N8775A

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 30,803 hrs · 28,434 cycles

FLOOR LEVEL EMERGENCY PATH LIGHTING INOP FROM RAW 6-FORWARD TO ROW 1 DEFERRED CABIN EMER LIGHT IAW MEL33-57-1A PLACARD INSTALLED ENTERED IN MMO2 PER MOC 96074. $$$$$$$ REMOVED & REPLACED EMRGENCY LIGHT BATTERY AT PS2LF AND FLOOR LIGHTING STRIP DS13LX #2 AND LEFT FLOOR EMER EXIT LIGHT DS14LY IAW CRJ200 AMM 33-51-04 DEFER CLEARED MM02 UPDATED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,075 hrs · 27,680 cycles

DURING ROUTINE CHECK FOUND EMERGENCY FLOOR TRACK LIGHTS 2ND,3RD, AND 4TH STRIPS FROM FWD CABIN GOING AFT INOP. REMOVED AND REPLACED EMERGENCY FOOR TRACK LIGHT STRIPS IAW AMM 33-51-01 OPS CHECK GOOD NO FURTHER DEFECTS NOTED P/N 36262-4

Part: LIGHT — INOPERATIVE (ROWS 2-3 CD) · airframe 30,048 hrs · 27,651 cycles

FLOOR STRIP (EMERGENCY LED STRIPS) OUT ON ROWS 2CD AND 3CD. RESECURED FLOOR TRACK EMERG LIGHT IAW CRJ 200 AMM 33-51-01. OPS TEST PASSED IAW CRJ 200 AMM 33-51-00. NO FAULTS AT THIS TIME.

Part: FLOOR SUPPORT — CORRODED (BS 559-574) · airframe 29,972 hrs · 27,574 cycles

AFT CABIN FLOOR SUPPORT STRUCTURE-TIE DOWN BEAM TOP CAP CORRODED FROM STA-559+80 TO STA-574, RIGHT SIDE OUTBOARD BEAM RBL 27. REMOVED CORROSION BY BLENDOUT AND FOUND TO BE WITHIN LIMITS IAW BOMBARDIER REO 601R-53-00-005 REV: B STA 559+86 (.050" ORIGINAL - .031" MIN REMAIN - .030" MIN ALLOWED) STA 559+93 (.050" ORIGIANAL - .036" MIN REMAIN - .030MIN ALLOWED) INSTALLED NEW REPAIR ANGLE AT STA 559 + 98 IAW BOMBARDIER REO 601R-53-00-027 REV: D.

Part: SUPPORT BRACKET — DEFECTIVE (LT MLG WW) · airframe 29,972 hrs · 27,574 cycles

LH MLG W/W BRAKE PRESSURE TRANSDUCER SUPPORT BRACKET IMPROPERLY FABRICATED, AND POORLY INSTALLED. ALL HDWR IS LOOSE. REMOVED AND REPLACED L/H MLG W/W BRAKE PRESSURE TRASDUCER SUPPORT BRKT IAW CRJ-200 SRM 51-41-02, 51-41-06. AAR SM 107

Part: SKIN — CHAFED (RT AILERON LE) · airframe 29,972 hrs · 27,574 cycles

RIGHT AILERON LOWER LEADING EDGE IS CHAFED. REMOVED RIGHT AILERON LOWER LEADING EDGE SKIN AND INSTALLED A NEW SECTION OF SKIN IAW SRM 51-42-06 AND SRM 51-42-21.

Part: RETAINER — CRACKED (PANEL) · airframe 29,972 hrs · 27,574 cycles

UPON SEAL REMOVAL ,FOUND PANEL 422AT SEAL RETAINER CRACK (REQUIRE NEW RETAINER AND NEW SEAL) REMOVED/REPLACED DAMAGED SEAL RETAINER IAW CRJ 200 SRM 51-42-06 AAR SM 58

Part: SHIELD — CHAFED · airframe 29,972 hrs · 27,574 cycles

PANEL 422DB HAS CHAFED AREA PANEL RACK REMOVED AND REPLACED DIVIDERS ON PANEL 422DB IAW CRJ 200 SRM 51-42-06.

Part: FLOOR SUPPORT — CORRODED (AFT CABIN) · airframe 29,972 hrs · 27,574 cycles

AFT CABIN FLOOR SUPPORT STRUCTURE IN CARGO COMPT. -BEAM TOP CAP CORRODED AT RIGHT OUTBOARD BEAM AFT END REMOVED DAMAGE IAW CRJ 200 EA CRJ253-09094 AND EA CRJ253-09102.

Part: SUPPORT — CRACKED (CARGO DOOR) · airframe 29,972 hrs · 27,574 cycles

CARGO DOOR FWD. TRACK SUPPORT STRUCTURE CRACKED AT LOWER END OF TRACK REPLACED BRACKET IAW CRJ 200 SRM 51-42-06 AAR SM 109

Part: ANGLE — CRACKED (PAX DOOR) · airframe 29,972 hrs · 27,574 cycles

PAX DOOR LWR EDGE MEMBER IS CRACKED AT PREVIOUS REPAIR REPAIRED PREVIOUS REPAIR ANGLE ON PAX DOOR LWR EDGE MEMBER IAW REO 601R-52-11-279. AAR SM 107

Part: CARGO TRACK — CORRODED (BS 559) · airframe 29,972 hrs · 27,574 cycles

RBL27 CARGO TRACK AT FS599.0+94 HAS CORROSION. REMOVED AND REPLACED RBL27 CARGO TRACK AT FS559.0 + 94 IAW CRJ-200 AMM 53-00-49.

Part: SKIN — CRACKED (LT NACELLE) · airframe 29,972 hrs · 27,574 cycles

LH ENGINE LOWER CORE COWL 435AB FWD CORER AT HINGE SIDE IS DAMAGED. REPAIRED PANEL 435AB FWD CORER IAW CMM 71-12-01-300-826-A01.

Part: STRAP — CORRODED (BS 559) · airframe 29,972 hrs · 27,574 cycles

CORROSION ON STRAP AT STA 559 L/H OTBD. UNDER FLOOR PANEL 261DLF. REMOVED AND REPLACED STRAP AT STA 559 IAW CRJ-200 SRM 51-42-06. AAR SM 58

Part: WEB — CRACKED (PAX DOOR) · airframe 29,972 hrs · 27,574 cycles

PAX DOOR FWD WEB IS CRACKED AT LWR PART OF RISER FOR 832CT REPAIRED PAX DOOR FWD WEB AT LWR PART OF RISER FOR STEP 832CT IAW REO 601R-52-11-702. AAR SM 107

Part: CARGO TRACK — CORRODED (BS 559) · airframe 29,972 hrs · 27,574 cycles

RBL9 CARGO TRACK AT FS559.0+94 HAS CORROSION. REMOVED CORROSION AND LIMITS EXCEEDED REMOVED AND REPLACED PART RBL9 CARGO TRACK AT F.S. 559.0 + 94 IAW SRM 51-21-06, CRJ-200 AMM 53-00-49. AAR SM 107

Part: FLOOR SUPPORT — CORRODED (BS 559) · airframe 29,972 hrs · 27,574 cycles

AFT CABIN FLOOR SUPPORT STRUCTURE-SILL CORRODED AT STA-559+80 TO STA-559+96 RIGHT SIDE. BLENDED CORROSION IAW 51-21-06. INSTALLED REPAIR DOUBLER IAW EA CRJ253-09095 REV B.

Part: WEB — CRACKED (PAX DOOR) · airframe 29,972 hrs · 29,972 cycles

PAX DOOR AFT WEB IS CRACKED AT PREVIOUS REPAIR AT HANDRAIL STOW BRACKET REPAIRED PREVIOUS REPAIR PART AT HAND RAIL STOW BRACKET ON PAX DOOR AFT WEB IAW REO 601R-52-11-702. AAR SM 107

Part: SEAT TRACK — CONTAMINATED (SIDEWALL) · airframe 29,972 hrs · 27,574 cycles

SIDE WALL SEAT TRACK DIRECTLY FORWARD OF LAV IS CONTAMINATED BY BLUE JUICE. REMOVED AND REPLACED SEAT TRACK I.A.W. CRJ-200 AMM 53-01-11

Part: PANEL — CHAFED (PYLON) · airframe 29,972 hrs · 27,574 cycles

PYLON PANEL 412DB HAS 2EA. WORN SEPERATOR PANELS. REMOVED AND REPLACED SEPERATORS IAW SRM 51-42-06.

Part: PANEL — CHAFED (PYLON) · airframe 29,972 hrs · 27,574 cycles

PYLON PANEL 422DB HAS 2EA. WORN SEPERATOR PANELS. REMOVED AND REPLACED SEPERATORS ON PANEL 422DB IAW CRJ 200 SRM 51-42-06 AAR SM 58

Part: SEAT TRACK — CORRODED (CABIN) · airframe 29,972 hrs · 27,574 cycles

LEFT AISLE SEAT TRACK NEAREST THE LAV, IS CONTAMINATED BY BLUE JUICE AND PRESUMED TO BE CORRODED. REMOVED AND REPLACED SEAT TRACK I.A.W. CRJ-200 AMM 53-01-11 AAR SM 58

Part: SEAT TRACK — CORRODED (CABIN) · airframe 29,972 hrs · 27,574 cycles

LEFT AISLE SEAT TRACK #2 HAS CORROSION. REMOVED AND REPLACED LEFT AISLE SEAT TRACK # 2 IAW CRJ 200 AMM 53-01-11 AAR SM 58

Part: GUIDE — CHAFED (ACCESS PANEL) · airframe 29,972 hrs · 27,574 cycles

ACCESS PNL 597BB HAS LE CHAFING DAMAGE. REMOVED & RPLACED UNSERVICABLE GUIDE PLATE ON PNL 597BB IAW CRJ 200 SR IAW CRJ 200 SRM 51-42-06. RESTORED COATING IAW SRM 51-25-16.

Part: RUB STRIP — CHAFED (LT NACELLE) · airframe 29,972 hrs · 27,574 cycles

LEFT ENGINE COWL PANEL 432AB RUB STRIP KNIFE EDGED. REMOVED AND REPLACED RUB STRIP ON PANEL 432AB IAW CMM 71-14-01.

Part: BRACKET — CRACKED (THRUST REVERSER) · airframe 29,972 hrs · 27,574 cycles

L/H T/R UPPER TRACK HAS TWO EACH STANG FAIRING BROKEN/CRACKED. REMOVED DAMAGED BRACKETS FROM L/H T/T UPPER TRACK & INSTALLED NEW BRACKETS FOR STANG FAIRING IAW BOMBARDIER (SHORTS) CMM 20-42-06. AAR SM 33

Part: RUB STRIP — CHAFED (LT NACELLE) · airframe 29,972 hrs · 27,574 cycles

LEFT ENGINE COWL PANEL 432AT RUB STRIP KNIFE EDGED. REMOVED AND REPLACED RUB STRIP ON COWLING 432AT IAW BOMBARDIER CMM 71-14-01 AAR SM 58

Part: RUB STRIP — CHAFED (RT NACELLE) · airframe 29,972 hrs · 27,574 cycles

RIGHT ENGINE COWL PANEL 442AT RUB STRIP KNIFE EDGED. REMOVED AND REPLACED DAMAGED RUB STRIP WITH NEW RUB STRIP IAW BOMBARDIER CMM 71-14-01. AAR SM 58

Part: BPSU — FAILED (TE FLAP) · airframe 28,921 hrs · 26,445 cycles

FLAPS FAIL 0 DEGREES AT CRUISE 21,000 FEET. R&R RT BPSU IAW AMM 27-51-10, ALL CKS GOOD, OK FOR SVC.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 28,904 hrs · 26,426 cycles

FA JUMPSEAT FLASHLIGHT IS INOP. REMOVED AND REPLACED FA FLASHLIGHT IAW CMM 25-60-02. NO FURTHER DEFECTS AT THIS TIME.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,483 hrs · 25,990 cycles

SERVICE DOOR EMERGENCY LIGHT INOP. REMOVED AND REPLACED LIGHT BULB IN SERVICE DOOR EMERGENCY ASSY IAW AMM 33-51-21. OPS CHECK GOOD P/N OFF/ON 1317.

Part: BULB — INOPERATIVE (EMEGENCY LIGHT) · airframe 28,417 hrs · 25,916 cycles

CEILING EMERGENCY FLOOD LIGHT NR 3 WAS INOPERATIVE. REPLACED THE BULB IAW AMM 33-51-16. OP CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,250 hrs · 25,743 cycles

FLIGHT ATTENDANT INDICATION LIGHTS ON THE EMERGENCY EXIT SIGN ARE NOT WORKING. RESET THE EMERGENCY LIGHT CIRCUIT BREAKER IAW AMM 33-51-00. OPS CHECKED GOOD

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 28,241 hrs · 25,734 cycles

LIGHTED OVERHEAD EXIT SIGN IN CABIN HAS REAR BACKLIGHT INOPERATIVE. R & R THE SIGN ASSY IAW AMM 33-51-04. OPS CHECKED GOOD

Part: OIL SYSTEM — LOW PRESSURE (RT ENGINE) · airframe 27,971 hrs · 25,431 cycles

RIGHT ENGINE OIL PRESSURE MASTER WARNING DURING CRUISE POWER, OIL PRESSURE EICAS SHOWED AS LOW AS 15 PSI. R & R THE RT ENGINE OIL PUMP IAW AMM 79-21-03. R & R THE RT ENGINE OIL TRANSDUCER IAW AMM 79-31-05. R & R THE RT ENGINE OIL PRESSURE SWITCH IAW AMM 79-31-03. R & R THE RT ENG OIL FILTER BYPASS SENSOR IAW AMM 79-33-01. LEAK AND OPS CHECKED GOOD AND OIL CONSUMPTION RUN GOOD.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 27,215 hrs · 24,626 cycles

F/O FLASHLIGHT NOT FLASHING RED. REMOVED AND REPLACED THE FLASHLIGHT BATTERY. OPS CHECKED GOOD.

Part: HOSE — LEAKING (CREW OXYGEN) · airframe 26,800 hrs · 24,191 cycles

CREW OXYGEN HAS A LEAK. FOUND OXYGEN LEAK ON FLEX HOSE CONNECTED TO CREW OXYGEN BOTTLE MAIN SUPPLY. REMOVED AND REPLACED HOSE IAW AMM 35-11-00-01, SERVICED CREW OXYGEN TO 1800 PSI, LEAK NO LONGER EXISTS. ACFT OK FOR SERVICE

Part: HOSE — DAMAGED (OXYGEN MASK) · airframe 26,800 hrs · 24,191 cycles

FO'S OXYGEN MASK HAS A HOLE IN THE HOSE. REMOVED AND REPLACED THE FIRST OFFICER'S OXYGEN MASK IAW AMM 35-11-12. OPS AND LEAK CHECKED GOOD.

Part: SCAVENGE PUMP — INOPERATIVE · airframe 26,770 hrs · 24,160 cycles

AT LEVEL OFF 32000 FT, AT 250 KIAS RECEIVED A RT ENGINE LOW OIL PRESSURE & GAUGE INDICATED <20 PSI ALREADY & WAS STILL CREEPING DOWN. OIL TEMP WAS 110 C+/-5C BEFORE GOING TO IDLE R OIL TEMP WAS >85C. RAN QRH SHUT DOWN R ENGINE & LANDED UNSUCCESSFULLY 2 KMEM- NORMAL LANDING. NOTHING UNUSUAL SHOWN WITH VISUAL CHECK AROUND R ENGINE. OIL LEVEL CHECK A-OK. PERFORMED ENGINE AND T/S PER FIM 79-20-02 FOUND LOW OIL PRESSURE TRANSDUCER SWITCH CANNON PLUG LOOSE. TIGHTENED PLUG. PERFORMED MULTIPLE ENGINE STARTS WITH CREW. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. MOC NOTIFIED #98765. SEE AML 3365132-1 RH ENGINE LOW OIL PRESS MESSAGE, T/S PER MOTR/MOC. R/R RH ENGINE LUBE & SCAVENGE PUMP IAW AMM 79-21-01. OP CHECK & LEAK CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,586 hrs · 22,937 cycles

DURING WALK AROUND FOUND LEFT SIDE EMERGENCY LIGHT INOP. R&R EMER BULB IAW AMM 33-51-21.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 25,180 hrs · 22,529 cycles

STRONG ELECTRICAL ODOR IN CABIN, STRONGEST NEAR THE CEILING AFT OF ROW 5. R & R THE EMERGENCY LIGHT BATTERY PACK AT BS 439 & 499, AND BATTERY CHARGER ASSY. OPS CHECKED GOOD IAW AMM 33-51-04 & 33-51-05.

Part: SKIN — DENTED (FUSELAGE) · airframe 25,038 hrs · 22,397 cycles

2 DENTS ON LOWER FUSE SKIN AT STA 670 BETWEEN STR 27 AND STR 26 RT. REPAIRED DENTS IAW EA CRJ253-04381, REV A.

Part: HINGE — WORN (FUSELAGE) · airframe 25,038 hrs · 22,397 cycles

PASSENGER DOOR HINGE, FUSELAGE SIDE, FAILED FUNCTION TEST AND REQUIRES REPLACEMENT. REMOVED WORN HINGE HALF AND INSTALLED NEW HINGE HALF IAW SRM 53-21-23.

Part: ANGLE — CRACKED (PAX DOOR) · airframe 25,038 hrs · 22,397 cycles

PASSENGER DOOR POWER ASSIST MOUNTING ANGLE IS CRACKED. R & R PASSENGER DOOR POWER ASSIST MOUNTING ANGLE IAW SRM 51-42-06 AND SRM 51-40-11, S/M-107.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 25,038 hrs · 22,397 cycles

PASSENGER DOOR DRAG ANGLE CRACKED 97A002. COMPLIED WITH REPAIR REO 601R-52-11-513.

Part: FRAME — CORRODED (FUSELAGE) · airframe 25,038 hrs · 22,397 cycles

FRAME AT FS 605 IS CORRODED BETWEEN STR 21 RT AND 25 LT. REPAIRED CORRODED FRAME SECTION AT FS 605 IAW CRJ253-04369.

Part: GUIDE PLATE — WORN (PAX DOOR) · airframe 25,038 hrs · 22,397 cycles

PASSENGER DOOR UPPER FORWARD GUIDE PLATE IS WORN. REPLACED WORN GUIDE PLATE IAW SRM 51-42-10 AND 51-42-06.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 25,038 hrs · 22,397 cycles

SERVICE DOOR LOWER DOOR SILL IS CORRODED UNDER FWD AND AFT DOOR FITTINGS. REMOVED UNSERVICEABLE CORRODED SERVICE DOOR LOWER. SILL AND REPLACED IT WITH A SERVICEABLE NEW SILL, PN 601R-38303-253, TAG B84810 IAW SRM 51-42-21 & 51-42-06.

Part: GUIDE PLATE — WORN (PAX DOOR) · airframe 25,038 hrs · 22,397 cycles

PASSENGER DOOR UPPER AFT GUIDE PLATE IS WORN. REPLACED WORN GUIDE PLATE IAW SRM 51-42-06 AND 51-42-10.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 25,038 hrs · 22,397 cycles

CARGO FLOOR LT SILL HAS CORROSION ON TOP AND BOTTOM SURFACES FROM FS 559+112 - 621. REPAIRED CARGO FLOOR SILL FS 559+112-621 IAW REO 601R-53-61-690.

Part: BRACKET — CORRODED (CARGO BAY) · airframe 25,038 hrs · 22,397 cycles

CARGO COMP FWD CARGO NET ANCHOR BRACKET IS CORRODED. REMOVED, FABRICATED, LOCATED AND INSTALLED REPLACEMENT ANCHOR BRACKET IAW SRM 51-24-21, 51-40-01, AND 51-42-01.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 25,038 hrs · 22,397 cycles

IN MAIN CABIN LT SEAT TRACK, NR 1 HAS MULTIPLE AREAS OF CORROSION AND GOUGES. R & R LT NR 1 SEAT TRACK IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 25,038 hrs · 22,397 cycles

IN MAIN CABIN LT SEAT TRACK NR 2 HAS MULTIPLE AREAS OF CORROSION AND GOUGES. R & R NR 2 LT SEAT TRACK IAW AMM 53-01-11.

Part: FRAME — CORRODED (FUSELAGE) · airframe 25,038 hrs · 22,397 cycles

FRAME 319.70 HAS CORROSION ON THE FWD AND AFT SIDES BETWEEN STR 25L AND 25R, IN THE FWD ELECTRONIC AND EQUIPMENT BAY. R & R FRAME SECTION 319.70 BETWEEN STR 25L AND 25R IN FWD E & E BAY, PN 601R32003-61, TAG: B00355 IAW SRM 51-42-06 AND SRM 51-40-11.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 25,038 hrs · 22,397 cycles

LEFT CENTER POST LOWER WINDSHIELD BRACKET AT STA 202, WL 110.00 IS CRACKED. R & R LEFT CENTER POST BRACKET PN 601R33237-15, TAG. REPLACED BRACKET IAW SRM 51-42-21.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 25,038 hrs · 22,397 cycles

RT SIDE SEAT RAIL, NR 3 FROM FS 409+16 TO FS 409+112 HAS CORROSION. R & R NR 3 RT SIDE SEAT TRACK IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 25,038 hrs · 22,397 cycles

LEFT NR 5 SIDE SEAT RAIL FROM FS 449+85 TO FS 499.0 HAVE CORROSION. R & R LT 5 SIDE SEAT RAIL IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 25,038 hrs · 22,397 cycles

RT SIDE SEAT RAIL NR 8 FROM FS 559+16 TO FS 559+80 HAS CORROSION. R & R NR 8 SIDE SEAT TRACK IAW AMM 53-01-11.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 25,038 hrs · 22,397 cycles

FLT DECK FLOOR AFT LANDING IS CRACKED AT BOTH SIDES, ON THE FWD SIDE OF BEAM 280, JUST INBD OF LBL9 AND RBL 9, VIEWED FROM THE VERY FWD E & E BAY. R & R FLT DECK FWD LANDING BEAM BS 280 IAW SRM 51-42-21 AND SRM 51-42-06.

Part: STRIP — DAMAGED (NR 2 COWLING) · airframe 25,038 hrs · 22,397 cycles

NR 2 ENGINE LOWER FAN COWL HAS DAMAGE ON T/E. R & R AFT EDGE STRIP, PN: 228-50081-108, TAG: B76210 IAW CMM 71-14-01.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 25,038 hrs · 22,397 cycles

LBL 27, FLOORBEAM CAP HAS LIGHT CORROSION ON INBD AND OTBD FLANGED BETWEEN FS 559+112 -621. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. FABRICATED NEW BEAM CAP INSTALLED AND TREATED IAW SRM 51-21-06, 53-00-00, AND REO 601R-53-61-3778.

Part: FRAME — CRACKED (FUSELAGE) · airframe 25,038 hrs · 22,397 cycles

PASSENGER CABIN, FS 333, FRAME CRACKED AT S-1L. REPAIRED PASSENGER CABIN, FS 333, FRAME AT S-1L IAW REO 601R-53-21-2723.

Part: ATTACH BRACKET — CRACKED (FUSELAGE) · airframe 25,038 hrs · 22,397 cycles

PAX CABIN, PAX DOOR UPPER SILL ATTACH BRACKET CRACKED ABOVE AND BELOW S-3L AT FS 280. R & R INBD & OTBD BRACKETS AT PASSENGER DOOR ABOVE & BELOW S3L AT FS 280 IAW SRM 51-42-06, 51-42-21.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 25,038 hrs · 22,397 cycles

RIGHT SIDE SEAT RAIL NR 4 BETWEEN 409+112 TO 449+85 HAS CORROSION. R & R NR 4 RT SIDE SEAT TRACK IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 25,038 hrs · 22,397 cycles

LEFT NR 4 SIDE SEAT RAILS HAVE CORROSION BETWEEN 409+112 TO FS 449+85. R & R NR 4 LT SIDE SEAT TRACK IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 25,038 hrs · 22,397 cycles

RT SIDE SEAT RAIL NR 7 FROM FS 544.0 TO FS 559+16 HAS CORROSION. R & R NR 7 RT SIDE SEAT TRACK IAW AMM 53-01-11.

Part: STRAP — CORRODED (FUSELAGE) · airframe 25,038 hrs · 22,397 cycles

FLOOR SUPPORT STRAP BETWEEN LBL9 AND LBL27 AT FS 589 IS CORRODED. REMOVED, FABRICATED, LOCATED. DRILLED AND INSTALLED REPAIR FLOOR STRAP, LBL9 TO LBL27, FS 589 IAW SRM 51-40-11 AND 51-42-06.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 25,038 hrs · 22,397 cycles

AFT EQUIPMENT BAY, CRACKED BRACKET AFT LT SIDE OF APB AT S-14L. R & R UNSERVICEABLE BRACKET AT AFT LT SIDE OF APB AT S-14L IAW SRM 51-42-21.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 25,038 hrs · 22,397 cycles

AFT PRESSURE BULKHEAD CRACKED AT LINTEL FITTING, WL 108 AND LBL 46. REPAIRED AFT PRESSURE BULKHEAD LINTEL FITTING CRACK AT WL 108, LBL 46 IAW REO 601R-53-61-1230.

Part: A/C PACK — OVERHEATED (LEFT) · airframe 24,684 hrs · 22,052 cycles

PILOT REPORTED VIBRATION FROM FLOOR & BURNING ODOR WITH PACKS ON. FOUND LEFT PACK OVERHEATED. R & R LEFT ACM IAW AMM 21-51-10. PERFORMED OPS TEST OF THE AIR CONDITIONING SYS AND FOUND UNSATISFACTORY IAW AMM 21-51-00-710-801. LEFT PRSOV REPLACED IAW AMM 21-51-43. OPEN

Part: LIFE VEST — UNSERVICEABLE (CABIN) · airframe 24,655 hrs · 22,025 cycles

1 INFANT LIFE VEST HAS HOLE IN BAG. R & R 1 INFANT LIFE BEST IAW PA 25-096A.

Part: ROLLER — OUT OF ADJUST (PAX DOOR) · airframe 24,422 hrs · 21,804 cycles

PAX DOOR WILL NOT OPEN. ADJUSTED PAX DOOR INNER HANDLE ROLLER IAW AMM 52-11-00, CHECKED GOOD. OK FOR SERVICE.

Part: CONNECTOR — BROKEN (CABIN) · airframe 27,658 hrs · 24,454 cycles

EMERGENCY LIGHT STRIP CONNECTOR BROKEN AT PANEL 261ALF. R & R EMERGENCY LIGHT STRIP CONNECTOR AT PANEL 261ALF IAW ESPM 20-17-31. OPERATIONS CHECKED GOOD IAW AMM 33-51-00-710-801.

Part: POWER CABLE — FAULTY (CABIN) · airframe 24,380 hrs · 21,764 cycles

ORANGE STRIP AT SEAT 1C OF EMERGENCY EXIT FLOOR PATH LIGHTING INOPERATIVE. R & R POWER CABLE FOR FRONT EMERGENCY EXIT FLOOR PATH IAW AMM 33-51-01, OPERATIONS CHECKED GOOD.

Part: PIN — ICED (MAIN DOOR) · airframe 24,015 hrs · 21,419 cycles

MAIN DOOR WOULD NOT OPEN DUE TO ICE ON PINS. DE-ICED & OPERATIONS CHECKED PAX DOOR IAW AMM 52-11-00. OPERATIONS CHECKED GOOD, OK FOR SERVICE.

Part: UNKNOWN — ODOR (GALLEY) · airframe 23,856 hrs · 21,253 cycles

GALLEY HEAT AND GALLEY LIGHTS PRODUCING A BURNING ODOR WHEN TURNED ON FULL. OPS CHECKED GALLEY LIGHTS IAW AMM 33-26-00. OPS CHECKED GALLEY HEAT IAW AMM 21-23-05, NO BURNING ODOR NOTICED.

Part: MANIFOLD — DAMAGED (APU FUEL) · airframe 23,726 hrs · 21,128 cycles

WITH APU RUNNING THERE IS AN ODOR LIKE JET FUEL WITH PACKS ON. REMOVED AND REPLACED APU PRIMARY FUEL MANIFOLD IAW AMM 49-31-07 OPS AND LEAK CHECKED GOOD.

Part: UNKNOWN — ODOR (CABIN) · airframe 23,640 hrs · 21,039 cycles

INTERMITTENT FUEL ODOR. RAN A/C WITH BOTH ENGINES, SINGLE ENGINE, AND WITH JUST APU. NO FUEL ODOR NOTED FROM EITHER PACK IAW AMM 21-51-00. ACFT OK FOR SERVICE. NOTED NO LEAKS IN AFT EQUIPMENT BAY.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHT) · airframe 23,032 hrs · 20,436 cycles

EMERGENCY EXIT FLOOR PATH LIGHTS VERY DIM FROM ROW 2 TO ROW 6. R & R ROW 2 TO 5 POWER STRIP & POWER CONNECTOR IAW AMM 33-51-01. OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE · airframe 22,998 hrs · 20,403 cycles

CARGO BOTTLE TEST 2 WILL NOT LIGHT UP THE CARGO SMOKE PUSH RED PUSH BUTTONS ON LOWER PANEL. PERFORMED OPS CHECK OF THE CARGO FIDEX SYSTEM. CARGO FIDEX WORKS AS REQUIRED IAW AMM 26-25-00. ACFT RETURNED TO SERVICE.

Part: CONTROL UNIT — FAILED (NLG STEERING) · airframe 22,941 hrs · 16,277 cycles

STEERING INOPERATIVE CAUTION MESSAGE AFTER PUSH BACK. R & R STEERING ELECTRONIC CONTROL UNIT IAW AMM 32-51-10. PERFORMED AN OPERATIONAL TEST IAW 32-51-10. OPS TEST GOOD AT THIS TIME.

Part: STEERING SYS — FAILED · airframe 22,868 hrs · 20,278 cycles

NOSE WHEEL STEERING FAILED, RESET IN AIR AND FAILED AGAIN ENROUTE. EMERGENCY DECLARED. R & R RT STEERING RVDT, ADJUSTED RUDDER RVDT. PERFORMED OPS CHECK OF NOSE WHEEL STEERING, OPS CHECKED NORMAL. NOSE WHEEL STEERING DISCONNECTED ON GROUND. RIGGED LT & RT STEERING RVDT’S, R & R STEERING HAND CONTROL MODULE. OPS CHECK NORMAL.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 22,829 hrs · 20,235 cycles

SMELLED A BURNING ODOR IN COCKPIT. INSPECTED AIR CONDITION SYSTEM IAW AMM 21-51-00, NO DEFECTS NOTED. OK FOR SERVICE.

Part: FIRE BOTTLE — NO TEST (CARGO BAY) · airframe 22,767 hrs · 20,173 cycles

NR 2 CARGO FIRE BOTTLE WILL NOT TEST WARNING.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 22,665 hrs · 20,072 cycles

EMERGENCY PATH LIGHTS CENTER SECTION INOPERABLE. REMOVED AND REPAIRED NR 3 EMERGENCY BATTERY STATIC INVERTER IAW AMM 33-51-07. ALL OPERATIONS NORMAL.

Part: BULKHEAD — CHAFED (FUSELAGE) · airframe 22,536 hrs · 19,949 cycles

FORWARD FACE OF FS 621 PRESSURE BULKHEAD SKIN IS CHAFED UNDER FIRE BLOCK. REPAIRED IAW BOMBARDIER REO 601R-53-61-2155.

Part: FITTING — CRACKED (FUSELAGE) · airframe 22,536 hrs · 19,949 cycles

FS 484 CLIPS CRACKED AT LBL 27 AND LBL 36. REPAIRED IAW BOMBARDIER REO 601R-53-41-059.

Part: FITTING — CRACKED (FUSELAGE) · airframe 22,536 hrs · 19,949 cycles

FS 484 CLIP CRACKED AT LBL 27. REPAIRED IAW BOMBARDIER REO 601R-53-41-059.

Part: FITTING — CRACKED (CARGO BAY) · airframe 22,535 hrs · 19,949 cycles

LOWER CLIP ON CARGO DOOR SUPPORT STRUCTURE CRACKED. REPAIRED IAW SRM SRM 51-42-21/51-40-11/51-25-16.

Part: FITTING — CRACKED (FUSELAGE) · airframe 22,536 hrs · 19,949 cycles

RIGHT FS 484 CLIP CRACKED AT RBL 36. REPAIRED IAW BOMBARDIER REO 601R-53-41-059.

Part: LANDING GEAR — MALFUNCTIONED (NOSE) · airframe 21,291 hrs · 18,733 cycles

FLIGHT 3691, RECEIVED "HYD 3 LO PRESS" CAUTION MESSAGE AND GEAR DISAGREE" WARNING MESSAGE AFTER TAKEOFF. NOSE GEAR INDICATED DOWN AND BOTH MAIN GEAR HAD RED DASHES FOR ABOUT 2 MINUTES HYD 3 SYSTEM SHOWS 100 PERCENT AND 3000 PSI. GEAR CAME DOWN NORMALLY. AIR RETURNED. BLED NR 3 HYDRAULIC SYSTEM IAW AMM TASK 29-10-00-810-803, COMPLIED WITH PA 05-018G SCENARIO 1. COMPLIED WITH FUNCTIONAL TEST OF EXTENSION AND RETRACTION SYSTEM IAW AMM 32-30-00-720-801. OPS CHECKED GOOD. APPROVED FOR RETURN TO SERVICE. AIRCRAFT OK FOR SERVICE.

Part: WIRE — DISCONNECTED (CABIN) · airframe 20,404 hrs · 17,813 cycles

MCD - WHITE EMERGENCY LIGHT STRIP INOP TAPPED COVER, NO CHANGE. RECONNECTED WIRE CONNECTORS FOR LIGHT STRIP NEAR PAX DOOR IAW ESPM AND OPS CHECKED LIGHT IAW AMM 33-51-19. NO DEFECTS NOTED.

Part: SPOILER SYS — MALFUNCTIONED · airframe 20,139 hrs · 17,587 cycles

INBOARD GROUND SPOILER" AND "OUTBOARD GROUND SPOILER" CAUTION MESSAGES ON TOUCHDOWN. TRIED "MAN ARM" TO DEPLOY MANUALLY, BUT THEY DID NOT DEPLOY. AFTER FLAP RETRACTION, THE MESSAGES WENT AWAY, AND RECEIVED "IB & OB GND SPOILER FAULT" STATUS MESSAGES ON ED2. FOUND CB'S 4A4 & 5 PULLED. PUSHED IN CB'S AND OPS CHECKED SPOILERS IAW AMM 27-61-00. OPS CHECKED NORMAL. ACFT OK FOR SERVICE.

Part: PUMP — DEFECTIVE (HYDRAULIC SYS) · airframe 20,016 hrs · 17,519 cycles

GEAR DISAGREE WARNING, HYD SYSTEM 3 LOW PRESSURE, DECLARED EMERGENCY. THREE GREEN GEAR DOWN. COMPLIED WITH PA05-018B GEAR DISAGREE EVENT PROCEDURES. REMOVED & REPLACED PUMP 3B PER CRJ AMM 29-12-03. OPS CHECK AND LEAK CHECK GOOD.

Part: THROTTLE CABLE — BINDING (RT ENGINE) · airframe 20,012 hrs · 17,517 cycles

DURING ENGINE START, 2 APPEARED TO BE A HUNG START 2 DID START BUT WHEN ADVANCING THE THRUST LEVER, THERE SEEMS TO BE BINDING AND POSSIBLY SOMETHING RESTRICTING EITHER LEVER ADVANCEMENT OR SPOOL OF ENGINE. C/W FIM 76-11-00 FIGURE 101 AND FOUND RT AFT THROTTLE CABLE FAILED FUNCTION TEST. FOUND RT AFT THROTTLE CONTROL CABLE AND RT ENGINE THROTTLE CONTROL CABLE BINDING. REMOVED AND REPLACED RT AFT THROTTLE CONTROL CABLE IAW AMM 76-11-07 AND REMOVED AND REPLACED RT ENGINE THROTTLE CONTROL CABLE FROM GEARBOX IAW AMM 76-11-09. REMOVED AND REPLACED SHUTOFF VALVE, GEARBOX, THROTTLE CABLE AND RED HARNESS ON RT SIDE. REFERENCE NON-ROUTINE CARD #13548. CHECKED RT ENGINE THROTTLE CABLE RIG IAW AMM 76-11-00. CHECKS NORMAL. PERFORMED OPS CHECK OF RT ENGINE THROTTLE CABLES IAW AMM 76-11-00.

Part: PRIORITY VALVE — FAILED (NLG DOORS) · airframe 19,830 hrs · 17,283 cycles

GEAR DISAGREE. COMPLIED WITH PA 05-18B GEAR DISAGREE EVENT PROCEDURES COMPLIED WITH WO325993. PSEU CODES INDICATED NOSE DOORS DID NOT OPEN. R & R NLG PRIORITY VALVE IAW AMM 32-33-15. OPS CHECKED GOOD. LEAK CHECKED GOOD.

Part: UNKNOWN — MALFUNCTIONED (LANDING GEAR) · airframe 19,814 hrs · 17,271 cycles

GEAR DISAGREE ON APPROACH, NOSE GEAR DIDN’T EXTEND ON FIRST ATTEMPT, CREW RECYCLED GEAR AND NOSE GEAR CAME DOWN. COMPLIED WITH PA 05-018B GEAR DISAGREE EVENT PROCEDURES. NO FAULT FOUND. PERFORMED OPERATIONAL TEST OF LANDING GEAR EXTENSION AND RETRACTION SYS IAW AMM 32-30-00. NO FAULTS FOUND THIS CLEARS DM 53536, PLACARD REMOVED. OK FOR SERVICE.

Part: CABLE — OBSTRUCTED (ELEVATOR) · airframe 19,720 hrs · 17,180 cycles

PREVIOUS ISSUE WITH ELEVATOR HAS RETURNED CAPT ELEV DOESN’T MOVE WHEN F/O PULLS BACK ON YOKE. FOUND DISC CABLE HANGING ON SAFETY WIRE ON 2 WSRSWITCH REMOVED OBSTRUCT. OPS CHECKED IAW AMM 31-31-06 CHECK GOOD.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 19,591 hrs · 17,046 cycles

F/A FLASHLIGHT DOES NOT FLASH. REMOVED AND REPLACED F/A'S FLASHLIGHT BATTERY IAW AMM 25-61-04. OPS CHECK GOOD. VERIFIED PART EFFECTIVITY.

Part: BULKHEAD — DAMAGED (FUSELAGE) · airframe 19,375 hrs · 16,837 cycles

FS 559 BULKHEAD FAILED NDT WITH INDICATION ON WEB AT RBL 18 GREATER THAN 50 PERCENT FSH. REPAIRED IAW BOMBARDIER REO 601R-53-41-260 REV E AND BOMBARDIER REO 601R-53-41-609 REV B DEVIATION "E".

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 19,375 hrs · 16,837 cycles

FS 559 BULKHEAD FAILED NDT WITH CRACK INDICATION ON RIGHT WEB RBL 18 GREATER THAN 50 PERCENT FSH. REPAIRED IAW BOMBARDIER REO 601R-53-41-260 REV E AND REO 601R-53-41-609 REV B DEVIATION "E".

Part: STRUT — LOW PRESSURE (NLG) · airframe 19,228 hrs · 16,710 cycles

STATION LEFT GND AIR DOOR OPEN AIR RETURN FOUND NOSE GEAR EXTREMELY LOW. SERVICED NOSE STRUT IAW AMM 12-12-32. NO LEAKS DETECTED. OK FOR SERVICE. C/W PA 05-018B GEAR DISAGREE EVENT PROCEDURES AND CRJ FIM 32-60-09.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 18,640 hrs · 16,234 cycles

THE 621 PRESSURE BULKHEAD CRACKED 1.5 INCHES ABOVE CARGO DOOR TRACK AT LBL 27.5 AND WL 130. REPAIRED IAW BOMBARDIER REO 601R-53-61-1541.

Part: UNKNOWN — MALFUNCTIONED (AUTOPILOT SYS) · airframe 18,646 hrs · 16,191 cycles

UNCOMMANDED CLIMB OCCURED WITH AUTOPILOT ENGAGED, REPORTED BY CREW. DFDR WAS PERFORMED & SENT TO ENGINEERING.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 18,082 hrs · 15,641 cycles

ANTI-ICE DUCT WARNING MSG ON CLIMBOUT OF ATL AND EN ROUTE STANDBY SEEMS TO WORK OK PERFORMED ENGINE RUNS IAW AMM 71-00-00 WING ANTI ICE SYS OPS CK'S GOOD IAW AMM 30-11-00.

Part: SPLICE — DAMAGED (ANIT-ICE SYSTEM) · airframe 18,082 hrs · 15,641 cycles

ANTI-ICE DUCT WARNING MSG INFLIGHT AFTER TAKEOFF. REPAIRED SPLICE & TIGHTEN LOOSE GROUND. OPS CHECK GOOD IAW AMM 30-11-00.

Part: UPLOCK — LEAKING (RT MLG) · airframe 17,733 hrs · 15,292 cycles

RIGHT MAIN GEAR DISAGREE ON DEPARTURE. RAN QRH GOT 3 GREEN AND RETURNED. REMOVED AND REPLACED RT MLG UPLOCK IAW AMM 32-32-05. OPC GOOD. NEEDS GEAR SWING. REF AML DISC NR 1. PERFORMED GEAR SWING IAW AMM 32-30-00. C/W PA 05-018A. OPC GOOD. OK FOR SERVICE.

Part: HINGE — CORRODED (PAX DOOR) · corrosion level 2 · airframe 17,672 hrs · 15,235 cycles

PASSENGER DOOR TOP STEP HINGE AT THRESHOLD CORRODED. REMOVED AND REPLACED HINGE IAW CRJ 200 SRM 51-41-00.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,672 hrs · 15,235 cycles

FLOOR SEAT TRACK AT RBL 9 AND RBL 27 BETWEEN FS 559.00+64 AND FS 559.00+96 LEVEL 2 CORRODED. REMOVED SEAT TRACK AT RBL 9 AND RBL 27 BETWEEN FS 559.00+64 AND FS 559.00+96. INSTALLED NEW SEAT TRACK IAW CRJ 200 SRM 51-41-04, BSC EO 601R-53-19655 AND CRJ 200 AMM 53-01-11-400-802.

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 17,672 hrs · 15,235 cycles

LT LOWER PLANK FUEL ACCESS HOLE AT WS 12.245 HOLE NR 2 HAS CORROSION ON INBOARD EDGE OF CUTOUT MEASURE APPROXIMATELY .003 INCH DEEP NOT IN CRITICAL AREA. REPAIRED LT LOWER FUEL ACCESS HOLE AT WS 12.245 HOLE NR 2 ON INBOARD EDGE OF CUTOUT NOT IN CRITICAL AREA IAW BOMBARDIER REO 601R-57-21-030, REV H. TOTAL MATERIAL REMOVED IS .004 INCH, WHICH LEAVES A PLANK THICKNESS OF .182.

Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 17,672 hrs · 15,235 cycles

RT LOWER PLANK FUEL ACCESS HOLE AT WS 54.897 HOLE NR 1 HAS CORROSION ON INBOARD EDGE OF CUTOUT MEASURE APPROXIMATELY .002 INCH DEEP NOT IN CRITICAL AREA. REPAIRED RT LOWER FUEL ACCESS HOLE AT WS 54.897 HOLE NR 1 ON INBOARD EDGE OF CUTOUT NOT IN CRITICAL AREA IAW BOMBARDIER REO 601R-57-21-030, REV H. TOTAL MATERIAL REMOVED IS .005 INCH, WHICH LEAVES A PLANK THICKNESS OF .184 INCH.

Part: RETAINER — CORRODED (E&E DOOR) · corrosion level 2 · airframe 17,664 hrs · 15,227 cycles

AVIONICS DOOR SEAL RETAINERS HAVE CORROSION. REMOVED AND REPLACED 4EA SEAL RETAINERS, P/N'S CC670-38662-5, CC670-38675-3, CC670-38674-3, AND CC670-38663-5, FROM AVIONICS DOOR IAW CRJ-200 SRM 51-42-06 AND 51-23-00.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,664 hrs · 15,227 cycles

PASSENGER DOOR SILL PLATE ANGLE INCURRED LEVEL 2 CORROSION FROM FS 319 TO FS 349. REMOVED AND REPLACED PASSENGER DOOR SILL PLATE ANGLE.

Part: SEAT TRACK — CORRODED (BS 559) · corrosion level 2 · airframe 17,672 hrs · 15,235 cycles

CABIN FLOOR SEAT RAIL AT RBL 9 FROM FS 559.00+48 TO FS 559.00+86 IS CORRODED. REMOVED AND REPLACED CABIN FLOOR SEAT TRACK AT RBL 9 FROM FS 559.00+48 TO FS 559.00+86 IAW CRJ 200 AMM 53-01-11-400-802 AND REO 601R-53-19632.

Part: COMPUTER — MALFUNCTIONED (LANDING GEAR) · airframe 16,930 hrs · 14,558 cycles

PROX SYS FAULT WHITE STATUS MESSAGE DURING CLIMBOUT RESET PROX SYS COMPUTER CHECKS GOOD IAW AMM 32-60-00. OK FOR SERVICE.

Part: THRUST REVERSER — MALFUNCTIONED (ENGINE) · airframe 16,603 hrs · 14,258 cycles

AFTER REACHING CRUISE ALTITUDE ON A FLIGHT FROM KPNS TO KMEM, THE R REV ICON ON THE N1 GAUGE BEGAN TO FLICKER, FOLLOWED BY A R REV UNLOCKED CAUTION MESSAGE. THE FLIGHT CREW PERFORMED THE QRH AND INFORMED CENTER AND THE COMPANY DISPATCHER. THE AIRCRAFT WAS DIVERTED TO THE NEAREST SUITABLE AIRPORT. AN OTHERWISE NORMAL APPROACH AND LANDING WAS MADE AT KJAN. MAINTENANCE INSPECTED THE AIRCRAFT, DEFERRED THE RT THRUST REVERSER AND RELEASED THE AIRCRAFT FOR SERVICE PER THE MEL.

Part: SELECTOR VALVE — MALFUNCTIONED (NLG)

GEAR DISAGREE WHEN GEAR SELECTED DOWN ON APPROACH INTO DTW, QRH FOLLOWED DECLARED EMERGENCY, UNEVENTFUL LANDING. REMOVED AND REPLACED NOSE LANDING GEAR SELECTOR VALVE IAW AMM OPERATIONAL AND LEAK CHECK PERFORMED WITH NO DEFECTS. (A)

Part: SMOKE DETECTOR — MALFUNCTIONED (LAVATORY)

SMOKE TOILET MESSAGE ON FINAL. LANDING UNEVENTFUL. PERFORMED OPERATIONAL TEST OF LAV SMOKE SYSTEM, IAW AMM AND OF THE LAV SMOKE DETECTOR IAW AMM. BOTH OPS CHECK GOOD. (K)

Part: G SWITCH — FAILED (ELT)

ELT FAILS G-SWITCH TEST. REMOVED IAW PA 25-048D AND FAR PART 91.207 FOR REPAIR. REMOVED ELT FOR MAINTENANCE IAW FAR 91.207. (K)