N927EV

Part: LIGHT — INOPERATIVE (RT WING) · airframe 35,025 hrs · 34,382 cycles

FWD EMER LIGHT OVER RIGHT WING INOPERATIVE. REMOVED AND REPLACED RH EMER LIGHT IAW AMM 33-51-21. BM1-0006-002

Part: BULKHEAD — DAMAGED (BS 559) · airframe 34,807 hrs · 34,106 cycles

L/H 9G BULKHEAD HAS 19EA AREAS OF DAMAGE AROUND POTTED INSERTS. REPAIRED RH 9G BULKHEAD IAW MHIRJ ENGINEERING ORDER CL-600-2B19-53-L06718 REV IR, DATED 4/15/2021.

Part: BULKHEAD — DAMAGED (BS 559) · airframe 34,807 hrs · 34,106 cycles

CENTER 9G BULKHEAD HAS 6EA AREAS OF DAMAGE AROUND PUTTED INSERTS REPAIRED CENTER 9G BULKHEAD IAW MHIRJ ENGINEERING ORDER CL-600-2B19-53-L06719 REV IR, DATED 4/15/2021.

Part: BULKHEAD — DAMAGED (BS 559) · airframe 34,807 hrs · 34,106 cycles

R/H 9G BULKHEAD HAS 20EA AREAS OF DAMAGE AROUND POTTED INSERTS. REPAIRED RH 9G BULKHEAD IAW MHIRJ ENGINEERING ORDER CL-600-2B19-53-L06720 REV IR, DATED 4/15/2021.

Part: FRAME — CORRODED (BS 333 S22R) · airframe 34,807 hrs · 34,106 cycles

FS 333 STR 22R FWD SIDE OF FRAME HAS CORROSION AROUND RIVETS. REMOVED AND REPLACED FRAME SECTOR IAW CRJ 200 SRM 51-40-11,51-42-06 AND 51-42-20.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 34,807 hrs · 34,106 cycles

L/H SIDE SEAT RAIL IS CORRODED BETWEEN FS 559+16 TO FS 559+32 REMOVED AND REPLACE SIDE SEAT RAILS FS 559+16 - 559+32 IAW MHI REO 601R-53-00-005 REV C 19-3-21 AND CRJ 200 AMM 53-01-11-000/400-802

Part: HANDLE — FAILED (EMERGENCY EXIT) · airframe 34,807 hrs · 34,106 cycles

R/H OVERWING EMERGENCY EXIT FAILED FUNCTIONAL TEST, HANDLE SHOULD RELEASE WITH 20-40 LBS OF FORCE, REQUIRED 50 LBS. LUBRICATED AND CORRECTLY PERFORMED FUNCTIONAL TEST OF RH OVERWING EMER EXIT IAW CRJ 200 AMM 12-20-52-640-802, 52-21-00-720-801. TEST GOOD. NO DEFECTS NOTED. SDR ITEM PER GMM 11-06 C/W.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 34,807 hrs · 34,106 cycles

R/H SIDE SEAT RAIL IS CORRODED BETWEEN FS 559 TO FS 559+16 REMOVED AND REPLACE SIDE SEAT RAILS FS 559 - 559+16 IAW MHI REO 601R-53-00-005 REV C 19-3-21 AND CRJ 200 AMM 53-01-11-000/400-802

Part: SEAT TRACK — CORRODED (BS 409) · airframe 34,807 hrs · 34,106 cycles

L/H SIDE SEAT RAIL IS CORRODED BETWEEN FS 409+16 TO FS 409+32 REMOVED AND REPLACE SIDE SEAT RAILS FS 409+16 - 409+32 IAW MHI REO 601R-53-00-005 REV C 19-3-21 AND CRJ 200 AMM 53-01-11-000/400-802

Part: SUPPORT BEAM — CRACKED (BS 621) · airframe 34,807 hrs · 34,106 cycles

CARGO DOOR SUPPORT BEAM BOTTOM CLIP ON THE FS 621 BULKHEAD IS CRACKED REMOVED AND REPLACE CLIP IAW CRJ 200 SRM 51-40-11 AND 51-42-21.

Part: LIGHT — INOPERATIVE (FWD CABIN) · airframe 33,925 hrs · 33,017 cycles

FWD EMERGENCY CEILING FLOOD LIGHT INOPERATIVE. REMOVED AND REPLACED CHARGER 1 FOR EMERGENCY LIGHTS, OPS CHECK GOOD, IAW CRJ200 AMM 33-51-05.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 33,334 hrs · 32,344 cycles

EXTERIOR EMERGENCY LIGHTS FWD OF PASSENGER EXIT AND SERVICE DOOR INOP REMOVED AND REPLACED BATTERY PACK AT PS1LF. DID NOT FIX. REMOVED AND REPLACED CAHRGER ASSY. OPS CHECK GOOD IAW CRJ 200 AMM 33-51-04 AND CRJ 200 AMM 33-51-05. BATTERY P/N OFF 2013-1A S/N OFF 11934. P/N ON 2013-1 ASMI S/ON ON 12099. BATTERY CHARGER P/N OFF BA5-0933-901.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 33,043 hrs · 32,044 cycles

DURING ROUTINE CHECK FOUND BOTH FWD EXTERIOR EMERGENCY LIGHTS OUT NEXT TO PAX DOOR AND SERVICE DOOR REMOVED AND REPLACED #1 EMRGENCY BATTERY IAW JOB CARD 33-900-701 AND CHARGER IAW AMM 33-51-05. OPS CHECK GOOD NO FURTHER DEFECTS NOTED AT THIS TIME. BATTERY POS PS1LF PN OFF 2013-BR ON 2013-1A SN OFF B10732 ON 119344 CHARGER POS PS1LF PN OFF BA5-0933-901 ON BA500933-90

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 32,600 hrs · 31,584 cycles

FOUND RH FORWARD (OUTSIDE) EMERGENCY LIGHT INOP DURING ROUTINE CHECK. REPLACED THE LAMP IAW AMM 33-51-21 OPS CHECK GOOD .

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,407 hrs · 31,390 cycles

CEILING EMERGENCY EXIT LIGHT AT ROW 7 WILL NOT ILLUMINATE. REPLACED CEILING EMERGENCY CALL LIGHT @ ROW 7 IAW MEL 33-51-14. OPS CK GOOD, OK FOR SERVICE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 32,362 hrs · 31,344 cycles

LBL 27 I/B FLOOR LANDING HAS CORROSION BETWEEN FS 559+112 AND FS 574, IN THE CARGO BAY. REPAIRED LBL27 FLOORBEAM LANDING IAW EA CRJ 253-09319 REV IR THIS IS A MAJOR REPAIR.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 32,362 hrs · 31,344 cycles

THIS IS SUPPLEMENTAL INFORMATION TO A PRIOR SUBMISSION. PART NUMBER WAS RECEIVED THAT WAS REPLACED AFTER THIS EVENT. LT AFT EMER EXIT EMER LIGHT NOT COMING ON. REMOVED AND REPLACED LIGHT BULB AT LT AFT EXTERIOR EMER LIGHT IAW CMM 33-52-06 OPS TEST ACCOMPLISHED ON W/O 1017379-2000-0086 S/N 7206763.

Part: RIB — CORRODED (LT PYLON) · airframe 32,362 hrs · 31,344 cycles

LT PYLON O/B RIB HAS CORROSION AND PITS AROUND AFT ENGINE MOUNT INNER RACE CUT OUT. REPAIRED LT PYLON RIB IAW REO 601R-54-50-036 AND 601R-71-22-026 GAP CHECK GOOD IAW REO 601R-71-22-026 THIS IS A MAJOR REPAIR.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 32,362 hrs · 31,344 cycles

FLOOR PANEL LANDING AT FS 621 IS CRACKED JUST I/B OF THE LH FOOR SILL, IN THE CARGO BAY. REPAIRED FLOOR PANEL LANDING @ FS 621 IAW REO 601R-53-61-117.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 32,362 hrs · 31,344 cycles

AFT ACCY. COMPT.SYSTEM-2 HYD. MANIFOLD MOUNTING STRUCTURE CRACKED AT LOWER AFT CORNER. REMOVED/REPLACED MOUNTING STRUCTURE IAW SRM 51-42-06 LK AND OPS CK GOOD IAW AMM 12-00-06-863-801.

Part: RIB — CORRODED (RT PYLON) · airframe 32,362 hrs · 31,344 cycles

RT PYLON O/B RIB HAS CORROSION AND PITS AROUND AFT MOUNT INNER RACE CUT-OUT. REPAIRED RT PYLON RIB IAW REO 601R-54-50-036 AND 601R-71-22-026 GAP CHECK GOOD IAW REO 601R-71-22-026 THIS IS A MAJOR REPAIR.

Part: RIB — CRACKED (LT ELEVATOR) · airframe 32,362 hrs · 31,344 cycles

DURING REPLACEMENT OF THE LT ELEVATOR SHEAR PINS FOUND ELEVATOR LEADING EDGE ACCESS PANEL SUPPORT RIB CRACKED. REMOVED/REPLACED LT SUPPORT RIB IAW SRM 51-42-21 AND 51-42-06.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 32,362 hrs · 31,344 cycles

THERE IS CORROSION AT RBL9 AT FS409+112 ON FLOORBEAM. REPAIRED FLOORBEAM AT FS409+112 AND RBL9 IAW SRM 53-00-43.

Part: ACCESS PANEL — CRACKED (LT ENGINE) · airframe 32,362 hrs · 31,344 cycles

LT ENGINE LOWER PCU ACCESS PANEL 432AC IS SUSPECTED TO BE CRACKED. REMOVED AND REPLACED LOUVERS ON PANEL 432AC IAW CMM 20-42-10. APPLIED FINISH COAT IAW CMM 20-25-16.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 32,362 hrs · 31,344 cycles

AFT ACCY. COMPT.SYSTEM-1 HYD. MANIFOLD MOUNTING STRUCTURE CRACKED AT FORWARD END. REPAIRED MOUNTING STRUCTURE IAW SRM 51-71-12 AND RESTORED FINISH IAW SRM 51-25-16 LK AND OPS CK GOOD IAW AMM 12-00-06-863-801.

Part: SKIN — GOUGED (TE FLAP) · airframe 32,362 hrs · 31,344 cycles

RT IB FLAP LOWER SKIN HAS GOUGE OB OF PATCH ON IB END. REMOVED PREVIOUS REPAIR DOUBLER, CUTOUT ADDITIONAL GOUGE DAMAGE AND INSTALLED NEW REPAIR DOUBLER WITH FILLERS IAW SRM 57-52-00 FIG 202.

Part: HINGE — CRACKED (CARGO DOOR) · airframe 32,362 hrs · 31,344 cycles

CARGO DOOR THRESHOLD, HINGES HAVE CORROSION AND AND CRACKS. LOCATED AND DRILLED NEW HINGES IAW SRM TR 51-42. INSTALLED ON NEW THRESHOLD PLATE IAW SRM 51-42-06.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 32,362 hrs · 31,344 cycles

RBL 27 IB AND OB FLOOR PANEL LANDINGS HAS CORROSION SPOTS BETWEEN FS 589 THRU FS 610, IN THE CARGO BAY. REMOVED & REPLACED RBL 27 FLOORBEAM CAP FS589 TO FS 610 IAW SRM 51-42-21 & 51-42-22.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 32,362 hrs · 31,344 cycles

FLOOR SEAT TRACK LT #2 HAS CORROSION. REMOVED/REPLACED SEAT TRACK IAW AMM 53-01-11.

Part: SKIN — CRACKED (PAX DOOR) · airframe 32,362 hrs · 31,344 cycles

WHILE REMOVING CORROSION ON INNER SKIN FOUND SKIN CRACKED FWD UPPER CORNER. REPAIRED SKIN ON FWD UPPER CORNER OF PAX DOOR IAW EA CRJ252-09290.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 32,362 hrs · 31,344 cycles

SERVICE DOOR THRESHOLD HAS SEVERAL SPOTS OF CORROSION. EVALUATED SERVICE DOOR THRESHOLD, PLACE FOUND TO BE OUT OF LIMITS. RECEIVED NEW SERVICE DOOR THRESHOLD, LOCATED AND DRILLED NEW SRM 51-42-06.

Part: MOUNT FITTING — NICKED (RT ENGINE) · airframe 32,362 hrs · 31,344 cycles

RT PYLON FWD ENGINE MOUNT FITTING AFT UPPER LUG IS NICKED AT THE AFT UPPER EDGE. REPAIRED IAW REO 601R-54-51-203 THIS IS A MAJOR REPAIR.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 32,362 hrs · 31,344 cycles

FLOOR SEAT TRACK LT #1 HAS CORROSION. REMOVED AND REPLACED IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 32,362 hrs · 31,344 cycles

FLOOR SEAT TRACK RT #2 HAS CORROSION. REMOVED AND REPLACED RT #2 SEAT TRACK IAW AMM 53-01-11.

Part: YOKE — NICKED (RT ENGINE) · airframe 32,362 hrs · 31,344 cycles

RT ENGINE YOKE HAS NICK ON THE IB FWD EDGE. REPAIRED IAW REO 601R-71-21-078.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 32,362 hrs · 31,344 cycles

LT AISLE SEAT STICK #4 TRACK HAS CORROSION SPOTS BETWEEN FS 559 THRU FS 559+80, IN THE CABIN. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 32,362 hrs · 31,344 cycles

RT AISLE SEAT STICK # 4 TRACK HAS CORROSION SPOTS BETWEEN FS 559 THRU FS 559+80, IN THE CABIN. REMOVED/REPLACED SEAT TRACK IAW AMM 53-01-11.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 32,362 hrs · 31,344 cycles

LWR SURFACE OF DOUBLER FOR REAR SERVICING POINT BETWEEN FS559.0+112 TO FS559.0+80 AND STRR21 AND STR 24 HAS CORROSION. REPAIRED LWD SURFACE OF DOUBLER FOR REAR SERVICING POINT BETWEEN FS559.0+112 TO FS559.0+80 AND STR 21 TO STR 24 IAW EA CRJ 253-09151.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 32,362 hrs · 31,344 cycles

SEAT TRACK ON TOP OF LBL 9 HAS CORROSION BETWEEN FS 559+112 AND FS 574, IN THE CARGO BAY. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-00-49.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 32,362 hrs · 31,344 cycles

SEAT TRACK ON TOP OF LBL 9 HAS CORROSION BETWEEN FC 559+80 AND FS 559+ 96, IN THE CARGO BAY. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-00-49.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 32,362 hrs · 31,344 cycles

FS 280.00 FLOOR SUPPORT BEAM ATTACH ANGLE RBL 9 OTBD CRACKED. REMOVED AND REPLACED OUTBD FS 280 RBL 9 FLOORBEAM ATTACHED ANGLE IAW SRM 51-42-21.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 32,362 hrs · 31,344 cycles

SEAT TRACK ON TOP OF RBL 27 HAS CORROSION BETWEEN FS 559+80 AND FS 559+96, IN THE CARGO BAY. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-00-49.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 32,362 hrs · 31,344 cycles

SEAT TRACK ON TOP OF RBL 9 HAS CORROSION BETWEN FS 559+112 AND FS 574, IN THE CARGO BAY. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-00-49.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 32,362 hrs · 31,344 cycles

SEAT TRACK ON TOP OF LBL 9 JUST FWD OF FS 621 HAS CORROSION, IN THE CARGO BAY. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-00-49.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 32,362 hrs · 31,344 cycles

SEAT TRACK ON TOP OF RBL 9 HAS CORROSION BETWEEN FS 559+80 AND FS 559+96 IN THE CARGO BAY. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-00-49.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 32,362 hrs · 31,344 cycles

SEAT TRACK ON TOP OF LBL 27 HAS CORROSION BETWEEEN FS 559+80 AND FS 559+96, IN THE CARGO BAY. REMOVED AND REPLACED SEAT TRACK IAW AM 53-00-49.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 32,362 hrs · 31,344 cycles

RT FLOOR SEAT TRCK #1 HAS CORROSION. REMOVED AND REPLACED IAW AMM 53-01-11.

Part: COWLING — CRACKED (LT ENGINE) · airframe 32,362 hrs · 31,344 cycles

LT ENG UPPER CORE COWL INBD LE IS CRACKED. REPAIRED LT UPPER CORE COWL INBD LE IAW CMM 71-12-01.

Part: ATTACH BRACKET — CRACKED (FUSELAGE) · airframe 32,362 hrs · 31,344 cycles

CARGO DOOR, FWD TRACK, LWR ATTACH BRACKET IS CRACKED. REMOVED AND REPLACED WITH NEW LOWER ATTACH BRACKET AT CARGO DOOR FWD TRACK IAW SRM 51-42-06.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 30,723 hrs · 29,602 cycles

CAPTAIN`S FLASHLIGHT WAS INOPERATIVE. REMOVED AND REPLACED THE FLASHLIGHT BATTERY IAW AMM 25-61-00. OPS CHECKED GOOD.

Part: BRACKET — DAMAGED (NLG) · airframe 30,158 hrs · 28,966 cycles

LANDING GEAR DISAGREE DURING TAKEOFF, NOSE STAYED DOWN & LOCKED. NOSE GEAR DOORS OPEN. REMOVED AND REPLACED THE OLEO SENSOR PS14 BRACKET IAW CMM 32-20-04. REINSTALLED PS14 SENSOR AND RIGGED IAW IAW AMM 32-61-05.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 29,709 hrs · 28,468 cycles

LEFT OVERWING EXIT DOOR, FLOOR LEVEL EXIT LIGHT WAS INOPERATIVE. REMOVED & REPLACED THE NR 2 EMERGENCY LIGHT INVERTER IAW AMM 33-51-07. OPERATIONAL CHECKED GOOD IAW AMM 33-51-00.

Part: EXTINGUISHER — EMPTY (LAVATORY) · airframe 29,471 hrs · 28,197 cycles

LAVATORY FIRE EXTINGUISHER EMPTY. REPLACED THE FIRE EXTINGUISHER BOTTLE IAW AMM 26-26-01.

Part: OXYGEN BOTTLE — EMPTY (CABIN) · airframe 29,258 hrs · 27,972 cycles

ONE PORTABLE OXYGEN BOTTLE READS 0 PSI. R & R DEPLETED OXYGEN BOTTLE IAW AMM 35-31-01.

Part: BATTERY PACK — INOPERATIVE (FLASHLIGHT) · airframe 28,983 hrs · 27,687 cycles

PILOT EMERGENCY FLASHLIGHT INOPERATIVE. REPLACED THE BATTERY AND OPS CHECKED GOOD IAW AMM 25-61-00-960-801, STEP 2.

Part: SEAT TRACK — CORRODED (BS 409) · airframe 28,983 hrs · 27,687 cycles

LEFT NR 3 SEAT TRACK FROM BS 409+7 TO 409+126 HAS CORROSION. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-21-41, FIG 101, TABLE 1. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11-000-802, AND AMM 53-01-11, STEP 2 (A-B).

Part: LIGHT — WORN (CABIN) · airframe 28,911 hrs · 27,615 cycles

RIGHT SIDE EMERGENCY EXIT LIGHT WORN IN FRONT HALF OF PASSENGER CABIN. R & R EMERGENCY LIGHT IAW AMM 33-51-01.

Part: LIGHT — BROKEN (CABIN) · airframe 28,911 hrs · 27,615 cycles

EMERCENY LIGHT NEXT TO SERVICE DOOR FWD BASE ASSY FOUND BROKEN AND MISSING PEICES. REPLACED THE EMERCENCY LIGHT ASSYOP CHECKS GOOD IAW AMM 33-51-10.

Part: COALESCER BAG — CONTAMINATED · airframe 26,436 hrs · 24,963 cycles

AFTER T/O CLIMBING THROUGH 2000 FT SMOKE TOILET CAUTION CAME ON WITH A STRONG ODOR OF BURNING OIL. IN THE COCKPIT AND CABIN, SMOKE TOILET LIGHT OUT ON FINAL BUT SMOKE ODOR STAYED. ACFT RETURNED TO DEPARTURE, AFTER T/O. R & R THE COALESCER IAW AMM 21-70-10. OPS CHECK STILL NOT GOOD, FOUND THAT THE APU IS SPILLING OIL.

Part: SKIN — DAMAGED (BS 319.7) · airframe 26,348 hrs · 24,866 cycles

BURN FOUND ON SKIN AT BS 319.7, STRINGER 26R. REMOVED EXISTING BURNED FASTENER AND WET INSTALLED NEW. RESTORED SURFACE FINISH IAW GREO 601R-53-00-115 REV E, SRM 51-25-01. REPAIR CLASSIFIED AS MAJOR IAW GMM 5-3.

Part: SKIN — DAMAGED (BS 333) · airframe 26,348 hrs · 24,866 cycles

BURN FOUND ON SKIN RIVET, BS 333, 26R. REMOVED EXISTING FASTENER AND WET INSTALLED TEMP FASTENER, RESTORED SURFACE FINISH IAW GREO 601R-53-00-115 REV E, SRM 51-25-01. REPAIR CLASSIFIED AS MAJOR IAW GMM 5-3.

Part: SKIN — DAMAGED (BS 589-605) · airframe 26,348 hrs · 24,866 cycles

BURN FOUND ON SKIN, BS 589 - 605, STRINGERS 24-25L. DRILLED SKIN IAW REO 601R-53-00-115, REPAIR PROCESS NR 1B3. INSTALLED RIVET IN DRILL HOLE IAW SRM 51-42-13. MAJOR REPAIR IAW GMM 5-3.

Part: SKIN — DAMAGED (BS 621-625) · airframe 26,348 hrs · 24,866 cycles

BURN FOUND ON SKIN BETWEEN BS 621 - 625.3, STRINGERS 24-25L. BLENDED SKIN IAW REO 601R-53-00-115, REPAIR PROCESS NR 1B2. MAJOR REPAIR IAW GMM 5-3.

Part: FLOOR SUPPORT — CORRODED (BS 409) · airframe 26,238 hrs · 24,746 cycles

DURING PREP FPR FLOOR PANEL CLOSE, TECH FOUND CORROSION ON FLOOR SUPPORT BEAM CAP AT SPLICE END BETWEEN FS 409.00 AND FS 409+16 AND BL 9.00. C/W REO:601R-53-00-027, REV D. C/W EC/TC REO 6901R-53-00-027 AND MET ALL THE REQUIREMENTS OF REO 601R-53-00-0237, REV C.

Part: FLOORBEAM — CRACKED (BS 621) · airframe 26,238 hrs · 24,746 cycles

CARGO BAY FLOOR SUPPORT AT FS 621.00 BULKHEAD IS CRACKED ON RT SIDE. REPAIRED IAW REO 601R-53-61-5545. REO 601R-53-61-5545, REV HAS BEEN ACCOMPLISHED AND ALL STEPS HAVE BEEN DOCUMENTED AND SIGNED FOR ON A NRI WORK CARD.

Part: BRACKET — CRACKED (BS 319) · airframe 26,238 hrs · 24,746 cycles

JOINT BRACKET AT LOWER SILL, FS 319.70 IS CORRODED AND HAS MATERIAL MISSING OR EATEN AWAY. REMOVED 2 OF CLIPS COMMON TO RT LOWER SILL BRACKET AT FS 319.70 IAW SRM 51-42-06 AND 51-42-21. REMOVED JOINT BRACKET FROM LOWER SILL FS 319.70, 601R38335 IAW SRM 51-42-21. LOCATED, DRILLED AND STARTED INSTALL OF JOINT BRACKET FS 319.70, PN 601R38335 IAW SRM 51-40-11, 51-42-21. INSTALLED JOINT BRACKET, PN 601R38335-1 IAW SRM 51-42-21.

Part: SKIN — CRACKED (LT WING) · airframe 26,238 hrs · 24,746 cycles

LEFT WING PLANK ACCESS HOLE AT 550GB HAS INDICATIONS ON LANDING AROUND CIRCUMFERENCE OF HOLE 65 PERCENT FULL SCREEN HEIGHT. AREAS MARKED ON ACFT. FAILED NDT. COMPLIED WITH EC/TC EO 600-57-81, C/W IAW REO 601R-57-21-030, REV L.

Part: SKIN — CORRODED (WING) · airframe 26,238 hrs · 24,746 cycles

FUEL TANK CUTOUT FOR PANEL 540BB HAS FRETTING DAMAGE INBD AND OTBD ENDS. BLENDED IAW REO:601R-57-21-030, FOUND TO BE OUT OF LIMITS. REO:601R-57-21-2349 HAS BEEN ACCOMPLISHED AND ALL STEPS HAVE BEEN DOCUMENTED AND SIGNED FOR ON A NON-ROUTINE WORK CARD. COMPLIED WITH EC/TC EO 600-57-81. C/W IAW REO:601R-57-21-030, REV L.

Part: SKIN — CORRODED (WING) · airframe 26,238 hrs · 24,746 cycles

FUEL TANK CUTOUT FOR FUEL PANEL 510AB HAS FRETTING DAMAGE AROUND ENTIRE CIRCUMFERENCE. BLENDED IAW REO:601R-57-21-030. FOUND TO BE OUT OF LIMITS. REO:601R-57-21-2349 HAS BEEN ACCOMPLISHED AND ALL STEPS HAVE BEEN DOCUMENTED AND SIGNED FOR ON A NON-ROUTINE WORK CARD. COMPLIED WITH EC/TC EO 600-57-81. C/W IAW REO:601R-57-21-030, REV L.

Part: SKIN — CRACKED (LT WING) · airframe 26,238 hrs · 24,746 cycles

LEFT WING PLANK ACCESS HOLE AT 540BB HAS INDICATIONS ON LANDING 65 PERCENT FULL SCREEN HEIGHT. AREAS MARKED ON ACFT. FAILED NDT. BLENDED IAW REO 601R-57-21-030. FOUND TO BE OUT OF LIMITS. REO 601R-57-21-2349 HAS BEEN ACCOMPLISHED AND ALL STEPS HAVE BEEN DOCUMENTED AND SIGNED FOR ON A NON-ROUTINE WORK CARD. COMPLIED WITH EC/TC EO 600-57-81 C/W IAW REO 601R-21-030, REV L.

Part: SKIN — CORRODED (WING) · airframe 26,238 hrs · 24,746 cycles

FUEL TANK CUTOUT FOR PANEL 640BB HAS FRETTING DAMAGE INBD AND OTBD ENDS. COMPLIED WITH EC/TC EO600-57-81, C/W IAW REO 601R-57-21-030, REV L.

Part: SEAT TRACK — CORRODED (BS 349-395) · airframe 26,238 hrs · 24,746 cycles

RT RBL 9 FIRST SEAT TRACK IS CORRODED FROM FS 349 TO FS 395. COMPLETED AND INSTALLED ON RBL 9 FIRST SEAT TRACK FS 349 TO FS 395 IAW SRM 53-21-49 & IAW AMM 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 559-574) · airframe 26,238 hrs · 24,746 cycles

IN CARGO COMPARTMENT, BETWEEN BS 559+112 - 574 RBL 9 SEAT TRACK HAS CORROSION. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-41-02, AND SRM 51-41-04.

Part: FRAME — CORRODED (BS 319) · airframe 26,238 hrs · 24,746 cycles

FS 319 HAS CORROSION BETWEEN STRINGERS 26 - 27L. REMOVED LOWER FRAME SECTOR AT FS 319.00 IAW SRM 51-42-06 AND 51-42-21. LOCATED AND DRILLED NEW SERVICEABLE LOWER FRAME SECTOR AT FS 319.00 IAW SRM 51-40-11. INSTALLED FS 319.00 LOWER FRAME SECTOR, PN:601R32003-61 IAW SRM 51-42-06 AND 51-42-21.

Part: FLOOR SUPPORT — CORRODED (BS 559-621) · airframe 26,238 hrs · 24,746 cycles

IN CARGO COMPARTMENT UNDER FLOORBOARD BETWEEN BS 559+112 - 621 RBL 36 THE RT FLOOR SUPPORT HAS CORROSION. COMPLIED WITH EC/TC REO 601R-53-00-526 01 AND GREO 601R-53-00-526, REV.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 26,238 hrs · 24,746 cycles

IN CARGO COMPARTMENT BETWEEN FS 559.00+96 TO FS 559.00+112 ON RBL 9.00 THE FLOOR SEAT TRACK HAS PITTING CORROSION. REPLACED & INSTALLED NEW SEAT TRACK ON RBL 9.00, FS 559.00+96 TO FS 559.00+112 IAW SRM 51-41-04.

Part: FLOORBEAM — CORRODED (BS 589) · airframe 26,238 hrs · 24,746 cycles

IN CARGO COMPARTMENT FLOORBEAM BS 589 BETWEEN RBL 27 - 36 HAS CORROSION. REMOVED AND REPLACED THE FLOORBEAM TOP CAP IAW SRM 51-42-06-00, AND 51-42-10.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 26,238 hrs · 24,746 cycles

IN CARGO COMPARTMENT BETWEEN BS 559+96 TO 559+112 ON RBL 27 THE FLOOR SEAT TRACK HAS CORROSION. R & R FITTING SEAT TRACK IAW SRM 251-41-04.

Part: FLOOR SUPPORT — CORRODED (BS 310-319) · airframe 26,238 hrs · 24,746 cycles

RIGHT FLOOR SILL IS CORRODED BETWEEN FS 310-319. FLOOR SILL BETWEEN FS 310-319 RT ORIG MATERIAL 0.063", MATERIAL BLENDED OFF 0.008", REMAINING MATERIAL 0.054". IN LIMIT ALLOWED IAW REO 601R-53-00-530 AND SRM 51-21-06. COMPLIED WITH REO 601R-53-00-530, REV A DATED 10/7/14. REPAIRED FLOOR SILL BETWEEN FS 280 TO 409+128 IAW REO 601R-53-00-530, REV A. COMPLIED WITH REO 601R-53-00-530, REV A DATED 10/7/2014.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 26,238 hrs · 24,746 cycles

IN CARGO COMPARTMENT BETWEEN FS 559.00+96 TO FS 559.00+112 ON LBL 27.00 THE FLOOR SEAT TRACK HAS PITTING CORROSION. REMOVED FLOOR TRACK AT FS 559+96 TO FS 559+112 LBL 27 IAW SRM 51-41-02. REPLACED AND INSTALLED FLOOR TRACK AT FS 559.00+96 TO FS 559.00+112, LBL 27.00 IAW SRM 51-41-04, PN 601R38779-9.

Part: SEAT TRACK — CORRODED (BS 349-395) · airframe 26,238 hrs · 24,746 cycles

LT LBL 9 FIRST SEAT TRACK IS CORRODED FROM FS 349 TO FS 395. COMPLETED AND INSTALLED ON LBL 9 FIRST SEAT TRACK, FS 349 TO FS 395 IAW SRM 53-21-49 & IAW AMM 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 26,238 hrs · 24,746 cycles

IN CARGO COMPARTMENT, BETWEEN BS 559+96 TO 559+112 ON LBL 9.00 THE FLOOR SEAT TRACK HAS CORROSION. REPLACED & INSTALLED NEW SEAT TRACK IAW SRM 51-41-04.

Part: FLOOR SUPPORT — CORRODED (BS 280-409) · airframe 26,238 hrs · 24,746 cycles

CORROSION AROUND SCREW HOLE JUST AFT OF FS 349 LT SIDE ON SILL. REPAIRED FLOOR SILL BETWEEN FS 280 TO FS 409+128 IAW REO 601R-53-00-530, REV A.

Part: SEAT TRACK — CORRODED (BS 559-574) · airframe 26,238 hrs · 24,746 cycles

IN CARGO COMPARTMENT BETWEEN BS 559+112 - 574 LBL 9 THE SEAT TRACK HAS CORROSION. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-41-02 AND SRM 51-41-04.

Part: FLOOR SUPPORT — CORRODED (BS 559) · airframe 26,238 hrs · 24,746 cycles

IN PASSENGER COMPARTMENT FROM FS 559.00+48 TO FS 559.00+80 ON LBL 36.00 THE LT FLOOR SILL AROUND FLOORBOARD ATTACHMENT HOLES AT SEVERAL LOCATIONS HAVE PITTING CORROSION. COMPLIED WITH REO 601R-53-00-526. COMPLIED WITH EC/TC REO 601R-53-00-526 AND GREO 601R-53-00-526, REV- DATED 05/22/2015 AS WRITTEN.

Part: FLOOR SUPPORT — CORRODED (BS 310-319) · airframe 26,238 hrs · 24,746 cycles

RT FLOOR SILL DOUBLER IS CORRODED BETWEEN FS 310-319. UPON FURTHER INVESTIGATION, FOUND FLOOR SILL DOUBLER TO BE OUT OF LIMITS, REQUIRES REPLACEMENT. REMOVED FLOOR SILL DOUBLER IAW SRM 51-42-06. RECEIVED NEW SERVICEABLE FLOOR SILL DOUBLER. LOCATED AND DRILLED NEW SERVICEABLE DOUBLER IAW SRM 51-40-11. INSTALLED DOUBLER IAW SRM 51-42-06.

Part: FLOOR SUPPORT — CORRODED (BS 589-619) · airframe 26,238 hrs · 24,746 cycles

IN CARGO COMPARTMENT BETWEEN BS 589 - 619 LBL 27 FLOOR SUPPORT HAD CORROSION. REMOVED THE CORROSION IAW REO 601R-53-00-005, REV B. FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED THE FLOOR SUPOPRT IAW SRM 51-42-21, 51-42-22, AND REO 601R-53-61-3778, REV A.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 26,238 hrs · 24,746 cycles

IN PASSENGER COMPARTMENT FROM FS 559.00+4 TO FS 559.00+117 ON RBL 9.00 THE RT FLOOR SEAT TRACK HAS PITTING CORROSION. INSTALLED NEW SEAT TRACK AT RBL 9 FS 559+4 TO FS 559+117 IAW REO 60R-53-00-485. LOCATED, DRILLED UP AND COUNTERSINK ON NEW SEAT TRACK RBL 9.00, FS 559.00+4 TO FS 559.00+117 IAW SRM 51-40-11. FABRICATED SEAT RAILS IAW GREO 601R-53-00-485, REV.A.

Part: FRAME — CORRODED (BS 333) · airframe 26,238 hrs · 24,746 cycles

FS 333 HAS CORROSION BETWEEN STR 26 - 27L. REMOVED UNSERVICEABLE RT VERTICAL POST FS 333 IAW SRM 51-42-06. INSTALLED NEW SERVICEABLE FRAME SECTOR AT FS 333.00 IAW SRM 51-42-06 AND SRM 51-42-21.

Part: CHANNEL — CORRODED (BS 280) · airframe 26,238 hrs · 24,746 cycles

FS 280, FWD "J" CHANNEL IS CORRODED. REMOVED UNSERVICEABLE FS 280.00, FWD "J" CHANNEL IAW SRM 51-42-06. RECEIVED NEW SERVICEABLE FWD "J" CHANNEL, PN 600-34017-351S. LOCATED AND DRILLED CHANNEL IAW SRM 51-40-11. INSTALLED NEW SERVICEABLE FWD "J" CHANNEL IAW SRM 51-42-06 AND SRM 51-42-21.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 26,238 hrs · 24,746 cycles

IN PASSENGER COMPARTMENT FROM FS 559.00+4 TO FS 559.00+117 ON LBL 9.00 THE LT FLOOR SEAT TRACK HAS PITTING CORROSION. INSTALLED NEW SEAT TRACK AT LBL 9, FS 559+4 TO FS 559+117 IAW REO 601R-53-00-485. LOCATED, DRILLED UP AND COUNTERSINK ON NEW SEAT TRACK LBL 9.00, FS 559.00+4 TO FS 559.00+117 IAW SRM 51-40-11. FABRICATED SEAT RAILS IAW GREO 601R-53-00-485 REV A.

Part: ANGLE — CRACKED · airframe 26,238 hrs · 24,746 cycles

IN FLIGHT COMPARTMENT THE PILOT'S SIDE WINDSHIELD POST THE LOWER OTBD ANGLE FITTING IS CRACKED. REMOVED CRACKED WINDSHIELD FITTING ON THE LOWER AFT SIDE OF PILOTS SIDE WINDSHIELD POST IAW SRM 51-42-21. DRILLED, LOCATED AND INSTALLED NEW SERVICEABLE WINDSHIELD FITTING ON THE AFT SIDE OF PILOT'S SIDE WINDSHIELD POST IAW SRM 51-40-11 AND SRM 51-42-21.

Part: VERTICAL SUPPORT — CRACKED (BS 409) · airframe 26,238 hrs · 24,746 cycles

FS 409+128 VERT POST BL 0 LT & RT SIDE HAVE INDICATIONS NOTED IN THE AFT FLANGE RADIUS AT WL 69 APPROX .250" LONG BY 90 PERCENT FSH. BOTH FAILED NDT INSP. REMOVED VERTICAL POST AT FS 409+128 BL 00 IAW SRM 51-42-06 & SRM 51-42-21. INSTALLED VERTICAL POST AT FS 409+128 BL 00 IAW SRM 51-42-06 & 51-42-22 & REO 601R-53-41-889. LOCATED & DRILLED NEW SERVICEABLE VERTICAL POSTS AND ANGLES AT FS 409+128, BL 0 IAW SRM 51-40-11. COMPLIED WITH EC/TC REO 601R-53-41-889 AND MET ALL THE REQUIREMENTS OF REO 601R-53-41-889, REV A.

Part: ANGLE — CRACKED (BS 280) · airframe 26,238 hrs · 24,746 cycles

FS 280 LOWER "J" ANGLE IS CRACKED AT RBL 9. COMPLIED WITH EC/TC REO 601R-53-11-171 AND MET ALL THE REQUIREMENTS OF REO 601R-53-11-171.

Part: ANGLE — CRACKED (BS 280) · airframe 26,238 hrs · 24,746 cycles

FS 280 LOWER "J" ANGLE IS CRACKED AT LBL 9. COMPLIED WITH EC/TC REO 601R-53-11-171 AND MET ALL THE REQUIREMENTS OF REO 601R-53-11-171.B.

Part: VERTICAL SUPPORT — CRACKED (BS 409) · airframe 26,238 hrs · 24,746 cycles

FS 409+128, RBL 18 VERT POST OTBD SIDE HAS AN INDICATION NOTED IN THE AFT FLANGE .250" LONG X 60 PERCENT FSH. FAILED NDT INSP. REMOVED FS 409+128 RBL 18 VERTICAL POST IAW SRM 51-42-06. INSTALLED NEW SERVICEABLE POST AT FS 409+128, RBL 18 IAW SRM 51-42-06 AND REO:601R-53-41-889. COMPLIED WITH EC/TC REO:601R-53-41-889 AND MET ALL REQUIREMENTS OF REO:601R-53-41-889, REV A. COMPLIED WITH EC/TC SNIEO:601R32208S16 AND SNIEO:601R32208 816 AS WRITTEN.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 26,238 hrs · 24,746 cycles

FS 280, RBL 9 INBD AND OUTBD ANGLES ARE CRACKED. REMOVED AND REPLACED THE ANGLE IAW SRM 51-42-21.

Part: ANGLE — CRACKED (BS 484) · airframe 26,238 hrs · 24,746 cycles

BS 484, ANGLE AT RBL 27 IS CRACKED. R & R ANGLE IAW RM 51-42-21 & 51-40-11.

Part: ATTACH BRACKET — CORRODED (SERVICE DOOR) · airframe 26,238 hrs · 24,746 cycles

ATTACH BRACKET FOR SERVICE DOOR AFT DRAIN CORRODED. R & R THE ATTACH BRACKET IAW SRM 51-41-02.

Part: ANGLE — CRACKED (BS 484) · airframe 26,238 hrs · 24,746 cycles

FS 484, ANGLE AT RBL 36 IS CRACKED AT PREVIOUS REPAIR. REMOVED ANGLE AT FS 484.0, RBL 36 IAW SRM 51-42-21. FABRICATED, DRILLED, LOCATED AND INSTALLED ANGLE, PN 601R-53-41-1940-2 IAW REO 601R-53-41-1940, REV-- DATED 2015/08/13, GREO 601R-53-41-059, REV B DATED 2009/09/16, SRM 51-24-21, 51-40-11, 51-42-21. REO 601R-53-41-1940, REV HAS BEEN ACCOMPLISHED AND ALL STEPS HAVE BEEN DOCUMENTED AND SIGNED FOR ON A NON-ROUTINE WORK CARD.

Part: ANGLE — CRACKED (BS 484) · airframe 26,238 hrs · 24,746 cycles

BS 484, ANGLE AT LBL 27 IS CRACKED. R & R THE ANGLE IAW SRM 51-42-21 & 51-40-11.

Part: ANGLE — CRACKED (BS 280) · airframe 26,238 hrs · 24,746 cycles

BS 280, STR 3L, UPPER ANGLE IS CRACKED. REMOVED AND REPLACED THE ANGLE IAW SRM 51-42-06, AND 51-42-21.

Part: ANGLE — CORRODED (SERVICE DOOR) · airframe 26,238 hrs · 24,746 cycles

SERVICE DOOR LOWER SILL UPPER ANGLE HAS PITTED CORROSION. REMOVED UNSERVICEABLE DOOR SILL ASSY IAW SRM 51-42-06, 51-42-21, 51-42-13. INSTALLED DOOR SILL ASSEMBLY WHICH INCLUDES ANGLE 601R38303-105, ITEM 3 AND ANGLE 601R38303-253, ITEM 4 IAW SRM 51-42-06, 51-42-21, 51-42-15, 51-42-36. UPON FURTHER INVESTIGATING SILL ANGLE, PN 601R38303-105 IS NOT CORRODED. SILL ANGLE REQUIRES INSTALL. REINSTALLED SILL ANGLE PN 601R38303-105, COMMON TO ANGLE 601R38303-253 IAW SRM 51-42-06 AND 51-42-13. ANGLE 601R38303-253 DRILLED AND NEEDS TO BE INSTALLED IAW SRM 51-40-11. TORQUED & SAFETIED LOWER DOCK FITTINGS & INSTALLED STEP PLATE IAW 25-33-01-400-802. ADJUSTMENT CHECK GOOD IAW 52-41-00-820-801.

Part: STIFFENER — GOUGED (PAX DOOR) · airframe 26,238 hrs · 24,746 cycles

INTERNAL PASSENGER DOOR, PRESSURE RELIEF DOOR INNER STIFFENER IS GOUGED APPROXIMATELY .100 LONG, .100 WIDE AND .020 DEEP. COMPLIED WITH REO 601R-52-11-1040, REV ISSUE 2006/10/30. REPAIR TO THE NICK, 1 GOUGE DAMAGE ON THE VENT FLAP ON THE PAX DOOR IS COMPLETED IAW REO:601R-52-11-1040. THE REPAIR MEETS ALL THE REQUIREMENTS OF REO:601R-52-11-1040.

Part: ANGLE — CRACKED (BS 484) · airframe 26,238 hrs · 24,746 cycles

FS 484, ANGLE AT LBL 36 IS CRACKED. REMOVED AND REPLACED THE ANGLE6 IAW SRM 51-42-21, AND REO 601R-53-41-1940, REV.

Part: BULKHEAD — CHAFED (BS 621) · airframe 26,238 hrs · 24,746 cycles

BS 621 PRESSURE BULKHEAD HAS 5 SCREW CHAFES AT LBL 18, 27, RBL 18, 27, 36, WL 103. REMOVED CHAFED MARKS BY BLENDED MATERIAL OFF 0.006". DETERMINED WITHIN LIMIT IAW REO 601R-53-61-2155, STEP 1 TO 5, REV A 2013-08-13. COMPLIED WITH EC/TC, REO 601R-53-61-2155 AND MET ALL THE REQUIREMENTS OF REO 601R-53-61-2155, REV A DATED 08/13/2013.

Part: ISOLATOR — BROKEN (BS 621 BULKHEAD) · airframe 26,238 hrs · 24,746 cycles

BS 621 PRESSURE BULKHEAD HAS TWO BROKEN ISOLATORS. REMOVED AND REPLACED THE ISOLATOR IAW SRM 51-42-06, AND SRM 51-42-06.

Part: STRINGER — CRACKED (BS 379) · airframe 26,238 hrs · 24,746 cycles

BS 379, STR 3L HAS A CRACK. CUT THE DAMAGED SECTION OF STRINGER. LOCATE AND DRILLED EXTRUSION S6807, NEW SERVICEABLE EXTRUSION. ALL WORK WAS DONE IAW SRM TR 53-51. FABRICATED SPLICES FROM S6957-17 AND S6957-18 IAW SRM TR 53-51. COMPLIED WITH SRM 53-00-03, TR 53-51. INSTALLATION COMPLETE. REPAIR DONE IAW SRM.

Part: FRAME — CORRODED (BS 349) · airframe 26,238 hrs · 24,746 cycles

FS 349, FRAME IS CORRODED AT STR 27. REMOVED LT AND RT FRAME STRAP IAW SRM 51-42-06. REINSTALLED LT AND RT FRAME STRAP GUSSETS AT FS 349 IAW SRM 51-42-06. REMOVED LT AND RT VERTICAL POST ATTACHED TO TRANSVERSE BEAM AND FS 349.00 IAW SRM 51-42-21. REINSTALLED SAME SERVICEABLE LT AND RT VERTICAL POST ATTACHING TRANSVERSE BEAM AND FRAME AT FS 349 IAW SRM 51-42-21. REMOVED LT AND RT INTERCOSTAL ATTACHED TO STR 25 IAW SRM 51-42-06. REINSTALLED INTERCOSTALS AT STR 25R AND 25L, FS 333-349 IAW SRM 51-42-06.

Part: ANGLE — CRACKED (NLG DOOR FRAME) · airframe 26,238 hrs · 24,746 cycles

NLG CUTOUT AFT LT CORNER IS CRACKED APPROXIMATELY .5"L. C/W ECTC REO 601R-53-11-0048 IAW REO 601R-53-11-0048, REV C1.

Part: SKIN — CORRODED (BS 559) · airframe 26,238 hrs · 24,746 cycles

LOWER FUSELAGE SKIN BS 559+80 - 559+112, STRINGER 26L - 26R CORRODED. FOUND OUT OF LIMITS IAW SRM 53-00-31. BLENDED DAMAGE IAW SRM 51-21-06. PERFORMED ULTRASONIC THICKNESS OF SKIN IAW NDTM 51-20-04. FOUND WITHIN LIMITS IAW EA 26-2015-100.

Part: SKIN — DAMAGED (BS 589-605) · airframe 25,058 hrs · 23,555 cycles

MULTIPLE GOUGES AND DENTS ON FUSELAGE AND REPAIR DOUBLERS FROM BS 589 TO FS 605, BETWEEN STR 21R AND STR 27. BLENDED MULTIPLE GOUGES AND DENTS ON FUSELAGE AND REPAIR DOUBLERS FROM FS 589 TO FS 605, BETWEEN STR 21R AND STR 27 IAW SRM 51-12-00. R & R 4 FASTENERS BETWEEN FS 589.00 AND FS 605.00 2 RIVETS ON STR 22R AND 2 ON STR 23R IAW REO 601R-53-61-5411. DRILLED .1562 HOLE AND INSTALLED NAS1097-5 RIVET IN THE MIDDLE OF THE NICK IAW REO 601R-53-61-5411. CREATED MCO A473539 FOR PERMANENT REPAIR FOR REO 601R-53-61-5411 AND MCO A473540 FOR PERMANENT REPAIR FOR REO 601R-53-61-5412 IAW SRM 51-13-01.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 24,156 hrs · 22,660 cycles

F/A'S FLASHLIGHT DOES NOT WORK. R & R FLASHLIGHT IAW AMM 25-60-00.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 22,452 hrs · 20,934 cycles

RT AFT EXTERNAL EMERGENCY LIGHT INOPERATIVE. R & R BULB IAW AMM 33-51-21. OP'S CHECKED GOOD.

Part: SKIN — CORRODED (BS 409) · airframe 21,947 hrs · 20,417 cycles

CORROSION WAS FOUND UNDER SELF-CONTOURING SEALING PAD FROM STR26 TO STR24, FROM 409+80 TO 409+400 ON BELLY SKIN. REPAIRED IAW SRM 51-21--06 AND REO 601R-53-31-789.

Part: FLOOR SUPPORT — CORRODED · airframe 21,947 hrs · 20,417 cycles

FLOOR SUPPORT SCREW HOLES HAVE CORROSION. REMOVED CORROSION IAW SRM 51-21-06-00.

Part: FLOOR SUPPORT — CORRODED (BS 574-621) · airframe 21,947 hrs · 20,417 cycles

LEFT FLOOR SUPPORT IN CARGO BAY CORRODED FROM FS 574 TO 621. REPAIRED IAW SRM 51-21-06-10, REO 601R-53-00-526.

Part: FLOOR SUPPORT — CORRODED (CARGO BAY) · airframe 21,947 hrs · 20,417 cycles

RT FLOOR SUPPORT CORRODED IN CARGO COMPT AT FS 559 + 112. REPAIRED IAW SRM 51-21-06-00, REO 601R-53-00-256 AND REO 601R-53-00-526 01.

Part: FLOOR SUPPORT — CORRODED (BS 618) · airframe 21,947 hrs · 20,417 cycles

RT FLOOR SUPPORT CORRODED IN CARGO BAY AT FS 618. REPAIRED IAW SRM 1-1-06-00 AND REO 601R-53-00-526.

Part: SIGN — BROKEN (EMERGENCY LIGHTS) · airframe 21,945 hrs · 20,414 cycles

SERVICE DOOR INNER HANDLE EXIT PLACARD SELF ILLUMINATED BROKEN AT LOWER SCREW ATTACHMENT. R & R EXIT PLACARD WITH SERVICEABLE ONE IAW AMM 33-51-09-000-802 AND 33-51-09-400-802. PERFORMED FUNCTIONAL CHECK OF EXIT PLACARD IAW AMM 33-51-09-720-801.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 21,946 hrs · 20,416 cycles

CRACKED INTERCOSTAL ON ASD AFT SIDE LOWER SECTION INSIDE PANEL 832BR. REMOVED DAMAGED INTERCOSTAL IAW SRM 51-42-06 AND DRILLED NEW INTERCOSTAL TO FIT IAW SRM 51-40-11 AND INSTALLED INTERCOSTAL IAW SRM 51-42-06.

Part: ANGLE — CRACKED (BS 625.3) · airframe 21,945 hrs · 20,414 cycles

ANGLE CRACKED AT FRAME BS 625.3, S14R IN AFT EQUIP BAY. REMOVED CRACKED ANGLE IAW SRM 51-42-20. INSTALLED SERIVCABLE ANGLE IAW SRM 51-42-21.

Part: ANGLE — CRACKED (BS 625.3) · airframe 21,945 hrs · 20,414 cycles

ANGLE CRACKED AT FRAME BS 625.3, S14L IN AFT EQUIP BAY. REMOVED CRACKED ANGLE IAW SRM 51-42-20. INSTALLED REPLACEMENT ANGLE IAW SRM 51-42-21-00.

Part: ROLLER — OUT OF ADJUST (PAX DOOR HANDLE) · airframe 21,945 hrs · 20,414 cycles

PAX DOOR HANDLE TAKES MORE THAN 16LBS OF FORCE TO FULLY UNLATCH. REMOVED SAFETY WIRE AND ADJUSTED PAX DOOR HANDLE ROLLER IAW AMM 52-11-25-830-801. REPLACED SAFETY WIRE ON PAX DOOR HANDLE AMM 20-24-00-910-802. PERFORMED OPS TEST OF PAX DOOR WARNING SYS IAW AMM 52-70-04-710-803, CK GOOD.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 21,490 hrs · 19,912 cycles

LIGHTED EXIT SIGN ON BULKHEAD NEAR PAX DOOR MISSING COVER. FOUND FLOODLIGHT COVER & RESECURED IAW AMM 33-51-19.

Part: DOOR — BINDING (MAIN PAX) · airframe 21,307 hrs · 19,718 cycles

PAX DOOR WILL NOT OPEN. PERFORMED OPS CHECK OF PAX DOOR IAW AMM 52-11-08. OPS CHECK GOOD.

Part: STEP — CRACKED (PAX DOOR) · airframe 20,197 hrs · 18,539 cycles

PASSENGER DOOR HAS A CRACK BELOW THE TOP STEP. REPAIRED IAW REO 601R-52-11-279.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 19,860 hrs · 18,164 cycles

CEILING EMERGENCY LIGHT INOPERATIVE. RELAMPED EMERGENCY FLOOD LIGHT. OPS CHECKED GOOD.

Part: OVERHEAT LOOP — UNSERVICEABLE (LT NACELLE) · airframe 19,709 hrs · 18,003 cycles

LEFT 14TH DUCT WARNING MESSAGE ON DESCENT THRU 18000 FEET. EMERGENCY DECLARED. R & R LT ENG PYLON 14TH STAGE SENSING LOOP IAW AMM 36-21-04.

Part: LAMP — INOPERATIVE (EMEGENCY LIGHT) · airframe 19,575 hrs · 17,848 cycles

LEFT EXTERIOR OVERWING FWD EMERGENCY LIGHT INOPERATIVE. RELAMPED LT SIDE EXTERIOR OVERWING FWD EMERGENCY LIHGT IAW AMM 33-51-21. OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,454 hrs · 17,700 cycles

ONE CEILING EMERGENCY LIGHT IS OUT. 2ND LIGHT BACK FROM FRONT. RESECURED CEILING EMERGENCY LIGHT IAW AMM 33-51-09. OPS CHECKED GOOD.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 19,202 hrs · 17,417 cycles

THE AFT EMERGENCY LIGHT OVER THE LEFT WING IS INOPERATIVE. RELAMPED THE AFT LEFT WING EMERGENCY LIGHT IAW AMM 33-51-21. OPS CHECKED GOOD.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 19,086 hrs · 17,280 cycles

NR 4 EXTERIOR EMERGENCY LIGHT INOPERATIVE. RELAMPED IAW AMM 33-51-21. OPS CHECKED GOOD.

Part: FLAP SYSTEM — FAILED (TE FLAP) · airframe 18,210 hrs · 16,325 cycles

RECEIVED FLAPS FAIL WHEN SELECTED FOR LANDING FAILED AT ZERO (EMERGENCY DECLARED AS A PRECAUTION) REFER TO AFDL 622132-1, AD 2009-06-12.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 17,483 hrs · 15,515 cycles

FWD AND AFT CEILING EMERGENCY LIGHT INOP // (RESOLVED ON W/O: 193469 TASKCARD: N/R-00004 ) / 3/2/11...RELAMPED FWD AND AFT CEILING EMERGENCY LIGHT IAW CRJ200 AMM 33-51-14. OPS CHECK GOOD / ITEM: 1 / 3/2/11...RELAMPED FWD AND AFT CEILING EMERGENCY LIGHTS IAW CRJ200 AMM 33-51-14. OPS CHECK GOOD

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 17,408 hrs · 15,429 cycles

F/A FLASHLIGHT INOP. R & R F/A FLASHLIGHT IAW AMM 25-61-00. OPS CHECKS GOOD.

Part: BRACKET — BENT (NLG) · airframe 17,189 hrs · 15,171 cycles

RECEIVED NOSE DOOR AND GEAR DISAGREE CAUTION MSGS NOSE GEAR DID NOT RETRACT CYCLED GEAR 2 MORE TIMES - CONDITION REPEATED LANDED AT 50,000 LBS WITH TOUCH DOWN RATE LESS THAN. (ACFT RETURNED TO DEPARTURE AFTER TO -- EMERGENCY DECLARED) COMPLIED WITH GEAR SWINGS IAW AMM 32-30-00. R & R NLG PROX SENSOR BRACKET IAW AMM 32-52-01, PROX SENSOR REQUIRES ADJUSTMENT AND GEAR SWINGS. ADJUSTED NLG PROX SENSOR IAW 32-61-05, CLEARANCE CKS GOOD / ITEM: 3 / COMPLIED WITH GEAR SWINGS IAW AMM 32-30-00. (CLOSED)

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHT) · airframe 17,058 hrs · 15,013 cycles

RT OVERWING FLOOR LEVEL EXIT ID INOPERATIVE. R & R NR3 EMERGENCY LIGHT INVERTER IAW MM 33-51-07-000-801 & -400-801. EMERGENCY LIGHTS OPS CK OK IAW MM 33-51-00-710-801.

Part: FLOORBEAM — CORRODED (BS 362) · airframe 17,046 hrs · 14,999 cycles

MWC 362, LBL 27, FLOORBEAM CAP IS CORRODED AROUND NUTPLATE AT FS 605. "12. C/W EC/TC REO 601R-53-61-3778 AND REO 601R-53-61-3778, REV DATED 08/21/2010 AS WRITTEN. FOUND TO BE SATISFACTORY."

Part: ANGLE — CRACKED (FUSELAGE) · airframe 17,046 hrs · 14,999 cycles

LEFT AND RIGHT OBLIQUE ANGLES CRACKED FS 621-625, STRG 15 LEFT AND RIGHT. RESOLVED ON W/O: 180442 TASKCARD: N/R-00693. REMOVED LT/RT OBLIQUE ANGLES FROM FS 625 STR 15 IAW CRJ 200 SRM 51-42-21. PREPARED AND DRILLED LT/RT OBLIQUE ANGLES IAW CRJ 200 SRM 51-40-11. INSTALLED LT/RT OBLIQUE ANGLES AT FS 625 STR 15 IAW CRJ 200 SRM 51-42-21. THIS REPAIR IS CLASSIFIED AS A MINOR REPAIR IAW ASA SOP 5702.

Part: ANCHOR FITTING — CRACKED (PAX DOOR) · airframe 17,053 hrs · 15,007 cycles

PAX DOOR ANCHOR FITTING CRACKED. REPLACED AFT PAX DOOR ANCHOR FITTING IAW AMM 52-11-17-000-804 AND 52-11-17-400-804. PAX DOOR OP'S CHECK GOOD RII ACCOMPLISHED ON LISTED WVAC NRI BY INSPECTOR.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 17,046 hrs · 14,999 cycles

LBL 27 FLOORBEAM CAP IS CORRODED AROUND NUTPLATES AT FS 605.00. FLOORBEAM REPAIRED IAW SRM 51-21-11. ACFT RETURNED TO SERVICE.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 17,046 hrs · 14,999 cycles

FS 349 FRAME HAS CORROSION ON SHEAR TIE AT STR 27. REO 601R-53-21-1199, HAS BEEN ACCOMPLISHED. ACFT RETURNED TO SERVICE.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 17,046 hrs · 14,999 cycles

BRACKET AT FS 559 BETWEEN RBL 9 AND BL 0.0 IS CRACKED AT RBL 9 FWD FASTENER HOLE. REMOVED BRACKET IAW SRM 51-42-06. BRACKET INSTALLED IAW SRM 51-42-06.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 17,046 hrs · 14,999 cycles

SEAT TRACK AT FS 559+86-559+96 LBL 9 HAS CORROSION. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-41-02. J REPAIR IS CLASSIFIED AS A MINOR REPAIR IAW SOP 5702.

Part: SEAT TRACK — CORRODED (BS 612-617) · airframe 17,046 hrs · 14,999 cycles

SEAT TRACK AT FS 612-617 LBL 9 HAS CORROSION. SEAT TRACK REPLACED IAW SRM 51-41-04.

Part: STRINGER — CORRODED (BS 333 S27) · airframe 17,046 hrs · 14,999 cycles

FRAME FS 333.00 SECTOR AT STRINGER 27 IS CORRODED. REMOVED FRAME IAW SRM 51-42-06. INSTALLED FRAME IAW SRM 51-42-06.

Part: SEAT TRACK — CORRODED (BS 574-605) · airframe 17,046 hrs · 14,999 cycles

(2 EA) SEAT TRACK ANCHOR POINTS AT FS 574-605 LBL 9 HAS CORROSION. SEAT TRACK REPLACED IAW SRM 51-41-04.

Part: SEAT TRACK — CORRODED (BS 559-574) · airframe 17,046 hrs · 14,999 cycles

SEAT TRACK ANCHOR POINTS (3EA) AT FS 559+96-574 ARE CORRODED LBL 27. SEAT TRACK ANCHOR POINTS AT F.S. 559+96-574 REPLACED IAW SRM 51-41-04.

Part: INTERCOSTAL — DAMAGED (BS 484) · airframe 17,046 hrs · 14,999 cycles

FS 484, RBL 27 AND RBL 36 INERCOSTAL REPAIR CLIPS ARE CRACKED FROM UPEPR FASTENER TO EDGE OF PART. REPAIR TO THE INTERCOSTAL COMPLETED IAW REO 601R-53-41-059 AND MEETS ALL THEIR REQUIREMENTS

Part: RIB — CRACKED (RT WING) · airframe 17,046 hrs · 14,999 cycles

RT BATT RIB IS CRACKED AT TOP FASTENER. COMPLIED WITH EC/TC REO 601R-57-51-046 REPAIR NR 2.

Part: SEAT TRACK — CORRODED (BS 559-568) · airframe 17,046 hrs · 14,999 cycles

SEAT TRACK AT FS 559+112-568, LBL 9 HAS CORROSION. REMOVED DAMAGED SEAT TRACK, LOCATED, DRILLED, AND INSTALLED NEW SERVICEABLE SEAT TRACK IAW SRM 51-41-02. REPAIR IS CLASSIFIED AS A MINOR REPAIR IAW SOP 5702.

Part: ANCHOR FITTING — CRACKED (PAX DOOR) · airframe 17,046 hrs · 14,999 cycles

PASSENGER DOOR AFT ANCHOR FITTING IS CRACKED. REPAIRED ANCHOR FITTING SIDE PASSENGER DOOR IAW AMM 52-11-17-000-804 AND 52-11-17-400-804.

Part: RIB — CRACKED (LT WING) · airframe 17,046 hrs · 14,999 cycles

LT BATT RIB IS CRACKED AT TOP FASTENER. COMPLIED WITH REO 601R-57-51-046 REPAIR NO.2 STEPS 1, 2, 3 AND 4. COMPLIED WITH REO 601R-57-51-046 REPAIR NR 2 STEPS 5-10.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 17,046 hrs · 14,999 cycles

PAX DOOR AFT DRAG ANGLE IS CRACKED. REMOVED CRACKED ANGLE, INSTALLED NEW ANGLE IAW SRM 51-42-06/-13/-15/-22. REPAIR IS CLASSIFIED AS A MINOR REPAIR IAW SOP 5702.

Part: PLACARD — WORN (ESCAPE HATCH) · airframe 17,046 hrs · 14,999 cycles

CREW ESCAPE HATCH SILKSCREENS AND PLACARDS ARE WORN. APPLIED NEW SILKSCREENS ON CREW ESCAPE HATCH IAW MM 11-10-03-400-801.

Part: FLOORBEAM — CORRODED (BS 605) · airframe 17,046 hrs · 14,999 cycles

LBL 27, FLOORBEAM CAP IS CORRODED AROUND NUTPLATES AT FS 605.00. BLENDED CORROSION ON FLOORBEAM & FOUND TO BE OUT OF LIMITS IAW SRM 53-61-43, 53-00-00 FIG 101. REMOVED FLOORBEAM CAP IAW SRM 51-42-06, 51-42-21. LOCATED AND DRILLED FLOORBEAM CAP IAW REO 601R-53-61-3778. INSTALLED FLOORBEAM CAP IAW CRJ REO'S 601R-53-61-3778 AND 601R-53-61-3889.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 17,046 hrs · 14,999 cycles

SEAT TRACK AT FS 559+80-559+96 LBL 27 HAS CORROSION. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-41-02. REPAIR IS CLASSIFIED AS A MINOR REPAIR IAW SOP 5702.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 17,046 hrs · 14,999 cycles

SEAT TRACK AT FS 559+86-559+96, RBL 9 HAS CORROSION. SEAT TRACK REPLACED IAW SRM 51-41-04.

Part: SEAT TRACK — CORRODED (BS 559-574) · airframe 17,046 hrs · 14,999 cycles

SEAT TRACK AT FS 559+112-574, RBL 9 HAS CORROSION. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-41-02. REPAIR IS CLASSIFIED AS A MINOR REPAIR IAW SOP 5702.

Part: SILL — CORRODED (FUSELAGE) · airframe 17,046 hrs · 14,999 cycles

PAX DOOR CUTOUT LOWER FLOOR SILL IS CORRODED AT PROX SENSOR. RESOLVED ON W/O: 180442 TASKCARD: N/R-00546 . UPON FURTHER INVESTIGATION FOUND PAX DOOR LOWER SILL ANGLE TO BE CORRODED BEYOND LIMITS. LOWER SILL ANGLE REQUIRES REPLACEMENT. LOWER PAX DOOR SILL ANGLE REQUIRES REPLACEMENT. REMOVED THE PAX DOOR LOWER FLOOR SILL ANGLE. LOCATED AND DRILLED A NEW ANGLE TO MATCH THE FUSELAGE IAW CRJ20 SRM 51-42-01, 51-42-06, 51-0-11, 51-42-10. FLOOR SILL REQUIRES INSTALLATION. INSTALLED PAX DOOR LOWER FLOOR SILL ANGLE IAW CRJ 200 SRM 51-42-06, 51-42-21 AND 51-42-11. RIVETLESS NUTPLATES NEED INSTALLED ON PAX DOOR LOWER SILL PLATE. INSTALLED RIVETLESS NUTPLATES ON PAX DOOR LOWER SILL PLATE IAW CRJ 200 SRM 51-22-00. CURE CHECK REQUIRED ON PAX DOOR LOWER SILL PLATE RIVETLESS NUTPLATES. CURE CHECK GOOD IAW CRJ AMM 51-23-00-390-815. THIS REPAIR IS CLASSIFIED AS A MINOR REPAIR IAW ASA SOP 5702.

Part: BULKHEAD WEB — CRACKED (FUSELAGE) · airframe 17,046 hrs · 14,999 cycles

FOUND REAR PRESSURE BULKHEAD WEB HAS INDICATION NOTED AT LBL 27.50, WL 130 APPROX .2" IN LENGTH 60 PERCENT FSH LOCATED AT TOP OF AFT CARGO DOOR TRACK FAILED NDT INSP. COMPLIED WITH EC/TC REO 601R-53-61-1541 AND MET ALL THE REQUIREMENTS OF REO 601R-53-61-1541 REV B.

Part: BULKHEAD WEB — CRACKED (FUSELAGE) · airframe 17,046 hrs · 14,999 cycles

FOUND REAR PRESSURE BULKHEAD WEB THAT SURROUNDS LINTEL ATTACHMENT FITTING HAS INDICATION NOTED APPROX .1" IN LENGTH 50 PERCENT FSH FAILED NDT INSP. REPAIRED PER EC/TC REO 601R-53-61-1230 AND REPAIR C/W REQUIREMENTS OF EC/TC AND REO 601R-53-61-1230 REV D.

Part: BULKHEAD WEB — CRACKED (BS 559) · airframe 17,046 hrs · 14,999 cycles

FOUND FS 559 RT BULKHEAD WEB HAS INDICATION NOTED APPROX .2" IN LENGTH 50 PERCENT FSH AT WL 59-10 INBD OF RBL 18.0, FAILED NDT INSP. REPAIRED PRESSURE BULKHEAD WEB AND CAP ANGLES7 IAW REO 601R-53-41-260, REV E.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 16,924 hrs · 14,848 cycles

RIGHT EXIT EMERGENCY EXIT INDENTIFICATION SIGN INOP. R & R NR 4 EMERGENCY LIGHT BATTERY PACK IAW AMM 33-51-04. OPS CHECK GOOD.

Part: ANCHOR FITTING — CRACKED (FUSELAGE) · airframe 16,854 hrs · 14,764 cycles

AFT ANCHOR FITTING CRACKED. C/W INSP IAW REO 601R52-11-1846 NO FUTHER CRACK PROPAGATION NOTED AT THIS TIME ACFT OK FOR SERVICE. (CLOSED]

Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,599 hrs · 14,467 cycles

RT EMERGENCY FLOOR LEVEL EXIT LIGHT INOPERATIVE. R & R RT EMERGENCY FLOOR LEVEL EXIT PANEL IAW AMM 33-51-10. OPS CHECK GOOD NO DEFECTS AT THIS TIME.

Part: LAMP — BURNED OUT (EMERGENCY LIGHTS) · airframe 16,560 hrs · 14,424 cycles

RT NR 2 EXTERIOR EMERGENCY LIGHT INOP. RELAMPED RT NR 2 EXTERIOR EMERGENCY LIGHT IAW AMM 33-51-21. OPS CHECK GOOD. RELAMPED RT NR 2 EXTERIOR EMERGENCY LIGHT IAW AMM 33-51-21 OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,538 hrs · 14,400 cycles

RIGHT FWD EMERGENCY LIGHT INOP. R & R RT FWD EMERGENCY LIGHT IAW AMM 33-51-21.

Part: DOOR — BINDING · airframe 16,476 hrs · 14,328 cycles

F/A REPORTS PASSENGER DOOR HARD TO OPEN. INSPECTED PAX DOOR AND OPS CHECKS IAW AMM 52-11-00. NO DEFECTS NOTED. OK FOR SERVICE. (CLOSED)

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 15,986 hrs · 13,746 cycles

AFT CEILING EMERGENCY FLOOD LIGHT INOP. RELAMPED AFT CEILING EMERGENCY FLOOD LIGHT LAMP IAW AMM 33-51-16. OPS CK GOOD. RELAMPED AFT CEILING EMERGENCY FLOOD LIGHT LAMP IAW AMM 33-51-16. OPS CHK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,349 hrs · 13,017 cycles

NR 2 CEILING EMERGENCY LIGHT INOP.

Part: BULKHEAD — CRACKED (BS 202) · airframe 15,077 hrs · 12,717 cycles

FOUND CRACK AT PARKING BRAKE CABLE AT FS 202.75 AT BL 23.71 PRESSURE BULKHEAD. WORK COMPLETED IAW EC/TC REO 601R 53-11-1785.

Part: SIGN — INOPERATIVE (CABIN) · airframe 14,721 hrs · 12,335 cycles

EMERGENCY EXIT SIGN AT PASSENGER BOARDING DOOR INOP.

Part: UNKNOWN — UNKNOWN (FUEL SYSTEM) · airframe 14,068 hrs · 11,706 cycles

GOT A FUEL IMBALANCE IN FLIGHT. RAN QRH GOT FUEL BALANCED AFTER EXTENDED AMOUNT OF TIME. ON LANDING STILL HAD 200 LBS ON THE HEAVY SIDE. EMERGENCY DECLARED, ENROUTE TO ATL, ACFT DIVERTED TO CHA DUE TO MTC, FLT 5474 DEL 114 MINS.

Part: WEB — CRACKED (PAX DOOR) · airframe 13,082 hrs · 10,806 cycles

PAX DOOR AFT WEB IS CRACKED IN STEP JOINT RADIUS (832DT AND 832CT) AND (832CT AND FIX MID STEP).

Part: WEB — CRACKED (PAX DOOR) · airframe 13,082 hrs · 10,806 cycles

PAX DOOR FWD WEB HAS CRACKS IN RADIUS WHERE STAIRS 832DT AND CT MEET, 832CT AND MIC FIXED STEPS MEET. REPAIRED PAX DOOR FWD WEB IAW REO 601R-52-11-702.

Part: ANGLE — CRACKED (CARGO DOOR) · airframe 13,082 hrs · 10,806 cycles

CARGO DOOR BEAM AFT BOTTOM ANGLE AT THE REAR PRESSURE BULKHEAD IS CRACKED .5 INCH LONG IN O/B RADIUS. REMOVED CRACKED BRACKET FROM CARGO DOOR BEAM/AFT BULKHEAD. LOCATED, DRILLED & INSTALLED NEW SERVICEABLE BRACKET. ALL WORK PERFORMED IAW SRM 51-42-21.

Part: FITTING — CRACKED (FUSELAGE) · airframe 13,082 hrs · 10,806 cycles

FS 280 LBL 9 I/B STRINGER CLIP CRACKED. REMOVED INBOARD STRINGER CLIP IAW SRM 51-42-21. INSTALLED NEW SERVICEABLE STRINGER CLIP IAW SRM 51-42-21.

Part: FITTING — CRACKED (FUSELAGE) · airframe 13,082 hrs · 10,806 cycles

FS 280 LBL 9 O/B CLIP CRACKED. REPLACED O/B CLIP FS 280, RBL 9 IAW CRJ 200 SRM 51-40-11 AND SRM 51-42-21.

Part: ISOLATOR — BROKEN (BULKHEAD) · airframe 13,082 hrs · 10,806 cycles

FS 621.00 REAR PRESSURE BULKHEAD FWD FACE HAS TWO ISOLATORS BROKEN. REPLACED ISOLATORS AT FS 621.00 REAR PRESSURE BULKHEAD FWD FACE IAW SRM 51-42-10.

Part: FITTING — CRACKED (FUSELAGE) · airframe 13,082 hrs · 10,806 cycles

FS 280 RBL 9 I/B CLIP CRACKED. REMOVED AND REPLACED FS 280 RBL 9 INBOARD CLIP IAW SRM 51-42-21.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 13,082 hrs · 10,806 cycles

LEFT FS 484 FLOOR SUPPORT INTERCOSTAL ANGLE CRACKED .1 INCH LONG AT LBL 27. REPLACED ANGLE AT LT FS 484 LBL 27 IAW REO 601R-53-411-059, STEPS 8-11 AND 14. COMPLIED WITH ASA EC/TC REO 601R-53-41-059.

Part: FITTING — CRACKED (FUSELAGE) · airframe 13,082 hrs · 10,806 cycles

FS 280 LBL 9 O/B CLIP CRACKED. THIS SDR WILL REMAIN OPEN PENDING MTC DETERMINATION OF AN APPROPRIATE CORRECTIVE ACTION.

Part: COVER — OUT OF POSITION (CABIN) · airframe 13,082 hrs · 10,806 cycles

EMERGENCY LIGHT COVER BY PAX DOOR FELL OFF, KNOCKED OFF DURING DEPLANING.

Part: STEP — CRACKED (ASD) · airframe 13,042 hrs · 10,773 cycles

ASD BOTTOM STEP IS CRACKED.

Part: COALESCER BAG — DIRTY (A/C BAY) · airframe 12,569 hrs · 10,333 cycles

FUEL SMELL IN FLIGHT. SUSPECT BOTH LT AND RT PACK SOCKS. SMELL MOST INTENSE WHEN INCREASE OUTFLOW TEMP TO MAINTAIN CABIN TEMP. REPLACED BOTH COALESCER SOCKS PER CRJ 200 AMM 21-51-13. OPS CHECK GOOD. (S)

Part: DCU — MALFUNCTIONED (NR 1 & 2) · airframe 12,145 hrs · 9,951 cycles

ON APP INTO ATL FUEL TOTALIZER WENT TO -0- RIGHT MFD PANEL SHOWED NO FUEL IN LEFT TANK AND THE AUTO INHIBIT INDICATOR CAME ON. RIGHT TANK READ 1920 LBS. ALL INDICATIONS RETURNED TO NORMAL ON LANDING. FLT 4801 DEL 42 MINS. REMOVED AND REPLACED DCU 1 AND DCU 2 IAW CRJ AMM 31041-04. OPS CHECK GOOD.

Part: FLAP SYSTEM — FAILED (TE FLAPS) · airframe 11,313 hrs · 9,241 cycles

FLAP FAIL AT ZERO ON APPROACH, EMERGENCY DECLARED. FLTS 4291, 4907 CX AND ON 1/22/08 FLT 4450 CX.

Part: HANDLE — CRACKED (PAX DOOR) · airframe 10,255 hrs · 8,360 cycles

PAX DOOR OUTER HANDLE CRACKED.

Part: STEP — CRACKED (PAX DOOR) · airframe 10,255 hrs · 8,360 cycles

PAX DOOR BOTTOM STEP CRACKED.

Part: FLOORBEAM — CRACKED (BS 621) · airframe 8,341 hrs · 6,946 cycles

RIGHT FS 621.00 FLOORBOARD ANGLE CRACKED AT RBL 36.00. REO REPAIR 601R-53-61-117. REPAIRED IAW ALL SRMS. (CLOSED)

Part: ANGLE — CRACKED (BS 625) · airframe 8,341 hrs · 6,946 cycles

RIGHT FS 625.00 OBLIQUE ANGLE CRACKED. REPAIRED IAW ALL SRMS. (CLOSED)

Part: ANGLE — CRACKED (BS 625) · airframe 8,341 hrs · 6,946 cycles

LEFT FS 625.00 OBLIQUE ANGLE CRACKED. REMOVED CRACKED OBLIQUE ANGLE IAW CRJ 200 SRM 51-42-06. APPLIED TOPCOAT TO SERVICEABLE OBLIQUE ANGLE P/N 601-35012-51 IAW CRJ 200 SRM 51-42-21. INSTALLED OBLIQUE ANGLE WITH LOCK FASTENERS HST10AG5-5, PO 9147-1 AND HST10AG5-2, PO 9073-1 WITH NUTS KFN587-08, PO 9147-1. (CLOSED 11/14/06)

Part: FLOORBEAM — CRACKED (BS 621) · airframe 8,341 hrs · 6,946 cycles

LEFT FS 621.00 FLOORBOARD ANGLE CRACKED AT LBL 36.00 REO REPAIR 601R-53-61-117. REMOVED FASTENERS FOR REO 601R-53-61-117 FABRICATED REPAIR PARTS IAW REO 601R-53-61-117 USING P/N 601R35031-241 FLOORBEAM ANGLE. DH752 TOUCHED UP FINISH AT CUTLINE PER CRJ SRM 51-25-16. OK TO INSTALL. WET ASSEMBLED ALL ITEMS PER SRM 51-23-00 IAW REO 601R-53-61-117. OK TO SEAL AND PAINT APPLIED SEALANT AND TOPCOAT IAW CRJ SRM 51-23-00 AND 51-25-16. (CLOSED 11/15/06)

Part: INTERCOSTAL — CRACKED (BS 484) · airframe 8,341 hrs · 6,946 cycles

FS 484 INTERCOSTAL CRACKED AT I/B SIDE OF LBL 36, RESOLVED ON W/O: 41485 TASKCARD: N/R-00045. REMOVED FS 484 LBL36 CABLE GUIDES TO FOM REPAIR DH752. CUT AWAY DAMAGED ATTACHMENT FLANGE OF PN NR 601R31171-21 LT FS 484 INTERCOSTAL AND DEBURRED PER REO 601R-53-41-059. FABRICATED ANGLE, 1 FROM .063 2024 T3 MATERIAL PO NR 8743-1. DH752 REF W/C 285 FOR LPI OF THE CUTLINE AND FABRICATED ANGLE PER REO 601R-53-41-059 DH752 RA333. OK TO TOUCH UP FINISH AO23 RA333. APPLIED FINISH AO23 IAW CRJ SRM 51-25-16. DH752 OK TO INSTALL DETAILS RA333. INSTALLED -1 ANGLE ON PN NR 601R31171-21 LT FS484 INTERCOSTAL AT LBL36 USING HST10AG6 AND KFNS87-3 HILITE FASTENERS IN LIEU OF M<S20470ADS PER REO 601R-53-41-059 IAW CRJ SRM 51-

Part: INTERCOSTAL — CRACKED (BS 484) · airframe 8,341 hrs · 6,946 cycles

FS 484 INTERCOSTAL AT I/B SIDE OF RBL36 CRACKED, (RESOLVED ON W/O: 41485 TASKCARD: N/R-00046 ). REMOVED FS 484, RBL 36 CABLE GUIDES TO FOM REPAIR (DH752 ). CUT AWAY DAMAGED ATTACHMENT FLANGE OF P/N 601R3171-15 RT FS 484 INTERCOSTALS AND DEBURRED PER REO 601R-53-41-059. ( DH 752 ) FABRICATED ANGLE -2 FROM .063 2024T3 MATERIAL PO NR 8743-1 (DH 752) REF W/C 286 FOR LPI OF CUTLINE AND FABRICATED ANGLE PER REO 601R-53-41-059 ( DH 752 ). OK TO TOUCH-UP FINISH A023 ( RA165 ), TOUCHED-UP FINISH IAW CRJ SRM 51-25-16 ( LH 302 ). OK TO INSTALL REPAIR ANGLE (RA165 ), COMPLETED INSTALLATION OF REPAIR ANGLE IAW ASA REO 601R-53-41-059 (LH302). RE-INSTALLED CABLE GUIDES PER CRJ SRM 51-42-02 (LH 302) (RII 5000524).

Part: STRINGER CLIP — CRACKED (BS 484) · airframe 8,341 hrs · 6,946 cycles

FOUND FS 484 CLIP O/B OF RBL 27 IS CRACKED. REMOVED CRACKED RT FS 484 O/B OF RBL 27 CLIP AND DUPLICATED CLIP PER CRJ SRM 53-41-43 FIGURE I ITEM 3 MATERIAL REFERENCE USING P/N S6144-3 0.050 7075T6 ANGLE. APPLIED FINISH AO23 IAW CRJ SRM 51-25-16. OK TO INSTALL. INSTALLED SERVICEABLE CLIP AT RT FS484 RBL27 O/B IAW CRJ SRM 51-23-00, 51-42-21 AND TOUCHED UP FASTENERS IAW CRJ SRM 51-25-16

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 7,617 hrs · 6,382 cycles

FOUND EMERGENCY LIGHT COVER AT ROW 8 MISSING.

Part: WIRE — OUT OF POSITION (GALLEY)

FLT 4433 - DURING CRUISE FROM ATL-EVV, THE CREW NOTICED AN ELECTRICAL BURNING SMELL IN THE COCKPIT AND THE GALLEY AREA. UPON TURNING OFF THE COFFEE MAKER AND GALLEY POWER, THE SMELL DISSIPATED. THE CREW ALSO PULLED THE GALLEY CNTL AND IND CIRCUIT BREAKER. THE FLIGHT CONTINUED WITHOUT INCIDENT WITH THE AIRCRAFT LANDING SAFELY IN EVV. MAINTENANCE FOUND A WIRE TOUCHING THE HOT SECTION OF THE COFFEE POT AND READJUSTED THE WIRE. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: FCU — MALFUNCTIONED (FLAPS)

FLT 4456 - DURING APPROACH INTO DFW FROM LBB, WHEN SELECTING THE FLAPS TO 45 DEGREES THE CREW RECEIVED A FLAPS FAIL CAUTION MESSAGE INDICATIONG A FAILURE AT 30 DEGREES. THE QRH WAS COMPLIED WITH AND EMERGENCY WAS DECLARED AS A PRECAUTION FOR EMERGENCY EQUIPMENT TO BE ON STANDBY. THE AIRCRAFT LANDED SAFELY IN DFW. MAINTENANCE REMOVED AND REPLACED THE FLAPS ELECTRONIC CONTROL UNIT. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)