N422AW

Part: LIGHT — INOPERATIVE (CABIN) · airframe 33,601 hrs · 31,922 cycles

DURING FIRST FLIGHT ACCEPTANCE INSPECTION CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHTING WAS INOPERATIVE FROM ROW 1-5.

Part: DOWNLOCK SENSOR — FAILED (NLG) · airframe 33,583 hrs · 31,902 cycles

AFTER CLIMB OUT REC GEAR DISAGREE WARNING, NLG RED HASHES RAN QRH MSGS CLEARED RETURNED TO DEPARTURE IAW QRH. MESSAGES RECEIVED AT AROUND 7,000 FT AND 250 KTS GEAR WAS UP SLOWED TO C/W QRH WHEN HYD 2 AND 3B SEL ON MSG CLEARED. HYDS WERE IN AUTO AND INDICATIONS NORMAL. PSEU FAULT CODE S35 NEAR. REMOVED AND REPLACED NR 2 NLG DOWNLOCK SENSOR PER AMM 32-61-05. OPS CHECKED GOOD.

Part: DOOR — LACK OF LUBE (MAIN PAX) · airframe 33,361 hrs · 31,688 cycles

PAX DOOR WILL NOT OPEN FROM THE OUTSIDE. LUBRICATED PAX DOOR IAW SUP 15-053. OPS CHECKED GOOD.

Part: DOOR — LACK OF LUBE (MAIN PAX) · airframe 33,361 hrs · 31,688 cycles

PAX DOOR WILL NOT OPEN FROM OUTSIDE. LUBRICATED PAX DOOR PER 15-053. OPS CHECKED GOOD.

Part: ROLLER — DAMAGED (PAX DOOR) · airframe 32,895 hrs · 31,250 cycles

NUMBER 1 PAX DOOR VERY DIFFICULT TO MOVE TO THE OPEN POSITION FROM THE OUTSIDE. FOUND INSIDE HANDLE ROLLER DAMAGED, ROLLER HAS MULTIPLE FLAT SPOTS CAUSING ROLLER TO HANG UP IN DETENT. REPLACED THE ROLLER ON THE INNER PAX DOOR HANDLE RETENTION MECHANISM IAW AMM 52-11-21. BOTH INNER & OUTER DOOR HANDLES OPERATIONS CHECKED GOOD.

Part: FUEL — LEAKING (APU) · airframe 32,756 hrs · 31,117 cycles

FLIGHT 3914, 3930 STRONG FUEL ODOR COMING FROM THE PACKS. NOTED FUEL LEAK AROUND APU FUEL MANIFOLD & FILTER AREA. WIPED EXCESS FUEL IAW 299136 4 FOR MEL. DID NOT SMELL USING ENG BLEED AIR.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,420 hrs · 30,802 cycles

FLIGHT 3791 EMER LIGHTS ROW 1 INOPERATIVE & UNSECURE. R & R EMER LIGHT COVER IAW AMM 33-51-01. OPERATIONS CHECKED GOOD AT THIS TIME.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,149 hrs · 30,551 cycles

EMERGENCY FLOOR TRACK LIGHT ROW 5 - 7 ARE NOT WORKING;.

Part: ROD — OUT OF ADJUST (SERVICE DOOR) · airframe 36,234 hrs · 34,122 cycles

GALLEY SERVICE DOOR DIFFICULT TO OPEN FROM INSIDE & OUTSIDE. ADJUSTED UPPER STABILIZER ROD IAW AMM 52-41. OPERATIONS CHECKED GOOD. REMOVED PLACARD & FROM MEL.

Part: ROD — OUT OF ADJUST (SERVICE DOOR) · airframe 36,227 hrs · 34,115 cycles

CREW REPORTED SERVICE DOOR DIFFICULT TO OPEN AFTER UNLATCHING HANDLE INSIDE & OUTSIDE OF ACFT. INSPECTED DOOR FOR SAFETY & SECURITY. PLACED SERVICE DOOR ON MEL 52-21-01. REPOSITIONED ACFT TO MAKE FOR REPAIR. MX ADJUSTED UPPER STABILIZER ROD IAW AMM 52-41.

Part: SEAL — TORN (GALLEY DOOR) · airframe 36,195 hrs · 34,084 cycles

GALLEY SERVICE DOOR DIFFICULT TO OPEN & CLOSE. INSPECTED GALLEY SERVICE DOOR & FOUND LOWER AFT SECTION TORN IN TWO PLACES APPROX 1" LONG. R & R SERVICE DOOR SEAL, INSPECTED & OPERATED SERVICE DOOR, VERIFIED DOOR OPERATES, CLOSES & LOCKS NORMALLY.

Part: MOUNT BRACKET — CRACKED (FUSELAGE) · airframe 36,030 hrs · 33,934 cycles

EXTERNAL SERVICE INSTRUMENT PANEL, LOWER ANGLE MOUNTING BRACKET IS CRACKED, REPLACED.

Part: MOUNT BRACKET — CRACKED (FUSELAGE) · airframe 36,030 hrs · 33,934 cycles

AC POWER RECEPTACLE MOUNT BRACKET IS CRACKED AT THE FWD FASTENER HOLE, REPLACED.

Part: SUPPORT — CRACKED (SPOILER SYS) · airframe 36,030 hrs · 33,934 cycles

SPOILER ADAPTER OTBD SUPPORT CRACKED, REPLACED.

Part: BRACKET — CHAFED (FUSELAGE) · airframe 36,030 hrs · 33,934 cycles

BRACKET FOR RT BRAIDED HYD LINE RUNNING THRU INTERCOSTAL AT STRINGER 9R, BETWEEN FRAMES 645 & 672 IN THE AFT EQUIPMENT BAY IS CHAFED, REPAIRED.

Part: INTERCOSTAL — CRACKED (PAX DOOR) · airframe 36,030 hrs · 33,934 cycles

PASSENGER DOOR AFT UPPER INTERCOSTAL CRACKED, REPLACED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,030 hrs · 33,934 cycles

SEAT TRACK ON RBL 9 HAS CORROSION, BETWEEN FS 559+80 & FS 559+96 IN THE CARGO BAY. R & R SEAT TRACK IAW AMM 53-01-11.

Part: DRAG ANGLE — CRACKED (RT MLG WW) · airframe 36,030 hrs · 33,934 cycles

RIGHT MLG WW DRAG ANGLE FWD MOUNT STRUCTURE IS CRACKED. R & R RT MLG WW DRAG ANGLE FWD MOUNT STRUCTURE IAW EA 30-2015-523 & AWAC SUPPLEMENT 15-287.

Part: INTERCOSTAL — CRACKED (CARGO DOOR) · airframe 36,030 hrs · 33,934 cycles

CARGO DOOR LOWER AFT VERTICAL MEMBER IS CRACKED FROM TOP TO BOTTOM, CRACK 6" LONG. R & R CARGO DOOR LOWER AFT VERTICAL MEMBER, INTERCOSTAL, IAW SRM 51-42-06 & 51-42-21.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,030 hrs · 33,934 cycles

ON RBL 27, THE OTBD FLOOR LANDING HAS CORROSION, BETWEEN FS 605.0 & FS 621.0, IN THE CARGO BAY. REMOVED CORRODED FLOORBEAM CAP & REPLACED WITH NEW SERVICEABLE BEAM CAP IAW EA 40-2015-229 ISSUED 11 10 15.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,030 hrs · 33,934 cycles

SEAT TRACK ON LBL 9, BETWEEN FS 559+112 & 574.00 HAS CORROSION, IN THE CARGO BAY. R & R SEAT TRACK, PN 601R38779-5, ON LBL 9, BETWEEN FS 559+112 & 574.00 IAW AMM 53-01-11.

Part: DRAG ANGLE — CRACKED (RT MLG WW) · airframe 36,030 hrs · 33,934 cycles

RIGHT MLG WW DRAG ANGLE COMMON TO BAT RIB IS CRACKED IN THE AFT RADIUS. R & R RT MLG DRAG ANGLE COMMON TO BAT RIB IAW SRM 51-42-21.

Part: SKIN — CHAFED (FUSELAGE) · airframe 36,030 hrs · 33,934 cycles

FUSELAGE SKIN IS CHAFED NEXT TO PREVIOUS REPAIR CUT OUT, JUST FWD OF PAX DOOR OPENING & JUST ABOVE WL 79.50. REPAIRED FUSELAGE SKIN JUST FWD OF PAX DOOR OPENING & JUST ABOVE WL 79.50 IAW REO 601R-53-21-180 REV A.

Part: SUPPORT BRACKET — CRACKED (AC BAY) · airframe 36,030 hrs · 33,934 cycles

RIGHT DUEL HEAT EXCHANGER, SUPPORT BRACKET CLIP IS CRACKED. R & R CRACKED BRACKET ON RT DUEL HEAT EXCHANGER SUPPORT WITH SERVICEABLE FABRICATED BRACKET IAW SRM 51-42-06, 51-11-20.

Part: SKIN — CRACKED (FUSELAGE) · airframe 36,030 hrs · 33,934 cycles

LOWER FWD FUSELAGE SKIN AT NLG AFT DOOR CUT OUT, AFT RT RADIUS IS CRACKED. REPAIRED DAMAGED FUSELAGE SKIN CRACK AT NLG CUT OUT, AFT RADIUS RT SIDE IAW REO 601R-53-11-048 REV D.

Part: WEB — CRACKED (RT WING) · airframe 36,030 hrs · 33,934 cycles

RIGHT WING OTBD LE WEB IS CRACKED, BETWEEN ACCESS PANELS 630KZ & 630LZ. R & R RT OTBD LE WEB, BETWEEN ACCESS PANELS 630KZ & 630LZ IAW SRM 51-42-13.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,030 hrs · 33,934 cycles

SMALL SEAT TRACK ON LBL9, JUST FWD OF THE AFT PRESS BULKHEAD HAS CORROSION, IN THE CARGO BAY. R & R SMALL SEAT TRACK, PN 601R31032-51 ON LBL 9, JUST FWD OF THE AFT PRESS BULKHEAD IAW AMM 53-01-11.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 36,030 hrs · 33,934 cycles

APU ENCLOSURE SUPPORT STRUCTURE, RT FWD VERTICAL POST AFT ATTACH ANGLE CRACKED. R & R CRACKED ANGLE FROM RT VERTICAL POST AFT SIDE OF FWD POST OF APU ENCLOSURE WITH SERVICEABLE ANGLE IAW SRM 51-42-13 & 51-11-20.

Part: DRAG ANGLE — CRACKED (LT MLG WW) · airframe 36,030 hrs · 33,934 cycles

LEFT MLG WW DRAG ANGLE FWD MOUNT STRUCTURE IS CRACKED. R & R LT MLG WW DRAG ANGLE FWD MOUNT STRUCTURE IAW EA 30-2015-523 & SUP 15-287.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 36,030 hrs · 33,934 cycles

APU ENCLOSURE SUPPORT STRUCTURE, RT AFT ATTACH ANGLE SUPPORT BRACKET CRACKED. REMOVED CRACKED ATTACH ANGLE ON APU SUPPORT STRUCTURE, RT AFT SIDE & REPLACED WITH NEW SERVICEABLE BRACKET PN 601-97049-2 IAW SRM 51-42-06.

Part: FRAME SPLICE — BENT (FUSELAGE) · airframe 36,031 hrs · 33,934 cycles

FRAME SPLICE AT FS 736.00, STRINGER 6L - 7L BENT.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,030 hrs · 33,934 cycles

FLOORBEAM 589 CAP HAS CORROSION ON THE TOP SIDE, BETWEEN RBL 27 & THE RT FLOOR SILL, REPLACED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,030 hrs · 33,934 cycles

RIGHT AISLE SEAT TRACK STICK NR 3 HAS CORROSION, BETWEEN 409+128 & 559, REPLACED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,030 hrs · 33,934 cycles

RIGHT AISLE SEAT TRACK STICK NR 1 HAS CORROSION, BETWEEN FS 364 & 394, REPLACED.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 36,030 hrs · 33,934 cycles

PLATFORM SKIN IS CRACKED NEXT TO ADG RETRACTION PUMP, OTBD SIDE AT FRAME CUT OUT, REPAIRED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,030 hrs · 33,934 cycles

RIGHT AISLE SEAT TRACK STICK NR 4 HAS CORROSION, BETWEEN FS 559 & 559+96, REPLACED.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,030 hrs · 33,934 cycles

FLOORBEAM 559+80 CAP HAS CORROSION ON THE TOP SIDE, BETWEEN LBL 9 & RBL 9, REPLACED.

Part: FITTING — CRACKED (FUSELAGE) · airframe 33,031 hrs · 33,934 cycles

INBOARD CLIP ON STRINGER 3L CRACKED AT FS 280, IN CABIN.

Part: FITTING — CRACKED (FUSELAGE) · airframe 33,031 hrs · 33,934 cycles

OUTBOARD CLIP ON STRINGER 3L CRACKED AT FS 280, IN CABIN.

Part: STRIP — MISINSTALLED (CABIN) · airframe 31,300 hrs · 29,724 cycles

FLIGHT 3737, 3884 EMER FLOOR TRACK LIGHTING ARROWS POINT BACKWARDS, LAST SECTION. FOUND EMER FLOOR AFT STRIP BY LAVATORY INSTALLED INCORRECTLY. REINSTALLED EMER FLOOR LIGHT STRIP IAW AMM 33-51-01. OPERATIONS CHECKED GOOD ARROWS POINT IN CORRECT POSITION.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,703 hrs · 29,153 cycles

FLIGHT 3862, STRIP OF EMERGENCY FLOOR LIGHT NOT WORKING ROW 12. REPLACED ROW 12 FLOOR TRACK EMERGENCY STRIP IAW AMM 33-50. OPERATIONS CHECKED GOOD.

Part: ACTUATOR — FAILED (TE FLAPS) · airframe 34,668 hrs · 32,600 cycles

WHEN SELECTING FLAPS FROM 8 DEG TO 20 DEG, AT 17 LT & 15 RT INDICATED, FLAPS FAILED. COMPLIED WITH FLAP CIRCUIT BREAKER RESET. ON 3RD RETRACTION FLAPS FAILED WHEN SELECTED TO 20 DEG, INDICATION LT 22 & RT 20, FELT SLIGHT RUMBLE WHEN FAILED. FOUND LT NR 3 FLAP ACTUATOR BINDING. R & R ACTUATOR IAW MM 27-53-05. OPERATIONS CHECKED GOOD AT THIS TIME.

Part: CONNECTOR — MISSING (EMEGENCY LIGHT) · airframe 30,318 hrs · 28,780 cycles

REQUIRES INSPECTION OF FLOOR TRACK LIGHTING AT ROW 1D-F, PULLED FROM FLOOR BY PAX. INSPECTED FLOOR TRACK LIGHTING AT ROW 1 D & F, FOUND TRACK PULLED UP FROM FLOOR & CONNECTORS & CONNECTORS MISSING. SECURED WIRE WITH TAPE IAW 280733 3 FOR OPEN WRITE UP FOR FERRY FLIGHT.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 29,419 hrs · 27,914 cycles

ON TAKEOFF SELECTED GEAR UP & RECEIVED GEAR DISAGREE WARNING. COMPLIED WITH QRH & MSG CLEARED. GEAR EXTENDED NORMALLY ON EXTENSION.

Part: DRAG ANGLE — CRACKED (LT MLG) · airframe 31,196 hrs · 26,998 cycles

LEFT MLG DRAG ANGLE IS CRACKED, COMMON TO UPPER SKIN. R & R ANGLE IAW SRM 51-46-11 & 51-42-21.

Part: FRAME — CORRODED (BS 310) · airframe 31,196 hrs · 26,998 cycles

FS 310 FRAME HAS CORROSION. R & R FRAME SEGMENT.

Part: FRAME — CORRODED (BS 319) · airframe 31,196 hrs · 26,998 cycles

FS 319 FRAME CORRODED. R & R LWR FRAME SEGMENT.

Part: FRAME — CORRODED (BS 333) · airframe 31,196 hrs · 26,998 cycles

FS 333 FRAME CORRODED. R & R FRAME SEGMENT.

Part: FRAME — CORRODED (BS 349) · airframe 31,196 hrs · 26,998 cycles

FS 349 FRAME CORRODED. R & R FRAME SEGMENT.

Part: POST — CRACKED · airframe 31,196 hrs · 26,998 cycles

VERTICAL POST IS CRACKED AT 409+128 AND LBL 27 AT THE BOTTOM OF THE POST. REPAIRED IAW REO 601R-53-41-1734.

Part: CHANNEL — CRACKED (LT MLG WW) · airframe 31,196 hrs · 26,998 cycles

LEFT MLG WHEEL WELL AFT CHANNEL IS CRACKED AND BENT. REPAIRED LT MLG WHEEL WELL AFT CHANNEL IAW STS EA 15-20-13-447, REV A.

Part: FLOOR SUPPORT — CORRODED (BS 409-559) · airframe 31,196 hrs · 26,998 cycles

LEFT FLOOR SUPPORT CORRODED FROM FS 409+128 TO 559. BLEND TO ALLOWABLE LIMITS IAW REO 601R-53-41-1732, REV A.

Part: FAIRING — CRACKED (TAIL PIPE) · airframe 31,196 hrs · 26,998 cycles

RT ENGINE TAIL PIPE FAIRING IS CRACKED AT DRAIN LINE MOUNT. PERFORMED FILLER & DOUBLER REPAIR IAW STS EA 15-20-13-441.

Part: STRIKER — GOUGED (SERVICE DOOR) · corrosion level 2 · airframe 31,196 hrs · 26,998 cycles

SERVICE DOOR LOWER SEAL STRICKER HAS GOUGES. REMOVED AND INSTALLED A NEW SERVICE DOOR LOWER SEAL STRIKER.

Part: FLOOR SUPPORT — CORRODED (BS 310-320) · corrosion level 2 · airframe 31,196 hrs · 26,998 cycles

RT FLOOR SUPPORT CORRODED AT FS 310 TO 320. REMOVED FLOOR SUPPORT AND REPLACED IAW SRM 51-42-21.

Part: FLOORBEAM — CORRODED (BS 349) · corrosion level 2 · airframe 31,196 hrs · 26,998 cycles

FASTENERS ARE CORRODED IN FLOOR SUPPORT STRUCTURE AT FS 349 AND BETWEEN RBL 27 AND RBL 36. REMOVED THE FASTENERS CORROSION SPREAD TO THE FS 349 BEAM CUT OUT DAMAGE THEN INSTALLED A FILLER & DOUBLER IAW EA 15-2013-449. REMOVED THE FLOOR SILL AT FS 310-349 TO FOM CORROSION WAS FOUND NEW SEAL FABRICATED AND INSTALLED IAW 51-40-11 AND 51-42-21.

Part: ATTACH ANGLE — CRACKED (PAX DOOR) · airframe 31,196 hrs · 26,998 cycles

PAX DOOR CLOSING PLATE AFT ATTACH ANGLES ARE CRACKED. REMOVED CRACKED ANGLES DUPLICATED & INSTALLED NEW SERVICEABLE ANGLES.

Part: SKIN — DENTED · airframe 31,196 hrs · 26,998 cycles

LEFT MLG INNER SKIN IS DENTED AND CHAFED INBD OF DATA PLATE. R & R INNER SKIN REF FORM 412.

Part: PANEL — CORRODED (BS 310-349) · corrosion level 2 · airframe 31,196 hrs · 26,998 cycles

PANEL 832ET ASSY HAS CORROSION ON HINGE AND PACKER ON VISOR PANEL. REMOVED UNSERVICEABLE HINGE PACK AND REPLACED WITH SERVICEABLE HINGE AND PACKER.

Part: SILL — CORRODED (BS 319-349) · corrosion level 2 · airframe 31,196 hrs · 26,998 cycles

PAX DOOR SILL HAS CORROSION ON PROXIMITY SENSOR. REPAIRED PAX DOOR LOWER SILL IAW SRM TR 53-27, 51-42-21, 51-42-26, 51-42-65, 51-42-02, 51-41-02, 52-20-04, 50-17-00.

Part: SKIN — DENTED (BS 640) · airframe 31,196 hrs · 26,998 cycles

THREE DENTS IN FUSELAGE SKIN AT FS 640 BETWEEN STR 26 - 27R. ACCOMPLISHED OUT OF DAMAGE AREA AND INSTALLED DOUBLER IAW REO 601R-53-61-5046, REV A.

Part: PANEL — CORRODED · corrosion level 2 · airframe 31,196 hrs · 26,998 cycles

PANEL 832ET ASSY HAS CORROSION ON ALUMINUM STRIP ON VISOR PANEL ASSY. REMOVED UNSERVICEABLE PANEL AND REPLACED WITH SERVICEABLE PANEL.

Part: CLEAT — CORRODED (BS 319-330) · corrosion level 2 · airframe 31,196 hrs · 26,998 cycles

FWD & AFT CLEATS ON PAX DOOR LOWER SILL CORRODED. REMOVED CLEATS AND REPLACED WITH NEW.

Part: MOUNT — CORRODED (BS 319-332) · corrosion level 2 · airframe 31,196 hrs · 26,998 cycles

CORROSION ON INBD SIDE OF PAX DOOR SILL ON CONNECTOR PLUG MOUNTING BLOCKS. R & R IAW SRM DAMAGE BEYOND SERVICEABLE LIMITS.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 31,196 hrs · 26,998 cycles

FS 280 FLOORBEAM CRACKED AT INBD & OTBD OF LBL 9 & RBL9. R & R IAW SRM 53-21-43,51-42-21, 51-42-06, 51-40-11, 51-21-11, 51-25-06, 51-25-16, REO 601R-53-11-171.

Part: SKIN — DENTED (BS 333-349) · airframe 31,196 hrs · 26,998 cycles

SKIN DENTED BETWEEN FS 333-349. REPAIR IAW REO 601R-53-21-2468.

Part: BRACKET — CRACKED (BS 672) · airframe 31,996 hrs · 26,998 cycles

ADEL CLAMP MOUNT BRACKET FOR DUCT FWD OF EMERGENCY RAM AIR SHUTOFF VALVE CRACKED. REMOVED UNSERVICEABLE ADEL CLAMP MOUNT BRACKET AND REPLACED WITH SERVICEABLE ADEL CLAMP MOUNT BRACKET.

Part: STEP — CORRODED (PAX DOOR) · corrosion level 2 · airframe 31,196 hrs · 26,998 cycles

PAX DOOR LWR FOLDING STEP HAS CORROSION ON UNDER OTBD EDGE. CORROSION FOUND TO BE OUT OF LIMITS, REPAIRED NEW STEP, PN 601R31980-67.

Part: BRACKET — CORRODED (LAVATORY) · corrosion level 2 · airframe 31,196 hrs · 26,998 cycles

AFT LAVATORY LED LIGHT ATTACH STRUCTURE CORRODED. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00. R & R WITH SERVICEABLE BRACKET IAW SRM 51-41-02.

Part: FLOOR SUPPORT — CORRODED (BS 559-574) · corrosion level 2 · airframe 31,996 hrs · 26,998 cycles

RIGHT FLOOR SUPPORT CORRODED FROM FS 559+80 TO FS574, REPAIRED RT FLOOR SUPPORT IAW STS EA 15-2013-446.

Part: FLOOR SUPPORT — CORRODED (BS 621) · airframe 31,996 hrs · 26,998 cycles

FLOOR SUPPORT CORRODED ATR FASTENER HOLE FS 621 & LBL 18. CUTOUT CORRODED SECTION AND INSTALLED FILLER AND STRAP IAW REO 601R-53-61-5051.

Part: ATTACH ANGLE — CRACKED (RT WING) · airframe 31,196 hrs · 26,998 cycles

RIGHT WING INBD L/E O/C ATTACH ANGLE ON WING IS CRACKED. REPLACE IAW SRM 51-40-11, 51-41-02 AND 51-21-11.

Part: DRAG ANGLE — CRACKED (BS 529-559) · airframe 31,196 hrs · 26,998 cycles

RIGHT DRAG ANGLE AT BATTERY RIB IS CRACKED. REMOVED RT DRAG ANGLE SHOWING CRACKED AFTER FURTHER EVALUATION, NO CRACK NDTM 51-20-06. THERE WAS SLITE CORROSION BOTH FWD & AFT ENDS BLENDED 1 EA RT DRAG ANGLE IAW SRM 51-12-00 ORIG MAT .100. REMOVED .005 REMAINING .095 WITHIN LIMITS IAW SRM 57-00-00.

Part: MOUNT — CRACKED (BS 489-499) · airframe 31,196 hrs · 26,998 cycles

NR 3 HYD RESERVOIR IN WHEEL WELL AFT MOUNT IS CRACKED. REMOVED 1 EA AFT MOUNT IAW SRM 51-42-06. REQUIRED CONDUCTIVITY C/W IAW SRM 51-16-20, MAT .10 FABRICATED IAW SAMPLE IAW SRM 51-15-00 & SRM 51-11-20. INSTALLED A NEW AFT MOUNT IAW SRM 51-42-10.

Part: BRACKET — CRACKED · airframe 31,196 hrs · 26,998 cycles

ADEL CLAMP MOUNT BRACKET FOR PNEUMATIC LINE ON TOP OF ENGINE BOX BEAM OTBD BROKEN OFF. REMOVED UNSERVICEABLE BRACKET AND INSTALLED SERVICEABLE ADEL CLAMP MOUNT BRACKET.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 31,196 hrs · 26,998 cycles

LEFT L/E CENTER PICCOLO TUBE BRACKET OTBD CRACKED. R & R LT L/E CENTER PICCOLLO TUBE BRACKET OTBD WITH SERVICEABLE IAW SRM 51-40-11, SRM 51-41-02.

Part: FITTING — CRACKED (WINDSHILED) · airframe 31,196 hrs · 26,998 cycles

RT WINDSHIELD SIDE POST LOWER OTBD FITTING IS CRACKED. REPLACED FITTING IAW SRM.

Part: RIB — CRACKED (LEFT) · airframe 31,196 hrs · 26,998 cycles

LEFT BATTERY RIB IS CRACKED IN LT WHEEL WELL. DOUBLER REPAIR IAW REO 601R-57-51-046, REV B.

Part: RIB — CRACKED · airframe 31,196 hrs · 26,998 cycles

RIGHT BATTERY RIB IS CRACKED. PERFORM DOUBLER REPAIR IAW REO 601R-57-51-046, REV B.

Part: ANGLE — CRACKED (BS 484) · airframe 31,196 hrs · 26,998 cycles

RIGHT INBD AND OTBD BS 484 ANGLES ARE CRACKED. REMOVED DAMAGED ANGLES AND INSTALLED FABRICATED ANGLES IAW REO 601R-53-41-059, REV B.

Part: ANGLE — CRACKED (BS 484) · airframe 31,196 hrs · 26,998 cycles

LEFT INBD BS 484 ANGLE IS CRACKED. R & R ANGLE IAW REO 601R-53-41-059, REV B.

Part: FAN — CONTAMINATED · airframe 24,081 hrs · 22,743 cycles

DISPLAY COOL CAUTION MESSAGE IN FLIGHT, WOULD NOT CLEAR WHEN STANDBY FAN SELECTED. MESSAGE CLEARED IN STBY WHEN DESCENDING THROUGH 8000`. FOUND DEBRIS INSIDE NR 2 DISPLAY FAN, CLEANED DEBRIS. INSTALLED FAN. OPS CHECKED GOOD AT THIS TIME. NO MESSAGE NOTED IAW MM 21-24-19.

Part: HANDLE — LACK OF LUBE (PAX DOOR) · airframe 23,554 hrs · 22,235 cycles

EXTERNAL PAX DOOR HANDLE WILL NOT WORK. POPS OUT BUT DOES NOT ROTATE. LUBED PAX DOOR. OPS CHECKED GOOD IAW AWAC SUPP 52-11-00.

Part: HANDLE — LACK OF LUBE (PAX DOOR) · airframe 27,221 hrs · 25,358 cycles

PAX DOOR EXTERNAL HANDLE WILL NOT TURN TO UNLOCK DOOR. LUBED PAX DOOR OUTER HANDLE IAW AMM 52-10-00. OPS CHECK GOOD.

Part: MOTOR — FAILED (E/E BAY FAN) · airframe 22,677 hrs · 21,326 cycles

PILOT REPORTS BAD ODOR IN GALLEY/COCKPIT AREA. DURING INVESTIGATION OF ODOR, FOUND CBP1-C5 POPPED AND WILL NOT RESET. R & R AVIONICS EXHAUST FAN IA AMM 21-24-28. OPS CHECKED GOOD. ODOR FROM FAN BURNED MOTOR.

Part: A/C PACK — SMOKE · airframe 22,144 hrs · 20,801 cycles

WHEN SWITCHING FROM ENG AIR TO APU, BOTH PACKS PRODUCED SMOKE IN CABIN/COCKPIT. OPERATED BOTH PACKS USING ENG AIR, CLEARED DUCT CONTAMINATION USING AWAC SUPP 09-037A PROCEDURE. AT THIS TIME NO ODOR OR SMOKE IN CABIN USING ENGINE AIR.

Part: FLOORBEAM — CRACKED (FS 589) · airframe 26,539 hrs · 24,678 cycles

FLOORBEAM STRUCTURE AT FS 589 UNDER BAGGAGE DOOR SILL CRACKED IN 2 EA AREAS. REPAIRED FLOORBEAM STRUCTURE AT FS 589 IAW REO 601R-53-61-4229.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 26,539 hrs · 24,678 cycles

FLOOR SUPPORT UNDER FLOORBOARD 281JLF ON LBL27 AND LBL9 HAS CORROSION AROUND SCREW HOLES. R & R LBL27 IAW SRM 51-42-06, REPAIRED LBL 9 IAW SRM 53-00-43.

Part: SKIN — CRACKED (PAX DOOR) · airframe 26,539 hrs · 24,678 cycles

PAX DOOR INNER SKIN IS CRACKED IN HANDLE RADIUS CUT OUT. R & R PAX DOOR LOWER INNER SKIN WITH SERVICEABLE INNER SKIN IAW SRM 51-42-06, 51-42-10 AND MODSUM IS 601R52110030, REV B.

Part: HINGE — GOUGED (PAX DOOR) · airframe 26,539 hrs · 24,678 cycles

PAX DOOR HINGE GAS A DEEP GOUGE IN THE PAX DOOR HALF. BLENDED GOUGE OUT IN PAX DOOR HINGE HALF IAW REO 601R-52-11-1347.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 26,539 hrs · 24,678 cycles

DENT WITH TWO GOUGES LT FLAP LOWER SURFACE INBD HINGE ARM. REPAIRED IAW REO 601R-52-1792.

Part: INTERCOSTAL — CRACKED (PAX DOOR) · airframe 26,539 hrs · 24,671 cycles

INTERCOSTAL BEHIND PAX DOOR PANEL 832RR IS CRACKED. REMOVED CRACKED PAX DOOR INTERCOSTAL BEHIND PANEL 832RR THEN INSTALLED NEW INTERCOSTAL IAW SRM 51-41-11, 51-42-06.

Part: DOOR FRAME — CRACKED (BS 338) · airframe 26,539 hrs · 24,678 cycles

PAX DOOR FRAME 338.00 CRACKED. LOCATED NEAR UPPER TORQUE TUBE 601R-52-11-402, REV H. REPAIRED PAX DOOR FRAME AT 338.00 IAW B/A REO 601R-52-11-402, REV H.

Part: STEP — UNKNOWN (PAX DOOR) · airframe 26,539 hrs · 24,678 cycles

PAX DOOR STEP 832ET. REMOVED AND INSTALLED SERVICEABLE HINGE.

Part: TRANSCOWL — CHAFED (THRUST REVERSER) · airframe 26,539 hrs · 24,678 cycles

RT LOWER TRANSCOWL HAS CHAFE DAMAGE AT AFT POINT. REPAIRED DAMAGE TO RT LOWER TRANSCOWL AFT OF HINGE POINT IAW REO 601R-78-33-3969.

Part: STIFFENER — CHAFED (FS 625) · airframe 26,539 hrs · 24,678 cycles

CHAFE IN VERTICAL STIFFENER OF FRAME STATION 625 VERTICAL STIFFENER AT RBL .06 DOWN FROM TOP BLENDED CHAFED AREA IAW REO 601R-53-61-1523. FOUND THAT IT WAS WITHIN ALLOWABLE LIMITS OF REO 601R-53-61-1523.

Part: SKIN — CHAFED (WS 47.61) · airframe 26,539 hrs · 24,678 cycles

LOWER WING SKIN OTBD FWD OF LT & RT WHEEL WELLS HAVE CHAFING DAMAGE CAUSED BY FWD FAIRING. REPAIRED IAW REO 601R-53-21-880, REV C.

Part: ANGLE — CRACKED (FS 621- 625.3) · airframe 26,539 hrs · 24,678 cycles

RT SIDE BULKHEAD FROM REAR FACING FWD HAS OBLIQUE ANGLE CRACKED. R & R RT SIDE OBLIQUE ANGLE WITH NEW IAW REO 601R-53-61-422.

Part: ANGLE — CRACKED (BS 621-635.3) · airframe 26,539 hrs · 24,678 cycles

LT SIDE BULKHEAD FROM REAR FACING FWD HAS OBLIQUE ANGLE CRACKED AS MARKED. R & R LT SIDE BULKHEAD OBLIQUE WITH NEW IAW REO 601R53-61-422.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 26,539 hrs · 24,678 cycles

CORROSION ON LAST 2 EA CARGO TRACKS, RBL 9 IN BAGGAGE AREA. REMOVED CARGO TRACKS, LOCATED AND DRILLED SERVICEABLE CARGO TRACKS IAW SRM 51-40-11. INSTALLED IAW 53-01-11, AMM SUB TASK 53-01-11-944-01.

Part: LUG — CHAFED (RT WING TE FLAP) · airframe 26,539 hrs · 24,678 cycles

AFT LUGS FOR RT INBD HINGE ARM ATTACH POINTS ARE GOUGED AND CHAFED BLEND AREA IAW REO 601R-57-52-1536.

Part: VANE — CHAFED (RT WING TE FLAP)

RIGHT INBD FLAP VANE CHAFED WHERE IT CONTACTS STOP. BLEND CHAFED AREA WITHIN ALLOWABLE LIMITS.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 26,539 hrs · 24,678 cycles

LT INBD FLAP VANE CHAFED WHERE IT CONTACTS STOP, BLEND CHAFED AREA WITHIN ALLOWABLE LIMITS.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 26,539 hrs · 24,678 cycles

TWO CARGO TRACKS LBL 9 IN BAGGAGE AREA. R & R CARGO TRACKS IAW SRM 51-40-11, 53-01-11. SUB TASK 53-01-11-944-011.

Part: SKIN — CORRODED (PAX DOOR) · corrosion level 2 · airframe 26,539 hrs · 24,678 cycles

FWD CORNER OF PAX DOOR AT DRAINAGE RAMP AREA IN CORRODED AND HAS DOUBLE DRILLED HOLE. REMOVED UNSERVICEABLE FWD CORNER OF PAX DOOR AT DRAINAGE AREA AND INSTALLED SERVICEABLE CORNER AT PAX DOOR FWD CORNER IAW SRM 51-42-06.

Part: SEAT TRACK — CORRODED (CARGO COMP) · airframe 26,539 hrs · 24,678 cycles

LAST SEAT TRACK ON LBL 27 IN BAGGAGE AREA HAS CORROSION. REMOVED SEAT TRACK . LOCATED AND DRILLED SERVICEABLE SEAT TRACK AND INSTALLED IAW AMM 53-01-11.

Part: ATTACH FITTING — CORRODED (PAX DOOR) · airframe 26,539 hrs · 24,678 cycles

FIVE CLIPS EA CORRODED AT DRAINAGE RAMP AREA OF PAX DOOR. REMOVED 5 EA UNSERVICEABLE CLIPS FROM PAX DOOR DRAINAGE RAMP INSTALLED 5 SERVICEABLE CLIPS IAW SRM 51-42-06.

Part: A/C PACK — SMOKE (RIGHT) · airframe 25,763 hrs · 23,858 cycles

RIGHT PACK UNCONTROLLABLE IN AUTO AND MANUAL, LOW AIR FLOW FROM RT PACK WITH A SMOKIE HAZE IN CABIN. R & R AIR CYCLE MACHINE.

Part: WARNING LIGHT — FALSE ACTIVATION (PAX DOOR) · airframe 25,456 hrs · 23,545 cycles

AT FL310, THE PASSENGER DOOR OUTER HANDLE CAUTION MESSAGE APPEARED. COMPLIED WITH QRH, MESSAGE PERSISTED AFTER INNER HANDLE PULLED. DIVERTED, MESSAGE CLEARED AT 10,000 FT. CLEANED HANDLE AND INTERROGATED PSU, FOUND DI-13 FAULT CLEARED, PERFORMED OPS CHECK AND PRESSURE OF ACFT IAW FIM 52-11-03 AND AMM 212200 OPS CKS GOOD. REMOVED PLACARD AND MEL.

Part: HANDLE — INOPERATIVE (PAX DOOR) · airframe 23,450 hrs · 21,429 cycles

UNABLE TO OPEN PAX DOOR FROM OUTSIDE HANDLE WILL NOT ROTATE. C/A IN PROGRESS.

Part: STRIP — CHAFED (LT NACELLE) · airframe 17,039 hrs · 15,980 cycles

LT UPPER NOSE COWL AFT EDGE STRIP IS CHAFED. R & R STRIP ON LT ENGINE UPPER NOSE COWL AFT EDGE IAW BOM CMM 71-14-01.

Part: BULKHEAD — CRACKED (BS 202.75) · airframe 17,039 hrs · 15,980 cycles

FS 202 BULKHEAD CRACKED AT BRAKE CABLE. REPAIRED IAW REO 601R-53-11-563.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 17,039 hrs · 15,980 cycles

FS 280, FLOOR SUPPORT UPPER ANGLE CRACKED AT LBL 11.0. REPAIRED CRACKED FS 280, FLOOR SUPPORT ANGLE IAW REO REPAIR 601R-53-11-138, REV NC.

Part: HANDLE — MALFUNCTIONED (PAX DOOR) · airframe 22,064 hrs · 20,021 cycles

PAX DOOR HANDLE CAUTION MSG AT FL 290. CW QRH AND DURING DOOR HANDLE STOW RECEIVED MASTER WARNING. CAS MSG WAS PAX DOOR. MSG CLEARED AFTER 2 SECONDS BUT PAX DOOR STOW MESSAGE WAS EVIDENT WHILE THE PLUNGER WAS PULLED. REF W/O 145933 FOR R & R OF PAX DOOR OUTER HANDLE HSG AND LATCH MECHANISM PUSH RODS AMM 52-11, OPS CHECK GOOD. (K)

Part: STRUT — DISCHARGED (NLG) · airframe 22,020 hrs · 19,978 cycles

GEAR DISAGREE WHEN GEAR HANDLE MOVED TO UP POSITION. NOSE GEAR WOULD NOT RETRACT, FOLLOWED QRH AND GEAR CAME DOWN WITH MANUAL RELEASE. NO EMERGENCY DECLARED. NORMAL LANDING. SERVICED NLG SHOCK STRUT IAW AMM 12-12-32 IAW LANDING GEAR EXTEND AND RETRACT IAW 32-30-00, OPS CHECK GOOD.

Part: BULKHEAD — CRACKED · airframe 21,796 hrs · 19,774 cycles

FWD PRESSURE BULKHEAD IS CRACKED AT THE PARKING BRAKE LOCATION. FWD PRESSURE BULKHEAD AT THE PARKING BRAKE LOCATION REPAIRED IAW REO 601R-53-11-1772. (K)

Part: ANGLE — CRACKED (BS 559) · airframe 21,796 hrs · 19,774 cycles

RT LWR CAP ANGLE CRACKED AT FS 559.00, RBL 18, WL 46.5. RT LWR CAP ANGLE AT FS 559.00, RBL 18, WL 46.5. REPAIRED IAW REO 601R-53-41-609 REV A AND REO 601R-53-41-260, REV D. (K)

Part: BULKHEAD — GOUGED (BS 280) · airframe 21,796 hrs · 19,774 cycles

BULKHEAD WEB AFT FACE GOUGED AT FS 280.00, RBL 11.00, WL 93.00 (.110 "L X .200" W X 0.015 DEEP) GOUGES ON BULKHEAD WEB AFT FACE AT FS 280.00, RBL 11.00, WL 93.00. REPAIRED IAW REO 601R-53-11-1727, REV C (REPAIR 1).

Part: SKIN — CRACKED (BS 235) · airframe 21,796 hrs · 19,774 cycles

CRACK FOUND ON SKIN AT FS 235.00, LT AFT CORNER OF NOSE LANDING GEAR SKIN AT FS 235.00. LT AFT CORNER OF NLG REPAIRED AT REO 601R-53-11-068, REV A. (K)

Part: ANGLE — CRACKED (BS 559) · airframe 21,796 hrs · 19,774 cycles

LT LWR CAP ANGLE IS CRACKED AT FS 559.00, LBL 18, WL 46.5, LT LWR CAP ANGLE REPAIRED AT FS 559.00, LBL 18.00, WL 46.5 IAW REO 601R-53-41-260, REV D. (K)

Part: FLOORBEAM — CRACKED (BS 280)

INBD FLOORBEAM ANGLE AT FS 280.00, RBL 8, WL 72 IS CRACKED. INBD CLIP AT FS 280.00, RBL 8, WL 72 IS REPLACED IAW SRM 51-47-21. (K)

Part: LONGERON — CORRODED (BS 310-349) · corrosion level 1 · airframe 21,796 hrs · 19,774 cycles

PAX DOOR CUTOUT LWR SILL, LONGERON CORRODED. REPLACED LONGERON ON PAX DOOR CUTOUT LWR SILL, FS 310.00 TO 349.00, LBL 46.00, WL 72.00 IAW SRM 51-42-06. (K)

Part: ANGLE — CRACKED (BS 280) · airframe 21,796 hrs · 19,774 cycles

UPPER AFT ANGLE IS CRACKED AT FS 280.00, LBL 14.00, WL 72.00. UPPER AFT ANGLE REPAIR CARRIED OUT IAW REO 601R53-11-138. (K)

Part: INTERCOSTAL — CRACKED (BS 484) · airframe 21,796 hrs · 19,774 cycles

CRACK FOUND ON INTERCOSTAL FS 484.00, LBL 27.00, WL 71.00. INTERCOSTAL CLIP REPLACED AT FS 484.00, LBL 27.00, WL 71.00 IAW SRM 51-42-06 AND 51-42-21. (K)

Part: HANDLE — CRACKED (CARGO DOOR) · airframe 21,796 hrs · 19,774 cycles

CARGO DOOR HANDLE HOUSING IS CRACKED. CARGO DOOR HANDLE HOUSING REPLACED IAW SRM 51-42-21 AND DWG 601R35027 REV AY. (K)

Part: BRACKET — CORRODED (BS 310-349) · airframe 21,796 hrs · 19,774 cycles

PAX DOOR CUTOUT LWR SILL, FWD AND AFT BRACKETS ARE CORRODED. REPLACED FWD AND AFT BRACKETS ON PAX DOOR CUTOUT LWR SILL IAW SRM 51-42-06. (K)

Part: FLOORBEAM — CRACKED (BS 461) · airframe 21,796 hrs · 19,774 cycles

CRACK FOUND ON MACHINED FLOORBEAM FITTING AT FS 461.00, RBL 9.00 OTBD SIDE CRACK LENGTH IS .650" AT FS 461.00, RBL 9.00 OTBD SIDE, MACHINED FLOORBEAM FITTING REPLACED IAW SRM 51-42-21. (K)

Part: CARGO TRACK — CORRODED (BS 605-621) · airframe 21,796 hrs · 19,774 cycles

BAGGAGE RAIL CORRODED BETWEEN FS 605 TO 621 AT LBL 9. BAGGAGE RAIL REPLACED BETWEEN FS 605 AT LBL 9 IAW SRM 51-41-04. (K)

Part: CARGO TRACK — CORRODED (BS 559+112) · airframe 21,796 hrs · 19,774 cycles

BAGGAGE RAIL CORRODED AT FS 559+112, RBL 9. BAGGAGE RAIL REPLACED AT FS 559+112, RBL 9 IAW SRM 51-41-04. (K)

Part: SILL — CRACKED (BS 574) · airframe 21,796 hrs · 19,774 cycles

LT SILL CRACKED AT FS 574 UNDER STOP BRACKET CRACKED (CRACK LENGTH: .700) LT SILL CRACK AT FS 574 REPAIRED IAW REO 601R-53-61-1741. (K)

Part: INTERCOSTAL — CRACKED (BS 484) · airframe 21,796 hrs · 19,774 cycles

CRACK FOUND ON INTERCOSTAL AT FS 484.00, LBL 36.00, WL 71.00. REPAIR DONE IAW REO 601R-53-41-059, REV A. (K)

Part: INTERCOSTAL — CRACKED (BS 484) · airframe 21,796 hrs · 19,774 cycles

CRACK FOUND ON INTERCOSTAL FS 484.00, RBL 27.00, WL 71.00, INTERCOSTAL CLIP AT FS 484.00, RBL 27.00, WL 71.00. REPLACED IAW SRM 51-42-06 AND 51-42-21. (K)

Part: FLOORBEAM — CRACKED (BS 280)

FLOORBEAM IS CRACKED IN THE LOWER RADIUS, LBL 9.0, W/L 68.00. CRACK LENGTH IS .500" CUT/OUT OF FLOORBEAM, FABRICATION OF PIECES, NDT ON CUT/OUT AND FILLER, WET INSTALL, ALL THESE ABOVE IAW REO 601R-53-11-171, REV D. (K)

Part: FLOORBEAM — CRACKED (BS 280) · airframe 21,796 hrs · 19,774 cycles

FLOORBEAM IS CRACKED IN THE LWR RADIUS AT FS 280.00, W/L 68.00, CRACK LENGTH IS .500" CUT-OUT OF FLOORBEAM, FABRICATION OF PIECES, NDT FOR CUT/OUT AND FILLER, WET INSTALL. ALL THESE ABOVE IAW REO 601R-53-11-171, REV D. (K)

Part: BULKHEAD WEB — CRACKED (BS 621) · airframe 21,796 hrs · 19,774 cycles

REAR PRESSURE BULKHEAD WEB AT THE LINTEL LOCATION IS CRACKED. REAR PRESSURE BULKHEAD WEB AT THE LINTEL LOCATION REPAIRED IAW REO 601R-53-61-1230, REV D. (K)

Part: UPLOCK — DEFECTIVE (RT MLG) · airframe 21,373 hrs · 19,369 cycles

RT MLG DISAGREE, RT MAIN UPLOCK ASSY DEFECTIVE, PLACED GEAR RETRACTION SYSTEM ON MEL.

Part: FAN BLADE — DAMAGED (RT ENGINE) · airframe 20,651 hrs · 18,666 cycles

ON CLIMB, BIRD STRIKE IN RT ENGINE IMMEDIATELY AFTER SMOKE ODOR IN CABIN, RETURNED TO DEPARTURE. LANDED OVERWEIGHT 47,500 IN., RATE OF DESCENT, 300 FT PER MINUTE. REMOVED AND REPLACED 10 FAN BLADES. DAMAGED ONES AND BLADES 180 DEGREE OUT IAW AMM 72-20.

Part: UNKNOWN — ODOR (CABIN) · airframe 20,616 hrs · 18,630 cycles

F/A NOTED ELECTRICAL BURNING ODOR AT THE BACK OF THE ACFT DURING FLIGHT. RAMPERS ALSO SMELLED ELECTRICAL ODOR UPON OPENING THE CARGO DOOR. WILL ALL DOORS CLOSED, RAN ENGINES 15 MINUTES WITH BOTH AC PACKS ON, ALSO RAN HYD ACMP`S. INSP ALL AFT CABIN, LAV AND CARGO BAY LIGHTS. VERIFIED NO AC FANS BREAKERS POPPED OR FAIL MESSAGES. NO ELECTRICAL ODOR NOTED. ACFT OK FOR SERVICE, ALL CHECKS NORMAL. (K)

Part: ENGINE — ODOR (LT)

AFTER ENGINE SHUTDOWN, NR 1, NOTICED FUEL ODOR AND MORE THAN AVERAGE SMOKE FROM TAIL PIPE. FOUND ENGINE NR 1 THROTTLE AND PULL CONTROL RIG OFF, RERIGGED LT ENGINE REF AMM 76-10-00. INSPECTED LT ENGINE, CLEANED EXCESS OIL OUT OF COWLING DRY MOTOR ENGINE, NO SIGN OF SMOKE, PERFORMED OPERATIONAL RUN UP OF ENGINE. OPS CHECK GOOD. NO SIGNS OF SMOKE. (K)

Part: SKIN — DENTED (TE FLAP)

LT INBOARD FLAP HAS DENT MEASURING 2 INCHES LONG BY 2 INCHES WIDE AND .050 INCHES DEEP LOCATED 24 INCHES FROM INBOARD EDGE OF FLAP AND .500 INCH FROM TRAILING EDGE, LOWER SKIN. MAINTENANCE CUT AWAY DAMAGED SECTION OF SKIN AND INSTALLED NON-FLUSH REPAIR DOUBLER IAW CRJ SRM 57-52-00, REPAIR NR 3. (M)

Part: SKIN — DENTED (TE FLAP)

LT INBOARD FLAP HAS DENT MEASURING 1.5 INCHES LONG BY 2.5 INCHES WIDE AND .030 INCHES DEEP LOCATED 24 INCHES FROM INBOARD END OF FLAP AND 6 INCHES FROM TRAILING EDGE, LOWER SKIN. MAINTENANCE CUT AWAY DAMAGED SECTION OF SKIN AND INSTALLED A NON-FLUSH REPAIR DOUBLER IAW CRJ SRM 57-52-00, REPAIR NR 3. (M)

Part: ATTACH FITTING — CRACKED (FS 280)

RIGHT OUTBOARD 280 CLIP IS CRACKED APPROX .25 INCH LONG. SUP - MAINTENANCE REMOVED CRACKED CLIP AND INSTALLED A NEW CLIP, P/N 601R31113-58 IAW BSC STANDARD REPAIR 601R-53-0057A AND CRJ SRM 51-42-21. (M)

Part: STIFFENER — CRACKED (BULKHEAD)

THE STIFFENER POST AT RBL 18 ON THE FORWARD FACE OF THE 409 PLUS 128 BULKHEAD IS CRACKED ON THE OUTBOARD SIDE IN THE RADIUS BY THE LOWER RIVET. SUP - MAINTENANCE REPAIRED STIFFENER POST AT RBL 18 ON FWD FACE OF 409 PLUS 128 BULKHEAD BY TRIMMING OF DAMAGE, FABRICATED REPAIR AND INSTALLED IAW BOMBARDIER REO 601R-53-41-056 REV E. (M)

Part: CONNECTOR — DIRTY (HYD SYSTEM)

DURING CLIMB, HYDRAULIC NR 3 LOW PRESSURE MESSAGE APPEARED AND 0 PSI WAS INDICATED. FOUND 3A PUMP CIRCUIT BREAKER 2G15 POPPED, RESET ONCE, LOW PRESSURE MESSAGE CLEARED. ON GROUND, FOUND CB2N12 TO BE POPPED (HYD SYSTEM IND 3) TRIED ONE RESET C/B WOULD NOT RESET. CLEANED CONNECTOR ON HYD PRESSURE TRANSDUCER NR 3, RESET CB 2N12. OPS CHECK GOOD IAW AMM 29-10-00. NO DEFECTS NOTED AT THIS TIME. (M)

Part: STIFFENER — CRACKED (BULKHEAD)

THE STIFFENER POST AT RBL 9 ON THE AFT FACE OF THE BULKHEAD AT FS 559 IS CRACKED ON THE INBOARD AND OUTBOARD SIDES APPROX .5 INCH LONG AT THE LOWER RIVETS. SUP - MAINTENANCE PERFORMED MAJOR REPAIR TO STIFFENER POST AT BULKHEAD FS 559 AT RBL 9 IAW CRJ 200 SRM 51-42-06 AND BOMBARDIER REO 601R-53-41-057. (M)

Part: PUSHROD — OUT OF ADJUST (PAX DOOR) · airframe 14,976 hrs · 13,204 cycles

PASSENGER BOARDING DOOR WILL NOT OPEN FROM OUTSIDE, THE HANDLE WILL NOT TURN. ADJUSTED PUSHROD ASSY BETWEEN PIVOT LEVER ROLL LATCH TORQUE TUBE, OPS CHECK GOOD IAW AMM. (K)

Part: STIFFENER — CHAFED (FUSELAGE)

VERTICAL STIFFENER 2 MEMBER AT BL 0 ON AFT SIDE OF REAR PRESSURE BULKHEAD AT FS 621 IS CHAFED AT TOP AREA ON RADIUS .5 INCH BY .50 INC - .060 INCH DEEP. BLENDED AND TREATED CHAFED AREA ON OUTSIDE OF RADIUS AND NESTED A REPAIR ANGLE ON INSIDE OF RADIUS IAW BSC EO 601R-53-9437. (M)

Part: HINGE — CORRODED (FS 310)

PAX DOOR ATTACH HINGE HALF IS CORRODED ON IB SIDE FOR TOP STEP. MAINTENANCE REMOVED DAMAGED HINGE BY REMOVING SCREWS, INSTALLED NEW SERVICEABLE HINGE BY INSTALLED NEW SCREWS IAW CRJ AMM 20-21-00-910-801. (M)

Part: SKIN — DAMAGED (LT AILERON)

LEFT AILERON UPPER INBOARD TRAILING EDGE SKIN HAS MISSING FILLER. MAINTENANCE REPAIRED LEFT AILERON UPPER TRAILING EDGE BY INSTALLING FILLER AND DOUBLER IAW CRJ 200 SRM, 57-60-00 REPAIR 01. (M)

Part: SKIN — CORRODED (LT WING)

THE LEFT LOWER WING PLANK HAS CORROSION AT THE FUEL TANK ACCESS CUTOUT FOR PANEL 510AB HOLE NR 3 AT WS 32.263 APPROX .003 INCH DEEP BY .4 INCH LONG IN THE CRITICAL AREA OF THE FORWARD HOLE EDGE AND .003 INCH DEEP BY .4 INCH LONG IN THE CRITICAL AREA OF THE AFT HOLE EDGE. MAINTENANCE REPAIRED FUEL TANK ACCESS HOLE CUTOUT WING PLANK IAW BOMBARDIER INC REO 601R-57-21-030 REV D. (M)

Part: SKIN — CORRODED (LT WING)

THE LEFT LOWER WING PLANK HAS CORROSION AT THE FUEL TANK ACCESS CUTOUT FOR PANEL 550EB HOLE NR 13 AT WS 253.022 APPROX .004 INCH DEEP BY 1 INCH LONG IN THE CRITICAL AREA ON THE FORWARD HOLE EDGE AND APPROX .004 INCH DEEP BY .75 INCH LONG IN THE CRITICAL AREA ON THE AFT HOLE EDGE. MAINTENANCE REPAIRED FUEL TANK ACCESS HOLE CUTOUT WING PLANK IAW BOMBARDIER REO 601R-57-21-030 REV D. (M)

Part: SKIN — CORRODED (LT WING)

THE LEFT LOWER WING PLANK HAS CORROSION AT THE FUEL TANK ACCESS CUTOUT FOR PANEL 550DB HOLE NR 12 AT WS 230.415 APPROX .004 INCH DEEP BY 1.25 INCH LONG IN THE CRITICAL AREA ON THE FORWARD HOLE EDGE AND APPROX .004 INCH DEEP BY .75 INCH LONG IN THE CRITICAL AREA OF THE AFT EDGE. MAINTENANCE REPAIRED FUEL TANK ACCESS HOLE CUTOUT WING PLANK IAW BOMBARDIER REO 601R-57-21-030 REV D. (M)

Part: SKIN — CORRODED (LT WING)

THE LEFT LOWER WING PLANK HAS CORROSION AT THE FUEL TANK ACCESS CUTOUT FOR PANEL 550BB HOLE NR 10 AT WS 188.040 APPROX .005 INCH DEEP BY 2.75 INCH LONG IN THE CRITICAL AREA ON THE FORWARD HOLE EDGE AND APPROX .005 INCH DEEP BY 1.25 INCH LONG IN THE CRITICAL AREA ON THE AFT EDGE. MAINTENANCE REPAIRED FUEL TANK ACCESS HOLE CUTOUT WING PLANK IAW BOMBARDIER REO 601R57-57-21-030 REV D. (M)

Part: SKIN — CORRODED (LT WING)

THE LEFT LOWER WING PLANK HAS CORROSION AT THE FUEL TASK ACCESS CUTOUT FOR PANEL 540EB HOLE NR 7, WS 116.366 APPROX .004 INCH DEEP BY 2 INCH IN THE CRITICAL AREA ON THE FORWARD HOLE EDGE AND APPROX .004 INCH DEEP BY 1 INCH LONG IN THE CRITICAL AREA ON THE AFT HOLE EDGE. MAINTENANCE REPAIRED FUEL TANK ACCESS HOLE CUTOUT WING PLANK IAW BOMBARDIER REO 601R-57-21-030 REV D.

Part: SKIN — CORRODED (LT WING)

THE LEFT LOWER WING PLANK HAS CORROSION AT THE FUEL TANK ACCESS CUTOUT FOR PANEL 540CB HOLE NR 5 AT WS 76.161 APPROX .004 INCH DEEP BY 1.5 INCH LONG IN THE CRITICAL AREA OF THE FORWARD HOLE EDGE AND APPROX .004 INCH DEEP BY 2.25 INCH LONG ON THE CRITICAL AREA OF THE AFT HOLE. MAINTENANCE REPAIRED FUEL TANK ACCESS HOLE CUTOUT WING PLANK IAW BOMBARDIER REO 601R-57-21-030 REV D. (M)

Part: SKIN — CORRODED (LT WING)

THE LEFT LOWER WING PLANK HAS CORROSION AT THE FUEL TANK ACCESS CUTOUT FOR PANEL 550FB HOLE NR 14 AT WS 274.319 APPROX .005 INCH DEEP BY 1.5 INCH LONG ON THE CRITICAL AREA ON THE FORWARD HOLE EDGE AND APPROX .005 INCH BY .75 INCH IN THE CRITICAL AREA ON THE AFT HOLE EDGE. MAINTENANCE REPAIRED FUEL TANK ACCESS HOLE CUTOUT WING PLANK IAW BOMBARDIER REO 601R-57-21-030 REV D. (M)

Part: SKIN — CORRODED (LT WING)

THE LEFT LOWER WING PLANK HAS MINOR CORROSION AT THE FUEL TANK ACCESS CUTOUT FOR PANEL 540DB HOLE NR 6 AT WS 95.950 APPROX .003 DEEP BY .4 INCH LONG ON THE FORWARD HOLE EDGE AND .003 DEEP BY .4 INCH LONG ON THE AFT HOLE EDGE IN THE CRITICAL AREAS. MAINTENANCE REPAIRED FUEL TANK ACCESS HOLE CUTOUT WING PLANK IAW BOMBARDIER REO 601R-57-21-030 REV D. (M)

Part: SKIN — CORRODED (LT WING)

THE LEFT LOWER WING PLANK HAS CORROSION AT THE FUEL TANK ACCESS CUTOUT FOR PANEL 540BB HOLE NR 1 AT WAS 54.897 APPROX .005 INCH DEEP BY 1 INCH LONG IN THE NON CRITICAL AREA ON THE OUTBOARD HOLE EDGE. MAINTENANCE REPAIRED FUEL TANK ACCESS HOLE CUTOUT WING PLANK IAW BOMBARDIER REPAIRED FUEL TANK ACCESS HOLE CUTOUT WING PLANK IAW BOMBARDIER REO 601R-57-21-030 REV D. (M)

Part: SKIN — CORRODED (LT WING)

THE LEFT LOWER WING PLANK HAS CORROSION AT THE FUEL TANK ACCESS CUTOUT FOR PANEL 540FB HOLE NR 8 WS 136.676 APPROX .005 INCH DEEP BY 1.25 INCH LONG IN THE CRITICAL AREA ON THE FORWARD EDGE AND APPROX .005 INCH BY .4 INCH IN THE CRITICAL AREA ON THE AFT HOLE EDGE. MAINTENANCE REPAIRED FUEL TANK ACCESS HOLE CUTOUT WING PLANK IAW BOMBARDIER REO 601R-57-21-030 REV D.

Part: SKIN — CORRODED (LT WING)

THE LEFT LOWER WING PLANK HAS CORROSION AT THE FUEL TANK ACCESS CUTOUT FOR PANEL 540AB HOLE NR 4 AT WS 54.861 APPROX .004 INCH DEEP BY 3 INCH LONG ON THE CRITICAL AREAS OF THE FORWARD AND AFT HOLE EDGES. MAINTENANCE REPAIRED FUEL TANK ACCESS HOLE CUTOUT WING PLANK IAW BOMBARDIER REO 601R-57-21-030 REV D. (M)

Part: SKIN — CORRODED (LT WING)

THE LEFT LOWER WING PLANK HAS CORROSION AT THE FUEL TANK ACCESS CUTOUT FOR PANEL 550AB HOLE NR 9 WS 163 APPROX .005 INCH DEEP BY .25 INCH LONG IN THE CRITICAL AREA ON THE FORWARD HOLE EDGE AND APPROX .005 INCH BY 1 INCH THE CRITICAL AREA ON THE AFT HOLE EDGE. MAINTENANCE REPAIRED FUEL TANK ACCESS HOLE CUTOUT WING PLANK IAW BOMBARDIER REO 601R-57-21-030 REV D. (M)

Part: SKIN — CORRODED (LT WING)

THE LEFT LOWER WING PLANK HAS CORROSION AT THE FUEL TANK ACCESS CUTOUT FOR PANEL 510AB HOLE NR 2 AT WS 12.245 APPROX .005 INCH DEEP IN SEVERAL SPOTS IN THE CRITICAL AND NON CRITICAL AREAS OF THE FORWARD, AFT, INBOARD AND OUTBOARD HOLE EDGES. MAINTENANCE REPAIRED FUEL TANK ACCESS HOLE CUTOUT WING PLANK IAW BOMBARDIER INC REO 601R-57-21-030 REV D. (M)

Part: ANGLE — CRACKED (BS 625)

FOUND LEFT OBLIQUE ANGLE, FS 625 IS CRACKED APPROX 1 INCH LONG. MAINTENANCE REMOVED AND REPLACED LEFT OBLIQUE ANGLE AT FS 625 IAW CRJ 200 SRM 51-42-06. (M)

Part: INTERCOSTAL — CRACKED (BS 484)

FOUND RIGHT SIDE FS 484 INTERCOSTAL CRACKED APPROX 1 INCH IN UPPER CORNER AT RBL 36. (M)

Part: ANGLE — CRACKED (BS 625)

FOUND RIGHT OBLIQUE ANGLE, FS 625 IS CRACKED APPROX 1 INCH LONG. MAINTENANCE REMOVED AND REPLACED RT OBLIQUE ANGLE AT FS 625 IAW CRJ200 SRM 51-42-06. (M)

Part: INTERCOSTAL — CRACKED (BS 484)

FOUND FS 484 INTERCOSTAL ATTACH FLANGE IS CRACKED .4 INCH AT RBL 36, WL 73. MAINTENANCE CUT AWAY DAMAGE AND INSTALLED REPLACEMENT ANGLE IAW BOMBARDIER REO 601R-53-41-059 `A` AND BSC STANDARD REPAIR 601R-53-0030A. (M)

Part: SKIN — CORRODED (RT WING)

RT WING PLANK ACCESS CUTOUT FLANGE AT FUEL PANEL 640 ABS, HOLE NR 4 AT WAS 54.681 HAS MINOR CORROSION MEASURING APPROX 4 INCHES LONG .20 INCH WIDE, .002 INCH DEEP IN CRITICAL AREA. MAINTENANCE REPAIRED FUEL TANK ACCESS HOLE CUT OUT WING PLANK IAW BOMBARDIER INC REO 601R-57-21-030 REV D. (M)

Part: INTERCOSTAL — CRACKED (BS 484)

FOUND FS 484 INTERCOSTAL ATTACH FLANGE IS CRACKED .4 INCH AT RBL 36, WL 73. CUT AWAY ATTACHED FLANGE AND REMOVED BURRS AND SHARP EDGES IAW REO 601R-53-41-059 REV A STEPS 1 AND 2 LPI DUE COMPLIED WITH HFEC OF THE TRIM LINE AT FS 484 RBL 36 INTERCOSTAL REPAIR IAW REO 601R-53-41-059 STEP 3 AND CRJ 200 NDTM PRI 51-20-06. NO INDICATIONS NOTED. (M)

Part: ODOR — DETECTED (COCKPIT)

NOTICED STRONG ODOR OF ELECTRICAL CIRCUIT OVERHEATING. ODOR WAS TRANSIENT IN NATURE. OCCURRED 10 MINUTES PRIOR TO LANDING AND LASTED ABOUT 1 MINUTE, WAS ONLY NOTICED IN COCKPIT. PERFORMED VISUAL INSPECTION BEHIND OVERHEAD PANEL, CENTER PEDESTAL, BOTH SIDE PANELS, BOTH SIDE CONSOLES UNDER BOTH INSTRUMENT PANELS IAW AMM 25-16-00 FOR EVIDENCE OF OVERHEATING, ARCING OR ELECTRICAL ODOR. FOUND NO DEFECTS. GAINED ACCESS BEHIND C/B/P 1 THROUGH 4 IAW AMM 24-02-00. AVIONICS BAY FORWARD COMPARTMENT FOR EVIDENCE OF OVERHEATING, ARCING, OR ELECTRICAL ODOR AND FOUND NO DEFECTS. INSPECTED CONTACTOR 4XKA IAW AMM 24-51-25 FOR OVERHEATING, ARCING OR ELECTRICAL ODOR. NO DEFECT. (M)

Part: BPSU — FAILED (RIGHT)

FLAPS FAIL MESSAGE WHEN SELECTED 0 DEGREES TO 8 DEGREES IN FLIGHT STUCK AT 0 DEGREES. FECU SHOWS FAILURE OF RT BPSU, REMOVED AND REPLACED RIGHT BPSU AND RIGGED IAW AMM 27-51-10. (M)

Part: UNKNOWN — UNKNOWN · airframe 12,851 hrs · 11,170 cycles

ABORTED TAKEOFF DUE TO LOSS OF DIRECTIONAL CONTROL AT LOW SPEED (30 KNOTS) WHEN APPLIED POWER. AC WENT TO THE RT, FULL LT RUDDER HAD NO EFFECT. ENG PERAMETERS NORMAL AND NO THRUST LEVER SPLIT. CREW PERFORMED 2 HIGH SPEED TAXIS, PERFORMED POWER ASSURANCE RUNS ON BOTH ENGS, PERFORMED LOW SPEED TAXI WITH SETS OF RUDDER PEDAL AND TILLER WHEEL AND DID VISUAL INSPECTION OF AC IAW AMM. NO DEFECTS NOTED AC TAXIS NORMAL. ENG PARAMETERS AS WELL AS POWER LEVERS ARE EQUAL. OK FOR CONTINUED SERVICE. (K)

Part: DCU — MALFUNCTIONED (ELECTRICAL SYS)

DC ESS BUS CAUTION MESSAGE, SYSTEMS APPEARED TO BE UNAFFECTED, CBP4-B3 POPPED. RECYCLED C/B AND REMOVED AND REPLACED NR 2 DCU. OPS CHECK NORMAL IAW AMM 24-31-00. (M)

Part: WARNING LIGHT — ILLUMINATED (PAX DOOR) · airframe 9,812 hrs · 8,393 cycles

PAX DOOR OUTER HANDLE CAUTION MESSAGE APPEARED IN FLIGHT COMPLIED WITH QRH AND LANDED AT NEAREST SUITABLE AIRPORT DURING CLIMB THR FL210. INSPECTED PAX DOOR LOCKING MECHANISM, NO DEFECTS NOTED, CYCLED DOOR CLOSED AND OPEN SEVERAL TIMES. NOT MESSAGE APPEARED ON GROUND.

Part: LINE — CHAFED (HYD QTY IND) · airframe 9,642 hrs · 8,248 cycles

NR 1 HYDRAULIC QUANTITY INDICATOR 35 PERCENT AT FL310 WITH NORMAL PRESSURE (3000 PSI). FOUND NR 1 EAP SUCTION LINE CHAFED THROUGH. NO DAMAGE TO PRESSURE LINE. REPAIRED LINE IAW AMM 20-22-00. LEAK AND OPS CHECK GOOD.

Part: SHUTOFF VALVE — FAILED (RT A/C PACK)

RIGHT PACK WILL NOT COOL CABIN IN AUTO OR MANUAL MODE, AIR RETURN. REMOVED AND REPLACED RIGHT PACK PRSOV IAW AMM 21-51-43. NO FIX. PLACED ON MEL. REPLACED AND TIGHTENED AIR DUCT AT CAPTAINS FEET AREA. OPS CHECK GOOD. REMOVED OFF MEL. (M)

Part: WHEEL — BENT (NLG)

STRUCK SOMETHING ON RUNWAY ON TAKEOFF ROLL. NOSE WHEEL BENT, LESS THAN 60 KNOTS, MIN BRAKE USED. INSPECTED NOSE TIRES, NR 2 WHEEL HALF DAMAGED, VISUALLY INSPECTED NOSE STRUT AND SPINDLE. ALSO INSPECTED FUSELAGE, LEADING EDGE AND BOTH ENGINE INTAKES. NO DAMAGE NOTED AT THIS TIME. REMOVED AND REPLACED NOSE WHEEL TIRE ASSEMBLY IAW AMM 32-42-01. (M)

Part: ENGINE — VIBRATION (NR 1)

NR 1 ENGINE INDICATES VIB YELLOW CAUTION ON TAKEOFF ROLL BELOW 60 KNOTS. ABORTED TAKEOFF, NO VIBRATION FELT. REVIEWED HISTORY, PERFORMED TWO SEPARATE ENGINE POWER RUNS, NO VIBRATION NOTED. FAN BLADE INSPECTED, NO DISCREPANCIES. TAKEOFF WAS PERFORMED IN SEVERE ICING CONDITIONS. SUSPECT ICE BUILD-UP ON FAN. AIRCRAFT OK FOR SERVICE. (M)

Part: LINE — CHAFED (HYD SYSTEM)

HYDRAULIC LOW PRESSURE CAS MESSAGE COMPLIED WITH QRH AIR RETURN TO DEN OPERATE NR 1 EDP APPROXIMATELY 45 SECONDS BEFORE DISCONNECT. FOUND NR 1 HYD HIGH PRESSURE INBOUND FLEX LINE RUPTURED AND NR 1 HYD CASE DRAIN LINE CHAFED, CHAFE CAUSED BY LOWER FAIRLEAD WEAR. REPLACED CASE DRAIN LINE AND HIGH PRESSURE FLEX LINE PER AMM. (M)

Part: IDG — UNDERSERVICED (NR 1 GEN)

DURNG TAKEOFF, IDG 1 MESSAGE FOLLOWED BY GEN 1 MESSAGE. SERVICED IDG NR 1 WITH OIL IAW AMM 12-13-24. (M)

Part: IDG — FAILED (NR 1)

'IDG 1' AMGER CAS MESSAGE ON TAKEOFF ROLL, FOLLOWED BY 'GEN 1 OFF' AMBER CAS MESSAGE, CREW PERFORMED QRH AND ABORTED TAKEOFF. FOUND IDG NR 1 LOW OIL LEVEL, SERVICED IDG IAW AMM, GROUND RAN ENGINE, LEAK AND OPS CHECK GOOD. VOLTS AND FREQUENCY NORMAL, OK FOR SERVICE. (M)

Part: TRANSDUCER — FAILED (NR 1 ENG VIBRA)

DURING TAKE-OFF POWER APPLICATION RECEIVED VIBE INDICATION NR 1 ENGINE AT 88.1 PERCENT N1 IN PROGRESS. REPLACED VIBRATION TRANSDUCER WIRE HARNESS ON LEFT ENGINE, OPS CHECK GOOD. RAN LT ENGINE TO 90 PERCENT N1 NO N2 VIBRATION INDICATION NOTED. (M)

Part: VANE — CHAFED (TE FLAP)

FLAP VANE HAS A CHAFE APPROX .004 INCH DEEP BLENDED DAMAGED AREA IAW WVAC EO 601R-57-3998. (M)

Part: VANE — CHAFED (LT TE FLAP)

LEFT OUTBOARD FLAP VANE HAS A CHAFE APPROX .004 INCH DEEP BLENDED DAMAGED AREA IAW WVAC EO 601R-57-3998. (M)

Part: FLOOR SUPPORT — CRACKED (FUSELAGE)

RIGHT FLOOR SUPPORT ANGLE AT FS 621 IS CRACKED. REMOVED CRACKED PORTION OF ANGLE AND INSTALLED NEW ANGLE IAW BOMBARDIER AEROSPACE REO 601R-53-61-117 REV B. (M)

Part: FLOOR SUPPORT — CRACKED (FUSELAGE)

RIGHT FLOOR SUPPORT ANGLE AT FS 621 IS CRACKED. REMOVED CRACKED PORTION OF ANGLE AND INSTALLED NEW ANGLE IAW BOMARDIER AEROSPACE REO 601R-53-61-117 REV B.

Part: ANGLE — CRACKED (FUSELAGE)

OBLIQUE ANGLES AT FS 625 LEFT AND RIGHT ARE CRACKED. REMOVED AND REPLACED OBLIQUE ANGLES AT FS 625 LEFT AND RIGHT SIDES IAW CRJ SRM 51-42-06. (M)

Part: ANGLE — CRACKED (FUSELAGE)

OBLIQUE ANGLES AT FS 625 LEFT AND RIGHT ARE CRACKED. REMOVED AND REPLACED OBLIQUE ANGLES AT FS 625 LEFT AND RIGHT SIDES IAW CRJ SRM 51-42-06. (M)

Part: STRIKER — DAMAGED (DOOR SEAL)

DAMAGE AT EXISTING REPAIR ON PASSENGER DOOR SEAL STRIKER FS 310, LOWER FRAME/LATCH. REMOVED DAMAGED SECTION OF SEAL STRIKER AND INSTALLED A NEW SECTION OF SEAL STRIKER IAW REO 601R-52-11-008 ISSUE B. (M)

Part: STRIKER — DAMAGED (PAX DOOR)

DAMAGE AT EXISTING REPAIR ON PAX DOOR SEAL STRIKER FS 310, LOWER FRAME LATCH. REMOVED DAMAGED SECTION OF SEAL STRIKER AND INSTALLED A NEW SECTION OF SEAL STRIKER IAW REO 601R-52-11-008 ISSUE B. (M)

Part: ACCELEROMETER — MALFUNCTIONED (NR 1 ENGINE)

DURING TAKEOFF ROLL AT 70 KNOTS, OBSERVVED N2 ENGINE VIBE 'ICON' ON NR 1 ENGINE BTMS. ALL GREEN BANDS ON ABORTED TAKEOFF. PERFORMED PARTIAL ENGINE BORESCOPE. NO DAMAGE NOTED. REMOVED AND REPLACED NR 1 ENGINE ACCELEROMETER. NO DEFECTS NOTED. (M)

Part: LINE — CHAFED (HYD SYSTEM)

HYDRAULIC 2 LOW PRESSURE MESSAGE ON EICAS, NO QUANTITY NOTED. REMOVED AND REPLACED NR 2 EDP (HYD) AND CHAFED LINE IN PYLON (HYD). OPS AND LEAK CHECK GOOD. (M)

Part: INDICATOR — MALFUNCTIONED (RT TE FLAP)

RIGHT FLAP INDICATOR FLASHES BETWEEN 8 DEGREES AND 10 DEGREES WITH FLAPS SET AT 10 DEGREES. MEL M ACTION CAUSES FAULTS. REMOVED AND REPLACED FLAP POSITION TRANSMITTER. (M)

Part: RELAY — FAILED (NR 1 BUSS)

AC ESSENTIAL BUSS CAUTION MESSAGE. THE AC ESSENTIAL BUSS WOULD NOT ACCEPT POWER FROM EITHER AC BUSS 1 OR AC BUSS 2. T/S IAW FIM 24-20-00. FOUND RELAY K1XD BAD. REMOVED AND REPLACED RELAY K1XD. PN V210D090BC, IAW MM. OPS CHECK GOOD IAW MM.

Part: APU — MALFUNCTIONED (APU BAY)

STRONG FUEL ODOR WHEN APU WAS START AND BLEED SWITCH OVER IN FLIGHT, CONTINUED UNTIL APU WAS SHUTDOWN. PLACED APU ON MEL. (M)

Part: ODOR — DETECTED (CABIN)

STRONG FUEL SMELL WHEN SWITCHING BLEEDS OVER TO APU AIR. PERSISTED AFTER LANDING. RAN ENGINES AND APU AT 70 PERCENT FOR 20 MINUTES, ODOR DIMINISHED. OP CHECKS GOOD. (M)