N176PQ

Part: LAMP — INOPERATIVE (ZONE 200) · airframe 36,729 hrs · 27,175 cycles

AFT RH EXTERIOR EMERGENCY LIGHT INOP RE-LAMPED AFT RH EXTERIOR EMERGENCY LIGHT IAW CRJ900 AMM 33-51-15 OPS CHECK GOOD.

Part: BRAKE — INOPERATIVE · airframe 36,317 hrs · 26,820 cycles

DESENDING THROUGH 10,000 FEET ON ARRIVAL, BRAKE OVHT WARNING MESSAGE SHOWED AT 200 KNOTS AND LOWERED GEAR. RAN QRH AND MESSAGE CLEARED. DEFERED RH OUTBOARD BRAKE TEMP INDICATION MEL 2-46-1D CAT C M PROCEDURE C/W MOC NOTIFIED 7821 PLACARD INSTALLE BACK DATE 23 JULY 2024 CARLOS BRAVO-STS LINE MAINT. R & R RT OTBD BRAKE IAW JC 900-32-730-901. OPS AND LEAK CHECK GOOD. MMO2 UPDATED. PLACARD REMOVED. ALL MX PROCEDURES COMPLIED IWTH.

Part: LIGHT — INOPERATIVE · airframe 32,199 hrs · 23,393 cycles

RHOB SIDE EMERGENCY LIGHT, THIRD FROM FWD INOP (RIGHT AFT O/W). REMOVED & REPLACED LAMP IAW AMM 33-51-15. OPS CHECK GOOD. P/N ON & OFF 8GH005123-06.

Part: LAMP — INOPERATIVE · airframe 32,199 hrs · 23,393 cycles

RHOB SIDE EMERGENCY LIGHT, THIRD FROM FWD INOP. REMOVED & REPLACED LAMP IAW AMM 33-51-15. OPS CHECK GOOD. P/N ON & OFF 8GH005123-06.

Part: SPLICE — CORRODED · airframe 32,067 hrs · 23,280 cycles

FS 280.00 TO FS 319, SPLICE ANGLE CORRODED. REMOVED & REPLACED SPLICE ANGLE IAW CRJ 900 SRM'S 51-40-11-001-001-A01, 51-42-13-001-001-A01 & 51-42-06-001-001-A01.

Part: STRINGER — CORRODED · airframe 32,067 hrs · 23,280 cycles

STRINGER SEGMENT AT 25R HAS MULTIPLE SPOTS OF CORROSION FROM FS 985 TO FS 1098. SPLICE REPAIRED STRINGER 25R IAW ENDEAVOR AIR EA CRJ953-13267.

Part: NONE — CORRODED · airframe 32,067 hrs · 23,280 cycles

FS 280.00 TO FS 319, FLOOR SILL CORRODED. REMOVED & REPLACED RH FLOOR SILL IAW CRJ 900 SRM'S 51-40-11-001-001-A01, 51-42-13-001-001-A01 & 51-42-06-001-001-A01.

Part: PISTON — CORRODED · airframe 32,067 hrs · 23,280 cycles

NLG PISTON/AXLE ASSY CORRODED BELOW PISTON CHROME. REPAIRED NLG PISTON/AXLE ASSY IAW MHIRJ REO 690-32-21-129 DATED 2022-05-16

Part: FRAME — CORRODED · airframe 32,067 hrs · 23,280 cycles

MULTIPLE AREAS OF CORROSION FOUND ON FRAME 379 FROM STR 20R TO STR 25R. REMOVED & REPLACED FRAME SECTOR IAW CRJ 900 SRM 51-40-11-001-001-A01, 51-42-21-001-001-A01 & 51-42-06-001-001-A01.

Part: FRAME — CORRODED · airframe 32,067 hrs · 23,280 cycles

FRAME FS 295 BETWEEN STGR 26L TO 27 IS CORRODED. REMOVED & REPLACED FRAME SECTOR IAW CRJ 900 SRM 53-00-06-201-006-A01.

Part: STRINGER — CORRODED · airframe 32,067 hrs · 23,280 cycles

STRINGER 21R BETWEEN FS 333 AND FS 280 IS CORRODED. REMOVED, FABRICATED & REPLACED STRINGER IAW ENDEAVOR AIR EA CRJ953-12976.

Part: ANGLE — CORRODED · airframe 32,067 hrs · 23,280 cycles

SERVICE DOOR LOWER INBD MOUNTING ANGLE CORRODED. REPLACED SERVICE DOOR LOWER INBD MOUNTING ANGLE PN SH670-31996-3 IAW CRJ 900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.

Part: ANGLE — CORRODED · airframe 32,067 hrs · 23,280 cycles

SERVICE DOOR LOWER INBD SILL ANGLE CORRODED. REPLACED SERVICE DOOR LOWER INBD SILL ANGLE PN SH670-31982-1 IAW CRJ 900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.

Part: JOINT — CORRODED · airframe 32,067 hrs · 23,280 cycles

WATER WASTE SERVICE DOOR SURROUND STRUCTURE JOINT AT FS 379 STGR 21R IS CORRODED. REPLACED JOINT IAW CRJ 900 SRM 51-40-11-001-001-A01.

Part: STRINGER — CORRODED · airframe 32,067 hrs · 23,280 cycles

FS295 TO FS333 STGR 24R IS CORRODED. REPLACED STGR 24R FS295 TO FS333 IAW ENDEAVOR AIR EA CRJ953-13308 REV IR DATED 4/23/2022

Part: STRINGER — CORRODED · airframe 32,067 hrs · 23,280 cycles

STRINGER 23R BETWEEN FS333 AND FS379 IS CORRODED. REPLACED STGR 23R BETWEEN FS333 AND FS379 IAW CRJ-900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.

Part: STRINGER — CORRODED · airframe 32,067 hrs · 23,280 cycles

FS333 TO FS349 STGR21R IS CORRODED. REPLACED STGR 21R BETWEEN FS333 AND FS349 IAW CRJ-900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.

Part: FRAME — CRACKED · airframe 32,067 hrs · 23,280 cycles

FS333 FRAME IS CRACKED BETWEEN STGR1R AND STGR2R. REPAIRED FS333 FRAME BETWEEN STGR1R AND 2R IAW ENDEAVOR AIR EA CRJ953-13368 REVIR DATED 4/13/2022.

Part: STRAP — CRACKED · airframe 32,067 hrs · 23,280 cycles

PANEL195DR FAIRING STRAP CRACKED REMOVED AND REPLACED STRAP AND MODIFIED AFT PANEL "C" CHANNEL ON PNL 195DR IAW CRJ-900 SRM 51-41-02-001-001-A01 AND ENDEAVOR AIR EO R53573 REV 2 DATED 22FEB18.

Part: RETAINER — CORRODED · airframe 32,067 hrs · 23,280 cycles

L/H SIDE SEAT RAIL STRUCTURE @ F.S.744.15 IS CORRODED/CRACKED. REMOVED DAMAGED L/H SIDE SEAT RAIL RETAINER AT F.S.744.15 AND INSTALLED NEW SERVICABLE SEAT RAIL RETAINER IAW CRJ 900 AMM 53-00-49-400-801-A07.

Part: SPLICE — CORRODED · airframe 32,067 hrs · 23,280 cycles

SPLICE AT FS333 AND STRINGER 23R IS CORRODED. REPLACED STGR 23R SPLICE AT FS333 IAW CRJ-900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01

Part: SEAT TRACK — CORRODED · airframe 32,067 hrs · 23,280 cycles

LBL9 FLOOR SEAT TRACK BETWEEN F.S.661+32 TO F.S.693 IS CORRODED. REMOVED CORRODED LBL9 SEAT TRACK FROM F.S.661+32 TO F.S.693 AND INSTALLED NEW SERVICABLE SEAT TRACK IAW CRJ 900 AMM 53-00-49-400-801-A07 AND SRM 53-00-49-201-002-A01.

Part: FRAME — CORRODED · airframe 32,067 hrs · 23,280 cycles

FS319 FRAME CORRODED BETWEEN STGR 24R AND STGR 25R. REPAIRED FS319 FRAME BETWEEN STGR 25L AND STGR 23R IAW CRJ-900 SRM 53-00-06-201-006-A01, 51-42-06-001-001-A01, 51-42-21-001-001-A01, AND 51-42-13-001-001-A01

Part: INTERCOSTAL — CORRODED · airframe 32,067 hrs · 23,280 cycles

INTERCOSTAL AT 20R BETWEEN FS349 AND FS364 IS CORRODED REPLACED INTERCOSTAL AT 20R BETWEEN FS349 AND FS364 IAW CRJ-900 SRM 51-42-06-001-001-A01.

Part: STRINGER — CORRODED · airframe 32,067 hrs · 23,280 cycles

FS333 TO FS349 STR24R IS CORRODED REPAIRED STR24R IAW CRJ SRM 51-21-06-001-001-A01 AND 53-00-03-201-001-A02

Part: SPLICE — CORRODED · airframe 32,067 hrs · 23,280 cycles

SPLICE AT FS333 AND STRINGER 22R IS CORRODED. REPLACED STGR 22R SPLICE AT FS333 IAW CRJ-900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01

Part: PANEL — CHAFED · airframe 32,067 hrs · 23,280 cycles

PANELS 684ET AND HT HAS CHAFFING DAMAGE. REPAIRED CHAFFING DAMAGE TO PANEL 684ET IAW CRJ 900 SRM 51-12-00-001-001-A01. REPLACED DAMAGED PANEL 684HT IAW CRJ 900 SRM 51-40-11-001-001-A01.

Part: STRINGER — CORRODED · airframe 32,067 hrs · 23,280 cycles

FS333 TO FS349 STGR 22R IS CORRODED. REPLACED STGR 22R BETWEEN FS333 AND FS349 IAW CRJ-900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.

Part: BEAM — CORRODED · airframe 32,067 hrs · 23,280 cycles

FLOOR BEAM AT LBL27,FS 969.00 - FS1051.00, IS CORRODED. CORRODED FLOOR BEAM REPAIRED I.A.W CRJ 900 SRM # 53-00-41-201-001-A03.

Part: INTERCOSTAL — CORRODED · airframe 32,067 hrs · 23,280 cycles

INTERCOSTAL BETWEEN F.S.865 TO F.S.881 AT STGR 21R IS CORRODED. REPAIRED INTERCOSTAL IAW ENDEAVOR AIR EA CRJ953-13249 REV B DATED 4-26-2022.

Part: MOUNT — CHAFED · airframe 32,067 hrs · 23,280 cycles

R/H ENGINE YOKE MOUNT IS CHAFED AT 2 LOCATIONS. REPAIRED R/H ENGINE YOKE IAW MHIRJ REO 690-71-21-041 REV -- DATED 2022-04-23 AND BOMBARDIER REO 670-71-21-057 EV -- DATED 2013-09-13.

Part: STRINGER — CORRODED · airframe 32,067 hrs · 23,280 cycles

F.S.349 TO F.S.409 STGR 19R IS CORRODED. REPAIRED FUSELAGE STRINGER 19R FROM F.S.349 TO F.S.409 IAW CRJ 900 SRM 53-00-03-201-001-A02.

Part: INTERCOSTAL — CORRODED · airframe 32,067 hrs · 23,280 cycles

INTERCOSTAL CORRODED AT FS645 BETWEEN STGR 25L AND STGR 26L. REPLACED INTERCOSTAL AT FS645 BETWEEN STGR 25L AND 26L IAW CRJ-900 SRM 51-42-06-001-001-A01,51-52-21-001-001-A01, 51-42-13-001-001-A01, 51-42-21-001-001-A01, AND 51-21-16-001-001-A01

Part: STRIKER — CORRODED · airframe 32,067 hrs · 23,280 cycles

SERVICE DOOR LWR SEAL STRIKER FASTENER HOLES CORRODED. REPLACED THE SERVICE DOOR LWR SEAL STRIIKER P/N SH670-31412-7 IAW CRJ-900 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01

Part: INTERCOSTAL — CORRODED · airframe 32,067 hrs · 23,280 cycles

INTERCOSTAL/ 601R318057-1/CORRODED/INTERCOSTAL/ 601R318057-1 INTERCOSTAL/ 601R318057-1/CORRODED

Part: WEB — CORRODED · airframe 32,067 hrs · 23,280 cycles

FWD WEB ON PAX DOOR HAS MULTIPLE SPOTS OF CORROSION. REMOVED AND REPLACED PAX DOOR FWD WEB P/N601R317071-12 IAW CRJ-900 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01.

Part: SKIN — CORRODED · airframe 32,067 hrs · 23,280 cycles

FWD INNER SKIN ON PAX DOOR HAS MULTIPLE SPOTS OF CORROSION. REMOVED AND REPLACED PAX DOOR INNER SKIN P/N 601R318024-15 IAW CRJ-900 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01.

Part: FORMER — CORRODED · airframe 32,067 hrs · 23,280 cycles

PAX DOOR AFT FORMER IS CORRODED PN 601R318034-5S. REMOVED AND REPLACED PAX DOOR AFT FORMER P/N 601R318034-5 IAW CRJ-900 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01.

Part: INTERCOSTAL — CORRODED · airframe 32,067 hrs · 23,280 cycles

PAX DOOR FWD INTERCOSTAL INTERCOSTAL DD5 IS CORRODED REMOVED AND REPLACED INTERCOSTAL DD5 P/N 601R318091-5 IAW CRJ-900 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01

Part: WEB — CORRODED · airframe 32,067 hrs · 23,280 cycles

PAX DOOR AFT WEB IS CORRODED AND CRACKED P/N 601R317071-11 REMOVED AND REPLACED PAX DOOR AFT WEB P/N601R317071-11 IAW CRJ-900 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01.

Part: FORMER — CORRODED · airframe 32,067 hrs · 23,280 cycles

PAX DOOR FWD FORMER HAS CORROSION REMOVED AND REPLACED PAX DOOR FWD FORMER P/N 601R318031-5 IAW CRJ-900 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, AND 51-42-21-001-001-A01

Part: ANGLE — CRACKED · airframe 32,067 hrs · 23,280 cycles

RH VERT STAB AFT DRAG ANGLE HAS POSSIBLE CRACK. REMOVED AND REPLACED RH VERT STAB DRAG ANGLE IAW CRJ-900 SRM 51-42-21-001-001-A01, 51-42-10-001-001-A01, AND 51-42-06-001-001-A01

Part: STRINGER — CORRODED · airframe 32,067 hrs · 23,280 cycles

STGR AT 26L HAS MULTIPLE SPOTS OF CORROSION FROM F.S.985 TO F.S.1098. REPAIRED STRINGER 26L F.S.985 TO F.S.1088.20 IAW ENDEAVOR AIR EA CRJ953-13263 REV -- DATED 4-6-2022.

Part: STRINGER — CORRODED · airframe 32,067 hrs · 23,280 cycles

F.S.295 TO F.S.310 STGR 19R IS CORRODED. REMOVED CORRODED STRINGER 19R FROM F.S.280 TO F.S.319.70 AND INSTALLED NEW SERVICABLE STRINGER IAW CRJ 900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.

Part: ANGLE — CRACKED · airframe 32,067 hrs · 23,280 cycles

L/H VERTICAL STABILIZER AFT DRAG ANGLE HAS POSSIBLE CRACK. REMOVED CRACKED L/H AFT DRAG ANGLE AND INSTALLED NEW SERVICABLE DRAG ANGLE IAW CRJ 900 SRM 51-42-10-001-001-A01, 51-42-21-001-001-A01 AND 51-42-22-001-001-A01.

Part: ANGLE — CORRODED · airframe 32,067 hrs · 23,280 cycles

PAX DOOR UPPER SILL ANGLE IS CORRODED. REMOVED CORRODED PAX DOOR SILL ANGLE AND INSTALLED NEW SERVICABLE SILL ANGLE P/N SH670-31821-5 IAW CRJ 900 SRM 51-41-02-001-001-A01 AND 51-42-06-001-001-A01.

Part: ANGLE — CORRODED · airframe 32,067 hrs · 23,280 cycles

PAX DOOR UPPER SILL ANGLE IS CORRODED. REMOVED CORRODED PAX DOOR SILL ANGLE AND INSTALLED NEW SERVICABLE SILL ANGLE P/N SH670-31821-6 IAW CRJ 900 SRM 51-41-02-001-001-A01 AND 51-42-06-001-001-A01.

Part: FRAME — CORRODED · airframe 32,067 hrs · 23,280 cycles

FRAME AT F.S.969 CORRODED IN MULTIPLE PLACES FROM STGR 21R TO 25R. REPAIRED FRAME AT F.S.969 BETWEEN STGR 21R TO 25R IAW CRJ 900 SRM 53-00-06-201-001-A03.

Part: ANGLE — CORRODED · airframe 32,067 hrs · 23,280 cycles

PAX DOOR LOWER SILL ANGLE IS CORRODED. REMOVED CORRODED PAX DOOR SILL ANGLES AND INSTALLED NEW SERVICABLE SILL ANGLE P/N SH670-31821-5S IAW CRJ 900 SRM 51-42-21-001-001-A01 AND 51-42-06-001-001-A01.

Part: ANGLE — CORRODED · airframe 32,067 hrs · 23,280 cycles

PAX DOOR LOWER SILL ANGLE IS CORRODED. REMOVED CORRODED PAX DOOR SILL ANGLES AND INSTALLED NEW SERVICABLE SILL ANGLE P/N SH670-31875-7S IAW CRJ 900 SRM 51-42-21-001-001-A01 AND 51-42-06-001-001-A01.

Part: ANGLE — CORRODED · airframe 32,067 hrs · 23,280 cycles

PAX DOOR UPPER SILL ANGLE IS CORRODED. REMOVED CORRODED PAX DOOR SILL ANGLE AND INSTALLED NEW SERVICABLE SILL ANGLE P/N SH670-31825-9 IAW CRJ 900 SRM 51-41-02-001-001-A01 AND 51-42-06-001-001-A01.

Part: ANGLE — CORRODED · airframe 32,067 hrs · 23,280 cycles

PAX DOOR LOWER SILL ANGLE IS CORRODED. REMOVED CORRODED PAX DOOR SILL ANGLES AND INSTALLED NEW SERVICABLE SILL ANGLE P/N SH670-31821-6S IAW CRJ 900 SRM 51-42-21-001-001-A01 AND 51-42-06-001-001-A01.

Part: ANGLE — CORRODED · airframe 32,067 hrs · 23,280 cycles

F.S.280 AVIONICS FLOOR BOARD SUPPORT ANGLE IS CORRODED. REMOVED CORRODED AVIONICS FLOOR BOARD SUPPORT ANGLE AT F.S.280 AND INSTALLED NEW SERVICABLE ANGLE IAW CRJ 900 SRM 51-42-21-001-001-A01 AND 51-42-06-001-001-A01.

Part: NONE — CORRODED · airframe 32,067 hrs · 23,280 cycles

R/H SIDE RAIL SEAT TRACK IS CORRODED BETWEEN F.S. 765.00+15 AND F.S. 847.00+16. REPLACED SIDE SEAT RAIL IAW CRJ 900 AMM 53-00-49-000/400-801-A07.

Part: PANEL — CHAFED · airframe 32,067 hrs · 23,280 cycles

CHAFING DAMAGE ON PANEL 684GB. FOUND CHAFING DAMAGE ON 684GB OUT OF LIMITS, REMOVED AND REPLACED PANEL IAW CRJ 900 SRM 51-40-11-001-001-A01.

Part: NONE — CORRODED · airframe 32,067 hrs · 23,280 cycles

RH SEAT SIDE RAIL IS CORRODED AT FS 708. REPLACED SIDE SEAT RAIL IAW CRJ 900 AMM 53-00-49-000/400-801-A07.

Part: WEB — CRACKED · airframe 32,067 hrs · 23,280 cycles

SERVICE DOOR LOWER WEB CRACKED AND REQUIRES REPLACEMENT. REMOVED AND REPLACED LOWER WEB,I.A.W. CRJ SRM 'S #51-40-11-001-001-A01, 51-42-21-001-001-A01, 51-42-06-001-001-A01,

Part: STRINGER — CORRODED · airframe 32,067 hrs · 23,280 cycles

STGR 22R BETWEEN FS 280 TO FS 310 IS CORRODED. REMOVED, FABRICATED & REPLACED STRINGER IAW ENDEAVOR AIR EA CRJ953-13450.

Part: STRINGER — CORRODED · airframe 32,067 hrs · 23,280 cycles

STGR 23R BTW FS280 TO FS310 IS CORRODED. REPLACED STRINGER 23R FS280-FS333 IAW CRJ-900 SRM 51-40-11-001-001-A01,51-42-06-001-001-A01, AND 51-42-21-001-001-A01

Part: NONE — CORRODED · airframe 32,067 hrs · 23,280 cycles

RBL 9 FLOOR SEAT TRACK IS CORRODED BETWEEN FS 581 TO FS 661+32 REPLACED SEAT TRACK IAW CRJ 900 AMM 53-00-49-000/400-801-A07.

Part: INTERCOSTAL — CORRODED · airframe 32,067 hrs · 23,280 cycles

F.S.310 - FS319, STRGR 20R, INTERCOSTAL, IS CORRODED. REMOVED AND REPLACED CORRODED INTERCOSTAL, FS310.00 - FS 319.00, IAW CRJ 900 SRM #51-40-11-001-001-A01,#51-42-06-001-001-A01 AND #51-42-21-001-001-A01.

Part: STRINGER — CORRODED · airframe 32,067 hrs · 23,280 cycles

F.S.295 TO F.S.310 STGR 20R IS CORRODED. REMOVED CORRODED STRINGER 20R FROM F.S.295 TO F.S.319.70 AND INSTALLED NEW SERVICABLE STRINGER IAW CRJ 900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 29,169 hrs · 20,755 cycles

FORWARD FACING CURVED EMERGENCY LIGHTS ON CEILING ABOVE EXIT ROWS INOPERATIVE. REMOVED AND REPLACED EPSU BATTERY PACK PS43 IAW AMM 33-51-17. OPS CHECKED GOOD.

Part: LIGHT — DIM (CABIN) · airframe 27,578 hrs · 19,469 cycles

RH AFT EMERGENCY WING LIGHT DIM. REPLACED EMERGENCY LIGHT IAW AMM 33-51-15. OPS CHECK GOOD

Part: PRINTER — ODOR (COCKPIT) · airframe 26,199 hrs · 18,409 cycles

SMELLED SMOKE FL280, RAN QRH, PRINTER SMELLED BURNT, PRINTER CIRCUIT BREAKER TRIPPED INFLIGHT. R&R ACARS PRINTER AND COMPLIED WITH OPS TEST IAW 23-22-05 AND FOUND NO DEFECTS AT THIS TIME.

Part: FRAME — CORRODED (FUSELAGE) · airframe 25,294 hrs · 17,752 cycles

INITIAL INSPECTION. CORROSION ON FRAME FS 349 BTW STR 25L-25R. AT MAIN AVIONIC COMPARTMENT.(SM)(E/E)(TCI100-09). COMPLETE: SUMMARY: NRC 00223: CORROSION LEVEL 2 ON FRAME FS 349 BTW STR 25L-25R AT MAIN AVIONIC COMPARTMENT WAS REPAIRED PER REO. 6 70-53-21-1281 REV.--

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 25,294 hrs · 17,752 cycles

INITIAL INSPECTION; CORROSION ON FLOOR STRUCTURE AROUND HEXAGONAL FASTTENERS FS 1031 AT AFT CARGO COMPARTMENT (CCT) (TCI 100-15) COMPLETE: SUMMARY: FLOOR STRUCTURE AROUND HEXAGONAL FASTENERS FS 1031 LBL-27, LBL9, RBL9 AT AFT CARGO COMPARTMENT WERE REPAIRED PER REO 670-53-00-029 REV-A, REO 690-53-61-785.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 25,294 hrs · 17,752 cycles

INITIAL INSPECTION. CORROSION ON STRINGER 26L AND 26R FROM FS 339-364 AT MAIN AVIONICS COMPARTMENT.(SM)(E/E)(TCI 100-09) COMPLETE: SUMMARY: STRINGERS 26L AND 26R WERE PER REPLACE PER SRM 53-21-03-001-002-A01 AND 51-42-06-001-001-A01.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 25,294 hrs · 17,752 cycles

INITIAL INSPECTION. CORROSION ON STRINGER 27 FROM FS 280-297 AND 308-339 AT MAIN AVIONICS COMPARTMENT.(SM)(E/E)(TCI 100-09). COMPLETE: STRINGER 27 FROM FS = 280 - 297 AND 308 - 339 WERE REPLACED PER SRM 51-42-06-001-001-A01 AND 51-42-20-001-001-A01.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 25,294 hrs · 17,752 cycles

INITIAL INSPECTION. CORROSION ON STRINGER 26R FROM FS 280-339 AT MAIN AVIONICS COMPARTMENT.(SM)(E/E)(TCI 100-09). COMPLETE: SUMMARY: STRINGER 26R FROM FS = 280 - 339 DUE TO EXCCESIVE CORROSION IS OUT OF LIMIT OF ALLOWABLE DAMAGE PER SRM 53-21-03-101-002-A04 AND WAS REPLACED PER SRM 51-42-06-001-001-A01 AND 51-42-20-001-001-A01.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 25,294 hrs · 17,752 cycles

INITIAL INSPECTION. CORROSION ON STRINGER 25L FROM FS 280-339 AT MAIN AVIONICS COMPARTMENT.(SM)(E/E)(TCI 100-09). COMPLETE: SUMMARY: STRINGER 25L FROM FS= 280 - 339 DUE TO EXCCESIVE CORROSION IS OUT OF LIMIT OF ALLOWABLE DAMAGE PER SRM 53-21-03-101-002-A04 AND WAS REPLACED PER SRM 51-42-06-001-001-A01 AND 51-42-20-001-001-A01.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 25,294 hrs · 17,752 cycles

INITIAL INSPECTION. CORROSION ON STRINGER 25R FROM FS 280-339 AT MAIN AVIONICS COMPARTMENT.(SM)(E/E)(TCI 100-09). COMPLETE: SUMMARY: STRINGER WAS REPLACED PER SRM 51-42-06-001-001-A01 AND 51-42-20-001-001-A01.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 25,294 hrs · 17,752 cycles

INITIAL INSPECTION. CORROSION ON STRINGER SPLICE (5EAS) BTW FS 329-339 AND STR 25L-25R AT MAIN AVIONICS COMPARTMENT.(SM)(E/E)(TCI 100-09) COMPLETE: SUMMARY: NEW JOINT PIECE STRINGER (5EA) WERE INSTALLED PER SRM 51-42-06-001-001-A01 AND 51-42-20-001-001-A01. LEVEL CORROSION 2.

Part: FRAME — CORRODED (FUSELAGE) · airframe 25,294 hrs · 17,752 cycles

INITIAL INSPECTION. CORROSION ON FRAME INCLUDING PREVIOUS REPAIR ON FS 295 BTW STR 25L-25R AT MAIN AVIONIC COMPARTMENT.(SM)(E/E)(TCI 100-09). COMPLETE: SUMMARY OF NRC 00224: CORROSION LEVEL 2 ON FRAME INCLUDING PREVIOUS REPAIR ON FS 295 BTW STR 25L-25R AT MAIN AVIONIC COMPARTMENT WAS REPAIRED PER REO NUMBER 670-53-21-1281. REV.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 25,294 hrs · 17,752 cycles

INITIAL INSPECTION. CORROSION ON STRINGER 26L FROM FS 280-339 AT MAIN AVIONICS COMPARTMENT.(SM)(E/E)(TCI 100-09). COMPLETE: SUMMARY: DUE TO EXCCESIVE CORROSION STRINGER 26L FROM FS = 280 - 339 IS OUT OF LIMIT OF ALLOWABLE DAMAGE PER SRM 53-21-03-101-002-A04 AND WAS REPLACED PER SRM 51-42-06-001-001-A01 AND 51-42-20-001-001-A01.

Part: FRAME — CORRODED (FUSELAGE) · airframe 25,294 hrs · 17,752 cycles

INITIAL INSPECTION. CORROSION ON FRAME INCLUDING PREVIOUS REPAIR ON FS 333 BTW STR 25L-25R AT MAIN AVIONIC COMPARTMENT.(SM)(E/E)(TCI 100-09). COMPLETE: SUMMARY OF NRC 00227: CORROSION LEVEL 2 ON FRAME INCLUDING PREVIOUS REPAIR ON FS 333 BTW STR 25L-25R AT MAIN AVIONIC COMPARTMENT WAS REPAIRED PER REO NUMBER 670-53-21-1281. REV. --

Part: SKIN — PUNCTURED (FUSELAGE) · airframe 25,294 hrs · 17,752 cycles

DAMAGE T : DURING DRILLING WAS PERFORM A PUNCTURE ON EXTERNAL FUSELAGE SKIN STA FS355 AND STGR 26R (FUS) COMPLETE: FUSELAGE SKIN WAS REPAIRED PER EA CRJ953-07745 REV. IR.

Part: FRAME — CORRODED (FUSELAGE) · airframe 25,294 hrs · 17,752 cycles

INITIAL INSPECTION. CORROSION ON FRAME INCLUDING PREVIOUS REPAIR ON FS 310 BTW STR 25L-25R AT MAIN AVIONIC COMPARTMENT.(SM)(E/E)(TCI 100-09). COMPLETE: SUMMARY OF NRC 00225: CORROSION LEVEL 2 ON FRAME INCLUDING PREVIOUS REPAIR ON FS 310 BTW STR 25L-25R AT MAIN AVIONIC COMPARTMENT WAS REPAIRED PER REO NUMBER 670-53-21-1281. REV. --

Part: FRAME — CORRODED (FUSELAGE) · airframe 25,294 hrs · 17,752 cycles

INITIAL INSPECTION. CORROSION ON FRAME INCLUDING PREVIOUS REPAIR ON FS 319 BTW STR 25L-25R AT MAIN AVIONIC COMPARTMENT.(SM)(E/E)(TCI 100-09). COMPLETE: SUMMARY OF NRC 000226: CORROSION LEVEL 2 ON FRAME INCLUDING PREVIOUS REPAIR ON FS 319 BTW STR 25L-25R AT MAIN AVIONIC COMPARTMENT WAS REPAIRED PER REO NUMBER 670-53-21-1281. REV. --

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 25,294 hrs · 17,752 cycles

INITIAL INSPECTION: CORROSION ON SIDE SEAT RAILS IN SECTIONS [ FS= 572 TO FS= 661+16, PROJECTION STR 15L ] [ FS= 572 TO FS= 661+16, PROJECTION STR 15R ] [ FS= 661+16 TO FS= 661+90, PROJECTION STR 15L ] [ FS= 661+16 TO 672, PROJECTION STR 15R ] AT PAX CABIN. (CPAX) (TCI: 53 COMPLETE: SUMMARY OF NRC 00135 LEVEL CORROSION 2 : NEW SEAT SEAT RAILS IN SECTIONS [ FS= 572 TO FS= 661+16, PROJECTION STR 15L ] [ FS= 572 TO FS= 661+16, PROJECTION STR 15R ] [ FS= 661+16 TO FS= 661+90, PROJECTION STR 15L ] [ FS= 661+16 TO 672, PROJECTION STR 15R ] AT PAX CABIN WERE REPLACED PER SRM 51-41-02 AND AMM 53-00-49-400-801 PAR 4 (A) (B).

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 25,294 hrs · 17,752 cycles

INITIAL INSPECTION: CORROSION ON FLOOR SEAT RAILS IN SECTIONS [ FS= 349 TO FS= 485, 9RBL ] [ FS= 485 TO FS= 581, 27LBL/9RBL ] [ FS= 581 TO 661+32, 9LBL/9RBL ] [ FS= 661+32 TO FS= 693, 9LBL/9RBL ] AT PAX CABIN. (CPAX) (TCI: 53-20-243) COMPLETE: SUMMARY OF NCR 00118: LEVEL CORROSION 2, NEW FLOOR SEAT RAILS IN SECTIONS FS 349 TO FS=485 9RBL, FS=485 TO FS=581 27LBL/ 9RBL, FS= 581 TO 661+32, 9LBL/9RBL AND FS= 661+32 TO FS= 693, 9LBL/9RBL AT PAX CABIN. WERE REPLACED PER. SRM 51-41-02 AND AMM 53-00-49-400-801 PAR. 4 (A) (B).

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 25,294 hrs · 17,752 cycles

INITIAL INSPECTION: CORROSION ON SIDE SEAT RAILS IN SECTIONS [ FS= 677 TO FS= 720, PROJECTION STGR 15L ] [ FS= 744 TO FS= 761, PROJECTION STR 15R ] [ FS= 785 TO 847+16, PROJECTION STGR 15L ] [ FS= 847+16 TO FS= 906, PROJECTION STGR 15L ] AT PAX CABIN. (CPAX) (TCI: 53-20-233) COMPLETE: SUMMARY: SUMMARY OF NRC 00122: NEW SEAT RAILS IN SECTIONS [FS= 677 TO FS= 720, PROJECTION STGR 15L ] [ FS= 744 TO FS= 761, PROJECTION STGR 15R] [FS= 785 TO 847+16, PROJECTION STGR 15L] AT PAX CABIN WERE REPLACED PER SRM 51-41-02 AND AMM 53-00-49-400-801-PAR.(A)(B).

Part: CANISTER — CRACKED (LT WING) · airframe 25,294 hrs · 17,752 cycles

INITIAL INSPECTION : CRACK IN CANISTER, WELDED NO.3 IN STA. WS=148 AT LT MAIN FUEL TANK. (AI) COMPLETE: CANISTER WAS REPAIRED PER REO 670-57-42-577 REV.-- AND SRM 51-41-21.

Part: CANISTER — CRACKED (RT WING) · airframe 25,294 hrs · 17,752 cycles

INITIAL INSPECTION : CRACK IN CANISTER, WELDED NO.3 IN STA WS148 AT RT MAIN FUEL TANK. (AD) COMPLETE: SUMMARY OF NRC 00182:CANISTER WAS REPAIRED PER REO 670-57-42-577 REV. AND SRM 51-41-21.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 25,294 hrs · 17,752 cycles

INITIAL INSPECTION: CORROSION ON FLOOR SEAT RAILS IN SECTIONS [FS= 693 TO FS= 830, 9LBL/9RBL ] [ FS= 830 TO FS= 849, 9LBL/9RBL ] [ FS= 849 TO 977, 9LBL/9RBL ] AT PAX CABIN. (CPAX) (TCI: 100-20) COMPLETE: SUMMARY: SEAT RAILS ON STA FS= 693 TO FS= 830, 9LBL/9RBL ] [ FS= 830 TO FS= 849, 9LBL/9RBL ] [ FS= 849 TO 977, 9LBL/9RBL WERE REPLACED PER. SRM 51-41-02 AND AMM 53-00-49-400-801 PAR.4 (A) (B).

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 25,181 hrs · 17,676 cycles

LEFT & RIGHT FORWARD DOOR EMERGENCY LIGHTS WERE NOT WORKING. R & R THE NR 5 EMERGENCY LIGHT CHARGER, AND POWER SUPPLY ASSY IAW AMM 33-51-17. OPS CHECKED GOOD.

Part: COOLING FAN — ODOR (CABIN) · airframe 24,989 hrs · 17,533 cycles

DISPLAY COOLING FAN CAUSES INTERMITENT SQUEEKING SOUND WHILE IN FLIGHT ALSO LIGHT BURNING SMELL NOTED. R&R NR 1 DISPLAY COOL FAN IAW AMM 21-24-00. OPS CK GOOD. PN OFF/ON AE0804A04 S/N OFF 01133 S/N ON 0108.

Part: LIFE VEST — MISSING (CABIN) · airframe 24,816 hrs · 17,400 cycles

LIFE VEST MISSING 12C. INSTALLED LIFE VEST IAW AMM 25-61-03 AS REQUIRED.

Part: OXYGEN MASK — DAMAGED (LAVATORY) · airframe 24,569 hrs · 17,219 cycles

OXYGEN MASK HOSE IS DAMAGED DUE TO KINKING IN FWD LAV. REMOVED AND REPLACED DAMAGED OXYGEN MASK IN FWD LAVATORY PER AMM 35-21-09. PN ON/OFF: 289-301-066-2 SN ON/OFF: NSN

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 24,569 hrs · 17,219 cycles

FLOOR LEVEL EXIT SIGNS HAVE A FEW BURNT OUT. BULBS REPLACED ALL BURNED OUT LAMPS AND OPS CHECKS GOOD IAW AMM 33-51-00.

Part: OXYGEN MASK — DAMAGED (CABIN) · airframe 24,569 hrs · 17,219 cycles

HOSE TO BOTH FWD FA O2 MASKS ARE DAMAGED DUE TO KINKING. INSTALLED 2 OXYGEN MASKS ASSY PN 289-601-066-2 AT FWD FLIGHT ATTENDANT POSITION IAW AMM 35-21-09.

Part: STRUT — DEFLATED (NLG) · airframe 23,765 hrs · 16,645 cycles

AFTER TAKEOFF, A STEERING INOPERATIVE CAUTION MESSAGE DISPLAYED. A VIBRATION FELT IN NOSE. AFTER APPROXIMATELY 20 SECONDS, A GEAR DISAGREE WARNING MESSAGE. FOLLOWED QRH. VIBRATION FELT UNTIL GEAR HANDLE WAS PUT DOWN & HYD PUMP 3B TURNED ON VIA QRH CHECKLIST. NOSE GEAR CONTINUED TO CYCLE, MAINS CYCLED BETWEEN UP AND TRANSITION, NOSE GEAR NEVER RETRACTED. NOTED NLG STRUT FLAT, SERVICED NLG STRUT IAW 900-12-710-700. THE MLG EXTENDED FOUR TIMES IAW 32-30-00. OPS OK.

Part: LIGHT — MALFUNCTIONED (MAIN CABIN) · airframe 23,358 hrs · 16,354 cycles

EMERGENCY LIGHT INOPERATIVE. FORWARD CABIN LIGHTS COME ON MOMENTARILY,THEN GO OUT. AFT CABIN LIGHT STAY ON. PERFORMED OPS CHECK OF THE EMERGENCY LIGHTS IAW AMM 33-51-00. OPS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (FLASHLIGHT) · airframe 23,311 hrs · 16,322 cycles

MX NOTED DURING WAKE-UP CHECKLIST THE FIRST OFFICER`S FLASHLIGHT BATTERY DISCHARGED. REMOVED AND REPLACED THE FLASHLIGHT BATTERY IAW AMM 25-61-02. OPS TESTED GOOD IAW AMM 25-61-00.

Part: MOUNT BRACKET — CRACKED (CARGO DOOR) · airframe 23,294 hrs · 16,303 cycles

AFT CARGO DOOR FWD DOOR TRACK CENTER MOUNT BRACKET CRACKED. REMOVED & REPLACED NE BRACKET AT AFT CARGO DOOR FWD DOOR TRACK. CENTER MOUNT TREATED AND TOP COAT, IAW SRM 53-61-58 PG 6 ITEM 8, SRM 51-21-11 + SRM 51-42-06.

Part: ENGINE — VIBRATION (LEFT) · airframe 21,800 hrs · 15,231 cycles

ON T/O LEFT ENGINE VIBE AT 2.1 - RETURN TO ATL. REMOVED BLADES, PINS AND BUMPERS. PERFORMED GENERAL VISUAL INSPECTION OF FAN BLADES. RE-MAPPED FAN BLADES, LUBRICATED RETAINING PINS, INSTALLED FAN BLADES, PERFORMED CHECK OF THE ENGINE N1 VIBRATION LEVEL IAW TASK CARD TSWS CF34-8 FAN VIBE. AIRCRAFT RETURNED TO SERVICE. THIS WAS AN AIR RETURN.

Part: SKIN — DAMAGED (BS 1031-1051) · airframe 20,709 hrs · 14,457 cycles

FUSELAGE DAMAGE BETWEEN BS 1031 AND 1051 BETWEEN STRINGERS 21 - 27R. BLENDED IAW SRM 51-12-00 AND FOUND TO BE OUT OF LIMITS IAW SRM 53-61-01. T MAJOR REPAIR IAW GMM 5-3.

Part: SMOKE DETECTOR — FALSE INDICATION (LAVATORY) · airframe 19,493 hrs · 13,583 cycles

FWD LAV SMOKE WARNING MSG IN FLIGHT. COMPLIED WITH QRH NO SMOKE DETECTED. R & R FWD LAV SMOKE DETECTOR IAW AMM 26-16-01. OPS TEST GOOD AT THIS TIME.

Part: SMOKE DETECTOR — FALSE INDICATION (LAVATORY) · airframe 19,412 hrs · 13,523 cycles

SMOKE FWD LAV MESSAGE DURING FLIGHT, ENROUTE. ACFT DIVERTED DUE TO MAINTENANCE, LAVATORY SMOKE DETECTION SYSTEM. PERFORMED OPS CK OF FWD LAV SMOKE DETECTOR IAW AMM 26-16-00. OPS CHECKED GOOD. COULD NOT DUPLICATE.

Part: DOOR FRAME — CHAFED (LT NLG DOOR) · airframe 19,374 hrs · 13,486 cycles

LEFT NLG DOOR BONDING WIRE HAS CHAFED INTO THE FRAME. BLENDED DAMAGE TO AIRFRAME IAW SRM 51-12-00. RECEIVED AND COMPLIED WITH STS EA 20-2016-006 . REPAIR IS PERMANENT AND CLASSIFIED AS MINOR.

Part: LIGHT — MISSING (CABIN) · airframe 18,597 hrs · 12,918 cycles

EMERGENCY LIGHT STRIP BY GALLEY 3 CART MISSING. INSTALLED EMERGENCY LIGHT IAW AMM IAW 33-51-01.

Part: DOOR SILL — CORRODED (SERVICE DOORWAY) · airframe 17,663 hrs · 12,240 cycles

CORROSION ON SERVICE DOOR LOWER SILL ANGLE, BELOW CAP ANGLE. REMOVED THE GALLEY DOOR FLOOR PROTECTOR MOUNTING ANGLE IAW SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. INSTALLED NEW LOWER SILL ANGLE AT SERVICE DOOR IAW SRM 51-42-06-001-001-A01.

Part: FLOORBEAM — CRACKED (COCKPIT) · airframe 17,663 hrs · 12,240 cycles

RIGHT COCKPIT FLOORBEAM IS CRACKED. RECEIVED REO 690-53-11-752 FORMED AND HEAT TREATED REPAIR ANGLE -2 IAW SRM 51-24-06-001-001-A01. FORMED AND HEAT TREATED ANGLE -8 IAW SRM 51-24-06-001-001-A01. COMPLIED WITH REO 690-53-11-752. COMPLIED WITH ECTC REO 690-53-11-752.

Part: FLOORBEAM — CRACKED (COCKPIT) · airframe 17,663 hrs · 12,240 cycles

LEFT COCKPIT FLOORBEAM IS CRACKED. RECEIVED REO 690-53-11-752 FORMED AND AND HEAT TREATED REPAIR ANGLE -1 IAW SRM 51-24-06-001-001-A01. FORMED AND HEAT TREATED ANGLE -7 IAW SRM 51-24-06-001-001-A01. COMPLIED WITH REO 690-53-11-752. COMPLIED WITH ECTC REO 690-53-11-752.

Part: SKIN — DENTED (RUDDER) · airframe 17,663 hrs · 12,240 cycles

RUDDER DENTED ON LOWER RT SIDE BETWEEN RIB'S 3 & 4. COMPLIED WITH APPLICABLE REPAIR IAW SRM 51-41-01-201-001-A01. FOUND HINGE LINE WEIGHT ROTATIONAL INERTIA INCREASE TO BE WITHIN LIMTS. = 432.18 LBF TECH: 570634, DATE: 4-17-15. RECEIVED EC/TC AND COMPLIED WITH EC/TC EC/TC EO 980-55-0005. REPAIR RUDDER SKIN LT SIDE & LT SIDE & RT SL SRM 55-41-01-201001 AS WRITTEN, DATE: 5/2/15. MAJOR REPAIR.

Part: BULKHEAD WEB — CORRODED (BS 280) · airframe 17,663 hrs · 12,240 cycles

LEFT 280 WEB CORRODED. COMPLIED WITH ECTC REO 670-53-11-59401 AND GREO 670-53-11-594, REV-- .

Part: LENS — CRACKED (EMERGENCY LIGHT) · airframe 17,663 hrs · 12,240 cycles

PANEL 262NRW EMERGENCY EXIT LIGHT LENS CRACKED. REMOVED CRACKED EMERGENCY EXIT LIGHT LENS. REPLACED EMERGENCY EXIT LIGHT LENS IAW AMM 33-51-05-05-400-801-A13 4L, 4.

Part: ATTACH ANGLE — CRACKED (BS 280) · airframe 17,663 hrs · 12,240 cycles

RT LOWER 280 WEB ATTACH ANGLE AT BL26.00 IS CRACKED. REMOVED RT LOWER 280 WEB ATTACH ANGLE AT RBL 26 IAW SRM 51-42-06-001-001-A01. INSTALLED RT LOWER 280 WEB ATTACH ANGLE AT RBL 26 IAW SRM 51-42-06-001-001-A01.

Part: BULKHEAD WEB — CORRODED (BS 280) · airframe 17,663 hrs · 12,240 cycles

RIGHT 280 WEB CORRODED. COMPLIED WITH ECTC REO 670-53-11-59401 AND GREO 670-53-11-594, REV--.

Part: SKIN — DAMAGED (RUDDER) · airframe 17,664 hrs · 12,241 cycles

RUDDER T/E MADE CONTACT WITH TAIL STAND PULL OUT SLIDER. COMPLIED WITH SRM 51-41-01-201-001-A01 RUDDER REPAIR TOTAL HINGE LINE ROTATIONAL INERTIA IS 167.04, REPAIR WEIGHT .450, REMOVED WEIGHT .160, HINGE LINE IS 24". RECEIVED EC/TC EO 900-55-0005 & COMPLIED WITH EC/TC EO 900-55-0005, REPAIR RUDDER SKIN LT SIDE & RT SIDE, SRM 55-41-01-201-001, AS WRITTEN.

Part: SEAT TRACK — CORRODED (BS 720) · airframe 17,658 hrs · 12,237 cycles

RIGHT SIDE SEAT RAIL IS CORRODED AT FS 720.85. BLENDED CORROSION AT FS 720.85 IAW SRM 51-21-06-001-001-A01 & REO 670-53-00-013 ON SIDE SEAT RAIL RT. REMOVED RT SIDE RAIL AT FS 720.85 IAW AMM 53-00-49-000-801, CONFIG A07. INSTALLED NEW SEAT RAIL RT STA 672.0 TO 722.0 IAW AMM 53-00-49-400-801-A07.

Part: SKIN — DENTED (BS 581-597) · airframe 17,664 hrs · 12,241 cycles

SKIN DENTED BETWEEN BS 581-597, STRINGERS 16 & 17. COMPLIED WITH EA 32-2015-149. RECEIVED EC/TC EA 32-2015-149 AND COMPLIED WITH EC/TC EA 32-2015-149.

Part: SEAT TRACK — CORRODED (BS 785) · airframe 17,658 hrs · 12,237 cycles

RT SIDE SEAT RAIL IS CORRODED AT FS 785.15. REMOVED RT SIDE SEAT RAIL AT FS 785.15 IAW AMM 53-00-49-000-801-A07. INSTALLED NEW SEAT RAIL RT STA 784 TO 847.+16 IAW AMM 53-00-49-400-801-A07.

Part: SEAT TRACK — CORRODED (BS 744) · airframe 17,658 hrs · 12,237 cycles

LEFT SIDE SEAT RAIL IS CORRODED AT FS 744.15. REMOVED LT SIDE SEAT RAIL AT FS 744.15 IAW AMM 53-00-49-000-801-A07. INSTALLED NEW LT SEAT RAIL, STA 744.15 TO 761.85 IAW AMM 53-11-49-400-801-A07.

Part: SEAT TRACK — CORRODED (BS 785) · airframe 17,658 hrs · 12,237 cycles

LT SIDE SEAT RAIL IS CORRODED AT FS 785.15. REMOVED LT SIDE SEAT RAIL FS 785.15 IAW AMM 53-00-49-000-801-A07. INSTALLED NEW SEAT RAIL LT STA 784.0 TO 847+16 IAW AMM 53-00-49-400-801-A07.

Part: SEAT TRACK — CORRODED (BS 744) · airframe 17,658 hrs · 12,237 cycles

RIGHT SIDE SEAT RAIL IS CORRODED AT FS 744.15. REMOVED RT SIDE SEAT RAIL AT FS 744.15 IAW AMM 53-00-49-000-801-A07. INSTALLED NEW SEAT RAIL RT STA 744.15 TO 761.85 IAW AMM 53-00-49-400-801-A07.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 17,651 hrs · 12,230 cycles

RT 280, SHEAR BOX BEAM CORRODED. UPON INCORPORATION OF SB 670BA-53-041, SHEAR BOX BEAM, LONGITUDINAL BEAM CAP & FASTENERS REPLACED.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 17,651 hrs · 12,230 cycles

RT 280 CROSSBEAM CORRODED IN MULTIPLE AREAS. UPON REMOVAL OF DRIP TRAY FOR INCORPORATIONS OF SB 670BA-53-041 BEAM WAS FOUND TO ALSO BE CRACKED AT RBL12. R & R RT BEAM IAW SRM 51-42-10-001-001-A01 & 51-42-06-001-001-A01 AND DWG CC670-34010. REMOVED INTERCOSTAL AT RBL38.5 IAW SB670BA-53-041-03. INSTALLED INTERCOSTAL AT RBL 38.5 IAW SB670BA-53-041 03 & SRM 51-42-16-001-A01. REMOVED INTERCOSTAL AT RBL 26 IAW SB670BA-53-041 03. INSTALLED INTERCOSTAL AT RBL26 IAW SB670BA-53-041-03, SRM 51-42-16-001-A01.

Part: INTERCOSTAL — CORRODED (BS 349-364) · airframe 17,651 hrs · 12,230 cycles

INTERCOSTAL CORRODED BETWEEN FS 349 AND FS 364 AT STR 27L. REMOVED CORROSION FROM INTERCOSTAL STR 27L, FS 349 TO 364 IAW SRM 51-21-06-001-001-A01. FOUND TO BE OUT OF ALLOWABLE LIMITS IAW SRM 53-21-23-101-003-A01. RESTORED TO ORIGINAL DWG FINISH IAW SRM 51-21-06-001-001-A01 AND CIC 51-21-11-001-001-A01 AND COMPLIED WITH REPAIR IAW EA 32-2015-142.

Part: FLOOR SUPPORT — CRACKED (CABIN) · airframe 17,651 hrs · 12,230 cycles

FLOOR SILL CRACKED UNDER ADG HYD PUMP. COMPLIED WITH EC TC REO 670-53-11-509 AND GRO 670-53-11-509, REV B, DATED 1/28/14.

Part: STEP — CORRODED (PAX DOOR) · airframe 17,651 hrs · 12,230 cycles

PAX DOOR HAS CORROSION AT BASE OF FIRST STEP. REMOVED CORROSION ON PAX DOOR BASE OF FIRST STEP, INNER SKIN IAW SRM 51-21-06-001-001-A01 AND 51-12-00-001-001-A01. COMPLIED WITH EA 32-2015-154 SECTION 1, PERMANENT REPAIR. RECEIVED ECTC EA 32-2015-154 AND COMPLIED WITH ECTC EA 32-2016-154.

Part: FRAME — CORRODED (BS 310) · airframe 17,651 hrs · 12,230 cycles

FS310 AT STR 25RT IS CORRODED. REMOVED CORROSION FROM FRAME STA 295, STR 25R IAW SRM 51-21-06-001-001-A01. BLEND AREA IS OUT OF LIMITS IAW SRM 53-21-06-101-002-A02, DAMAGE IS ON 2 ELEMENTS IAW NOTE 1. COMPLIED WITH EA 32-2015-148. RECEIVED EC/TC EA 32-2015-148 AND COMPLIED WITH EC/TC EA 32-2015-148.

Part: SEAT TRACK — CORRODED (BS 349-485) · airframe 17,658 hrs · 12,237 cycles

FLOOR SEAT RAIL SEGMENT FROM FS 349 TO FS 485 AT RBL 9 IS CORRODED OUT OF LIMITS. R & R SEAT RAIL IAW AMM 53-00-49-000-801-A07, AND 53-00-49-400-801-A07.

Part: STRUCTURE — CORRODED (BS 349) · airframe 17,658 hrs · 12,237 cycles

PACKER CORRODED AT FS 349 AND RBL 9. REMOVED CORRODED PACKER AND INSTALLED 1 EA NEW SERVICEABLE PACKER IAW SRM 51-42-06-001-001 AND DWG SH670-32120.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 17,651 hrs · 12,230 cycles

AFT FLIGHT DECK FLOOR SUPPORT BEAM IS CORRODED IN MULIPLE AREAS. REMOVED FLIGHT DECK FLOOR SUPPORT AND WAS FOUND TO BE OUT OF LIMITS IAW SRM 53-11-10-991-804. R & R FLIGHT DECK FLOR SUPPORT BEAM IAW SRM 51-42-06-001-001, CC670-34095.

Part: DOOR SILL — CORRODED (BS 310) · airframe 17,658 hrs · 12,237 cycles

CORROSION ON SERVICE DOOR SILL CAP ANGLE AT FS 310. REMOVED CORROSION ON SERVICE DOOR SILL & DAMAGE AT FS 310-333 IAW SRM 51-21-001-001-A01 & 51-12-00-001-001-A1. INSTALLED NEW SERVICEABLE SERVICE DOOR SILL CAP ANGLE WHEN RECEIVED. INSTALLED NEW SERVICE DOOR CAP ANGLE IAW SRM 51-42-06-001-01-A01, 51-42-21-001-001-A01.

Part: SEAT TRACK — CORRODED (BS 370-485) · airframe 17,658 hrs · 12,237 cycles

FLOOR SEAT RAIL SEGMENT FROM APPROXIMATELY FS 370 TO FS 485 AT LBL 9 IS CORRODED AT FS 370. REMOVED CORROSION FROM SEAT RAIL LBL 9.0, STA 370.0 OUT OF LIMITS IAW SRM 53-21-49-991-804, SHTS 1-3. R & R SEAT RAIL LBL9.0, FS370 TO 485 IAW AMM 53-00-49-000-801-A07 AND 53-00-49-400-801-A07.

Part: FLOOR SUPPORT — CRACKED (BS 280-319) · airframe 17,651 hrs · 12,230 cycles

RT FLOOR SILL AT FS 280- FS 319 CORRODED IN MULTIPLE AREAS. REMOVED FASTENER FROM RT FLOOR SILL STA 280-319 IAW SRM 51-42-06-001-001-A01. REMOVED AND DRILLED NEW FLOOR SILL STA 280-319 RT IAW SRM 51-42-06-001-001-A01. INSTALLED NEW FLOOR SILL, RT STA 280-319 IAW SRM 51-42-06-001-001-A01.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 17,651 hrs · 12,230 cycles

LT 280 CROSSBEAM CORRODED IN MULTIPLE AREAS. UPON REMOVAL OF DRIP TRAY FOR INCORPORATION OF SB 670BA-53-041 BEAM WAS FOUND TO ALSO BE CRACKED AT LBL 12. R & R LT BEAM IAW SRM 51-42-10-001-001-A01 & 51-42-06-001-001-A01 AND DWG CC670-34010. REMOVED INTERCOSTAL AT LBL 38.5 IAW SB 670BA-53-041-03. INSTALLED INTERCOSTAL AT LBL 38.5 IAW SB670BA-53-041 03 & SRM 51-42-16-001-001-A01. REMOVED INTERCOSTAL AT LBL 26 IAW SB670BA-53-041-03. INSTALLED INTERCOSTAL AT LBL 26 IAW SB670BA-53041-03 & SRM 51-42-16-001-001-A01.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 17,651 hrs · 12,230 cycles

LT 280 SHEAR BOX BEAM CORRODED. UPON INCORPORATION OF SB 670BA-53-041, SHEAR BOX BEAM. LONGITUDINAL BEAM CAP & FASTENERS REPLACED.

Part: INTERCOSTAL — CORRODED (BS 349-364) · airframe 17,651 hrs · 12,230 cycles

INTERCOSTAL CORRODED BETWEEN FS 349 AND FS 364 AT STR 27, R. REMOVED CORROSION FROM INTERCOSTAL FS349 TO 364 IAW SRM 51-21-06-001-001-A01 AT STR 27R. FOUND TO BE OUT OF ALLOWABLE LIMITS IAW SRM 53-21-23-101-003-A01. RESTORED TO ORIGINAL DWG FINISH IAW SRM 51-21-16-001-001-A01 AND CIC 51-21-11-001-001-A01 AND COMPLIED WITH REPAIR IAW EA 32-2015-143.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 17,651 hrs · 12,230 cycles

ASD FLOOR SILL CAP ANGLE IS CORRODED. CAP SILL ANGLE BEYOND ALLOWABLE DAMAGE IAW SRM 53-21-23-101-001-A02. REPLACE PART WHEN REQUESTED. REMOVED LOCATED AND DRILLED AND INSTALLED NEW ASD FLOOR SILL CAP ANGLE IAW SRM 51-42-06-001-001-A01, AND 51-40-11-001-001-A01.

Part: STRUCTURE — CORRODED (BS 333) · airframe 17,658 hrs · 12,237 cycles

PACKERS CORRODED AT FS 333 AND ON RBL 9 ON BOTH SIDES OF FLOORBEAM. REMOVED, 2 EA CORRODED PACKERS AND INSTALLED 2 EA NEW SERIVCABLE PACKERS IAW SRM 51-42-06-001-001 AND DWG SH670-32120.

Part: DOOR SILL — DAMAGED (BS 349-409) · airframe 17,664 hrs · 12,241 cycles

2 DRILL STARTS AND 11 TEMP FASTENERS LOCATED BETWEEN FS 349-FS 409 LT SIDE AT STR 17L. COMPLIED IWTH EC/TC REO 690-53-21-736 PERMANENT REPAIR REFER TO W/O 364816, N/R 00018. COMPLIED WITH REO 690-53-21-736. RECEIVED ECTC REO 690-53-21-736 AND COMPLIED WITH ECTC REO 690-53-21-736.

Part: SKIN — GOUGED (BS 1144) · airframe 17,664 hrs · 12,241 cycles

SCRATCH/DENT FOUND ON FUSELAGE AT FS 1144.00 AND FS 1162.00 AND STR 21R AND STR 22R. COMPLIED WITH EC/TC REO 690-53-61-453. RECEIVED FINAL REO 690-53-61-453. COMPLIED WITH EC/TC REO 690-53-61-453.

Part: SKIN — DENTED (PAX DOOR) · airframe 17,664 hrs · 12,241 cycles

FOUND A DENT ON OUTER SKIN MIDDLE OF PAX DOOR. INSTALLED ALL MAS1241 FASTENER IAW EA 32-2015-150 AD REV A. COMPLIED ECTC EA32-2015-150 AND STS EA 32-2015-150, REV A.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 14,876 hrs · 10,426 cycles

RT OVERWING EMERGENCY LIGHT HAS A BROKEN WIRE. TERMINATED WIRE IAW ESPM 20-16-00. PERFORMED OPS TEST IAW AMM 33-51-15-710-801. OPS TESTED GOOD.

Part: STRAP — CORRODED (ACCESS PANEL) · airframe 14,876 hrs · 10,426 cycles

FOUND STRAP FOR 196DR ACCESS PANEL BADLY CORRODED. COMPLIED WITH EC/TC EO 900-53-0004 IAW DWG CC690-39171 AND AMM 53-82-83.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 14,876 hrs · 10,426 cycles

BOTH LT WING EMERGENCY LIGHTS HAVE ONE BROKEN WIRE. TERMINATED WIRES IAW ESPM 20-16-00. PERFORMED OPS TEST IAW AMM 33-51-15-710-801. OPS TESTED GOOD.

Part: STRAP — CRACKED (FLOOR PANEL) · airframe 14,876 hrs · 10,426 cycles

STRAP, ON FLOOR PANEL 196DR IS CRACKED. R & R STRAP ASSY IAW AMM 53-82-83-000-803 AND 53-82-83-400-803.

Part: CHANNEL — CRACKED (FLOOR PANEL) · airframe 14,876 hrs · 10,426 cycles

AFT C-CHANNEL ON FLOOR PANEL 196DR IS CRACKED. INSTALLED SERVICEABLE CHANNEL ON STRAP ASSY IAW DWG CC690-39171 AND SRM 51-42-13.

Part: WIRE — DISCONNECTED (EMERGENCY LIGHT) · airframe 14,473 hrs · 10,172 cycles

LEFT AFT EXTERIOR EMERGENCY LIGHT INOPERATIVE. CONNECTED EMERGENCY LIGHT WIRE. OPS CHECKED GOOD, IAW AMM 33-51-05.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 13,114 hrs · 9,328 cycles

COCKPIT FLASHLIGHT INOPERATIVE. INSTALLED NEW BATTERIES IN FLASHLIGHT IAW AMM 25-61-05. OPS CHECKED GOOD.

Part: WARNING MESSAGE — FALSE ACTIVATION (TE FLAPS) · airframe 12,495 hrs · 8,939 cycles

FLAPS FAILED AT 30 CAUTION. VERIFIED AND INSPECTED BOTH SFECU. PERFORMED OPS CHECK OF FLAP SYSTEM IAW AMM 27-52-00. NO DEFECTS NOTED AT THIS TIME. OPS CHECKED GOOD. AIRCRAFT OK FOR SERVICE.

Part: LIFE VEST — UNSERVICEABLE (COCKPIT) · airframe 12,471 hrs · 8,919 cycles

OBSERVER'S LIFE VEST BAG TORN. REMOVED AND REPAIRED OBSERVERS LIFE VEST IAW AMM 25-61-03.

Part: LIFE VEST — UNSERVICEABLE (CABIN) · airframe 12,444 hrs · 8,900 cycles

THE 12D LIFE VEST HAS HOLE IN BAG. REMOVED AND REPLACED SEAT 12D LIFE VEST IAW AMM 25-61-03.

Part: BLADE — LACK OF LUBE (LT ENGINE) · airframe 12,363 hrs · 8,832 cycles

ON FLIGHT 3814 (ATL TO IAD) ON TAKEOFF CREW NOTICED THAT THE LEFT ENG FAN VIBE IN YELLOW (1.9) HAD TO KEEP POWER BELOW 76% N1 TO KEEP VIBRATION IN GREEN RANGE. CREW ACCOMPLISHED QRH AND PERFORMED AIR RETURN TO ATL. APPLIED LUBRICATION ON THE FAN BLADE IAW CRJ 90 AMM 72-21-02 SEE ITEM 2 FOR OPERATIONS CHECK AML 2274553.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT) · airframe 11,717 hrs · 8,415 cycles

DURING HEAVY CHECK FOUND LEFT EXTERNAL AFT OF WING EMERGENCY LIGHT INOPERABLE. (AIRCRAFT IN HEAVY CHECK 12-19-2012 THROUGH 1-11-2013) CONNECTED CONNECTORS P877 & P5320 IAW CRJ 900 AMM 25-26-01. OPS TEST OF EXTERIOR EMERGENCY LIGHTS GOOD IAW CRJ 900 AMM 33-51-15.

Part: FRAME — CRACKED (FUSELAGE) · airframe 11,752 hrs · 8,436 cycles

RIGHT FS 280 FRAME CRACKED AND CORRODED AT WL 97.5. REMOVED AND REPLACED IAW SRM 51-40-11/51-42-06.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,752 hrs · 8,436 cycles

LEFT FS 280 BEAM CORRODED AT WL 97.5. REMOVED AND REPLACED IAW SRM 51-40-11/51-42-06.

Part: RIVET — CORRODED (EMERGENCY EXIT) · airframe 11,717 hrs · 8,415 cycles

DURING HEAVY CHECK FOUND RIGHT AFT EMERGENCY EXIT DOOR EXTERIOR RIVET SHOWING SIGNS OF CORROSION. (AIRCRAFT IN HEAVY CHECK 12/19/2012 THROUGH 1/11/2013) REMOVED AND REPLACED RIVET IAW CRJ 900 SRM 51-42-06.

Part: COVER — CRACKED (CABIN) · airframe 11,422 hrs · 8,211 cycles

APPROXIMATELY 6 FEET OF FLOOR TRACK EMERGENCY LIGHT TRIM COVER IS CRACKED AFT OF OVERWING EXITS. CURRENTLY DEFERRED UNDER DEF-074551-2012.

Part: HOUSING — BROKEN (EMERGENCY LIGHT) · airframe 10,741 hrs · 7,715 cycles

SERVICE DOOR EMERGENCY LIGHT HOUSING BROKEN. REMOVED AND REPLACED SERVICE DOOR EMERGENCY LIGHT HOUSING IAW CMM 33-51-01.

Part: LIGHT — MISSING (CABIN) · airframe 10,616 hrs · 7,616 cycles

EMERGENCY FLOOR PATH LIGHTING NEAR FWD GALLEY CARTS MISSING. INSTALLED FLOOR LIGHTING STRIP AT FWD GALLEY CART AREA IAW AMM 33-51-01. OK FOR SERVICE.

Part: BLADE — LACK OF LUBE (NR 1 ENGINE FAN) · airframe 9,926 hrs · 7,070 cycles

NR 1 ENGINE FAN VIBRATION, 1.8 IN CAUTION RANGE AT FLT LVL 320. PERFORMED FAN BLADE TANG LUBRICATION IAW AMM 72-21-02. PERFORMED HIGH POWER ENGINE RUN. OPS CHECKED GOOD. OK FOR SERVICE.

Part: SPOILER — MALFUNCTIONED (WING) · airframe 9,272 hrs · 6,649 cycles

GLD UNSAFE CAUTION, SPOILERS DID NOT DEPLOY ON TOUCH DOWN, NO ALT CALLS. RESET SPOILER IN GLD PER FIM 27-60-00, AIRCRAFT OK FOR SVC.

Part: BLADE — LACK OF LUBE (LT ENGINE) · airframe 9,268 hrs · 6,647 cycles

LEFT N1 FAN VIBRATION AT 1.9 AT 33,000FT. REDUCED POWER AND UNABLE TO CONTROL VIBRATION. DESENDED 31,00FT. ABLE TO CONTROL FAN VIBRATION AT 1.5-1.7. NO ICE AND FLYING IN CLEAR WEATHER. VERIFIED DISCREPANCY. PERFORMED FAN BLADE TANG LUBRICATION ON LEFT ENGINE IAW CRJ900 AMM 72-21-12. PERFORMED HIGH PERFORMANCE ENG RUN. OPS CHECK GOOD AT THIS TIME. OK FOR SERVICE.

Part: UNKNOWN — MALFUNCTIONED (COCKPIT) · airframe 9,176 hrs · 6,489 cycles

ARRIVED AT A/C, ALL AVIONICS ON. TUBES DISPLAY RED DISPLAY TEMP. BURNT SMELL IN COCKPIT. INSPECTED MFD'S, NO DEFECTS NOTED AT THIS TIME REF CRJ 900 AMM 31-61-01. OPS CHECK OF AVIONICS COOLING SHOWS NORMAL OPERATIONS, REF CRJ 900 AMM 21-24-00. OK FOR SERVICE.

Part: BRAKE — SEIZED (RT MLG) · airframe 9,008 hrs · 6,442 cycles

ANTISKID OUTBOARD CAUTION MSG ON TAKEOFF. REMOVED AND REPLACED RT MAIN LANDING GEAR O/B WHEEL SPEED TRANSDUCER ASSEMBLY IAW CRJ 900 AMM 32-44-01. OPS CHECK GOOD. OK FOR SERVICE. PART EFFECTIVITY VERIFIED. RIGHT OUTBOARD BRAKE LOCKED UP AFTER REJECTED TAKEOFF. REMOVED AND REPLACED RIGHT OUTBOARD BRAKE IAW CRJ 900 AMM 32-43-26. OPS CHECK GOOD, OK FOR SERVICE. PART EFFECTIVITY VERIFIED. REMOVED AND REPLACED RIGHT INBD TIRE IAW CRJ 900 32-41-01. OK FOR SERVICE PART EFFECTIVITY VERIFIED. REMOVED & REPLACED RT MAIN LANDING GEAR O/B WHEEL ASSEMBLY IAW CRJ 900 AMM 32-41-01. OPS CHECK GOOD. OK FOR SERVICE, PART EFFECTIVITY VERIFIED. PERFORMED GVI AFTER REJECTED TAKEOFF. NO DEFECTS NOTED IAW CRJ 900 AMM 05-51-27. OK FOR SERVICE. PERFORMED TIRE BURST INSP IAW CRJ900 AMM 05-51-27. NO DEFECTS NOTED. OK FOR SERVICE.

Part: LOOP — OUT OF POSITION (ANTI-ICE SYS) · airframe 8,844 hrs · 6,324 cycles

APPROX 1 MIN AFTER T/O, "ANTI-ICE DUCT" WARNING MSG ON ED1, FOLLOWED BY "ANTI-ICE DUCT" CAUTION MSG. PERFORMED QRH EP 11-2. BOTH MSGS OUT; DID NOT RE-APPEAR. REPOSITIONED LOOPS AS NEED AT SS184R IAW CRJ900 AMM 36-21-11, PERFORMED HI POWER RUNS & OPS CHECK OF WING ANTI-ICE SYST WITH NO DEFECTS DETECTED. FOUND OK FOR RETURN TO SERVICE. REF CRJ900 AMM 30-11-00.

Part: SENSOR — MALFUNCTIONED (LADING GEAR) · airframe 7,914 hrs · 5,689 cycles

LT MAIN LANDING GEAR MSG STILL IN WORK FOR LANDING GEAR PRESSURE SENSOR.

Part: SEAL — TORN (CARGO DOOR) · airframe 6,724 hrs · 4,927 cycles

TEAR TO THE AFT CARGO DOOR SEAL (REF PIN CC670-38730) DUE TO CONTACT WITH DAMAGED SEAL RETAINER LIP. DAMAGE MEASURES 0.5 INCH LONG. TEMPORARY REPAIR IAW BOMBARDIER REO 690-52-31-005. WITHIN 100 FH PERMANENTLY REPAIR SEAL IAW BOMBARDIER GREO 670-52-31-017 OR REPLACE SEAL.

Part: FAN BLADE — LACK OF LUBE (LT ENGINE) · airframe 6,216 hrs · 4,593 cycles

ON CLIMBOUT OF KATL EN ROUTE TO KCLE, THE LT ENGINE N1 VIBES WENT 2.0 MILS WHICH IS IN THE AMBER RANGE. THE FLIGHT CREW COMPLETED THE QRH AND CONFERRED WITH MAINTENANCE CONTROL BY ACARS. DUE TO A LACK OF MAINTENANCE FACILITIES IN KCLE THE CREW WAS ADVISED TO RETURN TO KATL. AN OTHERWISE NORMAL APPROACH AND LANDING WAS MADE AT KATL. MAINTENANCE INSPECTED THE ENGINE AND LUBRICATED THE FAN BLADES. A SUBSEQUENT ENGINE RUN SHOWED NORMAL VIBRATION AND THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: SENSING ELEMENT — OUT OF POSITION (BLEED AIR SYS) · airframe 5,480 hrs · 4,132 cycles

CREW REPORTS A BLEED AIR WARNING MESSAGE IN FLIGHT (INDICATED LEFT SIDE). RAN QRH, AND DESCENDED BELOW 10,000 FT. DECLARED EMERGENCY WITH ATL / ATC AND LANDED WITHOUT INCIDENT. UPON INSPECTION ATL MAINTENANCE FOUND MULTIPLE BLEED LOOPS TOUCHING THE BLEED DUCT INSULATION. REPOSITIONED THE BLEED LOOP ELEMENTS AS REQUIRED PER AMM 36-21-01.

Part: CLAMP — LOOSE (AC BAY) · airframe 5,393 hrs · 4,085 cycles

WHILE EN ROUTE TO ATL FROM MTY THE CREW WAS WARNED FROM A R BLEED DUCT FAULT MESSAGE. THE QRH WAS THEN STARTED TO CORRECT THE SITUATION. WHILE COMPLYING WITH THE QRH BOTH A/C PACKS AUTOMATICALLY SHUT DOWN. THE CREW DIVERTED TO IAH WHERE MAINTENANCE FOUND A LOOSE DUCT CLAMP WHICH CAUSED THE DUCT FAULT. MAINTENANCE TIGHTENED THE CLAMP AND RESET BOTH PACKS IAW CRJ 900 AMM 21-51-00.

Part: SHUTOFF VALVE — FAILED (ENGINE) · airframe 4,582 hrs · 3,522 cycles

DIVERTED EARLIER IN DAY TO TYS DUE TO L ENG BLEED CAUTION MESSAGE. MAINT WORKED ON AIRCRAFT ALL DAY WHILE CREW WAITED AT HOTEL. DURING PART 91 REPO FLIGHT BACK TO ATL, CAUTION MESSAGE RETURNED. AIR RETURN TO TYS WAS RESULT. REMOVED AND REPLACED L 10TH STAGE HIGH PRESSURE SHUTOFF VALVE IAW AMM 36-12-05. OPS CHECK GOOD.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 4,579 hrs · 3,517 cycles

APPROXIMATELY 3 MINUTES AFTER TAKEOFF, ACFT MASTER CAUTION WITH 'L ENG BLEED' MESSAGE. CAPTAIN (PF) DIRECTED 1ST OFFICER (PM) TO CONDUCT QRH PROCEDURES. DURING INITIAL TURN ON DEPARTURE, RECEIVED A LIGHTNING STRIKE TO NOSE. AIR RETURN. FOUND RT TRAILING EDGE HORIZ STAB TIP BURNT, ALL ACTIONS COMPLIED WITH FOR REO 670-55-12-017 GOOD FOR 600 FH. ON NOSE FOUND 8 FASTENERS BURNT LT NOSE AFT OF RADOME WITHIN SERVICEABLE LIMITS ACCEPTABLE AS IS IAW SRM 53-00-00 TYPE 4. OK TILL NEXT C CHECK WITH RE-INSP AT EACH 2ND A CHECK 531000 SEQ 1.