N108SY
Registered owner: SKYWEST AIRLINES INC, 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.
46 reports on file, 2015-01-20 – 2024-09-26.
Part: SHEAR PANEL — DAMAGED (ZONE 100) · airframe 27,310 hrs · 15,651 cycles
ELONGATED HOLE FOUND AFTER REMOVAL OF PANEL R/H END OF FR88 FOR R/H SHEAR PANEL ATTACHMENT (C-CHECK RO 10/15/2024) (FILED OPEN)REMOVED ELONGATED HOLE BY DRILLING TO SPECIFIC DIAMETER TO REMOVE DAMAGE. INSTALLED BUSHING.SEE CONTINUATION CARD FOR WORK PERFORMED. REF ETD2024-170-026011 REV:A. THIS REPAIR DOES NOT AFFECT WEIGHT AND BALANCE.
Part: BEAM — CORRODED (ZONE 200) · airframe 27,310 hrs · 15,651 cycles
AFTER REMOVAL OF R/H INBOARD BEAM FR12-20 FOUND CORROSION AT FR17 CROSSBEAM (C-CHECK RO 10/15/2024) (FILED OPEN)WEIGHT OF FR 17 CROSSBEAM REPAIR PARTS AND FASTENERS MEASURE 253.5 G. (TOOLING I.D# HG3-61241 DUE: 08/21/25) PERFORMED CROSSBEAM REPAIR AT FR17 REF: SRM 51-00-10/REPAIR 03P. WEIGHT OF REPAIR DOES NOT EFFECT WEIGHT AND BALANCE. SEE CONTINUATION CARD FOR MAINTENANCE PERFORMED.
Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 27,411 hrs · 15,721 cycles
AFTER REMOVAL OF R/H INBOARD BEAM FR12-20 FOUND CORROSION AT FR17 CROSSBEAM (C-CHECK RO 10/15/2024) (FILED CLOSED)WEIGHT OF FR 17 CROSSBEAM REPAIR PARTS AND FASTENERS MEASURE 253.5 G. (TOOLING I.D# HG3-61241 DUE: 08/21/25) PERFORMED CROSSBEAM REPAIR AT FR17 REF: SRM 51-00-10/REPAIR 03P. WEIGHT OF REPAIR DOES NOT EFFECT WEIGHT AND BALANCE. SEE CONTINUATION CARD FOR MAINTENANCE PERFORMED.
Part: BEAM — CORRODED (ZONE 100) · airframe 27,411 hrs · 15,721 cycles
CORROSION IN R/H I/B BEAM FR.12-20. (C-CHECK RO 10/15/2024) (FILED CLOSED)REMOVED AND REPLACED THE R/H I/B BEAM FR.12-20. REF EMB SRM 51-40-08. REPLACED WITH NEW OEM PART, NO WEIGHT AND BALANCE CHANGE REQUIRED.
Part: BEAM — CORRODED (ZONE 200) · airframe 27,411 hrs · 15,721 cycles
CORROSION IN L/H I/B BEAM FR.17-20. (C-CHECK RO 10/15/2024) (FILED CLOSED)REMOVED DAMAGE ON L/H I/B BEAM BY PERFORMING A CENTER BEAM UPPER CAP REPAIR AT FR 17 AND FR 18. REF SRM 53-10-10/REPAIR 01. REMOVED DAMAGE ON THE L/H I/B BEAM BETWEEN FR 19-20 BY BLENDING. MAX MATERIAL REMOVED FOUND TO BE WITHIN LIMITS. REF EMB ETD2024-17-026271. SEE CONTINUATION CARD FOR WORK PERFORMED. .REPAIR PARTS WEIGHT= 175.5 GRAMS THIS DOES NOT EFFECT AIRCRAFT WEIGHT AND BALANCE
Part: BEAM — CORRODED (ZONE 200) · airframe 27,310 hrs · 15,651 cycles
CORROSION IN R/H BEAM AT FR.87. (C-CHECK RO 10/15/2024) (FILED OPEN)REMOVED AND REPLACED THE R/H BEAM AT FR.87. REF EMB SRM 51-40-08. SEE CONTINUE CARD FOR WORK PERFORMED
Part: BEAM — CORRODED (ZONE 200) · airframe 27,411 hrs · 15,721 cycles
CORROSION IN R/H BEAM AT FR.87. (C-CHECK RO 10/15/2024) (FILED CLOSED)REMOVED AND REPLACED THE R/H BEAM AT FR.87. REF EMB SRM 51-40-08. SEE CONTINUE CARD FOR WORK PERFORMED
Part: BEAM — CORRODED (ZONE 200) · airframe 27,310 hrs · 15,651 cycles
CORROSION IN R/H I/B BEAM FR.12-20. (C-CHECK RO 10/15/2024) (FILED OPEN)REMOVED AND REPLACED THE R/H I/B BEAM FR.12-20. REF EMB SRM 51-40-08. REPLACED WITH NEW OEM PART, NO WEIGHT AND BALANCE CHANGE REQUIRED.
Part: BEAM — CORRODED (ZONE 100) · airframe 27,310 hrs · 15,651 cycles
CORROSION IN L/H I/B BEAM FR.17-20. (C-CHECK RO 10/15/2024) (FILED OPEN)REMOVED DAMAGE ON L/H I/B BEAM BY PERFORMING A CENTER BEAM UPPER CAP REPAIR AT FR 17 AND FR 18. REF SRM 53-10-10/REPAIR 01. REMOVED DAMAGE ON THE L/H I/B BEAM BETWEEN FR 19-20 BY BLENDING. MAX MATERIAL REMOVED FOUND TO BE WITHIN LIMITS. REF EMB ETD2024-17-026271. SEE CONTINUATION CARD FOR WORK PERFORMED. .REPAIR PARTS WEIGHT= 175.5 GRAMS THIS DOES NOT EFFECT AIRCRAFT WEIGHT AND BALANCE
Part: SEAT TRACK — GOUGED (ZONE 200) · airframe 27,310 hrs · 15,651 cycles
RH IB SEAT TRACK HAS GOUGING FROM FR 73 TO FR 84 (C-CHECK RO 10/15/2024) (FILED OPEN)REMOVED AND REPLACED RH IB SEAT TRACK FR 73-FR 84 REF SRM 51-40-08. OEM PARTS CHANGE - WEIGHT AND BALANCE NOT AFFECTED.
Part: SEAT TRACK — GOUGED (ZONE 200) · airframe 27,411 hrs · 15,721 cycles
LH IB SEAT TRACK HAS GOUGING FROM FR 73 TO FR 84 (C-CHECK RO 10/15/2024) (FILED CLOSED)REMOVED AND REPLACED LH IB SEAT TRACK SEGMENT FR 73 TO FR 84, REF SRM 51-40-08. REPLACED WITH NEW OEM PART, NO WEIGHT AND BALANCE ADJUSTMENT REQUIRED.
Part: SEAT TRACK — GOUGED (ZONE 200) · airframe 27,310 hrs · 15,651 cycles
LH IB SEAT TRACK HAS GOUGING FROM FR 73 TO FR 84 (C-CHECK RO 10/15/2024) (FILED OPEN)REMOVED AND REPLACED LH IB SEAT TRACK SEGMENT FR 73 TO FR 84, REF SRM 51-40-08. REPLACED WITH NEW OEM PART, NO WEIGHT AND BALANCE ADJUSTMENT REQUIRED.
Part: SEAT TRACK — GOUGED (ZONE 200) · airframe 27,310 hrs · 15,651 cycles
GOUGES ON R/H FLOOR SEAT TRACK BETWEEN FR 23-34 IN 10 LOCATIONS AS MARKED. (C-CHECK RO 10/15/2024) (FILED OPEN)REMOVED AND REPLACED R/H FLOOR SEAT TRACK BETWEEN FR 23-34. REF SRM 51-40-08. SEE CONTINUATION CARD FOR WORK PERFORMED. OEM PARTS CHANGE, THIS DOES NOT AFFECT WEIGHT AND BALANCE.
Part: SEAT TRACK — GOUGED (ZONE 200) · airframe 27,411 hrs · 15,721 cycles
RH IB SEAT TRACK HAS GOUGING FROM FR 73 TO FR 84 (C-CHECK RO 10/15/2024) (FILED CLOSED)REMOVED AND REPLACED RH IB SEAT TRACK FR 73-FR 84 REF SRM 51-40-08. OEM PARTS CHANGE - WEIGHT AND BALANCE NOT AFFECTED.
Part: SEAT TRACK — GOUGED (ZONE 200) · airframe 27,411 hrs · 15,721 cycles
GOUGES ON R/H FLOOR SEAT TRACK BETWEEN FR 23-34 IN 10 LOCATIONS AS MARKED. (C-CHECK RO 10/15/2024) (FILED CLOSED)REMOVED AND REPLACED R/H FLOOR SEAT TRACK BETWEEN FR 23-34. REF SRM 51-40-08. SEE CONTINUATION CARD FOR WORK PERFORMED. OEM PARTS CHANGE, THIS DOES NOT AFFECT WEIGHT AND BALANCE.
Part: BEAM — CORRODED (ZONE 800) · airframe 27,411 hrs · 15,721 cycles
AFT PAX DOOR LOWER BEAM FWD AND AFT EVACUATION SLIDE-FITTING CUTOUTS HAVE CORROSION AS MARKED. (C-CHECK RO 10/15/2024) (FILED CLOSED)INSTALLED NEW AFT PAX DOOR LOWER BEAM FWD AND AFT EVACUATION SLIDE-FITTING REF SRM 51-40-08 SEE CONTINUE CARD FOR WORK PERFORMED
Part: BEAM — CORRODED (PAX DOOR) · airframe 27,310 hrs · 15,651 cycles
AFT PAX DOOR LOWER BEAM FWD AND AFT EVACUATION SLIDE-FITTING CUTOUTS HAVE CORROSION AS MARKED. (C-CHECK RO 10/15/2024) (FILED OPEN)INSTALLED NEW AFT PAX DOOR LOWER BEAM FWD AND AFT EVACUATION SLIDE-FITTING REF SRM 51-40-08 SEE CONTINUE CARD FOR WORK PERFORMED
Part: BEAM — CORRODED (ZONE 800) · airframe 27,411 hrs · 15,721 cycles
AFT SERVICE DOOR LOWER BEAM FWD AND AFT EVACUATION SLIDE-FITTING CUTOUTS HAVE CORROSION AS MARKED. (C-CHECK RO 10/15/2024) (FILED CLOSED)REMOVED AND REPLACED THE AFT SERVICE DOOR LOWER BEAM. REF EMB SRM 51-40-08
Part: BEAM — CORRODED (SERVICE DOOR) · airframe 27,310 hrs · 15,651 cycles
AFT SERVICE DOOR LOWER BEAM FWD AND AFT EVACUATION SLIDE-FITTING CUTOUTS HAVE CORROSION AS MARKED. (C-CHECK RO 10/15/2024) (FILED OPEN)REMOVED AND REPLACED THE AFT SERVICE DOOR LOWER BEAM. REF EMB SRM 51-40-08
Part: SKIN — CORRODED (ZONE 100) · airframe 27,310 hrs · 15,651 cycles
WASTE BOX INTERNAL FLANGE CORRODED ON BOTH SIDES OF HINGE (C-CHECK RO 10/15/2024) (FILED OPEN).REMOVED AND REPLACE WASTE BOX INTERNAL DOUBLER AND WASTE BOX DOOR ASSY INCLUDING THE HINGE ASSY. REF EMB SRM 51-40-08. SEE CONTINUATION CARD FOR WORK ACCOMPLISHED. O.E.M. PARTS INSTALLED NO CHANGE TO WEIGHT AND BALANCE
Part: DOUBLER — CORRODED (ZONE 100) · airframe 27,411 hrs · 15,721 cycles
WASTE BOX INTERNAL FLANGE CORRODED ON BOTH SIDES OF HINGE (C-CHECK RO 10/15/2024) (FILED CLOSED).REMOVED AND REPLACE WASTE BOX INTERNAL DOUBLER AND WASTE BOX DOOR ASSY INCLUDING THE HINGE ASSY. REF EMB SRM 51-40-08. SEE CONTINUATION CARD FOR WORK ACCOMPLISHED. O.E.M. PARTS INSTALLED NO CHANGE TO WEIGHT AND BALANCE
Earlier reports · 2015–2022 · 25 reports
2022
Part: NONE — NONE · airframe 21,169 hrs · 11,528 cycles
WARRANTY - RIBS 10A , 11A, AND 12A MISLOCATED DURING DRILL UP OF NEW RIBS (C CHECK RO 03/07/2022) REMOVED AND REPLACED LH HORIZONTAL STABILIZER RIBS 10A , 11A, AND 12A, REF EMB175 SRM 51-40-08. SEE CONTINUATION FOR WORK PERFORMED.
Part: NONE — CRACKED · airframe 21,169 hrs · 11,528 cycles
FLOOR SUPPORT AT R/H FR. 86 CRACKED I/B OF AFT SERVICE DOOR. (C CHECK RO 03/07/2022) REMOVED AND REPLACED FLOOR SUPPORT AT R/H FR. 86 I/B OF AFT SERVICE DOOR AND APPLIED TOPCOAT TO FASTENERS REF SRM 51-40-08 AND 51-23-06
Part: NONE — CRACKED · airframe 21,169 hrs · 11,528 cycles
FLOOR SUPPORT AT R/H FR. 85 CRACKED I/B OF AFT SERVICE DOOR. (C CHECK RO 03/07/2022) REMOVED AND REPLACED FLOOR SUPPORT AT R/H FR. 85 I/B OF AFT SERVICE DOOR AND APPLIED TOPCOAT TO FASTENERS REF SRM 51-40-08 AND 51-23-06
Part: NONE — NONE · airframe 21,169 hrs · 11,528 cycles
LH HORIZONTAL STABILIZER UPPER SKIN MIS-DRILLED HOLE AT RIB 14 FWD END (C CHECK RO 03/07/2022) REPAIRED L/H HORIZONTAL STABILIZER UPPER SKIN AT RIB 14 FWD END. REF ETD2022-170-007380. SEE CONTINUATION FOR WORK PERFORMED.
Part: NONE — CORRODED · airframe 21,169 hrs · 11,528 cycles
AFT CARGO DOOR AFT DOOR SILL REST ( EXTERNAL SIDE) HAS CORROSION AROUND MULTIPLE NUTPLATES AS MARKED (C CHECK RO 03/07/2022) REMOVED AND REPLACED AFT CARGO DOOR SILL REST REF EMB SRM 51-40-08.
Part: NONE — DAMAGED · airframe 21,169 hrs · 11,528 cycles
RH ELEVATOR HINGE #4 BOLT AND NUT HAVE THREAD DAMAGE/NUT WILL NOT THREAD ONTO BOLT. (C CHECK RO 03/07/2022) REMOVED AND REPLACED RH ELEVATOR HINGE #4 BOLT AND NUT ON RACK. REF. EMB 175 AMM 27-31-05 SEE CP 24266583 FOR INSTALLATION.
Part: NONE — DAMAGED · airframe 21,169 hrs · 11,528 cycles
RH ELEVATOR HINGE #2 INBOARD BUSHING IS DENTED INTO THE INTERNAL DIAMETER AND WILL NOT ALLOW THE BOLT TO BE INSERTED. (C CHECK RO 03/07/2022) REMOVED AND REPLACED RH ELEVATOR HINGE #2 INBOARD BUSHING. REF EMB 175 AMM 20-10-08
Part: NONE — DAMAGED · airframe 21,169 hrs · 11,528 cycles
RH ELEVATOR HINGE #3 BOLT OUTBOARD HAT BUSHINGS (FLOATING AND PRESSED IN) HAVE DENTS/SCORING DAMAGE. (C CHECK RO 03/07/2022) REMOVED AND REPLACED RH ELEVATOR HINGE #3 BOLT OUTBOARD HAT BUSHINGS (FLOATING AND PRESSED IN). REF. EMB 175 AMM 20-10-08
Part: NONE — BINDS · airframe 21,169 hrs · 11,528 cycles
RH HORIZONTAL STABILIZER #3 HINGE BEARING IS BINDING/RATCHETING. (C CHECK RO 03/07/2022) REMOVED AND REPLACED RH HORIZONTAL STABILIZER #3 HINGE BEARING. REF. EMB 175 AMM 20-10-08
Part: NONE — DISPLACED · airframe 21,169 hrs · 11,528 cycles
LH ELEVATOR HINGE FITTING #3 INBOARD HAT BUSHING IS MIGRATED. (C CHECK RO 03/07/2022) REMOVED AND REPLACED LH ELEVATOR HINGE FITTING #3 INBOARD HAT BUSHING AS REQUIRED. REF. EMB 175 AMM 20-10-08
Part: NONE — DAMAGED · airframe 21,169 hrs · 11,528 cycles
LH ELEVATOR HINGE #2 INBOARD BUSHING IS DENTED INTO THE INTERNAL DIAMETER AND WILL NOT ALLOW THE BOLT TO BE INSERTED. (C CHECK RO 03/07/2022) REMOVED AND REPLACED LH ELEVATOR HINGE #2 INBOARD BUSHING. REF EMB 175 AMM 20-10-08
Part: NONE — DAMAGED · airframe 21,169 hrs · 11,528 cycles
RH ELEVATOR HINGE #2 HARDWARE STACK UP (BOLT/NUT/BUSHING/WASHERS) WAS FOUND SEIZED AND WERE DAMAGED DURING REMOVAL. (C CHECK RO 03/07/2022) REMOVED AND REPLACED RH ELEVATOR HINGE #2 HARDWARE AS REQUIRED ON RACK. REF. EMB 175 AMM 27-31-05. SEE CP 24266583 FOR INSTALLATION.
Part: NONE — BINDS · airframe 21,169 hrs · 11,528 cycles
RH HORIZONTAL STABILIZER #2 HINGE BEARING IS BINDING/RATCHETING. (C CHECK RO 03/07/2022) REMOVED AND REPLACED RH HORIZONTAL STABILIZER #2 HINGE BEARING, REF. EMB 175 AMM 20-10-08
Part: NONE — CRACKED · airframe 21,169 hrs · 11,528 cycles
CENTER COCKPIT FLOOR CONSOLE SUPPORT ANGLE IS CRACKED ON THE FORWARD SIDE OF FLOOR BEAM AT FRAME 12. (C CHECK RO 03/07/2022) / REMOVED AND REPLACED CENTER COCKPIT FLOOR CONSOLE SUPPORT ANGLE ON THE FORWARD SIDE OF FRAME 12 REF: EMB SM 51-40-08. SEE CONTINUATION FOR WORK PERFORMED
Part: NONE — CORRODED · airframe 21,169 hrs · 11,528 cycles
UNDER AFT WET AREA, FWD OF WASTE BOX, SHEAR CLIP CORRODED AT FRAME 88 BETWEEN STRINGERS 23R AND 24R (C CHECK RO 03/07/2022) REMOVED AND REPLACED SHEAR CLIP AT FR88 BETWEEN STGR 23R AND 24R REF EMB SRM 51-40-08. SEE CONTINUATION CARD FOR WORK PERFORMED.
Part: NONE — CORRODED · airframe 21,169 hrs · 11,528 cycles
AFT WET AREA, RH SIDE, PANEL, SHEAR CORRODED IN 2 PLACES, 2ND AND 4TH BOLT HOLES FROM RH END (C CHECK RO 03/07/2022) REMOVED AND REPLACED AFT WET AREA, RH SIDE, PANEL, SHEAR REF SRM 51-40-08. RESTORED SURFACE PROTECTION REF SRM 51-23-06
Part: NONE — CORRODED · airframe 21,169 hrs · 11,528 cycles
AFT WET AREA, RH SIDE, PANEL SUPPORT CORRODED IN 2 PLACES, AFT AND CENTER BOLT HOLES (C CHECK RO 03/07/2022) REMOVED AND REPLACED AFT WET AREA RH SIDE PANEL SUPPORT REF SRM 51-40-08. RESTORED SURFACE PROTECTION REF SRM 51-23-04, 50-23-05, AND 51-23-06.
Part: NONE — CORRODED · airframe 21,169 hrs · 11,528 cycles
AFT WET AREA, RH SIDE, GUSSET PLATE CORRODED AT INBOARD BOLT HOLE (C CHECK RO 03/07/2022) REMOVED AND REPLACED AFT WET AREA, RH SIDE, GUSSET PLATE AT FR90 REF EMB SRM 51-40-08 RESTORED SURFACE PROTECTION REF SRM 51-23-06 APPLIED CIC REF CPM 51-25-00
Part: NONE — DAMAGED · airframe 21,169 hrs · 11,528 cycles
L/H WING #2A O/B FLAP TRACK HAS WIDTH REDUCTION DAMAGE OF .031". (C CHECK RO 03/07/2022) LH WING #2A OB FLAP TRACK OUT OF LIMITS. NOMINAL 1.003" REMOVED.44" REMAINING .959" REF ERJ 175 SRM 57-52-03. TC2-8910 DATE11-23-22. REPLACED LH OB #2A FLAP TRACK. REF ERJ 175 AMM 57-54-25. HG4-50097 DATE 6-24-22
Part: NONE — CORRODED · airframe 21,169 hrs · 11,528 cycles
L/H AND R/H WING FLAP TRACK SUPPORT #2, #3, AND #4 FWD ATTACHMENT TO WING FITTING SPRING WASHERS CORRODED. (C CHECK RO 03/07/2022) REMOVED AND REPLACED L/H AND R/H WING FLAP TRACK SUPPORT #2, #3, AND #4 FWD ATTACHMENT TO WING FITTING SPRING WASHERS. REF EMB 175 AMM 57-54-21 & 57-57-31
Part: NONE — WORN · airframe 21,169 hrs · 11,528 cycles
LH SLAT #3 O/B TRACK THICKNESS REDUCTION .41MM OUT OF LIMITS. ASSET TC2-7153 DUE 11/18/22 (C CHECK RO 03/07/2022) / COMPLIED WITH PERMANENT REPAIR PER ETD2022-170-006810 / - DETAILED VISUAL INSPECTION (DET) AT REWORKED AREAS, THRESHOLD OF 7,500 FC, INTERVAL OF 7,500 FC. THIS IS AN / ADDITIONAL AND SPECIFIC INSPECTION REQUIREMENT. IT REPRESENTS THE REPAIR AIRWORTHINESS LIMITATION, HOWEVER, IT / DOES NOT DISMISS ANY OTHER EXISTING MAINTENANCE TASK. THRESHOLD IS COUNTED SINCE THE REPAIR ACCOMPLISHMENT. / - EMBRAER SHOULD BE CONTACTED IN CASE OF DECREASE OF THE DIMENSION "A" UNDER 42.51 MM.
Part: NONE — DAMAGED · airframe 21,169 hrs · 11,528 cycles
COMPLY WITH SCHEDULED MAINTENANCE CODE: RA47357-ETD2019-170-043590-N108SY-PR - DENT AND SCRATCH DAMAGE TO THE FWD FUSE SKIN BTWN FR10-FR11 AND STR14L-15L. PERFORMED TEMP ACTIONS IN REF TO ETD2019-170-043590, REV :/, DTD 03/29/2019. PERFORM PERM REPAIR PER SRM PART II-1802 - 53-10-01/REPAIR 12P FWD FUSE SKIN - EXTERNAL DIRECT RECTANGULAR REPAIR WITHIN 7500 FC. DUE BY TAC 15018, PART NUMBER: - , SERIAL NUMBER: 17000401, POSITION: (C CHECK RO 03/07/2022) PERFORMED REPAIR AT FWD FUSE SKIN BTWN FR10 - FR11 AND STR14L - 15L REF ETD2019-170-043590 AND SRM 53-10-01/REPAIR 12P.
2021
Part: UNKNOWN — ODOR (CABIN) · airframe 19,312 hrs · 10,461 cycles
FUME EVENT DURING CRUISE STRONG SULFUR ACIDIC SMELL. EYES AND THROAT IRRITATION. DID NOT GET TO ISOLATE ANY PACKS OR ENG BLEEDS AND NO APU ON TAXI IN. (FLIGHT 5819 - FILED CLOSED) PERFORMED FIM TASK 21-20-00-810-803-A AND FIM TASK 21-20-00-810-801-A. NO DEFECTS FOUND.
2019
Part: LINE — FAILED (HYD PRESSURE) · airframe 15,146 hrs · 8,124 cycles
RECEIVED HYDRAULIC 2 LOW PRESSURE AND HYD 2 QTY CAUTION MESSAGES IN FLIGHT. PERFORMED QRH. MESSAGES REMAINED. DIVERTED. LANDING GEAR MANUALLY EXTENDED. LANDING WAS UNEVENTFUL. (FLT#5647) FO: 07/12/2019 CLOSED REMOVED AND REPLACED LEFT #2 HYDRAULIC TRAILING EDGE PRESSURE LINE IAW AMM. OPS/LEAK CHECK GOOD.
2015
Part: ANTENNA — DAMAGED (TCAS) · airframe 1,604 hrs · 811 cycles
FOUND TCAS ANTENNA DAMAGED. R & R THE BOTTOM OMNI DIRECTIONAL TCAS ANTENNA IAW AMM. OPS CHECKED GOOD.