N676CA

Part: ROD — INOPERATIVE (ZONE 800) · airframe 38,400 hrs · 27,142 cycles

UNABLE TO OPEN PAX DOOR REPLACED PAX DOOR VENT FLAP ROD ASSY

Part: LAMP — INOPERATIVE (ZONE 200) · airframe 37,361 hrs · 26,319 cycles

CEILING EMERGENCY LIGHT AT ROW 10 INOP RELAMPED CEILING EMER LIGHT IAW CRJ 900 AMM 33-51-09 OPS CHECK GOOD

Part: LAMP — INOPERATIVE (UNKNOWN) · airframe 33,893 hrs · 23,400 cycles

EMERGENCY EXIT SIGN LIGHT INOP, CABIN CEILING. R & R LAMP BULB IAW AMM 33-51-07, PN ON/OFF: 6100945

Part: SPLICE — CORRODED · airframe 31,082 hrs · 20,996 cycles

PANEL 191AB SPLICE JOINT PLATE CORRODED IN MULTIPLE AREAS WITH A DEPTH OF .016". REMOVE AND REPLACE SPLICE JOINT.

Part: PLATE — CRACKED · airframe 31,082 hrs · 20,996 cycles

LH ENGINE LOWER TRANSCOWL BIFURCATION PANEL NYLON PLATE BROKEN MANUFACTURED NEW PLATE PER EA# CRJ954-13327.

Part: STRINGER — CORRODED · airframe 31,082 hrs · 20,996 cycles

STR 26L HAS MULTIPLE SPOTS OF CORROSION BETWEEN FS280-333 WITH UP TO 100% MATERIAL LOSS. REMOVE AND REPLACE STR 26L.

Part: STRINGER — CORRODED · airframe 31,082 hrs · 20,996 cycles

STR 24L CORRODED BETWEEN FS333-364. CORROSION MEASURES 7.0"X1.0"X.040" DEEP. REMOVE AND REPLACE STRINGER.

Part: INTERCOSTAL — CORRODED · airframe 31,082 hrs · 20,996 cycles

INTERCOSTAL BETWEEN FS349-364 JUST RIGHT OF STR27 LOWER FLANGE HAS EXFOLIATED CORROSION. REMOVE AND REPLACE INTERCOSTAL.

Part: SKIN — CORRODED · airframe 31,082 hrs · 20,996 cycles

FEED BAGGAGE DOOR SURROUND STRUCTURE BACKING SKIN CORRODED BETWEEN STR 24L-25L AND FS 517-565. MULTIPLE SPOTS OF CORROSION WITH A MAX DEPTH OF .007". REPAIRED CORROSION PER EA CRJ953-13302.

Part: COVER — CORRODED · airframe 31,082 hrs · 20,996 cycles

PAX DOOR UPPER, FWD AND AFT CORNER COVERS HAVE EXFOLIATED CORROSION. REPLACE CORNER COVERS. AFT P/N 600-31902-287 AND FWD P/N 600-31902-288

Part: ANGLE — CORRODED · airframe 31,082 hrs · 20,996 cycles

SUPPORT ANGLE AT STR 22R BETWEEN FS280-295 HAS MULTIPLE SPOTS OF EXFOLIATED CORROSION. REPLACE SUPPORT ANGLE

Part: NONE — CORRODED · airframe 31,082 hrs · 20,996 cycles

FS280.00 BUTT STRAP HAS AREAS OF CORROSION FROM STR 26R-26L. DIMENSIONS AFTER BLEND AS FOLLOWS. STR26R-27 10.0"X6.0"X.005" MAX DEPTH, STR26L-27 10.0"X6.0"X.005" MAX DEPTH REPAIRED CORROSION PER EA CRJ953-13363

Part: STRINGER — CORRODED · airframe 31,082 hrs · 20,996 cycles

STR 23L HAS MULTIPLE AREAS OF CORROSION BETWEEN FS319-333 WITH UP TO 100% MATERIAL LOSS. REPLACED STR 23L IAW EA CRJ953-13351

Part: NONE — CORRODED · airframe 31,082 hrs · 20,996 cycles

AVIONICS BAY DOOR SEAL RETAINER CORRODED. CORROSION MEASURES 10.0"X.200"X100% MATERIAL LOSS. REMOVE AND REPLACE SEAL RETAINER.

Part: FORMER — CORRODED · airframe 31,082 hrs · 20,996 cycles

PAX DOOR AFT FORMER HAS EXFOLIATED CORROSION ON THE INNER SIDE. REPLACE AFT FORMER.

Part: INTERCOSTAL — CORRODED · airframe 31,082 hrs · 20,996 cycles

PAX DOOR INTERCOSTAL HAS EXFOLIATED CORROSION ON THE WEB. 6TH INTERCOSTAL DOWN ON THE AFT SIDE. REPLACE PAX DOOR INTERCOSTAL.

Part: INTERCOSTAL — CORRODED · airframe 31,082 hrs · 20,996 cycles

PAX DOOR INTERCOSTAL HAS EXFOLIATED CORROSION ON THE LOWER FLANGE. 4TH INTERCOSTAL DOWN ON THE AFT SIDE. REPLACE PAX DOOR INTERCOSTAL.

Part: INTERCOSTAL — CORRODED · airframe 31,082 hrs · 20,996 cycles

PAX DOOR THIRD INTERCOSTAL DOWN IN MIDDLE OF DOOR HAS EXFOLIATED CORROSION ON THE WEB. REPLACE INTERCOSTAL.

Part: INTERCOSTAL — CORRODED · airframe 31,082 hrs · 20,996 cycles

PAX DOOR INTERCOSTAL CORRODED 3RD INTERCOSTAL DOWN ON THE FWD SIDE. UPPER FLANGE CORRODED 3.0"X1.0"X.019" DEEP. REPLACE PAX DOOR INTERCOSTAL.

Part: INTERCOSTAL — CORRODED · airframe 31,082 hrs · 20,996 cycles

PAX DOOR SEVENTH INTERCOSTAL DOWN MIDDLE OF PAX DOOR HAS EXFOLIATED CORROSION ON THE WEB. REPLACE INTERCOSTAL.

Part: INTERCOSTAL — CORRODED · airframe 31,082 hrs · 20,996 cycles

PAX DOOR INTERCOSTAL CORRODED 4TH INTERCOSTAL DOWN ON THE FWD SIDE. UPPER FLANGE CORRODED 3.0"X1.0"X.022" DEEP. REPLACE PAX DOOR INTERCOSTAL.

Part: INTERCOSTAL — CORRODED · airframe 31,082 hrs · 20,996 cycles

PAX DOOR FIRST INTERCOSTAL DOWN MIDDLE OF PAX DOOR HAS CORROSION ON THE WEB. BLENDED CORROSION DIMENSIONS AS FOLLOWS. 7.0"X3.0"X.021" DEEP. REPLACE INTERCOSTAL.

Part: INTERCOSTAL — CORRODED · airframe 31,082 hrs · 20,996 cycles

PAX DOOR FIFTH INTERCOSTAL DOWN ON FWD SIDE OF DOOR HAS EXFOLIATED CORROSION ON WEB. REPLACE INTERCOSTAL.

Part: STRINGER — CORRODED · airframe 31,082 hrs · 20,996 cycles

STR 24R HAS MULTIPLE AREAS OF CORROSION BETWEEN FS280-310 WITH UP TO 100% MATERIAL LOSS. REPLACED STR 24R FROM FS280-333 IAW EA CRJ953-13283

Part: STRINGER — CORRODED · airframe 31,082 hrs · 20,996 cycles

STR 22R HAS MULTIPLE AREAS OF CORROSION BETWEEN FS280-333 WITH UP TO 100% MATERIAL LOSS. REPLACED STR 22R FROM FS280-333 IAW EA CRJ953-13278.

Part: STRINGER — CORRODED · airframe 31,082 hrs · 20,996 cycles

STR 19R HAS MULTIPLE SPOTS OF CORROSION BETWEEN FS295-310 WITH UP TO 100% MATERIAL LOSS. REMOVE AND REPLACE STR 19R.

Part: SPLICE — CORRODED · airframe 31,082 hrs · 20,996 cycles

STR 22R SPLICE AT FS333 HAS SEVERAL AREAS OF CORROSION WITH A MAX DEPTH OF .043". REMOVE AND REPLACE STRINGER SPLICE.

Part: STRINGER — CORRODED · airframe 31,082 hrs · 20,996 cycles

STR 24R HAS MULTIPLE AREAS OF CORROSION BETWEEN FS333-349 WITH A MAX DEPTH OF .038". REPAIRED STRINGER PER CRJ900 SRM 53-00-03.

Part: CLEAT — CORRODED · airframe 31,082 hrs · 20,996 cycles

CLEAT ON STR 22R AT FS333 HAS AREA OF CORROSION WITH 100% MATERIAL LOSS. REMOVE AND REPLACE CLEAT.

Part: STRINGER — CORRODED · airframe 31,082 hrs · 20,996 cycles

STRINGER 21R HAS MULTIPLE AREAS OF CORROSION WITH 100% MATERIAL LOSS BETWEEN FS364-379 REMOVE AND REPLACE STRINGER 21R.

Part: STRINGER — CORRODED · airframe 31,082 hrs · 20,996 cycles

STRINGER 22L HAS MULTIPLE AREAS OF CORROSION BETWEEN FS349-400 WITH 100% MATERIAL LOSS. REMOVE AND REPLACE STRINGER.

Part: STRINGER — CORRODED · airframe 31,082 hrs · 20,996 cycles

STR 23L HAS CORROSION WITH 100% MATERIAL LOSS BETWEEN FS379-394. REMOVE AND REPLACE STRINGER.

Part: SPLICE — CORRODED · airframe 31,082 hrs · 20,996 cycles

STRINGER 23L SPLICE AT FS333 HAS AREA OF CORROSION WITH 100% MATERIAL LOSS. REMOVE AND REPLACE STRINGER SPLICE

Part: FRAME — CORRODED · airframe 31,082 hrs · 20,996 cycles

FS319.70 FRAME CORRODED AT STR 18L. BLENDED CORROSION, DIMENSIONS AS FOLLOWS: 2.3"X1.45"X.004" DEEP. FOUND TO BE WITHIN LIMITS IAW CRJ900 SRM 53-21-23.

Part: STRINGER — CORRODED · airframe 31,082 hrs · 20,996 cycles

STRINGER 23L HAS AREA OF CORROSION BETWEEN FS501-517 WITH 100% MATERIAL LOSS. REMOVE AND REPLACE STRINGER.

Part: PLATE — DAMAGED · airframe 31,082 hrs · 20,996 cycles

LOW PRESSURE GROUND AIR PROTECTION PLATE GOUGED. DAMAGE IN THE UPPER RH CORNER IS .035" DEEP AND GREO 670-53-61-1382 ONLY ALLOWS FOR .030" DEPTH OF DAMAGE. FABRICATED AND REPLACED PROTECTION PLATE IAW EA CRJ953-13357.

Part: HANDLE — CRACKED · airframe 31,082 hrs · 20,996 cycles

PAX DOOR OUTER HANDLE FLAP CRACKED. REMOVED AND REPLACED FLAP.

Part: DUCT — CORRODED · airframe 31,082 hrs · 20,996 cycles

APU EXHAUST DUCT HAS MULTIPLE AREAS OF CORROSION WITH A MAX DEPTH OF .006" REMOVE AND REPLACE APU EXHAUST DUCT.

Part: FRAME — CORRODED · airframe 31,082 hrs · 20,996 cycles

FS319.70 FRAME CORRODED BETWEEN STR 26R-26L. CORROSION MEASURES: 5.0"X.75"X.020" DEEP, 4.5"X.75"X.020" DEEP. REMOVE AND REPLACE FRAME.

Part: STRINGER — CORRODED · airframe 31,082 hrs · 20,996 cycles

STR 21L CORRODED BETWEEN FS349-364 WITH 100% MATERIAL LOSS. REMOVE AND REPLACE STRINGER.

Part: STRINGER — CORRODED · airframe 31,082 hrs · 20,996 cycles

STR 22R HAS MULTIPLE AREAS OF CORROSION BETWEEN FS333-349 WITH A MAX DEPTH OF .040". REMOVE AND REPLACE STRINGER.

Part: SKIN — CORRODED · airframe 31,082 hrs · 20,996 cycles

FUSELAGE BELLY SKIN HAS CORROSION JUST AFT OF FS847+16 BETWEEN STR 26R AND 26L. BLENDED CORROSION DIMENSIONS AS FOLLOW: .60" DIAMETER X .005" DEEP. FOUND TO BE WITHIN LIMITS IAW CRJ900 SRM 53-51-01.

Part: PANEL — WORN · airframe 31,082 hrs · 20,996 cycles

RH FLAP ACCESS PANEL 684ET CHAFED. BLENDED CHAFE DIMENSIONS AS FOLLOWS: 4.0"X.75"X.015" DEEP. REMOVE AND REPLACE PANEL.

Part: FAIRING — DEFORMED · airframe 31,082 hrs · 20,996 cycles

RH UPPER TRANSCOWL HINGE LINE FAIRING BUCKLED ON AFT END. REMOVE AND REPLACE HINGE LINE FAIRING.

Part: RETAINER — CORRODED · airframe 31,082 hrs · 20,996 cycles

AVIONICS DOOR SEAL RETAINER HAS CORROSION WITH 100% MATERIAL LOSS. REMOVE AND REPLACE RETAINER.

Part: HINGE — DEFORMED · airframe 31,082 hrs · 20,996 cycles

PAX DOOR HINGE ON FUSELAGE SIDE HAS ELONGATED HOLES. AFT 4 HOLES MEASURE .315". REMOVE AND REPLACE FUSELAGE SIDE PAX DOOR HINGE.

Part: NONE — CORRODED · airframe 31,082 hrs · 20,996 cycles

SERVICE DOOR LOWER SEAL STRIKER HAS AREA OF CORROSION WITH 100% MATERIAL LOSS. REMOVE AND REPLACE SEAL STRIKER.

Part: FRAME — CORRODED · airframe 31,082 hrs · 20,996 cycles

FS661.00 FRAME HAS CORROSION ON THE REAR FACE AT LBL45. FRAME CORROSION 1.0" X .7" X.001" DEEP. FRAME REINFORCEMENT ANGLE CORROSION 3.0" X 2.5" X .002" DEEP. REPAIRED CORROSION PER EA'S CRJ953-13306 AND CRJ953-13305.

Part: STRINGER — CORRODED · airframe 31,082 hrs · 20,996 cycles

STRINGER 19R HAS MULTIPLE AREAS OF CORROSION BETWEEN FS661+16 TO FS661+32 WITH 100% MATERIAL LOSS. REPAIRED STRINGER IAW CRJ900 SRM 53-00-03.

Part: FRAME — CORRODED · airframe 31,082 hrs · 20,996 cycles

FS645 FRAME CORRODED AT LBL45. CORROSION MEASURES 1.0" X .70" X .022" DEEP. REMOVE AND REPLACE FS645 FRAME.

Part: FRAME — CORRODED · airframe 31,082 hrs · 20,996 cycles

FS501 FRAME LOWER FLANGE CORRODED BETWEEN STR 23L-24L WITH 100% MATERIAL LOSS. PERFORM LOWER FLANGE REPAIR PER CRJ900 SRM 53-00-06.

Part: INTERCOSTAL — CORRODED · airframe 31,082 hrs · 20,996 cycles

INTERCOSTAL AT STR 24L BETWEEN FS501-517 CORRODED. CORROSION MEASURES 4.5" X .30" X .013" DEEP. REMOVE AND REPLACE INTERCOSTAL.

Part: STRINGER — CORRODED · airframe 31,082 hrs · 20,996 cycles

STRINGER 24L HAS AREA OF CORROSION BETWEEN FS501-517 WITH 100% MATERIAL LOSS. REMOVE AND REPLACE STRINGER.

Part: STEP — CORRODED · airframe 31,082 hrs · 20,996 cycles

PAX DOOR TOP STEP HAS AREA OF CORROSION WITH 100% MATERIAL LOSS. REMOVE AND REPLACE STEP.

Part: INTERCOSTAL — CORRODED · airframe 31,082 hrs · 20,996 cycles

LH FLOOR SILL CORROSION BETWEEN FS985-1000 CORROSION DIMENSIONS AS FOLLOWS: 4.8" X 1.8" X .017" DEEP, 2.0" X 1.8" X .004" DEEP. REMOVED CORROSION IAW EA# CRJ953-13219.

Part: SPLICE — CORRODED · airframe 31,082 hrs · 20,996 cycles

STR 18R JOINT SPLICE CORRODED AT FS477.00. SPLICE CORRODED AT FWD END WITH 100% MATERIAL LOSS. REPLACED STR 18R JOINT SPLICE.

Part: FRAME — CORRODED · airframe 31,082 hrs · 20,996 cycles

FS333.00 FRAME HAS AREA OF CORROSION WITH 100% MATERIAL LOSS AT STR 26L. REMOVE AND REPLACE FRAME.

Part: SKIN — CORRODED · airframe 31,082 hrs · 20,996 cycles

AFT BAGGAGE DOOR SURROUND STRUCTURE HAS MULTIPLE AREAS OF CORROSION ON THE BACKING SKIN BETWEEN STR 25L-24L AND FS629-661+16 WITH A MAX DEPTH OF .004". REPAIRED CORRODED AREA PER EA CRJ953-13250.

Part: DOUBLER — CORRODED · airframe 31,082 hrs · 20,996 cycles

ADF ANTENNA DOUBLER HAS MINOR SURFACE CORROSION. CORROSION MEASURES 4.75" X 3.75" X .004" DEEP. REMOVED CORROSION AND FOUND TO BE WITHIN LIMITS IAW CRJ900 SRM 53-00-01

Part: DOUBLER — CORRODED · airframe 31,082 hrs · 20,996 cycles

FWD BAGGAGE DOOR SURROUND STRUCTURE H DOUBLERS CORRODED BETWEEN STR 24L-25L AND FS517-565. FWD DOUBLER MULTIPLE AREAS OF CORROSION WITH A MAX DEPTH OF .001". AFT DOUBLER MULTIPLE AREAS OF CORROSION WITH A MAX DEPTH OF .001" REPAIRED CORROSION PER EA'S CRJ953-13300 AND CRJ953-13301.

Part: DOUBLER — CORRODED · airframe 31,082 hrs · 20,996 cycles

CENTER BAGGAGE DOOR SURROUND STRUCTURE H DOUBLERS CORRODED BETWEEN STR 24L-25L. FWD DOUBLER MULTIPLE AREAS OF CORROSION WITH A MAX DEPTH OF .004". AFT DOUBLER MULTIPLE AREAS OF CORROSION WITH A MAX DEPTH OF .004". REPAIRED CORROSION PER EA'S CRJ953-13298 AND CRJ953-13299.

Part: SKIN — CORRODED · airframe 31,082 hrs · 20,996 cycles

FWD BAGGAGE BAY BELLY SKIN HAS CORROSION BETWEEN FS517-533 AND STR27-26L. CORROSION MEASURES 15.0" X 1.0" X .005" DEEP. REMOVED CORROSION AND FOUND TO BE WITHIN LIMITS PER CRJ900 SRM 53-31-01.

Part: PLATE — CORRODED · airframe 31,082 hrs · 20,996 cycles

SERVICE DOOR LOWER SILL PROTECTOR PLATE HAS AREAS OF CORROSION WITH 100% MATERIAL LOSS. REMOVE AND REPLACE PROTECTOR PLATE.

Part: FITTING — CORRODED · airframe 31,082 hrs · 20,996 cycles

SERVICE DOOR SURROUND STRUCTURE FRAME FITTING AT FS319.7 CORRODED. BLENDED CORROSION DIMENSIONS AS FOLLOWS: 1.0" X .50" X .040" DEEP. REMOVE AND REPLACE FRAME FITTING.

Part: SKIN — CHAFED · airframe 31,082 hrs · 20,996 cycles

CENTER BAGGAGE DOOR HAS CHAFING ON INNER SKIN. DIMENSIONS AFTER BLEND AS FOLLOWS: FWD .8" X .160" X .002" DEEP, AFT 1.8" X .20" X .010" DEEP REPAIRED CENTER BAGGAGE DOOR INNER SKIN PER EA CRJ952-13358

Part: FRAME — CORRODED · airframe 31,082 hrs · 20,996 cycles

FS295.00 FRAME HAS AREA OF CORROSION 1.0" X 1.0" X .023" DEEP AT STR27 REMOVE AND REPLACE FRAME

Part: STRINGER — CORRODED · airframe 31,082 hrs · 20,996 cycles

STR 23R HAS CORROSION BETWEEN FS364-379 WITH 100% MATERIAL LOSS REMOVE AND REPLACE STRINGER

Part: SEAT TRACK — CORRODED · airframe 31,082 hrs · 20,996 cycles

RH SEAT TRACK HAS MULTIPLE AREAS OF CORROSION FROM FS693-834 WITH A MAX DEPTH OF .014" REMOVED AND REPLACED RH SEAT TRACK FROM FS693-834.

Part: SEAT TRACK — CORRODED · airframe 31,082 hrs · 20,996 cycles

RH SIDE CABIN SEAT TRACK HAS MULTIPLE SPOTS OF CORROSION BETWEEN FS477-693 WITH A MAX DEPTH OF .018" REMOVED AND REPLACED RH SEAT TRACK FROM FS477-581.

Part: SEAT TRACK — CORRODED · airframe 31,082 hrs · 20,996 cycles

RBL9 SEAT TRACK HAS MULTIPLE AREAS OF CORROSION FROM FS847-865 WITH A MAX DEPTH OF .014" REMOVED AND REPLACED RBL9 SEAT TRACK FROM FS847-865.

Part: SEAT TRACK — CORRODED · airframe 31,082 hrs · 20,996 cycles

RH SIDE CABIN SEAT TRACK HAS MULTIPLE SPOTS OF CORROSION BETWEEN FS847-977 WITH A MAX DEPTH OF .016" REMOVED AND REPLACED LH SEAT TRACK FROM FS847-975.

Part: SEAT TRACK — CORRODED · airframe 31,082 hrs · 20,996 cycles

LH SIDE CABIN SEAT TRACK HAS MULTIPLE SPOTS OF CORROSION BETWEEN FS477-693 WITH A MAX DEPTH OF .018" REMOVED AND REPLACED LH SEAT TRACK FROM FS581-693.

Part: SEAT TRACK — CORRODED · airframe 31,082 hrs · 20,996 cycles

LBL9 SEAT TRACK HAS MULTIPLE AREAS OF CORROSION FROM FS834-979 WITH A MAX DEPTH OF .015". REMOVED AND REPLACED LBL9 SEAT TRACK FROM FS834-979.

Part: INTERCOSTAL — CORRODED · airframe 31,082 hrs · 20,996 cycles

INTERCOSTAL AT STR 21L BETWEEN FS310-333 HAS EXFOLIATED CORROSION ACROSS THE WEB. REMOVE AND REPLACE INTERCOSTAL.

Part: INTERCOSTAL — CORRODED · airframe 31,082 hrs · 20,996 cycles

INTERCOSTAL AT STR21L BETWEEN FS333-349 HAS CORROSION WITH 100% MATERIAL LOSS. REMOVE AND REPLACE INTERCOSTAL.

Part: LEVER — CORRODED · airframe 31,082 hrs · 20,996 cycles

PAX DOOR FWD PULL IN LEVER HAS WEAR ON UPPER END. WEAR IS .058" DEEP. REPLACE FWD PULL IN LEVER.

Part: BRACKET — CORRODED · airframe 31,082 hrs · 20,996 cycles

PAX DOOR HANDRAIL MOUNTING LOCATOR BRACKET HAS GOUGES THAT ARE .050" DEEP REMOVE AND REPLACE BRACKET

Part: RISER — CORRODED · airframe 31,082 hrs · 20,996 cycles

PAX DOOR FWD STEP RISER HAS AREA OF CORROSION WITH 100% MATERIAL LOSS. REMOVED AND REPLACED FWD STEP RISER.

Part: STRIKER — DAMAGED · airframe 31,082 hrs · 20,996 cycles

FWD BAGGAGE DOOR SEAL STRIKER GOUGED. BLENDED GOUGE MEASUREMENTS AS FOLLOWS. 2.0" X .3" X .061" DEEP REMOVE AND REPLACE SEAL STRIKER

Part: DIAPHRAGM — CRACKED · airframe 31,082 hrs · 20,996 cycles

LH WHEEL WELL FWD DIAPHRAGM HAS 1.5" CRACK REMOVE AND REPLACE DIAPHRAGM

Part: FORMER — CORRODED · airframe 31,082 hrs · 20,996 cycles

FORMER601R318031-5FORMER FORMER601R318031-5

Part: INSERT — CRACKED · airframe 31,082 hrs · 20,996 cycles

LH UPPER TRANSCOWL BIFURCATION PANEL NYLON INSERT BROKEN REPLACE NYLON INSERT PER EA CRJ954-13473

Part: BRACKET — CORRODED · airframe 31,082 hrs · 20,996 cycles

BRAKE ACCUMULATOR FWD I/B BRACKET HAS 1.5" CRACK REMOVED AND REPLACED BRACKET.

Part: ANGLE — CORRODED · airframe 31,082 hrs · 20,996 cycles

NUTPLATE ANGLE UNDER PANEL 642AZ CORRODED. CORROSION MEASURES 2.5" X 1.0" X .030" DEEP REMOVE AND REPLACE ANGLE.

Part: INTERCOSTAL — CORRODED · airframe 31,082 hrs · 20,996 cycles

INTERCOSTAL BELOW STR 21R AT FS 295.00 HAS MULTIPLE AREAS OF CORROSION WITH 100% MATERIAL LOSS. REMOVE AND REPLACE INTERCOSTAL.

Part: NONE — CORRODED · airframe 31,082 hrs · 20,996 cycles

NUTPLATE ANGLE UNDER PANEL 542AZ CORRODED. CORROSION MEASURES 3.0" X 1.0" X .037" DEEP REMOVED AND REPLACE ANGLE.

Part: DOUBLER — CORRODED · airframe 31,082 hrs · 20,996 cycles

CANNON PLUG DOUBLER AT AFT POTABLE WATER SERVICE POINT CORRODED. CORROSION MEASURES 2.5" X .5" CORROSION IS EXFOLIATED. REMOVE AND REPLACE DOUBLER

Part: POST — CRACKED · airframe 31,082 hrs · 20,996 cycles

PAX DOOR AFT UPPER HANDRAIL POST HAS 3 EA CRACKS. REMOVED AND REPLACED HANDRAIL POST.

Part: STRAP — CRACKED · airframe 31,082 hrs · 20,996 cycles

AFT WING TO BODY FAIRING 195DL CENTER JOINT STRAP HAS 1.25" CRACK REMOVED AND REPLACE STRAP

Part: HANDLE — CRACKED · airframe 31,082 hrs · 20,996 cycles

PAX DOOR INNER HANDLE HAS .5" CRACK AT ATTACHMENT AREA. REMOVED AND REPLACED PAX DOOR INNER HANDLE.

Part: SKIN — CORRODED · airframe 31,082 hrs · 20,996 cycles

PAX DOOR INNER SKIN HAS AREAS OF EXFOLIATED CORROSION. REPLACE SKIN.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 30,292 hrs · 20,282 cycles

RIGHT WING FWD AND LEFT WING REAR EXTERIOR EMERGENCY OVERWING LIGHTS INOP. REMOVED & REPLACED #5 BATTERY PACK PS42 IAW AMM 33-51-17 OPS TEST GOOD AT THIS TIME. P/N OFF AD-2013-1A P/N ON 2013-1ASMI S/N OFF 141347 S/N ON 12437.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 28,299 hrs · 18,759 cycles

DURING THE FA'S PREFLIGHT INSPECTION, IT WAS OBSERVED THAT THE EMERGECNY EXIT SIGN IN ROW 12CD HAD A BURNT-OUT LIGHT BULB. DEFERRED RIGHT SIDE EMERGENCY LIGHT STRIP AT ROW 12CD IAW MEL 33-51-1F. PLACARD INSTALLED, MOC NOTIFIED 97766. (25% LIGHTING INOPERATIVE). RELAMPED FLOOR LEVEL LIGHTED EMERGENCY EXIT SIGN AT 12CD IAW CRJ 900 33-51-11(AMM). OPS CHECK GOOD. NO FURTHER DEFECTS NOTED AT THIS TIME.

Part: LIFE VEST — MISSING (CABIN) · airframe 26,683 hrs · 17,566 cycles

INFANT LIFE PRESERVER MISSING. INSTALLED INFANT LIFE PRESERVER IAW JOB CARD.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 26,619 hrs · 17,522 cycles

AFTER TAKEOFF, GEAR DISAGREE WARNING MSG AFTER GEAR RETRACTION. FOLLOWED BY STEERING INOP CAUTION. RAN THE QRH FOR BOTH AND RETURNED TO RDU. AFTER LANDING RAN THE FAULT RESET PROCEDURE STEERING INOP MSG GONE AND TAXIED TO GATE. PERFOMED MLG STURT RE-PACK IAW JOB CARD 900-32-710-901. PERFORMED MLG EXTENSION & RETRACTION OPS CHECK IAW AMM 32-30-00. OPS CHECK GOOD. PERFORMED NOSEWHEEL STEERING OPS CHECK IAW AMM 32-51-00. OPS CHECK GOOD. ACFT OK FOR SERVICE

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 26,311 hrs · 17,275 cycles

EXIT SIGN BULBS BURNED OUT. R&R BULBS FOR EXIT SIGN AS REQUIRED.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 25,830 hrs · 16,915 cycles

LEFT OTBD FLAP HAS A DENT AT FLAP STATION 200. REPAIRED IAW SRM 57-53-01-201-001-A01, STEP D, REPAIR TYPE 4.

Part: SKIN — CHAFED (RT COWLING) · airframe 23,581 hrs · 15,286 cycles

RT ENGINE CORE COWL INTERNAL SKIN CHAFED DAMAGED IN MULTIPLE AREAS. COMPLIED WITH EC/TC REO 670-54-23-959,REO 670-54-23-959, EC/TC REO 690-54-23-208,REO 690-54-23-208, FUR-71-10-00289, EC/TC FUR-71-10-00289,EC/TC 25-2014-387, EA 25-2014-387.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 23,581 hrs · 15,286 cycles

TCAS DOUBLER INTERNAL SKIN CORRODED AT STR 27 BTW FRAMES 295-310. REMOVED AND REPLACED TCAS DOUBLER BTW FS 295-310 AT STR 27 PER SRM 51-42-06-001-001-A01 AND DRAWING SH670-30023. P/N SH670-32364-7.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 23,581 hrs · 15,286 cycles

RT ATC ANTENNA DOUBLER INTERNAL SKIN CORRODED AT FS 356.50 BTW STR 26R-25R. REMOVED AND REPLACED RT ATC ANTENNA INTERNAL DOUBLER IAW SRM 51-42-06-001-001-A01,51-21-06-001-001-A01.

Part: CLEAT — CORRODED (FUSELAGE) · airframe 23,581 hrs · 15,286 cycles

CORRODED INTERCOSTAL AT STRINGER 20R BETWEEN FRAMES 319.70-333.00. REMOVED AND REPLACED INTERCOSTAL CLEATS P/N SH670-32014-2S, SH670-32605-2, SH670-32014-1 IAW SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01, AND DRAWING SH670-31950.

Part: BRACKET — CORRODED (FUSELAGE) · airframe 23,581 hrs · 15,286 cycles

CORROSION ON ANCHOR SUPPORT IN FWD CARGO BAY FS 565 AFT OF DOOR CUTOUT. REMOVED AND REPLACED ANCHOR BRACKET P/N SH670-33390-2 IAW SRM 51-42-15-001-001-A01, 51-42-21-001-001-A01, AND DRAWING SH670-33600.

Part: CROSSBEAM — CORRODED (FUSELAGE) · airframe 23,581 hrs · 15,286 cycles

CROSSBEAM AT FS 333 RBL9 IS CORRODED. COMPLIED WITH ECTC REO 690-53-21-898.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 23,581 hrs · 15,286 cycles

CORRODED INTERCOSTAL AT RBL 2 BTW FRAME 349 & 364. REMOVE AND REPLACED INTERCOSTAL AND GUSSET ON RBL 2 BTW FRAMES 349-364 IAW SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01,51-42-21-001-001-A01. P/N SH670-32075-4 AND DRAWING SH670-32075.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 23,581 hrs · 15,286 cycles

RT CABIN FLOOR SILL CORRODED AT FS 281-319.70 RBL 42. REMOVED AND REPLACED RT FLOOR SILL AT FS 280 WITH A NEW SILL IAW EC/TC REO 670-53-21-139 REV A AND REO 670-53-21-139 REV A DATED 2013-10-02 AS WRITTEN.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 31,245 hrs · 22,261 cycles

CORRODED INTERCOSTAL AT STR 20 RT BTW FRAMES 310-319.70. REMOVED AND REPLACED INTERCOSTAL AT STR 20 RT BTW FRAMES 310-319.70 PER SRM 51-42-06-001-001-A01, AND DRAWING SH670-31950 P/N SH670-32047-1.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 31,245 hrs · 22,261 cycles

CORROSION ON INTERCOSTAL AT APPROX FS 1000 RBL 39. COMPLIED WITH EC/TC REO 690-53-61-673 AND REO 690-53-61-673.

Part: RETAINER — DENTED (CARGO DOOR) · airframe 31,245 hrs · 22,261 cycles

NR 1 FWD CARGO DOOR LOWER FWD OUTER SEAL RETAINER DENTED. COMPLIED WITH EC/TC REO 670-52-35-127-01 AND REO 670-52-35-127-01 FOR REPAIR OF NR 1 FWD BAG BAY DOOR.

Part: RETAINER — DENTED (CARGO DOOR) · airframe 31,245 hrs · 22,261 cycles

NR 1 FWD CARGO DOOR LOWER FWD OUTER SEAL RETAINER DENTED. COMPLIED WITH EC/TC REO 670-52-35-127-01 AND REO 670-52-35-127-01 FOR REPAIR OF NR 1 FWD BAG BAY DOOR.

Part: FITTING — CRACKED (ZONE 100) · airframe 31,245 hrs · 22,261 cycles

ON PANEL 323 BT BONDING STRAP ATTACH POINT BROKEN. FABRICATED CLIP ASSY PER EC/TC EO 900-53-10-0004. AND INSTALLED PER SRM 51-42-06-001-001-A01.

Part: RETAINER — DENTED (CARGO DOOR) · airframe 31,245 hrs · 22,261 cycles

NR 2 FWD CARGO DOOR LOWER FWD OUTER SEAL RETAINER DENTED. COMPLIED WITH EC/TC REO 670-52-35-127-01 AND REO 670-52-35-127-01 FOR REPAIR OF NR 2 FWD BAG BAY DOOR.

Part: FLOOR SUPPORT — CORRODED (BS 349-364) · airframe 23,581 hrs · 15,286 cycles

RIGHT CABIN FLOOR SUPPORT CORRODED BETWEEN BS 349 - 364, RBL 42. COMPLIED WITH REO 690-53-21-897.

Part: STRUCTURE — DAMAGED (ZONE 800) · airframe 23,581 hrs · 15,286 cycles

UPON REMOVAL OF AFT RISER DRAG ANGLE TO ACCOMPLISH MODSUM IS 67052110107 FOUND 2EA. FASTENER HOLES WITH CRACKS. SUBMITTED DAMAGE TO THD AND REPAIRED HOLES BY COMPLYING WITH EC/TC REO 690-52-11-422 AND REO 690-52-11-422.

Part: SKIN — DAMAGED (LT WING) · airframe 23,581 hrs · 15,286 cycles

LT WING LOWER PLANK .450" FASTENER HOLE HAS CRACK INDICATION. STEPPED UP HOLE, COMPLIED WITH NDT, AND REPAIRED HOLE BY COMPLYING WITH EC/TC REO 690-57-21-249 AND REO 690-57-21-249 REV -- DATED 2017-03-16.

Part: HANDLE — CRACKED (PAX DOOR) · airframe 23,581 hrs · 15,286 cycles

ASD INNER ACCESS HANDLE CRACKED. REMOVED AND REPLACED ASD INNER HANDLE PER AMM 52-11-02-00-809 A02, 52-11-02-400-809 A02 P/N- 600-31887-15.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 23,581 hrs · 15,286 cycles

SKIN DAMAGE AT FS 927.00 STR 27. REPAIRED SKIN BY COMPLYING WITH EC/TC REO 670-53-00-290 01 AND REO 670-53-00-290 REV D DATED 09-10-2015.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 23,581 hrs · 15,286 cycles

PAX DOOR AFT DRAG ANGLE CRACKED AT ASSIST MOTOR PULLEY BRACKET. COMPLIED WITH EC/TC REO 670-52-11-072 AND REO 670-52-11-072. REPAIR OF PAX DOOR AFT DRAG ANGLE.

Part: FITTING — CORRODED (FUSELAGE) · airframe 23,581 hrs · 15,286 cycles

DURING REPAIR OF INTERCOSTAL 20R FS 319-349, FOUND CORRODED CLIP AT FS 349.00 STR 20R. REMOVED AND REPLACED CLIP PER SRM 51-40-11-001-001-A01.

Part: FITTING — CORRODED (FUSELAGE) · airframe 23,581 hrs · 15,286 cycles

DURING REPAIR OF INTERCOSTAL 20R FS 319-349, FOUND CORRODED CLIP AT FS 319.70 STR RT. REMOVED AND REPLACED CLIP PER SRM 51-40-11-001-001-A01.

Part: FRAME — CORRODED (FUSELAGE) · airframe 23,581 hrs · 15,286 cycles

FRAME 364 CORRODED AT STR 26R AROUND RIVET HOLE. COMPLIED WITH EC/TC REO 670-53-21-687 01 AND REO 670-53-21-687 01 REPAIR OF FRAME AT 364 STR 26R.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 23,581 hrs · 15,286 cycles

CORRODED INTERCOSTAL AT LBL2 BTW FRAME 349 & 364. REMOVE AND REPLACED INTERCOSTAL ON LBL2 BTW FRAMES 349-364 IAW SRM 51-42-06-001-001-A01 AND 51-40-11-001-001-A01,51-42-21-001-001-A01. P/N SH670-32075-3 AND DRAWING SH670-32075.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 23,581 hrs · 15,286 cycles

CORROSION FOUND ON STR 21R BETWEEN FS 319.00-349.00. REMOVED AND REPLACED STR 21R AT FS 319-349 PER SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01, DRAWING SH670-31630 AND EC/TC REO 690-53-21-900 AND REO 690-53-21-900.

Part: FRAME — CORRODED (FUSELAGE) · airframe 23,581 hrs · 15,286 cycles

FRAME 349.00 CORRODED FWD & AFT SIDES BTW STR 26L-26R. REMOVED AND REPLACED FRAME AT FS 349.00 BETWEEN STR 26R-26L PER SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. DRAWING SH670-31357. P/N SH670-31357-5.

Part: STIFFENER — CRACKED (PAX DOOR) · airframe 23,581 hrs · 15,286 cycles

PAX DOOR MOTOR SUPPORT STIFFENER (LOWER) CRACKED AT LOWER SECTION. REMOVED AND REPLACED LOWER STIFFENER ON PAX. DOOR MOTOR SUPPORT PER SRM 51-42-06-001-001-A01 AND DRAWING 601R31707 P/N 601R317745-7.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 23,581 hrs · 15,286 cycles

STRINGER 26R CORRODED BTW FRAMES 295-319.70. REMOVED AND REPLACED STRINGER 26R FS 280-333 PER SRM 51-42-06-001-001-A01 AND 51-21-11-001-001-A01. P/N SH670-31634-2S. DRAWING SH670-31634.

Part: FRAME — CORRODED (FUSELAGE) · airframe 23,581 hrs · 15,286 cycles

FRAME 310.00 CORRODED FWD SIDE BTW STR 26R-26L. COMPLIED WITH EC/TC REO 670-53-21-799 01 AND REO 670-53-21-799 01.

Part: STRAP — CORRODED (FUSELAGE) · airframe 23,581 hrs · 15,286 cycles

CIRCUMFERENTIAL STRAP INTERNAL SKIN CORRODED BTW STGRS 25R-26L FS 280.00. COMPLIED WITH EA 32-2017-066 AND EC/TC EA 32-2017-066. REPAIR OF STRAP FS 280.00 BTW STR 25R-26L.

Part: FAIRING — CRACKED (ZONE 400) · airframe 23,581 hrs · 15,286 cycles

PANEL 443BB CRACKED. REPAIRED CRACKED PANEL 443BB BY REMOVING CRACKED SECTION OF PANEL, FABRICATING NEW SECTION AND INSTALLING NEW DOUBLER IAW ECTC REO 670-78-33-998 AND REO 670-78-33-998. ALL DEFECTS CORRECTED.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 23,581 hrs · 15,286 cycles

SERVICE DOOR LOWER SILL AREA, (2) EA. ANGLES CORRODED, ANGLES 1 & 3 FWD TO AFT. REMOVED AND REPLACED 2 EA ANGLES AT SERVICE DOOR LOWER SILL AREA ANGLES 1 & 3 FWD TO AFT IAW SRM 51-42-06-001-001-A01.

Part: HOUSING — CORRODED (FLOORBOARD) · airframe 23,581 hrs · 15,286 cycles

FLOORBOARD 232BRF DRAIN HOUSING CORRODED. REMOVED AND REPLACED DRAIN HOUSING ASSY. ON FLOORBOARD 232 BRF I/A/W CRJ 900 AMM 53-00-47-000-802 A02,53-00-47-400-802 A02.

Part: FRAME — CORRODED (BS 319) · airframe 23,581 hrs · 15,286 cycles

FRAME BS 319.7 CORRODED BETWEEN STRINGERS 26R - 26L. REPAIRED IAW EC/TC REO 670-53-21-1308, AND REO 670-53-21-1308.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 23,581 hrs · 15,286 cycles

CABIN FLOORBEAM CORRODED, BS 280, LBL 42. REPAIRED IAW EC/TC REO 670-53-00-390, AND REO 670-53-00-390.

Part: FRAME — CORRODED (BS 333) · airframe 23,581 hrs · 15,286 cycles

FRAME BS 333 CORRODED AFT SIDE BETWEEN STRINGERS 27 - 26L. REPAIRED IAW EC/TC REO 670-53-21-1308, AND REO 670-53-21-1308.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 23,581 hrs · 15,286 cycles

LBL 9 CABIN SEAT RAIL SEGMENT FS 661+32 - 693.00 CORRODED. REMOVED SEAT RAIL IAW AMM 53-00-49-000-801 A07, COMPLIED WITH EC/TC REO 670-53-00-343 AND REO 670-53-00-343 REV M, INSTALLED SEAT RAIL IAW AMM 53-00-49-400-801 A07.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 23,581 hrs · 15,286 cycles

RT SIDE SEAT RAIL AT FS 785-847 IS CORRODED. FABRICATED NEW SEAT RAIL IAW EC/TC REO 670-53-00-343. REMOVED AND REPLACED CORRODED SEAT RAIL IAW AMM 53-00-49-000/400-801-A07.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 23,581 hrs · 15,286 cycles

RBL 9 CABIN SEAT RAIL SEGMENT FS 581.00 - 661+32 CORRODED. REMOVED SEAT RAIL IAW AMM 53-00-49-000-801 A07, COMPLIED WITH EC/TC REO 670-53-00-343 AND REO 670-53-00-343 REV M, INSTALLED SEAT RAIL IAW AMM 53-00-49-400-801 A07.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 23,581 hrs · 15,286 cycles

LBL 9 CABIN SEAT RAIL SEGMENT FS 485.00-581.00 CORRODED. REMOVED SEAT RAIL IAW AMM 53-00-49-000-801 A07, COMPLIED WITH EC/TC REO 670-53-00-343 AND REO 670-53-00-343 REV. M, INSTALLED SEAT RAIL IAW AMM 53-00-49-400-801 A07.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 23,581 hrs · 15,286 cycles

RT CABIN FLOOR SILL CORRODED @ FS 412.00, RBL 42. REMOVED CORROSION IAW SRM 51-12-00-001-001-A01 AND REPAIRED SILL BY COMPLYING WITH EC/TC REO 670-53-00-390 AND REO 670-53-00-390 REV DATED 01-22-2014.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 23,581 hrs · 15,286 cycles

LBL9 CABIN SEAT RAIL SEGMENT FS 485.00-581.00 CORRODED. REMOVED CORROSION IAW SRM 51-12-00-001-001-A01 AND REPAIRED SILL BY COMPLYING WITH EC/TC REO 670-53-00-343 AND REO 670-53-00-343 REV M.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 23,581 hrs · 15,286 cycles

LBL 27 CABIN SEAT RAIL SEGMENT FS 485.00 - 581.00 CORRODED. REMOVED SEAT RAIL IAW AMM 53-00-49-000-801 A07, COMPLIED WITH EEC/TC REO 670-53-00-343 AND REO 670-53-00-343 REV. M, INSTALLED SEAT RAIL IAW AMM 53-00-49-400-801 A07.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 23,581 hrs · 15,286 cycles

LBL9 CABIN SEAT RAIL SEGMENT FS 581.00-661+32 CORRODED. REMOVED CORROSION IAW SRM 51-12-00-001-001-A01 AND REPAIRED SILL BY COMPLYING WITH EC/TC REO 670-53-00-343 AND REO 670-53-00-343 REV M.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 23,581 hrs · 15,286 cycles

FLOOR PANEL 221 ALF AFT SUPPORT ANGLE CORRODED. REMOVED CORRODED ANGLE AND INSTALLED NEW ANGLE IAW SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01, 51-40-11-001-001-A01 AND 51-21-11-001-001-A01.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 23,581 hrs · 15,286 cycles

LBL9 CABIN SEAT RAIL SEGMENT FS 374.00-485.00 CORRODED. REMOVED CORROSION IAW SRM 51-12-00-001-001-A01 AND REPAIRED SILL BY COMPLYING WITH EC/TC REO 670-53-00-343 AND REO 670-53-00-343 REV M.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 23,581 hrs · 15,286 cycles

LBL9 CABIN SEAT RAIL SEGMENT FS 374.00-485.00 CORRODED. REMOVED CORROSION IAW SRM 51-12-00-001-001-A01 AND REPAIRED SILL BY COMPLYING WITH EC/TC REO 670-53-00-343 AND REO 670-53-00-343 REV M.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 23,581 hrs · 15,286 cycles

LBL9 CABIN SEAT RAIL SEGMENT FS 581.00-661+32 CORRODED. REMOVED CORROSION IAW SRM 51-12-00-001-001-A01 AND REPAIRED SILL BY COMPLYING WITH EC/TC REO 670-53-00-343 AND REO 670-53-00-343 REV M.

Part: STRUCTURE — CORRODED (BS 310) · airframe 23,581 hrs · 15,286 cycles

CORRODED PACKER AT BS 310, LBL 10. REMOVED CORRODED PACKER AND INSTALLED NEW PACKER IAW SRM 51-42-06-001-001-A01.

Part: SEAT TRACK — CRACKED (BS 785-847) · airframe 23,581 hrs · 15,286 cycles

LEFT SIDE SEAT TRACK AT BS 785-847 IS CORRODED. FABRICATED A NEW SEAT TRACK IAW EC/TC REO 670-53-00-343. REMOVED AND REPLACED CORRODED SEAT RAIL IAW AMM 53-00-49-000, & 400-801-A07.

Part: FLOOR SUPPORT — CORRODED (BS 977-1098) · airframe 23,581 hrs · 15,286 cycles

FLOOR SUPPORT CORRODED FROM BS 977 - 1098. BLENDED CORROSION IAW REO 670-53-00-390 AND EC/TC REO 670-53-00-390.

Part: FLOOR SUPPORT — CORRODED (BS 985-1088) · airframe 23,581 hrs · 15,286 cycles

LEFT FLOOR SUPPORT CORRODED BETWEEN BS 985-1088. BLENDED CORROSION ON RT FLOOR SUPPORT IAW SRM 51-21-06-001-001-A01, REO 670-53-00-390 AND EC/TC REO 670-53-00-390. RESTORED FINISH IAW SRM 51-21-16.

Part: BATTERY — DISCHARGED (CABIN) · airframe 23,012 hrs · 14,884 cycles

MULTIPLE EMERGENCY LIGHT INOP AT LT OVER-WING HATCH. ALLOWED BATTERY TO CHARGE FOR EMERGENCY LIGHTS. PERFORMED OPERATIONAL CHECK OF EMERGENCY LIGHTS IAW AMM 33-51-00. OPS CHECKED GOOD.

Part: MEGAPHONE — DAMAGED (CABIN) · airframe 22,218 hrs · 14,339 cycles

MEGAPHONE BATTERY HOLDER MELTED. REMOVED AND REPLACED THE MEGAPHONE IAW AMM 25-61-14. REF IPC 25-61-14, FIG 1, ITEM 5.

Part: UNKNOWN — SMOKE (CABIN) · airframe 21,237 hrs · 13,644 cycles

PASSING 800" AGL AFTER TAKEOFF THE AFT LAV SMOKE WARNING WENT OFF. THERE WAS SMOKE IN THE CABIN. F/A SAID SMOKE SEEMED TO EMINATE FROM MID CABIN. MADE EMERGENCY LANDING. C/W FIM 21-22-00-810-806, NO DEFECTS NOTED.

Part: MEGAPHONE — NOT REPORTED (CABIN) · airframe 21,054 hrs · 13,509 cycles

MEGAPHONE TO BE REPLACED TO C/W TC EO 700-25-0166. R & R MEGAPHONE IAW AMM 25-61-14. AIPC REF 25-61-14, FIG. 1, ITEM 5.

Part: SPRING — SEPARATED (PAX DOOR) · airframe 20,886 hrs · 13,396 cycles

PAX DOOR WILL NOT OPEN. FOUND SPRING ROD ASSY SEPARATED. INSTALLED SPRING ROD ASSY WITH NEW SAFETY TAB IAW AMM 52-11-02. ALL CHECKS GOOD AT THIS TIME.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 20,696 hrs · 13,261 cycles

EMERGENCY LIGHTS WILL NOT ILLUMINATED FOR MORE THAN A FEW SECONDS. CHARGED EMERGENCY LIGHTS IAW AMM 33-51-00, OPS CK GOOD.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 20,532 hrs · 13,160 cycles

RIGHT OVERWING EMERGENCY LIGHT ASSY LENS CRACKED. R & R RT OVERWING EMERGENCY LIGHT ASSY LENS IAW AMM 33-51-15.

Part: MEGAPHONE — CREW ERROR · airframe 18,681 hrs · 11,877 cycles

F/A REPORTS THAT MEGAPHONE IS INOPERATIVE. FOUND VOLUME TURNED DOWN ON MEGAPHONE. OPS CHECK GOOD IAW AMM 25-61-00.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 18,123 hrs · 11,502 cycles

EMERGENCY LIGHTS WILL NOT COME ON WHEN SWITCH SELECTED ON COCKPIT AND F/A. APPLIED POWER TO EMERGENCY BATTERY PACKS TO CHARGE. OPS CK GOOD IAW AMM 33-51-15.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 17,710 hrs · 11,229 cycles

EMERGENCY LIGHTS INOPERATIVE. R & R BATTERY PACK ASSY IN CABIN IAW AMM 33-51-17. COMPLIED WITH OPS CHECK GOOD AND AV COMPARTMENT BATTERY PACK FOR EMERGENCY LIGHTS R & R.

Part: BRACKET — CRACKED (PAX DOOR) · airframe 17,682 hrs · 11,215 cycles

DURING COMPLETION OF SB 670BA-52-033 DISCOVERED BRACKED CRACKED. R & R BRACKET IAW DWG CC 670-38625 & SRM 51-42-10-001-001-A01.

Part: STRINGER — CORRODED (BS 333-364) · airframe 17,682 hrs · 11,215 cycles

CORROSION DAMAGE ON STRINGER 26R FROM BS 333- 364. FOUND TO BE OUT OF LIMITS IAW SRM 53-21-23-101-003-A01. REMOVED THE STRINGER IAW SRM 51-42-06-001-001-A01.

Part: HOUSING — OUT OF LIMITS (RUDDER) · airframe 17,682 hrs · 11,215 cycles

LOWER CENTER RUDDER BEARING HOUSING BORE DIAMETER OUT OF LIMITS IAW DWG AV670-21140. REMOVED LOWER CENTER RUDDER HINGE FITTING AND RECEIVED SERVICEABLE HINGE FITTING, LOCATED AND TRANSFERED DRILLED MOUNT HOLES REF RIL 2103 AND SRM 51-40-11-001-001-A01.

Part: ANGLE — DAMAGED (BS 280) · airframe 17,681 hrs · 11,214 cycles

FOUND ELONGATED HOLE AT ANGLE LOCATED AT LT SIDE BULKHEAD L26.00, FS 280.00. REMOVED AND REPLACED THE ANGLE IAW SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01, AND SRM 51-42-06-001-001-A01.

Part: FLOOR PANEL — CRACKED (BS 193) · airframe 17,681 hrs · 11,214 cycles

FLOOR PANEL CRACKED BS 193. REPAIRED IAW GREO 670-53-11-509 REV B.

Part: LONGERON — CORRODED (BS 333-364) · airframe 17,682 hrs · 11,215 cycles

LONGERON 25R, FS 333- FS 364 HAS DEEP PITTING AROUND FASTENER HOLE. BLENDED DAMAGE FOUND TO BE OUT OF LIMITS REF SRM 53-21-23-101-003-A01. STARTED REMOVING FASTENERS COMMON TO LONGERON 25R & FUSELAGE SKIN REF SRM 51-42-06-001-001-A01. FINISHED REMOVING FASTENERS FROM LONGERON 25R REF SRM 51-42-06-001-001-A01. REMOVED DOUBLER FOR WATER DRAIN MAST TO FOM LONGERON 25R REMOVAL REF SRM 51-42-06-001-001. INSTALLED ALL FASTENERS COMMON TO DOUBLER AND SKIN PANEL ONLY REF SRM 51-42-06-001-001-A01 AND GWG SH 670-31350. REMOVED LONGERON 25R IAW SRM 51-42-06-001-001-A01.

Part: DOOR SILL — CORRODED (E/E BAY DOOR) · airframe 17,681 hrs · 11,214 cycles

CORROSION FOUND ON AVIONICS DOOR SILL INNER SURFACE BETWEEN 364.00-394.00 BETWEEN STR 25L-25R. COMPLIED WITH GREO 690-53-21-032, STEP 1, FIG 1, REV-03-07-2008. RECEIVED AND COMPLIED WITH EC/TC REO 690-53-21-032. REPAIR TO THE SURFACE DAMAGE ON THE SKIN INNER SURFACE, DWG SH69-31351, REV AT THE AVIONICS BAY DOOR CUTOUT BETWEEN FS 364 AND FS 394 AND BETWEEN STR 26L AND STR 25 COMPLETED IAW REO 690-53-21-032. COMPLIED WITH MODSUM IS6905321009 IAW CUSTOMER REQUEST 01-06-COMPLETED. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SOP 5702.

Part: SEAT TRACK — CORRODED (BS 485-553) · airframe 17,681 hrs · 11,214 cycles

RBL 9, SEAT TRACK BS 485 - 553 CORRODED. FOUND TO BE OUT OF LIMITS IAW GREO 670-53-00-013. R & R THE SEAT TRACK IAW AMM 53-00-49-000-801-A07 AND 53-00-49-400-801 A07.

Part: SEAT TRACK — CORRODED (BS 743-763) · airframe 17,659 hrs · 11,201 cycles

SEAT TRACK CORRODED BS 743 - 763. FOUND TO BE OUT OF LIMITS IAW GREO 53-00-013. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801-A07, SRM 51-40-11-001-001-A01 AND GREO 670-53-00-343, REV G.

Part: SEAT TRACK — CORRODED (BS 743-763) · airframe 17,681 hrs · 11,214 cycles

SEAT TRACK CORRODED BS 743 - 763. FOUND TO BE OUT OF LIMITS IAW GREO 670-53-00-013. REMOVED AND REPLACED THE SEAT TRACK IAW AMM TASK 53-00-49-000-801, SRM 51-40-11-001-001-A01 AND GREO 670-53-00-343, REV G.

Part: SEAT TRACK — CORRODED (BS 926-977) · airframe 17,681 hrs · 11,214 cycles

SEAT TRACK CORRODED AT MULTIPLE AREAS FROM BS 926- 977. . FOUND TO BE OUT OF LIMITS IAW GREO 670-53-00-013. R & R THE SEAT TRACK IAW AMM 53-00-49-000-801-A07 AND 53-00-49-400801 A07.

Part: SEAT TRACK — CORRODED · airframe 17,681 hrs · 11,214 cycles

SEAT TRACK CORRODED BS 784 - 847. FOUND TO BE OUT OF LIMITS IAW GREO 670-53-00-013. R & R THE SEAL TRACK IAW AMM 53-00-49-000-801.

Part: SEAT TRACK — CORRODED (BS 581-661) · airframe 17,681 hrs · 11,214 cycles

RBL 9 SEAT TRACK BS 581- 661 CORRODED. DAMAGE FOUND TO BE OUT OF LIMITS IAW GREO 670-53-00-013. R & R THE SEAT TRACK IAW AMM 53-00-49-000-801-A07 AND AMM 53-00-49-400-801 A07.

Part: SEAT TRACK — CORRODED (BS 672-722) · airframe 17,659 hrs · 11,201 cycles

SEAT TRACK CORRODED BS 672 - 722. FOUND TO BE OUT OF LIMITS IAW GREO 670-53-00-013. REMOVED AND INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-000-801-A07 AND 53-00-49-400-801-A07.

Part: SEAT TRACK — CORRODED (BS 784-847) · airframe 17,659 hrs · 11,201 cycles

SEAT TRACK CORRODED BS 784 - 847, FOUND TO BE OUT OF LIMITS IAW GREO 670-53-00-013. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801-A07, SRM 51-40-11-001-001-A01 AND GREO 670-53-00-343.

Part: FLOOR SUPPORT — CORRODED (BS 1000-1047) · airframe 17,659 hrs · 11,201 cycles

CORROSION FLOOR SUPPORT BS 1000 - 1047 LBL 45. REPAIRED IAW GREO 670-53-61-913 IAW REO 670-53-61-913.

Part: SEAT TRACK — CORRODED (BS 672-722) · airframe 17,681 hrs · 11,214 cycles

SEAT TRACK CORRODED AT MULTIPLE AREAS FROM BS 672 - 722. FOUND TO BE OUT OF LIMITS IAW GREO 670-53-00-013. R & R THE SEAT TRACK IAW AMM 53-00-49-000-801-A07 AND 53-00-49-400-801 A07.

Part: SEAT TRACK — CORRODED (BS 581-661) · airframe 17,681 hrs · 11,214 cycles

LBL 9, SEAT TRACK BS 581 - 661 CORRODED. FOUND TO BE OUT OF LIMITS IAW GREO 670-53-00-013. REMOVED AND REPLCED THE SEAT TRACK IAW AMM 53-00-49-000-801-A07 AND 53-00-49-400-801-A07.

Part: FLOOR SUPPORT — CRACKED (BS 260-280) · airframe 17,659 hrs · 11,201 cycles

FLOOR SUPPORT ANGLE CRACKED BETWEEN BS 260 - 280 LBL 9.0. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-44-06-001-001-A01, 51-42-06-001-001-A01, 51-40-11-001-001-A01 AND SRM 51-21-16-001-001-A01.

Part: FLOOR SUPPORT — CRACKED (BS 260-280) · airframe 17,659 hrs · 11,201 cycles

FLOOR SUPPORT ANGLE CRACKED BETWEEN BS 260 - 280 RBL 9. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-46-06-001-001-A01. AND REO 690-53-11-710, REV A.

Part: BULKHEAD WEB — CORRODED (BS 280) · airframe 17,659 hrs · 11,201 cycles

LEFT BS 280 LOWER WEB CORRODED. FOUND TO BE OUT OF LIMITS IAW SRM 11-10-201-003-A01, FIG 53-11-10-99 804. REPAIRED IAW REO 670-53-11-594 AND GREO 670-53-11-594, REV.

Part: BULKHEAD WEB — CORRODED (BS 280) · airframe 17,659 hrs · 11,201 cycles

RT FS 280.00 LOWER WEB CORRODED. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SOP 5702. CORROSION ON RT FS 280.00 LOWER WEB EXCEEDS THE ALLOWABLE LIMITS OF SRM 53-11-10-201-003-A01, FIG 53-11-10-991-804. COMPLIED WITH EC/TC REO 670-53-11-594 01 AND GREO 670-53-11-594 REV.

Part: ANGLE — CRACKED (BS 280 ANGLE) · airframe 17,659 hrs · 11,201 cycles

BS 280 BULKHEAD ANGLE IS CRACKED ON RT SIDE BL 26.00. REMOVED AND OBTAINED NEW ANGLE LOCATED, DRILL HOLES AS REQUIRED, DEBUR HOLES IAW SRM 51-40-11-001-001-A01 51-42-06-001-001-A01 AND DWG CC670-34010. INSTALLED RT SIDE ANGLE AT BL26.00, FS280 BULKHEAD IAW SRM 51-42-06-001-001-A01 AND DWG CC670-34010. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SOP 5702.

Part: FLOORBEAM — CRACKED · airframe 17,659 hrs · 11,201 cycles

COCKPIT FLOORBEAM IS CRACKED. FABRICATED REPAIR ANGLES IAW REO 690-53-11-710, REPAIRED IAW REO 690-53-11-710.

Part: SKIN — CHAFED (BS 935) · airframe 17,659 hrs · 11,201 cycles

CHAFE ON FUSELAGE AT BS 935, BL 0 LONGITUDINAL CHAFE. BLENDED CHAFED AREA IAW SRM 51-12-00-001-001-A01. REPAIRED DAMAGED AREA IAW REO 670-53-00-290, REV C.

Part: INTERCOSTAL — CORRODED (BS 349-364) · airframe 17,659 hrs · 11,201 cycles

INTERCOSTAL BS 349-364, STR 27R HAS CORROSION DAMAGE. CORROSION DAMAGE ON RT INTERCOSTAL FS 349.0 - 364.0 STR27 EXCEEDS THE ALLOWABLE DAMAGE LIMITS OF SRM 53-21-23-101-003-A01, FIG 53-21-23-99-808. R & R INTERCOSTAL REF SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01 AND DWG SH670-32050. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SOP 5702.

Part: SKIN — CHAFED (PAX DOOR) · airframe 17,659 hrs · 11,201 cycles

PAX DOOR FWD UPPER CORNER EXTERNAL SKIN CHAFED. BLENDED AREA IAW SRM 51-12-00-001-001-A01. PERFORMED THICKNESS INSPECTION OF OUTER SKIN IAW BSC NDT PROGRAM MANUAL SEC 4.3 MIN REMAINING THICKNESS IS .103", ORIGINAL IS .108", REMOVED IS .005" NO DAMAGE ALLOWED WITHIN 15+ PF ANY FASTENER LINE IAW SRM 52-00-01-101-001-A01. COMPLIED WITH STS EA 32-2014 031, SECTION 1 PERMANENT REPAIR STEPS 1A THROUGH STEP 1D.

Part: STRAP — CORRODED (BS 280) · airframe 17,656 hrs · 11,200 cycles

CORROSION DAMAGE ON FS 280 BUTT STRAP, STR 25LT-25RT. NO DAMAGE ALLOWED IAW SRM 53-21-01-101-002-A02. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SOP 5702. REMOVED RIVETS AT FS 280 BUTT STAP FROM STR 26LT-25RT & BLENDED CORROSION AS REQUIRED REF SRM 51-42-06-001-001 & SRM 51-21-06-001-001. PERFORMED EDDY CURRENT INSPECTION OF FS 280.00 BUTT STRAP IAW NDTM PT.1, 51-20-006-250-801 NO INDICATIONS NOTED AT THIS TIME.

Part: STRIKER — CORRODED (SERVICE DOOR) · airframe 17,649 hrs · 11,196 cycles

SERVICE DOOR LOWER SEAL STRIKER CORRODED AT FWD AND AFT SCREW HOLES. BLENDED DAMAGE IAW SRM 51-12-00-001-001-A01, SP 162207. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00-101-001-A01. REMOVED STRIKER FROM LOWER SERVICE DOOR IAW SRM 51-42-06-001-001-A01. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SOP 5702. INSTALLED SEAL STRIKER FITTING AT SERVICE DOOR IAW SRM 51-42-06-001-001-A01 AND DWG SH670-31412.

Part: STRINGER — CORRODED (BS 319-338) · airframe 17,656 hrs · 11,200 cycles

CORROSION ON STRINGER 25RT, FS 319.70-FS 338.0. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SOP 5702. BLENDED CORROSION FS 319.70-FS 333 REF SRM 51-21-06-001-001-A01. REMOVED SPLICE AT FS 333, STR 25R DUE TO PREVIOUSLY BLENDED OUT OF LIMITS REF SRM 51-42-06-001-001-A01. RECEIVED NEW SPLICE & PICKED UP FASTENER HOLES AT STR 25R & FS 333 REF SRM 51-40-11-001-001 & DWG SH670-32429. REMOVED FRAME TO STRINGER ATTACH CLIP AT STR 25R & FS 333. INSTALLED STRINGER ATTACH CLIPS ON STR 25R AT STA 333, 319,310 AND 295 IAW SRM 51-42-06-001-001-A01.

Part: ANGLE — CORRODED (PAX DOOR) · airframe 17,646 hrs · 11,192 cycles

PAX DOOR ANGLE KICKPLATE CORRODED. REMOVED KICKPLATE ANGLE IAW SRM 51-42-06-001-001-A01. LOCATED DRILLED DEBURRED FASTENER HOLES IAW SRM 51-42-06-001-001-A01. INSTALLED NUTPLATES ON PAX DOOR ANGLE KICKPLATE IN REF TO SRM 51-45-00-001-001-A01. COMPLETED KICK PLATE INSTALLATION IAW SRM TASK 51-42-06-001-001-A01, 51-42-21-001-001-A01.

Part: SEAT TRACK — CORRODED (BS 374-485) · airframe 17,659 hrs · 11,201 cycles

SEAT TRACK AT LBL 9, BS 374 - 485 CORRODED. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801 AND AMM 53-00-49-400-801.

Part: ANGLE — CORRODED (SERVICE DOOR) · airframe 17,649 hrs · 11,196 cycles

SERVICE DOOR ANGLE MOUNT CORRODED. REMOVED MOUNTING ANGLE AND LOWER SILL ANGLE IAW SRM 51-42-06-001-001-A01. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SOP 5702. ASSEMBLED NEW MOUNTING ANGLE AND EXISTING LOWER SILL ANGLE IAW SRM 51-42-06-001-001-A01 AND DWG SH670-31996. INSTALLED MOUNTING ANGLE AND SILL ANDLE ASSY AT SERVICE DOOR IAW SRM 51-42-06-001-001-A01 AND DWG SH670-31996.

Part: FRAME — CORRODED (BS 333) · airframe 17,656 hrs · 11,200 cycles

CORROSION DAMAGE ON BS 333, FRAME AFT SIDE, STR 26L-26R. BLENDED CORROSION IAW SRM 51-12-00-001-001-A01. PERFORMED UT THICKNESS INSPECTION OF FS 333, FRAME IAW BSC NDT PROGRAM MANUAL SEC. 4.3. MIN, REMAINING THICKNESS IS .049", ORIGINAL IS .050", REMOVED IS .001", NO DAMAGE ALLOWED IN BLEND AREAS IAW SRM 53-21-06-101-002-A02.

Part: FRAME — CORRODED (BS 295) · airframe 17,656 hrs · 11,200 cycles

CORROSION DAMAGE ON FS 295.00 FRAME AFT SIDE, STR 26L-26R. BLENDED CORROSION IAW SRM 51-12-00-001-001-A01. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SOP 5702. AFTER FURTHER EVALUATION SEVERE CORROSION WAS FOUND WITH 100 PERCENT MATERIAL LOSS FRAME REPAIR IS REQUIRED. REPAIRED FRAME STN 295 IAW REO 670-53-21-799 BY COMPLYING WITH EC/TC REO 670-53-21-799. REMOVE DAMAGED AREA OF FS 295.00 IAW GREO 670-53-21-799. REMOVED FASTENERS THROUGH THE SKIN FROM STRINGER 25LT TO 25RT ON FS 295 IN REF TO GREO 670-53-21-799.

Part: HINGE — GOUGED (PAX DOOR) · airframe 17,659 hrs · 11,201 cycles

PAX DOOR FUSELAGE HINGE AFT LUG LANDING GROOVED BY RETAINING PIN. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SOP 5702. BLENDED DAMAGE IAW SRM 53-21-23-101-001-A01, SRM CTJ900 51-12-00-001-001-A01, TEMP REV 51-0050. COMPLIED WITH GREO 670-53-21-582, REPAIR TYPE IV STEPS 1-3, DATED 2013-03-06, REV B.

Part: SEAT TRACK — CORRODED (BS 364-485) · airframe 17,659 hrs · 11,201 cycles

SEAT TRACK AT LBL 27, BS 364 - 485 CORRODED. R & R THE SEAT TRACK IAW AMM 53-00-49-000-801-A07 AND 53-00-49-400-801-A07.

Part: SEAT TRACK — CORRODED (BS 364-485) · airframe 17,659 hrs · 11,201 cycles

SEAT TRACK AT RBL 9, BS 364 - 485 CORRODED. R & R SEAT TRACK IAW AMM 53-00-49-00-801-A01 AND 53-00-49-400-801-A04.

Part: HAND RAIL — CHAFED (PAX DOOR) · airframe 17,659 hrs · 11,201 cycles

PAX DOOR AFT HAND RAIL CHAFED BY WHEEL STRUT. BLENDED SMOOTH IAW SRM 51-12-00-001-001-A01. COMPLIED WITH STS EA37-2014-050, SECTION 1, PERMANENT REPAIR STEPS 1A THROUGH 1D.

Part: FLOOR SUPPORT — CORRODED (BS 285) · airframe 17,659 hrs · 11,201 cycles

RT SIDE FLOOR SUPPORT AT FS285 CORRODED. BLENDED CORROSION AND FOUND BEYOND LIMITS IAW SRM 53-00-00-101-001-A01. REPAIRED IAW SRM 53-21-43-201-002-A01. MAJOR REPAIR.

Part: ANGLE — CORRODED (SERVICE DOOR) · airframe 17,656 hrs · 11,200 cycles

ALL 4 ANGLE CLIPS ON THE PROTECTOR CORRODED AT SERVICE DOOR. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SOP 5702. REMOVED 4 WEB FLOOR PROTECTORS IAW SRM 51-42-06-001-001-A01 UPON REMOVAL, FOUND CORRODED AND DETERMINED OUT OF LIMIT IAW SRM 53-21-23-101-002-A01. INSTALLED 4 WEB FLOOR PROTECTORS IAW SRM 51-42-06-001-001-A01 AND DWG SH670-32040 INSTALLED FWD & AFT MOUNTING ANGLES IAW SRM 51-42-06-001-001-A01 AND DWG SH670-31982. INSTALLED, 2 EA, REMAINING ANGLE CLIPS AT FWD AND AFT MID POSITIONS IAW SRM 51-42-06-001-001-A01.

Part: INTERCOSTAL — CORRODED (BS 349-364) · airframe 17,659 hrs · 11,201 cycles

INTERCOSTAL BS 349-364, STR 27L HAS CORROSION DAMAMGE. CORROSION DAMAGE ON LT INTERCOSTAL FS 349.0-FS 364.0, STR27 EXCEEDS THE ALLOWABLE DAMAGE LIMITS OF SRM 53-21-23-101-003-A01, FIG 53-21-23-991-808. R & R INTERCOSTAL REF SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01 AND DWG SH670-32050. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SOP 5702.

Part: ANGLE — CORRODED (PAX DOOR) · airframe 17,649 hrs · 11,196 cycles

PAX DOOR MID CAP ANGLE CORRODED. REMOVED CAP ANGLE IAW 51-41-02-001-001-A01. LOCATED & DRILLED NEW PART IAW SRM 51-42-06-001-001-A01, 51-42-15-001-001-A01, & 51-45-00-001-001-A01. INSTALLED MID CAP ANGLE IAW SRM TASK 51-41-02-001-001-A01.

Part: SKIN — GOUGED (BS 1144-1162) · airframe 17,649 hrs · 11,196 cycles

INNER FUSELAGE SKIN GOUGED BS 1144-1162, STR 6-7R. BLENDED DAMAGE IAW SRM TR 51-0050. AREA IS OUT OF ALLOWABLE LIMITS IAW SRM 53-61-01-101-001-A02. REPAIRED IAW EA 12-2014-268 P1. MAJOR REPAIR.

Part: HANDLE — LACK OF LUBE (EMERGENCY EXIT) · airframe 17,646 hrs · 11,192 cycles

LEFT AFT EMERGENCY EXIT DOOR HANDLE DOES NOT OPERATE FREELY. VISUAL INSPECTED HARDWARE NO DEFECTS. LUBED LT AFT EMERGENCY EXIT DOOR OPEN HANDLE IAW AMM 12-20-52-640-816, A01. HANDLE OPERATIONS FREELY.

Part: HANDLE — LACK OF LUBE (EMERGENCY EXIT) · airframe 17,646 hrs · 11,192 cycles

LT FWD EMERGENCY EXIT DOOR HANDLE DOES NOT OPERATE FREELY. LUBRICATED THE HANDLE IAW AMM 12-20-52-640-815, A01, HANDLE OPERATES FREELY.

Part: CROSSBEAM — CORRODED · airframe 17,646 hrs · 11,192 cycles

CROSSBEAM CORRODED. REPLACED THE CROSSBEAM IAW SB670BA-53-041.

Part: STRINGER — CRACKED (BS 1144-1162) · airframe 17,646 hrs · 11,192 cycles

STRINGER 7R CRACKED BETWEEN BS 1144 - 1162. PERFORMED EDDY CURRENT INSPECTION OF STR 7R CUTOUT IAW NDTM PT. 1, 51-20-006-250-A01 NO INDICATIONS NOTED AT THIS TIME. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SOP 5702. COMPLIED WITH GREO 670-53-61-292, REV C DATED. REPAIR ANGLE 670-53-61-292-1, FABRICATED FROM 2024-T3.050 ALUM SHT P.O M12115.

Part: LINK — OUT OF TOLERANCE (LEFT) · airframe 17,682 hrs · 11,215 cycles

FOUND LT REAR SPAR LINK TILTED AND TOUCHING FUSELAGE FRAME AND WING FITTING. COMPLIED WITH SB 670BA-57-016 01, PART "B" REMOVED AND INSTALLED NEW SERVICEABLE LEFT SIDE REAR LINK ASSEMBLY IAW SB 670BA-57-016 01. THIS REPAIR IS CLASSIFED AS A MAJOR REPAIR IAW SOP 5702.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 16,869 hrs · 10,657 cycles

PAX DOOR AFT DRAG ANGLE CRACKED AT MOTOR ASSIST CABLE PULLEY BRACKET. R & R DRAG ANGLE IAW SRM 52-11-04.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 16,859 hrs · 10,651 cycles

DRAG ANGLE ON AFT SIDE OF PAX DOOR IS CRACKED THROUGH VERTICAL LEG. R & R PREVIOUS REPAIR SECTION OF PAX DOOR AFT DRAG ANGLE AT PULLEY ASSIST BRACKET IAW SRM 52-11-04.

Part: LIGHT — INOPERATIVE (LT OVERWING) · airframe 15,700 hrs · 9,894 cycles

LEFT EXTERIOR EMERGENCY AFT MIDDLE LIGHT INOPERATIVE. R & R LT OVERWING EXIT LIGHT ASSY IAW AMM 33-51-15. OPS CHECKED GOOD, ACFT OK FOR RETURN TO SERVICE.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 15,283 hrs · 9,639 cycles

RT FWD EXT EMERGENCY LIGHT OUT AFT SERVICE DOOR. R & R EMERGENCY BATTERY POS NR 2 IAW 33-51-17 AND IPC 33-51-17, FIG 1, ITEM 6. OPS CHECKED GOOD.

Part: RETAINER — DAMAGED (CARGO DOOR) · airframe 15,107 hrs · 9,526 cycles

FWD CARGO DOOR SEAL RETAINER ON LOWER SIDE DENTED AND CHAFED. REPAIRED IAW REO 670-52-35-127, REV B. MAJOR REPAIR IAW GMM 5-3.

Part: RETAINER — DAMAGED (CARGO DOOR) · airframe 15,107 hrs · 9,526 cycles

MID CARGO DOOR SEAL RETAINER ON LOWER CORNERS CHAFED AND DENTED. REPAIRED IAW REO 670-52-35-127, REV B. MAJOR REPAIR IAW GMM 5-3.

Part: BRACKET — CRACKED (PAX DOOR) · airframe 15,107 hrs · 9,526 cycles

PAX DOOR AFT ANGLE BRACKET CRACKED MID WAY DOWN. REPAIRED IAW REO 670-52-11-287.

Part: BRACKET — CRACKED (PAX DOOR) · airframe 15,107 hrs · 9,526 cycles

PAX DOOR AFT ANGLE BRACKET CRACKED MID WAY DOWN.

Part: BRACKET — CRACKED (PAX DOOR) · airframe 15,107 hrs · 9,526 cycles

PAX DOOR AFT ANGLE BRACKET CRACKED MID WAY DOWN.

Part: BULKHEAD — DAMAGED (BS 169) · airframe 14,886 hrs · 9,391 cycles

FS 169, BULKHEAD DAMAGED. REMOVED BULKHEAD IAW SRM 51-42-06 AND SRM 51-42-13, AND SRM 51-42-21. INSTALLED NEW BULKHEAD IAW SRM 51-42-06 AND IAW DWG CC670-34090 AND DWG CC670-34204, CC670-33001 ,CC670-33030, CC670-33040, CC670-33045, CC670-34090.

Part: FLOORBEAM — CRACKED (COCKPIT) · airframe 14,743 hrs · 9,303 cycles

COCKPIT FLOORBEAM, BL 12L CRACKED. REPAIRED IAW REO 690-53-11-561 AND SRM 51-21-11,51-25-16,51-42-06,51-42-21 AND ISE STR-12-004, REV NC.

Part: CLAMP — LOOSE (BLEED SYS) · airframe 13,344 hrs · 8,424 cycles

ICE CAUTION IN NONE ICING CONDITIONS, LT WING DUCT OVERHEAT MASTER WARNING MESSAGE, LOST PRESSURE. OXYGEN MASK DEPLOYED, DECLARED EMERGENCY. FOUND TWO LOOSE V-BAND CLAMPS LOOSE. TORQUED BOTH IAW AMM 20-30-00. OPS CHECKED GOOD ON GROUND RUNS ACFT OK FOR SERVICE.

Part: WINDOW — CRACKED (COCKPIT) · airframe 11,926 hrs · 7,453 cycles

ON CLIMBOUT FROM ROC TO JFK CAPTAINS SIDE WINDOW INNER PLY CRACKED. EMERGENCY DECLARED, A/C DIVERTED BACK TO ROC LANDED SAFELY. REMOVED AND REPLACED CAPTAINS SIDE WINDOW.

Part: WARNING SYSTEM — FALSE ACTIVATION (BLEED AIR SYS) · airframe 9,700 hrs · 5,992 cycles

ON CLIMBOUT FROM DFW RECEIVED BLEED AIR DUCT WARNING MSG. A/C DEPRESSURIZED, EMERGENCY DECLARED. A/C RETURNED TO DFW LANDED SAFELY. INTEROGATED MDC FOUND LOOP MT 227 FLAGGED. INSPECTED LOOP MT 227 AND SURROUNDING LOOPS, NO DEFECTS NOTED. PERFORMED ANTI-ICE LEAK TEST AND BLEED AIR SYSTEM LEAK TEST. NO DEFECTS NOTED.

Part: SKIN — DENTED (FUSELAGE) · airframe 9,633 hrs · 5,957 cycles

DENT IN FUSELAGE ABOVE EMERGENCY LIGHT JUST AFT OF PAX DOOR. REMOVED DAMAGED AREA AND INSTALLED REPAIR DOUBLER OVER AREA IAW REO 690-53-21-214.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 3 · airframe 9,633 hrs · 5,957 cycles

FS 280 FLOOR SUPPORT (CAMLOC ANGLE) CORRODED. REMOVED AND REPLACED FLOOR SUPPORT (CAMLOC ANGLE) IAW SRM 51-42-06.

Part: BULKHEAD — CORRODED (FUSELAGE) · corrosion level 3 · airframe 9,618 hrs · 5,942 cycles

RIGHT 280.00 BULKHEAD IS CORRODED. REMOVED AND REPLACED RIGHT FS 280.00 LOWER BULKHEAD (CC670-34170-6) AS PER SRM 53-11-10 REPAIR "B".

Part: CROSSBEAM — CORRODED (FUSELAGE) · corrosion level 3 · airframe 9,633 hrs · 5,957 cycles

RIGHT CROSSBEAM AT FS 280 CORRODED. REMOVED AND REPLACED CROSSBEAM IAW DWG CC670-34010 REV A, SRM 51-42-06, SRM 51-42-13, AND SRM 51-42-22.

Part: POST — CORRODED (COCKPIT ENTRY) · corrosion level 3 · airframe 9,618 hrs · 5,942 cycles

CORROSION FOUND ON RIGHT COCKPIT ENTRY POST AT FS 280.00 AT FLOOR LEVEL. REPAIRED CORROSION AT FS 280.00 AS PER BOMBARDIER REO 690-53-11-311.

Part: BULKHEAD — CORRODED (FUSELAGE) · corrosion level 3 · airframe 9,618 hrs · 5,942 cycles

LEFT 280.00 BULKHEAD IS CORRODED. REMOVED AND REPLACED LEFT FS 280.00 LOWER BULKHEAD (CC670-34170-3) AS PER SRM 53-11-10 REPAIR "B".

Part: CROSSBEAM — CORRODED (FUSELAGE) · corrosion level 3 · airframe 9,633 hrs · 5,957 cycles

LEFT CROSSBEAM AT FS 280 CORRODED. REMOVED AND REPLACED CROSSBEAM IAW DWG CC670-34010 REV A, SRM 51-42-06, SRM 51-42-13, AND SRM 51-42-22.

Part: POST — CORRODED (FUSELAGE) · corrosion level 3 · airframe 9,618 hrs · 5,942 cycles

CORROSION FOUND ON LEFT COCKPIT ENTRY POST AT FS 280 AT FLOOR LEVEL. CUT AWAY CORRODED AREA OF DOOR POST, FABRICATED FILLER AND DOUBLER AND INSTALLED IAW REO 690-53-11-311.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,618 hrs · 5,942 cycles

FLOOR SILL DIRECTLY BEHIND SERVICE DOOR HAS CORROSION. REMOVED CORROSION IAW CRJ900 SRM 51-21-06-001-A01.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,618 hrs · 5,942 cycles

SERVICE DOOR SILL HAS CORROSION. REMOVED CORROSION IAW CRJ900 SRM 51-21-06-001-A01.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT)

EMERGENCY LIGHTS WILL NOT COME ON. REPLACED BATTERY PACK NR 2. (S)

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 2,094 hrs · 1,298 cycles

EMERGENCY LIGHTS WILL NOT COME ON. REPLACED BATTERY PACK NR 5. (S)

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 2,094 hrs · 1,298 cycles

EMERGENCY LIGHTS WILL NOT COME ON. REPLACED BATTERY PACK NR1. (S)

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 2,094 hrs · 1,298 cycles

EMERGENCY LIGHTS WILL NOT COME ON. REPLACED BATTERY PACK NR 4. (S)

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 2,094 hrs · 1,298 cycles

EMERGENCY LIGHTS WILL NOT COME ON. REPLACED BATTERY PACK NR 3. (S)

Part: CONTROL UNIT — FAULTY (ANTI-SKID SYS) · airframe 1,190 hrs · 762 cycles

FLIGHT 5105- RECEIVED BRAKE OVERHEAT MESSAGE ON TAKE-OFF ROLL. ABORTED TAKE-OFF, RETURNED TO GATE WITHOUT INCIDENT. REPLACED ANTI-SKID CONTROL UNIT. NO FURTHER DEFECTS.