N407AW
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| AIR WISCONSIN AIRLINES CORPORATION | Operator | 2008-12-14 – 2008-12-14 | Operator named in NTSB report |
| AIR WISCONSIN AIRLINES LLC (A6WA) | Operator | 2008-12-14 – 2008-12-14 | Operator named in NTSB report |
Accident & incident history
Maintenance disclosures
EMERGENCY LIGHTS, BETWEEN ROW 1- 5 WILL NOT LIGHT.
FORWARD EMER LIGHT CEILING LIGHT IS INOPERATIVE.
UNABLE TO OPEN SERVICE DOOR FROM OUTSIDE. DISASSEMBLED OUTER SERVICE DOOR HANDLE & INSPECTED IAW SUP 11-029B. MINOR DAMAGE ADDRESSED ON OUTER HANDLE SHAFT & ASSEMBLY. LUBRICATED & REASSEMBLED IAW AMM SUPP 11-029B.
SERVICE DOOR UNABLE TO BE OPENED FROM OUTSIDE. LUBED OUTER HANDLE & HANDLE RELEASE PIN AS REQUIRED. OPERATIONS CHECKED GOOD AT THIS TIME.
EMERGENCY FLOOR TRACK LIGHTING MISSING AMBER STRIP AT SEAT 1DF & MISSING END CAP.
FLIGHT 3825, ODOR OF ELEC BURNING IN CABIN AREA MID TO FWD. R & R BOTH POWER UNIT DIMMERS AT ROW 2D - F IAW AMM 33-21-04. OPS CHECKED GOOD. INSPECTED WIRING FOR POWER UNIT DIMMERS, NO FAULT FOUND, NO ELEC BURNING ODOR NOTED.
FLIGHT 3961STRONG ELECT BURNING SMELL AT ROW 3 IN CABIN. PER CREW, LIGHTING IS SUFFICIENT FOR DAY TIME FLIGHTS. ON CALL IDENTIFIED BALLAST ROW 3. PLACARDED & PLACED ON MEL. R & R 3 AC CEILING & SIDE WALL LIGHT POWER DIMMER UNITS IAW AMM 33-21-10 & 33-21-09. OPERATIONS CHECKED GOOD, REMOVED PLACARD.
FLAP FAIL AT 30 DEGREES IN FLIGHT. PERFORMED FLAP RESET PROCEDURE IAW AWAC, FLAPS RESET. PLACARD & PLACED ON MEL. TROUBLE SHOT IAW FIM 27-50-00 & AWAC SUP 98-018F, NO SDU LIGHTS. RECORDED FECU FAULT LOG & EVENT CIRCUMSTANCES LOG. FECU PASSED GND MX TEST. NOTED NO FLAP TWIST. FLAP CONTROL LEVEL FAULTS & CODES 19CI & 19C2 INDICATED A FALSE LEVER FAULT. FECU NR 7 TEST & FLAPS OPERATIONS NORMAL.
FORWARD AFT FACE OF FRAME 333 IS CORRODED.
FORWARD & AFT FACE FRAME 295 IS CORRODED.
CARGO BAY FLOORBEAM LBL 27 AT FS 589 TO FS 621 IS CORRODED AROUND SCREW HOLES.
RIGHT INBD FLAP LOWER OTBD EXTERIOR SKIN DENTED.
WIND SHIELD CTR POST ON RT LOWER ATTACH FITTING CRACKED.
NUMBER 3 HYD BRAKE ACCUMULATOR FWD MOUNTING BRACKET CRACKED.
LEFT WING LE ATTACH BRACKETS ARE CRACKED AT WS 139 & WS 149.
LEFT NR 2 SEAT TRACK HAS FOUR EACH AREAS OF CORROSION FS 394 - 409+128.
FUSELAGE SKIN UNDER LOWER T CAS ANTENNA IS CORRODED.
CARGO DOOR LOWER FWD TRACK MOUNT BRACKET CRACKED.
LEFT FS 484 CLIP CRACKED.
CLIP CRACKED FS 280 FLOORBEAM RBL10.
LEFT NR 3 FLOOR SEAT TRACK GOUGED & CORRODED.
EXTERIOR LOWER SKIN PANEL HAS CORROSION ON LOWER SURFACE AT FS 599+116 STRINGER 26L.
LEFT MLG DOOR ROLLER BRACKET CRACKED.
FLOOR SUPPORT BEAM HAS CRACKED CLIP AT FS 280, RBL 9 INBD CLIP.
PASSENGER DOOR INNER HANDLE CRACKED.
FS 409+128 VERTICAL BEAM AT RBL 18 IS CRACKED ON LOWER END.
INBOARD & OUTBOARD TIE CLIPS AT STRINGER 3L & FS 280 ARE CRACKED.
AFT SIDE OF FS 280 BULKHEAD CHAFED AT RBL 9 AT WL 86.L.
RIGHT FLOOR SEAT TRACK CORRODED FROM FS 424 - FS 559.
FORWARD EQUIPMENT COMPARTMENT FLOOR SKIN CRACKED ON LT SIDE AT FS 193.
FUSELAGE SKIN CRACKED AT AFT RT CORNER OF NLG WW.
RIGHT SEAT TRACK CORRODED BETWEEN FS 394 - FS 409+128.
RIGHT SEAT TRACK CORRODED BETWEEN FS 364 - FS 394.
RIGHT DRAG ANGLE COMMON TO BATTERY RIB CRACKED.
CARGO BAY TIE DOWN TRACK CORRODED, RBL 9 FROM FS 559+80 TO 559+112.
FLOOR SUPPORT FITTING AT FS 319 BELOW SERVICE DOOR IS CORRODED.
FLOORBEAM WEB CRACKED AT LBL 10 OTBD & FS 280 FROM LOWER OTBD PULLEY BRACKET ATTACHMENT BOLT HOLE.
FLOOR SUPPORT CROSSBEAM AT FRAME FS 349 CORRODED.
LEFT FLOOR SEAT TRACK CORRODED FS 364 - 394.
COMPLIED WITH CARD 4DMI17806 REPAIR DENTS FS 179 STRINGER 26 & 24.
CARGO DOOR SUPPORT BEAM LOWER CLIP AT FS 621 BULKHEAD CRACKED.
FRAME CORRODED AT FS 349 BETWEEN STRINGERS 25L & 25R.
LEFT SPOILERON CTR SPRING SEAL CRACKED.
AFT TIE CLIP STRINGER 3L TO FS 280 CRACKED.
DURING CLIMB ACFT YAWED UNCOMMANDED. COMPLIED WITH QRH, DISCONNECTED YAW DAMPERS & YAWING PERSISTED. FD NR 2 WAS ENGAGED. ACFT RETURNED TO PHL, EMERGENCY DECLARED. LANDED AT 46,900 LBS, NORMAL LANDING. IAW WO 212612 WC 5 FOR TROUBLESHOOTING & WORK PERFORMED. R & R YAW DAMPER LINEAR ACTUATOR, OPERATIONS CHECKED GOOD.
PAX DOOR SILL HAS CORROSION. FOUND CORROSION TO BE 100 PERCENT MATERIAL LOSS. REMOVED, FABRICATED, AND INSTALLED NEW SERVICEABLE SILL IAW SRM 51-42-06, 51-42-13, 51-42-21 AND 51-24-16.
LOWER CORE COWL 445AB HAS 1 EA GOUGE ON 2 INNER RIBS AND NUMEROUS SMALL GOUGES AND DENTS ON INNER SKIN. C/W REO 601R-71-12-4129 BY HAND BLENDING MINOR CHAFING CUTTING OUT DAMAGE AND FILLING WITH STRUCTURAL ADHESIVE. FABRICATED 3 EA DOUBLERS FOR OUT OF LIMITS.
PAX DOOR FWD PULL IN LEVER IS CHAFING THE PAX DOOR STRUCTURE. REPAIRED STRUCTURE IAW REO 601R-52-2058.
LEFT OTBD FLAP ROLLER FITTING CHAFED. PERFORMED REPAIR OF LT OTBD FLAP INBD ROLLER FITTING IAW REO 601R-57-53-943.
RIGHT MLG DOOR CHAFED ON LOWER L/E. REPLACED FILLER ON LOWER L/E ON RIGHT MLG DOOR IAW REO 601R-52-82-034.
THREE CARGO TRACKS ON LBL AND RBL 9 HAS CORROSION IN CARGO AREA. REMOVED AND INSTALLED SERVICEABLE CARGO TRACKS IAW AMM 53-01-11.
RT FLAP STUB FAIRING HAS CHAFING AND A DENT AFT END ASSEMBLED REPLACEMENT SERVICEABLE RT STUB FAIRING IAW SRM 51-40-11 AND 51-42-06.
PAX DOOR LATCH CAM TORQUE TUBE CLOSE OUT PANEL AFT ATTACHMENT BRACKET FWD .5 IS CRACKED. REMOVED CRACKED FWD BRACKET .5 LOCATED AND DRILLED NEW BRACKET, INSTALLED NUTPLATES ON BRACKET, INSTALLED NEW SERVICEABLE BRACKET ASSY IAW SRM 51-42-02, 51-40-11, 51-42-06 AND 51-45-00.
RT SIDE SEAT TRACK NR 3 GOUGED BEYOND LIMITS. R & R SEAT TRACK SECTION.
AFT PRESSURE BULKHEAD CENTER POST IS GOUGED AT TOP. REPAIRED AFT PRESSURE BULKHEAD CENTER POST FS 621 TO DEPTH. .055 AND FOUND TO BE WITHIN ALLOWABLE LIMITS IAW REO 601R-53-61-4636.
TOP OF PAX DOOR STAIR STRUCTURE HAS CORROSION. REMOVED OLD PAX DOOR EDGE MEMBER DUE THE CRACKS FOUND WHILE CLEANING CORROSION FABRICATED NEW EDGE MEMBER IAW SRMS 51-24-19, 51-42-06, 51-42-13.
MAIN CABIN DOOR WILL NOT OPEN FROM OUTSIDE. INSPECTED AND FOUND LOCKING PINS TO BE DRY. LUBED, ROLLERS AND LOCKING PINS IAW REF AMM 52-11-00. OPS CHECKS WITH CREW 5 TIMES. OPS CHECK GOOD.
DURING RON INSPECTION OF STARTER OIL, DISCOVERED THAT SEVERAL WIRE HARNESS COVERS WERE MELTED AND THERE WERE CARBON DEPOSITS ON THE ENG. SUSPECT POSSIBLE ENG FIRE. FOUND B-NUT ON THE FUEL FILTER OUTLET LOOSE AND LEAKING FUEL. ALL DAMAGE FOUND TO BE LIMITED IN NATURE AND DELT WITH INDIVIDUALLY ON WCS WITHIN THE WO IAW AMM 72-00-00-200-801, SPECIAL INSPECTION. REMOVED AND REPLACED NR 2 ENGINE REF CORE COWL HARNESS REF AMM TASK 71-50-00-000-804 AND 71-50-00-400-804.
AFTER SELECTING GEAR HANDLE UP, BOTH MLG RETRACTED, NLG DID NOT. RECEIVED GEAR DISAGREE AND NOSE DOOR OPEN WARNING MESSAGE. QRH- LANDED WITHOUT INCIDENT. REF WO 183218 FOR R & R OF NLG SELECTOR VALVE AND NLG PRIORITY VALVE REF AMM 32-3. OPS AND LEAK CK GOOD.
AFTER TAKE OFF DURING GEAR RETRACTION, RECEIVED GEAR DISAGREE GEAR UP CAUTION MESSAGE FOR APPROX 10 SECONDS WITH RT MLG RED HASH MARKS, THEN CLEARED. R & R RT MLG SIDE STAY ACTUATOR IAW AMM 32-32-01 & SUPP 11-015. OPS AND LEAK CHECKED GOOD.
AT ALTITUDE, RECEIVED RT ENGINE OIL WARNING MESSAGE. (FL30.0 APPROX 80 PERCENT N1) RETARDED THROTTLE TO 76 PERCENT N1 WARNING EXTINGUISHED, PRESSURE READ 33 PSI. AFTER 5 MIN WARNING RETURNED. AT THROTTLE IDLE PRESSURE INDICATED 30 PSI. INDICATION FLUXUATED 5 PERCENT AT ALLN1 SPEEDS. ALL OTHER ENGINE INDICATIONS NORMAL. INSPECTED AND FOUND SIGNIFICANT AMOUNT OF OIL LEAKING FROM ENG. FOURN RT ENG SCAVENGE PUMP OIL FILTER HSG O-RING MISSING, INSTALLED O-RING M83248-1-136. SERVICED 7 QTS OF OIL. VERIFIED OIL REPLENISHMENT, SYS OPS NORMAL.
DC EMERGENCY BUSS CAUTION MESSAGE ENROUTE. FOUND CBP1-R7 POSER SENSE TO BE POPPED. RESET BREAKER MESSAGES CLEARED. C/W OPS CHECK OF LT AND RT FIRE EXT IAW AMM 26-11-00, APU EXT IAW AMM 26-12-11, AND RT FUEL SOV IAW AMM 28-21-36, BATT DIRECT FEED IAW AMM 24-32-01, APU BATT DIRECT SERVICE IAW AMM 24-32-02. OPS CHECK GOOD.
LT OTBD FLAP OTBD VANE TRUCK IS NEARLY FLUSH WITH VANE SKIN. REQUIRES BUTTE DOOR RIGGING AFTER REPAIR. R & R LT OTBD FLAP VANE OTBD TRACK PN 601R14502-1, IAW REO 601R-57-53-016.
RT MLG DOOR HAS CHAFE DAMAGE AT FWD AND AFT LOWER INBD EDGES COMPLIED WITH REO 601R-52-82-033, REV A, REO 601R-52-82-034, REV NC, REO 601R-52-82-290 REV NC TO REPAIR CHAFE DAMAGE.
AFT FRAME ON PAX DOOR AT DATUM NR1 IS CRACKED. REPAIRED IAW REO 601R-52-11-402.
DENT ON TOP OF FUSELAGE AT STA 644. REPAIRED DENT WITH LAP PATCH. REPAIR IAW REO 601R-53-61-3805.
INTERCOSTAL IN UPR REAR CORNER ON PAX DOOR IS CRACKED. R & R IAW SRM 51-42-06.
NR 2 HYD RETURN MANIFOLD BRACKET IN AFT EQUIPMENT BAY CRACKED. REPAIRED NR2 HYD RETURN MANIFOLD BRACKET IAW REO 601R-53-62-031.
FWD AND AFT DOOR HANDRAIL CLEATS UNDER FLOOR PANEL 213 CLF HAVE CORROSION. R & R AFT UNSERVICEABLE CLEAT AND IAW SRM 51-42-06 & REPAIRED FWD SERVICEABLE CLEAT IAW SRM 53-00-00.
LT NR1 AND NR2 FROM FWD CABIN FLOOR SEAT TRACKS HAVE CORROSION. REMOVED UNSERVICEABLE SEAT TRACK LT NR1 AND LT NR2 AND REPALCED BY SERVICEABLE SEAT TRACK PN NK6-2075 IAW AMM 53-01-11.
SEAT TRACK RAIL STA 559+80, RBL 9, PN 601R387779-13 CORROSION ON ATTACH HOLES FOR SEAT RAIL AND ON FLANGES. R & R WITH NEW SECTION OF SEAT TRACK.
51847-1000-0022-280 F/S, LBLB 9.0, INBD FLOOR BEAM ATTACH CLIP IS CRACKED. REMOVED DAMAGED CLIP, FABRICATED NEW SERVICE CLIP AND INSTALLED.
FS 280 FLOOR SUPPORT ANGLE HAS CORROSION UNDER FLIGHT DECK CTR FLOOR PANEL. REMOVED CORRODED SUPPORT ANGLE FABRICATED AND INSTALLED NEW SERVICEABLE SUPPORT ANGLE AT FS 280.
51847-1000-0025-FS 280, RBL 9, INBD FLOORBEAM ATTACK CLIP IS CRACKED. REMOVED DAMAGED CLIP FABRICATED AND INSTALLED NEW SERVICEABLE CLIP.
FS 280 FLOOR SUPPORT ON OTBD SIDE OF LBL 9 IS CRACKED. REMOVED DAMAGED AREA FABRICATED AND INSTALLED NEW SERVICEABLE ANGLE SUPPORT.
51847-1000-0026 F/S 280, 9.0 OTBD FLOORBEAM ATTACH ANGLE IS CRACKED, FABRICATED, LOCATED AND INSTALLED NEW SERVICEABLE CLIP ANGLE.
NR 4 AND NR 5 SEAT TRACK FLOOR CORRODED. REMOVED UNSERVICEABLE SEAT TRACKS LT NR 4, LT NR 5 ON FLOOR CABIN AND REPLACED SERVICEABLE SEAT TRACKS. PN 126-2075 IAW AMM.
LT MLG DOOR HAS CHAFE DAMAGE ON LWR INBD L/E. R & R DAMAGED FILLER IAW REO 601R-52-82-034.
RT FS 484 CLIP AND INTERCOSTAL CLIP ON OTBD SIDE OF RBL 27 CRACKED C/W REO 601R-53-41-059.
SKIN AT FS 202.0, WHERE PARKING CABLE PASSES THROUGH TO FWD HYD COMPARTMENT IS CRACKED. REPAIRED FS 202 BULKHEAD SKIN IAW REO 601R-53-11-1969 REV A DATED 2010-09-06.
RT BATT RIB IS CRACKED. REPAIR IAW REO 601R-57-51-046, REV B, REPAIR NR 3.
LT BATT RIB CRACKED AT WS 53.60. REPAIRED LT BATT RIB IAW REO 601R-57-51-046, REV B.
FOUND FS BULKHEAD WEB TO HAVE 2 INDICATIONS NOTED. RT SIDE (1) OTBD OF RBL 9, WL 58.70, APPROX .2" L 50 PERCENT FSH, (2) RT SIDE INBD OF RBL 18 WL59.10 APPROX .3"L 50 PERCENT FSH, FS 559 LT CAP ANGLE INDICATION .3" L 80 PERCENT FSH. ALL FAILED NDT. PERFORMED A MAJOR REPAIR TO FS 559 BULKHEAD WEB AND CAP ANGLES BY COMPLYING WITH REO`S 601R-53-41-260 AND 601R-53-41-609. (K)
PASSENGER DOOR WILL NOT OPEN 1 FOOT. REMOVED AND REPLACED PAX DOOR ASSIST MOTOR AND FUSELAGE DOOR JAM MOTOR ASSIST ATTACH POINT EYE BOLT IAW AMM 52-11-08. OPS CHECKS GOOD. (K)
REQUEST INSP OF LANDING GEAR DUE TO YEAR DISAGREE MESSAGE INFLIGHT. REMOVED AND REPLACED RT SIDESTAY ACTUATOR. (K)
LT MLG DID NOT EXTEND ON LANDING.
RECEIVED CABIN ALTITUDE MASTER WARNING MESSAGE IN FLIGHT AIRCRAFT ALTITUDE 12,000FT CABIN ALTITUDE 10,200FT, PRESSURIZATION WORKED IN NORMAL MODE. REF LOG 186158/1-COMPLIED WITH OPS CHECK OF CABIN PRESSURIZATION IN MANUAL MODE IAW AMM 21-31-00, OPS CHECK AND LEAK CHECK GOOD ON THE GROUND. (A)
ACFT WOULD NOT PRESSURIZE AFTER TAKEOFF, SWITCHED CONTROLLERS, TRIED MANUAL NO ABNORMAL INDICATION. DURING TROUBLESHOOTING OF ACFT PRESSURIZATION SYS FOUND CABIN PRESSURE TUBE ASSY B NOT CROSS THREADED. R&R CABIN PRESS TUBE ASSY IAW MM 21-31-00 REF W/C 9 FOR LEAK CHECK.
CABIN ALT CAUTION MESSAGE, RAN QRH AUTO 1&2 CONTROLLER INTERMITTENT AND MANUAL INOPERATIVE. REMOVED DEBRIS FROM EJECTOR JET PUMP. INSPECTED BOTH OUTFLOW VALVES. PER RELIABILITY AS PRECAUTIONARY REPLACED NR 1 CPC PER AMM 21-31-16. OPS CHECK GOOD. REMOVED PLACARD AND MEL.
CAPTAIN WINDSHIELD SHATTERED IN FLIGHT AT FL 260. R & R CAPT WINDSHIELD IAW AMM 56-11-01. OPS CHECK GOOD. NO LEAKS.
AIRCRAFT DID NOT PRESSURIZE AFTER TAKEOFF, CABIN RATE OF CLIMB MATCHED AIRCRAFT RATE OF CLIMB. NO EICAS MESSAGE RECEIVED. PLACED BOTH AUTOPRESSURE CONTROLLERS ON MEL. REMOVED AND REPLACED AUTOPRESSURE REGULATOR IAW AMM21-31-07. (K)
FLOOR LEVEL EMERGENCY LIGHTING ADJACENT TO ROW 1, ORANGE SEGMENT FWD INOPERATIVE. (K)
LT REVERSER UNLOCKED MESSAGE IN FLIGHT. REACTIVATED LT THRUST REVERSER PERFORMED FUNCTIONAL TEST IAW 78-30-00. CHECKS NORMAL THIS TIME PLACARD AND MEL REMOVED. (K)
ABORTED TAKEOFF BELOW 80 KNOTS DUE TO FAILED STANDBY AIRSPEED INDICATOR 0 KNOTS. ALL BRAKE TEMPERATURES INDICATE NORMAL. FOUND WATER IN P3 DRAIN. PERFORMED P3 CONTAMINATION REMOVAL PER AMM 34-11-00. PERFORMED LEAK TEST OF P3 PER AMM 34-11-00-790-803 TEST OK. (M)
STAB TRIM/MACH TRIM CAUTION MESSAGE IN FLIGHT. STAB TRIM STUCK AT 4.4 DEGREES. FLAPS AT 20 WHEN FAILURE OCCURRED, BOTH CHANNELS. REMOVED AND REPLACED STAB/MACH TRIM PANEL ASSEMBLY IAW AMM 27-40-00. (M)
RIGHT PACK HIGH TEMP CAUTION MESSAGE ON THE GROUND. COMPLIED WITH QRH, HAD SLIGHT ODOR OF SMOKE APPARENT AND SLIGHT HAZE. (M) [07-31-07] INSPECTED RT PACK, NO DAMAGE NOTED, OIL SERVICE OK. OBSERVED CREW OPERATE LT PACK, NO SIGNS OF SMOKE OR HAZE. (K)
UNUSUAL REPETITIVE NOISE AFTER GEAR RETRACTION. NOISE PERSISTED UNTIL GEAR EXTENSION, REPETITIVE PUMPING. TROUBLESHOOTING REVEALED R-NOSE DOOR ACTUATOR OUT OF RIG. (M)
SMOKE TOILET CAUTION MESSAGE DURING CLIMB-OUT. COMPLIED WITH QRH, AIR RETURN TO PHL. NO OVERWEIGHT LANDING 41,000 LBS, NO VISUAL SMOKE IN LAV OR CABIN. INSPECTED LAV, FOUND SMOKE DETECTOR OK. PERFORMED OPS CHECK IAW AMM 26-16-01-710-801. NO DEFECTS NOTED. REMOVED AND REPLACED LEFT AND RIGHT COALESCER BAGS IAW AMM 21-51-13. OPS CHECK GOOD. NO SMOKE NOTED. (M)
SMOKE TOILET CAUTION MESSAGE ON TAKEOFF CLIMB, COMPLIED WITH QRH, AIR RETURNED TO PHL NO OVERWEIGHT LANDING WTW 41,000 LBS. NO VISUAL SMOKE IN LAV OR CABIN. (M) REMOVED AND REPLACED PRESS REGULATING VALVE ASSY ON RT ENG IAW AMM 25-31-05. PERFORMED COMP WASH AND POWER RUNS NO SMELLS NOTED AND NO SMOKE NOTED THROUGH ALL POWER RANGES, OK FOR SERVICE. (K)
FOUND LEFT FS 409 PLUS 128 INBOARD VERTICAL BEAM LBL 27 HAS A .25 INCH CRACK AT BOTTOM RADIUS. MAINTENANCE REPAIRED BULKHEAD AT FS 409 PLUS 128 POST AT BL 27, LT IAW REO 601R-53-41-056 REV D. (M)
FOUND RIGHT WING PLANK ACCESS HOLE BETWEEN BL 0.00 AND WS 12.245 FUEL PANEL 610AB HAS MINOR CORROSION AT INBOARD RADIUS. MAINTENANCE BLENDED MINOR CORROSION, PERFORMED EDDY CURRENT, ROTOPEENED, SANDED AND APPLIED FINISH IAW REO 601R-57-21-030. (M)
FOUND RIGHT FS 280 RBL 9.0 INBOARD AND OUTBOARD FLOOR SUPPORT CLIPS CRACKED. MAINTENANCE REMOVED AND REPLACED FLOOR SUPPORT CLIPS AT FS 280 RBL 9 INBOARD AND OUTBOARD POSITIONS IAW CRJ SRM 51-40-11, 51-42-21 AND BSC SB 601R-53-0057A. (M)
FOUND LEFT FS 280 LBL 9 INBOARD AND OUTBOARD FLOOR SUPPORT CLIPS CRACKED. MAINTENANCE REPLACED AND REPLACED FLOOR SUPPORT CLIPS AT FS 280 LBL INBOARD AND OUTBOARD POSITIONS IAW SRM 51-40-11, 51-42--21 AND BSC SB 601R-53-0057A. (M)
FOUND LEFT SIDE FS 621 TO FS 625 INTERCOSTAL AT STRINGER 14L IS CRACKED NEAR RADIUS APPROX .6 INCH LONG. MAINTENANCE REMOVED AND INSTALLED NEW INTERCOSTAL/CLIP IAW CRJ 200 SRM 51-42-06. (M)
RECEIVED EFIS COMP MON ABOVE 80 KNOTS IAS MESSAGE V1, AFTER TAKEOFF RECEIVED STALL FAIL CAUTION 800 FT EXTREMELY LOUD NOISE COCKPIT. RETURNED FOR LANDING. FOUND OXYGEN SERVICE DOOR OPEN. SECURED DOOR, NO DAMAGE FOUND. INSPECTED RVSM CRITICAL AREA NO DEFECTS FOUND. INTERROGATED MDC, NO FAULTS FOUND. SPC COMPLIED WITH FUNCTIONAL CHECK OF STALL PROTECTION SYSTEM. TEST OK IAW CRJ200 AMM. (M)
FO SIDE WINDOW CRACKED DURING DESCENT AT 24,000 FT DIFFERENTIAL PRESSURE NOTED AT 7.2 PRESSURE NORMAL CONTINUED DESCENT IAW QRH FOR UNPRESSURIZED FLIGHT AS PRECAUTION. REMOVED AND REPLACED FO SIDE WINDOW. PRESURIZED CABIN. LEAK CHECK GOOD. WINDOW HEAT OPS CHECK GOOD. (K)
FOUND SKIN GOUGED AT PANEL B2AL ATTACH SCREW AT 1 O'CLOCK POSITION. BLENDED AREA, PERFORMED EDDY CURRENT AND TREATED BARE MATERIAL. (M)
RT FS 625 OBLIQUE ANGLE CRACKED IN RADIUS .3750 INCH LONG. REMOVED CRACKED ANGLE, INSTALLED NEW ANGLE IAW SRM. (K)
THE LEFT AND RIGHT INTERCOSTAL ATTACH ANGLES/CLIPS ARE CRACKED .25 INCH AT LBL 27 AND RBL 27, FS 484, WL 73. (M) REMOVED CRACKED ANGLES AT FS 484, RBL 27 AND LBL 27. INSTALLED NEW ANGLES, IAW SRM AND BRAS STD REP. (K)
NOSE GEAR OPEN GEAR DISAGREE, WOW YELLOW MESSAGE AFTER TAKEOFF AND GEAR RETRACTION, NOSE GEAR INDICATED DOWN. INSPECTED NOSE GEAR FOUND STEERING LINK DISCONNECTED, RECONNECTED STEERING LINKAGE, NO FURTHER DEFECTS NOTED. AIRCRAFT OK FOR SERVICE. (M)
FS 625 AT STR 14R, FUSELAGE TO HORIZONTAL INTERCOSTAL CONNECTING CLEAT HAS A CRACK AT THE FORWARD RADIUS. REPLACED CLEAT WITH PN S6144-4 IAW EO 601R-53-4181. NEW BRACKET (CLEAT) INSTALLED REF CRJ SRM 51-42-06 AND 51-42-21.
THE LEFT AND RIGHT CARGO FLOOR SUPPORT STRUCTURE IS CRACKED AT AFT PRESSURE BULKHEAD FS 621, WL 73.5 AND LBL 40 AND RBL 40. REPAIR IAW REO 601R-53-611-117 REV A. (M)
FOUND LEFT FS 625 STRINGER 14 OBLIQUE ANGLE, P/N 601-35012-51, IS CRACKED APPROX 2 INCHES. (M)
FOUND FS 625 RIGHT UPPER OBLIQUE ANGLE, P/N 601-35012-52, AT STRINGER 14 IS CRACKED APPROX 2 INCHES. (M)
FOUND FS 625 RIGHT UPPER OBLIQUE ANGLE, STRINGER 14 IS CRACKED APPROXIMATELY 2 INCHES. REMOVED AND REPLACED OBLIQUE ANGLE IAW CRJ 200 SRM 51-42-06. (M)
FOUND STRINGER 14 OBLIQUE ANGLE P/N 601-35012-51 IS CRACKED APPROXIMATELY 2 INCHES. REMOVED AND REPLACED OBLIQUE ANGLE IAW CRJ 200 SRM 51-42-06. (M)
PASSENGER DOOR OUTER HANDLE WARNING CAME ON DURING CLIMB THROUGH 17K FEET. CLEANED SWITCH, CYCLED DOOR, OPS CHECK GOOD.
FLAPS FAIL CAS ON APPROACH, LANDED AT FLAPS ZERO. MAINTENANCE C/W AWAC SUPPLEMENT 98-18 IN AMM CHAPTER 27, NO CODED FAILS IN LAST 72 HOURS, SYSTEM RESET.
FLAP FAIL CAS MESSAGE ON APPROACH. MAINTENANCE C/W AWAC SUPPLEMENT 98-18 OPS GOOD ECU CODES, JAM, RBPSU, PDU DIFF.