N419AW

Part: DETECTOR — MALFUNCTIONED (BLEED LEAK) · airframe 39,330 hrs · 37,707 cycles

LT 10TH DUCT WARNING MESSAGE ILLUMINATED IN FLIGHT. C/W QRH, MESSAGE PERSISTS. DUCT (10TH) SHOWS RED BETWEEN LT 10TH SOV, PACK NR 1, 10TH ISOL VALVE, AND APU LCV ON ECS SYNOPTIC PAGE. AIRCRAFT REMOVED FROM SERVICE. R & R 10TH STAGE DUCTING LOOP B BLEED AIR SENSING ELEMENT, REF AMM 36-21-04. OPERATIONS CHECK GOOD. R & R BLEED LEAK DETECTION CONNECTOR P17WK, REF ESPM 20-17-11. OPERATIONS CHECK GOOD A/C FOR RETURN TO SERVICE.

Part: CONTROLLER — MALFUNCTIONED (ADG DEPLOY) · airframe 38,802 hrs · 37,154 cycles

SHORTLY AFTER TAKE OFF, THE AIRCRAFT'S AIR DRIVEN GENERATOR DEPLOYED WITHOUT INPUT FROM THE CREW. THE FLIGHT AIR RETURNED TO RIC AS A RESULT. AIRCRAFT REMOVED FROM SERVICE C/W ALT INSP AFTER ADG DEPLOYMENT DURING UNSCHEDULE MX CHECK IAW AWAC SUP 16-172. C/W VISUAL INSPECTION IAW AWAC SUP 10-066A. RETRACTED ADG IAW AWA SUP 16-015A TASK 24-23-01-840-805AW. REF 308152/1 FOR MEL R/R ADG AUTO DEPLOY CONTROLLER SERIAL#1611

Part: PDU — MALFUNCTIONED (TE FLAP) · airframe 38,673 hrs · 37,021 cycles

RECEIVED FLAP FAIL CAUTION MESSAGE AT 0 DEGREES WHEN SELECTING 0 TO 8 DEGREES. FOLLOWING LANDING THE FLAPS WERE RESET AND THE SYSTEM WAS PLACED ON MEL FOR 10 DAYS AS REQUIRED BY SUPPLEMENT 98-018G AIRCRAFT REMOVED FROM SERVICE. R/R FLAP PDU IAW AMM 27-52-01 OPS CHECK GOOD AT THIS TIME REMOVED PLACARD AND FROM MEL RII.

Part: BULKHEAD WEB — CRACKED (BS 621) · airframe 37,891 hrs · 36,271 cycles

AFT PRESSURE BULKHEAD HAS CRACK AT LBL9.5 , WL75 AT THE BOTTOM OF THE LINER SUPPORT. REPAIRED AFT PRESSURE BULKHEAD IAW REO 601R-53-61-7076 REV--.

Part: BEAM — DAMAGED (BS 574-621) · airframe 37,891 hrs · 36,271 cycles

BEAM 601R35050-64 HAS MARKS FROM DOOR CABLE ASSIST. REPLACED

Part: BRACKET — CRACKED (RT WING) · airframe 37,891 hrs · 36,271 cycles

RIGHT WING I/B LEADING EDGE ATTACH BRACKET IS CRACKED. REPLACED BRACKET IAW SRM 51-41-02.

Part: ANGLE — CRACKED (BS 621-625) · airframe 37,891 hrs · 36,271 cycles

AFB ANGLE CLIP AT RBL 36.20 CRACKED. REPLACED.

Part: ANGLE — CRACKED (BS 625) · airframe 37,891 hrs · 36,271 cycles

AFT PRESSURE BULKHEAD HAS A CRACKED ANGLE CLIP ST LBL36.20 BY THE 4TH INTERCOSTAL FROM THE FLOOR. REPLACED CLIP IAW CRJ200 SRM 51-42-21.

Part: SKIN — CRACKED (BS 187) · airframe 37,891 hrs · 36,271 cycles

LEFT TRU SKIN LANDING CRACKED NEAR LATCH. REPAIRED SKIN IAW SUPP. 19-016B.

Part: BRACKET — CRACKED (BS 193-202) · airframe 37,891 hrs · 36,271 cycles

POWER REC PLUG BOX LOWER BRACKET CRACKED. REPLACED.

Part: WARNING MESSAGE — ILLUMINATED (ANTI ICE) · airframe 37,422 hrs · 35,817 cycles

WHEN DE-SELECTING COWL A/ICE AT FL280, LH COWL A/ICE CAUTION WHEN SWITCH IN OFF POSITION. C/W QRH. DIVERTED TO BNA

Part: UNKNOWN — ODOR (COCKPIT)

CHEMICAL SCENT/LIGHTLY ACRID SMELL OBSERVED IN FLIGHT. ALL OTHER INDICATIONS NORMAL. ONLY OBSERVABLE IN COCKPIT. USING ENGINE AIR.

Part: FRAME — CORRODED (BS 605) · corrosion level 2 · airframe 34,639 hrs · 33,037 cycles

FRAME AT BS 605 IS CORRODED BETWEEN STRINGERS 20L AND 24L.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,639 hrs · 33,037 cycles

FLOOR SUPPORT BETWEEN LBL27 AND LBL9 HAS CORROSION AT FS621.

Part: RIB — CRACKED (RT PYLON) · airframe 34,639 hrs · 33,037 cycles

RIGHT PYLON RIB FOWARD LOWER SUPPORT FLANGE CRACKED UNDER PANEL 421AL

Part: SKIN — DENTED (BS 295-310) · airframe 34,639 hrs · 33,037 cycles

SKIN DENTED BS 295 - 310, STRINGER 12R - 16R

Part: DOOR SILL — CRACKED (FUSELAGE) · airframe 34,639 hrs · 33,037 cycles

BAGGAGE LT SILL IS CRACKED AT PREVIOUS CUTOUT AT FS 605.

Part: FLOOR SUPPORT — CORRODED (BS 559-564) · corrosion level 2 · airframe 34,639 hrs · 33,037 cycles

RBL27 FLOOR SUPPORT HAS CORROSION FROM BS 559+80 TO 564 AROUND SCREW HOLES

Part: FLOOR SUPPORT — CORRODED (BS 568-621) · corrosion level 2 · airframe 34,639 hrs · 33,037 cycles

LEFT CARGO FLOOR SUPPORT FROM BS 568 TO 621 CORRODED.

Part: FLOOR SUPPORT — CORRODED (BS 574-621) · corrosion level 2 · airframe 34,639 hrs · 33,037 cycles

RBL 27 FLOOR SUPPORT BTW BS 574 TO 621 HAS CORROSION AROUND SCREW HOLES.

Part: CROSSBEAM — CORRODED (BS 349) · corrosion level 2 · airframe 34,639 hrs · 33,037 cycles

CROSSBEAM BS 349 IS CORRODED AT RBL 42

Part: FLOOR SUPPORT — CORRODED (BS 349-364) · corrosion level 2 · airframe 34,639 hrs · 33,037 cycles

RIGHT FLOOR SUPPORT CORRODED BETWEEN BS 349 AND 364.

Part: BULKHEAD — CRACKED (BS 621) · airframe 34,639 hrs · 33,037 cycles

AFT PRESSURE BULKHEAD CRACKED AT LBL 18 AND WL 131.

Part: SEAT TRACK — CORRODED (BS 409-559) · corrosion level 2 · airframe 34,639 hrs · 33,037 cycles

LEFT SEAT TRACK CORRODED FROM BS 409+126 TO 559+4, LBL 9.

Part: SEAT TRACK — CORRODED (BS 409-559) · corrosion level 2 · airframe 34,639 hrs · 33,037 cycles

RIGHT FLOOR SEAT TRACK CORRODED FROM BS 409+128 TO 559+16, STRINGER 17L.

Part: ATTACH BRACKET — CRACKED (BS 468) · airframe 34,639 hrs · 33,037 cycles

RIGHT SIDE OVERWING EXIT ACCESS PANEL ATTACH BRACKET CRACKED, BS 468. REPLACED BRACKET IAW SRM 51-41-02, 51-42-06, AND 51-42-13.

Part: ATTACH BRACKET — CRACKED (BS 449) · airframe 34,639 hrs · 33,037 cycles

RIGHT OVERWING ACCESS PANEL ATTACH BRACKET CRACKED AT BS 449. REPLACED THE ATTACH BRACKET IAW SRM 51-42-06, AND 51-42-13.

Part: ATTACH BRACKET — CRACKED (BS 449) · airframe 34,639 hrs · 33,037 cycles

LEFT SIDE OVERWING ACCESS PANEL ATTACH BRACKET CRACKED AT BS 449. REPLACED ATTACH BRACKET IAW SRM 51-42-06, AND 51-42-13.

Part: BULKHEAD — CRACKED (BS 621) · airframe 34,639 hrs · 33,037 cycles

AFT PRESSURE BULKHEAD CRACKED AT RBL18 AND WL119.

Part: STIFFENER — CRACKED (EXHAUST FAIRING) · airframe 34,639 hrs · 33,037 cycles

LEFT EXHAUST FAIRING CRACKED ON FWD STIFFENER. REPAIRED THE FAIRING IAW CMM 78-11-00-300-810-A01, REPAIR SRS042.

Part: FRAME SPLICE — CORRODED (BS 409) · corrosion level 2 · airframe 34,639 hrs · 33,037 cycles

CIRCUMFERENTIAL SPLICE JOINT CORRODED BETWEEN STRINGER 26L AND 26R AFT OF FRAME BS 409. REPLACED CIRCUMFERENTIAL JOINT SPLICE IAW SRM 51-40-11, AND 53-21-15.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 34,367 hrs · 33,035 cycles

EMER FLOOR LIGHTING AT ROW 9 AND AFT INOP. R&R BATTERY PACK POSITION 4 IAW AMM 33-51-04. OPS CHECKED GOOD.

Part: STRINGER — CORRODED (BS 304-327) · corrosion level 2 · airframe 34,594 hrs · 32,995 cycles

1014036-2000-0004 - STRINGER 23R IS CORRODED BETWEEN FS 304 AND FS 327

Part: FRAME — CORRODED (BS 310) · corrosion level 2 · airframe 34,594 hrs · 32,995 cycles

FRAME BS 310 CORRODED, STRINGER 22, AND 23R

Part: FRAME — CORRODED (BS 310) · corrosion level 2 · airframe 34,594 hrs · 32,995 cycles

FRAME BS 310 IS CORRODED BETWEEN STRINGERA 23R AND 23L

Part: STRAP — CORRODED (BS 310-319) · corrosion level 2 · airframe 34,594 hrs · 32,995 cycles

1014036-2000-0012 - SPLICE STRAP UNDER STGR 23R BETWEEN FS 310 AND FS 319 IS CORRODED

Part: FRAME — CORRODED (BS 319) · corrosion level 2 · airframe 34,594 hrs · 32,995 cycles

FRAME BS 319 CORRODED AT STRINGER 23R

Part: ANGLE — CORRODED (BS 310) · corrosion level 2 · airframe 34,594 hrs · 32,995 cycles

REINFORCEMENT ANGLE 600-32002-113 IS CORRODED AT BS 310, STRINGERS 23 AND 24R

Part: ALTIMETER — READS HIGH (CAPTAIN'S) · airframe 34,461 hrs · 32,882 cycles

AT 32,000FT AND 300 KNOTS, CAPTAIN'S ALTIMETER WAS 100FT HIGH, STANDBY WAS 600FT HIGH AND FO'S READ 32,000FT. STANDBY ALTIMETER WAS NOT CLICKING.

Part: LIGHT — BROKEN (CABIN) · airframe 34,435 hrs · 32,861 cycles

IN CABIN, THE FWD EMERGENCY LIGHT NOT WORKING AND PLASTIC COVER BROKEN ORANGE STRIP LIGHT STICKING UP AND EXPOSED. REMOVED AND REPLACED EMERGENCY LIGHT IAW AMM 33-51-01.

Part: UNKNOWN — MALFUNCTIONED (AUTOPILOT SYS) · airframe 32,249 hrs · 30,778 cycles

SHORT ERRATIC UNCOMMANDED YAW MOTION, FOLLOWED BY YAW DAMPER 2 INOPERATIVE STATUS MSG. RE-ENGAGED YAW DAMPER 2 & UNCOMMANDED YAW PERSISTED. DISENGAGED BOTH YAW DAMPERS, THE RE-ENGAGED YAW DAMPER 1 ONLY. NO FURTHER UNCOMMANDED YAW.

Part: HANDLE — DAMAGED (SERVICE DOOR) · airframe 31,557 hrs · 30,098 cycles

SERVICE DOOR WILL NOT OPEN FROM OUTSIDE. REMOVED SERVICE DOOR OUTER HANDLE IAW AMM 52-41-03, FOUND DAMAGE ON HANDLE & HOUSING. REINSTALLED ORIGINAL HANDLE, PLACED ON MEL. REMOVED HANDLE ASSEMBLY & INSPECTED HOUSING IAW AMM 52-41-03 & SUPP 11-029B, NO DEFECTS NOTED ON HOUSING. R & R HANDLE ASSEMBLY IAW AMM 52-41-03 & RIGGED DOOR. OPERATIONS CHECKED GOOD. REMOVED PLACARD & REMOVED FROM MEL.

Part: SKIN — CHAFED (TE FLAP VANE) · airframe 30,984 hrs · 29,534 cycles

LEFT OTBD FLAP VANE HAS CHAFE.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,984 hrs · 29,534 cycles

LBL 27 AT FS 621 - 559+112 HAS CORROSION.

Part: MOUNT — CRACKED (FUSELAGE) · airframe 30,984 hrs · 29,534 cycles

AEB NR 1 HYD SYS PRESS FILTER MOUNT PLATE HAS CRACK IN LOWER AFT CORNER.

Part: MOUNT — CRACKED (FUSELAGE) · airframe 30,984 hrs · 29,534 cycles

AEB NR 2 HYD SYS RETURN FILTER MOUNT PLATE HAS CRACK IN AFT LOWER CORNER.

Part: ATTACH FITTING — CHAFED (RT HORIZ STAB) · airframe 30,984 hrs · 29,534 cycles

RIGHT HORIZONTAL STAB SCREW JACK ATTACH FITTING HAS CHAFES & GOUGES ON THE OTBD UPPER FWD & LOWER EDGES.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 30,984 hrs · 29,534 cycles

RIGHT INBD FLAP VANE, LE IS CHAFED IN 3 AREAS.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 30,985 hrs · 29,534 cycles

FS 574.00 LOWER U BRACKET CRACKED AT RIVET HOLE.

Part: POST — CRACKED (FUSELAGE) · airframe 30,985 hrs · 29,534 cycles

VERTICAL POST AT FS 409 & 28, LBL 27 INBD LOWER SIDE CRACKED.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 30,985 hrs · 29,534 cycles

PAX DOOR AFT DRAG ANGLE CRACKED AT POWER ASSIST LOWER MOUNT.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 30,985 hrs · 29,534 cycles

RIGHT OTBD 484 CLIP CRACKED.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 30,985 hrs · 29,534 cycles

AFT SIDE OF 621 BULKHEAD HAS CRACKED OBLIQUE ANGLE AT STRINGER L14.

Part: BRACKET — CRACKED (PAX DOOR) · airframe 30,985 hrs · 29,534 cycles

PAX DOOR CAM COVER PLATE AFT MOUNT IS CRACKED.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 30,985 hrs · 29,534 cycles

LEFT STRINGER 3 AT FS 280 CRACKED.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 30,985 hrs · 29,534 cycles

RIGHT CREW ESCAPE HATCH CUT OUT WEB IS CRACKED AT FS 280.00.

Part: SKIN — DENTED (TE FLAP) · airframe 30,985 hrs · 29,534 cycles

RIGHT INBD FLAP LOWER SKIN FWD OF MAIN SPAR INBD OF THE OTBD HINGE HAS TWO DENTS.

Part: TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,985 hrs · 29,534 cycles

LEFT TIE DOWN TRACK LBL 9 & FS 559+96 CORRODED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,985 hrs · 29,534 cycles

RIGHT FLOOR SEAT TRACK, FS 559+64 TO 559+80 CORRODED.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 30,985 hrs · 29,534 cycles

CARGO TIE DOWN TRACK RBL 9 AT FS 559+112 TO 574 CORRODED.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 30,985 hrs · 29,534 cycles

CARGO TIE DOWN TRACK AT LBL 9 FWD OF FS 621 CORRODED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,985 hrs · 29,534 cycles

LT & RT FLOOR SEAT TRACKS CORRODED AT FS 559+18.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,985 hrs · 29,534 cycles

LT & RT FLOOR SEAT TRACKS, FS 364 TO 409 CORRODED.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 30,985 hrs · 29,534 cycles

CARGO TIE DOWN TRACK LBL 9 AT FS 559+112 TO 574 CORRODED.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,985 hrs · 29,534 cycles

RIGHT FLOOR SILL HAS CORROSION FS 559 TO 621.

Part: STALL WARNING — ACTIVATED (COCKPIT) · airframe 30,112 hrs · 28,685 cycles

STALL FAIL CAUTION IN FLIGHT. COMPLIED WITH QRH & RETURNED.

Part: UNKNOWN — MALFUNCTIONED (LANDING GEAR) · airframe 29,698 hrs · 28,284 cycles

GEAR DISAGREE WARNING AFTER TAKEOFF WITH NOSE GEAR STATUS SHOWING CROSS HATCH SYMBOL. AFTER 5 SECONDS MSG CLEARED & GEAR RETRACTED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,299 hrs · 27,909 cycles

FLOOR EMER LIGHTING NOT FUNCTIONING FLOOR ROWS 2 - 6.

Part: DETECTOR LOOP — FAILED (LT PYLON) · airframe 28,582 hrs · 27,238 cycles

CLIMBING THROUGH 19000 FT, RECEIVED L 14TH DUCT WARNING MSG. COMPLIED WITH QRH. MSG PERSISTED. WING ANTI-ICE WAS OFF. SHOWED RED BETWEEN COWL ANTI-ICE VLV & MODULATING SOV IN 14TH STG. DECLARED AN EMERGENCY & RETURNED TO LEX. R & R LT 14TH STAGE PYLON SENSING LOOP A59WK IAW AMM 36-21. INSPECTED & RESEALED 14TH STAGE BLEED AIR DUCTS. OPERATIONS CHECKED GOOD.

Part: RVDT — FAULTY (NLG STEERING) · airframe 27,433 hrs · 26,100 cycles

4083 NWS INOPERATIVE CAUTION MSG ON INITIAL CLIMB OUT. COMPLIED WITH QRH. MESSAGE CLEARED, MESSAGE RETURNED IN CRUISE. WOULD NOT CLEAR. ON TAXI, NWS WANDERS LT TO RT. R & R LT NWS RVDT IAW AMM 32-51-20. TAXI CHECKED GOOD IAW AMM 32-51-20.

Part: CHECK VALVE — FAILED · airframe 27,133 hrs · 25,824 cycles

RECEIVED LT ENGINE OIL WARNING WITH ASSOCIATED DROP IN ENGINE OIL PRESSURE, ENGINE TO IDLE WITHIN 5 SECONDS. SHUTDOWN LT ENGINE IAW QRH. SERVICED LT ENGINE WITH 8 PTS. FOUND OIL TANK CHECK VALVE FAILED & LEAKING EXTERNALLY. R & R CHECK VALVE IAW AMM 79-12-13. OPS & LEAK CHECKED GOOD. PERFORMED 30 MIN OIL CONSUMPTION RUN, ZERO PINTS ADDED. OK FOR SERVICE.

Part: FUEL CONTROL — LEAKING (APU) · airframe 27,130 hrs · 25,796 cycles

APU STARTED, TWO FUEL LEAKS NOTED BOTH PRIOR TO AFT EQUIPMENT BAY DOOR. REQ INSPECTION. INSPECTED AND FOUND EXCESSIVE FUEL LEAK FROM APU FUEL CONTROL UNIT DRAIN. R & R APU FCU IAW AMM 49-31-01. OPS AND LEAK CHECKED GOOD.

Part: WIRE HARNESS — CHAFED (NLG) · airframe 26,642 hrs · 25,329 cycles

FOUND CHAFING ON NLG AT CENTERING PROXIMITY SENSOR HARNESS. BLENDED NLG CHAFE TO ALLOWABLE LIMITS IAW REO 601R-32-21-755.

Part: FITTING — CRACKED (WINDOW) · airframe 26,642 hrs · 25,329 cycles

COPILOTS SIDE WINDOW POST LOWER FITTING IS CRACKED, REPLACE PART.

Part: FITTING — CRACKED (WINDOW) · airframe 26,642 hrs · 25,329 cycles

PILOTS SIDE WINDOW POST LOWER FITTING IS CRACKED, REPLACE PART.

Part: STRUCTURE — CRACKED (LT NACELLE) · airframe 26,642 hrs · 25,329 cycles

LEFT UPPER CORE COWL HAS CRACK ON INBD EDGE NEAR FWD HINGE. REPAIR CRACK IAW EA 15-2013-350, TASK 71-12-01-300-826, AOL SRS 118.

Part: CHANNEL — BROKEN (BS 559-574) · airframe 26,642 hrs · 25,329 cycles

ATTACHING CHANNEL UNDER WALL LINER BROKEN UNDER 281 ALW. R & R CHANNEL IAW ARM 51-24-16, SRM 51-40-11 & SRM 51-42-06.

Part: VANE — CHAFED (LE FLAP) · airframe 26,642 hrs · 25,329 cycles

FOUND CHAFE ON CENTER L/E FLAP VANE SKIN AT FLA STA 108.135 TO BE OUT OF LIMITS. R & R SKIN IAW REO 601R-57-52-004, REV D.

Part: STEP — CRACKED (PAX DOOR) · airframe 26,642 hrs · 25,329 cycles

A CRACK & DENT ON PAX DOOR STAIR STRUCTURE WEB AROUND FASTENER HOLE BEHIND AFT DRAG ANGLE. CUT OUT DAMAGE MAKE FILLER & DOUBLER REPAIR IAW EA 15-2013-346.

Part: HANDLE — CRACKED (PAX DOOR) · airframe 26,642 hrs · 25,329 cycles

PAX DOOR INNER HANDLE CRACKED AT BALL POST INSERTION POINT. R & R HANDLE.

Part: MOUNT — CRACKED (GROUND POWER) · airframe 26,642 hrs · 25,329 cycles

ACFT GROUND POWER RECEPTACLE MOUNT IS CRACKED AT FASTENER HOLE. REPAIRED MOUNT IAW REO 601R-53-11-569, REV A.

Part: SILL — CORRODED (BS 310-349) · corrosion level 2 · airframe 26,642 hrs · 25,329 cycles

PAX DOOR LOWER SILL IS CORRODED. REMOVED CORRODED PAX DOOR SILL AND INSTALLED NEW SILL, PN 0637075-T6.

Part: SEAL — CRACKED (LT SPOILER) · airframe 26,642 hrs · 25,329 cycles

LEFT FLIGHT SPOILER CENTER SPRING SEAL CRACKED, R & R.

Part: HINGE — CRACKED (DOOR STEP) · airframe 26,642 hrs · 25,329 cycles

PAX DOOR TOP STEP HINGE CRACKED. REPLACE HINGE.

Part: STIFFENER — CRACKED (BS 524-540) · airframe 26,642 hrs · 25,329 cycles

LONGITUDIAL STIFFENER AT FS 524-540 RBL WS 47, WL 59 HAS .5 VERTICAL CRACK AT FWD & AFT END, R & R.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 26,642 hrs · 25,329 cycles

PAX DOOR AFT DRAG ANGLE CRACKED ON PREVIOUS REPAIR. R & R DRAG ANGLE IAW REO 601R-52-11-513.

Part: CARGO TRACK — CORRODED (BS 559-598) · airframe 26,642 hrs · 25,329 cycles

CARGO BAY CARGO TRACK LBL 27 AT BS 559+106, FS559+112, FS565 AND LBL9 FS484 AND FS 598 ARE CORRODED AND HAVE CORRODED ATTACHING HARDWARE. REMOVED UNSERVICEABLE CARGO TIE DOWNS DUE TO CORROSION OUT OF LIMITS AND INSTALLED SERVICEABLE CARGO TIE DOWNS IAW SRM 51-41-02, 53-61-49, AND AMM 20-21-00.

Part: STRUCTURE — DEBONDED (LT NACELLE) · airframe 26,642 hrs · 25,329 cycles

LEFT LOWER CORE COWL AT THE HINGE HAS PROTECTIVE METAL SHEET DISBONDED FROM INTERNAL COMPOSITE. FABRICATED AND INSTALLED RETAINING STRIP ON LT LOWER CORE COWL AT THE HINGE PROTECTIVE METAL SHEETING.

Part: STIFFENER — CRACKED (LT MLG) · airframe 26,642 hrs · 25,329 cycles

STIFFENER ON LT MLG CRACKED. R & R WITH NEW SERVICEABLE STIFFENER.

Part: FRAME — CRACKED (JETPIPE FAIRING) · airframe 26,642 hrs · 25,329 cycles

RIGHT JETPIPE FAIRING NR 1 FRAME CRACKED AT 3:00 POSITION AT TOOLING HOLE. REPAIRED IAW CMM 78-11-00, REPAIR SRS 043.

Part: ATTACH BRACKET — CRACKED (DOOR ASSIST) · airframe 26,642 hrs · 25,329 cycles

PAX DOOR POWER ASSIST MOTOR FWD ATTACH BRACKET IS CRACKED. REPLACED.

Part: RETAINER — CORRODED (DOOR SEAL) · corrosion level 2 · airframe 26,642 hrs · 25,329 cycles

AVIONICS DOOR SEAL RETAINER HAS CORROSIOON AND IS OUT OF LIMITS IAW SRM 52-42-00. REPLACED WITH SERVICEABLE FWD SEAL RETAINERS.

Part: PANEL — DAMAGED (RT NACELLE) · airframe 26,642 hrs · 25,329 cycles

RIGHT PYLON 422DB IS KNIFE EDGED. REPLACE KNIFE EDGED DIVIDERS ON PANEL 422DB.

Part: STRUCTURE — CHAFED (LT NACELLE) · airframe 26,642 hrs · 25,329 cycles

LEFT LOWER CORE COWL HAS 6 CHAFES ON INTERNAL COMPOSITE. MEASURED CHAFE MARKS ON LT LOWER CORE COWL INNER SKIN FOUND TO BE WITHIN SERVICEABLE LIMITS, 1 FOUND TO BE WITHIN REPAIREABLE LIMITS AND 1 FOUND TO HAVE PARTIAL PENETRATION AND REPAIRED IAW CMM 71-12-01, 2012-00 AND 71-12-01, SRS 046.

Part: ANGLE — CRACKED (BS 484) · airframe 26,642 hrs · 25,329 cycles

ANGLE CRACKED AT FS 484, RBL 27. REMOVED CRACKED ANGEL AND INSTALLED NEW SERVICEABLE ANGLE IAW SRMS 51-24-21, 51-40-11, 51-21-11, 51-25-06, 51-25-16, 51-42-06, 51-42-21.

Part: ANGLE — CRACKED (BS 280-) · airframe 26,642 hrs · 25,329 cycles

ANGLE CRACKED AT INBD & OTBD OF LBL 9 & RBL 9. R & R DISCREPANT ANGLE WITH SERVICEABLE MFG ANGLE .

Part: INTERCOSTAL — DENTED (LT NACELLE) · airframe 26,642 hrs · 25,329 cycles

LT LOWER CORE COWL HAS 8 DENTS ON INTERCOSTAL COMPOSITE. MEASURED DENTS ON LT LOWER CORE COWL, INNER SKIN 7 DENTS FOUND TO BE WITHIN SERVICEABLE LIMITS AND 1 FOUND TO HAVE PARTIAL PENETRATION AND REPAIRED IAW CMM 71-12-01 AND CMM 71-12-01 SRS 046.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 25,401 hrs · 24,124 cycles

ON APPROACH INTO MKE AT APPROX 2500 FT AGL, SELECTED FLAPS TO 8 AND RECEIVED A FLAP FAIL CAS MSG. WENT AROUND AND RECEIVED DELAY VECTORS TO RUN THE QRH AND PREPARE FOR A ZERO FLAP LANDING. DECLARED THE EMERGENCY AND MADE AN UNEVENTFUL LANDING.

Part: ESCAPE HATCH — UNSECURE (ZONE 800) · airframe 24,396 hrs · 23,123 cycles

CREW HATCH POPPED OPEN FROM REAR OF HATCH ABOUT 1 INCH. ABORTED TO AT 100 KNOTS. MAX BTMS 5,6,7,6. HES STOP INSP NOT REQUIRED IAW MXCTL.

Part: SILL — CORRODED (BS 310-349) · airframe 24,022 hrs · 22,754 cycles

PAX DOOR LOWER SILL FWD AND AFT CLEATS CORRODED. REMOVED FWD CLEAT, REMOVED CORROSION, RESTORED FINISH. REINSTALLED, REMOVED OUT OF LIMITS AFT CLEAT. LOCATED AND INSTALLED NEW CLEAT IAW SRM 51-21-06, 51-21-16, 51-42-13, 51-42-06.

Part: WARNING LIGHT — ILLUMINATED · airframe 23,687 hrs · 22,405 cycles

AT CLIMB OUT, RT STATIC HEAT, RT PITOT HEAT, RT AOA HEAT AND TAT PROBE HEAT CAUTION MESSAGES. C/W QRH WOULD NOT RESET. PERFORMED FIM RESET PROCEDURE SYS. OPS CHECKED GOOD.

Part: ACTUATOR — FAILED (LT MLG) · airframe 22,833 hrs · 21,583 cycles

GEAR SELECTED UP. NOSE AND RIGHT INDICATED UP. LEFT INDICATED DOWN. MESSAGE CLEARED & LEFT GEAR INDICATED UP AND LOCKED AFTER 30 SECONDS. ALONG GEAR DISSAGREE HAD PARK BRAKE SOV AND OTBD ANTISKID MSGS. THESE CLEARED AS WELL. R & R LT MLG SIDE STAY ACTUATOR IAW AMM 32-32-01. OPS CHECK GOOD.

Part: PRIORITY VALVE — FAILED (MLG) · airframe 22,732 hrs · 21,440 cycles

ON SELECTING GEAR UP, RECEIVED ANTI-SKID INBD CAUTION FOR 2 SECONDS, THEN MESSAGE EXTINGUISHED. R & R OF MLG PRIORITY VALVE. PERFORMED OPS CK OF ANTI-SKID SYS IAW 32-44-06, OPS CK GOOD.

Part: WIRE HARNESS — DAMAGED (LT MLG) · airframe 22,694 hrs · 21,400 cycles

AFTER TAKEOFF, RECEIVED ANTI-SKID INBD CAUTION MESSAGE. MESSAGE CLEARED WITH GEAR RETRACTION AND DID NOT RETURN WITH GEAR EXTENSION. R & R LT MLG INBD HARNESS IAW AMM 32-61-20. OPS CHECKED GOOD.

Part: CONNECTOR — DISCONNECTED (MLG) · airframe 22,515 hrs · 21,210 cycles

AFTER GEAR UP SELECTION, RECEIVED ANTI-SKID INBD CAUTION, THEN GEAR DISAGREE DOWN WHICH LASTED ABOUT 5 SECONDS. MESSAGES ALL CLEARED. TROUBLE SHOOTING FOUND A CONNECTOR ON RT INBD GEAR HARNESS DISCONNECTED, RECONNECTED CONNECTOR TO HARNESS. PERFORMED EXT AND RETRACTION TEST OF ALL GEARS IAW 32-30-00, OPS CHECK GOOD, REMOVED PLACARD AND REMOVED FROM MEL.

Part: SKIN — GOUGED (SERVICE DOOR) · airframe 21,741 hrs · 20,365 cycles

SERVICE DOOR HANDLE CUT OUT GOUGED. BLENDED OUT DAMAGE TO SMOOTH CONTOUR SERVICE DOOR CUT OUT IAW SRM 51-12-08 AND EXCEEDING MAX REPORTED DEPTH, BLEND OUTS ARE WITH LIMITS IAW REO 601R-52-41-183, REV.

Part: SKIN — DENTED (LT NACELLE) · airframe 21,741 hrs · 20,365 cycles

LT LWR CORE COWL DENT BETWEEN FWD AND AFT HINGES. REWORKED DENT BY REO 601R-71-12-4066.

Part: ANGLE — CRACKED (PAX DOOR) · airframe 21,741 hrs · 20,365 cycles

REMOVED CRACKED ANGLE, LOCATED ON UPPER FLANGE OF PAX DOOR STAIRS, THEN FABRICATED AND INSTALLED NEW ANGLE IAW REO 601R-52-11-1959.

Part: GUIDE — CHAFED (LT WING TE FLAP) · airframe 21,741 hrs · 20,365 cycles

LT OTBD FLAP ROLLER GUIDE FITTING CHAFED C/W IAW REO 601R-57-51-143.

Part: SKIN — CHAFED (WING) · airframe 21,741 hrs · 20,365 cycles

LT & RT WING CHAFING ON BOTTOM SKIN PLANK NR APPROX WS 45.0. ALSO TO INCLUDE (1) HI-LITE FASTENER HEAD ON RT WING. BLENDED AND SMOOTHED MINOR CHAFING IAW REO 601R-57-21-880. CHANGED OUT DAMAGED FASTENER IAW 601R-57-21-880.

Part: PANEL — CRACKED (PAX DOOR) · airframe 21,741 hrs · 20,365 cycles

PAX DOOR FWD STAIR STRUCTURE IS CRACKED NEXT TO FWD HANDRAIL BRACKET. REPAIRED FWD STAIR STRUCTURE NEXT TO FWD HANDRAIL BRACKET IAW REO 601R-52-11-702 REV C ZONE 2 REPAIR.

Part: PANEL — CRACKED (PAX DOOR) · airframe 21,741 hrs · 20,365 cycles

PAX DOOR AFT STAIR CRACKED NEXT TO AFT HANDRAIL 1 BRACKET AND CORNER OF 3RD STEP. REPAIRED AFT STAIR STRUCTURE NEXT TO AFT HANDRAIL BRACKET AND CORNER OF 3RD STEP. REPAIRED AFT STAIR STRUCTURE NEXT TO AFT HANDRAIL BRACKET AND CORNER OF 3RD STEP IAW REO 601R-52-11-702, REV C, ZONE 2, 3, 4.

Part: SKIN — CHAFED (LT MLG DOOR) · airframe 21,741 hrs · 20,365 cycles

LT MLG DOOR FWD CORNER CHAFED. REMOVED UNSERVICEABLE 1 FILLER AND INSTALLLED SERVICEABLE 1 FILLER IAW REO 601R-52-82-034.

Part: SKIN — CHAFED (RT MLG DOOR) · airframe 21,741 hrs · 20,365 cycles

RT MLG DOOR L/E IS CHAFED AT 2 FILLER. REMOVED CHAFED FILLER, FABRICATED NEW FILLER AND INSTALLED.

Part: SKIN — CHAFED (RT MLG DOOR) · airframe 21,741 hrs · 20,365 cycles

RT MLG DOOR (INTERIOR) IS CHAFED IN TWO PARTS. BLENDED AND REMOVED PAINT, SCRATCHES-ALODINED, PRIMED AND TOP COATED.

Part: RIB — CRACKED (LT WING) · airframe 21,741 hrs · 20,365 cycles

LT BATTERY RIB CRACKED CUT AWAY DAMAGE, FABRICATED ANGLE DOUBLER & FILLER IAW REO 601R-57-51-046. INSTALLED IAW REO 601R-57-51-046.

Part: SKIN — CHAFED (RT WING TE FLAP) · airframe 21,741 hrs · 20,365 cycles

RT INBD FLAP VANE L/E CHAFE POINTS 3 PLACES BLENDED, FOUND TO BE WITHIN LIMITS, ALODINED, PRIMED AND TEFLON TOP COATED.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 21,741 hrs · 20,365 cycles

LT OTBD FLAP VANE L/E CHAFE POINTS 3EA. BLEND AND FINISH IAW REO 601R-57-52-004, REV C. FINISH RESTORATION IAW SRM 51-21-16.

Part: ANGLE — CRACKED (BS 621) · airframe 21,741 hrs · 20,365 cycles

LT OBLIQUE ANGLE CRACKED. REMOVED UNSERVICEABLE LT OBLIQUE ANGLE AND INSTALLED SERVICEABLE ANGLE IAW SRM 51-42-21 AND REO 601R-53-61-422.

Part: ANGLE — CRACKED (BS 621) · airframe 21,741 hrs · 20,365 cycles

RT OBLIQUE ANGLE CRACKED. REMOVED UNSERVICEABLE RT OBLIQUE ANGLE AND INSTALLED SERVICEABLE ANGLE IAW SRM 51-42-21 & REO 601R-53-61-422.

Part: ENGINE — FAILED (LEFT) · airframe 21,706 hrs · 20,326 cycles

IN CLIMB, BETWEEN 8000-8500 FT A/P LT ENG MADE LOUD BANG FOLLOWED BY SHUDDERING AND VIBRATION ITT WELL ABOVE 900 DEGREES. BROUGHT LT ENGINE THRUST TO IDLE VIBRATION DAMPENED. ADVANCED ENGINE THRUST, BROUGHT NO ADDITIONAL THRUST RAN IMMEDIATE ACTION CHECKLIST FOR SEVERE ENGINE DAMAGE INFLT. COMPLIED WITH IAC AND QRH PROCEDURE MADE SINGLE ENGINE APPROACH, & LANDING. LT ENGINE WAS REPLACED. PRELIMINARY BORESCOPE NOTED COMPRESSOR DAMAGE. NO FAN DAMAGE WAS NOTED.

Part: BRAKE ASSY — LEAKING (MLG) · airframe 21,603 hrs · 20,215 cycles

LOG AFTER SHUTTING DOWN SMOKE COMING OFF LT GEAR/ BRAKE AREA, FLUID LEAKING CAUSING SMOKE AND POOLING UNDER LT MAIN GEAR. REPLACED NR 2 MLG BRAKE IAW 32-46-26. LEAK OPS CHECK GOOD.

Part: ATTACH FITTING — CORRODED (FUSELAGE) · airframe 21,714 hrs · 20,365 cycles

LOWER SECTION OF PAX DOOR DRAINAGE RAMP AREA HAS 4 CORRODED CLIPS 2 EA AT FS 320.10 & FS 338.00. REMOVED 4 CORRODED CLIPS 2EA AT FS 320.10 AND FS 338.00. THEN INSTALLED 4 NEW SERVICEABLE CLIPS 2 EA AT FS 320.10 & FS 338.00 IAW SRM 51-42-06, 51-42-21.

Part: PRESSURE BLKHD — CRACKED (BS 559) · airframe 2,001,254 hrs · 18,539 cycles

FOUND CRACK INDICATION AT FS 559, LBL9 AND WL 58.70. REPAIRED CRACK AT FS559, LBL 9 & WL 58.70 BY FULL CORPORATION OF REO 601R-53-41-260, REV E 2010/09/24 AND INCLUDING DEVIATION REO 601R-53-41-609 REV B DEVIATION E TO THE FS 559 PRESSURE BULKHEAD, LT & RT SIDES, LBL 27 TO RBL 27.

Part: STRIP — DIRTY (AILERON) · airframe 19,945 hrs · 18,476 cycles

AS SOON AS FLAPS ARE SELECTED TO 45 DEG, ACFT BECOMES UNSTABLE AROUND A LONGITUDINAL AXIS. ACFT SNAPS TO THE LT AND RT WITHOUT AILERON INPUT, AND WHEN APPLYING AILERON , CORRECTION AILERONS DOS100-0080-01 EFFECTIVE UNTIL SIGNIFICANT. CLEANED AND PAINTED INBD FLAP TEFLON ABRASION STRIP IAW AMM 27-54-01.

Part: UNKNOWN — ODOR (CABIN) · airframe 19,811 hrs · 18,344 cycles

AFTER PACKS WERE RUN ON APU 10-15 MINUTES, FUEL SMELL NOTED FROM ROWS 8-13. RAN PACKS ON ENGINE AND APU SMELL DID NOT SUBSIDE. INSPECTED A/C, NO EXTERNAL LEAKS NOTED. INSPECTED APU ENCLOSURE WITH APU RUNNING, NO LEAKS NOTED. RAN PACKS ON APU AND ENGINE BLEEDS. NO DISCREPANCIES NOTED AT THIS TIME.

Part: CARGO TRACK — CORRODED (BS 559-579) · airframe 17,143 hrs · 15,626 cycles

CARGO BAGGAGE RAIL BTW FS 574 AND 559+112, LBL 9.00 IS CORRODED. CARGO BAGGAGE RAIL BTW FS 574 AND 559+112, LBL 9.00. REPLACED IAW AMM 53-01-11-400-802. (K)

Part: CARGO TRACK — CORRODED (BS 621) · corrosion level 2 · airframe 17,143 hrs · 15,626 cycles

CARGO BAGGAGE RAIL FWD OFFS 621.00, LBL 9.00 IS CORRODED. NEW RAIL INSTALLED IAW SRM 51-41-04. (K)

Part: CARGO TRACK — CORRODED (BS 559-574) · corrosion level 2 · airframe 17,143 hrs · 15,626 cycles

CARGO BAGGAGE RAIL BTW FS 574 AND FS 559+112, RBL 9.0 IS CORRODED. CARGO BAGGAGE RAIL BTW FS 574 AND FS 559+112, RBL 9.0 REPLACED IAW AMM 53-01-11-400-802. (K)

Part: CARGO TRACK — CORRODED (BS 559) · corrosion level 2 · airframe 17,143 hrs · 15,626 cycles

CARGO BAGGAGE RAIL BTW FS 559+80 AND FS 559+96, LBL 27.00 IS CORRODED. CARGO BAGGAGE RAIL BTW FS 559+80 AND FS 559+96, LBL 27.00. REPLACED IAW AMM 53-01-11-400-802. (K)

Part: ANCHOR FITTING — CORRODED (CARGO BAY) · corrosion level 2 · airframe 17,143 hrs · 15,626 cycles

CARGO ANCHOR PLATE FWD OF FS 605.00, LBL 9.00 IS CORRODED. REPLACED ANCHOR IAW SRM 51-41-04. (K)

Part: PRESSURE BLKHD — CRACKED (BS 202) · airframe 17,143 hrs · 15,626 cycles

FWD PRESSURE BULKHEAD WEB AT 202.75, LBL 23.71, WL 69.79 IS CRACKED. FWD PRESSURE BULKHEAD WEB AT FS 202.75, LBL 23.71, WL 69.79 REPAIRED IAW REO 601R-53-11-563. (K)

Part: FLOORBEAM — CRACKED (BS 280) · airframe 17,143 hrs · 15,626 cycles

UPPER AFT ANGLE ON CROSSBEAM AT FS 280.00, LBL 9.0, WL 72.00 IS CRACKED. CRACK LENGTH IS .350. UPPER AFT ANGLE ON CROSSBEAM AT FS 280.00, LBL 9.00, WL 72.00. REPAIR IAW REO 601R-53-11-136, REV A. (K)

Part: FLOORBEAM — CRACKED (BS 280) · airframe 17,143 hrs · 15,626 cycles

CROSSBEAM AT FS 280.00, RBL 9.00, WL 71.00 IS CRACKED IN THE LOWER RADIUS. CROSSBEAM AT FS 280.00 RBL 9.00, WL 71.00 REPAIRED IAW REO 601R-53-11-171, REV D. (K)

Part: SEAT TRACK — CORRODED (BS 559) · corrosion level 2 · airframe 17,143 hrs · 15,626 cycles

SEGMENT TRACK BTWN FS 559+80 AND FS 559+96 CORRODED. SEGMENT TRACK BTWN FS559+80 AND FS 559+96, RBL 9.00 REPLACED IAW SRM 51-41-04. (K)

Part: ATTACH FITTING — CRACKED (BS 484) · airframe 17,143 hrs · 15,626 cycles

CLIP AT FS 484.00, RBL 27.00, WL 72.00 IS CRACKED. CRACKED LENGTH .200 INCH CLIP AT FS 484.00, RBL 27.00, WL 72.00 REPLACED IAW SRM 51-42.06. (K)

Part: ATTACH FITTING — CRACKED (BS 484) · airframe 17,143 hrs · 15,626 cycles

CLIP AT FS 484.00, LBL 27.00, WL 72.00, IS CRACKED. CRACKED LENGTH .250" CLIP AT FS 484.00, LBL 27.00, WL 72.00, REPLACED IAW SRM 51-42-06. (K)

Part: INTERCOSTAL — CRACKED (BS 484) · airframe 17,143 hrs · 15,626 cycles

INTERCOSTAL AT FS 484.00, LBL 36.00, WL 72.00 IS CRACKED. CRACK LENGTH IS .400 ". REPAIRED IAW REO 601R-53-41-059, REV A. (K)

Part: INTERCOSTAL — CRACKED (BS 484) · airframe 17,143 hrs · 15,626 cycles

INTERCOSTAL AT FS 484.00, RBL 36.00, WL 72 IS CRACKED. CRACK LENGTH IS .600 INCH. REPAIRED IAW REO 601R-53-41-059, REV A. (K)

Part: TARGET — LOOSE (MLG UPLOCK) · airframe 16,132 hrs · 14,654 cycles

LOG 198286/3 - RT MLG DISAGREE LIGHT CAME ON DURING RETRACTION. INSP BOTH NLG AND MLG WITH NO FAULTS FOUND. MX ACTION C/W PLACED ON MEL. LOG 198286/4 FOUND UPLOCK TARGET EXCESSIVELY LOOSE, RESECURED AND OP CHECKS IAW AMM 32-61-05 AND 32-30-00. OPS CHECKS GOOD, REMOVE FROM MEL. (K)

Part: O-RING — MISSING (LT ENGINE) · airframe 15,134 hrs · 13,702 cycles

AT CRUISE SPEED RECEIVED LT ENG OPERATION WARNING MESSAGE AND OIL PRESSURE INDICATED 25-36 PSI. MESSAGE RECURRED AND PRESSURE DROPPED TO 25 PSI SEVERAL TIMES IN FLIGHT. INSPECTED NR 1 ENG AND FOUND OIL LEAKING FROM SCAVENGE FILTER. UPON REMOVING FILTER FOUND O-RING MISSING. REPLACED O-RING AND FILTER IAW AMM 79-21-05. LEAK CHECK GOOD. (S)

Part: IDG — INOPERATIVE (NR 2) · airframe 13,478 hrs · 12,121 cycles

ON T/O ROLL RECEIVED (IDG 2) CAUTION MESSAGE FOLLOWED BY (GEN 2 OFF) CAUTION MESSAGE. ABORTED T/O AT APPROXIMATELY 70 KNOTS, MAX BTMS READINGS = 3,3,2,3. FOUND FAULT MESSAGE CHANGED AFTER IDG WAS PREVIOUSLY CHANGED FROM (NR 2 GEN OFF) MESSAGE TO (IDG 2) MESSAGE. RT GEN TO PYLON HARNESS CONTINUITY CHECK GOOD. RT GEN WAS LOW ON OIL, TOOK 24 PUMPS. FOUND SHAFT SEAL DAMAGED. REPLACED IDG IAW CHAP 24. LEAK AND OPS CHECK GOOD. (K)

Part: SKIN — CORRODED (FUSELAGE)

FOUND CORROSION ON SKIN CUT OUT OF MAIN AVIONIC DOOR SURROUND. MAINTENANCE PERFORMED BOMBARDIER MODSUM 601R53210045 TO COMPLY WITH REO 601R-53-21-781. (M)

Part: SKIN — CORRODED (E/E BAY DOOR)

FOUND CORROSION ON AVIONIC DOOR INNER SKIN AT FS 364 BTW STRINGER 25L TO STRINGER 25R. MAINTENANCE PERFORMED REPAIR TO AVIONIC DOOR APERTURE INNER DOUBLER FS 364 TO FS 379 STRINGER 27 TO STRINGER 25R IAW REO 601R-53-21-781. (M)

Part: RETAINER — CORRODED (E/E BAY DOOR)

CORROSION FOUND ON FORWARD SEAL RETAINER OF THE MAIN AVIONICS COMPARTMENT DOOR. SEAL RETAINER P/N 601R14533-41, CC670-386743 AND CC 670-38663-5 REPLACED IAW SRM 51-42-06. (M)

Part: DOOR — OUT OF RIG (EMERGENCY EXIT) · airframe 12,446 hrs · 11,123 cycles

110612 MWC NR 53 CREW ESCAPE HATCH FAILED FUNCTIONAL TEST, ADJUSTMENT TO BE CARRIED OUT IAW AMM 52-22-00-820-801. CREW ESCAPE HATCH RIGGED IAW AMM 52-22-00-820-801. CREW ESCAPE HATCH RIGGED IAW AMM 52-22-00-820-002. (K)

Part: CONTROL UNIT — MALFUNCTIONED (STAB TRIM) · airframe 11,818 hrs · 10,510 cycles

STAB TRIM RUNAWAY AFTER TAKEOFF, QRH COMPLIED WITH, RETURNED TO DEPARTURE. REMOVED AND REPLACED HORIZONTAL STAB TRIM CONTROL UNIT IAW AMM REF 27-41-01 AND FOUND SERVICEABLE. (K)

Part: PRIORITY VALVE — MALFUNCTIONED (NLG)

GEAR DISAGREE AFTER TAKEOFF. NOSE GEAR DID NOT COME OUT OF DOWN AND LOCKED. AIRSPEED MAINTAINED LESS THAN 190 KNOTS COMPLIED WITH QRH ALL GEAR WENT DOWN AND LOCKED AS NORMAL. REMOVED AND REPLACED NLG PRIORITY VALVE P/N 4622 IAW CRJ AMM 32-33-51. (M)

Part: CHECK VALVE — MALFUNCTIONED (RAM AIR)

AFTER TAKEOFF, HAD RIGHT PACK OVERTEMP MESSAGE AND SMOKE FROM AIR CONDITIONING VENTS. TURNED RIGHT PACK OFF AND SMOKE CLEARED. REMOVED AND REPLACED RAM AIR CHECK VALVE. INSPECTED RIGHT PACK, FOUND BLOWN GASKET ON PLATE ABOVE OIL SIGHT GAUGE, REF 148439/4. (M)

Part: ACTUATOR — MALFUNCTIONED (TE FLAPS)

FLAPS FAIL MESSAGE ILLUMINATED IN FLIGHT. ON APPROACH, FLAPS INDICATED 38 DEGREES. COMPLIED WITH QUICK REFERENCE HANDBOOK. REMOVED AND REPLACED LEFT OUTER OUTBOARD FLAP ACTUATOR S/N OFF 1686, LT OUTER INBOARD FLAP ACTUATOR S/N OFF 1851, RT INBOARD OUTER FLAP ACTUATOR S/N OFF 1890. (M)

Part: IDG — INOPERATIVE (ENGINE) · airframe 9,203 hrs · 7,995 cycles

IDG1 CAUTION ILLUMINATED ON T/O ROLL. ABORTED TAKEOFF AT 60 KNOTS. BTMS ALL GREEN. RESET GEN 1 OK. ACTION TAKEN: REMOVED AND REPLACED IDG NR 1. OPS AND LEAK CHECK GOOD. (K)

Part: DCU — MALFUNCTIONED (TE FLAPS) · airframe 8,670 hrs · 7,486 cycles

AFTER DEPARTURE, UPON FLAP RETRACTION, FLAP FAIL CAUTION MESSAGE APPEARED ON ED1 FLAP POSITION INDICATION ON ED1 READS ZERO DEGREES, FLIGHT CONTROL PAGE ALSO READS ZERO ON ED2. RETURN TO DEPARTURE FOR (FLAP ZERO LANDING). FOUND GROUND PROXIMITY MESSAGE ON MDC CH1 AND CH2. SHOOK WIRING FROM LT BPSU TO FECU - NO DEFECTS. EXCEPT POT NR 6GH7 OUT OF TOLERANCE. ADJ FECU POT 6.7 IAW. REMOVED AND REPLACED DCU NR 1, OK FOR SERVICE. HES INSPECTION NOT REQUIRED IAW MM. (K)

Part: DRAG ANGLE — DAMAGED (PAX DOOR) · airframe 7,483 hrs · 6,386 cycles

PAX DOOR AFT DRAG ANGLE CRACKED NEAR UPPER SUPPORT PULLEY. REPAIRED AFT DRAG ANGLE BY REMOVING DAMAGE, PERFORMED EDDY CURRENT INSPECTION, FABRICATED AND INSTALLED REPAIR PIECES IAW REO. (K)

Part: ANGLE — CRACKED (FUSLEAGE) · airframe 7,482 hrs · 6,385 cycles

LT OBLIQUE ANGLE AT FS 625, CRACKED ON AFT SIDE .5 INCHES LONG. REMOVED OBLIQUE ANGLE LT FS 625, INSTALLED NEW SERVICEABLE ANGLE IAW SRM. (K)

Part: ANGLE — CRACKED (FUSELAGE)

RT OBLIQUE ANGLE AT FS 625 CRACKED ON AFT EDGE APPROX 1 INCH LONG. REMOVED OBLIQUE ANGLE RT FS 625, INSTALLED NEW SERVICEABLE ANGLE IAW SRM. (K)

Part: FLOORBEAM — CRACKED (FUSELAGE)

LT SIDE FLOOR SUPPORT ANGLE AT FS 621 CRACKED APPROX 1.1 INCH LONG LBL 41.5, WL 73. CUT AWAY DAMAGED SECTION OF ANGLE AND INSTALLED REPAIR ANGLE IAW BOMBARDIER, INC REO 601R-53-61-117 REV C. (M)

Part: FLOORBEAM — CRACKED (FUSELAGE)

RIGHT SIDE FLOOR SUPPORT ANGLE AT FS 621 CRACKED APPROX 1.1 INCH LONG, RBL 41.5 WL 73. REPAIRED RIGHT SIDE FLOOR SUPPORT ANGLE AT FS 621 BY CUTTING AWAY DAMAGED AREA AND INSTALLED MG REPAIR PARTS IAW BOMBARDIER REO 601R-53-61-117 REV C. (M)

Part: CLIP — CRACKED (FUSELAGE)

CLIP AT FS 280, RBL 9, OUTBOARD SIDE IS CRACKED IN RADIUS APPROX .70 INCH LONG. (M)

Part: HINGE — CRACKED (ESCAPE HATCH) · airframe 7,482 hrs · 6,385 cycles

CREW ESCAPE HATCH HINGES ARE CRACKED AROUND BASE. REPLACED BOTH HINGE ARMS WITH NEW HINGE ARMS IAW REO SRM. (K)

Part: INTERCOSTAL — CRACKED (FUSELAGE)

LEFT INTERCOSTAL AT FS 484, LBL 27, IS CRACKED IN RADIUS APPROX .30 INCH LONG. REMOVED CRACKED ANGLE, P/N 601R31171-17. FABRICATED NEW ANGLE USING PERFORMED ANGLE P/N S6444-14 ETCHED, PRIMED, TOP COATED FABRICATED ANGLE. INSTALLED FABRICATED ANGLE ON LEFT SIDE, INTERCOSTAL FS 484, RBL 27, IAW BOMBARDIER REO 601R-53-41-059 AND BR. (M)

Part: INTERCOSTAL — CRACKED (FUSELAGE)

LEFT SIDE INTERCOSTAL AT FS 484, LBL S7, IS CRACKED IN RADIUS APPROX .30 INCH LONG. (M) REMOVED CRACKED ANGLE FABED NEW ANGLE USING PREFORMED ANGLE. ETCHED, ALODINED, PRIMED, AND TOP COATED FABED ANGLE. INSTALLED FABED ANGLE ON LT SIDE INTERCOSTAL FS 484, LBL 27, IAW MFG REO. (K)

Part: CLIP — CRACKED (FUSELAGE)

CLIP AT FS 280, RBL 9, INBOARD SIDE IS CRACKED IN RADIUS APPROX .40 INCH LONG. REMOVED CRACKED CLIP AT FS 280 RBL 9 LEFT SIDE AND INSTALLED NEW CLIP IAW CRJ 200 SRM 51-40-11, 51-23-00, 51-42-06 AND 51-42-21. (M)

Part: CLIP — CRACKED (FUSELAGE)

CLIP AT FS 280, LBL 9, OUTBOARD SIDE, IS CRACKED IN RADIUS APPROX .50 INCH LONG. REMOVED CRACKED CLIP AT FS 280 LBL 9 OUTBOARD SIDE AND REPLACED WITH NEW CLIP P/N 601R31113-57 IAW CRJ200 SRM 51-42-06 AND 51-42-21. (M)

Part: INTERCOSTAL — CRACKED (FUSELAGE)

LEFT SIDE INTERCOSTAL AT FS 484, LBL 36 IS CRACKED IN RADIUS APPROX .20 INCH LONG. REPAIRED LEFT SIDE INTERCOSTAL AT FS 484 LBL 36 IAW BOMBARDIER REO 601R-53-41-059 REV A AND BRAS STANDARD REPAIR 601R-53-0030. (M)

Part: INTERCOSTAL — CRACKED (FUSELAGE)

RIGHT SIDE INTERCOSTAL AT FS 484, RBL 36, IS CRACKED IN FLANGE FROM TOP RIVET HOLE TO EDGE, APPROX .35 INCH LONG. REPAIRED RIGHT SIDE INTERCOSTAL AT FS 484 RBL 36 IAW BOMBARDIER REO 601R-53-41-059 REV A AND BRAS STANDARD REPAIR 601R-53-0030. (M)

Part: APU — MAKING METAL (APU) · airframe 6,875 hrs · 5,859 cycles

APU FAULT CONDITION IN FLIGHT. SMOKE APPEARED IN CABIN. CLOSED PACKS AND SHUTDOWN APU. INSPECTED APU COMPARTMENT, NO FUEL OR OIL LEAKS NOTED CHECKED BOTH ACM`S IAW AMM. OIL LEVEL CHECK GOOD. CHECKED APU OIL LEVEL IAW AMM. OIL LEVEL GOOD. FOUND METAL INSIDE APU, REMOVED AND REPLACED APU. OPS CHECK AND LEAK CHECK GOOD. (K)

Part: SKIN — DAMAGED (NACELLE)

DURING POST FLIGHT WALK AROUND, RIGHT ENGINE COWLING DISCOVERED POSSIBLY OPENED IN FLIGHT. DAMAGED NOTED. (M) REMOVED AND REPLACED DOOR INSTALL LOWER CORE COWL. OPS CHECK GOOD. (K)

Part: ODOR — DETECTED (CABIN)

STRONG ODOR OF EXHAUST NOTED WHEN THRUST LEVERS ADVANCED. OPERATED PACKS AND COULD SMELL FAINT ODOR OF DIESEL. OPERATED PACKS ON APU FOR SEVERAL MINUTES, ODOR FADED. BELIEVE AIRSTART CART INGESTED ITS OWN EXHAUST. OPERATED PACKS ON BOTH ENGINES, ODOR DID NOT RETURN, AMM 21-51-00. (M)

Part: HANDLE — FAILED (MLG SELECTOR)

LANDING GEAR DID NOT RETRACT AFTER TAKEOFF. PARKING BRAKE SHUT-OFF VALVE MESSAGE AND ANTI-SKID IB MESSAGE. COMPLIED WITH QRH, RETURNED TO COS WITH UNEVENTFUL LANDING. REMOVED AND REPLACED GEAR SELECTOR HANDLE IAW MM FUNCTION AND OPS CHECK GOOD.

Part: SKIN — DENTED (FUSELAGE)

TEMPORARY REPAIR ON RT FORWARD FUSELAGE SKIN JUST FORWARD OF FS 202.75 BULKHEAD, DENT 4 INCHES BY .062 INCH DEEP. TEMP REPAIR WAS PERFORMED IAW REO 601R-53-11-327. PERFORMED A MAJOR REPAIR TO FUSELAGE SKIN AT FS 202.75 TO FS 204, BETWEEN STRINGERS 12R AND 13R BY REMOVING TEMPORARY REPAIR, RE-CONTOURING DAMAGED AREA, PERFORMING EDDY CURRENT INSPECTION, INSTALLING THREE RIVETS, APPLYING PROTECTIVE TREAT AND FINISH. (M)

Part: SKIN — DAMAGED (FUSELAGE)

TEMPORARY REPAIR ON RT FORWARD FUSELAGE SKIN JUST FORWARD OF FS 202.75 BULKHEAD, DENT 4 INCH LOG BY .062 INCH DEEP, TEMP REPAIR WS PERFORMED PER REO 601R-53-11-327. COMPLIED WITH STEPS 1 THROUGH 3 OF WVAC EO NR 601R-53-4413. PERFORMED EDDY CURRENT INSPECTION TO COMPLY WITH STEP 24 OF WVAC EO 601R-53-4413 OF RIGHT FWD FUSELAGE REPAIR. NO INDICATIONS NOTED AT THIS TIME. COMPLIED WITH STEPS 5 AND 6 OF WVAC EO 601R-53-4413. (M)

Part: VANE — CHAFED (TE FLAP)

LEFT OUTBOARD FLAP FIXED VANE LEADING EDGE CAP, P/N 601R-14574-7 IS CHAFED AT WS 297 APPROXIMATELY .25 INCH BY .5 INCH AND .001 DEEP. PERFORMED MAJOR REPAIR TO THE LEFT OUTBOARD FLAP LEADING EDGE FIXED VANE BY REMOVING AND REPLACING LEADING EDGE CAP P/N 601R-14574-7 IAW CRJ200 SRM 57-53-00, 51-40-11 AND 51-42-13. (M)

Part: VANE — CHAFED (TE FLAPS)

RIGHT INBOARD FLAP LEADING EDGE MOVEABLE VANE LEADING EDGE HAS THREE MINOR CHAFES AT WS 56.177, WAS 104.429 AND WS 140.364. ALL THREE CHAFES ARE LESS THAN .001 INCHE DEEP. PERFORMED A MAJOR REPAIR TO RIGHT INBOARD FLAP LEADING EDGE MOVEABLE VANE LEADING EDGE AT WS 56.177, WS 104.429 AND WS 140.364 BY BLENDING DAMAGED AREAS, RESTORING FINISH AND APPLYING TEFLON FILLED ABRASION RESISTANT COATING IAW BOMBARDIER, INC REO 601R. (M)

Part: VANE — CHAFED (TE FLAP)

LT INBOARD FLAP LEADING EDGE MOVEABLE VANE LEADING EDGE HAS 2 MINOR CHAFF AREAS AT WS 56.177 AND WS 104.429. BOTH CHAFES ARE LESS THAN .001 INCH DEEP. PERFORMED A MAJOR REPAIR TO LEFT INBOARD FLAP LEADING EDGE MOVEABLE VANE LEADING EDGE AT WS 56.177 AND WSL 104.429 BY BLENDING DAMAGED AREAS, RESTORING FINISH AND APPLYING TEFLON FILLED ABRASION RESISTANT COATING IAW BOMBARDIER, INC REO 601R-57-52-004 REV. (M)

Part: BATTERY — DISCHARGED (CABIN)

COCKPIT EMERGENCY LIGHT BATTERY IS DEAD. REMOVED AND REPLACED COCKPIT OVERHEAD EMERGENCY LIGHT, OPERATIONAL CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: PROX SWITCH — BROKEN (RT SPOILER)

FLT NR 6429 - IAD-JFK - DURING CLIMB-OUT, RETURNED TO IAD DUE TO THE SPOILER ADVISOR LIGHT ILLUMINATING. AIRCRAFT LANDED AND RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE OPENED DMI NR 07697 IAW MEL 27-9-3 ON THE SPOILER ADVISORY SYSTEM. MAINTENANCE LATER CLEARED DMI NR 07697 ON 02-04-95 BY REPAIRING THE SPLICE ON THE RT OUTBOARD GROUND SPOILER PANEL PROXIMITY SWITCH. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (Z)