Service difficulty reports · 14
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR CALA0300040Web · puncturedINSPECTION FOUND THREE PUNCTURES IN HORIZONTAL BEAM WEB AT STA 1119-1125, LBL 18, WL 264. THE PUNCTURES WERE REPAIRED IAW SRM 51-70-13, FIGURE 1 AND 51-40-02, FIGURE 3.SDR CALA0300039Frame · dentedINSPECTION FOUND INNER FORMED FRAME CHORD DENTED AT STA 1121, RBL 28, WL 292. REPAIRED IAW SRM 51-70-11, FIGURE 1.SDR CALA0300038Skin · dentedINSPECTION FOUND AFT CARGO DOOR EXTERNAL SKIN DENTED AT BS 827. REPAIRED IAW SRM 52-00-01, FIGURE 202.SDR CALA0300037Stiffener · bentINSPECTION FOUND FUSELAGE SECTION 48 HORIZONTAL STIFFENER BENT AT STA 1121, LBL 24. REPAIRED IAW SRM 51-70-11.SDR CALA0300033Frame · dentedINSPECTION FOUND INNER FORMED FRAME CHORD DENTED AT STA 1121, LBL 28, WL 292. REPAIRED IAW SRM 51-70-11, FIGURE 1.SDR CALA0300032Stiffener · bentINSPECTION FOUND FUSELAGE SECTION 48 HORIZONTAL STIFFENER BENT AT STA 1104, LBL 24. REPAIRED IAW SRM 51-70-11, FIGURE 1.SDR CALA0100252Actuator · inoperativeTHE RT MLG RED LIGHT REMAINED ILLUMINATED WITH NO GREEN LIGHT WHEN GEAR WAS EXTENDED ON APPROACH TO IAH. A MANUAL GEAR EXTENSION WAS PERFORMED SUCCESSFULLY AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE RT MLG UPLOCK ACTUATOR AT FAULT. THE SDR CALA0100245Floor Support · corrodedINSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 500D BETWEEN STRINGER 26L AND 26R IN FORWARD CARGO AREA. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-40-02 AND 53-30-53.SDR CALA0100230Seat Track · corrodedINSPECTION FOUND INBOARD RIGHT SEAT TRACK CORRODED AT STA 360, RBL 10. THE CORRODED SECTION OF SEAT TRACK WAS REMOVED AND A NEW SECTION WAS INSTALLED.SDR CALA0001508Channel · corrodedINSPECTION FOUND RT Z-CHANNEL CORRODED IN AFT PIT. THE Z-CHANNEL WAS REMOVED AND REPLACED IAW SRM 51-10-2.SDR CALA9900861Light · inopINSPECTION FOUND THE L-1 DOOR EMERGENCY FLASHLIGHT INOPERATIVE. THE FLASHLIGHT WAS REMOVED AND REPLACED.SDR CALA9800145Panel · leakingA FUEL LEAK FROM RT WING OVERWING FUEL TANK ACCESS PANEL LOCATED IN LINE WITH RIGHT ENGINE PYLON WAS OBSERVED WHILE EN ROUTE. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE FOUND SEVERAL LOOSE FASTENERS AND ONE STRIPPED NUT PLATE. THE PANEL WAS RESDR CALA9601220Gimbals · lack of lubeWHEN FLAPS WERE SELECTED TO 30 DEGREES ON FINAL APPROACH TO SLC, THE FLAPS WOULD NOT EXTEND PAST 15 DEGREES. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE LUBRICATED ALL FLAP JACKSCREW GIMBALS PER MM 12-22-21. THE FLAPS OPERATIONALLY CHECKED GOOD SEVERASDR CAL950232Hyd Pump · leakingEWR - FLT 1416 - THE B-SYSTEM HYDRAULIC QUANTITY BEGAN TO DROP ACCOMPANIED BY ILLUMINATION OF THE NR 2 ENGINE HYDRAULIC LOW PRESSURE LIGHT WHILE ON APPROACH TO EWR. THE NR 2 ENGINE HYDRAULIC PUMP WAS TURNED OFF PER 'ABNORMAL' PROCEDURES AND THE AIRCRAFT LANDE
Other aircraft with N14384 · 1
The FAA can assign a mark to another aircraft once a registration is cancelled. No aircraft carries N14384 now.