# N7867A: 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: 30633
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: March 2, 2018
- Certificate issued: February 10, 2026
- Expires: February 28, 2033
- Mode S code: AAAA1E
- 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=7867A
- Page: https://openairdocs.org/aircraft/N7867A

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 CFM56-7B24 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 N7867A.

## FAA accident and incident reports

None matched to N7867A.

## Service difficulty reports (195, 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 SWAA2025092215998](https://openairdocs.org/sdr/SWAA2025092215998), Sep 18, 2025: SLIDE. LOOSE. FWD SVC DOOR EMER SLIDE LOOSE. REMOVED AND REINSTALLED FWD SVC DOOR SLIDE AS REQUIRED REF MT 725-61-06.
- [SDR SWAA2025031104117](https://openairdocs.org/sdr/SWAA2025031104117), Mar 10, 2025: HANDLE. BROKEN. MAIN CABIN DOOR ASSIST HANDLE. BROKEN<[01] R AND R MAIN CABIN DOOR ASSIST HANDLE.<BR><BR><BR> IAW AMM 52-11-00
- [SDR SWAA2024112671890](https://openairdocs.org/sdr/SWAA2024112671890), Nov 25, 2024: GIRT BAR. OUT OF ADJUST. FWD SERVICE DOOR GIRT BAR HOLDER LOOSE<[01] INSPECTED GIRT BAR HOOKS ON SLIDE COVER; FOUND TO BE SERVICEABLE IAW AMM 25-66-01
- [SDR SWAA2024103054128](https://openairdocs.org/sdr/SWAA2024103054128), Oct 28, 2024: RETAINER. LOOSE. FOWARD SERVICE DOOR SLIDE GIRT BAR HOLDER LOOSE.<[01] TIGHTENED GIRT BAR RETAINER PER SIP.
- [SDR SWAA2024102250802](https://openairdocs.org/sdr/SWAA2024102250802), Oct 19, 2024: RING. MISSING. FWD SERVICE DOOR EVAC SLIDE MISSING STOP RING ON GIRT BAR.<[01] R/R'D FWD SERVICE DOOR GIRT BAR PER AMM 25-66-01.
- [SDR SWAA2024101748005](https://openairdocs.org/sdr/SWAA2024101748005), Oct 13, 2024: BULB. INOPERATIVE. R/H OVER WING EMERGENCY LIGHT INOP<[01] REMOVED AND REPLACED THE R/H OVER WING EMERGENCY LIGHT BULB REF AMM 33-51-04 OPS CHECK GOOD
- [SDR SWAA2023122634743](https://openairdocs.org/sdr/SWAA2023122634743), Dec 21, 2023: LIGHT. INOPERATIVE. STARBOARD OVERAWING EXIT ROW LIGHT BURNT OUT.<[01] RE-LAMP L/H OVERWING EXIT ROW LIGHT REF AMM 33-51-04.
- [SDR SWAA2023121129090](https://openairdocs.org/sdr/SWAA2023121129090), Dec 7, 2023: MEGAPHONE. INOPERATIVE. FWD MEGAPHONE INOP.<[01] REPLACED BATTERIES IN THE FWD MEGAPHONE PER AMM 25-64-00-900-804. OPS CHECK GOOD;[02] VERIFIED CORRECTIVE ACTION 1 AND MEASUREMENT TABL
- [SDR SWAA2023121226364](https://openairdocs.org/sdr/SWAA2023121226364), Dec 1, 2023: SIGN. INOPERATIVE. SEVERAL LAMPS DO NOT ILLUMINATE IN RIGHT OVERWING EXIT INDICATOR SIGN.<[01] REPLACED FIVE INOPERATIVE LAMPS IN RIGHT SIDE OVERWING EMERGENCY EXIT SIGN AND TESTE
- [SDR SWAA2023121226362](https://openairdocs.org/sdr/SWAA2023121226362), Dec 1, 2023: BULB. INOPERATIVE. AFT INCANDESCENT BULBS ON RIGHT AND LEFT OVERWING EXIT ILLUMINATION LIGHTS DO NOT ILLUMINATE.<[01] RELAMPED AFT SIDE OF LEFT AND RIGHT OVERWING EXIT ILLUMINATIO
- [SDR SWAA2023121126361](https://openairdocs.org/sdr/SWAA2023121126361), Dec 1, 2023: LIGHT. INOPERATIVE. EMERGENCY AISLE LIGHTS AT ROWS 19/20 L AND 16R DO NOT ILLUMINATE.<[01] RELAMPED AISLE LIGHTS AT ROWS 19/20L AND 16R AND TESTED PER AMM 33-51-03-960-801; NO FURT
- [SDR SWAA2023121226359](https://openairdocs.org/sdr/SWAA2023121226359), Nov 30, 2023: PANEL. DELAMINATED. PANEL 661AB HAS FIBER BREAKOUT AND DELAMINATION OF EXTERNAL PLY SKIN (MARKED)<[01] REFERENCE CORRECTION MADE TO STEP 4 ITEM 2.;[02] FIBER EXTERNAL PLY SKIN ON P
- [SDR SWAA2023121226358](https://openairdocs.org/sdr/SWAA2023121226358), Nov 30, 2023: PANEL. DELAMINATED. PANEL 661CB HAS FIBER BREAKOUT AND DELAMINATION OF EXTERNAL PLY SKIN (MARKED)<[01] REFERENCE CORRECTION MADE TO ITEM 4 STEP 2;[02] FIBER EXTERNAL PLY SKIN ON PA
- [SDR SWAA2023121223796](https://openairdocs.org/sdr/SWAA2023121223796), Nov 21, 2023: SUPPORT. CORRODED. AFT BAY LH FLOOR TO SIDEWALL SUPPORT IS CORRODED BTWEEN BS 747- 807 LBL 22<[01] REPLACED AFT BAY LH FLOOR TO SIDEWALL SUPPORT BETWEEN BS 727+4 TO BS 847; LBL 22
- [SDR SWAA2023121223793](https://openairdocs.org/sdr/SWAA2023121223793), Nov 21, 2023: SUPPORT. CORRODED. AFT BAY RH FLOOR TO SIDEWALL SUPPORT IS CORRODED BTWEEN BS 727A- 767 LBL 22<[01] CORRECT BL OF AFT BAY RH FLOOR TO SIDEWALL SUPPORT IS CORRODED BTWEEN BS 727A- 
- [SDR SWAA2023121223111](https://openairdocs.org/sdr/SWAA2023121223111), Nov 19, 2023: SUPPORT ANGLE. CRACKED. RIGHT WING T/E PANEL 661AB AFT PANEL SUPPORT ANGLE IS CRACKED AT I/B END<[01] REMOVED AND REPLACED RIGHT WING T/E PANEL 661AB AFT PANEL SUPPORT ANGLE AT I/B END
- [SDR SWAA2023121222673](https://openairdocs.org/sdr/SWAA2023121222673), Nov 17, 2023: SUPPORT ROD. CORRODED. LEFT WING T/E PANEL 551FB AFT O/B PANEL SUPPORT ROD IS CORRODED<[01] REMOVED AND REPLACED CORRODED SUPPORT ROD ON PANEL 551FB AFT OF O/B END. IAW AMM 20-50-11-9
- [SDR SWAA2023121221908](https://openairdocs.org/sdr/SWAA2023121221908), Nov 16, 2023: PRESSURE DECK. CRACKED. RH HORIZONTAL PRESSURE DECK HAS TWO CRACKS. 1) BS 664.5 RBL 40.5 WL 202 AND 2) BS 672.5 RBL 41.5 WL 202. FOUND ON HFEC INSPECTION.<[01] REPAIRED R/H BEADED PRES
- [SDR SWAA2023121122313](https://openairdocs.org/sdr/SWAA2023121122313), Nov 16, 2023: FLOOR PANEL. PEELING. FLOOR PANEL 242AF HAS REPAIR PEELING OFF<[01] FABRICATION OF NEW 242AF FLOORBOARD HAS BEEN COMPLETED IAW SRM 53-00-50-2R-0.<BR><BR>ATTACHED CURE SHEET TO THIS F
- [SDR SWAA2023121122314](https://openairdocs.org/sdr/SWAA2023121122314), Nov 16, 2023: FLOOR PANEL. PEELING. FLOOR PANEL 231XF HAS EXPOSED FIBERS PEELING OFF<[01] FLOORBOARD 231XF FABRICATION HAS BEEN COMPLETED IAW SRM 53-00-50-2R-0.<BR><BR>ATTACHED CURE SHEET TO THIS 
- [SDR SWAA2023103015740](https://openairdocs.org/sdr/SWAA2023103015740), Oct 28, 2023: LIGHT. INOPERATIVE. ROW 4 RIGHT SIDE NIGHT LIGHTS INOP<[01] R&R LAMP PER AMM 33-22-00.;[02] (NEEDS TO READ) OK TO CONTINUE PER MEL 33-2-03 SP 1B AUTH #163541;[03] C/W
- [SDR SWAA2023101209261](https://openairdocs.org/sdr/SWAA2023101209261), Oct 10, 2023: SEAL. CRACKED. RH FWD LOWER HORIZONTAL STAB SLIDER SEAL IS CRACKED<[01] REMOVED AND REPLACED SLIDER SEAL AMM 53-31-31.;[02] C/W INSPECTION
- [SDR SWAA2023101209268](https://openairdocs.org/sdr/SWAA2023101209268), Oct 10, 2023: SEAL. CRACKED. LH FWD HORIZONTAL STAB SLIDER SEAL CRACKED<[01] REMOVED AND REPLACED SLIDER SEAL PER AMM 53-31-31.;[02] C/W INSPECTION
- [SDR SWAA2023091801622](https://openairdocs.org/sdr/SWAA2023091801622), Sep 15, 2023: FLAP. DELAMINATED. LEFT WING OUTBOARD TRAILING EDGE AFT FLAP INBOARD SIDE SHEET METAL SKIN DISBONDED 6 INCHES IN LENGTH X 6 INCHES AT INBOARD EDGE; 3 INCHES AWAY FROM FASTENERS. (
- [SDR SWAA2023082492935](https://openairdocs.org/sdr/SWAA2023082492935), Aug 23, 2023: GIRT BAR. OUT OF ADJUST. FWD SERVICE DOOR GIRT BAR HARD O STOW.<[01] R & R FS DOOR FASTENER ON AFT GIRT BAR RETAINER PER SRM#51-40-02.<BR>REINSTALLED FS DOOR SLIDE PER MT # 725-61-06.
- [SDR SWAA2023062060444](https://openairdocs.org/sdr/SWAA2023062060444), Jun 18, 2023: LIGHT. INOPERATIVE. EMERGENCY LIGHTS INOP @ L1 DOOR; R1 OUTSIDE FLOOR LEVEL AND RH BULLNOSE @ 6DEF.<[01] REMOVED AND REPLACED FWD RT EMERGENCY LIGHT POWER SUPPLY IAW AMM 33-51-06.
- [SDR SWAA2023060254895](https://openairdocs.org/sdr/SWAA2023060254895), Jun 1, 2023: GIRT BAR. LOOSE. FWD SERVICE DOOR GIRT BAR LOOSE.<[01] ADJUSTED FWD SERVICE DOOR GIRT BAR PER SIP. OK FOR CONTINUED SERVICE.
- [SDR SWAA2023032118286](https://openairdocs.org/sdr/SWAA2023032118286), Mar 18, 2023: LIGHT. INOPERATIVE. EMERGENCY LIGHT ON L/H AFT BELLY IS INOP<[01] RELAMPED L/H AFT BELLY EMERGENCY LIGHT PER AMM 33-51-04; OPS CHECK GOOD.
- [SDR SWAA2022123086376](https://openairdocs.org/sdr/SWAA2022123086376), Dec 30, 2022: SIGN. INOPERATIVE. LH OVERWING EXIT FWD LOWER EMERGENCY EXIT SIGN INOPERATIVE. REMOVED AND REPLACED EMERGENCY SIGN IAW AMM 33-51-01
- [SDR SWAA2022101056987](https://openairdocs.org/sdr/SWAA2022101056987), Oct 7, 2022: NONE. INOPERATIVE. RH OVER WING EXIT SIDEWALL LIGHT INOP / [01] REMOVED AND REPLACED RH OVER WING EXIT LIGHT ASSEMBLY IN REF TO AMM 33-21-00. OPS CHECK GOOD AT THIS TIME
- [SDR SWAA2022072632846](https://openairdocs.org/sdr/SWAA2022072632846), Jul 22, 2022: GIRT BAR. OUT OF POSITION. ENTRY DOOR SLIDE GIRT BAR DOES NOT SECURE PROPERLY / [01] ADJUSTED AS PER SIP
- [SDR SWAA2022071828027](https://openairdocs.org/sdr/SWAA2022071828027), Jul 12, 2022: SKIN. CRACKED. -LEFT HORIZONTAL STAB LOWER INSPAR SKIN CRACKED APPROX 1 STAB STA 120.3 APPROX 11 INCHES FWD OF AFT END. / [01] REPAIRED LH HORZ STAB LOWER INSPAR SKIN PER EA 2
- [SDR SWAA2022051105546](https://openairdocs.org/sdr/SWAA2022051105546), May 7, 2022: LENS. BROKEN. FWD ENTRY EMERGENCY LIGHT LENS BROKEN / [01] REPLACED PER SIP
- [SDR SWAA2022021461737](https://openairdocs.org/sdr/SWAA2022021461737), Jan 15, 2022: RIB. CRACKED. CRACK INSPAR RIB STAB STA 157.10 LOWER CHORD COMMON TO FRONT SPAR LT HORIZONTAL STAB ; 2021-585238 / [01] TOOL USED EDDY CURRENT EQUIPMENT P/N: NORTEC 500D; S/N
- [SDR SWAA2022021461056](https://openairdocs.org/sdr/SWAA2022021461056), Jan 12, 2022: SEAT TRACK. CORRODED. CORROSION ON SEA TRACK LOCATED BS 540 AT RBL 24.75 ON PAX PASSENGER CABIN ; 2021-585227 / [01] REWORKED CORROSION AREA ON SEAT TRACK LOCATED BS 540 AT RBL 24.75
- [SDR SWAA2022021460020](https://openairdocs.org/sdr/SWAA2022021460020), Jan 9, 2022: SUPPORT. CORRODED. CORROSION SUPPORT ZEE LOC. BTW BSTA 747 AND BSTA 767 AT LEVEL STRINGER 25L AT AFT CARGO COMPARTMENT ; 2021-585172 / [01] REPLACED SUPPORT ZEE LOCATED BSTA 747 A
- [SDR SWAA2022021460018](https://openairdocs.org/sdr/SWAA2022021460018), Jan 8, 2022: STRUCTURE. DETERIORATED. DETERIORATED FLOOR STRUCTURE CIC BTW STA 270 TO STA 380 AT FWD GALLEY AREA ; 2021-585167 / [01] REPLACED FLOOR STRUCTURE CIC BTW STA 270 TO STA 380 AT FWD GALLE
- [SDR SWAA2022021460019](https://openairdocs.org/sdr/SWAA2022021460019), Jan 8, 2022: STRUCTURE. DETERIORATED. DETERIORATED FLOOR STRUCTURE CIC BTW STA 887 TO STA 1016 AT AFT GALLEY AREA ; 2021-585168 / [01] APPLIED CIC ON FLOOR STRUCTURE BTW STA 887 TO STA 1016 AT AFT G
- [SDR SWAA2022021460011](https://openairdocs.org/sdr/SWAA2022021460011), Jan 7, 2022: TRACK. CRACKED. CRACK TRACK RBL 13.84 LOCATED BS 500 AT FWD CARGO COMPARTMENT ; 2021-585157 / [01] TOOL USED CALIPER P/N: 500-197-30 S/N: A21147748 DUE DATE 02-OCT-22; [02] TOO
- [SDR SWAA2022021459039](https://openairdocs.org/sdr/SWAA2022021459039), Jan 6, 2022: FLOOR PANEL. BROKEN. BROKEN FLOOR PANEL 221BF AT PASSENGER CABIN ; 2021-585140 / [01] TOOL USED CALIPER P/N: 500-197-30 S/N: A18229508 DUE DATE: 29/SEP/22.; [02] TOOL USED: MICRO HO
- [SDR SWAA2022021459257](https://openairdocs.org/sdr/SWAA2022021459257), Jan 6, 2022: SUPPORT. CRACKED. CRACK ANGLE - SUPPORT LOCATED BS 947.5 AND LBL 8.10 AFT CARGO COMPARTMENT ; 2021-585144 / [01] REPLACED ANGLE - SUPPORT LOCATED BS 947.5 AND LBL 8.10 AFT CARGO 
- [SDR SWAA2022021459256](https://openairdocs.org/sdr/SWAA2022021459256), Jan 6, 2022: TRACK. CRACKED. CRACK TRACK RBBL 13.84 LOCATED BS 727E AND BS 767 AFT CARGO COMPARTMENT ; 2021-585143 / [01] HIGH FREQUENCY EDDY CURRENT INSPECTION DONE ON CUT OUT EDGES; AS PE
- [SDR SWAA2022021459037](https://openairdocs.org/sdr/SWAA2022021459037), Jan 6, 2022: FLOAT. CRACKED. CRACK ACCESS PANEL 532QB ON FLOAT AT LT WING ; 2021-585137 / [01] REPLACED FLOAT ON ACCESS PANEL 532QB AT LT WING IAW ROCKWELL COLLINS CMM 28-40-11. TASK CARD T
- [SDR SWAA2022021459038](https://openairdocs.org/sdr/SWAA2022021459038), Jan 6, 2022: FLOAT. CRACKED. CRACK ACCESS PANEL 632QB ON FLOAT AT RT WING ; 2021-585132 / [01] REPLACED FLOAT ON ACCESS PANEL 632QB AT RT WING IAW ROCKWELL COLLINS CMM 28-40-11. TASK CARD T
- [SDR SWAA2022021458394](https://openairdocs.org/sdr/SWAA2022021458394), Jan 5, 2022: STRINGER. CRACKED. CRACK STRINGER 23L LOCATED BS540 FWD CARGO COMPARTMENT ; 2021-585103 / [01] ULTRASONIC THICKNESS GAGE P/N:45MG; S/N: 130060401; DUE DATE: 22-APR-22.; [02] ULTRA
- [SDR SWAA2022021458393](https://openairdocs.org/sdr/SWAA2022021458393), Jan 5, 2022: STRINGER. CRACKED. CRACK STRINGER 27R AND BS540 FWD CARGO COMPARTMENT ; 2021-585106 / [01] ULTRASONIC THICKNESS GAGE P/N:45MG; S/N: 130060401; DUE DATE: 22-APR-22.; [02] TOOL USED
- [SDR SWAA2022021458392](https://openairdocs.org/sdr/SWAA2022021458392), Jan 5, 2022: STRINGER. CRACKED. CRACK STRINGER 26L LOCATED BS540 AT FWD CARGO COMPARTMENT ; 2021-585105 / [01] ULTRASONIC THICKNESS GAGE P/N:45MG; S/N: 130060401; DUE DATE: 22-APR-22.; [07] PE
- [SDR SWAA2022021458391](https://openairdocs.org/sdr/SWAA2022021458391), Jan 5, 2022: STRINGER. CRACKED. CRACK STRINGER 23R AND BS540 FWD CARGO COMPARTMENT ; 2021-585104 / [01] ULTRASONIC THICKNESS GAGE P/N:45MG; S/N: 130060401; DUE DATE: 22-APR-22.; [02] TOOL USED
- [SDR SWAA2022021458019](https://openairdocs.org/sdr/SWAA2022021458019), Jan 4, 2022: TIE CLIP. CRACKED. CRACK TIE CLIP LOCATED BS277 AND STR10R AT PASSENGER CABIN ; 2021-585092 / [01] REPLACED NEW TIE CLIP LOCATED BS277 AND STR10R AT PASSENGER CABIN IAW B737-700 S
- [SDR SWAA2022021458017](https://openairdocs.org/sdr/SWAA2022021458017), Jan 4, 2022: BRACKET. BROKEN. BROKEN BRACKET ASSY INSULATOR LOCATED BS344 TO BS727 AND BETWEEN STR10R TO STR15R AT PASSENGER CABIN (8 EA) ; 2021-585095 / [01] REPLACED BRACKET ASSY INSULATOR

All 195: https://openairdocs.org/aircraft/N7867A/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 N7867A

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N7867A before.

- [Cancelled 1965-05-04](https://openairdocs.org/deregistered/N7867A-1965-05-04): Cessna 180A, S/N 32764. Exported to Australia. Owner: [Missionary Aviation Fellowship](https://openairdocs.org/faa-owner/MISSIONARY%20AVIATION%20FELLOWSHIP), [Fullerton, CA](https://openairdocs.org/faa-place/CA/Fullerton)

## 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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