N313FL
Registered owner: CAE USA INC, FL (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.
23 reports on file, 2000-11-24 – 2005-04-22.
Part: COVER — MISSING (ENGINE) · airframe 34,115 hrs · 25,471 cycles
AIR RETURN TO DEN, ON CLIMB-OUT, BOTH ENGINE OIL QUANTITY INDICATORS WENT TO ZERO. BOTH OIL PRESSURE INDICATORS WENT TO ZERO. BOTH LOW OIL PRESSURE LIGHTS ILLUMINATED. ENGINES OPERATED APPROXIMATELY 15 MINUTES IN THAT CONDITION UNTIL LANDING, WHICH WAS WITHOUT INCIDENT. BOTH ENGINE EGT'S, VIBRATION AND OIL TEMPS REMAINED NORMAL FOR DURATION OF ENGINE OPERATIONS. INSPECTED BOTH ENGINES AND DETERMINED OIL LOSS WAS DUE TO N2 GEARBOX ROTATION DRIVE ACCESS COVERS NOT INSTALLED ON EITHER ENGINE. BOTH ENGINES ARE IN THE PROCESS OF BEING REPLACED. ENGINE INFORMATION IS AS FOLLOWS: CFM56-3B2. NR 1 ENGINE, S/N 856183, 32111.70 HRS., 24091 CYC NR 2 ENGINE, S/N 857192, 32907.4 HRS., 24616 CYC.
Part: ENGINE — LEAKING
APPROX 11 MIN INTO CLIMB AT FL260, BOTH ENGINES BEGAN TO LOSE OIL QUANTITY. AFTER A SHORT PERIOD OF TIME, OIL QUANTITY ON NR 1 ENG WENT TO ZERO, FOLLOWED BY NR 2 ENG ALSO GOING TO ZERO. NR 1 ENG OIL PRESS THEN DROPPED TO ZERO, NR 2 ENG OIL PRESS DROPPED TO MIDDLE OF AMBER BAND BEFORE DROPPING TO ZERO. AT THIS TIME, BOTH ENGINE AMBER LOW OIL PRESS LIGHTS ILLUMINATED WHILE AN IMMEDIATE RETURN TO THE AIRPORT WAS INITIATED. UPON LANDING AND AFTER ENGINE SHUTDOWN, OBVIOUS OIL LEAKAGE FROM BOTH ENGINES WAS EVIDENT. DETERMINED THAT N2 (PADS) (SP) HAD NOT BEEN REINSTALLED AFTER COMPLETION OF BORESCOPES, BOTH WERE HANGING ALONG SIDE ENGINES BY RESTRAINT LEADS. (K)
Part: SILL — CORRODED (L2 DOOR) · corrosion level 2 · airframe 34,111 hrs · 25,467 cycles
DURING C-4 CHECK INSPECTION, REPORTED L2 DOOR MOP SILL CORRODED. REPLACED L2 DOOR MOP SILL PER SRM 51-40-02.
Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,111 hrs · 25,467 cycles
DURING C-4 CHECK INSPECTION, REPORTED INTERCOSTAL AT BS 950, RBL 20 TO RBL 40, CORRODED. FOUND TO BE OUT OF LIMITS PER SRM 53-60-51. REPLACED INTERCOSTAL PER SRM 51-40-05, 51-40-02, AND 53-60-51.
Part: STRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,111 hrs · 25,467 cycles
DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON AFT GALLEY PAN STRAP AT BS 1016, BETWEEN RBL 30 AND LBL 30. FOUND TO BE OUT OF LIMITS PER SRM 53-60-61, FIG 101, DETAIL VII. REMOVED PAN STRAP PER SRM 51-40-02. FABRICATED NEW STRAP AND INSTALLED PER EA 53-53R-10753, SRM 51-10-02 AND SRM 51-40-02.
Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,111 hrs · 25,467 cycles
DURING C-4 CHECK INSPECTION, REPORTED R2 DOOR MOP SILL CORRODED. REPLACED R2 DOOR MOP SILL PER SRM 51-40-02.
Earlier reports · 2000–2004 · 17 reports
2004
Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 33,132 hrs · 24,893 cycles
FLIGHT CREW REPORTED ALTITUDE CABIN CLIMBED AT 150 FPM WITH BOTH PACKS IN AUTO AT CRUISE ALTITUDE. PRESSURIZED AIRCRAFT ON THE GROUND AND FOUND AN 8-INCH CRACK AT TOP OF RT WHEEL WELL, STA 664, RBL 37. REPAIRED PER SRM 53-60-51, FIGURE 203, DETAIL IV AND EA B3-53R-10554.
Part: CONTROL MODULE — INOPERATIVE (FLAP/SLATS) · airframe 32,364 hrs · 24,484 cycles
ABORTED TAKEOFF. FLIGHT CREW REPORTED L/E FLAPS TRANSIT LIGHT ILLUMINATED WITH NR 2 SLAT ON OVERHEAD PANEL SHOWING INTRANSIT. TAKEOFF ABORTED AT 111 KIAS. REPLACED FLAP/SLAT MODULE PER MM 27-88-41. CHECKED TARGET TO EXTEND SENSORS ON NR 2, 3 AND 5 SLATS PER MM 27-88-11. CHECKED NORMAL. COMPLIED WITH HIGH ENERGY INSPECTION PER MM 05-51-07, PAGES 201-203 (5). COMPLIED WITH RTO INSPECTION PER MM 05-51-07 AND 22-88-41. OPERATIONAL TEST WAS NORMAL ON FLAP/SLAT SYSTEM.
2003
Part: SNUBBER — INOPERATIVE (PAX DOOR) · airframe 29,739 hrs · 22,945 cycles
DURING C-3 CHECK, INSPECTION REPORTED R-1 DOOR LOCK PIN INOPERATIVE. ADJUSTED SNUBBER ON R-1 DOOR PER MM 52-41-00, PAGE 504, STEP 5.
2002
Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 27,617 hrs · 21,708 cycles
DURING C 2 CHECK, CORROSION WAS FOUND ON THE AFT CARGO PIT INTERCOSTAL SURFACE AND AROUND NUT PLATES BETWEEN STA 767 TO STA 794 AND RBL 21. NEW INTERCOSTAL WAS FABRICATED AND INSTALLED IAW SRM 51-10-02, SRM 51-40-02 AND SOPM 20-41-02.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,617 hrs · 21,708 cycles
DURING C 2 CHECK, THE AFT CARGO COMPARTMENT FLOOR TRACK WAS FOUND CORRODED AT STA 727D AT RBL 13.8 THE CORRODED SECTION OF TRACK WAS REPLACED BETWEEN STA 727 AND STA 767 IAW SRM 51-40-02
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,617 hrs · 21,708 cycles
DURING C 2 CHECK, AFT CARGO FLOOR TRACK WAS FOUND CORRODED AT STA 860, RBL 2. FLOOR TRACK WAS REPLACED BETWEEN STA 727 AND STA 947, RBL 2.5 IAW SRM 51-40-05 AND SRM 51-40-02.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,617 hrs · 21,708 cycles
DURING C 2 CHECK, CORROSION WAS FOUND OF THE AFT CARGO COMPARTMENT FLOOR TRACK AT STA 791, LBL 11.5. REMOVED AND REPLACED THE FLOOR TRACK IAW SRM 51-10-02 AND SRM 51-40-02, BETWEEN STA 727 AND STA 947 AT LBL 11.5.
Part: SKIN — PUNCTURED (LE FLAP) · airframe 27,617 hrs · 21,708 cycles
DURING C 2 CHECK, IT WAS NOTED RT, IN BOARD FORE FLAP HAD A HOLE IN THE LOWER SURFACE. FLAP WAS REMOVED AND REPAIRED IAW SRM 51-70-10 AND REINSTALLED IAW BOEING 737 MM 27-51-07.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,617 hrs · 21,709 cycles
DURING C 2 CHECK, AFT CARGO FLOOR TRACK WAS FOUND CORRODED AT STA 860, LBL 3.0 FLOOR TRACK REPLACED BETWEEN STA 791 TO STA 860. LBL 3.0, IAW SRM 51-40-02
Part: FLOOR PANEL — CORRODED (CARGO BAY) · corrosion level 2 · airframe 27,617 hrs · 21,708 cycles
DURING C 2 CHECK, THE AFT CARGO COMPARTMENT FLOOR TRANSITION PANEL WAS FOUND CORRODED BETWEEN STA 787 AND STA 807. AFT CARGO COMPARTMENT FLOOR TRANSITION PANEL WAS REMOVED AND REPLACED BETWEEN STA 727 AND 947, LBL 20 IAW SRM 53-60-53 AND SRM 51-40-02.
Part: TAIL CONE — DENTED (FUSELAGE) · airframe 27,617 hrs · 21,708 cycles
DURING C 2 CHECK, A DENT WAS FOUND ON THE LT SIDE OF THE TAIL CONE, NEAR THE ELEVATOR ATTACH POINTS. DENT WAS REPAIRED AND PAINTED IAW MAINTENANCE MANUAL 737-300 MM 51-21-99 AND SRM 51-70-06.
Part: SKIN — BIRD STRIKE (STABILIZER) · airframe 27,617 hrs · 21,708 cycles
DURING C 2 CHECK, A BIRD STRIKE WAS FOUND ON THE RT LEADING EDGE OF THE STABILIZER BETWEEN STA 184.7 AND STA 189.2. FABRICATED AND INSTALLED DOUBLER AND FILLER IAW SRM 55-10-01.
Part: CONTROL CABLE — BROKEN (AILERON) · airframe 26,175 hrs · 20,998 cycles
FLIGHT CREW REPORTED SIGNIFICANT RT ROLL TENDENCY ON FINAL APPROACH AND LANDING. CORRECTED ON TOUCHDOWN. FOUND AILERON BUS CABLE BROKEN. REMOVED RT AILERON CABLE ABSB-4 AND FABRICATED, INSTALLED, ADJUSTED AND TESTED REPLACEMENT CABLE PER MM 27-11-0, 27-09-14 AND 20-10-91 AND SYSTEM CHECKED OKAY.
Part: VIDEO UNIT — SHORTED (CABIN) · airframe 25,817 hrs · 20,824 cycles
FLIGHT CREW REPORTED ENTERTAINMENT TAPE RECORDER SMOKING EN ROUTE TO DEN. DIVERTED TO SLC AND LANDED WITHOUT INCIDENT. ISOLATED ELECTRICAL SHORT IN TAPE PLAYER. PULLED AND COLLARED CIRCUIT BREAKER E7 ON P6-1 PANEL. REMOVED TAPE PLAYER FROM WALL ABOVE FWD FLIGHT ATTENDANT SEAT AND SECURED CANNON PLUG TO WALL WITH TAPE. DEACTIVATED AND REMOVED TAPE REPRODUCER PER EA 23-737-021.
Part: ACTUATOR — INOPERATIVE (RUDDER TRIM) · airframe 26,525 hrs · 20,368 cycles
BLOCK TURNBACK. FLIGHT CREW REPORTED RUDDER WOULD NOT CENTER AFTER START UP AND TAXI. REPLACED RUDDER TRIM ACTUATOR AND CHECKED OKAY.
2000
Part: DOOR — OUT OF ADJ (MAIN PAX) · airframe 26,035 hrs · 10,499 cycles
DURING TAKEOFF, FLIGHT CREW REPORTED FORWARD ENTRY DOOR LIGHT ILLUMINATED. TAKEOFF WAS ABORTED AT 75 KIAS. MAINTENANCE ADJUSTED FORWARD ENTRY DOOR PER MM 52-11-0 AND PERFORMED ENTRY DOOR TEST. OPERATIONAL TEST AND LEAK CHECK OKAY. REPLACED NR 3 AND NR 4 MAIN TIRE AND WHEEL ASSEMBLIES. REMOVED DAMAGED RT. MAIN LANDING GEAR LOWER AND MIDDLE DOORS PER CDL 32-10-3.
Part: SPRING — UNSERVICEABLE (WHEEL WELL) · airframe 21,466 hrs · 18,716 cycles
DURING C-7 CHECK TEST FLIGHT, FLIGHT CREW REPORTED AILERONS STIFF IN MANUAL REVERSION. REPLACED AILERON CONTROL SPRING AND CHECKED OKAY.