N683SW

Part: BELLCRANK — BROKEN (TE FLAP) · airframe 78,200 hrs · 65,179 cycles

RIGHT O/H AFT FLAP I/B DELVE MECHANISM BELL CRANK BROKEN. REMOVED AND REPLACED RIGHT O/B AFT FLAP I/B DRIVE MECHENISM BELL CRANK AND VERIFIED ADJUSTMENT/RIG OF TRAILING EDGE FLAP IAW MM + MM 27-51-21-820-801.

Part: FLAP — DELAMINATED (LT WING) · airframe 78,642 hrs · 65,503 cycles

ON WALK-AROUND FOUND 1" DELAMINATION ON TRAILING EDGE OF OUTBOARD FT FLAP APPROX 12" FROM INBOARD END. REMOVED AND REPLACED LEFT OUTBOARD AFT FLAP. P/N: 65-46435-277 S/N OFF: BN-860 S/N ON: 966 L/H AFT

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,988 hrs · 65,026 cycles

SKIN CRACKED AT STA 727 E AND 3 BELOW STR 19L. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,280 hrs · 64,493 cycles

SKIN CRACKED AT BS 685+6, STR 10L. REPAIRED SKIN IAW EA.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 76,960 hrs · 64,239 cycles

EMERGENCY EXIT FLIGHT DECK EMERGENCY LIGHT INOP. RELAMPED LIGHT PER AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 76,960 hrs · 64,239 cycles

RIGHT OVERWING EMERGENCY EXIT LIGHT BULB INOP. REMOVED AND REPLACED BULBS IAW AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 76,960 hrs · 64,239 cycles

SKIN CRACKED AT BS 440, STR 16R. REPAIRED SKIN IAW ER AND EA.

Part: LIGHT — FAULTY (COCKPIT) · airframe 76,867 hrs · 64,167 cycles

CIRCUIT BREAKER FOR ANNUNCIATORS POPPED ACCOMPANIED BY ELECTRICAL SMELL PRIOR TO POPPING. RESET CIRCUIT BREAKER. RESET FIRST OFFICERS MASTER CAUTION LIGHT ASSY AND REMOVED AND REPLACED CAPTAINS MASTER CAUTION LIGHT ASSY PER MM.

Part: LENS — BROKEN (CABIN) · airframe 76,340 hrs · 63,758 cycles

R1 DOOR EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LENS PER AMM.

Part: SLIDE — LOW PRESSURE (L2 DOOR) · airframe 76,321 hrs · 63,743 cycles

L2 DOOR EVAC SLIDE PRESSURE IN THE RED. REMOVED AND REPLACED L2 DOOR SLIDE ASSY PER MT.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,173 hrs · 62,876 cycles

DURING SCHEDULED HC CHECK, FOUND SKIN CRACKED AT BS 454, STR 26L. REPAIRED SKIN IAW MT.

Part: WEDGE — DELAMINATED (TE FLAP) · airframe 75,173 hrs · 62,876 cycles

DURING SCHEDULED HC CHECK, FOUND RT WING IB TE FLAP WEDGE DELAMINATED. R&R WEDGE ASSY IAW MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,173 hrs · 62,876 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND SKIN CRACKED AT BS 454, STR 26L. REPAIRED SKIN IAW SRM.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 75,173 hrs · 62,876 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND L2 DOOR EMERGENCY EXIT SIGN BULBS INOP. REMOVED AND REPLACED BULBS PER MM.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 75,023 hrs · 62,763 cycles

DURING SCHEDULED MV3 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM.

Part: ENGINE — MALFUNCTIONED (NR 1) · airframe 75,014 hrs · 62,755 cycles

FLIGHT ATTENDANT REPORTED LOUD "AIR" NOISE AROUND MID CABIN, LT SIDE. ALSO NOTICED AN ACRID SMELL TOWARD THE REAR OF THE AIRCRAFT. REMOVED AND REPLACED NR 1 ENGINE PER MT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 74,382 hrs · 62,278 cycles

DURING SCHEDULED CV CHECK, FOUND L2 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,439 hrs · 61,575 cycles

DURING SCHEDULED 24Y CHECK FOUND, FRAME WEB CRACKED AT BS 616 BETWEEN S-17R AND S-18R. REPAIRED WEB PER EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 73,439 hrs · 61,575 cycles

DURING SCHEDULED 24Y CHECK FOUND, LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 727B, RBL 24.8. REPAIRED CHORD PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,439 hrs · 61,575 cycles

DURING SCHEDULED 24Y CHECK FOUND, FRAME CRACKED AT BS 663.75, S-3R. REPAIRED FRAME IAW EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 73,439 hrs · 61,575 cycles

DURING SCHEDULED 24Y CHECK FOUND, LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 727B, LBL 45.5. REPAIRED CHORD PER EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 73,439 hrs · 61,575 cycles

DURING SCHEDULED 24Y CHECK FOUND, FLOORBEAM CRACKED AT BS 727B, LBL 45.5. REPAIRED BEAM IAW EO.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 73,439 hrs · 61,575 cycles

DURING SCHEDULED 24Y CHECK FOUND, LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 663, RBL 2.0. REPAIRED CHORD PER EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 73,439 hrs · 61,575 cycles

DURING SCHEDULED 24Y CHECK FOUND, LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 709.5, LBL 24.5. REPAIRED CHORD PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,439 hrs · 61,575 cycles

DURING SCHEDULED 24Y CHECK FOUND, FRAME CRACKED AT BS 663.75, S-3L. REPAIRED FRAME IAW EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 73,439 hrs · 61,575 cycles

DURING SCHEDULED 24Y CHECK FOUND, LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED BETWEEN BS 708 TO BS 709, RBL 24.5. REPAIRED CHORD PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,439 hrs · 61,575 cycles

DURING SCHEDULED 24Y CHECK FOUND, FRAME CRACKED AT BS 663.75, S-2L. REPAIRED FRAME IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,439 hrs · 61,575 cycles

DURING SCHEDULED 24Y CHECK FOUND, FUSELAGE SKIN CRACKED AT R1 DOOR LOWER CUT OUT OF THE LOWER HINGE. REMOVED AND REPLACED SKIN PER EO.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 73,439 hrs · 61,575 cycles

DURING SCHEDULED 24Y CHECK FOUND, STRINGER CORRODED AT BS 328, STR 28R. REMOVED AND REPLACED STRINGER SECTION PER SRM.

Part: LIGHT — DELAMINATED (CABIN) · airframe 73,439 hrs · 61,575 cycles

DURING SCHEDULED 24Y CHECK FOUND, RT EEPLS DELAMINATED. REMOVED AND REPLACED EEPLS PER MM.

Part: SKIN — CRACKED (SLAT) · airframe 73,439 hrs · 61,575 cycles

DURING SCHEDULED 24Y CHECK FOUND, CRACKED EXTERNAL UPPER SKIN AROUND OF RIVETS LOCATED BETWEEN SLAT STA 59 TO SLAT STA 68 OF SLAT NR 4 RT WING. REPAIRED SKIN IAW EO.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,439 hrs · 61,757 cycles

DURING SCHEDULED 24Y CHECK FOUND, FRAME CRCKED AT BS 616, BETWEEN STR 17R TO STR 18R. REPAIRED FRAME PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,439 hrs · 61,757 cycles

DURING SCHEDULED 24Y CHECK FOUND, SKIN CRACKED AT BS 301, STR 17R. REPAIRED SKIN PER EA.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 73,439 hrs · 61,575 cycles

DURING SCHEDULED 24Y CHECK FOUND, CRACK ON VERTICAL ANGLE LOCATED AT BULKHEAD AREA OF THE BS 727 AND STR 27L AFT CARGO COMPARTMENT. REMOVED AND REPLACED ANGLE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,439 hrs · 61,575 cycles

DURING SCHEDULED 24Y CHECK FOUND, FUSELAGE SKIN CRACKED AT R1 DOOR CUTOUT, BS 305.5. REPAIRED SKIN PER EA.

Part: FLOORBEAM — CRACKED (BS 727B) · airframe 73,439 hrs · 61,575 cycles

DURING SCHEDULED 24Y CHECK FOUND, CRACKED LONGITUDINAL FLOORBEAM UPPER CHORD AFT END AROUND OF FASTENER BS 727B OF LBL 24.8. REPAIRED CHORD IAW EA.

Part: WEB — CRACKED (FUSELAGE) · airframe 73,439 hrs · 61,575 cycles

DURING SCHEDULED 24Y CHECK FOUND, CRACKED WAS FOUND ON WEB RBL 5.7 VERTICAL BEAM WL 180. REPAIRED WEB IAW EA.

Part: STRIP — DELAMINATED (CABIN) · airframe 73,439 hrs · 61,575 cycles

DURING SCHEDULED 24Y CHECK FOUND, LT EEPLS STRIP DELAMINATED. REMOVED AND REPLACED EEPLS STRIP PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 73,439 hrs · 61,757 cycles

DURING SCHEDULED 24Y CHECK FOUND, LT OVERHEAD EMERGENCY EXIT BULLNOSE LIGHT INOP AT ROW 13. RELAMPED PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 73,439 hrs · 61,757 cycles

DURING SCHEDULED 24Y CHECK FOUND, AFT EMERGENCY EXIT SIGN LIGHT BULB INOP. REMOVED AND REPLACED BULB PER MM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 73,439 hrs · 61,575 cycles

DURING SCHEDULED 24Y CHECK FOUND STRINGER CRACK AFT CARGO COMPARTMENT, BS 947.5 STR 26R. REPAIRED PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,439 hrs · 61,575 cycles

DURING SCHEDULED 24Y CHECK FOUND CRACK ON ELECTRICAL COMPARTMENT, FRAME, AT BS 328 BETWEEN STR 20R AND STR 21R. REPAIRED PER DOC.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,439 hrs · 61,575 cycles

DURING SCHEDULED 24Y CHECK, FOUND SKIN CRACKED AT BS 887+8.5, STR 22R. REPAIRED SKIN PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,439 hrs · 61,575 cycles

DURING SCHEDULED 24Y CHECK, FOUND CRACK ON RT SIDE OF FLIGHT CREW COMPARTMENT FRAME, BS 188, STR 17R. REPAIRED PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,439 hrs · 61,575 cycles

DURING SCHEDULED 24Y CHECK, FOUND AFT CARGO COMPARTMENT FRAME CRACK, BS 986.5, STR 25L. REPLACED STR PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,439 hrs · 61,575 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 188, STR 17L. REPAIRED FRAME PER SRM.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 73,439 hrs · 61,575 cycles

DURING SCHEDULED 24Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 859, RBL 3.0. REPAIRED CHANNEL PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,439 hrs · 61,575 cycles

DURING SCHEDULED 24Y CHECK, FOUND SKIN CRACKED AT BS 727D+4, STR 19L. REPAIRED SKIN PER SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 73,439 hrs · 61,575 cycles

DURING SCHEDULED 24Y CHECK, FOUND ANGLE CORRODED AT BS 727D+5, LBL 3.0. REPAIRED ANGLE PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,439 hrs · 61,575 cycles

DURING SCHEDULED 24Y CHECK, FOUND CRACK FSLG SKIN AT CHEM-MILLED STEP BS 747 , STR 19R. REPAIRED PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,439 hrs · 61,575 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 312, STR 18R. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 73,439 hrs · 61,575 cycles

DURING SCHEDULED 24Y CHECK, FOUND RT WING NR 5 SLAT LOWER SKIN CRACKED BETWEEN STA 159 TO STA 153. REPAIRED SKIN PER SRM.

Part: WIRE — BROKEN (CABIN) · airframe 73,439 hrs · 61,575 cycles

DURING SCHEDULED 24Y CHECK, FOUND R1 DOOR EEPLS WIRES BROKEN. REPAIRED WIRES PER SWPM.

Part: BRACKET — CRACKED (EVAC SLIDE) · airframe 73,439 hrs · 61,575 cycles

DURING SCHEDULED 24Y CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE BRACKET ASSY CRACKED. REMOVED AND REPLACED BRACKET ASSY PER SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 73,439 hrs · 61,575 cycles

DURING SCHEDULED 24Y CHECK, FOUND WEB CORRODED BETWEEN BS 420 TO BS 440, STR 17R. REPAIRED FRAME PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,439 hrs · 61,575 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 20R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 73,439 hrs · 61,575 cycles

DURING SCHEDULED 24Y CHECK, FOUND WEB CRACKED AT BS 727, RBL 41. REMOVED AND REPLACED WEB PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,439 hrs · 61,575 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 380, STR 16L. REPAIRED FRAME PER SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 73,439 hrs · 61,575 cycles

DURING SCHEDULED 24Y CHECK, FOUND WEB CORRODED BETWEEN BS 500A TO BS 500B, STR 17R. REMOVED AND REPLACED WEB PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 73,439 hrs · 61,575 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CORRODED AT BS 500C, BETWEEN STR 27R TO STR 28R. REPAIRED FRAME PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 73,439 hrs · 61,575 cycles

DURING SCHEDULED 24Y CHECK, FOUND WEB CRACKED AT BS 727, LBL 13. REMOVED AND REPLACED WEB PER SRM.

Part: SLAT — DELAMINATED (LT WING) · airframe 73,439 hrs · 61,575 cycles

DURING SCHEDULED 24Y CHECK, FOUND LT WING NR 3 SLAT I/B UPPER EDGE DELAMINATED. REPAIRED SLAT PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 73,439 hrs · 61,575 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CRACKED AT BS 420, STR 28L. REMOVED AND REPLACED STRINGER PER SRM AND BAC DWG.

Part: SKIN — CRACKED (LE SLAT) · airframe 73,439 hrs · 61,575 cycles

DURING SCHEDULED 24Y CHECK, FOUND LT WING LOWER SLAT SKIN CRACKED BETWEEN STA 297 TO STA 301. REPAIRED SKIN PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 73,439 hrs · 61,575 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CORRODED AT BS 500C, BETWEEN STR 26R TO STR 27R. REPAIRED FRAME PER SRM.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 73,439 hrs · 61,575 cycles

DURING SCHEDULED 24Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 859, RBL 8.10. REPAIRED CHANNEL PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,439 hrs · 61,575 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 12R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,439 hrs · 61,575 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 847, STR 14L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 73,439 hrs · 61,575 cycles

DURING SCHEDULED 24Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 772, RBL 8.10. REPAIRED CHANNEL PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,439 hrs · 61,575 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 947.5, STR 25R. REPAIRED CLIP PER EA.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 73,439 hrs · 61,575 cycles

DURING SCHEDULED 24Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 859, LBL 3. REPAIRED CHANNEL PER EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 73,439 hrs · 61,575 cycles

DURING SCHEDULED 24Y CHECK, FOUND AFT CARGO COMPARTMENT CORROSION ON LOWER FRAME BS 867 BETWEEN STR 26R TO STR 27R. REPAIRED PER SRM.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 73,439 hrs · 61,575 cycles

DURING SCHEDULED 24Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 772, LBL 8.10. REPAIRED CHANNEL PER EA.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 73,439 hrs · 61,575 cycles

DURING SCHEDULED 24Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 772, RBL 3.0. REPAIRED CHANNEL PER EA.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 73,439 hrs · 61,575 cycles

DURING SCHEDULED 24Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 772, LBL 12.5. REPAIRED CHANNEL PER EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 73,439 hrs · 61,575 cycles

DURING SCHEDULED 24Y CHECK FOUND CORROSION FWD CARGO COMPARTMENT ON FRAME, BS 500A END BETWEEN STR 28R TO STR 28L. REPAIRED PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,439 hrs · 61,575 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 807, STR 25L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 73,439 hrs · 61,575 cycles

DURING SCHEDULED 24Y CHECK, FOUND FLOORBEAM CRACKED BETWEEN BS 663.75 TO BS 670, LBL 24.5. REPAIRED BEAM PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,439 hrs · 61,575 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 19L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,439 hrs · 61,575 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 24R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,439 hrs · 61,575 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STR 16R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,439 hrs · 61,575 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 559, STR 11R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,439 hrs · 61,575 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 827, STR 25L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,439 hrs · 61,575 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 23R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 73,439 hrs · 61,575 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CRACKED AT BS 500, STR 8L. REPAIRED STRINGER PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,439 hrs · 61,575 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 927, STR 26R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,439 hrs · 61,575 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500C, STR 26R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 73,439 hrs · 61,575 cycles

DURING SCHEDULED 24Y CHECK, FOUND VERTICAL ANGLE CRACKED AT BS 369, LBL 45.5. REMOVED AND REPLACED ANGLE PER SRM AND BAC DWG.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 73,439 hrs · 61,575 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CRACKED BETWEEN BS 380 TO BS 400, STR 15R. REPAIRED STRINGER PER SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 73,439 hrs · 61,575 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME ANGLE CORRODED AT BS 328, STR 20L. REMOVED AND REPLACED ANGLE PER SRM AND BAC DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 78,696 hrs · 65,543 cycles

CRACK INDICATION FOUND ON THE FRAME STUB BEAM LOCATED AT BS 616 BETWEEN S-17R AND S-18R. PERFORMED REPAIR ON THE STUB BEAM IAW EA 1-353-15638 AND EO AEM-HC53-714/11 R0.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,439 hrs · 61,575 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 727B, BETWEEN STR 14L TO STR 15L. REPAIRED FRAME PER SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 73,439 hrs · 61,575 cycles

DURING SCHEDULED 24Y CHECK, FOUND AFT CARGO COMPARTMENT CRACK ON TIE CLIP, BS 947.5, STR 26R. REPLACED TIE PER SRM.

Part: LIGHT — BROKEN (CABIN) · airframe 72,523 hrs · 60,886 cycles

DURING SCHEDULED SPV CHECK, FOUND FWD LAVATORY WALL EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: LIGHT — BROKEN (CABIN) · airframe 71,357 hrs · 59,984 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: GASPER FAN — FAULTY (E&E BAY) · airframe 71,031 hrs · 59,739 cycles

BURNED ODOR REPORTED AT MID CABIN LASTING ABOUT 1 MINUTE ON DESCENT APPROX 18,000: NO SMOKE OBSERVED OR REPORTED. GASPER FAN WAS ON AT THE TIME AND WAS TURNED OFF AS PRECAUTION. R&R GASPER FAN MOTOR PER MM.

Part: SLIDE — LOOSE (L1 DOOR) · airframe 70,746 hrs · 59,523 cycles

L1 DOOR EMERGENCY EVAC SLIDE LOOSE. SECURED SLIDE PER MM.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 70,127 hrs · 59,047 cycles

DURING SCHEDULED SPV CHECK, FOUND LT KEEL BEAM CORRODED BETWEEN BS 560 TO BS 574. REPAIRED BEAM PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,127 hrs · 59,047 cycles

DURING SCHEDULED SPV CHECK, FOUND GROUND AIR CONDITIONING ACCESS DOOR CUTOUT CRACKED AT LT FWD CORNER. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,130 hrs · 59,048 cycles

DURING SCHEDULED SPV CHECK, FOUND GROUND AIR CONDITIONING ACCESS DOOR SKIN CUTOUT CRACKED AT RT FWD CORNER. REPAIRED SKIN PER ER.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 70,130 hrs · 59,048 cycles

DURING SCHEDULED SPV CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 70,130 hrs · 59,048 cycles

DURING SCHEDULED SPV CHECK, FOUND LT KEEL BEAM CORRODED BETWEEN BS 560 TO BS 574. REPAIRED BEAM PER ER.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 70,130 hrs · 59,048 cycles

DURING SCHEDULED SPV CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 70,130 hrs · 59,048 cycles

DURING SCHEDULED SPV CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,130 hrs · 59,048 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BETWEEN BS 740 TO BS 793, BETWEEN STR 17L TO STR 19L. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,130 hrs · 59,048 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 792, STR 17L. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,892 hrs · 58,109 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE SKIN CRACKED AT LOWER HINGE CUTOUT, BS 303.25, WL 238.25. REPAIRED SKIN PER SWA EA.

Part: BEAR STRAP — CRACKED (FUSELAGE) · airframe 68,473 hrs · 57,784 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE BEAR STRAP SKIN CRACKED AT BS 289,WL 233, RT SIDE. REPAIRED SKIN PER ER.

Part: BEAR STRAP — CRACKED (FUSELAGE) · airframe 68,473 hrs · 57,784 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE BEAR STRAP SKIN CRACKED AT BS 291, BETWEEN WL 253 TO WL 255, RT SIDE. REPAIRED SKIN PER ER.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 68,473 hrs · 57,784 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CRACKED AT BS 296, STR 10L. REPAIRED STRINGER PER ER.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 68,473 hrs · 57,784 cycles

DURING SCHEDULED 22Y CHECK, FOUND FLOORBEAM UPPER CAP CORRODED AT BS 986, LBL 7. REPAIRED FLOORBEAM PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,473 hrs · 57,784 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,473 hrs · 57,784 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,473 hrs · 57,784 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,473 hrs · 57,784 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER ER.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,473 hrs · 57,784 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 757C, STR 5R. REMOVED AND REPLACED STR CLIP PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 68,473 hrs · 57,784 cycles

DURING SCHEDULED 22Y CHECK, FOUND FLOORBEAM UPPER CAP CRACKED AT BS 344, LBL 25 TO RBL 25. REPAIRED FLOORBEAM PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,473 hrs · 57,784 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 7R. REMOVED AND REPLACED STR CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,473 hrs · 57,784 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 6R. REMOVED AND REPLACED STR CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,473 hrs · 57,784 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 663.75, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 68,473 hrs · 57,784 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CRACKED AT BS 300, STR 15L. REPAIRED STRINGER PER ER & SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 68,473 hrs · 57,784 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CRACKED AT BS 500C, STR 9L. REMOVED AND REPLACED STRINGER PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,473 hrs · 57,784 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 7R. REMOVED AND REPLACED CLIP PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 68,473 hrs · 57,784 cycles

DURING SCHEDULED 22Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 660, BL 0. REPAIRED BEAM PER ER.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,473 hrs · 57,784 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 480, STR 9L. REMOVED AND REPLACED CLIP PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 68,473 hrs · 57,784 cycles

DURING SCHEDULED 22Y CHECK, FOUND FLOORBEAM CORRODED AT BS 947, RBL 52. REPAIRED BEAM PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 68,473 hrs · 57,784 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CRACKED AT BS 500C, STR 8L. REPAIRED STRINGER PER ER.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,473 hrs · 57,784 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STR 9L. REMOVED AND REPLACED CLIP PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 68,473 hrs · 57,784 cycles

DURING SCHEDULED 22Y CHECK, FOUND WEB CRACKED BETWEEN BS 294 TO BS 303, STR 16L. REPAIRED WEB PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,473 hrs · 57,784 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 847, STR 10L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,473 hrs · 57,784 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 10R. REMOVED AND REPLACED CLIP PER SRM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 68,473 hrs · 57,784 cycles

DURING SCHEDULED 22Y CHECK, FOUND WEB SUPPORT ANGLE CRACKED AT BS 290, WL 240, BETWEEN STR 12R TO STR 13R. REMOVED AND REPLACED ANGLE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,473 hrs · 57,784 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 887, STR 8R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 68,473 hrs · 57,784 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CRACKED AT BS 360, STR 7L. REMOVED AND REPLACED STRINGER PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,473 hrs · 57,784 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 9R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,473 hrs · 57,784 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 9L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,473 hrs · 57,784 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 9L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,473 hrs · 57,784 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 707, STR 10R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,473 hrs · 57,784 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 8L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,473 hrs · 57,784 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 10R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 727A S9R) · airframe 68,473 hrs · 57,784 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 9R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,473 hrs · 57,784 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 5L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 727C S5L) · airframe 68,473 hrs · 57,784 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 5L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,473 hrs · 57,784 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 5L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,473 hrs · 57,784 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 9R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,473 hrs · 57,784 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 5L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,473 hrs · 57,784 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 4R. R&R CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 674,444 hrs · 57,041 cycles

DURING SCHEDULED SPV CHECK, FOUND AFT CARGO DOOR CUTOUT SKIN CRACKED AT LOWER FWD CORNER. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,444 hrs · 57,041 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT, BS 430. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,444 hrs · 57,041 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT, BS 390. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,444 hrs · 57,041 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT, BS 410. REPAIRED SKIN PER EA.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 67,180 hrs · 56,852 cycles

DURING SCHEDULED HC1 CHECK, FOUND L1 DOOR SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,180 hrs · 56,852 cycles

DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 798, STR 17L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,180 hrs · 56,852 cycles

DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR FWD LOWER CORNER. REPAIRED SKIN PER SWA EA.

Part: FLAP — DELAMINATED (RT WING) · airframe 67,180 hrs · 56,852 cycles

DURING SCHEDULED HC1 CHECK, FOUND RT WING O/B FORE FLAP DELAMINATED. REPLACED FLAP PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,180 hrs · 56,852 cycles

DURING SCHEDULED HC1 CHECK, FOUND SKIN CRACKED AT AFT CARGO DOOR HANDLE, AFT UPPER CORNER CUTOUT. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,582 hrs · 56,423 cycles

DURING SCHEDULED MV1 CHECK, FOUND SKIN CRACKED AT BS 803, STR 19L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,582 hrs · 56,423 cycles

DURING SCHEDULED MV1 CHECK, FOUND SKIN CRACKED AT BS 748, STR 18L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 779 S18L) · airframe 66,413 hrs · 56,296 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 779, STR 18L. REPAIRED SKIN PER SWA EA.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 65,933 hrs · 55,919 cycles

L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: SLAT — DELAMINATED (LT WING) · airframe 65,822 hrs · 55,840 cycles

DURING MV2 CK, FOUND NR 2 L/E SLAT OUTBOARD T/E DELAMINATED. REMOVED AND REPLACED SLAT ASSY PER MM.

Part: WIRE — CHAFED (CABIN) · airframe 65,822 hrs · 55,840 cycles

EMERGENCY EXIT LIGHT ILLUMINATED ERRATICALLY. FOUND ELEC WIRE CHAFED AT BS 945. REPAIRED PER MM.

Part: ANNUNCIATOR — FALSE INDICATION (EMERGENCY LIGHTS) · airframe 65,411 hrs · 55,530 cycles

EMERGENCY LIGHTS ILLUMINATED WITH ALL SWITCHES IN NORMAL POSITION. THE ANNUNCIATOR LIGHT DID NOT ILLUMINATE WHEN COVERED SWITCH WAS PLACED OFF. RESET CIRCUIT BREAKER PER MM. OPS CHECKED GOOD.

Part: LENS — MISSING (CABIN) · airframe 65,328 hrs · 55,455 cycles

BULLNOSE EMERGENCY EXIT LIGHT LENS MISSING AT ROW 1 DEF. INSTALLED LENS PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 65,177 hrs · 55,357 cycles

R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: CHARGER — FAULTY (CABIN) · airframe 64,605 hrs · 54,937 cycles

EMERGENCY EXIT LIGHTS C/B OPENED INFLIGHT, C/B WOULD RESET. REMOVED AND REPLACED FWD CABIN BATTERY CHARGER PER MM.

Part: BATTERY PACK — FAULTY (CABIN) · airframe 64,283 hrs · 54,700 cycles

DURING CLIMBOUT OF DAL ALL EMERGENCY EXIT LIGHTS ILLUMINATED. REMOVED AND REPLACED BATTERY PACKS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,198 hrs · 54,630 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 740E, STR 18L. REPAIRED SKIN PER SWA EA.

Part: LOGIC CARD — FAULTY (NLG) · airframe 63,985 hrs · 54,462 cycles

AIR TURNBACK / DECLARED EMERGENCY. DURING CLIMB FROM HOU NLG WARNING LIGHTS ILLUMINATED. CYCLED GEAR, NO HELP. REMOVED AND REPLACED LOGIC CARD PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 63,975 hrs · 54,458 cycles

DURING SCHEDULED MV1 CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: SKIN — CRACKED (BS 960) · airframe 63,751 hrs · 54,285 cycles

DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 960, R2 DOOR LOWER FWD CORNER. REPAIRED SKIN PER SRM.

Part: GIRT BAR — LOOSE (R2 DOOR SLIDE) · airframe 63,751 hrs · 54,285 cycles

DURING SCHEDULED HC1 CHECK, FOUND R2 DOOR AFT GIRT BAR ATTACH FITTING LOOSE. SECURED AFT GIRT BAR ATTACH FITTING PER MM.

Part: SKIN — CRACKED (BS 960) · airframe 63,751 hrs · 54,285 cycles

DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 960, R2 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 63,749 hrs · 54,284 cycles

DURING SCHEDULED HC1 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. REPOSITIONED R1 DOOR EMERGENCY EVAC SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 63,749 hrs · 54,284 cycles

DURING SCHEDULED HC1 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. REMOVED AND REPLACED L2 DOOR EMERGENCY EVAC SLIDE PER MM.

Part: LIGHT — BROKEN (MID CABIN) · airframe 63,749 hrs · 54,284 cycles

DURING SCHEDULED HC1 CHECK, FOUND LEFT OVERWING EMERGENCY EXIT LIGHT ASSY BROKEN. REMOVED AND REPLACED LEFT OVERWING EMERGENCY EXIT LIGHT PER MM.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 63,749 hrs · 54,284 cycles

DURING SCHEDULED HC1 CHECK, FOUND R2 DOOR LOWER EMERGENCY EXIT LIGHT LENS MISSING. REMOVED AND REPLACED R2 DOOR LOWER EMERGENCY EXIT LIGHT PER MM.

Part: LIGHT — INOPERATIVE (R2 DOOR) · airframe 63,749 hrs · 54,284 cycles

DURING SCHEDULED HC1 CHECK, FOUND R2 DOOR LOWER EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED R2 DOOR LOWER EMERGENCY EXIT LIGHT PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 63,453 hrs · 54,080 cycles

R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,193 hrs · 53,877 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 938, STR 23R. REPAIRED SKIN PER SRM.

Part: BATTERY — FAULTY (CABIN) · airframe 62,941 hrs · 53,685 cycles

DURING SCHEDULED MV4 CHECK, FWD CABIN EMERGENCY EXIT LIGHTS STAY ILLUMINATED WITH SWITCH IN OFF POSITION. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 62,782 hrs · 53,556 cycles

FWD CABIN EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LIGHT LENS PER MM.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 62,135 hrs · 53,049 cycles

L1 DOOR EMERGENCY EXIT LIGHT INOP. FOUND GROUND WIRE BROKEN. REPAIRED GROUND WIRE PER MM.

Part: FRAME — CRACKED (BS 500B S20L) · airframe 62,134 hrs · 53,047 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500B, STR 20L. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (BS 500D S20L) · airframe 62,134 hrs · 53,047 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500D, STR 20L. REPAIRED FRAME PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 62,134 hrs · 53,047 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER 26R CORRODED AT BS 540. REPAIRED STRINGER PER SRM.

Part: BEARING — WORN (RT ELEVATOR) · airframe 62,134 hrs · 53,047 cycles

DURING SCHEDULED 20Y CHECK, RIGHT ELEVATOR FAILED FREE PLAY CHECK. REMOVED AND REPLACED NR 1 HINGE BEARING AND BUSHING PER MM.

Part: CONTROL ROD — CRACKED (ELEVATOR TAB) · airframe 62,134 hrs · 53,047 cycles

DURING SCHEDULED 20Y CHECK, FOUND RIGHT ELEVATOR TAB CONTROL ROD CRACKED AT DRAIN HOLE. REMOVED AND REPLACED CONTROL ROD PER MM.

Part: BEARING — WORN (LT ELEVATOR) · airframe 62,134 hrs · 53,047 cycles

DURING SCHEDULED 20Y CHECK, LEFT ELEVATOR FAILED FREE PLAY CHECK. REMOVED AND REPLACED NR 1 HINGE BEARING AND BUSHING PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,134 hrs · 53,047 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,134 hrs · 53,047 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,134 hrs · 53,047 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 320, STR 21L. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,134 hrs · 53,047 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727D, STR 14L. REPAIRED FRAME PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,134 hrs · 53,047 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER SRM.

Part: STRINGER CLIP — CRACKED (BS 827 S14L) · airframe 62,134 hrs · 53,047 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 827, STR 14L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 344 S9R) · airframe 62,134 hrs · 53,047 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 344, STR 9R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 767 S14L) · airframe 62,134 hrs · 53,047 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 14L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (BS 500C S8L) · airframe 62,134 hrs · 53,047 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 400 S8R) · airframe 62,134 hrs · 53,047 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 887 S8L) · airframe 62,134 hrs · 53,047 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 887, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,134 hrs · 53,047 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 277, STR 16L. REPAIRED FRAME PER SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 62,134 hrs · 53,047 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER SPLICE CRACKED AT BS 907, STR 4L. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 62,134 hrs · 53,047 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 867, STR 9R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,134 hrs · 53,047 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,134 hrs · 53,047 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,134 hrs · 53,047 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500B, STR 20R. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 67,402 hrs · 53,997 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 14L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 767 S25L) · airframe 62,134 hrs · 53,047 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 25L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 717C S23L) · airframe 62,134 hrs · 53,047 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 717C, STR 23L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 380 S26R) · airframe 62,134 hrs · 53,047 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 26R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 61,560 hrs · 52,569 cycles

R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: GLOWSTRIP — WORN (CABIN) · airframe 60,288 hrs · 51,558 cycles

DURING SCHEDULED C1 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP WORN AT ROW 11 DEF. REMOVED AND REPLACED EEPLS PHOTOLUMINESCENT STRIP PER MM.

Part: SKIN — CRACKED (BS 750 S18L) · airframe 60,288 hrs · 51,558 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 750, STR 18L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 720 S18L) · airframe 60,288 hrs · 51,558 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 770, STR 18L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 770 S19L) · airframe 60,288 hrs · 51,558 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 770, STR 19L. REPAIRED SKIN PER SRM.

Part: GLOWSTRIP — WORN (CABIN) · airframe 60,288 hrs · 51,558 cycles

DURING SCHEDULED C1 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP WORN AT ROW 21 ABC. REMOVED AND REPLACED EEPLS PHOTOLUMINESCENT STRIP PER MM.

Part: SKIN — CRACKED (BS 972 S24L) · airframe 60,288 hrs · 51,558 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 972, STR 24L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 750 S19L) · airframe 60,288 hrs · 51,558 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 750, STR 19L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 933 S24R) · airframe 60,288 hrs · 51,558 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 933, STR 24R. REPAIRED SKIN PER SWA EA.

Part: BATTERY PACK — FAULTY (EMERGENCY LIGHT) · airframe 59,961 hrs · 51,286 cycles

DURING SCHEDULED MV1 CHECK, FOUND FWD CABIN EMERGENCY EXIT LIGHTS ON WITH SWITCH OFF. REMOVED AND REPLACED FWD CABIN EMERGENCY EXIT BATTERY PACKS PER MM.

Part: LIGHT — BROKEN (CABIN) · airframe 59,409 hrs · 50,850 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FWD ENTRY DOOR EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: STRIP — WORN (CABIN) · airframe 59,341 hrs · 50,797 cycles

DURING SCHEDULED C4 CHECK, FOUND EEPLS STRIP WORN AT ROW 6 ABC. REMOVED AND REPLACED EEPLS STRIP PER MM.

Part: STRIP — WORN (CABIN) · airframe 59,341 hrs · 50,797 cycles

DURING SCHEDULED C4 CHECK, FOUND EEPLS STRIP WORN AT ROW 9 DEF. REMOVED AND REPLACED EEPLS STRIP PER MM.

Part: LIGHT — BROKEN (MID CABIN) · airframe 58,576 hrs · 50,223 cycles

RIGHT OVERWING EMERGENCY EXIT LIGHT ASSY BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 58,335 hrs · 50,031 cycles

DURING SCHEDULED C3 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 58,335 hrs · 50,031 cycles

DURING SCHEDULED C3 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 57,831 hrs · 49,637 cycles

L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: SLIDE — DISLODGED (L1 DOOR) · airframe 57,831 hrs · 49,637 cycles

L1 DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM.

Part: FRAME — CRACKED (FWD CARGO) · airframe 57,771 hrs · 49,590 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FWD CARGO DOOR CUTOUT AFT FRAME CRACKED AT NR 5 STOP FITTING. REMOVED AND REPLACED FWD CARGO DOOR AFT FRAME IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,771 hrs · 49,590 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND AFT CARGO DOOR CUTOUT FWD FRAME CRACKED AT NR 5 STOP FITTING. REMOVED AND REPLACED AFT CARGO DOOR FWD FRAME IAW SRM.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 57,771 hrs · 49,590 cycles

DURING SCHEDULED SPECIAL VISIT, COCKPIT EMERGENCY EXIT LIGHT CIRCUIT BREAKER TRIPPED. REPAIRED WIRE NR W1160-42-22 IAW WDM. OPS CHECK OK IAW MM.

Part: FRAME — CRACKED (FWD CARGO) · airframe 57,771 hrs · 49,590 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE FRAME CRACKED AT FWD CARGO DOOR CUTOUT, FWD FRAME NR 5 STOP FITTING. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: STRINGER — CRACKED (BS 727B) · airframe 57,771 hrs · 49,590 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE STRINGER CRACKED AT BS 727B, STR 14R. REMOVED AND REPLACED STRINGER SECTION PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 57,771 hrs · 49,590 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE SHEAR TIE CRACKED AT BS 360, STR 14R TO STR 15R. REPAIRED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (BS 360) · airframe 57,771 hrs · 49,590 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 13R TO STR 14R. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (BS 360) · airframe 57,771 hrs · 49,590 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 360, STR 10L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 360) · airframe 57,771 hrs · 49,590 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 360, STR 11L. REMOVED AND REPLACED CLIP PER SRM.

Part: BULKHEAD — CRACKED (BS 178) · airframe 57,771 hrs · 49,590 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE VERTICAL BEAM WEB CRACKED AT BS 178 BULKHEAD, LBL 5.7, WL 179. REMOVED AND REPLACED VERTICAL BEAM WEB PER SRM.

Part: SKIN — CRACKED (BS 923) · airframe 57,771 hrs · 49,590 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 923, STR 23R. REPAIRED SKIN PER SRM.

Part: CONTROL VALVE — FAULTY (TE FLAPS) · airframe 57,129 hrs · 49,077 cycles

FLAP LEVER MOVEMENT WAS RESTRICTED & BINDING WAS FELT IN FLAP LEVER. REMOVED AND REPLACED T/E FLAP CONTROL VALVE PER MM.

Part: BATTERY PACK — INOPERATIVE (AFT CABIN) · airframe 56,985 hrs · 48,964 cycles

DURING SCHEDULED SERVICE CHECK, FOUND L2 & R2 DOORS EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — FAILED (AFT CABIN) · airframe 56,985 hrs · 48,964 cycles

DURING SCHEDULED SERVICE CHECK, AFT CABIN EMERGENCY LIGHTS FAILED TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 56,364 hrs · 48,444 cycles

DURING SCHEDULED C1 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,931 hrs · 48,107 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 943, STR 24L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,931 hrs · 48,107 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727D + 13, STR 19R. REPAIRED SKIN PER SWA EA & SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,931 hrs · 48,107 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 517, STR 12L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,625 hrs · 47,852 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 970, STR 18L. REPAIRED PER SWA EA & SRM.

Part: SKIN — DELAMINATED (RT WING FLAP) · airframe 55,406 hrs · 47,677 cycles

DURING SCHEDULED C4 CHECK, FOUND RT WING, T/E OUTBOARD AFT FLAP DELAMINATED. REMOVED AND REPLACED RT WING OUTBOARD AFT FLAP PER MM.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 53,849 hrs · 46,479 cycles

DURING SCHEDULED 1/4D CHECK, FOUND AFT PRESSURE BULKHEAD RADIAL STIFFENER WEB AT BS 1016, STRINGER 7R, CRACKED. REPAIRED WEB PER EA.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 53,849 hrs · 46,479 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BEADED PRESSURE WEB AT BS 665, RBL 42, CRACKED. REPAIRED PRESSURE WEB PER SRM.

Part: BELTFRAME — CORRODED (FUSELAGE) · airframe 53,849 hrs · 46,479 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BELTFRAME AT BS 500, STRINGER 24R, CORRODED. REPAIRED BELTFRAME PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 53,849 hrs · 46,479 cycles

DURING SCHEDULED 1/4D CHECK, FOUND 3 EACH CRACKS ON THE AFT PRESSURE BULKHEAD WEB AT BS 1016, 1 O'CLOCK, 2 O'CLOCK AND 5 O'CLOCK POSITIONS. REPAIRED BULKHEAD WEB PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,849 hrs · 46,479 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FWD ENTRY DOOR UPPER HINGE CUTOUT AFT CORNER, CRACKED. REPAIRED FWD ENTRY DOOR CUTOUT PER EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 53,849 hrs · 46,479 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM FWD FLANGE UNDERSIDE AT BS 986 LT AFT GIRT BAR MOUNT, CORRODED. REPAIRED FLOORBEAM FLANGE PER SRM.

Part: STIFFENER — CRACKED (BULKHEAD) · airframe 53,849 hrs · 46,479 cycles

DURING SCHEDULED 1/4D CHECK, FOUND AFT PRESSURE BULKHEAD STIFFENER AT BS 1016, 3 O'CLOCK POSITION, CRACKED. REPAIRED STIFFENER PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,849 hrs · 46,479 cycles

DURING SCHEDULED 1/4D CHECK, FOUND 2 EACH STRINGER CLIPS AT BS 500B, STRINGER 25L AND BS 500C, STRINGER 25L, CRACKED. REMOVED AND REPLACED STRINGER CLIPS PER SRM.

Part: HOOK — LOOSE (R1 DOOR GIRTBAR) · airframe 53,849 hrs · 46,479 cycles

DURING SCHEDULED 1/4D CHECK, FOUND R1 DOOR EVAC SLIDE GIRT BAR HOOK LOOSE. SECURED R1 DOOR EVAC SLIDE GIRT BAR HOOK PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,849 hrs · 46,479 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN AT BS 931, STRINGER 25R, CRACKED. REPAIRED SKIN PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 53,849 hrs · 46,479 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM AT BS 668, LBL 25, CRACKED. REPAIRED FLOORBEAM PER EA.

Part: SKIN — DELAMINATED (LT WING FOREFLAP) · airframe 53,849 hrs · 46,479 cycles

DURING SCHEDULED 1/4D CHECK, FOUND LT WING OUTBOARD T/E FOREFLAP DELAMINATED. REPAIRED FOREFLAP PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 53,849 hrs · 46,479 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM AT BS 663, RBL 25, CRACKED. REPAIRED FLOORBEAM PER EA.

Part: SLIDE — DISLODGED (L1 DOOR) · airframe 53,470 hrs · 46,171 cycles

L1 DOOR EVAC SLIDE FELL OUT, DID NOT DEPLOY. REINSTALLED L1 DOOR EVAC SLIDE PER MM.

Part: SLIDE — DISLODGED (L1 DOOR) · airframe 53,545 hrs · 46,156 cycles

L1 DOOR EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED AND SECURED SLIDE PER MM.

Part: GLOWSTRIP — DELAMINATED (ROW 7) · airframe 52,668 hrs · 45,529 cycles

PHOTOLUMINESCENT STRIP AT ROW 7 ABC, DELAMINATED. REMOVED AND REPLACED FLOOR STRIP PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 52,614 hrs · 45,478 cycles

DURING SCHEDULED C1 CHECK, FOUND L2 DOOR AND R2 DOOR OVERHEAD EMERGENCY EXIT LIGHTS INOP. RELAMPED LIGHTS PER MM.

Part: CABLE — MISROUTED (L2/R2 DOORS) · airframe 52,614 hrs · 45,478 cycles

DURING SCHEDULED C1 CHECK, FOUND L2 AND R2 DOOR EVAC SLIDE CABLES MISROUTED. REROUTED L2 AND R2 DOOR EVAC SLIDE CABLES PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,971 hrs · 44,966 cycles

DURING SCHEDULED SPV, FOUND STRINGER CLIPS CRACKED AT BS 663.75, STRINGER 4R AND BS 683, STRINGER 4R. REMOVED AND REPLACED STRINGER CLIPS PER SRM.

Part: INDICATOR — FAULTY (COCKPIT) · airframe 51,971 hrs · 44,966 cycles

AIRTURN BACK, DUE TO AIRSPEED INDICATORS DID NOT AGREE. REMOVED AND REPLACED F/O AIRSPEED INDICATOR PER MM.

Part: SENSOR — OUT OF ADJUST (NOSE GEAR) · airframe 51,813 hrs · 44,822 cycles

DURING CRUISE AT FL 22O, 250 KIAS, NOSE GEAR UNSAFE LIGHT ILLUMINATED. AIRCRAFT SLOWED TO 220 KIAS, GEAR CYCLED, LIGHT WENT OUT. ADJUSTED NLG UPLOCK SENSOR PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,652 hrs · 43,890 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727E, STR 19R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,080 hrs · 42,632 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 950, STR 21R. REPAIRED SKIN PER SRM.

Part: BATTERY — WEAK (CABIN) · airframe 46,430 hrs · 40,543 cycles

DURING SCHEDULED A1 CHECK, FOUND BOTH AFT EMERGENCY FLASHLIGHTS HAVE WEAK BATTERIES. REMOVED AND REPLACED FLASHLIGHT BATTERIES PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,063 hrs · 40,242 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 950, STR 24R. REPAIRED SKIN PER SRM.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 45,561 hrs · 39,804 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FWD ENTRY DOOR CUTOUT DOUBLER CRACKED AT LOWER STOP FITTING. REMOVED AND REPLACED DOUBLER PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 45,561 hrs · 39,804 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FWD ENTRY DOOR FWD CUTOUT FRAME VERTICAL WEB CRACKED AT BS 303.9, STR 16R. REMOVED AND REPLACED VERTICAL WEB PER SRM.

Part: FRAME — CRACKED (FWD ENTRY DOOR) · airframe 45,561 hrs · 39,804 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FWD ENTRY DOOR AFT FRAME CRACKED AT 7TH FROM TOP STOP PIN FITTING. REPAIRED FRAME PER SWA RA.

Part: FLOORBEAM — CRACKED (MID CABIN) · airframe 45,561 hrs · 39,804 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CRACKED AT BS 663, BL-0. REPAIRED FLOORBEAM PER SWA RA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 45,561 hrs · 39,804 cycles

DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIP CRACKED AT BS 1138, STR 13L. REMOVED AND REPLACED STR CLIP PER SRM.

Part: FLOORBEAM — CORRODED (AFT CARGO) · airframe 45,561 hrs · 39,804 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CORRODED FROM BS 770 TO 846, LBL 8.0. REPAIRED FLOORBEAM PER SWA RA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 45,561 hrs · 39,804 cycles

DURING SCHEDULED 1/2D CHECK, FOUND RT OUTBOARD SIDE CHORD CRACKED AT BS 178, WL 207 AND RBL 26. REMOVED AND REPLACED CHORD PER SRM.

Part: FLOORBEAM — CORRODED (AFT CARGO) · airframe 45,561 hrs · 39,804 cycles

DURING SCHEDULED 1/2D CHECK, FOUND LONGITUDINAL FLOORBEAM CORRODED FROM BS 757 TO 947, RBL 12.0. REPAIRED FLOORBEAM PER SRM.

Part: FRAME — CRACKED (FWD SVC DOOR) · airframe 45,561 hrs · 39,804 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FWD SVC DOOR AFT FRAME CRACKED AT CUTOUT FOR 4TH FROM TOP STOP PIN FITTING. REPAIRED FRAME PER SWA T1-152-003.

Part: FLOORBEAM — CORRODED (AFT CARGO) · airframe 45,561 hrs · 39,804 cycles

DURING SCHEDULED 1/2D CHECK, FOUND LONGITUDINAL FLOORBEAM CORRODED FROM BS 793 TO 825, LBL 3. REPAIRED FLOORBEAM PER SRM.

Part: FLOORBEAM — CORRODED (AFT CARGO) · airframe 45,561 hrs · 39,804 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CORRODED AT RBL 3.0, BS 727D TO BS 847. REPAIRED FLOORBEAM PER SWA RA.

Part: WEB — CRACKED (FUSELAGE) · airframe 45,561 hrs · 39,804 cycles

DURING SCHEDULED 1/2D CHECK, FOUND VERTICAL BEAM WEB CRACKED (2 EA) AT BS 183, WL 183, LBL 17.1 AND RBL 17.1. REPAIRED WEB PER SRM.

Part: BRACKET — CRACKED (AFT SVC DOOR) · airframe 45,561 hrs · 39,804 cycles

DURING SCHEDULED 1/2D CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE FWD FLOOR ATTACH BRACKET CRACKED. REMOVED AND REPLACED BRACKET PER MM.

Part: WEB — CRACKED (FUSELAGE) · airframe 45,561 hrs · 39,804 cycles

DURING SCHEDULED 1/2D CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 179, WL 227 AND RBL 17.1. REPAIRED WEB PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 45,561 hrs · 39,804 cycles

DURING SCHEDULED 1/2D CHECK, FOUND BULKHEAD WEB CRACKED (2 EA) AT BS 178, WL 234, LBL 11 AND RBL 11. REPAIRED WEB PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 45,561 hrs · 39,804 cycles

DURING SCHEDULED 1/2D CHECK, FOUND VERTICAL WEBS CRACKED (2 EA) AT BS 179, WL 227 AND LBL 17.1 AND BS 183, WL 230 AND LBL 17.1. REPAIRED WEBS PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 45,561 hrs · 39,804 cycles

DURING SCHEDULED 1/2D CHECK, FOUND BULKHEAD WEB CRACKED AT BS 178, WL 234 AND LBL 12. REPAIRED WEB PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 45,127 hrs · 39,465 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED 1.0 INCH LONG AT BS 500D, STR 12R. REPAIRED SKIN PER SRM.

Part: LENS — BROKEN (CABIN) · airframe 44,167 hrs · 38,730 cycles

DURING SCHEDULED C4 CHECK, FOUND OVERHEAD BIN BULL NOSE EMERGENCY LIGHT LENS BROKEN AT ROW 3 ABC. R&R LENS PER MM.

Part: SLIDE — OUT OF ADJ (SERVICE DOOR) · airframe 43,331 hrs · 38,025 cycles

DURING SCHEDULED C3 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUSTMENT. ADJUSTED EMERGENCY EVAC SLIDE PER MM.

Part: LIGHT — INOPERATIVE (FUSELAGE) · airframe 42,935 hrs · 37,682 cycles

DURING SCHEDULED A1 CHECK, FOUND EMERGENCY EXIT LIGHT INOP AT AFT RIGHT FUSELAGE. RELAMPED EXIT LIGHT PER MM.

Part: FLAP — DELAMINATED (LT WING) · airframe 42,397 hrs · 37,235 cycles

DURING SCHEDULED C2 CHECK, FOUND LT WING OUTBD AFT FLAP DELAMINATED AT INBD END. R&R AFT FLAP PER MM.

Part: SKIN — CRACKED (L/E SLAT) · airframe 42,397 hrs · 37,235 cycles

DURING SCHEDULED C2 CHECK, FOUND NR 2 L/E SLAT LOWER SKIN CRACKED AT AFT ROW OF FASTENERS, 20 INBD OF ACTUATOR. REPAIRED SLAT SKIN PER SRM.

Part: SKIN — DELAMINATED (T/E FLAP) · airframe 42,397 hrs · 37,235 cycles

DURING SCHEDULED C2 CHECK, FOUND RT WING INBD AFT FLAP DELAMINATED ON UPPER SURFACE. R&R AFT FLAP PER MM.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 42,113 hrs · 36,996 cycles

DURING SCHEDULED SERVICE CHECK, FOUND BS 663 BULKHEAD VERTICAL STIFFENERS CRACKED AT RBL 6.15 & LBL 6.15. REPAIRED STIFFENERS PER SWA RA.

Part: RETAINER — LOOSE (GIRT BAR) · airframe 41,396 hrs · 36,391 cycles

DURING SCHEDULED C1 CHECK, FOUND FWD SVC DOOR AFT GIRT BAR RETAINER HOOK LOOSE. SECURED RETAINER HOOK PER MM.

Part: RETAINER — LOOSE (GIRT BAR) · airframe 41,396 hrs · 36,391 cycles

DURING SCHEDULED C1 CHECK, FOUND FWD SVC DOOR AFT GIRT BAR RETAINER HOOK LOOSE. SECURED RETAINER HOOK PER MM.

Part: DOWNLOCK SENSOR — FAILED (NLG) · airframe 41,228 hrs · 36,252 cycles

AIR TURNBACK, NOSE GEAR WOULD NOT RETRACT AFTER T/O. RECYCLED GEAR - BOTH GREEN & RED NOSE GEAR LIGHT ILLUMINATED. A/C HANDLED AS THOUGH NLG WAS DOWN. R&R NOSE GEAR LOGIC CARD PER MM. PERFORMED GEAR SWING; LIGHTS/GEAR CHECKED NORMAL PER MM. AT OAK, DURING DEPATURE, NOSE GEAR RETRACTED BUT BOTH NLG RED & GREEN LIGHTS ILLUMINATED. REPLACED S845 NOSE GEAR DOWN SENSOR (P/N 65C28018) & ACCOMPLISHED GEAR SWING PER MM OPS CHECK GOOD.

Part: DOOR SEAL — OUT OF POSITION (AFT CARGO DOOR) · airframe 40,782 hrs · 35,886 cycles

DUAL AIR TURNBACK, CABIN PRESS WARNING HORN SOUNDED DURING CLIMB IN STNBY MODE. DEFERRED PER MEL 24-14. SECOND TURNBACK, FOUND AFT CARGO DOOR PRESS SEAL OUT OF POSITION. REPOSITIONED SEAL PER MM. OPS CHECK GOOD.

Part: SLIDE — DISLODGED (PAX DOOR) · airframe 40,741 hrs · 35,852 cycles

DURING FWD ENTRY DOOR CLOSURE, GIRT BAR WAS SNAGGED AND INADVERTANTLY PULLED EVAC SLIDE OUT OF CASE. REINSTALLED SLIDE PER MM.

Part: INDICATOR — INOPERATIVE (COCKPIT) · airframe 39,933 hrs · 35,161 cycles

ABORTED TAKEOFF, NR 1 ENG EGT INDICATOR FAILED. SWAPPED EGT INDICATORS, OPS CHECK GOOD PER MM.

Part: GCU — FAILED (NR 1 ENGINE) · airframe 39,933 hrs · 35,161 cycles

ABORTED TAKEOFF, NR 1 ENG GENERATOR TRIPPED ALONG WITH NR 1 TR BUS. REMOVED AND REPLACED NR 1 ENG GCU. OPS CHECK GOOD PER MM.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED 1/4D CHECK, FOUND BS 178 BULKHEAD CRACKED AT LBL 14 AND LBL 6. REPAIRED BULKHEAD PER SRM.

Part: CONNECTORS — LOOSE (TE FLAPS)

DURING APPROACH TO ABQ, L/E ANDT/E FLAPS FAILED TO EXTEND, ALT SYSTEM ACTIVATED, FLAPS POSITIONED TO 15 FOR LANDING. A/C MADE AN UNEVENTFUL LANDING. CLEANED AND RESEATED CONNECTORS ON BOTH FLAP TRANSMITTERS, RUN FLAPS SEVERAL TIMES OPS NORMALLY. REMOVED AND REPLACED OPC STYLUS PEN BATTERY, OPS CKS NORMAL.

Part: O-RING — BROKEN (NR 1 ENGINE)

DIVERTED TO LAS DUE TO NR 1 ENGINE OIL LOW QUANTITY DECREASING IN FLIGHT. AIRCRAFT MADE AN UNEVENTFUL LANDING. REMOVED AND REPLACED NR 1 ENGINE STARTER GARLOCK O-RING PER BOEING M/M.

Part: STRAP — CRACKED (BS 313)

DURING SCHEDULED D-CHECK, FOUND STRAP CRACKED AT BS 313, RBL 41, WL 276. REPAIRED PER BOEING SRM.

Part: BULKHEAD ANGLE — CORRODED (BS 500)

DURING SCHEDULED D-CHECK, FOUND FLOOR TO BULKHEAD SUPPORT ANGLE CORRODED AT BS 500D. REPLACED PER BOEING SRM.

Part: SPLICE — CRACKED (BS 907)

DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICES CRACKED AT BS 907, AT S4L AND S4R. REPLACED PER BOEING SRM.

Part: SLAT — DAMAGED (NR 6 LE SLAT)

DURING SCHEDULED D-CHECK, FOUND NR 6 SLAT CRACKED IN LOWER T/E SKIN NEAR O/B UPSTOP. REPAIRED PER BOEING SRM AND BOEING DRAWING 65C30133.

Part: STRINGER — CRACKED (BS 1140-1145)

DURING SCHEDULED D-CHECK, FOUND STRINGER 5 LOWER CHORD CRACKED AT BS 1140 TO 1145. INSTALLED NEW CHORD PER BOEING SRM.

Part: SUPPORT — CORRODED (BS 983)

DURING SCHEDULED D-CHECK, FOUND FLOOR SUPPORT CORRODED AT BS 983, LBL 17.5. REPLACED PER BOEING SRM.

Part: ANGLE — CRACKED (BS 294)

DURING SCHEDULED D-CHECK, FOUND L-ANGLE CRACKED AT BS 294, RBL 54.5, WL 208. REPLACED PER BOEING SRM.

Part: FRAME — CRACKED (BS 616)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACK AT BS 616, WL 200, LBL 65. REPAIRED PER BOEING SRM.

Part: SUPPORT — CRACKED (BS 540)

DURING SCHEDULED D-CHECK, FOUND FLOOR SUPPORT CRACK AT BS 540, LBL 207. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (NR 2 LE SLAT)

DURING SCHEDULED D-CHECK, FOUND NR 2 SLAT T/E SKIN CRACKED BELOW ACTUATOR ATTACH POINT. REPAIRED PER BOEING SRM AND DRAWING 65C30133.

Part: FRAME — CRACKED (FUSELAGE)

DURING SCHEDULED D-CHECK, FOUND HAT RACK ATTACH BRACKET BODY FRAMES CRACKED AT BS 847, S9L, AT BS 827, S9L, AT BS 907, S9R, AND AT BS 767, S9L. REPAIRED PER TRAMCO EWO 97-0204 AND BOEING SRM.

Part: ANGLE — CORRODED (BS 270)

DURING SCHEDULED D-CHECK, FOUND Z-ANGLE CORRODED AT BS 270, WL 208. REPAIRED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 967.5)

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORRODED AROUND FASTENER HOLES, BS 967.5, LBL 44 , WL 208. REPAIRED PER BOEING SRM.

Part: SKIN — DAMAGED (BS 939/349)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DAMAGED AT BS 939, WL 192 AND AT BS 349, WL 151, LBL 23. REPAIRED PER BOEING SRM.

Part: MOPSILL — CORRODED (BS 950-992)

DURING SCHEDULED D-CHECK, FOUND MOPSILL CORRODED AT BS 950 TO 953 AND 963 TO 992, BL 50.5 AND 52, WL 208 AND 209. REPAIRED PER BOEING SRM.

Part: ANGLE — CRACKED (BS 936)

DURING SCHEDULED D-CHECK, FOUND SHEAR WEB UPPER ATTACH ANGLE CRACKED AT BS 936, BL 0. REPAIRED PER BOEING SRM.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED D-CHECK, FOUND BS 178 BULKHEAD CRACKED ON AFT SIDE, BL 0, WL 190, AT LBL 67, WL 201 TO 202.5, AT LBL 4.7, AND WL 199 TO 199.5. REPAIRED PER BOEING SRM AND TRAMCO EWO 97-0211.

Part: ANGLE — CRACKED (BS 936)

DURING SCHEDULED D-CHECK, FOUND SHEAR WEB UPPER ATTACH L-ANGLE CRACKED AT BS 936, BL 0, WL 208. REPAIRED PER BOEING SRM.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED D-CHECK, FOUND BS 178 BULKHEAD CRACKED AT RBL 4.7, WL 201.5 TO 202.25. REPAIRED PER BOEING SRM AND TRAMCO EWO 97-0210.

Part: FLOORBEAM — CORRODED (BS 987)

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORRODED AROUND FASTENER HOLES, BS 987, LBL 4.5, 33, 27, 21, WL 208. REPAIRED PER TRAMCO EWO 97-0212.

Part: FLOORBEAM — CRACKED (BS 947)

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CRACKED AROUND FASTENER HOLE, BS 947, LBL 53. REPAIRED PER BOEING SRM.

Part: COALESCER BAG — DIRTY (RIGHT)

INFLIGHT, RIGHT PACK TRIPPED OFF. RESET AND IT TRIPPED AGAIN, REPORTED LIGHT SMOKE. RETURNED TO LAS AND MADE AN UNEVENTFUL LANDING. CHECKED SYSTEM AND AIR CYCLE MACHINE FOR LEAKS, NONE FOUND. REPLACED COALESCER BAGS AND OP CHECKED PER BOEING M/M.

Part: PACK — FAILED (RIGHT)

INFLIGHT, RT PACK TRIPPED OFF ALONG WITH A SMOKE SMELL. ISOLATED TO RIGHT PACK, LEFT PACK CLEARED SMELL. AIRCRAFT RETURNED TO BNA AND MADE AN UNEVENTFUL LANDING. REPLACED COMPRESSOR DISCHARGE, TURBINE INLET AND DUCT OVERHEAT SENSORS PER BOEING M/M.

Part: CONTROLLER — INOPERATIVE (E/E BAY)

AFTER TAKEOFF, CREW WAS UNABLE TO PRESSURE AIRCRAFT, RETURNED TO PHX AND MADE AN UNEVENTFUL LANDING. REPLACED PRESSURE CONTROLLER AND OP CHECKED SYSTEM PER BOEING M/M.

Part: SKIN — CRACKED (L2 DOOR CUTOUT)

DURING SCHEDULED 1/2 D CHECK, FOUND CRACK IN UPPER CORNER OF LOWER HINGE SKIN CUTOUT AT FWD SERVICE DOOR. REPAIRED PER SWA ACO 3189-52.