N471ZW
Registered owner: CSI AVIATION INC, TX (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
DURING HEAVY MAINTENANCE, FOUND CORROSION ON FLOOR SUPPORT BEAM AT BL 27L, BETWEEN FS 574 AND FS 621. REPAIR INCLUDED BLENDING OF MINOR CORROSION, CUT AWAY OF CORROSION THAT WAS BEYOND LIMITS, HFEC OF REQUIRED AREAS, REPLACEMENT OF CUT OUT AREAS, AND REINFORCEMENT OF DAMAGED AREAS, APPLICATION OF SURFACE TREATMENT, SEALANT, AND PAINT AS REQUIRED. ALL WORK PER MHI REO 601R-53-61-8459 IR, AND APPLICABLE SRM AND NDTM MANUALS REFERENCED IN REO.
FLOOR SUPPORT ALONG AFT PRESSURE BULKHEAD FS 621 HAS CORROSION ON UPPER AND LOWER SURFACE AROUND NUTPLATES BETWEEN BL 9L AND 27L. BLENDED CORROSION, INSPECTED, REBUILT WITH EPOXY, INSTALLED DOUBLER, RESTORED SURFACE TREATMENT, APPLIED CIC.
REQUEST INSPECTION FOR F/O'S WINDSHIELD CRACKS. INSPECTED AND FOUND F/O WINDSHIELD TO BE OUT OF LIMITS IAW AWAC SUPP 14-201D REQUIRES REPLACEMENT. AIRCRAFT REMOVED FROM SERVICE.
AT 28000 FT DURING DECENT F/O AIRSPEED DECREASING AND EFIS COMP MON IAS CAUTION PRESENT AT 16000 FT F/O AIRSPEED RETURNED TO NORMAL. REMOVED AND REPLACED #2 ADC. OPS CHECK AND LEAK CHECK GOOD AT THIS TIME
ON CLIMB OUT REC'V GEN 1 OFF CAUTION MESSAGE. C/W QRH MESSAGE DISAPPEARED. REMAINED EXTINGUISHED REST OF FLIGHT. ***** AIRCRAFT REMOVED FROM SERVICE ***** R/R #1 IDG ASSEMBLY IAW AMM 24-11-01 REF 370816-4 FOR REQ LEAK AND OPS CHECK. SERVICED IDG IAW AMM SUP 17-086
SMOKE TOILET CAU MSG IN FLT NO FIRE OR SMOKE PRESET IN LAV CAU PERSISTED C/W QRH MSG PERSITED UNTIL LANDING. NO ONE IN LAV WHEN MSG APPEARED. NO OVERWEIGHT LDG. AIRCRAFT REMOVED FROM SERVICE. R/R LAV SMOKE DETECTOR PER AMM 26-16-01 OPS CHECK GOOD AT THIS TIME
DURING TAKE-OFF ROLL, RECEIVED IDG 2 DISC CAUTION FOLLOWED BY YD 2 INOP STATUS MESSAGE AND CONFIG SPLRS WARNING MESSAGE FOLLOWED BY GEN 2 OFF CAUTION MESSAGE. ABORTED TAKE-OFF AT 56 KNOTS. ALL BRAKE TEMPS BELOW 5, BTMS REMAINED GREEN. *******AIRCRAFT REMOVED FROM SERVICE******** INSPECTED AND FOUND OVERFLOW DRAIN CAP LEFT OFF ON IDG #2 NO OIL IN IDG TS PER FIM 24-10-00. IDG 2 DISCONNECT. SERVICED IDG #2 IN REF AWAC SUP 16-364A. NO LEAKS NOTED.OPS CHECK OF THE RIGHT IDG GOOD AT THIS TIME EF AMM 24-11-01. PERFORMED OPS CHECK OF THE YAW DAMP PANEL IN REF AMM 22-22-01. OPS CHECK GOOD. OPS CHECK SPLRS FEF AMM 27-61-00 OPS CHECK GOOD.
AFTER GEAR RETRACTION RECIEVED GEAR DISAGREE AND NOSE DOOR OPEN WARNING MSGS. C/W QRH MSGS CLEARED. ****AIRCRAFT REMOVED FROM SERVICE*********** INSP AND FOUND NLG PROX SW DMG'ED. PULLED CODE S23 NGOEXT. OPS CHECKED NLG DOOR IAW AMM 32-22-01. OPS CK GOOD. C/W M ACTION OF MEL 32-30-01. REF 363274-2 FOR MEL. REPLACED THE WOFFW NO. 2 AND CENTERED HARNESS ASSEMBLY PER AWA SUPP 12-029E, OPS CHECK GOOD. REMOVED PLACARD AND MEL.
471 20123 457-900-342 10HOURS ***** AIRCRAFT REMOVED FROM SERVICE ***** RH WING LEADING EDGE AT ANTI ICE STUB DUCT INBOARD BRACKET FOUND WITH CORROSION. REMOVED AND REPLACED 1EA BRACKET P/N 601R120371-245 AT RH FORWARD SPAR AT WS139.54 TO WS149.58. IAW CRJ200 SRM 51-42-06 REV 39. TT:39,576, TC:41531
471 20081 330500 MFG 453-900-500 41.3 HRS RH FLOOR DOOR SILL STRUCTURE HAS 4 SPOTS OF EXFOLIATION FS295-FS349. AIRCRAFT REMOVED FROM SERVICE. BLENDED CORROSION ON ANGLE P/N 601R38303-239 TO SERVICE DOOR SILL BETWEEN FS319.7 TO FS349 AND EVALUATED ORIGINAL MATERIAL THICKNESS IS 0.063ÿ½. MINIMUM REMAINING THICKNESS IS 0.037, L= 4.5ÿ½ X W=1.5ÿ½ FWD BLEND #1 AND MINIMUM REMAINING THICKNESS IS 0.043 L=9.5ÿ½ X W=1.5ÿ½ AFT BLEND #2. TEMPORARY DISPOSITION: THE SUBJECT CONDITION IS STRUCTURALLY ACCEPTABLE FOR 5,000 FLIGHT HOURS FROM THE TIME OF INCORPORATION OF REO # 601R53-21-3661 REVÿ½DATED 2023-11-10. AND REMOVED AND REPLACED 1EA ANGLE SUPPORT P/N 601R38783-13 AND 1EA FITTING P/N 601R38672-3 AT FS349 RBL36 TO RBL41 ON RH FLOOR STRUCTURE IAW CRJ SRM 51-42-06, 51-42-13, AND 51-42-20.PERFORMED HFEC WITH NO INDICATIONS. VERIFIED NO LOOSED OR PULLED RIVETS AND DENT IS SMOOTH AND FREE OF CREASE.
471 20103 330500 MFG 427-680-100 3 HRS LH UPPER FLOOR SKIN AND SILL HAVE NUMEROUS AREAS OF CORROSION BETWEEN FS339-FS259. ***** AIRCRAFT REMOVED FROM SERVICE ***** REMOVED AND REPLACED 1EA CLEAT P/N 601R31527-176, 1EA BRACKET ASSY P/N 601R31527-217 ON PASSENGER DOOR SURROUND STRUCTURE AT FS333+8 LBL42 AND 1EA ANGLE SUPPORT P/N 601R38673-43 ON LH FLOOR STRUCTURE AT FS349 LBL36 TO LBL42 AND RESTORED ALL FINISHES IAW CRJ200 SRM 51-42-06, 51-42-13, AND 51-42-20 PERFORMED HFEC WITH NO INDICATIONS.
471 20103 330500 MFG 427-680-100 3 HRS LH UPPER FLOOR SKIN AND SILL HAVE NUMEROUS AREAS OF CORROSION BETWEEN FS339-FS259. ***** AIRCRAFT REMOVED FROM SERVICE ***** REMOVED AND REPLACED 1EA CLEAT P/N 601R31527-176, 1EA BRACKET ASSY P/N 601R31527-217 ON PASSENGER DOOR SURROUND STRUCTURE AT FS333+8 LBL42 AND 1EA ANGLE SUPPORT P/N 601R38673-43 ON LH FLOOR STRUCTURE AT FS349 LBL36 TO LBL42 AND RESTORED ALL FINISHES IAW CRJ200 SRM 51-42-06, 51-42-13, AND 51-42-20 PERFORMED HFEC WITH NO INDICATIONS.
DENT ON THE R/H INBD UPPER SURFACE INBD END. DENT ON R/H INBD FLAP UPPER SKIN WS 50.489+13. L=5.200ÿ½ X W=0.400ÿ½ X D=0.008ÿ½ FOUND TO BE OUT OF LIMITS IAW SRM 57-52-00 REV 39. AIRCRAFT REMOVED FROM SERVICE. PERFORMED HFEC WITH NO INDICATIONS. VERIFIED NO LOOSED OR PULLED RIVETS AND DENT IS SMOOTH AND FREE OF CREASE.
STAB AND MACH TRIM DROPPED OFFLINE. AIRCRAFT REMOVED FROM SERVICE. OPS CHECKED GOOD, COULD NOT DUPLICATE. R & R HSTCU IAW AMM 27-41-01, PREVENTIVE. OPS CHECKED GOOD.
FLAP FAILURE CAUTION. FLAPS FAILED AT 8 DEGREES. PERFORMED FLAP RESET PROCEDURE IAW AWAC SUP 98-18I BOX 12. FLAPS RESET. PLACARDED AND PLACED ON MEL ***AIRCRAFT REMOVED FROM SERVICE*** FLAP FAILURE CAUTION. FLAPS FAILED AT 8 DEGREES. PERFORMED FLAP RESET PROCEDURE IAW AWAC SUP 98-18I BOX 12. FLAPS RESET. PLACARDED AND PLACED ON MEL ***ATW RON 8/23*** 1MH
AFTER THE CREW SELECTED FLAPS OUT OF ZERO THEY RECEIVED FLAP FAIL CAUTION MESSAGE. THE CREW COMPLIED WITH THEIR QRH AND PERFORMED A FLAP ZERO LANDING. THE CREW STATED THEY HAD A SMOOTH LANDING. MESSAGE WAS RESET AND A/C WAS FERRIED TO MKE FOR REPAIR. AIRCRAFT REMOVED FROM SERVICE. MX IN PROGRESS.
AFTER THE CREW SELECTED FLAPS OUT OF ZERO THEY RECEIVED FLAP FAIL CAUTION MESSAGE. THE CREW COMPLIED WITH THEIR QRH AND PERFORMED A FLAP ZERO LANDING. THE CREW STATED THEY HAD A SMOOTH LANDING. MESSAGE WAS RESET AND A/C WAS FERRIED TO MKE FOR REPAIR. AIRCRAFT REMOVED FROM SERVICE. REF AWAC WO 301427 FOR TROUBLESHOOTING AND DETAIL MX OF REPLACEMENT OF 8 FLAP ACTUATOR FOR OFF WING FREEZE TEST. FLAP SYS RETURNED TO FULLY SERVICEABLE CONDITION REF ASSOCIATED MX WC FOR ALL REQUIRED RII.
FLAPS FAIL CAUTION ON APPROACH, FLAPS FAILED AT 20 DEGREES. CREW PREFORMED GO-AROUND AND COMPLIED WITH THE QRH. ONCE ON THE GROUND AND AT THE GATE FLAP RESET PROCEDURE WAS FOLLOWED, IAW AWAC SUPPLEMENT 98- 18I BOX 12. FLAPS RESET. AIRCRAFT REMOVED FROM SERVICE. REF WORKORDER 301426 AND MX WORK CARD 15, FOUND LT BPSU DOES NOT HOLD TOLERANCE. R & R BPSU, IAW AMM 27-51-10. REMOVED PLACARD AND REMOVED FROM MEL.
FLAPS FAIL AT 20 ON APROACH CW QRH LANDED UNEVENTFULLY. FLAP FAIL OCCURED WHEN SELECING FROM 20 TO 30 DEG. PERFOREMED FLAP RESET PROCEEDURE, IAW AWAC SUP 98-18I BOX 12. FLAPS RESET. PLACARDED AND PLACED ON MEL. AIRCRAFT REMOVED FROM SERVICE. T/S RT BPSU FOUND TO BE BAD. R & R RT BPSU, IAW AMM 27-51-10. OPERATIONS CHECK GOOD. REM PLACARD REMOVED FROM MEL
***SUPPLEMENTAL**** ODOR OF FUEL IN COCKPIT AFTER APU START IN FLT. ODOR DISSIPATED AS SOON AS BLEED WHERE TURN OFF. AIRCRAFT REMOVED FROM SERVICE THE APU WAS PLACED ON MEL,48-10-01-01 AND MX C/W SUP 09-037C FOR UNUSUAL ODORS OF CONTAMINATION FROM THE APU OR ACM. TROUBLESHOOT AND FOUND APU AUTOSHUTDOWN TWICE @60% DURING START. METAL FOUND ON DIL DRAIN PLUG. SUSPECT FUEL ISSUE CAUSING FUEL SMELL IN CABIN IS OVERFUELING APU POSSIBLE FUEL CONTROL INTERMITTENT FAIL. NO NEW CODES ON ECU AFTER BOTH SHUTDOWN IN HANGAR APU AND GEN REQUIRE REPLACEMENT. REPLACED APU.
STRONG FUEL SMELL IN COCKPIT& CABIN AFTER STARTING APU. R&R EXCITER PER AMM 49-41-01-000-801, OPS CHECK GOOD. R&R BOTH APU IGNITORS PER AMM 49-41-05-000-801, OPS CHECK GOOD. SN OFF:1366J SN ON:J11060014 C/W AWA SUP 09-037C, NO UNUSUAL SMELL NOTED, NO FUEL LEAKS FOUND.
FUEL SMELL IN COCKPIT AND CABIN IN FLIGHT IMMEDIATELY AFTER APU START FOUND BOTH FUEL FEED AND FUEL RETURN LINES @ APU FUEL CONTROL LOOSE TIGHTENED AS REQUIRED.OPS CHECK GOOD IAW, AMM 49-10 AND AMM 21-00. NO UNUSAUL ODORS AT THIS TIME C/W SUP 09-037C. OPS CHECK GOOD. NO DEFECTS NOTED AT THIS TIME.
AFTER TAKEOFF, RECEIVED GEAR DISAGREE WARNING, NLG BOX WAS RED & NOSE DOOR WARNING MESSAGE. OCCURED IN ICING. MESSAGE CLEARED ON ITS OWN. THEN DURING APPROACH, RECEIVED GEAR DISAGREE AGAIN WITH RED NLG BOX & NOSE DOOR WARNING. CYCLED GEAR AND PUT HYD 2B & 3B PUMPS ON, MESSAGE THEN CLEARED. ALL HYD INDICATIONS WERE NORMAL. NO OTHER MESSAGES. AIRCRAFT REMOVED FROM SERVICE INSTALLED GEAR PINS IAW AWAC SUPP 11-054A. REF 312214/4 FOR MEL CHRISTOPHER PYLE A&P 3019835 R/R'D WOFF W2 SENSOR HARNESS (PS46A) REF AMM 32-61-05 UP TO 4.A. BOTH PROX SENSORS REQ'D ADJUSTMENT AND OPS CK REF 32-61-00-710-801 REF NEW WORK CARD FOR ADJUSTMENT AND CLOSEOUT
LEFT WING A/ICE (C) MSG CAME ON IN FLT. C/W QRH. MSG PERSISTS. WERE IN ICING CONDITIONS. CLIMBED TO HIGHER ALTITUDE TO LEAE ICING CONDITIONS. LEFT FUSELAGE AND WING SHOWED IN AMBER. AFTER CLIMBING ABOVE ICING CONDITIONS RCVD L WINGA/ICE, R WING A/ICE + ICE (C) MSG WITH BOTH WING+COWL WAS ON POSITION. AS WE INSPECTED WING FROM THECOCKPIT IT APPEARED CLEAN OF ICE. AIRCRAFT REMOVED FROM SERVICE PERFORMED OPS TEST OF ICE DET. SYSTEM IAW AMM 30-81-00, AND TEST OF WING ANTI-ICE IAW AMM 30-12-00 AND ENGINE COWLS TEST IAW AMM 30-22-00, ALL CHECKS GOOD. REMOVED PLACARD AND FROM MEL.
RIGHT TR UNLOCK CAUTION MESSAGE DISPLAYED DURING FLIGHT C/W QRH EMER STOW MESSAGE REMAINED. CREW LANDED NEAREST SUITABLE AIRPORT (IND) PER QRH. AIRCRAFT REMOVED FROM SERVICE LUBRICATED RT TR IAW AMM 12-20 OPS CHECK GOOD AT THIS TIME REMOVED PLACARD REMOVED FROM MEL
RECEIVED FLAP FAIL CAUTION MESSAGE ON APPROACH. EICAS INDICATES FLAPS @ 30 DEGREES. COMPLIED WITH QRH, EMERGENCY DECLARED. FLAPS SUCCESSFULLY RESET IAW AWAC SUPP. 98-018G AIRCRAFT REMOVED FROM SERVICE COULD NOT DUPLICATE FLAP FAIL CAUTION MSG. INTEREGATED F.E.C.U. FAULT CODES IAW FIM 27-50-00 & AWA SUPP 98-018G. REPLACED FLAP POSITION HANDLE ASSY IAW CRJ AMM 27-51-01. PERFORMED OPS CHECK OF FLAPS (27-54-00--710-801). REMOVED PLACARD, REMOVED FROM MEL.
RH FLOOR SILL FS 559+80 TO FS574 HAS CORROSION. REPLACED AIRCRAFT REMOVED FROM SERVICE REPLACED RH FLOOR SILL FS 559+80 TO FS574 IAW CRJ 200 SRM 51-42-06
RH FLOOR SILL FS 409+96 TO 409+112 HAS CORROSION. REPAIRED AIRCRAFT REMOVED FROM SERVICE REPAIRED RH FLOOR SILL FS 409+96 TO 409+112 IAW ASAP EA# AWAC-CRJ253-01375
SERVICE DOOR SEAL RETAINER AT BOTTOM CENTER OF DOOR HAS CORROSION AROUND FASTENERS AIRCRAFT REMOVED FROM SERVICE REMOVED AND REPLACED SEAL RETAINER ON SERVICE DOOR IAW AWAC SUPPLEMENT 19-310
NOSE LANDING GEAR SPADE DOOR CUT OUT RH AND LH AFT CORNERS CRACKED AIRCRAFT REMOVED FROM SERVICE REPAIRED NOSE LANDING GEAR SPADE DOOR CUTOUT SKIN RH AND LH CORNERS IAW BOMBARDIER REO 601R-53-11-010
LT INBOARD FLAP VANE HAS 3 CHAFES ON LEADING EDGE AIRCRAFT REMOVED FROM SERVICE REMOVED AND REPLACED FLAP VANE LEADING EDGE SKIN IAW CRJ200 SRM 51-42-13
PAX DOOR SEAL STRIKER IS GOUGED AT PREVIOUS REPAIR NEAR TOP, AFT, LATCH PIN FITTING AIRCRAFT REMOVED FROM SERVICE REPLACED DAMAGED STRIKER REPAIR IAW B/A REO 601R-53-22-033
LH FLOOR SEAT RAIL FROM FS 409+128 TO FS 559 HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE REPLACED LH FLOOR SEAT RAIL FROM FS 409+128 TO FS 559 IAW AWAC SUPP 19-254A
RH FLOOR SEAT RAIL FROM FS 409+128 TO 559 HAS CORROSION. REPLACED AIRCRAFT REMOVED FROM SERVICE REPLACED RH FLOOR SEAT RAIL FROM FS 409+128 TO 559 IAW CRJ 200 AMM 53-01-11
UPON REMOVAL OF FLOOR SILL FS559+80 TO FS 574 FOUND LOWER DOUBLER CORRODED. REPLACED AIRCRAFT REMOVED FROM SERVICE REPLACED LOWER DOUBLER IAW CRJ 200 SRM 53-51-43
FS 409+128 VERTICAL POST AT BL0 ANGLE CRACKED. REPLACED AIRCRAFT REMOVED FROM SERVICE REPLACED FS 409+128 VERTICAL POST AT BL0 ANGLE IAW REO 601R-53-41-889 REV D
RIGHT AILERON LEADING EDGE HAS CHAFFING MARKS ALONG UPPER SIDE AIRCRAFT REMOVED FROM SERVICE REMOVED AND REPLACED R/H L/E OF AILERON IAW CRJ200 SRM 51-42-06 AND AWAC SUP. 14-270
CARGO DOOR BEAM 601R35050-64 CUT BY CABLE ASSIST. REPLACED AIRCRAFT REMOVED FROM SERVICE REPLACED CARGO DOOR BEAM 601R35050-64 IAW CRJ 200 SRM 51-42-06
LEFT WING HINGE BOX @ WS80-50 HAS BROKEN BONDING WIRE TAB. AIRCRAFT REMOVED FROM SERVICE REPLACED TAB IAW CRJ 200 SRM 51-42-21.
SUPPLEMENTAL INFORMATION, NR 1 FLOOR SEAT TRACK ON RBL 9 HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE. REPLACED NR 1 FLOOR SEAT TRACK ON RBL 9 IAW AMM 53-01-11.
RIGHT PRESSURE FLOOR SILL CORRODED. AIRCRAFT REMOVED FROM SERVICE REPAIRED IAW CRJ 200 SRM 51-42-06, REO 601R-53-41-666 REV-C.
AFT PRESSURE BULKHEAD COUNTER BALANCE SPRING BOX MOUNT BRACKET CRACKED. AIRCRAFT REMOVED FROM SERVICE REMOVED AND REPLACED MOUNT BRACKET IAW CRJ-200 SRM 51-52-06
CARGO DOOR BEAM ATTACH ANGLE IS CRACKED. AIRCRAFT REMOVED FROM SERVICE REPLACED ANGLE IAW CRJ 200 SRM 51-42-21, 53-61-23, TR51-42.
FS 280 RBL 9 INBOARD CLIP IS CRACKED AIRCRAFT REMOVED FROM SERVICE REMOVED AND REPLACED CLIP IAW CRJ200 SRM 51-42-06 AND 51-42-42
FWD CARGO DOOR TRACK LOWER ATTACH POINT IS CRACKED. AIRCRAFT REMOVED FROM SERVICE REMOVED AND REPLACED FWD CARGO TRACK LWR ATTACH POINT BRACKET IAW CRJ 200 SRM 51-42-21 AND 51-41-00
DURING CRUISE FLIGHT, THE FLIGHT CREW RECEIVED A FLAPS FAIL CAUTION MESSAGE WITH FLAPS AT ZERO DEGREES. THE CREW COORDINATED WITH DISPATCH, DECLARED AN EMERGENCY AND LANDED IN IAD WITHOUT FURTHER INCIDENT. FLAP RESET ATTEMPT WAS NOT SUCCESSFUL.
FLAPS FAILED AT 0 DEGREES AT CRUISE FLIGHT.
DURING CRUISE FLIGHT, THE FLIGHT CREW RECEIVED A FLAPS FAIL CAUTION MESSAGE. THE CREW DECLARED AN EMERGENCY AND CONTINUED TO DESTINATION. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT.
FLAPS FAIL AT 20 DEGREES ON APROACH PERFORMED FLAPS RESET PROSEDURE IAW AWAC SUP 98-018G FLAPS RESET PLACARDED AND PLACED ON MEL
FORWARD PRESSURE BULKHEAD FS 202.75 & BL 23.71 IS CRACKED IN FIVE PLACES WHERE THE THE PARKING BRAKE CABLE PASSES THROUGH. CAN BE REPAIRED WITH GREO 601R-53-11-0563
AIRCRAFT HAS EXCESSIVE RIGHT HAND ROLL TENDENCY DURING ROTATION AND CLIMB. BOTH AUTOPILOTS ON AND OFF. REQUIRES APPROX 1/2 LEFT HAND WING DOWN TRIM FOR STRAIGHT AND LEVEL FLIGHT. THRUST WAS MATCHED FOR N1. FLIGHT CONTROL PAGE INDICATES LEFT AILERON SLIGHTLY UP. AIRCRAFT SPEED AND FLAP POSITION MAKE NO DIFFERENCE. AIRCRAFT REMAINS TOTALLY CONTROLLABLE IN ALL PHASES OF FLIGHT. AIRCRAFT WAS RIGGED CORRECTLY LAST NIGHT IN MKE. POSSIBLY PREVIOUS REPAIRS TO FLAPS. OTHER THAN AN REO MAY NEED TO CHANGE 2 FLAPS WHERE DAMAGE WAS REPAIRED. REPAIRS ARE 2 BY 2 AND THERE ARE 2 PATCHES ON 2 FLAP PANELS INSPECTED BOTH AILERONS FOUND THE RT AILERON SLIGHTLY UP FROM CENTER (0) ADJUSTED RT AILERON PCU INPUT LINK 1/2 TURN IAW AMM 27-11-00. TRAVEL CHECKS OK.
AIRCRAFT HAS EXCESSIVE RIGHT HAND ROLL TENDENCY DURING ROTATION AND CLIMB. BOTH AUTOPILOTS ON AND OFF. REQUIRES APPROX 1/2 LEFT HAND WING DOWN TRIM FOR STRAIGHT AND LEVEL FLIGHT. THRUST WAS MATCHED FOR N1. FLIGHT CONTROL PAGE INDICATES LEFT AILERON SLIGHTLY UP. AIRCRAFT SPEED AND FLAP POSITION MAKE NO DIFFERENCE. AIRCRAFT REMAINS TOTALLY CONTROLLABLE IN ALL PHASES OF FLIGHT. AIRCRAFT WAS RIGGED CORRECTLY LAST NIGHT IN MKE. POSSIBLY PREVIOUS REPAIRS TO FLAPS. OTHER THAN AN REO MAY NEED TO CHANGE 2 FLAPS WHERE DAMAGE WAS REPAIRED. REPAIRS ARE 2 BY 2 AND THERE ARE 2 PATCHES ON 2 FLAP PANELS. INSPECTED BOTH AILERONS FOUND THE RT AILERON SLIGHTLY UP FROM CENTER (0) ADJUSTED RT AILERON PCU INPUT LINK 1/2 TURN IAW AMM 27-11-00. TRAVEL CHECKS OK.
CLIMBING THOUGH 9000 FT, RECEIVED A LT JET OVERHEAT FAIL CAUTION MESSAGE. 15 SECONDS LATER RECEIVED A LT JETPIPE OVERHEAT WARNING WITH AUDIO. COMPLIED WITH QRH AND MESSAGE CLEARED AT 70% N1. LANDED, NORRMAL BRAKING. PERFORMED GVI OF LEFT JETPIPE SENSING ELEMENT AND CONNECTORS AND WIRES IAW AMM 26-11-04, PERFORMED CONTINUITY TEST ON THE LEFT JETPIPE SENSING ELEMENT IAW CMM 26-11-67, PERFORMED AN OPS TEST OF JETPIPE IAW AMM 26-11-00, OPS CHECKED GOOD, NO DEFECTS NOTED.
PAX DOOR AFT RISER PANEL CRACKED BEHIND AFT DRAG ANGLE.
PAX DOOR AFT RISER PANEL DRAG ANGLE IS CRACKED BY ASSIST MOTOR PULLEY YOKE.
LEFT WING LOWER SKIN CRACKED AT WS 148.019.
RIGHT WING LOWER SKIN CRACKED AT WS 148.019.
LEFT FLOOR SUPPORT CRACKED AT BS 589, IN THE CARGO BAY
RIGHT AIR CONDITIONING PRESSURE MANIFOLD LOWER ATTACH ANGLE CRACKED.
FLOOR SUPPORT AT BS 484, RBL 36 CRACKED.
PREVIOUS REPAIR ON THE RT FLOOR SUPPORT HAS CORROSION AT BS 559+96, IN THE CARGO BAY.
CARGO DOOR LOWER AFT VERTICAL STRUCTURE CRACKED. REPLACED THE VERTICAL STRUCTURE IAW SRM 51-42-07, 51-42-13, AND 51-42-21.
PAX DOOR FWD RISER ANGLE FILLER FROM PREVIOUS REPAIR IS CRACKED
RIGHT AFT PRESSURE BULKHEAD ZEE ANGLE TO BS 625 FRAME INTERCOSTAL CRACKED OTBD OF RBL 36
COMPLY WITH PERMANENT REPAIR PER ORDER CARD 263160 / 4DMI19173. COMPLIED WITH PERMANENT REPAIR IAW SRM 51-42-06, SUPP 17-280 DATED 11/06/2017 AND REO 601R-53-11-3151 REV -- DATED 2017-11-13.
RIGHT INBD FLAP LWR SKIN IS DENTED AT THE OTBD AFT CORNER.
RT TAIL PIPE FIRE SHIELD CRACKED AT 9 O'CLOCK POSITION. REPAIRED FIRE SHIELD IAW CMM 78-11-00-350-012-A01.
PAX DOOR LOWER AFT CLEAT CORRODED. REPLACED THE CLEAT IAW SRM 53-00-00, 51-40-06, 53-21-23, 51-21-06, AND 51-42-06.
PRESSURE BULKHEAD WEB FITTING BS 621 DAMAGED. REPAIRED THE BULKHEAD WEB IAW REO 601R-53-61-1230 REV-F.
LEFT MLG WHEEL WELL BAT RIB DRAG ANGLE IS CRACKED. REPLACED THE DRAG ANGLE IAW SRM 51-42-21.
SPARKS COMING FROM THE APU START & STOP PANEL ON OVERHEAD. REMOVED ALL POWER FROM AIRCRAFT, NO ARCING AT THIS TIME. NO FUMES OR ODORS NOTED. APU WAS RUNNING AND APU GENERATOR WAS ON. R & R THE APU POWER & FUEL AND START/STOP SWITCHES IAW ESPM 24-00. OPS CHECKED GOOD. INSPECTED PANEL, NO EVIDENCE OF DAMAGE NOTED.
4199 ON CLIMBOUT RECEIVED ANTIICE DUCT WARNING MSG. CW QRH MSG PERSISTS. MSG CLEARED ON DECENT WITH THRUST LEVERS AT IDLE. MSG RETURNED WITH THRUST LEVERS ADVANCED. ANTIICE WAS SELETED OFF DURING THE EVENT (MC-AS PART OF THE QRH PROCEEDURE) RH FUSELAGE WAS RED ON THE ANTIICE SYNOPTIC PAGE. THE 14TH STAGE SHUTOFF VLV WAS CLOSED AS PART OF THE QRH PROCEEDURE. RETURNED TO PHL. LANDING WEIGHT 45000LBS MAX BTMS READINGS WERE 5,6,3,5. SHORTLY AFTER ANTIICE DUCT WARNING MSG WAS RECEIVED, RECEIVED RIGH COWL ANTIICE CAUTION MSG. MSG CLEARED WHEN 14TH STAGE SOV WAS CLOSED. 14TH STAGE ISOLATION VLV WAS CLOSED AT ALL TIMES. MC-DIDNT SELELECT STBY, CAPTAIN THOUGHT THE DUCT FAIL AND OVERHEATLIGHTS WERE ON ON THE OVERHEAD PANEL
FLOOR EMERGENCY LIGHTS INOPERATIVE ROW 9 THROUGH 13. FOUND A LOOSE CONNECTOR, CONNECTED IAW AMM 33-51-01, OPS CHECKED GOOD.
A STRONG ODOR OF BURNING PLASTIC IN GALLEY AREA. INSPECTED GALLEY LIGHT , BALLAST, AND VENTILLATION IAW AMM 33-26-AND 25-21 NO ODORS DETECTED . INSPECTED SIDEWALL BALLAST IN OVERHEAD BIN 3DF, AND FOUND THE BALLAST WARM TO THE TOUCH AND ASSOCIATED LIGHTS BURNED OUT. REMOVED POWER FROM BALLAST AND THE ODOR CLEARED.
DURING CRUISE FLIGHT AT FL320, FLAPS DEGRADED STATUS MESSAGE. FLAPS REPEATEDLY MOVED FROM 0-3 AND BACK TO ZERO. AP ENGAGED, AIRCRAFT PORPOISED REPEATEDLY. 270KTS. ALL 3 B PUMPS INTERMITTENT. AIRSPEED RASTER RED. PULLED CBP1-B5 AND CBP2-B5 FLAPS REMAINED AT ZERO. DIVERTED WITH A SMOOTH LANDING.
AFTER SELECTING GEAR UP- 3 GREEN UP, A LOUD BANGING FROM NOSE GEAR DOOR AREA. SELECTED GEAR DOWN AND BANGING WENT AWAY. NO MESSAGES. RETURNED TO DEPARTURE AND LANDED NORMAL.
RECEIVED A, SKID OTBD AND INBD CAUTION MSGS WHEN EXTENDING GEAR ON APPROACH. C/W QRH, LANDED WITH NO ISSUES, BTMS 2-3-3-2. REPAIRED BROKEN WIRE AT LT INBD TRANSDUCER IAW AWAC SUP 12-075B. SYSTEM OPS CHECKS GOOD.
REQUEST INSPECTION OF BURNED RUBBER ODOR AT ROW 6 & ROW 7.
EMERGENCY EXIT LIGHT PLACARDS WILL NOT ILLUMINATE BY PAX & SERVICE DOOR.
FLIGHT 3782, FLOOR LEVEL EMERGENCY LIGHTS INOPERATIVE AT ROW 1.
FLIGHT 4007 EMERGENCY EXIT LIGHTS, FLOOD, AT PAX & SERVICE DOOR ARE NOT OPERATING. CONNECTED EMERGENCY LIGHTS AT 1DF, OPS CHECKED IAW AMM 33-11-00. OPS CHECKED GOOD.
ROWS 5 - 8 EMER FLOOR TRACK LIGHTING INOPERATIVE.
LEFT INTERCOSTAL MEMBER OTBD AT STRINGER 13L & FS 624.00 IS CRACKED, REPLACED.
RIGHT FLOOR SILL, JUST FWD OF THE SERVICE DOOR OPENING ASST FS 319.70 CORRODED, REPLACED.
GALLEY MOUNT SUPPORT PLATE ON THE SILL AT FS 310 CORRODED, REPLACED.
LOWER FRAME BRACKET AT FS 319.70 IS EXFOLIATED, REPLACED.
RIGHT WINDSHIELD OTBD SIDE POST, LOWER AFT ANGLE FITTING IS CRACKED, REPLACED.
INBD FLOOR LANDING ON LBL 27, BETWEEN FS 559+80 - FS 574 HAS CORROSION, REPLACED.
RIGHT FLOOR SILL, BETWEEN FS 559+80 - 559+112 HAS CORROSION SPOTS, REPAIRED.
ATTACH ANGLE IN LT MLG BAY AT APPROX FS 529.0 & LBL 50 CRACKED, REPLACED.
FLOORBOARD LANDING ON THE OTBD SIDE OF LBL 27, BETWEEN FS 571 - 621 HAS SEVERAL CORROSION SPOTS, REPLACED.
SKIN BELOW AFT LATCH FOR PANEL 211AL CRACKED, REPAIRED.
INTERCOSTAL AT FS 473.15, STRINGER 10L GOUGED, REPLACED.
LEFT LOWER CORE COWL OUTER SKIN AT NR 4, LATCH IS CRACKED, REPAIRED.
ANCHOR FITTING AT FS 349.00 CORRODED, REPLACED.
RIGHT WING INBD FLAP VANE LE RUBSTRIP IS CHAFED, WS 120.382.
COMPLIED WITH JC 4DMI17389, REPAIR INTERCOSTAL AT FS 621 BH CAP 601R-53-61-5079, REPAIRED.
RIGHT WING, INBD FLAP VANE LE RUB STRIP IS CHAFED, WS 104.099.
RIGHT OTBD CLIP AT STRINGER 12R & FS 624 IS CRACKED, REPLACED.
RIGHT WING INBD FLAP, LE VANE RUB STRIP IS CHAFED, WS 75.27.
SEAT TRACK ON RBL 9 HAS CORROSION, BETWEEN 559+112 & FS 574, REPLACED.
LEFT OTBD CLIP AT STRINGER 12L & FS 624.00 IS CRACKED, REPLACED.
PASSENGER DOOR SILL FLOOR SUPPORT ANGLE, HAS CORROSION INBD & OTBD SURFACES FROM FS 310.00 - 349.00, REPLACED.
RIGHT FLOOR ANGLE ON FWD SIDE OF FS 621 BULKHEAD IS CRACKED, REPLACED.
CARGO NET FLOOR TIE DOWN MOUNTING PLATE HAS SEVERAL CORROSION SPOTS, BETWEEN FLOORBEAMS 589 & 606, JUST INBD OF CARGO DOOR LOWER SILL, REPAIRED.
PASSENGER DOOR OPENING LOWER SILL, AFT CLEAT IS CORRODED IN CABIN. REMOVED CORRODED AFT CLEAT & BRACKET & INSTALLED REPLACEMENT AFT CLEAT & BRACKET ON PAX DOOR LOWER SILL IAW SRM 51-21-06, 53-00-00, 51-42-06, 51-42-13, 51-40-11 & 51-25-16.
PASSENGER DOOR LOWER SILL, FWD CLEAT IS CORRODED IN CABIN. REMOVED CORRODED FWD CLEAT & BRACKET. INSTALLED REPLACEMENT FWD CLEAT & BRACKET ON PAX DOOR LOWER SILL IAW SRM 51-21-06, 53-00-00, 51-42-06, 51-42-13, 51-40-11 & 51-25-16.
ANGLE CLIP IS CRACKED AT THE OTBD SIDE OF LBL 9 AT BEAM 280, REPLACED.
ANGLE CLIP IS CRACKED ON THE OTBD SIDE OF RBL 27 AT FS 484, REPLACED.
ANGLE CLIP IS CRACKED AT THE OTBD SIDE OF RBL 9, AT BEAM 280, REPLACED.
FLIGHT 3758 FLOOR LEVEL LIGHT ROW 9 - 12 NOT COMING ON.
FLIGHT 3846 ON CLIMB OUT, RT RUDDER TRAVELING TO THE LT & NOSE KICKING TO THE RT, FELT & SAW INDICATION ON ED2. HAPPENED ON CLIMB OUT, CRUISE & DESCENT, NO MSGS OBSERVED. R & R NR 1 & NR 2 YAW DAMP ACTUATORS.
FLIGHT 3868 IN CRUISE FLIGHT, RECEIVED PROXIMITY SYSTEM FAULT STATUS MESSAGE. 30 MINUTES LATER, WITH FLAPS 20, ON GEAR DOWN RECEIVED PARKING BRAKE SOV & INBOARD ANTI-SKID AMBER CAUTION MESSAGES. GO AROUND GEAR UP, CAUTION MESSAGES CLEARED, PROXIMITY REMAINED. ON GEAR DOWN, CAUTION MESSAGES RETURNED AT GATE. PSEU FLAGGED ELECTRONIC UNIT FAILURE. R & R PSEU ELECTRONIC UNIT IAW AMM 32-61-00. OPERATIONS CHECKED GOOD.
FLIGHT 3739, SMOKE COMING FROM LIGHTS OVER SERVICE DOOR IN GALLEY. SHUT LIGHTS OFF, SMOKE STOPPED. R & R A BURNED RECEPTACLE ON THE SECOND TO BOTTOM GALLEY LIGHT ASSEMBLY IAW ESPM 20-16. OPS CHECKED GOOD.
LOWER EMERGENCY LIGHT DOES NOT LIGHT UP AT ROW 1.
ON DIVERSION RECEIVED GLD UNSAFE CAUTION. QRH PROCEDURE COMPLIED WITH. MSG CLEARED BUT FLIGHT SPOILERS GO INTERMITTENT DEPLOYMENT ON FLIGHT CONTROL PAGE WITH HYD SYS PRESSURIZED.
AFTER TAKEOFF THRUST APPLIED RECEIVED IDG NR 2 CAUTION & GEN NR 2 CAUTION MSG. ABORTED TAKEOFF AT LESS THAN 20 KTS.
ON SELECTING GEAR DOWN, GOT GEAR DISAGREE WARNING. RAN QRH, NOSE WAS GREEN, BOTH MAINS WERE WHITE BOXES. USED MANUAL RELEASE TO GET THE MAINS DOWN. COMPLIED WITH ACTION OF MEL 32-30-01. PSEU REPORTS CURRENT FAILURE D043 DOWN ERROR MAIN GEAR EXTEND. SOLENOID REPLACED MAIN GEAR SELECTOR VLV IAW AMM 32-30. OPERATIONS & LEAKS CHECKED GOOD. REMOVED PLACARD REMOVED MEL.
STRONG FUEL SMELL OBSERVED DURING APU OPERATION INFLT & ON THE GND. SMELL DISSIPATES WHEN APU IS SHUTDOWN. INSPECTED APU & FOUND FUEL TO BE COMING FROM POWER SECTION. PERFORMED ENG RUNS & NO FUEL SMELL IN COCKPIT OR CABIN WITH APU OFF. R & R APU POWERPLANT IAW 49-10-00 & MTC 000-49-310-001AW. OPERATIONS CHECKED LEAK, CHECKED GOOD.
RIGHT PYLON PANEL 422AT HAS CRACKED SEAL RETAINER. REMOVED, FABRICATED & INSTALLED NEW SEAL RETAINER.
LEFT BUTE DOOR HINGE CRACKED. R & R BUTE DOOR HINGE.
CARGO DOOR FLOOR SILL HAS CORROSION ALONG THE LENGTH FROM FS 621 TO FS 570. BLENDED CORROSION FOUND TO BE OUT OF LIMITS. REMOVED UNSERVICEABLE FLOOR SILL & INSTALLED A SERVICEABLE FLOOR SILL IAW REO 601R-53-61-1574 REV A.
PASSENGER DOOR MOTOR ASSIST LOWER MOUNT BRACKET IS CRACKED AT BOTTOM. R & R PN 601R317745-7 IAW CRJ 200 SRM 51-42-06.
CARGO DOOR OUTER HANDLE IS CRACKED. R & R IAW CRJ 200 SRM 51-42-21 PN 601R35060-5.
FUSELAGE STATION 379, 3L STRINGER CRACKED. REPAIRED IAW SRM 53-00-03.
RIGHT INBD FLAP FIXED VANE LE CHAFED. R & R FLAP VANE LE SKIN AT WING STATION 143.
CARGO DOOR LOWER FWD ATTACH BRACKET CRACKED. R & R PN 601R35050-25 IAW CRJ 200 SRM 51-42-06.
RIGHT FLIGHT SPOILER INBD SPRING SEAL IS CRACKED. R & R UNSERVICEABLE SPRING SEAL.
PASSENGER DOOR UPPER AFT CAM FITTING GOUGED ON LOWER EDGE. R & R PAX DOOR UPPER AFT CAM FITTING.
RIGHT EXHAUST FAIRING FWD UPPER STIFFENER IS GOUGED. R & R DAMAGED STIFFENER.
BRACKET CRACKED LT SIDE AFT FACE OF 621 PRESS BULKHEAD STRINGER 14L AREA. CONDITION ACCEPTABLE AS IS 6000 FH IAW REO 601R-53-61-5079.
PASSENGER DOOR AFT SEAL STRIKER HAS DEEP GOUGE. REPAIRED PAX DOOR AFT SEAL STRIKER IAW REO 601R-53-22-033,
WHEEL WELL BRAKE HYD LINE MOUNT BRACKET CRACKED. R & R HYD LINE BRACKET.
LEFT LOWER NOSE HYD BAY UPPER HYD ACCUMULATOR FWD ATTACH BRACKET CRACKED. R & R LT NOSE HYD COMP UPPER HYD ACCUMULATOR FWD ATTACH BRACKET IAW SRM.
FLOOR SEAT RAILS AT FS 349-409+112 ARE CORRODED. R & R UNSERVICEABLE SEAT RAIL SECTIONS AT FS 344-409+112 LBL & RBL WITH NEW SERVICEABLE SEAT RAILS IAW CRJ 200 AMM 53-01-11.
RETURN FILTER MOUNT HAS CRACK. REPAIR IAW REO 601R-53-62-031 REV A.
FLOOR SUPPORT INTERCOSTAL ATTACH CLIP AT FS 484 BL 57 CRACKED. REPLACED FLOOR SUPPORT INTERCOSTAL ATTACH CLIP AT FS 484 BL 57 IAW REO 601R-53-41-059.
CARGO DOOR SILL SUPPORT STRUCTURE CLIP IS CRACKED AT FS 605.0 FWD INBD ANGLE. R & R CRACKED CLIP.
FLOOR SUPPORT INTERCOSTAL ATTACH CLIP AT FS 484 BL 27 CRACKED. REPLACED FLOOR SUPPORT INTERCOSTAL ATTACH CLIP AT FS 484 BL 27 IAW REO 601R-53-41-059.
BRACKET CRACKED LT SIDE AFT FACE OF 621 PRESS BULKHEAD APPROXIMATELY 8 INCHES INBD OF STRINGER 14L. R & R.
BRACKET CRACKED RT SIDE AFT FACE OF FS 621 PRESS BULKHEAD APPROXIMATELY 8 INCHES INBD OF STRINGER 14R. R & R.
FLOOR SUPPORT INTERCOSTAL ATTACH CLIP AT FS 484 RBL 36 IS CRACKED. FABRICATED & INSTALLED NEW SERVICEABLE CLIP IAW REO 601R-53-41-059 REV B.
STRINGER 32 INBD & OTBD CLIPS CRACKED, AFT SIDE PILOTS 280 BULKHEAD TIE IN ANGLE WAS ALSO CRACKED. REMOVED UNSERVICEABLE INBD & OTBD CLIPS. REPLACED, FABRICATED SERVICEABLE CLIPS FOR INBD & OTBD & TIE IN ANGLE WAS R & R WITH SERVICEABLE FABRICATED ANGLE.
LBL & RBL 9 280 INBD CLIPS CRACKED. R & R LBL & RBL 9 280 INBD CLIPS.
DURING INCORPORATION OF THE MLG TRUNNION LOWER FLANGE, COLD WORKING FOUND TWO EACH OVERSIZED HOLES IN THE STRAP, PLANK & LOWER FLANGE. ONE ON THE LT SIDE & ONE ON THE RT SIDE. COMPLIED WITH REO 601R-57-21-2020 REV FOR COLD WORKING TWO EACH OVERSIZED FASTENER HOLES.
AFT LOWER SUPPORT CLIPS ON CARGO BAY DOOR RAIL SUPPORT BRACKET AT 621 BULKHEAD CRACKED. REMOVED CRACKED CLIP, THEN FABRICATED NEW SERVICEABLE CLIP AND INSTALLED IAW CRJ SRM 51-24-16.
DURING CLIMBOUT, VERY LOUD SQUEAL HEARD FROM PAX DOOR. R & R BROKEN ICE DOOR CABLE IAW AMM 52-11-15 PRESSURIZED ACFT, OPS CHECKED GOOD.
PAX DOOR AFT LATCH MECHANISM TORQUE TUBE PASS THROUGH FITTING UNDER PANEL 832AR IS CRACKED. REMOVED DOUBLER, LOCATED AND INSTALLED SERVICEABLE DOUBLER PN 601R318894-2 IAW SRM 51-40-11.
BRACKET IS CRACKED IN FUEL TANK. R & R BRACKET.
POST AT FS 409+128 LBL 27 APPEARS CRACKED AT LOWER INBD SIDE REPAIRED LBL POST AT FS 409+128 BY REMOVING DAMAGE AND INSTALLING FILLER AND REPAIR ANGLE IAW REO 601R-53-41-056, REV E.
POST AT FS 409+128, RBL 18 APPEARS CRACKED AT LOWER OTBD SIDE. REPAIRED RBL 18 POST AT FS 409+128 BY REMOVING DAMAGE AND INSTALLING FILLER AND REPAIR ANGLE IAW REO 601R-53-41-056, REV E.
RT SIDE SEAT TRACK NR 5 POSITION SHOWS SIGNS OF CORROSION. R & R RT SIDE SEAT TRACK IAW AMM 53-01-11-000-802, SRM 51-24-34, 51-40-11, 51-21-11.
PAX DOOR STAIR ATTACHMENT ANGLE (AFT) IS CRACKED (MOTOR SUPPORT AREA) DRAG ANGLE REMOVED PREVIOUSLY INSTALLED REPAIR ANGLE FABRICATED NEW ANGLE AND INSTALLED IAW REO 601R-52-11-513.
RT SIDE SEAT TRACK NR4 SHOWS SIGNS OF CORROSION. R & R NEW SERVICEABLE RT SIDE SEAT TRACK NR 4 IAW AMM 53-01-11-000-802, SRM 51-23-36, 51-21-11, AMM 53-01-11, PG 406.
LT SIDE SEAT TRACK NR 7 POSITION SHOWS SIGNS OF CORROSION. R & R NR 7 SIDE SEAT TRACK IAW AMM 53-01-11-000-802, SRM 51-24-34, 51-40-11, 51-21-11.
RT SIDE SEAT TRACK NR6 POSITION SHOWS SIGNS OF CORROSION. R & R NR6 SIDE SEAT TRACK IAW AMM 53-01-11-000-802, SRM 51-24-34, 51-21-11, & 51-40-11.
LT SIDE SEAT TRACK NR 6 POS SHOWS SIGNS OF CORROSION. R & R NR6 LT SIDE SEAT TRACK IAW AMM 53-01-11-000-802 & SRM 51-24-34 & 51-40-11 & 51-21-11.
LT SIDE SEAT TRACK NR 5 SHOWS SIGNS OF CORROSION. R & R NEW SERVICEABLE NR 5 LT SIDE SEAT TRACK IAW AMM 53-01-11-000-802, SRM 51-24-36, 51-40-11, 51-21-11, AMM 53-01-11, PG 406.
LT SIDE SEAT TRACK NR 4 POSITION SHOWS SIGNS OF CORROSION. R & R NR4 LT SIDE SEAT TRACK IAW AMM 53-01-11-000-802, SRM 51-24-34 & 51-40-11, 51-21-11.
LT SIDE SEAT TRACK NR3 POS SHOWS SIGNS OF CORROSION. R & R LT NR3 SEAT TRACK IAW AMM 53-01-11-000-802, SRM 51-24-34, 51-40-11, 51-21-11.
FLOOR SUPPORT UNDER FLOORBOARD 281LLF ARE CORRODED IN SEVERAL PLACES. FLOORBEAM FOUND TO BE CRACKED. REMOVED FLOORBEAM CAP FROM FS 621 TO 574 AT SPLICE, TRIMMED, DRILLED, AND INSTALLED NEW BEAM CAP.
LT UPPER CORE COWL INBD L/E DAMAGE. REPAIRED DAMAGE TO LT UPPER CORE COWL IAW CMM 71-12-01.
RT FLOOR SILL BETWEEN 559+80 TO 559+112 BLEND AS REQUIRED AND NDT FOR FURTHER DAMAGE.
PAX DOOR SUPPORT WHEEL PULLEY BRACKET ATTACHED TO LOWER STAIR IS CRACKED. R & R PAX DOOR SUPPORT WHEEL PULLEY BRACKET IAW SRM 51-42-06.
APU HEAT SHIELD CRACKED AT 7 O`CLOCK POSITION. REPAIRED IAW REO 601R-49-81-003.
DOOR CRACKED AT FWD SUPPORT. FABRICATED AND INSTALLED NEW SERVICEABLE FWD SUPPORT STRUCTURE.
RT ACCESS PANEL 699BB CHAFED. REPAIRED IAW REO 601R-57-60-020.
LT MLG DOOR CHAFED ON LOWER L/E. REPAIRED IAW REO 601R-52-82-034.
CORROSION ON RT FLOOR SILL IN AREA JUST AFT OF OVERWING EXIT REPAIRED IAW 601R-53-41-666.
CHAFE CAUSED BY BLOCKER DOOR ON RT LOWER CORE COWL BY FWD LATCHES. R & R CHAFED DOUBLER IAW CMM 71-12-01.
LT INBD FLAP CHAFED 3 PLACES. BLENDED CHAFED AREAS IAW SRM 51-12-00 AND REO 601R-57-52-004.
RT AILERON LWR L/E CHAFED IN 2 PLACES. BLENDED CHAFED AREAS IAW SRM 51-12-00 AND REO 601R-57-60-020.
RT SIDE OF FS 621 BLK FWD FACE HAS 3 CHAFE MARKS 2-.5 FT ABOVE FLOOR. BLEND OUT DAMAGE IAW REO 601R-53-61-2155.
THE LT LOWER FWD SIDE OF FS 621 BULKHEAD HAS 3 CHAFED SPOTS FROM FASTENERS APPROX 2" OFF FLOOR BLEND OUT DAMAGE IAW REO 601R-53-61-2155.
FS 280, RBL 10 FLOORBEAM CRACKED. REMOVED UNSERVICEABLE TEE AND REPLACED WITH SERVICEABLE TEE.
REAR PRESSURE BULKHEAD CENTER VERTICAL STIFFENER CHAFED FROM ISOLATOR VALVE (E-VAL) BLEND OUT CHAFING IAW REO 601R-53-61-1523 AND SRM 51-12-00.
BOTH REPAIRS TO PAX DOOR CUT OUT SEAL STRIKER ARE DAMAGED/BENT. REPAIRS WERE NOT FINISHED CORRECTLY. REMOVED/REPLACED 2 EA POPCYCLE REPAIRS ON PAX DOOR CUT OUT SEAL STRIKER IAW REO 601R-53-22-033.
FLOOR SUPPORT SYS AFT OF PAX DOOR CUT OUT HAS CORROSION ON RT SIDE. UPON FURTHER INVESTIGATION FOUND ONLY RIVET HEADS, 10 EA CORRODED. REMOVED AND INSTALLED 10 EA CORRODED RIVETS PN CR 3212-5-4. NO OTHER DEFECTS NOTED IAW SRM 51-42-10.