N125NK
Registered owner: NORMAN KRAMER E, SD (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
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.
7 reports on file, 1996-02-13 – 1997-05-21.
Part: BATTERY PACK — DISCHARGED (CABIN)
DTW - FLT 621 - RIGHT OVERWING EXIT LIGHT INOPERATIVE. FOUND LIGHT SOCKET BROKEN AND BATTERY PACK BATTERIES LOW, REPLACED LIGHT ASSY AND BATTERY PACK BATTERIES. (X)
Part: PS4 LINE — BROKEN (NR 2 ENGINE)
CHS - FLT 301 - RIGHT NR 2 ENGINE LOST PARTIAL POWER FROM 1.95 TO 1.6 FOR A FEW MINUTES AND THEN SPOOLED DOWN TO IDLE. WOULD NOT PRODUCE MORE THAN 1.1 FPR. FOLLOWED CHECKLIST AND LANDED AT CHS. FOUND BROKEN PS4 LINE IN FAN DUCTED AREA. REMOVED AND REPLACED LINE IAW PRATT AND WHITNEY MM 72-00. PERFORMED HIGH POWER CHECK, CHECKS GOOD. (M)
Part: CONNECTOR — LOOSE (APU)
ACY - FLT 514 - DURING PUSH BACK AT RSW, APU SHUT ITSELF DOWN FOR NO REASON. A RESTART WAS SUCCESSFUL, BUT APU AGAIN SHUT ITSELF OFF AFTER APPROXIMATELY 30 SECONDS. FOUND LOOSE CANNON PLUG ON CENTRIFUGAL SWITCH, SECURED, AND SERVICED OIL IAW 49-60-1. OPS CHECK GOOD. (X)
Part: SWITCH — FAILED (LT TR UNIT)
DTW - FLT 905 - LEFT THRUST REVERSER UNLOCK LIGHT STAYED ON AFTER DEPLOYMENT. DEFERRED IAW MEL 78-1, CAT 'C' DMI NR 00210. REMOVED AND REPLACED REVERSER UNLOCK LIGHT MICROSWITCH IAW DOUGLAS DC-9 MM CHAPTER 78. OPS CHECK NORMAL SEVERAL TIMES. CLEARS DMI NR 00210.
Part: CONNECTOR — CORROSION (LT MLG DNLOCK)
LOG PAGE 028581. AIR RETURN. AFTER TAKEOFF, GEAR RETRACTED. LEFT MAIN LANDING GEAR INDICATED DOWN WITH NO RED (UNSAFE) LIGHT. DOOR LIGHT WAS OUT. GEAR INDICATION NORMAL, LANDING NORMAL. CORRECTIVE ACTION: FOUND MINOR CORROSION IN LEFT MAIN GEAR DOWNLOCK SWITCH CONNECTOR. CLEANED CORROSION, SWUNG GEAR IAW DC-9MM, CHAPTER 32-60-0, 4 TIMES, OPS CHECKED GOOD. (X)
Part: RELEASE MECH — OUT OF ADJUST (TAIL CONE)
LOG PAGE 027001. TAIL CONE FAILED TO RELEASE DURING TAIL CONE RELEASE SYSTEM CHECK. ADJUSTED TAIL CONE RELEASE SYSTEM MECHANISM IAW DC-9 MM 53-50-0. OPS CHECKS GOOD. (X)
Part: OIL FILTER — LEAKING (NR 1 ENGINE)
LOG PAGE 03409 - LEFT ENGINE LOST OIL QUANTITY. ENGINE SHUT DOWN WITH 3 QUARTS OF OIL REMAINING. FOUND OIL LEAK COMING FROM MAIN OIL FILTER. INSTALLED NEW FILTER, REPLACED PACKINGS, SERVICED OIL. OPS AND LEAK CHECK GOOD IAW DC-9 MM CHAPTER 79. (X)