N33608
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.
16 reports on file, 1995-11-13 – 2007-08-27.
Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 37,815 hrs · 20,068 cycles
INSPECTION FOUND C-2 DOOR CUTOUT CORRODED AT LOWER AFT CORNER ON BELTFRAME AT STA 847, S25R TO S26R. THE FRAME WAS REPLACED IAW ECRA 5310-04652.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 37,815 hrs · 20,068 cycles
INSPECTION FOUND CABIN FLOORBEAM CORRODED AT STA 986, LBL 12 TO LBL 31. A REPLACEMENT T-CHORD SECTION WAS INSTALLED IAW REPAIR -B- OF ECRA 5310-04494.
Part: ANGLE — CRACKED (FUSELAGE) · airframe 37,815 hrs · 20,068 cycles
INSPECTION FOUND A 1.5 INCH CRACK IN BELTFRAME ANGLE AT STA 616, S17R TO S18R, JUST BELOW FLOOR. REPAIRED IAW ECRA 5311-01158.
Part: CONTROL PANEL — INOPERATIVE (FIRE SUPPRESSION) · airframe 36,806 hrs · 19,528 cycles
THE OVERHEAT DETECT LIGHT ON CAPTAIN'S SIX PACK ILLUMINATED WITH THE AFT CARGO COMPARTMENT AMBER B-LOOP LIGHT ALSO ILLUMINATING ON TAKEOFF FROM IAH. BOTH FIRE BOTTLES WERE DISCHARGED AND THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AFT CARGO COMPARTMENT AND FOUND NO EVIDENCE OF FIRE. THE COCKPIT FIRE SUPPRESSION PANEL WAS REPLACED AND TESTED GOOD IAW MM 26-23-10, PAGE 210. IN ADDITION, BOTH FIRE BOTTLES WERE REPLACED.
Earlier reports · 1995–2005 · 12 reports
2005
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 31,190 hrs · 16,626 cycles
INSPECTION FOUND FLOORBEAM CORRODED AROUND SCREW HOLE AT STA 986, LBL 44, L17L. REPAIRED IAW SRM 53-60-51.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 31,190 hrs · 16,626 cycles
INSPECTION FOUND FLOORBEAM CORRODED AROUND SCREW HOLES AT STA 986, RBL 3 TO RBL 12. THE FLOORBEAM WAS REPAIRED IAW SRM 53-00-51.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 31,190 hrs · 16,626 cycles
INSPECTION FOUND FLOORBEAM CORRODED AROUND SCREW HOLES AT STA 986.5, RBL 29. REPAIRED IAW SRM 53-00-51, FIGURE 203.
2003
Part: DOUBLER — CRACKED (FUSELAGE) · airframe 28,251 hrs · 15,112 cycles
INSPECTION FOUND THE EXTERNAL POWER DOOR CUTOUT SKIN DOUBLER CRACKED AT THE FORWARD LOWER CORNER. THE SKIN DOUBLER WAS REPAIRED IAW ECRA 5330-03290. IN ORDER TO VERIFY CRACK REMOVAL IN THE DOUBLER, THE II-SECTION(EXTRUSION) REQUIRED REMOVAL. THE II-SECTION AND THE SKIN DOUBLER WERE DAMAGED DURING REMOVAL REQUIRING TRIM OF THE SKIN DOUBLER AND REMOVAL OF THE II-SECTION UPPER FLANGE. THE II-SECTION AND ASSOCIATED SKIN DOUBLER WERE REPAIRED IAW ECRA 5330-03289.
2002
Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 26,052 hrs · 13,980 cycles
INSPECTION FOUND A 1 INCH CRACK IN FLOOR SUPPORT WEB UPPER FLANGE BETWEEN STA 344 AND 360, BL 0. THE FLOOR SUPPORT WEB WAS REMOVED AND REPLACED IAW SRM 51-10-2.
2001
Part: MEGAPHONE — INOPERATIVE (CABIN) · airframe 22,672 hrs · 12,056 cycles
THE FORWARD MEGAPHONE WAS FOUND INOPERATIVE. THE MEGAPHONE WAS REPLACED IAW MM 25-00-00.
2000
Part: SKIN — TORN (DOOR JAMB) · airframe 19,468 hrs · 10,334 cycles
DOOR JAMB SKIN TORN ALONG EDGE STA 787 FROM L24 - 24R FWD JAMB AFT CARGO (12). REMOVED AND REPLACED JAMB SKIN PER SRM 51-10-2.
Part: SKIN — DENTED (GARGO DOOR) · airframe 19,468 hrs · 10,334 cycles
AFT CARGO DOOR EXTERIOR SKIN HAS DENT JUST AFT OF HANDLE WELL. CUT OUT DAMAGED AREA. INSTALLED DOUBLER REPAIR PER SRM 52-00-01 FIG 203.
Part: WEB — CRACKED (FUSELAGE) · airframe 19,468 hrs · 10,334 cycles
FORWARD BAG BIN AFT OF DOOR AND 5 INCHES ABOVE TRANSITION PANEL WEB CRACKED AT STA 492.8 (1). INSTALLED WEB REPAIR PER SRM 51-70-13.
1998
Part: TARGET — OUT OF ADJUST (RT MLG)
THE RT MLG RED UNSAFE LIGHT REMAINED ILLUMINATED WHEN GEAR WAS EXTENDED ON APPROACH. THE GEAR WAS CYCLED AND THE RED LIGHT EXTINGUISHED. MAINTENANCE FOUND THE RT MLG DOWNLOCK SENSOR TARGET GAP OUT OF LIMITS. THE SENSOR GAP WAS ADJUSTED IAW MM 32-61-31, PAGE 403. A GEAR SWING WAS PERFORMED WITH OPERATION AND INDICATIONS CHECKING GOOD.
1995
Part: SKIN — CRACKED (NR 5 LE SLAT)
IAH - FLT 1879 - INSPECTION FOUND A 3 INCH CRACK IN LOWER SKIN AT INBOARD END OF NR 5 LEADING EDGE SLAT. A FILLER AND DOUBLER REPAIR WAS INSTALLED IAW ECRA 5750-02394. (X)
Part: SKIN — CRACKED (NR 4 LE SLAT)
IAH - FLT 1879 - INSPECTION FOUND A 3 INCH CRACK IN LOWER SKIN AT OUTBOARD END OF NR 4 LEADING EDGE SLAT. A FILLER AND DOUBLER REPAIR WAS INSTALLED IAW ECRA 5750-02393. (X)