N914DN

Part: UNKNOWN — ODOR (CABIN) · airframe 59,092 hrs · 32,433 cycles

TURNING PACKS ON BRINGS ABOUT AROMA OF HOT PLASTIC, FUMES ONLY, NO SMOKE. PREFORMED FULL DUCT BURNOUT COULD NOT FIND CAUSE OF PLASTIC SMELL. (LP# 5216874)

Part: DEFLECTOR — MISSING (NLG) · airframe 58,980 hrs · 32,356 cycles

RIGHT NOSE LANDING GEAR DEBRIS DEFLECTOR MISSING. REPLACED LEFT AND RIGHT DEFLECTORS. (LP# 0829043)

Part: SPAR — CRACKED (VERTICAL STAB) · airframe 58,355 hrs · 31,935 cycles

RIGHT VERTICAL STAB WAS CRACKED, INDICATION WAS AT THE 9TH HOLE DOWN FROM ZFS 52.267 (M). REPAIRED THE SPAR IAW PRI 570807-14AD, REV 0 & 1, AND ER/A 570807-14AD, REV ORIGINAL.

Part: SKATE ANGLE — CRACKED (TAIL) · airframe 58,355 hrs · 31,935 cycles

TAIL EXTERIOR RT SKATE ANGLE WAS CRACKED, EMANATING FROM THE REAR SPAR ATTACH FASTENER. REPAIRED THE SKATE ANGLE IAW PRI 570843-14, REV 0, AND ERA 570843-14 REV ORIGINAL.

Part: DOOR FRAME — CRACKED (NLG) · airframe 58,004 hrs · 31,726 cycles

DURING A WALK AROUND, FOUND THE FWD RT MAIN GEAR DOOR FRAME CHANNEL CRACKED AT SEVERAL PLACES. REMOVED AND REPLACED THE DOOR FRAME CHANNEL IAW DWG 5930584. OPS CHECKED RT MLG DOOR.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 57,565 hrs · 31,474 cycles

AFT BULKHEAD EMERGENCY EXIT SIGN DOES NOT ILLUMINATE. R & R THE BATTERY PACK. OPS TESTED NORMAL.

Part: SLIDE — BROKEN (L1 DOOR) · airframe 57,211 hrs · 31,268 cycles

AT THE GATE, FA NOTICED THE L1 DOOR SLIDE PACK BROKEN. R & R THE L1 DOOR SLIDE IAW AMDS 2561-4641.

Part: SWITCH — DEFECTIVE (AC BAY) · airframe 57,022 hrs · 31,155 cycles

PERFORMED AN AIR TURN BACK TO MSP. ON TAKE-OFF THROUGH 4000FT FROM MSP OBSERVED FLOW LIGHT ON PRESS PANEL. NO FLOW INDICATION ON BOTH PACKS. OPERATION OF BOTH PACKS WITH NORMAL FLOW. PERFORMED BOTH SINGLE PACK CONFIDENCE CHECKS. OPERATIONS NORMAL. REPLACED SECOND SEGMENT CLIMB SWITCHES S1 -296 / S1-297 AND S1-486. PRESSURIZED A/C TO 7PSI WITH LT PACK AND RT PACK.

Part: CABIN PRESSURE — MALFUNCTIONED · airframe 56,854 hrs · 31,037 cycles

CABIN FAILED TO PRESSURIZE ON DEPARTURE. QRH COMPLIED WITH. LOUD HISSING NOISE REPORTED FROM L2 DOOR 20 MINUTES INTO FLIGHT. PACKS RETURNED TO NORMAL OPERATION. MAINTENANCE PRESSURIZED AIRCRAFT TO 5 PSI AND CHECKED L2 DOOR. SLIGHT NOISE. NO DEBRIS AND LUBRICATED SEAL. PERFORMED PACK ODI PREVENTION ON BOTH PACKS. AIRCRAFT OKAY FOR SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 56,575 hrs · 30,872 cycles

CAT WALK EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED THE BATTERY PACK IAW MM. OPS CHECKED GOOD.

Part: UNKNOWN — ODOR (CABIN) · airframe 55,640 hrs · 30,299 cycles

GASOLINE ODOR IN AFT CABIN AT WAKE UP. TRANSFERRED FUEL FROM OUTER WINGS TO CENTER AND OUT TO WINGS. PULLED FLOORBOARDS ABOVE CENTER TANK. USED BORESCOPE AND FOUND NO LEAKS. USED SNIFFER IN AREA, NO READINGS. RAN PACKS FROM APU TO ENGINES. INSPECTED AIR, APU AND ENGINE INLETS. TOPPED OFF ALL TANKS AND RAN ENGINES AT TAKE-OFF POWER. NO FUEL ODORS NOTED AT THIS TIME.

Part: ACM — OVERSERVICED (NR 1) · airframe 55,640 hrs · 30,299 cycles

FLIGHT ATTENDANTS REPORTED STRONG ODOR OF GASOLINE IN VICINITY OF ROWS 30 AND 31 AT FL340. ODOR DISSIPATED ON GROUND. INSPECTED ENGINES, APU AND HYDRAULICS. NR 1 ACM IS OVERSERVICED. CORRLECTLY SERVICED THE ACM .REMOVED AND REPLACED COALESCER BAGS AND O-RINGS. COMPLIED WITH NO GO ODI PREVENTION TASK.

Part: FRAME — CRACKED (NLG WW) · airframe 55,389 hrs · 30,146 cycles

LEFT NOSE WHEEL WELL FRAME CRACKED FORWARD END. INSTALLED DOUBLER AND FILL IAW ERA 495600-14.

Part: FRAME — CRACKED (NLG WW) · airframe 55,411 hrs · 30,158 cycles

NOSE GEAR WHEEL WELL FRAME CRACKED FORWARD END. REPAIRED IAW ERA 558876-14.

Part: LENS — MISSING (CABIN) · airframe 54,600 hrs · 29,742 cycles

EMERGENCY EXIT OVERHEAD LIGHT LENS COVER MISSING. REMOVED AND REPLACED LIGHT ASSEMBLY PER MM. OPERATIONS CHECK OK.

Part: LENS — DAMAGED (CABIN) · airframe 54,029 hrs · 29,422 cycles

EMERGENCY EXIT COVER LENS DAMAGED. REPLACED.

Part: SUPPORT RIB — CRACKED (VERTICAL STAB) · airframe 53,332 hrs · 28,963 cycles

ISSUED ERA 549947-14 FOR FATIGUE CRACKS IN THE GIMBAL MOUNT SUPPORT RIB AT ZRS=134.062. REPAIRED IAW ER/A549947-14.

Part: ANGLE — CORRODED (SERVICE DOOR) · airframe 53,699 hrs · 29,210 cycles

CORROSION ON ANGLE, AFT SERVICE DOOR, LEFT LOWER CORNER OF DOOR. REPLACED STOP ANGLES PER DWG 9915565.

Part: FILLER — CORRODED (FLOOR SUPPORT) · airframe 53,332 hrs · 28,963 cycles

FORWARD ENTRY DOOR FLOOR SUPPORT IS CORRODED. REPLACED FILLER IAW DWG 9936534.

Part: SKIN — CRACKED (BS 1437) · airframe 53,332 hrs · 28,963 cycles

FUSELAGE SKIN CRACKED, BS 1437 ABOVE RIGHT PYLON. REPAIRED IAW PRI/ERA 549946-14.

Part: FRAME — CRACKED (BS 962) · airframe 53,332 hrs · 28,963 cycles

FOUND CRACK INDICATION ON UPPER RADIUS OF FRAME BS 962 OVERWING TAB. REPAIRED IAW SRM 53-00901.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 53,288 hrs · 28,935 cycles

AFT CABIN EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY PACK IN AFT RIGHT LAVATORY. OPERATION CHECKS GOOD.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 52,853 hrs · 28,712 cycles

RUDDER POWER PACK OTBD ATTACH POINT TO CANTED BULKHEAD SCREWS LOOSE AND SHEARED OFF, ANGLE CRACKED. REPLACED FRAME SECTION IAW DWG 9911875.

Part: SPAR — CRACKED (HORIZONAL STAB) · airframe 52,769 hrs · 28,668 cycles

CRACK ON AFT BARREL NUT HOLE, RT HORIZONTAL STABILIZER UPPER AFT SPAR CHORD, INBD BARREL NUT BORES. R & R IAW AMDS 5510-4001.

Part: FRAME — DAMAGED (BS 1567) · airframe 52,769 hrs · 28,668 cycles

TAIL CONE ATTACH BELT FRAME, BS 1567 RUDDER POWER PACK ATTACH POINT FRAME IS DAMAGED, RT SIDE. FABRICATED AND INSTALLED NEW FRAME IAW DWG 9911843.

Part: CABLE — BROKEN (R1 DOOR SLIDE) · airframe 52,473 hrs · 28,501 cycles

R1 DOOR SLIDE LANYARD HAS BROKEN CABLE. REPLACED LANYARD IAW WC 2561-4641.

Part: CONTROL VALVE — MALFUNCTIONED (RT A/C PACK) · airframe 51,752 hrs · 28,070 cycles

RT PACK WAS UNABLE TO HOLD PRESSURIZATION AT FL310. FLIGHT CREW DESCENDED TO FL270 AND WAS ABLE TO HOLD PRESSURIZATION. COMPLIED WITH QRH, NO HELP. MAINTENANCE FOUND RT PACK TEMPERATURE CONTROL VALVE BOOT OFF. SECURED BOOT. PERFORMED HEALTH CHECK. OPERATIONS GOOD.

Part: CLAMP — LOOSE (RT A/C PACK) · airframe 49,694 hrs · 26,814 cycles

FLOW LIGHT ILLUMINATED AT FL280 AND VERY LITTLE AIR FROM PACKS FOR COOLING. FOUND RT PACK WOULD NOT PRESSURIZE ACFT AND HAD WEAK FLOW. RT PACK DEFERRED TO MEL. LT PACK PRESSURIZED ACFT NORMALLY. ACFT HAD ADDITIONAL WRITE-UP ON 4/12. COULD NOT PRESSURIZE ACFT AFTER TAKEOFF DUE TO LOSS OF FLOW FROM LT AC PACK. THE RT AC PACK WAS ON MEL DEFERRAL AT THE TIME. THE CREW COULD NOT PRESSURIZE THE CABIN WITH NO FLOW SO MAINTAINED ACFT AT 10,000 FT. MAINTENANCE FOUND LT ACM COMPRESSOR DISCHARGE CLAMP LOOSE AND LEAKING AT HEAT EXCHANGER. MAINTENANCE ALSO FOUND THE LT TEMP CONTROL VALVE LEAKING AT LOOSE CLAMP ON THE SPIDER DUCT SIDE. RESECURED CLAMP AT THE ACM, AND REPOSITIONED DUCT AND SECURED CLAMP AT THE TEMP CONTROL VALVE. NO OTHER LEAKS FOUND ON THE LT SIDE. ON THE RT PACK, MAINTENANCE FOUND A MAIN SUPPLY DUCT MISSING A BOOT CLAMP AT THE P-DOME. MAINTENANCE INSTALLED THE BOOT CLAMP. MAINTENANCE PERFORMED AIR CONDITIONING HEALTH CHECKS ON BOTH AC SYSTEMS AND PRESSIRUIZED THE ACFT TO 7 PSID USING EACH PACK SYSTEM INDIVIDUALLY. THE ACFT WAS RETURNED TO SERVICE. LP 6571424.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 49,564 hrs · 26,727 cycles

BOTH FORWARD OVERWING EXIT SIGNS INOPERATIVE. TROUBLESHOT. FOUND BATTERY PACK READING LOW. R & R BATTERY PACK AND CHARGER ASSY IAW AMM. OPS CHECKS GOOD.

Part: COALESCER BAG — ODOR · airframe 49,209 hrs · 26,518 cycles

ON LANDING, F/A NOTICED YELLOW SWEET SMELLING SMOKE COMING FROM VENTS. MAINTENANCE RAN ENGINES AND REVERSER WITH NO FINDINGS. CHANGED COALESCER BAGS AND PERFORMED DUCT BURNOUT. OK FOR SERVICE.

Part: BULKHEAD — CORRODED (BS 1395) · airframe 48,156 hrs · 25,831 cycles

CORROSION ON BS 1395, BULKHEAD AT L25R. REPAIRED IAW ERA 527397-14.

Part: FRAME — CORRODED (BS 1344) · airframe 48,156 hrs · 25,831 cycles

AFT CARGO BAY, FRAME BS 1344, L26R-L28L CORRODED. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED NEW FRAME IAW SRM 53-10-02.

Part: LONGERON — CORRODED (BS 1344-1364) · airframe 48,156 hrs · 25,831 cycles

AFT CARGO LONGERON 30, BS 1344-1364 CORRODED. INSTALLED REPAIR IAW SRM 53-10-02.

Part: WEB — CORRODED (BS 1395) · airframe 48,156 hrs · 25,831 cycles

AFT CARGO HAS EXFOLIATED WEB, FORWARD OF P-DOME AT BS 1395, RT LOWER EDGE. 100 PERCENT MATERIAL LOSS. REMOVED, FABRICATED AND INSTALLED RT WEB IAW SRM 51-30-02, 51-30-05 AND DWG 9915561, REV CG.

Part: BULKHEAD — CORRODED (AFT) · airframe 48,156 hrs · 25,831 cycles

AFT CARGO LOWER FORWARD SIDE OF PRESSURE BULKHEAD DOME, CORRODED FROM STRINGERS 28L AND 26R. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED DOUBLER AND FILLER IAW SRM 51-10-03 AND 53-10-03.

Part: LONGERON — CORRODED (BS 1344-1364) · airframe 48,156 hrs · 25,831 cycles

AFT CARGO, BS 1344-1364, L30 HAS CORROSION. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. REPLACED LONGERON AND SPLICE IAW SRM 51-30-05 AND DWG 5936667, REV CD.

Part: LONGERON — CORRODED (BS 1395) · airframe 48,156 hrs · 25,831 cycles

AFT CARGO BS 1395, L28R, CORRODED. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS 100 PERCENT MATERIAL LOSS.

Part: STRUCTURE — CORRODED (CARGO DOORWAY) · airframe 48,156 hrs · 25,831 cycles

NUMEROUS AREAS OF SURFACE CORROSION ON CENTER CARGO DOOR CUT OUT, TASK 52-321-02. REMOVED REPAIR SPACER, FABRICATED AND INSTALLED IAW SRM 53-60-02 AND 51-30-05.

Part: SKIN — CORRODED (BS 1395) · airframe 48,156 hrs · 25,831 cycles

FUSELAGE INNER SKIN IN AFT CARGO IS CORRODED, BS 1395, INBD OF L28R. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED NEW DOUBLER AND FILLER IAW SRM 53-31-02.

Part: LONGERON — CORRODED (BS 1395) · airframe 48,156 hrs · 25,831 cycles

AFT CARGO, CORROSION ON LONGERON 29R END FITTING, BS 1395. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED FITTING IAW SRM 51-10-03.

Part: BEAM — CORRODED (DOOR FRAME) · airframe 48,156 hrs · 25,831 cycles

AFT CARGO DOOR FRAME BEAM HAS CORROSION ON EDGE BETWEEN LOWER FITTINGS. REMOVED, FABRICATED AND INSTALL REPAIR PARTS IAW 53-60-02 AND DWG 5930483, REV AK.

Part: SKIN — CORRODED (BS 948) · airframe 48,156 hrs · 25,831 cycles

MAIN CABIN CENTER WING BOX UPPER SKIN, RT BS 948, BL 58 IS HEAVILY EXFOLIATED. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. REPAIRED IAW PRI 525993-14AD, REV 4.

Part: DOUBLER — CORRODED (BS 1395) · airframe 48,156 hrs · 25,831 cycles

AFT CARGO JACK POINT LOWER DOUBLER, BS 1395, EXFOLIATED. FABRICATED AND INSTALLED NEW AFT CARGO JACK POINT DOUBLER IAW SRM 51-10-03 AND DWG 9915561, REV CG.

Part: INTERCOSTAL — CORRODED (BS 1259) · airframe 48,156 hrs · 25,831 cycles

AFT CARGO DOOR FRAME INTERCOSTAL CORRODED BS 1259. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED NEW INTERCOSTAL IAW SRM 51-30-02, 51-30-05 AND DWG 5936026, REV A.

Part: SKIN — DAMAGED (BS 235) · airframe 48,156 hrs · 25,831 cycles

LEFT FUSELAGE SKIN AFT OF L1 DOOR, PREVIOUS SKIN SPLICE, HAS CREASE ABOVE L18L, BS 235. REPAIRED IAW PS 900-5-1, NR 4.

Part: BULKHEAD — CORRODED (BS 1395) · airframe 48,156 hrs · 25,831 cycles

AFT CARGO PRESSURE DOME, BS 1395, FORWARD FACE HAS CORRODED AREA, L25-26R. FOUND TO BE OUT OF LIMITS. REPAIRED IAW PRI ERA 527397-14, REV O.

Part: BRACKET — CRACKED (L1 DOOR) · airframe 48,156 hrs · 25,831 cycles

L1 DOOR UPPER FORWARD AND AFT ATTACH BRACKETS ARE CRACKED. R & R UPPER HEADER BEAM IAW DWG 9955752.

Part: CUSP WEB — CORRODED (BS 864-902) · airframe 48,156 hrs · 25,831 cycles

MAIN CABIN RT CUSP WEB, BS 864-902 CORRODED AND GOUGED IN NUMEROUS LOCATIONS. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 51-10-05 AND 51-10-03.

Part: SKIN — CORRODED (AFT FUSELAGE) · airframe 48,156 hrs · 25,831 cycles

AFT LOWER FUSELAGE SKIN CUTOUT HAS CORROSION. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED NEW INTERNAL SUPPORT PLATE IAW DWG 5936667, REV CC AND ERA 527393-14, REV O.

Part: SEAT TRACK — CORRODED (BS 408-569) · airframe 48,156 hrs · 25,831 cycles

MAIN CABIN SEAT TRACK, LBL 65, BS 408-569 HAS MULTIPLE AREAS OF CORROSION. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED NEW SEAT TRACK IAW SRM 51-10-03 AND 51-10-05.

Part: WEB — CORRODED (BS 160-200) · airframe 48,156 hrs · 25,831 cycles

FLOOR WEB BS 160-200 LBL 0-12 IS CORRODED. REPAIRED FORWARD WET AREA WEB IAW ERA 527391-14.

Part: PAN — PUNCTURED (CARGO DOOR) · airframe 48,156 hrs · 25,831 cycles

WHILE CHANGING CARGO DOOR PRESSURE SEAL, FOUND PUNCTURE IN RADIUS OF DOOR PAN AT FORWARD LOWER CORNER. REMOVED DAMAGE. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 52-30-02.

Part: SKIN — CORRODED (BS 788) · airframe 48,156 hrs · 25,831 cycles

FOUND SKIN CORRODED, BS 788. R & R DOUBLER IAW DWG 5936004, REV AM AND SRM 51-30-05.

Part: CUSP WEB — DAMAGED (BS 902-962) · airframe 48,156 hrs · 25,831 cycles

MAIN CABIN CUSP WEB, BS 902-962, CORRODED AND GOUGED AT NUMEROUS LOCATIONS. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED NEW IAW SRM 51-10-05.

Part: SKIN — CORRODED (BS 826-845) · airframe 48,156 hrs · 25,831 cycles

FUSELAGE SKIN HAS CORROSION BETWEEN L29 - 30R, BS 845-826. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED DOUBLER AND FILLER REPAIR IAW SRM 53-30-01 AND 51-10-03.

Part: MOUNT — CORRODED (GALLEY) · airframe 48,156 hrs · 25,831 cycles

RT GALLEY MOUNT FORWARD CORRODED OUT OF LIMITS. R & R GALLEY FORWARD MOUNT FITTING IAW SRM 51-30-01 AND DWG 9936535, REV CS.

Part: CUSP WEB — CRACKED (BS 807-826) · airframe 48,156 hrs · 25,831 cycles

RIGHT CUSP WEB, BS 807-826 CORRODED. EVALUATED CORROSION. FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED NEW DOUBLER IAW SRM 53-20-02 AND 51-30-01.

Part: SKIN — CORRODED (BS 731) · airframe 48,156 hrs · 25,831 cycles

SKIN CORRODED, BS 731. R & R IAW DWG 5936004 AND SRM 51-31-05.

Part: CUSP WEB — CRACKED (BS 674-685) · airframe 48,156 hrs · 25,831 cycles

RIGHT CUSP WEB AT BS 674-685 CORRODED. REMOVED, FABRICATED AND INSTALLED NEW CUSP WEB IAW SRM 51-10-05 AND DWG 9940443, REV A.

Part: CUSP WEB — CRACKED (BS 1349-1368) · airframe 48,156 hrs · 25,831 cycles

LEFT CUSP WEB, BS 1349-1368 CRACKED. CUT OUT DAMAGE. FABRICATED AND INSTALLED REPAIR IAW SRM 53-20-02, 51-10-03.

Part: CUSP WEB — CRACKED (BS 1349-1368) · airframe 48,156 hrs · 25,831 cycles

LEFT CUSP WEB, BS 1349-1368 CRACKED. CUT OUT DAMAGE, FABRICATED AND INSTALLED NEW REPAIR PARTS IAW SRM 53-20-02, 53-10-03.

Part: FLOOR SUPPORT — CORRODED (BS 180) · airframe 48,156 hrs · 25,831 cycles

FLOOR SUPPORT, BS 180, RBL 30 CORRODED. REMOVED, FABRICATED AND INSTALLED NEW FLOOR SUPPORT IAW SRM 51-10-02, 51-30-02, 51-30-05 AND DWG 9936534, REV BW.

Part: CUSP WEB — CORRODED (BS 769) · airframe 48,156 hrs · 25,831 cycles

MAIN CABIN LEFT CUSB WEB CORRODED, BS 769. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 53-70-02, FIG 7 AND ERA 520318-14MA, REV O.

Part: CUSP WEB — CORRODED (BS 1349-1368) · airframe 48,156 hrs · 25,831 cycles

RIGHT CUSP WEB, BS 1349-1368 CRACKED. CUTOUT DAMAGE. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 53-20-02, FIG 13 AND 51-10-03.

Part: CUSP WEB — CORRODED (BS 1231-1250) · airframe 48,156 hrs · 25,831 cycles

RIGHT CUSP WEB, BS 1231-1250 CORRODED. CUTOUT DAMAGE. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 53-20-02, FIG 10 AND 53-10-03, FIG 11, 51-10-03.

Part: STRUCTURE — CORRODED · airframe 48,156 hrs · 25,831 cycles

FOUND NR 2 TRANSMIT RADAR LANDING CORRODED. R & R DOUBLER IAW SRM 51-20-011, 51-30-02 AND DWG 5936004.

Part: SKIN — CORRODED (BS 1240) · airframe 48,156 hrs · 25,831 cycles

SKIN SPLICE CORRODED, BS 1240, LBL 12- RBL 6. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED SPLICE IAW SRM 51-10-05, 51-30-05 AND DWG 5936667.

Part: CUSP WEB — CORRODED (BS 712-732) · airframe 48,156 hrs · 25,831 cycles

LEFT CUSP WEB, BS 712-732 CORRODED. FOUND TO BE OUT OF LIMITS. CUT OUT DAMAGE AND INSTALLED REPAIR IAW SRM 53-20-02, FIG 7.

Part: SKIN — CORRODED (BS 864) · airframe 48,156 hrs · 25,831 cycles

FUSELAGE EXTERNAL LOWER SKIN BETWEEN LONGERONS 29-30R REPAIR DOUBLER IS CORRODED, BS 864. R & R DOUBLER IAW SRM 51-10-03, 53-30-01 AND 51-30-05.

Part: SKIN — CHAFED (BS 125) · airframe 48,156 hrs · 25,831 cycles

LEFT FORWARD FUSELAGE SKIN CUTOUT FOR L1 DOOR, GUST LOCK IS CHAFED AT APPROXIMATELY STA 125, L15L. BLENDED OUT DAMAGE. FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED NEW PAN IAW SRM 53-30-01 AND DWG 5911402, REV AD.

Part: FRAME — CORRODED (BS 1344) · airframe 48,156 hrs · 25,831 cycles

AFT CARGO BAY CORROSION FOUND ON FRAME BS 1344, L26R. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED REPAIR IAW SRM 53-10-02.

Part: SKIN — CORRODED (BS 948) · airframe 48,156 hrs · 25,831 cycles

SKIN BS 948 IS HEAVILY EXFOLIATED. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED REPAIR PARTS IAW ERA 526010-14AD.

Part: LANYARD — FRAYED (L1 DOOR SLIDE) · airframe 46,642 hrs · 24,924 cycles

DURING SERVICE CHECK, FOUND L1 DOOR SLIDE LANYARD FRAYED. MAINTENANCE R & R L1 DOOR SLIDE LANYARD IAW AMM.

Part: TERMINAL — BURNED (READING LIGHT) · airframe 45,897 hrs · 24,447 cycles

BURNING ELECTRICAL ODOR AT ROW 10C. PASSENGER SAW READING LIGHT FLICKERING AND TURNED IT OFF. ODOR DISSIPATED. MX R & R BURNED TERMINAL END AT LIGHT. OPS CHECKED OK. ADJUSTED LIGHT FOR PROPER CLEARANCE.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 44,789 hrs · 23,833 cycles

DURING SERVICE CHECK, MX FOUND TAIL COMPARTMENT EMERGENCY LIGHTS INOPERATIVE. REPLACED RAMP LIGHTS ASSY. OPERATION CHECKS GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 43,538 hrs · 23,125 cycles

DURING SERVICE CHECK, MX FOUND NUMEROUS EMERGENCY LIGHTS INOPERATIVE THROUGHOUT CABIN. LAMPED AS NECESSARY. OPS CHECKED GOOD. ACFT OK FOR SERVICE.

Part: CABLE — MISROUTED (TAIL CONE) · airframe 42,555 hrs · 22,571 cycles

TAILCONE EMERGENCY EXIT EXTERIOR HANDLE LOCKING CABLE MISROUTEED PER DWG 59133350 SHEET 2 VIEW J-J. ALSO EXTERNAL HANDLE IS SEALED WITH PAINT AND UNABLE TO MOVE. FREED EXTERNAL HANDLE. REROUTED LOCKING CABLE IAW AMM 53-52-01-0830-801 PG 4 FIGURES 503 AND 504. INSTALLATION OF CABLE DID NOT COMPROMISE ORIGINAL TAILCONE INSTALLATION. INSPECTION COMPLETED.

Part: STRINGER — CRACKED (LT WING) · airframe 42,394 hrs · 22,484 cycles

FOUND LEFT WING LOWER WING SURFACE STRINGER STATION 531.7 OUTBOARD OF AILERON ON FIXED WING, TWO CRACKS OMITTING FROM A RIVET MARKED. CRACK 1 1.R INCHES AND CRACK 2 1.0 INCHES. CUTOUT DAMAGE PER SRM 57-00-01. PERFORMED DAMAGE CONTAINMENT PER NDT SPM. NO DEFECTS NOTED QC2014. FABRICATED, DRILLED UPTREATED AND INSTALLED 2024 T3 .032 DOUBLER PER SRM 57-00-01 AND ERA 502602-14.

Part: BATTERY — OVERHEATED (MASTER) · airframe 42,316 hrs · 22,444 cycles

FLIGHT CREW REPORTED STRONG ELECTRICAL ODOR IN FORWARD CABIN. MAINTENANCE FOUND HOT, SHIPS BATTERIES. REMOVED AND REPLACED SHIPS BATTERIES. OPERATION CHECKED GOOD PER AMM.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 40,626 hrs · 21,616 cycles

DURING LINE CHECK, MAINTENANCE FOUND TWO EMERGENCY LIGHTS INOPERATIVE IN TAIL CONE UPPER AFT AREA. MAINTENANCE REPLACED POWER SUPPLY PER MAINTENANCE MANUAL. OPERATION CHECKS GOOD. AIRCRAFT OK FOR SERVICE.

Part: BALLAST — DEFECTIVE (CABIN) · airframe 40,225 hrs · 21,400 cycles

PRIOR TO PUSHBACK, FLIGHT CREW AND PASSENGERS COMPLAINED OF A CHEMICAL SMELL. FLIGHT CANCELED. MAINTENANCE FOUND SEVERAL BALLAST BAD. REMOVED AND REPLACED BALLAST ROWS 31-36 PER MAINTENANCE MANUAL. OPERATION CHECKS GOOD.

Part: SLIDE — DISCONNECTED (L1 DOOR) · airframe 38,964 hrs · 20,834 cycles

FLIGHT CREW FOUND THE 1L DOOR GIRT BAR TO SLIDE CABLE DISCONNECTED. MAINTENANCE RECONNECTED 1L DOOR GIRT BAR CABLE. AIRCRAFT OK FOR SERVICE.

Part: WIRE — DAMAGED (EMERGENCY LIGHTS) · airframe 36,369 hrs · 19,552 cycles

EMERGENCY EXIT IDENTIFIERS AT L2 AFT CABIN DOORS INOP. REMOVED BATTERY PACK IN O/H AT ROW 38CDE. REINSTALLED BATTERY PACK IN O/H AT ROW 38CDE. REPAIRED WIRING AT QUICK DISCONNECT AT L2 DOOR. FOUND PIN PUSHED BACK AT Q/D FOR AFT CABIN DOOR LIGHT. REINSTALLED PIN EMER LIGHTS, OPS CKS OK.

Part: FASTENER — LOOSE (ENGINE MOUNT) · airframe 34,047 hrs · 18,198 cycles

ENGINE AFT MOUNT SUPPORT FITTING FASTENER INSPECTION PER EA 02-469466-12AD. UPPER AFT FASTENER (AFT FASTENER ON ROW A) FAILED INSPECTION. REPLACED ALL 8 FASTENERS IN FITTING PER EA INSTRUCTIONS. REPLACEMENT OF DISCREPANT FASTENERS CONSTITUTES A MAJOR REPAIR PER EA. FASTENERS LOCATED ON NR 1 ENG AFT MOUNT FITTING.

Part: SKIN — DENTED (FUSELAGE) · airframe 28,362 hrs · 14,964 cycles

THE FUSELAGE SKIN WAS DENTED AT STA 250, L18L. THE DAMAGED SKIN WAS CUT AWAY AND A REPAIR DOUBLER WAS INSTALLED.

Part: STARTER — OVERHEATED (APU) · airframe 27,182 hrs · 14,290 cycles

APU WOULD NOT START 2 ATTEMPTS MADE. CONTROL C/B PULLED RAMP REPORTED SMOKE FROM APU COMPARTMENT. SMOKE STOPPED IN FIVE MINUTES. TORQUED RELAY TERMINALS. REPLACED APU STARTER AND CLAMP. INSPECTED TAIL PIPE AND STARTER HARNESS FOUND OK. BITE ECU, FAULTS APU DOOR, CLEARED MSG, APU STARTED 3X. REMOVED MCO/PLAC.

Part: SLIDE — NO TEST (L1 DOOR) · airframe 26,776 hrs · 14,049 cycles

L-1 DOOR SLIDE FAILED FUNCTIONAL CHECK OUT PER OPN 6800. SLIDE FAILED TO DEPLOY COMPLETELY. SLIDE P/N 100504-205, S/N D9F065, PACK DATE 05/24/05. REPLACED SLIDE AND FAILED THE SECOND TIME PER OPN 6800. SLIDE EMERGENCY LIGHTING WAS INOP ON THE FORWARD SIDE. SLIDE P/N 100504-205, S/N D9F013, PACK DATE 02/23/06. REPLACED SLIDE AGAIN, OPS CHECK OK.

Part: BRAKE — UNSERVICEABLE (LEFT MLG) · airframe 24,668 hrs · 12,915 cycles

DURING TAXIOUT FOR TAKEOFF, LEFT BRAKE GRABBED DURING TURN, CAUSING FLIGHT ATTENDANT TO STUMBLE. STOPPED A/C TO CHECK ON F/A CONDITION. UPON CONTINUING TAXI WITH TIGHT LEFT TURN ONTO PARALLEL TAXIWAY, NOSE GEAR SLID AT EDGE OF CONCRETE ONTO ASPHALT APRON. A/C STOPPED AND REQUESTED TOW IN. INSPECTED BRAKES, LT SIDE DRAGS, REPLACED BOTH NR 1 & 2 BRAKES PER AMM. INSPECTED NOSE GEAR VISUALLY AND OPERATION CHECKS GOOD.

Part: ELECTRICAL SYS — FAILED (NR 1 ENGINE) · airframe 23,614 hrs · 12,364 cycles

LEFT ELEC SYSTEM FAILED EN ROUTE. REPLACED LEFT ECU.

Part: SWITCH — UNSERVICEABLE (NR 2 ENGINE) · airframe 20,799 hrs · 10,989 cycles

RIGHT FUEL PRESSURE LIGHT ILLUMINATED ON TAKEOFF ROLL. REPLACED FUEL FILTER AND PRESSURE SWITCH PER MAINT MANUAL.

Part: ENGINE — FIRE (NR 1) · airframe 20,565 hrs · 10,862 cycles

RAMP AND FLEET SERVICE REPORT NR 1 ENG TAIL PIPE FIRE ON SHUTDOWN. REF ERA087224-14 NO COKING FOUND IN NR 5 BEARING SCAV TUBE ENG, LEAK AND OPS NORM PER PFHB.

Part: GENERATOR — INOPERATIVE (LEFT) · airframe 19,927 hrs · 10,516 cycles

SHORTLY AFTER T/O L GEN OFF MSG AND L AC POWER FAULT MSG APPEARED ON OAP. ISOLATED LT GEN PER CHECKLIST AND RETURNED TO SLC SENCE APU WAS ALSO INOP. STATUS MSG SHOWED L ELEC SYSTEM FAIL. REPLACED LEFT GEN CONVERTER RAN ENG GEN OPS NORMAL OK FOR SVC.

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 18,504 hrs · 9,816 cycles

FWD OVERHEAD EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK AND CHARGER. FAILED DURING OPERATION TEST. NOW TESTS GOOD.

Part: STRUT — WORN (ENGINE MOUNT) · airframe 18,303 hrs · 9,716 cycles

A THRUST STRUT WAS FOUND TO HAVE WEAR DAMAGE BEYOND CMM LIMITS. A DER PROVIDED A BLEND REPAIR FOR THE ONE AREA OF DAMAGE. A DTA ASSESSMENT IS REQUIRED FOR CONTINUED SERVICE BEYOND THE TIME LIMITED REPAIR LIMIT.

Part: STRUT — WORN (ENGINE MOUNT) · airframe 18,303 hrs · 9,716 cycles

THE THRUST STRUT WAS FOUND TO HAVE WEAR DAMAGE IN TWO PLACES ON THE STRUT BODY. A TIME LIMITED BLEND REPAIR WAS APPROVED BY A DER. A DTA ASSESSMENT IS REQUIRED TO AUTHORIZE CONTINUED SERVICE BEYOND THE TIME LIMITED REPAIR.

Part: STRUT — WORN (ENGINE MOUNT) · airframe 18,303 hrs · 9,716 cycles

A THRUST STRUT WAS FOUND TO HAVE THREE AREAS OF WEAR DAMAGE BEYOND CMM LIMITS. A DER APPROVED BLEND REPAIR WAS PROVIDED. A DTA ASSESSMENT IS REQUIRED FOR CONTINUED SERVICE BEYOND THE TIME LIMITED REPAIR LIMIT.

Part: TRANSFORMER — FAILED (COCKPIT) · airframe 15,423 hrs · 8,275 cycles

L9 CIRCUIT BREAKER POPPING. T1-20 RIGHT INSTRUMENT TRANSFORMER REPLACED.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 14,799 hrs · 7,944 cycles

THE FS 1520 CANTED BULKHEAD WEB WAS FOUND CRACKED ALONG THE WEB SPLICE JOGGLE LINES AT STRINGER 8L AND 8R. THE CRACKED SECTIONS OF WEB WERE CUTOUT TO REMOVE THE DAMAGE. THE WEB AND SPLICE WERE RESTORED BY THE INSTALLATION OF 2 ALUMINUM REPAIR DOUBLERS AT EACH LOCATION PER ER/A 381189-14, REV A.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 14,431 hrs · 7,750 cycles

AFT OVERRHEAD AISLE EMERGENCY LIGHTS INOP. REPLACED POWER SUPPLY.

Part: LENS — MISSING (ROW 14) · airframe 13,972 hrs · 7,502 cycles

FLOOR EMER LT AT ROW 14 LENSE MISSING. RPLCD LENSE.

Part: BULB — INOPERATIVE (CABIN) · airframe 13,972 hrs · 7,502 cycles

OVERHEAD EMERGENCY LIGHT AT ROW 1R INOP. RELAMPED. CHKS GOOD.

Part: CABLE — OUT OF ADJ (TAILCONE) · airframe 13,593 hrs · 7,313 cycles

FOUND DURING ROUTINE TAIL CONE JETTISON CHECK AT DFW, D-2 LETTER CHECK. FROM NON ROUTINE CARD 50: HANDLE INOP DURING TAIL CONE JETTISON TEST, OUTSIDE DEPLOY HANDLE WOULD NOT OPERATE. HANDLE APPEARS TO BE CAUGHT BEHIND AIRCRAFT SKIN. STRAIGHTENED AND ADJUSTED HANDLE RETAINING CLIPS. OPS CHECK GOOD.

Part: ADC — DAMAGED (E/E BAY) · airframe 12,552 hrs · 6,769 cycles

AT ROTATION A GREATER THAN 40KT AIRSPEED DISCREPENCY OCCURRED BETWEEN CAPT AND F/O INSTRUMENTS. CONTROL OF AIRCRAFT WAS TRANSFERRED TO F/O. CONTINUOUS OVERSPEED WARNING SOUNDED OVER CAWS. A 100KT A/S DISCREPENCY WAS NOTED AT ONE POINT. SELECTED BOTH CADC ON 2. AIRSPEEDS STABILIZED TO NORMAL. AN ACS FAULT MESSAGE WAS NOTED AT THAT TIME. FOUND NR 1 CADC HAD NO POWER AND WOULD NOT SELF TEST. REPLACED NR 1 CADC PER MM, NR 1 CADC FUNCTION TEST GOOD PER MM.

Part: VIDEO UNIT — MALFUNCTIONED (CABIN) · airframe 11,957 hrs · 6,445 cycles

FLT ATTENDANT NOTICED ELEC SMELL FROM VIDEO UNIT. POWER TURNED OFF AND SMELL WENT AWAY THEN RETURNED. BREAKERS PULLED AND SMELL WENT AWAY. FOUND SMELL COMING FROM VTR-2. REPLACED SAME, CHECKS OK.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

EMERGENCY LIGHTS CAME ON ROW 38 DURING T/O. REPLACED DEFECTIVE POWER SUPPLY.

Part: ANGLE — CRACKED (BS 940)

FUSELAGE ATTACH FITTING, VERTICAL STAB TO FUSE ANGLE, REPAIR FOR CRACK. THE VERTICAL STABILIZER TO FUSELAGE ATTACH ANGLE WAS FOUND WITH A .75 CRACK BETWEEN FASTENERS AT FS 940 ON THE LT SIDE OF THE FUSELAGE. THE CRACKED AREA WAS ROUTED OUT OF THE ANGLE AND REPAIRED WITH A STEEL REPAIR ANGLE PER ER/A 366304-14.