N827AS

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 36,420 hrs · 32,484 cycles

MISSING EXIT SIGN COVER BY PAX DOOR. INSTALLED COVER IAW AMM 33-51-19.

Part: HANDLE — LACK OF LUBE (PAX DOOR) · airframe 35,007 hrs · 31,167 cycles

PAX DOOR HANDLE HARD TO OPEN. CLEANED AND LUBED PAX DOOR HANDLE IAW AMM 52-11-02. OPS CHECKED GOOD NO DEFECTS NOTED.

Part: MOTOR — FAILED (APU STARTER) · airframe 34,204 hrs · 30,428 cycles

APU WOULD NOT START. TWO ATTEMPTS MADE ON GROUND POWER AND ONE ATTEMPT ON BATTERY. APU RPM WOULD NOT GO ABOVE 18 PERCENT. OBSERVED SMOKE COMING FROM INTAKE BELOW NR 1 ENGINE, R & R APU STARTER MOTOR IAW AMM 49-41-07. OPS CHECKED GOOD, COMPLETED THREE APU STARTS. RAN APU AND PACKS FOR 30 MINUTES. NO OVERTEMPS NOTED.

Part: COWL DOOR — MISSING (RT NACELLE) · airframe 34,008 hrs · 30,251 cycles

DURING DESCENT, FELT WHAT WAS LIKE WAKE TURBULANCE. UPON POST FLIGHT FOUND TOP OF RT ENGINE COWL MISSING. PERFORMED INSPECTIONS OF ENGINE, PYLON, AND EMPENNAGE AE, REF L/P'S 667135 AND 667141, NO FAULTS NOTED. INSTALLED NEW COWL IPC 71--14-01 ITEM 5 IAW AMM 71-14-01. OK FOR SERVICE.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 33,699 hrs · 29,968 cycles

CAPTAIN'S FLASHLIGHT INOPERATIVE. R & R FLASHLIGHT IAW AMM 25-61-04.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 33,339 hrs · 29,645 cycles

EXIT SIGN AT SERVICE DOOR FAILED OPS TEST. REMOVED NR 2 BATTERY CHARGER ASSY IAW AMM 33-51-01-000-801. INSTALLED SERVICEABLE CHARGER IAW AMM 33-51-05-400-801. PERFORMED OPS TEST IAW AMM 33-51-04-740-801. OPS TESTED GOOD.

Part: FLOOR SUPPORT — CORRODED (BS 559-621) · airframe 33,337 hrs · 29,642 cycles

FLOOR SUPPORT CORRODED FROM FS 559+80 TO 621. REPAIRED IAW REO 601R-53-00-460.

Part: DOOR FRAME — CORRODED (E/E BAY) · airframe 33,337 hrs · 29,642 cycles

FS 364.00, BELLY FWD EDGE OF AVIONICS DOOR CUT OUT T-FITTING FRAME CORRODED ON FORWARD SIDE FROM STRINGER 25L TO 25R BOTH LEGS OF ANGLE. CLASSIFIED AS A MAJOR.

Part: FLOOR SUPPORT — CORRODED (BS 559-621) · airframe 33,337 hrs · 29,642 cycles

FLOOR SUPPORT CORRODED FROM FS 559+80 TO FS 621. PERFORMED NDT IAW NDTM 51-20-06. NO INDICATIONS NOTED. REPAIRED IAW 601R-53-51-182.

Part: FRAME — CORRODED (BS 364) · airframe 33,337 hrs · 29,642 cycles

FS 364.00 BELLY FWD EDGE OF AVIONICS DOOR CUT OUT, TEE FITTING ANGLE CORRODED ON FORWARD SIDE FROM STRINGER 25L TO 25R BOTH LEGS OF ANGLE. REMOVED CORROSION FROM ANGLES IAW SRM 51-21-06. REMOVED AND REPLACED ANGLES IAW SRM 51-42-06.

Part: FLOOR SUPPORT — CORRODED (BS 559-621) · airframe 33,337 hrs · 29,642 cycles

RT FLOOR SUPPORT CORRODED FROM FS 559+80 TO 621. REPAIRED IAW REO 601R-53-21-2251.

Part: ANGLE — CORRODED (PAX DOOR) · airframe 33,337 hrs · 29,642 cycles

ANGLE CORRODED ON PAX DOOR. REMOVED CORROSION FROM ANGLE IAW SRM 51-21-06 2. ANGLE BEYOND REPAIR LIMITS IAW SRM 51-21-06. INSTALLED SERVICEABLE ANGLE IAW SRM 51-42-06.

Part: FLOOR PANEL — DAMAGED · airframe 33,337 hrs · 29,642 cycles

FLOOR PANEL 251CLF HAS A BROKEN INSERT ON AFT EDGE. REPLACED AND INSTALLED NEW INSERT ON FLOOR PANEL 251CLF IAW REPAIR MANUAL. REPAIR METHOD "L" RC161862.

Part: ACCESS PANEL — DAMAGED (LT WING) · airframe 33,337 hrs · 29,642 cycles

LEFT WING LOWER WING ACCESS PANEL HOLE 550GB CORRODED, AND GOUGED. REPAIRED IAW REO 601R-57-21-030, REV 4.

Part: ACCESS PANEL — GOUGED (LT WING) · airframe 33,337 hrs · 29,642 cycles

LT WING LOWER WING ACCESS PANEL HOLE 540AB GOUGED. REPAIRED IAW REO 601R-87-21-030, REV 4.

Part: ACCESS PANEL — CORRODED (LT WING) · airframe 33,337 hrs · 29,642 cycles

LEFT WING LOWER WING ACCESS PANEL HOLE 550CB CORRODED. REPAIRED IAW REO 601R-57-21-030, REV 4.

Part: ACCESS PANEL — CHAFED (WING) · airframe 33,337 hrs · 29,642 cycles

WING FUEL TANK ACCESS PANEL HOLE CHAFED ON BOTH CORNERS. REPAIRED IAW REO 601R-87-21-030, REV 4.

Part: ACCESS PANEL — CHAFED (WING) · airframe 33,337 hrs · 29,642 cycles

WING FUEL TANK ACCESS PANEL HOLE HAS CHAFFING ON BOTH CORNERS INBD AND OTBD 640BB. REPAIRED IAW REO 601R-87-21-030, REV 4.

Part: ACCESS PANEL — CHAFED (WING) · airframe 33,337 hrs · 29,642 cycles

FUEL TANK ACCESS PANEL CHAFED ON OTBD CORNER. REPAIRED IAW REO 601R-87-21-030, REV 4.

Part: DOOR FRAME — CORRODED (E/E BAY DOOR) · airframe 33,337 hrs · 29,642 cycles

FS 364.00 BELLY FWD EDGE OF AVIONICS DOOR CUTOUT, FITTING FRAME CORRODED ON FORWARD SIDE FROM STRINGER 25L TO 25R BOTH LEGS OF ANGLE. INSTALLED NEW FRAME IAW DWG 601R32009 AND SRM 51-42-06.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 33,337 hrs · 29,642 cycles

CORROSION AND GOUGES ON SEAT TRACK AT RBL 9. BETWEEN FS 559+64 TO +112. REMOVED DAMAGED SEAT TRACK IAW SRM 53-51-49. INSTALLED NEW SEAT TRACK IAW AMM 53-01-11-400-802.

Part: CROSSBEAM — CORRODED (BS 559) · airframe 33,337 hrs · 29,642 cycles

CORROSION ON CROSSBEAM BETWEEN RBL 27 AND RT SILL AT FS 559+112. REMOVED CORROSION IAW SRM 51-21-06. REMOVED .0013" OF MATERIAL, FOUND WITHIN LIMITS IAW SRM 53-00-00 LESS THAN 10 PERCENT.

Part: STRUCTURE — CORRODED (BS 559) · airframe 33,337 hrs · 29,642 cycles

LEFT FLOOR EDGE MEMBER HAS CORROSION AT NUT PLATE ATTACH POINTS FROM FS 559+80 TO +121. REMOVED CORROSION IAW SRM 51-21-06, MATERIAL REMOVED IS .002. FOUND WITHIN LIMITS IAW SRM.

Part: INTERCOSTAL — CORRODED (BS 349) · airframe 33,337 hrs · 29,642 cycles

LEFT INTERCOSTAL AT FS 349.00 CORRODED. BLENDED CORROSION IAW SRM 51-21-06. REMOVED LESS THAN .001" OF MATERIAL.

Part: INTERCOSTAL — CORRODED (BS 364 S27R) · airframe 33,337 hrs · 29,642 cycles

FS 364 BELLY INTERCOSTAL JUST RT OF STRINGER 27 IS CORRODED ON OTBD SIDE BOTH ENDS ON BOTH LEGS. REMOVED AND REPLACED INTERCOSTAL IAW SRM 51-42-06 AND 51-42-21.

Part: INTERCOSTAL — CORRODED (BS 364 S27L) · airframe 33,337 hrs · 29,642 cycles

FS 364 BELLY INTERCOSTAL JUST LT OF STINGER 27 CORRODED ON BOTH LEGS. REMOVED AND REPLACED INTERCOSTAL IAW SRM 51-40-06, 51-40-11 & 51-42-06 & 51-42-20.

Part: STRUCTURE — CORRODED (BS 559-621) · airframe 33,337 hrs · 29,642 cycles

RIGHT FLOOR EDGE MEMBER IS CORRODED FROM FS 559+80 TO FS 621. REMOVED CORROSION IAW SRM 51-21-06 AND 51-12-00. PERFORMED UT THICKNESS INSPECTION IAW MAC NDT PROCEDURES UT-3, MIN MATERIAL REMAINING .059" ORIGINAL .063" REMOVED .004" COMPLIED WITH STEP 2 OF REO 601R-53-00-460 IAW NDTM 51-20-06 NO INDICATIONS NOTED AT THIS TIME.

Part: SEAT TRACK — CORRODED (BS 364-400) · airframe 33,337 hrs · 29,642 cycles

SEAT TRACK LBL 9 AT FS 364 TO FS 400 CORRODED. REMOVED SEAT TRACK IAW AMM 53-01-11-000-802. INSTALLED NEW TRACK IAW AMM 53-01-11-400-802.

Part: INTERCOSTAL — CORRODED (BS 364 S27) · airframe 33,337 hrs · 29,642 cycles

FS 364 BELLY INTERCOSTAL JUST LT OF STRINGER 27 IS CORRODED ON OTBD SIDE MULTIPLE SPOTS. REMOVED AND INSTALLED INTERCOSTAL IAW SRM 51-42-06.

Part: SEAT TRACK — CORRODED (BS 364-469) · airframe 33,337 hrs · 29,642 cycles

SEAT TRACK LBL 9 AT FS 364.00-469.0+128 CORRODED. REMOVED CORROSION IAW SRM 51-21-06 MATERIAL LOSS 0.005, FOUND WITHIN LIMITS IAW SRM 53-00-00.

Part: SEAT TRACK — CORRODED (BS 364) · airframe 33,337 hrs · 29,642 cycles

SEAT TRACK, RBL 9 AT FS 364+400 IS CORRODED. REMOVED SEAT TRACK SRM IAW 53-01-11-000-802. INSTALLED NEW SEAT TRACK IAW AMM 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 364-409) · airframe 33,337 hrs · 29,642 cycles

SEAT TRACK RBL 9 AT FS 364.00 TO 409.0+122 CORRODED. REMOVED SEAT TRACK IAW AMM 53-01-11-000-802. INSTALLED NEW SEAT TRACK IAW AMM 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 409) · airframe 33,337 hrs · 29,642 cycles

LEFT SEAT TRACK AT FS 409+20 HAS AREA OF CORROSION. REMOVED CORROSION IAW SRM 51-21-06 & VERIFIED WITHIN LIMITS IAW SRM 53-21-41, FIG 101.

Part: BRACKET — CRACKED (BULKHEAD) · airframe 33,337 hrs · 29,642 cycles

LEFT AFT PRESSURE BULKHEAD STANDOFF BRACKET CRACKED AT LBL 9-27. REMOVED DEFECTIVE BRACKET IAW SRM 51-42-06. INSTALLED BRACKET IAW SRM 51-42-06.

Part: SENSING ELEMENT — FAILED (OVERHEAT DETECT) · airframe 32,565 hrs · 28,932 cycles

AFTER TO CLIMBING THRU APPRX 3000 FT, MLG BAY OVERHEAT MSG COMPLY WITH QRH MSG EXTINGUISHED. ACFT RETURNED TO DEPARTURE AFTER T/O -- EMERGENCY DECLARED AS A PRECAUTION. MLG BAY OVERHEAT DETECTION SYS (BTMS OPERATIVE) - SYS DEACTIVATED. R & R BOTH LT & RT SENSING ELEMENTS IAW AMM 26-14-04. OPS CHECK GOOD, DEFER CLEARED, PLACARD REMOVED.

Part: HANDLE — BINDING (PAX DOOR) · airframe 31,412 hrs · 27,899 cycles

PASSENGER DOOR EXTERIOR HANDLE WILL NOT TURN. PERFORMED OPS CHECKS, OPERATED HANDLE SEVERAL TIMES, NO DEFECTS NOTED IAW AMM 52-11-03. (CLOSED)

Part: SENSOR — UNKNOWN (APU OIL TEMP) · airframe 30,731 hrs · 27,291 cycles

AFTER LANDING APU SHUTDOWN WHILE TAXIING TO GATE VERY STRONG FUEL SMELL INSIDE COCKPIT AND CABIN CAUSING EYES TO BURN. R & R APU OIL TEMP BULB IAW AMM 49-91-25. OPS CK GOOD. DEFER CLEARED PLACARD REMOVED. (CLOSED)

Part: APU — ODOR · airframe 30,693 hrs · 27,256 cycles

ON DESCENT, TRIED TO START APU BUT NO LIGHT OFF OCURRED, ON SECOND TRY APU STARTED BUT A STRONG ODOR OF JET FUEL FILLED THE CABIN AND WE SHUTDOWN THE APU. INTERROGATED APU ECU AND FOUND NO DISCREPANCIES AND NO FUEL LEAKS, OPS CK GOOD AT THIS TIME IAW AMM 49-30-00. (CLOSED)

Part: SKIN — CORRODED (BS 349) · airframe 28,901 hrs · 25,668 cycles

FS 349.00 SKIN IS CORRODED ON BELLY SIDE FWD OF AVIONICS DOOR CUTOUT. REMOVED FRAME AND FLOOR SUPPORT AT F.S. 333 IAW SRM 51-42-06 AND 51-42-21. INSTALLED NEW SERVICEABLE FRAME AT FS 333 BETWEEN STR 23L AND 23R. REINSTALLED AVIONICS BAY FLOOR SUPPORT IAW SRM 51-42-06 AND 51-42-21. REQUIRES PAINT AND CORROSION INHIBITING COMPOUND. PAINT AND CORROSION INHIBITING COMPOUND APPLIED TO AREA COMMON TO FRAME 333 IAW SRM 51-21-11 AND SRM 51-21-16. PRESSURIZATION CHECK DUE. LEAK CHECK GOOD IAW AMM 21-23-00-863-801

Part: POST — CRACKED (BS 409) · airframe 28,901 hrs · 25,668 cycles

FOUND FS 409.0+128 VERTICAL POST RBL 18.0 INBD SIDE HAS INDICATION NOTED APPROX .2" IN LENGTH 50 PERCENT FSH AT WL 69.0 AFT FLANGE RADIUS FAILED NDT INSP. REMOVED VERTICAL POST FS 409+128, RBL 18 INBD SIDE LOCATED AND DRILLED NEW POST IAW SRM 51-42-06. NEW INBD POST REQUIRES INSTALLATION. INSTALLED NEW INBD POST FS 409+128 LT IAW SRM AND REO 601R-53-41-889. POST REQUIRES EDGE SEAL AND PAINT TOUCH UP. COMPLIED WITH EC/TC REO 601R-53-41-889 AND MET ALL THE REQUIREMENTS OF REO 601R-53-41-889 REVISION A. POST REQUIRES EDGE SEAL & PAINT. EDGE SEALED POST IAW AMM 51-23-00-390-804 & PAINTED POST IAW SRM 51-25-01.

Part: POST — CRACKED (BS 409) · airframe 28,901 hrs · 25,668 cycles

FOUND FS 409.0+128 VERTICAL POST BL 0.0 LT AND RT SIDE HAS INDICATIONS NOTED APPRPOX .3" IN LENGTH LT SIDE 80 PERCENT FSH, R SIDE 60 PERCENT FSH AT WL 39.0 AFT FLANGE RADIUS FAILED NDT INSP. REMOVED VERTICAL POST ASSY AT FS 409+128 BL 0 IAW SRM 51-42-06. FS 409+128 BL 0 VERT POST INSTALL REQ INSTALLED NEW POSTS FS 409+128 BL 0 IAW REO 601R-53-41-1184. FASTENERS REQUIRE TOUCH UP PAINT. REPAIR TO THE BULKHEAD 409+128 POST AT BL 0.00 ON ACFT IS COMPLETED IAW REO 601R-53-41-1184 AND MEETS WITH ALL ITS REQUIREMENTS. EDGE SEAL & PAINT REQUIRED. EDGE SEALED POST IAW AMM 51-23-00-390-804 & TOUCHED UP PAINT IAW SRM 51-25-01.

Part: FLOORBEAM — CRACKED (BS 484) · airframe 28,901 hrs · 25,668 cycles

FS 484 SUPPORT CLIP AT LBL 27 IS CRACKED. R & R FS 484 SUPPORT CLIP AT LBL 27 IAW SRM 51-42-21.

Part: FLOORBEAM — CRACKED (BS 484) · airframe 28,901 hrs · 25,668 cycles

FS 484 FLOOR CLIP AT RBL 27 IS CRACKED. R & R FS 484 FLOOR SUPPORT CLIP AT RBL 27 IAW SRM 51-42-21.

Part: FLOOR SKIN — CRACKED (BS 460) · airframe 28,901 hrs · 25,668 cycles

FOUND FS 460 PRESSURE FLOOR SKIN HAS INDICATION NOTED BETWEEN BL 0.0 AND LBL 4.0 APPROX 3.5" IN LENGTH 20 PERCENT FSH CONFIRMED WITH LPI TO FIND LENGTH 3.5" AND ORIENTATION FAILED NDT INSP AREAS MARKED ON ACFT. REPAIRED PRESSURE FLOOR WEB FWD OF FS 460.00 AT BL 0.0 - LBL 9.00 IAW REO 601R-53-41-1180. REPAIRED PRESSURE FLOOR WEB FWD OF FS 460.00 AT BL 0.0 - LBL 9.0 IAW ASA REO 601R-53-41-1180. COMPLIED WITH EC/TC REO 601R-53-41-1180 AND REO 601R-53-41-1180 REV M DATED: 03/11/2010.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 28,901 hrs · 25,668 cycles

FOUND REAR PRESSURE BULKHEAD WEB LBL 27.50 APPROX WL 130 HAS INDICATION NOTED APPROX .2" IN LENGTH 90/5 FSH JUST ABOVE AFT CARGO DOOR TRACK FAILED NDT INSP. AREA MARKED ON ACFT. COMPLIED WITH EC/TC REO 601R-53-61-1541 AND MET ALL THE REQUIREMENTS OF REO 601R-53-61-1541 REV B.

Part: LIGHT — NO TEST (CABIN) · airframe 28,901 hrs · 25,668 cycles

EXIT PULL BETA LIGHTS ON PAX DOOR HANDLE & LT & RT OVERWING EXIT FAILED FUNCTION TEST & SERVICE DOOR HANDLE. R & R PAX DOOR HANDLE PULL EXIT BETA LIGHT IAW AMM 3-51-09-000-801 & 33-51-09-400-801. R & R SERVICE DOOR BETA LIGHTS IAW AMM 33-51-09-000-802 & 33-51-09-400-802. FUNCTIONAL CHECK GOOD.

Part: LIGHT — INOPERATIVE (LT OVERWING) · airframe 28,638 hrs · 25,387 cycles

FWD LT OVERWING EXTERIOR EMERGENCY LIGHT INOP.

Part: HOLDER — OVERHEATED (COCKPIT) · airframe 28,638 hrs · 25,387 cycles

CAPT CHART HOLDER LIGHT BEGAN TO OVER HEAT AND SMOKE WITH LIGHT ON, TURNED IT OFF AND SMOKE STOPPED. (COCKPIT/FLIGHT DECK/FLIGHT INSTRUMENT LIGHTING SYSTEMS EXCLUDING EFIS )

Part: TRANSMITTER — FAILED (TE FLAPS) · airframe 28,541 hrs · 25,272 cycles

AFTER TAKEOFF AT FLAP RETRACTION, LT FLAP FROZE AT 4 DEGREES FOR APPROX 5-8 MINUTES. NO FLAP FAIL MSG RCVD. BUT ACFT HAD A RT ROLL TENDENCY. FLAP DID EVENTUALLY RETRACT WE DID NOT OPERATE FLAPS FURTHER AND LANDED FLAPS 0 DEGREES WITH TOUCHDOWN OF LESS THAN 100 FPM. (EMERGENCY DECLARED)

Part: CONTROLLER — DEFECTIVE (COCKPIT) · airframe 27,929 hrs · 24,603 cycles

THE "L, WSHLD HEAT" CAUTION MESSAGE IN FLIGHT RESET PER QRH. RETURNED AFTER A COUPLE OF MIN. SMELLED ELECTRICAL SMOKE. L, WHSLD HEAT (A11) AND HEATER CONTROLLER (F12) HAVE POPPED. EMERGENCY DECLARED. FIRE TRUCKS ROLLED AS A PRECAUTION. WINDSHIELD AND SIDE WINDOW ANTI-ICE CONTROLLERS - ONE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,906 hrs · 24,579 cycles

LEFT AND RIGHT AFT OVERWING EMERGENCY EXIT LIGHTS INOP.

Part: BATTERY — DISCHARGED (CABIN) · airframe 27,549 hrs · 24,225 cycles

NR 4 EMERGENCY BATTERY DEAD.

Part: WARNING LIGHT — ILLUMINATED (TE FLAPS) · airframe 26,755 hrs · 23,472 cycles

FLAP FAIL MSG AFTER SELECTING FLAPS 20.0 / FLAPS FAIL AT 8.0 [EMERGENCY DECLARED]...FLT 5341 DEL 34 MINS.

Part: STRUCTURE — CORRODED (BS 559 S23R) · airframe 25,686 hrs · 22,475 cycles

MINOR CORROSION AROUND FASTENERS BELOW LAV SERVICING POINT FS 559+80 - 559+112 STR 23R. REMOVED FASTENERS BELOW LAV SERVICING POINT. REMOVED CORROSION & REINSTALLED FASTENERS IAW SRM 51-42-06 & SRM 51-21-06. PRESSURIZATION CHECK DUE. PRESSURIZATION CHECK GOOD IAW AMM 21-32-00-863-801. REPAINT THE BELLY FUSELAGE TO MATCH SURROUNDING AREA. PAINTED REPAIR IAW SRM 51-25-16. (S)

Part: BULKHEAD — CRACKED (BS 559) · airframe 25,686 hrs · 22,475 cycles

FS 559 BULKHEAD WEB HAS INDICATIONS AT WL 58.70 I/B OF RBL 18 APPROX 1.3" IN LENGTH AND O/B OF RBL 9 APPROX .4" IN LENGTH, AND CAP ANGLE AT LBL 18, AND RBL 18 APPROX .5 IN LENGTH FAILED NDT INSP. (B) REPAIRED FS 559 BULKHEAD WEB AND CAP ANGLE ON LT AND RT SIDE FROM LBL 27 TO LBL 9 AND RBL 27 TO RBL 9 IAW REO 601R-53-41-754. RII C/W 5300002.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 25,686 hrs · 22,475 cycles

REAR PRESSURE BULKHEAD WEB THAT SURROUND THE LINTEL ATTACHMENT FITTING HAS AN INDICATION NOTED APPROX .2" IN LENGTH 1005 FULL SCREEN HEIGHT FAILED NDT INSP. (B) REPAIR PER EC/TC REO 601R-53-61-1230 HAS BEEN COMPLETED AND THE REPAIR C/W THE REQUIREMENTS OF EC/TC AND REO 601R-53-61-1230 REV D. RII C/W 53000002. (A)

Part: SUPPORT BEAM — CRACKED (FUSELAGE) · airframe 25,686 hrs · 22,475 cycles

CARGO DOOR SUPPORT BEAM LOWER ANGLE IS CRACKED APPROX 1.5". REMOVED SUPPORT BEAM LOWER AFT BRACKET AND INSTALLED NEW SERVICEABLE BRACKET IAW SRM 51-42-21. LEAK CHECK DUE. PRESSURIZED ACFT IAW AMM 21-32-00-863-801. LEAK CHECK GOOD. (S)

Part: SILL — CORRODED (BS 409-559) · airframe 25,686 hrs · 22,475 cycles

NUMEROUS AREAS OF MINOR CORROSION ON PRESSURE FLOOR SILL FROM FS 409.0+128 TO FS 559.0, RBL 36.0 TO RBL 47.0 WL 73.0. REMOVED MINOR CORROSION FROM PRESSURE FLOOR SILL FROM FS 409.0+128 TO FS 559.0, RBL 36.0 TO RBL 47.0, WL 73.0 IAW SRM 51-21-06. RUBATEX TAPE REQUIRE INSTALLATION. INSTALLED RUBATEX TAPE ON PRESSURE FLOOR SILL FROM FS 409.0 TO FS 559.0, RBL 36.0 TO RBL 47.0, WL 73.0 IAW AMM 53-01-01-400-802.

Part: SILL — CORRODED (BS 409-559) · airframe 25,686 hrs · 22,475 cycles

NUMEROUS AREAS OF MINOR CORROSION ON PRESSURE FLOOR SILL FROM FS 409.0+128 TO FS 559.0, LBL 36.0 TO LBL 47.0, WL 73.0. REMOVED MINOR CORROSION ON PRESSURE FLOOR SILL IAW SRM 51-21-06. RUBATEX TAPE REQUIRES INSTALLATION. INSTALLED RUBATEX TAPE IAW MM 53-01-01-400-802.

Part: ANCHOR FITTING — CORRODED (PAX DOOR) · airframe 24,739 hrs · 21,645 cycles

ASD FWD ANCHOR FITTING SERRATED PLATES CORRODED.

Part: ANCHOR FITTING — CORRODED (AIRSTAIR) · airframe 24,739 hrs · 21,645 cycles

ASD AFT ANCHOR FITTING SERRATED PLATES CORRODED.

Part: FLAP — MALFUNCTIONED (WING) · airframe 24,452 hrs · 21,419 cycles

ON APPROACH AT 170 KNOTS WITH FLAPS SELECTED AND INDICATING 20 DEG, SELECTED FLAPS TO 30 DEG, RECEIVED FLAPS FAIL AT 20 DEG. EN ROUTE TO SCE A/C DIVERTED TO MDT DUE TO MTC. EMERGENCY EQUIPMENT ON STANDBY.

Part: STRIP — CRACKED (CABIN) · airframe 23,968 hrs · 21,009 cycles

EMERGENCY LIGHT STRIP AT ROW 5 CRACKED.

Part: STRIP — CRACKED (CABIN) · airframe 23,968 hrs · 21,009 cycles

EMERGENCY LIGHT STRIP CRACKED AT ROW 12.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,064 hrs · 19,568 cycles

EMERGENCY CEILING LIGHT AT ROW 5AB IS INOP.

Part: CAUTION MESSAGE — ILLUMINATED (NLG STEERING) · airframe 22,009 hrs · 19,525 cycles

STEERING INOP MSG, ON TAKEOFF. COMPLIED WITH QRH 13-5. FLT 4477 DEL 20 MINS. EMERGENCY EQUIPMENT WAS REQUESTED TO BE ON STANDBY AS A PRECAUTION.

Part: DOOR — STIFF (MAIN PAX) · airframe 21,671 hrs · 19,269 cycles

PAX DOOR VERY DIFFICULT TO CLOSE.

Part: CLIP — CRACKED (FUSELAGE) · airframe 21,203 hrs · 18,871 cycles

RANRC 405. CLIP AT FS 280 ON I/B SIDE OF THE LBL 9 IS CRACKED.

Part: SKIN — CORRODED (FUSELAGE) · airframe 21,203 hrs · 18,871 cycles

RANRC 456. MINOR SURFACE CORROSION ON FUSELAGE UNDERNEATH VHF NR 1 ANTENNA (UPPER).

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 21,203 hrs · 18,871 cycles

RANRC 372. FLOOR SUPPORT ANGLE AT FS 280.00 CRACKED JUST O/B OF LBL9.

Part: DOOR FRAME — CRACKED (PAX DOOR) · airframe 21,203 hrs · 18,871 cycles

RANRC 424. PAX DOOR FRAME CRACKED; FS 338.00 AT APPROX 6.0" FROM FORWARD END.

Part: SKIN — CORRODED (FUSELAGE) · airframe 21,203 hrs · 18,871 cycles

RANRC 411. CORROSION DISCOVERED ON FUSELAGE UNDERNEATH THE ADF ANTENNA.

Part: WEB — CRACKED (FUSELAGE) · airframe 21,203 hrs · 18,871 cycles

RANRC 395. FS 280.00 WEB CRACKED JUST O/B OF LBL9.

Part: INTERCOSTAL — CRACKED (PAX DOOR) · airframe 21,203 hrs · 18,871 cycles

RANRC 425. PAX DOOR UPPER AFT INTERCOSTAL CRACKED.

Part: RIB — CRACKED · airframe 21,203 hrs · 18,871 cycles

FOUND RIGHT BATTERY RIB CRACKED.

Part: CONNECTOR — BROKEN (EMERGENCY LIGHT) · airframe 21,203 hrs · 18,871 cycles

FOUND EMERGENCY LIGHT STRIP FLEXIBLE LIGHTS NUMBERS 2, 3, AND 4 COUNTING FROM FRONT HAVE BROKEN ELECTRICAL CONNECTOR PINS.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHT) · airframe 21,203 hrs · 18,871 cycles

FOUND EMERGENCY FLOOR TRACK LIGHTING ELECTRICAL CONNECTOR, COMING THROUGH PASSENGER COMPARTMENT FLOOR PANEL 141 ALF, IS DAMAGED.

Part: PANEL — DEPARTED (RT WING) · airframe 21,045 hrs · 18,729 cycles

AFTER LIFTOFF IT WAS REPORTED TO FA THERE WAS A HOLE IN RT WING. WENT BACK AND INSPECTED IT AND FOUND ACCESS PANEL IN FRONT OF IB GLD AND DEPARTED THE ACFT. IT WAS REPORTED TO HAVE HAPPENED JUST AFTER LIFTOFF. A/C RETURNED TO DEPARTURE. FLT 4846 DEL 226 MINS, REFER TO ENTRY 272502-2 FOR OVER WEIGHT LANDING. REFER TO ENTRY 272500-20 FOR FUEL LEAK CHECK***JLG

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,036 hrs · 18,723 cycles

ONE SECTION OF EMERGENCY LOWER TRACK LIGHT INOP.

Part: STEP — DAMAGED (DOOR)

DURING A HANGAR INSPECTION, THE PASSENGER DOOR BOTTOM STEP WAS FOUND DAMAGED. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR BOTTOM STEP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)

Part: LAMP — BURNED OUT (FUSELAGE)

DURING A GROUND INSPECTION, THE EXTERIOR RT SIDE, SECOND FROM THE FRONT, EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE EXTERIOR RT SIDE, SECOND FROM THE FRONT, EMERGENCY LIGHT ASSY. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)

Part: STEP — BROKEN (PAX DOOR)

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

Part: COVER — LOOSE (FLOODLIGHT)

DURING A GROUND INSPECTION IN ATL, THE EMERGENCY FLOOD LIGHT COVER, NEAR THE PASSENGER DOOR, WAS FOUND TO BE UNSECURED. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY FLOODLIGHT, NEAR THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LENS — MISSING (CABIN)

FLT 4084 - DURING A GROUND INSPECTION IN ATL, THE FLOOR LEVEL EMERGENCY EXIT SIGN ON THE FORWARD BULKHEAD WAS FOUND TO BE MISSING A COVER. MAINTENANCE REPLACED THE FLOOR LEVEL EMERGENCY EXIT SIGN MISSING COVER ON THE FORWARD BULKHEAD. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: STEP — CRACKED (PAX DOOR)

DURING AN A-CHECK IN BTR, THE TOP STEP ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE TOP STEP ON THE PASSENGER DOOR. (M)

Part: DOUBLER — CRACKED (FUSELAGE)

DURING AN A-CHECK, THE FS 640 RH DOUBLER, FS 640 RT FRAME AND BONDED SKIN DOUBLER AT RT FS 640, STRINGER 8-13 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE FS 640 RT DOUBLER AND THE FS 640 RT FRAME. MAINTENANCE IS ALSO REPAIRING THE BONDED SKIN DOUBLER AT RT FS640, STRINGER 8-13 IAW REO. (K)

Part: STEP — SEPARATED (PAX DOOR)

DURING HANGAR MAINTENANCE IN MCN, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND SEPARATING AT THE ATTACHMENT POINT STAY ROD. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. (M)

Part: STEP — BROKEN (PAX DOOR)

DURING A GROUND INSPECTION IN MHT, THE PASSENGER DOOR BOTTOM STEP ATTACH POINT FOR THE DEPLOYMENT ROD WAS FOUND BROKEN OFF FROM THE STEP. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR BOTTOM STEP. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: COVER — MISSING (CABIN)

DURING A GROUND INSPECTION, THE EMERGENCY EXIT SIGN COVER BY THE PASSENGER DOOR WAS FOUND MISSING. MAINTENANCE INSTALLED AN EMERGENCY EXIT SIGN COVER BY THE PASSENGER DOOR. AIRCRAFT OK FOR SERVICE. (K)

Part: PRESSURE PANEL — CORRODED (FUSELAGE)

DURING A C-CHECK IN MCN, THE PRESSURE FLOOR AT FS 473-559 RT WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS SUBMITTING A REPAIR REQUEST TO BOMBARDIER FOR AN REO TO REPAIR THE PRESSURE FLOOR AT FS 473-559 RT. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

DURING A C-CHECK IN MCN, THE FLOORBEAM AT FS 574-621 WERE FOUND TO BE CORRODED BEYOND LIMIT. MAINTENANCE IS SUBMITTING A REPAIR REQUEST TO BOMBARDIER FOR AN REO TO REPAIR THE FLOORBEAMS AT FS 574-621. (M)

Part: PRESSURE PANEL — CORRODED (FUSELAGE FLOOR)

DURING A C-CHECK IN MCN, THE PRESSURE FLOOR AREA AT FS 484-559, BL 36 LEFT WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS SUBMITTING A REPAIR REQUEST TO BOMBARDIER FOR AN REO TO REPAIR THE FLOOR PRESSURE FLOOR AT FS 484-559, BL 36 LEFT. (M)

Part: SKIN — CRACKED (LT & RT WING)

DURING A C-CHECK IN MCN, THE LOWER WING PLANKS AT WS 148.019 LT/RT WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE LOWER WING PLANKS AT WS 148.019 LHS/RHS IAW ASA EO 600-57-0134A. (M)

Part: SUPPORT BEAM — CRACKED (CENTER ENGINE)

DURING A C-CHECK IN MCN, THE CENTER ENGINE SUPPORT BEAM UPPER AND LOWER WEB AT BL 0 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE CENTER ENGINE SUPPORT BEAM UPPER AND LOWER WEB AT BL 0 IAW ASA EO 600-53-0072. (M)

Part: PRESSURE PANEL — CORRODED (FUSELAGE FLOOR)

DURING A C-CHECK IN MCN, THE PRESSURE FLOOR BETWEEN FS 449.85-473.15 LT/RT WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS SUBMITTING A REPAIR REQUEST TO BOMBARDIER FOR AN REO TO REPAIR THE FLOOR PRESSURE FLOOR BETWEEN FS 449.85-473.15 LEFT AND RIGHT. (M)

Part: PRESSURE PANEL — CORRODED (FLOOR)

DURING A C-CHECK IN MCN, THE PRESSURE FLOOR AREA AT FS 484 LEFT WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS SUBMITTING A REPAIR REQUEST TO BOMBARDIER FOR AN REO TO REPAIR THE PRESSURE FLOOR AREA AT FS 484 LEFT. (M)

Part: FLOOR SUPPORT — CRACKED (FUSELAGE)

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

Part: CLIP — CRACKED (CARGO DOOR SILL)

DURING A C-CHECK IN MCN, THE CLIP AT FS 589 LEFT OUTBOARD BY THE CARGO DOOR SILL WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE CLIP AT FS 589 LEFT OUTBOARD BY THE CARGO DOOR SILL. (M)

Part: CLIP — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE CLIPS AT FS 484, LBL 27 AND RBL 27 INBOARD AND THE CLIPS AT FS 484, LBL 36 AND RBL 36 OUTBOARD WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE CLIPS AT FS 484, LBL 27 AND RBL 27 INBOARD AND REPAIRING THE CLIPS AT FS 484, LBL 36 AND RBL 36 OUTBOARD IAW ASA EO 600-53-0098. (M)

Part: SILL — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE CARGO COMPARTMENT SILL PLATE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE CARGO COMPARTMENT SILL PLATE. (M)

Part: FLOOR SUPPORT — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE FLOOR SUPPORT ANGLE AT FS 621 RT WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE FLOOR SUPPORT ANGLE AT FS 621 RT IAW ASA EO 600-53-0105. (M)

Part: STEP — CRACKED (PAX DOOR)

DURING AN A-CHECK IN BTR, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHT)

DURING A GROUND INSPECTION IN DFW, THE LEFT FORWARD EXTERNAL EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 2 AND NR 3 BATTERY CHARGER ASSEMBLIES. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: ACM — MALFUNCTIONED (RIGHT)

FLT 4739 - DURING CLIMB-OUT FROM LEX-DFW, WITH THE LEFT PACK DEFERRED THE CREW RECEIVED A RIGHT PACK HIGH PRESSURE MESSAGE. THE QRH WAS COMPLIED WITH BUT THE RIGHT PACK WOULD NOT RESET. SOME PASSENGERS WERE REPORTED AS FEELING ILL AND DIZZY WITH THE COCKPIT BECOMING VERY HOT. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT DIVERTED TO CVG, LANDING SAFELY. MAINTENANCE RESET THE RIGHT PACK AIR CYCLE MACHINE. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: SKIN — CRACKED (FUSELAGE)

DURNG HANGAR MAINTENANCE IN MCN, THE LEFT AND RIGHT CORNERS OF THE FUSELAGE SKIN AT FS 235, BL 6 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE PERFORMED A TEMPORARY REPAIR TO THE LEFT SIDE FUSELAGE STRUCTURE AT FS 235, STRINGER 26 IAW BOMBARDIER REO 601R-53-11-802. THIS REPAIR IS VALID FOR 500 FLIGHT HOURS FROM THE TIME OF INCORPORATION. MAINTENANCE ALOS PERFORMED A TEMPORARY REPAIR TO THE RIGHT SIDE FUSELAGE SIN AT FS 235, BL 6 IAW BOMBARDIER REO 601R-53-11-047. THIS REPAIR IS VALID FOR 400 CYCLES FROM RETURNT O SERVICE. BOTH TEMPORARY REPAIRS ARE TO BE REINSPECTED EVERY 100 FLIGHT HOURS. THIS MRR WILL REMAIN OPEN PENDING COMPLETION OF THE PERMANENT REPAIRS. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVI

Part: LAMP — BURNED OUT (EMERGENCY LIGHT)

DURING HANGAR MAINTENANCE IN BTR, THE SECOND FROM AFT EMERGENCY CEILING LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE SECOND FROM AFT EMERGENCY CEILING LIGHT LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LAMP — BURNED OUT (EMERGENCY LIGHT)

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

Part: CABLE — BINDING (PAX DOOR)

FLT 4442 - DURING A GROUND INSPECTION IN DFW, THE PASSENGER DOOR WAS HARD TO CLOSE. MAINTENANCE ADJUSTED THE PASSENGER DOOR CABLE. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: STEP — BROKEN (PAX DOOR)

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

Part: ACTUATOR — BINDING (PAX DOOR)

FLT 4628 - DURNIG A GROUND INSPECTION IN ATL, THE FLIGHT ATTENDANT REPORTED THE PASSENGER DOOR WOULD NOT CLOSE ALL THE WAY. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR SERVO MOTOR ACTUATOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: COALESCER BAG — DIRTY (AIR DISTRIBUTION)

FLT 4529 - DURING CLIMB-OUT FROM ATL-MGM, THE CREW NOTICED A BURNING ODOR COMING FROM THE LEFT PACK. THE ODOR BEGAN TO DECREASE WITH THE POWER SET TO IDLE DURING DESCENT. THE AIRCRAFT LANDED SAFELY IN MGM. MAINTENANCE REMOVED AND REPLACED THE LEFT COALESCER BAG AND CLEANED OIL OUT OF THE AIR CYCLE MACHINE CANISTER. OPS CEHCKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: COALESCER BAG — DIRTY (AIR DISTRIBUTION)

FLT 4526 - DURING CRUISE FROM MGM-ATL, A SMALL AMOUNT OF SMOKE WAS NOTICED IN THE CABIN WHEN THE RIGHT ACM WAS SELECTED. THE AIRCRAFT LANDED SAFELY IN ATL. MAINTENANCE REMOVED AND REPLACED THE RIGHT COALESCER BAG, AND CLEANED THE COALESCER BAG COVER. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE (M)

Part: PROXIMITY SENSOR — FAILED (MLG)

FLT 4306 - DURING TAKEOFF FROM ATL-CLT, THE CREW SELECTED THE GEAR HANDLE UP, BUT THE NOSE GEAR DID NTO RETRACT. QRH PROCEDURES WERE COMPLIED WITH, AN EMERGENCY DECLARED AND THE AIRCRAFT RETURNED TO ATL, LANDING SAFELY. MAINTENANCE ADJUSTED THE NOSE DOOR PROXIMITY SENSOR SWITCH ON THE RIGHT SIDE AND ALSO CLEANED THE NR 2 DOWN LOCK SWITCH CANNON PLUG ON THE NOSE DOOR IN ADDITION TO CYCLING THE GEAR TWENTY TIMES WITHOUT ANY DEFECTS NOTED. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LIGHT — INOPERATIVE (CABIN)

FLT 4823 - DURING A GROUND INSPECTION IN SHV, THE RIGHT WING AFT EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE RIGHT WING AFT EMERGENCY LIGHT LAMP. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: FITTING — CRACKED (PAX DOOR)

DURING HANGAR MAINTENANCE IN MCN, THE FORWARD PASSENGER DOOR CABLE ANCHOR FITTING WAS FOUND TO BE CRACKED. MAINTENANCE WILL MONITOR THE CRACK AND REPLACE DOOR CABLE FITTING WITHIN 100 FLIGHT HOURS PER REO 601R-11-420. (M)

Part: STEP — CRACKED (FUSELAGE)

DURING HANGAR MAINTENANCE IN MCN, THE BOTTOM PASSENGER DOOR STEP WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE BOTTOM PASSENGER DOOR STEP. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: WIRE — BROKEN (EMERGENCY LIGHT)

DURING HANGAR MAINTENANCE IN MCN, THE CENTER SECTION EMERGENCY FLOOR TRACK WIRES WREE FOUND TO BE BROKEN. MAINTENANCE REPAIRED THE CENTER SECTION EMERGENCY FLOOR TRACK WIRING. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

DURING A C-CHECK IN MCN, THE FLOORBEAM AT FS 280 ENTRY TO THE COCKPIT SECTION WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE FLOORBEAM AT FS 280 ENTRY TO THE COCKPIT SECTION IAW ASA O600-53-0052. (M)

Part: CLIP — CRACKED (FLOORBEAM)

DURING A C-CHECK IN MCN, THE FLOORBEAM CLIPS AT BULKHEAD FS 280, LBL AND RBL 9 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE FLOORBEAM CLIPS AT BULKHEAD FS 280, LBL AND RBL 9 IAW SRM 51-42-20. (M)

Part: WINDSHIELD — CRACKED (COCKPIT)

DURING HANGAR INSPECTION IN BTR, THE NR 3 WINDSHIELD WAS FOUND TO BE CRACKED FROM TOP TO BOTTOM. MAINTENANCE REMOVED AND REPLACED THE NR 3 WINDSHIELD. OPERATIONAL AND PRESSURE CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: BULB — BURNED OUT (CABIN)

FLT 4505 - DURING GROUND INSPECTION IN XNA, THE NR 2 CABIN CEILING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BURNED OUT CEILING EMERGENCY LIGHT BULB. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LIGHT — BURNED OUT (EXTERIOR)

FLT 4505 - DURING SCHEDULED INSPECTION IN XNA, THE LEFT EXTERNAL AFT EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BURNED OUT EXTERNAL EMERGENCY LIGHT BULB. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: HYDRAULIC LINE — CRACKED (LT WING)

FLT 4721 - APPROACH TO MMY, GEAR WAS SELECTED DOWN, RECEIVED A GEAR DISAGREE WARNING WITHIN FIVE SECONDS. THEN RECEIVED A HYDRAULIC NR 3 LOW PRESSURE AND A ZERO PRESSURE WARNING. WHEN THE GEAR WAS SELECTED UP THE MESSAGES CLEARED. AN EMERGENCY GEAR EXTENSION WAS PERFORMED. EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED SAFELY IN MMY. MAINT R&R THE TWO FLEX LINES FOR THE TWO HYDRAULIC PUMPS, 3A AND 3B, AND SERVICED THE HYDRAULIC SYSTEM. THIS WAS NOT THE PROBLEM. UPON FURTHER INSPECTION, THE LEFT WING AILERON OUTBOARD PCU HYDRAULIC LINE AS FOUND TO BE CRACKED AND LEAKING AT FUEL PANEL 550GB. MAINTENANCE REPAIRED CRACKED LINE. OPERATIONAL AND LEAK CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: HYDRAULIC LINE — CRACKED (HYDRAULIC SYS)

FLT 4721 - APPROACH IN MMY, WHEN GEAR WAS SELECTED DOWN, CAPTAIN RECEIVED A GEAR DISAGREEMENT WARNING WITHIN FIVE SECONDS. THE CAPTAIN THEN RECEIVED A HYDRAULIC NR 3 LOW PRESSURE AND A ZERO PRESSURE WARNING MESSAGE. WHEN THE GEAR WAS SELECTED UP THE MESSAGES DECLARED AND THE AIRCRAFT LANDED SAFELY IN MMY. MAINTENANCE REMOVED AND REPLACE THE TWO FLEX LINES FOR THE TWO HYDRAULIC PUMPS, 3A AND 3B, AND SERVICED THE HYDRAULIC SYSTEM. THIS WAS DISCOVERED NOT TO BE THE PROBLEM. UPON FURTHER INSPECTION, THE LEFT WING AILERON OUTBOARD PCU HYDRAULIC LINE WAS FOUND TO BE CRACKED AND LEAKING AT FUEL PANEL 550GB. MAINTENANCE REPAIRED CRACKED LINE. OPERATIONAL AND LEAK CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: CONTROLLER — FAILED (CABIN PRESSURE)

DSM-ATL - FLT 4756 - DURING FLIGHT, CAPTAIN REPORTED PRESSURE UNCONTROLLABLE IN AUTO AND MANUAL. CREW RESET PRESSURE AND MASKS DROPPED. AT FL100 CABIN ALTITUDE 15000 DP -2.1 TO -4.1. CABIN ALTITUDE AND DP WAS FLUCTUATING UP AND DOWN DURNIG DESCENT. AIRCRAFT LANDED SAFELY IN ATL.

Part: MOTOR — INOPERATIVE (HYD PUMP)

FLT 4411 - DURING FLIGHT FROM SBN TO ATL, CREW REPORTED HYDRAULIC 3 PRESSURE EICAS MESSAGE DURING INITIAL DESCENT TOWARD ATL. SYNOPITC PAGE SHOWED HYDRAULIC QTY OF 5 PERCENT IN NR 3. CREW FOLLOWED QRH FOR ABNORMAL PROCEDURES, INCLUDING MANUAL GEAR EXTENSION. CREW DECLARED AN EMERGENCY AND LANDED SAFELY AT BNA. MAINTENANCE ASA REPRESENTATIVES AT BNA REMOVED AND REPLACED SYSTEM 3A ALT CURRENT MOTOR PUMP IAW 29-12-03. OPERATIONAL AND LEAK CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: ACTUATOR — INOPERATIVE (TE FLAP)

FLT 4639 - CREW SELECTED FLAPS TO 8 DEGREES AND FLAPS FAIL MESSAGE APPEARED ON EICAS. CREW FOLLOWED PROCEDURES AS LAID OUT IN ABNORMAL SECTION OF QRH PAGE 8-8. CREW INFORMED ATC OF SITUATION, DECLARED AN EMERGENCY, AND REQUESTED EMERGENCY VEHICLES BE STANDING BY. CAPTIAN SAFELY PERFORMED A ZERO FLAP LANDING. MAINTENANCE REPLACED LEFT AND RIGHT FLAP ACTUATORS, BPSU''S AND FLEX SHAFTS. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: POWER UNIT — INOPERATIVE (TE FLAPS)

FLT 4444 - ON DOWNWIND FOR RUNWAY 22 AT 210 KTS, CREW SELECTED FLAPS TO 8 DEGREES AND FLAPS FAIL MESSAGE APPEARED ON EICAS. CREW FOLLOWED PROCEDURES AS LAID OUT IN ABNORMAL SECTION OF QRH PAGE 8-8. CREW INFORMED ATC OF SITUATION, DECLARED AN EMERGENCY, AND REQUESTED EMERGENCY VEHICLES BE STANDING BY. CAPTAIN SAFELY PERFORMED A ZERO FLAP LANDING. MAINTENANCE REMOVED AND REPLACED THE PDU. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: ACM — FAILED (FUSELAGE)

FLT 4623 - UPON TAXI OUT, THE TOILET SMOKE EICAS MESSAGE ILLUMINATED. THE AIRCRAFT WAS STOPPED AND THE FLGIHT ATTENDANT WAS INSTRUCTED TO INSPECT THE LAVATORY WHILE THE COCKPIT CREW EXECUTED THE APPROPRIATE CHECKLIST. THE CREW WAS INFORMED THAT THERE WAS SMOKE IN THE CABIN AND IT WAS MOVING FORWARD. CAPTAIN OPENED THE COCKPIT DOOR AND VISUALLY SAW THICK SMOKE IN CABIN, EVACUATED THE PASSENGERS, REQUESTED FIRE FIGHTING EQUIPMENT, AND SHUTDOWN THE AIRCRAFT. MAINTENANCE FOUND NO OIL INTHE ACM. REMOVED AND REPLACED THE ACM. OPERATIONAL AND LEAK CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: CONNECTOR — BROKEN (CABIN)

DURING INSPECTION, FOUND FORWARD MOST WIRE CONNECTOR BROKEN ON FLOOR EMERGENCY LIGHTING. MAINTENANCE REPLACED THE EMERGENCY LIGHT WIRE CONNECTOR. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (X)