N995DL

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 71,518 hrs · 51,964 cycles

DURING SVC FOUND FWD CABIN EMERGENCY LIGHT INOP. T/S PER MD88 AMM:33-50 AND ROBBED EMERGENCY BATTERY FROM A/C 963 . OPS CHECK OK A/C OK FOR SVC. (LP6658249)

Part: FUSE — FAILED (EMERGENCY LIGHTS) · airframe 71,021 hrs · 51,500 cycles

EXIT ROW LIGHTS OUT FROM ROW 31 AFT. TROUBLE SHOOT TO BAD FUSE IN POWER PACK. REPLACED FUSE IAW CMM 33-21-70. OPS CHECK GOOD. (LP5158525)

Part: DUCT — BLOWN (ANTI-ICE) · airframe 69,829 hrs · 50,475 cycles

RIGHT ENGINE FIRE LIGHT BELLS PASSING APPROX. 800 FT ON TAKEOFF. NO ENGINE INDICATIONS OF FIRE OR DAMAGE. FIRE LIGHT WENT OUT BEFORE BLOWING FIRE BOTTLE OR SHUT DOWN ENGINE. LANDED WITH RIGHT ENGINE AT IDLE PER QRH. FOUND ANTI ICE DUCT BLOWN. NO DAMAGE TO CASE OR COWLS. REMOVED AND REPLACED DUCT AND COWL ANTI ICE VALVE PER AMM 75-10. OPS AND LEAK CHECKED GOOD. OK FOR SERVICE.

Part: SLIDE — FAILED (CABIN) · airframe 69,682 hrs · 50,354 cycles

RT SLIDE FAIL DEPLOYMENT TEST. FORECAST NR 88-0526-8-0406, MPN. D29982, S/N 0883, DATE, OCT 1986. RT SLIDE REMOVED & REPLACED REF. STK# 97-2561-9-0001, W/C 2561-4964. (LP0917957)

Part: BATTERY — DISCHARGED (CABIN) · airframe 69,609 hrs · 50,289 cycles

FWD OVHD EM LIGHTS IN-OP. REPLACED BATTERIES IN EM LT PWR SUPPLY 5-23 IAW AMM 33-55 CKS GOOD. (LP4753077)

Part: UNKNOWN — ODOR (COCKPIT) · airframe 69,431 hrs · 50,143 cycles

BOTH PILOTS SMRLT RUBBER ODER WHEN DEPARTING BHM ON T/O ODER DISSIPATED BEFORE REACHING 10000 FT. REF NO GO ODI LOG 0867036. OPENED SADDLE DUCTS CAPS ON NBR 1 AND NBR 2 ENGINES FOR BOROSCOPE. BOROSCOPE INSPECTED NBR 1 & 2 ENGINE SADDLE DUCTS. NO OIL RESIDUE FOUND. C/W NO GO ODI 2172 STEPS 1,2. C/W W/C 2120-2367, 2120-2368 & 7100-2619. WHEN T/S STEP 2 ON W/C 2120-2367 SENSED A VERY LIGHT ODOR IN COCPIT FROM LT ENG / PACK. AFTER FULL DUCT BURN OUT NO ODOR FROM LT / RT ENGS AND PACKS. (LP5082792)

Part: UNKNOWN — ODOR (CABIN) · airframe 69,430 hrs · 50,141 cycles

DURING TO AND INITIAL CLIMB, THE FA AT THE TAILCONE SMELLED AN ODOR. THE RUBBERY ODOR SMELL DISSIPATED 5 MINUTES AFTER TO. IT WAS A NORMAL PWR TO. PACKS ON, ENG ANTI ICE OFF, AND APU OFF. THERE WAS NO SMOKE, ONLY RUBBERY, CHEMICAL ODOR FROM EXIT ROWS AFT TO THE TAILCONE. INSP APU INLET, #1 AND #2 ENG INLET/EXHAUST, AND L/R PACK OUTLETS NO EVIDENCE OF FLUID CONTAMINATION. C/W NO GO ODI PREVENTION 2172. PERFORMED PNEU DUCT BURNOUT PER WC 7100-2619. NO ADDITIONAL ODORS FOUND. ALL SYSTEMS NML. OK FOR SVC. (LP5082786)

Part: RIB — CRACKED (ELEVATOR) · airframe 69,371 hrs · 50,091 cycles

UPPER RIB FORMER IS CRACKED OUT OF RIVET HOLE. ( P/N 9936146-13) UPPER ROW, THIRD HOLE RT FROM CENTER. REPAIRED PER 573506-14 REV O. (LP0852904)

Part: DOUBLER — WORN (L1 DOOR) · airframe 68,837 hrs · 49,606 cycles

WORN REPAIR DOUBLER, FWD, UPPER CORNER AT THE L1 DOOR. THE REPAIR DOUBLER WAS REPLACED IAW SRM 52-05, FIG 18A.

Part: FLOOR PANEL — DELAMINATED (PAX CABIN) · airframe 68,837 hrs · 49,606 cycles

DELAMINATED FLOOR PANEL 826D IN THE PAX CABIN. THE FLOOR PANEL WAS FABRICATED AND REPLACED IAW AMM 53-20-01-201.

Part: PANEL — DAMAGED · airframe 68,837 hrs · 49,606 cycles

LAVATORY SERVICE PANEL DAMAGED. REPAIRED IAW ER/A 536216-14, REV A, SECT III, AND ETI-88-18-068, REV 2.

Part: SKIN — WORN (RT WING SPOILER) · airframe 68,837 hrs · 49,606 cycles

WEAR ON THE AFT UPPER SURFACE OF THE RT WING GROUND SPOILER. REPAIRED IAW SRM 51-70-1B, P.11.

Part: SKIN — CORRODED (BS 1307) · corrosion level 2 · airframe 68,837 hrs · 49,606 cycles

FUSELAGE SKIN, AFT LAVATORY SERVICE DOOR CUTOUT BS 1307, LONGERON 22L WAS CORRODED. ACCOMPLISH ERA 536216-14 REV A SECTION IV.

Part: SLIDE — DAMAGED (L1 DOOR) · airframe 68,837 hrs · 49,606 cycles

BROCKEN SAFETY THREADS AT L1 SLIDE. THE SLIDE WAS REPLACED IAW AMM 25-62-00-201.

Part: LIGHT — INOPERATIVE (SEAT 14ED) · airframe 68,115 hrs · 49,036 cycles

SEAT 14ED EMERGENCY LIGHT WAS FOUND INOPERATIVE. REMOVED AND REPLACED THE EMERGENCY LIGHT ASSY IAW AMM 33-53. OPS CHECKED GOOD.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHTS) · airframe 67,259 hrs · 48,450 cycles

EXTERIOR EMERGENCY LIGHTS INOPERATIVE. FOUND THE RT OVERWING EMERGENCY LIGHT NOT CONNECTED. RECONNECTED THE CONNECTOR. ALL LIGHTS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 67,020 hrs · 48,269 cycles

EMERGENCY LIGHTS INOPERATIVE, ROW 27 AFT TO REAR DOOR. REPLACED THE BATTERIES IN PAX OVERHEAD BIN 33. OPS CHECKED OK.

Part: DOOR FRAME — CRACKED (RT MLG DOOR) · airframe 66,915 hrs · 48,190 cycles

DURING A CHECK, FOUND THE RT WHEEL WELL FWD DOOR FRAME CRACKED. VISUALLY INSPECTED AND STOP DRILLED IAW ENGINEERING. REMOVED & REPLACED FWD RT WHEEL WELL DOOR FRAME SECTION IAW DRAWING.

Part: WHEEL — UNDERTORQUED (MLG) · airframe 66,192 hrs · 47,615 cycles

AFTER LANDING & NORMAL BRAKING, DURING LANDING BOTH BRAKES EXHIBITED SIGNIFICANT SHUDDER DURING STOP ATTEMPTS. AIRPLANE HAD TROUBLE STOPPING DUE TO THE BRAKE CHATTER. BRAKE TEMP AROUND 201 DEG. THIS WAS MORE THAN THE NORMAL BRAKE CHATTER. IT WAS VERY VIOLENT & THE AIRPLANE WAS DIFFICULT TO STOP. FOUND THE NR 1, 2 & 4 WHEELS TORQUE LOW. TORQUED ALL MAIN WHEEL.

Part: WIRE HARNESS — DEFECTIVE (CABIN) · airframe 66,146 hrs · 47,584 cycles

ON SERVICE CHECK FOUND SEAT 35C EMERGENCY SEAT LIGHT INOP. REPLACED EMERGENCY LIGHT SEAT HARNESS AT 35C. OPERATION IS NOW NORMAL. OK FOR SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 65,450 hrs · 47,102 cycles

ONE RED EMERGENCY LIGHT ON SEAT 24D INOPERATIVE. REPLACED THE LAMPS IAW AMM 33-53. CHECKED GOOD.

Part: RIB — CRACKED (RT WING) · airframe 63,701 hrs · 45,851 cycles

CRACKED RT WING LEADING EDGE RIB XRS 276. RIB WAS REPLACED IAW SRM 51-30-2, 51-10-4, AND 51-10-3.

Part: HAND RAIL — MISINSTALLED (EMERGENCY EXIT) · airframe 63,701 hrs · 45,851 cycles

FUNCTIONAL FAIL ON AFT EMERGENCY DOOR HANDLE. EMERGENCY VENTRAL DOOR HANDLE ASSEMBLIES REMOVED AND INSTALLED CORRECTLY AND FAILURE WAS CORRECTED IAW 52-63-1.

Part: HINGE — WORN (CARGO DOOR) · airframe 63,701 hrs · 45,851 cycles

FREE PLAY ON FWD & AFT HINGE AT MID CARGO DOOR. FWD. AFT HINGES REMOVED, REPAIRED AND INSTALLED IAW ERA 497387-14MA REV B AND AMM 52-31-02.

Part: HINGE — WORN (CARGO DOOR) · airframe 63,701 hrs · 45,851 cycles

FREE PLAY ON FWD & AFT HINGE AT FWD CARGO DOOR. HINGES WERE REMOVED REPAIRED AND INSTALLED IAW ER/A 497387-14 REV B AND FREE PLAY WAS CORRECTED INSTALLATION OF HINGES WAS PERFORMED IAW AMM 52-31-02.

Part: PAN — WORN (CARGO DOOR) · airframe 63,701 hrs · 45,851 cycles

WORN PLATE AND PAN ON AFT EDGE LWR CORNER OUTER SURFACE AT FWD CARGO DOOR. AFT EDGE LWR CORNER WAS REPAIRED I.A.W. DC-9/MD-80 ETI- 88-16-253 REV. 2 AND ERA:547843-14 REV: ORIGINAL.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 63,701 hrs · 45,851 cycles

CRACK OF 0.250 WAS FOUND ON STRINGER 17R XCW 10, INSIDE CENTER TANK. STRINGER 17 WAS REPAIRED PER ER/A 547822-14 REV. ORIG. 547823-14 REV. ORIG.

Part: SUPPORT FITTING — CORRODED · corrosion level 2 · airframe 63,701 hrs · 45,851 cycles

CORROSION BUSHING BORE AND SPOT FACE AT RIGHT GEAR RETRACT ACTUATOR SUPPORT FITTING. THE REPAIR WAS ACCOMPLISHED IAW ETI-88-16-248 REV 4 AND ER/A 547834-14AD REV ORIG.

Part: ANGLE — CRACKED (LT WING LE) · airframe 63,701 hrs · 45,851 cycles

CRACKED FORMER ANGLES ON FIXED LEADING EDGE COMPARTMENT XOS 354, XOS 361, XOS 251, XOS 257 AND XOS 470 AT LT WING. FORMER ANGLES WERE REPLACED IAW SRM 51-30-2/51-30-5/51-10-4/51-10-3 AND DRAWING 9937589 REV. D, 9919329 REV.T.

Part: SUPPORT FITTING — CORRODED (MLG ACTUATOR) · corrosion level 2 · airframe 63,701 hrs · 45,851 cycles

CORROSION ON BUSHING BORE OF BEARING AT RIGHT GEAR RETRACT ACTUATOR SUPPORT FITTING. THE REPAIR WAS ACCOMPLISHED IAW ETI-88-16-248 REV 4 AND ER/A 547834-14AD REV ORIG.

Part: SUPPORT FITTING — CORRODED (MLG ACTUATOR) · corrosion level 2 · airframe 63,701 hrs · 45,851 cycles

CORROSION ON BUSHING BORE AND SPOT FACE AT LEFT GEAR, RETRACT ACTUATOR SUPPORT FITTING. THE REPAIR WAS ACCOMPLISHED IAW ETI-88-16-248 REV 4 AND ER/A 547834-14AD REV ORIG.

Part: STRINGER — CRACKED · airframe 63,701 hrs · 45,851 cycles

CRACK OF 0.312 "WAS FOUND ON STRINGER 17L XCW=12, INSIDE CENTER TANK. STRINGER WAS REPAIRED PER ER/A 547822-14 REV. ORIG. 547823-14 REV. ORIG.

Part: PAN — CRACKED (CARGO DOOR) · airframe 63,701 hrs · 45,851 cycles

CRACKED PLATE ON AFT EDGE AND BEAM 1 BEHIND STOP NR 1 AT AFT CARGO DOOR. INNER PAN WAS REPAIRED IAW ETI-88-16-254 REV:2 AND ERA 547852-14 REV. ORIGINAL.

Part: SKIN — CRACKED (RT WING) · airframe 63,701 hrs · 45,851 cycles

DURING NDT INSPECTION, A DISCREPANT AREA WAS FOUND ON LOWER SKIN BETWEEN XRS=163 TO 168 REAR SPAR AT RT WING. REPAIRED IAW ER/A 547818-14 REV. ORIGINAL.

Part: SKIN — CRACKED (BS 1463-1446) · airframe 63,701 hrs · 45,851 cycles

TWO CRACKS IN FUSELAGE SKIN BS 1463 -1446. REPAIRED IAW ETI 88-16-255 REV 2 ER/A 547855-14 REV ORG.

Part: SKIN — CRACKED (LT WING) · airframe 63,701 hrs · 45,851 cycles

DURING NDT INSPECTION A DISCREPANT AREA WAS FOUND ON LOWER SKIN BETWEEN XRS=163 TO 168 REAR SPAR AT LT WING. REPAIRED IAW ER/A 547818-14 REV.ORIGINAL.

Part: SUPPORT FITTING — CORRODED (MLG ACTUATOR) · corrosion level 2 · airframe 63,701 hrs · 45,851 cycles

CORROSION ON BUSHING BORE OF BEARING AT LEFT GEAR RETRACT ACTUATOR SUPPORT FITTING. REPAIR ACCOMPLISHED IAW ETI-88-16-248 REV. 4 AND ER/A 547834-14AD REV ORIG.

Part: FRAME — CRACKED (BS 1510) · airframe 63,701 hrs · 45,851 cycles

CRACK VISIBLE ON FRAME BS 1510 AFT SIDE NEXT TO UPPER LEFT TAIL CONE LATCH HOOK. REPLACED THE FRAME IAW SRM 51-30-1, 51-30-2, 51-10-4, 51-10-3 AND DWG 9911843 REV AC.

Part: ANGLE — CORRODED (BS 1350) · corrosion level 2 · airframe 63,701 hrs · 45,851 cycles

CORRODED ANGLE BS 1350 X 17LT TO 17RT Z 0, LOWER VENTRAL DOOR JAMB ANGLE. LOWER VENTRAL DOOR JAMB WAS REPAIRED IAW SRM 53-05 FIG.34 AND ER/A 547838-14 REV.1.

Part: INTERCOSTAL — CRACKED (BS 1485) · airframe 63,701 hrs · 45,851 cycles

CRACKED INTERCOSTAL ON BS 1485 AND BTW 1 AND 2 HRS POSITION AT AFT ACCESSORY COMPARTMENT. INTERCOSTAL WAS REPAIRED IAW SRM 53-01, 51-30-2, 51-30-5, AND DWG. 9911875.

Part: FRAME — CRACKED (BS 1510) · airframe 63,701 hrs · 45,851 cycles

CRACKED FRAME BS 1510. FRAME WAS REPLACED IAW DWG 9911843 AND SRM 51-30-2.

Part: PAN — CRACKED (CARGO DOOR) · airframe 63,701 hrs · 45,851 cycles

CRACKED INNER PAN ON AFT EDGE AND BEAM 5 AT FWD CARGO DOOR. PAN REPAIRED IAW SRM 52-03 D FIG 8.

Part: CUSP WEB — CRACKED (BS 459-479) · airframe 63,701 hrs · 45,851 cycles

CRACK ON CUSP WEB BS 459 - 479 AND X -54 TO X -60. REPAIRED IAW SRM 53-05 FIG 131A-14.

Part: CARGO TRACK — CORRODED (BS 1007-1322) · corrosion level 2 · airframe 63,701 hrs · 45,851 cycles

CORRODED CARGO TRACK BETWEEN BS 1007 - 1322. THE CARGO TRACK WAS REPLACED IAW SRM 51-10-4, 51-10-3 PAR 21 AND 14 , 51-30-2, 51-30-1 AND 51-30-5.

Part: BELLCRANK — CORRODED (RUDDER) · corrosion level 2 · airframe 63,701 hrs · 45,851 cycles

CORROSION ON BELLCRANK AT RUDDER THROW-LIMITER. RUDDER BELLCRANK ASSY WAS REPLACED IAW AMM 27-20-03.

Part: WEB — CRACKED (BS 1463) · airframe 63,701 hrs · 45,851 cycles

CRACKED FRAME WEB BS 1463 BETWEEN 10 AND 11 HRS. WEB WAS REPLACED IAW DWG 9953015 REV AH AND SRM 51-30-2 AND 51-30-5.

Part: LONGERON — CORRODED (BS 1287-1309) · corrosion level 2 · airframe 63,701 hrs · 45,851 cycles

SEVERAL AREAS OF CORROSION ON LONGERON 22L BETWEEN BS 1287 -- 1309. THE LONGERON WAS REPAIRED IAW SRM 53-02 FIG. 18 / 51-10-3 / 51-30-5.

Part: DOUBLER — WORN (CARGO DOOR) · airframe 63,701 hrs · 45,851 cycles

WORN FWD & AFT DOUBLER ON LWR EDGE AT MID CARGO COMPARTMENT DOOR. THE DOUBLER WAS REPLACED IAW SRM 51-30-2 AND AFT DOUBLER WAS CLEANED IAW PSM 900-1-2 AND NO FOUND DAMAGE.

Part: STRINGER — CRACKED (LT WING FLAP) · airframe 63,701 hrs · 45,851 cycles

CRACK ON STRINGER 11 AT THE OUTBOARD FLAP, INBOARD DRIVE HINGE AT STA XRS=160. LH SIDE. CRACKED LH STRINGER 11 AT THE OUTBOARD FLAP, INBOARD DRIVE HINGE AT STA XRS- =160, WAS REPAIRED IN REFERENCE TO CARD 5712 01030-03 AND IN ACCORDANCE WITH SERVICE REWORK DRAWING SR09570100. (LP2588226)

Part: DUCT — WORN · airframe 63,701 hrs · 45,851 cycles

WEAR ON LOWER AREA (2 EA) AT Y DUCT. REPAIR WAS PERFORMED IAW ETI 88-16-238 REV 3. AND ER/A 547821-14 REV. ORIGINAL. (LP2586709)

Part: SUPPORT — CRACKED · airframe 63,701 hrs · 45,851 cycles

CRACKS ON UPPER SETTLEMENT AREA AND MID SUPPORT ON "Y" DUCT. REPAIR WAS PERFORMED IAW ETI 88-16-238 REV 3. AND ER/A 547821-14 REV. ORIGINAL.

Part: SKIN PANEL — DAMAGED (FUSELAGE) · airframe 63,701 hrs · 45,851 cycles

INITIAL LIGHTING STRIKES ON RT WINDOW BELT ON FWD AN AFT UPPER CORNER AT WINDOW PASSENGER BETWEEN STA Y598 TO 617. WINDOW BELT PANE STA Y=598-617, RT WAS REPAIRED AND IT IS WITHIN LIMITS IAW ER/A 547845-14, REV ORIGINAL, SECTION I.

Part: SKIN — DAMAGED (BS 1060-1079) · airframe 63,701 hrs · 45,851 cycles

LIGHTING STRIKE ON RT WINDOW BELT AFT LOWER CORNER BS 1060 - 1079. WINDOW BELT PANEL WAS REPAIRED AND WITHIN LIMITS IAW ER/A 547849-14 REV. ORIGINAL SECTION I.

Part: SKIN PANEL — DAMAGED (FUSELAGE) · airframe 63,701 hrs · 45,851 cycles

INITIAL, LIGHT STRIKE ON RT WINDOW BELT AFT UPPER CORNER BETWEEN STA Y= 712-731. WINDOW BELT PANEL STA Y=712-731 RT WAS REPAIRED AND IT IS WITHIN LIMITS IAW ER/A 547846, REV ORIGINAL SECTION I.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,701 hrs · 45,851 cycles

CORROSION ON CUSP ANGLE BETWEEN STA Y=170 TO Y=205 AND BETWEEN X=-54 - X=-60 AT W1 AREA. ANGLE CUSP WAS REPAIRED IAW SRM 53-05, 51-10-3, 51-30-2, 51-30-5.

Part: SKIN PANEL — DAMAGED (FUSELAGE) · airframe 63,701 hrs · 45,851 cycles

INITIAL, LIGHTING STRIKE ON RT WINDOW BELT AFT LOWER CORNER BETWEEN STA Y=1022-1041. WINDOW BELT PANEL STA Y=1022-1041 RT WAS REPAIRED AND IT IS WITHIN LIMITS IAW ER/A 547848-14, REV ORIGINAL SECTION I.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,701 hrs · 45,851 cycles

CORROSION ON AFT CARGO COMPARTMENT DOOR JAMB WEB FROM STA Y=1150 TO Y=1155 BETWEEN LONGERONS 26RT AND 25RT. CARGO COMPARTMENT DOOR JAMB WEB FROM STA Y=1150 TO Y=1155 WAS REPAIRED IAW SRM 53-01, FIG 4, SHEET 4.

Part: SKIN PANEL — DAMAGED (FUSELAGE) · airframe 63,701 hrs · 45,851 cycles

INITIAL, LIGHTING STRIKE ON RT WINDOW BELT FWD, AFT LOWER CORNER BETWEEN STA Y= 503-522. WINDOW BELT PANEL STA Y= 503-522, RT WAS REPAIRED AND IT IS WITHIN LIMITS IAW ER/A 547844-14, REV ORIGINAL SECTION I.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 63,701 hrs · 45,851 cycles

INITIAL CRACKED STIFFENER AT AFT PRESSURE BULKHEAD 12 O'CLOCK POSITION AT PASSENGER CABIN. STIFFENER WAS REPLACED IAW SRM 51-30-2 AND SPRING AT EMERGENCY EXIT PRESSURE BULKHEAD DOOR ARM WAS REMOVED AND INSTALLED IAW AMM 53-53-02 AND ADJUSTMENT, CHECK OF AFT ENTRANCE EMERGENCY DOOR MECHANISM MUST BE PERFORMED WITH CARD 5350-01077-0101.

Part: INTERCOSTAL — CRACKED (BS 1338-1357) · airframe 63,701 hrs · 45,851 cycles

CRACKED INTERCOSTAL BS 1338 TO 1357, RBL 16 AND RBL 24. INTERCOSTAL REPAIRED IAW SRM 53-01 FIG 2 STH. 4.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 63,701 hrs · 45,851 cycles

CORROSION ON SETTLEMENT AREA AND COUNTERSINKS OF LT WING FUEL TANK ACCESS PANEL 1371C. THE ACCESS PANEL WAS REPLACED IAW SRM 51-22-2A.

Part: SPACER — CORRODED (DOOR FRAME) · corrosion level 2 · airframe 63,701 hrs · 45,851 cycles

CORROSION ON LWR DOOR FRAME SPACER BETWEEN BS 674 - 696. THE SPACER WAS REPLACED IAW 53-05. FIG. 123, 51-30-5, 51-30-4, 51-10-4, AND 51-10-3 PAR. 21/14.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,701 hrs · 45,851 cycles

CRACKED INTERCOSTAL, 2 EA, ON STA Y= 1338 TO Y= 1357, X= 16R AND X=-24R, INTERCOSTAL THAT ATTACHES 6 PULLEYS BRACKET, AT W2. CRACKED INTERCOSTAL, 2 EA, WERE REPAIRED IAW SRM 53-01, FIG 2.

Part: SKIN — DENTED (CARGO DOOR) · airframe 63,701 hrs · 45,851 cycles

SEVERAL DENTS ON OUTER SKIN AT AFT CARGO DOOR. REPAIRED IAW ERA N0 547851-14 REV 14 ORIGINAL.

Part: SKIN — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 63,701 hrs · 45,851 cycles

CORROSION ON UPPER BARREL NUT HOLE 21 IN LT HORIZONTAL STABILIZER STA XH 27.234. REPAIRED IAW ETI-88-16-237 REV 1 AND ER/A 547820-14 REV ORIG.

Part: PAN — CRACKED (CARGO DOOR) · airframe 63,701 hrs · 45,851 cycles

CRACKED INNER PAN FWD EDGE BTW BEAM NR 1 AND 2 AT FWD CARGO DOOR. THE PAN WAS REPAIRED IAW SRM 52-05D FIG. 26A.

Part: VANE — DELAMINATED (TE FLAP) · airframe 63,701 hrs · 45,851 cycles

DELAMINATE RT WING OTBD FLAP, INBD VANE NR 1. RT WING OTBD FLAP INBD VANE NR 1 WAS REPAIRED IAW SRM 57-03D, PAR 11 AND A/C 0995, CARD 2000-8149-04.

Part: VALVE — WORN (AC BAY) · airframe 63,701 hrs · 45,851 cycles

WORN CORNERS ON LT RAM AIR DIVERTER VALVE. REPAIR WAS PERFORMED IAW ETI-88-16-247, REV ORIGINAL AND ER/A 547833-14, REV ORIGINAL.

Part: PAN — CRACKED (ENTRY DOOR) · airframe 63,701 hrs · 45,851 cycles

CRACKED INNER PAN ON FORWARD, UPPER CORNER AT FORWARD ENTRY DOOR. INNER PAN ON FWD/UPPER CORNER WAS REPAIRED IAW SRM 52-05D, FIGURE 18A.

Part: SKIN — CORRODED (LT HORIZ STAB) · corrosion level 2 · airframe 63,701 hrs · 45,851 cycles

REF NRC SERIAL NR 927 HIDDEN DAMAGE: CORROSION ON LOWER BARREL NUT HOLE NR 29 AT LT HORIZONTAL STABILIZER STA XH=27.234. REPAIR WAS PERFORMED IAW ER/A 547820-14, REV ORIGINAL.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 63,701 hrs · 45,851 cycles

CRACKED SUPPORT ON STA Y=1398 AND X=18RT TO X=23RT AT CPAX. SUPPORT WAS REPAIRED IAW SRM 53-01, FIG 2, 51-10-3, PAR 21 AND 14, 51-30-2 AND 51-30-5.

Part: CHANNEL — CRACKED (LT MLG DOOR) · airframe 63,701 hrs · 45,851 cycles

CRACK OTBD CHANNEL FWD CORNER STA 953 APPROXIMATELY AT LT MLG DOOR. Z CHANNEL WAS REPAIRED IAW SRM 52-05D, FIG 59 AND 51-30-2.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 63,701 hrs · 45,851 cycles

CORROSION ON SETTLEMENT AREA AND COUNTERSINKS OF LT WING FUEL TANK ACCESS PLATE NR 1361C. ACCESS PLATE WAS REPLACED IAW SRM 51-22-2A.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 63,701 hrs · 45,851 cycles

CORROSION ON COUNTERSINK OF RT WING FUEL TANK ACCESS PLATE NR 1436C. ACCESS PLATE WAS REPLACED IAW SRM 51-22-2A.

Part: DOUBLER — WORN (CARGO DOOR) · airframe 63,701 hrs · 45,851 cycles

WORN FORWARD, AFT DOUBLER ON LOWER EDGE AT FORWARD CARGO COMPARTMENT DOOR. FORWARD, AFT DOUBLER LOWER EDGE AT FORWARD CARGO COMPARTMENT DOOR C1 WERE REPLACED IAW ER/A 486624-14MA, REV ORIG AND SRM 51-30-2.

Part: BEAM — CRACKED (L1 DOOR) · airframe 63,701 hrs · 45,851 cycles

CRACKED BEAM NR 7 AFT SECTION ON FORWARD ENTRY DOOR L1. BEAM NR 7 WAS REPAIRED IAW SRM 52-05D, FIG 109, 51-30-2, 51-30-5 AND 51-10-3 PAR 14.

Part: FLOOR PANEL — CRACKED (CABIN) · airframe 63,701 hrs · 45,851 cycles

CRACK FLOOR PANEL NR 541A AT CABIN PASSENGER. CRACK ON FLOOR PANEL WAS REPAIRED IAW SRM 53-01 FIG 4 AND 51-30-02.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 63,701 hrs · 45,851 cycles

CRACKED DOUBLER ON CUSP WEB STA Y=220 BETWEEN X=-54 AND X=-60 RT AT PAX CABIN. CUSP WEB WAS REPLACED IAW SRM 53-05, FIG 131A-24 AND 51-10-4, 51-30-2 AND 51-30-5.

Part: BEAM — CRACKED (R1 DOOR) · airframe 63,701 hrs · 45,851 cycles

CRACKED BEAM NR 1 ON FWD AND AFT SECTION AT FWD ENTRY DOOR. R1 BEAM NR 1 WAS REPAIRED IAW SRM 52-05D, FIG 81 AND 82, 51-30-1, 51-30-2, 51-30-5 AND 51-10-3 PAR. 14.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,701 hrs · 45,851 cycles

CORROSION ON RIGHT CUSP WEB AT STA Y=1010 BETWEEN X=-54 AND X=-60 AT PASSENGER CABIN. CUSP WEB WAS REPAIRED IAW SRM 53-05, FIG 131A-13, 51-30-2, 51-30-5 AND 51-10-3 PAR 14, 21 AND 38.

Part: CUSP WEB — DAMAGED (FUSELAGE) · airframe 63,701 hrs · 45,851 cycles

HIDDEN DAMAGE, ELONGATED HOLES ON DIAPHRAGM BETWEEN STA Y=180 TO Y=200 AND X=-54 - X=-44 AT W1 AREA. CUSP WEB WAS REPAIRED 51-70-4. REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-30-20, 51-30-5 AND 51-70-4, FIG 2.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,701 hrs · 45,851 cycles

CRACKED INTERCOSTAL BETWEEN STA Y=1287 TO 1309, X= 0, Z= -1, AT CPAX. INTERCOSTAL WAS REPLACED IAW SRM 51-30-1, 51-30-5 AND 51-10-4.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 63,701 hrs · 45,851 cycles

CRACK ON RT INTERNAL STRUCTURE FUSELAGE ON LONGERON 4 RT STA Y = 907. CRACK ON RT INTERNAL STRUCTURE FUSELAGE ON LONGERON 4 RT STA Y =907 WAS REPAIRED IAW SRM 53-02, FIG 18, SRM 51-30-1, 51-30-2, 51-30-5, SRM 51-10-3 PAR 14, 21. SRM 51-10-4, 51-10-2, AND 51-10-2A.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 63,701 hrs · 45,851 cycles

CORROSION AND EVALUATED IAW SRM 51-22-2A. CENTER FUEL TANK ACCESS PLATE NR 2301C WAS REPLACED UNDER CONDITION III IAW SRM 51-22-2A.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 63,701 hrs · 45,851 cycles

CORROSION ON STTLEMENT AREA AND COUNTERSINKS OF LT WING FUEL TANK ACCESS PLATE NR 1303C. FUEL ACCESS PLATE 1303C WAS REPLACED FOR A NEW ONE UNDER CONDITION III SRM 51-22-2A.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 63,701 hrs · 45,851 cycles

CORROSION ON SETTLEMENT AREA AND COUNTERSINKS OF LT WING FUEL TANK ACCESS PLATE NR 1355C. FUEL ACCESS WAS REPLACED IAW SRM 51-22-2A.

Part: BEAM — CRACKED (L1 DOOR) · airframe 63,701 hrs · 45,851 cycles

CRACKED BEAM NR 7 AFT SECTION ON FORWARD ENTRY DOOR. L1 BEAM NR 7 WAS REPAIRED IAW SRM 52-05D, FIG 109, 51-30-2, 51-30-5 AND 51-10-3, PAR 14.

Part: PAN — CRACKED (L1 DOOR) · airframe 63,701 hrs · 45,851 cycles

CRACKED INNER PAN ON FORWARD, UPPER CORNER AT FORWARD ENTRY DOOR. L1 INNER PAN ON FORWARD, UPPER CORNER WAS REPAIRED IAW SRM 52-05D, FIG 18A.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 63,701 hrs · 45,851 cycles

CORROSION ON SETTLEMENT AREA AND COUNTERSINKS OF LT WING FUEL TANK ACCESS PLATE NR 1307C. ACCESS PLATE NR 1307C WAS REPLACED UNDER CONDITION III IAW SRM 51-22-2A.

Part: CHANNEL — CRACKED (FLOOR PANEL) · airframe 63,701 hrs · 45,851 cycles

CRACKED CHANNELS ON FLOOR PANELS NRS 541F, 927E, 1003F, 313A, AND 256A AT CAB PAX. CRACKS ON FLOOR PANELS WERE REPAIRED IAW SRM 53-05, FIG 131B & 131C AND 51-30-02. LONG OF CRACKS 541F=0.125", 927E=0.093", 1003F=0.140", 313A=.200", AND 256A=0.170".

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,701 hrs · 45,851 cycles

CRACKED AND WORN INTERCOSTAL BETWEEN STA Y= 1022 TO 1041, X=0, Z= -1 AT CPAX. CRACK WAS ATTENDED IAW SRM 53-01, FIG 2, WORN WAS BLENDED IAW SRM 53-01, FIG 1 UT WAS ACCOMPLISHED IAW NDT SPM 04-00-07 PAR 5, FIG 3.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 63,701 hrs · 45,851 cycles

CORROSION ON SETTLEMENT AREA OF RT WING FUEL TANK ACCESS PLATE NR 1409C. FUEL ACCESS PLATE 1409C WAS REPLACED UNDER CONDITION III IAW SRM 51-22-2A AND IPC 57-30-00.

Part: CUSP WEB — CRACKED (BS 1028) · airframe 63,701 hrs · 45,851 cycles

PUNCTURED CUSP WEB BS 1028 RBL 54-60. CUSP WEB WAS REPAIRED IAW SRM 53-01 FIG.1 (SHEET1), 51-10-3 PAR. 21, 14, AND 51-30-2.

Part: CUSP WEB — CRACKED (BS 237) · airframe 63,701 hrs · 45,851 cycles

CRACKED RT CUSP WEB BS 237, X 56. THE CUSP WEB WAS REPAIRED IAW SRM 53-05 FIG 131A-6 51-30-01, 51-30-03, 51-30-05, AND 51-10-03 PAR 14, 21, 38.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 63,701 hrs · 45,851 cycles

CORROSION ON SETTLEMENT AREA AND COUNTERSINKS OF LT WING FUEL TANK ACCESS PLATE 1357C. ACCESS PLATE WAS REPLACED IAW SRM 51-22-2A.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 63,701 hrs · 45,851 cycles

CRACKED LONGERON 3 LT ON STA Y=1437 AT AFT ACCESSORY COMPARTMENT. SECTION DAMAGED LONGERON AND SPLICE WERE REMOVED IAW SRM 51-30-5 AND 51-30-2. NEW SPLICE WAS FABRICATED IAW SRM 51-10-2 AND 51-10-2A AND NEW SPLICE AND SECTION LONGERON WERE INSTALLED IAW SRM 53-02, FIG 18, 51-30-5 AND 51-30-2.

Part: ANGLE — CRACKED (DOOR BEAM) · airframe 63,701 hrs · 45,851 cycles

CRACK ON ANGLE IN AFT EDGE NR 1 BEAM AT EMERGENCY DOOR RT FWD. A NEW ANGLE WAS FABRICATED IAW SRM 51-10-2, AND DWG 9957735 REV. G. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-30-2, AND SRM 51-30-5.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 63,701 hrs · 45,851 cycles

CORROSION ON SETTLEMENT AREA AND COUNTERSINKS OF LT WING FUEL TANK ACCESS PLATE 1365C. THE ACCESS PLATE WAS REPLACED IAW SRM 51-22-2A.

Part: CUSP WEB — CRACKED (BS 826-845) · corrosion level 2 · airframe 63,701 hrs · 45,851 cycles

CORROSION ON CUSP WEB FROM BS 826 - 845 BETWEEN LBL 54 - 60. CUSP WEB WAS REPAIRED IAW SRM 53-05 FIG131A-14.

Part: PAN — CRACKED (GALLEY DOOR) · airframe 63,701 hrs · 45,851 cycles

CRACKED PAN FWD NR 4 EDGE BEAM AT FWD GALLEY SERVICE DOOR. PAN WAS REPAIRED IAW SRM 52-03 D FIG. 3, 51-30-01, 51-30-02, 51-30-04, AND 51-10-03 PAR. 21 AND 14.

Part: LONGERON — CRACKED (BS 1437) · airframe 63,701 hrs · 45,851 cycles

LONGERON 16R, BS 1437 CRACKED. LONGERON WAS REMOVED AND REPLACED IAW SRM 53-14-4, 51-30-5, AND 51-30-2.

Part: FITTING — CRACKED (EMERGENCY EXIT) · airframe 63,701 hrs · 45,851 cycles

CRACK ON CLIP IN AFT EDGE BEAM NR 1 AT EMERGENCY EXIT DOOR RT AFT. CLIP DAMAGE WAS REMOVED IAW SRM 51-30-2 AND SRM 51-30-5. NEW CLIP WAS FABRICATED IAW SRM 51-10-2 AND DWG 9957735, REV G. NEW CLIP WAS INSTALLED IAW SRM 51-30-2 AND SRM 51-30-5.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 63,701 hrs · 45,851 cycles

CORROSION ON SETTLEMENT AREA AND COUNTERSINKS OF LT FUEL TANKS ACCESS PLATE NR 1335C. ACCESS PLATE NR 1335C WAS RELACED.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,701 hrs · 45,851 cycles

CORROSION ON LT CUSP WEB, STA 760 BETWEEN X54- X60 AT PAX CABIN. CUSP WEB WAS REPAIRED IAW SRM 53-05, PAR 144, FIG 131A-13, 51-30-05 AND 51-10-03 PAR 14, 21 & 38.

Part: DOUBLER — WORN (TAILCONE) · airframe 63,701 hrs · 45,851 cycles

WEAR ON PREVIOUS REPAIR DOUBLER OF TAIL CONE SLIDE PLATFORM AT AFT ACCESSORY COMPARTMENT. DOUBLER WAS REPLACED IAW ER/A 41283-14AM.

Part: FLOOR PANEL — BROKEN (CABIN) · airframe 63,701 hrs · 45,851 cycles

BROKEN FLOOR PANELS NR 148C, 160F, 148A, 148B, 160E, 120C, 160B, 160D, 120E, 200E, 200C, AND 769D AT PAX CABIN. FLOOR PANELS NRS 148C, 160F, 148A, 148B, 160E, 120C, 160B, 160D, 120E, 200E, 200C, AND 769D AT PAX CABIN WERE FABRICATED IAW AMM 53-20-01-201.

Part: BEAM — CRACKED (R1 DOOR) · airframe 63,701 hrs · 45,851 cycles

HIDDEN DISCREPANCY: CRACKED BEAM NR 4 FWD EDGE AT SERVICE DOOR, R1. BEAM NR 4 WAS REPLACED IAW SRM 51-30-01, 51-30-02.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 63,701 hrs · 45,851 cycles

CORROSION ON FUEL ACCESS PLATE COUNTERSINK, SETTLEMENT AREA 141AL. ACCESS PLATE WAS REPLACED.

Part: FITTING — CRACKED (EMERGENCY EXIT) · airframe 63,701 hrs · 45,851 cycles

CRACK ON CLIP IN AFT EDGE BEAM NR 1 AT EMERGENCY DOOR RT FWD CLIP DAMAGE WAS REMOVED IAW SRM 51-30-2 AND SRM 51-30-5, AND NEW CLIP WAS FABRICATED IAW SRM 51-10-2 AND DWG 9957735, REV G AND NEW CLIP WAS INSTALLED IAW SRM 51-30-2 AND SRM 51-30-5.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 63,701 hrs · 45,851 cycles

CRACKED CUSP WEB FROM STA Y=693 TO Y=712 BETWEEN X=54 AND X=60 LT AT PASSENGER CABIN. CUSP WEB WAS REPAIRED IAW SRM 53-05, FIG 131A.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,701 hrs · 45,851 cycles

CORROSION ON CUSP WEB FROM STA Y=1248 BETWEEN STA X=54 TO X=60 LT SIDE AT PASSENGER CABIN. CUSP WEB WAS REPAIRED IAW SRM 53-05, FIG 131A.

Part: FITTING — CRACKED (SERVICE DOOR) · airframe 63,701 hrs · 45,851 cycles

CRACKED CLIP BELOW BEAM NR 1 FWD PAN AREA AT FWD GALLEY SERVICE DOOR INTERNAL STRUCTURE. CLIP WAS REPLACED IAW DWG 9911579, REV L AND SRM 51-30-5.

Part: VANE — WORN (RT WING TE FLAP) · airframe 63,701 hrs · 45,851 cycles

WEAR AT OUTBOARD FLAP VANE 3 RT WING. FLAP VANE REPLACED IAW SRM 57-03D PAR.11.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 63,701 hrs · 45,851 cycles

CRACKED RT CUSP WEB ON STA Y=905 BETWEEN X=-54 - X=-60. CUSP WEB WAS REPAIR AND CIC WAS APPLIED IAW SRM 51-30-2,53-05, FIG 131A-3 AND 51-10-3 PAR 38.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 63,701 hrs · 45,851 cycles

CRACK ON RT INTERNAL FUSELAGE LONGERON 2 RT ON STA Y=579. LONGERON WAS REPAIRED IAW SRM 53-02, FIG 18, 51-30-2, 51-30-5, 51-10-3 PAR 14 AND 21.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 63,701 hrs · 45,851 cycles

CRACKED LONGERON 16 LT ON STA Y=1437 AT AFT ACCESSORY COMPARTMENT. CRACK LONGERON WAS R & R IAW SRM 53-14-4. 51-30-5 AND 51-30-2.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 63,701 hrs · 45,851 cycles

CORROSION ON SETTLEMENT AREA AND COUNTERSINKS OF LT WING FUEL TANK ACCESS PLATE NR 1456C. FUEL TANK ACCESS PLATE NR 1456C WAS REPLACED.

Part: RUDDER — DAMAGED (TAIL) · airframe 63,701 hrs · 45,851 cycles

DAMAGE RUDDER FLAME SPRAY LT & RT SIDE. FLAME SPRAY ON RUDDER LT & RT SIDE WERE REPAIRED IAW ERA 092613-14MA, REV B AND SRM 51-70-1A, PARA 23.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 63,701 hrs · 45,851 cycles

CRACKED LONGERON 12 LT ON STA Y=1437 AT AFT ACCESSORY COMPARTMENT. CRACKED LONGERON WAS R & R IAW SRM 53-14-4 AND 51-30-2, 51-30-5.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 63,701 hrs · 45,851 cycles

CORROSION ON COUNTERSINKS OF LT WING FUEL TANK ACCESS PLATE NR 1363C. ACCESS PLATE NR 1363C WAS REPLACED.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 63,701 hrs · 45,851 cycles

HIDDEN DISCREPANCY: CRACKS WERE FOUND ON LT CUSP WEB FROM STA Y=1079 TO Y=1098 AT PAX CABIN. CUSP WEB, STA Y=1040 TO1060 LT WAS REPAIRED IAW SRM 53-05, FIG 131A-15, 51-10-3 PAR 14, 21 AND 38.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 63,701 hrs · 45,851 cycles

CRACK ON CUSP WEB, STA Y=503 BETWEEN X=-44 AND X=-54 RT AT PASSENGER CABIN. CUSP WEB ON STA Y=503 BETWEEN X=-44 AND X=-54 WAS REPAIRED IAW SRM 53-05, FIG 131A-17, 51-10-3 PAR 14, 21.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,701 hrs · 45,851 cycles

CORROSION ON CUSP WEB DOUBLER FROM STA Y=636 TO Y=655 BETWEEN X=54 AND X=60 LT AT PASSNEGER CABIN. PREVIOUS REPAIR DOUBLER WAS REPLACED IAW SRM 53-05, FIG 131A.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 63,701 hrs · 45,851 cycles

CRACK ON CUSP WEB, STA Y=905 BETWEEN X=54 AND X=60 LT AT PASSENGER CABIN. CUSP WEB, STA Y=905, LT WAS REPAIRED IAW SRM 53-05, FIG 131-15, 51-10-3 PAR 14, 21 AND 38.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,701 hrs · 45,851 cycles

INITIAL CRACKED FRAME, STA Y=1322, LONG 17 RT AT PASSENGER CABIN. CRACK ON FRAME, STA Y=1322 WAS REPAIRED IAW ER/A 493697-14 MA, REV: B.

Part: CUSP WEB — DAMAGED (FUSELAGE) · airframe 63,701 hrs · 45,851 cycles

ELONGATED HOLE ON CUSP WEB STA Y=617 BETWEEN X=22 AND X=44 LT AT PASSENGER CABIN. CUSP WEB STA Y=617 LT WAS REPAIRED IAW SRM 53-05, FIG 131A-15, 51-10-3 PAR 14, 21 AND 38.

Part: LONGERON — CRACKED (BS 540) · airframe 63,701 hrs · 45,851 cycles

CRACK ON LT INTERNAL FUSELAGE LONGERON 4L BS 540. THE LONGERON WAS REPAIRED IAW. SRM. 53-02 FIG.18 (SHEET. 1), SRM. 51-30-2, 51-30-5 AND 51-10-3 PAR 14, 21.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,701 hrs · 45,851 cycles

CORROSION ON RT CUSP WEB BETWEEN STA Y=488 TO Y=497 AND BETWEEN X=-54 TO X=-60, AT PAX CABIN. AREA WAS REPAIRED IAW SRM 53-05, FIG 131A-14.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 63,701 hrs · 45,851 cycles

CRACK ON RT CUSP WEB BETWEEN STA Y=459 TO Y=479 AND BETWEEN X=-54 TO X=-60 AT PAX CABIN. CRACK WAS REPAIRED IAW SRM 53-05, FIG 131A-14. (LP2559756)

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 63,701 hrs · 45,851 cycles

CRACK ON RT CUSP WEB STA Y=540 AND X=-60 AT PASSENGER CABIN. AREA WAS REPAIRED IAW SRM 53-05, FIG 131A, 51-30-2, 51-30-5, 51-10-3, PARA 14, 21 AND 38.

Part: PAN — CRACKED (FUSELAGE) · airframe 63,701 hrs · 45,851 cycles

CRACK ON LT UPPER FWD WINDOW RING PAN AT STA Y=769 AND STA Y=886, AT FUSELAGE CABIN STRUCTURE. RING PANS WERE REPAIRED IAW SRM 53-05, FIG 122, 51-10-3 PAR 21,14, 51-30-2, 51-30-5, 51-30-03, ER/A 493648-14 MA, REV A AND ER/A 487747-14 MA, REV A.

Part: PAN — CRACKED (FUSELAGE) · airframe 63,701 hrs · 45,851 cycles

CRACK ON LT LOWER FWD WINDOW RING PAN AT STA Y=984, Y=1022, Y=1041, Y=1079 AND Y=1098, AT CABIN FUSELAGE STRUCTURE. RING PANS WERE REPAIRED IAW SRM 53-05, FIG 122, 51-10-3, PAR 21, 14, 51-30-2, 51-30-5, 51-30-03, ER/A 493648-14MA REV A AND ER/A 487747-14MA, REV A.

Part: PAN — CRACKED (FUSELAGE) · airframe 63,701 hrs · 45,851 cycles

CRACK ON RT UPPER AFT WINDOW RING PAN AT STA Y=1041, Y= 1098, Y=1117, Y=1193 AND 1212 AT CABIN FUSELAGE STRUCTURE. RING PANS WERE REPAIRED IAW SRM 53-05, PAR 139, FIG 122, 51-30-02, 51-30-05, ERA487747-14MA, REV A, 493648-14 MA, REV A.

Part: PAN — CRACKED (FUSELAGE) · airframe 63,701 hrs · 45,851 cycles

CRACK ON RT UPPER FWD WINDOW RING PAN AT STA Y=886, AND Y=946 AT CABIN FUSELAGE STRUCTURE. RING PAN WERE REPAIRED IAW SRM 53-05, PAR 139, FIG 122, 51-30-02, 51-30-05, ERA 487747-14MA, REV A AND 493648-14MA, REV A.

Part: CUSP WEB — DAMAGED (FUSELAGE) · airframe 63,701 hrs · 45,851 cycles

ELONGATED HOLE ON LT CUSP WEB STA Y=389 BETWEEN X=44 AND X=54 AT PASSENGER CABIN. CUSP WEB ON STA Y=389 WAS REPAIRED IAW SRM 53-05, FIG 131A-17, 51-10-3 PARA 14, 21.

Part: PAN — CRACKED (FUSELAGE) · airframe 63,701 hrs · 45,851 cycles

CRACK ON RT LOWER FWD WINDOW RING PAN AT STA Y=1136, Y=1155, Y=1193 AND Y=1231 AT CABIN FUSELAGE STRUCTURE. REPAIR PARTS WERE INSTALLED IAW SRM 53-05, PAR 139, FIG 122, 51-30-2, 51-30-05, ERA 487747-14MA, REV A, 493648-14 MA, REV A.

Part: PAN — CRACKED (FUSELAGE) · airframe 63,701 hrs · 45,851 cycles

CRACK ON LT UPPER FWD WINDOW RING PAN AT STA Y=275, Y=522, Y=560, Y=693 AND Y=712 AT FUSELAGE CABIN STRUCTURE. RING PANS WERE REPAIRED IAW SRM 53-05, FIG 122, 51-10-3, PAR 21, 14 AND 51-30-2, 51-30-5, 51-30-03 AND ER/A 487747-14MA, REV A.

Part: PAN — CRACKED (FUSELAGE) · airframe 63,701 hrs · 45,851 cycles

CRACK ON LT LOWER AFT WINDOW RING PAN AT STA Y=598 AND Y=826 AT CABIN FUSELAGE STRUCTURE. RING PANS WERE REPAIRED IAW SRM 53-05, FIG 122, 51-10-3, PAR 21, 14 AND 51-30-2, 51-30-5, 51-30-03 AND ER/A 487747-14MA, REV A.

Part: PAN — CRACKED (FUSELAGE) · airframe 63,701 hrs · 45,851 cycles

CRACK ON LT UPPER AFT WINDOW RING PAN AT STA Y=1041, Y=1079, Y=1193, Y=1212, Y=1231, AND Y=1250 AT CABIN FUSELAGE STRUCTURE. RING PAN WERE REPAIRED IAW SRM 53-05, FIG 122, 51-10-3 PAR 21, 14 AND 51-30-2, 51-30-5, 51-30-03 AND ER/A 487747-14MA, REV A.

Part: FRAME — CRACKED (RT MLG WW) · airframe 62,999 hrs · 45,347 cycles

CRACK IN RT WHEEL WELL FWD FRAME. REPAIRED RT WHEEL WELL FWD FRAME IAW ERA 544460-14 TEMP REPAIR. PERMANENT REPAIR WILL NEED TO BE C/W IN 10 DAYS FROM 2/29/16.

Part: LINE — DAMAGED (CABIN PRESSURE) · airframe 62,080 hrs · 44,693 cycles

DURING DESCENT INBD, LEAVING FL240 FOR FL190 WITH ENGINE ANTI-ICE ON, THE CREW RECEIVED FLICKERING FLOW LIGHT ON OVERHEAD CABIN PRESSURIZATION CONTROL PANEL. FLOW LIGHT THEN ILLUMINATED STEADY WITH CABIN ALTITUDE CLIMBING AT 1500 FT./MIN. CREW DECLARED AN EMERGENCY AND DESCENDED TO 10K, AND REPORTED THAT THE CABIN ALTITUDE REACHED A MAXIMUM OF 11K FEET. CONTROL OF THE CABIN WAS REGAINED AT FL100 AND THE CABIN DESCENT RATE REMAINED NORMAL UNTIL TOUCHDOWN. MAINTENANCE FOUND THAT MUZZLE PRESSURE LINE WAS BROKEN AT THE LT THE AUGMENTATION VALVE TO ANTICIPATOR AND LEAKING. THEY REPLACED THE AUGMENTATION VALVE MUZZLE LINE. PERFORMED SUCCESSFUL CHECKS AND RETURNED ACFT TO SERVICE.

Part: SERVICE PANEL — CORRODED (AFT LAVATORY) · corrosion level 2 · airframe 61,064 hrs · 43,984 cycles

AFT LAV SERVICE PANEL WITH CORROSION PILLOWING, LOWER AFT EDGE. REPAIRED IAW PRI 536216-14, REV 1 AND C/W ER/A 536216-14, REV ORIGINAL.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 58,191 hrs · 42,014 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE FORWARD EMERGENCY EXIT LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES IN THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.

Part: SEAL DEPRESSOR — CRACKED (E/E BAY DOORWAY) · airframe 56,902 hrs · 41,191 cycles

DURING SCHEDULED MX CHECK, FWD UPPER E & E COMPARTMENT DOOR SEAL DEPRESSOR WAS FOUND TO BE CRACKED IN THE RADIUS LOWER AFT AREA. REPAIRED IAW ER/A 518888-14.

Part: CABLE — CORRODED (TAILCONE) · airframe 56,902 hrs · 41,191 cycles

DURING SCHEDULED CHECK, THE TAIL CONE TEE PIN CABLE WAS NOTED TO BE RUSTY AT BOTH ENDS OF THE LT TAIL ACCESSORY COMPARTMENT. THE RUST WAS REMOVED AND THE CABLE WAS TREATED IAW WC 5350-01077-0101 AND THE REQUIRED INSPECTION WAS COMPLETED.

Part: GUIDE — CORRODED (TAILCONE) · airframe 56,902 hrs · 41,191 cycles

DURING SCHEDULED MX CHECK, TAIL CONE RELEASE TEE PIN CABLE GUIDE BLOCK WAS FOUND TO BE CORRODED ON THE LT SIDE OF THE TAIL ACCESSORY COMPARTMENT. THE CORROSION WAS REMOVED FROM THE GUIDE BLOCK AND IT WAS TREATED AND REINSTALLED IAW AMM 53-53. THE REQUIRED INSPECTION WAS ALSO COMPLETED.

Part: RELEASE CABLE — FRAYED (TAILCONE) · airframe 56,902 hrs · 41,191 cycles

DURING SCHEDULED MX CHECK, THE TAIL CONE UPPER LATCH LEVER CABLE AT THE 11:00 POSITION WAS FOUND TO BE FRAYED. THE CABLE WAS REPLACED IAW AMM 53-53-00 AND THE REQUIRED INSPECTION WAS COMPLETED.

Part: INTERCOSTAL — CRACKED (BS 1497) · airframe 56,902 hrs · 41,191 cycles

DURING SCHEDULED CHECK, A CRACKED INTERCOSTAL WAS FOUND AT BS 1497. REPAIRED IAW ER/A 518778-14.

Part: CAM — WORN (TAILCONE RELEASE) · airframe 56,902 hrs · 41,191 cycles

MX DISCOVERED THAT THE TAILCONE RELEASE MECHANISM CAM BASE WAS WORN OUT OF ALLOWABLE LIMITS. THE CAM BASE WAS REPLACED AND THE SYS WAS RIGGED TO SPECIFICATIONS. THE RII WAS SATISFACTORY.

Part: BRACKET — CRACKED (TAILCONE LATCH) · airframe 56,902 hrs · 41,191 cycles

MX DISCOVERED THAT THE TAILCONE RT UPPER LATCH, LOWER BRACKET HAD ELONGATED HOLE. THE BRACKET WAS REPLACED AND THE SYS WAS RIGGED TO SPECIFICATIONS. FUNCTIONAL CHECK WAS COMPLETED SATISFACTORILY.

Part: RECEPTACLE — WORN (TAILCONE LATCH) · airframe 56,902 hrs · 41,191 cycles

MX DISCOVERED THAT ALL OF THE TAILCONE RELEASE SYSTEM GUIDE PIN RECEPTACLES WERE WORN BEYOND ALLOWABLE LIMITS. THE RECEPTACLES WERE REPLACED AND THE SYSTEM WAS RIGGED TO SPECIFICATIONS. THE FUNCTIONAL CHECK WAS COMPLETED SATISFACTORILY.

Part: RECEPTACLE — WORN (TAILCONE LATCH) · airframe 56,902 hrs · 41,191 cycles

MX DISCOVERED THAT THE LT UPPER RELEASE LATCH RECEPTACLE FOR THE TAILCONE WAS WORN, OUT OF ALLOWABLE LIMITS. THE RECEPTACLE WAS REPLACED AND THE SYS WAS RIGGED TO SPECIFICATIONS. THE FUNCTIONAL CHECK WAS COMPLETED SATISFACTORILY.

Part: BRACKET — CRACKED (TAILCONE LATCH) · airframe 56,902 hrs · 41,191 cycles

MX DISCOVERED THAT THE TAILCONE LT UPPER LATCH, LOWER BRACKET WAS CRACKED. THE BRACKET WAS REPLACED AND THE SYS WAS RIGGED TO SPECIFICATIONS. FUNCTIONAL CHECK WAS COMPLETED SATISFACTORILY.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 56,773 hrs · 41,097 cycles

DURING LINE CHECK, CEILING MOUNTED EMERGENCY EXIT LIGHTS WERE FOUND TO BE INOPERATIVE FROM ROWS 11 THROUGH 34. BATTERY PACKS WERE REPAIRED AND INOPERATIVE BULBS REPLACED. THE SYSTEM THEN CHECKED NORMALLY IAW AMM 33-50.

Part: LANYARD — DETACHED (L1 DOOR SLIDE) · airframe 56,100 hrs · 40,650 cycles

THE PILOT DISCOVERED THAT THE L1 DOOR SLIDE LANYARD WAS DETACHED. MX SECURED THE LANYARD AS DESIGNED. ACFT HAS RETURNED TO SERVICE.

Part: WIRE HARNESS — MALFUNCTIONED (EMERGENCY LIGHT) · airframe 55,429 hrs · 40,235 cycles

DURING SERVICE CHECK, MX FOUND EMERGENCY ESCAPE PATHWAY LIGHT INOPERATIVE AT ROW 26D. R & R WIRE HARNESS IAW MM. OPS CHECKED GOOD.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,443 hrs · 38,923 cycles

DURING PSV CHECK IN MSP THE 9911842-129 FRAME WAS FOUND WITH A CRACK AT STA 1458, ZR=35.0, X=20.00 AS SHOWN IN FIG 1. THE FRAME IS MADE FROM 0.050" 7075-T6.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 51,738 hrs · 37,848 cycles

DURING LINE CHECK MAINTENANCE FOUND EMERGENCY LIGHT POWER SUPPLY B5-101 INOPERATIVE. MAINTENANCE REPLACED B5-101 PER AMM 33-53. EMERGENCY LIGHTS CHECK, NOW CHECK OK.

Part: UNKNOWN — ODOR (CABIN) · airframe 50,167 hrs · 36,894 cycles

PASSENGERS AND FLIGHT ATTENDANTS REPORTED A STRONG ELECTRICAL BURNING SMELL AFTER TAKEOFF AND WHEN AIRCRAFT REACHED 10,000 FEET. THE SCENT WAS STRONGEST NEAR THE FORWARD OVERWING EXITS. MAINTENANCE PERFORMED OPERATION 5088 PNEUMATIC DISTRIBUTION CABIN SMOKE ODOR TROUBLESHOOTING AND OPERATION 5089 - PNEUMATIC SYSTEM DUCT BURNOUT. NO TROUBLE WAS FOUND. AIRCRAFT IS OKAY FOR SERVICE. (2010-D1282)(DL738102953)

Part: APU — MALFUNCTIONED (APU BAY) · airframe 49,657 hrs · 36,509 cycles

AFTER TAKEOFF BURNT OIL SMELL WITH FWD AND AFT LAVATORY SMOKE DETECTORS SOUNDING WAS REPORTED. SMOKE DISSIPATED SO FLIGHT CONTINUED TO ATL. AFTER ARRIVAL MAINTENANCE REPLACED THE APU AND PERFORMED OPN 5089 DUCT BURNOUT (2010-D0944)(DLM88102089).

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 49,657 hrs · 36,509 cycles

DURING A LAYOVER CHECK, MAINTENANCE FOUND THAT THE LEFT AND RIGHT OVERWING EMERGENCY LIGHTS WILL NOT ILLUMINATE. MAINTENANCE REPLACED THE BATTERY POWER SUPPLY B5-49. AN OPERATIONAL CHECK WAS PERFORMED AND THE AIRCRAFT WAS RETURNED TO SERVICE (2010-D0967)(DLM88102087).

Part: CARGO TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,366 hrs · 36,308 cycles

DURING HMV3, AFT CARGO TIE DOWN TRACK FWD OF DOOR CUTOUT RT SIDE HAS SPOTS OF CORROSION END TO END. R & R NR 3 TIE DOWN TRACK IAW SRM 51-30-1 AND 51-30-5 FROM STA 1007 TO 1130 RT.

Part: FLOOR PANEL — CRACKED (MAIN CABIN) · airframe 49,366 hrs · 36,308 cycles

DURING HMV, AT MAIN CABIN FLOOR PANEL NR 886C RT SIDE OF PANEL, CLOSE OUT PANEL STRIP BROKEN, REMOVED BROKEN STRIP, FOUND SUPPORT CRACKED IN 3EA PLACES. REMOVED CRACKED CLOSE OUT STRIP, REMOVED CRACKED SUPPORT, REPLACED EACH, FABBED STRIP (.025-7075T6), SUPPORT FURNISHED PN 9936639U13.

Part: SHEAR TIE — CORRODED (BS 1309 L26L/R) · corrosion level 2 · airframe 49,366 hrs · 36,308 cycles

DURING HMV3, STA 1309 LONG 26R-26L AFTER REMOVAL OF FRAME FOUND SHEAR TIE TO BE CORRODED. REMOVED CORROSION ON STA 1309 SHEAR TIE L26R-26L IAW SRM 51-10-3 ORIG MAT.050, REMOVED .012, .038 REMAINING. FOUND TO BE OUT OF LIMITS IAW SRM 53-01, FIG1, SH3. DRILLED AND DEBURRED NEW SHEAR TIE 9912243-219 L26R-26L IAW SRM 51-10-4. R & R NEW SHEAR TIE ON NRC MOO/102 2030N00724. (DLM88101563)

Part: STRUCTURE — CORRODED (BS 1324 L28L) · corrosion level 2 · airframe 49,366 hrs · 36,308 cycles

AFT CARGO STA 1324 LONG 28L CORRODED. REMOVED CORROSION L28L, ORIG MAT .125, REMOVED .028, .097 REMAINING. FOUND TO BE OUT OF LIMITS IAW SRM 51-10-3 AND 53-01 FIG 1, SH3. REMOVED L28L STA 1297-1338. FABRICATED AND INSTALLED NEW LONGERON SECTION SECTION S1242886 AND REPAIR SPLICE (FAB ON PEMCO TRAVLER 2030N01278) IAW SRM 53-02 FIG 18. (DLM88101570)

Part: CHANNEL — CORRODED (BS 1155 L28-29R) · corrosion level 2 · airframe 49,366 hrs · 36,308 cycles

DURING HMV, AFT CARGO STA 1155 AT L28R-L29R CHANNEL CORRODED. CORROSION WAS OUT OF LIMITS. REMOVED CHANNEL,FAB NEW CHANNEL IAW DWG 5936660, INSTALLED NEW CHANNEL IAW SRM 51-30-2, 51-30-5 (DLM8801567)

Part: ATTACH ANGLE — CORRODED (BS 1380 L26L/R) · corrosion level 2 · airframe 49,366 hrs · 36,308 cycles

DURING HMV3, AFT ACCESSORY COMPT STA 1380 L26L TO L26R ATTACHMENT ANGLE HAS CORROSION. REMOVED CORROSION STA 1380 L28L TO L26R FOUND TO BE OUT OF LIMITS IAW SRM 53-01, FIG1, SH33 REMOVED APU FIRE EX LINE, FAN AIR SUPPLY LINE FUEL FEED LINE IAW AMM 26-26-04, 53-20-05 AND 28-20-10-20L. REMOVED DRIP PAN 2EA WEBS AND TEE ANGLE IAW SRM 51-10-4 INSTALLED TEE ANGLE, 2EA WEBS AND DRIP PAN IAW SRM 51-30-02 AND 51-30-5. (DLM8810165)

Part: INTERCOSTAL — CORRODED (BS 1380 S28L) · corrosion level 2 · airframe 49,366 hrs · 36,308 cycles

DURING HMV, AFT ACCY STA 1380 L28L INTERCOSTAL HAS CORROSION. FOUND 100 PERCENT MATERIAL LOSS, FABED DOUBLER AND INSTALLED ON INTERCOSTAL IAW SRM 51-30-5. (DLM88101573)

Part: CUSP WEB — CORRODED (BS 693-712) · corrosion level 2 · airframe 49,366 hrs · 36,308 cycles

DURING HMV, MAIN PASSENGER CABIN STA 693 TO STA 712 LT CUSP WEB CORRODED TOP AND BOTTOM AND SKIN CRACKED. REMOVED DAMAGED SECTION OF CUSP WEB AND INSTALLED DOUBLER IAW EA 53-05D SH 1 & 3 DWG 53-1060.

Part: STRINGER — CRACKED (BS 1338 L7R) · airframe 49,366 hrs · 36,308 cycles

DURING HMV, MAIN CABIN RT AFT LAV STA 1338 L7R END FITTING IS CRACKED. REMOVED DAMAGED STRINGER END FITTING OBTAINED NEW FITTING PN 4912515-501N INSTALLED IAW SRM 51-10-4, 51-30-5.

Part: LONGERON FITTING — CORRODED (L26L) · corrosion level 2 · airframe 49,366 hrs · 36,308 cycles

DURING HMV, AFT CARGO LONGERON 26L AFT END FITTING CORRODED. CORROSION OUT OF LIMITS R & R END FITTING PN 3914590-501 IAW SRM 51-10-4,51-30-5 & DWG 3914590. (DLM88101574)

Part: LONGERON — CORRODED (BS 1287-1328) · corrosion level 2 · airframe 49,366 hrs · 36,308 cycles

DURING HMV, AFT CARGO LONGERON 23L STA 1287 TO 1328 CORRODED. R & R LONGERON STRIP IAW SRM 51-10-4, 51-10-3 AND 51-30-5. (DLM88101587)

Part: FLOOR SUPPORT — CORRODED (BS 1117-1255) · corrosion level 2 · airframe 49,366 hrs · 36,308 cycles

DURING HMV, AFT CARGO COMPARTMENT FLOOR SUPPORT STA 1117-1255 L29R BOTTOM LEG OF BEAM CORRODED. R & R FLOOR SUPPORT PN 5936037501 IAW SRM 51-10-4, 51-30-5.

Part: ATTACH ANGLE — DAMAGED (BS 1120 L28R) · airframe 49,366 hrs · 36,308 cycles

DURING HMV, AT STA 1120 L-28R SILL PLATE ATTACH ANGLE HOLES ELONGATED. R & R WITH NEW ANGLE FABRICATED IAW SRM 51-00 & DWG 593660 INSTALLED ANGLE IAW SRM 51-30-05, 51-30-01.

Part: LONGERON — CRACKED (BS 1338 L7L) · airframe 49,366 hrs · 36,308 cycles

DURING HMV, MAIN CABIN LT AFT LAV STA 1338 L-7-L END FITTING IS CRACKED. REMOVED END FITTING, RECEIVED NEW FITTING PN 4913329-501, INSTALLED IAW SRM 51-30-5, 51-10-3 (DLM88101571)

Part: CUSP WEB — CORRODED (BS 1060-1079) · corrosion level 2 · airframe 49,366 hrs · 36,308 cycles

DURING HMV, MAIN CABIN STA 1060-1079 RT CUSP WEB CORRODED. REMOVED CORROSION, FOUND 100 PERCENT MATERIAL LOSS, FABRICATED AND INSTALLED REPAIR CUSP WEB IAW SRM 53-01 FIG1, 51-30-1, 51-10-4, EA53-05D FIG 827D SH.3 DWG 53-10-60. (DLM88101572)

Part: ATTACH ANGLE — CORRODED (BS 1211 L28-29R) · corrosion level 2 · airframe 49,366 hrs · 36,308 cycles

DURING HMV, AFT CARGO STA1211 LONG 28R AND 29R FLOOR ATTACH ANGLE CORRODED. CORROSION OUT OF LIMITS REMOVED, FAB NEW ANGLE IAW DWG 5956705. INSTALLED NEW ANGLE IAW SRM 51-30-2,51-30-5. (DLM88101566)

Part: ATTACH ANGLE — CORRODED (BS 1401-1418) · corrosion level 2 · airframe 49,366 hrs · 36,308 cycles

DURING HMV, AFT ACCY COMPT STA 1401-1418 L-26-L ATTACH ANGLE HAS CORROSION. CORROSION OUT OF LIMITS FAB NEW ANGLE IAW DWG 991199 INSTALLED NEW ANGLE IAW SRM 51-30-2, 51-30-5. (DLM88101577)

Part: SKIN — CORRODED (BS 1175-1190) · corrosion level 2 · airframe 49,366 hrs · 36,308 cycles

DURING HMV3, AFT CARGO LOWER DOOR JAMB UNDER STRUCTURE STA 1175-1190 BELLY SKIN CORRODED. REQUIRES FURTHER INSP AFTER JAMB REMOVAL. REMOVED CORROSION FROM INNER SKIN STA 1117 TO STA 1231 BTW L28R AND L29R AND AROUND DOOR CUTOUT IAW SRM 51-30-3 ORIG MAT .069 IAW DWG PL5936033. PERFORMED UT THICKNESS INSP IAW NDT SPM 04-00-06. AREA AT BS1183 BTW L28R AND EDGE OF DOOR CUTOUT FOUND TO BE .043 TOOL NR A4015 CAL DATE 4JUN10 FOUND TO BE OUT OF LIMITS IAW SRM 53-01. TRIMMED OUT DAMAGED AREA OF INNER SKIN AND INSTALLED FILLER IAW SRM 53-05 FIG 109. (DLM88101568)

Part: SHEAR TIE — CORRODED (BS 1212 L29L/R) · corrosion level 2 · airframe 49,366 hrs · 36,308 cycles

DURING HMV, AFT CARGO STA1212 BETWEEN LONG 29L AND 29R SHEAR TIE CORRODED. CORROSION OUT OF LIMITS FABRICATED NEW TIE AND INSTALLED IAW SRM 51-10-3,53-01 FIG1 SH-3,51-30-05, 51-30-02, 53-14-3 FIG 3 SH 3 AND OPS 900-2-4-1, 900-3-6 (DLM88101580)

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,366 hrs · 36,308 cycles

DURING HMV, MID CARGO CORROSION ON INTERCOSTAL UNDER RT CARGO TRACK. CORROSION OUT OF LIMITS R & R WITH NEW INTERCOSTAL PN 9915554-16 IAW SRM 53-01,51-30-2. (DLM88101579)

Part: DOOR FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,366 hrs · 36,308 cycles

DURING HMV, AFT CARGO WEB AT LOWER DOOR JAMB CORRODED END TO END. CORROSION OUT OF LIMITS R & R WEB WITH PN 5936442-3 IAW SRM 51-10-4, 51-30-5, 51-30-2, DPS 900-2-4-1. RESTORED AREA IAW SRM 51-30-5, 51-30-2.

Part: FRAME — CRACKED (BS 1446 L17R) · airframe 49,366 hrs · 36,308 cycles

DURING HMV3, AFT ACCESSORY COMPT STA 1446 L17R CANTED FRAME HAS APPROX .1250" CRACK. REMOVED RT PYLON T/E WEDGE FOR FASTENER ACCESS. TRIMMED OUT DAMAGED AREA 1.0" X .75" FABRICATED AND INSTALLED REPAIR DOUBLER AND INSTALLED T/E WEDGE IAW SRM 51-30-1, 51-30-2 AND 51-70-5 FIG 1, 53-14-4 FIG 3.

Part: SHEAR TIE — CORRODED (BS 1287 L27L/R) · corrosion level 2 · airframe 49,366 hrs · 36,308 cycles

AFT CARGO STA 1287 L27L - L27R SHEAR TIE CORRODED, BELLY SKIN REQUIRES INSP UNDER SHEAR TIE. REMOVED SHEAR TIE AT 1287 L27L TO L27R CORROSION WAS 100 PERCENT MAT LOSS OUT OF LIMITS IAW SRM 53-01. RECEIVED, LOCATED, DRILLED AND INSTALLED NEW SHEAR TIE AT STA 1287 L27L TO L27R P/N 9957739-101 IAW SRM 51-30-5, 51-30-2, 51-10-4 PERFORMED DVI ON BELLY SKIN WITH 10X MAG CLASS NO CORROSION NOTED IAW 09-00-03. (DLM88101545)

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,366 hrs · 36,308 cycles

DURING HMV, NR 2 CARGO COMPT AIRFRAME 769-B/H WALL LT 28 LONGERON INTERCOSTAL CORROSION AROUND FASTENER TO SURFACE. CORROSION HAD 100 PERCENT MAT LOSS R & R INTERCOSTAL.

Part: FRAME — CORRODED (BS 1287) · corrosion level 2 · airframe 49,366 hrs · 36,308 cycles

AFT CARGO STA 1287 L29R FRAME CORRODED. REMOVED CORROSION ON FRAME STA 1287 ORG MAT .063. REMOVED .030. REMAINING .033 TOOL USED H6458 CAL 15JUN10 FOUND OUT OF LIMITS IAW SRM 53-01 CUT AND REMOVED DAMAGE FRAME AT LBL 4 TO RBL 15 INSTALLED FRAME REPAIR SR9530057-7003 IAW SRM 53-03D FIG2A.(DLM88101544)

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 49,366 hrs · 36,308 cycles

LT SIDE AFT OF FUEL BOOST PUMP ACCESS CORROSION ON SKIN. R & R LT WING HEATER BLANKET AND PERFORMED SUCCESSFUL TESTING IAW AMM 30-80-02 AND EA 09-070683-03AD REV L.

Part: LONGERON SPLICE — CORRODED (BS 1287 L25L) · corrosion level 2 · airframe 49,366 hrs · 36,308 cycles

DURING HMV, AFT CARGO STA 1287, LONG 25L, SPLICE CORRODED. CORROSION WAS OUT OF LIMITS FABRICATED AND INSTALLED NEW SPLICE ON TRAVELER 2030N01458.

Part: CARGO TRACK — CORRODED (BS 1212-1322) · corrosion level 2 · airframe 49,366 hrs · 36,308 cycles

DURING HMV, AFT CARGO STA 1212-1322 RT TIE DOWN TRACK CORRODED. CORROSION WAS OUT OF LIMITS R & R TIE DOWN TRACK PN 5936667-505 IAW SRM 51-30-5,51-30-1.

Part: FRAME — CORRODED (BS 1309 L27L/R) · corrosion level 2 · airframe 49,366 hrs · 36,308 cycles

DURING HMV3, AFT CARGO STA 1309 L27L-27R CORROSION ON FRAME. FOUND FRAME STA 1309 L27-27L TO BE OUT OF LIMITS DUE TO EXFOLIATION IAW SRM 51-10-3. REMOVED AND CUT FRAME BTW L25R-26R AND L25L-26L. DRILLED, TRIMMED AND INSTALLED FRAME REPAIR PARTS IAW SRM 53-03D FIG 2A.

Part: LONGERON — CRACKED (BS 1336 L6L) · airframe 49,366 hrs · 36,308 cycles

DURING HMV, LT AFT LAV STA 1336 L6L CRACKED. R & R NEW END FITTING PN 4912515-515 IAW SRM 51-30-5.

Part: LONGERON — CRACKED (BS 1338 L14R) · airframe 49,366 hrs · 36,308 cycles

DURING HMV3, L14R END FITTING CRACKED AT STA 1338. R & R END FITTING AT STA 1338 L14R.

Part: ATTACH ANGLE — CORRODED (BS 1211 L28-29R) · corrosion level 2 · airframe 49,366 hrs · 36,308 cycles

DURING HMV, AFT CARGO STA 1211, LONG 28R AND 29R FLOOR ATTACH ANGLE CORRODED. CORROSON OUT OF LIMITS, REMOVED, FAB NEW ANGLE IAW DWG 5956705 INSTALLED IAW SRM 51-30-2, 51-30-5.

Part: CUSP WEB — CORRODED (BS 845-864) · corrosion level 2 · airframe 49,366 hrs · 36,308 cycles

DURING HMV3, MAIN PASS CABIN BTW STA 845-864 RT CUSP WEB CORRODED TOP AND BOTTOM OF SKIN. REMOVED CORROSION FOUND 100 PERCENT MATERIAL LOSS AROUND FASTENERS HOLES. CUTOUT DAMAGE 1" X 3" INSTALLED REPAIR IAW SRM 53-01, FIG1, DRD 53-05D FIG 827D AND SRM 51-30-01.

Part: STRINGER — CORRODED (L28L) · corrosion level 2 · airframe 49,366 hrs · 36,308 cycles

DURING HMV3, AFT CARGO L28L AFT END FITTING CORRODED. R & R L28L AFT END FITTING.

Part: STRAP — CORRODED (BS 1155-1164) · corrosion level 2 · airframe 49,366 hrs · 36,308 cycles

DURING HMV3, AFT CARGO DOOR STA 1155-1164 STRAP ON BELLY SKIN CORRODED. REMOVED CORROSION IAW SRM 51-10-3 (6"X1") ORG MAT .063 MAT REMOVED .016 REMAINING MAT .047 OUT OF LIMITS IAW SRM 53-01. REPLACED STRAP BETWEEN STA 1155 AND STA 1164 L28R TO L29R MAT. .063 7075-T6 PO 0923174 IAW SRM 51-30-2, SRM 51-10-4, SRM 51-60-00. (DLM88101547)

Part: SKIN — CORRODED (JACK PAD) · corrosion level 2 · airframe 49,366 hrs · 36,308 cycles

DURING HMV3, AFT CARGO JACK PAD HAS CORROSION. REMOVED CORROSION ON JACK PAD ORG MAT .100 REMOVED .026. FOUND TO BE OUT OF LIMITS. INSTALLED NEW JACK PAD PN 5917497-501.

Part: LONGERON — CORRODED (24L) · corrosion level 2 · airframe 49,366 hrs · 36,308 cycles

DURING HMV,AFT CARGO LONGERON 24L AFT END FITTING CORRODED. CORROSION WAS OUT OF LIMITS R & R END FITTING PN 3914590-501. (DLM88101554)

Part: FRAME — DAMAGED (BS 1255 S29L/R) · corrosion level 2 · airframe 49,366 hrs · 36,308 cycles

AFT CARGO STA 1255 L/R 29L-29R HAS CORROSION ON BOTH SIDES OF FRAME. REMOVED EXISTING REPAIR, CUT OUT IS 15.5" X 4" NDT VERIFIED DAMAGE IS CONTAINED. LOCATED, FIT, DRILLED AND INSTALLED FRAME REPAIR FROM PN SR09530057-5 SPLICE, -13 PLATE, -9 ANGLE AND -25 FRAME. REPAIR REMOVED WEIGHT 1.6 OZ NEW REPAIR WEIGHED 6.8 IAW SRM 51-30-5, 51-10-2, 53-03 FIG 2A, 51-10-4 53-14-3 FIG 3A. NDT SPM 06-10-01.001 A2583 18MAY10, DPS 900-2-4-1 NR2. (DLM88101549)

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,366 hrs · 36,308 cycles

DURING HMV, AFT CARG LOWER DOOR CUTOUT ATTACH ANGLE CORRODED. CORROSION OUT OF LIMITS FABED ANGLE IAW DWG NR 5936070 ON TRAVELER 2030N01668 INSTALLED ANGLE IAW SRM 51-30-5 & 51-10-9.

Part: INTERCOSTAL — CORRODED (BS 778-788) · corrosion level 2 · airframe 49,366 hrs · 36,308 cycles

DURING HMV3, MID CARGO CORROSION ON INTERCOSTAL UNDER RT CARGO TRACK STA 778-788. REMOVED CORROSION ORG MAT .070, REMOVED .020 REMAINING .050 FOUND TO BE OUT OF LIMITS. R & R NEW INTERCOSTAL PN 9915554-16 IAW SRM FIG 1 51-10-3, 51-30-4, 51-30-5, 51-30-2 AND 53-14-2 FIG2.

Part: CARGO TRACK — CORRODED (BS 693-788) · corrosion level 2 · airframe 49,366 hrs · 36,308 cycles

DURING HMV, MID CARGO COMPARTMENT FROM STA 693-788 RT CARGO TRACK HAS CORROSION AROUND SEVERAL FASTENERS & FASTENER HOLES. CORROSION WAS OUT OF LIMITS R & R TRACK PN 5936594-527. (DLM88101546)

Part: ATTACH ANGLE — CRACKED (BS 1485 L9R) · airframe 49,366 hrs · 36,308 cycles

AFT ACCESSORY COMPT STA 1485 L9R CANTED FRAME FWD SIDE RAIN DRAIN PAN ATTACHMENT ANGLE IS CRACKED. R & R ATTACH ANGLE IAW SRM 51-10-4 AND 51-30-05. FABRICATED NEW ATTACH CLIP OUT OF .040 2024-T3 RECEIVED ON PO NO 0922117 IAW DAC DWG PL4967110 REVA. INSTALLED NEW ATTACH CLIP WET WITH HILOCKS IAW SRM 51-30-05.

Part: FUEL CONTROL — MALFUNCTIONED (LT ENG) · airframe 48,642 hrs · 35,856 cycles

AT FL 35 LT ENG EPR, N1 AND N2 STARTED TO ROLL BACK. RT ENG STAYED AT 2.0 EPR. LT WENT DOWN TO 1.1 EPR. F/A HEARD LOUD NOISE OR BANGING FROM ENG. ANTIICE ON IN MO TURBULANCE DURING DESCENT LOST PRESSURIZATION. LT ENG STARTED TO RESPOND AROUND FL 20 AND BY FL 10 ENG AND PRESSURIZATION OK.

Part: BRACKET — SHEARED (LT WHEEL WHEEL) · airframe 48,062 hrs · 35,487 cycles

MLG DOOR LIGHT ON TAKEOFF. FOUND DOOR SENSOR BRACKET BROKEN. REPLACED BRACKET AND ADJUSTED SENSOR.

Part: SKIN — DAMAGED (WINDOW BELT) · airframe 46,515 hrs · 34,507 cycles

LIGHTNING STRIKE ON SKIN AT WINDOW CUTOUT BETWEEN FS 484-FS 503. COMPLETED TEMPORARY BLEND OUT REPAIR.

Part: DUCT — BLOWN · airframe 43,013 hrs · 32,356 cycles

TAIL COMPARTMENT HIGH MSG FL 180 AND CLIMBING. FOLLOWED QRH LIGHT EXTINGUISHED AND THEN CAME BACK ON. DURING DESCENT TO ATL LIGHT STAYED EXTINGUISHED. MTC IS PROGRESS DNTC. FOUND DUCT ASSY BLOWN REF: 21-20-00-04 ITEM 385 MFG NR 5924037-513 DUCT ASSY (HEADER).

Part: OVEN — UNSERVICEABLE (FWD GALLEY) · airframe 42,183 hrs · 31,821 cycles

SMOKE FUMES NOTICED IN FWD CABIN/COCKPIT. SECURED OVEN AND FUMES DISSIPATED. DIVERTED TO KRIC. REPLACED FIRST CLASS GALLEY OVEN. OPN CKS NML. REMOVED MCO AND PLCD.

Part: BALLAST — UNSERVICEABLE (27 ABC) · airframe 34,153 hrs · 26,371 cycles

REPORTED BY OVERNIGHT CLEANING CREW, SMOKE COMING FROM OVERHEAD BIN 27. FOUND BALLAST BURNED. REPLACED SAME, ALL OPS NOW NORMAL.

Part: BRAKE — FAILED (NR 4) · airframe 34,097 hrs · 26,332 cycles

NR 4 BRAKE SEIZED CAUSING NR 4 TIRE TO WEAR THROUGH AND DEFLATE. REPLACED WHEELS AND BRAKE ASSY.

Part: CASTING — BROKEN (L/E WING 0 SLAT) · airframe 29,558 hrs · 23,066 cycles

LEFT WING PULLEY SUPPORT CASTING BROKEN AFT OF 0 SLAT STA XCW 121. CABLE FRAYED SAME LOCATION CABLE 209 SEG B ZERO SLAT EXTEND CABLE. N/R CARD 70 FOUND DURING LETTER CK J-1 CA RPLD SUPPORT CASTING AND CABLE.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 28,373 hrs · 22,165 cycles

AFT JUMPSEAT AFT EMERGENCY USE ONLY FLASHLIGHT STRAP BROKEN AND REMOVED. FLASHLIGHT LED BLINKING OUT OF LIMITS. REPLACED EMERGENCY FLASHLIGHT AND INSTALLED NEW EMERGENCY USE ONLY STRAP.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 28,373 hrs · 22,165 cycles

AFT CENTER JUMPSEAT FORWARD EMERGENCY USE ONLY FLASHLIGHT STRAP BROKEN AND REMOVED. FLASHLIGHT LED NOT BLINKING. REPLACED EMERGENCY FLASHLIGHT AND INSTALLED NEW EMERGENCY USE ONLY STRAP.

Part: PLACARD — TORN (ELT) · airframe 28,203 hrs · 22,028 cycles

AUTOMATIC ACTIVATION SAFETY PLACARDS TORN ON ELT. REPLACED ELT. FOUND DURING A LAYOVER.

Part: ENGINE — FOD (NR 1) · airframe 25,500 hrs · 20,004 cycles

IRR: ON TAKE OFF JUST AFTER ROTATION NBR.1 ENGINE COMPRESSORSTALL CORR: FND IGV DAMAGE, R/R NBR 1 ENG.

Part: ENGINE — STALLED (NR 1) · airframe 23,864 hrs · 18,819 cycles

DURING CLIMB THRU FL240, LEFT ENGINE COMPRESSOR STALLED AND EGT CLIMBED ABOVE 640 DEGREES. SHUTDOWN ENGINE AND RETURNED TO MCI. REPLACED ENGINE.

Part: FAN — FAILED (COCKPIT)

CLIMBING THRU 14,000 FT, ELECTRICAL ODOR IN COCKPIT AND FWD CABIN. AIR TURNBACKTO MEM. FOUND RECIRC FAN AT FAULT. REPLACED SAME.

Part: BATTERY — DISCHARGED (CABIN)

FLT ATTENDANT ADVISED MAINTENANCE THAT F/C EMER FLASHLIGHT DID NOT BLINK. REPLACED BATTERY AND BULB.

Part: LENS — MISSING (CABIN)

EMERGENCY FLOOR TRACK LIGHT DAMAGED AT SEAT 2C. INSTALLED CLEAR LENS MODULE, NOW CKS NORMAL.

Part: IRU — FAILED (E/E COMP)

ON LIFT OFF, PFD FAILED. IN ATTITUDE THE PFD CAME BACK. REPLACED NR 1 IRU AND BATTERY. ALIGNMENT NORMAL, DISPLAYS NORMAL.

Part: ENGINE — BIRD STRIKE (NR 2 ENGINE)

DURING CLIMBOUT, THE AIRCRAFT ENCOUNTERED A BIRD STRIKE TO THE RT SIDE OF THE A/C. THEN FOLLOWED A STRONG BURNING SMELL IN THE COCKPIT AND THE CABIN. CREW SUSPECTED A BIRD INJESTION INTO THE RT ENGINE. CONTRACT MTC COMPLETED BIRD STRIKE INSPECTION IAW MD88 MTC MANUAL 05-51-08, NO DAMAGE WAS FOUND. BIRD REMAINS WERE REMOVED FROM THE AIRCRAFT.

Part: EEL POWER SUPPLY — INOPERATIVE (CABIN)

FOUND 2 E-PATH LIGHTING STRIPS NOT WORKING. REPLACED BATTERY PWR SUPPLY, OPN NOW CKS GOOD.

Part: HYD HOSE — MISROUTED (TAIL COMP LEFT)

ON APPROACH TO LGA, THE LEFT GEN DROPPED OFF LINE WITH CROSSTIE LOCKOUT MSG ON EOAP. APU WAS STARTED WOULD NOT GO ON BUS. ALSO, HAD LEFT HYDRAULIC SYSTEM LOOSE PRESSURE AND FLUID. FOUND GENERATOR FEEDER CABLES SHORTED TO LEFT HYDRAULIC PRESSURE LINE FROM PUMP TO FILTER MODULE. THE CHAFING OCCURED JUST ABOVE THE FILTER MODULE. REPLACED HYD LINE, FILTER AND PUMP. REPAIRED BURNED A, B, C FEEDER CABLES FROM R5-2 TO S3-280, OPERATION NORMAL.