N414WF
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| SIMMONS AIRLINES | Operator | on 1995-09-06 | Operator named in NTSB report |
Accident & incident history
Operated by SIMMONS AIRLINES (per NTSB report)
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.
104 reports on file, 1996-01-10 – 2012-10-24.
Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 34,365 hrs · 33,986 cycles
THE CREW REPORTED THE SERVICE DOOR EMERGENCY SIGN WAS MISSING COVER. THE ACFT WAS REMOVED FROM SERVICE. RESECURED SERVICE DOOR EMERGENCY SIGN COVER AND OPERATIONALY TESTED IAW JIC 33-50-OPT-10000. TESTED SATISFACTORY. THE ACFT WAS RETURN TO SERVICE.
Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT) · airframe 34,295 hrs · 33,902 cycles
DURING MX INSPECTION, FOUND THE CABIN PASSENGER DOOR EMERGENCY LIGHT ON BOTTOM STEP INOPERATIVE. ACFT REMOVED FROM SERVICE. SECURED AIR STAIR ELECTRICAL CONNECTOR AND TESTED IAW JIC 33-50-00 ALL TEST OK. ACFT RETURNED TO SERVICE.
Part: WIRE — LOOSE (TEMP SENSOR) · airframe 34,166 hrs · 33,755 cycles
THE CREW REPORTED THAT DURING CURISE THE RT ENGINE WAS SURGING. A 10 PERCENT TORQUE SURGE, CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. FOUND LOOSE PIN ON RED WIRE ON TEMP SENSOR AIR BLEED. REPINED IAW SWM 20-43-13. THE OPS CHECK WAS GOOD. THE ACFT WAS RETURNED TO SERVICE.
Part: LIGHT — BROKEN (AFT GALLEY AREA) · airframe 34,049 hrs · 33,625 cycles
DURING B INSPECTION, FOUND THE GALLEY AFT EMERGENCY LIGHT BROKEN. THE ACFT WAS REMOVED FROM SERVICE. R & R THE GALLEY AFT EMERGENCY LIGHT IAW CMM 33-52-10. THE OPS CHECK WAS GOOD IAW W/C 335000-OPT-10000-001. THE ACFT WAS RETURNED TO SERVICE.
Part: BATTERY — INOPERATIVE (MAIN) · airframe 33,923 hrs · 33,479 cycles
DURING MAINTENANCE INSPECTION, FOUND THE MAIN BATTERY HAS NO POWER. THE ACFT WAS REMOVED FROM SERVICE. R & R THE BATTERY AND THE EMERGENCY BATTERY IAW WC EX-243185-RAI-10010-006. THE ACFT WAS RETURNED TO SERVICE.
Part: CAP — MISSING (EMERGENCY LIGHT) · airframe 33,880 hrs · 33,426 cycles
DURING B INSPECTION, FOUND SEVERAL EMERGENCY FLOOR LIGHT END CAPS MISSING. ACFT REMOVED FROM SERVICE. INSTALLED EMERGENCY FLOOR LIGHT END CAPS IAW CMM 33-52-10. ACFT RETURNED TO SERVICE.
Part: CAP — MISSING (EMERGENCY LIGHT) · airframe 33,828 hrs · 4,820 cycles
DURING B INSPECTION, FOUND THE FORWARD EMERGENCY FLOOR STRIP LIGHT MISSING END CAP IN GALLEY AREA . THE ACFT WAS REMOVED FROM SERVICE. INSTALLED FORWARD EMERGENCY FLOOR STRIP LIGHT END CAP IN GALLEY AREA IAW JIC 25-28-21 RAI 10000. THE AIRCRAFT WAS RETURNED TO SERVICE.
Part: CAP — MISSING (EMERGENCY LIGHT) · airframe 33,774 hrs · 33,302 cycles
THE CREW REPORTED THE END CAP ON FLOOR EMERGENCY EXIT LIGHT IN FRONT OF GALLEY AND AT 15B ARE MISSING. ACFT REMOVED FROM SERVICE. REPLACED AND SECURED END CAPS ON FLOOR PATH EMERGENCY LIGHTS BY GALLEY AND ROW 15 IAW MM 33-50-00 OPT 10000. THE OPS CHECKED GOOD. ACFT RETURNED TO SERVICE.
Part: LIGHT — LOOSE (GALLEY AREA) · airframe 33,608 hrs · 33,108 cycles
DURING B INSPECTION, FOUND THE EMERGENCY FLOOR LIGHT STRIP LOOSE IN GALLEY AREA. ACFT REMOVED FROM SERVICE. RESECURED EMERGENCY FLOOR LIGHT STRIP IN GALLEY AREA IAW JIC 25-28-21. ACFT RETURNED TO SERVICE.
Part: CAP — MISSING (EMERGENCY LIGHT) · airframe 33,536 hrs · 33,029 cycles
DURING B INSPECTION, FOUND THE EMERGENCY LIGHT FLOOR STRIP MISSING END CAP IN GALLEY AREA. THE ACFT WAS REMOVED FROM SERVICE. INSTALLED END CAP IAW 33-50-00. THE OPS CHECKED GOOD. ACFT RETURNED TO SERVICE.
Part: BATTERY — WEAK (FLASHLIGHT) · airframe 33,495 hrs · 32,979 cycles
DURING MX INSPECTION, FOUND THE FLASHLIGHT IN BACK OF ACFT WEAK. ACFT REMOVED FROM SERVICE. REPLACED BATTERY. ACFT RETURNED TO SERVICE.
Part: CAP — MISSING (EMERGENCY LIGHT) · airframe 33,495 hrs · 32,979 cycles
DURING MX INSPECTION, FOUND GALLEY EMERGENCY LIGHT, MISSING END CAP. ACFT REMOVED FROM SERVICE. INSTALLED END CAP IAW 33-50-00. ACFT RETURNED TO SERVICE.
Part: COVER — BROKEN (EMERGENCY LIGHT) · airframe 33,495 hrs · 32,979 cycles
DURING MX INSPECTION, FOUND ESCAPE PATH LIGHTING COVER BROKEN. ACFT REMOVED FROM SERVICE. INSTALLED LIGHT COVER IAW 33-5-00. ACFT RETURNED TO SERVICE.
Part: CONNECTOR — LOOSE (ENGINE) · airframe 33,461 hrs · 32,931 cycles
CREW REPORTED THE NR 2 ENGINE SURGED DURING CLIMBOUT, TORQUE BETWEEN 78.5 TO 81.5. DECLARED AN EMERGENCY AND PREFORMED AN OVERWEIGHT LANDING. THE ACFT REMOVED FROM SERVICE. PERFORMED ERU GROUND RUN UP ON NR 2 ENGINE. OPS CHECKED GOOD, NO SURGING NOTED IAW JIC 72-00-00-ERU-10040. COMPLIED WITH ENGINE TURBINE WASH PROCEDURES IAW EO E2-7200-008R5. PERFORMED ERU GROUND RUN UP ON NR 2 ENGINE. OPS CHECKED GOOD, NO SURGING NOTED IAW JIC 72-00-00-ERU-10040. CHECK FIRE WALL CONNECTOR, FOUND ALL FOUR ENGING TO AIRFRAME HARNESSES LOOSE AND BACK SHELLS ALSO LOOSE AND NOT SECURED. RESECURED ALL FIRE WALL CONNECTORS IAW AMM 72-00-00 AND SAFETY WIRED CONNECTOR IAW SPM 20-21-18 AND CLOSE THE AFT COWLS IAW AMM 72-00-00. THE ACFT WAS RETURNED TO SERVICE.
Part: HEATER — MALFUNCTIONED (NR 1 ENGINE FUEL) · airframe 33,439 hrs · 32,906 cycles
THE CREW REPORTED A HAZE DURING FINAL APPROCH IN CABIN AFTER LANDING IT WAS GONE. THE ACFT WAS REMOVED FROM SERVICE. HAZE POSSIBLE CAUSE IS RESIDUE FROM REPAIR. R & R NR 1 ENGINE FUEL HEATER IAW MM- 72-01-40. THE ACFT WAS RETURNED TO SERVICE. THE F/A REPORTED NO HAZE ON RETURN TO BASE.
Part: FUEL HEATER — FAILED (NR 1 ENGINE) · airframe 33,443 hrs · 32,912 cycles
DURING DESCENT AND APPROACH, FLT ATTENDANT NOTICED LIGHT SMOKE AND AN OILY ODOR. ACFT LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. R & R NR 1 ENGINE FUEL HEATER IAW MM- 72-01-40. ACFT RETURNED TO SERVICE.
Part: FUEL HEATER — FAILED (NR 1 ENGINE) · airframe 33,436 hrs · 32,902 cycles
DURING FINAL DESCENT AND APPROACH THE F/A REPORTED LIGHT SMOKE AND OILY ODOR. THE ACFT LANDED WITH OUT INCIDENT. THE ACFT WAS REMOVED FROM SERVICE. R & R NR 1 ENGINE FUEL HEATER IAW MM-72-01-40. R & R O-RINGS. PN: AS3209-110; MS9386-112. THE OPS CHECK WAS GOOD. THE ACFT WAS RETURNED TO SERVICE.
Part: UNKNOWN — SMOKE · airframe 33,426 hrs · 32,892 cycles
THE CREW REPORTED THE NR 1 PACK VALVE FAULT LIGHT ON APROX 1 MIN LATER FAS REPORT SEEING LIGHT SMOKE AND ODOR OF SMOKE. RAMP PERSONNEL REPORTED DETECTING SMOKE WHEN OPENING FWD CARGO DOOR. THE ACFT WAS REMOVED FROM SERVICE. THE OPS CHECKED NR 1 PACK SYS AND FOUND WORKING PROPERLY IAW JIC 21-10-00. OPS CHECKED GOOD. THE ACFT WAS RETURNED TO SERVICE.
Part: POWER SUPPLY — UNSERVICEABLE (EMERGENCY LIGHTS) · airframe 33,426 hrs · 32,892 cycles
THE CREW REPORTED THAT SEVERAL EMERGENCY LIGHTS ARE OUT. THE ACFT WAS REMOVED FROM SERVICE. R & R POWER SUPPLY 61WL IAW JIC 33-51-21, RAI 10000 & 33-51-21 RAI 10000. THE OPS CHECKED GOOD. THE ACFT WAS RETURNED TO SERVICE.
Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 33,378 hrs · 32,839 cycles
DURING MX, FOUND LEFT FORWARD EMERGENCY EXIT SIGNS INOPERATIVE. ACFT REMOVED FROM SERVICE. R & R POWER SUPPLY UNITS IAW JIC33-51-21, RAI10000 AND R & R THE POWER SUPPLY BATTERIES IAW RAI 10010. THE OPS CHECKED GOOD. ACFT RETURNED TO SERVICE.
Part: MOUNT — UNSERVICEABLE (ENGINE) · airframe 33,347 hrs · 32,805 cycles
DURING B INSPECTION, FOUND THE RT ENGINE, LT SIDE FORWARD MOUNT CRACKED OUT OF LIMITS. THE ACFT WAS REMOVED FROM SERVICE. R & R THE RT ENGINE LT SIDE FORWARD MOUNT IAW QEC BUILD UP GUIDE SECTION 71-00-04. THE OPS CHECK WAS GOOD. THE ACFT WAS RETURNED TO SERVICE.
Part: BULB — LOOSE (EMERGENCY LIGHT) · airframe 33,254 hrs · 32,693 cycles
DURING INSPECTION, FOUND THE EMERGENCY EXIT LIGHTS IN CABIN ROW 1A-1B INOPERATIVE. THE ACFT WAS REMOVED FROM SERVICE. RESECURED LOOSE LIGHT BULBS. THE OPS CHECKED GOOD IAW MM33-20-00. THE ACFT WAS RETURNED TO SERVICE.
Part: SWITCH — UNSERVICEABLE (EMERGENCY LIGHT) · airframe 33,076 hrs · 32,475 cycles
THE CREW REPORTED THE EMERGENCY LIGHTS WILL STAY ON WHEN ARM POSITION, AFTER BOTH ENG RUNNING HAS TO TURN OFF & THAN ARM TO LIGHTS TO EXTINGUISH. THE ACFT WAS REMOVED FROM SERVICE. R & R SWITCH 2WL. THE OPS CHECK WAS GOOD IAW JIC 33-50-00. THE ACFT WAS RETURNED TO SERVICE.
Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 33,059 hrs · 32,458 cycles
THE CREW REPORTED THAT AFTER START OR SHUTDOWN THE EMERGENCY LIGHTS STAYED ON, AND HAD TO BE RESET. THE ACFT WAS REMOVED FROM SERVICE. ACCOMPLISHED TEST IAW JIC 33-50, OPERATES OK, RAN ENGINE LIGHT, RESET CORRECTLY. NO PARTS REMOVED OR REPLACED. THE AIRCRAFT WAS RETURNED TO SERVICE.
Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 33,019 hrs · 32,413 cycles
THE CREW REPORTED THE EMERGENCY LIGHT NOT WORKING FORWARD LT SIDE "PLUG DOOR". THE ACFT WAS REMOVED FROM SERVICE. R & R BULB IAW AMM 33-50-00. THE OPS CHECK WAS GOOD. THE ACFT WAS RETURNED TO SERVICE.
Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 32,989 hrs · 32,373 cycles
THE CREW REPORTED EMERGENCY LIGHT NOT WORKING FWD LT SIDE "PLUG DOOR". THE ACFT WAS REMOVED FROM SERVICE. R & R BULB. THE OPS CHECK WAS GOOD IAW AMM 33-50-00. ALSO THE NR1 INVERTER FAULT LIGHT CAME ON. R & R NR 1 INVERTER IAW JIC 24-21-81 SYS CHECK GOOD.
Earlier reports · 1996–2011 · 78 reports
2011
Part: CAP — MISSING (EMERGENCY LIGHT) · airframe 33,060 hrs · 32,459 cycles
DURING MX BASE INSP FOUND THE EMERGENCY LIGHT FLOOR STRIP MISSING END CAP AT SEAT 3B. THE ACFT WAS REMOVED FROM SERVICE. REINSTALLED THE EMERGENCY LIGHT FLOOR END CAP AT SEAT 3B IAW JIC 33-51-24 RAI1 0000. THE ACFT WAS RETURNED TO SERVICE.
Part: BULB — INOPERATIVE (EMERGENCY LIGHTS) · airframe 32,828 hrs · 32,192 cycles
EMERGENCY LIGHT FWD LEFT SIDE INOPERATIVE. RESEATED BULB. OPS CHECKED GOOD. REF AMM 33-10-00.
Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 32,670 hrs · 32,018 cycles
FLASHLIGHT AT F/A NR 1 STATION DOES NOT APPEAR TO BE CHARGING. THERE IS NO RED LIGHT. PERFORMED OPS CHECK OF F/A NR1 FLASHLIGHT IAW CMM 25-60-02. OPS CHECK GOOD.
Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 32,604 hrs · 31,948 cycles
2 EMERGENCY LIGHTS INOPERATIVE, 1 ON THE LT SIDE AND THE OTHER BY THE SERVICE DOOR. RELAMPED LIGHT 21LW AND REPAIRED WIRE 33512602 IAW SPWM 20-27-17. OPS CHECKED GOOD IAW JIC 33-50-00.
Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 32,576 hrs · 31,918 cycles
EMERGENCY LIGHT STRIP HAS INOPERATIVE LIGHT AT SEAT 8AB. R & R EMERGENCY LIGHT STRIP LAMP AT SEAT 8AB IAW CMM 33-52-10.
Part: CONTACT — DIRTY (EMERGENCY LIGHT) · airframe 32,515 hrs · 31,854 cycles
RIGHT FLOOD LIGHT BY THE SERVICE DOOR IS OUT. CLEANED CONTACT POINTS ON FLOOD LIGHT SOCKET. OPS CHECKED GOOD IAW JIC 33-50-00, OPT 100000-001.
Part: SKIN — CRACKED (MAIN PAX DOOR) · airframe 32,435 hrs · 31,772 cycles
PAX DOOR HAS CRACK ON OUTER SKIN AT HINGE END OF DOOR. PAX DOOR WAS R & R WITH SERVICEABLE UNIT.
Part: SKIN — CRACKED (PAX DOOR)
PAX DOOR SKIN CRACK NEAR FORWARD SIDE LOWER FITTING PAX DOOR WAS REMOVED AND REPLACED WITH SERVICEABLE UNIT. OFF UNIT TO BE REPAIRED IAW SRI DO/TS-4818/11-15963
Part: STRUCTURE — CORRODED (NR 2 NACELLE)
SMALL AREA OF CORROSION JUST INBOARD OF THE NR 2 ENGINE. BLENDED OUT CORROSION AND FOUND IT TO WITHIN LIMITS IAW SRM 51-21-42. TREATED, PRIMED AND TOP COATED IAW SRM 51-21-17 AND 51-21-27.
Part: SKIN — CRACKED (PAX DOOR)
PAX DOOR SKIN CRACK NEAR FWD SIDE LOWER FITTING. OPEN
Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 32,313 hrs · 31,646 cycles
THE CREW REPORTED THE EMERGENCY EXIT LIGHTS ABOVE BOTH F/A NR1 AND F/A, NR2 JUMPSEATS STAY ON WHILE ON THE GROUND THEN TURN OFF ONCE THE AIRPLANE WAS AIRBORN. THE ACFT WAS REMOVED FROM SERVICE. AT THIS TIME, THE OPS CHECK WAS PERFORMED AND FOUND THE EMERGENCY LIGHTS WORKING PROPERLY IAW MM W/C EX-335000 OPT 10000-02. NO PARTS R & R. THE ACFT WAS RETURNED TO SERVICE.
Part: UNKNOWN — UNKNOWN · airframe 32,057 hrs · 31,378 cycles
DURING T/O ROLL MASTER WARNING ENG ON CAP UNNABLE TO RESET AND OBTAIN A CLEAN CONFIG TEST. RUN UP RT ENGINE IAW AMM 72-00-00. FOUND OK.
Part: LAMP — LOOSE (EMERGENCY LIGHT) · airframe 31,902 hrs · 31,226 cycles
ONE AISLE PATH EVACUATION LIGHT BY ROW 7 BURNED OUT. REPOSITIONED BULB ON ROW 7 OPS CHECKED, FOUND OK IAW MM 33-50-00.
Part: CONTROL UNIT — ERRATIC (AUTOFEATHER) · airframe 31,466 hrs · 30,745 cycles
DURING DESCENT NR 1 ENGINE LOST POWER FOR 10 SECONDS OR LESS. ENG WARNING ON CAP NR 1 TORQUE INDICATE WENT TO ZERO & ACW GEN WENT OFF LINE. POWER RETURNED TO NORMAL. PERFORMEDED OPS CK IAW EX-055007-CS-20000-001. COULD NOT DUPLICATE THE PROBLEM. OPS CHECKED GOOD. LT/ENG NH AND NL INDICATION ERRATIC ON LOW POWER SETTING. R & R LT ENGINE AUTO FEATHER CONTROL UNIT IAW MM 72-01-10. PERFORMED GROUND RUN PERFORMANCE CHECK IAW 72-00-00-ERU-10040 AND 61-22-00-OPT-10010-003. NO DEFECTS FOUND.
2010
Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 31,172 hrs · 30,393 cycles
EMERGENCY EXIT LIGHTS REMAIN ILLUMINATED AFTER BEING TURNED OFF/ARMED. RESET SYS AND OPS CHECKED GOOD IAW AMM JIC 33-50-00 OPT 10000 ACFT, OK FOR SERVICE.
Part: CONTACTOR — BURNED (DC BUSS TIE) · airframe 31,011 hrs · 30,230 cycles
DC SERVICE UTILITY BUSS SHED DURING FLIGHT. DOES NOT RESET. SMELLED BURNING RELAY IN THE COCKPIT. REMOVED AND REPLACED DC BUSS TIE CONTACTOR 16PU IAW JIC 24-00-00 RAI 10040003
Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,616 hrs · 29,791 cycles
2 EMERGENCY EXIT PATH LIGHTS INOP IN FRONT OF GALLEY. REPLACED ASSY 2 EMERGENCY EXIT PATH LIGHTS IAW JIC 33-51-21.
Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 30,181 hrs · 29,344 cycles
LT WING FRONT SPAR BETWEEN ENG AND FUSELAGE 2 LOCK FASTERNERS SURROUNDING CORRODED. COMPLIED WITH LT WING LOWER SKIN CORROSION BLEND OUT IAW EO NR E2-5700-384 ( FWD SPAR RIBS 6 AND 7) DEFFERRED AS (ER TD,O AITJ NR 414570423. FOR FUTURE TOLERANCE INSP AND IAW MX REPAIR INSTRUCTIONS. DUE IN 12 MONTHS. (MAY 7, 2011). WORK ITEM TURNOVER. PERFORMED MAPING PROCEDURE OF LT WING RIB 6 & 7 FWD SPAR CORRODED AT THE LOCK FASTENER USING ULTRA SONIC METHOD. (PARAMETERS 37DL) SUBMITTED TO PROCEDURE FOR EVALUATION OF BLEED AREA. PERFORMED NDT (EDDY CURRENT) INSP ON BLEND AERA (LT WING FWD SPAR RIB 7&8) USING ETN 51-008 PROCEDURES (NSRTEC 000S & PENCIL PROBE 50W). NO DEFECT NOTICE AT THIS TIME.
Part: SPAR — CORRODED (LT WING) · airframe 30,181 hrs · 29,344 cycles
LT WING FRONT SPAR BETWEEN ENGINE AND FUSELAGE CORROSION AROUND 2 LOCK FASTENER. OPEN
2009
Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 29,164 hrs · 28,175 cycles
ON THE WAY FROM DFW TO SJT FLIGHT DIVERTED TO ACT WITH F/O WINDSHIELD CRACKED. AWAITING AML PAGE FOR FURTHER DETAILS.
Part: WINDSHIELD — FAILED (COCKPIT) · airframe 29,164 hrs · 28,175 cycles
DURING FLIGHT IN MODERATE RAIN AT 11,000 FT, A SPARK IN F/O WINDSHIELD BOTTOM RIGHT SIDE WAS SEEN, THEN ANOTHER ONE AND A CRACK BEGAN TO RUN DIAGONALLY ALONG FRONT WINDSHIELD. BEFORE ANYTHING COULD BE DONE FRONT WINDSHIELD SHATTERED AND F/O WINDSHIELD HEAT FAULT LIGHT ILLUMINATED. FOLLOWED CHECKLIST ON AOM AND LANDED. REMOVED AND REPLACED F/O WINDSHIELD IAW JIC NR 56-11-00.
Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 29,151 hrs · 28,163 cycles
EVIDENCE OF CORROSION UNDER PAX DOOR THRESHOLD AT FRAME 38. REMOVED CORROSION UNDER PAX DOOR THRESHOLD IAW ATR-72 SRM NR 51-21-42.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 29,151 hrs · 28,163 cycles
LT INBD AFT SEAT TRACK CORRODED BETWEEN FRAMES 33 AND 36. REMOVED AND INSTALLED SEAT TRACK IAW ATR-72 SRM NR 51-25-02.
Part: WINDSHIELD — FAILED (COCKPIT) · airframe 29,147 hrs · 28,161 cycles
CAPT WINDSHIELD BROKEN. AWAITING AML PAGE FOR FURTHER DETAILS.
Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 29,147 hrs · 28,161 cycles
LEFT WINDSHIELD CRACKED IN FLIGHT. REMOVED AND REPLACED LT WINDSHIELD IAW JIC NR 56-11-00-RAI-10000. PERFORMED PRESSURIZATION TEST AND FOUND SATISFACTORY.
2008
Part: LIGHT — FAILED (AIRSTAIR) · airframe 26,767 hrs · 25,679 cycles
EMERGENCY EVACUATION PATH LIGHT AT THE BOTTOM OF CABIN DOOR STAIR IS OUT. REMOVED AND REPLACED EMERGENCY GROUND ILLUMINATION FLOOD LIGHT ASSEMBLY ON MAIN CABIN DOOR STAIRS IAW AMM JIC NR 33-51-24.
2007
Part: PUMP — FAILED (HYD SYSTEM) · airframe 26,171 hrs · 25,062 cycles
AFTER GEAR UP SELECTION, DURING T/O, LOUD BANG HEARD AND UNLOCK INDICATION ON LT MLG. REMOVED AND REPLACED GREEN HYDRAULIC PUMP. PERFORMED EXTENSION AND RETRACTION OF LANDING GEARS. OPS GOOD IAW JIC 29-10-00.
Part: POWER SUPPLY — FAILED (EMERGENCY LIGHTS) · airframe 25,922 hrs · 24,803 cycles
CABIN DOOR EMERGENCY "EXIT" LIGHT SIGN INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY AND PERFORMED OP CK IAW JIC NR 33-50-00.
Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 25,880 hrs · 24,765 cycles
EMERGENCY LIGHT IN MAIN CABIN DOOR INOPERATIVE. RELAMPED MAIN CABIN DOOR EMERGENCY LIGHT.
Part: THRESHOLD — CRACKED (FUSELAGE) · airframe 25,732 hrs · 24,619 cycles
RT THRESHOLD GUTTER BETWEEN FRAME 36 TO 39 IS CRACKED AND CORRODED. RT THRESHOLD GUTTER FRAME 36-39. REPLACED IAW SRM 51-25-07.
Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 25,732 hrs · 24,619 cycles
CORROSION FOUND ON FWD PRESSURE BULKHEAD RT BL 187.5 AND BL 350. FWD PRESSURE BULKHEAD RT BL 187.5 AND BL 350 REPAIRED AS PER SRM 53-11-10 FIG 408.
Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 25,732 hrs · 24,619 cycles
RT THRESHOLD ANGLES (3) AT FRAME 36,37 AND 39 ARE CORRODED. RT THRESHOLD ANGLE FRAME 36, 37, 39. REPLACED IAW SRM 51-25-01.
Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 25,732 hrs · 24,619 cycles
CORROSION FOUND FWD PRESSURE BULKHEAD LT LOWER BONDING POINT. FWD PRESSURE BULKHEAD LT LOWER BONDING POINT REPAIRED AS PER SRD 53-00-00 FIG 438.
Part: BRACKET — CORRODED (FUSELAGE) · airframe 25,732 hrs · 24,619 cycles
LT FOLDING STEP BRACKETS ON THRESHOLD BETWEEN FRAME 36 TO 39 ARE CORRODED. LT FOLDING STEP BRACKET REPLACED IAW SRM 51-25-04.
Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 25,732 hrs · 24,619 cycles
RT THRESHOLD PLATE AT FRAME 36 IS CORRODED. RT THRESHOLD PLATE REPLACED IAW SRM 51-25-01.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 25,732 hrs · 24,619 cycles
RT FLOOR SUPPORT BETWEEN FRAME 36 TO 38 IS CORRODED. RT FLOOR SUPPORT BETWEEN 36-38 REPLACED IAW SRM 51-25-01.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 25,732 hrs · 24,619 cycles
LT SEAT TRACK BETWEEN FRAME 36 TO 39 IS CORRODED. LT SEAT TRACK BETWEEN FRAME 36-TO 39 IS REPLACED BY NEW ONE IAW SRM 51-25-04.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 25,732 hrs · 24,619 cycles
UPPER FLOORBEAM AT FRAME 41 IS CORRODED. UPPER FLOOR AT FRAME 41 IS REPAIRED IAW SRM 53-00-00 FIG 450.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 25,732 hrs · 24,619 cycles
RT SEAT TRACK BETWEEN FRAME 36-39 IS CORRODED. RT SEAT TRACK BETWEEN FRAME 36-39 IS REPLACED BY NEW ONE IAW SRM 51-25-04.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 25,732 hrs · 24,619 cycles
FLOORBEAM AT FRAME 38 IS CORRODED. NEW FLOORBEAM INSTALLED IAW SRM 51-25-01 AND 51-25-04.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 25,732 hrs · 24,619 cycles
FLOORBEAM AT FRAME 40 IS CORRODED. FLOORBEAM AT FRAME 40 REPAIRED AS PER 53-00-00 FIG 435.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 25,732 hrs · 24,619 cycles
FLOORBEAM AT FRAME 39 IS CORRODED. NEW FLOORBEAM IS INSTALLED IAW SRM 51-25-0 AND 51-25-04.
Part: STRUCTURE — CORRODED (LT AILERON) · airframe 25,732 hrs · 24,619 cycles
LT AILERON, LIGHTING STRIP CORRODED AND DISBONDED ON TOP SURFACE. LT AILERON LIGHTING STRIP REPLACED ON NWRC 180721.
Part: CHANNEL — CORRODED (AILERON TAB) · airframe 25,732 hrs · 24,619 cycles
LT AILERON, TRIM TAB, CLOSING CHANNEL CORRODED. NEW TRIM TAB CLOSING CHANNEL REPLACED ON LT AILERON IAW SRM 51-25-03.
Part: CHANNEL — CORRODED (LT AILERON) · airframe 25,732 hrs · 24,619 cycles
LT AILERON, CLOSING CHANNEL CORRODED. LT AILERON, CLOSING CHANNEL (NEW) REPLACED IAW SRM 51-25-03.
Part: SELECTOR VALVE — FAILED (MLG) · airframe 25,587 hrs · 24,490 cycles
AFTER T/O AND GEAR HANDLE SELECTED UP, L/G TOOK APPROXIMATELY 1.5 MIN TO FULLY RETRACT. BOTH RED AND GREEN INDICATION ON PANEL. L/G WAS CYCLED AS PER MOC REQUEST. UPON SECOND RETRACTION, SAME RESULTS OCCURED. REMOVED AND REPLACED L/G SELECTOR VALVE IAW JIC NR 32-31-51 RAI 10000. L/G INDICATION ALL NORMAL.
Part: LIGHT — INOPERATIVE (CABIN)
WHILE PERFORMING PS-2 CHECK MECH FOUND RT GALLEY EMERGENCY LIGHT INOPERATIVE. REPLACED RT GALLEY EMERGENCY LIGHT IAW MM 33-50-00. (K)
2004
Part: HMU — ERRATIC (LT ENGINE)
ABORTED TAKEOFF DUE TO LEFT ENGINE NR 1 ITT WENT TO 771 DEGREES. REMOVED AND REPLACED LEFT ENGINE HYDROMECHANICAL UNIT. (M)
Part: WINDSHIELD — CRACKED (COCKPIT)
F/O`S OUTER LAYER OF WINDSHIELD CRACKED IN FLIGHT. REMOVED AND REPLACED WINDSHIELD.
2000
Part: FLOORBEAM — CORRODED (FUSELAGE)
SAW - DURING CPCP-2 INSPECTION MAINTENANCE, REPORTED FLOORBEAMS 38 AND 39 CORRODED. MAINTENANCE REPAIRED BOTH FLOORBEAMS IAW SRM 53-00-00 FIGURE 435. AIRCRAFT RETURNED TO SERVICE. (M)
Part: SEAT TRACK — CORRODED (CABIN)
SAW - DURING CPCP-2 INSPECTION MAINTENANCE REPORTED THE RIGHT AFT INBOARD SEAT TRACK CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK IAW EO E9-5300-013. AIRCRAFT WAS RETURNED TO SERVICE. (M)
Part: FLOORBEAM — CORRODED (FUSELAGE)
SAW - DURING CPCP-2 INSPECTION MAINTENANCE, REPORTED FLOORBEAMS 38 AND 39 CORRODED. MAINTENANCE REPAIRED BOTH FLOORBEAMS IAW SRM 53-00-00 FIGURE 435. AIRCRAFT RETURNED TO SERVICE. REF SIMA3322. (M)
Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 14,208 hrs · 14,780 cycles
DFW - FLT 3544 - EMERGENCY EXIT LIGHT SWITCH COVER ON REAR FLIGHT ATTENDANT CONTROL PANEL IS MISSING. MAINTENANCE REPLACED COVER FOR LIGHT SWITCH. AIRCRAFT RETURNED TO SERVICE. (X)
Part: LAMP — INOPERATIVE (CABIN)
DFW - FLT 3759 - EMERGENCY FLOOR LIGHT BY PASSENGER DOOR BURNED OUT. REMOVED AND REPLACED LIGHT BULB AND OPS CHECK EMERGENCY LIGHTING SYSTEM IAW ATR72 JIC 33-50, OPS CHECK GOOD. (M)
Part: LIGHT — INOPERATIVE (CABIN) · airframe 14,133 hrs · 14,711 cycles
DFW - FLT 3565 - NUMEROUS EMERGENCY EXIT FLOOR PATH AND OVERHEAD LIGHTS DIM OR INOPERATIVE. (X)
Part: SPACER — CRACKED (MLG)
ON BOTH MAIN LANDING GEARS, THE SPACER ABOVE THE SWINGING LEVER IS CRACKED. DISCREPANCY FOUND DURING PERFORMANCE OF FCD E2-32-004, VISUAL INSPECTION OF LANDING GEAR SWINGING LEVER SPACER. (M)
1999
Part: BATTERY PACK — DISCHARGED (CABIN)
SGF - FLT 4370 - FLOOR PROXIMITY LIGHTS IN AFT CABIN AND SERVICE DOOR EMERGENCY EXIT SIGN DO NOT ILLUMINATE. REMOVED AND REPLACED A BATTERY PACK FOR THE FLOOR PROXIMITY LIGHTS AND THE LIGHT BULBS IN THE EMERGENCY EXIT SIGN. OPERATIONAL CHECKS GOOD. (M)
Part: BULBS — FAILED (CABIN)
SGF - FLT 4370 - FLOOR PROXIMITY LIGHTS IN AFT CABIN AND SERVICE DOOR EMERGENCY EXIT SIGN DO NOT ILLUMINATE. REMOVED AND REPLACED A BATTERY PACK FOR THE FLOOR PROXIMITY LIGHTS AND THE LIGHT BULBS IN THE EMERGENCY EXIT SIGN. OPERATIONAL CHECKS GOOD. (M)
1998
Part: ACM — SEIZED (LT PACK)
MIA - FLT 5804 - FOUL ODOR MIXED WITH POSSIBLE SMOKE IN THE CABIN/COCKPIT. SMELL ISOLATED TO THE LEFT ACM. REMOVED AND REPLACED AIR CYCLE MACHINE. (M)
Part: SEAT TRACK — CORRODED (CABIN)
SAW - DURING CPCP-8 INSPECTION, FOUND LEFT FLIGHT ATTENDANT, LEFT AFT INBOARD AND OUTBOARD, LEFT AND RIGHT FORWARD OUTBOARD AND RIGHT MIDDLE SEAT TRACKS CORRODED. REMOVED AND REPLACED SEAT TRACKS. AIRCRAFT RETURNED TO SERVICE. (M)
Part: SEAT TRACK — CORRODED (CABIN)
SAW - DURING CPCP-8 INSPECTION, FOUND LEFT FLIGHT ATTENDANT, LEFT AFT INBOARD AND OUTBOARD, LEFT AND RIGHT FORWARD OUTBOARD AND RIGHT MIDDLE SEAT TRACKS CORRODED. REMOVED AND REPLACED SEAT TRACKS. AIRCRAFT RETURNED TO SERVICE. (M)
Part: ZEE MEMBER — CORRODED (FUSELAGE)
SAW - DURING CPCP-8 INSPECTION, FOUND LEFT AFT ZEE MEMBER, BETWEEN FRAME 39 AND 40 CORRODED. REMOVED AND REPLACED ZEE MEMBER. AIRCRAFT RETURNED TO SERVICE. (M)
Part: SEAT TRACK — CORRODED (CABIN)
SAW - DURING CPCP-8 INSPECTION, FOUND LEFT FLIGHT ATTENDANT, LEFT AFT INBOARD AND OUTBOARD, LEFT AND RIGHT FORWARD OUTBOARD AND RIGHT MIDDLE SEAT TRACKS CORRODED. REMOVED AND REPLACED SEAT TRACKS. AIRCRAFT RETURNED TO SERVICE. (M)
Part: SEAT TRACK — CORRODED (CABIN)
SAW - DURING CPCP-8 INSPECTION, FOUND LEFT FLIGHT ATTENDANT, LEFT AFT INBOARD AND OUTBOARD, LEFT AND RIGHT FORWARD OUTBOARD AND RIGHT MIDDLE SEAT TRACKS CORRODED. REMOVED AND REPLACED SEAT TRACKS. AIRCRAFT RETURNED TO SERVICE. (M)
Part: SEAT TRACK — CORRODED (CABIN)
SAW - DURING CPCP-8 INSPECTION, FOUND LEFT FLIGHT ATTENDANT, LEFT AFT INBOARD AND OUTBOARD, LEFT AND RIGHT FORWARD OUTBOARD AND RIGHT MIDDLE SEAT TRACKS CORRODED. REMOVED AND REPLACED SEAT TRACKS. AIRCRAFT RETURNED TO SERVICE. (M)
Part: SEAT TRACK — CORRODED (CABIN)
SAW - DURING CPCP-8 INSPECTION, FOUND LEFT FLIGHT ATTENDANT, LEFT AFT INBOARD AND OUTBOARD, LEFT AND RIGHT FORWARD OUTBOARD AND RIGHT MIDDLE SEAT TRACKS CORRODED. REMOVED AND REPLACED SEAT TRACKS. AIRCRAFT RETURNED TO SERVICE. (M)
Part: FLOORBEAM — CORRODED (CABIN)
SAW - DURING CPCP-8 INSPECTION, FOUND FLOORBEAM 36 CORRODED. REMOVED AND REPLACED FLOORBEAM 36. AIRCRAFT RETURNED TO SERVICE. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
DFW - FLT 3541 - AFT SECTION OF EMERGENCY FLOOR LIGHTING SYSTEM IN CABIN WILL NOT EXTINGUISH. REMOVED AND REPLACED BATTERY PACK IAW JIC 33-51-71 SYSTEM TESTED NORMAL. AIRCRAFT WAS RETURNED TO SERVICE. (M)
1997
Part: BATTERY — DISCHARGED (CABIN)
DFW - FLT 3631 - DURING DEPARTURE A PORTION OF FLOOR EMERGENCY LIGHTS WERE OUT. CREW RETURNED TO GATE. NO FURTHER INCIDENT WAS REPORTED. RAI'D FORWARD LEFT NR 1 EMERGENCY BATTERY. OPS CHECK GOOD. (M)
Part: UPLOCK BOX — INOPERATIVE (RT MLG)
CRP - FLT 3858 - RIGHT GEAR UNSAFE LIGHT ON LOWER PANEL ILLUMINATED INTERMITTENTLY AND THEN THE SOUND OF THE GEAR RELEASING, OVERHEAD PANEL SHOW SAFE. RAI'D RT MLG UPLOCK BOX. OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M)
Part: BELLCRANK — LOOSE BEARING (RT AILERON)
DFW - DURING COMPLIANCE OF ENGINEERING ORDER E9-2700-001 AD 92-22-10 REPETITIVE INSPECTION OF AILERON CONTROL SYSTEM, MAINTENANCE FOUND THE OUTBOARD AILERON BELLCRANK IN THE RIGHT WING WITH THE CENTER BEARINGS LOOSE. BELLCRANK REMOVED AND REPLACED. OPS CHECK WAS SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. (X)
1996
Part: EEC — FAILED (NR 2 ENGINE)
ORD - FLT 4381 - DURING CLIMB NR 2 ENGINE TORQUE FLUCTUATED BETWEEN 70 AND 100 PERCENT AT ONE POINT. THE TORQUE DROPPED TO ZERO THEN THE ENGINE RELIT, PROP SYNC WAS TURNED OFF WITH NO EFFECT. AIRCRAFT RETURNED TO ORD WITHOUT FURTHER INCIDENT. RAI'D NR 2 ENGINE. EEC OPS CHECK GOOD ON FCF. AIRCRAFT WAS RETURNED TO SERVICE. (M)
Part: O-RING — FAILED (RT TE FLAP ACT)
HOU - FLT 3545 - BLUE SYSTEM HYD LOW LEVEL INDICATION, CRUISE FLIGHT. FOUND FLUID LEAKING ON RIGHT OUTBOARD FLAP ACTUATOR. REPLACED O-RING ON FLAP ACTUATOR AND SERVICE RESERVOIR, OPS AND LEAK CHECKED GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M)
Part: POWER SUPPLY — INOPERATIVE (CABIN)
DFW - FLT 3742 - EMERGENCY LIGHTS ON FLOOR LIGHTING STAYS ON CONTINUOUSLY. REPAIRED POWER SUPPLY AT 61WL. AIRCRAFT RETURNED TO SERVICE. (X)
Part: POWER PACK — INOPERATIVE (CABIN)
ORD - FLT NR 4029 - DURING TAXI, THE FLOOR EMERGENCY LIGHTS ILLUMINATED. MAINTENANCE REPLACED THE FORWARD NR 1 POWER SUPPLY, CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
DFW - FLT NR 3350 - EMERGENCY LIGHTS STILL ILLUMINATED WITH SWITCH OFF. RAI'D BATTERY PACK IN POWER SUPPLY 61WL. (M)
Part: POWER SUPPLY — INOPERATIVE (CABIN)
DFW - FLT 3543 - FORWARD CABIN EMERGENCY FLOOR LIGHTS INOPERABLE. REPLACED BATTERY PACK AND POWER SUPPLY CHECKED GOOD. RETURNED TO SERVICE. REFERENCE OPERATOR CONTROL NR SIMA960103.
Part: BATTERY PACK — DISCHARGED (CABIN)
DFW - FLT 3543 - FORWARD CABIN EMERGENCY FLOOR LIGHTS INOPERABLE. REPLACED BATTERY PACK AND POWER SUPPLY CHECKED GOOD. RETURNED TO SERVICE. REFERENCE OPERATOR CONTROL NR 96ZZZX311. (X)