# N7869A: 2006 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: 29365
- Year built: 2006
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Experimental, showing compliance
- Airworthiness date: September 3, 2018
- Certificate issued: January 9, 2023
- Expires: January 31, 2030
- Mode S code: AAAA64
- 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=7869A
- Page: https://openairdocs.org/aircraft/N7869A

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 737-79P)

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

## NTSB investigations

None matched to N7869A.

## FAA accident and incident reports

None matched to N7869A.

## Service difficulty reports (146, 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 SWAA2026051397568](https://openairdocs.org/sdr/SWAA2026051397568), May 11, 2026: SLIDE. DETACHED. FWD ENTRY DOOR SLIDE HANGING DOWN. REPOSITIONED SLIDE PER MT725-61-06.
- [SDR SWAA2026012062730](https://openairdocs.org/sdr/SWAA2026012062730), Jan 18, 2026: SEAT. UNLOCKED. PAX SEAT 14B WILL NOT STAY IN THE LOCKED UPRIGHT POSITION. FOUND TO BE OVERWING EXIT SEAT, ENSURED SEAT LOCKED UP IAW AMM 25-22-00.
- [SDR SWAA2025103129197](https://openairdocs.org/sdr/SWAA2025103129197), Oct 28, 2025: LAMP. INOPERATIVE. OVERHEAD BIN EMERGENCY BULL NOSE LIGHT INOP AT 24ABC. RELAMPED O/H BIN EMERGENCY LIGHT AT SEAT 24C PER AMM 33-51-03
- [SDR SWAA2025100923017](https://openairdocs.org/sdr/SWAA2025100923017), Oct 9, 2025: SLIDE. OUT OF ADJUST. FWD GALLEY SLIDE FELL OUT. REINSTALLED FWD SERVICE DOOR SLIDE PER MT725-61-06
- [SDR SWAA2025082909596](https://openairdocs.org/sdr/SWAA2025082909596), Aug 28, 2025: SLIDE. UNPACKED. FORWARD SERVICE DOOR ESCAPE SLIDE PARTIALLY FELL OUT OF THE STORAGE CONTAINER WHEN THE DOOR WAS OPENED. SECURED FWD SVC DOOR ESCAPE SLIDE IAW AMM 25-66-01.
- [SDR SWAA2024121777319](https://openairdocs.org/sdr/SWAA2024121777319), Dec 13, 2024: LIGHT. BROKEN. FWD ENTRY DOOR EMERGENCY LIGHT BROKEN.<[01] REMOVED AND REPLACED LIGHT ASSY IAW AMM 33-51-01.
- [SDR SWAA2024092742738](https://openairdocs.org/sdr/SWAA2024092742738), Sep 26, 2024: GIRT BAR. LOOSE. CREW REPORTS R1 DOOR; AFT GIRT BAR LOOSE<[01] REPLACED SEARED RIVET IAW SRM 51-40-02
- [SDR SWAA2024082628758](https://openairdocs.org/sdr/SWAA2024082628758), Aug 22, 2024: PAN. CRACKED. AFT ENTRY (L2) DOOR LOWER LINER PAN CRACKED AT SUPPORT BRACKET<[01] REMOVED AND REPLACED AFT ENTRY (L2) DOOR LOWER LINER PAN PER AMM 52-13-61
- [SDR SWAA2024081324984](https://openairdocs.org/sdr/SWAA2024081324984), Aug 11, 2024: BATTERY PACK. INOPERATIVE. FOUND MULTIPLE EMERGENCY LIGHTS INOP.<[01] REMOVED AND REPLACED BATTERY BACK JUST FWD OF LH OVER WING EMERGENCY DOOR PER AMM 33-51-06 OPS CHECK GOOD
- [SDR SWAA2024062003261](https://openairdocs.org/sdr/SWAA2024062003261), Jun 18, 2024: WHEEL. ABNORMAL. AFTER LANDING AT TAXI. SPEED FELT SLIGHT SHIMMY FROM NOSE WHEEL AND TOWER REPORTED SMALL AMOUNT OF SMOKE FROM FRONT OF AIRCRAFT/ ONCE INFORMED OF SMOKE AIRCRAFT
- [SDR SWAA2024052990171](https://openairdocs.org/sdr/SWAA2024052990171), May 27, 2024: CONNECTOR. DISCONNECTED. EMERGENCY EXIT LIGHT ABOVE FWD ENTRY DOOR IS INOP<[01] PERFORMED TROUBLESHHOTING EXIT LIGHT ABOVE FWD ENTRY DOOR INOP; FOUND CONNECTOR D40040P NOT CONNECT AT DO
- [SDR SWAA2024052989839](https://openairdocs.org/sdr/SWAA2024052989839), May 25, 2024: SKIRT. MISINSTALLED. FWD ENTRY DOOR ESCAPE SLIDE SKIRT IMPROPERLY PACKED; YELLOW INTERNAL COVERING EXPOSED.<[01] ADJUSTED FWD ENTRY DOOR ESCAPE SLIDE SKIRT YELLOW INTERNAL COVERING 
- [SDR SWAA2024052989614](https://openairdocs.org/sdr/SWAA2024052989614), May 25, 2024: BATTERY PACK. INOPERATIVE. LEFT AND RIGHT EMERGENCY SLIDE GROUND LIGHTS DO NOT ILLUMINATE.<[01] UPON FURTHER INVESTIGATION; FOUND EMERGENCY BATTERY PACK M1670 TO BE BAD; BATTERY PACK REPL
- [SDR SWAA2024052989617](https://openairdocs.org/sdr/SWAA2024052989617), May 25, 2024: BATTERY PACK. NO TEST. LEFT OVERWING EXIT SIGN DOES NOT ILLUMINATE.<[01] REMOVED EMERGENCY EXIT LIGHT BATTERY PACK M1668 AND INSTALLED SERVICEABLE BATTERY PACK AND PERFORMED GOOD INST
- [SDR SWAA2024052989618](https://openairdocs.org/sdr/SWAA2024052989618), May 25, 2024: BATTERY PACK. INOPERATIVE. FORWARD EMERGENCY LAMP IN LEFT OVERWING HATCH WINDOW LIGHT ASSEMBLY DOES NOT ILLUMINATE.<[01] UPON FURTHER INVESTIGATION; FOUND EMERGENCY BATTERY PACK M1668 TO 
- [SDR SWAA2024052989619](https://openairdocs.org/sdr/SWAA2024052989619), May 25, 2024: BATTERY PACK. NO TEST. AISLE LIGHTS AT SEATS 6/7L; 8/9R; 9L; 11/12L; 14L; AND 17L DO NOT ILLUMINATE. AISLE LIGHTS AT SEATS 6/7L 8/9R 9L 11/12L 14L AND 17L DO NOT ILLUMINATE.<[01] REMO
- [SDR SWAA2024052989620](https://openairdocs.org/sdr/SWAA2024052989620), May 25, 2024: BATTERY PACK. INOPERATIVE. SECONDARY OVERWING EXIT SIGN AFT OR LIFE RAFT DOES NOT ILLUMINATE.<[01] REMOVED EMERGENCY EXIT LIGHT BATTERY PACK M1670 AND INSTALLED SERVICEABLE BATTERY PACK A
- [SDR SWAA2024052989616](https://openairdocs.org/sdr/SWAA2024052989616), May 25, 2024: WIRE. NOT SEATED. EMERGENCY EXIT SIGN AND EXIT LIGHT OVER AFT SERVICE DOOR DO NOT ILLUMINATE.<[01] PERFORMED TROBLESHOOTING EMERGENCY LIGHT AND EXIT LIGHT OVER AFT SERVICE DOOR; 
- [SDR SWAA2024052989277](https://openairdocs.org/sdr/SWAA2024052989277), May 24, 2024: LIGHT. WRONG PART. EMERGENCY EXIT LIGHT ON AFT FACE OF LAV-A HAS INCORRECT MARKING FOR POSITION<[01] REMOVED AND REPLACED EMERGENCY EXIT LIGHT ON AFT FACE OF LAV -A PER AMM 33-51-
- [SDR SWAA2024052984871](https://openairdocs.org/sdr/SWAA2024052984871), May 13, 2024: WIRE. TORN. FWD LAV EMERGENCY EXIT INDICATOR LIGHT WIRE TORN. INVESTIGATION SHOWED GROUND WIRE W4142-0152-20 FOR EMERGENCY LIGHT L1187 PULLED OUT OF GD3782-DC. REPAIRED WIR
- [SDR SWAA2024052983822](https://openairdocs.org/sdr/SWAA2024052983822), May 8, 2024: RIB. CRACKED. RIGHT HORIZONTAL STAB RIB AT STAB STA. 120.30 LOWER FLANGE AT 4TH STIFFENER CRACKED. ACCOMPLISHED HFEC SURFACE SCAN OF SUSPECTED CRACKED AREA IAW NDTM PART 6 CH
- [SDR SWAA2024052981722](https://openairdocs.org/sdr/SWAA2024052981722), May 2, 2024: FLOOR SUPPORT. CRACKED. CRACKED INTERCOSTAL BS 277-294 RBL 1 WL 208.<[01] REMOVED; LOCATED AND DRILLED NEW AND INSTALLED INTERCOSTAL BS 277-294 RBL 1 WL 208 ALL I.A.W SRM 51-40-02-0G-0
- [SDR SWAA2024052981723](https://openairdocs.org/sdr/SWAA2024052981723), May 2, 2024: CHANNEL. CRACKED. FWD ENTRY DOOR MOP SILL CRACKED ON VERTICAL FLANGE AT BS 303 LBL 58 WL 208.<[01] CRACK ON FED ENTRY DOOR MOP SILL EXCEED LIMITS GIVEN IN THE SRM; FOUND TO BE OU
- [SDR SWAA2024052981724](https://openairdocs.org/sdr/SWAA2024052981724), May 2, 2024: FLOOR SUPPORT. CRACKED. CACKED INTERCOSTAL AT BS 294-312 LBL 46 WL 208. CRACKED INTERCOSTAL AT BS 328-344 LBL 46 WL 208<[01] REMOVED DAMAGE INTERCOSTAL BS328-344 LBL 46 WL 208;LOCATED 
- [SDR SWAA2024052981725](https://openairdocs.org/sdr/SWAA2024052981725), May 2, 2024: FLOOR SUPPORT. CRACKED. CRACKED INTERCOSTAL BS 312-328 LBL 46 WL 208.<[01] REMOVED DAMAGE INTERCOSTAL BS 312-328 LBL 46 WL 208;LOCATED ;DRILLED AND INSTALLED NEW ALL I.A.W SRM 51-10-02
- [SDR SWAA2024052981739](https://openairdocs.org/sdr/SWAA2024052981739), May 2, 2024: FLOOR SUPPORT. CRACKED. CRACKED INTERCOSTAL AT BS 380-400 LBL 1 WL 208.<[01] REMOVED; LOCATED AND DRILLED NEW AND INSTALLED INTERCOSTAL BS380-BS400 LBL 1 WL 208 ALL I.A.W SRM 51-40-02-
- [SDR SWAA2024052981729](https://openairdocs.org/sdr/SWAA2024052981729), May 2, 2024: FLOOR SUPPORT. CRACKED. CRACKED INTERCOSTAL AT BS 380-400 LBL 14 WL 208.<[01] REMOVED; LOCATED ;DRILLED NEW AND INSTALLED INTERCOSTAL BS380-BS400 LBL 14 WL 208 ALL I.A.W SRM 51-40-02-0
- [SDR SWAA2024052981740](https://openairdocs.org/sdr/SWAA2024052981740), May 2, 2024: FLOOR SUPPORT. CRACKED. CRACKED INTERCOSTAL ART BS 380-400 RBL 8 WL 208.<[01] REMOVED AND REPLACED INTERCOSTAL T BS 380-BS 400;RBL8; WL208 IAW SRM 51-40-02-0G-0 AND DWG 143A5400;[02] V
- [SDR SWAA2024052981721](https://openairdocs.org/sdr/SWAA2024052981721), May 2, 2024: INTERCOSTAL. CORRODED. CORROSION ON LAV A MOUNT INTERCOSTAL BS 294-312 LBL 46 WL 208. REMOVED DAMAGE INTERCOSTAL DUE NO ALLOWABLE LIMIT GIVEN SRM; LOCATED ; DRILLED NEW INTERCOSTAL AN
- [SDR SWAA2024052981176](https://openairdocs.org/sdr/SWAA2024052981176), May 1, 2024: STRAP. CORRODED. CORROSION ON AFT CARGO BAY FLOOR T STRAP BS 767+5 RBL 8 WL 156. EVALUATED CORROSION ON FLOOR T STRAP BS 767+5 RBL 8 WL 156 AND FOUND TO BE OUT OF LIMITS DUE TO 
- [SDR SWAA2024052981479](https://openairdocs.org/sdr/SWAA2024052981479), May 1, 2024: FLOORBEAM. CORRODED. CORROSION ON UPPER FLANGE OF BS 986 FLOORBEAM RBL 38-46 WL 208. ACCOMPLISHED UPPER FLANGE ON BS 986 FLOORBEAM REPAIR IAW SRM 53-70-51-2R-6; ALTERNATIVE 3.; FIG 
- [SDR SWAA2024052981476](https://openairdocs.org/sdr/SWAA2024052981476), May 1, 2024: FLOORBEAM. CORRODED. CORROSION ON UPPER FLANGE OF BS 986 FLOOR BEAM LBL 44-46 WL 208. ACCOMPLISHED UPPER FLANGE ON BS 986 FLOOR BEAM REPAIR IAW SRM 53-70-51-2R-6, ALTERNATIVE 3, FIG
- [SDR SWAA2024052980947](https://openairdocs.org/sdr/SWAA2024052980947), Apr 30, 2024: SHIELD. CRACKED. FWD CARGO BAY FWD SHIELD BS420+1 RBL22 WL156 IS CRACKED AT FASTENER HOLE<[01] REMOVED DAMAGED SHIELD; LOCATED; DRILLED; APPLIED CIC AND INSTALLED NEW FWD CARGO 
- [SDR SWAA2024052980943](https://openairdocs.org/sdr/SWAA2024052980943), Apr 30, 2024: INTERCOSTAL. CORRODED. CORROSION AFT CARGO BAY INTERCOSTAL BS767+2 S-27R WL150. CORROSION ON AFT CARGO BAY INTERCOSTAL BS 767 TO 787 STR 27R FOUND TO BE OUT OF LIMITS. REMOVED; REPLAC
- [SDR SWAA2024052980948](https://openairdocs.org/sdr/SWAA2024052980948), Apr 30, 2024: SIDEWALL SUPPORT. CORRODED. CORROSION AFT CARGO BAY R/H FLOOR TO SIDEWALL SUPPORT PLATE HAS MULTIPLE AREAS AROUND NUT PLATE HOLES BS727B TO BS767 RBL22 WL156. REAPPLIED WHITE ENAMEL AS PER
- [SDR SWAA2024052980949](https://openairdocs.org/sdr/SWAA2024052980949), Apr 30, 2024: SIDEWALL SUPPORT. CORRODED. CORROSION AFT CARGO BAY L/H FLOOR TO SIDEWALL SUPPORT PLATE MULTIPLE AREAS AROUND NUT PLATE HOLES BS727B TO BS767 LBL22 WL156. REAPPLIED WHITE ENAMEL AS PER ACO
- [SDR SWAA2024052980950](https://openairdocs.org/sdr/SWAA2024052980950), Apr 30, 2024: SHIELD. CORRODED. CORROSION AFT CARGO BAY SHIELD FWD OF CARGO DOOR AROUND MULTIPLE NUT PLATE HOLES BS767+3 TO BS794 RBL22 WL156. REAPPLIED WHITE ENAMEL AS PER ACO 5360-E-16462. C
- [SDR SWAA2024052979727](https://openairdocs.org/sdr/SWAA2024052979727), Apr 26, 2024: LENS. MISSING. CABIN SIDEWALL PANEL 231YHW EMERGENCY LIGHT LENS MISSING.<[01] REMOVED AND REPLACED CABIN SIDEWALL PANEL 231YHW EMERGENCY LIGHT LENS PER AMM 33-51-01-960-801;[0
- [SDR SWAA2024052979707](https://openairdocs.org/sdr/SWAA2024052979707), Apr 26, 2024: RIB. CRACKED. RH HORIZONTAL STABILIZER RIB #4 STAB STA 120.30; 3RD STIFFENER FROM FRONT IS CRACKED. REPAIRED RH HORIZONTAL STABILIZER RIB #4 STAB STA 120.30; 3RD STIFFENER FR
- [SDR SWAA2024052979708](https://openairdocs.org/sdr/SWAA2024052979708), Apr 26, 2024: SKIN. CRACKED. LH HORIZONTAL STABILIZER LOWER SKIN AT STATION 193.90 CRACKED. REMOVED CRACK DAMAGE ON LEFT HORIZONTAL STABILIZER LOWER SKIN AT STA 193.90 AND INSTALLED REPAIR 
- [SDR SWAA2024052979059](https://openairdocs.org/sdr/SWAA2024052979059), Apr 25, 2024: SKIN. DEBONDED. PANEL 194CR OUTER SKIN IS DISBONDED. (MARKED)<[01] REPAIRED DISBONDED OUTER SKIN ON PANEL 194CR IAW SRM 51-70-05-2R-2 AND SRM 51-70-05-2R-11;[02] VERIFIED CORRE
- [SDR SWAA2024052979061](https://openairdocs.org/sdr/SWAA2024052979061), Apr 25, 2024: SKIN. DEBONDED. PANEL 193B OUTER SKIN IS DISBONDED. (MARKED)<[01] 04 - REPAIRED PER [SRM 51-70-05-2R-2-A00733 (REPAIR 2 - REPAIR OF DAMAGE THAT IS MORE THAN 0.50 INCH (12.70 MM
- [SDR SWAA2024052989611](https://openairdocs.org/sdr/SWAA2024052989611), Apr 25, 2024: CABLE. LOW TENSION. HORIZ STAB CONTROL CABLES STA AND STB HAVE LOW TENSION. REMOVED DRIP SHIELD IAW AMM 27-41-00-820-801 STEP 2.G.(6). ADJUSTED HORIZ STAB CABLES STA & STB IAW AMM 
- [SDR SWAA2024052978381](https://openairdocs.org/sdr/SWAA2024052978381), Apr 23, 2024: BRACKET. CRACKED. BLEED AIR SUPPORT BRACKET ON CENTER SECTION IS CRACKED AT BS 540 LBL 8.<[01] REPLACED BLEED AIR SUPPORT BRACKET ON CENTER SECTION AT BS 540 LBL 8 IAW SRM 51-40-
- [SDR SWAA2024052978388](https://openairdocs.org/sdr/SWAA2024052978388), Apr 23, 2024: BRACKET. CRACKED. BLEED AIR SUPPORT BRACKET ON CENTER SECTION IS CRACKED AT BS 540 RBL 8.<[01] REPLACED BLEED AIR SUPPORT BRACKET ON CENTER SECTION AT BS 540 RBL8 IAW SRM 51-40-0
- [SDR SWAA2024052978620](https://openairdocs.org/sdr/SWAA2024052978620), Apr 23, 2024: ATTACH ANGLE. CRACKED. B.S. 663 LOWER COMPOSITE BULKHEAD UPPER ATTACH ANGLE IS CRACKED AT R.B.L. 10; W.L. 164.<[01] CRACK FOUND TO BE OUT OF LIMITS AS PER SRM 57-10-10-1A-2. REMOVED D
- [SDR SWAA2024020748796](https://openairdocs.org/sdr/SWAA2024020748796), Feb 5, 2024: HOLDER. LOOSE. FORWARD ENTRY DOOR GIRT BAR HOLDER IS LOOSE<[01] RESECURED L1 DOOR GIRT BAR HOLDER ON DOOR PER SIP OPS GOOD
- [SDR SWAA2026071488360](https://openairdocs.org/sdr/SWAA2026071488360), Aug 10, 2023: NOZZLE. INOPERATIVE. NR 2 ENGINE OIL QTY DROPPED TO 0 AT CRUISE, IN DECENT OIL PRESSURE DROPPED AND WENT RED, SHUTDOWN ENGINE. SMOOTH UNEVENTFUL LANDING. R & R PRIMARY NOZZLE ASSY I
- [SDR SWAA2023081488360](https://openairdocs.org/sdr/SWAA2023081488360), Aug 10, 2023: NOZZLE. INOPERATIVE. #2 ENGINE OIL QTY DROPPED TO 0 AT CRUISE; IN DECENT OIL PRESSURE DROPPED AND WENT RED; SHUTDOWN ENGINE. SMOOTH UNEVENTFUL LANDING.<[01] R/R PRIMARY NOZZLE ASSY 
- [SDR SWAA2023050545518](https://openairdocs.org/sdr/SWAA2023050545518), May 4, 2023: BATTERY PACK. INOPERATIVE. FWD ENTRY EMERGENCY LIGHTS INOP.<[01] REMOVED AND REPLACED M1675 POWER SUPPLY BATTERY PACK PER AMM 33-51-06; OPS CHECKS GOOD.

All 146: https://openairdocs.org/aircraft/N7869A/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 N7869A

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N7869A before.

- [Cancelled 1973-06-24](https://openairdocs.org/deregistered/N7869A-1973-06-24): Cessna 180A, S/N 32766. Owner: [Meredith Robert](https://openairdocs.org/faa-owner/MEREDITH%20ROBERT), [Valleto, CA](https://openairdocs.org/faa-place/CA/Valleto)

## 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

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.