N935F

Part: SKIN — MISREPAIRED (FUSELAGE)

MZJ - PREVIOUS FUSE SKIN PANEL REPAIR AT FS 133.425 NOT PER SRM 53-04, FIG 12B, SHEET 2. ALSO HAS NUMEROUS GOUGES IN REPAIR. REPAIRED PER ECRA 935-53-048-2 REV A AND SRM 53-04 FIG 12B. (M)

Part: FASTENER — DAMAGED (ELEVATOR)

MZJ - FASTENER HEAD COMING OFF/BENDING BACK, LOWER SIDE OF RIGHT ELEVATOR 23.5 INCH INBOARD OF OUTBOARD TIP. REPAIRED PER ECRA 935-55-047-2. (M)

Part: OIL SYTEM — LEAKING (NR 2 ENGINE)

IN FLIGHT, NR 2 ENGINE OIL QTY DECREASED TO 0 DURING CRUISE, DIVERTED TO KCPR. AFTER LANDING FOUND OIL LEAKING FROM COWLING. (M)

Part: STRIKER — FAILED (LANDING GEAR)

ABQ - AFTER TAKEOFF FROM PHX, LANDING GEAR UP, LEFT GEAR UNSAFE LIGHT ON, PERFORMED ABNORMAL CHECKLIST AND LIGHT REMAINED ON. REPLACED STRIKER FOR GEAR LIGHT, OPERATIONALLY CHECKED GOOD PER MM 32-31-4. (M)

Part: SPLICE — CORRODED (BS 794-813)

PHX - DURING C-CHECK, LOWER AFT CARGO BAY, LONGERON 30 SPLICE HAS CORROSION FROM FS 794 TO 813. (M)

Part: FLOORBEAM — CORRODED (BS 756)

PHX - DURING C-CHECK, MAIN CABIN FLOORBEAM HAS CORROSION AT FS 756 LEFT SIDE AND INTERCOSTAL FS 737-756 LBL 56 HAS CORROSION. (M)

Part: INTERCOSTAL — CORRODED (BS 737-755)

PHX - DURING C-CHECK, MAIN CABIN FLOORBEAM HAS CORROSION AT FS 756 LEFT SIDE AND INTERCOSTAL FS 737-756 LBL 56 HAS CORROSION. NRC W129. (M)

Part: LONGERON — CORRODED (BS 996-1080)

PHX - DURING C-CHECK, LONGERON 25L HAS CORROSION FROM FS 996-1080. REPAIRED PER SRM 53-11-4. (M)

Part: PAN — DAMAGED (BS 341)

PHX - DURING C-CHECK, LOWER CARGO DOOR OUTER PAN FS 341 WAS FOUND DAMAGED. NRC H051. REPAIRED PER SRM 52-05 FIG 50. (M)

Part: FRAME — DAMAGED (BS 439)

PHX - DURING C-CHECK, FUSELAGE FRAME AT FS 439, LBL 18 HAS TOOLING MARKS. NRC W344. REPAIRED PER SRM 53-01, EA DC9-53-202 AND ECRA 935-51-038-1. (M)

Part: FRAME — DAMAGED (BS 313)

PHX - DURING C-CHECK, MAIN DECK CARGO DOOR FRAME FS 313 APPROX 36 INCHES ABOVE FLOOR LEVEL HAS DAMAGE. REPAIRED PER SRM 53-01 AND 51-30. (M)

Part: FRAME — CRACKED (BS 737)

PHX - DURING C-CHECK, FUSELAGE FRAME FS 737 HAS A CRACK AT LONGERON 17L. REPAIRED PER SB 53-131. (M)

Part: FRAME — GOUGED (BS 303)

PHX - DURING C-CHECK, FUSELAGE FRAME AT FS 303, LONGERON 18L HAS GOUGE. NRC W342. REPAIRED PER SRM 53-01, EA DC9-53-203 AND ECRA 935-51-038-1. (M)

Part: LONGERON — DAMAGED (BS 455)

PHX - DURING C-CHECK, LONGERON S24L AND 25L WERE FOUND TO HAVE DAMAGE AT FS 455. REPAIRED PER SRM 53-02 FIG 18, EA DC9-53-207 AND ECRA 935-51-038-1. (M)

Part: LONGERON — CRACKED (BS 965)

PHX - DURING C-CHECK, LONGERON 13R IS CRACKED AT FS 965. REPAIRED PER SRM 53-02 FIG 18. (M)

Part: WEB — MISREPAIRED (BS 515)

PHX - DURING C-CHECK, MAIN CABIN CUSP WEB AT FS 515 LBL 56 WAS FOUND TO HAVE AN IMPROPER REPAIR INSTALLED PER SRM. REPAIRED PER SRM 53-01 FIG 4. (M)

Part: LONGERON — CORRODED (BS 1006)

PHX - DURING C-CHECK, LONGERON 23L HAS CORROSION FROM FS 1006. REPAIRED PER SRM 53-02 FIG 18. (M)

Part: BEAM — CORRODED (BS 50)

PHX - DURING C-CHECK, RIGHT NOSE GEAR SUPPORT BEAM AT FS 50 HAS CORROSION NRC E045. REPAIRED PER EA DC9-53-188 AND ECRA 935-51-038-1. (M)

Part: SPLICE — CORRODED (BS 945)

PHX - DURING C-CHECK, FUSELAGE FRAME SPLICE AT FS 945 LONGERON 28L TO 30 HAS CORROSION. REPAIRED PER SRM 53-11-3 FIG 3A. (M)

Part: JAMB — DAMAGED (CARGO DOORWAY)

PHX - DURING C-CHECK, MAIN DECK CARGO DOOR CUTOUT, UPPER FORWARD CORNER WAS FOUND DAMAGED. THE PIN AND RETAINER REQUIRED BY AD 89-11-02 R1 AND SB 52-170, REQUIRED MODIFICATION/DEVIATION. ACCOMPLISHED DEVIATIONS PER EA DC9-53-190 AND DC9-53-204, ECRA 935-51-038-1. (M)

Part: SKIN — CRACKED (RUDDER)

PHX - DURING C-CHECK, RUDDER LEADING EDGE SKIN WAS FOUND CRACKED AT ZR 95.2. NRC N074. REPAIRED PER EA DC9-55-009 AND ECRA 935-51-038-1. (M)

Part: SKIN — DAMAGED (RUDDER)

PHX - DURING C-CHECK, RUDDER SKIN AT TRAILING EDGE WAS FOUND DAMAGED. NRC N102. REPAIRED PER SRM 55-40-1. (M)

Part: LONGERON — DAMAGED (BS 455)

PHX - DURING C-CHECK, LONGERON S24L AND 25L WERE FOUND TO HAVE DAMAGE AT FS 455. REPAIRED PER SRM 53-02 FIG 18, EA DC9-53-207 AND ECRA 935-51-038-1. (M)

Part: LONGERON — CRACKED (BS 965)

PHX - DURING C-CHECK, LONGERON 6R IS CRACKED AT FS 965. REPAIRED PER SRM 53-02 FIG 18. (M)

Part: SKIN — CRACKED (BS 301)

PHX - DURING C-CHECK, FUSELAGE SKIN AT FS 301 WAS FOUND CRACKED, AT THE LOWER AFT CORNER OF THE MAIN DECK CARGO DOOR. REPAIRED PER SRM 53-05 FIG 103. (M)

Part: SPAR — CRACKED (WS 267)

PHX - DURING C-CHECK, LEFT WING AFT SPAR UPPER CHORD XRS 267 AT NR 3 FLAP HINGE HAS A CRACK. REPAIRED PER EA DC9-57-135 AND SERVICE BULLETIN 57-179 REV 1, DRWG JO60272 AND ECRA 935-51-038-1. (M)

Part: SKIN — CRACKED (BS 995)

PHX - DURING C-CHECK, FUSELAGE SKIN CRACKED AT LEFT PYLON FS 995. NRC P157. REPAIRED PER SRM 53-04 FIG 17A. (M)

Part: SILL — CORRODED (CARGO DOOR)

PHX - DURING C-CHECK, MAIN DECK CARGO DOOR LOWER SILL PLATE HAS CORROSION, NRC W338. REPAIRED PER SRM EA DC9-53-198 AND ECRA 935-51-038-1. (M)

Part: FRAME — DAMAGED (CARGO DOOR)

PHX - DURING C-CHECK, MAIN DECK CARGO DOOR LOWER FORWARD CORNER FRAME WEB HAS DAMAGE. REPAIRED PER SRM 51-10-2. (M)

Part: SPAR — CRACKED (RT WING)

PHX - DURING C-CHECK, RIGHT WING AFT SPAR UPPER CHORD AT NR 3 FLAP HINGE HAS A CRACK. REPAIRED PER EA DC9-57-135 AND SERVICE BULLETIN 57-179 REV 1, DRWG J060272 AND ECRA 935-51-038-1. (M)

Part: SUPPORT — DAMAGED (BS 180)

PHX - DURING C-CHECK, MAIN CABIN FLOOR SUPPORT 'T' FITTING AT FS 180 FROM RBL 24-44 DAMAGE WAS FOUND. REPAIRED BY REPLACEMENT OF 'T' SECTION PER SRM 53-11-1 FIG 16. (M)

Part: LONGERON — CORRODED (BS 996-1033)

PHX - DURING C-CHECK, LONGERON 24L HAS CORROSION FROM FS 996-1033. REPAIRED PER SRM 51-11-4 FIG 6 AND FIG 18. (M)

Part: SKIN — CRACKED (RUDDER)

PHX - DURING C-CHECK, RUDDER SKIN AT RIGHT RIB NR 4 WAS FOUND CRACKED. REPAIRED PER SRM 55-03 FIG 11. (M)

Part: BLKHD STIFFENER — CRACKED (AFT PRESS BLKHD)

PHX - DURING C-CHECK, AFT RPESSURE BULKHEAD AFT SIDE HAS A CRACKED STIFFENER AT 4 O'CLOCK AND 5 O'CLOCK POSITIONS. REPAIRED PER SRM 53-11-3. (M)

Part: SPAR — CORRODED (VERT STAB)

PHX - DURING C-CHECK, VERTICAL STABILIZER REAR SPAR LEFT AND RIGHT AFT CHORD HAS CORROSION FROM ZRS .5 TO ZRS154. OUT OF LIMITS AT ZRS 112. NRC N062, N063. REPAIRED PER EA DC9-55-013 AND ECRA 935-51-038-1. (M)

Part: SPAR — CRACKED (WS 84)

PHX - DURING C-CHECK, FOUND CRACK IN LEFT WING FORWARD SPAR UPPER CHORD AT XIS 84.5. NRC A182. REPAIRED PER, EA DC9-57-140 AND ECRA 935-51-038-1. (M)

Part: SKIN — DENTED (BS 965-980)

PHX - DURING C-CHECK, FUSELAGE SKIN HAS DENT FROM FS 965-980 AT LONGERON 22R NRC F024, F078, F080. REPAIRED PER EA DC9-53-183, SRM 53-04 FIG 12B, SRM 53-02 FIG 18 AND ECRA 935-51-038-1. (M)

Part: WEB — CORRODED (BS 727-756)

PHX - DURING C-CHECK, MLG FLOOR WEB AT FS 727-756 LBL 5-10 HAS CORROSION NRC W395. REPAIRED PER SRM 53-10, 51-10-3, 51-30-0 AND EA DC9-53-197 AND ECRA 935-51-038-1. (M)

Part: FLOORBEAM — CORRODED (BS 218)

PHX - DURING C-CHECK, MAIN CABIN FLOORBEAM HAS CORROSION AT FS 218 AND RBL 47. NRC V120. REPAIRED PER EA DC9-53-200 AND ECRA 935-51-038-1. (M)

Part: FLOORBEAM — CORRODED (BS 200)

PHX - DURING C-CHECK, MAIN CABIN FLOORBEAM HAS CORROSION AT FS 200 AND RBL 44. NRC V118. REPAIRED PER EA DC9-53-199 AND ECRA 935-51-038-1. (M)

Part: FITTING — MISLOCATED (FWD DOOR)

PHX - DURNG C-CHECK, FORWARD SERVICE DOOR HINGE MOUNT FITTING OBSTRUCTS DOOR RIGGING. NRC V113. REPAIRED PER, EA DC9-52-010 AND ECRA 935-51-038-1. (M)

Part: SKIN — DAMAGED (RT TE FLAP)

PHX - DURING C-CHECK, RIGHT INBOARD TRAILING EDGE FLAP LEADING EDGE SKIN HAS DAMAGE AT XFLS 60 AND 105. REPAIRED PER EA DC9-57-137 AND ECRA 935-51-038-1. (M)

Part: FLOORBOARD — CRACKED (BS 180-1037)

PHX - DURING C-CHECK, MAIN CABIN FLOORBOARDS FROM FS 180-1037, NUMEROUS SPOTS OF CORROSION, CRACKS AND GOUGES WERE FOUND. NRC W039, W046, W058, W074, W076, W086, W155, W291, W298, W317, W329, W424, V049, W508, W337, W466, W502, W168. MANY REPAIRED FLOOR PANELS WERE COVERED BY SRM CHAPTER 51 GENERAL REPAIRS. ADDITIONALLY EA DC9-53-206 WAS GENERATED FOR SPECIFIC REPAIRS NOT COVERED BY SRM ECRA 935-51-038-1. (M)

Part: FRAME — DAMAGED (BS 446)

PHX - DURING C-CHECK, FUSELAGE FRAME AT FS 446 AT LONGERON 18L HAS TOOLING DAMAGE NRC W343. REPAIRED PER EA DC9-53-195 AND ECRA 935-51-038-1. (M)

Part: SKIN — CRACKED (RUDDER)

PHX - DURING C-CHECK, RUDDER LOWER EDGE OF SKIN WAS FOUND CRACKED. NRC N074. REPAIRED PER EA DC9-55-010 AND ECRA 935-51-038-1. (M)

Part: SKIN — CHAFED (BS 937)

PHX - DURING C-CHECK, FUSELAGE SKIN AT RIGHT PYLON LEADING EDGE HAS CHAFE MARKS, FS 937 LONGERON 15R. REPAIRED PER SRM 53-04 FIG 3A. (M)

Part: FRAME — CRACKED (BS 756)

PHX - DURING C-CHECK, FUSELAGE FRAME FS 756 HAS A CRACK AT THE LEFT SIDE AND RIGHT. REPAIRED PER SB 53-168. (M)

Part: SEAT TRACK — CORRODED (BS 180-989)

PHX - DURING C-CHECK, MAIN CABIN FLOOR SEAT TRACKS FROM FS 180-989, NUMEROUS SPOTS OF CORROSION ON SPLICE FITTINGS WERE FOUND, FS 180-227 RBL 24 W473, FS 180-227 LBL 44 V091, FS 218-230 RBL 45 V089, FS 218-230 LBL 45, FS 218-513 LBL 37 W095, FS 223-435 BL 0 W073, FS 237-481 LBL 0-16 V099, FS 305-425 LBL 16 W094, FS 330-340 RT OUTBOARD W269, FS 408 RBL 45 W270, FS 408-512 LBL 37 W095 AND W103, FS 579 RBL 45 W172, FS 668 RBL 44 W496, FS 670-745 LBL 18 W433, FS 689 RBL 30 W174, FS 718-986 LBL 58 W432, FS 739-785 RBL 34 W312, FS 748 LBL 24 W406, FS 766-822 RBL 56 W446, FS 770 RBL 5 W176, FS 822-986 RBL 49 Y054, FS 832 RBL 12 W175, FS 832-986 RBL 58 W393, FS 856 LBL 34 W507, FS 929-989 LBL 44 W427. REPAIRED SEAT T

Part: LONGERON — CRACKED (BS 945)

PHX - DURING C-CHECK, LONGERON 17R IS CRACKED AT FS 945. REPAIRED PER SRM 53-11-03 FIG 4C. (M)

Part: LONGERON — CRACKED (BS 945)

PHX - DURING C-CHECK, LONGERON 17L IS CRACKED AT FS 945. REPAIRED PER SRM 53-02 FIG 18. (M)

Part: FRAME — CORRODED (BS 965)

PHX - DURING C-CHECK, AFT BAG BIN FRAME ST FS 965 HAS CORROSION FROM LONGERON 28L TO 28R. REPAIRED PER SRM 53-03 FIG 2A. (M)

Part: FRAME — CORRODED (BS 218)

PHX - DURING C-CHECK, FUSELAGE FRAME AT FS 218 HAS CORROSION AT LONGERON 30. REPAIRED PER SRM 53-03 FIG 5. (M)

Part: WEB — CRACKED (BS 218-969)

PHX - DURING C-CHECK, MAIN CABIN CUSP WEBS FROM FS 218, SEVERAL LOCATIONS WERE FOUND WITH VARIOUS DISCREPANCIES, CRACKS, CORROSION, DENTED, NRC FS 218 AT RBL 44 V105, FS 218-235 LT W462, FS 237-255 RBL 44 V106, FS 237 RBL 60 W399, FS 285-313 RT W318, FS 313 LT W365, FS 313-354 RT W319, FS 515 RBL 56 W465, FS 579-598 RT W358, FS 611 RT W151, FS 598-617 RT W357, FS 658-699 RT W376, FS 689 RT W403, FS 690-699 LBL 54 W404, FS 718-986 LT W322, FS 740 LBL 53 W141, FS 756 LBL 58 W143, FS 832 RBL 49 Y083, FS 832-897 RT 7048, FS 870-899 LT 7049, FS 935-965 RT Y022, FS 945-969 LT 7025. 22 TOTAL DISCREPANCIES ON THIS ITEM. REPAIRED PER SRM 53-11-2, 53-01 FIG 4, 53-11-10B. (M)

Part: DOUBLER — CORRODED (FUSELAGE)

PHX - DURING C-CHECK, AFT PRESSURE BULKHEAD SKIN HAS DAMAGE AND CORROSION, THESE ITEMS DON'T GIVE GOOD DESCRIPTIONS OTHER THAN BEING IDENTIFIED AS PSE 53.09.025. NRC L045, L106, L107. REPAIRED PER EA DC9-53-210, BOEING MESSAGE MISC-C743/PPS AND ECRA 935-51-038-1. (M)

Part: DOUBLER — CORRODED (FUSELAGE)

PHX - DURING C-CHECK, AFT PRESSURE BULKHEAD SKIN HAS DAMAGE AND CORROSION, THESE ITEMS DON'T GIVE GOOD DESCRIPTIONS OTHER THAN BEING IDENTIFIED AS PSE 53.09.025. NRC L045, L106, L107. REPAIRED PER EA DC9-53-210, BOEING MESSAGE MISC-C743/PPS AND ECRA 935-51-038-1. (M)

Part: SKIN — CORRODED (FUSELAGE)

PHX - DURING C-CHECK, AFT PRESSURE BULKHEAD SKIN HAS DAMAGE AND CORROSION, THESE ITEMS DON'T GIVE GOOD DESCRIPTIONS OTHER THAN BEING IDENTIFIED AS PSE 53.09.025. NRC L045, L106, L107. REPAIRED PER EA DC9-53-210, BOEING MESSAGE MISC-C743/PPS AND ECRA 935-51-038-1. (M)

Part: DOUBLER — CORRODED (BS 718)

PHX - DURING C-CHECK, RIGHT MAIN GEAR WHEEL WELL, FS 718 AT RBL 37, CEILING DOUBLER HAS CORROSION. REPAIRED PR SRM 53-01, AND EA DC9-53-186 AND ECRA 935-51-038-1. (M)

Part: SPAR — CRACKED (WS 164)

PHX - DURING C-CHECK, RIGHT WING AFT SPAR LOWER CHORD AT XRS 164 NR 2 FLAP HINGE ATTACH AREA A CRACK WAS FOUND. REPAIRED PER DRAWING J06027, EA DC9-57-136 AND ECRA 935-51-038-1. (M)

Part: SUPPORT — CORRODED (BS 218)

PHX - DURING C-CHECK, VERTICAL SUPPORT HAS HEAVY CORROSION AT BS 218 AT LBL 20. NRC G041. REPAIRED SUPPORT PER SRM 53-01 FIG 2. (M)

Part: FLOORBEAM — CORRODED (BS 945)

PHX - DURING C-CHECK, BS 945 FLOORBEAM HAS CORROSION AT RBL 48. NRC Y036. REPAIRED PER SABER TECH DC9-53-189 AND ECRA 935-51-038-1. (M)

Part: SPAR — CORRODED (WS 270)

PHX - DURING C-CHECK, LEFT WING REAR SPAR UPPER CHORD HORIZONTAL LEG HAS CORROSION AT WS 270. REPAIRED PER SABER TECH DC9-57-138 AND ECRA 935-51-038-1. (M)

Part: LONGERON — CRACKED (BS 965)

PHX - DURING C-CHECK, LONGERON 17R CRACKED AT BS 965. REPLACED DAMAGED SECTION PER SRM 53-11-3 FIG 4. (M)

Part: PAN — CRACKED (L1 DOOR)

PHX - DURING C-CHECK, L1 DOOR FORWARD PAN AT HINGE CUTOUT CRACKED, NR 1, NR 2, NR 5 AND NR 6 BEAM FORWARD ENDS CRACKED. REPLACED CRACKED PAN, REPAIRED BEAMS PER SRM 52-05 FIG 25, 18 AND 31. (M)

Part: COWL — CRACKED (NR 2 ENGINE)

PHX - DURING C-CHECK, NR 2 ENGINE NOSE COWL HAS LARGE CRACKS AT 4 O'CLOCK POSITION. NRC R040. REPAIRED PER SRM 54-04B FIG 1 AND SABER TECH EA DC9-54-013 AND ECRA 935-51-038-1. (M)

Part: SKIN — GOUGED (TE FLAP)

PHX - DURING C-CHECK, LEFT WING FLAP LEADING EDTE AT XRS 167.5, A GAUGE WAS FOUND IN THE LEADING EDGE SKIN. NRC A071. REPAIRED PER SABER TECH EA DC9-57-177 AND ECRA 935-51-038-1. (M)

Part: WEB — CRACKED (BS 965)

PHX - DURING C-CHECK, BS 965 RIGHT BULKHEAD FORWARD FACE IS CRACKED AT FASTENER HOLE. NRC Y053. REPAIRED PER SRM 51-10-03 AND SABER TECH EA DC9-53-191 AND ECRA 935-51-038-1. (M)

Part: BEAM — CRACKED (L1 DOOR)

PHX - DURING C-CHECK, L1 DOOR FORWARD PAN AT HINGE CUTOUT CRACKED, NR 1, NR 2, NR 5 AND NR 6 BEAM FORWARD ENDS CRACKED. REPLACED CRACKED PAN, REPAIRED BEAMS PER SRM 52-05 FIG 25, 18 AND 31. (M)

Part: PAN — CRACKED (CARGO DOOR)

PHX - DURING C-CHECK, LOWR AFT CARGO DOOR OUTER PAN HAS MULTIPLE CRACKS AT FORWARD NR 1 STOP. REPLACED DOOR PAN PER SRM 51-10-02. (M)

Part: INTERCOSTAL — CRACKED (PAX DOOR)

PHX - DURNG C-CHECK, L1 DOOR HANDLE PAN AND INTERCOSTAL FOUND CRACKED, NRC V044. REPLACED DOOR PAN AND INTERCOSTAL PER SRM 51-30-0. (M)

Part: BEAM — CRACKED (BS 50)

PHX - DURING C-CHECK, LEFT NOSE GEAR SUPPORT BEAM AT FS 50 WAS FOUND CRACKED. NRC E043, E042. REPAIRED BEAM PER SRM 53-15 FIG 110. (M)

Part: FRAME — MISDRILLED (BS 639)

PHX - DURING C-CHECK, BS 639 FRAME HAS HOLE DRILLED PARTIALLY THROUGH AT LONGERON 10L. NRC W275. REMOVED DAMAGED AREA AND INSTALLED REPAIR STRAP AND REPAIR PER SRM 51-10-02 AND SABER TECH EA DC9-53-187 AND ECRA 935-51-038-1. (M)

Part: LONGERON — CRACKED (BS 965)

PHX - DURING C-CHECK, LONGERON 16L CRACKED AT BS 965. NRC Y014. REPLACED DAMAGED SECTION AND INSTALLED SPLICE PER SRM 53-11-3 FIG 4 AND 53-02 FIG 18. (M)

Part: FRAME — CRACKED (BS 980)

PHX - DURING C-CHECK, BS 980 FRAME CRACKED AT LONGERON 17R. NRC 7013. REPAIRED PER SRM 53-05 FIG 32 AND 51-30-02. (M)

Part: WEB — CORRODED (BS 737-775)

PHX - DURING C-CHECK, WEB CUSP HAS CORROSION AT FS 737-775 LEFT SIDE. NRC W0304. REPLACED CUSP WEB PER SRM 51-10-02, 53-11-03. (M)

Part: SEAT TRACK — WORN (BS 680)

PHX - DURING C-CHECK, SEAT TRACK AT BS 680 HAS TAB WORN BEYOND LIMITS AT BL 12. REPLACED SECTION OF SEAT TRACK PER SRM 53-05 FIG 4B, 33 INCH SECTION REPLACED. (M)

Part: DOOR LATCH — MALFUNCTIONED (LANDING GEAR)

BIL - LOG PAGE: F32722 - AFTER TAKEOFF, GEAR DOOR WOULD NOT CLOSE. AIRCRAFT RETURNED TO BIL, NO PROBLEMS DURING LANDING. BYPASS DOOR OPEN. CLOSED DOOR AND MAIN DOOR CLOSED NORMALLY. (X)

Part: TIRE — FAILED (NR 3 MLG)

OAK - LOG PAGE: F77497 - DURING THE TAKEOFF ROLL AT 135K, A LOUD NOISE WAS HEARD FOLLOWED BY AIRCRAFT VIBRATION. AFTER TAKEOFF, THE GEAR WAS LEFT EXTENDED AND AIRCRAFT RETURNED TO OAK, NO PROBLEMS DURING LANDING. FIRE DEPT RELAYED INFO THAT NR 3 TIRE WAS BLOWN. AIRCRAFT TAXIED INTO BLOCKS WITH NO PROBLEMS. (X)

Part: SCRAPER — DAMAGED (NLG)

PAJN - LOG PAGE: F32570 - AFTER TAKEOFF AT PAJN, LANDING GEAR HANDLE WOULD NOT MOVE TO RETRACT POSITION, NOSE WHEEL WAS STEERABLE. FOUND NOSE GEAR STRUT SCRAPPER RING BINDING. REPACKED STRUT WITH NEW O-RINGS AND SCRAPPER. (X)

Part: TORQUE LINK — LACK OF LUBE (NLG)

PDX - ON DEPARTURE FROM KPDX, UNABLE TO RAISE LANDING GEAR. NOSE WHEEL WAS STEERABLE AND STILL IN GROUND MODE GCR. FOUND NOSE GEAR TORQUE LINKS VERY STIFF AND DRY, CAUSING BINDING WHEN THE STRUT EXTENTION WAS VARIED WITH NITROGEN. LUBED TORQUE LINKS PER MM. LINKS MOVED FREELY. STRUT SERVICING CHECKED GOOD. (M)

Part: STRUT — REQ'D SERVICE (NLG)

AFTER TAKEOFF, AIRCRAFT WOULD NOT SHIFT INTO FLIGHT MODE. LANDING GEAR DID RETRACT. SERVICED NOSE LANDING GEAR. (M)

Part: ANGLES — CRACKED (BS 598)

SAT - FORWARD CARGO BAY BS 598 STRINGER 28R BOTH HORIZONTAL AND VERTICAL PANEL SUPPORT ANGLES ARE CRACKED. FABRICATED AND INSTALLED HORIZONTAL ANGLE PER SRM 51-30-2, 53-21-0 FIG 7C SHEET 1 AND 3. FABRICATED AND INSTALLED VERTICLE ANGLE PER SRM 51-30-2, 53-01 FIG 2 SHEET 4 AND SRM 53-21-0 FIG 7C SHEET 1/3. SECOND STRUCTURE. (M)

Part: LONGERON — CORRODED (BS 963)

SAT - LONGERON 28R HAS EXFOLIATION CORROSION AT STATION 963 BEYOND LIMITS. REMOVED LONGERON 28R FROM FS 945-996 IAW SRM 53-11-3 FIG 4 AND 51-10-1 FABRICATED LONGERON AND INSTALLED IAW SRM 53-11-3 FIG 4 AND 51-10-1 FIG 15. (M)

Part: FLOOR SUPPORT — CORRODED (BS 996)

SAT - FS 996 LOWER SUPPORT ANGLE HAS EXFOLIATION CORROSION FROM LONGERON 25L TO 25R. FABRICATED AND INSTALLED FLOOR SUPPORT ANGLE FS 996 FROM LONGERON 26L TO 29R PER SRM 53-01 FIG 2 AND SRM 53-11-3. (M)

Part: FITTING — CRACKED (FR 237)

SAT - FORWARD CARGO BAYFRAME 237 FLOOR SUPPORT FITTING AT LONGERON 24R IS CRACKED. REMOVED AND REPLACED FITTING PER SRM 51-30-2. (M)

Part: FRAME — CRACKED (FR 718)

SAT - FRAME 718 RIGHT IS CRACKED BEYOND SERVICABLE LIMITS OF S/B 53-131. REMOVED AND REPLACED FRAME PER S/B 53-131 AND SRM 51-30-2. INTERCOSTAL IAW SRM 53-11-3 AND 51-30-2. (M)

Part: FLOOR SUPPORT — CORRODED (BS 218-285)

SAT - FORWARD CARGO COMPARTMENT FRAME 362 TO FORWARD BULKHEAD HAS LIGHT SURFACE CORROSION ON FLOOR SUPPORT AT STATION 28R. REMOVED FLOOR SUPPORT, FABRICATED AND INSTALLED REPLACEMENT CHANNEL LE IAW SRM 51-30-2 FROM STATION 218 TO 285, FROM AREA 285 TO 362. REMOVED CORROSION IAW SRM 51-10-3, AREA FROM STATION 285 TO 362 WITHIN LIMITS. (M)

Part: FRAME — CORRODED (BS 237)

SAT - FRAME 237 LONGERON 24R CORRODED. FABRICATED AND INSTALLED REPAIR SPLICE TO FRAME BS 237 LONGERON 24R PER SRM 53-03 FIGURE 2A. (M)

Part: INTERCOSTAL — CRACKED (BS 718-737)

SAT - FLOOR SUPPORT INTERCOSTAL RB 153 STATION 718 TO 737 CRACKED. FABRICATED REPLACEMENT INTERCOSTAL WEB STATION 718 TO 737 RBL 53 PER SRM 51-10-1 AND 51-30-2. (M)

Part: FITTING — CRACKED (BS 718)

SAT - LEFT WHEEL WELL TO KEEL BEAM ATTACH FITTING STATION 718 IS CRACKED. CRACK EMANATES FROM THE FORWARD VERTICAL BOLT HOLE FORWARD IN THE HORIZONTAL FLANGE OF THE FITTING. REMOVED AND REPLACED FITTING IAW SRM 51-30-2 AND 51-20-0. (M)

Part: FRAME — CHAFFED (FRAME 1038)

SAT - FRAME 1038 AT STRINGER 5L HAS A HOLE CHAFFED IN FRAME WEB BY LEFT AIR CONDITIONING PACKAGE ROTARY ACTUATOR. FABRICATED AND INSTALLED WEB DOUBLER REPAIR FRAME 1038 STRINGER 5L PER SRM 53-11 FIG 1. (M)

Part: ANGLE — CORRODED (FS 996)

SAT - CORRODED FLOOR SUPPORT ANGLE AT AFT CARGO STATION 996 STRINGER 25L-25R. FABRICATED NEW ANGLES AND INSTALLED PER SRM 53-01 FIG 2 AND 51-30-2. (M)

Part: JAMB — CORRODED (BS 370-427)

SAT - CORRODED FORWARD CARGO LOWER DOOR JAMB AT STATION 370-427. FABRICATED NEW SECTION AND INSTALLED PER SRM 53-05 FIG 44, 51-30-2 AND 51-10-3. (M)

Part: INTERCOSTAL — CORRODED (BS 218/237)

SAT - FORWARD CARGO BAY INTERCOSTAL BETWEEN STATION 218 AND 237 AT STRINGER 27R/28R CORRODED. REMOVED, FABRICATED AND INSTALLED INTERCOSTAL PER SRM 53-11-2 FIG 1D AND SRM 53-10-1 FIG 3. (M)

Part: FRAME — CRACKED (FR 274)

SAT - FRAME 274 LOWR FLAGNE CRACKED AT ATTACHMENT POINT STRINGER 29L AND 29R. FABRICATED NEW ANGLES AND FILLERS AND INSTALLED PER SRM 51-10-3 FIG 5, 51-10-3 AND 51-30-2. (M)

Part: SUPPORT — CORRODED (BS 218-285)

SAT - FORWARD CARGO BAY FRAME 362 FLOOR SUPPORT IS CORRODED AT STRINGER 28R. FABRICATED AND INSTALLED FLOOR SUPPORT CHANNEL FROM BS 218 TO 285 AND 285 TO 362 PER SRM 53-21-0, 53-01 FIGURE 2 AND 51-21-3. (M)

Part: TIE DOWN RAILS — CORRODED (BS 756-900)

SAT - AFT CARGO BAY LEFT AND RIGHT TIE DOWN RAILS BS 756 TO 900 CORRODED. FABRICATED AND INSTALLED TIE DOWN RAILS PER SRM 53-21-0 FIGURE 8 AND 51-30-2. (M)

Part: FLOOR STRUT — CRACKED (FR 237)

SAT - FORWARD CARGO BAYFRAME 237 FLOOR SUPPORT STRUT AT LONGERON 24R IS CRACKED. REMOVED, FABRICATED AND INSTALLED FLOOR SUPPORT STRUT AT FR 237 LONGERON 24R PER DAC DRAWING 5922079 AND SRM 51-30-2. (M)

Part: BULKHEAD CHORD — CORRODED (BS 756)

SAT - BULKHEAD 756 UPPER T-CHORD CORRODED LBL 22 TO LBL 31. FABRICATED AND INSTALLED BULKHEAD T-CHORD SECTION BS 756 LBL 22 TO LBL 31 PER SRM 53-01 FIG 2, 51-10-3 AND 53-14-3. (M)

Part: FRAME — CRACKED (CARGO COMPT)

SAT - AFT CARGO HAS CRACKS IN FRAME 908-937 UPPER CEILING WEB AT STRIGNER 19L ABOVE AFT CARGO DOOR LIGHT. STOP DRILLED CRACKS, PERFORMED EDDY CURRENT INSPECTION ON STOP DRILL HOLES, FABRICATED DOUBLER AND INSTALLED PER SRM 51-10-3, 53-11-3 FIGURE 1, 2 AND 3, 53-01 FIGURE 3 SHEET 1, 2 AND 3 AND NDTS PM 06-00-07. (M)

Part: FLOOR PANEL — CORRODED (CARGO BAY)

SAT - FORWARD CARGO BAY FLOOR PANEL NR 3 IS CORRODED. REPAIRED FLOOR PANEL PER SRM 51-70-2. (M)

Part: CHANNEL — CORRODED (BS 90)

SAT - 'J' CHANNEL CORRODED FS 90 LBL 6 TO LBL 12 NOSE WHEEL WELL. REMOVED, FABRICATED AND INSTALLED 'J' CHANNEL PER SRM 51-00, 51-30-2 AND 51-30-3. (M)

Part: ANGLE — CRACKED (BS 598)

SAT - FORWARD CARGO COMPARTMENT STATION 598, STRINGER 28R HORIZONTAL AND VERTICAL PANEL SUPPORT ANGLES ARE CRACKED. FABRICATED AND INSTALLED HORIZONTAL ANGLE IAW SRM 51-30-0, FIGURE 76 SHEET 1 AND 3. REMOVED DAMAGED AREA ON VERTICAL ANGLE IAW SRM 53-01 FIGURE 2 SHEET 4. FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 51-30-2, 53-01 FIGURE 2 SHEET 4 AND 53-21-0 FIGURE 7C SHEET 1 AND 3. (M)

Part: DOUBLER — CRACKED (LEFT ENGINE)

SAT - FOUND LEFT ENGINE UPPER THRUST REVERSER BUCKET DOUBLER CRACKED AT OUTBOARD FORWARD END. CUT OUT DAMAGED AREA PER OHM 78-30-1 FIG 404. FABRICATED REPAIR DOUBLER PER SRM 54-01 AND INSTALLED PER SRM 51-00 AND 51-30-2. (M)

Part: FRAME — CRACKED (FRAME 1168)

SAT - AFT ACCESSORY COMPARTMENT FRAME 1168 WEB AT 1 O'CLOCK IS CRACKED. REMOVED, FABRICATED AND INSTALLED CRACKED WEB ANGLE PER SRM 53-10-4 FIG 4 AND SRM 51-30-0. (M)

Part: INTERCOSTAL — CORRODED (BS 945-965)

SAT - AFT BAG BIN BS 945-965 INTERCOSTAL AT STATION 28R HAS EXFOLIATION CORROSION. REMOVED, FABRICATED AND INSTALLED REPLACEMENT INTERCOSTAL IAW SRM 51-11-3 AND 51-30-2. (M)

Part: INTERCOSTAL — CORRODED (FR 579 - 598)

SAT - CORROSION ON TOP FLANGE OF INTERCOSTAL FRAME 579 TO 598 BETWEEN STRINGER 27R AND 28R IS OUT OF LIMITS. FABRICATED AND INSTALLED REPAIR DOUBLER FR 579 TO 598 INTERCOSTAL BETWEEN STRINBER 27R AND 28R PER SRM. (M)

Part: BULKHEAD — GOUGE (BS 37)

SAT - FOUND FUSELAGE STATION 37 BULKHEAD WEB GOUGED AT STRINGER 18L. REMOVED DAMAGED AREA AND INSTALLED DOUBLER REPAIR PER SRM 53-01 FIG 4 ITEM 4. (M)

Part: WEB — CRACKED (BS 737)

SAT - FOUND RIGHT MAIN LANDING GEAR WHEEL WELL FS 737 RBL 52 AT STRINGER 18R WEB IS CRACKED. FABRICATED AND INSTALLED DOUBLER REPAIR PER SRM 53-01 FIG 4 AND SRM 51-30-2. (M)

Part: BULKHEAD WEB — GOUGE (BS 37)

SAT - FOUND FUSELAGE STATION 37 BULKHEAD WEB GOUGED AT STRINGER 18R. REMOVED DAMAGED AREA AND INSTALLED DOUBLER REPAIR PER SRM 53-01 FIG 1 AND FIG 2. (M)

Part: CHANNEL — CRACKED (ACCESSORY COMP)

SAT - AFT ACCESSORY COMPARTMENT PLUG DOOR LOWER SEALING CHANNEL FRAME IS CRACKED. REMOVED AND INSTALLED NEW SEAL CHANNEL FRAME IAW SRM 51-00 AND SRM 51-30-2. (M)

Part: FITTING — BROKEN (NR 2 ENGINE)

KTN - AFTER TAKEOFF, RIGHT ENGINE EPR REDUCED TO 1.6 (FROM 2) AND EGT CLIMBED TO 565 C. N1 DROPPED FROM 95 PERCENT TO 85 PERCENT. OIL PRESSURE WAS NORMAL. RETURNED TO PAKT. FOUND PS4 MANIFOLD FITTING ON PRBC BROKEN IN HALF. REPLACED FITTING. PERFORMED ENGINE RUN PER MM 71-00. ALL CHECKS WERE GOOD. (M)

Part: ENGINE — MALFUNCTIONED (LEFT)

KTN - LEFT ENGINE EPR ABRUPTLY DROPPED TO 1.4 AND EGT PEGGED, CLIMB AT FL 260 ACCOMPANIED BY STRONG VIBRATION, REDUCING THRUST LEVER TO IDLE LESSENED VIBRATION AND EGT CAME DOWN TO 500 DEGREES. WHEN EPR INITIALLY DROPPED TO 1.4, N1 DROPPED TO 38 PERCENT AND N2 DROPPED TO 62 PERCENT. (M)

Part: EEL — MALFUNCTIONED (CABIN)

DEN - EMERGENCY EXIT LIGHT LOCATED AT MAIN ENTRANCE SWITCH IS BROKEN, STAYS ON ALL THE TIME. REPLACED LIGHT ASSY, EMERGENCY EXIT PANEL, SYSTEM OPS. CHECK GOOD IAW MM 33-50-00. (M)