# N7876A: 2004 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: 29355
- Year built: 2004
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: July 29, 2016
- Certificate issued: December 15, 2022
- Expires: December 31, 2029
- Mode S code: AAADB2
- 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=7876A
- Page: https://openairdocs.org/aircraft/N7876A

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 N7876A.

## FAA accident and incident reports

None matched to N7876A.

## Service difficulty reports (248, 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 SWAA2026092150178](https://openairdocs.org/sdr/SWAA2026092150178), Sep 15, 2026: RING. BROKEN. AFT ENTRY DOOR GIRT BAR RING BROKEN. REPLACED THE STOP RING IAW AMM 25-66-01.
- [SDR SWAA2026072720484](https://openairdocs.org/sdr/SWAA2026072720484), Jul 23, 2026: LAMP. INOPERATIVE. AFT ATTENDANT STATION PANEL'S WORK LIGHT BUTTON AND EMERGENCY LIGHT BUTTON BACK LIGHTS ARE INOPERATIVE. REPLACED THE LAMPS AFT ATTENDANT STATION PANEL'S WORK LI
- [SDR SWAA2026071773120](https://openairdocs.org/sdr/SWAA2026071773120), Jul 13, 2026: SLIDE. LOOSE. FORWARD ENTRY DOOR SLIDE PACK LOOSE. DOOR OPENED BEFORE GIRT BAR PULLED. INSTALLED FWD ENTRY DOOR SLIDE PACK IAW MT 725--61-06. ACFT OK FOR SERVICE.
- [SDR SWAA2026062413321](https://openairdocs.org/sdr/SWAA2026062413321), Jun 4, 2026: STRAP. OUT OF ALIGNMENT. BS 328 FRAME STRAP FROM STR 22R TO STR 20R DOES NOT MATCH WITH CONFIGURATION TASK 5311-1-17336-NG FIGURE 15 IAW EA 26-153-01522; THE CONFIGURATION IS ACCEPTABLE
- [SDR SWAA2026062409347](https://openairdocs.org/sdr/SWAA2026062409347), Jun 4, 2026: STUB FRAME. CRACKED. CRACK INDICATION FOUND IN OPEN FASTENER HOLE AFT POSITION AT STUB BEAM STRAPS AREA AT BS 639 RBL 45.57. CRACK DIRECTION 3 O`CLOCK LOOKING FWD FROM INBD FACE REP
- [SDR SWAA2026062409348](https://openairdocs.org/sdr/SWAA2026062409348), Jun 4, 2026: SEAL. CRACKED. CRACKED BLADE ACCESS PANEL 343AT SEAL RT HORIZONTAL STAB. REPLACED ACCESS PANEL 343AT SEAL AND FASTENER AT RT HORIZONTAL STAB IAW SRM 51-40-02. AND SRM 51-10-02
- [SDR SWAA2026062409094](https://openairdocs.org/sdr/SWAA2026062409094), Jun 3, 2026: PLATE. CRACKED. CRACK CORRUGATED PLATE TRAILING EDGE LOCATED ORSS241 AT LT WING. REPLACED FASTENERS AND CORRUGATED PLATE TRAILING EDGE LOCATED ORSS 241 AT LT WING IAW SRM 51-40
- [SDR SWAA2026062409092](https://openairdocs.org/sdr/SWAA2026062409092), Jun 3, 2026: PLATE. CRACKED. CRACKED CORRUGATED PLATE TRAILING EDGE LOCATED ORSS272 AT RT WING. REPLACED CORRUGATED PLATE AND FASTENERS ON TRAILING EDGE LOCATED ORSS 272 AT RT WING IAW SRM 
- [SDR SWAA2026062409093](https://openairdocs.org/sdr/SWAA2026062409093), Jun 3, 2026: PLATE. CRACKED. CRACKED 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; S
- [SDR SWAA2026062408976](https://openairdocs.org/sdr/SWAA2026062408976), Jun 3, 2026: FITTING. DAMAGED. ELONGATED HOLE ON FITTING TRAILING EDGE LOCATED ORSS256 AT LT WING. REPLACED FITTING LOCATED ON TRAILING EDGE ORSS 256 AT LT WING IAW SRM 51-40-02-0G-0, SRM 51-
- [SDR SWAA2026062409091](https://openairdocs.org/sdr/SWAA2026062409091), Jun 3, 2026: PLATE. CRACKED. CRACK CORRUGATED PLATE TRAILING EDGE LOCATED ORSS272 AT LT WING. REPLACED CORRUGATED PLATE ON TRAILING EDGE LOCATED ORSS272 AT LT WING IAW SRM 51-40-02 AND DWG 
- [SDR SWAA2026062408975](https://openairdocs.org/sdr/SWAA2026062408975), Jun 3, 2026: ACCESS PANEL. DAMAGED. ELONGATED HOLES ON ACCESS PANEL 561CB TRAILING EDGE AT LT WING. REPAIRED ACCESS PANEL 561CB TRAILING EDGE AT LT WING IAW SRM 51-70-04-2R-9, REPAIR 9.
- [SDR SWAA2026062408977](https://openairdocs.org/sdr/SWAA2026062408977), Jun 3, 2026: ACCESS PANEL. DAMAGED. ELONGATED HOLES ON FITTING ACCESS PANEL 651GB AT RT WING. REPLACED FITTING ACCESS PANEL 651GB AT RT WING IAW SRM 51-40-02, SRM 51-10-02 ITEM 9, AND DWG 115A2714
- [SDR SWAA2026062408974](https://openairdocs.org/sdr/SWAA2026062408974), Jun 3, 2026: ACCESS PANEL. DAMAGED. ELONGATED HOLES ACCESS PANEL 561BB AT LT WING. REPAIRED ACCESS PANEL 561BB AT LT WING IAW SRM 51-70-04-2R-9 REPAIR 9.
- [SDR SWAA2026062408451](https://openairdocs.org/sdr/SWAA2026062408451), Jun 2, 2026: CROSSBEAM. CRACKED. CRACKED BRAKE PANEL FLOOR STRUCTURE LOCATED BETWEEN BS 540 AND BL 0 TO RBL 24.75. REPLACED BRAKE PANEL AND FASTENERS ON BS 540 BETWEEN BL 0 TO RBL 24.75 IAW SRM
- [SDR SWAA2026062408450](https://openairdocs.org/sdr/SWAA2026062408450), Jun 2, 2026: ANGLE. CRACKED. CRACKED ANGLE FLOOR STRUCTURE LOCATED BS 695 AND RBL 24.75. REPLACED ANGLE FLOOR STRUCTURE LOCATED BS 695 AND RBL 24.75 PASSENGER CABIN IAW SRM 51-40-02; DWG 11
- [SDR SWAA2026062408446](https://openairdocs.org/sdr/SWAA2026062408446), Jun 1, 2026: BRACKET. CRACKED. CRACKED DEFLECTION CONTROL RIB TRAILING EDGE BRACKET LOCATED ORSS 272 LT WING. REPLACED DEFLECTION CONTROL RIB TRAILING EDGE BRACKET LOCATED ORSS 272 LT WING IA
- [SDR SWAA2026062407749](https://openairdocs.org/sdr/SWAA2026062407749), May 29, 2026: LIGHT. DETERIORATED. DETERIORATED PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING STRIP IN THE PASSENGER CABIN. REPLACED PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING STRIP IAW AMM 33-51-15-9
- [SDR SWAA2025120442421](https://openairdocs.org/sdr/SWAA2025120442421), Dec 4, 2025: STOP. DAMAGED. AFT SERVICE ESCAPE SLIDE GIRT BAR RELEASE STOP DAMAGED. REPLACED AFT SERVICE ESCAPE SLIDE GIRT BAR RELEASE STOP IAW AMM 25-66-01.
- [SDR SWAA2025081805326](https://openairdocs.org/sdr/SWAA2025081805326), Aug 16, 2025: LENS. MISSING. EMERGENCY EXIT SIGN LIGHT COVER MISSING AT ROW 11 ON CAPT SIDE. REINSTALLED EMERGENCY LIGHT LENS AT SEAT 11 ABC IAW AMM 33-51-03.
- [SDR SWAA2025060276260](https://openairdocs.org/sdr/SWAA2025060276260), May 29, 2025: PLUG. DAMAGED. R1 DOOR EXIT SIGN CONNECTOR DAMAGED <[01]. R/R`D R1 DOOR EXIT SIGN D2968 PLUG IAW SWPM 20-61-28. REF WDM 33-51-12. OPS CHECKS NORMAL.
- [SDR SWAA2025032006547](https://openairdocs.org/sdr/SWAA2025032006547), Mar 18, 2025: ACTUATOR. LOW PRESSURE. AFTER FLAPS 5 HYD A SYSTEM LOW PRESSURE LIGHTS ON BOTH ENG AND ELECTRIC PUMP SHORTLY AFTER LOW PRESSURE LIGHTS ON HYD SYSTEM A CAME ON. SYS A QTY WENT TO 0. WE 
- [SDR SWAA2025032007746](https://openairdocs.org/sdr/SWAA2025032007746), Mar 18, 2025: PUMP. LOW PRESSURE. AFTER FLAPS 5 HYD A SYSTEM LOOW PRESSURE LIGHTS ON BOTH ENG AND ELECTRIC PUMP SHORTLY AFTER LOW PRESSURE LIGHTS ON HYD SYSTEM A CAME ON. SYS A QTY WENT TO 0. WE
- [SDR SWAA2025032007747](https://openairdocs.org/sdr/SWAA2025032007747), Mar 18, 2025: FILTER. LOW PRESSURE. AFTER FLAPS 5 HYD A SYSTEM LOW PRESSURE LIGHTS ON BOTH ENG AND ELECTRIC PUMP SHORTLY AFTER LOW PRESSURE LIGHTS ON HYD SYSTEM A CAME ON. SYS A QTY WENT TO 0. WE 
- [SDR SWAA2025032007748](https://openairdocs.org/sdr/SWAA2025032007748), Mar 18, 2025: MODULE. LOW PRESSURE. AFTER FLAPS 5 HYD A SYSTEM LOOW PRESSURE LIGHTS ON BOTH ENG AND ELECTRIC PUMP SHORTLY AFTER LOW PRESSURE LIGHTS ON HYD SYSTEM A CAME ON. SYS A QTY WENT TO 0. WE
- [SDR SWAA2025012087376](https://openairdocs.org/sdr/SWAA2025012087376), Jan 17, 2025: SIGN. LOOSE. CREW REPORTS OVER WING EXIT SIGN LOOSE<[01] RESECURED EXIT SIGN AS PER SIP
- [SDR SWAA2024110555696](https://openairdocs.org/sdr/SWAA2024110555696), Nov 1, 2024: CRADLE. BROKEN. FWD UPPER EMERGENCY FLASH LIGHT HOLD IS BROKEN<[01] FOUND FLASHLIGHT HOLDER IN SERVICEABLE CONDITION. R&R BROKEN FLASHLIGHT STRAP IAW AMM 25-64-00.
- [SDR SWAA2024100143056](https://openairdocs.org/sdr/SWAA2024100143056), Sep 28, 2024: POWER SUPPLY. INOPERATIVE. DURING EMERGENCY LIGHT CHECK FOUND FORWARD CABIN CEILING EMERGENCY LIGHT WONT TURN ON.<[01] T/S PERFORMED PER WDM 33-51-12-6 AND FOUND POWER SUPPLY M1674 IS BAD
- [SDR SWAA2024092038521](https://openairdocs.org/sdr/SWAA2024092038521), Sep 17, 2024: LIGHT. INOPERATIVE. EXTERNAL EMERGENCY LIGHT INOP JUST AFT OF THE FWD SERVICE DOOR.<[01] RELAMPED AND OPS CHECKED GOOD IAW MM 33-51-04.
- [SDR SWAA2024090634179](https://openairdocs.org/sdr/SWAA2024090634179), Sep 5, 2024: LIGHT. WORN. PASSENGER CABIN - FWD L/H EGRESS STRIP WORN<[01] R&R PASSENGER CABIN - FWD L/H EGRESS STRIP PER AMM 33-51-15
- [SDR SWAA2024090634178](https://openairdocs.org/sdr/SWAA2024090634178), Sep 5, 2024: BATTERY PACK. INOPERATIVE. EMX BATT PACK M02335 FAILS TO ILLUMINATE LIGHTS<[01] 01 - REMOVED AND REPLACED EMX BATTERY PACK AND POWER SUPPLY AT M02335 PER [AMM 33-51-06-960-806-NG (POWER S
- [SDR SWAA2024090634858](https://openairdocs.org/sdr/SWAA2024090634858), Sep 5, 2024: POWER SUPPLY. INOPERATIVE. EMX BATT PACK M02335 FAILS TO ILLUMINATE LIGHTS<[01] 01 - REMOVED AND REPLACED EMX BATTERY PACK AND POWER SUPPLY AT M02335 PER [AMM 33-51-06-960-806-NG (POWER S
- [SDR SWAA2024071802699](https://openairdocs.org/sdr/SWAA2024071802699), Jun 17, 2024: SUPPORT ANGLE. CRACKED. CRACK SUPPORT ANGLE LOCATED IN WEATHER RADAR TRASCEIVER MOUNT RH SIDE AT EQUIPMENT ELECTRONIC COMP 2024-376755<[01] REPLACED SUPPORT ANGLE LOCATED IN WEATHER RA
- [SDR SWAA2024071802245](https://openairdocs.org/sdr/SWAA2024071802245), Jun 16, 2024: ANGLE. CRACKED. CRACK ANGLE ACCESS PANEL 343AT AT RT WING 2024-376742<[01] REPLACED ANGLE ON ACCESS PANEL 343AT AT RT WING IAW B737-700 #DWG: 186A3005 SHEET:1 REV:B SRM 51-40-0
- [SDR SWAA2024071802112](https://openairdocs.org/sdr/SWAA2024071802112), Jun 15, 2024: WEB. CRACKED. CRACK ON LOWER SNUBBER WEB AT FWD ENTRY DOOR 2024-376728<[01] REPLACED (ACESS PANEL) LOWER SNUBBER WEB AT FWD ENTRY DOOR IAW B737-700 SRM 51-10-02 ITEM 9 AND DR
- [SDR SWAA2024071801505](https://openairdocs.org/sdr/SWAA2024071801505), Jun 13, 2024: ANGLE. CRACKED. CRACK ANGLE LOCATED STA663.75 AND LBL8 AT CENTER WING BOX 2024-376712<[01] TOOL USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 23-J
- [SDR SWAA2024071801300](https://openairdocs.org/sdr/SWAA2024071801300), Jun 13, 2024: FRAME. CRACKED. CRACK ON FRAME WEB LOCATED BS259.5 BTW STR9L AND STR10L AT PASSENGER CABIN 2024-376710<[01] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600D; S/N: 600091
- [SDR SWAA2024071801301](https://openairdocs.org/sdr/SWAA2024071801301), Jun 13, 2024: WEB. CRACKED. CRACK ON FRAME WEB LOCATED BS259.5 BTW STR9R AND STR10R AT PASSENGER CABIN 2024-376711<[01] TOOL USED: EDDY CURRENT FLAW DETECTOR P/N: NORTEC 600; S/N: 60007161
- [SDR SWAA2024071801044](https://openairdocs.org/sdr/SWAA2024071801044), Jun 13, 2024: FITTING. DETERIORATED. DETERIORATED GIRT BAR FITTING HARDWARE AT FWD SERVICE DOOR 2024-376689<[01] REPLACED GIRT BAR FITTING HARDWARE AT FWD SERVICE DOOR I.A.W B737-700 AMM 25-66-02-4
- [SDR SWAA2024071801045](https://openairdocs.org/sdr/SWAA2024071801045), Jun 13, 2024: FITTING. DETERIORATED. DETERIORATED GIRT BAR FITTING HARDWARE AT FWD ENTRY DOOR 2024-376690<[01] REPLACED GIRT BAR FITTING HARDWARE AT FWD ENTRY DOOR I.A.W B737-700 AMM 25-66-02-400-8
- [SDR SWAA2024071801046](https://openairdocs.org/sdr/SWAA2024071801046), Jun 13, 2024: PLATE. DETERIORATED. DETERIORATED GIRT BAR FITTING ADAPTER PLATE AND SHIM AT FWD ENTRY DOOR 2024-376691<[01] REPLACED GIRT BAR FITTING ADAPTER PLATE AND SHIM AT FWD ENTRY DOOR I.A.W
- [SDR SWAA2024071813988](https://openairdocs.org/sdr/SWAA2024071813988), Jun 13, 2024: SHIM. DETERIORATED. DETERIORATED GIRT BAR FITTING ADAPTER PLATE AND SHIM AT FWD ENTRY DOOR 2024-376691<[01] REPLACED GIRT BAR FITTING ADAPTER PLATE AND SHIM AT FWD ENTRY DOOR I.A.W
- [SDR SWAA2024071801051](https://openairdocs.org/sdr/SWAA2024071801051), Jun 13, 2024: PLATE. DETERIORATED. DETERIORATED GIRT BAR FITTING ADAPTER PLATE AND SHIM AT FWD SERVICE DOOR 2024-376692<[01] REPLACED GIRT BAR FITTING ADAPTER PLATE AND SHIM AT FWD SERVICE DOOR I
- [SDR SWAA2024071813989](https://openairdocs.org/sdr/SWAA2024071813989), Jun 13, 2024: SHIM. DETERIORATED. DETERIORATED GIRT BAR FITTING ADAPTER PLATE AND SHIM AT FWD SERVICE DOOR 2024-376692<[01] REPLACED GIRT BAR FITTING ADAPTER PLATE AND SHIM AT FWD SERVICE DOOR I
- [SDR SWAA2024071701055](https://openairdocs.org/sdr/SWAA2024071701055), Jun 13, 2024: FITTING. DETERIORATED. DETERIORATE HARDWARE OF GIRT BAR FITTING AT AFT ENTRY DOOR 2024-376706<[01] REPLACED HARDWARE OF GIRT BAR FITTING AT AFT ENTRY DOOR I.A.W B737-700 AMM 25-66-02-
- [SDR SWAA2024071701056](https://openairdocs.org/sdr/SWAA2024071701056), Jun 13, 2024: FITTING. DETERIORATED. DETERIORATE ADAPTER PLATE (2EA) AND SHIM(2EA) OF GIRT BAR FITTING AT AFT SERVICE DOOR 2024-376705<[01] REPLACED ADAPTER PLATE (2EA) AND SHIM(2EA) OF GIRT BAR FI
- [SDR SWAA2024071701057](https://openairdocs.org/sdr/SWAA2024071701057), Jun 13, 2024: FITTING. DETERIORATED. DETERIORATE ADAPTER PLATE (2EA) AND SHIM (2EA) OF GIRT BAR FITTING AT AFT ENTRY DOOR 2024-376704<[01] REPLACED ADAPTER PLATE (2EA) AND SHIM (2EA) OF GIRT BAR FI
- [SDR SWAA2024071800664](https://openairdocs.org/sdr/SWAA2024071800664), Jun 12, 2024: SCUFF PLATE. CRACKED. CRACK IN SCUFF PLATE OF SERVICE DOOR AT FWD GALLEY AREA 2024-376665<[01] TOOL USED DIGITAL CALIPER P/N: 500-196-30; S/N: B23399190; DUE DATE: 04 / MAR / 25.;[02
- [SDR SWAA2024071800665](https://openairdocs.org/sdr/SWAA2024071800665), Jun 12, 2024: SCUFF PLATE. CRACKED. CRACK CENTER SCUFF PLATE AT AFT CARGO COMPARTMENT 2024-376667<[01] TOOL USED DIGITAL CALIPER P/N: 500-196-30; S/N: B23399190; DUE DATE: 04 /MAR / 25.;[02] TOOL 
- [SDR SWAA2024071800871](https://openairdocs.org/sdr/SWAA2024071800871), Jun 12, 2024: DOUBLER. UNKNOWN. REJECT - IMPROPERLY GROUND SERVICE DOOR 114AR FABRICATED REPAIR DOUBLER AT LOWER FUSELAGE (REPAIR DOBLER MADE THICK 0.040 INCHES INSTEAD 0.050 INCHES) 2024-3766

All 248: https://openairdocs.org/aircraft/N7876A/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

## Earlier aircraft with N7876A

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N7876A before.

- [Cancelled 1957-02-28](https://openairdocs.org/deregistered/N7876A-1957-02-28): Cessna 180A, S/N 32773. Owner: [Cessna Aircraft Co](https://openairdocs.org/faa-owner/CESSNA%20AIRCRAFT%20CO), [Wichita, KS](https://openairdocs.org/faa-place/KS/Wichita)

## 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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