N816FX
Registered owner: FEDERAL EXPRESS CORP, TN (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
FUSELAGE WING ATTACHMENT FITTING, LT FWD INTERIOR FRAME 25 RIB 4 MIDDLE AFT HOLE HAS FLAW INDICATION. REPAIRED PER SRAS S535R0181. 26497 ISSUE A, DATED 11/19/2025.
STRINGER 1L BETWEEN FRAMES 38 - 39 HAD TOOLING DAMAGE. REPAIRED IAW SRM 53-00-00--300-824-A01, REV 120.
AFT CARGO DOOR FWD SHOCK STRUT MOUNT BENDING AT ATTACH POINT. REPAIRED PER ATR72 SRM 51-25-01 REV. 120.
RIGHT WING LANDING ACCESS DOOR PANEL 622CT HAS LEVEL 2 CORROSION. CORRECTIVE ACTION: REPAIRED PER SRAS DO/TS-3018/09...05261 ISSUE H, DATED 10/22/2025.
LEFT WING FWD SPAR UPPER STRIP SLAT LOWER SURFACE HAS LEVEL 2 CORROSION, RIB 0-4L. REPAIRED IAW SRAS DO/TS-4637/05. 03375 ISSUE C.
RIGHT WING FWD SPAR UPPER STRIP SLAT BOTTOM SURFACE HAS LEVEL 2 CORROSION BETWEEN RIBS 0-5R. REPAIRED PER SRAS S571K0138. 26447 ISSUE B, DATED 11/18/2025.
LEFT WING ACCESS DOOR PANEL LANDING 521DT HAS LEVEL 2 CORROSION. REPAIRED PER SRAS DO/TS-3018/09...05261 ISSUE H, DATED 10/22/2025.
LEFT WING ACCESS DOOR PANEL LANDING 522CT HAS LEVEL 2 CORROSION. REPAIRED IAW SRAS DO/TS-3018/09...05261 ISSUE H, DATED 10/22/2025.
WO 247829 NR 100036 HEAVY CHECK COE/MAJOR REPAIR: COCKPIT FLOOR LONGERON BETWEEN FRAMES 5-6 LHS HAS LEVEL 2 CORROSION. CORRECTIVE ACTION: REPLACED LONGERON PER ATR SRAS ES_0222970_01...21371 ISSUE A, DATED 10/4/2023.
WO 247829 NR 100033 HEAVY CHECK COE/MINOR REPAIR: COCKPIT FLOOR CROSSBEAM AT FR5 (L) HALF HAS LEVEL 2 CORROSION. CORRECTIVE ACTION: REPLACED FLOORBEAM 5 IAW SRM 51-25-01, 51-25-04.
WO 247829 NR 100033 HEAVY CHECK COE/MINOR REPAIR: COCKPIT FLOOR CROSSBEAM AT FR5 (R) HALF HAS LEVEL 2 CORROSION. CORRECTIVE ACTION: REPLACED FLOORBEAM 5 IAW ATR72 SRM 51-25-01, 51-25-04.
WO 247829 NR 100042 HEAVY CHECK COE/MINOR REPAIR: INTERNAL FUSELAGE, FLOORBEAM 13 TOP SURFACE BETWEEN L/H INBOARD AND R/H INBOARD SEAT TRACKS HAS LEVEL 2 CORROSION: CORRECTIVE ACTION: REPLACED FLOORBEAM 13 IAW ATR72 SRM 530000-300-853-A01.
WO 247829 NR 100034 HEAVY CHECK COE/MINOR REPAIR: FR7 FLOOR SUPPORT CROSSBEAM HAS LEVEL 2 CORROSION. CORRECTIVE ACTION: REPLACED FLOORBEAM 7 IAW ATR72 SRM 51-25-01 & 51-25-04.
WO 247829 NR 100037 HEAVY CHECK COE/MINOR REPAIR: COCKPIT FLOOR LONGERON BETWEEN FRAMES 5-6 RHS HAS LEVEL 2 CORROSION. CORRECTIVE ACTION: REPLACED LONGITUDINAL FLOOR SUPPORT IAW ATR72 SRM 51-25-01, 51-25-04.
WO 247829 NR 500015 HEAVY CHECK COE/MAJOR REPAIR: L/H WING PANEL 522CT LANDING HAS FRETTING DAMAGE. CORRECTIVE ACTION: REPAIRED 522CT LANDING PER SRAS DO/TS-3018/09...5261 ISSUE G, DATED 9/29/2023.
WO 247829 NR 600027 HEAVY CHECK COE/MAJOR REPAIR: R/H WING PANEL 622CT LANDING HAS FRETTING. CORRECTIVE ACTION: REPAIRED PER SRAS DO/TS-3018/09...5261 ISSUE G, DATED 9/29/2023.
WO 247829 NR 500017 HEAVY CHECK COE/MAJOR REPAIR: L/H WING PANEL 521DT LANDING HAS FRETTING DAMAGE. CORRECTIVE ACTION: REPAIRED PANEL LANDING PER SRAS DO/TS-3018/09...5261 ISSUE G, DATED 9/29/2023.
WO 247829 NR 500014 HEAVY CHECK COE/MAJOR REPAIR: L/H WING UPPER STRIP SLAT HAS CHAFE DAMAGE BETWEEN RIBS 4-5 UNDER SIDE, FWD SPAR. CORRECTIVE ACTION: REPAIRED PER SRAS DO/TS-4637/05...3375 ISSUE B, DATED 10/5/2023.
WO 247829 NR 100024 HEAVY CHECK COE/MINOR REPAIR: AFT CARGO DOOR THRESHOLD WEB HAS LEVEL 2 CORROSION BETWEEN FRAMES 36-39. CORRECTIVE ACTION: REPLACED THRESHOLD WEB PER ATR72 SRM 51-25-01 & 51-21-08.
WO 247829 NR 200107 HEAVY CHECK COE/MINOR REPAIR: STRINGER 2AR BETWEEN FRAMES 18-20 HAS LEVEL 2 CORROSION. CORRECTIVE ACTION: REPAIRED STRINGER IAW ATR72 SRM 530000-300-824-A01.
WO 247829 NR 800002 HEAVY CHECK COE/MAJOR REPAIR: AFT AVIONICS DOOR 851, AFT SIDE HAS CHAFE DAMAGE. CORRECTIVE ACTION: REPAIRED PER SRAS ES_0090821_01...21256 ISSUE A, DATED 10/2/2023.
WO 247829 NR 200071 HEAVY CHECK COE/MINOR REPAIR: FR28B STRINGER 3L-2R SHEAR TIE HAS LEVEL 2 CORROSION. CORRECTIVE ACTION: REPLACED SHEAR TIE AT FR28B BETWEEN STRINGERS 3L-3R IAW ATR72 SRM 51-25-01.
WO 229094 NR 800002 HEAVY CHECK COE/MAJOR REPAIR: AFT CARGO DOOR LOWER FORWARD CORNER OF EXTERNAL SKIN IS BENT. CORRECTIVE ACTION: REPAIRED PER SRAS ES_0144115_01...18078 DATED 9/9/2021, ISSUE A.
WO 229094 NR 100007 HEAVY CHECK COE/MAJOR REPAIR: INTERNAL FUSELAGE, PAX THRESHOLD UPPER SURFACE HAS LEVEL 2 CORROSION FWD AND AFT OF FRAME 38. CORRECTIVE ACTION: REPAIRED PER SRAS DO/TS-3037/09...5270 DATED 9/10/2021, ISSUE B.
WO 229094 NR 100010 HEAVY CHECK COE/MAJOR REPAIR: EXTERNAL FUSELAGE LH AFT LOWER PANEL HAS LEVEL 2 CORROSION ON THE EXTERIOR SURFACE AT THE DME ANTENNA LOCATION. CORRECTIVE ACTION: DOUBLER REPAIR PER SRM 53-11-29-300-802-B01.
WO 229094 NR 100009 HEAVY CHECK COE/MAJOR REPAIR: INTERNAL FUSELAGE, L/H M7 LONGITUDINAL FLOORBEAM IS CRACKED AT FRAME 40. CORRECTIVE ACTION: REPAIRED PER EMPIRE AIRLINES E.O. 5315-02.0
FLIGHT 8663 FAI-ANC DISCREPANCY: BURNING SMELL IN FLIGHT WITH #1 RECIRCULATION FAN FAULTING INTERMITTENTLY. NO EMERGENCY DECLARED. CORRECTIVE ACTION: MAINTENANCE DEFERRED THE ISSUE. MAINTENANCE REPLACED THE RECIRCULATION FAN. OPS CHECKS GOOD.
FLIGHT 8663 ANC-FAI DISCREPANCY: STRONG ELECTRICAL BURNING SMELL ON DESCENT, NO VISIBLE SMOKE, NO WARNINGS. CREW RAN THE ELECTRICAL SMOKE CHECKLIST. NO EMERGENCY DECLARED. LANDED WITHOUT INCIDENT. CORRECTIVE ACTION: MAINTENANCE PERFORMED INSPECTION. VERIFIED NO VISUAL ELECTRICAL ARCS OR BURNS IN WIRE BUNDLES TO AVIONICS RACKS/COMPONENTS. PERFORMED ENGINE RUNS. NO DEFECTS OR SMELLS NOTED.
FLIGHT 8299, ENROUTE AFW-TUL/ DISCREPANCY: DURING APPROACH INTO TULSA, THE CREW RECEIVED A #2 ENGINE FIRE WARNING. THE #2 ENGINE WAS SHUTDOWN AND #2 ENGINE FIRE BOTTLE WAS ACTIVATED. AN EMERGENCY WAS DECLARED. THE AIRCAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE IS CURRENTLY TROUBLESHOOTING. A SUPPLEMENTAL SDR WITH CORRECTIVE ACTION WILL BE SUBMITTED. THIS IS A SUPPLEMENTAL TO PREVIOUSLY SUBMITTED SDR COEA2019110113816 FOR CORRECTIVE ACTION: MAINTENANCE TROUBLESHOT, REPLACED LH/RH ENGINE FIRE BOTTLES, CARTRIDGES AND THE #2 ENGINE FIRE DETECTION UNIT. DISCOVERED THE #2 ENGINE FIRE SENSING ELEMENT AT 34WD CAUSING SHORT CIRCUIT. REPLACED THE ELEMENT. OPS CHECK OF FIRE DETECTION SYSTEM GOOD.
R/H LONGITUDINAL FLOORBEAM CRACKED AFT OF FRAME 23C. CORRECTIVE ACTION: REPAIRED PER EMPIRE AIRLINES E.O. 5315-02.
WO 202967 NR 2 HEAVY CHECK COE/MINOR REPAIR: LEVEL 2 CORROSION ON RT AFT NOSE LANDING GEAR DOOR AFT HINGE FITTING. CORRECTIVE ACTION: REPLACED WITH OEM PART.
WO 198725 NR 200092 HEAVY CHECK COE/MINOR REPAIR: HORIZONTAL ANGLE BETWEEN FRAMES 13-14 UNDER THE PANEL RACK HAS LEVEL 2 CORROSION. CORRECTIVE ACTION: REPLACED ANGLE CLIP WITH NEW.
WO 198725 NR 200031 HEAVY CHECK COE/MAJOR REPAIR: DAMAGED HOLE ON LT CREASE BEAM WEB BETWEEN FRAMES 13-14. CORRECTIVE ACTION: REPLACED PART BY FABRICATION.
WO 198725 NR 200030 HEAVY CHECK COE/MAJOR REPAIR: LT FRAME 13 FLOORBEAM DAMAGED ON UPPER SURFACE AT STRINGER 15. CORRECTIVE ACTION: REPAIR PER SRAS ES_0102310_01...14932 ISSUE A, DATED 9/11/2019.
L/H INBOARD SEAT TRACK HAS LEVEL 2 CORROSION FRAMES 39-41. REPLACED WITH OEM PART.
WO 198725 NR 100037 HEAVY CHECK COE/MAJOR REPAIR: FORWARD PRESSURE BULKHEAD UPPER BONDING POINT AT LBL 187.5 HAS LEVEL 2 CORROSION. CORRECTIVE ACTION: REPAIR PER SRAS DO/TS-3897/05...3326 ISSUE C, DATED 9/12/2019.
CORROSION ON MATING SURFACE OF R/H WING PANEL 623GT. REPLACED WITH OEM PART.
WO 198725 NR 600013 HEAVY CHECK COE/MAJOR REPAIR: RT OUTBOARD FLAP CENTER HINGE FITTING HAS PLAY AT THE AFT ATTACH POINT ON THE FLAP. CORRECTIVE ACTION: REPAIR PER SRM 575000-300-801-A01.
R/H CREASE BEAM WEB FRAMES 27-28 HAS GOUGES, UPPER FWD SURFACE. CORRECTIVE ACTION: REPLACED PART BY FABRICATION.
RT FLOOR SUPPORT CRACKED BETWEEN FRAMES 30-31. REPAIRED IAW E.O. 5315-02.
L/H LONGITUDINAL FLOORBEAM CRACKED AFT OF FRAME 17. REPAIRED IAWE.O. 5315-02.
FORWARD CARGO DOOR CENTER LATCH FITTING CHAFED FROM CONTACT WITH DOOR HOOK FITTING. REPAIRED IAW ES-3571/17.
AFT LT NLG DOOR MIDDLE FITTING HAS CORROSION. REPLACED THE FITTING.
RIGHT OTBD FLOOR SUPPORT IS CRACKED BETWEEN FRAMES 28 - 28A. REPAIRED IAW E.O. 5315-2.
HEAVY CHECK COE/MAJOR REPAIR: PANEL 522CT LANDING HAS LEVEL 2 FRETTING CORROSION. REPAIR PER SRAS DO/TS-3018/09. 5261 DATED 8/16/2017.
PANEL 622CT LANDING CORRODED. REPAIRED IAW DO/TS-3018/09.
PANEL 521DT LANDING CORRODED. REPAIRED IAW DO/TS-2018/09.
FRAME 24, LT OUTBOARD LONGITUDINAL FLOOR SUPPORT CRACKED. REPAIRED IAW EO 5315-01.
FRAME 23D LT OTBD LONGITUDINAL FLOOR SUPPORT CRACKED. REPAIRED IAW EO 5315-01.
RT OUTBOARD SEAT TRACK FRAMES 24 - 25, GOUGED AND DENTED. REPAIRED THE SEAT TRACK IAW SRM 53-00-00-300-853-A01.
FORWARD CARGO DOOR CENTER HOOK FITTING HAS WEAR DAMAGE. REPAIRED IAW ES-3450/17.
LEFT ENGINE NACELLE INBOARD LATERAL PANEL LANDING HAS CHAFING AND CORROSION. REPAIRED IAW SRAS PCE-1570/17.
WO 148276 NR 500040 HEAVY CHECK COE & MAJOR REPAIR. LT WING, OUTER BOX, UPPER FIXED PANEL HAS CHAFE DAMAGE ON THE LANDING FOR PANEL 523GT. REPAIR IAW SRAS ES 4336 15 9597 DATED 9 10 2015.
HEAVY CHECK COE & MAJOR REPAIR. REAR CTR FUSELAGE, RT LATERAL LOWER SKIN PANEL HAS AREAS OF TOOLING MARKS & LIGHT CORROSION. REPAIR IAW SRAS S536R0256 9574 DATED 9 3 2015.
HEAVY CHECK COE & MINOR REPAIR. LT ELEVATOR OTBD END CLOS OUT FITTING HAS LEVEL 2 CORROSION. REPLACED WITH NEW OEM PART.
WO 148276 NR 200064 HEAVY CHECK COE & MAJOR REPAIR. LT SUB FRAME 27A HAS WEAR DAMAGE FROM WIRE CONDUIT. REPAIR IAW SRAS CE-4077 15 9479 DATED 8 6 15.
WO 148276 NR 200060 HEAVY CHECK COE & MAJOR REPAIR. FIRST OFFICERS SEAT FITTING HAS LEVEL 2 CORROSION ON 3 OF 4 RAISED AREAS COMMON TO NUTPLATES. REPAIR PER SRAS CE-4120 15 9480 DATED 8 6 15.
WO 148276 NR 500033 HEAVY CHECK COE & MAJOR REPAIR. UPPER WING PANEL LANDING FOR PANEL 521DT HAS FRETTING. REPAIR IAW SRAS DO TS 3018 09 5261 ISSUE D DATED 7 31 15.
WO 148276 NR 300014 HEAVY CHECK COE & MINOR REPAIR. RT ELEVATOR OTBD ON THE AFT END CLOSE OUT FITTING HAS LEVEL 2 CORROSION. REPLACED WITH NEW OEM PART.
HEAVY CHECK COE & MAJOR REPAIR. LEFT VERTICAL STABILIZER SKIN HAS FRETTING DAMAGE, LEVEL 2, ABOVE THE UPPER VORTEX GENERATOR. REPAIRED IAW SRAS CE-4167/15 9528 DATED 8 13 15.
WO 148276 NR 500034 HEAVY CHECK COE & MAJOR REPAIR. UPPER WING PANEL LANDING FOR PANEL 522CT HAS FRETTING. REPAIR IAW SRAS DO TS 3018 09 5261 ISSUE D DATED 7 31 15.
HEAVY CHECK COE & MAJOR REPAIR. UPPER WING PANEL LANDING FOR PANEL 622CT HAS FRETTING. REPAIR IAW SRAS DO TS 3018 09 5261 ISSUED DATED 7 31 15.
HEAVY CHECK COE & MAJOR REPAIR. RT ENG NACELLE PANEL LANDING AT STATION 3197 HAS LEVEL 2 FRETTING & CORROSION ON THE OTBD SIDE. REPAIR PER SRAS CE-4126 15 9493 DATED 8 7 15.
HEAVY CHECK COE & MAJOR REPAIR. LT CREASE BEAM WEB BETWEEN FRAMES 19 - 20 HAS TOOLING DAMAGE. REPLACED PART BY FABRICATION.
HEAVY CHECK COE & MAJOR REPAIR. FWD PRESS BULKHEAD HAS BURN MARK RBL 10 IN. REPAIR IAW SRAS DO TS-3897 05 3326 DATED 8 4 15.
WO 148276 NR 500019 HEAVY CHECK COE & MAJOR REPAIR. LT FLAP SUPPORT BEAM AT RIB 13 HAS PLAY & FRETTING AT THE LOWER WING ATTACH POINT, LEVEL 2 CORROSION. REPAIR IAW SRAS CE 4020 15 9565 DATED 8 27 2015.
HEAVY CHECK COE & MAJOR REPAIR. LT FRAME 39 DOUBLER AT FLOOR LEVEL HAS LEVEL 2 CORROSION. REPAIR IAW SRAS CE-3965 15 9444 DATED 7 24 15.
HEAVY CHECK COE & MAJOR REPAIR. STRINGER 2AR HAS TOOLING MARKS & CORROSION FRAME 16 - 17. REPAIR IAW SRM 53-00-00-300-824-A01.
WORK ORDER 148276 NR 200019 HEAVY CHECK COE & MAJOR REPAIR. STRINGER 7R HAS A CRACK, FRAME 13 - 14. REPAIRED USING SRM 530000-300-824-A01.
DURING HEAVY CHECK, FUEL PANEL 521DT HAS FRETTING CORROSION ON UNDERSIDE OF PANEL. REPLACED PANEL WITH OEM PART.
DURING HEAVY, LT HORIZONTAL STAB L/E HAS CORROSION UNDER DEICE BOOT. BLENDED.
DURING HEAVY CHECK, LT WING ACCESS PANEL 521DT HAS FRETTING DAMAGE. REPAIR IAW SRAS DO/TS-3018/09, 5261, ISSUE C.
DURING HEAVY CHECK, LT INBD SEAT TRACK HAS WEAR DAMAGE WITH POSSIBLE CORROSION BETWEEN FR15 TO FR18. SPLICE REPAIR IAW SRM 53-00-00, FIG 454, REV 86.
DURING HEAVY CHECK, RT WING ACCESS DOOR CUTOUT FOR PANEL 622CT HAS FRETTING DAMAGE. REPAIRED IAW SRAS DO/TS-3018/09, 5261, ISSUE C. MAJOR REPAIR.
DURING HEAVY CHECK, LT WING ACCESS PANEL 522CT HAS FRETTING DAMAGE. REPAIR IAW SRAS DO/TS-3018/09, 5261, ISSUE C.
DURING HEAVY CHECK, RT ENGINE COWL 445AT INBD OUTER CHANNEL SECTION IS CRACKED. REPLACED WITH OEM PART.
DURING HEAVY CHECK, LEFT CARGO FLOOR SUPPORT IS CRACKED AT FRAME 30. REPAIRED IAW EO 5315-02.
DURING HEAVY CHECK, RT CARGO LONGITUDINAL FLOOR SUPPORT IS CRACKED AT FR18. SPLICE REPAIR IAW EO 5315-02.
DURING HEAVY CHECK, AFT CARGO DOOR THRESHOLD HAS CORROSION. REPLACED THRESHOLD WEB WITH OEM.
DURING HEAVY CHECK, LEFT SEAT TRACK AT FRAME 38 HAS CORROSION. REPLACED WITH OEM PART.
DURINGHEAVY CHECK, LT INBD SEAT TRACK AT FRAME 27 HAS A MOUNT CLAW ABOVE FR27 THAT IS BENT DOWN TO THE CENTER OF THE TRACK. SPLICE REPAIR IAW SRM 53-00-00, FIG 454.
DURING HEAVY CHECK, LT CARGO LONGITUDINAL FLOOR SUPPORT IS CRACKED AT FRAME 28D. REPLACED FLOOR SUPPORT IAW WASB-15 M7 ICAW, DWG 72-7005.
DURING HEAVY CHECK, RT CARGO LONGITUDINAL FLOOR SUPPORT IS CRACKED AT FRAME 28. REPLACED FLOOR SUPPORT IAW WASB-15 M7 ICAW, DWG 72-7005.
DURING HEAVY CHECK, STRINGER 1A LT IS CRACKED AT FRAME 20. INSTALLED STRINGER SPLICE IAW SRM REV 86 53-00-00, FIG 426.
PANEL P/N S57112378-200 HEAVY CHECK / MAJOR REPAIR: LEFT WING LOWER SKIN AT RIB 13 JOINT HAS CHAFE FROM PANEL 552AB SEAL. BLENDED OUT AND REPAIRED (PANEL P/N S57112378-200) PER SRAS DT/S-3140/12..7177 LEFT WING SURFACE SKIN AT RIB 13 JUNCTION FITTING BL4750 BETWEEN STIFFENERS 8-10.
HEAVY CHECK / MAJOR REPAIR: LEFT WING LOWER SKIN AT RIB 13 JOINT HAS CHAFE FROM PANEL 552AB SEAL. BLENDED OUT AND REPAIRED PER SRAS DT/S-3140/12..7177 LEFT WING LOWER SURFACE SKIN AT RIB 13 JUNCTION FITTING BL 4750 BETWEEN STIFFENERS 8-10.
HEAVY CHECK / MAJOR REPAIR: OVERSIZED FASTENER HOLE IN STRINGER COMMON TO M7 HARD POINT ASSEMBLY AT NET NR 2 (FS 344.5) STR 11R FRAMES 19 - 20. REPAIRED AND COMPLIED WITH M7 VERTICAL NET HARDPOINT ZN2 BRACKET ALTERATION ON STRINGER 11R PER M7 DRAWING 72R1101-02.
HEAVY CHECK / MAJOR REPAIR: LEFT WING LOWER SKIN AT RIB 13 JOINT HAS CHAFE FROM PANEL 552AB SEAL. BLENDED OUT AND REPAIRED PER SRAS DT/S-3140/12..7177 LEFT WING LOWER SURFACE SKIN AT RIB 13 JUNCTION FITTING BL 4750 BETWEEN STIFFENERS 8-10.
HEAVY CHECK / MAJOR REPAIR: FOUND GOUGES AND MINOR CORROSION ON FUSELAGE SKIN AT ADF ANTENNA LOCATION. REMOVE EXISTING DOUBLER PERFORM EDDY CURRENT INSP, RESTORE AND INSTALL NEW STRUCTURE AT NET NR 6 (FS 680.27). SRM REPAIR FUSELAGE SKIN CROWN PANEL UNDER ADF ANTENNA DOUBLE BETWEEN FR 28C & 28D, BETWEEN STR 1R & 1L.
HEAVY CK COE / MAJOR REPAIR: STRINGER 7AL HAS A DENT BETWEEN FRAME 23D - 24. REPAIRED BY INSTALLING STRINGER SPLICE PER SRM AT STRINGER 7AL, 48 INCHES FWD OF FR 25 (23C-23D) TO FR25.
HEAVY CK COE / LEVEL 2 CORROSION: RT WING SPRING BRACKETS FOR PANEL 631AB HAS LEVEL 2 CORROSION ON SURFACE. (LENGTH 2.5", WIDTH 3.5", DEPTH .009") REMOVED AND REPLACED SPRING BRACKET.
HEAVY CK COE / LEVEL 2 CORROSION: RT WING INBOARD AND CENTER SPRING BRACKET FOR PANEL 631BB HAS LEVEL 2 CORROSION ON SURFACE. (LENGTH 5.5", WIDTH 3.5", DEPTH .009") REMOVED AND REPLACED SPRING BRACKET.
LINE 1 HEAVY CK COE / MAJOR REPAIR: INTERCOSTAL AT STR 12AR FR 17-18 HAS DENT. REPAIR PER ATR72 SRM.
HEAVY CK COE / MAJOR REPAIR / LEVEL 2 CORROSION FLIGHT DECK FIRST OFFICERS SEAT MOUNT HAS MULTIPLE AREAS OF CORROSION ON TOP SURFACE. REPAIR PER STRUCTURAL REPAIR INSTRUCTIONS FROM ATR AND REF AERITALIA DWG S53173206.
HEAVY CK COE / MAJOR REPAIR / LEVEL 2 CORROSION FLIGHT DECK CAPTAIN'S SEAT MOUNT HAS MULTIPLE AREAS OF CORROSION ON TOP SURFACE. REPAIR PER STRUCTURAL REPAIR INSTRUCTION FROM ATR AND REF AERITALIA DWG S53173206.
HEAVY CK COE / MAJOR REPAIR / LEVEL 2 CORROSION LT WING SKIN UPPER ACCESS DOOR 522CT CUT OUT FLANGE HAS LEVEL 2 CORROSION. REPAIR PER ATR72 STRUCTURAL REPAIR MANUAL AND SRAS FROM ATR.
HEAVY CK COE / MAJOR REPAIR / LEVEL 2 CORROSION / RT WING ACCESS DOOR 622CT CUT OUT FLANGE HAS FRETTING ON UPPER SURFACE AND AROUND TOP OF INNER SURFACE (LEVEL 2 CORROSION). REPAIR PER ATR72 STRUCTURAL REPAIR MANUAL AND SRAS FROM ATR.
HEAVY CK COE / MAJOR REPAIR: STRINGER 2AL HAS DENTS AND CRACKS AT FRAME 23. FABRICATED AND INSTALLED NEW STRINGER SECTION AND SPLICE IAW STRUCTURL REPAIR MANUAL.
HEAVY CK COE / MAJOR REPAIR: STRINGER 1R AT FRAME 20 HAS CRACK AT DRAIN HOLE. REPAIR PER ATR 72 STRUCTURAL REPAIR MANUAL.
HEAVY CK COE / MAJOR REPAIR: STRINGER 1AR AFT OF FRAME 20 HAS CRACK COMMON TO DRAIN HOLE. REPAIR PER ATR 72 STRUCTURAL REPAIR MANUAL.
HEAVY CK COE / MAJOR REPAIR: STRINGER 1R FORWARD SIDE OF FRAME 23 HAS DENTS AND CRACK. REPAIR PER ATR72 STRUCTURAL REPAIR MANUAL.
HEAVY CK COE / MAJOR REPAIR: SKIN HAS A DRILL START AT FRAME 17 STR 1AL-2L. REPAIR PER ATR72 STRUCTURAL REPAIR MANUAL.
HEAVY CK COE / MAJOR REPAIR: STRINGER 7R FORWARD OF FRAME 25 HAS GOUGES. STRINGER SPICE REPAIR PER ATR72 STRUCTURAL REPAIR MANUAL.
HEAVY CK COE / MAJOR REPAIR: RT LONGITUDINAL FLOORBEAM FR 38-39 CRACKED. REPLACE SECTION OF RT LONGITUDINAL FLOORBEAM BETWEEM FRAMES 36-40 IAW M7 SB WITH REFERENCE TO M7 STC.
HEAVY CK COE / MAJOR REPAIR: RIGHT SIDE M7 LONGITUDINAL FLOORBEAM BETWEEN FRAMES 23 AND 23A BROKEN. REPLACE SECTION OF RT LONGITUDINAL FLOORBEAM IAW M7 SB.
WO 103198 NR 200009 HEAVY CK COE / MAJOR REPAIR: DISCREPANCY: STRINGER 1R AT AFT SIDE OF FRAME 23 IS DENTED AND CRACKED. CORRECTIVE ACTION: REPAIR PER STRUCTURAL REPAIR MANUAL.
HEAVY CK COE / MAJOR REPAIR: FRAME 28D IS CORRODED ON THE AFT SIDE STR 21L-21R LOWER FLANGE AND WEB AT BL 0. REPAIR PER STRUCTURAL REPAIR INSTRUCTIONS FROM ATR AND SRM.
HEAVY CK COE / MAJOR REPAIR: CENTER LONGITUDINAL FLOORBEAM FR 28D-29 IS CRACKED. REPLACE SECTION OF CENTER LONGITUDINAL FLOORBEAM IAW M7 SB 72-53-015.
HEAVY CK COE / MAJOR REPAIR: LT LONGITUDINAL FLOORBEAM FR 23B-23C IS CRACKED. REPLACE FLOORBEAM SECTION IAW M7 SB 72-053-015.
HEAVY CK COE / MAJOR REPAIR / LEVEL 2 CORROSION: SERVICE DOOR THRESHOLD HAS AREAS OF CORROSION BEYOND LIMITS AND MISSING SURFACE PROTECTION ON THE UPPER SURFACE. REPAIR PER STRUCTURAL REPAIR MANUAL BY FABRICATING AND INSTALLING THRESHOLD.
HEAVY CK COE / MAJOR REPAIR / LEVEL 2 CORROSION: INTERIOR FUSELAGE SKIN AT FR 28D COMMON TO NUT PLATES 1'-6" RIGHT OF BL 0 HAS LEVEL 2 CORROSION. REPAIR PER STRUCTURAL REPAIR INSTRUCTIONS FROM ATR AND SRM.
HEAVY CK COE / MAJOR REPAIR: INTERIOR FUSELAGE SKIN AT FR28D COMMON TO NUT PLATES 1" - 6" LEFT OF BL 0 HAS LEVEL 2 CORROSION. REPAIR PER STRUCTURAL REPAIR INSTRUCTIONS FROM ATR.
HEAVY CK COE / MAJOR REPAIR: FORWARD PRESSURE BULKHEAD UPPER LT BONDING POINT HAS FRETTING AND A DENT. REPAIR PER ATR72 STRUCTURAL REPAIR MANUAL.
HEAVY CK / COE / MAJOR REPAIR: FRAME 20 HAS OVERSIZED AND OUT OF ROUND HOLE IN FRAME TIE NEAR STR13L. REPAIR PER STRUCTURAL REPAIR INSTRUCTION FROM ATR.
HEAVY CK COE / MAJOR REPAIR: FRAME 24 HAS 3 DRILL STARTS AND SCRATCHES BLENDED ON FORWARD SIDE BETWEEN STR 2AL - 3L. REPAIR PER STRUCTURAL REPAIR INSTRUCTIONS FROM ATR.
HEAVY CK COE / MAJOR REPAIR / LEVEL 2 CORROSION: RT OUTBOARD AILERON HINGE FITTING AT RIB 31 HAS LEVEL 2 CORROSION ON INBOARD SIDE AT BONDING STRAP ATTACH HOLE. REPAIR PER STRUCTURAL REPAIR INSTRUCTIONS AND SRM.
COE HEAVY CK / MAJOR REPAIR: FRAME 20, FRAME TIE RIVET OVERSIZED AND OUT OF ROUND HOLE ON FRAME 20 LT COMMON TO THE SPLICE AT STR 13. REPAIR PER STRUCTURAL REPAIR INSTRUCTIONS FROM ATR.
COE HEAVY CK / MAJOR REPAIR: INTERNAL FUSELAGE UPPER PRESSURE DECK LT SPLICE ANGLE FR 27 STR 4 IS CRACKED WITH CRACK EXTENDING INTO THE SIDE BOX INTERCOSTAL. UPPER PRESSURE DECK ANGLE CRACKED AT FR 27 APPEARS TO HAVE PROPAGATED BEYOND PREVIOUS REPORTED MARK ON SRAS 4920/05...3364, ALSO FOUND PART BETWEEN FR 27-28 CRACKED. CRACK ON P/N S53573201210 IS 2.6" LONG APPROX 1" ABOVE STR 4L. CRACK ON P/N S53373201204 IS APPROX 1.6" LONG APPROX 1" ABOVE STRINGER 4L. REPAIR PER STRUCTURAL REPAIR INSTRUCTIONS FROM ATR.
COE HEAVY CHECK/ MAJOR REPAIR: INTERNAL FUSELAGE UPPER PRESSURE DECK RT SPLICE ANGLE FR 27 STR 4 IS CRACKED. UPPER PRESSURE DECK ANGLE CRACKED AT FR 27 APPEARS TO HAVE PROPAGATED BEYOND PREVIOUS REPORTED MARK ON SRAS 4920/05...3364. CRACK ON P/N S53573201211 IS 2.1" APPROX 1" ABOVE STR 4R. REPAIR PER STRUCTURAL REPAIR INSTRUCTIONS FROM ATR.
ANC FLIGHT 8663: AIR TURNBACK AND ENGINE SHUT DOWN: ON CLIMBOUT NP DROPPED 20-30 PERCENT W/POPPING NOISE & A/C SHUTTER ACCOMPANIED BY MFC 1B FAULT. CREW SHUT DOWN THE NUMBER ONE ENGINE; DECLARED AN EMERGENCY. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED NR 1 MFC IAW ATR-72 JIC-31-48-81-RAI-10000. OPS CHECK IAW ATR-72 JIC-31-48-81-RAI-10000. FUNCTION CHECKS GOOD.
FAI FLT 7663 ABORTED TAKEOFF. EFIS COMP HEADING FAULT LIGHT ILLUMINATED ON TAKEOFF. PILOT ABORTED TAKEOFF AND TAXIED BACK TO RAMP. MAINTENANCE REMOVED AND REPLACED THE LT AHRU UNIT. AIRCRAFT RETURNED TO SERVICE.
FLIGHT NR 8663 FROM ANC, EFIS WARNING LIGHT ILLUMINATED ON TAKEOFF ROLL. AIRCRAFT RETURNED TO RAMP. MAINTENANCE REMOVED AND REPLACED AHRU. AIRCRAFT RETURNED TO SERVICE.
FLIGHT NR 8663 FROM ANC, EFIS WARNING LIGHT ILLUMINATED ON TAKEOFF ROLL. AIRCRAFT RETURNED TO RAMP. MAINTENANCE REMOVED AND REPLACED AHRU. AIRCRAFT RETURNED TO SERVICE.
HEAVY CHECK: FOUND LEVEL 2 CORROSION ON LT WING OTBD FLAP, INBD HINGE FITTING AT LOWER HINGE POINT. REMOVED AND REPLACED LT OTBD FLAP INBD FITTING ASSY.
HEAVY CHECK: FOUND LEVEL 2 CORROSION ON AFT PASSENGER DOOR THRESHOLD.
HEAVY CHECK: FOUND LEVEL 2 CORROSION ON LT WING FEEDER TANK CUTOUT FLANGE FOR UPPER ACCESS PANEL 522CT.
RT WING FRONT SPAR UPPER FLANGE ANGLE IS SHOWING WEAR MARKS. RT WING FRONT SPAR TOP FLANGE HAS FRETTING DAMAGE WHERE THE ANTI CHAFE STRIP IS WORN THROUGH. REPAIRED BY BLENDING DAMAGED AREA AND LEAVING AS IS. (S)
LEVEL 2 CORROSION. SURFACE CORROSION ON MATTING SURFACE OF PANEL 521DT. BLENDOUT OF CORROSION BLENDED BEYOND SRM LIMITS. S/D HC AT COE. REMOVED AND REPLACED DRY BAY ACCESS PANEL 521DT. (S)
TOOL DAMAGE TO FWD SIDE OF FWD PRESSURE BULKHEAD. THREE SMALL NICKS FOUND AT THE LT UPPER RADOME BONDING CONTACT POINT. S/D HC AT COE. S/D SRM REPAIR, BLENDED OUT DAMAGE AND INSTALLED REPAIR DOUBLER TO THE BULKHEAD WEB. (S)
LEVEL 2 CORROSION: LT WING FUEL OVERFLOW/VENT TANK NACA DUCT (AIR INTAKE DUCT) FLANGE HAS AREAS OF SURFACE CORROSION. CORROSION BLENDOUT TO MATTING SURFACE OF FLANGE WAS BLENDED BEYOND SRM LIMITS. REMOVED & REPLACED DUCT ASSEMBLY. (S)
ENG FAILURE: DURING WALK AROUND BETWEEN FLIGHTS, THE FLIGHT CREW NOTICED THAT THE RT PROP WAS HARD TO SPIN. A CLOSER LOOK AT THE ENGINE DISCOVERED FINE PIECES OF METAL IN THE TAIL PIPE. REMOVED AND REPLACED THE RT ENG. (S)
AIR TURN BACK. FLT NR 8663, CREW RECEIVED A LEVEL 3 CAP ALERT LANDING GEAR NOT DOWN FOLLOWED BY A STICK PUSHER/ STICK SHAKER FAULT, TERRAIN ALERT WARNING SYS (TAWS) WARNING, RADIO ALTIMETER WENT TO 0. CREW ELECTED TO RETURN TO DEPARTURE, AIRCRAFT LANDED NORMALY AND SAFELY. (K)