N331CA

Part: FITTING — CORRODED (ZONE 100) · airframe 43,276 hrs · 33,585 cycles

O/B BUSHING FOR THE L/H MLG SIDESTAY IN WHEEL WELL IS WORN. VISUAL INSPECTION REVEALED CORROSION AND LIGHT PITTING INSIDE BORE AND ON OUTBOARD FACE (SURFACES IN CONTACT WITH O/B BUSHING) OF LH MLG SIDE STAY FITTING P/N CC670-10608-5. ENGINEERING DISPOSITION REQUIRED FOR REPAIR. REPAIRED IAW MHIRJ REO 670-57-11-230 REV - DATED 5/13/2025 ON O/B BUSHING FOR THE L/H MLG SIDESTAY

Part: STRINGER — CORRODED (ZONE 100) · airframe 43,276 hrs · 33,585 cycles

STGR26L HAS CORROSION AROUND FASTENER TAILS FROM FS409- FS453. REMOVED CORRODED STRINGER 26L FROM F.S.409 TO F.S.453 AND INSTALLED NEW SERVICABLE STRINGER IAW CRJ 700 SRM 51-42-06-001-001-A01.

Part: SHEAR TIE — CORRODED (ZONE 100) · airframe 43,276 hrs · 33,585 cycles

FRAME AT FS421 HAS CORROSION ON SHEAR TIE ON AFT SIDE OF FRAME AROUND FASTENER. REPAIRED LOWER FUSELAGE FRAME SECTOR AT F.S.421 BETWEEN STGR 26L AND 26R IAW MHIRJ REO 670-53-21-2527 REV -- DATED 2024-12-28.

Part: STRINGER — CORRODED (ZONE 100) · airframe 43,276 hrs · 33,585 cycles

STGR 26L HAS CORROSION AROUND FASTENER HEADS FS879-FS885. REPAIRED STRINGER 26L BETWEEN F.S.879 AND F.S.885 IAW MHIRJ REO 670-53-51-328 REV-- DATED 2025-01-13.

Part: STRINGER SPLICE — CORRODED (ZONE 100) · airframe 43,276 hrs · 33,585 cycles

UPON REMOVAL OF STGR 21R FS280-FS333, FOUND JOINT PIECE SPLICE (P/N:SH670-31197-1) AT FS333.00 TO HAVE CORROSION REQUIRES EVAL REPLACED AND INSTALLED NEW SERVICEABLE JOINT SPLICE (P/N:SH670-31197-1S) @ FS333 STGR 21R IAW CRJ 700 51-42-06-001-001-A01 LOCATED AND DRILLED SPLICE @ FS 333 S21R P/N SH670-31197-1S IAW CRJ700 SRM 51-40-11-001-001-A01 RESTORED SURFACE TO FINISH IAW CRJ 700 SRM 51-21-16-001-001-A01 (TR51-0068) GROUNDING WIRE PLATE AT STGR 21R FS333 LOCATED ON JOINT PIECE SPLICE (P/N:SH670-31197-1S) FS333 STGR 21R. REF. BARCODE IDENTIFIER HN00204628 FOR INSTALLATION AND REPLACEMENT

Part: STRINGER SPLICE — CORRODED (ZONE 100) · airframe 43,276 hrs · 33,585 cycles

UPON REMOVAL JOINT PIECE STGR P/N:SH670-33241-1 FROM FS.477 STGR 26L FOUND PART TO BE HEAVILY CORRODED, REQUIRES REPLACEMENT. EVALUATED JOINT SPLICE AT STGR 26L, FS477 HAS PITTING CORROSION THROUGH PART. 100% MATERIAL LOSS. FOUND OUT OF LIMITS. CRJ700 SRM 53-00-- 00-101-001-A01 LOCATED AND DRILLED NEW SERVICEABLE JOINT PIECE (PN# SH670-33241-1) FROM STRG26 AND FS 477 IAW CRJ700 SRM 51-40-11-001-001-A01 INSTALLED NEW SERVICEABLE JOINT PIECE (PN#SH670-33241-1) FROM STRG 26 AND FS 477 IAW CRJ700 SRM 51-42-06-001-001-A01 FOR APPLY CIC ON NEW SERVICEABLE JOINT PIECE PN:SH670-33241-1 FS. 477.00, REFER TO MWC BARCODE IDENTIFIER: HR00499224.

Part: STRINGER — CORRODED (ZONE 100) · airframe 43,276 hrs · 33,585 cycles

UPON REMOVAL OF STGR 24R FROM FS280-FS333 FOUND STGR 24R SPLICE AT FS 333 TO BE CORRODED REMOVED CORROSION ON STGR 24R SPLICE IAW CRJ 700 SRM 51-21-06-001-001-A01. ORIGINAL MATERIAL THICKNESS WAS .063, MATERIAL REMOVED WAS .011, REMAINING MATERIAL THICKNESS IS .052 AND IS FOUND TO BE OUT OF ALLOWABLE DAMAGE LIMITS IAW CRJ 700 SRM 53-00-00-101-001-A01 DISPLACED CLEAT ON FS 333 AT STGR 24R IAW CRJ 700 SRM 51-42-06-001-001-A01 REMOVED STGR 24R SPLICE AT FS 333 IAW CRJ 700 SRM 51-42-06-001-001-A01 LOCATED AND DRILLED NEW STGR 24R SPLICE (PN: SH670-32429-2) IAW CRJ 700 SRM 51-40-11-001-001-A01 INSTALLED NEW SERVICEABLE STRINGER JOINT PIECE (SPLICE) P/N SH670-32429-2 AT STGR 24R - FS 333 IAW CRJ700 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01. RE-INSTALLED SOLID RIVETS ON SAME SERVICEABLE CLEAT ON FS 333 AT STGR 24R IAW CRJ700 SRM 51-42-06-001-001-A01. RESTORED FINISH IAW CRJ700 SRM 51-21-11-001-001-A01

Part: STRINGER — CORRODED (ZONE 100) · airframe 43,276 hrs · 33,585 cycles

STRINGER 24R HEAVILY CORRODED BETWEEN FS333.00 AND FS394.00. REPAIRED STRINGER 24R FS333-FS394 PN: SH670-31368-6 IAW CRJ700 SRM 53-00-03-201-001-A01

Part: STRINGER — CORRODED (ZONE 100) · airframe 43,276 hrs · 33,585 cycles

STRINGER 24R BETWEEN FS 295 TO FS 310 IS CORRODED. REMOVED 10 EA RIVETS FROM STR 24R BETWEEN FS 295 TO FS 310 FOR ACCESS TO REMOVE CORROSION IAW CRJ700 SRM 51-42-06-001-001-A01 DISPLACED CLEATS ON STGR 24R AT FS 310 AND FS 319 IAW CRJ700 SRM 51-42-06-001-001-A01 DISPLACED CLEAT AT FS 333 FOR STGR 24R REQUIRES INSTALL REMOVED SPLICE JOINT PIECE FROM FS 333 AND STR 24R IAW CRJ700 SRM 51-42-06-001-001-A01. REMOVED DAMAGED STR 24R FROM FS 280 TO FS 333 IAW CRJ700 SRM 51-42-06-001-001-A01. AND 51-42-21-001-001-A01 LOCATED AND DRILLED NEW STGR 24R (PN SH670-31212-2U) IAW CRJ 700 SRM 51-40-11-001-001-A01 INSTALLED NEW STGR 24R FROM FS 280 TO FS 333 IAW CRJ700 SRM 51-42-06-001-001-A01. AND 51-42-21-001-001-A01 INSTALLED 10EA RIVETS IN STR 24R BETWEEN FS 295 TO FS 310 IAW CRJ700 SRM 51-42-06-001-001-A01 INSTALLED STGR CLEATS ON STGR 24R AT FS 310 AND FS 319 IAW CRJ 700 SRM 51-42-06-001-001-A01 FOR INSTALL OF CLEAT AT FS 333 STGR 24R REFER TO HN00209674 S/N:975 FOR INSTALL OF SPLICE JOINT PIECE FROM FS 333 AND STR 24R REFER TO HN00209674 S/N:975 EDGE SEALED IAW CRJ700 SRM 51-23-00-001-001-A01 AND RESTORED FINISH IAW CRJ700 SRM 51-21-11-001-001-A01

Part: STRINGER SPLICE — CORRODED (ZONE 100) · airframe 43,276 hrs · 33,585 cycles

UPON REMOVAL OF STGR 21R FS280-FS333, FOUND JOINT PIECE SPLICE (P/N:SH670-31197-1) AT FS333.00 TO HAVE CORROSION REQUIRES EVAL. EPLACED AND INSTALLED NEW SERVICEABLE JOINT SPLICE (P/N:SH670-31197-1S) @ FS333 STGR 21R IAW CRJ 700 51-42-06-001-001-A01 LOCATED AND DRILLED SPLICE @ FS 333 S21R P/N SH670-31197-1S IAW CRJ700 SRM 51-40-11-001-001-A01 RESTORED SURFACE TO FINISH IAW CRJ 700 SRM 51-21-16-001-001-A01 (TR51-0068) GROUNDING WIRE PLATE AT STGR 21R FS333 LOCATED ON JOINT PIECE SPLICE (P/N:SH670-31197-1S) FS333 STGR 21R. REF. BARCODE IDENTIFIER HN00204628 FOR INSTALLATION AND REPLACEMENT

Part: DOOR SILL — CORRODED (ZONE 200) · airframe 43,276 hrs · 33,585 cycles

"WHILE INSTALLING NEW AFT CARGO DOOR SURROUND, LOWER SILL P/N MM670-35655-003 FOUND 1 EACH FASTENER HOLE DRILLED NEXT TO A PILOT HOLE AT APPROX. FS1044, LBL 43. REMOVED AFT CARGO DOOR SURROUND, LOWER SILL P/N MM670-35655-003 IAW CRJ700 SRM 51-42-13-001-001-A01. FABRICATED AFT INNER CHORD P/N MM670-35670-003 USING 7075-O 0.063"" PO# 5-32567 IAW CRJ700 SRM 51-24-16-001-001-A01. RECEIVED NEW SERVICEABLE AFT INNER CHORD P/N MM670-35670-003 FROM STOCK. LOCATED AND DRILLED NEW SERVICEABLE AFT INNER CHORD P/N MM670-35670-003 IAW CRJ-700 SRM 51-40-11-001-001-A01. REF JOB HN201318 SN 447 FOR INSTALL."

Part: FRAME — CORRODED (ZONE 100) · airframe 43,276 hrs · 33,585 cycles

F.S. 295 FRAME IS CORRODED ON FWD SIDE OF AT STGR 26R - STGR 27. REPAIRED PER CRJ-700 SRM 53-00-06-201-006-A01.

Part: STRINGER SPLICE — CORRODED (ZONE 100) · airframe 43,276 hrs · 33,585 cycles

STGR SPLICE P/N: SH670-32429-1 AT FS 333.00 STGR 23L FOUND HEAVY CORRODED. LOCATED AND DRILLED NEW STGR SPLICE P/N:SH670-32429-3 IAW CRJ700 SRM 51-40-11-001-001-A01.INSTALLED NEW STGR SPLICE P/N: SH670-32429-3 AT FS 333.00 STGR 23L IAW CRJ700 SRM 51-42-06-001-001-A01

Part: STRINGER SPLICE — CORRODED (ZONE 100) · airframe 43,276 hrs · 33,585 cycles

JOINT PIECE FS 333.00 STGR 22L FOUND HEAVY CORRODED. LOCATED AND DRILLED NEW STGR SPLICE P/ N: SH670-32429-3 IAW CRJ700 SRM 51-40-11-001-001-A01.INSTALLED NEW STGR SPLICE P/N: SH670-32429-3 AT FS 333.00 S22L IAW CRJ700 SRM 51-42-06-001-001-A01

Part: STRINGER — CORRODED (ZONE 100) · airframe 43,276 hrs · 33,585 cycles

BETWEEN FS 349.00 AND FS 364.00 L/H STRINGER 23L IS CORRODED. REPAIRED STRINGER 23L BETWEEN F.S.349 TO F.S.364 IAW CRJ 700 SRM 53-00-03-201-001-A01.

Part: FITTING — DAMAGED (ZONE 800) · airframe 43,276 hrs · 33,585 cycles

PAX DOOR FWD FITTING FOUND TO HAVE 5 EACH ELONGATED HOLES UPON REMOVAL FOR ACCESS. REMOVED DAMAGED FITTING. FABRICATED, DRILLED AND INSTALLED NEW FABRICATED FITTING PN 600-38044-S0101 IAW MHIRJ EO 600-380440S01 AND 601R31702-S12

Part: DOOR FRAME — CORRODED (ZONE 200) · airframe 43,276 hrs · 33,585 cycles

PAX DOOR FRAME FS313.56 BETWEEN DD4 AND DD5 CORRODED AND REQUIRES REPLACEMENT. REMOVED DAMAGED FRAME. LOCATED, DRILLED AND INSTALLED NEW SERVICEABLE FRAME (P/N 601R318086-1) IAW CRJ 700 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01.

Part: STRINGER — CORRODED (ZONE 100) · airframe 43,276 hrs · 33,585 cycles

STRINGER 22R BETWEEN FS 319.00 AND FS 333.00 IS CORRODED. LOCATED AND DRILLED NEW SERVICEABLE STR 22R FROM FS 280 TO FS 333 (PN# SH670-31210-2U) IAW CRJ700 SRM 51-40-11-001-001-A01. INSTALLED NEW SERVICEABLE STR 22R FROM FS 280 TO FS 333 (PN# SH670-31210-2U) IAW CRJ700 SRM 51-41-06-001-001-A01 AND 51-42-21-001-001-A01.

Part: STRUCTURE — CORRODED (AFT BAGGAGE DOOR) · airframe 43,276 hrs · 33,585 cycles

"UPON INVESTIGATION, AFT INNER CHORD P/N: MM670-35657-003 OF AFT BAGGAGE DOOR SURROUND STRUCTURE WITH CORROSION. REMOVED CORROSION IAW CRJ 700 SRM 51-21-06-001-001-A01, FINAL THICKNESS 0.013"" OF NOMINAL THICKNESS 0.063"" NOT ALLOWED DAMAGE. REQUIRES REPLACEMENT. LOCATED, DRILLED AND DEBURRED NEW AFT INNER CHORD PN MM670-35670-003 IAW CRJ700 SRM 51-40-11-001-001-A01. REPLACED AFT INNER CHORD (PN: MM670-35670-003) IAW CRJ 700 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. REMOVED EWIS PROTECTION SURROUNDING THE AFT CARGO DOOR SURROUND STRUCTURE"

Part: FORMER — CORRODED (ZONE 800) · airframe 43,276 hrs · 33,585 cycles

PAX DOOR FORMER @FS 335.163 IS CORRODED AND REQUIRES REPLACEMENT. REMOVED CORRODED FORMER. LOCATED AND DRILLED NEW SERVICEABLE FORMER IAW CRJ 700 SRM 51-40-11-001-001-A01. INSTALLED NEW SERVICEABLE FORMER P#601R31902-15 IAW CRJ 700 SRM 51-42-06-001-001-A01.

Part: FORMER — CORRODED (ZONE 800) · airframe 43,276 hrs · 33,585 cycles

PAX DOOR FORMER FS311.75 HAS PREVIOUS REPAIR THAT INTERFERES WITH NEW MODSUM. REQUIRES REPLACEMENT. LOCATED AND DRILLED PAX DOOR FORMER @ FS311.75 IAW CRJ 700 SRM 51-40-11-001-001-A01. INSTALLED NEW SERVICEABLE FORMER P#601R318031-5S IAW CRJ 700 SRM 51-42-06-001-001-A01 AND 52-42-21-001-001 -A01.

Part: STRINGER — CORRODED (ZONE 100) · airframe 43,276 hrs · 33,585 cycles

STRINGER SPLICE AT FS 333.00 STGR 22R CORRODED. REPLACED STRINGER SPLICE

Part: INTERCOSTAL — CORRODED (ZONE 800) · airframe 43,276 hrs · 33,585 cycles

PAX DOOR INTERCOSTAL DD7A FWD CORRODED AND REQUIRES REPLACEMENT. LOCATED AND DRILLED INTERCOSTAL IAW CRJ 700 SRM 51-40-11-001-001-A01. INSTALLED NEW SERVICEABLE INTERCOSTAL PN:601R318083-1 IAW CRJ 700 SRM 51-42-06-001-001-A01.

Part: STRINGER — CORRODED (ZONE 100) · airframe 43,276 hrs · 33,585 cycles

UPON REMOVAL OF AVIONICS SUPPORT BRACKET ANGLE AT F.S.295, STGR 21R FOUND CORROSION ON STGR 21R UNDER BRACKET REMOVED ALL RIVETS ON STRINGER 21R BETWEEN FS 280.00 AND FS 333.00 IAW CRJ 700 SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01. REMOVED STRINGER 21R JOINT PIECE SPLICE (P/N:SH670-31197-1) AT FS333.00 IAW CRJ 700 SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01. REMOVED 2EA GUSSETS FOR ACCESS ON FS310 AND FS319 AT STGR 21R IAW CRJ 700 SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01. LOCATED AND DRILLED NEW STRINGER 21R FROM FS 280 TO FS 319 PN SH670-31636-1U IAW CRJ-700 SRM 51-40-11-001-001-A01 INSTALLED NEW STGR 21R P/N:SH670-31636-1 SEGMENT BETWEEN FS 280.00 AND FS 333.00 IAW CRJ700 SRM 51-42-06-001-001-A01. AND CRJ700 SRM 51-42-21-001-001-A01. INSTALLED 2EA GUSSETS FOR ACCESS ON FS310 AND FS319 AT STGR 21R IAW CRJ 700 SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01. STRINGER 21R JOINT PIECE SPLICE (P/N:SH670-31197-1) REF. BARCODE IDENTIFIER HN00208873 FOR REPLACEMENT AND INSTALLATION.

Part: INTERCOSTAL — CORRODED (ZONE 100) · airframe 43,276 hrs · 33,585 cycles

F.S.394 TO F.S.409 CENTER LEFT INTERCOSTAL AT STGR 27 IS CORRODED ON BOTTOM FLANGE. REMOVED INTERCOSTAL (PN# SH670-32075-4) FROM STR 27 BETWEEN FS 394 - FS 409 IAW CRJ700 SRM 51-42-06-001-A01 AND 51-42-21-001-001-A01. LOCATED AND DRILLED NEW SERVICEABLE INTERCOSTAL (PN# SH670-32075-4S) IAW CRJ700 SRM 51-40-11-001-001-A01.INSTALLED NEW SERVICEABLE INTERCOSTAL (PN# SH670-32075-4S) FROM STR 27 BETWEEN FS 394 - FS 409 IAW CRJ700 SRM 51-42-06-001-A01 AND 51-42-21-001-001-A01.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 43,276 hrs · 33,585 cycles

R/H FS712-FS756 SIDE SEAT RAIL IS CORRODED. REMOVED UNSERVICEABLE SIDE SEAT RAIL P/N:SH670-37509-1 ON R/H BETWEEN FS712-FS763. IAW CRJ700 53-00-49-000-801-A03.PAINTED NEW SERVICEABLE SEAT RAIL P/N:SH670-37509-1 IAW BOMBARDIER MODSUM IS67053000195 REV A. DATED 2018/02/07. INSTALLED NEW SERVICEABLE SEAT RAIL P/N:SH670-37509-1 ON R/H SIDE BETWEEN FS712-FS763. IAW CRJ700 AMM 53-00-49-400-801-A03.

Part: STRINGER — CORRODED (ZONE 100) · airframe 43,276 hrs · 33,585 cycles

STRINGER 22L BETWEEN F.S.333 TO F.S.349 IS CORRODED. REPAIRED PER CRJ700 SRM 53-00-03-201-001-A01.

Part: STRINGER — CORRODED (ZONE 100) · airframe 43,276 hrs · 33,585 cycles

STRINGER 21R AT F.S.364 IS CORRODED. REMOVED DAMAGED STGR 21R SEGMENT BETWEEN FS 333.00 AND FS 379.00 IAW CRJ700 SRM 51-42-06-001-001-A01. INSTALLED NEW STGR 21R P/N:SH670-31383-1S BETWEEN FS 333.00 AND FS 379.00. IAW CRJ700 SRM 51-42-06-001-001-A01.

Part: STRINGER — CORRODED (ZONE 100) · airframe 43,276 hrs · 33,585 cycles

STRINGER 22R BETWEEN F.S.333 TO F.S.349 IS CORRODED. EVALUATED DAMAGE FOUND TO BE 100% MATERIAL LOSS, FOUND P/N SH670-31379-1 TO BE OUT OF ALLOWABLE LIMITS IAW CRJ700 SRM 53-21-03-101-006-A01 REQUIRES REPLACEMENT INSTALLED NEW SERVICEABLE STRG SPLICE FROM FS 333 AND STR 22R IAW CRJ700 SRM 51-42-06-001-001-A01 INSTALLED STGR CLEAT AT FS 349.00 STGR 22R IAW CRJ700 SRM 51-42-06-001-001-A01. INSTALLED CLEAT AT STR 22R AND FS 333 IAW CRJ700 SRM 51-42-06-001-001-A01. REMOVED DAMAGED STGR 22R BETWEEN FS 333.00 AND FS 349.00 IAW CRJ700 SRM 51-42-06-001-001-A01. INSTALLED NEW STGR 22R P/N: SH670-31397-1S BETWEEN FS 333.00 AND FS 349.00 IAW CRJ700 SRM 51-42-06-001-001-A01. LOCATED AND DRILLED NEW STGR 22R P/N:SH670-

Part: FRAME — CORRODED (ZONE 100) · airframe 43,276 hrs · 33,585 cycles

FS863 FRAME IS CORRODED FROM STGR 26L-26R ON FWD AND AFT SIDE IF FRAME AND ON SHEAR TIES. REPAIRED IAW ENDEAVOR AIR EA# CRJ753-17935, REV IR, DATED 12/15/2024.

Part: LUG — DAMAGED (ZONE 600 AILERON) · airframe 43,276 hrs · 33,585 cycles

"RH AILERON # 2 AND #3 HINGE LUGS WERE FOUND OVERSIZED UPON REMOVAL OF BEARINGS. #2 LUG BORE IS .9895"" THE #3 LUG BORE IS .9935"" C/W MHIRJ REO 690-57-61-351 REV A DATED 2024-12-21."

Part: FRAME — CORRODED (ZONE 100) · airframe 43,276 hrs · 33,585 cycles

F.S. 517 STR 25L-25R CORRODED AFT SIDE LEG AND GOING UP FACE OF FRAME LOCATED AND DRILLED NEW SERVICEABLE BOTTOMS STUB FRAME AT FS518 BETWEEN STGRS25L AND 26L IAW CRJ-700 SRM 51-40-11-001-001-A01. INSTALLED NEW SERVICEABLE BOTTOM STUB FRAME P/N SH670-33260-3S AT FS517 FROM BETWEEN STGR26L-25L IAW CRJ-700 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01

Part: BUSHING — DAMAGED (ZONE 500) · airframe 43,276 hrs · 33,585 cycles

"LH AILERON PCU LUGS MARKED C AND F WERE FOUND OVERSIZED UPON REMOVAL OF BUSHINGS. COMPLIED WITH STEPS #6.2, #6.5, & #6.6 OF BOMBARDIER REO 670-57-61-107 REV. -B DATED 2019-01-14. STEP #6.2 - FINAL LUG BORE INTERNAL DIAMETERS ARE (C = 0.8445"") & (F = 0.8450""). STEP #6.5 - FABRICATED (QTY. 2) O/S AILERON BUSHINGS (P.N. S10009-225Y) USING MATERIAL AMS5659 15-5 PH H1000 (P.O. 5-35803). STEP #6.6 - BUSHING FLANGE DIAMETER CONFIRMATION. PERFORMED EDDY CURRENT OF LH AILERON PCU LUGS BORES IAW BOMBARDIER REO 670-57-61-107 REV B STEP 6 5I NO INDICATIONS NOTED AT THIS TIME APPLIED BRUSH CAD-PLATING TO 2 EA. NEW BUSHINGS IAW STEP #6.5.A.II OF BOMBARDIER REO 670-57-61-107 REV. -B DATED 2019-01-14. REFERENCE HR00204039 FOR INSTALLATION OF BUSHINGS."

Part: INTERCOSTAL — CORRODED (ZONE 800) · airframe 43,276 hrs · 33,585 cycles

PAX DOOR INTERCOSTAL DD4 IS CORRODED REMOVED DAMAGED INTERCOSTAL. LOCATED, DRILLED AND INSTALLED NEW DD4 INTERCOSTAL PN 601R318081-1S IAW CRJ700 51-40-11-001-001-A01, 51-42-21-001-001-A01 AND 51-42-06-001-001-A01

Part: INTERCOSTAL — CORRODED (ZONE 800) · airframe 43,276 hrs · 33,585 cycles

PAX DOOR INTERCOSTAL DD3 IS CORRODED. INSTALLED NEW SERVICEABLE INTERCOSTAL PN:601R318056-1S IAW CRJ 700 SRM 51-42-06-001-001-A01.

Part: DOOR SILL — CORRODED (ZONE 100) · airframe 43,276 hrs · 33,585 cycles

AFT CARGO DOOR SILL CORRODED MULTIPLE PLACES BETWEEN F.S. 1000 - F.S. 1047 REMOVED AND INSTALLED NEW AFT CARGO DOOR SILL PN P/N MM670-35655-003 IAW CRJ700 SRM 53-61-23-201-001-A01 AND CRJ700 SRM 51-42-13-001-001-A01 AND CRJ700 SRM 51-45-00-001-001-A01 AND CRJ700 SRM 51-42-15-001-001-A01

Part: LAMP — INOPERATIVE (ZONE 200) · airframe 43,273 hrs · 33,584 cycles

RIGHT FWD AND LEFT AFT EXTERIOR EMERGENCY LIGHTS INOP AND LENS COVERS DETERIORATED. R&R EMERGENCY LIGHTS BULBS AND LENS COVERS PER AMM 33-51-15. CHECK GOOD. PN ON/OFF 8GH002473-08, 9EL400042-11

Part: FITTING — GOUGED · airframe 42,019 hrs · 32,423 cycles

INSPECTED THE L/H WING AILERON BUSHING BORE AT WS 343.50 AND FOUND DAMAGE TO THE TOP CENTER OF THE O/B BUSHING BORE. - FOUND L/H WING AILERON BUSHING BORE TOP CENTER OF THE I/B BUSHING BORE REPAIRED BORE IAW MHIRJ 670-57-51-455, REV.A DATED 2021-11-10.

Part: FITTING — GOUGED · airframe 42,019 hrs · 32,423 cycles

SUPPLEMENTAL INFORMATION / CORRECTED INFORMATION. THIS CONTAINS THE CORRECT ATA AND AIRCRAFT MODEL NUMBER.

Part: BATTERY — FAILED (EMERGENCY LIGHT) · airframe 40,230 hrs · 30,744 cycles

OVERHEAD AISLE EMERGENCY FLOOD LIGHTS AND EMERGENCY EXIT SIGN DO NOT ILLUMUNATE W/EMERGENCY LIGHTING ACTIVE. REMOVED AND REPLACED EMERGENCY BATTERY PACK NR 2, IAW CRJ 700 JOBCARD 33-900-701. OPS CHECK GOOD.

Part: LIGHT — BROKEN (CABIN) · airframe 37,624 hrs · 28,386 cycles

EMERGENCY ESCAPE PATH LIGHTING BROKEN AND MISSING AT EXIT ROW.REPLACED SAFETY GLOW EXIT ROW AT LH SIDE REPLACING WITH SAFETY GLOW FROM ROW 1A IAW CRJ 900AMM 33-51-01.

Part: SKIN — CRACKED (PAX DOOR) · airframe 36,744 hrs · 27,536 cycles

PASSENGER DOOR INTERNAL SKIN AT PANEL 832AL IS CRACKED. REPAIRED INTERNAL SKIN IAW REO 670-52-11-1025 DATED 2018-06-19.

Part: BRACKET — CRACKED (PAX DOOR) · airframe 36,744 hrs · 27,536 cycles

TWO BRACKETS FOUND CRACKED AT THE PASSENGER DOOR UPPER EDGE. REMOVED AND REPLACED IAW SRM 51-40-00.

Part: FRAME — CRACKED (BS 333) · airframe 36,744 hrs · 27,536 cycles

FRAME BS 333, STRINGER 0 FOUND CRACKED. REMOVED AND REPLACED THE FRAME IAW SRM 51-42-06, 51-42-21, 51-40-11, 53-21-23, 51-32-59, 51-24-36, AMM 20-70-00, 20-30-00, DRAWING SH670-41536, AND SH670-698-41558.

Part: ANGLE — CORRODED (PAX DOOR) · airframe 36,744 hrs · 27,536 cycles

PASSENGER DOOR MID-CAP IS CORRODED. REMOVED AND REPLACED THE MID-CAP IAW SRM 51-42-02, 51-40-11, AMM 52-70-04, AND 20-21-00.

Part: HINGE — EXCESS PLAY (PAX DOOR) · airframe 36,744 hrs · 27,536 cycles

PASSENGER DOOR HINGE HAD PLAY. : REPAIRED THE DOOR HINGE IAW EO 670-53-21-582, REV F, AND REO 670-53-21-1527.

Part: BRACKET — CRACKED (AFT E/E BAY) · airframe 36,744 hrs · 27,536 cycles

AFT EQUIPMENT BAY WATER LINE BRACKET AT STRINGER 9L WAS FOUND CRACKED. REPLACED THE BRACKET IAW SRM 51-42-21, AND AMM 20-21-00.

Part: LINK ASSY — CRACKED (PAX DOOR) · airframe 36,774 hrs · 27,536 cycles

PASSENGER DOOR LATCH MECHANISM LINK SUB-ASSEMBLY CRACKED. REPLACED PASSENGER DOOR LATCH MECHANISM LINK SUB-ASSEMBLY IAW AMM 52-11-02.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 36,744 hrs · 27,536 cycles

NR 1 SEAT TRACK, BS 350 - 485 WAS CORRODED. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49.

Part: SEAT TRACK — CORRODED (BS 384-475) · airframe 36,744 hrs · 27,536 cycles

SEAT TRACK NR 1 FROM BS 374 - 485 WAS CORRODED. FABRICATED AND INSTALLED A NEW SEAT TRACK IAW REO 670-53-00-013, REV J, AND REO 670-53-00-343, REV M.

Part: GUSSET — CORRODED (BS 319) · airframe 36,744 hrs · 27,536 cycles

GUSSET AT BS 319.7, STRINGER 21R HAS SIGNS OF CORROSION. REMOVED AND REPLACED THE GUSSET IAW SRM 53-21-23, 51-42-06, 51-40-11, 51-42-21, 51-25-16, AND 51-21-11.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 36,744 hrs · 27,536 cycles

INTERCOSTAL BETWEEN FS 310.00 AND 319.00 IS CORRODED. REMOVED AND REPLACED INTERCOSTAL(PN:SH670-32047-1) IAW SRM 51-21-23, 51-42-21, 51-42-06, 51-40-11, 51-21-11, 51-25-16, ESPM 20-23-01, AND 20-12-00

Part: FRAME — CORRODED (FUSELAGE) · airframe 36,744 hrs · 27,536 cycles

FRAME 319.70 AT STGR 20R IS CORRODED. REMOVE AND REPLACED FRAME 319.70(PN: SH670-32029-3) IAW SRM 51-42-21, 51-40-11, 51-21-11, 51-42-06, 51-42-13, AND 51-25-16.

Part: ANGLE — CORRODED (SERVICE DOOR) · airframe 36,744 hrs · 27,536 cycles

KICK ANGLE SHOWING SIGNS OF CORROSION ON THE SERVICE DOOR. REMOVED AND REPLACED THE KICK ANGLE IAW SRM 51-42-06, AND 51-42-21.

Part: BAFFLE — CRACKED (LT LOWER) · airframe 36,744 hrs · 27,536 cycles

LEFT LOWER TRANSCOWL BAFFLE IS CRACKED. REMOVED AND REPLACED THE BAFFLE IAW SRM 51-42-06.

Part: FITTING — CORRODED (THRESHOLD) · airframe 36,744 hrs · 27,536 cycles

FOUR EACH FITTINGS AT SERVICE DOOR THRESHOLD HAD SIGNS OF CORROSION. REMOVED AND REPLACED THE FITTINGS ON THE SERVICE DOOR THRESHOLD IAW SRM 53-21-23, 51-42-21, 51-40-11, 51-25-16, 51-42-06, AND AMM 53-21-27.

Part: CAP — CORRODED (SERVICE DOOR) · airframe 36,744 hrs · 27,536 cycles

SERVICE DOOR SURROUND STRUCTURE MID CAP HAS SIGNS OF CORROSION. REMOVED AND REPLACED THE CAP IAW SRM 51-42-06, AND 51-42-21.

Part: STRAP — CORRODED (ZONE 100) · airframe 36,744 hrs · 27,536 cycles

RT WING TO BODY EYEBROW PANEL ATTACHMENT STRAP HAS SIGNS OF CORROSION. REPLACED RT WING TO BODY EYEBROW PANEL ATTACHMENT STRAP IAW SRM 51-42-13, 51-42-06.

Part: STRUCTURE — GOUGED (RT WING AILERON) · airframe 36,744 hrs · 27,536 cycles

RIGHT AILERON UPPER LEADING EDGE FOUND GOUGED. REPAIRED AILERON, PERFORMED NDT, AND RESTORED THE FINISH IAW REO 670-57-61-279 REV --.

Part: DOOR SILL — CORRODED (AFT CARGO) · airframe 36,744 hrs · 27,536 cycles

AFT CARGO DOOR SILL HAS SIGNS OF CORROSION AT SEVERAL AREAS. REMOVED AND REPLACED THE DOOR SILL IAW SRM 51-42-06, 51-42-21, 51-40-11, 51-42-13, 51-25-16, 51-21-11, AND 53-61-23.

Part: FITTING — CORRODED (BS 319) · airframe 36,744 hrs · 27,536 cycles

FRAME BS 319.7 FITTING AT STRINGER 18R HAS SIGNS OF CORROSION. REMOVED AND REPLACED THE FITTING IAW SRM 51-42-21, 51-40-11, 51-25-16, 51-21-11, AND 53-21-23.

Part: DOOR SILL — CORRODED (SERVICE DOORWAY) · airframe 36,744 hrs · 27,536 cycles

GALLEY SERVICE DOOR SILL AND SILL LIP HAVE SIGNS OF CORROSION. REMOVED AND REPLACED THE DOOR SILL IAW SRM 51-42-06, AND 51-42-21.

Part: STRAP — CRACKED (WING TO BODY) · airframe 36,744 hrs · 27,536 cycles

AFT WING TO BODY FAIRING STRAP CRACKED. REMOVED AND REPLACED THE STRAP IAW SRM 51-26-00, AND 51-42-10.

Part: TRIPLER — GOUGED (BS 977) · airframe 36,744 hrs · 27,536 cycles

AFTER FUSELAGE, BS 977, STRINGER 27, TRIPLER GOUGED. REMOVED AND REPLACED THE TRIPLER IAW REO 670-53-61-56,2 REV A.

Part: SUPPORT BRACKET — CORRODED (BS 969) · airframe 36,744 hrs · 27,536 cycles

AFT LOWER FUSELAGE WING TO BODY FAIRING SUPPORT L BRACKET AT BS 939.00 AND STGR 27 HAS SIGNS OF CORROSION. REMOVED AND REPLACED SUPPORT BRACKET IAW SRM 51-42-06.

Part: SEAT TRACK — CORRODED (NOT REPORTED) · airframe 36,744 hrs · 27,536 cycles

RIGHT NR 2 SEAT TRACK HAS SIGNS OF CORROSION. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 36,744 hrs · 27,536 cycles

BS 280 FLOORBEAM HAD SIGNS OF CORROSION. REMOVED AND REPLACED THE FLOORBEAM IAW SRM 51-42-06, 51-42-13, 51-42-21, AND 53-11-41.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 36,744 hrs · 27,536 cycles

LEFT AND RIGHT INBD NR 3 SEAT TRACKS HAVE SIGNS OF CORROSION. REMOVED AND REPLACED THE SEAT TRACK IAW REO 670-53-00-013, AND AMM 53-00-49.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 36,744 hrs · 27,536 cycles

FLOORBEAM ANGLE AT RBL 26, BS 280 CRACKED. REMOVED AND REPLACED THE FLOORBEAM ANGLE IAW SRM 51-42-06, 51-42-13, AND 51-25-16.

Part: BRACKET — OUT OF POSITION (BS 1015-1031) · airframe 33,480 hrs · 24,761 cycles

TWO MISLOCATED BRACKETS ON STRINGER 14R BETWEEN BS 1015 AND 1031. REPAIRED IAW REO 670-53-61-1277.

Part: FLOORBEAM — CORRODED (BS 1031) · airframe 33,480 hrs · 24,761 cycles

CORROSION FOUND ON FLOORBEAM AT LBL 9.00 BS 1031. NO DAMAGE ALLOWED IN THIS AREA.

Part: HANDLE — DEFECTIVE (APX DOOR) · airframe 32,930 hrs · 24,343 cycles

PASSENGER OUTER DOOR HANDLE CAUTION MSG INTERMITTENT DURING FLT. DEFERRED PASSENGER OUTER DOOR HANDLE IAW MEL 52-70-01, CAT A.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 32,857 hrs · 24,088 cycles

STRINGER 26R IN AVIONICS BAY IS CORRODED, BETWEEN FS 333 & 349.00. R & R STRINGER 26R IAW SRM 51-42-06 & 51-42-21.

Part: FRAME — CORRODED (FUSELAGE) · airframe 32,857 hrs · 24,088 cycles

FS 364 FRAME IN AVIONICS BAY IS CORRODED. CUT OUT DAMAGED SECTION OF FRAME. CUT & INSTALLED NEW SECTION OF FRAME WITH REPAIR SPLICES & DOUBLERS IAW REO 670-53-21-687 DATED 03 AUG 2012 & REO 670-53-21-1291 DATED 26 APR 2016.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 32,857 hrs · 24,088 cycles

STRINGER 26L IS CORRODED, BETWEEN FS 333 & 349. R & R STRINGER IAW SRM 51-42-06 & 51-42-21.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 32,857 hrs · 24,088 cycles

MAIN AVIONICS DOOR SURROUND STRUCTURE FWD LT INBD INTERCOSTAL HAS CORROSION. R & R INTERCOSTAL IAW SRM 51-42-06 & 51-42-21.

Part: HANDLE — CORRODED (PAX DOOR) · airframe 32,857 hrs · 24,088 cycles

PASSENGER DOOR, EXTERNAL HANDLE FLAPPER DOOR IS CRACKED. REMOVED PAX DOOR EXTERNAL FLAPPER DOOR HANDLE & INSTALLED SERVICEABLE PAX DOOR EXTERNAL FLAPPER DOOR HANDLE IAW AMM 51-42-06, 51-40-11 & 20-60-06.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 32,857 hrs · 24,088 cycles

FORWARD RT FLOOR SILL HAS SIGNS OF CORROSION. REMOVED RT FLOOR SILL & INSTALLED SERVICEABLE SILL IAW SRM 51-42-06, 51-42-13 & 51-42-21.

Part: SKIN — CORRODED (FUSELAGE) · airframe 32,857 hrs · 24,088 cycles

CORROSION ON INNER FUSELAGE SKIN AT FRAME 364 & STRINGER 26R. REMOVED CORROSION, REMAINING MATERIAL OUT OF LIMITS, FABRICATED AND INSTALLED SHIM IAW REO 670-53-1290 DATED 4 21 16 & SRM 53-21-01 & 53-00-00. NDT PERFORMED.

Part: FRAME — CORRODED (FUSELAGE) · airframe 32,857 hrs · 24,088 cycles

FS 295 FRAME IS CORRODED, BETWEEN STRINGER 25L & 26L, BETWEEN 25R & 24R, & BETWEEN 27R & 26R. CUT OUT DAMAGED SECTION OF FRAME 295, FROM 25L TO 25R. CUT & INSTALLED NEW SECTION OF FRAME WITH REPAIR PARTS IAW REO 670-53-21-799 DATED 30 JAN 2012.

Part: FITTING — CORRODED (GALLEY) · airframe 32,857 hrs · 24,088 cycles

GALLEY 2 HAS ONE CORRODED FOOT. REMOVED CORRODED GALLEY 2 FOOT. INSTALLED SERVICEABLE FOOT IAW AMM 20-21-00.

Part: FRAME — CORRODED (FUSELAGE) · airframe 32,857 hrs · 24,088 cycles

FS FRAME 319 IS CORRODED, BETWEEN STRINGER 25L & 26R. CUT OUT DAMAGED SECTION OF FRAME 319, FROM STRINGER 25L - 26R. CUT & INSTALLED NEW FRAME SECTION, PN SH670-31355-1S, WITH REPAIR PARTS IAW REO 670-53-21-799 DATED 30 JAN 2012.

Part: FITTING — CORRODED (GALLEY) · airframe 32,857 hrs · 24,088 cycles

GALLEY 1 HAS TWO CORRODED FEET. REMOVED GALLEY 1 CORRODED FEET & DOUBLERS. INSTALLED SERVICEABLE FEET & DOUBLERS IAW CMM 25-33-42.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 32,857 hrs · 24,088 cycles

MAIN AVIONICS DOOR SURROUND STRUCTURE AT FS 364, FWD RT INBD INTERCOSTAL HAS CORROSION. R & R INTERCOSTAL IAW SRM 51-42-06 & 51-42-21.

Part: PANEL — GOUGED (ZONE 400) · airframe 32,857 hrs · 24,088 cycles

LEFT LOWER COWL GANG DRAIN PANEL GOUGED. BLENDED DAMAGE, FOUND TO BE OUT OF LIMITS. FABRICATED & INSTALLED DOUBLER IAW SRM 54-23-00, 51-42-06, 51-25-06 & AMM 51-21-10. NDT PERFORMED.

Part: STRINGER — DAMAGED (FUSELAGE) · airframe 32,857 hrs · 24,088 cycles

STRINGER 7L IN AFT EQUIPMENT BAY HAS BROKEN BRACKET & CHAFE DAMAGE. ACCOMPLISHED MAJOR REPAIR TO STRINGER 7L AT FRAME STATION 1144.00 CHAFE DAMAGE BY REMOVING DAMAGED STRINGER, PERFORMING NDT, FABRICATING REPAIR PARTS & INSTALLING A NEW STRINGER & REPAIR PARTS IAW REO 670-53-61-1230 REV DATED 2016 04 14 & INCORPORATED IS67053610094. NDT PERFORMED.

Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 32,857 hrs · 24,088 cycles

FS 280 BULKHEAD WEBS, LT & RT ARE CORRODED. REMOVED DAMAGED AREA, FABRICATED & INSTALLED REPAIR PARTS IAW REO 670-53-11-594 & SRM 51-42-06.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 32,857 hrs · 24,088 cycles

AFT COCKPIT 1/4 TURN ANGLE IS CORRODED. REMOVED AFT COCKPIT 1/4 TURN ANGLE, PN CC670-33292-13S, & INSTALLED SERVICEABLE AFT COCKPIT 1/4 TURN ANGLE IAW SRM 51-42-06, 51-42-13 & 51-40-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 32,857 hrs · 24,088 cycles

RIGHT & LEFT 280 BEAM IS CORRODED. ACCOMPLISHED PERMANENT REPAIR TO THE BEAM TO CORRECT CORROSION, BY R & R THE LT & RT 280 BEAMS IAW SRM 51-42-21, 53-11-41, 51-42-13, 53-11-41, 51-40-11, 51-42-22 & AMM 20-70-00 & SB 670-BA-53-026 REV B DATED 05 2006. NDT PERFORMED.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 32,857 hrs · 24,088 cycles

FLOORBEAM AT LBL 27, BETWEEN FS 1015 & 1031 IS CORRODED. ACCOMPLISHED MAJOR REPAIR TO THE FLOORBEAM BY CUTTING OUT CORRODED SECTION, PERFORMING NDT, FABRICATING REPAIR PARTS & INSTALLING THEM IAW REO 670-53-00-029 REV A DATED 2010 08 31 & AMM 51-21-01, 20-70-00, SRM 51-42-21, 51-25-16, 51-21-11, 51-25-06, 51-42-06, 53-00-41 & 51-25-06. NDT PERFORMED.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 32,857 hrs · 24,088 cycles

PASSENGER DOOR FWD & AFT CLOSE OUT ANGLES HAVE SIGNS OF CORROSION. REMOVED FWD CLOSE OUT ANGLE & INSTALLED SERVICEABLE CLOSE OUT ANGLE. AFT CLOSE OUT ANGLE DAMAGE FOUND TO BE IN PAINT, PRIMED & TOP COATED IAW SRM 51-42-21, 51-42-06, 51-25-06, 51-25-16 & 53-21-23.

Part: ANGLE — CORRODED (PAX DOOR) · airframe 32,857 hrs · 24,088 cycles

PASSENGER DOOR FWD & MID-CAPS HAVE SIGNS OF CORROSION. R & R PAX DOOR FWD & MID-CAPS, PN SH670-31821-5 & PN SH670-31825-9S, IAW SRM 51-42-06, 51-41-02, 51-41-00 & 51-40-11. WO 80394, WC 8067.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 32,857 hrs · 24,088 cycles

STRINGER 25R IN MAIN AVIONICS COMPARTMENT, BETWEEN FS 295 & 333 HAS SIGNS OF CORROSION. R & R STRINGER 25R IAW SRM 51-42-06 & 51-42-21. WO 80394 & WC 1126.

Part: DOUBLER — GOUGED (FUSELAGE) · airframe 32,857 hrs · 24,088 cycles

THE DOUBLER & TRIPLER FROM PREVIOUS REPAIR AT FS 977, LOWER FUSELAGE SKIN IS GOUGED. REMOVED EXISTING REPAIR PARTS. FABRICATED DOUBLER & TRIPLER & INSTALLED IAW REO 670-53-61-562 REV-A DATED 01 MAR 2010. ADDITIONALLY ACCOMPLISHED MODSUM IS670538200021, REV C TO AFT FAIRING C CHANNEL. WO 80394, WC 1108.

Part: WIRE HARNESS — DISCONNECTED (CABIN) · airframe 31,969 hrs · 23,611 cycles

CEILING EMER LIGHT AT ROW 15 INOPERATIVE. CONNECTED HARNESS TO PLUG. OPERATIONS CHECKED GOOD AT THIS TIME IAW AMM 33-51-00.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 31,814 hrs · 23,497 cycles

PASSENGER DOOR CAUTION MSG ON LANDING. PERFORMED INSPECTION OF THE PAX DOOR PROXIMITY SENSORS & PROXIMITY SWITCH IAW AMM 52-70-04. PERFORMED OPERATIONS CHECK IAW AMM 52-70-00. OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,138 hrs · 22,980 cycles

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

Part: DOOR — OPEN (GROUND POWER) · airframe 31,045 hrs · 22,902 cycles

GPU DOOR OPEN IN FLIGHT. PERFORMED INSPECTION OF GPU DOOR & SURROUNDING AREA IAW AMM 05-21-00. ZONAL INSPECTION, NO DEFECTS OR DAMAGE NOTED AT THIS TIME.

Part: CONNECTOR — DIRTY (ANTENNA) · airframe 30,952 hrs · 22,836 cycles

GLD UNSAFE CAUTION ON TAKEOFF. CLEANED ANTENNA COAX CONNECTORS. PERFORMED BIT TEST. OPERATIONS CHECKED GOOD IAW AMM 34-44-01.

Part: PROXIMITY SWITCH — DIRTY (PAX DOOR) · airframe 30,122 hrs · 22,197 cycles

PASSENGER DOOR LATCH CAUTION MSG DURING FLIGHT. INSPECTED & CLEANED PAX DOOR PROX SWITCHES. PERFORMED OPERATIONS CHECK IAW AMM 52-11-00. OPERATIONS CHECKED GOOD AT THIS TIME.

Part: SENSOR — DIRTY (PAX DOOR) · airframe 30,021 hrs · 22,119 cycles

PASSENGER DOOR MASTER WARNING ON LANDING. CLEANED PAX DOOR SENSORS, NO FAULTS SHOWN. PERFORMED OPERATIONS CHECK IAW AMM 52-11-00. OPERATIONS CHECKED GOOD.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 30,011 hrs · 22,112 cycles

PASSENGER DOOR MASTER CAUTION WARNING ON TAXI. INSPECTED PAX DOOR, NO DEFECTS NOTED. OPERATIONS CHECKED GOOD IAW AMM 52-70-00.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,003 hrs · 22,107 cycles

CEILING EMER LIGHT AT ROW 15 INOPERATIVE. DEFERRED CEILING FLOOD LIGHT IAW MEL 33-51-01B CAT C.

Part: HOLDER — LOOSE (CABIN) · airframe 29,890 hrs · 22,023 cycles

LIFE VEST HOLDER AT SEAT 5C HANGING LOOSE. SECURED LIFE VEST UNDER SEAT 5C IAW AMM 25-61-03. ALL OPERATIONS CHECKED GOOD.

Part: PROXIMITY SENSOR — OUT OF ADJUST (PAX DOOR) · airframe 29,884 hrs · 22,018 cycles

PASSENGER DOOR LATCH CAUTION MSG IN FLIGHT. INSPECTED PX 101 WIRING, FOUND NO DEFECTS. ADJUSTED PX 101 IAW AMM 52-70-04. OPERATIONS CHECKED GOOD, NO MSG NOTED AT THIS TIME.

Part: COVER — UNSECURE (EMERGENCY EXIT) · airframe 29,690 hrs · 21,875 cycles

EMERGENCY EXIT HANDLE COVER AT SEAT 12A NEEDS TO BE SECURED. SECURED EMER EXIT HANDLE COVER AT SEAT 12A IAW SRM 51-22-00. NO DEFECTS NOTED.

Part: WIRE — LOOSE (PAX DOOR) · airframe 29,661 hrs · 21,851 cycles

PASSENGER DOOR MASTER CAUTION ON TAKEOFF ROLL. INSPECTED PAX DOOR WIRING, HARNESS & PX 101. FOUND LOOSE WIRE INSIDE DOOR, SECURED WIRE. REMOVED, INSPECTED & CLEANED DOOR HARNESS. REINSTALLED DOOR HARNESS IAW AMM 52-11-00 & AMM 52-70-04. OPERATIONS CHECKED GOOD.

Part: LINKAGE — LACK OF LUBE (PAX DOOR) · airframe 29,522 hrs · 21,746 cycles

PAX DOOR HANDLE BECAME UNSTOWED DURING TAXI, CAUSING MASTER CAUTION MSG. LUBRICATED PAX DOOR LINKAGE IAW AMM 12-20-5. PERFORMED FUNCTIONAL CHECK OF PAX DOOR HANDLE WITH FORCE GAUGE. OPERATIONS CHECKED & FUNCTIONAL CHECKED GOOD IAW AMM 52-11-03.

Part: PROXIMITY SWITCH — DIRTY (PAX DOOR) · airframe 29,488 hrs · 21,723 cycles

MASTER CAUTION ON PAX DOOR AT LANDING. INSPECTED PX25, CLEANED & OPERATIONS CHECKED DOOR IAW AMM 52-11-00. ACFT OK FOR SERVICE.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 29,403 hrs · 21,658 cycles

PAX DOOR WARNING DURING TAXI. CYCLED PAX DOOR SEVERAL TIMES. PERFORMED DOOR SENSOR TEST ON MDC IAW AMM 32-61-01. OPERATIONS CHECKED GOOD IAW AMM 52-11-00, NO MSG NOTED.

Part: FASTENER — UNSECURE (HYD ACCESS PANEL) · airframe 29,066 hrs · 21,392 cycles

LOUD VIBRATION THRU OUT CABIN, LOUDER IN AFT CABIN. INSPECTED ACFT & FOUND LOWER HYD ACCESS PANEL 195AB FASTENERS UNSECURE. SECURED PANEL 195AB IAW AMM 53-52-32. INSPECTED PANEL FOR DEFECTS, NONE NOTED.

Part: LIGHT — INOPERATIVE (PAX DOOR) · airframe 29,056 hrs · 21,383 cycles

PAX DOOR STAIR LIGHT INOPERATIVE. DEFERRED PAX DOOR LIGHT IAW MEL 33-21-02 CAT D.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,012 hrs · 21,351 cycles

PAX DOOR STAIR ENTRANCE LIGHT INOPERATIVE. DEFERRED STAIR ENTRANCE LIGHT IAW MEL 33-21-02 CAT D.

Part: CABLE — BROKEN (DOOR) · airframe 28,600 hrs · 21,027 cycles

ICE BREAKER CABLE BROKEN. R & R ICE BREAKER CABLE IAW AMM 52-11-15.

Part: LENS — CRACKED (SERVICE DOOR) · airframe 28,507 hrs · 20,951 cycles

SERVICE DOOR EXIT LENS CRACKED. R & R SERVICE DOOR EXIT LENS IAW AMM 33-51-05. OPERATIONS CHECKED GOOD.

Part: PLACARD — WORN (PAX DOOR) · airframe 28,507 hrs · 20,954 cycles

PAX DOOR OPEN ARROW PLACARD WORN. R & R PAX DOOR ARROW PLACARD IAW AMM 20-60-04.

Part: PLACARD — WORN (SERVICE DOOR) · airframe 28,507 hrs · 20,954 cycles

SERVICE DOOR OPEN ARROW WORN. R & R SERVICE DOOR OPEN ARROW PLACARD IAW AMM 20-60-04.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 27,913 hrs · 20,503 cycles

FLOOR SUPPORT ANGLE ON FS 280 BEAM FWD SIDE HAS CORROSION. R & R FLOOR SUPPORT ANGLE ON FWD SIDE OF 280 BEAM IAW SRM 51-42-06.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 27,913 hrs · 20,503 cycles

SERVICE DOOR THRESHOLD CORRODED. R & R SERVICE DOOR THRESHOLD IAW AMM 25-33-01.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 27,913 hrs · 20,503 cycles

ANGLE IN FRONT OF 280 BEAM CTR IS CORRODED. R & R ANGLE IAW SRM 51-42-06 & 51-42-20.

Part: AHRS — FAILED (NR 1) · airframe 27,740 hrs · 20,366 cycles

NUMBER 1 AHRS FAILED ON TAKEOFF. R & R NR 1 AHRS IAW CRJ700 AMM 34-21-01. PERFORMED OPERATIONS CHECKED, NO DEFECTS NOTED AT THIS TIME.

Part: WARNING LIGHT — FALSE ACTIVATION (PAX DOOR) · airframe 27,468 hrs · 20,165 cycles

PAX DOOR MASTER WARNING. PERFORMED OPS CHECK OF PAX DOOR SYS IAW AMM 52-70-04. OPS CHECKED GOOD.

Part: HANDLE — DAMAGED (PAX DOOR) · airframe 27,468 hrs · 20,165 cycles

PAX DOOR HANDLE MASTER CAUTION IN FLIGHT AND MASTER WARNING AFTER LANDING. INSPECTED PAX DOOR. FOUND HANDLE TO BE DAMAGED. CUT OFF PAX DOOR HANDLE SO DOOR OPERATES NORMALLY FROM INSIDE. OPERATION AND ALL LOCKING INDICATION IS GOOD. FOUND OK FOR A 1 TIME FERRY.

Part: LIGHT — INOPERATIVE (AFT CABIN) · airframe 27,382 hrs · 20,097 cycles

AFT EMERGENCY CEILING FLOODLIGHT INOPERATIVE.

Part: WARNING LIGHT — FALSE ACTIVATION (PAX DOOR) · airframe 27,356 hrs · 20,077 cycles

PAX DOOR MASTER WARNING ON TAXI. INSPECTED AND CLEANED PAX DOOR SENSORS PX23, PX26, PX46, PX101, PX107 AND INSPECTED DOOR HARNESS. FOUND ALL SWITCHES/ HARNESSS TO BE IN GOOD CONDITION IAW AMM 52-70-00.OP'S CHECK IAW AMM 52-70-04. OP'S CHECK GOOD AT THIS TIME.

Part: HOOK AND LOOP — LOOSE (EMERGENCY EXIT) · airframe 27,239 hrs · 19,988 cycles

RT OVERWING EMERGENCY EXIT DOOR HANDLE COVER LOOSE. SECURED THE HOOK AND LOOP IAW AMM 33-50-00

Part: HOOK AND LOOP — LOOSE (HANDLE) · airframe 27,157 hrs · 19,921 cycles

HOOK AND LOOP ON RT SIDE EMERGENCY HANDLE, LOOSE. REAPPLIED HOOK AND LOOP AND SECURED RT SIDE EMERGENCY HANDLE IAW AMM 51-22-61.

Part: CABLE — OUT OF ADJUST (PAX DOOR) · airframe 24,926 hrs · 17,905 cycles

KICK STAND ON MAIN CABIN DOOR DID NOT COME OUT WHEN DOOR WAS OPENED MAIN CABIN DOOR HIT GROUND WHEN OPENED. ADJUSTED CABLE ON PAX DOOR SUPPORT WHEEL IAW AMM 52-11-13. OPS CHECKED GOOD.

Part: WARNING LIGHT — FALSE INDICATION (YAW DAMPER) · airframe 26,863 hrs · 19,701 cycles

NR 1 YAW DAMPER INOPERATIVE STATUS MESSAGE DURING TAXI. SWAPPED YAW DAMPER SWITCHES NR 1 & NR 2, FOR TROUBLESHOOTING IAW AMM 20-41-00. REPOSITIONED SWITCHES TO ORIGINAL POSITIONS IAW 20-51-00. PERFORMED OP'S CHECK OF YD1 AND YD 2, IAW AMM 22-22-04. OP'S CHECKED GOOD.

Part: HOOK AND LOOP — LOOSE (EMERGENCY EXIT) · airframe 26,774 hrs · 19,632 cycles

HOOK AND LOOP LOOSE ON RT EMERGENCY EXIT DOOR HANDLE COVER. R & R FAULTY HOOK AND LOOP ON RT EMERGENCY EXIT HANDLE COVER IAW AMM 25-26-01.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 25,118 hrs · 19,333 cycles

EXIT ROW CEILING F/A CALL LIGHT BURNED OUT. R & R F/A CALL LIGHT IN EMERGENCY EXIT SIGN IAW AMM 33-22-05.

Part: SEAL — DIRTY (PAX DOOR) · airframe 26,028 hrs · 19,061 cycles

PAX DOOR SQUEALS LOUDLY. CLEANED SEAL, OP'S CHECKED GOOD, NO DEFECTS NOTED.

Part: WARNING MESSAGE — FALSE ACTIVATION (CARGO DOOR) · airframe 26,021 hrs · 19,056 cycles

FWD CARGO DOOR CAUTION MESSAGE AND PROX 2 FAIL. INSPECTED FWD CARGO DOOR HARNESS, OPENED AND CLOSED DOOR, ALL OPERATIONS ARE NORMAL. NO EICAS MESSAGE AT THIS TIME IAW AMM 52-70-00.

Part: COVER — OUT OF POSITION (EMERGENCY LIGHT) · airframe 25,850 hrs · 18,924 cycles

SERVICE AND PAX DOOR EMERGENCY LIGHT COVER ON LT, FACING WRONG WAY. SECURED SERVICE AND PAX DOOR EMERGENCY LIGHT COVER TO THE CORRECT WAY IAW AMM 33-51-13.

Part: SEAL — DIRTY (PAX DOOR) · airframe 2,486,208 hrs · 18,199 cycles

PAX DOOR SQUEAL. CLEANED PAX DOOR SEAL AND OPS CHECK IAW AMM 52-11-07, OP'S CHECKED GOOD AT THIS TIME.

Part: SEAL — LEAKING (PAX DOOR) · airframe 24,683 hrs · 18,063 cycles

PAX DOOR HAS LOUD SQUEAL UNTIL 13000 FT. APPLIED SEAL ON PAX DOOR IAW AMM 52-11-07.

Part: FRAME — CORRODED (BS 310) · airframe 23,369 hrs · 17,130 cycles

CORROSION FOUND ON FRAME AT FS 310 FROM S8R - S25L. REPAIRED IAW REO 670-53-21-790.

Part: STRINGER — CORRODED (BS 310) · airframe 23,363 hrs · 17,124 cycles

CORROSION FOUND ON S26R AT BS 310. STRINGER REPAIRED IAW SRM 53-00-03-201-001-A01.

Part: FRAME — CORRODED (BS 333) · airframe 23,363 hrs · 17,124 cycles

MAIN AVIONICS COMPARTMENT FRAME BS 333 BETWEEN S25 AND 26R CORRODED. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. NO DAMAGE ALLOWED IAW SRM FIG 53-21-06-991-840 AND 53-21-06-991-841. REPAIRED IAW REO 670-53-21-800.

Part: FRAME — CORRODED (BS 310) · airframe 23,363 hrs · 17,124 cycles

CORROSION FOUND ON FRAME AT FS 310 FROM S25R - 25L. REPAIRED IAW REO 670-53-21-790.

Part: STRINGER — CORRODED (BS 310) · airframe 23,363 hrs · 17,124 cycles

CORROSION FOUND ON STRINGER 26 RT AT FS 310. REMOVED STRINGER SPLICE IAW SRM 51-42-06-001-001. PERFORMED CUTOUT OF STRINGER SECTION IAW SRM 53-00-03-201-001-A01. REMOVED DAMAGED SECTION. REFORMED EDDY CURRENT INSPECTION OF CUTOUT IAW SRM 53-00-03-201-001-A01, PARA 4A (3) IAW NDTM PART 1, 51-20-006-250. NO INDICATIONS NOTED. LOCATED AND DRILLED NEW STRINGER SPLICE AND INSTALLED IAW SRM 51-40-11-001-001 AND SRM 51-42-06-001-001-CRJ700.

Part: WEB — CORRODED (BS 280) · airframe 23,363 hrs · 17,124 cycles

LEFT WEB AT BS 280.00 CORRODED. REPAIRED IAW REO 670-53-11-594.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 23,363 hrs · 17,124 cycles

FS 280.00 FLOORBEAM TEE CORRODED, REPAIRED IAW REO 670-53-11-047 AND REO 670-53-11-047, REV E.

Part: ANGLE — CORRODED (SERVICE DOOR) · airframe 23,363 hrs · 17,124 cycles

SERVICE DOOR LOWER ANGLE FWD SECTION CORRODED. REMOVED AND INSTALLED NEW ANGLE IAW SRM 51-42-06-001-001-A01.

Part: WEB — CORRODED (BS 280) · airframe 23,363 hrs · 17,124 cycles

RIGHT WEB AT FS 280 CORRODED INBD SECTION. INSTALLED WEB AND SPLICE STRAP IAW REO 670-53-11-594.

Part: ANGLE — CORRODED (FLOOR SUPPORT) · airframe 23,363 hrs · 17,124 cycles

CORROSION ON COCKPIT FLOOR SUPPORT ANGLE. REMOVED FWD REINFORCING ANGLES BETWEEN FLOOR SUPPORT ANGLE AND FLOOR SIDE SUPPORT STRUCTURE. INSTALLED REINFORCING ANGLES LT & RT IAW SRM 51-42-21-001-001-A02 & 51-42-22-001-001-A01.

Part: HINGE FITTING — CORRODED (PAX DOOR) · airframe 23,363 hrs · 17,124 cycles

INSIDE ASD AT HINGE END 2 CLIPS ARE CORRODED AT REF FS 318. REMOVED CORRODED CLIPS FROM ASD AT HINGE END. INSTALLATION OF NEW CLIPS REQUIRED IAW SRM 51-42-06-001-001-A01. OK TO INSTALL CG161726 01/13/12. INSTALLED 2 EA CLIPS AT HINGE END AND ON ASD SRM 51-42-06-001-001-A01. THIS REPAIR REQUIRES MAJOR/MINOR CLASSIFICATION IAW ASA SOP 5702. THIS REPAIR IS CLASSIFIED AS A MINOR REPAIR IAW ASA SOP 5702. (SDR CLOSED)

Part: SEAT TRACK — CORRODED (BS 581-683) · airframe 23,363 hrs · 17,124 cycles

MAIN CABIN BETWEEN FS 581.00 & 683.00, RBL 9.00 SEAT TRACK HAS CORROSION. FOUND TO BE OUT OF LIMITS, FABRICATED NEW PART IAW REO670-53-343. INSTALLED SEAT TRACK IAW AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 736.05) · airframe 23,363 hrs · 17,124 cycles

RT SIDE SEAT TRACK CORRODED AT FS 736.05. COMPLIED WITH EC/TC REO 670-53-00-343 AND REO 670-53-00-343 REV A.

Part: HINGE — CORRODED (PAX DOOR) · airframe 23,363 hrs · 17,124 cycles

INSIDE ASD ON HINGE END FWD CORNER PIECE HAS CORROSION. REMOVED CORNER PIECE IAW SRM 51-40-11-001-001-A01. INSTALLED CORNER PIECE IAW SRM 51-42-06-001-001-A01.

Part: DOOR FRAME — CORRODED (BS 280) · airframe 23,363 hrs · 17,124 cycles

LEDT SIDE DOOR POST AT BOTTOM END HAS CORROSION DAMAGE FS 280.00 AT LBL 9.0. REPAIRED IAW REO 670-53-11-678.

Part: HINGE — CORRODED (PAX DOOR) · airframe 23,363 hrs · 17,124 cycles

INSIDE ASD AT HINGE END TWO CLIPS ARE CORRODED AT REF FS 340.563. REMOVED AND REPLACED CLIPS IAW SRM 51-42-06-001-001-A01.

Part: FLOOR PANEL — CRACKED (E/E BAY) · airframe 23,363 hrs · 17,124 cycles

LEFT FWD ELECTRICAL BAY FLOOR CRACKED AT FS 193. REPAIRED IAW REO 670-53-11-509.

Part: SEAT TRACK — CORRODED (BS 785.15) · airframe 23,363 hrs · 17,124 cycles

LEFT SEAT TRACK CORRODED AT FS 785.15. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. MAX MATERIAL REMOVAL ID .028. MAX ALLOWED MATERIAL REMOVAL IS .035 (DIM.V) FOUND TO BE WITHIN LIMITS IAW SRM 53-41-49-101-001-A01.

Part: SEAT TRACK — CORRODED (BS 708) · airframe 23,363 hrs · 17,124 cycles

RIGHT SEAT TRACK CORRODED AT FS 708.00. REMOVED SEAT TRACK IAW SRM 51-41-02-001-001-A01. COMPLIED WITH EC/TC REO 670-53-00-343 AND GENERIC REO 670-53-00-343, REV A. INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-400-801.

Part: ANGLE — CORRODED (BS 310-349) · airframe 23,363 hrs · 17,124 cycles

ASD SILL PLATE AREA CORRODED FROM FS 310.00 - 349. FOUND MOUNTING ANGLE TO HAVE EXCESSIVE CORROSION, FOUND TO BE OUT OF LIMITS IAW SRM 53-21-23. REMOVED MOUNTING ANGLE IAW SRM 51-42-06. LOCATED ALL FASTENER HOLES IN SERVICEABLE MID CAP ANGLE IAW SRM 51-40-11-001-001-A01. INSTALLED NUTPLATES CAP ANGLES AND REINSTALLED FWD AND AFT CAP ANGLES SRM 51-21-16.

Part: SEAT TRACK — CORRODED (BS 863) · airframe 23,363 hrs · 17,124 cycles

RIGHT SEAT TRACK CORRODED AT FS 863.00 AREA. REMOVED CORROSION IAW SRM 51-21-06-001-A01, MAX MATERIAL REMOVED IS .020 MAX ALLOWED MATERIAL. REMOVED .035 (U) WITHIN LIMITS IAW SRM 53-51-49-101-001-A01.

Part: SEAT TRACK — CORRODED (BS 553-565) · airframe 23,363 hrs · 17,124 cycles

RIGHT SEAT TRACK CORRODED AT FS 553.00 THRU FS 565.00. REMOVED SEAT TRACK IAW SRM 51-41-02-001-001-A01, FOUND TO EXCEED ALLOWABLE LIMITS IAW SRM 53-31-49-101-001-A01. FABRICATED NEW SEAT TRACK IAW REO 670-53-00-343, INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 1000) · airframe 23,363 hrs · 17,124 cycles

SEAT TRACK LBL 9.00 CORRODED AT FS 1000.00 AREA. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. DAMAGE EXCEEDS LIMITS IAW SRM 53-51-49-101-001-A01. INSTALLED SERVICEABLE SEAT TRACK IAW AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 517-565) · airframe 23,363 hrs · 17,124 cycles

SEAT TRACK CORRODED AT FS 517.00 THRU FS 565.00. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01, DAMAGE EXCEEDS LIMITS SRM 53-51-49-101-001-A01. REPLACED SEAT RAIL IAW GREO 670-53-00-343.

Part: SEAT TRACK — CORRODED (BS 736.05) · airframe 23,363 hrs · 17,124 cycles

RIGHT SEAT TRACK CORRODED AT FS 736.05. REMOVED DAMAGE AND FOUND TO BE OUT OF ALLOWABLE LIMITS IAW SRM 53-41-49-101-001-A01. REMOVED SEAT TRACK FROM FS 713 -763, CUT AND DRILLED NEW SEAT TRACK IAW REO 670-53-00-343. INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-400-801.

Part: ANGLE — CORRODED (THRESHOLD) · airframe 23,363 hrs · 17,124 cycles

SERVICE DOOR THRESHOLD SUPPORT NUTPLATE ANGLE CORRODED. REMOVED LIGHT CORROSION, FOUND TO BE WITH IN LIMITS IAW SRM 51-21-06-001-001-A01. TREATED, PRIMED AND PAINTED IAW SRM 51-21-11-001-001-A01, 51-25-06-001-001-A01, 25-16-001-001-A01.

Part: ANGLE — CORRODED (SERVICE DOOR) · airframe 23,363 hrs · 17,124 cycles

SERVICE DOOR LOWER ANGLE FWD SECTION CORRODED. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. FOUND CORROSION TO BE OUT OF LIMITS IAW SRM 53-21-23. REMOVED ANGLE IAW SRM 51-42-06. DRILLED OPS NEW ANGLE IAW SRM 53-40-11-001-601 AND SRM 51-12-12-00-001-001. INSTALLED IAW SRM 51-41-02.

Part: SEAT TRACK — CORRODED (BS 581) · airframe 23,363 hrs · 17,124 cycles

LEFT SEAT TRACK CORRODED AT FS 581.00. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01, MAX MATERIAL REMOVAL IS .018 MAX ALLOWED MAITERIAL REMOVAL IS .035 (DIM. U), FOUND TO BE WITHIN LIMITS OF SRM 53-31-49-101-001-A01.

Part: SEAT TRACK — CORRODED (BS 785.15) · airframe 23,363 hrs · 17,124 cycles

RIGHT SEAT TRACK CORRODED AT FS 785.15. REMOVED SEAT TRACK IAW SRM 51-42-02-001-001-A01. FOUND TO BE OUT OF LIMITS IAW SRM 53-51-49-101-001-A01. FABRICATED AND INSTALLED SEAT TRACK IAW AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 708) · airframe 23,363 hrs · 17,124 cycles

LEFT SEAT TRACK CORRODED AT FS 708.00. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. MAX MATERIAL REMOVAL IS .023 MAX ALLOWABLE MATERIAL REMOVAL IS .035 (DIM. V) FOUND TO BE WITHIN LIMITS IAW SRM 53-41-49-101-001-A01.

Part: SILL — CORRODED · airframe 23,363 hrs · 17,124 cycles

ASD SILL PLATE ANGLE CORRODED. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. FOUND CORROSION TO BE OUT OF LIMITS IAW SRM 53-21-23-101-002-A01. REMOVED AND REPLACEED SILL ANGLE IAW SRM 51-42-06.

Part: WEB — CORRODED (BS 280) · airframe 23,363 hrs · 17,124 cycles

RIGHT WEB AT FS 280.00 CORRODED. REPAIRED IAW REO 670-53-11-594.

Part: SEAT TRACK — CORRODED (BS 469) · airframe 23,363 hrs · 17,124 cycles

RT SIDE SEAT TRACK CORRODED AT FS 469.00. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. MAX MATERIAL REMOVAL 1S .016, MAX ALLOWED MATERIAL REMOVED IS .035 (U) WITHIN LIMITS IAW SRM 53-21-49-101-001-A01.

Part: SEAT TRACK — CORRODED (BS 963-813) · airframe 23,363 hrs · 17,124 cycles

SEAT TRACK RBL 9.00 CORRODED AT FS 693.00 THRU FS 813.00. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. DAMAGE EXCEEDS LIMITS IAW SRM 53-51-49-101-001-A01. REPLACED SEAT TRACK IAW GREO 670-53-00-343.

Part: WEB — CORRODED (BS 280) · airframe 23,363 hrs · 17,124 cycles

LEFT WEB AT FS 280.00 CORRODED INBD SECTION. REPAIRED IAW REO 670-53-11-594.

Part: SEAT TRACK — CORRODED (BS 501-565) · airframe 23,363 hrs · 17,124 cycles

SEAT SEAT TRACK RBL 9.00 CORRODED AT FS 501.00 THRU FS 565.00. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. DAMAGE EXCEEDS LIMITS SRM 53-51-49-101-001-A01. REPLACED SEAT TRACK IAW GREO 670-53-00-343.

Part: SEAT TRACK — CORRODED (BS 830.48) · airframe 23,363 hrs · 17,124 cycles

SEAT TRACK LBL 9.00 CORRODED AT FS 830.48 AREA. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. DAMAGE EXCEEDS LIMITS IAW SRM 53-51-49-101-001-A01. REPLACED SEAT TRACK IAW AMM 53-00-49-400-801.

Part: FLOOR PANEL — CRACKED (BS 193) · airframe 23,363 hrs · 17,124 cycles

RIGHT FWD ELECTRICAL BAY FLOOR CRACKED AT FS 193. REPAIRED IAW REO 670-53-11-509.

Part: SEAL — TORN (LT NACELLE) · airframe 23,363 hrs · 17,124 cycles

LEFT AFT CORE COWL FWD SEAL TORN. REMOVED TORN LT AFT CORE COWL SEAL IAW SRM 51-42-06-001-001-A01. DRILLED UP, TRIMMED TO FIT & DEBURRED IAW SRM 51-40-11-001-001-A01. INSTALL SERVICEABLE SEAL, NG161765 1/12/12. INSTALLED FWD SEAL ON AFT LT CORE COWL IAW SRM 51-42-06-001-001-A01. THIS REPAIR REQUIRES MAJOR/MINOR CLASSIFICATION IAW ASA SOP 5702. THIS REPAIR IS CLASSIFIED AS MAJOR/MINOR REPAIR IAW ASA SOP 5702. (SDR CLOSED)

Part: FRAME — CORRODED (BS 310 S25L-R) · airframe 23,363 hrs · 17,124 cycles

CORROSION FOUND ON FRAME AT FS 310 FROM S25R TO S25L. R & R FRAME SECTION IAW SRM 53-21-06-101-002-A02 AND REO 670-53-21-790.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 23,363 hrs · 17,124 cycles

FS 280.00 FLOORBEAM CORRODED. REMOVED AND REPLACED IAW SRM 51-42-06-001-001-A02, SRM 51-42-03-001-001-A01 & SRM 51-42-21-001-001-A01.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 23,363 hrs · 17,124 cycles

PANEL 141 ALF FWD FLOORBEAM BRACKET AT FS 280 CORRODED. R & R FLOORBEAM BRACKET AT FS 280 IAW SRM 51-42-06.

Part: FLOOR PANEL — CRACKED (BS 193) · airframe 23,363 hrs · 17,124 cycles

LEFT FWD ELECTRICAL BAY FLOOR CRACKED AT FS 193. REPAIRED IAW REO 670-53-11-509.

Part: INTERCOSTAL — CORRODED (BS 364) · airframe 23,363 hrs · 17,124 cycles

CORROSION FOUND FS 364 ON INTERCOSTAL S26L. R & R INTERCOSTAL AT FS 364, STR 26RT IAW SRM 53-21-23.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 23,249 hrs · 17,042 cycles

EMERGENCY LIGHTS WOULD NOT TEST, FOUND F/A SWITCH IN ON POSITION. BROUGHT APU GEN ON LINE, EMERGENCY LIGHTS DISCREPANCY NO LONGER EXISTS.

Part: PLACARD — DETERIORATED (PAX DOOR) · airframe 23,051 hrs · 16,898 cycles

PAX DOOR EXIT PLACARD DETERIORATED. R & R PAX DOOR EXIT PLACARD PLACARD IAW AMM 20-60-04.

Part: WINDOW — BURNED (COCKPIT) · airframe 19,016 hrs · 14,025 cycles

R & R F/O'S WINDOW IAW AMM 56-12-01 REFER TO AFDL 537395-2FOR LEAK AND OPS CHECKS. (CLOSED)

Part: HEATER — BURNED (COCKPIT WINDOW) · airframe 19,016 hrs · 14,025 cycles

AFTER T/O A LOUD POP FROM F/O WINDOW FOLLOWED BY STRONG ELECTRICAL SMELL AND SMALL AMOUNT OF SMOKE. RETURN TO DEPARTURE, ALSO RECEIVED R WINDOW HEAT CAUTION. EMERGENCY DECLARED -- ACFT RETURNED TO DEPARTURE AFTER T/O.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 18,694 hrs · 13,777 cycles

LT AFT EXTERIOR EMERGENCY LIGHT BULB OUT. REPLACED LIGHT BULB ON LT AFT EXTERIOR EMERGENCY LIGHT REF ESON 20-36-00. C/W OPS TEST OF EXTERIOR EMERGENCY LIGHT AMM 33-51-15-710-801. TESTED GOOD.

Part: SEAT TRACK — CORRODED (BS 485-570) · airframe 18,684 hrs · 13,771 cycles

FS485 TO FS570 LT SIDE SEAT RAIL HAS SURFACE CORROSION. CORROSION REMOVED FROM SEAT TRACK AS PER REO 670-53-00-013.

Part: SEAT TRACK — CORRODED (BS 785-863) · airframe 18,684 hrs · 13,771 cycles

FS785.15 TO FS863 RT SIDE SEAT RAIL; FS785.15 AND FS813.70 HAS SURFACE CORROSION. REMOVED CORROSION ON RH SEAT TRACKS AS PER REO 670-53-00-013.

Part: SEAT TRACK — CORRODED (BS 677-830) · airframe 18,684 hrs · 13,771 cycles

FS677 TO FS830, LBL9.0 SEAT TRACK HAS CORROSION AT FS736, 755 AND 813.70. CLEANED CORROSION SEAT TRACK FAILS WITHIN SPECS OF REO 670-53-00-013.

Part: SEAT TRACK — CORRODED (BS 485-570) · airframe 18,684 hrs · 13,771 cycles

FS 485 TO 570, RT SIDE SEAT RAIL; FS490 TO FS570 HAS SURFACE CORROSION. REMOVED CORROSION FROM SEAT RAIL AS PER REO 670-53-00-013.

Part: SEAT TRACK — CORRODED (BS 379-485) · airframe 18,684 hrs · 13,771 cycles

FS379 TO FS485 LT SIDE SEAT RAIL HAS SURFACE CORROSION. CORROSION REMOVED FROM SEAT TRACK AS PER REO 670-53-00-013.

Part: SEAT TRACK — CORRODED (BS 785.15-863) · airframe 18,684 hrs · 13,771 cycles

FS 785.15 TO 863.00; FS 785.15, 797, 813.70 AND 838 HAS SURFACE CORROSION (LT SIDE SEAT RAIL). CORROSION REMOVED FROM LT SIDE SEAT TRACK AS PER REO 670-53-00-013.

Part: SEAT TRACK — DAMAGED (BS 485-581) · airframe 18,684 hrs · 13,771 cycles

FS 485 TO 581 SEAT TRACK AT RBL9.0 HAS CORROSION AT FS 495 AND GOUGES AT FS 511 (FLOOR SEAT TRACK). REMOVE CORROSION AND GOUGES AT FS495 AND FS511. DAMAGE IS WITHIN SPECS OF REO 670-53-00-013. COMPLIED WITH ECTC PER REO 670-53-00-013.

Part: SEAT TRACK — CORRODED (BS 830-977) · airframe 18,684 hrs · 13,771 cycles

SEAT TRACK FS 830 TO 977 LBL 9.0 IS CORRODED BEYOND LIMITS AND NEEDS REPLACING. BLENDED SEAT TRACK AT FS830 TO 997 LBL9.0 AS PER REO 670-53-00-013.

Part: SEAT TRACK — CORRODED (BS 570-677) · airframe 18,684 hrs · 13,771 cycles

FS570 TO FS677 LT SIDE SEAT RAIL; FS581, 613, 629, 677 HAS SURFACE CORROSION. REMOVED CORROSION FROM SEAT TRACK AS PER REO 670-53-00-013.

Part: SEAT TRACK — CORRODED (BS 708-761) · airframe 18,684 hrs · 13,771 cycles

FS708 TO FS761.85 LT SIDE SEAT RAIL; FS708, FS724.08 AND 736.05 HAS SURFACE CORROSION. REMOVED CORROSION FROM SEAT TRACK AS PER REO 670-53-00-013.

Part: SEAT TRACK — CORRODED (BS 830-977) · airframe 18,684 hrs · 13,771 cycles

SEAT TRACK FS830 TO 977, RBL9.0 IS CORRODED BEYOND LIMITS AND NEEDS REPLACING. BLENDED SEAT TRACK AT FS830 TO 977 RBL9.0 PER REO 670-53-00-013.

Part: SEAT TRACK — CORRODED (BS 863-969) · airframe 18,684 hrs · 13,771 cycles

FS863 TO FS969 RT SIDE SEAT RAIL; FS870, 879, 893, 906, 923 HAS SURFACE CORROSION. REMOVED CORROSION ON RH SEAT TRACKS AS PER REO 670-53-00-013.

Part: SEAT TRACK — CORRODED (BS 581-677) · airframe 18,684 hrs · 13,771 cycles

FS 581 TO 677, RBL 9.0 SEAT TRACK IS CORRODED IN SEVERAL PLACES, FS 584, 613, 630 AND 645 (FLOOR SEAT TRACK). REMOVED CORROSION FROM FS584, 613, 630 AND 645 RBL9.0 FLOOR SEAT TRACK AND AREAS ARE WITH SPEC PER REO 670-53-00-013.

Part: SEAT TRACK — CORRODED (BS 379-485) · airframe 18,684 hrs · 13,771 cycles

FS 379 TO 485, RT SIDE SEAT RAIL; FS379 TO 409, 415 TO 437, 450 TO 453, 466 TO 469 AND 480 TO 485, SURFACE CORROSION. CORROSION REMOVED FROM RT SIDE SEAT TRACKS AS PER REO 670-53-00-013.

Part: SEAT TRACK — CORRODED (BS 677-761.85) · airframe 18,684 hrs · 13,771 cycles

FS 677 TO 761.85, RT SEAT (SIDE) RAIL HAS SURFACE CORROSION. CORROSION REMOVED FROM SEAT RAIL AS PER REO 670-53-00-013.

Part: SEAT TRACK — CORRODED (BS 349-455) · airframe 18,684 hrs · 13,771 cycles

FLOOR SEAT TRACK FROM FS 349 TO 455 LBL AND RBL9 ARE CORRODED BEYOND LIMITS AND NEED REPLACING. REMOVED CORRODED FLOOR SEAT TRACK PER AMM 53-00-49-000-801 (CONFIG A03). INSTALLED NEW SECTIONS OF SEAT TRACK PER SRM 51-40-11-001-001-A01, 51-41-02-001-001-A01 AND 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 863-969) · airframe 18,684 hrs · 13,771 cycles

FS 863 TO 969 LT SIDE SEAT RAIL; FS874 TO 880, FS905 TO 917, FS920 AND FS932 HAVE SURFACE CORROSION. CORROSION REMOVED FROM LH SIDE SEAT TRACK AT FS785.15 TO 863.00 AS PER REO 670-53-00-013.

Part: SEAT TRACK — CORRODED (BS 677-830) · airframe 18,684 hrs · 13,771 cycles

FS677 TO FS830, RBL9.0 SEAT TRACK HAS CORROSION AT FS724, 726, 755, 813.70 AND 830.40. REMOVE CORROSION, DAMAGE WAS WITHIN SPEC REF REO 670-53-00-013.

Part: BULKHEAD — CORRODED (BS 280) · airframe 18,684 hrs · 13,771 cycles

FS280 LT BULKHEAD WEB IS CORRODED ON INBD BOTTOM CORNER. REMOVED CORROSION FROM FS280 LH BULKHEAD PER SRM 51-21-06-001-001-A01. REMOVED .002 TO .003 APPROX .038 TO .037 LEFT AFTER BLENDOUT WITHIN LIMITS PER SRM 53-11-10-201-003-A01. ALODINED, PRIMED AND TOP COATED PER AMM 51-21-00-380-801-A01 AND SRM 51-25-06-001-001-A01 AND 51-25-16-001-001-A01.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 18,684 hrs · 13,771 cycles

FS 280 FLOORBEAM AT APPROX LBL 11.0 TO 12.0 IS EXFOLIATED. REMOVED FLOORBEAM PER SRM 51-42-06-001-001-A01, 51-42-13-001-001-A01, & 51-42-21-001-001-A01. FABRICATED NEW SPLICE PER REO 670-53-11-047 REV E. DRILLED NEW FLOORBEAM PER SRM 51-40-11-001-001-A01. ET INSPECTION PER REO 670-53-11-047 REF NDTM 51-20-006. NO DEFECTS NOTED BEYOND CUT LINE. INSTALLED FLOORBEAM PER REO 670-53-11-047 REV E IAW SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01 & 51-23-00-001-001-A01.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 18,684 hrs · 13,771 cycles

FS 280 COCKPIT FLOORBEAM IS CORRODED BEYOND LIMITS IAW SRM 53-00-00-101-001-A01. REMOVE COCKPIT FLOOR SUPPORT IAW CRJ7/9 51-42-06-001-001-A01, 51-42-22-001-001-A01 AND 51-42-21-001-001-A01. DRILLED UP NEW COCKPIT FLOOR SUPPORT IAW SRM 51-40-11-001-001-A01. INSTALLED NEW COCKPIT FLOOR SUPPORT IAW SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01 AND 51-42-22-001-001-A01 AND 51-23-00-001-001-A01.

Part: HANDLE — STIFF (EMERGENCY EXIT) · airframe 18,684 hrs · 13,771 cycles

RT OVERWING EMERGENCY EXIT REQUIRES EXCESSIVE FORCE TO OPERATE THE HANDLE. COMPLIED WITH IAW AMM 52-21-00-000-801, 25-28-09-000-801, 25-28-09-400-801, 52-21-00-820-801, 52-21-00-400-801, 52-21-00-720-801. REMOVED RT EMERGENCY DOOR TO FOM IAW AMM 52-21-00-000-801. REINSTALLED RT EMERGENCY DOOR LINER IAW AMM 25-26-09-000-801. COMPLIED WITH ADJUSTMENT OF RT EMERGENCY DOOR STEPS 1-4(4)(B) AND 4(6)-(10) IAW AMM 52-21-00-820-801. INSTALLED RT EMERGENCY DOOR IAW AMM 52-21-00-400-801. REINSTALLED RT EMERGENCY DOOR LINER IAW AMM 25-26-09-400-801. FUNCTIONAL TEST GOOD ON RT EMERGENCY DOOR IAW AMM 52-21-00-720-801.

Part: HANDLE — STIFF (GALLEY DOOR) · airframe 18,684 hrs · 13,771 cycles

GALLEY SERVICE DOOR REQUIRES EXCESSIVE FORCE TO COMPLETE THE UNLATCH CYCLE. PERFORMED FUNCTIONAL TET OF THE GALLEY SERVICE DOOR IAW AMM 51-41-00-720-801 FUNCTIONAL TEST FAILED EXCESS FORCE TO OPEN GALLEY SERVICE DOOR. ADJUSTED THE GALLEY SERVICE DOOR IAW AMM 52-41-00-820-804. PERFORMED OPS TEST OF THE GALLEY SERVICE DOOR IAW AMM 52-41-00-710-801 OPS TEST GOOD.

Part: WINDOW — FAILED (COCKPIT) · airframe 18,356 hrs · 13,522 cycles

F/O RT SIDE WINDOW SHATTERED. (EMERGENCY DECLARED)

Part: FLASHLIGHT — UNKNOWN (CABIN) · airframe 17,804 hrs · 13,092 cycles

FLASHLIGHT AT FORWARD FLIGHT ATTENDANT STATION REQUIRES REPLACEMENT

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,475 hrs · 12,839 cycles

CEILING EMERGENCY LIGHT 5TH FROM FRONT INOP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,475 hrs · 12,839 cycles

EMERGENCY EXIT SIGN GALLEY RT LWR AFT OF SERVICE DOOR HAS SEVERAL BULBS BURNED OUT.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 15,893 hrs · 11,602 cycles

GI GALLEY LOWER EMERGENCY LIGHT HAS SEVERAL INOP BULBS.

Part: LIGHT — MISSING (CABIN)

FLT 4185 - EMERGENCY LIGHT MISSING AT RT SIDE OF ACFT. REPLACED MISSING LIGHT, OK FOR SERVICE IAW AMM 33-51-01.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 14,835 hrs · 10,822 cycles

EMERGENCY LIGHT IN CEILING AT ROW 16 INOPERATIVE. CABIN EMERGENCY LIGHTS - CEILING LEVEL FLOODLIGHTS. RESECURED EMERGENCY LIGHT IN CEILING AT ROW 16. OPS CHECK GOOD IAW AMM 33-51-09 DEFER CLEARED PLACARD REMOVED. (S)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,853 hrs · 10,142 cycles

AFT SIDE EMERGENCY EXIT LIGHT CENTERLINE AT WING EXIT IS NOT ILLUMINATING.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 13,853 hrs · 10,142 cycles

RIGHT FWD WING EXTERIOR EMERGENCY LIGHT INOP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,853 hrs · 10,142 cycles

LEFT LOWER OVERWING EMERGENCY DOOR EXIT LIGHT INOP.

Part: GLOWSTRIP — DAMAGED (CABIN) · airframe 13,853 hrs · 10,142 cycles

EMERGENCY FLOOR PHOTOLUMINESCENT TRACK DAMAGED IN SEVERAL PLACES. REMOVED EMERGENCY FLOOR PHOTOLUMNESENT TRACK IAW AMM 33-51-01-000-801 DISCARED AND REBUILT IAW CRJ 700 AMM 33-51-01-961-801. INSTALLED AND OPS CHECKED EMERGENCY FLOOR PHOTOLUMNESENT TRACK IAW AMM 33-51-01-400-801 AND 33-51-01-710-801.

Part: DOOR — INOPERATIVE (EMERGENCY EXIT) · airframe 13,853 hrs · 10,142 cycles

RT OVERWING EMERG EXIT DOOR FAILED FUNCTIONAL CK PER 52-840-100.

Part: SEAT TRACK — CORRODED (BS 477-570) · airframe 13,853 hrs · 10,142 cycles

LT SIDEWALL SEAT RAIL FS 477.40 TO FS 570.0 HAS CORROSION DAMAGE. REMOVED CORROSION AND FOUND TO BE WITHIN LIMITS IAW CRJ 700 SRM 53-31-49. APPLIED ALODINE IAW CRJ 700 SRM 51-21-16.

Part: SEAT TRACK — CORRODED (BS 581-693) · airframe 13,853 hrs · 10,142 cycles

LT FLOOR SEAT RAIL FS 581.0 TO FS 693.0 AT LBL 9.0 HAS CORROSION DAMAGE ON RAIL AND HARDWARE.

Part: SEAT TRACK — CORRODED (BS 693-830) · airframe 13,853 hrs · 10,142 cycles

RT FLOOR SEAT RAIL FS 693.0 TO FS 830.40 AT LBL 9.0 HAS CORROSION DAMAGE ON RAIL AND HARDWARE. R & R RT FLOOR SEAT RAIL FS 693.0 TO FS 830.40 AT LBL 9.0 PER CRJ700 MM 53-00-49.

Part: SEAT TRACK — CORRODED (BS 830-985) · airframe 13,853 hrs · 10,142 cycles

LT FLOOR SEAT RAIL FS 830.40 TO FS 985.0 AT LBL 9.0 HAS CORROSION DAMAGE ON RAIL AND HARDWARE. REMOVED CORROSION AND FOUND TO BE WITHIN LIMITS IAW CRJ 700 SRM 53-51-49. APPLIED ALODINE IAW CRJ 700 SRM 51-31-16.

Part: SEAT TRACK — CORRODED (BS 477-581) · airframe 13,853 hrs · 10,142 cycles

LT FLOOR SEAT RAIL FS 477.40 TO FS 581.0 HAS CORROSION DAMAGE ON RAIL AND HARDWARE.

Part: SEAT TRACK — CORRODED (BS 863-969) · airframe 13,853 hrs · 10,142 cycles

LT SIDEWALL SEAT RAIL FS 863.0 TO FS 969.0 HAS CORROSION DAMAGE. REMOVED CORRISION AND FOUND TO BE WITHIN LIMITS IAW CRJ 700 SRM 53-51-49. APPLIED ALODINE IAW CRJ 700 ARM 51-21-16.

Part: SEAT TRACK — CORRODED (BS 693-830) · airframe 13,853 hrs · 10,142 cycles

LT FLOOR SEAT RAIL FS 693.0 TO FS 830.40 AT LBL 9.0 HAS CORROSION DAMAGE ON RAIL AND HARDWARE.

Part: SEAT TRACK — CORRODED (BS 477-581) · airframe 13,853 hrs · 10,142 cycles

RT FLOOR SEAT RAIL FS 477.40 TO FS 581.0 AT LBL 9.0 HAS CORROSION DAMAGE ON RAIL AND HARDWARE. THIS SDR WILL REMAIN OPEN PENDING MAINTENANCE DETERMINATION OF AN APPROPRIATE CORRECTIVE ACTION.

Part: SEAT TRACK — CORRODED (BS 785-863) · airframe 13,853 hrs · 10,142 cycles

RT SIDEWALL SEAT TRACK FS 785.15 TO FS 863.0 HAS CORROSION DAMAGE. REMOVED AND REPLACED RT SIDEWALL SEAT TRACKIAW AMM 53-00-49.

Part: SEAT TRACK — CORRODED (BS 379-477) · airframe 13,853 hrs · 10,142 cycles

LT SIDEWALL SEAT RAIL FS 379.0 TO FS 477.40 AT HAS CORROSION DAMAGE. REMOVED CORROSION AND FOUND TO BE WITHIN LIMITS IAW SRM 53-21-49. APPLIED ALODINE IAW CRJ 700 SRM 51-21-16.

Part: SEAT TRACK — CORRODED (BS 785-863) · airframe 13,853 hrs · 10,142 cycles

LT SIDEWALL SEAT RAIL FS 785.15 TO FS 863.0 HAS CORROSION DAMAGE. REMOVED AND REPLACED, LT SIDEWALL SEAT TRACK IAW AMM 53-00-49.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 13,853 hrs · 10,142 cycles

RIGHT SIDEWALL SEAT RAIL FS 570.0 TO FS 708.0 HAS CORROSION DAMAGE. REMOVED CORROSION AND FOUND TO BE WITHIN LIMITS IAW CRJ 700 SRM 53-31-49. APPLIED ALODINE IAW CRJ 700 SRM 51-21-16. SUPPLEMENTAL SDR CLOSED 2/12/08.

Part: SEAT TRACK — CORRODED (BS 347-477) · airframe 13,853 hrs · 10,142 cycles

LT FLOOR SEAT RAIL FS 347.0 TO FS 477.0 AT LBL 9.0 HAS CORROSION DAMAGE ON TRACK AND HARDWARE.

Part: SEAT TRACK — CORRODED (BS 708-761) · airframe 13,853 hrs · 10,142 cycles

LT SIDEWALL SEAT TRACK FS 708.0 TO FS 761.85 HAS CORROSION DAMAGE. REMOVED AND REPLACED LT SIDEWALL SEAT TRACK IAW AMM 53-00-49.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 13,853 hrs · 10,142 cycles

RIGHT SIDEWALL SEAT RAIL FS 708.0 TO FS 761.85 HAS CORROSION DAMAGE. REMOVED AND REPLACED RT SIDEWALL SEAT RAIL FS 708.0 TO 761.85 IAW CRJ 700 AMM 53-00-49. TO7011593 02/12/08. SUPPLEMENTAL SDR CLOSED 2/14/08.

Part: SEAT TRACK — CORRODED (BS 581-693) · airframe 13,853 hrs · 10,142 cycles

RT FLOOR SEAT RAIL FS 581.0 TO FS 693.0 AT LBL 9.0 HAS CORROSION DAMAGE ON RAIL AND HARDWARE.

Part: SEAT TRACK — CORRODED (BS 863-969) · airframe 13,853 hrs · 10,142 cycles

RT SIDEWALL SEAT RAIL FS 863.0 TO FS 969.0 HAS CORROSION DAMAGE. REMOVED CORRISION AND FOUND TO BE WITHIN LIMITS IAW CRJ 700 SRM 53-51-49. APPLIED ALODINE IAW SRM 51-21-16.

Part: SEAT TRACK — CORRODED (BS 379-477) · airframe 13,853 hrs · 10,142 cycles

RT SIDEWALL SEAT RAIL FS 379.0 TO FS 477.40 HAS CORROSION DAMAGE. REMOVED CORROSION AND FOUND TO BE WITHIN LIMITS IAW CRJ 700 SRM 53-21-49. APPLIED ALODINE IAW CRJ 700 SRM 51-21-16.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 13,853 hrs · 10,142 cycles

RIGHT SIDEWALL SEAT RAIL FS 477.40 TO FS 570.0 HAS CORROSION DAMAGE. REMOVED CORROSION AND FOUND TO BE WITHIN LIMITS IAW CRJ 700 SRM 53-31-49. APPLIED ALODINE IAW CRJ 700 SRM 51-21-16. SUPPLEMENTAL SDR CLOSED 2/12/08.

Part: SEAT TRACK — CORRODED (BS 570-708) · airframe 13,853 hrs · 10,142 cycles

LT SIDEWALL SEAT RAIL FS 570.0 TO FS 708.0 HAS CORROSION DAMAGE. REMOVED AND REPLACED SEAT RAIL IAW CRJ 700 AMM 53-00-49.

Part: PANEL — CRACKED (RT SPOILER) · airframe 13,853 hrs · 10,142 cycles

RT MULTI FUNCTION SPOILER CLOSEOUT PANEL CRACKED AT INBOARD AFT CORNER.

Part: DRAG ANGLE — CRACKED (VERTICAL STAB) · airframe 13,853 hrs · 10,142 cycles

VERTICAL STAB TO FUSELAGE RT DRAG ANGLE CRACKED. REPAIRED RT VERT STAB DRAG ANGLE IAW REO 670-55-31-018 REFER TO ATTACHED M-234 ITEMS 2-5 FOR COMPLIANCE. CUT OUT DAMAGE, FABRICATED AND DRILLED FILLER AND DOUBLER ALL WORK IAW REO 670-55-31-31-018, FILLER AND DOUBLER MADE OUT OF 2024T3 .090 P030031186. PERFORMED ET INSP OF CUTLINES PER NDTM CRJ 700 51-20-006, NO DEFECTS NOTED. SEALED AND STARTED INSTALLING RT REPAIR FILLER AND DOUBLER ON RT DRAG ANGLE, ALL RIVETS SHOT NEEDS HI-LOKS INSTALLED IAW REO670-55-31-018. FINISHED INSTALLING FILLER AND DOUBLER FILLET SEALED EDGES AND PAINTED ALL WORK IAW REO 670-55-31-018. SUPPLEMENTAL SDR CLOSED 2/15/08.

Part: DRAG ANGLE — CRACKED (VERTICAL STAB) · airframe 13,853 hrs · 10,142 cycles

VERTICAL STAB TO FUSELAGE LT DRAG ANGLE CRACKED. REPAIRED LT DRAG ANGLE IAW REO 670-55-31-018 REFER TO ATTACHED M-234 ITEMS 2- 5 FOR COMPLIANCE. CUT OUT, DAMAGE FABRICATED AND DRILLED FILLER AND DOUBLER ALL WORK IAW REO 670-55-31-018 FILLER AND DOUBLER MADE OUT OF 2024T3 .090 0030031186. PERFORMED ET INSP OF CUTLINES IAW CRJ 700NDTM 51-20-006, NO DEFECTS NOTED. SEALED AND STARTED INSTALLING LT DRAG ANGLE REPAIR FILLER AND DOUBLER ALL RIVETS SHOT ALL BUT (5) HI-LOKS INSTALLED IAW REO 670-55-31-018. FINISHED INSTALLING FILLER AND DOUBLER FILLET SEALED EDGES AND PAINTED ALL WORK IAW REO 670-55-31-019. SUPPLEMENTAL SDR CLOSED 2/15/08.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 13,853 hrs · 10,142 cycles

RT FWD INBOARD FLOOR TRACK AND LAV HOLD DOWN FITTINGS CORRODED. THIS SDR WILL REMAIN OPEN PENDING MAINTENANCE DETERMINATION OF AN APPROPRIATE CORRECTIVE ACTION.

Part: HANDLE — CORRODED (EMERGENCY EXIT) · airframe 13,853 hrs · 10,142 cycles

CREW ESCAPE HANDLE CORRODED.

Part: HANDLE — CRACKED (E/E DOOR) · airframe 13,853 hrs · 10,142 cycles

AVIONICS COMPT DOOR HANDLE CRACKED. REMOVED AND REPLACED HANDLE ASSY IAW MM 52-42-02-000-801 AND SRM 51-42-20.

Part: FRAME — CORRODED (BS 645) · airframe 13,853 hrs · 10,142 cycles

LIGHT SURFACE CORROSION ON FRAME AT FS 645.00 BETWEEN BL 27L AND 27R AND BELLY SKIN JUST AFT OF FRAME INSIDE FWD CARGO BAY. CLEAN IMMEDIATE SURROUNDING AREA AND INSPECT FOR FURTHER CORROSION DAMAGE.

Part: BULKHEAD — CRACKED (BS 280) · airframe 13,853 hrs · 10,142 cycles

LT STA 280 BULKHEAD WEB CORRODED AT CROSSBEAM. INSTALLED BULKHEAD WEB. ALL WORK IAW 670-53-11-052 BM 7024222. STARTED FABRICATING AND DRILLING NEW WEB. WEB FABRICATED IAW 670-53-11-052 BU 7024222. FINISH DRILLING OF WEB IAW 670-53-11-052. OK TO INSTALL. INSTALLED WEB PER STEP/ITEM 2. PERFORMED FINAL CLEAN UP AS REQUIRED.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 13,853 hrs · 10,142 cycles

STA 280 CROSSBEAM CORRODED.

Part: BULKHEAD — CRACKED (BS 280) · airframe 13,853 hrs · 10,142 cycles

RT STA 280 BULKHEAD WEB CORRODED AT CROSSBEAM. REPAIRED IAW IAE REO 670-53-11-052.

Part: GLOWSTRIP — MISSING (CABIN) · airframe 13,708 hrs · 10,050 cycles

PAX COMPARTMENT RIGHT SIDE OVERWING AFT EMERGENCY TRACK LIGHTING PHOTOLUMINESENT STRIP IS MISSING.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 11,503 hrs · 8,528 cycles

FLIGHT 5656 - LEFT WINDSHIELD SHATTERED AT FL 360. DECLARED EMERGENCY, DIVERTED TO ATL. LANDED WITHOUT INCIDENT. REPLACED LEFT WINDSHIELD.

Part: SENSOR — FAULTY (AOA) · airframe 11,209 hrs · 8,324 cycles

FLIGHT 5440 - STALL FAIL CAUTION MESSAGE IN FLIGHT, AIRCRAFT DIVERTED TO CVG AND LANDED SAFELY. REMOVED AND REPLACED NR 2 AOA SENSOR.

Part: ANTI-ICE VALVE — MALFUNCTIONED (RT ENGINE) · airframe 10,980 hrs · 8,230 cycles

FLIGHT 5228 - DURING CLIMBOUT RECEIVED A RIGHT ENGINE BLEED CAUTION MESSAGE, FLIGHT RETURNED TO CVG. REPLACED THE COWL ANTI-ICE VALVE.

Part: SEAT TRACK — CORRODED (BS 595-599) · corrosion level 3 · airframe 10,692 hrs · 7,963 cycles

LEFT SIDE SEAT TRACK CORRODED. REPAIRED IAW REO 670-53-00-013.

Part: ANGLE — CORRODED (PAX DOOR) · corrosion level 3 · airframe 10,692 hrs · 7,963 cycles

PAX DOOR THRESHOLD MIDCAP EXTRUSION ANGLE CORRODED. REPLACED ANGLE IAW SRM 51-41-02.

Part: SEAT TRACK — CORRODED (BS 597-613) · corrosion level 3 · airframe 10,692 hrs · 7,963 cycles

RIGHT SIDE SEAT TRACK CORRODED. REPAIRED IAW REO 670-53-00-013.

Part: SKIN — CHAFED (TE FLAPS) · corrosion level 3 · airframe 10,692 hrs · 7,963 cycles

RIGHT INBOARD FLAP UPPER SKIN IS CHAFED FROM THE MOVABLE FLAP VANE ACTUATOR (INSIDE THE FLAP). REPAIRED IAW COMAIR EO 70-5752-01448.

Part: CROSSBEAM — CORRODED (BS 280) · corrosion level 3 · airframe 10,692 hrs · 7,963 cycles

CROSSBEAM SUPPORT FLANGE CORRODED. REPAIRED IAW COMAIR EA 70-5311-01447.

Part: SEAL — TORN (PAX DOOR) · airframe 3,317 hrs · 7,469 cycles

FLIGHT 5307- EN ROUTE ATL-PWM ENCOUNTERED LOSS OF PRESSURIZATION THROUGH THE CABIN DOOR SEAL CAUSING LOUD NOISE. FLIGHT DIVERTED TO RDU. REPLACED THE CABIN DOOR SEAL.

Part: ISOLATION VALVE — FAULTY (THRUST REVERSER) · airframe 8,818 hrs · 6,788 cycles

FLIGHT 5281 - DURING TAKEOFF ROLL RECEIVED A LEFT THRUST REVERSER UNSAFE MESSAGE, ABORTED TAKEOFF AND RETURNED TO THE GATE. REPLACED THE LEFT THRUST REVERSER ISOLATION VALVE.

Part: RELAY — FAULTY (THRUST REVERSER) · airframe 8,818 hrs · 6,788 cycles

FLIGHT 4974 - DURING TAKEOFF RECEIVED A LEFT THRUST REVERSER MESSAGE, ABORTED TAKEOFF AND RETURNED TO THE GATE. REPLACED THE LEFT THRUST REVERSER GROUND RELAY.

Part: WARNING LIGHT — FALSE ACTIVATION (LT BLEED SYS) · airframe 8,713 hrs · 6,715 cycles

FLIGHT 5683 - LT ENGINE BLEED CAUTION. SYSTEM CHECKS WERE SATISFACTORY.

Part: CONTROL UNIT — MALFUNCTIONED (SLATS) · airframe 9,632 hrs · 6,157 cycles

FLIGHT 5316 - SLAT FAIL CAUTION. CLEARED FAULTS FROM COMPUTER. SYSTEM TEST NORMAL.

Part: CYLINDER — CORRODED (NLG) · airframe 7,694 hrs · 5,907 cycles

NLG OUTER CYLINDER P/N 52101-1, S/N BA0003 IS CORRODED. CORROSION REPAIRED IAW REO 670-32-21-064 AND GOODRICH SCR 0008-04 REV C.

Part: CROSSBEAM — CORRODED (FS 280) · corrosion level 2 · airframe 7,693 hrs · 5,907 cycles

THE TRANSVERSE BEAM AT FS 280 IS CORRODED FROM LBL 36 TO RBL 36. REMOVED THE CORRODED TRANSVERSE BEAM AND INSTALLED A NEW TRANSVERSE BEAM IAW BOMBARDIER REO 670-53-11-047 REV C.

Part: WEB — CORRODED (FS 280) · corrosion level 2 · airframe 7,693 hrs · 5,907 cycles

THE LT AND RT LOWER WEBS BELOW THE FLOOR AT FS 280 ARE CORRODED FROM LBL 36 TO RBL 36. REMOVED THE CORRODED WEBS AND INSTALLED NEW WEBS IAW REO 670-53-11-052 REV A.

Part: WARNING LIGHT — FALSE ACTIVATION (PAX DOOR) · airframe 6,670 hrs · 5,156 cycles

FLIGHT 5493 DURING CLIMBOUT OF JAX RECEIVED A CABIN DOOR WARNING, CREW DECLARED AN EMERGENCY AND RETURNED TO THE FIELD. AIRCRAFT FERRIED TO CVG, CHECKED SENSOR PX27 FOR GAP, PRESSURIZED AIRCRAFT, DISCREPANCY COULD NOT BE DUPLICATED BY MAINTENANCE.

Part: WINDSHIELD — LEAKING (COCKPIT) · airframe 5,934 hrs · 4,597 cycles

FLIGHT 5538, COPILOTS FLOOD LIGHT IS SMOKING. FOUND WATER LEAKING ONTO FLOOD LIGHT. REPLACED LIGHT AND RETORQUED WINDOW I STRAP SCREWS.

Part: ACTUATOR — MALFUNCTIONED (NR 3 SLAT) · airframe 3,050 hrs · 3,880 cycles

FLIGHT 5023 SLATS FAIL CAUTION MESSAGE. REPLACED THE NR 3 SLAT ACTUATOR.

Part: WARNING LIGHT — ILLUMINATED (SLATS) · airframe 5,044 hrs · 3,875 cycles

FLIGHT 5641 SLATS FAIL CAUTION MESSAGE. COULD NOT DUPLICATE. OPERATIONAL CHECK WAS NORMAL. RESET TRIP INDICATOR AT OUTBOARD SLAT ACTUATOR.

Part: CONNECTOR — FAULTY (RT MLG) · airframe 3,442 hrs · 2,626 cycles

FLIGHT 9490 DURING CRUISE FLIGHT RECEIVED A GEAR DISAGREE CAUTION ASSOCIATED WITH A PROXIMITY SYSTEM FAULT AND MLG FAULT, CREW DECLARED AN EMERGENCY AND LANDED AT CVG SAFELY. REPLACED FAULTY CONNECTOR P614 FOR THE RIGHT MLG PROXIMITY SENSOR PX18.

Part: SELECTOR VALVE — MALFUNCTIONED (MLG) · airframe 3,437 hrs · 2,618 cycles

FLIGHT 5287 GEAR DISAGREE WARNING. REPLACED THE GEAR SELECTOR VALVE.

Part: PROXIMITY SENSOR — MALFUNCTIONED (RT MLG) · airframe 3,435 hrs · 2,616 cycles

FLIGHT 5366 GEAR DISAGREE WARNING. COULD NOT DUPLICATE. REPLACED THE RT MLG UPLOCK PROXIMITY SENSOR HARNESS PX 18.

Part: CONTROL UNIT — MALFUNCTIONED (TE FLAPS) · airframe 3,376 hrs · 2,572 cycles

FLIGHT 5476 FLAPS HALF SPEED MESSAGE. REPLACED THE SFECU.

Part: VALVE — FAILED (AFT EQUIP BAY) · airframe 2,709 hrs · 2,060 cycles

FLIGHT 5095 RECEIVED A RT BLEED AND COWL CAUTION DURING CRUISE FLT. AIRCRAFT PERFORMED AN UNSCHEDULED LANDING AT CVG. REPLACED THE RIGHT ENGINE PRSOV.

Part: ENGINE — VIBRATES (LEFT) · airframe 2,514 hrs · 1,910 cycles

FLIGHT 5080 LEFT ENGINE VIBRATION, INDICATED AS HIGH AS 3.2. REPLACED LEFT ENGINE.

Part: WINDOW — FAILED (COCKPIT) · airframe 2,081 hrs · 1,569 cycles

FLIGHT 5742 COPILOTS SIDE WINDOW SHATTERED. REPLACED WINDOW.

Part: ADC — FAILED (COCKPIT) · airframe 1,240 hrs · 920 cycles

FLIGHT 6899 ADC NR 1 FAILED. RESET ADC, OPERATIONAL CHECK SATISFACTORY.

airframe 858 hrs · 637 cycles

F.S. 1098.20 PRESSURE BULKHEAD RIGHT SIDE RBL34 TO RBR 41 BETWEEN STRINGERS 8R AND 9R. HAS ONE INCH CRACK ON BULKHEAD.INCORPORATED RIGHT PRESSURE BULKHEAD BOMBARDIER, INC. REO 670-53-61-059 REV NC. REMOVED DAMAGED FITTING AND INSTALLED P/N 670-53-61-038-2.

airframe 858 hrs · 637 cycles

F.S. 1098.20 PRESSURE BULKHEAD RIGHT SIDE RBL 34 & 0 RBR 41 BETWEEN STRINGERS 8R AND 9R HAS ONE INCH CRACK ON BULKHEAD.INCORPORATED RIGHT PRESSURE BULKHEAD BOMBARDIER, INC. REO 670-53-61-034 REV A. REMOVED DAMAGED AREA AND INSTALLED FITTING P/N 670-53-61-026-2.

Part: SELECTOR VALVE — MALFUNCTIONED (WING) · airframe 544 hrs · 410 cycles

FLIGHT 5097 LANDING GEAR DISAGREE WARNING.REPLACED THE LANDING GEAR SELECTOR VALVE.

Part: PROXIMITY SENSOR · airframe 263 hrs · 226 cycles

FLIGHT 5132 NLG DOORS WARNING AND PROX SYSTEM FAULT.ADJUSTED NLG PROXIMITY SENSORS.

Part: STRUCTURE — BIRDSTIKE (AIRFRAME)

SMF - BIRD STRIKE AFTER ROTATION REPORTED. MAINTENANCE INSPECTED AREA FOR DAMAGE. NO DAMAGE NOTED. AIRCRAFT RETURNED TO SERVICE. (M)

Part: DOOR — NOT LATCHED (BAGG COMPT)

LAX - POD DOOR CAME OPEN TAKEOFF. AIRCRAFT RETURNED TO STATION. MAINTENANCE INSPECTED POD DOOR AND LATCH MECHANISM FOR DAMAGE. NO DAMAGE NOTED. RESECURED DOOR. AIRCRAFT RETURNED TO SERVICE. (M)

Part: CONNECTOR — DIRTY (RT ENGINE)

ACV - RIGHT ENGINE EGT AND TORQUE FLUCTUATION REPORTED WHILE POWER WAS ADVANCED FOR TAKEOFF. ABORTED TAKEOFF. MAINTENANCE DEFERRED RT SRL AND TTL SYSTEMS PER MEL 76-1 AND MEL 76-2. AIRCRAFT RETURNED TO SERVICE. MAINTENANCE SUBSEQUENTLY CLEARED DEFERRAL BY CLEANING RIGHT TORQUE RING CANNON PLUG. COULD NOT DUPLICATE DISCREPANCY. OPERATIONAL CHECK SATISFACTORY DURING GROUND RUN. (M)

Part: ENGINE — FAILED (LEFT)

FAT - LEFT ENGINE FAILED TO REACH MINIMUM STATIC TAKEOFF TORQUE. TAKEOFF ABORTED WITHOUT INCIDENT. MAINTENANCE REPLACED LEFT ENGINE. AIRCRAFT RETURNED TO SERVICE. (M)

Part: ENGINE — BIRD STRIKE (LEFT)

LAX - BIRD STRIKE AT LEFT ENGINE REPORTED. MX INSPECTED LEFT PROPELLER AND SPINNER, LEFT ENGINE INLET AND IMPELLER, AND LEFT WING LEADING EDGE AND NACELLE IAW WITH BIRD STRIKE INSPECTION J3101 MM 0550-50. NO EVIDENCE OF BIRD IMPACT AND NO DAMAGE NOTED. AIRCRAFT RETURNED TO SERVICE. (M)

Part: RADIUS ROD — FAILED (RT MLG)

FAT - RT MAIN GEAR INTRANSIT LIGHT INTERMITTENT IN FLIGHT. MAINTENANCE REPLACED RIGHT MAIN GEAR RADIUS ROD. OPERATIONAL AND LEAK CHECK SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SWITCH — FALSE INDICATION (LT MLG)

FAT - DURING CLIMB-OUT, LT MLG INTRANSIT LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. AIRCRAFT RETURNED TO FAT WITHOUT INCIDENT. MAINTENANCE REPLACED UPLOCK MICROSWITCH. SYSTEM OPERATIONAL CHECK NORMAL DURING GEAR RETRACTION CHECK. AIRCRAFT RETURNED TO SERVICE. (X)

Part: SWITCH — FAILED (LT MLG)

LAX - DURING CLIMB-OUT LEFT MAIN LANDING GEAR INTRANSIT LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. MX INSPECTED AND CLEANED UPLOCK MICROSWITCH. SYSTEM OPERATIONAL CHECK NORMAL DURING GEAR RETRACTION CHECK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: WINDSHIELD — BIRD STRIKE (RT COCKPIT)

LAX - BIRD STRIKE REPORTED ON AIRCRAFT AT FLIGHT OFFICERS WINDSHIELD WIPER AREA. MAINTENANCE ACCOMPLISHED BIRD STRIKE INSPECTION. NO DAMAGE NOTED. AIRCRAFT RETURNED TO SERVICE. (M)

Part: EGT INDICATOR — FAILED (RT ENGINE)

SFO - RIGHT ENGINE EGT GAUGE INDICATION DROPPED TO 450 DEGREES AND STUCK DURING CLIMB-OUT. AIRCRAFT RETURNED TO STATION WITHOUT INCIDENT. MAINTENANCE REPLACED RIGHT EGT GAUGE. SYSTEM OPERATIONAL CHECK NORMAL, AIRCRAFT RETURNED TO SERVICE. (M)

Part: FCU — OUT OF ADJUST (LEFT ENGINE)

LAX - LEFT ENGINE FAILED TO DEVELOP REQUIRED TAKEOFF POWER. TAKEOFF ABORTED WITHOUT INCIDENT. MAINTENANCE ADJUSTED LEFT ENGINE FUEL CONTROL UNIT RIGGING. ENGINE GROUND RUN NORMAL. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SWITCH — BROKEN WIRE (RT MLG)

SEA - RIGHT MAIN LANDING GEAR INTRANSIT LIGHT FAILS TO ILLUMINATE. MAINTENANCE REPAIRED BROKEN WIRE AT RIGHT MAIN LANDING GEAR UPLOCK MICROSWITCH. GEAR INDICATIONS NORMAL DURING GROUND TEST. AIRCRAFT RETURNED TO SERVICE. (M)

Part: WINDSHIELD — BIRD STRIKE (RT COCKPIT)

LAX - BIRD STRIKE REPORTED ABOVE FLIGHT OFFICERS WINDSHIELD ON TAKEOFF ROLL. TAKEOFF ABORTED WITHOUT INCIDENT. MAINTENANCE ACCOMPLISHED BIRD STRIKE INSPECTION. NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. (M)

Part: FCU — FAILED (LT ENGINE)

SMF - LEFT ENGINE UNCOMMANDED INCREASE IN TORQUE FROM 40 PERCENT TO 100 PERCENT IN-FLIGHT. TORQUE REDUCED TO 30 PERCENT WITH PROPELLER BROUGHT TO FLIGHT IDLE POSITION. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED LEFT ENGINE FUEL CONTROL UNIT. LEFT ENGINE OPERATIONAL CHECK NORMAL DURING GROUND RUN. AIRCRAFT RETURNED TO SERVICE. (X)

Part: FLAP SELECTOR — FAILED (COCKPIT)

RDD - GEAR HORN CAME ON IN FLIGHT AN UNABLE TO CANCEL UNTIL GEAR WAS EXTENDED. AIRCRAFT LANDED IN RDD WITHOUT INCIDENT. MAINTENANCE REPLACED FLAP SELECTOR AND PERFORMED AND OPERATIONAL CHECK OF FLAP AND GEAR WARNING SYSTEM AND FOUND TO BE OPERATING NORMALLY. AIRCRAFT RETURNED TO SERVICE. (W)

Part: TRANSDUCER — MALFUNCTION (RT WING)

SFO - RT STALL IDENT LIGHT ILLUMINATED AND STICK SHAKER ACTIVATION REPORTED AT 150 KTS. MAINTENANCE ADJUSTED REPLACED AND ADJUSTED RIGHT STALL SYSTEM LIFT TRANSDUCER. STALL SYSTEM OPERATIONAL CHECK NORMAL ON GROUND. AIRCRAFT RETURNED TO SERVICE. (Z)

Part: TRANSDUCER — REQ'D ADJ (LT AND RT WING)

FAT - EN ROUTE SFO TO VIS AT 12,000 FEET, STALL IDENT LIGHT ILLUMINATED FOLLOWED BY STICK SHAKER AND STALL WARNING HORN ACTIVATION. AIRCRAFT DIVERTED TO STATION, LANDING WITHOUT INCIDENT. MAINTENANCE ADJUSTED LEFT AND RT STALL SYSTEM LIFT TRANSDUCER. STALL SYSTEM OPERATIONAL CHECK NORMAL ON GROUND AND DURING SUBSEQUENT TEST FLIGHT. AIRCRAFT RETURNED TO SERVICE. (Z)