N970DL

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 74,336 hrs · 55,180 cycles

EMERGENCY LIGHTS INOP AT BACK OF COCKPIT OVD PNL AND ABOVE L1 R1 DOORS. RPLCD EMERG BATTERY PACK ASSY AND BATTERIES FOR OVHD EMERG LIGHTS LOCATED ON FWD CTR ISLE DROP DOWN PNL NO HELP. 772386. RPLCD EMERG LTS BATT PACK B5-23 REF MD88 AMM 33-51 OPERATION NML (LP6404321)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 74,062 hrs · 54,914 cycles

SEAT ROW 21 EMERG LIGHT INOP. RPLCD EMERGENCY LIGHT AT SEAT ROW 21. REF AMM 33-52. CKS GOOD. (LP6406723)

Part: FIRE WARNING — FALSE ACTIVATION (NR 1 ENGINE) · airframe 73,414 hrs · 54,311 cycles

NO 1 ENGINE FREE LOOP B CAME ON AT CRUISE. CHECKLIST COMPLETED FREE LOOP A TEST GOOD. T/S PER MD88 AMM 26-10. INSPECTED, CLEANED, AND SECURED FIRE LOOPS. FOUND INSULATION ON ONE CLAMP INBOARD SIDE OF ENGINE DISPLACED AND NOT SECURED PROPERLY. UNABLE TO DUPLICATE AT THIS TIME OPS CHECK GOOD. (LP5503362)

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,017 hrs · 53,135 cycles

AWR- MTC REQUEST IN REFERENCE LOG 0249740 FUSELAGE - SKIN - STA 1380 - L13R-L14R - CRACK AND EXISTING REPAIR JOB NOR 44 PERFORM ER/A 551385-14 REV.A SECTION II. PERMANENT REPAIR WAS PERFORMED AT FUSELAGE SKIN BETWEEN STA 1380 AND L13R-L14R PER ETI-88-18-069 REV. 2 AND ER/A NO.: 551385-12 REV.: B SECTION II. (LP0800438)

Part: DOUBLER — WORN (TE FLAP) · airframe 72,017 hrs · 53,135 cycles

WEAR ON UPPER DOUBLER OF RT WING OUTBOARD FLAP INBOARD VANE. RT WING OUTBD FLAP INBD VANE WAS REPAIRED PER SRM 57-03D. PAR 11.

Part: FRAME — CRACKED (FUSELAGE) · airframe 72,017 hrs · 53,135 cycles

INITIAL INSPECTION: CRACK ON FRAME STA 1510 AT 4 AND 5 OCLOCK POSITION. FRAME STA 1510 AT 4 AND 5 OCLOCK POSITION WAS REPAIRED PER ETI-88-18-070 REV. 2 AND ER/A: 572579-14 REV. ORIGINAL. (LP0799059)

Part: SKIN — DAMAGED (FUSELAGE) · airframe 72,017 hrs · 53,135 cycles

DAMAGE TO FUSELAGE SKIN BETWEEN FS 370 AND 400 BELOW L-23L. PERMANENT REPAIR WAS PERFORMED AT FS 370- FS 400, BELOW L-23L PER ETI-88-18-071 REV ORIG AND ER-A NR 557644-14 REV A SECTION V.

Part: BEAM — CRACKED (FUSELAGE) · airframe 72,017 hrs · 53,135 cycles

CRACK ON BEAM BELOW TORQUE TUBE STA 1485 AT AFT ACCESSORIES COMPARTMENT. NRC 00275: BEAM BELOW TORQUE TUBE STA 1485 AT AFT ACCESSORIES COMPARTMENT WAS REPLACED AND INSTALLED PER SRM 51-30-1, 51-30-2 AND 51-30-5. (LP #0794790)

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,017 hrs · 53,135 cycles

CRACKED FUSELAGE SKIN STA Y 1309 BTW LONGS 6R-7R (FUS). NRC 00016: AREA WAS REPAIRED PER SRM 53-04-2 FIG. 2 SHEET 15. PERFORM A GENERAL VISUAL INSPECTION OF THE REPAIR INITIAL AT 8,000 CYCLES AND REPETITIVE EVERY 8,000 CYCLES PER SRM 53-04-2 PARAGRAPH 3D. MAINTENANCE ACTIVITIES WILL BE DONE BY LOG 0789029. (LP #0789007)

Part: THRESHOLD — CRACKED (FUSELAGE) · airframe 72,017 hrs · 53,135 cycles

BEND AND CRACK ON THRESHOLD OF L1 ENTRACE. BEND AND CRACK ON THRESHOLD OF L1 WERE REPAIRED PER ER/A 552864-14MA REV. A AND SRM 51-10-2. (LP0787158)

Part: SPLICE — CRACKED (RT WING) · airframe 72,017 hrs · 53,135 cycles

INITIAL INSPECTION: CRACKED SPLICE AND ANGLE STA XRS=164 AT RT WING FRONT SPAR. SPLICE AND ANGLE AT STA XRS=164 ON RT WING FRONT SPAR WERE REPLACED PER PER SRM 51-30-5, ER/A378293-14 REV. ORIG. AND DWG 9937517 REV J. (LP0785943)

Part: DOUBLER — WORN (CARGO DOOR) · airframe 72,017 hrs · 53,135 cycles

INITIAL INSPECTION: WEAR ON LOWER CORNERS DOUBLERS AT FWD CARGO COMPARMENT DOOR. CORNERS DOUBLERS AT FWD CARGO COMPARMENT DOOR WERE REPLACED PER ER/A NR 486624-14MA REV. ORIGINAL. (LP0783466)

Part: APU — FAILED · airframe 71,335 hrs · 52,543 cycles

DURING BOARDING, THE APU HAD AN AUTO SHUTDOWN, AN ODOR BEGAN TO FILL CABIN. PASSENGERS DEPLANED. MAINTENANCE DETERMINED APU HAD AN INTERNAL FAILURE WITH SMOKE COMING OUT OF THE INLET. MAINTENANCE PERFORMED FULL DUCT BURNOUT, REPLACED THE COALESER BAGS AND THE APU WAS DEFERRED AS INOPERATIVE.

Part: COUPLING — LOOSE (HYDRAULIC SYS) · airframe 71,164 hrs · 52,402 cycles

EMERGENCY DECLARED. AIRCRAFT DIVERTED TO TLH DUE TO ODOR NEAR ROW 35. THE ODOR PERSISTED UNTIL ENGINE SHUTDOWN. AN OVERWEIGHT LANDING WAS PERFORMED. MAINTENANCE FOUND THE APU INLET WET WITH HYDRAULIC FLUID AND A HYDRAULIC LEAK IN LEFT WHEEL WELL AT A COUPLING ON THE 2 SPEED VALVE. THE COUPLING WAS SECURED. THE WHEEL WELL AND THE AIRCRAFT BELLY WERE CLEANED. THE APU INLET DOOR ASSEMBLY WAS CLEANED. A MINI DUCT BURN OUT WAS PERFORMED AND AN OVERWEIGHT LANDING INSPECTION WAS COMPLIED WITH. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SKIN — CRACKED (RT MLG DOOR) · airframe 70,317 hrs · 51,733 cycles

RT INBOARD GEAR DOOR SKIN CRACKED. REMOVED AND REPLACED RT MLG INBOARD DOOR REF AMM 32-12. ADJ/ TEST GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 69,988 hrs · 51,491 cycles

RED EMERGENCY LIGHT AT EXIT ROW 24 DE INOP. RELAMPED OP CKS OK. (LP3358413)

Part: PAINT — CRACKED (RUDDER) · airframe 72,017 hrs · 53,135 cycles

ON WALKAROUND FOUND PAIN MISSING AND CRACKED ON UPPER RIGHT SIDE OF RUDDER. PAINT MISSING AND CRACKED ON UPPER RIGHT SIDE OF RUDDER WAS REPAIRED PER ERA-092613-14MA REV A STEPS 1-3.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT) · airframe 67,954 hrs · 49,924 cycles

ROW 16 EMERGENCY LIGHTING INOPERATIVE. CONNECTED THE CONNECTOR IAW ESPM 20, OPS CHECKED NORMAL.

Part: SPAR CAP — DAMAGED (HORIZONTAL STAB) · airframe 72,159 hrs · 53,258 cycles

HORIZONTAL STAB RHS UPPER, AFT SPAR CAP FASTENER HOLE OVERSIZE ER/A 549705-14AD. LEVEL OF ER/A 549705-14AD IS REV. B. LOGPAGE IS OKAY TO TERMINATE. RESULTS OF DTA/DTE HAVE BEEN INCORPORATED. INSPECTION REQUIREMENTS ARE NOW BEING TRACKED VIA 0834658 AND 0834662. (LP2799791)

Part: LIGHT — FAILED (ANTI COLLISION) · airframe 67,524 hrs · 49,620 cycles

BURNING RUBBER ODOR DURING TAKE OFF ROLL TO 2000 FT, NO OTHER INDICATIONS. SMELL SUBSIDED AT 2000' AT 3000', SNAP HEARD AND FOUND CIRCUIT BREAKER L11 UPPER ANTI COLLISION TRIPPED. COMPLIED WITH PNEUMATIC DIST. CABIN SMOKE/ODOR TROUBLESHOOTING IAW W/C 2120-2367 NO FAULT FOUND, R & R UPPER ANTI-COLLISION LIGHT ASSY IAW AMM 33-42 OPS CK NORMAL OK FOR SERVICE.

Part: RELEASE CABLE — FRAYED (TAILCONE) · airframe 67,423 hrs · 49,544 cycles

UPPER LEFT HAND TAILCONE RELEASE CABLE IS FRAYED. REPLACED AND RIGGED TAILCONE RELEASE CABLE PER AMM 53-53-00 AND AMDS 5350-01077-0101.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 67,423 hrs · 49,544 cycles

DURING OPPORTUNITY INSPECTION, BS 1429 SKIN SPLICE. SPLICE DOUBLER CRACKED RBL 10". COMPLIED WITH PRI 551376-14 REV ORIGINAL, AND ER/A 551376-14 REV ORIGINAL.

Part: FRAME — CRACKED (FUSELAGE) · airframe 67,423 hrs · 49,544 cycles

DURING OPPORTUNITY INSPECTION FOUND FRAME 1418 CRACKED AT LONGERON 1L. REPAIRED PER PRI 551806-14 REV 0 AND COMPLIED WITH ERA 551806-14 REV ORIG.

Part: CABLE — FRAYED (TAILCONE) · airframe 67,423 hrs · 49,544 cycles

TAIL CONE CABLE FRAYED AND DETERIORATED. REPLACED CABLE PER AMM 53-53-00.

Part: SLIDE — CRACKED (L1 DOOR) · airframe 67,423 hrs · 49,544 cycles

L1 DOOR SLIDE BACK BOARD IS CRACKED. REMOVED AND REPLACED L1 DOOR SLIDE IAW AMDS WC 2561-4964.

Part: FRAME — DAMAGED (RT MLG WW) · airframe 67,423 hrs · 49,544 cycles

RT WING MLG WW CUT OUT FWD FRAME HAS A PREVIOUSLY INSTALLED FRAME REPAIR AND IS BULGED OUT AND CRACKED. REMOVED AND REPLACED FRAME IAW DWG 5930584.

Part: BELLCRANK — WORN (ELEVATOR TAB) · airframe 67,423 hrs · 49,544 cycles

EMPENNAGE, LT ELEVATOR GEAR TAB O/B BELL CRANK IS WORN FROM FAIRING CHAFE. REPLACED GEARED TAB PER AMDS 2730-4130 LT.

Part: SKIN — CRACKED (BS 1437) · airframe 67,423 hrs · 49,544 cycles

FUSELAGE SKIN CRACKED AT BS 1437, 5 INCHES OTBD VERTICAL STAB. REPAIRED IAW ERA#551476-14 REV. ORIGINAL.

Part: INTERCOSTAL — OUT OF POSITION (TAILCONE) · airframe 67,423 hrs · 49,544 cycles

TAIL CONE ACTIVATION CABLE SUPPORT INTERCOSTAL IS OUT OF POSITION AT AFT END BS 1510. REPLACED THE INTERCOSTAL IAW DWG 9917701. TREATED AND PRIMED IAW SRM 51-10-03.

Part: JACKSCREW — DAMAGED · airframe 67,423 hrs · 49,544 cycles

JACK SCREW HAS RAISED SHARP STEP WORN IN THREADED AREA. COMPLETED PRI 551391-14AD AND ER/A 551391-14AD. (LP2712179)

Part: TURBINE — DAMAGED (RT ENGINE) · airframe 67,317 hrs · 49,455 cycles

THE CREW PERFORMED AN AIR TURN BACK DUE TO THE RT ENGINE FAILING ON TAKEOFF. TURBINE DAMAGE WAS FOUND. THE ENGINE WAS REPLACED AND THE ACFT WAS RETURNED TO SERVICE.

Part: WIRE — PULLED (EMERGENCY LIGHT) · airframe 66,595 hrs · 48,918 cycles

EMERGENCY LIGHT WIRE PULLED OUT, SEAT 22DE. REPAIRED WIRES. PUSHED PINS BACK IN CONNECTOR. EMERGENCY LIGHTS CHECK GOOD.

Part: CABLE — BROKEN (NLG STEERING) · airframe 65,895 hrs · 48,409 cycles

NOSEWHEEL STEERING BROKE WHILE TURNING INTO GATE. FOUND NOSE STEERING CABLE BROKEN, 873231. REPLACED CABLE 123D AND ADJUSTED IAW AMM 32-51. OP'S CHECK AND TAXI CHECKED GOOD.

Part: HUB — DAMAGED (NR 1 ENGINE) · airframe 65,413 hrs · 48,125 cycles

NR 1 AND NR 2 ENGINE N1'S WENT TO 103 PERCENT FOR 7 SECS. DURING LOW ALTITUDE GO AROUND. REPLACED NR 2 ENGINE HUB IAW SPC 03-7201-9-0016. REPLACED NR 1 ENGINE HUB IAW SPC 03-7201-9-0016.

Part: SKIN — CRACKED (RT WING) · airframe 64,959 hrs · 47,799 cycles

DURING WALK AROUND FOUND A ONE CRACK ON RT WING T/E BETWEEN XRS 531.7 AND XW 536.861. ACCOMPLISHED INSTRUCTIONS IAW ERA 540555-14. PERMANENT REPAIR TO BE ACCOMPLISHED WITHIN 3 CALENDAR DAYS. OK FOR SERVICE.

Part: COVER — DAMAGED (TAILCONE SLIDE) · airframe 64,598 hrs · 47,532 cycles

AFT TAILCONE SLIDE COVER FWD HOLDDOWN STRAP WAS FOUND DAMAGED. MAINTENANCE REPLACED HOLDOWN STRAP.

Part: PIN — PULLED (L1 DOOR SLIDE) · airframe 63,803 hrs · 47,032 cycles

DURING LINE CHECK, MAINTENANCE FOUND THE L1 DOOR SLIDE PINS TO BE OUT OF THE PACK. MAINTENANCE REPLACED THE L1 DOOR SLIDE.

Part: PIN — PULLED (L1 DOOR SLIDE) · airframe 63,154 hrs · 46,577 cycles

MAINTENANCE FOUND L1 DOOR SLIDE PINS PULLED. MAINTENANCE REPLACED L1 SLIDE. RII COMPLIED WITH.

Part: UNKNOWN — ODOR (LAVATORY) · airframe 62,538 hrs · 46,168 cycles

DURING CLIMB, THE AFT RT LAVATORY SMOKE DETECTOR WENT OFF WITH A MILD ODOR AND HAZE. ALSO, HAD ODOR IN COCKPIT AT THE SAME TIME. MAINTENANCE PERFORMED PNEUMATIC SYSTEM DUCT BURNOUT.

Part: APU — FAILED · airframe 62,455 hrs · 46,110 cycles

ACFT DIVERTED DUE TO SMOKE IN CABIN. OIL FOUND BY APU INLET. APU CHANGED. LP 6180296 & 1651860.

Part: CAP — CRACKED (HORIZONTAL STAB) · airframe 62,279 hrs · 45,958 cycles

INTERNAL CRACK WAS FOUND ON INBD LOWER HOLES AT RT HORIZONTAL STABILIZER REAR UPPER CAP. RT HORIZONTAL STABILIZER CAP REPLACED IAW DWG N.-SR09550030, REV C AND SRM 51-30-2, 51-30-5, 51-30-1.

Part: LONGERON — CORRODED (BS 1287-1322) · corrosion level 2 · airframe 62,279 hrs · 45,958 cycles

CORROSION ON LONGERON 23L BETWEEN BS 1287-1322. CORROSION REMOVED IAW SRM 51-10-3, AND FOUND TO BE OUT OF LIMITS IAW SRM 53-01. SECTION OF LONGERON WAS REMOVED IAW SRM 53-02 FIG 18, DRILLED AND TRIMED IAW SRM 53-02, FIG 18, TREATED AND PAINTED IAW SRM 51-10-3, AND INSTALLED IAW SRM 53-02, FIG 18.

Part: FRAME — CRACKED (BS 1510) · airframe 62,279 hrs · 45,958 cycles

SEVERAL CRACKS ON FRAME, BS 1510 ,UPPER AND LOWER SECTION. FRAME REPAIR IAW ER/A 497316-14MA, REV ORIG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,279 hrs · 45,958 cycles

CRACKED EXTERNAL POWER RECEPTACLE CUTOUT FWD EDGE FUSELAGE SKIN. DOUBLER WAS FABRICATED AND INSTALLED IAW DWG 5911400-13, REV .

Part: BARRIER — DAMAGED (CARGO DOOR) · airframe 62,279 hrs · 45,958 cycles

DENTS, SCRATCHES, WEAR AND PUNCTURES ON OTBD FACE PANEL AT AFT DOOR BARRIER. FOUND OUT OF LIMITS. REPAIRED IAW ER/A 094625-14 MA REV "D".

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 62,279 hrs · 45,958 cycles

CORROSION ON COUNTERSINK AREA AT LT WING ACCESS PANEL. CORROSION REMOVED, FOUND OUT OF LIMITS. REPLACED IAW SRM 51-22-2A, CONDITION II.

Part: WEB — CRACKED (BS 190-200) · airframe 62,279 hrs · 45,958 cycles

CRACK FOUND ON WEB BELOW FLOOR SUPPORT, BS 190-200 AND X=08. REPAIRED IAW ER/A 528215-14, REV ORIGINAL AND ETI-88, 14-157, REV 2.

Part: SKIN — CORRODED (BS 1307) · airframe 67,524 hrs · 49,620 cycles

CORROSION AT AFT LAV CUTOUT SKIN AND DOUBLER, BS 1307-38, L19L-23. REPAIRED WITH INTERNAL AND EXTERNAL DOUBLERS.

Part: ANGLE — CORRODED (BS 674-693) · corrosion level 2 · airframe 62,279 hrs · 45,958 cycles

CORROSION ON RT CUSP ANGLE X -57 TO X -60, BS 674 - 693. CUSP ANGLE REPAIRED IAW ER/A 526996-14, REV ORIG.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 62,279 hrs · 45,958 cycles

CRACK IN AFT CARGO DOOR EXTERNAL SKIN AROUND DOOR HANDLE. CRACK WAS WORKED IAW ERA 486446-14MA, FIG 1. FOUND WITHIN LIMITS IAW ERA 486446-14MA. TREATED AND PAINTED IAW SRM 51-10-3, PARA 14 AND 21.

Part: ANGLE — CRACKED (BS 1162) · airframe 62,279 hrs · 45,958 cycles

CRACK ON UPPER ANGLE, LOCATED ON UPPER EDGE OF AFT CARGO DOOR BS 1162, NEAR TO FWD HINGE. DAMAGE SECTION AND PARTS WERE REMOVED IAW SRM 51-30-1, 51-30-2, 51-30-4, SECTION NEW ANGLE AND DOUBLER WERE FABRICATED IAW SRM 52-30-0, 51-70-5, SECTION AND NEW ANGLE AND DOUBLER WERE DRILLER IAW SRM 51-10-4, REPAIR PARTS WERE TREATED AND PAINTED IAW SRM 51-10-3, PAR 21 AND 14. REPAIR PARTS WERE INSTALLED IAW SRM 51-30-2, 51-30-4, BRACKETS, STRAPS AND INNER RETAINERS OF SEAL WERE INSTALLED IAW SRM 51-30-1, 51-30-2.

Part: SUPPORT — CRACKED (CARGO DOOR) · airframe 62,279 hrs · 45,958 cycles

CRACKS FOUND BEYOND STOP DRILL ON REPAIR FOR UPPER SUPPORT OF FWD CARGO COMPARTMENT DOOR BARRIER. DOUBLER REMOVED IAW SRM 51-30-2, CRACKS STOP DRILLED IAW SRM 53-01, FIG 2, HOLES WERE PAINTED AND TREATED IAW SRM 51-10-3, PAR 14 AND 21. REPAIR INSTALLED IAW SRM 53-01, FIG 2.

Part: CHANNEL — BROKEN (CABIN) · airframe 62,279 hrs · 45,958 cycles

BROKEN CHANNEL. CHANNEL REPLACED IAW SRM 51-30-1, SRM 51-10-4, AND DWG 9936639, REV P.

Part: ANGLE — CRACKED (AFT CARGO DOOR) · airframe 62,279 hrs · 45,958 cycles

CRACKED ANGLE AFT CARGO DOOR BARRIER. ANGLE REMOVED AND REPLACED IAW SRM 51-30-2, DWG 5917332, REV J, SRM 51-10-3, PAR 14, AND 21, SRM 51-30-5.

Part: DOUBLER — CRACKED (RT MLG DOOR) · airframe 62,279 hrs · 45,958 cycles

CRACKED DOUBLER, BS 995 UPPER SKIN OTBD SECTION AT RT MLG INBD DOOR. NEW DOUBLER INSTALLED IAW SRM 51-10-4,51-30-2 AND 51-30-5.

Part: TEE FITTING — CRACKED (DOOR FRAME) · airframe 62,279 hrs · 45,958 cycles

CRACK ON AFT TEE FITTING BELOW NR 1 BEAM AT FWD R1 SERVICE DOOR. DAMAGED FITTING REMOVED AND REPLACED IAW SRM 51-30-2 AND 51-30-5, SRM 51-10-4, SRM 51-10-3, PAR 14 AND 21, AND SRM 51-30-1.

Part: BEAM — CRACKED · airframe 62,279 hrs · 45,958 cycles

CRACK RT AFT BEAM CORNER OF STAIRWAY WALKING BRIDGE, CATWALK, A/A, SM, CARD 67, ZONE 60. CRACK WAS STOP DRILL IAW SRM 53-01, FIG 2. DOUBLER WAS FABRICATED IAW SRM 53-01, FIG 2, NEW DOUBLER WAS TREATED AND PAINTED IAW SRM 51-10-3, PAR 14 AND 21, NEW REPAIR PART WAS INSTALLED IAW SRM 52-01, FIG 2.

Part: CARGO TRACK — CORRODED (BS 1003-1322) · corrosion level 2 · airframe 62,279 hrs · 45,958 cycles

CORROSION ON CARGO TRACK BS 1003 - 1322. CARGO TRACK WAS REMOVED AND REPLACED IAW SRM 51-10-3, PAR 14, 21 AND 51-30-1 AND 51-30-5.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 62,279 hrs · 45,958 cycles

CORROSION ON COUNTERSINKS OF RT WING ACCESS PANEL 1470C. HOLES WERE OPENED IAW SRM 51-22-2A, BUSHINGS FABRICATED IAW SRM 51-22-2A. BUSHINGS AND REWORKED AREA WERE TREATED IAW SM 51-10-3, PAR 21, REPAIR BUSHINGS INSTALLED IAW SRM 51-22-2A.

Part: FLOORBEAM — DAMAGED (BS 1322) · airframe 62,279 hrs · 45,958 cycles

ELONGATED HOLES ON FLOORBEAM AT BULKHEAD BS 1322. REPAIRED IAW SRM 51-10-4 AND 51-10-3, PAR 21 AND 14.

Part: BEAM — CRACKED (R1 DOOR) · airframe 62,279 hrs · 45,958 cycles

CRACKS FOUND ON FWD AND AFT SECTION OF FWD R1 SERVICE DOOR BEAM. DAMAGE BEAM WAS REPLACED IAW SRM 51-10-4, 51-30-1, 51-30-5, 51-10-3.

Part: DOUBLER — CORRODED (BS 769) · corrosion level 2 · airframe 62,279 hrs · 45,958 cycles

CORROSION ON REPAIR DOUBLER BELOW RUB STRIPS, BS 769 LONGERON 28R. DOUBLER WAS FOUND INCORRECT IAW SRM 53.04, FIG 57, DOUBLER REMOVED, NEW DOUBLER FABRICATED, TRIMMED & DRILLED, TREATED, PAINTED AND INSTALLED IAW SRM 53.04, FIG 57.

Part: SUPPORT BRACKET — CRACKED (CARGO DOOR) · airframe 62,279 hrs · 45,958 cycles

CRACK FWD AND AFT MID CARGO COMPARTMENT DOOR BARRIER SPAR SUPPORT BRACKET SUPPORTS WERE REMOVED, NEW SUPPORTS WERE DRILLED. NEW SUPPORTS HOLES WERE TREATED AND PAINTED. NEW SUPPORTS WERE INSTALLED IAW SRM 51-30-2, 51-30-1 , 51-10-4 AND 51-10 -3, PAR 21 AND 14.

Part: FLOOR SUPPORT — CORRODED (BS 160-200) · corrosion level 2 · airframe 62,279 hrs · 45,958 cycles

CORROSION ON FLOOR SUPPORT BS 160 - 200 BETWEEN X=54 AND X=60. REMOVED AND REPLACED THE FLOOR SUPPORT IAW 51-30-2,51-30-5, 51-10-4 , 51-14-1, 51-10-3, PAR 21 AND 14, 51-30-2, 51-30-5, AND 51-10-3, PAR 38.

Part: STRUCTURE — CRACKED (VERTICAL STAIR) · airframe 62,279 hrs · 45,958 cycles

CRACKED RT FLAPPER OF VERTICAL STAIRWAY AT AFT ACCESSORY BAY. FLAPPER STOP DRILLED IAW SRM 53-01, FIG 4, DOUBLER AND FILLER FABRICATED IAW SRM 53-01, FIG 4, SRM 51-10-3, PAR 14 / 21, AND INSTALLED IAW SRM 51-30-2.

Part: PAN — CRACKED (L1 DOOR) · airframe 62,279 hrs · 45,958 cycles

CRACK ON FWD EDGE OF PAN BETWEEN BEAMS 5 & 6, AT L1 DOOR. CRACKED DOUBLER REMOVED AND REPLACED IAW SRM 51-30-1, 51-30-2, 51-30-2, SRM 51-30-1 AND 51-10-3, PAR 14.

Part: BULKHEAD — CRACKED · airframe 62,279 hrs · 45,958 cycles

CRACK ON AFT BULKHEAD OF STAIRWAY WALKING BRIDGE. BULKHEAD WAS REMOVED IAW SRM 51-30-2 AND 51-30-4, FABRICATED IAW SRM 53-14-3, TREATED AND PAINTED IAW SRM 51-10-3, PAR 14 AND 21, NEW BULKHEAD INSTALLED IAW SRM 53-01, FIG 2.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 62,279 hrs · 45,958 cycles

CORROSION ON RT WING ACCESS PANEL 1454C. CORROSION WAS REMOVED IAW SRM 51-22-2A, BUSHING FABRICATED IAW SRM 51-22-2A, TREATED IAW SRM 51-10-3, PAR 21, AND INSTALLED IAW SRM 51-22-2A, CONDITION II.

Part: CUSP WEB — CORRODED (BS 789-903) · corrosion level 2 · airframe 62,279 hrs · 45,958 cycles

CORROSION ON RT CUSP WEB BS Y 789--903 X -56 TO X -60. CUSP WEB REPAIRED IAW SRM 53-05, FIG 131A-3, FIG 131A-13 AND FIG 131A-14.

Part: CARGO TRACK — CORRODED (BS 1212-1322) · corrosion level 2 · airframe 62,279 hrs · 45,958 cycles

CORROSION ON RT CARGO TRACK, BS 1212 - 1322. CORROSION REMOVED, AND FOUND OUT OF LIMITS. CARGO TRACK REMOVED AND REPLACED IAW SRM 51-10-3, PAR 26, 14, 21 51-30-1.

Part: BULKHEAD — CRACKED · airframe 62,279 hrs · 45,958 cycles

CRACKED RT LOWER FWD BULKHEAD CORNER OF STAIRWAY WALKING BRIDGE. CRACK STOP DRILLED IAW SRM 53-01, FIG 2, DOUBLER WAS FABRICATED IAW SRM 53-01, FIG 2 PART WAS TREATED AND PAINTED IAW SRM 51-10-3, PAR 14/21. REPAIR PART WAS INSTALLED IAW SRM 53-01, FIG 2.

Part: SKIN — CRACKED (LT WING) · airframe 62,279 hrs · 45,958 cycles

CRACK ON INTERNAL SKIN OF LT WING MID BUTTE DOOR MID SECTION. REPAIRED IAW ER/A 466345-14MA, REV "B", LP 1588966.

Part: DOOR FRAME — CORRODED (BS 1157-1210) · corrosion level 2 · airframe 62,279 hrs · 45,958 cycles

CORROSION ON AFT CARGO BAY LOWER DOOR FRAME BEAM REPAIR DOUBLER BS 1157 - 1210. REPAIR DOUBLER REPLACED IAW SRM 53-05, FIG 123.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 62,279 hrs · 45,958 cycles

CRACK FOUND ON FWD CARGO DOOR OUTER SKIN AROUND DOOR HANDLE. , DAMAGE REMOVED IAW ER/A 486446-14MA, REV ORIGINAL AND AREA WAS TREATED AND PAINTED IAW SRM 51-10-3, PAR 21 AND 14.

Part: BEAM — CRACKED (L1 DOOR) · airframe 62,279 hrs · 45,958 cycles

CRACKED BEAM AFT EDGE AT MAIN ENTRANCE L1 DOOR. CRACK REMOVED IAW SRM 51-30-1, DOUBLER FABRICATED IAW SRM 52-05D, FIG 81, AND WAS INSTALLED IAW SRM 51-30-1.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 62,279 hrs · 45,958 cycles

CRACK ON NR 3 STOP FITTING AFT EDGE OF AFT CARGO DOOR. STOP FITTING WAS REMOVED AND REPLACED IAW SRM 51-30-1, 51-30-5, SRM 51-10-4, SRM 51-10-3, AND SRM 51-30-4.

Part: LONGERON — CORRODED (BS 1287-1322) · corrosion level 2 · airframe 62,279 hrs · 45,958 cycles

CORROSION ON LONGERON 23L BETWEEN BS 1287-1322. LONGERON REPAIRED IAW SRM 53-02, FIG 18.

Part: ANGLE — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 62,279 hrs · 45,958 cycles

CORROSION ON MID CARGO DOOR LOWER EDGE ANGLE BETWEEN BS 1165 - 1200 INNER STRUCTURE. LOWER WEDGE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-30-2, SRM 52-33-0, SRM 51-10-3, PAR 14, 21, SRM 51-30-2, AND SRM 51-10-3, PAR 8.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 62,279 hrs · 45,958 cycles

CRACK ON MID CARGO DOOR STOP FITTING NR 2 AND 3 AT BS 693. STOP FITTINGS WERE REMOVED IAW SRM 51-30-1,51-30-5. NEW FITTING WERE DRILLED IAW SRM 51-10-4 NEW DRILLED FITTING WERE TREATED AND PAINTED IAW SRM 51-10-3, PAR 14 AND 21 STOP FITTINGS WERE INSTALLED IAW SRM 51-30-1, 51-30-5.

Part: DOOR FRAME — CORRODED (BS 643-688) · corrosion level 2 · airframe 62,279 hrs · 45,958 cycles

CORROSION ON MID CARGO BAY DOOR FRAME LOWER BEAM REPAIR DOUBLER BS 643-688. NEW DOUBLER INSTALLED IAW SRM 51-30-5, 53-05, FIG 23, 51-10-3, PARA G 14, 21 AND 38.

Part: BRACKET — CRACKED (CARGO DOOR) · airframe 62,279 hrs · 45,958 cycles

CRACKS FWD AND AFT SPAR BRACKETS OF FWD CARGO DOOR BARRIER. , DAMAGE BRACKETS WERE REMOVED AND REPLACED IAW SRM 51-30-2, 51-10-4 AND 51-10-3, PARAGRAPH 14 AND 21.

Part: BEAM — CRACKED · airframe 62,279 hrs · 45,958 cycles

CRACK BEYOND PREVIOUSLY STOP DRILL AT LT FWD BEAM CORNER OF STAIRWAY WALKING BRIDGE, CAT WALK. CRACK WAS STOP DRILLED IAW SRM 53-01, FIG 2, DOUBLER WAS FABRICATED IAW SRM 53-01, FIG 2. DOUBLER WAS TREATED AND PAINTED IAW SRM 51-10-3, PAR 14 AND 21; DOUBLER WAS INSTALLED IAW SRM 51-30-2.

Part: PAN — CRACKED (EMERGENCY EXIT) · airframe 62,279 hrs · 45,958 cycles

CRACKED PAN ON FWD UPPER CORNER OF RT FWD EMERGENCY EXIT DOOR, SM, CARD 9, ZONE 201. DAMAGE WAS REPAIRED IAW SRM 52-05D, FIG -51, 51-30-1, 51-30-2 , 51-01, PARA 21 AND 14 PS 900-5-1 N. 04.

Part: CHANNEL — CRACKED (LT MLG DOOR) · airframe 62,279 hrs · 45,958 cycles

CRACKED CHANNEL BS 955, UPPER OTBD SECTION AT LT MLG INBD DOOR. REPAIR ANGLES REMOVED AND REPLACED IAW SRM 51-30-2, AND ER/A 486334-14 MA, REV.

Part: SKIN — CRACKED (PAX DOOR) · airframe 62,279 hrs · 45,958 cycles

CRACKED OUTER SKIN AT CUTOUT OF MAIN PAX DOOR HANDLE. REPAIRED IAW ER/A NR 501106-14MA, REV ORIGINAL.

Part: FRAME — CRACKED (BS 1380) · airframe 62,279 hrs · 45,958 cycles

CRACK ON FRAME ANGLE BS 1380, BETWEEN LONGERONS 15 - 16R. PNEUMATIC DUCT AND VALVE FLOW CONTROL WERE REMOVED EXHAUST DUCT APU WAS REMOVED. FRAME ANGLE WAS REMOVED, FABRICATED, TREATED, PAINTED, AND INSTALLED IAW AMM AND SRM 36-00-00-201, 49-80-01, 51-30-2, 51-30-05, 51-10-2 DWG 9912246, REV C4 AND 51-10-3, PAR 14, 21.

Part: SPAR — WORN (CARGO DOOR) · airframe 62,279 hrs · 45,958 cycles

FWD AND AFT SPARS OF FWD CARGO DOOR BARRIER IS WORN. DAMAGE SPARS WERE REMOVED AND REPLACED IAW SRM 51-30-1, 51-10-4, 51-30-2 AND 51-10-3 PARA 14 AND 21.

Part: FRAME — CORRODED (BS 1322) · corrosion level 2 · airframe 62,279 hrs · 45,958 cycles

CORROSION ON FRAME, STA Y=1322 BETWEEN LONGERON 25LT -30. MRB 53-139-05, SM, ZONE 57/ CARD 4. FASTENERS AND CORROSION WAS REMOVED, AREA OUT LIMITS WAS CUT OUT, REPAIR PARTS WAS FABRICATED, ADJUSTED AND RILLED REPAIR PARTS WAS INSTALLED, REPAIR WAS IDENTIFIED, CIC WAS APPLIED IAW SRM 51-30-2, 51-30-5, 51-10-3, PAR 21, 14, 26, 38 PS 900-5-1 NR 04-53-03D, FIG 2A.

Part: INTERCOSTAL — CORRODED (BS 1309-1322) · corrosion level 2 · airframe 62,279 hrs · 45,958 cycles

CORROSION ON INTERCOSTAL BETWEEN LONGERON 27- 28L AND BS 1309-1322. INTERCOSTAL REMOVED AND REPLACED IAW SRM 51-30-2, AND 51-30-5.

Part: FRAME — CORRODED (BS 1309) · corrosion level 2 · airframe 62,279 hrs · 45,958 cycles

CORROSION ON REPAIR ON FRAME BS 1309 AND LONGERON 26R. ANGLE WAS REMOVED IAW SRM 51-30-5, NEW ANGLE WAS ADJUSTED, DRILLED, TREATED, PAINTED AND INSTALLED IAW SRM 51-10-3, PAR 14, 21 AND 53-03D, FIG. 2-A.

Part: FITTING — CRACKED (BS 864-886) · airframe 62,279 hrs · 45,958 cycles

CRACKED FITTING OF FILLET SUPPORT PANELS BS 864-886 AND BL 0. REMOVED, DRILLED AND INSTALLED NEW FITTINGS IAW SRM 51-30-5, 51-30-2 AND 51-10-4.

Part: FRAME — CORRODED (BS 1309) · corrosion level 2 · airframe 62,279 hrs · 45,958 cycles

CORROSION ON FRAME BS 1309, FROM LONGERONS 23-30L. FRAME SECTION REMOVED IAW SRM 53-03, FIG 2-A. NEW FRAME SECTION WAS ADJUSTED, DRILLED, TREATED, PAINTED AND INSTALLED IAW SRM 51-10-3, PAR 14, 21 AND 53-030 FIG 2-A.

Part: PAN — CRACKED (SERVICE DOOR) · airframe 62,279 hrs · 45,958 cycles

CRACK FOUND IN FWD SERVICE DOOR PAN, APPROXIMATELY BS 172 BETWEEN BEAMS 3 AND 4 BEHIND LOWER DOOR HINGE SECTION R1. RETAINER WAS REMOVED, DOUBLER AND SHIM FABRICATED, TREATED, PAINTED AND INSTALLED RETAINERS AND BEAM WERE INSTALLED IAW SRM 51-30-4, FIG 3 AND 7, 51-10-3, PAR 14 AND 21.

Part: SUPPORT — CRACKED (BS 1497) · airframe 62,279 hrs · 45,958 cycles

CRACKED SUPPORT BETWEEN STA Y=1485, CANT Y=1497, CANT APPROX 7 HRS POSITION. SM, ZONE 100 / CARD 152. DAMAGE WAS REMOVED IAW SRM 53-01, FIG 2, SHEET 4, NEW REPAIR FASTENER FABRICATED IAW SRM 53-01, FIG 2, SHEET 4, NEW REPAIR PARTS WERE TREATED AND PAINTED IAW SRM 51-10-3, PAR 14 AND 21 NEW REPAIR PARTS WERE INSTALLED IAW SRM 51-30-2 AND 51-30-5.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 62,279 hrs · 45,958 cycles

CORROSION ON COUNTERSINK AREA AT RT MAIN FUEL TANK ACCESS PLATE NR 1462C AND 1464C MRB 57-083-02,AYP, CARD 107, ZONE 10, FUEL. CORROSION ON COUNTERSINK OF ACCESS PLATE NR 1462C WAS REMOVED IAW SRM 51-22-2A, COUNTERSINK WERE MEASURED AND MAXIMUM DIAMETER ALLOWABLE IS 0.532" AND WERE FOUND 3 COUNTERSINK ADJACENTS OUT OF LIMITS, MEASURED 0.540", 0.550" AND 0.540" ON ACCESS PLATE NR 1462C. THEREFORE ACCESS PLATE WAS REPLACED IAW SRM 51-22-2A CONDITION II.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 62,279 hrs · 45,958 cycles

CORROSION ON SETTLEMENT AREA AND COUNTERSINK AT LT MAIN FUEL TANK ACCESS PLATE 1357C, 1355C, MRB 57-083-02, AYP, CARD 102, ZONE 10. FUEL, CORROSION ON COUNTERSINKS OF ACCESS PLATE NR 1355C WAS REMOVED IAW SRM 5122-2A, COUNTERSINKS WERE MEASURED AND MAXIMUM DIAMETER ALLOWABLE IS 0.532" AND WERE FOUND 3 COUNTERSINK ADJACENTS OUT OF LIMITS, MEASURED: 0.596", 0.597" AND 0.585" ON ACCESS PLATE NR 1355C THEREFORE ACCESS PLATE WAS REPLACED IAW SRM 51-22-2A, CONDITION II. CORROSION ON COUNTERSINKS OF ACCESS PLATE NR 1357C WAS REMOVED IAW SRM 51-22-2A COUNTERSINKS WERE MEASURED AND MAXIMUM DIAMETER ALLOWABLE IS 0.532" AND WERE FOUND 3 COUNTERSINKS ADJACENTS DUT OF LIMITS, MEASURED: 0.578", 0.563" AND 0.565" ON ACCESS PLATE NR 1357C THEREFORE ACCESS PLATE WAS REPLACED IAW SRM 51-22-2A CONDITION II.

Part: CUSP WEB — CORRODED (BS 619-710) · corrosion level 2 · airframe 62,279 hrs · 45,958 cycles

CORROSION ON RT CUSP WEB X=-56 TO X=-58 STA Y= 619 TO 675, 675 TO 710 AT FLOOR STRUCTURE MRB 53-037-01. SM, CARD 131, ZONE 201, FOR EXCESIVE DAMAGE ON CUSP WEB; THIS WAS REPLACED. DAMAGE CUSP WEB WAS REMOVED, WITH FITTINGS, STRAPS AND DUCTS, NEW CUSP WEB WAS DRILLED, NEW HOLES WERE TREATED AND PAINTED, NEW CUSP WEB, FITTINGS, STRAPS AND DUCTS WERE INSTALLED IAW SRM 51-30-2, 51-30-5, SRM 51-10-3 PAR 14, 21 AND 38 AND DWG 9930538, REV BF.

Part: CUSP WEB — CORRODED (BS 1155-1174) · corrosion level 2 · airframe 62,303 hrs · 45,980 cycles

CORROSION ON RT CUSP WEB BETWEEN BS 1155 - 1174 AND X -55 - X -60. DAMAGE ON CUSP WEB REMOVED, DOUBLER AND FILLER WERE FABRICATED, TREATED AND PAINTED IAW SRM 51-30-2 AND 53-05, FIG 131A-8.

Part: SUPPORT ANGLE — CRACKED (LT WING) · airframe 62,279 hrs · 45,958 cycles

CRACK ON FWD INBD SUPPORT ANGLE OF LT VORTILON INTERNAL SUPPORT STRUCTURE LOCATED ON LT WING LOWER SECTION, LOWER. FASTENERS AND FORMER WERE REMOVED, DOUBLERS WERE FABRICATED, WERE TREATED AND PAINTED, WERE INSTALLED AND FORMER PREVIOUSLY REMOVED WAS INSTALLED IAW SRM 57-01 FIG 3 5H3 51-30-2, 51-30-5 AND 51-10-3 PAR 21/14.

Part: FLOOR SUPPORT — CORRODED (BS 1155-1212) · corrosion level 2 · airframe 62,279 hrs · 45,958 cycles

CORROSION ON FLOOR SUPPORT BS 1155-1212. FLOOR SUPPORT REPLACED IAW SRM 51-10-3 P 14, 21, 51-30-2, 51-30-5, & 51-10-4.

Part: CUSP WEB — CORRODED (BS 618-625) · corrosion level 2 · airframe 62,279 hrs · 45,958 cycles

CORROSION ON LT CUSP WEB REPAIR DOUBLER X=54 TO X=60 BETWEEN BS 618-625. CUSP WEB WAS REPLACED IAW SRM 51-30-2, 51-30-1, 51-30-5, 51-10-3 AND DWG 9930538, REV BF.

Part: BEAM — CRACKED (L1 DOOR) · airframe 62,279 hrs · 45,958 cycles

CRACKED BEAM FWD EDGE OF L1 DOOR. FITTINGS AND STOPS WERE REMOVED IAW SRM 51-30-1. CRACK WAS STOP DRILLED IAW SRM 52-05, FIG 58, SHEET 3. NEW DOUBLER WAS FABRICATED IAW SRM 52-05, FIG 58, SHEET 3, NEW DOUBLER AND AREA WERE TREATED AND PAINTED IAW SRM 51-30-1, 51-30-2 AND 51-30-5.

Part: CUSP WEB — CRACKED (BS 219-227) · airframe 62,279 hrs · 45,958 cycles

CRACKED ON RT CUSP WEB X-57 BS 219 -227. CUSP WEB REMOVED AND REPLACED IAW SRM 51-30-1, 51-30-2, 51-30-5, 51-10-4 AND 51-10-3.

Part: FLOOR SUPPORT — CORRODED (BS 1155) · corrosion level 2 · airframe 62,279 hrs · 45,958 cycles

CORROSION ON FLOOR SUPPORT BS 1155. FLOOR SUPPORT WAS REPLACED IAW SRM 51-30-5, 51-10-3 P 14 - 21, & 51-10-4.

Part: CUSP WEB — CORRODED (BS 543-549) · corrosion level 2 · airframe 62,279 hrs · 45,958 cycles

CORROSION ON LT CUSP WEB REPAIR DOUBLER AND RING DOUBLER X= 54 TO X=60 BETWEEN BS 543 - 549. REPAIR REMOVED IAW SRM 51-30-5 . NEW PARTS FABRICATED AND AJUSTED IAW SRM 53-05, FIG 131A. TREATED AND PAINTED IAW SRM 51-10-3, PAR 21 AND 14.

Part: RIB — CORRODED (RT WING SLAT) · corrosion level 2 · airframe 62,279 hrs · 45,958 cycles

OTBD AND INBD RIBS OF SLAT PANEL IN RT WING CORRODED. DAMAGE REMOVED AND REPAIRED. BUSHINGS FABRICATED AND INSTALLED IAW SRM 57-02, PAR 9.

Part: FLOOR SUPPORT — CORRODED (BS 1309-1347) · corrosion level 2 · airframe 62,279 hrs · 45,958 cycles

CORROSION ON FLOOR SUPPORT X=17, BS 1309 - 1347. SUPPORT FOUND OUT LIMITS AND WAS REPLACED IAW SRM 51- 30-1, 51-10-3 PAR 14, 21, 38.

Part: CVR — CORRODED (BS 1097-1117) · corrosion level 2 · airframe 62,303 hrs · 45,980 cycles

CORROSION ON RT CUSP WEB X -55 - X -60 BS 1097 - 1117. CORROSION WAS REMOVED AND AREA OUT OF LIMITS. REPAIRED IAW SRM 53-05, FIG 131A-7, 51-10-3, PAR 26 AND ER/A 511165-14, MA REV B.

Part: FILLET — CORRODED (BS 1079-1139) · airframe 62,279 hrs · 45,958 cycles

CORROSION ON SETTLEMENT AREA OF FILLET BETWEEN LONGERONS 26 - 30L BS 1079 - 1139. CORROSION REMOVED, TREATED AND PAINTED IAW SRM 51-10-3 AND 53-04, PAR 57.

Part: PANEL — CORRODED (BS 1079-1136) · airframe 62,279 hrs · 45,958 cycles

CORROSION ON SETTLEMENT AREA OF FILLET PANELS BETWEEN LONGERONS 26 - 30R BS 1079 - 1136. CORROSION WAS REMOVED. AREAS TREATED AND PAINTED IAW SRM 53-04, PAR 57.

Part: PANEL — CORRODED (BS 984-1136) · airframe 62,279 hrs · 45,958 cycles

CORROSION ON SETTLEMENT AREA OF FILLET PANELS BETWEEN LONGERON 18 - 26L BS 984 - 1136. CORROSION REMOVED IAW SRM 53-04.

Part: PANEL — CORRODED (BS 940-1136) · airframe 62,279 hrs · 45,958 cycles

CORROSION ON SETTLEMENT AREA OF FILLET PANEL BETWEEN LONGERONS 18 - 26R AT BS 940 - 1136. CORROSION REMOVED AND AREAS WERE TREATED AND PAINTED IAW SRM 53-04, P57.

Part: SKIN — CORRODED (BS 720-820) · airframe 62,279 hrs · 45,958 cycles

CORROSION ON FUSELAGE SKIN BELOW RUB STRIPS BS 720 - 820 LONGERON 25-30R. CORROSION REMOVED AND AREAS REWORKED. TREATED AND PAINTED IAW SRM 51-10-3 AND 53-04, PAR 57.

Part: SKIN — CORRODED (BS 720-755) · airframe 62,279 hrs · 45,958 cycles

CORROSION ON FUSELAGE SKIN BELOW RUB STRIPS BS 720 - 755 BETWEEN LONGERONS 25 - 30L AT CENTER FUSELAGE. CORROSION REMOVED AND FOUND WITHIN LIMITS IAW SRM 53-04, PAR 57 AND 51-10-3.

Part: FLOOR SUPPORT — CORRODED (BS 160-218) · corrosion level 2 · airframe 62,279 hrs · 45,958 cycles

CORROSION ON FLOOR SUPORT BS 160-218. FLOOR SUPPORT REPLACED IAW SRM 51-10-11 ND DWG 9936534, REV BW.

Part: SIGN — DIM (CABIN) · airframe 62,279 hrs · 45,958 cycles

LOW BRIGHTNESS ON, TWO SELF ILLUMINATED EXIT SIGNS. SIGNS REPLACED IAW AMM 11-00-01 AND 25-00-00.

Part: BULKHEAD WEB — CORRODED (BS 1333) · corrosion level 2 · airframe 62,303 hrs · 45,980 cycles

CORROSION ON BULKHEAD WEB S 1333 BETWEEN LONGERON 26L - 26R. BULKHEAD WEB WAS REPLACED WITH FABRICATED PARTS. TREATED, PAINTED, AND INSTALLED IAW SRM 51-30-2 AND 51-30-5.

Part: SKIN — WORN (LT WING) · airframe 62,279 hrs · 45,958 cycles

WEAR ON LOWER SKIN BETWEEN STA XCW= 58 AND XCW= 62 AND STA Y=973 APROX AT LT WING FASTENERS WERE REMOVED IAW SRM 51-30-2 AND 51- 30-1, DAMAGE WAS REMOVED IAW SRM 51-70-4, FIG 1, SHEET 2. DOUBLER AND SKIN WERE FABRICATED IAW SRM 51-70-4, FIG 1, SHEET 2. PARTS WERE TREATED AND PAINTED IAW SRM 51-10-3 PAR 21 AND 14. DOUBLER AND SKIN WERE INSTALLED IAW SRM 51-30-2 AND 51-30-1, AND DWG 5936844, REV CN.

Part: INTERCOSTAL — CRACKED (BS 1338-1341) · airframe 62,279 hrs · 45,958 cycles

CRACKED INTERCOSTAL BS 1338-1341 BETWEEN LONGERONS 3-4R. INSTERCOSTAL REPAIRED IAW SRM 51-30-2, SRM 53-01, FIG 2, SRM 53-01, FIG 2, SRM 51-10-3, PAR 14- 21, SRM 51-30-2, SRM 51-30-2 AND 51-30-5.

Part: ANGLE — CRACKED (BS 1940) · airframe 62,279 hrs · 45,958 cycles

CRACK ON ANGLE AT OUTBOARD CHANNEL BS 1940 AND XCW= 39 LT WHEEL WELL. ANGLE REPLACED IAW DWG 5930584, REV BY, SRM 51-30-2, & 51-30-5.

Part: LONGERON — CORRODED (BS 1334) · corrosion level 2 · airframe 62,303 hrs · 45,980 cycles

CORROSION ON LONGERON 29R BS 1334. LONGERON R & R IAW SRM 51-10-4 AND 51-30-5.

Part: SKIN — DAMAGED (RUDDER) · airframe 62,279 hrs · 45,958 cycles

DAMAGED PAINT AND METALIZED ON LT/RT FACE OF RUDDER SKIN, VHS, SM. LT/RT FACE OF RUDDER SKIN WERE PAINTED AND REPAIRED IAW SRM 51-70-1A.

Part: SEAT TRACK — CORRODED (BS 406-409) · corrosion level 2 · airframe 62,279 hrs · 45,958 cycles

CORROSION ON LT SEAT TRACK X=54 BETWEEN BS 406-409. REMOVED AND REPLACED IAW SRM 53-05, FIG 4A AND 51-10-3.

Part: FLOORBEAM — CORRODED (BS 1212) · corrosion level 2 · airframe 62,279 hrs · 45,958 cycles

CORROSION ON FLOORBEAM BS 1212. FLOORBEAM REPLACED IAW SRM 51-30-2, 51-10-3, & 51-10-4.

Part: CUSP WEB — CORRODED (BS 583-585) · corrosion level 2 · airframe 62,279 hrs · 45,958 cycles

CORROSION ON LT CUSP WEB X=54 TO X= 60 BETWEEN BS 583-585. REPAIRED IAW SRM 53-05 FIG 131A-13 AND 51-30-2 AND 51-10-3.

Part: SKIN — CORRODED (BS 218-227) · corrosion level 2 · airframe 62,279 hrs · 45,958 cycles

CORROSION ON REPAIR DOUBLER BETWEEN BS 218-227, LONGERONS 29L - 29R IN FWD CARGO BAY. REPAIR DOUBLER REMOVED AND REPLACED IAW SRM 53-04-2, 51-10-3 AND 51-30-2.

Part: PAN — CRACKED (BS 674-826) · airframe 62,279 hrs · 45,958 cycles

CRACKED FWD UPPER CORNER ON WINDOW RING PAN BETWEEN BS 674-826. REPAIRED IAW SRM 53-05, FIG 122, 51-10 -3, 51-30-2, 51-30-5, ER/A 493648-14 MA REV ORIG AND ER/A 487747-14, MA REV ORIG.

Part: FLOOR SUPPORT — CORRODED (BS 1309-1347) · corrosion level 2 · airframe 62,279 hrs · 45,958 cycles

CORROSION ON FLOOR SUPPORT X-17 BETWEEN BS 1309 - 1347. FLOOR SUPPORT FOUND TO BE OUT OF LIMITS. REPLACED IAW SRM 51-30-1 AND ER/A 511165-14 MA REV B, SRM 51-10-3 PAR 21/14, 51-30-1, 51-10-4 AND SRM 51-10-3, PAR 38.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 62,279 hrs · 45,958 cycles

CORROSION ON SETTLEMENT AREA OF RT MAIN FUEL TANK ACCESS PANEL 1409C. ACCESS PANEL REPLACED IAW SRM 51-22-2A, CONDITION III.

Part: FLOOR SUPPORT — CORRODED (BS 150-200) · corrosion level 2 · airframe 62,279 hrs · 45,958 cycles

CORROSION ON FLOOR SUPPORT BS 150-200 X=-8. FLOOR SUPPORT REMOVED AND REPLACED IAW SRM 51-30-1, 51-10-4, 51-10-3, PAR 21 AND 14 51-20-0.

Part: LONGERON — CRACKED (BS 1437) · airframe 62,279 hrs · 45,958 cycles

CRACK ON LONGERON 16L BS 1437 AT AFT ACCESSORIES COMPARTMENT. LONGERON REMOVED AND REPLACED IAW SRM 51-30-2, 51-30-5, 51-10-4, 51-10-3, PAR 14 AND 21.

Part: RIB — CRACKED (LT WING) · airframe 62,279 hrs · 45,958 cycles

CRACK ON LT WING FIXED L/E RIB XOS=448. RIB REMOVED AND REPLACED IAW SRM 51-30-2, 51-30-5, 51-10-4, 51-10-3 PAR 14 AND 21.

Part: ANGLE — CRACKED (LWS 448) · airframe 62,279 hrs · 45,958 cycles

CRACKED RIB ANGLE ON LT WING L/E RIB XOS 448. DAMAGED ANGLE REMOVED AND REPLACED IAW SRM 51-30-2, DWG 9919329, ITEM 15, REV T AND SRM 51-30-2, 51-10-3 PAR 14, 21.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 62,279 hrs · 45,958 cycles

CORROSION ON LT WING FUEL TANK ACCESS PANEL. CORROSION REMOVED AND FOUND WITHIN LIMITS, TREATED IAW SRM 51-22-2A.

Part: ANGLE — CRACKED (VERTICAL STAB) · airframe 62,279 hrs · 45,958 cycles

CRACKED ANGLE ON END OF REAR SPAR AT VERTICAL STABILIZER RT SIDE (VHS). ANGLE REMOVED IAW SRM 51-30-5, NEW ANGLE FABRICATED IAW DWG 9911834, REV. ANGLE TREATED AND PAINTED IAW SRM 51-10-3, PAR 14 AND 21, AND INSTALLED IAW SRM 51-30-5.

Part: STIFFENER — CRACKED (BS 1338) · airframe 62,279 hrs · 45,958 cycles

CRACK ON STIFFENER BS 1338 LONGERONS 7 - 8R. STIFFENER REMOVED, NEW STIFFENER DRILLED, TREATED, PAINTED, AND INSTALLED IAW SRM 51-10-3, PAR 21114, 51-10-4, 51-30-1, 51-30-2, 51-30-5.

Part: RECEPTACLE — CRACKED (EXTERNAL POWER) · airframe 62,279 hrs · 45,958 cycles

CRACKED EXTERNAL POWER RECEPTACLE. RECEPTACLE WAS FABRICATED IAW DWG 5957232, REV CM.

Part: FRAME SPLICE — CORRODED (BULKHEAD) · corrosion level 2 · airframe 62,279 hrs · 45,958 cycles

CORROSION ON AFT PRESSURE BULKHEAD LOWER FRAME SPLICE LOCATED BETWEEN LONGERONS 26 - 27R. FRAME SPLICE WAS REMOVED IAW SRM 51-30-5, SRM 53-03 FIG 37, SRM 51-10-3, PAR 14 - 21, AND SRM 51-30-5.

Part: LONGERON — CRACKED (BS 1437) · airframe 62,279 hrs · 45,958 cycles

CRACK ON LONGERON 12L, BS 1437. REMOVED AND REPLACED THE LONGERON AND SPLICE IAW SRM 51-30-2, 51-30-5, 53-02 PAR 12, 51-10-4, 51-10-3 PAR 14 AND 21.

Part: ANGLE — CRACKED (BS 101-110) · airframe 62,279 hrs · 45,958 cycles

CRACK ON ANGLE BETWEEN BS 101 - 110 X=44. ANGLE REMOVED AND REPLACED IAW SRM 51-30-2, 51-30-5, DWG 9957820-85, REV GR.

Part: SLIDE — UNLACED (L1 DOOR) · airframe 61,858 hrs · 45,658 cycles

DURING LINE CHECK, MAINTENANCE FOUND THE L1 DOOR EVACUATION SLIDE PACK UNLACED. MAINTENANCE REMOVED AND REPLACED THE SLIDE.

Part: FASTENER — DAMAGED · airframe 66,202 hrs · 48,626 cycles

FOUND DAMAGE APPROXIMATELY 2 FT BELOW NR 6 WINDOW LT SIDE IAW SRM 53-04-1, PARAGRAPH 6, DAMAGE CLASSIFIED CONDITION 1 FASTENER DAMAGED. REPLACED FASTENER IAW SRM 53-04-2.

Part: FASTENER — DAMAGED · airframe 66,202 hrs · 48,626 cycles

INSPECTION FOUND DAMAGE IN REPAIR LOWER AFT CORNER LT SIDE OF L1 DOOR IAW SRM 53-04-1 PARAGRAGH 6, ONE FASTENER DAMAGED. REPLACED FASTENER IAW SRM 53-04-2.

Part: FASTENER — DAMAGED · airframe 66,202 hrs · 48,626 cycles

INSPECTION FOUND DAMAGE APPROXIMATELY 3 FT BELOW NR 2 WINDOW LT SIDE IAW SRM 53-04-1 PARAGRAPH 6, ONE FASTENER DAMAGE. REPLACED FASTENER IAW SRM 53-04-2.

Part: FASTENER — DAMAGED · airframe 66,202 hrs · 48,626 cycles

INSPECTION FOUND DAMAGE APPROXIMATELY 2 FT BELOW NR 7 WINDOW IAW SRM 53-04-1 PARAGRAPH 6. ONE FASTENER DAMAGE. REPLACED FASTENER IAW SRM 53-04-2.

Part: FASTENER — DAMAGED · airframe 66,202 hrs · 48,626 cycles

INSPECTION FROM DAMAGE APPROXIMATELY 3 FT BELOW NR 4 WINDOW LT SIDE IAW SRM 53-04-1 PARA 6. ONE FASTENER DAMAGED. REPLACED FASTENER IAW SRM 53-04-2.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 61,277 hrs · 45,276 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE OVERHEAD EMERGENCY PATHWAY LIGHTING AT ROW 15 AND AFT WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACKS FOR THE NOTED LIGHTED AREAS AND THE OPS CHECK WAS GOOD.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 59,947 hrs · 44,311 cycles

DURING ROUTINE INSPECTION, THE LT AND RT AFT DOOR OVERWING EMERGENCY EXIT LIGHTED SIGNS WERE FOUND TO BE INOPERATIVE. BATTERIES WERE REPLACED FOR THE SUBJECT LIGHTS AND THE SYS THEN CHECKED NORMALLY.

Part: SKIN — CRACKED (BS 1418) · airframe 59,185 hrs · 43,787 cycles

FOUND CRACK IN SKIN AT FIRST FASTENER OTBD OF SKATE ANGLE, BS 1418, LONGERON 2R. REPAIR IAW ER/A 514317-14AD.

Part: SKIN — CRACKED (BS 1418) · airframe 59,185 hrs · 43,787 cycles

1 INCH LONG CRACK IN SKIN, BS 1418 JUST FORWARD OF FASTENER HOLE OF OLD REPAIR DOUBLER. REPAIRED IAW ER/A 514317-14AD.

Part: FRAME — CRACKED (BS 1485) · airframe 59,185 hrs · 43,787 cycles

CANTED FRAME BS 1485 WEB CRACKED NEAR THE 8 0CLOCK POSITION, AT THE INTERIOR CONE RELEASE HANDLE SUPPORT STRUCTURE. REPAIRED IAW ER/A 514296-14.

Part: CLAMP — OUT OF POSITION · airframe 59,185 hrs · 43,787 cycles

DURING SCHEDULED INSPECTION, CABLE CLAMP NR 18 WAS FOUND TO BE LOCATED LESS THAN .5" FROM THE CONDUIT IN THE AFT ACCESSORY COMPARTMENT AT THE FRAME AT 7 O'CLOCK POSITION. ADJUSTED CLAMP CLEARANCE IAW AMM 53-53-00-501 AND AMDS CARD 5350-01077-0101. REQUIRED INSPECTION COMPLETE.

Part: STIFFENER — CRACKED (BS 1418) · airframe 59,185 hrs · 43,787 cycles

FRAME STIFFENER CRACKED BS 1418 AT L2R. REPAIRED IAW ERA 514320-14.

Part: SKIN — CRACKED (BS 1418) · airframe 59,185 hrs · 43,787 cycles

SKIN CRACKED, RADIATING OUT .1250" AT BS 1418, BETWEEN L2-3R. APPLIED REPAIR IAW ER/A 514317-14AD.

Part: RELEASE CABLE — DIRTY (TAILCONE) · airframe 59,185 hrs · 43,787 cycles

DURING SCHEDULED INSPECTION, THE TAILCONE RELEASE CABLES WERE FOUND TO BE GUMMED UP AND DIRTY AT THE CONDUITS ON THE AFT ACCESSORY AREA FRAME AT THE 7 O'CLOCK POSITION. THE CABLES AND CONDUITS WERE CLEANED IAW PS900-1-2-1, NR 01 AND THE REQUIRED INSPECTION WAS COMPLETED.

Part: PIN — WORN (TAILCONE) · airframe 59,185 hrs · 43,787 cycles

DURING SCHEDULED INSPECTION, THE TAILCONE GUIDE RECEPTICLES WERE NOTED TO BE WORN. THE GUIDE PIN RECEPTICLES WERE REPLACED IAW SRM 51-01 AND THE REQUIRED INSPECTION WAS COMPLETED.

Part: RELEASE CABLE — WORN (TAILCONE) · airframe 59,185 hrs · 43,787 cycles

DURING SCHEDUED INSPECTION, THE TAILCONE RELEASE CABLE LOCATED IN THE TAILCONE INTERIOR WAS NOTED TO BE WORN & FRAYED. THE CABLE WAS REPLACED IAW AMM 53-53-00.

Part: PIN — LOOSE (TAILCONE) · airframe 59,185 hrs · 43,787 cycles

DURING SCHEDULED INSPECTION, THE TAILCONE GUIDE PIN WAS DETERMINED TO BE LOOSE AT THE 12 O'CLOCK POSITION. THE GUIDE PIN WAS RESECURED IAW AMM 53-53-00 AND THE REQUIRED INSPECTION WAS COMPLETED.

Part: CONDUIT — LOOSE (TAILCONE RELEASE) · airframe 59,185 hrs · 43,787 cycles

DURING SCHEDULED INSPECTION, THE CABLE CONDUITS FOR THE TAILCONE RELEASE CABLE WERE FOUND TO BE LOOSE ON THE AFT ACCESSORY COMPARTMENT FRAME AT THE 7 O'CLOCK POSITION. RESECURED CABLE CONDUITS WITH NEW CLAMPS IAW AMM 53-53. REQUIRED INSPECTION COMPLETED.

Part: ATTACH BRACKET — CRACKED (TAILCONE) · airframe 58,982 hrs · 43,647 cycles

DURING LIGHTNING STRIKE INSPECTION, FOUND CRACKS IN BOTH UPPER TAILCONE ATTACH BRACKETS. THE TAILCONE WAS REPLACED WITH A SERVICEABLE UNIT IAW WC 5350-4287. TAIL CONE SLIDE WAS REPLACED IAW AMM 25-62.

Part: TAB — DAMAGED (RT ELEVATOR) · airframe 58,982 hrs · 43,647 cycles

DURING SCHEDULED MX, THE RT ELEVATOR ANTI FLOAT TAB WAS FOUND TO HAVE LIGHTNING STRIKE DAMAGE. REPAIRED IAW SRM 55-04.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 58,974 hrs · 43,639 cycles

DURING SERVICE CHECK, THE CEILING EMERGENCY LIGHTS FROM ROW 27 TO 31 WERE FOUND INOPERATIVE. REPLACED BATTERIES AT B5-106 IAW AMM 33-53. BATTERY PACK AND LIGHT OPERATION CHECKED NORMALLY.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 57,100 hrs · 42,353 cycles

DURING LINE CHECK, MAINTENANCE FOUND THE OVERHEAD EMERGENCY ESCAPE LIGHTS AT ROWS 16, 18 AND 20 TO BE INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 56,846 hrs · 42,179 cycles

DURING LINE CHECK, MAINTENANCE FOUND THE COCKPIT EMERGENCY LIGHTS TO BE INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES AND RESECURED THE LOOSE WIRES IN THE BATTERY PACK. THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION AFTER A FUNCTIONAL CHECK OF THE SYSTEM. AIRCRAFT OKAY FOR SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 56,559 hrs · 41,978 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE OVERHEAD EMERGENCY ESCAPE LIGHTING IN ROWS 16-20 OF THE CABIN WERE INOPERATIVE. MAINTENANCE CHARGED THE BATTERY PACK AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 55,876 hrs · 41,517 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING AT ROW 23D/E IN THE CABIN, WERE INOPERATIVE. MAINTENANCE FOUND A CONNECTOR IN THE WIRE HARNESS UNPLUGGED, RECONNECTED IT, AND FUNCTIONALLY CHECKED THE SYSTEM.

Part: BALLAST — BURNED (CABIN LIGHTS) · airframe 53,594 hrs · 39,921 cycles

DURING FLIGHT, THE F/A NOTICED ELECTRICAL SHORTING AND SMOKE EMITTING FROM ROW 25ABC. MX FOUND LIGHT BALLAST AND HARNESS BURNED AT ROW 24AB. BALLAST WAS REPLACED BUT HARNESS WAS NOT IN STOCK AND FWD OVERHEAD LIGHTS ON MCO 33-00-02.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 52,149 hrs · 38,945 cycles

MAINT FOUND MULTIPLE CTR AISLE OVERHEAD EMERGENCY LIGHTS TO BE INOPERATIVE. MX REPLACED THE B5-102 & B5-106 EMERGENCY LIGHT BATTERY PACKS. AN OPS CHECK WAS PERFORMED AND THE ACFT WAS RETURNED TO SERVICE. (DLM88101509)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 51,467 hrs · 38,480 cycles

DURING L/O FOUND CABIN EMERGENCY LIGHTS IN CEILING INOP ROWS 17-21. REPLACED BATTERIES AT BATT PACK B5-102. OPS CK OK.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 51,467 hrs · 38,480 cycles

CABIN EMERGENCY LIGHTS IN CEILING INOP, ROWS 17-21 REPL BATTERIES AT BATTERY PACK B5-102. OP CK OK.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 50,741 hrs · 38,033 cycles

EMERGENCY ESCAPE LIGHTING INOP ABOVE L1 DOOR, R1 DOOR, AND COCKPIT DOOR. RELAMPED LIGHT ASSY ABOVE L1 DOOR AND REPLACED BATTERY PACK.

Part: SKIN — DAMAGED (FS 313-427) · airframe 48,193 hrs · 36,407 cycles

FUSELAGE BELLY SKIN FROM FS 313 TO FS 427, AND L26L TO L26R WAS SPLICED DUE TO NUMEROUS GOUGES, TWO PREVIOUS SKIN REPAIRS, AND REMNANTS OF AN ANTENNA MODIFICATION THAT IS NO LONGER USED. THE SKIN SPLICE WAS PER THE SRM, AND INCLUDED PLUGGING PREVIOUS REPAIR FASTENER HOLES IN THE PRODUCTION DOUBLER (BEAR STRAP).

Part: SKIN — GOUGED (BS 360-427) · airframe 48,193 hrs · 36,407 cycles

DEEP GOUGES ON EXTERNAL FUSELAGE SKIN FROM STA 360-427 BTW LONG 27 RT-30. GOUGES WERE BLENDED OUT IAW SRM 53-04D FIG 38, SOME FOUND OUT OF LIMITS. DAMAGED SKIN REMOVED IAW SRM 53-04 FIG 12C. NEW SKIN INSTALLED IAW SRM 53-04D FIG 12C VIEW T AND H. REPAIR IDENTIFIED IAW PS 900-5-1 NR 4.

Part: TAB — CONTAMINATED (RT ELEVATOR) · airframe 48,193 hrs · 36,407 cycles

REPAIR RT ELEVATOR ANTI-FLOAT TAB DUE TO PRESENCE OF WATER IN HONEYCOMB STRUCTURE. WATER IN HONEYCOMB STRUCTURE REMOVED IAW SRM 51-70-2 PAR 6C. TAB WAS BALANCED IAW SRM 55-20-2D.

Part: TAB — CONTAMINATED (LT ELEVATOR) · airframe 48,193 hrs · 36,407 cycles

REPAIR LT ELEVATOR ANTI-FLOAT TAB DUE TO PRESENCE OF WATER IN HONEYCOMB STRUCTURE. WATER REMOVED IAW SRM 51-70-2 PAR 6C. TAB WAS BALANCED IAW SRM 55-20-2D.

Part: TAB — DELAMINATED (RT ELEVATOR) · airframe 48,193 hrs · 36,407 cycles

DELAMINATED UPPER SKIN ON RT ELEVATOR CONTROL TAB. THIS NR WAS ACCOMPLISHED IAW OPN 1031. WEIGHT AND BALANCE CHECK TO BE ACCOMPLISHED PER NR T0111759.

Part: SKIN — DAMAGED (TRIM TAB) · airframe 48,193 hrs · 36,407 cycles

SWOLLEN UPPER SKIN OF RT GEARED TAB OTBD SECTION. RT GEARED TAB OTBD SECTION WAS REPAIRED IAW SRM 55-04 PAR 3 FIG 2 AND OPN 1031 CARD 1260.

Part: TAB — UNKNOWN (ELEVATOR) · airframe 48,193 hrs · 36,407 cycles

LIGHTNING STRIKES ON T/E OF RT ELEVATOR CONTROL TAB. THIS N/R CARD WAS ACCOMPLISHED IAW OPN 1031 CARD NO 1242. RT ELEVATOR CONTROL TAB WAS BALANCED IAW SRM 55-20-2D.

Part: TAB — PUNCTURED (LT ELEVATOR) · airframe 48,193 hrs · 36,407 cycles

PUNCTURE UPPER SURFACE OF LT ANTI-FLOAT TAB. PUNCTURE REPAIRED IAW OPN 1031 CARD 1178. WEIGHT AND BALANCE WILL BE ACCOMPLISHED PER N/R T0111845.

Part: TAB — NICKED (LT ELEVATOR) · airframe 48,193 hrs · 36,407 cycles

NICKS ON LOWER SURFACE OF LT ANTI-FLOAT TAB. NICK ON LOWER SURFACE OF LT ANTI FLOAT TAB WAS REPAIRED IAW OPN 1031 CARD 1187.

Part: DOOR FRAME — CORRODED (BS 370-408) · airframe 48,193 hrs · 36,407 cycles

EXFOLIATION CORROSION ON LOWER C1 DOOR JAMB FROM STA 370-408. DAMAGED SECTION OF JAMB PAN WAS REMOVED IAW SRM 53-08D. NEW JAMB SECTION DRILLED AND TRIMMED IAW 53-05D FIG 804D. REPAIR ANGLES FABRICATED IAW SRM 53-05D FIG 804D. NEW SECTION OF JAMB PAN AND REPAIR PARTS INSTALLED IAW SRM 53-05D FIG 804D. REPAIR IDENTIFIED PER PS 900-5-1 NO 04.

Part: RUDDER — DAMAGED · airframe 48,193 hrs · 36,407 cycles

DAMAGED METALIZED PROTECTION COAT ON RUDDER ASSY. DAMAGED METALIZED WAS SANDED IAW SRM 51-70-1AD PAR 23 FIG 58. ONE PLY OF STYLEROGLASS FIBER FABRIC AND ASTRO STRIKE LAMINATE IMPREGNATE WITH EA956 AB WERE INSTALLED IAW SRM 51-70-1AD PAR 23. ASSEMBLY WAS CURED IAW SRM 51-70-1AD.

Part: SKIN — DENTED (BS 206) · airframe 48,193 hrs · 36,407 cycles

DENT ON FUSELAGE SKIN STA 206 BTW LONG 16 AND 17. DENT FOUND WITHIN LIMITS IAW SRM 53-04 FIG 38 TABLE COND 1B. PER NDT SPM 06.10.001 HFEC ACCOMPLISHED, NO CRACKS FOUND. NEW FILLER AND DOUBLER FABRICATED IAW ERA 362959-14 REV B. NEW DOUBLER AND FILLER INSTALLED IAW ERA 362959-14REVB.

Part: SKIN — DENTED (BS 229-245) · airframe 48,193 hrs · 36,407 cycles

DENTS ON REPAIR DOUBLER STA 229-245 BTW LONG 16 AND 18 LT. DENT OUT OF LIMITS. REMOVED DOUBLER AND FILLER IAW SRM 51-30-2 AND 51-30-5. REPAIR PARTS INSTALLED IAW ERA 330121-14 REV E.

Part: DOOR FRAME — CORRODED (BS 636-693) · airframe 48,193 hrs · 36,407 cycles

EXFOLIATION CORROSION ON LOWER DOOR JAMB FRAME BTW STA 636-693 WITHIN C2. REMOVED CORROSION IAW SRM 51-10-3, FOUND OUT OF LIMITS. FABRICATED REPAIR PARTS WERE INSTALLED IAW SRM 53-05 FIG 123.

Part: MOUNT — SCRATCHED (NR 1 ENGINE) · airframe 48,193 hrs · 36,407 cycles

SCRATCHED INNER WALL ON FLANGE OF AFT MOUNT BOLTS FOR LT ENGINE. SCRATCHES REWORKED IAW EA 49-469467-14. WITHIN LIMITS AND NO CRACKS NOTED IAW EA 49-469467-14 REV ORIGINAL.

Part: BOLT — WORN (RT ENGINE) · airframe 48,193 hrs · 36,407 cycles

WEAR ON AFT CONE BOLT FLANGES (BOTH SIDES) ON RT ENGINE. WEAR REWORKED IAW EA 49-469467-14 REV ORIG. WITHIN LIMITS AND NO CRACKS NOTED IAW EA 49-469467-14 REV ORIGINAL.

Part: SKIN — DENTED (BS 674 STR 21L) · airframe 48,193 hrs · 36,407 cycles

DUE ERA 093410-14 REV A FUSELAGE SKIN STA 674 STR 21L REPAIR OF DENT. ACCOMPLISH PERM REPAIR AT NEXT HMV. DAMAGED AREA WAS CUT OUT IAW SRM 53-04 FIG 12C. REPAIR PARTS WERE FABRICATED IAW 53-04D FIG 12C. REPAIR PARTS WERE INSTALLED IAW SRM 53-04D FIG 12C AND IDENTIFIED IAW PS 900-1-4 NO 04.

Part: TAB — BENT (TRIM SYSTEM) · airframe 48,097 hrs · 36,336 cycles

BENT LT ANTI-FLOAT TAB AT OUTBOARD AFT CORNER. BENT LT ANTI-FLOAT TAB AT OTBD AFT CORNER WAS REPAIRED IAW OPN 1031 CARD 1196. WEIGHT AND BALANCE WILL BE ACCOMPLISHED PER NR T0111845.

Part: CLAMP — DETACHED (LT ACM) · airframe 42,670 hrs · 32,848 cycles

RAPID DEPRESSURIZATION AT FL 330 MASKS DID NOT DROP PRIOR LOSS OF CABIN FLOW-LIGHT BLINKED. NO OTHER LIGHTS WERE ON, CABIN ALT CLIMBED TO 10500 FT MAX. FOUND DUCT CLAMP OFF AT INLET OF LT PACK ACM. RESECURED CLAMP AND PRESSURIZED CABIN USING LT ENG AS PNEU SUPPLY ALSO PERFORMED CABIN PRESSURIZATION USING RT PACK AND ENG ALL SYSTEMS NORMAL.

Part: B-NUT — LOOSE (HYDRAULIC SYS) · airframe 41,677 hrs · 32,184 cycles

LOST LT HYD QTY AND BURNING SMELL IN CABIN. FOUND B NUT LOOSE ON UNION BELOW T/R ACCUM, SECURED SAME. LK CKS GOOD. PERFORMED OP 5090 ALT DUCT BURN OUT.

Part: B-NUT — LOOSE (HYDRAULIC SYS) · airframe 41,673 hrs · 32,182 cycles

ON TAXI OUT, GOT SMELL IN CABIN AND COCKPIT, SHUT DOWN APU. SMELL SLOWLY DISSIPATED. FOUND B-NUT LOOSE ON 4-WAY HYD UNION ABOVE T/R CONTROL VALVE, SECURED SAME, LEAK CK GOOD.

Part: BALLAST — OVERHEATED (CABIN) · airframe 40,913 hrs · 31,656 cycles

DIV TO BNA, F/A REPORTS BURNING ELECTRICAL SMELL IN MID CABIN. FOUND BALLAST AT SEAT 25ABC BURNT. REPLACED SAME.

Part: CONNECTOR — LOOSE (EMERGENC LIGHTS) · airframe 38,937 hrs · 30,216 cycles

SEAT MOUNTED EMERGENCY LIGHTS INOP AT SEAT 24DE. SECURED LOOSE CONNECTOR, OPERATION NORMAL.

Part: CAP — LEAKING (APU OIL SYSTEM) · airframe 38,889 hrs · 30,175 cycles

HAZE IN CABIN FROM AC PACKS. FOUND OIL IN APU INLET. CLEANED SAME. PERFORMED DUCT BURNOUT.

Part: SEAL — LEAKING (GALLEY DOOR) · airframe 38,250 hrs · 29,710 cycles

ACFT WOULD NOT PRESSURIZE, RETURNED TO CVG LOUD NOISE FROM AFT GALLEY DOOR SEAL. OPENED DOOR / INSP DOOR SEAL, NO TROUBLE FOUND. PRESS CKD ACFT NORMALLY.

Part: GCU — FAILED (E/E BAY) · airframe 34,145 hrs · 26,898 cycles

AFTER TAKE OFF, HAD LEFT GENERATOR FAIL AND AC CROSSTIE LOCK OUT MSG. AIR RETURN TO PHX T/S LEFT GCU WITH GCU FAULT LIGHT REPLACED LEFT GCU. INSP LT GEN AND CURRENT TRANSFORMERS. ALL CKS GOOD. RAN AC CROSSTIE TEST. FAILED TEST. REPLACED LT GEN POWER RELAY. NOW CKS OK.

Part: APU — LEAKING (AFT) · airframe 34,068 hrs · 26,852 cycles

WITH CONDITIONED AIR AND PACKS POWERED BY START CART FUMES ENTERED CABIN. TURNED OFF PACKS FUMES DISSIPATED. AFTER TAKEOFF, CABIN WAS KEPT COOL AND FUMES DISSIPATED TOTALLY. IN CRUISE WHEN TEMP SELECTED ABOVE 60 DEG FUMES NOTICED AGAIN. PERFORMED OPNS 5088,5089 CABIN SMOKE/ODER T/S AND DUCT BURNOUT. NO CABIN FUMES NOW NOTED

Part: DOUBLER — WORN (FUSELAGE) · airframe 32,873 hrs · 25,993 cycles

DURING HMV-2, WEAR WAS FOUND ON ALL 4 CORNERS OF THE UNDERLYING SKIN DOUBLER SURROUNDING THE AFT LAV SERVICE DOOR JAMB. THE DAMAGE WAS REMOVED AND DOUBLERS INSTALLED.

Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY) · airframe 32,813 hrs · 25,949 cycles

F/C LAVATORY SMOKE DETECTOR ACTIVATED ON TAKEOFF. NO SMOKE, FIRE, OR FUMES. WOULD NOT RESET.

Part: BATTERY — DISCONNECTED (CABIN) · airframe 30,238 hrs · 24,064 cycles

RT AFT LAV SMOKE DETECTOR WILL NOT TEST RESEATED BATTERY. OPN NML.

Part: GENERATOR — FAILED (PAX CABIN) · airframe 28,687 hrs · 22,888 cycles

RIGHT HAND PASSENGER CHEMICAL OXYGEN GENERATOR UNIT FAILED TO FIRE DURING ACTIVATION, PRIOR TO DISPOSAL IN HAZARDOUS WASTE DRUM. TRIED SEVERAL TIMES TO ACTIVATE. GENERATOR WAS BEING REPLACED DUE TO TIME. MANUFACTURE DATE-9-89.LOT NO.1314.

Part: COALESCER BAG — CONTAMINATED (AFT ACCESSORY) · airframe 27,497 hrs · 22,009 cycles

F/A REPORTED ELECTRICAL SMELL IN CABIN RETURNED TO LGA. NO SMELL NOTED ON A/C ARRIVAL INSPECTED LIGHTS AND BALLASTS IN CABIN AND CARGO BINS NTF OR SMELL NOTED. REMOVED OVENS AND CKED WIRING NTF. INSPECTED AND RAN RECIRC FANS, PACKS CKED WATER COMPRESSOR ALL NML. INSPECTED E/E AREA, NTF OR ELECTRICAL SMELL. REPLACED BOTH WATER SEPARATOR BAGS, CKED 8TH AND 13TH STAGE DOME CAPS, NO OIL FOUND. RAN ENGS PER PFHB, NO SMELL NOTED.

Part: WINDSHIELD — OVERHEATED (COCKPIT) · airframe 26,784 hrs · 21,462 cycles

F/O AND F/A , REPORTED BURNING ODOR. FOUND WINDSHIELD OVERHEAT MSG ON OAP. TURNED SWITCH OFF, ODOR DISAPPEARED. RAN WINDSHIELD HEAT FOR 25 MINUTES. NO MSG. NO ODOR NOTED.

Part: UNKNOWN — ODOR (COCKPIT)

FLT ATTENDANTS REPORTED STRONG ODOR LIKE BURNING PLASTIC IN CABIN. ODOR WAS STRONGER IN AFT CABIN. ODOR EVIDENT IN COCKPIT. OCCURRED JUST AFTER T/O. PNUE XFEED CLOSED AIRFOIL ANTI-ICE OFF, ENGINE ANTI-ICE OFF, TEMP CONTROL VALVE POSITION BOTH SET AT 2 O'CLOCK. SMOKE WAS NEVER PRESENT. PERFORMED DUCT BURN-OUT. COALESCER BAGS CK. OK.

Part: RECIRC FAN — SEIZED (A/C BAY)

SHORTLY AFTER T/O, STRONG ODOR SMELLED IN AFT CABIN. ODOR DISSIPATED AFTER 7-9 MIN. PASSENGER REPORTED, RUBBER SMELL. F/A REPORTED, ELECTRICAL SMELL. MTC FOUND AFT RECIRCULATION FAN LOCKED UP. REPLACED SAME.

Part: COALESCER — CONTAMINATED (WATER SEPARATOR)

STRONG ELECTRICAL ODOR REPORTED IN AFT CABIN ON CLIMBOUT AT 15,000 FT. ODOR WAS SMELLED IN COCKPIT SOON AFTERWARD. RETURNED TO ATL. PERFORMED DUCT BURN-OUT. REPLACED COALESCER BAGS.

Part: SKIN — DAMAGE (BS 207)

FUSELAGE SKIN FS 207-218 S-16L - 17L DENT REPAIR. DENT DAMAGE TO SKIN BETWEEN FS 207 AND 218 AND BETWEEN S-17L AND 16L. SKIN CUTOUT 9.25 BY 7.26 TO REMOVE DENT DAMAGE. SKIN DOUBLER REPAIR INSTALLED PER ER/A 362959-14.

Part: SKIN — DENTED (BS 207-218)

THE AIRCRAFT SUSTAINED JETWAY DAMAGE BETWEEN STA 207 AND 218, STR 16L AND 17L. THE CUTOUT MEASURES 9.25 X 7.26 AND IS IN THE FIRST SKIN LAYER ONLY (.050 THICK CLAD 2024-T42). THE REPAIR IS PER THE INSTRUCTIONS OF DAL MD88 SRM 53-04, FIGURE 12B, SHEET 12. THIS REPAIR DOUBLER WILL OVERLAP THE L-1 DOOR SURROUND DOUBLER.

Part: FRAME — CRACKED (BS 1418)

MAINTENANCE FOUND A 1 INCH CRACK ATR FS 1418, L-2R AT THE TYPICAL LOCATIONS COVERED BY EO 9-63538-03. THE A/C COVERED IN THIS ER/A IS NOT COVERED BY THE REF EO (A/C 901-963), BUT AS A REPAIR AND PREVENTION OF FUTURE FATIGUE, THE EO WOULD BE PERFORMED ON THIS A/C. PERFORM EO 9-63538-03, OPN 0104 ON A/C 970 WITH THE FOLLOWING EXCEPTION: RETAIN AND USE THE EXISTING AFT STIFFENER WITH REPAIR KIT. DO NOT USE THE KIT SUPPLIED REPAIR AFT STIFFENER.

Part: SKIN — DENTED (BS 218)

THE SKIN OF THE AIRCRAFT WAS FOUND DENTED BEYOND LIMITS SPECIFIED BY THE SRM. THE DENT IS LOCATED AT STA 218 BETWEEN STR 18L AND 19L. LOCAL SKIN IS 0.050 2024-T3 CLAD SHEET. THE CUT OUT PORTION OF THE SKIN MEASURES APPROXIMATELY 5.0 IN THE LONGITUDINAL DIRECTION AND 4.5 IN THE CIRCUMFERENTIAL DIRECTION. REPAIR SIMILAR TO SRM 53-04 FIG 38.

Part: SKIN — DENTED (BS 237)

THE FUSELAGE SKIN WAS FOUND TO HAVE A DENT AT STA 237, STR 18 TO 20L. THE DENT IS 12 BY 12 AND MAX. 0.030 DEEP. THE SKIN IS MANUFACTURED FROM 0.050 2024-T3 CLAD SHT. THE DAMAGED AREA OF SKIN WAS CUT OUT AND MTC REPORTS THAT THERE WAS NO INTERNAL STRUCTURE DAMAGE DUE TO THE DENT. WHEN THE SKIN WAS CUT OUT, IT WAS DISCOVERED THAT THERE WAS A CRACK IN THE FINGER DOUBLER AT THE CUSP LINE NEAR FS 237. SLOT OUT DAMAGE IN THE FINGER DOUBLER ONLY MAINTIANING 0.25R; ONE .025 FINGER DOUBLER FILLER; ONE 0.063 EXTERNAL DOUBLER, ONE 0.050 FILLER.

Part: SKIN — GOUGED (BS 408)

THE FUSELAGE SKIN WAS FOUND GOUGED AT FS 408 BETWEEN STR 29R TO 30, JUST FWD AND O/B OF THE ANTENNA. THE RESULTING DAMAGE CUT OUT IS 6 (I/B / O/B) BY 3.5 (FWD /AFT). THE SKIN IS MANUFACTURED FROM 0.050 2024-T3 CLAD SHT. - 0.050 SKIN FILLER, 1 0.063 EXTERNAL DOUBLER, FINGER DOUBLERS ON I/B AND O/B SIDES.

Part: SKIN — DENTED (BS 541)

A DENT WAS FOUND ON THE FUSELAGE SKIN AT FS 541 AND STR 26R, JUST BELOW A SKIN OVERLAP. THIS DENT WAS CUT OUT MEASURING 6.1 FWD/AFT BY 2 UP/DOWN. THE SKIN IS 0.050 2024-T3 CLAD MATERIAL. 0.050 2024-T3 CLAD SHT FILLER; 0.063 2024-T3 CLAD SHT EXTERNAL DOUBLER; 0.050 2024-T3 STRUCTURAL FILLER (SKIN SPLICE OVERLAP); DTA ANALYSIS, 60,000 CYCLES LIMIT DTA.

Part: SKIN — DENTED (BS 237)

THE FUSELAGE SKIN WAS FOUND DENTED AT APPROX STA 237 BETWEEN STR 17L AND 18L. THE FINAL SKIN CUTOUT DIMENSIONS WERE 10.5 IN THE FWD/AFT DIRECTION AND 12.25 ABOVE/BELOW 0.063 2024-T3 CLAD SHT REPAIR DOUBLER.

Part: SKIN — CORROSION (BS 769-807)

CORROSION WAS FOUND UNDER THE RT RUB STRIP IN SEVERAL LOCATIONS BETWEEN STA 769 AND 807 AT APPROX STR 28R. THE CORROSION WAS BLENDED WITH A MAX DEPTH REMOVAL OF 0.026 AT STA 769. ALL LOCATIONS EXCEPT STA 769 REPAIR PER SRM BLEND ALLOWABLES STA 769 INSTALL A 0.063 REPAIR DOUBLER.

Part: FRAME — CRACKED (BS 1418)

MAINTENANCE FOUND A 1 INCH CRACK AT FS 1418, L-2R AT THE TYPICAL LOCATIONS COVERED BY EO 9-63538-03. THE AIRCRAFT COVERED IN THIS ER/A IS NOT COVERED BY THE REFERENCE EO (A/C 901-963), BUT AS A REPAIR AND PREVENTION OF FUTURE FATIGUE, THE EO WOULD BE PERFORMED ON THIS AIRCRAFT. PERFORM EO 9-63538-03, OPN 0104 ON A/C 970 WITH THE FOLLOWING EXCEPTION: RETAIN AND USE THE EXISTING AFT STIFFENER (DAC P/N 5913595-81) WITH REPAIR KIT. DO NOT USE THE KIT SUPPLIED REPAIR AFT STIFFENER (DAC P/N SR0953003-39).

Part: SKIN — DENTED (BS 323)

A DENT WAS FOUND IN THE FUSELAGE SKIN AT FS 313 DIRECTLY OVER STR 20R. THE DAMAGE REMOVAL RESULTED IN A CUTOUT 9 FWD/AFT AND 3 INCHES ABOVE/BELOW. REPAIR PER MD-88 SRM 53-04, FIG 12B, SHT 4, WITH THE FOLLOWING EXCEPTION, DO NOT INSTALL THE FINGER DOUBLER ABOVE THE DAMAGE. (THIS WILL INTERFERE WITH THE FINGER DOUBLER INSTALLED FOR THE ABOVE SPLICE).

Part: APU — DIRTY (AFT FUSELAGE)

SMOKE REPORTED IN AFT CABIN IMMEDIATELY AFTER T/O. AFT LAV\SMOKE DETECTOR WENT OFF, UNUSUAL SMELL IN COCKPIT. FOUND OIL LEAKING FROM APU, FWD APU TO MCO AND PLAC. CLEANED OILY AREA AROUND APU INLET, REPLACED WATER SEPARATOR BAGS AND SYSTEM CHECKS NORMAL.

Part: HOLD OPEN HOOK — BENT (PAX DOOR)

ON A/C INSPECTION, FOUND THE L1 DOOR HOLD OPEN HOOK BENT. REPLACED DOOR HOLD OPEN HOOK.

Part: HOLD OPEN HOOK — BENT (PAX DOOR)

FWD ENTRY DOOR HOLD OPEN HOOK BENT, WON,T HOOK DOOR. REPLACED HOOK, CKS GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN)

ON LAYOVER, FOUND ALL EMERGENCY LIGHTS INOP IN AFT CABIN. REPLACED BATTERY PACK, ALL LIGHTS OP NORMAL.

Part: WINDSHIELD — FAILED (FLT DECK)

DURING CLIMBOUT AT 5,000 FT, HEARD LOUD POP FROM CENTER WINDSHIELD AND THEN LOUD AIR RUSHING NOISE. FLIGHT RETURNED OAK. REPLACED CENTER WINDSCREEN.

Part: ANGLE — CRACKED (NR 1 ENG PYLON)

.50 INCH CRACK IN UPPER PYLON ATTACH ANGLE 18 INCHES FROM AFT WEDGE. FOUND DURING E-1 LTR CK. REPAIRED PER SRM 54-04A PG 17-18.

Part: BRACKET — CRACKED (RT MLG DOOR)

ON CLIMBOUT, HAD LANDING GEAR DOOR OPEN LIGHT. CYCLED GEAR, DID NOT GO OUT. RETURNED ATL. FOUND RIGHT MAIN LDG GEAR DOOR PROX SWITCH MOUNT BRACKET BROKEN. REPLACED BRACKET, OPERATION NORMAL.