N8566Z
Registered owner: UMB BANK NA TRUSTEE, UT (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
39 reports on file, 2018-04-05 – 2026-08-21.
Part: SEAT TRACK — WORN (ZONE 200) · airframe 28,102 hrs · 14,373 cycles
FIRST OFFICERS AFT INBD SEAT TRACK WORN. THE SEAT TRACK WAS R & R IAW MM 25-11-11.
Part: FLASHLIGHT — OUT OF ADJUST (ZONE 200) · airframe 27,521 hrs · 14,069 cycles
AFT GALLEY OTBD FLASHLIGHT WILL NOT TEST. ADJUSTED AFT GALLEY OTBD FLASHLIGHT, OPS CHECKED NORMAL IAW AMM 25-64-00.
Part: FLASHLIGHT — INOPERATIVE (ZONE 200) · airframe 27,300 hrs · 13,950 cycles
FWD J/S LT FLASHLIGHT INOPERATIVE. OK TO CONTINUE ON MEL 25-12-01. REMOVED AND REPLACED FWD OTBD JUMP SEAT FLASHLIGHT IAW AMM 25-64-00. OPS CHECKED GOOD.
Part: BRACKET — INOPERATIVE (GIRT BAR) · airframe 27,249 hrs · 13,920 cycles
AFT SERVICE DOOR (R2) GIRT BAR HAS LOCKING ISSUES. REPLACED R-2 GIRT BAR FLOOR BRACKET. REF AMM 25-66-02.
Part: LATCH — FOD (GIRT BAR) · airframe 27,245 hrs · 13,919 cycles
AFT SERVICE DOOR GIRT BAR FLOOR LATCH HARD TO LOCK, CLEANED DEBRIS AND FREED UP FLOOR LATCH ON R2 DOOR IAW AMM SIP. NO DEFECTS NOTED ; LATCH OK AT THIS TIME.
Part: COVER — OUT OF ADJUST (ZONE 200) · airframe 26,558 hrs · 13,564 cycles
EMERGENCY EXIT COVER. FELL OFF. INSTALLED COVER ON EMERGENCY EXIT FWD RH SIDE;[02] ADD: AMM 20-30-11
Part: COVER — MISSING (ZONE 200) · airframe 264,870 hrs · 13,529 cycles
PLASTIC COVER FOR EMERGENCY EXIT LIGHT IN CEILING BY 2D IS MISSING. REMOVED AND REPLACED LENS COVER IN CEILING BY 2D IAW MM 33-51-00
Part: COVER — MISSING (ZONE 200) · airframe 26,374 hrs · 13,476 cycles
OVERWING EMERGENCY EXIT SIGN COVER MISSING. REPLACED COVER IAW AMM 33-51-01
Part: COVER — DETACHED (ZONE 200) · airframe 26,080 hrs · 13,337 cycles
EMERENCY EXIT SIGN CENTER AISLE DETACHED. REINSTALLED THE EMERGENCY SIGN COVER IAW SIP.
Earlier reports · 2018–2025 · 30 reports
2025
Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 25,733 hrs · 13,156 cycles
R1 SERVICE DOOR EMERGENCY LIGHT INOPERATIVE. R & R R1 SLIDE/OVERWING LAMP IAW AMM 33-51-04 NO FIX. FOUND MUTIPLE INTERIOR EXIT LIGHTS INOP ON FWD R/H AREA. R & R FWD BATTERY PACK IAW AMM 33-51-06. OPS CHECKED GOOD.
Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 24,868 hrs · 12,708 cycles
AFT RT EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED AFT RT EMERGENCY LIGHT BATTERY PACK IAW AMM 33-51-06. OPS CHECKED GOOD.
2024
Part: FLASHLIGHT — UNSECURE (AFT CABIN) · airframe 19,674 hrs · 9,965 cycles
3 AFT GALLEY FLASHLIGHTS WILL NOT TEST<[01] REINSTALLED 3 AFT GALLEY FLASHLIGHTS INTO THE CRADLES; TEST FUNCTION OPS CHECK GOOD.REF AMM 25-64-00
Part: FLASHLIGHT — UNSECURE (FWD CABIN) · airframe 19,671 hrs · 9,963 cycles
FA FLASHLIGHT IN FORWARD CABIN IS INOP<[01] RESEATED FWD FLASHLIGHT IAW AMM 25-64-00. NO DEFECTS NOTED.
Part: LENS — INCORRECT (EMERGENCY LIGHT) · airframe 19,659 hrs · 9,956 cycles
RT FWD OVERWING EXIT LOWER EXIT LIGHT LENS APPEARS TO BE INCORRECT<[01] REMOVED AND REPLACED RT FWD OVERWING EXIT LOWER PROXIMITY LIGHT ASSY PER B737-800NG AMM TASK 33-51-01-960-802 EXIT SIGN LIGHT ASSEMBLY REPLACEMENT. OPS CHECK GOOD;[02] 02 - INSPECTED PER [AMM 25-21-20-401-NG (EMERGENCY EXIT DOORWAY LINING - REMOVAL/INSTALLATION - PERMANENT)]
Part: HANDLE — OUT OF ADJUST (L2 DOOR ASSIST) · airframe 19,659 hrs · 9,956 cycles
L2 DOOR ASSIST HANDLE NEEDS SECURED<[01] RESECURED L2 DOOR ASSIST HANDLE PER B737-800 NG AMM TASK 52-41-31-400-802 GALLEY SERVICE DOOR LINING INSTALLATION;[02] VERIFIED RESECURED L2 DOOR ASSIST HANDLE PER B737-800 NG AMM TASK 52-41-31-400-802
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 19,659 hrs · 9,956 cycles
L1 DOOR EMERGENCY LIGHT BATTERY PACK M1675 IS INOP.<[01] VERIFIED INSTALL OF L1 DOOR EMERGENCY LIGHT BATTERY PACK AND CHARGER AND OPS CHECK GOOD PER B737NG AMM 33-51-06-960-805 & 33-51-06-960-806.;[02] 01 - REMOVED AND REPLACED PER [33-51-06-960-805 & 33-51-06-960-806];[03] C/W TASK CARD
Part: BAFFLE — CRACKED (FWD CARGO) · airframe 19,659 hrs · 9,956 cycles
FWD CARGO BAFFLE 143A7510-22 IS CRACKED AT UPPER FWD CORNER<[01] REMOVED AND REPLACED CRACKED BAFFLE PT#143A7510-22 PO#1084939.1 IAW B737-800 SRM 51-40-02; BAC DWG 143A 7510 REV:-;[02] VERIFIED REMOVAL AND REPLACEMENT OF CRACKED BAFFLE PT#143A7510-22 PO#1084939.1 IAW B737-800 SRM 51-40-02; BAC DWG 143A 7510 REV:-
Part: STRINGER CLIP — CRACKED (BS 500H S26R) · airframe 19,659 hrs · 9,956 cycles
FWD CARGO ATTACH CLIP AT AFT SIDE OF STA 500H S26R IS CRACKED<[01] REMOVED AND REPLACED STA 500H S26R ATTACH CLIP PER B737-800 SRM 51-40-02 AND BAC DWG 143A7505 REV -;[02] VERIFIED REMOVED AND REPLACED STA 500H S26R ATTACH CLIP PER B737-800 SRM 51-40-02 AND BAC DWG 143A7505 REV-.
Part: FLOOR PANEL — CRACKED (MAIN CABIN) · airframe 19,659 hrs · 9,956 cycles
MAIN CABIN FLOOR PANEL 221GF FWD O/B FINGER CRACKED<[01] REPAIRED MAIN CABIN FLOOR PANEL 221GF FWD O/B FINGER CRACKED IAW B737-800 SRM 53-00-50-24-0.
Part: STRINGER CLIP — CRACKED (BS 500I S26R) · airframe 19,659 hrs · 9,956 cycles
FWD. CARGO AT STA. 500 I AT S26R; STRINGER CLIP CRACKED AS MARKED. DOT#S741<[01] REMOVED AND REPLACED NEW STRINGER CLIP INSTALLED IAW B737-800 SRM 51-40-02 AND BAC DWG 143A1234 REV -
Part: FLOOR PANEL — CORRODED (FWD CARGO) · airframe 19,659 hrs · 9,956 cycles
FWD. CARGO FLOOR BETWEEN STA.500A AND 500I AT S26R; R/H TRANSITION PANEL UPPER SURFACE HAS CORROSION AS MARKED. DOT #S735<[01] REPAIRED TRANS PNL. STA. 500A TO 500I RT. HD. IAW B737-800 SRM 53-00-53 REPAIR 5.;[02] VERIFIED REPAIRED TRANS PNL. STA. 500A TO 500I RT. HD. IAW B737-800 SRM 53-00-53 REPAIR 5.
Part: FLOOR SUPPORT — CORRODED (BS 500I) · airframe 19,659 hrs · 9,956 cycles
FWD. CARGO AFT BULKHEAD AT STA.500 I; FLOOR PANEL LATERAL SUPPORT HAS NUMEROUS CORROSION AS MARKED. DOT#S739<[01] REMOVED AND REPLACED FLOOR PANEL LATERAL SUPPORT IAW B737-800 SRM 51-40-02 AND BAC DWG 143A9481 REV -;[02] REMOVED AND REPLACED FLOOR PANEL LATERAL SUPPORT IAW B737-800 SRM 51-40-02 AND BAC DWG 143A9481 REV -
Part: ATTACH FITTING — CRACKED (BS 500H S26R) · airframe 19,659 hrs · 9,956 cycles
FWD. CARGO AT STA.500H AT S26R; FRAME ATTACH CLIP CRACKED AS MARKED. DOT#S742<[01] REMOVED AND REPLACED STA 500H S26R FRAME ATTACH CLIP PER B737-800 SRM 51-40-02 AND BAC DWG 143A7505 REV -;[02] VERIFIED REMOVED AND REPLACED STA 500H S26R FRAME ATTACH CLIP PER B737-800 SRM 51-40-02 AND BAC 143A7505 REV-
Part: MOUNT — CORRODED (BS 947) · airframe 19,659 hrs · 9,956 cycles
AFT WET AREA STA947 AFT L/H LAV INBD MOUNT STRUCTURE HAS CORROSION AFT WET AREA STA947 AFT L/H LAV INBD MOUNT STRUCTURE HAS CORROSION G335<[01] EVALUATED MOUNT STRUCTURE PER BOEING737-800 SRM 51-10-02 MOUNT STRUCTURE FOUND TO HAVE NO ED AT FASTENER HOLE WERE CORROSSION IS EVIDENT OF 50 PERCENT OF MATERIAL LOST REQUIRES TO BE REPLACED REMOVED MOUNT STRUCURE AND MOUNT AND INTERCOSTAL PER BOEING 737-800 SRM 51-40-02;[02] REMOVED AND REPLACED INTERCOSTAL PN: 147A5660U3 BN:461926 IAW B737-800 DWG: 147A5650 REV C; SRM 51-40-02;[03] VERIFIED ALL STEPS COMPLETE AND REMOVAL AND REPLACEMENT OF INTERCOSTAL PN: 147A5660U3 BN:461926 IAW B737-800 DWG: 147A5650 REV C; SRM 51-40-02
Part: FLOORBEAM — CORRODED (BS 787) · airframe 19,659 hrs · 9,956 cycles
AFT PIT TRANSVERSE FLOOR PANEL SUPPORT AT STATION 787 CORRODED<[01] REMOVED AND REPLACED FLOOR PANEL SUPPORT AT STA 727 PER B737-800 AMM 25-52-10 AND B737-800 SRM 51-40-02;[02] VERIFIED REMOVE AND REPLACE OF FLOOR PANEL SUPPORT AT STA 727 PER B737-800 AMM 25-52-10 AND B737-800 SRM 51-40-02
Part: FLOORBEAM — CORRODED (BS 727I) · airframe 19,659 hrs · 9,956 cycles
AFT PIT TRANSVERSE FLOOR PANEL SUPPORT AT STATION 727I CORRODED<[01] REMOVED AND REPLACED FLOOR PANEL SUPPORT AT STA 727I PER B737-800 AMM 25-52-10 AND B737-800 SRM 51-40-02;[02] VERIFIED REMOVE AND REPLACE OF FLOOR PANEL SUPPORT AT STA 727I PER B737-800 AMM 25-52-10 AND B737-800 SRM 51-40-02
Part: HANDLE — CRACKED (L2 DOOR) · airframe 19,659 hrs · 9,956 cycles
L2 AFT ENTRY DOOR FWD OF DOOR OPENING ASSIST HANDLE HAS CRACKED RETAINER<[01] INSTALLED L2 AFT ENTRY DOOR ASSIST HANDLE IAW B737 AMM 52-13-31-020-008;[02] VERIFIED INSTALL OF L-2 AFT ENTRY ASSIST HANDLE IAW B737 AMM 52-13-31-020-008
Part: BRACKET — CRACKED (LT WING) · airframe 19,659 hrs · 9,956 cycles
LEFT WING TRAILING EDGE SUPPORT BEAM AT DEFLECTION GUIDE CENTER ATTACH BRACKET BACK SIDE CRACKED. LEFT WING TRAILING EDGE SUPPORT BEAM AT DEFLECTION GUIDE CENTER ATTACH BRACKET BACK SIDE CRACKED<[01] 01 - REMOVED AND REPLACED PER [SRM 51-40-02-0G-0-B00069 (GENERAL - FASTENER INSTALLATION AND REMOVAL - AIRFRAME - PERMANENT)]<BR>FITTING PN: 115A2953-1 PO: 1075114.1;[02] VERIFIED REMOVED AND REPLACED PER [SRM 51-40-02-0G-0-B00069 (GENERAL - FASTENER INSTALLATION AND REMOVAL - AIRFRAME - PERMANENT)]<BR>FITTING PN: 115A2953-1 PO: 1075114.1
Part: SUPPORT — CRACKED (RT WING) · airframe 19,659 hrs · 9,956 cycles
R/H I/B UPPER FIXED TRAILING EDGE; PANEL SUPPORT CRACKED AT THE O/B EDGE OF UPPER FLANGE APPROX. WS 278.50. R/H I/B UPPER FIXED TRAILING EDGE PANEL SUPPORT CRACKED AT THE O/B EDGE OF UPPER FLANGE APPROX. WS 278.50.<[01] REMOVED AND REPLACED ANGLE PN: 115A2156-8 PO: 1083448.1 IAW B737-800 SRM 51-40-02 AND BAC DWG 115A2156 REV D.;[02] REMOVED AND REPLACED ANGLE PN: 115A2156-8 PO: 1083448.1 IAW B737-800 SRM 51-40-02 AND BAC DWG 115A2156 REV D.;[03] VERIFIED STEPS COMPLIED WITH
2023
Part: FLASHLIGHT — FAILED (ZN 200 FUS TOP) · airframe 18,175 hrs · 9,098 cycles
FORWARD ENTRY EMERGENCY FLASHLIGHT WILL NOT TEST<[01] R AND R'D FWD INBD EMER FLASHLIGHT ASSY PER AMM 25-64-00 OPS CHECK GOOD.
Part: SLIDE — OUT OF ADJUST (ZN 200 FUS TOP) · airframe 16,970 hrs · 8,429 cycles
FORWARD SERVICE DOOR SLIDE FELL OUT<[01] INSTALLED SLIDE PER AMM 25-66-01
2022
Part: FLASHLIGHT — INOPERATIVE (PAX CABIN) · airframe 14,799 hrs · 7,187 cycles
AFT RIGHT FLASHLIGHT F.O. SIDE INOP. / [01] R & R AFT GALLEY O/B FLASHLIGHT REF AMM#25-64-00.
Part: BATTERY — FAULTY (AFT CABIN) · airframe 14,086 hrs · 6,779 cycles
AFT CABIN I/B FLASHLIGHT FLASHING RED / [01] REMOVED AND REPLACED BATTERY; REF AMM 25-64-00.FLASHLIGHT OPS CHECK NORMAL
2021
Part: COVER — MISSING (CABIN) · airframe 12,683 hrs · 5,970 cycles
FO SIDE AFT SERVICE DOOR; FRAME EMERGENCY EXIT SIGN MISSING. ; / [01] INSTALLED AFT SERVICE DOOR FRAME EMERGENCY EXIT LIGHT LENSE COVER PER AMM 33-51-01.
2020
Part: SEAL — OUT OF POSITION (HORIZONTAL STAB) · airframe 8,489 hrs · 3,785 cycles
LT. HORIZONTAL STAB AFT LOWER SLIDING SEAL OUT OF CHANNEL / REMOVED AND RE-INSTALLED SEAL IAW AMM 20-50-11. INSPECTOR H46
Part: SEAL — OUT OF POSITION (HORIZONTAL STAB) · airframe 8,489 hrs · 3,785 cycles
RT. HORIZONTAL STAB AFT LOWER SLIDING SEAL OUT OF CHANNEL / REMOVED SEAL IAW AMM 20-50-11. INSPECTOR H46
2018
Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 1,647 hrs · 702 cycles
FORWARD EMERGENCY FLASHLIGHT OUTBOARD INOP. R&R FLASHLIGHT PER MM.
Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 720 hrs · 322 cycles
LT FORWARD FLASHLIGHT INOP. R&R FLASHLIGHT PER AMM.
Part: SIGN — DETACHED (OVERWING) · airframe 219 hrs · 97 cycles
EXIT SIGN AT OVERWING FELL OFF. SECURED THE SIGN IAW AMM.