N958DN

Part: SUPPORT — DAMAGED (FUSELAGE) · airframe 51,931 hrs · 27,811 cycles

FORWARD CARGO COMPARTMENT AFT BULKHEAD DAMAGED AT STA 522, L29R. REMOVED WALL SUPPORT. INSTALLED NEW SUPPORT IAW SRM 51-30.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 51,585 hrs · 27,599 cycles

CATWALK EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY. OPERATION CHECKED OK.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 51,169 hrs · 27,336 cycles

FOUND CATWALK EMERGENCY LIGHTS, LEFT SIDE INOPERATIVE. REMOVED AND REPLACED BATTERY PACK AT FLIGHT ATTENDANT SEAT. OPS CHECKED GOOD.

Part: SKIN — CORRODED (FUSELAGE) · airframe 51,125 hrs · 27,310 cycles

CORROSION ON RIGHT SIDE OF FUSELAGE AFT OF C3 DOOR. REPAIRED IAW ERA 549447-14.

Part: PANEL — DAMAGED · airframe 51,117 hrs · 27,304 cycles

FOUND RIGHT MAIN LANDING GEAR FLAP CLOSEOUT SPRING PANEL DAMAGED. REMOVED AND REPLACED INBOARD BUTE DOOR AND BEAM ASSEMBLY IAW DWG 5936844.

Part: TRANSDUCER — MALFUNCTIONED (ANTI-SKID SYS) · airframe 50,796 hrs · 27,111 cycles

RIGHT INBD ANTISKID FAULT ON LANDING. CREW INFORMED BY TOWER THAT RT INBD TIRE WAS FLAT. MAINTENANCE R & R RT INBD TRANSDUCERS AND NR 3 AND NR 4 TIRES. FORWARD ANTISKID SHUTOFF VALVE TO MCO/PLAC IAW MEL 32-45-01B. 20JUN RECONNECTED ANTISKID RETURN SHUTOFF VALVE. RETURN TO SERVICE CHECK OK. MCO/PLAC REMOVED.

Part: TIRE — BLOWN (RT MLG) · airframe 50,777 hrs · 27,097 cycles

EXPERIENCED A RT INBD BLOWN TIRE EVENT UPON LANDING. MAINTENANCE REPLACED NR 3 AND NR 4 TIRES. AIRCRAFT OK FOR SERVICE.

Part: TIRE — BLOWN (MLG) · airframe 50,777 hrs · 27,097 cycles

EXPERIENCED A BLOWN TIRE EVENT ON LANDING. RT OTBD ANTI-SKID EOAP CAUTION MESSAGE ON LANDING. PERFORMED AACU BITE. AACU FAULTS RT OTBD WHEEL NOT TURNING. REPLACED BOTH NR 3 AND NR 4 MLG TIRE ASSEMBLIES, NR 4 BRAKE ASSEMBLY AND NR 4 DACM DUE TO LEAKING. LEAK AND OPERATIONS CHECK GOOD. ACFT OK FOR SERVICE.

Part: ANTI-SKID SYS — MALFUNCTIONED (MLG) · airframe 50,903 hrs · 27,173 cycles

ON LANDING, AIRCRAFT DISPLAYED RT OTBD ANTI-SKID AND ANTI-SKID FAULT MESSAGES WITH A SUBSEQUENT BLOWN NR 4 MAIN TIRE ASSEMBLY. MAINTENANCE PERFORMED AN AACU BITE. FOUND PRESENT FLIGHT FAULT OF RO WHL NOT TURN. FAULTS STATUS SHOWED NO CURRENT FAULTS OR EOAP MESSAGES. MAINTENANCE FOUND THE NR 4 TIRE ASSEMBLY BLOWN WITH NO EVIDENCE OF FLAT SPOTTING. AFTER INSPECTING THE AIRCRAFT FOR DAMAGE THE NR 4 AND 3 MAIN TIRE ASSEMBLIES WERE REMOVED AND REPLACED PER AMM. AIRCRAFT WAS RETURNED TO SERVICE.

Part: FITTING — CORRODED (BS 207) · airframe 49,661 hrs · 26,453 cycles

CORROSION ON INBD FORWARD FITTING FOR NR 2 GALLEY, BS 207. FOUND TO BE OUT OF LIMITS. REPAIRED IAW ERA 543268-14, REV O.

Part: SEAT TRACK — CORRODED (BS 200-236) · airframe 49,661 hrs · 26,453 cycles

GALLEY 2 SEAT TRACK CORRODED AT BS 200 -- 236, RBL 24. FOUND TO BE OUT OF LIMITS. REPLACED SEAT TRACK IAW SRM 53-40-01.

Part: INTERCOSTAL — CRACKED · airframe 48,840 hrs · 25,934 cycles

INTERCOSTAL ATTACH WEB CRACKED AT LT VENTRAL STAIR STIFFENER. REMOVED, FABRICATED AND INSTALLED REPAIR PARTS IAW ERA 539471-14.

Part: CATWALK — MALFUNCTIONED · airframe 48,112 hrs · 25,534 cycles

VENTRAL STAIR CATWALK WILL NOT STOW IN THE UP POSITION. R & R CLEVIS TO VENTRAL STAIR CATWALK IAW MM. OPS CHECKS OK.

Part: DISPLAY — ODOR (COCKPIT) · airframe 47,490 hrs · 25,117 cycles

F/O PFD DISCOLORED AND FLICKERED WITH A FAINT ELECTRICAL ODOR. TURNED OFF AND THE ODOR WENT AWAY. VERIFIED ODOR IN REMOVED PFD. R & R PFD IAW AMM. OPS CHECKS NORMAL.

Part: SKIN — DAMAGED (BS 1212) · airframe 46,521 hrs · 24,479 cycles

FUSELAGE SKIN REPAIR AT STA 1212, BETWEEN L24R AND L25R DAMAGED. REPAIRED IAW ERA 530255-14, SECTION I.

Part: CONTROLLER — MALFUNCTIONED (CABIN PRESSURE) · airframe 45,167 hrs · 23,622 cycles

RED CABIN ALT ANNUNCIATOR ACCOMPANIED BY AURAL WARNING AT FL280 WITH NO WARNING CABIN AT ALT FL100. INITIATED DESCENT. FOLLOWED QRH AND CABIN ALT NEVER EXCEEDED FL100. F/A AT L2 DOOR REPORTED LOUD WIND NOISE AND RUSH OF COLD AIR DURING DESCENT. AUTO 1 INOPERATIVE. LIGHT NEVER ILLUMINATED UNTIL 5000'. FWD TO MCO/PLAC IAW MEL 21-31-01A. R & R NR 1 CONTROLLER IAW AMM. OPS CHECK GOOD.

Part: SKIN — CRACKED (BS 1475) · airframe 44,496 hrs · 23,207 cycles

FUSELAGE SKIN CRACKED AT BS 1475, 3 INCHES RT OF VERTICAL STABILIZER/TAIL. CUTOUT DAMAGE, INSTALLED DOUBLER, TRIPLER AND LONGERON SPLICE IAW PRI 522196, REV O AND FINAL ERA 5221914, REV O.

Part: FRAME — CRACKED (BS 953) · airframe 44,462 hrs · 23,185 cycles

CRACKED WEB AT CANTED FRAME BS 953, LBL 23. REPAIRED.

Part: UNKNOWN — ODOR (CABIN) · airframe 43,170 hrs · 22,404 cycles

FLIGHT CREW REPORTED ELECTRICAL BURNING ODOR COMING FROM FORWARD GALLEY. ODOR DISSIPATED WITH ACFT IN SAME CONFIGURATION. NO ODOR EVIDENT. INSPECTED FORWARD GALLEY EQUIPMENT, E & E COMPARTMENT AFT OF NLG AND STATIC INVERTER. ACFT OK FOR SERVICE.

Part: LIGHT — OVERHEATED (SEAT 28A) · airframe 43,170 hrs · 22,404 cycles

FLIGHT CREW REPORTED READING LIGHT AT 28A OVERHEATING AND STRONG BURNING PLASTIC ODOR. MX R & R LIGHT ASSY 28A IAW AMM. OPS CHECKS OK.

Part: DOUBLER — CRACKED (VERTICAL STAB) · airframe 43,044 hrs · 22,334 cycles

VERTICAL STABILIZER, LT SIDE RAM AIR INLET ACCESS PANEL INNER DOUBLER CRACKED AT LOWER AFT CORNER. REMOVED INNER DOUBLER AND CRACKED INNER DOUBLER IAW ERA 516334-14. DAMAGE CONTAINED QC1974. REPAIRS DONE IAW ERA 516334-14, REV O.

Part: SKIN — CRACKED (VERTICAL STAB) · airframe 43,044 hrs · 22,334 cycles

VERTICAL STABILIZER, LT SIDE AT RAM AIR INLET ACCESS PANEL LOWER AFT CORNER SKIN CRACKED. REMOVED CRACKED SKIN ERA 516334-4. DAMAGE CONTAINED. REPAIRS COMPLETED IAW ERA 516334-14, REV O.

Part: SKIN — CRACKED (VERTICAL STAB) · airframe 43,044 hrs · 22,334 cycles

REMOVED SECTION OF DORSAL ATTACHMENT SKATE ANGLE LT, BS 1494 FOR ACCESS TO DORSAL SKIN CRACK. REMOVED SECTION OF ANGLE FOR ACCESS. ACCOMPLISHED ERA 516367-14 REV O, SECTION I. REQUIRED INSPECTION COMPLETED QC1984.

Part: SCOOP — CRACKED (RAM AIR) · airframe 43,044 hrs · 22,334 cycles

DURING SPECIAL VISIT, ATTEMPTS TO WELD CRACKS IN RAM AIR SCOOP WERE UNSUCCESSFUL, ERA 516402-14 ISSUED. ACCOMPLISHED SECTION I OF ERA 516402-14, REV O.

Part: SKATE ANGLE — DAMAGED (VERTICAL STAB) · airframe 43,044 hrs · 22,334 cycles

RIGHT INBD SKATE ANGLE WAS FOUND DAMAGED DURING DVI OF SURROUNDING STRUCTURE OF DORSAL FIN. REMOVED RIGHT INNER SKATE ANGLE. DRILLED NEW ANGLE. INSTALLED ANGLE IAW SRM 55-30-05, P27 AND DWG 5912188.

Part: SHEAR TIE — CRACKED (BS 1486) · airframe 43,019 hrs · 22,321 cycles

BS 1486, LONGERON 2R CRACKED SHEAR TIE. REMOVED AND INSTALLED SHEAR TIE IAW SRM 51-10.

Part: STRUCTURE — CRACKED (RAM AIR INLET) · airframe 43,044 hrs · 22,334 cycles

RAM AIR INLET UPPER AFT EDGE CRACKED. PERFORMED WELD REPAIR IAW SRM 55-30-05. FPI AND HFEC IAW PS 900-6-3, NR 2 AND 06-10-01.001, NO CRACKS.

Part: CABLE — LOOSE (ESCAPE SLIDE) · airframe 41,810 hrs · 21,634 cycles

DURING SERVICE CHECK, MX FOUND L1 DOOR SLIDE DEPLOY CABLE HANGING LOOSE. R & R SLIDE IAW AMDS CARD DECK 2500-4332. ACFT OK FOR SERVICE.

Part: LAMP — WEAK (EMERGENCY LIGHT) · airframe 40,933 hrs · 21,145 cycles

DURING SERVICE CHECK, MAINTENANCE FOUND AFT LEFT OVERWING EMERGENCY EXIT LIGHTED SIGN OVER DOOR VERY DIM. MAINTENANCE FOUND ONLY THREE BULBS WORKING. REPLACED LAMPS. OPS CHECKED GOOD.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 40,605 hrs · 20,959 cycles

DURING SERVICE CHECK, MAINTENANCE FOUND OVERWING EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED POWER PACK PER AMM OPERATION CHECKS GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 40,450 hrs · 20,868 cycles

DURING SERVICE CHECK, MAINTENANCE FOUND OVERWING EMERGENCY LIGHTS REMAIN ILLUMINATED WITH SWITCH TURNED OFF. REMOVED AND REPLACED OVERWING BATTERY PACK PER AMM. OPERATION CHECKS GOOD.

Part: FASTENER — UNKNOWN (ENGINE MOUNT) · airframe 39,396 hrs · 20,288 cycles

AS PER EA 02-476701-12AD ME0101 STEP 20 SDR REQUIRED. REPLACED UPPER ROW OF ENGINE AFT MOUNT SUPPORT FASTENERS (ROW A) INSPECTED ROW B, NO DEFECTS NOTICED.

Part: FASTENER — UNKNOWN (ENGINE MOUNT) · airframe 39,396 hrs · 20,288 cycles

AS PER EA 02-476701-12AD REV E ME0301 STEP 20 SDR REQUIRED. REPLACED UPPER ROW OF ENGINE AFT MOUNT SUPPORT FITTING FASTENERS (ROW A) INSPECTED ROW B, NO DEFECTS NOTED.

Part: FITTING — CORRODED (VERTICAL STAB) · airframe 27,098 hrs · 13,731 cycles

VERTICAL STABILIZER FITTING CORROSION REPAIR OD2006-SR-044 NRC B55-061119-344 BOEING APPROVAL 1-259780511-3.

Part: SKIN — DENTED (FUSELAGE) · airframe 38,795 hrs · 19,997 cycles

REPAIR OF DENT ON THE SKIN AT STA 273 OD2010-SR-008 NRC HRB20101206-01-01 BOEING APPROVAL SHY-SHY-10-0084-02B.

Part: STRUCTURE — DAMAGED (WING) · airframe 27,098 hrs · 13,731 cycles

REPAIR OF WING LEADING EDGE WORN DAMAGE OD2006-SR-042 NRC B55-061119-228 BOEING APPROVAL 1-255950271-5.

Part: ATTACH ANGLE — DAMAGED (VERTICAL STAB) · airframe 27,098 hrs · 13,731 cycles

FUSELAGE TO VERTICAL STABILIZER ATTACH ANGLE REPAIR OD2006- SR-043 NRC B55-061119-328 BOEING APPROVAL 1-257893345-5.

Part: SKIN PANEL — CRACKED (LE SLAT) · airframe 27,098 hrs · 13,731 cycles

SLAT SKIN PANEL CRACK REPAIR IAW OD2006-SR-041 NRC B55-061119-230 BAC APPROVAL 1-257893301-2.

Part: PAN — CORRODED (CARGO BAY) · airframe 27,098 hrs · 13,731 cycles

FWD CARGO DOOR JAMB PAN CORROSION REPAIR IAW SRM 53-05 NRC B55-061119-047 AND BAC APPROVAL 1-253499901-2

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 27,098 hrs · 13,731 cycles

MID CARGO DOOR JAMB CORROSION REPAIR NRC 48 SRM 53-05.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 27,098 hrs · 13,731 cycles

MID CARGO DOOR JAMB CORROSION NRC 25.