N784AX
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.
37 reports on file, 2000-03-26 – 2014-03-03.
Part: SKIN PANEL — CORRODED (LT WING) · airframe 55,088 hrs · 39,845 cycles
FORWARD CORNER OF UPPER TE PANEL AT INBD END OF NR 4 SPOILER RAISED. BLENDED OUT CORROSION ON MACHINED TE OF WING AT STATION WS 463 TO WS 469 & REPAIRED AREA IAW REA B657-60898. SDR INFO PN 112T3101-5, SN NSN, PART NAME WING SKIN PANEL, LOCATION WS 463 TO WS 469, FROM LT WING TE, CORROSION. ACFT WAS GROUNDED.
Part: INTERCOSTAL — CRACKED (NR 1 COWLING) · airframe 55,088 hrs · 39,845 cycles
NR 1 ENG OTBD CORE COWL HAS CRACK INSIDE ON LOWER STIFFENER BETWEEN STATION 291 & STATION 304. REMOVED CRACKED INTERCOSTAL, INSTALLED NEW INTERCOSTAL PN 314T1210-259 IAW SRM 51-40-02. SDR INFO PN 314T1210-259, SN NSN, PART NAME INTERCOSTAL, LOCATION NAC STATION 291 TO 304 .50 CRACK. ACFT WAS GROUNDED.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,088 hrs · 39,845 cycles
STRINGER TO BULKHEAD CLIP AT STATION 1702, STRINGER 3L CRACKED. R & R STRINGER CLIP STATION 1702, STRINGER 3L IAW DWG 148T2120. SDR INFO PN 148T1303Y1, CRACKED LENGTH 3/16 INCH, PART NAME CLIP, EXACT FUSELAGE LOCATION 1702 EXACT STRINGER LOCATION 3L. ACFT WAS GROUNDED.
Part: BEAM — CORRODED (RT WING) · corrosion level 2 · airframe 55,088 hrs · 39,845 cycles
RIGHT WING, LE FWD STRUCTURE AREA HAS CORROSION ON INNER PANEL FWD EDGE OF LE SPAR R AREA. LOCATED AT LES 600.10. R & R NOSE BEAM 114T2300-138 IAW DWG 114T2300 & SRM 51-40-02. SDR INFO PN 114T2300, SN NSN, PART NAME NOSE BEAM, CORRODED LEVEL 2, EXACT STRING & WING STATION LOCATION FROM LES 600 TO LES 625. ACFT WAS GROUNDED.
Earlier reports · 2000–2012 · 33 reports
2012
Part: STRINGER — CRACKED (CENTER FUEL TANK) · airframe 53,437 hrs · 38,837 cycles
CTR FUEL TANK UPPER STRINGER 17 RBL 74.81 CRACKED. CONFIRMED WITH HFEC IAW B767 NDTM PART 6 51-00-19 CRACK LENGTH 2.250. REPAIRED STRINGER AREA IAW B767 SRM 57-00-03 AND REA B657-59896-MR, ACFT WAS GROUNDED.
Part: SEAT TRACK — CRACKED (COCKPIT) · airframe 53,437 hrs · 38,837 cycles
CAPTAINS LEFT FORWARD SEAT TRACK CRACKED AT STOP ATTACH HOLES AT FORWARD END. REMOVED AND REPLACED CAPTAINS LEFT FORWARD SEAT TRACK IAW B767 200 AMM 20-11-00, ACFT WAS GROUNDED.
Part: RIB — CORRODED (LT WING) · airframe 53,437 hrs · 38,837 cycles
CORROSION, LEFT WING L/E RIB STRUCTURE AT OSS 884.73 APPROX. REMOVED AND REPLACED LEFT WING LEADING EDGE RIB STRUCTURE AT OSS 884.73 IAW B767 SRM 51-40-02, PARA 7.D, ACFT WAS GROUNDED.
Part: SEAL DEPRESSOR — DENTED (FUSELAGE) · airframe 53,437 hrs · 38,837 cycles
MAIN CARGO DOOR JAMB AFT CENTER SEAL DEPRESSOR IS GOUGED & DENTED. REMOVED AND REPLACED MAIN CARGO DOOR SEAL DEPRESSOR IAW B767 SRM 51-40-02. ACFT WAS GROUNDED.
Part: ANGLE — CORRODED (LE SLAT) · airframe 53,437 hrs · 38,837 cycles
NR 7 SLAT INBOARD LINK DOOR, AFT ANGLE CORRODED UNDER NUT PLATES. REMOVED NR 7 SLAT INBOARD LINK DOOR, REMOVED AND REPLACED ANGLE ON DOOR, RE-INSTALLED NR 7 SLAT INBOARD LINK DOOR IAW B767 AMM 57-41-59-4, B767 SRM 51-40-02, DWG 114T0129, FABRICATED REPLACEMENT ANGLE IAW DWT 114T0129, ACFT WAS GROUNDED.
Part: BRACKET — CRACKED (LE SLAT) · airframe 53,437 hrs · 38,837 cycles
BRACKET ADJACENT TO NR 6 SLAT CONTROL ROD ATTACH FITTING CRACKED. REMOVED AND REPLACED BRACKET NR 6 SLAT AT ROD ATTACH FITTING IAW B767 SRM 51-40-02, B767 AMM 51-21-00-7, ACFT WAS GROUNDED.
Part: STRIP — CRACKED (RT WING) · airframe 53,437 hrs · 38,837 cycles
RIGHT WING PANEL 621AFB HAS A CRACKED EROSION STRIP. REMOVED AND REPLACED EROSION STRIP ON PANEL 621AFB IAW B767 SRM 51-40-02, B767 MM 51-21-04-7, B767 MM 51-21-10-7, DWG114T2400, ACFT WAS GROUNDED.
Part: RIB — CORRODED (LT WING) · airframe 53,437 hrs · 38,837 cycles
CORROSION, LEFT WING SLAT NR 3 L/E NOSE BEAM AND RIB STRUCTURE AT OSS 734.04 APPROX. REMOVED AND REPLACED LEFT WING L/E RIB AT OSS 731 IAW B767 SRM 51-40-02, ACFT WAS GROUNDED.
Part: RIB — CORRODED (LT WING) · airframe 53,437 hrs · 38,837 cycles
CORROSION, LEFT WING L/E RIB STRUCTURE AT OSS 731 APPROX SLAT NR 3. REMOVED AND REPLACED LEFT WING L/E RIB AT OSS 731 IAW B767 SRM 51-40-02. ACFT WAS GROUNDED.
Part: SPAR — CORRODED (LT WING) · airframe 53,437 hrs · 38,837 cycles
CORROSION, LEFT WING FRONT SPAR, LES 419 APPROX. REMOVED & RE-INSTALLED PANELS IAW 767 SRM 51-40-02. REMOVED END FITTINGS, PULLEY BRACKET, FRONT SPAR CORD, SPLICE CAP, SPLICE PLATE FILLER. PERFORMED HFEC IAW NDTM 51-00-19. FABBED SPLICE PLATE FILLER IAW REA B657-59897, BOEING DWG 112T7001 & SB 767-54-0069, ACFT WAS GROUNDED.
2011
Part: HARNESS — MISSING (COCKPIT) · airframe 52,206 hrs · 38,172 cycles
CREW SERVICE AREA MISSING 1 DESCENT HARNESS. DEFERRED IAW MEL 21-61-1-2 CAR C. MBCB 4/26/11. PLACARD INSTALLED.
Part: UNKNOWN — DEPLOYED (CABIN) · airframe 52,067 hrs · 38,108 cycles
1 DESCENT DEVICE DEPLOYED IN SUPERNUMERARY AREA- DESCENT DEVICE REMOVED. DEF DI 68111 CODE 11. DEF 1 DESCENT DEVICE IN SUPERNUMERARY AREA-NO PASS RESTRICTIONS PER MEL 25-61.
2010
Part: PLATE — CORRODED (CARGO BAY) · airframe 51,566 hrs · 37,728 cycles
FWD LOWER CARGO BAY HAS CORROSION BY THE EDGE OF A PANEL ON A FLOOR SEAM PLATE AT STA 610 AROUND LBL 18. REMOVED CORROSION & REPAIRED AREA IAW B767-200 SRM 53-00-07 FIG 201.
Part: FRAME — CRACKED (NACELLE) · airframe 51,566 hrs · 37,728 cycles
CUT OUT LOWER FRAME IS CRACKED AT FWD END UNDER PANEL 437 ELX. REPLACED FRAME UNDER PANEL 437 ELX IAW B767 SRM 51-40-02
Part: FRAME — CRACKED (NACELLE) · airframe 51,566 hrs · 37,728 cycles
CUTOUT FRAME IS CRACKED AT FWD END UNDER PANEL 437 ERX. REPLACED FRAME UNDER PANEL 437 ERX IAW B767 SRM 51-40-2.
Part: ANGLE — CRACKED (FUSELAGE) · airframe 51,566 hrs · 37,728 cycles
ANGLE CRACKED AT STA 1395 BETWEEN S39L AND S39R. REMOVED AND REPLACED ANGLE IAW B767 SRM 51-40-02.
Part: SLAT TRACK — CORRODED (LE SLAT) · airframe 51,566 hrs · 37,728 cycles
NR 8 SLAT OUTBOARD MAIN TRACK CORRODED. REMOVED CORRODED SLAT TRACK AND INSTALLED NEW SERVICEABLE SLAT TRACK IAW B767 AMM 27-81-02-4.
2008
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 50,572 hrs · 37,149 cycles
RNO - MAINTENANCE FOUND FORWARD ENTRY DOOR EXTERIOR SLIDE EMERGENCY LIGHT INOP. REMOVED AND REPLACED LAMP HOLDER ASSEMBLY IAW AMM 33-51-06-02. OPS CHECKED GOOD.
2007
Part: WIRE — MISSING (EMERGENCY LIGHTS) · airframe 49,886 hrs · 36,820 cycles
COVER ON EMERGENCY EXIT LIGHT SWITCH MISSING WIRE. REMOVED AND REPLACED OVERHEAD EMERGENCY LIGHT/CREW 02 SWITCH PANEL IAW B767 AMM 35-51-08-4. OPS CHECKED GOOD.
Part: FSEU — DEFECTIVE (T/E FLAP) · airframe 49,036 hrs · 36,489 cycles
A 27 51 12 00 STATUS MSG; FLAP/SLAT ELEC FLAP INDICATOR INDICATES 1 WITH FLAP LEVER IN UP POSITION. REPLACED FSEU IAW B767 MM 27-51-01.
2006
Part: INTERCOSTAL — CORRODED (LT WING) · airframe 47,685 hrs · 36,008 cycles
LEFT INTERCOSTAL WAS CORRODED JUST OUTBOARD OF LEFT MAIN LANDING GEAR. REMOVED AND REPLACED LEFT INTERCOSTAL IAW B767 SRM.
Part: ATTACH ANGLE — CRACKED (NR 2 PYLON) · airframe 47,685 hrs · 36,008 cycles
NR 2 ENGINE PYLON TRAILING EDGE FAIRING AFT OUTBOARD ATTACH ANGLE WAS CRACKED. REMOVED AND REPLACED ANGLE IAW B767 SRM 51-40-02.
Part: STIFFENER — CRACKED (NOSE WHEEL WELL) · airframe 47,685 hrs · 36,008 cycles
RIGHT BUTT LINE NOSE WHEEL WELL VERTICAL STIFFENER AT STA 287 WAS CRACKED APPROX 14 INCHES DOWN FROM TOP. REPAIRED AREA IAW B767 SRM 51-70-12.
Part: SKIN — CORRODED (RT WING TE FLAPS) · airframe 47,685 hrs · 36,008 cycles
RIGHT INBOARD FLAP TRAILING EDGE PANEL BULGED AROUND NUMEROUS FASTENERS. REPLACED RIGHT INBOARD FLAP ON NR 0121 IAW B767 SRM.
2004
Part: STRUCTURE — DAMAGED (RT WING SLAT) · airframe 45,019 hrs · 35,064 cycles
EICAS MESSAGE, L/E SLAT ASYM DISPLAYED, LEADING EDGE LIGHT ILLUMINATED. REPAIRED PER REA B657-50865 FOR NON-REV FERRY FLIGHT TO REPOSITION FOR PERMANENT REPAIRS IAW GMM CHAP 1, SECT 7.04. REPLACED NR 8 SLAT IAW B767 MM 27-81-02.
Part: WINDOW — CRACKED (CABIN) · airframe 44,307 hrs · 34,825 cycles
DURING SERVICE CHECK WALK AROUND, FOUND MAIN DECK CARGO WINDOW AT STA 785-90 RIGHT SIDE CRACKED, PART OF OUTER PANE MISSING, THIRD WINDOW FORWARD OF THE OVERWING EXIT. REPLACED STA 785.90 OUTER WINDOW PANE, RIGHT SIDE, IAW 56-21-01-4. LEAK CHECKED GOOD IAW 05-51-24-2.
2003
Part: BATTERY — DEFECTIVE (EMERGENCY LIGHT) · airframe 43,498 hrs · 34,554 cycles
DURING MAINTENANCE INSPECTION, FOUND SPARE EMERGENCY BATTERY CHARGER INOP, LOWER UNIT. REPLACED EMERGENCY BATTERY CHARGER IAW AMM 33-51-00-210. OPS GOOD.
2002
Part: LATCH — DIRTY (NLG DOOR) · airframe 41,322 hrs · 33,812 cycles
UPON DEPARTURE, WHEN LANDING GEAR WAS RAISED, A LOUD NOISE WAS HEARD AND A LARGE AMOUNT OF VIBRATION WAS FELT. LANDING GEAR WAS EXTENDED AND THREE GREEN INDICATED. AIRCRAFT LANDED UNEVENTFULLY. FOUND LEFT FORWARD NOSE LANDING GEAR DOOR OPEN. MANUALLY CLOSED DOOR AND DISCOVERED DOOR NOT LATCHING PROPERLY. INSPECTED DOOR CLEARANCE AND FORWARD STOP CLEARANCE. FOUND TO BE WITHIN LIMITS. DISCOVERED EXCESSIVE DIRT AND LUBRICANT ON DOOR LATCHING MECHANISM. CLEANED AND LUBED DOOR MECHANISM. MANUALLY OPENED AND CLOSED DOOR AND GOT POSITIVE LOCK EACH TIME IAW B767 AMM 32-22-02.
Part: BUSHING — CORRODED (RT MLG) · airframe 41,141 hrs · 33,747 cycles
RIGHT MAIN LANDING GEAR LOWER AFT SIDE STRUT, LOWER FORWARD BUSHING WAS CORRODED. REPLACED THE RIGHT MAIN LANDING GEAR LOWER AFT SIDE STRUT IAW BOEING B767 MM 32-11-05.
2001
Part: FRAME — CRACKED (FUSELAGE) · airframe 39,074 hrs · 33,058 cycles
DURING EDDY CURRENT INSPECTION OF THE RIGHT OUTER CHORD FLANGE, STA 1809.5, FOUND A CRACK AT WL 25.3. CRACK STARTED AT THE FORWARD END OF FLANGE, RAN THROUGH THE FIRST AND SECOND FASTENER HOLES TO THE AFT RADIUS, REF 53-80-04, FIG 1, NOTES 1 & 2 AD 2001-09-13. FLANGE WAS REPLACED IAW SB 767-53-0078.
Part: FRAME — CRACKED (FUSELAGE) · airframe 39,074 hrs · 33,058 cycles
DURING EDDY CURRENT INSPECTION OF THE LEFT OUTER CHORD FLANGE, STA 1809.5, FOUND A CRACK AT WL 25.3. CRACK STARTED AT THE FORWARD EDGE OF FLANGE AND RAN TO THE FIRST FASTENER HOLE. REF BOEING NDT MANUAL 53-80-04, FIG 1, NOTE 2 AD 2000-09-13. FLANGE WAS REPLACED IAW SB 767-53-0078.
2000
Part: ACTUATOR — DEFECTIVE (LT MLG) · airframe 37,783 hrs · 32,659 cycles
DURING APPROACH, EICAS MESSAGE; GEAR DOORS DISPLAYED, AND DOORS AMBER LIGHT ILLUMINATED WITH GEAR DOWN. THE CREW RE-CYCLED LANDING GEAR AND THE LIGHT EXTINGUISHED. MAINTENANCE INSPECTED AND REPLACED THE LEFT MAIN GEAR FORWARD ACTUATOR, AND ADJUSTED THE LEFT MAIN LANDING GEAR DOOR SEQUENCE VALVE.
Part: SLIDE — DEPLOYED (PAX DOOR) · airframe 36,125 hrs · 32,143 cycles
ENTRY DOOR EMERGENCY SLIDE DID NOT FULLY INFLATE WHEN ACCIDENTLY DEPLOYED. REPLACED ENTRY DOOR ESCAPE SLIDE PACK IAW B767 MM 25-66-01-04.