# N7877H: 2005 Boeing 737-7Q8

- Status: Valid registration
- Airframe: [Boeing 737-7Q8](https://openairdocs.org/model/boeing-737-7q8) (registry code 1384418, 149 seats)
- Engine: [CFM International CFM56-7B24 series](https://openairdocs.org/engine/cfm-international-cfm56-7b24-series) (registry code 13044)
- Serial number: 29359
- Year built: 2005
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: June 7, 2016
- Certificate issued: December 21, 2022
- Expires: December 31, 2029
- Mode S code: AAADDC
- Registered owner: [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 is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=7877H
- Page: https://openairdocs.org/aircraft/N7877H

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 737-7Q8)

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 N7877H.

## FAA accident and incident reports

None matched to N7877H.

## Service difficulty reports (220, 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 SWAA2026102632324](https://openairdocs.org/sdr/SWAA2026102632324), Oct 22, 2026: TRANSMITTER. FAULTED. TRAILING EDGE FLAP ASYMMETRY. LANDED FLAPS 15, FOUND FAULT CODE 27-52260 IN PREVIOUS LEG. AHM DATA ALSO SHOW RT FLAP TRANSMITTER BEHIND LT. REMOVED AND REPLACED
- [SDR SWAA2026021068258](https://openairdocs.org/sdr/SWAA2026021068258), Feb 6, 2026: SEAL. CRACKED. RIGHT HORIZONTAL STAB FORWARD UPPER SLIDING SEAL HAS A 4 INCH VERTICAL CRACK PARALLEL TO THE FORWARD TRACK. REMOVED AND REPLACED THE RT HORIZONTAL STAB FORWARD 
- [SDR SWAA2026012062157](https://openairdocs.org/sdr/SWAA2026012062157), Jan 16, 2026: SEAT BACK. LOOSE. PASSENGER SEAT ROWS 11 DEF, SEAT BACK LOOSE. TIGHTENED THE SEAT BACK IAW CMM 25-21-45, REV 6, STEP 3.Y.(6).
- [SDR SWAA2026012062162](https://openairdocs.org/sdr/SWAA2026012062162), Jan 16, 2026: SEAT BACK. LOOSE. PASSENGER SEAT ROWS 11 BC, SEAT BACK LOOSE. TIGHTENED THE SEAT BACKS IAW CMM 25-21-45, REV.6, STEP 3.Y.
- [SDR SWAA2026012062159](https://openairdocs.org/sdr/SWAA2026012062159), Jan 16, 2026: COVER. OUT OF ADJUST. PAX CABIN AFT RT DOOR SLIDE LOWER COVER RUBBING AGAINST WITH THE DOOR SCUFF PLATE AT CLOSE POSITION. INSTALLED CORRECTLY PAX CABIN AFT RT DOOR SLIDE LOWER COVER
- [SDR SWAA2026012062150](https://openairdocs.org/sdr/SWAA2026012062150), Jan 16, 2026: ASSIST HANDLE. LOOSE. PAX CABIN FWD ENTRY DOOR ASSIST HANDLE LOOSE. TIGHTENED PAX CABIN FWD ENTRY DOOR ASSISTANT HANDLE IAW AMM 52-11-31-400-802, STEP 3 G(2).
- [SDR SWAA2026011962155](https://openairdocs.org/sdr/SWAA2026011962155), Jan 16, 2026: FITTING. LOOSE. AFT GALLEY L2 DOOR AFT GIRT BAR FITTING LOOSE. TIGHTENED AFT GALLEY L2 DOOR AFT GIRT BAR FITTING IAW AMM-25-66-02-400-801. TESTED OK.
- [SDR SWAA2026012056564](https://openairdocs.org/sdr/SWAA2026012056564), Dec 29, 2025: FITTING. CRACKED. CRACKED FITTING LOCATE FRONT SPAR INSPAR RIB HSS 120.30 RT HORIZONTAL STABILIZER. REPLACED FITTING LOCATE FRONT SPAR INSPAR RIB HSS 120.30 RT HORIZONTAL STABILI
- [SDR SWAA2026012056563](https://openairdocs.org/sdr/SWAA2026012056563), Dec 29, 2025: RIB. CRACKED. CRACK INSPAR RIB LOC FWD UPPER CHORD STAB 120.30 AND 1IN FROM FRONT SPAR HSS 120.30 AT RT HORIZONTAL STAB. REPAIRED INSPAR RIB LOC FWD UPPER CHORD STAB 120.30 A
- [SDR SWAA2026012056565](https://openairdocs.org/sdr/SWAA2026012056565), Dec 29, 2025: RIB. CRACKED. CRACK IN SPAR RIB LOCATED FWD LOWER CHORD STAB 120.30 AND 1 INCH FROM FRONT HSS 120.30 AT RT HORIZONTAL STAB. REPAIRED INSPAR RIB LOC FWD LOWER CHORD HSS 120.30
- [SDR SWAA2026012056575](https://openairdocs.org/sdr/SWAA2026012056575), Dec 29, 2025: PLATE. CRACKED. CRACK ON CORRUGATED PLATE LOCATED TRAILING EDGE ORSS261 AT RT WING. REPLACED CORRUGATED PLATE AND FASTENERS LOCATED TRAILING EDGE ORSS261 AT RT WING IAW SRM 51-
- [SDR SWAA2026012056583](https://openairdocs.org/sdr/SWAA2026012056583), Dec 29, 2025: PLATE. CRACKED. CRACK ON CORRUGATED PLATE LOCATED TRAILING EDGE IRSS216 AT LT WING. REPLACED CORRUGATED PLATE LOCATED TRAILING EDGE IRSS216 AT LT WING IAW SRM 51-0-02, ITEM 9, 
- [SDR SWAA2026012056587](https://openairdocs.org/sdr/SWAA2026012056587), Dec 29, 2025: PLATE. CRACKED. CRACK ON CORRUGATED PLATE LOCATED TRAILING EDGE ORSS261 AT LT WING. REPLACED CORRUGATED PLATE LOCATED TRAILING EDGE ORSS261 AT LT WING IAW SRM 51-0-02, ITEM 9, 
- [SDR SWAA2026012056580](https://openairdocs.org/sdr/SWAA2026012056580), Dec 29, 2025: PLATE. CRACKED. CRACK ON CORRUGATED PLATE TRAILING EDGE LOCATED ORSS241 AT RT WING. REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED ORSS241 AT RT WING IAW SRM 51-10-02, ITEM 9,
- [SDR SWAA2026012056582](https://openairdocs.org/sdr/SWAA2026012056582), Dec 29, 2025: SUPPORT BRACKET. CRACKED. CRACK ON SUPPORT BRACKET TRAILING EDGE LOCATED ORSS273 RT WING. REPLACED SUPPORT BRACKET AND FASTENERS LOCATED ON TRAILING EDGE ORSS273 RT WING. MEASUREMENT OF 
- [SDR SWAA2026012056586](https://openairdocs.org/sdr/SWAA2026012056586), Dec 29, 2025: PLATE. CRACKED. CRACK ON CORRUGATED PLATE TRAILING EDGE LOCATED ORSS241 AT LT WING. REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED ORSS241 AT LT WING IAW SRM 51-10-02, ITEM 9,
- [SDR SWAA2026012056588](https://openairdocs.org/sdr/SWAA2026012056588), Dec 29, 2025: SUPPORT BRACKET. CRACKED. CRACK ON SUPPORT BRACKET LOCATED TRAILING EDGE ORSS273 INTERNAL AREA AT LT WING. REPLACED SUPPORT BRACKET LOCATED TRAILING EDGE ORSS273 INTERNAL AREA AT LT WING
- [SDR SWAA2026012056584](https://openairdocs.org/sdr/SWAA2026012056584), Dec 29, 2025: SUPPORT ANGLE. CRACKED. CRACK ON SUPPORT ANGLE LOCATED TRAILING EDGE ORSS273 AT LT WING. REPLACED SUPPORT ANGLE LOCATED TRAILING EDGE ORSS273 AT LT WING IAW SRM 51-10-02, ITEM 9; SRM 5
- [SDR SWAA2026011956589](https://openairdocs.org/sdr/SWAA2026011956589), Dec 29, 2025: BEAM. CRACKED. CRACKED BEAM LOCATED TRAILING EDGE ORSS285 AT LT WING. REPLACED BEAM AND FASTENERS LOCATED TRAILING EDGE ORSS285 AT LT WING IAW SRM 51-40-02, SRM 51-10-02, ITEM
- [SDR SWAA2026011955971](https://openairdocs.org/sdr/SWAA2026011955971), Dec 27, 2025: RIB. CRACKED. CRACKED INSPAR RIB 120.30 LOCATED AT 36 INCHES OF FRONT SPAR AT RT HORIZONTAL STAB. REPAIRED INSPAR RIB LOCATED STAB STA 120.30 AND 36 INCH FROM REAR SPAR AT RT
- [SDR SWAA2026012055861](https://openairdocs.org/sdr/SWAA2026012055861), Dec 26, 2025: ACCESS PANEL. DAMAGED. ELONGATED HOLE ON ACCESS PANEL 571EB TRAILING EDGE AT LT WING. REPAIRED ACCESS PANEL 571EB TRAILING EDGE AT LT WING IAW SRM 51-70-04-2R-9 REPAIR 9. STEP 14 BASE
- [SDR SWAA2026011955860](https://openairdocs.org/sdr/SWAA2026011955860), Dec 26, 2025: SCUFF PLATE. CRACKED. CRACKED AFT CORNER SCUFF PLATE AT AFT CARGO BAY. REPAIRED AFT CORNER SCUFF PLATE IAW SRM 53-60-15-2R-1, REPAIR 1, PARAGRAPH 4. B; STEPS 2 AND 4 TO 7.
- [SDR SWAA2025101624521](https://openairdocs.org/sdr/SWAA2025101624521), Oct 15, 2025: SEAT BACK. OUT OF RIG. PASSENGER CABIN SEAT 11C IS IN AN EMERGENCY EXIT ROW AND RECLINES A SMIDGE. IT IS NOT SUPPOSED TO RECLINE AT ALL ADJUSTED SEAT RECLINE AT SEAT 11C PER CMM 25-21
- [SDR SWAA2025060276367](https://openairdocs.org/sdr/SWAA2025060276367), May 30, 2025: STRIP. MISSING. PASSENGER CABIN PHOTO LUMINIST STRIP MISSING NEXT TO AFT LEFT WIND SCREEN <[01]. INSTALLED MISSING PHOTO LUMINESCENT STRIP PER AMM 33-51-15; [02] INSPECTION C/W
- [SDR SWAA2024052990070](https://openairdocs.org/sdr/SWAA2024052990070), May 26, 2024: LAMP. INOPERATIVE. RH OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. RELAMPED RH OVERWING EMERGENCY EXIT LIGHT OPS OK. IAW AMM 33-51-04
- [SDR SWAA2024030155747](https://openairdocs.org/sdr/SWAA2024030155747), Feb 13, 2024: SUPPORT ANGLE. ELONGATED. ELONGATED HOLE ANGLE - SUPPORT LOCATED BS 440 AND S-22R AT FWD CARGO COMPARTMENT 2024-77444<[01] REPLACED NEW SUPPORT ANGLE AND FASTENERS LOCATED BS 440 AND S-2
- [SDR SWAA2024022948456](https://openairdocs.org/sdr/SWAA2024022948456), Feb 3, 2024: ACCESS PANEL. CRACKED. CRACK ON MARKER BEACON ANTENNA ACCESS PANEL 192F BODY STATION 616 AT KEEL BEAM. REPLACED MARKER BEACON ANTENNA PANEL 192F AT LOWER FUSELAGE I.A.W B737-700 AMM 3
- [SDR SWAA2024022948454](https://openairdocs.org/sdr/SWAA2024022948454), Feb 3, 2024: FRAME. CRACKED. CRACK FRAME ON BS 947.5 BTW STR26L TO STR27L AFT CARGO COMPARTMENT 2024-77399<[01] REPLACED FRAME AND FASTENERS LOCATED BS 947.5 BTW STR 23R TO STR 23L IAW B737
- [SDR SWAA2024022948455](https://openairdocs.org/sdr/SWAA2024022948455), Feb 3, 2024: FITTING. CRACKED. CRACK ON FITTING LOCATED BS947.5 AND STR26L AT AFT CARGO COMPARTMENT. REPLACED FITTING AND FASTENERS LOCATED BS947.5 AND STR26L AT AFT CARGO COMPARTMENT IAW B73
- [SDR SWAA2024022948056](https://openairdocs.org/sdr/SWAA2024022948056), Feb 3, 2024: WEB. CRACKED. CRACK ON WEB LOC. BS 294.5 BTW RBL 54 TO RBL 60 AND WL 208.1 AT PASSENGER CABIN 2024-77397<[01] REPLACED WEB LOC. BS 294.5 BTW RBL 54 TO RBL 60 AND WL 208.1 AT 
- [SDR SWAA2024030447949](https://openairdocs.org/sdr/SWAA2024030447949), Feb 2, 2024: RIB. CRACKED. CRACK ACCESS PANEL 331B ON RIB LOCATED LE STA 105.29 AT LT HORIZONTAL STABILIZER 2024-77389<[01] REPLACED RIB AND FASTENERS LOCATED LE STA 105.29 AT LT HORIZONT
- [SDR SWAA2024030147542](https://openairdocs.org/sdr/SWAA2024030147542), Feb 1, 2024: STRINGER. CRACKED. CRACK STRINGER 23R LOCATED BS540 FWD CARGO COMPARTMENT 2024-77383 CRACK STRINGER 23R LOCATED BS540 FWD CARGO COMPARTMENT<[01] TOOL USED UT EQUIPMENT P/N: 45MG; 
- [SDR SWAA2024030147681](https://openairdocs.org/sdr/SWAA2024030147681), Feb 1, 2024: ACCESS PANEL. DELAMINATED. DELAMINATED ACCESS PANEL 193AL BELLY FAIRING FWD EDGE APPROXIMATELY 16 INCHES FROM TOP EDGE AT LOWER FUSELAGE 2024-77386<[01] TOOL USED:CALIPER PN: 500-197-30 S
- [SDR SWAA2024030147261](https://openairdocs.org/sdr/SWAA2024030147261), Jan 31, 2024: GUSSET. CRACKED. CRACK GUSSET LOCATED BS500D AND STR19R FWD CARGO COMPARTMENT 2024-77370<[01] REPLACED GUSSET LOCATED BS500D; STRINGER 19R FWD CARGO COMPARTMENT IAW B737-700 SRM
- [SDR SWAA2024022946840](https://openairdocs.org/sdr/SWAA2024022946840), Jan 31, 2024: MEGAPHONE. DETERIORATED. DETERIORATED WINDSCREEN LT SIDE THE BATTERIE MEGAPHONE EMERGENCY EQUIPMENT AT AFT GALLEY AREA (8 EA) 2024-77348<[01] REPLACED WINDSCREEN LT SIDE THE BATTERIE ME
- [SDR SWAA2024022946841](https://openairdocs.org/sdr/SWAA2024022946841), Jan 31, 2024: MEGAPHONE. DETERIORATED. DETERIORATED WINDSCREEN LT SIDE THE BATTERIE MEGAPHONE EMERGENCY EQUIPMENT AT FWD GALLEY AREA (8 EA) 2024-77349<[01] REPLACED WINDSCREEN LT SIDE THE BATTERIE ME
- [SDR SWAA2024030146832](https://openairdocs.org/sdr/SWAA2024030146832), Jan 30, 2024: BRACKET. WORN. WEAR HARDWARE ON GIRT BAR FLOOR BRACKETS AT FWD ENTRY AND SERVICE DOOR 2024-77334<[01] REPLACED HARDWARE ON GIRT BAR FLOOR BRACKETS AT FWD ENTRY AND SERVICE DOO
- [SDR SWAA2024022946387](https://openairdocs.org/sdr/SWAA2024022946387), Jan 29, 2024: FRAME. CRACKED. CRACK FRAME STA 312 BETWEEN STR 5LTO STR 6L AT PASSENGER CABIN 2024-77304<[01] PERFORMED PERMANENT REPAIR ON FRAME IAW M-22-153-01244 SEE INDIVIDUAL SIGN OFF BE
- [SDR SWAA2024022946385](https://openairdocs.org/sdr/SWAA2024022946385), Jan 29, 2024: FRAME. CRACKED. CRACK FRAME STA259.5 AT LEVEL STR 9R AT PASSENGER CABIN 2024-77317<[01] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600D; S/N: 200048001; DUE DATE: 01-MA
- [SDR SWAA2024022946388](https://openairdocs.org/sdr/SWAA2024022946388), Jan 29, 2024: STUB FRAME. CRACKED. CRACK FRAME STUD LOCATED STA 294.5 AT LEVEL STR 17R AT PASSENGER CABIN 2024-77315<[01] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600D; S/N: 200048001; 
- [SDR SWAA2024022945845](https://openairdocs.org/sdr/SWAA2024022945845), Jan 28, 2024: LIGHT. BROKEN. BROKEN PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING AT PASSENGER CABIN (10 EA) 2024-77259<[01] REPLACED PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING AT PASSENGER CABI
- [SDR SWAA2024030445152](https://openairdocs.org/sdr/SWAA2024030445152), Jan 26, 2024: FLOORBEAM. CRACKED. CRACK FLOOR STRUCTURE ANGLE ON BS 540 BTW BL 0 TO RBL 12 AT PASSENGER CABIN 2024-77202<[01] REPLACED ANGLE LOCATED ON FLOOR STRUCTURE ON BS 540 BTW BL 0 TO RBL 
- [SDR SWAA2024030445153](https://openairdocs.org/sdr/SWAA2024030445153), Jan 26, 2024: FLOORBEAM. CRACKED. CRACK ANGLE FLOOR STRUCTURE ON BS 540 BTW BL 0 TO LBL 12 AT PASSENGER CABIN 2024-77211<[01] REPLACED ANGLE LOCATED ON FLOOR STRUCTURE ON BS 540 BTW BL 0 TO LBL 
- [SDR SWAA2024022945292](https://openairdocs.org/sdr/SWAA2024022945292), Jan 26, 2024: SCUFF PLATE. CRACKED. CRACK ON AFT CORNER SCUFF PLATE ON FWD CARGO COMPARTMENT DOOR CUTOUT. REPAIRED AFT CORNER SCUFF PLATE ON FWD CARGO COMPARTMENT IAW BOEING 737-700 SRM 53-30-15-2
- [SDR SWAA2024030144218](https://openairdocs.org/sdr/SWAA2024030144218), Jan 24, 2024: HANDLE. BROKEN. BROKEN LINING HANDLE AFT ENTRY DOOR AT AFT GALLEY AREA (1 EA) 2024-77079<[01] REPLACED LINING HANDLE AFT ENTRY DOOR AT AFT GALLEY AREA (1 EA) I.A.W B737-700 AMM
- [SDR SWAA2024030144219](https://openairdocs.org/sdr/SWAA2024030144219), Jan 24, 2024: LIGHT. INOPERATIVE. INOP LAMPS ASSY GALLEY 4 EMERGENCY EXIT AFT GALLEY AREA (1EA) 2024-77077<[01] REPLACED LAMPS ASSY GALLEY 4 EMERGENCY EXIT AFT GALLEY AREA (1EA) IAW B737-700 AMM
- [SDR SWAA2023120427409](https://openairdocs.org/sdr/SWAA2023120427409), Dec 3, 2023: PITOT TUBE. UNRELIABLE. BIRDSTRIKE LEFT SIDE AIRCRAFT ON ROTATION; AIRSPEED CAPTS SIDE UNRELIABLE; NO ABNORMAL SMELLS OR ENGINE INDICATIONS<[01] R/R CAPT PITOT PROBE PER AMM 34-11-01. 
- [SDR SWAA2023103115521](https://openairdocs.org/sdr/SWAA2023103115521), Oct 28, 2023: SUPPORT BRACKET. CRACKED. RT. WING UPPER INBD FWD UPPER PANEL SUPPORT BRACKET CRACKED. (Z BRACKET)<[01] REMOVED AND REPLACED RT WING UPPER INBD FWD UPPER PANEL SUPPORT BRACKET (Z BRACKET
- [SDR SWAA2023101911032](https://openairdocs.org/sdr/SWAA2023101911032), Oct 16, 2023: LIGHT. INOPERATIVE. FLOOR TRACK LIGHTING BY ROW 1 INOP<[01] REPLACED FWD SECTION OF SAF-T-GLO TRACK AND CKS OK. REF SIP
- [SDR SWAA2023082493051](https://openairdocs.org/sdr/SWAA2023082493051), Aug 24, 2023: LIGHT. INOPERATIVE. CABIN R/H EMERGENCY EXIT SIDEWALL LIGHT IS INOPERATIVE.<[01] REMOVED AND REPLACED CABIN R/H EMERGENCY EXIT SIDEWALL LIGHT IN REF TO AMM 33-51-03

All 220: https://openairdocs.org/aircraft/N7877H/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 737-7Q8 aircraft: https://openairdocs.org/model/boeing-737-7q8/aircraft.md
- The CFM International CFM56-7B24 series engine: https://openairdocs.org/engine/cfm-international-cfm56-7b24-series.md

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