N8886A

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 30,506 hrs · 28,207 cycles

DURING FIRST FLIGHT PREPARATIONS, FOUND INTERIOR AND EXTERIOR OVER WING AND FLOOR TRACK LIGHTS INOP REMOVED AND REPLACED THE #2 AND #3 EMERGENCY LIGHT BATTERY PACKS IAW AMM 33-51-04. OPS CHECK GOOD

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,129 hrs · 27,816 cycles

FLOOR LEVEL EMERGENCY LIGHT AT THE PASSENGER DOOR IS NOT WORKING. R&R'D FLOOR LEVEL EMERGENCY FLOOD LIGHT ASSY IAW AMM 33-51-19. OPS CHECK GOOD

Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 29,723 hrs · 27,369 cycles

EMERGENCY LIGHTS IN GALLEY WONT ILLUMINATE WHEN TESTED. REPAIRED BROKEN WIRE TO LIGHT ASSEMBLY IAW CRJ200 ESPM 20-16-00 . OPS CHECK GOOD.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 29,053 hrs · 26,655 cycles

FLOOR LEVEL EXIT SIGN INOP. REPLACED EXIT SIGN IAW AMM 33-51-10 OPS CHECK GOOD

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 28,177 hrs · 25,736 cycles

LBL27 FLOOR SUPPORT BETWEEN FS574.0 AND FS609.0 HAS CORROSION. REMOVED CORROSION IAW SRM 51-21-06 FOUND TO BE OUT OF LIMTS IAW SRM 53-00-00. REMOVED AND REPLACED SEAT RAIL BEAM LBL 27 SRM 51-42-21.

Part: FRAME — CRACKED (FUSELAGE) · airframe 28,177 hrs · 25,736 cycles

CARGO BAY AT 605 9L FRAME CRACKED. REPAIRED FRAME 605 IAW REO 601R-53-61-5214.

Part: RETAINER — CRACKED · airframe 28,177 hrs · 25,736 cycles

NR 1 ENG PNL 412BT SEAL RETAINER IS CRACKED. REMOVED AND REPLACED SEAL RETANER ON PNL 412BT IAW SRM 51-42-06.

Part: FITTING — CORRODED (FUSELAGE) · airframe 28,177 hrs · 25,736 cycles

RT O/B FLOORBEAM ATTACH TO APB, HAS CORROSION AT FASTENER HOLE. REPAIRED RT O/B FLOORBEAM FITTING IAW EA 253-07317.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 28,177 hrs · 25,736 cycles

STR 3L IS CRACKED JUST BELOW THE UPPER PAX DOOR SILL AT FS 379, IN THE CABIN. R&R STRINGER 3L STATION 379 TO 409 IAW SRM 51-42-06. OPS TEST OF LIGHTING C/W ON W/O.

Part: STIFFENER — CRACKED (APU BAY) · airframe 28,177 hrs · 25,736 cycles

CRACK IN WELD AT APU ENCLOSURE UPPER CENTER STIFFENER AT AFT END. REPAIRED APU ENCLOSURE UPPER CENTER STIFFENER IAW REO 601R-49-11-071.

Part: FITTING — CRACKED (COCKPIT) · airframe 28,177 hrs · 25,736 cycles

FLIGHT DECK CENTER WINDSHIELD POST LOWER LEFT FITTING IS CRACKED. (NDT HAS VERIFIED). REMOVED AND REINSTALLED REF ITEMS 1-4-7 IAW REM ITEMS 1-4& 7 OPS TEST OF EFDS 3 & 4 GOOD IAW AMM 31-61-01-710-801 ISI WAS NEVER REMOVED THEREFORE LEAK CHECK OF THE P3 S3 AND S45 NOT REQUIRED. REMOVED AND REPLACED CENTER POST LOWER FITTING IAW SRM 51-42-21.

Part: FITTING — CRACKED (FUSELAGE) · airframe 28,177 hrs · 25,736 cycles

FLOOR SUPPORT BEAM CLIP IS CRACKED AT FS484.00 BL36R. REPAIRED FLOOR SUPPORT BEAM CLIP AT STATION 484 BL36R IAW REV 601 R-53-41-059.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 28,177 hrs · 25,736 cycles

EVIDENCE OF A CRACK ON AN ANGLE BRACKET OF THE AFT PRESSURE BULKHEAD RT SIDE AROUND STR 14A. REMOVED AND REPLACED ANGLE AT STRINGER 14R IAW SRM 51-42-06.

Part: POST — CRACKED (FUSELAGE) · airframe 28,105 hrs · 25,654 cycles

DURING COMPLIANCE OF TC53-160-604, 10K INSP, VERT POST RBL 27.00 AT FS 409+128 HAS A CRACK ON THE IB CHANNEL. CRACK EXTENDS UP FROM THE BOTTOM EDGE UP TO BUT NOT PAST 2ND RIVET UP. PERMANENTLY REPAIRED VERTICAL POST RBL 27.00 AT FS 409+128 IAW REO 601R-53-41-0056. THIS IS A MAJOR REPAIR.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 27,826 hrs · 25,355 cycles

EXTERIOR LT AFT EMERGENCY LIGHT OUT. REMOVED AND REPLACED THE EMERGENCY LIGHT IAW AMM 33-51-21. OPS CHECKED GOOD.

Part: INTERCOSTAL — CRACKED (BS 621-625) · airframe 27,074 hrs · 24,518 cycles

RIGHT TOP INTERCOSTAL OTBD OF RBL 36.2 BS 621 TO 625.3, STRINGER 14R CRACKED ONE INCH.

Part: MICROPHONE — INOPERATIVE (OXYGEN MASK) · airframe 26,865 hrs · 24,289 cycles

OBSEVER OXYGEN MASK MICROPHONE INOPERATIVE. R & R THE OXYGEN MASK IAW AMM 35-11-12. PERFORMED AN OPS CHECK IAW AMM 23-51-00. CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,746 hrs · 24,151 cycles

FORWARD FLOOR EMERGENCY LIGHT IS INOPERATIVE. REMOVED AND REPLACED THE LIGHT IAW AMM 33-51-01. OPERATIONAL CHECKED GOOD IAW AMM 33-51-00.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 26,094 hrs · 23,443 cycles

FOUND LIGHTED EXIT SIGN FLOOR LEVEL AT MAIN ENTRANCE ON LEFT, INOPERATIVE. REMOVED AND REPLACED THE SIGN IAW AMM 33-51-10. OPS CHECKED GOOD.

Part: CONTROL UNIT — LOOSE · airframe 26,067 hrs · 23,416 cycles

FIRST OFFICER`S OXYGEN MASK FAILED TO TEST OVER THE SPEAKER. REPLACED THE OXYGEN BOX IAW AMM 35-11-15. DURING OPERATIONAL CHECKS, FOUND THE AECU LOOSE IN THE RACK. SECURED AECU 23-51-00. REPERFORMED OPERATIONAL CHECKS OF THE FO OXYGEN BOX, ALL CHECKS (AUDIO AND LEAK) GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 25,891 hrs · 23,224 cycles

RIGHT OVERWING EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMP IAW AMM 33-51-00, OPS TESTED NORMAL.

Part: ELT — INOPERATIVE · airframe 25,746 hrs · 23,069 cycles

ELT FAILS OPERATIONAL TEST. REMOVED AND REPLACED ELT IN ACCORDANCE WITH AMM 25-62-01. OPS GOOD AT THIS TIME P/N ON AND OFF 453-5000 S/N ON 04010 S/N OFF 170-14569.

Part: OXYGEN MASK — UNWANTED DEPLOY (CABIN) · airframe 25,592 hrs · 22,911 cycles

FOUND OXYGEN MASKS DEPLOYED. STOWED ALL OXYGEN MASKS IAW AMM 35-21-09. PERFORMED OPS TEST IAW AMM 35-20-00. TEST PASS. ACFT OK FOR SERVICE.

Part: DETECTOR — INOPERATIVE (FLAP SKEW) · airframe 25,428 hrs · 22,748 cycles

FLAPS FAIL MASTER CAUTION FLAPS SELECTED OUT OF ZERO TO 20 FLAPS FAILED AT 0 DEGREES. INSPECTED SDU NOTED FAULTS ON LT AND RT CHANNELS, RESET SDU IAW AMM 27-51-15. PERFORMED OPERATIONAL TEST OF THE FLAP SYS IAW 27-54-00. PLACED FLAP SYSTEM IN MEL DUE TO DUAL CHANNEL FAILURE IAW MEL 27-50-00. PERFORMED 5 CONSECUTIVE FLAP CYCLES FAULT DID NOT RETURN. REMOVED AND REPLACED THE SKEW DETECTION UNIT.

Part: OXYGEN MASK — UNWANTED DEPLOY (SEAT 4 CD) · airframe 25,306 hrs · 22,620 cycles

OXYGEN MASKS DROPPED OVER SEAT 4 CD. REPACKED THE OXYGEN MASK IAW AMM 35-21-09. OPS CHECKED GOOD. OK FOR SERVICE.

Part: ACM — OUT OF ADJUST (AC BAY) · airframe 25,089 hrs · 22,412 cycles

AFTER TAKEOFF AND SWITCHES TO 10TH STAGE BLEEDS THERE WAS A NOTICEABLE ODOR IN FLIGHT DECK AND CABIN. ODOR DISSIPATED IN CABIN BUT PERSISTED IN FLIGHT DECK, MINOR BUT DETECTABLE. PERFORMED ADJUSTMENT TEST OF ACM IAW AMM 21-51-00. NO DEFECTS NOTED.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 24,787 hrs · 22,091 cycles

RIGHT FWD EXTERNAL EMERGENCY LIGHT INOPERATIVE. R & R LAMP AT RT FWD EXTERIOR EMERGENCY LIGHT IAW AMM 33-51-21. NO FURTHER DEFECTS NOTED.

Part: WIRE — DAMAGED (CABIN) · airframe 24,541 hrs · 21,843 cycles

CABIN DOOR NOT LIGHTING UP, EMER LIGHTS. REPAIRED WIRE AT LIGHT IAW ESPM 20-16-00. OPERATIONS CHECKED GOOD.

Part: LANDING — DAMAGED (WING) · airframe 24,234 hrs · 21,527 cycles

ACCESS HOLE FOR FUEL PANEL 540BB HAS DAMAGE ON THE LANDING. REPAIRED 540BB FUEL ACCESS WING PLANK LANDING. REF STEPS 1 - 4 FOR WORK PERFORMED. REO 601R-57-21-2418 COMPLIED WITH. THIS IS A MAJOR REPAIR.

Part: BATTERY PACK — DISCHARGED (FLASHLIGHT) · airframe 24,234 hrs · 21,527 cycles

PILOT & CO-PILOT EMER FLASHLIGHTS ARE INOPERATIVE. REMOVED & INSTALLED NEW SERVICEABLE BATTERY PACK, PN P4-01-0021, IN PILOT & CO-PILOT EMER FLASHLIGHTS IAW AMM 25-61-00-960-801. OPERATIONS CHECKED GOOD AT THIS TIME.

Part: STEP — DENTED (PAX DOOR) · airframe 24,234 hrs · 21,527 cycles

PASSENGER DOOR, MID FIXED STEP IS DENTED, APPROX 2" IN DIAMETER. LOCATED, DRILLED & COUNTERSUNK NEW SERVICEABLE FIXED MID STEP, PN 601R317076-9, IAW SRM CH 51-40-11.

Part: BULKHEAD — CHAFED (FUSELAGE) · airframe 24,234 hrs · 21,527 cycles

FS 621 BULKHEAD IS CHAFED IN MULTIPLE LOCATIONS, FROM CARGO LINER SCREWS. CONTINUATION CARD 8788611 OP 171 & 187. REPAIRED CHAFE IN 621 BULKHEAD IAW STEPS 1 - 12 FOR WORK PERFORMED. THIS IS A MAJOR REPAIR IAW 601R-53-61-1285 REV D 2155 REV A & - 5648.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 24,234 hrs · 21,527 cycles

WARDROBE COMPARTMENT EMER FLASHLIGHT INOPERATIVE. R & R WARDROBE COMPARTMENT EMERGENCY FLASHLIGHT IAW AMM 20-21-00-910-801 & BY REMOVING 2 SCREWS, INSTALLING NEW LIGHT & INSTALLING 2 SCREWS.

Part: SKIN — CORRODED (FUSELAGE) · airframe 24,234 hrs · 21,527 cycles

EXTERIOR SKIN FS 559+64 - 559+112, STRINGER 25L - 25R, HAS CORROSION AROUND LOCK FASTENERS. CONTINUATION CARD 8788611 OP 160 & 223. REPAIRED EXTERIOR SKIN CORROSION AROUND LOCK FASTENERS IAW EA CRJ253-04013. REF JC 8788611 OPS 63, 160, & 223 STEPS 1 - 12 FOR WORK COMPLETED.

Part: RIB — CORRODED (LT WING) · airframe 24,234 hrs · 21,527 cycles

BATTERY RIBS ON LT SIDE AT WING STATION 48.30 & 53.60, HAVE CORROSION. CONTINUATION CARD 8788615 OP 50, 51, 53 & 70. R & R LT WING LOWER SKIN PANEL, PN 601R10213-3, IAW SRM 51-42-21. REPAIRED IAW EA CRJ257-04062. R & R BATTERY RIB, PN 601R10203-27, AT WS 53.60 IAW SRM 51-42-21 & EA CRJ257-04034 REV C DATED 02 22 2016. REPAIRED LT WING LOWER WING PLANK TE IAW EA CRJ257-04034 REV C DATED 02 22 2016. REF ATTACHED COPY FOR WORK PERFORMED. THIS IS A MAJOR REPAIR.

Part: CONNECTOR — BROKEN (CABIN) · airframe 24,234 hrs · 21,527 cycles

CABIN TRACK LIGHTING, FWD CONNECTION HAS A BROKEN CONNECTOR PLUG. EMER FLOOR TRACK LIGHTING WAS REPAIRED BY REPLACING SPLICE IAW ESPM 20-17-31 & REPLACING NR 4 BATTERY CHARGER IAW AMM 33-51-05-400-801. OPERATIONS CHECKED GOOD.

Part: LANDING — DAMAGED (RT WING) · airframe 24,234 hrs · 21,527 cycles

FOUND RT FUEL ACCESS HOLE 650AB LANDING, INBD SIDE HAS MULTIPLE INDICATIONS NOTED APPROX 7.O" INCHES LONG BY .250 WIDE 50% FSH, FAILED NDT INSPECTION. REPAIRED IAW REO 601R-57-21-030 REV L. THIS IS A MAJOR REPAIR.

Part: BULKHEAD — DAMAGED (FUSELAGE) · airframe 24,234 hrs · 21,527 cycles

FOUND REAR PRESS BULKHEAD WEB THAT SURROUNDS THE LINTEL ATTACHMENT FITTING HAS INDICATION NOTED APPROX .100" IN LENGTH, 50% FSH, FAILED NDT INSPECTION. REPAIRED IAW REO 601R-53-61-1230 REV F DATED 10 31 11. THIS IS A MAJOR REPAIR.

Part: PANEL — DAMAGED (STABILIZER) · airframe 24,234 hrs · 21,527 cycles

PANEL 326BL FOUND TO BE SPLIT ON UPPER RT CORNER OF PANEL. REPAIRED PANEL 326BL IAW REO 601R-55-32-233 REV A DATED 05 05 09 & SRM 51-25-01. REINSTALLED PANEL 326BL IAW AMM 55-32-05-400-805.

Part: HINGE — DAMAGED (FUSELAGE) · airframe 24,234 hrs · 21,527 cycles

AFT CARGO BAY STEP PLATE FWD HINGE REQUIRES REPLACEMENT DUE TO ELONGATED HOLE, AS WELL AS CTR HINGE. R & R FWD & MIDDLE HINGES, PN 601R35205-69 IAW SRM 51-42-06 & 51-40-11. ALSO PN 601R35205-67.

Part: HINGE — BROKEN (WING) · airframe 24,234 hrs · 21,527 cycles

BUTTE DOOR PANEL 694JB HINGE IS BROKEN. R & R BUTTE DOOR PANEL 694JB HINGE IAW SRM 51-25-16, 51-42-06 & 51-25-06.

Part: LANDING — DAMAGED (WING) · airframe 24,234 hrs · 21,527 cycles

ACCESS HOLE FOR FUEL PANEL 640BB HAS DAMAGE TO THE LANDING. CONTINUATION CARD 8788611 OP 222. REPAIRED FUEL TANK CUT OUT FOR 640BB IAW REO 601R-57-21-030 REV L DATED 02 05 14. LEAK CHECKED GOOD. THIS IS A MAJOR REPAIR.

Part: STRIKER — DENTED (PAX DOOR) · airframe 24,234 hrs · 21,527 cycles

PASSENGER DOOR SILL STRIKER ON AFT SIDE, APPROX 6" FROM TOP, IS DENTED APPROX 1". REPAIR PAX DOOR SEAL STRIKER AFT SIDE IAW SRM 52-11-10, 51-24-21 & REO 601R-53-22-033 TYPE 1 & TYPE 3.

Part: FRAME — CORRODED (FUSELAGE) · airframe 24,234 hrs · 21,527 cycles

FRAME SECTOR FS 585 AT STRINGER 26R IS CORRODED. CONTINUATION CARD 8788611 OP 167 & 172. REPLACED FRAME AT FS 589, DUE TO CORROSION BEING OUT OF LIMITS IAW SRM 51-42-06, 51-42-21. IAW MWC JOB 8788611 110, 167 & 172 FOR WORK PERFORMED. FRAME AT 589 NOT 585 CORRODED.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 24,234 hrs · 21,527 cycles

AIRCRAFT GND POWER RECEPTACLE BRACKET IS CRACKED. CONTINUATION CARD 8788611 OP 165 & 178. REPLACED ACFT GND POWER RECEPTACLE BRACKET IAW SRM 51-40-00, 51-42-21, 51-40-11, 51-42-06 & 51-23-00. REF MWC JOB 8788611 65, 165, 178 & 206 FOR WORK PERFORMED.

Part: FAIRING — GOUGED (FUSELAGE) · airframe 24,234 hrs · 21,527 cycles

RIGHT STUB FAIRING HAS GOUGE MEASURING .015" DEEP. RECEIVED NEW SERVICEABLE STUB FAIRING ASSEMBLY PN 601R31199-92. INSTALLED SEAL ONTO STUB FAIRING IAW SRM 51-42-15. REF MWC JOB 8788610 OP 507 FOR INSTALL OF STUB FAIRING.

Part: FRAME — CORRODED (FUSELAGE) · airframe 24,234 hrs · 21,527 cycles

FRAME SECTOR FS 605 AT STRINGER 26R IS CORRODED. CONTINUATION CARD 8788611 OP 158, 164, 180, & 211. R & R FS 605 FRAME IAW SRM 51-42-06, 51-42-11 & 51-42-21. REF JC 8788611 OPS 111, 158, 164, 180 & 211 STEPS 1 - 25 FOR WORK PERFORMED.

Part: FRAME — CORRODED (FUSELAGE) · airframe 24,234 hrs · 21,527 cycles

FRAME SECTOR FS 333 IS CORRODED, BETWEEN STRINGER 26R & 26L. CONTINUATION CARD 8788611 OP 166. R & R FS 333 FRAME SECTOR IAW SRM 51-42-06 & 51-42-21.

Part: RETAINER — CORRODED (E&E DOOR) · airframe 24,234 hrs · 21,527 cycles

AVI BAY DOOR SEAL RETAINERS ARE CORRODED FWD EDGE AFT OF SEAL MARKED WITH TAPE. CONTINUATION CARD 8788611 OP 159 & 192. R & R AVI BAY DOOR SEAL RETAINERS IAW SRM 51-42-06 & 51-40-11. REF MWC JOB 8788611 85, 159 & 192 FOR WORK PERFORMED.

Part: HINGE FITTING — DAMAGED (TE FLAP) · airframe 24,234 hrs · 21,527 cycles

UPON REMOVAL OF RT INBD FLAP ASSEMBLY, NOTICED DAMAGE TO INBD HINGE ARM & BOX ATTACHMENT POINT. REPLACED RT INBD FLAP HINGE FITTING YOKE, IAW STEPS 1 - 5 FOR WORK PERFORMED IAW REO 601R-57-52-2105, REF PWI D538479 FOR DTA REQUIREMENTS.

Part: VANE — CHAFED (TE FLAP) · airframe 24,234 hrs · 21,527 cycles

RIGHT INBD FLAP VANE IS CHAFED AT 3 LOCATIONS, WORST IS APPROX 1"" L X 1/2"" W X .010"" D. CONTINUATION CARD 8788611 OP 169. R & R RT INBD FLAP VANE MID SKIN IAW SRM 51-42-13. REPAIRED INBD & OTBD LOCATIONS IAW GREO 601R-57-52-004.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 24,234 hrs · 21,527 cycles

PASSENGER DOOR AFT DRAG ANGLE IS CRACKED AT PREVIOUS REPAIR. CONTINUATION CARD 8788611 OP 181. REPAIRED PAX DOOR AFT DRAG ANGLE IAW STEPS 1 - 6 FOR WORK PERFORMED ON MWC 8788611 OP 89.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 24,234 hrs · 21,527 cycles

THREE EACH INTERCOSTALS CRACKED IN RADIUS AT FS 621 BULKHEAD, AT STRINGERS 13L - 15L. CONTINUATION CARD 8788611 OPS 173 & 174. REPLACED THREE EACH INTERCOSTALS AT 621 BULKHEAD, AT STRINGER 13L - 15L. REF STEPS 1 - 13 FOR WORK PERFORMED. THIS IS A MAJOR REPAIR. PNS REPLACED 601R350121-9, 601R350121-5 & 601R350121-3.

Part: BULKHEAD — DAMAGED (FUSELAGE) · airframe 24,234 hrs · 21,527 cycles

FOUND REAR PRESS BULKHEAD WEB AT LBL 27.50, WL 130, HAS INDICATION NOTED APPROX .500" IN LENGTH 100% FSH, FAILED NDT INSPECTION. REPAIRED IAW REO 601R-53-61-1541 & REO 601R-53-61-5649. REF STEPS 1 - 3 FOR WORK PERFORMED.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 24,234 hrs · 21,527 cycles

FLOORBEAM CAP IS CORRODED AT FS 585, BETWEEN RBL 9 - 27. REPLACED FLOORBEAM CAP IAW STEPS 1 - 2 FOR WORK PERFORMED.

Part: SKIN — CRACKED (PAX DOOR) · airframe 24,234 hrs · 21,527 cycles

PASSENGER DOOR, AFT SIDE SKIN IS CRACKED AT MID-FIXED STEP. CONTINUATION CARD 8788611 OP 168. REPAIRED PAX DOOR AFT SIDE SKIN CRACK, AT MID-FIXED STEP IAW EA CRJ252-04017 & REO 601R-52-11-702.

Part: RETAINER — CRACKED (PANEL) · airframe 24,234 hrs · 21,527 cycles

PANEL 412DB FWD & AFT SEPARATOR PANELS ARE CHAFED ALONG THE TOP EDGE, PLUS THE SEAL RETAINER IS CRACKED. REMOVED SEAL RETAINER IAW SRM 51-42-06. REPAIRED SEAL RETAINER IAW EA CRJ254-04028 REV IB. INSTALLED SEAL RETAINER IAW SRM 51-42-06. R & R FWD & AFT SEPARATOR PANELS IAW SRM 51-42-06.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 24,234 hrs · 21,527 cycles

RIGHT SIDE FLOOR SEAT TRACK HAS MULTIPLE LOCATIONS OF CORROSION. TRACK 1 & 2. CONTINUATION CARD 8788611 OP 163. R & R RT SIDE FLOOR SEAT TRACKS 1 & 2 IAW AMM 53-01-11-000-802 & 53-01-11-400-802.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 24,234 hrs · 21,527 cycles

RIGHT SIDE ACCESS FAIRING SUPPORT ANGLES AT FS 461.5, 469.63 & 476.67 ON TOP OF WING ARE CRACKED, 3 EACH. R & R RT SIDE ACCESS FAIRING SUPPORT ANGLES IAW SRM 51-42-06, 51-42-21 & 51-40-11.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 24,234 hrs · 21,527 cycles

FS 621 OBLIQUE ANGLE IS CRACKED, STRINGER 14L. LOCATED, DRILLED & INSTALLED NEW SERVICEABLE OBLIQUE ANGLE, PN 601-35012-51, IAW SRM 51-40-11 & SRM 51-42-06.

Part: CAP — DENTED (PAX DOOR) · airframe 24,234 hrs · 21,527 cycles

PASSENGER DOOR, 2 UPPER CORNER CAPS ARE DENTED, APPROX 1" IN DIAMETER. INSTALLED & REMOVED MARKING TAPE AS REQUIRED. REPLACED PAX DOOR, 2 EACH UPPER CORNER CAPS IAW SRM 51-42-13.

Part: VANE — CHAFED (TE FLAP) · airframe 24,234 hrs · 21,527 cycles

LEFT INBD FLAP VANE IS CHAFED AT 3 LOCATIONS, APPROX 1" LX .5" W X .010" D. INSTALLED & REMOVED MARKING TAPE AS REQUIRED. REPLACED 3 EA LT INBD FLAP VANE LE CAPS IAW SRM 51-42-13, 51-23-00 & 51-25-26.

Part: FITTING — BROKEN (TE FLAP) · airframe 24,234 hrs · 21,527 cycles

LEFT FLAP STUB FAIRING, FWD AIRFRAME MOUNT IS BROKEN OFF. R & R LT FLAP FITTING, PN 601R10371-1 IAW SRM 51-42-21.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 24,234 hrs · 21,527 cycles

LEFT SIDE FLOOR SEAT TRACK 2 HAS MULTIPLE LOCATIONS OF CORROSION. FABRICATED & REPLACED SEAT TRACK AT LBL 9, FROM FS 409 - 409+128 IAW GREO 601R-53-00-485 & AMM 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 24,234 hrs · 21,527 cycles

CARGO SEAT TRACK SEGMENT IS CORRODED AT LBL 9, BETWEEN FS 572 - 559+112. INSTALLED & REMOVED MARKING TAPE AS REQUIRED. REPLACED CARGO SEAT TRACK AT LBL 9, BETWEEN FS 572 - 559+112 IAW AMM 53-00-49-400 000-801.

Part: STOP FITTING — BROKEN (WING) · airframe 24,234 hrs · 21,527 cycles

PANEL 694JB HAS BUTTE DOOR STOP TAB BROKEN OFF THE END OF THE PANEL. R & R BUTTE DOOR STOP ASSEMBLY, PN 600-10196-16, IAW SRM 51-42-06.

Part: RETAINER — DENTED (CARGO DOOR) · airframe 24,234 hrs · 21,527 cycles

CARGO DOOR BOTTOM AFT & BOTTOM AFT CORNER SEAL RETAINER FOUND DENTED, REQUIRES REPLACEMENT. REPLACED CARGO DOOR SEAL RETAINER BOTTOM AFT & BOTTOM AFT CORNER IAW SRM 51-40-11, 51-42-06, 51-25-00 & 51-23-00-910-801.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 24,234 hrs · 21,527 cycles

SEAT TRACK RAIL AT RBL 9, BETWEEN FS 559+80 - 559 HAS PITTING CORROSION & GOUGES AT MULTIPLE LOCATIONS. FABRICATED NEW SEAT TRACK IAW REO 601R-53-00-485. REMOVED & INSTALLED SEAT TRACK AT FS 559+80 - 559, RBL 9 IAW AMM 53-01-11-000 400-802.

Part: DOOR — LACK OF LUBE (EMERGENCY EXIT) · airframe 24,234 hrs · 21,527 cycles

LEFT OVERWING EMER EXIT FAILED FUNCTION CHECK. HANDLE REQUIRED MORE THAN 40 POUNDS OF FORCE TO OPEN. LUBRICATED LT WING OVERWING EMER EXIT IAW AMM 12-30-52-640-801 & ACCOMPLISHED FUNCTIONAL CHECK IAW AMM 52-21-00-720-801. FUNCTIONAL CHECK IS GOOD AT THIS TIME.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 24,234 hrs · 21,527 cycles

SEAT TRACK RAIL AT LBL 9, BETWEEN FS 559.0 - 559+80, HAS PITTING CORROSION & GOUGES AT MULTIPLE LOCATIONS. R & R SEAT TRACK RAIL AT LBL 9, BETWEEN FS 559.0 - 559+80 IAW GREO 601R-53-00-485 REV DATED 09 28 12 & AMM 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 24,234 hrs · 21,527 cycles

CARGO SEAT TRACK SEGMENT IS CORRODED AT LBL 27, BETWEEN FS 559+80 - 559+96. R & R CARGO SEAT TRACK SEGMENT AT LBL 27, BETWEEN FS 559+80 - 559+96 IAW AMM 53-01-11-400-802.

Part: OXYGEN MASK — UNWANTED DEPLOY (CABIN) · airframe 24,082 hrs · 21,381 cycles

UPON APPLYING EXTERNAL POWER TO ACFT PAX OXY MASKS DEPLOYED. REPACKED 02 MASKS IAW AMM 35-21-09. PERFORMED OPERATIONAL TEST OF PAX OXYGEN SYS IAW AMM 35-20-00. ACFT OK FOR SERVICE.

Part: CABLE — BROKEN (PAX DOOR) · airframe 24,021 hrs · 21,327 cycles

PAX DOOR LOWER SUPPORT-WHEEL CABLE BROKEN. DEFERRED PASSENGER DOOR ASSIST IAW MEL 52-11-11 ENTERD INTO DMR PLACARD INSTALLED AUTHORIZATION 010183. R & R PAX DOOR LOWER SUPPORT-WHEEL CABLE IAW AMM 52-11-13, OPS CHECK GOOD, OK FOR SERVICE. PN ON/OFF 601R38370-5, SN ON/OFF.

Part: OXYGEN MASK — UNWANTED DEPLOY (CABIN) · airframe 23,276 hrs · 20,581 cycles

UPON STARTING THE ACFT THE PAX OXYGEN MASK DEPLOYED. RESET O2 DEPLOYMENT SYS STOWED MASK & PERFORMED OPERATIONS CHECK IAW AMM 35-20-00 & 35-21-09.

Part: LIFE VEST — UNSERVICEABLE (COCKPIT) · airframe 22,420 hrs · 19,744 cycles

FIRST OFFICER`S LIFE VEST BAG TORN. R & R FIRST OFFICER`S LIFE VEST IAW AMM 25-61-03.

Part: OXYGEN MASK — BROKEN (COCKPIT) · airframe 22,232 hrs · 19,557 cycles

OBSERVER`S O2 MASK IS BROKEN. DEFERRED, R & R OBSERVER`S O2 MASK IAW AMM 35-11-12.

Part: LOCK PIN — LACK OF LUBE (EMERGENCY EXIT) · airframe 21,633 hrs · 18,968 cycles

RIGHT OVERWING EMERGENCY EXIT FAILED FUNCTIONAL TEST (EXCEEDED 40 POUNDS). LUBED RT OVERWING EXIT LOCKPINS IAW AMM 12-20-52-640-802. REPERFORMED FUNCTIONAL TEST OF THE RT OVERWING EMERGENCY EXIT IAW AMM 52-21-00-720-801. OPENING FORCE DID NOT EXCEED 40 POUNDS. NO DEFECTS NOTED.

Part: LOCK PIN — LACK OF LUBE (EMERGENCY EXIT) · airframe 21,633 hrs · 18,968 cycles

LEFT OVERWING EMERGENCY EXIT FAILED FUNCTIONAL TEST (EXCEEDED 40 POUNDS). LUBRICATED LT OVERWING EXIT LOCKPINS IAW AMM 12-20-52-640-802. REPERFORMED FUNCTIONAL TEST IAW AMM 52-21-00720-801. OPENING FORCE DID NOT EXCEED 40 POUNDS. NO DEFECTS NOTED.

Part: POTENTIOMETER — OUT OF ADJUST (TE FLAPS) · airframe 21,633 hrs · 18,968 cycles

FLAPS FAILED MESSAGE POSTED WHILE PERFORMING FUNCTIONAL TEST OF FLAP SYS AT STEP 4.A.16 (G-I) REF AMM 27-54-00-720-801. ADJUSTED LT FLAP POSITION TRANSMITTER POTENTIOMETER. PERFORMED FUNCTIONAL TEST OF FLAP SYS IAW AMM 27-54-00-720-801. NO DEFECTS NOTED.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 21,593 hrs · 18,932 cycles

SIX DAMAGED RIVETS AT WL 86.5, LBL AND RBL 9.5, 18, 27.5, TWO GOUGES AT WL 86.5, LBL 8 AND RBL 7, TEN DAMAGE MARKS AT WL 103, LBL 7.75, RBL 6.75, LBL AND RBL 9, 18, 27.5, AND 36.2, MEASURING 0.004" TO 0.014" DEEP. REPAIRED IAW REO 601R-53-61-2155.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,495 hrs · 18,832 cycles

EMERGENCY LIGHT INOPERATIVE IN CABIN. PERFORMED OPS CHECK OF CABIN EMERGENCY LIGHT IAW AMM 33-51-00. OPS CHECKED GOOD.

Part: LIGHT — DISLODGED (CABIN) · airframe 21,472 hrs · 18,811 cycles

EMERGENCY LIGHTS AT ROW 1CD LOOSE. R & R EMERGENCY LIGHT IAW AMM 33-51-01. OPS CHECKED GOOD.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 21,434 hrs · 18,769 cycles

FLAPS DEGRADED STATUS MESSAGE, COMPLETED OPS TEST OF SKEW DETECTION SYS (IBIT) AND RESET SYS MESSAGE WENT AWAY OPERATED FLAPS THROUGH MESSAGE DID NOT RETURN, WORK DONE IAW FIM 27-50-00 AND AMM 27-51-15.

Part: TILLER — OUT OF POSITION (NLG STEERING) · airframe 21,422 hrs · 18,757 cycles

AIRCRAFT PULLS CONSIDERABLY TO THE LEFT FROM 0 TO 080 KTS WITH BOTH TILLER AND LDG. REMOVED, INSPECTED AND CLEANED STEERING TILLER BUT TILLER WILL NOT CENTER. REINSTALLED TILLER . NOSE WHEEL STEERING TILLER NOT CENTERING PROPERLY WAS CAUSING THE DISCREPANCY.

Part: SIGN — INOPERATIVE (CABIN) · airframe 20,062 hrs · 17,392 cycles

LIGHTED EXIT SIGN ON PASSENGER ENTRANCE INOP. REMOVED AND REPLACED LIGHTED EXIT SIGN IAW AMM 33-50-00. OPS CHECK GOOD.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 20,050 hrs · 17,369 cycles

F/A'S FLASHLIGHT INOP. REMOVED AND REPLACED F/A FLASHLIGHT BATTERY IAW AMM 25-61-01. OPS CHECK GOOD. DM CLEARED.

Part: LIFE VEST — UNSERVICEABLE (CABIN) · airframe 19,253 hrs · 16,588 cycles

F/A LIFE VEST BAG TORN. REMOVED AND REPLACED F/A LIFE VEST IAW AMM 25-61-03.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 18,705 hrs · 16,068 cycles

FS 559 SEMI-PRESSURE BULKHEAD CRACKED AT RBL 18. REPAIRED IAW BOMBARDIER REO 601R-53-41-260 AND 601R-53-41-609 AS AUTHORIZED BY PA 53-025.

Part: FITTING — BROKEN (THRUST REVERSER) · airframe 18,567 hrs · 15,999 cycles

RT REV UNLOCK CAUTION MSG IN FLIGHT. FOUND THE BOTTOM (2) ANTIROTATION TANGS ON BALLSCREW ACTUATORS BROKEN AND T/R OUT OF RIG. REMOVED AND REPLACED ANTI ROTATION TANGS IAW HONEYWELL CMM 78-30-29 RIGGED RT T/R IAW AMM 78-30-00 OP/C GOOD.

Part: FUEL LINE — LEAKING (APU) · airframe 18,335 hrs · 15,707 cycles

XFLOW/APU PUMP-CAUTION MSG INFLIGHT DURING CRUISE W/ APU OFF FUEL QUANTITIES WERE NORMAL. FOUND FUEL LINE LEAKING FROM THE APU FUEL SOLENOID. RESCURED THE LINE AND PERFORMED OP CHECK APU IAW AMM 49-10-00. OP CHECK GOOD, LEAK CHECK GOOD.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 17,792 hrs · 15,255 cycles

LEFT LOWER WING PLANK FUEL ACCESS HOLE AT WS 12.245 HOLE NR 2 HAS PITTING CORROSION ON I/B, O/B, AND FWD EDGE OF CUTOUT MEASURING APPROX .003D X .025W X .025L IN BOTH CRITICAL AND NON-CRITICAL REGIONS. REPAIRED IAW BOMBARDIER REO 601R-57-21-030 REV H.

Part: BULKHEAD — CHAFED (FUSELAGE) · airframe 17,792 hrs · 15,255 cycles

REAR PRESSURE BULKHEAD CHAFED ON PREVIOUS REPAIRS 3 LOCATIONS ON RT SIDE AT RBL 18, RBL 27, RBL 36, ALL LOCATED 30.00" ABOVE FLOOR LEVEL. REPAIRED IAW BOMBARDIER REO 601R-53-6-2155.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 17,792 hrs · 15,255 cycles

LEFT LOWER WING PLANK FUEL ACCESS HOLE AT WS 54.897 HOLE NR 1 HAS PITTING CORROSION ON I/B, O/B, AND FWD EDGE OF CUTOUT MEASURING APPROX .004D X .030W X .030L IN BOTH CRITICAL AND NON-CRITICAL REGIONS. REPAIRED IAW BOMBARDIER REO 601R-57-21-030 REV H.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 17,792 hrs · 15,255 cycles

RIGHT LOWER WING PLANK FUEL ACCESS HOLE AT WS 54.897 HOLE NR 1 HAS PITTING CORROSION ON I/B EDGE OF CUTOUT MEASURING APPROX .003D X .022W X .022L IN NON-CRITICAL REGION. REPAIRED IAW BOMBARDIER REO 601R-57-21-030 REV H.

Part: BEAM — DAMAGED (FUSELAGE) · corrosion level 2 · airframe 17,792 hrs · 15,255 cycles

FS 280 TRANSVERSE BEAM IS CRACKED AND CORRODED. REPAIRED IAW BOMBARDIER REO 601R-53-11-926 REV B.

Part: SKIN — DAMAGED (ELEVATOR) · airframe 17,792 hrs · 15,255 cycles

RT ELEVATOR TOP SKIN HAS LIGHTNING STRIKE DAMAGE ON TRAILING EDGE AT ES 103.00. BURN MEASURES APPROX 0.500 LX.250"W. REPAIRED IAW BOMBARDIER REO 601R-55-21-327.

Part: SKIN — DAMAGED (ELEVATOR) · airframe 17,792 hrs · 15,255 cycles

RT ELEVATOR TOP SKIN HAS LIGHTNING STRIKE DAMAGE ON TRAILING EDGE AT ES 103.00. BURN MEASURES APPROX .500 LX .250W. REPAIRED IAW BOMBARDIER REO 601R-55-21-327.

Part: BULKHEAD — CHAFED (FUSELAGE) · airframe 17,792 hrs · 15,255 cycles

REAR PRESSURE BULKHEAD CHAFED ON PREVIOUS REPAIRS 3 LOCATIONS ON RT SIDE AT RBL 18, RBL 27, AND RBL 36 ALL LOCATED 30 INCHES ABOVE THE FLOOR LEVEL. REPAIRED IAW BOMBARDIER REO 601R-53-61-2155.

Part: BULKHEAD — CHAFED (FUSELAGE) · airframe 17,792 hrs · 15,255 cycles

REAR PRESSURE BULKHEAD CHAFED ON PREVIOUS REPAIRS 2 LOCATIONS ON LT SIDE AT LBL 18 AND LBL 27 ALL LOCATED 30 INCHES ABOVE THE FLOOR LEVEL. REPAIRED IAW BOMBARDIER REO 601R-53-61-2155.

Part: SKIN — DENTED (FUSELAGE) · airframe 17,792 hrs · 15,255 cycles

FUSELAGE SKIN IS DENTED AT FS 642 BETWEEN STR 21L & 22L. DENT MEASURES APPROX .650" DIA X .045"D. REPAIRED IAW BOMBARDIER REO 601R-53-61-4132.

Part: POST — DAMAGED (INOPERATIVE) · airframe 17,792 hrs · 15,255 cycles

FOUND FS 409.0+128 VERTICAL POST RBL 18.0 OTBD SIDE HAS INDICATION NOTED APPROX .2" IN LENGTH 60 PERCENT FSH AT WL 69.0 AFT. FLANGE RADIUS FAILED NDT INSPECTION. REPAIRED IAW SRM 51-42-06, 51-42-22, AND BOMBARDIER REO 601R-53-41-889.

Part: POST — DAMAGED (FUSELAGE) · airframe 17,792 hrs · 15,255 cycles

FOUND FS 409.0+128 VERTICAL POST BL 0.00 LT & RT SIDES HAVE INDICATIONS NOTED APPROX .2 INCH IN LENGTH 60 PERCENT FSH AT WL 69.0 AFT FLANGE RADIUS BOTH FAILED NDT INSPECTION. REPAIRED IAW SRM 51-42-06 AND BOMBARDIER REO 601R-53-41-889.

Part: FLOOR SUPPORT — CORRODED (CARGO BAY) · corrosion level 2 · airframe 17,792 hrs · 15,255 cycles

CARGO FLOOR SUPPORT BEAM CAP ANGLE HAS CORROSION AROUND FASTENER HOLES BETWEEN FS 589-FS 621, LBL 27. REPAIRED IAW SRM 51-42-34, 51-45-00,51-42-21, 5142-22, AND BOMBARDIER REO 601R53-61-3788 REV A.

Part: ENGINE — MALFUNCTIONED (RIGHT) · airframe 16,897 hrs · 14,415 cycles

CREW REPORTED SMOKE IN THE CABIN EMERGENCY DECLARED. T/S TO THE RIGHT ENGINE CAUSING THE SMOKE IN CABIN WITH EITHER LT OR RT PACKS RUNNING OFF RT ENGINE, A/C WAS FERRIED TO TYS FOR BOROSCOPE AND POSSIBLE ENGINE CHANGE.

Part: CONTROL UNIT — MALFUNCTIONED (HORIZ STAB) · airframe 16,800 hrs · 14,301 cycles

STAB TRIM RUNAWAY ON DEPARTURE. AIR RETURN TO JFK. QRH COMPLETED. REMOVED AND REPLACED HSTCU IAW AMM 27-41-01. PERFORMED OPS CHECK ON HSTCU. OPS CHECK GOOD. OK FOR SERVICE.

Part: CARBON SEAL — LEAKING (RT ENGINE) · airframe 16,731 hrs · 14,234 cycles

ON CLIMBOUT OF KDTW THE CAPTAIN SAW SMOKE COMING FROM A VENT. THIS WAS FOLLOWED BY A SMOKE TOILET CAUTION MESSAGE. THE FLIGHT CREW COMPLIED WITH THE QRH, DECLARED AN EMERGENCY AND REQUESTED TO RETURN TO KDTW. AN OTHERWISE UNEVENTFULL APPROACH AND LANDING WAS MADE AT KDTW. AFTER CFR INSPECTION, THE AIRCRAFT WAS TAXIED TO THE GATE. MAINTENANCE INSPECTED THE AIRCRAFT AND DISCOVERED A NUMBER ONE BEARING CARBON SEAL LEAKING ON THE RIGHT ENGINE. THE CARBON SEAL WAS REPLACED AND THE COMPRESSOR WASHED. HIGH POWER GROUND RUNS TO DRY OUT THE ENGINE PRODUCED NO SMOKE IN THE COCKPIT OR CABIN OR EVIDENCE OF FURTHER LEAKAGE.

Part: SHUTOFF VALVE — INOPERATIVE (FUEL SYSTEM) · airframe 15,948 hrs · 13,485 cycles

REFUEL PANEL INOP. NOT READING CORRECTLY. REFUEL SOV INOP. OPERATIONAL CHECK OF FUEL SYSTEM GOOD IAW AMM 28-00-00. THIS CLEARS DM 27692.

Part: CONTROL PANEL — MALFUNCTIONED (AILE/RUDDER TRIM)

RUDDER TRIM RUNAWAY WITH FULL DEFLECTION TO THE LT ON CLIMBOUT. REMOVED AND REPLACED AILERON RUDDER TRIM CONTROL PANEL IAW AMM. (A)

Part: CONTROL SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 4,280 hrs · 3,589 cycles

FLAP FAIL MESSAGE. INSPECTED PER AD 98-20-01. NO DEFECTS NOTED. RESET FLAPS PER MANUFACTURES FAULT ISOLATION MANUAL (FILM). OPERATIONALLY CHECKS GOOD.

Part: ELT — FAILED (CABIN)

ELT FAILS G-SWITCH TEST. REMOVED ELT FOR MAINTENANCE IAW FAR 91.207.