N842AS

Part: SKIN — DAMAGED (BS 640-755) · airframe 34,726 hrs · 31,443 cycles

AFT SKIN AT BS 640 - 755 STR 20L-20R, FOUND CRACKED, BUCKLED, DENTED AND DEFORMED.

Part: LIGHT — DAMAGED (GALLEY) · airframe 34,500 hrs · 31,214 cycles

FLOOR LEVEL EMERGENCY FLOODLIGHT AT GALLEY DAMAGED. R & R FLOODLIGHT IAW AMM 33-51-19. SYSTEM OPS CHECKED GOOD.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 34,194 hrs · 30,925 cycles

EMERGENCY LIGHT IS INOPERATIVE, AFT INBD. FOUND TWO WIRES ON LAMP ASSY BROKEN. REPAIRED WIRES IAW 0ESPM 20-16-00. PERFORMED OPS TEST OF EMERGENCY LIGHTING IAW 0AMM 33-51-00-710-801 OPS TEST GOOD AT THIS TIME.

Part: ISOLATOR — CRACKED (BULKHEAD) · airframe 34,194 hrs · 30,925 cycles

LT LOWER SIDE OF AFT PRESSURE BULKHEAD HAS TWO BAD ISOLATORS CRACKED. INSTALLED NEW ISOLATORS IAW SRM 51-42-13.

Part: ACCESS PANEL — CRACKED (RT WING) · airframe 34,193 hrs · 30,924 cycles

CRACK DISCOVERED ON ON RT WING LOWER PLANK, T/E AT WS 119.58 REMOVED UPPER & LOWER SKIN AND LOWER ACCESS PANELS IAW SRM 57-42-06 & 51-42-10. MAJOR REPAIR.

Part: ANGLE — CRACKED (BS 261) · airframe 34,193 hrs · 30,924 cycles

RT ANGLE BRACKET AT AFT FUSELAGE S13AR, FS 261 HAS CRACK AT LOWER AFT RIVET HOLE, MARKED W/TAPE. R & R RT ANGLE BRACKET AT AFT FUSELAGE STR 15A, FS 261 IAW SRM 51-42-01.

Part: ANGLE — CRACKED (BS 261) · airframe 34,193 hrs · 30,924 cycles

LT ANGLE BRACKET AT AFT FUSELAGE S15L, FS 261 HAS CRACK AT LOWER AFT RIVET HOLE. REMOVED ANGLE BRACKET IAW SRM 51-42-06. INSTALLED ANGLE BRACKET IAW SRM 51-42-06.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 34,193 hrs · 30,924 cycles

CORROSION ON LBL 9 SEAT TRACK BS 559 - 559+80. FOUND TO BE OUT OF LIMIT IAW SRM 51-21-00. REMOVED SEAT TRACK IAW SRM 51-41-02. INSTALLED SEAT TRACK IAW AMM 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 364-409) · airframe 34,193 hrs · 30,924 cycles

CORROSION ON LBL 9, SEAT TRACK BS 364-409. FOUND TO BE OUT OF LIMITS IAW SRM 53-21-49. REMOVED CORRODED SEAT TRACK IAW SRM 53-01-11-000-802. INSTALLED NEW SEAT TRACK IAW AMM 53-01-11-400-802.

Part: FLOOR SUPPORT — CORRODED (BS 295-310) · airframe 34,193 hrs · 30,924 cycles

CORROSION ON RT FLOOR SUPPORT BETWEEN BS 295 - 310. REPAIRED FLOOR SUPPORT BETWEEN BS 280 & 409+128 IAW REO 601R-53-00-530.

Part: SEAT TRACK — CORRODED (BS 364-394) · airframe 34,193 hrs · 30,924 cycles

CORROSION ON RBL 9 SEAT TRACK BS 364 - 394, R & R SEAT TRACK IAW AMM 53-01-11-000-802 AND 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 394-409) · airframe 34,193 hrs · 30,924 cycles

CORROSION ON LBL 9, SEAT TRACK BS 394 - 409+128. FOUND TO BE OUT OF LIMITS IAW SRM 53-21-49. R & R SEAT TRACK IAW AMM 53-01-1-000-802 AND 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 394-409) · airframe 34,193 hrs · 30,924 cycles

CORROSION ON RBL 9, SEAT TRACK BS 394 - 409+128. FOUND TO BE OUT OF LIMITS IAW SRM 53-21-49. REMOVED CORRODED SEAT TRACK IAW AMM 53-01-11-000-802. INSTALLED NEW SEAT RAIL IAW AMM 53-01-11-400-802.

Part: STRUCTURE — CRACKED (PAX DOOR) · airframe 34,193 hrs · 30,924 cycles

PAX DOOR EDGE MEMBER CRACKED AT FWD LOCATION. COMPLIED WITH EC/TC REO 601R-52-11-279 IAW REO 601R-52-11-279.

Part: FRAME — CRACKED (BS 320) · airframe 34,193 hrs · 30,924 cycles

FRAME CRACKED AT BS 320.10, TOP OF DOOR. COMPLIED WITH REO 601R-52-11-402 FOR REPAIR. MAJOR REPAIR.

Part: ISOLATOR — BROKEN (BULKHEAE) · airframe 34,193 hrs · 30,924 cycles

BROKEN ISOLATER ON REAR PRESSURE BULKHEAD. R & R BROKEN ISOLATOR ON REAR PRESSURE BULKHEAD IAW SRM 51-42-13.

Part: FRAME — CORRODED (BS 338) · airframe 34,193 hrs · 30,924 cycles

FRAME CRACKED AT BS 338 TOP OF DOOR. COMPLIED WITH REO 601R-52-11-402 FOR REPAIR. MAJOR REPAIR.

Part: SEAT TRACK — CORRODED (BS 400) · airframe 34,193 hrs · 30,924 cycles

LEFT SEAT TRACK SEGMENT IS CORRODED AT BS 400. REMOVED DAMAGED SEAT TRACK IAW AMM 53-01-11-0000-802 FROM BS 364 - 409+16. INSTALLED NEW SEAT TRACK IAW AMM 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 552-559) · airframe 34,193 hrs · 30,924 cycles

LEFT SEAT TRACK SEGMENT CORRODED IN TWO SPOTS, BS 552 -559+24. FOUND OUT OF LIMITS IAW SRM 53-41-49. R & R SIDE SEAT TRACK IAW AMM 53-01-011-000/400-802 AND EC/TC REO 601R-53-00-055. COMPLIED WITH EC/TC REO 601R-53-00-055 AND REO 601R-53-00-055 REV A.

Part: SEAT TRACK — CORRODED (BS 409) · airframe 34,193 hrs · 30,924 cycles

LT SIDE SEAT TRACK SEGMENT AT FS 409.20. SEAT TRACK FOUND OUT OF LIMITS IAW SRM 53-31-49, PAGE 101. COMPLETED FABRICATION OF REPAIR SECTION INSTALLED REPAIR IAW EC/TC REO 601R-53-00-055. COMPLIED WITH EC/TC REO 601R-53-00-055 AND REO 601R-53-00-55, REV A.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 34,193 hrs · 30,924 cycles

EMERGENCY LIGHT ON RT SIDE FROM 1-6 SEATS IS INOPERATIVE. REPLACED EMERGENCY LIGHT IAW CMM 33-60-13.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 34,193 hrs · 30,924 cycles

EMERGENCY LIGHT ON FWD WARDROBE HAS A BROKEN WIRE. REPAIRED BROKEN WIRE IAW ESPM 20-17-10. PERFORMED OPS TEST OF THE EMERGENCY LIGHTING IAW AMM 33-1-00-710-801, OPS TESTED GOOD.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 33,983 hrs · 30,710 cycles

CABIN CEILING NR 3 EMERGENCY LIGHT INOPERATIVE. REPLACED LAMPS IAW AMM 33-51-16. OPS CHECKED GOOD.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 32,266 hrs · 28,930 cycles

EMERGENCY LIGHTS INOPERATIVE. CHARGED BATTERY PACKS. OPS CHECKED OK IAW AMM 33-51-00.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 30,223 hrs · 26,794 cycles

LEFT HORIZONTAL STAB ANGLE AND STRAP UNDER UPPER SURFACE OF STAB TIP FAIRING HAS LIGHTNING STRIKE DAMAGE. ON INSTALLATION OF UPPER ANGLE, FOUND A CRACKED NR 9 RIB AT UPPER FLANGE. REMOVED CRACKED RIB. REMOVED LOWER ANGLE AND CLIPS ATTACHED TO DAMAGED PART IAW SRM 51-42-06. INSTALLED REPAIRED RIB IAW SRM 51-42-06 AND 51-42-13.

Part: FLOORBEAM — CORRODED (BS 349) · airframe 30,217 hrs · 26,788 cycles

CORROSION ON FLOORBEAM AT LBL 35 ON FS 349. TREATED AND REFINISHED BLEND AREAS IAW SRM 51-21-06, STEP 3D.

Part: WEB — CORRODED (BS 409-559) · airframe 30,217 hrs · 26,788 cycles

LEFT PRESSURE FLOOR SILL PANEL AND SILL ANGLES HAVE NUMEROUS AREAS OF CORROSION BETWEEN FS 409+128 AND 559. BLENDED OUT AREAS OF CORROSION IAW REO 601R-53-41-666. PERFORMED NDT IAW REO 601R-53-41-666 STEPS 5 & 12 AND CNDTM PT 1 51-20-06. NO INDICATIONS NOTED. FINISHED, SEALED AND APPLIED CORROSION INHIBITING COMPOUND IAW REO 601R-53-41-666.

Part: FLOORBEAM — CORRODED (BS 349) · airframe 30,217 hrs · 26,788 cycles

CORROSION ON FLOORBEAM AT LBL 35 ON FS 349. REMOVED CORROSION IAW SRM 51-21-06, STEP 3D. FOUND OUT OF LIMITS IAW SRM 53-00-00, FIG 102. REPLACED IAW SRM 51-40-11 AND 51-42-06.

Part: FLOOR SUPPORT — CORRODED · airframe 30,217 hrs · 26,788 cycles

AFT LOWER FLOOR SUPPORT ANGLE IS CORRODED. R & R AFT LOWER FLOOR SUPPORT ANGLE IAW SRM 51-42-21. REPAIR CLASSIFIED AS MINOR.

Part: WEB — CORRODED (BS 409-559) · airframe 30,217 hrs · 26,788 cycles

RIGHT PRESSURE FLOOR SILL PANEL AND SILL ANGLES HAVE NUMEROUS AREAS OF CORROSION BETWEEN FS 409+128 AND 559. BLENDED CORROSION IAW REO 601R-53-41-666. FOUND OUT OF LIMITS IAW REO 601R-53-41-666, STEP 1. REPAIRED .

Part: FLOOR SUPPORT — CORRODED · airframe 30,217 hrs · 26,788 cycles

PAX DOOR THRESHOLD FLOOR SUPPORT HAS MINOR CORROSION. REMOVED AND REPLACED IAW SRM 51-42-06, 51-42-13 AND 51-42-21.

Part: FLOOR SUPPORT — CRACKED (BS 193) · airframe 30,217 hrs · 26,788 cycles

LEFT AND RIGHT FWD EQUIPMENT BAY FLOOR SUPPORT AT FS 193.00 IS CRACKED APPROX .5L. REPAIRED IAW REO 601R-53-11-245, REV B.

Part: ISOLATOR — CRACKED (BS 621 BULKHEAD) · airframe 30,217 hrs · 26,788 cycles

THREE ISOLATORS ON BS 621 BULKHEAD ARE CRACKED. R & R ISOLATORS IAW SRM 51-42-13.

Part: SUPPORT — CRACKED (BS 484) · airframe 30,217 hrs · 26,788 cycles

FS 484.00, LBL 27.00 VERTICAL SUPPORT CRACKED. R & R VERTICAL SUPPORT CLIP IAW SRM 51-42-21.

Part: GLOWSTRIP — MISSING (CABIN) · airframe 30,217 hrs · 26,788 cycles

232EZ AFT PHOTOLUMINESCENT STRIP MISSING. INSTALLED NEW PHOTOLUMINESCENT STRIP IAW AMM 11-30-00-400-801.

Part: SUPPORT BRACKET — CRACKED (WINDSHIELD) · airframe 30,217 hrs · 26,788 cycles

CO-PILOT WINDSHIELD SIDE POST AFT LOWER SUPPORT BRACKET CRACKED. R & R LOWER AFT WINDSHIELD POST BRACKET IAW SRM 51-42-20.

Part: SUPPORT BRACKET — CRACKED (WINDSHIELD) · airframe 30,217 hrs · 26,788 cycles

PILOT WINDSHIELD SIDE POST AFT LOWER SUPPORT BRACKET CRACKED. REMOVED CRACKED PILOT WINDSHIELD AFT LOWER POST BRACKET. FIT, DRILLED AND INSTALLED NEW BRACKET IAW SRM 51-42-21.

Part: FLOORBEAM — CRACKED (BS 484) · airframe 30,217 hrs · 26,788 cycles

FS 484.00, RBL 27 AND RBL 36 FLOORBEAM CRACKED. R & R IAW SRM 51-42-21.

Part: SKIN — CORRODED (BS 559) · airframe 30,217 hrs · 26,788 cycles

FUSELAGE EXTERNAL SKIN HAS AREA OF CORROSION AT STR 24R AT BS 559.00 +112. REMOVED LIGHT CORROSION IAW SRM 51-21-06.

Part: SKIN — CORRODED (BS 559) · airframe 30,217 hrs · 26,788 cycles

FUSELAGE SKIN HAS AREA OF CORROSION AT FS 559 +112 AT STR 24R. REMOVED LIGHT CORROSION IAW SRM 51-21-06.

Part: POST — CRACKED (BS 409) · airframe 30,217 hrs · 26,788 cycles

FS 409+128 VERTICAL POST BL 0 FAILS NDT WITH A CRACK INDICATION IN LT AFT RADIUS OF POST WITH AN INDICATION GREATER THAN 50 PERCENT SCREEN HEIGHT APPROX .2 LONG. REMOVED POST IAW SRM 51-42-06 & 51-42-21. LOCATED, DRILLED & SUBASSEMBLED NEW SERVICEABLE POST IAW SRM CH 51-42-06 & 51-40-11. INSTALLED NEW SERVICEABLE POST IAW SRM 51-42-06 & REO 601R-53-41-889.

Part: SKIN — CORRODED (BS 559) · airframe 30,217 hrs · 26,788 cycles

FUSELAGE SKIN CORRODED BETWEEN FS 559+80 TO FS 559+112 AT STR 23R. REMOVED LIGHT CORROSION IAW SRM 51-21-06.

Part: FLOOR PANEL — CRACKED (BS 193) · airframe 30,217 hrs · 26,788 cycles

LEFT & RIGHT FWD EQUIPMENT COMPARTMENT FLOOR STRUCTURE AT FS 193.00 IS CRACKED APPROX .5L. TRIMMED CRACKED SECTION OF FLOOR WEB IAW REO 601R-53-11-245. PERFORMED EDDY CURRENT IAW STEP 4 OF REO 601R-53-11-245. NO INDICATIONS NOTED. FABRICATED REPAIR AND INSTALLED IAW REO 601R-53-11-245.

Part: FLOOR SUPPORT — CORRODED (BS 574-621) · airframe 30,217 hrs · 26,788 cycles

CARGO FLOOR SUPPORT IS CORRODED AROUND NUTPLATE HOLES LOCATED AT LBL 27 APPROX BETWEEN FS 574.0 TO 621.0. REMOVED CARGO FLOORBEAM CAP IAW SRM 51-42-06 AND SRM 51-42-21. LOCATED NEW SERVICEABLE FLOORBEAM CAP IAW SRM 51-40-11-00. INSTALLED NEW SERVICEABLE FLOORBEAM CAP IAW SRM 51-42-31 AND REO 601R-53-61-3778, REV A.

Part: SKIN — CORRODED (BS 559) · airframe 30,217 hrs · 26,788 cycles

FUSELAGE SKIN CORRODED BETWEEN FS 559+80 TO FS 559+112 AT STR 23R. REMOVED LIGHT CORROSION IAW SRM 51-21-06.

Part: SKIN — CORRODED (BS 559) · airframe 30,217 hrs · 26,788 cycles

FUSELAGE SKIN HAS SEVERAL AREAS OF CORROSION BETWEEN FS 559+80 TO FS 559+112 BETWEEN STR 26 LT AND RT. REMOVED LIGHT CORROSION IAW SRM 51-21-06.

Part: SKIN — CORRODED (BS 559) · airframe 30,217 hrs · 26,788 cycles

FUSELAGE SKIN HAS AREA OF CORROSION AT STR 24R AT BS 559.00+112. REMOVED LIGHT CORROSION IAW SRM 51-21-06.

Part: SEAT TRACK — CORRODED (BS 409-559) · airframe 30,217 hrs · 26,788 cycles

SEAT TRACK CORRODED AT LBL 9.0 FROM 409+128 TO 559. REMOVED SEAT TRACK IAW AMM 53-01-11-000-802. INSTALLED NEW SERVICEABLE SEAT TRACK IAW SRM 51-41-02 AND AMM 53-01-11-400-802.

Part: FLOOR SUPPORT — CORRODED (PAX DOORWAY) · airframe 30,217 hrs · 26,788 cycles

PAX DOOR THRESHOLD VERTICAL FLOOR SUPPORT HAS MINOR CORROSION. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-42-06 AND 51-42-13.

Part: FLOOR SUPPORT — CORRODED (FUSLEAGE) · airframe 30,217 hrs · 26,788 cycles

LOWER FLOOR SUPPORT ANGLE CORRODED. REMOVED LWR FLOOR SUPPORT ANGLE IAW SRM 51-42-21, 51-42-10, 51-42-06 AND 51-42-34. LOCATED & DRILLED NEW FLOOR SUPPORT & INSTALLED IAW SRM 51-42-21, 51-42-10, 51-42-06 AND 51-42-34.

Part: SKIN — CORRODED (BS 559) · airframe 30,217 hrs · 26,788 cycles

FUSELAGE SKIN CORRODED AT FS 559+112 AT STR 24R. REMOVED LIGHT CORROSION IAW SRM 51-21-06.

Part: SEAT TRACK — CORRODED (BS 409-559) · airframe 30,217 hrs · 26,788 cycles

SEAT TRACK CORRODED AT RBL 9.0 FROM FS 409+128 TO 559.00. REMOVED SEAT TRACK IAW AMM 53-01-11-000-802. INSTALLED NEW SEAT TRACK IAW MM TASK 53-01-11-400-802.

Part: BPSU — OUT OF ADJUST (TE FLAPS) · airframe 29,995 hrs · 26,535 cycles

FLAPS FAILED ON RETRACTION FROM 8 TO ZERO. ACFT RETURNED AFTER TAKEOFF. EMERGENCY DECLARED. R & R LT BPSU IAW AMM 27-51-10. OPS CHECKED GOOD.

Part: CONTROLLER — FAILED (TE FLAPS) · airframe 30,135 hrs · 26,689 cycles

FLAPS FAIL AT 18 ENROUTE, ACFT DIVERTED, EMERGENCY DECLARED. R & R LT/RT BPSU AND FECU IAW AMM 27-51-10 AND 27-51-05. NO DEFECTS NOTED. OPS TEST GOOD. RII C/W IAW GMM 3-3.

Part: FLAP SYSTEM — FAILED (TE FLAPS) · airframe 29,950 hrs · 26,485 cycles

FLAPS FAILED AT 8 ON DEPARTURE, RETURNED TO DEPARTURE, LANDED 47000 LBS. EMERGENCY DECLARED. (OPEN)

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 29,457 hrs · 25,948 cycles

RT AFT OVERWING EMERGENCY LIGHT INOPERATIVE. REPLAMPED RT AFT OVERWING EMERGENCY LIGHT IAW AMM 33-51-21.

Part: PLACARD — DETERIORATED (CABIN) · airframe 28,661 hrs · 25,052 cycles

EXIT PLACARD ON PAX DOOR DAMAGED. REMOVED EXIT PLACARD IAW AMM 11-30-00.

Part: LIGHT — DAMAGED (CABIN) · airframe 28,253 hrs · 24,599 cycles

EMERGENCY EXIT LIGHT ASSY DAMAGED AT ENTRYWAY ON WARDROBE. R & R EMERGENCY EXIT LIGHT ON WARDROBE IAW AMM 33-51-19, OP'S CHECK GOOD. R & R EMERGENCY EXIT LIGHT ON WARDROBE IAW AMM 33-51-19, OP'S CHECK GOOD.

Part: SIGN — UNKNOWN (CABIN) · airframe 27,256 hrs · 23,453 cycles

REPLACED COVER EXIT SIGN OVER SERVICE DOOR, OPS OK IAW AMM 33-50-00 NEF CLEARED. (CLOSED)

Part: WARNING MESSAGE — FALSE ACTIVATION (SPOILERS) · airframe 27,213 hrs · 23,395 cycles

RECEIVED 3 AMBER MESSAGES SPOILERON FLIGHT SPOILERS, AND GRND SPOILER DEPLOY MESSAGES. (EMERGENCY DECLARED) C/W FIM 27-60-00 FOR SPOILERON, FLIGHT SPOILERS, AND GROUND SPOILER DEPLOY CAUTION MESSAGES, NO FAULTS FOUND. OPS TEST OF THE SPOILERON FLIGHT SPOILERS, AND GRND SPOILERS GOOD. ACFT OK FOR SERVICE. (CLOSED)

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 27,200 hrs · 23,379 cycles

RT NR 2 EXTERNAL EMERGENCY LIGHT INOP. RELAMPED RT NR2 EXTERNAL EMERGENCY LIGHT IAW AMM 33-51-21. OPS CHECK GOOD. RELAMPED RT NR2 EXTERNAL EMERGENCY LIGHT IAW AMM 33-51-21. OPS CHECK GOOD. (CLOSED)

Part: COMPUTER — FAILED (FUEL SYSTEM) · airframe 26,673 hrs · 22,762 cycles

ON DECENT RECEIVED FUEL CH 1/2 FAIL CAUTION MSG ON AND OFF FOR SEVERAL MINUTES THEN STAYED ON WITH DASHED LINES IN FUEL INDICATION DISPLAY, CLEARED ITSELF UPON LANDING. (EMERGENCY DECLARED AS A PRECAUTION]) R & R FUEL SYS COMPUTER IAW AMM 28-41-16 AND OPS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 26,597 hrs · 22,663 cycles

EMERGENCY LIGHT BATTERY PACK NR 3 WILL NOT HOLD A CHARGE. R & R NR 3 EMERGENCY BATTERY PACK WITH A SERVICEABLE BATTERY PACK IAW AMM 33-51-04-000-801 AND 33-51-04-400-801. OPS CHECK GOOD AT THIS TIME IAW AMM 33-51-04-740-801. SERVICEABLE PARTS TAG REQUIRED. REMOVED NR 3 BATTERY PACK INSTALLED IN STEP 1 IAW AMM 33-51-04-000-801. INSTALLED SERVICEABLE BATTERY PACK IN NR 3 POSITION IAW AMM 33-51-04-400-801, SELF TEST GOOD.

Part: POST — CRACKED (BS 409) · airframe 26,580 hrs · 22,640 cycles

FOUND FS 409.0+128 VERTICAL POST LBL 18.0 OTBD SIDE HAS INDICATION NOTED APPROX .2" IN LENGTH 60 PERCENT FSH AT WL 69 AFT FLANGE RADIUS. FAILED NDT INSPECTION. REMOVED INBD AND OTBD POST IAW SRM 51-42-06. LOCATED & DRILLED NEW VERTICAL POST IAW SRM 51-40-11. INSTALLED VERTICAL POST IAW SRM 51-42-06 & SRM 51-42-22. CORROSION INHIBITING COMPOUNDS APPLIED & FILLET SEALED AROUND VERTICAL POST IAW SRM 51-21-11 & SRM 51-23-00. COMPLIED WITH EC/TC REO 601R-53-41-889 AND MET ALL THE REQUIREMENTS OF REO 601R-53-41-889, REV A.

Part: POST — CRACKED (BS 409) · airframe 26,580 hrs · 22,640 cycles

INBD SIDE OF VERTICAL POST RBL 27 ON 409.00+128 BULKHEAD IS CRACKED AT BOTTOM RIVET APPROX .250 LONG. COMPLIED WITH EC/TC REO 601R-53-41-056 IAW REO 601R-53-41-056 REV E.

Part: FRAME — CORRODED (E/E BAY) · airframe 26,580 hrs · 22,640 cycles

AVIONICS COMPARTMENT FS 349.00 AND FS 319.70 FRAMES HAVE CORROSION. R & R FRAME AT FS 319.00 FROM STR 23L TO 23R IAW SRM 51-42-06 AND 51-42-21. REMOVED FRAME AT FS 349.00 STR 34L-23R AND LOCATED AND DRILLED NEW FRAME IAW SRM 51-40-11, 51-42-06 AND 51-42-21. PRIMED, PAINTED AND APPLIED CORROSION PREVENTITIVE IAW SRM 51-25-06, 51-25-16 AND 51-21-11. RECONNECTED GROUND WIRES IAW AMM 51-80-00-400-802. RESISTANCE CHECK GOOD. NO DEFECTS NOTED AT THIS TIME.

Part: BULKHEAD — CRACKED (BS 409) · airframe 26,580 hrs · 22,640 cycles

OTBD SIDE OF VERTICAL POST RBL 18 ON 409.00+128 BULKHEAD IS CRACKED APPROX .250 LONG AT BOTTOM RIVET. REF C.O. 7304210 JOB 8730425 OP 137.

Part: POST — CRACKED (BS 409) · airframe 26,580 hrs · 22,640 cycles

FOUND FS 409.0+128 VERTICAL POST RBL 18.0 INBD AND OTBD SIDE HAVE INDICATIONS NOTED APPROX .2" IN LENGTH 60 PERCENT AND 50 PERCENT FSH AT WL 69.0 AFT FLANGE RADIUS. FAILED NDT INSPECTION. REMOVED VERTICAL POST. LCOATED, DRILLED & JOINED POST IAW SRM 51-42-06. INSTALLED BOLTS ON INBD SIDE OF VERTICAL POST IAW REO 601R-53-41-889. INSTALLED REMAINING FASTENERS COMMON TO VERTICAL POST OTBD IAW SRM 51-42-22. FILLET SEALED AND APPLIED ANTI-CORROSION COMPOUNDS IAW SRM 51-23-00 & SRM 51-21-11. COMPLIED WITH EC/TC REO 601R-53-41-889 AND MET WITH ALL THE REQUIREMENTS OF REO 601R-53-41-889 REV A.

Part: BULKHEAD — CRACKED · airframe 26,580 hrs · 22,640 cycles

FOUND REAR PRESSURE BULKHEAD WEB HAS A INDICATION NOTED APPROX .2" IN LENGTH 50 PERCENT FSH AT LBL 27.50 WL 130. FAILED NDT INSPECTION. COMPLIED WITH EC/TC REO 601R-53-61-1541 AND MET ALL THE REQUIREMENTS OF REO 601R-53-61-1541 REV B.

Part: FRAME — CORRODED (BS 333) · airframe 26,580 hrs · 22,640 cycles

AVIONICS COMPARTMENT FS 333.00 FRAME HAS CORROSION. REMOVED CORRODED FRAME AND LT VERTICAL POST AT FS 333.00, LOCATED FASTENER HOLES IN NEW FRAME IAW SRM 51-42-06, 51-42-21 AND 51-40-11. INSTALLED FRAME AT FS 333.00 FROM STR 23L - 23R AND VERTICAL POST AT STR 23L IAW SRM 51-42-06 & 51-41-21. FRAME REQUIRES PAINT & CORROSION PREVENTITIVE. INSTALLED GROUND STUDS IAW SRM 51-41-04. BOND TEST IAW AMM 51-80-00-760-802 IS GOOD.

Part: ANGLE — CRACKED · airframe 26,580 hrs · 22,640 cycles

RT & LT 625 OBLIQUES ARE CRACKED. R & R LT/RT 625 OBLIQUES IAW SRM 51-42-21 AND 51-42-06.

Part: PLACARD — DETERIORATED (EMERGENCY EXIT) · airframe 26,580 hrs · 22,640 cycles

(CREW ESCAPE HATCH) EMERGENCY EXIT PLACARD IS DETERIORATED. APPLIED EMERGENCY EXIT SILKSCREEN ON 831 IAW MM 11-10-03-400-801.

Part: LIGHT — BROKEN (CABIN) · airframe 26,580 hrs · 22,640 cycles

LEFT EXIT LIGHT ASSY IS BROKEN. R & R LT EXIT LIGHT ASSY ON WINDSCREEN IAW MM 33-51-13-000-801 AND 33-51-13-400-801. OPS TEST DUE. OPS TEST OF THE LT WINDSCREEN EMERGENCY EXIT LIGHT IS GOOD IAW AMM 33-51-00-710-810.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,171 hrs · 22,189 cycles

RT FWD OVERWING EMERGENCY LIGHT INOP.

Part: BULB — BLOWN (EMERGENCY LIGHTS) · airframe 26,171 hrs · 22,189 cycles

R & R EMERGENCY EXIT LIGHT BULB IAW AMM 33-51-21. ITEM: 1. R & R EMERG EXIT LIGHT BULB IAW AMM 33-51-21. (CLOSED)

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 25,242 hrs · 21,225 cycles

COCKPIT EMERGENCY PUSHBUTTON LIGHT SWITCH DOES NOT FLASH WHEN PRESSED.

Part: HOSE — LEAKING (HYD SYSTEM)

HYD 1 LOW PRESS CAUTION MESSAGE IN FLIGHT. FLT 4258,4391 CX-(EMERGENCY DECLARED). REMOVED AND REPLACED HOSE ASSY NR 1 FOR RESERVOIR PRESS AND HOSE ASSY FOR AC PUMP SUCTION, OPS CHECK GOOD AT THIS TIME. WORK DONE IAW AMM 29-10-00 (SDR CLOSED). (A)

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 22,856 hrs · 19,068 cycles

EMERGENCY LIGHT PLASTIC COVER DAMAGED, MISSING FROM EMERGENCY EXIT LIGHT BY MAIN CABIN DOOR. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY PER AMM 33-53-19. (S)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 22,380 hrs · 18,649 cycles

FWD FLOORBEAM ANGLE AT FS 280 CORRODED. REMOVED CORRODED ANGLE. LOCATED & DRILLED NEW ANGLE IAW SRM 51-40-11. OK TO INSTALL. INSTALLED SERVICEABLE ANGLE IAW SRM 51-42-06.

Part: FITTING — CRACKED (FUSELAGE) · airframe 22,380 hrs · 18,649 cycles

CLIP AT FS 280 I/B OF RBL 9.0 CRACKED. REMOVED CRACKED CLIP AT FS280 IB OF RBL 9 AND FABRICATED -5 CLIP AS REF IN REO 601R-53-11-171 REV D AND INSTALLED FABRICATED CLIP AT FS 280 IB OF RBL 9 PER CRJ SRM 51-42-21

Part: RIB — CRACKED (WING) · airframe 22,380 hrs · 18,649 cycles

AAR - 1023 - LEFT BATT RIB CRACKED. REMOVED LEFT BATT RIB DOUBLER LOCATED HOLES IN NEW SERVICEABLE BATT RIB DOUBLER IAW CRJ 200 SRM 51-40-11. OK TO ALODINE AND PRIME. ALODINED AND PRIMED IAW 51-25-06. OK TO INSTALL. INSTALLED NEW SERVICEABLE BATT RIB DOUBLER IAW REO 601R-57-51-046. OK TO PAINT AND INSTALL RECEPTACLES. PAINTED AND INSTALLED RECEPTACLES. PERFORMED OP CHECKS BTMU IAW CRJ AMM 32-46-06. PROX COMPUTER IAW CRJ AMM 32-61-00. ANTI SKID COMPUTER IAW CRJ AMM 32-44-06. RETRACTION / EXTENSION OF LANDING GEAR IAW CRJ AMM 32-30-00. ALL OPS CHECKS GOOD. SUPPLEMENTAL SDR CLOSED 4/10/08.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 22,380 hrs · 18,649 cycles

AAR - 1022 - FS 280 CRACKED O/B OF LBL 9 JUST O/B OF PULLEY BRACKET. COMPLIED WITH EO 600-53-91. REPAIR OF AFT FLAP SUPPORT ANGLE AT FS 280 AND REO 601R-53-11-311. REPAIRED J-ANGLE ON THE PILOTS BULKHEAD AT FS 280.0 LEFT BL 9.0 IAW EO 600-53-0091. SUPPLEMENTAL SDR CLOSED 4/10/08.

Part: ATTACH ANGLE — CRACKED (PAX DOOR) · airframe 22,380 hrs · 18,649 cycles

AAR - 8011 - PAX DOOR UPPER TORQUE TUBE AFT COVER PLATE ATTACHMENT, 1 EACH ANGLE IS CRACKED. REMOVED CRACKED PAX DOOR UPPER TORQUE TUBE COVER AFT ATTACHMENT ANGLE AND REPLACED WITH SERVICEABLE ANGLE P/N: 601R31902-555 IAW CRJ 200 SRM 51-41-02. NF15062 03/26/08. SUPPLEMENTAL SDR CLOSED 4/3/08.

Part: DOUBLER — CRACKED (WING) · airframe 22,380 hrs · 18,649 cycles

AAR - 7006 - RIGHT BATT RIB CRACKED. UPON FURTHER EVALUATION, FOUND RIGHT BATT RIB PREVIOUS REPAIR DOUBLER TO BE CRACKED. REMOVED CRACKED REPAIR DOUBLER FROM RIGHT BATT RIB & DUPLICATED SERVICEABLE REPAIR DOUBLER FROM P/N S6144-4 .063 IAW REO 601R-57-51-046. INSTALLED SERVICEABLE REPAIR DOUBLER IAW REO 601R-57-51-046. SUPPLEMENTAL SDR CLOSED 4/3/08.

Part: FITTING — CRACKED (FUSELAGE) · airframe 22,380 hrs · 18,649 cycles

CLIP AT FS 280 O/B LBL 9 CRACKED. REMOVED CRACKED CLIP AT FS 280 O/B OF LBL 9 AND FABRICATED -2 CLIP AS REF IN REO 601R-53-11-171 REV D AND INSTALLED FABRICATED CLIP AT FS 280 O/B OF LBL PER CRJ SRM 51-42-21.

Part: FITTING — CRACKED (FUSELAGE) · airframe 22,380 hrs · 18,649 cycles

CLIP AT FS 484 RBL 27 CRACKED. REMOVED DAMAGED CLIP, DUPLICATED SERVICEABLE CLIP AS SHOWN IN REO 601R-53-41-059. INSTALLED NEW CLIP IAW SRM 51-42-21.

Part: FITTING — CRACKED (FUSELAGE) · airframe 22,380 hrs · 18,649 cycles

AAR - INTERCOSTAL CLIP CRACKED AT FS 484 LBL 36. REMOVED AND REPLACED CRACKED CLIP FS 484 LBL36 IAW REO 601R-53-41-059.

Part: FITTING — CRACKED (FUSELAGE) · airframe 22,380 hrs · 18,649 cycles

FITTING AT FS 484 RBL 9 CRACKED. REMOVED DAMAGED FITTING. DUPLICATED SERVICEABLE FITTING AS SHOWN IN REO 601R-53-41-059. INSTALLED NEW SERVICEABLE FITTING IAW SRM 51-42-21.

Part: FITTING — CRACKED (FUSELAGE) · airframe 22,380 hrs · 18,649 cycles

CLIP AT FS 280 O/B RBL 9 CRACKED. REMOVED CRACKED CLIP AT FS280 OB OF RBL 9. FABRICATED -5 CLIP AS REF IN REO 601R-53-11-171 REV D AND INSTALLED FABRICATED CLIP AT FS280 OB OF RBL9 PER CRJ SRM 51-42-21.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 22,380 hrs · 18,649 cycles

AAR - BRACKET AT FS 484 LBL 36 CRACKED. REMOVED BRACKET AT FS 484 LBL 36, FABRICATED AND INSTALLED IN ACCORDANCE WITH EC/TC REO 601R-53-41-059. DR 15098. SUPPLEMENTAL SDR CLOSED 4/1/08.

Part: STRUCTURE — CRACKED (PAX DOOR) · airframe 22,380 hrs · 18,649 cycles

AAR - PAX DOOR AFT EDGE MEMBER CRACKED UNDER STEP 832ET. REPAIRED PAX DOOR AFT EDGE MEMBER CRACK UNDER STEP 832ET IAW REO 601R-52-11-279. NDF 15062. COMPLIED WITH EC/TC EO600-52-43 C/W. VS 13330 03/26/08. SUPPLEMENTAL SDR CLOSED 4/1/08.

Part: FITTING — CRACKED (FUSELAGE) · airframe 22,380 hrs · 18,649 cycles

AAR - INTERCOSTAL CLIP CRACKED AT FS 484 LBL 28. REMOVED AND REPLACED CRACKED CLIP FS 484 LBL36 IAW REO 601R-53-41-059.

Part: FITTING — CRACKED (FUSELAGE) · airframe 22,380 hrs · 18,649 cycles

CLIP AT FS 484 LBL 27 CRACKED. REMOVED DAMAGED CLIP, DUPLICATED SERVICEABLE CLIP AS SHOWN IN REO 601R-53-41-059. INSTALLED NEW CLIP IAW SRM 51-42-21

Part: FITTING — CRACKED (FUSELAGE) · airframe 22,380 hrs · 18,649 cycles

AAR - BATH TUB FITTING AT RBL 9 CRACKED. REMOVED UNSERVICEABLE BATHTUB FITTING AT RBL 9. LOCATED HOLES IN NEW SERVICEABLE BATHTUB FITTING IAW CRJ 200 SRM 51-40-11. OK TO INSTALL. INSTALLED NEW BATHTUB FITTING IAW 51-42-21, DR 15098. SERVICEABLE FITTING P/N 600-31068-19, RB 13335. SUPPLEMENTAL SDR CLOSED 3/28/08.

Part: DRAG ANGLE — CRACKED (FUSELAGE) · airframe 22,380 hrs · 18,649 cycles

RT BATTERY RIB DRAG ANGLE CRACKED IN GEAR BAY. REMOVED CRACKED DRAG ANGLE AND LOCATED FASTNER HOLES IN SERVICEABLE DRAG ANGLE IAW SRM 51-40-11.

Part: DRAG ANGLE — CRACKED (FUSELAGE) · airframe 22,380 hrs · 18,649 cycles

LT BATTERY RIB DRAG ANGLE CRACKED IN GEAR BAY. REMOVED UNSERVICEABLE RIB DRAG ANGLE. LOCATED HOLES IN NEW SERVICEABLE DRAG ANGLE IAW SRM 51-40-11. OK TO INSTALL. INSTALLED NEW DRAG ANGLE IAW SRM 51-42-21. OK TO TOPCOAT. TOPCOATED IAW SRM 51-26-16.

Part: LIGHT — FAILED (PAX DOOR) · airframe 22,380 hrs · 18,649 cycles

PASSENGER DOOR HANDLE LEVER, "EXIT/PULL" BETA LIGHT FAILED FUNCTIONAL TEST. REMOVED DOOR HANDLE LEVER LIGHT AND REPLACED WITH SERVICEABLE LIGHT P/N 1961002 IAW SRM 51-41-02. PASSED FUNCTIONAL TEST IAW AMM 33-51-09-720-801.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 22,380 hrs · 18,649 cycles

RIGHT UPPER ANGLE CRACKED ON ENGINE BEAM AT RBL 45 WL 119.12. REMOVED CRACKED RT UPPER ANGLE ON ENGINE BEAM. LOCATED NEW SERVICEABLE ANGLE PN 601-35006-62 IAW SRM 51-40-11. OK TO INSTALL INSTALLED ANGLE IAW SRM 51-42-21. OK TO TOPCOAT FASTENERS. APPLIED FINISH TO FASTNERS IAW SRM 51-21-16.

Part: DOOR — MALFUNCTIONED · airframe 21,696 hrs · 18,049 cycles

SERVICE DOOR WILL NOT OPEN FROM OUTSIDE.

Part: PLACARD — TORN (PAX DOOR) · airframe 21,562 hrs · 17,949 cycles

EXIT PLACARD ON PAX DOOR TORN AND NOT SECURE.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 21,501 hrs · 17,902 cycles

F/O'S FLASHLIGHT INOP.

Part: SIGN — WORN (PAX DOOR) · airframe 20,512 hrs · 17,104 cycles

EXIT ARROW AT PAX DOOR ENTRANCE WORN.

Part: ELT — NO TEST (CABIN) · airframe 20,172 hrs · 16,837 cycles

ELT DOES NOT TEST.

Part: BRACKET — CRACKED (CARGO DOOR) · airframe 20,077 hrs · 16,764 cycles

CARGO DOOR STRUCTURE AFT ANGLE BRACKET IS CRACKED.

Part: BULKHEAD — CRACKED (BS 621) · airframe 20,113 hrs · 16,792 cycles

AFT PRESSURE BULKHEAD FS 621 IS CRACKED AT LINTEL ATTACHMENT FITTING.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 19,960 hrs · 16,686 cycles

FOUND POSSIBLE CRACK ON RT 640 FRAME DOUBLER NEEDS NDT.

Part: LIGHT — INOPERATIVE (FUSE EXTERIOR) · airframe 19,232 hrs · 16,156 cycles

LEFT FUSELAGE 1 EACH EXTERIOR EMERGENGY LIGHT INOP.

Part: HYDRAULIC SYSTEM — LOW PRESSURE (NR 1) · airframe 18,033 hrs · 15,267 cycles

NR 1 HYD LOW PRESS, FLT 4377 CX & FLT 4641 CX AS A C/O. AN EMERGENCY WAS DECLARED, ENROUTE TO IAD-ATL, FLIGHT DIVERTED TO GSO.

Part: OXYGEN MASK — MALFUNCTIONED (CABIN) · airframe 17,997 hrs · 15,234 cycles

OBSERVERS OXYGEN MASK DOES NOT TEST CORRECTLY, FLT 4522 DEL 20 MINS.

Part: LIGHT — INOPERATIVE (FUSELAGE) · airframe 17,941 hrs · 15,182 cycles

REF DML NR 023796. RT WING EXT OVERWING FWD EMERGENCY LIGHT INOP. A/C SWAP TO 830, FLT 4323 DEL 46 MINS.

Part: POWER SUPPLY — INOPERATIVE (ZONE 200) · airframe 17,925 hrs · 15,164 cycles

RT WING FWD EMERGENCY EXIT LIGHT INOP. BATTERY CHARGER AT ROW 9CD CEILING IS INOP, FLT 4247 DEL 44 MINS.

Part: LIGHT — INOPERATIVE (FUSELAGE) · airframe 17,922 hrs · 15,160 cycles

FOUND RT WING EXT OVERWING FWD EMERGENCY LIGHT INOP. REMOVED AND REPLACED BATTERY PACK AND CHARGER PS2LF IAW CRJ 200 AMM. DEFFERAL CLEARED, PLACARD REMOVED. A/C OK FOR SERVICE. (CLOSED)

Part: PLATE — CORRODED (BS 310-349) · airframe 17,844 hrs · 15,102 cycles

FOUND CORROSION ON HORIZ PLATE FS310 TO 349, UNDER PAX DOOR HINGE BL45 LT. REPAIRED CORROSION ON HORIZONTAL PLATE AT FS 310-349 IAW REO600-53-0341 (CLOSED)

Part: BULKHEAD — CRACKED (BS 280) · airframe 17,844 hrs · 15,102 cycles

FOUND 280 WEB IS CRACKED O/B OF LBL9. REPAIRED PILOTS BULKHEAD AT FS 280 LBL 9.0 IAW EO 600-53-0090.

Part: PRESSURE PANEL — CORRODED (FUSELAGE) · airframe 17,844 hrs · 15,102 cycles

LT FS 536 PRESSURE DECK CORRODED AT NUTPLATE (RESOLVED ON W/O: 22159 TASKCARD: N/R-00247. BLENDED CORROSION ON PRESSURE DECK IAW CRJ 200 SRM 51-41-45 REQUEST THICKNESS CHECK OF BLENDED AREA. C/W THICKNESS CHECK AT BLENDED AREA IAW CRJ 200 NDT MANUAL 51-20-04 PART 1, MINIMUM THICKNESS IS .050" C/W EDDY CURRENT INSPECTION OF REWORKED AREA PER REO601R-53-41-412 IAW CRJ 200 NDTM 51-20-06. NO DEFECTS NOTED. FASTENERS BLENDED ARE INSIDE THE ACCEPTED LIMITS ALSO RESTORED THE FINISH PER REO 601R-53-41-412 SM 7023171RII REQUIREMENTS SATISFACTORY PER SP607. COMPLIED WITH EC/TC REO 601R-53-41-412 .

Part: DOUBLER — CORRODED (BS 544) · airframe 17,844 hrs · 15,102 cycles

FOUND LT FS 544 DOUBLER CORRODED AT BL42-44 (RESOLVED ON W/O: 22159 TASKCARD: N/R-00248 ). BLENDED CORROSION ON FS 544 DOUBLER AT BL42-44 IAW CRJ 200 SRM 51-41-45 REQUEST THICKNESS CHECK OF BLENDED AREA DK 7022603 COMPLIED WITH THICKNESS CHECK AT BLENDED AREA IAW CRJ 200 NDT MANUAL 51-20-04 PART 1, MINIMUM THICKNESS IS .079". C/W EDDY CURRENT INSPECTON OF REWORKED AREA PER REO601R-53-41-412 IAW CRJ 200 NDTM 51-20-06. NO DEFECTS NOTED. FASTENERS BLENDED ARE INSIDE THE ACCEPTED LIMIITS ALSO RESTORED THE FINISH PER REO 601R-53-41-412 SM 7023171. RII REQUIREMENTS SATISFACTORY PER SP607. COMPLIED WITH EC/TC REO 601R-53-41-412.

Part: DOUBLER — CORRODED (BS 544) · airframe 17,844 hrs · 15,102 cycles

FOUND CORROSION ON DOUBLER AT FS 544 - BL42-44RT.

Part: SEAT TRACK — CORRODED (BS 364-394) · airframe 17,844 hrs · 15,102 cycles

FOUND CORROSION ON FLOOR SEAT TRACK -SEC 1, FS 364 TO 394 -BL9LT.

Part: DOUBLER — CORRODED (BS 439) · airframe 17,844 hrs · 15,102 cycles

FOUND CORROSION ON DOUBLER AT FS 439=BL42-44RT, RESOLVED ON W/O: 22159 TASKCARD: N/R-00216. BLENDED CORRODED AREA IAW CRJ 200 SRM 51-41-45 REQUEST THICKNESS CHECK OF BLENDED AREA DK 7022603 ALSO BLENDED OUTSIDE OF DOUBLER AREA REQUIRES THICKNESS CHECK. C/W THICKNESS CHECK AT BLENDED AREA IAW CRJ 200 NDT MANUAL 51-20-04 PART 1, MINIMUM THICKNESS IS .079".C/W EDDY CURRENT INSPECTION OF REWORKED AREA PER REO601R-53-41-413 IAW CRJ 200 NDTM 51-20-06. NO DEFECTS NOTED.FASTENERS BLENDED ARE INSIDE THE ACCEPTED LIMITS ALSO RESTORED THE FINISH PER REO 601R-53-41-412 SM 7023171RII REQUIREMENTS SATISFACTORY PER SP607 COMPLIED WITH EC/TC REO 601R-53-41-412.

Part: UNKNOWN — CORRODED (BS 558) · airframe 17,844 hrs · 15,102 cycles

FOUND CORROSION AROUND N/P AT FS558 - BL39RT, RESOLVED ON W/O: 22159 TASKCARD: N/R-00207. C/W CORROSION AROUND N/P IAW E/C REO 601R-53-41-413.

Part: DOUBLER — CORRODED (BS 499-513) · airframe 17,844 hrs · 15,102 cycles

FOUND CORROSION ON DOUBLER AT FS 499-513 - BL44-41RT. REPAIRED CORROSION ON DOUBLER IAW T/C REO 601R-53-41-413.

Part: UNKNOWN — CORRODED (BS 451) · airframe 17,844 hrs · 15,102 cycles

FOUND CORROSION AROUND N/P AT FS 451- BL44-42RT, RESOLVED ON W/O: 22159 TASKCARD: N/R-00191. C/W CORROSION AROUND N/P IAW E/C REO 601R-53-41-413.

Part: DOUBLER — CORRODED (BS 455) · airframe 17,844 hrs · 15,102 cycles

FOUND CORROSION ON DOUBLER AT FS 455 - BL44LT.

Part: STRUCTURE — CORRODED (BS 486) · airframe 17,844 hrs · 15,102 cycles

FOUND CORROSION AROUND NUTPLATE AT FS486 - BL43. C/W CORROSION AROUND NUTPLATE IAW E/C REO 601R-53-41-413.

Part: DOUBLER — CORRODED (BS 540) · airframe 17,844 hrs · 15,102 cycles

FOUND CORROSION ON DOUBLER, FS 540 - BL44-41RT. REPAIRED CORROSION ON DOUBLER IAW T/C REO 601R-53-41-413

Part: DOUBLER — CORRODED (BS 509-513) · airframe 17,844 hrs · 15,102 cycles

FOUND CORROSION ON DOUBLER AT FS 509-513 - BL44-37RT. REPAIRED CORROSION ON DOUBLER IAW T/C REO 601R-53-41-413.

Part: DOUBLER — CORRODED (BS 448-451) · airframe 17,844 hrs · 15,102 cycles

FOUND CORROSION ON PRESS DECK DOUBLER AT FS 448-451 - BL44-42RT (RESOLVED ON W/O: 22159 TASKCARD: N/R-00190). C/W CORROSION ON PRESSURE DECK IAW E/C REO 601R-53-41-413.

Part: UNKNOWN — CORRODED (BS 478) · airframe 17,844 hrs · 15,102 cycles

FOUND CORROSION AROUND N/P AT FS478 - BL43LT, RESOLVED ON W/O: 22159 TASKCARD: N/R-00224. BLENDED CORRODED AREA OF PRESSURE DECK AROUND NUT PLATE FS 478 - BL43LT IAW CRJ 200 SRM 51-41-45 REQUEST THICKNESS CHECK OF BLENDED AREA DK 7022603. C/W THICKNESS CHECK AT BLENDED AREA IAW CRJ 200 NDT MANUAL 51-20-04 PART 1, MINIMUM THICKNESS IS .052". C/W EDDY CURRENT INSPECTION OF REWORKED AREA PER REO601R-53-41-412 IAW CRJ 200 NDTM 51-20-06. NO DEFECTS NOTED. FASTENERS BLENDED ARE INSIDE THE ACCEPTED LIMITS ALSO REPAINTED THE SURFACES PER REO601R-53-41-412 BAT23167. RII C/W SATISFACTORY COMPLIED WITH EC/TC REO 601R-53-41-412.

Part: DOUBLER — CORRODED (BS 473-479) · airframe 17,844 hrs · 15,102 cycles

FOUND CORROSION ON DOUBLER AT FS 473-479 - BL44 RT TO 37 RT, RESOLVED ON W/O: 22159 TASKCARD: N/R-00197. REPAIRED CORROSION ON DOUBLER IAW T/C REO 601R-53-41-413.

Part: DOUBLER — CORRODED (BS 540) · airframe 17,844 hrs · 15,102 cycles

FOUND CORROSION ON DOUBLER AT FS 540 - BL44, 42RT.

Part: DOUBLER — CORRODED (BS 461) · airframe 17,844 hrs · 15,102 cycles

FOUND CORROSION ON P/D DOUBLER AT FS461- BL44-41RT, (RESOLVED ON W/O: 22159 TASKCARD: N/R-00193 ). REPAIRED CORROSION ON DOUBLER IAW T/C REO 601R-53-41-413.

Part: SEAT TRACK — CORRODED (BS 394-409) · airframe 17,844 hrs · 15,102 cycles

FOUND CORROSION ON FLOOR SEAT TRACK - SEC 2- FS 394 TO 409+128 - BL9RT.

Part: PRESSURE PANEL — CORRODED (BS 455) · airframe 17,844 hrs · 15,102 cycles

FOUND CORROSION ON PRESS DECK AT FS455 - BL44 LT, (RESOLVED ON W/O: 22159 TASKCARD: N/R-00219). BLENDED CORRODED AREA IAW CRJ 200 SRM 51-41-45 REQUEST THICKNESS CHECK OF BLENDED AREA DK 7022603. C/W THICKNESS CHECK AT BLENDED AREA IAW CRJ 200 NDT MANUAL 51-20-04 PART 1, MINIMUM THICKNESS IS .051". C/W EDDY CURRENT INSPECTON OF REWORKED AREA PER REO601R-53-41-412 IAW CRJ 200 NDTM 51-20-06. NO DEFECTS NOTED. FASTENERS BLENDED ARE INSIDE THE ACCEPTED LIMITS ALSO REPAINTED THE SURFACES PER REO601R-53-41-412 BAT23167RII REQUIREMENTS SATISFACTORY PER SP607. COMPLIED WITH EC/TC REO 601R-53-41-412.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 17,844 hrs · 15,102 cycles

FOUND CORROSION ON FLOOR SEAT TRACK SEC 4 - FS559 TO 559+86 - BL9L, RESOLVED ON W/O: 22159 TASKCARD: N/R-00232. BLENDED ALL CORROSION ON PAX SEAT TRACK 559-559+86 LBL9 AS REQUIRED IAW CRJ 200 SRM 53-41-49 AND 53-00-00 AS REQUIRED. ALL REMOVED DAMAGE IS WITHIN LIMITS, SM 17032 JOB COMPLETE.

Part: UNKNOWN — CORRODED (BS 462) · airframe 17,844 hrs · 15,102 cycles

FOUND CORROSION AROUND N/P AT FS462 - BL43RT, RESOLVED ON W/O: 22159 TASKCARD: N/R-00192. C/W CORROSION AROUND N/P IAW E/C REO 601R-53-41-413.

Part: UNKNOWN — CORRODED (BS 508) · airframe 17,844 hrs · 15,102 cycles

FOUND CORROSION AROUND N/P FS508 - BL43RT, RESOLVED ON W/O: 22159 TASKCARD: N/R-00202. C/W CORROSION AROUND N/P IAW E/C REO 601R-53-41-413.

Part: SEAT TRACK — CORRODED (BS 364-394) · airframe 17,844 hrs · 15,102 cycles

FOUND CORROSION ON FLOOR SEAT TRACK - SEC1 - FS364 TO 394 - BL9RT.

Part: DOUBLER — CORRODED (BS 498-513) · airframe 17,844 hrs · 15,102 cycles

CORROSION ON DOUBLER AT FS 498-513 - BL42-44LT (RESOLVED ON W/O: 22159 TASKCARD: N/R-00226 ). BLENDED CORRODED AREA ON DOUBLER AT FS 498-513-BL42-44LT IAW CRJ 200 SRM 51-41-45 REQUEST THICKNESS CHECK OF BLENDED AREA ALSO AROUND 491.5 OF PRESSURE DECK DK 7022603. C/W THICKNESS CHECK AT BLENDED AREA IAW CRJ 200 NDT MANUAL 51-20-04 PART 1, MINIMUM THICKNESS IS .077". C/W EDDY CURRENT INSPECTION OF REWORKED AREA PER REO601R-53-41-412 IAW CRJ 200 NDTM 51-20-06. NO DEFECTS NOTED. REMOVED AND REPLACED ONE FASTENER ALL OTHERS WITHIN LIMITS REPAINTED SURFACE PER REO 601R-53-41-412 AND CRJ 200 SRM 51-42-06 BAT23167. RII REQUIREMENTS SATISFACTORY PER SP607. COMPLIED WITH EC/TC REO 601R-53-41-412.(SUPPLEMENTAL SDR 4

Part: DOUBLER — CORRODED (BS 469-473) · airframe 17,844 hrs · 15,102 cycles

FOUND CORROSION ON DOUBLER AT FS 469-473 - BL42RT. REPAIRED CORROSION ON DOUBLER IAW T/C REO 601R-53-41-413.

Part: CARGO TRACK — CORRODED (FUSELAGE) · airframe 17,844 hrs · 15,102 cycles

ALL CARGO FLOOR TRACKS CORRODED.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 17,844 hrs · 15,102 cycles

FOUND CORROSION ON DOUBLER, FS 544 - 44-41RT. REPAIRED CORROSION ON DOUBLER IAW T/C REO 601R-53-41-413.

Part: PRESSURE PANEL — CORRODED (BS 439) · airframe 17,844 hrs · 15,102 cycles

FOUND CORROSIOIN ON PRESS DECK DOUBLER AT FS 439 - BL44-42RT (RESOLVED ON W/O: 22159 TASKCARD: N/R-00189). COMPLIED WITH CORROSION ON PRESSURE DECK IAW E/C REO 601R-53-41-413.

Part: PRESSURE PANEL — CORRODED (BS 493) · airframe 17,844 hrs · 15,102 cycles

FOUND CORROSION ON PRESS DECK AT FS493 - BL44RT. COMPLIED WITH CORROSION ON PRESSURE DECK IAW E/C REO 601R-53-41-413.

Part: UNKNOWN — CORRODED (BS 485) · airframe 17,844 hrs · 15,102 cycles

FOUND CORROSION AROUND N/P 485 - BL43LT, RESOLVED ON W/O: 22159 TASKCARD: N/R-00225. BLENDED CORRODED AREA AROUND NUT PLATE ON PRESSURE DECK FS 485-BL 43LT IAW CRJ 200 SRM 51-41-45 REQUEST THICKNESS CHECK OF BLENDED AREA DK 7022603. C/W THICKNESS CHECK AT BLENDED AREA IAW CRJ 200 NDT MANUAL 51-20-04 PART 1, MINIMUM THICKNESS IS .053". C/W EDDY CURRENT INSPECTION OF REWORKED AREA PER REO601R-53-41-412 IAW CRJ 200 NDTM 51-20-06. NO DEFECTS NOTED. FASTENERS BLENDED ARE INSIDE THE ACCEPTED LIMITS ALSO REPAINTED THE SURFACES PER REO601R-53-41-412 BAT23167RII REQUIREMENTS SATISFACTORY PER SP607 COMPLIED WITH EC/TC REO 601R-53-41-412.

Part: DOUBLER — CORRODED (BS 555-558) · airframe 17,844 hrs · 15,102 cycles

FOUND CORROSIOIN ON DOUBLER AT FS 555-558, BL44-42 RT.

Part: STRUCTURE — CORRODED (BS 468) · airframe 17,844 hrs · 15,102 cycles

FOUND CORROSION AROUND N/P AT FS 468 - BL43RT, RESOLVED ON W/O: 22159 TASKCARD: N/R-00195. C/W CORROSION AROUND N/P IAW E/C REO 601R-53-41-413.

Part: UNKNOWN — CORRODED (BS 468) · airframe 17,844 hrs · 15,102 cycles

FOUND CORROSION AROUND N/P AT FS468 - BL43LT, RESOLVED ON W/O: 22159 TASKCARD: N/R-00220. BLENDED CORRODED AREA IAW CRJ 200 SRM 51-41-45 REQUEST THICKNESS CHECK OF BLENDED AREA DK 7022603. C/W THICKNESS CHECK AT BLENDED AREA IAW CRJ 200 NDT MANUAL 51-20-04 PART 1, MINIMUM THICKNESS IS .051". C/W EDDY CURRENT INSPECTION OF REWORKED AREA PER REO601R-53-41-412 IAW CRJ 200 NDTM 51-20-06. NO DEFECTS NOTED. FASTENERS BLENDED ARE INSIDE THE ACCEPTED LIMITS ALSO REPAINTED THE SURFACES PER REO601R-53-41-412 SM 7023171. RII REQUIREMENTS SATISFACTORY PER SP607. COMPLIED WITH EC/TC REO 601R-53-41-412.

Part: DOUBLER — CORRODED (BS 522-529) · airframe 17,844 hrs · 15,102 cycles

FOUND CORROSION ON DOUBLER, FS 522 - 529, BL44-41RT, RESOLVED ON W/O: 22159 TASKCARD: N/R-00203. REPAIRED CORROSION ON DOUBLER IAW T/C REO 601R-53-41-413.

Part: FLOOR SUPPORT — CORRODED (BS 621-559) · airframe 17,844 hrs · 15,102 cycles

FOUND CORROSION ON FLOOR ATTACH ANGLE, FS621 TO 559+60. COMPLIED WITH CORROSION ON FLOOR IAW REO 601R-53-00-161.

Part: DOUBLER — CORRODED (BS 484) · airframe 17,844 hrs · 15,102 cycles

FOUND CORROSION ON DOUBLER AT FS 484 - BL44-41RT. REPAIRED CORROSION ON DOUBLER IAW T/C REO 601R-53-41-413

Part: DOUBLER — CORRODED (BS 555-558) · airframe 17,844 hrs · 15,102 cycles

FOUND CORROSION ON DOUBLER FS 555 TO 558- BL44-41RT. REPAIRED CORROSION ON DOUBLER IAW T/C REO 601R-53-41-413.

Part: DOUBLER — CORRODED (BS 422-427) · airframe 17,844 hrs · 15,102 cycles

FOUND CORROSION ON DOUBLER AT FS 422-427 - BL44-37 LT, (RESOLVED ON W/O: 22159 TASKCARD: N/R-00215). BLENDED CORROSION ON DOUBLER IAW 53-41-45 REQUEST THICKNESS CHECK OF BLENDED AREA SM18595. COMPLIED WITH UT THICKNESS CHECK OF BLENDED AREA IAW CRJ NDTM 51-20-04 FOUND MIN THICKNESS TO BE .055"C/W EDDY CURRENT INSPECTION OF REWORKED AREA PER REO601R-53-41-412 IAW CRJ 200 NDTM 51-20-06. NO DEFECTS NOTED. FASTENERS BLENDED ARE INSIDE THE ACCEPTED LIMITS ALSO RESTORED THE FINISH PER REO 601R-53-41-412 BAT23167RII REQUIREMENTS SATISFACTORY PER SP607. COMPLIED WITH EC/TC REO 601R-53-41-412.

Part: FLOOR SUPPORT — CORRODED (BS 300-312) · airframe 17,844 hrs · 15,102 cycles

CORROSION ON FLOOR ATTACH ANGLE AT FS300-312 - BL45RT, RESOLVED ON W/O: 22159 TASKCARD: N/R-00210. REMOVED FITTINGS AROUND CORROSION AT FS 300 FOM REMOVED CORROSION AT FS 300 AND 312 IAW CRJ 200 SRM 53-12-00. BLEND WAS FOUND TO BE WITHIN LIMITS, APPLIED ALODINE PRIME AND PAINT. REINSTALLED FITTING AT FS 300 IAW CRJ 200 SRM 51-42-00 DB 20877.

Part: DOUBLER — CORRODED (BS 522-529) · airframe 17,844 hrs · 15,102 cycles

FOUND CORROSION ON DOUBLER AT FS 522-529-BL41-44LT, RESOLVED ON W/O: 22159 TASKCARD: N/R-00228. BLENDED CORRODED AREA OF DOUBLER AT FS 522-529-BL41-44LT IAW CRJ 200 SRM 51-41-45 REQUEST THICKNESS CHECK OF BLENDED AREA DK 7022603. C/W THICKNESS CHECK AT BLENDED AREA IAW CRJ 200 NDT MANUAL 51-20-04 PART 1, MINIMUM THICKNESS IS .079". C/W EDDY CURRENT INSPECTION OF REWORKED AREA PER REO601R-53-41-412 IAW CRJ 200 NDTM 51-20-06. NO DEFECTS NOTED. FASTENERS BLENDED ARE INSIDE THE ACCEPTED LIMITS ALSO REPAINTED THE SURFACES PER REO601R-53-41-412 BAT23167 RII REQUIREMENTS SATISFACTORY PER SP607. COMPLIED WITH EC/TC REO 601R-53-41-412.

Part: DOUBLER — CORRODED (BS 460-462) · airframe 17,844 hrs · 15,102 cycles

FOUND CORROSION ON DOUBLER AT FS 460-462- BL42-44LT, RESOLVED ON W/O: 22159 TASKCARD: N/R-00218. BLENDED CORROSION AREA ALONG WITH NUT PLATE AT FS 460 BL42-44LT IAW CRY 200 SRM 53-41-45 REQUEST THICKNESS CHECK OF WORKED AREA DK 7022603. C/W THICKNESS CHECK AT BLENDED AREA IAW CRJ 200 NDT MANUAL 51-20-04 PART 1, MINIMUM THICKNESS IS .080". C/W EDDY CURRENT INSPECTION OF REWORKED AREA PER REO601R-53-41-412 IAW CRJ 200 NDTM 51-20-06. NO DEFECTS NOTED. FASTENERS BLENDED ARE INSIDE THE ACCEPTED LIMITS ALSO REPAINTED THE SURFACES PER REO601R-53-41-412 BAT23167. RII REQUIREMENTS SATISFACTORY PER SP607. COMPLIED WITH EC/TC REO 601R-53-41-412.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 17,844 hrs · 15,102 cycles

FOUND CORROSION ON FLOOR SEAT TRACK - SEC 4 - FS559 TO 559+86 - BL9RT.

Part: DOUBLER — CORRODED (BS 484) · airframe 17,844 hrs · 15,102 cycles

FOUND CORROSION ON DOUBLER AT FS 484-BL41-44LT (RESOLVED ON W/O: 22159 TASKCARD: N/R-00223 ). BLENDED CORRODED AREA OF DOUBLER AT FS 484 BL41-44LT IAW CRJ 200 SRM 51-41-45 REQUEST THICKNESS CHECK OF BLENDED AREA DK 7022603 C/W THICKNESS CHECK AT BLENDED AREA IAW CRJ 200 NDT MANUAL 51-20-04 PART 1, MINIMUM THICKNESS IS .078". C/W EDDY CURRENT INSPECTON OF REWORKED AREA PER REO601R-53-41-412 IAW CRJ 200 NDTM 51-20-06. NO DEFECTS NOTED. FASTENERS BLENEDED ARE INSIDE THE ACCECPTED LIMITS ALSO REPAINTED THE SURFACES PER REO601R-53-41-412 SM 7023171. RII REQUIREMENTS SATISFACTORY PER SP607. COMPLIED WITH EC/TC REO 601R-53-41-412.

Part: DOUBLER — CORRODED (BS 469-473) · airframe 17,844 hrs · 15,102 cycles

FOUND CORROSION ON DOUBLER AT FS 469-473 - BL37-44 LT (RESOLVED ON W/O: 22159 TASKCARD: N/R-00221). BLENDED CORRODED AREA OF DOUBLER AT FS 469-473 BL37-44LT IAW CRJ 200 SRM 51-41-45. REQUEST THICKNESS CHECK OF BLENDED AREA DK 7022603.C/W THICKNESS CHECK AT BLENDED AREA IAW CRJ 200 NDT MANUAL 51-20-04 PART 1, MINIMUM THICKNESS IS .081". C/W EDDY CURRENT INSPECTION OF REWORKED AREA PER REO601R-53-41-412 IAW CRJ 200 NDTM 51-20-06. NO DEFECTS NOTED. FASTENERS BLENDED ARE INSIDE THE ACCEPTED LIMITS ALSO REPAINTED THE SURFACES PER REO601R-53-41-412 SM 7032171, RII C/W SATISFACTORY COMPLIED WITH EC/TC REO 601R-53-41-412.

Part: DOUBLER — CORRODED (BS 513-517) · airframe 17,844 hrs · 15,102 cycles

FOUND CORROSION ON DOUBLER FS 513-517 - BL42-44LT (RESOLVED ON W/O: 22159 TASKCARD: N/R-00227 ). BLENDED CORRODED AREA OF DOUBLER FS 513-517-BL42-44LT IAW CRJ 200 SRM 51-41-45 REQUEST THICKNESS CHECK OF BLENDED AREA DK 7022603. C/W THICKNESS CHECK AT BLENDED AREA IAW CRJ 200 NDT MANUAL 51-20-04 PART 1, MINIMUM THICKNESS IS .077". C/W EDDY CURRENT INSPECTION OF REWORKED AREA PER REO601R-53-41-412 IAW CRJ 200 NDTM 51-20-06. NO DEFECTS NOTED. FASTENERS BLENDED ARE INSIDE THE ACCEPTED LIMITS ALSO REPAINTED THE SURFACES PER REO601R-53-41-412 BAT23167 RII REQUIREMENTS SATISFACTORY PER SP607. COMPLIED WITH EC/TC REO 601R-53-41-412.

Part: DOUBLER — CORRODED (BS 522-529) · airframe 17,844 hrs · 15,102 cycles

FOUND CORROSION ON DOUBLER AT FS 522-529 - BL41-44 LT.

Part: DOUBLER — CORRODED (BS 473-477) · airframe 17,844 hrs · 15,102 cycles

FOUND CORROSION ON DOUBLER AT FS 473-477 -BL41-44 LT (RESOLVED ON W/O: 22159 TASKCARD: N/R-00222 ). BLENDED CORRODED AREA OF DOUBLER AT FS 473-477 BL41-44LT IAW CRJ 200 SRM 51-41-45. REQUEST THICKNESS CHECK OF BLENDED AREA DK 7022603. C/W THICKNESS CHECK AT BLENDED AREA IAW CRJ 200 NDT MANUAL 51-20-04 PART 1, MINIMUM THICKNESS IS .079". C/W EDDY CURRENT INSPECTION OF REWORKED AREA PER REO601R-53-41-412 IAW CRJ 200 NDTM 51-20-06. NO DEFECTS NOTED. FASTENERS BLENDED ARE INSIDE THE ACCEPTED LIMITS ALSO REPAINTED THE SURFACES PER REO601R-53-41-412 SM 7023171. RII REQUIREMENTS SATISFACTORY PER SP607. COMPLIED WITH EC/TC REO 601R-53-41-412.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 17,844 hrs · 15,102 cycles

FOUND CORROSION ON FLOORBEAM END AT FS 349 - BL45RT, RESOLVED ON W/O: 22159 TASKCARD: N/R-00209. REPAIRED CORROSION ON FLOORBEAM IAW REO601R-53-21-659 AND REO 601R-53-21-326 AND REO 601R-53-21-661.

Part: FITTING — CRACKED (SERVICE DOOR) · airframe 17,844 hrs · 15,102 cycles

ASD FWD ANCHOR FITTING CRACKED. REMOVED AND REPLACED THE FORWARD AND AFT COUTERBALANCE SWIVEL AND ANCHOR FITTINGS IAW EO600-52-66.

Part: CLIP — BROKEN (BS 484) · airframe 17,844 hrs · 15,102 cycles

FOUND BS 484 CLIP BROKEN LT SIDE- BL27LT.

Part: FRAME — CRACKED (BS 280) · airframe 17,844 hrs · 15,102 cycles

SUSPECTED CRACK IN LOWER RADIUS OF 280 FRAME - APPROX BL 12RT (RESOLVED ON W/O: 22159 TASKCARD: N/R-00121). REPAIRED PILOTS BULKHEAD AT FS 280 RBL 9.0 IAW EO 600-53-0090.

Part: FLOOR SUPPORT — CORRODED (COCKPIT FLOOR) · airframe 17,844 hrs · 15,102 cycles

FOUND COCKPIT FLOOR AFT ATTACH ANGLE AT FS 279 CORRODED.

Part: OXYGEN MASK — NO TEST (CABIN) · airframe 17,844 hrs · 15,102 cycles

CABIN O2 MASKS 3CD - 7CD - 8CD WILL NOT DEPLOY, RESOLVED ON W/O: 22160 TASKCARD: N/R-00055. ADJUSTED LATCHES AT ROWS 3CD - 7CD - AND 8CD IAW CRJ 200 AMM 35-21-05. OPERATIONAL CHECK OF THE PASSENGER OXYGEN SYSTEM COMPLIED WITH IAW CRJ 200 35-20-00. NO DEFECTS NOTED AT THIS TIME, MV 22816 04/29/2006.

Part: FRAME — CRACKED (BS 718 S13) · airframe 17,844 hrs · 15,102 cycles

FOUND 718 FRAME CRACKED ABOVE STR 13, AFT EQUIP BAY.

Part: CLIP — CRACKED (FUSELAGE)

DURING C-CHECK, THE CLIP ON RT FS 461, RBL9 OB PRESSURE FLOOR AREA, WAS FOUND TO BE CRACKED.

Part: PLACARD — MISSING (CABIN)

DURING A GROUND INSPECTION, THE PASSENGER DOOR EXIT PLACARD WAS FOUND TO BE MISSING. MAINTENANCE REPLACED THE PASSENGER DOOR EXIT PLACARD. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)

Part: STEP — BROKEN (FUSELAGE)

DURING A GROUND INSPECTION IN MCO, THE PASSENGER DOOR BOTTOM STEP WAS FOUND TO BE BROKEN. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR BOTTOM STEP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LIGHT — DAMAGED (CABIN)

DURING A HANGAR INSPECTION IN BTR, THE EMERGENCY LIGHT ON THE FLIGHT ATTENDANTS CABINET WAS FOUND TO BE DAMAGED. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT ASSEMBLY, ON THE FLIGHT ATTENDANTS CABINET. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT)

DURING A GROUND INSPECTION IN MGM, THE AFT EMERGENCY CEILING LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE AFT EMERGENCY CEILING LIGHT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LAMP — BURNED OUT (EMERGENCY LIGHT)

DURING OVERNIGHT MAINTENANCE, THE RT OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE RT OVERWING EMERGENCY LIGHT. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. (K)

Part: HANDLE — BINDING (PASSENGER DOOR)

DURING A GROUND INSPECTION, THE FLIGHT ATTENDANT REPAORTED THE PASSENGER DOOR DIFFICULT TO OPEN. MAINTENANCE REMOVED, REBUILT, AND REINSTALLED THE PASSENGER DOOR HANDLE ASSY. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. (K)

Part: STEP — BROKEN (PAX DOOR)

FLT 4418 - DURING A GROUND INSPECTION IN ATL, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: BRACKET — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE FORWARD BRACKET ON THE LEFT FUSELAGE FRAME FS 718, STRINGER 10-11 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE LEFT FUSELAGE FRAME FS 718, STRINGER 10-11 IAW ASA EO 600-53-0066. (M)

Part: STEP — CRACKED (PAX DOOR)

DURING A C-CHECK IN MCN, THE TOP STEP ON THE PASSENGER DOOR WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE TOP STEP ON THE PASSENGER DOOR IAW CRJ200 MM 52-10-00. (M)

Part: STEP — BROKEN (PAX DOOR) · airframe 13,874 hrs

DURING HANGER MAINTENANCE, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR.

Part: LIGHT — BROKEN (CABIN) · airframe 13,874 hrs

DURING HANGER MAINTENANCE, THE EMERGENCY FLOOR FLOOD LIGHT AT THE PASSENGER DOOR WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY FLOOR FLOOD LIGHT AT THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE.

Part: STEP — CRACKED (PAX DOOR)

DURING AN A-CHECK IN BTR, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE REPAIRED THE BOTTOM STEP ON THE PASSENGER DOOR IAW THE CRJ-200 MM. (M)

Part: LAMP — BURNED OUT (EMERGENCY LIGHT)

DURING HANGER MAINTENANCE, THE NR 3 EMERGENCY CEILING LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 3 EMERGENCY CEILING LIGHT LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE.

Part: DOUBLER — CRACKED (FUSELAGE)

DURING AN A-CHECK IN BTR, THE LEFT DOUBLER AT FS 640, STRINGER 9 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LEFT DOUBLER AT FS 640, STRINGER 9. (M)

Part: DOUBLER — CRACKED (FUSELAGE)

DURNG AN A-CHECK IN BTR, THE LT AND RT FS 640 AT BL 45 DOUBLERS WERE FOUND CRACKED. UPON REMOVAL OF THE DOUBLERS MAINTENANCE FOUND FS 640 AT BL 45 TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMVOED AND REPLACED FS 640 AT BL 45. (M)

Part: STEP — BROKEN (PAX DOOR)

DURING HANGAR MAINTENANCE IN MCN, THE PASSENGER DOOR BOTTOM STEP WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED TEH PASSENGER DOOR BOTTOM STEP. (M)

Part: STEP — CRACKED (PAX DOOR)

FLT 4884 - DURING A GROUND INSPECTION IN DFW, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT)

DURING A ROUTINE CHECK IN SHV, THE RIGHT EXTERIOR OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE RIGHT EXTERIOR OVERWING EMERGENCY LIGHT LAMP. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: CONTROL QUADRANT — DIRTY (AILERONS)

DURING CLIMB-OUT FROM DFW-MOB, THE CREW EXPERIENCED THE AILERONS SHOWING SIGNS OF BINDING WHEN INITIATING LEFT TURNS. WITH SUFFICIENT INPUT THE AILERON POPPED FREE AND THE AIRCRAFT JERKED LEFT. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO DFW, LANDING SAFELY. MAINTENANCE INSPECTED THE LEFT AND RIGHT AILERON QUADRANTS INCLUDING THE LEFT AND RIGHT AILERON PULLEYS IN THE BRAKE AND POSITION SENSOR UNTI AREA. THE LEFT AND RIGHT AILERON QUADRANTS WERE FOUND TO BE SOILED AND GRITTY ON BOTH SIDES. MAINTENANCE CLEANED BOTH THE AILERON QUADRANTS AND PULLEYS IAW SERVICE LETTER NR RJ-SL-27-080. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: CLIP — CRACKED (FLOORBEAM)

DURING HANGAR MAINTENANCE, FLOORBEAM CLIPS AT BULKHEAD FS 280 LBL AND RBL 9 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE PERFORMED A TEMPORARY REPAIR BY STOP DRILLING THE ENDS OF THE CRACKS OF THE FLOORBEAM CLIPS AT BULKHEAD FS 280, LBL AND RBL 9 IAW ASA EO 600-53-0100. (M)

Part: O-RING — LEAKING (APU FUEL LINE)

DURING CRUISE A STRONG FUEL ODOR OCCURRED IN THE COCKPIT AND CABIN. THE AIRCRAFT LANDED SAFELY IN JAN. MAINTENANCE REMOVED AND REPLACED THE AUXILIARY POWER UNITS FUEL FEED LINE O-RINGS, ([P/N'S MS29513-218, MS29513-222, MS29513-015). OPERATIONAL AND LEAK CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: CONNECTOR — INOPERATIVE (EMERGNECY LIGHT)

FLT 4753 - DURING A GROUND INSPECTION IN ATL, THE FLIGHT ATTENDANT REPORTED THE EMERGENCY FLOOR LIGHTS FROM ROW 8 TO THE BACK OF THE CBIN WERE INOPERATIVE. MAINTENANCE RESECURED FLOOR LIGHT STRIP CONNECTORS AT ROW 8. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: BRACKET — CRACKED (FUSELAGE)

DURING A C-CHECK INSPECTION IN MCN, THE LEFT AND RIGHT ANGLE BRACKETS BELOW THE ENGINE SUPPORT BEAM WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE LEFT AND RIGHT ANGLE BRACKETS BELOW THE ENGINE SUPPORT BEAM IAW SRM 51-00. (M)

Part: FRAME — CRACKED (FUSELAGE)

DURING A C-CHECK INSPECTION IN MCN, THE LEFT AND RIGHT FRAMES FS 718 BETWEEN STRINGERS 10 TO 12 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING LEFT AND RIGHT FRAMES FS 718 BETWEEN STRINGERS 10 TO 12 IAW ASA EO 600-53-0067A. (M)

Part: SUPPORT — CRACKED (FUSELAGE)

DURING A C-CHECK INSPECTION IN MCN, THE LEFT AND RIGHT ENGINE SUPPORT BEAMS AT BL 36.20 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE CRACKED LEFT AND RIGHT ENGINE SUPPORT BEAMS AT BL 36.20 IAW ASA EO 600-53-0073. (M)

Part: WINDSHIELD — CRACKED (COCKPIT)

FLT 4766 - DURING APPROACH INTO AUS, THE FIRST OFFICER NOTICED WHAT APPEARED TO BE A SCRATCH OR CRACK IN THE UPPER CORNER ON THE NR 3 WINDSHIELD. THE AIRCRAFT LANDED SAFELY IN AUS. MAINTENANCE DETERMINED THE NR 3 WINDSHIELD TO BE CRACKED, REMOVED AND REPLACED IT. OPERATIONAL AND LEAK CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: O-RING — DAMAGED (LT ENGINE)

DURING CLIMB-OUT OF PIA EN ROUTE TO ATL, CAPTAIN REPORTED THE LEFT ENGINE OIL PRESSURE WARNINGS AND ANALOG INDICATION FLUXED FROM 45 TO 24 PSI. INDICATIONS WERE NORMAL AT LOWER POWER SETTINGS. AIRCRAFT DIVERTED TO EVV AND THE CAPTAIN SHUTDOWN THE LEFT ENGINE ON APPROACH DUE TO THE LOW OIL PRESSURE WARNING. AIRCRAFT LANDED IN EVV WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE O-RING ON THE OIL PRESSURE SWITCH. MAINTENANCE ALSO SERVICED THE LEFT ENGINE WITH 6 QUARTS OF OIL. GROUND RUNS WERE GOOD. NO LEAKS WERE FOUND. AIRCRAFT OK FOR SERVICE. (M)

Part: SMOKE DETECTOR — ACTIVATED (CARGO BAY)

DURING FLIGHT, CREW REPORTED CARGO SMOKE LIGHT ILLUMINATED. CREW DECLARED EMERGENCY AND DISCHARGED FIRE BOTTLES. AC LANDED SAFELY. MAINTENANCE INSP CARGO COMPARTMENT, NO EVIDENCE OF FIRE, REMOVED AND REPLACED FIRE BOTTLES AND SQUIBBS. AC RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN)

FLT 4737 - CREW REPORTED EMERGENCY LIGHTS FROM ROW 1 TO ROW 8 ARE INTERMITTENT. MAINTENANCE CLEANED AND DRIED THE EMERGENCY LIGHT EXIT STRIPS AS NEEDED. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (M)