N635AS

Part: LIGHT — INOPERATIVE (PAX DOOR) · airframe 31,077 hrs · 34,737 cycles

PAX DOOR LOWER STEP BOARDING LIGHT INOP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,981 hrs · 34,633 cycles

CABIN FLOOR EMERGENCY LIGHT TRACK HAS A LIGHT OUT AT SEAT 17B.

Part: ENGINE — FAILED (LEFT) · airframe 29,566 hrs · 33,174 cycles

LEFT ENGINE FAILURE IN FLT. EMERGENCY DECLARED.

Part: ENGINE — FAILED (LEFT) · airframe 29,530 hrs · 33,134 cycles

LEFT ENG FAILED IN FLT. EMERGENCY DECLARED. FLT 4628 CX.

Part: BRACKET — BROKEN (FUSELAGE) · airframe 29,303 hrs · 32,855 cycles

FOUND ANGLE BRACKET BROKEN ON FRAME 23D IN WING BOX.

Part: WEB — CORRODED (WING) · airframe 29,303 hrs · 32,855 cycles

CORROSION FOUND ON THE LOWER WEB OF LE 612. REFER TO EXELTECH WORK PACKAGE YUL000164 NRTC 600-28 FOR ALL WORK ACCOMPLISHED. CORROSION REMOVED AS PER SRM 51-21-42 ON THE LOWER WEB OF L/E 612 AND FOUND WITHIN LIMIT AS PER SRM 51 10 10 REPAIR DETERMINED NOT TO BE A MAJOR REPAIR IAW SP 663 AND FAR 43 APPENDIX A REPAIR ACCOMPLISHED IAW 57 53 10. MATERIA THICKNESS .080" MATERIAL REMOVED .001" WITHIN LIMITS AS PE SRM 51 10 10...SUPPLEMENTAL - SDR CLOSED 01/23/07...

Part: RIB — CORRODED (RT WING) · airframe 29,303 hrs · 32,855 cycles

RT WING, OUTB FLAP, FLAP BEAM AT RIB 14 AFT PICK UP, CORROSION FOUND. REFER TO EXELTECH WORK PACKAGE YUL000164 NRTC 600-23 FOR ALL WORK ACCOMPLISHED. RT WING OUTBD FLAP, FLAP BEAM ATRIB 14 AFT PICK UP. CORROSION REMOVED AS PER SRM 51 21 42. AND FOUND WITH IN LIMIT S PER SRM 57 53 10 FIG 310 REPAIR DETERMINED NOT TO BE A MAJOR REPAIR IAW SP 663 AND FAR 43 APPENDIX A REPAIR ACCOMPLISHED IAW 57 55 10. MATERIA THICKNESS .475" MATERAIL REMOVED .001" WITHIN LIMITS AS PER SRM 57 55 10 FIG 310.

Part: BRACKET — BROKEN (LT WING) · airframe 29,303 hrs · 32,855 cycles

LT WING AT RIB 8 FWD UPPER INBOARD OMEGA IS BROKEN .

Part: RIB — BROKEN (LT WING) · airframe 29,303 hrs · 32,855 cycles

LT WING AT RIB 13 UPPER FLAP BEAM OMEGA BRACKET BROKEN.

Part: CONTROL CABLE — FRAYED (AILERONS) · airframe 29,303 hrs · 32,855 cycles

AILERON SERVO AUTO PILOT CABLE FRAYING AND SERVO ACTUATOR DRUM DAMAGED. REFER TO EXELTECH WORK PACKAGE YUL000164 NRTC AILERON AUTO PILOT ROLL ACTUATOR AND CABLES REMOVED IAW JIC 22-13-71 RAI 10000, AILERON SERVO AUTO PILOT CABLE AND SERVO ACTUATOR REPLACED IAW JIC 22-13-71 RA110000, AILERON SERVO AUTO PILOT ACTUATOR TESTED SERVICEABLE IAW AMM JIC 22-13-71 OPT 10000.

Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 29,303 hrs · 32,855 cycles

FR1 FWD PRESSURE BULKHEAD CORROSION FOUND AT BONDING POINTS (6X SPOTS).

Part: BRACKET — BROKEN (LT WING) · airframe 29,303 hrs · 32,855 cycles

LT WING AT RIB 8 FWD OUTBOARD OMEGA BRACKET ID BROKEN.

Part: DOOR — STUCK (EMERGENCY EXIT) · airframe 29,303 hrs · 32,855 cycles

ETNRTC 800-11 ON RT EMERGENCY DOOR, FORCE TO OPEN DOOR. TS 700 HIGH. REFER TO EXELTECH WORK PACKAGE YUL000-164 NRTC 2000-89 FOR ALL WORK ACCOMPLISHED. CABIN WINDOW NR 6 LT REPLACED IAW JIC 56 21 00 RAI 10000 001.

Part: RIB — BROKEN (LT WING) · airframe 29,303 hrs · 32,855 cycles

LT WING AT RIB FWD HINGE AFT OMEGA BRACKET BROKEN.

Part: BRACKET — BROKEN (TE FLAP) · airframe 29,303 hrs · 32,855 cycles

LT WING AT RIB 13 UPPER FLAP BEAM OMEGA BRACKET BROKEN AT LOWER SECTION.

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS) · airframe 29,220 hrs · 32,756 cycles

EMERGENCY EXIT SIGN LOWER AT ROW 1AB HAS LIGHT BULBS INOP.

Part: HYDRAULIC SYSTEM — LOW · airframe 29,069 hrs · 32,568 cycles

AFTER T/O AND FLAP RETRACTION HYD CAP - BLUE SYST LOW LEVEL FOLLOWED BY BLUE LO PRESS. DECLARED EMERGENCY, AFTER FOLLOWING QRH. LANDED AND TOWED TO PARKING.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,977 hrs · 32,461 cycles

FOUND CABIN FLOOR EMERGENCY LIGHTS INOP AT ROWS 7 AND 17AB.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,760 hrs · 32,205 cycles

CABIN FLOOR EMERG LIGHT STRIP AFT LIGHT INOP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,656 hrs · 32,081 cycles

EMERGENCY LIGHT ON BOTTOM PAX DOOR STEP IS INOP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,192 hrs · 31,513 cycles

EMER EXIT SIGN AT FWD LOWER SECTION OF RT REAR SERVICE DOOR EMER EXIT, LIGHT IS INOP.

Part: SUPPORT BRACKET — CRACKED (RT WHEEL WELL)

DURING HANGAR MAINTENANCE, THE RT WHEEL WELL AFT UPPER SUPPORT BRACKET WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE FABRICATED AND INSTALLED A DOUBLE IN THE RT WHEEL WELL AFT UPPER AREA IAW SRM. (K)

Part: LAMP — BURNED OUT (FUSELAGE)

DURING HANGAR MAINTENANCE, THE PASSENGER DOOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE PASSENGER DOOR EMERGENCY LIGHT. OPERATIONAL CHECKS GOOD. (K)

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT)

DURING A GROUND INSPECTION IN MGM, THE FLIGHT COMPARTMENT OVERHEAD PANEL EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE OVERHEAD PANEL EMERGENCY EXIT LIGHT. OPERATIONAL CHECKS GOOD. (M)

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS)

FLAP CONTROL ASSEMBLY, MALFUNCTIONED. (K)

Part: ACTUATOR — MALFUNCTIONED (RT WING TE FLAPS)

RT OB ACTUATOR, MALFUNCTIONED, RT WING. (K)

Part: ACTUATOR — MALFUNCTIONED (TE FLAPS)

FLT 4092 - DURING FINAL APPROACH INTO ATL FROM AVL, THE CREW RECEIVED A FLAP UNLOCK MESSAGE AND EXECUTED A MISSED APPROACH TO COMPLY WITH THE QRH. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT PERFORMED A REDUCED FLAP LANDING SAFELY INTO ATL. MAINTENANCE REMOVED AND REPLACED THE LEFT AND RIGHT INBOARD AND OUTBOARD FLAP ACTUATORS. OPERATIONAL AND LEAK CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: ACTUATOR — MALFUNCTIONED (TE FLAPS)

LT IB ACTUATOR, MALFUNCTIONED. LT WING.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

DURING A C-CHECK IN YUL, THE RIGHT FLOOR SUPPORT BETWEEN FRAME 38 AND 39 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE RIHT FLOOR SUPPORT BETWEEN FRAME 38 AND 39 IAW SRM 51-25-01. (M)

Part: FRAME — CORRODED (FUSELAGE)

DURING A C-CHECK, THE OUTER CHORD AT FR 17 LT WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE OUTER CHORD AT FR17 LT IAW SRM. (K)

Part: FLOORBEAM — CORRODED (FUSELAGE)

DURING A C-CHECK IN YUL, THE FLOORBEAM AT FRME 40 LT/RT WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE FLOORBEAM AT FRAME 40 LEFT/RIGHT IAW SRM 51-25-01. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

DURING A C-CHECK IN YUL, THE FLOORBEAM AT FRAME 36, STRINGER 14 L/R WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE FLOORBEAM AT FRAME 36, STRINGER 14 L/R, IAW SRM 51-25-01. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

DURING A C-CHECK IN YUL, THE LOWER FLOORBEAM AT FRAME 41, STRINGER 18R WAS FOUND TO BE CORRODED BEYOND LIMITS ON TOP OF THE FLANGE AND UNDER THE ANCHOR NUT. MAINTENANCE REMOVED AND REPLACED THE LOWER FLOORBEAM AT FRAME 41, STRINGER 18R IAW SRM 51-25-01. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

DURING A C-CHECK IN YUL THE LEF Z-FLOOR SUPPORT AT FRAME 39-40 AND THE RIGHT Z-FLOOR SUPPORT BETWEEN FRAME 39 AND 41 WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LEFT Z-FLOOR SUPPORT AT FRAME 39-40 AND THE RIGHT Z-FLOOR SUPPORT BETWEEN FRAME 39 AND 41 IAW SRM 51-25-01. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

DURING A C-CHECK IN YUL, THE RIGHT SEAT TRACK BETWEEN FRAME 39 AND 40 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE RIGHT SEAT TRACK BETWEEN FRAME 39 AND 40 IAW SRM 51-25-04. (M)

Part: DOUBLER — CORRODED (FUSELAGE)

DURING A C-CHECK IN YUL, THE DOUBLER ON THE FORWARD SIDE OF FRAME 39, STRINGER 14R WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE DOUBLER ON THE FORWARD SIDE OF FRAME 39, STRINGER 14R IAW SRM 51-25-01. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

DURING A C-CHECK IN YUL, THE LEFT AND RIGHT SEAT TRACKS BETWEEN FRAME 36 AND 39 WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LEFT AND RIGHT SEAT TRACKS BETWEEN FRAME 36/39 IAW SRM 51-25-04. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

DURING A C-CHECK IN YUL, THE RIGHT OUTBOARD SEAT TRACK BETWEEN FRAME 33/36 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE RIGHT OUTBOARD SEAT TRACK BETWEEN FRAME 33/36 IAW SRM 51-25-04. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

DURING A C-CHECK IN YUL, THE LEFT SEAT TRACK BETWEEN FRAME 39 AND 41 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LEFT SEAT TRACK BETWEEN FRAME 39 AND 41 IAW SRM 51-25-01 AND 51-25-04. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

DURING A C-CHECK IN YUL, THE LEFT AND RIGHT FLOOR SUPPORTS BETWEEN FRAME 36/38 WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LEFT AND RIGHT FLOOR SUPPORTS BETWEEN FRAME 36/38 IAW SRM 51-25-01. (M)

Part: CHANNEL — CRACKED (LT WING)

DURING C-CHECK, THE OMEGA BRACKET ON THE LT IB WING AT RIB 8 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE OMEGA BRACKET ON THE LT IB WING AT RIB 8 IAW SRM. (K)

Part: HOUSING — CORRODED (FUEL PANEL)

DURING A C-CHECK, THE HOUSING ON FUEL PANEL 622CT BETWEEN RIBS 4 AND 5 ON THE RT WING WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REPAIRED THE HOUSING ON FUEL PANEL 622CT BETWEEN RIBS 4 AND 5 ON THE RT WING IAW EO. (K)

Part: FRAME — CORRODED (FUSELAGE)

DURING A C-CHECK, THE FAIL SAFE FRAME SEGMENT IN THE AFT AVIONICS COMPARTMENT AT FR46, STRINGER 19L AND 19R WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE FAIL SAFE FRAME SEGMENT IN THE AFT AVIONICS COMPARTMENT AT FR 46, STRINGER 19L AND L19R IAW SRM. (K)

Part: SKIN — CRACKED (FUSELAGE)

DURING HANGAR MAINTENANCE, THE FUSELAGE SKIN AT THE T/E OF THE AFT EQUIPMENT COMPARTMENT ACCESS WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE PERFORMED A TEMPORARY REPAIR TO THE FUSELAGE SKIN AT THE T/E OF THE AFT EQUIPMENT COMPARTMENT ACCESS BY STOP DRILLING THE CRACKS IAW SRM 51-25-06. THE PERMANENT REPAIR IS TO BE PERFORMED WITHIN 50 FLIGHTS, IAW SRM 53-81-04, FIG 301, ZONE D. MAINTENANCE PERFORMED PERMANENT REPAIR IAW EO72-53-0159. AIRCRAFT OK FOR SERVICE.

Part: MODULE — SHORTED (EMERGENCY LIGHT)

FLT 4258 - FOLLOWING TAKEOFF FROM ATL-DHN, THE FLIGHT ATTENDANT NOTICED SMOKE IN THE CABIN. THE PILOT VERIFIED WITH THE FILGHT ATTENDANT THAT NO FIRE WAS PRESENT. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO ATL, LANDING SAFELY. MAINTENANCE FOUND A LOOSE WIRE SHORTING ON THE LIGHT SOCKET CLAMP OF THE PASSENGER SERVICE UNTI AT SEAT 13 A/B AND REMOVED AND REPLACED THE LIGHTING MODULE ASSEMBLY. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: WIRE — BROKEN (EMERGENCY LIGHT)

FLT 4276 - DURING A GROUND INSPECTION IN ATL, THE WIRING TO THE TWO AFT EMERGENCY FLOOR LIGHTS WAS FOUND BROKEN AND THE LENS COVER LOOSE. MAINTENANCE RESECURED THE WIRING AND LENS COVER ONTHE TWO AFT EMERGENCY FLOOR LIGHT TRACKS. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LIGHT — INOPERATIVE (PAX DOOR)

DURING AN A-CHECK IN MCN, THE EMERGENCY LIGHT ON THE PASSENGER DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT ASSEMBLY ON TH PASSENGER DOOR. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LAMP — BURNED OUT (EMERGENCY LIGHT)

DURING A GROUND INSPECTION, THE EMERGENCY LIGHT ON THE PASENGER DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT LAMP ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE.

Part: WARNING LIGHT — ILLUMINATED (TE FLAPS)

DURING APPROACH INTO AVL FROM ATL, THE CREW RECEIVED A FLAP UNLOCK MESSAGE WITH A MASTER WARNING. A GO-AROUND WAS INITIATED AND THE CREW REQUESTED EMERGENCY EQUIPMENT AS A PRECAUTION. A ZERO DEGREE FLAP LANDING WAS ACCOMPLISHED AND THE AIRCRAFT LANDED SAFELY IN AVL. MAINTENANCE INSPECTED THE FLAPS, ACTUATORS, SPOILERS AND HYDRAULIC SYSTEM FOR LEAKS. NO DEFECTS WERE NOTED. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LAMP — BURNED OUT (EMERGENCY LIGHT)

DURING HANGAR INSPECTION, THE PASSENGER DOOR EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR EMERGENCY LIGHT LAMP. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

DURING A C-CHECK IN BNA, THE LEFT AND RIGHT SEAT TRACKS AT FS 36 TO FS 39 WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LEFT AND RIGHT SEAT TRACKS AT FS 36 TO FS 39 IAW SRM 51-25-02. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

DURING A C-CHECK IN BNA, THE LEFT SEAT TRACK AT FS 39 TO FS 41 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LEFT SEAT TRACK AT FS 39 TO FS 41 IAW SRM 51-25-02. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

DURING A C-CHECK IN BNA, THE RT SEAT TRACK AT FS 39 TO FS 40 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE RIGHT SEAT TRACK AT FS 39 TO FS 40 IAW SRM 51-25-02. (M)

Part: BRACKET — CORRODED (TAIL CONE)

DURING A C-CHECK IN BNA, THE TAIL CONE MOUNTING BRACKETS AND SEAL RETAINERS WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE TAIL CONE MOUNTING BRACKETS AND SEAL RETAINERS IAW SRM 51-25-01. (M)

Part: COVER — LOOSE (EMERGENCY LIGHT)

DURING A GROUND INSPECTION IN ATL, THE EMERGENCY EXIT LIGHT COVER AT THE SERVICE DOOR WAS FOUND TO BE UNSECURED. MAINTENANCE RESECURED THE EMERGENCY EXIT LIGHT COVER AT THE SERVICE DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: DOUBLER — CRACKED (FUSELAGE)

DURING AN A-CHECK IN MCN, THE FORWARD PASSENGER/CREW DOOR FIRST STEP DOUBLER WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE PERFORMED A TEMPORARY REPAIR OF THE FORWARD PASSENGER/CREW DOOR FIRST STEP DOUBLER IAW ASA EO 72-52-0072. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DURING HANGAR MAINTENANCE IN MCN, THE PASSENGER DOOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR EMERGENCY LIGHT ASSEMLBY. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DURING A HANGAR CHECK IN MCN, THE FLOOR EMERGENCY LIGHT AT SEATS 14 A-B WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPAIRED A FLOOR EMERGENCY LIGHT GROUND WIRE AT SEATS 14 A-B. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: FLOORBOARD — CORRODED (FUSELAGE)

DURING C-CHECK INSPECTION IN BNA, THE FLOORBOARD SCREW HOLES AT FRAMES 9 AND 10 SHOWED SIGNS OF CORROSION AND SEVERAL ELONGATED HOLES WERE FOUND. MAINTENANCE REMOVED CORROSION AND REPAIRED ELONGATED HOLES WERE FOUND. MAINTENANCE REMOVED CORROSION AND REPAIRED ELONGATED HOLES IAW ASA E072-53-0123. THIS EO REF FAA FORM 8110-3, REPORT NR 01-295, WHICH INCLUDES REPAIR SPECIFICATIONS FOR AIRCRAFT. (M)

Part: ATTACH FITTING — DAMAGED (FUSELAGE)

DURING C-CHECK INSPECTION IN BNA, THE LEFT AFT WING FITTING AT FRAME 27 WAS FOUND TO BE ELONGATED. THE HOLE IN THE FRAME WAS ALSO ELONGATED. MAINTENANCE FABRICATED A NEW FITTING AND REPAIRED THE ELONGATED HOLE IAW ASA EO 72-53-0122. THIS EO REF SRM 51- AND ATR DRAWING 15S 535R 0181. THIS EO ALSO INCLUDES REPAIR SPECIFICATIONS FOR THE LEFT AFT WING FITTING AT FRAME 27 FOR AIRCRAFT. AIRCRAFT WILL RETURN TO SERVICE UPON COMPLETION OF C-CHECK. (M)

Part: FRAME — CRACKED (FUSELAGE)

DURING C-CHECK INSPECTION IN BNA, A CRACK WAS FOUND ON FRAME 26 AT BL 0. MAINTENANCE REPAIRED THE CRACK IN FRAME 26 IAW ASA E072-53-0121. THIS AIRCRAFT WILL RETURN TO SERVICE UPON COMPLETION OF C-CHECK. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

DURING C-CHECK INSPECTION IN BNA, THE RIGHT INBOARD SEAT TRACK, AT FRAME 35 TO 36, WAS FOUND TO HAVE CORROSION. MAINTENANCE REPAIRED CORRODED IAW ASA E072-53-0123. THIS EO REF FAA FROM 8110-3, REPORT NR 01-295, WHICH INCLUDES REPAIR SPECIFICATIONS FOR AIRCRAFT. (M)

Part: FLOORBOARD — CORRODED (FUSELAGE)

DURING C-CHECK INSPECTION IN BNA, THE TOP AND BOTTOM SURFACES OF THE FLOORBOARDS TOP FLANGE WERE FOUND TO BE CORRODED AT FRAMES 36, 38, 39, AND 40. MAINTENANCE REPAIRED CORROSION IAW WITH ASA EO72-53-0123. THIS EO REFERENCE FAA FORM 8110-3, REPORT NR 01-295, WHICH INCLUDES REPAIR SPECIFICATIONS FOR AIRCRAFT. (M)

Part: BATTERY PACK (CABIN)

ON GROUND IN ATL, CAPTAIN REPORTS RIGHT FRONT EMERGENCY EXIT LIGHT IS OUT. MAINTNANCE REMOVED AND REPLACED EMERGENCY EXIT LIGHT ON THE RIGHT SIDE AND THE BATTERY PACK AT 43VU. AIRCRAFT RETURNED TO SERVICE. (M)

Part: LINE — INOPERATIVE (HYD SYSTEM)

FLT 4082 - IN FLIGHT FROM CSG-ATL, CREW REPORTED WHEN THE LANDING GEAR WAS LOWERED A MASTER CAUTION MESSAGE ON THE GREEN HYDRAULIC SYSTEM. THE LANDING GEAR WAS SHOWING DOWN AND LOCKED WITH THE GREEN HYDRAULIC PRESSURE SHOWING ZERO. CREW DECLARED AND EMERGENCY AND LANDED SAFELY. MAINTENANCE REPLACED THE RIGID LINE TO GEAR UNLOCK ACTUATOR. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: IGNITERS — MALFUNCTIONED (RT ENGINE)

IN CRUISE FLIGHT CSG-ATL, WITH CONTINUOUS RELIGHT ON, RIGHT ENGINE TORQUE DROPPED TO ZERO FOR 8-10 SECONDS. ENGINE RELIT ON ITS OWN AND CONTINUED FOR THE REMAINDER OF THE FLIGHT. UPON LANDING, CONTINUOUS RELIGHT COULD NOT BE EXTINGUISHED. ATL MAINTENANCE BOROSCOPED THE ENGINE, FOUND NO DEFECTS. REMOVED AND REPLACED HIGH AND LOW PRESSURE FUEL FILTERS AND BOTH IGNITERS. OPERATED DE-ICE SYSTEM AND PERFORMED OPERATED TEST OF IGNITION IN CONTINUOUS RELIGHT MODE WITH NO DEFECTS NOTED. TEST FLIGHT PERFORMED SATISFACTORILY AND THE AIRCRAFT WAS RELEASED FOR FURTHER SERVICE. (M)

Part: SEAT TRACK — CORRODED (CABIN)

SAW - DURING '4 C' CHECK INSPECTION, MAINTENANCE REPORTED LT FA SEAT TRACK CORRODED. INSTALLED NEW LT FA SEAT TRACK IAW ASA EO 72-53-0035. AIRCRAFT RETURNED TO SERVICE.

Part: SUPPORT — CORRODED (FUSELAGE)

DURING C-CHECK INSPECTION, MAINTENANCE REPORTED RT Z-MEMBER CORRODED AT FRAMES 39-41. INSTALLED NEW RT Z-MEMBER IAW ATR 72 SRM 51-25-03. AIRCRAFT RETURNED TO SERVICE.

Part: SEAT TRACK — CORRODED (CARGO COMPT)

SAW - DURING '4 C' CHECK INSPECTION, MAITNENANCE REPORTED RT AFT CARGO SEAT TRACK CORRODED BEYOND LIMITS. INSTALLED NEW RT AFT CARGO SEAT TRACK IAW ASA EO 72-53-0036. AIRCRAFT RETURNED TO SERVICE.

Part: FILLER — CORRODED (SERVICE DOOR)

SAW - DURING C-CHECK INSPECTION, MAINTENANCE REPORTED FILLER PLATE ON SILL PLATE CORRODED. FABRICATED AND INSTALLED NEW PLATE IAW BASIC SHEET METAL PRACTICES AND INSTALLED IAW ASA EO 72-43-011. AIRCRAFT RETURNED TO SERVICE.

Part: SEAT TRACK — CORRODED (CABIN)

SAW - DURING '4 C' CHECK INSPECTION, MAINTENANCE REPORTED RT FA SEAT TRACK CORRODED. INSTALLED NEW RT FA SEAT TRACK IAW ASA EO 72-53-0035. AIRCRAFT RETURNED TO SERVICE.

Part: SUPPORT — CORRODED (FUSELAGE)

SAW - DURING C-CHECK INSPECTION, MAINTENANCE REPORTED SERVICE DOOR FLOOR SUPPORT CORRODED FRAMES 38-39. REPLACED FLOOR SUPPORT IAW ATR 72 SRM 51-25-03. AIRCRAFT RETURNED TO SERVICE.

Part: CHANNEL — CORRODED (CABIN)

SAW - DURING C-CHECK INSPECTION, MAINTENANCE REPORTED PASSENGER DOOR FLOOR SUPPORT CORRODED FRAMES 38 - 39. REPLACED FLOOR SUPPORT AT PASSENGER DOOR BETWEEN FRAMES 38 AND 39 IAW SRM 51-25-01. AIRCRAFT RETURNED TO SERVICE.

Part: SEAT TRACK — CORRODED (CABIN)

SAW - DURING C-CHECK INSPECTION, MAINTENANCE REPORTED RIGHT INBOARD AFT SEAT TRACK TO BE CORRODED. REPLACED RIGHT AFT INBOARD SEAT TRACK IAW ASA E.O. 72-53-0036. AIRCRAFT RETURNED TO SERVICE.

Part: SILL — CORRODED (SERVICE DOOR)

SAW - DURING C-CHECK INSPECTION, MAINTENANCE REPORTED SERVICE DOOR SILL PLATE CORRODED. INSTALLED SERVICE DOOR SILL PLATE KIT A01 IAW EO 72-53-0011 AND SB ATR 72-53-1048. AIRCRAFT RETURNED TO SERVICE.

Part: LATCH — NOT LATCHED (RT ENG COWL)

ON FINAL APPROACH AGS-ATL, RECEIVED A RIGHT ENG FIRE WARNING AT 200'. CREW ADVISED THE TOWER AND TOWER REPORTED VISIBLE FLAME. THE CREW DECLARED AN EMERGENCY, LANDED THE A/C AND PULLED THE T-HANDLE, THE WARNING REMAINED. THE F/O FIRED OFF THE ENG FIRE BOTTLE AND THE F/A'S EVACUATED THE A/C. THE FIRE WARNING WENT OUT. ATL MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND NO EVIDENCE OF FIRE, HOWEVER, FOUND 3 COWLING DOOR LATCHES NOT PROPERTY SECURED. LATCHES WERE SECURED AND THE AIRCRAFT INSPECTED AND FOUND SAFE FOR A FERRY FLIGHT TO MCN FOR REPAIR AND REPLACEMENT OF THE COWLING DOOR. FERRY FLIGHT AND SUBSEQUENT LANDING WERE UNEVENTFUL. (M)

Part: BATTERIES — DISCHARGED (CABIN)

CAPTAIN TESTED THE EMERGENCY LIGHT SYSTEM WITH A/C ON BATTERY POWER ONLY AND FOUND SEVERAL FLOOR LIGHTS AND OVERHEAD DOME LIGHTS FLICKERING. REMOVED AND REPLACED EMERGENCY LIGHT BATTERIES IAW MM. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: ACTUATOR — FAILED (LT ELEVATOR TAB)

RECEIVED A 'PITCH MISTRIM' MESSAGE ON ADU IN FLIGHT ATL-TRI. PILOT DISCONNECTED THE AUTOPILOT AND ATTEMPTED TO TRIM MANUALLY AS WELL AS USING THE STANDBY SYSTEM. NO TRIM LESS THAN 1/4 NOSE DOWN TRIM WAS AVAILABLE. AIRCRAFT RETURNED TO ATL WHERE LANDING WAS MADE SAFELY AND WITHOUT FURTHER INCIDENT. REMOVED AND REPLACED THE LEFT ELEVATOR TRIM TAB ACTUATOR IAW MM. OPERATIONAL CHECKS WERE GOOD ON GROUND RUN AND AIRCRAFT WAS RELEASED FOR FURTHER SERVICE. (M)