# N7865A: 2002 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 series](https://openairdocs.org/engine/cfm-international-cfm56-series) (registry code 13802) - Serial number: 30647 - Year built: 2002 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: January 6, 2018 - Certificate issued: February 11, 2026 - Expires: February 28, 2033 - Mode S code: AAA9D8 - 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=7865A - Page: https://openairdocs.org/aircraft/N7865A 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 model are included. ## ADs that may apply (OpenAirDocs): 55 in force ### Matched by airframe (Boeing 737-7Q8) 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/N7865A/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 N7865A. ## FAA accident and incident reports None matched to N7865A. ## Service difficulty reports (199, 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 SWAA2025120140306](https://openairdocs.org/sdr/SWAA2025120140306), Nov 26, 2025: COFFEEMAKER. ODOR. UNKNOWN BURNING IN THE FWD GALLEY. PERFORMED INSPECTION IAW AMM 05-51-56 NO ISSUES FOUND BELIEVE COFFEE MAKER. TO BE BAD. ACFT OK FOR SERVICE. - [SDR SWAA2025082206127](https://openairdocs.org/sdr/SWAA2025082206127), Aug 20, 2025: SKIN. CORRODED. LH INBOARD AFT FLAP HAS INTERGRANULAR CORROSION AT TRAILING EDGE APPROX. MID WAY DAMAGE IS LOCATED AT TRAILING EDGE 30.5' FROM OUTBOARD EDGE. DAMAGE IS 3.875 ' - [SDR SWAA2025082106137](https://openairdocs.org/sdr/SWAA2025082106137), Aug 20, 2025: STRINGER SPLICE. CORRODED. AFT CARGO LEFT CENTER CATSTRIP CORRODED. REMOVED AND REPLACED CAPSTRIP PER AMM 25-52-06. - [SDR SWAA2025062083318](https://openairdocs.org/sdr/SWAA2025062083318), Jun 18, 2025: FLOOR PANEL. CRACKED. AFT CARGO FLOOR PANEL IS CRACKED AFT CARGO FLOOR PANEL IS CRACKED2945286 <[01]. REPAIRED FLOOR PANEL IN AFT CARGO COMPARTMENT PER AMM 25-52-01. A/C OK TO CONTIN - [SDR SWAA2025021094476](https://openairdocs.org/sdr/SWAA2025021094476), Feb 8, 2025: BRACKET. LOOSE. FORWARD SERVICE DOOR GIRT BAR BRACKET LOOSE<[01] OK TO CONTINUE PER TLD ; EA M-23-125-01839 ATTACHED
FWD SVC DOOR GIRT BRACKET SECURED WITH SAFETY WIRE
- [SDR SWAA2024121777019](https://openairdocs.org/sdr/SWAA2024121777019), Dec 13, 2024: GIRT BAR. OUT OF POSITION. FA REPORTS AFT ENTRY DOOR GIRT BAR NOT PROPERLY STOWED.<[01] STOWED AFT ENTRY DOOR GIRT BAR PER AMM 25-66-01 - [SDR SWAA2024102451189](https://openairdocs.org/sdr/SWAA2024102451189), Oct 21, 2024: RETAINER. OUT OF ALIGNMENT. AFT SERVICE DOOR ESCAPE SLIDE GIRT BAR RETAINING RING DOES NOT LOCK ONTO THE GIRT BAR.<[01] REMOVED AND REPLACED AFT SERVICE DOOR ESCAPE GIRT BAR RETAINER RING. - [SDR SWAA2024052287701](https://openairdocs.org/sdr/SWAA2024052287701), May 19, 2024: SLIDE. DISLODGED. REF TTG8Q00TF4HQ LP 2662364 FOR ORIGINAL WRITE UP: AFT ENTRY EMERGENCY EXIT SLIDE FELL OUT OF HOLDER WHEN PROVO ATTEMPTED TO SHUT THE DOOR<[01] REINSTALLED AFT - [SDR SWAA2024052287697](https://openairdocs.org/sdr/SWAA2024052287697), May 19, 2024: SLIDE. DISLODGED. AFT ENTRY EMERGENCY EXIT SLIDE FELL OUT OF HOLDER WHEN PROVO ATTEMPTED TO SHUT THE DOOR REF TTG8Q00TF5B3 FOR NON-ROUTINE REFERENCING MT 725-61-06-AE (REP - EMER - [SDR SWAA2024022655965](https://openairdocs.org/sdr/SWAA2024022655965), Feb 24, 2024: ACTUATOR. OUT OF ADJUST. SEAT 11D RECLINES INTO EXIT ROW<[01] ADJUSTED SEAT 11D RECLINE ACTUATOR PER AMM 25-22-00 OPS CHECKS GOOD - [SDR SWAA2024010837836](https://openairdocs.org/sdr/SWAA2024010837836), Jan 4, 2024: COVER. MISSING. F/A REPORTS R/H O/W EXIT EMERGENCY EXIT LIGHT COVER MISSING<[01] REPLACED MISSING LENS PER AMM 33-51-03 - [SDR SWAA2023120825686](https://openairdocs.org/sdr/SWAA2023120825686), Nov 29, 2023: LIGHT. INOPERATIVE. EMERGENCY EXIT AISLE LIGHT AT SEAT ROW 16FED IS INOP.<[01] RELLAMPED EMERGENCY EXIT AISLE LIGHT AT SEAT ROW 16FED AND PERFORMED GOOD TEST IAW AMM 33-51-03-960-8 - [SDR SWAA2023121125682](https://openairdocs.org/sdr/SWAA2023121125682), Nov 22, 2023: LIGHT. INOPERATIVE. WIRE W3142-0456-20 FOUND DEPINNED FROM GD3664 (MARKED) WIRE LOCATED AT STA767<[01] REPINNED WIRE W3142-0456-20 TO GD3664 PER SWPM 20-90-15. PERFORMED GOOD GROUN - [SDR SWAA2023121123814](https://openairdocs.org/sdr/SWAA2023121123814), Nov 22, 2023: BRACKET. CRACKED. BRACKET CRACKED AT BS 867 STR 3R<[01] REMOVED FLOOR PANEL 321UF PER AMM 53-21-00-000-801;[02] EDIT: ACTION ENTERED IN ERROR; WRONG TASK;[03] COMPLETED STEP 1. C - [SDR SWAA2023121121942](https://openairdocs.org/sdr/SWAA2023121121942), Nov 15, 2023: SKIN. CRACKED. CRACK ON FUSELAGE SKIN BS907+10' JUST ABOVE STR22L COMMON TO WASTE TANK EXHAUST PORT CUTOUT<[01] THIS IS A CATEGORY B REPAIR AS PER SRM 53-70-01-2R-3.;[02] TASK - [SDR SWAA2023121121949](https://openairdocs.org/sdr/SWAA2023121121949), Nov 15, 2023: SLAT. CRACKED. LEFT WING; LOWER SURFACE; L/E SLAT NOSE SKIN AT ACTUATOR RIB IS CRACKED AT FASTENER (MARKED) SLAT #3<[01] UPDATED PARTS;[02] TORQUED LEADING EDGE SLAT ACTUATOR - [SDR SWAA2023121121945](https://openairdocs.org/sdr/SWAA2023121121945), Nov 15, 2023: SUPPORT BEAM. CORRODED. LEFT WING TRAILING EDGE SUPPORT BEAM IS CORRODED AT FASTENERS; I/B #1 FLAP CARRIAGE; O/B #2 FLAP CARRIAGE<[01] VERIFIED MEASUREMENTS TABLE.;[02] REMOVED; REPLAC - [SDR SWAA2023121121944](https://openairdocs.org/sdr/SWAA2023121121944), Nov 15, 2023: SUPPORT BEAM. CORRODED. LEFT WING TRAILING EDGE SUPPORT BEAM IS CORRODED AT FASTENERS AFT OF #1 SLAT ACTUATOR; O/B #1 FLAP CARRIAGE<[01] REMOVED AND REPLACED TRAILING EDGE SUPPORT BEAM - [SDR SWAA2023121121948](https://openairdocs.org/sdr/SWAA2023121121948), Nov 15, 2023: SUPPORT BEAM. CORRODED. RIGHT WING TRAILING EDGE SUPPORT BEAM IS CORRODED AT FASTENER HOLES;I/B #7 FLAP CARRIAGE; O/B DEFLECTION RIB<[01] REMOVED AND REPLACED I/B #7 FLAP CARRIAGE; O/B - [SDR SWAA2023121121941](https://openairdocs.org/sdr/SWAA2023121121941), Nov 15, 2023: SUPPORT BEAM. CORRODED. RIGHT WING TRAILING EDGE SUPPORT BEAM IS CORRODED AT FASTENER HOLES; O/B #7 FLAP CARRIAGE; I/B #8 FLAP CARRIAGE<[01] UPON FURTHER INVESTIGATION; THERE'S NO ALLO - [SDR SWAA2023121121410](https://openairdocs.org/sdr/SWAA2023121121410), Nov 14, 2023: STRINGER. CRACKED. AREA AFT OF FWD CARGO COMPARTMENT HAS A CRACKED STR AT STR 27R; BS 520+19<[01] VERIFIED MEASUREMENT TABLE - [SDR SWAA2023121121411](https://openairdocs.org/sdr/SWAA2023121121411), Nov 14, 2023: STRINGER. CRACKED. AREA AFT OF FWD CARGO COMPARTMENT HAS A SUSPECTED CRACKED STR AT STR 25R; BS 520+19<[01] VERIFIED MEASUREMENT TABLE;[02] CRACKED STRINGER WAS FOUND TO BE OUT LI - [SDR SWAA2023121121407](https://openairdocs.org/sdr/SWAA2023121121407), Nov 14, 2023: STRINGER. CRACKED. AREA AFT OF FWD CARGO COMPARTMENT HAS A CRACKED STR AT STR 27L; BS 520+19<[01] VERIFIED MEASUREMENT FIELD - [SDR SWAA2023120821158](https://openairdocs.org/sdr/SWAA2023120821158), Nov 14, 2023: THRESHOLD. CRACKED. AFT CARGO BAY AFT CORNER THRESHOLD IS CRACKED<[01] CRACK FOUND TO BE OUT OF LIMITS AS PER SRM 53-60-15-1A-1.;[02] AFT CARGO BAY AFT CORNER SCUFF PLATE REPAIRED - [SDR SWAA2023121121029](https://openairdocs.org/sdr/SWAA2023121121029), Nov 13, 2023: SEAT TRACK. CORRODED. CABIN SEAT TRACK HAS CORROSION IN WELL OF CROWN AT BS 847+12; RBL 25; WL 208<[01] UPDATED STEPS 1 AND 2;[02] UPDATED MEASURMENTS TABLE
USED DIAL DEPTH GAGE T - [SDR SWAA2023120821137](https://openairdocs.org/sdr/SWAA2023120821137), Nov 13, 2023: LENS. OUT OF ADJUST. PASSENGER CABIN OVERHEAD R/H BIN #6 EMERGENCY LIGHT LENS IS DIS-BONDED. (MARKED)<[01] REMOVED AND REINSTALLED EMERGENCY LIGHT LENS ON PASSENGER OVERHEAD BIN R/H - [SDR SWAA2023101711038](https://openairdocs.org/sdr/SWAA2023101711038), Oct 15, 2023: SEAT. OUT OF ADJUST. EMERGENCY EXIT SEAT 11 D RECLINES<[01] ADJUSTED EMERGENCY EXIT SEAT 11D ; REF AMM 25-22-00; OPS CK GOOD.
ACCOMPLISHED BY 141645 ON LOGPAGE 2504709 - [SDR SWAA2023052451334](https://openairdocs.org/sdr/SWAA2023052451334), May 23, 2023: GIRT BAR. BENT. FWD ENTRY DOOR SLIDE BRACKET BENT WHERE GIRT BAR STORES<[01] REPOSITIONED GIRT BAR PER SIP OPS CHECK GOOD. AC OK FOR SERVICE. - [SDR SWAA2022120678863](https://openairdocs.org/sdr/SWAA2022120678863), Dec 5, 2022: BATTERY. INOPERATIVE. FWD MEGAPHONE INOP / [01] REPLACED BATTERIES; OPS CHECK NORMAL; WORK DONE PER 25-64-00 OF THE AMM - [SDR SWAA2022070123839](https://openairdocs.org/sdr/SWAA2022070123839), Jun 28, 2022: SLIDE. OUT OF POSITION. L1 SLIDE PACK IS PARTIALLY DROP OUT OF COMPARTMENT / [01] REINSTALLED L1 DOOR SLIDE IAW AMM 25-66-01. A/C OK FOR SERVICE - [SDR SWAA2022051808034](https://openairdocs.org/sdr/SWAA2022051808034), May 14, 2022: FLASHLIGHT ASSY. LOOSE. FWD EMER FLASHLIGHT BASE LOOSE / [01] RESECURED BOTH FWD EMERGENCY FLASHLIGHT BASES PER SIP. - [SDR SWAA2022012461726](https://openairdocs.org/sdr/SWAA2022012461726), Jan 14, 2022: LIGHT. INOPERATIVE. BULLNOSE EMERGENCY EXIT LIGHT AT 6FED IS INOP ; RELAMPED BULLNOSE EMERGENCY EXIT LIGHT AT 6FED AND LIGHT IS STILL INOP. ALL WORK PERFORMED AS PER AMM. 33-51-03- - [SDR SWAA2022012461725](https://openairdocs.org/sdr/SWAA2022012461725), Jan 14, 2022: LIGHT. INOPERATIVE. FWD SERVICE DOOR EMERGENCY EXIT LIGHT INOP ; / [01] RELAMPED FWD SERVICE DOOR EMERGENCY EXIT SLIDE LIGHT AND LIGHT IS STILL INOP. ALL WORK PERFORMED AS PER AMM. - [SDR SWAA2022012461512](https://openairdocs.org/sdr/SWAA2022012461512), Jan 14, 2022: SCUFF PLATE. CRACKED. F.E.D. AFT INNER SCUFF PLATE IS CRACKED ; / [01] UPDATED PART; [02] INSTALLED AND SEALED ROBBED SCUFF PLATE AT FED AFT INNER POSITION PER AMM 53-11-01-420-801; - [SDR SWAA2022012457091](https://openairdocs.org/sdr/SWAA2022012457091), Dec 30, 2021: BRACKET. CRACKED. WIRE SUPPORT BRACKET CRACKED AT B.S 897 STRINGER 3 R/H ; / [01] ENTRY TO CORRECT B.S DISCREPANCY IS AT B.S 867 STRINGER 3R/H; [02] REMOVED DAMAGED WIRE SUPPORT - [SDR SWAA2022012456256](https://openairdocs.org/sdr/SWAA2022012456256), Dec 26, 2021: FAIRING. DELAMINATED. SUPPLEMENTAL INFORMATION: FAIRING 195CL HAS DELAMINATIONS OVER CORE AREA NEXT TO EDGEBAND OF PANEL SEE FAULT TTG8Q009PY4M. ; / [01] IDENTIFIED PANEL MATERIAL IA - [SDR SWAA2022012454693](https://openairdocs.org/sdr/SWAA2022012454693), Dec 18, 2021: SUPPORT ANGLE. CORRODED. CORROSION; AFT CARGO SIDEWALL LWR SUPPORT CLIP; BS 906 RBL 24 ; / [01] REMOVED CORROSION ON AFT CARGO SIDEWALL LOWER SUPPORT CLIP; BS 906; RBL 24; WORK AREA; W - [SDR SWAA2022012454177](https://openairdocs.org/sdr/SWAA2022012454177), Dec 16, 2021: ATTACH BRACKET. CRACKED. PNEUMATIC DUCT TIE ROD SUPPORT ATTACH POINT BRACKET AT BS 540 LBL 58 IS CRACKED ; / [01] REMOVAL OF PNEUMATIC DUCT TIE ROD SUPPORT ATTACH BRACKET AT B.S. 540 LB - [SDR SWAA2022012453277](https://openairdocs.org/sdr/SWAA2022012453277), Dec 15, 2021: BAFFLE. CRACKED. FWD CARGO BAY BAFFLE CRACKED BS 400-420 RBL 25 WL 165 ; / [01] APPLICABILITY STATEMENT NO DAMAGE ALLOWED ON SRM FOUND; REPLACE PART FOR REPAIR IAW SRM 51-10-02; - [SDR SWAA2022012451345](https://openairdocs.org/sdr/SWAA2022012451345), Dec 8, 2021: BEAR STRAP. CRACKED. FOUND 1.5' CRACK AT FWD SERVICE DOOR SURROUND; BS 294 3.5' UNDER S-8R AROUND FASTENER COMMON TO THE BEAR STRAP. AREA MARKED ; / VERIFIED SRM 53-10-01-2R-6 IS AP - [SDR SWAA2022012451326](https://openairdocs.org/sdr/SWAA2022012451326), Dec 8, 2021: FAIRING. CRACKED. FAIRING 195CL IS CRACKED IN RADIUS AT AFT EDGE. ; / REMOVED DAMAGE FROM AFT RADIUS; AFT EDGEBAND; AND UPPER EDGEBAND; ALL ON INNER SURFACE; ALL DAMAGES CONNECT; - [SDR SWAA2022012451324](https://openairdocs.org/sdr/SWAA2022012451324), Dec 7, 2021: CHANNEL. CRACKED. SUPPLEMENTAL INFORMATION: CRACK ON PASSENGER CABIN FWD ENTRY DOOR MOP SILL AT LBL 56 BS 294+9 WL 208. ; / [01] REMOVED FWD ENTRY DOOR MOP SILL B.S 270-360 LBL56 - [SDR SWAA2022012451317](https://openairdocs.org/sdr/SWAA2022012451317), Dec 7, 2021: INTERCOSTAL. CRACKED. SUPPLEMENTAL INFORMATION: CRACK ON PASSENGER CABIN INTERCOSTAL AT LBL 46 BS 328+7 WL 208. ; / [01] REMOVED AND LOCATED HOLES IN NEW INTERCOSTAL; AN INSTALLED AT - [SDR SWAA2022012451316](https://openairdocs.org/sdr/SWAA2022012451316), Dec 7, 2021: INTERCOSTAL. CRACKED. CRACK ON PASSENGER CABIN INTERCOSTAL AT LBL 46 BS 312+8 WL 208. ; / [01] COMPLETED STEPS 1 AND 2
REQUEST OK TO INSTALL; [02] CORRECTED REPAIR LOCATION AND ME - [SDR SWAA2022012451066](https://openairdocs.org/sdr/SWAA2022012451066), Dec 7, 2021: SUPPORT. CORRODED. CORROSION ON FLOOR TO SIDEWALL SUPPORT AT AFT CARGO BAY BS767 - BS727D+13 RBL20. MARKED. ; / [01] REMOVED CORROSION FLOOR TO SIDEWALL SUPPORT AT AFT CARGO BAY B - [SDR SWAA2022012451064](https://openairdocs.org/sdr/SWAA2022012451064), Dec 7, 2021: STRINGER. CRACKED. CRACK ON FWD CARGO BAY BS 540 R/H STRINGER 23. ; / [01] EVALUATED CRACK MEASUREMENTS ON FCB BS 540; STR 23RH ; STRINGER DAMAGE FOUND TO BE OUT LIMITS IAW SRM 53 - [SDR SWAA2022012451312](https://openairdocs.org/sdr/SWAA2022012451312), Dec 7, 2021: SHEAR WEB. CORRODED. SUPPLEMENTAL INFORMATION: CORROSION ON PASSENGER CABIN SHEAR WEB AT BS 1016 LBL 13 WL 208.1. ; / [01] REMOVED CORROSION ON PASSENGER CABIN SHEAR WEB AT BS 1016 - [SDR SWAA2022012451067](https://openairdocs.org/sdr/SWAA2022012451067), Dec 7, 2021: CARGO TRACK. CRACKED. CRACKED TRACK AT AFT CARGO BAY BS767; BS727E RBL13 WL156. MARKED. ; / EVALUATED CRACKED TRACK AT AFT CARGO BAY BS767; BS727E RBL13 WL156. DIMENSIONS L: 0.370' A - [SDR SWAA2022012451065](https://openairdocs.org/sdr/SWAA2022012451065), Dec 7, 2021: STRINGER. CRACKED. CRACK ON FWD CARGO BAY BS 540 R/H STRINGER 26. ; / STRINGER DAMAGE FOUND TO BE OUT LIMITS IAW SRM 53-00-03-1A FIG 103.; [02] VERIFIED APPLICABILITY FOR REPAIR B - [SDR SWAA2022012451062](https://openairdocs.org/sdr/SWAA2022012451062), Dec 7, 2021: STRINGER. CRACKED. CRACK ON FWD CARGO BAY BS 540 R/H STRINGER 21. ; / STRINGER DAMAGE FOUND TO BE OUT LIMITS IAW SRM 53-00-03-1A FIG 103.; [02] VERIFIED APPLICABILITY FOR REPAIR B All 199: https://openairdocs.org/aircraft/N7865A/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 N7865A The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N7865A before. - [Cancelled 1976-02-03](https://openairdocs.org/deregistered/N7865A-1976-02-03): Cessna 180A, S/N 32762. Exported to Canada. Owner: [Commander Aviation Corp](https://openairdocs.org/faa-owner/COMMANDER%20AVIATION%20CORP), [Bismarck, ND](https://openairdocs.org/faa-place/ND/Bismarck) ## Related - Other Boeing 737-7Q8 aircraft: https://openairdocs.org/model/boeing-737-7q8/aircraft.md - The CFM International CFM56 series engine: https://openairdocs.org/engine/cfm-international-cfm56-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.