N915DN

Part: WIRE — EXPOSED (COCKPIT LIGHT) · airframe 57,953 hrs · 32,106 cycles

CAPT'S LIGHT INOP. CANISTER PART OF LIGHT SHORTS OUT AND SPARKS WHEN IT TOUCHES BARE CONNECTOR. FOUND HEAT SHRINK ON CAPTAINS GRIMES LIGHT CONNECTOR CUT EXPOSING TERMINAL. REMOVED AND INSTALLED NEW HEAT SHRINK PER SWPM CHAPTER 20. CKS GOOD.

Part: ENGINE — FIRE (RIGHT) · airframe 57,327 hrs · 31,696 cycles

ATB, IFSD RIGHT ENGINE SURGE FOLLOWED BY FIRE INDICATION PASSING 14K. RAN QRH, DISCHARGED 2 FIRE BOTTLES INTO RT ENG. FIRE EXTINGUISHED AFTER 3 MINUTES. EGT REACHED 1100 EGT. ENGINE REPLACED.

Part: O-RING — LEAKING (WATER SEPARATOR) · airframe 57,109 hrs · 31,571 cycles

ATTENDANTS REPORTED A FUEL ODOR FROM ROW 27 AND BACK. INSPECTED EXTERNAL AREAS OF THE ACFT, APU FUEL SHROUD DRAIN AND APU INLET. NO EVIDENCE OF FUEL LEAKS. CHANGED COALESCER BAGS FOR BOTH SIDES. FOUND AN O-RING INSIDE THE WATER SEPARATOR. CLEANED INSIDE OF WATER SEPARATOR. COMPLETED A PACK BURNOUT IAW AMM 21-53.

Part: DOOR FRAME — CRACKED (NLG AREA) · airframe 56,742 hrs · 31,368 cycles

CRACKED LT NLG DOOR FRAME BS 49. REPAIRED IAW SRM 53-90-01, PAR 8, FIG 6, VOL I, SRM 51-30-05, VOL.II, AND SRM 51-30-02, VOL II.

Part: DOOR FRAME — CRACKED (RT MLG WW) · airframe 56,742 hrs · 31,368 cycles

CRACKED ON FWR DOOR JAMB (OUTBD END) AT RTMLG W/W. FWR DOOR JAMB (OUTBD END) AT RT MLG W/W WAS REPLACED PER SRM 51-30-02 VOL II, SRM 51-30-05 VOL II AND DWG 5930584.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 55,124 hrs · 30,385 cycles

LOWER EMERG EXIT SIGN NEXT TO AFT F/A JUMP SEAT HAS 2 BULBS OUT. RELAMPED, OPS GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 55,124 hrs · 30,385 cycles

EMERGENCY LIGHTS INOP. R&R BATTERY AT B5-237.

Part: OVEN — FAILED (GALLEY) · airframe 54,347 hrs · 29,948 cycles

WHEN GALLEY OVEN WAS TURNED ON, THE FAN WAS NOISY AND SMOKE WAS PRESENT. OVEN WAS TURNED OFF AND SMOKE CEASED. CIRCUIT BREAKER WAS PULLED AND COLLARED.

Part: UNKNOWN — ODOR (CABIN) · airframe 54,175 hrs · 29,860 cycles

DURING TAXI OUT, 2 FLIGHT ATTENDANTS NOTICED BURNING PLASTIC ODOR CONCENTRATED NEAR CEILING AIR VENT IN FORWARD GALLEY. MAINTENANCE TROUBLESHOT IAW FIM. NO FINDINGS. RAN ENGINES. NO FINDINGS. PERFORMED MINI-DUCT BURNOUT PER NO-GO ODI WC 4950-20001.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,386 hrs · 29,434 cycles

CRACK IN 48 SECTION RIGHT SIDE. REMOVED EXISTING INTERNAL DOUBLER ADJACENT TO DAMAGE PER ERA 55541-14.

Part: LONGERON — DAMAGED · airframe 52,032 hrs · 28,593 cycles

LONGERON 22L DAMAGED. COMPLIED WITH ERA 549519-14.

Part: FRAME — DAMAGED (BS 750) · airframe 52,032 hrs · 28,593 cycles

FRAME BS 750 DAMAGED, COMPLIED WITH ERA 549516-14.

Part: PAN — CORRODED (LAVATORY) · airframe 51,921 hrs · 28,540 cycles

BACK SIDE OF AFT LAVATORY PAN BETWEEN BS 1364 - 1379 IS CORRODED. REMOVED AND REPLACED DOUBLER IAW DWG 5965767.

Part: WEB — CRACKED (VERTICAL STAB) · airframe 51,921 hrs · 28,540 cycles

VERTICAL STABILIZER HAS A CRACK AT SUPPORT WEB FLANGE AT JACKSCREW GIMBAL NUT , LEFT ATTACH FITTING. COMPLIED WITH PRI/ERA 548544-14, REV O.

Part: WEB — CRACKED (VERTICAL STAB) · airframe 51,921 hrs · 28,540 cycles

VERTICAL STABILIZER HAS A CRACK AT SUPPORT WEB FLANGE AT JACKSCREW GIMBAL NUT, RIGHT ATTACH FITTING. COMPLIED WITH PRI 548544-14, REV 0, 1, 2 AND ERA 548544-14, REV O.

Part: ACTUATOR — LEAKING · airframe 51,921 hrs · 28,540 cycles

TAIL COMPARTMENT CATWALK ACTUATOR LEAKING. REMOVED AND REPLACED ACTUATOR IAW MM. OPERATION AND LEAK CHECK OKAY. (LP# 2574562)

Part: STRUCTURE — UNKNOWN (UNKNOWN) · airframe 51,917 hrs · 28,539 cycles

FOUND RAISED SHARP EDGES AT LOWER SECTION OF THE ACME SCREW. COMPLIED WITH PRI/ERA 54850-14AD.

Part: SKIN — CRACKED (BS 1475) · airframe 51,917 hrs · 28,539 cycles

TAIL COMPARTMENT, L2 CRACKED AT BS 1475. REPAIRED IAW PRI/ERA 548593-14.

Part: FRAME — CRACKED (BS 943) · airframe 51,917 hrs · 28,539 cycles

FOUND A CRACK IN THE OVERWING FRAME TAB , BS 943 RIGHT. REMOVED AND INSTALLED FRAME IAW AMDS 5310-01375-08RT.

Part: SLIDE — MALFUNCTIONED (R1 DOOR) · airframe 49,168 hrs · 26,941 cycles

R1 SERVICE DOOR SLIDE DID NOT DEPLOY EXCEPT BY MANUAL TAB ONLY. R & R SLIDE.

Part: GUIDE — WORN (TAILCONE) · airframe 47,747 hrs · 26,067 cycles

GUIDE ON TAILCONE WORN. R & R GUIDE IAW SRM.

Part: CABLE — WORN (JETTISON SYS) · airframe 47,747 hrs · 26,067 cycles

JETTISON BOTTLE CABLE WAS FOUND WORN. R & R TAILCONE JETTISON CABLE.

Part: BEAM — CORRODED (DOOR FRAME) · airframe 46,809 hrs · 25,429 cycles

MID CARGO BAY DOOR FRAME BEAM IS CORRODED AT LOWER TANG AND PREVIOUS BLEND OUT. REMOVED CORROSION. FABRICATED AND INSTALLED NEW MID CARGO DOOR FRAME BEAM IAW SRM 51-30-01, 51-10-05 AND DWG 5930481.

Part: BEAM — CORRODED (DOOR FRAME) · airframe 46,809 hrs · 25,429 cycles

AFT CARGO DOOR FRAME BEAM HAS CORROSION AT LOWER TANG AND FORWARD FACE BY PREVIOUS BLENDOUTS. REMOVED AND INSTALLED NEW DOOR FRAME BEAM IAW DWG 5930481.

Part: SKIN — DENTED (BS 295) · airframe 46,809 hrs · 25,429 cycles

DENT ON EXTERIOR FUSLEAGE SKIN, BS 295, BETWEEN L6 & 7L. FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED DOUBLER AND FILLER REPAIR IAW SRM 53-31-02.

Part: SKIN — CORRODED (BS 843-862) · airframe 46,809 hrs · 25,429 cycles

CORROSION FOUND UNDER RUB STRIP, BS 843-846, L28R AND BS 859-862. L29R. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED TRIPLER AND PERMANENT REPAIR IAW SRM 53-30-01.

Part: SKIN — DENTED (BS 297) · airframe 46,809 hrs · 25,429 cycles

DENT ON EXTERIOR FUSELAGE SKIN, BS 297, L21L. CUT OUT DAMAGE. FABRICATED AND INSTALLED FINGER DOUBLER AND FILLER REPAIR IAW SRM 53-31-02.

Part: SKIN — DENTED (BS 238) · airframe 46,809 hrs · 25,429 cycles

DENT ON EXTERIOR FUSELAGE SKIN, BS 238, L7L. FOUND OUT OF LIMITS. FABRICATED AND INSTALLED DOUBLER AND SKIN FILLER REPAIR IAW SRM 53-31-02.

Part: SKIN — DENTED (BS 351) · airframe 46,809 hrs · 25,429 cycles

DENT ON EXTERIOR FUSELAGE SKIN BS 351, BETWEEN L2 AND 3L. FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 53-30-02, FIG 2.

Part: ATTACH FITTING — CRACKED (VERTICAL STAB) · airframe 46,809 hrs · 25,429 cycles

AFT ACCESSORY, VERTICAL STABILIZER DORSAL FIN ATTACH FITTING, RT SIDE HAS CRACK INDICATION. R & R DAMAGED FITTING IAW ERA 526008-14, REV 1.

Part: SKIN — DENTED (BS 358) · airframe 46,809 hrs · 25,429 cycles

DENT ON EXTERIOR FUSELAGE SKIN BS 358, L6L. FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 53-31-02.

Part: SKIN — DENTED (BS 535) · airframe 46,809 hrs · 25,429 cycles

DENT ON EXTERIOR FUSELAGE SKIN BS 535, L5L. CUTOUT DAMAGED AREA. FABRICATED AND INSTALLED NEW INTERNAL DOUBLER IAW SRM 53-31-02.

Part: SKIN — DENTED (BS 712) · airframe 46,809 hrs · 25,429 cycles

DENT ON EXTERIOR FUSELAGE SKIN BS 712, LONGERON 4 L. FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED FINGER DOUBLER REPAIR IAW SRM 53-31-02.

Part: DOOR FRAME — CORRODED (CARGO DOORWAY) · airframe 46,809 hrs · 25,429 cycles

FORWARD CARGO, LOWER DOOR FRAME CORRODED ON LOWER BEAM. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED NEW ANGLE IAW SRM 53-60-02.

Part: FRAME — CORRODED (BS 1395 BULKHEAD) · airframe 46,809 hrs · 25,429 cycles

AFT CARGO BAY BS 1395, AFT PRESSURE BULKEHAD FRAME DOUBLER IS CORRODED. R & R FRAME BETWEEN L28L - 28R IAW SRM 51-30-02 AND 51-30-05.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 46,809 hrs · 25,429 cycles

CORROSION FOUND ON FLOOR SUPPORT ANGLES INBOARD OF R1 SERVICE DOOR. CUT OUT DAMAGE. FABRICATED AND INSTALLED DOUBLER AND FILLER IAW SRM 51-30-05 AND ERA 526000-14, REV O.

Part: SEAT TRACK — CHAFED (BS 845-1079) · airframe 46,809 hrs · 25,429 cycles

LEFT CABIN SEAT TRACK, BS 845-1079, LBL 54 HAS DEEP CHAFE AREAS. FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED NEW SEAT TRACK IAW SRM 53-40-01, FIG 4 AND 6.

Part: BULKHEAD — CORRODED (BS 1395) · airframe 46,809 hrs · 25,429 cycles

AFT CARGO BAY BS 1395, FORWARD BULKHEAD WEB CORRODED BETWEEN LONGERONS 29 AND 30R. REMOVED CORROSION. COMPLIED WITH ERA 526006-14, REV O.

Part: FLOOR SUPPORT — CORRODED (BS 160-202) · airframe 46,809 hrs · 25,429 cycles

BS 160-202, RBL 52 FLOOR SUPPORT IS CORRODED. FABRICATED NEW FLOOR SPPORT IAW DWG 9936534 AND SRM 51-30-02.

Part: CUSP WEB — CRACKED (BS 943) · airframe 46,809 hrs · 25,429 cycles

CRACKED CUSP WEB AT BS 943 IN RADIUS OF CUT OUT AFT SIDE OF FRAME. CUT OUT DAMAGE. FABRICATED AND INSTALLED NEW CUSP WEB SECTION AND SPLICE IAW SRM 53-40-02, FIG 26 AND FIG 29.

Part: CUSP WEB — CORRODED (BS 984-1003) · airframe 46,809 hrs · 25,429 cycles

CABIN LEFT CUSP WEB SHOWS SIGNS OF CORROSION, BS 984-1003. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED NEW CUSP WEB SECTION IAW DWG 9910151.

Part: LONGERON — CORRODED (BS 814) · airframe 46,809 hrs · 25,429 cycles

AFT CARGO BAY BS 814, LONGERON 23L CORROSDED. REMOVED, FABRICATED AND INSTALLED STRAP IAW SRM 51-10-03 AND DWG 5911423, REV CD.

Part: SEAT TRACK — CORRODED (BS 788-1270) · airframe 46,809 hrs · 25,429 cycles

CABIN SEAT TRACK AT RBL 22, HAS MULTIPLE SPOTS OF CORROSION, BS 788-826 AND BS 1250-1270. REMOVED CORROSION. FOUND OUT OF LIMITS. FABRICATED AND INSTALLED NEW SEAT TRACK IAW SRM 53-40-01.

Part: STRUCTURE — CORRODED (BS 1003) · airframe 46,809 hrs · 25,429 cycles

CORROSION ON TOP OF CENTER WING BOX UPPER SKIN, LBL 50-54, FS 1003. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. WORKED AREA PER SRM 51-10-03 AND ERA 526001-14, REV I.

Part: SEAT TRACK — CORRODED (BS 1140-1328) · airframe 46,809 hrs · 25,429 cycles

SEAT TRACK, RBL 56 CORRODED BS 1140-1328. REMOVED AND INSTALLED NEW SEAT TRACK IAW SRM 51-10-03 AND 53-40-01, FIG 6.

Part: CUSP WEB — CORRODED (BS 1212-1231) · airframe 46,809 hrs · 25,429 cycles

RIGHT SIDE OF CUSP WEB SHOWS SIGNS OF CORROSION AT BS 1212-1231. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED DOUBLER AND FILLER IAW SRM 53-20-01.

Part: SEAT TRACK — CORRODED (BS 200-220) · airframe 46,809 hrs · 25,429 cycles

RBL 48, BS 200-220 SEVERAL SPOTS OF CORROSION ON SEAT TRACK. CUT OUT DAMAGED AREA. FABRICATED AND INSTALLED NEW SEAT TRACK IAW SRM 53-40-01.

Part: SEAT TRACK — CORRODED (BS 200-234) · airframe 46,809 hrs · 25,429 cycles

LBL 22, BS 200-234 HAS SEVERAL SPORT OF CORROSION ON SEAT TRACK. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED NEW SEAT TRACK IAW SRM 53-40-01, FIG 6.

Part: SEAT TRACK — CORRODED (BS 598-846) · airframe 46,809 hrs · 25,429 cycles

RBL 56 SEAT TRACK HAS MULTIPLE CORROSIONS BETWEEN BS 598-846. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED NEW SECTION IAW 53-40-01, FIG 4 AND 51-10-05.

Part: CUSP WEB — CORRODED (BS 560-579) · airframe 46,809 hrs · 25,429 cycles

CABIN LT CUSP WEB SHOWS SIGNS OF CORROSION AT BS 560-579. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED FILLER AND DOUBLERS IAW SRM 53-20-02.

Part: CUSP WEB — CORRODED (BS 541-560) · airframe 46,809 hrs · 25,429 cycles

LEFT CUSP WEB SHOWS SIGNS OF CORROSION AT BS 541-560. REMOVED DAMAGE AND FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED FILLER AND DOUBLER IAW SRM 53-20-02, FIG 12.

Part: CUSP WEB — CORRODED (BS 1175-1194) · airframe 46,809 hrs · 25,429 cycles

CABIN RT CUSP WEB SHOWS SIGNS OF CORROSION AT BS 1175-1194. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED REPAIR IAW SRM 53-20-02.

Part: SEAT TRACK — CORRODED (BS 200-265) · airframe 46,809 hrs · 25,429 cycles

CABIN SEAT TRACK AT RBL 22, BS 200-265 HAS EXCESSIVE CORROSION. R & R SECTION OF SEAT TRACK IAW SRM 53-40-01, FIG 6.

Part: FRAME — CRACKED (BS 943) · airframe 46,536 hrs · 25,233 cycles

FOUND FRAME AT BS 943, LT CRACKED ON UPPER RADIUS. R & R CRACK FRAME IAW SR 90530027.

Part: PIN — DISENGAGED (DOOR SLIDE) · airframe 45,625 hrs · 24,676 cycles

WHILE PERFORMING SLIDE PIN ENGAGEMENT, FOUND PARACHUTE ENGAGEMENT PIN ON FORWARD ENTRY DOOR NOT ENGAGED. R & R FORWARD ENTRY DOOR SLIDE IAW AMDS WC 2500-4332.

Part: ATTACH ANGLE — CRACKED (VERTICAL STAB) · airframe 45,399 hrs · 24,528 cycles

DURING VERTICAL STABILIZER INSPECTION, FOUND RIGHT INTERNAL ATTACH ANGLE CRACKED. REMOVED AND REPLACED ANGLE AND FASTENERS IAW DWG 5912188 AND SRM 51-30.

Part: CONTROLLER — FAILED (CABIN TEMP) · airframe 45,156 hrs · 24,372 cycles

FLIGHT CREW REPORTED SLIGHT HAZE AND WARM AIR COMING FROM REAR OF ACFT. R & R LEFT TEMPERATURE CONTROL IAW AMM. OPS CHECKED GOOD. MCO/PLAC REMOVED.

Part: CABLE — FRAYED (TAILCONE JETTISO) · airframe 44,891 hrs · 24,211 cycles

DURING SERVICE CHECK, TAILCONE JETTISON RELEASE CABLE FOUND FRAYED. R & R TAILCONE JETTISON RELEASE CABLE IAW IPC AND JIC.

Part: SOCKET — INOPERATIVE (EMERGENCY LIGHT) · airframe 44,861 hrs · 24,190 cycles

OVERHEAD EMERGENCY LIGHTS INOPERATIVE AT SEAT 15C AND 31B. TROUBLESHOT. R & R LIST SOCKET ASSY.

Part: UNKNOWN — ODOR (CABIN) · airframe 44,580 hrs · 24,040 cycles

ELECTRICAL ODOR DETECTED BY PASSENGERS AND CREW FROM OVERHEAD AT ROWS 4C/D AN D10 C/D/E IMMEDIATELY AFTER LANDING. MX TROUBLESHOT. REMOVED PSU PANELS, CEILING PANELS, INSPECTED WIRING. NO ODOR OR DEFECT. PERFORMED DUCT BURNOUT. R & R COALESCER BAGS. NO SOURCE IDENTIFIED.

Part: SKIN — DAMAGED (LT WING) · airframe 44,114 hrs · 23,727 cycles

LT WING L/E HAS SMALL HOLE WORN THROUGH SKIN APPROX 2" OTBD OF SLAT ANTI-ICE DUCT. REMOVED DAMAGE, FABRICATED AND INSTALLED PERMANENT REPAIR IAW SRM 57-20-01, FIG 11.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 43,625 hrs · 23,406 cycles

DURING SERVICE CHECK, EMERGENCY LIGHTS IN AFT CABIN INOPERATIVE. R & R BATTERY PACK IAW AMM. OPERATION CHECKS GOOD.

Part: CONNECTOR — BROKEN (EMERGENCY LIGHT) · airframe 43,625 hrs · 23,406 cycles

DURING SERVICE CHECK, TAIL COMPARTMENT EMERGENCY LIGHT INOPERATIVE. R & R 2 BROKEN CONNECTORS AT LIGHT. OPERATION CHECKS OK.

Part: CABLE — OUT OF RIG (TAIL) · airframe 42,837 hrs · 22,939 cycles

DURING INSPECTION AND RIG CHECK OF THE VENTRAL STAIRWAY MOVEABLE CEILING, MX FOUND CABLE TENSION IN LOWER LIMIT AND LATCH PLUNGER HOUSING HITTING STEP. ADJUSTED IAW AMM. OPS CHECKED GOOD.

Part: SKATE ANGLE — CRACKED (VERTICAL) · airframe 42,576 hrs · 22,748 cycles

LEFT SKATE ANGLE CRACKED, INBD FASTENER ROW 15 INCHES FROM AFT END. REPAIRED PER ERA 506579-14 REV ORIG.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 42,576 hrs · 22,748 cycles

LT HORIZONTAL STAB UPPER AFT SKIN CRACKED. LOCATED IN AREA OF INSPECTION PER OPN 5950 SCAN NR 2 REF FIG 3-3 AND 3-5. REPAIRED PER ERA 506496-14AD REV ORIGINAL.

Part: FRAME — CRACKED (BS 1522 L8-9R) · airframe 42,576 hrs · 22,748 cycles

DAMAGED FRAME BS 1520 AFT SIDE BETWEEN L8 AND L9R. REPAIRED PER ERA NR 506524-14 REV "O".

Part: SKIN — BENT (FUSELAGE) · airframe 41,742 hrs · 22,298 cycles

AFT B/B DOOR OPENING AFT EDGE SEAL STRIKER CRACKED AND FUSELAGE SKIN BENT. C/W REPAIR PER ERA 502475-14 REV O.

Part: GIRT BAR — BROKEN (L1 DOOR) · airframe 41,668 hrs · 22,255 cycles

FLIGHT CREW REPORTED L1 DOOR GIRT BAR FITTING, BROKEN. MAINTENANCE REMOVED L1 DOOR SLIDE COVER AND SLIDE AND INSTALLED SLIDE AND SERVICEABLE SLIDE COVER PER JIC OPN 7008. AIRCRAFT OKAY FOR SERVICE.

Part: WIRE — DISCONNECTED (CABIN) · airframe 39,239 hrs · 21,017 cycles

DURING LINE CHECK MAINTENANCE FOUND EMERGENCY PATH LIGHTS AT ROW 14, 17, 21, 25, 32, 36, 39 LEFT INOPERATIVE. MAINTENANCE FOUND WIRE L827BX18 DISCONNECTED AT J2-165. WIRE WAS RECONNECTED AND OPERATION OF LIGHTS NOW CHECKS OK.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 39,209 hrs · 21,002 cycles

RT HORIZONTAL UPPER AFT SKIN CRACKED AT INBD CORNER REF OPERATION 5951 AND N/R196 ERA492608-14.

Part: GENERATOR — LEAKING (RIGHT) · airframe 35,443 hrs · 19,164 cycles

BOTH ENG GENERATORS FAILED IN FLIGHT. INSPECTED RT GEN FOUND LEAKING 514447206. REMOVED REPLACED RT ENG GENERATOR IAW AMM. INSPECTED LT GEN FOUND LEAKING 574447206. REMOVED & REPLACED LT ENGINE GENERATOR IAW AMM.

Part: VALVE — MALFUNCTIONED (NLG STRUT) · airframe 35,346 hrs · 19,104 cycles

ON TAKEOFF NOSEGEAR DID NOT RETRACT. GREEN LIGHT WENT OUT AND RED LIGHT REMAINED ON. FOLLOWED QRH ,GEAR EXTENDED WITH NORMAL DOWN AND LOCKED INDICATIONS. FOUND NOSE LANDING GEAR STRUT DEFLATED AT GATE NO EVIDENCE OF STRUT FLUID LEAKAGE REMOVED AND REPLACED STRUT AIR CHARGING VALVE AND SERVICED NOSE LANDING GEAR STRUT IAW AMM TASK 32-20-01-619-801 JACKED NOSE GEAR STRUT ASSY IAW AMM PERFORMED EXTENSION/RETRACTION OF NOSE GEAR ASSY IAW AMM EXSTENSION/RETRACTION CHECK GOOD. ACFT OK FOR SERVICE.

Part: SLIDE — MALFUNCTIONED (TAILCONE) · airframe 32,509 hrs · 17,435 cycles

INADVERTANT DEPLOYMENT OF TAIL CONE FROM EXTERNAL HANDLE, SLIDE DID NOT DEPLOY. RE-INSTALLED TAIL CONE PER AMM. TAIL CONE DISPLACEMENT SYS NITROGEN CYLINDER ALSO SERVICED PER AMM. COMPLIED WITH RII REQUIREMENT FOR TAIL CONE INSTALLATION/SAFETY/SECURITY AND ADJUSTMENT OF TAIL CONE RELEASE SYSTEM PER AMM.

Part: SKIN — CORRODED (FS 795-885) · airframe 32,336 hrs · 17,319 cycles

DURING CURRENT HMV, DAMAGE (CORROSION) WAS FOUND ON FUSELAGE SKIN AT WING TO BODY FAIRING. REPAIR WAS ACCOMPLISHED PER SRM 53-04 FIGURE 53. MANUFACTURER APPROVED USE OF SUBJECT SRM ON 9215 PROVIDED THERE WERE NO DEVIATIONS. ADDRESSED ON ERA 470199-14.

Part: FITTING — CORRODED (BS 1395) · airframe 32,336 hrs · 17,319 cycles

FOUND FITTING CORRODED. REPLACED FITTING REF SRM`S 51-30-02, 51-30-05, 53-10-01, & 53-10-02D.

Part: ANGLE — CORRODED (BS 1250-1265) · airframe 32,336 hrs · 17,319 cycles

FOUND CORROSION FROM STA 1250 TO 1265. REPLACED ANGLE PER SRM 51-30-03 AND 51-30-05.

Part: FITTING — CORRODED (BS 1261276 L29) · airframe 32,336 hrs · 17,319 cycles

FOUND CLIP CORRODED. REPLACED CLIP.

Part: SKIN — CORRODED (BS 795-885) · airframe 32,336 hrs · 17,319 cycles

CORROSION ON FUSELAGE SKIN STA 795-885 AT ATTACH POINTS FOR LOWER WING TO BODY FAIRING. REPAIRED DAMAGED SKIN IAW SRM 53-04 FIG 53.

Part: SEAT TRACK — GOUGED (BS 1269 LBL 54) · airframe 32,336 hrs · 17,319 cycles

FOUND SEAT TRACK GOUGED, REPAIRED.

Part: INTERCOSTAL — CORRODED (BS 1328-1344 L30) · airframe 32,336 hrs · 17,319 cycles

FOUND INTERCOSTAL EXFOLIATED, REPLACED.

Part: SUPPORT — CORRODED (STA 160-200) · airframe 32,336 hrs · 17,319 cycles

FOUND SUPPORT CORRODED. REPLACED SUPPORT.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 32,336 hrs · 17,319 cycles

FOUND SUPPORT CORRODED. REPLACED SUPPORT.

Part: CUSP WEB — PUNCTURED (FS 360 LBL 54) · airframe 32,336 hrs · 17,319 cycles

CABIN CUSP WEB PUNCTURED ON I/B SIDE OF SEAT TRACK AT FS 360 CBL 54/CUT OUT DAMAGED AREA AND INSTALLED REPAIR DOUBLER IAW SRM 51-11-01 VOL 1.

Part: PROXIMITY SENSOR — MALFUNCTIONED (RT MLG W/W) · airframe 32,073 hrs · 17,180 cycles

AFTER T/O RAISED GEAR HANDLE AND RT GEAR UNSAFE LIGHT STAYED ILLUMINATED. REPLACED RT MAIN UP LATCH PROX SENSOR D1-25. PERFORMED GEAR SWING 3 TO 4 TIMES. ALL INDICATIONS CHECKED NORMAL. PROX SENSOR ALWAYS SHOWED FAR WITH ORIGINAL AND NEW PSEU.

Part: SENSOR — OUT OF LIMITS (LT MLG) · airframe 30,722 hrs · 16,437 cycles

UNSAFE LEFT MAIN GEAR INDICATION. INSPECTED LT GEAR AREA FOR DAMAGE, CKS GOOD. FOUND LT GEAR DOWN AND LOCKED PROXIMITY SENSOR ON OUTER RANGE LIMIT. ADJUSTED PER MM 32-61-02-420-802-CK'D PSEU NOW SHOWS NEAR AND INDICATION IS NORMAL, PSEU SHOWS NO ADDITIONAL FAULTS. SENSOR SHOWS PASS AND CLOSE.

Part: FIRE LOOP — MALFUNCTIONED (LEFT) · airframe 28,480 hrs · 15,181 cycles

LEFT ENGINE FIRE DETECT FAULT ILLUMIINATED ON OAP. REPLACED LT ENG DET. PERFORMED HIGH VOLTAGE MEG OHM CHECK ON ALL LT ENG A LOOP WIRES NO FAULTS FOUND FROM CONDUCTOR TO GROUND. REPLACED FAN FIRE DET LOOP A D1-910. REPLACED LOOP D1-911D1-912D1-914D1-915 NEEDS CHECKOUT 889313 LT ENG A A B FIRE SYS TEST NORMAL AND ENG RUN CKS NORMAL.

Part: LINE — LEAKING (RT GENERATOR) · airframe 28,000 hrs · 14,915 cycles

RIGHT ELECTRICAL SYSTEM FAIL WITH RIGHT GEN OIL PRESSURE MESSAGE ON OAP. FIVE MINUTES LATER RIGHT GEN FAIL. ON ARRIVAL LAS, FOUND NO OIL IN GENERATOR. FOUND OIL OUT LINE LEAKING. REPLACED LINE AND GENERATOR. SERVICED WITH OIL. OPS CHKS GOOD PER AMM. OIL LINE P/N 242210081.

Part: LENS — MISSING (EMERGENCY LIGHTS) · airframe 26,441 hrs · 13,993 cycles

EMERGENCY LIGHT LENS MISSING AT FIRST CLASS COACH DIVIDER. INSTALLED LENS, LIGHT OPS CHECKS OK.

Part: ENGINE — MALFUNCTIONED (NR 1) · airframe 26,417 hrs · 13,977 cycles

LEFT ENGINE BEGAN TO SHUDDER FOLLOWED BY A COMPRESSOR STALL AND PARAMETER ROLLBACK AND EGT INCREASE. C/W BORESCOPE INSPECTION OF THE HPC AS PER AMM. FOUND NUMBER STAGES DAMAGED AND OUT OF LIMITS. REPLACED ENGINE PER TRANS 2T102.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHT) · airframe 22,361 hrs · 11,808 cycles

FIRST CLASS FLOOR TRACK EMERGENCY LIGHTS INOP. REPLACED BATTERY PACK AND BATTERY CHARGER FOR FIRST CLASS FLOOR TRACK EMERGENCY LIGHTS. REPAIRED SHORTED WIRE IN FLOOR TRACK, ALL EMERGENCY LIGHTS OPN NORMAL.

Part: CIRCUIT BREAKER — TRIPPED (HYD SYSTEM) · airframe 21,510 hrs · 11,406 cycles

RIGHT HYD SYSTEM FAILURE. DECLARED EMERGENCY LANDING, NO HYD. FOUND RIGHT INSTR TRANSFER C/B POPPED. RESET L9 C/B, ALL INDICATIONS. OPERATED PUMPS SYSTEM, CHECKS OK. NO LEAKS FOUND.

Part: TRANSMITTER — MALFUNCTIONED (ELEVATOR) · airframe 21,182 hrs · 11,264 cycles

PYLON FLAP FAULT AND ELEVATOR SPLIT MESSAGE CAME ON AT FL310. REMOVED AND REPLACED RT AND LT ELEVATOR POSITION SENSORS PER M/M. ADJUSTED BOTH PER M/M. BOTH LEFT AND RIGHT TRANSMITTERS WITHIN M/M LIMITS. PYLON FLAP TEST CHECK GOOD.

Part: HINGE — BROKEN (LT WING SPOILER) · airframe 20,938 hrs · 11,151 cycles

FOUND WHILE WORKING MCO FOR SPOILER DEPLOY MSG. FOUND LEFT INBOARD FLT SPOILER I/B HINGE BROKEN. CAUSED DAMAGE TO THE POSITION SENSOR AND PUNCTURED HOLE INTO O/B FORE FLAP. REPLACING NEXT HIGHER ASSY THE SPOILER AND THE LEFT O/B FORE FLAP.

Part: BATTERY — DISCHARGED (CABIN) · airframe 20,382 hrs · 10,874 cycles

FWD SECTION OF FLOOR TRACK EMERGENCY LIGHTS INOP. REPLACED BATTERY PACK, NOW OPS NORMAL.

Part: RELAY — FAILED (APU) · airframe 18,631 hrs · 9,944 cycles

CREW REPORTS THAT AFTER BLOCK IN THE RAMP REPORTED HEAVY SMOKE/ELECTRIC ODOR EMINATING FROM THE APU. REPLACED STARTER AND START RELAY FOR SLOW SPOOL.

Part: BEARING — CRACKED (HORIZONTAL STAB) · airframe 17,658 hrs · 9,472 cycles

HORIZONTAL STAB PIVOT BEARINGS CRACKED. FOUND DURING HORIZONTAL STAB PIVOT BEARING FREE PLAY. REPLACED.

Part: SKIN — CRACKED (EMPENNAGE) · airframe 17,629 hrs · 9,458 cycles

DURING HMV-1, FOUND RAM AIR INLET CRACKED INLET ASSY WAS TOO EXTENSIVE. THEREFORE, A WELD REPAIR WAS DONE. REPAIRED PER ERA 378736+14

Part: RESERVOIR — LEAKING (NR 1 ENGINE) · airframe 11,995 hrs · 6,490 cycles

IN CLIMB LT HYD PRESS LOW MESSAGE ON OAP. PRESSURE EVENTUALLY DROPPED TO 0 PSI. RAN HYD PRESSURE LOW CHECKLIST AND LT HYD FAILURE CHECKLIST. INDICATIONS STABILIZED AT 0 PSI AND 27QTS. FOUND LEFT HYD RESERVOIR FAILED CAUSING AIR IN LEFT SYS AND NR 1 ENG DRIVEN PUMP FAILURE. EVIDENCE OF BURNT HYDRAULIC FLUID AND TAR BUILD UP AT EDP AND EDP HYD LINES. REPLACED LEFT PTU, THE LEFT HYDRAULIC RESERVOIR, AND LEFT EDP. ALSO, FLUSHED LINES PER MM AND REPLACED ALL FOUR HYD FILTERS ON LEFT SIDE.

Part: TIRE — FAILED (MLG) · airframe 11,882 hrs · 6,430 cycles

LEFT OUTBOARD MAIN TIRE BLEW ON LANDING. VSI ESTIMATED AT 100 FPM, RAN ANTISKID AND ABS RTS TESTS, ALL OK. REPLACED NR 1 & 2 TIRES AND BRAKES.

Part: TUBE — CRACKED (NR 2 ENGINE)

LOST OIL QTY DURING T/O ROLL AT ABOUT 90 KTS. FIRST INDICATION ON OAP, LOOKED DOWN AND SAW OIL PRESSURE AT 75-80 PSI. PRESSURE STARTED COMING BACK UP THEN QTY DROPPED TO 0. FOUND OIL LINE TO SCAVENGE DIFFERENTIAL PRESSURE SWITCH LEAKING. REPLACED OIL LINE, LEAK CHECKS OK.

Part: SLIDE — DEPLOYED (GALLEY DOOR)

R1 DOOR SLIDE ACCIDENTLY DROPPED OUT OF DOOR CRADLE AND DEPLOYED. REPLACED DOOR SLIDE PER M/M.

Part: SENSOR — MALFUNCTIONED (RT ELEVATOR)

AT 31,000 FT GOT PYLON FLAP MESSAGE FOLLOWED BY ELEVATOR SPLIT MESSAGE THEN PYLON FLAP MESSAGE WENT OUT. AIRCRAFT RETURNED TO DFW. REPLACED ACU AND RT ELEV POS SENSOR .

Part: BEARING — LOOSE (MLG WHEEL)

ON DEPARTURE PUSHBACK, GROUND CREW HEARD LOUD NOISE FROM THE RIGHT MAIN GEAR. FOUND NR 4 MAIN WHEEL INNER BEARING RACE LOOSE IN WHEEL CASTING. REPLACED WHEEL ASSY.

Part: SKIN — LIGHTNING STRIKE (BS 812/793/775)

LIGHTNING STRIKE DAMAGE WAS FOUND ON THE WINDOW BELT SKIN PANEL SURROUNDING WINDOWS 29, 30 AND 31. THE DAMAGE WAS BLENDED OUT. THE DAMAGE AT WINDOW 30 WAS FOUND TO BE ACCEPTABLE AND THE DAMAGE AT WINDOW 29 AND 31 WAS REPAIRED PER DAC REWORK DWG SRO9530053. THE REPAIR WAS DOCUMENTED PER ER/A 364363-14 AND APPROVED PER FAA 8110-3.