# N7827A: 2003 Boeing 737-79P

- Status: Valid registration
- Airframe: [Boeing 737-79P](https://openairdocs.org/model/boeing-737-79p) (registry code 13844JA, 149 seats)
- Engine: [CFM International CFM56-7B24 series](https://openairdocs.org/engine/cfm-international-cfm56-7b24-series) (registry code 13044)
- Serial number: 28255
- Year built: 2003
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: August 28, 2015
- Certificate issued: December 20, 2022
- Expires: December 31, 2029
- Mode S code: AA9B42
- 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=7827A
- Page: https://openairdocs.org/aircraft/N7827A

From the FAA registry file of October 28, 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 DCA23FA149](https://openairdocs.org/ntsb/DCA23FA149), Feb 4, 2023: Boeing 737-79P (N7827A), Austin, TX, incident, no damage. Probable cause: the local controller’s incorrect assumption that the Southwest Airlines (SWA) airplane would depart from the runway before the Federal Express airplane arrived on the same runway, which resulted in a…

## FAA accident and incident reports

None matched to N7827A.

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

### Matched by airframe (Boeing 737-79P)

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 (270, 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 SWAA2026100625805](https://openairdocs.org/sdr/SWAA2026100625805), Oct 2, 2026: SEAT TRACK. WORN. FLIGHT DECK, FO AFT IB SEAT TRACK WORN TO BEYOND LIMIT. FLIGHT DECK FO AFT IB SEAT TRACK WORN TO BEYOND LIMIT. R & R FLIGHT DECK FO AFT IB SEAT TRACK IAW AMM 25
- [SDR SWAA2026100649912](https://openairdocs.org/sdr/SWAA2026100649912), Oct 2, 2026: SEAL. CRACKED. RIGHT HORIZONTAL STAB FWD UPPER SLIDING SEAL CRACKED ALONG FWD TRACK EDGE. REMOVED AND REPLACED THE RT HORIZONTAL STAB FWD UPPER SLIDING SEAL IAW AMM 53-31-31.
- [SDR SWAA2026090817976](https://openairdocs.org/sdr/SWAA2026090817976), Sep 4, 2026: SLIDE. OUT OF POSITION. AFT LEFT SLIDE HANGING LOW. REPOSITION THE SLIDE IAW MT 725-61-06, & AMM 25-66-01.
- [SDR SWAA2026081703523](https://openairdocs.org/sdr/SWAA2026081703523), Aug 11, 2026: GIRT BAR. OUT OF ADJUST. FORWARD ENTRY DOOR SLIDE APPEARS TO BE UNPACKING, ADJUSTED GIRT BAR IAW AMM 25-66-01
- [SDR SWAA2026081401009](https://openairdocs.org/sdr/SWAA2026081401009), Aug 10, 2026: SLIDE. OUT OF ADJUST. AFT SERVICE DOOR ON CAPTAINS SIDE GIRT BAR IMPACTS GALLEY WALL WHEN OPENING AND CLOSING DOOR FORWARD ENTRY DOOR SLIDE APPEARS TO BE UNPACKING_ ADJUSTED GIRT BAR
- [SDR SWAA2026060106701](https://openairdocs.org/sdr/SWAA2026060106701), May 27, 2026: FUSE. INOPERATIVE. RH OVER WING EMERGENCY EXIT LIGHTS ARE INOP(SIDEWALL; ABOVE WINDOW) RH OVER WING EMERGENCY EXIT LIGHTS ARE INOP(SIDEWALL ABOVE WINDOW). REMOVED AND REPLACED RH 
- [SDR SWAA2026050594810](https://openairdocs.org/sdr/SWAA2026050594810), May 1, 2026: SLIDE. DISLODGED. DURING PROVO; L-2 EMER SLIDE PACK BECAME DISLODGED FROM DOOR HARNESS -NOT SLIDE DID NOT DEPLOY. REINSTALLED L2 DOOR SLIDE PER MT 725-61-06 AND AMM 25-66-01. OPS
- [SDR SWAA2026043094172](https://openairdocs.org/sdr/SWAA2026043094172), Apr 25, 2026: TIRE. BURST. NR 3 MLG TIRE BURST ON TAKEOFF<[01] ACCOMPLSIHED CONDITIONAL INSPECTION IAW AMM 05-51-54; FOUND MULTIPLE AREAS WITH DAMAGE. REF. TTG8Q01BVDGT; TTG8Q01BVEQE AND 
- [SDR SWAA2026042892644](https://openairdocs.org/sdr/SWAA2026042892644), Apr 24, 2026: TIRE. FAILED. POSSIBLE TIRE TREAD LOSS ON TAKEOFF OUT OF DEN.
- [SDR SWAA2026031378638](https://openairdocs.org/sdr/SWAA2026031378638), Mar 10, 2026: FUSE. INOPERATIVE. LIGHT ON OVERWING EMERGENCY EXIT DOOR IS NOT WORKING FO SIDE, REPLACED TWO LAMPS, NO HELP. OK CONTINUE IAW MEL 33-2-03. FOUND ROW 15 DEF WINDOW LIGHT INOP WITH 
- [SDR SWAA2026031177626](https://openairdocs.org/sdr/SWAA2026031177626), Mar 8, 2026: SHAFT. SHEARED. NR 2 ENGINE DID NOT MAKE TAKEOFF POWER. PERFORMED THE FUEL PUMP IMPELLER SHAFT INSPECTION IAW M-26-173-00258. FOUND SHEARED SHAFT, REMOVED AND REPLACED NR 2 ENG
- [SDR SWAA2026031178669](https://openairdocs.org/sdr/SWAA2026031178669), Mar 8, 2026: HMU. INOPERATIVE. NR 2 ENGINE DID NOT MAKE TAKEOFF POWER. PERFORMED FUEL PUMP IMPELLER SHAFT INSPECTION IAW M-26-173-00258. FOUND A SHEARED SHAFT. REMOVED AND REPLACED THE NR 2 E
- [SDR SWAA2026011259281](https://openairdocs.org/sdr/SWAA2026011259281), Jan 8, 2026: SKIN. DELAMINATED. LEFT WING OTBD AFT FLAP HAS 3' X 8' AREA DELAMINATION AT AFT INBOARD CORNER. REMOVED FLAP IAW MM 27-51-22, C/W RII REQUIREMENT FOR REMOVED FLAP IAW MM 27-51-22.
- [SDR SWAA2025092416765](https://openairdocs.org/sdr/SWAA2025092416765), Sep 21, 2025: COVER. MISSING. EMERGENCY EXIT SIGN ON BULKHEAD NEAR FWD ENTRY DOOR FOUND MISSING. REPLACED COVER IAW AMM 33-51-01.
- [SDR SWAA2025091915164](https://openairdocs.org/sdr/SWAA2025091915164), Sep 16, 2025: LAMP. INOPERATIVE. LEFT FUSELAGE EMERGENCY LIGHT INOP RIGHT BEHIND LEFT WING TRAILING EDGE FLAPS. RELAMPED LEFT FUSELAGE EMERGENCY LIGHT PER AMM 33-51-04.
- [SDR SWAA2025081905306](https://openairdocs.org/sdr/SWAA2025081905306), Aug 17, 2025: BATTERY PACK. INOPERATIVE. INTERIOR EMERGENCY EXIT LIGHT AT FWD ENTRY DOOR INOP. REMOVED AND REPLACED THE FWD LEFT POWER SUPPLY BATTERY PACK AND OPS TESTED GOOD IAW AMM 33-51-06.
- [SDR SWAA2025081905305](https://openairdocs.org/sdr/SWAA2025081905305), Aug 17, 2025: BULB. INOPERATIVE. EMERGENCY LIGHT AT ROW 4 A, B, C INOPERATIVE. REMOVED AND REPLACED BULB FOR EMERGENCY LIGHT IAW SIP AND OPS CHECKED GOOD IAW AMM 33-51-00.
- [SDR SWAA2025061782492](https://openairdocs.org/sdr/SWAA2025061782492), Jun 16, 2025: LIGHT. INOPERATIVE. L2 DOOR EMERGENCY LIGHT INOP. REPLACED L2 DOOR EMERGENCY LIGHT IAW AMM 33-51-04-960-801 TEST IS OK.
- [SDR SWAA2025061782496](https://openairdocs.org/sdr/SWAA2025061782496), Jun 16, 2025: HANDLE. LOOSE. FWD GALLEY AREA FWD SERVICE DOOR ASSISTANCE HANDLE LOOSE. 2025-349145<[01] TIGHTENED ASSISTANCE HANDLE FWD SERVICE DOOR AT FWD GALLEY AREA IAW B737-700 SOPM 20-
- [SDR SWAA2025061775499](https://openairdocs.org/sdr/SWAA2025061775499), May 27, 2025: BATTERY PACK. INOPERATIVE. INOP EMERGENCY EXIT BATTERY PACK LT SIDE ON LOWERED CEILING AT AFT GALLEY AREA. REPLACED EMERGENCY EXIT BATTERY PACK LT SIDE ON LOWERED CEILING AT AFT GALLEY AR
- [SDR SWAA2025061775498](https://openairdocs.org/sdr/SWAA2025061775498), May 27, 2025: BATTERY PACK. INOPERATIVE. INOP EMERGENCY EXIT BATTERY PACK RT SIDE ON LOWERED CEILING AT AFT GALLEY AREA. REPLACED EMERGENCY EXIT (BATTERY PACK) RT SIDE ON LOWERED CEILING AT AFT GALLEY 
- [SDR SWAA2025061675323](https://openairdocs.org/sdr/SWAA2025061675323), May 27, 2025: HANDLE. DETERIORATED. DETERIORATED ENTRY DOOR LINING PANEL ASSIST HANDLE NUT AT AFT GALLEY AREA (2 EA). REPLACED ENTRY DOOR LINING PANEL ASSIST HANDLE NUT AT AFT GALLEY AREA (2 EA) I
- [SDR SWAA2025061675310](https://openairdocs.org/sdr/SWAA2025061675310), May 26, 2025: ANGLE. CRACKED. CRACK ANGLE FLOOR STRUCTURE LOCATED STA695 AND BL0 PASSENGER CABIN. REPLACED ANGLE FLOOR STRUCTURE LOCATED STA695 AND BL0 AT PASSENGER CABIN IAW B737-700 SRM 51
- [SDR SWAA2025061675312](https://openairdocs.org/sdr/SWAA2025061675312), May 26, 2025: FLOORBEAM. CRACKED. CRACK BRAKE PANEL FLOOR STRUCTURE LOCATED STA540 AND LBL1 AT PASSENGER CABIN. NOT FOUND ALLOWABLE DAMAGE FOR BRAKE PANEL ON SRM 53-30-51-1A-1 MEASURES ARE:L= 1.
- [SDR SWAA2025061675316](https://openairdocs.org/sdr/SWAA2025061675316), May 26, 2025: PRESSURE DECK. CRACKED. CRACK INDICATION ON HORIZONTAL PRESSURE DECK WEB LBL 31 STA 663 AT PASSENGER CABIN (1E/A). CRACK LENGTH APPROX. 0.601 INCH. PERFORMED REPAIR CATEGORY B LOC BTW 
- [SDR SWAA2025061675317](https://openairdocs.org/sdr/SWAA2025061675317), May 26, 2025: TEE ANGLE. DAMAGED. ELONGATED HOLE ACCESS PANEL 651FB TRAILING EDGE TEE ANGLE RT WING. REPLACED TEE ANGLE LOCATED ON ACCESS PANEL 651FB TRAILING EDGE RT WING IAW B737-700 SRM 51-10
- [SDR SWAA2025061675308](https://openairdocs.org/sdr/SWAA2025061675308), May 26, 2025: ACCESS PANEL. ELONGATED. ELONGATED HOLE ACCESS PANEL 651FB TRAILING EDGE SUPPORT ANGLE RT WING. REPLACED SUPPORT ANGLE LOCATED ON ACCESS PANEL 651FB TRAILING EDGE RT WING IAW B737-700 S
- [SDR SWAA2025061775147](https://openairdocs.org/sdr/SWAA2025061775147), May 25, 2025: HANDLE. DETERIORATED. DETERIORATED ENTRY DOOR LINING PANEL ASSIST HANDLE NUT AT FWD GALLEY AREA (4 EA). REPLACED ENTRY DOOR LINING PANEL ASSIST HANDLE NUT AT FWD GALLEY AREA (4 EA) I
- [SDR SWAA2025061774822](https://openairdocs.org/sdr/SWAA2025061774822), May 25, 2025: SCUFF PLATE. CRACKED. CRACK CENTER SCUFF PLATE AT AFT CARGO COMPARTMENT. REPAIRED THE CENTER (MIDDLE) SCUFF PALTE AT AFT CARGO COMPARTMENT IN ACCORDING WITH B737-700 SRM 53-60-15-2R-
- [SDR SWAA2025061674821](https://openairdocs.org/sdr/SWAA2025061674821), May 25, 2025: SCUFF PLATE. CRACKED. CRACK AFT CORNER SCUFF PLATE AT FWD CARGO COMPARTMENT. REPAIRED AFT CORNER SCUFF PLATE AT FWD CARGO COMPARTMENT IAW BOEING 737-700 SRM 53-30-15-2R-1 REPAIR 1; A
- [SDR SWAA2025061674823](https://openairdocs.org/sdr/SWAA2025061674823), May 25, 2025: SCUFF PLATE. CRACKED. CRACK SCUFF PLATE AFT CORNER AT AFT CARGO COMPARTMENT. REPAIRED SCUFF PLATE AFT CORNER AT AFT CARGO COMPARTMENT I.A.W. BOEING 737-700 SRM 53-60-15-2R-1 REPAIR 1
- [SDR SWAA2025061674820](https://openairdocs.org/sdr/SWAA2025061674820), May 25, 2025: SCUFF PLATE. CRACKED. CRACK FWD CORNER SCUFF PLATE AT FWD CARGO COMPARTMENT. REPAIRED FWD CORNER SCUFF PLATE AT FWD CARGO COMPARTMENT IAW BOEING 737-700 SRM 53-30-15-2R-1 REPAIR 1; A
- [SDR SWAA2025032609465](https://openairdocs.org/sdr/SWAA2025032609465), Mar 26, 2025: HANDLE. LOOSE. SUPPLEMENTAL INFORMATION: L2 DOORWAY ASSIST HANDLE LOOSE (GALLEY SIDE)<[01] TIGHTENED L2 DOORWAY ASSIST HANDLE PER AMM 25-21-25.
- [SDR SWAA2025032609462](https://openairdocs.org/sdr/SWAA2025032609462), Mar 26, 2025: GIRT BAR. OUT OF ADJUST. L2 DOOR SLIDE GIRT DRAGS<[01] REPACKED L2 DOOR SLIDE GIRT PER AMM 25-66-01.
- [SDR SWAA2025032609466](https://openairdocs.org/sdr/SWAA2025032609466), Mar 26, 2025: GIRT BAR. OUT OF ADJUST. R2 DOOR SLIDE GIRT DRAGS<[01] REPACKED R2 DOOR SLIDE GIRT PER AMM 25-66-01.
- [SDR SWAA2025032609467](https://openairdocs.org/sdr/SWAA2025032609467), Mar 26, 2025: SEAL. CRACKED. LEFT HORIZONTAL STAB FWD UPPER SLIDING SEAL CRACKED. REMOVED AND REPLACED L/H HORIZONTAL STAB FWD UPPER SLIDING SEAL IAW AMM 53-31-31.
- [SDR SWAA2025032609469](https://openairdocs.org/sdr/SWAA2025032609469), Mar 26, 2025: SEAL. CRACKED. RIGHT HORIZONTAL STAB FWD UPPER SLIDING SEAL CRACKED. R&R RH HORIZONTAL STABILIZER FWD UPPER SLIDING SEAL REF. AMM 53-31-31.
- [SDR SWAA2025032609448](https://openairdocs.org/sdr/SWAA2025032609448), Mar 26, 2025: GIRT BAR. OUT OF ADJUST. L1 DOOR ESCAPE SLIDE GIRT REPACK REQUIRED.<[01] RE-PACKED L1 DOOR ESCAPE SLIDE GIRT REF AMM 25-66-01.
- [SDR SWAA2024102853913](https://openairdocs.org/sdr/SWAA2024102853913), Oct 27, 2024: MODULE. FAULTY. PERFORMED A HIGH SPEED REJECTED TAKE OFF AT +- 110KTS DUE TO VISUAL AND AURAL FIRE INDICATIONS OF BOTH ENGINES; APU; AND WHEEL WELL. OVHT INDICATIONS AS WELL FO
- [SDR SWAA2024071712866](https://openairdocs.org/sdr/SWAA2024071712866), Jul 16, 2024: ISOLATION MOUNT. CRACKED. AFT ENTRY DOOR FWD SLIDE MOUNT ISOLATOR CRACKED<[01] R&R AFT ENTRY DOOR FWD SLIDE MOUNT ISOLATOR IAW SRM 51-40-02.
- [SDR SWAA2024071512648](https://openairdocs.org/sdr/SWAA2024071512648), Jul 14, 2024: PACKING. LEAKING. LOSS OF A HYDRAULICS FLUID. DROPPED TO 20%.<[01] INSPECTED; FOUND HYDRAULIC LEAK COMING FROM A SYSTEM HYDRAULIC PUMP ACOUSTIC FILTER INLET UNION (SWIVEL ELBOW).
- [SDR SWAA2024032567538](https://openairdocs.org/sdr/SWAA2024032567538), Mar 25, 2024: LENS. LOOSE. FORWARD ENTRY LOWER EXIT SIGN PLASTIC LENS NOT SECURE<[01] SECURED LENS PER AMM 20-50-11
- [SDR SWAA2024030558534](https://openairdocs.org/sdr/SWAA2024030558534), Mar 3, 2024: GIRT BAR. OUT OF ADJUST. FORWARD GALLEY SERVICE DOOR GIRT BAR DOES NOT STAY LOCKED IN PLACE AND IS LOOSE<[01] INSPECTED AND ADJUSTED GIRT BAR RETAINING CLIPS . OPS CHECK GOOD REF AMM 25
- [SDR SWAA2024021250515](https://openairdocs.org/sdr/SWAA2024021250515), Feb 9, 2024: DOUBLER. CRACKED. EXTERNAL GROUND POWER RECEPTACLE DOOR SURROUND DOUBLER CRACKED AT LOWER TAB REF ORIGINAL FAULT # TTG8Q00QXA44<[01] REPAIRED PER SRM 53-10-15-2R-4.
- [SDR SWAA2024020247509](https://openairdocs.org/sdr/SWAA2024020247509), Feb 1, 2024: PIN. MISALIGNED. ON AFT ENTRY DOOR; RIGHT SIDE ESCAPE SLIDE GIRT BAR MAKES CONTACT WITH EDGE OF AFT GALLEY STORAGE DOOR WHEN DOOR IS OPENED OR CLOSED<[01] FOUND LOWER MOUNTING S
- [SDR SWAA2024011842425](https://openairdocs.org/sdr/SWAA2024011842425), Jan 18, 2024: SLIDE. DISLODGED. AFT ENTRY DOOR SLIDE FELL OUT OF CONTAINER<[01] RESECURED AFT ENTRY DOOR SLIDE IN CONTAINER PER MT 725-61-06. A/C OK FOR SERVICE.
- [SDR SWAA2023110316093](https://openairdocs.org/sdr/SWAA2023110316093), Oct 30, 2023: SWITCH. FAULTY. EMERGENCY LIGHT SWITCH IN COCKPIT FAULTY<[01] REPLACED COCKPIT EMERGENCY LIGHT SWITCH REF SWPM 20-83-00. OPS CHECK GOOD AT THIS TIME
- [SDR SWAA2023083094805](https://openairdocs.org/sdr/SWAA2023083094805), Aug 29, 2023: HOUSING. BROKEN. EMERGENCY EXIT LIGHT HOUSING OVER FWD SERVICE DOOR IS BROKEN AND WILL NOT HOLD EXIT LENS REF M-21-133-00720-TLD.<[01] REMOVED AND REPLACED EMERGENCY EXIT LIGHT 
- [SDR SWAA2023082893719](https://openairdocs.org/sdr/SWAA2023082893719), Aug 25, 2023: SIGN. DETACHED. FORWARD SERVICE DOOR EXIT SIGN FELL OFF.<[01] OK TO CONTINUE ON TLD PER EA M-21-133-00720. SIGN SECURED WITH TRANSPARENT TAPE.
- [SDR SWAA2023071071247](https://openairdocs.org/sdr/SWAA2023071071247), Jun 25, 2023: ANGLE. CRACKED. CRACK ANGLE AT BS 747 CELING PANEL STRUCTURE AT AFT CARGO COMPARTMENT 2023-365739<[01] EDDY CURRENT EQUIPMENT USED P/N: NORTEC 600D; S/N:210138003 AND DUE DATE:

All 270: https://openairdocs.org/aircraft/N7827A/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 N7827A

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N7827A before.

- [Cancelled 1957-01-17](https://openairdocs.org/deregistered/N7827A-1957-01-17): Cessna 180A, S/N 32724. Owner: [Cessna Aircraft Co](https://openairdocs.org/faa-owner/CESSNA%20AIRCRAFT%20CO), [Wichita, KS](https://openairdocs.org/faa-place/KS/Wichita)

## Related

- Other Boeing 737-79P aircraft: https://openairdocs.org/model/boeing-737-79p/aircraft.md
- The CFM International CFM56-7B24 series engine: https://openairdocs.org/engine/cfm-international-cfm56-7b24-series.md

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