N8943A
Registered owner: GOLD COAST AVIATION, FL (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
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.
147 reports on file, 2004-11-05 – 2021-03-23.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 26,025 hrs · 26,134 cycles
EMEERGENCY LIGHTS DON'T COME ON WITH F/A PANEL OR F/D PANEL REPLACED BATTERY PACKS 1,2,3 AND 4 IAW CRJ200 AMM 33-51-04. OPS TEST GOOD
Earlier reports · 2004–2020 · 146 reports
2020
Part: VANE — DENTED (LT WING TE FLAP) · airframe 24,646 hrs · 24,545 cycles
LH INBD FLAP VANE CHAFED 1""L X .5""W JUST OTBD OF ACCESS PANEL 584ET. REMOVED AND REPALCED LH FLAP VANE INBD L/E ON INBD FLAP IAW CRJ 200 SRM 51-40-11, 51-42-10 AND 51-25-16.
Part: ANGLE — CORRODED (PAX DOOR) · airframe 24,646 hrs · 24,545 cycles
PAX DOOR FWD CLIP UNDER HINGE IS CORRODED LOCATED, DRILLED AND INSTALLED NEW PAX DOOR FWD LOWER CLIP P/N 601R319034-1 IAW CRJ 200 SRM 51-40-11 (TR# 51-42) AND 51-42-06/13/21 REV 37 JUL 10/18. WVAC EMP# 7006 COMPLETED 303.1, 303.6 AND 908.1 FORMS AS REQUIRED. E-MAILED CUSTOMER. WVAC EMP# 6500
Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 24,646 hrs · 24,545 cycles
PAX DOOR LOWER AFT INTERCOSTAL P/N 601R31902-317 HAS SIGNS OF CORROSION LOCATED, DRILLED AND INSTALLED NEW PAX DOOR LWR AFT INTERCOSTAL P/N 601R31902-317A IAW CRJ 200 SRM 51-40-11 (TR# 51-42) AND 51-42-06 REV 37 JUL 10/18. WVAC EMP# 7006 COMPLETED 303.1, 303.6 AND 908.1 FORMS AS REQUIRED. E-MAILED CUSTOMER. WVAC EMP# 6500
Part: ANGLE — CRACKED (BS 621-625) · airframe 24,646 hrs · 24,545 cycles
AFT EQUIPMENT BAY R/H SIDE FS 621-625 OBLIQUE ANGLE CRACKED REMOVED AND REPLACED CRACKED OBLIQUE ANGLE AT FS621-625 RH SIDE IAW CRJ 200 SRM 51-40-11 TR 51-42 AND 51-42-21 (PN#601-35012-52) WVAC EMP #575756
Part: SKIN — CORRODED (PAX DOOR) · airframe 24,646 hrs · 24,545 cycles
PAX DOOR INNER SKIN CORRODED IN MULTIPLE LOCATIONS REPLACED INNER SKIN PN#601R318024-15S IAW CRJ 200 SRM 51-40-11(TR51-42)51-42-061-131-211-22 REV 37 JULY 10/18 WVAC EMP #6500
Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 24,646 hrs · 24,545 cycles
PAX DOOR DD3 INTERCOSTAL CORRODED AT APPROX STGR12L AND BETWEEN FS319 AND FS347 COMPLETED 303.1, 303.6, AND 908.1 FORMS AS REQUIRED.
Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 24,646 hrs · 24,545 cycles
PAX DOOR DD6 INTERCOSTAL CORRODED AT APPROX STGR 15L AND BETWEEN FS319 & FS347.25 COMPLETED 303.1, 303.6, AND 908.1 FORMS AS REQUIRED.
Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 24,646 hrs · 24,545 cycles
PAX DOOR DD4 INTERCOSTAL CORRODED AT APPROX STGR 13L AND BETWEEN FS319.00 AND FS347.00 COMPLETED 303.1, 303.6, AND 908.1 FORMS AS REQUIRED.
Part: SKIN — CORRODED (LT WING) · airframe 24,646 hrs · 24,545 cycles
LH WING LOWER WING PLANK ACCESS HOLE CORRODED UNDER PANEL 540BB REPAIRED WING PLANK HOLE 540BB IAW REO 601R-57-21-030 REV L. WVAC STAMP EMP# 717 MTC
Part: BULKHEAD — DAMAGED (BS 621) · airframe 24,646 hrs · 24,545 cycles
AFT FUSE FS 621 BULKHEAD DAMAGED FROM SCREW SHANKS @ RBL 9, 18, 27, 36 AND LBL 18, 27 APPRX 28" ABOVE FLOOR REPAIRED FS 621 BULKHEAD AT RBL 9,18,27 AND LBL 18 AND 27 IAW REO 601R-53-61-2155 REV A. REPAIRED FS 621 BULKHEAD AT RBL 36 IAW REO 601R-53-61-1285 REV E. WVAC STAMP EMP# 717 MTC
Part: SKIN — CORRODED (RT WING) · airframe 24,646 hrs · 24,545 cycles
RH WING LOWER PLANK ACCESS HOLES CORRODED UNDER PANELS 640BB AND 640FB REPAIRED WING PLANK HOLES 640BB AND 640FB IAW REO 601R-57-21-030 REV L. WVAC STAMP EMP# 717 MTC
Part: FITTING — CRACKED (RT WING FLAP) · airframe 24,646 hrs · 24,545 cycles
R/H FLAP STUB FAIRING FWD FITTING IS CRACKED AND BENT REMOVED AND REPLACED RH FLAP STAB FAIRING FWD FITTING IAW CRJ 200 SRM 51-42-20 AND TR 51-42 WVAC EMP #750 MTC
Part: FLOOR SUPPORT — CORRODED (BS 451-499) · airframe 24,646 hrs · 24,545 cycles
MID CABIN FS 451-499 SIDE SILL CORRODED L/H/S REPIARED MID CABIN L/H SIDE SILL CORROSION @ FS 451-499 IAW BSC REO 601R-53-41-666 REV-C DATED 2012-11-06 WVAC EMP #722 MTC
Part: SEAT TRACK — CORRODED (BS 559-574) · airframe 24,646 hrs · 24,545 cycles
CARGO BAY SEAT RAILS CORRODED FS 559+89-559+96, 559+12-574, FS609-615, LBL9 (3EA) REMOVED (3 EACH) CORRODED SEAT RAIL IN CARGO BAY AND INSTALLED NEW SERVICEABLE RAIL AT FS 559+89-559+96, 559+112-574, AND FS 609-615 LB 9 IAW CRJ 200 AMM 53-01-11-000/400-802. WVAC EMP #575756
Part: SEAT TRACK — CORRODED (BS 559) · airframe 24,646 hrs · 24,545 cycles
CARGO BAY SEAT RAIL FS 559+80-559+96, RBL27 CORRODED INSTALLED NEW BAGGAGE RAIL + SEAT TRACK FITTIGN IAW CRJ 200 AMM 53-01-11-801 WVAC EMP #750 MTC.
Part: SEAT TRACK — CORRODED (BS 609-615) · airframe 24,646 hrs · 24,545 cycles
CARGO BAY SEAT RAILS CORRODED FS 559+89-559+96, 559+12-574, FS609-615, LBL9 (3EA) REMOVED (3 EACH) CORRODED SEAT RAIL IN CARGO BAY AND INSTALLED NEW SERVICEABLE RAIL AT FS 559+89-559+96, 559+112-574, AND FS 609-615 LB 9 IAW CRJ 200 AMM 53-01-11-000/400-802. WVAC EMP #575756
Part: SKIN — DENTED (LT WING TE FLAP) · airframe 24,646 hrs · 24,545 cycles
LEFT INBOARD FLAP LOWER SKIN HAS DENT WITH GOUGE LOCATED AT FLAP STATION 74.8 (24.4"" OTBD OF INBD END), 5.1"" FWD OF TRAILING EDGE. MEASURES APPROX. 1.0"" X 1.0"" X 0.040"" WITH GOUGE. REMOVED AND REPLACED DAMAGED I/B FLAP SKIN IAW CRJ 200 SRM 57-52-00 REPAIR 3.
Part: SEAT TRACK — CORRODED (BS 559) · airframe 24,646 hrs · 24,545 cycles
CARGO BAY SEAT RAILS CORRODED FS 559+89-559+96, 559+12-574, FS609-615, LBL9 (3EA) REMOVED (3 EACH) CORRODED SEAT RAIL IN CARGO BAY AND INSTALLED NEW SERVICEABLE RAIL AT FS 559+89-559+96, 559+112-574, AND FS 609-615 LB 9 IAW CRJ 200 AMM 53-01-11-000/400-802.
2019
Part: LIGHT — DAMAGED (CABIN) · airframe 24,359 hrs · 24,239 cycles
EMERGENCY TRACK LIGHT DAMAGED AT SEAT 4CD REPLACED EMERGENCY TRACK LIGHT STRIP AT 4DC IAW CRJ 200 AMM 33-51-01. P/N ON/OFF: 36262-4. OPS CHECK GOOD.
Part: FAIRING — CRACKED (HORIZONTAL STAB) · airframe 23,976 hrs · 23,837 cycles
RH HORIZONTAL STAB TIP CAP CRACKED ON UNDERSIDE & HAS LEADING EDGE EROSION ALL THE WAY THROUGH REMOVED AND REPLACED RH HORIZONTAL STAB FAIRING IAW CRJ 200 AMM 55-12-04 AND SRM 51-74-00.
Part: SELECTOR VALVE — MALFUNCTIONED (MLG) · airframe 23,842 hrs · 23,687 cycles
AFTER T/O RWY 21L WE GOT GEAR DISAGREE WARNING MESSAGE, ALONG WITH A/SKID INBD AND PARK BREAK SOC CAUTION MESSAGE MAIN LANDING DID NOT RETRACT WITHIN 6 SEC. FOLLOWED QRH CYCLE THE GEARS DOWN AND UP UNFORTUNATLEY NO FIX. HEAVY LANDING RWY 22L WITH RATE OF DECENT RATE OF LESS THAN 100'FT. REMOVED AND REPLACED LANDING GEAR CONTROL HANDLES IAW AMM 32-31-01. NO FIX. REMOVED AND REPLACED MLG SELECTOR VALVE IAW AMM 32-32-10. PERFORMED FUNCTIONAL TEST OF THE LANDING GEAR EXTENSION AND RETRACTION SYSTEM IAW AMM 32-0-00. OPS CHECK GOOD. SEE CONTINUATION CARDS 121153 AND 121154 FOR MORE DETAILS. P/N OFF/ON: 7-4502-5 S/N OFF:1586 S/N ON: 1711 P/N OFF/ON: 750005000 S/N OFF: 0141T S/N ON: 0602.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,840 hrs · 23,685 cycles
FLOOR EMERGENCY LIGHT STRIP FOUND INOP DURING PRE-FLIGHT. REMOVED AND REPLACED AFT FLEX LAMP TOWARDS THE LAV AREA IAW AMM 33-51-01, OPS CHECK GOOD, OK FOR SERVICE.
Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 23,402 hrs · 23,209 cycles
DURING WAKE UP CHECK NOTED RH FWD OVERWING EMERGENCY LIGHT INOP. REMOVED AND REPLACED RH FWD OVERWING EMERGENCY LIGHT LAMP P/N 1317. OPS CHECK OF EMERGENCY LIGHTS GOOD IAW CRJ 200 AMM 33-51-00.
Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 23,317 hrs · 23,118 cycles
RH FWD EXT EMERG LIGHT INOP RE-LAMPEDRH FWD EXT EMERG LIGHT PER AMM 33-51-21 OPS CHECK GOOD PER AMM 33-51-00
2018
Part: VALVE — MALFUNCTIONED (MLG) · airframe 22,433 hrs · 22,140 cycles
ON DEPARTURE GEAR RETRACTION GEAR DISAGREE WARNING MESSAGE WITH NOSE GEAR BOX RED RAN QRH PROCEDURE GEAR INDICATED DOWN WITH THREE GREEN NORMAL APPROACH AND LANDING REMOVED AND REPLACED RESTRICTOR VALVE PN OFF JETC1872240D PN ON FCLX0515700BB REF CRJ200 AMM 32-33-10 OPS AND LEAK CHECKS GOOD
Part: PROXIMITY SENSOR — OUT OF ADJUST (LANDING GEAR) · airframe 22,351 hrs · 22,038 cycles
CLIMBING THROUGH 200' AGL, AFTER SWITCHING GEAR HANDLE TO "UP" WE GOT "NOSE DOOR OPEN" & "GEAR DISAGREE WARNING MESSAGES W/ MAINS WHITE-HASHED ("UNKNOW POSITION") & NOSE RED-HASHED. ADJUSTED PROXIMITY SENSOR CLEARANCE OF PS1GA, PS2GA, IAW AMM 32-61-05, OPS CHECK GOOD IAW AMM 32-61-00.
Part: LIGHT — INOPERATIVE (CALL) · airframe 21,745 hrs · 21,356 cycles
CENTER CABIN FLIGHT DECK TO FLIGHT ATTENDANT CALL LIGHT INOPERATIVE.
Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 21,638 hrs · 21,238 cycles
EMERGENCY LIGHT, THE BULB BURNED OUT. REPLACED THE BULB. PERFORMED AN OPS TEST IAW AMM 31-52-00. OPS CHECKED GOOD.
Part: PDU — INOPERATIVE (THRUST REVERSER) · airframe 21,409 hrs · 20,969 cycles
RIGHT THRUST REVERSER UNLOCK CAUTION MESSAGE DURING FLIGHT. ACCOMPLISHED QRH, AND SHUT DOWN RIGHT ENGINE. AIRSPEED 270, ALTITUDE 1400 WHEN CAUTION ACCURED. EMERGENCY STOW BUTTON DID NOT STOW THE REVERSER. REMOVED AND REPLACED THE RIGHT THRUST REVERSER STOW SWITCH AND PDU IAW AMM 78-37-01-400-801, & 78-32-03-400-803. OPS CHECKED GOOD.
Part: SKIN — DAMAGED (LT WING) · airframe 21,402 hrs · 20,962 cycles
EXTERIOR SURFACE OF CTR WING HAS BARE METAL WITH MINOR FRETTING AT LBL 45 FROM CONTACT WITH WING AERODYNAMIC FAIRING 193AB. REPAIRED THE SKIN IAW SRM 57-21-31, 54-42-21, 51-24-11, REO 601R-57-21-2724, AND REO 601R-57-21-880. IAW AMM 28-11-00-790-802.
Part: FLOOR SUPPORT — CORRODED (BS 589-605) · airframe 21,402 hrs · 20,962 cycles
CORROSION ON THE FLOOR SUPPORT BETWEEN BS 589 AND 605, LBL 9. REMOVED AND REPLACED THE FLOOR SUPPORT IAW REO 601R-53-00-005, SRM 51-42-21, 53-61-43, 51-24-36, 51-40-11, AND 51-42-21.
Part: CHANNEL — CRACKED · airframe 21,402 hrs · 20,962 cycles
CHANNEL CRACKED. REMOVED AND REPLACED THE CHANNEL IAW SRM 51-42-06.
Part: ANGLE — CRACKED (BS 200) · airframe 21,402 hrs · 20,962 cycles
ATTACH ANGLE IN NLG WHEEL WELL AT BS 200, RBL 6 FOUND CRACKED. REPAIRED IAW CRJ-200 SRM 51-42-06.
Part: INTERCOSTAL — CRACKED · airframe 21,402 hrs · 20,962 cycles
NR 2 HYD PRESSURE AND RETURN MANIFOLD SUPPORT INTEROSTAL CRACKED AT AFT LWR CORNER. REPAIRED THE INTERCOSTAL IAW SRM 53-00-00.
Part: ANGLE — CRACKED (BS 280) · airframe 21,402 hrs · 20,962 cycles
INBD ANGLE IS CRACKED ON STRINGER 3L JUST AFT OF BS 280, IN THE CABIN. REMOVED AND REPLACED THE ANGLE IAW SRM 51-42-06, 51-40-11, 51-24-36.
Part: BRACKET — CRACKED · airframe 21,402 hrs · 20,962 cycles
NR 1 HYD PRESSURE AND RETURN MANIFOLD INTERCOSTAL FWD STIFFNER BRACKET CRACKED, ADJACENT TO RETURN MANIFOLD. REMOVED & REPLACED THE BRACKET IAW SRM 51-42-06.
Part: DRAG ANGLE — CRACKED (LT WING) · airframe 21,402 hrs · 20,962 cycles
LEFT WING INBD DRAG ANGLE CRACKED. REMOVED & REPLACED THE DRAG ANGLE IAW SRM 51-42-21.
Part: DRAG ANGLE — CRACKED (RT WING) · airframe 21,402 hrs · 20,962 cycles
RIGHT WING INBD DRAG ANGLE CRACKED. REMOVED AND REPLACED THE DRAG ANGLE IAW SRM 51-42-21.
Part: BRACKET — CRACKED · airframe 21,402 hrs · 20,962 cycles
PRESSURE FUELING BRACKET IS CRACKED. REMOVED AND REPLACED BRACKET IAW SRM 51-42-06.
2017
Part: OXYGEN MASK — BROKEN (CAPTAIN'S) · airframe 21,283 hrs · 20,846 cycles
CA SIDE OXYGEN MASK TAB BROKEN SWAPPED CA SIDE OXY MASK BOX WITH OBSERVERS MASK BOT PER AMM 35-11-15. DEFFERED OBSERVERS SEAT AND MASK PER MEL 35-10-1 MOC NOTIFIED #98765 PLACARD INSTALED & MEI 25-12-A1/// REMOVED AND REPLACED OBSERVER O2 MASK IAW CRJ200 AMM 35-11-12. OPS & LEAK CHECK GOOD. MM02 UPDATED. PLACARD REMOVED. MOC #53430 NOTIFIED. THIS CLEARS THE OBSERVER SEAT MEL 25-12-1A.
Part: LIGHT — DAMAGED (FWD CABIN) · airframe 21,219 hrs · 20,775 cycles
FWD FLOOR EMERGENCY LIGHT DAMAGED. R & R THE EMERGENCY LIGHT IAW AMM 33-51-01. OPS CHECKED GOOD. OK FOR SERVICE.
Part: ENGINE — POWER LOSS (LEFT) · airframe 21,132 hrs · 20,678 cycles
DURING CLIMB OUT, N1 FOR THE LT ENGINE KEPT GOING DOWN ABOUT 10% AND LEFT ENGINE NOISE WAS GOING DOWN AS WELL & PLANE WAS YAWING TO THE LEFT HAPPENED MULTIPLE TIMES, NO OTHER ABNORMAL INDICATION ON ITT OR N2. DIVERTED. PERFORMED ENGINE RUNS IAW AMM 76-00-00, WITH BOTH SPEED SWITCHES ON AND OFF COULD NOT DUPLICATE. PERFORMED OPS CHECK OF APR IAW AMM 76-13-00, OPS CHECKED PASSED.
Part: SMOKE WARNING — FALSE ACTIVATION (LAVATORY) · airframe 20,027 hrs · 19,501 cycles
SMOKE TOILET CAUTION MESSAGE ON FINAL APPROACH. F/A CHECKED THE LAVATORY. NO DEFECTS NOTED. PERFORMED OPS CHECK OF THE LAVATORY SMOKE DETECTION SYSTEM IAW AMM 26-16-01. OPS CHECKED GOOD.
Part: BATTERY PACK — DISCHARGED (FLASHLIGHT) · airframe 20,007 hrs · 19,481 cycles
CAPTAIN`S & FIRST OFFICER'S FLASHLIGHT BATTERIES ARE DEAD. REPLACED THE BATTERY PACKS IAW AMM 25-61-00, OP CHECKED GOOD.
Part: OXYGEN MASK — UNSERVICEABLE (PORTABLE O2) · airframe 19,976 hrs · 19,448 cycles
PORTABLE O2 BOTTLE S/N ST 60291 HAS UNSERVICEABLE 4 LPM MASK. REMOVED & REPLACED O2 BOTTLE MASK IAW AMM 35-31-01.
Part: LIGHT — UNSECURE (CABIN) · airframe 19,965 hrs · 19,436 cycles
EMER EXIT LIGHT STRIP DAMAGED. RESECURED EXIT LIGHT STRIP (EMER) IAW AMM 33-51-00. OK FOR SVC.
Part: OXYGEN MASK — LEAKING (COCKPIT) · airframe 19,888 hrs · 19,351 cycles
OBSERVERS OXYGEN MASK LEAKING WHEN TESTED. R & R OBSERVERS OXYGEN MASK IAW AMM 35-11-12. OPS AND LEAK CHECKED GOOD.
Part: OXYGEN MASK — INOPERATIVE (COCKPIT) · airframe 19,736 hrs · 19,203 cycles
OBSERVER'S O2 MASK INOP. DEFERRED OBSERVER'S O2 MASK IAW MEL 35-10-01 CAT 'A'. REMOVED AND REPLACED OBSERVER 02 MASK IAW AMM 35-11-12. OPS CHECK GOOD.
2016
Part: LIGHT — INOPERATIVE (SEAT 10) · airframe 19,546 hrs · 19,014 cycles
EMERGENCY LIGHT AT SEAT 10 INOPERATIVE. REMOVED AND REPLACED THE LIGHT STRIP IAW AMM 33-51-01-04.
Part: PROXIMITY SENSOR — MALFUNCTIONED (NLG) · airframe 18,911 hrs · 18,361 cycles
DURING DEPARTURE, GEAR RETRACTION, NOSE DOOR OPEN & GEAR DISAGREE WARNINGS ANNUNCIATED, NOSE WHEEL STAYS IN DOWN & LOCKED POSITION. R & R NLG CENTERING PROXIMITY SENSOR BRACKET SUB ASSY IAW AMM 32-21-01. PERFORMED FUNCTIONAL TEST OF THE LANDING GEAR EXTENSION/RETRACTION SYSTEM IAW AMM 32-30-00. ALL CHECKED GOOD.
Part: WIRE HARNESS — DAMAGED (NLG) · airframe 18,678 hrs · 18,121 cycles
NOSE DOOR OPEN & GEAR DISAGREE MASTER CAUTION MSGS AT GEAR RETRACTION. FOUND NOSE GEAR CENTERED PROX SWITCH HARNESS DAMAGED DUE TO TOW COLLAR SLIP. R & R NLG WOW 2 & OLEO CENTERED HARNESS & PROX SWITCH BRACKET IAW AMM-32-61-25 & CMM 32-21-00. OPERATIONS & FUNCTIONAL CHECKED GOOD. SEE NRWC 537102 FOR WORK DETAILS.
Part: PROXIMITY SENSOR — OUT OF POSITION (NLG) · airframe 18,354 hrs · 17,799 cycles
ON SELECTING GEAR UP ON CLIMB OUT, DEPARTURE MASTER WARNING GEAR DISAGREE WITH MASTER WARNING NOSE DOOR OPEN. NOSE WHEEL INDICATION WAS DOWN & GREEN WITH MAINS BOTH UP & WHITE & NOSE GEAR HANDLE SELECTED UP. MOTR BUY BACK FAIL REQUIRES BLG SERVICE IAW AMM TASK 12-12-32-610-803 & OLEO CENTERED & EXTENDED PROX SENSOR PX14GA BRACKET REPLACEMENT. FOUND TOW GUARD COLLAR MOVED UP PUSHING ON THE OLEO CENTERED EXTENDED PROX SENSOR ON THE NOSE LANDING GEAR. TORQUE LINK PROX SENSOR. PS14GA REMOVED OLEO CENTERED EXTENDED PROX SENSOR WITH BRACKET & INSPECTED, NO DEFECT NOTED. REINSTALLED BRACKET & RIGGED SENSOR IAW AMM 32-61-05. PERFORMED GEAR RETRACTION & EXT CHECK IAW AMM 32-61-05. OPERATIONS CHECKED GOOD IAW NRWC 536464. SERVICED NOSE STRUT WITH OIL & NITROGEN ON GND IAW AMM 12-12-32. INSTALLED OLEO CENTERED & EXTENDED PROX SENSOR BRACKET, PN 16215-105 OFF & ON IAW SUBTASK 32-52-01-410-001. OPERATIONS CHECK OF LANDING GEAR EXTENSION & RETRACTION, OPERATIONS CHECKED GOOD IAW AMM 32-30-00.
Part: STRUCTURE — DAMAGED (LT WING) · airframe 18,101 hrs · 17,544 cycles
LEFT FUEL ACCESS HOLE 550DB, HAS AN INDICATION ON OTBD SIDE, APPROX .25 W X 9.0 L 50% FSH, FAILED NDT. REPAIRED 550DB CUT OUT IAW REO 601R-57-21-030 REV L DATED 2 5 2014. REFER TO ATTACHED REO FOR WORK PERFORMED. THIS IS A MAJOR REPAIR.
Part: CONNECTOR — DEFECTIVE (CABIN) · airframe 18,101 hrs · 17,544 cycles
FORWARD SECTION OF EMER LIGHT TRACK INOPERATIVE. REPLACED TWO CONNECTORS FOR EMER LIGHT & TRACK IAW ESPM 20-17-31. OPERATIONS CHECKED GOOD.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,101 hrs · 17,544 cycles
THE NR 7 EMER FLOOR TRACK LIGHT IS INOPERATIVE. R & R FLOOR TRACK 7 & 9 IAW AMM 33-51-01-400-801. OPERATION CHECKED GOOD.
Part: WIRE — DAMAGED (CABIN) · airframe 18,101 hrs · 17,544 cycles
ENTRANCE STORAGE COMPARTMENT OTBD SIDE HAS A DAMAGED WIRE, MARKED WITH RED TAPE. WIRE LY32B22 CONTACT REPLACED, PN M39029 31-229, & CONNECTOR PN 48-7190 ON WIRE LY32B22 IAW ESPM 20-17-10. OPERATIONS CHECKED GOOD.
Part: ANGLE — CORRODED (FUSELAGE) · airframe 18,101 hrs · 17,544 cycles
PASSENGER DOOR FLOOR SILL ANGLE IS CORRODED, BETWEEN FS 310 - 349. CONTINUATION CARD 8794311 OP 146. R & R PAX DOOR FLOOR SILL ANGLE IAW SRM 51-40-11, 51-42-06, 51-42-13 & 51-42-20.
Part: BULKHEAD — DAMAGED (FUSELAGE) · airframe 18,101 hrs · 17,544 cycles
FOUND RT FS 559 BULKHEAD WEB HAS INDICATION NOTED INBD OF RBL 18.0, WL 59.10, APPROX .300 IN LENGTH 50% FSH, FAILED NDT INSPECTION. COMPLIED WITH REPAIR OF FS 559 BULKHEAD WEB IAW EO P53025.
Part: TAB — BROKEN (APU EXHAUST) · airframe 18,101 hrs · 17,544 cycles
PART 9 53-61-101, APU EXHAUST NOZZLE ASSEMBLY ALIGNMENT TAB BROKEN. WELDED REPLACEMENT TAB ON APU NOZZLE & NDT'D IAW CMM 49-81-00 REV 7 STEP BB.
Part: LENS — CRACKED (WING) · airframe 18,101 hrs · 17,544 cycles
LIGHT LENS ON PANEL 571JT IS CRACKED AT FASTENER HOLE. R & R 571JT LIGHT LENS IAW AMM 57-30-39-400-801.
Part: SKIN — CHAFED (TE FLAP VANE) · airframe 18,101 hrs · 17,544 cycles
RIGHT INBD FLAP VANE, LE SKIN HAS CHAFE DAMAGE IN 3 PLACES. DAMAGE AT INBD END MEASURES APPROX 1.1"" LONG X 0.5"" WIDE X 0.015"" DEEP. DAMAGE AT MID-SPAN MEASURES APPROX 1.1"" LONG X 0.45"" WIDE X 0.025"" DEEP. DAMAGE AT OTBD END MEASURES APPROX 1.1"" LONG X 0.4"" WIDE X 0.010"" DEEP. CONTINUATION CARD 8794311 OP 165. REPAIRED RT INBD FLAP VANE INBD & OTBD LOCATIONS IAW REO 601R-57-52-004. R & R MIDDLE SKIN IAW SRMS 51-42-10 & 51-42-13. SEE JOB CARD 8794311 OP 35 FOR STEPS 1 - 6.
Part: MOUNT — CRACKED (FUSELAGE) · airframe 18,101 hrs · 17,544 cycles
WHILE PERFORMING APU DOOR HEALTH CHECK, FOUND APU ACTUATOR MOUNTING STRUCTURE CRACKED. APU INTAKE ACTUATOR MOUNTING STRUCTURE REPAIRED IAW EA CRJ253-03927.
Part: SCUFF PLATE — CRACKED (FUSELAGE) · airframe 18,101 hrs · 17,544 cycles
CARGO DOOR SCUFF PLATE IS DEFORMED & CRACKED. NEEDS REPLACED. LOCATED HOLES IN NEW SCUFF PLATE, PN 601R35004-337, IAW SRM 51-40-11. REFERENCE JOB 8794310 OP 510 FOR REMOVAL & INSTALLATION.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 18,101 hrs · 17,544 cycles
FLOOR SEAT TRACK AT LBL 9 IS CORRODED AT MULTIPLE LOCATIONS, BETWEEN FS 409 TO 409+128. REMOVED, FABRICATED & INSTALLED FLOOR SEAT TRACK IAW REO 601R-53-00-485 REV.
Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 18,101 hrs · 17,544 cycles
SERVICE DOOR FLOOR SILL IS CORRODED, BETWEEN FS 319 - 349. CONTINUATION CARD 167. R & R SERVICE DOOR LOWER SILL ANGLE IAW SRM 51-42-21, 51-42-06, 51-42-10, 51-42-21 & 51-42-36. SEE JC 8794311 OP 129 FOR STEPS 1 - 5.
Part: BRACKET — CRACKED (PAX DOOR) · airframe 18,101 hrs · 17,544 cycles
PASSENGER DOOR ASSIST MOTOR, LOWER BRACKET IN THE OPEN POSITION IS CRACKED. R & R CRACKED PAX DOOR MOTOR BRACKET 601R317745-7 IAW SRM 51-42-06 & 51-77-00.
Part: ANGLE — CORRODED (FUSELAGE) · airframe 18,101 hrs · 17,544 cycles
CLIP ATTACHING TO SERVICE DOOR FLOOR SILL ANGLE AT FS 319 IS CORRODED. R & R CLIP ATTACHING FLOOR SILL ANGLE AT FS 319 IAW SRM 51-42-06, 51-42-12 & 51-42-2.
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 18,101 hrs · 17,544 cycles
INTERCOSTAL AT FS 621 BULKHEAD, STRINGER 13L IS CRACKED. REMOVED & INSTALLED SERVICEABLE INTERCOSTAL IAW SRM 51-42-06. "
Part: ANGLE — CRACKED (FUSELAGE) · airframe 18,101 hrs · 17,544 cycles
OBLIQUE INTERCOSTAL ANGLE IS CRACKED AT FS 621 BULKHEAD STRINGER 14L. R & R OBLIQUE INTERCOSTAL ANGLE IAW SRM 51-42-06, 51-42-21 & 51-77-00.
Part: FITTING — CORRODED (FUSELAGE) · airframe 18,101 hrs · 17,544 cycles
FITTING ON FRAME AT FS 319 AT RBL 45, APPROX WL 74, IS CORRODED. R & R FITTING ON FRAME AT FS 319 AT RBL 45, APPROX WL 74, PN 601R38335-1S, IAW SRM 51-42-21.
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 18,101 hrs · 17,544 cycles
INTERCOSTAL AT FS 621 BULKHEAD STRINGER 14L IS CRACKED. R & R INTERCOSTAL IAW SRM 51-42-21, 51-42-22 & 51-77-00.
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 18,101 hrs · 17,544 cycles
RIGHT SIDE, FS 621.00 - 625.30, INTERCOSTAL AT STRINGER 14R IS CRACKED IN RADIUS, APPROX 1.0"" LONG. REMOVED DAMAGED INTERCOSTAL & REPLACED WITH NEW SERVICEABLE INTERCOSTAL, PN 601-35012-52, IAW SRM 51-42-21.
Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 18,101 hrs · 17,544 cycles
PASSENGER DOOR AFT DRAG ANGLE CRACKED. PAX DOOR AFT DRAG ANGLE REPAIRED IN ITS ENTIRETY. WORK PERFORMED IAW REO 601R-52-11-513 REV B DATED 07 05 15.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 18,101 hrs · 17,544 cycles
FLOOR SEAT TRACK AT RBL 9 HAS PITTING CORROSION AT MULTIPLE LOCATIONS, BETWEEN FS 409 - 409+128. R & R SEAT TRACK WITH A NEW FABRICATED SEAT TRACK IAW REO 601R-53-00-485 & SRM 51-41-04.
Part: HEAT SHIELD — CRACKED (APU EXHAUST) · airframe 18,101 hrs · 17,544 cycles
APU EXHAUST HEAT SHIELD IS CRACKED IN 2 LOCATIONS. REPAIRED APU EXHAUST HEAT SHIELD IAW REO 601R-49-81-003.
Part: BRACKET — CRACKED (RT MLG WW) · airframe 18,101 hrs · 17,544 cycles
RIGHT MLG WW HYD PRESS TRANSDUCER BRACKETS ARE CRACKED, TWO & HAT CHANNEL. R & R MLG BRAKE PRESS TRANSDUCER HAT BRACKET, PN 601R75262-157, IAW SRM 51-42-06. R & R MLG BRAKE PRESS TRANSDUCER LINE Z BRACKET, PN 601R75262-153 IAW SRM 51-42-06.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 18,101 hrs · 17,544 cycles
FLOOR SEAT TRACK AT RBL 9 IS CORRODED, BETWEEN FS 409+128 - FS 559. R & R SEAT TRACK WITH A NEW FABRICATED SEAT TRACK IAW REO 601R-53-00-485 & SRM 51-41-04.
Part: FITTING — BROKEN (TE FLAP) · airframe 18,101 hrs · 17,544 cycles
LEFT WING TE AT WS 48.30, THE FITTING FOR THE FLAP STUB FAIRING IS BROKEN OFF. R & R FLAP FITTING, PN 601R10371-1 IAW SRM 51-42-21.
Part: MOUNT BRACKET — CHAFED (TE FLAP) · airframe 18,101 hrs · 17,544 cycles
LEFT & RIGHT FLAP STUB FAIRINGS, FWD INSIDE MOUNTS ARE CHAFED. R & R WITH NEW SERVICEABLE MOUNTING BRACKETS IAW SRM 51-42-06, PN 601R31199-5 7 601R31199-6.
Part: ACCESS PANEL — CHAFED (RT WING) · airframe 18,101 hrs · 17,544 cycles
RIGHT WING PANEL 699BB IS CHAFED, APPROX 5"" L X 1"" W X 0.030"" DEEP. LOCATED, DRILLED & PAINTED NEW ACCESS PANEL IAW SRM 51-40-11 & 51-25-01. REFER MASTER PANEL BOOK FOR REMOVAL OF UNSERVICEABLE PANEL & INSTALLATION OF NEW PANEL.
2015
Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 17,955 hrs · 17,401 cycles
FLIGHT ATTENDANT FLASH LIGHT UNDER JUMP SEAT NOT FLASHING RED LIGHT. R & R FWD UNDER FLIGHT ATTENDANTS SEAT EMER LIGHT ASSEMBLY IAW AMM 25-61-02. OPERATIONS CHECKED GOOD, OK FOR SERVICE.
Part: OXYGEN MASK — LEAKING (COCKPIT) · airframe 17,840 hrs · 17,279 cycles
FIRST OFFICERS OXYGEN MASK, HARNESS LEAK TOP LT TUBE. SWAPPED FIRST OFFICERS & OBSERVERS OXYGEN MASK IAW AMM 35-11-12. OPERATIONS CHECKED GOOD. DEFERRED OBSERVERS 02 MASK IAW MEL 35-10-01. PLACARD INSTALLED, PROCEDURE COMPLIED WITH & ENTERED INTO PMR IAW MOC 96074. RETURNED OBSERVERS & FIRST OFFICERS O2 MASK TO POSITION. R & R FIRST OFFICERS O2 MASK IAW AMM 35-11-12. OPERATIONS CHECK & LEAK CHECKED GOOD AT THIS TIME. THIS CLEARS DM 002607 & PLACARD REMOVED.
2014
Part: LIGHT — DEFECTIVE (CABIN) · airframe 17,124 hrs · 16,522 cycles
EMERGENCY EXIT FLOOR LIGHT STRIP AT SEAT 7C IS DIM & FLICKERS INTERMITTENTLY. R & R EMER LIGHT STRIP IAW AMM 33-51-01. OPERATIONS CHECKED GOOD.
Part: INVERTER — INOPERATIVE (CABIN) · airframe 17,005 hrs · 16,403 cycles
EMERGENCY FLOOR STRIP INOPERATIVE FROM SEAT 2C TO 5C & SEAT 1C MISSING ORANGE OVERLAY. R & R EMER BATTERY NR 2 INVERTER & INSTALLED ORANGE OVERLAY IAW AMM 33-51-01. OPERATIONS CHECKED GOOD.
Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 16,761 hrs · 16,154 cycles
IAW MEL 33-51-14 EMER LIGHT STRIP INOPERATIVE SEATS. RECYCLE CB C2 FROM PANEL NR ON EMER FLOOR LIGHTS IAW AMM 33-51-01. OPERATIONS CHECKED PANEL. REMOVED PLACARD, REMOVED FROM MMO2.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,653 hrs · 16,041 cycles
EMERGENCY EXIT FLOOR LEVEL LIGHTS ARE INOPERATIVE FROM SEATS 2C TO 5C. DEFERRED EMER LIGHTS UNDER MEL 33-51-17.
2013
Part: SKIN — DENTED (RT WING TE FLAP) · airframe 15,886 hrs · 15,261 cycles
RT INBD UPPER FLAP SKIN AT FLS71 DENTED. REPAIRED IAW SRM 57-52-00.
Part: SKIN — DENTED (LT WING TE FLAP) · airframe 15,886 hrs · 15,261 cycles
LEFT INBD UPPER FLAP SKIN AT FLS82.9 DENTED. REPAIRED IAW SRM 57-52-00.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 15,807 hrs · 15,205 cycles
EMERGENCY EXTERIOR LIGHTS INOPERATIVE. REPLACED NR 1 - 4 EMERGENCY LIGHT BATTERY PACK IAW AMM 33-51-04. OPERATIONS TESTED GOOD. THIS CLEARS DM 020159.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 15,807 hrs · 15,205 cycles
EMERGENCY CABIN LIGHTS INOPERATIVE. REPLACED NR 1 - 4 EMERGENCY BATTERY PACK IAW AMM 33-51-04. OPERATIONS TESTED GOOD. THIS CLEARS DM 020158.
Part: LIGHT — UNSECURE (CABIN) · airframe 15,587 hrs · 14,998 cycles
EMERGENCY FLOOR LIGHTING FRONT F/O SIDE COMING LOOSE. RESECURED FLOOR TRACK COVER IAW AMM 33-51-01. REPLACED LIGHT STRIP IAW AMM 33-51-01.
Part: CONTAINER — TORN (LIFE VEST) · airframe 15,358 hrs · 14,752 cycles
INFANT LIFE VEST BAG TORN. R & R INFANT LIFE VEST IAW PA25-096A.
Part: CONTAINER — TORN (LIFE VEST) · airframe 15,286 hrs · 14,677 cycles
CAPTAIN LIFE VEST BAG TORN. R & R VEST IAW AMM 25-61-03.
Part: MEDICAL KIT — UNSERVICEABLE (CABIN) · airframe 14,638 hrs · 14,059 cycles
WITNESS SEAL MISSING ON FIRST AID KIT. REMOVED AND REPLACED FIRST AID KIT IAW AMM 25-61-06.
Part: UNKNOWN — SMOKE (CABIN) · airframe 14,598 hrs · 14,013 cycles
FLT 4094 / DTW / TVC- CREW REPORTED VISUALLY AND SMELL SMOKE IN THE CABIN. THEY PULLED INTO THE GATE AND ONLY THE APU WAS RUNNING WITH PACKS ON AT THE TIME WHEN THE SMOKE WAS REPORTED. CREW SHUT THE APU DOWN, DEPLANED, AND CALLED FIRE DEPARTMENT. CONTACTING MAINTENANCE AT THIS TIME. EMERGENCY DECLARED AND EVERYONE IS OK. MAINTENANCE IS EN ROUTE TO COMPLY WITH SMOKE IN THE CABIN WORKSCOPE
Part: IDG — MALFUNCTIONED (NR 2) · airframe 14,468 hrs · 13,890 cycles
NR 1 IDG CAUTION MESSAGE DURING FLIGHT, PILOT ACARS IN THAT NR 2 IDG MESSAGE WAS ILLUMINATED IN FLIGHT FLICKERING AND INTERMITTENTLY. GENERATOR STAYED ONLINE. ALSO TO NOTE NR 1 IDG WAS PREVIOUSLY DEFERRED. PILOT DECLARED EMERGENCY AND LANDED AT SCHEDULED AIRPORT. NR 2 IDG OUTPUT WAS 8KVA, 112V, 402HZ. SWAPPED NR 1 GCU INTO NR 2 POSITION. NR 2 IDG OUTPUT- 7 KVA, 116V, 401HZ. OPS CHECKED NR 2 IDG FOR 45 MINS. CONTINUOUSLY IAW AMM 24-11-01. NO DEFECTS NOTED. OK FOR SERVICE.
Part: OIL SYSTEM — LOW (APU) · airframe 14,134 hrs · 13,566 cycles
ON FLIGHT 4285 (MSP TO YYZ) CREW REPORTED DURING LANDING THEY STARTED THE APU AND COULD SMELL FUEL FOR 5 SECONDS. DEFERRED PER MEL 49-10-11. FOUND APU OIL LOW, SERVICE OIL IAW AMM 12-13-49. BEGAN APU AND NO SMELL OF FUEL WAS DETECTED. CLEARED DEFERRAL 002209.
2012
Part: HINGE — CRACKED (PAX DOOR) · airframe 13,982 hrs · 13,411 cycles
IN HEAVY CHECK DURING ACCESS TO CHANGE PAX DOOR SEAL FOUND LOWER TOP FOLDING STEP HINGE CRACKED. REMOVED AND REPLACED PAX DOOR LOWER TOP FOLDING STEP HINGE IAW CRJ -200 SRM 51-42-06.
Part: RISER — CRACKED (PAX DOOR) · airframe 13,982 hrs · 13,411 cycles
IN HEAVY CHECK FOUND PAX DOOR AFT STAIR RISER CRACKED BY THE 4TH STEP FROM BOTTOM. A251-002 REPAIRED PAX DOOR AFT STAIR RISER IAW REO 601R-52-11-702.
Part: BATTERY PACK — DISCHARGED (FLASHLIGHT) · airframe 13,840 hrs · 13,270 cycles
CAPTAIN'S FLASHLIGHT RED LIGHT DOES NOT BLINK. REMOVED AND REPLACED CAPTAIN'S FLASHLIGHT BATTERY PACK IAW AMM 25-61-00. OPS CHECK GOOD. CLEARS DM 75038.
Part: BULKHEAD — CRACKED (AFT) · airframe 12,949 hrs · 12,382 cycles
REAR PRESSURE BULKHEAD IS CRACKED AT LINTEL FITTING IN 2 PLACES. REPAIRED REAR PRESSURE BULKHEAD IAW EO C53134.
Part: CROSSBEAM — CRACKED (BS 280) · airframe 12,949 hrs · 12,382 cycles
FS 280.00 CROSSBEAM CRACKED IN 3 LOCATIONS AT FLOOR POST ATTACHMENT AT LBL12.0 AND CRACKED 4 LOCATIONS AT FLOOR POST ATTACHMENT AT RBL12.0. REMOVED DAMAGE FROM LEFT AND RIGHT LOWER FLANGE OF FS 280 FLOOR ANGLE LBL12 AND RBL12. INSTALLED REPAIR DOUBLER, REPLACED LT INBOARD AND OUTBOARD CLIPS AT LBL9, REPLACED RT INBOARD AND OUTBOARD CLIPS AT RBL9 IAW REO-53-11-171. REMOVED DAMAGED SECTION OF UPPER ANGLE FS280 FROM LBL14.25 THRU RBL13.5, SPLICED IN REPAIR SECTION IAW REO-53-11-136 AND EO NRC53135. 600-34017-595 TAG B26888 AAR AM-68.
Part: BRACKET — CRACKED · airframe 12,949 hrs · 12,382 cycles
RT THRUST REVERSER STOW AND THROTTLE LOCKOUT SWITCH BRACKET ASSY ELECTRICAL CONNECTOR ATTACHMENT CLIP CRACKED. REMOVED AND REPLACED RT THRUST REVERSER STOW AND THROTTLE LOCKOUT SWTICH BRACKET ASSY ELECTRICAL CONNECTOR ATTACHMENT CLIP IAW SRM 51-42-06.
Part: MOUNT — BROKEN (BRAKE SYS) · airframe 12,949 hrs · 12,382 cycles
LEFT MLG BRAKE APPLICATION PRESSURE TRANSDUCER MOUNTING PLATE BROKEN. REMOVED AND REPLACED LT MLG BRAKE APPLICATION PRESSURE TRANSDUCER MOUNTING PLATE IAW SRM 51-42-06 AAR SM-57.
Part: MOUNT — BROKEN (BRAKE SYS) · airframe 12,949 hrs · 12,382 cycles
RIGHT MLG BRAKE APPLICATION PRESSURE TRANSDUCER MOUNTING PLATE BROKEN. REMOVED AND REPLACED RT MLG APPLICATION PRESSURE TRANSDUCER MOUNTING PLATE IAW CRJ-200 SRM 51-42-00.
Part: SEAT TRACK — CORRODED · airframe 12,949 hrs · 12,382 cycles
LEFT SIDE SEAT TRACK NR 4 WORN AND CORRODED. REMOVED AND REPLACED LT SIDE TRACK NR 4 IAW AMM 53-01-11.
Part: HINGE — CRACKED (PAX DOOR) · airframe 12,949 hrs · 12,382 cycles
PAX DOOR HINGE SECTOR IS WORN (A/C SIDE). REMOVED AND REPLACED PAX DOOR HINGE HALF, A/C SIDE IAW SRM 53-21-23.
Part: HINGE — WORN (PAX DOOR) · airframe 12,949 hrs · 12,382 cycles
PAX DOOR HINGE SECTOR IS WORN (PAX DOOR SIDE). REMOVED AND REPLACED PAX DOOR HINGE HALF, DOORSIDE IAW SRM 52-10-31.
Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 12,949 hrs · 12,382 cycles
PAX DOOR AFT DRAG ANGLE CRACKED. REMOVED AND REPLACED PAX DOOR AFT DRAG ANGLE IAW REO 601R-52-11-513 PN 601R31772-55 TAG B03397.
Part: VANE — CHAFED (LT WING TE FLAP) · airframe 12,949 hrs · 12,382 cycles
LT INBD FLAP VANE LEADING EDGE SKIN IS CHAFED AT APPROX WS 56.30. REMOVED AND REPLACED INBOARD FLAP VANE INBOARD LEADING EDGE IAW SRM 51-42-13.
Part: ACCESS PANEL — CHAFED (RT WING) · airframe 12,949 hrs · 12,382 cycles
RIGHT WING LOWER PLANK ACCESS PANEL 640BB LAND CHAFED. BLENDED CHAFE ON FUEL PANEL LAND 640BB AND IS WITHIN LIMITS IAW REO 601R-57-21-030 AND IAW EO#C57072 RECEIVED ON 5/24/2012 AAR SM-74.
Part: STOP FITTING — CHAFED (E/E BAY DOORWAY) · airframe 12,949 hrs · 12,382 cycles
FWD E & E BAY DOOR OPENING FWD RT DOOR STOP FITTING IS CHAFED. REMOVED AND REPLACED WITH NEW END FWD RT DOOR STOP FITTING IAW CRJ 200 SRM 51-41-02 AAR AM-82.
Part: ACCESS PANEL — CHAFED (LT WING) · airframe 12,949 hrs · 12,382 cycles
LEFT WING LOWER PLANK ACCESS PANEL 550HB LAND CHAFED. BLENDED LEFT WING LOWER PLANK ACCESS PANEL 550HB LAND AND IS WITHIN LIMITS IAW REO 601R-57-21-030.
Part: ACCESS PANEL — CHAFED (RT WING) · airframe 12,949 hrs · 12,382 cycles
RIGHT WING LOWER PLANK ACCESS PANEL 650EB LAND CHAFED. BLENDED CHAFED ON ACCESS PANEL 950EB LAND AND IS WITHIN LIMITS OF REO 601R-57-21-030. RECEIVED EP#C57072 ON 5/24/12 AAR SM-74.
Part: ACCESS PANEL — CHAFED (RT WING) · airframe 12,949 hrs · 12,382 cycles
RIGHT WING LOWER PLANK ACCESS PANEL 650HB LAND CHAFED ON UPPER AND LOWER SURFACE. BLENDED CHAFE ON UPPER AND LOWER FUEL PANEL LAND 650HB AND IS WITHIN LIMITS IAW REO 601R-57-21-030.
Part: ACCESS PANEL — CHAFED (LT WING) · airframe 12,949 hrs · 12,382 cycles
LEFT WING LOWER PLANK ACCESS PANEL 540BB LAND CHAFED. BLENDED CHAFE ON LT WING LOWER PLANK ACCESS PANEL 540BB LAND AND LS WITHIN LIMITS IAW REO 601R-57-21-030 AND IAW RECEIVED EO#C57072 5/24/12 AAR SM-74.
Part: VANE — CHAFED (RT WING TE FLAP) · airframe 12,949 hrs · 12,382 cycles
RT WING INBOARD FLAP VANE LEADING IS CHAFED AT APPROX WS 56.30. REMOVED AND REPLACED RT INBOARD FLAP VANE LEADING SKIN IAW SRM 51-42-13.
Part: VANE — CHAFED (LT WING TE FLAP) · airframe 12,949 hrs · 12,382 cycles
LT INBD FLAP VANE LEADING EDGE CHAFED AT APPROX WS 104. REPAIRED LT INBOARD FLAP VANE LEADING EDGE IAW CRJ 200 SRM 57-52-00.
Part: FLOOR SUPPORT — CORRODED (BS 574-621) · airframe 12,949 hrs · 12,382 cycles
AFT CARGO BAY LBL 27 FROM BS 574 TO 621 CORRODED. REMOVED AND REPLACED FLOOR SUPPORT TEE SECTION AT LBL 27 BS 574-621 IAW SRM 53-00-43.
Part: VANE — CHAFED (RT WING TE FLAP) · airframe 12,949 hrs · 12,382 cycles
RT WING INBD FLAP VANE LEADING EDGE IS CHAFED AT APPROX WS 104. REPAIRED RT INBOARD FLAP VANE LEADING EDGE IAW CRJ 200 SRM 57-52-00.
Part: VANE — DAMAGED (LT WING TE FLAP) · airframe 12,949 hrs · 12,382 cycles
LEFT INBOARD FLAP VANE LEADING EDGE CHAFED AT APPROX WS 139. REMOVED AND REPLACED WITH NEW FLAP VANE LEADING EDGE SKIN IAW SRM 51-42-13.
Part: VANE — CHAFED (RT WING TE FLAP) · airframe 12,949 hrs · 12,382 cycles
RT WING INBOARD FLAP VANE LEADING EDGE IS CHAFED AT APPROX WS 139. REMOVED AND REPLACED WITH NEW LEADING EDGE SKIN IAW CRJ 200 SRM 51-42-13.
Part: PANEL — CRACKED (PAX DOOR) · airframe 12,949 hrs · 12,382 cycles
PAX DOOR FWD SIDE PANEL CRACKED AT UPPER STEP CUTOUT. REMOVED DAMAGE FROM PAX DOOR AND MADE A DOUBLER AND FILLERS AND INSTALLED IAW REO 601R-52-11-702TN.
Part: STRUCTURE — DAMAGED (TE FLAP) · airframe 12,949 hrs · 12,382 cycles
LEFT INBOARD FLAP TRAILING EDGE DAMAGED. REMOVED DAMAGED AREA AS REQUIRED AND INSTALLED REPAIR IAW SRM 57-52-00.
Part: SUPPORT BRACKET — CRACKED · airframe 12,949 hrs · 12,382 cycles
PASSENGER DOOR POWER ASSIST MOTOR SUPPORT CRACKED. REMOVED AND REPLACED SUPPORT BRACKET IAW SRM 51-42-06 5-7-12.
Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 12,949 hrs · 12,382 cycles
CARGO NET SUPPORT BEAM LOWER ATTACHMENT ANGLE TO THE AFT PRESSURE BULKHEAD CRACKED. REMOVED CRACKED BRACKET AND REPLACED WITH NEW BRACKET IAW CRJ 200 SRM 51-42-21.
Part: SEAT TRACK — CORRODED · airframe 12,949 hrs · 12,382 cycles
LEFT SIDE SEAT TRACK NR 5 WORN AND CORRODED. REMOVED LEFT SIDE SEAT TRACK NR 5 IAW AMM 53-01-11.
Part: SEAT TRACK — CORRODED · airframe 12,949 hrs · 12,382 cycles
LEFT SIDE SEAT TRACK NR 7 WORN AND CORRODED. REMOVED AND REPLACED LT SIDE TRACK NR 7 IAW AMM 53-01-11.
Part: SEAT TRACK — CORRODED · airframe 12,949 hrs · 12,382 cycles
LEFT SIDE SEAT TRACK NR 6 WORN AND CORRODED. REMOVED AND REPLACED LT NR 6 SEAT TRACK IAW AMM 53-01-11.
Part: SEAT TRACK — CORRODED · airframe 12,949 hrs · 12,382 cycles
RIGHT SIDE SEAT TRACK NR 7 WORN AND CORRODED. REMOVED AND REPLACED NR 7 SEAT TRACK IAW AMM 53-01-11.
Part: SEAT TRACK — CORRODED · airframe 12,949 hrs · 12,382 cycles
RIGHT SIDE SEAT TRACK NR 6 WORN AND CORRODED. REMOVED AND REPLACED NR 6 SEAT TRACK IAW AMM 53-01-11.
Part: SEAT TRACK — CORRODED · airframe 12,949 hrs · 12,382 cycles
RIGHT SIDE SEAT TRACK NR 5 WORN AND CORRODED. REMOVED AND REPLACED RIGHT SIDE SEAT TRACK NR 5 IAW AMM 53-01-11.
Part: SEAT TRACK — CORRODED · airframe 12,949 hrs · 12,382 cycles
LEFT SIDE SEAT TRACK NR 3 WORN AND CORRODED. REMOVED AND REPLACED LT NR 3 SEAT TRACK IAW AMM 53-01-011.
Part: PUMP — FAILED (HYD SYSTEM) · airframe 12,503 hrs · 11,838 cycles
AIR RETURN DUE TO GEAR DISAGREE NOSEWHEEL DOOR OPEN HYDRAULIC 3B PUMP AND HYD LOW PRESSURE WARNING AND CAUTION MESSAGES. FOUND ACMP 3B TO BE BAD. R & R PUMP 3B IAW AMM 29-12-03. OPS AND LEAK CHECKED GOOD.
2011
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 11,341 hrs · 10,492 cycles
FOUND EMERGENCY EXIT LIGHT BY SERVICE DOOR NOT WORKING AND THE LIGHT BY THE PASSENGER DOOR NOT WORKING. REPLACED BATTERY PACK CHARGER. OPS CHECKS GOOD IAW 33-51-04. PN ON/OFF BA5-0933-901, SN OFF C01475, SN ON C02049.
Part: PROXIMITY SENSOR — OUT OF ADJUST (NLG DOOR) · airframe 11,144 hrs · 10,272 cycles
AFTER SELECTING GEAR DOWN ON APPROACH, NOSE DOOR OPEN WARNING DISPLAYED. AIRSPEED WAS APPROX 180KIAS. PERFORMED POM CHECKLIST 7.10.10. AFTER A FEW MINUTES MESSAGE WENT AWAY. PERFORMED ADJUSTMENT CHECK OF PROX SENSOR PS17GA IAW AMM 32-61-05, OPS CHECKED GOOD. PERFORMED LANDING GEAR EXTENTION AND RETRACTION CHECK IAW AMM 32-30-00. ALL CHECKED GOOD AT TIME. NO DEFECTS NOTED AT TIME, MX NOTIFIED.
2010
Part: ACM — ODOR · airframe 10,682 hrs · 9,776 cycles
DURING SHORT FINAL F/A AND CREW NOTICED A BURNING ODOR COMING THROUGH THE ECS SYS, NO SMOKE OR HEAT DETECTED BY F/A OR CREW. ENGINE AIR WAS SOURCE FOR BLEED AIR. DEFERRED RT IAW MEL 21-51-1-1, C RAM AIR SOV VERIFIED OPERATIVE MX NOTIFIED 8483 ENTERED INTO MMO2. WHILE TROUBLESHOOTING FOUND RT PACK OIL APPEARS BLACK OR BURNED. SUSPECT RT ACM BAD. ITEM REMAINS DEFERRED MX NOTIFIED. R & R RT AIR CYCLE MACHINE IAW AMM 21-51-10. REMOVED FROM MEL 21-51-1-1C.
Part: LANDING GEAR — WARNING LIGHT · airframe 10,191 hrs · 9,210 cycles
RECEIVED A GEAR DISAGREE MASTER WARNING MESSAGE ON CLIMB OUT. COMPLETED THE EMERGENCY/NON-NORMAL PROCEDURE IN THE POM - 7,10,4. NOSE WHEEL WAS THE ONLY ONE IN DISAGREEMENT. RETURNED TO THE NEAREST SUITABLE AIRPORT. LANDED WITHOUT INCIDENT. FOUND PSEU FAULT CODE S22 FAR NGUPLK. INSPECTED NLG AND NLG DOORS, NO DEFECTS NOTED. SWUNG LANDING GEAR REPEATEDLY IAW AMM CH 32-30-00, NO DEFECTS NOTED. ALL CHECKS GOOD.
2009
Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY) · airframe 7,475 hrs · 6,399 cycles
"SMOKE TOILET" CAUTION MESSAGE RECEIVED AFTER DEPARTURE. FOLLOWED POM PROCEDURES 7.13.3 AND RETURNED TO CVG. CAUTION MESSAGE WENT OUT DURING RETURN TO LANDING. FLIGHT ATTENDANT REPORTED NO EVIDENCE OF SMOKE IN LAV OR CABIN. IMMEDIATELY AFTER MESSAGE RECEIVED WE FOLLOWED DEICE PROCEDURES AND CLEARED ENGINES FOR GREATER THEN 30 SECONDS AND DELAYED PACKS FOR NEARLY "10" MINUTES DURING TAXI. CREW REPORTED TO MXC THAT THEY SMELLED GLYCOL PRIOR TO MESSAGE. PERFORMED OPS CHECK OF LAV SMOKE DETECTION SYSTEM PER AMM 26-16. OPS CK GOOD. PERFORMED GROUND RUN/PACK RUN WITH FLIGHT CREW MESSAGE DID NOT REOCCUR A/C RELEASED FOR SERVICE.
2008
Part: COALESCER BAG — UNKNOWN · airframe 7,318 hrs · 6,238 cycles
AFTER TAKEOFF "SMOKE TOILET" CAUTION ILLUMINATED. FLIGHT ATTENDANT REPORTED SMOKE ALARM SOUNDING. COMPLETED POM CHECKLIST, PRECAUTIONARY LANDING. COMPLETED MM 409 NR 352872 REPLACEMENT OF L AND R COALESCER BAGS, INSPECTION FOR OIL LEAKS, REPLACEMENT OF LAV SMOKE DETECTOR. REF WORK CARD FOR DETAILS. FROM 409 352872 REPLACED LEFT AND RIGHT COALESCER BAGS PN 783689-3 IAW CRJ200 AMM 21-51-13 COMPLETED GROUND RUN AT PWR SETTINGS OPERATING NR 1 LT AND NR 2 RT A/C PACKS NO FAULT NOTED INSPECTED RT ACM INLET AND NO SIGN OF OIL NOTED REPLACED LAV SMOKE DETECTOR IAW AMM 26-16-00. OPS CK GOOD.
Part: SMOKE DETECTOR — FALSE INDICATION (LAVATORY) · airframe 7,297 hrs · 6,219 cycles
AFTER TAKEOFF SMOKE TOILET EICAS MSG ILLUMINATED POM PROCEDURE COMPLETED. LANDED AT NEAREST SUITABLE AIRPORT. FLT ATTENDANT REPORTED ODOR IN LAV AND SMOKE ALARM. AIRCRAFT WAS DE-ICED PRIOR TO DEPARTURE. RAN ENGINES IAW CRJ 200 AMM 71-00-00 FOR 30 MIN. MESSAGE EXTINGUISHED, UPON INITIAL RUN UP NOTED FAINT SMELL, BUT AFTER RUNNING ENGINES AND PACKS FOR 30 MIN. SMELL DISSIPATED AND DID NOT RETURN. NO SMOKE OR VAPOR NOTED. NO FURTHER ACTIONS REQUIRED.
Part: SMOKE DETECTOR — FALSE INDICATION (LAVATORY) · airframe 7,286 hrs · 6,206 cycles
ON CLIMB-OUT THE SMOKE TOILET MSG ILLUMINATED AND LAVATORY SMOKE ALARM SOUNDED FOR APPROX 5 MIN AND THEN EXTINGUISHED AFTER 5 MIN. THE CREW FOLLOWED THE AIRCRAFT NON-NORMAL PROCEDURES. THE CREW CONTACTED ATC AND DECLARED AN EMERGENCY AND REQUESTED PRIORITY BACK TO DTW, FLIGHT LANDED IN DTW WITHOUT FURTHER INCIDENT. THE FA AND PAX SMELLED AN ODOR THAT WAS VERY FOUL. THE FOUL SMELL DIDN'T APPEAR TO BE ELECTRICAL, RUBBER OR PETROLEUM. PERFORMED OP CHK LAV SMOKE DETECTION SYSTEM IAW AMM 26-16. OP CHECK GOOD NO EVIDENCE OF SMOKE OR FOUL SMELL IN THE LAV OR PAX COMPARTMENT. RAN PACKS OF BOTH ENGINES AND ALSO APU FOR 10 MINUTES.
Part: SMOKE DETECTOR — MALFUNCTIONED (LAVATORY)
AT 2000 FT GOT `SMOKE TOILET` EICAS MESSAGE AND DID AIR RETURN TO MSP. FLIGHT 3272 RETURNED TO MSP AFTER DEPARTURE DUE TO A LAVATORY SMOKE DETECTOR WARNING. THE CREW CALLED AFTER LANDING AND ACTUALLY SAID IT WAS A LAV SMOKE MESSAGE THAT WAS DISPLAYED RT AFTER T.O. THE CREW STAYED IN PATTERN, DECLARED AN EMERGENCY AND RETURNED TO MSP WITHOUT INCIDENCE. F/A VERIFIED NO SMOKE. REPLACED DETECTOR. (K)
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 5,983 hrs · 4,947 cycles
RT 625 OBLIQUE ANGLE IS CRACKED APPROX 1 INCH. REMOVED CRACKED ANGLE AND INSTALLED NEW ANGLE P/N 601-35012-52 IAW CRJ200 SRM 51-42-06.
Part: ANGLE — CRACKED (FUSELAGE) · airframe 5,983 hrs · 4,947 cycles
AT FS 625, LT SIDE, ANGLE IS CRACKED APPROX 1.0 IN. ANGLE WAS REPLACED WITH NEW.
2004
Part: BPSU — FAILED (TE FLAPS)
FLAPS FAIL AT 32 DEGREES ON APPROACH, QRH FOLLOWED UNEVENTFUL LANDING. REMOVED AND REPLACED LT BPSU (BRAKE POSITION SENSING UNIT) IAW 27 AMM. OPERATIONALLY TESTED GOOD.