- Registered owner
- Eastern 737 Asset Holdings LLC
- Location
- Kansas City, MO
- Owner type
- LLC
- Serial number
- 25098
- Year built
- 1992
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- July 10, 1992
- Certificate issued
- May 1, 2024
- Expires
- May 31, 2031
- Mode S code
- AAFD90
From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every CFM International CFM56 model are included below.
On this page
Airworthiness directives that may apply · 55
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1985 | 1 |
|---|---|
| 1986 | 1 |
| 1990 | 1 |
| 1991 | 1 |
| 1996 | 1 |
| 1997 | 5 |
| 1998 | 9 |
| 1999 | 2 |
| 2000 | 3 |
| 2001 | 5 |
| 2002 | 5 |
| 2003 | 2 |
| 2004 | 2 |
| 2005 | 1 |
| 2007 | 3 |
| 2008 | 2 |
| 2009 | 2 |
| 2010 | 4 |
| 2012 | 1 |
| 2013 | 2 |
| 2014 | 1 |
| 2015 | 2 |
| 2016 | 2 |
| 2017 | 2 |
| 2018 | 4 |
| 2019 | 2 |
| 2021 | 2 |
| 2022 | 1 |
| 2023 | 1 |
Engine · CFM International CFM56 series
AD 2023-05-05Turbine Engine Compressor SectionAD 2022-02-03Turbine Engine Accessory DriveAD 2021-16-08Turbine SectionInformation bulletins that may apply · 4
Advisory, not mandatory.
Historical bulletins · 5
SAIB NE-13-33R1Turbine Engine Air Inlet Section - LP Turbine, Stage 1 Nozzle VanesSAIB NE-13-33Turbine Engine Air Inlet Section - LP Turbine, Stage 1 Nozzle VanesSAIB NE-08-17R2Turbine Section - Propulsion Technology LLC Unapproved RepairSAIB NE-08-17R1Propulsion Technology LLC Unapproved RepairSAIB NE-08-17Propulsion Technologies International Unapproved Repair
NTSB investigations
No NTSB investigations matched to N807TJMatched by N-number and event date, checked against the reported serial number, make and model. Investigations from before this aircraft carried the mark are under Earlier aircraft. Investigations on Boeing 737-4Q8 aircraft
FAA incident reports · 1
FAA accident and incident reports matched to this aircraft by N-number and event date, checked against the reported make and model.
Service difficulty reports · 15
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 2026FA0000070Power Supply · inoperativeR/H MID TO AFT EMERGENCY LIGHT POWER SUPPLY INOPSDR 2026FA0000069Power Supply · inoperativeR/H MID TO AFT EMERGENCY LIGHT POWER SUPPLY INOPSDR I5EA2023090800003Battery Pack · no testAISLE LIGHT AT STA 500E + R INOP FOR EMERGENCY LIGHT. REMOVED AND REPLACED BATTERY PACK FOR AILSE LIGHT M1468 STA 500C + 10L IAW B737-400 AMM 33-51-51.SDR I5EA2023081100019Unknown · unknownFUSELAGE SKIN CRACK AT STA. 727E, STR 24R, REPAIRED FUSELAGE RH SKIN AT STA.727E, STR. 24R, IAW B737-400 SRM 53-00-01, REPAIR 31SDR I5EA2023051600006Module · no testMODULE M1134 REQUIRES REPLACEMENT. REMOVE AND REPLACE MODULE M1134 AT STA. 634L IAW B737-400 AMM 33-51-51. OPS CHECK GOOD.SDR I5EA2023051600005Battery Pack · no testOVERWING EMERGENCY EXIT LIGHT FOR HATCH INOP. REMOVED AND REPLACED BATTERY PACK AT M1134 AT STA. 634L IAW B737-400 AMM 33-51-51. OPS CHECK GOOD.SDR I5EA2023020600002Battery Pack · inoperativeEMERGENCY LIGHT INOP AT STA. 727A+17 BULLNOSE. REMOVED AND REPLACED EMERGENCY BATTERY BACK AT M1576 STA. 727A WITH SERVICEABLE UNIT IAW B737-400 AMM 33-51-51, TEST OKSDR I5EA2022110100002Battery Pack · no testFWD SERVICE LIGHT INOP. REMOVE AND REPLACE BATTERY PACK AT M1133 STA. 330L IAW B737-400 AMM 33-51-51. TEST GOOD.SDR I5EA2022110100001Battery Pack · no testEMERGENCY EXIT LIGHT INOP AT ROW 3 CLASS DIVIDERS. REMOVED AND REPLACE BATTERY PACK AT M1132 STA. 330R IAW B737-400 AMM 33-51-51. TEST GOOD.SDR I5EA2022101700008Battery Pack · dischargedEMERGENCY LIGHT OUT AT OVERWING HATCH EXIT LIGHT RIGHT, REMOVED AND REPLACED EMERGENCY BATTERY WITH SERVICEABLE AT M1474, STA. 598R, IAW B737-400 AMM 33-51-51SDR I5EA2022101400006Power Supply · no testEMERGENCY LIGHT OUT OVERWING. REMOVED AND REPLAED EMERGENCY LIGHT POWER SUPPLY M1134, STA. 634L FOR LEFT OVERWING IAW B737 AMM 33-51-51, OPS CHECK GOODSDR I5EA2022101700007Battery Pack · dischargedEMERGENCY LIGHT OUT AISLE LIGHT RIGHT STA. 704R. REMOVED AND REPLACED BATTERY PACK FOR AISLE LIGHT AT M1435, STA. 747R, IAW B737-400 AMM 33-51-51SDR I5EA2021081700012Circuit Breaker · trippedLANDING GEAR WILL NOT MOVE TO THE UP POSITIOON AFTER TAKEOFF. DURING TROUBLESHOOT, FOUND CIRCUIT BREAKER (LATCH & PRESS WARN) POPPED OUT, RESET CIRCUIT BREAKER IAW B737 AMM 20-60-01. PERFORMED GEAR EXTENSION AND RETRACTION TEST IAW AMM 32-32-00, TEST NORMAL. SDR I5EA201910110906Power Supply · inoperativeBULLNOSE EMERGENCY LIGHT INOP AT SEAT ROW 14DF, 16DF, AND 18DF.SDR I5EA2018071701Downlock Sensor · contaminatedUPON GEAR EXTENSION FOR LANDING, GOT GREEN LIGHTS FOR MAIN GEAR, GOT RED LIGHT FOR NOSE WITH NO GREEN LIGHT. FOLLOWED QRH WITH MANUAL EXTENSION, NO CHANGE. LANDED WITHOUT INCIDENT, STOPPED ON TAXIWAY, HAD ANOTHER SWIFT PILOT PIN NOSE GEAR. TROUBLE SHOT AND
STCs that may be installed · 7
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Engine · CFM International CFM56 series
STC SE04840NYInstallation of HarcoSemco Exhaust Gas Temperature (EGT) Electrical Harnesses in CFM56-7 engineSTC SE03036CHApplication 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.STC SE00032ENInstallation of Pratt & Whitney (P&W) Global Material Solutions (GMS) CFM56-3 Fan/Booster Module.STC SE00033ENInstallation of Pratt & Whitney (P&W) Global Material Solutions (GMS) CFM56-3 High Pressure Compressor ModuleSTC SE00034ENInstallation of Pratt & Whitney (P&W) Global Material Solutions (GMS) CFM56-3 High Pressure Turbine ModuleSTC SE00035ENInstallation of Pratt & Whitney (P&W) Global Material Solutions (GMS) CFM56-3 Low Pressure Turbine ModuleSTC SE00822CHInstall 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.