N934DN

Part: SKIN — CRACKED (LT WING) · airframe 43,587 hrs · 26,782 cycles

WHILE ACCOMPLISHING OPEN HOLE INSPECTION IAW PRI 568225-14, R1, STEP 7, FOUND A CRACKED INDICATION ON THE NR 7 LT WING UPPER SURFACE XOS 324, REAR SPAR. ACCOMPLISHED A PERMANENT REPAIR IAW ER/A 268226-14, REV ORIGINAL. HFEC ACCOMPLISHED.

Part: SPAR — CORRODED (LT WING) · corrosion level 2 · airframe 43,587 hrs · 26,782 cycles

LEFT WING UPPER PANELS FOUND THE AFT SPAR, LOWER FWD CHORD EXFOLIATED AT XRS 545.38. ACCOMPLISHED A PERMANENT REPAIR ON AFT SPAR IAW ER/A 568227-14, REV ORIGINAL. HFEC ACCOMPLISHED.

Part: TAB — DAMAGED (RUDDER) · airframe 43,589 hrs · 26,783 cycles

RUDDER TAB HAD FOUR AREAS OF MISSING PAINT AND FLAME SPRAY ON THE RT SIDE ALL UNDER FOUR SQUARE INCHES NOT LONGER THAN 2 INCHES IN ANY DIRECTION, AND ARE SEPARATED BY MORE THAN 2 INCHES AND NOT TOTALING MORE THAN 20 SQUARE INCHES. REPAIRED THE RUDDER TAB IAW SRM 55-41-01.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 43,520 hrs · 26,739 cycles

FOUND L2 EMERGENCY EXIT IDENTIFIER LIGHT INOPERATIVE. R & R THE EMERGENCY LIGHT ASSY IAW AMM 33-51. OPS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 43,357 hrs · 26,642 cycles

R1 DOOR EMERGENCY EXIT SIGN INOPERATIVE. REPLACED BATTERY PACK. EMERGENCY LIGHTS TESTED NORMAL.

Part: TIRE — FAILED (MLG) · airframe 43,340 hrs · 26,633 cycles

TIRE FAILURE DURING TAKE OFF ROLL. ABS LIGHT CAME ON JUST PRIOR TO ROTATION. FLIGHT CONTINUED AND LANDED WITH NO ISSUES. FOUND THE NR 3 MAIN TIRE FAILED. REPLACED THE NR 3 AND 4 MAIN WHEEL ASSEMBLIES. REPLACED THE NR 3 BRAKE ASSEMBLY AND ANTISKID TRANSDUCER.

Part: RING — DEFECTIVE (RT ENGINE) · airframe 43,302 hrs · 26,609 cycles

DIV INTO DEN DUE TO RIGHT ENGINE IN INFLIGHT SHUT DOWN CAUSED BY LOW OIL PRESSURE. MTC FOUND OIL LEAKING FROM VSCF GENERATOR DRIVE PAD DRAIN. WINDMILLING INSPECTIONS PERFORMED AND VSCF SEAL FACE AND ROTATING RING REPLACED. LEAK CHECKS PERFORMED AND AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 42,929 hrs · 26,383 cycles

CEILING EXIT SIGN INOP AT 26 ABC-DEF. RELAMPED EXIT SIGN AT 26ABC-DEF CEILING REF AMM 33-51. CKS OK.

Part: SPAR CAP — DAMAGED (VERTICAL STAB) · airframe 42,654 hrs · 26,219 cycles

DAMAGE FOUND IN FASTENER HOLE VERTICAL STABILIZER, LEFT FRONT SPAR CAP . FORWARD FLANGE. CLEANED HOLE FABRICATED AND INSTALLED REPAIR STRAP IAW PRI/ERA 564082-14AD.

Part: FIRE WARNING — FALSE ACTIVATION (LT NACELLE) · airframe 41,913 hrs · 25,773 cycles

DURING APPROACH, DECLARED AN EMERGENCY DUE TO A LEFT ENGINE FIRE WARNING. FLIGHT CREW SHUTDOWN THE LEFT ENGINE, TEE HANDLE WAS PULLED AND BOTH FIRE BOTTLES WERE DISCHARGED. NO EVIDENCE OF ACTUAL FIRE. MAINTENANCE R & R BOTH FIRE BOTTLES. R & R THE ENGINE FIRE WARNING HARNESS AND MULTIPLE OVERHEAT/FIRE DETECTION LOOPS.

Part: LANYARD — DETACHED (EVAC SLIDE) · airframe 41,564 hrs · 25,579 cycles

LANYARD DETACHED FROM ESCAPE SLIDE AT R1 DOOR. RE-ATTACHED LANYARD.

Part: DUCT — DELAMINATED (THRUST REVERSER) · airframe 41,374 hrs · 25,477 cycles

ABORTED TAKE OFF DUE TO LT ENGINE FIRE DET FAULT AT 80 KNTS. FOUND LEFT ENGINE LOWER THRUST REVERSER C-DUCT DELAMINATED IN COLD STREAM. PERFORMED TAKE OFF POWER RUNS ON LT ENGINE. LT ENG FIRE DET FAULT OCCURRED AT 1.39 EPR. REPLACED LT ENG LWR C-DUCT. RAN ENGINE TO POWER WITH NO FAULTS. PERFORMED ALL NO GO ODI TASKS. NO FAULTS FOUND. THE DELAMINATION OF THE LWR C-DUCT IS SUSPECTED TO HAVE IMPACTED NORMAL OPERATION OF THE FIRE LOOP OPERATION.

Part: FRAME — CRACKED (NLG WW) · airframe 40,822 hrs · 25,152 cycles

NOSE WHEEL WELL LEFT FRAME AT DOOR STOP HAS FORWARD UPPER FASTENER HOLE CRACKED. REPAIRED IAW SRM 51-10-03, 51-10-04 AND 53-90-01.

Part: CONNECTOR — DAMAGED (CHARGER) · airframe 40,824 hrs · 25,154 cycles

OVERWING EMERGENCY BATTERY PACK HAS DAMAGED CONNECTOR ON THE CHARGER. REMOVED AND REPLACED. OPERATION CHECKS GOOD.

Part: FLOOR SUPPORT — DAMAGED (FUSELAGE) · airframe 40,822 hrs · 25,152 cycles

ELONGATED HOLE ON FLOOR SUPPORT, STA 984 RBL 54. REMOVED AND REPLACED FLOORBEAM IAW SRM 51-30-05 AND DWG 9915527.

Part: DOOR FRAME — CRACKED (NLG WW) · airframe 40,822 hrs · 25,152 cycles

NOSE WHEEL WELL RIGHT FRAME AT FORWARD DOOR STOP IS CRACKED T UPPER FASTENER HOLE. REMOVED AND REPLACED CUT OUT FRAME IAW SRM 51-30-02 AND DWG 9910088, REV CJ.

Part: DOOR — DENTED (CABIN) · airframe 40,471 hrs · 24,966 cycles

DENT ON LEADING EDGE OF R1 DOOR APPROXIMATELY 18 INCHES FROM BOTTOM OF DOOR. STRAIGHTENED EDGE. HFEC, NO CRACKS.

Part: PIN — DISLODGED (L1 DOOR SLIDE) · airframe 39,245 hrs · 24,217 cycles

L1 DOOR SLIDE PIN OUT. REMOVED AND REPLACED SLIDE.

Part: LANYARD — BROKEN (R1 DOOR) · airframe 38,789 hrs · 23,952 cycles

FOUND R1 DOOR SLIDE LANYARD BROKEN. REPLACED SAME.

Part: CUSP WEB — CRACKED (BS 880) · airframe 35,791 hrs · 22,055 cycles

CRACKS ON LT CUSP WEB STA 880, BETWEEN 44-54, PASSENGER CABIN. REPAIRED IAW SRM 53-00-01, PARA 8. LP 1926234.

Part: STOP FITTING — CRACKED (DOOR FRAME) · airframe 35,791 hrs · 22,055 cycles

CRACKED STOP FITTING ON FORWARD EDGE PRJECTION BEAM 4 AND AFT EDGE PROJECTION BEAM 5 AT MID CARGO DOOR. BEAM 4 AND 5 WERE REMOVED AND NEW STOP FITTINGS FORWARD/AFT WERE INSTALLED IAW SRM 51-30-01 AND 51-30-05. LP 1927484.

Part: STRUCTURE — CORRODED (BS 952) · airframe 35,689 hrs · 21,997 cycles

CORROSION BS 952 AND X=55 LT SIDE AT PAX CABIN. REPAIRED IAW ERA 533328-14AD, REV A.

Part: DOUBLER — CORRODED (BS 1300-1307) · airframe 35,680 hrs · 21,989 cycles

CORROSION ON PRODUCTION DOUBLER OF INNER SKIN, STA 1300-1307, L22L AT AFT CARGO COMPARTMENT. R & R IAW ERA 534330-14, REV O.

Part: STRUCTURE — CORRODED (BS 902-984) · airframe 35,680 hrs · 21,989 cycles

EXFOLIATION CORROSION ON WING BOX, STA 984, X=54, 902 X=-44 TO 54, 933, X=45 AND 952, X=55. CORROSION WAS REMOVED. REPAIRED IAW ERA 533317-14, REV O. LP 1896303.

Part: ACCESS PANEL — CORRODED (WING) · airframe 39,766 hrs · 24,549 cycles

CORROSION ON COUNTERSINK OF FUEL ACCESS ACCESS PANEL 250HB. FOUND TO BE OUT OF LIMITS. REPAIRED THE ACCESS PANEL.

Part: ACCESS PANEL — CORRODED (WING) · airframe 39,766 hrs · 24,549 cycles

CORROSION ON COUNTERSINK OF FUEL ACCESS PANEL 620DB. FOUND OUT OF LIMITS. REPLACED THE ACCESS PANEL.

Part: STRUCTURE — CORRODED (BS 803-948) · airframe 35,680 hrs · 21,989 cycles

EXFOLIATION CORROSION ON WING BOX, FS 948 AND X=-44 BETWEEN 902-908, X=-44 TO -54, FS 803-894, X=-44 TO -54RT. REMOVED CORROSION. REPAIRED IAW ERA 53331-14, REV O. LP 1896307.

Part: INTERCOSTAL — CRACKED (BS 997) · airframe 35,680 hrs · 21,989 cycles

CRACKED INTERCOSTAL ON LOWER KEEL BEAM AT BS 997. R & R INTERCOSTAL IAW DWG 9936368, REV AW.

Part: CARGO TRACK — CORRODED (BS 1269-1288) · airframe 35,680 hrs · 21,989 cycles

CORROSION ON LT TIE TRACK BETWEEN BS 1269 TO 1288 AT AFT CARGO COMPARTMENT. TASK 53-100-19. REMOVED, FABRICATED AND INSTALLED REPAIR PART IAW SRM 53-40-01, 51-30-02 AND 51-10-05.

Part: CARGO TRACK — CORRODED (BS 1193-1250) · airframe 35,680 hrs · 21,989 cycles

CORROSION ON TIE TRACK FROM BS 1193 TO 1250 BETWEEN LONGERON 28L TO 27L AT AFT CARGO COMPARTMENT. REMOVED, FABRICATED AND INSTALLED REPAIR PART IAW SRM 51-30-01, 51-30-02 AND 53-40-01.

Part: DOOR FRAME — CORRODED (BS 693-750) · airframe 35,680 hrs · 21,989 cycles

CORROSION ON MID LOWER DOOR JAMB BEAM, BS 693-750 AT MID CARGO COMPARTMENT. REPAIRED DOOR JAMB BEAM IAW ERA 53333-14, REV O.

Part: ACCESS PANEL — CORRODED (WING) · airframe 39,766 hrs · 24,549 cycles

CORROSION ON COUNTERSINK OF FUEL ACCESS PANEL 620GB. FOUND OUT OF LIMITS. REPLACED THE ACCESS PANEL.

Part: DOOR FRAME — CORRODED (BS 370-427) · airframe 35,680 hrs · 21,989 cycles

CORROSION ON FORWARD LOWER CARGO DOOR JAMB BEAM, BS 370-427, TASK 53-121-02. R & R SECTION IAW SRM 53-60-02, FIG 11.

Part: ACCESS PANEL — CORRODED (WING) · airframe 39,766 hrs · 24,549 cycles

CORROSION ON COUNTERSINK ON FUEL ACCESS PANEL 520CB. FOUND TO BE OUT OF LIMITS. REPLACED THE ACCESS PANEL.

Part: DOOR FRAME — CORRODED (BS 408-427) · airframe 35,680 hrs · 21,989 cycles

SURFACE CORROSION ON FORWARD DOOR JAMB WEB, BETWEEN BS 408-427 AND FORWARD CARGO COMPARTMENT. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED DOUBLER REPAIR IAW SRM 53-00-01, 51-10-03, ERA 511165-14, MA, REV C AND 51-30-02.

Part: FLOOR PANEL — CRACKED · airframe 35,680 hrs · 21,989 cycles

CRACK ON GENERATION FLOOR NR 221XF. CRACK WAS STOPPED DRILLED. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 51-00-01 AND 53-00-01, FIG 4 AND 51-30-02.

Part: FLOOR SUPPORT — CRACKED · airframe 35,680 hrs · 21,989 cycles

CRACKS ON FLOOR CHANNELS. CRACKS WERE STOPPED DRILLED. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 53-20-03, FIG 13 AND 51-10-04.

Part: ACCESS PANEL — CORRODED (WING) · airframe 39,766 hrs · 24,549 cycles

CORROSION ON COUNTERSINK OF FUEL ACCESS PANEL 520LB. REMOVED CORROSION. INSTALLED THE ACCESS PANEL.

Part: ACCESS PANEL — CORRODED (WING) · airframe 39,766 hrs · 24,549 cycles

CORROSION ON COUNTERSINK FUEL ACCESS PANEL 520AT. FOUND OUT OF LIMITS. REPLACED THE ACCESS PANEL.

Part: ACCESS PANEL — CORRODED (WING) · airframe 39,766 hrs · 24,549 cycles

CORROSION ON COUNTERSINK OF FUEL ACCESS PANEL 520FT. FOUND OUT OF LIMITS. REPLACED THE ACCESS PANEL.

Part: FLOORBEAM — CRACKED (BS 984) · airframe 35,680 hrs · 21,989 cycles

CRACK ON FLOORBEAM, BS 984, X=58 AND X=-58. WING BOX AREA. REPLACED FLOORBEAM IAW SRM 51-30-02 AND 51-30-03 AND DWG 9915527, REV F.

Part: LONGERON — CRACKED (BS 1475) · airframe 35,680 hrs · 21,989 cycles

CRACK ON LONGERON 2R, BS 1475 AFT ACCESSORY COMPARTMENT. REPLACED SECTION IAW SRM 51-30-05, 51-10-05 AND 51-10-03.

Part: LONGERON — CRACKED (BS 1494) · airframe 35,680 hrs · 21,989 cycles

CRACKED LONGERON 3R, STA 1494 AFT ACCESSORY COMPARTMENT. REPAIRED IAW SRM 53-10-01, RIG 7 AND 51-10-03.

Part: ACCESS PANEL — CORRODED (WING) · airframe 39,766 hrs · 24,549 cycles

CORROSION ON FUEL ACCESS PANEL 520CB. FOUND OUT OF LIMITS. REPLACED THE ACCESS PANEL.

Part: ACCESS PANEL — CORRODED (WING) · airframe 39,772 hrs · 24,554 cycles

CORROSION ON THE FUEL ACCESS PANEL 620FT ON COUNTERSINKS. FOUND OUT OF LIMITS. REPLACED THE ACCESS PANEL.

Part: ACCESS PANEL — CORRODED (WING) · airframe 39,772 hrs · 24,554 cycles

CORROSION ON COUNTERSINK OF THE FUEL ACCESS PANEL 620CT. REPLACED THE ACCESS PANEL.

Part: ACCESS PANEL — CORRODED (WING) · airframe 39,772 hrs · 24,554 cycles

CORROSION ON COUNTERSINK OF THE FUEL ACCESS PANEL 520CT. REPLACED THE ACCESS PANEL.

Part: DOOR FRAME — CRACKED (RT MLG DOOR) · airframe 35,680 hrs · 21,989 cycles

CRACKED BEYOND STOP DRILL ON RT MLG FORWARD DOOR JAMB INBD CORNER. REMOVED DAMAGED CHANNEL. FABRICATED AND INSTALLED REPAIR PART IAW SRM 51-30-02 AND 51-30-05.

Part: ANGLE — CRACKED (VERTICAL STAB) · airframe 35,680 hrs · 21,989 cycles

CRACK ON LT/RT INTERNAL VERTIACL STABILIZER ATTACH DORSAL ANGLES BETWEEN STA Y=1458 TO 1486. DORSAL ANGLES WERE REMOVED, FABRICATED AND INSTALLED IAW SRM 51-30-02 AND 51-30-05.

Part: ACCESS PANEL — CORRODED (WING) · airframe 39,772 hrs · 24,554 cycles

CORROSION ON COUNTERSINK OF THE FUEL PANEL 620HB. REPLACED THE ACCESS PANEL.

Part: ACCESS PANEL — CORRODED (WING) · airframe 39,772 hrs · 24,554 cycles

CORROSION ON COUNTERSINK OF THE FUEL ACCESS PANEL 520QB. REPLACED THE ACCESS PANEL.

Part: SEAT TRACK — CORRODED (BS 507-560) · airframe 35,680 hrs · 21,989 cycles

CORROSION ON LT SEAT TRACK STA 507-510, 555-560, X=54. REMOVED DAMAGED AREAS AND INSTALLED IAW SRM 53-40-01.

Part: ANGLE — CRACKED (BS 1494) · airframe 35,680 hrs · 21,989 cycles

CRACKED CLIPS AT STA 1494, BETWEEN 2LT TO 3LT AND 2 RT TO3 RT AFT ACCESSORY COMPARTMENT. R & R CLIPS IAW SRM 51-30-02, 51-30-05, 51-10-03.

Part: ACCESS PANEL — CORRODED (WING) · airframe 39,772 hrs · 24,554 cycles

CORROSION ON COUNTERSINK OF THE FUEL ACCESS PANEL 620AT. REPLACED THE ACCESS PANEL.

Part: CUSP WEB — CORRODED (BS 536-541) · airframe 35,680 hrs · 21,989 cycles

CORROSION ON LT CUSP WEB BETWEEN BS 536 - 541, X=54 AND X=60. REPAIRED IAW SRM 53=20=02, FIG 16.

Part: DUCT — WORN (A/C DUCT) · airframe 35,680 hrs · 21,989 cycles

WEAR ON AIR CONITIONING EXHAUST DUCT. REPAIRED IAW SRM 53-50-03.

Part: ACCESS PANEL — CORRODED (WING) · airframe 39,772 hrs · 24,554 cycles

CORROSION ON COUNTERSINK OF THE FUEL ACCESS PANEL 620CB. REPLACED THE ACCESS PANEL.

Part: WEB — CRACKED (BS 146) · airframe 35,680 hrs · 21,989 cycles

CRACK ON WEB AT STA 146, COCKPIT FLOOR STRUCTURE. REPAIRED IAW SRM 53-00-01, FIG 6.

Part: ACCESS PANEL — CORRODED (WING) · airframe 39,772 hrs · 24,554 cycles

CORROSION ON COUNTERSINK OF THE FUEL ACCESS PANEL 520GB. REPLACED THE ACCESS PANEL.

Part: ACCESS PANEL — CORRODED (WING) · airframe 39,772 hrs · 24,554 cycles

CORROSION ON COUNTERSINK OF THE FUEL ACCESS PANEL 520DB. REPLACED THE ACCESS PANEL.

Part: PAN — CRACKED (CARGO DOOR) · airframe 35,680 hrs · 21,989 cycles

CRACK ON PAN AFT EDGE BETWEEN BEAMS NR 1 AND NR 2 MID CARGO COMPARTMENT DOOR. STOPPED CRACK IAW SRM 52-30-02, FIG 63. FABRICATED AND INSTALLED DOUBLER IAW SRM 52-30-06. AND 51-30-05.

Part: ACCESS PANEL — CORRODED (WING) · airframe 39,772 hrs · 24,554 cycles

CORROSION ON COUNTERSINK OF THE FUEL ACCESS PANEL 520DT. REPLACED THE ACCESS PANEL.

Part: ACCESS PANEL — CORRODED (WING) · airframe 39,772 hrs · 24,554 cycles

CORROSION ON COUNTERSINK OF THE FUEL ACCESS PANEL 620DT. REPLACED THE ACCESS PANEL.

Part: CUSP WEB — CORRODED (BS 785) · airframe 35,680 hrs · 21,989 cycles

CORROSION ON LT CUSP WEB STA 785, BETWEEN S=54 AND X=60. REPAIRED IAW SRM 53-20-02, FIG 11.

Part: CUSP WEB — CORRODED (BS 216-237) · airframe 35,680 hrs · 21,989 cycles

CORROSION ON OF CUSP WEB AND CRACK ON LIGHTNING HOLE BETWEEN STA 216 AND 237. X=44 TO X=54 RT SIDE. R & R WEB IAW SRM 51-30-05, 51-10-05 AND 51-10-03.

Part: SUPPORT ANGLE — CRACKED (1494) · airframe 35,680 hrs · 21,989 cycles

CRACKED LEFT ANGLE SUPPORT, STA 1494, AFT ACCESSORY COMPARTMENT. R & R ANGLE IAW SRM 51-10-03, 51-30-02, 51-30-05 AND ERA 9911840, REV DC.

Part: BEAM — CRACKED (PAX DOOR) · airframe 35,680 hrs · 21,989 cycles

CRACKED BEAM, NR 2 OF FORWARD ENTRANCE DOOR AFT SECTION. REPAIRED IAW SRM 52-10-02.

Part: STRUCTURE — DAMAGED (L1 DOOR) · airframe 35,151 hrs · 21,692 cycles

L1 DOOR, LOWER FORWARD CORNER ROLLED UNDER ALONG RIVET LINE. WORKED LOWER FORWARD CORNER OF L1 DOOR IAW SRM 52-01-01, PARA 8C.

Part: DOOR SILL — CORRODED (AFT CARGO) · airframe 33,196 hrs · 20,460 cycles

AFT CARGO DOOR SILL HAS LIGHT CORROSION. REPAIRED IAW SRM 53-60-02.

Part: DOUBLER — CRACKED (BS 1531 FRAME) · airframe 33,196 hrs · 20,460 cycles

TAIL INTERIOR, CANTED FRAME BS 1531 DOUBLER WEBS CRACKED LBL 23. ACCOMPLISHED ERA 524305-14, REV O.

Part: INTERCOSTAL — DAMAGED (BS 1567) · airframe 35,350 hrs · 21,794 cycles

RUDDER ACTUATOR OTBD ATTACH FITTING INTERCOSTAL BS 1567 DAMAGED. R & R THE INTERCOSTAL IAW SRM 51-00-00, VOL 1.

Part: FRAME — CRACKED (BS 1549) · airframe 33,171 hrs · 20,442 cycles

TAIL INTERIOR, CANTED FRAME BS 1549 WEB CRACKED LBL 19 AT FAST. REMOVED DAMAGE. FABRICATED AND INSTALLED WEB REPAIR IAW SRM 53-10-03, FIG 13.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 33,162 hrs · 20,439 cycles

DURING SERVICE CHECK, FOUND R1 SERVICE DOOR EXIT LIGHT INOPERATIVE. REPAIRED IAW ERA 524119-14, SECTION 1 ACCOMPLISHED. SECTION 2.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 32,834 hrs · 20,257 cycles

EMERGENCY LIGHT AT SEAT ROWS 36-37 CDE INOPERATIVE. R & R EMERGENCY CEILING LIGHT POWER SUPPLY BATTERY AT ROW 36DE IAW AMM. OPS CHECKED NORMAL.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 32,288 hrs · 19,918 cycles

DURING SERVICE CHECK, EMERGENCY CEILING LIGHTS, ROW 13-21, WILL NOT REMAIN ARMED. MAINTENANCE R & R B5-228 BATTERY PACK IAW AMM. OPS CHECKED NORMAL.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 31,340 hrs · 19,403 cycles

ON SERVICE CHECK, FOUND OVERWING EVACUATION LIGHTS ON WITH EMERGENCY POWER SWITCH IN ARMED POSITION. R & R BATTERY PACK B5-125. OPERATION CHECKS GO.

Part: SKIN — CRACKED · airframe 31,007 hrs · 19,224 cycles

SKIN CRACKED AT CANTED FRAME Y953-R 2.5 FEET BELOW PYLON. CUTOUT DAMAGE. FABRICATED DOUBLER AND FILLER IAW SRM 53-00-01, FIG 6.

Part: CABLE — BROKEN (COCKPIT DOOR) · airframe 29,898 hrs · 18,603 cycles

COCKPIT DOOR LOWER HINGE CABLE BROKEN. R & R COCKPIT DOOR LOWER HINGE CABLE IAW AMM. PERMANENT REPAIR COMPLIED WITH ERA 509212-14.

Part: BULKHEAD — DAMAGED (BS 1395 L22L) · airframe 28,528 hrs · 17,836 cycles

DURING HMV AT MIA, THE AFT FUSELAGE WAS DAMAGED DURING A JACKING INCIDENT. AREAS REPAIRED PER ERA 502764-14 REV O AT AFT PRESSURE BULKHEAD STA 1395 APB AND SKIN L-22L.

Part: SKIN — DAMAGED (BS 1276-1307) · airframe 28,528 hrs · 17,836 cycles

DURING HMV, AFT FUSELAGE WAS DAMAGED DURING A JACKING INCIDENT. AREAS REPAIRED PER ERA 502763-14 REV O AT STA 1276 TO 1307 L24R TO L26R.

Part: SKIN — DAMAGED (BS 1193-1231) · airframe 28,528 hrs · 17,836 cycles

DURING HMV AT MIA, THE AFT FUSELAGE WAS DAMAGED DURING A JACKING INCIDENT. AREAS REPAIRED PER ERA 502762-14 REV O AT STA 1193 THRU STA 1231 L20R- L26R.

Part: SKIN — DAMAGED (BS 816-1145) · airframe 28,529 hrs · 17,836 cycles

LIGHTNING STRIKE FUSELAGE SKIN BS 816 - 1145, LONGERON 2L. REPAIRED IAW ERA 499966-14.

Part: SKIN — DAMAGED (BS 350-360) · airframe 28,529 hrs · 17,836 cycles

FUSELAGE SKIN BS 350-360, LONGERONS 26-27R DAMAGED. REPAIRED IAW ERA 499998-14.

Part: WEB — DAMAGED (NLG) · airframe 28,529 hrs · 17,836 cycles

LANDING GEAR, NOSE GEAR, SUPPORT WEB DAMAGED. REPAIRED IAW ERA 499995-14.+

Part: FLOORBEAM — DAMAGED (BS 275, RBL 30) · airframe 28,529 hrs · 17,836 cycles

FLOORBEAM BS 275 RBL 30 DAMAGED. REPAIRED IAW ERA 499996-14.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 28,528 hrs · 17,836 cycles

FUSELAGE SKIN WRINKLED BETWEEN STA 769-807 BETWEEN L26R AND L26L DURING A JACKING INCIDENT. REPAIR PER ERA 487467-14 REV O.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 28,528 hrs · 17,836 cycles

DURING HMV AT MIA, THE AFT FUSELAGE WAS DAMAGED DURING A JACKING INCIDENT. AREAS REPAIRED ERA 502765-14 REV O.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 28,528 hrs · 17,836 cycles

FUSELAGE WRINKLED BETWEEN STA 769-788 BETWEEN L26L AND L18L DURING JACKING INCIDENT. REPAIRED PER ERA 491788-14 REV O.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 28,528 hrs · 17,836 cycles

LT UPPER FUSELAGE VENT BOX FWD STIFFENER CRACKED. REPLACED STIFFENER PER MD 90 SRM 51-30-05.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 28,528 hrs · 17,836 cycles

FUSELAGE SKIN AND FRAME CLIPS PULLED OUTWARD AT 4 EA EXTERNAL WEIGHT ATTACH POINTS. ALSO BOTH LOWER BLIND NUTS LOOSE STA 218 L19L TO L20L. DAMAGE OCCURRED DURING JACKING INCIDENT. REPAIRED AREAS PER ERA 491740-14

Part: FRAME — DAMAGED (FUSELAGE) · airframe 28,528 hrs · 17,836 cycles

APU COMP AT FWD PRESSURE BULKHEAD LWR FRAME DAMAGED DURING JACKING INCIDENT. BOEING AOG REPLACED FRAME UNDER BOEING AGREEMENT #DAL-RE-1207549R2 AND REPAIR INDEX ITEM # 7.2 DAMAGE SURVEY 21.

Part: SUPPORT FITTING — CORRODED (RT MLG) · airframe 28,528 hrs · 17,836 cycles

C/W EA 02-093855-03AD REV A ME 02 OPN 0201 REF R/C 178 AND N/R 830351 FOR AD 2010-16-11.

Part: SKIN — DENTED (FUSELAGE) · airframe 28,528 hrs · 17,836 cycles

SKIN DENTED IN 2 EACH AREAS LT UPPER FUS STA 237 & 262 & L-18L. CUT OUT 7 TRIMMED DAMAGED SKIN & REPAIR BETWEEN STA 229 THRU STA 263.5 & BETWEEN L-18L THRU L-16L AS PER MD90 SRM 53-30-01 FIG 5. TREATED, PRIMED & TOP COATED AS PER MD-90 SRM 51-10-03. INSTALLED FLUSH SKIN REPAIR BETWEEN STA 229 THRU STA 263.5 & L-18L - L-16L AS PER MD 90 SRM 53-30-01 FIG 5.

Part: SKIN — DENTED (FUSELAGE) · airframe 28,528 hrs · 17,836 cycles

SKIN DENTED IN 2 AREAS LT UPPER FUS STA 237 AND STA 262 AND L18L. REPAIRED PER MD 90 SRM 53-30-01 FIG 5.

Part: SKIN — CORRODED (RT ELEVATOR) · airframe 28,528 hrs · 17,836 cycles

RIGHT ELEVATOR O/B LOWER SKIN WITH CORROSION. REMOVED CORRODED AREA AND INSTALLED DOUBLER REPAIR PER MD SRM 55-20-03 FIG 2.

Part: SPAR — CRACKED (WING) · airframe 28,529 hrs · 17,836 cycles

WING REAR SPAR CRACKED. REPAIRED IAW AA 5710-01119.

Part: SKIN — DENTED (BS 212) · airframe 33,196 hrs · 20,460 cycles

DENT FOUND IN SKIN AT BS 212.687 BETWEEN S21-22R. REPAIRED IAW ERA 491740-14.

Part: CUSP WEB — CRACKED (BS 1344-1364) · airframe 28,529 hrs · 17,836 cycles

CUSP WEB CRACKED AT BS 1344-1364. REPAIRED IAW SRM 53-20-02, VOL 1, PAR 6.

Part: SKIN — DENTED (CARGO DOOR) · airframe 28,529 hrs · 17,836 cycles

DENT ON MID CARGO DOOR BS 718 L22-23R. REPAIRED IAW SRM 53-30-01, FIG 1, SHEET 2.

Part: CUSP WEB — CRACKED (CABIN) · airframe 28,529 hrs · 17,836 cycles

CUSP WEB CRACKED. REPAIRED IAW SRM 53.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 28,529 hrs · 17,836 cycles

ATTACH ANGLE CRACKED ON TOP FUSELAGE TO VERTICAL STAB LT AT STA 15230.225 REPAIRED IAW SRM 55.

Part: SKIN — CRACKED (BS 1475) · airframe 28,529 hrs · 17,836 cycles

FUSELAGE SKIN CRACKED AT BS 1475 AT LONGERON 2L & 2R. REPAIRED IAW TWX HLO-HLO-11-0009-17B - 8100-9.