# N7863A: 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: 30644
- Year built: 2002
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: December 2, 2017
- Certificate issued: January 4, 2026
- Expires: January 31, 2033
- Mode S code: AAA992
- Registered owner: [Unical Aviation Inc](https://openairdocs.org/faa-owner/UNICAL%20AVIATION%20INC)
- Location: [Litchfield Park, AZ](https://openairdocs.org/faa-place/AZ/Litchfield%20Park)
- 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=7863A
- Page: https://openairdocs.org/aircraft/N7863A

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 N7863A.

## FAA accident and incident reports

None matched to N7863A.

## Service difficulty reports (217, 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 SWAA2025062384172](https://openairdocs.org/sdr/SWAA2025062384172), Jun 20, 2025: SLIDE. LOOSE. FWD SERVICE DOOR ESCAPE SLIDE UNSECURED <[01]. REPLACED FWD SERVICE DOOR SLIDE IAW MT 725-61-06.
- [SDR SWAA2024122380232](https://openairdocs.org/sdr/SWAA2024122380232), Dec 21, 2024: MEGAPHONE. INOPERATIVE. FWD MEGAPHONE INOP. R&R MEGAPHONE IAW 25-64-00
- [SDR SWAA2024100744086](https://openairdocs.org/sdr/SWAA2024100744086), Oct 1, 2024: SKIN. DELAMINATED. RH WING OUTBOARD AFT FLAP INBD LOWER SKIN DELAMINATING<[01] REMOVED R/H O/B AFT FLAP PER AMM 27-51-22;[02] OK TO. INSTALL R/H O/B AFT FLAP;[03] 01 - REMOVED AND
- [SDR SWAA2024072516369](https://openairdocs.org/sdr/SWAA2024072516369), Jul 25, 2024: SEAT. OUT OF ADJUST. SEAT 11D RECLINES AND SHOULD NOT DUE TO BEING AN EMERGENCY ROW EXIT.<[01] ADJUSTED SEAT RECLINE AT 11D PER AMM 25-22-00
- [SDR SWAA2024072516366](https://openairdocs.org/sdr/SWAA2024072516366), Jul 25, 2024: SEAT. LOOSE. SEAT ROW 1DEF; 3DEF; 8DEF; 11DEF AND 13DEF IS LOOSE IN ITS TRACKS.<[01] SECURED SEATS PER AMM 25-22-00
- [SDR SWAA2024051485164](https://openairdocs.org/sdr/SWAA2024051485164), May 12, 2024: SLIDE. OUT OF ADJUST. AFT RIGHT SLIDE NEEDS REPACKING<[01] REPACKED AFT SERVICE DOOR SLIDE IAW AMM 25-66-01
- [SDR SWAA2024031262171](https://openairdocs.org/sdr/SWAA2024031262171), Mar 11, 2024: BATTERY. INOPERATIVE. AFT GALLEY MEGAPHONE INOP.<[01] REPLACED AFT GALLEY MEGAPHONE BATTERIES PER AMM 25-64-00. A/C OK FOR SERVICE
- [SDR SWAA2024030157367](https://openairdocs.org/sdr/SWAA2024030157367), Feb 29, 2024: SEAL. CRACKED. TAIL - LEFT HORIZONTAL FWD UPPER SLIDING SEAL CRACKED.<[01] REMOVED AND REPLACED LEFT UPPER FWD HORIZONTAL SLIDING SEAL IAW BOEING 737 AMM 53-31-31
- [SDR SWAA2024030157368](https://openairdocs.org/sdr/SWAA2024030157368), Feb 29, 2024: SEAL. CRACKED. TAIL - RIGHT HORIZONTAL FWD UPPER SLIDING SEAL CRACKED.<[01] REMOVED AND REPLACED RIGHT FWD UPPER HORIZONTAL SLIDING SEAL IAW BOEING 737 AMM 53-31-31
- [SDR SWAA2024012945495](https://openairdocs.org/sdr/SWAA2024012945495), Jan 27, 2024: SLIDE. PARTIAL DEPLOY. FWD SVC DOOR SLIDE PARTIALLY DEPLOYED<[01] REMOVED AND REPLACED FWD SERVICE SLIDE REF MM 25-66-01.;[02] REMOVED AND REPLACED FWD SERVICE SLIDE REF MT 725-61-06.
- [SDR SWAA2024011741498](https://openairdocs.org/sdr/SWAA2024011741498), Jan 15, 2024: OVERHEAT SENSOR. FAULTED. DURING DESCENT RIGHT WING TO BODY OVERHEAT ILLUMINATED RAN QRH PROCEDURE. LIGHT EXTINGUISHED<[01] R/R M1763 & M1764 FWD AND AFT WING TO BODY STRUT ELEMENTS PER 
- [SDR SWAA2023110919499](https://openairdocs.org/sdr/SWAA2023110919499), Nov 8, 2023: FLASHLIGHT. FAILED. FWD FLASHLIGHTS RED LIGHTS DO NOT BLINK. / [01] REPLACED BOTH FWD FLASHLIGHT BATTERIES PER AMM 25-64-00-900-806. OPS CHECK IS GOOD.;[02] VERIFIED CORRECTIVE ACT
- [SDR SWAA2023110919059](https://openairdocs.org/sdr/SWAA2023110919059), Nov 7, 2023: SIGN. INOPERATIVE. EMERGENCY EXIT SIGN ABOVE AFT SERVICE ENTRY DOOR HAS BURNED OUT BULBS / [01] REPLACED BURNED OUT BULBS FOR EMERGENCY EXIT SIGN ABOVE AFT SERVICE ENTRY AND PERFO
- [SDR SWAA2023111313820](https://openairdocs.org/sdr/SWAA2023111313820), Oct 23, 2023: SEAT TRACK. CRACKED. PASSENGER CABIN SEAT TRACK FWD FASTENER CRACKED AT BS727B RBL45 WL208.<[01] REMOVED AND REPLACED PASSENGER CABIN SEAT TRACK FWD FASTENER AT BS727B RBL45 WL208.I
- [SDR SWAA2023111013973](https://openairdocs.org/sdr/SWAA2023111013973), Oct 23, 2023: FRAME. CRACKED. BS 312 FRAME IS CRACKED APPROXIMATELY STR. 6L ABOVE FWD ENTRY DOOR UPPER SILL WEB.<[01] COMPLETED BS 312 FRAME UPPER CHORD REPAIR IAW WITH EA M-22-153-01244 REV
- [SDR SWAA2023111312768](https://openairdocs.org/sdr/SWAA2023111312768), Oct 20, 2023: SLAT. CRACKED. DURING HFEC COUNTERSINK INSPECTION (TTG8Q00P1JJU) FOUND 4EA HOLES WITH CRACKS IN COUNTERSINK ONLY ON RW #7 SLAT AT SLAT ACTUATOR<[01] VERIFIED CORRECTIVE ACTION
- [SDR SWAA2023111312369](https://openairdocs.org/sdr/SWAA2023111312369), Oct 19, 2023: SLAT. CRACKED. LW #3 LEADING EDGE SLAT SKIN (ACTUATOR RIB ATTACH POINT) - FOUND 2EA FASTENER HOLES TO BE CRACKED IN SKIN. MARKED LOCATIONS.<[01] #3 L/E SLAT REMOVED; REPLACED;
- [SDR SWAA2023111012382](https://openairdocs.org/sdr/SWAA2023111012382), Oct 19, 2023: ATTACH ANGLE. CRACKED. L/H BS663 UPPER ATTACH ANGLE IS CRACKED ON VAPOR BARRIER LBL8 WL167.68<[01] CORRECTION TO TASK DETAIL SHOULD STATE ' R/H BS663 UPPER ATTACH ANGLE IS CRACKED ON 
- [SDR SWAA2023111311731](https://openairdocs.org/sdr/SWAA2023111311731), Oct 18, 2023: PANEL. DEBONDED. PANEL 193CL UPPER AFT CORNER IS DISBONDED. (MARKED)<[01] PANEL 193CL WILL BE REPLACED ON FAULT#TTG8Q00P2SJR;[02] VERIFIED CORRECTIVE ACTION ITEM 1 AND MEASUREME
- [SDR SWAA2023111311737](https://openairdocs.org/sdr/SWAA2023111311737), Oct 18, 2023: PANEL. DEBONDED. PANEL 194AL OUTER SKIN AT LOWER FWD EDGE IS DISBONDED. (MARKED)<[01] PANEL 194AL OUTER SKIN AT LOWER FWD EDGE WITH DISBOND AS MARKED WAS REPAIRED PER SRM 51-70-
- [SDR SWAA2023111012000](https://openairdocs.org/sdr/SWAA2023111012000), Oct 18, 2023: PRESSURE DECK. CRACKED. HORIZONTAL PRESSURE DECK WEB RBL 40 + .5' - FOUND CRACK TO BE .3' MARKED ENDS.<[01] REMOVED AND REPAIRED HORIZONTAL PRESSURE DECK WEB I.A.W SRM 53-40-51-2R-2 RE
- [SDR SWAA2023111012137](https://openairdocs.org/sdr/SWAA2023111012137), Oct 18, 2023: SCUFF PLATE. CRACKED. AFT CARGO BAY FWD CORNER SCUFF PLATE IS CRACKED<[01] CRACK ON SCUFF PLATE FOUND TO BE OUT OF LIMITS AS PER SRM 53-60-15-1A-1;[02] WELDED CRACK ON THE CORNER SCU
- [SDR SWAA2023071177181](https://openairdocs.org/sdr/SWAA2023071177181), Jul 11, 2023: TRAY. OUT OF ADJUST. TRAY TABLE LATCH BROKEN AT 11C (EMERG EXIT ROW)<[01] REMOVED AND REPLACED TRAY TABLE LATCH PER SIP
- [SDR SWAA2023062671652](https://openairdocs.org/sdr/SWAA2023062671652), Jun 24, 2023: SLIDE. LOOSE. R1 EMERGENCY SLIDE FELL OUT OF HOLDER<[01] R&R R1SLIDE IAW 25-66-01
- [SDR SWAA2022042595639](https://openairdocs.org/sdr/SWAA2022042595639), Apr 19, 2022: BRACKET. BROKEN. PANEL 192E LEFT FWD ATTACHING BRACKET BROKEN / [01] R&R PANEL 192E LEFT FWD ATTACHING BRACKET PER REF AMM 53-12-12.
- [SDR SWAA2022021472166](https://openairdocs.org/sdr/SWAA2022021472166), Feb 11, 2022: NONE. NONE. LANDING GEAR LEVER WOULD NOT MOVE OUT OF THE OFF POSITION. COMPLIED WITH QRH. EXTENDED LANDING GEAR MANUALLY. ; / [01] PERFORMED SYSTEM TEST - LANDING GEAR CONT
- [SDR SWAA2022013164960](https://openairdocs.org/sdr/SWAA2022013164960), Jan 27, 2022: HANDLE. BROKEN. L1 DOOR ASSST HANDLE BROKEN ; / [01] REMOVED AND REPLACED FORWARD ENTRY DOOR ASSIST HANDLE. PER AMM 25-66-00.
- [SDR SWAA2021122350679](https://openairdocs.org/sdr/SWAA2021122350679), Dec 4, 2021: ACCESS PANEL. CORRODED. CORROSION ACCESS PANEL 532PB ON CLAMP RING AT LT WING (1) ; 2021-520755 / [01] PERFORMED PERMANENT REPAIR ON CLAMP RING ACCESS PANEL 532PB LT WING IAW B737-700 
- [SDR SWAA2021122350680](https://openairdocs.org/sdr/SWAA2021122350680), Dec 4, 2021: ACCESS PANEL. CORRODED. CORROSION ACCESS PANEL 532QB ON CLAMP RING AT LT WING ; 2021-520756 / [01] PERFORMED PERMANENT REPAIR ON CLAMP RING ACCESS PANEL 532QB LT WING IAW B737-700 SRM 
- [SDR SWAA2021122248266](https://openairdocs.org/sdr/SWAA2021122248266), Nov 28, 2021: LIGHT. BROKEN. BROKEN GALLEY 4 EMERGENCY EXIT LIGHT ASSY AT AFT GALLEY AREA ; 2021-520715 / [01] REPLACED GALLEY 4 EMERGENCY EXIT LIGHT ASSY AT AFT GALLEY AREA IAW B737-700 AM
- [SDR SWAA2021122250885](https://openairdocs.org/sdr/SWAA2021122250885), Nov 24, 2021: ACCESS PANEL. BROKEN. SUPPLEMENTAL INFORMATION: BROKEN COVER ACCESS PANEL 651FB AT RT WING ; 2021-520716 / [01] REPLACED COVER ACCESS PANEL 651FB AT RT WING IAW B737-700 SRM 51-10-02
- [SDR SWAA2021122246722](https://openairdocs.org/sdr/SWAA2021122246722), Nov 22, 2021: FLOOR PANEL. CRACKED. CRACK FLOOR PANEL DRAINS SERVICE DOOR SIDE AT FWD GALLEY AREA (2 EA) ; 2021-520697 / [01] REPLACED FLOOR PANEL DRAINS SERVICE DOOR SIDE AT FWD GALLEY AREA (2 EA
- [SDR SWAA2021122246495](https://openairdocs.org/sdr/SWAA2021122246495), Nov 21, 2021: NONE. CRACKED. CRACK INTERCOSTAL, WEB FLOOR STRUCTURE BTW BS 380 TO BS 400 AT RBL 10 AT PASSENGER CABIN. REPLACED WEB FLOOR STRUCTURE BTW BS 380 TO BS 400 AT RBL 10 AT PASSENG
- [SDR SWAA2021122246490](https://openairdocs.org/sdr/SWAA2021122246490), Nov 21, 2021: INTERCOSTAL. CRACKED. CRACK INTERCOSTAL - WEB FLOOR STRUCTURE BTW BS 277 TO BS 291.5 AT BL 0 AT PASSENGER CABIN ; 2021-520688 / [01] REPLACED INTERCOSTAL LOC. FLOOR STRUCTURE BTW BS 
- [SDR SWAA2021122246493](https://openairdocs.org/sdr/SWAA2021122246493), Nov 21, 2021: STRUCTURE. CRACKED. CRACK ANGLE FLOOR STRUCTURE BTW BS 291.5 TO BS 294 AT RBL 45 AT PASSENGER CABIN ; 2021-520694 / [01] REPLACE ANGLE FLOOR STRUCTURE BTW BS 291.5 TO BS 294 AT RBL
- [SDR SWAA2021122246491](https://openairdocs.org/sdr/SWAA2021122246491), Nov 21, 2021: STRUCTURE. CRACKED. CRACK FLOOR STRUCTURE BTW BS 312 TO BS 328 AT LEVEL RBL 31 AT PASSENGER CABIN ; 2021_520689 / [01] REPLACED INTERCOSTAL FLOOR STRUCTURE LOC. BTW BS 312 TO BS 32
- [SDR SWAA2021122246492](https://openairdocs.org/sdr/SWAA2021122246492), Nov 21, 2021: NONE. CRACKED. CRACK INTERCOSTAL, WEB FLOOR STRUCTURE BTW BS 344 TO BS 360 AT LBL 11 AT PASSENGER CABIN. PERFORMED REPAIR ON INTERCOSTAL WEB FLOOR STRUCTURE BTW BS 344 TO BS 3
- [SDR SWAA2021122246485](https://openairdocs.org/sdr/SWAA2021122246485), Nov 21, 2021: FRAME. CRACKED. CRACK FRAME BS727A BETWEEN STR 8R TO STR 9R AT PASSENGER CABIN ; 2021-520686 / [01] REPAIRED FRAME BS727A BETWEEN STR 8R TO STR 9R AT PASSENGER CABIN IAW EA 1-A
- [SDR SWAA2021122246488](https://openairdocs.org/sdr/SWAA2021122246488), Nov 21, 2021: FRAME. CRACKED. CRACK FRAME BS787 BETWEEN STR 8R TO STR 9R AT PASSENGER CABIN ; 2021-520685 / [01] REPAIRED FRAME BS787 BETWEEN STR 8R TO STR 9R AT PASSENGER CABIN IAW EA 1-A53
- [SDR SWAA2021122246472](https://openairdocs.org/sdr/SWAA2021122246472), Nov 20, 2021: BRACKET. CRACKED. SUPPLEMENTAL INFORMATION: CRACK SUPPORT BRACKET BODY STATION 540 LH SIDE KEEL BEAM ; 2021-520678 / [01] REPLACED SUPPORT BRACKET BODY STATION 540 LH SIDE KEEL B
- [SDR SWAA2021122246471](https://openairdocs.org/sdr/SWAA2021122246471), Nov 20, 2021: BRACKET. CRACKED. SUPPLEMENTAL INFORMATION: CRACK SUPPORT BRACKET BODY STATION 540 RH SIDE KEEL BEAM ; 2021-520677 / [01] REPLACED SUPPORT BRACKET BODY STATION 540 RH SIDE KEEL B
- [SDR SWAA2021122246456](https://openairdocs.org/sdr/SWAA2021122246456), Nov 20, 2021: FLOOR PANEL. CORRODED. SUPPLEMENTAL INFORMATION: CORROSION SLEEVE FLOOR PANEL 241ABF AT AFT GALLEY AND LAV (6 EA) ; 2021-520665 / [01] TOOL USED: SCALE P/N: SCA-301 S/N: AE-412120 DUE
- [SDR SWAA2021122346467](https://openairdocs.org/sdr/SWAA2021122346467), Nov 20, 2021: FLOOR PANEL. DELAMINATED. DELAMINATED FLOOR PANEL 221BF AT PASSENGER CABIN ; 2021-520672 / [01] REPLACED FLOOR PANEL 221BF AT PASSENGER CABIN IAW B737-700 AMM 52-21-00-400-801; [02] COMP
- [SDR SWAA2021122346470](https://openairdocs.org/sdr/SWAA2021122346470), Nov 20, 2021: FLOOR PANEL. DELAMINATED. DELAMINATED FLOOR PANEL 221GF AT PASSENGER CABIN ; 2021-520674 / [01] REPLACED FLOOR PANEL 221GF AT PASSENGER CABIN IAW B737-700 AMM 53-21-00-400-801; [02] VERI
- [SDR SWAA2021122346460](https://openairdocs.org/sdr/SWAA2021122346460), Nov 20, 2021: FLOOR PANEL. CRACKED. CRACK FLOOR PANEL 241ZF AT PASSENGER CABIN. REMOVED INSERTS ON DAMAGE AREA AND REMOVED DAMAGE ON FLOOR PANEL 241ZF AS PER B737-700 SRM 53-00-50-2R-6 REPAIR 6 PA
- [SDR SWAA2021122246475](https://openairdocs.org/sdr/SWAA2021122246475), Nov 20, 2021: FLOOR PANEL. DELAMINATED. DELAMINATED FLOOR PANEL 242BF AT PASSENGER CABIN ; 2021-520679 / [01] REPLACED FLOOR PANEL 242BF AT PASSENGER CABI IAW B737-700 AMM 53-21-00-400-801; [02] REPLA
- [SDR SWAA2021112446461](https://openairdocs.org/sdr/SWAA2021112446461), Nov 20, 2021: SPAR. CRACKED. CRACK FRONT SPAR ANGLE LOCATED FUEL BOSST PUMP IFSS 120 AREA AT RT WI NG (1 EA) 2021-520664 / TOOL USED DIGITAL CALIPER P/N 500-193-30 S/N 0000291 DUE DATE 16-S
- [SDR SWAA2021122246455](https://openairdocs.org/sdr/SWAA2021122246455), Nov 19, 2021: NONE. CRACKED. SUPPLEMENTAL INFORMATION: CRACK WEB - INTERCOSTAL LOCATED BETWEEN BS420 TO BS440 AND RBL22 FWD CARGO COMPARTMENT ; 2021-520654 / [01] REPLACED WEB - INTERCOSTAL
- [SDR SWAA2021122246454](https://openairdocs.org/sdr/SWAA2021122246454), Nov 19, 2021: TRACK. CRACKED. SUPPLEMENTAL INFORMATION: CRACK TRACK LOCATED BS460 AND RBL14 AT FWD CARGO COMPARTMENT ; 2021-520624 / [01] TOOL USED EDDY CURRENT FLAW DETECTOR P/N: NORTEC 600
- [SDR SWAA2021122746023](https://openairdocs.org/sdr/SWAA2021122746023), Nov 19, 2021: ACCESS PANEL. CRACKED. CRACK ACCESS PANEL 532NB INDICATOR FUEL FLOAT AT LT WING ; 2021-520600 / [01] REPLACED ACCESS PANEL 532NB INDICATOR FUEL FLOAT AT LT WING IAW ROCKWELL COLLINS C

All 217: https://openairdocs.org/aircraft/N7863A/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 N7863A

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N7863A before.

- [Cancelled 1971-02-26](https://openairdocs.org/deregistered/N7863A-1971-02-26): Cessna 180, S/N 32760. Owner: [Kippenham Lester A](https://openairdocs.org/faa-owner/KIPPENHAM%20LESTER%20A), [Anchorage, AK](https://openairdocs.org/faa-place/AK/Anchorage)

## 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

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