N906DA

Part: STARTER — ODOR (APU) · airframe 62,075 hrs · 33,875 cycles

APU FAULT MESSAGE WITH ATTEMPTED APU START ACCOMPANIED BY REPORTED UNUSUAL ODOR BY FLIGHT ATTENDANTS IN THE BACK OF AIRCRAFT. APU INSPECTED AND BURN SMELL COMING FROM APU STARTER. R/R APU STARTER MOTOR PER MD90 AMM 49-44. INSPECTED APU STARTER CABLES/WIRE AS REQUESTED. R/R RELAY R2-792 AS PRECAUTION. REPLACED BATTERIES. (LP# 4688972, 4688973, 4688980)

Part: THRUST REVERSER — OUT OF RIG (LEFT) · airframe 59,688 hrs · 32,475 cycles

DIVERTED TO ORD DUE TO LT REVERSER EOAP ILLUMINATED SHORTLY AFTER TAKE OFF. LT REVERSER UNLOCK LIGHT ILLUMINATED. FOUND LT THRUST REVERSER IN THE STOWED LOCKED POSITION AND ALL INDICATION LIGHTS OUT. FWD LT THRUST REVERSER TO MEL 78-32-01. UPDATE 23DEC MSP FOUND UPPER REVERSER HALVES OUT OF RIG. RIGGED UPPER REVERSER PER MM. INSTALLED CROSS OVER FLEX SHAFT. OPERATION CHECKS GOOD. MCO/PLACARD REMOVED.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 59,450 hrs · 32,332 cycles

L2 OVERHEAD EXIT SIGN BROKEN. REMOVED AND REPLACED THE SIGN.

Part: SIGN — MISSING (CABIN) · airframe 58,432 hrs · 31,725 cycles

FORWARD EXIT SIGNS MISSING. REPLACED.

Part: PRESSURE BLKHD — DAMAGED · airframe 57,744 hrs · 31,356 cycles

FASTENER HOLE DAMAGED IN P DOME, ANGLE TAB, FORWARD OUTBOARD HOLE INBOARD OF STRINGER 26L END FITTING. REPAIRED IAW ERA 556923-14, REV O.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 57,125 hrs · 31,013 cycles

TWO BULBS INOPERATIVE AT R1 DOOR EMERGENCY EXIT. REMOVED AND REPLACED THE BULBS. OPERATION CHECKED OKAY.

Part: ANGLE — CRACKED (TAIL) · airframe 52,739 hrs · 28,321 cycles

TAIL INTERIOR SUPPORT ANGLE CRACKED AT LT OTBD END OF VENTRAL STAIR TORQUE TUBE SUPPORT BEAM. COMPLIED WITH PRI 535833-14, REV O. REPAIRED IAW ERA 535833-14, REV O. LP 1945829.

Part: LANYARD — WORN (DOOR SLIDE) · airframe 51,631 hrs · 27,656 cycles

FORWARD RT SERVICE DOOR SLIDE COVER LANYARD CABLE ASSY WORN. R & R SLIDE COVER LANYARD ASSY IAW AMM.

Part: SLIDE — LOW PRESSURE (R1 DOOR) · airframe 49,690 hrs · 26,424 cycles

DURING SERVICE CHECK, FOUND R1 DOOR SLIDE PRESSURE LOW. R & R R1 SLIDE IAW AMDS CARD 2500-4332.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 48,512 hrs · 25,705 cycles

DURING SERVICE CHECK, MX FOUND CEILING EMERGENCY LIGHT 10L INOPERATIVE. FOUND BROKEN SPLICE CONNECTOR OVER CEILING PANEL. REPAIRED IAW SWPM. OPS CHECKS GOOD.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 48,512 hrs · 25,705 cycles

DURING SERVICE CHECK, MX FOUND CEILING EMERGENCY LIGHT 10R, INOPERATIVE. FOUND BROKEN SPLICE CONNECTOR OVER CEILING PANER REPAIRED IAW SWPM. OPS CHECKS GOOD.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 48,512 hrs · 25,705 cycles

DURING SERVICE CHECK, MX FOUND CEILING EMERGENCY LIGHT 37L INOPERATIVE. TROUBLESHOT, FOUND SPLICE CONNECTOR ABOVE CEILING PANEL OPEN. REPAIRED SPLICE CONNECTOR IAW SWPM. OPS CHECKS GOOD.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 48,512 hrs · 25,705 cycles

DURING SERVICE CHECK, MX FOUND CEILING LIGHT 30L , EMERGENCY LIGHT INOPERATIVE. FOUND BROKEN SPLICE CONNECTOR ABOVE OVERHEAD PANEL. REPAIRED IAW SWPM. OPERATION CHECKS GOOD.

Part: FLOOR SUPPORT — CRACKED (BS 344-360) · airframe 48,233 hrs · 25,534 cycles

FORWARD WET ARE, BS 344 - 360, LBL 11, FLOOR SUPPORT INTERCOSTAL IS CRACKED AT NUTPLATE HOLE. REMOVED AND REPLACED INTERCOSTAL IAW DWG 141A5400.

Part: FLOORBEAM — CORRODED (BS 1364) · airframe 48,233 hrs · 25,534 cycles

FLOORBEAM AT BS 1364 HAS CORROSION ON THE BEAM. REPAIRED OUT OF LIMITS FLOORBEAM IAW ERA 516865-14, REV O.

Part: PRESSURE BLKHD — CORRODED · airframe 48,233 hrs · 25,534 cycles

AFT PRESSURE BULKHEAD, ON LOWER DOOR JAMB VERTICAL FRAME, CORRODED. REMOVED CORROSION. MATERIAL LOSS IS OUT OF LIMITS. REPAIRED IAW ERA 516848-14, REV O, PRI 516848, REV O.

Part: DOOR FRAME — GOUGED (PAX DOORWAY) · airframe 48,233 hrs · 25,534 cycles

AFT CABIN ENTRY DOOR FRAME, BOTTOM SIDE, IS GOUGED IN SEVERAL AREAS. REMOVED DAMAGE. FOUND TO BE OUT OF LIMITS. R & R CHANNEL IAW SRM 51-30-05, 51-30-02 AND 51-30-04.

Part: DOOR FRAME — GOUGED (PAX DOORWAY) · airframe 48,233 hrs · 25,534 cycles

AFT CABIN ENTRY DOOR FRAME IS GOUGED IN SEVERAL PLACES. REMOVED DAMAGE. FOUND TO BE OUT OF LIMITS. R & R CHANNEL IAW SRM 51-30-05, 51-30-02, 51-30-04.

Part: SKIN — CHAFED (NR 2 PYLON) · airframe 48,233 hrs · 25,534 cycles

NR 2 ENGINE PYLON LOWER SKIN HAS CHAFING DAMAGE AT OTBD END FROM FRONT SPAR TO AFT ENGINE MOUNT. REPAIRED CHAFING IAW ERA PRI 561053-14, REV 1, ERA 516053-14, REV O.

Part: FRAME — DENTED (CARGO DOOR) · airframe 48,233 hrs · 25,534 cycles

AFT CARGO DOOR, FORWARD INNER FRAME EDGE HAS DENT APPROXIMATE 6 INCHES BELOW CENTER OF DOOR SKIN OVERLAP. ACCOMPLISH REPAIR TO AFT CARGO DOOR INNER PAN LOWER FORWARD EGE IAW ERA 516850-14, REV O.

Part: DOOR FRAME — GOUGED (PAX DOORWAY) · airframe 48,233 hrs · 25,534 cycles

AFT CABIN ENTRY DOOR LOWER RT FRAME GOUGED. R & R AFT CABIN ENTRY DOOR LOWER RT IAW SRM 51-30-02, 51-30-01, AND DWG 9929480.

Part: CUSP WEB — CRACKED (BS 1360) · airframe 48,233 hrs · 25,534 cycles

BS 1360, CUSP WEB HAS CRACK. REPAIRED CRACKED CUSP WEB IAW SRM 53-20-02.

Part: SKIN — CRACKED (BS 1475) · airframe 48,233 hrs · 25,534 cycles

WHILE ACCOMPLISHING REPETITIVE INSPECTION OF FUSELAGE SKIN REPAIR AT BS 1475 BETWEEN LONGERONS 1 AND 3R, FOUND REPAIR TO HAVE 2" CRACK IN RADIUS, STA 1475 BETWEEN LONGERON 1 AND L2R AT INBD DAMAGE CUTOUT. R & R ANGLE IAW SRM 51-30-05.

Part: CUSP WEB — CRACKED (BS 1360) · airframe 48,233 hrs · 25,534 cycles

PASSENGER CABIN STA 1360, RIGHT CUSP WEB HAS CRACK. REMOVED, FABRICATED, TREATED, PRIMED AND INSTALLED FILLER AND DOUBLER IAW SRM 51-10-03, 51-30-02.

Part: CUSP WEB — CORRODED (BS 1267-1305) · airframe 48,233 hrs · 25,534 cycles

MAIN CABIN LT CUSP WEB IS CORRODED FROM STA 1267 -1305. R & R DAMAGED CUSP WEB IAW SRM 51-30-02, 51-30-03, AND 51-10-05.

Part: SPAR CAP — DAMAGED (VERTICAL STAB) · airframe 48,233 hrs · 25,534 cycles

DURING NDT INSPECTION FOUND 1EACH FASTENER HOLE WITH CRACK ON RT VERTICAL STAB FRONT SPAR CAP FORWARD FLANGE. STA ZFS-52.267. REMOVED UPPER L/E SURFACE AND REMOVED DAMAGE. HFEC TRIMOUT. NO DEFECTS NOTED. FABRICATED REPAIR ANGLE, STRAP AND FILLERS IAW DWG 09550005. 3 RIBS BELOW REPAIR, DERIVETED FOM AND RIVETS REINSTALLED. OPEN HOLES DURING REPAIR HFEC INSPECTED. NO DEFECTS NOTED.

Part: CUSP WEB — DAMAGED (BS 883) · airframe 48,233 hrs · 25,534 cycles

CUSP WEB AT BS 883+14" LT SIDE HAS DAMAGE. REPAIRED CUSP WEB IAW SRM 53-20-02, FIG 28.

Part: CUSP WEB — CORRODED (BS 655-674) · airframe 48,233 hrs · 25,534 cycles

RIGHT CABIN CUSP WEB BS 655-674 CORRODED. FOUND OUT OF LIMITS. FABRICATED AND INSTALLED WEB IAW SRM 53-10-02 AND DWG 990443, REV A.

Part: SEAT TRACK — CORRODED (BS 735) · airframe 48,233 hrs · 25,534 cycles

PASSENGER CABIN LT OTBD SEAT TRACK, BS 735 HAS CORROSION. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. R & R SEAT TRACK IAW AMM.

Part: BULKHEAD — CORRODED · airframe 48,233 hrs · 25,534 cycles

AFT PRESSURE BULKHEAD, UNDERSIDE OF DOOR FRAME IS CORRODED. REMOVED CORROSION. 100 PERCENT MATERIAL LOSS. R & R DOOR SILLL IAW DWG 5917579, SRM 51-10-4, 51-10-05, 51-10-03, 51-30-01, AND 53-00-01.

Part: CUSP WEB — CORRODED (BS 598-617) · airframe 48,233 hrs · 25,534 cycles

MAIN CABIN BS 598 - 617 LBL 60 CUSP WEB UPPER SURFACE HAS CORROSION. REPAIRED OUT OF LIMITS CUSP WEB IAW SRM 53-20-02.

Part: CUSP WEB — CORRODED (BS 617-636) · airframe 48,233 hrs · 25,534 cycles

MAIN CABIN BS 617-636 LBL 60 CUSP WEB UPPER SURFACE HAS CORROSION. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED REPAIR IAW SRM 53-20-02, FIG 12, 51-10-03, 51-30-02.

Part: CUSP WEB — DAMAGED (BS 552) · airframe 48,233 hrs · 25,534 cycles

CUSP WEB BS 552 DAMAGED. FOUND TO BE OUT OF LIMITS. REMOVED, FABRICATED, TREATED, PRIMED AND INSTALLED REPAIR DOUBLER AND FILLER IAW SRM 51-30-00, 51-30-01, 53-20-02, 51-10-03.

Part: CUSP WEB — CORRODED (BS 544) · airframe 48,233 hrs · 25,534 cycles

MAIN CABIN BS 544, LBL 60 CUSP WEB UPPER SURFACE HAS CORROSION. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED REPAIR IAW SRM 53-20-02, FIG 12, 51-10-03, 51-30-02.

Part: CUSP WEB — DAMAGED (BS 698) · airframe 48,233 hrs · 25,534 cycles

RIGHT CABIN CUSP WEB, BS 698 DAMAGED. REMOVED DAMAGE AREA AND REPAIRED IAW SRM 53-20-02, FIG 19.

Part: SEAT TRACK — CORRODED (BS 579-588) · airframe 48,233 hrs · 25,534 cycles

LEFT OTBD CABIN SEAT TRACK CORRODED, BS 579-588, LBL 54. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. R & R SEAT TRACK IAW SRM 53-40-01, FIG 6 AND 51-30-01, PG 1.

Part: CUSP WEB — DAMAGED · airframe 48,233 hrs · 25,534 cycles

CUSP WEB DAMAGED. FABRICATED DOUBLER, RING DOUBLER AND CUSP WEB IAW SRM 51-30-02, 53-20-02, FIG 19, 51-10-03 PARA 21.

Part: FLOORBEAM — CORRODED (BS 179) · airframe 48,233 hrs · 25,534 cycles

FORWARD WET AREA, FLOORBEAM HAS CORROSION ON TOP TEE BS 179 FROM LBL 17-38. REMOVED CORROSION. FOUND OUT OF LIMITS. REPLACED FLOORBEAM TEE IAW SRM 51-30-02 PARA 1.

Part: FLOOR SUPPORT — CORRODED · airframe 48,233 hrs · 25,534 cycles

MAIN CABIN BS 148+9, RBL 58 FLOOR SUPPORT ANGLE HAS CORROSION. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED ANGLE IAW SRM 51-30-02.

Part: FRAME — CORRODED (BS 1366) · airframe 48,233 hrs · 25,534 cycles

AFT CARGO FRAME, BS 1366, HAS AREAS OF CORROSION BETWEEN LONGERONS 28L AND 28R. TASK 35-302-07. FOUND TO BE OUT OF LIMITS. REPAIRED IAW SRM 53-10-02, FIG 2.

Part: SEAT TRACK — CORRODED (BS 1210-1212) · airframe 48,233 hrs · 25,534 cycles

BS 1210-1212, LBL 45 SEAT TRACK HAS CORROSION AROUND FLOORBOARD HOLES. REPAIRED SEAT TRACK. R & R WITH NEW REPAIR SECTION IAW SRM 53-40-01.

Part: SUPPORT — CORRODED (R1 DOOR) · airframe 48,233 hrs · 25,534 cycles

R1 DOOR, CLOSE OUT ABOVE FIBERGLASS SUPPORT CORRODED. BOTTOM SECTION IS OUT OF LIMITS 100 PERCENT MATERIAL LOSS. REPLACED BOTTOM SECTION IAW SRM 51-00-01, 51-30-00, 51-10-03, 51-10-04, 51-30-02 ADN 51-30-01.

Part: SUPPORT FRAME — CRACKED (BS 998) · airframe 48,233 hrs · 25,534 cycles

LOWER FUSELAGE AT KEELBEAM, BS 998, RBL 6, LANDING GEAR DOOR SUPPORT FRAME IS CRACKED. REMOVED CHANNEL (FRAME) AT KEEL BEAM, STA 998, RBL 6. LOCATED, DRILLED AND INSTALLED NEW CHANNEL (FRAME) IAW SRM 51-30-02 AND 51-30-05 AND DWG 5930584.

Part: SEAT TRACK — CORRODED (BS 845) · airframe 48,233 hrs · 25,534 cycles

SEAT TRACK AT RBL 56, BS 845+12 HAS CORROSION. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. R & R SEAT TRACK IAW SRM 53-40-01, FIG 6 AND 51-30-01 PAGE 1.

Part: FITTING — CRACKED (BS 845) · airframe 48,233 hrs · 25,534 cycles

FORWARD KEEL BEAM FITTING ON RIGHT SIDE AT BS 845 HAS A CRACK LOCATED NEAR RADIUS. R & R KEEL BEAM FITTING ON RT SIDE AT STA 845 IAW SRM 51-30-05 AND DWG 5936360, REV BE.

Part: CUSP WEB — CORRODED (BS 494) · airframe 48,233 hrs · 25,534 cycles

RIGHT CABIN CUSP WEB, PREVIOUS REPAIR, CORRODED, BS 494. BLENDED CORROSION. FOUND TO BE OUT OF LIMITS. CUTOUT DAMAGED AREA. FABRICATED, TREATED, PRIMED AND INSTALLED REPAIR PARTS IAW SRM 51-10-03, 53-20-02. REMOVED AND REINSTALLED SEAT TRACK IAW SRM 51-30-01.

Part: SKIN — CORRODED (BS 807-826) · airframe 48,233 hrs · 25,534 cycles

RIGHT SIDE RUBSTRIP AREA HAS CORROSION ON ACFT SKIN AT BS 807 -826. FOUND DURING NEW RUB STRIP INSTALLATION. BLENDED OUT CORROSION. FOUND TO BE OUT OF LIMITS. FABRICATED, ALODINED, PRIMED ADN INSTALLED DOUBLER IAW SRM 51-30-01, 53-30-01, 53-31-01.

Part: CUSP WEB — CORRODED (BS 494) · airframe 48,233 hrs · 25,534 cycles

RT CABIN CUSP WEB CORRODED BS 494, TASK 53-211-02. BLENDED CORROSION. FOUND TO BE OUT OF LIMITS. CUTOUT DAMAGED AREA IAW SRM 53-00-01. FABRICATED AND INSTALLED REPAIR IAW SRM 53-20-02.

Part: CUSP WEB — CORRODED (BS 303) · airframe 48,233 hrs · 25,534 cycles

RIGHT CABIN CUSP WEB CORRODED BS 303, BLENDED CORROSION. FOUND TO BE OUT OF LIMITS. REMOVED AND INSTALLED REPAIRED PARTS IAW SRM 53-20-02.

Part: FLOOR SUPPORT — CORRODED (BS 160-200) · airframe 48,233 hrs · 25,534 cycles

FORWARD WET AREA, FLOOR SUPPORT LOCATED LBL 7, BS 160-200 HAS MULTIPLE AREAS OF CORROSION. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. LOCATED, INSTALLED AND DRILLED NEW PART IAW SRM 51-10-03, 53-00-01, 51-40-00, 51-10-06 AND 51-30-01.

Part: FLOORBEAM — CORRODED (BS 200) · airframe 48,233 hrs · 25,534 cycles

MAIN CABIN BS 200, RBL 42 - 52, FLOORBEAM UPPER TEE HAS MULTIPLE AREAS OF CORROSION. R & R FLOORBEAM TEE IAW SRM 51-30-02. CORROSION FOUND TO BE OUT OF LIMITS.

Part: FLOORBEAM — CORRODED (BS 200) · airframe 48,233 hrs · 25,534 cycles

MAIN CABIN BS 200, RBL 42 - 52, FLOOR SUPPORT UPPER SURFACE HAS MULTIPLE AREAS OF CORROSION. R & R FLOOR SUPPORT IAW SRM 51-30-02. CORROSION WAS FOUND TO BE OUT OF LIMITS.

Part: FRAME — CORRODED (BS 1328) · airframe 48,233 hrs · 25,534 cycles

AFT CARGO BILGE FRAME CORRODED BS 1328, LONGERON 28 - 28R TASK 53-302-07. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. R & R FRAME AT STA 1328, LONGERON 28L -28R IAW SRM 51-30-02, PG 1-6.

Part: SEAT TRACK — CORRODED (BS 1159-1163) · airframe 48,233 hrs · 25,534 cycles

PASSENGER CABIN SEAT TRACK, BS 1159-1163 LBL 55, UPPER SURFACE OF CROWN IS CORRODED. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. R & R IAW SRM 53-40-01, FIG 2.

Part: LONGERON SPLICE — CORRODED (BS 1350-1362) · airframe 48,233 hrs · 25,534 cycles

AFT CARGO BILGE, LONGERON 30, SPLICE CORRODED AROUND RUSTED FASTENERS BS 1350-1362. REPLACED CORRODED SPLICE ON LONGERON 30, STA 1350-1362 IAW SRM 51-30-05, PG 3 , 53-10-01, PG 11-18 AND DWG 5940866.

Part: FRAME — CORRODED (BS 1379) · airframe 48,233 hrs · 25,534 cycles

AFT CARGO FRAME, BS 1379, BETWEEN LONGERONS 28L - 28R, HAS AREAS OF CORROSION ON FWD SIDE OF FRAME. FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED PARTS IAW SRM 53-10-02.

Part: SEAT TRACK — CORRODED (BS 1359-1360) · airframe 48,233 hrs · 25,534 cycles

PASSENGER CABIN SEAT TRACK BS 1359 -1360, LBL 22, UPPER SURFACE OF CROWN IS CORRODED. BLENDED CORROSION. FOUND TO BE OUT OF LIMITS. REMOVED SEAT TRACK, TREATED, PRIMED, PAINTED AND INSTALLED SEAT TRACK IAW SRM 53-40-01, FIG 6, 51-30-03, 51-10-03 AND 51-10-43, PARA 21, 14.11.

Part: SEAT TRACK — CORRODED (BS 254) · airframe 48,233 hrs · 25,534 cycles

LEFT OTBD CABIN SEAT TRACK CORRODED BS 254, LBL 54. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. R & R SEAT TRACK IAW SRM 53-40-01.

Part: CUSP WEB — CORRODED (BS 268) · airframe 48,233 hrs · 25,534 cycles

LEFT CABIN CUSP WEB CORRODED AT BS 268. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. FABRICATED, TREATED, PRIMED, PAINTED AND INSTALLED REPAIR DOUBLER IAW SRM 51-10-03 AND 53-20-02.

Part: ATTACH ANGLE — CRACKED (BS 522) · airframe 48,233 hrs · 25,534 cycles

FORWARD CARGO, AFT BULKHEAD LOWER ATTACH ANGLE CRACKED, BS 522, LONGERON 29L. INSTALLED NEW ANGLE IAW DWG 5936592 AND SRM 51-30-02.

Part: CUSP WEB — CORRODED (BS 803) · airframe 48,233 hrs · 25,534 cycles

RIGHT CABIN CUSP WEB CORRODED, BS 788-807, TASK 53-211-02. REMOVED CORROSION. 100 PERCENT MATERIAL LOSS. INSTALLED REPAIR AT BS 803 IAW SRM 53-00-01, 51-10-03 AND 53-20-02.

Part: SEAT TRACK — GOUGED (BS 883-984) · airframe 48,233 hrs · 25,534 cycles

PASSENGER CABIN SEAT TRACK AT RBL 22 INBD LOWER FLANGE GOUGED FROM FS 883 TO 984+8". REPAIRED DAMAGED SEAT TRACK BS 883 - 921, IAW SRM 53-40-01, FIG 6.

Part: SEAT TRACK — CORRODED (BS 207-216) · airframe 48,233 hrs · 25,534 cycles

MAIN CABIN BS 207+6 TO 216+10, RBL 55, SEAT TRACK INBD AND OTBD UPPER FLANGE HAS MULTIPLE AREAS OF CORROSION. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. REMOVED AND REPAIRED SEAT TRACK FROM STA 207 TO 266, RBL 55 IAW SRM 53-40-01, FIG 6 AND SRM 51-30-01.

Part: CUSP WEB — CORRODED (BS 522-532) · airframe 48,233 hrs · 25,534 cycles

RIGHT CABIN CUSP WEB CORRODED, BS 522-532. CUTOUT CORROSION. FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW SRM 51-10-03, 53-00-01, 53-20-02 AND AMM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 48,233 hrs · 25,534 cycles

FORWARD WET AREA, FLOORBOARD SUPPORT HAS CORROSION AROUND SCREW HOLE AREA ON UPPER AND LOWER FLANGE SURFACE. TASK 53-211-01. R & R FLOORBOARD SUPPORT IAW SRM 51-30-02 AND 51-30-05.

Part: STRUCTURE — CRACKED (CARGO DOOR) · airframe 48,233 hrs · 25,534 cycles

AFT CARGO BAY DOOR, AFT EDGE, 1ST FROM TOP STOP PAD FITTING, IS CRACKED AND LOOSE. INSTALLED AFT CARGO DOOR AFT UPPER EDGE TOP STOP PAD FITTING IAW SRM 51-10-05, FIG 1 AND FIG 4 AND OM 52-30-1, FIG 1 SHEET 5 (T).

Part: SEAT TRACK — CORRODED (COCKPIT) · airframe 48,233 hrs · 25,534 cycles

F/O OTBD SEAT TRACK AFT CORNER HAS CORROSION. COMPLIED WITH ERA 51601-14, REV O AND PRI ER/A 516041-14, REV O.

Part: WEB — CORRODED (BS 195-200) · airframe 48,233 hrs · 25,534 cycles

FORWARD WET AREA, FLOOR WEB IN FRONT OF SERVICE DOOR, CORRODED, BETWEEN BS 195 AND 200, RBL 45 - 53. REMOVED DAMAGE, REPAIRED IAW SRM 51-11-01 AND 51-30-02.

Part: WEB — DAMAGED (BS 195-200) · airframe 48,233 hrs · 25,534 cycles

FORWARD WET AREA FLOOR WEB IN FRONT OF SERVICE DOOR CORRODED BETWEEN FS 195 - 200 RBL 45 & 53. REMOVED DAMAGE, REPAIRED IAW SRM 51-11-01 AND 51-30-02.

Part: CARGO TRACK — CORRODED (BS 1269-1307) · airframe 48,233 hrs · 25,534 cycles

CARGO TRACK CORRODED, BS 1269-1307, TASK 53-302-07. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. R & R CARGO TRACK IAW SRM 51-30-01 AND 53-40-01, FIG 7, PG 40, 47.

Part: SEAT TRACK — CORRODED (BS 757-769) · airframe 48,233 hrs · 25,534 cycles

SEAT TRACK AT RBL 56 HAS CORROSION FROM FS 757+6 TO FS 769. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. R & R SEAT TRACK IAW SRM 53-40-01, 51-10-03, 51-10-05 AND 53-42-01-020-801.

Part: SEAT TRACK — CORRODED (BS 237) · airframe 48,233 hrs · 25,534 cycles

BS 237, RBL 45, SEAT TRACK CORRODED. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. R & R SEAT TRACK BS 200 -247, IAW SRM 51-30-05.

Part: SHEAR TIE — CORRODED (BS 408) · airframe 48,233 hrs · 25,534 cycles

FORWARD CARGO BAY, SHEAR TIE FOR FS 408 BETWEEN LONGERONS 29-30R HAS CORROSION. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. R & R SHEAR TIE IAW SRM 53-10-02.

Part: SKIN — CORRODED (FUSELAGE) · airframe 48,233 hrs · 25,534 cycles

DOME NUT MATING SURFACES IN THE AFT CARGO BAY, CORRODED. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. REPAIRED DAMAGE IAW SRM 53-30-01, PARA II, 51-10-03 PARA 26, PROCESS STANDARD 900-5-1, NR 4.

Part: CUSP WEB — CORRODED (BS 474) · airframe 48,233 hrs · 25,534 cycles

RIGHT CABIN CUSP WEB CORRODED BS 474, TASK 53-211-02. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. REMOVED DAMAGE PARTS AND INSTALLED REPAIR PARTS IAW SRM 51-30-02.

Part: SHEAR TIE — CORRODED (BS 1344) · airframe 48,233 hrs · 25,534 cycles

AFT CARGO, FRAME SHEAR TIE HAS CORROSION BS 1344 LONGERON 28L - 28R. AFTER REPLACEMENT OF THE SHEAR TIE, THERE ARE SEVERAL FASTENERS INSTALLED INCORRECTLY ORIGINAL LP 0971305. REPLACED OR SHAVED RIVETS IAW SRM 51-30-02.

Part: FITTING — CRACKED (CARGO DOOR) · airframe 48,233 hrs · 25,534 cycles

AFT CARGO COMPARTMENT DOOR, FORWARD EDGE TOP DOOR STOP FITTING IS CRACKED AND PAD IS LOOSE IN FITTING. R & R AFT CARGO COMPARTMENT DOOR FORWARD EDGE TOP DOOR STOP FITTING IAW SRM 51-30-05, PARA 7 AND PARA 8, VOL II.

Part: FITTING — CRACKED (CARGO DOOR) · airframe 48,233 hrs · 25,534 cycles

AFT CARGO COMPARTMENT DOOR, FORWARD EDGE 2ND FROM BOTTOM DOOR STOP FITTING IS CRACKED AND PAD IS LOOSE. R & R AFT CARGO COMPARTMENT DOOR, FORWARD EDGE 2ND FROM BOTTOM DOOR STOP FITTING IAW SRM 51-30-05, PARA 7 AND PARA 8, VOL II.

Part: SEAT TRACK — GOUGED (BS 943) · airframe 48,233 hrs · 25,534 cycles

PASSENGER CABIN SEAT TRACK AT RBL 22 IS GOUGED AT FS 943+14". REMOVED GOUGES. FOUND TO BE OUT OF LIMITS. REMOVED PARTS, LOCATED, DRILLED, TREATED, PRIMED AND INSTALLED NEW SERVICEABLE PARTS IAW SRM 53-40-01, PGS 1-25.

Part: SKIN — CRACKED (VERTICAL STAB) · airframe 47,186 hrs · 24,940 cycles

FUSELAGE SKIN OTBD OF RIGHT VERTICAL STABILIZER SKATE ANGLE CRACKED. CRACKS TRIMMED OUT, HFEC INSPECTED FOR CONTAINMENT. REPAIRED IAW SG09530003-7011 AND ER/A 510725-14.

Part: SKIN — CRACKED (VERTICAL STAB) · airframe 47,186 hrs · 24,940 cycles

FUSELAGE SKIN OTBD OF LT VERTICAL STABILIZER SKATE ANGLE CRACKED. TRIMMED OUT AND HFEC FOR CONTAINMENT. REPAIRED SG09530003-7009 AND ER/A 510732-14. RII C/W QC1984.

Part: SKIN — CRACKED (BS 1494) · airframe 47,173 hrs · 24,935 cycles

FUSELAGE SKIN CRACKED AT STA 1494, 4" OTBD OF VERTICAL STABILIZER LEFT SKATE ANGLE. VERIFIED WITH HFEC AND MARKED ENDS. REMOVED SKIN DAMAGE 1" DIAMETER AT THIS LOCATION. HFEC, DAMAGE CONTAINED. FABRICATED FILLER AND DOUBLER IAW SRM 53-00-01, PARA 8. TREATED AND PRIMED NEW DOUBLER AND FILLER. OK TO INSTALL QC202. INSTALLED DOUBLER IAW SRM 53-00-01.

Part: BALLAST — INOPERATIVE (EMERGENCY LIGHTS) · airframe 45,969 hrs · 24,263 cycles

DURING SERVICE CHECK, MAINTENANCE FOUND LEFT AND RIGHT OVERHEAD EMERGENCY FLOOD LIGHTS ROW 2, INOPERATIVE. REMOVED AND REPLACED BALLAST PER AMM. OPS CHECKEDS GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 45,940 hrs · 24,245 cycles

DURING SERVICE CHECK, MAINTENANCE FOUND 2 EMERGENCY BULBS INOPERATIVE IN EXIT SIGNS IN AFT STAIRWELL TAIL CONE. LAMPED, OPS CHECKED GOOD.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 45,575 hrs · 24,061 cycles

DURING SERVICE CHECK, MAINTENANCE FOUND FORWARD EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED POWER SUPPLY AND BATTERIES PER AMM. OPERATION CHECKED NORMAL.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT) · airframe 45,404 hrs · 23,968 cycles

DURING SERVICE CHECK, MAINTENANCE FOUND EMERGENCY LIGHT ABOVE SEAT 37AB INOPERATIVE. FOUND CONNECTOR DISCONNECTED, RECONNECTED. OPS CHECKED OKAY.

Part: GLOWSTRIP — INOPERATIVE (CABIN) · airframe 43,625 hrs · 23,117 cycles

DURING LINE CHECK, MAINTENANCE FOUND 8 INCHES OF EMERGENCY ESCAPE PATHWAY PHOTO LUMINESCENT STRIP INOPERATIVE AT DOOR 2L JUMP SEAT. MCO/PLACARD INSTALLED PER MEL 33-51-01B. MAINTENANCE INSTALLED 8 INCHES OF PHOTO LUMINESCENT EMERGENCY PATH LIGHTING PER MAINTENANCE MANUAL. MCO/PLACARD REMOVED. OPERATION CHECKS GOOD. AIRCRAFT OKAY FOR SERVICE.

Part: GLOWSTRIP — MISSING (CABIN) · airframe 43,625 hrs · 23,117 cycles

DURING LINE CHECK, MAINTENANCE FOUND 7 INCHES OF PHOTO LUMINESCENT EMERGENCY PATHWAY LIGHTING MISSING ON THE RIGHT SIDE ROW 26. MCO/PLACARD INSTALLED PER MEL 33-51-01B. MAINTENANCE INSTALLED 7 INCHES OF EMERGENCY PATHWAY LIGHTING PER MAINTENANCE MANUAL. MCO/PLACARD REMOVED. OPERATION CHECKS GOOD.

Part: LANYARD — DISCONNECTED (EVAC SLDIE) · airframe 42,971 hrs · 22,797 cycles

DOOR 1L SLIDE LANYARD FOUND DISCONNECTED. MAINTENANCE RECONNECTED. AIRCRAFT OKAY FOR SERVICE.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 42,031 hrs · 22,379 cycles

FLIGHT CREW NOTIFIED MCC, VIA ACARS THAT 1R DOOR SLIDE PANEL FELL OFF AND SLIDE PACK FELL OUT. MAINTENANCE RE-INSTALLED SLIDE PER MAINTENANCE MANUAL. ALL CHECKS GOOD. AIRCRAFT OKAY FOR SERVICE.

Part: SKIN — DENTED (BS 271 L29-30R) · airframe 41,743 hrs · 22,263 cycles

FUSELAGE DENTED AT STA 271 BETWEEN LONGERON 30 AND LONGERON 29RT. DENT CAUSED BY MAINT ATTEMPT TO JACK ACFT AT FWD LAV DRAIN HOLE DURING NLG STRUT SERVICING. DENT WAS CUT-OUT AND REPAIRED IAW ERA 488513-14. NON ROUTINE NR1.

Part: ACTUATOR — INTERMITTENT (NLG DOOR) · airframe 41,019 hrs · 21,939 cycles

ACTION CLIMBING THROUGH 11,000 FT AND ACCELERATING THROUGH 310 KNOTS, NOSE GEAR DOOR CAME OPEN. SLOWED TO 250 KNOTS, DOOR APPEARED TO CLOSE. REPLACED NOSE GEAR DOOR LINK ACTUATOR AND RIGGED SAME IAW AMM. PERFORMED NOSE GEAR RETRACTION CHECK.

Part: RELEASE MECH — LACK OF LUBE (LANDING GEAR) · airframe 40,994 hrs · 21,929 cycles

THE ACFT RETURNED TO DEPARTURE, DUE TO VIBRATION FELT IN THE NOSE AREA DURING TAKEOFF. MX FOUND THE LT NOSE GEAR DOOR OPEN ON LANDING. THE DOOR RELEASE HANDLE WAS CLEANED, LUBED, AND CYCLED. FUNCTIONAL CHECK OF THE DOOR CLOSING AND SECURING WAS NORMAL.

Part: LIGHT — DAMAGED (CABIN) · airframe 40,487 hrs · 21,710 cycles

CREW WROTE UP EMERGENCY FLOOR LIGHT AT ROW 39C AS DAMAGED AND INOPERATIVE. MAINTENANCE RE-INSTALLED LIGHTING CONDUIT AND SPLICED AS NEEDED. OPERATIONAL CHECK OF LIGHT NOW CHECKS GOOD (2010-D0813)(DLM90101774).

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 39,881 hrs · 21,364 cycles

INBOUND PILOT CREW WROTE UP 4 EMERGENCY TRACK LIGHTS WERE OUT AT ROW 10-13. SLC. MX REPAIRED BROKEN WIRE IN LIGHT TRACK. OPS OF EMERGENCY LIGHTS NOW OPERATIONAL.

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS) · airframe 39,782 hrs · 21,313 cycles

EMERGENCY RED LIGHT AT 28C INOPERATIVE. REPLACED BULB AND LIGHT SOCKET ASSY. SYS CHECKS GOOD.

Part: STRUT — DISCHARGED (NLG) · airframe 39,395 hrs · 21,117 cycles

RED NOSE POSITION LIGHT REMAINED ILLUMINATED AFTER T/O RETRACTION. PERFORMED NLG STRUT EXT CHECK, FOUND X DIMENSION BELOW LIMITS. SERVICED NOSE STRUT TO PROPER LIMITS. JACKED ACFT NOSE RETRACTED NOSE GEAR SEVERAL TIMES. OPS OK. RETURNED ACFT TO NORM CONFIG.

Part: DOOR — OUT OF RIG (NLG) · airframe 38,959 hrs · 20,871 cycles

AFTER RAISING LANDING GEAR ON T/O EXPERIENCED VERY LOUD VIBRATION IN NOSE AREA. SLOWED DOWN PUT GEAR DOWN AND NOISE DECREASED MAX SPEED 200 KTS VIBRATION VBS. STILL BAD AT 160 KTS. RIGGED NOSE DOORS PER M/M. CYCLED GEAR SEVERAL TIMES, ALL INDICATIONS NORMAL. OK FOR SERVICE.

Part: ACTUATOR — MALFUNCTIONED (LT ENG STATER) · airframe 34,834 hrs · 18,464 cycles

LEFT ENGINE SHUT ITSELF DOWN ON APPROACH INTO SEA. LEFT ENG RESTARTED. REPLACED L ENG STATOR VANE ACTUATOR PER AMM, STILL NEEDS L CHECK AND ENG TEST NR 3 AND 11, DC 690463. LEAK CHECKS E AND C/W TEST NR 3 AND NR 11.

Part: CONTROL VALVE — ICED (MLG) · airframe 34,625 hrs · 18,337 cycles

WHEN ATTEMPTING TO LOWER THE LANDING GEAR FOR LANDING "LANDING GEAR HANDLE JAMMED UP." INSPECTED GEAR WELL AREA, FOUND ICE ON CABLES FOR LANDING GEAR CONTROL VALVE. FOUND RT AUTODRAIN VALVE AND TUBE PLUGGED. ALSO FOUND ALL FOUR EMERGENCY EXITS OVERWING DOOR SEALS ON POOR CONDITION AND CABIN FLOOR AREA WAS WET. REPLACED EMERGENCY DOOR SEAL REF ITEMS 004, 005, 006, 007, 008, 009, 016. PERFORMED GEAR SWING AFTER JACKING A/C. NO FURTHER TROUBLES FOUND.

Part: ESCAPE HATCH — LOOSE (FUSELAGE) · airframe 34,505 hrs · 18,266 cycles

FLIGHT DIVERTED TO DEN DUE TO FLAPS NOT DEPLOYING AND GEAR HANDLE WOULD NOT MOVE TO THE DOWN POSITION. AFTER ARRIVAL SYS CK FOUND FLAPS AND GEAR HANDLE OPS NML. FOUND WATER IN AREA OF FLOOR WHERE CABLES AND FAIRLEADS FOR FLAP AND GEAR ACTUATION PASS INTO THE GEAR WELL. FOUND ALL 4 OVERWING EXIT DOORS OUT OF RIG. THEY DID NOT HAVE THE MIN AMOUNT OF PRESS. REQUIRED TO LATCH THE DOOR. NO OTHER CAUSE OF WATER SOURCE FOUND. REMOVED WATER, ADJUSTED OVERWING DOORS PER M/M. SUSPECT WATER MIGRATED FROM OVERWING DOOR AND INTO AREA AND FROZE FAIRLEADS. A/C BACK IN SERVICE 04:30 02/02/08.

Part: CONVERTER — FAULTED (LT AC POWER) · airframe 34,336 hrs · 18,171 cycles

LT AC PWR FAULT. REMOVED AND REPLACED VSC CONVERTER PER AMM. OPS GOOD PART NO 1B189-5.

Part: B-NUT — LOOSE (HYD LINE) · airframe 34,027 hrs · 17,987 cycles

ACFT DECLARED EMERGENCY FOR LOW LEFT SYSTEM HYDRAULIC QTY. TIGHTENED B NUT TO BRAKE ACCUMULATOR. SERVICED HYDRAULIC SYSTEM LEAK CHECK OK.

Part: ENGINE — INTERMITTENT (NR 1) · airframe 33,383 hrs · 17,629 cycles

LT ENG STRAINER CLOG ILLUMINATED DURING INITIAL CLIMB COMPLETED WITH CK LIST AND RETURNED TO LAND. ENG WAS NOT SHUT DOWN AND LANDING WAS NOT OVERWEIGHT. INSP/CLEANED SCAVENGE OIL FILTER PER MEL REF. NO DEPOSITS NOTED. FWD TO MCO AND PLAC PER MEL 79-36-01. ITEM TO CKD ONCE EACH FLT DAY. RAN ENG NO LEAKS. FOUND DEFECTIVE WIRING OB OF PYLON CONNECTOR. REPAIRED WIRING RAN ENGINE. ENG INDICATIONS NORMAL. MCO AND PLAC RMVD. REMOVED C FILTER LK CK OK.

Part: CONTROL VALVE — INOPERATIVE (LT A/C PACK) · airframe 33,168 hrs · 17,504 cycles

LEFT PACK COULD NOT PRESSURIZE A/C BECAUSE TO FLOW CONTROL VALVE WAS INOP AND WOULD NOT OPEN BEYOND 1/4 OF A INCH.

Part: CONTROL VALVE — STICKING (A/C PACK FLOW) · airframe 33,168 hrs · 17,504 cycles

RETURNED TO SLC BECAUSE WITH ONLY THE LEFT PACK ON FLOW LIGHT ILLUMINATED. WITH CLIMB POWER AT 7000'. FLOW LEVEL AT 10000 TO RETURN FOR LANDING, CABIN CLIMBED TO 7000'. VERY HOT IN CABIN. FOUND LT FLOW CONTROL VALVE STICKING INTERMITTENTLY. REPLACED LEFT FLOW CNTL VALVE PER M/M. LT PACK FLOWS NORMALLY AND SUPPLIES 40 DEGREE AIR.

Part: SKIN — DEFORMED (BS 474-588) · airframe 33,033 hrs · 17,433 cycles

DEFORMATION SKIN STA 474 TO 588 STR L-29R TO L27R. REMOVED FASTENERS AND SHIMMED ERA 462055-14 REV ORIG DATED 7-13-07 REF AAR OKC N/R 1000-0317.

Part: SKIN — BUCKLED (BS 229-475.5) · airframe 33,033 hrs · 17,433 cycles

LOWER FUSE SKIN BULGED AND WRINKLED STA 229-395 LONGERON 28-30 RT. REMOVED AND REPLACED SKIN FROM STA 229 TO 475.5 LONGERON 26L TO 26R PER ERA 462055-14 REV ORIG DATED 07-13-07.

Part: STATOR — BROKEN (NR 2 BRAKE) · airframe 33,033 hrs · 17,433 cycles

NR 2 BRAKE IS LEAKING AT FWD BOTTOM PLUG. FOUND BRAKE ROTORS AND STATOR BROKEN. REMOVED AND REPLACED NR 2 BRAKE IAW MD-90 M/M 32-47-01.

Part: ANGLE — CRACKED (RT MLG WW) · airframe 33,033 hrs · 17,433 cycles

RT MLG WHEEL WELL O/B AFT CORNER ANGLE CRACKED, REPAIRED PER SRM 53-60-02D REF AAR N/R 1000-0296.

Part: FRAME — DAMAGED (BS 446 L28L) · airframe 33,033 hrs · 17,433 cycles

STA 446 LONGERON 28L HAS DOUBLE DRILLED HOLES. FABBED NEW FORMER PER DRAWING. INST PER SRM 53-10-02D, REF N/R 1000-0320.

Part: CUSP WEB — CORRODED (BS 1231-1276) · airframe 33,033 hrs · 17,433 cycles

RT CUSP WEB STA 1231-1276 CORRODED OUT OF LIMITS BETWEEN STA 1231 AND 1250. REPAIRED RT CUSP WEB STA 1231-1250 IAW DELTA ERA 398191-14MA DATED 9-18-02.

Part: CUSP WEB — CORRODED (BS 1231-1276) · airframe 33,033 hrs · 17,433 cycles

RT CUSP WEB STA 1231-1276 CORRODED OUT OF LIMITS BETWEEN STA 1231 AND 1250. REPAIRED RT CUSP WEB STA 1231-1250 IAW DELTA ERA 398191-14MA DATED 9-18-02.

Part: SEAT TRACK — CORRODED (BS 850) · airframe 33,033 hrs · 17,433 cycles

SEAT TRACK RBL 22 BLENDED OUT OF LIMITS AT FS 850. REMOVED DAMAGED SECTION OF TRACK BETWEEN FS 722-850. SPLICED IN NEW SECTION IAW MD90 SRM 53-40-01 FIG 6.

Part: SEAT TRACK — CORRODED (BS 655-760) · airframe 33,033 hrs · 17,433 cycles

SEAT TRACK FS 655-760 LBL 24 FOUND TO BE CORRODED OUT OF LIMITS. REPAIRED SEAT TRACK IAW MD-90 SRM 53-40-01.

Part: LONGERON — DENTED (BS 315) · airframe 33,033 hrs · 17,433 cycles

LONGERON 28 LT HAS A SMALL DENT AT STA 315. REMOVED AND REPLACED LONGERON 28 LT IAW MD-90 SRM 53-10-02 FIG 2.

Part: FLANGE — CRACKED (THRUST REVERSER) · airframe 33,033 hrs · 17,433 cycles

NR 2 ENGINE AFT LOWER INBOARD SECTION OF THRUST REVERSER V SEAL FLANGE HAS 16 INCH CRACK. REPLACED ENGINE. INSTALLATION TO BE COMPLIED WITH ON 1002751, 4000-0103, OPN 7004AD CARD 986.

Part: SHEAR TIE — CRACKED (L1 DOOR) · airframe 33,033 hrs · 17,433 cycles

L1 DOOR SHEAR TIE BEHIND DOOR INNER HANDLE IS CRACKED. REMOVED AND REPLACED INTERCOSTAL IAW MD-90 SRM 51-30-02, 51-10-05 AND 51-30-05.

Part: SEAT TRACK — CORRODED (BS 655) · airframe 33,033 hrs · 17,433 cycles

SEAT TRACK STA. 655.760 LBL 24 FOUND CORRODED OUT OF LIMITS. REPAIRED PER SRM 53-40-01 REF AAR N/R 2700-0146.

Part: CUSP WEB — CORRODED (BS 617-636) · airframe 33,033 hrs · 17,433 cycles

RIGHT CUSP WEB STA 617-636 CORRODED OUT OF LIMITS. FABRICATED REPLACEMENT CUSP WEB FROM .020 7075-T6 AND INSTALLED IAW MD90 SRM 51-10-05 VOL 2 AND 51-30-02.

Part: DOOR FRAME — CORRODED (CARGO DOORWAY) · airframe 33,033 hrs · 17,433 cycles

MID - PIT LWR DOOR JAMB BEAM HAS MULITPLE AREAS OF CORROSION. REPAIRED JAMB BEAM IAW MD-80 SRM 5308 FIG 63.

Part: SKIN — GOUGED (LT WING) · airframe 33,033 hrs · 17,433 cycles

LT WING FIXED L/E JUST I/B OF SLAT TRACK NR 9 SKIN IS GOUGED REPAIRED LT WING L/E IAW MD-90 SRM 57-20-01 FIG 11 VOL I.

Part: CUSP WEB — CORRODED (BS 579-598) · airframe 33,033 hrs · 17,433 cycles

RIGHT CUSP WEB STA 579-598 CORRODED OUT OF LIMITS. REMOVED DAMAGED CUSP WEB AND REPLACED WITH A SERVICEABLE WEB IAW THE MD 90 SRM 51-30-02, 51-30-01, 51-10-05 AND 51-30-05

Part: CUSP WEB — CORRODED (BS 503-579) · airframe 33,033 hrs · 17,433 cycles

RIGHT CUSP WEB STA 503-579 CORRODED OUT OF LIMITS. REMOVED DAMAGED CUSP WEB AND REPLACED WITH A SERVICEABLE WEB IAW THE MD90 SRM 51-30-02, 51-30-01, 51-10-05, AND 51-30-05.

Part: SKIN — GOUGED (LT WING) · airframe 33,033 hrs · 17,433 cycles

LT WING FIXED L/E BETWEEN SLAT TRACK NR 8 AND 7 SKIN HAS GOUGES. REPAIRED DAMAGE TO WING L/E IAW MD-90 SRM 57-20-01 FIG 11 VOL 1.

Part: CUSP WEB — CORRODED (BS 484-503) · airframe 33,033 hrs · 17,433 cycles

FWD PIT RT CUSP WEB CORRODED AROUND LIGHTENING HOLES STA 484-503 LOWER SURFACE. FABRICATED AND INSTALLED REPAIR DOUBLER IAW EA 413196-14MA REV ORG ISSUED 5/13/03.

Part: SKIN — DENTED (BS 220) · airframe 33,033 hrs · 17,433 cycles

FOUND FUSELAGE SKIN DENTED AT LONG 17 LT STA 220 ON LONGERON. REPAIRED SKIN IAW MD90 SRM 51-30-01 FIG 5 VOL I.

Part: CUSP WEB — CORRODED (BS 655-674) · airframe 33,033 hrs · 17,433 cycles

LT CUSP WEB AT FS 655-674 OUT OF LIMITS, CORROSION. REPAIRED CUSP WEB IAW ERA 398191-14MA DATED 5/15/07.

Part: NONE — NONE (NONE) · airframe 33,033 hrs · 17,433 cycles

TEMP REPAIR INSTALLED ON FUSELAGE SKIN AT RT CANT FRAME STA 1531 APPROX 16 IN UP FROM DOOR CUT OUT. REMOVED TEMP REPAIR AND INSTALLED PERM. REPAIR IAW MD90 SRM 53-00-01 FIG 4 VOL I.

Part: SEAT TRACK — CORRODED (BS 579) · airframe 33,033 hrs · 17,433 cycles

SEAT TRACK CORRODED OUT OF LIMITS RBL 22 AND STA 579. FABRICATED AND REPLACED SEAT TRACK STA 522-579 AT RBL 22 IAW MD90 SRM 53-40-01 FIG 6.

Part: SKIN — DENTED (BS 218 S17-18L) · airframe 33,033 hrs · 17,433 cycles

UPPER FUSELAGE SKIN HAS 2 DENTS CONTAINED IN ONE BAY STA 218 LONGERON 17-18L. DEPTH = .031 BY MINOR = .75 DEPTH = .015 BY MINOR = .25 2ND DENT CLOSER THAN 1 INCH FROM STRUCTURE. REPAIRED SKIN IAW MD90 SRM 53-30-01 FIG 5.

Part: CUSP WEB — CORRODED (BS 564-550) · airframe 33,033 hrs · 17,433 cycles

LT CUSP WEB AT FS 564 AND 550 OUT OF LIMITS CORROSION. REPAIRED CUSP WEB IAW MD80 SRM 53-05D FIG 827D.

Part: CUSP WEB — CORRODED (BS 602-601) · airframe 33,033 hrs · 17,433 cycles

LT CUSP WEB AT FS 602 AND 621 OUT OF LIMITS. CORROSION REPAIRED CUSP WEB IAW MD-80 SRM 53-05D FIG 827D.

Part: ELEVATOR — DAMAGED (RIGHT) · airframe 33,033 hrs · 17,433 cycles

RT ELEVATOR O/B T/E HAS COMPOSITE DAMAGE. REPAIRED ELEVATOR O/B T/E DAMAGED IAW MD-90 SRM 51-10-04D PAR 8J.

Part: CUSP WEB — CORRODED (BS 1174) · airframe 33,033 hrs · 17,433 cycles

RT CUSP WEB STA 1174-1231 CORRODED OUT OF LIMITS BETWEEN STA 1174 TO 1193. REMOVED DAMAGED CUSP WEB, LOCATED AND DRILLED NEW CUSP WEB AND INSTALLED IAW MD-90 SRM 51-30-2 AND 51-30-05.

Part: SHEAR TIE — CORRODED (BS 1379) · airframe 33,033 hrs · 17,433 cycles

AFT CARGO STA 1379 AFT SIDE OF SHEAR TIE FROM L-29R TO L-28L IS CORRODED. REMOVED AND REPLACED WITH NEW SHEAR TIE AT STA 1379 FROM L-29R TO L-26L IAW MD-90 SRM 51-10-05, 51-30-02 AND 51-30-05.

Part: ATTACH FITTING — CORRODED (VERTICAL STAB) · airframe 33,033 hrs · 17,433 cycles

RT I/B VERTICAL STAB TO HORIZONTAL ATTACH PLATE HAS CORROSION ON PLATE FACE AND BORE. REPAIRED RT I/B VERTICAL STAB TO HORIZONTAL HINGE IAW MD90 SRM 55-30-05 PAR 5.

Part: DEFLECTOR — BROKEN (NLG) · airframe 31,746 hrs · 16,739 cycles

ON APPROACH ATTEMPTED TO LOWER GEAR. UNSAFE LIGHT FOR NOSE GEAR REMAINED ON. LANDED AT DEN WITH NOSE GEAR NOT EXTENDED EXTENSIVE DAMAGE TO FUSELAGE AROUND NLG OPENING AND E/E DOOR. INVESTIGATION IN PROGRESS BUT FOUND LEFT WHEEL SPRAY DEFLECTOR DAMAGED. ACCOMPLISHED HARD LANDING INSPECTION PER MD 90 AMM 05-51-04A AND REPAIRED AIRCRAFT PER ERAS 458321-14 REV A/458235-14 REN ORIG/458358-14 REV A/458373-14 REV ORIG/458377- REV ORIG/458442-14 REV ORIG/458153-14 REV ORIG.

Part: STRUT — DISCHARGED (NLG) · airframe 29,332 hrs · 15,358 cycles

FELT JOLT/SHUTTER JUST AFTER TAKEOFF RAISING GEAR HANDLE. THOUGHT PROBLEM MIGHT BE WITH NOSE GEAR, HOWEVER JOLT/SHUT FELT FROM COCKPIT TO AFT FLT ATTENDANT STA. ALL COCKPIT IND NORMAL THROUGHOUT FLT. RETURNED TO SLC. SERVICED NOSE GEAR PER MM 31-21-01. CYCLED NOSE GEAR SEVERAL TIMES, OPERATION AND IND CHECKED NORMAL. RAISED AND LOWERED FLAP AND CYCLED ALL MOVEABLE FLT CONTROLS. ALL CHECKED NORMAL.

Part: CONTROL UNIT — INOPERATIVE (E/E BAY) · airframe 28,613 hrs · 14,958 cycles

MOMENTARY POWER INTERRUPTION INFLT. EMERGENCY LTS FLICKER. INSTS FLICKER. HAPPENED IMMEDIATELY AFTER T/O AND TWO MORE TIMES IN CLIMBOUT. APU STARTED AS PRECAUTION. NO EPCU FAULTS, VSCF FANS TEST OK. REPLACED EPCU PER MM, NEEDS FUNCTIONAL TEST TASK 24-21-03-720-801. C/W FUNCTIONAL CHECK OF EPCU/ELECT SYSTEM PER M/M, ALL INDICATION AND OPERATION NORMAL.

Part: WHEEL — DAMAGED (MLG) · airframe 26,762 hrs · 14,013 cycles

ON OVERNIGHT WALKAROUND TRANSIT CHECK - AMT FOUND DAMAGE TO NR 2 MLG WHEEL ASSY AND BRAKE. DAMAGE OCCURRED WHEN THE INSIDE KEY OF NR 2 WHEEL ASSY HOLDING BOLT SHEARED AND THE KEY BACKED OUT STRIKING THE NR 2 BRAKE ASSY. THE KEY WAS HELD IN PLACE BY THE BRAKE ROTOR CUT OUTS AND CONTINUED TO ROTATE WITH THE WHEEL ASSY. REPLACED WHEEL AND BRAKE.

Part: BLEED VALVE — FAILED (NR 2 ENGINE) · airframe 24,060 hrs · 12,719 cycles

NR 2 ENG COMPRESSOR STALLS LESS THAN 1.2 EPR. REPLACED 7TH STAGE BLEED VALVE.

Part: BATTERY PACK — DISCHARGED (FLASHLIGHT) · airframe 23,205 hrs · 12,299 cycles

FWD FLT ATTN STATION EMERGENCY FLASHLIGHT FAILS LED. REPLACED EMERGENCY FLASHLIGHT BATTERY PACK PER M/M CKS GOOD

Part: LINE — CRACKED (LT MLG WW) · airframe 22,841 hrs · 12,122 cycles

RT SYS HYD PRESS DROPPED TO 0 PASSING APPROX 18K QTY ON RT SIDE WENT UP TO 27 QTS. RAN CHECKLIST. WHEN RT ENG PUMP WAS OFF WITH AUX PUMPS ON, PRESS ON RT SIDE WENT FROM 0 TO 700 PSI. THE LT PRESS WENT FROM 3000 TO 2800 PSI. AUX PUMPS AND RT ENG PUMPS NOW IAW CHECKLIST. MTC FOUND CRACKED LINE IN LT W/W, REPLACE LT RESERVOIR AND ENGINE DRIVEN PUMP.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 22,348 hrs · 11,874 cycles

RIGHT WINDSHIELD OUTER PANE CRACKED. REPLACED RT WINDSHIELD HEAT CONTROLLER AND WINDSHIELD.

Part: BOTTLE — DISCHARGED (ESCAPE SLIDE) · airframe 22,303 hrs · 11,853 cycles

FIRST CLASS GALLEY SLIDE BOTTLE PRESS IS LOW. REPLACED GALLEY DOOR SLIDE PER M/M SYCLED DOOR ARM AND DISARM OK.

Part: SKIN — DENTED (T/E FLAP) · airframe 19,391 hrs · 10,385 cycles

THE LEFT INBOARD FLAP, INBOARD AFT REMOVABLE WEDGE LOWER SKIN WAS FOUND DENTED. REPAIR PER ER/A 410735-14.

Part: FRAME — MISLOCATED (STAIR SHROUD) · airframe 16,264 hrs · 8,785 cycles

WHILE ACCOMPLISHING A MODIFICATION TO THE VENTRAL STAIRWAY SHROUD FRAME AT FS 1418 PER DAC S/B MD90-27-026 AS MANDATED PER AD 99-21-32, AN EXISTING BRACE WAS FOUND LOCATED IN THE MOD AREA WHICH WAS NOT SHOWN IN THE S/B OR DESIGN DRAWINGS. THE EXISTING BRACE WAS EVALUATED AND DETERMINED TO BE AN ACCEPTABLE SUBSTITUTE FOR THE S/B BRACE. THE CONFIGURATION DEVIATION WAS AUTHORIZED PER ER/A 379083-14AD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,201 hrs · 8,753 cycles

AFT CABIN EMERGENCY TRACK LIGHTING INOP. REPLACED AFT CABIN EMERGENCY LIGHTING BATTERY AND PACK, OPS OK.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 15,125 hrs · 8,159 cycles

THE CANTED BULKHEAD AT STA 1520.225 WAS FOUND WITH A 1.5 INCH CRACK IN THE WEB NEAR STR 8R AND A 5 INCH CRACK IN THE WEB NEAR STR 8L. THE DAMAGED SECTIONS OF WEB WERE TRIMMED OFF TO REMOVE ALL DAMAGE. NEW SECTIONS OF WEB WERE SPLICED IN WITH ALUMINUM DOUBLERS PER ER/A 377314-14, REV B.

Part: PANEL — DELAMINATED (ROW 1 & 2 CEILING) · airframe 14,844 hrs · 8,013 cycles

DURING CRUISE, ELECTRICAL BURNING SMELL IN CABIN AT ROWS 4 THRU 12. CABIN OVERHEAD LIGHTS TURNED OFF AND SMELL WENT AWAY. FOUND CEILING PANELS AT SEAT 1AB AND 2AB DELAMINATING AND TOUCHING LIGHTS. REPAIRED SAME.

Part: ENGINE — FAILED (NR 1)

LEFT ENGINE FAILURE WHEN T/O POWER APPLIED. REPLACED ENGINE.

Part: LIGHT — BROKEN (ROW 1C)

EMERGENCY FLOOR LIGHT BY SEAT 1C IS BROKEN AND FLOOR LIGHT TRACK IS CRACKED. REPLACED LIGHT ASSY AND WIRING, OPS CKD NORMAL.

Part: GENERATOR — FAILED (RIGHT)

AT ALT C/P LIGHTS FLICKERED SEVERAL TIMES THEN GOT RT GEN OFF MSG ON OAP. ALSO, RT AC BUS OFF MSG. REPLACED RT GENERATOR CONVERTER CKS OK.

Part: RELAY — FAILED (E/E COMPT)

SHORTLY AFTER T/O, EMERGENCY PWR IN USE LIGHT CAME ON. CAPT PFD FAILED. LATER ACS FAULT MSG IN OAP. RETURNED TO ABQ. REMOVED AND REPLACED RELAY R2-47.

Part: FIRE LOOP — SHORTED (NR 2 ENGINE)

RT ENG FIRE DET FAULT ILLUMINATED ON CLIMBOUT 12,000 FT, 280 KIAS FLICKERED AT FIRST THEN ON STEADY TILL 3,000 FT. ON DECSENT A-LOOP ONLY ILLUMINATED ON OVERHEAD. FOUND A-LOOP WIRE SHORTED UNDER CORE COWL. REPAIRED WIRING.

Part: LINES — CHAFED (RT HYD SYST)

RT HYD QTY DECREASED TO 6 QTS IN-FLIGHT. TURNED OFF RT HYD PUMP IAW CHECK LIST. QTY/PRESSURE HELD THROUGH CONFIGURATION THEN WENT TO QTY 2 PRESSURE 5. FOUND PRESSURE AND RETURN LINES CHAFED ON AUXILIARY HYDRAULIC PUMP. REPLACED SAME.