N914HA

Part: CONTROL WHEEL — BINDING (TRIM) · airframe 69,901 hrs · 79,359 cycles

AFTER TAKEOFF, TRIMS WERE SET. TRIM WHEEL AND INDICATOR OPERATED NORMALLY, HOWEVER ACFT WAS FLYING TAIL HEAVY REGARDLESS OF TRIM SETTINGS. INSPECTED AND FOUND LT ELEVATOR TIM CONTROL WHEEL BINDING, GROOVES IN WHEEL ASSEMBLY TRACK AND INDICATOR PIN MISALIGNED. R & R CONTROL WHEEL AND REALIGNED INDICATOR PIN IAW MM 27-36-00. INSPECTED CABLES IN APU AREA. NO OBVIOUS DEFECTS FOUND. CABLES MOVE FREELY.

Part: BULB — DIM (EMERGENCY LIGHT) · airframe 69,616 hrs · 79,031 cycles

EMERGENCY EXIT LIGHT IS DIM AT ROW 4DF. R & R THE BULB. OPS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 6,961 hrs · 79 cycles

EMERGENCY EXIT LIGHTS ARE INOPERATIVE. R & R EMERGENCY LIGHT BATTERY. OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 69,577 hrs · 78,987 cycles

SIDEWALL EMERGENCY EXIT LIGHT HAS ONE BULB INOPERATIVE AT ROW 4. R & R THE BULB. OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS) · airframe 60,577 hrs · 78,987 cycles

EMERGENCY LIGHT INOPERATIVE. R & R THE BULB. OPS CHECKED GOOD.

Part: BULB — DIM (EMERGENCY LIGHT) · airframe 69,170 hrs · 78,503 cycles

FORWARD RT EMERGENCY SIGN ABOVE EMERGENCY EXIT IS DIM. R & R BULBS. OPS CHECKED GOOD.

Part: INDICATOR — MALFUNCTIONED (NR 1 ENGINE OIL) · airframe 69,093 hrs · 78,397 cycles

NR 1 ENGINE OIL PRESSURE FLUCTUATED BETWEEN 80-100 PSI IN FLIGHT. INDICATION WENT TO MAX ON THE GROUND. PRESSURE REMAINED AT 40 PSI AFTER ENGINE SHUTDOWN. R & R NR 1 ENGINE OIL PRESSURE INDICATOR. GROUND RAN ACFT. OPS CHECKED GOOD.

Part: LOCK — DEPLOYED (NLG) · airframe 68,804 hrs · 78,043 cycles

AFTER GEAR RETRACTION, LT, RT, AND NOSE DOOR AMBER LIGHT AND NOSE GREEN AND RED LIGHTS REMAINED ILLUMINATED. AFTER ALTERNATE EXTENSION, RED UNSAFE LIGHT WENT OUT AND ALL 3 GREEN GEAR INDICATIONS ILLUMINATED. INSPECTED ACFT AND FOUND NOSE GEAR GROUND LOCK DEPLOYED. NO OTHER DEFECTS NOTED. INSPECTED NOSE GEAR GROUND LOCK. OPS CHECKED NORMALLY. RESET NOSE GEAR GROUND LOCK. ACFT RELEASED FOR EVALUATION FLIGHT. EVALUATION FLIGHT WAS SATISFACTORY.

Part: MONITOR — INOPERATIVE (AC POWER) · airframe 68,746 hrs · 77,978 cycles

AC POWER MONITOR IS BLANK. R & R AC POWER MONITOR IAW 24-29-05. OPS CHECKED GOOD.

Part: AUTOFEATHER SYS — MALFUNCTIONED · airframe 68,166 hrs · 77,278 cycles

AUTOFEATHER DID NOT ARM DURING TAKEOFF ROLL, CYCLED CIRCUIT BREAKER Q4 NO FIX. GROUND RAN ACFT AND PERFORMED OPS CHECK OF AUTO FEATHER SYS IAW MANUAL. SYS OPERATES NORMAL AT THIS TIME.

Part: CONTROLLER — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 67,798 hrs · 76,823 cycles

EMERGENCY LIGHTS CAME ON ENROUTE. RIGHT SECONDARY BUSS VOLTAGE STEADY AT 26.6 VOLTS. PROPELLER HEAT OFF. NO WARNING OR CAUTIONS. R & R EMERGENCY LIGHT CONTROL BOX AND POWER SUPPLY IAW WC 33-50-05R, 33-50-03Q. OPS CHECKED GOOD AT THIS TIME.

Part: RELAY — FAILED (AUTOFEATHER) · airframe 67,787 hrs · 76,805 cycles

AUTOFEATHER DID NOT ARM, DOES STATIC TEST OK. COULD NOT DUPLICATE. R & R RELAY 6121-K5 FOR TROUBLESHOOTING. GROUND RAN, OPS CHECKED GOOD AT THIS TIME.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 67,488 hrs · 76,442 cycles

FOURTH RED EMERGENCY FLOOR LIGHT IS INOPERATIVE. R & R BULB. OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 67,414 hrs · 76,350 cycles

FLOOR EMERGENCY ESCAPE PATH LIGHT HAS ONE BULB INOPERATIVE AT ROW 1. R & R BULB. OPS CHECKED GOOD.

Part: INDICATOR — INACCURATE (TE FLAPS) · airframe 67,164 hrs · 76,048 cycles

FLAP POSITION INDICATOR READS 2.5 DEG W/ FLAP SELECTED TO ZERO. R & R FLAP POSITION INDICATOR IAW -8MM, 27-53-05. OPS CK GOOD.

Part: WARNING LIGHT — MALFUNCTIONED (MLG) · airframe 67,128 hrs · 76,000 cycles

WHEN GEAR SELECTED UP, THE THREE GREEN LIGHTS STAYED ON AND THE THREE RED UNSAFE LIGHTS ILLUMINATED. AFTER APPROX 90 SECONDS, GEAR RETRACTED AND LIGHTS WENT OUT. OPS NORMAL AFTER THAT. SWUNG GEAR, OPS CHECKED GOOD IAW MM 32-30-05. NO DEFECTS NOTED. R & R GEAR SELECT CONTROL PANEL AS PRECAUTION. REF MM 32-30-05. OPS CHECKED GOOD AT THIS TIME. OK FOR SERVICE.

Part: GROUND WIRE — BROKEN (MLG) · airframe 67,130 hrs · 76,003 cycles

AFTER TAKEOFF, ON GEAR RETRACTION, ALL GEAR REMAINED DOWN. ALL THREE GREEN, RED AND HANDLE LIGHTS REMAINED ILLUMINATED IAW CHECKLIST, SELECTED GEAR DOWN THEN HAD 3 GREEN AND 3 AMBER, GEAR DOORS INDICATED CLOSED 5 MINUTES LATER. JACKED ACFT, CYCLED GEAR SEVERAL TIMES. AFTER SEVERAL CYCLES, GEAR FAILED TO EXTEND. FOUND GROUND WIRE FOR SELECTOR VALVE BROKEN AT CONNECTOR PLUG. RESOLDERED WIRE TO CONNECTOR PLUG. SWUNG GEAR SEVERAL TIMES. OPS CHECKED GOOD. OK FOR SERVICE AT THIS TIME.

Part: CONTROL HEAD — INTERMITTENT (NR 2 COMMS) · airframe 67,051 hrs · 75,907 cycles

NR 2 COMM HEAD BLANK AND INTERMITTENTLY SHOWS TEST MESSAGE ON SCREEN. R & R NR 2 COMM CONTROL HEAD. OPS CHECKED GOOD IAW MM 23-21-04.

Part: PUMP — MALFUNCTIONED (HYD SYSTEM) · airframe 66,959 hrs · 75,792 cycles

ON TAXI OUT TO RUNWAY, NR 2 STANDBY HOT CAUTION LIGHT ILLUMINATED. GOOD HYD QTY AND PRESSURE. SWAPPED NR 2 STANDBY HYD PUMP TO SPAR TEMP SENSOR IAW SP29.5. OPS CHECKED GOOD AT THIS TIME.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 66,538 hrs · 75,293 cycles

EMERGENCY SIDEWALL LIGHTS ARE INOP AT ROW 4AC. REMOVED LENS. R & R ONE BULB. OPS CHECKED GOOD. REINSTALLED LENS.

Part: GENERATOR — SLOW (NR 1 AC) · airframe 66,301 hrs · 75,006 cycles

NR 1 AC GENERATOR IS SLOW TO COME ON LINE WHEN SELECTED ON WITH PROP AT 785. REQUIRES SEVERAL RESETS. COULD NOT DUPLICATE. GROUND RAN ACFT IAW RUN UP MANUAL. OK FOR SERVICE.

Part: GENERATOR — WARNING LIGHT (NR 2) · airframe 66,288 hrs · 74,988 cycles

RT AC BUSS CAUTION LIGHT ILLUMINATED AFTER NR 2 AC GENERATOR WAS BROUGHT ON LINE. CYCLED NR 2 AC GENERATOR. CAUTION LIGHT AND BUSS FAULT LIGHT WENT OUT. R & R NR 2 GCU IAW 24-21-02 AND NR 2 AC GENERATOR IAW WC 24-20-11R. OPS AND LEAK CHECKED GOOD.

Part: WIRE — CHAFED (NR 1 NACELLE) · airframe 67,894 hrs · 76,841 cycles

F/A REPORTED EMERGENCY LIGHTS ILLUMINATED DURING CLIMBOUT FOR A FEW SECONDS AND REMAINED OFF FOR REST OF THE FLIGHT WITH NO OTHER ASSOCIATED LIGHTS. INSPECTED WIRING AT NR 1 RGB IN NACELLE. FOUND SEVERAL WIRES CHAFED NEAR AC GENERATOR CONNECTOR PLUG. APPLIED CHAFE PROTECTION TO AFFECTED WIRES. ALSO COMPLIED WITH EMERGENCY LIGHT BLOCKING DIODE, CHECK WORK CARD. NO DEFECTS NOTED. RAN ENGINE. ALL SYSTEMS CHECKED GOOD. OK FOR SERVICE.

Part: CONTROL BOX — INTERMITTENT (EMERGENCY LIGHT) · airframe 66,098 hrs · 74,751 cycles

ALL EMERGENCY LIGHTS ILLUMINATED INTERMITTENTLY. MX INSPECTED BOTH BRUSH BLOCKS AND ADJACENT WIRE HARNESS. NO DEFECTS NOTED. GROUND RAN ACFT AND COULD NOT DUPLICATED. R & R EMERGENCY LIGHT CONTROL BOX FOR MX CONVENIENCE. OPS CHECKED GOOD IAW 33-51-00. OK FOR SERVICE.

Part: LEAD — BURNED (PROP HEAT) · airframe 60,760 hrs · 67,606 cycles

EMERGENCY LIGHTS FLICKERED ON IN CRUISE FLIGHT WITH PROP HEAT ON. INSPECTED WIRING AND CHECKED RESISTANCE FOR NR 1 AND NR 2 BRUSH BLOCKS AND SLIP RINGS. CHECKED GOOD. INSTALLED PANELS. FOUND HEATER LEAD CRACKED ON NR 200 NR 3 BLADE. R & R HEATER LEAD IAW MM 61-13-00. GROUND RAN ACFT. NO DEFECTS NOTED AT THIS TIME.

Part: WIRE HARNESS — SATURATED (PROP HEAT) · airframe 65,921 hrs · 74,531 cycles

EMERGENCY LIGHTS FLICKERS WITH PROP HEAT ON. OK WITH OFF. OK AT 1050 NP. UNABLE TO DUPLICATE PROBLEM ON GROUND RUN. INSPECTED BOTH PROP BLADE LEADS CHECKED GOOD. NR 1 ENGINE HARNESS FROM BRUSH BLOCK P5 TO J4 SOAKED WITH OIL. REPLACED HARNESS. GROUND RAN ACFT PROP HEAT. OPS CHECKED GOOD. NO FLICKERING OF EMERGENCY LIGHTS AT 1050 NP.

Part: BRUSH BLOCK — DIRTY (PROP DEICE) · airframe 65,921 hrs · 74,531 cycles

ALL CABIN EMERGENCY LIGHTS FLICKERING, WHEN PROP AT 1050, OP HEAT ON AND PHASE 2A. EMERGENCY LIGHTS DO NOT FLICKER WHEN SELECTED TO 900. CLEANED AND INSPECTED PROP BRUSH BLOCKS ON BOTH ENGINES IAW MM 61-10-11. OPS CHECKED GOOD.

Part: BRUSH BLOCK — INTERMITTENT (PROP HEAT) · airframe 65,921 hrs · 74,531 cycles

EMERGENCY LIGHTS FLICKER WITH PROP HEAT ON. OK AT 1050 NP. R & R NR 1 AND NR 2 BRUSH BLOCK ASSY'S IAW DASH 8 MM 61-10-11. GROUND RAN ACFT WITH NO DEFECTS NOTED. OPS CHECKED GOOD AT THIS TIME.

Part: CONTROL CABLE — OUT OF ADJUST (ELEVATOR) · airframe 65,782 hrs · 74,369 cycles

ELEVATOR CONTROLS VERY SLOPPY AND DIFFICULT TO MAINTAIN PITCH ATTITUDE ON APPROACH AND LANDING. ADJUSTED ELEVATOR CABLE TENSIONS IAW MM 27-00-00. COMPLETED RII OF ELEVATOR CABLE TENSION.

Part: BRUSH BLOCK — MALFUNCTIONED (PROP DE ICE) · airframe 65,719 hrs · 74,294 cycles

EMERGENCY FLOOR LIGHT FLICKER DURING CLIMB OUT WITH ASSOCIATED WARNINGS. NR 2 AC GENERATOR VOLTS DROP ON "B" PHASE. INSPECTED NR 2 PROP R & R BRUSH BLOCK AND OPS CHECKED IAW RUN UP MANUAL. OPS CHECKED GOOD.

Part: CONTROLLER — INTERMITTENT (EMERGENCY LIGHTS) · airframe 65,684 hrs · 74,256 cycles

EMERGENCY LIGHTS FLICKER WITH NR 2 PROP A PHASE ACTIVE. R & R EMERGENCY CONTROL BOX IAW -8 MM 33-51-00. GROUND RAN ACFT. OPS CHECKED GOOD.

Part: SWITCH — SHORTED (EMERGENCY LIGHTS) · airframe 65,544 hrs · 74,086 cycles

EMERGENCY LIGHTS FLICKERED ON CLIMBOUT WITH PROP HEAT AND IGNITERS ON. LIGHTS DID NOT FLICKER DURING CRUISE OR IN DECENT. R & R F/A EMERGENCY LIGHT SWITCH. SYS CHECKED GOOD IAW AMM 33-52-00. OK FOR SERVICE. FOUND F/A SWITCH SHORTING DURING SYS INSPECTION.

Part: BRUSH BLOCK — UNKNOWN (PROP DE ICE) · airframe 65,522 hrs · 74,057 cycles

EMERGENCY LIGHTS FLICKERED ON CLIMBOUT WITH NR 2 PROPELLER A PHASE. REMOVED FWD UPPER COWL PANEL ON NR 2 ENGINE. INSPECTED BRUSH BLOCK ASSY SLIP RINGS AND HEATER LEADS. NO FAULTS FOUND, REINSTALLED PANEL. REMOVED FORWARD UPPER COWL AND NR 1 ENGINE ENGINE AND INSPECT SAME R & R NR1 BRUSH BLOCK ASSY.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 65,467 hrs · 73,981 cycles

EMERGENCY LIGHT IS INOPERATIVE. REMOVED PLASTIC COVERING. R & R BULB. REINSTALLED PLASTIC COVERING. OPS CHECKED GOOD.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 64,905 hrs · 73,285 cycles

EMERGENCY FLOOR RED LIGHT IS INOPERATIVE AT ROW 1. REMOVED LENS, REMOVED AND REPLACED BULB. OPS CHECKED GOOD.

Part: HMU — FAILED (NR 1) · airframe 64,426 hrs · 72,715 cycles

DURING TAKEOFF, NR 1 POWER LEVER HAD 2 KNOB SPLIT. WHEN SWITCH SET TO NORM, THE NR 1 ENGINE TORQUE SURGED TO 96 PERCENT MOMENTARILY, THEN DROPPED TO 80 PERCENT. NO CAUTION LIGHT OR ENGINE REVERSION. R & R 1 HMU IAW WORKCARD 73-20-01R, 76-00-01Q AND 72-01-01X. OPS AND LEAKED CHECKED GOOD. CLEARED MEL.

Part: CONTACTOR — INOPERATIVE (EMERGENCY LIGHTS) · airframe 64,200 hrs · 72,467 cycles

EMERGENCY LIGHTS FLICKERED INFLIGHT. R & R 2431-K18 SECONDARY BUSS CONTACTOR IAW STD PRACTICES, OPS CHECKED GOOD

Part: CONTROL BOX — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 64,138 hrs · 72,400 cycles

EMERGENCY LIGHTS FLICKERED THE ENTIRE FLIGHT. ALL FLOOR EMERGENCY AND ROW 1DF LOWER EXIT SIGN. R & R NR 2 BRUSH BLOCK. OPS CHECKED GOOD IAW MM 30-61-00. R & R EMERGENCY LIGHTS CONTROL BOX IAW MM 33-51-00. OPS CHECKED GOOD. RT TRU WAS ALSO CHANGED.

Part: HYDRAULIC SYSTEM — DISCHARGED · airframe 63,818 hrs · 72,037 cycles

LOSS OF NR 2 HYD FLUID IN FLIGHT. PRESSURE AT ZERO FOR MORE THAN 20 MINUTES. NR 1 HYD QUANITY DROPPED TO ZERO WHEN PARK BRAKE APPLIED. ACFT WAS BEING POSITION FOR REMOVAL OF OTBD ROLL SPOILER AND ENGINE DRIVEN PUMP.

Part: BRUSH BLOCK — FAILED (NR 2 PROPELLER) · airframe 63,293 hrs · 71,445 cycles

EMERGENCY LIGHTS FLICKERED DURING CLIMB. R & R NR1 AND NR 2 PROP BRUSH BLOCK IAW MM 61-10-11. COMPLIED WITH WORKCARD 33-50-03Q. EMERGENCY LIGHT SYS OPS CHECKED GOOD.

Part: CONTROL BOX — FAILED (EMERGENCY LIGHTS) · airframe 63,287 hrs · 71,437 cycles

FLOOR EMERGENCY LIGHTS FLICKERED DURING CLIMB OUT. R & R LIGHT CONTROL BOX IAW WORKCARD 33-50-03Q.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 62,597 hrs · 70,602 cycles

STRONG ODOR IN COCKPIT IN FLIGHT. CYCLED BLEEDS OFF, NO DIFFERENCE NOTED (NO ODOR IN CABIN). INSPECTED ACFT FOR ODORS, NONE FOUND. INSPECTED AVIONICS RACK, TRU'S AND INVERTERS DURING ENGINE RUNS. NO ODORS NOTED. ACFT OK FOR SERVICE.

Part: MODULE — INOPERATIVE (EMERGENCY LIGHT) · airframe 62,477 hrs · 70,459 cycles

MIDCABIN FLOOR EMERGENCY LIGHT AT ROW 2DF WILL NOT ILLUMINATE. INSTALLED NEW LIGHT MODULE AS REQUIRED.

Part: SPLICE — FAILED (EMERGENCY LIGHT) · airframe 62,477 hrs · 70,459 cycles

RIGHT FORWARD EMERGENCY EXIT LIGHT DOES NOT ILLUMINATE. FOUND DIODED MATRIX SPLICE 3352-CR6 BROKEN. R & R DIODED. EXIT LIGHT OPERATED NORMALLY ON GROUND.

Part: PANEL — CORRODED (WING) · airframe 62,477 hrs · 70,459 cycles

PANEL 523AT HAS PITTING IN NUMEROUS COUNTERSINKS. REMOVED PITTING IAW RD8-57-1686.

Part: PANEL — GROOVED (WING) · airframe 62,477 hrs · 70,459 cycles

PANEL 522AT HAS DEEP GROOVES AND PITTING IN COUNTERSINKS. REMOVED GROOVES AND PITTING IAW RD8-57-1686.

Part: PANEL — CORRODED (WING) · airframe 62,477 hrs · 70,459 cycles

PANEL 622AT HAS PITTING IN MARKED COUNTERSINKS. REMOVED PITTING IAW RD8-57-1686.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 62,477 hrs · 70,459 cycles

RT INBD AFT SEAT RAIL IS CORRODED ALONG OTBD FLANGE. REMOVED OLD SEAT RAIL, INSTALLED NEW RT INBD AFT SEAT RAIL IAW DWG 85330129 AND RD8-53-4472.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 60,942 hrs · 68,740 cycles

EMERGENCY FLOOR PATH LIGHT AT ROW 8 WILL NOT ILLUMINATE. R & R EMERGENCY FLOOR PATH MINIATURE BULB LIGHT ASSY AT ROW 8.

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS) · airframe 60,769 hrs · 68,551 cycles

ROW 2AC OVERHEAD EMERGENCY LIGHT. R & R ROW 2AC OVERHEAD EMERGENCY LIGHT BULB, OPS CHECKED GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 60,646 hrs · 68,409 cycles

ROW 1AC, 3RD RED FLOOR EMERGENCY PATH LIGHT INOP. RELAMP 3RD RED FLOOR EMERGENCY PATH LIGHT AT ROW 1 IAW AMM 33-20-00.

Part: SWITCH — INOPERATIVE (EMERGENCY LIGHTS) · airframe 60,405 hrs · 68,134 cycles

F/A EMERGENCY GREEN LIGHT SWITCH IS INOP. INSPECTED AND FOUND TO BE BAD SWITCH. REMOVED THE OLD SWITCH AND INSTALLED NEW SWITCH. OPS CHECKED GOOD.

Part: UNKNOWN — UNKNOWN (CABIN AIR) · airframe 59,732 hrs · 67,359 cycles

WHILE TAXIING, MOTOR NOISE HEARD LABORING AND CHANGING SPEED, FUMES AND SLIGHT MIST APPEARED IN CABIN AND FLIGHT DECK AND DISSAPATED AFTER TURNING BLEEDS OFF. DUCT TEMP INCREASED TO OVER 60 DEGREES

Part: TARGET — MISSING (NLG) · airframe 59,714 hrs · 67,334 cycles

WOW CAUTION LIGHT ILLUMINATED AFTER GEAR RETRACTION AND REMAINED ILLUMINATED FOR REST OF FLIGHT. REPLACED MISSING TARGET IN NLG TRAIL ARM IAW 32-20-01. OPS CHECKED GOOD.

Part: TIRE — DEFLATED (LT MLG) · airframe 59,419 hrs · 66,987 cycles

NR 2 LT MAIN TIRE PICKED UP PIECE OF METAL ON TAXI OUT, RETURN TO GATE, TIRE COMPLETELY DEFLATED. R & R NR1 AND NR2 MAIN WHEEL ASSY IAW WORK CARD 32-20-03.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 59,086 hrs · 66,621 cycles

ROW 1 FIRST TWO RED FLOOR LEVEL LIGHTS NOT WORKING. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY AT POSITION 3352-PS2.

Part: BULB — BURNED OUT (EMERGENCY LIGHTS) · airframe 59,030 hrs · 66,558 cycles

EMERGENCY LIGHT IN CEILING AT ROW 2 IS NOT WORKING. R & R EMERGENCY LIGHT BULB IN CEILING ROW 2. CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 59,031 hrs · 66,558 cycles

EMERGENCY FLOOR LIGHT BAD AT ROW 1. R & R EMERGENCY FLOOR LIGHT AT ROW 1. CHECKED GOOD.

Part: APU — ODOR · airframe 58,999 hrs · 66,522 cycles

STRONG FUEL OIL ODOR IN CABIN AND COCKPIT. MX INSPECTED AND WITH BLEEDS ON, ADVISED A STRONG FUEL ODOR FROM THE APU IN THE CABIN AND COCKPIT.

Part: SHUTOFF VALVE — WARNING LIGHT (NR 1 BLEED SYS) · airframe 57,794 hrs · 65,185 cycles

NR 1 BLEED HOT CAUTION LIGHT WENT ON AND OFF AT 3000 FEET WITH ODOR FROM DUCTS. SELECTED NR 1 BLEED OFF AND LIGHT WENT OFF BUT ODOR DID NOT DISSIPATE. REMOVED AND REPLACED NR 1 H/P BLEED SOV IAW AMM 21-11-16, OPS CHECK GOOD.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 57,728 hrs · 65,113 cycles

REPORTED BY PILOT OF A SMELL OF HOT ELECTRONICS FROM COCKPIT. PILOT RAN BLEEDS FULL HOT AND THAN COLD, ODOR DISSIPATED. SUSPECT NEW DUCTING INSTALLED AT RON TO BE SOURCE. CURRENT LEVEL OF ODOR IS ACCEPTABLE TO CREW. NO ODOR WITH BLEEDS OFF. FLIGHT DECK AIR CONDITIONING MODIFIED PER FCD8-21-09-0180 TO RELOCATE CONDITIONED AIR TO SIDEWALL GASPERS. NO DETECT NOTED AT THIS TIME.

Part: SWITCH — FAILED · airframe 57,430 hrs · 64,788 cycles

TAKEOFF WARNING HORN SOUNDED DURING LANDING AND WOULD NOT SILENT. REMOVED AND REPLACED SWITCH 3151-S6 ON NR 2 PWR LAYSHAFT. OPS CK GOOD IAW WORK CARD 31-50-00Q

Part: LIGHT — INOPERATIVE (CABIN) · airframe 57,255 hrs · 64,609 cycles

EMERGENCY LIGHT IN FLOOR ESCAPE PATH LIGHT 3RD FROM FRONT. RELAMPED EMERGENCY LIGHT AT ROW 1 IN ESCAPE PATH LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 57,110 hrs · 64,456 cycles

EMERGENCY LIGHT INOP IN CEILING AT ROW 8. REPLAMPED CEILING LIGHT, OPS GOOD.

Part: LIGHT — DEFECTIVE (EXTERIOR) · airframe 56,314 hrs · 63,607 cycles

DURING ROM MAINTENANCE, THE LEFT FORWARD EMERGENCY EGRESS LIGHT WAS FOUND TO BE DIM. THE BULB WAS REPLACED AND LIGHTING, OPS CHECKED GOOD.

Part: CIRCUIT BREAKER — FAILED (CABIN) · airframe 54,219 hrs · 61,349 cycles

GREEN LIGHT NOT ILLUMINATING ON EMERGENCY LIGHT SWITCH AT F/A'S PANEL. REPLACED SWITCH (P/N AML21GBA2CD) NO FIX, REPLACED C/B, OPS CK'D GOOD.

Part: CIRCUIT BREAKER — FAULTY (CABIN) · airframe 54,219 hrs · 61,349 cycles

GREEN LIGHT NOT ILLUMINATING ON EMERGENCY LIGHT SWITCH AT F/A'S PANEL. REPLACED SWITCH (P/N AML21GBA2CD), NO FIX, REPLACED C/B, OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 54,219 hrs · 61,349 cycles

AFT CEILING EMERGENCY LIGHT INOP. REPLACED BURNED OUT LAMP, OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 54,219 hrs · 61,349 cycles

EMERGENCY EXIT SIGN BY RIGHT SIDE AFT DOOR HAS INOP LAMP. REPLACED BURNED OUT LAMP, OPS CK'D GOOD.

Part: PSEU — FAILED (LANDING GEAR) · airframe 54,205 hrs · 61,335 cycles

AFTER TAKEOFF, WHEN THE LANDING GEAR WAS RETRACTED, THE CREW OBSERVED AMBER WARNING LIGHTS FOR BOTH RIGHT AND LEFT MAIN GEAR DOORS AND A RED UNSAFE INDICATION FOR THE NOSE GEAR. THE CREW THEN LOWERED THE GEAR AND LEFT IT IN THE DOWN POSITION FOR THE REMAINDER OF THE FLIGHT. THE FLIGHT THEN RETURNED TO THE FIELD AND DECLARED AN EMERGENCY WHERE CRASH RESCUE WAS DISPATCHED. THE AIRCRAFT THEN LANDED WITHOUT INCIDENT AND TAXIED NORMALLY. MAINTENANCE JACKED THE AIRCRAFT AND CYCLED THE LANDING GEAR WITHOUT DISCREPANCIES. THE PSEU WAS CHANGED AND SYSTEM WAS CYCLED SEVERAL MORE TIMES TO VERIFY SYSTEM OPERATION. NO FURTHER FAULTS WERE FOUND AND AIRCRAFT WAS THEN RELEASED FOR SERVICE.

Part: STRUCTURE — CRACKED (NACELLE) · airframe 53,968 hrs · 61,071 cycles

DURING INSPECTION, FOUND CRACKS IN THE NR 1 FORWARD RADIUS AT ABOUT 2 O’CLOCK AND NR 2 HORSE COLLAR FORWARD RADIUS AT THE 2 O’CLOCK AND 10 O’CLOCK POSITIONS. REPAIRED ALL THREE CRACKS PER RD8-54-2451 AND RD8-54-1736.

Part: OIL SYSTEM — LOW PRESSURE (NR 1 ENGINE) · airframe 53,845 hrs · 60,933 cycles

ON CLIMBOUT NR 1 ENG OIL PRESSURE GAUGE FLUX, FOLLOWED BY NR 1 ENGINE OIL WARNING LIGHT. CREW REDUCED POWER AND LEVELED OFF, OIL PRESSURE STABILIZED AND NR 1 ENG OIL WARNING LIGHT EXTINGUISHED. NR 1 OIL PRESSURE FLUX BETWEEN 60 AND 30 PSI FOR APPROX 5 MIN.

Part: TRANSMITTER — MALFUNCTIONED (NR 1 ENGINE)

NR 1 ENG OIL PRESS WENT TO 40 PSI IN FLT NO WARNING LIGHT. SHUT DOWN NR 1 ENGINE. REMOVED AND REPLACED NR 1 OIL PRESSURE TRANSMITTER. LEAK AND OPS CHECK GOOD.

Part: EEC — MALFUNCTIONED (NR 2 ENGINE) · airframe 52,841 hrs · 59,882 cycles

NR 2 ENGINE MANUAL LIGHT ILLUMINATED & TORQUE DROPPED BY 50 PERCENT. CREW DECLARED EMERGENCY AND LANDED ON RUNWAY 22 WITHOUT INCIDENT. THE CAPTAIN WAVED OFF THE EMERGENCY EQUIPMENT. ALL PASSENGERS WERE FINE. REMOVED AND REPLACED EEC UNIT. OPS CHECK GOOD.

Part: STRINGER SPLICE — CORRODED (BS 488 S28R) · corrosion level 2 · airframe 51,477 hrs · 58,476 cycles

CABIN UNDER FLOOR STATION 488 STRINGER SPLICE ON STRINGER 28S IS CORRODED. REPLACED SPLICE.

Part: FRAME — CORRODED (BS 467 S31-32R) · corrosion level 2 · airframe 51,477 hrs · 58,476 cycles

FRAME LEG IS CORRODED BETWEEN STRINGERS 31 AND 32 AT X467 R/S. REPLACED LOWER FRAME SEGMENT.

Part: STRINGER — CORRODED (BS 488-531 S32R) · corrosion level 2 · airframe 51,477 hrs · 58,476 cycles

STRINGER 32 BETWEEN STATION 488 AND 531 REPLACED DUE TO HEAVY CORROSION.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 51,477 hrs · 58,476 cycles

STRINGER TIE REPLACED AT X424 STRINGER 25 DUE TO CORROSION.

Part: FRAME — CORRODED (BS 467 S24-31L) · corrosion level 2 · airframe 51,477 hrs · 58,746 cycles

FRAME LEGS BETWEEN STRINGERS 24 THROUGH 31 ARE CORRODED. REPLACED FRAME SEGMENT.

Part: FRAME — CORRODED (BS 445 S26-31R) · corrosion level 2 · airframe 51,477 hrs · 58,476 cycles

CORROSION TO FRAME LEGS AT X445 BETWEEN STRINGERS 26 THROUGH 31. REPLACED FRAME SECTION.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,477 hrs · 58,476 cycles

STRINGER TIE REPLACED DUE TO CORROSION AT X424 STRINGER 23 RT.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,477 hrs · 58,476 cycles

FWD SIDE OF STRINGER TIE AT X424 STRINGER 31S WAS REPLACED DUE TO CORROSION.

Part: FLOOR SUPPORT — CORRODED (BS 445) · corrosion level 2 · airframe 51,477 hrs · 58,476 cycles

BOTTOM OF RIGHT FLOOR SUPPORT AT 445 IS CORRODED. REPLACED SUPPORT.

Part: SHEAR TIE — CORRODED (BS 215) · corrosion level 2 · airframe 51,477 hrs · 58,746 cycles

CLEAT ATTACHING FORWARD FRAME TO SKIN REMOVED AND REPLACED DUE TO CORROSION.

Part: FLOORBEAM — CORRODED (BS 291) · airframe 51,477 hrs · 58,476 cycles

CABIN UNDER FLOOR FRAME LEG BETWEEN 32-33 L/S AT FRAME BEHIND RECIRC FAN MOUNT IS CORRODED AT X291. CLEANED AREA OF FRAME LEG AND FOUND MINOR CORROSION AROUND I/B MOST RIVET. CLEANED ALODINED AND PRIMED AREA.

Part: STRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,477 hrs · 57,846 cycles

LONG STRAP AT TOP OF INTERCOSTAL IS CORRODED. FABRICATED NEW STRAP AND INSTALLED PER 85320462.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,477 hrs · 58,476 cycles

STRINGER TIE REPLACED DUE TO CORROSION AT X424 STR 26S.

Part: ANCHOR FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,477 hrs · 58,476 cycles

ATTACH CLEAT ON STRINGER 29S AT X434 IS CORRODED. REMOVED AND REPLACED CLEAT.

Part: STRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,477 hrs · 58,476 cycles

INTERNAL JOINT STRAP AT X424 BETWEEN STRINGERS 31 AND 32 R/S WAS REPLACED DUE TO CORROSION.

Part: FITTING — CORRODED (BS 531 S31R) · corrosion level 2 · airframe 51,477 hrs · 58,476 cycles

VERTICAL LEG OF TENSION FITTING AT X531 IS BARE AND PITTED. REPLACED FITTING.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,477 hrs · 58,476 cycles

STRINGER TIE ON STRINGER 29S X424 WAS REPLACED DUE TO CORROSION.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,477 hrs · 58,476 cycles

FRAME LEG BETWEEN STR 31 AND 30 R/S AT X531 REPLACED DUE TO CORROSION.

Part: BRACKET — CORRODED (BS 253) · corrosion level 2 · airframe 51,477 hrs · 58,746 cycles

BRACKET ATTACHING INTERCOSTAL TO AFT FRAME CASTING REMOVED AND REPLACED DUE TO CORROSION.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,477 hrs · 58,476 cycles

STRINGER TIE AT X424 STRINGER 26S WAS REPLACED DUE TO CORROSION.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,477 hrs · 58,476 cycles

DOUBLER ON AFT SIDE OF SPAR BETWEEN STRINGERS 28 AND 30S AT X424 WAS REPLACED DUE TO CORROSION.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,477 hrs · 58,476 cycles

CENTER AISLE AFT SIDE OF FRAME AT X424 INBOARD FWD ANGLE ON RT KEEL BEAM WEB WAS REPLACED DUE TO CORROSION.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,477 hrs · 58,476 cycles

STRINGER 31 R/S BETWEEN 424 AND 434 WAS REPLACED DUE TO CORROSION.

Part: SEAT TRACK — CORRODED (BS 434-510) · corrosion level 2 · airframe 51,477 hrs · 57,476 cycles

RIGHT REAR SEAT RAIL REPLACED DUE TO CORROSION.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,477 hrs · 58,476 cycles

STRINGER TIE ON 27S AT X424 WAS REPLACED DUE TO CORROSION.

Part: STRAP — CORRODED (ZONE 100) · corrosion level 2 · airframe 51,477 hrs · 58,746 cycles

SHORT AFT STRAP LOCATED ON TOP OF INTERCOSTAL WAS REPLACED DUE TO CORROSION.

Part: FRAME — CORRODED (BS 434 S25-32R) · corrosion level 2 · airframe 51,477 hrs · 58,476 cycles

FRAME LEGS BETWEEN STR 32 AND 26 ARE CORRODED AT 434. REPLACED FRAME SEGMENT.

Part: ANGLE — CORRODED (BS 222) · corrosion level 2 · airframe 51,477 hrs · 58,746 cycles

CLEAT ATTACHING INTERCOSTAL TO FWD MAIN DOOR FRAME REMOVED AND REPLACED DUE TO CORROSION.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,477 hrs · 58,476 cycles

STRINGER TIE ON STRINGER 29S AT X424 REPLACED DUE TO CORROSION.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,477 hrs · 58,476 cycles

STRINGER SPLICE AT X488 STRINGER 32S WAS REPLACED DUE TO CORROSION.

Part: STRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,477 hrs · 58,476 cycles

JOINT STRAP AT 424 BETWEEN STRINGERS 28 AND 30 R/S WAS REPLACED DUE TO CORROSION.

Part: SEAT TRACK — CORRODED (BS 312 S23L) · corrosion level 2 · airframe 51,477 hrs · 58,476 cycles

CLEAT REPLACED DUE TO BEING CRACKED AND CORRODED AT X312 STR 23P AT SEAT RAIL ATTACH POINT LT SIDE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,477 hrs · 58,476 cycles

RIGHT FLOOR SUPPORT AT X488 REPLACED DUE TO CORROSION.

Part: FRAME — CORRODED (BS 270) · corrosion level 2 · airframe 51,477 hrs · 58,476 cycles

CABIN UNDER FLOOR FORWARD SIDE OF FRAME LEG CORRODED AT X270 BETWEEN STRINGERS 27 28 R/S. REMOVED AFFECTED CHINE FRAME, INSTALLED CHINE FRAME, (NEW) IAW DRWG 5 85320210 85321385.

Part: ATTACH ANGLE — CORRODED (BS 222) · corrosion level 2 · airframe 51,477 hrs · 58,746 cycles

AT PAX DOOR ANGLE ATTACHING INTERCOSTAL TO FWD FRAME CASTING REPLACED DUE TO CORROSION.

Part: ATTACH FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,477 hrs · 45,876 cycles

CLEAT ATTACHING INTERCOSTAL TO FORWARD MAIN DOOR FRAME ON INBOARD SIDE REMOVED DUE TO CORROSION. FABRICATED AND REPLACED CLEAT.

Part: STRINGER SPLICE — CORRODED (BS 201 S25-28R) · corrosion level 2 · airframe 51,477 hrs · 58,476 cycles

UNDER FLOOR CORROSION ON STRINGER SPLICE AT STRINGER 29 AND X201. REPLACED SPLICE.

Part: INTERCOSTAL — CORRODED (BS 215-523) · corrosion level 2 · airframe 51,477 hrs · 58,476 cycles

PAX DOOR ENTRANCE UNDER FLOOR INTERCOSTALS HAS SEVERAL AREAS WITH CORROSION. REPLACED INTERCOSTALS.

Part: STRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,477 hrs · 58,476 cycles

INTERNAL JOINT STRAP AT X424 FROM STR 29 TO 29 REPLACED DUE TO CORROSION.

Part: INTERCOSTAL — CORRODED (BS 204 S23L) · corrosion level 2 · airframe 51,477 hrs · 58,476 cycles

AT PAX THRESHOLD FIRST STRINGER INTERCOSTAL INBOARD OF DOOR OPENING WAS REPLACED DUE TO CORROSION ON FORWARD END.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,477 hrs · 58,476 cycles

STRINGER TIE AT 424 STRINGER 24S WAS REPLACED DUE TO CORROSION.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,477 hrs · 58,476 cycles

STRINGER 31 IS CORRODED JUST AFT OF TENSION FITTING BETWEEN X424 AND X436 R/S. REPLACED STRINGER.

Part: STRINGER SPLICE — CORRODED (BS 488 S26R) · corrosion level 2 · airframe 51,477 hrs · 58,746 cycles

STRINGER SPLICE ON STR 26S AT X445 WAS REPLACED DUE TO CORROSION.

Part: ANGLE — CORRODED (BS 354 S23L) · corrosion level 2 · airframe 51,477 hrs · 58,476 cycles

CLEAT REPLACED DUE TO CORROSION AND CRACKING AT X354 STRINGER 23P.

Part: FRAME — CORRODED (BS 436 S30-31R) · corrosion level 2 · airframe 51,477 hrs · 58,476 cycles

CABIN UNDER FLOOR FRAME LEG IS CORRODED AT X436 BETWEEN STRINGERS 30 AND 31. REMOVED AND REPLACED RIGHT HAND BOTTOM FRAME SEGMENT AT STA X434 IAW DEHAVILLAND DRAWINGS 85330057 AND 85330012.

Part: THRESHOLD — CORRODED (BS 240 S23L) · corrosion level 2 · airframe 51,477 hrs · 58,476 cycles

PAX DOOR THRESHOLD FRAME REPLACED DUE TO CORROSION.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,477 hrs · 58,476 cycles

STRINGER TIE ON STRINGER 28S AT X424 WAS REPLACED DUE TO CORROSION.

Part: ANGLE — CORRODED (BS 467) · corrosion level 2 · airframe 51,477 hrs · 58,746 cycles

REINFORCING ANGLE AT 467 ON LOWER RIGHT HAND FRAME SEGMENT IS CORRODED. REPLACED ANGLE.

Part: SKIN PANEL — CORRODED (BS 190-201) · corrosion level 2 · airframe 51,477 hrs · 58,476 cycles

LOWER SILL ON LAV SERVICE AREA CORRODED. REPAIRED IN ACCORDANCE WITH ENGINEERING ORDER EO8-53-06-0420.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 51,477 hrs · 58,476 cycles

CABIN UNDER FLOOR CORROSION ON FRAME LEG BETWEEN STR 30 AND 31 AT X370 R/S. CLEANED AREA & FOUND MINOR CORROSION AROUND RIVET FASTENER REPAIRED IAW SRM 51-20-11, ALODINED & PRIMED IAW SRM 51-20-16 & 51-20-36.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,477 hrs · 58,476 cycles

STRINGER SPLICE ON STRINGER 30 AT X488 R/S WAS REPLACED DUE TO CORROSION.

Part: SKIN PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,477 hrs · 58,476 cycles

SEVERAL AREAS OF CORROSION ON SKIN PANEL BETWEEN X434 TO X488 REPLACED PANEL.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,477 hrs · 58,476 cycles

FRAME AT X510 BETWEEN STRINGER 31S AND 31P HAS BEEN REPLACED DUE TO CORROSION.

Part: FLOOR SUPPORT — CORRODED (BS 467) · corrosion level 2 · airframe 51,477 hrs · 58,476 cycles

BOTTOM OF RIGHT FLOOR SUPPORT AT STATION 467 IS CORRODED. REPLACED FLOOR SUPPORT.

Part: STRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,477 hrs · 58,476 cycles

INTERNAL LONGITUDINAL STRAP RT SIDE AT X424 BETWEEN STRINGERS 27 AND 28 WAS REPLACED DUE TO CORROSION.

Part: FRAME — CORRODED (BS 436 S31-32R) · corrosion level 2 · airframe 51,477 hrs · 58,476 cycles

CENTER AISLE UNDER FLOOR FRAME LEG CORRODED BETWEEN STRINGERS 31 AND 32 AT FRAME 436. REMOVED AND REPLACED RIGHT HAND BOTTOM FRAME SEGMENT.

Part: PLATE — CORRODED (BS 467) · corrosion level 2 · airframe 51,477 hrs · 58,746 cycles

REINFORCING PLATE AT 467 WAS REPLACED DUE TO CORROSION.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,477 hrs · 58,476 cycles

REINFORCING DOUBLER FOR MARKER ANTENNA BETWEEN X467 AND X488 WAS REPLACED DUE TO CORROSION.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,477 hrs · 58,476 cycles

INTERCOSTAL BETWEEN 424 AND 434 WAS REPLACED DUE TO CORROSION.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,477 hrs · 58,476 cycles

STRINGER SPLICE AT X488 STRINGER 29S WAS REPLACED DUE TO CORROSION.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 51,476 hrs · 58,475 cycles

LEFT CENTER SEAT RAIL HAS SPOTS OF CORROSION WHERE SEATS ATTACH. REPLACED SEAT RAIL

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 51,476 hrs · 58,475 cycles

RIGHT FORWARD SEAT RAIL HAS SPOTS OF CORROSION WHERE SEATS ATTACH. REPLACED SEAT RAIL.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 51,476 hrs · 58,475 cycles

LEFT AFT SEAT RAIL HAS SPOTS OF CORROSION WHERE SEATS ATTACH. REPLACED SEAT RAIL.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,476 hrs · 58,475 cycles

RT REAR SEAT RAIL HAS SPOTS OF CORROSION AT SEAT ATTACH AREAS. REMOVED AND REPLACED SEAT RAIL.

Part: FRAME — CORRODED (BS 436 S30-31R) · corrosion level 2 · airframe 51,476 hrs · 58,475 cycles

FRAME LEG IS CORRODED AT X436 BETWEEN STRINGERS 30 AND 31S. REPLACED FRAME SEGMENT.

Part: WARNING SYSTEM — MALFUNCTIONED (NLG) · airframe 32,515 hrs · 35,387 cycles

UPON GEAR RETRACTION NOSE GEAR RED UNSAFE LIGHT AND GEAR HANDLE LIGHT REMAINED ILLUMINATED. CYCLED GEAR UP AND DOWN, INDICATIONS WERE NORMAL. INSPECTED NOSE GEAR, NO DEFECTS NOTED. ISSUED INFORMATIONAL DISCREPANCY. HNAA INFO AS PER MP+P LOGIC DIAGRAM STEP 4.

Part: PROXIMITY SENSOR — BROKEN (LT MLG) · airframe 51,257 hrs · 58,240 cycles

AFTER GEAR RETRACTION LT MAIN GEAR DOOR AMBER LIGHT REMAINED ILLUMINATED. VISUALLY CONFIRMED DOOR CLOSED. REMOVED AND REPLACED THE LT GEAR FORWARD DOOR PROXIMITY SENSOR.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 45,719 hrs · 52,190 cycles

FOUND LEFT EXIT EGRESS LIGHT (2), AFT CABIN OVERHEAD, PAX OVERHEAD EXIT SIGN IS INOP WHILE ATTEMPTING TO PERFORM SCHEDULED MX. W/C 33-50-03Q CLT MX FOUND SEVERAL EMERGENCY LIGHTS NOT WORKING, HAD TO CHANGE TWO BATTERIES.

Part: WARNING SYSTEM — INTERMITTENT (FIRE WARNING) · airframe 45,298 hrs · 51,723 cycles

SMOKE WARNING AND FIRE DETECT WARNING LIGHT ILLUMINATED ON SHORT FINAL. REMOVED AND REPLACED MASTER WARNING CONTROL BOX AND MASTER WARNING PANEL.

Part: STRINGER — CORRODED (FUSLEAGE) · airframe 45,222 hrs · 51,644 cycles

DURING C-CHECK, FOUND CORROSION ON STR 31S THAT REQUIRED REMOVAL AND REPLACEMENT OF STR. FRAME SEGMENT AT X291 REMOVED TO FACILITATE INSTALLATION OF REPLACEMENT STR SECTION. IAW EO8-53-03-1062

Part: STRINGER — CORRODED (FUSELAGE) · airframe 45,222 hrs · 51,644 cycles

DURING C CHECK, FOUND CORROSION ON STR31 SEVERE ENOUGH TO WARRANT REMOVAL AND REPLACEMENT FROM X 182 TO F/SPAR X387. IAW EO8-53-0-30-1055

Part: STRINGER — CORRODED (FUSELAGE) · airframe 45,222 hrs · 51,644 cycles

CORROSION ON STR SPLICE AT STR 32S AND FRAME X351.

Part: SKIN PANEL — BUCKLED (FUSELAGE) · airframe 45,222 hrs · 51,644 cycles

A/C SUFFERED HARD LANDING RESULTING NUMEROUS AREAS OF BUCKLED FUSELAGE SKIN ON LHS. REPAIR IS TO HEAVY WINDOW BETWEEN THE F/SPAR AND R/SPAR.

Part: SKIN PANEL — BUCKLED (FUSELAGE) · airframe 45,222 hrs · 51,644 cycles

A/C SUFFERED HARD LANDING RESULTING NUMEROUS AREAS OF BUCKLED FUSELAGE SKIN ON LHS. REPAIR IS TO HEAVY WINDOW BETWEEN THE F/SPAR AND R/SPAR.

Part: SKIN PANEL — DENTED (FUSELAGE) · airframe 44,952 hrs · 51,367 cycles

MAJOR REPAIR DENTS ON THE SIDE OF THE FUSELAGE.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 42,293 hrs · 48,612 cycles

CREW REPORTED THAT THE FIRST TWO RED FLOOR EMERGENCY ESCAPE PATH LIGHTS AT FWD EXIT AND ALL FOUR RED LIGHTS AT ROW 4 EXIT WERE INOPERATIVE. PERFORMED OPERATIONAL CHECK OF EMERGENCY LIGHTS SYSTEM. COULD NOT DUPLICATE THE DISCREPANCY

Part: CIRCUIT BREAKER — TRIPPED (COCKPIT) · airframe 41,879 hrs · 48,159 cycles

BOTH STANDBY HYDRAULIC PUMP CIRCUIT BREAKERS TRIPPED AND NORMAL BRAKES FAILED WHEN NR 1 ENGINE WAS SHUTDOWN DURING TAXI. MAINTENANCE RESET CIRCUIT BREAKERS AND PERFORMED ASSOCIATED OP CHECKS AND COULD NOT DUPLICATE PROBLEM.

Part: PUMP — LEAKING (NR 2 ENGINE) · airframe 40,242 hrs · 46,407 cycles

ON TAKEOFF ROLL, TORQUE ON NR 2 ENGINE WENT TO 122 PERCENT. RETURNED TO GATE. FOUND LARGE AMOUNT OF FLUID LEAKING FROM NR 2 ENGINE AND PROP AREA. NO CAUTION LIGHT OR WARNING LIGHTS. REMOVED AND REPLACED PCU PUMP.

Part: ANGLE — CRACKED (LT WING) · airframe 39,887 hrs · 46,021 cycles

CRACK IN CLOSING ANGLE BETWEEN OUTBOARD SIDE OF NR 1 NACELLE AND WING FRONT SPAR. REPAIRED IAW EO8-57-01-509.

Part: HANDLE — MALFUNCTIONED (MLG CONTROL) · airframe 37,541 hrs · 43,517 cycles

UPON APPROACH, WHEN GEAR SELECTED DOOWN, ONLY 3 RED LIGHTS AND GEAR DID NOT OPERATE. AFTER MISSED APPROACH, SELECTED LEVER UP AND SELECTED GEAR DOWN, OPERATED OK.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 36,856 hrs · 42,785 cycles

RIGHT REAR EMERGENCY EXIT EXTERNAL EMERGENCY LIGHT WAS FOUND TO BE INOP. FOUND BATTERY PACK 3351-PS4 DISCHARGED. REPLACED BATTERY PACK.

Part: REGULATOR — STRIPPED (NR 1 ENGINE) · airframe 36,368 hrs · 42,252 cycles

CREW RECEIVED NR 1 ENGINE OIL PRESSURE CAUTION LIGHT AND THE OIL PRESSURE WENT TO ZERO. CREW SHUT DOWN NR 1 ENGINE. FOUND OIL LEAK AT OIL PRESSURE REGULATOR DUE TO STRIPPED THREADS IN A FITTING BOSS. REPLACED OIL PRESSURE REGULATOR AND PERFORMED MAINTENANCE MANUAL PROCEDURE 05-00-00 FOR LOSS OF OIL PRESSURE.

Part: BULB — FAILED (CABIN) · airframe 35,667 hrs · 41,523 cycles

EMERGENCY FLOOR LIGHT NR 20 WAS FOUND TO BE INOP. REPLACED BULB.

Part: SKIN — DENTED (SPOILER)

DENT ON INBOARD GROUND SPOILER UPPER SKIN AT INBOARD END. EXCEEDS MAX, CHORDWISE DIMENSION A OF RD8-27-014. COMPLIED WITH EO 8-53-99-240. MARKED DENT WITH YELLOW DOT.

Part: SKIN — DENTED (SPOILER)

DENT ON OUTBOARD ROLL SPOILER INBOARD OF CENTER HINGE. EDGE DISTANCE TO FWD FASTENER .625 OUT OF LIMITS OF RTD8-27-014. DENT IS ON UPPER SKIN. COMPLIED WITH EO 8-53-99-240. MARKED DENT WITH YELLOW DOT.

Part: FRAME — CORRODED (BS 510)

FRAME AT STATION X510 HAS CORROSION AND IS SPLIT WHERE IT MEETS THE SKIN. DAMAGES ARE JUST O/B OF STRINGER 31S. MANUFACTURED REPAIR ANGLE IAW SRM 53-20-21, ALODINED AND PRIMED ANGLE. REMOVED AND REPLACED FRAME LEG.

Part: FASTENERS — CORRODED (HORIZ STAB)

HORIZONTAL STAB ON UNDERSIDE, 4 HI-LOKS CORRODED AT CENTER BOX, CENTER DOUBLER AFT ROW (MARKED). REMOVED AND REPLACED HI-LOKS.

Part: FRAME — CORRODED (BS 510)

FRAME AT STATION X510 HAS CORROSION AND IS SPLIT WHERE IT MEETS THE SKIN. DAMAGE IS JUST O/B OF STRINGER 31S. MANUF REPAIR ANGLE IAW SRM 53-20-21. ALODINED AND PRIMED ANGLE, INSTALLED ANGLE AS REQUIRED.

Part: LINK — CRACKED (BS 545)

LINK SUPPORTING RT CHANNEL AND LWR CHANNEL TOGETHER AT STA X545.0 IS CRACKED. REMOVED AND REPLACED LINK.

Part: STRINGER — CORRODED (BS 504)

STRINGER 25S HAS CORROSION AND PITTING AT X504, REMOVAL OF THE RIVET REQUIRED. REMOVED RIVET AT LOCATION, EVALUATED AND BLENDED CORROSION FOUND AREA OUT OF LIMITS APPROX .013. BLENDED AND REMOVED ALL CORROSION, INSTALLED NESTED ANGLE AS SAME TYPE AS STRINGER TO EXTEND 4 FASTENERS EITHER SIDE OF THE DAMAGE AREA. ALODINED, PRIMED AND PAINTED AREA.

Part: SILL PLATE — CORRODED (PASSENGER DOOR)

LOWER PAX DOOR SILL PLATE HAS AREAS OF CORROSION. ALSO ADJOINING STRUCTURE HAS CORROSION ON LOWER SIDE AT TWO RIVETS AND NUT PLATES. UPPER PLATE NEEDS REMOVED FOR FURTHER EVAL. REMOVED UPPER PLATE THRESHOLD FOR EVAL, REMOVED CORROSION ON LOWER SIDE AT RIVET AND NUT PLATES AND LOWER SILL PLATE. TREATED AND PRIMED SURFACES. INSTALLED NEW SILL PLATE AND SHIMMED AS REQUIRED.

Part: STRINGER — CORRODED (BS 520 & 517)

STRINGER 31S HAS PITS AT TWO RIVETS, LOCATED AT APPROX X520 & X517. RIVETS NEED REMOVED FOR FURTHER EVALUATION. REMOVED FIVE RIVETS AT STRINGER 31S APPROX X520 & X517. FOUND AREA EXCESSIVELY PITTED. REMOVED AND REPLACED SECTION OF STRINGER AND TENSION FITTING.

Part: STRINGER — CORRODED (BS 517-520)

STRINGER 31S HAS PITTS AT TWO RIVETS, LOCATED AT APROX X520 AND X512. RIVETS NEED REMOVED FOR FURTHER EVALUATION. REMOVED FIVE RIVETS AT STRINGER 31S APROX X520 AND X517. FOUND AREA EXCESSIVELY PITTED. TWO AREAS OUT OF LIMITS APROX .015 AND ONE AREA IN RADIUS APROX .020. REMOVED AND REPLACED STRINGER.

Part: SKIN — WRINKLED (BS 771.803)

SEVERAL WRINKLES ON BOTTOM FUSELAGE SKIN AT FS 771.803, JUST FORWARD OF TAIL BUMPER BETWEEN STRINGER 31P AND 31S. PER ENGINEERING DISPOSITION, NO FURTHER ACTION REQUIRED, APPLIED YELLOW DOT TO AREA.

Part: STRINGER — CORRODED (BS 500)

CORROSION IN BELLY AT STRINGER 30P AT STATION 500 (WILL NEED SPLICE). REMOVED AND REPLACED STRINGER SPLICE.

Part: SKIN — DENTED (BS 190)

DENT AT STRINGER 23S AT X190 TOTAL DENT IS APPROX 1.5 DIA .025. DEEP PERFORMED HFEC, NO CRACKS DETECTED. DISPOSITION YELLOW DOT.

Part: SEAT TRACK — CORRODED (BS 202 & 207)

RT CENTER SEAT RAIL HAS SEVERE PITTING CORROSION ON I/B WHICH HAS COMPLETELY CORRODED THROUGH THE METAL - OUT OF LIMITS. REMOVED AND REPLACED RAIL SECTION AND SPLICE.

Part: SEAT TRACK — CORRODED (BS 134)

RT CENTER SEAT RAIL AT FS 134 HAS DRILL HOLE DAMAGE. A DRILL HOLE MEASURING .100 DEEP ON TOP FLANGE (APPROX) REMAINING MATERIAL THICKNESS .042- OUT OF LIMITS. REMOVED AND REPLACED SEAT RAIL AND SPLICE.

Part: SEAT TRACK — CORRODED (BS 130)

RT CENTER SEAT RAIL AT FS 130.0 (APPROX) HAS PITTING CORROSION ON TOP FLANGE APPROX .015 DEEP. .010 ALLOWABLE - OUT OF LIMITS. REMOVED AND REPLACED RAIL AND SPLICE.

Part: STRINGER — CRACKED (NR 2 NACELLE)

NR 2 NAC INBOARD STRINGER BELOW THE DECK IS CRACKED JUST PRIOR TO PREVIOUS REPAIR. REMOVED AND REPLACED STRINGER.

Part: STIFFENER — CRACKED (NR 2 NACELLE)

NR 2 NAC AFT STIFFENER IS CRACKED. REMOVED AND REPLACED STIFFENER.

Part: STRINGER — CRACKED (NR 2 NACELLE)

NR 2 NAC OUTBOARD STRINGER IS CRACKED IN TWO PLACES AT THE REPAIR. REMOVED AND REPLACED STRINGER.

Part: ANGLE — CRACKED (CENTER WING)

AFT LEFT CLOSING ANGLE IS CRACKED. REMOVED AND REPLACED CLOSING ANGLE.

Part: STRINGER — CRACKED (NR 1 NACELLE)

NR 1 NAC AFT STRINGER IS CRACKED. REMOVED AND REPLACED AFT STRINGER.

Part: HANDLE — BINDING (AIRSTAIR DOOR)

UNABLE TO OPEN AIRSTAIR DOOR FROM OUTSIDE. HANDLE BINDING, REPLACED HANDLE STOP.

Part: BRACKET — CRACKED (NR 2 NACELLE)

PRESSURE MANIFOLD BRACKET IN NR 2 NACELLE CRACKED IN LOWER FORWARD CORNER. REPAIRED IN ACCORDANCE WITH STRUCTURAL REPAIR MANUAL.

Part: CABLE — LOOSE (PAX DOOR)

BWI - FLT 3249 - PAX DOOR WILL NOT OPEN. REMOVED AND REPLACED AIRSTAIR DOOR OUTER CABLE ASSY. (M)

Part: BATTERY — DISCHARGED (CABIN)

DCA/ORF - FLT 3105 - DURING PRE-FLIGHT CHECKS, FOUND SEVERAL RED FLOOR ESCAPE PATH LIGHTS INOPERABLE. REMOVED AND REPLACED 3352-PS2 EMERGENCY BATTERY. (X)

Part: SELECTOR VALVE — FAILED (COCKPIT)

FLT 3200 - DCA-BWI - THE LANDING GEAR WOULD NOT EXTEND WITH LANDING GEAR SELECTED DOWN. PERFORMED ALTERNATE GEAR EXTENSION. THE AIRCRAFT LANDED WITHOUT INCIDENT. SECURED LOOSE CONNECTOR AT LANDING GEAR INHIBIT SWITCH. LATER IN THE DAY, LANDING GEAR WOULD NOT EXTEND UPON SELECTION. REMOVED AND REPLACED THE LANDING GEAR CONTROL VALVE AND LANDING GEAR SELECTOR HANDLE. REFERENCE HNAA9791415.

Part: CONTROL VALVE — FAILED (RT MLG WW)

FLT 3200 - DCA-BWI - THE LANDING GEAR WOULD NOT EXTEND WITH LANDING GEAR SELECTED DOWN. PERFORMED ALTERNATE GEAR EXTENSION. THE AIRCRAFT LANDED WITHOUT INCIDENT. SECURED LOOSE CONNECTOR AT LANDING GEAR INHIBIT SWITCH. LATER IN THE DAY, LANDING GEAR WOULD NOT EXTEND UPON SELECTION. REMOVED AND REPLACED THE LANDING GEAR CONTROL VALVE AND LANDING GEAR SELECTOR HANDLE. (M)

Part: ENGINE — FAILED (NR 1)

FLT 3088 - MIA-TPA - DURING CLIMB-OUT, NR 1 ENGINE TORQUE, FUEL FLOW, AND OIL PRESSURE INDICATION WAS ZERO. SHUT DOWN THE ENGINE IAW EMERGENCY SHUTDOWN CHECK LIST. THE AIRCRAFT TURNED BACK TO MIA AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED THE NR 1 ENGINE. (M)

Part: SENSOR TARGET — DETACHED (NLG)

MIA/EYW - FLT 3042 - AFTER TAKEOFF, THE NOSE GEAR DOOR AMBER LIGHT REMAINS ON AFTER GEAR RETRACTION. THE CREW CYCLED THE GEAR, LIGHT REMAINED ILLUMINATED. THE AIRCRAFT RETURNED TO MIA AND LANDED WITHOUT INCIDENT. THE NOSE GEAR DOOR POSITION SENSOR TARGET WAS FOUND DETACHED. REINSTALLED SAME. OPS CHECK GOOD. (X)