N338NG
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.
35 reports on file, 2011-02-05 – 2015-05-14.
Part: SKIN — DENTED (ZONE 100) · airframe 8,190 hrs · 7,838 cycles
DURING HEAVY CHECK, MAINTENANCE C/W REPAIR OF MULTI FUSELAGE SKIN DAMGE IAW R/D 8/4-53-6820. ACFT REMAINS OUT OF SERVICE FOR HEAVY CHECK COMPLETION.
Part: SKIN — DENTED (ZONE 100) · airframe 8,190 hrs · 7,838 cycles
DURING HEAVY CHECK, MAINTENANCE C/W REPAIR OF MULTIBLE DENTS ON FUSALAGE IAW RD 8/4-53-6820. AIRCRAFT REMAINS OUT OF SERVICE FOR HEAVY CHECK COMPLETION.
Part: SKIN — DENTED (BS 714-728) · airframe 8,190 hrs · 7,838 cycles
WHILE ACFT WAS IN FOR HEAVY CHECK. MAINTENANCE FOUND DENT BETWEEN FS X714.602 TO X728.102 AND STR 29P TO 30P. MAINTENANCE PERFORMED "MAJOR" REPAIR ON DENT BETWEEN FS X714.602 TO X728.102 AND STR 29P TO 30P IAW RD 8/4-53-6803 AND SRM 51-21-10, 51-25-10, 51-42-05, 51-25-15 AND NDTM 51-00-01. ACFT IS CURRENTLY STILL OUT OF SERVICE FOR HEAVY CHECK.
Part: SKIN — CRACKED (ZONE 200) · airframe 8,190 hrs · 7,838 cycles
DURING HEAVY CHECK, MAINTENANCE C/W PERMANENT REPAIR OF DENT/CRACK ON LT FUSELAGE SKIN IAW RD 8/4-53-6803. ACFT REMAINS OUT OF SERVICE FOR HEAVY CHECKS COMPLETION.
Part: CHANNEL — CRACKED (ZONE 200) · airframe 8,190 hrs · 7,838 cycles
DURING HEAVY CHECK, MAINTENANCE REPORTED A THREE INCH CRACK ON THE UPPER CHANNEL ON THE WING TO FUSELAGE SUPPORT STRUCTURE UNDER PANEL 264AR. MAINTENANCE R & R THE UPPER CHANNEL ON THE WING TO FUSELAGE SUPPORT STRUCTURE UNDER PANEL 264AR IAW SRM 51-42-05 AND 51-40-07. ACFT IS CURRENTLY STILL OUT OF SERVICE FOR HEAVY CHECK COMPLETION.
Part: SKIN — DENTED (BS 281-301) · airframe 8,190 hrs · 7,838 cycles
DURING HEAVY CHECK, MAINTENANCE PERFORMED REPAIR OF DENTS ON RT FUSELAGE IAW R/D 8/4-53-6824. AIRCRAFT REMAINS OUT OF SERVICE FOR HEAVY CHECK COMPLETION.
Part: SKIN — DENTED (BS 866-882) · airframe 8,190 hrs · 7,838 cycles
WHILE ACFT WAS IN FOR HEAVY CHECK, FOUND DENT ON AFT FUSELAGE AT BS 866.303 AND 882.703. MAINTENANCE CUTOUT DAMAGED AREA AND INSTALLED DOUBLER IAW RD 8/4-55-1115 ON SKIN PN 85537506 BETWEEN FRAMES NR 1 AND NR 2 AND STR 30S-31S. ACFT REMAINS FOR COMPLETION.
Part: THRESHOLD — CORRODED (EMERGENCY EXIT) · corrosion level 2 · airframe 8,190 hrs · 7,838 cycles
DURING HEAVY CHECK, MAINTENANCE REPORTED CORROSION ON THE EMERGENCY EXIT THRESHOLD. MAINTENANCE R & R THE EMERGENCY EXIT THRESHOLD IAW SRM 51-21-00, 51-40-07, 51-42-05, 51-40-00, 51-25-15 & AMM 25-23-00 & 25-26-16.
Part: THRESHOLD — CORRODED (ZONE 100) · corrosion level 2 · airframe 8,190 hrs · 7,838 cycles
DURING HEAVY CHECK, MAINTENANCE FOUND CORROSION ON EMERGENCY EXIT THRESHOLD. R & R IAW SRM 51-42-05-02-01
Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 8,190 hrs · 7,838 cycles
DURING HEAVY CHECK, MAINTENANCE FOUND CORROSION ON SEAT TRACK NR 10. R & R SEAT TRACK IAW SRM 51-42-05-02-01,
Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 8,190 hrs · 7,838 cycles
DURING HEAVY CHECK, MAINTENANCE FOUND CORROSION ON SEAT TRACK NR 16. R & R SEAT TRACK IAW SRM 51-42-05-02-01.
Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 8,190 hrs · 7,838 cycles
DURING HEAVY CHECK, MAINTENANCE FOUND CORROSION ON SEAT TRACK NR 11. R & R SEAT TRACK IAW SRM 51-42-05-02-01.
Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 8,190 hrs · 7,838 cycles
DURING HEAVY CHECK, MAINTENANCE FOUND CORROSION ON SEAT TRACK NR 9. R & R SEAT TRACK IAW SRM 51-42-05-02-01.
Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 8,190 hrs · 7,838 cycles
DURING HEAVY CHECK, FOUND SEAT RAIL NR 10 HAS PREVIOUSLY BLENDED CORROSION ON AFT END. MX BLENDED SEAT RAIL IAW SRM 53-20-49-02-02 AND FOUND TO BE OUT OF LIMITS. R & R SEAT RAIL, PN 85328210-121 IAW SRM 51-42-05-02-01. ACFT REMAINS FOR COMPLETION.
Part: SEAT TRACK — CORRODED (NR 16) · corrosion level 2 · airframe 8,190 hrs · 7,838 cycles
DURING HEAVY CHECK, FOUND SEAT RAIL NR 16 HAS CORROSION ON AFT END UNDERNEATH CLAWS. MAINTENANCE BLENDED SEAT RAIL AND FOUND TO BE OUT OF LIMITS, R & R NR 16 SEAT RAIL IAW SRM 51-40-07-02-01, AND 51-42-05-02-01.
Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 8,190 hrs · 7,838 cycles
DURING HEAVY CHECK, MAINTENANCE FOUND CORROSION ON SEAT TRACK NR 15. R & R SEAT TRACK IAW SRM 51-42-05-02-01.
Part: SEAT TRACK — CORRODED (NR 15) · corrosion level 2 · airframe 8,190 hrs · 7,838 cycles
DURING HEAVY CHECK, FOUND SEAT RAIL NR 15 HAS CORROSION ON AFT END. MAINTENANCE BLENDED SEAT RAIL AND FOUND TO BE OUT OF LIMITS. R & R NR 15 SEAT TRACK RAIL IAW SRM 51-42-05-02-01 AND 51-40-15-02-01, PN 85338210-115. A/C REMAINS FOR COMPLETION.
Part: SEAT TRACK — CORRODED (NR 9) · corrosion level 2 · airframe 8,190 hrs · 7,838 cycles
DURING HEAVY CHECK, FOUND SEAT RAIL NR 9 HAS CORROSION ON TOP AFT END. MAINTENANCE BLENDED SEAT RAIL AND FOUND TO BE OUT OF LIMITS, R & R NR 9 SEAT RAIL IAW SRM 51-42-05-02-01 AND 51-40-15-02-01.
Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 8,190 hrs · 7,838 cycles
DURING HEAVY CHECK FOUND SEAT RAIL 11 HAS PREVIOUSLY BLENDED CORROSION ON FWD END. MAINTENANCE INSPECTED AND FOUND TO BE OUT OF LIMITS, MAINTENANCE R & R NR 11 SEAT RAIL, PN 85328210-115 IAW SRM 51-40-18-02-01, AND 51-42-05-02-01. ACFT REMAINS FOR COMPLETION.
Part: SKIN — DENTED (BS 321-341) · airframe 8,190 hrs · 7,838 cycles
DURING HEAVY CHECK, MAINTENANCE C/W PERMANENT REPAIR OF DENT ON LT FUSELAGE IAW RD 8/4-53-6774 AND 8/4-53-5330. AIRCRAFT REMAINS OUT OF SERVICE FOR HEAVY CHECK COMPLETION.
Part: SKIN — DENTED (BS 321-341) · airframe 8,190 hrs · 7,838 cycles
DURING HEAVY CHECK, FOUND DENT ON LT FUSELAGE X321 TO X341, STR 12P TO 13P FROM TEMP REPAIR RD 8/4-53-5330. MAINTENANCE INSTALLED A REPAIR DOUBLER IAW RD 8/4-53-6774, ISSUE 1.
Part: FITTING — UNKNOWN (ZONE 400) · airframe 8,190 hrs · 7,838 cycles
DURING HEAVY CHECK, MAINTENANCE C/W REAR SPAR FITTING AND ATTACHING STRUCTURE-MID-AFT NACELLE RETROFIT LT AND RT SIDES IAW EO R400EO-54-16-0001 AND SB 84-54-16, REV A. ACFT REMAINS OUT OF SERVICE FOR HEAVY CHECKS COMPLETION.
Earlier reports · 2011–2014 · 13 reports
2014
Part: BATTERY PACK — INOPERATIVE (FLASHLIGHT) · airframe 7,770 hrs · 7,445 cycles
CREW REPORTED THAT COCKPIT FLASHLIGHT WAS INOPERATIVE. MAINTENANCE R & R THE FLASHLIGHT BATTERIES IAW AMM AND OPS CHECKED GOOD.
Part: SKIN — DENTED (BS 111-124) · airframe 7,557 hrs · 7,259 cycles
BIRD STRIKE DENT DAMAGE ON RIGHT NOSE COMPARTMENT SKIN FROM BS 111 - 124. MAINTENANCE PERFORMED PERMANENT REPAIR IAW RD8/4-53-6379. ACFT RETURNED TO SERVICE.
Part: PROXIMITY SENSOR — OUT OF ADJUST (L1 DOOR) · airframe 6,854 hrs · 6,583 cycles
CREW REPORTED THAT THE L1 DOOR INDICATES OPEN WHEN IT WAS CONFIRMED CLOSED AND LOCKED. MAINTENANCE ADJUSTED THE CLOSED PROXIMITY SENSOR IAW AMM AND OPS CHECKED GOOD.
Part: CAM — WORN (SERVICE DOOR) · airframe 6,719 hrs · 6,459 cycles
CREW REPORTED THAT THE AFT RT SERVICE DOOR WOULD NOT CLOSE. MAINTENANCE INSPECTED AND FOUND A WORN PART IN THE DOOR JAM. MAINTENANCE R & R THE CAM ASSEMBLY IAW AMM AND OPS CHECKED GOOD.
Part: BATTERY PACK — INOPERATIVE (FLASHLIGHT) · airframe 6,256 hrs · 6,039 cycles
CREW REPORTED THAT THE FLIGHT DECK FLASHLIGHT WAS NOT WORKING. MAINTENANCE R & R FLASHLIGHT BATTERIES AMM AND OPS CHECKED GOOD.
2013
Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 5,897 hrs · 5,704 cycles
CREW REPORTED THAT THE COCKPIT FLASHLIGHT BATTERIES INOPERATIVE. R & R BATTERIES IAW AMM AND OPS CHECKED GOOD.
Part: BATTERY PACK — DISCHARGED (FLASHLIGHT) · airframe 5,657 hrs · 5,464 cycles
CREW REPORTED COCKPIT FLASHLIGHT WEAK. REPLACED FLASHLIGHT BATTERIES IAW AMM AND OPS CHECKED GOOD.
2012
Part: LIGHT — INOPERATIVE (CABIN) · airframe 3,796 hrs · 3,658 cycles
CREW REPORTED THAT THE F/A EMERGENCY LIGHTING NORMAL/ON PUSHBUTTON LIGHT WAS INOP. MAINTENANCE RELAMPED EMERGENCY LIGHTING AS REQUIRED PER Q400 AMM.
Part: RIB — CRACKED (WING) · airframe 2,675 hrs · 2,551 cycles
INBOARD AND OUTBOARD CLOSING RIBS CRACKED ON LEADING EDGE.
2011
Part: TAB — DAMAGED (AILERON) · airframe 2,206 hrs · 2,086 cycles
RIGHT AILERON GEAR TAB LIGHTNING STRIKE DAMAGE REPAIRED IAW TD 400-57-11-15 REV 1.
Part: DOOR — UNSECURE (CARGO BAY) · airframe 708 hrs · 660 cycles
AT LEVEL OFF AT 10,00 FT THE CREW RECEIVED THE FWD CARGO DOOR UNSAFE LIGHT. FLT TURNED BACK TO PIT. NO LOSS OF PRESSURIZATION OCCURED. CARGO DOOR WAS FOUND NOT FULLY LATCHED. ALL OPS CHECKED GOOD.
Part: TERMINAL — DIRTY (WINDSHIELD) · airframe 583 hrs · 543 cycles
PILOT LOGBOOK WRITE-UP: "SMOKE NOTED ON WINDSHIELD HEAT CONTACTOR ON LEFT SIDE W/S; W/S HEAT TURNED OFF AND SMOKE STOPPED" THOUGH THE LOGBOOK ENTRY DOES NOT STATE, THIS DISCREPANCY HAPPENED AFTER TAKEOFF FROM ALB, AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO LAND AT ALB. THE STATION LISTED IN THE "STA" BLOCK OF THE LOGBOOK WRITE-UP INCORRECTLY READS "EWR". MAINTENANCE AT ALB WAS CONTACTED AND CORRECTED THE DISCREPANCY AS FOLLOWS. REMOVED CLEANED TERMINALS RECONNECTED IAW Q400 M/M CHP 56-10-01. PERFORMED OPS CHECK IAW 30-41-00. NO FURTHER DISCREPANCIES NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.
Part: DOOR — UNSECURE (CARGO BAY) · airframe 502 hrs · 469 cycles
DURING CLIMB CREW RECEIVED A FORWARD DOOR INDICATION. CREW COMPLIED WITH CHECKLIST AND RETURNED TO FIELD IN EWR. UPON LANDING, MECHANICS DISCOVERED THAT THE DOOR WAS NOT SECURED PROPERLY. DOOR OPS CHECKED GOOD.