N828AS

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHT) · airframe 34,498 hrs · 30,600 cycles

EMERGENCY FLOOR LEVEL FLOODLIGHT IS INOPERATIVE AT PAX DOOR. R & R TB 105-3 WITH SERVICEABLE DIODE BLOCK IAW ESPM 20-18-10. R & R BATTERY CHARGER PS2LF WITH SERVICEABLE UNIT IAW AMM 33-51-05-00-801 AND 33-51-05-400-8001. SDR CLOSED.

Part: STRAP — CORRODED (BS 559) · airframe 34,497 hrs · 30,598 cycles

NUT PLATE STRAP CORRODED AT RBL 27 TO FLOOR SUPPORT AT FS 559. BLENDED OUT CORROSION IAW REO 601R-53-51-203.

Part: SEAT TRACK — CORRODED (BS 349-409) · airframe 34,497 hrs · 30,598 cycles

SEAT TRACK LBL 9 AT FS 394 TO 409 + 128 CORRODED. FOUND CORRODED BEYOND LIMITS IAW SRM 53-21-49. REMOVED SEAT TRACK IAW AMM 53-01-11. FABRICATED REPLACEMENT SEAT TRACK IAW REO 601R-53-00-485. INSTALLED REPLACEMENT SEAT TRACK IAW AMM 53-01-11-400-802.

Part: FRAME — CORRODED (BS 473.15) · airframe 34,497 hrs · 30,598 cycles

RT FRAME INBD DOUBLER AT FS 473.15 HAS CORROSION LOCATED JUST BELOW LAST ROW OF RIVETS. REMOVED CORROSION IAW SRM 51-21-06. COMPLIED WITH REO 601R-53-41-1641.

Part: ATTACH ANGLE — CORRODED (BS 348) · airframe 34,498 hrs · 30,600 cycles

REMOVED CLIP FOR CORROSION REMOVAL AT FS 348. CORROSION REMOVED FROM CLIP, CLIP FOUND TO BE OUT OF LIMITS IAW SRM 53-21-43. DRILLED UP NEW CLIP IAW SRM 51-40-11-00, MP161880 11/18/12. INSTALLED NEW CLIP ALL WORK DONE IAW SRM 51-42-06. SDR CLOSED.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · airframe 34,498 hrs · 30,600 cycles

SERVICE DOOR SURROUND STRUCTURE CLIP AT FS 319.70 CORRODED. REMOVED CLIP AT FS 319.70 IAW SRM 51-42-06. INSTALLED NEW PART ALL WORK DONE IAW SRM 51-42-06 & 51-42-21. FORMED SERVICE DOOR SURROUND STRUCTURE CLIP IAW DWG 601R38303 AND SRM 51-24-21.

Part: SUPPORT ANGLE — CORRODED (BS 349) · airframe 34,497 hrs · 30,598 cycles

RT WINDSCREEN SUPPORT ANGLE AT FS 349 CORRODED. BLENDED SUPPORT ANGLE AND FOUND TO BE OUT OF LIMITS IAW SRM 53-21-43 ALLOWABLE DAMAGE. REMOVED RT SUPPORT ANGLE IAW SRM 51-42-06. INSTALLED NEW SUPPORT ANGLE IAW SRM 51-42-06-00 AND 51-42-13-00 AND 51-42-21-00.

Part: CHANNEL — CORRODED (PAX DOOR HINGE) · airframe 34,497 hrs · 30,598 cycles

CENTER HINGE CHANNEL FOUND TO BE CORRODED AT HINGE SIDE OF PAX DOOR. REMOVED PAX DOOR CENTER HINGE CHANNEL IAW SRM 51-42-06, 51-42-21. INSTALLED SERVICEABLE PAX DOOR CENTER HINGE CHANNEL IAW SRM 51-42-06, 51-42-21.

Part: ATTACH ANGLE — CORRODED (BS 349) · airframe 34,498 hrs · 30,600 cycles

SERVICE DOOR SURROUND STRUCTURE CLIP AT FS 349.00 CORRODED. FABRICATED AND INSTALLED NEW CLIP, IAW SNIEO 601R31148 S01.

Part: ANGLE — CORRODED (PAX DOOR) · airframe 34,497 hrs · 30,598 cycles

AFT PAX DOOR CORNER ASSY FOUND TO BE CORRODED ON HINGE SIDE. REMOVED AFT PAX DOOR CORNER ASSY IAW SRM 51-42-06, 51-42-21. INSTALLED SERVICABLE PAX DOOR AFT CORNER ASSY IAW SRM 51-42-06, 51-42-21.

Part: ANGLE — CORRODED (PAX DOOR) · airframe 34,497 hrs · 30,598 cycles

FIVE HINGE SIDE LT ANGLES FOUND TO BE CORRODED. R & R PAX DOOR ANGLES IAW SRM 51-42-06.

Part: ANGLE — CORRODED (PAX DOOR) · airframe 34,497 hrs · 30,598 cycles

FWD PAX DOOR CORNER ASSY FOUND TO BE CORRODED ON HINGE SIDE. REMOVED FWD PAX DOOR CORNER ASSY IAW SRM 51-42-06. INSTALLED SERVICABLE PAX DOOR FWD CORNER ASSY IAW SRM 51-42-06.

Part: ANGLE — CORRODED · airframe 34,498 hrs · 30,600 cycles

GALLEY SERVICE DOOR SILL PLATE COVER AFT NUTPLATE ANGLE CORRODED. FORMED AND INSTALLED GALLEY SERVICE DOOR SILL PLATE COVER AFT ANGLE IAW DWG 601R38695 AND SRM 51-24-21.

Part: SEAT TRACK — CORRODED (BS 349) · airframe 34,497 hrs · 30,598 cycles

RBL 9 SEAT TRACK CORRODED AT FRAME BS 349. REMOVED SEAT TRACK IAW AMM 53-01-11-000-802. FOUND TO BE CORRODED BEYOND LIMITS IAW SRM 51-21-06 AND 53-21-49. INSTALLED NEW SEAT TRACK IAW AMM 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 349) · airframe 34,497 hrs · 30,598 cycles

LBL 9 SEAT TRACK CORRODED AT FRAME BS 349. SEAT TRACK CORRODED BEYOND 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: ANGLE — CORRODED (PAX DOOR) · airframe 34,497 hrs · 30,598 cycles

PAX DOOR UPPER ATTACH RODS, SILL RETAINER ANGLES CORRODED. R & R THRESHOLD ANGLE FS 310 AND 349 IAW SRM 51-42-06 AND 51-42-13.

Part: FLOOR SUPPORT — CORRODED (BS 310) · airframe 34,497 hrs · 30,598 cycles

LEFT FLOOR SUPPORT CORRODED AT FRAME BS 310. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM TR 53-27. R & R FLOOR SUPPORT IAW SRM 51-42-06-00 AND 51-42-13-00.

Part: FITTING — CORRODED (AFT BULKHEAD) · airframe 34,497 hrs · 30,598 cycles

LIGHT CORROSION ON FITTING ON CARGO FLOOR AT LT SIDE AFT PRESSURE BULKHEAD. REMOVED CORROSION DAMAGE IAW SRM 51-21-06-00 FOUND FITTING/SPLICE TO BE OUT OF TOLERANCE IAW SRM 53-61-23-00. REMOVED FITTING/SPLICE IAW SRM 51-42-06-00 AND 51-42-21-00. INSTALLED NEW SPLICE FITTING IAW SRM 51-42-06. SDR CLOSED.

Part: STRAP — CORRODED (DOOR FRAME) · airframe 34,497 hrs · 30,598 cycles

PAX DOOR FRAME CUTOUT HAS CORROSION ON A STRAP UPPER AFT CORNER. R & R PAX DOOR FRAME UPPER AFT STRAP IAW DWG 600-31153 AND SRM 51-40-11 AND 51-42-20.

Part: CHANNEL — CORRODED (BS 559) · airframe 34,497 hrs · 30,598 cycles

NUT PLATE CHANNEL CORRODED AT BS 559.00 BETWEEN RBL 9 AND LBL 9. BLENDED NUTPLATE CHANNEL IAW SRM 51-21-06. AREAS BLENDED IN COMPLIANCE WITH REO 601R-53-51-203.

Part: FLOOR SUPPORT — CORRODED (BS 559) · airframe 34,497 hrs · 30,598 cycles

NUTPLATE CHANNEL CORRODED BETWEEN LEFT FLOOR SUPPORT AND LBL 27 AT FS 559.00. COMPLIED WITH REO 601R-53-51-203.

Part: FRAME — CORRODED (BS 349) · airframe 34,498 hrs · 30,600 cycles

FRAME BS 349.00 CORRODED AT STRINGER 17 RT. FRAME REPAIRED IAW REO 601R-53-21-2374 REV(P3).

Part: ANGLE — CRACKED (BS 280) · airframe 34,497 hrs · 30,598 cycles

ANGLE CRACKED AT BS 280 CROSSBEAM. FABRICATED NEW ANGLE IAW REO 601R-53-11-171. INSTALLED NEW ANGLE IAW SRM 51-42-06 & 51-42-20.

Part: FITTING — CORRODED (BULKHEAD) · airframe 34,497 hrs · 30,598 cycles

LIGHT CORROSION ON FITTING ON CARGO FLOOR AT LT SIDE AFT PRESSURE BULKHEAD. REMOVED FITTING/SPLICE IAW SRM 51-42-06-00 AND 51-42-21-00. INSTALLED NEW SPLICE FITTING IAW SRM 51-42-06. SDR CLOSED.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 34,497 hrs · 30,598 cycles

SEAT TRACK AT LBL 27 CORRODED BETWEEN FS 559+80 AND 559+96. REMOVED CORROSION FROM SEAT TRACK AND FOUND TO BE OUT OF LIMITS IAW SRM 51-21-06, 53-51-49 AND 53-21-49. R & R SEAT TRACK IAW AMM 53-01-11-000-802 AND 53-01-11-400-802.

Part: CARGO TRACK — CORRODED (BS 589-605) · airframe 34,497 hrs · 30,598 cycles

CARGO TRACK CORRODED AT LBL9 BETWEEN FS 605 AND FS 589. R & R CARGO TIE DOWN PLATE WITH SCREWS IAW SRM 51-41-02 & 51-41-04.

Part: CARGO TRACK — CORRODED (BS 589-874) · airframe 34,497 hrs · 30,598 cycles

CARGO TRACK CORRODED AT LBL9 BETWEEN FS874.00 AND 589.00. R & R CARGO TRACK IAW SRM 51-41-02 & 51-41-04.

Part: SEAT TRACK — CORRODED (BS 559-574) · airframe 34,497 hrs · 30,598 cycles

SEAT TRACK LBL 9 CORRODED BETWEEN FS 559+112 AND 574. BLENDED CORROSION AND FOUND TO BE OUT OF LIMITS MATERIAL LOSS .027 WITH MAXIMUM ALLOWABLE .020 IAW SRM 53-61-49 AND 51-21-06. REMOVED OLD TRACK AND INSTALLED NEW SEAT TRACK IAW SRM 53-61-42.

Part: FLOOR SUPPORT — CORRODED (BS 559-589) · airframe 34,497 hrs · 30,598 cycles

RT FLOOR SUPPORT PLATE CORRODED FROM FS 589 TO 559+112. REMOVED CORROSION FROM FLOOR SUPPORT PLATE IAW SRM 51-21-06.

Part: FLOOR SUPPORT — CORRODED (BS 559) · airframe 34,497 hrs · 30,598 cycles

LT FLOOR SUPPORT PLATE CORRODED BETWEEN FS 559+80 AND 559+112. REMOVED CORROSION FROM LT FLOOR SUPPORT PLATE IAW SRM 51-21-06 13 EA LOCATIONS.

Part: CARGO TRACK — CORRODED (BS 559-574) · airframe 34,497 hrs · 30,598 cycles

CARGO TRACK CORRODED AT LBL 27 BETWEEN FS 559+112 AND 574. R & R CARGO TRACK IAW SRM 51-41-02 & 51-41-04.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 34,497 hrs · 30,598 cycles

SEAT TRACK CORRODED AT LBL 9 BETWEEN FS 559+88 AND 559+96. REMOVED CORROSION FROM SEAT TRACK AND FOUND TO BE OUT OF LIMITS IAW SRM 51-21-06, 53-51-49 AND 53-21-49. R & R SEAT TRACK IAW AMM 53-01-11-000-802 AND 53-01-11-400-802.

Part: CARGO TRACK — CORRODED (BS 559) · airframe 34,497 hrs · 30,598 cycles

CARGO TRACK CORRODED AT LBL 27 BETWEEN FS 559+96 AND 559+112. R & R CARGO TRACK IAW SRM 51-41-02 & 51-41-04.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 34,497 hrs · 30,598 cycles

SEAT TRACK AT RBL 27 CORRODED BETWEEN FS 559+80 AND 559+96. BLENDED SEAT TRACK IAW SRM 51-21-06. FOUND TO BE OUT OF LIMITS IAW SRM 51-61-49. R & R SEAT TRACK IAW AMM 53-01-11-000-802 AND 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 559-574) · airframe 34,497 hrs · 30,598 cycles

SEAT TRACK CORRODED AT RBL 9 BETWEEN FS 559+112 AND 574. BLENDED SEAT TRACK IAW SRM 51-21-06. FOUND TO BE OUT OF LIMITS IAW SRM 51-61-49. R & R SEAT TRACK IAW AMM 53-01-11-000-802 AND 53-01-11-400-802.

Part: FLOOR SUPPORT — CORRODED (BS 559) · airframe 34,497 hrs · 30,598 cycles

RT FLOOR SUPPORT CORRODED BETWEEN FRAMES BS 559+48 AND 559+80. REMOVED CORROSION FROM RT FLOOR SUPPORT PLATE IAW SRM 51-21-06.

Part: FLOOR PANEL — CRACKED (BS 193) · airframe 34,497 hrs · 30,598 cycles

FLOOR PANEL CRACKED AT FS 193.00. REPAIRED IAW GREO 601R-53-11-111.

Part: FLOOR SUPPORT — CORRODED (BS 559) · airframe 34,497 hrs · 30,598 cycles

RT FLOOR SUPPORT PLATE CORRODED BETWEEN FRAMES BS 559+16 AND 559+32. REMOVED CORROSION ON RT FLOOR SUPPORT PLATE IAW SRM 51-21-06.

Part: FLOOR SUPPORT — CORRODED (BS 559) · airframe 34,497 hrs · 30,598 cycles

RT FLOOR SUPPORT CORRODED BETWEEN FRAMES BS 559+80 AND 559+112. REMOVED CORROSION FROM RT FLOOR SUPPORT PLATE IAW SRM 51-21-06.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 34,497 hrs · 30,598 cycles

SEAT TRACK AT RBL 9 CORRODED BETWEEN FS 559+88 AND 559+96. BLENDED SEAT TRACK IAW SRM 51-21-06. FOUND TO BE OUT OF LIMITS IAW SRM 51-61-49. R & R SEAT TRACK IAW AMM 53-01-11-000-802 AND 53-01-11-400-802.

Part: SEAL — CRACKED (RT WING) · airframe 34,497 hrs · 30,598 cycles

RIGHT WING FLIGHT SPOILER CUTOUT CENTER SILL PLATE CRACKED. R & R CRACKED SEAL IAW SRM 51-40-06,51-42-01 & 51-40-2.

Part: PDU — FAILED (THRUST REVERSER) · airframe 34,233 hrs · 30,362 cycles

RIGHT THRUST UNLATCHED MASTER CAUTION IN FLIGHT, COMPLIED WITH QRH. EMERGENCY DECLARED AND ACFT RETURNED TO DEPARTURE. R & R RT ENGINE THRUST REVERSER PDU. RT ENGINE THRUST REVERSER OP CHECKED GOOD IAW AMM 78-32-03. NO FURTHER DEFECTS NOTED.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHTS) · airframe 34,037 hrs · 30,178 cycles

EMERGENCY LIGHT ON F/A PANEL ON POSITION EMERGENCY LIGHT ARE NOT OPERATING. CHARGED BATTERY SUPPLY IAW AMM 33-51-00 AND OPS CHECKED GOOD.

Part: DOOR — BINDING (GALLEY) · airframe 33,142 hrs · 29,406 cycles

GALLEY SERVICE DOOR WILL NOT OPEN OR CLOSE. UNBOUND DOOR AND OPS CHECKED GOOD IAW AMM 52-70-00.

Part: NUT — MISSING (GROUND TERMINAL) · airframe 33,142 hrs · 29,406 cycles

EMERGENCY SIGN ON GALLEY NEAR SERVICE DOOR INOP. REPLACED MISSING NUT ON GROUND TERMINAL OPS CHECKED GOOD IAW AMM 33-51-10.

Part: SENSOR — INTERMITTENT (TE FLAPS) · airframe 32,653 hrs · 28,993 cycles

FLAP FAIL CAUTION MESSAGE AT 0 DEGREES DURING APPROACH. EMERGENCY DECLARED. R & R RT FLAP BRAKE POSITION SENSOR IAW AMM 27-51-10. OP'S CHECKED GOOD.

Part: FLAP SYSTEM — FAILED (TE FLAPS) · airframe 32,483 hrs · 28,834 cycles

ENROUTE, SELECTED FLAPS, 8 FLAPS FAIL CAUTION MESSAGE, FLAPS FAILED AT ZERO. ACFT DIVERTED, EMERGENCY DECLARED. ACFT OK FOR SERVICE. MCO CLEARED.

Part: PRIORITY VALVE — FAILED (NLG) · airframe 31,626 hrs · 28,034 cycles

ON TAKEOFF RECEIVED A GEAR DISAGREE, NOSE WHEEL WAS DOWN AND MAINS WERE UP. RAN QRH, DID THE EMERGENCY GEAR EXTENTION. ACFT RETURNED TO DEPARTURE. UPON TOUCHDOWN, HAD NO NOSE WHEEL STEERING. R & R NLG PRIORITY VAVLE IAW AMM 32-33-15, PERFORMED FUNCTIONAL TEST OF THE LANDING GEAR EXTENSION & RETRACTION SYS IAW AMM 32-30-00. FUNCTIONAL TESTED GOOD, NO FURTHER DEFECTS FOUND.

Part: CONTROL PANEL — INTERMITTENT (CABIN PRESSURE) · airframe 30,911 hrs · 27,372 cycles

DURING CLIMBOUT, ACFT FAILED TO PRESSURIZE. CABIN WAS CLIMBING AT SAME RATE AS ACFT. WE GOT CABIN ALT CAUTION . RAN QRH. PRESSURIZATION DID NOT RESPOND IN MANUAL MODE. ACFT DELTA P WAS AT ZERO. RETURNED TO LAND. ACFT RETURNED TO DEPARTURE AFTER T/O -- EMERGENCY DECLARED AS A PRECAUTION. REMOVED AND REPLACED PRESSURE CONTROL PANEL , OP CHECKS GOOD IAW AMM 21-31-10. NO FURTHER DEFECTS, ACFT PRESSURIZED NUMEROUS TIMES WITH APU AND ENGINE BLEEDS.

Part: THERMAL SWITCH — FAILED (ANTI ICE SYS) · airframe 30,439 hrs · 26,978 cycles

ENROUTE, HOLDING AT 14K RECEIVED ANTI-ICE DUCT WARNING IN ICING CONDITIONS WITH WING AND COWL ANTI-ICE ON. RT WING SHOWED RED ON SYNOPTIC PAGE. FOLLOWED QRH AND RETURNED TO IAD AND DECLARED AN EMERGENCY. (ACFT RETURNED TO DEPARTURE AFTER T/O -- EMERGENCY DECLARED -- EQUIPMENT STANDING BY) R & R ALL 21 BLEED LEAK THERMAL SWITCHES IN RT WING IAW AMM 36-21-07. OPS CHECK GOOD. NO FURTHER DEFECTS NOTED. CURE TIME TRANSFERRED TO AFDL 598883-2.

Part: MODULE — MALFUNCTIONED (HYD SYSTEM) · airframe 30,439 hrs · 26,978 cycles

ENROUTE, RECEIVED STEERING INOP MSG FOLLOWED QRH AND MSG WOULD NOT EXTINGUISH. DECLARED EMERGENCY, LANDED IAD TOWED BACK TO GATE. (EMERGENCY DECLARED -- EQUIPMENT STANDING BY) R & R ELECTRO HYD MODULE IAW AMM 32-51-15. PERFORMED OPS CHECK IAW AMM 32-51-10. OPS AND LEAKS CHECK GOOD. DEFER CLEAR PLACARD REMOVED. (CLOSED)

Part: CONTROL UNIT — FAILED (NLG STEERING) · airframe 30,437 hrs · 26,976 cycles

NOSE WHEEL STEERING INOP CAUTION MESSAGE IN FLT (EMERGENCY DECLARED). R & R NOSE WHEEL STEERING ECU IAW AMM 32-51-10. OPS CHECK GOOD. (CLOSED)

Part: DOOR — LACK OF LUBE (MAIN PAX) · airframe 30,406 hrs · 26,947 cycles

UNABLE TO OPEN PAX DOOR FROM OUTSIDE UPON ARRIVAL AT AIRCRAFT. LUBED PAX DOOR AND PERFORMED OPS CHECKED , NO DEFECTS NOTED AT THIS TIME. ACFT OK FOR SERVICE PER AMM 52-11-00.

Part: SEAT TRACK — GOUGED · airframe 30,359 hrs · 26,906 cycles

LEFT NR 3 SEAT TRACK IS GOUGED AT FS 450. REMOVED AND REPLACED SEAT TRACK WITH NEW SERVICEABLE TRACK IAW AMM 53-01-11 THIS IS A MAJOR REPAIR.

Part: SEAT TRACK — CORRODED · airframe 30,356 hrs · 26,903 cycles

LT SEAT TRACK CORRODED. INSTALLED SERVICEABLE NR2 SEAT TRACK IAW AMM 53-01-11. MAJOR REPAIR.

Part: SEAT TRACK — CORRODED · airframe 30,356 hrs · 26,903 cycles

RT SEAT TRACK CORRODED. REPLACED SEAT TRACK IAW AMM 53-01-11.

Part: STRUCTURE — CORRODED (BS 449.85) · airframe 30,356 hrs · 26,903 cycles

CORROSION FOUND ON FLOOR STRUCTURE 1 LOCATION AT FS 449.85, RBL 43.

Part: STRUCTURE — CORRODED (BS 439-544) · airframe 30,356 hrs · 26,903 cycles

CORROSION FOUND ON FLOOR STRUCTURE, 12 LOCATIONS FROM FS 439 TO 544 LBL43. BLENDED CORROSION FLOOR STRUCTURE 12EA LOCATIONS FS 439 TO FS 544, LBL 43 AND WAS FOUND TO BE IN LIMITS IAW SRM 51-21-06 AND 53-00-00.

Part: FRAME — CORRODED (BS 333) · airframe 30,356 hrs · 26,903 cycles

FS 333.0 IS CORRODED AT STR 25 LT TO 25 RT. REMOVED DAMAGED FS 333.0 FRAME AND INSTALLED SERVICEABLE FRAME IAW SRM 51-42-06.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 30,356 hrs · 26,903 cycles

FS 280 BULKHEAD FLOORBEAM CRACKED LBL10 & RBL 10. REMOVED CRACKED FLOORBEAM AND REINSTALLED SERVICABLE FLOOREAM IAW SRM 51-42-06, SRM 51-41-00, & SRM 20-21-00.

Part: ISOLATOR — BROKEN (BULKHEAD) · airframe 30,356 hrs · 26,903 cycles

7 EA ISOLATORS ON AFT BLKHD ARE BROKEN & DAMAGED. R & R ISOLATORS IAW SRM 51-42-10 ON AFT BULKHEAD.

Part: ANGLE — CORRODED · airframe 30,356 hrs · 26,903 cycles

SERVICE DOOR SILL ANGLE FOR FLOORBOARD ATTACHMENT IS CORRODED. REMOVED MINOR SURFACE CORROSION ON SILL ANGLE IAW SRM 51-21-06. APPROX .001 IN MATERIAL LOSS. TREATED, PRIMED, AND TOPCOATED METAL IAW SRM 51-25-06, 51-25-16.

Part: PROXIMITY SWITCH — OUT OF RIG (MLG) · airframe 30,217 hrs · 26,781 cycles

GEAR DISAGREE AFTER TAKEOFF. (ACFT RETURNED TO IAD AFTER T/O -- EMERGENCY DECLARED) UPON INSP FOUND NLG EXTEND PROX SWITCH OUT OF RIG. CREW STATED RAMP HAD TO ADJUST TOW STOP AND THE HEARD A LOUD "BANG." ADJUSTED NLG PROX SWITCH IAW CRJ-200/32-65-05. OK FOR CONT SERVICE.

Part: PROXIMITY SWITCH — OUT OF ADJUST (PAX DOOR) · airframe 29,817 hrs · 26,417 cycles

INFLIGHT RECEIVED PAX OUT HANDLE MESSAGE. (TOWER HAD EMERGENCY VEHICLES STANDING BY) (PASSENGER DOOR INDICATION SYS (PHASE III DOOR) ) ADJUSTED PAX OUTER HANDLE PROX SWITCH PS2MB. OPS CK GOOD IAW IAW AMM 52-70-04 DEFER CLEARED PLACARD REMOVED.

Part: LIGHT — NO TEST (CABIN) · airframe 29,677 hrs · 26,293 cycles

RT SIDE DOORS ( SERVICE AND EMERGENCY EXITS ) BETA LIGHTS FAILED FUNCTIONAL CHECK. R & R RT SIDE DOORS (SERVICE AND EMERGENCY EXITS & BETA LIGHTS IAW AMM CH 33-51-09-400-801. COMPLIED WITH FUNCTI0NAL TEST OF THE DOOR EXIT SIGN BETA-LIGHTS ON THE RT SERVICE DOOR AND EMERGENCY EXIT IAW AMM TASK 33-51-09-920-801. NO DEFECT NOTED.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 29,677 hrs · 26,293 cycles

FS280 BEAM CRACKED ON LT SIDE, LT OF PULLEY BRACKET AT LBL9. REPAIRED FS 280 BEAM IAW EC/TC REO 601R-53-11-171 AND REO 601R-53-11-171. (CLOSED)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,677 hrs · 26,293 cycles

LT SIDE DOORS (ASD AND EMERGENCY EXIT) BETA LIGHTS FAILED FUNCTIONAL CHECK. R & R ASD DOOR EXIT BETA LIGHT IAW AMM 11-30-02-00, 33-51-09-000-801, AND 33-51-09-400-801. FUNCTIONAL TEST OF ASD BETA LIGHT GOOD IAW AMM 33-51-09-720-801. EMERGENCY EXIT DOOR STILL DUE INSTALLATION OF BETA LIGHT. R & R LT EMER EXIT DOOR BETA LIGHT AND PERFORMED FUNCTIONAL TEST IAW AMM 35-51-09-000-802, 33-51-09-400-802, 33-51-09-720-801. OPS CHECK GOOD AT THIS TIME.

Part: SEAT TRACK — CORRODED (BS 364-394) · airframe 29,677 hrs · 26,293 cycles

LT AND RT FLOOR SEAT TRACKS CORRODED FROM FS 364.00 TO FS 394.00. REMOVED LT AND RT SEAT RAILS AT FS 364.00 TO FS 394.00 IAW AMM TASK 53-01-11-000-802. INSTALLED NEW LT AND RT FLOOR SEATS TRACKS FORM FS 364.00 TO FS 394.00 IAW AMM 53-01-11-400-802. (CLOSED)

Part: TILLER — FAILED (NLG STEERING) · airframe 28,999 hrs · 25,695 cycles

AFTER TAKEOFF RECIEVED NOSEWHEEL STEERING CAUTION MESSAGE. FOLLOWED QRH PROCEDURE AND WAS UNABLE TO RECOVER SYS. (EMERGENCY DECLARED) NWS ECU WAS FLAGGING CODE "2" (PILOT HANDWHEEL INOP). R & R NWS TILLER IAW AMM 32-51-01. PERFORMED OPS CK OF NWS SYS IAW AMM 32-51-00 WITH NO DEFECTS, ACFT OK FOR SERVICE. (CLOSED)

Part: PIVOT — DAMAGED (SERVICE DOOR) · airframe 28,848 hrs · 25,556 cycles

F/A REPORTS SERVICE DOOR IS HARD TO OPEN. R & R DAMAGED PIVOT ROD AND OPS CHECKED IAW AMM 52-42-02, OPS NORMAL. (CLOSED)

Part: LIGHT — INOPERATIVE (GALLEY) · airframe 28,027 hrs · 24,676 cycles

LWR EMERGENCY LIGHTS INOP IN GALLEY AREA.

Part: UNKNOWN — MALFUNCTIONED (LANDING GEAR) · airframe 27,436 hrs · 24,048 cycles

UPON PUTTING GEAR UP GOT GEAR DISAGREE W/ MAINS UP AND NOSE GEAR DOWN. NOSE DOOR OPEN RED AMBER WOW INPUT, NWS INOP. RAN QRH GOT NOSE AND GEAR TO AGREE, ALSO GOT NWS BACK. RETURNED TO ATL. FLT 4971 DEL 62 MINS. AIRCRAFT RETURNED TO ATL AFTER T/O, EMERGENCY DECLARED, EQUIPMENT WAITING.

Part: DOOR — BINDING (PAX DOOR) · airframe 26,793 hrs · 23,391 cycles

F/A REPORTS PAX DOOR DIFFICULT TO CLOSE AND LOCK HAD TO HAVE ASSISTANCE FROM RAMP PERSONNEL OUTSIDE.

Part: SKIN — CORRODED (BS 559) · airframe 25,978 hrs · 22,612 cycles

RT FUSELAGE LOWER SKIN HAS CORROSION DAMAGE AROUND FASTENER HOLES AT FS 559.00+80 TO 559+112 STR 21R TO 23R, APPROX DEPT .003.

Part: SKIN — CORRODED (BS 559) · airframe 25,978 hrs · 22,612 cycles

LOWER FUSELAGE SKIN FROM FS 559.00 TO FS 559.00+112 STR 23L TO 25R HAS CORROSION DAMAGE AROUND FASTENER HOLES ON EXTERNAL SURFACE AND EXTERNAL SKIN SURFACE APPROX DEPT .009.

Part: SKIN — CORRODED (BS 559) · airframe 25,978 hrs · 22,612 cycles

LT LOWER FUSELAGE SKIN HAS CORROSION DAMAGE AROUND FASTENER HOLES AT FS 559+80 TO 559.00+96 STR 19L - 20L, APPROX .003 DEEP.

Part: FLOOR SUPPORT — CORRODED (FS 589-605) · airframe 25,972 hrs · 22,606 cycles

CARGO BAY FLOOR SUPPORT AT LBL 27 HAS CORROSION (INTERGRANULAR) ON O/B FLANGE FROM FS 589 TO FS 605. FOUND CORROSION TO BE BEYOND ALLOWABLE LIMITS. ANGLE ON FLOOR SUPPORT REQUIRES REPLACEMENT. REMOVED CARGO BAY FLOOR SUPPORT. LOCATED FASTENER LOCATIONS AND INSTALLED NEW SERVICEABLE FLOOR SUPPORT IAW EC/TC 601R-53-61-2883. PRIMED AND PAINTED REPAIRED AREA IAW SRM 51-25-00. REMOVED AND INSTALLED SAME SERVICEABLE INSULATION IN APPLICABLE AREAS IAW AMM 25-81-02-400-801.

Part: SILL — CORRODED (BS 559) · airframe 25,972 hrs · 22,606 cycles

LT SIDE PRESSURE FLOOR SEAL HAS CORROSION INTERMITTANT FROM FS 409+128 TO FS 559 LBL 36 TO LBL 47. FOUND CORROSION TO BE ONLY LIGHT SURFACE CORROSION WHICH IS WITHIN REPAIR LIMITS IAW SRM 53-61-43. REMOVED CORROSION, PREPPED, PRIMED & PAINTED DOORS IAW SRM 51-21-06. INVESTIGATED, MAPPED & BLENDED LT SIDE PRESSURE FLOOR SILL CORROSION AREAS IAW REO 601R-53-41-666. AREA FAILS DIMENSIONAL LIMITS OF EO DUE TO LOCATIONS OF FASTENER HOLES & SPACE BETWEEN AREAS OF CORROSION. ENGINEERING DISPOSITION REQUIRED. REPAIRED CORROSION DAMAGE TO PRESSURE FLOOR PANEL & ANGLES IAW REO 601R-53-41-805. EC/TC REQUIRED. WORK PERFORMED IAW EC/TC REO 601R-53-41-805.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 25,972 hrs · 22,606 cycles

REAR PRESSURE BULKHEAD WEB THAT SURROUNDS LINTEL FITTING HAS AN INDICATION NOTED APPROX 1 INCH IN LENGTH 90 PERCENT FULL SCREEN HEIGHT. FAILED NDT INSPECTION. REPAIRED REAR PRESSURE BULKHEAD WEB IAW REO 601R-53-61-1230, STEPS 1 THRU 24. REPAIR OF THE REAR PRESSURE BULKHEAD WEB WAS ACCOMPLISHED IAW REO 601R-53-61-1230.

Part: ANGLE — CRACKED (FS 621) · airframe 25,972 hrs · 22,606 cycles

CARGO DOOR SUPPORT BEAM LOWER ANGLE IS CRACKED APPROX 1.0 INCH. REMOVED AND REPLACED CARGO DOOR SUPPORT BEAM LOWER ANGLE WITH NEW IAW SRM 51-42-21.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 25,972 hrs · 22,606 cycles

LT / RT FS 559.0 BULKHEAD WEB HAS INDICATIONS NOTED LT WEB WL 52.10 O/B OF LBL 9 .2 INCH IN LENGTH RT WEB WL 58.70 I/B OF RBL 18 APPROX 1 INCH IN LENGTH WL 58.70 O/B RBL 9. .3 INCH IN LENGTH AND WL 54.10 O/B RBL 9 1INCH IN LENGTH. ALL THESE AREAS FAILED NDT MARK ON WEBS. REPAIRED LT AND RT FS 559.0 BULKHEAD WEB IAW BOMBARDIER REO 601R-53-41-802. WORK PERFORMED IAW ASA EC/TC 601R-53-41-802.

Part: SILL — CORRODED (BS 409) · airframe 25,972 hrs · 22,606 cycles

RT SIDE PRESSURE FLOOR SEAL HAS CORROSION INTERNITTANT FROM FS 409+128 TO FS 559 RBL 36 TO RBL 47. FOUND CORROSION TO BE ONLY LIGHT SURFACE CORROSION WHICH IS WITHIN ALLOWABLE REPAIR LIMITS IAW SRM 53-61-43. REMOVED CORROSION, PREPPED, PRIMED & PAINTED AREAS IAW SRM 51-21-06. INVESTIGATED, MAPPED AND BLENDED RT PRESSURE FLOOR SILL CORROSION AREAS IAW REO 601R-53-41-666. AREAS FAIL DIMENSIONAL LIMITS OF EO DUE TO LOCATIONS OF FASTENER HOLES & SPACE BETWEEN AREAS OF CORROSION. ENGINEERING DISPOSITION REQUIRED. REPAIRED CORROSION DAMAGE TO PRESSURE FLOOR PANEL & ANGLES IAW REO 601R-53-41-805. EC/TC REQUIRED. WORK PERFORMED IAW EC/TC REO 601R-53-41-805.

Part: BATTERY PACK — FAILED (CABIN) · airframe 25,972 hrs · 22,606 cycles

EMERGENCY LIGHTS BATTERY PACK NR 3 FAILED TEST. REMOVED FAULTY BATTERY PACK NR 3 IAW AMM 33-51-04-000-801. INSTALLED SERVICEABLE BATTERY PACK IN SAME LOCATION IAW AMM 33-51-04-400-801. OPS CHECK DUE OF EMERGENCY LIGHTS SYS. PERFORMED OPS CHECK OF BATTERY PACK NR 3 IAW AMM 33-51-04-740-801. OPS CHECK GOOD AT THIS TIME.

Part: HANDLE — DIRTY (PAX DOOR) · airframe 25,610 hrs · 22,259 cycles

MAIN PASSENGER DOOR HANDLE REPORTED BY FLIGHT ATTENDANT, DIFFICULT TO STOW. ONCE STOWED, THE DOOR CLOSED INDICATION WAS DIFFICULT TO SHOW. COMPLIED WITH INSPECTION OF PAX DOOR LOCKING MECHANISM/CLEANED AND LUBED INNER HANDLE AND EXTERNAL HANDLE SERVICE LETTER RJ-52-003. (S)

Part: HANDLE — MALFUNCTIONED (PAX DOOR)

MAIN PAX DOOR OUTER HANDLE DIFFICULT TO STOW FROM INSIDE ACFT ON 2 LEGS. COMPLIED WITH INSP OF PAX DOOR OUTER HANDLE, CLEANED AND LUBE. PERFORM OPERATIONAL CHECK GOOD PER AMM 52-11. OK FOR SERVICE. (A)

Part: ATTACH FITTING — CRACKED (BS 484) · airframe 25,530 hrs · 22,190 cycles

OUTBOARD CLIP AT FRAME STA 484, LBL 27 IS CRACKED. REMOVED CRACKED CLIP FROM PREVIOUS REPAIR. FABRICATED NEW - 1 CLIP FROM 2024 T-3. LPI WAS ACCOMPLISHED ON -1 CLIP FROM 2024 T-3. 063 REF REO 601R-53-41-059 AND CRJ 200 AMM 51-20-08. MB14369 7/14/2008. NO DEFECTS NOTED. OK TO INSTALL. (S)

Part: FLOORBEAM — CRACKED (BS 484) · airframe 25,524 hrs · 22,184 cycles

FLOOR SUPPORT ANGLE CRACKED AT FS 484 LBL 27. REMOVED FLOOR SUPPORT ANGLE AT FS 484 LBL 27 AND DRILLED NEW ANGLE IAW CRJ 200 SRM 53-41-00. OK TO INSTALL FLOOR SUPPORT ANGLE. (S)

Part: STRUCTURE — CORRODED (BS 559) · airframe 25,524 hrs · 22,184 cycles

CORROSION FOUND AT FS 559 RBL 44. REMOVED CORROSION AT FS 559 RBL 44 IAW SRM 51-21-06. MATERIAL LOSS .002 FOUND TO BE WITHIN LIMITS IAW CRJ 200 SRM 51-21-06. RESTORED FINISH IAW SRM 51-25-00. (S)

Part: FLOORBEAM — CRACKED (BS 461) · airframe 25,511 hrs · 22,171 cycles

FLOORBEAM FITTING AT FS 461 ON O/B SIDE OF RBL 9 CRACKED REMOVED FITTING AND DRILLED NEW SUPPORT FITTING. OK TO INSTALL FLOORBEAM FITTING. (B)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 25,498 hrs · 22,157 cycles

VARIOUS EMERGENCY LIGHTS IN CABIN. REMOVED AND REPLACED NR 4 POWER SUPPLY UNIT AND BATTERY PACK ASSY IAW CRJ200 AMM33-50. OPS GOOD. NO OTHER DEFECTS NOTED AT THIS TIME. (B)

Part: LIGHT — BROKEN (CABIN) · airframe 25,358 hrs · 22,038 cycles

FWD ENTRY DOOR EMERGENCY LIGHT BROKEN. FLT 4839 DEL 22 MINS. REPLACED LIGHT ASSY OPS OK PER 33-50-01.

Part: DOOR — STIFF (MAIN PAX) · airframe 25,348 hrs · 22,028 cycles

FLIGHT ATTENDANT AND RAMPERS REPORT CABIN DOOR EXTREMELY DIFFICULT TO CLOSE. FLT 4900 DEL 27MINS. CYLCED PAX DOOR SEVERAL TIMES. OPS CK GOOD IAW CRJ 200 AMM 52-11-01.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 25,124 hrs · 21,840 cycles

NR 8 OVERWING EMERGENCY LIGHT, SECTION 9-13 FLOOR STRIP LIGHTING AND NR 3 DOME LIGHT INOP. REMOVED AND REPLACED NR 4 BATTERY CHARGER IAW CRJ 200 AMM 33-51-05. REMOVED AND REPLACED NR 4 BATTERY CHARGER IAW CRJ 200 AMM 33-51-05.

Part: STEP — BROKEN (PAX DOOR) · airframe 24,704 hrs · 21,483 cycles

FOUND PAX DOOR BOTTOM STEP BROKEN.

Part: FLAP — MALFUNCTIONED (WING) · airframe 24,345 hrs · 21,189 cycles

FLAPS FAIL ON DEPARTURE AT 0 DEGREES, EMERGENCY DECLARED.

Part: LANDING GEAR — MALFUNCTIONED · airframe 23,965 hrs · 20,880 cycles

FLT 4666 - GEAR DISAGREE WARNING MSG "BOTH MAIN GEARS UP" FOLLOWED QRH, MANUALLY DEPLOYED MAIN GEARS, EMERGENCY DECLARED. LANDING GEAR RETRACTION SYSTEM.

Part: LANDING GEAR — MALFUNCTIONED · airframe 23,958 hrs · 20,875 cycles

UPON SELECTION OF GEAR HANDLE TO DOWN BOTH RT AND LT GEAR INDICATORS SHOWED UNSAFE, FOLLOWED BY GEAR DISAGREE WARNING. COMPLIED WITH QRH PROCEDURES AND USED LANDING GEAR MANUAL RELEASE HANDLE TO GET MAIN GEAR DOWN, EMERGENCY DECLARED.

Part: LANDING GEAR — MALFUNCTIONED · airframe 23,937 hrs · 20,857 cycles

GEAR DISAGREE MSG UPON EXTENSION OF HANDLE. RAN QRH, GEAR DEPLOYED USING FREE FALL METHOD. EMERGENCY DECLARED. EMERGENCY EQUIPMENT ON STANDBY. LANDING GEAR RETRACTION SYSTEM.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 23,933 hrs · 20,854 cycles

SELECTING GEAR DOWN GEAR DISAGREE WARNING NOSE GEAR INDICATED DOWN LT AND RT MAIN WERE NOT DOWN. FOLLOWED QRH USED MLG MANUAL RELEASE TO EXTEND GEAR. EMERGENCY EQUIPMENT ON STANDBY. FLTS 4269, 4263, 4646, 4665 CX. LANDING GEAR RETRACTION SYSTEM.

Part: STEERING SYS — MALFUNCTIONED (NLG) · airframe 22,233 hrs · 19,552 cycles

ON TAKEOFF FROM ATL, AFTER GEAR RETRACTION RECEIVED STEERING INOP CAUTION MESSAGE RAN QRH PROCEDURE AND RETURNED ATL WITH NOSEWHEEL STEERING OFF. LANDED NORMALLY TAXIED TO GATE. AIRCRAFT RETURNED TO ATL AFTER T/O. EMERGENCY DECLARED. FLT 4711 DEL 261 MINS.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 22,227 hrs · 19,549 cycles

LEFT FWD EXTERIOR EMERGENCY LIGHT INOP.

Part: INTERCOSTAL — CRACKED (BS 484) · airframe 21,168 hrs · 18,761 cycles

RANRC 440// 484 INTERCOSTAL CRACKED AT RBL 27. REMOVED AND DUPLICATE CRACKED ANGLE USING 2024-T3 .063 PO 7960-1 MATERIAL ID FROM ASA REO 601R-53-41-059. INSTALLED DUPLICATE ANGLE. ALL WORK DONE IAW CRJ SRM 51-24-26, 51-40-11, 51-42-21. 302 TODD HAM RA 328 (CLOSED)

Part: INTERCOSTAL — CRACKED (BS 484) · airframe 21,168 hrs · 18,761 cycles

RANRC 401. FLANGE IS CRACKED AT FS 484 RBL 36. REPAIRED CRACKED FLANGE ON FS 484 INTERCOASTAL IAW REO 601R-53-41-059. REFER TO W/C 439 LPI. 302 TODD HAM RA328 (CLOSED)

Part: ANGLE — CRACKED (FUSELAGE) · airframe 21,168 hrs · 18,761 cycles

RANRC 262, 280 RT, LBL 9 INBOARD ANGLE CRACKED. REMOVED DAMAGED ANGLE AT F.S. 280, LBL 9.0, I/B SIDE. FABRICATED ANGLE, LOCATED AND DEBURRED IAW CRJ SRM 53-21-43. ALODINED, PRIMED, AND PAINTED SERVICEABLE ANGLE IAW CRJ SRM 51-25-16. INSTALLED SERVICEABLE ANGLE IAW CRJ SRM 51-42-20. (CLOSED)

Part: FLOORBEAM — CRACKED (BS 310) · airframe 21,168 hrs · 18,761 cycles

RANRC 268, FLOORBEAM LBL 27 OUTBOARD AT APPROX 310 HAS CRACK PROTRUDED FROM RIVET, MARKED. CUT-OUT APPX 2IN OF DAMAGED WEB FLANGE AT LBL 27.0, FWD OF F.S. 310 IAW CRJ SRM 51-71-59. FABRICATED REPAIR ANGLE FROM 2024-T3 .040 PO 864-3-1 AND REPAIR FILLER IAW CRJ SRM 51-71-59. LOCATED & DEBURRED FASTENER HOLES IN REPAIR ANGLE, REPAIR FILLER & WEB IAW CRJ SRM 51-40-11. OK TO ALODINE, PRIMED, AND PAINT REPAIR ANGLE AND REPAIR FILLER. ALODINED, PRIMED, & PAINTED, REPAIRED ANGLE AND REPAIR FILLER IAW CRJ SRM 51-25-16. OK TO INSTALL REPAIR ANGLE & REPAIR FILLER. INSTALLED REPAIR ANGLE & FILLER IAW CRJ SRM 51-71-59. FOUND REPAIR INSTALLATION UNSERVICEABLE REFERENCE W/C 515 FOR CORRECTIVE ACTION. (CLOSED)

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 21,168 hrs · 18,761 cycles

RANRC NR 179 PAX DOOR AFT DRAG ANGLE CRACKED.

Part: WARNING SYSTEM — MALFUNCTIONED (COCKPIT) · airframe 20,640 hrs · 18,350 cycles

LEFT MAIN GEAR DISAGREE RAN QRH GEAR EXTENDED LANDED NORMAL. (AN EMERGENCY WAS DECLARED)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,541 hrs · 18,265 cycles

LEFT WING FUSELAGE REAR EMERGENCY LIGHT IS OUT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 20,256 hrs · 18,044 cycles

FOUND LT FUSELAGE AFT EXTERIOR EMERGENGY LIGHT INOP.

Part: ANGLE — CRACKED (FUSELAGE)

DURING A HANGAR INSPECTION, THE LT SIDE FS 640 REINFORCEMENT ANGLE WAS FOUND TO BE CRACKED. THIS MRR WILL REMAIN OPEN PENDING MAINTENANCES DETERMINATION OF AN APPROPRIATE C/A. (K)

Part: STEP — BROKEN (DOOR)

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

Part: MECHANISM — MALFUNCTIONED (NLG UNLOCK)

DURING CLIMB OUT, THE CREW RECEIVED A GEAR DISAGREE MESSAGE AND THE NOSE LANDING GEAR WOULD NOT RETRACT. THE QRH WAS COMPLIED WITH, THE CREW DECLARED AN EMERGENCY AND RETURNED, WHERE IT LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED THE NOSE GEAR UNLOCK ASSEMBLY IAW AMM. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)

Part: STEP — BROKEN (PAX DOOR)

DURING A GROUND INSPECTION IN ATL, 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: CONNECTOR — DIRTY (EMERGENC LIGHTS)

DURING A GROUND INSPECTION IN TPA, THE EMERGENCY LIGHTS REMAINED ON WITH THE SWITCH IN THE ARMED POSITION. MAINTENANCE CLEANED THE CONNECTOR ON JUNCTION BOX 6 PANEL. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: STEERING SYS — UNKNOWN (NLG)

DURING TAKEOFF FROM MSP-CVG, UPON GEAR RETRACTION THE CREW RECEIVED GEAR DISAGREE WARNING, NOSE DOOR OPEN WARNING, STEERING INOPERATIVE CAUTION, AND WEIGHT ON WHEELS INPUT CAUTION MESSAGES. THE QRH WAS COMPLIED WITH. AN EMERGENCY WAS DECLARED DUE TO THE LOSS OF NOSE WHEEL STEERING. THE AIRCRAFT RETURNED TO MSP AND LANDED SAFELY WITH EXCEPTION TO THE NOSE WHEEL STEERING BEING INOPERATIVE. THE AIRCRAFT WAS SAFELY TOWED TO THE GATE. MAINTENANCE FOUND THE NOSE LANDING GEAR SCISSOR LINKS DISCONNECTED AND RECONNECTED THEM. MAINTENANCE PERFORMED OPERATIONAL CHECKS OF THE NOSE WHEEL STEERING, INSPECTED THE NLG AND NG AREA WITH NO DEFECTS NOTED AND RESTOWED THE MLG RELEASE HANDLE. AIRCRAFT OK FOR SERVICE. (M)

Part: DOOR FRAME — CRACKED (PAX DOOR)

DURING A C-CHECK IN MCN, THE PASSENGER DOOR INNER FRAME AT FS 320 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE PASSENGER DOOR INNER FRAME AT FS 320 IAW BOMBARDIER REO 601R-52-11-678. (M)

Part: SKIN — CRACKED (PAX DOOR)

DURING A C-CHECK IN MCN, THE PASSENGER DOOR INNER SKIN AT THE LOWER INTERCOSTAL AND FORWARD STEP FRAME WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE PASSENGER DOOR INNER SKIN AT THE LOWER INTERCOSTAL AND FORWARD STEP FRAME IAW ASA EO 600-52-0082. (M)

Part: CLIP — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE FS 484 CLIPS AT LBL 27 AND RBL 27 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE FS 484 CLIPS AT LBL 27 AND RBL 27 IAW ASA EO 600-53-0098. (M)

Part: INTERCOSTAL — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE FS 484 INTERCOSTAL AT LBL 36 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE FS 484 INTERCOSTAL AT LBL 36 IAW ASA EO 600-53-0098. (M)

Part: SKIN — CRACKED (RT WING)

DURING A C-CHECK IN MCN, THE LOWER TRAILING EDGE WING PLANK AT WS 148.019 RHS WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE LOWER TRAILING EDGE WING PLANK AT WS 148.019 RHS IAW ASA EO 600-57-0134A. (M)

Part: SKIN — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE NOSE LANDING GEAR FUSELAGE SKIN RADIUS RHS AT FS 235 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE NOSE LANDING GEAR FUSELAGE SKIN RADIUS RHS AT FS 235 IAW ASA EO 600-53-0122. (M)

Part: CONNECTOR — INOPERATIVE (EMERGENCY LIGHT)

FLT 4460 - DURING A GROUND INSPECTION IN DFW, THE EMERGENCY LIGHTING AT ROWS 9 TO 14 WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT EMERGENCY FLOOR LIGHT CONNECTOR, FLEX LAMP P/N 362624, AT ROW 10, CABLE ASSY AT ROWS 9-14, AND THE FLOOR TRACK COVER. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LAMP — BURNED OUT (EMERGENCY LIGHT)

DURING A HANGAR INSPECTION IN BTR, THE RIGHT FORWARD EXTERIOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE RIGHT FORWARD EXTERIOR EMERGENCY LIGHT LAMP. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LAMP — BURNED OUT (EMERGENCY LIGHT)

FLT 4140 - DURING A GROUND INSPECTION IN DFW, THE FORWARD EXTERIOR RIGHT WING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD EXTERIOR RIGHT WING EMERGENCY LIGHT LAMP. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: WIRE — INOPERATIVE (EMERGENCY LIGHT)

DURING A GROUND INSPECTION IN SHV, THE EMERGENCY EXIT SIGN BY THE FLOOR AT THE PASSENGER DOOR WAS FOUND INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE TO THE EMERGENCY EXIT SIGN BY THE FLOOR AT THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: ENGINE — FAILED (RIGHT)

DURING DESCENT, AT APPROX 24,000 FT THE CREW HEARD A LOUD POP FOLLOWED BY A VIBRATION INDICATION ON THE RT ENGINE GAUGE. QRH PROCEDURES WERE COMPLIED WITH. THE CREW REDUCED RT ENGINE POWER TO BELOW FIFTY PERCENT AND THE VIBRATION SUBSIDED. AN EMERGENCY WAS DECLARED AND THE CREW PERFORMED A TWENTY DEGREE FLAPS APPROACH AND LANDING. THE AIRCRAFT LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED THE RT ENGINE. OPS AND LEAK CHECKS GOOD. AIRCRAFT OK FOR SERVICE. BUSED ON THE TEAR DOWN REPORT RESULTS, IT WAS CONCLUDED THE ENGINE SUSTAINED FOREIGN OBJECT DAMAGE FROM THE INGESTION OF ICE. THE ENGINE IS BEING REPAIRED AND WILL RETURN TO SERVICE. (M)

Part: PDU — FAILED (T/E FLAP)

FLT 4600 - DURING APPROACH INTO YOW FROM ATL, THE CREW SELECTED THE FLAPS TO TWENTY DEGREES AND AT ELEVEN DEGREES RECEIVED A FLAPS FAIL CAUTION MESSAGE, WITH THE FLAPS REMAINING AT ELEVEN DEGREES. QRH PROCEDURES WERE COMPLIED WITH AND AN EMERGENCY DECLARED. THE FLAPS WERE SELECTED TO EIGHT DEGREES AND THE AIRCRAFT LANDED SAFELY IN YOW. LOCAL MAINTENANCE INSPECTED AND RESET THE FLAPS IAW AD 98-20-01. ASA MAINTENANCE REMOVED AND REPLACED THE FLAPS POWER DRIVE UNIT. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

DURING A C-CHECK IN MCN, THE FLOORBEAMS AT FS 349 ON THE RIGHT INBOARD AND OUTBOARD SIDES WRE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE FLOORBEAMS AT FS 349 ON THE RIGHT INBOARD AND OUTBOARD SIDES IAW ASA EO 600-53-0052. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

DURING A C-CHECK IN MCN, THE SEAT TRACKS ON THE LEFT AND RIGHT SIDES AT FS 349 AND LBL 9 WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE SEAT TRACKS ON THE LEFT AND RIGHT SIDES AT FS 349 AND LBL 9 IAW SRM 51-00. (M)

Part: PLATE — CORRODED (FUSELAGE)

DURING A C-CHECK IN MCN, THE CARGO DOOR FLOOR LANDING PLATE AT THE FORWARD LOWER DOOR STOP WAS FOUND TO BE CRACKED AND CORRODED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE CARGO DOOR FLOOR LANDING PLATE AT THE FORWARD LOWER DOOR STOP IAW SRM 51-00. (M)

Part: ANGLE — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE CARGO COMPARTMENT FLOOR SUPPORT ANGLE AT FS 621 ON THE LEFT AND RIGHT SIDES, WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE CARGO COMPARTMENT FLOOR SUPPORT ANGLE AT FS 621 ON THE LEFT AND RIGH SIDES IAW ASA EO 600-53-0105. (M)

Part: SIGN — INOPERATIVE (CABIN)

DURING HANGAR MAINTENANCE IN MCN, THE LIGHTED EMERGENCY EXIT SIGN AT THE PASSENGER DOOR ON THE FORWARD WALL WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BURNED OUT EMERGENCY LIGHT BULB. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: BEAM — CRACKED (FUSELAGE)

WHILE COMPLYING WITH ASA EO600-53-0043A, INSPECTION OF THE ENGINE SUPPORT BEAM, THERE WAS A CRACK FOUND AT THE LEFT AND RIGHT ACCESS PANEL. BOTH CRACKS WERE ON THE INBOARD FORWARD SIDE OF THE PANELS. MAINTENANCE REPAIRED THE CRACKED ENGINE SUPPORT BEAM IAW ASA EO 600-53-0073. (M)

Part: FRAME — CRACKED (FUSELAGE)

DURING HANGAR INSPECTION IN MCN, FRAME STATION 718 WAS FOUND TO BE CRACKED ON BOTH THE LEFT AND RIGHT SIDE. MAINTENANCE REPAIRED THE CRACKED FRAME IAW ASA EO 600-53-0067. (M)

Part: LAMP — BURNED OUT (FUSELAGE)

DURING GROUND INSPECTION, THE FORWARD MOST EXTERNAL EMERGENCY LIGHT ON THE LEFT SIDE OF THE FUSELAGE WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BURNT OUT EXTERNAL EMERGENCY LIGHT BULB. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN)

FLT 4605 - DURING GROUND INSPECTION IN CAK, THE FLOOR PATH EMERGENCY LIGHTING JUST AFT OF THE WING EMERGENCY EXIT WAS INOPERATIVE. MAINTENANCE FOUND THE ELECTRIC CABLE CONNECTING TO THE AFT MOST FLOOR LIGHT STRIP DAMAGED AND SHORTED. MAINTENANCE REMOVED AND REPLACED THE FLOOR EMERGENCY LIGHTING WIRING PIG TAIL CONNECTOR AT ROW 12. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: WINDOW — CRACKED (COCKPIT)

FLT 4473 - DURING FLIGHT FROM ATL TO HPN, RIGHT SIDE WINDOW CRACKED. CAPTAIN DIVERTED TO TRI AND LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED THE RIGHT SIDE WINDOW. OPS AND LEAK CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: FUEL CONTROL — OUT OF RIG (ENGINE)

FLT 4409 - DURING FLIGHT FROM SBH TO ATL WHEN POWER WAS REDUCED TO FLIGHT IDLE THE RIGHT ENGINE STOPPED RUNNING. CREW SECURED ENGINE AND RESTARTED PER QRH PROCEDURES. FLIGHT LANDED SAFELY IN ATL. MAINTENANCE FOUND WITH CONTROL LEVERS IN FLIGHT IDLE, THE FUEL CONTROL UNIT TO BE IN RIG BELOW IDLE TOWARDS SHUTOFF. MAINTENANCE RE-RIGGED FUEL CONTROL UNIT. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: LINE — FAILED (NR 2 ENGINE)

FLT 4582 - EN ROUTE TO QRH AT 29,000 FEET, CREW RECEIVED HYDRAULIC 2 LOW PRESSURE MESSAGE WITH A SLIGHT SHUTTER AND A DIPPING OF WING WHILE IN AUTOPILOT. CREW FOLLOWED QRH PROCEDURES AND DIVERTED TO RIC. AIRCRAFT LANDED SAFELY. MAINTENANCE REPLACED THE FLEX PRESSURE LINE TO THE NR 2 ENGINE HYDRAULIC PUMP. OPERATIONAL AND LEAK CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: WIRE — FAILED (CABIN)

DURING INSPECTION, FOUND EMERGENCY FLOOR LIGHTS INOPERATIVE. MAINTENANCE REPAIRED WIRING ON FLOOR LIGHTS. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT RELEASED FOR FURTHER SERVICE. (X)

Part: BULB — FAILED (EXTERIOR)

OUTSTATION ROA - FLT 4714 - CREW REPORTED THE 2 EXTERIOR EMERGENCY EXIT LIGHTS ON THE RT REAR OF THE AIRCRAFT WERE INOPERATIVE. LOCAL MAINTENANCE SWAPPED AN OPERABLE BULB FROM THE LEFT SIDE TO THE RIGHT IAW MEL 33-51-2 AND FLIGHT CONTINUED TO ATL. ATL MAINTENANCE REMOVED AND REPLACED BURNED OUT LIGHT BULBS. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RELEASED FOR FURTHER SERVICE (X)

Part: TRANSDUCER — FAILED (LT ENGINE)

ATL/CHA - FLT 4621 - EN ROUTE, LEFT ENGINE OIL PRESSURE WENT TO ZERO PSI. CREW SHUT DOWN THE LEFT ENGINE PER QRH SINGLE ENGINE PROCEDURE AND DECLARED AN EMERGENCY. AIRCRAFT LANDED AT CHA UNEVENTFULLY. ASA MECHANIC SWAPPED THE PRESSURE TRANSDUCERS AND CONFIRMED INDICATION ONLY. AIRCRAFT WAS INSPECTED AND FOUND SAFE FOR A FERRY FLIGHT TO MCN. MCN MAINTENANCE REMOVED AND REPLACED THE LEFT ENGINE OIL PRESSURE TRANSDUCER. OPERATIONAL AND LEAK CHECKS WERE GOOD AND THE AIRCRAFT WAS RELEASED FOR FURTHER SERVICE. (X)