N810HC

No registry detail on file · not in current registry

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.

86 reports on file, 2016-09-26 – 2020-01-15.

WARNING INDICATION · 2020-01-15 Matched by certificate designator
ATA 2913

Part: PUMP — FAILED (HYD SYSTEM) · airframe 27,741 hrs · 30,221 cycles

FLIGHT 301,AIR TURNBACK. BLUE SIDE LOW LEVEL WARNING LIGHT AND CCAS BLUE HYDRAULIC CAUTION IN FLIGHT. AIRCRAFT WAS RETURNED TO HNL. EMERGENCY WAS DECLARED. LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE BLUE HYDRAULIC PUMP, HYDRAULIC HOSE AND GREEN HYDRAULIC SYSTEM PRESSURE FILTER. OPS AND LEAK CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Source: SDR COEA2020011651810
Earlier reports · 2016–2019 · 85 reports

2019

OTHER · 2019-10-22 Matched by certificate designator
ATA 5330

Part: SKIN — CORRODED (FRAMES 40-41) · corrosion level 2 · airframe 27,691 hrs · 30,156 cycles

WO 205731 NR 200141 HEAVY CHECK COE/MAJOR REPAIR: REAR FUSELAGE UPPER L/H SKIN INTERIOR SURFACE HAS LEVEL 2 CORROSION BETWEEN FRAMES 40-41, ABOVE STRINGER 7L. CORRECTIVE ACTION: DOUBLER REPAIRED PER SRM 530000-300-803-A01.

Source: SDR COEA201911222810
OTHER · 2019-10-08 Matched by certificate designator
ATA 5312

Part: BULKHEAD — CORRODED (ZONE 200) · corrosion level 2 · airframe 27,691 hrs · 30,156 cycles

WO 205731 NR 200135 HEAVY CHECK COE/MAJOR REPAIR: FORWARD PRESSURE BULKHEAD UPPER L/H INBOARD CORNER BOND AREA HAS LEVEL 2 CORROSION. CORRECTIVE ACTION: REPAIRED PER SRAS ES_0107423_01...15385 ISSUE A, DATED 11/20/2019.

Source: SDR COEA2019112287810
OTHER · 2019-10-06 Matched by certificate designator
ATA 5330

Part: SKIN — CORRODED (FRAMES 28D-29) · corrosion level 2 · airframe 27,691 hrs · 30,156 cycles

WO 205731 NR 200121 HEAVY CHECK COE/MAJOR REPAIR: CENTER FUSELAGE UPPER R/H SKIN INTERIOR SURFACE HAS LEVEL 2 CORROSION BETWEEN FRAMES 28D-29 BETWEEN STRINGERS 10R-11R. CORRECTIVE ACTION: REPAIRED PER SRAS ES_0107986_01...15487 ISSUE A, DATED 11/20/2019.

Source: SDR COEA2019112640810
OTHER · 2019-10-06 Matched by certificate designator
ATA 5330

Part: SKIN — CORRODED (FRAMES 40-41) · corrosion level 2 · airframe 27,691 hrs · 30,156 cycles

WO 205731 NR 200064 HEAVY CHECK COE/MAJOR REPAIR: REAR FUSELAGE UPPER R/H SKIN INTERIOR SURFACE HAS LEVEL 2 CORROSION NEAR FRAMES 40-41, STRINGERS 3R-4R. CORRECTIVE ACTION: BLENDOUT PER SRAS ES_0107970_01...15483 ISSUE A, DATED 11/18/2019.

Source: SDR COEA2019112268810
OTHER · 2019-10-06 Matched by certificate designator
ATA 5330

Part: SKIN — CORRODED (FRAMES 39-40) · corrosion level 2 · airframe 27,691 hrs · 30,156 cycles

WO 205731 NR 200078 HEAVY CHECK COE/MAJOR REPAIR: REAR FUSELAGE UPPER R/H SKIN INTERIOR SURFACE HAS LEVEL 2 CORROSION BETWEEN FRAMES 39-40, STRINGERS 4R-5R. CORRECTIVE ACTION: REPAIRED PER SRAS ES_0107970_01...15483 ISSUE A, DATED 11/18/2019.

Source: SDR COEA2019112260810
OTHER · 2019-10-06 Matched by certificate designator
ATA 5330

Part: SKIN — CORRODED (FRAMES 39-40) · corrosion level 2 · airframe 27,691 hrs · 30,156 cycles

WO 205731 NR 200079 HEAVY CHECK COE/MAJOR REPAIR: REAR FUSELAGE UPPER R/H SKIN INTERIOR SURFACE HAS LEVEL 2 CORROSION BETWEEN FRAMES 39-40, STRINGERS 3R-4R. CORRECTIVE ACTION: REPAIRED PER SRAS ES_0107970_01...15483 ISSUE A, DATED 11/18/2019.

Source: SDR COEA2019112261810
OTHER · 2019-10-06 Matched by certificate designator
ATA 5330

Part: SKIN — CORRODED (FRAMES 28-28A) · corrosion level 2 · airframe 27,691 hrs · 30,156 cycles

WO 205731 NR 200130 HEAVY CHECK COE/MAJOR REPAIR: CENTER FUSELAGE UPPER R/H SKIN INTERIOR SURFACE HAS LEVEL 2 CORROSION BETWEEN FRAMES 28-28A STRINGERS 7R-8R. CORRECTIVE ACTION: REPAIRED PER SRAS ES_0107986_01...15487 ISSUE A, DATED 11/20/2019.

Source: SDR COEA2019112236810
OTHER · 2019-10-06 Matched by certificate designator
ATA 5330

Part: SKIN — CORRODED (FRAME 23C) · corrosion level 2 · airframe 27,691 hrs · 30,156 cycles

WO 205731 NR 200108 HEAVY CHECK COE/MAJOR REPAIR: CENTER FUSELAGE UPPER R/H SKIN INTERIOR SURFACE HAS LEVEL 2 CORROSION AFT OF FRAME 23C BELOW STRINGER 8R. CORRECTIVE ACTION: REPAIRED PER SRAS ES_0107986_01...15487 ISSUE A, DATED 11/20/2019.

Source: SDR COEA2019112639810
OTHER · 2019-10-06 Matched by certificate designator
ATA 5330

Part: SKIN — CORRODED (FRAMES 41-42) · corrosion level 2 · airframe 27,691 hrs · 30,156 cycles

WO 205731 NR 200061 HEAVY CHECK COE/MAJOR REPAIR: REAR FUSELAGE UPPER R/H SKIN INTERIOR SURFACE HAS LEVEL 2 CORROSION BETWEEN FRAMES 41-42, STRINGERS 5R-6R. CORRECTIVE ACTION: REPAIRED PER SRAS ES_0107970_01...15483, ISSUE A, DATED 11/18/2019.

Source: SDR COEA2019112267810
OTHER · 2019-10-06 Matched by certificate designator
ATA 5330

Part: SKIN — CORRODED (FRAMES 28A-28B) · corrosion level 2 · airframe 27,691 hrs · 30,156 cycles

WO 205731 NR 200127 HEAVY CHECK COE/MAJOR REPAIR: CENTER FUSELAGE UPPER R/H SKIN INTERIOR SURFACE HAS LEVEL 2 CORROSION BETWEEN FRAMES 28A-28B BETWEEN STRINGERS 10R-11R. CORRECTIVE ACTION: REPAIRED PER SRAS ES_0107986_01...15487 ISSUE A, DATED 11/20/2019.

Source: SDR COEA201911225810
OTHER · 2019-10-06 Matched by certificate designator
ATA 5330

Part: SKIN — CORRODED (FRAME 23B) · corrosion level 2 · airframe 27,691 hrs · 30,156 cycles

WO 205731 NR 200101 HEAVY CHECK COE/MAJOR REPAIR: CENTER FUSELAGE UPPER R/H SKIN INTERIOR SURFACE HAS LEVEL 2 CORROSION AFT OF FRAME 23B BELOW STRINGER 8R. CORRECTIVE ACTION: REPAIRED PER SRAS ES_0107986_01...15487 ISSUE A, DATED 11/20/2019.

Source: SDR COEA2019112638810
OTHER · 2019-10-06 Matched by certificate designator
ATA 5330

Part: SKIN — CORRODED (FRAMES 28C-28D) · corrosion level 2 · airframe 27,691 hrs · 30,156 cycles

WO 205731 NR 200125 HEAVY CHECK COE/MAJOR REPAIR: CENTER FUSELAGE UPPER R/H SKIN INTERIOR SURFACE HAS LEVEL 2 CORROSION BETWEEN FRAMES 28C-28D BETWEEN STRINGERS 8R-10R. CORRECTIVE ACTION: REPAIRED PER SRAS ES_0107986_01...15487 ISSUE A, DATED 11/20/2019.

Source: SDR COEA201911224810
OTHER · 2019-10-06 Matched by certificate designator
ATA 5330

Part: SKIN — CORRODED (FRAME 23A) · corrosion level 2 · airframe 27,691 hrs · 30,156 cycles

WO 205731 NR 200091 HEAVY CHECK COE/MAJOR REPAIR: CENTER FUSELAGE UPPER R/H SKIN INTERIOR SURFACE HAS LEVEL 2 CORROSION FORWARD OF FRAME 23A, BETWEEN STRINGERS 8-9R. CORRECTIVE ACTION: REPAIRED PER SRAS ES_0107986_01...15487 ISSUE A, DATED 11/20/2019.

Source: SDR COEA201911228810
OTHER · 2019-10-06 Matched by certificate designator
ATA 5330

Part: SKIN — CORRODED (FRAMES 28D-29) · corrosion level 2 · airframe 27,691 hrs · 30,156 cycles

WO 205731 NR 200122 HEAVY CHECK COE/MAJOR REPAIR: CENTER FUSELAGE UPPER R/H SKIN INTERIOR SURFACE HAS LEVEL 2 CORROSION BETWEEN FRAMES 28D-29 BETWEEN STRINGERS 7R-8R. CORRECTIVE ACTION: REPAIRED PER SRAS ES_0107986_01...15487 ISSUE A, DATED 11/20/2019.

Source: SDR COEA2019112263810
OTHER · 2019-10-06 Matched by certificate designator
ATA 5322

Part: SHEAR TIE — CORRODED (FRAME 41) · corrosion level 2 · airframe 27,691 hrs · 30,156 cycles

WO 205731 NR 200071 HEAVY CHECK COE/MAJOR REPAIR: FRAME 41 SHEAR TIE STRINGER 4L-5L HAS LEVEL 2 CORROSION. CORRECTIVE ACTION: REPLACED BY FABRICATION.

Source: SDR COEA2019111267810
OTHER · 2019-10-06 Matched by certificate designator
ATA 5330

Part: SKIN — CORRODED (FRAME 40) · corrosion level 2 · airframe 27,691 hrs · 30,156 cycles

WO 205731 NR 200077 HEAVY CHECK COE/MAJOR REPAIR: REAR FUSELAGE UPPER R/H SKIN INTERIOR SURFACE HAS LEVEL 2 CORROSION FORWARD OF FRAME 40, ABOVE STRINGER 6R. CORRECTIVE ACTION: REPAIRED PER SRAS ES_0107970_01...15483 ISSUE A, DATED 11/18/2019.

Source: SDR COEA201911227810
OTHER · 2019-10-06 Matched by certificate designator
ATA 5330

Part: SKIN — CORRODED (FRAMES 29-30) · corrosion level 2 · airframe 27,691 hrs · 30,156 cycles

WO 205731 NR 200117 HEAVY CHECK COE/MAJOR REPAIR: REAR FUSELAGE UPPER R/H SKIN INTERIOR SURFACE HAS LEVEL 2 CORROSION BETWEEN FRAMES 29-30, STRINGERS 3R-4R. CORRECTIVE ACTION: DOUBLER REPAIR PER SRAS ES_0107970_01...15483 ISSUE A, DATED 11/18/2019.

Source: SDR COEA2019112264810
OTHER · 2019-10-06 Matched by certificate designator
ATA 5330

Part: SKIN — CORRODED (FRAMES 32-33) · corrosion level 2 · airframe 27,691 hrs · 30,156 cycles

WO 205731 NR 200109 REAR FUSELAGE LOWER R/H SKIN INTERIOR SURFACE HAS LEVEL 2 CORROSION BETWEEN FRAMES 32-33 STRINGERS 12R-13R. CORRECTIVE ACTION: REPAIRED PER SRM 530000-300-805-A01.

Source: SDR COEA2019110865810
OTHER · 2019-10-06 Matched by certificate designator
ATA 5330

Part: SKIN — CORRODED (FRAMES 23-23A) · corrosion level 2 · airframe 27,691 hrs · 30,156 cycles

WO 205731 NR 200092 HEAVY CHECK COE/MAJOR REPAIR: CENTER FUSELAGE UPPER R/H SKIN INTERIOR SURFACE HAS LEVEL 2 CORROSION BETWEEN FRAMES 23-23A, STRINGERS 6AR-7R. CORRECTIVE ACTION: REPAIRED PER SRAS ES_0107986_01...15487 ISSUE A, DATED 11/20/2019.

Source: SDR COEA201911229810
OTHER · 2019-10-06 Matched by certificate designator
ATA 5330

Part: SKIN — CORRODED (FRAME 17) · corrosion level 2 · airframe 27,691 hrs · 30,156 cycles

WO 205731 NR 200085 HEAVY CHECK COE/MAJOR REPAIR: FWD FUSELAGE UPPER R/H INTERIOR SURFACE HAS LEVEL 2 CORROSION FWD OF FRAME 17 BETWEEN STRINGERS 9R-10R. CORRECTIVE ACTION: REPAIRED PER SRM 530000-300-803-A01.

Source: SDR COEA2019110864810
OTHER · 2019-10-06 Matched by certificate designator
ATA 5330

Part: SKIN — CORRODED (FRAMES 13-14) · corrosion level 2 · airframe 27,691 hrs · 30,156 cycles

WO 205731 NR 200080 HEAVY CHECK COE/MAJOR REPAIR: FORWARD FUSELAGE R/H UPPER SKIN INTERIOR SURFACE HAS LEVEL 2 CORROSION BETWEEN FRAMES 13-14, STRINGERS 5R-6R. CORRECTIVE ACTION: REPAIRED PER SRAS ES_0107816_01...15468 ISSUE A, DATED 11/15/2019.

Source: SDR COEA20191119810
OTHER · 2019-10-06 Matched by certificate designator
ATA 5330

Part: SKIN — CORRODED (FRAMES 40-41) · corrosion level 2 · airframe 27,691 hrs · 30,156 cycles

WO 205731 NR 200064 HEAVY CHECK COE/MAJOR REPAIR: REAR FUSELAGE UPPER R/H SKIN INTERIOR SURFACE HAS LEVEL 2 CORROSION BETWEEN FRAMES 40-41, STRINGERS 3R-4R. CORRECTIVE ACTION: DOUBLER REPAIR PER SRAS ES_0107970_01...15483 ISSUE A, DATED 11/18/2019.

Source: SDR COEA2019112269810
OTHER · 2019-10-01 Matched by certificate designator
ATA 5330

Part: DOUBLER — CORRODED (FRAMES 8-9) · corrosion level 2 · airframe 27,691 hrs · 30,156 cycles

WO 205731 NR 100043 HEAVY CHECK COE/MAJOR REPAIR: EXTERNAL FUSELAGE #2 DME ANTENNA DOUBLER HAS LEVEL 2 CORROSION. CORRECTIVE ACTION: REPAIRED PER SRAS ES_0108050_01...15501 ISSUE A, DATED 11/20/2019.

Source: SDR COEA2019112215810
OTHER · 2019-09-29 Matched by certificate designator
ATA 2710

Part: CONTROL ROD — CORRODED (RT AILERON) · corrosion level 2 · airframe 27,691 hrs · 30,156 cycles

WO 205731 NR 600023 HEAVY CHECK COE/MINOR REPAIR: R/H WING AILERON TAB CONTROL ROD HAS LEVEL 2 CORROSION. CORRECTIVE ACTION: REPLACED WITH OEM PART.

Source: SDR COEA2019111491810
OTHER · 2019-09-28 Matched by certificate designator
ATA 5414

Part: PANEL — CORRODED (LT NACELLE) · corrosion level 2 · airframe 27,691 hrs · 30,156 cycles

WO 205731 NR 400024 HEAVY CHECK COE/MAJOR REPAIR: L/H NACELLE PANEL LANDING FLANGE FOR OUTBOARD SIDE OF PANEL 477AB HAS LEVEL 2 FRETTING. CORRECTIVE ACTION: REPAIRED PER SRAS ES_0107238_01...15460 ISSUE A, DATED 11/5/2019.

Source: SDR COEA2019112298810
OTHER · 2019-09-28 Matched by certificate designator
ATA 5414

Part: PANEL — CORRODED (RT NACELLE) · corrosion level 2 · airframe 27,691 hrs · 30,156 cycles

WO 205731 NR 400009 HEAVY CHECK COE/MAJOR REPAIR: R/H NACELLE PANEL LANDING FOR INBOARD SIDE OF PANEL 487AB HAS LEVEL 2 FRETTING. CORRECTIVE ACTION: REPAIRED PER SRAS ES_0106922_01...15444 ISSUE A, DATED 10/31/2019.

Source: SDR COEA2019112094810
OTHER · 2019-09-28 Matched by certificate designator
ATA 5410

Part: LANDING — CORRODED (LT NACELLE PANEL) · corrosion level 2 · airframe 27,691 hrs · 30,156 cycles

WO 205731 NR 400026 L/H NACELLE LANDING FOR AFT EDGE OF PANEL 477AB HAS FRETTING. LEVEL 2 CORRECTIVE ACTION: REPLACEMENT WITH OEM PART.

Source: SDR COEA201911086810
OTHER · 2019-09-28 Matched by certificate designator
ATA 5410

Part: LANDING — CORRODED (RT NACELLE) · corrosion level 2 · airframe 27,691 hrs · 30,156 cycles

WO 205731 NR 400012 HEAVY CHECK COE/MINOR REPAIR: R/H NACELLE LANDING FOR THE AFT EDGE OF PANEL 487AB HAS LEVEL 2 FRETTING. CORRECTIVE ACTION: REPLACED WITH OEM PART.

Source: SDR COEA2019112085810
OTHER · 2019-09-28 Matched by certificate designator
ATA 5420

Part: WEB — CORRODED (LT NACELLE) · corrosion level 2 · airframe 27,691 hrs · 30,156 cycles

WO 205731 NR 400022 HEAVY CHECK COE/MINOR REPAIR: L/H NACELLE INBOARD REBATE HAS FRETTING AT THE AFT END OF PANEL 474AR, LEVEL 2. CORRECTIVE ACTION: REPLACED WITH OEM PART.

Source: SDR COEA201911128810
OTHER · 2019-09-28 Matched by certificate designator
ATA 5414

Part: PANEL — CORRODED (RT NACELLE) · corrosion level 2 · airframe 27,691 hrs · 30,156 cycles

WO 205731 NR 400008 HEAVY CHECK COE/MAJOR REPAIR: R/H NACELLE PANEL LANDING OUTBOARD SIDE OF PANEL 487AB HAS LEVEL 2 FRETTING. CORRECTIVE ACTION: REPAIRED PER SRAS ES_0106922_01...15444 ISSUE A, DATED 10/31/2019.

Source: SDR COEA2019112023810
OTHER · 2019-09-28 Matched by certificate designator
ATA 5415

Part: TEE FITTING — CORRODED (LT NACELLE) · corrosion level 2 · airframe 27,691 hrs · 30,156 cycles

WO 205731 NR 400025 HEAVY CHECK COE/MINOR REPAIR: L/H NACELLE PANEL LANDING FLANGE FOR THE INBOARD SIDE OF PANEL 477AB HAS FRETTING, LEVEL 2. CORRECTIVE ACTION: REPLACED WITH OEM PART.

Source: SDR COEA201911129810
OTHER · 2019-09-28 Matched by certificate designator
ATA 5414

Part: PANEL — CORRODED (RT NACELLE) · corrosion level 2 · airframe 27,691 hrs · 30,156 cycles

WO 205731 NR 400007 HEAVY CHECK COE/MAJOR REPAIR: R/H NACELLE REBATE PANEL LANDING (484AR) HAS LEVEL 2 FRETTING. CORRECTIVE ACTION: REPAIRED PER SRAS ES_0106922_01...15444 ISSUE A, DATED 10/31/2019.

Source: SDR COEA2019112092810
OTHER · 2019-09-27 Matched by certificate designator
ATA 5751

Part: CHANNEL — CORRODED (RT AILERON) · corrosion level 2 · airframe 27,691 hrs · 30,156 cycles

WO 205731 NR 600013 HEAVY CHECK COE/MINOR REPAIR: R/H AILERON CONTROL TAB CLOSEOUT CHANNEL HAS LEVEL 2 CORROSION. CORRECTIVE ACTION: REPLACED WITH OEM PART.

Source: SDR COEA2019112096810
OTHER · 2019-09-27 Matched by certificate designator
ATA 5751

Part: CHANNEL — CORRODED (RT AILERON) · corrosion level 2 · airframe 27,691 hrs · 30,156 cycles

WO 205731 NR 600016 HEAVY CHECK COE/MINOR REPAIR: R/H AILERON FIXED TAB CLOSEOUT CHANNEL HAS LEVEL 2 CORROSION. CORRECTIVE ACTION: REPLACED WITH OEM PART.

Source: SDR COEA2019112272810
OTHER · 2019-09-26 Matched by certificate designator
ATA 5330

Part: SKIN — DENTED (FRAME 23C) · airframe 27,691 hrs · 30,156 cycles

WO 205731 NR 205731 HEAVY CHECK COE/MAJOR REPAIR: DENTS ON CENTER FUSELAGE L/H UPPER SKIN PANEL FORWARD OF FRAME 23C BETWEEN STRINGERS 4L-7AL. CORRECTIVE ACTION: REPAIRED PER SRAS ES_0106844_01...15312 ISSUE A, DATED 11/20/2019.

Source: SDR COEA2019112296810
OTHER · 2019-09-26 Matched by certificate designator
ATA 5246

Part: DOOR — CORRODED (POTABLE WATER) · corrosion level 2 · airframe 27,691 hrs · 30,156 cycles

WO 205731 NR 200005 HEAVY CHECK COE/MINOR REPAIR: POTABLE WATER SERVICE DOOR HAS LEVEL 2 CORROSION ON EXTERIOR AND INTERIOR SURFACES. CORRECTIVE ACTION: REPLACED DOOR WITH OEM PART.

Source: SDR COEA2019110763810
OTHER · 2019-09-26 Matched by certificate designator
ATA 5730

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 27,691 hrs · 30,156 cycles

WO 205731 NR 600008 HEAVY CHECK COE/MINOR REPAIR: R/H WING FUEL PANEL 623GT HAS LEVEL 2 CORROSION AROUND SCREWS. CORRECTIVE ACTION: REPLACED WITH OEM PART.

Source: SDR COEA2019112291810
PARTIAL RPM/PWR LOSS · 2019-08-17 Matched by certificate designator
ATA 6120

Part: CONTROL UNIT — FAULTED (NR 1 PROPELLER) · airframe 27,664 hrs · 30,129 cycles

FLIGHT 1701, ENROUTE, AT 16,000 FT, THE NR 1 ENGINE TORQUE DROPPED FROM 70% TO 20% THEN RECOVERED. ALL OTHER PARAMETERS NORMAL. AFTER EXTENSIVE TROUBLESHOOTING, MAINTENANCE REPLACED THE NR 1 PROP CONTROL UNIT. ALL OPS & LEAKS CHECKS GOOD.

Source: SDR COEA2019082072810
FALSE WARNING · 2019-01-18 Matched by certificate designator
ATA 3411

Part: PITOT TUBE — OBSTRUCTED (NR 2) · airframe 27,395 hrs · 29,776 cycles

FLIGHT 1700, ENROUTE HNL - ITO DISCREPANCY: AMBER MESSAGE ON ADU DADC DATA INVALID AFTER V1, CONTINUED TAKE OFF. LOST AIRSPEED FO SIDE, NO YAW DAMP, NOT ABLE TO SET ALTITUDE. CREW RETURNED TO HNL. NO EMERGENCY DECLARED. CORRECTIVE ACTION: MAINTENANCE TROUBLESHOT AND CLEARED OBSTRUCTION FROM THE NR 2 PITOT TUBE. ALL OPS AND LEAK CHECKS GOOD.

Source: SDR COEA2019011801810

2017

OTHER · 2017-10-20 Matched by certificate designator
ATA 5313

Part: STRINGER — DAMAGED (FRAMES 17-18) · airframe 27,152 hrs · 29,450 cycles

DAMAGED STRINGER 1AL BETWEEN FRAMES 17 - 18. INSTALLED A SPLICE REPAIR IAW SRM 53-00-00-300-847-A01.

Source: SDR COEA2017102029810
OTHER · 2017-09-22 Matched by certificate designator
ATA 5313

Part: STRINGER — DAMAGED (FUSELAGE) · airframe 27,152 hrs · 29,450 cycles

BRIDGING CHECK COE/MAJOR REPAIR: STRINGER 13R HAS DAMAGED HOLE. SPLICE REPAIR SRM 530000-300-824-A01.

Source: SDR COEA2018022230810
OTHER · 2017-07-19 Matched by certificate designator
ATA 5311

Part: FRAME — CORRODED (FRM 46) · corrosion level 2 · airframe 27,152 hrs · 29,450 cycles

FOUND CORROSION ON FRAME 46 AFT SURFACE RIGHT OF BL 0 AT PASS THROUGH. REPAIRED IAW SRAS PCE-1389/17.

Source: SDR COEA2017071916810
OTHER · 2017-07-18 Matched by certificate designator
ATA 5313

Part: STRINGER — DAMAGED (FRAMES 15-16) · airframe 27,152 hrs · 29,450 cycles

DAMAGED STRINGER 2AL BETWEEN FRAMES 15 - 16. A SPLICE REPAIR WAS INSTALLED IAW SRM 53-00-00-300-847-A01.

Source: SDR COEA2017071828810
OTHER · 2017-07-16 Matched by certificate designator
ATA 5720

Part: STRIP — DAMAGED (LT WING) · airframe 27,152 hrs · 29,450 cycles

LEFT WING FRONT SPAR UPPER STRIP SLAT HAS ONE HOLE WITH DAMAGE, RIB 7 - 8. REPAIRED IAW SRAS ES-3446/17.

Source: SDR COEA2017071615810
OTHER · 2017-07-13 Matched by certificate designator
ATA 5340

Part: STRINGER CLIP — CORRODED (FRAME 13) · corrosion level 2 · airframe 27,152 hrs · 29,450 cycles

CORROSION ON STRINGER CLIP 19L, FRAME 13. REPLACED THE STRINGER CLIP.

Source: SDR COEA2017071325810
OTHER · 2017-07-13 Matched by certificate designator
ATA 5344

Part: HINGE FITTING — NICKED (EMERGENCY EXIT) · airframe 27,152 hrs · 29,450 cycles

RIGHT FUSELAGE OPENING FOR EMERGENCY EXIT, FWD LOWER HINGE FITTING IS NICKED ON BOTH EARS. REPAIRED IAW ES-3199/17.

Source: SDR COEA2017071322810
OTHER · 2017-07-13 Matched by certificate designator
ATA 5344

Part: HINGE FITTING — NICKED (EMERGENCY EXIT) · airframe 27,152 hrs · 29,450 cycles

RIGHT FUSELAGE OPENING FOR EMERGENCY EXIT, AFT LOWER HINGE FITTING IS NICKED ON BOTH EARS. REPAIRED IAW ES-3199/17.

Source: SDR COEA2017071323810
OTHER · 2017-07-13 Matched by certificate designator
ATA 5313

Part: STRINGER — CORRODED (FRAMES 12-13) · corrosion level 2 · airframe 27,152 hrs · 29,450 cycles

CORROSION FOUND ON STRINGER 21R, BETWEEN FRAMES 12 & 13. REPLACED THE STRINGER.

Source: SDR COEA2017071324810
OTHER · 2017-07-13 Matched by certificate designator
ATA 5322

Part: SHEAR TIE — CRACKED (FRAME 28D) · airframe 27,152 hrs · 29,450 cycles

FRAME 28D SHEAR TIE HAS A CRACK BETWEEN STRINGERS 1R-1AR. CORRECTIVE ACTION: REPLACED SHEAR TIE WITH NEW PART.

Source: SDR COEA2017071326810
OTHER · 2017-07-13 Matched by certificate designator
ATA 5313

Part: STRINGER — CORRODED (FRAMES 9-10) · corrosion level 2 · airframe 27,152 hrs · 29,450 cycles

STRINGER 20R BETWEEN FRAMES 9 - 10 CORRODED. REPAIRED IAW SRAS PCE-1347/17.

Source: SDR COEA2017071314810
OTHER · 2017-07-12 Matched by certificate designator
ATA 5210

Part: FITTING — DAMAGED (PAX DOOR) · airframe 27,152 hrs · 29,450 cycles

PASSENGER DOOR UPPER FWD SHOOT BOLT ROLLER FITTING HAS IMPACT DAMAGE. REPAIRED IAW SRAS PCE-1321/17.

Source: SDR COEA2017071219810
OTHER · 2017-07-12 Matched by certificate designator
ATA 5210

Part: FITTING — DAMAGED (PAX DOOR) · airframe 27,152 hrs · 29,450 cycles

PASSENGER DOOR UPPER AFT SHOOT BOLT ROLLER FITTING HAS IMPACT DAMAGE. REPAIRED IAW SRAS PCE-1321/17.

Source: SDR COEA2017092218810
OTHER · 2017-07-12 Matched by certificate designator
ATA 5210

Part: FITTING — DAMAGED (PAX DOOR) · airframe 27,152 hrs · 29,450 cycles

PASSENGER DOOR CENTER FWD SHOOT BOLT ROLLER FITTING HAS IMPACT DAMAGE. REPAIRED IAW SRAS PCE-1321/17.

Source: SDR COEA2017071220810
OTHER · 2017-07-12 Matched by certificate designator
ATA 5210

Part: ROLLER — DAMAGED (PAX DOOR) · airframe 27,152 hrs · 29,450 cycles

PASSENGER DOOR CENTER AFT SHOOT BOLT ROLLER FITTING HAS IMPACT DAMAGE. REPAIRED IAW PCE-1321/17.

Source: SDR COEA2017071221810
OTHER · 2017-07-11 Matched by certificate designator
ATA 5310

Part: LANDING — CORRODED (FRAMES 45-46) · corrosion level 2 · airframe 27,152 hrs · 29,450 cycles

AFT AVIONICS DOOR LANDING CORRODED. REPAIRED IAW SRAS PCE-1346/17.

Source: SDR COEA2017071113810
OTHER · 2017-07-07 Matched by certificate designator
ATA 5313

Part: STRINGER — GOUGED (FUSELAGE) · airframe 27,152 hrs · 29,450 cycles

HEAVY CHECK COE/MAJOR REPAIR: STRINGER 2L JUST AFT OF FRAME 16 IS GOUGED. SPLICE REPAIR SRM 53-00-00-300-847-A01.

Source: SDR COEA2017070727810

2016

OTHER · 2016-12-01 Matched by certificate designator
ATA 5340

Part: ATTACH BRACKET — CORRODED (FRAMES 36-39) · corrosion level 2 · airframe 27,152 hrs · 29,450 cycles

SERVICE DOOR THRESHOLD, UPPER SURFACE ATTACH BRACKETS AT FRAMES 36, 37 & 39 HAVE CORROSION. REPLACED ATTACH BRACKET.

Source: SDR COEA2016120109810
OTHER · 2016-12-01 Matched by certificate designator
ATA 5340

Part: ATTACH BRACKET — CORRODED (FRAMES 36-39) · corrosion level 2 · airframe 27,152 hrs · 29,450 cycles

SERVICE DOOR THRESHOLD, UPPER SURFACE ATTACH BRACKETS AT FRAMES 36, 37 & 39 HAVE CORROSION. REPLACED AFFECTED ATTACH BRACKET.

Source: SDR COEA2016120110810
OTHER · 2016-12-01 Matched by certificate designator
ATA 5320

Part: ATTACH BRACKET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,152 hrs · 29,450 cycles

BRIDGING CHECK COE/MINOR REPAIR: SERVICE DOOR THRESHOLD, UPPER SURFACE ATTACH BRACKETS AT FRAMES 36, 37 & 39 HAVE LEVEL 2 CORROSION. REPLACED AFFECTED ANGLE WITH OEM PART.

Source: SDR COEA2016120111810
OTHER · 2016-11-05 Matched by certificate designator
ATA 5210

Part: SPLICE — CORRODED (PAX DOOR) · corrosion level 2 · airframe 27,152 hrs · 29,450 cycles

AFT PAX DOOR, LOWER PAN FWD SPLICE HAS CORROSION. REPLACED FWD SPLICE.

Source: SDR COEA2016110502810
OTHER · 2016-10-12 Matched by certificate designator
ATA 5347

Part: SEAT TRACK — CORRODED (FRAMES 16-18) · corrosion level 2 · airframe 27,152 hrs · 29,450 cycles

RIGHT OTBD SEAT TRACK ABOVE STRINGER 16R HAS AREAS OF CORROSION BETWEEN FRAMES 16 & 18. REPAIRED IAW SRM 530000-300-85-A01.

Source: SDR COEA2016101204810
OTHER · 2016-10-12 Matched by certificate designator
ATA 5347

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,152 hrs · 29,450 cycles

BRIDGING CHECK COE/MAJOR REPAIR: LT INBOARD SEAT TRACK HAS LEVEL 2 CORROSION BETWEEN FRAMES 33-36. REPAIRED PER SRM 530000-200-804-A01.

Source: SDR COEA2018022233810
OTHER · 2016-10-12 Matched by certificate designator
ATA 5347

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,152 hrs · 29,450 cycles

BRIDGING CHECK COE/MAJOR REPAIR. REAR FUSELAGE RT INBOARD SEAT TRACK HAS LEVEL 2 CORROSION BETWEEN FRAMES 29-30. REPAIRED PER SRAS ES-5363/16.10967 DATED 12/26/2016.

Source: SDR COEA2016101212810
OTHER · 2016-10-12 Matched by certificate designator
ATA 5320

Part: WEB — CORRODED (FRAMES 39-40) · corrosion level 2 · airframe 27,152 hrs · 29,450 cycles

LEFT FLOOR SUPPORT WEB AT INBOARD EDGE OF LT CREASE BEAM HAS CORROSION BETWEEN FRAMES 39-40. REPAIRED IAW CETS-5083/16.

Source: SDR COEA2016101213810
OTHER · 2016-10-12 Matched by certificate designator
ATA 5320

Part: WEB — CORRODED (FRAMES 36-39) · corrosion level 2 · airframe 27,152 hrs · 29,450 cycles

PAX DOOR THRESHOLD HAS AREAS OF CORROSION BETWEEN FRAMES 36 & 39. REPLACED THE WEB.

Source: SDR COEA2016101208810
OTHER · 2016-10-12 Matched by certificate designator
ATA 5320

Part: WEB — CORRODED (FRAMES 37-37) · corrosion level 2 · airframe 27,152 hrs · 29,450 cycles

RIGHT WEBS BETWEEN FRAMES 35 & 37 OTBD OF RT SEAT TRACK HAD AREAS OF CORROSION. REPLACED THE WEB.

Source: SDR COEA2016101207810
OTHER · 2016-10-12 Matched by certificate designator
ATA 5347

Part: SEAT TRACK — DAMAGED (FRAMES 33-35) · airframe 27,152 hrs · 29,450 cycles

LEFT OTBD SEAT TRACK ABOVE STRINGER 16L HAS NICKS BETWEEN FRAMES 33 & 35. REPAIRED IAW SRM 530000-300-853-A01.

Source: SDR COEA2016101203810
OTHER · 2016-10-12 Matched by certificate designator
ATA 5347

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,152 hrs · 29,450 cycles

BRIDGING CHECK COE/MAJOR REPAIR: LT OUTBOARD SEAT TRACK HAS LEVEL 2 CORROSION BETWEEN FRAMES 14-17. SPLICE REPAIR SRM 530000-200-804-A01.

Source: SDR COEA2016101232810
OTHER · 2016-10-10 Matched by certificate designator
ATA 5740

Part: ATTACH FITTING — CORRODED (LT WING) · corrosion level 2 · airframe 27,152 hrs · 29,450 cycles

BRIDGING CHECK COE/MAJOR REPAIR: WING ATTACH FLANGE FOR FUEL PANEL 522BT HAS FRETTING, LEVEL 2. REPAIRED PER SRAS ES-4702/16...10939 DATED 12/6/2016.

Source: SDR COEA2016101034810
OTHER · 2016-10-05 Matched by certificate designator
ATA 5730

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 27,152 hrs · 29,450 cycles

WING ACCESS PANEL 523GT HAS CORROSION. REPLACED THE ACCESS PANEL.

Source: SDR COEA2016122312810
OTHER · 2016-10-01 Matched by certificate designator
ATA 5210

Part: SUPPORT ANGLE — CORRODED (PAX DOOR) · corrosion level 2 · airframe 27,152 hrs · 29,450 cycles

LT AFT PASSENGER DOOR, UNDERSIDE OF THIRD STEP FROM THE TOP HAS CORROSION AROUND NUTPLATES. REPLACED THE TREAD SUPPORT ANGLE.

Source: SDR COEA2016100103810
OTHER · 2016-10-01 Matched by certificate designator
ATA 5210

Part: SUPPORT ANGLE — CORRODED (PAX DOOR) · corrosion level 2 · airframe 27,152 hrs · 29,450 cycles

THE LEFT AFT PASSENGER DOOR, UNDERSIDE OF FORTH STEP FROM THE TOP HAS CORROSION AROUND NUTPLATES. REPLACED TREAD SUPPORT ANGLE.

Source: SDR COEA2016100104810
OTHER · 2016-10-01 Matched by certificate designator
ATA 5210

Part: SUPPORT — CORRODED (PAX DOOR) · corrosion level 2 · airframe 27,152 hrs · 29,450 cycles

LEFT AFT PASSENGER DOOR, UNDERSIDE OF SECOND STEP FROM THE TOP HAS CORROSION AROUND NUTPLATES. REPLACED TREAD SUPPORT.

Source: SDR COEA2016100102810
OTHER · 2016-10-01 Matched by certificate designator
ATA 5210

Part: SUPPORT — CORRODED (PAX DOOR) · corrosion level 2 · airframe 27,152 hrs · 29,450 cycles

THE LT AFT PASSENGER DOOR, UNDERSIDE OF TOP STEP HAS CORROSION AROUND NUTPLATES. REPLACED TREAD SUPPORT.

Source: SDR COEA2016100101810
OTHER · 2016-09-30 Matched by certificate designator
ATA 5210

Part: SUPPORT — CORRODED (PAX DOOR) · corrosion level 2 · airframe 27,152 hrs · 29,450 cycles

LEFT AFT PAX DOOR ASSY, THIRD STAIR TREAD FROM TOP HAS NUMEROUS AREAS OF CORROSION. : REPLACED TREAD SUPPORT.

Source: SDR COEA2016093001810
OTHER · 2016-09-30 Matched by certificate designator
ATA 5210

Part: SUPPORT — CORRODED (PAX DOOR) · corrosion level 2 · airframe 27,152 hrs · 29,450 cycles

BRIDGING CHECK/MINOR REPAIR, LT AFT PASSENGER DOOR STAIR ASSEMBLY, TOP STAIR TREAD SUPPORT HAS LEVEL 2 CORROSION. REPLACED WITH OEM PART.

Source: SDR COEA2016093008810
OTHER · 2016-09-30 Matched by certificate designator
ATA 5210

Part: SUPPORT — CORRODED (PAX DOOR) · corrosion level 2 · airframe 27,152 hrs · 29,450 cycles

BRIDGING CHECK/MINOR REPAIR, LT AFT PASSENGER DOOR STAIR ASSEMBLY TREAD SUPPORT HAS LEVEL 2 CORROSION. REPLACED TREAD SUPPORT WITH OEM PART.

Source: SDR COEA2016093006810
OTHER · 2016-09-30 Matched by certificate designator
ATA 5210

Part: SUPPORT ANGLE — CORRODED (PAX DOOR) · corrosion level 2 · airframe 27,152 hrs · 29,450 cycles

BRIDGING CHECK/MINOR REPAIR, LT AFT PASSENGER DOOR STAIR ASSEMBLY TREAD SUPPORT ANGLE HAS LEVEL 2 CORROSION. REPLACED WITH OEM PART.

Source: SDR COEA2016093007810
OTHER · 2016-09-30 Matched by certificate designator
ATA 5210

Part: STEP — CORRODED (PAX DOOR) · corrosion level 2 · airframe 27,152 hrs · 29,450 cycles

BRIDGING CHECK/MINOR REPAIR, LT AFT PASSENGER DOOR STEP ASSY, 2ND STAIR TREAD FROM TOP HAS LEVEL 2 CORROSION. REPLACED WITH OEM PART.

Source: SDR COEA2016093009810
OTHER · 2016-09-30 Matched by certificate designator
ATA 5210

Part: SUPPORT — CORRODED (AFT PAX DOOR) · corrosion level 2 · airframe 27,152 hrs · 29,450 cycles

LEFT AFT PASSENGER DOOR STEP ASSEMBLY, 5TH STAIR TREAD SUPPORT HAS CORROSION. REPLACED SUPPORT.

Source: SDR COEA2016122311810
OTHER · 2016-09-30 Matched by certificate designator
ATA 5210

Part: STEP — CORRODED (PAX DOOR) · corrosion level 2 · airframe 27,152 hrs · 29,450 cycles

BRIDGING CHECK/MINOR REPAIR, LT AFT PASSENGER DOOR STEP ASSEMBLY, 4TH STAIR TREAD FROM TOP HAS LEVEL 2 CORROSION. REPLACED WITH OEM PART.

Source: SDR COEA2016093010810
OTHER · 2016-09-29 Matched by certificate designator
ATA 5280

Part: SKIN — DAMAGED (LT MLG DOOR) · airframe 27,152 hrs · 29,450 cycles

BRIDGING CHECK COE/MAJOR REPAIR: LT MLG DOOR OUTER SKIN TRAILING EDGE DAMAGED AND HONEYCOMB IMPACTS AT LEVEL OF FWD HINGE FITTING. REPAIRED PER SRAS CETS-5480/16. 10973 DATED 12/30/2016.

Source: SDR COEA2016022235810
OTHER · 2016-09-28 Matched by certificate designator
ATA 5210

Part: PAN — CORRODED (PAX DOOR) · corrosion level 2 · airframe 27,152 hrs · 29,450 cycles

LEFT AFT PAX DOOR UPPER PAN TOP AFT AREA HAS CORROSION. REPLACED THE PAN.

Source: SDR COEA2016092806810
OTHER · 2016-09-28 Matched by certificate designator
ATA 5210

Part: SKIN — CORRODED (PAX DOOR) · corrosion level 2 · airframe 27,152 hrs · 29,450 cycles

LEFT AFT PAX DOOR INNER SKIN HAS AREAS OF CORROSION FROM UPPER PAN TO BEAM 4. REPLACED DOOR INNER SKIN.

Source: SDR COEA2016092805810
OTHER · 2016-09-26 Matched by certificate designator
ATA 5730

Part: LANDING — DAMAGED (LT WING) · corrosion level 2 · airframe 27,152 hrs · 29,450 cycles

BRIDGING CHECK/MAJOR REPAIR, LT WING PANEL LANDING FOR ACCESS PANEL 522CT HAS LEVEL 2 FRETTING DAMAGE. REPAIRED PER SRAS CETS-4582/16.10715 ISSUE A DATED 12/13/2016.

Source: SDR COEA2016092605810