N834SY
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
INITIAL INSPECTION: SHEARED OFF AND LOOSE RIVETS ON RETAINER CLIP ON L1/L2 ESCAPE SLIDES. OPEN
INITIAL INSPECTION: WEAR ON SUPPORT LH ON L2 ESCAPE SLIDE. OPEN
ENG 2 VIBRATIONS WERE AT 4.3 WHILE IN CRUISE. EMERGENCY DECLARED. R&R #2 ENG PER W/0 100261 T/C 710000000
DEFECT 749304: 1L BOARDING DOOR SLIDE PATIALLY DEPLOYED. - RESOLUTION: PERFORMED L1 DOOR SLIDE CHECK IAW AMM 25-66-01. FOUND LATCH ASSEMBLY BROKEN. R & R LATCH ASSEMBLY AND REINSTALLED 1L SLIDE ASSEMBLY IAW AMM 25-66-01. A/C OK FOR SERVICE.
L1 DOOR SLIDE GRIT BAR AFT CLIP IS LOOSE AND NOT SECURING GRIT BAR WELL. RESECURED L1 DOOR SLIDE GRIT BAR IAW SRM 51-40-02 AND REINSTALLED L1 DOOR SLIDE IAW AMM 25-66-01
AFT RIGHT OVEN SMOKING BADLY AND BLACK AND HOT AT TOP RIGHT GASKET. REMOVED AND REPLACED OVEN IN REF. TO AMM 25-30-61. OPS CHECK GOOD.
WO 82545 // TASK CARD: L1 DOOR AFT GIRT BAR LATCH HAS SHEARED RIVETS. REPLACED SHEARED L1 AFT GIRT BAR RIVET REF SRM 51-40-02
R2 DOOR AFT GIRT BAR LATCH HAS SHEARED RIVETS. REPLACED SHEARED R2 GIRT BAR LATCH RIVET REF SRM 51-40-02
DEFECT NR00303: FLOOR BEAM AT STA 344 LBL 10 SRM REPAIR MODIFICATION. - - - RESOLUTION: REMOVED EXISTING REPAIR AND MODIFIED FLOOR BEAM AT STA 344 LBL 10 TO COMPLY WITH SRM 53-10-51-2R-10 REPAIR.
DEFECT: NR00284: FWD CARGO COMPARTMENT, BETWEEN BS 500F AND 500G, WL 160, S-26L BAFFLE IS CRACKED. - - - RESOLUTION: REMOVED AND REPLACED CRACKED BAFFLE BS 500F-500G IAW B737 SRM 51-40-02-0G-0 AND SRM 53-30-53-2R-1.
DEFECT NR00272: FWD CARGO COMPARTMENT BAFFLE AT BS 500G - 500H LLBL 24 WL 160 CRAKCED.- - - RESOLUTION: REPLACED BAFFLE AT BS 500G - 500H LBL 24 WL160 PER B737-800 SRM 51-40-02-0G-0 AND BOEING DRAWING 143A7505.
DEFECT NR00269: DAMAGE FOUND ON INTERCOSTAL @STA 294.5+12 LBL 11, WL 208. - - - RESOLUTION: REMOVED AND REPLACED INTERCOSTAL AT STA 294.5+12 LBL 11, WL 208 IAW B737 SRM 51-40-02-0G AND DWG 141A5600
DEFECT NR00228: CORROSION ON FLOOR BEAMAT STA 344 LBL10 APPROX. - - - RESOLUTION: AFTER FURTHER INVESTIGATION FOUND CORROSION TO BE OUT OF LIMITS ON FLOOR BEAM AT STA344 LBL 10 APPROX INSTALLED A REPAIR IAW ER 23-10-01666 REV IR ENG-53SCA-11146-REV00. REPLACED INTERCOSTAL, TRIMMED OUT CORNER OF INTERCOSTAL.
DEFECT NR00222: L2 MOP SEAL HAS AREAS OF CORROSION (MARKED). - - - RESOLUTION: EVALUATED CORROSION ON MOP SEAT L2 FOUND TO BE OUT OF LIMITS, REMOVED AND REPLACED MOP SEAL PER B737-800 SRM 51-40-02-0G AND DWG #147A8501 REV B. SRM REF 53-70-15-1A-1. CAUSE OF CORROSION: MOISTURE.
DEFECT: NR00229: CORROSION ON FLOOR BEAM AT STA 294 LBL 10 APPROX (MARKED). - - - RESOLUTION: REPAIRED FLOOR BEAM AT STA 294 LBL 10 IAW B737 SRM 53-10-51-2R-14. REPAIR IS A CAT-A REPAIR.
FWD CARGO BAY ON RH SHIELD HAS SIGNS OF CORROSION AROUND FASTENER HOLES AT STA 500 TO 500A. REMOVED AND REPLACED NEW SHIELD REPLACEMENT, PART # 143A8126, ON FWD CARGO BAY RH STA 500 TO 500A PER B737 SRM 51-40-02, SRM 51-40-05 AND BOEING DWG 143A008 REV - AT RBL 25 WL 160.
FWD CARGO BAY THRESHOLD WEB AT DOOR HAS EVIDECE OF CORROSION AROUND FASTENER HOLES 9. CORROSION DAMAGE ON FWD CARGO BAY THRESHOLD WEB AT DOOR EVALUATED AND FOUND TO BE OUT OF LIMITS PER B737 SRM 53-30-15-1A-1 FIG 103 DETAIL D. REMOVED AND REPLACED THRESHOLD WEB PER B737 SRM 51-40-02 AND BOEING DRAWING 143A8330 REV A AND SRM 51-40-05.
DEFECT NR 00187: FCB HAS CRACKED BAFFLE CLIP AT STA 500G FWD L/H SIDE BL 24 (MARKED) - - -RESOLUTION: REMOVED AND REPLACED BAFFLE CLIP AT STA 500G FWD L/H BL 24 IAW B737 SRM 51-40-02-0G-0 AND BOEING DWG #143A7505 ID 109.
DEFECT NR00158: CORROSION ON 986 FLOOR BEAM UPPER SURFACE RBL 44. - - - RESOLUTION: REPAIRED BS 986 FLOOR BEAM UPPER CAP IAW SCA ENG-53SCA-11180 REV 00 AND ATS ER/A 23-01523 REV IR. CAUSE OF CORROSION: MOISTURE.
CORROSION ON FLOOR BEAM UPPER SURFACE LBL 44. REPAIRED BS 986 FLOOR BEAM UPPER CHORD PER B737 SRM 53-70-51-2R-4 LBL 50 TO RBL 11. CORROSION DAMAGE FOUND TO BE OUT OF LIMITS PER B737 SRM 53-70-51-1A-1 PARA. 4 H (2),(B)(1) FIG 104 DETAIL C. CAUSE OF CORROSION: MOISTURE.
DEFECT: TRAILING EGDE FLAPS DISAGRE INFLIGHT. FLAP HANDEL AT 30; FLAPS INDICATED JUST OVER 25 . FLAPS DID NOT MOVE UP WHEN SELECTED INFLIGHT BUT DID MOVE TO 30 AFTER LANDING.: RESOLUTION: TROUBLESHOOTING SHOWED FAULTY L/H FLAP POSITION TRANSMITTER.R&R'D L/H FLAP POSITION TRANSMITTER REF. AMM. 27-50-01-400-801 TESTS GOOD. ALSO R&R'D CKPT INDICATOR REF. AMM. 27-58-00.CHECKS GOOD. ADDITIONAL INFORMATION: FLAPS DISAGREE ON APPROACH TO MSP AND EMERGENCY DECLARED. FLIGHT LANDED SAFELY WITHOUT INCIDENT IN MSP.
DEFECT 744805: TRAILING EGDE FLAPS DISAGRE INFLIGHT. FLAP HANDEL AT 30; FLAPS INDICATED JUST OVER 25 . FLAPS DID NOT MOVE UP WHEN SELECTED INFLIGHT BUT DID MOVE TO 30 AFTER LANDING. (EMERGENCY DECLARED, LANDED SAFELY) - - - - - RESOLUTION: TROUBLESHOOTING SHOWED FAULTY L/H FLAP POSITION TRANSMITTER.R&R'D L/H FLAP POSITION TRANSMITTER REF. AMM. 27-50-01-400-801 TESTS GOOD. ALSO R&R'D CKPT INDICATOR REF. AMM. 27-58-00.CHECKS GOOD.
FUEL SMELL NOTED IN PAX CABIN AS CREW ENTERED AIRCRAFT : RESOLUTION: GASOLINE SMELL WAS NOTED PRE TAXI. AUTO FUEL SMELL WAS ATTRIBUTED TO GAS POWERED HEAT CART PREVIOUSLY ATTACHED TO A/C.
L2 EMERGENCY SLIDE SIGHT GLASS MISSING. FOUND SIGHT GLASS AND RESECURED. REF AMM INTRODUCTION NR 2. OK FOR SERVICE
DEFECT: 1L GIRT BAR LOOSE - SLIDE FELL OFF WHEN OPENING. RESOLUTION: GIRT BAR RESECURED REF AMM 25-66-00. OK FOR SERVICE.
L/H L/E WING PANEL 521JB HAS TWO EA. DAMAGED FASTENER HOLES. REPAIRED 2 EA. DAMAGED FASTENER HOLES ON L/H L/E WING PANEL 521JB. IAW B737 SRM 57-41-01-2R-1 AND B737 SRM 51-70-05-2R-9.
#5 SLAT UPPER SURFACE HAVE A DENT LOCATED 3.750" FROM TRAILING EDGE AND 3" FROM OUTBOARD EDGE. REPAIRED DENT LOCATED 3.75" FROM TRAILING EDGE AND 3" FROM OUTBOARD EDGE ON #5 SLAT UPPER SURFACE PER 737-800 SRM 57-42-01-2R-11 AND SRM 51-70-10-2R-2.
R/H WING L/E PANEL 621QB HAS EXPOSED COMPOSITE ON EXTERIOR SURFACE. REPAIRED DAMAGED COMPOSITE ON EXTERIOR SURFACE ON R/H WING L/E PANEL 621QB IAW SRM 57-41-01-2R-1 AND SRM 51-70-05-2R-10.
LEFT HAND WING #3 SLAT UPPER SURFACE HAVE A DENT 51" FROM OUTBOARD AND 3" FROM TRAILING EDGE. REPAIRED DENT AT 51" FROM OUTBOARD AND 3" FROM TRAILING EDGE ON LEFT HAND WING #3 SLAT UPPER SURFACE IAW B737 SRM 57-42-01-2R-11 + SRM 51-70-10-2R-2.
L/H L/E WING PANEL 521NB HAS SURFACE DAMAGE ON EXTERIOR SURFACE. REPAIRED SURFACE DAMAGE ON EXTERIOR SURFACE ON L/H L/E WING PANEL 521NB IAW SRM 57-41-01-2R-1 AND SRM 51-70-05-2R-10.
LEFT AFT OVERWING LIGHT ON TAKEOFF ROLL LOW SPEED REJECT LESS THAN 30KTS. REPLACED FLIGHT LOCK SOLENOID ON AFT LT OVERWING DOOR AND TESTED PER AMM 52-22-41. OK FOR SERVICE.