N824AS

Part: CHARGER — FAILED (EMERGENCY LIGHTS) · airframe 37,740 hrs · 34,721 cycles

EMERGENCY LIGHTS STAY ILLUMINATED AT OVERWING EXITS. R & R THE AFT BATTERY CHARGER IN THE CABIN.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 37,106 hrs · 34,260 cycles

EMERGENCY LIGHTS INOPERATIVE. PERFORMED OPS CHECK OF EMERGENCY LIGHTS AFTER CHARGING, OPS CHECKED GOOD IAW AMM 33-51-00, ACFT OK FOR SERVICE.

Part: DOOR FRAME — CRACKED (PAX DOOR) · airframe 37,094 hrs · 34,246 cycles

PAX DOOR FRAME CRACKED AT BS 320.1, TOP OF DOOR. REPAIRED IAW 52-11-04-000-808 AND 52-11-04-000-810 AND SRM 51-42-13-00. COMPLIED WITH OPS TEST F/O ASD IAW AMM 52-11-00-710-801, OPS TESTED GOOD. MAJOR REPAIR.

Part: FRAME — CRACKED (PAX DOOR) · airframe 37,094 hrs · 34,246 cycles

PAX DOOR FRAME CRACKED AT BS 338 TOP OF DOOR. REPAIRED IAW REO 601R-52-11-402 .

Part: FLOOR SUPPORT — CRACKED (CABIN) · airframe 37,094 hrs · 34,246 cycles

FLOOR SUPPORT CRACKED & CORRODED. REMOVED FLOOR SUPPORT IAW SRM 51-42-06 AND SRM 51-42-21. INSTALLED NEW FLOOR SUPPORT IAW SRM 51-42-06 AND SRM 51-42-21 AND REO: 601R-53-61-593.

Part: FLOOR SUPPORT — CORRODED (BS 521-559) · airframe 37,094 hrs · 34,246 cycles

FLOOR SUPPORT CORRODED BETWEEN BS 559+112 TO 521 LT SIDE. FLOOR SUPPORT REPLACED IAW REO 601R-53-61-593.

Part: FLOOR SUPPORT — CRACKED (BS 484) · airframe 37,094 hrs · 34,246 cycles

FS 484, FLOOR SUPPORT CRACKED AT RBL 27.0. REMOVED D & INSTALLED NEW FLOOR SUPPORT IAW SRM 51-42-21.

Part: RUB STRIP — WORN (VERTICAL STAB) · airframe 37,094 hrs · 34,246 cycles

VERTICAL STABILIZER LT UPPER VISOR ASSY FWD RUB STRIP IS WORN AND DETACHED. RECEIVED AND COMPLIED WITH ECTC OF REO 601R-52-11-2219 FOR DEVIATION OF GENERIC REO 601R-52-11-402. EC/TC REO 601R-52-11-2216 HAS BEEN COMPLETED AND ALL STEPS HAVE BEEN DOCUMENTED AND SIGNED FOR ON A NON ROUTINE WORK CARD. COMPLIED WITH EC/TC OF REO 601R-52-11-402 AND GENERIC REO 601R-52-11-402. REPAIR IS CLASSIFIED AS MAJOR.

Part: FLOOR SUPPORT — CORRODED (BS 574-621) · airframe 37,094 hrs · 34,246 cycles

LEFT CARGO FLOOR SUPPORT HAS CORROSION BETWEEN BS 574 - 621, LBL 27 OTBD SIDE. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-42-21 AND 51-42-22.

Part: FLOOR SUPPORT — CORRODED (BS 559) · airframe 37,094 hrs · 34,246 cycles

CARGO LT FLOOR SUPPORT HAS CORROSION BETWEEN BS 559+80-FS 559+96, LBL 47. REPAIRED IAW EC/TC REO 601R-53-00-526 AND REO 601R-53-00-526.

Part: FLOOR SKIN — CRACKED (BS 460) · airframe 37,094 hrs · 34,246 cycles

PRESSURE FLOOR SKIN CRACKED APPROX 3 INCH AT FS 460 BETWEEN BL 0 AND RBL 9. COMPLIED WITH REO:601R-53-41-1808.

Part: ISOLATOR — BROKEN (BS 621 BULKHEAD) · airframe 37,094 hrs · 34,246 cycles

FOUR ISOLATORS BROKEN ON FWD FACE OF FS 621 BULKHEAD IN CARGO BAY. REMOVED BROKEN ISOLATORS FROM MOUNTING BRACKETS IAW SRM 51-42-06 (4 EA). INSTALLED NEW SERVICEABLE ISOLATORS ON MOUNTING BRACKETS IAW SRM 51-42-06 (4 EA).

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 35,811 hrs · 32,928 cycles

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

Part: FUSE — BLOWN (EMERGENCY LIGHTS) · airframe 35,431 hrs · 32,550 cycles

NR 2 AND 4 CEILING EMERGENCY LIGHTS INOPERATIVE. REPLACED FUSE ON NR 4 BATTERY POWER SUPPLY IAW CMM 33-21-70. OPS CHECKED GOOD IAW AMM 33-51-00.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 35,431 hrs · 32,550 cycles

RIGHT REAR EMERGENCY LIGHT INOPERATIVE. REPLACED LAMPS IAW AMM 33-51-21. OPS CHECKED GOOD.

Part: STRUCTURE — CRACKED (PAX DOOR) · airframe 35,227 hrs · 32,326 cycles

PAX DOOR HAS A CRACK. REPAIRED IAW REO 601R-52-11-1359-01.

Part: DOOR — BINDING (MAIN PAX) · airframe 35,046 hrs · 32,139 cycles

PAX DOOR IS HARD TO OPEN , F/A CANNOT GET THE HANDLE TO STOW , .2500" GAP AT THE TOP OF THE DOOR. PREFORMED OPS CHECK OF PAX DOOR IAW AMM 52-11-00, PRESSURIZED ACFT , OPS CHECKED GOOD.

Part: RIB — CRACKED (HORIZTONAL STAB) · airframe 34,942 hrs · 32,029 cycles

RT HORIZONTAL STAB RIB 9 IS CRACKED. REMOVED THE RT HORIZONTAL STAB RIB AND DRILLED NEW RIB AND TRANSFERED ALL ANGLES AND BRACKETS IAW SRM 51-42-13 AND IAW SRM 51-42-06. INSTALLED NEW RIB 9 IAW SRM 51-42-13 , 51-45-00.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 34,737 hrs · 31,818 cycles

STRONG BURNING ODOR THROUGH COCKPIT GASPERS. F/A CALLED AND REPORTED THE SAME. ELECTRICAL COMPONENT BURNING ODOR. F/A REPORTED NO SMOKE BUT ODOR WAS STRONG. HAD F/A PULL GALLEY C/B'S AND ODOR WENT AWAY AFTER 1-2 MINUTES. ( GALLEY HEATING SYSTEM: FAN ) EMERGENCY DECLARED AS A PRECAUTION. OPEN.

Part: LATCH — JAMMED (PAX DOOR) · airframe 34,166 hrs · 31,212 cycles

PASSENGER DOOR LATCH HARD TO CLOSE AND OPEN. LOWER LATCH ESPCIALLY. PERFORMED OPS CHECK OF PAX DOOR IAW AMM 52-11-03. OPS CHECKED GOOD. SDR CLOSED.

Part: HANDLE — INOPERATIVE (PAX DOOR) · airframe 34,069 hrs · 31,112 cycles

PASSENGER DOOR WILL NOT OPEN FROM THE INSIDE OR OUTSIDE. R & R HANDLE. OPS CHECKED GOOD. ACFT OK FOR FURTHER SERVICE.

Part: DOOR — LACK OF LUBE (MAIN PAX) · airframe 33,901 hrs · 30,938 cycles

MAIN CABIN DOOR DIFFICULT TO OPEN. LUBRICATED PAX DOOR , OPS CHECKED GOOD IAW AMM 52-11-00.

Part: COUNTERBALANCE — OUT OF ADJUST (PAX DOOR) · airframe 33,710 hrs · 30,729 cycles

F/O UNABLE TO OPEN PAX DOOR ( DOORS AND OVERWING EMERGENCY EXITS ) ADJUSTED PAX DOOR COUNTERBALANCE IAW AMM 52-11-17, OPS CK GOOD DEFER CLEARED PLACARD REMOVED.

Part: LATCH — CONTAMINATED (PAX DOOR) · airframe 33,710 hrs · 30,729 cycles

F/A UNABLE TO OPEN MAIN PAX DOOR. FOUND DEBRIS IN LATCH ON MECHANISM CLEANED OUT AND LUBRICATED IAW AMM 52-11-03. ALL ROLL FITTINGS ACFT OK FOR SERVICE.

Part: HANDLE — LACK OF LUBE (PAX DOOR) · airframe 33,666 hrs · 30,684 cycles

PAX OUTER HANDLE HARD TO PUSH OPEN. PAX OUTER HANDLE LUBRICATED IAW AMM 52-11-03. OPS CHECKED GOOD.

Part: HANDLE — OBSTRUCTED (PAX DOOR) · airframe 33,647 hrs · 30,663 cycles

MAIN PASSENGER DOOR WILL NOT OPEN FROM INSIDE OR OUTSIDE. FOUND EXCESSIVE DEBRIS AND GREASE ON DOOR LOCKING HANDLE MECHANISM, CLEANED AND PERFORMED OPS TEST IAW AMM 52-11-00. OPS TESTED GOOD ACFT OK FOR SERVICE.

Part: FLOOR SUPPORT — CORRODED (BS 349) · airframe 33,584 hrs · 30,594 cycles

RT FLOOR SUPPORT BEHIND FS 349 IS CORRODED. INSTALLED NEW FLOOR SUPPORT SECTION IAW REO 601R-53-21-425.

Part: STRAP — CORRODED (BS 5559) · airframe 33,584 hrs · 30,594 cycles

STRAP AT FS 559 AT RBL 36-45 CORRODED. APPLIED FINISH TO REWORKED AREA IAW SRM 51-21-11.

Part: FLOORBEAM — CORRODED (BS 349) · airframe 33,584 hrs · 30,594 cycles

AFTER REMOVAL OF SERVICE DOOR SILL, FOUND CORROSION ON FS 349 FLOORBEAM LATERAL FRAME AT RBL 42. FOUND TO BE OUT OF LIMITS IAW SRM 51-21-06. CUT AWAY DAMAGE ON FLOORBEAM IAW REO 601R-53-21-2320, STEP 1 & 3. COMPLIED WITH STEP 2 OF REO 601R-53-21-2320 IAW NDTM PART 1, 51-20-06 NO INDICATION NOTED AT THIS TIME. INSTALLED REPAIR.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 33,584 hrs · 30,594 cycles

SEAT TRACK AT RBL 9.0 BETWEEN FS 559+4 - 559+86 CORRODED. FOUND TO BE OUT OF LIMITS IAW SRM 53-21-49. REMOVED SEAT TRACK IAW AMM 53-01-11-000-802. INSTALLED NEW SEAT TRACK IAW AMM 53-01-11-400-802.

Part: LIGHT — BROKEN (CABIN) · airframe 33,584 hrs · 30,594 cycles

EMERGENCY EXIT LIGHT ASSY AT GALLEY/SERVICE DOOR BROKE. REMOVED UNSERVICEABLE GALLEY 1 EMERGENCY EXIT LIGHT ASSY IAW AMM TASK 25-31-01-000-802 SUBTASK 25-31-01-000-011. INSTALLED SERVICEABLE GALLEY 1 EMERGENCY EXIT LIGHT ASSY IAW AMM 25-31-01-400-802.

Part: SUPPORT BRACKET — CORRODED (BS 349) · airframe 33,584 hrs · 30,594 cycles

CORROSION ON UPPER AND LOWER SURFACE OF TOP FLANGE ON WINDSCREEN SUPPORT BRACKET. INSTALLED NEW SUPPORT ANGLE IAW SRM 51-42-06-00 & 51-42-21-00.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 33,584 hrs · 30,594 cycles

CARGO TRACK AT RBL 9 BETWEEN FS 559+86 - 559+94 CORRODED. FOUND TO BE UNSERVICEABLE IAW SRM 53-61-49. REMOVED CARGO TRACK IAW AMM 53-01-11-000-802. INSTALLED CARGO TRACK IAW AMM 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 399-409) · airframe 33,584 hrs · 30,594 cycles

SEAT TRACK AT LBL 9 BETWEEN FS 399 - 409+125 CORRODED. FOUND TO BE OUT OF LIMITS IAW SRM 53-21-49. REMOVED SEAT TRACK IAW AMM 53-01-11-000-802. INSTALLED NEW SEAT TRACK IAW AMM 53-01-11-400-802.

Part: FLOORBEAM — CORRODED (BS 589) · airframe 33,584 hrs · 30,594 cycles

CARGO FLOORBEAM AT FS 589 BETWEEN RBL 27 - RBL 41 IS CORRODED. BLENDED DAMAGE AND FOUND TO BE OUT OF LIMITS IAW SRM 51-321-06 & SRM 53-00-00. PERFORMED UT INSPECTION OF BLEND AREA IAW MWC NDT INSPECTION PROCEDURE UT-3. REPAIRED IAW REO 601R-53-61-4557.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 33,584 hrs · 30,594 cycles

SEAT TRACK AT LBL 9 BETWEEN FS 559+86 CORRODED. REMOVED CORRODED SEAT TRACK IAW AMM 53-01-11-000-802. INSTALLED NEW SEAT TRACK IAW AMM 53-01-11-400-802.

Part: CARGO TRACK — CORRODED (BS 559) · airframe 33,584 hrs · 30,594 cycles

CARGO TRACK AT LBL 27.0 BETWEEN FS 559+78 - 559+94 CORRODED. REMOVED SEAT TRACK IAW AMM 53-01-11-000-802. INSTALLED SERVICEABLE SEAT TRACK IAW AMM 53-01-11-400-802.

Part: CARGO TRACK — CORRODED (BS 559-570) · airframe 33,584 hrs · 30,594 cycles

CARGO TRACK AT LBL 9 BETWEEN FS 559+110 - 570 IS CORRODED. CARGO TRACK FOUND TO BE UNSERVICEABLE IAW SRM 55-61-49. R & R CARGO TRACK IAW SRM 53-61-49 AND 51-41-02 DWG 601R381981.

Part: SEAT TRACK — CORRODED (BS 364-399) · airframe 33,584 hrs · 30,594 cycles

SEAT TRACK AT RBL 9 BETWEEN FS 364 - 399 CORRODED. FOUND TO BE OUT OF LIMITS IAW SRM 51-21-06 AND SRM 53-21-49. REMOVED AND INSTALLED SERVICEABLE SEAT TRACK IAW AMM 53-01-11-000-802, AMM 53-01-11-400-820.

Part: STRAP — CORRODED (BS 559) · airframe 33,584 hrs · 30,594 cycles

STRAP AT FS 559 RBL 36-45 CORRODED. BLEND CORROSION ON STRAP AT FS559.0 AT RBL 36-45 AND EVALUATE. BLENDED CORROSION IAW SRM 53-00-00, FIG 101. PERFORMED UT THICKNESS INSPECTION PROCEDURE UT-3. REPAIRED IAW REO 601R-53-41-1584.

Part: FLOOR SUPPORT — CORRODED (BS 559-621) · airframe 33,584 hrs · 30,594 cycles

CARGO RT FLOOR SILL IS CORRODED BETWEEN FS 559+80 - 621. REMOVED CORROSION IAW SRM 51-21-06. PERFORMED UT THICKNESS INSPECTION OF BLEND AREA IAW MAC NDT INSPECTION PROCEDURE UT-3. WITHIN LIMITS OF SRM 53-00-00.

Part: FLOOR SUPPORT — CORRODED (BS 559) · airframe 33,584 hrs · 30,594 cycles

CARGO LT FLOOR SILL IS CORRODED BETWEEN FS 559.00+80 TO 559.00+112. REMOVED CORROSION IAW SRM 51-21-06. PERFORMED UT THICKNESS INSPECTION OF BLEND AREA IAW MAC NDT INSPECTION PROCEDURE UT-3. MIN MATERIAL REMAINING IS .061" ORIGINAL IS .063" MATERIAL REMOVED IS .002". REPAIRED IAW REO 601R-53-51-163

Part: FLOORBEAM — CORRODED (BS 621) · airframe 33,584 hrs · 30,594 cycles

CARGO FLOORBEAM AT FS 621 BETWEEN LBL 9 - 27 CORRODED. REMOVED CORROSION IAW SRM 51-21-06. BEYOND LIMITS IAW SRM 53-61-49.

Part: CARGO TRACK — CORRODED (BS 559-570) · airframe 33,584 hrs · 30,594 cycles

CARGO TRACK AT RBL 9 BETWEEN FS 559+110 - 570 CORRODED. CARGO TRACK FOUND TO BE UNSERVICEABLE IAW SRM 55-61-49. R & R CARGO TRACK IAW SRM 53-61-49 AND 51-41-02 DWG 601R387981.

Part: SILL — CORRODED (BS 319-349) · airframe 33,591 hrs · 30,602 cycles

SERVICE DOOR SILL IS CORRODED BETWEEN FS 319-349. R & R SERVICE DOOR SILL IAW EO 600-53-0724.

Part: FLOOR SUPPORT — CORRODED (BS 349) · airframe 33,584 hrs · 30,594 cycles

RT FLOOR SUPPORT BEHIND FS 349 IS CORRODED. REMOVED CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00. REMOVED CORRODED SECTION OF FLOOR SUPPORT IAW SRM 51-42-06. FABRICATED PARTS IAW REO 61R-53-21-425 (STEP7) IAW SRM 51-24-21. REPLACED IAW SRM 51-42-06, 51-26-00, 51-21-11, & REO 601R-53-21-425.

Part: SEAT TRACK — CORRODED (BS 399-409) · airframe 33,584 hrs · 30,594 cycles

SEAT TRACK AT RBL 9 BETWEEN FS 399 - 409+125 CORRODED. SEAT TRACK FOUND TO BE OUT OF LIMITS IAW SRM 53-21-49. REMOVED SEAT TRACK IAW AMM 53-01-11-000-802. INSTALLED SERVICEABLE SEAT TRACK IAW AMM 53-01-11-400-802.

Part: CARGO TRACK — CORRODED (BS 559) · airframe 33,584 hrs · 30,594 cycles

CARGO TRACK AT LBL 27, BETWEEN FS 559+78 - 559+94 IS CORRODED. FOUND TO BE UNSERVICEABLE IAW SRM 53-61-49. R & R CARGO TRACK IAW AMM 53-01-11-000-802 / 53-01-11-400-802.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 33,584 hrs · 30,594 cycles

CABIN FLOORBEAM AT FS 280.00, RBL 9.0 IS CRACKED. REPAIRED IAW REO 601R-53-11-171.

Part: SEAT TRACK — CORRODED (BS 409-559) · airframe 33,584 hrs · 30,594 cycles

SEAT TRACK AT LBL 9.0 BETWEEN FS 409+125 - 559+4 CORRODED. FOUND TO BE OUT OF LIMITS IAW SRM 53-21-49. REMOVED SEAT TRACK IAW AMM 53-01-11-000-802. DRILLED SEAT TRACK AND INSTALLED IAW AMM 53-01-11-420-001.

Part: SEAT TRACK — CORRODED (BS 364-399) · airframe 33,584 hrs · 30,594 cycles

SEAT TRACK AT LBL 9.0 BETWEEN FS 364 -399 CORRODED. FOUND TO BE OUT OF LIMITS IAW SRM 53-21-49. REMOVED SEAT TRACK IAW AMM 53-01-11-000-802. INSTALLED SEAT TRACK IAW AMM 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 409-559) · airframe 33,584 hrs · 30,594 cycles

SEAT TRACK AT RBL 9 BETWEEN FS 409+125 - 559+4 CORRODED. SEAT TRACK FOUND TO BE OUT OF LIMITS IAW SRM 53-21-49. REMOVED SEAT TRACK IAW AMM 53-01-11-000-802. INSTALLED NEW SEAT TRACK IAW AMM 53-01-11-400-802.

Part: CARGO TRACK — CORRODED (BS 612-616) · airframe 33,584 hrs · 30,594 cycles

CARGO TRACK AT LBL 9 BETWEEN FS 612 - 616 IS CORRODED. CARGO TRACK FOUND TO BE UNSERVICEABLE IAW SRM 53-61-49. R & R CARGO TRACK IAW AMM 53-01-11-000-802.

Part: FLOORBEAM — CORRODED (BS 574) · airframe 33,584 hrs · 30,594 cycles

CARGO FLOORBEAM AT FS 574 BETWEEN LBL 9.0 - RBL 9.0 IS CORRODED. REMOVED CORROSION IAW SRM 51-21-06. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00. REMOVED AND INSTALLED CAP STRIP IAW SRM 51-42-06 AND 51-45-00, 51-42-15 AND DWG NR 601R35031.

Part: CARGO TRACK — CORRODED (BS 559) · airframe 33,584 hrs · 30,594 cycles

CARGO TRACK AT LBL 9 BETWEEN FS 559+86 - 559+94 IS CORRODED. REMOVED CARGO TRACK IAW SRM 51-41-02. INSTALLED NEW CARGO TRACK IAW SRM 51-41-02 AND 53-61-49.

Part: FLOORBEAM — CORRODED (BS 349) · airframe 33,584 hrs · 30,594 cycles

CARGO FLOORBEAM AT FS 349 BETWEEN LBL 27 - LBL 42 IS CORRODED ON UNDERSIDE. REPAIRED IAW SRM 51-42-06, 51-42-21.

Part: ISOLATOR — CRACKED (BULKHEAD) · airframe 33,584 hrs · 30,594 cycles

ISOLATOR CRACKED ON MOUNT BRACKET ON REAR PRESSURE BULKHEAD FORWARD FACE. R & R ISOLATOR, ALL WORK DONE IAW SRM 51-42-13. THIS REPAIR REQUIRES MAJOR/MINOR CLASSIFICATION IAW ASA SOP 5702. THIS REPAIR IS CLASSIFIED AS A MINOR REPAIR IAW ASA SOP 5702. (SDR CLOSED)

Part: SEAT TRACK — CORRODED (BS 394-409) · airframe 33,584 hrs · 30,594 cycles

RIGHT SIDE SEAT TRACK HAS CORROSION BETWEEN FS 394 AND 409. REMOVED CORROSION IAW SRM 51-21-06. FOUND TO BE WITHIN LIMITS IAW SRM 53-21-49. PERFORMED LPI, TYPE 1, METHOD C ON BLEND AREA IAW SRM 51-12-00 IAW MAC NDT INSPECTION PROCEDURE PT-1, NO INDICATIONS NOTED. RESTORED FINISH TO SIDE SEAT TRACK IAW SRM 53-21-49.

Part: SEAT TRACK — CORRODED (BS 364-409) · airframe 33,584 hrs · 30,594 cycles

LEFT SIDE SEAT TRACK HAS CORROSION BETWEEN FS 364.00 AND FS 409.00+16. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-01-11-000-802.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 33,591 hrs · 30,602 cycles

PERFORMED OPS CHECK OF EMERGENCY LIGHTS IAW AMM 33-51-00-710-801, FAILED OPS CHECK. TROUBLESHOT EMERGENCY LIGHTS AND FOUND ALL 4 BATTERY PACKS FULLY DISCHARGED IAW AMM 33-51-00-00. REPLACED ALL 4 EMERGENCY LIGHT BATERY PACKS IAW AMM 33-51-04-000-801 & 33-51-04-400-801. PERFORMED OPS CHECK OF EMERGENCY LIGHTS IAW AMM 33-51-00-710-801 & BATTERY PACK/CHARGER ASSY 33-51-04-740-801. OPS CHECKED GOOD.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 33,591 hrs · 30,602 cycles

PERFORMED OPS CHECK OF EMERGENCY LIGHTS IAW AMM 33-51-00-710-801 FAILED OPS CHECK. TROUBLESHOT EMERGENCY LIGHTS AND FOUND ALL 4 BATTERY PACKS FULLY DISCHARGED IAW AMM 33-51-00-00. REPLACED ALL 4 EMERGENCY LIGHT BATERY PACKS IAW AMM 33-51-04-000-801 & 33-51-04-400-801. PERFORMED OPERATIONAL TEST OF BATTERY PACK/CHARGER ASSY IAW AMM 33-51-04-740-801 & EMERGENCY LIGHT ADJUSTMENT TEST IAW AMM 33-51-00-710-801. OPS CHECKED GOOD.

Part: SEAT TRACK — CORRODED (BS 499-544) · airframe 33,584 hrs · 30,594 cycles

RT SIDE SEAT TRACK HAS CORROSION BETWEEN FS 499.00 AND 544.00. REMOVED CORROSION IAW SRM 51-21-06. MATERIAL REMAINING 0.336 AT LOCATION AT FS 522 MAT REMOVED 0.011 AT LOCATION U, AND FS 537 MAT REMAINING 0.354 AT LOCATION Y, REWORKED AREAS FOUND TO BE WITHIN ALLOWABLE DAMAGE LIMITS IAW SRM 53-41-49 AND SRM 53-21-49, FIG 101, TABLE 1. PERFORMED LPI, TYPE 1, METHOD C ON BLEND AREA IAW SRM 51-12-00 IAW MAC NDT INSPECTION PROCEDURE PT-1, NO INDICATIONS NOTED. RESTORED FINISH IAW SRM 51-21-16.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 33,585 hrs · 30,595 cycles

PERFORMED OPS CHECK OF EMERGENCY LIGHTS IAW AMM 33-51-00-710-501. FAILED OPS CHECK. TROUBLESHOT EMERGENCY LIGHTS & FOUND ALL FOUR BATTERY PACKS FULLY DISCHARGED IAW AMM 33-51-00-00. REPLACED EMERGENCY LIGHT BATTERY PACKS IAW AMM 33-51-04-000-801 & 33-51-04-400-801.

Part: SEAT TRACK — CORRODED (BS 424) · airframe 33,584 hrs · 30,594 cycles

LEFT SIDE SEAT TRACK HAS CORROSION JUST AFT OF FS 424. REMOVED SEAT TRACK IAW AMM 53-01-11-000-802. INSTALLED SERVICEABLE SEAT TRACK IAW AMM 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 409) · airframe 33,584 hrs · 30,594 cycles

RIGHT SIDE SEAT TRACK HAS CORROSION BETWEEN FS 409.00+48 AND 409.00+80. REMOVED CORROSION IAW SRM 51-21-06. FOUND TO BE WITHIN LIMITS IAW SRM 53-21-49. REMOVED 0.19. PERFORMED LPI, TYPE 1, METHOD C ON BLEND AREA IAW SRM 51-12-00 IAW MAC NDT INSPECTION PROCEDURE PT-1. NO INDICATIONS NOTED. RESTORED FINISH ON RT SIDE SEAT TRACK IAW SRM 51-21-16.

Part: SEAT TRACK — CORRODED (BS 409) · airframe 33,584 hrs · 30,594 cycles

RIGHT SIDE SEAT RAIL HAS CORROSION BETWEEN FS 409.00 + 16 AND FS 409.00+32. REMOVED CORROSION IAW SRM 51-21-06. FOUND TO BE WITHIN LIMITS IAW SRM 53-21-49. REMOVED 0.19. PERFORMED LPI, TYPE 1, METHOD C ON BLEND AREA IAW SRM 51-12-00 IAW MAC NDT INSPECTION PROCEDURE, PT-1. NO INDICATIONS NOTED. RESTORED FINISH TO RT SIDE SEAT TRACK IAW SRM 53-21-49.

Part: SEAT TRACK — CORRODED (BS 409) · airframe 33,584 hrs · 30,594 cycles

LEFT SIDE SEAT TRACK HAS CORROSION BETWEEN FS 409.00+16 AND FS 409.00+112. REMOVED SEAT TRACK IAW AMM 53-01-11-000-802. DRILLED & INSTALLED SERVICEABLE SEAT TRACK IAW AMM 53-01-11-400-802.

Part: LIGHT — MISSING (CABIN) · airframe 32,325 hrs · 29,187 cycles

LOWER LIGHTED EXIT SIGN ON BOARDING DOOR MISSING. R & R FWD "LT OF ENTRY" LOWER EMERGENCY FLOODLIGHT ASSY. OPS TEST GOOD. REF AMM 33-51-19. (CLOSED)

Part: HANDLE — FOD (PAX DOOR) · airframe 32,197 hrs · 29,039 cycles

MAIN CABIN DOOR JAMS WHEN OPENING. REMOVED FOD FROM OUTER HANDLE. MAIN PASSENGER DOOR OPERATES CORRECTLY IAW AMM 52-11-00. (CLOSED)

Part: CONVERTER — FAILED (RADIO ALTIMETER) · airframe 31,995 hrs · 28,826 cycles

IN FLIGHT, REX RA FAULT, TCAS FAIL, GPWS FAIL, & OTBD GND SPL FAULT. COMPLIED W/ QRH & RECEIVED INBD GND SPOILER, FLT SPOILER, OTBD GND SPOILERS, & SPOILERONS CAUTION MSGS. COMPLIED W/ QRH. EMERGENCY DECLARED AS A PRECAUTION. R & R RAD ALTIMETER CONVERTER ASSY, IAW AMM 34-44-04. OPS TEST GOOD. ALL MSGS EXTINGUISHED.

Part: SPOILER SYS — FAILED · airframe 31,995 hrs · 28,826 cycles

IN CRUISE RECEIVED FOLLOWING FAULTS: OTBD GND SPOILER FAULT, TCAS FAIL, GPWS FAIL, AND RAD ALT FLAG. FOLLOWED QRH, SPOILERS FAULTS PERSISTED. RAD ALT, TCAS AND GPWS FAULTS CLEARED WITH NO CREW ACTION. EMERGENCY DECLARED AS A PRECAUTION. SPOILER FAULT MSGS CLEARED IAW FIM ATA 27, PG 106-107. RESET PROCEDURES. RAD ALT, TCAS AND GPWS FAULTS CLEARED WITH NO CREW ACTION. NO FURTHER ACTION REQUIRED.

Part: LINKAGE — LACK OF LUBE (PAX DOOR) · airframe 31,567 hrs · 28,344 cycles

F/A REPORTS PAX DOOR HARD TO OPEN- HANDLE STICKS ABOUT HALFWAY TRAVEL. LUBED INNER LINKEAGE IAW AMM 52-11-21. (CLOSED)

Part: HANDLE — DIRTY (PAX DOOR) · airframe 30,419 hrs · 27,044 cycles

MAIN PAX DOOR HANDLE IS HARD TO MOVE/OPEN. INSP LINKAGE AND REMOVED DEBRIS. LUBE DOOR AND ROLLERS. OPS CHECKS GOOD WITH NO DEFECTS NOTED. REF AMM 52-11-02. (CLOSED)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,382 hrs · 27,001 cycles

NR 1 POSITION EXTERIOR EMERGENCY LIGHT INOP. R & R NR1 EXTERIOR EMERGENCY LIGHT IAW AMM 33-51-21. OPS CHECK GOOD. R & R NR1 EXTERIOR EMERGENCY LIGHT IAW AMM 33-51-21. OPS CHECK GOOD.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 30,346 hrs · 26,963 cycles

EMERGENCY LIGHT FWD OF PAX DOOR INOP. R & R EMERGENCY LIGHT FWD OF PAX DOOR IAW AMM 33-51-21. R & R EMERGENCY LIGHT FWD OF PAX DOOR IAW AMM 33-51-21. (CLOSED)

Part: HANDLE — BINDING (PAX DOOR) · airframe 29,998 hrs · 26,574 cycles

F/A AND F/O HAD TROUBLE OPENING CABIN DOOR HANDLE, BINDING. PERFORMED OPS TEST OF MAIN CABIN DOOR IAW MM 52-11-00 WITH NO DEFECTS NOTED. (CLOSED)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,994 hrs · 26,568 cycles

NR 4 EXT EMERGENCY LIGHT IS INOP. RELAMPED NR 4 EXT EMERGENCY LIGHT IAW AMM 33-51-21, OP'S CHECK GOOD.

Part: POST — CRACKED (BS 409) · airframe 29,808 hrs · 26,358 cycles

FOUND FS 409+128 VERTICAL POST BL 0.0 LT SIDE HAS INDICATION NOTED APPROX .3 IN LENGTH 80 PERCENT FSH AT WL 60.0 AFT FLANGE RADIUS. FAILED NDT INSP. COMPLIED WITH EC/TC REO 601R-53-41-1213 AND REO 601R-53-41-1213 REV A DATED 05/18/2010 AS WRITTEN.

Part: FLOOR SUPPORT — CORRODED (BS 605-621) · airframe 29,789 hrs · 26,334 cycles

CONTINUED FROM MWC 87220321, OP 360, FLOORBEAM CAP AT RBL 9 FS 621 TO FS 605 HAS MINOR CORROSION. FLOORBEAM CAP AT RLB 9 BETWEEN FS 569 TO FS 621 NEEDS DRILLED TO ACFT AND INSTALLED. LOCATED & DRILLED NEW SERVICEABLE BEAM CAP AT RBL 9 FS 621 TO FS 605 IAW SRM 51-40-11. BEAM CAP REQUIRES FINAL REAM, COUNTERSUNK, DEBURRED AND INSTALLED. FINAL REAMED COUNTERSUNK, DEBURRED AND INSTALLED FLOORBEAM CAP AT RBL 9, FS 569-FS 621 IAW REO 601R-53-61-3679. PREPPED AND PAINTED FASTENERS IAW SRM 51-25-01. EC/TC REQUIRED TO BE COMPLIED WITH. DISPOSITION FOR THE ALTERNATE FASTENER USE FOR FLOORBEAM CAP INSTALLATION BETWEEN FS 569 AND FS 621 LBL 9.0 AND RBL 9.0 ON ACFT SN 7203 IS COMPLETED IAW REO 601R-53-61-3679 AND MEETS WITH ALL IT'S REQUIREMENTS.

Part: FLOORBEAM — CORRODED (BS 621) · airframe 29,789 hrs · 26,334 cycles

BULKHEAD FITTING ON FLOORBEAM CAP RBL 9 AT FS 621 CORRODED. REMOVED BULKHEAD FITTING ON FLOORBEAM CAP IAW SRM 51-42-21. DRILLED AND LOCATED NEW SERVICEABLE FITTING IAW SRM 51-40-11. INSTALLED FITTING AT FLOORBEAM CAP IAW SRM 51-41-02 AND REO 601R-53-61-3679. COMPLETED IAW REO 601R-53-61-3679 AND MEETS ALL ITS REQUIREMENTS.

Part: POST — CRACKED (BS 409) · airframe 29,789 hrs · 26,334 cycles

FOUND FS 409.0+128 VERTICAL POST RBL 18.0 INBD AND OTBD SIDE HAVE INDICATIONS NOTED APPROX .3" IN LENGTH 80 PERCENT FSH AT AFT FLANGE RADIUS FAILED NDT INSPECTION. COMPLIED WITH EC/TC REO 601R-53-41-889 AND INSTALLED THE REQUIREMENTS OF REO 601R-53-41-889 REVISION A.

Part: SEAT TRACK — CORRODED (BS 424-461) · airframe 29,789 hrs · 26,334 cycles

PASSENGER RT SIDE SEAT RAIL AT FS 424.00 & FS 461.00 HAS CORROSION. REMOVED CORRODED SEAT RAIL AT FS 424.00 AND FS 461.00 RT SIDE IAW SRM 51-41-02. INSTALLED NEW SEAT RAIL RT FWD AT FS 424.00, FS 461 IAW AMM 53-01-11-400-802. CLEANED AND REMOVED SURFACE CORROSION IN SPOTS AT THE AFT SIDE SEAT RAIL RT IAW SRM 51-21-06. FOUND ONE SPOT IN AFT RAIL WITH CORROSION THAT IS OUT OF LIMITS. CUT AWAY CORRODED SECTION IN AFT SIDE SEAT TRACK 7" LONG AND REPLACED WITH EQUIVALENT SECTION IAW REO 601R-53-00-055. INSTALLED NEW SEAT RAIL AND AFT SEAT RAIL AT FS 424 TO FS 461.00 IAW AMM 53-01-11-400-802.

Part: FLOOR SUPPORT — CORRODED (BS 605-621) · airframe 29,789 hrs · 26,334 cycles

FLOORBEAM CAP AT RBL 9, FS 621 TO FS 605 HAS MINOR CORROSION. REMOVED CORROSION ON FLOORBEAM CAP AT RBL 9 BETWEEN FS 605 AND FS 621 IAW SRM 51-21-06. CORROSION FOUND TO BE OUT OF REPAIRABLE LIMITS AND FLOORBEAM CAP REQUIRES REPLACEMENT. REPLACE FLOORBEAM CAP AT RBL 9 BETWEEN FS 569 AND FS 621. REMOVED FLOORBEAM CAP AT RBL 9 BETWEEN FS 569 AND FS 621 IAW SRM 51-42-06 AND SRM 51-42-21. FLOORBEAM CAP AT RBL 9 BETWEEN FS 569 AND FS 621 NEEDS DRILLED AND INSTALLED. INSTALLED NUTPLATES ON FLOORBEAM CAP IAW SRM 51-45-00 AND SRM 51-42-06. LOCATED AND INSTALLED BLIND NUTS ON FLOORBEAM CAP RBL 9 IAW SRM 51-42-34. FLOORBEAM CAP AT RBL 9 BETWEEN FS 569 AND FS 621 NEEDS DRILLED TO ACFT AND INSTALLED.

Part: FLOOR SUPPORT — CORRODED (BS 605-621) · airframe 29,789 hrs · 26,334 cycles

FLOORBEAM CAP AT LBL 9, FS 621 TO FS 605 HAS MINOR CORROSION. FURTHER INVESTIGATION, FOUND THE CORROSION BEYOND ALLOWABLE LIMITS IAW SRM 51-21-06. REMOVED FLOORBEAM CAP IAW SRM 51-42-06 AND 51-42-21. NEW FLOOR BEAM CAP REQUIRES DRILLING AND INSTALLATION. LOCATED AND DRILLED NEW SERVICEABLE BEAM CAP AT LBL 9 F.S. 621 TO 605 IAW SRM 51-40-11. BEAM CAP REQUIRES FINAL REAM COUNTERSUNK, DEBURRED, AND INSTALLED. REAMED, COUNTERSUNK AND DEBURRED BEAM CAP IAW SRM 51-40-11. FLOORBEAM CAP REQUIRES INSTALLED. INSTALLED FLOOR BEAM CAP FASTENERS AT LOCATION A AND LOCATION B IAW EC/TC REO 601R-53-61-3400 AND AT SPLICE SIDES AND FLANGES. REMAINING FASTENERS BETWEEN FS 621 AND FS 618 REQUIRE INSTALL. INSTALLED REMAINING FASTENERS AT LBL 9, FS 621-569 IAW REO 601R-53-61-3679 STEPS 3, 4, 5, 6 & 7. PAINTED FASTENERS IAW SRM 51-25-01. EC/TC REQUIRES TO BE COMPLIED WITH.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 29,789 hrs · 26,334 cycles

CABIN FLOOR STRUCTURE AT PASSENGER DOOR HAS CORROSION. REMOVED BRACKETS AND CLEATS AT PAX DOOR IAW SRM 51-40-11. FOUND THEM TO BE CORRODED BEYOND ALLOWABLE LIMITS IAW SRM 51-21-06. REMOVED FLOOR SUPPORT ANGLE AT PAX DOOR FS 310-349. REMOVED CORROSION ON FLOOR SUPPORT ANGLE. FOUND TO BE WITHIN LIMITS, MAX DEPTH .005" (ANGLE .063"). INSTALLED SERVICEABLE FLOOR SUPPORT ANGLE AND 2 NEW SERVICEABLE BRACKET AND CLEATS AT PAX DOOR FLOOR STRUCTURE IAW SRM 51-42-06/51-21-06. SEALED CABIN FLOOR STRUCTURE AT PAX DOOR IAW SRM 51-23-00. APPLIED PROTECTIVE PAINT IAW SRM 51-25-00.

Part: POST — CRACKED (BS 409) · airframe 29,789 hrs · 26,334 cycles

FOUND FS 409.0+128 VERTICAL POST BL0.0 LT SIDE HAS INDICATION NOTED APPROX .3" IN LENGTH 80 PERCENT FSH AT WL 60.0 AFT FLANG RADIUS FAILED NDT INSP. REMOVED VERTICAL POST NR FS 409.0+128 BL 0.0 IAW SRM 51-42-06. FABRICATED REPLACEMENT POST AND REINFORCEMENT IAW REO 601R-53-31-697 AND SRM 51-24-21. REF DWG NR 601R32208. VERTICAL POST INSTALLED IAW EC/TC REO 601R-53-41-889 AND MET ALL THE REQUIREMENTS OF REO 601R-53-41-889 REV A EC/TC REQUIRE FOR REO'S 601R-53-31-687 AND 601R-53-41-1213 REV.A. COMPLIED WITH EC/TC REO 601R-53-31-097 AND REO 601R-53-31-697.

Part: PRESSURE PANEL — CRACKED (BS 460) · airframe 29,789 hrs · 26,334 cycles

FOUND FS 460 PRESSURE FLOOR HAS INDICATION NOTED BETWEEN BL 0.0 TO LBL 9.0 FWD OF INTERCOSTAL 2.7" IN LENGTH 70 PERCENT FSH. FAILED NDT INSPECTION. INDICATION MARKED ON ACFT. REPAIR FOR THE PRESSURE FLOOR WEB AT FS 464.00 ON ACFT SN 7203 IS COMPLETED IAW REO 601R-53-41-1217 AND MEETS ALL IT'S REQUIREMENTS.

Part: FLOOR SUPPORT — CORRODED (BS 621-574) · airframe 29,789 hrs · 26,334 cycles

FLOOR SUPPORT CAP AT LBL 27 FROM FS 621 TO FS 574 IS CORRODED. REMOVED FLOOR SUPPORT CAP IAW SRM 51-42-06 AND SRM 51-42-13. LOCATED AND DRILLED NEW SERVICEABLE FLOOR SUPPORT CAP IAW SRM 51-40-11. INSTALLED FLOOR SUPPORT CAP IAW SRM 51-42-22, 51-42-06, 51-42-34 & 51-42-21. C/W EC/TC REO 601R-53-61-3400 IAW REO 601R-53-61-3400, REV F.

Part: INTERCOSTAL — CRACKED (BS 484) · airframe 29,789 hrs · 26,334 cycles

INTERCOSTAL FS 484, LBL 27.00 - 36.00 ARE CRACKED (CLIPS). REPAIR TO THE INTERCOSTALS AT FS 484 BETWEEN LBL 27 AND LBL 36 IS COMPLETED IAW REO 601R-53-41-059 AND MEETS WITH ALL THEIR REQUIREMENTS.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 29,789 hrs · 26,334 cycles

FLOOR SUPPORT ANGLE AFT OF FS 280 IS CRACKED AT LBL 9.0. C/W EC/TC 601R-53-11-171 AND MET ALL REQUIREMENTS OF REO 601R-53-11-171. EC/TC REQUIRED FOR REO 601R-53-11-1901. COMPLIED WITH EC/TC REO 601R-53-11-1901 AND REO 601R-53-11-1901 REV A.

Part: INTERCOSTAL — CRACKED (BS 484) · airframe 29,789 hrs · 26,334 cycles

INTERCOSTAL FS 484, RBL 27.00 - 36.00 ARE CRACKED (CLIPS). REPAIR TO THE INTERCOSTALS AT FS 484 BETWEEN RBL 27.0 AND RBL 36.0 IS COMPLETED IAW REO 601R-53-41-059 AND MEETS WITH ALL THEIR REQUIREMENTS.

Part: SKIN — CRACKED (LT WING 148.019) · airframe 29,789 hrs · 26,334 cycles

LEFT LOWER WING PLANK AFT SPAR AREA AT WS 148.019 HAS VISUAL CRACK INDICATION, APPROX .5". C/W EC/TC EO 600-57-134 C/W. REO 601R-57-21-1294 REQUIRES A EC/TC. LT WING LOWER WING PLANK AT WS 148.019 REQUIRES FUEL LEAK CHECK. FUEL LEAK CHECK GOOD IAW MM 28-11-00-790-802. REO 601R-57-21-12 REQUIRES A EC/TC. DEVIATION TO GENERAIC REO 601R-57-21-130 REV H IS COMPLETED IAW REO 601R-57-21-1294 AND MEETS WITH ALL ITS REQUIREMENTS.

Part: FLASHLIGHT — WEAK (CABIN) · airframe 29,789 hrs · 26,334 cycles

CAPTAINS & F/O FLASHLIGHTS DIM. REPLACED BOTH FLASHLIGHT BATTERIES IAW 200 AMM 25-61-00. (CLOSED)

Part: INVERTER — FAILED (EMERGENCY LIGHTS) · airframe 29,283 hrs · 25,773 cycles

R & R NR 3 INVERTOR IAW AMM 33-51-07. OPS CHK GOOD. R & R NR 3 INVERTOR IAW AMM 33-51-07. OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (RT OVERWING) · airframe 29,284 hrs · 25,773 cycles

RIGHT OVERWING EMERGENCY FLOOR LIGHT INOP.

Part: BULB — FAILED (EMERGENCY LIGHTS) · airframe 29,216 hrs · 25,704 cycles

R & R LT FWD (FS 302.40L) EXTERNAL LIGHT BULB IAW AMM 33-51-21 OPS CK GOOD. 01-01-2010, ITEM: 1 R & R LT FWD (FS 302.40L) EXTERNAL LIGHT BULB IAW AMM 33-51-21, OPS CK GOOD 01-01-2010. (CLOSED)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,216 hrs · 25,704 cycles

LT FWD MOST EXTERNAL EMERGENCY LIGHT INOP.

Part: PLACARD — DETERIORATED (CABIN) · airframe 29,084 hrs · 25,560 cycles

PAX DOOR EXIT, OPEN AND ARROW PLACARD DETERIORATED.

Part: DOOR — STUCK (MAIN PAX) · airframe 28,910 hrs · 25,372 cycles

F/A REPORTS THAT THE MAIN PASSENGER DOOR IS DIFFICULT TO OPEN.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 28,598 hrs · 25,028 cycles

AFTER TAKEOFF, PULLED GEAR HANDLE UP, RECEIVED "GEAR DISAGREE" RED WARNING MSSG, COMPLIED WITH QRH, RETURNED TO ATL. UPON LANDING CLEARING 27R RECEIVED "HYD3 HI TEMP" MSSG AND LOSS OF NOSE WHEEL STEERING. COMPLIED WITH QRH, TOW TEAM PULLED AIRCRAFT INTO GATE. AIRCRAFT RETURNED TO ATL AFTER TAKEOFF. EMERGENCY DECLARED.

Part: PLACARD — DETERIORATED (PAX DOOR) · airframe 28,215 hrs · 24,653 cycles

PAX DOOR EXIT PLACARD DETERIORATED.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 28,040 hrs · 24,481 cycles

AFTER TO NOSE DISAGREE WARNING FOLLOWED QRH LANDED BACK ATL [EMERGENCY DECLARED]. FLT 5616 DEL 133 MINS

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,816 hrs · 24,251 cycles

SIDE WALL CABIN RT SIDE EMERGENCY LIGHT BURNED OUT BY OVERWING EXIT.

Part: DOOR — STUCK (PAX DOOR) · airframe 26,929 hrs · 23,458 cycles

PAX DOOR COULD NOT BE OPENED BY F/A AT THE END OF THE FLIGHT.

Part: DOOR — BINDING (SERVICE DOOR) · airframe 26,924 hrs · 23,454 cycles

CATERING REPORTS GALLEY SERVICE DOOR WILL NOT OPEN FROM OUTSIDE.

Part: DOOR — JAMMED (PAX DOOR) · airframe 26,917 hrs · 23,447 cycles

PASSENGER BOARDING DOOR JAMS CLOSED AND LOCKED AT TIMES IS TO UNLOCK AND OPEN FROM BOTH INSIDE AND OUTSIDE. FLT 5276 DEL 59 MINS.

Part: MECHANISM — FAULTY (PAX DOOR) · airframe 26,886 hrs · 23,421 cycles

PASSENGER AIRSTAIR DOOR LATCHING MECHANISM IS EXTREMELY HARD TO ACTUATE.

Part: DOOR — BINDING (PAX DOOR) · airframe 26,821 hrs · 23,358 cycles

CABIN ENTRY DOOR DIFFICULT TO OPEN FROM INSIDE.

Part: WARNING SYSTEM — ACTIVATED (PAX DOOR) · airframe 26,794 hrs · 23,335 cycles

PAX DOOR OUT HANDLE CAUTION DOOR VERY DIFFICULT TO OPEN. FLT 4919 DEL 26 MINS.

Part: CAM — LACK OF LUBE (PAX DOOR) · airframe 26,255 hrs · 22,856 cycles

MAIN CABIN DOOR WILL NOT OPEN FROM INSIDE. FLT 4251 DEL 37 MINS LUBED MAIN CABIN DOOR CAMS IAW AMM 12-20-52 OPS CHECK GOOD. (B)

Part: HANDLE — LACK OF LUBE (SERVICE DOOR) · airframe 26,228 hrs · 22,834 cycles

DOOR HANDLE RELEASE BUTTON ON SERVICE LUBE DOOR HANDLE IAW AMM 52-00 AC OK FOR SERVICE (B)

Part: HANDLE — LACK OF LUBE (PAX DOOR) · airframe 26,228 hrs · 22,834 cycles

PAX DOOR NOT CLOSING PROPERLY. GREEN ALIGNMENT MARKS WILL NOT ALIGN WITHOUT MOVING HANDLE WITH GREAT FORCE LUBE DOOR HANDLE IAW AMM 52-00 AC OK FOR SERVICE.

Part: DOOR — STUCK (SERVICE DOOR) · airframe 26,158 hrs · 22,777 cycles

CATERING ADVISED, CANNOT OPEN SERVICE DOOR FROM OUTSIDE. CLEANED AND LUBED SERVICE DOOR HANDLE. OPS CHECK AFTER SEVERAL CYCLES. REF CRJ200 AMM 52-41-03. (S)

Part: LATCH — OUT OF RIG (PAX DOOR) · airframe 26,158 hrs · 22,777 cycles

PASSENGER DOOR WILL NOT CLOSE WHILE UTILIZING OUTER HANDLE. INSPECTED PASSENGER DOOR AND FOUND THE FWD PULL IN LEVER TO BE HITTING THE FACE OF THE FWD DOOR CAM. REMOVED DOOR PANEL 832AL, REMOVED FWD PULL IN LEVER P/N 600-31689-36. INSTALLED NEW SERVICEABLE PULL IN LEVER P/N 600-31089-36 IAW S/B 601R-52-111. RIG THE DOOR LATCH MECHANISM. (S)

Part: ARM — CORRODED · airframe 26,144 hrs · 22,764 cycles

PANEL 196AR BOTTOM HINGE ARM CORRODED SEVERELY. REMOVED BOTTOM HINGE ARM IAW ASA SRM 51-42-21 AND ASSEMBLED NEW HINGE ARM USING P/N 601R35323-279 IAW ASA SRM 51-42-06. INSTALLED NEW HINGE ARM ON PANEL 196AR IAW CRJ 200.

Part: BULKHEAD — CRACKED (BS 559) · airframe 26,144 hrs · 22,764 cycles

FS 559 BULKHEAD WEB AND CAP ANGLE HAS INDICATIONS NOTED IN WEB RBL 9.00 WL 58.70 APPROX .4 INCH IN LENGTH. RBL 18.0 WL 58.70 APPROX 1.7 INCH IN LENGTH, AND CAP ANGLE LBL 18.00 AND RBL 18.0 IN RADIUS APPROX .5 INCH IN LENGTH FAILED NDT INSP. REPAIRED FS 559 BULKHEAD WEB AND CAP ANGLES FROM LBL 18 AND LBL 9, RBL 18 AND RBL 9 IAW REO 601R-53-41-260 REV B. REQUIRES SEALANT AND PAINT. SEALED FS 559 IAW CRJ 200 MM 51-23-00-390-809. PAINTED IAW CRJ SRM 51-25-01. COMPLIED WITH REO 601R-53-41-260. SUPPLEMENTAL SDR CLOSED 6/24/08.

Part: SEAT TRACK — CORRODED (BS 290-559)

SEAT RAIL AT RBL 9 FS 290 TO 559 HAS AREAS OF CORROSION. BLENDED CORROSION TO REMOVAL IAW CRJ200 SRM 51-21-06. DEPTH OF BLEND RANGED FROM 0.001" TO 0.008". 390 AND 409+128 AREAS STILL NEED CORROSION REMOVED. REMOVED CORROSION FROM FS 390 TO 409+128. DEPTH RANGED FROM .001 TO.008 WHICH IS WITHIN REPAIRABLE LIMITS IAW SRM 53-21-4. DAMAGE WAS REMOVED IAW 51-21-06 AND UPON INVESTIGATION FOUND ITEM 2 TO BE WITHIN REPAIRABLE LIMITS OF SRM 53-21-49. NEEDS ALODINE. APPLIED ALODINE IAW CRJ200 SRM 53-21-49. (A)

Part: CHANNEL — CRACKED (CARGO DOOR) · airframe 26,144 hrs · 22,764 cycles

CARGO DOOR FWD TRACK BOTTOM U CHANNEL IS CRACKED 1/4" LONG AT BOTTOM I/B RIVET. REMOVED CRACKED IAW SRM 51-42-06. LOCATED FASTENER HOLES IN NEW PART AND INSTALLED IAW SRM 51-40-11 AND 51-42-06. J. (B)

Part: SEAT TRACK — CORRODED (BS 290-559) · airframe 26,144 hrs · 22,764 cycles

SEAT RAIL AT RBL 9 F.S. 290 TO 559 HAS AREAS OF CORROSION. OPEN (B)

Part: SEAT TRACK — CORRODED (BS 290-559) · airframe 26,144 hrs · 22,764 cycles

SEAT RAIL AT RBL 9 FS 290 TO 559 HAS AREAS OF CORROSION. BLENDED CORROSION TO REMOVAL IAW SRM 51-21-06. DEPTH OF BLEND RANGED FROM 0.001" TO 0.008". 390 AND 406+128 AREAS STILL NEED CORROSION REMOVED. REMOVED CORROSION FROM FS 390 TO 406+128. DEPTH RANGED FROM .007 TO .008 WHICH IS WITHIN REPAIRABLE LIMITS IAW SRM 53-21-49. DAMAGE WAS REMOVED IAW 51-21-06 AND UPON INVESTIGATION FOUND TO BE WITHIN REPAIRBALE LIMITS OF SRM 53-21-49. 4. NEEDS ALODINE. APPLIED ALODINE IAW CRJ 200 SRM 53-21-49. (A)

Part: STIFFENER — CRACKED (BS 409) · airframe 26,144 hrs · 22,764 cycles

FS 409+128 BULKHEAD VERTICAL STIFFENER BEAM AT LBL 9 CRACKED AT OUTBOARD SIDE LOWER RADIUS APPROX 1/4" LONG. REMOVED 2 CLAMPS FROM HYD LINES AT LBL 9 OUTBD TO ACCESS FOR REPAIR IAW SRM 51-41-02. REPAIRED IAW REO 601R-53-41-237 AND REO 601R-53-41-237. REINSTALLED 2 CLAMPS ON HYD LINE AT LBL 9 IAW AMM 20-22-01-220-801. (B)

Part: STIFFENER — CRACKED (BS 409) · airframe 26,144 hrs · 22,764 cycles

FS 409.0+128 BULKHEAD VERTICAL STIFFENER BEAM AT LBL 27 AT INBOARD SIDE CRACKED APPROX 1/4" LONG AT BOTTOM FASTENER. (B) COMPLIED WITH REPAIR IAW REO 601R-53-41-056 AND REO 601R-53-41-056. (A)

Part: STIFFENER — CRACKED (BS 409 BULKHEAD)

FS 409.0+128 BULKHEAD VERTICAL STIFFENER BEAM AT RBL 27 CRACKED AT INBOARD SIDE AT BOTTOM RADIUS APPROX 1/4" LONG. COMPLIED WITH REPAIR OF BULKHEAD VERTICAL STIFFENER AT RBL 27 IAW REO 601R-53-41-056 AND REO 601R-53-41-056.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 26,144 hrs · 22,764 cycles

REAR PRESSURE BULKHEAD WEB HAS AN INDICATION NOTED APPROX 1.1 INCH IN LENGTH AT WL 108 RBL 36.20. FAILED NDT INSPECTION 50 PERCENT. REPAIRED REAR PRESSURE BULKHEAD WEB AT WL 108 AND RBL 36.20 IAW REO 601R-53-61-2678. COMPLIED WITH EC/TC REO 601R-53-61-2678 IAW BOMBARDIER REO 601R-53-61-2678.

Part: STIFFENER — CRACKED (BS 409) · airframe 26,144 hrs · 22,764 cycles

FS 409.0+128 BULKHEAD VERTICAL STIFFENER BEAM AT RBL 18 CRACKED AT OUTBOARD SIDE BOTTOM FASTENER APPROX .25 INCH LONG. COMPLIED WITH REPAIR OF FS 409 + 128 BULKHEAD VERTICAL STIFFENER AT RBL 27 IAW ASA CARD: REO 601R-53-41-056 AND BOMBARDIER REO601R-53-41-056. (B)

Part: STIFFENER — CRACKED (BS 409) · airframe 26,144 hrs · 22,764 cycles

FS 409.0+128 BULKHEAD VERTICAL STIFFENER BEAM AT LBL 18 CRACKED AT OUTBOARD SIDE LOWER RADIUS APPROX 1/2" LONG. (B) REPAIRED BULKHEAD VERTICAL STIFFENER IAW REO 601R-53-41-056 & REO 601R-53-41-056. (A)

Part: STIFFENER — CRACKED (BS 406) · airframe 26,144 hrs · 22,764 cycles

FS 406+128 BULKHEAD VERTICAL STIFFENER BEAM AT RBL 36 CRACKED AT INBOARD SIDE BOTTOM FASTENER APPROX 1/4" LONG. PERFORMED REPAIR IAW REO 601R-53-41-189 AND REO 601R-53-41-476. (A)

Part: SUPPORT BEAM — CRACKED (FUSELAGE) · airframe 26,144 hrs · 22,764 cycles

CARGO DOOR SUPPORT BEAM LOWER ANGLE IS CRACKED APPROX 1.5" IN LENGTH. REMOVED CRACKED ANGLE AND INSTALLED NEW SERVICEABLE PART IAW SRM 51-42-21. (B)

Part: VERTICAL BEAM — CRACKED (BS 409)

FS 409.0+128 BULKHEAD VERTICAL STIFFENER BEAM AT LBL 18 CRACKED AT OUTBOARD SIDE LOWER RADIUS APPROX .5 INCH LONG. REMOVED BRACKET ASSY P/N 601R96611-057 FROM LBL 18 TO LBL 27 POST TO GAIN ACCESS TO AREA CRACKS IAW SRM 51-42-06. VERTICAL POST REQUIRES REPAIR. COMPLIED WITH REPAIR OF FS 409.0+128 BULKHEAD VERTICAL STIFFENER AT LBL 18 IAW REO 601R-53-41-056 AND REO 601R-53-41-059. BRACKET ASSEMBLY REQUIRES REINSTALLED. REINSTALLED BRACKET ASSEMBLY ON LBL 18 LBL 27 IAW SRM 51-42-06. ASA RII COMPLIED WITH. (A)

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 26,144 hrs · 22,764 cycles

REAR PRESSURE BULKHEAD WEB THAT SURROUNDS THE LINTEL ATTACHMENT FITTING HAS AN INDICATION NOTED APPROX .2 INCH IN LENGTH 100PERCENT. FAILED NDT INSPECTION. REPAIR REAR PRESSURE BULKHEAD IAW REO 601R-53-61-1230, REV D. REPAIR PER EC/TC REO 601R-53-61-1230 HAS BEEN COMPLETE.

Part: SKIN — CRACKED (BS 732 S10-11R) · airframe 26,144 hrs · 22,764 cycles

FUSELAGE SKIN IS CRACKED AT RT FS 732 2.5L BETWEEN STR 10 &11 AND CHAFING DAMAGE FROM CONTACT WITH T/E PYLON BETWEEN FS 700.00 AND FS 755.00 BETWEEN S9-12. (B) REPAIRED SKIN IAW REO 601R-53-61-268 REV A NOTES 1-16. COMPLIED WITH REO 601R-53-61-268 AND COMPLETED ALL REQUIRED FORMS. (A)

Part: BULKHEAD — CRACKED (BS 202) · airframe 26,144 hrs · 22,764 cycles

202.75 PRESSURE BULKHEAD IS CRACKED AT LOWER LT CORNER 1.0" ABOVE AND 1.0" BELOW CUTOUT FOR PARKING BRAKE CABLE. COMPLIED WITH REO 601R-53-11-1412, INSTALLED SERVICEABLE INSULATION BLANKETS IAW AMM 25-81-01-400-801. COMPLIED WITH EC/TC REO 601R-53-11-1412 IAW REO 601R-53-11-1412. (A)

Part: FITTING — LACK OF LUBE (PAX DOOR) · airframe 2,610,751 hrs · 22,735 cycles

PSG DOOR STUCK AND WOULD NOT OPEN UPON ARRIVAL INTO SHV. LUBED AND CLEANED SHOOT DOOR FITTINGS AND PERFORMED OPS CK ON ASD IAW CRJ200 AMM 12-20-52 AND CRJ200 AMM 52-11-00. OPS CK GOOD A/C OK FOR SERVICE. [SDR CLOSED]

Part: BPSU — INOPERATIVE (TE FLAPS) · airframe 26,107 hrs · 22,735 cycles

FLAPS FAIL MSG WHEN SELECTING FLAPS FROM 20 DEG TO 30 DEG FLAPS FAILED AND 20 DEG. REMOVED AND REPLACED RT FLAPS BPSU ASSY AND FECU ASSY IAW AMM 21-51-10 AND 21-51-05. OPS CHECK GOOD. (B)

Part: DOOR — BINDING (SERVICE DOOR) · airframe 25,907 hrs · 22,571 cycles

SERVICE DOOR HARD TO OPEN FROM OUTSIDE.

Part: PLATE — BROKEN (EMERGENCY LIGHT) · airframe 25,863 hrs · 22,531 cycles

FORWARD EMERGENCY FLOODLIGHTS BASE PLATE BROKEN AT ENTRYWAY.

Part: LIGHT — BROKEN (CABIN) · airframe 25,804 hrs · 22,489 cycles

EMERGENCY LIGHT ON LEFT WALL ENTRANCE IS BROKEN. FLT 4247 DEL 84 MINS.

Part: PUMP — MALFUNCTIONED (HYDRAULIC SYS) · airframe 25,467 hrs · 22,210 cycles

HYD PUMP 2B FAILED ON SHORT FINAL INTO ATL. SWITCH WAS CYCLED AND 2B PUMP STARTED WORKING. EMERGENCY DECLARED.

Part: HANDLE — STUCK (PAX DOOR) · airframe 24,965 hrs · 21,799 cycles

MAIN PAX DOOR WILL NOT LATCH FROM INSIDE OR OUTSIDE A/C. JAMMED ITSELF TRYING TO STOW OUTER HANDLE.

Part: DOOR — STUCK (MAIN PAX) · airframe 24,907 hrs · 21,753 cycles

MAIN CABIN DOOR VERY DIFFICULT TO OPEN FROM THE OUTSIDE.

Part: DOOR — STUCK (MAIN PAX) · airframe 24,907 hrs · 21,753 cycles

F/A AND GROUND PERSONNEL HAD DIFFICULTY OPENING BOARDING DOOR.

Part: DOOR — STICKING (MAIN PAX) · airframe 24,576 hrs · 21,490 cycles

PAX DOOR DIFFICULT TO OPEN FROM INSIDE.

Part: DOOR — STIFF (MAIN PAX) · airframe 24,576 hrs · 21,490 cycles

FLIGHT ATTENDANT REPORTS, PAX DOOR DIFFICULT OPEN FROM INSIDE.

Part: DOOR — BINDING (PAX DOOR) · airframe 24,338 hrs · 21,287 cycles

MAIN CABIN DOOR WILL NOT OPEN. FLT 4728 DEL 70 MINS.

Part: DOOR — BINDING (PAX DOOR) · airframe 24,254 hrs · 21,221 cycles

MAIN PASSENGER DOOR IS VERY HARD TO OPEN. T-HANDLE FEELS LIKE IT POPS OUT BUT THE HANDLE CANNOT BE TURNED FROM OUTSIDE OR THE LEVER HANDLE RAISED INSIDE THE AIRCRAFT.

Part: HANDLE — BINDING (PAX DOOR) · airframe 24,192 hrs · 21,174 cycles

F/A REPORTS PAX DOOR DIFFICULT TO OPEN. HANDLE FEELS AS IF IT'S BINDING TOWARDS TOP OF TRAVEL LIMIT.

Part: DOOR — BINDING (AIRSTAIR DOOR) · airframe 23,983 hrs · 21,021 cycles

AIRSTAIR DOOR VERY HARD TO OPEN.

Part: UNKNOWN — BINDING (PAX DOOR) · airframe 23,788 hrs · 20,856 cycles

F/A REPORTS, PAX DOOR IS HARD TO OPEN.

Part: DOOR — STIFF (MAIN PAX) · airframe 23,758 hrs · 20,833 cycles

FA REPORTS CABIN ENTRANCE DOOR DIFFICULT TO OPEN.

Part: FLAP SYSTEM — FAILED (TE FLAPS) · airframe 23,448 hrs · 20,588 cycles

FLAPS FAIL AT ZERO OUT OF 20,000 FT, WITHOUT TOUCHING FLAPS AT ALL. LANDING IN SBN NO PROBLEM, VERY SOFT LANDING. EMERGENCY EQUIPMENT ON STANDBY AS A PRECAUTION.

Part: FLAP SYSTEM — WARNING LIGHT (TE FLAPS) · airframe 23,448 hrs · 20,588 cycles

LEVEL AT 3,000' IN PATTERN AT MDT AT 200 KNOTS, RECEIVED FLAPS FAIL MSG AT 0 DEG, FOLLOWED QRH AND LANDED IN MDT. "FLAP HANDLE WAS NOT MOVED OUT OF 0 DEG OR TOUCHED". EMERGENCY EQUIPMENT ON STANDBY AS A PRECAUTION.

Part: FLAP — FAILED (WING) · airframe 23,356 hrs · 20,519 cycles

FLAPS FAIL AT ZERO. EMERGENCY DECLARED.

Part: FLAP — FAILED (WING) · airframe 23,356 hrs · 20,519 cycles

A -FLAPS FAIL- MSG ON APPR, A/S 155 KTS. LEFT FLAP INDICATED 39 DEG, RIGHT FLAPS INDICATED 38 DEG. EMERGENCY DECLARED.

Part: FLAP — MALFUNCTIONED (WING) · airframe 22,914 hrs · 20,185 cycles

FLAPS FAILED MSG FLAPS FAILED AT 0 WHEN FLAPS SELECT TO 8, LANDED WITH ZERO FLAPS. AS A PRECAUTION EMERGENCY EQUIP ON STANDBY.

Part: FLAP — MALFUNCTIONED (WING) · airframe 22,873 hrs · 20,157 cycles

FLAP FAIL ON ARRIVAL. EMERGENCY DECLARED.

Part: FLAP — FAILED (WING) · airframe 22,873 hrs · 20,157 cycles

ON APPROACH IN ROC, SELECTED FLAPS 8 AND FLAPS FAIL CAUTION MSG, FLAPS FAILED AT ZERO. C/W QRH AND DECLARED EMERGENCY, TOUCH DOWN SPEED AT BUF WAS 172 KNOTS, DIVERTED TO BUF. FLT 4249 CX ON 1/20/07.

Part: TRIM SYSTEM — DISCONNECTED (STABILIZER) · airframe 22,754 hrs · 20,066 cycles

STAB/MACH TRIM DISCONNECTED ON APPROACH. EMERGENCY DECLARED. FLT 4873 DEL 37 MINS.

Part: APU — ODOR (APU BAY) · airframe 22,027 hrs · 19,476 cycles

DURING DESCENT WITH APU OPERATING THE APU DOOR WENT TO INHIBIT CLOSED. THEN THERE WAS A SPIKE IN EGT WELL INTO THE RED WITH A STRONG BURNING SMELL.

Part: STEP — BROKEN (AIRSTAIR) · airframe 22,003 hrs · 19,457 cycles

LOWER AIRSTAIR STEP BROKEN.

Part: DOOR — MALFUNCTIONED (PAX DOOR) · airframe 21,677 hrs · 19,192 cycles

FA REPORTS MAIN CABIN DOOR IS DIFFICULT TO OPEN.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,419 hrs · 18,992 cycles

EMERGENCY LIGHTS NOT WORKING AT PANEL JUST FWD OF SERVICE DOOR, AT LOWER F/A STATION, AND FWD FLOOR STRIP IN CABIN.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 21,417 hrs · 18,989 cycles

CORROSION ON LT FLOOR LANDING AT FS 559+16 (MARKED)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 21,417 hrs · 18,989 cycles

RT SIDE PRESSURE FLOOR LANDING HAS CORROSION FROM FS 439 TO FS 544 (MARKED)

Part: CLIP — CRACKED (FUSELAGE) · airframe 21,417 hrs · 18,989 cycles

FS 280 CLIP CRACKED AT LBL 9.0 (IB) (MARKED). REMOVED AND REPLACED CLIP AT FS280 LBL 9.0 IAW SRM51-40-11. (CLOSED)

Part: PLATE — CORRODED (PAX DOOR) · airframe 21,417 hrs · 18,989 cycles

PAX DOOR AFT CABLE ANCHOR FITTING BASE PLATE CORRODED (MARKED). REMOVED AND REPLACED AFT ASD ANCHOR FITTING BASE PLATE IAW M/M 53. (CLOSED)

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 21,417 hrs · 18,989 cycles

CORROSION FOUND BETWEEN AT FS409+128 TO FS 559.00 AND LBL36 AND TO FLOOR STR.17L ( FLOOR WEATHER STRIPPING IS REQUIRED TO BE REMOVED AND CLEANED AREA TO INSPECT FURTHER POSSIBLE CORRODED AREAS)

Part: SILL — CORRODED (FUSELAGE) · airframe 21,417 hrs · 18,989 cycles

CARGO FLOOR PANEL AT FS 559+64 TO 621.00 CORROSION ON SILL STR 17R AROUND NUT PLATES NUT PLATE HOLES. REMOVED CORROSION AROUND NUTPLATES PER CRJ 200 SRM 51-21-06 BAT 23167 C/W REO 601R-53-00-167. REMOVED CORROSION AROUND NUTPLATES PER CRJ 200 SRM 51-21-06 BAT 23167 EC/TC REO 601R-53-00-167 COMPLIED WTIH (CLOSED)

Part: CLIP — CRACKED (FUSELAGE) · airframe 21,417 hrs · 18,989 cycles

FS 280 CLIP CRACKED AT RBL 9.0 (INBD) (MARKED) REMOVED AND REPLACED CRACKED CLIP AT FS280 RBL 9.0 INBOARD IAW SRM 51-40-11. (CLOSED)

Part: STRUCTURE — CORRODED (BS 260) · airframe 21,417 hrs · 18,989 cycles

CORROSION AROUND CAMLOCK RECPTACLES IN FLT COMPT FS 260 JUST AFT AND BELOW CENTER PEDESTAL. BLENDED CORROSION FOUND IN FLT COMP FS 260 BELOW CENTER PEDESTAL. FOUND WITHIN LIMITS NEEDS ALODINE PRIME AND PAINT. CORROSION BLENDED IAW CRJ 200 SRM 51-21-06 DK 7022603 ALODINED PRIMED AND PAINTED BLENDED AREA FS 260 JUST AFT AND BELOW CENTER PEDESTAL WRK DONE IAW CRJ 200 SRM 51-25-01 DK 7022603 (CLOSED)

Part: FLOORBEAM — CRACKED (BS 461) · airframe 21,417 hrs · 18,989 cycles

FLOORBEAM SUPORT BRACKET IB OF RBL 9 CRACKED AT FS 461. REMOVED SUPPORT FITTING AT OTBD. SIDE OF RBL 9.0 AT STA. 461, DRILLED UP NEW FITTING AND STARTED INSTALLING FASTNERS, REMOVED ACCESS PANEL THRU PRESS. FLOOR FOR ACCESS OF AFT END HORZ. FASTNERS REF. SRM 51-42-21 6/5/06 20423.FINISHED INSTALLING FASTNERS ON O/B SIDEOF RBL 9.0 AT STA. 461, REINSTALLED ACCESS PANELS THRU PRESSURE FLOOR IAW CRJ 200 SRM 51-42-21 06-06-06 JOB COMPLETED. (CLOSED)

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 21,417 hrs · 18,989 cycles

CORROSION AROUND CAMLOCK RECEPTACLES AT FS 280 BETWEEN LBL 9 AND RBL 9 (MARKED). DRILLED OUT FASTENERS AND REMOVED CORRODED ANGE AT FS280,PICKED UP EXISTING FASTENER HOLES IN NEW ANGLE, ALODINED AND INSTALLED ANGEL WET WITH SEALANT AND SOLID RIVETS PER THE CRJ SRM CHAPTERS 51-40-11 AND 51-42-00. JMP7016287FINISHED INSTALLING BLIND FASTENERS AND CAMLOCK RECEPTICLES ON COCKPIT FLOOR LAND AT 280 IAW SRM 51-42-06. SM17032 JOB COMPLETE (SUPPLEMENTAL SDR 6/22/2006) (SDR CLOSED)

Part: FRAME — CRACKED (FUSELAGE) · airframe 21,417 hrs · 18,989 cycles

FS 280 FRAME CRACKED AT LBL 11.0 AROUND ALT EXTENSION CABLE PULLEY BRACKET (MARKED).

Part: BRACKET — CRACKED (FUSELAGE) · airframe 21,417 hrs · 18,989 cycles

INTERCOSTAL AFT BRACKET CRACKED AT FS 484.00 AND LBL36 REMOVED AND REPLACE FS 484 LBL36 OTBD CLIP ALL WORK PER CRJ200, SRM51-42-12 JOB COMPLETED RI17912 (CLOSED)

Part: PLACARD — PEELING (CABIN) · airframe 21,103 hrs · 18,750 cycles

PAX DOOR EXIT PLACARD PEELING.

Part: POWER SUPPLY — MALFUNCTIONED (FUSELAGE)

DURING GROUND INSPECTIONS, THE AIRCRAFT`S EMERGENCY LIGHTS REMAINED ON WITH THE SWITCH IN THE OFF POSITION. MAINTENANCE REMOVED AND REPLACED THE BATTERY INVERTER AND THE BATTERY CHARGER. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)

Part: INVERTER — MALFUNCTIONED (FUSELAGE)

DURING GROUND INSPECTIONS, THE AIRCRAFT`S EMERGENCY LIGHTS REMAINED ON WITH THE SWITCH IN THE OFF POSITION. MAINTENANCE REMOVED AND REPLACED THE BATTERY INVERTER AND THE BATTERY CHARGER. OPERTIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)

Part: CHARGER — MALFUNCTIONED (FUSELAGE)

DURING GROUND INSPECTION, THE AIRCRAFT’S EMERGENCY LIGHTS REMAINED ON WITH THE SWITCH IN THE OFF POSITION. MAINTENANCE REMOVED AND REPLACED THE BATTERY INVERTER AND THE BATTERY CHARGER. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)

Part: STEP — BROKEN (PAX DOOR)

DURNG A GROUND INSPECTION, THE PASSENGER DOOR BOTTOM STEP RETRACTING HINGE LINKAGE WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. (K)

Part: DOOR — MALFUNCTIONED (MAIN PAX)

DURING A GROUND INSPECTION, THE FLIGHT ATTENDANT REPORTED THE PASSENGER DOOR STIFF TO OPEN AND CLOSE. MAINT OPERATED THE PASSENGER DOOR WITH NO DEFECTS NOTED. AIRCRAFT OK FOR SERVICE. (K)

Part: CABLE — UNSECURE (PAX DOOR)

FLT 4610 - DURING A GROUND INSPECTION IN ATL, THE PASSENGER DOOR WAS FOUND DIFFICULT TO OPEN. MAINTENANCE FOUND THE PASSENGER DOOR HANDRAIL PIN CABLE UNSECURED CAUSING IT TO STICK BETWEEN THE PASSENGER DOOR AND AIRFRAME. MAINTENANCE RESECURED THE PASSENGER DOOR HANDRAIL PIN CABLE. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: DOUBLER — CRACKED (FUSELAGE)

DURING AN A-CHECK IN BTR, THE FS 640 DOUBLER AT STRINGER 10, FRAME FS 640 AND THE SKIN BUTT JOINT STRAP LEFT FS 640, STRINGER 8-13 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE FS 640 DOUBLER AT STRINGER 10 AND THE FS 640 FRAME. MAINTENANCE IS REPAIRING THE SKIN BUTT JOINT STRAP LEFT, FS 640, STRINGER 8-13 IAW ASA EO 600-53-0107. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

FLT 4842 - DURING A GROUND INSPECTION IN ATL, THE FORWARD EMERGENCY LIGHTS WERE FOUND ILLUMINATING WITH THE EMERGENCY LIGHTS SWITCH IN THE OFF POSITION. MAINTENANCE REMOVED AND REPLACED THE NR 1 EMERGENCY LIGHTS BATTERY PACK. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LIGHT — MALFUNCTIONED (CABIN)

FLT 4158 - AFTER POWERING DOWN THE AIRCRAFT IN ATL, THE CREW REPORTED THAT THE EMERGENCY LIGHT REMAINED ON. THE CREW RESET THE CIRCUIT BREAKER TO THE EMERGENCY LIGHTS AND THE LIGHTS EXTINGUISHED. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: SCAVENGE PUMP — COKED (LT ENGINE)

DURING CLIMB-OUT, AT APPROXIMATELY 31,800 FT, THE CREW RECEIVED AN ENGINE OIL PRESSURE MASTER WARNING AND AURAL. THE QRH WAS COMPLIED WITH AND THE CREW SHUTDOWN THE LT ENGINE. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT DIVERTED, LANDING SAFELY. MAINTENANCE REMOVED AND REPLACED THE LT ENGINE LUBE SCAVENGE PUMP AND ALSO THE OIL PRESSURE TRANSDUCER IAW AMM 79-20-00. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE.

Part: DOUBLER — CRACKED (FUSELAGE)

DURING A C-CHECK, THE RT DOUBLER AT FS 640 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE RT DOUBLER AT FS 640.

Part: CLIP — CRACKED (FUSELAGE)

DURING A C-CHECK, THE IB AND OB CLIPS AT FS 484, LBL 27 AND LBL 36 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE IB CLIP AT FS 484, LBL 36 IAW EO 600-53-0098.

Part: STRINGER CLIP — CRACKED (FUSELAGE)

DURING A C-CHECK, THE OB CLIPS AT FS 625, STRINGER 15R WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE OB CLIP AT FS 625, STRINGER 15R IAW SRM 51-42-00.

Part: CLIP — CRACKED (FUSELAGE)

DURING A C-CHECK, THE IB AND OB CLIPS AT FS 484, RBL 27 AND RBL 36 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE IB CLIP AT FS 484, RBL 27 AND REPAIRING THE OB CLIP AT FS 484, RBL 36 IAW EO600-53-0098.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE)

DURING C-CHECK, THE LT AND RT FLOOR SUPPORT ANGLES AT FS 621 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE LT AND RT FLOOR SUPPORT ANGLES AT FS 621 IAW EO600-53-0105.

Part: SIGN — CRACKED (EMERGENCY EXIT)

DURING A C-CHECK, THE ENTRY WAY EMERGENCY EXIT LIGHT, JUST FORWARD OF THE PASSENGER DOOR, WAS FOUND TO HAVE THE COVERED CRACKED. MAINTENANCE REMOVED AND REPLACED THE CRACKED EMERGENCY EXIT LIGHT ASSEMBLY. OPERATIONAL CHECKS GOOD.

Part: SKIN PANEL — CRACKED (RT WING)

DURING A C-CHECK, THE RT WING PLANK AT APPROXIMATELY WS 148 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE RT WING PLANK AT APPROXIMATELY WS 148 IAW EO600-57-0134A.

Part: HANDLE — CRACKED (E/E BAY DOOR)

DURING A C-CHECK, THE MAIN AVIONICS BAY DOOR HANDLE WAS FOUND CRACKED AROUND THE BASE. MAINTENANCE IS REMOVING AND REPLACING THE MAIN AVIONICS BAY DOOR HANDLE.

Part: STEP — CRACKED (PAX DOOR)

DURING A C-CHECK, THE TOP STEP ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE IS REMOVING AND REPLACING THE TOP STEP ON THE PASSENGER DOOR.

Part: STEP — BROKEN (PAX DOOR)

FLT 4435 - 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 PASENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT)

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

Part: LAMP — BURNED OUT (EMERGENCY LIGHT)

DURING A GROUND INSPECTION, THE RT CENTER OVERWING EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE RELAMPED THE EXTERNAL OVERWING EMERGENCY LIGHT BULB. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: WARNING LIGHT — ILLUMINATED (TE FLAPS)

FLT 4586 - DURING APPROACH INTO LIT FROM DFW, THE CRWE RECEIVED A FLAPS FAIL MASTER WARNING WHEN THEY SELECTED THE FLAPS TO EIGHT DEGREES. THE QRH WAS COMPLIED WITH THE CREW REQUESTED EMERGENCY EQUIPMENT TO BE ON STANDBY AS A PRECAUTION. THE AIRCRAFT LANDED SAFELY IN LIT. MAINTENANCE RESET THE FLAP SYSTEM IAW AD98-20-01 AND ASA EO 600-27-0004. SYSTEM RESET AND OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: STEP — CRACKED (PAX DOOR)

DURING A HANGAR INSPECTION IN MCN, THE LOWER STEP ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE LOWER STEP ASSEMBLY ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LIGHT — INOPERATIVE (CABIN)

FLT 4629 - DURING A GROUND INSPECTION IN ATL, THE CREW FOUND THE EMERGENCY FLOOR LIGHTS AT ROWS 3 AND 4 C/D TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY FLOOR LIGHT STRIP AT ROWS 3/4 C/D. OPERATIONAL CHECKS GOOD. AIRCRAT OK FOR SERVICE. (M)

Part: CIRCUIT BREAKER — TRIPPED (EMERGENCY LIGHTS)

DURING HANGAR MAINTENANCE IN BTR, THE EMERGENCY LIGHTS REMAINED ON WHEN IN THE ARMED POSITION. MAINTENANCE RESET THE CIRCUIT BREAKER TO THE EMERGENCY LIGHTS. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

DURING A C-CHECK IN MCN, THE LEFT AND RIGHT FLOORBEAMS AT BL 27 IN THE SERVICE DOOR AREA WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE LEFT AND RIGHT FLOORBEAMS (P/N'S 601R53-037K1A AND 601R53-037K4A) AT BL 27 IN THE SERVICE DOOR AREA, IAW ASA EO 600-53-0052. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

DURING A C-CHECK IN MCN, THE LEFT AND RIGHT FLOORBEAMS AT BL 9 IN THE SERVICE DOOR AREA WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE LEFT AND RIGHT FLOORBEAMS (P/N'S 601R53-037K2A AND 601R53-037K3A) AT BL 9 IN THE SERVICE DOOR AREA, IAW ASA EO 600-53-0052. (M)

Part: ANGLE — CORRODED (FUSELAGE)

DURING A C-CHECK IN MCN, THE PASSENGER DOOR TOP STEP UPPER HINGE NUT PLATE ANGLE WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE PASSENGER DOOR TOP STEP UPPER HING NUT PLATE ANGLE IAW SRM 51-00. (M)

Part: HINGE — CORRODED (PAX DOOR)

DURING A C-CHECK IN MCN, THE UPPER HINGE AT THE TOP STEP OF THE PASSENGER DOOR WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE UPPER HINGE AT THE TOP STEP OF THE PASSENGER DOOR IAW SRM 51-00. (M)

Part: FLOORBEAM — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE FORWARD ATTACHING ANGLE ON THE RIGHT SIDE FLOORBEAM BELOW THE COCKPIT DOOR WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE FORWARD ATTACHING ANGLE ON THE RIGHT SIDE FLOORBEAM BELOW THE COCKPIT DOOR IAW SRM 51-00. (M)

Part: ANGLE — CORRODED (FUSELAGE)

DURING A C-CHECK IN MCN, THE LOWER METAL TRIM PANEL NUT PLATE ANGLE AT THE SERVICE DOOR ENTRANCE WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS REMOVING THE LOWER METAL PANEL NUT PLATE ANGLE AT THE SERVICE DOOR ENTRANCE IAW SRM 51-00. (M)

Part: SUPPORT BEAM — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE RIGHT ENGINE SUPPORT BEAM AT BL 36.20 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE RT ENGINE SUPPORT BEAM AT BL 36.20 IAW ASA EO 600-53-0070. (M)

Part: APU — SHUTDOWN (APU BAY)

FLT 4680 - DURING DESCENT INTO ATL AT APPROXIMATELY 13,000 FEET, THE AUXILIARY POWER UNIT SHUT ITSELF DOWN AUTOMATICALLY. THE CREW WAITED APPROXIMATELY TWO MINUTES AND RE-STARTED IT, AFTER WHICH THE ODOR OF FUEL OCCURRED IN THE COCKPIT AND CABIN. THE AIRCRAFT LANDED SAFELY IN ATL. MAINTENANCE CLEANED THE OIL PRESSURE SWITCH (P/N 3876001-6) CONNECTOR PLUG AND TIGHTENED THE FUEL LINE (P/N 3883449-1) ON THE FUEL CONTROL UNIT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: FRAME — CRACKED (FUSELAGE)

DURING HANGER MAINTENANCE, A CRACK WAS DISCOVERED ON FRAME 718 ON BOTH THE LEFT AND RIGHT SIDES. MAINTENANCE REPAIRED THE CRACKED FRAME IAW EO.

Part: SUPPORT — CRACKED (FUSELAGE)

DURING HANGER MAINTENANCE, THE LEFT ENGINE SUPPORT BEAM WAS FOUND TO BE CRACKED. MAINTENANCE REPAIRED THE CRACKED ENGINE SUPPORT BEAM IAW REO. THIS REO GIVES REPAIR SPECIFICATIONS FOR THE ENGINE SUPPORT BEAM CRACK, AS WELL AS OUTLINES A THRESHOLD OF CYCLES FOR THE PERMANENT REPAIR AND FOLLOW UP NDT INSPECTIONS. AIRCRAFT OK FOR SERVICE.

Part: LAMP — BURNED OUT (FUSELAGE)

DURING GROUND INSPECTION, AN EXTERNAL EMERGENCY LIGHT ON THE RIGHT HAND SIDE OF THE FUSELAGE WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BURNED OUT EMERGENCY LIGHT BULB. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE.

Part: WINDOW — CRACKED (COCKPIT)

FLT 4325 - DURING LANDING ROLL IN DHN, THE CAPTAINS LEFT SIDE WINDOW SHATTERED. MAINTENANCE REMOVED AND REPLACED THE SHATTERED LEFT SIDE PILOT WINDOW. A LEAK CHECK WAS PERFORMED, AND NO LEAKS WERE NOTED. AIRCRAFT RETURNED TO SERVICE. (M)

Part: WINDSHIELD — CRACKED (COCKPIT)

DURING DESCENT INTO DFW AT 25,000 FEET, THE FIRST OFFICERS WINDSHIELD CRACKED. AIRCRAFT LANDED IN DFW WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE RIGHT WINDSHIELD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SMOKE DETECTOR — MALFUNCTIONED (CARGO BAY)

FLT 4693 - DURING APPROACH INTO MYR FROM ATL, CREW HAD A CARGO SMOKE INDICATION LIGHT. CAPTAIN DECLARED AN EMERGENCY, BUT FIRE BOTTLES WERE NOT BLOWN. MAINTENANCE FOUND NO INDICATION OF CARGO FIRE. MAINTENANCE REMOVED AND REPLACED THE CARGO SMOKE DETECTOR. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BULB — FAILED (ROW 1AB)

DURING INSPECTION, EMERGENCY FLOOR BULB AT 1AB FOUND INOPERATIVE. MAINTENANCE REPLACED EMERGENCY LIGHTING SYSTEM BULB. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: ACTUATOR — MALFUNCTIONED (HORIZ STABILIZER)

ATL/ROA - FLT 7289 - DURING CLIMB-OUT, ELEVATOR TRIM WOULD NOT TRIM BELOW 3 UNITS DOWN. CONTROLABILITY IMPROVED WITH REDUCED AIRSPEED AND FLAPS. CREW DECLARED AN EMERGENCY AND RETURNED TO ATL, WHERE LANDING WAS MADE SAFELY AND WITHOUT FURTHER INCIDENT. ATL MAINTENANCE REMOVED AND REPLACED THE HORIZONTAL STABILIZER TRIM ACTUATOR. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RELEASED FOR FURTHER SERVICE.