# N7866A: 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 CFM56-7B24 series](https://openairdocs.org/engine/cfm-international-cfm56-7b24-series) (registry code 13044) - Serial number: 30648 - Year built: 2002 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: January 16, 2018 - Certificate issued: March 26, 2026 - Expires: March 31, 2033 - Mode S code: AAA9FB - 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=7866A - Page: https://openairdocs.org/aircraft/N7866A From the FAA registry file of October 29, 2026. ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination. The registry lists only the engine series, so ADs for every CFM International CFM56-7B24 model are included. ## ADs that may apply (OpenAirDocs): 19 in force ### Matched by airframe (Boeing 737-7Q8) None in force. ### Matched by engine (CFM International CFM56-7B24 series) - [AD 2023-05-05](https://openairdocs.org/ad/2023-05-05): Turbine Engine Compressor Section · CFM International CFM56-5B1, CFM56-5B1/2P, CFM56-5B1/3 and 98 more. Effective May 10, 2023 - [AD 2022-02-03](https://openairdocs.org/ad/2022-02-03): Turbine Engine Accessory Drive · CFM International CFM56-3, CFM56-3B, CFM56-3C and 34 more. Effective Mar 22, 2022 - [AD 2021-16-08](https://openairdocs.org/ad/2021-16-08): Turbine Section · CFM International CFM56-5B1, CFM56-5B1/2P, CFM56-5B1/P and 55 more. Effective Sep 28, 2021 - [AD 2018-26-01](https://openairdocs.org/ad/2018-26-01): Turbine Engine Compressor Section · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B20/3 and 46 more. Effective Jan 10, 2019 - [AD 2018-09-51](https://openairdocs.org/ad/2018-09-51): Engine · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B20/3 and 46 more. Effective Jun 7, 2018 - [AD 2015-18-04](https://openairdocs.org/ad/2015-18-04): 73-tooth gearshaft located in the engine accessory gearbox (AGB) · CFM International CFM56-3, CFM56-7B20, CFM56-7B20/2 and 47 more. Effective Oct 20, 2015 - [AD 2015-04-02](https://openairdocs.org/ad/2015-04-02): Dual engine thrust instability event · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B20/3 and 46 more. Effective Mar 31, 2015 - [AD 2010-13-09](https://openairdocs.org/ad/2010-13-09): Stage 3 low-pressure turbine (LPT) · CFM International CFM56-5, CFM56-5-A1/F, CFM56-5A4 and 88 more. Effective Jul 26, 2010 - [AD 2010-01-05](https://openairdocs.org/ad/2010-01-05): LP turbine rear frames · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B20/3 and 25 more. Effective Feb 18, 2010 - [AD 2009-11-02](https://openairdocs.org/ad/2009-11-02): HPC 4-9 spools · CFM International CFM56-2, CFM56-2A, CFM56-2B and 109 more. Effective Jun 23, 2009 - [AD 2008-03-09](https://openairdocs.org/ad/2008-03-09): Low pressure turbine rear frames (TRFs) · CFM International CFM56-7B18, CFM56-7B20, CFM56-7B22 and 10 more. Effective Mar 10, 2008 - [AD 2006-26-01](https://openairdocs.org/ad/2006-26-01): Fuel filters · CFM International CFM56-2, CFM56-2A, CFM56-2B and 93 more. Effective Jan 3, 2007 - [AD 2002-16-18](https://openairdocs.org/ad/2002-16-18): Low pressure turbine (LPT) nozzle segments · CFM International CFM56-5B1, CFM56-5B1/2P, CFM56-5B1/P and 33 more. Effective Sep 18, 2002 - [AD 2002-13-03](https://openairdocs.org/ad/2002-13-03): Turbofan Engines · CFM International CFM56-2, CFM56-2A, CFM56-2B and 55 more. Effective Aug 1, 2002 - [AD 2001-11-05](https://openairdocs.org/ad/2001-11-05): No. 4 Bearings · CFM International CFM56-2, CFM56-2B, CFM56-3 and 45 more. Effective Jun 11, 2001 - [AD 2001-02-12](https://openairdocs.org/ad/2001-02-12): On-Wing Torque Inspection · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B22 and 11 more. Effective Feb 14, 2001 - [AD 98-21-23](https://openairdocs.org/ad/98-21-23): Electronic Engine Control · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B22 and 10 more. Effective Nov 2, 1998 - [AD 98-19-20](https://openairdocs.org/ad/98-19-20): Hydromechanical Unit · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B22 and 7 more. Effective Oct 7, 1998 - [AD 98-14-51](https://openairdocs.org/ad/98-14-51): Accessory Gearbox · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B22 and 10 more. Effective Oct 1, 1998 ### Historical (superseded or no longer in force) - [AD 2021-10-09](https://openairdocs.org/ad/2021-10-09) (historical): Turbine Engine Compressor Section · CFM International CFM56-5B1, CFM56-5B1/2P, CFM56-5B1/3 and 82 more. Effective Jun 24, 2021 - [AD 2019-12-05](https://openairdocs.org/ad/2019-12-05) (historical): Turbine Section · CFM International CFM56-5B1, CFM56-5B1/2P, CFM56-5B1/P and 39 more. Effective Jul 5, 2019 - [AD 2018-18-01](https://openairdocs.org/ad/2018-18-01) (historical): Turbine Engine Compressor Section · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B20/3 and 46 more. Effective Oct 16, 2018 - [AD 2018-10-11](https://openairdocs.org/ad/2018-10-11) (historical): Turbine Engine Compressor Section · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B20/3 and 46 more. Effective Jun 1, 2018 - [AD 2018-09-10](https://openairdocs.org/ad/2018-09-10) (historical): Turbine Engine Compressor Section · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B20/3 and 46 more. Effective May 14, 2018 - [AD 2013-26-01](https://openairdocs.org/ad/2013-26-01) (historical): Oil dynamic seal assembly · CFM International CFM56-3, CFM56-3B, CFM56-3C and 52 more. Effective Feb 3, 2014 - [AD 2000-12-01](https://openairdocs.org/ad/2000-12-01) (historical): Critical Life-Limited Parts · CFM International CFM56-2, CFM56-2A, CFM56-2B and 54 more. Effective Dec 11, 2000 ## Information bulletins (advisory) (1 in force) - [SAIB NE-08-17R3](https://openairdocs.org/saib/NE-08-17R3): Turbine Section - Propulsion Technology LLC Unapproved Repair. Issued May 28, 2014 - [SAIB NE-08-17R2](https://openairdocs.org/saib/NE-08-17R2) (historical): Turbine Section - Propulsion Technology LLC Unapproved Repair. Issued Mar 7, 2011 - [SAIB NE-08-17R1](https://openairdocs.org/saib/NE-08-17R1) (historical): Propulsion Technology LLC Unapproved Repair. Issued May 22, 2008 - [SAIB NE-08-17](https://openairdocs.org/saib/NE-08-17) (historical): Propulsion Technologies International Unapproved Repair. Issued May 14, 2008 ## NTSB investigations None matched to N7866A. ## FAA accident and incident reports None matched to N7866A. ## Service difficulty reports (191, 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 SWAA2025110731480](https://openairdocs.org/sdr/SWAA2025110731480), Nov 4, 2025: SLAT. CRACKED. RIGHT WING, NR 7 SLAT HAS A CRACK AT ACTUATOR ATTACH POINT. VERIFIED WITH HFEC PART 6 51-00-00, PROCEDURE 23. C/W SLAT INSPECTION NO FOD FOUND. R & R NR 6 L/E S - [SDR SWAA2025082105688](https://openairdocs.org/sdr/SWAA2025082105688), Aug 18, 2025: SLIDE. PARTIAL DEPLOY. FORWARD SERVICE ENTRY ESCAPE SLIDE PARTIALLY DEPLOYED. REPOSITIONED FWD SERVICE ENTRY ESCAPE SLIDE PER AMM 25-66-01 AND MT 725-61-06. - [SDR SWAA2025030401958](https://openairdocs.org/sdr/SWAA2025030401958), Mar 4, 2025: HANDLE. BROKEN. L1 DOOR PLASTIC ASSIST HANDLE BROKEN. <[01] SWAPPED FWD LAV DOOR HANDLE WITH L1 DOOR ASSIST HANDLE PER AMM 52-11-31. PLACED FWD LAV ASSIST HANDLE ON MEL. OK TO - [SDR SWAA2025020491976](https://openairdocs.org/sdr/SWAA2025020491976), Feb 1, 2025: SKIN. CRACKED. AFT FUSELAGE SKIN HAS 1/2' LONG CRACK ON AFT SIDE OF VACUUM WASTE EXHAUST PORT. FUSELAGE STATION 918 AND 3.5 INCHES ABOVE STRINGER 22L. COMPLIED WITH TASK CARD. - [SDR SWAA2025020491670](https://openairdocs.org/sdr/SWAA2025020491670), Jan 31, 2025: ANGLE. CRACKED. RIGHT ENGINE; LPT COOLING TUBE SUPPORT ANGLE BRACKET CRACKED 4OCLOCK POSITION <[01]. REMOVED AND REPLACED CRACKED LPT COOLING TUBE SUPPORT ANGLE BRACKET AT 4 O? - [SDR SWAA2025013191669](https://openairdocs.org/sdr/SWAA2025013191669), Jan 31, 2025: BATTERY PACK. FAILED. PASSENGER CABIN; EMERGENCY LIGHTS BATTERY PACK M1670 FAILED CAPACITY TEST.<[01] R&R PASSENGER CABIN EMERGENCY LIGHTS BATTERY PACK M1670 IAW AMM 33-51-06. - [SDR SWAA2025013191668](https://openairdocs.org/sdr/SWAA2025013191668), Jan 31, 2025: BATTERY PACK. FAILED. PASSENGER CABIN; EMERGENCY LIGHTS BATTERY PACK M1675 FAILED CAPACITY TEST.<[01] R&R PASSENGER CABIN EMERGENCY LIGHTS BATTERY PACK M1675 IAW AMM 33-51-06. - [SDR SWAA2025013191658](https://openairdocs.org/sdr/SWAA2025013191658), Jan 31, 2025: HANDLE. LOOSE. AFT GALLEY SERVICE DOOR R2 DOOR HANDLE CAM LOOSE.<[01] RE-SECURED AFT GALLEY SERVICE DOOR R2 DOOR HANDLE CAM REF AMM 20-50-11. - [SDR SWAA2024010432086](https://openairdocs.org/sdr/SWAA2024010432086), Dec 15, 2023: FLOOR PANEL. DEBONDED. FLOOR PANEL 242AF UPPER SKIN HAS AN AREA OF DISBOND NEAR CENTER OF PANEL. (MARKED)<[01] FLOOR PANEL 242AF WITH DISBOND IN UPPER SKIN WAS REPLACED BY FABRICATING - [SDR SWAA2024010431565](https://openairdocs.org/sdr/SWAA2024010431565), Dec 14, 2023: WEB. CORRODED. CORROSION ON FWD CARGO BAY THRESHOLD WEB AT BS 447 TO BS 467; STR 25R TO 26R<[01] REMOVED AND INSTALLED NEW FCB SUB-THRESHOLD WEB IAW SRM 51-40-02-0G-0 AND DWG - [SDR SWAA2024010431567](https://openairdocs.org/sdr/SWAA2024010431567), Dec 14, 2023: SIDEWALL SUPPORT. CORRODED. CORROSION ON FWD CARGO BAY RH FLOOR-TO-SIDEWALL SUPPORT AT BS 498; STR 25R TO STR 26R THE DESCRIPTION OF ITEM SUPPOSED TO BE IS SHIELD AND NOT THE FLOOR TO SIDE - [SDR SWAA2024010431568](https://openairdocs.org/sdr/SWAA2024010431568), Dec 14, 2023: WEB. CORRODED. CORROSION ON AFT CARGO BAY THRESHOLD WEB AT BS 792 TO BS 847; STR 24R TO STR 26R<[01] REPLACED THRESHOLD WEB AT BS 792 TO BS 847 IAW SRM 51-40-02; DWG 146A8340. - [SDR SWAA2024010431566](https://openairdocs.org/sdr/SWAA2024010431566), Dec 14, 2023: SIDEWALL SUPPORT. CORRODED. CORROSION ON AFT CARGO BAY RH FLOOR-TO-SIDEWALL SUPPORT AT BS 865; STR 25R THE DESCRIPTION OF ITEM IS SUPPOSE TO BE SHIELD AND NOT FLOOR TO SIDEWALL<[01] BARCOD - [SDR SWAA2024010430628](https://openairdocs.org/sdr/SWAA2024010430628), Dec 12, 2023: SCUFF PLATE. CRACKED. FWD CARGO BAY FWD CORNER SCUFF PLATE CRACKED<[01] REPAIR FWD CARGO BAY FWD CORNER SCUFF PLATE IAW SRM 53-30-15-2R-1;[02] VERIFIED CORRECTIVE ACTION COMPLETE.
REMOVED SUPPORT ANGLE IAW - [SDR SWAA2024010331128](https://openairdocs.org/sdr/SWAA2024010331128), Dec 12, 2023: SEAT TRACK. CORRODED. SEAT TRACK LH HAS CORROSION ON CROWN AT LBL 45.5; STA 500B WL 208<[01] SEAT TRACK WILL BE REPLACED ON CARD#TTG8Q00Q8J4J.;[02] VERIFIED CORRECTIVE ACTION 1 AND M - [SDR SWAA2024010331117](https://openairdocs.org/sdr/SWAA2024010331117), Dec 12, 2023: SEAT TRACK. CORRODED. SEAT TRACK LH HAS CORROSION ON CROWN AT LBL 45.5; STA 380B+3' WL 208<[01] COMPLETED STEP 1.;[02] UPON FURTHER INVESTIGATION; CORROSSION IS AT BS 380+3'; LBL 45. - [SDR SWAA2024010331118](https://openairdocs.org/sdr/SWAA2024010331118), Dec 12, 2023: SEAT TRACK. CORRODED. SEAT TRACK LH HAS CORROSION ON CROWN AT LBL 45.5; STA 520 WL 208<[01] VERIFIED APPLICABILITY FOR SRM 53-00-52-1A-1 ALLOWABLE DAMAGE 1.;[02] VERIFIED APPLICABILI - [SDR SWAA2024010430451](https://openairdocs.org/sdr/SWAA2024010430451), Dec 11, 2023: ANGLE. CRACKED. CRACKED L-CLIP ON L/W T/E PANEL 551FB AT FWD UPPER EDGE 27' FROM O/B END<[01] TASK COMPLETE:
CRACKED L-CLIP WAS REMOVED IAW SRM 51-40-02-0G-0. NEW L-CLIP WAS - [SDR SWAA2023092704939](https://openairdocs.org/sdr/SWAA2023092704939), Sep 27, 2023: LIGHT. INOPERATIVE. FWD CABIN ROW 1 ABC EMERGENCY LIGHT OUT<[01] RELAMPED 1ABC EMERGENCY LIGHT PER AMM 33-51-03 - [SDR SWAA2023091400300](https://openairdocs.org/sdr/SWAA2023091400300), Sep 14, 2023: BATTERY PACK. FAILED. R/H FWD EMERGENCY LIGHTING BATTERY PACK FAILED CAPACITY CHECK.<[01] REMOVED AND REPLACED R/H FWD EMERGENCY LIGHTING BATTERY PACK PER AMM 33-51-06. - [SDR SWAA2023042831246](https://openairdocs.org/sdr/SWAA2023042831246), Apr 25, 2023: SLIDE. LOOSE. R1 DOOR EVACUATION SLIDE COVER LOOSE<[01] REPACKED R2 SLIDE OER 725-61-06 - [SDR SWAA2022112875399](https://openairdocs.org/sdr/SWAA2022112875399), Nov 25, 2022: BATTERY. INOPERATIVE. AFT RH OVERHEAD EMERGENCY LIGHTS INOP / [01] REMOVED AND REPLACED AFT RH OVERHEAD EMERGENCY LIGHT BATTERY PACK IAW AMM 33-51-06. OPS CHECK GOOD - [SDR SWAA2022101760445](https://openairdocs.org/sdr/SWAA2022101760445), Oct 16, 2022: BATTERY PACK. INOPERATIVE. EMERGENCY LIGHTS FOUND LAST 2 CABIN EMERGENY LIGHT AFT CEILING AND BOTH AFT OVER DOOR EMERGENCY LIGHTS TO BE INOP / [01] R&R AFT LH EMERGENCY LIGHT BATTERY PACK - [SDR SWAA2022072835358](https://openairdocs.org/sdr/SWAA2022072835358), Jul 27, 2022: LIGHT. INOPERATIVE. EMERGENCY LIGHT@ 9ABC INOP / [01] RELAMPED EMERGENCY LIGHT @ 9ABC IAW AMM 33-51-03. OPS CK GOOD - [SDR SWAA2022042596278](https://openairdocs.org/sdr/SWAA2022042596278), Apr 20, 2022: COVER. OUT OF POSITION. FWD SERVICE DOOR EMERG. SLIDE PARTIAL FELL OUT / [01] REPOSITIONED R1 SLIDE IN SLIDE COVER PER AMM25-66-01 - [SDR SWAA2022022376321](https://openairdocs.org/sdr/SWAA2022022376321), Feb 22, 2022: LENS. MISSING. FWD ENTRY DOOR LOWER EMERGENCY LIGHT LENS MISSING DIRECTIONAL ARROW / [01] REMOVE AND REPLACED FWD ENTRY LOWER E LIGHT LENS IAW AMM-33-51-01;[02] INSPECTED - [SDR SWAA2022022376322](https://openairdocs.org/sdr/SWAA2022022376322), Feb 22, 2022: LENS. MISSING. FWD SERVICE DOOR LOWER EMERGENCY LIGHT LENS MISSING DIRECTIONAL ARROW FWD SERVICE DOOR LOWER EMERGENCY LIGHT LENS MISSING DIRECTIONAL ARROW / [01] REMOVED AND R - [SDR SWAA2022022376324](https://openairdocs.org/sdr/SWAA2022022376324), Feb 22, 2022: LENS. LOOSE. RIGHT EMERGENCY EXIT DOOR INTERIOR LOWER EMERGENCY LIGHT LENS IS LOOSE / [01] RE SECURED RH EMERGENCY EXIT DOOR LOWER LIGHT LENS REF M/M 33-51-01;[02] INSPECTED - [SDR SWAA2022022376326](https://openairdocs.org/sdr/SWAA2022022376326), Feb 22, 2022: LIGHT. MISSING. R2 AND L2 LOWER EMERGENCY EXIT SIGN MISSING DIRECTIONAL ARROWS. / [01] REMOVED AND REPLACED R2 AND L2 EMERGANCY EXIT SIGN COVERS REF AMM 33-51-01;[02] INSPECTED - [SDR SWAA2022021463393](https://openairdocs.org/sdr/SWAA2022021463393), Jan 5, 2022: SKIN. CRACKED. CRACK INTERNAL SKIN INBOARD FAN COWL LOC. 8 OCLOCK APROX. ON ENGINE 2 ; 2021-576398 / [01] TOOL USED: ET EQUIPMENT P/N: NORTEC 600D; S/N: 200048001; CAL DUE DAT - [SDR SWAA2022021158655](https://openairdocs.org/sdr/SWAA2022021158655), Jan 5, 2022: BRACKET. CRACKED. CRACK BRACKET LOCATED VERTICAL BEAM BETWEEN BL0.0 TO LBL10.0 AND BS727 AT AFT CARGO COMPARTMENT ; 2021-576389 / [01] REPLACED BRACKET LOCATED VERTICAL BEAM BETW - [SDR SWAA2022021158654](https://openairdocs.org/sdr/SWAA2022021158654), Jan 5, 2022: BATTERY PACK. INOPERATIVE. INOP EMERGENCY DOOR BATTERY PACK LOCATED BTW BS597-BS616 RH SIDE AT PASSENGER CABIN (1 EA) ; 2021-576383 / [01] REPLACED EMERGENCY DOOR BATTERY PACK LOCATED BTW - [SDR SWAA2022010658653](https://openairdocs.org/sdr/SWAA2022010658653), Jan 5, 2022: FITTING. CORRODED. CORROSION FITTING ON DRAG BRACE OUTBOARD FWD LOCATED AFT REAR SPAR RT SIDE AT VERTICAL STABILIZER. REPLACED THE FITTING AND FASTENERS ON DRAG BRACE IAW SRM 51-4 - [SDR SWAA2022021457987](https://openairdocs.org/sdr/SWAA2022021457987), Jan 3, 2022: SPAR WEB. CORRODED. CUSTOMER REQUEST - CORROSION FRONT SPAR WEB LOCATED OFSS 261 AT LT WING ; 2021-576311 / [01] TOOL USED. ULTRASONIC THICKNESS GAGE. P/N: 45MG. S/N: 130066701. DU - [SDR SWAA2022021157989](https://openairdocs.org/sdr/SWAA2022021157989), Jan 3, 2022: ACCESS PANEL. ELONGATED. ELONGATED HOLE ACCESS PANEL 194BR AT LOWER FUSELAGE ; 2021-576315 / [01] HOT BONDER P/N:HCS9000B; S/N: 18175469; DUE DATE: 05-AUG-22.; [02] TOOL USED MULTIMETER - [SDR SWAA2022021157995](https://openairdocs.org/sdr/SWAA2022021157995), Jan 3, 2022: INTERCOSTAL. CRACKED. CRACK WEB - INTERCOSTAL LOCATED BETWEEN BS927 TO BS947.5 AND STR25R AT AFT CARGO COMPARTMENT ; 2021-576321 / [01] REPLACED WEB - INTERCOSTAL LOCATED BETWEEN BS9 - [SDR SWAA2022021157994](https://openairdocs.org/sdr/SWAA2022021157994), Jan 3, 2022: ANGLE. CRACKED. CRACK ANGLE LOCATED BETWEEN STR25R TO STR27R AND BS907 PLUS 7 INCH AT AFT CARGO COMPARTMENT ; 2021-576319 / [01] REPLACED FASTENERS AND ANGLE LOCATED BETWEEN ST - [SDR SWAA2022021157993](https://openairdocs.org/sdr/SWAA2022021157993), Jan 3, 2022: ANGLE. CRACKED. CRACK ANGLE LOCATED BETWEEN STR25R TO STR27R AND BS907 PLUS 11 INCH AT AFT CARGO COMPARTMENT ; 2021-576320 / [01] INSTALLED NEW ANGLE LOCATED BETWEEN STR25R TO - [SDR SWAA2022021157990](https://openairdocs.org/sdr/SWAA2022021157990), Jan 3, 2022: TRACK. CRACKED. CRACK CARGO TRACK LOCATED BS727E; RBL13.84 AND WL156 AT AFT CARGO COMPARTMENT ; 2021-576318 / [01] EDDY CURRENT EQUIPMENT P/N: NORTEC500D; S/N: N500X12101U10202 - [SDR SWAA2022021157556](https://openairdocs.org/sdr/SWAA2022021157556), Jan 3, 2022: BRACKET. DETERIORATED. DETERIORATED ENTRY DOOR GIRT BAR FLOOR BRACKETS HARDWARE AND PLATES AT AFT GALLEY AREA ; 2021-576294 / [01] REPLACED ENTRY DOOR GIRT BAR FLOOR BRACKETS HARDWARE - [SDR SWAA2022021171374](https://openairdocs.org/sdr/SWAA2022021171374), Jan 3, 2022: PLATE. DETERIORATED. DETERIORATED ENTRY DOOR GIRT BAR FLOOR BRACKETS HARDWARE AND PLATES AT AFT GALLEY AREA ; 2021-576294 / [01] REPLACED ENTRY DOOR GIRT BAR FLOOR BRACKETS HARDWARE - [SDR SWAA2022021157557](https://openairdocs.org/sdr/SWAA2022021157557), Jan 3, 2022: BRACKET. DETERIORATED. DETERIORATED AFT SERVICE DOOR GIRT BAR FLOOR BRACKETS HARDWARE AND PLATES AT AFT GALLEY AREA ; 2021-576295 / [01] REPLACED AFT SERVICE DOOR GIRT BAR FLOOR BRACK - [SDR SWAA2022021171375](https://openairdocs.org/sdr/SWAA2022021171375), Jan 3, 2022: PLATE. DETERIORATED. DETERIORATED AFT SERVICE DOOR GIRT BAR FLOOR BRACKETS HARDWARE AND PLATES AT AFT GALLEY AREA ; 2021-576295 / [01] REPLACED AFT SERVICE DOOR GIRT BAR FLOOR BRACK - [SDR SWAA2022021157541](https://openairdocs.org/sdr/SWAA2022021157541), Jan 2, 2022: STRUCTURE. CRACKED. CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BS277 TO BS294.5 BL0 FWD GALLEY AND LAV ; 2021-576259 / [01] REPLACED WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED - [SDR SWAA2022021157542](https://openairdocs.org/sdr/SWAA2022021157542), Jan 2, 2022: STRUCTURE. CRACKED. CRACK ANGLE - SUPPORT LOCATED BS380 TO BS400 BL0 AT FWD GALLEY AREA ; 2021-576260 / [01] REPLACED ANGLE - SUPPORT LOCATED BS380 TO BS400 BL0 AT FWD GALLEY AREA - [SDR SWAA2022021457098](https://openairdocs.org/sdr/SWAA2022021457098), Dec 29, 2021: NONE. CRACKED. CRACK CLIP LOCATED ON AFT FACE BS 500C AT LEVEL STR 26R AT FWD CARGO COMPARTMENT ; 2021-576210 / [01] REPLACED CLIP LOCATED ON AFT FACE BS 500C AT LEVEL STR 26R - [SDR SWAA2022021457094](https://openairdocs.org/sdr/SWAA2022021457094), Dec 29, 2021: NONE. CRACKED. CRACK CLIP LOCATED ON FWD FACE BS 500B AT LEVEL STR 26R AT FWD CARGO COMPARTMENT ; 2021-576209 / [01] REPLACED CLIP LOCATED ON FWD FACE BS 500B AT LEVEL STR 26R All 191: https://openairdocs.org/aircraft/N7866A/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 ## Related - Other Boeing 737-7Q8 aircraft: https://openairdocs.org/model/boeing-737-7q8/aircraft.md - The CFM International CFM56-7B24 series engine: https://openairdocs.org/engine/cfm-international-cfm56-7b24-series.md --- 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.