N16646
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
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.
16 reports on file, 2001-02-24 – 2010-12-22.
Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 34,149 hrs · 18,170 cycles
EMERGENCY FLASHLIGHT AT FWD F/A JUMPSEAT DOES NOT BLINK. REMOVED AND REPLACED BATTERY, OPS CHECK OK.
Part: INDICATOR — SLOW (COCKPIT) · airframe 33,903 hrs · 18,034 cycles
FOR SDR PURPOSES ONLY. FLAPS SELECTED TO 15 NORMAL, WHEN SELECTED TO 30 RT FLAP REMAINED AT 15 AND LEFT TRAVELED BETWEEN 15-25. FOUND RT T/E FLAP NEEDLE SLOW TO MOVE BETWEEN 25-30. REPLACEDD T/E FLAP POS IND & TESTED PER AMM 27-58-00-404-004 ALL IND'S NORMAL PERFORMEDD FLAP ASYMMETRY SYS TEST AMM 27-51-00-715-075, SYS OPS NORMAL. A/C OK FOR SERVICE. INSP'D T/E FLAPS AND OPERATION, NO DISCREPANCIES FOUND.
Part: SKIN — CRACKED (FUSELAGE) · airframe 32,572 hrs · 17,326 cycles
SUPPORT TASK: STA 303 LOWER HINGE CUTOUT, BTM. FASTENER HOLE HAS CRACK INDICATION ON HFEC PROBE INSP. (REF EA.5330-03736 STEP 20). REPAIRED FUSELAGE SKIN AT L-1 DOOR LOWER HINGE CUTOUT PER EC/RA 5330-04016. SEE WIP ENTRIES FOR WORK PERFORMED. GENERATED DIP 53-DIP CTRL NUMBER 04661 TO PERFORM AN INSP PER PART 2 OF EC/RA 5330- 04016 PRIOR TO 72,262 TOTAL FLT CYCLES. BEFORE THE ACCUMULATION OF 72,326 TOTAL A/C FLT CYC, PERFORM AN INSP PER PART 2 OF ECRA. PLANNING TO CONTACT ENGR AFTER ACCUMULATION OF 66,000 TOTAL FLT CYC BUT BEFORE 67,000 TOTAL FLT CYC FOR INSP DETAIL.
Earlier reports · 2001–2009 · 13 reports
2009
Part: BATTERY PACK — DISCHARGED (FLASHLIGHT) · airframe 29,682 hrs · 15,803 cycles
DURING SCHK FOUND FWD FLIGHT ATTENDANT STATION LT EMERGENCY FLASHLIGHT INOPERATIVE. REPLACED THE FWD LEFT EMERGENCY FLASHLIGHT BATTERY AT THE FLIGHT ATTENDANT STATION PER AMM 25-64-06.
2008
Part: FITTING — CORRODED (VERTICAL STAB) · airframe 28,169 hrs · 15,003 cycles
AFT LEFT-HAND OUTBOARD VERTICAL STABILIZER FORWARD FAIL-SAFE LUG INSIDE DIAMETER HAS CORROSION. OVERSIZED BORE TO REMOVE ALL CORROSION DAMAGE, INSPECTED REWORKED AREA, INSTALLED REPAIR BUSHING AND REINSTALLED DRAG ANGLE PER ECRA 5342-01054.
Part: LUG — GOUGED (VERTICAL STAB) · airframe 28,169 hrs · 15,003 cycles
AFT RIGHT-HAND OUTBOARD VERTICAL STABILIZER FORWARD FUSELAGE FITTING BUSHING IS GOUGED. REMOVED BUSHING, REWORKED LUG AND INSTALLED OVERSIZED REPAIR BUSHING PER ECRA 5342-01053.
Part: FITTING — CORRODED (VERTICAL STAB) · airframe 28,169 hrs · 15,003 cycles
AFT RIGHT OUTBOARD VERTICAL STABILIZER FORWARD FAIL-SAFE LUG INSIDE DIAMETER HAS CORROSION. OVERSIZED BORE TO REMOVE ALL CORROSION DAMAGE, INSPECTED REWORKED AREA, INSTALLED REPAIR BUSHING AND REINSTALLED DRAG ANGLE PER ECRA 5342-01054.
Part: FRAME — CORRODED (FUSELAGE) · airframe 28,169 hrs · 15,003 cycles
FUSELAGE FRAME HAS CORROSION STATION 992 RBL-48 AT FLOORLINE. CUT OUT DAMAGED SECTION OF FRAME AND INSTALLED DOUBLER AND FILLER REF SRM 51-70-11.
Part: FITTING — CRACKED (FUSELAGE) · airframe 28,169 hrs · 15,003 cycles
CLIP IS CRACKED AT STATION 706 SL1 11. REMOVED AND REPLACED CLIP AT STATION 706 SL1 11 REF SRM 51-40-02.
Part: FRAME — CRACKED (FUSELAGE) · airframe 28,169 hrs · 15,003 cycles
STATION 867 FRAME RIGHT CRACKED BETWEEN S8 AND S9 AFT SIDE OF AIR CONDITIONING (A/C) OUTLET ASSEMBLY SUPPORT BRACKET. REPAIRED FRAME PER EA 5310-04498 OP 2.
Part: FRAME — CRACKED (BS 787 S8-9L) · airframe 28,169 hrs · 15,003 cycles
FRAME STATION 787 LEFT CRACKED BETWEEN S8 AND S9 AFT SIDE OF AIRCONDITIONING (A/C) OUTLET ASSEMBLY SUPPORT BRACKET. REPAIRED FRAME PER EA 5310-04498 OP 2.
Part: FRAME — CRACKED (FUSELAGE) · airframe 28,169 hrs · 15,003 cycles
FRAME STATION 400 LEFT CRACKED BETWEEN S8 AND S9 AFT SIDE OF AIR CONDITIONING (A/C) OUTLET ASSEMBLY SUPPORT BRACKET. INSTALLED REPAIR ANGLES PER EA 5310-04498 OP 02.
2005
Part: CONTROL PANEL — INOPERATIVE (FIRE CONTROL) · airframe 21,438 hrs · 11,460 cycles
MASTER CAUTION LIGHT & FWD PANEL OVERHEAT/DET LIGHT ILLUMINATED. A-SYS TEST WAS RUN, CHECKED NORMAL. FIVE MINUTES LATER, RED FIRE LIGHT ON CARGO DETECTION SYS ILLUMINATED AND BELL SOUNDED. QRH FOLLOWED AND LIGHT EXTINGUISHED AFTER SECOND FIRE BOTTLE DISCHARGED. AIRCRAFT RETURNED WITHOUT INCIDENT. MX FOUND NO EVIDENCE OF FIRE. FAULT WAS ISOLATED TO COCKPIT FIRE SUPPRESSION PANEL. THE FIRE SUPRESSION PANEL WAS REMOVED AND REPLACED. BOTH CARGO FIRE BOTTLES, METERING VALVE, DIVERTER VALVE, AND LINE FILTERS WERE ALSO REPLACED IAW MM 26-23-10 AND MM 26-26-10. A TEST WAS PERFORMED ON THE FIRE PANEL IAW MM 26-16-10 AND ALL TESTED GOOD. AN OPERATIONAL CHECK OF THE CARGO FIRE SYSTEM CHECKED GOOD.
2003
Part: PANEL — CRACKED (HORIZONTAL STAB) · airframe 16,162 hrs · 8,726 cycles
INSPECTION FOUND CRACKS ON THE LOWER SIDE OF THE LT HORIZONTAL STABILIZER LEADING EDGE PANEL. THE CRACKS WERE CONFINED TO THE BONDED INTERNAL DOUBLER AT ONE FASTENER HOLE, 5.2 INCHES OB OF THE STA 188 RIB. THE AREA WAS REPAIRED IAW ECRA 5510-01695.
Part: SKIN — DENTED (C-2 DOOR) · airframe 16,162 hrs · 8,726 cycles
INSPECTION FOUND C-2 DOOR OUTER SKIN DENTED ABOVE HANDLE. THE DOOR SKIN WAS REPAIRED IAW SRM 52-00-01.
2001
Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 9,974 hrs · 5,327 cycles
INSPECTION FOUND FORWARD FLIGHT ATTENDANT RT EMERGENCY FLASHLIGHT INOPERATIVE. THE FLASHLIGHT BATTERY WAS REPLACED IAW MM 25-60-00.