N8965E

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 26,334 hrs · 26,628 cycles

DURING SCREW EXTRACTION FOUND CORROSION AROUND FASTENER HOLE AT FS 409.00 + 98 LBL 9 ( FLAGGED ) (48 MO INSP) RO 4/23/2020 REPAIRED FASTENER HOLE LOCATION AT F.S. 409.00+96 LBL 9 IAW BOMBARDIER REO ACCOMPLISHED HFEC IAW CRJ200 NTM. NDN ACCOMPLSHED U/T THICKNESS IAW CRJ 200 NTM. OLYMPUS 600 NORTEC AV8958. JULY, 2020. OLYMPUS 650 EPOCH AV8959. JULY, 2020.

Part: BEAM — CRACKED (FUSELAGE) · airframe 26,334 hrs · 26,628 cycles

CRACK FOUND ON 280BEAM AT FS 280 LBL 10 FWD (48 MO INSP) RO 4/23/2020 ACCOMPLISHED REPAIR OF 280 BEAM IAW CRJ200 REO

Part: SKIN — DAMAGED (FUSELAGE) · airframe 26,334 hrs · 26,628 cycles

LARGE AREA OF SKIN DAMAGE AFT OF LOW PRESSURE AIR ACCESS DOOR (172BR) RH SIDE BETWEEN FS 589.00 AND FS 605.00 FROM STGR 21R TO STGR 26R (48 MO INSP) RO 4/23/2020 ACCOMPLISHED CUTOUT AND REPAIR OF SKIN DAMAGE TO FUSELAGE SKIN BETWEEN FS 574 AND FS 621, STRINGER 24L TO STRINGER 20R IAW CRJ200 REO. WEIGHT ADDED 10.52 LBS AT FS 597.5

Part: BRACKET — CRACKED (FUSELAGE) · airframe 26,334 hrs · 26,628 cycles

CRACK FOUND ON FLOOR BEAM BRACKET AT FS 461 RBL 10 (48 MO INSP) RO 4/23/2020 REMOVED, DRILLED AND REPLACED FLOOR BEAM BRACKET AT FS 461 RBL 10. REMOVED AND REINSTALLED PRESSURE FLOOR PANELS AND WING TO FUSELAGE PANEL TO INSTALL FASTENERS. CRJ200 SRM), CRJ200 SRM, CRJ 200 AMM

Part: BRACKET — CRACKED (FUSELAGE) · airframe 26,334 hrs · 26,628 cycles

CRACK FOUND ON FLOOR BEAM BRACKET AT FS 484 LBL 35 (48 MO INSP) RO 4/23/2020 REMOVED AND REPLACED BRACKET CLIP AT FS 484.0 AND LBL 35 IAW BOMBARDIER DWG AND CRJ 200 SRM

Part: FRAME — CORRODED (FUSELAGE) · airframe 26,334 hrs · 26,628 cycles

CORROSION FOUND ON FRAME AT FS 605 UPPER & LOWER STRG R18 STRG L19 (48 MO INSP) RO 4/23/2020 UPON EVALUATION CORROSION WAS FOUND TO BE OUT OF LIMITS REMOVED AND REPLACED FRAME AT F.S. 605 FROM STR 21R TO STR 21L PER CRJ200 SRM.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 26,334 hrs · 26,628 cycles

CRACK FOUND ON FLOOR BEAM BRACKET AT FS 484 LBL 27 (48 MO INSP) RO 4/23/2020 REMOVED AND REPLACED FLOOR BEAM BRACKET AT FS 484 LBL 27 PER CRJ200 SRM.

Part: BRACKET — CRACKED (CARGO DOOR) · airframe 26,334 hrs · 26,628 cycles

CRACK FOUND ON CARGO DOOR TRACK BRACKET AR FS 574 (48 MO INSP) RO 4/23/2020 REMOVED CRACKED CARGO DOOR TRACK BRACKET AT FS 574. FABRICATED NEW PART, MATCH DRILLED, INSTALLED, AND RESTORED SURFACE FINISH. CRJ200 BOMBARDIER DRAWING, CRJ200 SRM.

Part: SKIN — CORRODED (LT WING) · airframe 26,334 hrs · 26,628 cycles

FRETTING AND PITTING FOUND ON LH WING PLANK ACCESS HOLE LOWER (510AB) (48 MO INSP) RO 4/23/2020 REPAIRED FUEL ACCESS PANEL CUTOUT 510AB IAW REO. ORIGINAL MATERIAL .190, MAX BLENDOUT .012, REMAINING MATERIAL THICKNESS .178. REF REO FOR REINSPECTION THRESHOLD. INSTALLED PANEL, BOND CHECK GOOD, LEAK CHECK GOOD. IAW REO PRESSURE GAUGE AG1134 CAL DUE AUG 2020 / TACHOMETER AV1335 CAL DUE JUL 2020

Part: SKIN — CORRODED (RT WING) · airframe 26,334 hrs · 26,628 cycles

FRETTING AND PITTING FOUND ON RH WING PLANK ACCESS HOLE LOWER (640BB) (48 MO INSP) RO 4/23/2020 REPAIRED FUEL ACCESS PANEL CUTOUT IAW REO. ORIGINAL MATERIAL .190, MAX BLEND OUT .011, REMAINING THICKNESS .179. REF REO FOR REPEAT INSPECTION THRESHOLD. INSTALLED PANEL, BOND CHECK GOOD, LEAK CHECK GOOD. IAW BOMBARDIER REO PRESSURE GAUGE. AG1134 CAL DUE AUG2020 / TACHOMETER. AV1335 CAL DUE JUL 2020

Part: PRIORITY VALVE — FAILED (NLG) · airframe 25,132 hrs · 25,240 cycles

AFTER TAKEOFF THE NOSE GEAR WOULD NOT RETRACT. GOT GEAR DISAGREE WARNING MESSAGE. RAN THE QRH. STILL WOULD NOT RETRACT. RETURNED TO FIELD. (FLT#3756) FO: 07/10/2019 CLOSED REMOVED AND REPLACED NLG PRIORITY VALVE AND NLG SELECTOR VALVE IAW AMM. OPS AND LEAK CHECKS GOOD IAT AMM.

Part: PROXIMITY SENSOR — OUT OF ADJUST (NLG STEERING) · airframe 24,499 hrs · 24,529 cycles

NOSE WHEEL STEERING INOP CAUTION MESSAGE FOLLOWED BY A WOW INPUT CAUTION MESSAGE AFTER TAKEOFF AND GEAR RETRACTION. DECLARED EMERGENCY. (FLT#7394) CLOSED RERIGGED LT NWS RVDT IAW AMM. READJUSTED PROX SENSOR SO3 PROX SENSOR IAW AMM. ALL MESSAGES CLEARED.

Part: SKIN — CHAFED (RT AILEORN) · airframe 22,937 hrs · 22,758 cycles

RIGHT AILERON, LOWER OUTBOARD SURFACE, LEADING EDGE CHAFED. BLENDED THE RIGHT AILERON LOWER OUTBOARD SURFACE LEADING EDGE TO A SMOOTH CONTURE IAW REO.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 22,937 hrs · 22,758 cycles

RIGHT INBOARD FLAP CENTER VANE CAP IS CHAFED. REMOVED & REPLACED THE FLAP CENTER VANE CAP IAW SRM.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 22,937 hrs · 22,758 cycles

LEFT INBOARD FLAP CENTER VANE CAP IS CHAFED. REMOVED & REPLACED THE FLAP CENTER VANE CAP IAW SRM.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 22,937 hrs · 22,758 cycles

LEFT INBOARD FLAP INBOARD VANE CAP IS CHAFED. REMOVED AND REPLACED THE FLAP VANE CAP IAW SRM.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 22,937 hrs · 22,758 cycles

RIGHT INBOARD FLAP OUTBOARD VANE CAP IS CHAFED. REMOVED & REPLACED THE FLAP O-B VANE CAP IAW SRM.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 22,937 hrs · 22,758 cycles

LEFT INBOARD FLAP OUTBOARD VANE CAP IS CHAFED. REMOVED & REPLACED THE FLAP O-B VANE CAP IAW SRM.

Part: FLOORBEAM — GOUGED (BS 618) · airframe 22,937 hrs · 22,758 cycles

CARGO FLOOR BEAM LBL27 HAS GOUGE ON OB FLANGE AT FS618. (C-CHECK) RO: 04/20/2018 BLENDED GOUGE DAMAGE ON CARGO FLOOR BEAM AT LBL 27 ON OB FLANGE AT FS618 IAW SRM AND REO. NDT PERFORMED WITH NO DEFECTS NOTED.

Part: SKIN — GOUGED (E/E DOOR) · airframe 22,937 hrs · 22,758 cycles

AVIONIC BAY DOOR CUTOUT HAS DEEP GOUGE ON FWD CENTER INTERIOR SIDE. INSTALLED DOUBLER IAW REO.

Part: SKIN — DENTED (BS 627) · airframe 22,937 hrs · 22,758 cycles

EXTERIOR ACFT AT BS 627, STRINGERS 2-3 DENTED. INSTALLED A DOUBLER IAW REO.

Part: FLAP SYSTEM — FAILED · airframe 19,418 hrs · 18,988 cycles

FLAP FAIL IN FLIGHT AT 0 DEGREES RIGHT AFTER DEPARTURE. DECLARED EMERGENCY AT DESTINATION. RESET AND OPERATED FLAPS IAW FIM AND AD.

Part: FLOOR SUPPORT — CORRODED (BS 559-621) · airframe 19,301 hrs · 18,868 cycles

LT SIDE CABIN FLOOR SUPPORT CORRODED BEYOND LIMITS BETWEEN BS 559+112 - 621. R & R LT SIDE CABIN FLOOR SUPPORT IAW REO. PERFORMED ACFT PRESSURE CHECK IAW AMM. ALL CHECKED GOOD.

Part: DOOR SILL — CORRODED (BS 310-349) · airframe 19,301 hrs · 18,868 cycles

STRUCTURE LOWER SILL ANGLE AT STR. 17, BETWEEN FS 310.00 TO FS 349.00 CORRODED. REMOVED PAX DOOR SILL LOWER ANGLE ASSY ON STRUCTURAL FUSELAGE AT STR 17 BETWEEN FS 310.00 TO FS 349.00. INSTALLED NEW SERVICEABLE PAX DOOR SILL ANGLE ASSY ON STRUCTURAL SIDE OF PAX DOOR ENTRY, PN 601R31527-221 IAW SRM.

Part: ACTUATOR — FAILED (TE FLAP) · airframe 16,865 hrs · 16,441 cycles

FLAP FAIL CAUTION IN FLIGHT FAILED AT 0 DEGREES DARING EXTENSION AIRSPEED 195 KTS FLIGHT OAT -10 DEGREES C. DEFERRED FLAPS IAW MEL 27-50-00 IAW DF AT MOC. PLACARD INSTALLED. ENTERED INTO DMR. REPLACE RT NR 1 ACTUATOR, INBD FLAP, INBD ACTUATOR.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 16,140 hrs · 15,714 cycles

NR 1 CEILING EMERGENCY LIGHT INOPERATIVE. DEFERRED IAW MEL 33-51-11. R&R NR 1 CHARGER IAW AMM 33-51-05 OP CK GOOD

Part: BATTERY — WEAK (CABIN) · airframe 16,109 hrs · 15,682 cycles

NR 1 & NR 2 EMER LIGHT BATTERIES WEAK. R & R NR 1 & NR 2 EMER LIGHT BATTERY IAW AMM 33-51-04.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 15,765 hrs · 153,238 cycles

FLIGHT ATTENDANT`S EMERGENCY FLASHLIGHT, RED LIGHT NOT FLASHING. REPLACED BATTERIES FOR FLIGHT ATTENDANT`S EMERGENCY FLASHLIGHT IAW AMM 25-61-01, OPERATIONS CHECKED GOOD.

Part: FLIGHT RECORDER — INOPERATIVE (COCKPIT) · airframe 15,746 hrs · 15,311 cycles

FDR ULB INOPERATIVE. R & R FDR ULD IAW AMM 31-31-05. FUNCTIONAL TEST OF FDR ULD GOOD IAW AMM 31-31-05-720-801.

Part: LIGHT — DEFECTIVE (CABIN) · airframe 15,746 hrs · 15,311 cycles

RT EMERGENCY EXIT BETA LIGHT DEFECTIVE. REMOVED 2 NUTS & SCREWS FROM HANDLE ASSEMBLY, EXTRACTED DEFECTIVE BETA LIGHT. INSERTED SERVICEABLE BETA LIGHT, INSTALLED 2 NUTS & SCREWS INTO HANDLE ASSEMBLY.

Part: RIB — CRACKED (LT WING) · airframe 15,722 hrs · 15,288 cycles

LEFT MLG FWD BATTERY RIB CRACKED 0.47 INCHES LONG. REPAIRED IAW REO 601R-57-51-046.

Part: RIB — CRACKED (RT WING) · airframe 15,722 hrs · 15,288 cycles

RIGHT MLG BATTERY RIB IS CRACKED AT WS 53.6, 0.95 INCHES LONG. REPAIRED IAW REO 601R-57-51-046.

Part: TORQUE SHAFT — FAULTY (TE FLAP) · airframe 15,499 hrs · 15,070 cycles

AFTER LANDING DURING FLAP RETRACTION WE GOT A FLAPS FAIL AMBER EICAS MESSAGE. FLAPS REMAINED AT 45, AIR TEMP WAS -28 C, AIRSPEED WAS 0, TIME INTO FLIGHT WHEN FAILURE HAPPENED WAS 1:16. TROUBLE SHOT IAW BOMB FIM REV 45 IAW AD 2009-06-12 PARA H 6I, AMOC DATED 7/22/2013 & PA AD27-052N. FOUND FAULT CODES 1JAM, 2 RT BPSU & 3 PDU DIFFERENTIAL. FOUND PRE TQ CHECKS LT = 13.8, RT = 25. PERFORMED FLAP LUBE CHECKLIST, REPLACED RT NR 1, 3 & 5 TQ SHAFTS, INSPECTED RT ACTUATORS, NO DEFECTS & LUBED ACTUATORS. POST MX TQ CHECKS ARE LT = 13 & RT = 11.

Part: SAFETY WIRE — BROKEN (FIRST AID KIT) · airframe 15,408 hrs · 14,979 cycles

MEDICAL KIT SAFETY WIRES BROKEN. R & R FIRST AID KIT IAW AMM 25-60-00.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 14,825 hrs · 14,380 cycles

NR 3 EMERGENCY FLOOD LIGHT AND AFT SIDE OF THE CENTER CURVED EXIT SIGN INOPERATIVE.

Part: BATTERY — SHORTED (EMERGENCY LIGHTS) · airframe 14,825 hrs · 14,380 cycles

ELECTRICAL FUMES AND SMOKE IN CABIN NEAR LAVATORY, ACFT POWERED DOWN AND OFF WHEN CREW DETECTED IT. FOUND BURNS AND ELECTRICAL SHORT ON EMERGENCY BATTERY ASSY NR 3. R & R EMERGENCY BATTERY AND CHARGER ASSY NR 3 IAW AMM 33-51-04 AND 33-51-05. OPS CHECKED GOOD.

Part: PBE — UNSERVICEABLE (COCKPIT) · airframe 14,798 hrs · 14,355 cycles

FLIGHT DECK PBE SEAL BROKEN. R & R PBE IN FLIGHT DECK.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 14,235 hrs · 13,780 cycles

SUPPORT ANGLE FS 621 AND LBL 36 BELOW CARGO BAY DOOR SUPPORT CHANNEL IS CRACKED. REPLACED IAW SRM 53-61-23, 51-40-11, 51-42-21, 51-24-36.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,995 hrs · 13,551 cycles

NR 2 CEILING EMERGENCY LIGHT WILL NOT TEST. REMOVED AND REPLACED CEILING EMERGENCY FLOOD LIGHT IAW AMM 33-51-16. OPS CHECK GOOD. PLACARD REMOVED. THIS CLEARS DM.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 13,261 hrs · 12,828 cycles

FIRST OFFICERS FLASHLIGHT IS NOT BLINKING. REMOVED AND REPLACED FIRST OFFICERS FLASHLIGHT ASSY IAW AMM 25-61-02. OPS CHECK GOOD. OK FOR SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 12,900 hrs · 12,460 cycles

MID CABIN EMERGENCY EXIT SIGN AND OVERWING LIGHTS INOPERATIVE. REMOVED AND REPLACED NR 3 EMERGENCY LIGHTS BATTERY ASSY IAW AMM 33-51-04.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 12,720 hrs · 12,256 cycles

FLOORBEAM AT RBL 9 AT FS 280 CRACKED. REPAIRED FLOORBEAM IAW EO C53144.

Part: BULKHEAD — CRACKED (BS 280) · airframe 12,720 hrs · 12,256 cycles

FS 280 BULKHEAD LOWER WEB CRACKED AT RBL 9. REPAIRED RT BULKHEAD IAW EO C53144.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 12,720 hrs · 12,256 cycles

RT FS 280 UPPER FLOORBEAM ANGLE CRACKED. REPAIRED RT BS 280 UPPER FLOORBEAM ANGLE AT RBL 9 IAW EO NR C53144.

Part: FIREWALL — CRACKED (LT NACELLE) · airframe 12,720 hrs · 12,256 cycles

FOUND LEFT PYLON FIREWALL WEB CRACKED. REPAIRED FIREWALL IAW REO NR 601R-54-51-120 AND EO NR C54003.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 12,720 hrs · 12,256 cycles

RT INBD FLAP VANE INBD LEADING CHAFED. REMOVED AND REPLACED RT INBOARD FLAP VANE LEADING EDGE IAW SRM 51-42-13.

Part: PROXIMITY SENSOR — OUT OF TOLERANCE (MLG) · airframe 9,834 hrs · 8,940 cycles

AFTER SELECTING GEAR UP ON TAKEOFF, RECEIVED A GEAR DISAGREE AURAL WARNING AND TRIPLE CHIME ON EICAS MSG. RAN POM CHECKLIST AND PULLED EMERGENCY GEAR EXTENSION HANDLE. NOSE GEAR INDICATION WAS RED BOX. AFTER RUNNING CHECKLIST WE GOT 3 GREEN LIGHTS. FOUND NLG CENTERED/EXTENDED PROX SENSOR OUT OF CLEARANCE AND OFFSET. ADJUSTED NLG CENTERED/EXTENDED PROX SNSR TO CORRECT CLEARANCE AND OFFSET TOLERANCE IAW AMM 32-61-05. PERFORMED GEAR SWINGS IAW AMM 07-11-00. ALL CHECKS GOOD AT THIS TIME.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 9,748 hrs · 8,850 cycles

RECEIVED A STEERING INOP MESSAGE PRIOR TO THE GEAR DISAGREE. PERFORMED OPS CHECK OF EXTENSION AND RETRACTION TEST IAW 32-30-00 OPS CHECK PROXIMITY SENSOR SYSTEM IAW 32-61-00. OPS CHECK STEERING SYSTEM IAW 32-50-00. OPS CHECK GOOD AT THIS TIME. SEE CONTINUATION CARDS FOR FURTHER DETAILS.

Part: UNKNOWN — FUMES (CABIN/COCKPIT) · airframe 8,827 hrs · 7,967 cycles

PASS AND CREW COMPLAINT ABOUT EXHAUST FUMES NOTICED MORE DURING CRUISE AT 5000-7000 FT WITH HEAT ON. GROUND RAN ENGINES AT HIGH POWER SETTINGS. PERFORMED OPS CHECK OF TEMP CTRL SYS IAW AMM 21-60. RAN ACFT AT FULL HOT NO EXHAUST FUMES NOTED. OPS CHECK GOOD AT THIS TIME.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 8,780 hrs · 7,915 cycles

EMER LTS ON STATUS MSG ILLUMINATED MULTIPLE TIMES IN FLIGHT ACCOMPANIED BY FLICKERING EMERGENCY LIGHTS IN CABIN. REPLACED NR 1 EMERGENCY LIGHTS BATTERY PACK POWER SUPPLY PN OFF/ON SN OFF 23214, SN ON 11257 IAW AMM 33-51-04-04, OPS CHECK GOOD.

Part: SWITCH — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 8,765 hrs · 7,895 cycles

EMER LIGHTS ON WHITE ADVISORY MSG CAME ON AT 5000 MEL CYCLED OFF THEN CAME ON ONE SHORT FINAL. BUSES ALL NORMAL. F/A SAYS THE FIRST 1/3 OF THE EMER LIGHTS WERE ON. R & R F/A EMERGENCY LIGHT SWITCH IAW AMM 33-52-00. OP CK GOOD. NO DEFECTS NOTED. OK FOR SERVICE.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 8,737 hrs · 7,865 cycles

NOTED PAX DOOR AND SERVICE DOOR EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY CHARGER ASSY AT PS1LF IAW 33-51-05 AND REMOVED AND REPLACED BATTERY ASSY PS1LF IAW AMM 33-51-04. OPS CHECKS GOOD.

Part: FLAP SYSTEM — FAILED (TE FLAPS) · airframe 6,307 hrs · 5,263 cycles

FLAP FAIL CAUTION FLAP FAIL AT 30 DEG 6900/160 KTS/GEAR DOWN. COMPLETED WITH FLAP FAIL RESET PROCEDURE IAW CRJ POM SECTION 3.8. (S)

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 5,711 hrs · 4,703 cycles

LT INBD FLAP VANE L/E CHAFED AT INBD STOP CONTACT .020" D. REMOVED I/B FLAP VANE L/E LOCATED AND DRILLED NEW L/E IAW CRJ SRM 51-40-11. INSTALLED NEW L/E IAW CRJ SRM 51-42-06. PAINTED LT I/B FLAP VANE L/E STOP IAW CRJ SRM 51-25-26.

Part: INTERCOSTAL — CRACKED (BS 625) · airframe 5,711 hrs · 4,703 cycles

LT INTERCOSTAL OBLIQUE ANGLE AT FS 625 UPPER IN AFT EQUIPMENT COMPARTMENT IS CRACKED 1 INCH LONG. REMOVED/INSTALLED NEW INTERCOSTAL IAW CRJ 200 SRM 51-42-06.

Part: CONTROL SYSTEM — MALFUNCTIONED (TE FLAPS)

(REF NR: 05-093) FLAPS FAIL AT 20 WHEN SELECTED ON TAXI. RESET SYSTEM AND PLACED 72 HOUR WATCH IAW AD 98-20-01. (K)