N14629
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.
21 reports on file, 2003-08-16 – 2012-05-13.
Part: CONTROL LEVER — FAILED (MLG) · airframe 45,662 hrs · 24,017 cycles
ABOUT 400 FT FROM TOUCHDOWN, GEAR UNSAGE LIGHT CAME ON AND GPWS " TO LOW GEAR" ANNOUNCED WENT AROUND GEAR RETRACTED NORMALLY AND EXTENDED NORMALLY ON 2ND LANDING REF TO N/R 4572410 FOR REPLACEMENT OF LANDING CONTROL LEVER IAW MM-32-31-11. SWUNG GEAR SEVERAL TIMES. LANDING GEAR INDICATION CHECKS GOOD.
Part: IRU — FAILED (E/E BAY) · airframe 45,521 hrs · 23,948 cycles
AT ROTATION CAPTS EADI PITCH & AMP; ROLL FLAGS APPEARED. F/O EADI WENT BLANK. RT IRS FAULT LIGHT ILLUMINATED. TAXI IN CAPTS COMPARITOR LIGHT ILLUMINATED. SEE NR 4537211 & AMP; 4537213 FOR C/A. ALSO, PERFORMED LAND VERIFY IAW MM 22-03-10 & AMP; GMM 05-35-40. ALL TESTS PASSED. ACFT RETAINS FULL A/L CAPABILITY. ALSO, OPS CHECKS NORMAL FOR R4 RELAY R & AMP; R IAW MM 24-21-00-735-001. ACFT OK TO CONTINUE.
Part: WIRE HARNESS — DEFECTIVE (NR 1 ENGINE) · airframe 45,491 hrs · 23,934 cycles
CLIMBING THROUGH FL 200 NR 1 EGT AND RED LIGHT SPIKED ON POWER R EDUCTION EGT WAS SWUNG FULL RANGE 0 - RED LINE BOTH DIGITAL AND ANALOG T/S TO BAD EGT HARNESS. REF TO N/R 4537204 FOR REPLACEMENT OF HARNESS ON NR 1 ENG. PERFORMED TEST NR 5 REF MM-71-00-00-725-C00. ALL ENG PARA WITHIN LIMITS.
Earlier reports · 2003–2011 · 18 reports
2011
Part: UNKNOWN — MALFUNCTIONED (FUEL SYSTEM) · airframe 44,361 hrs · 23,381 cycles
AT APROXIMATELY 3000FT ON DEPARTURE THE AIRCRAFT REQUIRED SIGNIFICANT RIGHT AILERON TO HOLD WINGS LEVEL FLIGHT. A CHECK OF THE FUEL GAUGES SHOWED NR 1 TANK FULL NR 2 TANK WITH 6400 LBS, CTR TANK 4900 LBS. ALL PUMPS WERE ON XFEED (CONTINUE ON L/P 8961987). (REF L/P'S 8961988, 8961989 & 8961990) PERFORMED TEST ON FUEL QTY INDICATION SYSTEM AND VERIFIED STICK MEASURING ALL TANKS FUEL IN REF TO AMM 28-41-03. SYSTEM TESTS NORMAL AT THIS TIME. PERFORMED OVERWEIGHT LANDING INSP REF AMM 05-51-74-212-001. FOUND NORMAL. A/C OK TO CONTINUE. (REF L/P 8961990) PERFORMED TEST ON FUEL QTY INDICATION SYSTEM AND VERIFIED STICK MEASURING ALL TANKS FUEL, IN REF. TO AMM 28-41-03. SYSTEM TESTS NORMAL AT THIS TIME. PERFORMED OVERWEIGHT LANDING INSP REF AMM 05-51-74-212 001. FOUND NORMAL. A/C OK TO CONTINUE.
Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 44,062 hrs · 23,218 cycles
REF L/P 8870953, 8870954 AND 8870955 EMERG EXIT PATH LIGHTING ROWS 21-27 INOP. REMOVED AND REPLACED EMERG EXIT POWER SUPPLY CHARGER AT ROW 25 REF AMM 33-51-06. OPS CHECK GOOD AT THIS TIME.
Part: UNKNOWN — MALFUNCTIONED (LANDING GEAR) · airframe 43,518 hrs · 22,921 cycles
AFTER PUTTING GEAR IN DOWN POSITION 3 RED LIGHTS REMAINED ILLUMINATED. HANDLE WAS DOWN AND IN. WENT AROUND. PERFORMED QRH PROCEDURE. LANDING GEAR EXTENDED NORMALLY ON SECOND ATTEMPT. PERFORMED MLG EXTENSION AND RETRACTION TEST REF M/M 32-32-00 NUMEROUS TIMES. COULD NOT DUPLICATE PROBLEM WITH NO FAULTS OR DEFECTS NOTED. A/C OK TO CONTINUE.
2010
Part: SKIN — DENTED (CARGO DOOR) · airframe 42,111 hrs · 22,151 cycles
SUPPORT TASK - WHEN PERFORM DMG LOG PAGE 6311298 INSP ON ABB DOOR FOUND DENT OUT OF LIMIT PER SRM 52-00-01. A/Y =18.8. LOCATED 16 IN FROM AFT EDGE AND 21 IN FROM TOP CUT OUT DAMAGED AREA, FABRICATED DOUBLER, ALODINED AND PRIMED AND INSTALLED REPAIR DOUBLER PER SRM 52-00-01 FIG 201.
Part: HINGE FITTING — CRACKED (L1 DOOR) · airframe 42,111 hrs · 22,151 cycles
L-1 DOOR LOWER HINGE FITTING IS CRACKED. REMOVED AND REPLACED L-1 DOOR LOWER HINGE FITTING REF SRM 51-40-02.
Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 42,111 hrs · 22,151 cycles
CREASE BEAM WEB HAS CORROSION STA 847LT TO 867LT. REMOVED AND REPLACED WEB AT STA 847-867 LT REF SRM 51-40-02.
Part: FRAME — CRACKED (FUSELAGE) · airframe 42,111 hrs · 22,151 cycles
SUPPORT TASK, FUSELAGE FRAME WEB AT STA 303.9 AND STRINGER 16LT HAS CRACKS AROUND THE OVAL HOLE. PERFORMED REPAIR AT FUSELAGE FRAME AT STA 303.9 PER EA 5310- 04659 OP 02.
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 42,111 hrs · 22,151 cycles
E&E COMPT, INTERCOSTAL LOCATED AT LBL 10.0 AND BETWEEN FRAMES 344 AND 360 CRACKED IN TWO PLACES (MARKED) IN UPPER "L"ANGLE REMOVED &. INSTALLED NEW ANGLE / SRM 51-40-02.
2008
Part: FRAME — CRACKED (BS 360 S9L) · airframe 36,207 hrs · 19,044 cycles
FRAME CRACKED STATION 360 S-9L. REPAIED CABIN FRAME STATION 360 S-8L TO S-9L PER ECRA5310-04808 AND CREATED A DIP FOR INTERCOSTAL CLIP ON N/R LOG 9695077 , DIP 89478 PER ECRA 5310-04808 STEP 11. CREATED A SECOND DIP FOR FRAME INSPECTION ON N/R LOG 9695078 DIP 89477 PER ECRA 5310-04808 REV A STEP 12.
Part: FRAME — CRACKED (BS 827 S9L) · airframe 36,207 hrs · 19,044 cycles
FRAME CRACKED AT STATION 827 S-9LT. PERFORMED INTERIM REPAIR BY REMOVING DAMAGE, PERFORMING NDT INSPECTION, FABRICATING AND INSTALLING REPAIR DOUBLERS PER ECRA 5310-04807 PART 1. INITIATED DIP 089441 TO PERFORM THE INSPECTION PER ECRA 5310-04807 PART 2 ON THE FRAME REPAIR BETWEEN S-8 AND S-9, ON LEFT SIDE STATION 827 BEFORE 56250 TOTAL AIRCRAFT CYCLES.
Part: FRAME — CRACKED (BS 907 S9L) · airframe 36,207 hrs · 19,044 cycles
FRAME CRACKED STATION 907 AT S-9L. CUT OUT DAMAGED SECTION OF FRAME AND INSTALLED REPAIR DOUBLERS PER EA 5310-04498 OP 2.
Part: FRAME — CRACKED (BS 747 S9L) · airframe 36,207 hrs · 19,044 cycles
FRAME CRACKED STATION 747 AT S-9L. INSTALLED REPAIR ON FRAME AT STATION 747 S-9L PER EA 5310-04498.
Part: FRAME — CRACKED (BS 867 S9L) · airframe 36,207 hrs · 19,044 cycles
FRAME CRACKED STATION 867 AT S9L. REPAIRED FRAME PER EA 5310-04498 OP2.
Part: FRAME — CRACKED (BS 867 S9R) · airframe 36,207 hrs · 19,044 cycles
FRAME CRACKED STATION 867 AT S-9 RIGHT. REPAIRED FRAME PER EA 5310-04498 OP2.
Part: FRAME — CRACKED (BS 400 S9R) · airframe 36,207 hrs · 19,044 cycles
FRAME CRACKED STATION 400 AT S-9 RIGHT. REPAIRED FRAME PER EA 5310-04498 OP2.
Part: FRAME — CRACKED (BS 380 S9R) · airframe 36,207 hrs · 19,044 cycles
FRAME CRACKED STATION 380 AT S-9 RIGHT. REPAIRED FRAME PER EA 5310-04498 OP2.
2006
Part: SPAR — CORRODED (STAB STA 193.90) · airframe 29,651 hrs · 15,611 cycles
INSPECTION FOUND LT HORIZONTAL STABILIZER UPPER REAR SPAR CAP CORRODED JUST O/B OF STAB STA 193.90. AN INTERIM REPAIR WAS INSTALLED IAW ECRA 5510-01826. A DIP WAS ISSUED TO PERFORM A PERMANENT REPAIR PER PART 3 OF ECRA 5510-01826 WITH NO FURTHER INSPECTIONS REQUIRED AT THIS TIME.
2003
Part: SKIN — GOUGED (LT ELEVATOR) · airframe 24,037 hrs · 12,632 cycles
INSPECTION FOUND SKIN UPPER SURFACE OF LT ELEVATOR GOUGED. THE SKIN WAS REPAIRED IAW ECRA 5520-01335.