N369CA

Part: ENGINE — STALLED (NR 1) · airframe 6,825 hrs · 2,709 cycles

IN CRUISE THE # 1 ENGINE DID AN UNCOMMANDED SHUTDOWN. THE CREW RESTARTED THE ENGINE BUT OBSERVED THAT THE ITT WAS HIGHER THAN THE OTHER ENGINES. THE POWER LEVER FOR THE # 1 ENGINE WAS BROUGHT BACK TO IDLE AND THE AIRCRAFT DIVERTED TO KTEB.

Part: INTERCOSTAL — CORRODED (BS 319-349) · airframe 36,474 hrs · 27,016 cycles

INTERCOSTAL BS 319.7 - 349 AT STRINGER 20R HAD SIGNS OF CORROSION. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 51-42-06, 53-21-23, 51-42-21, 51-40-11, 51-25-16, 51-21-11, 51-21-06, AND AMM 53-21-23.

Part: DRAG ANGLE — CRACKED (VERTICAL STAB) · airframe 36,474 hrs · 27,016 cycles

LEFT VERTICAL STABILIZER AFT DRAG ANGLE WAS CRACKED AT BS 1200. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED A REPAIR IAW REO 670-55-31-018, REV.

Part: DRAG ANGLE — CRACKED (VERTICAL STAB) · airframe 36,474 hrs · 27,016 cycles

VERTICAL STABILIZER FWD DRAG ANGLE WAS CRACKED AT BS 1200. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED A REPAIR IAW REO 670-55-31-018, REV A, AND 670-55-31-108.

Part: INTERCOSTAL — CORRODED (BS 310-333) · airframe 36,474 hrs · 27,016 cycles

INTERCOSTAL AT BS 310 TO 333, STINGER 21L HAD SIGNS OF CORROSION. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 53-21-23, 51-42-06, 51-40-11, 51-42-21, 51-42-13, 51-25-16, AND 51-21-11.

Part: STRIKER — CORRODED (GALLEY DOOR SEAL) · airframe 36,474 hrs · 27,016 cycles

GALLEY SERVICE DOOR LOWER SEAL STRIKER HAD SIGNS OF CORROSION AROUND FASTENER HOLES. REMOVED AND REPLACED THE GALLEY SERVICE DOOR LOWER SEAL STRIKER IAW SRM 51-42-21, 51-25-21, 51-40-11, 51-42-06, AND 51-25-06.

Part: FRAME — CORRODED (BS 319.7) · airframe 36,474 hrs · 27,016 cycles

THE FRAME AT BS 319.70, BETWEEN STRINGERS 18L - 21L HAD SIGNS OF CORROSION. REMOVED AND REPLACED THE FRAME SECTION BETWEEN STRINGERS 18L - 21L IAW SRM 51-42-06, 51-42-21, 51-40-11, 51-25-16, AND 51-21-11.

Part: BRACKET — CRACKED (PAX DOOR) · airframe 36,474 hrs · 27,016 cycles

PAX DOOR OTBD CLOSE ASSIST BRACKET WAS CRACKED. REMOVED AND REPLACED THE BRACKET IAW SRM 51-42-06, AND 51-42-10.

Part: ANGLE — CORRODED (PAX DOOR) · airframe 36,474 hrs · 27,016 cycles

PASSENGER DOOR MID-CAP ANGLE HAD SIGNS OF CORROSION. REMOVED AND REPLACED THE PASSENGER DOOR MID-CAP ANGLE IAW SRM 51-41-02.

Part: FIRE SEAL — TORN (LT NACELLE) · airframe 36,474 hrs · 27,016 cycles

LEFT LOWER ENGINE COWLING DRAIN PAN FIRE SEAL WAS TORN. REPAIRED THE FIRE SEAL IAW REO 670-54-23-959, REV E, AND REO 670-54-23-1166.

Part: SKIN — GOUGED (BS 969-977) · airframe 36,474 hrs · 27,016 cycles

FUSELAGE SKIN GOUGED AT BS 977, STRINGER 27. REPAIRED THE SKIN IAW REO 670-53-135, AND REO 670-53-00-290, REV D.

Part: PLATE — CORRODED (LEFT) · airframe 36,474 hrs · 27,016 cycles

OVERWING EMERGENCY EXIT RT AND LT STEP PLATES HAD SIGNS OF CORROSION AROUND FASTENER HOLES. EVALUATED THE LT AND RT OVERWING EXIT STEP PLATES, RT STEP PLATE HAD NO CORROSION NOTED, CLEANED AND RESTORED FINISH IAW SRM 51-25-21, 51-21-11, AND 51-25-06. THE LT STEP PLATE WAS FOUND TO BE OUT OF LIMITS IAW SRM 53-41-06, REMOVED AND REPLACED THE LT STEP PLATE IAW AMM 20-21-00.

Part: WEB — CRACKED (FUSELAGE) · airframe 36,474 hrs · 27,016 cycles

RT FLOOR WEB IN FORWARD EQUIPMENT COMPARTMENT IS CRACKED. REPAIRED RT FLOOR WEB IN FORWARD EQUIPMENT COMPARTMENT IAW REO 670-53-11-509 REV D DATED 2016-06-29 AND NDTM PART 1 51-20-006.

Part: SEAT TRACK — CORRODED (BS 581-691) · airframe 36,474 hrs · 27,016 cycles

LEFT SEAT TRACK, BS 581 - 691 WAS CORRODED BEYOND LIMITS. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49.

Part: BRACKET — CRACKED (RT SLAT TRACK) · airframe 36,474 hrs · 27,016 cycles

RIGHT WING SLAT TRACK 1 - 3 HOUSING BRACKET WAS CRACKED. REPAIRED THE BRACKET IAW REO 670-57-42-577, REV--.

Part: SEAT TRACK — CORRODED (B 485-581) · airframe 36,474 hrs · 27,016 cycles

LEFT SEAT TRACK FROM BS 485 - 581 WAS CORRODED BEYOND LIMITS. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49.

Part: SEAT TRACK — CORRODED (BS 485-581) · airframe 36,474 hrs · 27,016 cycles

RIGHT SEAT TRACK, BS 485 - 581 WAS CORRODED BEYOND LIMITS. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49.

Part: SEAT TRACK — CORRODED (BS 581-691) · airframe 36,474 hrs · 27,016 cycles

RIGHT SEAT TRACK, BS 581 - 691 WAS CORRODED BEYOND LIMITS. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49.

Part: WEB — CRACKED (BS 193) · airframe 36,474 hrs · 27,016 cycles

LEFT FLOOR WEB IN THE FWD EQUIPMENT BAY WAS CRACKED. REPAIRED THE WEB AT BS 193 IAW REO 670-53-11-509, REV D.

Part: ANGLE — CRACKED (PAX DOOR HANDLE) · airframe 36,474 hrs · 27,016 cycles

PAX DOOR INNER ANGLE FOR DOOR LATCH MECHANISM CRACKED. REPLACED THE ANGLE IAW SRM 51-25-21, 51-21-11, AND 51-42-06.

Part: BRACKET — BENT (DOOR PULLEY) · airframe 36,474 hrs · 27,016 cycles

PAX DOOR SUPPORT WHEEL CABLE, LOWER PULLEY BRACKET WAS BENT. REMOVED AND REPLACED THE LOWER PULLEY BRACKET IAW SRM 51-40-11, 51-42-06, 51-25-21.

Part: RETAINER — DAMAGED (FWD CARGO DOOR) · airframe 36,474 hrs · 27,016 cycles

FWD CARGO DOOR AFT, LOWER INBD AND OTBD SEAL RETAINERS WERE BENT AND GOUGED. REPAIRED IAW REO 670-42-35-127, AND SRM 51-21-16.

Part: COVER — BROKEN (EMERGENCY EXIT) · airframe 35,284 hrs · 25,913 cycles

RIGHT EMERGENCY EXIT HANDLE COVER BROKEN OFF. REPLACED THE HANDLE COVER IAW NEF 25-100-6.

Part: WARNING MESSAGE — ILLUMINATED (DOOR HANDLE) · airframe 35,050 hrs · 25,699 cycles

SERVICE DOOR OUTER HANDLE CAUTION MESSAGE.

Part: WARNING MESSAGE — ILLUMINATED (PAX DOOR HANDLE) · airframe 34,595 hrs · 25,273 cycles

PAX DOOR OUTER HANDLE CAUTION.

Part: STRINGER — CORRODED (BS 517-533) · airframe 33,646 hrs · 24,450 cycles

STRINGER 24L BETWEEN BS 517-533 CORRODED. REPAIRED IAW SRM 53-00-03, 51-42-06, 51-42-21, 51-42-13, 51-21-11, 51-25-16, 51-25-06, AND AMM 51-21-01.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 33,646 hrs · 24,450 cycles

DAMAGE TO FUSELAGE SKIN INTERIOR SURFACE BETWEEN FS517-FS533 AND STR 20-21L. BLENDED DAMAGE AND RESTORED FINISH IAW REO 670-53-31-407, DATED 2017-03-07, SRM 51-25-16, 51-21-11, AND 51-25-06. NDT PERFORMED.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 33,646 hrs · 24,450 cycles

SKIN SIDE FOOT OF INTERCOSTAL ANGLE LBL24 HAS SIGNS OF CORROSION. REPAIRED BY BLENDING IAW REO 670-53-32-030 REV_ 2017-3-08. NDT PERFORMED. NO CRACK INDICATIONS NOTED.

Part: STRINGER — CORRODED (BS 517-533) · airframe 33,646 hrs · 24,450 cycles

SIGNS OF CORROSION ON STRINGER 21L BETWEEN BS 517 AND 533. BLENDED AND RESTORED FINISH IAW SRM 53-31-03, 51-42-06, 51-21-11, 51-25-06, AND 51-25-16. FOUND TO BE WITHIN ALLOWABLE LIMITS.

Part: AILERON — GOUGED (LT WING) · airframe 33,646 hrs · 24,450 cycles

LT AILERON IB TRAILING EDGE GOUGED. REPAIRED LT AILERON IB TRAILING EDGE IAW REO 670-57--61-001 REV C, DATED 2012-01-16. NDT PERFORMED.

Part: SKIN — DAMAGED (RIGHT WING) · airframe 32,162 hrs · 23,347 cycles

WHILE PERFORMING SB 670BA-57-020, REV C, FOUND 2 EA FASTENERS IN THE RT WING PLANK TO BE OVERSIZE.

Part: BULKHEAD — DAMAGED (BS 202) · airframe 32,162 hrs · 23,347 cycles

FS 202.75 FWD SIDE OF BULKHEAD, LBL30 STIFFENER HAS AN INDICATION .25" LONG IN THE UPPER EDGE OF FLANGE. FAILED NDT INSPECTION.

Part: FRAME — CRACKED (BS 235) · airframe 32,162 hrs · 23,347 cycles

RT FS 235 HAS AN INDICATION .200" LONG PROPAGATING FROM THE RADIUS AT STR 13A.

Part: MOUNT — DISCONNECTED (DOOR) · airframe 31,760 hrs · 23,028 cycles

MAIN CABIN LT HANDLE MOUNT DISCONNECTED. POSITIONED MAIN CABIN LT HANDLE MOUNT IAW AMM 52-11-05. OPERATIONS CHECKED GOOD.

Part: STRUCTURE — SCRATCHED (RT HORIZ STAB) · airframe 31,637 hrs · 22,935 cycles

RIGHT HORIZONTAL STABILIZER IS SCRATCHED. CUT OUT, OUT OF LIMITS DAMAGE, FABRICATED & INSTALLED REPAIR PARTS IAW REO 670-55-11-314 DATED 15 FEB 2016. BLENDED & RESTORED FINISH IAW REO 670-55-11-001 DATED 17 NOV 2004.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 31,637 hrs · 22,935 cycles

PASSENGER DOOR AFT DRAG ANGLE 1/2 WAY UP IS CRACKED. R & R DAMAGED DRAG ANGLE SECTION PN 601R31772-5 IAW SRM 51-42-13, 51-42-06, 51-40-11, 51-25-06 & 51-25-16.

Part: SUPPORT BRACKET — CRACKED (PAX DOOR) · airframe 31,637 hrs · 22,935 cycles

PASSENGER DOOR, AFT LOWER PULLEY SUPPORT BRACKET IS CRACKED. R & R PAX DOOR AFT LOWER PULLEY SUPPORT BRACKET, PN 601R317186-1, IAW SRM 51-42-06, AMM 52-11-13, 52-11-13-400-802.

Part: CABLE — FRAYED (PAX DOOR) · airframe 31,637 hrs · 22,935 cycles

PASSENGER DOOR, ASSIST CABLE IS FRAYED. R & R PAX DOOR ASSIST CABLE, PN 2R59573001-1SD, IAW AMM 52-11-08.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 31,637 hrs · 22,935 cycles

AFT WING TO FUSELAGE FAIRING SUPPORT STRUCTURE, LT BRACKET CRACKED FS 939.00. R & R LT ANGLE, PN SH670-39189-1, IAW SRM 51-42-06, 51-45-00 & 51-25-16.

Part: BRACKET — CORRODED (BS 939) · airframe 31,637 hrs · 22,935 cycles

AFT WING TO FUSELAGE FAIRING SUPPORT STRUCTURE LT BRACKET AT FS 939.00 IS CORRODED. R & R LT BRACKET, PN:SH670-39189-1 IAW SRM 51-42-06, 51-45-00, 51-25-16.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 31,637 hrs · 22,935 cycles

AVIONICS BAY AT FS 364.00 2 INTERCOSTAL LT INBD & RT INBD, SHOWING SIGNS OF CORROSION. R & R 2 INTERCOSTAL, LT & RT INBD INTERCOSTALS, PN SH670-32075-3 & -4, IAW SRM 51-42-06, 51-42-21 & 51-40-11.

Part: OIL SYSTEM — LOW (APU) · airframe 31,448 hrs · 22,793 cycles

APU OVERTEMP MASTER WARNING IN FLIGHT, NR 2 IDG ALREADY DEFERRED. INSPECTED APU IAW AMM 49-10-00, SERVICED APU OIL IAW AMM 12-13-49 & INSPECTED APU THERMOCOUPLE WIRING IAW AMM 49-61-03, NO FAULTS NOTED. OPERATIONS CHECKED GOOD.

Part: COVER — LOOSE (EMERGENCY EXIT) · airframe 31,422 hrs · 22,771 cycles

RIGHT SIDE EMER EXIT ROW HANDLE COVER LOOSE. SECURED RT SIDE EMER DOOR EXIT HANDLE COVER IAW ALL 25-26-09.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,332 hrs · 22,694 cycles

EMERGENCY CEILING LIGHT AT ROW 9 INOPERATIVE. DEFERRED EMER CEILING LIGHT AT ROW 9 IAW MEL 33-51-01 CAT C.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,217 hrs · 22,610 cycles

CEILING EMER LIGHT INOPERATIVE AT ROW 9. DEFERRED EMER LIGHT IAW MEL 33-51-01B.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,217 hrs · 22,610 cycles

CROSS AISLE EMER LIGHT INOPERATIVE. R & R BULB IAW AMM 33-51-00.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,213 hrs · 22,610 cycles

CROSS AISLE EMER LIGHT OUT. RELAMPED AS REQUIRED. OPERATIONS CHECKED GOOD IAW AMM 33-51-00.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,213 hrs · 22,610 cycles

CEILING EMER LIGHT AT 9 INOPERATIVE. DEFERRED IAW MEL 33-51-01B CAT C.

Part: DOOR SEAL — DIRTY (EMERGENCY EXIT) · airframe 31,076 hrs · 22,498 cycles

LOUD WHISTLING NOISE COMING FROM RT OVERWING EMER EXIT DOOR INFLIGHT. PRESSURIZATION OK & DOOR SHOWS CLOSED. PERFORMED INSPECTION OF RT EMER EXIT DOOR. FOUND DEBRIS ON SEAL, CLEANED DEBRIS FROM THE HANDLE SEAL IAW AMM 52-21-07. LEAK CHECKED IAW 52-00-00.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,987 hrs · 211,687 cycles

EMERGENCY LIGHT UNDER FWD FLASHLIGHT IS INOPERATIVE. R & R FLOOR LEVEL EMER LIGHT BULBS IAW AMM 33-51-11. OPERATIONS CHECKED GOOD.

Part: WARNING MESSAGE — ACTIVATED (COCKPIT) · airframe 29,908 hrs · 21,627 cycles

PASSENGER DOOR LATCH CAUTION MSG. DEFERRED PAX DOOR LATCH MSG IAW MEL 52-70-01 CAT C.

Part: PROXIMITY SENSOR — OUT OF ADJUST (PAX DOOR) · airframe 29,459 hrs · 21,307 cycles

PASSENGER DOOR LATCH CAUTION MSG. ADJUSTED PX46 SENSOR IAW AMM 52-70-04. OPERATIONS CHECKED GOOD.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 29,435 hrs · 21,288 cycles

PASSENGER DOOR LATCH CAUTION MSG. DEFERRED PAX DOOR INDICATION SYS IAW MEL 52-70-01 CAT A.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 29,380 hrs · 21,246 cycles

ANTI-ICE DUCT WARNING MSG ON RT SIDE. PERFORMED BLEED & ICE DUCT SYS IAW AMM 36-10-00. OPERATIONS CHECKED GOOD.

Part: WIRE — BROKEN (PAX DOOR) · airframe 29,380 hrs · 21,246 cycles

PASSENGER DOOR LATCH CAUTION MSG. R & R PX26 & REPAIRED BROKEN WIRE IAW AMM 52-70-04. OPERATIONS CHECKED GOOD AT THIS TIME.

Part: INDICATION SYS — FALSE ACTIVATION (COCKPIT) · airframe 29,343 hrs · 21,215 cycles

PASSENGER DOOR LATCH CAUTION MSG. DEFERRED PAX DOOR INDICATION SYS IAW MEL 52-70-01 CAT A.

Part: CABLE — FRAYED (PAX DOOR) · airframe 29,202 hrs · 21,106 cycles

MAIN PAX DOOR SUPPORT WHEEL CABLE FRAYED. R & R FWD OAX DOOR SUPPORT WHEEL BOTTOM CABLE ASSEMBLY IAW AMM 52-11-13. OPERATIONS CHECKED GOOD AT THIS TIME.

Part: LENS — MISSING (CABIN) · airframe 29,161 hrs · 21,075 cycles

FLOOR LEVEL EMER LIGHT LENS BELOW FWD FLASHLIGHT MISSING. DEFERRED LIGHT LENS IAW NEF 25-100-12 CAT 1.

Part: CABLE — BROKEN (DOOR) · airframe 28,739 hrs · 20,739 cycles

ICE BREAKER CABLE BROKEN. R & R ICE BREAKER CABLE IAW AMM 52-11-15. OPERATIONS CHECKED GOOD AT THIS TIME.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 28,158 hrs · 20,291 cycles

PASSENGER DOOR WARNING. PERFORMED GVI OF PAX DOOR, VERIFIED DOOR IS CLOSED & LOCKED. ALL LOCK INDICATORS ARE ALIGNED IAW AMM 52-11-00. SAFE FOR ONE TIME FLIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,124 hrs · 20,265 cycles

EMERGENCY EXIT LIGHTS IN GALLEY AREA HAVE BURNED OUT BULBS. RELAMPED IAW AMM 33-51-05. OPERATIONS CHECKED GOOD AT THIS TIME.

Part: WARNING MESSAGE — FALSE ACTIVATION (COCKPIT) · airframe 28,096 hrs · 20,244 cycles

REJECTED TAKEOFF LOW SPEED 10-20 KNOTS DUE TO CONFIG SPOILER MSG. PERFORMED SPOST 2 IAW AMM 27-40-00. PERFORMED OPERATIONS CHECK OF SPOILER CONTROL SYS IAW AMM 27-61-00. OPERATIONS CHECKED GOOD AT THIS TIME.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 27,994 hrs · 20,161 cycles

RUDDER LIMITER CAUTION MSG. PERFORMED FIM TASK 27-61-05. NO MSG NOTED AT THIS TIME, OPERATIONS CHECKED GOOD.

Part: VALVE — OPEN · airframe 27,727 hrs · 19,943 cycles

COULD NOT PRESSURIZE IN FLIGHT. MANUALLY CLOSED GND VLV IAW AMM 21-24-18. OPERATIONS CHECKED GOOD AT THIS TIME.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 27,566 hrs · 19,814 cycles

TCAS ANTENNA MOUNT CHANNEL AT FS 295 IS CORRODED. R & R CHANNEL IAW SRM 51-42-06.

Part: SENSOR — OUT OF ADJUST (PAX DOOR) · airframe 27,591 hrs · 19,835 cycles

PAX DOOR LATCH CAUTION MESSAGE ASSOCIATED PROXIMITY TWO MESSAGES. TROUBLESHOOT & FOUND PAX DOOR PROXIMITY SENSOR PX 46 REQUIRED ADJUSTMENT. ADJUSTED PAX DOOR SENSOR IAW AMM 52-70-04. OPS CHECKED GOOD.

Part: WARNING MESSAGE — FALSE ACTIVATION (PAX DOOR) · airframe 27,591 hrs · 19,835 cycles

PAX DOOR LATCH CAUTION MESSAGE DURING CRUISE FLIGHT. CLEANED SENSOR PX 46, PERFORMED OPS CHECK OF PAX DOOR IAW AMM 52-11-00. OPS CHECKED GOOD ON THE GROUND.

Part: OUTFLOW VALVE — MALFUNCTIONED (CABIN PRESSURE) · airframe 27,574 hrs · 19,820 cycles

ACFT DID NOT PRESSURIZE ON CLIMB OUT. REACTIVATED GROUND VALVE IAW AMM 21-24-18.

Part: RIB — CRACKED (LT WING) · airframe 27,566 hrs · 19,814 cycles

LEFT HAND FIXED WING LE RIB AT SLAT STATION 27.75 CRACKED. CUT OUT DAMAGE, FABRICATED & INSTALLED DOUBLER IAW REO 670-57-42-505.

Part: SKIN — DENTED (FUSELAGE) · airframe 27,566 hrs · 19,814 cycles

LEFT FUSELAGE SKIN HAS DENT FWD OF FWD BAGGAGE DOOR AT FS 517.00. CUT OUT DAMAGED AREA. FABRICATED & INSTALLED DOUBLER IAW 670-53-31-319.

Part: MECHANISM — JAMMED (PAX DOOR) · airframe 27,566 hrs · 19,814 cycles

PAX DOOR INNER HANDLE RETENTION MECHANISM JAMMED. REPAIRED PAX DOOR INNER HANDLE RETENTION MECHANISM BY REPLACING INNER PARTS. HAFT PN 600-38040-19, BEARING PN 600-38040-33, & COMPRESSION SPRING PN LC-063F-6M IAW AMM 21-11-02.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 27,566 hrs · 19,814 cycles

UNDER FLOOR CRAWL WAY ANGLE SUPPORT AT FS 280 BL 0 CORRODED. R & R UNDER FLOOR CRAWL WAY ANGLE SUPPORT AT FS 280 BL 0 IAW SRM 51-42-21, 51-21-00, 51-25-16, 51-21-11, 51-40-11 & 51-42-06. WORK ORDER 80209 & WORK CARD 1132.

Part: ANCHOR FITTING — CORRODED (CABIN) · airframe 27,566 hrs · 19,814 cycles

LEFT FWD STORAGE CABINET, FWD INBD & OTBD FLOOR ANCHOR FITTINGS CORRODED. R & R BOTH FLOOR ANCHOR FITTINGS IAW CRJ700 SRM 51-42-21, 51-21-11, 51-25-06 & 51-25-16.

Part: ANCHOR FITTING — CORRODED (FUSELAGE) · airframe 27,566 hrs · 19,814 cycles

GALLEY 1 FWD INBD & OTBD ANCHOR FITTINGS CORRODED. R & R GALLEY 1 FWD INBD & OTBD ANCHOR FITTINGS IAW SRM 51-42-21. WORK ORDER 80209 & WORK CARD 1117.

Part: CROSSBEAM — CORRODED (FUSELAGE) · airframe 27,566 hrs · 19,814 cycles

FS 280 FLOOR CROSSBEAM CORRODED. R & R CROSSBEAM WITH NEW BEAM PN CC670-34175-7S, IAW CRJ700 SRM CHAPTER 51.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 27,566 hrs · 19,814 cycles

PASSENGER DOOR SURROUND FLOOR KICK ANGLE IS CORRODED. R & R KICK ANGLE WITH NEW PN SH670-31875-3S IAW CRJ-700 SRM CHAPTERS 51-21, 51-25, 51-40, 51-42 & 51-45.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 27,566 hrs · 19,814 cycles

SERVICE DOOR SURROUND KICK ANGLE IS CORRODED. R & R SERVICE DOOR KICK ANGLE IAW CRJ-700 SRM CHAPTERS 51-21, 51-25, 51-40 & 51-42.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 27,566 hrs · 19,814 cycles

PASSENGER DOOR ENTRY FLOOR MID CAP CORRODED. R & R MID CAP PN SH670-31825-9S IAW CRJ-700 SRM CHAPTERS 51-41, 51-42 & 51-45.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 27,566 hrs · 19,814 cycles

RIGHT INBD INTERCOSTAL, FWD OF THE FWD AVIONICS BAY DOOR CORRODED. R & R INTERCOSTAL WITH NEW PART NR SH670-32075-4 IAW CRJ700 SRM 51-42-21, 51-42-06, 52-70-08, 53-21-23, 51-40-11, 51-25-16 & 51-21-11. WORK ORDER 80209 & WORK CARD 1128.

Part: RIVET — DAMAGED (PAX DOOR) · airframe 27,566 hrs · 19,814 cycles

PASSENGER DOOR LOWER SURROUND STRUCTURE HAS TWO DAMAGED RIVETS ON THE FWD & AFT CORNER CAPS. R & R RIVETS IAW CRJ 700 SRM 51-42-13.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 27,566 hrs · 19,814 cycles

LEFT INBD INTERCOSTAL, FWD OF THE FWD AVIONICS BAY DOOR CORRODED. R & R INTERCOSTAL WITH NEW PART NR SH670-32075-3 IAW CRJ700 SRM 51-42-21, 51-42-06, 52-70-08, 53-21-23, 51-40-11, 51-25-16 & 51-21-11. WORK ORDER 80209 & WORK CARD 1128.

Part: LENS — MISSING (CABIN) · airframe 27,351 hrs · 19,656 cycles

EMERGENCY LIGHT LENS COVER AT ENTRANCE IS MISSING, NO WORDING ON LENS. DEFERRED EMERGENCY LIGHT LENS COVER AT ENTRANCE IAW NEF 25-100-12 CAT 1.

Part: COVER — LOOSE (EMERGENCY EXIT) · airframe 27,296 hrs · 19,615 cycles

RIGHT EMERGENCY EXIT DOOR HANDLE COVER LOOSE. SECURED VELCRO TAPE AT EMERGENCY EXIT ROW WINDOW RT COVER FOR HANDLE IAW AMM 51-22-61.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 27,231 hrs · 19,570 cycles

PASSENGER DOOR LATCH CAUTION MESSAGE IN FLIGHT. PERFORMED OPERATIONS CHECK OF PAX DOOR IAW CRJ 700 AMM 52-11-00, COULD NOT DUPLICATE MESSAGE AT THIS TIME. OPERATIONS CHECKED GOOD AT THIS TIME.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,796 hrs · 19,228 cycles

EXIT LIGHT INOPERATIVE. R & R BOTH LOWER OVERWING EXIT LIGHTS IAW AMM 33-51-01. OPS CHECKED GOOD AT THIS TIME.

Part: OVERHEAT LOOP — OUT OF POSITION · airframe 26,053 hrs · 18,619 cycles

INTERIGATED MDC AND FOUND BLEED AIR DETECTION LOOP, MT 143 AND MT 205 FAULTY. INSPECTED LOOPS AND FOUND MT205 TOUCHING DUCT INSULATION. REPOSITIONED LOOP MT205 IAW AMM 36-21-03. OP'S AND LEAK CHECKED GOOD AT THIS TIME.

Part: ENGINE — MALFUNCTIONED (NR 2) · airframe 25,826 hrs · 18,456 cycles

OBSERVED POWER LOSS ON NR 2 ENGINE AT ROTATION. OBSERVED ENGINE SURGING N1 FROM 80 TO 70 PERCENT, HEARD POPPING SOUND, SHUTDOWN ENGINE IAW QRH. R & R NR 2 ENGINE IAW AMM 71-00-00, SP-09 FOR COMPLETION OF RUNS AND RII'S.

Part: CONNECTOR — LOOSE (DOOR WARNING) · airframe 25,623 hrs · 18,309 cycles

PAX DOOR OUTER HANDLE CAUTION. INSPECTED FOUND LOOSE CONNECTOR A268P1, RESECURED CONNECTOR, PERFORMED OP'S CHECK OF PAX DOOR PROXIMITY WARNING SYS IAW AMM 52-70-00, NO FAULTS OF DEFECTS NOTED AT THIS TIME.

Part: KNOB — LOOSE (RUDDER ADJUST) · airframe 25,602 hrs · 18,295 cycles

RUDDER ADJUSTMENT KNOB IS LOOSE. ADJUSTED AND RESECURED RUDDER TRIM KNOB, OP'S CHECK C/W IAW 27-22-00, OP'S CHECK GOOD AT THIS TIME.

Part: CABLE — BROKEN (PAX DOOR) · airframe 25,054 hrs · 17,886 cycles

ICE BREAKER CABLE BROKEN. PLACED ON C/O 23456.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 24,757 hrs · 17,660 cycles

CEILING EMERGENCY FLOOD LIGHT INOPERATIVE. RELAMPED AFT CEILING EMERGENCY FLOOD LIGHT IAW AMM 33-53-09. OP'S CHECKED GOOD.

Part: LIGHT — BURNED OUT (CABIN) · airframe 24,740 hrs · 17,649 cycles

CEILING OVERHEAD EMERGENCY FLOOD LIGHT BURNED OUT.

Part: LIGHT — UNKNOWN · airframe 24,295 hrs · 17,302 cycles

EMERGENCY EXIT SIGN LIGHT INOPERATIVE. OP'S CHECKED GOOD AT THIS TIME.

Part: SIGN — INOPERATIVE (CABIN) · airframe 24,295 hrs · 17,302 cycles

FORWARD LOWER LT EMERGENCY EXIT SIGN INOPERATIVE. OP'S CHECK GOOD AT THIS TIME.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,295 hrs · 17,302 cycles

ROW 9 CEILING EMEGENCY LIGHT INOPERATIVE. R & R EMERGENCY POWER SUPPLY UNIT, IAW AMM 33-51-17, OP'S CHECKED GOOD AT THIS TIME.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 3 · airframe 20,581 hrs · 14,709 cycles

STRINGER 25 RIGHT CORRODED AT FS 304.00. REMOVED DAMAGED SECTION OF STRINGER AND SPLICED IN NEW SECTION IAW 53-00-03, SOLUTION 1, STRINGER SPLICE FIGURE 53-00-03-991-803 SHEET 10 AND DEVIATION REO 670-53-00-300.

Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 20,581 hrs · 14,709 cycles

RIGHT BULKHEAD AT FS 280 HAS CORROSION AT THE FLOOR LEVEL. REMOVED AND REPLACED DISCREPANT PANEL IAW SRM 51-42-06 AND 51-42-13.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 20,581 hrs · 14,709 cycles

THE "T" BRACKET AT FS 280 LBL 9 IS CRACKED. REMOVED AND REPLACED DISCREPANT BRACKET IAW SRM 51-42-21.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 20,581 hrs · 14,709 cycles

THE "T" BRACKET AT FS 280 RBL 9 IS CRACKED. REMOVED AND REPLACED DISCREPANT BRACKET IAW SRM 51-42-21.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 20,581 hrs · 14,709 cycles

FS 280 FLOOR SUPPORT CRACKED AT LBL 9 AND RBL 9. REMOVED AND REPLACED DISCREPANT FLOORBEAM IAW SRM 51-42-06 AND 51-42-21.

Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 20,581 hrs · 14,709 cycles

LEFT BULKHEAD AT FS 280 HAS CORROSION ON AFT SIDE AT THE FLOOR LEVEL. REMOVED AND REPLACED DISCREPANT PANEL IAW SRM 51-42-06 AND 51-42-13.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 18,382 hrs · 13,165 cycles

ON APPROACH INTO TLH RECEIVED STEERING INOP CAUTION MSG. EMERGENCY DECLARED, A/C LANDED SAFELY. THIS FAULT IS INCLUDED IN THE FIM NUISANCE MSG LIST. RESET NWS PER FIM EICAS NUISANCE MSG RESET PROCEDURE. NO FURTHER DEFECTS NOTED.

Part: FAN BLADE — DEFECTIVE (LT ENGINE) · airframe 15,469 hrs · 11,142 cycles

EN ROUTE ATL-MKE THE LEFT ENGINE VIBRATION INDICATION REACHED 1.8 AMBER, REDUCED THRUST TO INDICATE GREEN. CREW DIVERTED TO MKE AND LANDED WITHOUT INCIDENT. REPLACED ALL FAN BLADES ON THE LEFT ENGINE.

Part: ACM — FAILED (A/C BAY) · airframe 12,776 hrs · 9,302 cycles

FLIGHT 5128 - RIGHT PACK SMOKING. REMOVED AND REPLACED RIGHT ACM.

Part: BPSU — FAULTY (LT WING SLATS) · airframe 11,990 hrs · 8,760 cycles

FLIGHT 5535 - SLATS FAIL CAUTION MESSAGE AND NO DEPLOYMENT WHEN SELECTED ON APPROACH. REMOVED AND REPLACED LEFT SLAT BPSU.

Part: SLAT SYSTEM — MALFUNCTIONED (LE SLATS) · airframe 11,917 hrs · 8,703 cycles

FLIGHT 5466 - RECEIVED SLAT FAIL MESSAGE ON DESCENT. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. CLEARED INHIBITS FROM SLAT SYSTEM. VISUALLY INSPECTED SLATS, OPERATED SYSTEM, NO FURTHER DEFECTS.

Part: SLAT SYSTEM — MALFUNCTIONED · airframe 11,917 hrs · 8,703 cycles

FLIGHT 5466 - RECEIVED SLAT FAIL MESSAGE ON DESCENT. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. CLEARED INHIBITS FROM SLAT SYSTEM. VISUALLY INSPECTED SLATS, OPERATED SYSTEM, NO FURTHER DEFECTS.

Part: VALVE — LEAKING (LAVATORY FAUCET) · airframe 11,220 hrs · 8,215 cycles

FLIGHT 5328 - EN ROUTE CVG-PBI DISCOVERED THE FORWARD AND AFT LAVATORY WERE LEAKING POTABLE WATER INTO THE CABIN, FLIGHT RETURNED TO CVG. REPLACED THE FORWARD LAVATORY FAUCET.

Part: SENSE LINE — FAULTY (RT ENGINE) · airframe 11,162 hrs · 8,170 cycles

FLIGHT 4950 - RIGHT ENGINE REVERTED TO IDLE WITH RIGHT FADEC MESSAGE AND HIGH TEMP OF 790. DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. REPLACED RIGHT ENGINE P3 LINE. NO FURTHER DEFECTS.

Part: FMU — MALFUNCTIONED (RT ENGINE) · airframe 11,162 hrs · 8,170 cycles

FLIGHT 4950 - RIGHT ENGINE REVERTED TO IDLE WITH RIGHT FADEC MESSAGE AND HIGH TEMP OF 790. DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. REPLACED RIGHT ENGINE FMU, NO FURTHER DEFECTS.

Part: ACTUATOR — MALFUNCTIONED (RT ENGINE) · airframe 11,162 hrs · 8,170 cycles

FLIGHT 4950 - RIGHT ENGINE REVERTED TO IDLE WITH RIGHT FADEC MESSAGE AND HIGH TEMP OF 790. DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. REPLACED RIGHT ENGINE MASTER VG ACTUATOR. NO FURTHER DEFECTS.

Part: TRANSDUCER — FAULTY (LT OUTBD MLG) · airframe 10,467 hrs · 7,678 cycles

FLIGHT 5642- AFTER LANDING UNDER LIGHT TO MODERATE BRAKING, ABOUT 10 KTS, THE BRAKES RELEASED, BY 50 PERCENT THEN GRABBED HARD AT ABOUT 5 KTS. TROUBLESHOOTING SHOWED ERRONEOUS DATA FROM RIGHT INBOARD AND LEFT OUTBOARD WHEEL TRANSDUCERS. CLEANED CONNECTOR ON TRANSDUCERS, DID NOT FIX. REPLACED LEFT OUTBOARD WHEEL SPEED TRANSDUCER, NO FURTHER DEFECTS.

Part: TRANSDUCER — FAULTY (RIGHT INBD MLG) · airframe 10,467 hrs · 7,678 cycles

FLIGHT 5642 - AFTER LANDING UNDER LIGHT TO MODERATE BRAKING, ABOUT 10 KTS, THE BRAKES RELEASED BY 50 PERCENT THEN GRABBED HARD AT ABOUT 5 KTS. TROUBLESHOOTING SHOWED ERRONEOUS DATA FROM RIGHT INBOARD AND LEFT OUTBOARD WHEEL TRANSDUCERS. CLEANED CONNECTOR ON TRANSDUCERS, DID NOT FIX. REPLACED RIGHT INBOARD WHEEL SPEED TRANSDUCER, NO FURTHER DEFECTS.

Part: PDU — FAULTY (SLATS) · airframe 9,595 hrs · 7,163 cycles

DURING CRUISE FLIGHT RECEIVED A SLAT FAIL CAUTION AT 10 DEGREES, CREW DECLARED AN EMERGENCY AND FLIGHT LANDED WITHOUT INCIDENT. REPLACED THE SLAT PDU.

Part: PDU — FAULTY (SLATS) · airframe 9,588 hrs · 7,158 cycles

FLIGHT 5725 - DURING APPROACH RECEIVED A SLAT FAIL CAUTION AT 10 DEGREES. REPLACED THE SLAT POWER DRIVE UNIT.

Part: SEAT TRACK — CORRODED (BS 280-477) · corrosion level 2 · airframe 7,298 hrs · 6,137 cycles

THE RT SEAT TRACK FROM FS 280.00 TO FS 477.00 IS CORRODED. REMOVED THE CORRODED SEAT TRACK AND INSTALLED NEW SEAT TRACK IAW CRJ 700 SRM 51-41-01-001-001-A01.

Part: SEAT TRACK — CORRODED (FS 280-477) · corrosion level 2 · airframe 7,328 hrs · 6,137 cycles

THE LT SEAT TRACK FROM FS 280.00 TO FS 477.00 IS CORRODED. REMOVED THE CORRODED SEAT TRACK AND INSTALLED NEW SERVICEABLE SEAT TRACK IAW CRJ 700 SRM 51-11-02-001-001-A01.

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 7,928 hrs · 6,137 cycles

MINOR CORROSION ON WING PLANK AT FUEL PANEL ACCESS CUTOUT FOR PANEL 541AB/BB. ACCOMPLISHED MINOR REPAIR IAW BRAS EO 601R-57-7672.

Part: ACM — SMOKE (CABIN COOLING) · airframe 6,923 hrs · 5,367 cycles

SMOKE IN CABIN. REPLACED RT ACM.

Part: ACM — MALFUNCTIONED (CABIN COOLING) · airframe 6,923 hrs · 5,367 cycles

SMOKE IN AFT LAV. REPLACED RT ACM.

Part: WINDOW — FAILED (COCKPIT) · airframe 6,727 hrs · 5,225 cycles

PILOT SIDE WINDOW SHATTERED. REPLACED WINDOW.

Part: BEAM — CORRODED (FUSELAGE) · airframe 3,711 hrs · 2,915 cycles

TRANSVERSE BEAM AT FS 280 FROM LBL 36 TO RBL 36 IS CORRODED ALONG THE UPPER AND LOWER EDGES. REPLACED THE TRANSVERSE BEAM AT FS 280 IAW BOMBARDIER INC REO 670-53-11-047, AND CRJ 700 SRM 51-42-06-001-001-A01.

Part: WARNING LIGHT — FALSE INDICATION (E/E BAY DOOR) · airframe 6,213 hrs · 4,781 cycles

FLIGHT 5756 AVIONICS DOOR CAUTION. COULD NOT DUPLICATE. OPERATIONAL CHECK SATISFACTORY.

Part: CYLINDER — CORRODED (NLG) · airframe 5,902 hrs · 4,585 cycles

NLG OUTER CYLINDER IS CORRODED. CORROSION REPAIRED IAW BOMBARDIER REO 670-32-21-036 AND GOODRICH SCR 0008-04 REV C.

Part: BEAM — CORRODED (FUSELAGE) · airframe 5,902 hrs · 4,585 cycles

TRANSVERSE BEAM AT FS 280 FROM LBL 36 TO RBL 36 IS CORRODED ALONG THE UPPER AND LOWER EDGES. REPLACED THE TRANSVERSE BEAM AT FS 280 IAW BOMBARDIER AEROSPACE REO 670-53-11-047, BRAS EO'S 610R-53-5986, 601R-53-5987, 601R-53-5977 AND CRJ 700 SRM 51-42-06-001-001-AO1.

Part: BULKHEAD — CORRODED (FUSLAGE) · airframe 5,902 hrs · 4,585 cycles

FS 280 LT AND RT BULKHEADS HAVE MAJOR CORROSION ON AFT SIDE ALONG THE BOTTOM EDGES. REPLACED LOWER WEBS AT FS 280 BULKHEAD IAW BOMBARDIER AEROSPACE REO 670-53-11-052 AND BRAS EO 601R-53-5986, 601R-53-5987, AND 601R-53-5977.

Part: WARNING LIGHT — ILLUMINATED (THRUST REVERSER) · airframe 4,066 hrs · 3,130 cycles

LEFT THRUST REVERSER UNSAFE CAUTION MESSAGE. DEFERRED MAINT ON THRUST REVERSER PER MEL.

Part: CONTROL UNIT — FAILED (SPOILER) · airframe 3,992 hrs · 3,072 cycles

FLIGHT 5078 SPOILER, STAB AND RUDDER LIMIT FAULT MESSAGE DURING T/O. COULD NOT DUPLICATE. RESET SSCU 1 AND 2, SYSTEM CHECK SATISFACTORY.

Part: WARNING LIGHT — ICED (THRUST REVERSER) · airframe 3,305 hrs · 2,532 cycles

FLIGHT 5661 RIGHT THRUST REVERSER CAUTION DURING T/O. DEFERRED MAINT ON T/R PER MEL.

Part: WARNING SYSTEM — ACTIVATED (E/E DOOR) · airframe 3,137 hrs · 2,400 cycles

FLIGHT 5073 AVIONICS BAY DOOR CAUTION MESSAGE DURING T/O. DEFERRED MAINT ON DOOR WARNING SYSTEM PER MEL.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 2,240 hrs · 1,751 cycles

FS 1098.20 BULKHEAD RIGHT WEB BETWEEN STRINGERS 8R AND 9R IS CRACKED. REPAIRED BY REMOVING AND INSTALLING A BATHTUB FITTING IAW BOMBARDIER, INC REO 670-53-61-034 REV B.

Part: WARNING LIGHT — ILLUMINATED (TE FLAPS) · airframe 1,546 hrs · 1,219 cycles

FLIGHT 5668 ABORTED T/O FOR FLAP CONFIG WARNING. T/O WAS SUCCESSFUL ON SECOND ATTEMPT.

Part: WARNING LIGHT — FALSE INDICATION (PAX DOOR) · airframe 1,531 hrs · 1,206 cycles

FLIGHT 5717 AVIONICS DOOR CAUTION MESSAGE DURING T/O. COULD NOT DUPLICATE. INSPECTED DOOR AND WARNING SYSTEM, NO FAULTS FOUND.

Part: SELECTOR VALVE — INOPERATIVE (LANDING GEAR) · airframe 474 hrs · 386 cycles

FLIGHT 9455 NWS INOP MESSAGE.REPLACED THE LANDING GEAR SELECTOR VALVE.

Part: SELECTOR VALVE — INOPERATIVE (LANDING GEAR) · airframe 472 hrs · 385 cycles

FLIGHT 5429 GEAR DISAGREE WARNING, GEAR DID NOT EXTEND.REPLACED THE LANDING GEAR SELECTOR VALVE.