N975DL

Part: RELEASE CABLE — OUT OF POSITION (R1 DOOR) · airframe 72,484 hrs · 53,733 cycles

MANUAL RELEASE CABLE NOT ROUTED CORRECTLY ON R-1 DOOR SLIDE. ROUTED CABLE PROPERLY, REF AMM 25-62-01. (LP0885790)

Part: CABLE — WORN (RT JETTISON) · airframe 72,484 hrs · 53,733 cycles

R/H JETTISON CABLE WORN, 2PLCS. REPLACED CABLE, REF MD 88 AMM 53-53-00. (LP0881150)

Part: DOUBLER — NONE · airframe 72,484 hrs · 53,733 cycles

ERA472703-14 REV ORIG FUSELAGE/DOUBLER-FWD TOILET SERVICE DOOR J AMB DOUBLER P/N 5953050-85/FS=288, LONG 20-21L/BLEND OUT REPAIR TIME-LIMITED. THIS LOGPAGE IS SUPERSEDED BY LOGPAGE 0873134. THE REPAIR INSTALLED PER ER/A 472703-14 HAS BEEN REMOVED, AND IS INCORPORATED INTO A NEW REPAIR INSTALLED PER ER/A 573901-14. ALL TIME-LIMITED ITEMS AND REQUIRED INSPECTIONS TRACKED PER THIS LOGPAGE ARE NOW BEING TRACKED BY LOGPAGE 0873134. OK TO CLOSE THIS LOGPAGE. ER/A 472703-14 WILL BE REVISED TO REV A TO NOTE ACCOMPLISHMENT OF NEW REPAIR AND OF NEW LOGPAGE TRACKING. (LP0590513)

Part: TAB — DENTED (RT ELEVATOR) · airframe 72,484 hrs · 53,733 cycles

RT ELEVATOR GEARED TAB UPPER SURFACE HAS 6 DENTS (MARKED). REPLACED RT GEARED TAB PER AMDS W/C 2730-4130-RH TAB, ELEVATOR, OFF 09-5522-9-0032 53267. (LP0871702)

Part: TAB — DENTED (LT ELEVATOR) · airframe 72,484 hrs · 53,733 cycles

LT ELEVATOR GEARED TAB HAS 7 DENTS ON UPPER SURFACE (MARKED). REPLACED LT GEARED TAB PER AMDS W/C 2730-4130-H. (LP0871725)

Part: TAB — BENT (RT ELEVATOR) · airframe 72,484 hrs · 53,733 cycles

RT ELEVATOR CONTROL TAB HAS 9 BENTS ON UPPER SURFACE (MARKED). REPLACE CONTROL TAB PER AMDS W/C 2730-4634-RH TAB, ELEVATOR C OFF 88-5520-9-0007 49189. (LP0871680)

Part: TAB — DENTED (LT ELEVATOR) · airframe 72,484 hrs · 53,733 cycles

LT ELEVATOR ANTI-FLOAT TAB HAS 8 DENTS ON UPPER SURFACE (MARKED). REPLACED LT ANTI-FLOAT TAB PER AMDS W/C 2730-4382-LH TAB, ELEVATOR; OFF 88-5525-9-0003 53342. (LP0871953)

Part: TAB — DENTED (RT ELEVATOR) · airframe 72,484 hrs · 53,733 cycles

RT ELEVATOR ANTI FLOAT TAB HAS 6 DENTS ON UPPER SURFACE (MARKED). REPLACED ANTI-FLOAT TAB PER AMDS WC / 2730-4382-RH TAB, ELEVATOR OFF 88-5520-9-0006 73955. (LP0871994)

Part: SPAR CAP — CRACKED (VERTICAL STAB) · airframe 72,484 hrs · 53,733 cycles

BHEC INSPECTION SHOWS CRACK INDICATIONS IN LH VERTICAL STABILIZER FRONT SPAR CAP FORWARD FLANGE AT 3RD FASTENER HOLE BELOW ZFS=52.267 SPLICE AND 14TH HOLE BELOW SPLICE. MARKED. REF STEP 2 OF 5530-01045-0602. REPAIRED REF ERA 498510-14AD REV A AND 498493-14AD REV A. (LP0871796)

Part: FRAME — CRACKED (FUSELAGE) · airframe 71,934 hrs · 53,257 cycles

CANTED FRAME CRACKED AT TAIL CONE ALIGNMENT PIN JUST BELOW RT UPPER LATCH. REMOVED AND REPLACED AFT FUSELAGE TAIL CONE CANTED ATTACH FRAME.

Part: FLAP — DAMAGED (RT WING) · airframe 71,347 hrs · 52,752 cycles

RT FLAP TRAILING EDGE DAMAGED. REMOVED AND REPLACED RT IB TRAILING EDGE FLAP PER W/C 2751-5324.

Part: FRAME — CRACKED (RT MLG WW) · airframe 71,243 hrs · 52,668 cycles

FOUND THE RT WHEEL WELL CUTOUT CRACKED. REMOVED AND REPLACED THE FRAME IAW ERA 568949-14, SECTION 2, DWG 590584, AND ERA 568949-14, SECTION 2.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 71,219 hrs · 52,648 cycles

LT FWD OVERWING EMER EXIT 1 BULB INOP. REPLACED LT FWD OVERWING EMER EXIT BULB PER AMM 33-50. OPS CHECK GOOD AT THIS TIME.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 70,154 hrs · 51,827 cycles

CEILING EMERGENCY LIGHTS OUT AT ROWS 12,13,AND 14. REPLACED BATTERIES IN THE POWER SUPPLY.

Part: UNKNOWN — ODOR (CABIN) · airframe 69,506 hrs · 51,280 cycles

AFTER TAKE OFF A STRONG FUME SMELL IN THE ENTIRE AIRCRAFT. FUMES SMELLED LIKE GAS. AFTER RUNNING QRH AND NOTICING RIGHT PACK FLUCTUATING +/- .5 PSI. PACK WAS TURNED OFF AND SMELL DISSAPATED IN COCPIT AND AFT AIRCRAFT. SMELL REMAINED IN 1ST CLASS FOR MAJORITY OF FLIGHT. BEGAN SMOKE/ODOR TROUBLESHOOTING PER CARD 2120-2367. REMOVED CABIN FLOOR PANEL ABOVE CTR WING BOX(424150) INSPECTED SADLE DUCTS ON ENG 1 AND 2. ALL CLEAN. NO DEFECTS. COMPLIED WITH WC 2120-2367(SMOKE/ODOR TROUBLESHOOTING) COMPLIED WITH WC 2120-2368 (AIR COND SYS OIL CONTAMINATION CLEANING). CABIN FLOOR PANEL ABOVE CENTER WING BOX INSTALLED. COMPLIED WITH WC 7100-2619( PNEMATIC SYS DUCT BURN OUT) A/C OK FOR SERVICE.

Part: BRACKET — CRACKED (BS 1463) · airframe 68,445 hrs · 50,474 cycles

FOUND CRACK IN LOUVER BRACKET AT STATION L5 OF BS 1463 CANTED FRAME. R & R LOUVER MOUNT BRACKET AT STATION L5 OF 1463 CANTED FRAME IAW MD88 SRM 53-14-4 FIG 4 AND BOEING DRAWING 9911839. (LP2977886)

Part: SLIDE — DAMAGED (L1 DOOR) · airframe 67,813 hrs · 50,067 cycles

L1 DOOR SLIDE GIRT BAR HARD TO INSTALL. FOUND SLIDE BUSTLE DAMAGED AND NOT ALLOWING GIRT BAR TO ENGAGE COMPLETELY. R & R THE L1 DOOR SLIDE ASSY IAW AMDS WC 2561-4964. CHECKED GOOD.

Part: JACKSCREW — WORN (HORIZONTAL STAB) · airframe 67,456 hrs · 49,828 cycles

HORIZONTAL STAB JACKSCREW THREADS HAVE STEP WEAR. REPAIRED IAW PRI 553056-14AD REV 0 AND COMPLIED WITH ERA 553056-14AD REV ORIG.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 66,993 hrs · 49,481 cycles

DURING SERVICE CHECK FOUND ROW 26DE EMERGENCY LIGHT INOPERATIVE. REATTACHED EMERGENCY LIGHT CONNECTOR WOW 26DE. CK OK.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT) · airframe 66,795 hrs · 49,321 cycles

SEAT 34 ED EMERGENCY LIGHT INOPERATIVE. FOUND QUICK RELEASE PLUG LOOSE. CONNECTED IAW AMM 33-00. OPS CHECKED NORMAL.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 66,743 hrs · 49,285 cycles

AFT CEILING EMERGENCY LIGHTS OVER AFT SERVICE DOOR INOPERATIVE. INSTALLED NEW BATTERIES IN POWER SUPPLY FOR AFT CEILING LIGHTS. OPS CHECKED OK. OK FOR SERVICE.

Part: CONNECTOR — INOPERATIVE (EMERGENCY LIGHTS) · airframe 66,699 hrs · 49,254 cycles

SEAT 34D EMERGENCY LIGHT INOPERATIVE. REPLACED CONNECTOR AT SEAT 34D IAW AMM 33-50. OPS CHECKED GOOD.

Part: PIN — DISENGAGED (L1 DOOR SLIDE) · airframe 66,071 hrs · 48,786 cycles

THE FLIGHT CREW FOUND THE PARACHUTE PINS DISENGAGED ON THE L-1 DOOR EMERGENCY ESCAPE SLIDE. MAINTENANCE REPLACED THE L1 EMERGENCY ESCAPE SLIDE ASSY.

Part: SPAR — CRACKED (LT WING) · airframe 65,865 hrs · 48,639 cycles

LT REAR SPAR SHOWS A CRACK INDICATION OF 0.100" IAW NDT SPM 06-01.001 AT THE 5:30 POSITION. CRACK VERIFIED LESS THAN 1". PERFORMED REPAIR IAW DWG JO60271.

Part: SPAR — DAMAGED (LT WING) · airframe 65,865 hrs · 48,639 cycles

LEFT WING LOWER AFT SPAR, VERTICAL LEG BS 154-164 HAS 14 HOLES MIS-DRILLED, ELIPITICAL. ACCOMPLISHED REWORK OF HOLES 14EA IAW ER/A 544925-14AD.

Part: HINGE — DAMAGED (LT WING TE FLAP) · airframe 65,865 hrs · 48,639 cycles

LT FLAP HINGE INBD HOLE. CIRCUMVENTIAL SEMI-CIRCLE WORN, GOUGE ON WING SPAR FLANGE. R & R FLAP HINGE FITTING IAW AMM 57-40-01.

Part: STRUCTURE — CRACKED (LT WING TE FLAP) · airframe 65,865 hrs · 48,639 cycles

REMOVE INBD FLAP HINGE FITTING FOR LT WING OTBD FLAP TO DETERMINE CRACK LENGTH. FLAP FITTING IS LOCATED ON AFT WING SPAR BS 164. MEASURED AND MARKED ENDS OF CRACK IAW NDTSPM 06-10-01.001. CRACK MEASURES .625 IN LENGTH. INSTALLATION OF INBD FLAP FITTING TO BE ACCOMPLISHED ON NR NR 15. REPAIR OF CRACK TO BE ACCOMPLISHED ON NR 1, PRI 544925-14AD.

Part: STRUT — CORRODED (NLG) · corrosion level 2 · airframe 65,865 hrs · 48,639 cycles

NLG SHOCK STRUT HAS CORROSION IN INNER BORE RT SIDE AXLE AREA. SEE NR FOR ADDITIONAL INFORMATION 006-0001:3230-5003/002 00003. REPLACED NLG SHOCK STRUT IAW AMM 32-21-02 AND REPLACED SEALS IAW AMDS CARD 3221-6192.

Part: SHUTOFF VALVE — MALFUNCTIONED · airframe 65,764 hrs · 48,564 cycles

ACFT WOULD NOT PRESSURIZE AFTER T/O RAN QRH PROCEDURES. NO HELP. CABIN SUPPLY TEMP REACHED 150F NO AIRFLOW AFTER T/O COULD FEEL AIRFLOW CYCLE 2 OR 3 TIMES ON THEN BACK OFF DURING FLIGHT. R & R LT PRSOV IAW AMM 21-31. LT FLOW CONTROL VALVE SLOW TO OPERATE. REPLACED SAME OPEN CKS AND LEAK CKS OK. REPLACED 575 DEGREE THERMOSTAT DUE TO AIR LEAKAGE IAW AMMM 21-61. PERFORMED SINGLE PACK CONFIDENCE CHECKS IAW AMM 21-00 AND HULL LEAK CHECK. PERFORMED ALL STEPS OF ODI PREVENTION WITH NO CONTAMINATION OF PNEU DUCTS, ENGINE AND ACFT SYSTEMS. C/W CARDS 2120-2367 AND 7100-2619, FULL DUCT BURN WITH NO ODORS NOTED.

Part: BOTTLE — LOW PRESSURE (ESCAPE SLIDE) · airframe 64,920 hrs · 47,935 cycles

MAINTENANCE FOUND AFT CABIN SERVICE DOOR EMERGENCY ESCAPE SLIDE PRESSURE LOW. THE SLIDE WAS REPLACED.

Part: PIN — PULLED (L1 DOOR SLIDE) · airframe 64,868 hrs · 47,886 cycles

FOUND L1 DOOR SLIDE PIN PULLED. THE SLIDE WAS REPLACED.

Part: WIRE — PULLED (EMERGENCY LIGHT) · airframe 63,067 hrs · 46,673 cycles

MAINTENANCE FOUND THE EMERGENCY PATH LIGHT INOPERATIVE AT SEAT 28R. MAINTENANCE RE-INSERTED A PINNED WIRE BACK INTO THE OTBD HARNESS CONNECTOR AT SEAT 28R AND FIXED THE PROBLEM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 62,253 hrs · 46,102 cycles

COCKPIT EMERGENCY LIGHT DOES NOT ILLUMINATE. REPLACED FORWARD BATTERY POWER PACK AND THE LIGHTS WERE OPERATIONAL.

Part: BARRIER — CRACKED (CARGO DOOR) · airframe 62,224 hrs · 46,079 cycles

SEVERAL CRACKS BEYOND PREVIOUS STOP DRILLS ALSO ON PREVIOUS MID SCREW HOLES OF MID CARGO COMPARTMENT DOOR BARRIER. DOUBLERS WERE REMOVED IAW SRM 51-30-2 DAMAGE WAS REMOVED IAW SRM 53-01, FIG 4, SHEET 4 DOUBLERS AND SPLICES WERE FABRICATE IAW SRM 53-01. DOUBLERS AND SPLICES WERE TREATED AND PAINTED IAW SRM 51-10-3, PAR 14/21. DOUBLERS AND SPLICES WERE INSTALLED IAW SRM 51-30-2.

Part: BARRIER — DAMAGED (CARGO DOOR) · airframe 62,224 hrs · 46,079 cycles

SEVERAL CRACKS BEYOND PREVIOUS STOP DRILLS ALSO ON PREVIOUS MID SCREW HOLES OF MID CARGO COMPARTMENT DOOR BARRIER. ANGLE WAS REMOVED IAW SRM 51-30-2 THEN ANGLE WAS FABRICATED IAW DWG 9935747, REV J THEN ANGLE WAS TREAT/PAINT IAW SRM 51-10-3, PAR 21 AND 14. THEN ANGLE WAS INSTALLED IAW SRM 51-30-2 AND DWG 9935747, REV J.

Part: BULKHEAD — CRACKED (BS 1003) · airframe 62,253 hrs · 46,102 cycles

CRACK ON FWD BULKHEAD PANEL BEAM STA Y=1003 X=22 AND Z=-1 AT AFT CARGO COMPARTMENT SUMMARY ANGLE WAS REMOVED CRACK STOPPED, REPAIR DOUBLER WAS TRIMMED AND DRILLED REPAIR DOUBLER WAS TREATED PAINTED AND INSTALLED ANGLE WAS INSTALLED REPAIR WAS IDENTIFIED IAW SRM 53-01, FIG 2, SHEET 4, 51-10-3, PAR 21, 14, 51-60-0,51-30-5, DWG 9958212, PS 900-5-1N.

Part: HINGE — CRACKED (CARGO DOOR) · airframe 62,253 hrs · 46,102 cycles

CRACKS FOUND ON FWD AND AFT HINGE SECTION OF MID CARGO DOOR BARRIER, HINGE REMOVED IAW SRM 51-30-2, AND A NEW SECTION OF HINGE DRILLED IAW SRM 51-10-4.

Part: FLOOR SUPPORT — CORRODED (BS 1212) · corrosion level 2 · airframe 62,224 hrs · 46,079 cycles

CORROSION ON UPPER FLOOR SUPPORT BS 1212 BETWEEN LONGERONS 28-29R. FOUND OUT LIMITS AND WAS REPLACED IAW SRM 51-30-5, 51-10-3 P. 14-21-26, 51-10-4.

Part: ANGLE — CRACKED (CARGO DOOR) · airframe 62,253 hrs · 46,102 cycles

CRACKED ANGLE FWD AND AFT AT UPPER SUPPORTS MID CARGO DOOR (C2) (SH-CP-SM. ANGLE REMOVED IAW SRM 51-30-2 AND A NEW ANGLE FABRICATED IAW SRM 51-10-2. ANGLE TREATED AND PAINTED IAW SRM 51-10-3, PAR 21 AND 14, AND WERE INSTALLED IAW SRM 51-30-2.

Part: BEAM — CRACKED (FUSELAGE) · airframe 62,253 hrs · 46,102 cycles

CRACKED BEAM FWD END NR 4 AT FWD SERVICE DOOR, R1, SM, CARD 7, ZONE 58. NEW BEAM WAS INSTALLED IAW SRM 51-30-1,51-30-2 AND 51-30-5.

Part: SKIN — DEBONDED (LT WING) · airframe 62,253 hrs · 46,102 cycles

DEBONDED SKIN FWD OTBD EDGE OF 2.500" X 0.500" AND OUTBD EDGE OF 2500" X 0.500" AT LT HEATER BLANKET, SM, REPAIR WAS PERFORMED IAW AMM 30-80-02-801, PARA 2A, 9, 1674412.

Part: BAR — CORRODED (RT WING TE FLAP) · airframe 67,375 hrs · 49,778 cycles

CORROSION ON FLEX JOINT LOWER BAR AT RT FLAP WAS REPAIRED IAW ER/A.

Part: DOOR FRAME — CORRODED (CARGO BAY) · corrosion level 2 · airframe 62,222 hrs · 46,077 cycles

CORROSION ON MID CARGO BAY LOWER DOOR FRAME BEAM REPAIRED IAW ER/A 529350-14 MA, REV ORIGINAL AND SRM 53-05, FIG 123A.

Part: SKIN — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 62,294 hrs · 46,133 cycles

CORROSION ON HORIZONTAL STABILIZER UPPER SKIN. CORROSION WAS REMOVED AND FOUND WITHIN LIMITS IAW SRM 55-03D, PAR 30. REPAIR BUSHINGS WERE FABRICATED AND INSTALLED IAW SRM 55-3. REPAIRED IAW ETI-88-14-219 REV ORIG AND ER/A 52935214, REV ORIG.

Part: SKIN — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 62,294 hrs · 46,133 cycles

CORROSION ON HORIZONTAL STABILIZER UPPER SKIN. CORROSION REMOVED AND FOUND WITHIN LIMITS IAW SRM 55-03D, PAR 30. REPAIR BUSHINGS WERE FABRICATED AND INSTALLED IAW SRM 55.03.

Part: ANGLE — CORRODED (BS 180-200) · corrosion level 2 · airframe 62,222 hrs · 46,077 cycles

CORROSION ON CUSP WEB ANGLE BETWEEN X -60 TO X -54, BS 180 - 200. REMOVE CORROSION ON CUSP WEB ANGLE AND FOUND TO BE OUT OF LIMITS IAW SRM 53-01, FIG 1. ANGLE WAS REPAIRED IAW SRM 53-05, FIG 55 AND ETI-88-14-215.

Part: SKIN — SCRATCHED (BS 427-965) · airframe 62,222 hrs · 46,077 cycles

SCRATCHES ON RT WINDOW BELT BETWEEN BS 427-965. SCRATCHES BLENDED OUT IAW SRM 53-05, FIG 111, ER/A 529358-14 REVISION ORIGINAL.

Part: SKIN — DAMAGED (BS 374-378) · airframe 65,875 hrs · 48,643 cycles

SCRATCHES ON LOWER CORNER WINDOW BELT BS 319 AND BETWEEN BS 374 - 378 AT LT FWD FUSELAGE. SCRATCHES WERE BLENDED OUT MEASURED AND TREATED IAW SRM 53-05, FIG 111 AND ER/A 529358-14, REV ORIGINAL. A PERMANENT REPAIR WAS ACCOMPLISHED.

Part: SKIN — DAMAGED (BS 522-541) · airframe 62,222 hrs · 46,077 cycles

LIGHTNING STRIKE ON LOWER WINDOW BELT BETWEEN BS 522 - 541. DAMAGE BLENDED OUT IAW SRM 53-05, FIG 111, ER/A 529358-14, REV ORIGINAL AND ER/A 529360-14, REV ORIGINAL.

Part: CARGO TRACK — DAMAGED (BS 712-786) · airframe 62,222 hrs · 46,077 cycles

ENLOGATED HOLES ON LT CARGO TRACK BS 712 - 786. CARGO TRACK REPLACED IAW SRM 53-05, FIG 4G AND 51-30-2, 51-10-4, 51-10-3 PAR. 14 AND 21.

Part: ACCESS PANEL — CORRODED (WING) · airframe 62,222 hrs · 46,077 cycles

CORROSION ON COUNTERSINK HOLES AT ACCESS PANEL. CORROSION WAS REMOVED IAW SRM 51-22-2A, AND FOUND OUT OF LIMITS. THE ACCESS PANEL WAS REPLACED IAW SRM 51-22-2A CONDITION II.

Part: PAN — CRACKED (EMERGENCY EXIT) · airframe 62,222 hrs · 46,077 cycles

CRACKED PAN ON FWD UPPER CORNER OF LT FWD OVERWING EMERGENCY EXIT DOORS. CRACK ON PAN WAS STOPPED REPAIR DOUBLER WAS FABRICATED, PAINTED AND INSTALLED IAW SRM 52-05 A, FIG 51.

Part: CUSP WEB — CORRODED (BS 218) · corrosion level 2 · airframe 62,222 hrs · 46,077 cycles

CORROSION ON CUSP WEB BELOW SEAT TRACK X- 54 BS 218 . CUSP WEB REPAIRED IAW SRM 53-05, FIG 131A-17, AND SRM 51-30-2.

Part: BEAM — CORRODED (CARGO DOOR FRAME) · corrosion level 2 · airframe 62,222 hrs · 46,077 cycles

CORROSION ON MID CARGO DOOR FRAME UPPER BEAMBS 655 - 693. REMOVED AND REPLACED THE BEAM IAW 53-14-2, FIG 2, 51-30-2, SRM 51-30-5 AND SRM 53-14-2, FIG 2.

Part: DOOR FRAME — CORRODED (BS 1171-1174) · airframe 67,375 hrs · 49,778 cycles

CORROSION ON AFT CARGO DOOR FRAME NUT STRIP BS 1171-1174. REMOVED, FABRICATED NEW STRIP, TREATED, PAINTED AND INSTALLED.

Part: CUSP WEB — CORRODED (BS 200) · corrosion level 2 · airframe 62,222 hrs · 46,077 cycles

CORROSION ON RT CUSP WEB BS 200, X 44-54. CUSP WEB WAS REMOVED AND REPLACED IAW 51-30-2, 51-30-5, SRM 51-10-3, PARA 26 AND 53-01, FIG 1, SRM 53-14-1 AND 51-10-4.

Part: PAN — CRACKED (EMERGENCY EXIT) · airframe 62,222 hrs · 46,077 cycles

CRACKED PAN ON AFT UPPER INTERCOSTAL OF RT AFT OVERWING EMERGENCY EXIT DOOR. CRACK ON PAN WAS STOPPED AND REPAIR DOUBLER WAS FABRICATED PAINTED AND INSTALLED IAW SRM 52-05D, FIG 51.

Part: INTERCOSTAL — CRACKED (BS 953-958) · airframe 62,222 hrs · 46,077 cycles

CRACK ON INTERCOSTAL AT RT MLG INBD DOOR BETWEEN BS 953 - 958 . INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-30-2 AND 51-30-5.

Part: DOOR FRAME — CORRODED (AFT CARGO) · corrosion level 2 · airframe 62,222 hrs · 46,077 cycles

CORROSION ON AFT CARGO DOOR FRAME BEAM . REPAIRED IAW SRM 51-30-5, 53-05, FIG 123, 51-10-3, PAR 21 AND 14.

Part: CARGO TRACK — CORRODED (BS 1212-1287) · corrosion level 2 · airframe 62,222 hrs · 46,077 cycles

CORROSION ON RT CARGO TRACK, BS 1212-1287. CARGO TRACK WAS REMOVED, AND CORROSION WAS REMOVED AND FOUND OUT OF LIMITS. THE CARGO TRACK WAS REPLACED IAW SRM 51-30-1 AND 51-30-2, SRM 51-10-3, PAR 26, 21 AND 14, SRM 53-05, FIG 4C, SRM 51-10-4.

Part: CARGO TRACK — CORRODED (BS 693-788) · airframe 67,375 hrs · 49,778 cycles

CORROSION ON LT CARGO TRACK BS 693 - 788 . CORROSION FOUND TO BE OUT OF LIMITS. REPAIRED THE CARGO TRACK.

Part: SEAT TRACK — CORRODED (BS 200) · airframe 67,375 hrs · 49,778 cycles

CORROSION ON RT SEAT TRACK BS 200, X -43 TO X -45. THE SEAT TRACK WAS REMOVED AND REPLACED.

Part: CARGO TRACK — CORRODED (BS 1222-1289) · corrosion level 2 · airframe 62,222 hrs · 46,077 cycles

CORROSION ON LT CARGO TRACK, BS 1222-1289. REMOVED AND REPLACED THE CARGO TRACK IAW 51-10-3, PAR 14, 21, 26, 53-05, FIG 4C, 51-30-1, 51-30-2, 51-30-5, 51-10-4.

Part: FRAME — CRACKED (BS 984) · airframe 62,222 hrs · 46,077 cycles

CRACKED FRAME BS 984. REMOVED AND REPLACED IAW 51-30-1 AND 51-30-2,51-30-5

Part: CUSP WEB — CRACKED (BS 845) · airframe 62,222 hrs · 46,077 cycles

CRACKED RT CUSP WEB BS 845 BETWEEN X -52 TO X -60 . DAMAGE WAS REMOVED, REPAIR PARTS WERE FABRICATED TREATED AND PAINTED IAW SRM 53-05, FIG 131A-21, 51-10-3, PAGE 14, 21 AND REPAIR PARTS WERE INSTALLED IAW SRM 53-05, FIG 131A-21.

Part: SKIN — CORRODED (RUDDER) · airframe 62,222 hrs · 46,077 cycles

DAMAGED METALLIZED ON BOTH FACES OF RUDDER METALLIZED ON BOTH FACES OF RUDDER WERE REPAIRED IAW SRM 51-70-1A, PAR 23.

Part: CAM — WORN (TAILCONE) · airframe 62,222 hrs · 46,077 cycles

MAINTENANCE FOUND A WORN TAILCONE CAM BASE. MAINTENANCE REPLACED THE TAILCONE CAM BASE AND THE RII STEPS WERE COMPLETED.

Part: ANGLE — CORRODED (BS 1322 BULKHEAD) · corrosion level 2 · airframe 62,222 hrs · 46,077 cycles

CORROSION ON AFT CARGO BAY AFT BULKHEAD LOWER ANGLE BS 1322 BETWEEN LONGERONS 24L-24R. CORROSION REMOVED, AND FOUND OUT OF LIMITS. THE ANGLE WAS REPAIRED IAW SRM 51-30-2, SRM 51-10-3, PAR 26, 21 AND 14, ER/A 511165-14 MA, REV B.

Part: CUSP WEB — CORRODED (BS 560-579) · corrosion level 2 · airframe 62,222 hrs · 46,077 cycles

CORROSION ON REPAIR DOUBLER BS 560-579 AND X 54 - 60. CUSP WEB REMOVED AND REPLACED IAW SRM 51-10-3,51-30-2 , 51-30-5 AND 51-30-1.

Part: FRAME — CRACKED (BS 1485) · airframe 62,222 hrs · 46,077 cycles

CRACKED FRAME BS 1485. FRAME REMOVED IAW AMM 20-12-01, FASTENERS WERE REMOVED IAW SRM 51-30-2, 51-30-5, REPAIR ANGLE WAS FABRICATED IAW SRM 53-03, FIG 43. CRACK WAS STOP DRILLED IAW SRM 53-03, PAR 38; REPAIR ANGLE WAS TREATED AND PAINTED IAW SRM 51-10-3, PAR 14, 21. REPAIR ANGLE WAS INSTALLED IAW SRM 53-03, FIG 48 AND 51-30-2, 51-30-5.

Part: FRAME — CORRODED (BS 1322) · corrosion level 2 · airframe 62,222 hrs · 46,077 cycles

CORROSION ON FRAME BS 1322 LONGERONS 29 - 30R. FRAME SECTION WAS REMOVED AND REPLACED IAW SRM 51-30-2, 51-30-5, 53-03 D, FIG 2A, 51-10-3, PAR 14, 21 AND 38.

Part: HINGE — CORRODED (HORIZONTAL STAB) · airframe 62,222 hrs · 46,077 cycles

CORROSION LT HINGE NR 6 ON LT HORIZONTAL STABILIZER. SRM 55-01, PARA 3A, FOUND TO BE OUT OF LIMITS IAW DWG NR 4918019, REV D, HINGE WAS REPLACED.

Part: FRAME — CORRODED (BS 1271) · airframe 67,375 hrs · 49,778 cycles

CORROSION ON FRAME AT UPPER AND LOWER CAP BS 1271 LONGERONS 28R - 28L. CORROSION WAS REMOVED, A REPAIR WAS INSTALLED.

Part: LONGERON — CORRODED (BS 1257-1307) · corrosion level 2 · airframe 62,222 hrs · 46,077 cycles

CORROSION ON LONGERON 23L BETWEEN BS 1257 - 1307. LONGERON REMOVED AND REPLACED IAW SRM 51-10-3 PAR. 14, 21 AND 51-30-2.

Part: FRAME — CORRODED (BS 1380) · airframe 62,222 hrs · 46,077 cycles

CORROSION ON TEE FRAME BS 1380 BETWEEN LONGERONS 24 - 30RT. TEE FRAME WAS REPLACED IAW SRM 51-10-4, 51-10-3, 51-10-2, 51-30-5 AND DWG 9912246, REV "DE".

Part: CUSP WEB — CORRODED (BS 1043-1049) · corrosion level 2 · airframe 62,222 hrs · 46,077 cycles

CORROSION ON RT REPAIR DOUBLER BS 1043-1049 AT RT CUSP WEB X -53 TO X -60. NEW REPAIR DOUBLER, FILLER AND RING DOUBLER WERE INSTALLED, TREATED, PAINTED AND APPLIED CIC IAW SRM 53-05, FIG 131A-7, SHEET 1, 51-30-2, 51-30-5 AND 51-10-3 PAR 14/21/38.

Part: FRAME — CORRODED (BS 1309) · airframe 62,222 hrs · 46,077 cycles

CORROSION ON FRAME, BS 1309, ABOVE LONGERON 30. FRAME CLIP WAS REMOVED, AREA OUT OF LIMITS WAS REMOVED, REPAIR PARTS WERE DRILLED, ADJUSTED, FABRICATED, TREATED AND PAINTED. REPAIR PARTS WERE INSTALLED, CIC WAS APPLIED, AREA WAS IDENTIFIED IAW SRM 51-30-2, 51-30-5, 53-03 D FIG 2A, 51-10-3 PAR. 14-21-38, PS 900-5-1, NR 04.

Part: CUSP WEB — CORRODED (BS 833-838) · airframe 67,375 hrs · 49,778 cycles

CORROSION ON THE REPAIR DOUBLER OF CUSP WEB BS 833-838, X 54-60. REMOVED AND REPLACED THE REPAIR DOUBLER.

Part: CUSP WEB — CORRODED (BS 1184-1200) · airframe 67,375 hrs · 49,778 cycles

CORROSION ON RT CUSP WEB BS 1184-1200 X -55 TO X -58. THE CUSP WEB WAS REPAIRED.

Part: BEAM — CORRODED (CARGO DOOR FRAME) · corrosion level 2 · airframe 62,222 hrs · 46,077 cycles

CORROSION ON AFT CARGO DOOR FRAME UPPER BEAM FROM BS 1200 - 1212. THE BEAM WAS REPLACED IAW SRM 51-10-3 P. 14-21-26 51- 30-5, 51-10-4 & NDT SPM 04-00-07 PAR 5, FIG 3, SHEET 1 AND 2.

Part: CUSP WEB — CRACKED (BS 800-803) · airframe 62,222 hrs · 46,077 cycles

CRACK ON LEFT CUSP WEB BETWEEN BS 800-803 AND X 54-60 . CUSP WEB WAS REMOVED AND REPLACED IAW, SRM 51-10-3, PAR 14, 21 AND DWG 9930538 REV CF.

Part: CUSP WEB — CORRODED (BS 218) · corrosion level 2 · airframe 62,222 hrs · 46,077 cycles

CORROSION ON CUSP WEB BELOW SEAT TRACK X-54 BS 218. DAMAGE WAS REMOVED, REPAIR FABRICATED, TREATED AND PAINTED, AND INSTALLED IAW SRM 53-05, FIG 131A-17, 51-10-3, PARA 14 AND 21.

Part: DOUBLER — CORRODED (BS 484-503) · corrosion level 2 · airframe 62,222 hrs · 46,077 cycles

CORROSION ON RT REPAIR DOUBLER BS 484-503, X 54-60. REMOVED AND REPLACED IAW SRM 51-30-2, 53-05, FIG 131, A-6, 51-10-3 PARR 21 AND 14.

Part: FLOORBEAM — CRACKED (BS 984) · airframe 62,222 hrs · 46,077 cycles

CRACKED FLOORBEAM BS 984 BETWEEN X 22 TO X -22. REMOVED AND REPLACED IAW 51-30-5, 51-10-4 AND 53-14-3, FIG. 12.

Part: CUSP WEB — CORRODED (BS 1082-1083) · corrosion level 2 · airframe 62,222 hrs · 46,077 cycles

CORROSION ON RT CUSP WEB BS 1082-1083, X -56 TO X -60. REPAIRED IAW SRM 51-10-3 PAR 21,14 53-05, FIG 131-A 13 AND 51-30-5.

Part: CUSP WEB — CORRODED (BS 345-348) · corrosion level 2 · airframe 62,222 hrs · 46,077 cycles

CORROSION FOUND ON RT CUSP WEB, BS 345-348 BETWEEN X -56 TO X -60. DAMAGE WAS REMOVED, REPAIR FABRICATED TREATED PAINTED AND INSTALLED IAW SRM 53-05, FIG 131A-13.

Part: FRAME — CORRODED (BULKHEAD) · corrosion level 2 · airframe 62,222 hrs · 46,077 cycles

CORROSION ON C1 AFT BULKHEAD LOWER FRAME ABOVE LONGERON 27. FRAME WAS REMOVED, CORROSION ON FRAME WAS REMOVED, UT, WAS ACCOMPLISHED. AREA WAS FOUND OUT OF LIMITS. REPAIRED IAW SRM 51-30-2, 51-10-3 PAR 26., 51-10-3 PAR 21, 51-10-3 PAR 14, 51-10-3 PAR 38, AND 53-01.

Part: INTERCOSTAL — CORRODED (BS 1305) · corrosion level 2 · airframe 62,222 hrs · 46,077 cycles

CORROSION ON INTERCOSTAL BS 1305. REPAIRED IAW SRM 51-10-4, 51-10-3, PAR 21,14, SRM 51-30-1, 51-30-2, AND SRM 51-10-3, PAR 38.

Part: SUPPORT — DAMAGED (BS 1231) · airframe 62,222 hrs · 46,077 cycles

SLANT SUPPORT BS 1231 BETWEEN LONGERONS 28LT-29RT DAMAGED. REPLACED SUPPORT IAW SRM 51-103 PAR 26, 21, 14. SRM 51-104, SRM 51-30-2 AND 51-30-5 AND ER/A 413029-14 MA.

Part: CARGO TRACK — CORRODED (BS 1007-1155) · corrosion level 2 · airframe 62,222 hrs · 46,077 cycles

CORROSION ON RT CARGO TRACK UPPER AND LOWER SURFACE FROM BS 1007 - 1155 . CARGO TRACK WAS REMOVED AND REPLACED IAW SRM 51-30-1, 51-30-5, 51-10-4, 51-10-3 PAR 21 AND 14.

Part: FLOOR SUPPORT — DAMAGED (CARGO BAY) · airframe 62,222 hrs · 46,077 cycles

INADEQUATE HOLES ON FLOOR SUPPORT AT BS 218 IN FWD CARGO BAY. REMOVE SUPPORT, NEW SUPPORT WAS TREATED AND PAINTED, SUPPORT WAS INSTALLED IAW SRM 51-30-1, SRM 53-14-1, SRM 51-10-3 PAR. 14 AND 21 SRM 51-30-1.

Part: CUSP WEB — CORRODED (BS 603-605) · corrosion level 2 · airframe 62,222 hrs · 46,077 cycles

CORROSION ON RT CUSP BS 603-605 BETWEEN X -56 TO X -60. DAMAGE REMOVED IAW SRM 53-05, FIG 131A-13. REPAIR FABRICATED IAW SRM 53-05, FIG 131A-13, REPAIR TREATED AND PAINTED IAW SRM 51-10-3 P4 AND 14, AND INSTALLED IAW SRM 51-30-5.

Part: CUSP WEB — CORRODED (BS 591-686) · corrosion level 2 · airframe 62,222 hrs · 46,077 cycles

CORROSION ON LT CUSP WEB BETWEEN BS 591-686 AND X 54 TO X 60. DAMAGE REMOVED AND REPAIRED, IAW SRM 53-05, FIG 131A-13 AND 51-10-3 AND 51-30-2.

Part: SKIN — CRACKED (BS 1380) · airframe 62,222 hrs · 46,077 cycles

CRACKS ON OUTER FUSELAGE SKIN BS 1380 BETWEEN LONGERONS 13-14L. DAMAGE WAS REMOVED IAW SRM 53-04, FIG 18. FILLER AND DOUBLER FABRICATED IAW SRM 53-04, FIG 18, FILLER AND DOUBLER TREATED AND PAINTED IAW SRM 51-10-3, PAR 14 AND 21.

Part: FRAME — CRACKED (BS 256) · airframe 62,222 hrs · 46,077 cycles

CRACK ON UPPER AFT CORNER OF FRAME BS 256 AND LONGERON 11R AT PAX CABIN. REMOVE INTERCOSTAL IAW SRM 51-30-2. STOP CRACK AND FABRICATED REPAIR IAW SRM 53-01, FIG 2, TREATED AND PAINTED REPAIR PARTS IAW SRM 51-10-3, PAR 14, 21 INSTALLED REPAIR IAW SRM 51-30-2 AND INTERCOSTAL WAS INSTALLED IAW SRM 51-30-5. PERFORM VISUAL INSPECTION EACH "L" CHECK IAW TOPP 30-10-70.

Part: LONGERON — CRACKED (BS 1437) · airframe 62,222 hrs · 46,077 cycles

CRACKED IN LONGERON 12L, BS 1437. LONGERON SECTION WAS REMOVED AND REPLACED IAW SRM 51-30-2, 51-30-5, 51-10-4, 53-02, 51-10-3 PAR 14-21.

Part: CUSP WEB — CORRODED (BS 676-682) · airframe 67,375 hrs · 49,778 cycles

CORROSION ON LT PREVIOUS REPAIR DOUBLER OF CUSP WEB BS 676-682 AND X=54 - 60. REMOVED PREVIOUS REPAIR, AND A NEW CUSP WEB REPAIR WAS FABRICATED, TREATED, PAINTED AND INSTALLED.

Part: LONGERON — CRACKED (BS 1437) · airframe 62,222 hrs · 46,077 cycles

CRACKED LONGERON 16 LT AT INTERSECTION WITH BS 1437. LONGERON AND LONGERON ENDS WERE REMOVED, NEW LONGERON WAS DRILLED AND ADJUSTED, TREATED, PAINTED, AND INSTALLED IAW SRM 51-30-2, 51-30-5, 51-10-4, AND 51-10-3 PAR 14 AND 21.

Part: ANGLE — CRACKED (VERTICAL STAB) · airframe 62,222 hrs · 46,077 cycles

CRACKED LT/RT ANGLES FWD UPPER SECTION STA YV=170 AT VERTICAL STABILIZER TIP FAIRING. CLIPS 2EA WERE REMOVED FABRICATED, TREATED, PAINTED, AND INSTALLED IAW SRM 51-10-3, DWG 9911962.

Part: INTERCOSTAL — WORN (BS 769-788) · airframe 62,222 hrs · 46,077 cycles

WORN INTERCOSTAL BS 769 - 788 X 0. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-10-2, SRM 51-10-4, SRM 51-10-3, PAR 21, 14, AND SRM 51-30-2.

Part: PAN — CRACKED (WINDOW) · airframe 62,222 hrs · 46,077 cycles

CRACK ON LOWER AFT CORNER, BS 731-750. ALSO, UPPER AFT CORNER BS 465-484 AT LT WINDOW RING PAN. RING PAN REPAIRED IAW SRM 53-05, FIG 122 51-10-3, 51-30-5, 51-30-2 AND ER/A 493648-14 MA REV ORIG AND ER/A 487797-14 MA REV ORIG.

Part: CUSP WEB — DAMAGED (BS 313) · airframe 62,222 hrs · 46,077 cycles

LT CUSP WEB BS 313 X 49 DAMAGED. DAMAGE REMOVED, REPAIR PARTS FABRICATED, TREATED AND INSTALLED IAW SRM 51-10-3, 51-30-2 AND 53-05 FIG 131A.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 62,222 hrs · 46,077 cycles

CORROSION ON SETTLEMENT AREA AT FUEL TANK ACCESS PANEL. ACCESS PANEL REPLACED IAW SRM 51-22-2A, CONDITION III

Part: SEAT TRACK — CORRODED (BS 484-580) · corrosion level 2 · airframe 62,222 hrs · 46,077 cycles

CORROSION ON SEAT TRACK BETWEEN BS 484 - 580. REPAIRED IAW SRM 51-30-1, 53-05, FIG 41, 51-10-3 P21-14 AND 51-30-5.

Part: LOCK — BROKEN (TAILCONE) · airframe 62,180 hrs · 46,042 cycles

DURING CHECK, MAINTENANCE FOUND THE TAILCONE UPPER LT ATTACH LATCH LOCK WAS BROKEN. MAINTENANCE R & R THE LATCH AND A FUNCTIONAL TEST WAS PERFORMED.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 61,190 hrs · 45,365 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE OVERHEAD EMERGENCY PATHWAY LIGHTING AT DOOR 2L AND AFT. ALSO AT SEATS 11-15 WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACKS FOR THE NOTED LIGHTED AREAS AND THE OPS CHECK WAS GOOD.

Part: ADC — FAILED · airframe 60,300 hrs · 44,721 cycles

DURING CRUISE, DECLARED AN EMERGENCY, AFTER LOSING BOTH NR 1 & 2 AIR DATA SYSTEMS. INITIALLY RECEIVED MACH TRIM INOPERATIVE LIGHT FOLLOWED BY DUAL AUTOTHROTTLE AND AUTOPILOT DISENGAGEMENT. CAPTAIN`S & F/O`S AIRSPEED INDICATIONS SUBSEQUENTLY BECAME UNRELIABLE. LANDED SAFELY USING STANDBY INSTRUMENTS ONLY. MX REPLACED BOTH AIR DATA COMPUTERS IAW AMM 34-16-01 AND ALSO REPLACED THE RAT PROBE IAW AMM 34-1 WITH ALL SUBSEQUENT CHECKS OK. A VERIFICATION FLIGHT WAS PERFORMED AFTER MAINTENANCE. THE ACFT WAS RETURNED TO SERVICE.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHTS) · airframe 59,523 hrs · 44,154 cycles

DURING ROUTINE LINE CHECK, THE EMERGENCY ESCAPE PATH LIGHT AT ROW 14D WAS NOTED TO BE INOPERATIVE. A LOOSE CONNECTOR WAS RESECURED AND OPERATION CHECKED NORMALLY.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 59,523 hrs · 44,154 cycles

DURING ROUTINE LINE INSPECTION, AN EMERGENCY PATH LIGHT CLEAR LENS WAS NOTED TO BE MISSING AT ROW 15D. THE LENS WAS REPLACED.

Part: ATTACH BRACKET — WORN (TAIL CONE) · airframe 59,027 hrs · 43,827 cycles

MX DISCOVERED THAT BOTH OF THE TAILCONE ATTACH BRACKETS ARE WORN FROM THE SPRING. THE BRACKETS WERE REPLACED AND THE SYSTEM WAS RIGGED TO SPECIFICATIONS. THE RII STEPS WERE COMPLETED AND THE FUNCTIONAL CHECK WAS COMPLETED SATISFACTORILY.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 58,934 hrs · 43,758 cycles

DURING LINE CHECK, BOTH AFT OVERWING EXIT SIGNS WERE NOTED TO BE INOPERATIVE. THE BATTERY PACK WAS FOUND TO BE DISCHARGED AND WOULD NOT ACCEPT A CHARGE. THE BATTERY PACK WAS REPLACED IAW AMM 33-51, AD OPS CHECKED GOOD.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 58,787 hrs · 43,656 cycles

DURING A SCHEDULED MAINTENANCE CHECK, THE EMERGENCY LIGHTS IN THE AFT VENTRAL STAIR (CATWALK) AREA WERE FOUND TO BE INOPERATIVE. THE BATTERIES FOR THE AFT EMERGENCY LIGHTS WERE REPLACED IAW AMM 33-51 AND THE SYS OPS CHECKED GOOD.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHT) · airframe 58,581 hrs · 43,488 cycles

DURING OVERNIGHT MX, THE FWD OVERWING EMERGENCY EXIT SIGNS ABOVE THE LT AND RT DOORS WERE FOUND TO BE INOPERATIVE. THE BATTERIES WERE FOUND TO BE DISCHARGED AND WERE REPLACED IAW AMM 33-50 AND THE EMERGENCY LIGHT OPS CHECKED GOOD.

Part: FORMER — CRACKED (LT WING) · airframe 58,224 hrs · 43,258 cycles

LEFT WING L/E FORMER CRACKED AT XFS 70.812. CUT AND REMOVED PORTION OF EXISTING DOUBLER. FABRICATED NEW DOUBLER, DRILLED, AND INSTALLED DOUBLER AND TRIPLER IAW SRM 57-06B (378175).

Part: DUCT — CONTAMINATED (APU BLEED) · airframe 56,907 hrs · 42,339 cycles

ON TAKEOFF, CABIN CREW NOTIFIED FLIGHT CREW OF A BURNING ODOR IN THE CABIN. FLIGHT CREW THEN PERFORMED AN UNEVENTFUL AIR TURN BACK. ON INSPECTION, MAINTENANCE FOUND OIL IN THE APU BLEED DUCT. MAINTENANCE PERFORMED A DUCT BURN OUT AND RETURNED THE AIRCRAFT TO SERVICE.

Part: OIL SYSTEM — LEAKING (APU) · airframe 56,907 hrs · 42,339 cycles

DURING TAKEOFF, FLIGHT CREW NOTED A BURNING OIL ODOR FROM THE PACKS. FUMES DISSIPATED AND THE FLIGHT LANDED UNEVENTFULLY AT DESTINATION. ON INSPECTION, MAINTENANCE FOUND OIL LEAKING FROM THE APU. PERFORMED A DUCT BURNOUT AND RETURNED THE AIRCRAFT TO SERVICE.

Part: SKIN — DAMAGED (VERTICAL STAB) · airframe 55,404 hrs · 41,319 cycles

VERTICAL STABILIZER RT SIDE EXTERIOR SKIN DAMAGED AT SCREW HOLE ONE FASTENER ABOVE ZFS 52.267. NOTE: DAMAGE ON REMOVABLE LEADING EDGE SECTION P/N 5930610-3.

Part: SKIN — DAMAGED (VERTICAL STAB) · airframe 55,404 hrs · 41,319 cycles

DURING PSV VISIT IN MSP FOUND ELONGATED HOLE WHILE PERFORM ACJIC 0401. DAMAGED HOLE FOUND ON RIGHT SIDE OF THE VERTICAL STAB FRONT SPAR CHORD JUST ABOVE ZFS=52.267. DAMAGE REPAIRED PER ER/A 498509-14AD. WORKED ON NRC 89.

Part: SKIN — DAMAGED (VERTICAL STAB) · airframe 55,404 hrs · 41,319 cycles

VERTICAL STAB LF SIDE EXTERIOR SKIN DAMAGE AT SCREW HOLE 3 FASTENER BELOW ZFS 52.267. NOTE: DAMAGE ON STABILIZER ROOT SECTION BELOW REMOVABLE LEADING EDGE.

Part: SKIN — DAMAGED (VERTICAL STAB) · airframe 55,404 hrs · 41,319 cycles

DURING PSV VISIT IN MSP FOUND VERTICAL LEADING EDGE FASTENER HOLE OUT OF LIMITS PER ACJIC 0401. ELONGATED HOLE IS ON A/C LEFT SIDE FRONT SPAR CHORD 3 FASTENERS BELOW ZFS=52.267. THIS IS REPAIRED PER ER/A 498510-14AD. WORKED ON NRC 90.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 55,404 hrs · 41,319 cycles

LEFT OUTBOARD FLOOR TRACK CORROSION STA 196 TO STA 256 LBL 44. REPAIRED IAW MD88 SRM 53-05 FIG 4F AND ERA 498618-14 REV ORIGINAL.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 55,404 hrs · 41,319 cycles

DURING PSV VISIT MSP, MTC FOUND A CRACK ALONG FWD LAV PANEL CUTOUT. REPAIR PANEL PER ERA 497806-14, ON N/R 42.

Part: RELEASE SYSTEM — MALFUNCTIONED (TAILCONE) · airframe 55,404 hrs · 41,319 cycles

EMERGENCY EXIT TAIL CONE FAILED TO DROP DURING OPN 6908AD FUNCTIONAL CHECK OF TAIL CONE RELEASE SYSTEM COMPLIANCE CHECK IN MSP. TAIL CONE WAS REPAIRED PER NRC 60 AND 61.

Part: FUSE — BLOWN (BATTERY HOLDER) · airframe 53,716 hrs · 40,055 cycles

DURING A SERVICE CHECK, MAINTENANCE FOUND L1 & R1 EXIT LIGHTS, ROWS 1-4, AND ROWS 10-12 EMERGENCY LIGHTS TO BE INOPERATIVE. MAINTENANCE REPLACED FUSE IN BATTERY HOLDER IN OVERHEAD ROW 3 AND NOW THE OPERATION OF LIGHTS CHECKS GOOD.

Part: LIGHT — INOPERATIVE (SEAT 3C) · airframe 51,865 hrs · 38,831 cycles

MX FOUND THE EMERGENCY LIGHT AT SEAT 3C TO BE INOPERATIVE. MX REPLACED THE LIGHT ASSY. AN OPS CHECK WAS PERFORMED AND THE ACFT WAS RETURNED TO SERVICE.

Part: FUSE — BLOWN (EMERGENCY LIGHTS) · airframe 50,796 hrs · 38,091 cycles

SEAT MOUNTED EMERGENCY ESCAPE LIGHT AT 4CD DAMAGED. REPLACED SEAT MOUNTED LIGHT ASSY WHEN PERFORMING OPS CK. FOUND ALL SEAT MOUNTED LIGHTS FROM ROW 1-12 INOP. T/S FOUND BLOWN FUSES IN BATTERY PACK. REPLACED FUSES NOW ALL LIGHTS, OPS CK NML.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 48,101 hrs · 36,364 cycles

DURING TEST EMERGENCY OVERWING LIGHTS FOUND BURNED. REPLACED BATTERY PACK BOX PER MM 33-53-00-401.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 48,101 hrs · 36,364 cycles

EXFOLIATION CORROSION ON LWR DOOR JAMB BTW STA Y=636 TO 693 REPAIRED PER SRM 53-05D FIG 123.

Part: DOOR FRAME — CORRODED (CARGO DOORWAY) · airframe 48,101 hrs · 36,364 cycles

EXFOLIATION CORROSION ON LOWER DOOR JAMB BTW STA Y=370 TO 427 AT FWD CARGO COMPARTMENT. REPAIRED PER SRM 53-05D FIG 804D.

Part: DOOR FRAME — CORRODED (CARGO DOORWAY) · airframe 48,101 hrs · 36,364 cycles

EXFOLIATION CORROSION ON LWR BEAM BTW STA Y-1155 TO 1212 AT AFT CARGO COMPARTMENT DOOR JAMB. CORROSION REMOVED PER 51-10-3. BLENDED OUT OF LIMITS, SRM 53-05 FIG 123. DAMAGED AREA REMOVED SRM 53-05 FIG 123 SHEET 5.

Part: FRAME — CRACKED (BS 1437) · airframe 48,101 hrs · 36,364 cycles

CRACKED UPPER CAPS (2 EACH) ON FRAME 1437 BETWEEN LONGERON 2 RT AND 2 LT, NRC T0121147. CAPS WERE REMOVED. DOUBLERS WERE FABRICATED. REPAIR ANGLES WERE FABRICATED ERA 472134-14.

Part: SKIN — DENTED (AFT OF L1 DOOR) · airframe 48,101 hrs · 36,364 cycles

DENT AFT OF L-1 DOOR 19 INCHES AFT AND 12 INCHES FROM FLOOR LEVEL. REPAIRED PER SRM 53-04D FIG 12B.

Part: PAN — CRACKED (C1 DOOR) · airframe 48,101 hrs · 36,364 cycles

CRACKED FWD INNER PAN BELOW STOP BRACKET AND BEAM NR 2 AT C1 DOOR. REPAIRED PER SRM 52-05D FIG 50.

Part: PAN — CRACKED (C1 DOOR) · airframe 48,101 hrs · 36,364 cycles

CRACKED AFT INNER PAN BELOW STOP BRACKET AND BEAM NR 3 AT C1 DOOR. REPAIRED PER SRM 52-05 FIG 50.

Part: PAN — CRACKED (CARGO DOOR) · airframe 48,101 hrs · 36,364 cycles

CRACKED FWD INNER PAN BELOW STOP BRACKET AND BEAM NR 2 AT C1 DOOR. REPAIRED PER SRM 52-05D FIG 50.

Part: DOOR FRAME — CORRODED (CARGO DOORWAY) · airframe 48,101 hrs · 36,364 cycles

EXFOLIATION CORRROSION ON LWR DOOR JAMB BRW STA Y636 TO 693 NRC T0120749 HMV. REPAIRED PER SRM 53-05 FIG 123.

Part: FRAME — CRACKED (BS 1437) · airframe 48,101 hrs · 36,364 cycles

THE FS 1437 UPPER FRAME BETWEEN LONGERON 1 AND 3R WAS FOUND CRACKED IN THE INNER AND OUTER CAPS AND THE WEB, APPROXIMATELY 3.75 INCH. THE WEB WAS REPLACED. THE TWO CAPS HAD THE DAMAGE CUTOUT, AND REPAIR ANGLES WERE INSTALLED.

Part: SKIN — CRACKED (BS 1437) · airframe 48,101 hrs · 36,364 cycles

CRACK ON FUSELAGE SKIN STA Y=1437 BTW LONGERON 3L AND 4L. REPAIRED PER SRM 53-04D FIG 27.

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,101 hrs · 36,364 cycles

TWO CRACKS ON FUSELAGE SKIN STA Y=172 AND STA Y=175. REPAIRED PER SRM 53-05D FIG 112.

Part: CONTROL CABLE — BROKEN (TAIL CONE) · airframe 48,101 hrs · 36,364 cycles

BROKEN CONTROL CABLE ASSY OF RELEASE HANDLE TO JETTISON TAIL CONE, REPLACED CABLE.

Part: ENGINE — MALFUNCTIONED (NR 2) · airframe 46,283 hrs · 35,098 cycles

TAKEOFF DISCONTINUED AT 100KTS BECAUSE EPR WOULD NOT RISE ABOVE 1.68 AND N1 BEGAN TO FLASH AT 102 PERCENT. REMOVED AND REPLACED NR 2 ENG EPR TRANS AND SNUBBER PER MM. COMPLETE THRU 77-11-02-201 ST 3.B.11 984600. C/W EPR IND SYS OPR NR 2 ENG PER AMM. CKS NORMAL.

Part: AMPLIFIER — MALFUNCTIONED (FIRE DETECTION) · airframe 38,811 hrs · 29,990 cycles

ENGINE FIRE DETECTION SYSTEM RIGHT ENGINE LOOP-B LIGHT AND FIRE WARNING ON IN FLIGHT MOMENTARILY, THEN WENT OFF. BOTH INDICATIONS AGAIN ON THE GROUND BOTH WITH ENGINE RUNNING AND AFTER ENGINE SHUT DOWN. TESTED FIRE WARNING. FOUND NR 2 ENGINE B-LOOP STICKING IN TEST WITH FIRE INDICATION. REPLACED A2-6 RIGHT FIRE DETECT AMP (CONTROL). TESTED FIRE WARNING SEVERAL TIMES. OPS TEST NORMAL ON B-LOOP NR 2 ENGINE. A-LOOP NR 2 ENGINE STILL ON MCO AND PLACARD.

Part: AMPLIFIER — FAILED (FIRE DETECTION) · airframe 38,811 hrs · 29,990 cycles

NR 2 ENGINE FIRE WARNING CAME ON INTERMITTENTLY, ON AND OFF INCLUDING FIRE BELL/ B-LOOP LIGHT / VOICE / HANDLE LIGHT. A-LOOP WAS ON MCO. REPLACED A2-6 FIRE DETECTOR AMP. OPS GOOD ON B-LOOP.

Part: SWITCH — SHORTED (COCKPIT) · airframe 33,044 hrs · 25,988 cycles

AT APPROXIMATE TIME OF WING LANDING LIGHT ACTIVATION THERE WAS A FAINT ELEC ODOR AND SMALL AMOUNT OF SMOKE. ODOR AND SMOKE DISSIPATED AFTER SWITCHES TURNED OFF. REPLACED LT WING LANDING LIGHT SWITCH. FOUND SIGN OF ARCING ON ONE OF THE TERMINALS.

Part: BATTERY PACK — INOPERATIVE (LT & RT OVERWING) · airframe 32,267 hrs · 25,429 cycles

LT AND RT AFT EMERGENCY OVERWING LIGHTS INOPERATIVE. REPLACED BATTERY PACK OPS NORMAL.

Part: PUMP — FAILED (NR 1 ENGINE) · airframe 30,059 hrs · 23,771 cycles

LEFT SYS HYD FAILURE AT FLT 290 WITH 19 QT OF FLUID AT ZERO PRESSURE. ATTEMPT TO RESTORE HYD POWER AS PER POM WITH AUX PUMP ON AND TRANSFER PUMP ON IN FLT AND STILL HAD NO PRESSURE IN THE LEFT SIDE. REPLACED LEFT ENGINE HYD PUMP. ALSO, REPLACED ALL FILTERS.

Part: OXYGEN MASK — WILL NOT TEST (COCKPIT) · airframe 29,773 hrs · 23,540 cycles

CAPT'S O2 MASK WON'T TEST. REPLACED CAPT'S O2 MASK.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 29,699 hrs · 23,476 cycles

FLT ATTENDANT FLASHLIGHT MID-CABIN INOP. REPLACED FLASHLIGHT.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 28,046 hrs · 22,241 cycles

PWR SUPPLY WILL NOT LIGHT LIGHTS/F1 AND F2 OPEN. REPLACED PWR SUPPLY.

Part: FAN — FAILED (RECIRCULATION) · airframe 26,962 hrs · 21,446 cycles

A/C DIVERTERD TO IAD DUE TO FUMES IN CABIN THAT WERE BELIEVED TO BE ELECTRICAL. ON ARRIVAL THE CABIN RECIRC FAN C/BS WERE FOUND POPPED. REPLACED RECIRC FAN.

Part: VALVE — LOOSE (RIGHT) · airframe 25,410 hrs · 20,259 cycles

IN FLIGHT RIGHT HYDRAULIC QTY READ 3 QTS. COMPLIED WITH POM, CONTINUED, DECREASE TO 1 QT. FOUND FITTING ON FWD I/B SIDE OF IBCV LOOSE. TIGHTEN SAME, SERVICED RIGHT HYDRAULICS SYSTEM. NO LEAKS.

Part: WIRE — DAMAGED (R1 GALLEY)

EMERGENCY LIGHTS INOP AT FWD GALLEY. FOUND WIRE PULLED FROM SPLICE UNDER CARPET. RETERMINATED WIRE. CKS GOOD.

Part: HINGE FITTING — CORROSION (RT SPOILER)

THE RIGHT HAND SIDE I/B SPOILER HINGE FITTING WAS FOUND TO HAVE CORROSION LOCATED IN THE BORE THAT ACCEPTS ASBY10-18 BEARING. THE HOLE WILL BE OVERSIZED AND A BUSHING INSTALLED TO RETURN THE HOLE TO B/P DIAMETER. THEN THE BEARING WILL BE REINSTALLED. THE HOLE WAS OVERSIZED TO A FINAL DIA OF 1.250. REPAIRED PER ERA 330604-14.

Part: SKIN — DENTED (BS 351)

THE FUSELAGE SKIN AT L-21R AND FS 351 IS DENTED. THE DENT MEASURES 0.030 IN DEPTH AT THE DEEPEST POINT, 1.5 IN WIDTH AND 16 IN LENGTH. THE DENT WAS INSPECTED FOR CRACKS, NONE WERE FOUND. THIS DENT IS CONSIDERED ALLOWABLE DAMAGE AND APPROVED PER FAA/ DER FORM 8110-3, DER DESIGNATION SO-775.

Part: SKIN — CORROSION (BS 806)

CORROSION WAS FOUND UNDER THE RIGHT RUB STRIP AT FS 806 BETWEEN STR 27R AND 29R. THE RUB STRIP IS LOCATED WHERE THE WING TO BODY FAIRING MEETS THE FUSELAGE. THE DEPTH OF THE BLEND IS 0.036 IN A .5 DIAMETER AREA. REPAIRED PER ERA 330567-14.

Part: FRAME — CRACKED (BS 1418)

MAINTENANCE FOUND AN APPROX .5 INCH CRACK AT STA 1418, AT STR-2L AT THE TYPICAL LOCATION COVERED BY EO 9-63538-3. THIS AIRCRAFT WAS NOT INCLUDED BY THIS EO. HOWEVER, THIS EO WILL BE ACCOMPLISHED ON THIS AIRCRAFT AS A PREVENTATIVE MEASURE. THIS REPAIR WAS APPROVED BY FAA/DER FORM 8110-3, DER DESIGNATION NM-2145, DTD 8-7-97. REPAIRED PER ERA 330564-14.

Part: COMPRESSOR — STALLED (NR 2 ENGINE)

AT FL 300, NR 2 ENGINE COMPRESSOR STALLED. RETURNED TO ATL. FAILED BORESCOPE, REPLACED ENGINE. ENGINE TOTAL CYCLES, 16,082.

Part: SKIN — CORROSION (BS 598)

THE INNER SURFACE OF THE FUSELAGE SKIN AT STA 598 AND STR 29R WAS FOUND CORRODED BETWEEN THE UNDERLYING C2 DOOR CUTOUT DOUBLER. ACCOMPLISHED REPAIRS PER DL 271817-14.