N901DE

Part: BATTERY — DISCHARGED (CABIN) · airframe 70,557 hrs · 52,039 cycles

FWD FLIGHT DECK / GALLEY OVERHEAD EMERGENCY LIGHT INOP. REPLACED BATTERIES FWD DROP DOWN CEILING FOR FWD FLIGHT DECK GALLEY OVERHEAD EMRG LIGHT IAW AMM 33-50. OPS CHECK GOOD. (LP6188026)

Part: ENGINE — FAILED (LEFT) · airframe 70,376 hrs · 51,877 cycles

LEFT ENG FAILURE 2-4 SEC AFTER LIFT OFF ENGINE INDICATIONS SHOWED 0 PER N2 AND 0 PER NE EGT APROX 628 SHUT DOWN ENGINE IAW CHECKLIST. REPLACE NR 1 ENGINE ON SPC 88-7110-9-010.

Part: WIRE HARNESS — BROKEN (CABIN) · airframe 69,472 hrs · 51,090 cycles

EMERGENCY LIGHTS AT 35ED NOT WORKING. FOND HARNESS BROKEN. REPLACED OPS NML. REF AMM 3352. (LP5845514)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 69,177 hrs · 50,844 cycles

OVERHEAD EMERGENCY ESCAPE PATH LIGHTING INOP FROM ROWS 14-22. REPL BATTERY PACK REF MD88 AMM 33-53. OPS CHECK GOOD. (LP4702230)

Part: FITTING — CRACKED (RT WING) · airframe 68,409 hrs · 50,181 cycles

LATE FINDING (IN REF 5700-2246): RT CRACK ON OUTBD FITTING TO ATTACH SLAT TRACK NR 10 AT SLAT PANEL NR 3 RT WING. SLAT PANEL ASSY 3 RT PART NUMBER OFF : 5922533-504 SERIAL NUMBER OFF: DL27 WAS REMOVED PER WORK CARD 2700-4224-RH-03 AND SERVICEABLE SLAT PANEL ASSY 3 RT PART NUMBER ON: 5922533-504 SERIAL NUMBER ON: DL34 WAS INSTALLED PER WORK CARD 2700-4224-RH-03. (LP0772984)

Part: SPRING — BROKEN (TAILCONE RELEASE) · airframe 68,406 hrs · 50,180 cycles

AWR, HIDDEN CRACK: IN REF AMDS 5350-01077-0101 STEP 2. BROKEN SPRING OF TAILCONE EMERGENCY RELEASE MECHANISM AT AFT PASSENGER DOOR UPPER DOOR JAMB. SPRING OF TAILCONE EMERGENCY RELEASE MECHANISM AT AFT PASSENGER DOOR UPPER DOOR JAMB WAS REPLACED PER MD-88 AMM 53-53-02-201.(LP0770185)

Part: FRAME — CRACKED (BS 1510) · airframe 68,406 hrs · 50,180 cycles

CRACKED FRAME ON STA 1510 CANT REF LONG 10R AT AFT ACC COMPARTMENT. FRAME OF STA1510 AT AFT ACC COMPARTMENT BTW POSITION 9 HRS TO 3 HRS WAS REPLACE PER DC-9/MD 80 SRM 51-30-1, SRM 51-30-2 AND SRM 51-30-5 AND DWG. 9911893 REV. "E". (LP0760687)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 68,297 hrs · 50,060 cycles

ROWS 10 - 15, THE EMERGENCY LIGHTS WERE DIM DURING A TEST. REPLACED THE EMERGENCY LIGHT BATTERY AT ROW 12. OPS CHECKED GOOD.

Part: LENS — DAMAGED (CABIN) · airframe 67,969 hrs · 49,806 cycles

THE EMERGENCY EXIT COVER DIFFUSER LENS DAMAGED OR MISSING. MAINTENANCE REPLACED THE EMERGENCY EXIT COVER DIFFUSER LENS. OPERATIONAL CHECK IS NORMAL AND THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ENGINE — MALFUNCTIONED (RIGHT) · airframe 67,858 hrs · 49,709 cycles

DUE TO I/B W/U OF RT ENG OIL STAINER CLOG MSG. REPLACING ENG ON SPC NUM 2 88-7110-9-0010 REF LOG 3714976. PER MCC NOTIFICATION, AN EMERGENCY WAS DECLARED.

Part: WIRE HARNESS — DEFECTIVE (CABIN) · airframe 67,273 hrs · 49,209 cycles

EMERGENCY LIGHTS AT SEAT 17 AND 26DE INOP SEAT MOUNTED. REPLACED SEAT HARNESS AT SEATS 17DE AND 26DE PER AMM 33-52. OPS CKS GOOD.

Part: BRAKE — MALFUNCTIONED (RT MLG) · airframe 66,897 hrs · 48,911 cycles

RIGHT MAIN TIRE BRAKE SMOKING ON TAXI INBOUND. R&R NR 4 MAIN WHL ASSY & NR 4 BRAKE ASSY PER AMM 32-41 & AMM 32-44. LK CK OK.

Part: UNKNOWN — MALFUNCTIONED (BRAKE SYSTEM) · airframe 66,746 hrs · 48,795 cycles

WHILE TAXIING IN AND MAKING LEFT TURN ON TAXIWAY Z THE RIGHT BRAKE SEEMED TO LOCK UP AND PULL AIRCRAFT TOWARDS EDGE OF TAXIWAY AIRPLANE DEPARTED TAXIWAY AND HIT 2-3 TAXI LIGHTS. INSPECTED A/C PER AMM 05-51-03 NO DAMAGE FOUND. JACKED RT GEAR AND CYCLED BRAKES SERAL TIMES NO BINDING FOUND PER AMM 32-42. A/C OK FOR SERVICE.

Part: ACTUATOR — MALFUNCTIONED (SLAT SYSTEM) · airframe 65,798 hrs · 48,012 cycles

WITH SLATS EXTENDED, THE AIRCRAFT ROLLED TO THE RIGHT, SUBSTANTIALLY. TRIM REQUIRED IS 3 DEGREES LT OF THE TRIM REQUIRED WITH A CLEAN WING. DURING CRUISE THE REQUIRED TRIM IS LESS THAN 1 UNIT RIGHT BOTH RUDDER/AILERON WITH BALANCED POWER & FUEL. FLAP BUSS TENSIONS IN LIMITS IAW AMM 27-50 AT 550 LBS. FOUND FLAP ACTUATORS BYPASSING AT L1, R1, AND R3 POSITIONS. REMOVED L1, R1, R3 FLAP ACTUATORS IAW AMM 27-52. INSTALLED THE FLAP ACTUATORS IAW AMM 27-52. FINAL INSTALLATION SAFTIES, OPS AND LEAK CHECKED GOOD IAW AMM 27-52. (LP3517149)

Part: WEDGE — DAMAGED (RT WING TE FLAP) · airframe 65,223 hrs · 47,573 cycles

DENTED RT TE FLAP 20 INCHES FROM THE OTBD END APROX 9 BY 18 INCHES, APROXIMATELY .40 DEEP AND A BENT T/E WEDGE, FWD END LOWER SURFACE. REMOVED THE OTBD TRAILING EDGE WEDGE. INSTALLED A NEW OTBD FLAP OTBD TRAILING EDGE WEDGE IAW AMM 57-50.

Part: WIRE HARNESS — OUT OF POSITION · airframe 64,884 hrs · 47,304 cycles

DURING VIS INSPECTION OF THE OVERHEAD WIRE BUNDLE, FOUND THE WIRE BUNDLE CHAFING AGAINST RELAY. ROUTED THE WIRE BUNDLE FOR CLEARANCE AND FOUND NO DAMAGED WIRES. ACFT OKAY FOR SERVICE.

Part: BRAKE — DRAGGING (NR 4) · airframe 64,825 hrs · 47,260 cycles

NR 4 BRAKE DRAGGING. REPLACED THE NR 4 BRAKE ASSY IAW AMM 32-42.

Part: WIRE — BROKEN (R1 DOOR) · airframe 64,565 hrs · 47,062 cycles

1R GIRT BAR WIRE BROKEN. PER AMM 52-12 REPLACED GRT BAR LANYARD. OK FOR SVC.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 64,115 hrs · 46,764 cycles

CEILING EMERGENCY LIGHTS INOPERATIVE AT ROW 26-28. REPLACED THE BATTERY PACKS IAW AMM 33-53. OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 63,919 hrs · 46,597 cycles

LT AFT OUTSIDE EMERGENCY LIGHT OUT. RELAMPED IAW AMM 33-50. OPS CHK GOOD.

Part: SKIN — DAMAGED (RT AILERON) · airframe 63,580 hrs · 46,313 cycles

AWR HIDDEN DAMAGE: PERFORMED RT WING HINGE COVER AILERON TAB MOD, ELONGATED FASTENER HOLE WAS FOUND ON RT AILERON T/E LOWER SKIN STA XAT=1.978. AILERON WAS REPAIR IAW ER/A NM 550281-14, REV ORIGINAL AND ETI -88-16-296, REV 3.

Part: DOOR — CORRODED (RT MLG) · corrosion level 2 · airframe 63,580 hrs · 46,313 cycles

AWR HIDDEN DISCREPANCE, CM: CORROSION ON LOWER OTBD FACE AT RT MLG FIXED DOOR IN REF CARD 00693. MLG FIXED DOOR RT WAS REPLACED IAW AMM 32-12-01-201.

Part: TAB — NICKED (LT ELEVATOR) · airframe 63,580 hrs · 46,313 cycles

RE-WRITE: LATE FINDING: NICK ON LT ELEVATOR CONTROL TAB T/E. ELEVATOR CONTROL TAB OFF SN 53378 WAS REPLACED BY ELEVATOR CONTROL TAB ON SN 53380 IAW IPC 55-20-03 AND WAS INSTALLED IAW CARD 2730-4334; JOB 001-0232.

Part: SUPPORT FITTING — CORRODED (RT MLG) · airframe 63,580 hrs · 46,313 cycles

CORROSION ON RT MLG SUPPORT FITTING BUSHING BORE. REPAIRED IAW ER/A 549274-14AD REV ORIG.

Part: SPRING — BROKEN (DOOR) · airframe 63,580 hrs · 46,313 cycles

AWR RII: BROKEN EMERGENCY EXIT PRESSURE BULKHEAD DOOR ARM SPRING. SPRING PN 4951062-1 WAS REPLACED IAW AMM 53-53-02 AND WAS VERIFIED WITH IPC 52-10-02.

Part: SPRING ASSY — CORRODED (RUDDER) · corrosion level 2 · airframe 63,580 hrs · 46,313 cycles

RUSTED PISTON END AT RUDDER TRIM TAB ACTUATOR ON AFT ACCESSORY COMPARTMENT. RUDDER TRIM LOAD-FEEL SPRING ASSY WAS REMOVED AND INSTALLED IAW AMM 27-207. AREA AT SHAFT OF RUDDER TRIM LOAD-FEEL SPRING ASSY WAS REWORKED MEASUREMENT ORIGINAL 0.686" AND MINIMUM REMAINING IS .685" IS WITHIN LIMITS IAW DWG NR 3652587, REV D CADMIUM PLATE WAS APPLY IAW DWG 3652587, REV B AND DPS 9.74.

Part: HINGE BRACKET — DAMAGED (TE FLAP) · airframe 63,580 hrs · 46,313 cycles

AWR: HIDDEN DISCREPANCY, ELONGATED HOLES ON NR 4 FORWARD FIXED FLAP HINGE BRACKET STA XW=333.147 RT WING. FORWARD FIXED FLAP HINGE BRACKET STA XW= 333.147 RT WING WAS REPLACED IAW AMM 57-40-01-201, STEP 3H, 1 TO 9B.

Part: DOUBLER — WORN (CARGO DOOR) · airframe 63,580 hrs · 46,313 cycles

INITIAL, WEAR ON EXTERNAL PREVIOUS REPAIR DOUBLER ON FORWARD LOWER CORNER AT FORWARD CARGO COMPARTMENT DOOR. DAMAGE DOUBLER ON FORWARD LOWER CORNER WAS REPLACED IAW ER/A 486624-14MA, REV ORIGINAL.

Part: DOOR FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,580 hrs · 46,313 cycles

INITIAL, CORROSION ON UPPER DOOR JAMB, STA Y=1160 BETWEEN LONG PROJECTION 18 RT TO 19 RT AT AFT CARGO COMPARTMENT, C3. DUE TO EXCESSIVE DAMAGE BEAM ON C3 WAS REPLACED IAW SRM 51-10-3/51-10-4, 51-30-5 AND DWG N-5936072 REV U.

Part: DOOR — CRACKED (LT WING) · airframe 63,580 hrs · 46,313 cycles

INITIAL: CRACKED LT WING OTBD FLAP INBD BUTE DOOR MID SECTION INNER AREA. LEFT WING OTBD FLAP INBD BUTE DOOR WAS REPAIRED IAW ER/A466345-14MA, REV B.

Part: BEAM — CRACKED (L1 DOOR) · airframe 63,580 hrs · 46,313 cycles

CRACKED AFT EDGE BEAM NR 1 AT MAIN ENTRANCE DOOR, L1. THIS CARD WAS ATTENDED WITH ERA 549270-14, REV ORIGINAL.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,580 hrs · 46,313 cycles

CORROSION ON INTERNAL DOUBLER AROUND AFT LAVATORY SERVICE PANE. CORROSION ON INTERNAL DOUBLER WAS REPAIRED IAW ER/A 549257-14, REV ORIGINAL REPETITIVE INSPECTION WILL BE PERFORMED WITH LOG 2657213, ER/A 549257-14, REV ORIGINAL, SECTION II.

Part: STRINGER — CRACKED (LT WING) · airframe 63,580 hrs · 46,313 cycles

CRACK ON STRINGER 11, LT WING, OTBD SIDE STA XRS=168 APPROXIMATELY STR 11, LT WING WAS REPAIRED IAW DWG NR SR-09570100, REV B AND ER/A 549281-14AD, REV ORIGINAL REPETITIVE INSPECTION WILL BE MONITORED WITH LOG PAGE 2660039 IAW ERA 549281-14AD, REV ORIGINAL, SECT 2.

Part: BULKHEAD — UNKNOWN (FUSELAGE) · airframe 63,580 hrs · 46,313 cycles

RIGHT APB LOWER CHORD CUT LINE DOES NOT MEET REQUIREMENTS OF SRM, STA Y=1338, AREA WAS REPAIRED IAW ER/A 549254-14, REV ORIGINAL.

Part: RELEASE MECH — WORN (TAILCONE) · airframe 63,580 hrs · 46,313 cycles

WORN TAILCONE RELEASE CAM AT AFT ACCESSORY COMPARTMENT. WORN ON TAILCONE RELEASE MECHANISM CAM BASE WAS MEASURED AND WAS FOUND OUT OF LIMITS, MAX PERMISSIBLE 0.025" X 0.280" MAX MEASURED 0.062" X 0.- 328 IAW CMM 53-50-07. THEREFORE CAM WAS REPLACED IAW AMM 53-53-02.

Part: SKIN — BULGED (BS 608-617) · airframe 63,580 hrs · 46,313 cycles

BULGING FUSELAGE SKIN BS 608 - 617, LONGERONS 29 - 30R. DOUBLERS WERE REPLACED IAW SRM 51-30-2, 51-30-5, 51-30-3, 51-10-3 PARR. 14, 21, 51-20-0 AND DWG 5911412 REV. DU.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,580 hrs · 46,313 cycles

CORROSION ON INTERNAL DOUBLER AROUND AFT LAVATORY SERVICE PANEL. FRAME CLIP STA Y=1309 & Y=1322 FROM LONGERON 18LT TO 26LT; LONGERON 20 LT & 21 LT FROM STA Y=1322 TO Y=1338; INTERCOSTALS, 2 EA, BETWEEN LONG 21 LT AND 22 LT FROM STA Y=1322 TO Y=1338; AND LONGERON 19 LT & 22 LT FROM STA Y=1287 TO Y=1338 WERE INSTALLED AND CIC WAS APPLIED IAW SRM 51-10-3, PAR 38, 51-30-2 AND 51-30-5. REPETITIVE INSPECTION WILL BE PERFORMED WITH LOG 2657213, ER/A 549257-14, REV ORIGINAL SECTION II.

Part: FITTING — CORRODED (R1 DOOR) · corrosion level 2 · airframe 63,580 hrs · 46,313 cycles

CORRODED R1 GIRT BAR FITTINGS ABOVE FLOOR PANEL 160G. R1 GIRT BAR FITTINGS ABOVE FLOOR PANEL 160G WERE REPLACED IAW DWG 3936193, REV ORIGINAL.

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 63,580 hrs · 46,313 cycles

CORROSION ON INTERNAL HOLES LOWER ACCESS DOOR CUTOUT STA XRS=189 TO 214 BETWEEN STR 12 AND STR 15 AT LT WING. CORROSION ON HOLES WERE REPAIRED IAW ER/A 549272-14AD, REV ORIGINAL. THIS DOCUMENT IS READY TO ENTRY AND MONITOR WILL BE WORK IAW ER /A 549272-14AD, REV ORIGINAL LOG PAGE 2652628.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,580 hrs · 46,313 cycles

CRACKED FRAME ON STA Y=1485 CANT BELOW OF STAIR VENTRAL ACTUATOR AT AFT ACCESSORY COMPARTMENT. FRAME ON STA Y=1485 CANT BELOW OF STAIR VENTRAL ACTUATOR AT AFT ACCESSORY WAS REPAIRED IAW SRM 53-03D, FIG 43.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 63,580 hrs · 46,313 cycles

INITIAL: LIGHTNING STRIKE ON LT WINDOW BELT BETWEEN STA Y:731-750, FORWARD AND AFT CORNERS. LIGHTNING STRIKE ON LT WINDOW BELT WAS REPAIRED IAW ER/A 549248-14AD REV ORIGINAL.

Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 63,580 hrs · 46,313 cycles

CORROSION ON INTERNAL HOLES LOWER ACCESS DOOR CUTOUT STA XRS=-189 TO 214 BETWEEN STR 12 AND STR 15 AT RT WING. CORROSION ON HOLES WAS REPAIRED IAW ER/A 549272-14AD, REV ORIGINAL. THIS DOCUMENT IS READY TO ENTRY AND MONITOR WILL BE WORKED IAW ER/ A 549272-14 AD, REV ORIGINAL LOG PAGE 2652628.

Part: FINGER DOUBLER — BENT (FUSELAGE) · airframe 63,580 hrs · 46,313 cycles

BENT EDGE ON FINGER DOUBLER AT FUSELAGE SKIN REPAIR BETWEEN STA Y=237 TO STA 256 AND LONGERONS 17LT TO 18LT, REF LOG NR 1542341. SECTION STRIP DOUBLER WAS REPAIRED IAW SRM 53-04-3, FIG 12.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,580 hrs · 46,313 cycles

CORROSION ON PREVIOUS REPAIR DOUBLER AND LOWER DOOR JAMB AT FWD CARGO COMPARTMENT DOOR JAMB. LOWER DOOR JAMB WAS REPAIRED IAW SRM 53-05, FIG 44A.

Part: SKIN — DELAMINATED (ELEVATOR TAB) · airframe 63,580 hrs · 46,313 cycles

DELAMINATED RT ELEVATOR GEARED TAB UPPER SKIN AT HORIZONTAL STABILIZER. THE GEARED TAB WAS REPLACED IAW SRM SRM 55-04 P.4.

Part: SKIN — BULGED (BS 636-655) · airframe 63,580 hrs · 46,313 cycles

BULGING FUSELAGE SKIN BTW BS 636 - 655, LONGERONS 29 - 30R. DOUBLER WAS REPLACED IAW SRM 51-30-2 AND 51-30-5.

Part: SKIN — NOT REPORTED (BS 229-260) · airframe 63,580 hrs · 46,313 cycles

PERFORM PERMANENT REPAIR ON FUSELAGE SKIN BS 229 - 260 BETWEEN LONGERONS 16 - 18L SRM 53-04 FIG 12C.

Part: SKIN — CORRODED (CONTROL TAB) · corrosion level 2 · airframe 63,580 hrs · 46,313 cycles

CORROSION ON RIGHT ELEVATOR CONTROL TAB LOWER SKIN AT HORIZONTAL STABILIZER. DUE THE AMOUNT OF DAMAGE ON OUTER SKIN AND SRM 54-04 P.4, THE COMPONENTE WAS REPLACED.

Part: SKIN — DAMAGED (VERTICAL STAB) · airframe 63,580 hrs · 46,313 cycles

LOOSE FASTENERS ON VERTICAL STABILIZER LEADING EDGE UPPER/LOWER SPLICE VSS 52.267. HOLES ON VERTICAL STABILIZER LEADING EDGE WERE REPAIRED IAW SRM 55-03D PAR. 28 FIGURE 30 AND PAR. 27 FIGURE 29.

Part: SKIN — DAMAGED (VERTICAL STAB) · airframe 63,580 hrs · 46,313 cycles

LOOSE FASTENERS ON VERTICAL STABILIZER LEADING EDGE UPPER/LOWER SPLICE VSS 52.267. HOLES ON VERTICAL STABILIZER LEADING EDGE WERE REPAIRED IAW SRM 55-03D PAR. 28 FIGURE 30 AND PAR. 27 FIGURE 29.

Part: SKIN — DAMAGED (BS 693-712) · airframe 63,580 hrs · 46,313 cycles

LIGHTNING STRIKE ON LEFT WINDOW BELT BETWEEN BS 693 - 712. THE WINDOW BELT WAS REPAIRED IAW ER/A 549290-14 REV. ORIGINAL SECTION I.

Part: SKIN — CRACKED (BS 1418) · airframe 63,580 hrs · 46,313 cycles

CRACK WAS FOUND ON FUSELAGE SKIN AT BS 1418 AND BETWEEN LONGERON 2 AND 3R.

Part: CUSP WEB — CORRODED (BS 475-484) · corrosion level 2 · airframe 63,580 hrs · 46,313 cycles

CORROSION ON RIGHT CUSP WEB BS 475 - 484 AND X -54 TO X -60. REPAIRED IAW SRM 53-05 FIG. 131A-11.

Part: FLOOR PANEL — DAMAGED · airframe 63,580 hrs · 46,313 cycles

DELAMINATION AND DAMAGED FERRULES AT FLOOR PANEL 160E. THE FLOOR PANEL WAS FABRICATED IAW AMM 53-20-01-201 PAR.7(C).

Part: LONGERON — CRACKED (BS 256) · airframe 63,580 hrs · 46,313 cycles

CRACKED LONGERON 17L ON BS 256. THE LONGERON NBR WAS REPAIRED IAW SRM 53-02 FIG. 18.

Part: SKIN — DAMAGED (BS 636-655) · airframe 63,580 hrs · 46,313 cycles

LIGHTNING STRIKE ON LT WINDOW BELT BETWEEN BS 636 - 655. THE WINDOW BELT WAS REPAIRED IAW ER/A 549289-14 REV. ORIGINAL SECTION I.

Part: FERRULE — DAMAGED (FLOOR PANEL) · airframe 63,580 hrs · 46,313 cycles

DAMAGED FERRULE ON THE FLOOR PANEL. THE FERRULE WAS REPLACED IAW AMM 53-20-01-201.

Part: FRAME — CRACKED (BS 1485) · airframe 63,580 hrs · 46,313 cycles

CRACKED FRAME WEB ON BS 1485 CANT BETWEEN 10 AND 9 HRS PODITION AT AFT ACCESSORY COMPARTMENT. FRAME WAS REPAIRED IAW 53-03D FIG. 48.

Part: SUPPORT FITTING — CORRODED (LT MLG) · corrosion level 2 · airframe 63,580 hrs · 46,313 cycles

CORROSION ON LT MLG SUPPORT FITTING BUSHING BORE. BORE HOLE WAS REAMED WITH FINAL I.D. 2.322. FOUND WITHIN LIMITS IAW DWG SR09570087 REV. B.

Part: SKIN — DAMAGED (BS 617-636) · airframe 63,580 hrs · 46,313 cycles

LIGHTNING STRIKE ON LEFT WINDOW BELT BETWEEN BS 617 - 636. THE WINDOW BELT WAS REPAIRED IAW ER/A 549288-14 REV. ORIGINAL SECTION I.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 63,580 hrs · 46,313 cycles

DELAMINATION AT FLOOR PANELS NR 541D AND 927C. FLOOR PANEL 927C WAS FABRICATED IAW AMM 53-20-01-201 PAR 7C. FLOOR PANEL 541D WAS REPAIRED IAW AMM 25-00-00-801, PARA 3D.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 63,580 hrs · 46,313 cycles

DELAMINATION AT FLOOR PANELS NR 120A, 120B, 120C, 120D, 120E, 148A,148C, 160A, 160B, 160C, 160D, 160F, 200A, 200B, 200C, 200D, 200E, 200F W1 AREA. FLOOR PANELS NR 120A, 120B, 120D WERE ATTENDED WITH NRC NR 01030. FLOOR PANEL 200F WAS REINSPECTED AND NO DISCREPANCIES WERE FOUND AND FLOOR PANEL 200A WAS REPAIRED IAW SRM 51-70-1D, PAR 10. FLOOR PANELS NR 148C, 160F, 200C, 200D, 160D, 160C, 120C, 148A, 160B, 120E, 160A, 200B AND 200E WERE FABRICATED IAW SRM AMM 53-20-01-201, PAR 7 C.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,580 hrs · 46,313 cycles

CORROSION ON LT CUSP WEB BETWEEN STA Y=1212 AND Y=1227 AND X=54 TO X=60 AT PASSENGER CABIN. AREA WAS REPAIRED IAW SRM 53-05, FIG 131A, 51-30-2, 51-10-3, 51-30-5.

Part: PAN — CRACKED (CARGO DOOR) · airframe 63,580 hrs · 46,313 cycles

CRACKED ON LOWER PAN, STA Y = 674 AT MID CARGO DOOR. CRACK ON LOWER PAN WAS REPAIRED IAW SRM 52-03D, PAR 4.

Part: SKIN PANEL — DAMAGED (RUDDER) · airframe 63,580 hrs · 46,313 cycles

DAMAGED METALLIZED ON RT, LT RUDDER SKIN PANELS AT VERTICAL STABILIZER. RT & LT RUDDER SKIN WERE REPAIRED BY ER/A 092613-14MA, REV-B.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 63,580 hrs · 46,313 cycles

DELAMINATION ALSO DAMAGED FERRULES AT FLOOR PANELS NR 1250C, 1003D AND 693C. FLOOR PANELS NR 1250C AND 1003D WERE FABRICATED IAW AMM 53-20-01-201, PARA 7C AND FLOOR PANEL NR: 693C WERE REPLACED FERRULES IAW AMM 53-20-01-201, PARA 7B.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 63,580 hrs · 46,313 cycles

DELAMINATION AT FLOOR PANELS NR 1079B, 1174C, 1174D, 1174E AND 1174F. FLOOR PANELS NR: 1174C AND 1174D WERE FABRICATED IAW AMM 53-20-01-201. FLOOR PANEL NR 1079B WAS REPAIRED IAW AMM 25-00-00-801 PARA 3D. FLOOR PANEL NR: 1174E WAS REPAIRED IAW AMM 25-00-00-801, PARA 3B. FLOOR PANEL NR 1174F WAS RE-INSPECTED AND NO DAMAGED FOUND.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 63,580 hrs · 46,313 cycles

AWR HIDDEN DISCREPANCY: DELAMINATED FLOOR PANEL NR 148D AT CABIN CREW. FLOOR PANEL NR 148D AT CABIN CREW WAS FABRICATED IAW AMM 53-20-01-201, PAR 7C.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 63,580 hrs · 46,313 cycles

LIGHTNING STRIKE AT FUSELAGE 200, LONGERON 7L, RT SIDE ON REF LP 0532712. PERMANENT REPAIR WAS PERFORMED IAW SRM 53-04-2, FIG 2. PERFORMED VISUAL INSPECTION ON PERMANENT REPAIR AT INITIAL 8000 FC AND REPETITIVE ENTRY 8000 FC IAW SRM 53-04-2, FIG 2, PAR D.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 63,580 hrs · 46,313 cycles

INITIAL: LIGHTING STRIKE ON RT WINDOW BELT AFT LOWER CORNER STA Y=613. ALSO, FWD LOWER CORNER STA Y= 796. LIGHTNING STRIKE ON RT WINDOW BELT STAY=598-617 WAS REPAIRED ER/A 549267-14, REV ORIGINAL SECTION 1 AND MUST BE MONITORED WITH MONITOR 2638502.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,580 hrs · 46,313 cycles

CORROSION ON RT CUSP WEB BETWEEN STA Y=1182 TO Y=1187 ALSO BETWEEN STA Y=1202 TO Y=1204 AT RT PASSENGER CABIN FLOOR SERIAL 1302. DAMAGE ON CUSP WEB BETWEEN STA Y=1182 TO Y=1187 ALSO BETWEEN STA Y=1202 TO Y=1204 AT RT PASSENGER CABIN FLOOR WERE REPAIRED IAW SRM 53-05, FIG 131A2. SEAT TRACK WAS REMOVED AND INSTALLED IAW SRM 51-30-1.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 63,580 hrs · 46,313 cycles

CRACKED LONGERON NR 16RT STA Y=1437 AT AFT ACCESSORY COMPARTMENT. CRACKED LONGERON WAS R & R IAW SRM 53-14-4, 51-30-5, 51-30-2,51-10-4 AND 51-10-3, PAR 21 AND 14.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 63,580 hrs · 46,313 cycles

CRACKED LONGERON NR 12RT STA Y=1437 AT AFT ACCESSORY COMPARTMENT. CRACK LONGERON WAS R & R IAW SRM 51-30-2, 51-30-5 AND 51-10-4, 51-10-3 PAR 21,14 AND DWG 5911433-85, REV BS.

Part: CUSP WEB — CORRODED (BS 1078) · corrosion level 2 · airframe 63,580 hrs · 46,313 cycles

CORROSION ON RT CUSP WEB BS 1078 BETWEEN X -54 TO X -60. THE CUSP WEB WAS REPAIRED IAW SRM 53-05 FIG 131A-9 SRM 51-30-1 AND SRM 51-10-3 PAR 14, 21, 38.

Part: CVR — DAMAGED (FUSELAGE) · corrosion level 2 · airframe 63,580 hrs · 46,313 cycles

OUT OF LIMITS, LT CUSP WEB STA Y=542-Y=549, 567-575 AND 582-585. CUSP WEB WAS REPAIRED IN STA Y=542-549, Y=567-575 AND Y=582-585 IAW SRM 53-05, FIG 131A-9 AND -6.

Part: CUSP WEB — CORRODED (BS 986-1003) · corrosion level 2 · airframe 63,580 hrs · 46,313 cycles

CORROSION BS 986 - 1003 ON LT CUSP WEB. THE DAMAGE WAS REMOVED, REPAIR FABRICATED, TREATED AND PAINTED. THE REPAIR WAS INSTALLED IAW SRM 53-05 FIG 131A, 51-10-3 PAR 14, 21, 38 AND 51-30-5.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 63,580 hrs · 46,313 cycles

CORROSION ON FUEL ACCESS PLATE COUNTERSINKS NR 1409C, 1410C AND 1464C AT RT WING. OUT OF LIMITS DUE TO CORROSION DAMAGE EXCEEDS IAW SRM 51-22-2A, CONDITION II. THEREFORE WERE REPLACED IAW SRM 51-22-2A, CONDITION III.

Part: SPACER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,580 hrs · 46,313 cycles

CORROSION ON PREVIOUS REPAIR SPACER AT CENTER LOWER CARGO COMPARTMENT DOOR JAMB AREA STA Y=636-693 AT C2. SPACER AND NUTSTRIP WERE REPLACED IAW SRM 53-05, FIG 123, 51-10-3,51-10-4, 51-30-4 AND 51-30-5.

Part: CUSP WEB — CORRODED (BS 1212-1235) · corrosion level 2 · airframe 63,580 hrs · 46,313 cycles

CORROSION ON RT CUSP WEB BETWEEN BS 1212 - 1235. DAMAGE REMOVED. REPAIR FABRICATED AND INSTALLED IAW SRM 53-05 FIG 131A.

Part: LONGERON — CRACKED (BS 1437) · airframe 63,580 hrs · 46,313 cycles

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

Part: LONGERON — CRACKED (BS 1437) · airframe 63,580 hrs · 46,313 cycles

CRACKED LONGERON 12R BS 1437. THE LONGERON WAS REMOVED AND REPLACED IAW SRM 51-30-2, 51-30-5 AND 51-10-4, 51-10-3 PAR 21, 14.

Part: STRUCTURE — CORRODED (RT HORIZ STAB) · corrosion level 2 · airframe 63,580 hrs · 46,313 cycles

CORROSION ON BARREL NUT HOLE NR 10 STA XH=27 AT HORIZONTAL STABILIZER RT SIDE. REPAIR WAS ACCOMPLISHED IAW ETI-88-16-291 REV 1 AND ER/A 549238-14, REV ORIGINAL.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 63,580 hrs · 46,313 cycles

LIGHTNING STRIKE ON LT WINDOW BELT BETWEEN STA Y655-674, UPPER AFT CORNER. LIGHTNING STRIKE ON LT WINDOW BELT STA 655-674, AFTER UPPER CORNER WAS REPAIRED IAW ER/A 549237-14, REV ORIGINAL, SRM 51-10-3, PARA 21 AND SRM 53-05, FIG 111.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 63,580 hrs · 46,313 cycles

LIGHTNING STRIKE ON LT WINDOW BELT BETWEEN STA Y712-731, FWD AND AFT SECTION. LIGHTNING STRIKE LT WINDOW BELT BETWEEN STA 712-731, AFT/FWD MID SECTION WERE REPAIRED IAW ER/A 549237-14, REV ORIGINAL, SRM 53-05, FIG 111 AND SRM 51-10-3, PARA 21.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 63,580 hrs · 46,313 cycles

LIGHTNING STRIKE ON LT WINDOW BELT BETWEEN STA Y=674-Y=693, LOWER AFT CORNER. LIGHTNING STRIKE ON LT WINDOW BELT BETWEEN STA 674-693. AFT LOWER CORNER, WAS REPAIRED IAW ER/A 549237-14, REV ORIGINAL, SRM 53-05, FIG 111 AND SRM 51-10-3 PARA 21.

Part: FITTING — CRACKED (FUSELAGE) · airframe 63,580 hrs · 46,313 cycles

CRACKED FRAME CLIP ON STA Y=1437 BETWEEN LONGERONS 1 TO 4 RT AT AFT ACCESSORY COMPARTMENT. CLIPS WERE REPLACED IAW SRM 53-14-4, 51-10-3, PAR 21 AND 14, 51-30-5.

Part: BEAM — CRACKED (R1 DOOR) · airframe 63,580 hrs · 46,313 cycles

CRACK ON BEAM 4 AT R1 DOOR FORWARD CORNER. BEAM NR 4 WAS REPLACED IAW SRM 51-30-2, 51-30-4, 51-30-5 AND DWG 9911582, REV T.

Part: FITTING — CRACKED (R1 DOOR) · airframe 63,580 hrs · 46,313 cycles

CRACKED FWD EDGE CLIP OVERBEAM 1 AT FWD SERVICE DOOR (R1). NEW CLIP WAS INSTALLED IAW SRM 51-30-5 AND DWG 9911579, REV 1.

Part: BEAM — CRACKED (R1 DOOR) · airframe 63,580 hrs · 46,313 cycles

CRACKED FWD EDGE ON BEAM NR 1 AT GALLEY SERVICE DOOR. R1 BEAM WAS REPLACED IAW SRM 51-30-1, 51-30-2, 51-30-4 AND 51-30-5.

Part: PAN — CRACKED (CARGO DOOR) · airframe 63,580 hrs · 46,313 cycles

HIDDEN DISCREPANCY: CRACKED OUTER PAN BELOW STOP FITTING NR 4 AT FWD CARGO COMPARMENT DOOR FWD EDGE. CRACKED OUTER PAN WAS REPAIRED IAW SRM 52-05D, FIG 50.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 63,580 hrs · 46,313 cycles

CRACK ON AFT SUPPORT STA Y= 1356, X= 18 RT TO X=24 RT, Z=-2 AT CPAX, W2. 6 PULLEYS AFT SUPPORT. SUPPORT WAS INSTALLED AND REPAIRED IAW SRM 53-01 FIG-2, 51-30-2 AND 51-30-5.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,580 hrs · 46,313 cycles

CORROSION OUT OF LIMITS ON RT CUSP WEB STA Y 570 TO Y 579 AT PAX CABIN FLOOR STRUCTURE. CUSP WEB WAS REPAIRED IAW SRM 53-05-FIG 131A-10, 51-30-2 AND 51-30-5.

Part: PAN — CRACKED (SERVICE DOOR) · airframe 63,580 hrs · 46,313 cycles

CRACKED PAN ON BEAM NR 4 AT FWD GALLEY SERVICE DOOR. PAN ON BEAM NR 4 WAS REPAIR IAW SRM 52-03D, FIG 3.

Part: STRUCTURE — CORRODED (LT HORIZ STAB) · corrosion level 2 · airframe 63,580 hrs · 46,313 cycles

CORROSION ON BARREL NUT HOLE NR 14 AND 26, STA XH= 27 LT AT HORIZONTAL STABILIZER. REPAIR WAS ACCOMPLISHED IAW ETI-88-16-298 REV:1, ER/A 549253-14 REV ORIGINAL AND SRM 55-03, PAR 30.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 63,580 hrs · 46,313 cycles

CRACKED RT CUSP WEBS STA Y=807 ALSO AT STA Y=845 BETWEEN X=-54 AND X=-60. CRACKED RT CUSP WEBS STA Y=807 ALSO AT STA Y=845 BETWEEN X=-54 AND X=-60. WERE REPAIRED IAW SRM 53-05, FIG 131A-9, 51-30-02, 51-10-03 PAR 14, 21, 38.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,580 hrs · 46,313 cycles

CORROSION ON RT CUSP WEB STA Y=744-746 AND 735-737. AREA ON DAMAGE WAS ATTENDED IAW SRM 53-05, FIG 131A-7.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,580 hrs · 46,313 cycles

CORROSION ON PREVIOUS RT CUSP WEB REPAIR DOUBLER UPPER, LOWER SURFACE X=-54 TO X=-60 STA Y=465 TO Y= 484 PAX CABIN. PRODUCTION DOUBLER WAS REPLACED IAW SRM 53-05, FIG 131A.

Part: CUSP WEB — CORRODED (BS 855-880) · airframe 63,580 hrs · 46,313 cycles

CORROSION OUT OF LIMITS ON RT CUSP WEB BS 855 - 857 AND BS 878 - 880. REPAIRED IAW SRM 51-30-2, 51-10-3 PARS 21,14, 38, AND 53 05 FIG 131A & 14.

Part: CUSP WEB — CORRODED (BS 845-905) · airframe 63,580 hrs · 46,313 cycles

CORROSION ON RT CUSP WEB UPPER & LOWER SURFACES FROM BS 845 TO 905. CORROSION REMOVED AND FOUND AREAS OUT OF LIMITS. REPAIRED IAW ER/A 511165-14MD.

Part: CUSP WEB — CORRODED (BS 1003-1022) · airframe 63,580 hrs · 46,313 cycles

CORROSION FROM BS 1003 - 1022 ON LT CUSP WEB. DAMAGE WAS REMOVED, NEW REPAIR FABRICATED, TREATED,PAINTED AND INSTALLED.

Part: SEAT TRACK — CORRODED (BS 200-280) · airframe 63,580 hrs · 46,313 cycles

CORROSION ON RT SEAT TRACK X -22 BETWEEN BS 200 - 280. THE SEAT TRACK WAS REPAIRED IAW SRM 53-05 FIG.

Part: FLOOR PANEL — DAMAGED (NOT REPORTED) · airframe 63,580 hrs · 46,313 cycles

CORROSION AND DISBONDED RUB STRIPS ON FLOOR PANEL NR 256A. FOUND TO BE OUT LIMITS. REPAIRED IAW SRM 53-01 FIG 4.

Part: CUSP WEB — CORRODED (BS 611-670) · airframe 63,580 hrs · 46,313 cycles

CORROSION OUT OF LIMITS ON LT CUSP WEB X 54 - 60, BS 611 - 670. REPAIRED IAW SRM 53-05 FIG. 131A-6.

Part: SKIN — DAMAGED (RT WING) · airframe 63,580 hrs · 46,313 cycles

DURING NDT INSPECTION A DISCREPANT AREA WAS FOUND ON LOWER SKIN REAR SPAR BETWEEN XRS=163 TO 168 AT RT WING. INSPECTION WAS PERFORMED PER ERA 549240-14AD.

Part: SKIN — DAMAGED (LT WING) · airframe 63,580 hrs · 46,313 cycles

DURING NDT INSPECTION A DISCREPANT AREA WAS FOUND ON LOWER SKIN REAR SPAR BETWEEN XRS=163 TO 168 AT LT WING. INSPECTION WAS PERFORMED IAW ER/A 549240-14AD.

Part: SKIN — CORRODED (TAB) · corrosion level 2 · airframe 63,580 hrs · 46,313 cycles

CORROSION ON RT ELEVATOR ANTI-FLOAT TAB UPPER SKIN. REPLACED IAW SRM 55-04 PAR. 4,.

Part: FRAME — CRACKED (BS 1448) · airframe 63,580 hrs · 46,313 cycles

CRACKED FRAME ANGLE BS 1448, LONGERONS 17 AND 18L. THE FRAME ANGLE WAS REPLACED IAW SRM 53-14-4, 51-30-2, 51-30-5, AND 51-10-3 PAR 21 - 14.

Part: SKIN — DAMAGED (RT ELEVATOR TAB) · airframe 63,580 hrs · 46,313 cycles

LIGHTNING STRIKE ON RT ELEVATOR CONTROL TAB UPPER SKIN AT HORIZONTAL STABILIZER. RT ELEVATOR CONTROL TAB WAS REPLACED IAW IPC 55-20-00-05.

Part: WEB — DAMAGED (BS 218) · airframe 63,580 hrs · 46,313 cycles

DAMAGE ON RT DIAPHRAGM BETWEEN BS 218 AND X -54E. DIAPHRAGM WAS REPAIRED IAW SRM 51-70-4 FIG 2.

Part: INTERCOSTAL — CRACKED (BS 1309-1322) · airframe 63,580 hrs · 46,313 cycles

CRACK ON INTERCOSTAL BS 1309 - 1322, X 0, Z -2. INTERCOTAL REPAIRED IAW SRM. 53-01 FIG. 2.

Part: BUSHING — DAMAGED (HEATER BLANKET) · corrosion level 2 · airframe 63,580 hrs · 46,313 cycles

CORROSION AND ELONGATED HOLES ON RT WING HEATER BLANKET TRAILING EDGE BUSHINGS. BUSHINGS WERE REPLACED IAW EA:09-070683-03 AD REV. L AND SRM 51-30-10 PAR. 7.

Part: FEEDER CABLE — DAMAGED (HYD PUMP) · airframe 63,580 hrs · 46,313 cycles

DAMAGED LACING ON AUXILIARY HYDRAULIC PUMP POWER FEEDER WIRING AT EH WHEEL WELL. LACING REPLACED IAW ER/A 467688-14MAAD REV D.

Part: VANE — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 63,580 hrs · 46,313 cycles

CORROSION FOUND ON LOWER SKIN OF RT OTBD FLAP OTBD GUIDE VANE. RIGHT OTBD FLAP OUTBD GUIDE VANE REPLACED IAW SRM 57-03D PA 11.

Part: PAN — CRACKED (BS 905) · airframe 63,580 hrs · 46,313 cycles

CRACKED RING PAN ON RIGHT AFT LOWER CORNERS BS 905. REPAIR INSTALLED IAW SRM 53-05 FIG.122, ERA 493648-14MA REV. A, ERA 487747-14MA REV ORIG, AND 51-30-5, 51-30-2.

Part: PAN — CRACKED (BS 927) · airframe 63,580 hrs · 46,313 cycles

CRACKED RING PAN ON RIGHT FWD UPPER CORNERS BS 927. REPAIR INSTALLED IAW SRM 53-05 FIG.122, ERA 493648-14MA REV. A, ERA 487747-14MA REV ORIGINAL, AND 51-30-5, 51-30-2.

Part: SPACER — CORRODED (BS 1154-1212) · corrosion level 2 · airframe 63,580 hrs · 46,313 cycles

CORROSION ON SPACER ON AFT LOWER COMPARTMENT DOOR FRAME BS 1154 - 1212. THE SPACER WAS REPLACED IAW SRM 51-10-3 PAR. 14, 21, 38, 51-30-4, 51-30-5, AND 53-05 FIG. 123.

Part: PAN — CRACKED (BS 946-1174) · airframe 63,580 hrs · 46,313 cycles

CRACKED RING PAN ON RIGHT FWD LOWER CORNERS BS 946, 1136 AND 1174. REPAIR INSTALLED IAW SRM 53-05 FIG.122, ERA 493648-14MA REV. A, ERA 487747-14MA REV ORIGINAL, AND 51-30-5, 51-30-2.

Part: PAN — CRACKED (BS 1193) · airframe 63,580 hrs · 46,313 cycles

CRACK ON LEFT RING PAN UPPER AFTER CORNER BS 1193. REPAIRED IAW SRM 53-05-FIG. 122 AND ER/A 493648-14 MA REV. A, ER/A 487747-14 MA REV. ORIG.

Part: PAN — CRACKED (BS 845-886) · airframe 63,580 hrs · 46,313 cycles

CRACKED RING PAN ON LT UPPER FWD CORNERS BS 845 - 886. PAN REPAIRED IAW SRM 53-05-FIG. 122 AND ER/A N?493648-14MA REV A, ER/A 487747-14 MA REV. ORIG.

Part: PAN — CRACKED (FUSELAGE) · airframe 63,580 hrs · 46,313 cycles

CRACK ON LT RING PAN ON LOWER FWD AND AFT CORNERS BETWEEN STA Y=1060 TO 1079. RING PAN ON LOWER FWD AND AFT CORNERS BETWEEN STA Y=1060 TO 1079 WAS REPAIRED IAW SRM 53-05-FIG 122 AND ER/A 493648-14 MA REV A , ER/A 487747-14 MA REV ORIGINAL.

Part: PAN — CRACKED (FUSELAGE) · airframe 63,580 hrs · 46,313 cycles

CRACKED RING PAN ON RT AFT UPPER CORNERS STA Y=1003, Y=1079 AND Y=1250. REPAIR PARTS WERE INSTALLED IAW SRM 53-05, FIG 122, ERA 493648-14MA, ERA 487747-14MA, REV ORIGINAL AND 51-30-5, 51-30-2.

Part: PAN — CRACKED (FUSELAGE) · airframe 63,580 hrs · 46,313 cycles

CRACKED RING PAN ON LT AFT LOWER CORNER STA Y=905. RING PAN ON LT AFT LOWER CORNER STA Y=905 WAS REPAIRED IAW SRM 53-05-FIG 122 AND ER/A 493648-14 MA, ER/A 487747-14 MA.

Part: PAN — CRACKED (FUSELAGE) · airframe 63,580 hrs · 46,313 cycles

CRACKED RING PAN ON LT AFT LOWER CORNERS STA Y=598 AND Y=927. RING PAN ON LT AFT LOWER STA Y=598 AND WAS REPAIRED IAW SRM 53-05, FIG 122 AND ER/A 493648-14 MA, REV A.

Part: PAN — CRACKED (FUSELAGE) · airframe 63,580 hrs · 46,313 cycles

INITIAL, CRACK ON LT RING PAN ON LOWER AFT CORNER ON STA Y=1098. RING PAN ON LOWER AFT CORNER ON LT STA Y=1098 WAS REPAIRED IAW SRM 53-05-FIG 122 AND ER/A 493648-14MA REV A, ER/A 487747-14 MA REV ORIGINAL.

Part: PAN — CRACKED (FUSELAGE) · airframe 63,580 hrs · 46,313 cycles

CRACKED RING PAN ON LT FWD LOWER CORNER STA Y=927. RING PAN ON LT STA Y=927 WAS REPAIRED IAW SRM 53-05 FIG 122 AND ER/A 493648-14 MA, ER/A 487747-14 MA.

Part: RELEASE CABLE — MISRIGGED (TAILCONE) · airframe 60,638 hrs · 44,226 cycles

MAINTENANCE FOUND THAT THERE WAS EXCESSIVE TENSION IN THE RELEASE CABLE SYSTEM. SO MUCH TENSION THAT THE CONE RELEASED WITHOUT PULLING THE CABLE. ALSO, THE KEVLAR SLEEVE OVER THE RELEASE CABLE FOR THE TAILCONE WAS WORN OUT OF ALLOWABLE LIMITS. THE CABLE WAS REPLACED AND THE SYSTEM WAS RIGGED TO SPECIFICATIONS. THE RII STEPS WERE COMPLETED AND THE FOLLOW-UP CHECK WAS SUCCESSFUL.

Part: RELEASE CABLE — FRAYED (TAILCONE) · airframe 60,638 hrs · 44,226 cycles

MAINTENANCE DISCOVERED THAT THE TAILCONE EMERGENCY RELEASE CABLE WAS FRAYED BEYOND ALLOWABLE LIMITS. THE CABLE WAS REPLACED AND THE SYSTEM WAS RIGGED TO SPECIFICATIONS.

Part: LIGHT — NO TEST (LT WING) · airframe 60,611 hrs · 44,213 cycles

LEFT AFT WING ANTI-COLLISION LIGHT INTENSITY TEST FAILED. R & R AFT LT WING ANTI-COLLISION LIGHT IAW AMM 33-43-01/201, OPS CHECK GOOD.

Part: SKIN — CRACKED (TAIL) · airframe 60,611 hrs · 44,213 cycles

TAIL INTERIOR CROWN SKIN IS CRACKED.

Part: CLAMP — OUT OF ADJUST (TAILCONE) · airframe 59,731 hrs · 43,639 cycles

MAINTENANCE FOUND TAILCONE EXTERNAL RELEASE CABLE CLAMPS LT AND RT, ITEMS 20 AND 21 OF AMDS WC 5350-01077-0101, FIG 5, OUT OF ADUSTMENT. MAINTENANCE ADJUSTED RELEASE CLAMPS IAW AMDS 5350-01077-0101.

Part: STRAP — CONTAMINATED (TAILCONE SLIDE) · airframe 59,721 hrs · 43,635 cycles

MAINTENANCE FOUND TWO AFT TAILCONE SLIDE RETENTION STRAPS ATTACHED AT FRAME OIL SOAKED. MAINTENANCE R & R STAPS.

Part: CABLE — TWISTED (TAILCONE) · airframe 59,714 hrs · 43,632 cycles

MAINTENANCE FOUND TAILCONE AFT LT UPPER LATCH LOCKING CABLE TWISTED. MAINTENANCE REPLACED AND ADJUSTED CABLE.

Part: TEE FITTING — DAMAGED · airframe 59,731 hrs · 43,639 cycles

MAINTENANCE FOUND A TEE PIN, ITEM 11, BUSHING LT AN RT HAVE FLAT STOPS THIS TEE PIN IS LOCATED AT THE TAILCONE INTERNAL RELEASE HANDLE. MAINTENANCE R & R BUSHINGS. IAW AMDS CARD 5350-01077-0101.

Part: FRAME — CRACKED (TAILCONE) · airframe 59,714 hrs · 43,632 cycles

BS 1510, FRAME CRACKED AT UPPER RT TAIL CONE LATCH. REPLACED THE FRAME IAW SRM 51-01.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 63,580 hrs · 46,313 cycles

WORKING LIGHTNING STRIKE DAMAGE AT STA 368, STR 25L. INSTALLED TEMP REPAIR AT STA 368, STR 25L, REF SRM53-04-2, PARA 1. AREA WAS REPAIRED IAW SRM 53-04-2, FIG 2.

Part: LIGHT — INOPERATIVE (SEAT 12D) · airframe 58,091 hrs · 42,463 cycles

DURING LINE CHECK, MAINTENANCE FOUND THE SEAT MOUNTED EMERGENCY LIGHT AT SEAT 12D WAS INOPERATIVE. MAINTENANCE R & R THE SEAT 12D EMERGENCY LIGHT AND THE LIGHTS RETURNED TO AN OPERATIVE STATE.

Part: STRUCTURE — WORN (TAILCONE SLIDE) · airframe 56,547 hrs · 41,415 cycles

THE TAIL CONE SLIDE PACK PLATFORM IS WORN UNDER THE FWD EDGE OF THE TAILCONE SLIDE PACK COVER LT SIDE. REPAIRED IAW ER/A 497244-14MA.

Part: SUPPORT — CRACKED (MLG) · airframe 56,533 hrs · 41,404 cycles

UPPER WING GEAR SUPPORT PLATE "BEAVER TAIL" HAS A CRACK AT A FASTENER HOLE. COMPLIED WITH ER/A 519400-14.

Part: ANGLE — CORRODED (THRESHOLD) · corrosion level 2 · airframe 56,533 hrs · 41,404 cycles

DURING SCHEDULED CHECK, CORROSION WAS FOUND IN NUMEROUS AREAS ON THE AFT CARGO DOOR THRESHOLD ZEE ANGLE STRAP. ANGLE STRAP WAS REPLACED.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 56,533 hrs · 41,404 cycles

DURING SCHEDULED CHECK, FUEL TANK ACCESS PANEL 1311C ON THE TOP OF THE LT WING CORRODED IN THE TANK PLATE HOLES. ACCESS PANEL REPLACED IAW AMM 28-0.

Part: ANGLE — CORRODED (THRESHOLD) · corrosion level 2 · airframe 56,533 hrs · 41,404 cycles

DURING SCHEDULED CHECK, THE AFT CARGO BIN THRESHOLD ZEE ANGLE STRAP HAD CORROSION IN MULTIPLE AREAS AT THE RIVNUTS. FABRICATED NEW SPACER AND REPLACED SPACER AND ZEE ANGLE STRAP IAW SRM 53-05.

Part: FLOOR SUPPORT — CORRODED (BS 1136-1155) · corrosion level 2 · airframe 56,533 hrs · 41,404 cycles

DURING SCHEDULED CHECK, THE AFT CARGO FLOOR SUPPORT BETWEEN BS 1136-1155 HAD CORROSION IN NUMEROUS AREAS. FLOOR SUPPORT REPLACED IAW DWG 5936071.

Part: FLOOR SUPPORT — CORRODED (BS 1212) · corrosion level 2 · airframe 56,533 hrs · 41,404 cycles

DURING SCHEDULED CHECK, AFT CARGO FLOOR SUPPORT AT BS 1212 BETWEEN 28L & 29R HAD CORROSION IN TWO AREAS THAT WAS BEYOND ACCEPTABLE LIMITS. THE FLOOR SUPPORT WAS REPLACED IAW DWG 5936597.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 56,272 hrs · 41,181 cycles

THE EMERGENCY LIGHT LENS BETWEEN THE AFT ROW OF PASSENGER SEATS IS MISSING. THE LENS WAS REPLACED AND OPS CHECK OF THE SYS WAS NORMAL.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 56,232 hrs · 41,148 cycles

DURING ROUTINE LINE CHECK, NOTED INTERIOR CEILING EMERGENCY EXIT LIGHTS AT ROWS 3-4 WERE INOPERATIVE. OVERWING (INTERIOR) EMERGENCY EXIT SIGN AT ROW 25 WAS ALSO INOPERATIVE. EMERGENCY LIGHT BATTERY PACKS B5-100 & B105 REPLACED IAW AMM 33-50 AND OPS CHECKED NORMAL.

Part: FUSE — BLOWN (EMERGENCY LIGHT) · airframe 54,663 hrs · 40,037 cycles

DURING SERVICE CHECK, MX FOUND ROWS AFT OF 31 THRU TO 36 EMERGENCY LIGHTS INOPERATIVE. FOUND FUSE BLOWN AT BATTERY PACK B5-212. REPLACED FUSE. OPS CHECKS NORMAL.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 54,584 hrs · 39,992 cycles

DURING SERVICE CHECK, MX FOUND COCKPIT AND FORWARD ENTRY AREA EMERGENCY LIGHTS INOPERATIVE. R & R BATTERIES IN BATTERY PACK BP523. OPS CHECKS NORMAL.

Part: WIRE HARNESS — DAMAGED (EMERGENCY LIGHTS) · airframe 54,486 hrs · 39,927 cycles

DURING LINE CHECK, MX FOUND THAT THE EMERGENCY PATHWAY LIGHTING AT ROW 21D IN THE CABIN WAS INOPERATIVE. MX FOUND WIRES PULLED OUT OF THE CONNECTOR. THE WIRE HARNESS WAS REPLACED AND THE SYS RETURNED TO NORMAL OPERATION.

Part: INLET — CONTAMINATED (APU ENGINE) · airframe 54,100 hrs · 39,648 cycles

ON TAXI IN, WHEN APU IS PROVIDING AIR TO AIR CONDITIONING, AN ABNORMAL ODOR IS OMITTED FROM ACFT VENTS. ACFT IS NORMAL ON ENGINE AIR. TROUBLESHOT FOUND APU INLET CONTAMINATED WITH HYDRAULIC FLUID. CLEANED INLET, PERFORMED APU DUCT BURNOUT AND REPLACED COALESCER BAGS. LEAK CHECKS GOOD. OK FOR SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 53,973 hrs · 39,562 cycles

DURING SERVICE CHECK, MX FOUND EMERGENCY ESCAPE PATHWAY LIGHT INOPERATIVE AT ROW 34. LAMPED ESCAPE PATHWAY LIGHT AT ROW 34. OPS CHECKED GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 53,973 hrs · 39,562 cycles

DURING SERVICE CHECK, MX FOUND EMERGENCY ESCAPE PATHWAY LIGHT AT ROW 13 INOPERATIVE. MX LAMPED ESCAPE PATHWAY LIGHT AT ROW 13. OPS CHECKED GOOD.

Part: CONTROL VALVE — LEAKING (HYD SYSTEM) · airframe 53,883 hrs · 39,503 cycles

FLIGHT ATTENDANT REPORTED FUMES CAUSING EYE IRRITATION AND ODOR IN CABIN DURING FLIGHT. FLIGHT CREW SHUT DOWN RIGHT AIR CONDITIONING PACK, AFTER WHICH THE FUMES AND ODOR WENT AWAY. MAINTENANCE FOUND THE AFT STAIR DOOR CONTROL VALVE LEAKING AND REPLACED THE VALVE. LEAK AND OPERATIONAL CHECKS WERE GOOD. CLEANED HYDRAULIC FLUID FROM THE AFT LOWER COMPARTMENT AND APU INLET. PERFORMED OPN 5090 ALTERNATE DUCT BURN, LEFT SIDE OK, RIGHT SIDE ODOR STILL PRESENT. REPEATED OPN 5090 STEP 2G THROUGH 2P AND STEP 3 AND COMPLETED OPN 5090. NO ODOR PRESENT. OK FOR SERVICE.

Part: LANYARD — BROKEN (L1 DOOR SLIDE) · airframe 53,336 hrs · 39,108 cycles

L1 DOOR SLIDE GIRT BAR LANYARD BROKEN. REMOVED AND REPLACED LATCH ASSEMBLY PER AMM. AIRCRAFT OKAY FOR SERVICE.

Part: SPAR — CRACKED (VERTICAL STAB) · airframe 52,948 hrs · 38,869 cycles

VERTICAL STABILIZER FRONT SPAR LT CHORD AT ZFS-52 CRACKED. ACCOMPLISH SECTION II REPAIR AT NEXT C-CHECK OR 3000 CYCLES AFTER SECTION 1, WHICHEVER COMES FIRST. REF NR 37 FOR FABRICATION OF SG09550005-3 REPAIR STRAP. 227037 REMOVED TEMPORARY REPAIR STRAP INSTALLED ON SECTION 1 OF ERA 488147-14.

Part: ROD — OUT OF RIG (TAILCONE) · airframe 52,948 hrs · 38,869 cycles

DURING TAIL CONE FUNCTIONAL CHECK A/C JIC CARD OPN 6908AD THE AFT ENTRANCE DOOR EXTEND ROD WAS FOUND OUT OF RIG. THE ROD WAS ADJUSTED PER OPN 6908AD AND THE MD -88 AMM 53-53-00 AND THE OPS CHECK WAS GOOD.

Part: SPAR — DAMAGED (VERTICAL STAB) · airframe 52,948 hrs · 38,869 cycles

WHILE IN MSP FOR PSV, AND DURING INSPECTION PER EA 09-470871-12AD, AN ELONGATED HOLE WAS FOUND ON THE LT LOWER AFT HOLE (HOLE COMMON TO LT SPAR FWD FLANGE). A BUSHING ONLY REPAIR FOR THIS HOLE LOCATION IS NOT ALLOWED PER SG09550004 REV "B". REPAIR ACCOMPLISHED PER ER/A 502538-14AD.

Part: SKIN — DAMAGED (VERTICAL STAB) · airframe 52,948 hrs · 38,869 cycles

DURING PSV IN MSP, 2EA ELONGATED HOLES WERE FOUND ON THE LT SIDE OF THE VERTICAL STABILIZER LOWER FIXED SKIN JUST BELOW ZFS=52, COMMON TO LT SPAR CHORD. THE HOLES WILL BE OPENED IN THE FIXED L/E SKIN TO A MAX SIZE OF 0.327 DIA AND A BUSHING/DOUBLER REPAIR INSTALLED TO RESTORE THE NOMINAL HOLE SIZE PER ER/A 502542-14 AD.

Part: SPAR CAP — DAMAGED (VERTICAL STAB) · airframe 52,948 hrs · 38,869 cycles

DURING INSPECTION PER AD 2011-15-0, EA 09-470871-12, AND SECTION 111OF ER/A 488147-14AD REV B MTC NOTED 5 ELONGATED HOLES COMMON TO THE VERTICAL STABILIZER LT SPAR CAP LOCATED JUST ABOVE THE PREVIOUSLY BUSHED HOLE AT ZFS =52. THE SUBJECT CAP IS MACHINED TO VARYING THICKNESSES OF 7075-T6AL. REPAIR PER ER/A 488147-14AD.

Part: SPAR CAP — DAMAGED (VERTICAL STAB) · airframe 52,948 hrs · 38,869 cycles

DURING INSPECTION PER AD 2011-15-01 AND EA 09-470871-12AD, MTC NOTED 8 ELONGATED HOLES COMMON TO THE VERTICAL STABILIZER RT SPAR CAP LOCATED JUST ABOVE ZFS=52. THE SUBJECT CAP IS MACHINED TO VARYING THICKNESS OF 7075-T56 AL. REPAIR ACCOMPLISHED PER ER/A 502519-14AD.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 52,925 hrs · 38,855 cycles

DURING SERVICE CHECK, MAINTENANCE FOUND FIRST CLASS SEAT EMERGENCY LIGHTS INOPERATIVE. REPLACED FIRST CLASS EMERGENCY LIGHT BATTERY PACK CHARGER PER AMM. OPERATION CHECKS NORMAL.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 52,863 hrs · 38,818 cycles

DURING SERVICE CHECK, MAINTENANCE FOUND FIRST CLASS EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED FIRST CLASS BATTERY PACK. OPERATION CHECKS GOOD.

Part: POWER SUPPLY — MALFUNCTIONED (CABIN) · airframe 51,638 hrs · 38,006 cycles

DURING LINE CHECK, MAINTENANCE FOUND AFT EMERGENCY WING EGRESS LIGHTS STAY ILLUMINATED WHEN EMERGENCY LIGHTS SELECTED OFF. MAINTENANCE REMOVED AND REPLACED WING EGRESS EMERGENCY POWER SUPPLY PER MAINTENANCE MANUAL. OPERATION CHECKS NORMAL.

Part: BATTERY — DISCHARGED (CABIN) · airframe 50,953 hrs · 37,518 cycles

DURING LINE CHECK, MAINTENANCE FOUND RIGHT FORWARD DOOR, LEFT FORWARD AND AFT OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. MAINTENANCE REPLACED BATTERIES ON FORWARD AND AFT EMERGENCY LIGHTS UPPER ASSEMBLIES PER MAINTENANCE MANUAL. OPERATION CHECKS GOOD.

Part: LANYARD — MISROUTED (DOOR SLIDE) · airframe 49,799 hrs · 36,767 cycles

DURING LINE CHECK MX, FOUND L1 AND L2 DOOR SLIDE LANYARDS INCORRECTLY ROUTED TO GIRT BAR. MX REROUTED LANYARDS IAW MM 25-62-00. ON 12-04-10 ON LOG 4736535001 L1 & L2 SLIDE DOOR LANYARDS WERE FOUND INCORRECTLY INSTALLED. MX REROUTED LANYARDS MM 25-62-00.

Part: LANYARD — MISINSTALLED (DOOR SLIDE) · airframe 49,660 hrs · 36,684 cycles

ON LINE CHECK, MX FOUND L2 DOOR SLIDE LANYARD FRAYED AND INSTALLED INCORRECTLY. ALSO FOUND L1 DOOR SLIDE LANYARD INSTALLED INCORRECTLY. MX REPOSITIONED L1 DOOR SLIDE LANYARD AND REPLACED L2 DOOR SLIDE LANYARD IAW MM.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHTS) · airframe 49,103 hrs · 36,336 cycles

DURING LINE CHECK, MX FOUND THE EMERGENCY PATH LIGHTS AT SEATS 3 AND 19 TO BE INOPERATIVE. MX RECONNECTED A CONNECTOR AT SEAT 3 AND RE-LAMPED THE LIGHTS AT SEAT 19. OPS CHECK OF LIGHTS IS NOW GOOD.

Part: PAN — CRACKED (CARGO DOORWAY) · airframe 48,982 hrs · 36,252 cycles

DURING HMV3, FOUND MID CARGO DOOR AFT END BETWEEN NR 2 AND NR 3 BEAMS. BEAM PAN HAS APPROX 2" CRACK ABOVE END FITTING. STOP DRILLED CRACK IAW SRM 51-01, HFEC INSP VERIFIED CRACK CONTAINMENT IAW NDT SPM 06-10-01 LOCATED DRILLED AND INSTALLED NEW REPAIR DOUBLER PN SR09520013-3 IAW SRM 51-10-2, 51-10-2, 51-10-4, 51-30-2, 51-30-5 AND 51-30-1.

Part: FLOOR SUPPORT — CORRODED (BS 180-200) · corrosion level 2 · airframe 48,982 hrs · 36,252 cycles

DURING HMV3, FOUND MAIN PAX CABIN FLOOR SUPPORT HAS CORROSION SPOTS AT BL 0 FROM STA 180-200. R & R FLOOR SUPPORT IAW SRM 53-10-4, 51-30-1.

Part: SKIN — CRACKED (LT WING) · airframe 48,982 hrs · 36,252 cycles

LT WING L/E SKIN/LOWER SURFACE XOS 243 CRACKED. INSTALLED PERMANENT REPAIR IAW ERA 380953-14MA AND ERA 482367-14.

Part: ATTACH ANGLE — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 48,982 hrs · 36,252 cycles

MID CARGO DOOR LOWER FWD ATTACH ANGLE TO INTERCOSTAL WEB BELOW FWD FITTING HAS CORROSION. REMOVED T ANGLE AND REPLACED IAW SRM 51-30-2 AND 51-30-5. ORIGINAL ANGLE FOUND TO BE BEYOND SRM LIMITS.

Part: CARGO TRACK — CORRODED (BS 1211-1322) · corrosion level 2 · airframe 48,982 hrs · 36,252 cycles

AFT CARGO BETWEEN STA 1211 AND 1322 RT TIE DOWN TRACK HAS CORROSION. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. R & R TIE DOWN TRACK IAW SRM 51-30-1 AND 51-30-5.

Part: CUSP WEB — CORRODED (BS 712-731 L18R) · corrosion level 2 · airframe 48,982 hrs · 36,252 cycles

MID CARGO, STA 712 TO 731, LONGERON 18R, CUSP WEB HAS CORROSION ON BOTTOM SIDE AT CTR OTBD LIGHTNING HOLE. REMOVED CORROSION, FOUND TO BE BEYOND LIMITS. INSTALLED REPAIR IAW DRD 53-05D FIG 827D.

Part: FLOOR SUPPORT — CRACKED (CABIN) · airframe 48,982 hrs · 36,252 cycles

FLOOR PANEL NR886C, 2EA SIDE EXPANSION SUPPORTS CRACKED AND CHAFED 13EA PLACES. FABRICATED COVER IAW SRM 51-10-2 AND REPLACED RT EXPANSION SUPPORT AND INSTALLED BOTH IAW SRM 51-30-8 AND 51-20-0.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,982 hrs · 36,252 cycles

AFT ACCESSORY COMPARTMENT AIRSTAIR, FWD END SEAL ATTACH ANGLE CORRODED. FOUND TO OUT OF LIMITS IAW SRM 53-01, FIG 1. FABBED NEW ATTACH ANGLE IAW SRM 51-10-2 AND INSTALLED IAWSRM 51-30-2 AND SRM 51-30-1.

Part: DEPRESSOR — CORRODED (L1 DOOR SEAL) · corrosion level 2 · airframe 48,982 hrs · 36,252 cycles

L-1 DOOR SEAL DEPRESSORS, 2 EA, HAVE CORROSION THROUGHOUT 20 SQ INCHES. 100 PERCENT MATERIAL LOSS. R & R SEAL DEPRESSOR IAW SRM 51-10-2, 51-10-4 AND 51-30-5.

Part: FORMER — CHAFED (APU ENCLOSURE) · airframe 48,982 hrs · 36,252 cycles

APU CUTOUT FWD END BETWEEN STR 28L-29L, FORMER CHAFED THROUGH. REPAIRED FORMER IAW PS 900-6-3 AND ERA 094719-14MA AND REINSTALLED FORMER.

Part: FLOOR SUPPORT — CORRODED (BS 157-200) · corrosion level 2 · airframe 48,982 hrs · 36,252 cycles

MAIN PAX ABIN FLOOR SUPPORT HAS CORROSION AT LBL 48, BETWEEN BS 157 AND BS 200. 100 MATERIAL LOSS. R & R FLOOR SUPPORT IAW SRM 51-10-4, 51-30-1 AND 51-30-5.

Part: SKIN — CRACKED (RT ELEVATOR) · airframe 48,982 hrs · 36,252 cycles

RT ELEVATOR GEAR TAB FAIRING 3612A IS CRACKED ON LOWER SKIN APPROX .5 ". REMOVED DAMAGED SKIN AND INSTALLED NEW SKIN IAW SRM 51-30-2.

Part: CUSP WEB — CORRODED (BS 1098-1174) · corrosion level 2 · airframe 48,982 hrs · 36,252 cycles

MAIN CABIN INTERIOR; L-2 DOOR CUSP WEB HAS CORROSION. FOUND TO BE 100 PERCENT MATERIAL LOSS. R & R CUSP WEB FROM STA 1098 TO STA 1174 IAW SRM 51-30-1, 51-30-2 AND 51-30-5.

Part: ATTACH BRACKET — CORRODED (GIRT BAR) · corrosion level 2 · airframe 48,982 hrs · 36,252 cycles

MAIN CABIN R1 DOOR GIRT BAR MOUNT ATTACH BRACKET CORRODED. FOUND TO BE BEYOND SRM LIMITS. RECEIVED AND INSTALLED NEW GIRT BAR FITTING IAW SRM 53-15-1,FIG 11, 51-30-1 AND 53-01, FIG1.

Part: PLUG — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,982 hrs · 36,252 cycles

HMV3 CORROSION ON O/B SEAT TRACK PLUG STA 465 LBL 54. REPLACED PLUG IAW SRM 51030-1 53-05 FIG 4A (DLM88101816).

Part: SHEAR TIE — CRACKED (FUSELAGE) · corrosion level 2 · airframe 48,982 hrs · 36,252 cycles

HMV3 SHEAR TIE CRACKED STA 1429 L13R-L12R. REPLACED SHEAR TIE IAW SRM 51-30-2 51-30-3 (DLM88101819).

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,982 hrs · 36,252 cycles

HMV3 CABIN LT SIDE CUSP WEB CORRODED STA 674-693 LBL 60. REPAIR CUSP WEB IAW SRM DRD EA 53-05D FIG 827D (DLM88101909).

Part: DOUBLER — DAMAGED (FUSELAGE) · airframe 48,982 hrs · 36,252 cycles

HMV3 FUSELAGE EXTERIOR STA 229 L17L HAS CREASE IN GOUGE REPAIR IAW SRM 53-04D FIG 12B. CUT OUT DAMAGE AND INSTALLED DOUBLER (DLM88101908).

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,982 hrs · 36,252 cycles

HMV3 FUSELAGE SKIN STA 1437, 2 INCHES ABOVE L2L SKIN CRACKED. REPAIR PER SRM 53-01 FIG 4 (DLM88101884).

Part: SKIN — CRACKED (BS 1437 L3R) · airframe 48,982 hrs · 36,252 cycles

FUSELAGE EXTERIOR STA 1437 1IN ABOVE LONGERON 3R, SKIN CRACKED APPROX .5 IN. REPAIRED IAW SRM 53-01, FIG 4.

Part: SKIN PANEL — CRACKED (VERTICAL STAB) · airframe 48,982 hrs · 36,252 cycles

HMV3 VERTICAL STAB LOWER LT SKIN PANEL CRACKED AT LOWER AFT CORNER OF PANEL. CUT OUT REPAIR SKIN PANEL IAW SRM 55-01 FIG 2 55-32-0 (DLM88101838).

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,982 hrs · 36,252 cycles

HMV3 CORROSION ON CUSP WEB STA 617-636 LBL 60 L18L. FABRICATED AND INSTALLED FILLER AND REPAIR DOUBLER IAW MD88 SRM 53-05D FIG 827D (DLM88101808).

Part: SKIN — CHAFED (VERTICAL STAB) · airframe 48,982 hrs · 36,252 cycles

VERTICAL STAB STR LT SIDE LOWER AFT SIDE OF CUTOUT, SKIN PANEL CHAFED. BLENDED CHAFED AREA, FOUND TO BE BEYOND SRM LIMITS. REPAIRED IAW SRM 55-01, FIG 4.

Part: ATTACH FITTING — CRACKED (VERTICAL STAB) · airframe 48,982 hrs · 36,252 cycles

HMV3 VERTICAL STAB LOWER RT SIDE ATTACH CLIP TO FUSELAGE CRACKED. REPLACED ATTACH CLIP IAW 51-10-2, 51-30-5, 51-30-2, 51-10-4 (DLM88101830).

Part: CUSP WEB — GOUGED (FUSELAGE) · airframe 48,982 hrs · 36,252 cycles

HMV3 CABIN LT SIDE I/B CUSP WEB HAS 1 INCH GOUGE STA 598 LBL 48. REPAIR PER SRM 53-05D FIG 827D (DLM88101912).

Part: STIFFENER — CRACKED (VERTICAL STAB) · airframe 48,982 hrs · 36,252 cycles

HMV3 VERT STAB LOWER L/E INTERIOR RT SIDE FIFTH STIFFENER FROM TOP CRACKED REPAIR IAW SRM 51-70-05 51-10-2 51-10-3 51-30-02. INSTALLED REPAIR ANGLES (DLM88101910).

Part: CARGO TRACK — CORRODED (BS 1007-1155) · corrosion level 2 · airframe 48,982 hrs · 36,252 cycles

AFT CARGO BETWEEN STA 1007 AND 1155 RT SIDE, TIE DOWN TRACK HAS CORROSION (MRB 53-100-17). REMOVED CORROSION, BEYOND SRM LIMITS. REPLACED CARGO TIE DOWN TRACK IAW SRM 51-30-1 AND SRM 51-30-5.

Part: THRESHOLD — CORRODED (AIRSTAIR) · corrosion level 2 · airframe 48,982 hrs · 36,252 cycles

CABIN AFT AIRSTAIR THRESHOLD IS EXFOLIATED, CORROSION. REMOVED CORROSION, 100 MATERIAL LOSS. INSTALLED NEW DOOR JAMB PN 5917463-11 IAW SRM 51-30-1, 51-30-2 AND 51-30-5.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,982 hrs · 36,252 cycles

HMV3 CABIN FLOOR SUPPORT STA 197 LBL 46 CORRODED. REPLACED FLOOR SUPPORT IAW SRM 53-01 SH 3 53-14-1 FIG 11 (DLM88101907).

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,982 hrs · 36,252 cycles

HMV3 LT SIDE CENTER SEAT TRACK CORRODED UPPER SURFACE STA 218-230. REPLACED SEAT TRACK IAW SRM 53-05 FIG 4B (DLM88101840).

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 48,982 hrs · 36,252 cycles

HMV3 SEAT TRACK STA 200-313 LBL 22 CORRODED. REPLACED SEAT TRACK IAW SRM 53-05 FIG 4B1 53-24-0 FIG 3 (DLM88101827).

Part: RUB STRIP — CHAFED (TE FLAP) · corrosion level 2 · airframe 48,982 hrs · 36,252 cycles

HMV3 LEFT WING I/B FLAP NR 2 RUB STRIP CHAFED. REPLACED RUB STRIP IAW SRM 51-30-2 (DLM88101828).

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,982 hrs · 36,252 cycles

HMV3 CABIN FLOOR SUPPORT CORRODED STA 200 LBL 2.5-10.5. REPLACED FLOOR SUPPORT IAW SRM 53-01 FIG 1 53-14-1 (DLM88101841).

Part: BRACKET — CRACKED (FUSELAGE) · airframe 48,982 hrs · 36,252 cycles

HMV3 INTERCOSTAL BRACKET CRACKED STA 788 BETWEEN L28R-L27R. REPLACED BRACKET IAW SRM 51-30-2 51-30-5 (DLM88101824).

Part: SKIN — CORRODED (BS 693 L29-30R) · corrosion level 2 · airframe 48,982 hrs · 36,252 cycles

MID CARGO, FWD OF STA 693 BETWEEN LONG 30 & 29R, SKIN HAS CORROSION. REMOVED CORROSION, FOUND TO BE BEYOND SRM LIMITS. ALSO FOUND ANTENNA DOUBLER TO BE CORRODED BEYOND LIMITS. REMOVED DOUBLER. INSTALLED SKIN DOUBLER AND ANTENNA DOUBLER IAW SRM 51-30-1 AND 51-30-5.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,982 hrs · 36,252 cycles

HMV3 CABIN FLOOR SUPPORT AT LBL 14 STA 160-200 CORRODED. REPLACED FLOOR SUPPORT IAW SRM 53-01 FIG 1 (DLM88101814).

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,982 hrs · 36,252 cycles

HMV3 INTERCOSTAL CORRODED AT STA 236 BETWEEN R27-R28. REMOVED AND REPLACED INTERCOSTAL IAW SRM 51-10-3 53-01 FIG 1 (DLM88101811).

Part: CUSP WEB — CORRODED (BS 712-731) · corrosion level 2 · airframe 48,982 hrs · 36,252 cycles

MID CARGO STATION 712 TO 731, LONG 18R, CUSP WEB HAS CORROSION ON BOTTOM SIDE AT CTR OTBD LIGHTNING HOLE. REMOVED CORROSION, FOUND TO BE OUT OF SRM LIMITS. REPAIRED IAW SRM 53-05D, FIG 827D.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,982 hrs · 36,252 cycles

HMV3 CABIN FLOOR SUPPORT CORRODED STA 180-200 RBL 36. REPLACED FLOOR SUPPORT IAW SRM 51-10-3 (DLM88101813).

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 48,982 hrs · 36,252 cycles

HMV3 CUSP WEB CRACKED STA 218 AND 237 LT SIDE. REPLACED CUSP WEB PER SRM 51-30-5 (DLM88101913).

Part: DOUBLER — CHAFED (CARGO DOOR) · corrosion level 2 · airframe 48,982 hrs · 36,252 cycles

HMV3 FWD CARGO DOOR EXTERIOR SKIN DOUBLER CHAFED. REPLACED DOUBLER IAW EA 52-05D FIG 806D SHEET 4 (DLM88101822).

Part: DOUBLER — CHAFED (CARGO DOOR) · airframe 48,982 hrs · 36,252 cycles

HMV3 FWD CARGO DOOR EXT SKIN DOUBLER AT FWD CORNERS CHAFED. REPLACED DOUBLERS AT FWD CORNERS IAW EA 52-05D FIG 806D (DLM88101823).

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 48,982 hrs · 36,252 cycles

HMV3 CARGO TRACK CORRODED STA 693-788 RIGHT SIDE. REPLACED CARGO TRACK IAW SRM 51-10-3 (DLM88101812).

Part: STRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,982 hrs · 36,252 cycles

HMV3 STA 1174 TIE STRAP L28L-L29L CORRODED. REPLACED STRAP IAW SRM 53-01 FIG 1 53-14-3 FIG 3A (DLM88101818).

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 48,982 hrs · 36,252 cycles

HMV3 FWD CARGO DOOR AFT END NR 1 STOP CRACKED. REPLACED STOP IAW SRM 51-30-5 (DLM88101842).

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,982 hrs · 36,252 cycles

HMV3 INTERCOSTAL CORRODED STA 1211-1231 L29L. REPLACED INTERCOSTAL IAW SRM 51030-05 (DLM88101815).

Part: STRAP — CORRODED (FUSELAGE) · airframe 48,982 hrs · 36,252 cycles

HMV3 TIE STRAP CORRODED STA 1193 L28R-L29R. REPLACED TIE STRAP IAW SRM 53-01 FIG 1 (DLM88101821).

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,982 hrs · 36,252 cycles

HMV3 TEMP REPAIR CRACKED RT WW AFT FRAME O/B END REPAIR FRAME IAW SRM 53-05D (DLM88101887).

Part: FRAME — CRACKED (LT MLG WW) · airframe 48,982 hrs · 36,252 cycles

HMV3 TEMP REPAIR CRACKED LT WW AFT FRAME O/B END. REPAIRED FRAME IAW SRM 53-05 FIG 809D SHEET 5, 51-10-2, 51-30-2 (DLM88101886).

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,837 hrs · 36,150 cycles

HMV3 CORROSION ON CUSP WEB STA 1174 LBL 60 L18L. REPAIRED CUSP WEB STA 1174 LBL 6 L18L PER DRD EA 53-05 FIG 827D SHEET 1.

Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 48,164 hrs · 35,697 cycles

EMERGENCY LIGHTS INOP AT SEATS 11, 13, 19, 23, 24, AND 28. RELAMPED SEATS 11131923. REPAIRED BROKEN WIRE AT SEAT 24 LIGHT TERMINAL CONNECTION REPLACED LIGHT ASSY AT SEAT 28. OPS, CK GOOD.

Part: SWITCH — ARCED (COCKPIT) · airframe 46,489 hrs · 34,559 cycles

DURING PUSH BACK GOT A STRONG ELECTRICAL ODOR IN THE COCKPIT. THE CAPT'S ND AND PFD STARTED TO FLASH ON AND OFF. ALSO, THE CAPT'S A/S, VSI AND ALT OFF FLAGS FLASHED ON AND OFF. EMERGENCY SWITCH ARCING DURING STANDBY PWR CK. REMOVED AND REPLACED SWITCH. PERFORMED CK OUT PER M/M 24-23-02-401 NORMAL PER CK OUT.

Part: ENGINE — MALFUNCTIONED (NR 1) · airframe 38,529 hrs · 29,319 cycles

CREW REPORTED THE LEFT ENGINE OIL TEMP STARTED FLUCTUATING. TEMP WENT ABOVE 135 DEG AND THEN BACK TO NORMAL. TEMP THEN ROSE TO 165 AND CREW SHUT DOWN ENGINE PER QRH. NONE NOTED. MILLION AIR MTC AP 2664148, REPLACED LT ENG OIL TEMP BULB RAN ENG PER MM. CK-OUT OIL TEMP CKS NML. NO FLUX NOTED.

Part: FITTING — LEAKING (CASE FILTER) · airframe 33,585 hrs · 25,807 cycles

ON TAXI IN LOST ALL HYDRAULIC PRESSURE ON BOTH SIDES WITH ENGINES RUNNING AND ELECTRICAL PUMPS ON. QUANTITY WAS NORMAL. FOUND LT FWD CASE DRAIN FILTER LEAKING FROM OUTBOARD FITTING. TIGHTENED FITTING AND CLEANED AREA. PRESSURE AND INDICATIONS ALL NORMAL ON ENG RUN.

Part: SKIN — DAMAGED (LT WING SLAT) · airframe 31,381 hrs · 24,321 cycles

NR 1 SLAT OUTER SKIN ASSEMBLY, XFS 155 TO XFS 168 REPAIR OF DAMAGE TO OUTER SKIN. REPAIRED PER ER/A 418073-14.

Part: VALVE — INOPERATIVE (#1 ENGINE) · airframe 30,219 hrs · 23,527 cycles

IRR- LEFT ENG FUEL HEAT VALVE INOP FLIGHT DIVERTED TO JAX UNABLE TO CONTINUE TO ORIGINAL DESTINATION. CORR.ACT.- REPLACED VALVE PER M/M ALTERNATE PART NBR USED 320115

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 29,753 hrs · 23,209 cycles

FLASHLIGHT AT AFT DOOR NOT BLINKING. REPLACED BATTERIES IN EMERGENCY FLASHLIGHT.

Part: LIMITER — DAMAGED (BRAKE SYSTEM) · airframe 24,843 hrs · 19,547 cycles

BRAKE HYD LIMITER HAD BROKEN AT FUSE LEVER INDICATOR. REPLACED LIMITER.

Part: BOTTLE — DISCHARGED (TAIL CONE SLIDE) · airframe 24,408 hrs · 19,236 cycles

ON SERVICE CHECK FOUND LOW BOTTLE PRESSURE ON TAIL CONE EMERGENCY ESCAPE SLIDE. REPLACED SLIDE.

Part: RHEOSTAT — FAILED (CABIN LIGHTS) · airframe 24,246 hrs · 19,115 cycles

UPON ARRIVAL AT AIRCRAFT IN MGM CABIN HAD RESIDUAL SMOKE AND STRONG ELECTRICAL SMELL NEAR BUS PANEL BEHIND CAPTAINS SEAT. REPLACED UPPER CABIN LIGHT RHEOSTAT.

Part: FRAME — CRACKED (BS 1418)

A CRACK WAS FOUND ON THE STA 1418 FRAME AT L-2R. CRACK IS COVERED IN S/B 53-184. CRACK WAS DUE TO FATIGUE. REPAIRED PER ERA 332255-14.

Part: SKIN — DAMAGED (C-1 DOORWAY)

THE OUTER FUSELAGE SKIN AT THE C-1 CARGO DOOR CUTOUT WAS FOUND DAMAGED AT THE AFT EDGE. THE DAMAGE IS APPROXIMATELY 0.5 X 1.5. DAMAGE WAS CAUSED BY GROUND DAMAGE. REPAIRED PER ERA 272471-14.

Part: JAMB — CORRODED (CARGO DOOR)

THE LOWER JAMB PAN OF THE FWD CARGO DOOR CUTOUT SURROUND STRUCTURE WAS FOUND CORRODED. THE PAN SECTION BETWEEN THE FWD AND AFT CORNERS OF THE DOOR WAS REMOVED AND A NEW SECTION SPLICED IN PER THE MD-88 SRM 53-05, FIG 44 AND PER ER/A 364169-14.

Part: CROSS TIE RELAY — FAILED (E/E COMPT)

RT GEN FAILED INFLT A/C CROSS TIE DID NOT WORK. REPLACED CROSS TIE RELAY, OPS NORMAL.

Part: SWITCH — INOPERATIVE (NLG)

AFTER GEAR RETRACTION AT 10,000 FEET, NOSE UNSAFE RED LIGHT ILLUMINATED. RETURNED TO ATL. REPLACED NOSE GEAR LOCKSWITCH.

Part: SWITCH — INOPERATIVE (NLG)

RED NOSE GEAR UNSAFE LIGHT ON WITH GEAR HANDLE UP, PREFORMED POM PROCEDURES INCLUDING CYCLING GEAR. REPLACED NOSE GEAR INTERLOCK SWITCH, SWUNG NOSE GEAR AND CHECKS OK.

Part: EEL BULB — FAILED (CABIN)

EMER PATH LIGHT INOP AT SEAT 20D AND 24D. RELAMPED, OPS CHECK GOOD.