N310FL
Registered owner: D & T OUTLAW PROPERTIES LLC, TX (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.
52 reports on file, 1999-10-02 – 2004-10-04.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,284 hrs · 24,595 cycles
DURING C-4 CHECK, INSPECTION REPORTED FLOORBEAM SUPPORT CORRODED AT STA 1010, RBL 10. REPLACED FLOORBEAM SUPPORT PER SRM 51-40-02, 51-40-05 AND BAC DRAWING 65C33375.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,284 hrs · 24,595 cycles
DURING A-4 CHECK, INSPECTION REPORTED PARTITION SUPPORT CORRODED AT FLOORBEAM, STA 986.5 - 1006, RBL 16. REPLACED PARTITION SUPPORT AT FLOORBEAM PER SRM 51-40-06 AND DRAWING 65C32675.
Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,284 hrs · 24,595 cycles
DURING C-4 CHECK, INSPECTION REPORTED FLOOR WEBS AFT OF STA 1016 FLOORBEAM, CENTER OF FUSELAGE, CORRODED. REPLACED FLOOR WEB HAT CHANNEL, STA 1016, BL 0, PER DRAWING 69-77731, AND SRM 51-40-02 AND 53-60-51.
Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,284 hrs · 24,595 cycles
DURING C-4 CHECK, INSPECTION REPORTED FLOOR PANEL SUPPORT CORRODED AT STA 986.5 - 1006, RBL 20. REPLACED FLOOR SUPPORT INTERCOSTAL PER SRM 51-40-02 AND 53-60-51.
Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,284 hrs · 24,595 cycles
DURING C-4 CHECK, INSPECTION REPORTED L2 MOP SILL CORRODED. REPLACED L2 MOP SILL PER SRM 51-10-2 AND 51-40-02.
Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,284 hrs · 24,595 cycles
DURING C-4 CHECK, INSPECTION REPORTED R2 MOP SILL CORRODED. REPLACED R2 MOP SILL PER SRM 51-10-2 AND 51-40-02.
Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,284 hrs · 24,595 cycles
DURING C-4 CHECK, INSPECTION REPORTED FLOOR INTERCOSTAL FROM STA 947 - 986 LEFT OF CENTER CORRODED AT FLOOR PANEL NUT PLATES. REPLACED INTERCOSTAL PER SRM 51-40-02, 51-30-01 AND DRAWING 65C33375.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,284 hrs · 24,595 cycles
DURING C-4 CHECK, FLOORBEAM GOUGED AND CORRODED AT STA 947.5 - 967, RBL 16. REPLACED DAMAGED INTERCOSTAL PER SRM 51-40-02 AND 53-60-51.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,284 hrs · 24,595 cycles
DURING C-4 CHECK, INSPECTION REPORTED FLOORBEAM SUPPORT AT STA 947.5 - 967, LBL 14, CORRODED. REPLACED INTERCOSTAL AT STA 947.5 - 967, LBL 14, PER SRM 51-40-02, 51-30-01 AND DRAWING 65C33375.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,284 hrs · 24,595 cycles
DURING C-4 CHECK, INSPECTION REPORTED FLOORBEAM AT STA 986.5 CORRODED AT FLOOR PANEL NUT PLATES. REPLACED FLOORBEAM UPPER CHORD AT STA 986.5 PER SRM 53-60-51, 53-00-51, FIG 202, AND MM 51-20-01.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,284 hrs · 24,595 cycles
DURING C-4 CHECK, INSPECTION REPORTED FLOORBEAM AT STA 947.5 CORRODED AT FLOOR PANEL NUT PLATES. REPAIRED FLOORBEAM UPPER CHORD PER SRM 53-00-51, 51-40-02, 51-20-01 AND MM 51-21-01.
Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 34,284 hrs · 24,595 cycles
DURING C-4 CHECK, INSPECTION REPORTED FLOOR SUPPORT CRACKED AT STA 927 - 947.5, RBL 16. REMOVED FLOOR SUPPORT TO REPLACE CRACKED FLANGE. REPAIRED CRACKED FLANGE AND REINSTALLED FLOOR SUPPORT PER BOEING DRAWING 65-36656, 737-300 SRM 51-40-02 AND 51-10-02, AND SOPM 20-41-02.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,284 hrs · 24,595 cycles
DURING C-4 CHECK, INSPECTION REPORTED FLOORBEAM AT STA 328 CRACKED 20 INCHES IN FROM FUSELAGE OUTER SKIN. VERTICAL ANGLE CRACKED ON LOWER END LT. REPLACED SHEAR TIE AT LBL 45 ON FWD SIDE OF STA 328 FLOORBEAM PER SRM 51-40-02, 51-40-05 AND SOPM 20-41-02.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,284 hrs · 24,595 cycles
DURING C-4 CHECK, INSPECTION REPORTED FLOORBEAM AT STA 967, RBL 27.16, CORRODED AT FLOOR PANEL SCREW NUT PLATE. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR PARTS PER SRM 53-00-51, FIG 202.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,284 hrs · 24,595 cycles
DURING C-4 CHECK, INSPECTION REPORTED FLOORBEAM BETWEEN STA 294.5 AND 312, 10.5 INCHES FROM CENTER LT, CORRODED AT STA 312 END. REMOVED UPPER T-CHORD ON FLOOR SUPPORT AT LBL 10.5, STA 294.5 THRU 312, AND INSTALLED NEW UPPER T-CHORD IAW SRM 51-40-02.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,284 hrs · 24,595 cycles
DURING C-4 CHECK, INSPECTED REPORTED FLOORBEAM AT STA 967, LBL 42, CORRODED AT FLOOR PANEL SCREW NUT PLATE. FOUND FLOORBEAM TO BE CORRODED BEYOND LIMITS PER SRM 53-60-51. REMOVED DAMAGED AREA, FABRICATED REPAIR SECTION AND REPAIR PARTS AND INSTALLED PER SRM 53-00-51, 51-20-01 AND 20-41-02.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,284 hrs · 24,595 cycles
DURING C-4 CHECK, INSPECTION REPORTED TOP OF FLOORBEAM AT STA 294.5 CORRODED IN SEVERAL SPOTS FROM 10 INCHES LEFT OF CENTER TO 40 INCHES RT OF CENTER. ALL SCREW HOLES IN THIS AREA CORRODED. SCRATCH ON TOP OF BEAM RT SIDE, 12 INCHES FROM CENTER TO WALL. REPAIRED FLOORBEAM AT STA 294.5 FROM LBL 20 TO RT BULKHEAD PER SRM 53-10-51, SECTION 41, FIG 205.
Part: SKIN — DENTED (FUSELAGE) · airframe 34,284 hrs · 24,595 cycles
DURING C-4 CHECK, COMPLIED WITH RW0000198, DENT IN FUSELAGE, AFT OF CARGO DOOR AT STA 500-500A. REMOVED DAMAGE, FABRICATED, LOCATED AND INSTALLED REPAIR IAW BAC 737-300 SRM 53-00-01, PROCEDURE V, DETAIL VII-IX AND SOPM 40-20-01.
Part: STRUCTURE — CRACKED (MLG WW) · airframe 34,282 hrs · 24,594 cycles
ON WALK AROUND, MAINTENANCE REPORTED A 4-INCH CRACK IN RT FWD TOP WHEEL WELL. REPAIRED IAW SRM 53-10-51, PAGE 213, FIGURE 203.
Earlier reports · 1999–2002 · 33 reports
2002
Part: STRAP — TORN (FUSELAGE) · airframe 27,293 hrs · 20,723 cycles
DURING C-2 CHECK, INSPECTION REPORTED SMALL TEAR IN FLOORBEAM STABILIZER STRAP AT STA 328, LBL 8, AND FASTENER HEADS WORN DOWN. REPLACED DAMAGED STABILIZER STRAP PER SRM 51-40-02.
Part: SPLICE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,293 hrs · 20,723 cycles
DURING C-2 CHECK, INSPECTION REPORTED FLOOR SPLICE IN AFT CARGO COMPARTMENT AT BS 767 CORRODED. FABRICATED AND INSTALLED REPLACEMENT FLOOR SPLICE PER SRM 53-60-53.
Part: STRAP — TORN (FUSELAGE) · airframe 27,293 hrs · 20,723 cycles
DURING C-2 CHECK, INSPECTION REPORTED FLOORBEAM STABILIZER STRAP TORN AND MISSING A SECTION, STA 312 TO 328, BL -0-. REPLACED DAMAGED STABILIZER STRAP PER SRM 51-40-02.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,293 hrs · 20,723 cycles
DURING C-2 CHECK, INSPECTION REPORTED AFT CARGO COMPARTMENT FLOOR SUPPORT CORRODED AT STA 767. FABRICATED AND INSTALLED REPAIR ON CARGO TRACK AT STA 767, RBL 13.8, PER SRM 53-00-53, FIG 202.
Part: FAIRING — CRACKED (L1 DOOR) · airframe 27,293 hrs · 20,723 cycles
DURING C-2 CHECK, INSPECTION REPORTED UPPER HINGE FAIRING AT L1 DOOR BENT AT FWD END AND CRACKED AT AFT END. FABRICATED AND INSTALLED REPLACEMENT UPPER L1 DOOR HINGE FAIRING PER SRM 51-30-01.
Part: FRAME — DAMAGED (FUSELAGE) · airframe 27,293 hrs · 20,723 cycles
DURING C-2 CHECK, INSPECTION REPORTED FRAME AT STA 460, RBL 7 TO 14, DAMAGED. FABRICATED AND INSTALLED REPAIR AND FRAME CLIP PER SRM 53-00-07.
Part: CARGO TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,293 hrs · 20,723 cycles
DURING C-2 CHECK, INSPECTION REPORTED CORROSION ON FLOOR TRACK IN CARGO COMPARTMENT AT RBL 13.8, BETWEEN STA 795 AND 827. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PER SRM 53-00-63, 53-00-53, 51-41-02 AND SOPM 20-41-02.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,293 hrs · 20,723 cycles
DURING C-2 CHECK, INSPECTION REPORTED CORROSION ON FLOOR SUPPORT AT STA 767, RBL 3. REMOVED CORROSION ON FLOOR SUPPORT, FABRICATED REPLACEMENT PARTS AND INSTALLED REPAIR PER SRM 53-00-53.
Part: DOOR FRAME — DAMAGED (FUSELAGE) · airframe 27,293 hrs · 20,723 cycles
DURING C-2 CHECK, INSPECTION REPORTED HOLE IN AFT CARGO DOOR FWD FRAME CAP WEB. FABRICATED AND INSTALLED WEB REPAIR PER SRM 51-70-13, 51-10-02 AND 51-70-13.
2001
Part: BUSHING — WORN (LT ELEVATOR TAB) · airframe 23,477 hrs · 18,885 cycles
AIR TURNBACK. FLIGHT CREW REPORTED VIBRATION TO FLIGHT CONTROLS DURING CLIMB. NO VIBRATION INDICATION, ALL ENGINE INDICATIONS NORMAL. CYCLED GEAR AT LOWER SPEED AND ALTITUDE AND VIBRATION STOPPED. VIBRATION PRESENT WITH AUTOPILOT BOTH ON AND OFF. FOUND NR 1 INBOARD LT ELEVATOR TRIM TAB ATTACH HARDWARE WORN. REPLACED HARDWARE, PERFORMED FLIGHT CONTROL TEST/INSPECTION, PERFORMED TEST FLIGHT AND SYSTEM CHECKED OK.
2000
Part: STRUCTURE — BROKEN (FUSELAGE)
DEN - DURING C-7 CHECK INSPECTION, REPORTED EXPANSION JOINT FORWARD OF CENTER FUEL TANK, LEFT OF CENTER LINE, BROKEN. MAINTENANCE REPLACED CHANNEL ASSY PER SRM 53-21-00. (M)
Part: HOUSING — CORRODED (TORQUE BOX) · airframe 20,879 hrs · 17,449 cycles
DEN - DURING C-7 CHECK, INSPECTION REPORTED CORROSION AT CORNER ATTACH BOLT NUTPLATES OF R-2 DOOR TORQUE BOX. MAINTENANCE REMOVED AND REPLACED TORQUE BOX HOUSING PER SRM 52-41-04. (X)
Part: FLOOR SUPPORT — CRACKED (FUSELAGE)
DEN - DURING C-7 CHECK INSPECTION REPORTED FLOOR SUPPORT BETWEEN BS 787 AND BS 820, RBL 16, CRACKED AND CORRODED. MAINTENANCE REPLACED FLOOR SUPPORT IAW SRM 53-00-53 FIG 202 SHEET 1 AND 2. (M)
Part: CHANNEL — CRACKED (FUSELAGE)
DURING C-7 CHECK INSPECTION REPORTED CABIN FLOOR EXPANSION JOINT CHANNEL CRACKED AT BS 540 BL 0 TO RBL 20. MAINTENANCE REMOVED AND REPLACED RIGHT CENTER EXPANSION JOINT CHANNEL PER SRM 53-21-00. (M)
Part: ANGLE — CRACKED (FUSELAGE)
DEN - DURING C-7 CHECK INSPECTION, FOUND TIE ANGLE UNDER CABIN FLOOR CRACKED AT STATION 727B, LBL 47. MAINTENANCE FABRICATED AND INSTALLED REPLACEMENT TIE ANGLE PER SRM 51-10-2. (M)
Part: ANGLE — CRACKED (FUSELAGE)
DEN - DURING C-7 CHECK INSPECTION, REPORTED TIE ANGLE UNDER CABIN FLOOR CRACKED AT BS 727B, LBL 47. MAINTENANCE REPLACED TIE ANGLE PER SRM 51-10-2. (M)
Part: SHEAR TIE — CRACKED (FUSELAGE)
DEN - DURING C-7 CHECK INSPECTION REPORTED SHEAR TIE CRACKED AT STRINGER 6R. MAINTENANCE REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPLACEMENT SHEAR TIE PER SRM 53-10-15 AND 51-10-2. (M)
Part: ANGLE — CRACKED (FUSELAGE)
DEN - DURING C-7 CHECK INSPECTION, REPORTED CRACK IN SUPPORT ANGLE ON FRAME FORWARD OF R1 DOOR, BETWEEN STRINGER 9R AND STRINGER 10R. MAINTENANCE REPLACED SUPPORT ANGLE PER SRM 51-40-2. (M)
Part: ANGLE — CRACKED (FUSELAGE)
DEN - DURING C-7 CHECK INSPECTION, REPORTED CRACK IN SUPPORT ANGLE ON FRAME FORWARD OF R1 DOOR, BETWEEN STRINGER 10R AND STRINGER 11R. MAINTENANCE REPLACED SUPPORT ANGLE PER SRM 51-40-2. (M)
Part: ANGLE — CRACKED (FUSELAGE)
DEN - DURING C-7 CHECK INSPECTION, REPORTED CRACK IN SUPPORT ANGLE ON FRAME FORWARD OF R1 DOOR, BETWEEN STRINGER 12R AND STRINGER 13R. MAINTENANCE REPLACED SUPPORT ANGLE PER SRM 51-40-2. (M)
Part: ANGLE — CRACKED (FUSELAGE)
DEN - DURNG C-7 CHECK INSPECTION, REPORTED CRACK IN SUPPORT ANGLE ON FRAME FORWARD OF R1 DOOR, BETWEEN STRINGER 11R AND STRINGER 12R. MAINTENANCE REPLACED SUPPORT ANGLE PER SRM 51-40-2. (M)
Part: ANGLE — CORRODED (THRESHOLD)
DEN - DURING C-7 CHECK INSPECTION REPORTED CORROSION ON R-2 DOOR THRESHOLD SCUFF PLATE SUPPORT ANGLE. MAINTENANCE REMOVED CORROSION PER SRM 51-10-2, AND CLEANED AND INSTALLED SUPPORT ANGLE PER SRM 51-40-2. (M)
Part: FRAME — CRACKED (FUSELAGE)
DEN - DURING C-7 CHECK INSPECTION, REPORTED FUSELAGE FRAME CRACKED ON TOP FLANGE AND RADIUS AT STATION 727B, STRINGER 23R, IN AFT CARGO PIT. MAINTENANCE REMOVED DAMAGED SECTION OF FRAME, FABRICATED REPAIR DOUBLER PER EO 51-00-737-001, AND INSTALLED REPAIR DOUBLER PER SRM 51-70-11 AND 51-40-02. (M)
Part: SHEAR TIE — CRACKED (FUSELAGE)
DEN - DURING C-7 CHECK INSPECTION, REPORTED SHEAR TIE CRACKED AT STATION 294, STRINGER 6R. MAINTENANCE FABRICATED AND INSTALLED NEW SHEAR TIE PER SRM 51-10-2. (M)
Part: BRACKET — CRACKED (FUSELAGE)
DEN - DURING C-7 CHECK INSPECTION, REPORTED CORNER BRACKET CRACKED UNDER FLOORBEAM AT STATION 767, RBL 60. MAINTENANCE FABRICATED AND INSTALLED REPLACEMENT ANGLE FOR FLOORBEAM PER SRM 51-10-2. (M)
Part: FLOORBOARD — CORRODED (FUSELAGE)
DEN - DURING C-7 CHECK INSPECTION, FOUND CORROSION ON FLOORBOARD ATTACH ANGLE STATION 960 TO 986.5, STRINGER 17R. MAINTENANCE REMOVED CORROSION, TREATED, PRIMED AND PAINTED FLOORBOARD ATTACH ANGLE PER SRM 51-10-2 AND MM 25-25-0. (M)
Part: DOOR FRAME — CORRODED (CARGO DOOR)
DEN - DURING C-7 CHECK INSPECTION REPORTED, FOUND CORROSION AT LOWER FORWARD CORNER OF AFT CARGO DOOR FRAME BETWEEN S25R AND S26R. MAINTENANCE FABRICATED, AND INSTALLED REPLACEMENT L ANGLE AT LOWER FORWARD CORNER OF AFT CARGO DOOR BETWEEN S25R AND S26R PER SRM 51-30-1. (M)
Part: SKIN — DAMAGED (AILERON)
DEN - DURING C-7 CHECK, INSPECTION REPORTED HOLE IN LOWER SURFACE OF AILERON AT OUTBOARD END. MAINTENANCE REMOVED AILERON. REPAIRED HOLE PER SRM 51-70-04 AND 51-70-03 AND PAINTED AND BALANCED PANEL. INSTALLED AILERON PER MM 27-11-11. PERFORMED OPERATIONAL CHECK PER MM 27-11. (M)
Part: WEB — CRACKED (FUSELAGE)
DEN - DURING C-7 CHECK INSPECTION, REPORTED CRACK IN AFT CARGO DOOR OPENING WEB, BS 847 - BS 867, STRINGER 26. MAINTENANCE REMOVED DAMAGED AREA. FABRICATED AND INSTALLED REPLACEMENT WEB PER SRM 53-40-2. (M)
Part: WEB — CORRODED (DOOR JAMB)
DEN - DURNG C07 CHECK INSPECTION, FOUND CORROSION ON AFT CARGO DOOR OPENING WEB AT FORWARD SIDE OF DOOR, STAITON 847-867, STRINGER 26. MAINTENANCE FABRICATED AND INSTALLED REPLACEMENT WEB PER SRM 51-10-2 AND MM 25-25-0. (M)
Part: WEB — CORRODED (DOOR JAMB)
DEN - DURING C-7 CHECK INSPECTION, FOUND CORROSION ON AFT CARGO DOOR OPENING WEB AT FORWARD SIDE OF DOOR, STATION 787, BETWEEN STRINGER 23 AND 25. MAINTENANCE FABRICATED AND INSTALLED REPLACEMENT WEB PER SRM 51-10-2 AND MM 25-25-0. (M)
Part: HINGE — LOOSE (RT ELEVATOR)
LGA-DEN - FLT 583 - DURING CRUISE, FLIGHT CREW REPORTED VIBRATION IN YOKE AT 250 TO 280 KTS, VIBRATION INCREASED INCENTER CABIN DURING BANKS. MX FOUND .012 INCH VERTICAL PLAY AT RT ELEVATOR OUTBOARD TAB NR 4 HINGE ASSY (OUTBOARD). REPLACED TAB ASSY, ALSO REPLACED WORN BOLT AND BUSHING ON LT TAB NR 1 HINGE (INBOARD). ACCOMPLISHED ELEVATOR TAB ADJUSTMENT AND TEST PER MM 27-31-00 AND 27-31-31. PERFORMED TEST FLIGHT AND ALL SYSTEMS CHECKED NORMAL. (M)
1999
Part: BATTERY CHARGER — FAILED (BS 975)
DEN - DURING SERVICE CHECK, INSPECTION REPORTED THE RT WING LOWER AFT WING-TO-BODY EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REPLACED BATTERY CHARGER AT BS 975R (M1157) AND SYSTEM CHECKED OKAY. CYCLES: 10. (X)