N157GJ

Part: WEB — CORRODED (FUSELAGE) · airframe 34,638 hrs · 23,812 cycles

RT 280.00 WEB IS CORRODED. REMOVED CORRODED AREA, FABRICATED AND INSTALLED REPAIR PARTS IAW REO 670-53-11-093 REV--B DATED 2013-03-14.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 34,638 hrs · 23,812 cycles

25R LONGERON AFT OF FS 349.00 IS CORRODED. REMOVED AND REPLACED LONGERON 25R AT FS 349.00 IAW SRM 51-40-11, 51-42-21, 51-42-06, 51-25-21, AND 51-21-11.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 34,638 hrs · 23,812 cycles

STRINGER 25R IS CORRODED BETWEEN FS 280.00-349.00. REMOVED AND REPLACED STR 25R IAW SRM 51-42-21, 51-42-06, 51-41-02, 51-40-11, 51-26-00, 51-25-21, AND 51-25-06.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 34,638 hrs · 23,812 cycles

STRINGER 26R IS CORRODED BETWEEN FS 280.00-349.00. REMOVED AND REPLACED STR 26R IAW SRM 51-42-06, 53-00-06, 51-21-11, 51-25-06, 51-25-21, 51-26-00, 51-40-11, 51-41-02, 51-42-06, AND 51-42-21.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 24,628 hrs · 23,812 cycles

LH AND RH F.S.280 CROSSBEAM CRACKED. CORRECTIVE ACTION: REMOVED AND REPLACED LH AND RH F.S.280 CROSSBEAM (P/N: CC670-34175-7S) IAW BOMBARDIER REO 670-53-11-493 DATED 2010/03/16, REO 670-53-11-493 REV.B DATED 2013-03-14, CRJ700 SRM 51-42-10, 51-25-21, 51-25-06, 51-21-11, 51-42-21, 51-42-13, 51-42-06, 51-40-11, 51-41-02, 51-24-36, 51-11-42, AND AMM 20-70-00 NDTM PART1 51-20-006

Part: DRAG ANGLE — CRACKED (VERTICAL STAB) · airframe 34,638 hrs · 23,812 cycles

VERTICAL STABILIZER L/H AFT DRAG ANGLE IS CRACKED. REMOVED CRACKED SECTION, FABRICATED AND INSTALLED REPAIR PARTS IAW REO 670-55-31-018 REV A DATED 2016-11-10, AND 670-55-31-113 REV- DATED 2018-12-05.

Part: STRAP — CRACKED (ZONE 100) · airframe 34,638 hrs · 23,812 cycles

AFT WING TO BODY FAIRING STRAP IS CRACKED. FABRICATED AND INSTALLED AFT WING TO BODY FAIRING STRAP IAW DRAWING PLCC670-39121, SRM 551-25-06, 51-25-00, 51-40-11, 51-24-16, 51-42-06, 51-41-02, 51-25-21.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 34,638 hrs · 23,812 cycles

GALLEY/SERVICE DOOR SURROUND, TWO LOWER SILL ANGLES ARE CORRODED. REMOVED AND REPLACED ANGLES (PN:SH670-39182-1) IAW SRM 53-21-23, 51-42-06, 51-42-21, 51-40-11, 51-21-11, 51-25-06, AND 51-25-21.

Part: CROSSBEAM — CHAFED (FUSELAGE) · airframe 34,638 hrs · 23,812 cycles

AFT CARGO DOOR SURROUND SUPPORT STRUCTURE, CROSSBEAM AFT END IS CHAFFED FROM CABLE. REPAIRED CROSSBEAM BY CUTTING AWAY DAMAGE, FABRICATING AND INSTALLING REPAIR PARTS IAW REO 670-53-61-1506 DATED 2018-12-02.

Part: SUPPORT BRACKET — CORRODED (FUSELAGE) · airframe 34,638 hrs · 23,812 cycles

STIFFENER SUPPORT BRACKET AT FS 661.00 AND STR 19R IS CORRODED. REMOVED AND REPLACE STIFFENER SUPPORT BRACKET (PN:SH670-39113-1) IAW SRM 53-31-43, 51-42-06, 51-42-21, 51-40-11, 51-25-16, AND 51-21-11.

Part: PLATE — CORRODED (ZONE 200) · airframe 34,638 hrs · 23,812 cycles

RT OVERWING EXIT STEP PLATE ASSY IS CORRODED. REMOVED AND REPLACE OVERWING STEP PLATE ASSY (PN:SH670-36550-1) IAW SRM 51-42-02, AND 53-00-00.

Part: LANDING — CRACKED (E&E DOOR) · airframe 34,638 hrs · 23,812 cycles

RT FWD FUSELAGE FWD EQUIP BAY ACCESS DOOR 212AR, DOOR LANDING IS CRACKED. REMOVED AND REPLACE DOOR LANDING (PN:CC670-33151-6S) IAW SRM 51-42-06, 51-42-13, 51-40-11, AND 51-25-16.

Part: WEB — CRACKED (FUSELAGE) · airframe 34,638 hrs · 23,812 cycles

FWD EQUIP COMPARTMENT FLOOR WEB RT SIDE AT FS 193.00 IS CRACKED. REMOVED CRACKED AREA FABRICATED AND INSTALLED REPAIR PARTS IAW REO 670-53-11-509 REV E DATED 20180208.

Part: DIAPHRAGM — CRACKED (PAX SEAT) · airframe 34,638 hrs · 23,812 cycles

PASSENGER SEAT 2D HAS A CRACKED SEAT BOTTOM DIAPHRAGM. REPAIRED CRACKED SEAT BOTTOM DIAPHRAGM BY REMOVING CRACKED BRACKETS, FABRICATING AND INSTALLING REPAIR PARTS IAW REO 670-25-21-002 REV- DATED 2018-11-30.

Part: SUPPORT CHANNEL — CRACKED (AFT CARGO DOOR) · airframe 34,638 hrs · 23,812 cycles

AFT CARGO DOOR AFT TRACK SUPPORT CHANNEL IS CRACKED. CORRECTIVE ACTION: REMOVED AND REPLACED CHANNEL(PN:MM670-35552-003) IAW CRJ 700 SRM 51-42-21, 51-42-06, 51-25-16.

Part: TRIPLER — GOUGED (BS 977) · airframe 34,638 hrs · 23,812 cycles

AFT LOWER FUSELAGE EXISTING REPAIR AT F.S. 977.00 AND STGR 27 HAS A GOUGE. CORRECTIVE ACTION: REPAIRED FUSELAGE SKIN AT F.S. 977.00 AND STGR 27 IAW BOMBARDIER REO 670-53-61-1505 REV.B(P1) DATED 2018-12-04, 670-53-61-1505 REV. A DATED 2018-12-03, 670-53-61-920 REV.-B(P1) DATED 2018-11-26, 670-53-00-290 REV.-D DATED 2015-09-10.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 34,638 hrs · 23,812 cycles

RIGHT HAND FLOOR SILL AT F.S. 280.00 IS CORRODED. CORRECTIVE ACTION: REMOVED AND REPLACED R/H FLOOR SILL(PN:SH670-32172-5) IAW CRJ 700 SRM51-26-00, 51-42-06, 51-42-21, 51-40-11, 51-21-11, 51-25-16, AND 53-21-23.

Part: BEAM — CHAFED (AFT CARGO) · airframe 34,638 hrs · 23,812 cycles

AFT CARGO DOOR BEAM ASSY CAM TRACK SUPPORT IS CHAFED.. CORRECTIVE ACTION: REPAIRED AFT CARGO DOOR BEAM ASSY CAM TRACK SUPPORT, BY CUTTING AWAY DAMAGE FABRICATING AND INSTALLING REPAIR PART IAW BOMBARDIER REO 670-53-61-1506, DATED 2018-12-02.

Part: SMOKE DETECTOR — MALFUNCTIONED (LAVATORY) · airframe 34,496 hrs · 23,713 cycles

AFT LAV SMOKE WARNING MSG IN FLIGHT. DEFERRED LAV SMOKE DET OCN 70046424 PER MEL 26-16-01 CAT C.

Part: WARNING LIGHT — ILLUMINATED (EMERGENCY EXIT) · airframe 33,526 hrs · 23,084 cycles

LEFT OVERWING EMERGENCY EXIT CAUTION ON LANDING.

Part: DOOR — NOISY (MAIN PAX) · airframe 33,190 hrs · 22,866 cycles

MAIN CABIN DOOR MAKES A LOUD NOISE AT ALTITUDE. PERFORMED CABIN PRESSURE CONTROL SYS TEST IAW AMM 21-31-00, NO DEFECTS NOTED.

Part: LIGHT — INOPERATIVE (GALLEY) · airframe 32,676 hrs · 22,500 cycles

GALLEY EMERGENCY LIGHT INOPERATIVE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 32,676 hrs · 22,500 cycles

EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMPS IAW AMM 33-51-05, OPS OK.

Part: UNKNOWN — ODOR (COCKPIT & CABIN) · airframe 30,735 hrs · 21,035 cycles

BURNING ODOR IN COCKPIT AND CABIN, NO SMOKE. PERFORMED MY5 SENSE ELEMENT WITH THE PACK ON, NO BURNING ODOR NOTED, LT AND RT PACKS OPS CHECKED GOOD IAW AMM 21-51-00. OK FOR SERVICE.

Part: DOOR — UNSECURE (EMERGENCY EXIT) · airframe 29,466 hrs · 20,277 cycles

LEFT EMERGENCY DOOR CAUTION MESSAGE DURING LANDING. INSPECTED AND SECURED THE LT OVERWING EXIT, OPS CHECKED GOOD IAW AMM 52-21-00.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 29,515 hrs · 20,094 cycles

FLOOR LEVEL EMERGENCY EXIT LIGHT RT WING LIGHTS BURNED OUT. R AND R EMERGENCY LIGHTS ON RT EXIT FLOOR LEVEL SIGN IAW AMM 33-51-11.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 29,489 hrs · 20,074 cycles

BS 280 FLOORBEAM CRACKED NEAR THE LEFT DRIP TRAY. REPAIRED IAW REO 670-53-11-493

Part: HINGE — LACK OF LUBE (PAX DOOR) · airframe 28,354 hrs · 19,273 cycles

PASSENGER DOOR DIFFICULT TO OPEN & CLOSE. LUBRICATED HINGE NUTS & JOINTS OF THE MAIN PAX DOOR. PERFORMED FUNCTIONAL CHECK IAW AMM 52-11-00. NO DEFECTS NOTED AT THIS TIME.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 27,609 hrs · 18,765 cycles

DAMAGE TO RT SIDE OF THE FUSELAGE AT APPROX FS 1040 - 1085, BETWEEN STRINGERS 18R & 19R. REPAIRED DAMAGE IAW REO 670-53-61-1186.

Part: ASSIST ASSY — FAULTY (PAX DOOR) · airframe 26,985 hrs · 18,303 cycles

MAIN PAX DOOR WON’T OPEN ALL THE WAY. DEACTIVATED PAX DOOR POWER ASSIST MOTOR & CABLE IAW AMM 52-11-00. PAX DOOR ASSIST SYS DEFERRED IAW MEL 52-11-01A.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 26,523 hrs · 17,981 cycles

RIGHT EMER DOOR EXIT, DOOR CAUTION MSG. DEFERRED RT EMER EXIT DOOR INDICATION IAW MEL 52-70-03 CAT C.

Part: DOOR — NOISY (EMERGENCY EXIT) · airframe 26,284 hrs · 17,819 cycles

RIGHT EMER EXIT SQUEALS. PERFORMED INSPECTION OF & CLEANING OF THE RT OVERWING EMER EXIT IAW AMM 52-21-00. NO DEFECTS NOTED AT THIS TIME.

Part: DOOR SEAL — DAMAGED (ENTRY DOOR) · airframe 26,186 hrs · 17,747 cycles

FIX ENTRANCE DOOR MAKING LOUD WHISTLE IN FLIGHT. R & R PAX DOOR SEAL IAW AMM 52-11-07. OPERATIONS CHECKED GOOD AT THIS TIME.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 26,127 hrs · 17,692 cycles

LEFT SIDE SKIN OF NLG SURROUND STRUCTURE DAMAGED. R & R SKIN, PN CC670-33106-3 IAW SRM 51-42-06, 51-40-11, 51-42-22 & REO 670-53-11-1045 DATED 17 APRIL 2015.

Part: SUPPORT BEAM — DAMAGED (FUSELAGE) · airframe 26,127 hrs · 17,692 cycles

RIGHT NLG SIDE SUPPORT BEAM AT BL 7.5, FWD LOWER AREA HAS FOUR DISTORTED HOLES. R & R RT NLG SIDE SUPPORT BEAM, PN CC670-32193-14S, AT BL 7.5 IAW SRM 51-42-21, 51-40-11, EO CC670-32020, DATED 17 APRIL 2015, EO CC670-32030 DATED 17 APRIL 2015 & MEMO ISE-STR-15-024 REV A DATED 18 APRIL 2015.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 26,127 hrs · 17,692 cycles

LOWER SKIN FROM FS 202.0 - 280.0 DAMAGED DURING LANDING. R & R LOWER SKIN PANEL, PN CC670-33103-3 IAW SRM 51-40-11, 51-42-26, 51-42-21, 51-21-11, 51-21-16 & REO 670-53-11-1046, DATED 17 APRIL 2015.

Part: LANDING — DAMAGED (FUSELAGE) · airframe 26,127 hrs · 17,692 cycles

FORWARD RT SURROUND STRUCTURE OF NLG, LANDING DAMAGED. R & R LANDING, PN CC670-32142-3 IAW SRM 51-42-06, 51-40-11 & REO 670-53-11-1044.

Part: BEAM — BENT (FUSELAGE) · airframe 26,127 hrs · 17,692 cycles

LEFT SIDE BEAM SUPPORT STRUCTURE AT BL 7.50 IS BENT. R & R SIDE BEAM AT BL 7.50 PN CC670-32193-13 IAW SRM 51-42-21, 51-40-11 & EO CC670-32020 DATED 18 APRIL 2015, DWG CC670-32020 REV C & MEMO ISE STR-15-024 REV A DATED 18 APRIL 2015.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 26,127 hrs · 17,692 cycles

STIFFENING ANGLE AT FS 265, STRINGER 25L - 25R & 2 INTERCOSTAL FROM FS 265 - 280, STRINGER 27 ARE CORRODED. R & R CORRODED STIFFENING ANGLE & 2 INTERCOSTAL IAW SRM 51-42-06 & 51-42-21. PARTS, SUPPORT PN CC670-32179-1. WO 80281 WC 1013.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 26,127 hrs · 17,692 cycles

STIFFENING ANGLE AT FS 265.0, STRINGER 25L - 25R & 2 INTERCOSTALS FROM FS 265.0 - 280.0 ARE CORRODED. R & R STIFFENING ANGLE PN CC670-34104-1, INTERCOSTALS SUPPORT PN CC670-32179-1 & -2 IAW SRM 51-42-06, 51-42-21, 51-40-11, 51-25-16, 51-21-11 & 51-42-13.

Part: UNKNOWN — MALFUNCTIONED (NLG) · airframe 26,124 hrs · 17,691 cycles

AIRCRAFT LANDED WITH NLG RETRACTED. ACFT IS CURRENTLY UNDER REPAIR.

Part: FLAP — MALFUNCTIONED (WING) · airframe 26,006 hrs · 17,618 cycles

FLAPS HALF SPEED CAUTION MSG. RESET FLAPS & PREFORMED OPERATIONS CHECK IAW AMM 27-50-00.

Part: WHEEL — MALFUNCTIONED (PAX DOOR) · airframe 25,972 hrs · 17,599 cycles

PASSENGER DOOR SUPPORT WHEEL DID NOT DEPLOY, PAX DOOR HIT GND. INSPECTED PAX DOOR, NO DAMAGE FOUND. PERFORMED ADJUSTMENT TEST OF PAX DOOR IAW AMM 52-11-00. OPERATIONS CHECKED GOOD. NO DEFECTS WERE NOTED.

Part: DOOR SEAL — LACK OF LUBE (PAX DOOR) · airframe 25,733 hrs · 17,444 cycles

PASSENGER DOOR WHISTLES LOUDLY IN FLIGHT. LUBED AMIN PAX DOOR SEAL IAW AMM 21-31-00. OPERATIONS CHECKED GOOD.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 25,590 hrs · 17,356 cycles

LEFT WING ANTI-ICE CAUTION MSG. DEFERRED LT WING ANTI-ICE DETECTION SYS IAW MEL 30-10-01A CAT C.

Part: DOOR SEAL — DIRTY (CABIN DOOR) · airframe 25,528 hrs · 17,313 cycles

MAIN CABIN DOOR SEAL MAKING NOISE. CLEANED DEBRIS FROM SEAL & DOOR FRAME, LUBED SEAL IAW AMM 52-00-00.

Part: UNKNOWN — MALFUNCTIONED (FLIGHT CONTROL) · airframe 25,446 hrs · 17,256 cycles

AIRCRAFT STARTED TO YAW UNCOMMANDED, VIBRATION THROUGH RUDDER PEDALS THROUGH CLIMB OUT. PERFORMED OPERATIONS CHECK ON YAW DAMPER LINEAR ACTUATOR IAW AMM 22-22-01, PASSED TEST. PERFORMED RUDDER OPERATIONS CHECK IAW AMM 2721-00. OPERATIONS CHECKED NORMAL. OK FOR SERVICE.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 25,173 hrs · 17,078 cycles

DAMAGE TO RT SIDE OF FUSELAGE BETWEEN FS 364 & 394. ACCOMPLISHED REPAIR TO AFFECTED AREA IAW REO 670-53-21-1136 REV B.

Part: DOOR SEAL — DIRTY (PAX DOOR) · airframe 25,128 hrs · 17,048 cycles

MAIN PAX DOOR HAS LOUD WHISTLE IN FLIGHT. NO LOSS OF PRESSURIZATION. CLEANED & INSPECTED DOOR SEAL IAW AMM 52-11-07. NO DEFECTS NOTED AT THIS TIME.

Part: FITTING — CORRODED (CABIN) · airframe 24,753 hrs · 16,810 cycles

RIGHT CABIN DIVIDER, WIND SCREEN, HAS CORROSION ON INBD & OTBD FLOOR FITTINGS. R & R CABIN DIVIDER FLOOR FITTINGS PN CDSP2019-7C-650 IAW AMM 20-21-00.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 24,753 hrs · 16,810 cycles

STRINGER 26R IS CORRODED FWD OF FS 364.00. SPLICED IN REPLACEMENT STRINGER, PN SH670-31372-4, AT STRINGER 26 FWD OF FS 364.00 IAW REO 670-53-21-1119, DATED 26AUGUST2014. WORK ORDER 80242 & WORK CARD 1083.

Part: DOOR SEAL — DAMAGED (EMERGENCY EXIT) · airframe 24,753 hrs · 16,810 cycles

RIGHT EMER OVERWING EXIT DOOR PRESS SEAL HAS A HOLE IN IT. REPLACED RT EMER OVERWING EXIT DOOR PRESS SEAL WITH NEW SEAL IAW AMM 52-21-07. SEE WORK ORDER 80242, WORK CARD 8045. PN SH670-36505-3 SEAL.

Part: CABLE — BROKEN (PAX DOOR) · airframe 24,753 hrs · 16,810 cycles

PAX DOOR ASSIST CABLE HAS BROKEN STRANDS. R & R PAX DOOR ASSIST CABLE IAW AMM 52-11-03 & 52-11-08. WORK ORDER 80242 WC 2138.

Part: RETAINER — CORRODED (E&E DOOR) · airframe 24,753 hrs · 16,810 cycles

MAIN AVIONICS DOOR CORRODED UNDER PRESS SEAL AT FED SIDE. R & R MAIN AVIONICS DOOR PRESS SEAL RETAINER IAW SRM 51-42-06. WORK ORDER 80242 WC 8040. PART CC670-38674-3 SEAL RETAINER.

Part: FRAME — CORRODED (FUSELAGE) · airframe 24,753 hrs · 16,810 cycles

CORROSION PIT ON ATTACHED FLANGE ON FRAME 364 BETWEEN STRINGER 27 & 26L. REPAIRED DAMAGED IAW REO 670-53-21-1115 DATED 2014-08-22 REV. SEE WORK ORDER 80242 WC 1082.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 24,753 hrs · 16,810 cycles

TCAS ANTENNA DOUBLER IS CORRODED. R & R TCAS ANTENNA DOUBLER PN SH670-32364-7 IAW SRM 51-42-06, 54-43-07, 51-42-21, 51-40-11, 51-21-00, 51-25-16 & AMM 34-43-00. WORK ORDER 80242 & WORK CARD 1084.

Part: CROSSBEAM — CRACKED (FUSELAGE) · airframe 24,753 hrs · 16,810 cycles

LEFT & RIGHT FS 280.00 CROSSBEAM IS CRACKED. R & R FS 280.00 CROSSBEAM, PN C670-34175-7S IAW REO 670-53-11-493 REV B. NDT PERFORMED DATED 21 AUGUST 2014, WORK ORDER 80242, WORK CARD 1087.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 24,753 hrs · 16,810 cycles

FS 280.00 CRAWLWAY ANGLE IS CORRODED. R & R FS 280.00 CRAWLWAY ANGLE PN C670-34256-3 IAW SRM 51-42-06, 51-42-13, 51-42-21 & 51-25-21. ORDER 80242 & WORK CARD 1085.

Part: HINGE — CRACKED (PAX DOOR) · airframe 24,753 hrs · 16,810 cycles

TOP PAX FOLDING STEP HINGE BROKEN. R & R TOP PAX FOLDING STEP HINGE IAW SRM 51-40-11 & 51-41-02. SEE WORK ORDER 80242 WC 8050.

Part: STEP — CRACKED (PAX DOOR) · airframe 24,753 hrs · 16,810 cycles

PAX DOOR TOP STEP CORNER IS CRACKED ON AFT SIDE. REPAIRED CRACK ON PAX DOOR TOP STEP AFT CORNER IAW SRM 52-11-04. SEE WORK ORDER 80242 WC 8052.

Part: FASTENER — LOOSE (SERVICE DOOR) · airframe 24,753 hrs · 16,810 cycles

GALLEY SERVICE DOOR AFT CTR LATCH PIN BRACKET LOOSE. R & R LOOSE FASTENERS IAW SRM 51-42-13 & 54-42-21. SEE WORK ORDER 80242 WC 8047.

Part: RIVET — CHAFED (PAX DOOR) · airframe 24,753 hrs · 16,810 cycles

PAX DOOR FWD & AFT OF LOWER STEP HAS 1 RIVET CHAFFED EACH SIDE. R & R 1 EACH RIVET FWD & AFT OF LOWER STEP IAW SRM 51-42-13. SEE WO 80242 WC 8041.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 24,675 hrs · 16,766 cycles

PAX DOOR OUTER HANDLE CAUTION MSG. DEFERRED IAW MEL 52-70-01 CAT A.

Part: COVER — LOOSE (EMERGENCY EXIT) · airframe 24,608 hrs · 16,726 cycles

LEFT EMER DOOR HANDLE COVER HAS LOOSE VELCRO. SECURED LT EMER DOOR HANDLE COVER IAW AMM 51-22-61.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 24,486 hrs · 16,647 cycles

PAX DOOR LATCH CAUTION MSG. COMPLIED WITH FIM TASK 52-70-04. OPERATIONS CHECK COMPLIED WITH. NO DEFECTS NOTED, NO FURTHER ACTION REQUIRED.

Part: CONNECTOR — LOOSE (PAX DOOR) · airframe 24,315 hrs · 16,540 cycles

INTERMITTENT PAX DOOR WARNING MSG IN FLIGHT. FOUND CP BACKSHELL LOOSE, SECURED CP. PERFORMED OPERATIONS CHECK ON PAX DOOR IAW 52-11-00. OPERATIONS CHECKED GOOD AT THIS TIME.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 24,222 hrs · 16,479 cycles

ABORTED TAKEOFF DUE TO LT ENG IIT FLAGGING RED & OVER TEMPED. PERFORMED FIM TASK IAW CRJ700 72-00-00, NO FAULTS NOTED AT THIS TIME. OK FOR SERVICE.

Part: FAIRING — CRACKED (FUSELAGE) · airframe 24,166 hrs · 16,440 cycles

FORWARD PAX DOOR HINGE FAIRING SCREW HOLE CRACKED. REMOVED FWD PAX DOOR HINGE FAIRING IAW AMM 53-22-85. PLACED ON CDL.

Part: DOOR FRAME — DIRTY (EMERGENCY EXIT) · airframe 24,054 hrs · 16,367 cycles

RIGHT OVERWING EMERGENCY EXIT DOOR CAUTION ON LANDING. CLEANED RT OVERWING EMERGENCY EXIT DOOR FRAME AREA, OPERATIONS CHECKED IAW AMM 52-21-00, NO DEFECTS NOTED AT THIS TIME.

Part: LIMITER — FAULTED (RUDDER) · airframe 23,709 hrs · 16,151 cycles

RUDDER LIMITER FAULT STATUS MSG. METERED ALL WIRING BETWEEN NR 1 & NR 2 SSCU'S & RUDDER LIMITER ACTUATORS IAW 27-25-01, SWAPPED NR 1 & NR 2 SSCU'S IAW AMM 27-61-05, OPERATIONS CHECKED GOOD.

Part: ACM — SEIZED (AC BAY) · airframe 23,313 hrs · 15,911 cycles

RIGHT PACK AUTO FAIL ON LANDING, FOLLOWED BY SMOKE IN THE COCKPIT. AUDIBLY VERIFIED RT ACM IS SEIZED. DEFERRED RT PACK IAW MEL 21-51-01A CAT C.

Part: CABLE — DEFECTIVE (CABIN DOOR) · airframe 22,944 hrs · 15,673 cycles

MAIN CABIN DOOR WILL NOT OPEN. R & R SUPPORT LOWER CABLE IAW CRJ700 AMM 52-11-13, OPERATIONS CHECKED GOOD.

Part: COVER — UNSECURE (CABIN) · airframe 22,858 hrs · 15,613 cycles

PLASTIC COVER CAME OFF ON FLOOR ESCAPE EMERGENCY LIGHTS BETWEEN 3 & 4 ON LT SIDE. R & R LIGHT STRIP BETWEEN 3 & 4 IAW CRJ700 AMM 33-51-01, OPERATIONS CHECKED GOOD AT THIS TIME.

Part: VALVE — FAILED (LT ENGINE) · airframe 21,876 hrs · 14,967 cycles

LEFT ENGINE SURGE VALVE CLOSED, CAUTION MESSAGE. R & R OBV IAW AMM 75-31-01. OP'S AND LEAK CHECKED GOOD AT THIS TIME.

Part: LIGHT — LOOSE (CABIN) · airframe 21,598 hrs · 14,791 cycles

LUMINESCENT STRIP LOOSE AT ROW 11, RESECURED LUMINESCENT STRIP IAW AMM 51-22-00. OK FOR SERVICE AT THIS TIME.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,822 hrs · 14,286 cycles

CEILING EMERGENCY FLOOD LIGHT INOPERATIVE IN ROW 17. R & R EMERGENCY LIGHT IAW AMM 33-51-09, OPS CHECKED GOOD AT THIS TIME.

Part: WARNING MESSAGE — ILLUMINATED (MLG) · airframe 20,780 hrs · 14,257 cycles

GEAR DISAGREE MASTER WARNING AFTER TAKEOFF.

Part: DRAIN — DIRTY (PAX DOOR) · airframe 20,370 hrs · 13,971 cycles

PAX DOOR DRAINS REQUIRE CLEANING. CLEANED PAX DOOR DRAINS.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 20,086 hrs · 13,780 cycles

EMERGENCY EXIT FLOODLIGHT HAS TWO BURNED OUT LIGHTS RT ROW 12. R & R OVERWING EMERGENCY EXIT LIGHT BULBS IAW AMM 33-51-05. OP'S CHECKED GOOD AT THIS TIME.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 20,086 hrs · 13,780 cycles

EMERGENCY EXIT FLOOD LIGHT HAS A BURNED OUT LIGHT ON ACFT LT SIDE ROW 12. R & R LT OVERWING EMERGENCY EXIT LOWER LIGHT BULB IAW AMM 33-51-05. OP'S CHECKED GOOD AT THIS TIME.

Part: INTERCOSTAL — CORRODED (BS 364) · airframe 19,754 hrs · 13,575 cycles

AVIONICS BAY DOOR FORWARD CENTER INTERCOSTALS NEAR S27 AT FS 364.00 CORRODED. R & R 2 INTERCOSTALS IN AVIONICS BAY IAW SRM 51-42-06.

Part: SUPPORT ANGLE — CORRODED (BS 280) · airframe 19,754 hrs · 13,575 cycles

COCKPIT STORAGE SUPPORT ANGLE CORRODED AT FS 280.00. R & R ANGLE AT FS 280.00 IAW SRM 51-42-06.

Part: ANGLE — CORRODED (DOOR FRAME) · airframe 19,754 hrs · 13,575 cycles

PAX DOOR SURROUND CUT OUT ANGLES CORRODED AT STRINGER 18L, FS310-FS333. REMOVED AND REPLACED ANGLES IAW SRM 51-42-06

Part: SUPPORT ANGLE — CORRODED (BS 939) · airframe 1,975,405 hrs · 13,575 cycles

AFT WING TO FUSELAGE SUPPORT ANGLE CORRODED AT FS 939. R & R ANGLE AT FS 939 IAW SRM 51-42-06.

Part: FLOOR SUPPORT — CORRODED (BS 280-319.2) · airframe 19,754 hrs · 13,575 cycles

RT FLOOR SILL FROM FS 280 TO FS 319.20 CORRODED ON STRINGER 18R. R & R RT FLOOR SILL FROM FS280.00 TO FS319.20 ON STRINGER 18R IAW SRM 51-42-06

Part: SKIN — CHAFED (BS 969-985) · airframe 19,754 hrs · 13,575 cycles

CHAFING DAMAGE ON FUSELAGE SKIN AT STRINGER 27 AT FS 969-985. REMOVED DAMAGED AREA, PERFORMED EDDY CURRENT INSPECTION, COMPLETED REPAIR INSTALLATION IAW REO 670-53-61-920.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 19,754 hrs · 13,575 cycles

BS 280 FLOORBEAM CRACKED ON BOTH SIDES. R & R FLOORBEAM IAW REO 670-53-11-047.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,993 hrs · 13,074 cycles

EMERGENCY CEILING FLOOD LIGHT ROW 15 INOPERATIVE.

Part: PROXIMITY SENSOR — OUT OF ADJUST (PAX DOOR) · airframe 18,697 hrs · 12,878 cycles

WHILE ENROUTE, INTERMITTENT PAX DOOR LATCH CAUTION MESSAGE WITH AN OCCASIONAL PROXIMITY SYS FAULT 2 STATUS MESSAGE. ADJUSTED PASSENGER DOOR PROXIMITY SENSOR, PX46 IAW AMM 52-70-04. PERFORMED OPS TEST OF DOOR IAW AMM 52-11-00.

Part: PROXIMITY SWITCH — LOOSE (PAX DOOR) · airframe 18,685 hrs · 12,869 cycles

PAX DOOR LATCH CAUTION MESSAGE FOLLOWED BY PROXIMITY SYS 2 FAULT STATUS MESSAGE. FOUND PROXIMITY SENSOR PX46, LOOSE. SECURED SENSOR, JAM NUT. OPS CHECKED IAW AMM 52-70-04.

Part: WARNING SYSTEM — MALFUNCTIONED (PAX DOOR) · airframe 18,683 hrs · 12,867 cycles

PASSENGER DOOR LATCH MESSAGE OVER 50 TIMES IN FLIGHT. ADJUSTED PX23, PERFORMED OPS CHECK OF PAX DOOR NO DEFECTS NOTED IAW AMM 52-70-04.

Part: FLAPPER VALVE — LOOSE (PAX DOOR) · airframe 18,384 hrs · 12,672 cycles

PAX DOOR OUTER FLAPPER LOOSE. PERFORMED OPS CHECK OF THE PAX DOOR IAW AMM 52-11-00, OPS CHECKED GOOD.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 18,228 hrs · 12,251 cycles

OVERHEAD EMERGENCY EXIT LIGHT ROW 7 BURNED OUT. R & R ONE OVERHEAD EMERGENCY LIGHT BULB ROW 7 IAW AMM.

Part: SEAL — LEAKING (PAX DOOR) · airframe 18,201 hrs · 12,550 cycles

PAX DOOR SQUEAL. INSPECTED ACFT AND FOUND SAFE FOR 1 TIME FERRY FLIGHT.

Part: PROXIMITY SENSOR — FAULTED (PAX DOOR) · airframe 18,054 hrs · 12,454 cycles

PASSENGER DOOR WARNING MESSAGE AND PROXIMITY SYS FAULT 2 STATUS MESSAGE. CLEANED PROXIMITY SENSORS. PERFORMED OPS CHECK OF DOOR WARNING SYS, OPS CHECKED NORMAL IAW AMM 52-70-04.

Part: PROXIMITY SWITCH — DIRTY (PAX DOOR) · airframe 18,017 hrs · 12,428 cycles

PAX DOOR WARNING, CLEANED PROXIMITY SWITCH 23, PERFORMED OPS CHECK OF PAX DOOR. OPS CHECKED OK IAW AMM 52-11-00.

Part: SWITCH — FAULTY (PAX DOOR) · airframe 18,008 hrs · 12,419 cycles

PAX DOOR CAUTION MESSAGE IN FLIGHT. R & R PX25 SWITCH PERFORMED, OPS CHECK OF PAX DOOR SYS IAW AMM 52-11-00.

Part: WARNING MESSAGE — FALSE INDICATION (PAX DOOR) · airframe 18,008 hrs · 12,419 cycles

PAX DOOR LATCH CAUTION MESSAGE IN FLIGHT. RAN ENGINE AND PRESSURIZED ACFT IAW AMM 52-70-00. NO DEFECTS NOTED AT THIS TIME.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 17,533 hrs · 12,121 cycles

2 EMERGENCY LIGHTS ARE OUT. REMOVED AND INSTALLED 2 EA LIGHT BULBS, CEILING EMERGENCY FLOOD LIGHTS IAW AMM 33-51-09.

Part: COVER — UNSECURE (EMERGENCY EXIT) · airframe 17,147 hrs · 11,869 cycles

LEFT OVERWING EXIT HANDLE COVER IS HANGING DOWN. REPLACED HOOK AND LOOP TAPE ON HANDLE COVER IAW AMM 51-22-61.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 16,978 hrs · 11,764 cycles

EMERGENCY LIGHT OVER ROW 15 IS OUT. R & R EMERGENCY LIGHT BULB OVER ROW 15 IAW AMM 33-51-09. CHECKED GOOD.

Part: RELAY — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 16,032 hrs · 11,172 cycles

EMERGENCY LIGHTS WON'T SHUTOFF IN ARMED POSITION. RESET RELAY FOR EMERGENCY LIGHTS ON PCB5 IN JB11. ALL EMERGENCY LIGHTS FUNCTION NORMALLY AT THIS TIME IAW AMM 24-06-11.

Part: CABLE — BROKEN (PAX DOOR) · airframe 15,397 hrs · 10,772 cycles

MAIN CABIN DOOR WILL NOT CLOSE AND LOCK. FOUND VENT FLAP CABLE BROKEN AND OBSTRUCTING DOOR OPERATION. R & R BROKEN CABLE IAW AMM 52-11-15. OPS CHECKED GOOD.

Part: WARNING MESSAGE — FALSE ACTIVATION (EMERGENCY LIGHTS) · airframe 15,354 hrs · 10,750 cycles

EMERGENCY LIGHTS ON STATUS MSG. RESET POWER TO ACFT AND PERFORMED OPS TEST OF EMERGENCY LIGHTS IAW AMM 33-51-00. OPS TEST GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,322 hrs · 10,730 cycles

EMERGENCY EXIT FLOOD LIGHTS INOP AT ROWS 7 AND 15. DEFFERED CEILING LEVEL EMERGENCY FLOOD LIGHTS ON DMI 16140 IAW MEL 33-51-01B, CAT C. CLEARED DMI 16140. R & R LIGHTS AT ROWS 7 AND 15 IAW AMM 33-51-09. OPS CHECKED GOOD AT THIS TIME.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 14,651 hrs · 10,322 cycles

CEILING EMERGENCY LIGHT INOP (3RD BACK). IAW TELECON, DEFERRED CEILING LIGHT ON DMI 16595 IAW MEL 33-51-01B, CAT C.

Part: IDG — FAILED (NR 1) · airframe 14,598 hrs · 10,284 cycles

IDG 1 CAUTION MESSAGE. R & R IDG 1 IAW AMM 24-11-01, OPS CHECK AND LEAK TEST GOOD AT THIS TIME.

Part: COVER — LOOSE (EMERGENCY LIGHT) · airframe 14,415 hrs · 10,156 cycles

FLOOR LEVEL EMERGENCY LIGHT PLASTIC COVER LOOSE AT SEAT 7 THROUGH 9 LT SIDE. RESECURED FLOOR LEVEL EMERGENCY LIGHT PLASTIC COVER AT SEAT 7 THROUGH 9 LT SIDE IAW AMM 33-51-01.

Part: MOUNT — CORRODED (BS 290) · airframe 14,334 hrs · 10,105 cycles

(V0XR) GALLEY MOUNT STA 290, (APROX) LBL 18, CORRODED. R & R GALLEY MOUNT IAW SRM 51-42-21.

Part: FITTING — CORRODED (BS 314 S18L) · airframe 14,334 hrs · 10,105 cycles

(V0XR) CLOSING FITTING STR 18L, FS 314 CORRODED. DRILLED UP NEW FITTING PN SH670-31840-3 AND INSTALLED NUTPLATES IAW SRM 53-20-00 AND RE-INSTALLED ON ACFT.

Part: ANGLE — CORRODED (ZONE 200) · airframe 14,334 hrs · 10,105 cycles

(V0XR) SERVICE DOOR THRESHOLD MOUNTING ANGLE CORRODED. R & R LOWER SEAL ANGLE AND THRESHOLD MOUNTING ANGLE IAW SRM 51-42-06. REINSTALLED LWR DOOR CLOSURE FITTINGS IAW SRM 51-42-00 AND 51-23-00.

Part: MOUNT — CORRODED (BS 310) · airframe 14,334 hrs · 10,105 cycles

(V0XR) GALLEY MOUNT STA 310, APPROX LBL 18, CORRODED. TRANSFERRED HOLES TO NEW GALLEY MOUNT PN SH670-31754-1 IAW SRM 53-20-00 AND INSTALLED WET.

Part: STRIKER — CORRODED (SERVICE DOOR) · airframe 14,334 hrs · 10,105 cycles

(V0XR) STRIKER SEAL SERVICE DOOR LWR THRESHOLD CORRODED BEYOND LIMITS. REINSTALLED SERVICE DOOR SCUFF PLATE IAW AMM TASK 53-21-23-400-801. INSTALLED SERVICE DOOR STRIKER IAW SRM 51-21-11, 51-41-00, 51-42-00, 51-21-16, AND 51-25-21.

Part: SILL — CORRODED (ZONE 200) · airframe 14,334 hrs · 10,105 cycles

(V0XR) AFT CARGO DOOR SILL CORRODED BEYOND LIMITS. REMOVED AND FIT, DRILL, PREP AND INSTALLED NEW AFT CARGO DOOR SILL IAW SRM CODEV, 51-41-00, 51-42-00 AND 51-23-00.

Part: MOUNT — CORRODED (BS 312) · airframe 14,334 hrs · 10,105 cycles

(V0XR) GALLEY MOUNT STA 312, RBL 6. APPROX CORRODED. INSTALLED GALLEY MOUNT IAW SRM 53-20-00, PN SH 670-32149-3.

Part: ANGLE — CORRODED (ZONE 200) · airframe 14,334 hrs · 10,105 cycles

(V0XR) SERVICE DOOR THRESHOLD LOWER SILL ANGLE CORRODED. R & R THE LOWER SILL ANGLE IAW SRM 51-42-06.

Part: ANGLE — CORRODED (ZONE 200) · airframe 14,334 hrs · 10,105 cycles

(V0XR) PAX DOOR KICK ANGLE CORRODED. TRANSFERRED HOLES AND INSTALLED NEW NUTPLATES TO ANGLE IAW SRM 53-20-00.

Part: BULKHEAD — CORRODED (BS 280) · airframe 14,334 hrs · 10,105 cycles

(V0XR) LT LOWER BULKHEAD FS 280 CORRODED OUT OF LIMITS. R & R LT LWR BULKHEAD FS 280 IAW SRM 53-11-10.

Part: THRESHOLD — CORRODED (ZONE 200) · airframe 14,334 hrs · 10,105 cycles

(V0XR) PAX DOOR THRESHOLD MIDCAP CORRODED. TRANSFERRED HOLES TO NEW PART NR SH670-31825-7 IAW SRM 53-20-00 AND INSTALLED.

Part: BULKHEAD — CORRODED (BS 280) · airframe 14,334 hrs · 10,105 cycles

(V0XR) RT LOWER BULKHEAD FS 280 CORRODED OUT OF LIMITS. R & R RT LWR BULKHEAD, FS280 IAW SRM 53-11-10.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 13,648 hrs · 9,638 cycles

EMERGENCY LIGHT OUT AT ROW NR7 (OVERHEAD CEILING LIGHT). R & R LIGHT BULB AND OPS CHECKED ROW 7 EMRGENCY LIGHT IAW AMM 33-51-00.

Part: LENS — MISSING (LIGHTS) · airframe 13,225 hrs · 9,346 cycles

SMALL RED LIGHT COVER ON BACK OF OVERWING EXIT SIGN IS MISSING. REPLACED MISSING LENS COVER IAW AMM 33-24-00.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,189 hrs · 9,325 cycles

CEILING EMERGENCY FLOODLIGHT NEAR ROW 9 INOP, IAW TELECOM, DEFFERED ON DMI 8152 IAW MEL 33-51-01B, CAT C.

Part: LINE — LOOSE (HYD SYSTEM) · airframe 11,428 hrs · 8,134 cycles

HYD NR3 SYS FLUID EMPTY RETURN TO FIELD. FOUND HYD LINE TO FILTER ASSY LOOSE RETIGHTEND IAW AMM 20-22-00 SERVICED NR3 HYD SYS IAW AMM 29-12 00. OPS & LEAK CHECKED GOOD AT THIS TIME.

Part: LENS — MISINSTALLED (EMERGENCY LIGHT) · airframe 10,110 hrs · 7,192 cycles

SERVICE DOOR EMERGENCY LIGHT LENS POSITION INCORRECT. CORRECTED SERVICE DOOR EMERGENCY LT LENS POSITION BY TURNING LENSE TOP TO 11 O`CLOCK POSITION IAW AMM 33-51-15.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 9,894 hrs · 7,036 cycles

EMERGENCY LIGHTS ON IN CABIN, DISAGREEMENT WITH SWITCH SELECTION. RESET POWER TO ACFT AND PREFORMED OPS TEST OF EMERGENCY LIGHT SYS IAW AMM 33-51-00 NO DEFECTS NOTED.

Part: WARNING LIGHT — FALSE ACTIVATION (A/C BUSS) · airframe 9,481 hrs · 6,739 cycles

POSS AC BUSS 1 FAIL. T/S TO TRIP GEN 1 SW, GROUND RUN WITH CREW. RESET NR 1 GEN. OPS CHECK NORMAL IAW AMM 24-11-00.

Part: WARNING MESSAGE — ILLUMINATED (SLATS) · airframe 9,365 hrs · 6,653 cycles

SLATS FAIL CAUTION MESSAGE. COMPLIED WITH MFG SL 27-054 REV C, MANUALLY EXTENDED SLATS TO 20 DEGREES EICAS POSITION AND MEASURED WITH CLINOMETERS TO VERIFY DEGREE POSITION. ACFT RELEASED FOR ONE TIME FERRY FLIGHT.

Part: LIGHT — LOOSE (CABIN) · airframe 8,861 hrs · 6,297 cycles

ESCAPE PATH LIGHTING ON SVC DOOR COMING OFF. RESECURED ESCAPE PATH LIGHTING ON SVC DR IAW AMM 33-51-01.

Part: WARNING SYSTEM — MALFUNCTIONED (CABIN) · airframe 7,902 hrs · 5,579 cycles

EMERGENCY LIGHTS ON STATUS MESSAGE. CYCLED POWER, ACCOMPLISHED EMERGENCY LIGHTS RESET IAW M/M 33-51-00.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 7,281 hrs · 5,184 cycles

FLMX-ORD - PAX DOOR EMERGENCY LIGHT LENS BROKEN. PLACED ON DMI CONTROL NUMBER 8477 PER CDL 33-60. (A)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 6,383 hrs · 4,576 cycles

AFT CEILING LEVEL FLOODLIGHT INOPERATIVE. DEFERRED LIGHT IAW MEL 33-51-01-2A.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 5,850 hrs · 4,218 cycles

CABIN LEVEL CEILING EMERGENCY LIGHT INOP AT ROW 14 AND 15. DEFERRED IAW MEL 33-51-01-2A.

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS) · airframe 4,700 hrs · 3,378 cycles

EMERGENCY LIGHTS BY SERVICE DOOR INOPERATIVE. REPLACED BULB OPS OK.