N768AS

Part: ARM — LACK OF LUBE (L2 DOOR HINGE) · airframe 69,347 hrs · 47,137 cycles

L2 DOOR IS HARD TO OPEN AND CLOSE. ACFT GROUNDED. LUBRICATED THE DOOR HINGE ARM, OPS NORMAL.

Part: ANGLE — CRACKED (BS 540 BULKHEAD) · airframe 68,192 hrs · 46,204 cycles

LEFT BS 540 BULKHEAD LOWER SPLICE ANGLE IS CRACKED AT FASTENER HOLE INLINE WITH UPPER RAM AIR ANGLE. ACFT GROUNDED. R & R SPLICE IAW EA 400, 53EA 17220 REV 00.

Part: SKIN — CRACKED (BS 727D-727F) · airframe 68,192 hrs · 46,204 cycles

CRACK IN FUSELAGE SKIN AT BS 727D+2" BELOW STR 23R AT CHEM MILL STEP. ACFT GROUNDED. REPAIRED SKIN IAW SRM 53-00-01-2R-31, DETAIL VII. THIS IS A CATEGORY B REPAIR. INSPECTION THRESHOLD SET AT 66,000 CYCLES. REFER TO THE OPERATORS REPAIR ASSESSMENT PROGRAM FOR METHODS AND INTERVALS. REF SRM 53-00-01-2R-31, TABLE IX.

Part: SKIN — CRACKED (BS 727C-727E) · airframe 68,192 hrs · 46,204 cycles

CRACK IN FUSELAGE SKIN AT BS 727D+2" BELOW STR 23L AT CHEM MILL STEP. ACFT GROUNDED. REPAIRED FUSELAGE SKIN AT BS 727D+2" IAW SRM 53-00-01, REPAIR 31. THIS IS A CATEGORY B REPAIR WITH AN INSPECTION THRESHOLD OF 66000 FLT. CYCLES, REFER TO OPERATORS REPAIR ASSESSMENT PROGRAM FOR METHODS AND INTERVALS.

Part: SKIN — CRACKED (BS 727F-727G) · airframe 68,192 hrs · 46,204 cycles

CRACK IN FUSELAGE SKIN AT BS 727F+4" BELOW STR 23L AT CHEM MILL STEP. ACFT GROUNDED. REPAIRED SKIN IAW SRM 53-00-01-2R-31, DETAIL VII. THIS IS A CATEGORY B REPAIR. INSPECTION THRESHOLD SET AT 66,000 CYCLES. REFER TO THE OPERATORS REPAIR ASSESSMENT PROGRAM FOR METHODS AND INTERVALS. REF SRM 53-00-01-2R-31, TABLE IX.

Part: SKIN — CRACKED (BS 320-335) · airframe 68,192 hrs · 46,204 cycles

R1 DOOR CUTOUT LOWER AFT CORNER IS CRACKED. ACFT GROUNDED. REPAIRED DAMAGE TO LOWER AFTER CORNER OF R1 DOOR CUTOUT IAW SRM 53-10-01-2R-19, REPAIR 19. THIS IS A CATEGORY B REPAIR WITH AN INSPECTION THRESHOLD OF 60,000 TOTAL FLIGHT CYCLES REFER TO THE REPAIR ASSESSMENT GUIDELINES D6-38669 FOR METHODS AND INTERVALS.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHT) · airframe 67,862 hrs · 45,943 cycles

AFT L2 DOOR TOP EMERGENCY EXIT LIGHT INOPERATIVE AND AT ROW 27 ABC EMERGENCY EGRESS LIGHT REF LOGPAGE 11371753. ACFT GROUNDED. EMERGENCY LIGHT POWER SUPPLY R & R IAW AMM 33-51-51-962-016 AND WDM 33-51-00, PG 101, SHEET 1 AND SHEET 2. OPS CHECK GOOD.

Part: LENS — DETACHED (EMERGENCY LIGHT) · airframe 66,063 hrs · 44,410 cycles

EXIT SIGN OVER FLIGHT DECK DOOR FELL OFF. ACFT GROUNDED. REPLACED EMERENCY EXIT LENS OVER FLIGHT DECK DOOR.

Part: DOOR — BINDING (L1) · airframe 65,896 hrs · 44,278 cycles

L1 DOOR DIFFICULT TO CLOSE. ACFT GROUNDED.

Part: CHANNEL — CRACKED (BS 500-500A) · airframe 65,799 hrs · 44,206 cycles

FWD CARGO COMPARTMENT VH NR 2 ANTENNA SUPPORT CHANNEL CRACKED BETWEEN STR 28L AND 28R, STA 500 TO 500A. ACFT GROUNDED. R & R CHANNEL IAW SRM 51-40-02-0G-0.

Part: ANGLE — CRACKED (BS 277-291) · airframe 65,799 hrs · 44,206 cycles

OTBD ANGLE ON INTERCOSTAL BETWEEN STA 277 AND 291.5 IS CRACKED AT STR 11R. ACFT GROUNDED. INSTALLED NEW ANGLE IAW SRM 51-40-02-0G-0.

Part: SKIN — CRACKED (BS 945-960) · airframe 65,799 hrs · 44,206 cycles

FUSELAGE SKIN AT FWD SIDE OF L2 DOOR HINGE LOWER CUTOUT IS DAMAGED. ACFT GROUNDED. REPAIRED SKIN IAW EA 400, 53EA, 14954, REV NEW.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 65,799 hrs · 44,206 cycles

FWD CARGO DOOR IS CRACKED FROM FASTENER JUST AFT OF HANDLE CUTOUT UPPER CORNER TO HANDLE CUTOUT. ACFT GROUNDED. REPAIRED FWD CARGO DOOR SKIN IAW SRM 52-00-01-2R-3.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 65,799 hrs · 44,206 cycles

FWD CARGO DOOR IS CRACKED FROM FASTENER JUST AFT OF HANDLE CUTOUT UPPER CORNER TO HANDLE CUTOUT. ACFT GROUNDED. REPAIRED FWD CARGO DOOR SKIN IAW SRM 52-00-01-2R-3.

Part: FRAME — CRACKED (BS 299) · airframe 65,799 hrs · 44,206 cycles

AFTER R1 DOOR STOP INTERCOSTAL REMOVAL AT STR 8R, BS 299, FOUND R1 DOOR UPPER FRAME SECTION CRACKED. ACFT GROUNDED. R & R UPPER FRAME SECTION IAW SRM 51-40-02-0G-0.

Part: FITTING — CRACKED (HORIZONTAL STAB) · airframe 65,799 hrs · 44,206 cycles

RT SIDE AFT LOWER THRUST BEAM CORNER FITTING IS CRACKED REQUIRES EC-SB737-55-1091-400-2 TO BE ASSIGNED TO WORK PACKAGE. ACFT GROUNDED. REPLACED RT HORIZONTAL STABILIZER CENTER SECTION THRUST BEAM CORNER FITTINGS IAW T/C SB737-55-1091-400-2 AND EA 400-55EA-14862.

Part: INTERCOSTAL — CRACKED (BS 277-294) · airframe 65,799 hrs · 44,206 cycles

INTERCOSTAL AT BS 277 AND BL 0 CRACKED ON BOTTOM SIDE IN RADIUS. ACFT GROUNDED. R & R INTERCOSTAL IAW SRM 51-40-02-0G-0.

Part: STRINGER CLIP — CRACKED (BS 727A) · airframe 65,799 hrs · 44,206 cycles

STRINGER CLIP AT STA 727A AND STR 4R IS CRACKED. ACFT GROUNDED. R & R CRACKED STRINGER CLIP AT STA 727A, STR 4R IAW SRM 51-40-02.

Part: ATTACH ANGLE — CRACKED (STRINGER 15L) · airframe 65,799 hrs · 44,206 cycles

STRINGER 15L INTERCOSTAL FWD ATTACH ANGLE IS CRACKED IN RADIUS AT STA 348.2. ACFT GROUNDED. R & R ATTACH ANGLE AT BS 348.2, STR 15L IAW SRM 51-40-02.

Part: CUSP WEB — CORRODED (BS 727A-727B) · corrosion level 2 · airframe 65,799 hrs · 44,206 cycles

CUSP WEB AT STA 727B RT CORRODED. ACFT GROUNDED. R & R CUSP WEB AT FS 727B RT SIDE IAW SRM 51-40-02-0G-0, W 2", O .032, R .028, L 3", D 1".

Part: WEB — CRACKED (BS 639) · airframe 65,799 hrs · 44,206 cycles

STA 639, LT WEB AT LONG 15 CRACKED. ACFT GROUNDED. R & R LT WEB AT STA 639 AFT OF OVERWING EXIT IAW SRM 51-40-02-0G-0.

Part: STIFFENER — CORRODED (BS 1112-1116) · corrosion level 2 · airframe 65,799 hrs · 44,206 cycles

APU AIR INLET CUTOUT FWD STIFFENER IS CORRODED. GROUNDED - YES. REMOVED AND REPLACED DAMAGED FWD STIFFENER IAW SRM 51-40-02-0G-0, W .75", O .06, R .045, L 6", D .015.

Part: STRINGER CLIP — CRACKED (BS 827) · airframe 65,799 hrs · 44,206 cycles

STRINGER CLIP AT STA 827 CRACKED STR 4 RT. ACFT GROUNDED. R & R CRACKED STRINGER CLIP AT STA 827, STR 4R IAW SRM 51-40-02.

Part: CREASE BEAM — CORRODED (BS 500D-500E) · corrosion level 2 · airframe 65,799 hrs · 44,206 cycles

CREASE BEAM WEB AT STA 500D AND LBL60 CORRODED ON LOWER SIDE. ACFT GROUNDED. R & R LT CREASE BEAM SHEAR WEB, STA 500D-500E IAW SRM 51-40-02-0G-0, W 1.5, O .036, R .026, L .75, D .010.

Part: CREASE BEAM — CORRODED (BS 500F-500G) · corrosion level 2 · airframe 65,799 hrs · 44,206 cycles

CREASE BEAM WEB AT LBL 60 AND STA 500G CORRODED ON LOWER SIDE. ACFT GROUNDED. R & R LT CREASE BEAM, SHEAR WEB, STA 500F, 500G IAW SRM 51-40-02-0G-0, W 2.0, O .036, R .025, L 1.0, D .011.

Part: WEB — CORRODED (BS 867-887) · corrosion level 2 · airframe 65,799 hrs · 44,206 cycles

RT OTBD WEB AT STA 881, APPROXIMATELY, CORRODED. ACFT GROUNDED. R & R RT OTBD SHEAR WEB AT FS 881 IAW SRM 51-40-02-0G-0.

Part: STRINGER CLIP — CRACKED (BS 727B) · airframe 65,799 hrs · 44,206 cycles

STRINGER CLIP AT STA 727B IS CRACKED AT STR 4R. ACFT GROUNDED. R & R CRACKED STRINGER CLIP AT STA 727B, STR 4R IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (BS 540-727B) · corrosion level 2 · airframe 65,799 hrs · 44,206 cycles

FLOORBEAM, LBL 45 FLANGE CORRODED AT STA 578-601. ACFT GROUNDED. R & R FLOORBEAM, LBL 45, UPPER CAP IAW SRM 51-40-02-0G-0, W 4", O .090", R .077", L 150", D .013.

Part: STRINGER CLIP — CRACKED (BS 727G) · airframe 65,799 hrs · 44,206 cycles

STRINGER CLIP IS CRACKED AT STA 727G AND STR 10R. ACFT GROUNDED. R & R CRACKED STRINGER CLIP AT STA 727G, STR 10R IAW SRM 51-40-02.

Part: SEAT TRACK — CORRODED (BS 520-540) · corrosion level 2 · airframe 65,799 hrs · 44,206 cycles

PAX CABIN LT UNDER OTBD SEAT TRACK AT FS 520 AND BL 46 POSITION FLOORBEAM SUPPORT CORRODED. ACFT GROUNDED. R & R PIVOT LINK ASSEMBLIES IAW SRM 51-40-02-0G-0 AND AMM 20-50-11-912-002.

Part: CUSP WEB — CORRODED (BS 867-887) · corrosion level 2 · airframe 65,799 hrs · 44,206 cycles

AFT CABIN LT SIDE FROM FS 867 TO FS 887, CUSP WEB CORRODED. ACFT GROUNDED. R & R CUSP WEB IAW SRM 51-40-02, PAR 4 AND PG 6, PAR D, W 2.00, O .032, R .026, L 6, D .006".

Part: SUPPORT — CORRODED (BS 520-540) · corrosion level 2 · airframe 65,799 hrs · 44,206 cycles

PAX CABIN UNDER OTBD SEAT TRACK AT FS 520 AND BL 46 POSITION FLOORBEAM SUPPORT CORRODED. ACFT GROUNDED. R & R PIVOT LINK ASSEMBLIES IAW SRM 51-40-02-0G-0 AND AMM 20-50 11-918-002.

Part: SEAT TRACK — CORRODED (BS 520-540) · corrosion level 2 · airframe 65,799 hrs · 44,206 cycles

PAX CABIN RT UNDER OTBD SEAT TRACK AT FS 520 AND BL 46 POSITION FLOORBEAM SUPPORT CORRODED. ACFT GROUNDED. R & R PIVOT LINK ASSEMBLIES IAW SRM 51-40-02-0G-0 AND AMM 20-50-11-918-002.

Part: CHANNEL — CORRODED (BS 927-1006) · corrosion level 2 · airframe 65,799 hrs · 44,206 cycles

AFT CABIN LT SIDE IN FRONT OF L2 DOOR LOWER MOP SILL CORRODED. ACFT GROUNDED. R & R L2 DOOR MOP SILL IAW SRM 51-40-05-0G-0 AND 51-40-02-0G-0.

Part: STRINGER — CORRODED (TORQUE BOX) · corrosion level 2 · airframe 65,799 hrs · 44,206 cycles

APU TORQUE BOX RT CUTOUT LOWER STRINGER CORRODED. ACFT GROUNDED. R & R APU TORQUE BOX LOWER STRINGER IAW SRM 51-40-02-0G-0, W .75 O, .065, R .044, L 6IN., D .021.

Part: STRINGER — CORRODED (TORQUE BOX) · corrosion level 2 · airframe 65,799 hrs · 44,206 cycles

APU TORQUE BOX RT CUTOUT UPPER STRINGER CORRODED. ACFT GROUNDED. R & R APU TORQUE BOX UPPER STRINGER IAW SRM 51-40-02-0G-0, W .75", O .065, R .041, L 6", D .024.

Part: CUSP WEB — CORRODED (BS 767-787) · corrosion level 2 · airframe 65,799 hrs · 44,206 cycles

AFT CABIN LT SIDE FROM FS 767 TO FS 787 CUSP WEB CORRODED. ACFT GROUNDED. R & R CUSP WEB IAW SRM 51-40-02, PAR 4 AND PG 6, PAR D, W 3.00, O .032", R .021", L 4.00", D .011".

Part: CUSP WEB — CORRODED (BS 440-460) · corrosion level 2 · airframe 65,799 hrs · 44,206 cycles

PAX CABIN RT SIDE FROM FS 440 TO FS 460 CUSP WEB CORRODED. ACFT GROUNDED. R & R CUSP WEB RT SIDE FROM FS 440 TO FS 460 IAW SRM 51-40-02.

Part: SEAT TRACK — CORRODED (BS 520-540) · corrosion level 2 · airframe 65,799 hrs · 44,206 cycles

PAX CABIN LT UNDER OTBD SEAT TRACK AT FS 520 AND BL 46 POSITION FLOORBEAM SUPPORT CORRODED. ACFT GROUNDED. R & R PIVOT LINK ASSEMBLIES IAW SRM 51-40-02-0G-0 AND AMM 20-50-11-912-002, W 1", O .110, R 0, L 1". D .110.

Part: ANGLE — CRACKED (BS 277-291) · airframe 65,799 hrs · 44,206 cycles

ANGLE FWD OF R1 DOOR STA 277-291.5, STR 13R TO 14R IS CRACKED. ACFT GROUNDED.

Part: FITTING — CRACKED (LT MLG) · airframe 65,799 hrs · 44,206 cycles

LT MLG BEAM AFT SUPPORT FITTING IS CRACKED AT 4TH FROM INBD UPPER FASTENER. ACFT GROUNDED. INSPECTED LT MLG BEAM AFT SUPPORT FITTING IAW EA 400, 57 EA 14810.

Part: FILLER — CORRODED (BS 1112-1116) · corrosion level 2 · airframe 65,799 hrs · 44,206 cycles

FWD FILLER APU INLET FLANGE HAS EVIDENCE OF CORROSION. ACFT GROUNDED. R & R FILLER IAW SRM 51-40-02-0G-0, W .75", O .100, R.088, L 8", D .012.

Part: FLOORBEAM — CRACKED (BS 727B) · airframe 65,799 hrs · 44,206 cycles

LONGITUDINAL FLOORBEAM CRACKED STA RBL 24.82, REQUIRES TO BE REPAIRED IAW T/C EC20080506 400-53-5. GROUNDED - YES. REPAIRED LONGITUDINAL FLOOR BEAM IAW ASA T/C AD20080506 400-57-5, REV 02, AND EA 400, 57EA 14930, REV NEW.

Part: FLOORBEAM — CRACKED (BS 727B) · airframe 65,799 hrs · 44,206 cycles

LONGITUDINAL FLOORBEAM CRACKED STA 727B AND RBL 45.57 REQUIRES REPAIR IAW T/C AD20080506 40053-6. ACFT GROUNDED. REPAIRED LONGITUDIANAL FLOORBEAM IAW T/C AD20080506 400-57-6 REV O2, DATED 24APR13 AND EA 400, 57EA 14930, REV NEW DATED 20APR15.

Part: FLOOR SUPPORT — CORRODED (BS 907-927) · corrosion level 2 · airframe 65,799 hrs · 44,206 cycles

AFT CARGO BAY FLOOR SUPPORT CORRODED, BS 907-927, RBL 3. ACFT GROUNDED. R & R AFT PIT FLOOR SUPPORT RBLS FS 797-917 IAW SRM 53-00-53-2R-1, W 1.0, O .063, R 0, L 40, D .063.

Part: STRINGER CLIP — CRACKED (BS 947) · airframe 65,799 hrs · 44,206 cycles

AFT PIT FRAME 947, STR 27R ATTACH CLIP CRACKED. ACFT GROUNDED. R & R STRINGER CLIP IAW SRM 51-40-02-0G-0.

Part: FLOOR SUPPORT — CORRODED (BS 837-877) · corrosion level 2 · airframe 65,799 hrs · 44,206 cycles

AFT CARGO BAY FLOOR SUPPORT AT BS 847-857, LBL 3 CORRODED. ACFT GROUNDED. R & R THE FLOOR SUPPORT IAW SRM 53-00-53-2R-1.

Part: FRAME — CORRODED (BS 927) · corrosion level 2 · airframe 65,799 hrs · 44,206 cycles

AFT PIT FRAME 927, STR 26R-27R CORRODED. ACFT GROUNDED. REMOVED CORRODED SECTION OF FRAME, REPAIRED AND RESTORED FINISH AT FS 927, STR 24R-STR 27R IAW SRM 53-00-07-2R-4 REPAIR 4 AND AMM 51-21-73-370-802, CATEGORY B, REPAIR WITH A THRESHOLD OF 66,000 CYCLES, CONTACT ENGINEERING FOR METHODS AND INTERVALS PRIOR TO THE THRESHOLD, W .75, O=.063, R=.054, L=1.5, D=.009. DTI TRACKING IN FILEMAKER PRO.

Part: FLOOR SUPPORT — CORRODED (BS 747) · corrosion level 2 · airframe 65,799 hrs · 44,206 cycles

AFT PIT, BS 747 RBL 3, FLOOR SUPPORT CORRODED ON BOTTOM SIDE. ACFT GROUNDED. R & R AFT PIT FLOOR SUPPORT CHANNEL RBL3, FS 738-797 IAW SRM 53-00-53-2R-1, W 1.0, O .063, R 0, L 4.0, D .063.

Part: FLOOR SUPPORT — CORRODED (BS 847-857) · corrosion level 2 · airframe 65,799 hrs · 44,206 cycles

AFT PIT, FLOOR SUPPORT AT STA 847-857 AT RBL 8.1 HAS HEAVY CORROSION. ACFT GROUNDED. R & R AFT CARGO FLOOR SUPPORT CHANNEL RBL 8.1, FS 737, FS 877, IAW SRM 53-00-53-2R-1, W 1.0, O .063, R 0, L 6., D .063.

Part: FITTING — CRACKED (BS 291) · airframe 65,799 hrs · 44,206 cycles

FITTING IS CRACKED ON THE AFT SIDE OF STA 291.5 AT UPPER STOP FITTING. ACFT GROUNDED. R & R FITTING IAW SRM 51-40-02-0G-0.

Part: INTERCOSTAL — CRACKED (BS 727A-727B) · airframe 65,799 hrs · 44,206 cycles

INTERCOSTAL IS CRACKED BETWEEN FS 727A AND FS 727B, S26R AND S27R. ACFT GROUNDED. INSTALLED REPLACEMENT INTERCOSTAL BETWEEN FS 727A - FS 727B, S26R AND S27R IAW DWG 69-40709 AND SRM 51-40-02-0G-0.

Part: FLOOR SUPPORT — CORRODED (BS 792) · corrosion level 2 · airframe 65,799 hrs · 44,206 cycles

AFT CARGO BS 792, LBL 13 FLOOR SUPPORT CORRODED LOWER SIDE. ACFT GROUNDED. R & R THE FLOOR SUPPORT IAW SRM 53-00-53-2R-1.

Part: FLOOR SUPPORT — CORRODED (BS 757-877) · corrosion level 2 · airframe 65,799 hrs · 44,206 cycles

AFT PIT FLOOR SUPPORT AT STA 847-857, LBL 8.1 CORRODED. ACFT GROUNDED. R & R AFT PIT FLOOR SUPPORT CHANNEL LBL 8.1, FS 757-877 IAW SRM 53-00-53-2R-1, W 1.0, O .063, R 0, L 3.0, D .063.

Part: STRINGER CLIP — CORRODED (BS 727F) · corrosion level 2 · airframe 65,799 hrs · 44,206 cycles

STRINGER CLIP IS CORRODED BETWEEN STRINGER AND CLIP AT FS 727F, S25L. ACFT GROUNDED. R & R CORRODED STRINGER CLIP AT FS 727F, STR 25L IAW SRM 51-40-02-0G-0.

Part: CARGO TRACK — CORRODED (BS 817-877) · corrosion level 2 · airframe 65,799 hrs · 44,206 cycles

AFT CARGO LT FLOOR TRACK AT LBL 17.20 CORRODED. ACFT GROUNDED. R & R DAMAGED SECTION OF CARGO TRACK IAW SRM 53-00-53-2R-2, W 1, O .071, R 0, L 36, D .071.

Part: STRINGER — CORRODED (BS 500G) · corrosion level 2 · airframe 65,799 hrs · 44,206 cycles

FWD CARGO COMPARTMENT LT AT AFT OF STA 500G, S-28 CORRODED. ACFT GROUNDED. REPAIRED STRINGER 28L IAW SRM 53-30-12-2R-2, W 1.0", O .125', R 0, L 4", D .125".

Part: FLOOR SUPPORT — CORRODED (BS 500G) · corrosion level 2 · airframe 65,799 hrs · 44,206 cycles

FWD CARGO COMPARTMENT RT AT STA 500G AND S-27 POSITION FLOOR SUPPORT CORNER ANGLE BRACKET CORRODED. ACFT GROUNDED. R & R ANGLE BRACKET FS 500G, STR 27R IAW SRM 51-40 02-0.

Part: HINGE — CRACKED (CARGO DOOR) · airframe 65,799 hrs · 44,206 cycles

MAIN CARGO DOOR AFT UPPER HINGE CRACKED SEVERAL AREAS. ACFT GROUNDED. R & R MAIN CARGO DOOR AFT HINGE ASSY IAW SRM 51-40-02-0G-0.

Part: STRINGER — CORRODED (BS 500G) · corrosion level 2 · airframe 65,799 hrs · 44,206 cycles

FWD CARGO COMPARTMENT RT AT AFT OF STA 500G, S-28, CORRODED. ACFT GROUNDED. REPAIRED STRINGER 28R IAW SRM 53-30-12-2R-2, W 1.0", O .0125", R 0", L 4", D .125".

Part: SKIN — CRACKED (BS 298-328) · airframe 65,799 hrs · 44,206 cycles

CHEM MILL CRACK AT BS 312 BETWEEN STR 19R AND 20R. ACFT GROUNDED. REPAIRED SKIN IAW SRM 53-00-01, REPAIR 31, DET XII THIS IS A CAT "B" REPAIR REFER TO OPERATORS REPAIR ASSESSMENT PROGRAM FOR INSPECTION METHODS AND INTERVALS.

Part: SNUBBER — BINDING (L1 DOOR) · airframe 65,670 hrs · 44,100 cycles

L-1 DOOR DIFFICULT TO CLOSE. ACFT GROUNDED. R & R FWD ENTRY (L-1) DOOR SNUBBER IAW AMM 52-11-71 AND ADJUSTED GUIDE ARM IAW AMM 52-11-00.

Part: DOOR — BINDING (L1) · airframe 65,393 hrs · 43,869 cycles

L1 DOOR DIFFICULT TO CLOSE FROM THE INSIDE, NOT CLOSING PROPERLY.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 64,833 hrs · 43,397 cycles

EXIT LIGHT COVER LOOSE IN FORWARD VESTIBULE. ACFT GROUNDED. REPLACED FWD VESTIBULE L1 DOOR EXIT LIGHT COVER.

Part: SIGN — DETACHED (L1 DOOR) · airframe 64,757 hrs · 43,330 cycles

EXIT LEFT FWD L1 DOOR FELL OFF. ACFT GROUNDED. REPLACED L1 DOOR EPL ASSY. OPS NORMAL.

Part: LENS — DETACHED (EMERGENCY LIGHT) · airframe 64,740 hrs · 43,317 cycles

EMERGENCY EXIT LENS BY L1 DOOR FELL OFF. ACFT GROUNDED. REINSTALLED LENS. OPS NORMAL.

Part: LENS — DISLODGED (EMERGENCY LIGHT) · airframe 64,702 hrs · 43,287 cycles

EXIT LIGHT LENS BY L1 DOOR FELL OFF OF LIGHT. ACFT GROUNDED. REPLACED L1 EMERGENCY EXIT LENS ASSY, OPS CHECKED NORMAL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 64,322 hrs · 42,933 cycles

R1 DOOR EMERGENCY EXIT LIGHT INOPERATIVE. ACFT GROUNDED. REPLACED THE LAMPS. OPS CHECKED GOOD IAW MM 33-51-11.

Part: LENS — DISLODGED (EMERGENCY LIGHT) · airframe 64,154 hrs · 42,784 cycles

EMERGENCY EXIT LIGHT COVER POPPED OFF AT L1 DOOR. ACFT GROUNDED. REPLACED MISSING LENS COVER.

Part: LENS — DETACHED (EMERGENCY LIGHT) · airframe 64,019 hrs · 42,672 cycles

EXIT LIGHT COVER NEXT TO L1 DOOR BECAME DETATCHED. ACFT GROUNDED. REATTATCHED COVER OPS CHECKED LIGHT GOOD COVER SECURE.

Part: COVER — DISLODGED (EMERGENCY LIGHT) · airframe 63,995 hrs · 42,648 cycles

F/A REPORTS EMERGENCY EXIT LIGHT SIGN, IN FWD VESTIBULE, COVER IS BROKEN. ACFT GROUNDED. REATTACHED COVER KNOCKED OFF BY L1 DOOR, OPS NORMAL.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 63,966 hrs · 42,624 cycles

L1 VESTIBULE EXIT SIGN COVER BROKEN. ACFT GROUNDED. REPLACED L1 DOOR EXIT SIGN ASSY. OPS NORMAL.

Part: SPLICE — CORRODED (BS 772-773) · corrosion level 2 · airframe 63,927 hrs · 42,595 cycles

AFT CARGO BAY FLOOR PANEL SPLICE TEE IS CORRODED AT BS 772, RBL 20-LBL20. ACFT GROUNDED. R & R SPLICE TEE IAW AMM 25-52-51-404-011.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 63,916 hrs · 42,586 cycles

EMERGENCY EXIT LIGHT COVER NEAR L1 DOOR BROKEN. ACFT GROUNDED. REPLACED LIGHT AND COVER, OPS CHECKED GOOD.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 63,897 hrs · 42,573 cycles

F/A REPORTED PLASTIC COVER ON EMERGENCY EXIT SIGN AT L1 DOOR IS BROKEN. ACFT GROUNDED. RESECURED L1 DOOR EMERGENCY EXIT SIGN COVER REF CMM 33-50-10.

Part: SIGN — DISLODGED (EMERGENCY LIGHTS) · airframe 63,745 hrs · 42,435 cycles

EMERGENCY EXIT SIGN COVER NEAR FOWARD L1 DOOR FELL OFF. ACFT GROUNDED. REINSTALLED FWD L-1 DOOR EMERGENCY EXIT SIGN COVER. OPS NORMAL.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 63,501 hrs · 42,224 cycles

SMALL EMERGENCY EXIT LIGHTED SIGN COVER NEAR L1 AND F/A PHONE STATION LOOSE AND FALLS OFF EASILY. ACFT GROUNDED. REPLACED EMERGENCY EXIT LENS AT FWD F/A STATION.

Part: LENS — BROKEN (EXIT SIGN) · airframe 63,393 hrs · 42,133 cycles

EMERGENCY EXIT SIGN COVER BROKEN. ACFT GROUNDED. REPLACED SIGN ASSY IAW MM 33-51-11, OPS GOOD.

Part: LENS — DISLODGED (EMERGENCY LIGHT) · airframe 63,354 hrs · 42,107 cycles

EMERGENCY EXIT LIGHT COVER BY L1 DOOR FEEL OFF. ACFT GROUNDED. INSTALLED NEW LENS.

Part: BEARING — OUT OF ADJUST (R2 WINDOW) · airframe 63,313 hrs · 42,076 cycles

F/O SLIDING WINDOW WILL NOT CLOSE. ACFT GROUNDED. SECURED LOOSE FWD ROLLER, OPS NORMAL REFAMM 56-12-11.

Part: LENS — DISLODGED (EMERGENCY LIGHTS) · airframe 63,161 hrs · 41,944 cycles

F/A REPORTED EMERGENCY EXIT SIGN NEAR L1 DOOR FELL OFF. ACFT GROUNDED. REPLACED DAMAGED LENS ASSY. OPS. CKS GOOD.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 63,003 hrs · 41,813 cycles

L1 DOOR EMERGENCY EXIT SIGN LENS IS BROKEN. ACFT GROUNDED. REMOVED SIGN AND INSTALLED NEW IAW AMM 33-51-11. OPS CHECKED NORMAL.

Part: DOOR — LACK OF LUBE (L1) · airframe 62,927 hrs · 41,752 cycles

L1 DOOR EASY TO OPEN BUT HARD TO CLOSE. ACFT GROUNDED. LUBED L1 DOOR. L1 DOOR OPS CHECKED NORMAL, OK FOR SERVICE. REF AMM 52-11-00-705-060.

Part: LENS — DISLODGED (EMERGENCY LIGHT) · airframe 62,802 hrs · 41,648 cycles

EXIT LIGHT COVER L1 FELL OFF. ACFT GROUNDED. INSTALLED EXIT LIGHT COVER L1 DOOR.

Part: LENS — DISLODGED (EMERGENCY LIGHT) · airframe 62,787 hrs · 41,638 cycles

F/A REPORTS L1 DOOR EXIT SIGN MISSING. ACFT GROUNDED. INSTALLED EXIT SIGN COVER LIGHT, OPS CHECKED OK.

Part: HOUSING — BROKEN (EMERGENCY LIGHT) · airframe 62,687 hrs · 41,554 cycles

L1 DOOR EXIT LIGHT BROKEN. ACFT GROUNDED. R & R L1 DOOR EXIT LIGHT ASSY, OPS CHECKED NORMAL, REF AMM 33-51-81.

Part: LAMP — UNSECURE (EMERGENCY LIGHT) · airframe 62,579 hrs · 41,467 cycles

L2 DOOR EMERGENCY EXIT LIGHT INOPERATIVE. ACFT GROUNDED. RESEATED LAMP AND OPS CK GOOD IAW MM 33-51-22-962-001.

Part: FLOOR PANEL — PUNCTURED (BS 727F-772) · airframe 62,579 hrs · 41,467 cycles

RAMP REPORTS DAMAGE ON FLOOR PANEL NR 4 AFT CARGO BAY. ACFT GROUNDED.. FABRICATED NEW FLOOR PANEL IAW SRM 51-40-05-0G-0.

Part: CHANNEL — CORRODED (DRAIN MAST) · corrosion level 2 · airframe 62,579 hrs · 41,467 cycles

AFT DRAIN MAST SUPPORT STRUCTURE INTERNAL CHANNEL CORRODED. ACFT GROUNDED. REPLACED DAMAGED CHANNEL IAW EA 400-53EA-11745, REV NEW ISSUED 08DEC13 .

Part: FRAME — CRACKED (BS 492) · airframe 62,579 hrs · 41,467 cycles

BS 492, FRAME REVEL WEB CRACKED AND PIECE MISSING ON LOWER END. ACFT GROUNDED. FABRICATED, LOCATED AND DRILLED NEW REVEAL WEB OF STA 492 IAW SRM 51-40-08-0G-0.

Part: CARGO TRACK — CORRODED (BS 540) · corrosion level 2 · airframe 62,579 hrs · 41,467 cycles

MAIN DECK CARGO CARGO LT LATERAL SEAT TRACK AND ATTACH FASTENERS AT BS 540 CORRODED. ACFT GROUNDED. REMOVED AND INSTALLED NEW CARGO TRACK IAW AMM 20-50-11-912-002

Part: FRAME — CORRODED (BS 887) · corrosion level 2 · airframe 62,579 hrs · 41,467 cycles

AFT CARGO BAY, CORROSION ON AFT SIDE OF FRAME AT BS 887 AND FIRE BOTTLE SUPPORT STRUCTURE LOWER MOUNT POINT. ACFT GROUNDED. REMOVED LT AFT TRANSITION PANEL IAW SRM 51-40-02-0G-0, PARA 4, FIG 8. FABRICATED, LOCATED AND DRILLED NEW TRANSITION PANEL IAW SRM 51-40-05-0G-0, FIG 2, DETAIL I INSTALLED NEW TRANSITION PANEL IAW SRM 51-40-02-0G-0-PARA 4, W 1.50", O .040", R .019", L 2.50", D .021".

Part: CARGO TRACK — GOUGED (BS 460) · airframe 62,579 hrs · 41,467 cycles

MAIN DECK CARGO BAY, RT LATERIAL CARGO TRACK AT BS 460 LUGS DAMAGED. ACFT GROUNDED. REMOVED RT LATERAL CARGO TRACK FOUND TO BE OUT OF LIMITS IAW SRM 53-30-84-FIG 102, SHT 3, DETAIL III. INSTALLED NEW CARGO TRACK IAW AMM 20-50-11-912-002 & BSOPM 20-41-02, STEP 6F.

Part: CARGO TRACK — CORRODED (MAIN CARGO) · corrosion level 2 · airframe 62,579 hrs · 41,467 cycles

MAIN DECK CARGO BAY RT LATERAL CARGO TRACK AT BS 500F CORRODED. ACFT GROUNDED. FOUND TO BE OUT OF LIMITS IAW SRM 53-30-84, FIG 102, SHT3 DETAIL III. INSTALLED NEW CARGO TRACK IAW AMM 20-50-11-912-002 & BSOPM 20-41-02.

Part: CARGO TRACK — CORRODED (MAIN CARGO) · corrosion level 2 · airframe 62,579 hrs · 41,467 cycles

MAIN DECK CARGO BAY, RT LATERAL CARGO TRACK BS 520 CORRODED. R & R SEAT TRACK IAW AMM 20-50-11-912-002.

Part: CARGO TRACK — CORRODED (BS 500E) · corrosion level 2 · airframe 62,579 hrs · 41,467 cycles

MAIN DECK CARGO BAY LT LATERAL CARGO TRACK AT BS 500E CORRODED. ACFT GROUNDED. FOUND TO BE OUT OF LIMITS IAW SRM 53-30-84, FIG 102, SHT 3, DETAIL III. REMOVED CARGO TRACK AND INSTALLED NEW IAW AMM 20-50-11-912-002, ORIG.

Part: CARGO TRACK — CORRODED (BS 540-612) · corrosion level 2 · airframe 62,579 hrs · 41,467 cycles

CARGO TRACK NR 3 FROM APPROX BS 540-612 AT BL0 HAS CORRODED AND BARE METAL IN SEVERAL AREAS. ACFT GROUNDED. BLENDED CORR IAW SRM 53-30-84 DETAIL VII, ON CARGO TRACK NR 3 FROM APPROX FS 540-612 AT BL0 FOUND TO BE OUT OF LIMITS IAW SRM 53-30-84, DETAIL VII, R & R CARGO TRACK IAW SRM 51-40-02-0G-0, W 1.40", O .070", R .050", L 72.0", D .020".

Part: CARGO TRACK — CORRODED (BS 480-520) · corrosion level 2 · airframe 62,579 hrs · 41,467 cycles

CARGO TRACK NR 1 FROM BS 360-520 AT BL 0 HAS LIGHT SURFACE CORROSION AND BARE METAL IN SEVERAL AREAS. ACFT GROUNDED. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-30-84. R & R SEAT TRACK IAW SRM 51-40-02-0G-0, PG 6 & ASA EA 400-53EA-04953.

Part: CARGO TRACK — CORRODED (BS 520) · corrosion level 2 · airframe 62,579 hrs · 41,467 cycles

MAIN DECK CARGO BAY LT LATERAL CARGO TRACK AND ATTACH FASTENERS, BS 520 CORRODED. ACFT GROUNDED. R & R CARGO TRACK.

Part: ANGLE — CHAFED (BS 540-545) · airframe 62,579 hrs · 41,467 cycles

GROUND AIR DOOR INBD ANGLE IS CHAFED. ACFT GROUNDED. R & R ANGLE IAW SRM 51-40-02-0G-0, PAR 4.

Part: SKIN — BENT (L1 DOOR) · airframe 62,579 hrs · 41,467 cycles

L1 DOOR INNER SKIN IS BENT ON LIGHTNING HOLE CUTOUT JUST AFT OF WINDOW OIL CANNED. ACFT GROUNDED. REPAIRED L1 DOOR SKIN IAW SRM 51-70-13-0G-0, FIG 1.

Part: ANGLE — CRACKED (LT WING) · airframe 62,579 hrs · 41,467 cycles

LT WING FIXED T/E JUST OTBD OF IFOT FAIRING HAS CRACKED ANGLE. ACFT GROUNDED. R & R ANGLE IAW SRM 51-40-02-0G-0, LT WING FIXED T/E OTBD OF IFOT FAIRING.

Part: VERTICAL SUPPORT — CRACKED (BS 294) · airframe 62,579 hrs · 41,467 cycles

E/E BAY E1 RACK RT FWD VERTICAL SUPPORT CRACKED REPAIRED E1 RACK RT FWD VERTICAL SUPPORT IAW SRM 51-70-11-0G-0.

Part: VERTICAL SUPPORT — CRACKED (BS 312) · airframe 62,579 hrs · 41,467 cycles

E & E BAY, E1 RACK RT AFT VERTICAL SUPPORT TO MOISTURE SHROUD ATTACH CRACKED. ACFT GROUNDED. REPAIRED MOISTURE SHROUD ATTACH IAW SRM 51-70-13-0G-0.

Part: STRUCTURE — CHAFED (LT WING TE FLAP) · airframe 62,579 hrs · 41,467 cycles

LT WING OTBD FOREFLAP L/E INBD CORNER IS CHAFED. FABRICATED, DRILLED AND INSTALLED NEW REPAIR DOUBLER ON LT OTBD FORELFAP INBD L/E IAW SRM 57-53-01-2R-1, FIG 201.

Part: PLATE — CHAFED · airframe 62,579 hrs · 41,467 cycles

RT T/E CLOSE OUT PANEL CHAFED OTBD NR 6 FLAP FAIRING. ACFT GROUNDED. FABRICATED NEW IAW SRM 51-40-05-0G-0, RESTORED FINISH IAW BSOPM 20-41-02.

Part: FLOOR SUPPORT — CRACKED (BS 328) · airframe 62,579 hrs · 41,467 cycles

FLOOR SUPPORT STRAP IN E & E BAY CRACKED, FS 328 AT APPROX, RBL 20. ACFT GROUNDED. REPAIRED FLOOR SUPPORT PLATE, STRAP, IAW SRM 53-10-51-2R-4.

Part: FRAME — CRACKED (BS 500D) · airframe 62,579 hrs · 41,467 cycles

FRAME BS 500D, RT SIDE, HAS A CRACK APPROX .2500 INCH LONG, ONE WIRE PENETRATION HOLE AT 4 O`CLOCK POSITION. ACFT GROUNDED. TRIMMED OUT CRACK AND INSTALLED REPAIR ANGLES AND NEW STRINGER TIES IAW SRM 53-00-07-2R-13. REPAIR 13 AT FRAME 500D RT, STR. 20-21. THIS IS A CATAGORY B REPAIR WITH INSPECTION THRESHOLD OF 66,000 FLIGHT CYCLES AND A REPEAT INSPECTION AT 24,000 FLIGHT CYCLES INTERVALS, CURRENT FLIGHT CYCLES ON ACFT IS 41,467.

Part: FRAME — CRACKED (BS 492) · airframe 67,185 hrs · 38,632 cycles

FWD CARGO DOORWAY AFT FRAME IS CRACKED .2500 AT THE UPPER RADIUS AT STA 492 (LOWER STOP PAD) INBD CORNER, DETECTED BY HFEC FROM AFT SIDE. ACFT GROUNDED. R & R FRAME AT STA 492, STR 16R-28R IAW SRM 51-40-05-0G-0 AND 51-40-02-0G-0.

Part: PANEL — GOUGED (LT WING TE FLAP) · airframe 62,579 hrs · 41,467 cycles

LT INBD T/E FLAP PANEL IS GOUGED ON LOWER SURFACE AT T/E. ACFT GROUNDED. REPAIRED PANEL IAW EA 400-57EA-11747, REV NEW ISSUED 08DEC13.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 62,285 hrs · 41,235 cycles

L1 DOOR FLOOR EMERGENCY EXIT LIGHT LENS BROKEN. ACFT GROUNDED. REPLACED L1 DOOR FLOOR EMERGENCY EXIT LIGHT LENS. OPS CHECK SAME GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 61,897 hrs · 40,906 cycles

RT WING AFT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. ALSO AISLE LIGHT, ROW 18. ACFT GROUNDED. FOUND BATTERY M1435 CEILING PANEL RT SIDE ROW 23-24 BAD. REPLACED M1435 BATTERY PACK. OPS CHECK IT, RT WING EXT AFT 2, & AISLE ROW 18 EMERGENCY EXIT LIGHTS GOOD.

Part: LENS — DISLODGED (EMERGENCY LIGHT) · airframe 61,593 hrs · 40,624 cycles

EXIT SIGN BY L1 DOOR FELL OFF. ACFT GROUNDED. REPLACED LENS COVER, SECURED.

Part: LENS — DETACHED (EMERGENCY LIGHT) · airframe 61,394 hrs · 40,436 cycles

L1 DOOR EXIT SIGN DETACHED. ACFT GROUNDED. ATTACHED COVER FOR EXIT SIGN L-1.

Part: WINDOW — OUT OF ADJUST (COCKPIT) · airframe 61,371 hrs · 40,416 cycles

CAPTAIN`S WINDOW WILL NOT OPEN. ACFT GROUNDED. ADJUSTED LOWER FORE AND AFT BELCRANK ARM, REF 56-12-11, OPS CHECK NORMAL.

Part: SLIDING WINDOW — INOPERATIVE (COCKPIT) · airframe 61,306 hrs · 40,363 cycles

CAPTAINS SLIDING WINDOW WOULD NOT OPEN. ACFT GROUNDED. CLEANED DIRT AND DEBRIS FROM WINDOW TRACK, OPS NORMAL.

Part: GUIDE ARM — LACK OF LUBE (L1 DOOR) · airframe 61,244 hrs · 40,310 cycles

L1 DOOR HARD TO CLOSE. ACFT GROUNDED. LUBRICATED UPPER AND LOWER DOOR HINGE ARMS. REF MM 12-25-21. MADE SMALL ADJUSTMENT TO L1 DOOR GUIDE ARM IAW MM 52-11-00-705-007, STEP G. ACCOMPLISHED L1 DOOR TEST IAW MM 52-11-00-755-051. OPS TEST GOOD. DOOR HANDLE TORQUES ARE WITHIN LIMITS DURING ALL PHASES OF DOOR OPERATION.

Part: LAMP — INOPERATIVE (RT OVERWING EXI) · airframe 61,077 hrs · 40,166 cycles

RT WING LOWER EMERGENCY LIGHT INOPERATIVE. ACFT GROUNDED. REPLACED LAMP, OPS NORMAL.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 60,742 hrs · 39,871 cycles

EMERGENCY EXIT LT COVER BROKEN ON L-1 DOOR NEXT TO F/A SEAT. REPLACED COVER L-1 DOOR AND LIGHT ASSY OPS CK GOOD REF MM 33-51-41.

Part: LENS — UNSECURE (EMERGENCY LIGHT) · airframe 60,556 hrs · 39,707 cycles

F/A REPORTS WHITE LIGHT COVER NEXT TO PHONE/ OUTSIDE FWD F/A JUMPSEAT KEEPS FALLING OFF. ATTACHED & SECURED FWD ENTRY EMERGENCY EXIT LT COVER. OPS CHECKED NORMAL.

Part: SIGN — UNSECURE (PAX CABIN) · airframe 60,537 hrs · 39,690 cycles

EXIT SIGN COVER NEXT TO (OTBD) FWD F/A JUMP SEAT FELL OFF. REPOSITIONED EMERGENCY EXIT SIGN COVER IAW MM 33-51-11-032-030.

Part: GUIDE ARM — OUT OF ADJUST (R2 DOOR) · airframe 59,812 hrs · 39,036 cycles

F/A STATES R2 DOOR REQUIRES MORE THAN NORMAL EFFORT TO OPEN AND SEEMS TO BE BINDING IN THE DOOR OPENING. ADJUSTED R2 DOOR GUIDE ARM IAW AMM 52-41-21-404-004, STEP 6. R2 DOOR OPERATES CORRECTLY IAW AMM 52-41-21-714-010.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 59,718 hrs · 38,947 cycles

EXIT LIGHT COVER MISSING NEAR L1 DOOR. INSTALLED NEW EXIT LIGHT COVER FWD BULKHEAD AT L1 DOOR AREA.

Part: SLIDING WINDOW — STICKS (COCKPIT) · airframe 59,642 hrs · 38,887 cycles

PILOT SLIDING WINDOW STICKS AS IT SLIDES AFT. OPEN

Part: FITTING — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 59,642 hrs · 38,887 cycles

LEFT INBD MIDFLAP, INBD TORQUE TUBE, INBD RIB HAS SURFACE CORROSION. ACFT GROUNDED. R & R NEW RIB FITTING IAW SRM 51 40 02.

Part: SEAT TRACK — CRACKED (BS 629-727) · airframe 59,642 hrs · 38,887 cycles

LEFT OTBD SEAT TRACK AT BS 727 CRACKED. REPAIRED DAMAGED SEAT TRACK IAW SRM 53 00 52, FIG 201, REPAIR 6.

Part: ATTACH ANGLE — CRACKED (BS 291.5) · airframe 61,580 hrs · 33,748 cycles

DURING R-1 HINGE CUTOUT INSP, FOUND STA 291.5, STR 9R INTERCOSTAL ATTACH ANGLE APPEARS TO BE CRACKED. ACFT GROUNDED. R & R WITH NEW INTERCOSTAL ATTACH ANGLE IAW SRM-51-40-02, PGS 2, 10 & 30.

Part: SEAT TRACK — CORRODED (BS 500C) · corrosion level 2 · airframe 59,642 hrs · 38,887 cycles

SEAT TRACK AT BS 500C ON LT SIDE HAS SURFACE CORROSION. ACFT GROUNDED. REMOVED CORROSION AND CHECKED LIMITS IAW SRM 53-30-84, FIG 102. R & R SEAT TRACK IAW SRM 51 40 02, PG 6, PARA D.

Part: FRAME — CRACKED (BS 942 S24L) · airframe 59,642 hrs · 38,887 cycles

AFT FUSELAGE SKIN CRACKED 2.5 LONG AT BS 942 ABOVE STR 24L IN CHEM MILLED EDGE. REPAIRED FUSELAGE SKIN CRACK IAW ASA EA NR 400 53, EA 08922.

Part: FRAME — CRACKED (BS 500B) · airframe 59,642 hrs · 38,887 cycles

FRAME AT BS 500B HAS A CRACK AT 1.04 WIRE PENETRATION HOLE 900 POS AS VIEWED LOOKING AFT EXTENDING INWARD APROX .1250 LONG. ACFT GROUNDED. REPAIRED FRAME IAW SRM 53-00-07, REP 13.

Part: SEAT TRACK — CORRODED (BS 520) · corrosion level 2 · airframe 59,642 hrs · 38,887 cycles

SEAT TRACK AT STA 520 ON RT SIDE HAS SURFACE CORROSION. ACFT GROUNDED. REMOVED CORROSION AND CHECKED LIMITS FOUND TO BE OUT OF LIMITS IAW SRM 53-30-84, FIG 102. R & R SEAT TRACK IAW SRM 51 40 02, PG 6, PAR D W 1.00 O .230 R .197 L .033 D .033

Part: SEAT TRACK — CORRODED (BS 500C) · corrosion level 2 · airframe 59,642 hrs · 38,887 cycles

SEAT TRACK AT STA 500C ON LT SIDE HAS SURFACE CORROSION. ACFT GROUNDED. REMOVED CORROSION AND CHECKED LIMITS IAW SRM 53 30 84, FIG 102. R & R SEAT TRACK IAW SRM 51-40-02, PG 6, PARA D, W 1.00, O .230, R .0195, L .035, D .035.

Part: FRAME — CRACKED (BS 500B) · airframe 59,642 hrs · 38,887 cycles

FRAME AT BS 500 RT HAS AT 1.04 WIRE PENETRATION HOLE 300, POS AS VIEWED LOOKING AFT EXTENDING INWARD APPROX .2500 LONG. ACFT GROUNDED. REPAIRED FRAME IAW SRM 53-00-07, REPAIR 13.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 58,589 hrs · 37,947 cycles

L1 DOOR EMERGENCY EXIT LIGHT LENS COVER BROKEN. REPLACED L1 DOOR LENS COVER WITH SERVICABLE UNIT. OK FOR SERVICE.

Part: DOOR — BINDING (L1) · airframe 58,108 hrs · 37,512 cycles

L1 DOOR DIFFICULT TO CLOSE. VISUALLY INSPECTED DOOR NO DEFECTS NOTED. PERFORMED TORQUE CHECK ON FORCE REQUIRED TO OPERATE DOOR. TORQUE IS WITHIN LIMITS SPECIFIED IN AMM 52-11-00-755-051 PAGE 2 STEP D5.

Part: BOLT — LOOSE (L1 DOOR) · airframe 57,815 hrs · 37,243 cycles

F/A REPORTS L1 DOOR HANDLE HARD TO CLOSE. ACCOMPLISHED L1 DOOR TORQUE TEST PER AMM 52 11 00 755 051 STEP D5 D AND D5 E. TORQUE WAS OVER LIMITS ON BOTH STEPS. NOTE FOUND UPPER GUIDE ARM FITTING ON DOOR MOUNT BOLTS LOOSE TIGHTENED MOUNT BOLTS. ADJ GUIDE ARM PER 52 11 705 007 STEP (G).

Part: LENS — MISSING (L1 DOOR) · airframe 57,655 hrs · 37,101 cycles

COVER L1 EMERGENCY LT LOWER MISSING. INSTALLED NEW COVER L1 DOOR.

Part: BATTERY — DISCHARGED (CABIN) · airframe 56,851 hrs · 36,385 cycles

RT AFT AND R2 DOOR EMERGENCY LTS INOP ON TEST. REPLACED BATT M1137, OPS CHECK NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 56,811 hrs · 36,349 cycles

EMERGENCY LIGHTS INOP: CENTER AISLE OVERHEAD AT WING EXITS BULLNOSE RT/SIDE ROW 20, 24, 27. R2 DOOR LT ABOVE DOOR AND EXIT R2 DOOR EXTERNAL SLIDE LIGHT. REPLACED BATTERY PACK AND CHARGER AT STATION/LOCATION M1134 AND M1197 REF AMM 33 50 00, OPS GOOD.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 56,313 hrs · 35,895 cycles

DURING AFT PIT AFT BULKHEAD SUPPORT INSTALL FOUND LT BULKHEAD LOWER SUPPORT CORRODED ABOVE STR 25L. REMOVED ANGLE FABRICATED AND INSTALLED REPLACEMENT PART IAW B737 400 SRM 51 30 01 AND 51 40 02.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 56,313 hrs · 35,895 cycles

LATERAL TRACK LUG DAMAGE RT BS 560. REMOVED AND REPLACED LATERAL TRACK IAW PEMCO SRM 53 30 84 DETAIL III FIG 102 AND B737 400 SRM 51 40 02.

Part: STRIP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,313 hrs · 35,895 cycles

FWD PIT RT NR 3 CAP STRIP IS CORRODED. FABRICATED AND INSTALLED NEW CAP STRIP IAW B737 400 SRM 53 30 53 FIG 101.

Part: STRIP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,313 hrs · 35,895 cycles

FWD PIT NR 2 CAP STRIP IS CORRODED. FABRICATED AND INSTALLED NEW CAP STRIP IAW B737 400 SRM 53 30 53 FIG 101.

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 56,313 hrs · 35,895 cycles

RT LATERAL SEAT TRACK GOUGED BS 380. REMOVED AND REPLACED SEAT TRACK IAW B737 400 SRM 51 40 02.

Part: STIFFENER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,313 hrs · 35,895 cycles

AFT PRESSURE BULKHEAD Z STIFFENER IS CORRODED. REMOVED DAMAGED AREA, FABRICATED REPAIR PARTS AND INSTALLED REPAIR IAW ASA EA 400 53EA 05609.

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 56,313 hrs · 35,895 cycles

RT LATERAL FLOOR TRACK AT BS 460 GOUGED SEVERAL PLACES. FABRICATED NEW LATERAL SEAT TRACK AND INSTALLED IAW B737 400 SRM 51 40 05 PEMCO 737 400 SRM 53 30 84 BAC1520 841.

Part: BULKHEAD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,313 hrs · 35,895 cycles

AFT PRESSURE BULKHEAD WEB FORWARD SIDE CORRODED. REMOVED DAMAGED AREA, FABRICATED FILLER AND DOUBLER AND INSTALLED REPAIR IAW ASA EA 400 53EA 05609.

Part: SEAT TRACK — CHAFED (FUSELAGE) · airframe 56,313 hrs · 35,895 cycles

LT LATERAL FLOOR TRACK CHAFED BS 540. REMOVED AND REPLACED LATERAL TRACK IAW B737 400 SRM 51 40 02.

Part: SKIN — DELAMINATED (SPOILER) · airframe 56,313 hrs · 35,895 cycles

LT WING NR 0 SPOILER UPPER SURFACE EXISTING REPAIR DOUBLER DELAMINATED. REMOVED DAMAGED AREA, FABRICATED REPAIR PARTS AND BONDED IAW B737 400 SRM 51 70 10 REPAIR 4.

Part: SKIN — DEBONDED (NR 8 SPOILER) · airframe 56,313 hrs · 35,895 cycles

NR 8 SPOILER LOWER SURFACE PREVIOUS REPAIR IS DISBONDING. REMOVED PREVIOUS REPAIR FABRICATED REPAIR PARTS AND BONDED REPAIR IAW SRM 51-70-10 REPAIR 2.

Part: SKIN — DENTED (SPOILER) · airframe 56,313 hrs · 35,895 cycles

NR 8 SPOILER UPPER SURFACE HAS MULTIPLE PROTRUDING DENTS. REMOVED DAMAGED AREA, FABRICATED FILLER AND DOUBLER AND BONDED IAW B737 400 SRM 51-70-01 REPAIR 4.

Part: SKIN — DELAMINATED (FOREFLAP) · airframe 56,313 hrs · 35,895 cycles

RT INBOARD FORE FLAP UPPER SURFACE DELAMINATION. REMOVED DAMAGED AREA, FABRICATED REPAIR PARTS AND BONDED IAW B737 400 SRM 51 70 10 REPAIR 4.

Part: FLAP — DENTED (RT WING) · airframe 56,313 hrs · 35,895 cycles

RT INBOARD FORE FLAP HAS A SHARP DENT 66 INCHES FROM INBOARD END. REMOVED DAMAGED AREA FABRICATED REPAIR PARTS AND BONDED IAW B737 400 SRM 51 70 10 REPAIR 4.

Part: FLAP — CHAFED (RT WING) · airframe 56,313 hrs · 35,895 cycles

RT OUTBOARD FOREFLAP OUTBOARD LEADING EDGE IS CHAFED. REPAIRED L/E IAW B737 400 SRM 57 53 01 FIG 201.

Part: SUPPORT FITTING — CHAFED (FOREFLAP) · airframe 56,313 hrs · 35,895 cycles

LT OUTBOARD FORE FLAP LOWER OUTBOARD BEARING SUPPORT FITTING CHAFED. REMOVED AND REPLACED FITTING IAW B737 400 SRM 51 40 02.

Part: CLOSEOUT PANEL — CHAFED (RT WING) · airframe 56,313 hrs · 35,895 cycles

RIGHT WING CLOSE OUT PANEL JUST OUTBOARD OF THE NR 6 FLAP TRACK FAIRING IS CHAFED. REMOVED DAMAGED PANEL FABRICATED AND INSTALLED NEW CLOSE OUT PANEL AND SEALS IAW B737 400 SRM 51 40 05.

Part: SUPPORT FITTING — CHAFED (FOREFLAP) · airframe 56,313 hrs · 35,895 cycles

LT OUTBOARD FORE FLAP OUTBOARD UPPER BEARING SUPPORT FITTING CHAFED. REMOVED AND REPLACED SUPPORT FITTING IAW B737 400 SRM 51 40 02.

Part: SKIN — DENTED (VERTICAL STAB) · airframe 56,313 hrs · 35,895 cycles

VERTICAL STAB L/E HAS A DENT WITH SCRIBE LINE LOCATED 7 FT FROM TOP OF VERTICAL STAB L/E FIN STA 231 231. REPAIRED DAMAGED AREA IAW B737 400 SRM 55 30 01.

Part: REPAIR — CHAFED (FOEFLAP) · airframe 56,313 hrs · 35,895 cycles

RT OUTBOARD FOREFLAP INBOARD LEADING EDGE IS CHAFED IN PREVIOUS REPAIR. REPAIRED L/E IAW B737 400 SRM 57 53 61.

Part: SKIN — DELAMINATED (SPOILER) · airframe 56,313 hrs · 35,895 cycles

NR 7 SPOILER HAS PROTRUDING DENTS WITH DELAMINATION UPPER SURFACE. REMOVED DAMAGED AREA, FABRICATED FILLER AND DOUBLER AND BONDED IAW B737 400 SRM 51 70 10 REPAIR 4.

Part: GUIDE ARM — WORN (L1 DOOR) · airframe 56,256 hrs · 35,848 cycles

L1 (FORWARD ENTRY) DOOR HARD TO CLOSE FROM INSIDE. REMOVED AND REPLACED GUIDE ARM IAW B737 400 AMM 52 11 21. OPERATIONAL CHECK NORMAL.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 56,313 hrs · 35,895 cycles

EXTERIOR SKIN AT STA 727E + 9" AT STR 24R HAS A NICK/DENT. REMOVED DAMAGED SKIN FABRICATED REPAIR PARTS AND INSTALLED REPAIR IAW B737 400 SRM 53 00 01 FIG 201 REPAIR 31.

Part: SKIN — NICKED (FUSELAGE) · airframe 55,948 hrs · 35,579 cycles

NICK ON FUSELAGE SKIN (EXTERIOR) 9 INCHES FORWARD OF BS 727E AT STR 24R LOCATION. ACCOMPLISHED TEMPORARY REPAIR PER SRM 53-00-01 ALLOWABLE DAMAGE 1. REMOVED DAMAGED SKIN FABRICATED REPAIR PARTS AND INSTALLED IAW SRM 53-00-01 REPAIR 31.

Part: FLAP — DELAMINATED (LT WING) · airframe 56,313 hrs · 35,895 cycles

LEFT OUTBOARD FOREFLAP DAMAGED 30 IN FROM INBOARD END. REMOVED DAMAGED AREA, FABRICATED REPAIR PARTS AND BONDED IAW B737 400 SRM 51 70 10 REPAIR 3 AND 4.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 55,553 hrs · 35,241 cycles

INTERIOR OVERWING EMERGENCY EXIT LIGHTING PANELS INOP RIGHT & LEFT LOWER PANELS INOP. REPLACED BATTERY PACK M1134 AT STA 634 PER B737 400 AMM 33 51 51.

Part: SKIN — DENTED (FOREFLAP) · airframe 53,266 hrs · 33,204 cycles

LEFT I/B FORE FLAP UPPER SURFACE DENTED 18 INCHES FROM O/B END. REMOVED DAMAGED AREA, FABBED PARTS AND BONDED.

Part: SLAT — DELAMINATED (WING) · airframe 53,266 hrs · 33,204 cycles

NUMBER 3 SLAT O/B TRAILING EDGE CORNER DELAMINATED. REPAIRED DAMAGE TO NR 3 SLAT.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 53,266 hrs · 33,204 cycles

RT WING NR 5 SLAT I/B UPPER SURFACE HAS 1 DELAMINATED AREA. REPAIRED DAMAGE TO RT WING NR 5 SLAT.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,266 hrs · 33,204 cycles

R2 DOOR CUTOUT AFT JAMB LOWER FRAME CORRODED AT CREASE BEAM. CUT OUT DAMAGED SECTION OF FRAME AND SPLICED IN NEW.

Part: PANEL — DAMAGED (AILERON) · airframe 53,266 hrs · 33,204 cycles

RIGHT WING AILERON HAS MULTIPLE AREAS OF DAMAGE ON COVE PANEL LANDINGS. REPAIRED DAMAGED AREAS IAW EA 400 57EA 03176.

Part: SKIN — CHAFED (MIDFLAP) · airframe 53,266 hrs · 33,204 cycles

RIGHT WING OUTBOARD MID FLAP LOWER SURFACE SKIN T/E CHAFED JUST OUTBOARD OF NR 8 TRACK. CUT OUT DAMAGE, INSTALLED FILLER AND TWO EACH EXTERNAL REPAIR DOUBLER IAW 400 57EA 03179.

Part: STRAP — DAMAGED (FUSELAGE) · airframe 53,266 hrs · 33,204 cycles

SCRIBE LINE AT FS 360. LENGTH 2.2 IN. UPPER STR 9R DISTANCE FROM UPPER STRINGER CENTERLINE 4.9 IN. LOWER STR 10R DISTANCE FROM LOWER STRINGER CENTERLINE 1.3 INCH MAX DEPTH 0.002 INCH. REMOVED STRAP, FABRICATED AND INSTALLED NEW STRAP IAW B737 SRM 51 40 05 AND 51 40 02.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,266 hrs · 33,204 cycles

FS 520 RBL 50 LATERAL SEAT TRACK HAS LIGHT CORROSION. REPAIRED SEAT TRACK IAW EA 400 53EA 03126.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,266 hrs · 33,204 cycles

FS 500 RBL 50 LATERAL SEAT TRACK HAS LIGHT CORROSION. REMOVED AND REPLACED SEAT TRACK IAW EA 400 53EA 03126.

Part: WEDGE — DENTED (MIDFLAP) · airframe 53,266 hrs · 33,204 cycles

RIGHT I/B MID FLAP WEDGE LOWER SURFACE DENTED 15 INCHES FROM I/B END 6 INCHES FROM AFT EDGE. REPAIRED BY INSTALLING 2024 T3 .016 FILLER AND DOUBLER IAW B737 400 SRM 51 70 10 REPAIR 4.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,266 hrs · 33,204 cycles

FS 500D LBL 50 LATERAL SEAT TRACK IS CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EA 400 53EA 03126.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,266 hrs · 33,204 cycles

FS 500G RBL 50 LATERAL SEAT TRACK HAS LIGHT CORROSION.

Part: RIB — GOUGED (AILERON) · airframe 53,266 hrs · 33,204 cycles

LT AILERON 4TH FRAME FROM OUTBOARD IS GOUGED. REMOVED AND REPLACED NOSE RIB LT AILERON IAW B737 SRM 51 40 02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,266 hrs · 33,204 cycles

UPPER FLANGE OF FLOORBOARD SUPPORT STA 270 & BL 0 IS CORRODED. REPAIRED UPPER FLANGE OF Z-CHORD BY CUTTING OUT DAMAGE AND INSTALLING 0.063 INCH 7075 T6 REPAIR ANGLE AND FILLER IAW EA 400 53EA 03120.

Part: AILERON — DAMAGED (LT WING) · airframe 53,266 hrs · 33,204 cycles

LT AILERON CARBON FIBER COVE PANEL MISSING MATERIAL. TRIMMED AND SEALED AILERON.

Part: AILERON — DELAMINATED (LT WING) · airframe 53,266 hrs · 33,204 cycles

MULTIPLE AREAS OF DELAMINATION ON LEFT AILERON OUTBOARD. TRIMMED AND SEALED DELAMINATION.

Part: SKIN — CHAFED (AILERON) · airframe 53,266 hrs · 33,204 cycles

LT AILERON BOTTOM SKIN IS CHAFED NEAR CONTROL ROD HINGE POINT. BLENDED AND SEALED SKIN.

Part: AILERON — DELAMINATED (LT WING) · airframe 53,266 hrs · 33,204 cycles

LT AILERON COVE PANEL LOCATED AT THE MID INBOARD HINGE IS DELAMINATED. TRIMMED AND SEALED AILERON.

Part: STRINGER — DAMAGED (FUSELAGE) · airframe 532,663 hrs · 33,204 cycles

STRINGER 21L STA 440 HAS HOLE IN IT. REMOVED DAMAGED SECTION, FABRICATED AND INSTALLED REPAIR J-ANGLE.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,266 hrs · 33,204 cycles

LT FRAME 727D IS CRACKED BETWEEN STR 8 & 9. REPAIRED FRAME WITH DOUBLERS.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,266 hrs · 33,204 cycles

LT FUSELAGE FRAME CRACKED BETWEEN STR 8L AND 9L AT STA 867. INSTALLED DOUBLERS.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,266 hrs · 33,204 cycles

RT FRAME 787 IS CRACKED BETWEEN STR 8 & 9. REPAIRED FRAME WITH DOUBLERS.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,266 hrs · 33,204 cycles

LT FRAME AT 827 CRACKED. REPAIRED FRAME WITH DOUBLERS.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,266 hrs · 33,204 cycles

LT FRAME 787 IS CRACKED BETWEEN STR 8 & 9. REPAIRED FRAME WITH DOUBLERS.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,266 hrs · 33,204 cycles

RT FUSELAGE FRAME CRACKED. REPAIRED FRAME WITH DOUBLERS.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,266 hrs · 33,204 cycles

RT FRAME AT 907 CRACKED BETWEEN STR 8 AND 9. REPAIRED FRAME WITH DOUBLERS.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,266 hrs · 33,204 cycles

LT FRAME AT 727F CRACKED BETWEEN STR 8 AND 9. REPAIRED FRAME WITH DOUBLERS.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,266 hrs · 33,204 cycles

LT FRAME 747 IS CRACKED BETWEEN STR 8 & 9. REPAIRED FRAME WITH DOUBLERS.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,266 hrs · 33,204 cycles

RT FRAME 867 IS CRACKED BETWEEN STR 8 & 9. REPAIRED FRAME WITH DOUBLERS.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,266 hrs · 33,204 cycles

RT FRAME AT 747 CRACKED BETWEEN STR 8 AND 9. REPAIRED FRAME WITH DOUBLERS.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,266 hrs · 33,204 cycles

LT FRAME AT 907 CRACKED BETWEEN STR 8 AND 9. REPAIRED FRAME WITH DOUBLERS.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,266 hrs · 33,204 cycles

RT FRAME AT 727F CRACKED BETWEEN STR 8 AND 9. REPAIRED FRAME WITH DOUBLERS.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 532,663 hrs · 33,204 cycles

FLOORBEAM STA 967 REPAIR SECTION CORRODED. CUT OUT DAMAGED SECTION. INSTALLED REPAIR ANGLE.

Part: RIB — CRACKED (LT WING) · airframe 53,266 hrs · 33,204 cycles

LT WING LOWER RIB CHORD CRACKED AFT OF NR 2 STRINGER. INSTALLED TWO FILLERS AND REPAIR T'S.

Part: SKIN — DENTED (FOREFLAP) · airframe 53,266 hrs · 33,204 cycles

LEFT O/B FORE FLAP LOWER SKIN HAS CLUSTER OF DENTS. REPAIRED DENT DAMAGE.

Part: SKIN — DAMAGED (RUDDER) · airframe 532,663 hrs · 33,204 cycles

RUDDER HAS DAMAGE AT AFT LOWER CORNER. REPAIRED SKIN DAMAGE.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 532,663 hrs · 33,204 cycles

SCRIBE LINE AT 908 LENGTH 19.5 INCHES UPPER STR 2L TO LOWER STR 4L MAX DEPTH .002 INCH. REMOVED DAMAGED DOUBLER. TREATED PRIMED AND INSTALLED NEW DOUBLER.

Part: SKIN — CORRODED (FUSELAGE) · airframe 532,663 hrs · 33,204 cycles

FUSELAGE SKIN CORRODED UNDER LOWER MARKER BEACON ANTENNA STA 620. REMOVED, FABRICATED AND INSTALLED NEW SKIN.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,266 hrs · 33,204 cycles

STR CLIP CRACKED STA 807 AND STR 4 RT. REMOVED AND REPLACED STR CLIP.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 53,266 hrs · 33,204 cycles

STA 500E FRAME TO STR 26L ATTACHING CLIP IS CRACKED. REMOVED AND REPLACED CRACKED CLIP.

Part: FRAME — DENTED (FUSELAGE) · airframe 53,266 hrs · 33,204 cycles

AFT PIT FRAME AT 727E UPPER FLANGE DENTED BETWEEN STR 22L AND 23L. INSTALLED REPAIR DOUBLER.

Part: WEDGE — DELAMINATED (MIDFLAP) · airframe 53,266 hrs · 33,204 cycles

RIGHT I/B MIDFLAP WEDGE LOWER SURFACE DELAMINATED 1 INCH FROM T/E 44 INCHES FROM I/B END. REPAIRED DAMAGED AREA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,266 hrs · 33,204 cycles

STA 500B FRAME TO STR 23L ATTACH CLIP IS CRACKED. REMOVED AND REPLACED CLIP.

Part: FRAME — DENTED (FUSELAGE) · airframe 53,266 hrs · 33,204 cycles

AFT PIT FRAME AT 727C DENTED BETWEEN STR 23L AND 24L. INSTALLED REPAIR DOUBLER.

Part: FRAME — DENTED (FUSELAGE) · airframe 53,266 hrs · 33,204 cycles

AFT PIT TOP OF FRAME AT 727G DENTED ABOVE STR 24R. INSTALLED REPAIR DOUBLER.

Part: SKIN — DELAMINATED (SPOILER) · airframe 53,266 hrs · 33,204 cycles

NR 5 SPOILER LOWER SKIN REPAIR DELAMINATED 6 INCHES AFT OF L/E AT PANEL CENTER. REMOVED DAMAGED REPAIR AND INSTALLED DOUBLER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,266 hrs · 33,204 cycles

RT FRAME AT 727D CRACKED BETWEEN STR 8 AND 9. REPAIRED FRAME WITH DOUBLERS.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 53,266 hrs · 33,204 cycles

LEFT WING LOWER SKIN ON NR 3 SLAT DOUBLER AT I/B AND DISBONDED. INSTALLED DOUBLER.

Part: FLANGE — DELAMINATED (AILERON) · airframe 53,266 hrs · 33,204 cycles

RT AILERON INBOARD LOWER AREA OF FORWARD FLANGE DELAMINATED. REMOVED DAMAGED AREA AND REPAIRED.

Part: STRAP — CORRODED (FUSELAGE) · airframe 53,266 hrs · 33,204 cycles

FLOORBEAM RBL 24 BETWEEN STA 1006 1025. REMOVED DAMAGED STRAP, FABRICATED AND INSTALLED NEW STRAP.

Part: FRAME — GOUGED (FUSELAGE) · airframe 53,266 hrs · 33,204 cycles

FRAME AT 727A STR 25L IS GOUGED. REPAIRED FRAME.

Part: STRINGER CLIP — GOUGED (FUSELAGE) · airframe 53,266 hrs · 33,204 cycles

STR CLIP DAMAGED AT STA 500C AND STR 5. REMOVED AND REPLACED STR CLIP.

Part: STRINGER CLIP — GOUGED (FUSELAGE) · airframe 53,266 hrs · 33,204 cycles

STR CLIP DAMAGED AT STA 520 AND STR 5. REMOVED AND REPLACED STR CLIP.

Part: STRINGER CLIP — GOUGED (FUSELAGE) · airframe 53,266 hrs · 33,204 cycles

STR CLIP DAMAGED AT STA 500E AND STR 5. REMOVED AND REPLACED STR CLIP.

Part: SKIN — GOUGED (RT ELEVATOR) · airframe 53,266 hrs · 33,204 cycles

RT ELEVATOR LOWER SURFACE IS DAMAGED 10 INCHES FROM T/E BONDED REPAIR OF ELEVATOR.

Part: STRINGER CLIP — GOUGED (FUSELAGE) · airframe 53,266 hrs · 33,204 cycles

STR CLIP DAMAGED AT STA 500D AND STR 5. REMOVED AND REPLACED STR CLIP.

Part: BEAR STRAP — CORRODED (FUSELAGE) · airframe 532,663 hrs · 33,204 cycles

FWD CARGO DOOR CUTOUT AFT LOWER CORNER CORRODED. REMOVED DAMAGED SECTION OF BEAR STRAP. FABRICATED AND INSTALLED REPAIR DOUBLER AND TRIPLER.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 53,266 hrs · 33,204 cycles

LT WING L/E NR 3 SLAT I/B TRAILING EDGE DELAMINATED. INSTALLED DOUBLER.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 53,266 hrs · 33,204 cycles

RT WING NR 6 SLAT I/B UPPER SURFACE HAS 2 INCH DELAMINATION AREA MARKED. REPAIRED WITH DOUBLER.

Part: STRINGER CLIP — GOUGED (FUSELAGE) · airframe 53,266 hrs · 33,204 cycles

STA 727D LT STR 10 CLIP CRACKED. REMOVED AND REPLACED CLIP.

Part: FITTING — GOUGED (FUSELAGE) · airframe 53,266 hrs · 33,204 cycles

SILL INSTALLED AFT ENTRY DOOR LWR MAIN: APB FLOOR SUPPORT FITTING BOLT HOLE IS GOUGED AT BOLT 81L. REPLACED APB FITTING IAW B737 400 SRM 51 40 02 AND 51 40 05.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 53,266 hrs · 33,204 cycles

FS 520 LBL 50 SEAT TRACK IS CORRODED. REMOVED AND REPLACED SEAT TRACK IAW B737 SRM 51 40 02 PG 4 AND EA 400 53EA 03126 REV NEW.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 53,266 hrs · 33,204 cycles

SCRIBE LINE AT FS 500C LENGTH 18 INCHES UPPER STR 1 DISTANCE FROM STRINGER CENTERLINE 9.5 INCHES. LOWER STR 4R DISTANCE FROM LOWER STRINGER CENTERLINE 1.5 INCHES. MAX DEPTH 2 SCRIBES AT 0.002 INCH. REMOVED AND REPLACED DAMAGED SPLICE STRAP IAW B737 400 SRM 51 40 02.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,266 hrs · 33,204 cycles

FS 500D RBL 50 LATERAL SEAT TRACK IS CORRODED. REPAIRED SEAT TRACK IAW EA 400 53EA 03126 REV NEW DATED 03/24/10.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,266 hrs · 33,204 cycles

FS 500E LBL 50 LATERAL SEAT TRACK HAS LIGHT CORROSION. REPAIRED SEAT TRACK IAW EA 400 53EA 03126 REV NEW DATED 03/24/10.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,266 hrs · 33,204 cycles

FS 600 RBL 50 LATERAL SEAT TRACK HAS LIGHT CORROSION. REPLACED SEAT TRACK IAW EA 400 53EA 03126 REV NEW DATED 03/24/10.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,266 hrs · 33,204 cycles

FS 500F RBL 50 LATERAL SEAT TRACK HAS LIGHT CORROSION. REPAIRED SEAT TRACK IAW EA 400 53EA 03126 REV NEW DATED 03/24/10.

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 53,266 hrs · 33,204 cycles

FS 460 RBL 50 LATERAL SEAT TRACK IS GOUGED. REMOVED AND REPLACED SEAT TRACK IAW EA 400 53EA 03126.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,266 hrs · 33,204 cycles

FS 500E RBL 50 LATERAL SEAT TRACK IS CORRODED. REPLACED SEAT TRACK IAW EA 400 53EA 03126 REV NEW DATED 03/24/10.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,266 hrs · 33,204 cycles

FS 500A RBL 50 LATERAL SEAT TRACK HAS LIGHT CORROSION. REPAIRED SEAT TRACK IAW EA 400 53EA 03126 REV NEW DATED 03/24/10.

Part: SILL — CRACKED (FUSELAGE) · airframe 532,663 hrs · 33,204 cycles

MOP SILL STA 530 - 536 LT SIDE CRACKED ACROSS SPLICE. REMOVED DAMAGED SECTION, FABRICATED AND INSTALLED MOP SILL.

Part: STRINGER — GOUGED (FUSELAGE) · airframe 53,266 hrs · 33,204 cycles

AFT CABIN S12L INNER SURFACE IS GOUGED. STRINGER OUT OF LIMITS. REMOVED AND REPLACED THE STRINGER.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 53,266 hrs · 33,204 cycles

MAIN CARGO DOOR INNER INTERCOSTAL IS CRACKED ABOVE FWD ACTUATOR MOUNT FITTING. REMOVED AND REPLACED DAMAGED INTERCOSTAL IAW B737 400 SRM 51 40 02.

Part: BEAM — DAMAGED (NR 1 PYLON) · airframe 53,266 hrs · 33,204 cycles

NR 1 ENGINE AFT PYLON FAIRING HORIZONTAL I BEAM AT APPROX NAC STA 314 CENTER ATTACH FITTING HAS 2 FASTENERS PULLING THROUGH BEAM AND FITTING. FABRICATED HORIZONTAL BEAM AND FITTING AND INSTALLED.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 53,266 hrs · 33,204 cycles

FLOORBEAM AT FS 987 RBL 10 REPAIRED SECTION HAS CORROSION IN MULTIPLE AREAS. REMOVED REPAIR SECTION, FABRICATED REPAIR CHORD, SPLICES AND INSTALLED REPAIR PARTS.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 53,266 hrs · 33,204 cycles

MAIN CARGO DOOR INNER INTERCOSTAL IS CRACKED BELOW AFT ACTUATOR LOWER FITTING. REMOVED AND REPLACED INTERCOSTAL.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 53,266 hrs · 33,204 cycles

FLOORBEAM UPPER CAP AT STA 294 RBL 44. REMOVED DAMAGED FLOORBEAM UPPER CAP, FABRICATED NEW AND INSTALLED.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 53,266 hrs · 33,204 cycles

FLOORBEAM AT FS 947 LBL 15 TO RBL 15 REPAIRED SECTION HAS CORROSION IN MULTIPLE AREAS. REMOVED REPAIR SECTION, FABRICATED REPAIR CHORD, ANGLES AND INSTALLED REPAIR PARTS.

Part: SILL — CORRODED (FUSELAGE) · airframe 53,266 hrs · 33,204 cycles

R2 DOOR HAS MULTIPLE AREAS OF CORROSION LOCATED AT DOOR CUTOUT MOP SILL. REMOVED CORRODED MOP SILL MATCH, DRILLED NEW MOP SILL AND INSTALLED IAW B737 SRM 51 40 02.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,266 hrs · 33,204 cycles

CABIN FRAME CRACKED AT FS 400R STRINGER 8R. REMOVED DAMAGED AREA, FABRICATED REPAIR ANGLES AND INSTALLED REPAIR PARTS.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,266 hrs · 33,204 cycles

CABIN FRAME CRACKED AT FS 380 RT AT STRINGER 8R. CUT OUT DAMAGED SECTION IN FRAME, FABRICATED AND INSTALLED REPAIRS.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,266 hrs · 33,204 cycles

CABIN FRAME CRACKED AT FS 440 RT AT STRINGER 8R TO 9R. CUT OUT DAMAGED SECTION IN FRAME, FABRICATED AND INSTALLED REPAIRS.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 53,266 hrs · 33,204 cycles

APU BAY RT TORQUE BOX AIR INLET CUTOUT UPPER BEAM CORRODED FS 1121. REMOVED CORRODED STRINGER AND INSTALLED NEW STRINGER.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 53,266 hrs · 33,204 cycles

APU COMPARTMENT TORQUE BOX AIR INLET CUTOUT LOWER STRINGER CORRODED AT FS 1121 RBL 12. REMOVED AND REPLACED STRINGER AT STA 1121.

Part: FAILSAFE — GOUGED (FUSELAGE) · airframe 53,266 hrs · 33,204 cycles

AFT PIT FRAME FAIL SAFE ANGLE IS GOUGED SEVERAL PLACES ON O/B SIDE OF INTERCOSTAL FWD ATTACH ANGLE. REMOVED AND REPLACED ANGLE.

Part: SKIN — DENTED (TE FLAP) · airframe 53,266 hrs · 33,204 cycles

RIGHT I/B AFT FLAP LWR SURFACE DENTED OUT OF LIMITS. REPAIRED RIGHT I/B AFT FLAP LWR SURFACE.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 53,266 hrs · 33,204 cycles

SCRIBE LINE AT FS 727G LENGTH 2.2 INCH UPPER STRINGER 10R. DISTANCE FROM UPPER STRINGER CENTERLINE 1.5 INCH LOWER STRINGER 11R. DISTANCE FROM LOWER STRINGER CENTERLINE 4.8 INCH. MAX DEPTH 0.001 INCH. REMOVED AND REPLACED DAMAGED SECTION OF SPLICE PLATE IAW EA 400 53EA 03141 REV NEW DATED 03/26/10.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 53,266 hrs · 33,204 cycles

SCRIBE LINE AT FS 727G LENGTH 22 INCHES, UPPER STR 4L. DISTANCE FROM UPPER STRINGER CENTERLINE 0.0 INCH, LOWER STR 7L. DISTANCE FROM LOWER STRINGER 5.3 INCHES. MAX DEPTH 0.003 INCH. REMOVED AND REPLACED DAMAGED SECTION OF SPLICE STRAP IAW EA 53EA 03141 REV NEW DATED 03/26/10.

Part: SKIN — DENTED (SPOILER) · airframe 53,266 hrs · 33,204 cycles

NR 4 SPOILER HAS 2 CREASED DENTS 30 INCHES FROM I/B EDGE. REPAIRED NR 4 SPOILER SURFACE.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 53,266 hrs · 33,204 cycles

SCRIBE LINE AT FS 727G LENGTH 2.0 INCHES UPPER STR 5R. DISTANCE FROM UPPER STRINGER 3.5 INCHES LOWER STR 6R. DISTANCE FROM LOWER STRINGER CENTERLINE 3.9 INCHES. MAX DEPTH 0.002 INCH. REMOVED AND REPLACED DAMAGED SECTION OF SPLICE STRAP IAW EA 400 53EA 03141 REV NEW DATED 03/26/10.

Part: SKIN — DELAMINATED (SPOILER) · airframe 53,266 hrs · 33,204 cycles

NR 5 SPOILER UPPER SURFACE O/B PREVIOUS REPAIR DELAMINATED. REPAIRED NR 5 SPOILER SURFACE.

Part: SKIN — PERFORATED (RUDDER) · airframe 53,266 hrs · 33,204 cycles

RUDDER HAS PERFORATION ON LOWER RT SECTION. REPAIRED SKIN DAMAGE.

Part: SKIN — SCRATCHED (FUSELAGE) · airframe 53,266 hrs · 33,204 cycles

SCRIBE LINE AT STA 727G LENGTH 0.8 INCH UPPER STRINGER 3R. DISTANCE FROM STRINGER CENTERLINE 5 INCHES LOWER STRINGER 4R DISTANCE FROM LOWER STRINGER CENTERLINE 3.7 INCHES MAX DEPTH 0.002 INCH. REMOVED AND REPLACED SPLICE STRAP IAW B737 400 SRM 51 40 02.

Part: SKIN — DAMAGED (FOREFLAP) · airframe 532,663 hrs · 33,204 cycles

LEFT WING I/B FOREFLAP LWR SURFACE HAS SEVERAL CLUSTER OF DENTS SOME OF WHICH ARE CREASED AND PUNCTURED. REPAIRED THE LEFT I/B FOREFLAP.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 53,266 hrs · 33,204 cycles

LEFT WING L/E NR 1 SLAT INBOARD T/E DELAMINATED. REPAIRED DAMAGE TO LEFT WING NR 1 SLAT.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 53,266 hrs · 33,204 cycles

EXTERNAL FUSELAGE SKIN HAS A DENT WITH A GOUGE LOCATED AT STA 500C+16 BELOW STR 22L. CUT OUT DAMAGE AREA, FABRICATED REPAIR DOUBLER AND TRIPLER, AND INSTALLED.

Part: SKIN — DENTED (FUSELAGE) · airframe 53,266 hrs · 33,204 cycles

DAMAGED SKIN. REMOVED DAMAGED SKIN AND INSTALLED NEW SKIN.

Part: GUIDE ARM — OUT OF ADJUST (L1 DOOR) · airframe 51,318 hrs · 31,454 cycles

PILOT REPORTS L1 DOOR HARD TO CLOSE ADJUSTED L1 DOOR GUIDE ARM. OPS CHECKS OK, REF AMM 52 01 00 FIG 104.

Part: DOOR — OUT OF ADJUST (L1 DOOR) · airframe 50,590 hrs · 30,832 cycles

FORWARD ENTRY DOOR (L1) WILL NOT CLOSE. ADJUSTED FWD ENTRY DOOR PER MM 52 11 00 705 007. NON ASA EMP 442702827.

Part: INTERCOSTAL — DAMAGED (FUSELAGE) · airframe 50,588 hrs · 30,830 cycles

INTERCOSTAL AT BS 727A - 727B RBL 19 HAS OVERSIZED NR 40 HOLES NUT PLATES. REMOVED AND REPLACED INTERCOSTAL.

Part: LIGHT — DIRTY (CABIN) · airframe 50,588 hrs · 30,830 cycles

PHOTO LUMINESCENT FLOOR PROX LIGHTING FAILS TEST. AVG SHOULD BE 50 LUX IS 23 LUX. REPLACED ALL LT AND RT PAX CEILING LIGHTS PER MM 33-21-12. CLEANED INSIDE AND OUTSIDE CEILING LIGHT LENS COVERS PER SOPM 20-30-03.

Part: SKIN PANEL — CRACKED (ELEVATOR) · airframe 50,588 hrs · 30,830 cycles

PANEL 344KB IS CRACKED. R&R 344KB PANEL

Part: SUPPORT — DAMAGED (FUSELAGE) · airframe 50,588 hrs · 30,830 cycles

AFT CARGO BAY SIDEWALL SUPPORT AT FRAME 787 HAS OVERSIZED HOLE AT LOWER END. REPAIRED SIDEWALL SUPPORT.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 50,588 hrs · 30,830 cycles

CAPSTRIP IS GOUGED AND HAS CORROSION. REMOVED CAPSTRIP, FABRICATED NEW CAPSTRIP.

Part: SEAL DEPRESSOR — GOUGED (FUSELAGE) · airframe 50,588 hrs · 30,830 cycles

MAIN CARGO DOOR CUTOUT SEAL DEPRESSOR DAMAGED/GOUGED AFT LOWER CORNER. REPLACED CUTOUT SEAL DEPRESSOR.

Part: SUPPORT — DAMAGED (FUSELAGE) · airframe 50,588 hrs · 30,830 cycles

AFT CARGO BAY SIDEWALL SUPPORT AT FRAME 727G HAS OVERSIZED HOLE LBL 21.7. REPAIRED SIDEWALL SUPPORT.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,588 hrs · 30,830 cycles

RIGHT FLOOR SUPPORT RBL 25 HAS AREAS OF CORROSION FROM BS 727D 727F.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,588 hrs · 30,830 cycles

RIGHT FLOOR SUPPORT RBL 25 HAS AREAS OF CORROSION FROM BS 727D THRU 727F. REPAIRED FLOOR SUPPORT ZEE.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 50,588 hrs · 30,830 cycles

FRAME BS 727F AT FLOOR TO SIDEWALL SUPPORT HAS ENLARGED FASTENER HOLES LEFT. REPAIRED.

Part: BEAR STRAP — CRACKED (BS 303 S10L) · airframe 50,588 hrs · 30,830 cycles

L1 DOOR LOWER HINGE CUTOUT FASTENER HOLE CRACKED IN BEAR STRAP. REPAIRED PER EA 400-53EA-00721.

Part: BEAR STRAP — CRACKED (BS 303) · airframe 50,588 hrs · 30,830 cycles

L1 DOOR LOWER HINGE CUTOUT FASTENER HOLE CRACKED IN BEAR STRAP. REPAIRED PER EA 400-53EA-00721.

Part: WEB — CORRODED (BS 847-851) · airframe 50,588 hrs · 30,830 cycles

CORROSION ON WEB AT NUTPLATE. REMOVED AND REPLACED WEB.

Part: SHEAR TIE — CORRODED (BS 727G S26-27L) · airframe 50,588 hrs · 30,830 cycles

CORROSION ON SHEAR TIE BS 727G LT BETWEEN STR 27 & 26. REMOVED AND REPLACED SHEAR TIE.

Part: STRUCTURE — CORRODED (BS 727D-727F) · corrosion level 2 · airframe 50,588 hrs · 30,830 cycles

CAPSTRIP CORROSION ON IT FABRICATED AND REPLACED CAPSTRIP.

Part: THRESHOLD — CRACKED (BS 440-490) · airframe 50,588 hrs · 30,830 cycles

FWD CARGO DOOR SUB THRESHOLD WEB IS CRACKED. REPLACED WEB.

Part: FRAME — DAMAGED (BS 727C) · airframe 50,588 hrs · 30,830 cycles

AFT CARGO BAY FRAME AT BS 727C HAS OVERSIZED HOLES COMMON TO FLOOR TO SIDEWALL SUPPORT. REPAIRED FRAME AT BS 727C.

Part: FRAME — DAMAGED (BS 787) · airframe 50,588 hrs · 30,830 cycles

AFT CARGO BAY FRAME AT BS 787 HAS OVERSIZED HOLES COMMON TO FLOOR TO SIDEWALL SUPPORT. REPAIRED AFT CARGO BAY FRAME AT 787.

Part: FRAME — DAMAGED (BS 727G) · airframe 50,588 hrs · 30,830 cycles

AFT CARGO BAY FRAME AT BS 727G HAS OVERSIZED HOLES COMMON TO FLOOR TO SIDEWALL SUPPORT. REPAIRED AFT CARGO BAY FRAME AT 727G.

Part: SUPPORT — CORRODED (BS 727-760) · airframe 50,588 hrs · 30,830 cycles

AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT HAS CORROSION. REPLACED SUPPORT.

Part: SKIN — GOUGED (BS 860-887) · airframe 50,588 hrs · 30,830 cycles

UPPER FUSELAGE SKIN AT DORSAL FIN MOUNT AREA IS GOUGED. FABRICATED AND INSTALLED REPAIR PARTS.

Part: FRAME — DAMAGED (BS 727D) · airframe 50,588 hrs · 30,830 cycles

AFT CARGO BAY FRAME AT BS 727D HAS OVERSIZED HOLES COMMON TO FLOOR TO SIDEWALL SUPPORT. REPAIRED ACB FRAME AT 727D.

Part: FRAME — DAMAGED (BS 727B) · airframe 50,588 hrs · 30,830 cycles

AFT CARGO BAY FRAME AT BS 727B HAS OVERSIZED HOLES COMMON TO FLOOR TO SIDEWALL SUPPORT. FABRICATED AND INSTALLED REPAIR PARTS.

Part: FRAME — DAMAGED (BS 767) · airframe 50,588 hrs · 30,830 cycles

AFT CARGO BAY FRAME AT BS 767 HAS OVERSIZED HOLES COMMON TO FLOOR TO SIDEWALL SUPPORT. REPAIRED AFT CARGO BAY FRAME AT 767.

Part: FRAME — DAMAGED (BS 747) · airframe 50,588 hrs · 30,830 cycles

AFT CARGO BAY FRAME AT BS 747 HAS OVERSIZED HOLES COMMON TO FLOOR TO SIDEWALL SUPPORT. REPAIRED AFT CARGO BAY FRAME AT 747.

Part: FRAME — DAMAGED (BS 807) · airframe 50,588 hrs · 30,830 cycles

AFT CARGO BAY FRAME AT BS 807 HAS OVERSIZED HOLES COMMON TO FLOOR TO SIDEWALL SUPPORT. FABRICATED AND INSTALLED REPAIR PARTS.

Part: FRAME — DAMAGED (BS 727E) · airframe 50,588 hrs · 30,830 cycles

FRAME AT BS 727E HAS OVERSIZED HOLES COMMON TO FLOOR TO SIDEWALL SUPPORT AT RBL 19 AND 21. REPAIRED FRAME AT BS 727E RBL 19.

Part: FRAME — DAMAGED (BS 727F) · airframe 50,588 hrs · 30,830 cycles

ACB FRAME AT BS 727F HAS OVERSIZED HOLES COMMON TO FLOOR TO SIDEWALL SUPPORT AT RBL 19 AND 21. REPAIRED AFT CARGO BAY FRAME AT 727F AT RBL 19 AND RBL 21.7.

Part: FRAME — DAMAGED (BS 727A) · airframe 50,588 hrs · 30,830 cycles

FRAME AT BS 727A HAS OVERSIZED HOLES COMMON TO FLOOR TO SIDEWALL SUPPORT AT RBL 19 AND 21. REPAIRED OVERSIZED HOLE.

Part: FRAME — DAMAGED (BS 767) · airframe 50,588 hrs · 30,830 cycles

AFT CARGO BAY FRAME AT BS 727G HAS OVERSIZED HOLES COMMON TO FLOOR TO SIDEWALL SUPPORT. DISCREPANCY REPAIRED ON MIG 5.

Part: FRAME — DAMAGED (BS 727G) · airframe 50,588 hrs · 30,830 cycles

AFT CARGO BAY SUBFRAME AT .5 INCHES FORWARD OFBS 727G HAS OVERSIZED HOLES COMMON TO FLOOR TO SIDEWALL SUPPORT. REPAIRED SUB FRAME AT BS 727G.

Part: FRAME — DAMAGED (BS 727G) · airframe 50,588 hrs · 30,830 cycles

AFT CARGO BAY FRAME AT BS 727G HAS OVERSIZED HOLES COMMON TO FLOOR TO SIDEWALL SUPPORT AT LBL 19 AND 21. REPAIRED FRAME AT BS 727G LBL 21 IAW SRM 51 70 11.

Part: FRAME — DAMAGED (BS 747) · airframe 50,588 hrs · 30,830 cycles

ACB FRAME AT BS 747 HAS OVERSIZED HOLES COMMON TO FLOOR TO SIDEWALL SUPPORT AT RBL 19 AND 21. REPAIRED FRAME AT BS 747.

Part: FLOORBEAM — CRACKED (BS 537) · airframe 50,588 hrs · 30,830 cycles

FLOORBEAM CRACKED. R&R.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 50,588 hrs · 30,830 cycles

FRAME 727A HAS OVERSIZED HOLES COMMON TO FLOOR TO SIDEWALL SUPPORT RBL 19 AND RBL 21.7. FABRICATED AND INSTALLED REPAIR PARTS.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 50,588 hrs · 30,830 cycles

CARGO BAY CAPSTRIP CORRODED. FABRICATED AND REPLACED CAPSTRIP.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 50,588 hrs · 30,830 cycles

CAPSTRIP BS727D TO BS727F LT SIDE HAS AREAS OF CORROSION. FABRICATED AND REPLACED CAPSTRIP.

Part: SKIN — GOUGED (BS 309 S10-12L) · airframe 50,588 hrs · 30,830 cycles

FUSELAGE SKIN GOUGED BS 309 BELOW FWD ENTRY DOOR UPPER HINGE FITTING. REMOVED, FABRICATED NEW SKIN AND INSTALLED.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 50,588 hrs · 30,830 cycles

CARGO BAY CAPSTRIP CORRODED. FABRICATED AND REPLACED CAPSTRIP.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 50,588 hrs · 30,830 cycles

CAPSTRIP BS 727D LT SIDE HAS AREAS OF CORROSION. REMOVED CAPSTRIP, FABRICATED NEW CAPSTRIP AND INSTALLED.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 50,588 hrs · 30,830 cycles

CAPSTRIP RT BS727 TO BS727D SIDE HAS AREAS OF CORROSION. REMOVED CAPSTRIP, FABRICATED NEW STRIP.

Part: SKIN — CHAFED (NR 4 SLAT) · airframe 50,588 hrs · 30,830 cycles

NR 4 SLAT CHAFFING ON TE LOWER SURFACE AT IB SIDE CORE WITH INTERNAL DOUBLER AND EXTERNAL DOUBLER BONDED REPAIR. REPAIRED NR 4 SLAT TE WEDGE IB END BY ACCOMPLISHING FULL DEPTH BOND.

Part: FLOOR PANEL — DENTED (BS 727-727D) · airframe 50,588 hrs · 30,830 cycles

AFT CARGO BAY NR 1 FLOOR PANEL DENTED AND GOUGED. REPLACED FLOOR PANEL.

Part: FLOOR PANEL — DAMAGED (BS 727D-727F) · airframe 50,588 hrs · 30,830 cycles

AFT CARGO BAY NR 2 FLOOR PANEL DENTS AND GOUGED. REPLACED FLOOR PANEL.

Part: SCUFF PLATE — WORN (FUSELAGE) · airframe 50,588 hrs · 30,830 cycles

AFT CARGO BAY SCUFF PLATE WORN THROUGH. R&R SCUFF PLATE.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 50,588 hrs · 30,830 cycles

FLOOR SUPPORT CHANNEL CRACKED. R&R.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 50,588 hrs · 30,830 cycles

FLOOR SUPPORT CRACKED PAX CABIN. R&R FLOOR SUPPORT.

Part: CLOSEOUT PANEL — CRACKED (FUSELAGE) · airframe 50,588 hrs · 30,830 cycles

FORWARD ENTRY DOOR UPPER STOP FITTING CLOSE OUT PANEL IS CRACKED. REMOVED AND REPLACED PANEL.

Part: SEAT TRACK — WORN (FUSELAGE) · airframe 50,588 hrs · 30,830 cycles

RT LATERAL SEAT TRACK AT BS 480 WORN OB AND IB ENDS. REMOVED AND REPLACED SEAT TRACK SEGMENT.

Part: REVEAL — DAMAGED (FUSELAGE) · airframe 50,588 hrs · 30,830 cycles

AFT CARGO COMPARTMENT AFT DOOR FRAME CLOSE OUT LOWER WEB IS DAMAGED. REMOVED FABBED AND INSTALLED NEW CLOSEOUT WEB PER DWG 65 56654/65 47960.

Part: SCUFF PLATE — WORN (FUSELAGE) · airframe 50,588 hrs · 30,830 cycles

FWD CARGO BAY SCUFF PLATE HAS A HOLE WORN THROUGH. REPLACED.

Part: SKIN — DENTED (LT HORIZ STAB) · airframe 50,588 hrs · 30,830 cycles

LT HORIZONTAL STAB DENTED 100" FROM IB END. REPAIRED LT HORIZONTAL STAB LEADING EDGE.

Part: RELEASE MECH — LACK OF LUBE (L1 DOOR) · airframe 49,891 hrs · 30,223 cycles

L1 DOOR SAFETY RELEASE STUCK IN OPEN POSITION. LUBRICATED LATCH RELEASE, OP'S NORMAL. OK FOR SERVICE.

Part: FLAP — SPLIT (LEFT) · airframe 43,610 hrs · 25,029 cycles

LT OB AFT FLAP IB END T/E SPLIT. REMOVED AND REPLACED LT OB FLAP IAW AMM. (K)

Part: SPAR — DAMAGED (LT AILERON)

PAE - FOUND LEFT AILERON, OUTBOARD HINGE ACCESS PANEL ATTACH POINT DAMAGED. REPLACED LEFT AILERON LOWER FRONT SPAR. (M)

Part: SKIN — DENTED (SPOILER ASSEMBLY)

PAE - FOUND DENT ON LOWER SURFACE OF RIGHT GROUND SPOILER 3 INCHES OUTBOARD OF INBOARD END. REPAIRED RIGHT GROUND SPOILER NR 5. (M)

Part: ACCESS PANEL — SCRATCHED (FUSELAGE)

PAE - FOUND SCRATCH DAMAGE JUST AFT OF AFT LAVATORY SERVICE PANEL, SCRATCHES WERE BLENDED AND FOUND TO BE OUT OF ALLOWABLE LIMITS PER SRM 53-00-01. REPAIRED SCRATCH/GOUGE AT STAITON 1006/STRINER 25R. (M)

Part: SKIN — DENTED (FUSELAGE)

GYR - FOUND LWER FUSELAGE BELLY SKIN HAS DENT AFT OF FRAME AT STATION 807 BETWEEN STRINGER 27L AND 27R. REMOVED DAMAGED AREA AND REINSTALLED DOUBLER PER SRM 53-00-01, DETAIL XI PG 368 AT STATION 807 BETWEEN STRINGER 27L AND 27R. LOWER FUSELAGE BELLY SKIN. (M)

Part: FRAME — DAMAGED (FUSELAGE)

GYR - FOUND AFT PIT STAITON 787 LEFT SIDE FRAME ZEE ANGLE ATTACHMENT HOLES ARE DAMAGED. REMOVED DAMGAED AREA AT FS 787 LEFT FRAME. FABRICATED REPAIR REF SRM 51-70-11. TREATED, PRIMED AND APPLIED TOPCOAT, REF 51-20-01, AND INSTALLED REPAIR REF 51-40-02. (M)

Part: SKIN — DAMAGED (FUSELAGE)

GYR - FOUND LOWER FUSELAGE BELLY SKIN IS CREASED ALONG THE FRAME AT FS 827 BETWEEN STRINGER 27L AND 27R. TRIMMED OUT DAMAGED AREA AND REINSTALLED REPAIR DOUBELR PER SRM 53-00-01 DETAIL 11 PAGE 368 AT STATION 827 BETWEEN STRINGER 27L AND 27R LOWER FUSELAGE. (M)

Part: SKIN — DENTED (FUSELAGE)

GYR - FOUND LOWER FUSELAGE BELLY SKIN HAS DENT AFT OF FRAME AT FS 767 BETWEEN STRINGER 27L AND 27R. TRIMMED OUT DAMAGED AREA AND REINSTALLED REPAIR DOUBLER PER SRM 53-00-01 DETAIL 11 PAGE 368 AT STATION 767 BETWEEN STRINGER 27L AND 27R LOWER FUSELAGE. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

GYR - FOUND BS 986.5 FLOORBEAM IS CORRODED RBL 8 TO RBL 44. SPLICED IN NEW UPPER CAP OF TEE CHORD FLOORBEAM FROM RBL 8 TO RBL 53. (M)

Part: FLOORBEAM — CORRODED (FUSLEAGE)

GYR - FOUND BS 947.5 FLOORBEAM IS CORRODED LBL 20 TO RBL 20. REPAIRED FLOORBEAM IAW REO A00224. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

GYR - FOUND CORROSION ON FLOORBEAM. REPAIRED FLOORBEAM PER SRM. (M)

Part: LIGHT — INOPERATIVE (ROW 3-7)

LAS - DURING MAINTENANCE, FOUND EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE FROM ROWS 3-7. RESECURED AND CONNECTED FLOOR TRACK WIRING. OPS CHECKED GOOD. (M)

Part: WIRE — INOPERATIVE (EMERGENCY LIGHT)

DURING MAINTENANCE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS AT MID CABIN INOPERATIVE. REPAIRED WIRE ADN OPERATIONAL CHECKED GOOD. (M)

Part: WIRE — DAMAGED (CABIN)

PDX - FOUND TRACK LIGHTS INOPERATIVE AT ROW 14-17. REPAIRED, WIRES OPS CHECKED NORMAL. (M)

Part: FAN — FAULTY (RIGHT)

SEA - AT FLIGHT LEVEL 330, RAPID INCREASE IN ELECTRICAL BURNING SMELL FOLLOW WITH A HAZE IN THE CABIN. RIGHT CABIN AIR RECIRC FAN CIRCUIT BREAKER POPPED. SMELL AND HAZE DISSIPATED RAPIDLY ON DESCENT. REMOVED AND REPLACED RIGHT RECIRC FAN, OPS CHECKED NORMAL. (M)

Part: WIRE — BROKEN (CABIN)

FAI - DURING LINE CHECK, FOUND EMERGENCY TRACK LIGHTING AT ROW 16 INOPERATIVE. REPLACED BROKEN WIRE. LIGHTS THEN FUNCTIONED PROPERLY. (M)

Part: STRAP — CORRODED (FUSELAGE)

PAE - DURING C-CHECK, FOUND CORROSION ON INTERNAL FRAME STRAP AT BS 794, RBL 23, WL 157 IN AFT CARGO BAY. REPAIRED IAW EA. (M)

Part: FRAME — CORRODED (FUSELAGE)

PAE - DURING C-CHECK, FOUND CORROSION ON FRAME AT BS 794, RBL 23, WL 154 AFT CARGO BAY. REPAIRED IAW EA. (M)

Part: DOUBLER — CORRODED (FUSELAGE)

PAE - DURING C-CHECK, FOUND CORROSION ON INTERNAL FRAME DOUBLER AT BS 794, RBL 23, WL 155 IN AFT CARGO BAY. REPAIRED PER EA. (M)

Part: SKIN — CRACKED (GALLEY DOOR)

PAE - DURING C-CHECK, FOUND CRACK ON FORWARD GALLEY DOOR LOWER HINGE CUT OUT. REPAIRED IAW EA. (M)

Part: SKIN — DENTED (CARGO DOOR)

PAE - DURING C-CHECK, FOUND AFT CARGO DOOR HAS NUMEROUS DENTS OUT OF LIMITS. REMOVED AND REPLACED AFT CARGO DOOR SKIN IAW SRM. (M)

Part: LIGHT — DISCONNECTED (CABIN)

ANC - DURING LINE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTING INOPERATIVE AT ROW 19 TO 20. RECONNECTED EMERGENCY FLOOR TRACK LIGHTING. OPERATIONS CHECK GOOD. (M)

Part: WIRE — DISCONNECTED (ROW 26)

PDX - PRIOR TO FLIGHT 521 - THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROWS 26 AND AFT WERE FOUND TO BE INOPERATIVE. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROWS 12 AND 13 WERE FOUND TO BE INOPERATIVE. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

PDX - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (M)

Part: ARM — OUT OF ADJ (PAX DOOR)

PDX - PRIOR TO FLIGHT 316, THE L1 DOOR CLOSED NORMALLY, BUT WAS VERY DIFFICULT TO LATCH. LUBRICATED L1 DOOR AND ADJUSTED GUIDE ARM, DOOR OPERATED NORMALLY. (M)

Part: SNUBBER — DAMAGED (PAX DOOR)

SEA - PRIOR TO FLT 457, THE L1 DOOR WAS DIFFICULT TO CLOSE. REPLACED THE L1 DOOR SNUBBER AND THE DOOR OPERATED NORMALLY. (M)

Part: FLOORBEAM — CORRODED (BS 344)

PHX - DURING SI CHECK, FOUND MAIN CABIN FLOORBEAM CORRODED AT STATION 344, LBL 14. REPAIRED PER EA 5310-01682. (M)

Part: SEAT TRACK — GOUGED (BS 889)

PHX - DURING SI CHECK, FOUND MAIN CABIN LEFT OUTBOARD SEAT TRACK GOUGED AT STATION 889. REPAIRED PER SRM 53-00-52. (M)

Part: FLOORBEAM — CORRODED (BS 986)

PHX - DURING SI CHECK, FOUND FLOORBEAM T-CAP AT BS 986, RBL 8 CORRODED ON AFT FLANGE. REPAIRED PER SRM 53-00-51, FIG 203. (M)

Part: FLOORBEAM — CORRODED (BS 967)

PHX - DURING SI CHECK, FOUND MAIN FLOORBEAM T-CAP AT BS 967, LBL 30 CORRODED AROUND SCREW HOLES ON TOP AND BOTTOM SIDES. REPAIRED PER SRM 53-60-51, FIG 203. (M)

Part: ANGLE — CORRODED (BS 297-337)

PHX - DURING SI CHECK, FOUND MAIN CABIN RIGHT CUSP ANGLE AT STATION 279-337 CORRODED ON UPPER SURFACE OF HORIZONTAL FLANGE. REPAIRED PER SRM 51-40-2. (M)

Part: FLOORBEAM — CORRODED (BS 947.5)

PHX - DURING SI CHECK, FOUND FLOORBEAM T-CAP AT BS 947.5, RBL 48 CORRODED AROUND SCREW HOLES ON FORWARD SIDE. REPAIRED PER SRM 53-60-51, FIG 203. (M)

Part: FLOORBEAM — CORRODED (BS 986)

PHX - DURING SI CHECK, FOUND MAIN FLOORBEAM T-CAP AT BS 986, LBL 34 CORRODED AROUND SCREW HOLES. REPAIRED PER SRM 53-60-51, FIG 203. (M)

Part: FLOORBEAM — CORRODED (BS 312)

PHX - DURING SI CHECK, FOUND MAIN CABIN FLOORBEAM CORRODED AT STATION 312, LBL 1. REPAIRED PER SRM 53-10-51, FIG 205. (M)

Part: FLOORBEAM — CORRODED (BS 294.5)

SEA - DURING SI CHECK, FOUND MAIN CABIN FLOORBEAM, BS 294.5, RBL 18 TO 50 CORRODED ON UPPER CHORD. REPAIRED PER SRM 53-10-51, FIG 205. (M)

Part: FLOORBEAM — CORRODED (BS 360)

SEA - DURING SI CHECK, FOUND MAIN CABIN FLOORBEAM, BS 360, RLB 20.5 AND 25.5 CORRODED ON UPPER CHORD. REPAIRED PER SRM 53-00-51, FIG 201. (M)

Part: FLOORBEAM — CORRODED (BS 986)

SEA - DURING SI CHECK, FOUND CORROSION AROUND SCREW HOLES ON MAIN CABIN FLOORBEAM T-CP AT STATION 986 AND LBL 17 THROUGH 33. REPAIRED PER SRM 53-60-51, FIG 203. (M)

Part: LIGHT — INOPERATIVE (R2 DOOR)

SEA - DURING MAINTENANCE CHECK THE R2 DOOR OVERHEAD EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. REPLACED LIGHT ASSEMBLY AND LIGHT OPERATED NORMALLY. (X)

Part: RECORDER — MALFUNCTIONED (CABIN)

SEA - FLT 517 - DURING FLT SNA-SEA, CREW NOTICED ACRID SMELL IN FLT DECK. CO-PILOT INVESTIGATED AND OBSERVED PASSENGER ADDRESS TAPE REPORDUCER SMOKING. CREW PULLED TAPE REPRODUCER CIRCUIT BREAKER AND SMOKE STOPPED. AIRCRAFT LANDED IN SE A WITHOUT INCIDENT. MAINTENANCE VERIFIED CIRCUIT BREAKER PULLED AND COLLARED. AIRCRAFT WAS RELEASED PER MEL 25-10. MAINTENANCE SUBSEQUENTLY REPLACED TAPE REPRODUCER ON 5/29/98, OPS NORMAL. ORIGINAL TAPE REPORDUCER WAS SENT TO ASA AVIONICS SHOP FOR TROUBLESHOOTING AND REPAIR. (M)

Part: MECHANISM — LACK OF LUBE (L1 DOOR)

OAK - PRIOR TO FLT 469 - THE L1 DOOR HANDLE WAS FOUND TO BE HARD TO CLOSE. LUBED AND CYCLED DOOR, OPERATED NORMAL. (M)

Part: DUST COVER — BENT (L-1 DOOR)

ANC - FLT 82 - CREW REPORTED, L1 DOOR DIFFICULT TO CLOSE. FOUND DUST COVER ON LOWER HINGE BENT, STRAIGHTENED COVER AND DOOR OPERATED NORMALLY. (M)

Part: FRAME — ELONGATED HOLE (BS 727)

SEA - DURING C-CHECK, THE AFT CARGO COMPARTMENT INNER FLANGE OF THE FUSELAGE FRAME AT STATION 727D WAS FOUND TO HAVE AN ELONGATED HOLE BETWEEN STRINGERS 26R AND 27R. REPAIRED IAW ASA EA 5310-01516. (M)

Part: SOCKET — INOPERATIVE (CABIN)

JNU - DURING MAINTENANCE CHECK, THE AFT FOUR EMERGENCY EXITFLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. REPLACED TRACK LIGHT LAMP SOCKETAND ALL LIGHTS OPERATED NORMALLY.(M)

Part: EEL ASSY — BROKEN (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT LIGHT AT THE L-2 DOOR WAS FOUND BROKEN. REPLACED LIGHT ASSEMBLY AND LIGHT OPERATED NORMALLY. (X)

Part: EEL REFLECTOR — WORN (L-2 DOOR)

SEA - DURING MAINTENANCE CHECK, THE L-2 DOOR EXTERIOR EMERGENCY LIGHT WAS FOUND INOPERATIVE. REPLACED REFLECTOR/SOCKET ASSEMBLY AND LIGHT OPERATED NORMALLY. (M)

Part: EEL ASSY — DEFECTIVE (CABIN)

SEA - ON ARRIVAL OF FLT NR 103, CREW REPORTED THE EMERGENCY EXIT FLOOR TRACK LIGHTS FROM ROWS 10 TO 13 WERE FOUND INOPERATIVE. RECONNECTED WIRING AND REPLACED LIGHT ASSEMBLY AT ROW 11 AND LIGHTS OPERATED NORMALLY. REFERENCE ASAA9540049.

Part: EEL WIRING — DISCONNECTED (CABIN)

SEA - ON ARRIVAL OF FLT NR 103, CREW REPORTED THE EMERGENCY EXIT FLOOR TRACK LIGHTS FROM ROWS 10 TO 13 WERE FOUND INOPERATIVE. RECONNECTED WIRING AND REPLACED LIGHT ASSEMBLY AT ROW 11 AND LIGHTS OPERATED NORMALLY. (M)

Part: EEL WIRING — DISCONNECTED (CABIN)

SEA - FLT NR 413 - EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROWS 11 AND 12 WERE FOUND INOPERATIVE. RECONNECTED WIRING AT ROWS 11 AND 12, LIGHTS OPERATED NORMALLY. (M)

Part: EEL WIRING — DISCONNECTED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROW 12 WERE FOUND INOPERATIVE. REPAIRED TRACK WIRING AND LIGHTS OPERATED NORMALLY. (W)

Part: EEL WIRING — DISCONNECTED (CABIN)

SEA - ROW NR 9 WHITE FLOOR EMERGENCY LIGHT INOP. MAINTENANCE RECONNECTED LOOSE WIRE. (M)

Part: EEL WIRING — DISCONNECTED (CABIN)

SEA - AT CHECK, TRACK LIGHTS AT ROWS 14 TO 17 INOP. MAINTENANCE RECONNECTED WIRES. (W)

Part: EEL WIRING — LOOSE (CABIN)

SEA - DURING CHECK, EMERGENCY FLOOR LIGHTS INOP AT ROWS 15 AND 16. MAINTENANCE REPAIRED LOOSE WIRING. (W)