N8896A

Part: CHARGER — INOPERATIVE · airframe 32,936 hrs · 31,019 cycles

"CABIN CEILING - LEVEL EMERGENCY LIGHT EXIT SIGN INOPERATIVE (ROW 8).FR ONT ILLUMATES FULLY REAR HAS NO ILLUMINATION. " DEFERRED CABIN EMERGENCY LIGHTS IN ACCORDANCE WITH MEL 33-51-1A.MM02 UPDATED.PLACARD INSTALLED. MOC NOTIFIED. # 99758. REMOVED AND REPLACED BATTERY CHARGER ASSY AT PS3LF IAW AMM 33-51-05. OP'S CHECK GOOD. THIS CLEARS MEL#3771732-1. MM02 UPDATED. PLACARDS REMOVED.MOC #1390 NOTIFI

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 31,749 hrs · 29,489 cycles

EMERGENCY LIGHT WILL NOT STAY ON INTERIOR OR EXTERIOR. REMOVED/REPLACED 4 EMERGENCY BATTERY PACK, IAW AMM 33-51-04. OPERATIONS CHECK GOOD, NO DEFECTS NOTED AT THIS TIME.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 31,702 hrs · 29,421 cycles

FLOOR TRACKING LIGHTING LAMPS 6 TO 8 AND FLOOR PROX EXIT SIGN RIGHT OVERWING LIGHT INOPERABLE. REMOVED AND REPLACED INVERTER PS3LY P/N ON/OFF 5925-7, IAW CRJ 200 AMM 33-51-07. OPERATIONS TEST GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,115 hrs · 28,707 cycles

SECOND TO AFT EMERGENCY FLOOR TRACK LIGHT, INOPERATIVE. REPLACED THE EMERGENCY LIGHT IAW AMM 33-51-01. OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 29,045 hrs · 26,512 cycles

DURING WALK AROUND FOUND RH EXTERIOR EMERGENCY LIGHT INOP. R+R EMERGENCY LIGHT BULB IAW AMM 33-51-21 OPS CHECK GOOD. P/N ON/OFF 1317, S/N NSN.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,333 hrs · 25,742 cycles

DURING LINE CHECK FOUND AFT EMERGENCY FLOOR LIGHTS NOT WORKING. REPLACED AFT TWO EMERGENCY FLOOR TRACK LIGHT STRIPS PN 5946-5 AND PN 36378-2 IAW AMM 33-51-01.

Part: LIGHT — INOPERATIVE (ROWS 9-12) · airframe 28,128 hrs · 25,540 cycles

FLOOR TRACK EMERGENCY LIGHTS 9 THRU 12 INOP REMOVED AND REPLACED AFT EMERGENCY LIGHT CABLE ASSEMBLY AND #10 EMERGENCY LIGHT STRIP IAW CRJ 200 AMM 33-51-01. OPS CHECKS GOOD.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 28,128 hrs · 25,540 cycles

FOUND EXTERIOR EMERGENCY LIGHT 2 INOP. REMOVED AND REPLACED EXTERIOR EMERGENCY LIGHT 2 IAW CRJ 200 AMM 33-51-21.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 27,890 hrs · 25,290 cycles

REAR PRESSURE BULKHEAD HAS A CRACK AT AFT CARGO DOOR TRACK LBL 27.5 AND WL 225. REPAIRED CRACK DAMAGE TO REAR BULKHEAD PER REO 601R-53-61-6683/ REO 601R-53-61-1541.

Part: SKIN — CRACKED (FUSELAGE) · airframe 27,890 hrs · 25,290 cycles

LT TRU DOOR LAND IS CRACKED BELOW AFT LATCH. R&R LEFT TRU DOOR LAND IAW SRM 51-42-06.

Part: SKIN — GOUGED (TE FLAP VANE) · airframe 27,890 hrs · 25,290 cycles

LT INBD FLAP, FLAP VANE LEADING EDGE IS CHAFED INBD OF INBD VANE ACTUATOR. BLENDED FOUND OUT OF LIMITS IAW SRM51-42-13.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 27,890 hrs · 25,290 cycles

STR 3 LEFT JUST AFT OF FS280.00 HAS A CRACK. REMOVED AND REPLACED 2EA CLIPS AT STR 3L AFT OF FS280 BULKHEAD (NO CRACKS FOUND IN STRINGER) IAW SRM 51-42-06.

Part: FITTING — CRACKED (FUSELAGE) · airframe 27,890 hrs · 25,290 cycles

INTERCOSTAL AT FS484 OTBD OF RBL27 HAS CRACKED CLIP ON OTBD END. REPAIRED FS484 INTERCOSTAL CLIPS IAW REO 601R-53-41-059.

Part: HINGE — CRACKED (FUSELAGE) · airframe 27,890 hrs · 25,290 cycles

CARGO DOOR FOLDING THRESHOLD HINGES CRACKED. REMOVE AND REPLACED WITH NEW 3EA CARGO DOOR THRESHOLD HINGES IAW SRM 51-42-00.

Part: STAND OFF — BENT (FUSELAGE) · airframe 27,890 hrs · 25,290 cycles

21 EA APB LINER STAND-OFFS ARE BENT. REMOVED AND REPLACED 21 EA LINER STAND-OFFS IAW SRM 51-42-06.

Part: FITTING — CORRODED (FUSELAGE) · airframe 27,890 hrs · 25,290 cycles

CABIN STA 349 RBL 40 AREA FLOOR BEAM CORRODED AT FLOOR FITTING. REMOVED AND REPLACED FITTING AND PLASTIC COVER AT STA 349 RBL40 IAW SRM 51-42-13.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 27,890 hrs · 25,290 cycles

LT SIDE SEAT RAIL NR 5 FROM FS449.85 TO 499.0 HAS CORROSION. R&R LT SIDE SEAT RAIL IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 27,890 hrs · 25,290 cycles

LT SIDE SEAT RAIL NR 4 FROM FS409+112 TO FS449.85 HAS CORROSION. REMOVED AND REPLACED WITH NEW LT SIDE SEAT TRACK STA 409+112 449:85 IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 27,890 hrs · 25,290 cycles

LT SIDE SEAT RAIL NR 6 FROM FS499.0 TO FS544.0 HAS CORROSION. R&R WITH NEW NR 6 LT SIDE SEAT TRACK IAW AMM 53-01-11.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 27,890 hrs · 25,290 cycles

PASSENGER ENTRY DOOR AFT ANGLE IS CRACKED. REMOVED AND REPLACED PASSENGER ENTRY DOOR AFT DRAG ANGLE IAW REO 601R-52-11-513.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 27,890 hrs · 25,290 cycles

LT SIDE SEAT RAILS NR 7 FROM FS544.0 TO FS559+112 HAS CORROSION. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-00-49.

Part: COVER — DAMAGED (CABIN) · airframe 27,890 hrs · 25,290 cycles

EMER PATH LIGHTING COVER HAS SEVERAL CRACKS AND DAMAGED SPOTS IN CABIN. REMOVED & REINSTALLED EMERGENCY FLOOR TRACK LIGHTING IAW AMM 33-51-01-000-801 AND AMM 33-51-01-400-801. EMERGENCY FLOOR TRACK LIGHTING OPS CHECKED GOOD IAW AMM 33-51-00-710-801 STEPS 2A & 3A (1), (2) & (3) FLOOR TRACK LIGHTING LAMPS 1-8.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 27,890 hrs · 25,290 cycles

STA 280 FLOOR SUPPORT CORRODED BELOW FLT DECK DOOR AREA. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-42-06, 51-42-21.

Part: FRAME — CRACKED (FUSELAGE) · airframe 27,890 hrs · 25,290 cycles

FRAME AT FS333 UPPER FUSELAGE ABOVE THE PAX DOOR IS CRACKED. REPAIRED FRAME IAW EA CRJ253-07467.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 27,890 hrs · 25,290 cycles

LBL9 SEAT TRACK BETWEEN FS559.0 AND FS559.0+86 HAS CORROSION. REMOVED AND REPLACED LBL9 SEAT TRACK BETWEEN FS559.0 AND FS559.0+86 HAS CORROSION.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 27,890 hrs · 25,290 cycles

AFT CARGO COMPARTMENT SEAT TRACK CORRODED I/B FWD RT TRACK. REMOVED AND REPLACED SEAT TRACK.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 27,890 hrs · 25,290 cycles

AFT CARGO COMPARTMENT SEAT TRACK CORRODED O/B FWD RT TRACK. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-00-49 REF W/O 1016031/1600/0066 S6476423 FOR SEAT TRACK FAB.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 27,890 hrs · 25,290 cycles

AFT CARGO COMPARTMENT SEAT TRACK CORRODED I/B FWD LT TRACK. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-00-49 REF W/O 1016031/1600/0065 S6476422 FOR SEAT TRACK FAB.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 27,890 hrs · 25,290 cycles

AFT CARGO COMPARTMENT SEAT TRACK CORRODED I/B CENTER LT TRACK. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-00-49 REF W/O 1016031/1600/0063 S 6476420 FOR SEAT TRACK FAB.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 27,890 hrs · 25,290 cycles

AFT CARGO COMPARTMENT SEAT TRACK CORRODED O/B FWD LT TRACK. REMOVED AND REPLACED SEAT TRACK AT AFT CARGO COMPARTMENT O/B FWD LT TRACK IAW AMM 53-00-49.

Part: LEVER — BROKEN (O2 MASK) · airframe 27,781 hrs · 25,165 cycles

RED LEVER ON FO'S OXYGEN MASK BROKE DURING O2 TEST. REMOVED AND REPLACED F/O CREW O2 MASK, REF AMM 35-11-12, OPS CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 27,739 hrs · 25,121 cycles

EMERGENCY LIGHTS ONLY WORK FOR A FEW SECONDS WHEN "ON". REMOVED AND REPLACED ALL 4 EMERGENCY LIGHT BATTERY PACKS IAW AMM 33-510-04. OPS CHECK GOOD. ALL EMERGENCY LIGHTS ILLUMINATE WITH SWITCH SELECTED TO "ON". A/C OK FOR SVC.

Part: WIRE — DAMAGED (CABIN) · airframe 27,647 hrs · 25,028 cycles

EMERGENCY LIGHT WIRES UNDER FA JUMPSEAT WHEN STOWED WERE SNAPPED. EXIT AND FLOOD LIGHT INOPERATIVE. REPAIRED WIRING AT FWD LEVEL FLOODLIGHT AND EMER EXIT SIGN RE AMM CRJ200-20-10-00.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 26,186 hrs · 23,446 cycles

PASSENGER CABIN HAS TWO EMERGENCY LIGHTS INOPERATIVE. REPLACED EMERGENCY CEILING LIGHT LAMPS WITH SERVICEABLE LAMPS IAW AMM 33-51-16, OPS CHECKED GOOD.

Part: ELT — NO TEST (CABIN) · airframe 25,322 hrs · 22,561 cycles

ELT FAILED AN OPERATIONAL CHECK OF G-SWITCH. REMOVED & REPLACED THE ELT IAW AMM 25-62-01 OPS CHECKED GOOD.

Part: OXYGEN MASK — INOPERATIVE (COCKPIT) · airframe 24,549 hrs · 21,786 cycles

NOT ABLE TO BREATHE OUT OF CAPTAIN`S OXYGEN MASK WHEN DONNED. R & R THE OXYGEN MASK IAW AMM 35-11-12. OPS CHECKED GOOD.

Part: LIGHT — DETACHED (CABIN) · airframe 24,137 hrs · 21,358 cycles

FLOOR TRACK LIGHTING INOPERATIVE. RE-ATTACHED FLOOR TRACK LIGHTING IAW AMM 33-51-01. OPERATIONS CHECKED GOOD.

Part: SIGN — INOPERATIVE (CABIN) · airframe 24,018 hrs · 21,210 cycles

EMERGENCY EXIT SIGN BY PAX DOOR INOPERATIVE. R & R SIGN IAW AMM 33-51-10.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 23,813 hrs · 20,989 cycles

RIGHT NR 1 EXTERNAL E LIGHT INOPERATIVE. R & R NR 1 EXTERNAL E LIGHT IAW AMM 33-51-21. OPERATIONS CHECKED GOOD.

Part: BRACE — CRACKED (FUSELAGE) · airframe 23,810 hrs · 20,987 cycles

RIGHT ACM RACK LOWER HORIZONTAL BRACE Z ANGLE CRACKED. R & R BRACE IAW SRM 51-41-21.

Part: GUIDE PLATE — CHAFED (CARGO BAY) · airframe 23,810 hrs · 20,987 cycles

E & E BAY DOOR CUT OUT INTERIOR FWD RT GUIDE PLATE CHAFED. R & R WITH NEW GUIDE PLATE IAW SRM 51-41-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 23,810 hrs · 20,987 cycles

FLOORBOARD SUPPORT HAS CORROSION AT FASTENER HOLES, STATION 621, LBL 10 - 17. REPAIRED FLOOR SUPPORT IAW REO 601R-53-61-4690 & EA CRJ253-04 112.

Part: HINGE FITTING — FAILED (VERTICAL STAB) · airframe 23,810 hrs · 20,987 cycles

VERTICAL STAB TO RUDDER CTR LOWER BEARING FITTING FAILED PRE LOAD CHECK OF NEW BEARING. REMOVED CTR LOWER HINGE FITTING & INSTALLED NEW FITTING IAW RIL 0602 REV H.

Part: FAIRING — CHAFED (FUSELAGE) · airframe 23,810 hrs · 20,987 cycles

AFTER REMOVAL OF ATTACH BRACKET FROM RT STUB FAIRING ON NR 4429263, FOUND RT STUB FAIRING TO CHAFED AT BRACKET ATTACH POINT. RECEIVED NEW RT STUB FAIRING PART 601R31199-92. INSTALLED ON 4428521, WO 1012596 000 0074.

Part: PANEL — CHAFED (EMPENNAGE) · airframe 23,810 hrs · 20,987 cycles

EMPENNAGE PANEL 334BB IS CHAFED. REMOVED CORROSION & FOUND TO BE OUT OF LIMITS IAW SRM 51-21-06 & 55-20-00 FIG 1 SHT 2. RECEIVED NEW PANEL PN 600-24029-25. LOCATED, DRILLED, COUNTERSUNK HOLES & INSTALLED NUTPLATES IAW SRM 51-45-00 & 51-41-02. APPLIED FINISH IAW SRM 51-21-11 & 51-2.

Part: PANEL — CHAFED (EMPENNAGE) · airframe 23,810 hrs · 20,987 cycles

EMPENNAGE PANEL 334CB IS CHAFED. REMOVED CORROSION & FOUND TO BE OUT OF LIMITS IAW SRM 51-21-06 & 55-20-00 FIG 1 SHT 2. RECEIVED NEW PANEL, PN 600-24029-21S. LOCATED, DRILLED, & COUNTERSUNK HOLES & INSTALLED NUTPLATES IAW SRM 51-40-11 & 51-42-06. APPLIED FINISH IAW SRM 51-21-11, 51-25-06, & 51-25-16.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 23,810 hrs · 20,987 cycles

NUMBER 4 FLOOR SEAT RAIL AT LBL 9 HAS CORROSION AT 4 LOCATIONS. R & R NR 4 FLOOR SEAT RAIL AT LBL 9 IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 23,810 hrs · 20,987 cycles

CABIN, LT SIDE SEAT TRACK STICK HAS 6 AREAS OF CORROSION, 7TH SEAT TRACK STICK FROM FRONT. FABRICATED SEAT TRACK IAW REO 601R-53-00-485. INSTALLED SEAT TRACK IAW AMM 53-01-11-A.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 23,810 hrs · 20,987 cycles

CABIN, RT SIDE SEAT TRACK STICK HAS 4 AREAS OF CORROSION, 4TH SEAT TRACK STICK FROM FRONT. FABRICATED SEAT TRACK IAW REO 601R-53-00-485. INSTALLED SEAT TRACK IAW AMM 53-01-11-A.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 23,810 hrs · 20,987 cycles

CABIN, LT SIDE SEAT TRACK STICK HAS 5 AREAS OF CORROSION. 3RD SEAT TRACK STICK FROM FRONT. R & R LT SIDE SEAT TRACK WITH NEW SIDE TRACK IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 23,810 hrs · 20,987 cycles

NUMBER 1 FLOOR SEAT RAIL AT LBL 9 HAS CORROSION, AT MULTIPLE LOCATIONS FROM FWD END TO AFT END. R & R NR 1 LBL 9 SEAT TRACK IAW AMM 53-01-11.

Part: ATTACH ANGLE — BROKEN (VERTICAL STAB) · airframe 23,810 hrs · 20,987 cycles

VERTICAL STAB RT SIDE FAIRING, SMALL ATTACH ANGLE JUST AFT OF TRIM ACTUATOR BROKEN. R & R WITH FABRICATED ATTACH ANGLE ON VERTICAL STA6 RT SIDE SMALL FAIRING, JUST AFT OF TRIM ACTUATOR IAW SRM 51-24-21.

Part: FITTING — CRACKED (FUSELAGE) · airframe 23,810 hrs · 20,987 cycles

CLIP OTBD OF RBL 27 & FS 484 IS CRACKED. R & R CLIP AT RBL 27 & FS 484 IAW REO 601R-53-41-059.

Part: BULKHEAD — CHAFED (FUSELAGE) · airframe 23,810 hrs · 20,987 cycles

CARGO BAY AFT PRESS BULKHEAD FWD FACE ABOVE FLOOR HAS SMALL CHAFED AREAS IN 8 PLACES. REMOVED 8 EACH CHAFE MARKS & FOUND 17 EACH CHAFE MARKS TO BE WITHIN LIMITS AFTER BLEND OUT IAW REO 601R-53-61-2155 REV A . PAD UP .051" MIN REMAINING, .051" MIN ALLOWED, 063" ORIGINAL. WEB POCKETS .038" MIN REMAINING, .029" MIN ALLOWED & .043" ORIGINAL. INSTALLED REPAIR DOUBLER IAW REO 601R-53-61-1285 REV D TO DAMAGE BEYOND LIMITS AT RBL 18 WL 103, STATION 621. PAD UP .046" MIN REMAINING, .051" MIN ALLOWED & .063" ORIGINAL.

Part: LIGHT — CRACKED (CABIN) · airframe 23,500 hrs · 20,686 cycles

DMM 8835 SERVICE DOOR EMER LIGHT CRACKED. R & R SERVICE DOOR EMER LIGHT IAW 33-51-13. OPERATIONS CHECKED GOOD. THIS CLEARS DM 8835.

Part: LENS — CRACKED (EXIT SIGN) · airframe 23,181 hrs · 20,362 cycles

EMERGENCY EXIT SIGN FLOOD LIGHT ON GALLEY BY THE SERVICE DOOR LENS & BASE CRACKED. NEF C-6, 120 DAYS

Part: CONNECTOR — DISCONNECTED (SMOKE DETECTOR) · airframe 22,799 hrs · 19,985 cycles

SMOKE DETECTOR IN LAVATORY NOT WORKING. UPON REMOVAL OF LAVATORY SMOKE DETECTOR, FOUND CONNECTOR DISCONNECTED. RECONNECTED CONNECTOR & PERFORMED OPERATIONS CHECK IAW AMM 26-16-01. OPERATIONS CHECKED GOOD. OK FOR SERVICE.

Part: STRINGER — GOUGED (FUSELAGE) · airframe 22,781 hrs · 19,965 cycles

FOUND STRINGER 23R GOUGED & CRACKED APPROXIMATELY 0.785” LONG AT APPROXIMATELY FS 200. REPAIRED IAW EA CRJ253-02620.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 22,781 hrs · 19,965 cycles

FS 621 BULKHEAD CRACKED AT CARGO DOOR LINTEL FITTING. REPAIRED IAW REO 601R-53-61-1230.

Part: HINGE FITTING — OUT OF TOLERANCE (LT ELEVATOR) · airframe 22,781 hrs · 19,965 cycles

LT ELEVATOR NR 1 HINGE FITTING HAS 0.050 INCHES GAP BETWEEN HINGE FITTING HALVES. REPAIRED IAW SRM 51-42-6, 51-42-13, 51-42-21 & 51-40-11.

Part: HYDRAULIC SYSTEM — CONTAMINATED (NR 3) · airframe 22,201 hrs · 19,395 cycles

ON TAKEOFF HYD 3 LOW PRESS FOLLOWED BY GEAR DISAGREE & NOSE DOOR WARNINGS. HYD 3 PRESS AT 1600 DURING FAILURE, CLEARED IN 2 MINUTES, ALL MSGS WERE GONE. ALL PRESS RETURNED TO NORMAL. COMPLIED WITH PA 05-018 REV K SCENARIO 1 BLED NR 3 HYD SYS & INBD BRAKES. PERFORMED FUNCTIONAL CHECKS ON LG EXTENSION & RETRACTION. ALL CHECKS ARE GOOD. ACFT OK FOR SERVICE AT THIS TIME IAW AMM'S 32-30-00, 32-43-00 & 29-10-00.

Part: HYDRAULIC SYSTEM — CONTAMINATED (NR 3) · airframe 22,169 hrs · 19,361 cycles

ON CLIMB OUT OF ESC, RECEIVED MASTER WARNING FOR GEAR DISAGREE, NOSE DOOR OPEN. ALSO MASTER CAUTION FOR HYD LOW PRESS SYS 3. HYD QTY SHOWING 100% WITH WHITE DIAGONAL LINES TEMP 19C, GEAR FINALLY CAME UP & MESSAGES WENT AWAY. BLED HYD SYS NR 3 IAW AMM 29-10-00. PERFORMED GEAR SWING IAW AMM 32-30-00. SERVICED HYD SYS NR 3 IAW AMM 12-12-29. OPERATIONS CHECKED GOOD, OK FOR SERVICE.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 21,466 hrs · 18,637 cycles

F/O FLASHLIGHT IS INOPERATIVE.

Part: FEEDER CABLE — DAMAGED (EMERGENCY LIGHT) · airframe 21,188 hrs · 18,360 cycles

EMERGENCY LIGHT INOPERATIVEE. R & R EMERGENCY LIGHT POWER STRIP IAW AMM 33-51-01. COMPLIED WITH OPS TESTS OF THE EMERGENCY LIGHTS IAW AMM 33-51-00-710-801. NO DEFECTS NOTED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,114 hrs · 18,295 cycles

CABIN EMERGENCY LIGHT INOPERATIVE. R & R LIGHT IAW AMM 33-51-01. OPS CHECKED GOOD.

Part: HYDRAULIC LINE — LOOSE (HYDRAULIC SYS) · airframe 20,422 hrs · 17,606 cycles

ON FLIGHT 4084 (DTW TO ITH) ON CLIMBOUT OF DTW, RETRACTED GEAR AND INITIALLY GOT HYD 3 LOW PRESS CAUTION SHORTLY FOLLOWED BY NOSE DOOR MASTER WARNING FOLLOWED BY GEAR DISAGREE MASTER WARNING. DURING THIS MAIN GEAR WERE SHOWING YELLOW AND NOSE GEAR SHOWING WHITE. WHEN WE GOT DISAGREE MAIN GEAR TURNED RED AND THEN THE GEAR WENT UP AND THE MESSAGE WENT AWAY BEFORE WE COULD START THE QRH. PERFORMED AN AIR RETURN BACK TO DTW. FOUND SUCTION LINE ON PUMP 3B LOOSE AND LEAKING. RESECURED SUCTION LINE IAW AMM 29-12-03. COMPLIED WITH PA 05-018J SCENARIO 1 PER MOTOR REQUEST. NO DEFECTS NOTED. OK FOR SERVICE. ALSO BLED HYD SYSTEM 3 IAW AMM TASK 12-12-29-611-803.

Part: UNKNOWN — MALFUNCTIONED (LT ENGINE) · airframe 20,302 hrs · 17,489 cycles

LEFT ENGINE SPOOL UP TIME LAGS BEHIND RIGHT ENGINE CAUSING UNNECESSARY YAW TENDENCIES IN FLIGHT. ALSO CAUSE LOSS OF DIRECTIONAL CONTROL ON "THURST REVERSER" DEPLOYMENT. W N1 MATCHED, THE N2 FOR RIGHT ENGINE IS LOWER BY 25%. THRUST LEVERS ARE NEARLY IMPOSSIBLE TO SYNCH DU. PERFORMED ACCELERATED/DECELERATED CHECK IAW AMM 71-00-00. ALL CHECKS FOUND TO BE WITHIN LIMITS. AIRCRAFT OK FOR SERVICE.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 19,677 hrs · 16,869 cycles

CRACK FOUND IN CAP ANGLES AT FS 559 RBL 19, LBL 9, AND LBL 18. REPAIRED IAW BOMBARDIER REO 601R-53-41-260 AND REO 601R-53-41-609.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,550 hrs · 16,753 cycles

LAST TWO OVERHEAD EMERGENCY FLOODLIGHT OUT. REMOVED AND REPLACED OVERHEAD EMERGENCY LIGHTS IAW AMM 33-51-18. OPS CHECKED GOOD.

Part: LIFE VEST — UNSERVICEABLE (COCKPIT) · airframe 18,896 hrs · 16,107 cycles

F/O LIFE VEST BAG TORN. REMOVED AND REPLACED F/O LIFE VEST IN ACCORDANCE WITH AMM 25-61-03.

Part: TRIM SYSTEM — MALFUNCTIONED (AILERONS) · airframe 18,837 hrs · 16,048 cycles

AILREON TRIM DOES NOT WORK AT ALL IN FLIGHT OR ON GROUND. RESET AILERON TRIM SYSTEM IAW AMM 27-12-00. OPS CHECKED GOOD.

Part: PLUG — MISSING (RT ENGINE) · airframe 18,532 hrs · 15,750 cycles

RT ENG TAIL CONE HAS EVIDANCE OF BURN DAMAGE. FOUND BOROSCOPE PLUG S50 MISSING. REPLACED BOROSCOPE PLUG IAW AMM 72-00-00. REMOVED AND REPLACED RT EXHAUST FAIRING IAW AMM 78-11-01.

Part: ENGINE — VIBRATION (RIGHT) · airframe 18,403 hrs · 15,617 cycles

AIR RETURN AT 10,000 FEET AIRCRAFT STARTED SMALL VIBRATION, UNUSUAL SOUND FROM RIGHT SIDE OF AC, RIGHT ENGINE ITT WAS POINTING TO 12 O`CLOCK, RAN QRH, SHUTDOWN ENGINE, RETURNED TO DTW. REMOVED AND REPLACED RT ENGINE IAW AMM 71-00-00. REFERENCE DISC NR 1 AML PG 2169816. RT ENGINE OPS CHECKS GOOD. OK FOR SVC.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 18,213 hrs · 15,484 cycles

LT FUEL LOW PRESS CAUTION MSG IN FLIGHT ALL OTHER PRAMS NORMAL.

Part: SWITCH — DEFECTIVE (THRUST REVERSER) · airframe 18,179 hrs · 15,444 cycles

NR 2 ENGINE REV ICON AND NUMEROUS R REV UNLOCKED CAUTION FROM CRUISE THROUGH LANDING, NO CAUTION FROM 10000 FEET THRU TOP OF CLIMB. AT FL 330 R REV UNLOCKED STARTED INTERMITTENTLY THEN STAYED ON REST OF CRUISE CONTINUOUSLY. REMOVED AND REPLACED RT ENGINE T/R STOW SWITCH IAW AMM 78-37-01. RIGGED STOW SWITCH IAW AMM 78-37-01. OPS CHECK- GOOD THIS CLEARS DM 55454. PLACARD REMOVED.

Part: SWITCH — DEFECTIVE (THRUST REVERSER) · airframe 18,167 hrs · 15,432 cycles

THRUST REV (R) UNLOCK MSG CONTINUED TO DISPLAY INTERMITTENTLY EVERY FEW SECONDS FOR THE LAST 10-15 MIN OF FLIGHT. INTERFERES WITH SAFE OPERATIONS. VERIFIED MEL PROCEDURE, T/R DEFERRAL CORRECTLY. A/C OK FOR SERVICE AT THIS TIME PER MEL 78-30-01. REMOVED AND REPLACED RT ENGINE T/R STOW SWITCH IAW AMM 78-37-01. RIGGED STOW SWITCH IAW AMM 78-37-01. OPS CHECK- GOOD THIS CLEARS DM 55454. PLACARD REMOVED.

Part: SWITCH — OUT OF ADJUST (THRUST REVERSER) · airframe 18,167 hrs · 15,432 cycles

R REV UNLOCK MSG IN FLIGHT. ADJUSTED RT THRUST REV STOW SWITCH IAW CRJ 200 AMM 78-37-01. OPS CHECK GOOD. NO DEFECTS NOTED AT THIS TIME.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 18,155 hrs · 15,418 cycles

RT REV UNLOCKED CAUTION MSG EVERY 1 MIN TO 5 SEC INFLIGHT. INTERFERES W/SAFE OPERATION. RT T/R CHECKS GOOD IAW AMM 78-30-00. DEFER CLEARED.

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 17,357 hrs · 14,619 cycles

LT LOWER PLANK FUEL ACCESS HOLE AT WING STATION 12.245 HOLE NR 2 HAS FRETTING CORROSION WITH MINOR PITTING ON INBOARD AND OUTBOARD EDGE OF CUTOUT APPROX 0.002 DEEP AT WORST LOCATION IN A NON CRITICLAL REGION. REPAIRED IAW BOMBARDIER REO 601R57-21-030 H.

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 17,357 hrs · 14,619 cycles

LT LOWER PLANK FUEL ACCESS HOLE AT WING STATION 54.897 HOLE NR 1 HAS FRETTING CORROSION WITH MINOR PITTING ON INBOARD AND OUTBOARD EDGE OF CUTOUT APPROX. 0.002 DEEP AT WORST LOCATION IN A NON CRITICLAL REGION. REPAIRED IAW BOMBARDIER REO 601R57-21-030 H.

Part: SKIN — DAMAGED (LT WING) · corrosion level 2 · airframe 17,357 hrs · 14,619 cycles

LT LOWER PLANK FUEL ACCESS HOLE AT WING STATION 274.319 HOLE NR 14 HAS 3 EACH CHAFES ON INBOARD EDGE OF CUTOUT ON LIP MEASURING APPROX 0.145L X 0.025W X 0.002DEEP IN A NON CRITICAL REGION. REPAIRED IAW BOMBARDIER REO 601R-57-21-030 REV H.

Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 17,357 hrs · 14,619 cycles

RT LOWER PLANK FUEL ACCESS HOLD AT WING STATION 54.897 HOLE NR 1 HAS FRETTING CORROSION WITH MINOR PITTING ON INBOARD AND OUTBOARD EDGE OF CUTOUT APPROX 0.002 DEEP AT WORST LOCATION IN A NON CRITICAL REGION. REPAIRED IAW BOMBARDIER REO 601R57-21-030 H.

Part: BULKHEAD — DAMAGED (FUSELAGE) · airframe 17,357 hrs · 14,619 cycles

FS 621 BULKHEAD IS DAMAGED FROM SCREW CONTACT AT WL 102.5 LBL 17.5 AND 27. AREA APPEARS TO BE PREVIOUSLY REPAIRED. REPAIRED IAW BOMBARDIER REO 601R-53-61-2155.

Part: BULKHEAD — DAMAGED (BS 621) · airframe 17,357 hrs · 14,619 cycles

FS 621 BULKHEAD IS DAMAGED FROM SCREW CONTACT AT WL 86, RBL 7.5. DAMAGE IS APPROX 0.125" LONG X 0.125" WIDE X 0.003" DEEP. REPAIRED IAW REO 601R-53-61-2155.

Part: BULKHEAD — SCRATCHED (FUSELAGE) · airframe 17,357 hrs · 14,619 cycles

FS 621 BULKHEAD IS SCRATCHED AS WL 140, RBL 16. DAMAGE IS APPROXIMATELY .5" LONG X 0.010" WIDE X 0.003" DEEP. REPAIRED IAW BOMBARDIER REO 601R-53-61-2155.

Part: SKIN — DAMAGED (LT WING) · airframe 17,357 hrs · 14,619 cycles

LT LOWER WING PLANK TRAILING EDGE HAS SEVERAL SMALL TOOLING MARKS COVERING A 1 SQUARE AREA AT APPROX WS 294.50. WORST SINGLE MARKS MEASURES APPROX .25 L X .005 W X .005D. REPAIRED IAW SRM 57-21-31, AND 51-12-00.

Part: BULKHEAD — SCRATCHED (FUSELAGE) · airframe 17,357 hrs · 14,619 cycles

FS 621 BULKHEAD IS SCRATCHED AT WL 140, RBL 16. DAMAGE IS APPROXIMATELY .5" LONG X 0.010" WIDE X 0.003" DEEP. REPAIRED IAW BOMBARDIER REO 601R-53-61-2155.

Part: BULKHEAD — DAMAGED (FUSELAGE) · airframe 17,357 hrs · 14,619 cycles

FS 621 BULKHEAD IS DAMAGED DUE TO SCREW CONTACT AT WL 102.5, RBL 17.5, 27, AND 36. REPAIRED IAW BOMBARDIER REO 601R-53-61-2155.

Part: ANGLE — DAMAGED (FUSELAGE) · airframe 17,357 hrs · 14,619 cycles

FS 621 BULKHEAD STIFFENER ANGLE IS DAMAGED FROM SCREW CONTACT ALONG THE TOP EDGE OF ANGLE WL 119.5 AT LBL 9, 17.5, 27, AND RBL 9. REPAIRED IAW SRM 53-00-00, AND 52-12-00.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 17,357 hrs · 14,619 cycles

FS 621 IS DAMAGED DUE TO SCREW CONTACT AT WL 102.5, RBL 9 AND RBL 7.5. DAMAGE IS APPROXIMATELY 0.003 INCH DEEP. REPAIRED IAW BOMBARDIER REO 601R-53-61-2155.

Part: STRUCTURE — CHAFED (RT WING) · airframe 17,357 hrs · 14,619 cycles

CHAFE BETWEEN WING LOWER AFT SKIN PLANK AND MLG FAIRING AT RBL 45 MEASURING 0.030" DEEP IN ZONE "A". REPAIRED IAW BOMBARDIER REO 601R-57-21-880 REV B.

Part: STRUCTURE — CHAFED (WING) · airframe 17,357 hrs · 14,619 cycles

CHAFE BETWEEN WING LOWER AFT SKIN PLANK AND MLG FAIRING AT RBL45 MEASURING 0.030" DEEP IN ZONE "A". REPAIRED IAW BOMBARDIER REO 601R-57-21-880 REV B.

Part: COWLING — OPEN (NR 2 ENGINE) · airframe 17,034 hrs · 14,315 cycles

THE CORE COWLS OF THE NR 2 ENGINE CAME OPEN DURING FLIGHT AND THE TRANSLATING COWLS WERE SUBSEQUENTLY ALSO DAMAGED WHEN THE THRUST REVERSERS WERE DEPLOYED UPON LANDING. BOMBARDIER REO 601R-71-12-4046 WAS ISSUED TO INSPECT THE COWLS FOR FERRY FLIGHT FOR PERMANENT REPAIR.

Part: LANDING GEAR — MALFUNCTIONED (LEFT) · airframe 16,722 hrs · 14,023 cycles

GEAR DISAGREE ON FINAL RT MAIN WAS RED DURING APPROACH 3 PREVIOUS FLTS IT TOOK LONGER FOR IT TO COME DOWN THAN OTHER GEAR RAN QRH CYCLED GEAR ALL CAME DOWN NORMAL. PERFORMED OK CHECK OF LANDING GEAR SYS BY PERFORMING GEAR SWING IAW AMM 32-30-00 AND C/W PA 05-018A OP CHECKED GOOD. OK FOR SERVICE.

Part: IDG — LACK OF LUBE (RIGHT) · airframe 16,509 hrs · 13,827 cycles

GEN 2 OFF CAUTION ON TAKEOFF ROLL. SERVICED RT IDG IAW CRJ AMM 12-13-24. RECONNECTED IDG AND OPS CHECKED NORMAL PER CRJ AMM 24-10-00. OK FOR SERVICE.