Service difficulty reports · 15
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR ASMF200601006O-Ring · leakingDURING OVERNIGHT CHECK, THE RIGHT ENGINE WAS REPLACED FOR MAINTENANCE CONVENIENCE AND DURING TESTS WAS DETECTED FUEL LEAK AT FLOW TRANSMITTER. THE TRANSMITTER O-RING WAS REPLACED AND TESTED IAW MM 71-00-02, ALL CORRECT.SDR ASMF200510011Start Valve · malfunctionedAIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF DURING LEFT ENGINE START, THE STARTER VALVE LIGHT TURNED ON AND EICAS MESSAGES, L ENG STARTED. DISPLAYED WITH START SELECTOR IN GND, ENGINE FAILED TO ROTATE. THE BREAKERS WERE RESEATED AND THE LEFT ENGINE WASSDR ASMF200510003Blade · damagedDURING TRANSIT CHECK, DETECTED A BLADE DAMAGED, LT ENGINE LPC 1ST STAGE. THE BLADE WAS OUT OF LIMITS WITH A DAMAGE OF 4 X 0.750 AT LEADING EDGE. DURING OVERNIGHT CHECK, THE TWO BLADES SET OF LPC 1 ST STAGE WAS REPLACED IAW MM 72-31-02, VIBRATION TEST NR 8 WASDR ASMF200510002Idg · failedAIRCRAFT RETURNED TO PLATFORM DURING TAXING. THE LT GENERATOR SHUTDOWN AND EICAS MESSAGES (RUDDER PCU, R ELEV PCU, L ELEV PCU, EQPT CLG TEST) WERE SHOWN. THE LT IDG REPORT WAS DEFERRED AND MAINTENANCE PROCEDURE WAS PERFORMED IAW MEL 24-00-1. THE LT IDG WAS RSDR ASMF200509013Valve · malfunctionedAIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF DURING ENGINES START, APU SHUT DOWN, FAULT LIGHT TURNED ON AND EICAS MESSAGE APU FAULT WAS DISPLAYED. THE FIM 49-11-00 PROCEDURES WAS PERFORMED. THE ENGINES START WAS PERFORMED WITH GROUND EQUIPMENT, ALL CORRSDR ASMF200509001Acm · failedAIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF DURING PUSHBACK, THE AIR CONDITION PACKAGE FAILED WITH EICAS MESSAGES OF RIGHT ENGINE PURGE VALVE DID NOT OPERATE. REPORT WAS DEFERRED IAW MEL 36-11-1.SDR ASMF200507016Elevator · out of rigCAPTAIN REPORTED THAT THE MESSAGE -ELEV ASYM- WAS SHOWN IN EICAS. THE FIM 27-09-00 FIG. 106 PROCEDURE WAS PERFORMED AND DURING CONTROLS TESTS REPEATED THE MESSAGE. DURING ELEVATOR SURFACE INSPECTION WAS DETECTED ASYMMETRY IN ELEVATORS. AIRCRAFT WAS SENT TO THESDR ASMF200506021Starter · failedACFT RETURNED TO PLATFORM. DURING RT ENGINE STARTING, N2 INDICATION REACHED 23 PERCENT AND WENT TO ZERO. PNEUMATIC STARTER AND PNEUMATIC STARTER VALVE REPLACED IAW MM 80-11-01 / -02, TESTED CORRECT.SDR ASMF200501015Valve · failedDURING TRANSIT CHECK WAS DETECTED A HYDRAULIC LEAK IN THE LEFT ENGINE FILTERS MODULE TUBE, TUBE WAS TIGHTENED AND ENGINE WAS MOTORIZED, BUT DURING THE PROCESS A NEW LEAK WAS DETECTED IN THE DE-OILER. AIRCRAFT WAS SENT TO THE HANGAR AND DURING OVERNIGHT SERVICSDR ASMF200412009Pump · damagedCAPT REPORTED LT HYD SYSTEM LOST, LT HYD QTY AT EICAS FAULT CODE 291106-01, LT HYD ELECTRIC PUMP FAULT CODE 291133-01, PTU FAULT CODE 292201-00 AND RT ELECTRIC PUMP OVERHEAT AT EICAS FAULT CODE 291113-02; THEREFORE LANDING GEAR WAS OPERATED IN ALTERNATE MODE. SDR ASMF200404024Tube · damagedDURING TRANSIT CHECK AN HYDRAULIC LEAK WAS DETECTED ON LT ENGINE. DURING MAINTENANCE REVISION AN HYDRAULIC TUBE (P/N 316N3100-28) WAS DETECTED WITH DAMAGE. PROVISIONAL FLEXIBLE HOSE WAS INSTALLED, LEAK TEST WAS PERFORMED, NO LEAK WAS DETECTED. DURING OVERNIGHTSDR MEX2003405Warning Light · illuminatedAIRCRAFT ARRIVED WITH CAPTAIN REPORT OF EICAS MESSAGE FLAP-SLAT ELEC. ONCE WE HAVE ADDITIONAL INFORMATION WE WILL SEND YOU AS SUPPLEMENT TO THIS REPORT.(K)SDR MEX2003408Wire · looseAIRCRAFT ARRIVED WITH CAPTAIN REPORT OF (WARN ELEX/ SLAT FLAP ELEC STATUS) MESSAGE IN EICAS. DURING REVISION WAS DETECTED BCPU POPPED DUE TO LOOSE OF WIRE NUMBER 5 TB 5001. THE BCPU C/B 6-14 WAS RESETED AND FSEU POWER OPERATED IN A NORMAL WAY TEST PERFORMED SDR MEX2003237Indicator · failedAIRCRAFT RETURN TO PLATFORM DUE TO TCAS NR 1 BLOCKED WITH INDICATION IN DISPLAY. THE INDICATOR VSI/TRA DISPLAY WAS REPLACED IAW 34-22-06, ALL TEST CORRECT.SDR MEX2002300Warning System · false activationAIRCRAFT RETURNED TO PLATFORM AS CONSEQUENCE OF THE LIGHT (OIL FILTER CLOGGING) TURNED ON DURING LT ENGINE STARTING. TECH PERFORMED AN ERASER PROCEDURE AND THE ENGINES WERE STARTED AGAIN, MESSAGE DID NOT APPEAR AGAIN AND PARAMETERS WERE, OK.
Other aircraft with N804AM · 2
The FAA can assign a mark to another aircraft once a registration is cancelled. N804AM is registered now to the first aircraft listed.