# N7824A: 2001 Boeing 737-7BK

- Status: Valid registration
- Airframe: [Boeing 737-7BK](https://openairdocs.org/model/boeing-737-7bk) (registry code 1384600, 149 seats)
- Engine: [CFM International CFM56 series](https://openairdocs.org/engine/cfm-international-cfm56-series) (registry code 13802)
- Serial number: 30617
- Year built: 2001
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: March 5, 2011
- Certificate issued: May 13, 2026
- Expires: May 31, 2033
- Mode S code: AA9AD9
- Registered owner: [Unical Aviation Inc](https://openairdocs.org/faa-owner/UNICAL%20AVIATION%20INC)
- Location: [Glendale, AZ](https://openairdocs.org/faa-place/AZ/Glendale)
- Owner type: Corporation
- Owner's area on the map: 33.5162° N, 112.4236° W: Placed by OpenAirDocs at the center of ZIP code 85340, within about 3 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=7824A
- Page: https://openairdocs.org/aircraft/N7824A

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 model are included.

## ADs that may apply (OpenAirDocs): 55 in force

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

None in force.

### Matched by engine (CFM International CFM56 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 2017-14-08](https://openairdocs.org/ad/2017-14-08): Turbine Engine Compressor Section · CFM International CFM56-3, CFM56-3B and CFM56-3C. Effective Aug 18, 2017
- [AD 2017-05-09](https://openairdocs.org/ad/2017-05-09): Accessory Gearboxes · CFM International CFM56-5B1, CFM56-5B1/2P, CFM56-5B1/3 and 33 more. Effective Apr 13, 2017
- [AD 2016-14-10](https://openairdocs.org/ad/2016-14-10): High-pressure turbine (HPT) disks · CFM International CFM56-3, CFM56-3B and CFM56-3C with STC SE00034EN. Effective Aug 9, 2016
- [AD 2016-02-04](https://openairdocs.org/ad/2016-02-04): Turbine rear frames (TRFs) · CFM International CFM56-5B1, CFM56-5B1/2P, CFM56-5B1/3 and 33 more. Effective Mar 1, 2016
- [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 2013-14-06](https://openairdocs.org/ad/2013-14-06): Hydro-mechanical unit (HMU) fuel control · CFM International CFM56-5, CFM56-5B1, CFM56-5B1/2P and 34 more. Effective Sep 3, 2013
- [AD 2012-02-03](https://openairdocs.org/ad/2012-02-03): Engine · CFM International CFM56-5B1/3, CFM56-5B2/3, CFM56-5B3/3 and 8 more. Effective Mar 15, 2012
- [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 2010-12-03](https://openairdocs.org/ad/2010-12-03): Fan blades · CFM International CFM56-3 and CFM56-3B. Effective Jul 13, 2010
- [AD 2010-09-14](https://openairdocs.org/ad/2010-09-14): Exhaust gas temperature (EGT) · CFM International CFM56-5B1/2P, CFM56-5B1/P, CFM56-5B2/2P and 16 more. Effective Jun 8, 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 2009-18-01](https://openairdocs.org/ad/2009-18-01): LP turbine rear frames · CFM International CFM56-5B1/3, CFM56-5B1/P, CFM56-5B2/3 and 19 more. Effective Oct 1, 2009
- [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 2007-24-04](https://openairdocs.org/ad/2007-24-04): Low pressure turbine (LPT) · CFM International CFM56-5C4/1. Effective Dec 6, 2007
- [AD 2007-03-15](https://openairdocs.org/ad/2007-03-15): Exhaust gas temperature (EGT) harness · CFM International CFM56-5, CFM56-5B1, CFM56-5B1/2P and 34 more. Effective Mar 19, 2007
- [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 2005-10-05](https://openairdocs.org/ad/2005-10-05): Air turbine starters · CFM International CFM56-5, CFM56-5B1, CFM56-5B1/2P and 50 more. Effective Jun 14, 2005
- [AD 97-09-02 R3](https://openairdocs.org/ad/97-09-02-R3): High pressure turbine rotor (HPTR) front shafts · CFM International CFM56-5C2, CFM56-5C3/G and CFM56-5C4. Effective Oct 14, 2004
- [AD 2004-10-13](https://openairdocs.org/ad/2004-10-13): Service main fuel pumps · CFM International CFM56-3, CFM56-5, CFM56-5-A1/F and 4 more. Effective Jun 24, 2004
- [AD 2002-22-12](https://openairdocs.org/ad/2002-22-12): Titeflex hoses · BAE Systems ATP, Avro 146-RJ100A, Avro 146-RJ70A and 122 more. Effective Dec 13, 2002
- [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 2002-02-13](https://openairdocs.org/ad/2002-02-13): Magnetic Drain Plug · CFM International CFM56-5, CFM56-5-A1/F, CFM56-5A4 and 33 more. Effective Mar 21, 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 2001-09-17](https://openairdocs.org/ad/2001-09-17): Fuel Manifold and CJ9L Harness · CFM International CFM56-5C2, CFM56-5C2/4, CFM56-5C2/F and 13 more. Effective May 14, 2001
- [AD 2001-04-06](https://openairdocs.org/ad/2001-04-06): Fan Disk · CFM International CFM56-3, CFM56-3B and CFM56-3C. Effective Apr 4, 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 2000-15-01](https://openairdocs.org/ad/2000-15-01): Fuel Leakage · CFM International CFM56-2, CFM56-2A, CFM56-2B and 39 more. Effective Oct 2, 2000
- [AD 2000-05-22](https://openairdocs.org/ad/2000-05-22): CFM International CFM56-2, CFM56-2A, CFM56-2B and 3 more. Effective May 2, 2000
- [AD 99-06-16](https://openairdocs.org/ad/99-06-16): High Pressure Turbine Rotor (HPTR) Front Air Seal · CFM International CFM56-5, CFM56-5-A1/F, CFM56-5A4 and 3 more. Effective Apr 21, 1999
- [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
- [AD 98-19-10](https://openairdocs.org/ad/98-19-10): Accessory Gearbox · CFM International CFM56-3, CFM56-3B and CFM56-3C. Effective Sep 28, 1998
- [AD 98-12-32](https://openairdocs.org/ad/98-12-32): High Pressure Turbine Rotor Disks · CFM International CFM56-2, CFM56-2A, CFM56-2B and 3 more. Effective Jul 20, 1998
- [AD 98-10-11](https://openairdocs.org/ad/98-10-11): Accessory Gearbox · CFM International CFM56-3, CFM56-3B, CFM56-3C and 31 more. Effective Jun 3, 1998
- [AD 98-07-02](https://openairdocs.org/ad/98-07-02): Air/oil Seal · CFM International CFM56-3, CFM56-3B and CFM56-3C. Effective Mar 30, 1998
- [AD 98-02-04](https://openairdocs.org/ad/98-02-04): Low Pressure Turbine Case · CFM International CFM56-5B1/2P, CFM56-5B2/2P, CFM56-5B3/2P and 1 more. Effective Mar 23, 1998
- [AD 89-23-06 R1](https://openairdocs.org/ad/89-23-06-R1): Magnetic Chip Detector · CFM International CFM56-2, CFM56-2A, CFM56-3 and 8 more. Effective Jan 28, 1998
- [AD 97-08-01](https://openairdocs.org/ad/97-08-01): Fan Disks · CFM International CFM56-3, CFM56-3B and CFM56-3C. Effective Jun 23, 1997
- [AD 97-06-01](https://openairdocs.org/ad/97-06-01): High Pressure Compressor Rotor (HPCR) Stage 1-2 Spool · CFM International CFM56-5, CFM56-5B1, CFM56-5B1/2P and 28 more. Effective Jun 3, 1997
- [AD 97-05-13](https://openairdocs.org/ad/97-05-13): Air Turbine Engine Starter · CFM International CFM56-5, CFM56-5-A1/F, CFM56-5A4 and 3 more. Effective Jun 3, 1997
- [AD 96-25-11](https://openairdocs.org/ad/96-25-11): Redesigned Fan Blades · CFM International CFM56-3B and CFM56-3C. Effective Jan 29, 1997

### 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 2013-02-02](https://openairdocs.org/ad/2013-02-02) (historical): High-pressure turbine (HPT) disks · CFM International CFM56-3, CFM56-3B and CFM56-3C with STC SE00034EN. Effective Jan 28, 2013
- [AD 2009-01-01](https://openairdocs.org/ad/2009-01-01) (historical): Exhaust gas temperature (EGT) · CFM International CFM56-5B1, CFM56-5B1/2P, CFM56-5B1/P and 22 more. Effective Dec 31, 2008
- [AD 97-09-02 R2](https://openairdocs.org/ad/97-09-02-R2) (historical): Low pressure turbine rotor (LPTR) · CFM International CFM56-5C2, CFM56-5C2/4, CFM56-5C2/F and 9 more. Effective Apr 29, 2003
- [AD 2003-02-04](https://openairdocs.org/ad/2003-02-04) (historical): Exhaust gas temperature (EGT) · CFM International CFM56-5 Series (all). Effective Feb 27, 2003
- [AD 97-09-02 R1](https://openairdocs.org/ad/97-09-02-R1) (historical): High Pressure Turbine rotor (HPTR) front shaft · CFM International CFM56-5C2/G, CFM56-5C2/G4, CFM56-5C3/G and 3 more. Effective Sep 24, 2002
- [AD 2001-17-14](https://openairdocs.org/ad/2001-17-14) (historical): LPT Conical Supports · CFM International CFM56-5C4/1. Effective Sep 7, 2001
- [AD 2001-08-51](https://openairdocs.org/ad/2001-08-51) (historical): Fuel leakage · CFM International CFM56-5 Series (all)
- [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
- [AD 99-08-16](https://openairdocs.org/ad/99-08-16) (historical): CFM International CFM56-2, CFM56-2A, CFM56-2B and 3 more. Effective May 13, 1999
- [AD 97-09-02](https://openairdocs.org/ad/97-09-02) (historical): High/Low Pressure Turbine Rotor · CFM International CFM56-5C2/G, CFM56-5C2/G4, CFM56-5C3/G and 3 more. Effective Jun 30, 1997

All 71: https://openairdocs.org/aircraft/N7824A/ads.md

## Information bulletins (advisory) (4 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-13-33R2](https://openairdocs.org/saib/NE-13-33R2): Turbine Engine Air Inlet Section - LP Turbine, Stage 1 Nozzle Vanes. Issued Jan 28, 2014
- [SAIB NE-12-29](https://openairdocs.org/saib/NE-12-29): Engine Fuel Distribution  CFM56-5B LPTACC Fuel Manifold. Issued Apr 27, 2012
- [SAIB NE-06-02](https://openairdocs.org/saib/NE-06-02): . Issued Oct 18, 2005
- [SAIB NE-13-33R1](https://openairdocs.org/saib/NE-13-33R1) (historical): Turbine Engine Air Inlet Section - LP Turbine, Stage 1 Nozzle Vanes. Issued Jun 24, 2013
- [SAIB NE-13-33](https://openairdocs.org/saib/NE-13-33) (historical): Turbine Engine Air Inlet Section - LP Turbine, Stage 1 Nozzle Vanes. Issued May 13, 2013
- [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 N7824A.

## FAA accident and incident reports

None matched to N7824A.

## Service difficulty reports (154, 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 SWAA2025081403550](https://openairdocs.org/sdr/SWAA2025081403550), Aug 12, 2025: LAMP. INOPERATIVE. CENTER AISLE AFT EMERGENCY EXIT SIGN HAS 2 LIGHTS INOP. RELAMPED CENTER AISLE AFT EMERGENCY EXIT SIGN REF AMM. 33-51-01. OPS CHECKS GOOD AT THIS TIME.
- [SDR SWAA2025080597318](https://openairdocs.org/sdr/SWAA2025080597318), Aug 1, 2025: BATTERY PACK. INOPERATIVE. SEVERAL FWD EMERGENCY LIGHTS INOP<[01] REMOVED AND REPLACED BATTERY AND POWER SUPPLY AT POSITION M1674 PER AMM 33-51-06.
- [SDR SWAA2025040721655](https://openairdocs.org/sdr/SWAA2025040721655), Apr 4, 2025: HANDLE. LOOSE. RT AFT SERVICE DOOR HANDLE IS LOOSE. CHECKED SECURITY OF AFT RH SERVICE DOOR PER AMM 52-41-31. OPERATED DOOR SEVERAL TIMES. NO DEFECTS NOTED.
- [SDR SWAA2025032106137](https://openairdocs.org/sdr/SWAA2025032106137), Mar 17, 2025: CABIN AIR SYS. ODOR. ELECTRICAL BURNING SMELL ON FLIGHT DECK AND FOLLOWED THROUGH CABIN THEN FEW MINUTES LATER; LEFT PACK TRIP OFF ANNUNCIATION LIGHT CAME ON <[01] EIE.
- [SDR SWAA2025013191734](https://openairdocs.org/sdr/SWAA2025013191734), Jan 31, 2025: LIGHT. INOPERATIVE. MID CABIN 3 ISLE EMERGENCY LIGHTS INOP<[01] REPLACED POWER SUPPLY CHARGER ASSY ON 12DEF REF AMM 33-51-06. EMERGENCY LIGHTS OP CHECK NORMAL.
- [SDR SWAA2025010783668](https://openairdocs.org/sdr/SWAA2025010783668), Jan 7, 2025: BATTERY PACK. INOPERATIVE. EMERGENCY LIGHTS INOPERATIVE INTERIOR EXIT DOOR AND EXTERIOR EXIT DOOR ROW 12 FED.<[01] 01 - REMOVED AND REPLACED PER [AMM 33-51-06-960-805-NG (POWER SUPPLY - B
- [SDR SWAA2024121777272](https://openairdocs.org/sdr/SWAA2024121777272), Dec 14, 2024: POWER SUPPLY. INOPERATIVE. EMERGENCY LIGHT R/H OVERWING INOP<[01] REMOVED AND REPLACED R/H OVERWING EMERGENCY LIGHTS POWER SUPPLY. TEST OK . REF AMM. 33-51-06. -END-
- [SDR SWAA2024112561791](https://openairdocs.org/sdr/SWAA2024112561791), Nov 20, 2024: WIRE. BROKEN. RH OVER-WING EMERGENCY EXIT SIGN ASSEMBLY HAS BROKEN WIRE.<[01] REMOVED AND REPLACED RH OVERWING EMERGENCY EXIT SIGN ASSEMBLY IN REF TO AMM 33-51-01. OPS CHECK 
- [SDR SWAA2024112561790](https://openairdocs.org/sdr/SWAA2024112561790), Nov 20, 2024: BATTERY PACK. INOPERATIVE. EXIT ROW EMERGENCY LIGHT INOP<[01] REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK AT ROW 12 RH SIDE IN REF TO AMM 33-51-06. OPS CHECK GOOD.
- [SDR SWAA2024102151102](https://openairdocs.org/sdr/SWAA2024102151102), Oct 19, 2024: SENSOR. FAULTY. RED NOSE GEAR LIGHT ON FORWARD PANEL STAYED ILLUMINATED AS WELL AS THE GREEN NOSE LIGHT ON OVERHEAD PANEL; ON RETRACTION. NORMAL ON LANDING<[01] REMOVED AND REP
- [SDR SWAA2024100444003](https://openairdocs.org/sdr/SWAA2024100444003), Sep 30, 2024: HANDLE. LOOSE. FWD NTRY DOO OPEN/CLOSE ASSIST HANDLE NEDS TO BE RESECURED. FWD ENTRY DOOR OPEN/CLOSE ASSIST HANDLE NEEDS TO BE RESECURED<[01] REINSTALLED ASSIST HANDLE PER AMM
- [SDR SWAA2024081926781](https://openairdocs.org/sdr/SWAA2024081926781), Aug 15, 2024: SIGN. DETACHED. EXIT SIGN AT RH OVERWING EXIT FELL OFF<[01] INSTALLED EXIT SIGN AT RH OVERWING EXIT PER AMM 33-51-01
- [SDR SWAA2024071512778](https://openairdocs.org/sdr/SWAA2024071512778), Jul 10, 2024: SWITCH. FAULTY. CIRCUIT BREAKER PANEL P6-2 CIRCUIT BREAKER B10 POPPED. PER MOC; CIRCUIT BREAKER WAS RESET AND IT POPPED AGAIN. CIRCUIT BREAKER IS LABELED STAB TRIM CONT<[01] R&
- [SDR SWAA2024071512771](https://openairdocs.org/sdr/SWAA2024071512771), Jul 10, 2024: MOTOR. FAULTY. CIRCUIT BREAKER PANEL P6-2 CIRCUIT BREAKER B10 POPPED. PER MOC; CIRCUIT BREAKER WAS RESET AND IT POPPED AGAIN. CIRCUIT BREAKER IS LABELED STAB TRIM CONT<[01] R&
- [SDR SWAA2024052889796](https://openairdocs.org/sdr/SWAA2024052889796), May 24, 2024: CIRCUIT BREAKER. TRIPPED. SET FLAP HANDLE TO 5; FLAP INDICATOR DID NOT MOVE. RAN QRH. WITH ALTERNATE FLAP POSITION SWITCH TO DOWN; RECEIVED SLIGHT ASYMMETRY. LANDED NO FLAPS; RAN BRAKE C
- [SDR SWAA2024021349875](https://openairdocs.org/sdr/SWAA2024021349875), Feb 8, 2024: LENS. OUT OF ADJUST. REJECT - EMERGENCY EXIT LIGHT LENS @ LH ROW 7 IS NOT SEATED AND PROTRUDING WITH BUILT UP SILICONE SEALANT<[01] REMOVED EMERGENCY EXIT LIGHT LENS AT L/H SEAT ROW
- [SDR SWAA2024021348811](https://openairdocs.org/sdr/SWAA2024021348811), Feb 5, 2024: LIGHT. BROKEN. EMERGENCY EXIT LIGHT ON BULLNOSE AT L/H ROW 7 IS BUSTED UP<[01] REMOVED AND REPLACED EMERGENCY EXIT LIGHT ON BULLNOSE AT L/H ROW 7; PERFORMED A GOOD FUNCTIONAL 
- [SDR SWAA2024021343932](https://openairdocs.org/sdr/SWAA2024021343932), Jan 23, 2024: PANEL. CRACKED. MID CABIN WING CENTER SECTION BREAK PANEL IS CRACKED AT FASTENER AT BS 540; RBL 1; WL 208<[01] REMOVED AND REPLACED MID CABIN WING CENTER SECTION BREAK PANEL AT
- [SDR SWAA2024021343686](https://openairdocs.org/sdr/SWAA2024021343686), Jan 23, 2024: FLOOR PANEL. PULLED. FLOOR PANEL 231XF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 231XF WITH UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A NEWLY FABRICAT
- [SDR SWAA2024021343687](https://openairdocs.org/sdr/SWAA2024021343687), Jan 23, 2024: FLOOR PANEL. PULLED. FLOOR PANEL 241AF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FABRICATION OF NEW FLOOR PANEL 241AF HAS BEEN COMPLETED IAW SRM 53-00-50-2R-0.<BR><BR>ATTACHED CU
- [SDR SWAA2024021343688](https://openairdocs.org/sdr/SWAA2024021343688), Jan 23, 2024: FLOOR PANEL. PULLED. FLOOR PANEL 241DF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 241DF WITH UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A NEWLY FABRICAT
- [SDR SWAA2024021343977](https://openairdocs.org/sdr/SWAA2024021343977), Jan 23, 2024: STRINGER. CRACKED. AREA AFT OF FCB HAS A CRACKED STR AT THE AFT FASTENER; STR 25R; BS 520+19<[01] 'REPAIRED PER EA 24-153-00206. THIS IS A CATEGORY A REPAIR AS DEFINED IN 737-700 
- [SDR SWAA2024021343373](https://openairdocs.org/sdr/SWAA2024021343373), Jan 21, 2024: PRESSURE DECK. CRACKED. RH HORIZONTAL PRESSURE DECK WEB CRACKED; BS 663 + 2; RBL 41<[01] NDT HFEC SURFACE INSPECTED AREAS IAW 737 NDTM PART 6 51-00-00 PROC 23. .400' LONG CRACK NOTED. 
- [SDR SWAA2023112724652](https://openairdocs.org/sdr/SWAA2023112724652), Nov 23, 2023: SIGN. MISSING. FWD SERVICE DOOR EMERGENCY EXIT LIGHT LENS MISSING FLOOR LEVEL<[01] REPLACED EXIT SIGN LIGHT ASSY REF AMM 33-51-01
- [SDR SWAA2023092805022](https://openairdocs.org/sdr/SWAA2023092805022), Sep 27, 2023: PIN. HANDLER ERROR. RT. GEAR WUOLD NOT RETRACT<[01] REMOVED RT. MLG PIN PER AMM 32-00-01
- [SDR SWAA2023090195698](https://openairdocs.org/sdr/SWAA2023090195698), Aug 31, 2023: ELEC CONNECTOR. ARCED. CAS L1 WINDOW AT TOP BY GRAB HANDLE ELECTRICAL CONTACT IN GLASS STARTED ARCING FOR ABOUT 10 SECONDS BRIEF BURNING SMELL AND STOPPED WINDOW CRACKED ON LANDING<[0
- [SDR SWAA2023052350536](https://openairdocs.org/sdr/SWAA2023052350536), May 20, 2023: GIRT BAR. OUT OF ADJUST. F/A REPORTS R1 GIRT BAR DIFFICULT TO OPERATE. (ARM/DISARM)<[01] VERIFIED POSITION OF SETTING AND ENGAGEMENT OF R1 DOOR SLIDE GIRT BAR WITH CORRESPONDING FLOOR M
- [SDR SWAA2023050142169](https://openairdocs.org/sdr/SWAA2023050142169), Apr 27, 2023: LENS. OUT OF POSITION. GROUND CREW REPORTS L1 DOOR EMERGENCY EXIT LIGHT LENS IS RECESSED<[01] REINSTALLED L1 DOOR EMERGENCY EXIT LIGHT LENS PER AMM 33-51-04. AIRCRAFT OK FOR SERVICE.
- [SDR SWAA2023030310649](https://openairdocs.org/sdr/SWAA2023030310649), Feb 28, 2023: BATTERY PACK. FAILED. R/H AFT CABIN EMERGENCY LIGHTS FAILED CAPACITY TEST<[01] REPLACED BATTERY PACK PER AMM 33-51-00
- [SDR SWAA2023030310638](https://openairdocs.org/sdr/SWAA2023030310638), Feb 28, 2023: BATTERY PACK. FAILED. L/H AFT CABIN EMERGENCY LIGHTS ILLUMINATED FOR 2 SECONDS THEN WENT OUT<[01] REPLACED BATTERY PACK PER AMM 33-51-00
- [SDR SWAA2023030310637](https://openairdocs.org/sdr/SWAA2023030310637), Feb 28, 2023: LIGHT. INOPERATIVE. L/H OVERWING EXIT AFT EMERGENCY LIGHT INOP.<[01] R&R CABIN EMERGENCY EXIT LIGHT PER AMM 33-21-00;[02] C/W INSPECTION
- [SDR SWAA2023012493721](https://openairdocs.org/sdr/SWAA2023012493721), Jan 20, 2023: SLIDE. DISLODGED. FWD SERVICE DOOR EMERGENCY SLIDE FELL OUT OF HOLDER<[01] RESTORED SLIDE IAW MM 25-66-01
- [SDR SWAA2022120577852](https://openairdocs.org/sdr/SWAA2022120577852), Dec 3, 2022: CONNECTOR. DISCONNECTED. OVERHEAD EMERGENCY LIGHT AT SEAT 9ABC INOPERATIVE. FOUND LIGHT ASSY ELECTRICAL CONNECTOR DISCONNECTED. REATTACHED THE CONNECTOR IAW SIP. EMERGENCY LIGHTS OPS TE
- [SDR SWAA2022071126407](https://openairdocs.org/sdr/SWAA2022071126407), Jul 7, 2022: PANEL. CRACKED. RT WING FIXED TE PANEL FITTING CRACKED AT APPR WS 278.5 / [01] R&R PANEL AS PER SRM 51-40-02
- [SDR SWAA2022062220179](https://openairdocs.org/sdr/SWAA2022062220179), Jun 18, 2022: PANEL. ELONGATED. 193B PANEL VARIOUS FASTENER HOLES (30) ARE ELONGATED. / [01] R & R 193B WING TO BODY PANEL PER AMM 53-51-21.
- [SDR SWAA2022033085887](https://openairdocs.org/sdr/SWAA2022033085887), Mar 21, 2022: PANEL. CORRODED. CORROSION BULKHEAD PANEL 121EW AT FWD CARGO COMPARTMENT 2022-109470 / [01] REPLACED BULKHEAD PANEL 121EW AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND 
- [SDR SWAA2022033078116](https://openairdocs.org/sdr/SWAA2022033078116), Feb 25, 2022: WEB. CRACKED. CRACK ON WEB FORWARD CARGO COMPARTMENT LOC.STR25L TO STR26L AND BETWEEN STA 460LH TO STA 480LH 2022-109408 / [01] TOOL USED P/N 500-196-30 S/N A20231804 CAL DUE
- [SDR SWAA2022033078115](https://openairdocs.org/sdr/SWAA2022033078115), Feb 25, 2022: SUPPORT. CRACKED. CRACK ON ANGLE SUPPORTS FORWARD CARGO COMPARTMENT LOC.SRT 25L TO 26L AND STA 460 2022-109409 / [01] REPLACED ANGLE SUPPORT LOC. FORWARD CARGO COMPARTMENT BTW SR
- [SDR SWAA2022033077072](https://openairdocs.org/sdr/SWAA2022033077072), Feb 23, 2022: PANEL. CRACKED. CRACK ACCESS PANEL 191D BODY FAIRING AT LOWER FUSELAGE 2022-109399 / [01] TOOL USED CALIPER P/N: 500-464; S/N: 15331932; DUE DATE: 26-OCT-22;[02] TOOL USED HOTB
- [SDR SWAA2022033076716](https://openairdocs.org/sdr/SWAA2022033076716), Feb 22, 2022: ANGLE. CRACKED. CRACK ON BRACKET LOCATED BTW BS 259.5 TO BS 277 AND STR 10L AT PASSENGER CABIN 2022-109386 / [01] TOOL USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 1
- [SDR SWAA2022033076717](https://openairdocs.org/sdr/SWAA2022033076717), Feb 22, 2022: ANGLE. CRACKED. CRACK ON BRACKET LOCATED BTW BS 259.5 TO BS 277 AND STR 8L AT PASSENGER CABIN 2022-109387 / [01] TOOL USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 14
- [SDR SWAA2022033076711](https://openairdocs.org/sdr/SWAA2022033076711), Feb 22, 2022: BRACKET. CRACKED. CRACK SUPPORT BRACKET LOCATED BS 540 BETWEEN BL 0 LBL 24.75 AT PASSENGER CABIN 2022-109370 / [01] REPLACED SUPPORT BRACKET LOCATED BS 540 BETWEEN BL 0 LBL 24.75
- [SDR SWAA2022033076332](https://openairdocs.org/sdr/SWAA2022033076332), Feb 21, 2022: ANGLE. CRACKED. CRACK ANGLE ON WATER SERVICE INTERNAL AREA LOCATED ON BS907 PLUS 11 INCHES AND RBL13 AFT CARGO COMPARTMENT 2022-109344 / [01] REPLACED ANGLE LOCATED ON WATER SE
- [SDR SWAA2022033076334](https://openairdocs.org/sdr/SWAA2022033076334), Feb 21, 2022: SUPPORT. CORRODED. CORROSION SUPPORT ZEE LOCATED BS727B TO BS787; LBL21 AND WL156.5 AFT CARGO COMPARTMENT 2022-109341 / [01] REPLACED NEW SUPPORT ZEE LOCATED BETWEEN BS727 TO BS84
- [SDR SWAA2022033075406](https://openairdocs.org/sdr/SWAA2022033075406), Feb 19, 2022: ANGLE. CORRODED. CRACK FRONT SPAR SUPPORT ANGLE LOCATED AT IFSS 120 AND WBL 94.24 AT RT WING 2022-109294 / [01] TOOL USED: DIGITAL CALIPER P/N: 500-193-30; S/N: 0000293; DUE DAT
- [SDR SWAA2022033075633](https://openairdocs.org/sdr/SWAA2022033075633), Feb 19, 2022: ANGLE. CRACKED. CRACK FRONT SPAR SUPPORT ANGLE LOCATED IFSS 120 AND WBL94.24 AT LT WING 2022-109296 / [01] TOOL USED: DIGITAL CALIPER P/N 500-193-30 S/N 0000293 DUE DATE 16 SEP
- [SDR SWAA2022033075404](https://openairdocs.org/sdr/SWAA2022033075404), Feb 18, 2022: TIE CLIP. CRACKED. CRACK TIE CLIP LOCATED AT BS 277 AND STRINGER 10R AT PASSENGER CABIN 2022-109285 / [01] REPLACED TIE CLIP LOCATED AT BS 277 AND STRINGER 10R AT PASSENGER CABIN 
- [SDR SWAA2022033075405](https://openairdocs.org/sdr/SWAA2022033075405), Feb 18, 2022: BEAM. CRACKED. CRACK EXISTING REPAIR ON STUD BEAM LOCATED BS 294.5 AND STRINGER 17R AT PASSENGER CABIN 2022-109286 / [01] REPLACED STUD BEAM(FRAME) AND FASTENERS LOCATED BS 29
- [SDR SWAA2022033073965](https://openairdocs.org/sdr/SWAA2022033073965), Feb 17, 2022: STRINGER. CRACKED. CRACK STRINGER 27R LOC BS540 AT FWD CARGO COMPARTMENT 2022-109250 / [01] TOOL USED: ULTRASONIC THICKNESS GAGE P/N: 45MG S/N:130064101 DUE DATE: 11-MAR-22;[02] T
- [SDR SWAA2022033073968](https://openairdocs.org/sdr/SWAA2022033073968), Feb 17, 2022: STRINGER. CRACKED. CRACK STRINGER 26L LOC BS540 AT FWD CARGO COMPARTMENT 2022-109256 / [01] TOOL USED: ULTRASONIC THICKNESS GAGE P/N: 45MG S/N:130064101 DUE DATE: 11-MAR-22;[02] E

All 154: https://openairdocs.org/aircraft/N7824A/reports.md

## STCs that may be installed (OpenAirDocs) (7)

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 series)

- [STC SE04840NY](https://openairdocs.org/stc/SE04840NY): Installation of HarcoSemco Exhaust Gas Temperature (EGT) Electrical Harnesses in CFM56-7 engine. Kilroy Aviation LLC. Lists CFM56-7B20
- [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. Lists CFM56-7B20
- [STC SE00032EN](https://openairdocs.org/stc/SE00032EN): Installation of Pratt & Whitney (P&W) Global Material Solutions (GMS) CFM56-3 Fan/Booster Module. Pratt & Whitney. Lists CFM56-3
- [STC SE00033EN](https://openairdocs.org/stc/SE00033EN): Installation of Pratt & Whitney (P&W) Global Material Solutions (GMS) CFM56-3 High Pressure Compressor Module. Pratt & Whitney. Lists CFM56-3
- [STC SE00034EN](https://openairdocs.org/stc/SE00034EN): Installation of Pratt & Whitney (P&W) Global Material Solutions (GMS) CFM56-3 High Pressure Turbine Module. Pratt & Whitney. Lists CFM56-3
- [STC SE00035EN](https://openairdocs.org/stc/SE00035EN): Installation of Pratt & Whitney (P&W) Global Material Solutions (GMS) CFM56-3 Low Pressure Turbine Module. Pratt & Whitney. Lists CFM56-3
- [STC SE00822CH](https://openairdocs.org/stc/SE00822CH): Install AeroControlex P/N 2604880-001 variable stator feedback control cable and P/N 2604880-002 variable bleed valve feedback control cable on CFM International engines. AeroControlex Group TransDigm Inc. Lists CFM56-2

## Earlier aircraft with N7824A

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N7824A before.

- [Cancelled 1957-01-08](https://openairdocs.org/deregistered/N7824A-1957-01-08): Cessna 180A, S/N 32721. Owner: [Cessna Aircraft Co](https://openairdocs.org/faa-owner/CESSNA%20AIRCRAFT%20CO), [Wichita, KS](https://openairdocs.org/faa-place/KS/Wichita)

## Related

- Other Boeing 737-7BK aircraft: https://openairdocs.org/model/boeing-737-7bk/aircraft.md
- The CFM International CFM56 series engine: https://openairdocs.org/engine/cfm-international-cfm56-series.md

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