FAA incident reports · 2
FAA accident and incident reports matched to this aircraft by N181FE and the event date: up to this one’s cancellation.
Incident 19990218011409IFinal Approach · Rochester, NYOn Thursday, February 18, 1999, a B-727-22, federal express flight 1492 extended the landing gear during approach to Rochester international airport. The NLG light stayed red, indicating an unsafe gear condition. The pilot executed a missed approach and…Incident 19901226062259IForced/Precautionary Landing · Indianapolis, INNR2 engine failure after rotation. Returned. Landed safely.
Service difficulty reports · 14
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 01FDEA00249Duct · failedNR 3 ENGINE STRUT OVERHEAT LIGHT ILLUM. DURING CLIMBOUT 17000 FT NR 1 BLD OPEN, NR 2 BLD CLOSED. LIGHT EXTINGUISHED WHILE RUNNING CKLIST FOR STRUT OVERHEAT LIGHT. *S/D* REPLACED DUCT ASSY PER MM 36-00-001-2. OPS AND LEAK CK OK.SDR 00FDEA00727Actuator · failedTAILSKID ANNUCIATOR WARN LIGHT ILLUM AND REMAIN ILLUM AFT LWR LAND GEAR FOR LAND. *S/D* REINSTALL ACTUATOR PER BAC 727-100 MM 32-71-11. OPS CK NORMAL.SDR 00FDEA00547Check Valve · leakingDURING CLIMBOUT GOT FIRE ALARM NR 3 ENGINE. WENT THRU RED TAB PROC, IND CEASED WHEN THROTTLE BROUGHT TO IDLE. REMOVED AND REPLACED 8TH STAGE CK VALVE, GASKETS AND CLAMPS IAW 727-100 MM 36-10-021-4, LEAK AND OPS CK NORM.SDR 00FDEA00415Indicator · failedNOSE GEAR DOWN LIGHT BURN OUT, DID GO AROUND. REPLACED ONE BULB & ALL INDICATIONS NORMAL. RELAMPED NOSE GEAR INDICATOR LIGHT OPERATION NORMAL PER MM 33-10-00.SDR 99FDEA00193Switch · failedNOSE GEAR DOOR LIGHT STAY ON 2ND OFF PANEL WITH RED DOOR WARNING ON FRONT PANEL. *S/D* REMOVED AND REPLACED RIGHT NOSE GEAR DOOR MICRO SWITCH PLUNGER ASSY PER MM 32-62-011-4 AND ADJUSTED AND TESTED PER MM 32-62-011-5. OPERATION TEST GOOD.SDR 98FDEA00427Bleed Line · loose98-0165 STA-FLL: LWR AFT BODY OVERHEAT LIGHT ILLUM PASSING FLT LEVEL 20. THE LIGHT EXTINGUISHED 3 MIN AFTER CLOSING NR 1 ENG BLEED AND THE LEFT PACK AS DIRECTED IN CHECKLIST. THE INITIAL CONFIGURATION WHEN THE LIGHT ILLUM WAS BOTH PACKS ON NR 1 AND RIGHT NRSDR 98FDEA00426Valve · overheat98-0164 - STA-AFW - IN CRUISE FLIGHT LEVEL 250 LOWER AFT BODY OVERHEAT LIGHT ILLUMINATED. AFTER OPENING NR 1 BLEED VALVE AND CLOSING THE LEFT NR 2 BLEED VALVE LIGHT EXTINGUISHED AFTER ABOUT 1 MINUTE. NO ANTI-ICE WAS USED. REMOVED AND REPLACED LEFT PACK VALSDR 98FDEA00422Pack Valve · leakingCLIMBING THRU 17,000 LOWER AFT BODY HEAT LIGHT CAME ON. COMPLIED WITH PROCEDURES. LIGHT WENT OUT AFTER SECURING NR 1 BLEED. LEAK BETWEEN PACK AND BLEED VALVE ON NUMBER 1 ACCORDING TO PROCEDURE. RAN ENGINE DUPLICATING BLEED CONFIGURATION. CHECKED DUCTING CSDR 98FDEA00007Overheat Light · illuminatedLOWER AFT BODY OVERHEAT LIGHT ILLUMINATED DURING CLIMBOUT PASSING FL270. ENGINE ANTI-ICE WAS OPEN DURING CLIMBOUT. NR 1 BLEED WAS OPENED AND NR 2 BLEEDS CLOSED AND RED TAB PROCEDURE WERE INITIATED. THE LIGHT EXTINGUISHED SHORTLY AFTER NR 2 ENGINE ANTI-ICE WSDR 97FDEA00598Oil Filter · failedENGINE NR 2 SHUTDOWN IN FLIGHT, FILTER BYPASS LIGHT ILLUMINATED. PRESSURE ON GAUGE READ APPROXIMATELY 32 PSI, OIL QUANTITY NORMAL. REMOVED AND REPLACED NR 2 ENGINE MAIN OIL FILTER. FILTER BYPASS LIGHT REMAINED OUT, OIL PRESSURE NORMAL. LEAK CHECK GOOD.SDR 97FDEA00341Overheat Wire · looseLOWER AFT BODY OVERHEAT LIGHT ILLUMINATED AT FL 250 REFERRED TO RED TAB OK LIST PG 2-/-14. LIGHT EXTINGUISHED AFTER STEP 14. A CHECKLIST INDICATES LEAK BETWEEN BLEED VALVE AND PACK VALVE. FOUND SENSING ELEMENT DISCONNECTED FROM SUPPORT CLAMP AND DROPPING DOSDR 96FDEA01316Skin · corrosionFUSELAGE SKIN CORROSION BETWEEN SKIN LAYERS FROM BS 1140 TO 1183 STR 15 TO 20R. REMOVED CORROSION AND CUT OUT DAMAGED SKIN BS 1148 TO 1183 STR 14 TO 20R. INSTALLED DOUBLER PER EA 7-5310-28796A AND SRM 53-30-3 FIG 12.SDR 96FDEA01272Ctr Wing Tank · corrodedDISCREPANCY: (NR 0701 ) CORROSION CENTER WING TANK, STA 866 SPAR AND LOWER CHORD CORRODED FROM LBL 20 TO RBL 50. CORRECTIVE ACTION: REMOVED CORROSION FROM LOWER CHORD AND INSTALLED REPAIR PER EA 7-5710-28806.SDR 96FDEA01271Ctr Wing Spar · corrodedNR0702 AND 703, CORROSION CTR WING TANK, STA 866 SPAR AND UPPER CHORD CORRODED FROM LBL 50 TO RBL 50. *S/D* REMOVED AND REPLACED REAR SPAR UPPER CHORD PER 51-40-4 FIG 1 AND EA 7-5710-28808.
Other aircraft with N181FE · 1
The FAA can assign a mark to another aircraft once a registration is cancelled. N181FE is registered now to the first aircraft listed.