N8722L
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.
42 reports on file, 2019-02-06 – 2026-08-11.
Part: WINGLET — DELAMINATED (ZONE 600) · airframe 18,763 hrs · 9,180 cycles
DELAMINATION ON RIGHT LOWER WINGLET STRAKE, OK TO CONTINUE IAW TLD IAW SRM 57-30-01. FOUND DAMAGE ON FWD RT WING STRAKE L/E APPROX 39 INCHES BELOW FWD POSITION LIGHT. DAMAGE WIDTH IS 1.5 INCHES AND LENGTH DAMAGE IS 1.5 INCHES. SPEED TAPE APPLIED REINSPECT EVERY 8 DAYS. PERMANENT REPAIR REQUIRED IN 730 DAYS.
Earlier reports · 2019–2025 · 41 reports
2025
Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 15,937 hrs · 7,749 cycles
COCKPIT EMERGENCY FLASHLIGHT LOW BATTERY. R & R COCKPIT EMERGENCY FLASHLIGHT BATTERY PER AMM 25-64-00
Part: MEGAPHONE — INOPERATIVE (ZONE 200) · airframe 15,375 hrs · 7,452 cycles
AFTER GALLEY MEGAPHONE INOP; NEAR L2 DOOR. REMOVED. REPLACED, AND INSPECTED AFT GALLEY MEGAPHONE PER AMM 25-64-00-SWA-806-MAX-1. OK FOR SVC.
Part: LENS — LOOSE (ZONE 200) · airframe 15,346 hrs · 7,435 cycles
PASSENGER CABIN CEILING; OVER WING EXIT ASSEMBLY IS MISSING LENS COVERS. INSTALLED 2X EXIT SIGN ACCESS COVER PLATES TO MID CABIN OVERHEAD EXIT LIGHT ASSY IAW AMM 33-51-01-960-802 STEP: 3. E. (2) (F).
Part: LENS — MISSING (ZONE 200) · airframe 15,346 hrs · 7,435 cycles
PASSENGER CABIN CEILING; OVER WING EXIT ASSEMBLY IS MISSING LENS COVERS. INSTALLED 2X EXIT SIGN ACCESS COVER PLATES TO MID CABIN OVERHEAD EXIT LIGHT ASSY IAW AMM 33-51-01-960-802 STEP: 3. E. (2) (F).
Part: LENS — MISSING (ZONE 200) · airframe 14,286 hrs · 6,902 cycles
AFTER GALLEY EXIT SIGN LENS MISSING. REMOVED AND REPLACED PER [AMM INTRODUCTION-MAX (USE OF STANDARD INDUSTRY PRACTICES - SIP - PERMANENT)]
2024
Part: BATTERY PACK — FAILED (ZONE 200) · airframe 12,626 hrs · 6,040 cycles
FOUND LH DATO PANEL OPENED FOR EMERGENCY LIGHT BATTERY REPLACEMENT / TROUBLESHOOTING AT SEAT ROW 8 ABC.<[01] ACCOMPLISHED ON WORK CARD TTG8Q00VY3TT; IAW AMM 33-51-06-960-802;[02] VERIFIED ITEM 1.
Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 12,626 hrs · 6,040 cycles
FOUND RH DATO PANEL OPENED FOR EMERGENCY LIGHT BATTERY REPLACEMENT / TROUBLESHOOTING AT SEAT ROW 8 DEF.<[01] ACCOMPLISHED ON WORK CARD TTG8Q00VY3TM; IAW AMM 33-51-06-960-802;[02] VERIFIED ITEM 1
Part: BATTERY PACK — FAILED (ZONE 200) · airframe 12,626 hrs · 6,040 cycles
FOUND LH DATO PANEL OPENED FOR EMERGENCY LIGHT BATTERY REPLACEMENT / TROUBLESHOOTING AT SEAT ROW 14 ABC.<[01] ACCOMPLISHED ON WORK CARD TTG8Q00VY3TT; IAW AMM 33-51-06-960-802;[02] VERIFIED ITEM 1.
Part: BATTERY PACK — FAILED (ZONE 200) · airframe 12,626 hrs · 6,040 cycles
EMERGENCY LIGHT BATTERY PACK (M2335) FAILS TO CHARGE (STA 500C+7 LBL 67)<[01] REPLACED EMERGENCY LIGHT BATT PACK M2335 IAW AMM 33-51-06-960-802. TESTS GOOD;[02] VERIFIED ITEM 1.
Part: BATTERY PACK — FAILED (ZN 200 FUS TOP) · airframe 12,626 hrs · 6,040 cycles
EMERGENCY LIGHT BATTERY PACK (M2816) FAILS TO CHARGE (STA 30 RBL 6)<[01] REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK (M2816) IAW BOEING AMM 33-51-06-960-802;[02] VERIFIED ITEM 1<BR><BR>AUDIT C/W
Part: BATTERY PACK — FAILED (ZONE 200) · airframe 12,626 hrs · 6,040 cycles
EMERGENCY LIGHT BATTERY PACK (M1676) FAILS TO CHARGE (STA 500C+7 RBL 67)<[01] REPLACED M1676 BATTERY PACK IAW AMM 33-51-06-960-802. OPS CHECK GOOD<BR>WN47858;[02] VERIFIED ITEM 1.
Part: BATTERY PACK — FAILED (ZN 200 FUS TOP) · airframe 12,626 hrs · 6,040 cycles
EMERGENCY LIGHT BATTERY PACK (M1675) FAILS TO CHARGE (STA 317 LBL 10)<[01] REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK (M1675) IAW BOEING AMM 33-51-06-960-802;[02] VERIFIED ITEM 1<BR><BR>AUDIT C/W
Part: SUPPORT ANGLE — CORRODED (ZONE 100) · airframe 12,626 hrs · 6,040 cycles
AFT CARGO COMPARTMENT FWD SHIELD SUPPORT ANGLE IS CORRODED ON LOWER SURFACE. STA 767-787 RBL 22 AT WL 155<[01] EVALUATED ALLOWABLE LIMITS: .050 ORIG 'T' .033 REMAINING .017 LOSS FOUND OUT OF LIMITS IAW SRM 53-60-15-1A-1 TOOL USED MIC #AAR 1714 DUE 10/11/2 REMOVED AND REPLACED ANGLE IAW SRM 51-40-02-0G-0 AND DWG 146A0081 REV:A;[02] AUDIT C/W
Part: SHIELD — CORRODED (ZONE 100) · airframe 12,626 hrs · 6,040 cycles
(A204 DOT 52) AFT CARGO STA 767 TO 787; RBL 22; WL 155; SPLASH SHIELD UPPER AND LOWER SURFACE HAS CORROSION.<[01] EVALUATED BLEND OUT AND FOUND TO BE OUT OF ALLOWABLE DAMAGE LIMITS<BR>IAW B737 SRM 53-60-15-1A-1 STEP 4.G.(2)(B); FIGURE 103 DETAIL G. AND REMOVED AND REPLACED PART IAW SRM 51-40-02-0G-0 AND DWG 146A0081-REV:A;[02] AUDIT C/W
Part: ANGLE — CORRODED (ZONE 100) · airframe 12,626 hrs · 6,040 cycles
(A204 DOT 60) AFT CARGO; STA 727J TO 847; LBL 22; WL 155; Z-ANGLE HAS CORROSION<[01] DAMAGED ZEEZ CHANNEL SIDEPLATE SECTION FROM STA 727 E+9 THRU STA 847 WAS FOUND TO BE OUT OF LIMITS; REMOVED; FABRICATED A NEW SECTION AND REPLACED I.A.W. SRM 53-00-53-2R-5 AND BOEING DWG 146A7500;[02] AUDIT C/W
Part: ANGLE — CORRODED (ZONE 100) · airframe 12,626 hrs · 6,040 cycles
(A204 DOT 56) AFT CARGO; STA 727E TO 727I; RBL 22; WL 155; Z-ANGLE HAS CORROSION<[01] 01 - REMOVED DAMAGE; EVALUATED AND FOUND TO BE WITHIN ALLOWABLE DAMAGE LIMITS PER [SRM 53-00-53-1A-2-D00297 (PERMANENT (NON-DENT DAMAGE TYPES))];[02] VERIFIED STEP 1<BR>AUDIT CW
Part: ANGLE — CORRODED (ZONE 100) · airframe 12,626 hrs · 6,040 cycles
(A204 DOT 58) AFT CARGO; STA 727B TO 727F; LBL 22; WL 155; Z-ANGLE HAS CORROSION<[01] FAULT RESOLVED ON OTHER FAULT. SEE FAULT TTG8Q00VQ3WJ FOR THE REPLACEMENT OF LH ZEE ANGLE ASSEMBLY STA 727 E+9 THRU STA 847;[02] AUDIT C/W
Part: ANGLE — CORRODED (ZONE 100) · airframe 12,626 hrs · 6,040 cycles
(A204 DOT 55) AFT CARGO; STA 727I TO 767; RBL 22; WL 155; Z-ANGLE HAS CORROSION<[01] 04 - REPAIRED ZEE CHANNEL SIDEPLATE BETWEEN STA 727I -11.000 IN. TO STA 767 AT RBL 22 AND WL 155 PER [SRM 53-00-53-2R-5-D00308 (REPAIR 5 - CARGO COMPARTMENT SIDEPLATE REPAIR BETWEEN FLOOR PANEL SPLICES - PERMANENT)];[02] VERIFIED STEP 1<BR>AUDIT CW
Part: ANGLE — CORRODED (ZONE 100) · airframe 12,626 hrs · 6,040 cycles
(A204 DOT 59) AFT CARGO; STA 727F TO 727J; LBL 22; WL 155; Z-ANGLE HAS CORROSION<[01] FAULT RESOLVED ON OTHER FAULT. SEE FAULT TTG8Q00VQ3WJ FOR THE REPLACEMENT OF LH ZEE ANGLE ASSEMBLY STA 727 E+9 THRU STA 847;[02] AUDIT C/W
Part: ANGLE — CORRODED (ZONE 100) · airframe 12,626 hrs · 6,040 cycles
DOT #114-013. FORWARD CARGO COMPARTMENT; RIGHT SIDE Z ANGLE HAS SEVERAL AREAS OF LIGHT CORROSION BETWEEN STA. 500A - 500E.<[01] REPAIRED Z ANGLE DAMAGE SECTION AREA AT STA 500A-500E IAW SRM 53-00-53-2R-5;[02] AUDIT C/W
Part: FLOOR PANEL — CORRODED (ZONE 100) · airframe 12,626 hrs · 6,040 cycles
FWD CARGO FLOOR PANEL 120AF HAS CORROSION AT FASTENER HOLES<[01] RECEIVED REPLACEMENT MATERIAL PN 2024-T3-071 A TAG A254110 AND VERIFIED IT TO BE CORRECT REPLACEMENT MATERIAL IAW SRM 53-60-53-0I-1 FABRICATED PANEL 120AF IAW AMM 50-10-04-400-801 TREATED AND PRIMED PANEL IAW SRM 51-20-01-0G-0 AND PLACED PANEL IN RACK;[02] VERIFIED ITEM 1<BR>C/W
Part: FLOOR PANEL — CORRODED (ZONE 100) · airframe 12,626 hrs · 6,040 cycles
FWD CARGO FLOOR PANEL 120CF HAS CORROSION AT FASTENER HOLES<[01] FABRICATED NEW FLOOR PANEL 120CF I.A.W SRM 53-30-53-0I-1 AND AMM 50-10-04-400-801 AND APPLIED ALODINE AND PRIMER I.A.W AMM 51-21-41-701 AND AMM 51-21-72-701;[02] AUDIT C/W
Part: FLOOR PANEL — CORRODED (ZONE 100) · airframe 12,626 hrs · 6,040 cycles
FWD CARGO FLOOR PANEL 120BF HAS CORROSION AT FASTENER HOLES<[01] RECEIVED REPLACEMENT MATERIAL PN 2024-T3-071 A TAG A254110 AND VERIFIED IT TO BE CORRECT REPLACEMENT MATERIAL IAW SRM 53-30-53-0I-1 FABRICATED PANEL 120BF IAW AMM 50-10-04-400-801 TREATED AND PRIMED IAW SRM 51-20-01-0G-0 AND PLACED ON PANEL RACK;[02] AUDIT C/W
Part: FLOOR PANEL — CORRODED (ZONE 100) · airframe 12,626 hrs · 6,040 cycles
AFT CARGO FLOOR PANEL 140DF HAS CORROSION AT FASTENER HOLES<[01] RECEIVED REPLACEMENT MATERIAL PN 2024-T3-071 A TAG A255451 AND VERIFIED TO BE CORRECT REPLACEMENT MATERIAL IAW SRM 53-60-53-0I-1 FABRICATED PANEL 140DF IAW AMM 50-10-04-400-801 TREATED AND PRIMED IAW SRM 51-20-01-0G-0 AND PLACED ON PANEL RACK;[02] AUDIT C/W.
Part: SCUFF PLATE — CRACKED (ZONE 100) · airframe 12,626 hrs · 6,040 cycles
AFT CARGO DOOR AFT CORNER SCUFF PLATE IS CRACKED<[01] AFT CARGO DOOR AFT CORNER SCUFF PLATE WAS REPAIRED ON BACKSHOP W/O 45948/1000/0001 SERIAL NO. 9376843 SHOP WELD IAW SRM 53-60-15-2R-1;[02] VERIFIED ITEM 1<BR>C/W
Part: FLOOR PANEL — CORRODED (ZONE 100) · airframe 12,626 hrs · 6,040 cycles
AFT CARGO FLOOR PANEL 140AF HAS CORROSION AT FASTENER HOLES<[01] UPON FURTHER INVESTIGATION FOUND THAT CORROSION WAS 30 INCHES IN LENGTH WITH A MAX ALLOWED LENGTH OF 3 INCHES FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-1;RECEIVED REPLACEMENT MATERIAL PN 2024-T3-071 A TAG A255451 AND VERIFIED TO BE CORRECT REPLACEMENT MATERIAL IAW SRM 53-60-53-0I-1;FABRICATED PANEL 140AF IAW AMM 50-10-04-400-801;TREAT AND PRIME IAW SAM 51-20-01-0G-0;[02] VERIFIED ITEM 1<BR><BR>AUDIT C/W
Part: FLOOR PANEL — CORRODED (ZONE 100) · airframe 12,626 hrs · 6,040 cycles
AFT CARGO FLOOR PANEL 140BF HAS CORROSION AT FASTENER HOLES<[01] 01 - REMOVED AND REPLACED PER [AMM 50-10-04-401-MAX (CARGO COMPARTMENT FLOOR PANEL - REMOVAL/INSTALLATION - PERMANENT)];[02] VERIFIED STEP 1<BR>AUDIT CW
Part: FLOOR PANEL — CORRODED (ZONE 100) · airframe 12,626 hrs · 6,040 cycles
AFT CARGO FLOOR PANEL 140EF HAS CORROSION AT FASTENER HOLES<[01] FABRICATED NEW FLOOR PANEL 140EF I.A.W AMM 50-10-04-400-801 AND APPLIED ALODINE AND PRIMER I.A.W <BR>AMM 51-21-41-701 AND AMM 51-21-72-701;[02] VERIFIED STEP 1.<BR>AUDIT C/W.
Part: FLOOR PANEL — CORRODED (ZONE 100) · airframe 12,626 hrs · 6,040 cycles
AFT CARGO FLOOR PANEL 140CF HAS CORROSION AT FASTENER HOLES<[01] REMOVED DAMAGE/CORROSION WAS OUT OF LIMITS ;FABRICATED NEW AFT CARGO FLOOR PANEL 140CF I/A/W AMM 50-10-04-400-801;[02] VERIFIED STEP 1<BR>AUDIT CW
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 12,029 hrs · 5,757 cycles
FWD OVER WING EXIT LIGHT EXTERNAL POSITION INOP<[01] REMOVED AND REPLACED BATTERY PACK M1670 R/H SIDE IAW AMM 33-51-06 OPS CHECK GOOD
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 12,029 hrs · 5,757 cycles
R/H OVER WING EXIT LIGHT AFT EXTERNAL POSITION INOP<[01] REMOVED AND REPLACED R/H BATTERY PACK M1671 IAW AMM 33-51-06 OPS CHECK GOOD
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 12,029 hrs · 5,757 cycles
AFT ENTRY DOOR EMERGENCY EXIT EXTERNAL LIGHT INOP<[01] REMOVED AND REPLACED AFT BATTERY PACK M1673 IAW AMM 33-51-06 OPS CHECK GOOD
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 12,011 hrs · 5,747 cycles
FWD AND AFT CABIN EMERGENCY LIGHTS INOP<[01] REMOVED AND REPLACED FORWARD AND AFT EMERGENCY LIGHTS BATTERY PACK REF AMM 33-51-06
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 10,967 hrs · 5,226 cycles
L/H FWD ENTRY DOOR EMERGENCY LIGHTS INOP<[01] REMOVED AND REPLACED BATTERY PACK M1675 BATTERY PACK IAW AMM 33-51-06 OPS CHECK GOOD
2023
Part: FLASHLIGHT — INOPERATIVE (ZN 200 FUS TOP) · airframe 8,880 hrs · 4,116 cycles
CAPT SIDE EMERGENCY FLASHLIGHT TEST FUNCTION INOP BUT FLASHLIGHT WORKS<[01] R&R CAPTAIN SIDE EMERGENCY FLASHLIGHT MOUNTING BRACKET; PERFORMED OPS TEST IAW AMM 25-64-00. OPS TEST GOOD.
2022
Part: BATTERY — FAILED (ZN 900 LAV/GALLE) · airframe 6,584 hrs · 3,013 cycles
SUPPLEMENTAL INFORMATION: FLIGHT DECK FLASHLIGHT TEST FAIL / [01] OK TO CONT PER MEL 25-64-02 SP1B A#10066;[02] REMOVED AND REPLACED FLIGHT DECK FLASHLIGHT BATTERY PER AMM 25-64-00
Part: FLASHLIGHT — FAULTY (AFT CABIN) · airframe 5,746 hrs · 2,623 cycles
AFT RT FLT ATTENDANT SEAT INBD FLASHLIGHT WONT TEST. / [01] OK TO CONTINUE PER MEL 25-64-02. SP#1B;[02] R&R AFT RH FA SEAT INBD FLASHLIGHT & BATTERY PER MM 25-64-00
Part: BATTERY — FAULTY (AFT CABIN) · airframe 5,746 hrs · 2,623 cycles
AFT RT FLT ATTENDANT SEAT INBD FLASHLIGHT WONT TEST. / [01] OK TO CONTINUE PER MEL 25-64-02. SP#1B;[02] R&R AFT RH FA SEAT INBD FLASHLIGHT & BATTERY PER MM 25-64-00
Part: FLASHLIGHT — LOOSE (FWD CABIN) · airframe 5,627 hrs · 2,574 cycles
FWD INBD F/A FLASHLIGHT DOES NOT TEST / [01] RESECURED INBOARD FA FLASHLIGHT TO HOLDER IAW AMM 25-64-00. OPS CHECK GOOD.
Part: FLASHLIGHT — BROKEN · airframe 5,140 hrs · 2,366 cycles
FWD FA FLASHLIGHT SEAL BROKEN / [01] INSTALLED NEW SEAL ON FWD FA FLASHLIGHT PER SIP
2019
Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 1,219 hrs · 543 cycles
FORWARD INBOARD POSITION EMERGENCY FLASHLIGHT INOP. R&R FLASHLIGHT ASSEMBLY PER AMM.