETACHED. REMOVED AND REPLACED AFT CABIN EXIT SIGN ASSY IAW AMM 33-51-01. OPS TESTED GOOD.
- [SDR SWAA2026081329049](https://openairdocs.org/sdr/SWAA2026081329049), Aug 8, 2026: BATTERY PACK. INOPERATIVE. AFT ENTRY DOOR EXIT LIGHT NOT WORKING MOUNTED TO AFT LAV BULKHEAD. REPLACED BATTERY PACK M1673 IAW B737-700 AMM 33-51-06-960-805 AND PERFORMED CHECK OF AFT ENTR
- [SDR SWAA2026081348903](https://openairdocs.org/sdr/SWAA2026081348903), Aug 8, 2026: BATTERY PACK. INOPERATIVE. EMERGENCY LIGHT ROW 23 ABC ON BIN BULLNOSE NOT WORKING. REPLACED BATTERY PACK M1673 IAW AMM 33-51-06-960-805 AND PERFORMED CHECK OF EMERGENCY LIGHT ROW 23 ABC O
- [SDR SWAA2026081329124](https://openairdocs.org/sdr/SWAA2026081329124), Aug 8, 2026: BATTERY PACK. INOPERATIVE. AFT ENTRY AND AFT SERVICE DOOR EXTERNAL EMERGENCY LIGHTS NOT WORKING. REPLACED BATTERY PACK M1673 IAW AMM 33-51-06-960-805 AND PERFORMED CHECK OF AFT ENTRY AND 
- [SDR SWAA2026081329490](https://openairdocs.org/sdr/SWAA2026081329490), Aug 8, 2026: BATTERY PACK. FAILED. AFT SERVICE DOOR UPPER EMERGENCY EXIT LIGHT NOT WORKING. REPLACED BATTERY PACK M1673 IAW AMM 33-51-06-960-805 AND PERFORMED CHECK OF AFT SERVICE DOOR UPPER EMER
- [SDR SWAA2026081186820](https://openairdocs.org/sdr/SWAA2026081186820), Jul 25, 2026: ANGLE. CRACKED. CRACK ON ANGLE ASSY AFT FACE, BS 440 BTWN S25L - 26L IN THE FWD CARGO BAY. REPLACED THE ANGLE & FASTENERS IAW SRM 51-40-02-0G-0, SRM 51-10-02-0G-0, & DWG 143A75
- [SDR SWAA2026081196185](https://openairdocs.org/sdr/SWAA2026081196185), Jul 24, 2026: ANGLE. CRACKED. CRACKED ANGLE ASSY, AFT FACE, BS 400 BTWN S25L - 26L IN THE FWD CARGO BAY. REPLACED THE ANGLE & FASTENERS IAW SRM 51-40-02-0G-0, SRM 51-10-02-0G-0, & DWG 143A75
- [SDR SWAA2026081158732](https://openairdocs.org/sdr/SWAA2026081158732), Jul 24, 2026: ANGLE. CRACKED. CRACKED ANGLE ASSY, FWD FACE, BS 420 BTWN S25L - 26L IN FWD CARGO BAY. REPLACED FASTENERS AND ANGLE ASSY, IAW SRM 51-10-02, STEP 9, SRM 51-40-02, AND DWG 143A12
- [SDR SWAA2026081169178](https://openairdocs.org/sdr/SWAA2026081169178), Jul 20, 2026: WEB. DAMAGED. ELONGATED HOLES ON THE WEB LOCATED BTWN BS 440 - 460, LBL 25 IN THE FWD CARGO BAY. REPLACED THE WEB & FASTENERS IAW SRM 51-40-02-0G-0, SRM 51-10-02-0G-0, ITEM 9
- [SDR SWAA2026081189299](https://openairdocs.org/sdr/SWAA2026081189299), Jul 20, 2026: WEB. ELONGATED. ELONGATED HOLES ON THE WEB LOCATED BTWN BS 500 - 500A, LBL 25 IN THE FWD CARGO BAY. REPLACED THE WEB & FASTENERS IAW SRM 52-40-02, AND DWG 143A7505, SHT 82, REV
- [SDR SWAA2026081100419](https://openairdocs.org/sdr/SWAA2026081100419), Jul 20, 2026: WEB. ELONGATED. ELONGATED HOLES ON WEB, BTW BS 400 - 420, LBL 25 IN THE FWD CARGO BAY. REPLACED THE WEB AND FASTENERS IAW SRM 51-40-02-0G-0, SRM 51-10-02-0G-0, ITEM 9, & DWG 14
- [SDR SWAA2026081180652](https://openairdocs.org/sdr/SWAA2026081180652), Jul 10, 2026: LIFE LINE. MISSING. MISSING RETAINER STRAP ON EMERGENCY EXIT LIFE LINE RT & LT SIDES IN THE PASSENGER CABIN. INSTALLED RETAINER STRAP IAW SOPM 20-50-12, REV 58.
- [SDR SWAA2026081162667](https://openairdocs.org/sdr/SWAA2026081162667), Jul 7, 2026: STRINGER. CRACKED. CRACKED STRINGER 23R, BS 540 IN THE FWD CARGO BAY. PERFORMED A PERMANENT REPAIR ON THE STRINGER BTWN BS 500D - 540 IAW SRM 53-00-03-2R-1, REPAIR 1.
- [SDR SWAA2026081164551](https://openairdocs.org/sdr/SWAA2026081164551), Jul 7, 2026: STRINGER. CRACKED. CRACKED STRINGER 25R, BS 540 IN THE FWD CARGO BAY. PERFORMED A PERMANENT REPAIR ON STRINGER 25R, BTWN BS 500D - 540 IAW SRM 53-00-03-2R-1. REPAIR 1.
- [SDR SWAA2026081161719](https://openairdocs.org/sdr/SWAA2026081161719), Jul 7, 2026: STRINGER. CRACKED. CRACKED STRINGER 26R, BS 540 IN THE FWD CARGO BAY. PERFORMED PERMANENT REPAIR ON STRINGER 26R, BETWEEN BS 500D - 540 IAW SRM 53-00-03-2R-1. REPAIR 1.
- [SDR SWAA2026081101285](https://openairdocs.org/sdr/SWAA2026081101285), Jul 7, 2026: STRINGER. CRACKED. CRACKED STRINGER 23L, BS 540 IN THE FWD CARGO BAY. PERFORMED A PERMANENT REPAIR ON STRINGER 23. BTWN BS 500D - 540 IAW SRM 53-00-03-2R-1, REPAIR 1.
- [SDR SWAA2026081123718](https://openairdocs.org/sdr/SWAA2026081123718), Jul 7, 2026: STRINGER. CRACKED. CRACKED STRINGER 26L, BS 540 IN THE FWD CARGO BAY. PERFORMED A PERMANENT REPAIR ON THE STRINGER BTWN BS 500D - 540, IAW SRM 53-00-03-2R-1. REPAIR 1.
- [SDR SWAA2026081150382](https://openairdocs.org/sdr/SWAA2026081150382), Jul 7, 2026: SUPPORT ANGLE. CRACKED. CRACKED SUPPORT ANGLE, BS 500D, S28L IN THE FWD CARGO BAY. REPLACED THE SUPPORT ANGLE & FASTENERS IAW SRM 51-40-02, AND DWG 143A7902, SHEET 126, REV A.
- [SDR SWAA2026081188083](https://openairdocs.org/sdr/SWAA2026081188083), Jul 6, 2026: WEB. CORRODED. CORRODED WEB, BS 767 - 794, RBL 21, WL 156 IN THE AFT CARGO BAY. REPLACED THE WEB IAW SRM 51-40-02-0G AND DWG 146A0081 SHEET 31 REV -.
- [SDR SWAA2026081155594](https://openairdocs.org/sdr/SWAA2026081155594), Jul 6, 2026: SUPPORT. CORRODED. CORRODED SUPPORT ZEE, BS 727D - 767, RBL 21, WL 156 IN AFT CARGO BAY. REPLACED THE SUPPORT ZEE BTWN BS 727 - 767 IAW SRM 51-40-02, AND DWG 146A7500, SHEET 85, R
- [SDR SWAA2026081124889](https://openairdocs.org/sdr/SWAA2026081124889), Jul 5, 2026: SCUFF PLATE. CRACKED. CRACKED FWD SERVICE DOOR SCUFF PLATE, FWD GALLEY. REPAIRED FWD SERVICE DOOR SCUFF PLATE IAW SRM 53-10-15-2R-2, REPAIR 2, AND BAC 5975.
- [SDR SWAA2026081196749](https://openairdocs.org/sdr/SWAA2026081196749), Jul 5, 2026: RAIL. CORRODED. CORROSION ON RAIL NUT-PLATE, OFSS 340, INTERNAL CAVITY, RT WING L/E. REPLACED THE RAIL NUT-PLATE AND FASTENERS IAW SRM 51-40-02, AND DWG 112A4402, SHEET 14, REV
- [SDR SWAA2026081188172](https://openairdocs.org/sdr/SWAA2026081188172), Jul 5, 2026: RAIL. CORRODED. CORROSION ON RAIL NUT-PLATE, OFSS 449 INTERNAL CAVITY LT WING L/E. REPLACED THE RAIL IAW SRM 51-40-02-0G-0, AND DWG 112A4402, SHEET 13, REV -.
- [SDR SWAA2026081127087](https://openairdocs.org/sdr/SWAA2026081127087), Jul 5, 2026: RAIL. CRACKED. CRACKED ON RAIL NUT-PLATE, OFSS 574 INTERNAL CAVITY RT WING L/E. REPLACED RAIL NUT-PLATE IAW SRM 51-40-02-0G-0.
- [SDR SWAA2026081112930](https://openairdocs.org/sdr/SWAA2026081112930), Jul 4, 2026: RIB. CRACKED. CRACK INDICATION ON RT WING OTBD AFT FLAP, INBD CLOSURE RIB RADIUS. REPLACED THE RT OTBD AFT FLAP ASSY IAW AMM 27-51-22-401.
- [SDR SWAA2026081108613](https://openairdocs.org/sdr/SWAA2026081108613), Jul 4, 2026: SUPPORT BRACKET. CRACKED. CRACKED SUPPORT BRACKET, BS 540, LBL 6 IN THE AIR CONDITIONING BAY. REPLACED THE SUPPORT BRACKET IAW SRM 51-40-02, DWG 212A1101, SHEET 4, REV -.
- [SDR SWAA2026081165477](https://openairdocs.org/sdr/SWAA2026081165477), Jul 4, 2026: NUT PLATE. CRACKED. CRACKED RAIL NUT PLATE, OFSS 574 INTERNAL CAVITY OF LT WING L/E. REPLACED THE RAIL NUT PLATE IAW SRM 51-40-02-0G-0.
- [SDR SWAA2026081126090](https://openairdocs.org/sdr/SWAA2026081126090), Jul 4, 2026: SUPPORT BRACKET. CRACKED. CRACKED SUPPORT BRACKET, BS 540, RBL 6 IN THE AIR CONDITIONING BAY. REPLACED THE SUPPORT BRACKET IAW SRM 51-40-02, DWG 212A1101, SHEET 4 , REV -.
- [SDR SWAA2026081110209](https://openairdocs.org/sdr/SWAA2026081110209), Jul 3, 2026: ACCESS PANEL. CRACKED. CRACKED ACCESS PANEL 542BB, LT WING. REPAIRED THE ACCESS PANEL IAW EA M-21-157-01063.
- [SDR SWAA2026081136726](https://openairdocs.org/sdr/SWAA2026081136726), Jun 30, 2026: ACCESS PANEL. DAMAGED. ELONGATED HOLES ON ACCESS PANEL 194E AT LOWER FUSELAGE. REPAIRED THE ACCESS PANEL 194E IAW SRM 51-70-05-2R-8, REPAIR 8.
- [SDR SWAA2026081125967](https://openairdocs.org/sdr/SWAA2026081125967), Jun 30, 2026: PANEL. CRACKED. CRACKED LT WING INBD FIXED TRAILING EDGE SHELF PANEL. REPLACED THE LT WING SHELF PANEL IAW SRM 51-40-02, AND DWG 115A2200, SHEET 2, REV D.
- [SDR SWAA2026081166486](https://openairdocs.org/sdr/SWAA2026081166486), Jun 28, 2026: PRESSURE WEB. CRACKED. CRACK INDICATION FOUND ON THE HORIZONTAL PRESSURE WEB, BS 663 PLUS 2 INCHES, RBL 40, -3 INCHES. PERFORMED A PERMANENT REPAIR ON THE HORIZONTAL PRESSURE DECK IN 
- [SDR SWAA2026081163050](https://openairdocs.org/sdr/SWAA2026081163050), Jun 28, 2026: SCUFF PLATE. CRACKED. CRACKED FWD SCUFF PLATE IN FWD CARGO BAY. REPAIRED THE FWD SCUFF PLATE IAW SRM 53-30-15-2R-1, REPAIR 1.
- [SDR SWAA2026081165349](https://openairdocs.org/sdr/SWAA2026081165349), Jun 27, 2026: GLOWSTRIP. DETERIORATED. DETERIORATED PHOTOLUMINESCENT ON SEVERAL POSITION ALONG PAX CABIN. REPLACED PHOTOLUMINESCENT STRIP ALONG PAX CABIN IAW AMM:33-51-15-400-802, & DWG 33500007, REV
- [SDR SWAA2026081104374](https://openairdocs.org/sdr/SWAA2026081104374), Jun 27, 2026: SKIN. CRACKED. BROKEN EXTERNAL SKIN, LOWER SIDE EXTERNAL POWER RECEPTACLE, LOWER FUSELAGE. PERFORMED PERMANENT REPAIR DOUBLER, FILLER, AND RUB BLOCK IAW SRM 51-40-02, SRM 53-1
- [SDR SWAA2026081162379](https://openairdocs.org/sdr/SWAA2026081162379), Jun 27, 2026: SCUFF PLATE. CRACKED. CRACKED AFT CORNER SCUFF PLATE IN THE AFT CARGO BAY. REPAIRED THE SCUFF PLATE IAW SRM 53-60-15-2R-1, REPAIR 1, AND BAC 5975.
- [SDR SWAA2026081153194](https://openairdocs.org/sdr/SWAA2026081153194), Jun 27, 2026: FLOOR PANEL. DELAMINATED. DELAMINATED FLOOR PANEL 232RF IN THE PAX CABIN. REPAIRED THE FLOOR PANEL 232RF IAW SRM 53-00-50-2R-7, REPAIR 7.
- [SDR SWAA2026081122189](https://openairdocs.org/sdr/SWAA2026081122189), Jun 27, 2026: SCUFF PLATE. CRACKED. CRACKED FWD CORNER SCUFF PLATE IN THE AFT CARGO BAY. REPAIRED THE FWD CORNER SCUFF PLATE IAW SRM 53-60-15-2R-1, REPAIR 1.
- [SDR SWAA2026060308885](https://openairdocs.org/sdr/SWAA2026060308885), Jun 3, 2026: BATTERY PACK. INOPERATIVE. 2 INTERIOR EMERGENCY CABIN AND 2 EXTERIOR EMERGENCY LIGHTS INOP. REMOVED AND REPLACED MID AFT BATTERY PACK FOR OVERWING ESCAPE GROUND EMERGENCY LIGHTS AND INTER
- [SDR SWAA2026041488202](https://openairdocs.org/sdr/SWAA2026041488202), Apr 11, 2026: SUPPORT BRACKET. CRACKED. RIGHT WING UPPER T/E PANEL SUPPORT Z BRACKET CRACKED. REMOVED AND REPLACED SUPPORT BRACKET IAW SRM 51-40-02-0G-0-A00729.
- [SDR SWAA2026040987802](https://openairdocs.org/sdr/SWAA2026040987802), Apr 9, 2026: BATTERY PACK. INOPERATIVE. AFT ENTRY DOOR EMERGENCY LIGHT INOP<[01] REMOVED BATTERY IN REF TO AMM 33-51-06.;[02] INSTALL BATTERY IN REF TO AMM 33-51-06.
- [SDR SWAA2026021670592](https://openairdocs.org/sdr/SWAA2026021670592), Feb 13, 2026: RIVET. SHEARED. GIRT BAR SNAGGED ON LEFT FWD ENTRY DOOR. FOUND SHEARED RIVET ON GIRT BAR ARM. REPLACED RIVET IAW SRM 51-40-02. SLIDE SEPARATED FROM CONTAINER. REINSTALLED SLIDE
- [SDR SWAA2025123056211](https://openairdocs.org/sdr/SWAA2025123056211), Dec 28, 2025: SLIDE. LOOSE. L1 DOOR SLIDE FELL OUT OF CONTAINER. INSTALLED L1 DOOR SLIDE IAW MT 725-61-06.
- [SDR SWAA2025102727915](https://openairdocs.org/sdr/SWAA2025102727915), Oct 23, 2025: COVER. LOOSE. OVERWING EXIT SIGN ON PORT SIDE HAS COVER NOT ATTACHED. SECURED OVERWING EXIT LIGHT COVER IAW SIP.
- [SDR SWAA2025100922829](https://openairdocs.org/sdr/SWAA2025100922829), Oct 9, 2025: SEAT BACK. UNLOCKED. PASSENGER CABIN SEAT AT EMERGENCY EXIT ROW 11B HAS UNLOCKED OUT RECLINE. ADJUSTED HYDRO-LOCK PER AMM 25-22-00.
- [SDR SWAA2025091514598](https://openairdocs.org/sdr/SWAA2025091514598), Sep 11, 2025: FUEL FILTER. BYPASSING. NUMBER 2 ENGING FUEL FILTER BYPASS LIGHT ILLUMINATED, FILTER R & R AT DEFERRAL. ITEM OK TO CONTINUE PER MEL 73-4-01 SP1. REMOVED AND REPLACED FUEL FILTER IAW MM
- [SDR SWAA2025052273677](https://openairdocs.org/sdr/SWAA2025052273677), May 22, 2025: SEAT. FAULTY. PASSENGER CABIN SEAT RECLINE OPERABLE ON EMERGENCY EXIT SEAT 11D. <[01] DISABLED PASSENGER CABIN SEAT RECLINE ON EMERGENCY EXIT SEAT 11D PER [CMM 25-21-45 (NO F
- [SDR SWAA2025010682918](https://openairdocs.org/sdr/SWAA2025010682918), Jan 4, 2025: LIGHT. INOPERATIVE. FWD PAX DOOR EMERGENCY LIGHT INOP<[01] 01 - REMOVED AND REPLACED PER [AMM 33-51-04-960-801-NG (SLIDE/OVERWING LIGHT - LAMP REPLACEMENT - PERMANENT)]
- [SDR SWAA2024092035208](https://openairdocs.org/sdr/SWAA2024092035208), Sep 8, 2024: SCUFF PLATE. CRACKED. CRACK ON FWD SERVICE DOOR SCUFF PLATE MID POSITION 2024-504467<[01] TOOL USED DIGITAL CALIPER P/N: 500-196-30; S/N: B32353969; DUE DATE: 17-MAR-25.;[02] TOOL US
- [SDR SWAA2024092035206](https://openairdocs.org/sdr/SWAA2024092035206), Sep 7, 2024: STRAP. CORRODED. CORROSION STRAP LOCATED BTW BS787 TO BS794.3 RBL20 AT AFT CARGO COMPARTMENT 2024-504278<[01] REPLACED STRAP AND FASTENERS LOCATED BTW BS787 TO BS794.3 RBL20 AT 

All 235: https://openairdocs.org/aircraft/N7880D/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 737-7K5 aircraft: https://openairdocs.org/model/boeing-737-7k5/aircraft.md
- The CFM International CFM56-7B24 series engine: https://openairdocs.org/engine/cfm-international-cfm56-7b24-series.md

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