N8059A
Registered owner: BANK OF UTAH 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
DURING FLIGHT FO REMOVED WINDOW SHADE FROM R1 AND IT CREATED SPARKS AND A LITTLE BIT OF SMOKE. RAN QRH, LEFT THE HEAT OFF FOR THAT WINDOW. CB DID NOT POP. INSPECTED FO WINDOW IAW AMM 56-11-00. NO DEFECTS NOTED AND PERFORMED WINDOW HEAT SYSTEM OPS TEST IAW AMM 30-41-00-710-801. OPS TEST NORMAL.
DURING FLIGHT FO REMOVED WINDOWSHADE FROM R1. THE R1 WINDOW THREW SPARKS AND TRIPPED CB. FOLLOWED QRH, DID NOT RESET CB. MX NOTIFIED. INSPECTED R1 WINDOW PER AMM 56-11-00-200-803, NO DEFECTS NOTED. RESET CB ON P6-12 B25 ACCCOMPLISHED WINDOW HEAT CONTROL UNIT BITE REF FIM 30-41 TASK 801 AND WINDOW HEAT OPS TEST REF AMM 30-41-00-710-801. OPS CHECKS GOOD.
DUE TO HISTORY OF LEFT MAIN LANDING GEAR STRUT LEAK- PERFORM REPLACEMENT OF THE ACTIVE AND SPARE SEALS IAW AMM 32-11-21-960-802. REMOVED AND REPLACED LT MAIN MANDING GEAR IAW CC 320400100.
L1 DOOR ESCAPE SLIDE GIRT BAR PROTRUDING ON AFT SIDE. PERFOREMED ESCAPE SLIDE PACK CHECK IAW AMM 25-66-01-200-802. NO DEFECTS NOTED.
WORK ORDER 866652, NR0514: EMERGENCY LIGHTS AT R1 DOOR ARE INTERMITTENT. - RESOLUTION (INPROGRESS)
L1 DOOR EMERGENCY LIGHTS ARE INOP. REMOVED AND REPLACED ABTTERY PACK M1675 PER B737 AM 33-51-06-960-801, OPS CHECK GOOD.
RIGHT HOR. STAB AFT BOTTOM ATTACHMENT BUSHING CRACKED. UNABLE TO CONFIRM WHETHER IF BUSHING IS A SHRINKFIT OR FORCEMENT & P/N IS UNAVAILABLE PER EAR #12 RESPONSE STEP 1. PERFORMED A DVI IAW SRM 51-10-04-0G-0 REV 23 10MAR2025, GOUGE (POSSIBLE) CRACK NOTED AT DEFEC AREA. PER EAR #12 RESPONSE STEP 2. REMOVED 2EA AFFECTED BUSHING ONTO RH HORIZ. STAB. REAR SPAR LOWER LUG IAW EAR #12, EA#737-5510-72-B0424 P1 STEP 2 AND BOEING SB 737-55-1074 FI 7 AND FIG 10 PART A STEP 1. PERFORMED CLEANING ON LOWER LUG BORE, LUG FWD FACE AND AFT FACE AT HORIZ STAB REAR SPAR RH IAW EA#737-5510-72-B0424 P1 STEP 2 AND BOEING SB 737-55-1074 FIG. 10 PART A STEP 2 AND 3.
LEFT AFT HOR. STAB. MIDDLE BUSHING OUTER COATING DETERIORATED. UNABLE TO CONFIRM IF BUSHING IS SHRRINK FIT OR FORCEMATE P/N CANNOT BEE CONFIRMED PER ENG RESPOSE STEP 1. BUSHING MIGRATED SEALANT WAS BROKEN AROUND ENTIRE CIRCUMFRANCE. NO OTHRER DAMAGE FOUND DUING GVI PE SRM 51-10-04-0G-0 REV 23 ENG RESPONSE STEP 2B. REMOVED 2EA AFFECTEED BUSHING ONTO LH HORIZ STAB REAR SPAR UPPER LUG IAW EAER #10, EA 737-5510-72 B0423 REEV. P1 AND STEP 2 AND SB 737-55-1074 FIG. 7 AND FIG. 9 PART , STEP 1. PERFORMED CLEANING ON UPPER LLUG BOR AND LUG FWD FACE AND LUG AFT FACE AT HORIZONTAL STAB L/H REAR SPAR IAW EA #737-5510-72-B0423 REV. P1 STEP 2 AND BOEING SB 737-55-1074 PART A. STEP 2 AND 3.
LEFT AFT HORIZONTAL STAB UPPER AFT BUSHING MIGRATING. SAA034 027 - RESOLUTION: SUBMIT TO ENG. UNABLE TO CONFIRM IF BUSHING IS SHRRINK FIT OR FORCEMATE P/N CANNOT BEE CONFIRMED PER ENG RESPOSE STEP 1. BUSHING MIGRATED SEALANT WAS BROKEN AROUND ENTIRE CIRCUMFRANCE. NO OTHRER DAMAGE FOUND DUING GVI PE SRM 51-10-04-0G-0 REV 23 ENG RESPONSE STEP 2 B. REMOVED 2EA AFFECTEED BUSHING ONTO LH HORIZ STAB REAR SPAR UPPER LUG IAW EAER #10, EA 737-5510-72 B0423 REEV. P1 AND STEP 2 AND BOEING SB 737-55-1074 FIG. 7 AND FIG. 9 PART , STEP 1. PERFORMED CLEANING ON UPPER LUG BORE AND LUG FWD FACE AND LUG AFT FACE AT HORIZONTAL STAB L/H REAR SPAR IAW EA #737-5510-72-B0423 REV. P1 STEP 2 AND BOEING SB 737-55-1074 PART A. STEP 2 AND 3.
CENTER BOX LEFT AFT LOWER HOR. STAB HAS BUSHING CRACKED. UNABLE TO CONFIRM WHETHE IF BUSHING IS SHRINKFIT OR FORCEMENT & P/N IS UNAVALIABKE, PER EAR #5 RESPONSE STEP 1. PERFORMED A DVI, IAW SRM 51-10-04-0G-0 REV 23, GOUGE & CRAVK NOTED AT DEFECT AREA. PER EAR #5 RESPOSE STEP 2. REMOVED 4EA AFFECTED BUSHING ONTO LHS HOR. STAB CENTER SEC SPAR LOWER CLEVIS FWD LUG AND AFT LUG IAW EA #737-5510-72-B0423 REV. P1 STEP 2 AND BOEING 5B 737-55-1074 FIG. 15 PART A STEP 1. PERFORMED CLEANING ON LOWER CLEVIS FWD LUG AND AAFT LUG AT LHSS HOR. STAB CENTER SEC. REAR SPAR IAW EA# 737-5510-72-B0423 REV. P1 STEP 2 AND BOEING SB 737-55-1074 FIG. 15 PART A STEP 2.
ON CENTER BOX LEFT AFT LOWER HOR. STAB HAS BUSHING CRACKED. UNABLE TO CONFIRM WHETHE IF BUSHING IS SHRINKFIT OR FORCEMENT & P/N IS UNAVALIABKE, PER EAR #5 RESPONSE STEP 1. PERFORMED A DVI, IAW SRM 51-10-04-0G-0 REV 23 10MAR2025, GOUGE & CRAVK NOTED AT DEFECT AREA. PER EAR #5 RESPOSE STEP 2. REMOVED 4EA AFFECTED BUSHING ONTO LHS HOR. STAB CENTER SEC SPAR LOWER CLEVIS FWD LUG AND AFT LUG IAW EA #737-5510-72-B0423 REV. P1 STEP 2 AND BOEING 5B 737-55-1074 FIG. 15 PART A STEP 1. PERFORMED CLEANING ON LOWER CLEVIS FWD LUG AND AAFT LUG AT LHSS HOR. STAB CENTER SEC. REAR SPAR IAW EA# 737-5510-72-B0423 REV. P1 STEP 2 AND BOEING SB 737-55-1074 FIG. 15 PART A STEP 2.
AIRCRAFT TAIL SECTION, RIGHT HAND HORIZONTAL STABILIZER, THE FORWARD LOWER MOUNT FORWARD BUSHING HAS A GOUGEON THE AFT SIDE AT THE THREE O CLOCK POSITION. (120-110) RESOLUTION: SUBMIT TO ENG. REMOVED THE RH FRONT FWD LWR BUSHING, IAW EAR#08 RESPONSE STEP 1, PER SB 737-55-1074 REV 2: JULY 21, 2017. PERMANENT REPAIR - PART 3. INSPECTED THE JOINT, IAW EAR#08 RESPONSE STEP 2, PER SB 737-55-1074 REV 2: JULY 21, 2017. PART 3. PERMANENT REPAIR, STEP 13. CORROSION NOTED. ACCOMPLISHED FILLING THE REPORT FORM FOR AFFECTED JOINT AS PER 737-NG-FTD-55-13002, JOINT DIMENSIONS REPORT. IAW EAR#08 RESPONSE STEP 2 & 4. REMOVED CORROSION FROM THE FWD AND AFT FACES OF THE LWR AND UPPER CLEVIS ON THE RH SIDE FWD MOUNT OF THE HORIZONTAL STABILIZER BY SPOT FACING AND CHAMFERING THE AFFECTED AREA IAW BOEING SB 737-55-1074 FIG.12 REV.2 DATED 21JUL2017 AND EAR #8.
DEFECT 794687: ESCAPE SLIDE FELL OUT OF L1 DOOR WHILE CLOSING DOOR. RESOLUTION: REINSTALLED L1 SLIDE IAW AMM 25-66-01 ESCAPE SLIDE.
DEFECT 723485: 3R WINDOW SPARKS AND ARCHING OBSERVED ON THERMAL SWITCH. - - RESOLUTION: FOUND EVIDENCE OF R3 THERMAL SWITCH IMPROPERLY SEATED INTO CLIP AND CAUSED ARCHING RESEATED THERMAL SWITCH REF AMM 30-41-31 AND OPS CHECK GOOD THIS CLEARS MEL 30-11-4 MDDR # 127486
DEFECT 777757: DOOR L1 GIRT BAR RETENTION HOOK WONT HOLD. - - RESOLUTION: ALIGNED STOP ASSEMBLY IAW AMM 25-66-01. OPS CHECK GOOD.
ON DECENT FLAPS LOCKED OUT NEAR ZERO WITH SLIGHT ASYMETRY OF 1/8" ON FLAP INDICATOR. USED ALERNATE FLAP EXTENTION AND LE FLAPS EXTENDED. (EMERGENCY DECLARED ) - RESOLUTION: FOUND FAULT CODE 27-53254. REPLACED #5 & #6 SKEW SENSO ON RIGHTHAND WING. CHECK WIRES AND CANNON. ALL OK PER FIM 27-59-805 & AMM 27-59-01-000-804. FLAPS OPERATE NORMAL WITH NO SPLITS.
DEFECT 767080 - - - AIRCRAFT DID NOT PRESSUREIZE AFTER TAKEOFF. - - - RESOLUTION - FOUND L1 DOOR NOT COMPLETLY SEALED WHEN CLOSED PERFORMED L1 DOOR SYSTEM TEST IAW 52-11-00-700-804 OPS CHECK GOOD.
DEFECT TC 203750000 NR 00117: CORROSION AFT CARGO LH ZEE CHANNEL STA 727 TO STA 867 STR 25L RESOLUTION: CORROSION ON ZEE CHANNEL FROM STA 727 TO STA 867, STR 25L AT AFT CARGO FOUND IT TO BE OUT OF LIMITS, REMOVED AND REPLACED AND APPLIED FINAL REFINISHED PER B737-800 SRM 53-00-53-1A-2 SRM 53-0053-2R-5 AND DWG # 146A7500 REV A.
DEFECT TC 203750000 NR0004: FWD CARGO BAY, RH AFT AFT SHIELD HAS SEVERAL COORODED FASTENER HOLES RESOLUTION: REMOVED, FABRICATED AND INSTALLED NEW FWD CARGO RH SHIELD AFT CARGO DOOR IAW SRM 51-40-02-0G-0 LOT# 5127013-1 ITEM HFAB53-RP-011.
DEFECT TC 203350000 NR00005: FWD CARGO BAY, RH Z CHANNEL HAS SEVERAL CORRODED FASTENER HOLES FROM STA 500A-500I. RESOLUITION: REPAIRED FWD CARGO BAY RH ZEE CHANNEL FROM STA 500A-500I IAW B737 SRM 51-40-02-0G, SRM 53-00-53-2R-5 REPAIR 5 AND DWG 143A7500.
DEFECT TC203750000 NR00120: CORROSION AFT CARGO DOOR SURROUND SUB THRESHOLD WEB. RESOLUTION: REMOVED AND REPLACED AFT CARGO DOOR SURROUND SUB THRESHOLD WEB IAW 51-40-02-0G-0 AND BOEING DWG 146A5120
DEFECT NR00204: UPON REMOVAL OF AFT CARGO DOOR SURROUND FORWARD SHIELD, FOUND CORROSION ON INTERSCOSTAL STA 787-794 STR 25R RESOLUTION: REMOVED AND REPLACED DAMAGED INTERCOSTAL STA 787-794 STR 25 IAW B737 SRM 51-40-02-0G-0 AND BOEING DWG 146A8320 REV A.
DEFECT TC 203750000 NR00169: CORROSION AFT CARGO RH AFT ZEE CHANNEL STA 867 TO STA 887 STR 25R. RESOLUTION: R/R NEW ZEE CHANNEL FROM STA 867 TO STA 887 STR 25R PER B737 SRM 51-40-02 AND DWG # 146A7500 REV A.
DEFECT TC 203750000 NR00170: CORROSION AFT CARGO RH AFT ZEE CHANNEL STA 887 TO STA 947 STR 25R. RESOLUTION: R/R NEW ZEE CHANNEL AT BSTA 887 TO BSTA 947 STR 25R PER B737-800 51-40-02, DWG 147A7500 REV A.
DEFECT TC 203750000 NR00166: CORROSION AFT CARGO RH ZEE CHANNEL STA 727 TO STA 767 STR 25R. RESOLUTION: REMOVED DAMAGED AFT CARGO RH ZEE FROM STA 737 TO 767 STR 25R PER BOEING 737 51-40-02-0G-0 REV 16 AND INSTALLED A NEW ZEE CHANNEL LOT # 5093502-1 PER BOEING 737 51-4002-0G-0 REV 16 AND DWG # 146A7502 REV-
DEFECT TC 203350000 NR00142: CORROSION IOON FWD CARGO BAFFLE BS 500C TO 500D LBL 25 WL 156. RESOLUTION: REMOVED AND REPLACED BAFFLE BS 500C TO 500D LBL 25 WL 156 ON FWD CARGO IAW B737 SRM 51-40-02-0G-0 AND DWG 143A7505.
DEFECT TC 203350000 NR00143: CORROSION ON FWD CARGO BAFFLE BS 500D TO 500E LBL 25 WL 156. RESOLUTION: REMOVED AND REPLACED BAFFLE BS 500D TO 500E LBL 25 WL 156 IAW B737 SRM 51-40-02-0G-0 AND DWG 143A7505.
DEFECT TC 203350000 NR 00147: CORROSION ON FWD CARGO BAFFLE BS 500H TO 500I LBL 25 WL 156. RESOLUTION: REMOVED AND REPLACED BAFFLE BS 500H TO 500I LBL 25 WL 156 IAW SRM 51-40-02-0G-0 AND DWG 143A7505.
DEFECT TC 203350000 NR00146: CORROSION ON FWD CARGO BAFFLE BS 500G TO 500H LBL 25 WL 156. RESOLUTION: REMOVED AND REPLACED BAFFLE BS 500G - 500H LBL 25 WL 156 IAW B737 SRM 51-40-02-0G.
DEFECT TC 206200000 NR00128: EVIDENCE OF CORROSION ON RH WING REAR SPAR AROUND AFT BOOST PUMP #2 RESOLUTION: CORROSION FOUND IN 2 EA AREAS AT AFT BOOST PUMP #2, RH WING REAR SPAR UPPER AREA MEASURES 3.25"L X 2.5" W X 0.046"D, LOWER AREA MEASURES 4.5"L X 3.5"W X 0.081"D BOTH AREAS FOUND IN LIMITS PER SRM 57-20-10-1A-3#5.D, FIGURE 105, PERFORMED FLAP PEEN AND APPLIED PROTECTIVE FINISHES PER SRM 57-20-10-1A--3, #2.C.(3,4 AND 6)
DEFECT TC 203350000 NR00148: CORROSION ON FWD CARGO BAFFLE CLIP BS 500C FWD SIDE FRAME LBL 25 WL 156. RESOLUTION: REMOVED AND REPLACED BAFFLE CLIP BS 500D FWD SIDE OF FRAME LBL 25 WL 156 IAW B737 SRM 51-40-02-0G-0 AND DWG 143A7505.
DEFECT TC 203350000 NR00157: FWD CARGO COMPARTMENT BAFFLE CLIP AT BS 500E LBL25 WL 156 FWD SIDE OF FRAME CRAKCED. RESOLUTION: R/R BAFFLE CLIP AT BS 500E LBL25 WL 156 FWD SIDE OF FRAME IAW SRM 51-40-02-0G-0 AND DWG 143A7505.
DEFECT TC 203350000 NR00144: CORROSION ON FWD CARGO BAFFLE BS 500E TO 500F LBL 25 WL 156. RESOLUTION: R/R BAFFLE BS 500E - 500F LBL 25 WL 156 IAW B737 SRM 51-40-02-0G.
DEFECT TC206200000 NR00128: EVIDENCE OF CORROSION ON RH WING REAR SPAR AROUND AFT BOOST PUMP #2. RESOLUTION: CORROSION FOUND IN 2 EA AREAS AT AFT BOOST PUMP #2, RH WING REAR SPAR UPPER AREA MEASURES 3.25"L X 2.5"W X .046"D, LOWER AREA MEASURES 4.5"L X 3.5"W X .081"D. BOTH AREAS FOUND IN LIMITS PER SRM 57-20-10-1A-3, #5.D, FIGURE 105. PERFORMED FLAP PEEN AND APPLIED PROTECTIVE FINISHES PER SRM 57-20-10-1A-3, #2.C. (3,4 AND 6) THERE WAS NO PART REPLACEMENT, ONLY THE BLENDOUTS.
DEFECT TC 203350000 NR00108: FWD CARGO BAY, LH SIDEPLATE "Z" CHANNEL HAS SEVERAL CORRODED FASTENER HOLES FROM STA 500D - 500I (MARKED). RESOLUTION: CORROSION ON FWD CARGO BAY, LH SIDEPLATE "Z" CHANNEL FOUND OUT OF LIMITS PER SRM 53-00-53-1A-2, #4.A.2.D REMOVED AND REPLACED DAMAGE ZEE CHANNEL PER DWG # 143A7500 AND SRM 51-40-02-0G-0 WITH SERVICEABLE REPLACEMENT.
DEFECT TC 203350000 NR00134: CORROSION ON FWD CARGO BAFFLE BS 500G - 500H RBL 25 WL 156. RESOLUTION: R/R BAFFLE BS 500G - 500H RBL 25 WL 156 IAW B737 SRM 51-40-02-0G.
DEFECT TC 203350000 NR00132: CORROSION ON FWD CARGO BAFFLE BS 500E - 500F RBL 25 WL 156. RESOLUTION: R/R BAFFLE BS 500E - 500F RBL 25 WL 156 IAW B737 SRM 51-40-02-0G.
DEFECT TC 203350000 NR00136: FWD CARGO BAFFLE BS 500B - 500C RBL 25 WL 156 CRACKED UPPER FLANGE. RESOLUTION: R/R BAFFLE BS 500B - 500C RBL 25 WL 156 IAW SRM 51-40-02-0G-0 AND DWG 143A7505.
DEFECT CORROSION ON FWD CARGO BAFFLE BS500D - 500E RBL 25 WL 156. RESOLUTION: R/R FWD CARGO BAFFLE BS500D - 500E RBL 25 WL 156 IAW SRM 51-40-02-0G-0 AND DWG 143A7505.
DEFECT TC 203350000 NR 00135: CORROSION ON FWD CARGO BAFFLE BS 500H-500I RBL 25 WL 156. RESOLUTION: R/R BAFFLE BS 500H-500I RBL 25 WL 156 IAW SRM 51-40-02-0G-0 AND DWG 143A7505
DEFECT TC 203350000 NR 00129: CORROSION ON FWD CARGO BAFFLE BS 500A - 500B RBL 25 WL 156. RESOLUTION. R/R BAFFLE BS 500A - 500B RBL 25 WL 156 IAW B737 SRM 51-40-02-0G-0 DWG 143A7505.
DEFECT TC 203350000 NR00138: FWD CARGO COMPARTMENT BAFFLE CLIP AT BS 500H LBL 25 WL 156 FWD SIDE OF FRAME CRAKCED. RESOLUTION: R/R BAFFLE CLIP AT BS 500H LBL 25 WL 156 FWD SIDE OF FRAME IAW SRM 51-40-02-0G-0 AND DWG 143A7505
DEFECT TC 203350000 NR00130: CORROSION ON FWD CARGO BAFFLE BS 500C - 500D RBL 25 WL 156. RESOLUTION: R/R BAFFLE BS 500C - 500D RBL 25 WL 156 IAW SRM 51-40-02-0G-0 DWG 143A7505.
AIRCRAFT WOULD NOT PRESSURIZE DUE TO L1 DOOR PRESSURE LEAK. FOUND L1 DOOR GUIDE ARM OUT OF ADJUSTMENT. ADJUSTED GUIDE ARM PER AMM 52-11-00. OPS CHECK AND PRESSURE CHECK NORMAL. AIRCRAFT OK FOR SERVICE
DEFECT: LE FLAPS TRANSIT ILLUMINATED AFTER FULLY CONFIGURED-SHORT FINAL VIS 24 ABE, WENT MISS, RAN "LE FLAPS TRANSIT" LIGHT CHECKLIST WHICH CALLED FOR FLAPS 15 LDG. LIGHT EXTINGUISHED UPON RETRACTION DURING MISS APPR AND ILLUMINATED AGAIN AT FLAPS 15. RESOLUTION: PERFORMED FIM 27-88 TASK 820 FSEU BITE, FOUND MX MESSAGE 27-81206 SL4 PROX OUTBD DISAGREE. UPON FURTHER INSPECTION FOUND O/B AND INBD PROX SENSOR TARGETS INSTALLED REVERSED. INSTALLED PROX TARGETS CORRECTLY IN REFERENCE TO B737 AMM 27-81-00. OPS CHECK GOOD AT THIS TIME. NO DEFECTS NOTED.