N16607
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.
8 reports on file, 1996-09-27 – 2008-04-13.
Part: LATCH — FRAYED (R2 DOOR SLIDE) · airframe 39,350 hrs · 20,808 cycles
R-2 DOOR ESCAPE SLIDE LATCH CABLE HAS BROKEN STRANDS. REPLACED SLIDE CABLE P/N 65C19901-15 PER 737-3/5 MM 25-61-35.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 35,733 hrs · 18,920 cycles
THE EMERGENCY LIGHTS ON SEATS 15C-21C WERE FOUND INOPERATIVE. THE BATTERY AND CHARGER (M1577) WERE REMOVED AND REPLACED IAW MM 33-51-00.
Part: THROTTLE CABLE — JAMMED (NR 1 ENGINE) · airframe 30,458 hrs · 16,162 cycles
THE NR 1 THROTTLE JAMMED AND DID NOT RETARD (STUCK AT 83 PERCENT N1) ON INITIAL LEVEL OFF. THE NR 1 ENGINE WAS SHUTDOWN FOLLOWING QRH. THROTTLES SPLIT. TRIED TURNING OFF AUTOTHROTTLE TO NO AVAIL. THE NR 1 THRUST CONTROL PUSH-PULL CABLE WAS REMOVED AND REPLACED IAW MM 76-11-00, PAGE 501. OPERATIONAL CHECKS WERE GOOD. THE ENGINE WAS RUN TO 86 PERCENT N1 WITH NO DISCREPANCIES NOTED.
Part: ANGLE — CORRODED (FUSELAGE) · airframe 30,306 hrs · 16,086 cycles
INSPECTION FOUND CABIN FLOOR R-2 ENTRYWAY Z-ANGLE CORRODED AT STA 943-993, RBL 50. THE Z-ANGLE WAS REMOVED AND REPLACED IAW SRM 51-40-02.
Part: SKIN — CRACKED (FUSELAGE) · airframe 30,306 hrs · 16,086 cycles
INSPECTION FOUND A .5 INCH CRACK IN PILOT'S FORWARD WINDOW POST SKIN AT NR 1 WINDSHIELD UPPER O/B CORNER, STA 196.5, S6L. THE CRACKED AREA WAS CUT OUT AND A DOUBLER REPAIR WAS INSTALLED IAW SRM 53-10-01, FIGURE 210.
Part: SKIN — CHAFED (LE FLAP) · airframe 19,004 hrs · 9,853 cycles
INSPECTION FOUND LT WING LEADING EDGE OF NR 1 FORE FLAP CHAFED DUE TO CONTACT WITH SPOILER ACTUATOR HYDRAULIC LINE. THE LEADING EDGE OF NR 1 FORE FLAP WAS REPLACED IAW ECRA 5753-01100.
Part: SKIN — DENTED (CARGO DOOR) · airframe 19,004 hrs · 9,853 cycles
INSPECTION FOUND AFT CARGO DOOR EXTERNAL SKIN DENTED IN TWO AREAS. THE DENTED AREAS WERE REMOVED AND REPAIRS WERE INSTALLED IAW SRM 52-30-01, FIGURE 202.
Part: SEAL — LEAKING (CSD DR PAD)
THE NR 1 ENGINE OIL DECREASED TO ZERO QUANTITY AND OIL PRESSURE FLUCTUATED WHILE EN ROUTE FROM EWR TO DFW. THE AIRCRAFT WAS DIVERTED TO ATL WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND OIL LEAKAGE AT THE CSD DRIVE PAD MAGNETIC SEAL. THE SEAL WAS REMOVED AND REPLACED IAW MM 72-60-00. LEAK AND OPERATIONAL CHECKS WERE GOOD DURING ENGINE RUN.