# N7881A: 2008 Boeing 737-7CT

- Status: Valid registration
- Airframe: [Boeing 737-7CT](https://openairdocs.org/model/boeing-737-7ct) (registry code 13844NE, 149 seats)
- Engine: [CFM International CFM56-7B24 series](https://openairdocs.org/engine/cfm-international-cfm56-7b24-series) (registry code 13044)
- Serial number: 35084
- Year built: 2008
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: September 15, 2016
- Certificate issued: April 6, 2016
- Expires: April 30, 2029
- Mode S code: AAB0BA
- 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=7881A
- Page: https://openairdocs.org/aircraft/N7881A

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.

## NTSB investigations (1)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB DCA23LA008](https://openairdocs.org/ntsb/DCA23LA008), Sep 29, 2022: Boeing 737 (N7881A), Denver, CO, no damage. Probable cause: An encounter with clear air turbulence during cruise flight.

## NTSB investigations on N7881A not matched to an aircraft (2)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB FTW74DPJ25](https://openairdocs.org/ntsb/FTW74DPJ25), Apr 19, 1974: Cessna 180 (N7881A), Stroud, OK, substantial damage
- [NTSB FTW69D0220](https://openairdocs.org/ntsb/FTW69D0220), Sep 26, 1968: Cessna 180A (N7881A), Stroud, OK, substantial damage

## FAA accident and incident reports

None matched to N7881A.

## Reports on N7881A not matched to an aircraft (1)

They name N7881A, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [Accident 19740419009479A](https://openairdocs.org/incident/19740419009479A), Apr 19, 1974: Cessna 180A (N7881A), Stroud, OK, Substantial damage. Gusting to 35K.

## ADs that may apply (OpenAirDocs): 19 in force

### Matched by airframe (Boeing 737-7CT)

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

## Service difficulty reports (185, 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 SWAA2026101351251](https://openairdocs.org/sdr/SWAA2026101351251), Oct 12, 2026: LOCK PIN. INSTALLED. LANDING GEAR DOES NOT RETRACT WHEN LANDING GEAR LEVER MOVED TO UP POSITION. REMOVED LANDING GEAR DOWN LOCK PINS IAW AMM 32-00-01
- [SDR SWAA2025120136615](https://openairdocs.org/sdr/SWAA2025120136615), Nov 18, 2025: SCUFF PLATE. CRACKED. FWD SERVICE DOOR SCUFF PLATE IS CRACKED AT AFT LOWER CORNER. REMOVE AND REPLACED FWD SERVICE DOOR SCUFF PLATE IS CRACKED AT AFT LOWER CORNER IAW AMM 53-11-01-42
- [SDR SWAA2025120132998](https://openairdocs.org/sdr/SWAA2025120132998), Nov 7, 2025: FLOORBEAM. CRACKED. DURING OK TO CLOSE, FOUND THE FLOORBEAM CRACKED AT BS 540, RBL 1 - 25. REMOVED AND REPLACED THE FLOORBEAM IAW SRM 51-10-02-0G-0, SRM 51-40-02-0G-0, AND DWG 143A
- [SDR SWAA2025120130518](https://openairdocs.org/sdr/SWAA2025120130518), Oct 31, 2025: PLATE. CRACKED. RIGHT WING T/E WIGGLE PLATE COMMON TO PANEL 651EB ON THE I/B SIDE IS CRACKED. REMOVED AND REPLACED THE RT WING T/E WIGGLE PLATE COMMON TO PANEL 651EB ON THE INB
- [SDR SWAA2025120130385](https://openairdocs.org/sdr/SWAA2025120130385), Oct 30, 2025: BULKHEAD. CRACKED. BS 663 LOWER COMPOSITE BULKHEAD IS CRACKED AT LBL 45, WL 173. THE COMPOSITE BULKHEAD WAS REPAIRED IAW SRM 51-70-04-2R-10.
- [SDR SWAA2025120129664](https://openairdocs.org/sdr/SWAA2025120129664), Oct 28, 2025: RIB. CRACKED. RIGHT HORIZONTAL STABILIZER NR 6 INSPAR RIB AT STABILIZER STATION 138.70; 3RD VERTICAL STIFFENER IS CRACKED. PERFORMED REPAIR AT HORIZONTAL STABILIZER NO 6 INSP
- [SDR SWAA2025120129201](https://openairdocs.org/sdr/SWAA2025120129201), Oct 27, 2025: FRAME. CRACKED. CRACKED FRAME BS 312 LBL 33 WL 282 ABOVE FWD ENTRY DOOR UPPER SILL WEB. REPAIRED IAW SRM 22-153-01244.
- [SDR SWAA2025120129202](https://openairdocs.org/sdr/SWAA2025120129202), Oct 27, 2025: STRINGER. CRACKED. CRACKED STRINGER 7L, BS 296, LBL 41, WL 274. THE DAMAGE WAS REPAIRED IAW SRM 53-00-03-2R-1, REPAIR 1, AND EA 25-153-02976 WITH AN INSPECTION PROGRAM DEFINED IN 
- [SDR SWAA2025120128469](https://openairdocs.org/sdr/SWAA2025120128469), Oct 25, 2025: GIRT BAR. LOOSE. AFT ENTRY DOOR SLIDE GIRT BAR BRACKET LOOSE. REMOVED AND REPLACED FASTENER AFT ENTRY DOOR SLIDE GIRT BAR BRACKET IAW SRM 51-40-02-0G-0.
- [SDR SWAA2025120128621](https://openairdocs.org/sdr/SWAA2025120128621), Oct 25, 2025: SKIN. CRACKED. RIGHT WING NR 8 SLAT NOSE SKIN AT ACTUATOR RIB HAS POSSIBLE CRACK. CLEANED RIGHT WING NR 8 SLAT NOSE SKIN AT ACTUATOR IAW SOPM 20-30-03. REPAIRED SLAT IAW SRM 5
- [SDR SWAA2025120128055](https://openairdocs.org/sdr/SWAA2025120128055), Oct 24, 2025: FLOOR PANEL. DELAMINATED. FWD FLOOR PANEL 221EF UPPER SURFACE DELAMINATED. THE FWD FLOOR PANEL 221EF WAS REPLACED WITH A SERVICEABLE FLOOR PANEL IAW SRM 51-10-02-0G-0, PARA 9.A.1,
- [SDR SWAA2025120127810](https://openairdocs.org/sdr/SWAA2025120127810), Oct 24, 2025: FLOOR PANEL. PULLED. AFT FLOOR PANEL 242RF UPPER SKIN HAS AREAS OF PULLED STRANDS. REPAIRED IAW SRM 53-00-50-2R-1-A00939, REPAIR 1.
- [SDR SWAA2025120128041](https://openairdocs.org/sdr/SWAA2025120128041), Oct 24, 2025: FLOOR SUPPORT. CORRODED. CORRODED FLOOR SUPPORT, BS 304, LBL 11, WL 208. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02-0G-0, AND DWG 141A5600, REV N.
- [SDR SWAA2025120128224](https://openairdocs.org/sdr/SWAA2025120128224), Oct 24, 2025: FLOORBEAM. CORRODED. CORRODED FLOORBEAM, BS 986, LBL 38-45, WL 208. REMOVED AND REPLACED THE FILLER IAW EXISTING REPAIR SRM 53-70-51-2R-6, ALT 4.
- [SDR SWAA2025120128225](https://openairdocs.org/sdr/SWAA2025120128225), Oct 24, 2025: FLOORBEAM. CORRODED. CORRODED FLOORBEAM, BS 986, RBL 38-45, WL 208. INSTALLED A REPAIR IAW SRM 53-70-51-2R-6, ALTERNATIVE 3, FIG 204, SHEET 1.
- [SDR SWAA2025120128049](https://openairdocs.org/sdr/SWAA2025120128049), Oct 24, 2025: FLOOR SUPPORT. CRACKED. CRACKED INTERCOSTAL, BS 315, RBL 30, WL 208. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 51-40-02-0G-0, AND DWG 141A5400, REV -.
- [SDR SWAA2025120127802](https://openairdocs.org/sdr/SWAA2025120127802), Oct 24, 2025: FLOOR PANEL. PULLED. AFT FLOOR PANEL 241UF UPPER SKIN HAS AREAS OF PULLED STRANDS. AFT FLOOR PANEL 241UF WITH UPPER SKIN AREAS OF PULLED STRANDS, REPLACED WITH A NEWLY FABRICATED FL
- [SDR SWAA2025120127808](https://openairdocs.org/sdr/SWAA2025120127808), Oct 24, 2025: FLOOR PANEL. PULLED. AFT FLOOR PANEL 241ADF UPPER SKIN HAS AREAS OF PULLED STRANDS. AFT FLOOR PANEL 241ADF WITH UPPER SKIN AREAS OF PULLED STRANDS WAS REPAIRED IAW SRM 53-00-50-2R-1
- [SDR SWAA2025120127809](https://openairdocs.org/sdr/SWAA2025120127809), Oct 24, 2025: FLOOR PANEL. PULLED. AFT FLOOR PANEL 241AEF UPPER SKIN HAS AREAS OF PULLED STRANDS. AFT FLOOR PANEL 241AEF WITH UPPER SKIN AREAS OF PULLED STRANDS WAS REPAIRED IAW SRM 53-00-50-2R-1
- [SDR SWAA2025120127814](https://openairdocs.org/sdr/SWAA2025120127814), Oct 24, 2025: FLOOR PANEL. PULLED. AFT FLOOR PANEL 242UF FWD O/B CORNER IS CRACKED. AFT FLOOR PANEL 242UF WITH FWD O/B CORNER CRACKED WAS REPAIRED PER SRM 53-00-50-2R-1.
- [SDR SWAA2025120127815](https://openairdocs.org/sdr/SWAA2025120127815), Oct 24, 2025: FLOOR PANEL. PULLED. AFT FLOOR PANEL 242WF UPPER SKIN HAS AREAS OF PULLED STRANDS. DUE TO THE EXTENT OF DAMAGE. REPLACED AFT FLOOR PANEL 242WF IAW SRM 51-10-02-0G-0 PARA 9 AND AIPC 
- [SDR SWAA2025120127816](https://openairdocs.org/sdr/SWAA2025120127816), Oct 24, 2025: FLOOR PANEL. DAMAGED. FLOOR PANEL 242XF IS SOFT IN THE MIDDLE OF PANEL.<[01] FLOOR PANEL 242XF WITH SOFT AREA IN THE MIDDLE OF PANEL WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER S
- [SDR SWAA2025120127302](https://openairdocs.org/sdr/SWAA2025120127302), Oct 23, 2025: FORMER. CRACKED. WING TO BODY FAIRING FORMER CRACKED, BS 500D BETWEEN S19 & 20L. REMOVED AND REPLACED THE WING TO BODY FAIRING SUPPORT IAW SRM 51-40-02, AND DWG 116A3010, REV-.
- [SDR SWAA2025120127305](https://openairdocs.org/sdr/SWAA2025120127305), Oct 22, 2025: STRAP. CORRODED. CORROSION AFT CARGO BAY FLOOR SPLICE STRAP AROUND NUT PLATE HOLE BS 727D+6, RBL 11.5, WL 156. EVALUATED CORROSION OF FLOOR STRAP. FOUND TO BE OUT OF LIMITS, REC
- [SDR SWAA2025120127295](https://openairdocs.org/sdr/SWAA2025120127295), Oct 22, 2025: SHIELD. CORRODED. CORROSION AFT CARGO BAY SHIELD FWD OF CARGO DOOR AROUND MULTIPLE NUT PLATE HOLES BS 767+3 - 794, RBL 22, WL 156. FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS GIVE
- [SDR SWAA2025120127291](https://openairdocs.org/sdr/SWAA2025120127291), Oct 22, 2025: SUPPORT PLATE. CORRODED. CORROSION AFT CARGO BAY LT FLOOR TO SIDEWALL SUPPORT PLATE MULTIPLE AREAS AROUND NUT PLATE HOLES, BS 727B - 767, LBL 22, WL 156. CORROSION ON AFT CARGO BAY L/H 
- [SDR SWAA2025120127290](https://openairdocs.org/sdr/SWAA2025120127290), Oct 22, 2025: SIDEWALL SUPPORT. CORRODED. CORROSION AFT CARGO BAY RT FLOOR TO SIDEWALL SUPPORT PLATE HAS MULTIPLE AREAS AROUND NUT PLATE HOLES, BS 727B - 767, RBL 22, WL 156. CORROSION ON AFT CARGO BAY 
- [SDR SWAA2025120126957](https://openairdocs.org/sdr/SWAA2025120126957), Oct 22, 2025: ATTACH ANGLE. CRACKED. BS 663, LOWER COMPOSITE BULKHEAD UPPER ATTACH ANGLE IS CRACKED AT LBL 45, WL 165. REMOVED, REPLACED, AND INSTALLED A NEW ATTACH ANGLE IAW SRM 51-40-02-0G-0, AND
- [SDR SWAA2025120127299](https://openairdocs.org/sdr/SWAA2025120127299), Oct 22, 2025: WEB. CORRODED. CORROSION AFT CARGO BAY SUB THRESHOLD WEB MULTIPLE AREAS AROUND NUT PLATE HOLES BS 794 - 847, RBL 26, WL 156. REMOVED AND REPLACED THE THRESHOLD WEB IAW SRM 51-
- [SDR SWAA2025120127296](https://openairdocs.org/sdr/SWAA2025120127296), Oct 22, 2025: SCUFF PLATE. CRACKED. FORWARD CARGO BAY AFT CORNER SCUFF PLATE IS CRACKED. WELDED THE CORNER SCUFF PLATE IAW SRM 53-30-15-2R-1, STEP 4.B.(4).
- [SDR SWAA2025120127297](https://openairdocs.org/sdr/SWAA2025120127297), Oct 22, 2025: SCUFF PLATE. CRACKED. AFT CARGO BAY AFT CORNER SCUFF PLATE IS CRACKED. WELDED THE CORNER SCUFF PLATE IAW SRM 53-60-15-2R-1, STEP 4.B.(4).
- [SDR SWAA2025120126946](https://openairdocs.org/sdr/SWAA2025120126946), Oct 22, 2025: DOUBLER. CRACKED. EGPR SURROUND DOUBLER CRACKED BS 233, WL 175+8, ABOVE S24R. TRIMMED DAMAGED AREA; FABRICATED REPAIR PARTS AND INSTALLED IAW SRM 53-10-15-2R-4, REPAIR 4, PARG 4 
- [SDR SWAA2025120127298](https://openairdocs.org/sdr/SWAA2025120127298), Oct 22, 2025: ATTACH ANGLE. CORRODED. CORROSION AFT CARGO BAY ATTACH ANGLE UNDER SHIELD HAS MULTIPLE AREAS UNDER NUT PLATES BS 767 TO 787, RBL 21, WL 156. CORROSION ON AFT CARGO BAY ATTACH ANGLE UND
- [SDR SWAA2025120126776](https://openairdocs.org/sdr/SWAA2025120126776), Oct 21, 2025: SWITCH. BROKEN. AFT ATTENDANCE PANEL EMERGENCY LIGHT SWITCH IS BROKEN. REMOVED AND REPLACED AFT ATTENDANT PANEL EMERGENCY LIGHT SWITCH COVER IAW SWPM 20-84-14..
- [SDR SWAA2025120126766](https://openairdocs.org/sdr/SWAA2025120126766), Oct 21, 2025: PANEL. DELAMINATED. PANEL 194CL DELAMINATED ON OUTER SURFACE. PANEL 194CL REPAIRED IAW SRM 51-70-05-2R-2.
- [SDR SWAA2024120273056](https://openairdocs.org/sdr/SWAA2024120273056), Dec 1, 2024: BUSTLE. OUT OF ADJUST. FWD SERVICE DOOR SLIDE BUSTLE TRIM HAS SHARP EDGE ON LOWER RIGHT CORNER.<[01] ADJ DOOR BUSTLE CORRECTED SHARP EDGE PER AMM 52-41-31. AC OK FOR SERVICE.
- [SDR SWAA2024111859384](https://openairdocs.org/sdr/SWAA2024111859384), Nov 13, 2024: WHEEL. SEPARATED. NOSE TIRE SEPARATION ON ROTATION AT ROTATION NOSEWHEEL VIBRATION INCREASED AND MATERIAL DEPARTED TO THE LEFT FROM THE NOSE WHEEL WELL AREA AND THE VIBRATION INC
- [SDR SWAA2024090433101](https://openairdocs.org/sdr/SWAA2024090433101), Sep 1, 2024: RIVET. MISSING. FWD SERVICE DOOR GIRT BAR RETAINING CLIP MISSING RIVET<[01] INSTALLED MISSING RIVET IAW AMM 25-66-01
- [SDR SWAA2024082931055](https://openairdocs.org/sdr/SWAA2024082931055), Aug 26, 2024: GIRT BAR. LOOSE. GIRT BAR RETAINING HOOK ON FORWARD GALLEY DOOR IS LOOSE<[01] C/W EA M-23-125-01839
- [SDR SWAA2023122133492](https://openairdocs.org/sdr/SWAA2023122133492), Dec 19, 2023: SKIRT. OUT OF ADJUST. L2 DOOR SLIDE SKIRT NEEDS ADJUST. IT HITS SCUFF PLATE WHEN CLOSING DOOR<[01] ADJUSTED L2- DOOR SLIDE SKIRT AS PER AMM 25-66-01-000-801;[02] VERIFIED STEP 1
- [SDR SWAA2023122133488](https://openairdocs.org/sdr/SWAA2023122133488), Dec 19, 2023: SKIRT. OUT OF ADJUST. R2 DOOR SLIDE SKIRT NEEDS ADJUST. IT HITS SCUFF PLATE WHEN CLOSING DOOR<[01] ADJUSTED R2- DOOR SLIDE SKIRT AS PER AMM 25-66-01-000-801;[02] VERIFIED STEP 1
- [SDR SWAA2023122131831](https://openairdocs.org/sdr/SWAA2023122131831), Dec 14, 2023: BATTERY PACK. INOPERATIVE. MULTIPLE EMERGENCY LIGHTS INTERIOR/EXTERIOR INOP.<[01] REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACKS<BR>M2335 BATTERY PACK STA 500C LEFT<BR>M1670 BATTERY P
- [SDR SWAA2023122134441](https://openairdocs.org/sdr/SWAA2023122134441), Dec 14, 2023: BATTERY PACK. INOPERATIVE. MULTIPLE EMERGENCY LIGHTS INTERIOR/EXTERIOR INOP.<[01] REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACKS<BR>M2335 BATTERY PACK STA 500C LEFT<BR>M1670 BATTERY P
- [SDR SWAA2023122134442](https://openairdocs.org/sdr/SWAA2023122134442), Dec 14, 2023: BATTERY PACK. INOPERATIVE. MULTIPLE EMERGENCY LIGHTS INTERIOR/EXTERIOR INOP.<[01] REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACKS<BR>M2335 BATTERY PACK STA 500C LEFT<BR>M1670 BATTERY P
- [SDR SWAA2023122131068](https://openairdocs.org/sdr/SWAA2023122131068), Dec 12, 2023: LIGHT. DAMAGED. EMERGENCY LIGHT ASSEMBLY ON G4 DAMAGED<[01] REMOVED AND REPLACED LIGHT ASSEMBLY I/A/W ENCORE CMM 25-31-05; OPS CHECK FOUND NORMAL;[02] VERIFIED STEP 1
- [SDR SWAA2023122125815](https://openairdocs.org/sdr/SWAA2023122125815), Nov 28, 2023: BEAM. CORRODED. MAIN CABIN AFT WET AREA FLOOR BEAM AT STA 986.5 LBL 44' HAS EXFOLIATING CORROSION THAT IS OUT OF LIMITS<[01] REPAIRED MAIN CABIN AFT WET AREA FLOOR BEAM AT STA 
- [SDR SWAA2023122125458](https://openairdocs.org/sdr/SWAA2023122125458), Nov 28, 2023: SEAL. CRACKED. RIGHT HORIZONTAL STABILIZER UPPER GAP COVER ACCESS PANEL 343AT BLADE METAL SEAL CRACKED<[01] REMOVED AND REPLACED RIGHT HORIZONTAL STAB UPPER GAP COVER ACCESS P
- [SDR SWAA2023122125459](https://openairdocs.org/sdr/SWAA2023122125459), Nov 28, 2023: SEAL. DETERIORATED. LEFT HORIZONTAL STABILIZER UPPER GAP COVER ACCESS PANEL 332AT RUBBER SEAL DETERIORATED AND BROKEN PIECE AT END TIP.<[01] REMOVED AND REPLACED LEFT HORIZONTAL ST
- [SDR SWAA2023122125220](https://openairdocs.org/sdr/SWAA2023122125220), Nov 27, 2023: FLOOR PANEL. CRACKED. MAIN CABIN FLOOR PANEL #221GF FWD SECTION TIP CRACKED<[01] APPLIED PERMANEMT REPAIR ON DAMAGE AREA AS MARKED ON MAIN CABIN FLOOR PANEL 221GF AS PER B737 SRM 53-
- [SDR SWAA2023122124947](https://openairdocs.org/sdr/SWAA2023122124947), Nov 27, 2023: SEAL. CRACKED. LEFT HORIZONTAL STABILIZER UPPER GAP COVER ACCESS PANEL 333AT BLADE SEAL CRACKED.<[01] REMOVED AND REPLACED BLADE SEAL AT LEFT HORIZONTAL STABILIZER UPPER GAP C

All 185: https://openairdocs.org/aircraft/N7881A/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 737-7CT aircraft: https://openairdocs.org/model/boeing-737-7ct/aircraft.md
- The CFM International CFM56-7B24 series engine: https://openairdocs.org/engine/cfm-international-cfm56-7b24-series.md

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